diff --git "a/data.ndjson" "b/data.ndjson"
--- "a/data.ndjson"
+++ "b/data.ndjson"
@@ -1,46016 +1,1191 @@
-[8.67848014831543, 4.728089332580566, "[TT] Primary Sensor of the Star tracker = Star tracker"]
-[11.503263473510742, 6.527320384979248, "[TT] Maximum Detectable Rigidity of the STD = Above 1 TeV for protons"]
-[10.431527137756348, 4.064397811889648, "[TT] Boom Length of the RIME = 16-m"]
-[6.46746301651001, 7.60965633392334, "[TT] Data Quantization of the POLDER-2 = 12 bit"]
-[12.442220687866211, 3.2052128314971924, "[TT] On-Board Propellant of the FormoSat-2 = 27 kg"]
-[5.0582194328308105, 7.134823799133301, "[TT] Command Uplink Data Rate of the NEMO-HD = 4 kbit/s"]
-[12.099466323852539, 6.327785015106201, "[TT] Total Number of Positrons Identified of the AMS = Excess of 400,000"]
-[4.9823431968688965, 0.8115627765655518, "[FF] Ready for Commercial Service Date of the European Aviation Network (EAN) = 11 Sept. 2017"]
-[9.425777435302734, 0.977189302444458, "[TT] Relative Velocity at Closest Approach of the Juno = 41,600 mph (67,000 km/h)"]
-[8.340781211853027, 1.2856478691101074, "[TT] Range of Values of the Precipitation over land ares = 0 - 25"]
-[6.3107452392578125, -1.3130079507827759, "[TT] Year of Launch of the GRACE = 2002"]
-[13.21137809753418, 5.418277740478516, "[FF] Solar Arrays of the NuSTAR = Deployed"]
-[5.480652332305908, 1.1829619407653809, "[FF] Testing Date of the BepiColombo Antenna Pointing Mechanism = 23\u201325 September 2015"]
-[3.1429283618927, 2.24657940864563, "[FF] Themes of the Copernicus = Sealed soil (imperviousness), tree cover density, forest type, and grasslands"]
-[8.032636642456055, 9.033866882324219, "[TT] Wavefront Planarity of the LRI = < \u03bb/8"]
-[5.393825054168701, 1.0520354509353638, "[FF] Release Date of the DIWATA-1 = Spring"]
-[5.70180082321167, 4.9135050773620605, "[TT] Function of the MEXIC = Make in-flight modifications to analyzer software"]
-[6.211206912994385, 5.6208600997924805, "[TT] CCD Synchronization of the FPGA = Yes"]
-[6.891186714172363, 5.19998025894165, "[FF] Power Distribution Modules of the Avionics System = On individual module cards"]
-[8.848240852355957, 9.513762474060059, "[FF] Band 4 Spectral Range of the TANSO-FTS-2 = 5.56 - 8.45 \u00b5m"]
-[8.89806842803955, 5.091498851776123, "[FF] Experiment Pointing System of the ATLAS-1 = Orbiter"]
-[4.605031490325928, 0.8402915596961975, "[TT] Planned Launch Year of the ESP-MACCS = 2024"]
-[6.143570899963379, 4.694345474243164, "[FF] Data Processing Center Lead of the INCUS = Phil Partain"]
-[7.972888469696045, 8.912105560302734, "[TT] Scattered Emission Wavelength of the CuPID = 121.6 nm"]
-[10.003402709960938, 3.0255985260009766, "[FF] Conference Presentation Date of the Dynamic Ionosphere CubeSat Experiment = April 21-23, 2010"]
-[7.823037624359131, 8.455904006958008, "[TT] Bands of the ABI = 2 visual spectrum bands, and 14 infrared bands"]
-[13.976900100708008, 7.1560797691345215, "[TT] Current of the Voltage 1 = 1000"]
-[6.7176055908203125, 6.776340484619141, "[TT] Performance Tuning of the Laser Communication Terminal = Ongoing"]
-[7.194535255432129, 2.790736436843872, "[TT] Launch Date of the MethaneSAT = Late 2022"]
-[6.873552322387695, 1.2742162942886353, "[FF] Observation Period of the Dynamics of the Radiative Environment = 11/2000-11/2001"]
-[5.201341152191162, 3.263371467590332, "[TT] Operator of the Beijing-3 = Twenty First Century Aerospace Technology Co., Ltd (21AT)"]
-[3.9816291332244873, 2.0494203567504883, "[TT] Launch Vehicle of the CHAMP = Kosmos-3M"]
-[11.572168350219727, 6.713700294494629, "[TT] Energy Range of the eROSITA = 0.5-2 keV"]
-[11.144328117370605, 5.66513729095459, "[FF] Thickness of the Laminate Material = Unknown"]
-[7.786859035491943, 1.107759714126587, "[FF] Liquid Core Diameter of the Mars = Half the diameter of the planet"]
-[8.090400695800781, 8.630695343017578, "[TT] Spectral Sampling Distance of the SWIR Spectrometer = 10 nm on average"]
-[7.418503761291504, 0.855119526386261, "[FF] Development Initiative of the LunaSAR = LunaNet"]
-[4.851296424865723, -1.9198559522628784, "[TT] Sample Collection Amount of the Chang'e-5 Lander = 0.5 kg from drilling and 1.5 kg scooped from the surface"]
-[9.036482810974121, 7.618422508239746, "[TT] SWIR Band Resolution of the Imager = 1 km"]
-[7.129238128662109, -0.19984520971775055, "[TT] Orbit Decay Rate of the GOCE = Less than 35 cm per day"]
-[8.490241050720215, 7.9837212562561035, "[TT] Pixel Pitch of the MS Bands = 52 \u00b5m"]
-[3.5473039150238037, 1.8357036113739014, "[FF] URL of the Sentinel Data Hub = https://senthub.esa.int/"]
-[7.089619159698486, 5.3249311447143555, "[FF] Modes of the Instrument = Four"]
-[4.993947982788086, -0.31996235251426697, "[TT] Launch Time (CEST) of the ESAIL = 03:51"]
-[7.001959800720215, 7.07307767868042, "[TT] Efficiency (Wall Plug) of the Laser = > 15%"]
-[8.181385040283203, 3.5247437953948975, "[TT] Instrument Type of the OCO-3 = Atmospheric chemistry"]
-[6.0213494300842285, 7.142528057098389, "[TT] Data Rate of the Instrument = 14.2 kbit/s"]
-[3.974320888519287, 6.716139316558838, "[TT] Antenna Type of the DCS platform = Electronically despun S-band antenna"]
-[5.0141448974609375, 3.216773748397827, "[FF] Manufacturer of the STPSat-3 = Ball Aerospace"]
-[8.182867050170898, 4.286091327667236, "[FF] Effect of Gravity of the Light = Energy loss, lower frequency, longer wavelengths"]
-[12.796305656433105, 2.0482518672943115, "[TT] IFOV of the SAGE-III = 1-2 km"]
-[4.196446418762207, 0.27448034286499023, "[FF] Meeting Date of the FalconSAT-3 = Oct. 12-16, 2009"]
-[5.3473429679870605, 3.003636121749878, "[TT] Development Responsibility of the \u00b5RTU = SRL"]
-[10.011014938354492, 4.493043899536133, "[FF] Actuation of the ACS = Three magnetic-torquer coils and four reaction wheels"]
-[4.817043781280518, 2.9530346393585205, "[TT] Control Center of the Colony I = SOC (Satellite Operations Center) at BPTF (Blossom Point Test Facility), located near LaPlata, MD"]
-[9.472317695617676, 4.889261722564697, "[TT] Shutdown Cause of the RTU = Loss of onboard power regulation and spacecraft attitude stabilization"]
-[7.022117614746094, 2.5318102836608887, "[FF] Visibility of the Malindi, Kenya = Once per 90 minute orbit"]
-[8.215028762817383, 7.929912090301514, "[TT] Number of Detector Elements of the SWIR channel detector = 4"]
-[5.057897567749023, 0.4596283733844757, "[TT] Launch Date of the LitianicaSAT-2 = June 23, 2017"]
-[5.455872535705566, 5.086832523345947, "[TT] Communication Protocol of the CIB = CAN bus"]
-[6.409571170806885, -0.4981379806995392, "[TT] Repeat Cycle of the TARANIS = 38 days"]
-[8.76630687713623, -0.13466493785381317, "[TT] Apogee of the Chang'e-2 = About 380,000 km"]
-[5.601052284240723, 4.043531894683838, "[TT] Equipment Selection of the AstroBus-L = Minimum Class 2 EEE parts, with compatibility to Class 1 in most cases"]
-[1.9358123540878296, -0.4022294580936432, "[FF] Detection of the Van Allen Probes = Increased number of even higher energy electrons"]
-[9.077587127685547, 8.154634475708008, "[TT] Distortion of the WPM = < 3.0%"]
-[5.162554740905762, 4.453121185302734, "[TT] Number of GPS Satellites of the T3000G2 receiver = 8"]
-[10.939406394958496, 6.941377639770508, "[TT] ?V Capability of the ISEE-3 = About 310 m/s"]
-[4.2932939529418945, 7.2737717628479, "[TT] Downlink Frequency of the RF Communications = X-band"]
-[4.949280738830566, 4.975515842437744, "[TT] Protein of the CASIS PCG-16 = LRRK2 (Leucine-Rich Repeat Kinase 2)"]
-[5.939933776855469, 2.373373031616211, "[FF] Members of the SET Project Scientist Team = Michael Xapsos, Yihua Zheng"]
-[14.377970695495605, 3.2573626041412354, "[TT] LI Mass of the LI = 93 kg"]
-[7.270762920379639, 2.0248355865478516, "[FF] Payloads of the Carbonite Series = Visible, MWIR, and X-band radar wavelengths"]
-[9.828889846801758, 8.150108337402344, "[TT] Lens Focal Length of the ISIR = 50.8 mm"]
-[4.677590847015381, 1.545117974281311, "[FF] Launch Date of the GHGSat Constellation = Early 2023"]
-[9.475085258483887, 5.840674877166748, "[TT] Viewing Angle Range of the Moon = -115\u00ba to +115\u00ba"]
-[7.671741008758545, 5.580629348754883, "[FF] Components of the Lateral Sensor = Camera, telecentric lens, fiber-coupled laser-diode bar, corner cube"]
-[8.198368072509766, 3.3130950927734375, "[FF] Required Climate Record of the Infrared Spectrometer = 22 years with CLARREO accuracy for a 95% confidence level of 0.1 K/decade"]
-[8.75571060180664, 7.1194000244140625, "[TT] PAN-A of the CartoSat-1 = Panchromatic Aft-pointing Camera"]
-[4.392117023468018, 5.43360710144043, "[TT] Orbit Lifetime of the GOMX-3 = Well over 1 year"]
-[6.7428507804870605, 0.8148444294929504, "[TT] First Perihelion of the Solar Orbiter = 15 June"]
-[5.222650051116943, 2.809779167175293, "[FF] Avionics of the STRaND-1 = Smartphone"]
-[9.754098892211914, -0.46776971220970154, "[TT] Orbit Altitude of the Satellite Constellation = 1100 and 1300 km"]
-[6.020961284637451, -0.37793922424316406, "[TT] Continuous Operation of the Fission Surface Power System = At least 10 years"]
-[10.053159713745117, -1.3338531255722046, "[TT] Inclination of the NigeriaSat-2 = 98.24\u00ba"]
-[9.971481323242188, -0.5410200357437134, "[TT] Orbit Altitude of the DubaiSat-2 = 600 km"]
-[7.179135322570801, 6.987429618835449, "[TT] Chirped Pulse Duration of the Feeder SSPA = 20 \u00b5s"]
-[10.691187858581543, 2.1508970260620117, "[TT] Distance of X-ray jet from the Manatee\u2019s head of the XMM-Newton = Approximately 300 light years"]
-[8.20783519744873, 8.26307487487793, "[TT] Wavelengths of the Mid-IR Imagers = 7 and 12.3 \u00b5m"]
-[7.786376476287842, 7.6370110511779785, "[FF] Image Color of the DMS = White, gray, black or navy"]
-[3.5091464519500732, 6.408969879150391, "[TT] Antenna Array Size of the PR = 2 m x 2 m"]
-[8.23325252532959, 3.1343178749084473, "[FF] Data Source of the OMI (Ozone Monitoring Instrument) = OMI (Ozone Monitoring Instrument) on NASA\u2019s Aura satellite"]
-[5.899250030517578, 5.612621784210205, "[TT] Radiation Hardened of the Proton P400K-SGMII-2-PCI104S-SD Space Computer = Yes"]
-[8.119954109191895, 0.17425517737865448, "[TT] In-Orbit Demonstration Date of the ELSA-M = Late 2024"]
-[10.256050109863281, 7.984253406524658, "[TT] Elevation/Azimuth Coud\u00e9-mount Telescope Size of the OCTL = 1 m"]
-[7.689482688903809, -2.5409278869628906, "[TT] Cadence of the GOLD = 30 min"]
-[11.94345474243164, 5.028698921203613, "[TT] Volume of the XRD = ~15.3 x 71 x 66 cm3"]
-[5.461434841156006, -1.7491893768310547, "[TT] End of Life Date of the KOMPSAT-2 = 31 Dec 2021"]
-[7.395208358764648, 2.319082021713257, "[FF] Senegal Population Coverage of the Astrocast = Almost 5%"]
-[5.303203105926514, 1.274025797843933, "[TT] Conference Location of the Peter Wegner = El Segundo, CA, USA"]
-[4.5399298667907715, 5.827768802642822, "[TT] Individuals Rescued of the 406 MHz beacons = More than 22,400"]
-[13.83770751953125, 5.6705169677734375, "[TT] Cell Efficiency of the Solar Panels = 28%"]
-[10.121330261230469, 5.844119548797607, "[TT] Cooling Temperature of the HgCdTe photoconductive detector = 108 K"]
-[5.807316780090332, 6.305907249450684, "[TT] Capacity of the SSR = 64 Gbit"]
-[9.42353343963623, 6.4442973136901855, "[TT] Azimuth Range of the Ambiguity = 23~14(mean:20)"]
-[9.307266235351562, 8.621654510498047, "[TT] Separation Distance of the Slits = 4.5 mm"]
-[7.608696460723877, -0.10271874815225601, "[TT] Final Stop of the Philae = A few meters away from the bounce"]
-[9.35970687866211, 4.810286045074463, "[FF] Presentation Date of the Attitude Control Module = August 13-16, 2012"]
-[6.818337440490723, 4.193209171295166, "[FF] Development Date of the HSC-III = Unknown"]
-[5.507639408111572, 0.5846865773200989, "[TT] Discovery Date of the NuSTAR = Feb. 28, 2017"]
-[4.06898307800293, 4.337492942810059, "[FF] Ground Segment of the RADARSAT-2 = Upgraded from the RADARSAT-1 infrastructure"]
-[14.109410285949707, 3.1213159561157227, "[TT] Client Mass of the ELSA-d = ~17 kg"]
-[8.515993118286133, 1.8150376081466675, "[TT] Range of Water Vapor Measurement of the TMR = 0.2 to 6.0 gm/cm2"]
-[5.001271724700928, 6.8620219230651855, "[TT] Number of TMTC Interfaces of the Heinrich Hertz = 1150"]
-[9.877522468566895, 4.4419474601745605, "[TT] Vector Components Random Error of the Ion Drift Velocity = < 200 m/s"]
-[6.278446674346924, -1.1387860774993896, "[TT] Operational Science Phase Duration of the GRACE-FO = 5 years"]
-[9.495335578918457, 3.978297710418701, "[FF] Pointing Vector of the CSC Fluxgate Magnetometer = Determined by CCD star imager"]
-[10.232924461364746, 5.467990875244141, "[TT] Thermal Control of the UVNS = Passive cooling to ensure that temperature conditions are adapted to the different requirements of the instrument modules"]
-[3.0969197750091553, 3.8900513648986816, "[TT] Revisit Time of the NISAR = 12 days"]
-[6.816742420196533, 1.1411120891571045, "[FF] Conference Date of the Solar Orbiter /PHI Full Disk Telescope = Oct. 7-10, 2014"]
-[8.414618492126465, 2.8298282623291016, "[TT] Measurement Category of the OSCAR-QUBE = Gravity, Magnetic and Geodynamic measurements"]
-[7.910702705383301, 9.106545448303223, "[TT] Wavelength of the Sub-mm = 860 \u00b5m"]
-[11.349808692932129, 3.6517531871795654, "[FF] Main hollow-cathode discharge and main discharge on of the DISC = PS-5 and PS-3 on"]
-[8.7369384765625, 3.103158712387085, "[TT] Deployment Length of the ROSA = 8.6 meters"]
-[5.178488731384277, 7.963089466094971, "[TT] Mirror Oscillation Frequency of the TIR Subsystem = About 7 Hz"]
-[9.559045791625977, 0.2961532473564148, "[TT] Accumulated Travel of the Yutu-2 = 178.9 meters"]
-[9.695555686950684, 8.141251564025879, "[TT] Lens of the Imager = f1.4/85 Zeiss lens"]
-[3.82515287399292, 4.693063259124756, "[TT] Accuracy of Along-Track Velocity Components of the RADARSAT-2 = \u00b14.0 m/s"]
-[9.019003868103027, 7.3702287673950195, "[TT] Resolution of the CUTE = 2048 x 515 pixel"]
-[8.052206993103027, 4.912346839904785, "[FF] Typical Value of the H2O = 3 x 10 8"]
-[8.229267120361328, 6.4674296379089355, "[FF] Imaging Capability of the BILSAT-1 = Stereoscopic"]
-[9.65602970123291, 4.194685459136963, "[TT] Quantity of the Magnetometer = 3 units"]
-[13.317548751831055, 6.58609676361084, "[TT] Orbit Average Power of the MightySAT I = 14-27 W"]
-[10.848445892333984, 7.399909973144531, "[TT] Width of the Nix = 36 km"]
-[5.931354522705078, 2.0829451084136963, "[FF] URL of the FalconSAT-3 = http://www.satnews.com/cgi-bin/story.cgi?number=207495260"]
-[9.256796836853027, 1.8490164279937744, "[FF] Purpose of the HARPS = Determine Mass"]
-[6.1739888191223145, 5.46708869934082, "[TT] Type of the OISLs = Bi-directional"]
-[6.632591247558594, 3.6720497608184814, "[FF] Data Source of the GPM = IMERG"]
-[10.074357032775879, 5.440632343292236, "[FF] Function of the Detector Heaters = Maintain a constant cryogenic detector temperature"]
-[14.445993423461914, 6.792471408843994, "[TT] Minimum Battery Voltage of the IXV = 30.8 V"]
-[5.581973552703857, -0.6856046319007874, "[TT] Design Life of the Meteosat = 5 years"]
-[7.335843086242676, 4.782929420471191, "[TT] Navigation of the P3RVX = Optical"]
-[10.132661819458008, -2.744518756866455, "[TT] Programming Time of the NAND-Flash = 700 \u00b5s per 4 kbyte data"]
-[6.204737186431885, 4.154876232147217, "[FF] Function of the COSMOS = Communicates with the various payload customers to receive reports on the status of the instruments and mission accomplishment goals, as well as to receive payload tasking requests"]
-[6.8167805671691895, 5.922699928283691, "[TT] Modes of the RA-1 = Ocean mode and ice mode"]
-[9.812552452087402, 8.593353271484375, "[TT] IFOV of the Telescope = 0.065 mrad 0.14 mrad 0.14 mrad"]
-[4.830754280090332, 7.320981025695801, "[TT] Data Rate of the EWC27 X-band transmitter = Up to 100 Mbit/s"]
-[14.01175594329834, 6.334563255310059, "[TT] Manufacturer of the NanoCom AX100 = GomSpace"]
-[4.095882415771484, 3.5643863677978516, "[FF] URL of the Galileo = http://m.esa.int/spaceinimages/Images/2018/07/Galileo_satellites_viewed_in_smartphone_app"]
-[9.669574737548828, -0.4064880907535553, "[TT] Altitude Region for NO of the MAHRSI = 48 to 160 km"]
-[14.265162467956543, 3.189149856567383, "[TT] Mass of the POLDER = 33 kg"]
-[10.928720474243164, 6.2729926109313965, "[TT] Mirror Coating of the PAN Camera = Enhanced AlO2coating"]
-[7.67796516418457, 9.34605598449707, "[TT] Maximum Upper Band Edge of the MS1 (NIR1) = 901 nm"]
-[8.278992652893066, 6.811773300170898, "[TT] Type of the RSI = Pushbroom"]
-[8.489981651306152, 2.7342114448547363, "[TT] Measurement Range of the TSI = Outer boundaries of atmosphere"]
-[8.300142288208008, 1.2553181648254395, "[TT] Precipitation Difference of the Konya Plain = About 38 percent less"]
-[5.9115071296691895, 3.2462875843048096, "[TT] Number of Scientists or Institutional Teams of the PUTC = More than 60"]
-[11.196871757507324, 5.942959308624268, "[TT] Subject of the TICTOC Study = Cotton"]
-[13.648041725158691, 2.9791641235351562, "[TT] Weight of the X-SAT = 350 kg"]
-[10.132895469665527, 5.701150417327881, "[TT] Temperature Measurement of the FIBOS = \u00b120oC"]
-[7.56441068649292, 2.947967290878296, "[FF] Initiative of the Jerry Brown = Develop a greenhouse gas satellite"]
-[8.60857105255127, 7.70255708694458, "[TT] Number of Megapixels of the HAWAII-2RG 4 Megapixel array = 4"]
-[6.611006736755371, 5.0917744636535645, "[FF] Data Availability of the SSM/I, SSM/T and SSM/T-2 = Available for the general user community"]
-[5.339069366455078, 1.2630506753921509, "[FF] Data Calibration Timeline of the SMAP = Over the next year"]
-[8.324140548706055, 2.063775062561035, "[FF] SFE of the ASCAT = Scatterometer Front End"]
-[4.678770542144775, 0.06509939581155777, "[TT] End of Life Date of the TUBSAT = Spring 2007"]
-[6.694362640380859, 3.474919557571411, "[FF] Objective of the DMSP = Collect and disseminate worldwide cloud cover data on a daily basis"]
-[4.865127086639404, 4.192042827606201, "[TT] Manufacturer of the SOAR = GomSpace"]
-[8.709826469421387, 5.4644598960876465, "[FF] Function of the AMS STD = Measure smaller curvatures"]
-[9.350072860717773, 3.248823404312134, "[FF] Use Requirement of the OPSE = Coronagraph fully operational, door open, and then with the entrance pupil in the umbra or low penumbra"]
-[4.841368675231934, 7.244376182556152, "[TT] Digital Recorder Dump Rate of the X-band = 15.36 Mbit/s"]
-[5.519092559814453, 1.2322750091552734, "[FF] Conference Presentation Date of the EO-1 = Aug. 13-16, 2007"]
-[8.520251274108887, 5.571936130523682, "[TT] Measurement Accuracy of the GPS = 7.5 cm"]
-[11.445805549621582, 4.504580497741699, "[TT] Size of the M82 X-2 = The size of Pasadena"]
-[5.239973068237305, 2.701139450073242, "[TT] Development Location of the LHASA Model = NASA/GSFC (Goddard Space Flight Center) in Greenbelt, Maryland"]
-[6.829019546508789, 4.198844909667969, "[FF] Overview of the Air Force ESEX Flight Experiment = Not provided"]
-[9.274009704589844, 4.996438980102539, "[FF] Telemetry Information of the Attitude Determination Quaternion Filter = Probability distributions for the selection of each different measurement matrix"]
-[6.6382904052734375, 4.910865783691406, "[FF] Function of the C&DH = Process instrument information and send commands to actuators"]
-[9.530281066894531, 4.879665374755859, "[FF] Payload of the PARASOL = Rotating wheel inside the payload could change the satellite orientation"]
-[7.718202114105225, 1.1049708127975464, "[TT] Bulk Water Inventory of the Mars = Global Equivalent Layer (GEL) of ~30 m"]
-[8.826489448547363, 3.6077306270599365, "[FF] Instrument Types of the Voyager 2 = Cosmic ray instrument, two instruments dedicated to studying plasma, magnetometer, low-energy charged particle instrument"]
-[9.503426551818848, 7.174483776092529, "[TT] Radiometric resolution of the L-band = 0.2 K"]
-[6.753840923309326, 8.385133743286133, "[FF] Function of the ND = Adjust the transmission of each spectral channel"]
-[5.458822727203369, 6.29873514175415, "[TT] Data Memory of the Payload = 512 Gbit"]
-[5.770540714263916, 7.15077543258667, "[TT] On-board Data Smoothing Factor of the OLS = 25"]
-[4.64718770980835, 7.929998397827148, "[TT] Ground Interference Frequency of the RAVAN = 450 MHz"]
-[5.972866058349609, 0.8093364238739014, "[FF] Publication Date of the Netherlands Image = 11 February 2021"]
-[4.78345251083374, 6.31987190246582, "[FF] Purpose of the Wireless Compose-2 = Conduct and execute low-power, low-weight, and wireless experiments on the International Space Station (ISS)"]
-[9.256826400756836, 3.5454344749450684, "[FF] Mission of the SIGMA = Measure the global magnetic field and radiation"]
-[5.015615463256836, 3.290666341781616, "[TT] Owner of the RADARSAT Constellation = Canadian Space Agency (CSA)"]
-[11.599617958068848, 3.4072556495666504, "[TT] Propulsion Type of the Eurostar E3000 = Electric (plasma) propulsion"]
-[8.694416046142578, 1.745316505432129, "[TT] Drift Rate of the OceanSat-1 = < 0.0003\u00ba/s"]
-[5.53346061706543, 1.0053966045379639, "[FF] Integration Date of the Second Scientific Instrument = Unknown"]
-[7.152257442474365, 7.136538028717041, "[TT] Uncompressed Pulse Width of the ALT = 3.2 \u00b5s"]
-[5.100467681884766, -0.2770853042602539, "[TT] Launch Date of the Arachne = Early 2025"]
-[5.491382122039795, 4.991026401519775, "[FF] Primary and Redundant CAN Buses of the CSM = Communication"]
-[14.308357238769531, 3.2480671405792236, "[TT] Mass of the AMS-02 = 6918 kg"]
-[5.304060935974121, 1.569083333015442, "[TT] Agreement Conclusion Date of the ALOS-2/Daichi-2 = April 30, 2015"]
-[9.037476539611816, 4.5226359367370605, "[FF] Nominal Scenario Orbit Phases of the PROBA-V = Geodetic attitude with yaw steering correction, Sun-bathing mode, Geodetic pointing mode, Reactivated to reach thermal stability"]
-[13.762042045593262, 3.253455400466919, "[FF] Mass of the Canadian Advanced Nanospace Experiment 2 = 3 kg"]
-[3.213061571121216, 3.852294683456421, "[TT] Contact Date of the TerraSAR-X = June 19, 2007"]
-[9.001705169677734, 0.4094640910625458, "[TT] Maximum Distance from Crater Center of the Disturbed Areas = Up to 15 m"]
-[8.288552284240723, 8.979177474975586, "[TT] Spectral Resolution of the Argus = About 6 nm"]
-[4.939061164855957, 5.1080002784729, "[TT] CCSDS ID of the GSAT-0210 = 26A"]
-[10.399774551391602, 2.3399293422698975, "[TT] X-ray Photon Detection Efficiency of the pnCCD Chip = At least 90% in the energy band from 0.3 keV to 10 keV"]
-[5.092859268188477, -0.34624627232551575, "[TT] Launch Date of the CBERS-2 = Oct. 21, 2003"]
-[5.484651565551758, 4.89288854598999, "[FF] Data Downlink of the GNOMES = Via commercial ground station networks"]
-[6.417067527770996, 5.2926130294799805, "[FF] LVCMOS/TTL Outputs of the C&DH SPAM board = General purpose"]
-[10.139707565307617, -1.4675476551055908, "[TT] Inclination of the SEOSAT-Ingenio = 98\u00ba"]
-[6.9747724533081055, 4.959110736846924, "[FF] Function of the SM = Zeros the DWS signal"]
-[5.69285774230957, 3.8263349533081055, "[FF] Constellation Size of the Global-8 and Global-9 = 30 satellites"]
-[5.267556190490723, -1.345513105392456, "[TT] Design Life of the Kondor-E = 5 years"]
-[8.286506652832031, 2.769620656967163, "[FF] Data of the CHAMP = Atmospheric Temperature Fields"]
-[8.995960235595703, 7.285498142242432, "[TT] Detection Area of the SXD = 1 cm2"]
-[6.392892837524414, 1.871469259262085, "[FF] Open Platform of the Google Earth Engine = Yes"]
-[3.678642988204956, 4.006602764129639, "[TT] Commissioning Start Date of the RISAT-1 SAR payload = 29 April 2012"]
-[13.409516334533691, 2.9730470180511475, "[TT] Payload Mass of the MightySAT I = 17 kg"]
-[5.236123085021973, 4.9911065101623535, "[TT] Lock Maintenance Period of the NovAtel GNSS receiver = 20 to 30 minutes"]
-[6.133302211761475, 5.124808311462402, "[TT] Performance of the GPS = Degraded"]
-[10.298803329467773, 5.610513210296631, "[TT] Temperature of the Deep Space = Approximately 4 K"]
-[6.441335678100586, 3.0899133682250977, "[TT] Mission of the WSF-M = Weather System Follow-on (WSF-M)"]
-[3.6683216094970703, 4.8533172607421875, "[TT] Spatial Resolution of Data of the RADARSAT-1 = 10-100 m"]
-[5.1161208152771, 4.358210563659668, "[TT] Number of additional DASS POC payloads with S-band anticipated to be deployed by 2019 of the GPS II = 12"]
-[8.706296920776367, 6.977755546569824, "[TT] Spectral Resolution of the DMC-3 = Four bands"]
-[5.842685699462891, -2.25337815284729, "[TT] Orbital Altitude of the KOMPSAT-2 = 685 km"]
-[13.826665878295898, 5.701728343963623, "[TT] Efficiency of the Solar Array Regulator = 94%"]
-[13.813974380493164, 2.6645190715789795, "[TT] Launch Mass of the Spacecraft = 588 kg"]
-[7.707345485687256, 6.446916580200195, "[TT] Images Collected of the ABI = 30-second Mesoscale, 5-minute CONUS, 15-minute Full Disk"]
-[4.586515426635742, -0.3267453908920288, "[TT] Docking Time of the Starliner = 26 hours after launch"]
-[4.478389739990234, 3.0354151725769043, "[TT] Ground Station of the RemoveDebris = SSTL\u2019s MOC (Mission Operations Centre) in Guildford"]
-[6.3649749755859375, -0.6542229056358337, "[TT] LTDN of the NEMO-AM = 9:30 hours"]
-[11.056863784790039, 1.5001373291015625, "[TT] Diameter of the STARSHINE-3 = 94.5 cm"]
-[9.804119110107422, 7.498567581176758, "[TT] GSD (Ground Sample Distance) of the GeoEye-1 = 0.41 m (Pan) 1.65 m (MS)"]
-[4.425415515899658, 6.767249584197998, "[FF] L-band region of the Inmarsat = Fourth full-service"]
-[7.9557785987854, -0.9349371790885925, "[FF] Data Combination of the GRACE-Follow On = Observations from ICESat and ICESat-2"]
-[9.29475212097168, 6.998184680938721, "[TT] Resolution of the iMTQ = 15 nT"]
-[4.732727527618408, -1.2932807207107544, "[TT] Collection Location of the Yuanwang-21 and -22 = Tianjin"]
-[6.5818586349487305, 2.3168740272521973, "[FF] Data Sheet URL of the ADIS16003 = http://www.analog.com/static/imported-files/data_sheets/ADIS16003.pdf"]
-[4.760781288146973, 0.03197333589196205, "[TT] End of Life Date of the DeMi = 8 March 2022"]
-[6.309345245361328, 2.0964934825897217, "[FF] Project Lead of the TEMPO = Kelly Chance of Harvard-Smithsonian/CfA (Center for Astrophysics), Cambridge, MA, USA"]
-[6.982916355133057, 4.320434093475342, "[FF] Unknown of the CrIS = Unknown"]
-[6.537017345428467, 4.112453937530518, "[FF] Payload of the MPQ442 = OrbitView"]
-[5.541800022125244, 5.028564929962158, "[FF] Type of the Tatara Bridge = Cable-stayed"]
-[5.363913536071777, 4.880164623260498, "[TT] Modes of the LPT = Space Network (SN), Ground Network (GN), GPS"]
-[8.698534965515137, 7.642739772796631, "[TT] Detector Size of the HSC-1700 = 640 x 480 pixels"]
-[7.589704990386963, 8.666594505310059, "[TT] Number of Bands of the Spectral Bands = 15"]
-[8.348261833190918, 5.751936912536621, "[FF] Functionality of the Active Calibration Source = Equivalent to a very large known reflector on the surface"]
-[10.78899097442627, -0.3249373137950897, "[TT] Commissioning Phase Duration of the TanDEM-X = About 3 months"]
-[2.9751341342926025, 4.441801071166992, "[TT] Modes of Operation of the XSAR = High resolution mode by sliding spotlight, Standard mode by stripmap technique and Wideswath mode by TOPS (Terrain Observation with Progressive Scan) technique"]
-[6.015751361846924, -0.5511214733123779, "[TT] Mission Duration of the TanSat = 5 years"]
-[9.02660846710205, 5.546947479248047, "[TT] Body-pointing Event Monitoring Capability of the ASNARO = \u00b145\u00ba in any direction from nadir"]
-[11.998268127441406, 6.608669281005859, "[TT] Energy Range of the B/C ratio = 0.5 GV to 500 GV"]
-[6.403623104095459, 8.143918991088867, "[TT] Number of Channels of the VISSR = 5"]
-[5.733778953552246, 0.5160169005393982, "[FF] Test Date of the SpinSat = May 21, 2015"]
-[9.77397632598877, 1.6094353199005127, "[FF] Final Results of the SPADUS = Planetary Space Science, Vol. 53, 2005, pp. 903-923"]
-[5.660045623779297, 0.760356068611145, "[FF] Bankruptcy Filing Date of the UrtheCast = October 24, 2020"]
-[12.063984870910645, 3.6798646450042725, "[TT] Pressure of the Airtight Vessel = 1200 mbar"]
-[8.000214576721191, -0.3676200807094574, "[FF] Annual Summer Minimum Date of the Arctic Sea Ice = September 18, 2019"]
-[5.68422794342041, 0.6941241025924683, "[TT] First Observation Date of the ISUAL = 4 July 2004"]
-[7.657305717468262, 9.071802139282227, "[TT] Wavelength Range of the Band 3 = 0.846-0.885 \u00b5m"]
-[8.095544815063477, -1.2237584590911865, "[TT] Device Type of the ICESat-2 = Laser altimeter system"]
-[5.687987804412842, 4.559082508087158, "[FF] Concept of Operation of the EDRS = Communication link sessions are planned and coordinated between the EDRS MOC and the user\u2019s MOC, making use of the visibility windows available between EDRS and the user satellites"]
-[11.732817649841309, 6.779446125030518, "[TT] 15% FWHM of the Energy Resolution = Energy resolution (delta E/E) 15% FWHM (Full Width Half Maximum)"]
-[6.150815486907959, 2.5322422981262207, "[FF] Contribution to the Orion Program of the European Service Module = IAC 2015"]
-[6.267643928527832, 5.075387477874756, "[FF] Function of the DPCC = Generate and execute FOP to delete the commands from the on-board time-tag TC buffer"]
-[7.678343296051025, -0.07825248688459396, "[TT] Collision with Cliff of the Philae = 45 minutes after landing"]
-[5.251877784729004, 4.810326099395752, "[TT] Configurable GNSS Signals of the GNSS-RO Receiver = GPS, GLONASS, and additional GNSS signals"]
-[8.684224128723145, 7.898570537567139, "[TT] Number of Arrays of the FPA (Focal Plane Assembly) = 4"]
-[5.643321990966797, 0.6290434002876282, "[FF] Observation Date of the Space Shuttle Columbia = 2004"]
-[4.502689361572266, 1.562933325767517, "[TT] Year of Launch of the ACRIMSat = 1999"]
-[7.870418071746826, -0.196798175573349, "[TT] Latency of the ATL10 Arctic/Antarctic Sea Ice Freeboard = 45 days"]
-[5.977725505828857, 1.184720516204834, "[FF] Publication Date of the The Space Mission at Kwajalein = 2012"]
-[10.398796081542969, 3.229264974594116, "[TT] Number of CubeSat Units of the Black Knight-1 = 1"]
-[6.497683525085449, 5.392315864562988, "[FF] Purpose of the Comparison of military grade commercial and radiation hardened bulk silicon anti-fuse-based field-programmable gate arrays = Comparison of military grade commercial and radiation hardened bulk silicon anti-fuse-based field-programmable gate arrays"]
-[11.44111156463623, 4.859921455383301, "[TT] Shape of the ASPIICS = Conic"]
-[6.164474010467529, 5.439698219299316, "[FF] Functions of the Digital Back-End (DBE) = Digital conversion of the radar echoes, digital beamforming, SCan On Receive, decimation, data compression, packetization"]
-[5.738430023193359, -0.8018167614936829, "[TT] Design Life of the RISAT-2 = 5 years"]
-[8.155109405517578, 0.09972303360700607, "[TT] Launch Date of the Meteor-1-1 = 26.03.1969"]
-[5.075532913208008, 4.009000778198242, "[TT] Provider of the Level 0-1b software = KNMI"]
-[7.66933012008667, 9.433622360229492, "[TT] Center Wavelength of the Band 8 = 6.19 \u00b5m"]
-[14.21273422241211, 3.1430375576019287, "[TT] Mass of the NIUSAT = 15 kg"]
-[8.352225303649902, 7.077023506164551, "[TT] CIR Film Type of the Metric Camera = KODAK Aerochrome Infrared Film 2443"]
-[13.363871574401855, 7.737694263458252, "[TT] Beacon Power of the RF Communication System = 100mW"]
-[5.269475936889648, 2.5525267124176025, "[TT] Affiliation of the Michel Sarthou = CNES"]
-[5.346569538116455, 7.2565507888793945, "[TT] Bandwidth of the Bartolomeo = 0.1 Mbit/s"]
-[7.855617523193359, -2.464500904083252, "[FF] Impact of Minor Geomagnetic Activity of the GOLD = Can have an impact"]
-[9.160332679748535, 7.477861404418945, "[TT] Payload Size of the Optical Payload = 1.5U"]
-[7.951087474822998, 4.479435443878174, "[FF] Interlaminar Strength of the 2-D carbon phenolic (CP) material = Relatively low"]
-[13.115269660949707, 5.685683250427246, "[FF] Biasing Step of the TJ array = Occurs if arcs do not occur on the high-voltage array"]
-[5.7636847496032715, -0.059147994965314865, "[TT] Operational Period of the ISS = Until 2030"]
-[3.3559532165527344, 5.295352458953857, "[TT] Wavelength of the SAR = 100-500 m"]
-[9.431164741516113, 0.5362346768379211, "[TT] Descent Duration of the Schiaparelli = Just under six minutes"]
-[11.846446990966797, 4.770608425140381, "[TT] Dimensions of the EIRSAT-1 = 22 by 10 by 10 cm"]
-[8.346388816833496, 4.095818996429443, "[TT] Measurement Record of the Total Irradiance Monitor (TIM) = 40 years"]
-[5.929362773895264, 7.123772621154785, "[TT] Source Data Rate of the Instrument = Up to 960 Mbit/s"]
-[4.152641773223877, 1.3847930431365967, "[TT] Orbit Change Date of the Meteosat-8 = May 22, 2007"]
-[13.929550170898438, 4.052914619445801, "[TT] Instrument mass of the Spectrometer = 152 kg"]
-[6.518533229827881, 6.214535236358643, "[FF] Location of the SMX-2 = More shielded location"]
-[6.025553226470947, -0.3689129054546356, "[TT] Operations Duration of the UniSat-3 = One year"]
-[10.180160522460938, 7.019266128540039, "[TT] Displacement Across-Track of the MWR = 272 km"]
-[2.84850811958313, 0.08563817292451859, "[TT] J2000 declination (deg) of the B0540-69 = -69.33171"]
-[6.061349868774414, -0.21952055394649506, "[FF] Mission Duration of the FORMOSAT-2 = Ten years"]
-[5.182364463806152, 2.684673309326172, "[TT] Type of the HPCA = Toroidal top-hat"]
-[13.321624755859375, 6.5019612312316895, "[TT] Predicted Pmp at BOL of the KOMPSAT-6 = 2,874 W"]
-[7.4464898109436035, 2.911592721939087, "[FF] Purpose of the MethaneSAT = Measure methane emissions worldwide"]
-[8.221539497375488, 2.213954448699951, "[FF] Affected by of the PRODES = High frequency of clouds over the Amazon region"]
-[5.528165817260742, 2.7442855834960938, "[FF] Funding Agency of the ASI Opportunity Payload = ASI (Italian Space Agency"]
-[4.293124198913574, 7.274064540863037, "[TT] Frequency of the RF communication = S-band"]
-[8.20822811126709, 0.11417397111654282, "[TT] Launch Date of the Meteor-1/Meteor-2/Meteor-Priroda Series = 01 Jan 1993"]
-[7.116680145263672, 2.321624994277954, "[FF] Date of the Superresolution Far-field Imaging = 18 December 2018"]
-[11.632479667663574, 6.845558166503906, "[TT] Energy Band of the ART-XC = Up to 30 keV"]
-[12.040430068969727, -0.11554982513189316, "[TT] Number of Images in Southern Panorama of the TESS = 208"]
-[5.216202259063721, 0.9603987336158752, "[TT] MOU Date of the AMS-02 = September 20, 1995"]
-[11.018637657165527, 7.594837188720703, "[TT] Swath Width of the MSU-50 = 940 km"]
-[6.569734573364258, 2.3476269245147705, "[FF] Image Credit of the VIIRS = NASA Earth Observatory image by Lauren Dauphin, using VIIRS data from NASA EOSDIS LANCE, GIBS/Worldview, and the Joint Polar Satellite System (JPSS)"]
-[9.655563354492188, 4.829636573791504, "[TT] Stabilization of the SeaSat = Three-axis"]
-[10.17202091217041, 1.9833345413208008, "[FF] Luminosity of the Sw J1644+57 = Temporarily boosted"]
-[11.2066068649292, 4.92799186706543, "[FF] Mast Length of the NuSTAR = Lengthy"]
-[3.278021812438965, 5.334681034088135, "[TT] Spotlight Scene Centre Wavelength of the SAR Antenna = 31 mm"]
-[7.604224681854248, 5.258333206176758, "[FF] Components of the SHU = Flash FPGA, CPU, telescope CCD sensors (HPC-R,G,B,M), sprite CMOS sensors (LSI-W,N), fish-eye CCD sensor (WFC), bolometer array sensor (BOL), VLF receiver (VLF-R)"]
-[3.9827802181243896, 3.4408133029937744, "[FF] Development Start Date of the Galileo Second Generation Satellites = Unknown"]
-[6.219663143157959, 8.022336959838867, "[TT] Number of Channels of the Receiver Board = Four"]
-[10.727226257324219, 2.8434953689575195, "[FF] Design Presentation Proceedings Page Numbers of the Microsatellites = pp. 20-33"]
-[13.813602447509766, 2.777693271636963, "[TT] Launch Mass of the QZS-1 = 4100 kg"]
-[4.327995777130127, 7.104770660400391, "[TT] Downlink Frequency of the Spacecraft = X-band"]
-[4.227939128875732, 7.184526443481445, "[TT] Type of the X-band carrier = Single"]
-[6.627204418182373, 4.987190246582031, "[FF] Continuity Providers of the MWI = SSM/I, TRMM TMI, SSMIS, AMSRE, AMSR-2, GMI"]
-[8.205127716064453, 5.535533428192139, "[TT] Accuracy of the DORIS = Sub-mm"]
-[9.033129692077637, 7.993428707122803, "[TT] Focal Plane CCD Lines of the Camera = 3"]
-[10.039301872253418, -1.5309569835662842, "[TT] Orbit Inclination of the MicroMAS-2a = 97.55\u00ba"]
-[13.365387916564941, 7.173262596130371, "[TT] Power Consumption of the XI-IV = Average consumption of 620 mW"]
-[5.3787713050842285, 3.1654138565063477, "[TT] Manufacturer of the WorldView Legion = Raytheon Space Systems"]
-[9.271775245666504, 1.4332749843597412, "[TT] Deployment Length of the Deployer = 1 m"]
-[6.30999755859375, 4.494398593902588, "[FF] Function of the POIC = Coordinates allocation of onboard resources"]
-[5.207923412322998, 4.891174793243408, "[TT] Average Pass Length of the Ground Station = 7.4 minutes"]
-[3.453342914581299, -0.8936290740966797, "[TT] Orbit of the CSG and CSK satellites = Circular sun-synchronous"]
-[6.838859558105469, 2.0772600173950195, "[FF] URL of the STEREO = http://www.nasa.gov/mission_pages/stereo/news/farside-060111.html"]
-[7.992335319519043, 2.0893054008483887, "[FF] Application of the FY-3 (FengYun-3) = Ocean"]
-[13.316425323486328, 7.616248607635498, "[TT] Chirp Signal Peak Power of the Altimeter = 2 kW"]
-[5.674344539642334, 6.2627763748168945, "[FF] Data Storage of the Telescope = Programmable time bins"]
-[3.5438287258148193, 6.440550804138184, "[FF] Antenna Footprint of the AIS = Has narrower size due to lower satellite orbit altitude"]
-[8.002692222595215, 8.819948196411133, "[TT] Spectral Range of the O2-A = 758-778 nm"]
-[4.017523288726807, 4.1927170753479, "[FF] Agency of the RISAT-1 = ISRO"]
-[9.630191802978516, 8.215621948242188, "[TT] Field of View of the Lens = 24\u00ba x 24\u00ba"]
-[8.087965965270996, -0.9881758093833923, "[FF] Data Use of the ICESat-2 = Update classical understanding of subglacial lakes in Antarctica"]
-[4.743061542510986, 2.982104539871216, "[TT] Data Downlink Locations of the TRISHNA = India, France"]
-[10.326842308044434, 1.4492520093917847, "[FF] Luminosity of the Eta Carinae = One of the most luminous and massive stellar systems in our galaxy"]
-[10.818278312683105, 7.488186359405518, "[TT] Swath of the LISS-IIM = 131 km"]
-[7.205687522888184, 3.5314691066741943, "[FF] Purpose of the PROBA-3 = Block out the brilliant solar disk for the other satellite to open up continuous views of the Sun\u2019s faint corona"]
-[9.079625129699707, 2.6436057090759277, "[TT] Duration of the Geomagnetic Storm = Feb. 3"]
-[7.947452068328857, 8.502925872802734, "[TT] Channel Band (\u00b5m) of the MWIR (Midwave Infrared) = 3.5-4.0 (high)"]
-[5.051713943481445, 3.129420518875122, "[FF] Development Contractor of the LLMS/IRIS = SAIT-Systems S. A. of Brussels"]
-[6.2762064933776855, 1.3433184623718262, "[FF] On-Orbit Verification Date of the Space Inflatable Structures = June 1-8, 2008"]
-[4.4410080909729, 0.7462952136993408, "[TT] Delivery Date of the CONDOR Mk3 = Fourth quarter of 2022"]
-[8.071357727050781, -0.7278438806533813, "[TT] Orbit Overlap of the CryoSat-2 = Every 19th orbit of CryoSat-2 and 20th orbit of ICESat-2"]
-[5.168832302093506, 2.2892978191375732, "[TT] Mission Type of the SVOM = Non-EO"]
-[7.05804443359375, 7.221471309661865, "[TT] Laser Pulses of the ATLAS = More than 50 billion times"]
-[8.76951789855957, 5.326174736022949, "[TT] Nadir Pointing of the Dove-1 = Twice per orbit"]
-[10.75050163269043, 4.916315078735352, "[TT] Coil Cross-Sectional Area of the VLF Experiment = 42 cm2"]
-[14.76232624053955, 6.5896315574646, "[TT] Capacity per Cell of the Lithium-ion Battery = 1.5 Ah"]
-[11.62901496887207, 3.3916494846343994, "[FF] Class of the Ion Engine System = 20 mN"]
-[6.9268975257873535, 1.5078701972961426, "[FF] Launch Date of the SporeSat = 18 April 2014"]
-[3.565521240234375, 4.782146453857422, "[TT] Sensor Type of the RISAT = C-band SAR (Synthetic Aperture Radar) imager"]
-[7.148805618286133, 6.5062255859375, "[TT] Maneuver Execution Time (240 minute window) of the RASP = 143.36 minutes"]
-[5.079481601715088, 1.0317691564559937, "[TT] Launch Date of the INSAT-3D = 26 July 2013"]
-[10.508427619934082, 2.350626230239868, "[TT] Time Resolution of the X-ray Satellite Navigation = 1 \u00b5s"]
-[5.097470283508301, 8.051141738891602, "[TT] Frequency of the AMSR = Eight"]
-[11.463889122009277, 5.0155158042907715, "[TT] Platforms Separation of the ASPIICS = About 145 m"]
-[10.919381141662598, 3.8931920528411865, "[TT] Formation Ranges of the CanX-4 = 1000 m, 500 m, 100 m"]
-[10.970052719116211, 6.303543567657471, "[TT] Material of the Focal Plane Array = SiC"]
-[6.7062883377075195, 2.1219024658203125, "[FF] URL of the Radio Aurora Explorer = http://rax.sri.com/index.html"]
-[9.543508529663086, 3.7708609104156494, "[FF] Type of the GMR System = Giant Magneto-Resistance"]
-[5.198450565338135, 2.671830654144287, "[TT] Affiliation of the ALMASat = University of Bologna"]
-[8.383428573608398, 7.556560516357422, "[TT] Detector Type of the REM = Silicon"]
-[9.141683578491211, -0.5961240530014038, "[TT] Orbit of the PROBA-3 = Highly elliptical Earth orbit, 600 km x 60,524 km"]
-[5.3895158767700195, 6.785537242889404, "[TT] Data Downlink Frequency of the eROSITA = Daily"]
-[4.898674964904785, 0.7800620794296265, "[TT] OpenApp Qualification Completion of the MANTIS = 2020"]
-[10.317413330078125, 1.769228458404541, "[FF] Sources of the Neutrons = Galactic Cosmic Radiation (GCR), Earth's radiation belt, Solar Particle Events (SPE)"]
-[5.825034141540527, -2.254641532897949, "[TT] Ground Target Distance Between Adjacent Passes of the KOMPSAT-5 = 95 km (at equator)"]
-[6.220585823059082, 0.24410559237003326, "[TT] Crew Capacity of the Space Station = 7 members"]
-[13.52925968170166, 5.856756687164307, "[FF] Power Generation of the Satellite = Solar array area"]
-[7.812244415283203, 5.901823043823242, "[FF] Function of the Camera Sensor = Anti-blooming and electronic integration control"]
-[8.104533195495605, 8.2199068069458, "[FF] Calibration of the AVHRR/3 = Calibration of the IR channels is performed with four internal blackbodies every scan line"]
-[14.256752967834473, 3.2347238063812256, "[TT] Mass of the Eristo/Osteo = 66 kg"]
-[5.452203273773193, 4.734979152679443, "[TT] Bus Type of the OBDH = ESA standard"]
-[14.571661949157715, 6.7412848472595215, "[TT] Battery Predicted Cycle Life of the EPS = 20000"]
-[11.534111022949219, 5.119680404663086, "[TT] Size Savings of the Prototype Chip = About 40%"]
-[5.194670677185059, 3.690114736557007, "[TT] Assembly Platform of the EDRS-C = SmallGEO platform"]
-[6.984386444091797, 8.026532173156738, "[FF] SNR of the TriG = Higher than previous generation receivers"]
-[9.743541717529297, -0.605262815952301, "[TT] Orbit Altitude of the OPAL = ~ 370 km"]
-[9.806947708129883, 8.206254959106445, "[TT] FOV of the ART-XC = 34 arcmin"]
-[8.522226333618164, 0.7273924350738525, "[TT] Area of the Pongara National Park = 540 km2"]
-[4.157796859741211, 7.323082447052002, "[TT] Band of the miniKaAR-C = Ka-band"]
-[5.757629871368408, 6.433063507080078, "[TT] Product Data Capacity of the Temporary storage = 7 days"]
-[5.0918707847595215, 4.626148223876953, "[TT] Quantity of the GPS/DASS = 17"]
-[5.483677864074707, 0.7391659617424011, "[TT] Crime Scene Investigation Start Date of the Hera = Late 2026"]
-[13.919424057006836, 7.095889091491699, "[TT] Voltage of the Third Grid = -8 kV"]
-[8.241691589355469, 4.480506420135498, "[FF] Description of the Part A = Does not advance towards or away from the target over multiple orbits"]
-[8.06873893737793, 4.868141174316406, "[FF] On-board Orbit Computation of the DORIS-DIODE = Operational"]
-[6.97685432434082, 0.08920798450708389, "[TT] Subcycle of the SeaSat = 3 days"]
-[12.613531112670898, 9.092389106750488, "[TT] Equator Crossing Time of the Satellite = 10:26 hours"]
-[3.4161438941955566, 5.725895404815674, "[TT] Number of T/R Modules per Group of the SAR antenna subsystem = 2"]
-[9.550538063049316, 7.0293731689453125, "[TT] Spatial Resolution of the MSASI = 1.25 km"]
-[10.340977668762207, 7.9939961433410645, "[TT] Primary Diameter of the Telescope = 120 mm"]
-[5.052699089050293, -0.34354421496391296, "[TT] Launch Date of the CBERS-2A = Oct. 21, 2003"]
-[10.127273559570312, -2.7432777881622314, "[TT] Technology Type of the SLC NAND-Flash = SLC NAND-Flash"]
-[7.23602819442749, 8.28244400024414, "[TT] SNR of the FTS = >400 (Band 1) >300 (Band 2 to 5) @SZA=30\u00ba, albedo=0.3) >300"]
-[5.185821533203125, 1.5199329853057861, "[TT] In-Orbit Demonstration of the DST = Planned for 2010"]
-[6.156248569488525, 6.452236652374268, "[TT] Latency Requirement of the S-3 NTC = Within 28 days"]
-[5.889793395996094, -0.712958812713623, "[TT] Orbit Lifetime of the NRCSD = 8-12 months"]
-[3.047999858856201, 1.9832152128219604, "[FF] Anomaly Updates of the Copernicus Sentinel-1B = 2"]
-[8.110143661499023, 1.579886794090271, "[FF] Temperature Increase of the Surrounding Ocean = Yes"]
-[3.888319253921509, 6.31451416015625, "[TT] Number of Elements of the Antenna Array = 4"]
-[4.403191089630127, 7.194036960601807, "[TT] Type of the Ka-ISLs = Bi-directional"]
-[5.4224042892456055, 2.3789994716644287, "[TT] Backup Astronaut of the SpaceX CRS-17 = Nick Hague"]
-[5.831313610076904, 6.435100555419922, "[TT] Code Generators of the GATE Signal Generator = Four independent code generators for primary and secondary codes per unit"]
-[12.227142333984375, 3.6887574195861816, "[FF] Objective of the CVX = Measure the viscosity of Xenon at temperatures very near its liquid-vapor critical point"]
-[11.240767478942871, 2.8265414237976074, "[TT] Mass of the Nanosatellite = ~ 3.8 kg"]
-[7.711898326873779, 6.864850044250488, "[TT] Picture Interval of the M-CAM 1 = Six seconds"]
-[10.757637977600098, -1.1347757577896118, "[FF] Altitude of the SLATS Microsatellite = Super low altitude"]
-[9.38425350189209, 6.183455467224121, "[TT] Viewing Angle of the ISS-LIS = Nadir or 5\u00ba off-nadir"]
-[14.300640106201172, 3.1316254138946533, "[TT] Mass of the DIWATA-1 = 50kg"]
-[6.678562164306641, 3.4085371494293213, "[FF] Data Processing of the Satellite = NASA-funded scientists"]
-[10.745763778686523, 2.8147449493408203, "[TT] Design Life of the Minisatellite = 5 years"]
-[7.243903160095215, 8.462265968322754, "[TT] Number of Ion Emitters of the ASPOC = 8"]
-[7.399874210357666, 0.8561477661132812, "[TT] Landing Site of the Beresheet = Moon"]
-[5.555737018585205, 7.124424934387207, "[TT] Usage of the LRIT = Low Rate Information Transmission"]
-[7.134666919708252, 5.220744609832764, "[FF] Function of the Optical Payload = Acquire images of small orbiting objects, pre-process the data relevant to the target\u2019s orbit and pass the processed data to the ground station"]
-[5.616090297698975, 7.097203731536865, "[TT] Data Rate of the XTU = 160 Mbit/s"]
-[5.370595455169678, -0.027326762676239014, "[TT] Detector Stability of the Ikonos-2 = < 3% degradation over its entire life to date"]
-[8.7966890335083, -0.11347039043903351, "[TT] Latitudinal Zones of the ILAS-II = 56\u00ba - 70\u00ba N and 63\u00ba - 88\u00ba S"]
-[6.362071990966797, 1.8973132371902466, "[FF] URL of the Cupola = https://web.archive.org/web/20131207132529/http://thalesaleniaspace-issmodules.com/index.php/cupola"]
-[8.283785820007324, 8.179295539855957, "[FF] Detector Line Arrays of the Whiskbroom Scanner = 16 for VNIR bands, 32 for PAN, and 8 detectors for TIR"]
-[5.054285526275635, 0.2774004340171814, "[TT] Adoption Year of the Coordinated Universal Time (UTC) = 1967"]
-[12.546195983886719, 7.549615383148193, "[FF] Instrument Power of the Pushbroom imager = < 69 W (peak power with all heaters on)"]
-[10.303304672241211, -0.536618173122406, "[TT] Booster Segments Trip Distance of the SLS = 2,800 miles"]
-[6.4434614181518555, 5.044892311096191, "[FF] Module Type of the CAN bridge = Unknown"]
-[3.833664655685425, 4.755611419677734, "[TT] Ground Track Tolerance of the RADARSAT-2 = Better than \u00b1 5km, with a goal of \u00b1 1km"]
-[13.843951225280762, 5.674843788146973, "[TT] Efficiency of the Solar Cells = 15%"]
-[5.434439659118652, 0.6758038401603699, "[TT] Discovery of the Vela Junior = Just 20 years ago"]
-[11.970794677734375, 5.007351398468018, "[TT] Small Size of the DC-DC converter = 95 mm x 60 mm x 19 mm"]
-[7.9014716148376465, 3.2769360542297363, "[FF] Mission Objective of the GNOS = Remote sensing of Earth\u2019s neutral atmosphere and the ionosphere"]
-[3.8934266567230225, 7.852628707885742, "[TT] Modulation of the VHF-band communications = FSK"]
-[6.760725021362305, 6.400540351867676, "[TT] Processing Time of the Level 0 = 42 s"]
-[13.543282508850098, 5.503614902496338, "[TT] Body-mounted solar cells of the CLAVIS = True"]
-[6.173050880432129, 2.9401097297668457, "[TT] Revisit Rate of the WorldView Legion = Over 15 times a day"]
-[3.8137094974517822, 7.9246110916137695, "[TT] Modulation of the XBT = QPSK"]
-[6.285319805145264, 7.9376420974731445, "[TT] Coding of the VBR = Convolutional + RS"]
-[9.774151802062988, 0.5438345074653625, "[TT] Relative Tangential Velocity of the STARE satellites = < 3 km/s"]
-[11.829407691955566, 6.6945037841796875, "[FF] Energy Threshold of the EPISEM = Specific energy threshold is different for electrons and protons"]
-[5.445377349853516, 0.702141284942627, "[FF] Launch Preparations Date of the Galaxy 30 Satellite = 30 June 2020"]
-[10.289321899414062, 2.318183660507202, "[FF] Instrument of the RHESSI = X-ray and \u03b3-ray imaging spectroscopy"]
-[3.602125883102417, 1.8143450021743774, "[FF] URL of the Sentinel-2B = http://m.esa.int/Our_Activities/Observing_the_Earth/Copernicus/Sentinel-2/Second_colour_vision_satellite_for_Copernicus_launched"]
-[5.2266740798950195, 0.0424053855240345, "[TT] Launch Date of the Tsikada = June 30, 1982"]
-[5.079931735992432, 0.3731308579444885, "[TT] Addition Date of the Axiom Space commercial module = 2024"]
-[9.41773796081543, 7.141497611999512, "[TT] Radiometric Resolution of the Sensor = 0.5\u00b0 K"]
-[10.03704833984375, 7.063864231109619, "[TT] Cross-Track Coverage of the MSI-0 and MSI-1 = 60 km"]
-[5.829227924346924, 1.4938656091690063, "[FF] Commissioning Date of the Small Satellite Constellation = Aug. 9-12, 2004"]
-[7.951271057128906, 4.246332168579102, "[FF] Shutter of the Satellite Instrument = Not used"]
-[8.353276252746582, 5.960069179534912, "[FF] Function of the Piezo Driver Board = Create the piezo drive voltages from the raw battery bus, command the stage position, read the stage position, operate the piezo stage in closed loop using strain gauge feedback, and implement a notch filter to avoid exiting resonant frequencies in the stage"]
-[6.031088829040527, 7.043766975402832, "[TT] User Data Rate of the Optical RTN service = 1.8 Gbit/s"]
-[9.736541748046875, -0.12396585196256638, "[TT] Altitude of the Tsubame = 250 km, 240 km, 230 km, 181.1 km, and 167.4 km"]
-[8.781180381774902, 6.331468105316162, "[TT] Ocean Backscatter Coefficient Accuracy of the ALT = 1 dB"]
-[8.287102699279785, 7.520118713378906, "[TT] Detector Type of the PMT detector = GaAs opaque photocathode and multiple dynode PMT"]
-[13.558467864990234, 7.097553253173828, "[TT] Peak Power of the EPS = 230 W"]
-[10.630186080932617, 1.7060500383377075, "[FF] Measurement Capability of the NICER = Cooling histories of young neutron stars"]
-[11.348932266235352, 5.004795551300049, "[TT] Module Quantity of the Straw Tubes = 328"]
-[6.71550178527832, 1.9211666584014893, "[FF] URL of the Back-Illuminated CCD = http://www.imagesensors.org/Past%20Workshops/2015%20Workshop/2015%20Papers/Sessions/Session_10/10-01_Suntharalingam_IISW2015.pdf"]
-[6.406447410583496, 4.426787853240967, "[FF] Function of the DPE = Ingests mission data, ancillary data, and auxiliary data to produce NPOESS data products"]
-[10.149162292480469, 3.1844305992126465, "[FF] Function of the APEX CubeSat = Perform a multispectral mineral survey of its makeup"]
-[6.586040496826172, 1.1869910955429077, "[FF] Program Date of the European Student Earth Orbiter = Aug. 10-15, 2013"]
-[5.867353439331055, -0.20510877668857574, "[FF] Retirement of the RASAT = Retired after operating for 11 years"]
-[5.166193008422852, 6.9550981521606445, "[TT] Downlink Data Rate of the TanSat = 8.192 kbit/s"]
-[7.1904520988464355, 1.7729172706604004, "[FF] Monitoring Duration of the Forest Alert Service (FAS) = Less than three years"]
-[8.048938751220703, 5.089315891265869, "[FF] Required Precision of the O3 Profile = 10, 10, 5%"]
-[10.045976638793945, 1.371390700340271, "[TT] Observation Reach of the Roman = More than 13 billion years of cosmic history"]
-[5.97660493850708, 1.5247671604156494, "[FF] Presentation Date of the Small Satellites = Oct. 4-8, 2004"]
-[12.094223022460938, 3.4698715209960938, "[TT] Propellant of the HEMPT Thruster Assembly = Xenon"]
-[4.832091808319092, 0.793712854385376, "[TT] Launch Date of the Lunar Pathfinder Comsat = End of 2023"]
-[13.371124267578125, 5.531991481781006, "[TT] Quantity of the Solar Panels (SPs) = 3"]
-[3.9858081340789795, 4.75130033493042, "[TT] Signal Reception Frequency of the RISAT-1 DRS = 8212.5 MHz"]
-[13.43425178527832, 5.485103607177734, "[FF] Surface Treatment of the High-voltage Solar Array = Completely covered with RTV adhesive"]
-[6.958071231842041, 7.089887619018555, "[TT] Frequency Noise Power Spectral Density of the Laser = 30 Hz/\u221aHz"]
-[7.243265628814697, 8.183507919311523, "[TT] Sensitivity of the Channel 8 = 0.4 K/pixel"]
-[5.957754135131836, 7.193582057952881, "[TT] Data Rate of the SAGE-III = 115 kbit/s"]
-[5.210784435272217, 5.194543361663818, "[TT] Crystal Oscillator of the Namuru V3.2 GPS Receiver = 10 MHz voltage controlled temperature compensated crystal oscillator (VC-TCXO)"]
-[8.914217948913574, 4.388368606567383, "[FF] Attitude Sensors of the SUNSAT = 3-axis fluxgate magnetometer, 2-axis horizon sensor, fine slit sun sensor, second star sensor"]
-[6.694332599639893, 3.3846139907836914, "[FF] Latency of the Satellite Constellation = Minimum"]
-[5.166619300842285, 2.940507650375366, "[TT] Prime Contractor of the SloshSat-FLEVO = NRL (National Aerospace Laboratory)"]
-[7.992650508880615, 8.818533897399902, "[FF] Wavelengths of the VIRR = 0.49 \u00b5m - 0.94 \u00b5m, 10.5 \u00b5m - 12.5 \u00b5m"]
-[8.154925346374512, 3.073834180831909, "[FF] Spatial Filtering of the GLM = Matches the IFOV of each detector element to the typical cloud-top area illuminated by a lightning stroke (i.e., in the order of about 10 km)"]
-[10.374628067016602, 2.2719197273254395, "[TT] Energy Range (Green) of the Chandra X-ray Observatory = 1,000 to 3,000 eV"]
-[4.411723613739014, 6.19423246383667, "[TT] Helical Antenna Frequency of the GOMX-3 = 1090 MHz"]
-[5.975265979766846, 5.961086750030518, "[TT] Data Processing Unit of the SAMPEX = Common DPU"]
-[13.641425132751465, 6.969954013824463, "[TT] Total Power Requirement of the EPS = Around 679 W"]
-[6.527280330657959, 0.9367310404777527, "[FF] Announcement Date of the NASA Moon Mission = Oct. 27, 2016"]
-[5.648816108703613, 2.7404515743255615, "[FF] File Transfer Capability of the JAXA Flight Controller = Between SSIPC and JAXA laptops in JEM"]
-[11.75343132019043, 6.712556838989258, "[FF] Energy Levels of the SEM-2 = Electrons: 0.05-20 keV, Protons: 0.05 - 20 keV"]
-[10.362099647521973, 7.962432384490967, "[TT] Telescope Diameter of the CE-SAT-1 = 40 cm"]
-[4.008289337158203, 1.6580548286437988, "[TT] Launch Status of the Global-9 = Failure"]
-[5.682264804840088, 11.356110572814941, "[FF] Approx. peak sensitivity altitude of the Channel 5 = Unknown"]
-[4.4778828620910645, 2.9669158458709717, "[TT] Location of the DFD = Germany"]
-[11.912469863891602, 5.433967113494873, "[TT] Size of the GOLD instrument = 40 x 30 x 70 cm"]
-[5.490365028381348, 5.79457950592041, "[TT] Processor Model of the BILGE = PowerQUICCII"]
-[6.7170867919921875, 6.036652565002441, "[TT] Activation of the AutoNav = Immediate upon activation of the S/C"]
-[3.689159393310547, -1.0098509788513184, "[TT] Orbit Type of the LAGEOS = Near-circular"]
-[11.440481185913086, 5.797436237335205, "[TT] Material of the Outer enclosure structure = Aluminium honeycomb"]
-[6.004052639007568, 2.868834972381592, "[TT] Attachment of the CALET = JEM-EF (Japanese Experiment Module Exposed Facility), Port #9"]
-[6.445062160491943, 5.092127799987793, "[FF] Module Type of the BCM = Unknown"]
-[10.06740665435791, -1.5735887289047241, "[TT] Inclination Angle of the Suomi-NPP = 98.74\u00b0"]
-[8.615961074829102, 4.663991928100586, "[FF] Purpose of the Star Sensors = Provide higher accuracies for image processing"]
-[5.590639591217041, 8.039395332336426, "[TT] Frequency in Rotating Mode of the FEP = 1.0 x 10-3 Hz"]
-[6.5355939865112305, 6.422840595245361, "[TT] Data Processing Time of the C3S = Less than 30 minutes"]
-[9.670265197753906, 4.60015869140625, "[TT] Type of the ADCS = Passive magnetic attitude stabilization system"]
-[11.54487419128418, 3.5974960327148438, "[TT] Firing Direction of the Micronozzle = -X"]
-[4.632534503936768, 1.5036152601242065, "[TT] Development Start Date of the GOSAT-2 = April 9, 2014"]
-[5.000972747802734, 3.468308925628662, "[TT] Provider of the RDRS = DERA"]
-[4.36922550201416, 6.360485553741455, "[TT] Communication Method of the Voyager 2 = Deep Space Network's 70-meter-wide (230-feet-wide) radio antenna in Canberra, Australia"]
-[8.633840560913086, 1.1002544164657593, "[TT] Operations End Date of the Aquarius Instrument = June 17, 2015"]
-[9.923317909240723, 7.988300323486328, "[TT] Field of View of the Telescope = 0.5\u00ba x 0.5\u00ba"]
-[7.49387788772583, 2.5150139331817627, "[TT] Measurement Category of the CAS500 = Multi-purpose imagery (land)"]
-[10.454432487487793, 3.317401170730591, "[TT] Device Type of the MicroMAS-2 CubeSat = 3U CubeSat"]
-[5.0834808349609375, 6.979958534240723, "[TT] Downlink TT&C Data Rate of the MightySat II.1 (Sindri) = 20 kbit/s"]
-[5.886485576629639, 1.8390004634857178, "[FF] Launch Date of the SLS with Orion = 8 March 2018"]
-[4.823857307434082, 0.42470496892929077, "[TT] Vacuum Test Completion Date of the Prichal = October 28"]
-[13.364863395690918, 7.3363142013549805, "[TT] Power of the FGM = 2..5 W"]
-[8.0775146484375, -0.6806532144546509, "[FF] Data Usage of the ESA's CryoSat mission = Monitoring mountain glaciers"]
-[6.340935707092285, 7.020001411437988, "[TT] BEP (Bit Error Probability) of the SILEX Optical Terminal = < 10 -6"]
-[9.414273262023926, 6.957574367523193, "[FF] Spatial Resolution Calculation of the Radiometer = Geometric mean of the minor and major axes of the ellipse projected on the earth, also accounting for earth curvature"]
-[4.029017925262451, 5.5050272941589355, "[TT] Frequency of the Radar Altimeters = Microwave"]
-[8.804500579833984, 2.537827968597412, "[TT] Total Orbits of the Aurora = 36836"]
-[8.855573654174805, 4.9483819007873535, "[TT] Navigation and Attitude Control of the EO-1 = Tensor GPS receiver of Space Systems/Loral (SS/L)"]
-[7.550144672393799, 6.613596439361572, "[TT] Image Delivery Time of the Data Center = Within one hour after data acquisition"]
-[5.516683578491211, 2.5739171504974365, "[TT] Mission of the ArgoMoon = Deep-space"]
-[10.74326229095459, 1.355075478553772, "[TT] Mass of the TOI 451 = 95% of our Sun\u2019s mass"]
-[7.512993335723877, 2.9745991230010986, "[TT] Focal Plane of the MethaneSAT = 2048-pixel wide"]
-[4.376661777496338, 1.932792067527771, "[TT] Image Acquisition Date of the RADARSAT-2 = May 6, 2013"]
-[13.975357055664062, 7.2137370109558105, "[TT] Power Input of the PDC = 28 VDC"]
-[7.028543949127197, 3.287362575531006, "[FF] Daily Global Maps of the PROBA-V = 65"]
-[7.526295185089111, 5.625638961791992, "[FF] Home Page of the RIS Retroreflector = http://www-lidar.nies.go.jp/RIS/index0-e.htm"]
-[4.659125804901123, 7.938645839691162, "[TT] Chirp Bandwidths of the Satellite = 320, 80, 20 MHz (Ku-band), 160 MHz (S-band)"]
-[8.193349838256836, -0.24855035543441772, "[FF] Meltwater Runoff of the Greenland = 357 billion tons per year on average"]
-[7.589112758636475, 5.674076557159424, "[FF] Manufacturer of the Flash Imaging LiDAR = CSEM (Swiss Centre for Electronics and Microsystems)"]
-[10.01118278503418, 0.16985543072223663, "[TT] Spacing of the GRACE-FO Satellites = 220 km"]
-[8.20993709564209, 8.594307899475098, "[FF] Wavelength Range of the MIRI Spectrometer = 4.8-29 \u00b5m"]
-[5.567205905914307, -1.9624727964401245, "[FF] Image Scene of the KOMPSAT-3 = Jeodong Port on Ulleungdo Island, Korea"]
-[10.325812339782715, 5.790896415710449, "[TT] Phase Transition Temperature of the Gallium Calibration Source = 29.76\u00b0C"]
-[12.707544326782227, 1.9409984350204468, "[FF] Science Objectives of the SAGE-III = Provide atmospheric data essential for the calibration and interpretation/correction of other satellite sensors"]
-[10.181690216064453, 8.133050918579102, "[TT] Telescope Focal Length of the SIS (Scanning Imaging Spectrograph) = 75 mm"]
-[10.875226020812988, 7.546792984008789, "[TT] Swath Width of the MWNIR = 1600 km"]
-[12.059100151062012, 4.525305271148682, "[TT] Size of the Spacecraft = 2.4 m x 1.6 m x 1.5 m"]
-[5.21429967880249, 1.3369722366333008, "[FF] Date of the Pacific Tic-Tac-Toe = 29 December 2021"]
-[8.155011177062988, -0.6766248345375061, "[FF] Observation Data of the CryoSat-2 = Changes in ice thickness for March/April 2011, 2012 and 2013"]
-[5.793246269226074, -0.8126005530357361, "[TT] Design Lifetime of the QuakeSat = One year"]
-[6.046281814575195, 5.1088409423828125, "[FF] Type of the On-board Computer Processing Systems = Powerful complement"]
-[7.790229797363281, 8.605226516723633, "[TT] Centre Wavelengths of the INSAT sounder = Ranging from 14.71 \u00b5m - 3.74 \u00b5m in the IR bands and 0.695\u00b5m in the VIS band"]
-[7.717470645904541, 5.792974948883057, "[FF] Functions of the Optical bench = Launch the laser beam to other S/C, superimpose the received beam and the local oscillator on the PRFs, convert the optical heterodyne signal to electrical signal, enable the beam steering, enable closed loop beam steering, image the OBA entrance aperture and the FSM onto the PRFs"]
-[5.5173258781433105, 7.667845726013184, "[TT] EIRP of the DRT = 21 dBW (min)"]
-[5.84790563583374, 2.9110169410705566, "[FF] Type of the NOSS-36A = Navy Ocean Surveillance Satellite"]
-[14.211716651916504, 3.3576343059539795, "[TT] Mass of the MIP = 29 kg"]
-[8.39501953125, -0.05266622453927994, "[TT] Orbit Altitude of the TOPEX/Poseidon = 1336 km"]
-[13.395094871520996, 7.706510543823242, "[TT] Power of the RF Output Power = 3 W"]
-[4.379415512084961, 0.7086604833602905, "[FF] Anomaly Date of the DMSP Flight-19 = March 7, 2016"]
-[8.12636947631836, -0.6052404046058655, "[TT] Measurement Category of the CryoSat = Gravity, Magnetic and Geodynamic measurements, Landscape topography, Ocean topography/currents, Sea ice cover, edge and thickness, Ice sheet topography"]
-[11.177919387817383, 5.627177715301514, "[TT] Thickness of the GDS = 3 mm"]
-[7.8995184898376465, 8.495038986206055, "[TT] Spectral Range of the HSC = 450 - 850 nm"]
-[6.488810062408447, -0.49629300832748413, "[TT] Total Hours of the Airglow = 910.29"]
-[6.405542850494385, -0.6406286954879761, "[TT] LTDN of the Aalto-1 = 9:30 hours"]
-[6.051679611206055, -0.7522242069244385, "[TT] Campaign Duration of the KORUS-OC = 18 days"]
-[13.177870750427246, 7.591053009033203, "[FF] Function of the ALScat = Return estimates of backscatter power"]
-[11.05871295928955, 0.653139591217041, "[FF] Purpose of the WFIRST = Directly image exoplanets by blocking out the light of their host stars"]
-[5.810518741607666, 0.708375096321106, "[FF] Launch Dates of the Orbiting Astronomical Observatories = 1966-1972"]
-[6.559175491333008, -0.44240546226501465, "[TT] Period of the DMSP = 101.6 minutes"]
-[6.34839391708374, 4.457291126251221, "[FF] Function of the POCs = Focus on the higher levels of science data processing, planning of payload operations, performance assessment of the payload and payload calibration"]
-[6.286763668060303, 7.177366733551025, "[FF] Signal Strength of the AAUSat-1 = Very weak"]
-[7.2753586769104, 1.0597373247146606, "[TT] Launch Date of the OceanSat-2 = 24 September 2009"]
-[6.44428014755249, 1.4236202239990234, "[FF] Program Date of the COSMO-SkyMed = May 18, 2001"]
-[6.550834655761719, -0.4830786883831024, "[TT] Repeat Cycle of the MUX = 31 days"]
-[7.441514492034912, 2.3732779026031494, "[FF] Observation Objectives of the TAIKI = Provide hyperspectral imagery for agricultural applications, Acquire visualization of Earth warming by measuring NDVI (Normalized Differential Vegetation Index), Provide high quality video data of Earth's surface using a HDTV (High Definition Television) camera"]
-[9.44827651977539, 7.738436698913574, "[TT] Detector Thickness of the Telescopes = A: 33 \u00b5m, B: 150 \u00b5m"]
-[13.387861251831055, 7.198037624359131, "[TT] Power Storage of the ABEX = 160 W-hr"]
-[5.440417289733887, 6.951849460601807, "[TT] Serial Input Speed of the CDSU = 1.25 Mbit/s"]
-[7.36572265625, 2.968602418899536, "[FF] Environmental Monitoring of the Geodetic Satellites = Unknown"]
-[11.431066513061523, 4.388720512390137, "[TT] Size of the NMTSat = 3U"]
-[11.339496612548828, 5.863122463226318, "[TT] Material of the Helical Antenna = Aluminum alloy"]
-[6.944321155548096, 4.1908698081970215, "[FF] Power Subsystem Issue of the DMSP-F13 = Sudden spike in temperature, followed by an unrecoverable loss of attitude control"]
-[11.569485664367676, 4.643316745758057, "[TT] Size of the Psyche = About the size of Massachusetts"]
-[10.330877304077148, 1.974369764328003, "[FF] Number of X-ray Photons of the eROSITA = Doubled"]
-[11.520670890808105, 3.457735061645508, "[FF] Review of the Electric Propulsion Space Experiment (ESEX) = Journal of Propulsion and Power, Vol.18 No.4, 2002, pp. 723-730"]
-[4.808710098266602, 7.443963050842285, "[TT] Uplink Data Rate of the UHF Radio System = 4 kbit/s"]
-[2.930468797683716, 2.0015788078308105, "[TT] Peak Vegetation Growth Month of the Copernicus Sentinel-2 = April and May"]
-[9.27380084991455, 3.1766390800476074, "[FF] Presentation Date of the Magnetospheric Multiscale (MMS) = Feb. 28 - March 4, 2011"]
-[6.059683799743652, -1.957828402519226, "[TT] Chair of the George Hurtt = True"]
-[9.539795875549316, 0.7068747282028198, "[TT] Distance Traveled of the D-Sat = More than 12 million km"]
-[10.026908874511719, -1.404577374458313, "[TT] Initial Orbit Inclination of the Starshine = 51.6\u00ba"]
-[9.600441932678223, 4.764119625091553, "[TT] Configuration of the MTG = Twin configuration of 3-axis stabilized satellites"]
-[7.489058971405029, 5.043898105621338, "[FF] Purpose of the ARM M0+ processing unit = Lower cost, more energy efficiency and longer battery life"]
-[3.923064947128296, 9.735279083251953, "[TT] Bandwidth (GHz) of the ICI-6 = 4.8"]
-[7.599764347076416, 7.001475811004639, "[TT] Cadence of the Fast Neutrons = In the range 1-20 MeV"]
-[3.8562943935394287, 1.9419358968734741, "[TT] Stage Type of the Soyuz = Kerosene-fueled first stage boosters"]
-[6.722077369689941, 1.8687896728515625, "[FF] URL of the Space Environment In-Situ Suite (SEISS) = http://www.goes-r.gov/spacesegment/seiss.html"]
-[9.771088600158691, -0.3776242733001709, "[TT] Altitude of the Plane = Lower"]
-[8.925905227661133, 7.860022068023682, "[FF] Angular Resolution of the Wolter Optics = Finer than MPO"]
-[5.541805267333984, 3.858152151107788, "[FF] Quantity of the U.S. Weather Satellites = 2"]
-[10.377073287963867, 5.424923419952393, "[TT] Heat Rejection (Payload and Spacecraft Equipments) of the TCS = 1200 W"]
-[16.5229549407959, 3.631044864654541, "[TT] Prime Contractor of the OneWeb = OneWeb Satellites \u2013 a joint venture between OneWeb and Airbus Defence and Space"]
-[8.014339447021484, -0.37594735622406006, "[FF] Extent in October 2020 of the Arctic Sea Ice = The lowest on record for any October"]
-[12.414128303527832, 0.6749351620674133, "[TT] Operating Temperature of the PLATO CCDs = Lower than -65\u00b0C"]
-[3.246090888977051, 5.632368087768555, "[TT] Width of the SAR Antenna = 2.9 m"]
-[6.6783623695373535, -0.3874349892139435, "[TT] Period of the Satellite = 97 minutes"]
-[8.98865032196045, 5.146914482116699, "[TT] Number of Gyros of the IMU = 3"]
-[6.698997974395752, 5.222109317779541, "[FF] PDU of the ASCAT = Power Distribution Unit"]
-[4.081026554107666, 4.3926286697387695, "[FF] Usage of the RADARSAT-2 = Maritime Surveillance"]
-[4.4194817543029785, 7.828405857086182, "[TT] Uplink Frequency (Lower extended C-band channel) of the Communication Payload = 6450-6650 MHz"]
-[3.9429731369018555, 9.706127166748047, "[TT] Frequency (GHz) of the ICI-9 = 448\u00b13.0"]
-[9.816533088684082, 6.339071750640869, "[TT] Detector Sensitive Area of the D-CIXS = 10 mm x 10 mm"]
-[9.224653244018555, 6.94187593460083, "[TT] Resolution of the Gen-2 Satellites = One-meter"]
-[7.5791015625, 1.6020539999008179, "[FF] Imagery Capture Date of the WorldView-3 and GeoEye-1 = Northern California Wildfires"]
-[9.480412483215332, 2.640594482421875, "[TT] Detection Distance of the ASPIICS = ~0.04 solar radii"]
-[10.510126113891602, 5.762564659118652, "[TT] Operating Temperature Range of the FEEU = 10:45\u00baC"]
-[4.295656681060791, 0.73294597864151, "[TT] Launch Date of the EDRS-A = January 2016"]
-[4.500616550445557, 3.054340362548828, "[FF] Location of the AFGWC (Air Force Global Weather Central) = Offutt Air Force Base, near Omaha, Nebraska"]
-[4.791141033172607, 0.4607625901699066, "[TT] Launch Date of the ITASat-1 = December 2018"]
-[9.670083999633789, -0.4430314302444458, "[TT] Altitude of the AlSat-2B = 720 km"]
-[4.277236461639404, 2.2091076374053955, "[TT] Launch Site of the CanX-2 = SDSC (Satish Dhawan Space Centre), Sriharikota, India"]
-[6.260039806365967, 4.628856658935547, "[FF] Command Execution Method of the Spacecraft = Immediate or Time-tag queue"]
-[6.588586330413818, -0.5324732661247253, "[FF] Observation Duration of the DELPHINUS = Long-time and continuous"]
-[5.5948262214660645, -1.9663143157958984, "[TT] Operation Status of the KOMPSAT-5/Arirang-5 spacecraft = Nominal"]
-[13.364278793334961, 7.094486236572266, "[TT] Power Dissipation of the ASTERIA = 24 W"]
-[9.597225189208984, 6.981259346008301, "[FF] Velocity Resolution of the ELENA = Down to 10%"]
-[6.283047199249268, 0.7051239013671875, "[TT] Measurement Date of the Gaia = 3 December 2020"]
-[7.625396728515625, 8.946148872375488, "[TT] Bands of the Spectral bands = 8.2 - 9.0 \u00b5m; 10.3 - 11.3 \u00b5m; 11.5 - 12.5 \u00b5m; and 7.0 - 13 \u00b5m"]
-[9.069100379943848, 0.5111371278762817, "[FF] Orbit Raise Maneuver Sequence of the ARTEMIS-P1 = Unknown"]
-[10.407444953918457, 5.784933090209961, "[TT] Temperature Range of the SDR-SDRAM = 0\u00baC to +70\u00baC"]
-[9.539664268493652, 0.9538564085960388, "[TT] Speed of the LEO Satellite = ~ 8 km/s (28,000 km/h)"]
-[10.275496482849121, 7.95828914642334, "[TT] Size of the Optical Telescope Assembly = 1.524 m x 0.787 m"]
-[7.548722743988037, 6.958921909332275, "[TT] Cadence of the Composition of the Radiation = 30 minutes"]
-[10.1776123046875, 9.376826286315918, "[TT] Nominal IGFOV of the Band 5 = 1 km"]
-[6.654728412628174, 5.489110469818115, "[FF] Setup of I/O Ports of the dsPIC33F microcontroller = Unknown"]
-[4.330190658569336, 0.3836763799190521, "[TT] Launch Date of the JWST = 2019"]
-[4.26210355758667, 2.160597324371338, "[FF] Potential Rocket Launch Provider of the Spacety = Indian rockets"]
-[9.816614151000977, -0.4005095660686493, "[TT] Altitude of the Spacecraft = 650 km"]
-[2.9699313640594482, 4.47094202041626, "[FF] Observation Mode of the PALSAR-2 = Major observation modes"]
-[5.412796497344971, 6.17196798324585, "[TT] Type of the DDR2 SDRAM = Double Data Rate Synchronous Dynamic Random Access Memory"]
-[12.083222389221191, 6.256694316864014, "[TT] Antiproton Background Rejection of the AMS = Close to 1 in a million"]
-[9.465184211730957, 4.9274373054504395, "[TT] Attitude Knowledge of the STPSat-1 = 0.03\u00ba"]
-[4.225679874420166, 0.23287639021873474, "[FF] Presentation Date of the FalconSAT-7 = Sept. 13-16, 2011"]
-[10.356734275817871, 2.912775754928589, "[FF] Website of the Kolibri-2000 = http://www.energia.ru/english/energia/sci-education/microsat/microsat-02.html"]
-[7.953834056854248, 8.697586059570312, "[TT] Wavelengths of the EPIC instrument = 10"]
-[13.23940658569336, 5.275995254516602, "[TT] Solar Array of the Spacecraft = 10.6 m2"]
-[4.90020751953125, 3.3980023860931396, "[TT] Manufacturer of the CDHS = Pumpkin Inc."]
-[8.095442771911621, 4.760008811950684, "[FF] Components of the ACU = Flash FPGA, CPU, star CCD sensors (HSS-1,2), gyro sensor (GYRO), high-precision sun sensors (SASH-1,2,3,4), reaction wheel unit (RW)"]
-[10.725103378295898, 7.392963886260986, "[TT] Swath of the OSCAT = 1400 km"]
-[4.640639305114746, 3.0416245460510254, "[TT] Location of the FMCC = CNES in Toulouse, France"]
-[10.457353591918945, 2.2504279613494873, "[TT] Sensitivity of the X-ray Instrument = Greater than those carried by Ulysses in the 1990s"]
-[8.086126327514648, 8.011420249938965, "[TT] Spectral Bands of the WiFS camera = 0.62 - 0.68 \u00b5m, 0.77 - 0.86 \u00b5m"]
-[10.947269439697266, 2.0694162845611572, "[FF] Measurement Date of the XMM-Newton = Unknown"]
-[7.171207904815674, 7.939096450805664, "[TT] Sound Pressure Level of the EDRS-C = Up to 140 dbA"]
-[4.569819927215576, 5.862573146820068, "[TT] Accuracy of the 406 MHz emergency beacon = Better than 4 km"]
-[6.809786319732666, 2.2569000720977783, "[FF] URL of the MicroMAS Project = http://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=1015&context=smallsat"]
-[11.82425308227539, 0.053479455411434174, "[TT] Number of Pulsating Giants Identified of the TESS = 158,505"]
-[13.39453411102295, 6.86030912399292, "[TT] Power for Payload of the Spacecraft = 511 W"]
-[5.26102352142334, 2.33465313911438, "[TT] Mission Type of the Solar-A / Yohkoh = Non-EO"]
-[9.008023262023926, -0.7664806246757507, "[TT] Orbit Graveyard of the MEO Constellation = MEO (+ 300 km)"]
-[13.599793434143066, 1.7328556776046753, "[TT] Delivered Supplies of the Dragon C2/3 spacecraft = 460 kg"]
-[4.72366189956665, 3.2483277320861816, "[TT] Manufacturer of the TANSO-FTS = ITT Exelis of Rochester, N.Y."]
-[12.048055648803711, 4.766007900238037, "[TT] Envelope Dimensions of the MIRAD = 100 mm x 105 mm x 105 mm"]
-[4.4252824783325195, 0.12001252919435501, "[TT] Next Starlink Launch Date of the SpaceX = February 15"]
-[7.952696800231934, 8.750727653503418, "[TT] Spectral Range of the AMI = 430-900 nm"]
-[10.747236251831055, 7.219895839691162, "[TT] Footprint Size of the CarbonSpec = ~2 km x 2 km"]
-[7.651413917541504, -0.48716479539871216, "[FF] Author of the IceCube = Madeleine O'Keefe"]
-[6.584010124206543, 4.804981231689453, "[FF] Subsystems of the CAST968 bus = Structure and mechanism, thermal control, attitude and orbit control, power supply, TT&C, antenna, housekeeping and electrical subsystems"]
-[11.278038024902344, 3.695683479309082, "[FF] All discharge on and beam on/off by command from orbit control system of the ORBIT = PS-3, PS-5 and PS-7 on and PS-1 on/off by command"]
-[6.621949672698975, 4.666863441467285, "[FF] Function of the Organ-Chips = Study organ physiology and diseases in a laboratory setting"]
-[9.11196517944336, 3.1842212677001953, "[FF] Mission Goals of the Swarm = Core dynamics, geodynamo processes, and core-mantle interaction; Lithospheric magnetization and its geological interpretation; 3-D electrical conductivity of the mantle"]
-[13.054226875305176, 7.11061954498291, "[TT] Power Consumption of the SGR-ReSI = 10 W"]
-[5.072582721710205, 1.0188288688659668, "[TT] Restructure Date of the NPOESS = February 2010"]
-[7.548729419708252, 2.8452978134155273, "[FF] Radar Altimeter of the HY-2A Satellite = Unknown"]
-[5.937376976013184, 0.8223005533218384, "[FF] First Light Image Capture Date of the MAXI = Aug. 18, 2009"]
-[4.6464409828186035, 0.6673760414123535, "[TT] Full Operational Service Date of the SARah = By the end of 2019"]
-[7.05654764175415, 8.333263397216797, "[TT] Estimated SNR of the Band 1 = 845.85 \u00b1 89.97"]
-[5.8965864181518555, 3.7258100509643555, "[TT] Number of Nanosatellites Launched of the Astrocast = 5"]
-[5.890215873718262, 5.987331867218018, "[TT] Data Collection Capacity of the Corvus-HD = 25 million square kilometres per day"]
-[6.883848667144775, 4.678715705871582, "[FF] Role of the CSC = Chaser"]
-[9.661471366882324, 1.4184662103652954, "[TT] Operation of the Pleiades System = Coordinated operation of the Pleiades satellites, spaced 180\u00ba apart in orbit"]
-[9.716309547424316, 7.003795623779297, "[TT] Spatial Resolution of the NSCAT = 25 km"]
-[7.700350284576416, 0.43419313430786133, "[TT] Mission Type of the Lunar IceCube = Non-EO"]
-[11.74914836883545, 0.09510979801416397, "[TT] Number of Small Planets to Deliver Information of the TESS = 50"]
-[6.57152795791626, -2.0312843322753906, "[TT] Operational Status of the Jason-3 = Operational as of August 2022"]
-[13.187325477600098, 5.497382640838623, "[FF] Components of the Spacecraft = Solar panels, spacecraft bus"]
-[10.096332550048828, 0.7464021444320679, "[TT] Separation of the Spacecraft = ~220 km"]
-[5.820298671722412, 5.112497806549072, "[FF] Capabilities of the WTCCS = Translation and transmission of commands; uplink of files; downlink of telemetry, log messages, and files; automation of each listed capability through a TCL API"]
-[6.970810890197754, 0.039585743099451065, "[FF] Orbit Insertion Time of the SeaSat-1 = Launch plus 57 minutes"]
-[5.824155330657959, 3.45525860786438, "[TT] Satellite Production Cost of the Satellogic = One-tenth the cost"]
-[6.665332317352295, 2.104929208755493, "[FF] Online Date of the Chinese Earth observation satellites = Jan. 12, 2017"]
-[8.789182662963867, 4.187365531921387, "[TT] Function of the Target Sensor = Solar and lunar acquisition"]
-[5.034151077270508, 1.974921703338623, "[TT] Landing of the ERO = Desert of Utah"]
-[4.4018144607543945, 1.81327486038208, "[TT] Number of Conflicts of the RADARSAT-2 = 202 in February"]
-[13.786323547363281, 5.351257801055908, "[TT] Type of the Solar Cells = Triple junction GaAs (Gallium Arsenide)"]
-[10.72982406616211, -1.0548121929168701, "[TT] Altitude Control System of the SLATS = Ion engine system"]
-[6.211485385894775, 4.1873884201049805, "[FF] Decoupling of the Satellite = Maximum"]
-[4.963505744934082, 8.126461029052734, "[TT] Signal Processing Bandwidth of the Digital Ka-band 3 x 3 channelizer = 200 MHz"]
-[10.1005220413208, -1.5597755908966064, "[TT] Inclination of the Corvus-BC 3 = 97.3\u00b0"]
-[4.921172142028809, 7.217305660247803, "[TT] Real-time Downlink Speed of the RF Communications = 150 Mbit/s"]
-[11.192445755004883, 1.0591809749603271, "[FF] Hardware of the LISA = Test masses, measurement devices, lasers"]
-[7.67390251159668, 3.9663565158843994, "[FF] Experiment of the TU Graz = Attempting to monitor signals emitted by devices in the 'Internet of Things' from space"]
-[8.569561004638672, 4.66206169128418, "[FF] Observation Modes of the OCO = Nadir, Glint, Target"]
-[14.706134796142578, 6.635378837585449, "[TT] Capacity of the Nickel-hydrogen battery = 89 Ah"]
-[8.060638427734375, 2.7479970455169678, "[FF] Measurement Category of the CAPI = Cloud and aerosol interference errors from CarbonSpec\u2019s measurements"]
-[5.999334335327148, 0.43936580419540405, "[FF] Data of the Rosetta = 2015, 2016"]
-[7.53329610824585, -0.6280046105384827, "[FF] Planned Launches in 2018 of the ICEYE = At least two additional missions"]
-[8.066364288330078, 1.6513264179229736, "[TT] Distribution of the TAO/Triton = Tropical Pacific"]
-[11.336286544799805, 4.269486904144287, "[TT] Size of the BRO-4 = 6U"]
-[9.917770385742188, 2.7416083812713623, "[FF] Deployment Method of the NanoRacks CubeSat = JEM airlock slide table"]
-[7.9970550537109375, 2.1731810569763184, "[TT] Observation Purpose of the PMI = Geophysical parameters of the land, ocean and atmosphere"]
-[12.031376838684082, 3.236466884613037, "[TT] Fuel of the Propulsion System = Green monopropellant fuel blend based on ADN (Ammonium Dinitramide)"]
-[5.7568182945251465, 0.5454540252685547, "[TT] Tandem Operations Start Date of the ERS-1 and ERS-2 = September 1995"]
-[8.179530143737793, -1.0219334363937378, "[TT] Measurement of the ICESat-2 = Height of the ice surface"]
-[7.721488952636719, 0.8724828362464905, "[TT] Variant of the Lunar Photon = High energy"]
-[7.664949893951416, 9.148591995239258, "[TT] Frequency of the NIRST = 3.8, 10.7 and 11.7 \u00b5m bands"]
-[5.855574131011963, 4.886593341827393, "[FF] L1-SAIF Signal Augmentation Performance Presentation of the QZSS = ION NTM (National Technical Meeting) 2007, San Diego, CA, USA, January 22-24, 2007"]
-[4.822977066040039, 4.430023193359375, "[FF] Bit Rates of the Argos-3 = Unknown"]
-[3.466637134552002, 6.415090560913086, "[TT] Aperture Size of the Antenna = 649 mm x 539 mm"]
-[5.77413272857666, 2.026448965072632, "[FF] Mission Status of the Kaber = Unknown"]
-[8.997346878051758, 5.6113972663879395, "[TT] Pointing Accuracy of the IPS = Within 1.2 arcseconds"]
-[4.728906154632568, 6.329880714416504, "[TT] Size of the APL\u2019s Frontier radio = Smaller than other deep-space radios"]
-[6.1906867027282715, 4.547823429107666, "[FF] Responsibilities of the Flight Operations System (FOS) = All flight operations of the Sentinel-2 spacecraft including monitoring and control, execution of all platform activities and commanding of the payload schedules"]
-[6.330358028411865, 3.661694288253784, "[TT] Operational Service of the GOES-18 = GOES West"]
-[11.69306468963623, 6.689706325531006, "[TT] Detector Energy Range of the ABEX = keV to MeV"]
-[13.429023742675781, 2.9337210655212402, "[TT] Mass of the RISAT-1 = 1858 kg"]
-[9.937549591064453, -0.5483835935592651, "[TT] Orbit Altitude of the MightySat I = 385 km"]
-[4.569556713104248, 1.5505882501602173, "[TT] Launch date of the GOSAT-2 = 29 October 2018"]
-[8.040229797363281, 8.09085464477539, "[TT] Bandpass of the TESS Camera = 600nm - 1000 nm"]
-[9.581485748291016, 7.275580406188965, "[TT] Ground Resolution of the Imager = 35 m"]
-[6.369469165802002, 1.4712226390838623, "[TT] Arrival Date of the Europa Clipper = Early June 2022"]
-[4.483601093292236, 6.785719394683838, "[FF] Command Transmission of the DCS = GOES-R antennas at WCDAS"]
-[7.594961166381836, 3.5548760890960693, "[FF] Technologies for Debris Removal of the RemoveDebris = Net capture, harpoon capture, vision-based navigation"]
-[6.88859748840332, 7.23468542098999, "[TT] Control of the Elevation Beam Width = Between 2.48\u00ba and 1.67\u00ba"]
-[14.003422737121582, 3.4503419399261475, "[TT] Weight of the Iris radio = 0.875 kg"]
-[12.794682502746582, 7.585216045379639, "[TT] Instrument Power of the MWHS-II = 116 W"]
-[5.754540920257568, 2.0553553104400635, "[FF] Mission Status of the ERS-2 = Unknown"]
-[7.9338884353637695, 8.404391288757324, "[TT] Sensitivity of the LWIR (Longwave Infrared) = NEDT \u2264 0.2 K"]
-[4.908420085906982, -0.27624642848968506, "[TT] Launch Window of the SpaceX = 5-hour window that opens at 8:02 p.m. EDT Sept. 15"]
-[13.18101692199707, 2.9522438049316406, "[TT] Maximum Mass of the Lunar Flashlight 6U CubeSat = 14 kg"]
-[4.208122730255127, 6.302308082580566, "[FF] Position of the Electric Field Antennas = Extends beyond the TPS"]
-[7.217827320098877, 2.8524258136749268, "[TT] Mission Control Centre Location of the MethaneSAT = New Zealand"]
-[7.614691734313965, 5.463051795959473, "[FF] Components of the Downlink = Off axis parabolic mirror, fast tip/tilt mirror, dichroic beam splitter, DM (Deformable Mirror), wavefront sensor, scoring camera, fiber coupled to the DPSK/PPM receiver, waveplate, slow tip/tilt mirror"]
-[6.175968647003174, 2.9387431144714355, "[TT] Revisit Rate of the WorldView Legion = Up to 40 times in a day"]
-[8.200746536254883, 0.19720283150672913, "[TT] Operators of the Meteor-M-2 = Russian Federal Space Agency (Roskosmos) and Federal Service for Hydrometeorology and Environmental Monitoring of Russia (Roshydromet)"]
-[7.981973648071289, -0.40218585729599, "[FF] Annual Maximum Date of the Antarctic Sea Ice = September 28, 2020"]
-[9.540226936340332, 5.728332996368408, "[TT] Lunar Axial Tilt of the DSN Stations = 4.5\u00ba to 5.5\u00ba"]
-[9.250405311584473, 7.839181423187256, "[TT] Detector Window Size of the NEA Scout Camera = 3840 x 3840 pixels"]
-[3.7537741661071777, 6.70176362991333, "[TT] Beam Width of the Altimeter Antenna = 1.1\u00ba for Ku-band and 2.7\u00ba for C-band"]
-[4.370785236358643, 7.567793846130371, "[TT] Frequency band of the Mobile Link = S-band (2.6 / 2.5 GHz)"]
-[11.454233169555664, 2.1850223541259766, "[TT] \u0394V (cm/s) of the FengYun 1C Debris = 0.71"]
-[9.042436599731445, 5.478055000305176, "[TT] Relative Performance Error of the Spacecraft = < 1.5 arcsec over 1.5 s (95%)"]
-[10.184835433959961, 2.040916919708252, "[TT] Observation Period of the Chandra X-ray Observatory = 2000 to 2013"]
-[10.505134582519531, 2.304344415664673, "[TT] Imaging Rate of the Cupid X-ray telescope = Hundreds of counts/s over the FOV"]
-[16.500782012939453, 3.599346399307251, "[FF] Connectivity Provider of the OneWeb = Arctic"]
-[8.072280883789062, 5.052757740020752, "[FF] Calibration Requirements of the MOPITT = Unknown"]
-[9.225709915161133, -0.4231835901737213, "[TT] Apogee of the Gravity Probe A = 10,000 km"]
-[7.759939670562744, 5.469447612762451, "[FF] Equipment of the The First smallsat of High School of Economics \u201cNIU VShE \u2014 DZZ\u201d = Experimental camera based on the stepped (Fresnel) lenses developed by the Samara University, and with a high-speed X-range transmitter"]
-[13.994564056396484, 3.14298939704895, "[TT] Weight of the HET-X = Less than 2 kg"]
-[5.674544811248779, 6.773965358734131, "[TT] Packet Size of the LPT = Variable"]
-[11.619576454162598, 3.353682279586792, "[TT] Propulsion System of the TanDEM-X = Cold gas propulsion system"]
-[10.517754554748535, 6.72062873840332, "[TT] Number of Concentric Layers of the NuSTAR Optics = 133"]
-[6.483080863952637, 1.860210657119751, "[FF] URL of the Shuttle Radar Topography Mission = http://www2.jpl.nasa.gov/srtm/srtmBibliography.html"]
-[9.035258293151855, 7.111164093017578, "[TT] Resolution of the Chang'E-2 stereo camera = 1.05 m"]
-[1.3173811435699463, 1.8993786573410034, "[TT] Cargo Capacity of the HTV-8 = Up to six tons"]
-[6.340089321136475, -1.3261629343032837, "[TT] Decommission Year of the GRACE = October 2017"]
-[7.470385551452637, 2.914942741394043, "[FF] Methane Emissions Detection of the MethaneSAT = Almost anywhere on Earth"]
-[6.294051647186279, 8.069236755371094, "[TT] Number of Passbands of the Channel 1 = 1"]
-[5.869487762451172, -0.7065198421478271, "[TT] Lifetime of the Expected orbital lifetime = ~10 years"]
-[5.896415710449219, 1.781099796295166, "[FF] Authors of the Hokkaido Satellite Project = T. Totati, T. Sakakibara, T. Yasunaka, K. Ishimura, S. Satori, K. Sugimoto, D. Igarashi, H. Hoshika, T. Uematsu, S. Era, A. Nakamura, K. Hori, R. Mitsuhashi, J. Nishidate, T. Sato, T. Yoneya, Y. Aoyanagi, T. Iwamoto"]
-[6.107125282287598, 2.3117032051086426, "[TT] Developer of the eROSITA = Max Planck Institute for Extraterrestrial Physics (MPE) in Germany"]
-[6.00468111038208, 4.4595208168029785, "[TT] Integration Method of the Platform = Soft-stacked"]
-[3.397993803024292, 6.396806716918945, "[TT] Size of the Antenna = 1510 mm x 990 mm x 1530 mm"]
-[8.044195175170898, 4.864060878753662, "[FF] HIS Calibrations Frequency of the TRUTHS = On occasions, particularly during commissioning phase"]
-[10.706727027893066, 2.8256874084472656, "[FF] Avionics Components of the Microsatellite = Four boards for C&DH, and power"]
-[4.2552714347839355, 3.2081751823425293, "[TT] Downlink Frequency Band of the Svalbard Ground Station = L-band"]
-[9.79548454284668, 4.514181613922119, "[TT] Control Method of the ADCS = Magnetic torque coils (magnetorquers)"]
-[7.662561416625977, 4.365545749664307, "[FF] Objective of the AMS-02 = Search for the 'missing universe' and understand the origin and structure of the Universe"]
-[9.545549392700195, 7.038308620452881, "[TT] Horizontal Spatial Resolution of the Tomorrow-R1 and -R2 = 5 km"]
-[5.591487884521484, 1.125794768333435, "[FF] Information Kit Date of the OasISS = May 2009"]
-[11.21760368347168, 1.0467796325683594, "[FF] Drag-free control concept of the LISA Pathfinder = Uses free-floating test masses sheltered inside each spacecraft as reference points for the measurement"]
-[5.867326736450195, 3.2080349922180176, "[TT] Total system cost of the WorldView-4 = $850 million"]
-[3.180335521697998, 3.9444658756256104, "[FF] Front-end Design of the NovaSAR-1 = Fully scalable solution"]
-[5.268620014190674, 5.54382848739624, "[TT] Communication Standard of the CFESat = IP (Internet Protocol)"]
-[8.752016067504883, 7.4834160804748535, "[TT] ISO of the Canon EOS 700D = 3200"]
-[7.387280464172363, 4.621027946472168, "[TT] Mounting Location of the OPSE = Center of the Occulter Disk"]
-[4.171203136444092, 6.174615859985352, "[FF] Design of the Antenna = Pre-deployed and designed to survive launch conditions in any orientation"]
-[5.135278701782227, 0.7251474261283875, "[TT] MCDR Pass Date of the LADEE = August 2, 2011"]
-[12.050995826721191, 4.539096355438232, "[TT] Deployed Dimensions of the Spacecraft = 3.6 m x 2 m x 1.1 m"]
-[6.640839099884033, 8.815407752990723, "[FF] Observation of the POLDER = Polarization and Directionality of Earth Reflectances"]
-[5.682717323303223, 6.619767665863037, "[TT] Encryption of the Transceivers = 128 AES"]
-[5.305750846862793, 5.134362697601318, "[TT] Comments of the L1-C/A = GPS interoperable signals"]
-[8.412206649780273, 6.864768028259277, "[TT] Design of the Imaging Subsystem = Dall-Kirkham"]
-[7.761294364929199, 5.82669734954834, "[TT] Instrument type of the SASS = Imaging multi-spectral radiometers (passive microwave)"]
-[11.802632331848145, 4.810875415802002, "[TT] Size in Launch Configuration of the S/C = 1.74 m x 1.9 m x 2.0 m"]
-[7.560034275054932, 3.7721216678619385, "[TT] Compatible Focal Lengths of the NightPod = 10.5 mm to 800 mm"]
-[10.97325325012207, 7.607666015625, "[FF] Swath Width of the POLDER = 1440 km x 2200 (across-track) km"]
-[5.656907081604004, 2.296809434890747, "[FF] Mission of the RamSat = Education"]
-[4.815809726715088, 0.5967332720756531, "[FF] Launch Date of the MetOp-SG = 2024-2039"]
-[3.253838539123535, 5.017724990844727, "[TT] Swath Width of the SAR = 20-150 km"]
-[13.813323974609375, 3.0555028915405273, "[TT] Spacecraft Mass of the TCS = 55 kg"]
-[6.704610824584961, 3.7560791969299316, "[FF] Considering Deals of the Rocket Lab = True"]
-[6.7414350509643555, 7.529565334320068, "[TT] Beamwidth of the HSB = 1.1\u00ba"]
-[5.138783931732178, 4.8597211837768555, "[TT] Types of the GPS Ephemerides = UltraRapid, Rapid, Final"]
-[12.268786430358887, 4.622081279754639, "[TT] Weight of the Sample Retrieval Lander = 5,291 pounds (2,400 kg)"]
-[7.260272979736328, 8.663516998291016, "[FF] Signal Bands of the BeiDou-3S = Legacy B1 signals, modernized signals in the L1, E5, and B3 band"]
-[8.091979026794434, -1.1993201971054077, "[FF] Laser Measurements of the ICESat-2 = Ice"]
-[3.4103031158447266, 5.312481880187988, "[TT] Downlink Frequency Band of the SAR/Galileo and SAR/GLONASS payloads = 1544 \u2013 1545 MHz (L-band)"]
-[8.341064453125, 2.803071975708008, "[TT] Measurement Domain of the Kolibri-2000 = Atmosphere, Gravity and Magnetic Fields"]
-[14.251441955566406, 3.29128360748291, "[TT] Mass of the HiSPiCO = 75 g"]
-[6.740303039550781, 3.058720111846924, "[FF] Data Source of the GOES 16 = GOES 16 data from NOAA and the National Centers for Environmental Information (NCEI)"]
-[6.568553924560547, -0.8374592661857605, "[TT] Measurement Frequency of the GRACE-FO = Month to month"]
-[6.34403657913208, 8.045856475830078, "[TT] Number of Channels of the GIIRS = 913"]
-[2.8913793563842773, 1.9679522514343262, "[TT] Image Capture Date of the Copernicus Sentinel-2 = May 6, 2022"]
-[8.453227996826172, 1.9164042472839355, "[FF] Likelihood to Stall of the Hurricanes = Increasing due to global warming signals"]
-[5.152514457702637, 3.470836877822876, "[TT] Manufacturer of the Satellite Vu = SSTL"]
-[9.241458892822266, -0.3664676249027252, "[TT] Perigee of the IBEX = 7,000 km"]
-[9.041898727416992, 7.218329429626465, "[TT] Image Resolution of the PMC = 2.5 m"]
-[9.564040184020996, 7.0561137199401855, "[TT] Spatial Resolution of the GIIRS = 16 km"]
-[8.355639457702637, 8.800689697265625, "[FF] Image Bands of the Herschel = 70 \u00b5m (blue), 160 \u00b5m (green) and 250 \u00b5m (red)"]
-[7.596202850341797, -0.8813173770904541, "[TT] Final Launch for Delta II of the ICESat-2 = Yes"]
-[7.969878673553467, 4.9219069480896, "[FF] Typical Value of the H2CO = 10"]
-[10.883727073669434, 5.583848476409912, "[FF] Purpose of the Semi-conductive coating = Release charges and prevent concentration of electric field"]
-[4.872878074645996, 3.1236648559570312, "[TT] Manufacturer of the ROSE-L = Airbus"]
-[4.910224914550781, 1.6533821821212769, "[TT] Calibration and Validation Phase of the G\u00f6kt\u00fcrk-2 = Ongoing"]
-[8.412908554077148, 4.353969573974609, "[TT] Maneuver Type of the Spacecraft = DTM (Direct Transfer Maneuvers)"]
-[6.595327377319336, -0.5239071249961853, "[TT] Period of the TRACE spacecraft = 96 minutes"]
-[8.350852012634277, 1.0980247259140015, "[TT] Ground Qualification Completion of the Aquajet = 2009"]
-[9.680179595947266, 7.016839981079102, "[TT] Spatial Resolution of the LISS-3 = 23.5 m"]
-[4.763049602508545, 6.999537944793701, "[TT] Simultaneous Operation of the Downlink = Imaging and Downlinking"]
-[3.721904993057251, 4.711310386657715, "[TT] Imaging Frequency Band of the RADARSAT-2 = C"]
-[9.495304107666016, 0.9104762077331543, "[TT] Closest Exploration Distance of the New Horizons spacecraft = 4 billion miles from the Sun"]
-[6.101711750030518, 4.345750331878662, "[FF] Scriptable Interface of the Gaia = Python, C, Java"]
-[7.706655979156494, -0.4186260998249054, "[FF] Publication Date of the IceCube = 10 March 2021"]
-[6.774481296539307, 2.534639596939087, "[FF] Photo of the WINGS = Image credit: NASA, Debora McCallum"]
-[9.80512809753418, 3.82149600982666, "[TT] Wave Speed of the STEREO spacecraft = 250 km/s"]
-[5.175192832946777, 6.644033908843994, "[TT] Command Link Rate of the F-15 and F-16 DMSP satellites = Higher"]
-[14.402851104736328, 6.52207612991333, "[TT] Maximum Battery Power Before 100% Depletion of the Satellite = 10 hrs"]
-[9.593640327453613, 4.221081733703613, "[TT] Time Cadence of the Three-axis magnetometer = Software defined and configurable, nominal product telemetered to the ground is 5 s"]
-[4.576955318450928, 7.321486949920654, "[TT] S-band Downlink of the UoSAT-12 = 2"]
-[6.203999042510986, 5.875855445861816, "[TT] Quantity of the SMM modules = 3"]
-[7.712719917297363, 0.664273738861084, "[TT] Water Ice Concentration Useful Quantity of the Lunar Flashlight = 0.5 wt%"]
-[6.63672399520874, -0.3696626126766205, "[TT] Period of the CSG and CSK satellites = 97 minutes"]
-[7.125808238983154, 2.448564291000366, "[TT] Edition of the Observation of the Earth and Its Environment = 4th"]
-[11.148380279541016, 5.566779613494873, "[TT] Thickness of the SAFI = <0.25 mm"]
-[6.456604480743408, 5.128698348999023, "[FF] Module Type of the PDM = Unknown"]
-[11.97021770477295, 4.987443923950195, "[TT] Size of the Module = 205 mm x 125 mm x 200 mm"]
-[9.491353988647461, 6.005888938903809, "[TT] Velocity of the Instrument = > 25\u00ba/s"]
-[4.2489800453186035, 7.1943039894104, "[TT] Frequency Band of the ASTERIA Telecommunication Subsystem = S-band"]
-[4.746438026428223, 4.942193508148193, "[FF] Information Provided of the Flightradar24 = Flight tracks, origins and destinations, flight numbers, aircraft types, positions, altitudes, headings, speeds"]
-[9.700510025024414, -0.6252390146255493, "[TT] Orbit Altitude of the Envisat = ~783 km"]
-[9.594261169433594, 8.215789794921875, "[TT] MTF of the Telescope = < 3 nm"]
-[5.870685577392578, -0.3421081304550171, "[TT] Routine Flight Operations Duration of the EDRS-C = At least 15 years"]
-[6.223276615142822, 8.475959777832031, "[TT] Function of the Hybrid Coupler = Synthesize \u00b145\u00ba polarized channels"]
-[1.7270684242248535, 6.135912895202637, "[TT] Hot Gas in Galaxy Clusters Percentage of the Universe = 4 percent"]
-[5.144343376159668, 8.470596313476562, "[TT] Bandwidth of the NewMag = 10Hz"]
-[7.519733905792236, 6.501424789428711, "[TT] Earth Scanning Time (LAC scenario) of the Instrument = 2.5 minutes"]
-[5.3484206199646, 1.3460369110107422, "[FF] Conference Date of the CHIPS = Aug. 13-16, 2001"]
-[8.197935104370117, 5.447214603424072, "[TT] Measurement Technique of the DORIS = DORIS"]
-[4.5999603271484375, 1.048134684562683, "[TT] Launch Date of the SAOCOM-1A = 2019"]
-[11.792254447937012, 5.3949809074401855, "[TT] Size of the CAPSTONE = Small microwave oven"]
-[3.8121471405029297, 4.571291923522949, "[TT] Sensor Module Capabilities of the RADARSAT-2 = Full polarimetric imaging"]
-[11.006780624389648, 3.7565455436706543, "[TT] Size of the ARKSAT-1 = 1U"]
-[12.791837692260742, 7.615358829498291, "[TT] Power Consumption of the CLARA Instrument = 5.6 W"]
-[7.389770030975342, 2.340855598449707, "[FF] Purpose of the NAOMI = Take high-resolution images of Algeria for cartography, agricultural management, crop monitoring, and disaster management"]
-[9.140695571899414, 2.9185593128204346, "[FF] Function of the XRS = Monitors solar flares and helps predict solar proton events"]
-[9.04251480102539, 8.11687183380127, "[TT] Angular Pixels of the WTS1 and WTS2 = 15"]
-[9.835794448852539, 6.632574081420898, "[FF] Function of the Lens System = Simultaneously image receive aperture and steering mirror pivot plane onto the photodetector"]
-[11.164785385131836, 0.5371800065040588, "[TT] Quantity of the Exoplanet = 5000+"]
-[7.294732093811035, 6.615211009979248, "[TT] Target Timeliness of the EARS Data Services = 15 to 30 minutes from instrument sensing"]
-[8.424872398376465, 5.514024257659912, "[TT] Geolocation accuracy of the ALOS-3/PRISM-2 = Better than PRISM"]
-[5.144435882568359, 2.715668201446533, "[TT] Mission Consortium of the CHEOPS = University of Geneva and University of Bern"]
-[8.374690055847168, 8.212540626525879, "[TT] Locking Performance of the Rb Spectroscopy Unit = Stayed locked during vertical accelerations reaching 12.5 g"]
-[9.749457359313965, 7.5494890213012695, "[TT] System Angular Resolution of the ART-XC = \u22641 arcmin"]
-[10.033782958984375, -1.5198825597763062, "[TT] Orbital inclination of the GPS-DASS = 64\u00ba"]
-[4.301967620849609, 0.7423611283302307, "[TT] Service Start Date of the EDRS-A = November 2016"]
-[5.481943607330322, 6.028871059417725, "[TT] ROM/RAM of the ACU = EEPROM(1MB x 2), SRAM(1MB x 2) for C&DH EEPROM(1MB), SRAM(1MB), MRAM(512KB) for HSS"]
-[8.501251220703125, 8.241020202636719, "[TT] Spectral Resolution of the Instrument = Better than 0.01\u00c5 (resolving power 105)"]
-[5.314688682556152, 6.3969011306762695, "[TT] Bus Speed of the BILGE = 50 MHz"]
-[6.09635066986084, 3.5706088542938232, "[FF] Project Responsibilities of the TSIS-1 = Project management, system engineering, safety and mission assurance, and engineering oversight for the TSIS-1 payload"]
-[4.981056213378906, 3.1918318271636963, "[FF] Partnership of the EDRS\u2013SpaceDataHighway = ESA and Airbus"]
-[6.164488792419434, 4.299360275268555, "[FF] Purpose of the Remote Agent = Reduce the cost of future S/C operations"]
-[13.879027366638184, 6.377449989318848, "[FF] Function of the Battery Holder = Battery control, battery overcharge protection and bus voltage regulation"]
-[6.802504539489746, 5.975807189941406, "[TT] Quantity of TQCMs of the AMO = 8"]
-[10.554128646850586, 3.338524103164673, "[TT] Form Factor of the Ultra-Compact Radiometer = 1U CubeSat"]
-[9.934614181518555, -0.5193684101104736, "[TT] Altitude of the NigeriaSat-2 = 700 km x 733 km"]
-[8.122416496276855, 9.153701782226562, "[TT] Ellipse Axis A of the Short Wavelength Band = 180 mm"]
-[3.9352104663848877, 4.274640083312988, "[FF] Imagery Provision of the RADARSAT-2 = To Europe's GMES (Global Monitoring for Environment and Security) program"]
-[11.10539722442627, 2.869853973388672, "[TT] Mass of the PACE nanosatellite = < 2 kg"]
-[7.293435096740723, 4.661046504974365, "[FF] Technology of the P3RVX = RV technology, in particular with non-cooperative targets, with two satellites, in a highly elliptical orbit, using optical Navigation"]
-[8.817743301391602, 7.60650634765625, "[TT] SWIR Resolution of the PROBA-V = 1024 pixels"]
-[8.029892921447754, 1.9626586437225342, "[TT] Imaging Area of the Ocean Surveillance mode = 530 km x 500 km"]
-[8.093650817871094, 4.577383518218994, "[FF] Research Center of the MEMS Space Telescope = Unknown"]
-[7.977982521057129, 9.155611991882324, "[TT] Wavelength for Oxygen Absorption Measurement of the LORE = Near 760 nm"]
-[13.486114501953125, 7.158820629119873, "[TT] Power Capability of the Buck-Boost Converter = 450 W per Converter"]
-[5.179970741271973, 0.16761641204357147, "[TT] Scheduled Deployment Date of the Cygnus spacecraft = Sunday, July 15th"]
-[9.601922035217285, -0.6320383548736572, "[FF] Target Orbit of the ExoMars TGO = Near-circular 400 km-altitude orbit"]
-[11.805678367614746, 4.778908729553223, "[TT] Size of the CEASE-2 = 10 cm x 10 cm x 8.2 cm"]
-[9.891663551330566, 6.469004154205322, "[TT] IFOV of the Earth Radiation Budget Experiment (ERBE) = 14 mrad"]
-[9.3509521484375, 4.055915355682373, "[FF] Illumination of the Solar Panels = Provided during rotation"]
-[6.6981000900268555, 2.669116735458374, "[FF] Source Data of the \u00b5SCIA = Planned to be posted onto the Internet"]
-[9.708890914916992, -0.20180799067020416, "[TT] Altitude of the Tsubame = 504 km"]
-[3.500974416732788, 5.252739429473877, "[TT] Frequency Bands of the SARR = 121.5 MHz and 406.05 MHz"]
-[9.269336700439453, 6.1820969581604, "[TT] Viewing Angle of the Argus = 0.1\u00b0"]
-[5.26889181137085, 1.1963720321655273, "[FF] Conference Date of the NPOESS = Sept. 9-11, 2008"]
-[5.216838359832764, 0.8085802793502808, "[FF] Published Online Date of the Hitomi = 13 November 2017"]
-[11.404666900634766, 4.3477067947387695, "[TT] Size of the E-TBEx = 3U"]
-[8.692703247070312, 7.665773868560791, "[TT] Size of the Detector = 2048 x 2048 pixels"]
-[8.606440544128418, 5.973837852478027, "[TT] Accuracy Requirement of the MAs and MCs = Within 50 \u00b5m"]
-[8.15397834777832, 8.31472110748291, "[TT] IR Channels of the Spectrometer = 22 channels from 12.78-12.85 \u00b5m (778.2-782.4 cm -1 ) with 0.2 cm -1  resolution"]
-[7.463759422302246, 0.6777920126914978, "[TT] Orbit Transition of the LunaH-Map = Several months"]
-[10.16984748840332, 3.0518579483032227, "[TT] Total Deployments from Space Station of the CubeSats = 185"]
-[4.174858570098877, 7.3056840896606445, "[TT] Operating Bands of the SES-14 = C- and Ku-bands"]
-[4.3523077964782715, 0.1581314653158188, "[TT] End of Life Date of the FalconSat-3 = 1 April 2017"]
-[10.54935359954834, 3.3299756050109863, "[TT] Spacecraft Type of the ABEX = 12U CubeSat"]
-[8.008978843688965, 0.6793220043182373, "[TT] Drought Period of the GRACE-FO satellites = 2000-2018"]
-[6.382926940917969, 5.144796848297119, "[FF] Unknown of the On-board computer processor module = Unknown"]
-[6.921716213226318, 1.5297783613204956, "[TT] Number of Transits for Observation of the James Webb Space Telescope = 5"]
-[4.621679782867432, 1.595009446144104, "[TT] Calibration Completion Date of the TanSat = Summer of 2017"]
-[9.66037368774414, 7.275264739990234, "[TT] Ground Resolution of the LISS-IIM = 32 m x 37 m"]
-[6.257328033447266, 0.3556303381919861, "[TT] Operating Mode Revisit Time of the ROSE-L SAR = 3 or 6 days"]
-[5.71049690246582, 4.508203506469727, "[FF] Operation of the EDRS-A hosted payload = Monitoring and telemetry reception"]
-[6.959918022155762, 5.844944000244141, "[TT] Number of Operational RAFS Clocks of the GIOVE-A = 1"]
-[3.6720662117004395, 6.39258337020874, "[TT] Diameter of the Ground Station = 3.4 m"]
-[8.525588989257812, 0.13755255937576294, "[FF] Data Collection of the Rosetta = Comet's dust, gas and plasma environment, its surface characteristics and its interior structure"]
-[10.309080123901367, 2.726010322570801, "[TT] Data Collection Duration of the NanoSat-1B = 518 days"]
-[9.493578910827637, 4.211123466491699, "[TT] Quantity of the Fluxgate Sensors = 3 orthogonal sensors per unit"]
-[5.515295505523682, 1.7553269863128662, "[FF] Mission Status of the KAGUYA-LALT = Present"]
-[6.712620258331299, 2.275524616241455, "[FF] Recommendation of the Commercial Smallsat Data Acquisition Program = Put into statute and robustly fund"]
-[4.8405914306640625, 2.8305914402008057, "[TT] Office Locations of the Spire = San Francisco, Boulder, Washington DC, Cambridge, Ontario, Glasgow, Oxfordshire, Luxembourg, and Singapore"]
-[8.223749160766602, 7.639529228210449, "[TT] Detector Elements of the AHI = 77,400"]
-[10.632434844970703, 6.227028846740723, "[FF] Surface of the Flight Mirror Assemblies = Non-reflective surfaces are procured un-anodized and will be wrapped in polyimide tape for increased emissivity"]
-[8.07053279876709, 2.7496509552001953, "[FF] Measurement of the TROPOMI = Trace gases, aerosol and cloud properties"]
-[6.787447929382324, 1.8749897480010986, "[TT] Expected Launch Year of the Nancy Grace Roman Space Telescope = 2027"]
-[9.137075424194336, 5.286890506744385, "[TT] Quaternion Uncertainty of the ABI = ~ 100 \u00b5rad"]
-[11.54265022277832, 4.893199920654297, "[TT] Diameter of the SpinSat = 558 mm"]
-[3.1519107818603516, 2.3317627906799316, "[FF] Usage of the Remote Sensing Data = Helping scientists figure out population changes of penguin species"]
-[4.882884502410889, 1.8043038845062256, "[FF] On-Orbit Thermal Analysis Date of the HORYU-2 = Oct. 10-13, 2012"]
-[11.37972640991211, 4.756368160247803, "[TT] Length of the Mast = 10 m"]
-[3.3989107608795166, -0.9345410466194153, "[TT] Orbit Type of the MethaneSAT = Sun-synchronous polar"]
-[4.782993316650391, -1.625349760055542, "[TT] Camera Type of the Tianwen-1 = Obstacle Avoidance Camera"]
-[10.370280265808105, 4.531725883483887, "[TT] Quantity of the Reaction Wheels = Four"]
-[5.002429008483887, 0.9653177261352539, "[TT] Launch Date of the OPS-SAT = December 2019"]
-[6.026699066162109, 6.454971790313721, "[TT] Latency of the ATL01 Reformatted Telemetry = 2 days"]
-[10.169912338256836, 0.9733439087867737, "[FF] Distance from Earth of the Chamaeleon I = Around 550 light-years"]
-[8.404353141784668, 1.9419586658477783, "[TT] Calibration Standard of the ISS-RapidScat = Golden standard"]
-[9.276420593261719, 5.037542819976807, "[TT] Attitude Control Accuracy of the Spacecraft = < 1.0\u00ba"]
-[4.593233585357666, 2.494797468185425, "[TT] Delivery Date of the BRITE Satellites = June 2011"]
-[5.011168003082275, 0.9500925540924072, "[FF] First Flight Date of the ATMOS Instrument = April 29 through May 6, 1985"]
-[5.761545181274414, -0.8614103198051453, "[TT] Survey Duration of the ART-XC = 2.5 years"]
-[9.36694622039795, 4.949830532073975, "[FF] Objectives of the UWE-2 = Continue the communication protocol experiments and to include technology tests related to attitude determination"]
-[6.951566219329834, 6.128620147705078, "[FF] Number of Instruments of the T/P = 7"]
-[12.068350791931152, 6.3185248374938965, "[FF] Electron and Positron Fluxes of the AMS = Fundamental Difference"]
-[9.441206932067871, 6.409693717956543, "[TT] Scan Profile of the Two-axis gimbaled mirror scan system = Tapered Elevation Scan (TES)"]
-[5.158681869506836, 2.354635715484619, "[TT] Mission Type of the CHOMPTT = Non-EO"]
-[9.75904655456543, -0.5864129662513733, "[TT] Orbit Altitude of the SAC-D/Aquarius = 657 km"]
-[6.676184177398682, 7.550355911254883, "[TT] A/D Converter of the C&DH subsystem = 11-bit 8-channel (or 12-bit 4-channel if used in differential mode)"]
-[4.885906219482422, 0.6426450610160828, "[TT] Launch Date of the GPM = 27 February 2014"]
-[7.163660049438477, 6.842685222625732, "[TT] Length Scales of the Laser = 700 km to 70 km"]
-[2.332360029220581, 1.3144088983535767, "[FF] Designers of the NanoSail-D2 = NASA/MSFC, NASA/ARC, ManTech/NeXolve Corporation"]
-[5.750447750091553, 0.629734992980957, "[FF] Publication Date of the Cluster STAFF experiment = 1997"]
-[9.483469009399414, 0.444007933139801, "[TT] Distance Range of the MCAM-2 = 920 km \u2013 6099 km"]
-[4.082653999328613, 3.62766432762146, "[TT] Operational Goal of the Galileo constellation = 2013"]
-[6.931251049041748, 7.759309768676758, "[TT] Distance to M2 of the Primary Reflector = 1587.998 mm"]
-[9.136932373046875, 7.471321105957031, "[TT] Imaging Resolution of the Satellogic = 30-meter"]
-[10.800305366516113, -0.24075600504875183, "[FF] Usage of the GHOST = Routinely to support many missions (GRACE, CHAMP, TerraSAR-X, TanDEM-X, PROBA-2)"]
-[5.900577545166016, 4.543084621429443, "[TT] Flight Hardware Provider of the LRI = STI (SpaceTech GmbH)"]
-[8.640583038330078, 3.730140209197998, "[TT] Function of the Instrument Package = Measure the total solar irradiance"]
-[6.438972473144531, 4.589686870574951, "[FF] Project Role of the USA = Guidance & Navigation Systems, Communications"]
-[3.55100154876709, 4.857362270355225, "[TT] Ground Segment Operation of the RISAT-1 = SAR payload operations"]
-[5.069135665893555, 0.5894260406494141, "[FF] Launch Date of the Dnepr Rocket = June 19, 2014"]
-[5.128697872161865, 8.415815353393555, "[TT] Bandwidth (MHz) of the PMI = 300"]
-[7.009030818939209, 5.307685375213623, "[FF] Units of the MWHS-II = Antenna and receiver unit, power supply unit and electronic unit"]
-[6.880745887756348, 6.323305606842041, "[TT] Number of the ADCs = 5"]
-[8.516012191772461, 2.2815001010894775, "[TT] Wind Profiling of the Aeolus = Yes"]
-[3.8120200634002686, 1.2364144325256348, "[FF] Landing Platform of the Autonomous Spaceport Drone Ship = Falcon-9 rocket first stage"]
-[4.957744121551514, 3.0780036449432373, "[TT] Manufacturer of the ION CubeSat Carrier = D-Orbit"]
-[8.959442138671875, 5.403202533721924, "[TT] Perceived Angular Offset of the GOMX-3 = 0.69\u00ba"]
-[5.00248384475708, 1.3771963119506836, "[TT] Data Release Date of the MIRAS = End of March 2010"]
-[5.358716011047363, 0.0927259624004364, "[TT] Retirement Year of the Space Shuttle = 2010"]
-[8.82420539855957, 3.04258131980896, "[FF] Duration of the Transient Luminous Events = Less than a millisecond to two seconds"]
-[10.810700416564941, 3.5080859661102295, "[TT] Size of the CubeLCT = 0.3 U CubeSat"]
-[4.279084205627441, 2.5770342350006104, "[TT] Launch Site of the EMIT = Kennedy Space Center in Florida"]
-[3.2392477989196777, 5.103032112121582, "[TT] Antenna Beamwidth (Elevation) of the Seasat SAR sensor = 6.2\u00ba"]
-[8.436661720275879, 2.000234842300415, "[FF] Effect of the Space Traffic = Controls the year-to-year variability of mid-latitude noctilucent clouds"]
-[5.932435512542725, 1.6090362071990967, "[FF] Presentation Date of the Quasi Zenith Satellite Bus System = June 1-8, 2008"]
-[8.12900161743164, 5.727900981903076, "[FF] Function of the Photometers = Measure the effects of erosion from quartz windows and re-deposition of material onto nearby optics"]
-[14.606849670410156, 6.642983436584473, "[TT] Battery Capacity of the TUBSAT-N = 5 Ah"]
-[13.508488655090332, 5.587253570556641, "[TT] Solar Panels of the EPS = 3"]
-[4.353411674499512, 0.9500789046287537, "[TT] Launch Date of the ARGOS = Feb. 23, 1999"]
-[9.338258743286133, 7.178732872009277, "[TT] HMDA Window Size of the MEIDEX = 40 cm"]
-[8.315911293029785, 3.7077114582061768, "[FF] Cal_solar data Collection of the OCO-2 = Absolute and Relative Instrument Response Calibration"]
-[9.10058307647705, 0.5117372274398804, "[TT] Injection Velocity Shortfall of the ARTEMIS = About 500 m/s"]
-[9.8040132522583, -0.26244139671325684, "[TT] Freezing Level Height of the GPM = Above 3 km"]
-[10.120777130126953, 1.6565461158752441, "[TT] Number of Sources in Six Months of the eROSITA = 1 million"]
-[10.145026206970215, -2.7534735202789307, "[TT] Maximum Operating Frequency of the NAND-Flash = 40 MHz"]
-[9.194334030151367, -0.39818018674850464, "[TT] Apogee and Perigee Attitudes of the Ariane 5 = 249 x 45,234 km"]
-[5.0656890869140625, 0.6129116415977478, "[TT] Launch Date of the COWVR = 21 December 2021"]
-[9.086174011230469, 7.545970916748047, "[TT] Spatial Resolution of the EOS-T = 0.3 m in its panchromatic band and 1.2 m in its multispectral bands"]
-[14.185718536376953, 3.351323127746582, "[TT] Module mass of the SDR-SMM = 1.15 kg"]
-[5.678049564361572, 6.3899126052856445, "[TT] Capacity of the ERS-1 onboard data recorder = 6.5 Gbit"]
-[6.127984046936035, 0.8053056001663208, "[TT] Image Capture Date of the CaSSIS camera = 13 June 2021"]
-[9.174141883850098, 5.235208511352539, "[TT] Attitude Determination of the Spacecraft = 10 arcsec"]
-[13.32065486907959, 7.665018558502197, "[TT] Peak Transmit Power of the Radar = 500 W"]
-[8.294965744018555, 2.9213645458221436, "[FF] Mission Goal of the TEMPO = Monitor major air pollutants from geostationary orbit across the North American continent hourly during daytime"]
-[9.06839656829834, 2.794903516769409, "[FF] Prioritized Science Goals of the ACE = 1. Discover the nature and consequences of the changes in the space environment in this unusual solar cycle; 2. Determine where and how energetic particle populations are accelerated; 3. Determine the spatial variations of particles and field in the inner heliosphere with multi-spacecraft studies; 4. Develop new space weather warnings using L1 data"]
-[4.773752212524414, 7.32570743560791, "[TT] Data Dumping Capacity of the X-band transmitter = 6 to 14 Gbit/ pass"]
-[6.01992654800415, 2.700486898422241, "[FF] Mission Focus of the WorldView Legion = Vehicle navigation, Environmental sustainability, Global connectivity, Disaster response, National security"]
-[8.025583267211914, -0.9858490824699402, "[FF] Data Used for Digital Elevation Model of the ICESat-2 = ICESat-2 data"]
-[9.53459358215332, 7.20184850692749, "[TT] Spatial Resolution of the Optical Arrangement = 250 m, 500 m, and at 1 km at nadir"]
-[6.333674430847168, 1.7800289392471313, "[TT] Development Location of the eROSITA = MPE"]
-[12.070296287536621, 4.660696506500244, "[TT] Size of the Spacecraft = 100 mm x 100 mm x 243 mm"]
-[10.064892768859863, 2.29671573638916, "[FF] Detection Capability of the NuSTAR = Hypothesized nanoflares"]
-[3.5186359882354736, 5.322497844696045, "[TT] Data Rate of the SAR = 739 Mbit/s (single pol.) 1478 Mbit/s (dual pol.) 556 Mbit/s (single pol.) 1112 Mbit/s (dual pol.) 564 Mbit/s 142 Mbit/s (single pol.) 284 Mbit/s (dual pol.)"]
-[5.583858966827393, 1.0121363401412964, "[TT] Start Time of the High-voltage experiment = 16:52 on Nov. 28, 2012 (UT)"]
-[3.0214812755584717, 2.097926616668701, "[TT] Image Credit of the Copernicus Sentinel-3 = ESA"]
-[5.419660568237305, 7.876219272613525, "[TT] Power Amplifier of the Ka-band = 2.2 W"]
-[5.871399402618408, -2.2632360458374023, "[TT] Orbit Inclination of the KOMPSAT-3 = 98.1\u00b0"]
-[4.477647304534912, 3.147224187850952, "[TT] Science Operations Center Location of the PROBA-3 = Belgium"]
-[6.8650078773498535, 7.472763538360596, "[TT] ADC Resolution of the RADFET Circuit = 10 bit"]
-[5.258016586303711, 2.471437454223633, "[TT] Earth environmental observation satellite of the ADEOS-II = Japanese (JAXA, formerly NASDA)"]
-[-4.064741134643555, 4.482382297515869, "[FF] Support Phase Time Period of the Mango Tango = from 09.09 onwards"]
-[12.156682968139648, 3.0163538455963135, "[TT] Propellant of the Propulsion subsystem = Monopropellant hydrazine (78 kg)"]
-[9.046722412109375, 5.234048843383789, "[TT] Quantity of the Inertial reference unit (IRU) = 1"]
-[13.551412582397461, 5.884331703186035, "[TT] Power of the Deployable sun-tracking solar array = 2.2 kW"]
-[6.012717247009277, 5.733625411987305, "[TT] FPGA of the ACU = Xilinx XC4VFX12-10FFG668I (Virtex4)"]
-[9.835968971252441, 6.3151702880859375, "[TT] Rotation Plane of the Precision Scene Select Mirror = 45\u00ba"]
-[10.567920684814453, 4.186901092529297, "[TT] Formation Retarget of the FF mission = -30\u00ba to +30\u00ba"]
-[7.779360771179199, 7.097987174987793, "[TT] Optical System of the PS2 = Five element"]
-[7.692768096923828, 6.427803039550781, "[TT] Scanner Modes of the TOMS = Five"]
-[7.258851051330566, 6.239944934844971, "[TT] Quantity of the CCDs = 16"]
-[4.481723785400391, 3.010110855102539, "[TT] Ground Station Location of the SAC-D/Aquarius = Cordoba, Argentina"]
-[6.934844493865967, 6.987677574157715, "[TT] Spare Units of the Laser Transmitter = One"]
-[9.328903198242188, 3.242262840270996, "[FF] Imaging Requirement of the NIRCam coronagraph = 0.6 arcsec (4\u03bb/D) of the star at \u03bb = 4.6 \u03bcm and to within 0.3 arcsec at \u03bb = 2.1 \u03bcm"]
-[2.883131265640259, 4.524825572967529, "[TT] Radio Wave Length of the PALSAR-2 = L-band"]
-[9.268402099609375, 5.885881423950195, "[TT] Calibration Points of the SSMIS = Hot and cold load"]
-[6.330239295959473, 3.6167690753936768, "[FF] Mission of the SET = Study how to better protect satellites in space"]
-[14.20928955078125, 3.1684651374816895, "[TT] Mass of the CION = 1.5 kg"]
-[4.752405166625977, 5.776004314422607, "[TT] Observables of the Receiver = L1CA, L1P & L2P code phase, L1CA & L2P carrier phase, Instantaneous Doppler, Time measurements"]
-[5.381036758422852, 4.968388080596924, "[FF] Activation of the Emergency Locator Transmitter (ELT) = Automatic after a crash"]
-[7.2646965980529785, 8.068349838256836, "[TT] Dynamic range of the Channel = approx. 4-340 K"]
-[8.105484962463379, 0.6935070753097534, "[TT] Measurement Type of the GRACE-FO = Groundwater Storage and Root Zone Soil Moisture"]
-[3.3423407077789307, 2.1327781677246094, "[TT] Launch Location of the Copernicus Sentinel-6 Michael Freilich = Vandenberg Air Force Base in California"]
-[7.902215480804443, 7.1324262619018555, "[TT] Number of the Arcing Detection Circuits = 2 (three redundant)"]
-[6.847479820251465, 5.132692337036133, "[TT] Components of the AP (Avionics Package) = Data acquisition and control electronics, power conditioning systems"]
-[6.87352180480957, -0.6618643999099731, "[TT] Orbit Period of the JAWSAT = 100.36 min"]
-[8.952346801757812, 4.5982465744018555, "[FF] Attitude Determination of the ALSAT-2B = Three gyroscopes and a star tracker"]
-[14.273117065429688, 3.0865941047668457, "[TT] Mass of the ALSAT-1B = 103 kg"]
-[7.051752090454102, 2.250985860824585, "[TT] Structure Integration and Builder of the Biomass = Airbus in the UK"]
-[6.474799156188965, 3.98996901512146, "[FF] URL of the Space Cube 2 = http://spacewire.computing.dundee.ac.uk/.../takahashi.pdf"]
-[3.686099052429199, 5.026134967803955, "[TT] Imaging Frequency Band of the IceEye-1 = X"]
-[8.383780479431152, 6.846731185913086, "[TT] Instrument Type of the SkySat Constellation = High resolution optical imagers"]
-[7.753437042236328, 6.532254219055176, "[TT] Form Factor of the Scanning Radiometer = 1U"]
-[6.366674423217773, 4.5511980056762695, "[FF] Operation of the Faraday-NICE = Remote-controlled"]
-[11.962903022766113, 6.912456035614014, "[TT] Amplified Output Energy of the LOM = > 1.8 mJ"]
-[10.671662330627441, 4.3489813804626465, "[TT] Panel Deployment of the DSAT-2 = Cross Shape"]
-[9.787069320678711, -0.5253263115882874, "[TT] Orbit Altitude of the NMS = 300-400 km"]
-[5.111709117889404, 2.104151725769043, "[TT] Mission Type of the Tatiana-2 = EO"]
-[8.141925811767578, 2.4888415336608887, "[FF] Function of the Multibeam Thermal-Infrared Instrument = Measure vertically-resolved cloud movements when clouds are present, measure the ocean surface temperature when clouds are not present"]
-[8.56002426147461, 8.759588241577148, "[TT] Observation Capabilities of the Herschel = Far-infrared imaging"]
-[6.163650035858154, 2.2891838550567627, "[TT] Principal Investigator of the ALICE = Alan Stern"]
-[5.0441131591796875, 5.213446617126465, "[TT] Limited Use Duration of the GPS Monarch receiver (GPSDR) = Approximately the first 16 months in orbit or through January 1994"]
-[6.272488117218018, 0.7204720973968506, "[TT] Release Date of the Gaia EDR3 = 3 December 2020"]
-[13.178223609924316, 7.35880184173584, "[TT] Power Consumption of the OBIS = 32 W"]
-[10.178674697875977, 9.357921600341797, "[TT] Nominal IGFOV of the Band 6 = 2 km"]
-[8.664423942565918, 4.717391490936279, "[TT] Observation Types of the TanSat = Nadir observations, sun-glint observations, and target observations"]
-[5.478604316711426, 3.899729013442993, "[FF] Number of Satellites in Orbit of the Satellogic = 60+"]
-[3.4450080394744873, 6.443040370941162, "[TT] Antenna Size of the KaRIn = 5 m x 0.25 m"]
-[3.815082550048828, 4.566062927246094, "[FF] Purpose of the Radar System = Calculate the performance of the radar systems and create simulated radar images"]
-[5.27597713470459, 1.2858636379241943, "[FF] Conference Date of the OMI = Oct. 14-17, 2008"]
-[5.3598432540893555, 8.741838455200195, "[TT] Bandwidth of the Band 6 = 0.481 \u00b5m (30 cm -1)"]
-[7.859743595123291, 3.12937068939209, "[FF] XCO2 Concentration of the TanSat = Varies"]
-[4.859684944152832, 0.3005818724632263, "[TT] Launch Date of the SPOT-7 = Late 2013"]
-[4.81062650680542, -1.8556307554244995, "[FF] Lunar Penetrating Radar (LPR) of the Chang\u2019e-4 Rover = Payload"]
-[10.078289031982422, -1.5669159889221191, "[TT] Inclination of the TRACE spacecraft = 97.8\u00ba"]
-[5.146791458129883, 8.455094337463379, "[TT] Bandwidth (MHz) of the PMI = 500"]
-[5.569023609161377, 2.666569232940674, "[TT] Total Budget of the ESA Space19+ ministerial conference = \u20ac14.5 billion for ESA for the next three years"]
-[7.817006587982178, 6.762392520904541, "[TT] Baseline Requirement of the Interferometric Mode = 17 days"]
-[9.523212432861328, 8.382216453552246, "[TT] Focal Length of the Long Wavelength Band = 12.5 cm (f/2.2)"]
-[7.587376117706299, 5.4300856590271, "[FF] Components of the ERA = Two end effectors, two wrists, two limbs, one elbow joint, electronics, and cameras"]
-[4.5927324295043945, 1.4145151376724243, "[TT] In-Orbit Operations End Date of the Alphasat = 7 December 2020"]
-[6.823740005493164, -0.5614097118377686, "[TT] Orbital Repeat Time of the OrbView-2 = 16 days"]
-[7.697059154510498, 6.561800956726074, "[TT] Image Processing Time of the SMOS = Less than a second"]
-[6.319528102874756, 0.1408720463514328, "[TT] Crew Capacity of the Shenzhou-11 = 2"]
-[7.633042335510254, 1.8149445056915283, "[TT] Coral Bleaching of the Fatu Huku Island = Observed"]
-[3.282909393310547, 4.871747970581055, "[TT] Days of data collection of the SAR = 48.0"]
-[4.909287929534912, 0.0988464504480362, "[FF] Launch Date of the SpaceX CRS 14 = 16 Jan. 2018"]
-[13.398028373718262, 7.4628705978393555, "[TT] Output Power of the HiSPiCO = 27 dBm"]
-[11.758336067199707, 3.477736234664917, "[TT] Thrust Level Increase of the IES = 25%"]
-[9.099798202514648, 5.524411678314209, "[TT] Maximum Pointing Adjustment Time of the ACS = < 2 minutes"]
-[7.809070110321045, 5.833751201629639, "[TT] Head Switch-over Time of the STOs and STAEs = 3 s"]
-[9.316009521484375, 10.74073314666748, "[TT] Polarization of the ICI-7 = V"]
-[8.819303512573242, 3.438995838165283, "[FF] Purpose of the TPS = Infer local plasma density and electron temperature determination"]
-[10.410859107971191, 5.716562747955322, "[TT] Structure Temperature of the Crew Capsule = ~ 150\u00baC"]
-[10.291765213012695, 5.821873188018799, "[TT] Qualification Temperatures of the AEISS telescope = -15\u00baC ~ +55\u00baC"]
-[10.497488975524902, 3.3245837688446045, "[TT] Satellite Type of the LEMUR-2 constellation = 3U CubeSats"]
-[7.0602641105651855, 8.255407333374023, "[TT] SNR Linearity of the SCATSat-1 = Even at SNRs as low as -45 dB"]
-[5.908055305480957, 0.6091097593307495, "[FF] Data Collection of the AMS = Many more years"]
-[9.28724479675293, 3.2420103549957275, "[TT] Duration of the Coronagraph Science Operations = About 4.5 months"]
-[4.9674811363220215, 0.31521177291870117, "[TT] Launch Date of the Odin = 20 Feb 2001"]
-[7.845842361450195, 5.982012748718262, "[FF] Image and Video Capture of the DoT-1 = Managed by Raspberry PI Camera"]
-[5.332642555236816, 0.9591789245605469, "[FF] Technical Commissioning Completion Date of the SPOT 6 = January 2013"]
-[7.589748859405518, 8.849396705627441, "[TT] Frequency Band of the Biomass = P-band"]
-[11.475793838500977, 4.948896884918213, "[TT] Linewidth of the LOM = < 5 pm"]
-[7.523324489593506, 5.272409439086914, "[FF] Transmission Profile of the PF2 = Unknown"]
-[7.554206848144531, 5.649947166442871, "[FF] URL of the LIDAR = http://www.hou.usra.edu/meetings/lpsc2015/pdf/1863.pdf"]
-[6.971521854400635, -0.4212181866168976, "[TT] Orbits per Day of the TecSAR = 15.22"]
-[6.757788181304932, -0.6376565098762512, "[TT] Orbit Period of the CBERS-4A = 97.3 minutes"]
-[14.35873794555664, 3.3069076538085938, "[TT] Mass of the SDS-4 = ~ 48 kg"]
-[8.895912170410156, 7.440751552581787, "[TT] Side-viewing Capability of the CCD Pushbroom Camera = \u00b132\u00ba"]
-[9.547415733337402, 5.013105869293213, "[TT] Rotation Rate of the Satellite = Less than 1\u00ba/s"]
-[7.767953872680664, 5.3213958740234375, "[FF] System Overview of the Microwave Radiometer (MWR) = Unknown"]
-[11.234851837158203, 5.058348655700684, "[TT] Subaperture Radius of the SMART = 0.8 to 0.2 mm"]
-[13.600130081176758, 5.881738185882568, "[TT] Average Power of the Silicon Solar Arrays = 12.3 W"]
-[7.492035388946533, 4.351335525512695, "[FF] Ability of the THEMIS = Orbit Adjustment"]
-[6.680023670196533, 5.094668865203857, "[FF] Components of the Ground Segment = Laptop computer, radio/RF unit, antenna rotator and antennas"]
-[14.288841247558594, 3.1591408252716064, "[TT] Mass of the ITASat-1 = ~8kg"]
-[12.07262897491455, 6.326876640319824, "[FF] Positron Fraction of the AMS = Unknown"]
-[8.094541549682617, 7.408751010894775, "[TT] Components of the HISUI = A multispectral sensor (MSS) and a hyperspectral sensor (HSS)"]
-[4.843070030212402, 8.537264823913574, "[TT] Center Frequency of the Channel 2 = 1695.7250 MHz"]
-[7.72943639755249, 5.817843914031982, "[FF] Data Processing Method of the TanDEM-X = Special algorithms that first evaluate each image individually and then combines them to form a global map"]
-[10.621773719787598, 5.507470607757568, "[TT] Design of the Thermal Subsystem = Largely passive solution using MLI (Multi-Layered Insulation) and surface coatings"]
-[6.226470947265625, 1.2215036153793335, "[FF] Conference Presentation Date of the SJ-9 Technology Demonstration Satellite = Oct. 1-5, 2012"]
-[9.1973295211792, 2.962993860244751, "[TT] Proposed Rate of Change of the Delta in Solar Phase of Apsides = 3.6\u00ba/ year"]
-[7.755805969238281, 2.0061213970184326, "[FF] Mediating Percentage of the Photosynthesis = 90% of carbon and water fluxes in the coupled biosphere-atmosphere system"]
-[7.980118751525879, 8.519950866699219, "[TT] Spectral Range (IR) of the VHRR = 10.5 - 12.5 \u00b5m"]
-[12.424968719482422, 0.6319790482521057, "[FF] Quantum Efficiency of the PLATO detectors = Highest over a broad wavelength range"]
-[5.185201168060303, 2.591562032699585, "[TT] Processing Location of the OSIRIS = University of Saskatchewan, Saskatoon, Canada"]
-[8.409687995910645, -0.2176515907049179, "[TT] Area of the Lake Eyre = 9,300 km2 (3,600 square miles)"]
-[10.176580429077148, 5.915299415588379, "[TT] UV Data of the Swift = Temperature dropped by about 50%, from around 71,500 to 35,500 degrees Fahrenheit (40,000 to 20,000 \u00ba Celsius)"]
-[6.21030330657959, 0.042353998869657516, "[TT] Operation Expectation of the FormoSat-2 = Next decade"]
-[9.34153938293457, -0.6147446632385254, "[TT] Orbit of the CICERO-4 = 500 km orbit"]
-[5.319575786590576, 2.461003303527832, "[FF] Name Origin of the Hoinga = Bad H\u00f6nningen am Rhein"]
-[9.60533618927002, 8.220925331115723, "[TT] Field of View of the CAPI = Wide"]
-[6.841092586517334, 3.131235122680664, "[FF] Commercial Weather Data Program of the NOAA = Operational"]
-[6.683131694793701, -1.8007973432540894, "[FF] Partners of the Jason-2 = NASA, CNES, NOAA, EUMETSAT"]
-[8.016799926757812, 8.636030197143555, "[TT] Spectral Range of the VNIS = VIS/NIR (0.45\u20130.95 \u00b5m), shortwave IR (0.9\u20132.4 \u00b5m)"]
-[4.430962562561035, 6.3260416984558105, "[FF] Parameter of the Antenna Subsystem = Value"]
-[9.805624961853027, 7.342545509338379, "[TT] Ground Sampling Distance of the Satellite = < 7 km(N/S) at Seoul GSD area"]
-[4.578780174255371, 3.014441967010498, "[TT] Location of the MOC = ESOC (Darmstadt, Germany)"]
-[3.4392971992492676, 6.372839450836182, "[TT] Size of the Active Antenna = 2 m x 2 m"]
-[13.716463088989258, 5.313750267028809, "[TT] Dimensions of the GaAs cells = 2cm x 4 cm"]
-[5.05824613571167, 1.352249264717102, "[FF] Workshop Date of the GIOVE-B = October 13, 2008"]
-[9.058699607849121, 2.799696683883667, "[FF] Purpose of the X-Ray Flux Monitor = Better space weather forecasts"]
-[7.223077774047852, 2.4898135662078857, "[FF] Purpose of the TRISHNA = Increasing understanding of ecosystem stress and water use, coastal and inland waters, urban microclimate monitoring, solid earth, the cryosphere, and the atmosphere"]
-[8.203178405761719, -0.4715242385864258, "[TT] Annual Minimum of the Antarctic sea ice = 2.6 million km2"]
-[8.109516143798828, 5.282966613769531, "[FF] Calibration Resolution of the Satellite Device = 1.3 k"]
-[9.44900131225586, 1.057723879814148, "[TT] Movement of the SAA = Slow-moving"]
-[7.932587623596191, 2.141951560974121, "[FF] Unknown of the Ocean Color and Temperature Scanner (OCTS) = Unknown"]
-[11.264418601989746, 5.345239639282227, "[TT] Scintillation Module Size of the Natalya-2M = 4.5 cm x 8 cm x 36 cm"]
-[14.556855201721191, 6.626218318939209, "[TT] Battery Capacity of the Spacecraft = 5.3 Ah"]
-[10.503486633300781, 6.630886077880859, "[TT] Number of Nested Mirror Shells of the Mirror System = 28"]
-[5.290628433227539, 0.6060518622398376, "[FF] Date of the Dnepr Cluster Mission 2013 = Nov. 21, 2013"]
-[12.063899040222168, 4.575394153594971, "[TT] Size of the Coronagraph Spacecraft = 985 mm x 1440 mm x 1238 mm"]
-[9.166815757751465, 8.262726783752441, "[FF] Segmentation of the LET = Central bull\u2019s-eye surrounded by a wide annular region"]
-[5.345305442810059, 3.9775547981262207, "[TT] Number of Satellites of the EarthDaily Constellation = 10"]
-[7.571406841278076, 4.268303871154785, "[FF] Test Location of the AMS-02 = CERN"]
-[10.313896179199219, 5.686746597290039, "[TT] Thermal Operating Range of the DORIS = -10-50\u00baC"]
-[7.929369926452637, 3.0366714000701904, "[TT] CO2 Measurement Accuracy of the CAPI instrument = 1 to 4 ppm"]
-[8.060650825500488, 7.4554948806762695, "[TT] SNR of the Imager = 6"]
-[9.760957717895508, 2.366393566131592, "[FF] Size of the NuSTAR = Small"]
-[13.185630798339844, 2.946336030960083, "[TT] Weight of the CubeSats = 14 kg"]
-[7.6865034103393555, 8.71320629119873, "[TT] Spectral Bands of the MSI = 13"]
-[9.24264907836914, 7.267390251159668, "[TT] Geometric Factor of the Particle Detector = 0.0085 cm 2  sr"]
-[9.254416465759277, 1.8554484844207764, "[TT] Use of the Harpoon = In space"]
-[11.76668930053711, 4.572078227996826, "[TT] Diameter at Launch of the Genesis-2 = 1.9 m"]
-[7.996497631072998, 1.3932827711105347, "[FF] Rainfall Accumulation Observation Period of the GPM = May 27 to June 5, 2020"]
-[6.510950088500977, 2.812323570251465, "[TT] Latitude of the Legion Constellation = 36\u00baN"]
-[5.42642068862915, 6.511317253112793, "[TT] SSMM Capacity of the PAZ spacecraft = 256 Gbit EOL"]
-[5.006533145904541, 3.284829616546631, "[TT] Owner of the RADARSAT-2 = Maxar Technologies Ltd."]
-[13.524446487426758, 2.8371164798736572, "[TT] Dry Mass of the G\u00f6kt\u00fcrk-1A = 1,060 kg"]
-[9.526864051818848, 8.176775932312012, "[TT] Field-of-View of the PanCam WAC = 37\u00b0 x 37\u00b0"]
-[8.960615158081055, 5.7080464363098145, "[FF] Measurement of the HGA = HGA gain"]
-[4.04225492477417, 2.2124369144439697, "[FF] Type of the General Dynamics Atlas E = Liquid-propellant intercontinental ballistic missile"]
-[5.436122894287109, 6.828433036804199, "[TT] Data Loss Tolerance of the EDSN = Accepts data packet loss"]
-[9.762760162353516, -0.5677650570869446, "[TT] Orbit Altitude of the Genesis-2 = 560 km"]
-[7.997906684875488, -2.5704832077026367, "[FF] Materials for Photo-Electron Current Measurement of the HORYU-4 = Gold, KaptonR (polyimide), and Black KaptonR"]
-[13.938207626342773, 7.162719249725342, "[TT] Current of the Voltage 4 = 250"]
-[6.9203691482543945, 1.475691556930542, "[FF] First Image Release Date of the Webb Telescope = 12 July 2022"]
-[5.561182975769043, 2.640904664993286, "[FF] Researchers of the SMART = Ben-Gurion University (BGU) researchers"]
-[6.800524711608887, 5.999856472015381, "[TT] Primary Modes of the Mode Manager = Safe and Nominal"]
-[4.9274773597717285, 1.0736632347106934, "[TT] Launch Date of the OPTOS = Nov. 21, 2013"]
-[6.400073051452637, -0.4710041582584381, "[TT] Ability to Revisit of the ZY-3A = 4-5 days"]
-[6.010652542114258, 5.745688438415527, "[FF] Qualification Status of the Virtex-4 FPGA = Not space-qualified in Europe"]
-[8.088894844055176, 7.058087348937988, "[TT] Technology of the Advanced Instrument Controller (AIC) = 0.35 micron, 3.3 V CMOS"]
-[3.2712202072143555, 5.052903175354004, "[TT] SAR Measurements Grid Resolution of the L2SMA = 3 km EASE-2"]
-[7.560444355010986, 3.1602728366851807, "[FF] Contents of the Level-3 = Spatially and temporally averaged data of geophysical parameters"]
-[9.12986946105957, 2.9069230556488037, "[FF] Predictability of the Solar Energetic Particles = Extraordinarily hard to predict"]
-[4.589860916137695, 1.4983731508255005, "[TT] Launch Date of the GOSAT-2 = October 2018"]
-[13.52491569519043, 6.938742637634277, "[TT] Source of the Miniaturized power supply = Indigenous"]
-[9.408431053161621, 7.204061985015869, "[TT] Spatial Resolution of the AWiFS sensor = 56 m"]
-[9.691822052001953, 7.718641757965088, "[TT] Frame Size of the SV-24 imager = 30 km2"]
-[3.9614675045013428, 2.153651714324951, "[TT] Launch Vehicle of the OrbView-2 = Pegasus XL rocket"]
-[7.621407508850098, 9.243141174316406, "[TT] Band 6 Wavelength of the OCM = From 670 nm to 620 nm"]
-[10.30905818939209, 5.734155178070068, "[TT] Operating Temperature of the SXS = 50 mK"]
-[5.000920295715332, 3.627612590789795, "[FF] Manufacturer of the TIR detector = TNO, SSTL"]
-[6.0108442306518555, -0.6836102604866028, "[TT] Expected Lifetime of the RADARSAT-2 = 7.25 years"]
-[10.547016143798828, 1.8546773195266724, "[FF] Purpose of the NICER XTI = Observations of neutron stars with high time resolution"]
-[8.737123489379883, 8.847344398498535, "[TT] Groove Density of the Convex Holographic Grating = 1450 grooves/mm"]
-[7.261626720428467, 1.9348125457763672, "[TT] Pointing Capability of the Carbonite-1 = \u00b145\u00ba"]
-[6.32017183303833, -1.354069709777832, "[TT] Launch Year of the GRACE-FO = May 2018"]
-[7.731767177581787, 5.437893867492676, "[FF] Data Collection of the DMS = Thousands of high-resolution photographs during a single flight"]
-[6.274693489074707, 3.953301429748535, "[FF] Mission Objective of the PROBA = Address issues of on-board operational autonomy"]
-[8.343542098999023, 2.7791450023651123, "[FF] Objectives of the AMSU-A = Atmospheric temperature profile measurements from the surface up to about 50 km in 15 channels"]
-[13.663067817687988, 6.885946750640869, "[TT] Power of the EPS Panels = 23 W"]
-[5.360077381134033, 6.289180755615234, "[TT] Microprocessor Clock Speed of the RCM3400 = 29.4 MHz"]
-[7.9211883544921875, 5.305822849273682, "[TT] Use Case of the FLLS = Monitoring the structural distortion before, during, and after deployment"]
-[6.427241802215576, 7.2062087059021, "[TT] Signal Output of the AEM = 2 signals"]
-[9.059380531311035, 8.017805099487305, "[TT] CCD Line Pixel Pitch of the Focal Plane Module = 6.5 \u00b5m"]
-[5.290501594543457, 3.395282745361328, "[FF] Manufacturer of the European Robotic Arm = Unknown"]
-[5.061564922332764, 1.273971676826477, "[TT] Launch Date of the Himawari-8 = October 7, 2014"]
-[7.856788158416748, 6.949985980987549, "[TT] Total Number of Shutters of the NIRSpec = Almost a quarter of a million"]
-[5.255117416381836, 6.888575553894043, "[TT] Download Rate of the Satellite = 100 Mbit/s"]
-[5.470882415771484, 3.232102155685425, "[FF] Cost Savings of the Maxar = $60 million"]
-[12.783208847045898, 7.466531276702881, "[TT] Power of the IMG = 150 W"]
-[3.4530537128448486, -0.8955265879631042, "[TT] Orbit Type of the UniSat-3 = Sun-synchronous orbit"]
-[6.417534351348877, 5.9463911056518555, "[FF] Data Integration of the CDE = Over several days"]
-[6.645266532897949, 6.14271354675293, "[TT] Number of Configurations of the SIM = 13"]
-[8.059768676757812, 5.066255569458008, "[FF] Calibration Method of the On Board Calibrator = Flat fielding"]
-[5.547534942626953, 6.573709011077881, "[TT] Data Volume Requirement of the HyperScout = 1.5 MB"]
-[4.834150791168213, 3.3456871509552, "[TT] Manufacturer of the SPOT 7 = Astrium"]
-[11.242903709411621, 4.65294075012207, "[TT] Inflation System of the DSAT-1 = High torsion springs"]
-[8.170329093933105, 7.7223663330078125, "[FF] Uncertainty Upgrade in Radiometric Performance of the Multi-Spectral Imager (MSI) = ~0.5% (k=1)"]
-[4.597530841827393, 1.5661277770996094, "[FF] Launch Date of the GHGSat-D = Early 2023"]
-[5.183925628662109, 3.3559188842773438, "[FF] PLM structural engineering of the RUAG Space Switzerland = Responsible"]
-[13.39020824432373, 5.481861591339111, "[TT] Solar Array Paddle of the ALOS = One"]
-[9.486189842224121, 4.788684844970703, "[TT] Attitude Control Computers of the GNB = 2 ARM7"]
-[11.125088691711426, 4.782039642333984, "[TT] Length of the Tether = 32 m"]
-[13.356119155883789, 2.9108710289001465, "[TT] Mass of the QSat-EOS = 49 kg"]
-[9.222419738769531, 2.765048027038574, "[FF] Objective of the RHESSI = Obtain high fidelity color movies of solar flares in X-rays and gamma rays"]
-[7.665954113006592, 2.9846537113189697, "[TT] Measurement Goal for Methane of the GOSAT-2 = 5 ppb"]
-[6.621769905090332, 1.8900904655456543, "[FF] URL of the SEXTANT = http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20150001327.pdf"]
-[9.732460021972656, -0.23174531757831573, "[TT] Elevation of the Camp I = 5,700 m"]
-[4.608999729156494, 4.7753472328186035, "[TT] Support Program of the Maritime AI-NAV = Navigation Innovation and Support Program (NAVISP)"]
-[5.103679180145264, 1.3414876461029053, "[FF] Conference Date of the GIOVE-B = May 3-6, 2009"]
-[13.216689109802246, 7.260234355926514, "[TT] Power Consumption of the FIBOS = ~ 1.5 W"]
-[14.245607376098633, 3.1678011417388916, "[TT] Mass of the BLITS = 7.53 kg"]
-[3.3225021362304688, 5.7448930740356445, "[TT] Panel Quantity of the SAR Antenna = 32 slotted waveguides"]
-[7.873452663421631, 1.8369741439819336, "[FF] Harmful Effects of the Wildfire Smoke = Degrade air quality, cause breathing and lung problems, contribute to heart disease and cancer"]
-[6.451213836669922, 5.249069690704346, "[FF] Function of the TTC Processor = Process TTC signals"]
-[5.494080066680908, 0.6781648993492126, "[FF] PDR Date of the NuSTAR = June 9-10, 2009"]
-[14.255074501037598, 3.1995460987091064, "[TT] Mass of the WPM = 263 kg"]
-[8.318231582641602, 7.353673458099365, "[TT] Provider of the IR-Camera = DLR-OS"]
-[5.310912132263184, 1.2740830183029175, "[FF] Launch Date of the ORBCOMM = Oct. 8, 2012"]
-[5.217581272125244, 0.7193817496299744, "[FF] Launch Date of the CALIPSO = Unknown"]
-[11.894208908081055, 6.490176677703857, "[FF] Energy Deposition of the RAMIS = Minimal ionizing protons up to relativistic iron nuclei"]
-[5.088000297546387, 3.6239876747131348, "[TT] Manufacturer of the GPS/MET = Allen Osborne Associates Inc."]
-[12.873854637145996, 7.538157939910889, "[TT] Power of the Total Instrument = 350 W"]
-[8.368435859680176, 3.1167500019073486, "[FF] Function of the POAM-II = Provide a measurement of the vertical distribution of atmospheric ozone, nitrogen dioxide, aerosol extinction, water vapour and temperature"]
-[5.5234904289245605, 6.002223491668701, "[TT] Flash Memory of the C&DH subsystem = 512 kB"]
-[8.677935600280762, 6.9145636558532715, "[TT] Image of the Wide Multi-Look Fine Mode = Single-pol (HH, VV, HV or VH)"]
-[8.027371406555176, 5.288913726806641, "[TT] Algorithm Version of the MWR = v2.0"]
-[8.178630828857422, -0.7488110661506653, "[FF] Emphasis of the Sea Ice Geophysical Measurements = Ice Motion"]
-[5.2818379402160645, 0.305620938539505, "[TT] Backup Laser Activation Date of the CALIPSO = March 12, 2009"]
-[8.79624080657959, 3.2671144008636475, "[FF] Flux of the Small Near-Earth Objects = Unknown"]
-[9.682875633239746, 0.32761165499687195, "[TT] Relative Distance Range of the PROBA-3 = 25 to 250 m"]
-[2.4094252586364746, 2.795386552810669, "[TT] PI of the HEPP = R. McIntosh, NASA/GSFC"]
-[7.46323823928833, 4.312230110168457, "[FF] Sensor Complement of the SLATS = Unknown"]
-[7.944717884063721, 8.136757850646973, "[TT] Sensor Provider of the Near-Infrared Spectroscopy and Photometry Instrument (NISP) = NASA"]
-[8.079913139343262, 8.79334545135498, "[TT] Spectral Range of the SOLSE-2 = 275 - 425 nm"]
-[7.294937610626221, 8.211291313171387, "[FF] SNR of the GOSAT-2 = b1: >200 (45/0.158)"]
-[5.223483562469482, 6.753019332885742, "[TT] Mission Data Downlink of the Spacecraft bus = 120 Mbit/s"]
-[4.891778469085693, 3.3278768062591553, "[TT] Manufacturer of the OBC = EADS Astrium SAS"]
-[6.590640068054199, 2.9036881923675537, "[FF] Mission Prime of the Weather System Follow-on \u2013 Microwave (WSF-M) = Ball Aerospace"]
-[4.3232879638671875, 4.831902027130127, "[TT] Width of the Vessel detection optimized beam mode = 450 km"]
-[6.742999076843262, 1.0225790739059448, "[TT] Collaboration Date of the Solar Orbiter = March 2012"]
-[4.978850841522217, 3.020653247833252, "[TT] Manufacturer of the Eutelsat Quantum = Airbus Defence and Space and Surrey Satellite Technology Limited"]
-[11.178292274475098, 5.975146770477295, "[TT] Material of the Titanium mandrel = Titanium"]
-[6.767783164978027, 4.9357523918151855, "[FF] Interfaces of the OBC = Power, telemetry\u2013telecommand (TM\u2013TC; RF), sensors, heaters, thrusters, reaction wheels"]
-[8.696471214294434, 0.5998673439025879, "[TT] Magnitude of the Tohoku-Kanto earthquake = 9.0"]
-[13.32961368560791, 7.794647216796875, "[TT] Power of the S-band Transmitter = 1 W"]
-[10.256324768066406, 5.744313716888428, "[TT] Temperature of the CCD Cooling = -20\u00b0C"]
-[7.864358425140381, -0.38472482562065125, "[FF] Purpose of the Radar systems = Study ice layers and Antarctica\u2019s bedrock"]
-[6.7157487869262695, 3.6924288272857666, "[TT] Pressure Vessel Cover of the CM (Crew Module) = Tiles"]
-[6.015366554260254, 5.196658611297607, "[FF] Data Access of the Airbus Satellite = Near real-time"]
-[4.373946189880371, 7.802395343780518, "[TT] Band Frequency of the Starlink = 10.7 GHz to 12.7 GHz"]
-[12.27973461151123, 6.938624858856201, "[TT] Energy Range for Si of the LEICA = 0.33 - 5.5 9.6 - 177 21 - 330 54 - 195 MeV/n"]
-[3.4634642601013184, -0.9241239428520203, "[TT] Orbit Type of the Main Payload = Sun-synchronous near-circular orbit"]
-[8.447319030761719, 6.216631889343262, "[TT] Cross Section Per Unit Area of the CCR = Maximum at 1.1 inches"]
-[9.92453384399414, 4.453799724578857, "[TT] Actuators of the Coarse ADCS = Magnetotorquers"]
-[7.126111030578613, 5.506577968597412, "[FF] Beam Pointing Direction of the LCT = Not specified"]
-[10.31087875366211, 2.174009084701538, "[FF] Source of the X-rays of the Juno = By Juno"]
-[7.965548515319824, 0.22817468643188477, "[FF] Parameter Measurement of the GRACE-FO = Movement of water based on variations of Earth\u2019s gravity field"]
-[2.293941020965576, 2.7728030681610107, "[TT] Co-PI of the EPI-Lo = Mihir Desai"]
-[8.282198905944824, 6.844256401062012, "[TT] Spectrometer Type of the The Rossi Explorer = Timing"]
-[11.686419486999512, 3.4314515590667725, "[FF] Design of the Resistojets = Simple design consisting of a resistive wire wound round a mandrel"]
-[9.72648811340332, 8.235746383666992, "[TT] Field of View of the EPIC Cameras = 30 arcmin"]
-[9.582046508789062, 8.12674617767334, "[TT] Field of View of the CERES = \u00b178\u00b0"]
-[4.936309337615967, 8.135153770446777, "[FF] Centre Frequencies of the Instrument = 6.925 GHz, 10.65 GHz, 18.7 GHz, 23.8 GHz, 36.5 GHz, 50.3 GHz, 52.8 GHz, 89.0A GHz, 89.0B GHz"]
-[8.677474021911621, 2.0285511016845703, "[TT] Accuracy of the Wind Speed Measurements = 2 m/s"]
-[3.779069423675537, 6.3311991691589355, "[TT] Antenna Systems Quantity of the DRS = 4"]
-[3.944247245788574, 5.506607532501221, "[TT] NESZ of the Radar = -29 dB"]
-[3.1573398113250732, 2.2971835136413574, "[FF] Data Measurement of the Sentinel-6 = Ocean Heat, Movement, Sea Level"]
-[12.441770553588867, 0.6009883284568787, "[TT] Measurement Interval of the PLATO CCDs = Every 2.5 seconds"]
-[5.796477794647217, 3.789073944091797, "[FF] Number of Satellites of the Sateliot IoT nanosatellite constellation = At least 250"]
-[8.011082649230957, 8.338586807250977, "[FF] Type of the Medium Wave Infra Red Telescope = Medium Wave Infra Red"]
-[9.493611335754395, 7.072159290313721, "[TT] Value of the Spatial Resolution = 8.4 x 4.4 km"]
-[5.44478178024292, 6.407046318054199, "[TT] Onboard Storage of the Kanopus-V 1 = 24 GB"]
-[13.397754669189453, 7.330394268035889, "[TT] Power of the SCDE = 2 W"]
-[12.165698051452637, 4.500796318054199, "[TT] Structure Dimensions of the DSP satellites = 2.1 m diameter and 1.23 m in height"]
-[14.158820152282715, 3.1644628047943115, "[TT] Mass of the IOF = 12 kg"]
-[11.424309730529785, 3.284864664077759, "[TT] Propulsion System Type of the Lunar Flashlight 6U CubeSat = \u201cgreen\u201d monopropellant"]
-[8.13934326171875, -1.0932163000106812, "[FF] Melt Pond Detection of the ICESat-2 = Automatic"]
-[6.355969429016113, 4.372081756591797, "[FF] Functions of the Ground Segment = Mission planning, sequence generation, station scheduling, spacecraft analysis, orbit determination, trajectory analysis and planning, maneuver design, instruments analysis, time correlation, data capture and distribution, science data gap reporting, generation of products for science support"]
-[10.189245223999023, -1.36922287940979, "[TT] Orbit Inclination of the Polar Scout 6U CubeSat = ~98\u00ba"]
-[6.914250373840332, 1.9699583053588867, "[FF] URL of the Tunneling Horizon Detector = http://micromachine.stanford.edu/projects/tunneling_sensors/THD/THDSummary.html"]
-[10.200278282165527, 4.056555271148682, "[TT] Booms of the Spacecraft = Two 12.5 m booms in the axial plane for electric field sensors"]
-[8.994733810424805, 5.705146312713623, "[TT] Bias Error of the NSTT = < 6 and 4 arcsec (3\u03c3)"]
-[10.709857940673828, 7.480937957763672, "[FF] Field of Regard of the Narrow-swath (stripmap mode) = 500 km"]
-[10.002135276794434, 8.045066833496094, "[TT] Type of the DMAC = Medium Aperture"]
-[6.643597602844238, 0.9909448623657227, "[TT] Data Availability of the Landsat 1-5 = All MSS data January 2009"]
-[5.288917064666748, 3.8981804847717285, "[TT] Number of Satellites of the GIOVE = 2"]
-[9.46409797668457, 0.6629071831703186, "[TT] Total Travel Distance of the BepiColombo = Nine billion kilometers"]
-[8.202424049377441, 6.897945404052734, "[TT] Number of Images of the POLO data set = Over 1000"]
-[5.493081092834473, 0.6937657594680786, "[FF] Launch Date of the FormoSat-5 = Unknown"]
-[8.1280517578125, 8.251744270324707, "[TT] Radiance Channels of the Sounder = 18 IR and one visible"]
-[14.276309967041016, 3.2247252464294434, "[TT] Mass of the ILAS = < 138 kg"]
-[9.749702453613281, 3.9765279293060303, "[TT] Height of the Magnetic Bottle-like Structure = Nearly 20,000 kilometers"]
-[14.243309020996094, 3.0118088722229004, "[TT] Mass of the UniSat-1 = 12 kg"]
-[7.042906761169434, 8.146286964416504, "[FF] Signal-to-Noise Ratio of the SNR = \u2265 64"]
-[8.229949951171875, 1.1834577322006226, "[TT] Range of Values of the Soil moisture = 0 - 60%"]
-[13.03095817565918, 4.957566738128662, "[TT] Main Body Volume of the Solar Orbiter = 2 m3"]
-[9.936888694763184, -1.2471448183059692, "[TT] Location of the IRNSS-1C = 83\u00baE"]
-[5.003069877624512, 8.336774826049805, "[TT] Frequency Range of the MWRI = 10.65-89 GHz"]
-[6.941212177276611, 4.459163188934326, "[FF] Deployment Process of the iROSA = Install the electrical cables and drive the final two bolts"]
-[6.29080057144165, 1.8443608283996582, "[FF] URL of the eROSITA = http://www.mpe.mpg.de/6686210/news-20170120"]
-[9.052759170532227, 0.5020313858985901, "[TT] Orbit Type of the ARTEMIS Probes = Lissajous orbit near the Earth-Moon Lagrange points"]
-[4.981814861297607, 7.431030750274658, "[TT] Data Rate of the XMOD = 800 Mbit/s"]
-[4.844166278839111, 3.3678054809570312, "[TT] Predecessor Organization of the DLR = DFVLR"]
-[8.767626762390137, 4.817432880401611, "[TT] Range of the Star sensor = 14.4\u00ba x 19.2\u00ba"]
-[7.166969299316406, 0.30617332458496094, "[FF] Mission Preparation Date of the REX-J = June 5-12, 2011"]
-[8.566998481750488, 2.382965326309204, "[FF] Purpose of the Aeolus = Measure wind from space"]
-[9.751903533935547, -0.5046482086181641, "[TT] Final Altitude of the SAC-D = 657 km"]
-[9.792966842651367, 5.668912887573242, "[TT] Tilt of the M4 = 100 \u00b5rad"]
-[5.1558051109313965, 8.273295402526855, "[TT] Window Channels of the SSM/I = 19.4, 22.2, 37.0, 85.5 GHz"]
-[6.6663818359375, 3.7929415702819824, "[FF] Operation Start of the Experiment = Launch"]
-[7.84696626663208, 5.24359130859375, "[TT] Micro Vibration Test of the Instrument = Successful"]
-[5.4607954025268555, 5.413461208343506, "[FF] Interface Type of the GS PD element = High availability, low latency distribution channel"]
-[5.1367363929748535, -0.5872462391853333, "[FF] CDR Completion Date of the TARANIS = April 2013"]
-[9.779366493225098, 4.745999813079834, "[TT] Stabilization of the Spacecraft = Spin-stabilized (100 rpm)"]
-[4.929138660430908, 0.355563223361969, "[TT] Date of the LPVEx = September and October 2010"]
-[5.354398250579834, 0.7720757722854614, "[FF] Launch Date of the SmallGEO = Jan. 28, 2017"]
-[10.942203521728516, 7.535353183746338, "[TT] Swath of the MSU-E = 45 km"]
-[7.406611442565918, 2.6426315307617188, "[FF] Regulatory Body for Satellite Light Pollution of the United States = None"]
-[4.855295658111572, 4.522494316101074, "[TT] Receiver Sensitivity of the Argos System = Increased"]
-[3.3715157508850098, 1.4585187435150146, "[TT] Launch Date of the Sentinel-2B = March 6"]
-[5.222456455230713, 3.196176052093506, "[TT] Development Company of the LunIR = Lockheed Martin Space Systems Company"]
-[8.685102462768555, 8.45495319366455, "[TT] Spectral Passband of the Miniature High-Resolution Imaging Spectrometer = 1600-1700 nm"]
-[8.20008373260498, -1.0190167427062988, "[TT] Snow Depth Measurement of the ICESat-2 = Up to 27 cm"]
-[11.38159465789795, 8.909396171569824, "[FF] Image Acquisition Date of the MODIS = Unknown"]
-[5.85033655166626, 6.114241123199463, "[FF] Data Storage of the TDI = TDI chain"]
-[7.124772548675537, -0.23191779851913452, "[TT] Number of Orbits of the Kolibri-2000 = 711"]
-[10.297657012939453, 2.350243091583252, "[FF] X-ray Range of the DAXSS = Soft X-rays"]
-[11.70364761352539, 0.1432531476020813, "[TT] Number of Planets Discovered of the TESS = 21"]
-[3.9436652660369873, 6.871343612670898, "[TT] PRF of the Altimeter Antenna = 4200 Hz (Ku), 1220 Hz (C)"]
-[5.658990859985352, 2.7302093505859375, "[TT] Funding Source of the ELFIN = AFRL (Air Force Research Laboratory)"]
-[7.5891432762146, -0.241190567612648, "[FF] Article Date of the Nav Canada = March 8, 2010"]
-[5.110016822814941, 0.166431725025177, "[FF] Installation Date of the Cygnus = 14 Nov. 2017"]
-[13.715272903442383, 3.0801656246185303, "[TT] Payload Mass of the SmallGEO = Up to 300 kg"]
-[7.084632873535156, 3.7487454414367676, "[FF] Formation Flying of the Proba-3 = Yes"]
-[3.573986291885376, -0.9291839599609375, "[TT] Orbit of the GRACE-FO satellites = Co-planar polar orbit"]
-[12.13393497467041, 4.560947895050049, "[TT] Bus Size of the Spacecraft = 1300 mm x 1310 mm x 1988 mm"]
-[9.568469047546387, 4.961711883544922, "[TT] Stability of the AOCS = 2 arcmin/s about the Z-axis"]
-[4.727738380432129, 1.5798792839050293, "[FF] Program Overview of the GCOM-Al = Not provided"]
-[9.873236656188965, 5.253608703613281, "[FF] N-S Stepping Time of the Mirror = Integer multiple of the filter wheel rotational period (200 ms)"]
-[4.831044673919678, 8.568593978881836, "[TT] Center Frequency of the Channel 8 = 52.80 GHz"]
-[1.746712327003479, -2.0746209621429443, "[TT] Departure Date of the Hayabusa2 = 13 November 2019"]
-[7.774920463562012, 8.342228889465332, "[TT] Number of Pan bands of the FPA = 2"]
-[10.058357238769531, -1.5483635663986206, "[TT] Inclination of the SARAL spacecraft = 98.538\u00ba"]
-[5.7246809005737305, 4.661314010620117, "[FF] Purpose of the Inter-satellite Links = Routinely cross-check their performance and reduce their dependency on the availability of ground installations"]
-[9.166439056396484, 7.003724098205566, "[TT] Imagery Resolution of the DMC-3 Constellation = 1.0 m GSD Pan and 3 m MS data"]
-[9.102807998657227, 5.731926441192627, "[TT] Pointing accuracy of the DST 35 = 2 arcmin"]
-[8.580538749694824, 6.034993648529053, "[TT] Absolute Accuracy of the OVM = 0.5 nT"]
-[11.99462890625, 3.2568652629852295, "[FF] Operation of the Iodine BIT-3 propulsion unit = Produces iodine vapor via sublimation"]
-[4.228195667266846, 4.311594486236572, "[TT] Ground Segment Communication of the RISAT-1 = Various mission computers and associated mission software and communication links"]
-[4.338796615600586, 2.9589524269104004, "[FF] Locations of the PDHS = Frascati (Ka-band), Kiruna, Sweden (X-band), Svalbard"]
-[7.116714954376221, 7.171432018280029, "[TT] Pulse Energy of the LOM = 200 \u00b5J"]
-[10.748126029968262, 3.455071449279785, "[TT] CubeSat Size of the RadCube = 3U"]
-[9.410341262817383, 7.045156002044678, "[TT] Spatial Resolution of the MSC = 5.8 m"]
-[8.254190444946289, 5.853332042694092, "[FF] Digitization Accuracy of the Experiment = \u00b1 0.14 nT"]
-[8.375787734985352, 8.532479286193848, "[TT] Spectral Resolution of the MSASI = 80,000 (\u03bb/\u0394\u03bb)"]
-[5.355681896209717, 0.8391841053962708, "[FF] Release Date of the XXL Survey = Dec. 15, 2015"]
-[4.462308883666992, 3.0907504558563232, "[TT] Location of the GEOLUT = Bangalore"]
-[8.218802452087402, 7.4265570640563965, "[TT] Function of the Photo MOSFET Switch = Probe cleaning"]
-[8.002366065979004, 2.4537901878356934, "[FF] Photo and Measurement Activities of the Beresheet = Landing Site"]
-[3.463355541229248, 1.7318501472473145, "[FF] Conference Presentation Date of the Sentinel-1 = June 7-10, 2010"]
-[8.080592155456543, 8.094645500183105, "[TT] Band of the Camera = MWIR (Midwave Infrared)"]
-[6.811077117919922, 0.5157636404037476, "[TT] Anticipated Fuel Depletion of the Kepler = Soon"]
-[10.726080894470215, 1.0020886659622192, "[TT] Mass of the GJ 367 b = Half the mass of Earth"]
-[4.748688697814941, -1.838905930519104, "[TT] Launch Date of the Chang'e-4 = December 8, 2018"]
-[10.238059043884277, 3.1113333702087402, "[TT] Quantity of the CubeSat Deployers = 2"]
-[8.203695297241211, 0.06248083338141441, "[FF] Mission Goal of the Philae Lander = Land on the surface of a comet and transmit data from the surface about the comet's composition"]
-[10.915806770324707, 10.087738037109375, "[FF] Observation Date of the Alpha Magnetic Spectrometer = 11 January 2018"]
-[3.840161085128784, 6.281911373138428, "[TT] Number of Antennas of the Antenna Subsystem = At least 9"]
-[6.69036865234375, 4.8144097328186035, "[FF] Data Access of the Vision-1 = Free basis to a range of stakeholders"]
-[10.85726261138916, -0.29162412881851196, "[FF] Acquisition Timeline of the TanDEM-X = Not provided"]
-[6.656500339508057, 6.426177501678467, "[TT] Data Processing Time of the PDS = Within 3 hours after sensing"]
-[4.727694511413574, -0.04386063665151596, "[TT] End of Life Date of the KySat-2 = 28 February 2014"]
-[4.424012184143066, 7.597369194030762, "[TT] Frequency of the IMI antenna = L/S/C"]
-[10.886743545532227, 7.541159152984619, "[TT] Swath Width of the MIVZA = 1500 km"]
-[4.74533224105835, 0.49486297369003296, "[TT] Launch Date of the Tomorrow-R1 and -R2 = April 2023 and June 2023"]
-[1.9356281757354736, -0.40412724018096924, "[TT] Current Status of the Van Allen Probes = Operating in a bridge phase"]
-[4.629052639007568, 4.512392997741699, "[FF] Full Form of the Lemur-2 = Low Earth Multi-Use Receiver-2"]
-[5.719402313232422, 2.834409475326538, "[TT] Funding Allocation of the Brazilian Ministry of Defense = 145 million real"]
-[3.4450860023498535, 6.367794513702393, "[TT] Mesh Size of the Net = 80 mm"]
-[9.376516342163086, 7.398813247680664, "[TT] Panchromatic Band Resolution of the Imager = <1 m GSD (Ground Sample Distance)"]
-[7.367320537567139, 4.476421356201172, "[FF] Unknown of the Sensor System = Unknown"]
-[5.2876458168029785, 2.1533875465393066, "[TT] Mission Type of the CryoSat = EO"]
-[5.515614032745361, 1.0818930864334106, "[FF] Calibration Phase Start Date of the Hitomi = Middle of April"]
-[7.675844669342041, 5.158998489379883, "[FF] Measurement Transformation of the DSX Sensor Suite = Estimates of the flux distribution with respect to the local pitch-angle"]
-[8.84373664855957, 4.498413562774658, "[FF] Navigation System of the New Horizons = Onboard gyros, star trackers and Sun sensors"]
-[5.5472092628479, 0.5312961935997009, "[TT] Science Operations Start Date of the NuSTAR = August 1, 2012"]
-[8.158465385437012, 6.117208957672119, "[TT] Closure Method of the NETCAM = Motor driven winches"]
-[9.049803733825684, 5.45002555847168, "[TT] Cross-Track Direction Body-Pointing Capability of the Kanopus-V 1 = Yes"]
-[5.633427143096924, 3.3696370124816895, "[FF] Operators of the SATis5 = Unknown"]
-[10.840198516845703, 3.969371795654297, "[TT] Semi-Major Axis Adjustment of the CanX-5 = Within Meters of What Was Planned"]
-[5.94330358505249, 0.29874446988105774, "[TT] Launch Date of the Rosetta = March 2, 2004"]
-[4.893900394439697, 3.3871755599975586, "[TT] Manufacturer of the MAC-200 = Bristol Aerospace"]
-[4.603442668914795, 7.357247829437256, "[TT] Uplink Receivers of the UoSAT-12 = 5"]
-[7.675735950469971, -2.5326762199401855, "[TT] Power Off Time of the GOLD instrument = Jan. 28, 7:40 p.m. EST"]
-[5.8461151123046875, 2.70296311378479, "[TT] Organizations of the CBERS program = INPE (National Institute for Space Research) and CAST (China Academy of Space Technology)"]
-[5.589196681976318, 0.24709345400333405, "[TT] Launch Date of the KIZUNA = Feb. 23, 2008"]
-[6.986054420471191, 6.946269989013672, "[TT] Configuration of the Laser 2c = 2a, 2b, 2c"]
-[6.902227878570557, 1.9215806722640991, "[FF] Mission URL of the GRACE = https://www.nasa.gov/feature/jpl/wet-winters-may-not-dampen-small-wildfires"]
-[5.566671848297119, 0.8381609916687012, "[FF] Clone Date of the Satellite Vu\u2019s original satellite = July 21, 2022"]
-[7.104036808013916, 8.338314056396484, "[TT] SNR in bands 1 and 2, in band 3 of the Scanning geometry = \u2265 200, \u2265 100"]
-[8.922001838684082, 6.468861103057861, "[FF] Image Content of the CaSSIS = Light-toned bedrock"]
-[5.105993270874023, 7.207591533660889, "[TT] Data Rates of the Fairchild RF = 0.125 to 1024 kByte/s"]
-[18.797748565673828, 3.4818835258483887, "[TT] \u0394r (m) of the Kirkuk = 10.0"]
-[4.0964226722717285, 7.027528285980225, "[TT] Frequency Band of the X-band patch antenna = X-band"]
-[10.099145889282227, 2.5656795501708984, "[TT] Altitude of the NanoRacks-QB50 CubeSats = ~ 400 km"]
-[3.7320423126220703, 4.610763072967529, "[TT] Imaging of the RADARSAT-2 = High-resolution radar imaging"]
-[9.729043960571289, 8.42818832397461, "[TT] FOV of the WTS1 and WTS2 = 15\u00ba"]
-[4.990168571472168, 0.5631077289581299, "[TT] Launch Date of the Dnepr Rocket = Nov. 6, 2014"]
-[6.706570625305176, 3.761103868484497, "[FF] Components of the Pressurized Cargo = UPA Fluids Control and Pump Assembly (FCPA), WFB (WPA Multifiltration Beds), a galley rack to be placed in Unity, and SAFER (Simplified Aid for EVA Rescue)"]
-[4.524316787719727, 5.899746894836426, "[TT] Signal Frequency of the 406 MHz beacons = 406 MHz"]
-[8.453060150146484, 8.322351455688477, "[TT] Spectral Resolution (FWHM) of the Instrument = 500 eV at 10 keV, 1.2 keV at 80 keV"]
-[5.236364364624023, 2.21675968170166, "[TT] Current Status of the SwissCube = Good health"]
-[8.610448837280273, 1.0631275177001953, "[TT] Mission Duration of the Aquarius = 2 \u00bd years on orbit"]
-[9.54968547821045, 4.995321750640869, "[TT] Stabilization of the Resurs-P1 = 0.005\u00ba/s"]
-[9.389443397521973, 7.031301975250244, "[TT] Resolution of the COSI = 1 m"]
-[7.344069480895996, 0.3015193045139313, "[FF] Conference Presentation of the OSIRIS-REx = SpaceOps 2014, 13th International Conference on Space Operations, Pasadena, CA, USA, May 5-9, 2014"]
-[6.418781757354736, 1.1613869667053223, "[FF] Update Date of the COSMIC-2 = Nov. 4, 2010"]
-[9.790000915527344, -0.37063145637512207, "[TT] Release Altitude of the Platform = Slightly higher than planned (405 km, versus the 400 km used for the simulations"]
-[7.3929290771484375, 1.5093461275100708, "[TT] Occupation of the Max Valier = Science-fiction writer and an amateur astronomer"]
-[1.3398505449295044, 1.9012540578842163, "[TT] Launch Mass of the HTV-5 = 16,500 kg"]
-[5.595922946929932, 5.609247207641602, "[TT] Type of the UT 699 LEON 3 FT microprocessor = UT 699 LEON 3 FT"]
-[12.406415939331055, 0.6268392205238342, "[FF] Photometry Observation of the PLATO = High-Precision"]
-[7.8578338623046875, -2.47845196723938, "[FF] Imaging of the GOLD = Earth\u2019s upper atmosphere"]
-[7.719303131103516, 6.622402667999268, "[TT] Image Downlink Time of the AgCam/ISSAC = Several hours of powered operations immediately following collection"]
-[4.764755725860596, 0.06335026025772095, "[TT] End of Life Date of the DMC-3 = 10 Oct 2022"]
-[7.836228370666504, 8.164860725402832, "[FF] NDVI NIR Band to Red Band Balance of the R3 System = Off"]
-[10.444869041442871, 4.079376220703125, "[TT] Configuration of the Hypersonic Grid Fins = X-wing"]
-[4.8517255783081055, 0.926127552986145, "[FF] Presentation Date of the TeLEOS-1 = Feb. 11-13, 2015"]
-[4.952419281005859, 4.255667686462402, "[TT] Number of the IC Stations = 39"]
-[4.465274810791016, 7.082828998565674, "[FF] Channel frequencies of the Cross dipole antenna = AIS #1: 161.975 MHz, AIS #2: 162.025 MHz AIS #3: 156.775 MHz, AIS #4: 156.825 MHz"]
-[14.419927597045898, 3.201364040374756, "[TT] Mass of the SIR-2 = 2.3 kg"]
-[5.062310218811035, 3.569132089614868, "[TT] Manufacturer of the CPU Board = BAE Systems"]
-[8.811924934387207, 3.5590763092041016, "[FF] Leading Noise Terms of the Satellite = Magnetic disturbances"]
-[6.336968421936035, 4.534142017364502, "[FF] Components of the C3S = Ground Station (GS) element, Mission Management Center (MMC) element, Data Routing and Retrieval (DRR) element"]
-[13.219510078430176, 5.260119915008545, "[TT] Size of the Deployable sun-tracking solar array = 9.29 m2"]
-[13.236532211303711, 7.193600654602051, "[TT] Maximum Power Consumption of the ROBUSTA picosatellite = 1 W"]
-[6.070686340332031, -1.9556339979171753, "[TT] Member of the Andrew Dessler = True"]
-[14.692914009094238, 6.676368713378906, "[TT] Capacity of the Batteries = 18 Ah"]
-[13.516595840454102, 7.3301167488098145, "[TT] Electrical Power of the CanX-2 = 5 W"]
-[9.026342391967773, 4.72507381439209, "[TT] Pointing Mode of the TanSat = Solar Panel Pointing"]
-[4.386175155639648, 7.594044208526611, "[TT] Frequency of the S-band = 2.45 GHz"]
-[7.999271869659424, 8.380763053894043, "[TT] Infrared Type of the GIIRS = MWIR (Mid-Wave Infrared)/TIR (Thermal Infrared)"]
-[7.507004737854004, 3.4463396072387695, "[FF] Task of the Night Cities = Identify Points in Night Images and Match Them to Positions on Maps"]
-[10.25772762298584, 3.251915454864502, "[TT] Spectrometer Frequency of the MicroMAS-2 CubeSat = Near 183 GHz"]
-[4.354989051818848, 0.12690788507461548, "[FF] Beta Test of the Starlink = Ongoing"]
-[9.551149368286133, 7.062777042388916, "[TT] Spatial resolution of the Microwave System = 19-260 km"]
-[7.53706693649292, 5.655622482299805, "[FF] Affiliation of the LiDAR camera = Suisse d'Electronique et de Microtechnique SA - Recherche et Development (CSEM), Switzerland"]
-[8.516559600830078, 8.185307502746582, "[TT] Pixels of the VNIR FPA = 31,152-15,576"]
-[4.406219959259033, 6.926098823547363, "[FF] Capability of the LRO Mini-RF Transmitter = Dual-band"]
-[9.46766185760498, 0.8710851669311523, "[TT] Closest Approach to Sun's Surface in 2021 of the Solar Orbiter = More than 20 million km"]
-[3.4550092220306396, -0.9267120957374573, "[TT] Orbit Type of the FY-3D = Sun-synchronous near-circular orbit"]
-[5.388942718505859, 3.9893455505371094, "[TT] Number of Indian Meteorological Satellites of the INSAT-3D = Three"]
-[6.229462623596191, 1.4883406162261963, "[FF] URL of the Swarm = http://pcwww.liv.ac.uk/~holme/RAS/haagmans.pdf"]
-[3.4905779361724854, 6.451084613800049, "[TT] Dimensions of the VDES Antenna = 62 x 62 x 73 cm"]
-[10.1353120803833, 7.083249568939209, "[TT] Frame Size of the NIUSAT = 50 km x 50 km"]
-[7.0690507888793945, 1.2839702367782593, "[TT] Switched Off Date of the Spitzer Space Telescope = 2020"]
-[8.279629707336426, -0.4528539478778839, "[TT] Uncertainty of the Sea Ice Concentration (SIC) = <5%"]
-[9.948859214782715, -0.5040942430496216, "[TT] Orbit Altitude of the SEOSat = 670 km"]
-[5.292943000793457, 2.897071361541748, "[TT] Developer of the Unicorn-2D = Alba Orbital UG (Germany)"]
-[8.153060913085938, 8.753355979919434, "[TT] Wavelength Range of the EUVS = 5 - 127 nm"]
-[7.143218040466309, 7.416448593139648, "[FF] Data Densities of the MABEL = 0.9 and 0.8 signal photons per 70 cm"]
-[9.300880432128906, 2.7900197505950928, "[TT] Solar Wind Speed and Beta of the ACE = ~55% lower on average from 2009 through the day 79 of 2013"]
-[7.9679412841796875, 2.91296124458313, "[FF] Pseudo-sounding Capability of the AMI = Provides atmospheric instability information"]
-[4.675569534301758, 7.207437992095947, "[TT] Data Transmission Rate of the X-band data transmission = 15.36, 30.72, 61.44, or 122.88 Mbit/s"]
-[5.5358123779296875, 5.581801414489746, "[TT] Microprocessor Core of the Chang'e-4 = LEON2-FT"]
-[11.831448554992676, 0.01247911062091589, "[FF] First Planets of the TESS = Unknown"]
-[7.428892135620117, 2.8910183906555176, "[FF] Purpose of the MethaneSAT = Fill critical data and observes gaps between point source and global mapping satellites"]
-[9.299039840698242, 4.565873146057129, "[FF] Attitude Control of the SEOSat = Three-axis stabilised with a gyroless Attitude and Orbit Control Subsystem (AOCS), star sensor, magnetometers, four reaction wheels"]
-[9.985489845275879, 7.791563987731934, "[TT] Celestial Sphere Coverage of the Telescope = 30% for > 197 days"]
-[4.597546100616455, 7.8897199630737305, "[TT] Frequency of the UHF Transceiver = 437.365MHz"]
-[7.631426811218262, -2.3926618099212646, "[TT] Data Dissemination Responsibility of the GOLD Instrument = UCF (University of Central Florida)"]
-[9.625563621520996, 4.995992660522461, "[TT] Pointing Stability of the AOCS = 10 \u00b5rad (N/S and E/W) peak to peak over 8 s period"]
-[13.969940185546875, 7.1436309814453125, "[TT] Flight Module Output of the C&DH Subsystem = +5 and +3.3 V"]
-[8.795328140258789, 3.657496690750122, "[FF] Measurement Objective of the Potential = Measure neutral and charged particles in the ionosphere"]
-[14.195202827453613, 2.9962594509124756, "[TT] Mass of the Deimos-1 = ~ 96 kg"]
-[5.599245071411133, 6.5010762214660645, "[TT] Data Usage for Near-Realtime Applications of the SMOS = Around 5 TB per year"]
-[9.575050354003906, 8.215001106262207, "[TT] Field of View of the EIC = \u00b18.5\u00ba"]
-[10.606764793395996, 5.5756306648254395, "[TT] Temperature of the Accelerated-Ion Interaction Region of the RHESSI = Above 105 K"]
-[8.783677101135254, 7.187027454376221, "[TT] GSD of the SLIM6 Line Scan Imager = 32 m"]
-[9.735655784606934, -0.5720183849334717, "[TT] Orbit Altitude of the OLS = 833 km"]
-[5.03319787979126, 2.3603768348693848, "[FF] Mission Type of the TUBSAT = EO"]
-[10.139758110046387, 8.200252532958984, "[TT] Configuration of the Aperture Stop = Deployed"]
-[6.238771438598633, 8.081281661987305, "[TT] Analog Channels of the EPH = Three"]
-[7.874924182891846, -2.4920759201049805, "[FF] Measurement of the GOLD = Changes in the chemical composition of the thermosphere during the total solar eclipse of July 2, 2019"]
-[8.041947364807129, 2.137516736984253, "[FF] Application of the FY-3 (FengYun-3) = Atmosphere"]
-[12.730154037475586, 3.9036340713500977, "[FF] Purpose of the CuPID = Identify under what conditions reconnection is spatially extended versus continuous and under what conditions it is bursty versus temporally stable"]
-[4.706408500671387, 7.082989692687988, "[TT] Data Rate of the X-band Downlink = 16.8 Mbit/s"]
-[10.275588035583496, 1.6816978454589844, "[FF] Locations of the Shocks = Universe around stars, supernova remnants, comets, and planets"]
-[5.395010471343994, 0.752153754234314, "[FF] Presentation Date of the Data Volume Increase Solution = May 4-7, 2009"]
-[9.257193565368652, 1.8744040727615356, "[FF] Imaging Capabilities of the HARP-2 = Wide swath, polarization, and multi-angular sampling"]
-[6.298725128173828, 8.08944320678711, "[TT] Auxiliary Channels of the ScaRaB = Channels 1 and 4"]
-[5.026931285858154, 7.0866241455078125, "[FF] Data Rate of the Downlink Communications = 61 Mbit/s to regional data centers, and up to 350 Mbit/s to the central data center"]
-[9.660908699035645, 1.4430687427520752, "[FF] Calibration Methods of the Pleiades Program = Unknown"]
-[5.734483242034912, 2.4447405338287354, "[FF] Team Members of the CIRiS = A. Amparan, A. Ghandour, T. Kampe, P. Kerrigan, J. Necas, D. Piqueira, G. Reavis, R. Rohrschneider, M. Veto, R. Warden"]
-[8.031119346618652, 1.4849363565444946, "[TT] Optimal Ground Condition of the SEIS (Seismic Experiment for Interior Structure) = Level ground without rocks larger than about 1.5 cm"]
-[6.2970662117004395, 1.9013419151306152, "[FF] URL of the IXV = http://esamultimedia.esa.int/multimedia/publications/ixv/offline/download.pdf"]
-[6.524779796600342, 4.7380852699279785, "[FF] Function of the Data Ingestion System = Ingests the raw data into the cloud for processing"]
-[5.60703182220459, 6.074656963348389, "[TT] Computing Power of the SCP = 1 MIPS"]
-[8.408448219299316, 5.520848751068115, "[TT] Standard Deviation of Error (Along-track) of the Geolocation Testing = 0.2-0.4 m"]
-[12.849141120910645, 7.424619674682617, "[TT] Power Consumption of the Field Measurement Device = < 0.5 W"]
-[13.386372566223145, 7.046142578125, "[TT] Reliability of the Electrical Power Subsystem = Exceeding 90%"]
-[11.507184028625488, 4.86710262298584, "[TT] Picosatellite Capacity of the OPAL = 6"]
-[5.378015995025635, 5.581933498382568, "[TT] Interface Type of the MSV = SPA-S (SPA-SpaceWire) compliant"]
-[13.08851432800293, 7.117198467254639, "[TT] Power of the Sun sensors = < 0.1 W"]
-[2.1240742206573486, -0.2760790288448334, "[FF] URL of the Radiation Belt Storm Probes = http://rbsp.jhuapl.edu/index.php"]
-[6.007154941558838, -0.43077728152275085, "[TT] Years of Service of the Admiral Paul F. Zukunft = 41 years"]
-[9.881500244140625, 8.75609016418457, "[TT] FOV Size of the AFS (Adjustable Field Stop) = 100 km"]
-[5.979208946228027, -0.5446469187736511, "[TT] Nominal Mission Duration of the INSPIRE = 3 months"]
-[7.807719707489014, -0.4656679034233093, "[TT] Trend of the Freeze-up = About a week later per decade"]
-[7.7155938148498535, 6.083557605743408, "[FF] Operation of the F-FEE = Operate the CCDs of the two fast cameras"]
-[11.854270935058594, 6.76284646987915, "[TT] Break Energy of the First Broken Powerlaw = 1.2 keV"]
-[13.251296043395996, 5.440512657165527, "[FF] Weight Difference of the X panels = The -X panel side is heavier than the +X panel side"]
-[8.47005558013916, 1.6923370361328125, "[TT] Ideal Ocean Temperature for Sustaining of the Tauktae = Above 27\u00b0 C"]
-[4.899428844451904, 7.931948184967041, "[TT] Clock Frequency of the FPGA = 20 MHz"]
-[6.403113842010498, 4.667475700378418, "[FF] Function of the Sentinel MCS = Monitoring and control of all spacecraft"]
-[5.155493259429932, 0.5921853184700012, "[TT] Establishment Date of the MERSEA = January 2003"]
-[13.467164039611816, 6.822486877441406, "[TT] Power of the ADEOS spacecraft = 4.5 kW"]
-[5.764756202697754, 6.411721229553223, "[TT] Storage Capacity of the GOES-R Access System = Seven days"]
-[4.179736137390137, 4.864911079406738, "[TT] Spatial Acquisition Duration of the Alphasat TDP1 = Reduced from 240 s at the very first tests to 34 s for default links"]
-[4.315014362335205, 7.386510848999023, "[TT] Intersatellite Link Frequency of the Communication = S-band"]
-[6.410655975341797, -0.40255987644195557, "[TT] Forecast Duration of the HWRF = 120 hours"]
-[8.460536003112793, 3.8555984497070312, "[FF] Measurement Type of the Polar-6 = Ground-truth measurements"]
-[4.792172431945801, 7.890578269958496, "[TT] Type of the CITRIS = Tri-frequency"]
-[7.544112682342529, 5.2618279457092285, "[FF] Subsystems of the AMR-2 = ESA (Electronics Structure Assembly) and RSA (Reflector Structure Assembly)"]
-[10.482111930847168, 3.3541228771209717, "[TT] Design of the MicroMAS-2 = 3U CubeSat"]
-[5.482150077819824, 2.631989002227783, "[TT] Number of Members of the OSCAR-QUBE = 15 students"]
-[7.461449146270752, 4.737250328063965, "[FF] Component of the RICH electronics boxes = Unknown"]
-[3.3749797344207764, 6.446296691894531, "[TT] Diameter of the Antenna = 0.65m"]
-[4.412158012390137, -0.019717391580343246, "[FF] Issue of the Starliner = Timing error in the software"]
-[13.52849006652832, 5.820320129394531, "[FF] Solar Array Power of the THEMIS (and ARTEMIS) spacecraft = Barely moved below BOL values"]
-[7.106295108795166, 5.8805365562438965, "[FF] Type of the DSAC = Miniaturized, ultra-precise mercury-ion atomic clock"]
-[7.556831359863281, 3.311971426010132, "[FF] Purpose of the Open Atlas of Night Time Images = Providing open access to night time images for use by the media, public, and scientists"]
-[5.64292049407959, -0.6887176036834717, "[TT] Operational Lifetime of the GOES-R = 10 years"]
-[5.815766334533691, 1.1016901731491089, "[FF] Launch Date of the EarthCARE = 2015"]
-[7.932499408721924, 6.199764728546143, "[FF] Imaging of the PhiSat-1 = Multi-spectral radiometers (vis/IR)"]
-[4.550324440002441, 0.31333842873573303, "[TT] End of Life Date of the HTV-9 = 20 August 2020"]
-[8.423226356506348, 7.816376686096191, "[TT] Number of Subsequent Detections of the LIGO = Two"]
-[10.230917930603027, 0.9684399962425232, "[TT] Distance from Earth of the Kepler-438b = 475 light-years"]
-[4.786261558532715, 4.720181941986084, "[FF] Oscillator Type of the Argos-3 = Stability Oscillator for the Doppler location"]
-[13.981047630310059, 3.3770694732666016, "[TT] Printed Circuit Board Mass of the Sprite = A few grams"]
-[10.535611152648926, 6.834070205688477, "[TT] Largest mirror diameter of the Mirror = 358 mm"]
-[8.896894454956055, -0.34175342321395874, "[TT] Inclination of the Meteor-M-2 = 98.8\u00b0"]
-[7.057638645172119, 3.9329004287719727, "[FF] Unknown of the Extraterrestrial Material = Unknown"]
-[11.556065559387207, 4.066688537597656, "[TT] Size of the AeroCube 11 = 3U"]
-[6.944052219390869, 5.262997150421143, "[FF] Electrical Currents of the Processing Unit = 5 different"]
-[4.506168365478516, -0.8722174763679504, "[FF] Launch Date of the SpaceX CRS-25 Dragon = 24 May 2022"]
-[5.603288650512695, 4.799500942230225, "[TT] Data Relay Station of the MarCO = Madrid, Spain, station of the Deep Space Network"]
-[4.106629371643066, 0.34109896421432495, "[TT] Launch Date of the Corvus = 12 January 2018"]
-[6.443628311157227, 2.338273763656616, "[FF] Formation Flying Demonstration of the PRISMA = Unknown"]
-[4.20932674407959, 6.321078777313232, "[FF] Signal Down-Conversion of the Active Antenna = IF"]
-[6.46530818939209, 5.382740020751953, "[FF] Manufacturer of the Linear Encoder = Not provided"]
-[5.558949947357178, 6.129194736480713, "[FF] Power Consumption of the DSU = Significantly reduced compared to the traditional solid state mass memory solutions"]
-[11.958556175231934, 3.429520606994629, "[TT] Quantity of the Propulsion Tanks = 2"]
-[8.649656295776367, 1.1626086235046387, "[FF] Complement of the Aquarius = Unknown"]
-[6.941896438598633, 4.134220600128174, "[FF] Function of the Formation Flying Manager (FFM) = Plans, coordinates and manages the formation flying activities of the mission in an autonomous way"]
-[9.676203727722168, 2.3629651069641113, "[FF] Unknown of the NuSTAR = Unknown"]
-[11.313570022583008, 0.925309419631958, "[TT] Extended Mission Duration of the LISA Pathfinder = Seven months"]
-[9.63165283203125, 8.133201599121094, "[TT] f/Number of the Custom design lens = f/5"]
-[7.031710624694824, 3.496415138244629, "[FF] URL of the PROBA-3 = http://www.affects-fp7.eu/helcats-meeting/data/workshop_presentations/"]
-[6.243560314178467, 3.9207229614257812, "[FF] Concept Purpose of the Dedicated Satellite Constellation = Exclusive control over a number of satellites over a specific geographical region"]
-[6.28447961807251, -0.31036344170570374, "[TT] Operation Duration of the ALOS = More than four years"]
-[10.95702075958252, 0.6159479022026062, "[TT] Number of Stars Observed of the Kepler = Approximately 1,000"]
-[3.4781126976013184, 5.031122207641602, "[FF] Function of the CSG = Generate configuration and timing information and the beam parameters for conducting the SAR payload operations"]
-[4.244330883026123, 0.7372570037841797, "[TT] Launch Year of the EDRS-C = 2019"]
-[13.386358261108398, 7.645033359527588, "[TT] Power Amplifier of the Navigation Antenna = 50 W"]
-[9.00493049621582, 5.608678817749023, "[TT] Control Error of the AOCS = \u2264 1200 \u00b5rad (3\u03c3) per axis"]
-[10.098742485046387, 8.1762113571167, "[TT] Aperture of the Video Camera = 1.27 cm"]
-[7.816369533538818, 2.1117966175079346, "[FF] Development Partners of the SGR-ReSI = SSTL, University of Surrey, National Oceanographic Centre, University of Bath, Polar Imaging Ltd."]
-[5.7289934158325195, -0.9119328260421753, "[TT] Design Life of the UniSat-1 = One year"]
-[5.575377464294434, 5.630087375640869, "[TT] Processor of the AOCS = MIL-STD 31750"]
-[8.807494163513184, 5.713192462921143, "[FF] Radiometric Stability of the Satellite Sensors = Crucial"]
-[6.280246734619141, 6.720063209533691, "[TT] Maximum Number of Transmission Attempts of the Drifting (Mobile) Platforms = 5 - 6"]
-[5.0048394203186035, 1.7557833194732666, "[TT] Power On Date of the Carmen-2 = June 22, 2008"]
-[4.919346332550049, 0.17444516718387604, "[TT] End of Life Date of the LADEE = April 18, 2014"]
-[8.074831008911133, 6.429219722747803, "[TT] Instrument Type of the DMC-3 = Imaging multi-spectral radiometers (vis/IR)"]
-[14.676498413085938, 6.607781410217285, "[TT] Li-ion Battery Capacity of the PARASOL microsatellite = 15 Ah"]
-[5.483461380004883, 1.5158907175064087, "[FF] Data Management Plan of the Small Explorer (SMEX) = Unknown"]
-[6.728742599487305, 4.521977424621582, "[FF] Telemetry Information of the FDIR = Reconfiguration flags, current configuration flags, failures reported through dedicated event packages"]
-[4.601283550262451, 5.895385265350342, "[TT] Capability of the MEOSAR = Detect UHF signals from emergency beacons"]
-[10.607338905334473, 6.859601020812988, "[TT] Primary Mirror Material of the Optical telescope = Clearceram\u00ae of OHARA, Inc., Japan"]
-[5.054582118988037, 1.9724708795547485, "[TT] Status of the MWR = Operating nominally"]
-[9.119422912597656, -1.2595070600509644, "[TT] Orbit of the TEMPO = Geostationary orbit"]
-[4.413323879241943, 7.113925457000732, "[FF] Function of the Ka-band broadband = Broadband for Africa"]
-[11.114520072937012, 1.2752265930175781, "[FF] Gravitational Wave Spectrum of the LISA = Broad range of astrophysical sources"]
-[9.347616195678711, 5.087176322937012, "[TT] Roll Maneuver Capability of the ADCS = \u00b135\u00ba"]
-[2.923522472381592, 1.9735562801361084, "[TT] Image Capture Date of the Copernicus Sentinel-2 = 24 July"]
-[6.873183250427246, 6.017320156097412, "[TT] Number of Concepts of the ALBus = Three"]
-[6.64711332321167, 7.517252445220947, "[TT] Sub-beams of the Multi-purpose beam mode = 8 (in the HH and HV polarization channels)"]
-[10.505293846130371, 2.7666382789611816, "[TT] Deployment Date of the Kaber Microsatellite Deployer = June 20, 2018"]
-[9.239350318908691, 0.23378972709178925, "[TT] Tower Height (European side) of the Yavuz Sultan Selim Bridge = 322 m"]
-[7.985402584075928, 7.063090801239014, "[TT] Pixels per Scan of the ScaRaB = 51"]
-[7.857968807220459, 3.05873703956604, "[FF] Components of the Dark Skies of ISS = Cities, Stars, Other Objects"]
-[6.21010160446167, 4.052792549133301, "[FF] Purpose of the DSX = Provide an important database for future designers of space missions intended to operate in the MEO environment"]
-[13.746821403503418, 2.8879263401031494, "[TT] Mass of the Spacecraft = ~ 1200 kg"]
-[4.859813690185547, 0.9240709543228149, "[FF] End of Observing Mission of the PROBA-V = June"]
-[6.053746700286865, 0.7058762311935425, "[TT] Lines of Source Code of the ASTERIA FSW = 201,000"]
-[7.700858116149902, 0.8053868412971497, "[FF] Meteoroid Flux of the Lunar impact monitoring = Kilogram-sized"]
-[4.859135627746582, 8.36293888092041, "[TT] Operating Frequencies of the MTVZA-GY = 10.6, 18.7, 23.8, 31.5, 36.7, 42, 48, and 91.65 GHz, 52-57 GHz, 183.31 GHz"]
-[4.496014595031738, 7.490799903869629, "[TT] S-band Downlink Modulation of the UoSAT-12 = BPSK"]
-[8.782099723815918, 3.9798946380615234, "[FF] Function of the MagEIS = Distinguish electrons from high-energy protons in the inner radiation belt"]
-[10.678462982177734, 5.362494468688965, "[TT] Concentration Range of the DN probe = 10^5 - 10^12 cm^-3"]
-[5.057130813598633, 3.290681838989258, "[TT] Manufacturer of the ESA = UCB/SSL"]
-[9.650887489318848, -0.22482910752296448, "[TT] Capsule Drop Altitude of the Hayabusa-2 = About 120 miles (or 200 km) above Earth\u2019s surface"]
-[7.842346668243408, 8.218705177307129, "[FF] Spatial Resolutions of the GOCE = Half-wavelength"]
-[10.712618827819824, 1.0627835988998413, "[TT] Mass of the Kepler-442b = About twice the mass of the Earth"]
-[6.260909080505371, 0.6911305785179138, "[TT] Data Gathering Period of the Gaia = Full nominal mission plus the first 6 months of the mission extension (66 months in total)"]
-[14.220145225524902, 3.071463108062744, "[TT] Mass of the BugSat-1 = 22 kg"]
-[13.726747512817383, 3.053391695022583, "[TT] Payload Module Mass of the Euclid = 800 kg"]
-[6.923644065856934, -1.7695415019989014, "[TT] Wet troposphere of the Jason-2 = 2 cm"]
-[9.535840034484863, 8.217408180236816, "[TT] Field of View of the intensified sprite imager = 20\u00ba x 3.15\u00ba"]
-[7.519641399383545, 3.854078531265259, "[FF] Operational Modes of the NightPod = Manual mode, other operational modes"]
-[7.989872932434082, 4.817881107330322, "[FF] Instrument Heritage of the EPI-Hi = LET (Low Energy Telescope) and HET (High Energy Telescope)"]
-[9.272271156311035, 4.889377593994141, "[FF] Pointing Locations of the SVOM Attitude = Near the equator, areas observable from both Hawaii, Chile and the Canary"]
-[6.861286163330078, 6.438838481903076, "[TT] Ground Station of the LaserCom = Table Mountain facility"]
-[4.208897590637207, 2.6171770095825195, "[TT] Launch Location of the ICESat-2 = Vandenberg Air Force Base in California"]
-[5.941303253173828, 2.5905473232269287, "[FF] Student Collaboration Goal of the IMAP = Contributes to diversifying space science"]
-[11.56700325012207, 4.462827205657959, "[TT] Payload Fairing Technology of the Minotaur = Advanced Grid-Stiffened Composite"]
-[4.228827476501465, 7.159739971160889, "[TT] TT&C Frequency of the RF communications = S-band"]
-[8.884026527404785, 5.574764251708984, "[TT] Stationkeeping Accuracy of the AOCS = \u00b10.5\u00ba in longitude and latitude"]
-[4.620875358581543, 7.508495330810547, "[FF] RF Communications of the HAUSat-2 = UHF, downlink data rate = 9.6 kbit/s VHF uplink data rate = 2.4 kbit/s FSK modulation"]
-[7.766384601593018, 9.148641586303711, "[TT] Wavelength Range of the Spectral band 4 = 10.5 - 12.5 \u00b5m"]
-[7.076766014099121, 2.1216351985931396, "[FF] Calibration of the Landsat-7 ETM+ = On-orbit"]
-[7.964629173278809, 5.357945442199707, "[TT] Measurement Accuracy of the FLLS (Fine Lateral and Longitudinal Sensor) = \u00b120.5 mm (lateral)"]
-[6.94603157043457, 6.959507942199707, "[TT] Quantity of the Laser Transmitter = 1"]
-[9.679207801818848, -0.5795345306396484, "[TT] Altitude of the GEMS = 35786 km"]
-[9.849275588989258, -0.34957391023635864, "[TT] Altitude of the CALIPSO = 705 km"]
-[8.734827995300293, -0.10314000397920609, "[FF] Spatial Resolution of the Chang'e-2 = 7 m ( 100 km altitude) 1.3 m ( 15 km altitude)"]
-[6.248156547546387, 0.9553201794624329, "[FF] First Light Date of the Storm Hunter = 23 May 2018"]
-[9.72065258026123, 6.697615623474121, "[TT] Spatial Resolution of the Earth Radiation Budget Experiment (ERBE) = 20 km at nadir"]
-[5.915894985198975, 1.8754650354385376, "[TT] Launch Date of the Orion MPCV = 5 Dec 2014"]
-[6.356175899505615, 4.627710819244385, "[FF] Function of the Spacecraft Bus = Supply electrical power to the science instruments, orient and stabilize the telescope, store and compress the data from the science instruments for later transmission to Earth, execute the stored commands to carry out the planned observing schedule, and communicate with the ground system"]
-[9.294757843017578, 3.76143741607666, "[FF] Objectives of the S 331 = Measurement of the three components of the DC and ULF magnetic field"]
-[9.881606101989746, 4.883856773376465, "[TT] Antenna Rotation Speed of the SWIM = ~6 rpm"]
-[10.090928077697754, -1.5900520086288452, "[TT] Inclination of the SMDC-ONE = 34.5\u00ba"]
-[9.598896026611328, 7.509617328643799, "[TT] Spectral Range of the Nadir Sensor Wide-Field Telescope = 300-380 nm"]
-[6.699166297912598, 0.8176197409629822, "[FF] Article Date of the Lunar Reconnaissance Orbiter = 11 February 2021"]
-[3.9660112857818604, 6.235622406005859, "[FF] Number of Feeds of the Antenna Device = Too many"]
-[10.659433364868164, -0.3967322111129761, "[TT] Revisit Time of the Tandem-L = 16 days"]
-[10.701786041259766, 7.132306098937988, "[TT] Footprint of the 5 = 25.8 x 17.5 km"]
-[8.963089942932129, 4.288179874420166, "[TT] Developer of the Sun sensor = Shihlin Electric & Engineering Corporation"]
-[11.165727615356445, 5.1728291511535645, "[TT] Formation Size of the MMS = 10 km"]
-[11.819740295410156, 4.845627307891846, "[TT] Dimensions of the MPA = 71 cm x 71 cm x 76 cm"]
-[5.1341753005981445, 0.829300582408905, "[FF] ESA Announcement Date of the Hitomi = July 6, 2016"]
-[6.799412727355957, 5.098299980163574, "[FF] Measurement Type of the GPS Antenna = Vertical measurements"]
-[9.103148460388184, 3.496138334274292, "[FF] Type of the PWI = Plasma Waves Investigation"]
-[7.186653137207031, 7.612454414367676, "[FF] Dynamic Range of the Satellite Device = 3-340 K"]
-[6.31903600692749, -0.012340954504907131, "[TT] Frequency of Issuing Requests for Information of the NASA = About once a year to once every 18 months"]
-[10.275186538696289, 2.176302433013916, "[FF] Imaging of the Chandra X-ray Observatory = Lower-energy X-ray light"]
-[14.217191696166992, 3.220494270324707, "[TT] Mass of the SBUV/TOMS = 20 kg"]
-[3.809281826019287, 6.719470024108887, "[FF] Antenna Type of the Altimetry Instrument = Dual-band C/Ku center-fed antenna"]
-[7.723303318023682, 9.537121772766113, "[TT] Center Wavelength of the B6 = 740 nm"]
-[4.754487991333008, 4.028815269470215, "[TT] Development Organization of the SiREUS = SELEX-GALILEO a Finemeccanica owned company (formerly BAE Systems of Edinburgh)"]
-[5.001374244689941, 3.3370203971862793, "[TT] Manufacturer of the Probe = Mitsubishi"]
-[12.166778564453125, -0.2717624604701996, "[TT] Monitoring Duration of the TESS = 27 days"]
-[14.686232566833496, 6.695011138916016, "[TT] Capacity of the NiCd Battery = 55Ah"]
-[10.354939460754395, 4.488192558288574, "[TT] Reaction Wheels of the NigeriaSat-2 = 4 SSTL Smallwheel 200SP wheels"]
-[8.183094024658203, 1.4336432218551636, "[FF] Rainfall Measurement of the IMERG = Over 310 mm"]
-[5.371420383453369, 5.830794811248779, "[TT] Power to sub-experiments of the STRV-2 DHS = 28 V isolated +5 V, \u00b112 V"]
-[6.662771701812744, -1.9362072944641113, "[FF] Orbit of the JASON-3 = Same as JASON-2"]
-[7.722442150115967, 6.926609992980957, "[TT] Sample Rate of the Cameras = 25 seconds"]
-[5.791850566864014, 4.823583602905273, "[FF] Objective of the PSat-2 = Use a two way communications transponder for relaying remote telemetry, sensor and user data from remote environmental experiments or other data sources back to experimenters via a global network of internet linked volunteer ground stations"]
-[8.16650390625, 3.0757670402526855, "[FF] Scientific Goals of the IME-HF = Identification of possible wave signatures associated with transient luminous phenomena during storms, Characterization of lightning flashes from their HF electromagnetic signatures, Identification of possible HF electromagnetic or/and electrostatic signatures of precipitated and accelerated particles, Determination of characteristic frequencies of the medium using natural waves properties, Global mapping of the natural and artificial waves in the HF frequency range"]
-[7.648258209228516, 4.935360908508301, "[FF] Purpose of the SPS = Understand Dione\u2019s charging environment"]
-[9.559796333312988, 0.6430563926696777, "[TT] Travel Distance Requirement of the Google Lunar X-Prize = 500 meters"]
-[3.1012542247772217, 3.895951747894287, "[TT] Launch Date of the NISAR = 2023"]
-[4.991717338562012, 6.847690105438232, "[TT] Signal Frequency of the AIS Data Receiver = 161.975 MHz, 162.025 MHz, 156.775 MHz, 156.825 MHz"]
-[11.597549438476562, 3.4175267219543457, "[FF] Components of the Electric Propulsion Test Subsystem = Quartz crystal microbalance, Langmuir probe and retarding potential analyzer"]
-[4.117641448974609, 0.179413840174675, "[TT] Next Launch Date of the Falcon 9 = February 5"]
-[7.464106559753418, 2.3878109455108643, "[FF] Operational Mode of the FY-4A = China area: 5000 km x 5000 km, Mesoscale area: 1000 km x 1000 km"]
-[14.2756929397583, 3.2057864665985107, "[TT] Total Mass of the Tsubame = ~ 49 kg"]
-[8.958126068115234, 6.253815650939941, "[TT] Beam Hopping Time of the Antenna = \u2264 10 \u00b5s at SS-TDMA"]
-[4.982609272003174, 8.323821067810059, "[TT] Channel Bands of the AMSU = 50 to 60 GHz, 183.3 GHz"]
-[4.841426849365234, 0.41647544503211975, "[TT] Launch Date of the Spektr-RG = March 2019"]
-[13.033300399780273, 7.136454105377197, "[FF] Power On Command of the SPAN Sensors = Via command from the SPP DPU to the SWEM"]
-[6.409174919128418, 3.5131402015686035, "[FF] Use Cases of the Satellite = Disaster response, event preparation, defense"]
-[13.859796524047852, 5.6664252281188965, "[TT] Efficiency of the Solar Cells = 30%"]
-[8.529838562011719, 4.65755558013916, "[FF] Components of the ADCS = CSS (Coarse Sun Sensor), FSS (Fine Sun Sensor), MAG (Magnetometer), and 2 ST (Star Tracker)"]
-[9.225358963012695, 1.5665801763534546, "[FF] Date of NASA Feature of the Jupiter's Auroras = 6 September 2017"]
-[3.336663007736206, 5.291706562042236, "[TT] Signal Wavelength of the L-band SAR = Around 10 inches (25 cm)"]
-[12.088407516479492, 6.361674785614014, "[TT] Positron Fraction Turnover of the AMS-02 = Beyond 200 GeV"]
-[4.830284118652344, 7.314141750335693, "[TT] Downlink Data Rate of the RF Communications = 4.8 kbit/s"]
-[7.524751663208008, 2.132004499435425, "[TT] Reality of the Marine litter detection = Becoming"]
-[11.028355598449707, 2.905938148498535, "[TT] Wall Thickness of the PSSCT Nanosatellite = 7.5 mm"]
-[4.7589898109436035, 2.1761574745178223, "[TT] Delay Announcement Date of the Quantum = 6 August 2019"]
-[9.68903923034668, 4.001709461212158, "[TT] Magnetic Field Strength Difference of the Oersted = -2400 nT to +1800 nT"]
-[9.705591201782227, 8.506869316101074, "[TT] Antenna FOV of the CXS-810C = 64\u00ba"]
-[4.925004005432129, 3.359602928161621, "[TT] Manufacturer of the IAS (Integrated Avionics System) = SEAKR Engineering Inc."]
-[13.420044898986816, 7.284055709838867, "[TT] Power of the EPDP = 18 W"]
-[8.13915729522705, 8.932998657226562, "[FF] Spot Size of the BIRCHES = Maintains the same spot size regardless of variations in altitude (by up to a factor of 5) or to vary spot size at a given altitude"]
-[6.861321449279785, 5.361688137054443, "[FF] Modules of the TTC Rx = LNA (Low Noise Amplifier), 208F Frequency Synthesiser, 10M7 Phase Detector, Power Supply"]
-[3.833658456802368, 6.492306232452393, "[TT] Antenna Type of the OPAL = 1/4 wavelength monopole"]
-[3.638249397277832, 2.6152729988098145, "[TT] Number of Launches of the Iridium NEXT = 7"]
-[6.436301231384277, 4.939712047576904, "[FF] Function of the STC = Station Computer"]
-[7.392985820770264, 1.0912048816680908, "[TT] Number of Workshops of the SeaSat = 13"]
-[10.075728416442871, 1.50007164478302, "[FF] Authors of the The Global Dynamical Atlas of the Milky Way Mergers = Khyati Malhan, Rodrigo A. Ibata, Sanjib Sharma, Benoit Famaey, Michele Bellazzini, Raymond G. Carlberg, Richard D'Souza, Zhen Yuan, Nicolas F. Martin, and Guillaume F. Thomas"]
-[4.877665042877197, 0.2959888279438019, "[TT] Installation Date of the Cupola = Feb. 2010"]
-[7.08784294128418, 8.339503288269043, "[TT] Number of Channels of the Filter Wheel = LWIR (7 channels), SWIR (6 channels) and the MWIR (5 channels)"]
-[9.119853019714355, 7.557408332824707, "[TT] Spatial Resolution of the WorldView-1 = 2 m MS (Multispectral) data"]
-[3.211979866027832, 5.053499221801758, "[TT] Spatial Resolution (km) of the SAR = 0.025"]
-[6.815221786499023, -0.5435774326324463, "[TT] Orbit File Latency of the EDOT = About 48 hours"]
-[5.798501491546631, 2.7903926372528076, "[TT] Main Outcome of the EMOC = Acquisition plan"]
-[8.054347038269043, 6.517800807952881, "[FF] Capabilities of the Advanced Baseline Imager (ABI) = Significantly Increased"]
-[13.970942497253418, 3.1325106620788574, "[TT] Mass of the KickSat = ~5.5 kg"]
-[6.8526129722595215, 4.73848295211792, "[FF] Update Cycle of the Navigation filter = Allows for the propagation of the state when no measurements are available, while updating the state only when they are available"]
-[3.1891462802886963, 4.568309307098389, "[TT] Type of the PALSAR-2 = Imaging microwave radars"]
-[11.352339744567871, 4.895210266113281, "[TT] Pit Diameter of the Ma'at = More than 100 m"]
-[8.700579643249512, 2.075106382369995, "[FF] Error Requirement of the Wind Speed Retrieval Algorithm = 2 m/s or 10% of the wind speed, whichever is greater"]
-[11.926468849182129, 5.002640724182129, "[TT] Size of the LALT-E = 241 mm x 301 mm x 88 mm"]
-[8.118239402770996, 1.3757522106170654, "[FF] Purpose of the IMERG = Add up the large rainfall totals"]
-[6.350904941558838, -0.4164103865623474, "[TT] Operational Autonomy of the COSMO-SkyMed spacecraft = 24 hours"]
-[12.031572341918945, -0.2316407710313797, "[TT] Data Returned of the TESS = More than 20 terabytes of southern sky data"]
-[11.265277862548828, 0.9609907269477844, "[FF] Journal Publication Date of the LISA Technology Package LTP = 2006"]
-[4.844922065734863, 5.363553047180176, "[TT] Antenna Array of the GPS/Galileo E1/E5a receiver = Two by two"]
-[9.52788257598877, 7.148349285125732, "[TT] Spatial Resolution of the PMI = 4-50 km"]
-[5.779287815093994, 7.736098766326904, "[FF] RFI Mitigation of the MWI = Implemented at the lowest frequency channel"]
-[8.149375915527344, 7.060914516448975, "[FF] Image Types of the Optical System = Panchromatic, multispectral MWIR"]
-[7.959715843200684, 1.08584463596344, "[FF] Purpose of the Irrigation Advisory System = Assess where crops need less or more water"]
-[5.518892765045166, 5.958021640777588, "[TT] Design of the DDMI = Based on the SGR-ReSI design"]
-[9.256353378295898, -1.0632178783416748, "[TT] Orbit Altitude of the EDRS-C = 35,876 km"]
-[6.426126003265381, 4.114649772644043, "[FF] Development Phase of the Avionic Validation Model (AVM) = Phase 1"]
-[6.396971225738525, 2.2147090435028076, "[FF] Image of the ATMS = Figure 9: Danielle Gallegos, ATMS program manager for Northrop Grumman, with the ATMS instrument behind her"]
-[10.24040412902832, 4.22380256652832, "[FF] Release Mechanism of the DACS (Deployable Aft Conical Section) = Firing three frangible pyrotechnic bolts"]
-[9.38068675994873, 0.7805835008621216, "[TT] Orbit Drift of the Bennu = About 280 m/year toward the Sun"]
-[9.6223783493042, 8.241132736206055, "[TT] Field of View, horizontal of the Instrument = 24\u00ba"]
-[4.489870071411133, 5.298431873321533, "[TT] Manufacturer of the GomX-4B = GomSpace in Denmark"]
-[8.999492645263672, 4.3521037101745605, "[FF] Redundant Attitude Determination of the Sun Sensors = Method"]
-[5.369109153747559, 1.2760432958602905, "[FF] Conference Date of the IASI-NG = 4-8 February 2013"]
-[11.961530685424805, 5.007760047912598, "[TT] Size of the ICARE = 281 mm x 155 mm x 71 mm"]
-[13.241517066955566, 7.175768852233887, "[TT] Heater Power of the SVM = 80 W"]
-[9.165980339050293, 7.202089786529541, "[TT] Spatial Resolution at Nadir of the Imager = 0.46 m GSD"]
-[5.9382548332214355, 4.0560455322265625, "[FF] Payloads of the EIRSAT-1 = Trio of Irish payloads"]
-[6.84950065612793, -0.4584873914718628, "[TT] Repeat Cycle of the GRACE-FO Satellites = 30 days"]
-[7.9383344650268555, 7.512657165527344, "[FF] Function of the Systematic and Radiometric Correction Processor = Corrects the raw hyperspectral image (HSI) data for systematic effects and converts them to physical at-sensor radiance values"]
-[11.655844688415527, 4.2140889167785645, "[TT] Jettison Altitude of the Fairings = ~160 km"]
-[8.684369087219238, 7.314822196960449, "[TT] Positioning Stability of the Detector = ~ 80 \u00b5m"]
-[13.399641036987305, 5.777738094329834, "[FF] G&C System of the STEREO spacecraft = Three-axis-stabilized with fixed solar arrays for power generation as well as a steerable HGA (High Gain Antenna) for heliocentric orbit communications"]
-[4.522463321685791, 7.927465438842773, "[TT] Tx frequency of the Antenna = 28.05 GHz\u00b1550 MHz"]
-[9.024073600769043, 5.0893144607543945, "[TT] Quantity of the Gyros = 4"]
-[5.5100297927856445, 2.67852783203125, "[FF] Subsystems of the TRISHNA = French Space Agency (CNES)"]
-[3.8716859817504883, 6.381232261657715, "[TT] Antenna of the MODEX-2 = Three-antenna"]
-[6.7442827224731445, -0.524692177772522, "[TT] Orbit File Latency of the EDOT = About 24 hours"]
-[13.775651931762695, 3.668214797973633, "[TT] Antenna Mass of the AMSR = Nearly 200 kg"]
-[7.445774555206299, 1.954831838607788, "[FF] Program of the GEOSAT = Navy satellite program to complete SeaSat altimetry mission"]
-[13.153926849365234, 7.297325611114502, "[TT] Maximum Power Use of the ScaRaB = 70 W"]
-[10.093523979187012, -1.4689711332321167, "[TT] Orbit Inclination of the Harmony satellites = 98.19\u00b0"]
-[7.191577434539795, 8.194369316101074, "[TT] SNR for Bright Objects of the MSU-100 = 200"]
-[4.0728936195373535, 0.33746227622032166, "[TT] Launch Date of the Corvus-BC 1 and 2 = July 14, 2017"]
-[4.743393898010254, 2.9189345836639404, "[TT] Headquarters of the EDF = New York"]
-[9.015694618225098, 4.6974287033081055, "[FF] Control Method of the Satellite = Using the target value to determinate the sign of the angular rate in the X- and Y-axis"]
-[5.0209059715271, 3.4299044609069824, "[TT] Manufacturer of the Cupola = TAS-I"]
-[5.819094657897949, 0.5918160676956177, "[TT] Next Operations Phase Examination of the Ibuki-2 = Approximately in the next 2.5-month period"]
-[6.253775119781494, 6.020747184753418, "[TT] Quantity of the TR modules = 288"]
-[7.013959884643555, -0.7991819977760315, "[TT] Orbital Period of the L 98-59b = 2.25 days"]
-[8.728219985961914, 8.420230865478516, "[TT] Manufacturer of the Miniature High-Resolution Imaging Spectrometer = MPB Communications Inc."]
-[6.209754467010498, 3.0531275272369385, "[FF] Objectives of the COTS 3 = On-Orbit Operations \u2014 Approach, ISS \u2014 Attached Operations, On-Orbit Operations \u2014 Departure, Recovery"]
-[13.587837219238281, 5.814507961273193, "[FF] Battery Recharge Method of the Sloshsat-FLEVO = Using the solar panels"]
-[4.388709545135498, 1.3101297616958618, "[FF] GNC 2011 Conference Date of the SEOSat/Ingenio = June 5-10, 2011"]
-[3.4549295902252197, -0.921042263507843, "[TT] Orbit Type of the OceanSat-1 = Sun-synchronous near-circular orbit"]
-[4.737086772918701, 2.3974437713623047, "[TT] NorSat-2 Mission Status of the NorSat-2 = Operating on-orbit"]
-[4.917471408843994, 3.0695278644561768, "[TT] Designed and Built by of the Sample Fetch Rover (SFR) = Airbus"]
-[5.452049732208252, 7.050928592681885, "[TT] Instantaneous Data Rate of the WCOM = 27 Mbps"]
-[4.4627580642700195, 7.4438958168029785, "[TT] Downlink Band of the SAS&R = UHF band"]
-[8.626157760620117, 0.2152046263217926, "[TT] Depth of the Sognefjord = 1308 m"]
-[11.814486503601074, 6.698610305786133, "[TT] Electron Energy Resolution of the REPT = 25%"]
-[6.50004768371582, -0.7534278035163879, "[TT] LTAN of the Satellite = 10:30 hours"]
-[5.49058198928833, 0.8838276863098145, "[FF] Presentation Date of the Hera = November"]
-[13.509757041931152, 7.3429694175720215, "[TT] Power Generation of the IRIS = 340 W"]
-[8.087505340576172, 0.5252053141593933, "[TT] Low Water Levels of the Vistula = Lowest level on record in 2019"]
-[10.700610160827637, 1.108483910560608, "[TT] Size of the TOI 2076 c and d = A little over four times larger than Earth"]
-[8.128090858459473, 5.558701038360596, "[FF] Calibration of the Advanced Land Imager = Spatial"]
-[11.688369750976562, 3.3979573249816895, "[FF] Development Steps Date of the RF-Ion Thrusters RIT = 2001"]
-[8.977545738220215, 4.399335861206055, "[TT] Sun Sensor of the AOCS = 4\u03c0 sun sensor"]
-[7.995471477508545, 4.635157585144043, "[FF] Total Ionizing Dose Measurement of the RADFET = Unknown"]
-[5.2682366371154785, 2.329508066177368, "[FF] Mission Type of the Resurs-DK1 = EO"]
-[14.610688209533691, 6.746655464172363, "[TT] Nominal Voltage of the NiH2 batteries = 10 V"]
-[3.8940839767456055, 4.37583065032959, "[TT] Routine Phase Operations of the RADARSAT-2 = 3 years"]
-[12.703780174255371, 1.9225531816482544, "[FF] Measured Quantity of the SAGE-III = Chemical composition of the atmosphere and the vertical distribution of aerosols and gaseous compounds"]
-[9.66534423828125, 4.5425262451171875, "[TT] Attitude Control of the GNB = Passive magnetic attitude control"]
-[8.522184371948242, 9.465850830078125, "[TT] Responsivity Requirement of the Responsivity Measurement = >0.89 A/W"]
-[8.428461074829102, 5.529041290283203, "[TT] Direction of Arrival Estimation Accuracy of the GPS/Galileo E1/E5a receiver = Within a few degrees"]
-[3.4020702838897705, 5.232593059539795, "[TT] Frequency of the SAR = L-band (1.275 GHz)"]
-[7.623075485229492, 1.3278357982635498, "[FF] Date of the SWOT Hydrology Workshop = Sept. 15-17, 2008"]
-[11.431614875793457, 4.796194553375244, "[TT] Shape of the PM = Cylindrical"]
-[5.18873929977417, 2.450727701187134, "[TT] CEO of the HawkEye 360 = John Serafini"]
-[6.087000846862793, 1.8089799880981445, "[FF] URL of the Gokturk-2 = https://iafastro.directory/iac/proceedings/IAC-19/IAC"]
-[4.496555805206299, 7.732770919799805, "[TT] Frequency Bands of the RF Communications = UHF/VHF (436/145 MHz)"]
-[10.802200317382812, 3.9888365268707275, "[FF] Enclosure Purpose of the CanX-7 = Converts the uncoiling motion of the tape springs into linear motion of the booms"]
-[9.93829345703125, 3.0963146686553955, "[TT] Fire Mapping Capability of the CubeSat = Nighttime"]
-[8.7362699508667, 9.393648147583008, "[TT] Spectral Range of the TANSO-CAI-2 = 0.333 - 1.675 \u00b5m"]
-[4.599913597106934, 7.328734874725342, "[TT] L-band Receivers Data Rate of the UoSAT-12 = 1 Mbit/s"]
-[7.69716215133667, 9.036161422729492, "[TT] Wavelength Bandpass of the UVS Instrument = 1:3.8 (cha. 1); 2:3.7 (cha. 2)"]
-[7.09174919128418, 4.410510063171387, "[FF] Unknown of the SBE (Scatterometer Back End) = Unknown"]
-[5.090025901794434, 3.34913969039917, "[TT] Manufacturer of the ERA = Fokker Space"]
-[6.705252170562744, -0.623009979724884, "[TT] Repeat Cycle of the Optsat-3000 = 2 days"]
-[6.979841709136963, 3.9095299243927, "[FF] Equipment of the Pilote experiment = Virtual reality headset and a haptic joystick"]
-[13.158303260803223, 7.226282119750977, "[TT] Power Consumption of the Sensor Complement = ~35 W (37 W on nightside, 21 W on the dayside of the orbit)"]
-[8.126789093017578, -1.1189192533493042, "[FF] Function of the ICESat Data Extraction Software = Automatically extract seafloor depth measurements from ICESat-2 laser data"]
-[4.9560866355896, 3.3340258598327637, "[TT] Manufacturer of the RSI = EADS Astrium SAS, France"]
-[12.390741348266602, 0.630378246307373, "[FF] Power Source of the PLATO = Ancillary Electronics Units (AEUs)"]
-[5.867776393890381, 3.2831902503967285, "[FF] Focus of the EIAST = Satellite development, manufacturing, integration and application utilization"]
-[9.082244873046875, 0.9120327830314636, "[FF] Momentum Factor of the Impact Ejecta = 3 to 5"]
-[8.736658096313477, 1.967659831047058, "[TT] Wind Speed Range of the Numerical Weather Model = 3 m/s to approximately 20 m/s"]
-[7.603461742401123, 3.295131206512451, "[FF] Imaging Time of the Satellite = Dawn to dusk throughout the day"]
-[6.341829776763916, 7.212674617767334, "[FF] Data Compression Algorithm of the DACS = Real-time flexible BAQ (Block Adaptive Quantization)"]
-[8.127540588378906, 6.879300117492676, "[TT] Components of the Photometer Unit = Photomultiplier tube, high voltage power supply, and pulse amplitude discriminator electronics"]
-[10.819276809692383, 3.9642863273620605, "[TT] Sail Deployment of the CanX-7 = Individual"]
-[5.293724060058594, 0.6289497017860413, "[TT] Launch Year of the Satellite = 1979"]
-[5.100442409515381, 4.807888031005859, "[FF] Objective of the SpooQySat = Demonstrate in-orbit a space-compatible quantum light source"]
-[12.107562065124512, -0.1827813684940338, "[TT] Observation Sectors of the TESS Cameras = 26 (13 per hemisphere)"]
-[4.967051029205322, 3.0783703327178955, "[TT] Developer of the CIMON = Airbus"]
-[6.927380084991455, -0.7257128357887268, "[TT] Orbit Period of the WD 1856 b = 34 hours"]
-[8.147875785827637, 5.897772312164307, "[FF] Field of View of the DarkCarb image sensor = Restricted"]
-[5.67042350769043, 0.5714555382728577, "[FF] Launch Date of the GeoEye-1 = Sept. 2008"]
-[5.719993591308594, 5.020987510681152, "[FF] Purpose of the GALANT = Test the signal array processing technology for mitigation and detection of radio interference in receivers of satellite navigation systems"]
-[5.72023868560791, 7.082808494567871, "[TT] Average Data Rate Over Land of the KaRIN = ~271 Mbit/s"]
-[5.067821979522705, 0.7858009934425354, "[FF] News Date of the DLR = 2 December 2021"]
-[8.865445137023926, 3.7192084789276123, "[FF] Energy Range of the MIPA = Optimized to cover accelerated ionospheric ions"]
-[5.423251628875732, 3.9450790882110596, "[TT] Number of Decommissioned Satellites of the HY-2 = 1"]
-[6.593140125274658, 6.756599426269531, "[TT] Laser Beam Link Frequency of the EDRS-A = Up to 15 times per day"]
-[8.11600399017334, -0.4652935564517975, "[TT] Lowest 14 Ice Extents of the Sea Ice = All occurred in the past 14 years"]
-[12.809871673583984, 2.0178654193878174, "[FF] Quantity of the SAGE-III = 1"]
-[7.1926398277282715, -0.4102040231227875, "[TT] Initial Rotation of the Philae = Slow"]
-[7.959705829620361, 5.585728645324707, "[FF] Close Range Solution of the VBS = 3DOF translational solution or a full 6 DOF pose/translation solution"]
-[11.804886817932129, 6.743013381958008, "[TT] Particle Energy Range of the LESSA = 100 eV - 50 keV"]
-[4.788676738739014, 0.5561771392822266, "[TT] Launch Date of the OTB-1 = 2015"]
-[8.387696266174316, 6.8905768394470215, "[TT] Instrument Type of the AEISS = High resolution optical imagers"]
-[4.878250598907471, 3.257891893386841, "[TT] Provider of the Next generation solar cells / Astrium = EADS Astrium GmbH"]
-[8.546024322509766, 5.603641986846924, "[TT] Vertical Guidance Accuracy of the EGNOS = Within 60 m altitude"]
-[4.5382490158081055, 7.6519293785095215, "[TT] Signal Filtering of the LICEF = RF and IF"]
-[4.302704334259033, 7.302825927734375, "[TT] Frequency Band of the Ka-band transmitter = Ka-band"]
-[5.089336395263672, -0.39642900228500366, "[TT] Scheduled Launch Date of the CBERS-3 = 2012"]
-[8.6383638381958, 1.2598177194595337, "[TT] Instrument Type of the HSC (SAC-D/Aquarius) = Precision orbit"]
-[10.245105743408203, 8.108261108398438, "[TT] Aperture Diameter of the SOT = 50 cm"]
-[7.936193466186523, 8.575444221496582, "[TT] Spectral Range of the SITQ = 380-2500 nm"]
-[4.554197311401367, 2.9879283905029297, "[TT] Location of the Ground Segment = Huntsville AL"]
-[5.848125457763672, -0.7162001132965088, "[TT] Consumable Supply Life of the SA-200HP = 10 years"]
-[6.314109802246094, 1.8906136751174927, "[FF] URL of the eROSITA = http://www.mpe.mpg.de/6541082/eROSITA_Bulletin7.pdf"]
-[9.844457626342773, 7.828436374664307, "[TT] Line Duration of the Telescope = 30 ms"]
-[8.740164756774902, 7.431121349334717, "[TT] Detection Threshold of the Point-source Detectors = ~100 parts per billion (ppb)"]
-[6.872767925262451, 2.8143811225891113, "[FF] Collaboration Partner of the MethaneSAT = EDF"]
-[6.6265974044799805, 4.048201560974121, "[FF] Type of the GOES Sounder = Sounder"]
-[9.458922386169434, 1.3364176750183105, "[TT] Deployment Velocity of the Dispensers = 1 to 2 m/s"]
-[6.900877475738525, 9.484830856323242, "[TT] NEDT at 300 K of the Band 1 = 1.5 K"]
-[5.707708835601807, -0.1790560781955719, "[TT] Launch Date and Time of the Spaceflight SSO-A: SmallSat Express = Monday, December 3rd at 10:34 a.m. PST (18:34 GMT)"]
-[7.616039752960205, -0.812431275844574, "[TT] Launch Date of the ICESat-2 = November 2018"]
-[10.717329978942871, 5.561927318572998, "[FF] Back Plate Coating of the Thermal Control Louvers = Highly emissive coating"]
-[3.811109781265259, -1.1280736923217773, "[FF] Orbit of the CAPSTONE = Near rectilinear halo orbit"]
-[7.376355171203613, 4.79644775390625, "[TT] Mounting of the M2 = Central fixture at back side"]
-[9.355083465576172, 5.86071252822876, "[FF] Motion of the Scan Mirror = Causes a small but well-defined disturbance of the spacecraft attitude"]
-[9.64828109741211, 8.18930721282959, "[TT] Mask Thickness of the Optical Head = 0.1 mm"]
-[7.603602886199951, 1.3349958658218384, "[FF] Function of the Stereo camera (CCD) = Obtain three-dimensional stereo image of the lunar surface"]
-[2.8324875831604004, 0.08888804912567139, "[TT] J2000 declination (deg) of the B1813-140 = -14.036"]
-[7.720806121826172, 9.117791175842285, "[TT] Bandpass of the Long Wavelength Band = 1335-1750 \u00c5"]
-[7.909257411956787, 2.110447645187378, "[FF] Operation of the SeaSat = All sensors operated at the same time, over the same region of the ocean"]
-[11.700078010559082, 3.341545820236206, "[TT] Thruster of the ABEX = Small maneuvering thruster"]
-[14.391847610473633, 6.846429347991943, "[FF] Voltage of the Battery = Unknown"]
-[6.785048007965088, 3.8977396488189697, "[FF] Unknown of the Spaceflight Industries = Unknown"]
-[4.827204704284668, 7.879024982452393, "[TT] Frequency Band of the GETR (Galileo Experimental Test Receiver) = E5b 1207.14 MHz"]
-[16.48714256286621, 3.5713491439819336, "[FF] Close Approach Complaint of the OneWeb = Filed in Federal Communications Commission"]
-[6.707435607910156, 8.000908851623535, "[TT] NEDT (K) of the SSM/I = 0.45, 0.42, 0.73, 0.37, 0.38, 0.69, 0.73"]
-[10.686875343322754, 1.0218461751937866, "[TT] Host Star Type of the WD 1856 b = White dwarf"]
-[10.083946228027344, -1.526426076889038, "[TT] Inclination of the Satellite = 98.1\u00ba"]
-[5.615632057189941, 2.713221788406372, "[TT] User of the PIRPL = The Pentagon\u2019s SDA (Space Development Agency)"]
-[12.147722244262695, 6.140923023223877, "[TT] Cosmic Ray Events of the AMS-02 = 40 billion"]
-[7.203141212463379, 8.161356925964355, "[TT] SNR of the Spacecraft = > 100:1"]
-[14.597685813903809, 6.629922866821289, "[TT] Battery Type of the S/C = Lithium-iodine"]
-[4.808328628540039, 3.2091310024261475, "[FF] Manufacturer of the HSTS = EADS Astrium"]
-[6.075443267822266, 8.474449157714844, "[FF] RF Frequency of the Overhauser Nuclear Magnetic Resonance Autooscillator = Variable"]
-[8.116674423217773, -0.45051175355911255, "[TT] Average Annual Ice Loss of the Greenland's ice sheet = 200 gigatons"]
-[5.556934833526611, -1.9393033981323242, "[FF] Applications of the KOMPSAT-3 = Public safety, resource management, environmental monitoring, location-based services, intelligence and disaster monitoring"]
-[13.351128578186035, 5.544175148010254, "[TT] Number of Arrays of the ISS Roll-out Solar Array (iROSA) = 6"]
-[10.907444953918457, 0.6379836797714233, "[TT] Number of Stars' Rotation Rates Measured of the Kepler = More than 750"]
-[7.739176273345947, 5.472057819366455, "[FF] Range of the Experiment = 36 nT"]
-[8.395364761352539, 8.64745807647705, "[TT] Spectral Range of the Prism Spectrometer = 450-1000 nm"]
-[7.570817947387695, 4.332553386688232, "[FF] Occulting Disk Size of the OSC = 1.4 m"]
-[9.038422584533691, 4.682932376861572, "[FF] On-orbit performance evaluation of the Propellant-free attitude control system = Not provided"]
-[6.116507053375244, 1.8140465021133423, "[FF] URL of the ABI = http://www.goes-r.gov/education/docs/Factsheet_ABI_v6.pdf"]
-[4.459105491638184, 3.0714359283447266, "[TT] Location of the Igloo = In front of the pallet"]
-[3.5144829750061035, -0.9219099879264832, "[FF] Type of the Science Orbit = Near-circular (non sun-synchronous) 21-day orbit"]
-[6.408263683319092, 3.7920000553131104, "[FF] Expenditure Profile of the Phase 1 = Low until Critical Milestone (CM)"]
-[9.998519897460938, 2.9211223125457764, "[FF] Maiden Flight Date of the Cubesats = Unknown"]
-[11.886363983154297, 4.954600811004639, "[TT] Grid Dimensions of the CVX\u20132 Device = 7 mm x 19 mm"]
-[7.24791955947876, 6.985830783843994, "[TT] NESZ (F/H/U) HH of the Radiometry = 1.31"]
-[11.976370811462402, 3.4465572834014893, "[TT] Fuel Mass of the Ion engine = 10 kg (Xenon)"]
-[13.484829902648926, 3.030441999435425, "[TT] Mass of the Satellite Bus = Approximately 3850 kg"]
-[13.609673500061035, 5.75780725479126, "[TT] Solar Panels of the ALTIUS = Two deployable solar panels with 120 W of power"]
-[3.4222843647003174, 2.1465773582458496, "[FF] GNSS-RO of the Sentinel-6 = Instrument"]
-[3.325934648513794, 5.012552261352539, "[TT] Mode of the SAR Sensor Subsystem = HR (High Resolution)"]
-[13.443842887878418, 5.767147541046143, "[TT] Voltage of the Solar Array = 20\u201340 V"]
-[7.701121807098389, 9.020933151245117, "[TT] Spectral Band of the KLIMAT = 10.5 - 12.5 \u00b5m"]
-[14.452991485595703, 6.824636936187744, "[TT] Nominal Voltage of the Lithium-ion Battery = 4.2 V"]
-[5.305383682250977, 7.00130558013916, "[TT] Data Link Speed of the CMS = 4 Mbit/s"]
-[4.544863700866699, 0.6495875120162964, "[TT] Launch Date of the COSPAS GOMS-1 = Oct. 31, 1994"]
-[5.230295658111572, 3.6560230255126953, "[TT] Platform of the exactView-1 = SSTL-100"]
-[13.355480194091797, 6.991332054138184, "[TT] Science Equipment Power of the Power Supply = 1500 W"]
-[5.136291980743408, 1.1048336029052734, "[TT] PFM Delivery Date of the SMOS = End of 2006"]
-[6.409141540527344, 5.46539831161499, "[FF] Function of the 300 V System CPU = Recovers from malfunctions"]
-[7.598841667175293, 3.5529561042785645, "[FF] Detector of the GHGSat-C1/-C2 = IR camera"]
-[7.815520763397217, 2.9909796714782715, "[FF] Team Leader of the Science requirement, CO2 Retrieval Algorithm, Validation and Application = Liu Yi"]
-[7.589869499206543, 6.646025657653809, "[TT] Time of Impact Resolution of the MPID = 0.1 s"]
-[12.025923728942871, 4.503217697143555, "[TT] Size of the Spacecraft = 9.9 m (x) x 16.5 m (y) x 3.7 m (z)"]
-[9.139163970947266, 7.432937145233154, "[TT] Spatial Resolution of the Spectral bands = 2 m for PAN, 8 m for MS imagery"]
-[14.061009407043457, 3.258460283279419, "[TT] Mass of the LARES-2 = 295 kg"]
-[6.3062849044799805, 1.853701114654541, "[FF] URL of the eROSITA = http://www.aip.de/People/ASchwope/papers/eROSITA_SPIE_2006.pdf"]
-[13.55426025390625, 5.773677825927734, "[FF] Power Source of the \u00d8rsted spacecraft = Solar panels and batteries"]
-[4.895259380340576, 1.7719478607177734, "[FF] URL of the Gokturk-2 = http://www.uzay.tubitak.gov.tr/tubitakUzay/en/newsArchive/gk-2.php"]
-[5.73598051071167, -0.7304755449295044, "[TT] Design Life of the ROSE-L satellite bus = Seven and a half years"]
-[11.727533340454102, 7.5082902908325195, "[FF] Observation Frequency of the Megha-Tropiques = A minimum of 4 per day over the 22\u00b0S-22\u00b0N band"]
-[13.337442398071289, 7.729586601257324, "[TT] Transmitter Power of the OPAL = 2.2 W"]
-[5.4760003089904785, 2.698101758956909, "[TT] Mission Owner of the INSAT-3D = ISRO (Indian Space Research Organisation)"]
-[4.4015913009643555, 0.17179036140441895, "[FF] Uplink of the STRaND-1 = Not optimal during the first two weeks"]
-[11.088445663452148, 5.974203109741211, "[TT] Insulators of the FSU = Machined sapphire rods"]
-[7.142343521118164, 4.513105869293213, "[FF] Purpose of the GRD = Detection of GRB events at apogee arc above the VAB"]
-[11.967448234558105, 5.005079746246338, "[TT] Volume of the Herley MD2000C-1 = 13.8 cm3"]
-[9.017963409423828, 5.4836812019348145, "[TT] Spacecraft Position of the ABI = 35 m in-track, 35 m cross-track and 70 m radial over 15 minutes"]
-[12.859243392944336, 2.0846028327941895, "[TT] Size of the SAGE-III = 73 cm x 45 cm x 93 cm"]
-[8.325593948364258, 7.627778053283691, "[TT] Detector Quantity of the TIR Subsystem = 50"]
-[5.460907936096191, 3.900934934616089, "[TT] Number of Weather Centrals in the United States of the IDPS = 4"]
-[4.396401405334473, 2.8989150524139404, "[TT] Location of the GNNO = New Norcia Australia"]
-[8.309847831726074, -0.580828845500946, "[TT] Spatial Resolution of the Ice sheets Rock basement = 50-100 km"]
-[6.670264720916748, 5.920280456542969, "[TT] Quantity of the FBGs = 2"]
-[7.9157867431640625, 2.0906221866607666, "[TT] Channels of the Ocean Color Scanner = 8"]
-[4.364080429077148, 2.122135877609253, "[TT] Replacement of the DubaiSat-1 = DubaiSat-2"]
-[6.235337257385254, 1.4047976732254028, "[FF] URL of the BepiColombo = http://www.lpi.usra.edu/meetings/lpsc2013/pdf/2172.pdf"]
-[7.923055171966553, 3.1668341159820557, "[TT] Absorption at 1.2 \u00b5m of the Water (H2O) = 10 -21 mol cm -2"]
-[7.77883243560791, 7.637641429901123, "[TT] Image Rejection of the Image-Reject Mixer = > 40 dB"]
-[8.162802696228027, 2.1811978816986084, "[FF] Cross-Calibration Target of the CloudSat = Ocean surface"]
-[8.598148345947266, 3.6433584690093994, "[FF] Purpose of the PREMOS = Measure UV solar radiance"]
-[10.05807876586914, -1.5296177864074707, "[TT] Orbit Inclination of the GF-3 Satellite = 98.41\u00ba"]
-[4.891139030456543, 1.751943588256836, "[TT] Launch Date of the HORYU-4 = Feb. 17, 2016"]
-[5.894721031188965, 1.334739327430725, "[FF] Presentation Date of the ERG Satellite = June 5-12, 2011"]
-[8.107169151306152, 6.74852991104126, "[TT] Accuracy of the SSI Monitoring Device = Better than 0.5% per year"]
-[5.714263916015625, 4.243968963623047, "[FF] Procedure Scripts of the SATLAB = PLUTO procedure scripts"]
-[7.765789031982422, 1.7652541399002075, "[TT] Regeneration Percentage of the Mangrove Forests = 6 percent"]
-[8.94936752319336, 3.8033440113067627, "[FF] Potential Generation of the SenPot = Maintains the IVM reference ground at the floating potential with respect to the plasma"]
-[9.112709045410156, 7.005338191986084, "[TT] Resolution of the FGM = 1 to 2 nT"]
-[11.380035400390625, 4.368987083435059, "[TT] Size of the FloripaSat-1 = 1U"]
-[9.392884254455566, -0.1905776709318161, "[TT] Optimal Radial Distance of the PIXIE = 6 RE"]
-[10.045256614685059, 3.0996458530426025, "[TT] Platform of the Inmarsat S \u2013 Europasat / Hellas-Sat 3 = Spacebus 4000 C4"]
-[8.335641860961914, 0.8236042857170105, "[TT] Range of values of the Snow water content = 0-50 cm"]
-[6.1472063064575195, 6.450268745422363, "[TT] Latency Requirement of the S-3 STC = Within 1,5 days (36 hr)"]
-[5.1681928634643555, 7.0218706130981445, "[TT] Payload Data Downlink Rate of the MERLIN = 180 to 310 Mbit/s"]
-[7.860785961151123, 6.501103401184082, "[TT] Integration Time of the Scanner Assembly = About 15 seconds"]
-[4.700186729431152, 7.317061901092529, "[TT] X-band Tx Data Rate of the RF communications = 76.53 Mbit/s"]
-[4.871291637420654, -0.2448180764913559, "[TT] Launch Time of the SpaceX CRS-19 = 17:29:24 UTC"]
-[6.502128601074219, 4.212010860443115, "[FF] Architecture of the Space Cube 2 = Space Cube Architecture"]
-[5.0794677734375, 7.529189586639404, "[TT] Data collection rate of the Millimeterwave receiver = 0.23 \u2013 2.53 kbit/s"]
-[6.064156532287598, 1.681889533996582, "[FF] URL of the FY-4 Program = http://www.nsmc.cma.gov.cn/newsite/NSMC_EN/Channels/100099.html"]
-[9.546358108520508, 0.839732825756073, "[TT] Distance from Solar System of the IBEX = 12-13 million km"]
-[12.039179801940918, 6.307297706604004, "[FF] Lithium Flux of the AMS = Behaves similarly to protons and helium"]
-[8.2476167678833, 5.915379047393799, "[TT] Precision of the Method = Better than 0.5%"]
-[7.629749298095703, 5.679711818695068, "[FF] Principle of the GNC = Image processing using LIDAR sensors and cameras"]
-[11.108190536499023, 1.540121078491211, "[TT] Mass of the STARSHINE = 39 kg"]
-[7.779964923858643, 1.859423279762268, "[FF] Monitoring Importance of the Ocean Acidification = Important for climate and environmental policy-making"]
-[7.0752716064453125, 5.81093692779541, "[FF] Adjustability of the RTEP (Real Time Event Processor) = Allows digital event detection algorithms and parameters to be more flexibly developed and optimized to operate reliably at the limits of instrument noise"]
-[11.582060813903809, 5.070051193237305, "[TT] Chip size of the PHA = 7.4 mm x 7.4 mm"]
-[10.122807502746582, 1.8610868453979492, "[FF] Accretion of the V404 Cygni = Material from a companion star"]
-[4.658105373382568, 0.550667405128479, "[TT] Operational Phase End Date of the HyperScout\u00ae = 2018"]
-[12.109697341918945, -0.3142547309398651, "[TT] Time to Final Orbit of the TESS = About 60 days"]
-[4.705830097198486, 5.618692398071289, "[FF] Distress Localization Accuracy of the MEOLUT = Unprecedented"]
-[9.86168384552002, 1.6775217056274414, "[FF] Observation Results of the Herschel = Gas filaments become unstable and form clumps of material bound together by gravity"]
-[4.54671049118042, 3.8754515647888184, "[TT] Number of active satellites of the GALILEO = 6/24"]
-[5.877853870391846, 0.9106343388557434, "[FF] Publication Date of the Small GEO Programme = 2012"]
-[5.617299556732178, -2.0375025272369385, "[FF] Calibration and Validation of the KOMPSAT-3 = Unknown"]
-[5.080254077911377, 7.070218086242676, "[TT] Downlink Rates of the LLCD PAT Systems = 622 Mbit/s"]
-[3.6065526008605957, 4.484419345855713, "[TT] SAR Constellation Data Distribution of the Spacety = Worldwide"]
-[6.275195598602295, 5.265531539916992, "[FF] Interface of the MMFU = PDICs (Payload Data Interface Controllers)"]
-[6.215133190155029, 4.966062545776367, "[FF] Purpose of the Interposer Board = Provide the interface between the 51-pin connector, the second connector, and the payload"]
-[6.044759750366211, 0.025843385607004166, "[FF] Observing Duration of the IMP-8 = 28 years"]
-[11.847387313842773, 4.8621015548706055, "[TT] Workspace Volume of the Research Facility = 15 cubic feet"]
-[5.154548645019531, 8.439903259277344, "[TT] Bandwidth/Passband of the 5 = 400 MHz"]
-[9.303472518920898, 5.029014587402344, "[TT] Attitude Accuracy of the Sentinel-1 = Stringent requirements on attitude accuracy"]
-[6.675421714782715, 8.790441513061523, "[FF] Measurement of the POLDER = Polarized reflectance in VIS/NIR"]
-[7.363395690917969, 5.717164039611816, "[TT] Number of Load Cells of the Truss = 6"]
-[6.302267551422119, 8.647195816040039, "[TT] Polarization of the SSM/I = Vertical, Horizontal"]
-[7.256900787353516, -0.4847392141819, "[FF] Behavior of the Alpha Circini = Shows complex behavior due to both rotation and pulsation"]
-[3.1850829124450684, 4.941082000732422, "[TT] Field of Regard of the L-SAR = 320 km"]
-[6.693826675415039, 6.052239894866943, "[TT] Quantity of the TRMs = 60"]
-[9.80329704284668, -0.7164560556411743, "[TT] Orbit Altitude of the SpaceX CRS-17 = ~ 400 km"]
-[4.871721267700195, 1.2336740493774414, "[FF] Presentation Date of the Delfi-n3Xt = Sept. 29 to Oct. 3, 2008"]
-[10.073586463928223, 2.775942325592041, "[FF] Support of the NanoSat MO Framework = Software updates"]
-[9.047954559326172, 7.556138038635254, "[TT] Swath of the CCD Camera = 6300 km"]
-[9.203959465026855, -0.4165201485157013, "[TT] Apogee of the Satellite = 1500 km"]
-[6.724099636077881, -0.3368481695652008, "[TT] Orbit Count of the Genesis-2 = 10,000"]
-[6.636312961578369, 0.7780499458312988, "[FF] Discovery Date of the Herschel = 13 Nov. 2017"]
-[3.4670681953430176, -0.8987423181533813, "[TT] Orbit Type of the CBERS-2B = Sun-synchronous orbit"]
-[4.634143829345703, 0.4734342396259308, "[TT] Launch Date Risk of the ORS-6 = Adds risk to the program"]
-[10.491006851196289, 1.4330124855041504, "[TT] Energy Emission of the NGC 5907 ULX = Same amount of energy as our sun does in 3.5 years in one second"]
-[11.733231544494629, 7.519643783569336, "[FF] Workshop Date of the Megha-Tropiques = October 7-10, 2014"]
-[13.548064231872559, 5.478179931640625, "[TT] Number of Cells of the Photo-Voltaic Array = 25 strings, 18 cells per string"]
-[5.70341157913208, 6.0490522384643555, "[TT] Number of Unidirectional Serial Ports of the NIC = 1"]
-[5.938732624053955, -0.4184507429599762, "[TT] Mission Duration of the GOCE = 4 years"]
-[4.983567237854004, -0.11728755384683609, "[TT] Launch Date of the Kleos Scouting Mission (KSM1) = November"]
-[8.938085556030273, 4.189367294311523, "[TT] Range of the Solar band = 0.32 \u00b5m to \u2265 100 \u00b5m"]
-[4.9530768394470215, 0.5288710594177246, "[TT] Launch Date of the SeaHawk-1 = 3 December 2018"]
-[6.943421363830566, 4.36706018447876, "[FF] Unknown of the NRO/MSD = Unknown"]
-[10.02341079711914, -1.5274641513824463, "[TT] Inclination of the Orbit = 97.8\u00ba"]
-[13.265493392944336, 5.499405860900879, "[FF] Technology of the Roll Out Solar Arrays (ROSA) = Roll up in a canister and then unfurl once in space"]
-[9.728461265563965, -0.5866414904594421, "[TT] Orbit Altitude of the Tomorrow-R1 and -R2 = 550 km"]
-[8.10802936553955, 6.97401237487793, "[TT] Infrared Multispectral Scanner of the HJ-1B = 1"]
-[7.643160343170166, 2.9533286094665527, "[FF] Mission of the TANGO satellite = Monitoring greenhouse gas emissions"]
-[4.2123212814331055, 4.855936527252197, "[TT] Application of the SDR = Aircraft tracking in remote areas where radar is unavailable"]
-[3.709723949432373, 4.686578750610352, "[TT] Sensor Module Imaging Modes of the RADARSAT-2 = Standard, Fine, ScanSAR Wide/Narrow, Polarimetric Standard/Fine, Multi-Look Fine and Ultra-fine"]
-[10.5955228805542, 7.389242172241211, "[TT] Swath Width of the Stripmap = 20 - 40 km"]
-[10.294137001037598, 4.035322666168213, "[TT] Mounting of the S-band receive and transmit antenna = Nadir-facing deployable boom"]
-[7.869363307952881, -2.492011070251465, "[FF] Observation of the GOLD = Ionosphere response"]
-[3.2733585834503174, 4.943112373352051, "[FF] Polarimetric Information of the ALOS-2 = Not enough compared to that of full-pol."]
-[5.5864434242248535, 3.9850573539733887, "[FF] Number of the Satellite = 3"]
-[-4.064877510070801, 4.482389450073242, "[FF] Support Phase Time Period of the Mango Tango = 11.08 to 08.09.2010"]
-[13.512812614440918, 5.833243370056152, "[TT] Total Power (BOL) of the Solar Array = 2300 W"]
-[3.2464656829833984, 1.6239811182022095, "[TT] Data Collection Frequency of the Sentinel-6/Jason-CS = Every 10 days"]
-[8.413195610046387, 6.878537178039551, "[TT] Design Feature of the Stereo Camera = TDI (Time Delay Integration) method"]
-[5.273290157318115, 1.1854438781738281, "[FF] Event Date of the ALOS = Dec. 5-7, 2006"]
-[11.573488235473633, 3.4672367572784424, "[FF] Test Conduct of the Integrated Firing Test = \u0394V thruster and RCS thrusters"]
-[4.98698091506958, 0.5939874053001404, "[TT] Scheduled Launch of the EMA (Euro Material Ageing) payload = 2022"]
-[13.752861976623535, 5.450095176696777, "[TT] Power Source of the S/C = Surface-mounted triple-junction solar cells"]
-[10.943808555603027, 6.03121280670166, "[TT] Components of the DBCP = Four wedges of birefringent material arranged in pairs"]
-[8.542132377624512, 5.648837566375732, "[TT] Baseline Accuracy of the GPS Data = 1 mm, 1D-sigma"]
-[4.327231407165527, 4.35747766494751, "[TT] Number of Mission Control Centers of the COSPAS-SARSAT system = 29"]
-[6.055589199066162, 5.988393783569336, "[TT] Number of Modules per Column of the T/R Modules = 32"]
-[11.730942726135254, 5.665225505828857, "[TT] Number of Wafers of the Collector Array = 55"]
-[5.063962459564209, 4.155961036682129, "[TT] Number of Unmanned Global Ground Stations of the C3S = 15"]
-[4.162407398223877, 4.822625637054443, "[TT] Spatial Acquisition Duration of the Alphasat TDP1 = Achieved in no more than 80 s"]
-[6.482934951782227, 7.610965728759766, "[TT] Data Quantization of the Instrument = 8 bit"]
-[14.0841646194458, 7.188268661499023, "[FF] Bus Support of the DC/DC converter = 30V-53V unregulated"]
-[6.7323527336120605, 0.8562198281288147, "[TT] Ion Tail Crossing Date of the Solar Orbiter = May 31"]
-[11.628958702087402, 4.6944355964660645, "[FF] Shape Options of the SPIDER = Squares to hexagons and even conformal concepts"]
-[10.975667953491211, 6.062891960144043, "[FF] Insulation of the Optical Cavity = Yes"]
-[3.642061233520508, -0.8296750783920288, "[FF] Orbit Type of the ABEX = Super-synchronous"]
-[8.038207054138184, 6.844302177429199, "[TT] Sensor Types of the FY-4 = Optical sensors and microwave sensors"]
-[6.226448059082031, 5.227126121520996, "[FF] Function of the Interface Chip = Provides a compliant implementation of the USB standard"]
-[8.084373474121094, -1.2316228151321411, "[TT] Instrument of the ICESat-2 = Laser"]
-[5.638705730438232, 2.9169576168060303, "[FF] Development of the SOLISS = Collaboratively developed by Sony Computer Science Laboratories, Inc. and JAXA Space Exploration Innovation Hub Center"]
-[9.587149620056152, 7.208726406097412, "[TT] Spatial resolution at nadir of the SBUS = 70/10 km"]
-[9.83470344543457, 8.242025375366211, "[TT] Effective Focal Length of the ASPIICS = 1150 mm"]
-[5.19330358505249, 2.242764711380005, "[TT] Mission Type of the Enxaneta = EO"]
-[6.267234802246094, -0.121290422976017, "[FF] Modification Time of the SCIP = Too long"]
-[6.6993327140808105, 1.166301965713501, "[FF] DOI of the SOFIE = 10.1002/2014JD021763"]
-[9.2332181930542, 5.755671501159668, "[FF] Output of the AD590 = Current proportional to the absolute temperature"]
-[6.391286373138428, 2.9020166397094727, "[FF] Development Team of the BioSentinel = Hugo Sanchez, James Chartres, Robert Hanel, Sharmila Bhattacharya, Antonio Ricco"]
-[6.528320789337158, -1.245033860206604, "[FF] Data Continuity of the GRACE = Still providing valuable information to the science community in 2015"]
-[6.012913703918457, 2.6532599925994873, "[TT] Managing Office of the IMAP = Heliophysics Program Office at NASA's Goddard Space Flight Center"]
-[8.085055351257324, 0.6384702920913696, "[FF] Groundwater Monitoring of the GRACE-FO = Global"]
-[9.541683197021484, 7.1233229637146, "[TT] Spatial Resolution of the MUX = 55 m"]
-[10.387980461120605, 4.549007892608643, "[TT] Quantity of the Reaction Wheels = Pyramid of 4 units"]
-[7.014955520629883, -0.8127758502960205, "[TT] Orbital Period of the TOI 270 b = 3.4 days"]
-[13.309816360473633, 7.420642375946045, "[TT] Output Power of the HPA = 34 W"]
-[6.390710830688477, 5.5638227462768555, "[TT] Inputs of the CDSU = Discrete digital inputs, analog inputs, thermistor inputs"]
-[5.896975994110107, -0.4422298073768616, "[TT] Mission Duration of the CM1 = September 2021 through 2026"]
-[12.129997253417969, 4.573183059692383, "[TT] Vacuum Chamber Dimensions of the GOES-R satellite = 8.8 m x 19.8 m"]
-[9.30956745147705, 10.738992691040039, "[TT] Polarization of the ICI-2 = V"]
-[7.71573543548584, 1.0432522296905518, "[FF] URL of the Airborne Lunar Spectral Irradiance (Air-LUSI) = https://airbornescience.nasa.gov/instrument/Air-LUSI"]
-[11.981158256530762, 5.041361331939697, "[TT] Volume of the ORA = 1230 x 1010 x 905 mm"]
-[7.160585403442383, -0.17812976241111755, "[TT] Total Orbits of the Total = 36836"]
-[14.234334945678711, 3.2192535400390625, "[TT] Mass of the Tatiana-2 = 100 kg"]
-[7.486438751220703, 3.542140007019043, "[FF] Application of the NightPod = Taking images of cities at night, mapping fishing activities, light pollution and fires"]
-[13.679667472839355, 5.752610206604004, "[TT] Solar Cells Power of the Tsubame = 130W"]
-[13.358391761779785, 2.911874532699585, "[TT] Mass of the Optsat-3000 = 368 kg"]
-[10.361845016479492, 3.2661209106445312, "[TT] CDR (Critical Design Review) of the SOURCE 3U CubeSat = Passed in July 2021"]
-[8.777113914489746, 5.484841346740723, "[TT] Ground Location Accuracy of the AOCS = < 220 m"]
-[9.25609302520752, 4.096355438232422, "[FF] Devices of the BCU Payload = ETP (Electron Temperature Probe) and MRM (Magneto-Resistance Magnetometer)"]
-[11.120434761047363, 5.187697410583496, "[FF] Experiment Date of the X-ray Gas Scintillation Spectrometer = Nov. 1985"]
-[5.102606773376465, 3.2074954509735107, "[TT] Manufacturer of the TanSat = Changchun Institute of Optics, Fine Mechanics and Physics/Chinese Academy of Sciences (CIOMP/CAS)"]
-[7.10352087020874, 3.2295186519622803, "[FF] Data Source of the GEOS Model = Actual measurements of physical properties"]
-[8.520366668701172, 4.1987223625183105, "[FF] Measurement Type of the Logarithmic Electrometers = Current"]
-[3.870234251022339, 7.881399631500244, "[TT] Modulation Scheme of the RF Communications = FSK"]
-[6.976027488708496, 3.2465498447418213, "[FF] Mission Goal of the Oculus-ASR = Exercise and validate techniques for determining an orbiting object's pose using unresolved ground imagery"]
-[9.080273628234863, 5.053751468658447, "[FF] Gyro Mode of the PARASOL = Used only for a few minutes on each rotation"]
-[3.021519184112549, 4.652254581451416, "[TT] Frequency of the GEOSAR = 406 MHz"]
-[13.33018970489502, 7.354658603668213, "[TT] Power of the SPEU = ~2.5 W"]
-[7.457146167755127, 6.992456436157227, "[TT] Number of Optical Terminals of the System = 6"]
-[8.984355926513672, 7.4785661697387695, "[TT] Crystal Size of the Detector = 30 mm x 30 mm x 1 mm"]
-[8.143741607666016, -0.3570140600204468, "[FF] Summer Ice Extent of the Arctic Sea Ice = Marked decreases in all seasons"]
-[6.064748764038086, 5.373159408569336, "[TT] Radiation Environment Behavior of the PIC (Peripheral Interface Controller) = Good"]
-[3.539321184158325, 5.087405204772949, "[TT] Detection Time of the SAR Transponders = Near-instantaneous"]
-[10.30026626586914, 1.9059526920318604, "[TT] Number of X-ray Sources of the eROSITA = More than 18,000"]
-[9.013297080993652, 3.3271517753601074, "[FF] Abundance in Plasmasphere of the He+ ions = Up to 15% of the total plasma density"]
-[5.105852127075195, -0.32241448760032654, "[FF] Launch Date of the CBERS-4A = Unknown"]
-[5.603668689727783, 3.9102578163146973, "[FF] Observation Requirement of the Cluster = At least four simultaneous observations"]
-[9.499008178710938, 1.2457326650619507, "[TT] Ejection Velocity of the DSAT-1 = ~ 0.05 m/s"]
-[7.086545467376709, 5.853882789611816, "[TT] Clock Stability Requirement of the DSAC = AD of at most 2.0 x 10-14 at one day"]
-[8.580650329589844, 7.676787376403809, "[TT] Array Size of the Detector Array = 2048 x 4096 square pixels"]
-[6.8172173500061035, 4.538744926452637, "[TT] Performed under Ground Segment control of the RVX FDIR = Yes"]
-[10.223458290100098, 5.703662872314453, "[TT] Temperature Accuracy of the Instrument = <4 k (goal 2 K @ 300 K)"]
-[8.787333488464355, 6.360389232635498, "[TT] Wave Height Measurement Accuracy of the Altimeter = \u00b1 10% or 0.5 m, whichever is greater"]
-[4.936713218688965, 1.0798895359039307, "[TT] Release Date of the HimawariCast Newsletter = 8 November 2016"]
-[6.0275654792785645, 6.662424564361572, "[TT] Telemetry Module Mode of the TTCS = PCM/DPSK/PM"]
-[11.773441314697266, 3.2623445987701416, "[TT] Quantity of the 8 N thrusters = 2"]
-[10.312668800354004, 7.897054672241211, "[TT] Instrument Size (Folded) of the DST (Dobson Space Telescope) = 100 mm x 100 mm x 60 mm"]
-[9.490117073059082, 0.5854841470718384, "[TT] Distance from Earth of the MarCO = 1 million kilometers"]
-[7.585509300231934, 2.680095911026001, "[FF] Mission Objectives of the FY-4 = Imagery, sounding, lightning mapping, and space environment monitoring"]
-[9.968957901000977, 2.40966534614563, "[FF] Science Goal of the HaloSat = Estimate the mass of the hot halo surrounding the Milky Way galaxy"]
-[8.147418975830078, 8.187607765197754, "[TT] Spectral Wavelength of the Imager = 777.4 nm"]
-[6.0587921142578125, 1.6066514253616333, "[FF] Conference Date of the Space Technology 5 = Feb. 3-7, 2007"]
-[10.003870010375977, 2.906130313873291, "[TT] AIV Completion Date of the IOD CubeSat = June 2017"]
-[13.377140998840332, 7.756814002990723, "[TT] Power of the VHF Transmitter = 8 W"]
-[3.0283491611480713, 2.0552399158477783, "[TT] Name Change Date of the Copernicus = December 11, 2012"]
-[8.041228294372559, 2.5451953411102295, "[TT] Measurement Domain of the MOMS = Ocean, Land"]
-[6.575133323669434, 0.31009724736213684, "[FF] Mission End Date of the CryoSat = Unknown"]
-[5.093802452087402, -0.3542204797267914, "[FF] Presentation Date of the CBERS = Feb. 4, 2009"]
-[8.007030487060547, 0.8319957852363586, "[FF] Distribution of the Maps = Online by the National Drought Mitigation Center at the University of Nebraska-Lincoln (UNL)"]
-[6.183990001678467, 2.7822301387786865, "[TT] Data Destination of the EMIT = NASA Land Processes Distributed Active Archive Center (DAAC)"]
-[9.11422061920166, 6.026839256286621, "[TT] Tracking Direction of the NEOSSat and Sapphire = Antisolar direction"]
-[8.407907485961914, 7.621246337890625, "[TT] Detector Arrays of the Imager = 5 linear detector arrays"]
-[7.817302703857422, 2.9880170822143555, "[FF] Measurement Frequency of the Copernicus Anthropogenic Carbon Dioxide Monitoring, CO2M = Weekly"]
-[4.8362956047058105, 1.2285979986190796, "[FF] Launch Date of the G\u00f6kt\u00fcrk-1 = 2015"]
-[8.399362564086914, 5.54642915725708, "[FF] Geo-Referencing Precision of the Claire = With sufficient precision to identify facilities of interest"]
-[6.7675886154174805, 3.7719850540161133, "[TT] Disposal of the DMSP F-20 = Scrapped"]
-[8.607516288757324, 2.907339572906494, "[FF] Observation Purpose of the TARANIS = To observe luminous, radiative and electromagnetic phenomena occurring at altitudes of 20 to 100 km over thunderstorms"]
-[7.114706993103027, 7.887943267822266, "[FF] Noise Measurement Window Length of the SCA = 8.5 ms and 10.8 ms"]
-[6.048333644866943, -0.5690192580223083, "[FF] Service Duration of the ZY-3 = Eight years"]
-[6.09009313583374, 4.4871134757995605, "[TT] AIV System Reuse of the PROBA Project = Ground segment software is used both as the AIV system and as the operations system"]
-[10.365374565124512, 3.2243025302886963, "[TT] Housekeeping Mode of the VELOX-PII CubeSat = Nominal"]
-[5.437177658081055, 2.962345838546753, "[TT] Manager of the CGS = Raytheon"]
-[4.353567600250244, 1.597154140472412, "[FF] Name Change of the ROCSat program = FormoSat"]
-[10.298455238342285, 5.77310037612915, "[TT] Detector Temperature Range of the MSU-E = -30 to -50\u00baC"]
-[6.472664833068848, 1.977689504623413, "[FF] Sale Approval of the ARTEMIS = ESA approves sale of Artemis telecom satellite to Avanti"]
-[4.85426139831543, 7.20589542388916, "[TT] Downlink Rate Capability of the S-band transceiver = Up to 2 Mbit/s"]
-[9.384222030639648, 7.623730182647705, "[TT] Field of Regard in Cross-Track of the Pan Imager = 780 km"]
-[5.519812107086182, 2.366436719894409, "[FF] Leader of the GeoNEX = Nemani"]
-[6.071902275085449, -0.5761794447898865, "[TT] Contract Extension of the RADARSAT-2 = Three years"]
-[5.35051155090332, 3.865030527114868, "[TT] Number of Satellites of the FengYun-4 = 7"]
-[13.518500328063965, 5.685263156890869, "[TT] Power Source of the Jason-3 = Two solar panels"]
-[4.799259662628174, 3.2865731716156006, "[TT] Manufacturer of the SPOT-6 = Astrium Services Division of EADS"]
-[7.347891330718994, 1.2056407928466797, "[FF] Objectives of the WISDOM = To investigate the three-dimensional geology and geological evolution of the landing site, characterize the electromagnetic properties of Martian soil, and observe the local distribution of well-compacted, sedimentary deposits"]
-[6.319250106811523, 2.6798863410949707, "[TT] Manufacturer of the XRS = LASP (Laboratory for Atmospheric and Space Physics) at the University of Colorado, Boulder, CO"]
-[5.638580322265625, 1.7159311771392822, "[FF] DEM Generation of the ALOS PRISM = Precise"]
-[12.075870513916016, 3.7005350589752197, "[TT] Pressure of the PROP unit = 300 bar"]
-[5.995303630828857, 2.070988655090332, "[FF] URL of the MSU Program = https://web.archive.org/web/20101201103604/http://space.msu.ru/eng/projects/"]
-[5.48117733001709, 0.3566473126411438, "[TT] Deployment Date from ISS of the Light-1 = February 3, 2022"]
-[8.671687126159668, 1.1007040739059448, "[FF] Mission Overview of the Aquarius/SAC-D = Aquarius/SAC-D Mission Overview"]
-[3.2390530109405518, 2.162996530532837, "[FF] Tracking Data Source of the A-68A = Copernicus Sentinel-3 mission, MODIS instrument on the US Terra mission, Copernicus Sentinel-1 mission"]
-[3.8753862380981445, 3.438823938369751, "[TT] Testing Start Date of the Galileo Second Generation Hardware = July 19, 2021"]
-[12.125907897949219, 7.598648548126221, "[TT] Mass of the Geoton-L1 imager = 310 kg"]
-[5.301558494567871, 1.7892401218414307, "[FF] Workshop Location of the ALOS-2 = ESA/ESRIN, Frascati, Italy"]
-[5.257082939147949, 7.196141242980957, "[TT] Image Telemetry Link of the SPOT-2 = 50 Mbit/s at 8 GHz"]
-[11.78260612487793, 4.511620044708252, "[TT] Span of the Rocket Landing Legs = 18 m"]
-[5.791574001312256, -0.7980976104736328, "[TT] Expected Orbit Lifespan of the Meteosat Satellites = At least seven years"]
-[6.470701694488525, 7.604887008666992, "[FF] A/D Quantization of the Instrument = 12 bit, 10 bit"]
-[11.9497709274292, 5.358153343200684, "[TT] Instrument Size of the Aquajet = 100 mm x 100 mm x 30 mm"]
-[6.590497016906738, 1.8758975267410278, "[FF] URL of the SARR and SARP = http://poes.gsfc.nasa.gov/sarr-sarp.html"]
-[7.884454250335693, 3.7338624000549316, "[TT] Measurement Capability of the ASCAT = Day and night"]
-[12.10719108581543, -0.3320397436618805, "[FF] Orbit Period of the TESS spacecraft = Order of 8-12 years"]
-[14.06420612335205, 4.000328540802002, "[TT] Mass of the Instrument mass = \u2264 70 kg"]
-[14.253775596618652, 3.0221097469329834, "[TT] Mass of the NewSat-6 = 43.5 kg"]
-[13.282506942749023, 5.450993061065674, "[TT] Installation Requirement of the Solar Arrays = Two spacewalks"]
-[14.283726692199707, 3.291351795196533, "[TT] Mass of the SADM = < 3.2 kg"]
-[6.236085414886475, 1.0405290126800537, "[TT] Observation Start Date of the SAGE-II = 1984"]
-[9.809619903564453, 4.90380334854126, "[TT] Z-axis Rotation Rate of the Satellite = 1 rotation per minute (rpm)"]
-[6.660980701446533, 5.484429836273193, "[TT] State-of-Health of the TT&C = Normal"]
-[5.072956085205078, 6.997380256652832, "[TT] Slot duration (ms) of the Service downlink = 127.4"]
-[7.510402679443359, -0.4379747807979584, "[FF] URL of the ICEYE X1 = https://www.iceye.com/press/press-releases/first-iceye-x1-radar-image-from-space-published"]
-[6.523738861083984, 0.015266157686710358, "[TT] Data Distribution Frequency of the CMC and USMCC = Daily"]
-[4.759954452514648, 8.28244686126709, "[TT] Center Frequency of the OBRC instrument = 9.623 GHz"]
-[3.6281299591064453, 2.69746470451355, "[FF] Number of Satellites of the Iridium Communications Inc. = 5"]
-[8.37826156616211, 0.8311969041824341, "[TT] Range of Values of the Snow water content = 0 - 50 cm"]
-[9.810564994812012, -0.40981581807136536, "[TT] Altitude of the LEO system = < 1000 km"]
-[8.568781852722168, 6.79127311706543, "[TT] Single Pass Stereo Coverage of the QuickBird-2 = Single scene (<10\u00ba off nadir track)"]
-[7.808897495269775, 3.021714448928833, "[FF] Mission of the TanSat = Global CO2 Observation and Monitoring"]
-[2.5589678287506104, 0.16730386018753052, "[TT] Pulse period (ms) of the B1509-58 = 150.658"]
-[7.269093036651611, 9.115509033203125, "[TT] Tuning Range of the FG (Filtergraph) = \u00b10.6 \u00c5"]
-[7.124887466430664, 6.895571231842041, "[FF] Turn-On Time of the GEDI Laser = Not specified"]
-[8.650609970092773, 7.689783096313477, "[TT] Pan Image Detector Size of the OIS = 4096 pixels x 4096 lines"]
-[9.18300724029541, 2.7122302055358887, "[FF] Observation Type of the RHESSI = CME ejection"]
-[11.078474044799805, 5.22275447845459, "[FF] Observation Modes of the Scintillation Detector = Monitoring of the electron flux, selection of the electron flux during flux splashes"]
-[5.037490367889404, 3.296873092651367, "[TT] Structure of the STPSat-1 = AeroAstro SpaceFrame"]
-[10.88914680480957, 7.355702877044678, "[TT] Swath Width of the SSM/T-2 = About 1500 km"]
-[9.257061958312988, 5.034042835235596, "[TT] Maneuver Angle of the ALSAT-2B = 30 deg"]
-[2.28337025642395, 2.771955966949463, "[TT] Co-PI of the EPI-Lo = Joe Giacalone"]
-[10.357691764831543, 4.505502223968506, "[TT] Quantity of the RW (Reaction Wheels) = 4"]
-[10.42241382598877, 3.265380382537842, "[TT] Interface Options of the Ubotica CogniSAT-XE1TM CubeSat Board = Gigabit Ethernet or USB2.0/3.0"]
-[8.104316711425781, 3.022779703140259, "[TT] Detects of the Geostationary Lightning Mapper (GLM) = Size and energy of lightning flashes"]
-[10.224103927612305, 5.333636283874512, "[FF] Radiator Function of the BepiColombo = Reflect heat directionally"]
-[9.26095199584961, 6.655111789703369, "[TT] Minimum Resolution of the Satellite = 1\u00ba/s"]
-[10.070626258850098, 7.598488807678223, "[TT] Image Diameter of the Imager = 43 mm"]
-[8.706884384155273, 7.575590133666992, "[TT] Image Sensor Pixel Size of the CMV4000 = 5.5 \u00b5m"]
-[7.7082719802856445, -2.538926601409912, "[TT] Imaging Cadence of the GOLD = Complete scan of each hemisphere every 15 minutes"]
-[3.4634170532226562, -0.8955895900726318, "[TT] Orbit Type of the JPSS-1 = Sun-synchronous orbit"]
-[14.028975486755371, 6.326564788818359, "[TT] NOR Flash of the GomSpace NanoMind A3200 = 128 MB"]
-[10.608275413513184, 2.8509092330932617, "[FF] Design Presentation URL of the Microsatellites = http://cddis.nasa.gov/lw13/docs/presentations/target_nicholas_1p.pdf"]
-[9.561684608459473, 4.1677093505859375, "[TT] Measurement Range of the Field Measurement Device = \u00b1 64 000 nT"]
-[6.100772380828857, 7.83256196975708, "[TT] Signal Transmission of the GIOVE-B = Two separate channels"]
-[10.183137893676758, 1.0395534038543701, "[TT] Handle Distance from Center of the The Teacup = Around 30,000 light years"]
-[6.739191055297852, 1.0749316215515137, "[FF] Article Publication Date of the Solar Orbiter = 26 April 2021"]
-[4.359399318695068, 7.365181922912598, "[TT] Uplink Frequency of the ABEX Telemetry, Tracking, & Command (TT&C) subsystem = S-band"]
-[6.969379901885986, 6.148196697235107, "[TT] Mode of the ALOS-2 = Stripmap"]
-[7.69527530670166, 6.830629825592041, "[TT] Exposure of the Observation = 40 ks"]
-[8.840550422668457, 3.2893357276916504, "[FF] Technique of the Alice = Absorption of sunlight by Pluto\u2019s atmosphere will show up as characteristic \u201cdips\u201d and \u201cedges\u201d in the ultraviolet part of the spectrum of light that Alice measures"]
-[4.034665584564209, 6.28444766998291, "[TT] Quantity of the ISL (Inter Satellite Link) System = 2 x Rx-Tx + 4 x antennas"]
-[7.890893459320068, 7.286962032318115, "[TT] Data Rate of the IMG = 882 kbit/s"]
-[11.159029960632324, 5.943363666534424, "[TT] Material of the FSU = Titanium"]
-[14.573762893676758, 6.75905179977417, "[TT] Rated Voltage of the NiMH battery = 1.2 V"]
-[5.350232124328613, 6.289039611816406, "[TT] Onboard Computer Memory of the F-15 and F-16 DMSP satellites = Increased"]
-[8.294707298278809, 1.466428279876709, "[FF] Sea Surface Salinity Retrieval of the WCOM IMI = Unknown"]
-[6.29701042175293, 2.662494421005249, "[TT] Manufacturer of the EUVS = LASP (Laboratory for Atmospheric and Space Physics) at the University of Colorado, Boulder, CO"]
-[7.707890033721924, 3.0988900661468506, "[FF] Methane Retrieval Algorithm of the Atmospheric Infrared Sounder = EOF-based regression algorithm"]
-[6.566667079925537, 6.949103355407715, "[TT] Duty Cycle of the Instrument = 20%"]
-[7.511478424072266, 5.798821449279785, "[FF] Measurement of the Lidar Instrument = Altimetric"]
-[10.450214385986328, 5.7899017333984375, "[TT] Temperature Range (Illuminated by the Sun) of the Spacecraft = -5 to +45\u00ba Celsius"]
-[8.045467376708984, 6.342272758483887, "[FF] Translation of the CCRR = Done using a set of high-accuracy translation stages"]
-[5.896831035614014, -1.0671398639678955, "[TT] Exceeded Design Life of the ACRIMSat = Yes"]
-[5.067306041717529, 3.5373501777648926, "[TT] Manufacturer of the Iris camera = UrtheCast Corp."]
-[10.029189109802246, 2.7180919647216797, "[TT] Orbital Period of the ISARA CubeSat = Approximately 90 minutes"]
-[14.238359451293945, 3.2567973136901855, "[TT] Mass of the MUX = 115 kg"]
-[9.466218948364258, 4.786675453186035, "[TT] Attitude Control of the DSAT-3 = Full 3 degree of freedom (3-DOF) control"]
-[6.994741439819336, 4.97686767578125, "[FF] Purpose of the VIPIR2 = Monitor the process"]
-[6.512712478637695, 3.1415181159973145, "[FF] Data Access of the TSIS Instrument = NASA\u2019s official website"]
-[5.843022346496582, 5.673224925994873, "[TT] Type of the X50M variant structure = X50M"]
-[8.361032485961914, 8.16965389251709, "[TT] Detector Array of the VNIR Spectrometer = 60 x 250 pixels"]
-[9.585264205932617, 7.026766300201416, "[TT] Spatial Resolution of the SLA-2 = Sub-kilometer"]
-[8.683782577514648, 3.8406240940093994, "[TT] Science Instruments of the Solar Orbiter = 10"]
-[5.55055046081543, 5.690639019012451, "[TT] Microcontroller of the OBC = ARM7"]
-[16.499765396118164, 3.5930583477020264, "[FF] Builder of the OneWeb = Telstra"]
-[10.002233505249023, 4.511369705200195, "[TT] Actuation Method of the SMA = Inductively using a network of voice coils and magnets"]
-[5.7707200050354, 7.3682026863098145, "[TT] Timing of the PLC = 2800-3700 Hz PRF (Pulse Repetition Frequency); 58-184 \u00b5s of data collection window"]
-[8.31786060333252, 1.8277558088302612, "[TT] Range of measurements of the Ocean SST = 3-4"]
-[6.665953159332275, 6.245362758636475, "[TT] Number of Elements of the PR = 128"]
-[5.200710773468018, 1.0779526233673096, "[FF] Collaboration Date with Turkey of the SPOT 6 & 7 = Dec. 20, 2012"]
-[3.8310763835906982, 6.272117614746094, "[TT] Number of Microstrip Patches per Array of the Active Antenna = 20"]
-[4.735660076141357, 0.37008729577064514, "[TT] Launch Date of the Restore-L = 2025"]
-[5.242716312408447, 5.205294609069824, "[TT] Processor of the Namuru V3.2 GPS Receiver = Actel SmartFusion A2F500 system on a chip that includes a hard wired ARM Cortex M3 processor"]
-[4.680305004119873, 0.28063467144966125, "[TT] Launch Date of the Myriade/AstroSat-100 = 29 June 2004"]
-[5.657524585723877, 3.230574369430542, "[TT] Equity Investment of the Eutelsat = $550 million"]
-[14.607601165771484, 6.639701843261719, "[TT] Battery Capacity of the Canopus Pipper = 2200 mAh"]
-[6.415052890777588, 5.132544994354248, "[FF] Module Type of the ADCS = Unknown"]
-[7.617509841918945, 9.042366027832031, "[TT] Incident Spectral Passband Wavelength of the GHGSat-D = 1600-1700 nm"]
-[11.686355590820312, 6.816756248474121, "[TT] Energy Range of the ART-XC = 6-30 keV"]
-[7.075403213500977, 1.3017377853393555, "[FF] Launch Date of the Spitzer Space Telescope = August 25, 2003"]
-[11.101430892944336, 5.889312744140625, "[TT] Material of the Baffles = SiC"]
-[2.9483542442321777, 2.411097764968872, "[FF] Measurement of the Copernicus Sentinel-5P = Nitrogen dioxide and other trace gases"]
-[9.76882553100586, -0.34638160467147827, "[TT] Altitude for Extended Mission of the SELENE/Kaguya = 50 km"]
-[8.135943412780762, 6.572262763977051, "[FF] Type of the TROPOMI = Passive grating pushbroom imaging spectrometer"]
-[12.136395454406738, 1.9822025299072266, "[FF] URL of the CartoSat-1 = http://www.gaf.de/.../pr_germany_euromap_antrix_01-2008.pdf"]
-[9.75943374633789, 7.21577262878418, "[TT] Number of Earth Viewing Positions of the Instrument = 28"]
-[9.372161865234375, 6.107973098754883, "[TT] Bias of the Electrostatic Analyzer = Negatively biased"]
-[9.45494556427002, 4.569875717163086, "[FF] Measurement Method of the RISE = Estimation of the precession and nutation of the spin axis"]
-[9.658987998962402, 4.770727634429932, "[TT] Controllers of the ACS = Proportional\u2013Integral\u2013Derivative"]
-[4.709930896759033, 2.922440767288208, "[TT] Provider of the ART-XC = RosKosmos (an IKI-led consortium)"]
-[6.954342365264893, 6.677067279815674, "[FF] Pumping Scheme of the Laser = Unknown"]
-[6.907495975494385, 7.533718585968018, "[TT] Beamwidth of the Reflector = 1.47\u00ba (azimuth) x 1.63\u00ba (elevation) for HH beam"]
-[6.59591007232666, 6.176292896270752, "[FF] CPU Recovery Time of the 300 V system = Unknown"]
-[8.418079376220703, 6.2904276847839355, "[FF] Imaging Payload Provider of the WorldView-4 = Raytheon"]
-[5.378584861755371, 0.4837038218975067, "[FF] Study Date of the EPIC = June 27"]
-[11.489408493041992, 3.5232980251312256, "[FF] Power of the UK-10 ion thruster hollow cathode = Unknown"]
-[4.166764736175537, 0.8707959651947021, "[FF] Booster Landing of the SpaceX CRS-24 = Successful"]
-[7.899731636047363, 3.9993762969970703, "[TT] Scattering Level of the External Occulter = Between 1 and 2 Rsun"]
-[8.868977546691895, 1.8037112951278687, "[TT] Second correction maneuver speed addition of the Webb = Around 6.3 mph (2.8 m/s)"]
-[4.152315616607666, 2.5707054138183594, "[TT] Launch Site of the SEOSAT-Ingenio = Europe's Spaceport in Kourou, French Guiana"]
-[7.802603721618652, 4.551911354064941, "[FF] Performance Characterization of the EarthCARE BBR Detectors = Unknown"]
-[5.746719837188721, 0.901416003704071, "[TT] Image Acquisition Date of the GOES-16 = 18 August 2021"]
-[5.540517807006836, 7.0430779457092285, "[TT] Data Rate of the ALOS-3 = 800 Mbit/s"]
-[6.5201311111450195, 5.819931983947754, "[TT] PRN of the GSAT-0102 = 12"]
-[11.275030136108398, 4.974589824676514, "[TT] Length of the NuSTAR = 33-foot-long (10-meter-long)"]
-[10.927937507629395, 3.748560667037964, "[TT] Solar Sail Deployment Test Support of the NEA Scout = Helium balloons"]
-[6.983755588531494, 3.8436262607574463, "[FF] Purpose of the Pilote experiment = Evaluate a new way of providing tactile and visual feedback to astronauts when operating robots"]
-[5.114716529846191, 2.056367874145508, "[TT] Mission Status of the GF-3 = Operational (nominal)"]
-[9.851335525512695, 6.269840717315674, "[TT] Mechanism of the Roof-top mirror = Double parallelogram linkage and flex pivots"]
-[14.542482376098633, 6.711272239685059, "[TT] Redundancy of the Battery = 1 pack loss allowed"]
-[9.033431053161621, 5.337662220001221, "[TT] Three-axis control accuracy of the GomX-3 = 3\u00ba"]
-[6.4611663818359375, 0.6772359609603882, "[FF] Article Date of the Landsat 9 = 9 January 2020"]
-[7.4958014488220215, 6.668704986572266, "[TT] Exposure Time of the Instrument = 33 ms"]
-[5.782715797424316, 1.7304332256317139, "[FF] Mission Description of the LARES 2 = Aerotecnica Missili & Spazio, The Journal of Aerospace Science, Technology and Systems, Vol. 97, No.3 July-September 2018, pp 135-144"]
-[9.806034088134766, -0.3870184123516083, "[TT] Operational Environment of the m-NLP system = LEO up to 1000 km altitude"]
-[8.398323059082031, 8.051878929138184, "[TT] Number of Pixels of the TDI Array = 7000 pixels for the panchromatic band"]
-[6.928689956665039, 5.692636013031006, "[TT] Availability of the SST = 98%"]
-[3.627385377883911, 4.667362689971924, "[FF] Sensor of the RISAT-1 = Synthetic Aperture Radar"]
-[4.55142068862915, 0.6482357382774353, "[TT] Launch Date of the ANGELS = December 18, 2019"]
-[5.868527889251709, 2.0361526012420654, "[FF] Image Content of the OPS-SAT = Uninhabited island north of Russia"]
-[8.418283462524414, 2.231618881225586, "[FF] Seismic Exploration of the InSight = Can feel whirlwinds pulling on the surface"]
-[7.225126266479492, 4.882366180419922, "[FF] Purpose of the MSPR-2 = Conduct a variety of experiments"]
-[13.37841796875, 7.3385233879089355, "[TT] Power of the CSS = 0.1 W"]
-[7.703028202056885, 3.5977063179016113, "[FF] Measurement Objective of the MPID = Collect information on orbital debris"]
-[4.482453346252441, 7.092623710632324, "[FF] Technology of the LRO Mini-RF Transmitter = MPM combines a solid state RF driver/preamplifier with a traveling wave tube amplifier"]
-[10.185022354125977, 3.101438522338867, "[TT] Deployment Mechanism of the CubeSat = ISS"]
-[6.754100799560547, -0.562415361404419, "[TT] Orbital Period of the Secondary Payloads = 103 minutes"]
-[12.16523551940918, 0.5943831205368042, "[TT] Consortium Lead of the PLATO = DLR Institute of Planetary Research"]
-[13.54658031463623, 5.916889190673828, "[TT] On-orbit Measured Solar Array Power of the Power Subsystem = Approximately 5 W greater than the predicted value"]
-[10.738840103149414, 5.563504219055176, "[TT] Ionized H Density of the RHESSI = \u22651015 cm-3"]
-[3.876854419708252, 7.858828067779541, "[TT] Modulation of the RF communications = FSK"]
-[12.333967208862305, 3.2606003284454346, "[TT] Propellant of the Webb = Exceeds the baseline estimate"]
-[13.213597297668457, 7.259779453277588, "[TT] Power Consumption of the WINGS suite = 1.3 W"]
-[6.325797080993652, -0.7614164352416992, "[TT] Spacewalk Elapsed Time of the Poisk = 7 hours 19 minutes"]
-[6.103288173675537, -0.47220364212989807, "[TT] Operation Duration of the KySat-2 = 4 months"]
-[13.381543159484863, 7.240359306335449, "[TT] Power of the AVNIR = 300W"]
-[9.50133228302002, 4.969621181488037, "[TT] Attitude Maintenance of the ACS = \u00b12\u00ba"]
-[9.276163101196289, 1.8608934879302979, "[FF] Image Binning of the HARP-2 = Fullsize full-resolution images"]
-[9.981389045715332, 9.063629150390625, "[TT] Effective FOV of the Channel 6 = 26 x 60 km"]
-[5.0215229988098145, 0.7953468561172485, "[FF] Development Start Date of the BDS = 1990s"]
-[7.588470935821533, 5.411634922027588, "[FF] Components of the SOT = OTA (Optical Telescope Assembly), FPP (Focal Plane Package)"]
-[5.803978443145752, 4.027453899383545, "[TT] Bus Type of the SPOT-6 & SPOT-7 = AstroBus-L (or AstroSat250)"]
-[10.765121459960938, 7.541494369506836, "[TT] Swath Width of the Pan = 20 km"]
-[11.213187217712402, 5.535804748535156, "[TT] Side Panel Thickness of the ESTCube-1 & -2 = 1 mm"]
-[8.234708786010742, 7.67538595199585, "[FF] Material of the CdZnTe detector technology = Cadmium Zinc Telluride"]
-[9.296924591064453, 5.070509910583496, "[TT] Attitude Determination Error of the AOCS = \u2264 10 \u00b5rad (2\u03c3) per axis"]
-[5.5498785972595215, 6.897840976715088, "[TT] Data Throughput of the CubeLCT = 4 GByte/day"]
-[10.796490669250488, 2.084916591644287, "[TT] Lead Scientist of the XMM-Newton X-ray observatory = Max Planck Institute for Extraterrestrial Physics"]
-[5.66816520690918, 5.2069220542907715, "[TT] Operating System of the BILGE = Integrity"]
-[4.9543938636779785, 3.709628105163574, "[TT] Provider of the ODTML = ONR (Office of Naval Research)"]
-[3.1192450523376465, 2.2896289825439453, "[FF] Application Categories of the Sentinel-3 = Numerical weather prediction, Climate change"]
-[8.845552444458008, 3.363661050796509, "[FF] Function of the Topsdie Ionospheric Sounder = Provide detailed global measurements of the electron distribution in the Earth's ionosphere"]
-[8.114209175109863, 2.696838140487671, "[TT] Measurement Domain of the HJ-1 = Atmosphere, Ocean, Land, Snow & Ice"]
-[2.892505168914795, 4.570330619812012, "[TT] Frequency of the PALSAR-2 = L-band"]
-[6.334630012512207, 1.8907004594802856, "[FF] URL of the Resurs-P1 = http://eng.ntsomz.ru/news/news_center/resurs-p_images_gallery_201505"]
-[10.157307624816895, 1.264465093612671, "[TT] Light Travel Time to Earth of the OJ 287 galaxy = 3.5 billion years"]
-[12.058655738830566, 6.279229164123535, "[TT] Proton Events of the AMS-02 = 2.42 x 109"]
-[6.8381876945495605, 1.1965820789337158, "[FF] Date of the Solar Storms = October and November of 2003"]
-[5.843657493591309, 2.2001521587371826, "[FF] Mission of the VIIRS = WSF-E"]
-[6.414860248565674, 6.784762382507324, "[TT] Optical Links of the EDRS-A = 20,000"]
-[10.393558502197266, 7.963435173034668, "[TT] Diameter of the Telescope = 60 cm"]
-[5.192223072052002, 2.3392038345336914, "[TT] Agency of the FormoSat-1 = NSPO"]
-[7.769008636474609, 7.274864673614502, "[TT] Data Rate of the Imager = 450 Mbit/s after compression"]
-[7.584454536437988, 4.388123989105225, "[FF] Sensor Complement of the F-1 = OLS,  SSH, SSJ/3, SSB, Contamination Monitor"]
-[6.957461833953857, -0.6007444858551025, "[TT] Orbit Localization Interval of the WEOS = 10 s"]
-[6.459846496582031, 1.8546923398971558, "[FF] URL of the Shuttle Radar Topography Mission = http://www.shuttlepresskit.com/sts-99/payload57.htm"]
-[8.723053932189941, 5.732400894165039, "[TT] Pointing Accuracy of the MSI instrument = 20 m"]
-[4.601961612701416, 2.9921205043792725, "[TT] Satellite Development Locations of the MetOp-SG = Toulouse, France and Friedrichshafen, Germany"]
-[6.806086540222168, 8.498703002929688, "[TT] Spectral Channels of the SAGE-III = 9 solar 290-1550 nm"]
-[5.341007709503174, 2.369873285293579, "[FF] Heritage of the OMPS = SBUV/2, TOMS and GOME"]
-[5.231039524078369, 8.029964447021484, "[TT] Frequency of the AEM = 20 Hz"]
-[7.364727020263672, 5.787318229675293, "[FF] Red-IR/UV Ratio of the Tatiana-2 = Varies"]
-[6.704133033752441, 4.509078025817871, "[FF] Function of the Formation Flying FDI (FF-FDI) = Coordinates the detection and flag processing coming from the different elements of the FFSW and provides alarms/warnings"]
-[4.495574951171875, 3.6678872108459473, "[FF] Overview of the GIOVE = GIOVE is the \"Galileo In-Orbit Validation Element\", a forerunner and technology demonstration project of the European Galileo constellation"]
-[7.677739143371582, 0.6568328738212585, "[FF] Purpose of the Lunar Flashlight = Detect naturally occurring surface ice believed to be at the bottom of craters on the Moon"]
-[6.75789737701416, -0.4765878915786743, "[TT] Orbit Period of the Harmony satellites = 98.74 minutes"]
-[7.8055572509765625, 5.368118762969971, "[FF] Purpose of the Microwave Imager Instrument = Remote sensing"]
-[12.132638931274414, 4.427983283996582, "[TT] Diameter of the DubaiSat-1 = 1.2 m"]
-[4.993366718292236, 0.47305190563201904, "[TT] Installation Date of the ACLS = 2 November 2018"]
-[4.144099712371826, 2.2533929347991943, "[TT] Launch Vehicle of the CADRE nanosatellite = ULA Atlas-V-401"]
-[1.3676495552062988, 2.7828681468963623, "[TT] Principal Absorbing Constituents of the Band 10 = Water vapor"]
-[8.514140129089355, 5.42238187789917, "[TT] Accuracy of the Satellite = Less than 1km"]
-[5.310032844543457, 4.071498394012451, "[FF] Number of Options for Satellite Navigation System of the UK = Around 10"]
-[9.488480567932129, -0.9405539035797119, "[TT] Longitude Gap of the Fast-sampling orbit = 25.714\u00ba"]
-[3.9450149536132812, 6.301673412322998, "[TT] Antenna Elements of the NanoCom Ant430 = 4"]
-[4.476900100708008, 2.9239845275878906, "[TT] Location of the GNOR = ESA/ESTEC, Noordwijk The Netherlands"]
-[10.419957160949707, 2.8257896900177, "[TT] Communication Protocol of the Nanosatellite = Bluetooth"]
-[8.552437782287598, 8.340253829956055, "[TT] Alpha (\u03b1) of the FCA = 0.2"]
-[8.081686973571777, 8.416264533996582, "[TT] Effective Absorption of the MLI = \u03b1 < 0.05"]
-[5.468663215637207, 4.423244476318359, "[TT] Ground Architecture of the SENSE = SMC/SD"]
-[7.764992713928223, 6.5038323402404785, "[FF] Images Collected of the ABI Scan Mode 6 = 30-second Mesoscale, 5-minute CONUS, 10-minute Full Disk"]
-[8.26452922821045, 8.80384635925293, "[TT] Width of the Fe XIV = ~0.1 nm"]
-[9.679681777954102, -0.3309738039970398, "[TT] Elevation of the Mount Aso = 1592 m"]
-[8.703947067260742, 3.4280357360839844, "[FF] Objective 2 of the CITRIS = Provide a global map of ionospheric densities and irregularities to improve current models of the ionosphere"]
-[14.566303253173828, 6.630700588226318, "[TT] Type of the Battery = Li-ion (rechargeable)"]
-[9.367135047912598, 4.105505466461182, "[FF] Type of the Sunshield = Highly Specular"]
-[4.812829971313477, 4.046548843383789, "[TT] Development Program Name of the SiREUS = SiREUS-FExp"]
-[5.399339199066162, 6.3021440505981445, "[TT] Die Capacity of the SDR-SDRAM = 512 Mbit"]
-[6.254631996154785, 5.925950050354004, "[TT] Quantity of the Power Distribution Modules = 3"]
-[7.457615852355957, 7.312649250030518, "[TT] Look Direction Switch Frequency of the CHORUS = About 15-20 times per day"]
-[8.464141845703125, 5.559834957122803, "[TT] Open Service Velocity Accuracy of the COMPASS/BeiDou = 0.2 m/s"]
-[5.753925800323486, 2.011218309402466, "[TT] Technology Readiness Level of the SMDC-ONE = TRL-7"]
-[2.898280620574951, 4.524556636810303, "[FF] Radio Frequency Interference of the PALSAR-2 = Issue"]
-[8.475927352905273, 6.990185737609863, "[TT] Instrument Type of the AVNIR = High resolution optical imagers"]
-[5.20094108581543, 2.314791679382324, "[TT] Mission Type of the CuPID = Non-EO"]
-[10.667659759521484, 7.132226943969727, "[TT] Footprint of the 1 = 25.8 x 17.5 km"]
-[7.541431427001953, 2.038431406021118, "[FF] Band 3 of the Landsat TM = Chlorophyll absorption, plant type discrimination"]
-[3.9363255500793457, 1.9755779504776, "[TT] Launch Vehicle of the Yubileyniy-2/MiR = Rockot/Briz-KM"]
-[7.844962120056152, -0.2627236545085907, "[TT] Date of the High-Latitude Cold-Season Snowfall Campaign = January 15, 2012 until March 3, 2012"]
-[9.886054039001465, 4.170713424682617, "[TT] Search Coil Length of the ULF Sensor = 20 cm"]
-[5.932623863220215, 4.569567680358887, "[FF] Operations Approach of the Twinkle = Streamlined, robust, safe, and high availability"]
-[6.3546223640441895, 3.9562642574310303, "[FF] Components of the Spacecraft Plug-n-Play Avionics (SPA) = Data transport, power delivery, time synchronization, single point ground connection, minimal \"hooks\" for self-description"]
-[7.997305870056152, 0.11294310539960861, "[TT] Destination of the CE-4R satellite = Moon Earth L2 point"]
-[13.05542278289795, 7.351574897766113, "[TT] Power Consumption of the Detector = 300 W"]
-[6.2915239334106445, 8.637798309326172, "[TT] Data Mode of the TanDEM-X = Stripmap single polarization (HH) mode"]
-[5.692830562591553, 7.136951923370361, "[TT] Data Rate (max) of the MHX-2400 = 83 kbit/s"]
-[14.03099536895752, 7.166436672210693, "[TT] Output Voltage (Redundant) of the LVPS Board = +1.5 V"]
-[6.535689830780029, -0.7993505597114563, "[TT] Drift LTAN of the AlSat-2B = 8:45"]
-[6.4700117111206055, 5.062857627868652, "[FF] Module Type of the STRx = Unknown"]
-[5.604705333709717, 1.093260645866394, "[TT] Sent to NASA Date of the Diwata-1 = January 18, 2016"]
-[8.95112419128418, 5.346749305725098, "[TT] Orbit Shift Distance of the GomX-4B = Up to 2000 km"]
-[3.1868057250976562, 2.333441734313965, "[FF] Land Cover Monitoring of the Sentinel-2 = Fire damage, deforestation, urban growth"]
-[13.334921836853027, 7.402950286865234, "[TT] Tx power of the HPA = 25 W"]
-[7.365976333618164, 1.607071876525879, "[TT] Latency of the GDP buoys = 2 months"]
-[8.128609657287598, 0.1361188441514969, "[TT] Launch Date of the Meteor-M2 spacecraft = July 8, 2014"]
-[14.651660919189453, 6.746438980102539, "[TT] Battery of the QuickBird-2 = 40 Ah NiH2"]
-[13.264410018920898, 5.288118362426758, "[TT] Weight per Unit Area of the Solar Panels = Half of the traditional solar arrays"]
-[9.551236152648926, 5.105569839477539, "[FF] Component of the Cryomag rectifiers = Unknown"]
-[9.298080444335938, 3.160740852355957, "[TT] FOV for Narrowband Imaging of the 20 cm off-axis internally occulted coronagraph = 1.05 to 1.5 Rsun"]
-[7.521202087402344, 6.863062381744385, "[TT] Cadence of the Pulse Height Analysis = 1 minute"]
-[7.224762439727783, 4.658438682556152, "[TT] Mounting Location of the SAWs = Externally"]
-[8.873921394348145, 4.497589111328125, "[FF] Attitude Sensing of the IRS-1C and IRS-1D = Star sensors, Earth sensors and gyros"]
-[13.41978645324707, 7.182993412017822, "[TT] Output Power of the PPM = 300 W"]
-[10.098443984985352, 7.867160320281982, "[TT] Telescope Modules of the LWFT instrument = 5"]
-[5.284860610961914, 5.762917995452881, "[TT] Spacecraft Housekeeping Data Bus of the SAMPEX = Mil-Std-1773B fiber optic data bus"]
-[4.8609089851379395, 0.19103653728961945, "[TT] Launch Date of the Crew-1 = Oct. 31"]
-[14.619928359985352, 6.6079020500183105, "[TT] Battery Capacity of the F-15 and F-16 DMSP satellites = Increased"]
-[5.047945976257324, 0.901090681552887, "[TT] Launch Date of the OPS-SAT = 2012"]
-[5.729674339294434, 4.8214945793151855, "[FF] Communications of the LPT = GN/SN (Ground Network/Space Network), GPS Tracking and Orbit Determination, Internet Protocol (IP), Range Safety"]
-[8.81698989868164, 5.412339687347412, "[TT] Intelligent Pointing System of the TANSO-FTS-2 = Present"]
-[6.087398529052734, -0.4017314016819, "[TT] Drift Recovery Phase Duration of the CanX-4&5 = Several Days"]
-[14.32472038269043, 3.208466053009033, "[TT] Mass of the Enxaneta = Approximately 10 kg"]
-[9.51463508605957, 5.513144016265869, "[TT] Azimuth Rotation Axis of the CPA = Perpendicular to the FUS baseplate"]
-[6.414170265197754, 4.088854789733887, "[FF] Ground Segment Sections of the Helios-2 = User ground segment, programming loop"]
-[4.054681301116943, 6.347267150878906, "[FF] Downlink Antenna of the Satellite = Independently steerable"]
-[8.168251037597656, 1.3137340545654297, "[FF] Parameter of the IMI = Freeze/thaw - Soil surface parameters"]
-[13.634444236755371, 5.812166213989258, "[TT] Average Power of the Solar Cells = 9.1 W"]
-[9.227468490600586, 8.598745346069336, "[TT] Slit Half Height of the WTS1 and WTS2 = 1\u00ba"]
-[11.810262680053711, 6.730626583099365, "[TT] Energy Measurement Range of the HEPD = 1 - 1000 MeV"]
-[7.78822660446167, 2.4176642894744873, "[FF] Data Products of the HY-1C = Ocean color products, SST, NSST"]
-[8.010448455810547, 8.62448787689209, "[TT] Spectral Coverage of the Hyperion = 400 - 2500 nm"]
-[5.387179851531982, 0.09126616269350052, "[TT] Operation End Date of the BIRD = December 2005"]
-[14.407243728637695, 6.597232341766357, "[TT] Type of the IMPS = Integrated Microelectronic Power Supply"]
-[10.681629180908203, 7.133792877197266, "[TT] Footprint of the 3 = 25.8 x 17.5 km"]
-[6.232745170593262, 6.417502403259277, "[TT] Group Delay Stability of the NAVANT = Of 21 ps"]
-[7.104145526885986, 0.2957763671875, "[TT] Cross-Track Motion Control of the CloudSat = Within \u00b11 km of the CALIPSO ground track"]
-[7.650328159332275, 1.6014983654022217, "[FF] Analysis Capability of the ROSE-L = Broad forest types"]
-[7.1099677085876465, 6.373318672180176, "[TT] Feedhorns of the MIS Instrument = 12"]
-[6.20273494720459, 7.2504754066467285, "[TT] Output Data Stream of the LIAU = 16-bit wide"]
-[7.916792869567871, 5.639174461364746, "[FF] Conference Presentation Date of the Korean Spaceborne Microwave Radiometer on STSat-2 = July 25-29, 2005"]
-[6.908141136169434, 5.285123825073242, "[FF] Function of the DPU = Image processing and non-destructive compression"]
-[7.277920722961426, 2.094839334487915, "[TT] Platform Type of the Carbonite Smallsat = High performance generic"]
-[4.627240180969238, 0.5382786393165588, "[TT] Launch Dates of the GOES-N, -O, -P = May 2006, June 2009, March 2010"]
-[6.106110572814941, 0.7324221730232239, "[TT] Geostationary Orbit Start Date of the WINDS = Late June 2008"]
-[9.46982192993164, 6.118185043334961, "[TT] Incidence Angle of the ALOS = 8-60\u00ba"]
-[12.403239250183105, 0.625868558883667, "[TT] Number of Telescopes of the PLATO = 26"]
-[11.72913932800293, 3.2609803676605225, "[TT] Number of Thrusters of the 8 thrusters = 8"]
-[11.84641170501709, 6.639126777648926, "[FF] Proton Energy of the GALS-VE = > 600 MeV"]
-[5.373264789581299, 7.732019901275635, "[TT] Amplification Factor of the Op-amp = 2.4"]
-[4.197763442993164, 2.108903169631958, "[TT] Launch Site of the NigeriaSat-1 = Plesetsk, Russia"]
-[7.9325361251831055, 4.259122848510742, "[TT] Measurement Frequency of the Operational Linescan System (OLS) = Twice each day"]
-[4.665838718414307, 7.1220703125, "[FF] Modulation and Coding of the S-band subsystems = Impact on the bit rate, consumption, and implementation complexity"]
-[4.4854607582092285, 2.891657590866089, "[TT] Location of the PDAS = Fucino (Italy)"]
-[8.194924354553223, 8.275482177734375, "[FF] Spectral Bands of the Pushbroom imager = Pan: 450-900 nm, MS: 450-520 (blue), 520-600 nm (green), 630-690 nm (red), 760-900 nm (NIR), SWIR: 1000-2400 nm (experimental)"]
-[9.314800262451172, 4.812135219573975, "[TT] Coarse Attitude Control Duration of the XACT = 20 minutes or more"]
-[4.871031284332275, 1.1036020517349243, "[TT] Delivery Date of the TANSO-FTS-2 = June 13, 2018"]
-[7.46239709854126, 3.32065486907959, "[TT] Pixel Size of the GHGSat = 30 x 30 m"]
-[5.197554588317871, 6.606307506561279, "[TT] Purpose of the Feeder Link = High-rate communication link between the payload and the HUB station"]
-[9.422247886657715, 3.7563087940216064, "[FF] Purpose of the Nexus S magnetometer = Measuring the local magnetic field"]
-[14.583611488342285, 6.626880645751953, "[TT] Battery Status of the Rumba = Weak"]
-[7.114007949829102, 4.905961990356445, "[FF] Manufacturing of the AOCE = Difficult to produce by repetitive manufacturing"]
-[9.66612720489502, 8.467025756835938, "[TT] FOV of the Receiving Antenna = \u00b11.5\u00ba"]
-[8.077022552490234, 9.16250991821289, "[TT] Ellipse Axis C of the Short Wavelength Band = 242.6 mm"]
-[13.994233131408691, 2.95988392829895, "[TT] Mass of the FalconSat-6 = 181 kg"]
-[10.710066795349121, 1.2849020957946777, "[TT] Size of the TOI 451 = 12% smaller than our Sun"]
-[8.267257690429688, 7.313131809234619, "[TT] Detector Type of the ELENA = MCP (Micro-Channel Plate) detectors"]
-[5.5682525634765625, 2.4327661991119385, "[FF] Location of the SPIV = University of Rome"]
-[10.065823554992676, 2.005600929260254, "[FF] Funding Status of the Chandra X-ray Observatory = Funded through 2025 with options to extend through 2030"]
-[6.483306407928467, 2.2221367359161377, "[FF] URL of the Gigabit Satellite Network = http://acts.grc.nasa.gov/docs/SCAN_20010911135953.PDF"]
-[7.673741340637207, -0.17839118838310242, "[TT] LTAN of the Meteor-M2 = 9:30 hours"]
-[8.46985912322998, 1.8049436807632446, "[FF] Temperature of the Farside Hemisphere = Cooler"]
-[11.771467208862305, 0.09810470044612885, "[FF] Data Usage of the Transiting Exoplanet Survey Satellite (TESS) = Discovering Alpha Draconis"]
-[5.593897342681885, 1.2271969318389893, "[FF] Test Date of the LARES = Sept. 27-Oct. 1, 2010"]
-[9.05256462097168, 7.45576286315918, "[FF] Resolution of the ALSAT-2B = 2.5m for the panchromatic band, and a 10 m for the four multispectral bands"]
-[6.42329216003418, 5.137662410736084, "[FF] Function of the Device = Transfer information at the end of the integration cycle"]
-[2.91640567779541, 4.5407304763793945, "[TT] Maximum Data Rate of the PALSAR = 240 Mbit/s"]
-[8.14482593536377, 2.6253557205200195, "[FF] Measuring Condition of the UVI instrument = Atmospheric correction of turbid water, dissolved organic matter"]
-[11.037386894226074, 2.8542659282684326, "[TT] Microsatellite Diameter of the ANDE-2 = 48.26 cm"]
-[8.308873176574707, 0.06862281262874603, "[TT] Comet Encounter Date of the ICE (International Cometary Explorer) = September 11, 1985"]
-[7.838583946228027, 1.1636296510696411, "[FF] Date of the West coast wildfires = 11 September 2020"]
-[5.999021053314209, -2.3362300395965576, "[TT] Orbit Inclination of the Kondor-E1 = 74.74\u00ba"]
-[9.38568115234375, -0.2267378270626068, "[TT] Orbit Perihelion Distance of the V7GA = 9.86 RS"]
-[6.42291259765625, 3.479637622833252, "[FF] Use of the DMSP-20 = Weather forecasting"]
-[10.277193069458008, 3.9847569465637207, "[TT] AstroTube Boom of the AlSat Nano = Deployed and stowed multiple times, including full 1.5 m length"]
-[6.964626789093018, -0.7583768963813782, "[TT] Orbital Period of the L 98-59d = 7.5 days"]
-[7.570943355560303, 2.3087778091430664, "[FF] Coverage Area of the HawkEye 360 = Millions of square kilometers"]
-[8.19471263885498, 0.5424203872680664, "[FF] Location of the Lake Nasser = Southern Egypt and northern Sudan"]
-[8.144638061523438, 3.091128349304199, "[FF] Background Illumination to Lightning Signal Ratio of the GLM = Often exceeds 100 to 1"]
-[9.06737995147705, -0.5734928250312805, "[TT] Science Target Orbit Perigee of the ABEX = 300 km"]
-[6.4455389976501465, 1.9665061235427856, "[FF] Mission URL of the PeruSAT-1 = http://www.airbus.com/space/earth-observation/perusat.html"]
-[5.09574556350708, 4.30861234664917, "[FF] Additional 30,000 Starlink satellites of the SpaceX\u2019s Proposal = Urgency of the issue"]
-[14.225764274597168, 3.23858380317688, "[TT] Mass of the Aquahab = 18 kg"]
-[5.601161956787109, 0.9415738582611084, "[TT] De-orbiting End Date of the ERBS satellite = August 15, 2003"]
-[5.316812038421631, 3.2173056602478027, "[TT] Manufacturer of the WorldView Legion = Maxar company SSL (Space Systems Loral)"]
-[4.4271559715271, 2.9767656326293945, "[TT] Location of the ESA = Esrange, Kiruna, Sweden"]
-[9.848142623901367, -0.599612295627594, "[TT] Altitude of the Galileo = 23,222 km"]
-[7.957659721374512, 2.2478225231170654, "[FF] Data Usage of the ISS-RapidScat = Tropical Cyclone Forecasting"]
-[9.162155151367188, 3.4773714542388916, "[FF] Purpose of the GEOTAIL = Measure the flow of energy and its transformation in the magnetotail created by the interaction between the solar wind and the Earth"]
-[4.832900047302246, 6.010505676269531, "[FF] Function of the IFS = Distribute the TDMA signals of each time slot to the beams"]
-[11.228144645690918, 5.74385404586792, "[TT] Material of the JUICE = Non-magnetic material"]
-[6.330345153808594, 5.562474250793457, "[FF] Data Storage of the SSB = Stores subarrays and full frame images"]
-[9.728401184082031, 8.126115798950195, "[TT] Image Size of the Lens = 24\u00ba x 24\u00ba"]
-[9.893133163452148, 8.968493461608887, "[TT] IFOV of the IR Channels = 1 km (vertical) x 13 km (horizontal)"]
-[6.46298885345459, -0.4946385324001312, "[TT] Duration of the Transfer Phase = 7 days"]
-[13.896267890930176, 3.853074789047241, "[TT] Mass of the Sensor Unit = 4.815 kg"]
-[5.525870323181152, 2.6677844524383545, "[TT] Affiliation of the MAHRSI = NRL (Naval Research Laboratory)"]
-[10.45920467376709, 5.67972469329834, "[TT] Thermal Environment of the RTV Adhesive = -100 to +70\u00baC"]
-[3.20745849609375, 4.9876933097839355, "[TT] HRS Resolution of the RISAT-SAR = < 2 m"]
-[7.711541652679443, 8.89832592010498, "[TT] Spectral Range of the Spectral Band A = 0.45 - 0.52 \u00b5m"]
-[8.059931755065918, 6.389631271362305, "[FF] Unknown of the RapidEye = Unknown"]
-[5.521207809448242, 6.355750560760498, "[TT] Internal Data Storage of the RAMIS = 2"]
-[10.21120834350586, 5.733968734741211, "[FF] Function of the TPM = Provides temperature control management of the DMAC instrument"]
-[8.154390335083008, 3.0178020000457764, "[FF] Objectives of the IMM = Unambiguous association of lightning with TLEs and TGFs, better understanding of the physical mechanisms behind them, variation in TLEs and TGFs"]
-[10.217026710510254, 2.1009600162506104, "[FF] X-ray emission source of the Chandra X-ray Observatory = Detected"]
-[9.762711524963379, 4.576247692108154, "[TT] Spin Rate of the Y-Thomson mode = 2\u00ba/s"]
-[6.589653491973877, 1.0841201543807983, "[FF] Unknown of the Formosat-2 = Unknown"]
-[13.824652671813965, 5.694938659667969, "[TT] Solar Cells Efficiency of the Tsubame = 27.5%"]
-[7.304976940155029, 8.255455017089844, "[FF] SNR of the GOSAT-2 = b3: >200 (46/0.106)"]
-[8.745980262756348, 3.5339205265045166, "[FF] Leading Noise Terms of the Satellite = Electric disturbances"]
-[9.168386459350586, 1.4608502388000488, "[TT] Current Location of the Voyager 2 = Interstellar space"]
-[11.811452865600586, 6.663803577423096, "[TT] Proton Energy Range of the REPT = 17 to >100 MeV"]
-[6.697807788848877, 3.440389394760132, "[FF] URL of the AMS = http://ams.cern.ch/AMS/ETB/Appendix%20A-AMSonISS_Technology_Applications_Interplanetary.pdf"]
-[7.827723026275635, -0.1347113698720932, "[TT] Launch Time of the Meteor-M2 spacecraft = 15:58:28 UTC"]
-[8.259021759033203, -0.9814302921295166, "[TT] Orbit of the ICESat-2 = From pole to pole"]
-[9.304779052734375, 7.486123085021973, "[TT] Pixel Size at Nadir of the CIPS = ~2 km"]
-[7.811407089233398, 3.0530996322631836, "[FF] Number of Instruments of the CO2 ground monitoring network = 6"]
-[5.4119672775268555, 3.940281629562378, "[TT] Number of Satellites of the HY-2 = 8"]
-[7.1041364669799805, 4.742403984069824, "[FF] Function of the MR LR = Provide a stowed interface for the Main Reflector providing a load path through the composite structure to the spacecraft interface"]
-[7.066734790802002, 8.213873863220215, "[TT] Measurement Channels of the CAPI = 5"]
-[10.853132247924805, -0.29847216606140137, "[TT] Science Phase of the TanDEM-X = 2014 to mid of 2016"]
-[8.889754295349121, 4.640867710113525, "[FF] ADCS Equipments of the TDS-1 = Gyros and magnetometers"]
-[6.406735420227051, 3.938706874847412, "[FF] Payloads of the DarkCarb = MWIR"]
-[7.462945461273193, 7.861138820648193, "[TT] Dynamic Range of the Instrument = >100"]
-[7.967855453491211, 8.46477222442627, "[TT] Parameters of the Reed Solomon = 255/223"]
-[7.775222301483154, 2.331763982772827, "[FF] Coverage of the ISS-LIS = CONUS (CONtinental US)"]
-[12.463293075561523, 0.6471924781799316, "[TT] Height of the Plato Camera = 80 cm"]
-[6.595426559448242, 0.11440839618444443, "[FF] Campaign Duration of the CryoSat-2 = Up to four months"]
-[7.219125270843506, 1.2092317342758179, "[TT] Sample Tubes of the Perseverance rover = 43"]
-[6.9872846603393555, 1.0714422464370728, "[FF] Mission Name of the Solar Probe Plus = Solar Probe Plus"]
-[7.38649845123291, 0.30666694045066833, "[FF] URL of the OSIRIS-REx = http://arc.aiaa.org/doi/pdf/10.2514/6.2014-1721"]
-[5.335233211517334, 7.042979717254639, "[TT] Data Rate of the GAMALINK = Up to 80 Mbit/s"]
-[14.606030464172363, 6.627960681915283, "[TT] Battery type of the EPS = Li-ion"]
-[5.339609146118164, 0.5390920639038086, "[FF] Proceedings Date of the SSMIS = Aug. 1993"]
-[7.775824069976807, 2.3749496936798096, "[FF] Function of the Poseidon-4 = Measure the range between the satellite and the mean ocean surface, determine significant wave height and wind speed, and provide the correction for the altimeter range path delay in the ionosphere"]
-[6.953983783721924, -0.48379504680633545, "[TT] Local Time of Ascending Node of the COMPASS-1 = 9:15 AM"]
-[5.586390972137451, 5.665247917175293, "[TT] Microprocessor of the OBC = 10 MIPS T805"]
-[10.035863876342773, -1.4528073072433472, "[TT] Orbit Inclination of the PRISMA = 98.19\u00b0"]
-[11.89957332611084, 6.612317085266113, "[TT] Energy Range of the Electron spectrum = 1 GeV to 500 GeV"]
-[5.9276347160339355, 7.568207263946533, "[TT] Sampling Rate of the CIP = 1 and 8 Hz"]
-[6.777091026306152, 6.36692476272583, "[TT] Number of Off-Source Pointings of the Mode 1 = 6"]
-[3.1333720684051514, 2.1640243530273438, "[FF] Data Contribution of the Copernicus Sentinel-1 = Included in the research"]
-[4.3823466300964355, 7.782523155212402, "[TT] Uplink Frequency of the Myriad RF board = 300 MHz up to 3.8 GHz"]
-[9.534690856933594, 0.8331787586212158, "[TT] Closest Approach Time of the Rosetta = 18:10 CEST"]
-[10.166865348815918, 3.205111265182495, "[FF] Mission of the AstroBio CubeSat = Biomolecule-detection"]
-[9.71986198425293, 1.4042937755584717, "[TT] Images Acquired of the Pleiades = More than 150"]
-[4.257556438446045, 7.301558971405029, "[TT] FIFO Buffer of the X-band transmitter = On-board"]
-[6.009921550750732, 1.8043121099472046, "[FF] Flight Dynamics of the Retrieval of the Eureca = Unknown"]
-[9.707963943481445, 6.2698140144348145, "[TT] Blackbody Calibration and Space Look of the Mirror = Slewing the mirror at a rate of 10\u00ba/s"]
-[6.26442813873291, 5.160932540893555, "[FF] Design of the Resurs-P = Modular"]
-[8.865713119506836, 8.63163948059082, "[FF] Slit Image Coalignment Requirement of the Spectrometer Channel = Within a small fraction of their size on the focal plane (~250 \u00b5m)"]
-[4.336881160736084, 0.9526742696762085, "[TT] Operation Start Year of the Argos = 1978"]
-[13.347355842590332, 7.8359551429748535, "[TT] Transmitter Output Power of the X-band data transmission = 10 W"]
-[4.36611270904541, 3.0084993839263916, "[FF] Location of the ISS = Iberian Peninsula"]
-[10.822222709655762, 3.932703971862793, "[FF] Uplink Margins of the CanX-2 = Sufficient"]
-[3.6260340213775635, 4.506618022918701, "[FF] Interface of the GISAR = MCC"]
-[6.109415531158447, 1.2615963220596313, "[FF] Publication Date of the Two-stage light-gas gun = 2010"]
-[6.319698333740234, 6.5826520919799805, "[TT] AGC Time Constant of the Receiver = \u2264 40 x10 -9 ms"]
-[7.132174491882324, 2.51363468170166, "[FF] Publisher of the Observation of the Earth and Its Environment = Springer Verlag"]
-[10.230424880981445, 4.64040994644165, "[TT] Momentum Envelope of the CMG = 0.8 mNms"]
-[10.569541931152344, 0.8959187865257263, "[FF] Orbit Ratio of the Kepler-1649c = 9:4 with outer planet"]
-[13.83676528930664, 5.689116954803467, "[TT] Efficiency of the Solar Panels = 28%"]
-[3.904017210006714, 7.848089218139648, "[TT] Payload Data Modulation of the Satellite = PCM/BPSK"]
-[6.477965354919434, 3.3334996700286865, "[TT] Mission Objective of the OSMA-1 = Conduct a series of demonstrations of in-space robotic assembly of an antenna and a boom"]
-[7.631218910217285, 3.453909158706665, "[TT] Impact Test Date of the DebriSat = 15 April, 2014"]
-[3.5149636268615723, 5.016815662384033, "[TT] Configuration of the SARP-2 = Improved SARP with memory"]
-[4.937251567840576, 8.29342269897461, "[TT] Spectral Bands of the CIMR = 1.4, 6.9, 10.65, 18.7, and 36.5 GHz"]
-[9.354659080505371, 5.00707483291626, "[TT] Attitude Accuracy of the DubaiSat-1 = 0.2\u00ba"]
-[9.153441429138184, 7.557758808135986, "[TT] Spatial Resolution of the Multispectral Instrument (MSI) = 60 m"]
-[10.015564918518066, 2.9482383728027344, "[FF] Date of the Welcome to the 2011 CubeSat Developer's Workshop = April 20-22, 2011"]
-[9.166487693786621, 7.456849098205566, "[TT] Pixel Size of the SCAMP Camera = 1.6 km"]
-[10.026102066040039, -1.4634000062942505, "[TT] Orbit Inclination of the HORYU-2 = 98.19\u00ba"]
-[7.098515033721924, 8.096675872802734, "[FF] SNR Ratio of the Instrument = Increased"]
-[8.659542083740234, 2.0808796882629395, "[TT] Wind Speed Measurement Accuracy of the SMMR = 2 m/s for winds ranging from 7 m/s to about 50 m/s"]
-[10.239953994750977, 7.2405242919921875, "[TT] Ground Range x Product Length of the High Resolution Spotlight = 10 x 5 km"]
-[5.092769145965576, 5.982815742492676, "[FF] VO Protocols of the Gaia = TAP for table, Simple Access Protocol for spectra"]
-[6.868275165557861, 8.86082649230957, "[FF] Spectrum Expansion of the POLDER-P = By adding a band in the near-infrared, POLDER-P expands the spectrum being analyzed"]
-[4.828849792480469, 6.520271301269531, "[TT] Components of the SES = Transmitter, receiver and digital signal processor"]
-[3.4364073276519775, 4.7887773513793945, "[TT] Development Completion Date of the S-band SAR = March 9, 2021"]
-[9.84920883178711, -0.4401950240135193, "[TT] Altitude of the CanX-6/NTS = 630 km"]
-[7.707465648651123, 2.055267333984375, "[FF] Dead Zone Impact of the Gulf of Mexico = Impacts fish and the regional economy"]
-[5.431979656219482, 6.660887241363525, "[TT] Data Download Limit of the STARE Satellite = About 1Mb per day"]
-[10.96783447265625, 2.966909885406494, "[TT] Size of the Nanosatellite = 10 cm x 10 cm x 34.5 cm"]
-[8.942700386047363, 3.7652740478515625, "[FF] NLC Observation Bottom-Out of the AIM spacecraft = During solar maximum"]
-[5.059813499450684, 0.1447492092847824, "[TT] End of Life Date of the ERS-2 = 04 Jul 2011"]
-[11.477383613586426, 5.16765022277832, "[TT] Collecting Area of the NICER = > 1800 cm2"]
-[13.76783275604248, 6.232045650482178, "[FF] Function of the LEDs = Indicate the power status of the main power line and of single battery low-voltage"]
-[9.610936164855957, 8.273262977600098, "[TT] Field of View of the NFI = ~2\u00ba"]
-[7.276669979095459, 5.706334114074707, "[FF] Proximity Electronics of the FPA = Provide clock pulses and biases for the operation of the detector array"]
-[11.165425300598145, 4.977569103240967, "[TT] Carries of the PolyITAN-2-SAU = FIPEX"]
-[12.050956726074219, 4.683304786682129, "[TT] Housing Dimensions of the MuREM = 10 x 6 x 6 cm"]
-[4.416110515594482, -0.05516010895371437, "[TT] Launch Date of the Starliner = Thursday, May 19"]
-[5.510679721832275, 7.113299369812012, "[TT] Data Transmission Rate of the MSR = 2000 MHz"]
-[5.7657575607299805, 1.126607894897461, "[FF] Announcement Date of the Boeing Pico-Satellite Mission = April 19, 2007"]
-[8.270251274108887, 3.499948740005493, "[FF] Sea Surface Calibration Mode of the EarthCARE satellite = CPR in Sea Surface Calibration mode"]
-[7.195720672607422, 7.955106735229492, "[TT] Number of Spectral Channels of the ABI = More than three times the current GOES Imagers"]
-[6.908149242401123, 7.523049354553223, "[TT] Beam width of the VNIR = 5.5 \u00b5rad"]
-[5.188690185546875, 3.6526589393615723, "[TT] Satellite of the Sentinel-5 = MetOp-SG"]
-[5.6895551681518555, -0.8646345734596252, "[TT] Design Life of the TRMM = 3 years"]
-[8.276632308959961, 8.568970680236816, "[TT] Spectral Range of the Spectrometer = 5-28.5 \u00b5m"]
-[5.364525318145752, 0.38107869029045105, "[FF] Launch Date of the CHEOPS = 18 December 2019"]
-[11.653334617614746, 6.851099014282227, "[TT] Energy Region of the ART-XC = 6-11 keV"]
-[5.340230464935303, 1.1791654825210571, "[FF] Mission Start Date of the SMAP = March 3, 2012"]
-[4.341714382171631, 0.31860998272895813, "[TT] Launch Date of the JPSS-1/NOAA-20 = Nov. 18, 2017"]
-[7.583641052246094, 4.948905944824219, "[FF] Components of the Spacecraft Bus = Star tracker, GPS receiver, IMU, fine sun sensor, magnetometer, reaction wheels, EPS, batteries, radio, antenna"]
-[13.444123268127441, 5.541612148284912, "[TT] Solar Arrays of the EPS = 6"]
-[8.15775203704834, 7.595972537994385, "[TT] Detector Elements Downlinked of the AHI = 7,856"]
-[6.0294365882873535, 0.966829240322113, "[TT] Product Specification Date of the Planet Imagery = April 2017"]
-[10.483381271362305, 6.920267581939697, "[TT] Diameter of the Primary Mirror = 450 mm"]
-[8.369636535644531, 6.905656814575195, "[TT] Revisit Time at 20\u00b0 off nadir or less (0.51 m GSD) of the WV60 imager = 5.9 days"]
-[3.4844517707824707, 5.160855293273926, "[FF] Technology of the SAR Antennas = DBF (Digital Beam Forming)"]
-[10.992471694946289, 2.8818044662475586, "[TT] Dimensions of the Microsatellite = 540 mm (height), 370 mm (full diameter)"]
-[9.96448040008545, -0.028675701469182968, "[TT] Altitude of the GRACE-FO Satellites = About 490 km"]
-[11.177330017089844, 4.248945713043213, "[TT] Area of the Icarus-1 = Approximately 6.7 m2"]
-[6.871220111846924, 4.719738960266113, "[FF] User of the P-POD = Unknown"]
-[7.884853363037109, 4.811025619506836, "[TT] Sensitivity of the Phoenix receiver = High levels of radiations"]
-[8.166244506835938, 3.27004337310791, "[FF] Purpose of the PREFIRE = Measure variations in Far-Infrared (FIR) emissivity and the greenhouse effect"]
-[5.0147175788879395, 8.358917236328125, "[TT] Radiometer Bands of the MicroMAS-2 = Near 90, 118, 183, and 206 GHz"]
-[6.513344764709473, 4.63208532333374, "[FF] Grid cleaning, short-circuit opening (function for failure) of the CM = Not specified"]
-[5.9480485916137695, 3.5245580673217773, "[FF] Cost-Effective of the Satellite = Yes"]
-[9.650979995727539, -0.3066933751106262, "[TT] Perilune Altitude of the Rstar = ~100 km"]
-[6.5581955909729, 6.93533182144165, "[TT] Duty Cycle of the LRDL = 55 - 90%"]
-[9.252915382385254, 3.1151890754699707, "[FF] Measurement Parameters of the SWOOPS = Density, speed and direction of the solar wind in three dimensions"]
-[6.067842960357666, 4.93253755569458, "[FF] Management of the CTDA = Counts with a central management point for the tasking and cataloguing of information"]
-[5.334829330444336, 1.4522864818572998, "[FF] Conference Presentation Date of the SMAP Mission = July 25-30, 2010"]
-[5.263446807861328, 1.2933313846588135, "[FF] Conference Date of the BIROS = June 11-15, 2012"]
-[11.882291793823242, 4.966879844665527, "[TT] Size of the Tsubame = 450 x 450 x 500 mm"]
-[14.2139253616333, 3.270888090133667, "[TT] Mass of the MIRAD = 0.5 kg"]
-[5.69681453704834, 4.80789041519165, "[FF] Function of the GOES = Relay data from remotely located in-situ sites to properly equipped receiving stations"]
-[7.760140895843506, 4.6031413078308105, "[FF] Ground Segment of the GAGE = Observable extraction and orbit determination software"]
-[5.48196268081665, 2.2101593017578125, "[FF] Affiliation of the Kazaya Yoshida = Unknown"]
-[5.440313816070557, 4.199802875518799, "[TT] Power Buses of the Satellite = 3"]
-[5.425470352172852, 3.37685227394104, "[TT] Manufacturer of the PARASOL = CNES"]
-[8.116990089416504, 6.696589469909668, "[TT] Instrument of the EMIT = Imaging Spectrometer"]
-[6.572264194488525, -2.0360841751098633, "[TT] Planning Start of the Jason-CS = 2009/10"]
-[7.976639747619629, 7.024816036224365, "[TT] Mode of the Camera = Full frame mode"]
-[5.358621597290039, 0.389239639043808, "[TT] Reentry Date of the SMDC-ONE = January 12, 2011"]
-[8.535444259643555, 3.847928762435913, "[FF] Measurement of the SEISS = Localized measurements of particles and fields in geosynchronous orbit"]
-[7.5555739402771, -0.5457162857055664, "[FF] Strategic Partnership of the Spire = ICEYE"]
-[5.671617031097412, 6.3552727699279785, "[TT] Data Storage of the FTHSI instrument = 134 MByte"]
-[8.618707656860352, 0.895999550819397, "[TT] Renamed Name of the Solar Probe Plus = Parker Solar Probe"]
-[9.365421295166016, -0.8130490779876709, "[TT] Orbit Parameters of the GEOS-1 = 1,114 x 2,273 km x 59.4\u00ba"]
-[14.666065216064453, 6.6439714431762695, "[TT] Battery Capacity of the CanX-2 = 4.8 Ah"]
-[7.009133815765381, 7.107711315155029, "[TT] Double-Pass Amplifier Output of the Power Laser Head (PLH) = About 150 mJ"]
-[10.360793113708496, 7.948653221130371, "[TT] Size of the Telescope = 17 cm x 12 cm x 12 cm"]
-[3.0740718841552734, -0.04397159814834595, "[TT] Orbital Slot of the GSAT-0206 = A05"]
-[9.93266773223877, 7.976426601409912, "[TT] Field of View of the Telescope Optical Unit (TOU) = Up to 18.9\u00b0"]
-[7.85989236831665, 8.36441421508789, "[FF] Bands of the HRV = PAN, Green, Red and Near Infrared (NIR)"]
-[7.949474334716797, 5.05617094039917, "[TT] Calibration Frequency of the TIR Instrument = Every 5 seconds"]
-[7.0350470542907715, 3.790003538131714, "[FF] Conference Presentation Date of the PROBA-3 Formation Flying Mission = March 13-15, 2013"]
-[3.834301710128784, 7.8546648025512695, "[FF] Function of the QKD = Generate private random encryption keys and share them between only two parties"]
-[5.80979585647583, -0.49359819293022156, "[TT] Lifetime of the Instrument = 3.25 years"]
-[7.631381511688232, 8.97812271118164, "[TT] NER of the Spectral Band D = 5.2 x 10^-7 W/(cm^2 sr \u00b5m)"]
-[10.842594146728516, 5.131062030792236, "[TT] Probe Diameter of the LPE = 20 mm"]
-[6.475979328155518, -0.5175872445106506, "[TT] Data Transmission Time of the TanSat = Within eight hours"]
-[8.7263765335083, 3.1265056133270264, "[FF] Image Capture of the NASA's Solar Dynamics Observatory = Full-disk Sun and the left side of the inset image"]
-[9.975828170776367, -1.4757153987884521, "[TT] Orbit Inclination of the SPOT-1, -2 and -3 = 98.7\u00b0"]
-[9.455227851867676, 1.028969168663025, "[TT] Processing Speed of the Orion's Computer = 480 million instructions/second"]
-[8.401569366455078, 3.3804492950439453, "[FF] Measurement Principle of the GFSE = Thermal technique to measure the flow rate of gas"]
-[11.390050888061523, 4.427778720855713, "[TT] Size of the Wren = 2.5U"]
-[5.503044605255127, 3.139604091644287, "[TT] Contract Award of the Lockheed Martin = $700 million"]
-[16.501821517944336, 3.587500810623169, "[TT] Service Availability of the OneWeb = Before the end of the year"]
-[13.26024341583252, 5.590330123901367, "[FF] Purpose of the ISS Power Augmentation (IPA) Mod Kit = Critical hardware to be installed during the upcoming ISS Roll-Out Solar Array (IROSA) spacewalks, allowing the space station program to continue deploying the upgraded solar arrays"]
-[7.782567024230957, 5.986819267272949, "[FF] Drive and Readout Circuits of the CIRC = Similar to those of the commercial IR camera"]
-[5.621211528778076, 7.198465824127197, "[TT] Transition Time Percentage of the VBR = 5% with 3-bit rates"]
-[5.23081636428833, 8.19534969329834, "[TT] Frequencies of the SSM/I = 4"]
-[9.655384063720703, 8.189298629760742, "[TT] Lens Count of the CAPI = 6"]
-[5.635019302368164, 7.095505237579346, "[TT] Data Rate of the DCP = 400 bit/s"]
-[9.22828197479248, 4.7434821128845215, "[FF] Innovation Date of the Attitude and Orbit Control Software = Unknown"]
-[9.369902610778809, 4.995968818664551, "[TT] Attitude Accuracy of the DubaiSat-2 = 0.15\u00ba"]
-[11.001032829284668, 4.048776149749756, "[TT] Sail Area of the CanX-7 Drag Sail = Approximately 5 m2"]
-[11.868630409240723, 6.690454006195068, "[TT] Energy of the GRD = 1.6 MeV"]
-[2.6106677055358887, 3.332632064819336, "[TT] Mass of the Flock-3 = 5 kg each"]
-[11.12446403503418, 1.5293707847595215, "[TT] Mass of the Starshine-1 = 39 kg"]
-[12.06107234954834, -0.41348397731781006, "[TT] Launch Timeframe of the TESS-L5 = 2026-2029"]
-[8.279534339904785, 6.525175094604492, "[FF] Scan Rate of the SSMIS = 31.9 scans/min (or 1.88 s/scan)"]
-[4.915855884552002, 1.432579517364502, "[TT] Operation Start Date of the Tatiana-1 = Jan. 21 2005"]
-[7.173887252807617, 4.4065399169921875, "[FF] Operation of the Mx = For most of the orbits based on the user demands"]
-[10.415215492248535, 4.052387714385986, "[TT] Length of the Boom = 8 m"]
-[7.041416168212891, -0.749764084815979, "[TT] Rotation Period of the TOI 451 = 5.1 days"]
-[7.3994460105896, 8.525588989257812, "[TT] Rejection Ratio of the Filter = Low in the visible"]
-[6.971171855926514, 3.968979597091675, "[FF] Experiment Renewal of the SPOT-5 = TAKE5 experiment"]
-[5.9731879234313965, 1.4261189699172974, "[FF] Contracts Awarded Date of the Joint Polar Satellite System = Unknown"]
-[6.41093635559082, 7.005764961242676, "[TT] Output Voltage of the High-response comparator = Repeats High/Low in periods of several microseconds (\u00b5s)"]
-[3.3668479919433594, 6.382624626159668, "[TT] Size of the Receive Antenna = 2.2 m dish"]
-[2.608501434326172, 3.3321428298950195, "[FF] Mass of the Flock-4v = Not provided"]
-[5.016407489776611, 0.7434829473495483, "[TT] Launch Date of the DMC-3 Constellation = 2014"]
-[7.798469543457031, 9.082395553588867, "[TT] Central Output Angle of the Long Wavelength Band = -5.28\u00ba"]
-[5.948781490325928, 2.5588488578796387, "[TT] Flight Heritage of the MHX-2400 = 4 missions"]
-[9.542295455932617, 3.68027925491333, "[TT] Movement of the Earth's Magnetic Field = Up to tens of km every year"]
-[11.7946195602417, 5.060175895690918, "[TT] Design of the SCM = Very compact"]
-[7.349453926086426, 3.1343002319335938, "[FF] Data Usage of the EnviSat = Studying and monitoring the Earth's environment"]
-[7.5850830078125, 6.903605937957764, "[TT] Small Window Time Resolution of the CCD = 0.3 seconds"]
-[4.937368869781494, 3.199559450149536, "[TT] Manufacturer of the AUTcube-2 = Aichi University of Technology, Japan"]
-[5.864619255065918, 2.9243404865264893, "[TT] Developer of the JPSS-1 = NASA"]
-[8.186335563659668, 1.3194187879562378, "[FF] Effect on Southwest U.S. of the La Ni\u00f1a = Tends to cause dry weather"]
-[9.579545021057129, 0.8304042816162109, "[TT] Closest Approach Distance of the Rosetta = 75,000 km"]
-[5.777479648590088, 3.039280891418457, "[TT] Development Status of the Mission Control System = Currently being developed"]
-[9.226131439208984, 4.709425926208496, "[FF] Attitude Determination and Control Strategies of the OPTOS Picosatellite = Unknown"]
-[14.335488319396973, 3.154670000076294, "[TT] Mass Requirement of the WCOM = 220 kg"]
-[8.025768280029297, -0.16948670148849487, "[TT] Orbit Period of the Meteor-M2 = 101.41 minutes"]
-[4.691523551940918, 1.076725721359253, "[TT] Operation Status of the FY-3C = Operating in 2016"]
-[12.104867935180664, 6.329763889312744, "[TT] Positron Rejection Power of the AMS = More than one in one million"]
-[10.632336616516113, 8.88027572631836, "[TT] Pixel Size of the Channel 1 = 32 x 32 km"]
-[5.449890613555908, 0.26436734199523926, "[FF] Location of the SAMMES Instrument Modules = 2-11 to 2-19"]
-[10.19864559173584, 5.893096923828125, "[TT] Temperature of the Optics Subsystem = 20 \u00b13\u00baC"]
-[8.723259925842285, 7.363382339477539, "[TT] Centroiding Error of the Detector = ~ 50 \u00b5m"]
-[7.710525035858154, 6.882420539855957, "[TT] Cadence of the Fast Cameras = 2.5 seconds"]
-[5.429376602172852, 3.3470094203948975, "[FF] Delivery of the CAPSTONE = Rapid commercial delivery"]
-[4.442914009094238, 3.2249536514282227, "[TT] Ground Station Location of the CBERS-4A = Cuiaba, MT"]
-[6.13213586807251, 6.22230339050293, "[TT] Quantity of the Net capture system = 1"]
-[5.922131538391113, 3.6083905696868896, "[FF] Factors for Selection of the Launch Vehicle = Reliability, cost, availability, and capability of lifting the satellite to its desired orbit"]
-[7.160360813140869, 5.903652667999268, "[TT] Atomic Clock Accuracy of the Galileo = Accurate to a few nanoseconds"]
-[5.5603485107421875, 0.8358022570610046, "[FF] Launch Date of the Satellite Vu\u2019s first satellite = June 2023"]
-[11.57261848449707, 4.6872382164001465, "[TT] Length of the Unpressurized Pallet Segments = About 2.8 m"]
-[8.97418212890625, 0.4444885551929474, "[TT] Size of the Boulders = 1 m"]
-[8.418112754821777, 6.922764778137207, "[TT] Instrument Type of the IMG = High resolution optical imagers"]
-[10.21325969696045, -1.326298713684082, "[TT] Orbit Inclination of the CubeSats = 97.6\u00ba"]
-[9.8338041305542, 4.8493266105651855, "[TT] Rotation Rate of the Pulsar = 30 times per second"]
-[3.5010862350463867, 4.735374450683594, "[FF] Program Start of the SIR-C/X-SAR = SIR-B in l984"]
-[14.172079086303711, 3.2741119861602783, "[TT] Mass of the M3MSat = 80 kg"]
-[4.740027904510498, 5.860269069671631, "[TT] Beacon Period of the Spectrum Analyzer = 15 seconds"]
-[8.721183776855469, 7.6429548263549805, "[TT] Small Window Imaging Area Pixels of the CCD = 100 x 100"]
-[8.12932014465332, 3.565237283706665, "[TT] Photometer Operation of the LAICE = Orbital night"]
-[5.432608604431152, 0.5800797939300537, "[FF] Mission Date of the NuSTAR = May 13, 2013"]
-[11.779647827148438, 3.296234607696533, "[TT] Thrusters of the FEEP = \u00b5N"]
-[6.300786972045898, 4.418961048126221, "[FF] Responsibilities of the TKSC = Spacecraft monitoring and control including operations planning"]
-[8.600738525390625, 3.6414363384246826, "[FF] Measurement of the TSIS = Total and spectral solar irradiance"]
-[4.913392543792725, 0.5841354131698608, "[TT] Launch Date of the AMS-02 = 16 May 2011"]
-[5.641791820526123, 0.9425638318061829, "[TT] Launch Date of the IBEX = October 19, 2008"]
-[7.534412384033203, 6.488407135009766, "[TT] Image Update Frequency of the GVAR = 5 minutes (Mode 4), 15 min (Mode 3)"]
-[4.419223308563232, 2.665900945663452, "[TT] Launch Location of the SARSAT-3 = US NOAA satellites and the European MetOp satellites"]
-[11.951753616333008, 5.00903844833374, "[TT] Size of the DACS = 260 mm x 210 mm x 150 mm"]
-[8.228658676147461, 7.364099025726318, "[TT] Operating Mode of the MBA detector = TDI (Time Delay Integration)"]
-[4.92235803604126, 2.9898412227630615, "[TT] Partner Agencies of the Odin = Canada, Finland and France"]
-[13.787330627441406, 5.973208904266357, "[TT] Power Source of the EPS = Solar cells and lithium-ion battery"]
-[5.970735549926758, 4.979445934295654, "[FF] Function of the ISL (Inter-Satellite Link) = Communicate with the platform"]
-[10.402935981750488, 5.922942638397217, "[TT] Brigthness Temperature (BT) Sensitivity of the Antenna = \u00b10.29 K"]
-[-4.0649542808532715, 4.482392311096191, "[FF] Support Phase Time Period of the Mango Tango = 02.07 to 02.08.2010"]
-[10.144725799560547, 10.002120971679688, "[TT] Return to Flight Schedule of the Vega = End Q1 2021"]
-[4.654262065887451, 6.973883152008057, "[TT] LISS-2A/B Data Downlink of the Satellite = X-band"]
-[11.970609664916992, -0.3572970926761627, "[TT] Data Processing Location of the TESS = NASA\u2019s Ames Research Center in Silicon Valley, California"]
-[9.357026100158691, 8.107224464416504, "[TT] Maximum Flux Measurement Rate of the Focal Plane Module = 10 4  s -1"]
-[7.499736309051514, 7.073709964752197, "[TT] Sampling Interval of the ScaRaB = 34 mrad"]
-[7.947244167327881, 7.8657121658325195, "[FF] Type of the NIR Camera = Near Infrared"]
-[6.749541282653809, 5.0694990158081055, "[FF] Canister Interconnection of the CVX-2 = Intercom connect cable for power and data transmission"]
-[10.845124244689941, 1.5636144876480103, "[TT] Material Consumption Rate of the SS 433 = About 30 times the mass of Earth per year"]
-[7.543996334075928, 6.9575982093811035, "[TT] Cadence of the MEGS = 10 seconds"]
-[7.9507551193237305, 2.229696273803711, "[FF] Data Products of the TOPEX/Poseidon = Sea surface topography, Significant wave height, Surface wind speed, Ocean tides, Vertically integrated atmospheric water vapor, Vertically integrated ionospheric electron content"]
-[10.297640800476074, 5.365858554840088, "[TT] Thermal Control of the EXIS = Active control , 2 zones"]
-[4.004048824310303, 1.9008018970489502, "[TT] Launch Vehicle of the HTV = H-IIB"]
-[11.41702651977539, 4.991817951202393, "[TT] Collecting Area of the Gaia = 0.7 m2"]
-[8.331877708435059, 4.250658988952637, "[FF] Purpose of the ASAP\u00ae ray tracing software = Perform stray light analysis"]
-[5.235378742218018, 0.942122220993042, "[FF] Launch Date of the EMIT = Unknown"]
-[5.466881275177002, 6.255103588104248, "[TT] RAM Capacity of the FC = 3 MB"]
-[3.804631233215332, 0.8729502558708191, "[FF] Launch Date of the PSLV-C41 = April 12, 2018"]
-[7.0365753173828125, 9.061980247497559, "[TT] Bandpass of the COR1 = 648-750 nm"]
-[4.582986831665039, 5.7322611808776855, "[FF] Mission Focus of the GOMX-3 = Attitude control, RF sensing, and high-speed data downlink"]
-[12.037439346313477, 4.698309898376465, "[TT] Size of the BRITE-Austria = 20 cm x 20 cm x 20 cm"]
-[8.273674964904785, 2.813854694366455, "[FF] Cloud Detection Scheme of the TANSAT = Unknown"]
-[3.452314615249634, -0.8911022543907166, "[TT] Orbit Type of the Argos-4 = Sun-synchronous orbit"]
-[7.889184951782227, 8.625571250915527, "[TT] Spectral Region of the SBUV = 0.250 - 0.340 \u00b5m"]
-[4.535511016845703, 7.733942031860352, "[FF] Bandwidth of the SARAL/AltiKa = Unknown"]
-[4.5920729637146, 1.5984845161437988, "[FF] URL of the VNREDSat-1 = https://vast.gov.vn/web/vietnam-academy-of-science-and-technology/tin-chi-tiet/-/chi-tiet/vnredsat-1-orbit-second-adjusted-to-avoid-collision-9103-871.html"]
-[5.494892120361328, 6.6706318855285645, "[TT] Data Storage of the AMS-02 = Approximately 200 TB"]
-[11.783662796020508, 4.826112747192383, "[TT] Dimensions of the S/C = 6 m x 4 m x 4 m"]
-[9.494155883789062, 6.178488731384277, "[TT] Incidence Angles of the MWR = 52\u00ba and 58\u00ba"]
-[3.8216679096221924, -1.1622754335403442, "[TT] Orbit Type of the PLATO = Halo orbit around L2"]
-[4.389766693115234, 5.432257652282715, "[FF] Conference Presentation Date of the GOMX-1 = May 26-30, 2014"]
-[5.567391395568848, 0.8068254590034485, "[FF] Contract Signing Date of the FormoSat-5 = June 17, 2010"]
-[8.157418251037598, -0.6097947359085083, "[TT] Ice Loss of the CryoSat = 76 Gt per year for Gulf of Alaska, 28 Gt of ice per year for High Mountain Asia"]
-[10.196183204650879, 5.7085862159729, "[TT] Detector Cooling of the FTS Interferometer = Passive cooling <100 K"]
-[5.283707618713379, 5.747289180755615, "[TT] Onboard Network Specification of the JWST Avionics = SpaceWire"]
-[6.912579536437988, 4.630194187164307, "[FF] Construction Method of the GCP Database = Fully automatic matching with acquired image data and image correction"]
-[9.182687759399414, 5.605169296264648, "[TT] Mounting Orientation of the Sensor = Approximately along the satellite velocity"]
-[9.554011344909668, 9.13871955871582, "[FF] Observation Resolution of the IRIS = Unprecedented"]
-[8.374676704406738, 3.560007333755493, "[FF] Mission Phases of the Solar Orbiter = Cruise phase and Science phase"]
-[6.321360111236572, 3.886594533920288, "[FF] Components of the Spacecraft Plug-n-Play Avionics (SPA) = Electronic datasheet"]
-[10.696723937988281, 0.8959192633628845, "[FF] Comparison of the Victoria Island = Only slighter smaller than the island of Great Britain"]
-[5.73594856262207, -2.1247060298919678, "[FF] Geolocation Accuracy of the KOMPSAT-3 = Unknown"]
-[5.8620100021362305, -0.651600182056427, "[TT] Years of the Mission Lifetime = Data and products until year 2030"]
-[5.758944034576416, 5.450193881988525, "[TT] Control Interface of the Payload 2 = I2C bus"]
-[4.020676136016846, 6.134925365447998, "[FF] Deployable Onboard of the ISIS Dipole Antenna = True"]
-[3.9599387645721436, 6.380880355834961, "[TT] Antenna Design of the Radio = Omnidirectional/medium gain"]
-[9.609648704528809, 8.329544067382812, "[FF] Effective FoV of the Camera = 1037\u00ba x 1037\u00ba for the \u201cnormal\u201d cameras and 619\u00ba x 619\u00ba for each of the two \u201cfast\u201d cameras"]
-[10.153446197509766, 10.01558780670166, "[FF] Date of the Vega flight VV16 = Unknown"]
-[7.167302131652832, 2.5286076068878174, "[FF] Author of the Observation of the Earth and Its Environment = Herbert J. Kramer"]
-[7.886392116546631, 3.1175038814544678, "[TT] Cloud Imager of the Atmospheric-sounding instrument = Built-in"]
-[6.335912227630615, 4.273349761962891, "[FF] Compatibility of the F\u2019 = Model-Based Systems Engineering (MBSE) artifacts"]
-[5.193361282348633, 4.725729465484619, "[TT] Constellations of the NovAtel OEM615 GNSS = GPS and GALILEO"]
-[6.610731601715088, 5.889263153076172, "[FF] Function of the Laser-optical payload = Intersatellite links"]
-[13.781667709350586, 3.250190258026123, "[TT] Mass of the AeroCube-4.0 = 1.1 kg"]
-[3.2882113456726074, 5.1885762214660645, "[TT] Incidence Angle Range of the SAR = 32\u00ba at the near range and 38\u00ba at the far range"]
-[7.606121063232422, 6.133355140686035, "[FF] Truth Data of the CCRR = Position measurements by the laser tracker"]
-[8.683939933776855, 8.867902755737305, "[TT] Grating Type of the MEGS = Single, holographic, spherical grating"]
-[4.172143936157227, 7.032357692718506, "[TT] MGA (Medium Gain Antenna) of the S/C Communication Subsystem = 1"]
-[7.395152568817139, 3.2051758766174316, "[FF] Purpose of the EEV = Ensure that the precious samples reach the Earth\u2019s surface intact"]
-[8.648221015930176, 2.0245275497436523, "[TT] Wind Speeds Accuracy of the SeaWinds scatterometer = 2 m/s"]
-[5.2443528175354, 4.03612756729126, "[FF] Satellite Orbit Types of the BeiDou-2 = 5 geostationary orbit (GEO) satellites and 30 medium Earth orbit (MEO) satellites"]
-[4.395145416259766, 3.1295557022094727, "[TT] Location of the RADARSAT MMO = CSA in Saint-Hubert, Quebec"]
-[14.255341529846191, 3.1209218502044678, "[TT] Mass of the AISSat-3 = 6.5 kg"]
-[10.637093544006348, 1.392431378364563, "[TT] Energy Emission of the TOI 451 = 35% less than our Sun"]
-[6.480818748474121, 3.5002641677856445, "[TT] Purpose of the Refabricator = Enable sustainable fabrication, repair, and recycling on long-duration space missions"]
-[9.824600219726562, 8.156662940979004, "[TT] Lens of the Nikon D3S = 400 mm"]
-[8.134305000305176, 3.5780351161956787, "[FF] Application of the Infrared Sensors = Astronomical observations"]
-[6.04490327835083, 1.333158254623413, "[TT] Extension Approval Date of the Swarm = 20 Nov. 2017"]
-[13.347322463989258, 7.1520819664001465, "[TT] Energy Range of the FSU = Modulator sized to withstand 8 kV"]
-[5.756453514099121, 3.0653128623962402, "[TT] Contract Value of the WorldView Legion = $35 million"]
-[4.337307453155518, 1.2173309326171875, "[TT] LTDN of the SEOSAT-Ingenio = 10:30 hours"]
-[5.4906840324401855, 0.828249990940094, "[FF] Discovery Date of the NICER = 10 May 2018"]
-[5.033401966094971, 7.226222038269043, "[TT] Data Rate from FPGA to S-band transmitter of the Transmission Module = 1 Mbit/s"]
-[3.170454740524292, 2.305067300796509, "[TT] Geographic Coverage of the Sentinel-2 = All land areas/islands covered (except Antarctica)"]
-[1.3962512016296387, 1.9258986711502075, "[TT] Expected Number of Tracked Cargo Vessels of the MDASat-i = 60000"]
-[8.42992877960205, 6.31632661819458, "[FF] Limb-Sounding Concept/Technology Test of the OMPS = ISIR (Infrared Spectral Imaging Radiometer) flown on Shuttle flight STS-85 (Aug. 7-19, 1997)"]
-[8.304030418395996, 8.82548999786377, "[TT] Slit 2 Spectral Range of the MEGS-A = 17.0 -37.0 nm"]
-[3.9889588356018066, 6.426511764526367, "[FF] Design Consideration of the Antenna = Longer and wider is better"]
-[5.5065789222717285, 6.486189365386963, "[TT] Data Returned of the Clementine = ~ 330 Gbit total"]
-[13.24796199798584, 7.598307132720947, "[TT] Power Consumption of the Transmitter = 61.1 W (max)"]
-[9.59517765045166, 7.189550399780273, "[TT] Spatial Resolution of the MWHS-II = ~15 km diameter at nadir, About 41 km x 27 km at outer edge of swath"]
-[4.901427745819092, 0.6026546955108643, "[TT] Failure Date of the NRCSD = August 2014"]
-[9.870965003967285, -0.4546838402748108, "[TT] Orbit Altitude of the KSF1 satellites = 525 km"]
-[11.496357917785645, 6.600944519042969, "[TT] Measurement Range of the Particle Detector = Deuteron : 8 MeV/n ~ 26 MeV/n"]
-[5.398130893707275, 2.544943332672119, "[TT] Operational Countries of the JJ-FAST = 77"]
-[3.873094320297241, 3.4233145713806152, "[FF] First Space Test Date of the Galileo's Search and Rescue System = Jan. 23, 2013"]
-[8.530447006225586, 7.563037395477295, "[FF] Temporal Resolution of the FTHSI = None"]
-[4.927549839019775, 0.8424268364906311, "[FF] Mission Date of the PROBA = Sept. 23-26,1999"]
-[9.995948791503906, 7.748242378234863, "[TT] Telescopes of the ASTRO-1 = 4"]
-[4.908810615539551, 6.972129821777344, "[TT] Method of the Direct Downlink = Direct downlink to users"]
-[7.219326972961426, 1.2667055130004883, "[TT] Full Science Mission Start of the ExoMars Trace Gas Orbiter = 2018"]
-[8.946041107177734, 5.304681301116943, "[TT] Orbit Altitude of the GOMX-3 = Approximately 400 km"]
-[6.966668605804443, 0.7968706488609314, "[TT] Detection Date of the InSight lander = Late 2018"]
-[7.709049701690674, -0.8291915059089661, "[TT] Deorbit Date of the ICESat = Sept. 2, 2010"]
-[7.898927688598633, 3.9971001148223877, "[TT] Instrument Type of the JPSS-2/NOAA-21 = Atmospheric chemistry, Atmospheric temperature and humidity sounders"]
-[8.12075424194336, -1.1789718866348267, "[TT] Green Laser Altimeter Accuracy of the ICESat-2 = Gauging seafloor depths down to 100 feet below the surface"]
-[4.383700847625732, 7.849843978881836, "[TT] Downlink Frequency (Lower extended C-band channel) of the Communication Payload = 3425-3625 MHz"]
-[3.223396062850952, 3.816152334213257, "[TT] Operational Date of the TerraSAR-X = January 2011"]
-[7.553823947906494, 2.710914373397827, "[FF] Usage of the Radar Altimeter = Vertical descent phase"]
-[11.225545883178711, 5.736448764801025, "[TT] Finesse of the Cavity = About 10,000"]
-[7.343488693237305, 1.1356821060180664, "[TT] Bulletin Release Year of the OceanSat-2 = 2010"]
-[8.027632713317871, 6.048962593078613, "[TT] Dynamic Range of the FFRF = 100 m to 30 km"]
-[5.970456600189209, -0.441449373960495, "[TT] Extended Mission of the Spacecraft = 5-7 years"]
-[8.15391731262207, 1.2837127447128296, "[FF] Purpose of the SMAP = Measure freeze/thaw timing, soil moisture, monitor droughts"]
-[10.14277458190918, 6.849668979644775, "[TT] Satellite Size of the Sounder Instrument = 6U"]
-[6.29132604598999, -0.15759964287281036, "[TT] Re-visit Time of the MSI = Short"]
-[10.082741737365723, 3.1713390350341797, "[FF] Purpose of the GRBAlpha smallsat = Demonstrate the detector technology and electronics for the future \u201cCubeSats Applied for MEasuring and LOcalizing Transients\u201d (CAMELOT) mission"]
-[8.457087516784668, 8.865714073181152, "[TT] Imaging Dual-Band Photometry Wavelength Bands of the PACS = 60-85 \u00b5m or 85-125 \u00b5m and 125-210 \u00b5"]
-[4.2822160720825195, 0.5767855048179626, "[TT] Return to Science Operations Date of the Integral = September 2020"]
-[5.79707145690918, -0.8109559416770935, "[TT] Available Consumables Lifetime of the Spacecraft = 7 years"]
-[6.25423002243042, 1.9893511533737183, "[FF] URL of the Alphabus = http://telecom.esa.int/telecom/www/object/index.cfm?fobjectid=30203"]
-[5.4027228355407715, 5.4133405685424805, "[TT] Onboard Computers of the STRV-1b spacecraft = Mil Std 1750A, (dual-redundant)"]
-[5.166296005249023, 8.105528831481934, "[TT] Operational Frequency Range of the TRMs = Wider"]
-[9.283214569091797, 8.35793685913086, "[TT] Optical Magnitude of the Mayak = -10"]
-[7.798717498779297, 0.8942961096763611, "[FF] Date of the Flooding in Eastern Australia = 11 April 2022"]
-[11.502062797546387, 3.467966079711914, "[FF] Function of the Ion Propulsion Assembly (IPA) = Compensated for the drag force experienced by the satellite\u2019s orbit in real-time"]
-[10.011073112487793, -1.5030176639556885, "[TT] Orbit Inclination of the OPAL = 51.6\u00ba"]
-[9.288335800170898, 1.787429690361023, "[TT] Trackable of the Net and Harpoon = Yes"]
-[8.103009223937988, 1.2801309823989868, "[TT] Eruption Date of the X-class flare = March 29, 2014"]
-[4.779233932495117, 0.8635907769203186, "[TT] Planned Observation Continuation of the Resurs-O1 = At least until 2000"]
-[11.942739486694336, 5.0071587562561035, "[TT] Dimensions of the IOU = 450 mm x 200 mm x 200 mm"]
-[9.2413969039917, -0.39485985040664673, "[FF] Injection Errors of the PUNCH Mission = 10 km on the injection apse, 80 km on the non-injection apse, and 0.15\u00b0 on inclination"]
-[6.099632740020752, 4.814984321594238, "[FF] Communication Architecture of the BioSentinel = CubeSat direct-to-ground communication, CubeSat to Tracking Data Relay Satellite System (TDRSS) communication, CubeSat constellation with Mothership direct-to-ground communication, and CubeSat Constellation with Mothership communication through KSA (K-band Single Access)"]
-[3.7105915546417236, 4.597369194030762, "[FF] Pre-defined Modes Performance of the RADARSAT-2 = Met requirements in all aspects of image quality"]
-[11.35931396484375, 5.874813556671143, "[TT] Material of the Chassis = Aluminum"]
-[8.927133560180664, 4.7894110679626465, "[FF] Function of the Attitude Control System = Pointing of the satellite"]
-[8.28574275970459, 1.4326132535934448, "[TT] Accuracy of Moisture Profiles of the CrIMSS = 15%"]
-[6.250455856323242, 2.601137161254883, "[FF] Function of the Spacecraft Adaptor and Fairings = Connects Orion to the launch vehicle"]
-[7.780656814575195, 6.000239849090576, "[TT] Function of the GAMALINK = Supports precise ranging measurements"]
-[6.061654567718506, 3.99438738822937, "[TT] Instrument Type of the TOMS = Space environment"]
-[4.704580783843994, 0.2978447377681732, "[TT] Launch Date of the SpaceLink = 2024"]
-[7.10004997253418, 1.3128732442855835, "[FF] Mission Type of the ExoMars TGO = Red Planet Investigation"]
-[8.739407539367676, 2.4195337295532227, "[FF] Data of the Aeolus = Most of the dust was 3\u20146 km above the ground"]
-[4.604110240936279, 7.907124996185303, "[TT] Frequency Range of the SGLS Link = 1755-1850 MHz"]
-[5.536866188049316, 6.313780784606934, "[TT] Number of Pan Scenes of the Memory = 31"]
-[11.65791130065918, 6.662866592407227, "[TT] Energy Measurement Range for Electrons of the Telescope 1 = >0.15, 0.35, 0.75 MeV"]
-[6.60566520690918, -0.5789453983306885, "[FF] Liftoff of the Antares = Ten minutes"]
-[5.455873966217041, 0.5203181505203247, "[FF] Update Date of the LROC = Sept. 25, 2013"]
-[8.20267105102539, -1.0747584104537964, "[TT] Bathymetry Mapping Depth of the ICESat-2 = 26 meters (85 feet)"]
-[7.4129133224487305, 4.925436973571777, "[FF] Components of the Central Propulsion Module = Propellant tanks, LAE (Liquid Apogee Engine), East panel with the L-band antenna feed, West panel with the IOL (Inter Orbit Link) antenna"]
-[1.7629932165145874, -2.0605521202087402, "[FF] URL of the Hayabusa 2 Project = https://web.archive.org/web/20120222130748/http://b612.jspec.jaxa.jp/hayabusa2/e/hayabusa2_e.html"]
-[4.863387107849121, -1.5650718212127686, "[TT] Design Lifetime of the Tianwen-1 = One Martian year, or 687 Earth days"]
-[8.373544692993164, 2.951286554336548, "[FF] Purpose of the MSX/UVISI = Probe the atmospheric composition accurately"]
-[8.901939392089844, 5.711993217468262, "[TT] Relative Pointing Error of the AOCS = \u2264 0.03 \u00b5rad/1.5 ms (3\u03c3); and \u2264 0.06 \u00b5rad/3.0 ms (3\u03c3)"]
-[9.04826831817627, 7.333850383758545, "[TT] Effective Area of the Detector = 200 cm 2 @ 1.5 keV"]
-[11.159634590148926, 0.6349495649337769, "[FF] Mission Type of the Hubble = Discovery of Diverse Exoplanets"]
-[9.82442855834961, -0.5589204430580139, "[TT] Orbit Altitude of the Landsat-9 = 705 km"]
-[5.417055130004883, 1.145475149154663, "[FF] Meeting Date of the LunaH-Map = 20-22 October, 2015"]
-[5.719364166259766, 4.420805931091309, "[FF] Technology Integration of the SATis5 = 5G communication environment including satellite and terrestrial components"]
-[5.0960373878479, 4.409914016723633, "[FF] Risk to Other Spacecraft of the Starlink Satellites = None"]
-[4.669600009918213, 7.977288246154785, "[TT] Frequency of the RF Output Frequency = 2214.97 MHz"]
-[7.922510623931885, 8.423303604125977, "[TT] Data Compression Ratio of the Spectral bands = 2.8 and 3.75 for PAN, 1.7 and 3.75 for MS"]
-[5.107779026031494, 6.810351371765137, "[TT] Output Frequency of the LDCM spacecraft = 8200.5 MHz"]
-[9.411093711853027, 0.6740326881408691, "[FF] Travel Behavior of the DIBS = Around the world"]
-[4.170344829559326, 7.351553440093994, "[TT] Terminal Type of the Pl\u00e9iades Neo = Reactive Ka-band"]
-[6.898411273956299, 4.433917999267578, "[FF] Unknown of the ICBC = Unknown"]
-[9.453462600708008, 3.782468795776367, "[FF] Data Contribution of the Scalar Magnetometer (OVM) = Update the IGRF model"]
-[9.75973129272461, 7.998549938201904, "[FF] Optical Configuration of the Telescope Optical Unit (TOU) = 6 lenses, plus one window"]
-[5.58207893371582, 7.7266435623168945, "[TT] G/T of the USAT (Ultra Small Aperture Terminal) = >13.5 dB/K"]
-[4.4127726554870605, 7.676313877105713, "[TT] Frequency of the IMI antenna = L-band"]
-[9.4382905960083, 6.9921064376831055, "[TT] Spatial Resolution of the MSU-50 = 120 m"]
-[5.336483955383301, 0.3327953517436981, "[TT] Manufacturing Start Date of the CHEOPS = Mid-2013"]
-[11.269915580749512, 3.622490644454956, "[TT] Propulsion System of the CanX-2 = Characterized"]
-[13.603914260864258, 1.7364468574523926, "[TT] Return Cargo of the Dragon = More than 1630 kg of research, hardware and crew supplies"]
-[10.280333518981934, 5.497379779815674, "[TT] Power of the Stirling Coolers = 0.2 watt"]
-[3.4996116161346436, -0.8658843636512756, "[TT] Orbit of the TSIS = Non-sun-synchronous, inclined at 51.6\u00b0 at an altitude of 407 km and a period of 93 minutes"]
-[7.335901260375977, 7.162797927856445, "[FF] Photon Detection of the ATLAS = Each blue dot"]
-[3.086550235748291, 2.3279967308044434, "[FF] Mission Type of the Sentinel-4 = Geostationary component of European (EC, ESA) operational atmospheric composition monitoring missions"]
-[6.246136665344238, 2.1234323978424072, "[TT] Principal Investigator of the SAGE-II = M. P. McCormick"]
-[4.7787184715271, 2.274975538253784, "[TT] Design Lifetime of the Eutelsat Quantum = 15 years"]
-[5.059600830078125, 0.7270923852920532, "[TT] Mission Launch Year of the IMAP = 2024"]
-[9.564090728759766, 9.139766693115234, "[TT] Flare Class of the IRIS = X-class"]
-[6.009490013122559, 2.5845470428466797, "[FF] Consortium Members of the Swarm Spacecraft = EADS Astrium Ltd., UK; GFZ Potsdam, Germany; DTU Space, Copenhagen, Denmark"]
-[4.20675802230835, 0.9360476732254028, "[TT] Launch Date of the H-IIA launch vehicle No. 37 = 23 December 2017"]
-[6.154027462005615, 1.1706849336624146, "[TT] Nominal Eclipses of the Cluster = 12"]
-[8.31472396850586, 1.2821478843688965, "[FF] Fly Over Precipitation of the RainCube = 6\u03c3 certainty within the first two days of payload operations"]
-[9.3890380859375, 7.07602596282959, "[TT] Mass Resolution of the COSIMA = 2000"]
-[12.100967407226562, 2.96197247505188, "[TT] Propulsion of the LEOStar-3 = Blowdown hydrazine, four 22 N thrusters and eight 4.5 N thrusters, 158 kg tank capacity"]
-[9.330324172973633, 7.471118450164795, "[TT] Ground Pixel Size of the MWIR = 351 m"]
-[4.683383464813232, 3.047001838684082, "[TT] Program Management Location of the SSETI Express = ESA Education Department at ESTEC"]
-[9.728436470031738, -0.4904289245605469, "[TT] Altitude of the ISS = ~400 km"]
-[5.085872650146484, 3.6026055812835693, "[TT] Manufacturer of the Microprocessor = PIC"]
-[10.71963882446289, 1.4091253280639648, "[TT] Size of the Companion Star = most likely half the primary\u2019s size"]
-[9.94961929321289, 5.773068428039551, "[FF] Function of the Imager = Regulate the temperature of the metering struts"]
-[7.711772918701172, 0.4958021640777588, "[FF] Orbital Path of the Lunar IceCube = Uses the gravity of the sun, Earth and moon"]
-[8.096077919006348, 6.274163246154785, "[FF] Operation Principle of the Imaging Pushbroom Spectrometer = A strip (swath) of the Earth's surface is imaged through the entrance optics on the field stop. The collimator optics realizes parallel light rays falling onto the grating. The grating disperses the different \u201ccolors\u201d that are focussed by the imager into the focal plane. Corresponding to the desired wavelength, CCD line arrays are mounted into the focal plane"]
-[9.71486759185791, 0.3702296018600464, "[TT] Size of the PROBA-V = 1 cubic meter"]
-[9.669193267822266, 4.58486795425415, "[FF] Type of the Momentum-bias Attitude Control Subsystem = Momentum-bias"]
-[11.736221313476562, 3.2586565017700195, "[TT] RCS Thrusters Fuel of the AOCS = 12 years"]
-[5.571725368499756, 6.116949558258057, "[TT] Quantity of the Memory System Supervisor = 2"]
-[4.4562764167785645, 1.0981789827346802, "[TT] Agreement Date of the GMES-S = October 2014"]
-[7.965035438537598, 4.033431053161621, "[FF] Quantity of the NINA = Unknown"]
-[5.534972667694092, 6.451869487762451, "[TT] Data Formatting Rate of the Mass Memory System = 2 x 280 Mbit/s"]
-[6.179280757904053, 1.7222083806991577, "[FF] Loss of Momentum and Expertise of the RISESAT = True"]
-[8.34398365020752, 3.3417115211486816, "[FF] Response to Gravity Wave Activity of the O2 Atmospheric Band airglow and NLC = Both feature horizontal and vertical structures that are a direct response to gravity wave activity"]
-[5.060155391693115, 3.8370983600616455, "[TT] Number of Satellites of the IRNSS = 7"]
-[9.179057121276855, 5.210986614227295, "[TT] Redundancy of the IRU (Inertial Reference Unit) = 3 among 4 cold redundancies for the inertial attitude estimation purpose"]
-[5.517127990722656, 0.5600587725639343, "[FF] Update of the NuSTAR = May 2010"]
-[11.697881698608398, 4.550659656524658, "[TT] Length of the STRV-2 payload = 0.82 m"]
-[6.14030647277832, 6.9233198165893555, "[TT] Optical Link Bandwidth (Downlink) of the OICETS satellite = 50 Mbit/s"]
-[8.755176544189453, 1.7834575176239014, "[TT] Speed of the Hurricane Grace = 15 miles (24 km) per hour"]
-[10.295415878295898, 3.2477951049804688, "[TT] Compatibility of the Iris Radio = Deep-space and CubeSat"]
-[11.833588600158691, 6.759013652801514, "[FF] Energy Overlap of the IMAP-Ultra = Overlaps in energy with IMAP-Hi for heliospheric energetic H"]
-[7.112485408782959, 4.224828720092773, "[FF] Unknown of the SPIRALE = Unknown"]
-[9.330564498901367, 5.256471157073975, "[TT] Acceleration Tolerance of the Procyon = 1\u00b0/s2"]
-[7.817380428314209, 5.584954261779785, "[FF] Purpose of the VISS = Provide an ultra-quiet environment for sensitive optical sensors, laser transmitters, and other detection and measurement devices"]
-[8.731695175170898, 2.1317403316497803, "[TT] Antenna Diameter of the WINDS = 45 cm"]
-[5.626978874206543, -0.3290082514286041, "[TT] Altitude Decay Date of the InflateSail = 3 September 2017"]
-[8.52377700805664, 2.3296608924865723, "[FF] Detection of the InSight = Thousands of passing whirlwinds"]
-[13.241072654724121, 7.2779645919799805, "[TT] Power Consumption of the ALT = 177 W"]
-[6.714861869812012, 6.380711078643799, "[TT] Majority Pass Time of the GNOMES-1 = Over 400 seconds"]
-[8.134805679321289, 5.881255626678467, "[FF] Objective of the MP-900M TV Camera = Monitoring (imaging) of reflected radiation of the Earth's surface and atmosphere (clouds)"]
-[13.922765731811523, 3.137604236602783, "[FF] Expected Mass of the DM particles = Large"]
-[8.009620666503906, 3.635618209838867, "[FF] Deputy Project Scientist of the OCO-2 = Annmarie Eldering"]
-[4.959667205810547, -1.6784074306488037, "[TT] Design Life of the Chang'e-3 = Exceeded by 14 months"]
-[5.750949382781982, 5.895806789398193, "[FF] Download Flag Reset of the Data Download System = Download flag can easily be set back to \u201cnot downloaded\u201d"]
-[7.7769927978515625, 4.295640468597412, "[FF] Robustness Requirements of the 6DoF controller = All significant sensor and actuator errors, CSC uncertainties, OSC uncertain/time varying orbital parameters"]
-[9.537952423095703, 7.708121299743652, "[TT] Scan Lines per Image of the Telescope = 5000 (each line of 5000 pixels)"]
-[6.397509574890137, 2.020087957382202, "[FF] Download URL of the Earth Observation Constellation Satellites = http://www.nspo.narl.org.tw/ICGPSRO2013/download/2nd_ICGPSRO_U3-4A-102-02_Chen-Joe_Fong_05-16-2013.pdf"]
-[5.402552604675293, 8.360954284667969, "[TT] Maximum Spectral Width of the VBR = Smaller than 375 MHz"]
-[10.090363502502441, -2.6703784465789795, "[TT] Output Data Rate (downlink) of the Astrium MMFU NAND-Flash SDR-SDRAM = 2 x 280 Mbit/s"]
-[7.01991081237793, 0.8048186302185059, "[TT] Number of Detected Marsquakes of the InSight lander = More than a thousand"]
-[5.284142017364502, 0.26972752809524536, "[TT] Launch Date of the RAVAN = November 2016"]
-[4.881215572357178, 3.015789031982422, "[TT] Mission Leader of the ASTRA LLC = ASTRA LLC"]
-[10.989700317382812, 6.339120388031006, "[TT] Mirror Material of the ALI = Silicon carbide (SiC)"]
-[10.699054718017578, 6.167270660400391, "[TT] Proton Shield Material of the eROSITA camera module = Copper"]
-[8.120770454406738, 1.2987185716629028, "[TT] Flare Eruption Time of the IRIS = 19:40 UTC"]
-[13.401177406311035, 6.799242973327637, "[TT] Power of the Genesis spacecraft = 202 W (EOL)"]
-[12.798797607421875, 7.604856014251709, "[TT] E-field Requirement of the Internal Equipment and Instruments = 32 V/m"]
-[5.7608561515808105, 4.858589172363281, "[FF] Augmentation of the L1-SAIF+ = GPS satellites"]
-[7.352339267730713, 6.291802883148193, "[FF] Function of the LRA = Acts as a reference target for laser tracking measurements performed by ground stations"]
-[4.251132965087891, 4.047848701477051, "[TT] Channels of the Galileo receiver module = Up to 7"]
-[3.183763027191162, 3.851271152496338, "[FF] Commissioning Phase Duration of the TerraSAR-X = Until the end of 2007"]
-[9.852932929992676, 8.020040512084961, "[FF] Requirement of the Lens System = Small coupling of tilt into the length measurement"]
-[9.64294719696045, -0.3006749451160431, "[FF] Altitude of the EFT-1 = Higher than any achieved by a spacecraft intended for human use since 1972"]
-[10.382696151733398, 5.692768573760986, "[TT] Thermal Conductance of the Thermal Strap = ~1 W/K"]
-[8.791951179504395, 3.4680755138397217, "[FF] Usage of the Tiny Ionospheric Photometer (TIP) = Not provided"]
-[5.334270000457764, 1.6602851152420044, "[TT] Mission Status of the ALOS-2/Daichi-2 = Operational"]
-[10.682361602783203, 6.575314044952393, "[TT] Micro-roughness of the Mirror = < 0.5 nm"]
-[13.408344268798828, 5.5331807136535645, "[FF] Components of the TOPEX/Poseidon = Solar array, Three batteries"]
-[10.036194801330566, -1.531490683555603, "[TT] Orbit Inclination of the Argos-4 = 98\u00ba"]
-[13.405749320983887, 2.9043567180633545, "[TT] Total Mass of the Eutelsat 172B = 9,969 kg"]
-[7.768458843231201, 9.187673568725586, "[TT] Wavelength of the X-band = 2.9 cm"]
-[8.259922981262207, 8.630584716796875, "[TT] Spectral Sensitivity of the Spectrometer = Lower in the NIR band region than the visible band region"]
-[8.978348731994629, 7.277614593505859, "[TT] FMC (Forward Motion Compensation) system of the Metric Camera = Not added"]
-[14.61679458618164, 6.74519157409668, "[TT] Nominal Voltage of the NiH2 Batteries = 12.5 V"]
-[9.488672256469727, 7.158198356628418, "[TT] Spatial Resolution of the EXI = Better than 8 km"]
-[5.873021602630615, 0.9724055528640747, "[TT] Image Acquisition Date of the GOES-17 = October 25"]
-[5.538780689239502, 0.293498158454895, "[FF] End Date of the ISS-RapidScat = Nov. 28, 2016"]
-[5.371676921844482, 0.6771420836448669, "[TT] Launch Date of the PlanetiQ satellites = Early 2020"]
-[8.00735092163086, 4.706777572631836, "[FF] Defined by the velocity vector and nadir of the ORF (Orbit Reference Frame) = -"]
-[7.8448944091796875, 7.051894664764404, "[TT] Stability of the Interferometer = Extremely stable"]
-[10.845711708068848, 1.6636149883270264, "[FF] Material Consumption Rate of the SS 433 = Phenomenal"]
-[7.052821636199951, 5.862419128417969, "[TT] Type of the PMDs = Identical"]
-[9.873366355895996, 0.1828487366437912, "[TT] Orbital Speed of the GRACE-FO = About 7.5 km/s"]
-[5.462122917175293, 6.286546230316162, "[TT] Capacity of the Memory = 50 GB"]
-[5.325039386749268, 3.972785711288452, "[TT] Number of Satellites of the Satellite Constellation = 4425"]
-[7.381749629974365, 2.4979031085968018, "[FF] Purpose of the SAOCOM constellation = Imagery and observations in the fields of agriculture, forestry, weather, hydrology, oceanography, natural resources of land and sea, cartography, geology, mining, soil exploitation and archeology"]
-[10.739936828613281, 7.1935014724731445, "[TT] Footprint of the 8 = 14.4 x 13.1 km"]
-[7.138700485229492, 0.31552815437316895, "[FF] Detection Date of the REXIS = Last fall"]
-[9.499534606933594, 7.187726020812988, "[TT] Resolution at Nadir of the Vidicons = 1.5 km"]
-[10.82235336303711, 0.6975874900817871, "[TT] Number of Planets of the TRAPPIST-1 = 7"]
-[4.843296051025391, 4.326562404632568, "[FF] Data Volumes of the Argos-3 = Unknown"]
-[10.276586532592773, 5.983757019042969, "[TT] Temperature Range of the NIRST = MWIR: 300-700 K and TIR: 250-500 K"]
-[6.4123358726501465, -1.2683051824569702, "[TT] Measurement Date of the GRACE-FO = December 7, 2020"]
-[8.88569450378418, 3.334756851196289, "[FF] Density Ratio of the Ionosphere = 1/1000th the neutral species"]
-[8.463410377502441, 5.819003582000732, "[FF] Function of the Scanning Mirror = Sweeps the FOV across the Earth limb to obtain vertical profiles of the natural airglow radiation"]
-[6.62100887298584, 7.115778923034668, "[TT] Common Electronics of the COR1 = Common electronics, 1 MHz readout rate, 14 bit/pixel quantization"]
-[3.8029303550720215, -1.1948096752166748, "[TT] Orbit of the PLATO = Lagrangian point L2 of the Sun-Earth system"]
-[6.917939186096191, 0.06547638028860092, "[TT] Mission Duration of the SeaSat-1 = 105 days"]
-[8.162620544433594, 0.112181156873703, "[TT] Launch Date of the Meteor M2-2 = July 5, 2019"]
-[7.568722248077393, -2.4398210048675537, "[FF] Project Update Date of the GOLD = April 17, 2015"]
-[5.871340274810791, 7.018226146697998, "[TT] Data Samples of the DSLP = More than 35 million"]
-[8.503315925598145, 1.380763053894043, "[FF] Measurement of the Aquarius = Sea Surface Salinity"]
-[10.088129997253418, -1.5467338562011719, "[TT] Orbit Inclination of the CanX-2 = 97.4\u00ba"]
-[9.57542610168457, 4.163002014160156, "[TT] Model of the Magnetometer = HM2003"]
-[12.134309768676758, 3.500786781311035, "[TT] Tank of the Propulsion = 2 x 96 liter"]
-[8.130839347839355, -0.6349202394485474, "[TT] Land Ice (large scale) Temporal Sampling of the CryoSat = 1 year"]
-[7.393766403198242, 2.0632596015930176, "[FF] URL of the High Spatio-Temporal Resolution Land Surface Temperature Mission = https://web.archive.org/web/20220808212453/https://ieeexplore.ieee.org/document/8517433"]
-[6.550475597381592, 7.626299858093262, "[TT] Data Quantization of the Pushbroom imager = 12 bit (10 bit coding for downlink)"]
-[9.582486152648926, 7.0378737449646, "[TT] Spatial Resolution of the GIIRS = 2 - 16 km"]
-[9.02133560180664, 6.47048807144165, "[TT] Image Center Coordinates of the CaSSIS = 28.79\u00baS/193.84\u00baE"]
-[4.548583507537842, 1.585824728012085, "[TT] Separation Date of the ASTRO and NextSat = April 17, 2007"]
-[5.086760997772217, 6.779646873474121, "[TT] Downlink Data Rate of the Spacecraft = From 9.6 kbit/s to 8.0 Mbit/s"]
-[8.146437644958496, 5.020988941192627, "[FF] Function of the SES = Confirm predictions of thermionic and photoelectric emission"]
-[14.202749252319336, 3.1902904510498047, "[TT] Mass of the Cygnus capsule mass simulator = ~3800 kg"]
-[5.806620121002197, -0.7599874138832092, "[TT] Design Life of the FY-2F = 6 years"]
-[6.207614898681641, 6.393847465515137, "[TT] Duration of the Planned data outage = < 3 hrs / yr"]
-[6.239557266235352, 2.4773623943328857, "[TT] Location of Heat Shield Extraction of the EFT-1 Orion = NASA/MSFC (Marshall Space Flight Center)"]
-[9.139452934265137, -1.2976415157318115, "[TT] Orbit Type of the Viasat = Geostationary"]
-[4.544672012329102, 0.5334830284118652, "[FF] Transition Point of the STP-H8 and H7 = Unknown"]
-[5.483125686645508, 6.8226728439331055, "[TT] Data Pipeline of the AMS-02 = 10 Gbit/s"]
-[7.1658034324646, 5.175128936767578, "[FF] Purpose of the COTS #1 = Examine controversial elements of analog electronics in which the Elder's phenomena has been observed"]
-[7.893192291259766, 7.199314117431641, "[TT] Spectral Stability of the FTS Interferometer = 3 x 10 -7  rms for 180 s"]
-[3.56312894821167, 5.763637542724609, "[TT] Antenna Type of the SAR Downlink Transmitter = Helical"]
-[6.884583473205566, -0.6769658923149109, "[TT] Orbital Period of the HAT-P-7 = 2.2 days"]
-[6.655101299285889, 8.787820816040039, "[FF] Comments/Observations of the POLDER-1/2 = Polarization moved to 490 nm"]
-[7.208934783935547, 3.185014486312866, "[FF] Objective 1 of the EPS (EUMETSAT Polar System) = Ensure continuity and availability for operational purposes of polar meteorological observations from the \"morning\" orbit to the global user community"]
-[5.354456424713135, 1.9070656299591064, "[TT] Mission Status of the ABEX = Planned"]
-[6.151182174682617, 7.087003231048584, "[TT] Multiplexed Subchannels of the Optical Downlink = Up to 16"]
-[5.65513801574707, 5.635978698730469, "[TT] Processor Architecture of the TriG = Dual processor"]
-[5.497412204742432, 6.468496322631836, "[TT] Storage Capacity of the GAMALINK = From 2 x 2 GB"]
-[3.41595458984375, 6.440494060516357, "[TT] Aperture Antenna Diameter of the COMMx = 3.66 m"]
-[4.294498443603516, -0.11058364063501358, "[FF] Also known as of the P35-10 = Ops-7040"]
-[9.245746612548828, 2.4560673236846924, "[TT] Count of the Sprites = 2,300"]
-[4.507719039916992, 0.7576953768730164, "[TT] Integration and Test Completion Date of the PROCYON = October 2014"]
-[8.639909744262695, 8.92664909362793, "[TT] Sensitivity of the NIRSpec MIRI = 3.1 x 10 -20  Wm -2  (22.5 \u00b5m, \u03c4 i =10,000 s, R=1200)"]
-[5.119880676269531, 3.501347541809082, "[TT] Data Transmission of the CSSS = JSpOC (Joint Space Operations Center)"]
-[10.524980545043945, 1.7761714458465576, "[FF] Parameter Measurement of the NuSTAR = Temperature variations in black hole winds"]
-[6.218840599060059, -0.5252208709716797, "[TT] Operation Duration of the Science Orbit = Three years"]
-[5.596183776855469, 0.514423668384552, "[TT] Discovery Year of the LINEAR = 1999"]
-[9.744332313537598, 4.859416961669922, "[FF] Momentum Offloading Management of the PROBA-V = De-activated 10 s before the next imaging sequence"]
-[7.889012336730957, 3.9535531997680664, "[FF] Mission of the BioSentinel = Detect, measure and compare the impact of deep space radiation on living organisms over long durations in deep space"]
-[6.5332512855529785, 0.8908801078796387, "[FF] Response Time of the FormoSat-2 = Quick"]
-[8.427518844604492, 0.13541322946548462, "[TT] Landing Site of the Rosetta = Comet 67P/Churyumov\u2013Gerasimenko"]
-[8.663678169250488, 7.514705657958984, "[TT] Image Repetivity of the CCD Camera = One scan line per minute"]
-[3.826977014541626, 3.412226438522339, "[TT] Launch Date of the Galileo Satellites = July 25, 2018"]
-[3.690910816192627, 4.893200397491455, "[FF] Function of the MMO = Plan user requests for payload (SAR) tasking"]
-[6.880014419555664, 0.4583547115325928, "[FF] Observatory Collaboration Date of the Crab Nebula = May 10, 2017"]
-[11.848567008972168, 3.360042095184326, "[TT] Propulsion Subsystem of the Spacecraft = > 10 mN of thrust, > 1000 s of I sp, 3 kg of Xenon"]
-[8.090919494628906, 8.45141887664795, "[TT] Phase of the OLCI = PDR (Preliminary Design Review)"]
-[8.462567329406738, 9.38404369354248, "[TT] Uncertainty of the Responsivity Measurement = \u00b1 5%, 2\u03c3 confidence level"]
-[4.764464855194092, -0.28217414021492004, "[TT] License to Operate of the CATS = Through February 2018, perhaps longer"]
-[8.940630912780762, 4.446377277374268, "[FF] Function of the CSC/OSC Attitude Guidance = Computes the S/C attitude reference based on the sun direction and relative position inputs"]
-[5.732816219329834, 6.2686381340026855, "[TT] Data Transmission of the SSMIS = Asynchronous"]
-[10.287253379821777, 8.024308204650879, "[TT] Telescope Diameter of the VIRR = 12.7 cm"]
-[8.18022632598877, 4.5490899085998535, "[TT] Total Ionizing Dose of the Orbit = <1 krad"]
-[10.218779563903809, 7.881649494171143, "[TT] Telescope Size of the GS-1 = 1 m"]
-[11.96654224395752, 3.4133763313293457, "[TT] Predecessor of the PPS-1350-G = SPT-100 (Stationary Plasma Thruster)"]
-[14.284040451049805, 3.269026517868042, "[TT] Total Mass of the SMILES = 475 kg"]
-[6.362612724304199, 8.686225891113281, "[TT] Polarization States of the MWR = 4"]
-[6.974991321563721, 8.11391830444336, "[TT] Type of the CNS = Correlated Noise Source"]
-[13.516362190246582, 5.8039326667785645, "[TT] Power Generation of the SPOT-3 = Solar array"]
-[8.048126220703125, 4.343597888946533, "[FF] Objective of the CREDO-II = To monitor aspects of space radiation which cause single event effects in microelectronic components"]
-[5.143217086791992, 4.277646064758301, "[TT] Number of L-band payloads scheduled for operational deployment by 2019 of the Glonass-K1 = Approximately 35"]
-[9.989094734191895, 7.941980361938477, "[TT] Light-Tight Requirement of the Telescope = Three-bounce"]
-[6.931628227233887, 6.846371650695801, "[TT] Type of the T2L2 = Laser Link"]
-[5.565720081329346, 7.731012344360352, "[TT] EIRP of the USAT (Ultra Small Aperture Terminal) = >55.0 dBW"]
-[12.024630546569824, 3.4601571559906006, "[TT] Thrust of the PPCU = 20 mN"]
-[11.748709678649902, 3.371539831161499, "[TT] Quantity Launched of the SuperDoves = 12"]
-[13.171709060668945, 7.2967658042907715, "[TT] Power Consumption of the POLDER-2 = 42 W"]
-[6.417194843292236, 3.9360883235931396, "[TT] Same Instrument as of the MAHRSI = STS-66 mission (CRISTA-SPAS-1)"]
-[8.0177583694458, 0.8720191121101379, "[FF] Date of the Turkey Experiences Intense Drought = 16 January 2021"]
-[6.0615644454956055, 2.2766733169555664, "[TT] Recovery Team of the Orion = U.S. Navy divers in several rigid hull and Zodiac boats"]
-[8.295570373535156, 8.278580665588379, "[TT] VNIR Detector Material of the GLI = Si"]
-[8.606072425842285, 6.081802845001221, "[TT] Measurement Range of the OVM = 16,000 - 64,000 nT"]
-[11.334392547607422, 3.6196110248565674, "[FF] Service of the Maxar Space Solutions = Providing a high-power solar electric propulsion spacecraft chassis"]
-[4.753541469573975, -1.1167107820510864, "[TT] Launch Site of the Long March 4B (LM-4B) = Taiyuan Satellite Launch Complex in Shanxi, China"]
-[7.0066986083984375, 7.798768997192383, "[TT] Field of View of the Micropore Reflector = 21.2\u00b0 squared"]
-[10.234444618225098, 1.9586018323898315, "[TT] Date of First X-ray Images of the eROSITA = 22 October 2019"]
-[7.999926567077637, 0.5388486385345459, "[FF] Measurement Unit of the GRACE-FO = Wetness Percentile"]
-[8.289472579956055, 3.036236524581909, "[TT] Atmospheric Species of the SciSat-1/ACE = Over sixty"]
-[11.708580017089844, 4.351112365722656, "[TT] Payload Fairing Diameter of the CBAS and EAGLE = 5 m"]
-[8.35580062866211, 7.892192840576172, "[TT] Number of Holes of the Spectrometer Wheel = 14"]
-[10.15483570098877, 7.896113395690918, "[TT] Telescope Rotation Angle of the MVIRI = 1.25 x 10-4 radians"]
-[9.73640251159668, -0.37825313210487366, "[TT] Altitude of the GCOM-C = 798 km"]
-[8.10245132446289, 8.382843971252441, "[FF] Technology of the SHIMMER = SHS (Spatial Heterodyne Spectroscopy)"]
-[5.223012924194336, 2.337331533432007, "[FF] Heritage of the AOE-2 = Heritage of STRV-1a"]
-[11.050909996032715, 6.149260520935059, "[TT] Material of the Glass Layers = W/Si, Pt/SiC, Pt/C"]
-[8.217062950134277, 6.49826192855835, "[FF] Optical Power of the Temperature-and-current-stabilized LD = Unknown"]
-[6.231130123138428, 4.821477890014648, "[FF] Function of the Payload OBC = Record and store data from GPS experiments"]
-[2.32657527923584, 1.3117172718048096, "[FF] Conference Presentation of the NanoSail-D = April 9-11, 2008"]
-[10.101362228393555, -2.6875407695770264, "[TT] Power (record & replay) of the Astrium MMFU NAND-Flash SDR-SDRAM = \u2264 130 W"]
-[13.606926918029785, 1.745706558227539, "[TT] Cargo Capacity of the Dragon = 2,630 kg"]
-[13.515868186950684, 5.739450931549072, "[FF] Power Source of the Psyche = Solar Arrays"]
-[3.3754448890686035, 6.451740741729736, "[TT] Antenna Diameter of the USAT = 45 cm"]
-[7.974571704864502, 1.7543959617614746, "[FF] Contribution of the GOCE = Map changes in gravity over time"]
-[8.582695960998535, 7.675089359283447, "[TT] Detector Array of the WiFS camera = 2 x 2048 pixels"]
-[9.424131393432617, 5.109678268432617, "[TT] Phase Center Stability of the NAVANT = Worst case of \u00b13.5 mm"]
-[8.833346366882324, 3.0090205669403076, "[FF] Light Emission of the Transient Luminous Events = Weak"]
-[9.686807632446289, 4.038883209228516, "[TT] Dynamic Range of the Vector Magnetometer = \u00b165,536 nT"]
-[7.123329162597656, 0.8528684377670288, "[TT] Date of the Tohoku-Kanto earthquake = March 11, 2011"]
-[6.337553024291992, 4.3765082359313965, "[FF] Function of the Spacecraft Operation Planning System = Operation planning of each ground station"]
-[8.174568176269531, 1.1989349126815796, "[TT] Soil Moisture Resolution of the SMAP = 10-km"]
-[14.220459938049316, 3.186814308166504, "[TT] Mass of the ASIM = 314 kg"]
-[7.635824680328369, 1.2645231485366821, "[TT] Purpose of the ShadowCam = Obtain optical images at high-resolution of the permanently shadowed regions at the lunar poles of the Moon"]
-[13.853432655334473, 7.037827014923096, "[FF] Power Interface of the ESEO-TriTel EQM = TriTel PS (Power Supply) board"]
-[6.474562644958496, 3.0154263973236084, "[TT] Revisit Rate of the Planet SkySats = As high as 10 times per day"]
-[3.810314416885376, -1.1413334608078003, "[TT] Orbit of the DELPHINUS = Halo orbit around the EML2"]
-[6.147320747375488, 8.011231422424316, "[TT] Number of Channels of the NorAIS-2 Receiver = Four"]
-[5.646914958953857, 2.586857318878174, "[FF] Budget of the Euro-Argo ERIC = Not specified"]
-[9.981121063232422, 4.350661754608154, "[FF] Development Team of the Magnetic Torquer = Y. Aoyanagi, T. Sato, T. Yoneya, J. Nishidate, T. Ono, Y. Tanaka, T. Iwamoto, R. Mitsuhashi, S. Satori, K. Ishimura, T. Totani, K. Sugimoto, D. Igarashi, H. Hoshika, T. Sakakibara, T. Yasunaka, T. Uematsu, S. Era, K.Hori, A. Nakamura,, N. Hirota"]
-[9.577451705932617, 7.324952602386475, "[TT] Pan Resolution at Nadir of the QuickBird-2 = 0.61 cm"]
-[6.74975061416626, 5.5051655769348145, "[FF] Phase Data of the BSC = Memorized"]
-[4.744357585906982, 0.5340933799743652, "[TT] Launch Date of the OSCAR-QUBE = 29 August 2021"]
-[7.319184303283691, 4.131300926208496, "[FF] Measurement Synergy of the GMI Radiometer = Mutual overlap of actively sensed, vertically-profiled, radar data at two frequencies in combination with the multi-channel passive data of GMI"]
-[10.750877380371094, 7.170891284942627, "[TT] Footprint of the Argus = 1 km x 1 km"]
-[5.593292236328125, 4.6798505783081055, "[FF] Services of the Hellas Sat 3 = Direct-to-home (DTH) TV broadcast and telecommunications services, distribution of high-definition (HD) and ultra-high definition (UHD) video content"]
-[4.860917091369629, 0.42308589816093445, "[TT] Installation Date of the SUVI = September"]
-[12.087053298950195, 6.926576614379883, "[TT] Photon Index Above the Break of the First Broken Powerlaw = 1.4"]
-[13.241056442260742, 5.248549461364746, "[TT] Solar Array Size of the TOPEX/Poseidon = 8.9 m x 3.3 m"]
-[7.046346664428711, 7.089391231536865, "[TT] Divergence of the Acquisition/Tracking Lasers = 500/1500 \u00b5rad"]
-[5.162627220153809, 2.1861937046051025, "[FF] Mission Type of the ST5 = EO"]
-[3.7545127868652344, 6.3420562744140625, "[TT] Antennas of the NSCAT = 6"]
-[8.362717628479004, 3.183971643447876, "[TT] Spectral Coverage of the Atmospheric Chemistry Suite = From 0.7 to 17 micrometers"]
-[10.867389678955078, 7.50558614730835, "[TT] Swath Width of the TOMS = About 3000 km"]
-[4.955545425415039, 3.109989643096924, "[TT] Design and Development Organizations of the MOMS = DLR, LMU, EADS Astrium GmbH"]
-[9.446839332580566, 5.038267135620117, "[TT] Attitude Accuracy of the ACS = \u00b12\u00ba"]
-[13.15132999420166, 7.2330169677734375, "[TT] Power Consumption of the MCU = 65 mA - active"]
-[9.686704635620117, 4.103761196136475, "[FF] Type of the In-panel magnetorquers = Unknown"]
-[5.010922431945801, 1.4265503883361816, "[TT] Launch Date of the Flying Laptop = 14 Jul 2017"]
-[8.966819763183594, 5.494400501251221, "[TT] Spacecraft Velocity of the ABI = < 6 cm/sec uncertainty per axis"]
-[4.927714824676514, 1.253433108329773, "[TT] Launch Year of the Himawari-9 = 2016"]
-[8.089468955993652, 8.234601974487305, "[TT] Quantum Efficiency of the Instrument = 0.8 at 630 nm"]
-[14.343409538269043, 3.0895369052886963, "[TT] Total Mass of the AlSAT-1 = 98 kg"]
-[5.0077996253967285, 1.6667044162750244, "[TT] Operation Status of the INSAT-3D = Nominal"]
-[9.821797370910645, 8.67513370513916, "[TT] FOV of the ScaRaB = 100\u00ba (3200 km)"]
-[11.795247077941895, 4.827133655548096, "[TT] Tray Dimensions of the UniSat-4 = 150 mm side with an overall height of 250 mm"]
-[9.809475898742676, -0.5493934750556946, "[TT] Orbit of the Spacecraft = 600-850 km altitude"]
-[9.773595809936523, 7.4614057540893555, "[TT] Ground Sample Distance of the GSD = 12 m at nadir"]
-[8.111836433410645, 4.189941883087158, "[TT] Maneuver Type of the Spacecraft = Formation flying demonstration maneuvers and Sun corona observation"]
-[4.865655899047852, 7.911627292633057, "[TT] Frequency Band of the GETR (Galileo Experimental Test Receiver) = E5a 1176.45 MHz"]
-[6.240604400634766, 2.6642401218414307, "[FF] Payloads of the Orion Vehicle = Unknown"]
-[9.91723346710205, 5.551152229309082, "[TT] Accuracy of the CLARREO = 0.1 K in brightness temperature"]
-[10.142879486083984, 4.605586051940918, "[FF] Goal of the Superconducting Magnet = Extend the energy range of particle and nuclei measurements to the multi-TeV region"]
-[4.256534576416016, 7.312663555145264, "[TT] Frequency of the S-band Transmitter = S-band"]
-[11.815263748168945, 6.764861583709717, "[TT] Electron Energy Range of the LIPS = 30 keV - 2 MeV"]
-[8.351547241210938, 7.246931552886963, "[TT] Integration Time of the PMC-2 Imagers = 1~96 levels"]
-[5.555823802947998, 3.9016780853271484, "[TT] Number of Satellites of the DMSP (Defense Meteorological Satellite Program) = 19"]
-[13.353625297546387, 7.839049339294434, "[TT] RF Output Power of the X-band Transmitter = 6 W"]
-[5.13539457321167, 1.136448621749878, "[FF] Presentation Date of the BEESAT-3 = Oct. 10-13, 2012"]
-[5.538398265838623, 4.4248881340026855, "[TT] Ground Control Network of the R3 spacecraft = Multi-station"]
-[5.896491527557373, 1.6118500232696533, "[TT] Back-up Ground Station of the IXPE Observatory = NEN ground station in Singapore"]
-[8.793578147888184, 3.025994062423706, "[FF] Mission Objective of the CADRE = Study of thermospheric properties"]
-[5.294367790222168, 5.097317218780518, "[FF] Signal of the GPS Receiver = L1"]
-[8.614413261413574, 5.7213664054870605, "[TT] Accuracy of the FTS Sensor = 0.1 K 3\u03c3"]
-[9.822144508361816, 7.776943206787109, "[FF] Quantity of the Telescope = 1"]
-[9.184619903564453, -0.38268542289733887, "[FF] Apogee Alignment of the MMS and THEMIS = Roughly 90\u00ba"]
-[7.699284076690674, 9.382757186889648, "[TT] Center Wavelength of the Band 6 = 2.25 \u00b5m"]
-[10.455955505371094, 6.065038204193115, "[TT] Camera Cooling Temperature of the eROSITA = -90\u00b0C"]
-[5.740294933319092, 3.3162901401519775, "[TT] Capital Raise of the Astrocast = Up to 50 million Francs"]
-[13.618080139160156, 5.7801408767700195, "[FF] Power Source of the Corvus-BC satellites = Body-mounted solar panels, two deployable panels, 48 Watt-hour batteries"]
-[10.817980766296387, 2.099787950515747, "[FF] Simultaneous Observations of the NuSTAR, Juno, and XMM-Newton = Conducted"]
-[14.468791961669922, 6.785487651824951, "[TT] Minimum Battery Voltage of the IXV = 30.4 V"]
-[4.796482086181641, 0.47384214401245117, "[TT] Launch Date of the SPROUT = May, 24 2014"]
-[8.17032527923584, 1.2165545225143433, "[TT] Rainfall of the Dnieper watershed = 70 percent of its usual"]
-[10.943888664245605, 2.070413827896118, "[TT] Mission Duration of the XMM-Newton = 20 years"]
-[6.8895673751831055, 5.087182521820068, "[FF] Input of the Onboard Neural Network = Magnetic or electric component in the VLF range"]
-[4.713996410369873, 0.0055604055523872375, "[TT] End of Life of the S3A = 2026"]
-[6.904709815979004, -0.6464894413948059, "[TT] Orbit Period of the AlSat-2A = 98 minutes"]
-[10.384469032287598, 2.3367552757263184, "[FF] Observation Type of the Soft X-ray Measurements = Line-of-sight observations"]
-[14.425100326538086, 3.3527231216430664, "[TT] Mass of the SDS-4 = ~50 kg"]
-[13.243119239807129, 2.9677011966705322, "[TT] Mass of the GHGSat = 35 kg"]
-[10.067767143249512, -1.5284976959228516, "[TT] Inclination of the OrbView-2 = 98.2\u00ba"]
-[6.653210163116455, 6.372590065002441, "[TT] Number of Switches of the DLP System = 5"]
-[11.66256332397461, 6.822150230407715, "[TT] Energy Resolution of the ART-XC = 1.4 keV at 14 keV"]
-[9.47439956665039, -0.9825153946876526, "[FF] Kinematic properties of the ISD = 25 km/s, ecliptic longitude of 252\u00ba & ecliptic latitude of 5\u00ba"]
-[7.1556549072265625, -0.747061550617218, "[TT] Orbital Period of the Beijing-1 = About 97.7 minutes"]
-[13.286351203918457, 7.5494465827941895, "[TT] SSPA Output Power of the VSAT (Very Small Aperture Terminal) = 40 W"]
-[3.467099189758301, 4.813711166381836, "[FF] Data Link Subsystem of the X-band SAR payload system = Included"]
-[6.064907550811768, 2.544990062713623, "[FF] Tester of the ISIM = Matt Greenhouse"]
-[5.768880844116211, -0.39816275238990784, "[TT] Release Time of the Intelsat 39 = 29 minutes after liftoff"]
-[4.821868419647217, 0.4977819621562958, "[TT] 1st LO of the HRIT HiRID = 1900"]
-[5.4560394287109375, 0.6605839729309082, "[TT] Arrival Date of the Messenger = 18 March 2011"]
-[3.7432308197021484, -0.7354863882064819, "[TT] Orbit of the AstroBus-L = Low Earth Orbit (LEO)"]
-[5.395811080932617, 1.656138300895691, "[FF] URL of the ALOS-2 = http://earth.esa.int/workshops/polinsar2009/participants/535/pres_8_Shimada_535.pdf"]
-[9.486841201782227, 7.326955318450928, "[TT] Radiometric resolution of the C-band = 0.6 K"]
-[10.402236938476562, 2.0804104804992676, "[TT] Survey Duration of the eROSITA X-ray telescope = 6 months"]
-[12.038082122802734, 4.404391288757324, "[TT] Size of the Spacecraft = 12U"]
-[4.060938835144043, 2.1571877002716064, "[TT] Launch Vehicle of the Herschel Telescope = Ariane-5 ECA"]
-[7.361506462097168, 7.374690055847168, "[FF] Dataset Sizes of the EO-ALERT = Wide range"]
-[7.150121688842773, 7.5516438484191895, "[TT] Sigma 0 Precision of the DPS = 0.5 dB"]
-[7.900918960571289, 6.594886779785156, "[FF] Measurement of the ATLAS = Atmospheric Backscatter"]
-[14.054457664489746, 4.007411479949951, "[TT] Mass of the Instrument = 320 kg"]
-[4.49459171295166, -0.2805441617965698, "[FF] Docking Attempt Date of the MEV-2 = 10 March 2021"]
-[11.723663330078125, 3.2883012294769287, "[TT] Duration Pulses of the LM thruster = Up to 8.0 sec"]
-[9.723809242248535, 7.433465480804443, "[FF] Ground Sampling Distance (GSD) of the Imager = Not provided"]
-[7.702691555023193, 9.24223518371582, "[TT] Wavelength Range of the Band 12 = 9.42-9.8 \u00b5m"]
-[9.729863166809082, 7.446089744567871, "[FF] Sequential Ground Sampling Distance (SGSD) of the Imager = Not provided"]
-[8.901676177978516, 4.440694808959961, "[TT] Attitude Sensing of the ACS = Sun sensors, star sensors and gyroscopes"]
-[5.6852641105651855, 5.5809149742126465, "[TT] Housekeeping Computers of the GNB = 1 ARM7"]
-[10.564180374145508, 0.6863204836845398, "[TT] Orbital Distances of the TRAPPIST-1 = Within the orbital distance of Mercury"]
-[7.178426265716553, 1.3686366081237793, "[FF] Purpose of the Mars Terrain Simulator = Validate and simulate ExoMars Rover Operations and to support the ExoMars Surface Mission"]
-[8.435235023498535, 6.0816874504089355, "[TT] Measurement Error of the Instrument = 0.5 K"]
-[7.385134220123291, 4.73556661605835, "[FF] Instruments of the NPOESS-C1 = CERES and TSIS"]
-[10.510458946228027, 1.584437608718872, "[TT] Number of Stars of the Six-star System = 6"]
-[8.00991153717041, 0.5827586650848389, "[FF] Survival of the Bdelloids = Can survive year-long droughts in the Sahara desert as well as in the frozen plains of Antarctica"]
-[14.266392707824707, 3.154470682144165, "[TT] Total Mass of the S/C = 100 kg"]
-[7.121771812438965, 5.525454044342041, "[FF] Quantity of the MSGI-MKA = 1"]
-[10.920442581176758, 5.052640438079834, "[TT] Probes Distance of the TPS = 10 cm"]
-[8.509196281433105, 2.196629285812378, "[FF] Date of the Long-lasting Dust Storm from Chihuahua = 18 March 2021"]
-[3.697033166885376, 5.46856164932251, "[FF] Output of the SARP = 2400 bit/s bit stream"]
-[6.509235382080078, 4.307709693908691, "[FF] Data Availability of the ResourceSat-1 = Unknown"]
-[6.944573402404785, -0.7723292708396912, "[TT] Orbit Period of the Beta Pictoris b = 21 years"]
-[6.342840194702148, 1.0786240100860596, "[TT] Image Acquisition Date of the Landsat 8 = February 5"]
-[11.437098503112793, 3.55007266998291, "[TT] Thruster Location of the CanX-4&5 = One face only"]
-[7.675595283508301, 0.72264164686203, "[FF] Mission of the Broadband InfraRedCompact High-resolution Exploration Spectrometer = Lunar Ice Cube"]
-[9.65659236907959, -0.4329436719417572, "[TT] Altitude of the SAOCOM-1A and -1B = 619.6 km"]
-[11.665390014648438, 6.633774280548096, "[TT] Energy: 0.4 keV (3.1 nm) of the N K-edge = N at 0.4 keV (3.1 nm)"]
-[6.021583080291748, 4.6948933601379395, "[FF] Unknown of the Satellite communication protocol experiment = Unknown"]
-[13.415904998779297, 7.335773944854736, "[TT] Power of the Total = 13.9 W"]
-[6.994292259216309, 7.743608474731445, "[TT] Size of the Reflector Cubes = No bigger than the tip of a pinkie finger"]
-[10.66659164428711, 2.7904856204986572, "[FF] Operation Date of the FASat-Bravo microsatellite = Jan. 15, 2003"]
-[8.694272994995117, 6.5319976806640625, "[FF] Imagery of the Maxar WorldView-2 = Acquired over the poorly charted area"]
-[6.558978080749512, 0.9214029312133789, "[FF] Functionality of the FormoSat-2 = About 70% after 11 years"]
-[9.6613130569458, -0.36133885383605957, "[TT] Maximum Elevation of the ASTERIA = Varies"]
-[6.778947830200195, 1.600091814994812, "[FF] URL of the Emirates Mars Mission (Hope) = https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=EMM-HOPE"]
-[14.24859619140625, 3.151172637939453, "[TT] Weight of the OSIRIS = Approximately 5 kg"]
-[7.450984954833984, 2.9358620643615723, "[TT] Methane Detection Limit of the MethaneSat = 2 parts per billion"]
-[14.440279006958008, 6.424565315246582, "[TT] Fabrication Defect of the Robusta = Prevents the CubeSat\u2019s batteries from being charged"]
-[5.232309341430664, 4.936942100524902, "[TT] Operating Voltage of the NovAtel OEMV-2 L1/L2-F GPS unit = 3.3 VDC"]
-[7.870271682739258, 4.817877292633057, "[FF] Method of the Estimation Filter = Combining measurements from several different sensors"]
-[8.067992210388184, 6.853538990020752, "[FF] Operation of the Hyperbolic detector = Detects targets with a high probability of detection while allowing a rather large number of false alarms"]
-[4.119692325592041, 9.448288917541504, "[TT] Frequency Band of the ISA = 3 x 10-5 \u2014 1 x 10-1 Hz"]
-[9.475323677062988, 6.271146774291992, "[TT] Scan Mirror Rotation Frequency of the GLI = 16.7 Hz"]
-[14.211173057556152, 3.2682268619537354, "[TT] Mass of the XRD = 4,026 g"]
-[9.619141578674316, 7.278911113739014, "[TT] Spatial Resolution of the POLDER-2 = 6 x 7 km at nadir"]
-[7.280107021331787, 2.412289619445801, "[FF] Area of the SAA = Stretching from Africa to South America"]
-[12.02529239654541, 6.262061595916748, "[TT] Antiproton Flux Accuracy of the AMS-02 = 1%"]
-[11.887080192565918, 5.625654697418213, "[TT] Material of the ICON FUV Instrument = CsI"]
-[7.09041690826416, 1.3348933458328247, "[TT] Flare Detection Date of the Spitzer Space Telescope = July 31, 2019"]
-[5.704832077026367, 3.124769926071167, "[TT] Operations Manager of the GOES-N = United States Space Force (USSF)"]
-[5.455535411834717, 2.9649465084075928, "[TT] Development Collaboration of the Satellite = ESA and CNES"]
-[8.169005393981934, 8.670406341552734, "[TT] Spectrometer Bands of the GeoCarb = 0.76 \u00b5m, 1.61 \u00b5m, 2.06 \u00b5m and 2.32 \u00b5m"]
-[5.595235347747803, 2.516310214996338, "[FF] Name Origin of the \u00d8rsted = Hans Christian \u00d8rsted"]
-[5.361006736755371, -0.29719460010528564, "[TT] Ignition Time of the ALOS-3 = 8:37 p.m. EST"]
-[4.504075527191162, 7.695794582366943, "[TT] Propagation distance of the Uplink (VHF) = ~ 1000 km"]
-[3.711961269378662, 4.850330829620361, "[TT] Range x Azimuth of the RADARSAT-1/2 = 25 x 28, 25 x 28, 40 x 28, 20 x 28, 10 x 9, 100x100, 50 x 50, 25 x 28, 11 x 9, 11 x 9, 3 x 3"]
-[4.980015277862549, 0.8510497808456421, "[TT] First Flight Date of the ESPA = March 9, 2007"]
-[7.111696243286133, 6.388518333435059, "[FF] Function of the ARC = Enable the dynamic control and optimization of power, throughput, beams and frequency allocation"]
-[12.140252113342285, 4.661050319671631, "[TT] Bus Height of the OSAM-1 = 14-foot-tall"]
-[4.191817760467529, 3.947666883468628, "[TT] RNSS Signal Allocations Deadline of the Galileo = Mid-2006"]
-[6.00986385345459, 2.5874476432800293, "[FF] ISS of the EUVI = Included"]
-[6.56688928604126, 5.0736799240112305, "[FF] Function of the NEXTAR Data & Command Subsystem = Data & Command Handling"]
-[13.521916389465332, 7.134342670440674, "[TT] Power Efficiency of the PS-1 and PS-2 = 90%"]
-[3.4356350898742676, 4.861732482910156, "[FF] Designers of the SAR-GMTI processing system = P. D. Beaulne, C. H. Gierull, C. E. Livinstone, I. C. Sikaneta, S. Chiu, S. Gong, M. Quinton"]
-[10.727485656738281, 0.9875315427780151, "[TT] Size of the KELT-9 b = 1.8 times bigger than Jupiter"]
-[14.230751037597656, 3.203721284866333, "[TT] Mass of the NINA = 40 kg"]
-[12.162023544311523, -0.07283314317464828, "[TT] Coating of the TESS Lens = Antireflection"]
-[4.996551513671875, 2.6042518615722656, "[TT] Compatible with of the STPSat-5 = ESPA-class secondary launch adaptors"]
-[10.970276832580566, 2.0436010360717773, "[TT] Mission Extension Period of the XMM-Newton = 1 January 2015 \u2013 31 December 2016"]
-[5.315069198608398, 3.711663007736206, "[TT] Instrument type of the Meteosat Comms = Communications"]
-[9.331851959228516, 3.283499240875244, "[FF] Function of the Solar concentrator = Protect the samples"]
-[5.478005409240723, 0.578207790851593, "[TT] Year of Launch of the QuikSCAT = 1999"]
-[8.470845222473145, 7.68744421005249, "[TT] Pixel Pitch of the Pan CCD detector module = 8.75 \u00b5m"]
-[4.254439353942871, 2.263883113861084, "[TT] Launch Site of the CANYVAL-X CubeSats = SDSC (Satish Dhawan Space Center) SHAR (Sriharikota) on the east coast of India"]
-[10.491592407226562, 5.784047603607178, "[TT] Thermal Conductivity of the Carbon-Carbon Radiator panel = 230 W/m K"]
-[9.686379432678223, 7.112201690673828, "[TT] Spatial Resolution of the AATSR = 1 km x 1 km"]
-[8.045513153076172, 8.175707817077637, "[FF] Shift of the Absorption Feature = Blue-shifted"]
-[10.196505546569824, 5.410531997680664, "[FF] Thermal Constraint of the S/Cs = Compliance required"]
-[5.024692058563232, -0.5007421970367432, "[TT] Contact Time after Launch of the Mey-Lin (C6), Gaspard (C7), and Oc\u00e9ane (C8) = Within 90 minutes"]
-[7.081022262573242, 3.7310452461242676, "[FF] Formation Flying of the PROBA-3 = Precise"]
-[3.7275710105895996, 4.574211120605469, "[TT] Quantity of the ICEYE-X4 and ICEYE-X4 SAR = 2"]
-[9.583564758300781, 8.213616371154785, "[TT] Field of View (Individual) of the HRV = 4.13\u00b0"]
-[5.173933982849121, 6.938361167907715, "[TT] Efficiency (bit/symbol) of the Service downlink = 2"]
-[5.143614768981934, 0.8839202523231506, "[TT] Launch Date of the EuTEF = Feb. 7 2008"]
-[9.882702827453613, 7.525845050811768, "[FF] Components of the OLS = Two telescopes and a photomultiplier tube (PMT)"]
-[11.674409866333008, 4.5601277351379395, "[TT] Primary Density of the Didymos = 2.1 g/cm3"]
-[5.551624774932861, 7.287062644958496, "[TT] Error Correction of the Demodulator = RS (255, 223)"]
-[18.665739059448242, 3.935987949371338, "[TT] NE\u0394T (K) of the ICI-1 = 0.6"]
-[7.877748966217041, 8.56423568725586, "[TT] MWIR and TIR Spectral Range of the GLI = 3.715 - 11.95 \u00b5m"]
-[6.614493370056152, 4.602628707885742, "[FF] Function of the Node-3 = Provides a pressurized passageway between berthed habitable volumes"]
-[11.172599792480469, 0.6235464811325073, "[FF] Configuration of the NIRISS = Grisms and filters optimized for first-light science and exo-planet observations"]
-[5.449028015136719, 5.077181339263916, "[FF] Ground Station Links of the Communication S/S = Up and down links"]
-[5.915202617645264, 1.4050554037094116, "[FF] Presentation Date of the HICO = June 7, 2010"]
-[7.046814441680908, 8.356812477111816, "[TT] SNR of the Band 5 = 110"]
-[12.097259521484375, -0.30957168340682983, "[TT] Orbit Period of the TESS = 51.4 days"]
-[14.183326721191406, 3.3330881595611572, "[TT] Average Mass of the ETB sub-experiment = 250 gram"]
-[8.846598625183105, 6.794073581695557, "[TT] Temporal Resolution of the HY-1C = 1 day"]
-[7.399104595184326, 2.2010183334350586, "[FF] Data Use of the PROBA-V = Global vegetation data for operational and scientific use"]
-[6.712718963623047, 0.24151918292045593, "[TT] Map Date of the CryoSat-2 = Dec. 15, 2014"]
-[10.5180082321167, 5.662789344787598, "[TT] Temperature Range of the VELOX-PII CubeSat = 20-40\u00baC"]
-[3.910842180252075, 4.245837211608887, "[TT] Imagery Provision of the RADARSAT-2 = Until November 2014"]
-[5.300491809844971, 1.4052201509475708, "[FF] Deorbit Date of the ORBCOMM = Oct. 15, 2012"]
-[10.345956802368164, 4.529299736022949, "[FF] Design Concept of the RW = Cluster of four wheels in hot redundancy"]
-[8.062630653381348, 0.6452576518058777, "[FF] Outlines Change of the Subglacial Lakes = Gradually as water enters and leaves the reservoirs"]
-[8.65364933013916, 7.571682453155518, "[TT] MS Image Frame Size of the OIS = 4 MByte for a single MS frame, 12 MB for a full MS frame"]
-[7.9047160148620605, 2.5153393745422363, "[FF] Objectives of the ABI = Hurricane track & intensity forecast"]
-[12.11612606048584, -0.304559588432312, "[TT] Period of the TESS = 13.7 days"]
-[10.600107192993164, 2.8294520378112793, "[FF] Project Goal of the Small or Nanosatellite = Develop \"building blocks\" for larger scale systems"]
-[7.10668420791626, 6.924562454223633, "[TT] Update Rate of the Metrology Laser = 100 Hz"]
-[6.37113094329834, 0.4107641577720642, "[TT] Development Phase of the ROSE-L = Phase C"]
-[8.318477630615234, 0.7464069128036499, "[TT] Evacuated People of the Calf Canyon-Hermits Peak fire = Thousands"]
-[7.852280139923096, 7.906914234161377, "[TT] TDI Lines of the R3 Sensor = 11, 19, 21, 21, 21, 21"]
-[5.603270053863525, 6.185694217681885, "[TT] Total Parameter Size of the C&DH module = 36 kB"]
-[4.8308796882629395, 0.43396735191345215, "[TT] Deployment Date of the CRISTA-SPAS-2 = Flight day one"]
-[6.0500030517578125, 3.0089995861053467, "[FF] Imaging Payload Provider of the WorldView Legion constellation = Raytheon"]
-[5.828866481781006, -0.8416803479194641, "[TT] Design Life of the Spacecraft = 3 years"]
-[7.95142126083374, 7.857531547546387, "[TT] Frame Rate of the HSC-III optics subsystem = 200 1/s"]
-[10.894050598144531, 2.1220736503601074, "[TT] Exposure Time per Frame of the XMM-Newton = About three minutes"]
-[4.893993854522705, 0.6251600384712219, "[FF] Testing Date of the GOES-T = 29 September 2020"]
-[9.143491744995117, 8.089949607849121, "[FF] Sample Size of the Vera C. Rubin Observatory = Very large"]
-[6.902923583984375, -0.8382551074028015, "[FF] Orbital Period of the A and C systems = Roughly every day and a half"]
-[2.605046510696411, 3.3344476222991943, "[TT] Quantity of the Flock-4v = 4"]
-[9.548666000366211, 8.065232276916504, "[FF] Field of View of the Limb Channel = Wide (along the limb) and short (in the vertical direction)"]
-[12.031551361083984, -0.3848266005516052, "[FF] Mission Date of the TESS = Unknown"]
-[9.357522010803223, 5.001074314117432, "[TT] Platform of the BILSAT-1 = Three-axis controlled platform with agile maneuvering capability"]
-[5.512948513031006, 6.36359977722168, "[TT] Data Storage of the MAC = 32 Gbit"]
-[5.3680853843688965, 3.951165199279785, "[TT] Total Satellites of the Planet = 149"]
-[6.477314472198486, 2.881582736968994, "[FF] Environment of the ISS = Permanently crewed operational environment"]
-[6.295083522796631, -0.2884696424007416, "[TT] Operation Time of the MEPSI = Up to 24 hours"]
-[7.9666948318481445, 7.460562229156494, "[TT] Data Bit Depth of the Camera = 12 or 8 bit"]
-[8.707822799682617, 4.231424808502197, "[TT] Calibration of the UVNS = High absolute accuracy using sunlight and on-board illumination sources every orbit"]
-[9.01559829711914, 0.545761227607727, "[TT] Manned Moon Landing Deadline of the Artemis Program = 2024"]
-[5.62653112411499, 5.494715213775635, "[TT] Model of the EC = SMJ3320C30"]
-[4.454086780548096, 0.5493261218070984, "[TT] Launch Date of the First COSPAS Payload Launch Date = June 29, 1982"]
-[5.5351057052612305, 6.390352725982666, "[TT] Capacity of the SSDRs = 2 GByte"]
-[4.528175354003906, -0.8561841249465942, "[TT] Spacecraft of the SpaceX = Dragon"]
-[7.61958122253418, 8.216999053955078, "[TT] Sensitivity Range of the SXS = Fe-K region"]
-[9.525673866271973, 6.0556111335754395, "[TT] Tilt of the PAN-A = -5\u00ba"]
-[3.7907509803771973, 4.3574371337890625, "[FF] Mission Scenario of the DLR SAR = Climate research and environmental monitoring"]
-[3.4658493995666504, -0.8557192087173462, "[TT] Orbit Type of the Tsubame = Sunynchronous"]
-[5.581379413604736, 5.949796199798584, "[TT] Processor FLOPS of the MPM = 10 FLOPS"]
-[5.897946357727051, 1.860680103302002, "[TT] Launch Date of the Orion EFT-1 = December 5, 2014"]
-[7.438081741333008, 4.204617977142334, "[FF] Mission Objectives of the WPIx = 1) Determine VLF injection efficiency from a space-based antenna. 2) Map VLF fields from geophysical and man-made sources 3) Measure precipitating particles scattered by VLF from geophysical, ground-based transmitter, and DSX VLF transmitter sources"]
-[6.822113513946533, 7.755128383636475, "[TT] Reflector Dish Diameter of the COMMx = ~3.75 m"]
-[6.848896503448486, 5.958159446716309, "[TT] Spore Quantity of the bioCD = 8"]
-[7.5699052810668945, 6.989412784576416, "[TT] Useful Scan Time of the ScaRaB = 3.18 s"]
-[8.546347618103027, 1.8493633270263672, "[TT] Error of the Ocean SST = \u00b11.0 K"]
-[13.924612045288086, 7.1247382164001465, "[TT] Output Voltage of the High Voltage Power Supplies = Additional 15 kV supply for the ions"]
-[9.032638549804688, 7.011906147003174, "[FF] Resolution of the ONC = High-resolution"]
-[7.532502174377441, 3.6205101013183594, "[FF] Usage of the NightPod = Take images of stars"]
-[7.515744686126709, 7.686964511871338, "[TT] Dynamic Range of the GLI = Wide"]
-[8.383015632629395, 7.929946422576904, "[TT] Type of Array of the NIR = HgCdTe"]
-[5.537420749664307, 0.8604068756103516, "[FF] Launch Date of the Satellite Vu\u2019s second satellite = Early 2024"]
-[10.237502098083496, 5.731647968292236, "[TT] Temperature of the CCDs = -22\u00baC"]
-[10.32402515411377, 2.7014272212982178, "[TT] Launch Time of the CADRE nanosatellite = 21:44:57 UTC"]
-[13.604846954345703, 5.875866889953613, "[FF] Function of the EPS board = Interface many solar arrays, integrate active solar array maximum power point tracking, protect the battery from under-voltage"]
-[11.568815231323242, 3.3976378440856934, "[TT] System of the Onboard Propulsion System = Dual-redundant"]
-[6.2429070472717285, 1.9203132390975952, "[FF] URL of the Resurs-P1 = http://www.russianspaceweb.com/resurs_p.html"]
-[8.467021942138672, 4.083062171936035, "[FF] Idle State of the RadFETs = Irradiation mode"]
-[11.161728858947754, 7.479978561401367, "[TT] Swath of the Megha-Tropiques = ~1700 km"]
-[8.48648452758789, 4.575214862823486, "[FF] Components of the ACS = Coarse Sun Sensors (CSS), Fine Sun Sensors (FSS), Magnetometers (MAG), Fiber-optical Gyros (Gyro), Star Sensors (STS)"]
-[9.749415397644043, 8.349637031555176, "[TT] IFOV (spatial resolution) of the ScaRaB = 48 mrad x 48 mrad (60 km x 60 km at nadir)"]
-[3.756024122238159, 4.82936429977417, "[TT] Spatial Resolution of the RADARSAT-1/2 = 250-750 m, 250-650 m, 125-300 m, 750-1000 m, 525-750 m, 250-750 m, 300-720 m, 250-600 m, 400-600 m, 400-750 m, 400-550 m"]
-[4.737443447113037, -1.8222577571868896, "[TT] Close Flyby Date of the Chang'e-2 = December 13, 2012"]
-[7.967402458190918, 6.28643274307251, "[TT] Instrument type of the PAN (FORMOSAT) = Imaging multi-spectral radiometers (vis/IR)"]
-[7.07293701171875, 3.54262113571167, "[FF] Ground Segment of the CO2Image = Earth Observation Centre (EOC)"]
-[5.1693010330200195, 4.938701629638672, "[TT] GPS Unit of the DSX = None"]
-[4.925180912017822, 3.0069212913513184, "[TT] Prime Industrial Contractor of the SEOSAT-Ingenio = Airbus Defence and Space"]
-[5.70373010635376, 2.7004027366638184, "[TT] Developer of the ASAN = Swedish Institute of Space Physics (IRF)"]
-[3.447096109390259, 3.613577127456665, "[TT] Mission of the PAZ = Dual-use (civil/defence)"]
-[4.642389297485352, 1.519344449043274, "[TT] First Update Schedule of the GCOM-C/SGLI = 2020"]
-[5.53730583190918, 7.274216175079346, "[TT] Data Bandwidth of the RTEPs = 6 Mbit/s"]
-[9.910894393920898, 8.901849746704102, "[FF] Effective Area of the Telescope = ~ 15 cm2 for FUV channel, 15-40 cm2 for NUV & VIS channels"]
-[7.477315425872803, 3.8142383098602295, "[FF] Purpose of the GPS receiver = Measure TEC of the ionosphere and density measurements of the troposphere"]
-[12.268607139587402, 0.5806466341018677, "[FF] Purpose of the PLATO = Planet-hunting"]
-[7.860378265380859, 2.0205109119415283, "[FF] Data Coverage of the QuikSCAT = Over 90% of the global ocean"]
-[8.081972122192383, 3.3256053924560547, "[FF] Unknown of the Lightning Imaging Sensor (LIS) = Unknown"]
-[5.970531940460205, 0.7894984483718872, "[FF] Date of the GW170817 and GRB 170817A = 16 October 2017"]
-[7.668778419494629, 3.4099044799804688, "[FF] Purpose of the Debris Sensor = Detecting the micro-debris impact on the surface of HORYU-2"]
-[7.683903217315674, 6.525341510772705, "[TT] Time for Full Disk Scan of the ABI = 26 minutes, 15 or 5 minutes"]
-[3.789461612701416, 7.155589580535889, "[TT] Gain of the TEC Antennas = Not less than 45 dB"]
-[7.721464157104492, 7.462475299835205, "[TT] Frame Rate of the HSC-III = 500 Hz"]
-[13.656158447265625, 3.566918134689331, "[TT] Mass of the TREX-823 X-band transmitter = 3 kg"]
-[3.204420566558838, 2.2814385890960693, "[FF] Program of the Multispectral Instrument = Sentinel-2"]
-[8.037110328674316, 4.962182998657227, "[FF] Calibration Approach of the UVN Instrument = In-flight calibration"]
-[5.558935642242432, 1.0300729274749756, "[FF] Mission Date of the Spaceflight SSO-A = 3 December 2018"]
-[11.203269958496094, 5.316845893859863, "[FF] Sensitivity of the Crystal Scintillator = Main prompt emission energy of GRBs"]
-[5.585455417633057, 5.640108585357666, "[TT] Microprocessor of the RCM3400 = Rabbit 3000 8-bit"]
-[13.964452743530273, 3.142740488052368, "[FF] Mass of the E-TBEx = Unknown"]
-[7.7166337966918945, 0.1613217443227768, "[TT] Availability of the Segments = Via AsteroidDay.org, via SES Satellite, via ESA Web TV, ESA\u2019s YouTube channel"]
-[6.279838562011719, 6.392528057098389, "[TT] Data Retrieval Time of the SafetyNet = Less than 28 minutes"]
-[8.48702335357666, 7.559384822845459, "[TT] Observation Range of the ASPIICS = From 1.04 Rsun"]
-[9.3958101272583, 7.153565406799316, "[TT] Radiometric Resolution of the AATSR = 0.1 K"]
-[10.386219024658203, 5.412363052368164, "[FF] Thermal Subsystem of the TARANIS = Partly passive, relying on the use of paints, MLI and SSM, and partly active using heaters"]
-[8.315834999084473, 7.143315315246582, "[TT] Imagers of the BILSAT-1 = Medium resolution panchromatic and multispectral"]
-[5.261549472808838, 0.2574925124645233, "[TT] Operation End Date of the TRACE = 2009"]
-[6.715117931365967, 0.8771694898605347, "[TT] Launch Date of the Solar Orbiter = February 10, 2020"]
-[5.094703197479248, 5.222672462463379, "[TT] Tracking of the GPS Receiver = L1 C/A tracking and semicodeless L2 P(Y) tracking"]
-[4.973451137542725, 1.2500674724578857, "[FF] Presentation Date of the GSC Missions = June 6-7, 2012"]
-[6.175236225128174, 0.991479754447937, "[TT] Acquisition Date of the Operational Land Imager (OLI) = October 7, 2020"]
-[7.451332092285156, 2.93049955368042, "[TT] Field of View of the MethaneSAT = 21\u00ba"]
-[7.310887336730957, -0.6833539009094238, "[TT] Orbit Repeat Cycle of the ICESat-2 = 91 days"]
-[10.585652351379395, 2.8826658725738525, "[FF] Mission of the SOTA = SOCRATES (Space Optical Communications Research Advanced Technology Satellite) microsatellite mission of NICT"]
-[8.691128730773926, 7.563029766082764, "[TT] Scan Rate of the INSAT-3D Imager = 20\u00b0/s"]
-[14.607338905334473, 6.684963703155518, "[TT] Battery Type of the EPS = 6 Ah NiCd batteries at 28 V"]
-[5.749906539916992, 6.047337532043457, "[TT] Percentage of New Subscribers of the SecureWatch = 70%"]
-[7.182875633239746, 2.1902642250061035, "[TT] Agency of the Biomass = ESA"]
-[5.687076568603516, 8.177383422851562, "[TT] Nr. of spectral or frequency bands of the Microwave System = 22 MW channels"]
-[8.415257453918457, 7.560328483581543, "[TT] Size of the HSC-III = 68 mm x 76 mm x 141 mm"]
-[13.15195369720459, 7.2735395431518555, "[TT] Power Consumption of the SMATTE = 5.3 W"]
-[13.854805946350098, 2.728072166442871, "[TT] Launch Mass of the IRNSS-1C = 1425.4 kg"]
-[11.840544700622559, 0.03439903259277344, "[TT] Number of Transits Observed of the TESS = 27"]
-[5.5234503746032715, 0.24765484035015106, "[TT] End of Life Date of the ISS-RapidScat = 19 Aug 2016"]
-[9.996050834655762, -1.5004709959030151, "[TT] Orbit Inclination of the SporeSat = 51.6\u00b0"]
-[3.841529369354248, 7.898454666137695, "[TT] Modulation Scheme of the X-band Downlink = QPSK"]
-[8.459839820861816, 5.164605617523193, "[TT] Number of Accelerometers of the IMU = 3"]
-[5.813994884490967, 6.0283074378967285, "[TT] Realtime Data Access of the TDP = Yes"]
-[9.491735458374023, 6.381997585296631, "[TT] Viewing Angle of the MTVZA-GY = 53.3\u00ba"]
-[13.934898376464844, 7.113935947418213, "[FF] Voltage of the Spacecraft Bus = Monitored"]
-[6.666210174560547, 4.332676410675049, "[FF] Ground System of the TET-1 = Unknown"]
-[9.94826602935791, -1.475675344467163, "[TT] Orbit Inclination of the ISS = 51\u00b0"]
-[6.226621627807617, 2.938042402267456, "[TT] Imaging Frequency of the Legion constellation = 6 times at \u226450cm, 10 times at \u22641m, 14 times at <\u22641.3m"]
-[4.724401473999023, 7.290555000305176, "[TT] Data Transmission Rate of the RF Communications = 1 kbit/s FSK modulated in S-band"]
-[5.020569801330566, 3.1422972679138184, "[TT] Manufacturer of the CubeSats = Technische Universit\u00e4t Berlin"]
-[5.789355278015137, 3.1920278072357178, "[FF] Number of the Spacewalks Planned = Four"]
-[3.481905698776245, 4.809399127960205, "[TT] Operating Mode of the RISAT-1 = MRS (Medium Resolution ScanSAR)"]
-[6.511238098144531, 5.821507453918457, "[TT] PRN of the GSAT-0210 = 1"]
-[7.78767728805542, 5.543176651000977, "[FF] Components of the VBS = Optical sensors and highly advanced image processing techniques"]
-[8.697301864624023, -0.2174985557794571, "[TT] Lunar Orbit Altitude of the Chang'e-3 = 100 km"]
-[6.675723075866699, 1.7337254285812378, "[FF] URL of the GaN Experiment = http://www.av.it.pt/medidas/space/Flayer/IT%20no%20Espa%C3%A7o%20EN_IT.pdf"]
-[5.207187652587891, 0.8503222465515137, "[FF] Launch Date of the AAUSAT3 = 25. February 2013"]
-[6.974547863006592, 0.010798731818795204, "[TT] Spatial Resolution of the Cheollian 2B satellite = 500 m x 250 m"]
-[4.82459831237793, 7.226398468017578, "[TT] Uplink Rate of the S-band transceiver = 100 kbit/s"]
-[13.497298240661621, 2.897512435913086, "[TT] Mass of the Satellites = <50 kg"]
-[6.871631622314453, -0.5059211850166321, "[TT] Orbit Repeat Cycle of the GOCE = 61 days"]
-[8.145545959472656, -1.0420283079147339, "[FF] Application of the Multibeam Photon-Counting Lidar = Determination of Local Slope on the Greenland Ice Sheet"]
-[3.769456386566162, 7.047677040100098, "[TT] Gain of the Yagi Antenna = 7.5 dBi"]
-[13.87193775177002, 3.877657890319824, "[TT] Telescope Mass of the ATLAS = 20.8 kg"]
-[10.067280769348145, -1.5628834962844849, "[TT] Inclination of the NEMO-AM = 97.64\u00ba"]
-[11.192140579223633, 5.774111747741699, "[TT] Operation of the Space Comb = Under vacuum conditions"]
-[5.561227321624756, 4.843625068664551, "[TT] Form Factor of the Corvus-HD satellites = 16U"]
-[4.135121822357178, 6.338629245758057, "[TT] Antenna Quantity of the ROSA = 1"]
-[6.40754508972168, 1.0197008848190308, "[FF] Ultimate Fate of the BepiColombo = To circle the Sun indefinitely in the vicinity of the planet"]
-[8.057290077209473, 2.5979979038238525, "[TT] Altitude of the MethaneSAT = 526 km"]
-[6.107937812805176, 1.2822895050048828, "[FF] Development Date of the Flight laser transmitter = July 23-27, 2018"]
-[4.386831760406494, 4.010733604431152, "[FF] Data Processing and Distribution Infrastructure of the GeoSat-2 = ENTICE"]
-[10.015413284301758, 1.6990892887115479, "[FF] Theory of Gravity of the General Theory of Relativity = Needs a modification"]
-[9.793929100036621, 8.455659866333008, "[TT] IFOV of the HIRS/4 = 10 km (0.7\u00ba)"]
-[3.140070915222168, 3.886331081390381, "[FF] Conference Location of the NovaSAR-1 = University of Greenwich, London, UK"]
-[6.584919452667236, 7.671699047088623, "[TT] Data Quantization of the Visual Sensor Array = 6 bit"]
-[10.447986602783203, 2.26033091545105, "[FF] Use of the X-ray telescopes = Photographing distant objects of the universe"]
-[11.610967636108398, 6.818154811859131, "[TT] Energy Range of the ART-XC telescope = 4\u201312 kiloelectron volt (keV)"]
-[9.002188682556152, 5.636171817779541, "[TT] Pointing of the AOCS = \u00b1 0.05\u00b0 (3\u03c3)"]
-[6.807255268096924, 3.3172616958618164, "[TT] Space Situational Awareness Increase of the SBSS-1 = Factor of three"]
-[4.156744956970215, 7.320427894592285, "[TT] Operating Bands of the SRAL = C-band and Ku-band"]
-[10.742960929870605, -1.1210521459579468, "[TT] Deployment Orbit Altitude of the SLATS = ~630 km"]
-[10.10704231262207, -1.5404255390167236, "[TT] Inclination of the Satellite = 98.8\u00ba"]
-[7.549341678619385, 3.606832504272461, "[FF] Sensor Types of the Pico Dragon = Gather data of the temperature, voltage and current of the satellite systems"]
-[9.55519962310791, 9.137310028076172, "[FF] Image Capture of the Iris Camera = Barcelona, Spain"]
-[10.836772918701172, 1.4252502918243408, "[TT] Mass of the Zeta Puppis = 60 times more massive than our sun"]
-[8.255054473876953, 5.419147968292236, "[TT] Calibration Equipment of the Monochromator = \u201cYokogawa AQ6376\u201d"]
-[9.259015083312988, 8.145462036132812, "[TT] Instrument Size of the LLNL imaging system = < 9.75 cm x 9.75 cm x 15 cm"]
-[4.411637783050537, 0.29303526878356934, "[TT] Launch Date of the JPSS-2/NOAA-21 = 10-11-2022"]
-[11.224678993225098, 5.344667434692383, "[TT] Scintillation Module Layers of the Natalya-2M = Two layers (4 crystals in each)"]
-[10.755696296691895, -1.1370270252227783, "[TT] Orbit of the SLATS = Circular orbit at an altitude of 393 km"]
-[3.4442591667175293, 6.47581672668457, "[TT] Diameter of the Retroreflector array = 1.27 m"]
-[12.06289291381836, 4.7116780281066895, "[TT] Bays of the Bus Structure = 9"]
-[9.310009002685547, 4.887906551361084, "[TT] Control Method of the SMA = Close-loop controlled using realtime attitude data supplied by the host spacecraft"]
-[4.752198696136475, 0.115742027759552, "[TT] End of Life Date of the SVOM = Planned for 3 Years"]
-[13.363338470458984, 7.742135047912598, "[TT] RF output power (max) of the RF communication subsystem = 1 W"]
-[9.143804550170898, 1.3361519575119019, "[FF] Mission Start Date of the New Horizons = Unknown"]
-[11.191161155700684, 5.5334248542785645, "[FF] Revert Thickness of the Separation Panel = Thicker"]
-[11.972431182861328, 5.022480487823486, "[TT] Size of the PPL1 and PPL2 = 131 x 221 x 262 mm"]
-[11.147698402404785, 0.566243052482605, "[TT] Survey Sample of the ARIEL = About 1000 extrasolar planets"]
-[6.939699649810791, -0.563647449016571, "[FF] Measurement Timing of the SIXS = All orbital phases of the MPO"]
-[8.122265815734863, -0.616157054901123, "[FF] Mission Purpose of the CryoSat = Determine the Fluctuations in Earth's Land and Marine Ice Fields"]
-[3.2325525283813477, 5.718930721282959, "[TT] SAR Antenna Length of the StriX-\u03b1 = 5 m"]
-[9.963702201843262, 8.19353199005127, "[TT] Effective Focal Length of the GT = 187 cm"]
-[7.860034942626953, -2.453730344772339, "[FF] Mission Goal of the GOLD = Study the boundary layer between Earth and space"]
-[7.154219627380371, 6.528624057769775, "[FF] Laser Altimetry Data Processing of the Chang\u2019E-1 = URL: ftp://202.127.24.130/pub/pjs/%D6%D0%B9%FA%BF%C6%D1%A7%D7%A8%BC%AD/AOGS-PS-0134_1.doc"]
-[7.490786075592041, -0.19284918904304504, "[TT] Touchdown Time of the Philae = 17:25 GMT"]
-[14.278975486755371, 3.2055881023406982, "[TT] Mass of the NEXTAR-300L = 100-500 kg"]
-[10.075555801391602, 6.976729393005371, "[TT] Detector Head Assembly Footprint of the Sounder = 10 km x 40 km"]
-[5.123122215270996, 3.3232758045196533, "[TT] Subcontractor of the SBSS = Ball Aerospace & Technologies Corp."]
-[4.638822555541992, 5.9433465003967285, "[FF] Radios of the Avionics bus = 1 Microhard 2420, 1 Stensat beacon"]
-[10.562163352966309, 1.018640398979187, "[TT] Diameter of the HIP 67522 b = About 10 times the diameter of Earth"]
-[13.995965957641602, 3.030829668045044, "[TT] Total Mass of the STRV-1b = 54 kg"]
-[5.704978942871094, 4.238492012023926, "[FF] Partnership of the Astrocast and iWire Group = Development and production of devices equipped with both Sigfox terrestrial connectivity and Astrocast Satellite IoT (SatIoT) services"]
-[8.267967224121094, 2.972571849822998, "[TT] Measurement Domain of the TEMPO = Atmosphere"]
-[11.790470123291016, 3.276895761489868, "[TT] LAM Thrust of the AOCS = 440 N"]
-[7.190087795257568, 1.7032620906829834, "[FF] URL of the SporeSat = http://www.nasa.gov/centers/ames/engineering/projects/sporesat.html#.U0J-C6KegkA"]
-[4.306278228759766, 7.298583507537842, "[TT] Data Downlink Frequency of the RF Communications = X-band (8.350 GHz)"]
-[11.604893684387207, 6.518375396728516, "[TT] Energy Range of the NuSTAR = 2-3 keV, 3-5 keV"]
-[7.255216598510742, 4.674172878265381, "[FF] Mounting of the LPT = Mounted on a two HH Single Bay Pallets (SBP) on top of the HH MPESS"]
-[11.690858840942383, 4.578454971313477, "[TT] Size of the Didymos B = About 530 feet (~160 m) across"]
-[5.412236213684082, 1.381570816040039, "[FF] Challenging Objectives of the SMOS = Synergistic scientific exploitation of SMOS data with other in-orbit and future Earth observation missions"]
-[7.43174409866333, 2.344468593597412, "[TT] Coverage of the APAA = Global"]
-[5.701746940612793, 2.763245105743408, "[TT] Funding Source of the NASA Heliophysics Technology and Instrument Development (H-TIDeS) = NASA"]
-[7.634533405303955, 6.604623317718506, "[TT] LTAN of the Imager = 13:00 \u00b1 0:15 hr"]
-[13.549848556518555, 6.9319305419921875, "[TT] Power of the EPS = 4.3 kW @ EOL (End of Life)"]
-[9.462532997131348, 7.342055797576904, "[TT] Spatial Resolution of the Telescope = 1 km for VIS and SWIR, 4 km for MWIR, 8 km for WV, 4 km for TIR-1 and TIR-2"]
-[11.268195152282715, 5.5654988288879395, "[TT] PCB Material of the CubeLCT = Copper-Invar-Copper"]
-[9.106585502624512, 6.6597900390625, "[TT] Resolution of the Altimeter = Around 100 km"]
-[4.279594421386719, 7.493834972381592, "[TT] X-band Frequency of the MSX = 8475 MHz"]
-[13.209287643432617, 7.265479564666748, "[TT] Power Consumption (Daytime) of the TANSO-CAI-2 = 350 W"]
-[3.0815060138702393, -0.042866483330726624, "[TT] Orbital Slot of the GSAT-0205 = A08"]
-[5.538524627685547, 3.8406951427459717, "[TT] Number of Satellites of the GPM (Global Precipitation Measurement) Mission = 12"]
-[7.065797328948975, 3.285571813583374, "[FF] Advancements of the Pelican = Higher revisit and higher spatial resolution, faster data access and delivery"]
-[5.3713059425354, 4.37175989151001, "[TT] Ground System Component of the MCCs = MCCs"]
-[7.9024977684021, 7.021163463592529, "[TT] Optical System of the SHS = Similar to the Twyman-Green interferometer"]
-[13.354999542236328, 5.48989725112915, "[FF] Conference Presentation of the ADM Aeolus = The ADM Aeolus Solar Array"]
-[5.763458251953125, 1.3463611602783203, "[TT] Launch Year of the ESA\u2019s Space Situational Awareness (SSA) program = 2009"]
-[13.476503372192383, 6.872761249542236, "[TT] End of Life of the EOL=1.48 kW = 1.48 kW"]
-[7.316617488861084, 7.791394233703613, "[TT] Dynamic range of the PHA = Up to 23000"]
-[8.106986045837402, 1.3583625555038452, "[FF] Rainfall Accumulation of the GPM = Particularly intense in the Mexican states of Yucat\u00e1n, Campeche, and Quintana Roo"]
-[7.956919193267822, 8.283848762512207, "[FF] Middle Wavelength Infrared (MWIR) and Thermal Infrared (TIR) band wavelengths of the HSRS = "]
-[9.49553108215332, 4.116861343383789, "[TT] Instrument Type of the MFI = Dual triaxial fluxgate magnetometers"]
-[5.800107955932617, 3.0604407787323, "[TT] Builder of the WorldView Legion Satellite Constellation = SSL"]
-[9.378052711486816, 4.804994583129883, "[TT] Attitude Control System Design Life of the ANUSat = 6 months"]
-[4.075578212738037, 0.24665836989879608, "[TT] Booster's Previous Flight Date of the Falcon 9 = Jan. 20"]
-[5.0442962646484375, 3.9079527854919434, "[TT] Location of the Antenna Assemblies = Nadir panel of the MetOp-SG satellite B"]
-[11.983498573303223, 4.870672225952148, "[TT] Dimensions of the GPS OEM Sensor = 41 mm x 71 mm x 13 mm"]
-[8.079766273498535, 3.3315742015838623, "[FF] Function of the Sprite camera = Maximize the contrast between the TLE and lightning events"]
-[10.917516708374023, 4.760405540466309, "[FF] Tether Connection of the NETCAM = Usually connected with the spacecraft via a tether"]
-[6.143126010894775, 1.743272304534912, "[FF] Documentation Concern of the RISESAT = True"]
-[5.889837265014648, 1.5471714735031128, "[TT] Program Manager of the ASTERIA = Lorraine Fesq"]
-[14.609663009643555, 6.630796432495117, "[TT] Batteries Type of the Power Subsystem = Lithium-ion"]
-[6.080931663513184, 7.0806379318237305, "[TT] Data Compression Rate of the Instrument = < 80%"]
-[6.334371089935303, 1.3568371534347534, "[TT] Launch Date of the COSMO-SkyMed-1 = June 8, 2007"]
-[5.003613471984863, 4.352321147918701, "[TT] Service Cost of the Starlink Premium = $500 per month"]
-[7.935546398162842, 0.07916093617677689, "[FF] Mass Changes of the GRACE = Varies"]
-[8.241859436035156, 2.823272228240967, "[TT] Measurement Domain of the TARANIS = Atmosphere"]
-[7.4340620040893555, 2.3722035884857178, "[FF] Data Collection of the AEISS = Landscape topography, multi-purpose imagery (land), vegetation"]
-[3.9383037090301514, 9.722392082214355, "[TT] Bandwidth (GHz) of the ICI-11 = 10"]
-[4.772914409637451, 7.771230220794678, "[TT] Operating Frequencies of the Back-end electronics = Up to 15 Msample/s"]
-[9.708269119262695, 4.211712837219238, "[TT] Quantity of the Magnetometer = 2"]
-[9.79398250579834, 2.653850793838501, "[FF] Mission Date of the NanoRacks = 13 July 2018"]
-[10.33289623260498, 7.1620635986328125, "[TT] In Field Separation of the MWIR = 18 km"]
-[5.337404727935791, 3.9167792797088623, "[TT] Number of Satellites of the Cluster = 4"]
-[5.360636234283447, 6.581052303314209, "[TT] INR Performance of the GOES-N spacecraft = Improved"]
-[7.807561874389648, 7.152175426483154, "[TT] Data Downlink Rate of the Camera = One frame per second"]
-[7.397010803222656, 6.5825724601745605, "[TT] Accuracy of the Laser Rangefinder = Within 1 m"]
-[9.229969024658203, 0.5307729244232178, "[TT] Distance from Mars of the Tianwen-1 = 2.2 million kilometers (1.4 million miles)"]
-[7.246396541595459, 1.2971374988555908, "[TT] Instrument of the ExoMars Trace Gas Orbiter = Nadir and Occultation for MArs Discovery (NOMAD)"]
-[6.8603434562683105, -0.6229597926139832, "[TT] Time on Orbit of the AlSat-2A = One year"]
-[6.277153968811035, 8.72121810913086, "[TT] Polarization of the StriX-\u03b1 = Single polarized (VV)"]
-[4.429592132568359, 7.8389739990234375, "[TT] F-chip (MHz) of the Service downlink = 0.538"]
-[6.8605451583862305, 7.477545738220215, "[TT] AD Convertor Resolution of the EPH = 10 bit"]
-[4.301168918609619, 4.807656288146973, "[TT] Number of Looks in the Azimuth Direction of the Ship detection optimized and multi-purpose beam modes = 1"]
-[13.513564109802246, 6.544830322265625, "[TT] Orbit Average Power of the Power System = 65 W"]
-[7.786594867706299, 1.9285192489624023, "[FF] Mission Objectives of the GOCE = Obtain a portrait of Earth's most intimate features"]
-[9.568288803100586, 9.184206008911133, "[TT] Observation Time of the IRIS = Eight months per year"]
-[13.356192588806152, 7.829658031463623, "[TT] RF Output Power of the X-band transmitter = Up to 2 W"]
-[8.768475532531738, 4.10166597366333, "[TT] Measurement Type of the Hot Ion Analyzer = Ion Density"]
-[7.990777015686035, 6.348499774932861, "[TT] Instrument Type of the RASAT VIS Panchromatic = Imaging multi-spectral radiometers (vis/IR)"]
-[8.929178237915039, 7.2597832679748535, "[TT] Resolution of the TOF = 120 ps"]
-[4.741086483001709, 7.224960803985596, "[TT] Data Transfer Rate of the X-band transmission system = 12 Mbit/s"]
-[13.331019401550293, 7.292344570159912, "[TT] Qualification Runs of the GaN-based Power Transistors = 15 W and 80 W"]
-[8.43011474609375, 1.3223557472229004, "[FF] Science Goals of the Aquarius = Observe and model the processes that relate salinity variations to climatic changes in the global cycling of water"]
-[5.549605846405029, 7.044979095458984, "[TT] Data Rate of the OSIRISv3 = Up to 1 Gbit/s"]
-[5.053163528442383, 1.308225154876709, "[TT] Naming Ceremony Date of the GIOVE = Nov. 9, 2005"]
-[8.765872955322266, 7.5788960456848145, "[TT] Window Size of the Windowed Mode = 64 x 64 pixels"]
-[6.838461399078369, 3.2584733963012695, "[FF] Data Distribution of the Satellite = NOAA (and NASA) for distribution and use by the civilian community"]
-[8.607070922851562, 1.3793554306030273, "[TT] Measurement of the Aquarius = Sea ice concentration"]
-[6.506082057952881, -0.03651105985045433, "[TT] Monitoring Frequency of the JJ-FAST = Once every 45 days"]
-[4.063512802124023, 6.35653829574585, "[TT] Pointing Direction of the Active Antenna = Nadir"]
-[8.554952621459961, 6.676575660705566, "[TT] Daily Acquisition Capacity of the SPOT-6 = 3 million km2"]
-[9.69782829284668, 8.422186851501465, "[TT] FOV of the Observation Instrument = 0.1\u00ba x 7.3\u00ba + 0.2\u00ba x 0.2\u00ba (7.5\u00ba full length)"]
-[6.7979631423950195, 5.223395824432373, "[FF] Function of the PCM = Power distribution"]
-[7.35532283782959, 6.507536888122559, "[TT] Subintervals Duration of the MWR = 30 ms"]
-[6.979681968688965, 5.359842777252197, "[FF] Device of the GAGE = Patch antenna and GPS sampling device, known as `Bitgrabber'"]
-[8.210753440856934, 5.635840892791748, "[FF] Purpose of the Webb's Fine Guidance Sensor (FGS) = Enable accurate science measurements and imaging with precision pointing"]
-[3.170161724090576, 2.213106393814087, "[FF] Data Source of the Climate Change Initiative = Copernicus Sentinel-1 mission, Envisat\u2019s ASAR instrument, JAXA\u2019s Advanced Land Observing Satellite (ALOS-1 and ALOS-2)"]
-[8.295111656188965, -0.826917290687561, "[FF] Freeboard Definition of the A-68A = The height of the ice above the sea surface"]
-[9.171111106872559, 6.880997657775879, "[TT] Downlink of the Image Location Knowledge = < 300 m"]
-[8.1954345703125, 4.838223457336426, "[TT] Calibration of the PREMOS = SI-traceable irradiance calibration in vacuum"]
-[10.181621551513672, 5.750705718994141, "[TT] Thermally Isolated of the HyperScout\u00ae Telescope = Yes"]
-[5.07087516784668, 2.3628499507904053, "[FF] Hosting Service of the EUTELSAT 5 West B = EGNOS"]
-[5.444633960723877, 6.423567295074463, "[TT] Onboard Storage of the Spacecraft = 14.5 GB"]
-[11.791872024536133, 6.679843902587891, "[TT] Measurement Range of the SWE Strahl sensor = 5 eV to 5 keV"]
-[7.879323482513428, 6.913616180419922, "[TT] Probability Value of the Contamination Probability = Smaller than 10\u20132"]
-[6.853943347930908, 3.7854697704315186, "[FF] Monitoring Capabilities of the GGAK-M = Space environment"]
-[5.130997657775879, 0.7465212941169739, "[FF] Progress Date of the NTSIC = Aug. 26-27, 2007"]
-[8.704933166503906, 3.8095266819000244, "[FF] Detection Type of the EPISEM = Detects penetrating beta/gamma radiation from energetic particles above a certain energy threshold"]
-[9.479747772216797, 4.217723369598389, "[TT] Sensor Type of the ACS = 3-axis magnetic sensor"]
-[7.529289245605469, 6.492588520050049, "[TT] Earth Scanning Time (FDC) of the Instrument = Less than 10 minutes"]
-[6.018896579742432, 1.000076413154602, "[FF] Image Acquisition Date of the DSCOVR = June 3 and June 4"]
-[13.606167793273926, 1.751362681388855, "[TT] Cargo Load for Return of the SpaceX Dragon = ~720 kg"]
-[6.384417533874512, 3.082407236099243, "[FF] Purpose of the ERA = Provide installation and removal of target loads on the surface of the station and monitoring of the state of the external surface of the station, as well as remotely controlled movement of astronauts in a portable workplace during spacewalks"]
-[7.726618766784668, 2.5694708824157715, "[FF] Applications of the VIS band = Daytime cloud imaging, snow and ice cover, severe weather onset detection, low-level cloud drift winds, fog, smoke, volcanic ash, flash flood analysis, hurricane analysis, winter storm analysis"]
-[13.092229843139648, 7.258533000946045, "[TT] Power Consumption of the Sensor Complement = \u2264200 W"]
-[8.373629570007324, 7.295010089874268, "[TT] Quantity of the Teledyne e2v CCD Bruy\u00e8res Image Sensors = 112"]
-[3.61065411567688, 2.677922010421753, "[TT] Number of Planned In-Orbit Spares of the Iridium NEXT = 3"]
-[8.353921890258789, 1.554189682006836, "[TT] Rain Rate Accuracy of the Lower atmosphere = 5 mm/h"]
-[7.8515448570251465, 9.053068161010742, "[TT] Wavelength Range of the PH1 = 160 to 260 nm"]
-[9.563751220703125, 6.698617458343506, "[TT] Azimuth Resolution of the Wide ultra fine = 2.8 m"]
-[10.193511962890625, 0.4780464172363281, "[TT] Cross-Track Separation of the TDX and TSX Satellites = 3600 m over the equator"]
-[10.221407890319824, -1.3468014001846313, "[TT] Orbit Inclination of the CANYVAL-X CubeSats = 97.55\u00ba"]
-[5.610022068023682, 3.36824369430542, "[TT] Operator of the Argos/DCS = NOAA"]
-[7.720279693603516, 5.583812236785889, "[FF] Purpose of the Upper Barrel Assembly = Accurately locate and maintain the position of the optical subsystems throughout the life cycle of the instrument, whilst providing acceptable unit level dynamic environments during launch conditions"]
-[5.719187259674072, 0.9899100065231323, "[TT] Technology and Development Phase Start Date of the GeoXO = July 21, 2021"]
-[5.863138675689697, 3.5992770195007324, "[TT] Development Status of the DSX = Final assembly and integration completed"]
-[11.476351737976074, 4.43450927734375, "[TT] Size of the CaNOP = 3U"]
-[8.976202011108398, 3.5920603275299072, "[FF] Purpose of the Langmuir Probe = Monitor the global parameters of the ionosphere in situ, study the coupling between lithosphere and ionosphere before, during and after earthquakes"]
-[8.096059799194336, 8.556370735168457, "[TT] Spectral Range of the Observation Instrument = 55-210 nm"]
-[9.611637115478516, 7.408675670623779, "[TT] Angular Resolution of the eROSITA = ~ 30 arcseconds"]
-[9.509085655212402, 0.9908972382545471, "[TT] Maximum Velocity of the Dust Accelerator = Up to 60 km/s"]
-[6.33522891998291, -1.3112635612487793, "[FF] Project Execution Location of the GRACE-FO = US"]
-[6.09700870513916, 5.496378421783447, "[TT] AOCS Guidance List of the TTTC = Included in each data take"]
-[5.768849849700928, 1.6176273822784424, "[FF] Complement of the ROSA = Unknown"]
-[7.737316131591797, 2.9544219970703125, "[FF] Mission Type of the CO2M = Monitoring and Tracking Carbon Dioxide Emissions"]
-[7.244725227355957, 0.7244802713394165, "[TT] Project Go-ahead Implementation Time of the SeaSat = 28 months"]
-[4.569704055786133, 3.21519136428833, "[FF] Role of the Thales Alenia Space = On-board Galileo 2nd Generation"]
-[5.6370415687561035, 1.1132904291152954, "[TT] Collaboration Announcement Date of the Astrocast = December 14, 2021"]
-[13.181411743164062, 7.270990371704102, "[TT] Average of the Power Consumption = 2.4 W"]
-[10.776932716369629, 4.400820732116699, "[FF] Desiccant Addition of the Valves = Done"]
-[4.293628215789795, 0.7755104303359985, "[FF] Launch Year of the ADRV = 2016"]
-[4.607737064361572, 2.875433921813965, "[TT] Location of the GSC = NASA/MSFC Huntsville AL"]
-[8.350896835327148, 8.14200210571289, "[TT] Resolution of the IR Systems = 16 channels from 5 to 30 \u00b5m"]
-[5.498289108276367, 6.4538702964782715, "[TT] Storage Capacity of the PDHT = 1410 Gbit"]
-[5.523794651031494, 2.323519468307495, "[FF] Launch of the OSIRISv3 = Unknown"]
-[5.33043098449707, 1.1125317811965942, "[FF] Date of the WCOM = July 13-18, 2014"]
-[5.336138725280762, 3.925173044204712, "[TT] Number of US Satellites of the NPOESS = 2"]
-[5.348585605621338, 6.5103759765625, "[TT] Max. Output data rate of the SDR-SMM = 1200 Mbit/s"]
-[7.906759262084961, 3.516785144805908, "[TT] Sensor complement / remarks of the Meteor-3-1 = MR-2000M, MR-900B, IR, SM, RMK-2"]
-[10.168211936950684, 3.11975359916687, "[TT] P-POD Deployment of the CubeSat - Launch 4 = Successful"]
-[8.803603172302246, 6.433183670043945, "[TT] Beam Direction Pointing Period of the SS-TDMA = 2 ms"]
-[11.770130157470703, 3.3425729274749756, "[TT] Electrical Consumption of the IES (Ion Engine System) = About half of total consumption of SLATS"]
-[6.396121025085449, 5.544616222381592, "[FF] Types of the DCPs = Regional, or international"]
-[11.191800117492676, 1.0251413583755493, "[FF] Structure Mapping of the LISA = First hundred million years of the history of the Universe"]
-[5.726916313171387, 0.8694170713424683, "[FF] Date of the Seroja Slams Australia = 13 April 2021"]
-[18.798200607299805, 3.480041265487671, "[TT] \u0394r (m) of the Karshi Khanabad = 26.4"]
-[8.928861618041992, 7.4506449699401855, "[TT] Image Resolution of the NAVCAM = 1024 x 1024 pixels"]
-[6.955752849578857, 1.240324854850769, "[TT] Location of the Planet Finder Spectrograph = Magellan Telescope in Chile"]
-[11.542021751403809, 3.4050416946411133, "[TT] System of the Onboard Propulsion System = Split into two modular units"]
-[6.095747947692871, -0.20118869841098785, "[TT] Interruption Period of the S-193 = 4-year and 30-day"]
-[4.856546878814697, 8.184562683105469, "[TT] Frequency of the ALScat = 1.26 GHz"]
-[5.996157169342041, 3.5378077030181885, "[FF] Grasp, refuel, and relocate of the Restore-L = Landsat-7"]
-[7.147709369659424, 4.375805854797363, "[FF] Unknown of the SOLSPEC = Unknown"]
-[6.227607250213623, 3.347480535507202, "[TT] Data Delivery of the SENSE = Air Force Research Laboratory at Kirtland Air Force Base"]
-[9.685874938964844, -1.4974312782287598, "[TT] Ascending Node of the SMART-1 = 237.721\u00ba"]
-[8.268163681030273, 9.003918647766113, "[TT] Spectral Range of the Argus = 900-1700 nm"]
-[10.212753295898438, 8.126646995544434, "[TT] Telescope Aperture of the Nanosatellite = 30 mm"]
-[13.795454978942871, 5.354153633117676, "[TT] Type of the Triple-junction GaAs solar cells = Triple-junction GaAs"]
-[4.943279266357422, 3.4396228790283203, "[TT] Power Subsystem Manufacturer of the MicroMAS-1 = Clyde Space"]
-[8.64555835723877, 7.640126705169678, "[TT] Pixel Count of the CCD Bruy\u00e8res = 4510 x 4510"]
-[5.801789283752441, -0.7355149388313293, "[TT] Design Life of the Satellite = 5 years"]
-[4.815821170806885, -0.997886061668396, "[TT] Construction Start Year of the China\u2019s space station = 1992"]
-[9.550833702087402, 3.72160005569458, "[FF] Structure of the GMR = Composed of magnetic and non-magnetic films"]
-[4.762819766998291, 8.090093612670898, "[TT] Center Frequency of the L1-SAIF = 1575.42MHz"]
-[5.161448955535889, 0.554970383644104, "[TT] Power Up Date of the COWVR = Jan. 7, 2022"]
-[5.207329273223877, 6.992643356323242, "[TT] Bit Rate Error of the Downlink = < 10 -6"]
-[7.8702263832092285, -0.14748753607273102, "[FF] Date of the Winter in the Appalachians = 25 February 2022"]
-[9.94911003112793, -0.2484244555234909, "[TT] Orbit Altitude of the Harmony satellites = 693 km"]
-[11.816734313964844, 6.716635704040527, "[TT] Energy Range for Electrons of the Spectrometer = 250 keV to 4 MeV"]
-[5.634513854980469, 6.978060722351074, "[TT] Telemetry of the CEASE-2 = 10 byte/min"]
-[14.658276557922363, 6.664464473724365, "[TT] Capacity of the Battery = 40 Ah NiCd"]
-[3.4275026321411133, 6.242398262023926, "[TT] Antenna Size of the Biomass satellite = 5 m diameter"]
-[10.386026382446289, 2.1455366611480713, "[FF] Imaging of the NuSTAR = High-energy X-rays"]
-[9.467907905578613, 0.5602319240570068, "[TT] Distance from Earth of the CU-E3 = 27 million km"]
-[8.92260456085205, 5.371622562408447, "[TT] Pointing Mode of the TanSat = Forward Nadir Pointing"]
-[6.95743465423584, -0.7988656759262085, "[TT] Orbit Stability of the WD 1856 b = Unstable"]
-[6.592733383178711, 0.9645320773124695, "[TT] Data Availability of the Landsat 7 ETM+ SLC-off and Landsat 5 TM = New global acquisitions July 2008"]
-[6.60551118850708, 7.674201965332031, "[TT] Data Quantization of the WV60 imager = 11-bit"]
-[6.007866382598877, 1.7211378812789917, "[FF] Data Downlink of the MEIDEX = During the mission"]
-[9.133925437927246, 3.11584210395813, "[TT] Number of Instruments of the Extreme Ultraviolet and X-ray Irradiance Sensor (EXIS) = 1"]
-[12.111907005310059, 7.627894401550293, "[TT] Mass of the Imager = ~130 kg"]
-[3.578401565551758, -0.9534350633621216, "[TT] Orbit Type of the Primary Payload = Circular"]
-[5.23382043838501, 2.032060146331787, "[TT] Mission Status of the LAICE = Planned"]
-[7.653608322143555, 6.402568817138672, "[FF] Planned Image Production of the GOCI = 8 times per day"]
-[6.059814453125, -0.5134677886962891, "[TT] Operation Time of the NorAIS-2 Receiver = Four and a half years"]
-[7.484534740447998, -0.9075385928153992, "[FF] Mission Duration of the ICESat-2 = Long-term"]
-[13.280027389526367, 7.225603103637695, "[TT] Power Consumption of the DPU = 130 W"]
-[8.997961044311523, 4.730129718780518, "[TT] SciC Mode Operation of the ADCS = +X of the spacecraft towards the velocity direction with +Y of the spacecraft pointing as close as possible towards nadir direction"]
-[9.293865203857422, 5.263012409210205, "[TT] Sun Angle of the OLCI = 12.2\u00b0"]
-[8.011096954345703, 3.444641590118408, "[FF] Measurement of the CDMS = Continuous, in situ measurement of individual impact events"]
-[7.873973369598389, 2.1455020904541016, "[TT] Type of the Ocean colour instruments = Multiple direction/polarisation radiometers"]
-[3.0826451778411865, -0.056866612285375595, "[TT] Orbital Slot of the GSAT-0102 = B06"]
-[3.5422556400299072, 4.496823310852051, "[TT] Predecessor of the SAR-Lupe system = SARah system"]
-[10.134033203125, 3.0603904724121094, "[FF] Purpose of the Unisat-7 smallsat = Tryout of technology for the precise orbit insertion of small satellites of CubeSat format"]
-[8.99425983428955, 4.413550853729248, "[FF] Science Instruments of the Dellingr = Boom-mounted fluxgate magnetometer, gated time-of-flight ion-neutral mass spectrometer (INMS)"]
-[7.96360969543457, 6.76010799407959, "[TT] Temporal Resolution of the Instrument = 2 \u00b5s"]
-[8.856529235839844, 7.418483257293701, "[TT] Detector Active Area of the RAMIS = 0.5 cm2"]
-[9.087091445922852, 6.946767330169678, "[TT] Horizontal Error 90% (HE90) of the WorldView-3 = 3.8 m"]
-[5.147378921508789, 0.7690839767456055, "[FF] On-Orbit Storage Date of the GOES-14 = Nov. 30, 2009"]
-[10.512638092041016, 3.9982218742370605, "[FF] Deployment Sequence of the Drag Augmentation Device = 1) The microprocessor control board receives twice a command from the Main Unit 2) A lock mechanism for the extension boom turns off with DC motor 3) The lock mechanism for the 350 mm x 3000 mm kapton film turns off with DC motor 4) The boom extends and deploys the 350 mm x 3000 mm kapton film with the DC motor"]
-[9.47305679321289, 7.009236812591553, "[TT] Spatial Resolution of the CIRC = 200 m (ALOS-2), 130 m (CALET)"]
-[9.764241218566895, 4.59856653213501, "[FF] Attitude Control System of the CanX-2 = Three-axis stabilised momentum-bias attitude control system"]
-[11.444167137145996, 3.4616901874542236, "[FF] Low Thrust Propulsion of the RVX = Requires advanced guidance techniques for hops"]
-[2.28749418258667, 2.769369125366211, "[TT] DPI of the EPI-Lo = Eric Christian"]
-[9.346002578735352, 4.9890217781066895, "[FF] Attitude Range of the CHEOPS = Not provided"]
-[7.97526741027832, 6.5436625480651855, "[FF] Imaging Cycles of the ABI = Faster than the current imager"]
-[8.742311477661133, 7.604708671569824, "[TT] Pixel Count of the Imager = 1372 x 1300 pixels"]
-[7.039755821228027, 0.23397229611873627, "[TT] Mean Separation Time from CALIPSO of the CloudSat = 15 seconds"]
-[11.315549850463867, 0.9355169534683228, "[TT] LTP Duration of the LISA Pathfinder = 90 days"]
-[9.295516967773438, 10.731033325195312, "[TT] Polarization of the ICEYE-X1 = Single VV"]
-[7.883100509643555, 3.231626510620117, "[FF] Data Retrieval of the IR-sounder IRFS-2 = Atmospheric and surface parameters"]
-[7.045149803161621, 5.214476585388184, "[FF] Activation Sequence of the Power Distribution Module = Turn on the instrument, IOBC, and CCD thermal control subsystem"]
-[3.7505972385406494, 4.703915119171143, "[TT] Nr. of Looks of the RADARSAT-1/2 = 1x4, 1x4, 1x4, 1x4, 1x1, 4x4, 2x2, 1x4, 1x1, 2x2, 1x1"]
-[4.158392429351807, 5.980578899383545, "[FF] Purpose of the JIB Antennas = Support Ship ID Capability"]
-[5.572745323181152, 1.4394423961639404, "[FF] URL of the Foton-M3 Mission = http://esamultimedia.esa.int/docs/foton/FOTON-M3_brochure.pdf"]
-[7.631423473358154, 9.200764656066895, "[TT] Band 1 Wavelength of the AEISS = 450nm - 900 nm"]
-[7.991208076477051, 6.384795665740967, "[TT] Instrument Type of the TANSO-CAI-2 = Imaging multi-spectral radiometers (vis/IR)"]
-[7.571048259735107, 1.9995020627975464, "[FF] Band 4 of the Landsat TM = Biomass surveys, water body delineation"]
-[13.410253524780273, 5.5056376457214355, "[TT] Number of Panels of the Solar Array = 3"]
-[7.027170181274414, 5.765009880065918, "[FF] Function of the GAMS = Perform time synchronization of all system clocks"]
-[5.608708381652832, 0.04060882329940796, "[FF] Time Series of the ISS LIS = 16 years"]
-[10.315608024597168, 7.85162353515625, "[TT] Telescope Size of the ASTERIA = 2.4-inch (6-centimeter)"]
-[3.707573413848877, 4.816758632659912, "[TT] Imaging Frequency Band of the RADARSAT-1 = C"]
-[5.646767616271973, 7.061474800109863, "[TT] Data Rate of the ODU = 6.5 Mbit/s"]
-[5.966603755950928, 5.957207679748535, "[TT] Data/Pilot of the E5a-I = Data"]
-[6.5158586502075195, 5.856900215148926, "[FF] Detection of the FIELDS = Natural, low-frequency radio signal"]
-[5.618313789367676, 2.8041927814483643, "[FF] Collaboration of the TES = Close collaboration with the IASI scientists"]
-[13.578543663024902, 3.0774989128112793, "[TT] Payload Capability of the PSLV-XL = 1425 kg for the Sub-GTO (Sub Geosynchronous Transfer Orbit) of 284 km x 21,000 km"]
-[3.417235851287842, 6.438789367675781, "[TT] Diameter of the Antenna = 0.1m"]
-[5.370352745056152, 0.2011701762676239, "[TT] Launch Date of the STS-9 = Nov. 28 - Dec. 8, 1983"]
-[5.6694207191467285, 4.423430919647217, "[FF] Connection Type of the Sateliot = 5G IoT"]
-[10.972894668579102, 7.323451042175293, "[TT] Swath Width of the Satellite = 105 km"]
-[5.043610572814941, 7.908029556274414, "[TT] Narrow Band Mode of the Receiver = \u00b1 6.0 kHz (-1 dB)"]
-[6.35393762588501, 8.60466194152832, "[TT] Polarization of the MTVZA-GY = Vertical and Horizontal"]
-[7.549895763397217, 5.368438720703125, "[FF] Components of the SLOSU = OME (Opto-Mechanical Enclosure), thermal radiators, FEE (Front End Electronics), the cooling system, and DA (Detection Assembly)"]
-[5.282889366149902, 1.113411545753479, "[FF] Presentation Date of the NPOESS = Oct. 4-8, 2004"]
-[6.738785743713379, 4.871213436126709, "[FF] Function of the EXPRESS Flowmeters = Measure the flow rates and provide a signal to command corresponding control valves for the EXPRESS racks"]
-[7.443286418914795, 2.9583780765533447, "[FF] Demonstration of the RRM3 = Transfer and long-term storage of liquid methane in microgravity"]
-[8.999178886413574, 7.3308329582214355, "[TT] Registration Between Images of the ABI = 36 \u00b5rad (0.5, 1.0 km), 16 \u00b5rad (0.5, 1.0 km), 21 \u00b5rad (2.0 km)"]
-[4.886045455932617, 0.6381410360336304, "[FF] Launch Date of the Resurs-P1 = May 2015"]
-[6.4912495613098145, 0.06831025332212448, "[TT] Production Frequency of the Nighttime SST Product = Hourly"]
-[5.917562007904053, 5.547150135040283, "[TT] Microcontroller Type of the Subsystems = FPGA-based"]
-[5.241023063659668, 2.0783283710479736, "[TT] Mission Status of the ERS-2 = Mission complete"]
-[7.48139762878418, 1.9751026630401611, "[FF] Band 7 of the Landsat TM = Hydrothermal mapping, geology"]
-[9.568255424499512, 0.2968900501728058, "[TT] Driving Distance of the Yutu-2 = 367.25 meters"]
-[13.230480194091797, 7.267033100128174, "[TT] Power Consumption of the MSU-50 = 6.8 W"]
-[5.829178810119629, 4.932855129241943, "[FF] Services of the SCPS = Spacecraft control and monitor data handling services based on and compatible with commercial Internet protocols"]
-[3.2551653385162354, 5.131539344787598, "[TT] Off-Nadir Look Angle of the RISAT-SAR = 11.5-49.5\u00ba"]
-[10.137508392333984, -1.5343950986862183, "[TT] Orbits of the Capella's Satellites = 45-degree mid-inclination (525 km altitude), 53-degree mid-inclination (575 km altitude), and 97-degree sun-synchronous orbit (525 km altitude)"]
-[4.7872090339660645, 0.6352198123931885, "[TT] Launch Date of the F-1 = 11.9.1976"]
-[8.28275203704834, 0.7811108231544495, "[FF] Acres Burned of the Wildfires = More than 300,000 acres (1,200 km2)"]
-[8.835747718811035, 7.560107707977295, "[TT] Pixels of the Camera = 4510 x 4510"]
-[6.903756618499756, 3.203927993774414, "[FF] Characteristics of the Data Products = High-accuracy, high spatial resolution, fast global coverage"]
-[8.560474395751953, 3.6876420974731445, "[FF] URL of the Total Solar Irradiance Calibration Transfer Experiment (TCTE) = http://lasp.colorado.edu/home/about/quick-facts-tcte/"]
-[11.134855270385742, 6.025688648223877, "[TT] Fittings of the OBA (Optical Bench Assemblies) = Titanium"]
-[6.365862846374512, 4.529966354370117, "[FF] Function of the PPS = Plan user image acquisition requests and generate spacecraft payload sequencing commands"]
-[4.949581623077393, -1.7703644037246704, "[TT] Orbital Period of the Chang'e-2 = Once every 118 minutes"]
-[3.2438106536865234, 5.060665130615234, "[TT] Resolution of the SAR (Synthetic Aperture Radar) Instrument = 3 m"]
-[8.061697006225586, 5.064108848571777, "[FF] Purpose of the SES = Calibrate and control the photon flux"]
-[4.907643795013428, 7.3036088943481445, "[TT] Downlink Data Rate of the RF Communications = 120 bit/s"]
-[5.14823579788208, 7.0018181800842285, "[TT] Command Uplink Speed of the Communication links = 2.0 kbit/s"]
-[8.078267097473145, 6.581869125366211, "[FF] f/5.3 Number (Spectral) of the Camera = Unknown"]
-[10.073841094970703, 1.8952947854995728, "[FF] Imaging of the NuSTAR = Andromeda galaxy"]
-[5.54079008102417, 0.3801615536212921, "[FF] Launch Year of the GeoEye-1 = Unknown"]
-[11.640000343322754, 3.3894288539886475, "[TT] Hall Effect Propulsion of the Electric Propulsion Test Subsystem = Isp = 1600 s \u00b1 160 s"]
-[4.079494953155518, 2.2168126106262207, "[TT] Rocket of the Landsat-9 = United Launch Alliance Atlas 5"]
-[9.214607238769531, 6.223789215087891, "[TT] Type of the Scan Mechanism = Momentum compensation devices"]
-[4.71230936050415, 2.7402820587158203, "[TT] Location of the GPM Core spacecraft ground segment = JAXA"]
-[5.408604145050049, 3.9601800441741943, "[FF] Number of Satellites of the NLS-8 = 3"]
-[7.375830173492432, 2.765596389770508, "[FF] Deformation of the Geosphere = DinSAR and time-series analysis, surface deformations caused by earthquakes, volcanic activities, subsidence, and landslides"]
-[9.708236694335938, 7.2379841804504395, "[TT] Ground Resolutions of the Back-end electronics = Ranging from 0.5 m to say 10 m"]
-[10.136567115783691, -1.538121223449707, "[TT] Inclination of the Satellite = 97.7\u00b0"]
-[8.396103858947754, 2.024021863937378, "[FF] Noctilucent Cloud Observation Frequency of the AIM = Late spring and early summer"]
-[7.973053932189941, 7.286468029022217, "[TT] Image Size of the File Transfer Test = 150 MByte"]
-[9.642061233520508, 8.339221000671387, "[TT] Field of View of the FOV = 4.2\u00ba"]
-[6.956925392150879, -0.6497116684913635, "[TT] Orbital Period of the ALL-STAR-1 = ~ 91 minutes"]
-[8.71291732788086, 1.5433818101882935, "[TT] Constellations of the Planet Labs = SkySat, Dove and RapidEye"]
-[8.408966064453125, 3.2047195434570312, "[FF] Purpose of the SBUV = Determine the total amount of atmospheric ozone in a vertical column above the subsatellite point; the vertical profile of ozone above the ozone maximum; measurements of ultraviolet solar spectral irradiance and its temporal variability over the 160 - 400 nm range (with a spectral resolution of 1 nm)"]
-[10.981711387634277, 0.7002123594284058, "[FF] Habitability of the Planet Candidate = Uninhabitable by life as we know it on Earth"]
-[4.650333404541016, 5.748933792114258, "[FF] Optical Beacons Modulation of the CHOMPTT = 1 Hz"]
-[6.753704071044922, -0.27577444911003113, "[TT] Operation Time of the LEO-to-ground radio link = Twelve minutes"]
-[5.601595878601074, 8.148209571838379, "[TT] Frequency Range of the EZ probe = 0 - 1000 Hz"]
-[5.524745464324951, 7.105482578277588, "[TT] Information Rate of the OPS (Onboard Packet Switch) = 4 - 32 kbit/packet"]
-[7.875730037689209, 2.054810047149658, "[FF] Data Usage of the SeaSat = Improve the forecast of winds, waves, and the location of storms"]
-[5.965961456298828, 0.11841977387666702, "[TT] Hibernation Duration of the Rosetta = 2010-2014"]
-[7.4278435707092285, 6.303948879241943, "[FF] Function of the Laser Altimeter = Times how long it takes light to travel to Earth\u2019s surface and back"]
-[4.202634811401367, 6.33651876449585, "[FF] Design, Position Error Analysis and Adjustment of the Antenna Array = Unknown"]
-[8.965859413146973, 4.402704238891602, "[TT] Quantity of the Coarse Earth sun sensor = 1"]
-[12.803289413452148, 7.613753795623779, "[TT] Power of the Instrument = 52.3 W (max), 14 W (standby)"]
-[4.563211917877197, -2.79598069190979, "[TT] Frequency (GHz) of the PMI = 19.1"]
-[6.238779067993164, 2.3595893383026123, "[FF] Image Credit of the \u00d8rsted satellite = DRSI"]
-[6.590642929077148, 1.2065701484680176, "[FF] Development Year of the STORM = 2006"]
-[4.524426460266113, -0.22116002440452576, "[FF] Function of the MEV-1 = Autonomous docking with a geostationary telecommunication satellite"]
-[3.2375385761260986, 5.033646583557129, "[TT] Swath width (km) of the SAR = 100"]
-[8.260700225830078, 7.661563396453857, "[TT] Detector of the Telescope = FDCCD (Full-depletion CCD)"]
-[13.799478530883789, 2.952671766281128, "[TT] Mass of the SPACE HAUC = 4 kg"]
-[6.180238723754883, 6.764941692352295, "[FF] Key Length of the Quantum-Safe Key Expansion Algorithm = 256 bits"]
-[11.455567359924316, 5.7566728591918945, "[TT] Design of the SEOSat = Aluminium-faced sandwich panel"]
-[13.21120834350586, 7.249484539031982, "[TT] Power Consumption of the ASC = 4.5 W"]
-[12.005326271057129, -0.32479268312454224, "[FF] Management of the TESS = NASA/GSFC (Goddard Space Flight Center)"]
-[3.4886677265167236, 5.221616744995117, "[TT] Type of the Passive Synthetic Aperture Radar = Passive Synthetic Aperture Radar"]
-[10.938268661499023, 3.483264207839966, "[TT] Form Factor of the Lunar Flashlight 6U CubeSat = 116.2 x 239.4 x 366 mm"]
-[6.212811470031738, 4.8094282150268555, "[FF] Interface Type of the MOC = File-based"]
-[5.512559413909912, 3.9912338256835938, "[TT] Hardware Modification of the TBIRD = Modified for the extreme environment of space"]
-[6.051346778869629, 3.2721993923187256, "[FF] Data Policy of the NPOESS = Large subset of data available free of charge"]
-[11.554403305053711, 5.535595417022705, "[TT] Effective Area of the XRD = ~95 cm2 (peak)"]
-[9.074751853942871, 7.713459491729736, "[TT] Validated Value of the MTF = 13%(PAN), 19%(MS)"]
-[6.665321350097656, 7.72257661819458, "[TT] Instrument of the EURECA = SOVA-1, SOVA"]
-[3.845782995223999, 3.4160382747650146, "[TT] Global UTC Time Dissemination of the Galileo = Within 30 billionths of a second"]
-[4.2753424644470215, 2.37157940864563, "[TT] Service Provider of the Atlas-V = ULA"]
-[11.220503807067871, 5.97236442565918, "[TT] Material of the OBA (Optical Bench Assembly) = Aluminum alloy"]
-[5.852376937866211, -0.47959503531455994, "[TT] Expected Deployment Duration of the Spaceflight SSO-A: SmallSat Express = Over a period of six hours"]
-[9.287142753601074, 3.231706380844116, "[FF] Purpose of the OBA = Mount the metrology equipment of both the CSC (Coronagraph Spacecraft) and of the OSC (Occulter Spacecraft)"]
-[3.190683603286743, 2.2317471504211426, "[TT] Precision of the Sentinel-6 Michael Freilich = Millimeter-scale"]
-[8.348684310913086, 1.2245395183563232, "[TT] Range of values of the Precipitation over land areas = 0-25"]
-[6.101418495178223, 3.1068005561828613, "[TT] Contract with NASA of the BlackSky = Five-year, sole source blanket purchase agreement"]
-[10.940168380737305, 5.6250224113464355, "[TT] Thickness of the Heat Shield = 4 cm"]
-[12.062828063964844, -0.14972521364688873, "[TT] Image Size of the TESS = 24-by-24 degrees"]
-[13.277682304382324, 5.654867172241211, "[FF] Location of the Inductor = Negative end of the high-voltage solar array and the end of the TJ arrays"]
-[7.4725117683410645, 8.754884719848633, "[TT] Band 2 of the Instrument = 0.6 - 0.7 \u00b5m"]
-[7.957894802093506, 2.0099825859069824, "[FF] Measurements of the NASA's satellites = Temperature, salinity, chlorophyll concentration"]
-[5.652145862579346, -0.3114180564880371, "[TT] Investigation Duration of the SpaceX Falcon-9 = Over the past four months"]
-[3.4832682609558105, -0.9298403859138489, "[TT] Launch Orbit of the MakerSat = Sun-synchronous polar orbit"]
-[8.172192573547363, 8.966063499450684, "[TT] Wavelength Range (NIR) of the Sentinel-4/UVN = 750-775 nm"]
-[9.537988662719727, 4.128084659576416, "[TT] Channels of the Magnetic Field Measurement System = 8"]
-[6.535392761230469, 6.479129791259766, "[TT] Number of Independent Samples of the PR = 64"]
-[8.73184871673584, 4.758701801300049, "[TT] Star Scanner of the ERG = Spin-type"]
-[3.3864099979400635, 1.4666874408721924, "[TT] Launch Date of the Sentinel-5P = October 2017"]
-[8.629359245300293, 5.809596538543701, "[TT] Elevation Beam Pointing Knowledge Accuracy of the Beam Pointing = Mean error near zero"]
-[8.069427490234375, 7.982463836669922, "[FF] Optical Alignment of the MWIR and TIR cameras = Ground pixel radiance can be co-registered in bands 1 and 2 at the same time"]
-[12.634317398071289, 3.8712973594665527, "[FF] Ion Dispersion of the Magnetospheric Cusps = Higher energy particles (and higher densities) are observed near the equator-ward edge of the cusp while lower energy (and lower densities) are observed at higher latitudes"]
-[6.375014781951904, 0.6826688647270203, "[TT] Number of Profiles of the FormoSat-3/COSMIC-1 = 10 million"]
-[9.862704277038574, -0.6740156412124634, "[TT] Orbit Altitude of the AFSPC-11 = 39,000 km"]
-[9.508861541748047, 7.289167404174805, "[TT] VNIR Imagery of the WNISAT-1 = 500 km x 500 km with a spatial resolution of 500 m"]
-[5.174594402313232, 2.803452491760254, "[TT] Countries of the Spacecraft = United States, Australia, Italy, Netherlands, Finland, South Korea, Spain, Switzerland, UK, Germany, Jordan, Kazakhstan, Thailand, Poland, Canada, Brazil, and India"]
-[6.2845001220703125, 2.1511363983154297, "[FF] Science Goals of the Euclid = Capture a 3D picture of the evolving distribution of both dark and ordinary matter in the cosmos, reconstruct the past few billion years of the Universe's expansion history, estimate the acceleration caused by the mysterious dark energy to percent-level accuracy, and possible variations in the acceleration to 10 percent accuracy"]
-[5.019684791564941, 0.2323904186487198, "[TT] Launch Date of the Genesis-2 = June 28, 2007"]
-[3.1934738159179688, 4.964715480804443, "[TT] Swath of the RISAT-SAR = 25 to 223 km"]
-[10.498403549194336, 4.745201587677002, "[TT] Cycle Life Test of the SMA Hinge Spring = 130 cycles"]
-[7.198799133300781, 5.941351413726807, "[FF] Measurement Capability of the NICER = Intrinsic clock stabilities of MSPs"]
-[5.297758102416992, 3.1250743865966797, "[TT] Provider of the SEM = CAST (Chinese Academy of Space Technology)"]
-[8.398741722106934, 3.5156991481781006, "[FF] Measurement of the IASI = Infrared radiation emitted from Earth\u2019s surface"]
-[8.93762493133545, 9.438288688659668, "[TT] Along-track Coverage of the TANSO-FTS-2 = \u00b140\u00b0"]
-[4.978564262390137, 3.3091890811920166, "[TT] Manufacturer of the Delfi-n3Xt = TU Delft (Delft University of Technology)"]
-[8.536857604980469, 4.588094234466553, "[FF] Function of the ASTERIA = Returns a star image to the same location on the telescope detector"]
-[6.204840183258057, 2.3349175453186035, "[TT] Principal Investigator of the New Horizons = Alan Stern"]
-[7.957836151123047, 6.3147077560424805, "[TT] Mission Status of the Imaging multi-spectral radiometers (vis/IR) = Operational (extended)"]
-[6.32373571395874, 0.746360182762146, "[FF] Survey Date of the Gaia = 23 March 2022"]
-[14.721174240112305, 6.677427291870117, "[TT] Battery Capacity of the XI-IV = 780 mAh"]
-[5.522771835327148, 8.626091957092285, "[FF] Polarization of the Channel = 10.85 \u03bd, h"]
-[5.376743316650391, 0.39134645462036133, "[TT] Launch Date of the LRO = June 18, 2009"]
-[7.546415328979492, -0.03673822060227394, "[TT] Landing Date of the Philae = 12 November 2014"]
-[5.433821678161621, 1.9659892320632935, "[FF] Mission Status of the PIXL-1 mission = In commissioning"]
-[9.769432067871094, 0.4402482211589813, "[TT] Formation Control Accuracy of the PROBA-3 = Less than 1 mm"]
-[7.566335678100586, -2.463810443878174, "[FF] Launch Date of the GOLD = 2017"]
-[10.298699378967285, 2.021757125854492, "[TT] Purpose of the Swift-BAT = Detect gamma-ray bursts"]
-[4.075920104980469, 5.30818510055542, "[TT] Endurance of the GPS Receiver = Against L-band SAR signal"]
-[7.406139373779297, 7.094488143920898, "[TT] Readout Rate of the Windowed Mode = 20 Hz"]
-[4.621519088745117, 4.988199710845947, "[FF] Functions of the MCC = Collect, store and sort the data from LUTs and other MCCs; provide data exchange within the Cospas-Sarsat System; and distribute alert and location data to associated RCC (Rescue Co-ordination Centers) or to SPOCs (SAR Points Of Contacts)"]
-[6.910161972045898, 4.5050787925720215, "[TT] Installation Location of the REM = Externally on the fore panel"]
-[5.44081974029541, 5.570213794708252, "[TT] Type of the SMU Interfaces = EPICA ASIC circuit developed by Thales Alenia Space"]
-[6.599721431732178, 1.9980506896972656, "[TT] Data Archive of the NuSTAR = NASA's High Energy Astrophysics Science Archive Research Center"]
-[5.836190700531006, 3.3915717601776123, "[TT] Investment of the IOD Program = \u01531.5 million"]
-[9.551600456237793, 4.748493194580078, "[TT] Attitude Control of the FY-3 series spacecraft = Three-axis stabilization (bias momentum control)"]
-[11.127503395080566, 3.315678358078003, "[FF] Function of the HPS = Provides propulsion for perigee and apogee raising, spin down, and orbital maneuvers"]
-[10.21782112121582, 4.585492134094238, "[TT] Reaction Wheel Spin of the Integral = 5 times its maximum when under control"]
-[9.215115547180176, 1.3454114198684692, "[TT] Data Resolution Improvement of the New Horizons = Ten times"]
-[7.969051837921143, 8.587102890014648, "[TT] Spectral Range of the TES = 3.2 \u03bcm to 15.4 \u03bcm"]
-[8.579119682312012, 4.571396350860596, "[FF] Function of the ASTERIA = Downloads images of the star so that its brightness can be observed over time"]
-[6.202565670013428, 1.3679651021957397, "[FF] Conference Date of the Metrology System = March 6-13, 2010"]
-[9.107826232910156, 1.3253254890441895, "[FF] Mission Objective of the New Horizons = Explore Pluto and its system of moons"]
-[3.9240477085113525, 9.736534118652344, "[TT] Bandwidth (GHz) of the ICI-3 = 3"]
-[5.553440093994141, 5.69248104095459, "[TT] CPU of the OBDH = TSC695F"]
-[8.573309898376465, 7.809861660003662, "[FF] Size Doubling of the Feed Array = Doubled"]
-[8.148476600646973, 1.42131769657135, "[TT] Application of the IMI = Soil moisture observation, salinity and sea surface temperature"]
-[8.69173526763916, 6.565604209899902, "[TT] Path Length Ratio of the SST Retrieval Algorithm = 1.54"]
-[7.686426162719727, 0.8271692991256714, "[FF] Function of the IIM (Imaging Interferometer Spectrometer) = Obtain the abundances and distributions of various elements/materials on the lunar surface"]
-[7.986744403839111, 0.2599075436592102, "[FF] Data Integration of the GRACE-FO = With other ground-based observations using a numerical model of water and energy processes at the land surface"]
-[7.298435211181641, 1.0992757081985474, "[TT] Mission Session Date of the OceanSat-2 = February 08-19, 2010"]
-[3.2051351070404053, 3.7873358726501465, "[TT] Years in Orbit of the TerraSAR-X = 11 years"]
-[10.104592323303223, -1.5840471982955933, "[TT] Orbit Inclination of the AlSat-2A = 98.23\u00ba"]
-[6.430803298950195, 1.0824718475341797, "[FF] Image of the Day Date of the NASA Earth Observatory = 20 May 2022"]
-[7.601181983947754, 0.7776443362236023, "[FF] Publication Date of the Lunar Flashlight = 15 July 2015"]
-[7.837853908538818, 2.0295825004577637, "[TT] Instrument Type of the SEM (JAXA) = Ocean colour instruments"]
-[4.730232238769531, 8.273329734802246, "[TT] Up-Conversion Frequency of the Ty module = Nominal 5.405 GHz center frequency"]
-[7.108040809631348, 4.427052974700928, "[FF] Navigation Technology of the ATV-5 = Cooperative rendezvous technology"]
-[9.99169635772705, 2.9178647994995117, "[FF] Launch Date of the DST 8 CubeSat = 2010"]
-[6.198133945465088, 2.1032400131225586, "[FF] Operating Condition of the Trisat-R = Without disruption"]
-[9.408448219299316, 6.296863079071045, "[TT] Scanning Method of the OCTS sensor = Mechanical rotating with a mirror"]
-[10.393776893615723, 7.937233924865723, "[TT] Dimensions of the X-ray Telescope = 10 cm x 20 cm x 30 cm"]
-[8.660493850708008, 1.9716967344284058, "[FF] Jet of Boiling Water Height of the Old Faithful geyser = High in the air"]
-[4.050638675689697, 0.3276308476924896, "[TT] Launch Date of the Corvus-BC 4 = December 3, 2018"]
-[5.1463775634765625, 3.381077527999878, "[TT] Manufacturer of the MSU-E = ISDE (Institute of Space Device Engineering, Moscow)"]
-[6.143975257873535, 4.556098461151123, "[FF] Function of the CBERS Ground Segment = Control the satellites and achieve the objectives of its remote sensing missions"]
-[10.154303550720215, 4.603666305541992, "[TT] Torque of the CMGs = Up to 6.1 Nm"]
-[13.865134239196777, 2.929931640625, "[TT] Mass of the TeleSat LEO Phase 1 = 168 kg"]
-[7.953531265258789, 7.703080654144287, "[TT] Spectral Bands of the Hyperspectral Imager = 150"]
-[11.732911109924316, 7.526880741119385, "[TT] Instruments of the Megha-Tropiques = ROSA, ScaRaB, SAPHIR, MADRAS"]
-[9.116083145141602, 5.699280738830566, "[TT] Pointing Knowledge of the RemoveSat = ~2.5\u00ba"]
-[13.547008514404297, 5.917530059814453, "[TT] Energy Supply of the Payload = Solar generator"]
-[9.617146492004395, 7.082614898681641, "[TT] Vertical Resolution of the MLS = 3 km"]
-[10.939169883728027, 7.547861576080322, "[TT] Combined Swath Width of the ResourceSat-2 = 740 km"]
-[6.989885330200195, 5.626827716827393, "[TT] Number of Mounting Sites of the CEPF = 2"]
-[9.008828163146973, 7.533762454986572, "[TT] Multispectral Band Resolution of the Imager = <4 m GSD"]
-[4.678241729736328, 8.035646438598633, "[TT] Frequency TX of the USAT (Ultra Small Aperture Terminal) = 28.05 GHz\u00b1550 MHz"]
-[6.259039878845215, 2.278897285461426, "[FF] MMOD Damage of the Orion EFT-1 = More than the computation models had predicted"]
-[8.110386848449707, 6.467538833618164, "[TT] Scan Period of the SSM/T-2 = 8 seconds per scan"]
-[5.231947898864746, 0.89760822057724, "[FF] Presentation Date of the MinXSS = June 3-5, 2013"]
-[8.706416130065918, 2.2404017448425293, "[TT] Density of the Giant Molecular Clouds = Up to a thousand atoms per cubic centimeter"]
-[7.89053201675415, 8.50228214263916, "[TT] Spectral Range of the HSC = 450-900 nm"]
-[7.292229652404785, 4.42586612701416, "[FF] Operator of the GESS (Galileo Experimental Sensor Stations) = Not specified"]
-[5.780961990356445, 2.843975305557251, "[FF] Funding Source of the Mission Operations Control Centre = Strategic Science Investment Fund"]
-[7.931725978851318, -0.5754004716873169, "[FF] Affiliation of the Scientists = UK Committee for Antarctic Place-Names"]
-[5.730383396148682, 3.6190109252929688, "[FF] Purpose of the ArgoMoon = Demonstrate the ability to perform operations in close proximity of the ICPS"]
-[14.365437507629395, 3.220740556716919, "[TT] Mass of the MKA-PN2 (Relek) = 59 kg"]
-[10.693899154663086, 0.8511680960655212, "[TT] Size of the Kepler 11145123 = More than twice the size of the Sun"]
-[7.1216511726379395, -0.5371488928794861, "[TT] Rotation Period of the MTVZA-GY = 2.5 s"]
-[8.021353721618652, 0.6256412863731384, "[FF] URL of the MASCOT Lander = http://arc.aiaa.org/doi/pdf/10.2514/6.2016-2386"]
-[7.526026725769043, 7.673470973968506, "[TT] Dynamic Range of the NewMag = \u00b165536 nT"]
-[8.846487045288086, 7.696015357971191, "[TT] Pixel Size of the CIRC = 25 \u00b5m square"]
-[6.8948073387146, 4.428292274475098, "[FF] Unknown of the Integ = Unknown"]
-[7.046479225158691, -0.7674770951271057, "[TT] Orbital Period of the GJ 367 b = Approximately eight hours"]
-[4.393562316894531, 0.3310066759586334, "[TT] Launch Date of the MERLIN = Early 2023"]
-[10.168707847595215, 0.9949227571487427, "[TT] Distance from Earth of the GSN 069 = About 250 million light years"]
-[10.418462753295898, 1.7811018228530884, "[FF] Activation Method of the Black Hole = Wait for a star to pass close to it and become disrupted"]
-[8.034101486206055, -0.4317273497581482, "[FF] Data Source of the SMMR of Nimbus-7 = Arctic sea ice growth in 2018"]
-[9.583800315856934, 6.327960968017578, "[TT] Cross-Track Detection Range of the Spectrometer = -30\u00ba to 10\u00ba"]
-[4.33621883392334, 2.985546588897705, "[TT] Location of the LPVEx = Helsinki Testbed and the Gulf of Finland"]
-[9.678730964660645, 7.248313903808594, "[TT] Nadir Resolution (VIS range) of the OLS = 0.55 km"]
-[9.270439147949219, 8.093505859375, "[TT] Plate Scale of the Focal Plane Module = 12.300/pixel"]
-[6.718935012817383, 6.920740604400635, "[TT] Regional Beams of the Eutelsat-9B = 4"]
-[6.721002101898193, -0.6223605275154114, "[TT] Orbit Period of the Corvus-BC = 94 - 97 minutes"]
-[4.832744121551514, 1.7862008810043335, "[TT] Mission Type of the Gokturk-2 = Dual use - civil and defense"]
-[5.161379337310791, 7.870401859283447, "[TT] Frequency Stability of the Receiver = \u00b11 x10 -9 dB"]
-[4.027159690856934, 4.181676387786865, "[FF] Application of the RISAT-2 = Resource conservation & sustainable development planning"]
-[5.1602678298950195, 0.6246981620788574, "[TT] Mission End Date of the GFO = October 22, 2008"]
-[3.453000783920288, 4.9637131690979, "[TT] Radar Measurements Grid Resolution of the L2SMAP = 9 km EASE-2"]
-[7.521750450134277, 8.367476463317871, "[TT] Band of the Trasser = Visible"]
-[6.274542808532715, 8.183548927307129, "[TT] No of bands/channels of the SBUS = 12"]
-[12.41296672821045, 0.6245969533920288, "[TT] Optical Bench Quantity of the PLATO Spacecraft = 1"]
-[8.745980262756348, 8.860865592956543, "[TT] Average Incidence Angle of the Convex Holographic Grating = Approximately 38.2 \u00ba"]
-[14.127425193786621, 3.1677730083465576, "[TT] Weight of the RPU = 16 kg"]
-[10.7705078125, 2.11565899848938, "[TT] Observation Date of the XMM Newton telescope = June 29, 2021"]
-[7.03579044342041, 8.259105682373047, "[TT] SNR of the ALOS/PRISM = >70"]
-[8.108736991882324, 4.498305320739746, "[FF] Performance of the 3D Imaging Electromagnetic Calorimeter = Not specified"]
-[6.427456378936768, 4.646554946899414, "[FF] Function of the ISSAC SOC = Coordinate with NASA for ISS and WORF rack operations"]
-[7.479281425476074, 3.7755863666534424, "[TT] Configuration of the VISS = Hexapod (Stuart platform)"]
-[10.231732368469238, 4.5240702629089355, "[TT] Actuation of the ADCS = 6 reaction wheels and 3 torque rods"]
-[5.98763370513916, 1.4063019752502441, "[FF] Publication Year of the Satellite = 1997"]
-[13.824311256408691, 2.997256278991699, "[TT] Total Payload Mass of the Spektr-RG = 1160 kg"]
-[5.822399616241455, 7.099318504333496, "[TT] Data Rate of the ILAS = 517 kbit/s"]
-[5.445522785186768, 0.5611967444419861, "[TT] Launch Date of the IMAGE = March 25, 2000"]
-[10.143084526062012, 6.953413009643555, "[TT] Frame Size of the Sounder = 640 km x 640 km"]
-[5.293631076812744, 6.437305450439453, "[FF] Accessible unit (erase) of the SDR-SMM = N/A"]
-[8.123690605163574, 5.973222732543945, "[FF] Components of the IRM = Semi-toroidal electrostatic deflection system, a pair of fast-switching time-of-flight electrodes, a hemispherical electrostatic analyzer, a microchannel plate (MCP) detector, and a 64 pixel anode"]
-[7.715203762054443, 8.479477882385254, "[FF] Filter Band Pass Targets of the EXI = Blue: 437\u00b15 nm CW, \u226420 nm FWHM; Green: 546\u00b15 nm CW, \u226420 nm FWHM; Red: 635\u00b15 nm CW, \u226420 nm FWHM; UV1: 260\u00b15 nm CW, \u226430 nm FWHM; UV2: 320\u00b15 nm CW, \u226430 nm FWHM"]
-[4.9468255043029785, 0.6613795757293701, "[TT] Launch Date of the Satellogic = 2016"]
-[9.224944114685059, 5.964784622192383, "[TT] Boresight Deviation of the PamCam = -0.27\u00b0 to -0.25\u00b0 in horizontal and 0.40\u00b0 to 0.48\u00b0 in vertical direction"]
-[8.386101722717285, 1.9319547414779663, "[FF] Climatology Comparison of the ASCAT = RapidScat"]
-[9.135457038879395, 5.289191246032715, "[TT] IRU of the AOCS = Inertial Reference Unit"]
-[9.68881893157959, 4.170543670654297, "[TT] Quantity of the Magnetometer = 1"]
-[8.104426383972168, 9.270604133605957, "[TT] Wavelength of the Responsivity Measurement = 1850 nm"]
-[10.098346710205078, -1.4873193502426147, "[TT] Coplanar Orbit of the Landsat 9 = Landsat-8, 180\u00ba apart"]
-[11.837484359741211, 5.515504360198975, "[TT] Instrument size of the DST 35 = 400 x 400 x 250 mm folded 400 x 400 x 1000 mm unfolded"]
-[5.445182800292969, 2.2347090244293213, "[TT] Instrument of the Odin = OSIRIS"]
-[9.645828247070312, 1.637039065361023, "[TT] Survey of the Herschel = Hi-GAL, the Herschel infrared Galactic Plane Survey"]
-[5.958468437194824, 5.6422247886657715, "[FF] Processor of the CORTEX 160 = Virtex 4FX FPGA with an embedded PowerPC processor running Linux"]
-[7.601329326629639, 8.682671546936035, "[TT] Number of Spectral Bands of the ALI = 10"]
-[7.430009365081787, 3.8554282188415527, "[FF] Purpose of the DSX = Gather data on the radiation environment in medium Earth orbit"]
-[8.154555320739746, 7.04735803604126, "[TT] Image Capture of the Imager = Five images in quick sequence"]
-[6.4563703536987305, 4.8165388107299805, "[FF] Quality Information of the L1C Products = Included"]
-[6.773782730102539, 5.564492225646973, "[TT] Switches of the P-POD = 2"]
-[5.732336044311523, 6.911547660827637, "[TT] Size of the DPU forward data buffer = Five megabytes"]
-[7.24264669418335, 1.6875535249710083, "[FF] Experiment of the SporeSat = Investigate the effect of gravity on the reproductive spores of the fern, Ceratopteris richardii"]
-[7.986939907073975, -2.579835891723633, "[TT] Brightness Reduction of the GOLD = >80% around totality"]
-[7.027939319610596, 7.122951030731201, "[TT] Pulse Energy of the Laser = 2 mJ"]
-[11.457706451416016, 5.156473159790039, "[TT] Surface Area of the CSS = 2 cm2"]
-[6.96030330657959, 0.3283752202987671, "[TT] Absorption Time of the Gaia-Enceladus = 8-10 billion years ago"]
-[6.02929162979126, -0.35573911666870117, "[TT] Operation Duration of the m-NLP system = 10 years"]
-[9.726765632629395, 7.171794891357422, "[TT] Ground Resolution of the Instrument = 5 m"]
-[14.661211013793945, 6.6707634925842285, "[TT] Capacity of the Two 6-cell NiCd battery packs = 6 Ah"]
-[11.307073593139648, 5.851892948150635, "[TT] Support Panel Material of the SAS Subassemblies = CFRP (Carbon Fiber Reinforced Polymer)"]
-[8.012563705444336, 1.2173609733581543, "[FF] Indicator of Climate Variations of the Water Mass Variations = Driven by natural and/or anthropogenic causes"]
-[6.970951557159424, 6.552122116088867, "[FF] Intended Use of the Laser Oscillators = DWL, GIFTS and ALADIN"]
-[10.726903915405273, 1.5877857208251953, "[TT] Magnetic Field Strength of the Swift J1818.0-1607 = Up to 1,000 times stronger than a typical neutron star"]
-[5.5691962242126465, 5.627213001251221, "[TT] Processor of the OBC = H8"]
-[13.368980407714844, 7.074512004852295, "[TT] Power of the Payload Power Capability = 17.8 W"]
-[5.091346263885498, 6.7434492111206055, "[TT] TT&C Downlink of the Spacecraft bus = 30 kbit/s"]
-[4.343263149261475, 6.28589391708374, "[FF] Function of the APAA = First hopping spot beam antenna"]
-[6.458375930786133, 5.964900493621826, "[FF] Operation Cases of the Optical Terminal = Establishment of optical links between the payload and an OGS, PAT operations for a moving user platform"]
-[6.991687774658203, 4.613648891448975, "[FF] Mission Objective of the FASTRAC = Demonstrate autonomous thruster operation using single-antenna on-orbit real-time GPS attitude determination"]
-[5.621407508850098, 6.268058776855469, "[FF] Data Storage of the LIRIS = Hard disks in ATV's cargo hold"]
-[2.911386728286743, 4.496635913848877, "[TT] Geometry of the PALSAR-2 = 5.34 RMSE"]
-[14.236489295959473, 3.1878244876861572, "[TT] Mass of the DPU = 9 kg"]
-[4.4487504959106445, 4.546433448791504, "[TT] Instrument of the CYGNSS observatory = DDMI (Digital Doppler Mapping Instrument)"]
-[7.1302032470703125, 3.8824431896209717, "[FF] Development Status of the TriG GNSS = Unknown"]
-[8.076053619384766, 0.8518720865249634, "[TT] Drought Level of the United States = At least a moderate level"]
-[7.464296340942383, 6.908990859985352, "[TT] Operating Cadence of the TIRS = 70 per second"]
-[6.060240268707275, 5.66805362701416, "[TT] Configuration of the FPGAs = Columnized FPGAs"]
-[8.228602409362793, 8.829154968261719, "[TT] Spectral Range of the HeII Coronagraph = 295-315 \u00c5"]
-[7.873325347900391, 7.535365581512451, "[FF] Symposium Date of the Small Satellite Hyperspectral Mission = Sept. 20-24, 2004"]
-[7.163259983062744, 6.425022125244141, "[FF] Instrument Speed of the MMS = Incredibly fast"]
-[3.838454246520996, 6.3565897941589355, "[TT] Antenna Version of the BlackJack = 4-antenna"]
-[4.892086029052734, 0.9704675078392029, "[FF] Launch Date of the PROBA-V = Unknown"]
-[6.292299270629883, 0.7300938367843628, "[FF] Survey Date of the Gaia = 13 May 2022"]
-[7.739124774932861, 9.165842056274414, "[TT] Wavelength Range of the HgCdTe = 10.4 - 12.5 \u00b5m"]
-[8.962608337402344, 5.0536370277404785, "[TT] Manufacturer of the Gyros = Analog Devices"]
-[9.675545692443848, 1.421105980873108, "[FF] Size of the Pelican Constellation = Not revealed"]
-[6.931529521942139, 2.1068849563598633, "[FF] Platforms of the Satshot = Mapcenter, Landscout and iCue"]
-[14.079333305358887, 7.202903747558594, "[TT] Power of the Voltage 1 = 28 @ 28 V worst-case"]
-[5.970142841339111, 7.851948261260986, "[TT] Transmit Power Amplification Channels of the T/R Module = 2"]
-[6.514261245727539, 3.3890135288238525, "[FF] Compatibility of the Earth Observation Payload Instruments = Space Plug and Play Compatible"]
-[9.86972713470459, 4.481561660766602, "[FF] Control Method of the ADCS = Three momentum wheels for control and three axis magnetic torque rods or coils for desaturation of wheels"]
-[13.898563385009766, 2.8809571266174316, "[TT] Dry Mass of the HY-1C = 429 kg"]
-[3.5598678588867188, 4.717746257781982, "[FF] Image Generation of the RISAT-1 = Hybrid Polarimetric SAR image generation"]
-[14.084057807922363, 7.166796684265137, "[TT] Bus Voltage of the EPS = 70 V"]
-[5.463377475738525, 0.6642302870750427, "[FF] Release Date of the Dusty deities = 6 August 2018"]
-[14.169733047485352, 3.0972259044647217, "[TT] Mass of the ALT = 93.8 kg"]
-[5.798672199249268, 6.852790355682373, "[TT] Data Size of the Processed Science Data Packet = 36 bytes"]
-[5.995772838592529, -0.26935938000679016, "[TT] Operation Duration of the SDS = At least two years"]
-[8.350386619567871, 2.300431251525879, "[FF] Unknown of the WindSat = Unknown"]
-[10.285761833190918, 4.04473876953125, "[FF] Mounting of the SWEA = STEREO boom"]
-[10.360381126403809, 2.363313674926758, "[FF] Purpose of the pnCCD Detectors = Accurate spectroscopy of X-rays as well as imaging with high time resolution"]
-[8.082992553710938, 3.2240378856658936, "[FF] Function of the Coherency Filter = Remove events not caused by lightning, including radiation hits and glint from Sun on the ocean"]
-[5.229468822479248, 0.3025068938732147, "[TT] Operation End Date of the BILSAT = August 2006"]
-[18.66451644897461, 3.935912609100342, "[TT] NE\u0394T (K) of the ICI-4 = 0.6"]
-[5.164413928985596, 0.3746874928474426, "[TT] Year Founded of the Saltworks = 1954"]
-[3.7545244693756104, -1.051676869392395, "[TT] Orbit Type of the STRV-1c and -1d = Elliptical GTO (Geosynchronous Transfer Orbit)"]
-[9.416759490966797, 6.77174186706543, "[TT] Spatial Resolution of the KazEOSat-2 = 6.5 m"]
-[6.691617965698242, 6.765223503112793, "[TT] Sample Time of the Channel = 1.8 ms"]
-[13.659262657165527, 5.809079170227051, "[TT] Peak Power of the Solar Panels = 10 W"]
-[8.06419849395752, 4.8987016677856445, "[TT] Imager Calibration Frequency of the TRUTHS = Daily"]
-[10.0109281539917, -1.5152692794799805, "[TT] Second Deployment Batch Inclination of the STP-2 = 24\u00ba"]
-[6.05230712890625, -0.32210037112236023, "[TT] Operation Duration of the LIMS = About 9 months"]
-[6.7535552978515625, 8.403732299804688, "[TT] Total Channels of the Spectral Bands = 1305"]
-[7.76570987701416, 1.9787731170654297, "[FF] Additional Goal of the PACE = Help determine the roles of the ocean and atmosphere in global bio-geochemical cycling"]
-[6.366838455200195, 4.286552906036377, "[FF] Qualification Program of the SGDR (Safe Guard Data Recorder) = Radiation tests, assembly qualification, construction analysis, electrical characterization, reliability tests like burn-in, destructive physical analysis, stress and life tests"]
-[5.0735344886779785, 8.646016120910645, "[FF] Center Frequency of the Channel = 23\u03bd"]
-[9.5407075881958, 8.748861312866211, "[TT] Inclination of the Iris Video Camera = 51.6\u00ba"]
-[13.342436790466309, 3.0912394523620605, "[FF] Projected Payload Capacity of the Terran R = In the same class as SpaceX\u2019s Falcon 9"]
-[10.20185375213623, 4.5079264640808105, "[TT] Type of the Reaction Wheels and Magnetic Torque Rods = Three-axis stabilized (nadir pointing)"]
-[6.089761734008789, 5.503774166107178, "[FF] Redundant Chain of the TMCU = QPSK-B / ATOP-B"]
-[8.177355766296387, 8.534178733825684, "[TT] Wavelength of the EUV Imager = 30.4 nm"]
-[5.146015167236328, 6.074640274047852, "[FF] Frequency of the SpaceWire Link = Set according to the need plus a significant margin"]
-[5.042335033416748, 8.243168830871582, "[TT] Bandwidth Range of the AMSR = 100 - 3000 MHz"]
-[7.896912574768066, 8.081351280212402, "[FF] Instrument of the CO2M = Near-infrared and shortwave-infrared spectrometer"]
-[8.156492233276367, -2.2935826778411865, "[TT] Orbit Altitude of the GOLD = 35,786 kilometers"]
-[5.444462776184082, 8.735512733459473, "[TT] Spectral Bandwidth of the COCTS = 734 to 754 nm"]
-[6.404397487640381, -0.6333615779876709, "[TT] LTDN of the PRISMA = 1030 hours"]
-[4.978819370269775, 5.476006984710693, "[TT] Operating Mode of the GPS Monarch receiver (GPSDR) = Dual-frequency"]
-[7.044630527496338, 4.064637660980225, "[FF] Risk Reduction Flight of the ANDE = Unknown"]
-[5.033797740936279, 4.3842973709106445, "[TT] Number of Ground Station of the PRISMA = 2"]
-[7.14857816696167, 3.2030177116394043, "[FF] Imagery of the GOES-18 = First Imagery"]
-[9.384530067443848, 5.775404453277588, "[TT] Path Offset/Revolution of the Satellite = 26.334\u00ba"]
-[13.637803077697754, 3.851076602935791, "[TT] Material of the Reflector Film = 1/4 mil aluminized mylar"]
-[10.172450065612793, 7.05703592300415, "[TT] Ground Velocity of the MWR = 6.82 km/s"]
-[10.31755542755127, 7.266136169433594, "[FF] Mirror Layout of the Telescope System = Primary mirror is a concave parabola, secondary mirror is a hyperbola"]
-[13.361618041992188, 7.186212539672852, "[TT] Power of the Electric Power Subsystem = 220 W"]
-[9.02169132232666, -0.2242075651884079, "[TT] Altitude of the Meteor-M2-3 = 816.3 km"]
-[6.486647605895996, -0.47472071647644043, "[TT] Period of the WV-1 = 94.6 minutes"]
-[12.147708892822266, -0.12538544833660126, "[TT] Camera of the TESS = 4"]
-[7.123163223266602, 0.046973612159490585, "[TT] Age of the DS Tuc Ab = 40 million years"]
-[9.198341369628906, 8.08008861541748, "[TT] Maximum Processing Rate of the Focal Plane Module = 400 events/s"]
-[8.340188980102539, 2.1612796783447266, "[FF] Sensor Description and Mission Overview of the WindSat = The WindSat Space Borne Polarimetric Microwave Radiometer: Sensor Description and Mission Overview"]
-[8.66845989227295, 4.488438606262207, "[FF] Attitude Sensing of the AOCS = Star tracker assembly (3 star tracker heads), 3 magnetometers, and a CESS (Coarse Earth and Sun Sensor) assembly"]
-[10.207209587097168, 7.6655473709106445, "[TT] Type of the Telescope = Zeiss 1 m \u2205 Ritchey-Chr\u00e9tien/Coud\u00e9 telescope"]
-[5.999383926391602, 4.275535583496094, "[FF] Objective of the CIL = Allow access to both optical and SAR satellite capabilities"]
-[2.5560221672058105, 0.16276134550571442, "[TT] Pulse period (ms) of the GROJ1744-28 = 467.000"]
-[8.210040092468262, 5.123813629150391, "[TT] In-flight Calibration of the SOSP = Provided"]
-[10.343130111694336, 3.2461304664611816, "[FF] Data Downlink Volume of the EPICHyper Constellation = 20-100 times the downlink volume as a traditional cubesat"]
-[5.73285436630249, 0.6595893502235413, "[FF] Accident Date of the Columbia = Feb.1, 2003"]
-[8.498680114746094, 7.4899115562438965, "[TT] Number of Pixels of the Quadrant Photodetector = 4"]
-[5.515876293182373, 6.05501127243042, "[TT] Data Backup of the ASAP-Light = Non-volatile flash memory"]
-[6.8470940589904785, -0.6424256563186646, "[TT] Orbit Period of the MethaneSAT = 100 minutes"]
-[8.354694366455078, 6.4785356521606445, "[TT] Hourly Measurements of the TEMPO instrument = 2.5 x 10^6 spectra/hour"]
-[5.14755392074585, 6.964638710021973, "[TT] Data Rate of the Payload Downlink = 20 Mbit/s"]
-[7.910621166229248, 6.664391040802002, "[FF] Support Spiders of the Optic = Unknown"]
-[4.494941711425781, 0.46444475650787354, "[FF] Mission Flexibility Demonstration of the Soyuz = April 26, 2016"]
-[3.750123977661133, -1.0814337730407715, "[TT] Orbit Type of the MKS-PN2 (Relek) = Elliptical"]
-[7.206070899963379, 6.909757614135742, "[FF] Design of the APD = Compact, lightweight, mechanically hard, low power consumption, high quantum efficiency"]
-[13.1804838180542, 7.456842422485352, "[TT] Power of the SDR = ~3 W TX, ~2.8 W RX, ~7.8 W Duplex"]
-[5.07554817199707, 3.2995526790618896, "[FF] Manufacturer of the SSUSI = JHU/APL"]
-[5.0977630615234375, 1.9006645679473877, "[TT] Status of the IKFS-2 = Fully functional"]
-[5.275343418121338, 0.8090997338294983, "[TT] Launch Date of the EFT-1 = December 2014"]
-[8.951857566833496, 3.4127466678619385, "[FF] Apogee Activity of the S/C = Coronagraphy, Formation Flying maneuver tests"]
-[4.868997097015381, -1.5630855560302734, "[TT] Orbiter Observation Duration of the Tianwen-1 = One Martian year"]
-[3.9808011054992676, 3.501845121383667, "[FF] URL of the Galileo = http://www.springer.com/%20cda/%20content/%20document/%20cda_downloaddocument/%209789400718296-c2.pdf?SGWID=0-0-45-1477020-p175271702"]
-[5.855493545532227, -0.7620298862457275, "[TT] Design Life of the Spacecraft = 3 years for prime plus 2 for extended mission"]
-[5.026596546173096, 0.28780120611190796, "[TT] Launch Year of the CYGNSS = 2016"]
-[8.247140884399414, -0.5443984270095825, "[FF] Previous Sea Ice Coverage Record of the Global Change Observation Mission 1st \u2013 Water \u201cSHIZUKU\u201d = 19.44 million km2"]
-[4.6319499015808105, 8.01312255859375, "[TT] Operating Frequency of the AltiKa = 35.75 GHz"]
-[14.089719772338867, 4.060603618621826, "[TT] Mass of the Instrument = 15 kg"]
-[6.453345775604248, 0.5070493221282959, "[TT] Data Release Frequency of the COSMIC-2 = Daily"]
-[5.321320056915283, 5.587481498718262, "[TT] Standard Interface of the CEASE-1 = RS-422 or MIL-STD-1553B"]
-[4.651706218719482, 7.123907566070557, "[TT] BER of the Miniaturized X-band transponders = < 1 x 10-5 for downlink"]
-[5.429957866668701, 6.856164932250977, "[TT] Downlink Data Volume of the IXPE = ~600 MB/day"]
-[11.216409683227539, 0.9945142269134521, "[TT] Compensates for of the LISA Pathfinder = Other forces acting upon it"]
-[10.014734268188477, -1.5281498432159424, "[TT] Orbit Inclination of the Aalto-1 = 97.44\u00ba"]
-[5.650511264801025, 3.2086100578308105, "[TT] Contract Value of the GeoOptics = $1 million"]
-[4.751293659210205, 7.947867393493652, "[TT] Carrier frequency (MHz) of the L1-B = 1575.420"]
-[10.26541805267334, 4.551676273345947, "[TT] Reaction Wheel of the ADCS = 30 mNms"]
-[14.62593936920166, 6.7568230628967285, "[TT] Battery Cells of the EPS = 4"]
-[5.331119060516357, 0.5328313708305359, "[FF] Reentry Date of the OCSE = March 5, 2001"]
-[10.147665977478027, 6.551614284515381, "[TT] Footprint Sampling of the MABEL = ~2 m every ~4 cm along track"]
-[8.457703590393066, 4.247086048126221, "[FF] Type of the IR Horizon Sensors = Unknown"]
-[8.008061408996582, 4.568423271179199, "[FF] Waypoints Location of the RVX = Around the orbit"]
-[7.503477096557617, 4.995273113250732, "[FF] Mode of Operation of the EPI-Lo = Single parameter measurement"]
-[5.681887626647949, 0.7643086314201355, "[TT] Publication Date of the TOI-178 = 25 January, 2021"]
-[4.811192989349365, 7.870620250701904, "[TT] Wide Band Receiver Tunable Frequencies of the IOF = 2000, 500, 125, and 31.1 kHz"]
-[10.671026229858398, 3.868502140045166, "[FF] Components of the InflateSail = Mix of COTS and custom components"]
-[11.358351707458496, 3.3117165565490723, "[FF] Mission of the Colloid Micro-Newton Thrusters = Space Technology 7"]
-[6.178885459899902, 1.824004888534546, "[FF] URL of the SpaceX CRS-24 = https://www.issnationallab.org/iss360/spacex-crs-24-mission-overview/"]
-[8.233850479125977, 0.5276867151260376, "[TT] Water Level Change of the Lake Mead = Dropped 5.53 feet (1.69 meters) between March and June"]
-[6.245509147644043, 6.40932559967041, "[TT] Data Collection Duration of the LPR = 2 days"]
-[5.260329246520996, 1.480450987815857, "[FF] Project Mutation of the CHIPSat = CHIPS project mutated to CHIPSat"]
-[13.633974075317383, 5.435715198516846, "[TT] Provider of the Flexible thin-layer solar cells = Solarion GmbH"]
-[8.325641632080078, 3.7142386436462402, "[FF] Measurement of the Planck = Direction of the polarized light emitted by the dust"]
-[5.544595241546631, 6.4079813957214355, "[TT] Image Data Storage Capacity of the CSM = 7 Gbit"]
-[10.36320686340332, 7.967391014099121, "[TT] Secondary Diameter of the Telescope = 34 mm"]
-[8.209117889404297, 4.003633975982666, "[FF] Sample Division of the ASME = The sample is divided into two identical units: one having been given a special surface treatment and another one without surface treatment"]
-[5.730302333831787, 0.7891709208488464, "[FF] Discovery Date of the Red Sprites = Unknown"]
-[7.873212814331055, 5.938077449798584, "[TT] Device Type of the SEM-2 = Monitor"]
-[8.164857864379883, 3.3760340213775635, "[FF] Measurement of the Conducted EMC Test = Conducted emissions"]
-[10.529287338256836, 2.294969081878662, "[FF] Data Telemetry of the X-ray and Microdosimeter = All survey data and roughly 1/3 of X-ray imaging data"]
-[4.458070755004883, 2.8840043544769287, "[TT] Location of the GMIZ = Mizusawa Japan"]
-[8.102781295776367, 0.6798090934753418, "[TT] Groundwater Storage Measurement Date of the GRACE-FO = March 15, 2021"]
-[6.182586193084717, 5.26680326461792, "[FF] Planning Cycle of the LMS = Constantly tries to schedule any request in its request database"]
-[12.081528663635254, -0.29127374291419983, "[FF] Lifetime of the TESS spacecraft = Several decades above GEO (>6.6 RE)"]
-[9.293769836425781, 4.8388214111328125, "[TT] Role of the QNA-PCI = Principal investigator for the attitude control experiment"]
-[6.38161039352417, 4.2194061279296875, "[FF] Ground Segment Components of the SARah system = All necessary components for the ground segment"]
-[6.924284934997559, 0.7307835817337036, "[FF] Potential Mission End Date of the InSight = Within a year from June 22, 2021"]
-[8.01041316986084, -0.6409949064254761, "[FF] Function of the ESA Radar = Provide a new look at sea ice"]
-[9.512214660644531, 8.444879531860352, "[TT] Type of the FUV Instrument = Off-axis Czerny-Turner"]
-[10.371774673461914, 2.286827564239502, "[FF] Ability of the X-rays = Pierce the hot plasma sheath"]
-[4.854135990142822, 0.1480255126953125, "[TT] Launch Date of the Crew-3 = Oct. 31"]
-[8.845484733581543, 0.47557875514030457, "[TT] Rock Deposits Size of the LRO = Less than 500 m across"]
-[4.769405364990234, -1.8034816980361938, "[TT] Orbit Maneuvers of the Chang'e-2 = More than 10"]
-[10.185098648071289, 5.775998592376709, "[TT] Power Dissipation of the Focal Plane = Less than 1 watt"]
-[7.577702045440674, 8.693556785583496, "[TT] GSD of the Spectral Band C = 5"]
-[10.637849807739258, 5.452023506164551, "[TT] Probe Development Location of the Electron Temperature Part = IKI (Institute of Space Research) Moscow, Russia"]
-[4.560925006866455, -2.8009517192840576, "[TT] Frequency (GHz) of the PMI = 90"]
-[8.604251861572266, 3.7109181880950928, "[FF] Purpose of the TSIS-1 TIM and SIM instruments = Provide total and spectral solar irradiance measurements"]
-[13.188830375671387, 7.277412414550781, "[TT] Power Consumption of the UPM-1T card = 3 W on average"]
-[4.5684003829956055, 0.1883341670036316, "[TT] Planned Launch Year of the SMILE = 2022"]
-[7.0537872314453125, 6.518857479095459, "[TT] Full Frame Scan Frequency of the Sounder = Every 3 hours"]
-[14.593745231628418, 6.628812789916992, "[TT] Battery Type of the EPS = Lithium Ion Polymer"]
-[11.447866439819336, 3.3274178504943848, "[TT] Propulsion System of the SkySat-3 = HPGP (High Performance Green Propulsion) system"]
-[11.589661598205566, 3.3300631046295166, "[TT] Total \u0394V of the CNAPS = 12 m/s"]
-[13.566476821899414, 5.402978897094727, "[TT] Number of Cell Types of the SCTE = 47"]
-[9.418181419372559, 9.150848388671875, "[TT] Spectral Regions of the IRIS = FUV (Far Ultraviolet) and NUV (Near Ultraviolet)"]
-[9.42054557800293, 2.5336499214172363, "[FF] Light Sensitivity of the DNB = Up to 10 million times fainter than daylight"]
-[6.145307540893555, 1.7365319728851318, "[FF] URL of the AISsat-1 = http://nordicspace.net/wp-content/uploads/2013/07/NSA240.pdf"]
-[6.666738510131836, 5.014642238616943, "[FF] Function of the EPC Layer = Control task"]
-[6.947318077087402, 1.4756884574890137, "[FF] Launch Date of the Webb Telescope = 25 December 2021"]
-[8.784473419189453, 5.647037029266357, "[TT] 3\u03c3 Low Result of the Close Approach Distance = 1.45 km"]
-[8.925317764282227, 5.331636905670166, "[TT] Radio Link Testing Distance of the GomX-4A and GomX-4B = Up to 750 km"]
-[5.854397773742676, 2.479570150375366, "[FF] Mission of the BeeSat = Berlin Experimental Educational Satellite"]
-[13.777786254882812, 3.086272716522217, "[TT] Payload Mass of the S/C = 266 kg"]
-[4.071153163909912, 0.3518003523349762, "[TT] Launch Date of the Corvus-HD suborbital test flight = August 2, 2017"]
-[9.69348430633545, 4.295279502868652, "[FF] ADCS System of the DeorbitSail = First demonstration of the CubeAIM system"]
-[8.335161209106445, 5.797329902648926, "[FF] Drag-Free Performance Metric of the Drag-Free Technology = Residual acceleration of the test mass in units of m/(s2Hz1/2)"]
-[7.903465270996094, 7.397261142730713, "[TT] Data Rate of the TDI Detector = 700 Mbit/s per detector"]
-[12.434477806091309, 0.5750541090965271, "[TT] Data Production of the Plato\u2019s payload = 103 Gb/day"]
-[5.371488094329834, 5.088678359985352, "[TT] Average Euclidean Difference of the NovAtel GNSS receiver = 7 km"]
-[6.277935981750488, 2.956049919128418, "[TT] Ground Sample Distance of the Legion Constellation = 0.3\u20131.3 meter"]
-[14.07829761505127, 7.048383712768555, "[TT] Number of Charge-to-Voltage Conversion Settings of the CTIA = 4"]
-[7.711071014404297, 9.401296615600586, "[TT] Center Wavelength of the Band 1 = 0.47 \u00b5m"]
-[9.857169151306152, 2.916572093963623, "[FF] Conference Location of the PnP Cube Satellite = Big Sky, Montana, USA"]
-[4.543898582458496, 3.179837465286255, "[TT] Location of the MOC = Redu"]
-[8.37581729888916, 6.548888683319092, "[TT] Instrument Type of the TEMPO = Spectrometer"]
-[11.824206352233887, -0.06226814538240433, "[FF] Event of the TESS = Watched a black hole tear apart a star"]
-[5.465015411376953, 6.409725666046143, "[TT] Onboard Data Storage of the Spacecraft = 128 GB"]
-[7.992402076721191, 2.1466495990753174, "[FF] Purpose of the MTVZA-GY = Monitor ocean and land surfaces, global atmospheric parameters, and obtain sea surface wind profiles"]
-[6.995630264282227, 3.8115899562835693, "[FF] URL of the Anti-Coincidence Counter = http://accms04.physik.rwth-aachen.de/~schael/AMS_Talks_files/07-Schael-Veto-klein.pdf"]
-[7.819203853607178, 9.197427749633789, "[TT] Wavelength of the Center wavelength = 427.8 nm"]
-[4.494604587554932, 1.5541516542434692, "[TT] Launch Date of the TUBSAT = 17 July 1991"]
-[10.261857032775879, 5.31540060043335, "[FF] Function of the Heat Pipes = Transport waste heat to the radiator"]
-[11.688721656799316, 4.569314002990723, "[TT] Length of the Genesis-2 = 4.4 m"]
-[13.31400203704834, 7.262847900390625, "[TT] Testing Duration of the GaN-based Power Transistors = More than 3000 hours"]
-[3.3015246391296387, 4.714450359344482, "[FF] Area of Observation of the SAR = Nantucket Shoals"]
-[5.309990882873535, 3.872209072113037, "[FF] Interconnection of the Heinrich Hertz = Direct single-hop"]
-[6.6638336181640625, 0.8369463086128235, "[TT] Observation Date of the Herschel Space Observatory = September 24, 2018"]
-[8.094482421875, 6.3322062492370605, "[FF] Unknown of the PMS Camera = Unknown"]
-[8.098159790039062, 8.790241241455078, "[TT] Wavelength Range (Visible) of the SOLSPEC = 350 to 900 nm"]
-[10.387337684631348, 1.7557580471038818, "[TT] Brightness of the M82 X-2 = 10 times less than NGC 5907 ULX"]
-[9.496240615844727, 7.426754951477051, "[TT] Ground Pixel Size of the WAOSS-B = 185 m"]
-[7.8346638679504395, -0.442892462015152, "[TT] Boil Off of the Cryogens = Occurs over time"]
-[8.324543952941895, 7.52198600769043, "[TT] Output Circuit of the CCID-80 = Single-stage MOSFET"]
-[14.163248062133789, 3.2499473094940186, "[TT] Mass of the M3S = 2800 kg"]
-[10.225396156311035, 8.321246147155762, "[TT] Telescope Pupil Size of the MSI instrument = 150 mm"]
-[11.76165771484375, 3.292903184890747, "[TT] Specific Impulse of the Chemical Propulsion Thrusters = 291 seconds"]
-[8.082725524902344, 8.302892684936523, "[TT] Type of the SAPPHIRE = Stanford AudioPhonic Photographic IR Experiment"]
-[7.877801418304443, 6.677792549133301, "[TT] Radial Blade Design of the SPIDER sensor = 37 arrays"]
-[4.6281208992004395, 0.09396276623010635, "[FF] Development Date of the STARS = 2007"]
-[6.997463703155518, 6.9640913009643555, "[TT] Laser Operation Time of the CATS = Over 24 continuous hours"]
-[9.106590270996094, 7.436446666717529, "[TT] Resolution of the Z-panel camera = 3 Mpixel"]
-[4.773525714874268, 5.889766216278076, "[TT] Beacon Signal of the HORYU-2 = Currently transmitting"]
-[6.713061809539795, 5.04559326171875, "[FF] Function of the DPU = Process data from SEISS"]
-[7.132931709289551, 5.411194801330566, "[FF] Function of the CCB = Command & control of the complete instrument, image data processing"]
-[11.972686767578125, 4.894686698913574, "[TT] Usable Volume of the Galaxy = 16.7 m3"]
-[11.361336708068848, 2.776698112487793, "[TT] Mass of the Minisatellite = ~ 200 kg"]
-[10.290115356445312, 5.873176097869873, "[TT] Operating Temperature of the VNIR, MWIR1, MWIR2, TIR1, TIR2 = 220 K"]
-[10.470643997192383, 2.3745298385620117, "[TT] Area of the X-ray Satellite Navigation = 2000 cm2"]
-[5.349620342254639, 0.21218860149383545, "[TT] Operation Termination of the PRARE = 1995"]
-[7.8054280281066895, 0.8276947140693665, "[FF] Discoveries of the MAP-PACE = Low energy ion distribution in the dayside of the Moon, low energy ion intrusion into the lunar wake region, mapping of the lunar magnetic anomalies"]
-[5.013672351837158, 7.579140663146973, "[TT] G/T of the UHF Antenna = over -36.6 dBk"]
-[9.590171813964844, -1.173108696937561, "[TT] Look Angle of the ICEYE-X1 = 11\u00ba"]
-[7.250055313110352, 5.0728044509887695, "[FF] Measurement Modes of the DPU = Acquisition Mode, Closed Loop mode, Open Loop mode"]
-[4.539103031158447, 0.39760205149650574, "[TT] Target Design Life of the M3MSat = Two years"]
-[13.335114479064941, 7.595932483673096, "[TT] Power Consumption of the Myriad RF board = > 4 W"]
-[7.375180244445801, 3.7055773735046387, "[FF] Operation of the NightPod = Designed to be operated with one hand"]
-[8.426942825317383, 8.98604679107666, "[TT] Grating Figure of the Short Wavelength Band = Ellipse of rotation"]
-[8.30215835571289, 7.457897663116455, "[TT] Detector Type of the IIR = Microbolometer"]
-[14.481884002685547, 6.658320426940918, "[TT] Type of the NiCd = NiCd"]
-[5.721004009246826, -0.7719528079032898, "[TT] Design Life of the DubaiSat-1 = 5 years"]
-[13.320711135864258, 5.526716709136963, "[TT] Length of the ISS Roll-Out Solar Array (iROSA) = 60-foot-long"]
-[9.136808395385742, 6.968053817749023, "[TT] Resolution of the STD = 1.5% at 10 GeV"]
-[6.7824249267578125, -0.07153546065092087, "[TT] Re-adjustment Time of the Earth = Several thousand years"]
-[4.03112268447876, 6.510015964508057, "[TT] Location of the X-band patch antenna = +Y face of the satellite"]
-[14.488838195800781, 6.595726013183594, "[TT] Battery Capacity of the Spacecraft = 60 Ah"]
-[5.9644317626953125, 3.469825506210327, "[FF] Cost of the Dellingr = Fraction of the cost of more traditional satellite missions"]
-[3.5054519176483154, -0.8964319825172424, "[TT] Type of the Satellite = Sun-synchronous dawn/dusk"]
-[5.878630638122559, 5.936927795410156, "[FF] Data Retention Mode Function of the Memory Modules = Store user data and refresh and scrub for error detection and correction"]
-[7.436245918273926, 6.228085994720459, "[FF] Measurement Data Noise of the EGG = Slightly higher-than-expected"]
-[10.837662696838379, 7.552144527435303, "[TT] Swath Width of the DMC-3 = 23 km"]
-[9.284591674804688, -0.5830324292182922, "[TT] Orbit of the OUTSat = Elliptical orbit of 770 km x 480 km"]
-[5.910820007324219, 0.06219152361154556, "[TT] Duration of Deep-Space Hibernation of the Rosetta = 31 months"]
-[7.85214900970459, 3.967298746109009, "[FF] Instrument Types of the Instruments = Multiple direction/polarisation radiometers, Imaging multi-spectral radiometers (vis/IR), High resolution optical imagers, Earth radiation budget radiometers, Atmospheric chemistry"]
-[10.013432502746582, 2.9259729385375977, "[FF] Launch Date of the CubeSat ELaNa III = October 2011"]
-[8.848280906677246, 0.2542000710964203, "[TT] Gas and Ash Column Height of the Anak Krakatoa Volcano = Around 200 m"]
-[5.8328633308410645, 2.262932062149048, "[TT] Affiliation of the eROSITA = NASA/MSFC, Huntsville, AL, USA"]
-[6.281362056732178, 8.643592834472656, "[TT] Polarization Mode of the Stripmap = HH or HV or VH or VV"]
-[9.787487030029297, 7.435787677764893, "[TT] Ground Sample Distance (GSD) of the PAN = 1 m"]
-[8.280243873596191, 5.656695365905762, "[FF] Calibration Method of the TIR Subsystem = Light from the ground enters the TIR subsystem through the \u201cEarth window\u201d and is reflected into the imaging optics by a calibration mirror"]
-[8.106779098510742, 2.640242576599121, "[TT] Measurement Domain of the CryoSat = Ocean, Land, Gravity and Magnetic Fields, Snow & Ice"]
-[11.30109977722168, 0.7372735142707825, "[TT] Type of the AU Microscopii = M dwarf"]
-[6.623233318328857, 4.444058895111084, "[FF] Unknown of the SET Payload = Unknown"]
-[10.297170639038086, 1.8288805484771729, "[FF] Purpose of the NuSTAR = Investigating the mysteries of black holes, supernovae, and other high-energy objects in space"]
-[5.291287899017334, 6.993947505950928, "[FF] Speed of the 1244 Mbit/s High-Speed Network = 1244 Mbit/s"]
-[8.603504180908203, 5.015357971191406, "[TT] Exposure time of the Star Tracker = 100 ms"]
-[5.0509161949157715, 3.2247378826141357, "[FF] Partnership of the EDRS = ESA and Airbus"]
-[5.193609714508057, 1.0733686685562134, "[FF] Launch Date of the OPS-SAT = Unknown"]
-[3.425715208053589, 4.864516258239746, "[FF] Recording Technology of the SAR (Synthetic Aperture Radar) Instrument = Solid-state"]
-[7.592477798461914, 6.4719719886779785, "[TT] Measurement Accuracy - Time of the Instrument = Tag at frame rate"]
-[8.289929389953613, 7.10515022277832, "[TT] Instrument Type of the OrbView-4 = High resolution optical imagers, Hyperspectral imagers"]
-[3.571751117706299, 4.708152770996094, "[FF] Mode Addition of the RADARSAT-2 = Spotlight mode, Five wider coverage stripmap modes, Two higher resolution ScanSAR modes for maritime surveillance, Extra wide swath 5 m resolution mode (Extra Fine)"]
-[6.449260234832764, -0.858704149723053, "[TT] LTAN of the G\u00f6kt\u00fcrk-2 = 10.30 hours"]
-[7.392704486846924, 2.880246877670288, "[TT] Monitoring Coverage of the MethaneSAT = More than 80 percent of global oil and gas production"]
-[9.77767276763916, -0.6156692504882812, "[TT] Flight Path of the Gravity Probe A = Ballistic (sub-orbital)"]
-[5.674704551696777, 11.350446701049805, "[FF] Approx. Peak Sensitivity Altitude of the Channel 4 = Unknown"]
-[6.038403511047363, 7.787240028381348, "[TT] Number of Auxiliary Signals for ECCM of the Complete Solution = 4"]
-[11.956469535827637, 3.5765438079833984, "[TT] Value of the Atmospheric Pressure = 1051.6 hPa"]
-[12.752544403076172, 1.9672901630401611, "[TT] Activation and Calibration Time of the SAGE-III = Approximately 90 days"]
-[14.296979904174805, 2.9698736667633057, "[TT] Mass of the AprizeSat-10 = 12 kg"]
-[5.520813465118408, 3.8837969303131104, "[TT] Payload Number of the Inmarsat S EAN = Ninth"]
-[5.926777362823486, 3.0580272674560547, "[TT] Test Phase of the D-Sat = LEOP (Launch and Early Operations Phase)"]
-[13.14928913116455, 6.206081867218018, "[FF] Efficiency of the iROSA = Degraded over time"]
-[4.426062107086182, 7.77064847946167, "[TT] Frequency of the Communication Payload = Ka-band (27.0-31.0 GHz and 18.1-21.2 GHz)"]
-[5.808822154998779, 6.046003818511963, "[TT] Number of Devices of the FMM (Flash Memory Module) = 76"]
-[6.501161098480225, 4.714900016784668, "[FF] Function of the EM = Supervising the overall systems and networks of the core GS"]
-[10.499096870422363, 4.512009620666504, "[TT] Camera of the DSAT-2 = Internally mounted"]
-[8.70639705657959, 7.05184268951416, "[TT] Image Quality of the CartoSat-2B = High"]
-[10.786873817443848, -0.2125128209590912, "[FF] Science Phase of the TanDEM-X = Three consecutive periods of different formation geometries"]
-[14.301107406616211, 6.473608493804932, "[TT] Continuous Peak Demand Operations in Eclipse of the Daughter Battery Module = ~20 Whr"]
-[4.793491840362549, 1.6872646808624268, "[FF] Development Status of the GCOM-C1 = Unknown"]
-[11.038594245910645, 0.6039986610412598, "[FF] Rotation Rate Measurement of the Exoplanet = Two to three times per orbital period for about seven orbital periods"]
-[4.579137325286865, 7.077644348144531, "[TT] Data Downlink of the SAST-5000 = X-band"]
-[5.020420551300049, 2.6909308433532715, "[TT] Location of Construction of the ATLAS = NASA's Goddard Space Flight Center in Greenbelt, Maryland"]
-[8.039493560791016, 2.4754836559295654, "[TT] Measurement Detailed of the VHRR = Precipitation intensity at the surface (liquid or solid), Cloud type, Land surface imagery, Upward long-wave irradiance at TOA, Earth surface albedo, Land surface temperature, Sea surface temperature, Wind profile (horizontal)"]
-[7.08770751953125, -0.24829953908920288, "[TT] Orbits of the Deimos-2 = Approximately 5,300 times during this year"]
-[11.744040489196777, 3.2915587425231934, "[TT] Quantity of the Main Thrusters = 4"]
-[8.804234504699707, 4.945490837097168, "[TT] Number of Sensors and Systems of the SSA = 375"]
-[8.272156715393066, 7.644050598144531, "[TT] Detectors of the Visible Spectral Band = Si photodiode"]
-[7.287765026092529, 3.9129316806793213, "[TT] Collision Avoidance of the PROBA-3 = Realistic demonstration"]
-[6.5486650466918945, 3.475574493408203, "[FF] Purpose of the Universal Waste Management System (UWMS) Installation and Spare Hardware = Critical installation and spare items to support operations of the next generation toilet system during the 2021 timeframe"]
-[6.757439136505127, 4.559533596038818, "[FF] Data of the RADMON = Research Data"]
-[8.301785469055176, 0.7636570334434509, "[FF] Burned Area of the SCU Lightning Complex = More than 137,000 acres"]
-[3.6548798084259033, 2.804274559020996, "[FF] Atomic Clocks of the Indian Regional Navigation Satellite System (IRNSS) = Replacement"]
-[10.368003845214844, 2.7821381092071533, "[FF] Space Launch Date of the PISAT nanosatellite = July 2016"]
-[7.832952499389648, -0.8885360360145569, "[TT] Measurement Period of the ICESat-2 = October 2018 to April 2019"]
-[6.258899688720703, 3.8833425045013428, "[FF] Responsibilities of the ALMASpace = Managing the project, formal interfaces to ESA/ESTEC, payload selection, qualification and integration onboard the spacecraft, mission implementation management"]
-[13.352493286132812, 5.442277908325195, "[TT] Solar Panels of the MicroMAS-2 CubeSat = Deployable"]
-[8.174504280090332, 1.2001971006393433, "[TT] Soil Moisture Maps Frequency of the SMAP = Every three days"]
-[7.765075206756592, 1.5268642902374268, "[FF] Public Data Release Date of the Global Precipitation Measurement (GPM) Mission = Unknown"]
-[3.3013157844543457, 2.2661726474761963, "[FF] Level-1 GRD Products of the Sentinel-1 = Focused data projected to ground range, detected and multi-looked"]
-[9.370565414428711, 2.5382442474365234, "[FF] Speed of the Solar Wind = Up to 800 km/s"]
-[5.902199745178223, 4.917081832885742, "[FF] Bus Modes of Operation of the C2B = Unknown"]
-[6.853009223937988, -0.651522696018219, "[TT] Operation Periods of the VWFC = Orbits 84 to 91, 94 to 96, and 98"]
-[5.904094696044922, -0.6583248376846313, "[TT] Duration of the SOC = Five years renewable"]
-[4.790471076965332, 0.23854205012321472, "[TT] Return Date of the Metcomp experiment = SpaceX CRS-21"]
-[10.58036994934082, 3.350142240524292, "[FF] Form Factor of the 6U CubeSat = 6U"]
-[6.70318078994751, 1.0701042413711548, "[FF] Arrival Date of the Mercury Magnetospheric Orbiter = May 27, 2015"]
-[13.41119384765625, 2.907844066619873, "[TT] Class of the Satellite = 100 kg"]
-[10.333404541015625, 4.106082439422607, "[TT] Debut Mission of the Grid Fins = SpX-5"]
-[5.707980155944824, 2.113351345062256, "[FF] Mission Status of the Satellite = Unspecified"]
-[8.154192924499512, -0.14158466458320618, "[TT] Period (min) of the Meteor-3-1 = 110.3"]
-[11.658645629882812, 6.667604446411133, "[TT] Low Energy Telescope Energy of the CRS = 5MeV"]
-[4.5201568603515625, 0.5447797179222107, "[TT] Release Date of the HTV-6 = January 27"]
-[7.113999366760254, 2.7829766273498535, "[FF] Launch Schedule of the MethaneSAT = 2021"]
-[5.478950023651123, 7.072139739990234, "[TT] Data Rate of the Instrument data downlink = ~55 Mbit/s (ABI only)"]
-[13.63370132446289, 7.01983118057251, "[TT] Power of the EPS = 65 W (max)"]
-[10.382902145385742, 6.525415420532227, "[FF] Retroreflector Coating of the Ralph = Reflects only one of the two transmitted laser wavelengths"]
-[7.04048490524292, 3.1003265380859375, "[FF] Data Usage of the Iridium Constellation Satellites = Characterize the large scale FACs in both hemispheres on time scales of several hours or less"]
-[6.079927444458008, 3.83038067817688, "[TT] Booster of the DMSP Block 5B and Block 5C satellites = Thor/Burner IIA"]
-[9.170074462890625, 4.88478422164917, "[TT] Designers of the Attitude Determination Quaternion Filter = Students of the Technical University of Delft"]
-[10.295595169067383, 5.63621711730957, "[TT] Components of the EP (Experiment Package) = Viscometer/sample cell, precision temperature control elements"]
-[7.207604885101318, 8.117024421691895, "[TT] SNR of the XRS = 1:1 over 10 minute average"]
-[3.736490249633789, -1.0781666040420532, "[TT] Orbit Type of the GEOS-1 = Elliptical orbit"]
-[7.949643135070801, 5.841175556182861, "[FF] Hosts of the Optical Bench = The cameras"]
-[9.618358612060547, 0.8428792953491211, "[TT] Optimize Distance of the Primary Objective = 144 m"]
-[10.609746932983398, 7.299081325531006, "[FF] Swath Width of the Instrument = 1600 km"]
-[6.488206386566162, 3.275296449661255, "[TT] Resolution of the BlackSky Constellation = Less than one-meter"]
-[7.4022650718688965, 6.6228837966918945, "[TT] Target of Opportunity (ToO) response of the Instrument = < 24 hours"]
-[2.9670169353485107, 4.442687511444092, "[TT] Ground Resolution (Spotlight mode) of the XSAR = Less than 1 m"]
-[11.04013442993164, 6.081467628479004, "[TT] Material of the Optical Bench = Titanium"]
-[7.057356834411621, 8.249114990234375, "[TT] SNR of the COCTS = 1000"]
-[9.502436637878418, 4.980294704437256, "[TT] Angular Velocity Stabilization Accuracy of the Resurs-DK1 = 0.005o/s"]
-[3.429250478744507, -0.9327577948570251, "[TT] Orbit Type of the HY-1D = Sun-synchronous orbit"]
-[9.402894020080566, 7.0586724281311035, "[TT] Resolution of the COSI = 3 m"]
-[6.322140693664551, 5.286620616912842, "[FF] Function of the PIC (Peripheral Interface Controller) = Resets the FPGA whenever a critical fault has occurred in the OBC"]
-[5.095111846923828, 0.6367706060409546, "[TT] Activation Date of the MEOSAR = January 23, 2013"]
-[10.146751403808594, -0.4621336758136749, "[TT] Orbit Altitude of the ISARA CubeSat = 450 km"]
-[6.164509296417236, 4.022688865661621, "[FF] Concept of the MOSAIC = Meteosat missions can be combined by the user to provide an integrated data access system"]
-[8.634795188903809, 4.744113445281982, "[FF] Ultimate Goal of the BRITE Constellation = Provide photometric data on all 286 stars brighter than visual magnitude +3.5"]
-[2.992953062057495, 4.342931270599365, "[FF] Science Capabilities of the PALSAR-2 = Global environmental monitoring, biospheric research, cryospheric research, coastal ocean research, disaster mitigation"]
-[16.500911712646484, 3.5874557495117188, "[TT] Broadband Start of the OneWeb = Early 2022"]
-[5.824960231781006, -2.2472622394561768, "[TT] Altitude of the KOMPSAT-3 = 625 km"]
-[6.801421165466309, -0.15057924389839172, "[TT] Exposure Time of the Satellite = 100 ks"]
-[7.275197505950928, 3.5773074626922607, "[FF] Occultation Trials of the CanX-2 = January 2009 to June 2009"]
-[7.0605387687683105, 2.529231071472168, "[FF] Purpose of the STARFM = Combine MODIS data with Landsat data to produce synthetic Landsat-like imagery on a daily basis"]
-[13.097147941589355, 3.693096160888672, "[TT] Volume Requirement of the WINCS payload = Nearly a full 1U"]
-[14.657965660095215, 6.626026630401611, "[TT] Energy Storage of the Lithium ion battery = Two to four times more than proven technology"]
-[9.763171195983887, 7.380018711090088, "[TT] Ground Sample Distance (GSD) of the MESSR = 50 m"]
-[6.156404495239258, 0.45280662178993225, "[TT] Observation Continuation of the SoloHI = Until it leaves its field of view on 22 December"]
-[6.285221099853516, 4.657717227935791, "[FF] Functionalities of the UIS = Reception, management of product order, generating image collection proposal, image collection request, submitting product generation request"]
-[10.67111873626709, 0.8675824999809265, "[TT] Difference in Radius of the Kepler 11145123 = 3 km"]
-[16.553062438964844, 3.644829750061035, "[TT] Number of Satellites of the OneWeb = 428"]
-[9.149381637573242, 5.318413734436035, "[TT] Pointing Control of the QuikTOMS spacecraft = 0.5\u00ba"]
-[5.585361480712891, 4.853808403015137, "[TT] Software Package of the PRISMA POD = GHOST (GPS High precision Orbit determination Software Tools)"]
-[11.765175819396973, 4.750792503356934, "[TT] Body Structure of the UniSat-1 = Octagonal prism, 40 cm in diameter and a height of 25 cm"]
-[5.089115619659424, 3.0471391677856445, "[TT] Manufacturer of the Diwata-2b = Philippine DOST (Department of Science and Technology)"]
-[10.864002227783203, -0.3065434694290161, "[FF] Conference Presentation Date of the TanDEM-X = July 22-27, 2012"]
-[8.36568546295166, -1.000530481338501, "[TT] Average Elevation of the ICESat-2 = 1500 to 1750 meters"]
-[10.30941390991211, 5.79826021194458, "[TT] Temperature Difference of the Hot and Cold Target = 50-60 K"]
-[7.988082408905029, 0.11294897645711899, "[FF] Contribution of the GRACE = New fundamental insights into the changing mass distribution"]
-[13.50100326538086, 2.9649569988250732, "[TT] Weight of the Corvus-HD satellites = Around 20 Kilograms"]
-[4.408205509185791, 5.43125581741333, "[TT] Mission Duration of the GomX-3 = 1 year"]
-[9.19572925567627, 5.295803546905518, "[TT] Scan Mode of the SSULI = Extends from 10\u00ba to 27\u00ba below the satellite horizon"]
-[4.84967041015625, 0.6882769465446472, "[TT] Launch Date of the GF-3 = 10 Aug 2016"]
-[5.364150524139404, 0.037448588758707047, "[FF] Data User's Manual Edition of the IRS-P6 = Oct. 1, 2003"]
-[8.031124114990234, 6.081564903259277, "[FF] Data of the LPR = Electromagnetic image of the far side subsurface structure"]
-[6.1464972496032715, 1.1044092178344727, "[FF] Conference Date of the WINDS = Oct. 2-6, 2006"]
-[9.174516677856445, 5.45531702041626, "[TT] Slew Time, 15\u00ba roll of the ADCS = \u2264 4.5 minutes"]
-[5.1599202156066895, 3.300565004348755, "[TT] Manufacturer of the LRR = Alcatel Space Industries, France"]
-[8.325380325317383, 2.9011378288269043, "[FF] Constellation of the TEMPO = Instruments measuring air quality over the Northern Hemisphere"]
-[6.600830078125, 6.185079097747803, "[TT] TRL Level of the RadSat = 9"]
-[8.233131408691406, 4.513567924499512, "[FF] Contribution to Environmental Monitoring of the LARES = Unknown"]
-[6.778736114501953, 4.452512264251709, "[FF] FDIR Strategy of the Reaction Wheels = Fault Detection Isolation and Recovery"]
-[8.581197738647461, 0.769727349281311, "[TT] Area of the Akanda National Park = 929 km2"]
-[10.764954566955566, 3.049686908721924, "[TT] Rotation Rate of the O/OREOS nanosatellite = 1 to 2 rpm"]
-[3.4207358360290527, -0.8941543102264404, "[TT] Orbit Type of the Meteor-M2-3 = Sun-synchronous orbit"]
-[6.8139519691467285, 3.2278950214385986, "[FF] Model Validation of the Oculus-ASR = Successful"]
-[6.00250244140625, 7.150268077850342, "[TT] Data Acquisition Rate of the HARP-2 = Minimum two frames/second"]
-[9.16209602355957, -0.6580965518951416, "[TT] Orbit of the CSC and OSC = Highly elliptical (600 x 60530 km)"]
-[7.764479637145996, 6.609414100646973, "[TT] Full Disk Imaging Time of the VISSR = 30 minutes"]
-[8.415863037109375, 5.452237129211426, "[TT] Tracking System Position of the MMS = Far side of Earth"]
-[8.395848274230957, 0.6034135818481445, "[TT] Volcano Status of the Hofsj\u00f6kull = Largest active volcano in Iceland"]
-[8.896221160888672, 4.7684102058410645, "[TT] Number of Sensors of the Rosetta Plasma Consortium = Five"]
-[9.245458602905273, 4.79344367980957, "[FF] Accuracy of the SpinKF = Best available attitude accuracy"]
-[6.330402851104736, 4.74065637588501, "[FF] Function of the UIS = Catalog searching, order placing, order status monitoring and product download"]
-[7.725535869598389, 8.698760986328125, "[TT] Spectral Bands of the AGRI = 14"]
-[13.651987075805664, 5.829751491546631, "[TT] Power Output of the Solar Panels = 33 W"]
-[6.961716175079346, 4.409006595611572, "[FF] Complement of the HSC = Unknown"]
-[8.319059371948242, 7.694018363952637, "[FF] Noise and Dark Current Performance of the STL-11000M SBIG Camera = Very good even at room temperature"]
-[4.892039775848389, 7.031133651733398, "[TT] Duplex of the High-speed link = Half"]
-[6.368066310882568, 6.4302802085876465, "[TT] Data Collection Duration of the GOCI = Eight hours"]
-[7.706936359405518, 6.954276084899902, "[TT] Maximum Length of the Video Product = 90 seconds"]
-[7.955334663391113, 5.357575416564941, "[TT] Long-range of the FLLS system = 70 \u2013 250 m"]
-[13.263615608215332, 5.266725063323975, "[TT] Solar Panel Fixing Tool of the Skylab = Pair of wire cutters at the end of a 8 m long pole"]
-[6.564458847045898, 0.8312168121337891, "[TT] Good Solar Pointing Start Date of the SOVAP = 22/7/2010"]
-[13.405293464660645, 7.280732154846191, "[TT] ARW of the TDP = 0.008\u00ba/sqrt h"]
-[5.336038589477539, 1.1717681884765625, "[FF] Creation Date of the 3D Map = 13 January 2021"]
-[5.456380367279053, 4.971551418304443, "[TT] Operation of the GPS Receiver = Successful delivery of GPS navigation fixes and raw measurements"]
-[6.612021446228027, 5.118231773376465, "[FF] Function of the Microcontroller = Collects data from the OSL, from the temperature sensors and from measurements issued from the DUTs"]
-[6.0142035484313965, 6.559117794036865, "[TT] Realtime Data Latency of the CATS = Less than six hours"]
-[6.447700500488281, 4.290762424468994, "[FF] Function of the Ground Software = Make finding charts with source lists"]
-[5.863646984100342, 3.0084803104400635, "[FF] Fundraising Goal of the Inspiration4 = $100 million"]
-[4.282110214233398, 0.9765968918800354, "[TT] Delivery Date of the Argos-3 = 2002"]
-[4.723726272583008, 3.1427066326141357, "[FF] Prime Contractor of the TANSO-FTS-2 = Mitsubishi Electric Corporation"]
-[7.481016635894775, 2.3291208744049072, "[FF] Application of the WiFS camera = Vegetation index mapping"]
-[5.632372856140137, 0.3376956284046173, "[TT] Pass Dates of the ATLAS = March 22, 2019 and June 21, 2019"]
-[7.407969951629639, 0.9754634499549866, "[FF] Conference Presentation Date of the GRAIL = March 10-14, 2008"]
-[8.774609565734863, 8.826239585876465, "[TT] Dimensions of the Grating = 10 cm x 20 cm"]
-[7.164658546447754, 5.214147090911865, "[TT] Location of the Batteries = Below the laser"]
-[5.1898064613342285, 4.981368064880371, "[TT] GPS Receiver of the CartoSat-2 = SPS (Satellite Positioning System), an 8-channel GPS receiver (C/A code)"]
-[10.31286907196045, 4.578925609588623, "[TT] Malfunctions of the FormoSat-2 = One gyro and one reaction wheel"]
-[5.61702299118042, 0.33604732155799866, "[TT] Wind Profile Date of the ISS-RapidScat = Oct. 3, 2014"]
-[4.303558349609375, 5.286872863769531, "[TT] Frequency of the COSPAS-SARSAT = 121.5 MHz and 406 MHz"]
-[11.851299285888672, 6.467555046081543, "[FF] Objective of the PM = To flight-prove a monitor which measures the upset rate due to high energy protons"]
-[7.5592265129089355, -2.463712215423584, "[FF] Project Start Date of the GOLD = April 7, 2015"]
-[6.485295295715332, 3.939915418624878, "[FF] Development Team of the Space Cube 2 = T. Takahashi, T. Takashima, S. Fukuda, S. Kuboyama, M. Nomachi, Y. Kasaba, T. Tohma, H. Hihara, S. Moriyama, T. Tamura"]
-[10.775018692016602, 3.487348794937134, "[TT] Size of the SOAR = 3U CubeSat"]
-[9.224818229675293, 7.534389495849609, "[TT] Pan-Sharpening Capability of the Hyperion = 10 m"]
-[5.51873254776001, 5.384806156158447, "[TT] Electrical Connection of the SPA Components = SPA standard connector"]
-[10.367961883544922, 2.2324626445770264, "[FF] X-ray Output of the SMC X-1 = Varies"]
-[8.008996963500977, 4.417895793914795, "[FF] Picture Taking of the STARE satellite = Orbital debris"]
-[7.122455596923828, 4.27345085144043, "[FF] Impact of the LPT = Enable newer, smaller, lighter, and more complex spacecraft"]
-[5.157437324523926, 3.198080062866211, "[TT] Data Center of the GBOT = Observatoire de Paris"]
-[5.587890625, 2.853278636932373, "[TT] Developers of the CPR = NASA/JPL and CSA"]
-[8.628833770751953, 7.094104290008545, "[FF] Imagery Throughput of the UK-DMC-2 = Order of magnitude more than the first generation DMC"]
-[6.101513385772705, 6.925520420074463, "[TT] Mean Height Values Rate of the GEOSAT = 1 Hz"]
-[9.904356956481934, -0.37129655480384827, "[TT] Altitude of the CSG and CSK satellites = 620km"]
-[6.119833946228027, -0.5091748237609863, "[FF] Mission Duration of the SciSat/ACE spacecraft = 10 years"]
-[4.798123359680176, 0.4442081153392792, "[TT] Launch Date of the SOAR = 3 June 2021"]
-[14.231012344360352, 3.0323965549468994, "[TT] Mass of the STSat-3 = ~ 150 kg"]
-[5.340010166168213, 1.3117164373397827, "[FF] Conference Date of the Deorbitsail = April 8-11, 2013"]
-[5.627880096435547, 6.924967288970947, "[TT] Data Rate of the Data Flow = 2.2 Gbit/day"]
-[7.672095775604248, -0.8080582022666931, "[FF] Image of the Day Date of the ICESat-2 = 12 December 2018"]
-[7.751998424530029, 9.43211841583252, "[TT] Center Wavelength of the SSM/I = 1.55 cm, 1.55 cm, 1.35 cm, 0.81 cm, 0.81 cm, 0.35 cm, 0.35 cm"]
-[7.976933002471924, 6.874985694885254, "[FF] Image Types of the SGLI = True color composite, Near-ultraviolet, Degree of polarization"]
-[8.69588851928711, 4.931248188018799, "[TT] FOV (Field of View) of the Star Tracker = 7:5\u00ba (half axis)"]
-[7.945545673370361, 4.009003639221191, "[TT] Diameter of the External Occulter (EO) = 50 mm"]
-[11.830698013305664, 5.414581775665283, "[TT] Size of the LCT instrument = 0.6 m x 0.6 m x 0.7 m"]
-[6.222324371337891, 6.976352214813232, "[FF] Energy Efficiency of the Optical Downlink = -4.6 dB detected photons/bit or 25-100 \u00b5J/bit"]
-[6.818713665008545, 7.051161766052246, "[TT] Number of Beams of the HTS Ku-band multi-spot beams = 20"]
-[8.004767417907715, 9.163796424865723, "[TT] Wavelengths of the CATS = 355, 532, and 1064 nm"]
-[6.682733535766602, -0.5912144184112549, "[TT] Inner Cycle in the CRS Mode of the RISAT-1 = 12 days"]
-[10.771957397460938, 5.628319263458252, "[TT] Material of the Thermal Covers = 5 \u00b5m polyimide"]
-[8.536584854125977, 7.7193169593811035, "[TT] Array Size of the Detector = 1k x 1k"]
-[7.110894203186035, 2.422194242477417, "[TT] Publication Year of the Observation of the Earth and Its Environment = 2002"]
-[8.724756240844727, 2.883192539215088, "[FF] Mission of the CuSP = Measure particles and magnetic fields in space, testing the practicality for a network of stations to monitor space weather"]
-[7.734369277954102, 5.665175437927246, "[FF] Function of the Robotic arm = Moved the LED target along a pre-programmed pattern"]
-[6.998802661895752, 4.218408584594727, "[FF] Unknown of the TATUs = Unknown"]
-[10.956063270568848, 3.98051118850708, "[FF] Principle of the SIRDARIA = Cross-sectional drag increase of the spacecraft by unfolding a triangular sail on two deployed booms"]
-[7.941853046417236, 2.512943744659424, "[FF] Accuracy of the Climate Models = Agree fairly well with observed data"]
-[10.671297073364258, 1.108155369758606, "[TT] Size of the HD 260655 b = About 1.2 times as big around as Earth"]
-[3.0698390007019043, 3.926290988922119, "[TT] Global Scan Frequency of the NISAR = Every 12 days"]
-[5.414945602416992, 0.3155288100242615, "[TT] Delivery Date to ISS of the OPALS = April 20, 2014"]
-[10.980018615722656, 5.648813724517822, "[FF] Type of the Ablative Heat Shield with Composite Carrier Structure = Heat Shield"]
-[6.905100345611572, 1.349882960319519, "[FF] Relationship to Gravity Field of the Europa = Mirrors the shape of the moon itself"]
-[5.497047424316406, 2.611154079437256, "[TT] Program of the NuSTAR = NASA's Explorer Program"]
-[5.0438337326049805, 0.6146942973136902, "[FF] Development Date of the PRARE-2 = August 1995"]
-[7.704730987548828, 6.759519577026367, "[FF] Cadence of the Imaging Instrument = Fast"]
-[7.410237789154053, 0.22811226546764374, "[FF] Orbit of the OSIRIS-REx = Bennu\u2019s orbital plane"]
-[6.1744489669799805, 8.542271614074707, "[TT] Polarization of the Acquisition/Tracking Signal = Left-hand circular"]
-[8.947997093200684, 7.487448692321777, "[TT] Resolution of the Optical Imager = 7.5 m in the panchromatic band and 15 m in the multispectral bands"]
-[6.44980001449585, 4.637933731079102, "[FF] Accessibility of the AIT Approach = Reactive in case of troubleshooting"]
-[8.154829978942871, 6.519540309906006, "[FF] Operation Strategy of the SLIM6 = Maximum imaging time in the sunlit phase of the orbit"]
-[5.678035259246826, 11.362724304199219, "[FF] Approx. Peak Sensitivity Altitude of the Channel 7 = Unknown"]
-[4.878947734832764, 5.847348213195801, "[FF] CW Transmission Mode of the HORYU-2 = Provides the sensor data of the satellite health monitoring, such as power, temperature, and attitude to the ground station via the Morse code"]
-[7.027144908905029, 7.1276350021362305, "[TT] Beam Divergence of the Laser = 1 mrad"]
-[10.399258613586426, 2.1557116508483887, "[TT] X-ray Energy Detection of the NuSTAR = Above 30,000 eV"]
-[8.986337661743164, 5.75040340423584, "[TT] Misalignment Tolerance of the Projectile = Up to 45\u00ba"]
-[1.7435358762741089, 4.560390472412109, "[FF] N/A of the safety valve = N/A"]
-[5.370061874389648, 0.7622929811477661, "[FF] Announcement Date of the New Method = 20 July 2021"]
-[4.62539005279541, 0.13569889962673187, "[TT] Launch Date of the FREESTAR = Jan. 16 -Feb. 1, 2003"]
-[7.678359031677246, -0.8879120945930481, "[TT] Budget Lag Date of the ICESat = January 4, 2010"]
-[9.528406143188477, 7.156707286834717, "[TT] Spatial Resolution of the KMSS VIS Scanning Imager = 50 m and 100 m"]
-[10.274613380432129, 5.791500568389893, "[TT] Cosmic Background Radiation Temperature of the Instrument = About 3 K"]
-[7.210569381713867, 1.958501935005188, "[TT] Groundstation Pass Sharing of the Carbonite-1 = With other commercial satellites operated by SSTL"]
-[9.51062297821045, 6.218864440917969, "[TT] Incidence Angle of the Wide fine Quad-Pol = 18 - 42\u00ba"]
-[5.11460018157959, 6.989785194396973, "[TT] Data Rate of the Downlink = High"]
-[8.655915260314941, 3.4142017364501953, "[FF] Objective of the CERES = Provide continuity of the top-of-the-atmosphere radiant energy measurements"]
-[3.6164605617523193, 4.633631229400635, "[TT] Bandwidth of the Capella X-SAR Constellation = 500 - 700 MHz"]
-[5.29640531539917, 2.99613881111145, "[FF] Location of the Lockheed Martin Sensing and Exploration Systems = USA"]
-[8.99504566192627, 5.704243183135986, "[TT] Dihedral Error Variation of the CCRR = 0.05 arcsec"]
-[8.075024604797363, 2.508822202682495, "[FF] Data Usage of the HIRS = Calculate atmospheric vertical temperature profiles, determine ocean surface temperatures, total atmospheric ozone, precipitable water, cloud height and coverage, and surface radiance"]
-[7.706069469451904, 2.237131118774414, "[FF] Purpose of the POSEIDON = Satellite altimetry"]
-[8.012007713317871, 7.6300811767578125, "[FF] Cameras of the Hypatia = Sub-meter multispectral and 30 m hyperspectral"]
-[4.18747615814209, 7.2290167808532715, "[TT] Frequency Band of the Syrlinks EWC27 CubeSat X-band transmitter = X-band"]
-[7.962242603302002, 7.2753987312316895, "[TT] Data Output of the CCD (Charge-Coupled Device) = 10 bits"]
-[9.652637481689453, 7.268173694610596, "[TT] Ground Resolution at Apoapsis / Priapsis of the EXI instrument = 4.9 / 2.3 km per pixel"]
-[5.584654808044434, -2.050111770629883, "[TT] Imaging Modes of the KOMPSAT-3 = Single pass stereo"]
-[8.306450843811035, 9.046638488769531, "[FF] Unknown of the Argus 1000 Spectrometer = Unknown"]
-[7.6778950691223145, 6.545290946960449, "[TT] Scan Time of the INSAT-3D = 160 minutes"]
-[4.404191970825195, 7.896075248718262, "[TT] Uplink/Downlink Frequency of the OPAL = 420-450 MHz"]
-[6.74862003326416, -0.48725607991218567, "[TT] Repeat Cycle of the Orbit = 24 days"]
-[5.945274353027344, 5.110774040222168, "[FF] Function of the ROSA = Determine position, velocity and time using GPS signals"]
-[7.645535469055176, 6.826563358306885, "[TT] Cadence of the FUV Imaging Instrument = 30-minute"]
-[11.380693435668945, 3.611687183380127, "[FF] Propulsion System of the Psyche = Solar Electric"]
-[8.636885643005371, 0.36152970790863037, "[FF] Origin of the Ryugu = Parent asteroid several tens of kilometers wide, most likely in the asteroid families Polana or Eulalia"]
-[7.062360763549805, 7.300577163696289, "[TT] Energy of the ATLAS lasers systems = 250-900 \u00b5J"]
-[5.3618855476379395, 8.71438980102539, "[TT] Bandwidth of the Band 5 = 650-670 nm"]
-[13.83564281463623, 2.68040132522583, "[TT] Launch Mass of the Spacecraft = 730 kg"]
-[6.471221923828125, 7.366269588470459, "[FF] Implementation of the MRCPB = Wavelet transform with bit plane coding"]
-[8.014100074768066, 7.259775638580322, "[TT] Door Stability of the CSM = Stable without power supply"]
-[3.2774064540863037, 1.9213377237319946, "[TT] Take Measurements Through Clouds of the Sentinel-3 = Yes"]
-[5.381112098693848, 0.6401467323303223, "[FF] Build Date of the Maspalomas MEOLUT = Oct. 8, 2013"]
-[6.535712242126465, 1.8732911348342896, "[FF] URL of the Shuttle Radar Topography Mission = http://www2.jpl.nasa.gov/srtm/"]
-[5.30699348449707, 1.1539382934570312, "[FF] Meeting Date of the NPOESS = Sept. 29 to Oct. 3, 2008"]
-[7.993768692016602, 0.0645642876625061, "[FF] Purpose of the GRACE and GRACE-FO = Track changes in ice sheets, water stored on land, and variations in ocean mass"]
-[7.479454040527344, 0.8203878998756409, "[FF] Landing of the OMOTENASHI = On the moon"]
-[3.648888111114502, 4.5209760665893555, "[FF] Imagery Type of the SAR Satellites = SAR"]
-[4.8600287437438965, 0.4323602318763733, "[TT] Retrieval Date of the CRISTA-SPAS-2 = Aug. 16"]
-[11.396710395812988, 4.433919429779053, "[TT] Size of the CREDANCE = No larger than a postcard"]
-[8.698501586914062, 5.308079719543457, "[TT] Ground Segment Locations of the Dove-2 = 5"]
-[4.400606632232666, 0.6605030298233032, "[TT] Launch Date of the DMSP F-19 = April 3, 2014"]
-[5.79241943359375, 2.1524925231933594, "[FF] Deployment of the HaloSat = Deployed"]
-[7.4007568359375, 3.272768497467041, "[FF] Field of View of the GHGSat = 12km"]
-[5.3632001876831055, 0.3497270941734314, "[FF] Launch Date of the CHEOPS = 2017"]
-[6.103330612182617, 4.10117244720459, "[FF] Program Purpose of the SBSS-1 Pathfinder = Develop and initiate operations"]
-[8.018311500549316, 8.637885093688965, "[TT] Spectral Bandwidth of the SWIR Spectrometer = 10 nm"]
-[9.391765594482422, 6.215847492218018, "[TT] Off-nadir Scanning Angle of the ATM = ~15\u00ba"]
-[2.9752297401428223, 4.417149543762207, "[TT] Ground Level Measurement Resolution of the NISAR = Higher than Sentinel-1"]
-[4.663008689880371, -0.8849515318870544, "[TT] Splashdown Time of the Crew Dragon spacecraft Resilience = 7:06 p.m. EDT"]
-[5.717366695404053, 0.9852771759033203, "[FF] Presentation Date of the BepiColombo = 2012"]
-[3.330703020095825, 5.356263160705566, "[TT] Wavelength of the SAR = 9.6 cm"]
-[11.305450439453125, 4.659667015075684, "[TT] Min. Depth of the TAO/Triton = 1 m"]
-[5.228705883026123, -0.8905220031738281, "[TT] End of Mission Date of the Kolibri-2000 = May 3, 2002"]
-[5.860252857208252, 2.314697742462158, "[FF] Project Team of the MiRaTA = Blackwell, Cahoy, Rebecca Bishop"]
-[8.510123252868652, 1.401766300201416, "[TT] Measurement of the Aquarius = Sea Surface Salinity (SSS)"]
-[11.460868835449219, 2.1885159015655518, "[TT] \u0394V (cm/s) of the FengYun 1C Debris = 2.68/2.68"]
-[8.336386680603027, 2.4906461238861084, "[TT] Number of Substorms Observed from Excellent Vantage Point of the THEMIS Constellation = 6-10"]
-[6.8198561668396, 3.3752951622009277, "[FF] Geodetic Parameter Estimation of the SLR Satellite Constellation = Consistent"]
-[4.9858269691467285, 3.2480220794677734, "[TT] Manufacturer of the C2B = Boeing"]
-[9.006291389465332, 6.589595317840576, "[TT] Image Calibration of the HyperScout = Not yet calibrated"]
-[5.928657054901123, 7.101778984069824, "[FF] Contact Number of the Randomizer for High Data Rates = 20959/07/D/MRP"]
-[14.715344429016113, 6.619528770446777, "[TT] Capacity of the Lithium-polymer battery assembly = 3.4 Ah"]
-[5.787271499633789, 5.274566173553467, "[FF] Connectivity of the SES-17 = High throughput, global reach and low-latency"]
-[12.498309135437012, 3.237537145614624, "[TT] Liquid Propellant Capacity of the PSLV-XL = 2.5 tons"]
-[10.913983345031738, 7.524850368499756, "[FF] Swath Width of the MS = 20 km"]
-[5.051436424255371, 3.3231594562530518, "[TT] Manufacturer of the PolyITAN-1 = KPI (Kiev Polytechnic Institute)"]
-[5.95924186706543, 0.7829943895339966, "[TT] Image Capture Date of the DMS = November 12"]
-[13.605411529541016, 5.902079105377197, "[TT] Solar Array Power of the MicroMAS-2 = About 60 percent more power than MicroMAS-1"]
-[3.7666079998016357, -0.6972396373748779, "[TT] Orbit of the SBSS = Low Earth Orbit (LEO)"]
-[8.184295654296875, 1.1982243061065674, "[TT] Number of Soil Moisture Measurements of the SMAP = About 500 times per day"]
-[4.299625873565674, -0.11095914244651794, "[TT] Launch Date of the P35-10 = 19.11965"]
-[9.725205421447754, 7.613932132720947, "[TT] Angular Resolution of the ART-XC = 1 arcmin"]
-[6.48674201965332, 5.219199180603027, "[FF] Security Perimeter of the DCU = Excludes OBSW"]
-[8.27214241027832, -0.10699741542339325, "[TT] Likely Rise of the Global Mean Sea Level = Between 0.29 m and 1.1 m by the end of this century"]
-[13.414501190185547, 6.735520362854004, "[TT] Total Power of the Satellite = 161 W"]
-[7.7123847007751465, 9.149517059326172, "[TT] Spectral Band Centers of the ISIR = 8.55, 10.8 and 11.8m"]
-[6.285830974578857, 6.387729644775391, "[TT] Data Collection Duration of the COWVR = Within two days"]
-[8.082326889038086, 8.340023040771484, "[TT] Spectral Bands of the Pixxel\u2019s planned satellites = 300 including Visible to Near Infrared (VNIR) and Short Wave Infrared (SWIR)"]
-[6.553294658660889, 8.752784729003906, "[TT] Polarization of the POLDER-2 = yes"]
-[9.649918556213379, 8.355690956115723, "[TT] Field of View of the FOV = 10\u00ba x 10\u00ba"]
-[5.932690620422363, -0.35353630781173706, "[FF] Duration of the Decommissioning = Within two months"]
-[5.01154088973999, 0.8333739042282104, "[TT] Health Check Completion Date of the Hitomi = March 26, 2016"]
-[10.763348579406738, 0.9712512493133545, "[TT] Mass of the Jupiter = Over 300 times that of Earth"]
-[8.96055793762207, 4.393274307250977, "[TT] Accuracy of the Sun Sensors = ~1\u00ba"]
-[10.708453178405762, -0.10126074403524399, "[TT] Formation Geometries of the TanDEM-X = Bistatic Close formation"]
-[7.167485237121582, 7.439115047454834, "[TT] Wavelength of the LIDAR = 1064 nm"]
-[4.944704532623291, 7.190071105957031, "[TT] Data Transmission Rate of the S-band = 1 Mbit/s"]
-[7.791738510131836, 9.129761695861816, "[TT] Wavelength Range of the RIS = 0.4 - 14 \u00b5m"]
-[11.81179141998291, 6.788780689239502, "[TT] Energy Range of the IMAP = 10 eV to 100 keV"]
-[8.541341781616211, 3.2963812351226807, "[FF] Measurement Principle of the OLME = Solar Backscatter Ultraviolet (SBUV)"]
-[10.223700523376465, 1.6282402276992798, "[FF] Population of the ULXs = Far larger than currently observed"]
-[7.6519880294799805, 1.8663908243179321, "[FF] Land Coverage of the Boreal forests = Almost 15 percent of Earth's land surface"]
-[12.082534790039062, 3.486877918243408, "[TT] MEOP of the PPCU ion thruster = 15 MPa"]
-[10.850083351135254, 2.0871503353118896, "[TT] Testing Date of the Xona's Navigation System = Earlier this year"]
-[4.238688945770264, 2.5988762378692627, "[TT] Launch Site of the QBITO = Space Launch Complex 41 at Cape Canaveral Air Force Station in Florida"]
-[4.106156826019287, 7.20902156829834, "[TT] TT&C of the Chang'e-2 = S -band, X-band"]
-[5.646954536437988, 7.0955586433410645, "[TT] Operational Data Rates of the ACTS Mobile Terminal = 2.4, 4.8, 9.6, 64, to 128 kbit/s"]
-[5.5011138916015625, 1.8657793998718262, "[FF] Mission Status of the OPTOS = Operating quite well"]
-[6.153278827667236, 1.341871738433838, "[FF] PNAS Publication Date of the Swarm = March 21, 2022"]
-[11.96777057647705, 4.951632499694824, "[TT] Overall Dimensions of the X50L = 620 x 620 x 780 mm"]
-[8.267707824707031, 8.271016120910645, "[TT] Wavelength Range of the IMG = 3.3 \u00b5m to 14 \u00b5m"]
-[8.098726272583008, 7.520345211029053, "[TT] Source Data Rate of the Pan CCD detector module = 16 x 15 Mpixel/s (or 3.84 Gbit/s)"]
-[4.229438781738281, 7.188800811767578, "[TT] Band of the ETS-VIII = S-band"]
-[7.27583646774292, 6.897938251495361, "[TT] Laser Footprint Diameter of the SLA sensor package = 100 m"]
-[5.543582439422607, 0.3115066885948181, "[FF] Extension Date of the International Space Station = 27 April 2023"]
-[9.66869831085205, 7.1671857833862305, "[TT] Ground Imagery Size of the VISIM = 200 km x 150 km"]
-[3.294259548187256, 5.514572620391846, "[TT] Azimuth Resolution of the SAR Antenna = 1 m / 3 m / 6 m / 10 m / 100 m"]
-[7.472393035888672, -0.06265999376773834, "[TT] Orbit Altitude of the Gokturk-2 = 684 km"]
-[3.3593907356262207, 6.3246378898620605, "[TT] Length of the Spin Axis Dipole Antenna = 15 m"]
-[8.545896530151367, 3.835644006729126, "[FF] On-board Calibration System of the CLARREO = Uses the Sun as part of its on-board calibration system"]
-[10.1983060836792, 5.782276153564453, "[TT] Optimal PMT Temperature of the Detector Box = -20\u00b0C"]
-[7.814625263214111, 5.900665760040283, "[FF] Camera Activation of the HORYU-2 = Signal from the OBC"]
-[13.425202369689941, 5.476513385772705, "[TT] Type of the Solar Arrays = Surface-mounted"]
-[8.3680419921875, 7.610560894012451, "[TT] Detector Type of the HSRL receiver = Photon counting detectors"]
-[5.944648742675781, 4.870978355407715, "[FF] Function of the Ground Station = Receive information from, or transmit information to the satellite"]
-[5.659849166870117, 2.070178508758545, "[FF] Mission Status of the Platform = Unknown"]
-[9.918121337890625, -0.33174771070480347, "[TT] Orbit Altitude of the Sentinel-2 satellites = 786 km"]
-[4.322803974151611, 5.2693257331848145, "[TT] Frequency of the COSPAS-SARSAT System = 121.5 MHz and 406 MHz"]
-[7.099234104156494, 7.661088466644287, "[TT] Quantity of the LRA = 192 quartz corner-cubes"]
-[7.808661937713623, 7.265281677246094, "[TT] Data Transfer Rate of the SpW = 135 Mbit between 2 consecutive image acquisitions"]
-[8.487845420837402, 2.2256131172180176, "[FF] Baseline of the Wind Speed Retrieval Algorithm = Extension of one previously developed for the UK-DMC spaceborne mission"]
-[4.032938003540039, 2.191631555557251, "[TT] Launch Vehicle of the SMART-1 = Ariane-5G"]
-[7.036534786224365, 7.703305244445801, "[TT] Sigma naught of the Jason-2 = 0.7 dB"]
-[3.2279505729675293, 5.700262069702148, "[TT] Antenna Radiating Area Dimensions of the SAR = 10 m by 3.5 m"]
-[14.233491897583008, 3.2389094829559326, "[TT] Mass of the Total = 40 kg"]
-[8.557202339172363, 3.033311128616333, "[FF] Objective of the Tatiana-2 = Measurement of TLEs (Transient Luminous Events) in Earth's atmosphere"]
-[7.476659297943115, 5.232985496520996, "[FF] Laser Observations Basis of the Starlette and Stella = Orbits and SLR stations' coordinates determination"]
-[13.781905174255371, 7.172878265380859, "[TT] Regulation (%) of the PS-1 = \u00b13"]
-[9.226175308227539, 0.2107231616973877, "[TT] Length of the Izmit Bay Bridge = 3.3 km"]
-[10.470010757446289, 2.3091938495635986, "[FF] Capabilities of the X-ray Navigation = Position, attitude, and timekeeping"]
-[4.625466346740723, 1.697887897491455, "[TT] Manufacturer of the AlSat-2B = ALAS"]
-[5.752810478210449, 7.155578136444092, "[TT] Data Rate of the Data rate = 368 kbit/s"]
-[5.180387496948242, 5.474020957946777, "[TT] Quantity of the Navigation signal generation units = 2"]
-[5.935565948486328, 8.096805572509766, "[TT] Sampling Scheme of the SSM/I sensor = 128 samples per scan for the 85 GHz channels, and 64 scene stations per two scans for the other channels"]
-[4.698412895202637, 1.625767469406128, "[FF] Conference Date of the AlphaSat TDP = May 15-17, 2013"]
-[3.6825733184814453, 6.5664777755737305, "[TT] Antenna of the IMI = 6 x 9 m parabolic cylinder mesh reflector"]
-[6.0114569664001465, -0.5006828308105469, "[TT] Mission Duration of the Iris Radio = Nominal 90 days"]
-[10.596792221069336, 5.009570598602295, "[TT] Power of the Langmuir Probe = 7 W"]
-[11.768411636352539, 3.3190205097198486, "[TT] Thruster Type of the Propulsion Subsystem = Water micro-resistojet"]
-[7.375504016876221, 6.3877644538879395, "[FF] Experimental Area of the ARC = Can be changed"]
-[14.047983169555664, 2.9547159671783447, "[FF] Total Mass of the GeneSat-1 = Not provided"]
-[5.3488993644714355, 2.499478816986084, "[TT] Astronauts of the AMS-02 = Andrew Feustel, Greg Chamitoff"]
-[10.155540466308594, -1.3419201374053955, "[TT] Orbit Inclination of the GHGSat-C2 (Hugo) = 97.6\u00ba"]
-[8.029797554016113, 9.021527290344238, "[TT] Wavelength of the UVSP = About 1380 \u00c5 in second order"]
-[4.749777317047119, 6.647373199462891, "[FF] Function of the IDHS and CNM = X-band payload data reception, processing and archiving/delivering the PRISMA data and products"]
-[5.224541664123535, 0.6493222117424011, "[TT] Mission Selection Date of the ICON = April 12, 2013"]
-[10.696277618408203, -0.38484492897987366, "[TT] LEOP Duration of the TanDEM-X = 3 days"]
-[7.205111503601074, 2.883411169052124, "[FF] Peak Detection Rate of the exact Earth Satellite = TBD"]
-[6.720800876617432, 5.061779022216797, "[FF] Function of the TCU = Ensure the management of the TCS and of the CSS"]
-[10.763134956359863, -1.1235568523406982, "[FF] Control Phase of the SLATS = Elliptical to circular"]
-[6.519311428070068, 2.030658483505249, "[FF] URL of the X-Series Missions = https://web.archive.org/web/20130929003813/http://www.sstl.co.uk/Products/EO---Science-Platforms/SSTL-X50-series"]
-[4.402125358581543, 7.8182291984558105, "[TT] Uplink Frequency of the RF communications = 1.767 GHz"]
-[5.176692008972168, 1.748876690864563, "[TT] Operational Status of the ICARE = Still operational as of 2007"]
-[5.231326580047607, 6.892693519592285, "[TT] Downlink Capacity of the Tandem-L = ~ 8 TB/day"]
-[7.222557544708252, 9.099514961242676, "[TT] Interference filter - Wavelength of the Instrument = 777.4 nm"]
-[7.666154861450195, 2.45336651802063, "[TT] Instrument type of the ALT (SeaSat) = Radar altimeters"]
-[5.502017498016357, 4.012836933135986, "[TT] Operational Satellites of the FY-4 = 3"]
-[6.662883281707764, 0.7687771916389465, "[FF] Image of the Week Date of the Herschel = August 24, 2015"]
-[8.898550987243652, 4.631938934326172, "[FF] Attitude Modes of the Spacecraft = Nadir-pointing, Ram-pointing, Inertial-pointing, Slew-pointing"]
-[13.854439735412598, 2.8185040950775146, "[TT] Dry Mass of the QZS-1 = 1800 kg"]
-[7.103532791137695, 4.553317070007324, "[FF] Attached to of the PEST = JAWSAT"]
-[7.6928534507751465, 4.508368015289307, "[FF] Function of the Orbit Dynamics System = Calculate the orbit of the satellite with high accuracy"]
-[4.9981536865234375, -0.08573511242866516, "[TT] Launch Time of the STP-2 mission = 2:30 a.m. (06:30 UTC) on Tuesday, June 25"]
-[6.861080646514893, 2.926208019256592, "[FF] Provider of Experimental Measurements and Models of the NASA = Unknown"]
-[6.327211856842041, 4.831446170806885, "[FF] Features of the AOCS = Standardization of hardware and software at the module level"]
-[8.099282264709473, 1.4233403205871582, "[FF] Purpose of the SMOS = Measure soil moisture and ocean salinity"]
-[10.110616683959961, -1.522148609161377, "[TT] Inclination of the Spacecraft = 98\u00b0"]
-[4.599276065826416, 8.012345314025879, "[TT] Radio frequency (GHz) of the ALT = 13.5"]
-[5.657918930053711, 4.891642093658447, "[FF] Software of the GPS Receiver = Special software to allow the tracking of weak GPS satellite sidelobe signals"]
-[8.752050399780273, 8.420811653137207, "[TT] IFOV motion (jitter) of the Spectrometer = < 50 \u00b5rad/axis"]
-[10.810638427734375, -0.2981872260570526, "[TT] Stereo Imaging Start Date of the TWINS-1 and -2 = June 2008"]
-[6.036170482635498, 3.0025274753570557, "[TT] Mission Objective of the OSMA-1 = Refuel Landsat-7 spacecraft"]
-[6.890180587768555, 2.4630439281463623, "[FF] Media of the Sojourner 2020 = Carved stone sculpture, liquid pigment experiments, sculptures made of transgender hormone replacement meds"]
-[9.933189392089844, -0.3927900493144989, "[TT] Altitude of the Satellite = 685 km"]
-[5.426180839538574, 2.151296615600586, "[FF] Mission of the ISEE-2 = Mother/daughter/heliocentric"]
-[9.794721603393555, -0.47238245606422424, "[TT] Orbit Altitude of the Sunstorm = 551 km"]
-[3.950155735015869, 6.530380725860596, "[TT] Antenna of the RF Communications = Isoflux antenna"]
-[10.018705368041992, -1.523887276649475, "[TT] Inclination of the ASTERIA = 51.6\u00b0"]
-[18.797882080078125, 3.4803354740142822, "[TT] Mean \u0394N (m) of the Menara = 4.4"]
-[6.776130199432373, 5.018360137939453, "[FF] Function of the CSS = Provides potable water, oxygen and nitrogen to the CM"]
-[7.630887508392334, 2.15411376953125, "[TT] Primary Use of the Band 4 = SST, day/night clouds"]
-[4.769304275512695, 8.104524612426758, "[TT] Operating Frequency of the OSCAT-3 = 13.515 GHz"]
-[1.9413392543792725, -0.40225955843925476, "[TT] Data Gathering Duration of the Van Allen Probes = Nearly seven years"]
-[13.781396865844727, 7.213464736938477, "[TT] Power Voltage of the PM = 120 V DC"]
-[13.787939071655273, 5.351999282836914, "[TT] Type of the Solar Array = Triple-junction GaAs cells"]
-[11.72931957244873, 6.581119060516357, "[TT] Energy Range of the LET = ~1.5 to ~60 MeV/nucleon"]
-[8.002039909362793, 2.4331753253936768, "[FF] Data Collection of the ECOSTRESS = Morning data for the summer season"]
-[8.800216674804688, 3.391179084777832, "[FF] Parameter of the ISSS = Detect plasma densities and particle fluxes of 10 MeV energy range near the Earth"]
-[13.619522094726562, 5.4569621086120605, "[TT] Technology of the Solar Arrays = Monocrystalline silicon panels"]
-[5.209843635559082, 4.908792495727539, "[TT] Receiver Type of the GPS Receiver = Geodetic grade COTS receiver"]
-[9.106759071350098, 3.050398826599121, "[FF] Conference Presentation of the Set of instruments for solar EUV and soft X-ray monitoring = 37th COSPAR Scientific Assembly. July 13-20, 2008, Montr\u00e9al, Canada"]
-[3.175880193710327, 5.021648406982422, "[TT] Size of the Digital SAR Scene = 100 km x 100 km"]
-[5.595681190490723, 2.3134894371032715, "[TT] EMC Test Types of the MPO spacecraft = Conducted and radiated"]
-[10.163841247558594, 8.092290878295898, "[TT] Focal Length of the Telescope = 2626 mm"]
-[6.813887596130371, 1.7853327989578247, "[FF] URL of the GOCE = http://www.esa.int/Our_Activities/Observing_the_Earth/GOCE/Earth_s_gravity_scarred_by_earthquake"]
-[7.999104022979736, 3.717158317565918, "[TT] Instrument Type of the Myriade/AstroSat-100 = High resolution optical imagers, Other, Atmospheric chemistry, Communications, Data collection, Lightning sensors"]
-[12.055261611938477, -0.24406908452510834, "[TT] Observation Period of the TESS = July 18 to Sept. 11, 2019"]
-[3.9301018714904785, 2.002476692199707, "[TT] Launch Vehicle of the Aditya-L1 = PSLV-XL"]
-[5.031159400939941, 4.495851039886475, "[TT] Connection of the Ground Station = Permanent"]
-[4.826150894165039, 1.294289469718933, "[FF] Control System Development and Verification of the Delfi-C3 = Oct. 2-6, 2006"]
-[7.661032199859619, 6.595588684082031, "[TT] Image Delivery Time of the CCOR = Within 30 minutes of acquisition"]
-[7.8300580978393555, 3.5243613719940186, "[TT] Instrument Type of the GOSAT = Imaging multi-spectral radiometers (vis/IR), Atmospheric chemistry"]
-[9.11380672454834, 6.941701889038086, "[TT] Horizontal Error 90% (HE90) of the WorldView-3 = 3.9 m"]
-[8.185822486877441, 5.8207807540893555, "[FF] Mass Measurement Range of the NMS = 1-40 AMU"]
-[10.013230323791504, 8.254952430725098, "[TT] Focal Length of the NESSI = 893 mm"]
-[7.032999515533447, 5.38550329208374, "[FF] Provides Electrical Interfaces to Detectors of the FEE (Front End Electronics) = Power supply, bias voltages, clock and video signals"]
-[10.949021339416504, 7.5827717781066895, "[FF] Variation of the MDSL Metric = Two-dimensional"]
-[6.4452080726623535, 7.579035758972168, "[TT] Data Quantization of the MSGI-MKA = 16 bit"]
-[7.709423542022705, 9.136754035949707, "[TT] Band Spacing of the NIR = 11.4 nm"]
-[5.875728130340576, 3.8690412044525146, "[FF] Type of the Block 5D-3 Satellite = Civil and military low-altitude weather satellite"]
-[5.750303745269775, 4.356128215789795, "[FF] Configuration of the SATCS = Easily configurable and customized"]
-[5.147786617279053, 7.511579990386963, "[FF] Frequency of the USO = Unknown"]
-[6.173447132110596, -0.5697033405303955, "[FF] Operation Duration of the RADARSAT-2 = 10 years"]
-[4.861684322357178, 7.286365032196045, "[FF] Data Rate of the EWC27 X-band HDR-TM = High Data Rate-Telemetry"]
-[7.466783046722412, 5.337337493896484, "[TT] Components of the Tube = SPS (Shadow Position Sensor), FDA (Front Door Assembly), entrance objective, IO (Internal Occulter) with field stop"]
-[5.378535270690918, 3.796238422393799, "[TT] Manufacturer of the Accelerometer = Analog Devices"]
-[8.4015474319458, 3.1950082778930664, "[TT] Vertical Coverage of the Ozone Measurement Instrument = Tropopause height to 60 km"]
-[7.778875827789307, 3.256188154220581, "[FF] Operation of the GRAS = Supplies atmospheric soundings of the temperature and humidity of the Earth\u2019s atmosphere"]
-[5.7087321281433105, 4.423513412475586, "[FF] Testing Tools of the EDSN = DevSats, Flatsats, EDUs"]
-[8.014887809753418, -0.9353959560394287, "[TT] Estimates of the ICESat-2 = Could be low"]
-[5.781052112579346, -0.4158962666988373, "[TT] Contact Time of the STSAT-3 = 89 minutes after lift-off"]
-[6.198025226593018, 4.9014410972595215, "[FF] Requirement of the RCM = High-volume automated information processing capacity at the users\u2019 premises"]
-[4.061248779296875, 6.181703567504883, "[FF] Receiving Antenna Location of the Pontianak and Biak = To cover the satellite operation in the Central and Eastern part of Indonesia"]
-[1.961512565612793, -0.3937375843524933, "[TT] Discovery Date of the Van Allen Probes = March 15, 2017"]
-[4.4817118644714355, 7.791616439819336, "[TT] Data Rate of the Cadet-U UHF radio = 3 Mbit/s"]
-[11.609848976135254, 3.3039591312408447, "[TT] Propulsion System of the SPOT-6 = Mono-propellant propulsion system"]
-[7.9971537590026855, 5.056389331817627, "[FF] Calibration Techniques of the SMOS = Initial Guess based Techniques (\u2018Gibbs\u2019 approaches), the Floor Error Mask, the Pre-Distorted G-matrix and the Average Pattern Reconstruction"]
-[4.974726676940918, 4.196840286254883, "[TT] Current User of the Ground Station = IRS"]
-[8.594502449035645, 3.8126113414764404, "[FF] Purpose of the SOLCON-2 = Measurement of the solar constant"]
-[8.549019813537598, 4.506103038787842, "[TT] Shutter Requirement of the AgCam/ISSAC = US Laboratory Window external shutter to be open"]
-[5.071256637573242, 5.175328731536865, "[TT] Tracking Channels of the GPS Monarch receiver (GPSDR) = 6"]
-[5.489858627319336, 2.420900583267212, "[FF] Affiliation of the Sungdong Park = SI (Satrec Initiative Co. Ltd.)"]
-[5.970261096954346, 2.5984556674957275, "[FF] Benefits of the Planet Orbit = Access to Planet-certified partners with specific domain expertise"]
-[11.739890098571777, 0.10977699607610703, "[TT] Exoplanet Candidates of the TESS = Nearly 2,100"]
-[7.341492176055908, 4.694995403289795, "[FF] Mounting Location of the SPS head = Under the lid of the FDA (Front Door Assembly)"]
-[7.9054059982299805, 5.20975923538208, "[TT] Application of the FLLS = Monitor satellite displacement"]
-[6.351273536682129, 8.610713005065918, "[TT] Polarization of the 3 = Horizontal"]
-[6.2934370040893555, 3.2242681980133057, "[TT] Mission Life of the BlackSky Global Satellite = 3 years"]
-[5.674943447113037, 5.075679302215576, "[TT] Operating System of the OBC = CANOE (Canadian Advanced Nanospace Operating Environment)"]
-[4.4345316886901855, 5.672643661499023, "[TT] Observation Range of Doppler Velocity of the CPR = \u00b110m/s"]
-[8.129274368286133, 2.9806199073791504, "[FF] Source of Mid-tropospheric CO2 of the AIRS = Airflow into the mid-troposphere from the near surface"]
-[10.3347806930542, 2.4245729446411133, "[FF] Feature of the SXI = Domestically produced X-ray CCDs"]
-[8.178733825683594, -0.2712358832359314, "[TT] Pressure of the Arctic Ocean = Low"]
-[10.911443710327148, 10.096101760864258, "[TT] Installation Date of the Alpha Magnetic Spectrometer (AMS-02) = May 19, 2011"]
-[13.61583423614502, 6.855298042297363, "[FF]  of the EPS = "]
-[5.23997688293457, 0.39849013090133667, "[TT] Flight Model Manufacturing Start Date of the CHEOPS = End of 2015"]
-[9.061907768249512, 7.081681728363037, "[TT] Spatial Resolution of the HSC-III = Approximately 60 m"]
-[2.9719603061676025, 0.06169324368238449, "[FF] Quasi-Periodic Oscillations of the Sw J1644+57 = Present"]
-[9.198079109191895, 8.511820793151855, "[TT] Wavelength of the Lens 2 = 0.87 \u00b5m and 0.67 \u00b5m @ 0\u00ba"]
-[5.500723361968994, 6.380009651184082, "[TT] Data Storage of the MMU = 32 Gbit"]
-[6.339070796966553, 4.358047008514404, "[FF] Functions of the DPS = Process the raw science data, generate the ocean colour data products, work order generation, online quality control, output media preparations, data quality evaluation, and feedback to mission operations"]
-[8.397879600524902, 3.1979451179504395, "[FF] Observation Capability of the SUSIM = Ozone and molecular oxygen profiles"]
-[6.1439619064331055, 6.295507907867432, "[TT] Operation Mode of the B11 and B12 bands = TDI mode"]
-[5.831153392791748, -0.6590374112129211, "[FF] Orbit Evolution of the POPACS = Data"]
-[5.711982250213623, 2.6446237564086914, "[TT] Management of the NuSTAR telescope = Caltech and the agency's Jet Propulsion Laboratory"]
-[6.040033340454102, 0.5424270629882812, "[TT] First Contact Attempt of the ASTERIA = 22 November 2017 at 00:39 UTC"]
-[13.851954460144043, 7.289752960205078, "[TT] Input Voltage of the Receiver = 5 V"]
-[10.636204719543457, 1.5696276426315308, "[TT] Distance from Neutron Star to Companion of the Absorption Signatures = 0.04% of the distance from the neutron star to the companion"]
-[10.776444435119629, 2.1153664588928223, "[TT] Testing Location of the XMM-Newton mirror modules = Panter facility of the MPE (Max-Planck Institut f\u00fcr Extraterrestrische Physik) Garching, Germany"]
-[11.623162269592285, 6.893373012542725, "[TT] T Parameter of the ART-XC = \u2265 4 keV"]
-[6.763813495635986, 3.968046188354492, "[FF] Unknown of the INDEX Satellite = Unknown"]
-[16.49951171875, 3.5868515968322754, "[TT] Second-Generation Network Launch of the OneWeb = 2025"]
-[8.365285873413086, -0.6406646966934204, "[TT] Dimensions of the Iceberg B-22 = 85 km long and 64 km wide"]
-[3.1624577045440674, 1.6790369749069214, "[TT] Geometric Revisit of the Sentinel-2 = 5 days"]
-[8.90478229522705, 7.480301380157471, "[TT] Image Resolution of the Visual Sensor Array = 13376 x 10000 pixels"]
-[6.238876819610596, 2.0448453426361084, "[FF] Presentation of the GPM = 28th ISTS (International Symposium on Space Technology and Science)"]
-[11.622970581054688, 5.033889293670654, "[TT] Overall Length of the ASPIICS = 700 mm"]
-[6.547236919403076, 1.904282569885254, "[FF] URL of the SpaceX = http://blogs.nasa.gov/spacex/wp-content/uploads"]
-[5.312587261199951, 7.570045471191406, "[TT] Required Eb/No of the Unit = 5 dB"]
-[5.203089714050293, 0.9421541690826416, "[TT] Launch Date of the BlackSky-1 = Sept. 26, 2016"]
-[9.70173168182373, 0.7160776257514954, "[TT] Heliocentric Orbit Distance of the Observatories = Nearly 1 AU"]
-[6.98740291595459, 5.057458877563477, "[FF] Function of the FEE = Convert the current sources of the SiPMs into voltage"]
-[8.056379318237305, 9.080211639404297, "[FF] Parameter Species Wavelength of the SSUSI = O 1356 \u00c5"]
-[7.912909984588623, 1.1816598176956177, "[FF] Wildfires of the British Columbia = More than 40 wildfires"]
-[6.460450172424316, -0.8775603175163269, "[TT] In-Orbit Checkout Period of the GRACE-FO = 85 days"]
-[5.561148643493652, 0.38496309518814087, "[TT] Launch Date of the ATLAS = June 2018"]
-[6.24155855178833, 4.794339179992676, "[FF] Conference Presentation Date of the On-Board Data Handling System = Nov. 22-26, 2004"]
-[6.231083869934082, 3.1330323219299316, "[FF] Image Credit of the GOES 2nd generation spacecraft = NOAA"]
-[5.831859111785889, 5.234586238861084, "[FF] Protocol Tests of the LPT = Mobile IP, NTP, UDP, MDP, FTP, SCP, SSH, IP"]
-[4.059452056884766, 6.226767539978027, "[TT] Alignment of the VLF Antennas = Normal to the local magnetic field line when spacecraft is within \u00b120\u00ba of equatorial"]
-[3.5875039100646973, 6.0538554191589355, "[TT] Number of Panels of the Antenna = 8"]
-[4.726140975952148, -1.1807606220245361, "[TT] Primary User of the Beijing-1 = 21AT"]
-[5.801736354827881, 1.805325984954834, "[TT] Launch Date of the Orion = December 2014"]
-[4.328305721282959, 1.2120497226715088, "[TT] Environmental Test Campaign Duration of the SEOSAT-Ingenio = 3 months"]
-[10.940070152282715, 7.5693888664245605, "[TT] Swath Width of the PMC = 69 km"]
-[6.562193393707275, 0.034729164093732834, "[TT] Mission Duration of the CryoSat-2 = More than 10 years"]
-[1.7487202882766724, -2.072713851928711, "[TT] Sample Collection Date of the Hayabusa-2 = February 21, 2019"]
-[3.788817882537842, 4.671192169189453, "[FF] Function of the Receiver Module (RXM) = Conditioning the radar echoes prior to injecting them in the DGRs"]
-[9.725141525268555, -0.5877446532249451, "[TT] Orbit Altitude of the TecSAR = 450 km x 580 km"]
-[5.587663650512695, 2.5174174308776855, "[FF] Goal of the LAPAN-A3/IPB = Provide actual, frequent and accurate data for observing and predicting the condition of the Indonesian archipelago"]
-[3.433581590652466, 6.415861129760742, "[TT] Antenna Diameter of the Satellite = 4.2 meters"]
-[6.528408050537109, -0.27733737230300903, "[TT] Age of the Black Hole = 5 years on Orbit"]
-[7.832083702087402, 3.930882453918457, "[FF] Purpose of the RAMIS = Radiation Measurements In Space"]
-[6.938601970672607, 4.448723793029785, "[FF] Safety of the RVX = Needs to be ensured throughout the whole RVX mission"]
-[4.0097784996032715, 6.76066255569458, "[TT] Use of the L-Band = Allows for miniaturized antennas"]
-[5.4520955085754395, 6.279449462890625, "[TT] Onboard Memory of the COSMO-SkyMed-1 = 300 Gbit"]
-[4.967323303222656, 3.4437713623046875, "[TT] Manufacturer of the RCS = UK"]
-[9.990312576293945, -1.4946774244308472, "[TT] Orbital Inclination of the MWRI-RM = 50\u00b0"]
-[7.009226322174072, 6.080974578857422, "[TT] Number of Instruments of the Voyager 2 = 5"]
-[7.416358947753906, 5.564651966094971, "[FF] Signal to Noise of the Polar Scout = Best at high elevation angles"]
-[4.859853267669678, 4.55755090713501, "[TT] Command Transmission Capability of the Argos System = S/C-to-platform"]
-[6.2971978187561035, 1.9822428226470947, "[FF] URL of the SSULI = http://www.silvereng.com/programs/ssuli.htm"]
-[9.945981979370117, -0.5169914364814758, "[TT] Orbit Altitude of the PhiSat-1 = About 329 miles (530 km)"]
-[11.90549373626709, 5.423826694488525, "[TT] Dimensions of the Instrument = 445 x 327 x 182 mm3"]
-[10.794676780700684, 3.4933855533599854, "[TT] Optic Diameter of the 3U Cubesat = < 10 cm"]
-[4.8685712814331055, 7.241419792175293, "[TT] Safe Mode Downlink Data Rate of the ASTERIA Transceiver = 10 kbit/s"]
-[7.97800874710083, 13.683924674987793, "[TT] SSD of the B11 = 20 m"]
-[8.864518165588379, 7.447139739990234, "[TT] Image Format of the SCAMP Camera = JPEG"]
-[9.214531898498535, 3.0996346473693848, "[FF] Purpose of the SWIPS = Measure the properties of solar wind ions originating from the Sun"]
-[8.447735786437988, 8.425928115844727, "[TT] Spectral Resolution of the Spectrometer = <2.5 cm -1"]
-[4.473027229309082, 2.8147690296173096, "[TT] Location of the CRISTA/MAHRSI = Europe"]
-[8.153254508972168, 5.168551921844482, "[TT] Spectral Calibration of the SUCHI = Pre-flight"]
-[7.830478191375732, 2.2059104442596436, "[FF] Instruments of the Oceansat-3 = Oceansat Scatterometer (OSCAT-3), Ocean Colour Monitor (OCM-3), Sea Surface Temperature Monitor (SSTM), ARGOS-4 data collection system"]
-[5.833070278167725, -2.2322840690612793, "[TT] Inclination of the KOMPSAT-3 = 98.13\u00ba"]
-[8.298513412475586, 2.3955655097961426, "[FF] Mechanisms of the Aerosol Indirect Effect = Clouds with smaller droplets appear to be thicker to visible-light wavelengths and clouds that are more polluted are believed to be less likely to produce rain or snow"]
-[14.714400291442871, 6.62337064743042, "[TT] Capacity of the Li-ion batteries = 30 Ah"]
-[12.021329879760742, 4.504083156585693, "[TT] Spacecraft Volume (After Inflatable and Sail Deployment) of the Spacecraft = 128 cm x 330 cm x 330 cm"]
-[9.749345779418945, 8.389426231384277, "[TT] FOV of the Hyperion = 0.624\u00ba"]
-[14.051100730895996, 2.7888741493225098, "[TT] Launch Mass of the AprizeSat-5 = 14 kg"]
-[6.002020835876465, 5.687131404876709, "[TT] Coverage Area of the Corvus-HD satellites = 25 million km\u00b2"]
-[6.03494930267334, 5.982236862182617, "[TT] Number of Columns of the T/R Modules = 16"]
-[11.78189754486084, 3.328058958053589, "[TT] Nominal Isp of the Ion Propulsion System = 2,250 s"]
-[8.434418678283691, 2.011171579360962, "[TT] First Noctilucent Cloud Observation of the AIM = 2007"]
-[3.6925172805786133, 2.565023422241211, "[TT] Feeder Links of the Iridium PRIME = 2"]
-[6.630987644195557, 4.854607105255127, "[FF] Function of the GAMS = Monitor navigation signals"]
-[9.058475494384766, -1.2092572450637817, "[TT] Orbit Type of the SES-14 = Geostationary"]
-[10.493558883666992, 2.2547149658203125, "[FF] X-ray Detection Range of the Ulysses = Unknown"]
-[10.156607627868652, 1.3532228469848633, "[TT] Previous Catalogue of the Gaia Catalogue of Nearby Stars = Gliese Catalogue of Nearby stars"]
-[10.208775520324707, 5.673225402832031, "[TT] Temperature Control of the OBA = Yes"]
-[7.438051223754883, 2.9859607219696045, "[TT] Room-temperature System of the MethaneSAT = Thermal Stability of the Optics"]
-[9.290817260742188, 2.8537724018096924, "[TT] Solar Wind Speed and Beta of the ACE = ~41% lower on average from 2009 through the day 79 of 2013"]
-[8.688570976257324, 1.8392949104309082, "[TT] Sustained Winds of the Tropical Storm Fred = 65 miles (105 km) per hour"]
-[11.113241195678711, 0.6404977440834045, "[FF] Influence on Exoplanets of the Stars = Can influence the climates and habitability of a star\u2019s hosted exoplanets"]
-[5.635345935821533, 7.551694869995117, "[TT] Receiver Type of the Jason-1 = Miniaturized 2nd generation receiver (5.6 kg), a bi-frequency system in 2 channels"]
-[7.583559989929199, 8.702117919921875, "[TT] Total No of Spectral Bands of the MSU-50 = 6"]
-[7.0076751708984375, 0.8456254601478577, "[FF] NASA Press Release of the Gravity Probe B = May 4, 2011"]
-[6.9592390060424805, 0.8107307553291321, "[TT] Launch Date of the Gravity Probe A = June 18, 1976"]
-[6.105822563171387, 1.3279030323028564, "[TT] Information Date of the Swarm = June 22, 2017"]
-[9.217751502990723, -0.6929367780685425, "[TT] Orbit Perigee of the Beijing-3B = 601 km"]
-[3.3293139934539795, 1.464467167854309, "[TT] Mission Duration of the Sentinel-2 = 20 years"]
-[7.711029529571533, 3.319244384765625, "[FF] Mission Goals of the ARMADILLO = Characterize in-situ sub-millimeter level dust and debris particles in LEO (Low Earth Orbit) by sensing impacts at varying times, directions and locations"]
-[4.743289947509766, 1.6549447774887085, "[FF] Presenter of the GCOM-W = Toru Fukuda"]
-[3.811037063598633, 7.9255523681640625, "[TT] Modulation of the X-band Transmitter = QPSK"]
-[9.495599746704102, 6.288799285888672, "[TT] Look Angle of the MSU-E = \u00b132\u00ba"]
-[3.3202931880950928, 1.499355673789978, "[TT] Launch Date of the Sentinel-6 = 30 September 2020"]
-[5.886450290679932, 5.150961399078369, "[TT] Function of the OBC = Task management, data conversion, time management"]
-[5.717352390289307, -0.9167563915252686, "[TT] Design Life of the EROS-A = 4 years"]
-[3.4024593830108643, 4.759740829467773, "[TT] Interface of the PAZ SAR Processor = HMA (Heterogeneous Mission Access)"]
-[7.936038970947266, 8.709249496459961, "[TT] Spectral Range of the Kuzgun = 0.8-1.7 \u00b5m"]
-[10.674190521240234, -0.13713224232196808, "[TT] Initial Separation of the TanDEM-X and TerraSAR-X = 15700 km"]
-[7.44186544418335, 6.28328800201416, "[FF] Function of the Retroreflector in Space (RIS) = Reflecting a transmitted laser beam back down to a designated ground station"]
-[5.925323009490967, 1.8667147159576416, "[FF] Mission Date of the Orion EM-1 = 1-5 October 2018"]
-[6.603145122528076, 2.038066864013672, "[FF] URL of the Beidou = http://www.globalsecurity.org/space/world/china/beidou.htm"]
-[6.170799255371094, 7.014184474945068, "[TT] Data Rate of the GPS OEM Sensor = Up to 1 Hz"]
-[6.331690788269043, 8.106351852416992, "[TT] Rx Channels of the Complete Solution = 5"]
-[8.836241722106934, 6.876247406005859, "[TT] Magnification of the EIT = Five times"]
-[9.68769645690918, 8.258769035339355, "[TT] Field of View of the GIM = 26\u00ba starting along the spin axis by about 3\u00ba in azimuth"]
-[6.284264087677002, 3.8612005710601807, "[FF] Conference Presentation Date of the Space Plug-and Play Avionics = April 25\u201328, 2005"]
-[9.04183292388916, 0.5671789646148682, "[TT] Orbit Maneuvers of the THEMIS (and ARTEMIS) spacecraft = 19 maneuvers between Sept. 25 and Oct. 22, 2013"]
-[5.99627685546875, 3.5984442234039307, "[FF] Constellation Purpose of the Kleos Space S.A. = Monitoring global events and key locations of interest"]
-[6.525978088378906, 4.289085865020752, "[FF] Test Objective of the Catalytic Reactor = Developmental environmental control and life support system (ECLSS) unit returning for testing, teardown, and evaluation (TT&E) to determine the cause of failure and subsequent re-flight"]
-[6.942193984985352, 3.9931721687316895, "[FF] Purpose of the Storage Box = Store the inflatable tubes and the membrane"]
-[4.698155403137207, 4.79899787902832, "[FF] Information Provided of the LRIT = Ship identity, location"]
-[5.080338001251221, 5.145874977111816, "[TT] Channels of the GPS Receiver = 12"]
-[10.114903450012207, 1.3733010292053223, "[TT] Thick Disc Metallicity Growth of the Milky Way = By more than a factor of 10"]
-[4.3593573570251465, 0.6177985072135925, "[TT] First Flight of the SSJ/5 = DMSP F16, launch Oct. 18, 2003"]
-[5.646409511566162, 3.7590420246124268, "[FF] Regional Components of the DBNet = DBNet-EUMETSAT (EARS), DBNet Asia Pacific (with two nodes in Tokyo and Melbourne), DBNet South America (with two nodes in INPE/CPTEC and Buenos Aires), DBNet-NOAA DBRTN (Direct Broadcast Real-Time Network) and partners"]
-[7.1030592918396, 6.70004415512085, "[FF] Purpose of the BE = Make the laser beam more than four times wider"]
-[6.350276947021484, 8.552507400512695, "[TT] Polarization Amplification Factor of the Overhauser Nuclear Magnetic Resonance Autooscillator = About 3000"]
-[4.872696876525879, 8.567450523376465, "[TT] Center Frequency of the Channel 3 = 23.8 GHz"]
-[8.294794082641602, 5.054003715515137, "[FF] Deformation Measurement of the SELENE = Unknown"]
-[9.709330558776855, -0.3664938807487488, "[TT] Geometric Tangent Altitude of the Figure 30a = 245 km"]
-[9.676880836486816, -0.4567992687225342, "[TT] Operating Altitude of the GRAIL = 23 km"]
-[7.660858631134033, 1.969123125076294, "[FF] Tracking Area of the BeaverCube = Northeastern section of the US coast"]
-[5.750070571899414, -0.9497369527816772, "[TT] Design Life of the QuikSCAT = 2 years"]
-[4.714863300323486, 0.5373409986495972, "[FF] Data Collection Status of the STP-H7 and H8 = Ongoing"]
-[10.07772445678711, -1.5495531558990479, "[TT] Inclination of the GOES-R = 0\u00ba"]
-[6.87957763671875, 5.754803657531738, "[TT] FOR of the LRI = > 4.5 mrad"]
-[8.325167655944824, 4.367349624633789, "[TT] Autonomous Maneuver Capability of the BIROS = Yes"]
-[9.782892227172852, -0.5697311162948608, "[TT] Orbit Altitude of the SporeSat = ~400 km"]
-[6.907029628753662, 7.6735053062438965, "[FF] Components of the Antenna Subsystem = 1.8-m Main Reflector (MR), four separate feed horns, and calibration targets"]
-[9.742592811584473, -0.38560280203819275, "[TT] Tangent Altitude of the Figure 30b = 95 km"]
-[8.510197639465332, 7.433294773101807, "[TT] Current Detection Range of the MGF = 0.1 \u00b5Am-2 or stronger"]
-[12.111833572387695, 7.6393208503723145, "[TT] Mass of the Pushbroom Imager = 380 kg"]
-[11.000785827636719, 0.8856555223464966, "[TT] Number of Spacecraft of the LISA = 3"]
-[7.808569431304932, -0.12119434028863907, "[TT] Latency of the ATL09 ATLAS Atmosphere Cloud Layer Characteristics = 45 days"]
-[4.951369762420654, 0.5819726586341858, "[FF] Launch Date of the ZY-3 = January 9, 2012"]
-[8.40609359741211, 5.997559070587158, "[TT] Beam Alignment Error of the LRI = < 50 \u00b5rad"]
-[8.477319717407227, 7.627956390380859, "[TT] Detector Arrays of the Radiometer = 5"]
-[5.298627853393555, 1.1427146196365356, "[FF] IGARSS Presentation Date of the SMOS = July 26-31, 2015"]
-[4.952648162841797, 3.2695937156677246, "[TT] Development Contractor of the SSOT = EADS Astrium SAS"]
-[10.926170349121094, 6.3333420753479, "[TT] Mirror Shells and Coating Materials of the Mirror System = Nickel and Iridium"]
-[8.094843864440918, 5.151078224182129, "[TT] Measurement Calibration Technique of the SAM-II = Langley technique"]
-[6.0196614265441895, -0.02875329926609993, "[FF] Experience of the Keith Masback = Over 30 years"]
-[5.962676525115967, 3.4499154090881348, "[FF] Constellation of the UrtheCast = Optical and SAR satellites"]
-[4.911794185638428, 3.004086971282959, "[TT] Prime Contractor of the SciSat/ACE = Bristol Aerospace Ltd."]
-[5.45594596862793, 2.8741390705108643, "[FF] Conference Presentation of the SPIDER = Katherine Badham, Alan Duncan, Richard L. Kendrick, Danielle Wuchenich, Chad Ogden, Guy Chriqui, Samuel T. Thurman, Tiehui Su, Weicheng Lai, Jaeyi Chun, Siwei Li, Guangyao Liu, S. J. B. Yoo"]
-[8.23879623413086, 8.644065856933594, "[TT] Spectral Resolution of the HySI = \u2264 15 nm"]
-[9.38805866241455, -1.3742436170578003, "[TT] Orbit Eccentricity of the UniCubeSat = About 0.07"]
-[4.402498722076416, 7.795751094818115, "[TT] Uplink Frequency of the RF communications = 145.84 MHz"]
-[12.088174819946289, 3.760925054550171, "[TT] Plenum Pressure of the T3\u00b5PS = 4.5 bar"]
-[9.830357551574707, 8.679671287536621, "[TT] FOV of the VIS = \u00b144\u00ba (700 km swath)"]
-[10.252211570739746, 8.072181701660156, "[TT] Entrance Aperture Diameter of the Telescope = 50 mm"]
-[10.191014289855957, 8.088932991027832, "[TT] Aperture Diameter of the IMG = 10 cm"]
-[12.67362117767334, 1.926061749458313, "[FF] Observation of the SAGE-II = Stratospheric ozone decline over the Antarctic"]
-[5.348134994506836, 2.341229200363159, "[FF] Location of the OSIRIS = Odin"]
-[13.722016334533691, 3.0022125244140625, "[FF] Mass and Volume of the Astrium Sentinel 2 MMFU = Decline accordingly"]
-[8.3798828125, 7.341659069061279, "[TT] Detector Type of the Camera = CMOS"]
-[3.3967955112457275, 2.0391364097595215, "[FF] Acquisition Strategy of the Sentinel-2 = Systematic push-broom acquisitions, plus lateral mode capability for emergency events monitoring"]
-[9.517833709716797, 5.009721755981445, "[TT] Stability of the AOCS = < 5 arcsec/s of the X and Y axis"]
-[7.0250325202941895, 4.839128494262695, "[FF] Sewing of the MLI = Connection Method"]
-[7.873061180114746, 3.1678578853607178, "[TT] Absorption at 1.265 \u00b5m of the Hydrogen Fluoride (HF) = 10 -19 mol cm -2"]
-[3.5319173336029053, 4.732490062713623, "[FF] Ability of the L-band Synthetic Aperture Radar (SAR) = Penetrating vegetation such as forests"]
-[7.567872047424316, 6.616207599639893, "[TT] Resolution Time of the LAP = < 2 minutes"]
-[8.281039237976074, 0.8201802968978882, "[FF] Application of the Attitude Determination System = Small asteroid lander"]
-[11.807372093200684, 4.528907299041748, "[TT] Height of the Spacecraft = 1.2 m"]
-[8.684150695800781, 3.1541097164154053, "[FF] Image Processing of the NASA's Solar Dynamics Observatory = Enhance small features"]
-[7.874172687530518, 3.539099931716919, "[TT] Sensor complement / remarks of the Intercosmos- Bulgaria 1300 (Intercosmos-22) = Bulgarian sensors on Meteor-2 satellite technology (ionospheric plasma and high-energetic fluxes of charged particles, electric and magnetic fields, etc.)"]
-[6.194637298583984, 4.236572265625, "[FF] Mission Operation System of the ADEOS-II = Ground System"]
-[5.733765125274658, 12.146292686462402, "[TT] Wavelength FWHM of an unresolved line of the Spectrometer = 0.111 \u00b5m"]
-[5.09642219543457, 8.286503791809082, "[FF] Channel of the SSMIS = 8 at 150 GHz"]
-[6.777978897094727, 4.7631425857543945, "[FF] Technology of the MSI = State-of-the-art"]
-[8.196532249450684, 5.1769537925720215, "[FF] Function of the SES = Verify that the instrument high voltage performance as expected over temperature"]
-[8.893209457397461, 7.451961517333984, "[TT] Resolution of the Video Product = 1920 x 1080 pixels"]
-[6.952563762664795, 2.5927016735076904, "[TT] Daily Visibility of the Galileo Satellites 13 and 14 = Three to nine hours"]
-[9.042879104614258, 7.666167736053467, "[TT] Image Dimension of the FTHSI instrument = One by n spatial dimension"]
-[4.444431304931641, 6.896638870239258, "[FF] RF Communications of the SAC-D/Aquarius = S-band and X-band"]
-[8.77017593383789, 3.456754684448242, "[FF] Objective of the TPS = Study ionospheric plasma parameter variations which might be related to forthcoming earthquake analysis"]
-[12.130243301391602, 6.13580322265625, "[TT] Detection Rate of the AMS-02 = About 50 million of cosmic rays/day"]
-[10.290392875671387, 7.073687553405762, "[TT] Mesoscale Square Size of the ABI = 1.60\u00ba 1.60\u00ba"]
-[13.823298454284668, 2.694072961807251, "[TT] Launch Mass of the Kanopus-V 1 = 450 kg"]
-[7.948767185211182, 0.5322008728981018, "[FF] Conference Presentation Date of the Near Earth Asteroid Scout = 2-9 March 2019"]
-[9.428601264953613, 7.068660259246826, "[TT] Earth-Viewing Section Cross-Track Resolution of the SIS = 0.8\u00ba"]
-[8.85793399810791, 7.65523099899292, "[TT] Number of Pixels of the pnCCD camera = 384 x 384"]
-[10.946803092956543, 2.1224355697631836, "[TT] Manufacturer of the XMM-Newton = ESA"]
-[10.835073471069336, -0.2727428674697876, "[TT] DEM Resolution of the TanDEM-X = 12 m"]
-[8.174973487854004, 1.4628156423568726, "[TT] Observation Purpose of the IMI = Soil moisture and sea salinity"]
-[4.708158493041992, -1.1638697385787964, "[TT] Docking Date of the Tianzhou-2 = 29 May 2021"]
-[9.959049224853516, 4.6739606857299805, "[FF] Reaction Wheel Momentum Offloading of the PROBA-V = Autonomously performed when the instrument is not imaging"]
-[11.501260757446289, 3.4093704223632812, "[TT] Propulsion System of the CASSIOPE mission = None"]
-[2.331336736679077, 1.3073136806488037, "[TT] Deployment Date of the NanoSail-D2 = January 20"]
-[7.890446186065674, 2.686903953552246, "[FF] Use of the Thermal Waveband = Track cold clouds in the upper atmosphere as well as forest fires on the Earth's surface"]
-[4.389542102813721, 7.8284454345703125, "[TT] UHF Downlink Frequency of the RF Communications = 466.5 MHz"]
-[7.476336479187012, 3.7205214500427246, "[TT] Utilization of the NightPod = ISS-based long-exposure imaging"]
-[7.960862159729004, -0.34494173526763916, "[FF] Second-Lowest Extent Date of the Arctic Sea Ice = 23 September 2020"]
-[8.161462783813477, 8.547527313232422, "[TT] Spectral Bandwidth of the VNIR Spectrometer = 10 nm"]
-[7.661060333251953, -2.517677068710327, "[TT] Observation Types of the GOLD = DAY, LIM, NI1, OCC"]
-[8.523530960083008, 2.1046714782714844, "[FF] Goal of the Scatterometer = Provide closely spaced observations of surface wind speed and direction"]
-[9.472756385803223, 0.8767065405845642, "[TT] Closest Approach Distance to Ganymede of the Juno = 645 miles (1,038 km)"]
-[6.326483249664307, 3.70524263381958, "[FF] DMSP Missions of the SSM/I = F-8, F-10, F-11, F-12, F-13, F-14, F-15"]
-[7.126652240753174, 3.5494680404663086, "[FF] Benefit of the Cryogenic Fluid = Minimizes the amount of fuel spacecraft are required to carry from Earth's surface"]
-[6.408427715301514, 1.5783730745315552, "[FF] Symposium Date of the MICROSCOPE = June 4-8, 2012"]
-[11.702848434448242, 5.34953498840332, "[TT] Size of the Quango = The size of a microwave"]
-[7.147136688232422, 4.462588310241699, "[TT] Conduct of the RVX = Autonomously"]
-[5.2391510009765625, 0.9449319243431091, "[FF] Formulation Date of the CLERREO = 2009"]
-[5.625511646270752, 6.414683818817139, "[TT] Onboard Data Recorder Capacity of the CartoSat-2 = 64 Gbit"]
-[14.296893119812012, 2.7703323364257812, "[FF] Light-weight and small-size of the Kondor-E = Unknown"]
-[10.948659896850586, 7.595994472503662, "[TT] Nominal Swath Width of the Wide fine = 120-170 km"]
-[9.232013702392578, 5.021811485290527, "[FF] Challenge of the Attitude Control System = Inability to achieve sustained nadir pointing"]
-[8.160008430480957, -0.6326006054878235, "[TT] Measurement Coverage of the CryoSat-2 = Arctic"]
-[7.834008693695068, 3.0533862113952637, "[TT] CO2 Relative Accuracy of the GOSAT = 1%"]
-[11.477673530578613, 3.421135663986206, "[FF] Quantity of the Propulsion (Thrust Vectoring) = Orbital maneuvering and 2-axis TVC"]
-[7.862762451171875, 6.043214797973633, "[FF] Payload of the VisionCube-1 = Multi-anode photon multiplier tube(MaPMT), a camera, and a real-time image processing engine"]
-[9.499930381774902, 1.6522753238677979, "[FF] Observation of the New Horizons = Fluxes of charged particles in Jupiter's magnetotail"]
-[14.008386611938477, 3.0219810009002686, "[TT] Total Mass of the STRV-1a = 52 kg"]
-[8.119503021240234, 6.650823593139648, "[FF] Purpose of the Portable Ultrasound Device = Medical Imaging"]
-[4.294732093811035, 2.577680826187134, "[TT] Launch Location of the RemoveDebris spacecraft = Kennedy Space Center in Florida"]
-[7.558811187744141, 6.5144734382629395, "[TT] Image Capture Frequency of the MSU-GS = Every 15 minutes"]
-[9.740983963012695, 1.3987090587615967, "[TT] Resolution of the Pleiades-1A = 70 cm"]
-[7.841304779052734, 6.092759132385254, "[FF] Function of the Imaging System = Capture high resolution pictures"]
-[7.931615352630615, 8.610054969787598, "[TT] Spectral Bands of the HyperScout = 45 visible and near-infrared"]
-[5.591078281402588, 5.659717559814453, "[TT] Microcontroller of the OBC = ARM Cortex-M4F"]
-[11.169962882995605, 5.661093235015869, "[TT] Thickness of the Surface Coating = 10-mil"]
-[6.56601095199585, 4.145101070404053, "[FF] Payload of the MPQ442 = OpenSpace365"]
-[9.9463472366333, -0.3350943326950073, "[TT] Altitude of the Satellite = 530 km"]
-[11.525225639343262, 5.634267330169678, "[TT] Density of the Inconel 718 = 8190 kg/m3"]
-[8.547964096069336, 1.3623387813568115, "[FF] Determination of the Aquarius = Sea Surface Density"]
-[9.378096580505371, 7.44455099105835, "[TT] Nadir ground resolution (IFOV) of the 16 mm camera = 370 m x 370 m"]
-[7.791133403778076, 0.024138884618878365, "[TT] Orbit Altitude of the GOCE = ~260 km"]
-[7.389763355255127, 0.9811211824417114, "[FF] Conference Date of the GRAIL = June 11-15, 2012"]
-[9.066354751586914, 5.561084270477295, "[TT] Steering Accuracy of the VISS = \u00b1 0.3\u00ba"]
-[13.883905410766602, 2.9581658840179443, "[TT] Total Weight of the ExoMars 2016 Trace Gas Orbiter and Schiaparelli = 4.300 kg"]
-[5.648983001708984, 3.1820034980773926, "[TT] Contract Award of the PlanetIQ = $3.5 million"]
-[6.239486217498779, -0.4627216160297394, "[TT] Commissioning Duration of the Spacecraft = 30 days"]
-[10.400193214416504, 5.773601531982422, "[TT] Electronics Box Temperature of the PICAM = Below 50 \u00b0C"]
-[6.247747898101807, 4.951160907745361, "[FF] Components of the NLS-1 = CanX-1, AAUSat, DTUSat, XI, CUTE-I"]
-[11.971376419067383, 4.749991416931152, "[TT] Height Envelope of the UKube-1 = < 108 mm"]
-[3.1690309047698975, 4.382199287414551, "[FF] Calibration Method of the TerraSAR-X = Antenna model approach"]
-[6.911404132843018, -0.6772146224975586, "[TT] Orbit Period of the HY-2A = 104.5 minutes"]
-[4.785792827606201, -1.5588499307632446, "[FF] Purpose of the Tianyan-2 / Yizheng-2 = Technology verification"]
-[10.97011661529541, 7.597256183624268, "[TT] Full Swath of the QLP/NRTP = 20 k range gates, 30-240 km in width"]
-[14.513280868530273, 6.806780815124512, "[TT] Batteries Voltage of the Tsubame = 22.2 V"]
-[5.8457722663879395, -0.402446448802948, "[TT] Deployment Time of the MightySat I = 10 minutes"]
-[9.680244445800781, -0.5902202129364014, "[TT] Orbit Altitude of the PSLV-C19 = 470 km x 480 km"]
-[6.5564985275268555, 5.747551441192627, "[TT] Number of Boards of the DIME = 2"]
-[6.905608654022217, 7.094422817230225, "[TT] Laser Diodes Power of the SILEX = 60 mW"]
-[5.937869071960449, 3.792224168777466, "[TT] Contact Success of the CYGNSS = 100%"]
-[5.510231018066406, -1.8467413187026978, "[FF] Launch Date of the KOMPSAT-3A = April 14, 2015"]
-[10.176555633544922, 7.144939422607422, "[TT] Ground Surface Side Length of the LSI-1 = 342 km"]
-[4.788448333740234, -1.8336371183395386, "[FF] Mission Objective of the Chang'e-2 = Obtain important technical data for future deep-space exploration"]
-[10.505425453186035, 5.348616123199463, "[FF] Components of the Thermal Control Louvers = Front and back plates, flaps, springs"]
-[9.987680435180664, 6.03615140914917, "[TT] Stability of the Optomechanical System = Athermal and actively temperature-controlled"]
-[13.818504333496094, 5.317965984344482, "[TT] Solar Cell Type of the Solar Cell Experiment = Triple junction GaAs cells"]
-[8.303986549377441, 7.0402727127075195, "[FF] Type of the ULEIS = Time-of-flight (TOF) mass spectrometer"]
-[4.280788898468018, 7.10978889465332, "[TT] Required Reception System of the UHRIT = X-band reception system"]
-[10.156598091125488, 4.558107852935791, "[TT] Wheel Enclosure of the ADCS = Does not require a pressurised enclosure"]
-[10.915397644042969, 7.529684543609619, "[TT] Swath Width of the AIS Data Receiver = \u2265950 km"]
-[5.446203231811523, 3.171610116958618, "[TT] Design of the BRITE = Low Cost and Risk Mitigation"]
-[3.8663034439086914, 7.879339694976807, "[TT] Modulation and Coding of the Unit = BPSK, Rate 1/2, K=7"]
-[4.738649368286133, -0.2857213318347931, "[TT] Data Release Date of the CATS = June 12"]
-[8.818045616149902, 6.496168613433838, "[FF] Images of the PROBA-V = More than 5000"]
-[14.189306259155273, 3.287032127380371, "[TT] Mass Resolution of the ELENA = M/\u0394M H and heavy species"]
-[12.209126472473145, 0.5760042667388916, "[FF] Planetary Transits and Oscillations of stars of the PLATO = Upcoming"]
-[4.706448078155518, 0.6655757427215576, "[FF] Connection Check Date of the MetOp-C = 4 October 2018"]
-[5.751513957977295, -0.9084820747375488, "[TT] Design Life of the \u00d8rsted = At least one year (three year goal)"]
-[9.736988067626953, 7.462296009063721, "[TT] GSD (Ground Sample Distance) of the Camera = 1.5 m at an altitude of 650 km"]
-[4.662622928619385, 2.9993178844451904, "[TT] Hosting Location of the CTDA = GMES Security Coordination Center"]
-[11.944622039794922, 4.532867908477783, "[TT] Diameter of the Spacecraft = 2.10 m"]
-[5.773221015930176, 4.913120746612549, "[FF] GPS Receiver of the S/C = Provides S/C location data for accurate orbit determinations and onboard time delivery"]
-[14.612095832824707, 6.682017803192139, "[TT] Battery Type of the EPS = NiCd"]
-[10.99229907989502, 2.22358775138855, "[TT] Energy Level of the XMM-Newton = Up to 11 keV"]
-[5.193823337554932, 6.781400203704834, "[TT] Telemetry, Tracking, and Command (TT&C) Data Link Downlink of the AstroBus-L = 2 Mbit/s"]
-[4.967200756072998, 3.3626060485839844, "[TT] First Low Flying Customer of the LCT = Sentinel-1A"]
-[6.380533695220947, 1.8505032062530518, "[FF] URL of the SOLSPEC = http://lasp.colorado.edu/sorce/workshops/09_19_06/pdf_presentations/14_Thuillier_SOLSPEC-ISS.pdf"]
-[5.478111267089844, 6.392061710357666, "[TT] Data Storage of the NSat = 2 GB SD card"]
-[9.051103591918945, 5.412228584289551, "[TT] Body-pointing Capability of the Spacecraft = Up to \u00b145\u00ba"]
-[7.557980537414551, 6.213167667388916, "[FF] Operation Basis of the SILEX = Direct-detection system"]
-[12.419334411621094, 0.5436687469482422, "[TT] Mission Status of the PLATO = Planned"]
-[6.0335869789123535, 3.3977761268615723, "[FF] Services of the GMES = Meteorology, agricultural monitoring, food supply forecasting, fisheries, ship-routeing, urban planning, climate change studies, emergency response, humanitarian aid, external EU actions, border surveillance, maritime security"]
-[3.981053352355957, 6.209714412689209, "[FF] Number of Antennas of the TRACKER = Multiple"]
-[6.277876853942871, 2.0161468982696533, "[FF] Presentation of the IXV = IXV avionics, from design to mission results"]
-[5.459327697753906, 1.1873794794082642, "[TT] Launch Date of the LARES-2 = 13 July 2022"]
-[8.147370338439941, 3.706467390060425, "[TT] Instrument Behavior of the OCO-2 = Change in flight"]
-[6.530516147613525, 0.04974263161420822, "[TT] Lunar Swing-by Date of the Queqiao = May 25, 2018"]
-[5.157293796539307, 8.046366691589355, "[TT] Frequency Response of the SCM = LF/MF range"]
-[4.991152763366699, 0.3596767783164978, "[TT] Original Launch Date of the Spacelab-1 = Summer of 1980"]
-[6.708743572235107, -0.6460721492767334, "[TT] Orbital Duration of the TSUBAME = 7 days"]
-[13.369077682495117, 7.276102066040039, "[TT] Average Power Level of the EDFA = 0.5 W"]
-[6.531076908111572, -0.6851990222930908, "[TT] LTDN of the Orbit = 10:30 hours"]
-[8.375490188598633, 8.71523666381836, "[TT] FWHM at 40 nm of the EUV Simulation = 5.1 arcmin"]
-[4.930913925170898, 2.7252635955810547, "[TT] Operations Center of the ASTERIA = JPL Earth Orbiting Mission Operations Center"]
-[9.307646751403809, 7.047978401184082, "[TT] Resolution of the SHIROP = <10 m"]
-[6.833235263824463, 5.5696892738342285, "[FF] Components of the Communications Payloads = Common, monolithic LNAs (Low Noise Amplifiers) and T/R (Transmit / Receive) switching protection circuits"]
-[5.356896877288818, 4.030817985534668, "[TT] Number of Satellites of the UrtheCast = 16"]
-[10.141363143920898, 8.176528930664062, "[TT] Aperture of the William Optics ZS 71 ED = 71 mm"]
-[7.738927841186523, 0.5497973561286926, "[FF] Mission of the Lunar IceCube = Investigate the amount and distribution of water ice on the Moon"]
-[4.628407001495361, 1.638763427734375, "[FF] Mission Operations Date of the SkySat = May 28-June 1, 2018"]
-[8.157513618469238, 1.2749278545379639, "[FF] Application of the SMAP = Flood potential forecasting, drought monitoring"]
-[5.473368167877197, 6.208566188812256, "[TT] Memory Card Capacity of the DSU = 1 Tbit at EOL"]
-[9.12795639038086, 3.882387399673462, "[FF] Definition of the Solar Phase of Apsides Angle = The angle between the line of apsides projected into the ecliptic plane and the Earth-Sun line"]
-[6.255943775177002, 0.4112075865268707, "[TT] Launch Date of the ROSE-L = 2028"]
-[10.858720779418945, -0.31832587718963623, "[TT] First Global Coverage Completion Date of the TanDEM-X = January 2012"]
-[5.81256103515625, 4.6126322746276855, "[FF] Responsibilities of the X-band stations = Scientific satellite tracking, science data reception, raw data recording, formatted outputting, data transfer to the Mission Center"]
-[4.721441745758057, 6.64817476272583, "[FF] Signal Routing of the SM (Switch Matrix) = Routes the output signals from each of the combining networks to the two receiver channel inputs of the SE"]
-[13.569029808044434, 5.704154014587402, "[FF] Power Supply of the Starshine-3 = Integrated power supply (combined solar cells and thin film batteries)"]
-[6.210270404815674, 1.3746639490127563, "[FF] Development Status Presentation Date of the Spacecraft Fire Experiment (Saffire) = July 13-17, 2014"]
-[10.9364595413208, 2.0736453533172607, "[FF] Observation Date of the XMM-Newton = June 2013"]
-[7.349369049072266, 5.812183856964111, "[FF] Dynamic Range Optimization of the FPA = Mastered"]
-[5.099732398986816, 7.064127445220947, "[TT] TT&C Uplink Rates of the MERLIN = 16, 32 and 64 kbit/s"]
-[9.215374946594238, 6.132477283477783, "[TT] Field of Regard of the Sensor = 144\u00ba"]
-[9.567461013793945, 0.9048064947128296, "[TT] Speed of the PhiSat-1 = Over 17,000 mph (27,500 km/h)"]
-[7.028046607971191, -0.5660527348518372, "[TT] Rotation Period of the Bennu = 4.5 hours"]
-[9.206987380981445, 0.23535968363285065, "[TT] Length over the Bosporus of the Yavuz Sultan Selim Bridge = 1,408 m"]
-[5.279917240142822, 3.4496326446533203, "[FF] Manufacturer of the RAD6000 = Unknown"]
-[8.463044166564941, 3.1480257511138916, "[FF] Measurement of the Total Ozone Mapping Spectrometer (TOMS) = Earth's ozone layer composition"]
-[9.812217712402344, 2.692411422729492, "[TT] Mission Count of the NanoRacks = 17"]
-[9.067496299743652, 9.989717483520508, "[TT] Array of the Eastman Kodak KLI14403 linear CCD sensor = 14,400"]
-[8.233386993408203, -0.6749550104141235, "[TT] Acceleration of the Getz Glaciers = Over 44% for three glaciers"]
-[4.139896392822266, 1.3909746408462524, "[FF] Expected Meteosat-11 Activation Date of the MSG-4 = After commissioning"]
-[7.178338527679443, 0.14716346561908722, "[FF] Age of the Hyades = 600\u2013700 million years"]
-[7.949936866760254, -0.5845926403999329, "[FF] Event of the Stockholm Glacier = IPCC fifth assessment report approval session in 2014"]
-[11.416918754577637, 2.165926456451416, "[TT] \u0394V (cm/s) of the Cosmos 2251 Debris = 1.09"]
-[5.731715679168701, 12.149515151977539, "[TT] Wavelength FWHM of an unresolved line of the Spectrometer = 0.036 \u00b5m"]
-[8.541999816894531, 6.961404800415039, "[FF] Prototype of the L1 Detector = Photograph"]
-[7.668328762054443, 9.222868919372559, "[TT] Wavelength Range of the Band 7 = 3.80-4.00 \u00b5m"]
-[10.156509399414062, 5.803282737731934, "[FF] Insensitivity of the Telescope = Against temperature changes, but also against temperature gradients"]
-[4.543388366699219, 5.9103569984436035, "[TT] Beacon Frequency of the Life Raft = 406 MHz"]
-[9.947354316711426, 2.9182958602905273, "[FF] Conference Presentation Date of the PnP Cube Satellite = March 3-10, 2012"]
-[14.400014877319336, 3.20357346534729, "[TT] Mass of the LISS-3 = 106.1 kg"]
-[8.667373657226562, 0.915103018283844, "[TT] Launch Date of the Parker Solar Probe = Summer of 2018"]
-[5.208917617797852, 8.414565086364746, "[TT] Bandwidth of the DPS = 5 MHz"]
-[7.672852039337158, 0.859062910079956, "[FF] Purpose of the Infrared Imaging Spectrometer = Patrol area lunar surface infrared spectroscopy and imaging exploration"]
-[10.442474365234375, 5.770539283752441, "[TT] Water Temperature of the Fatu Huku Island = Exceeding 30\u00b0C"]
-[12.040252685546875, 3.0285518169403076, "[FF] Propulsion System of the Clementine = Bipropellant nitrogen tetraoxide and monomethyl hydrazine system for the maneuvers in space"]
-[11.918089866638184, 4.903670310974121, "[TT] Size of the Power Supply Unit = 18 cm x 20 cm x 41 cm"]
-[3.2863736152648926, 2.2693870067596436, "[FF] Software Provider of the Copernicus ROSE-L Satellite = SPACEBEL"]
-[7.076596260070801, 6.160181045532227, "[TT] Number of Science Instruments of the IMAP = 10"]
-[9.272832870483398, 2.678367853164673, "[FF] Performance of the Pulse Processing Electronics = Measure the largest flares without saturation"]
-[7.384801387786865, 3.4612507820129395, "[FF] Purpose of the PROBA-3 = Study the Sun\u2019s faint corona closer to the solar rim"]
-[8.426287651062012, 7.6552734375, "[TT] Detector Array of the Instrument = Linear array"]
-[13.851653099060059, 3.4030184745788574, "[TT] Electronics Unit Weight of the PRARE ground transponder = 35 kg"]
-[10.366650581359863, 2.2502827644348145, "[TT] X-ray Spectral Band of the AstroSat = 0.3 \u2013 100 keV"]
-[8.998391151428223, 7.429052352905273, "[TT] Resolution of the AlSat-2A = 2.5 m for the panchromatic band, and 10 m in four multispectral bands"]
-[8.576886177062988, 1.3822643756866455, "[TT] Measurement of the Aquarius = Atmospheric Parameters"]
-[6.597308158874512, 3.059408664703369, "[TT] Name of the WMO = World Meteorological Organization"]
-[7.568591594696045, 3.7594330310821533, "[FF] Compensation Accuracy of the NightPod = Arcsecond"]
-[9.670540809631348, -0.5154356956481934, "[TT] Orbit Altitude of the CartoSat-2D = 505 km"]
-[10.556844711303711, 2.7766942977905273, "[TT] Altitude of the Nanosatellites = Low"]
-[8.972923278808594, 5.578624725341797, "[TT] Pointing Requirement of the Imaging Payload = Towards nadir"]
-[11.89046859741211, 4.498103141784668, "[TT] Payload Volume of the GOMX-1 = 9 cm x 9 cm x 12 cm"]
-[10.023117065429688, -1.5351192951202393, "[TT] Inclination of the Orbit = 28.5\u00ba"]
-[6.898167610168457, 3.878264904022217, "[FF] Carried Instruments of the Flying Laptop = Scientific instruments for multispectral Earth observation as well as spaceborne maritime ship surveillance"]
-[7.921438694000244, 4.978742599487305, "[TT] Development Lead of the HyperScout = cosine"]
-[10.680285453796387, 1.5792880058288574, "[FF] Brightness of the Neutron Star = Even brighter than average"]
-[9.718864440917969, -0.20570920407772064, "[TT] Equivalence Principle Test Range of the LARES-2 = About 12,300 km"]
-[5.8111572265625, 3.417971134185791, "[TT] Funds Raised of the Sateliot IoT Nanosatellite Constellation = 2.4 million euros ($2.8 million)"]
-[6.140546798706055, 8.07955265045166, "[TT] Filter Banks of the Dual-channel Receiver Unit (DRU) = Same as LGU"]
-[5.202966213226318, 0.6398944854736328, "[TT] Launch Date of the RASAT = 17 August 2011"]
-[9.699806213378906, 2.982731819152832, "[TT] Observation Location of the CuPID = Low Earth orbit"]
-[7.328880786895752, 6.919832706451416, "[TT] Default Measurement Mode of the SOVAP = Shuttered open/close sequence of the right channel"]
-[8.154748916625977, 2.9484589099884033, "[TT] Missed Lightning in Northern Hemisphere of the TRMM LIS = Up to 30% in the warm season months"]
-[5.707675933837891, 4.05588960647583, "[TT] Type of the SSULI = Space environment"]
-[8.020268440246582, 7.4468159675598145, "[TT] No of CCD Elements in Cross-Track of the MSU-100 = 8000"]
-[4.944148540496826, 0.3352868854999542, "[TT] Installation Date of the DESIS = July 2, 2018"]
-[3.528710126876831, 6.437936782836914, "[TT] Antenna Diameter of the Earth station = 2.4 m"]
-[8.721449851989746, 2.090625762939453, "[TT] Antenna Diameter of the WINDS = 1.2 m"]
-[3.4414267539978027, 1.759885311126709, "[FF] Presentation Date of the Sentinel-1 = Nov. 30-Dec. 4, 2009"]
-[3.8512120246887207, 3.434169292449951, "[FF] Launch Date of the Galileo-FOC FM1 = Unknown"]
-[7.860095500946045, 2.1047041416168213, "[FF] Image Type of the TIRS = Land surface temperatures"]
-[8.666418075561523, 1.1392569541931152, "[TT] NASA Senior Review of the Aquarius/SAC-D = 2015"]
-[4.795765399932861, 3.380568265914917, "[TT] Location of the MOC = MBRSC"]
-[11.64567756652832, 4.254804611206055, "[FF] Separation of the T9 Payload Fairing\u2019s Base Ring = Verified"]
-[6.848395347595215, -1.788041114807129, "[TT] RMS orbit (radial component) of the Jason-2 = 10/2.5/1.5 cm"]
-[3.7806692123413086, 6.699517726898193, "[TT] Antenna Type of the Knudsen Station = Quad array 436CP42UG cross polarized UHF Yagis"]
-[9.807754516601562, 8.639348983764648, "[TT] IFOV for VIS and SWIR of the Telescope = 28 \u00b5rad (1 km)"]
-[7.776245594024658, 0.7393244504928589, "[FF] Re-opening Date of the Yellowstone National Park = June 22, 2022"]
-[9.69103717803955, -0.3092072606086731, "[TT] Apolune Altitude of the Rstar = ~2400 km"]
-[12.176905632019043, -0.07218853384256363, "[FF] Detector of the TESS Camera = 16.8 Mpixel, low-noise, low-power, MIT/LL CCID-80 detector"]
-[3.386371374130249, 5.430787086486816, "[TT] Peak Power Radiation of the SAR Antenna = 3.3 kW with 3/5 aperture in Spotlight and Ultra-fine mode 6.1 kW with full aperture in High-sensitive, Fine and ScanSAR mode"]
-[9.422628402709961, 4.764054775238037, "[FF] Flight Heritage of the Passive Attitude Control System = Extensive"]
-[3.490642786026001, 1.8018370866775513, "[FF] URL of the Sentinel-2 = http://www.earthobservations.org/documents/cop/ag_gams/200707_01/gmes_sentinel2.pdf"]
-[9.196223258972168, -0.41369327902793884, "[TT] Apogee of the Orbit = 373,000 km"]
-[12.163901329040527, 4.5842695236206055, "[TT] Dimensions of the Spacecraft bus = 2.0 m x 1.8 m x 3.7 m"]
-[16.54441261291504, 3.6499500274658203, "[TT] Number of Buses Produced for OneWeb of the Airbus = Over 400"]
-[8.136933326721191, 2.5964338779449463, "[FF] Mission Objective of the AMSU = Obtain global temperature and humidity profiles"]
-[10.09154987335205, 0.5280526876449585, "[TT] Maximum Separation of the STARE satellites = < 100 km"]
-[8.43311595916748, 2.0896759033203125, "[FF] Measurement Results of the SMMR = The instrument has produced the first global maps of surface temperature together with maps of wind speed"]
-[6.335000514984131, 4.445040225982666, "[TT] Implementation of the SIM = ESA SIMULUS Simulation framework"]
-[4.979974746704102, 8.238451957702637, "[TT] Bands of the CubeRRT = Tuned over 10 different bands commonly used for Earth observing microwave radiometers"]
-[6.1075615882873535, -0.17919817566871643, "[TT] Operation Status of the Genesis-2 = Nominal in 2011"]
-[5.624868869781494, 0.73424232006073, "[FF] Acquisition Date of the UrtheCast = July 15, 2015"]
-[11.406855583190918, 5.881200790405273, "[TT] Structure Material of the New Horizons = Aluminum"]
-[5.240302085876465, 1.465165138244629, "[FF] Presentation Date of the Deimos-1 = April 16-18, 2013"]
-[4.282020092010498, 5.924108028411865, "[TT] Azimuth tracking of the Antenna = 360\u00ba Continuous"]
-[4.153416633605957, 0.19367267191410065, "[TT] Launch Date of the SpaceX Falcon-9 = Jan. 14, 2017"]
-[5.431581497192383, 1.1750168800354004, "[TT] Launch Date of the Oculus-ASR = 25 June 2019"]
-[8.6885347366333, 6.924504280090332, "[TT] Imaging Capability of the FY-4 Series = Enhanced"]
-[5.55509090423584, 7.983879089355469, "[TT] Response Frequency of the MAG = 2.5 Hz"]
-[13.350664138793945, 5.414593696594238, "[TT] Solar Panels of the Microsatellite = Four deployable solar panels of 0.5 m2"]
-[4.964005947113037, 3.5680840015411377, "[TT] Manufacturer of the EPS = GER/NL/IT/USA"]
-[4.549253940582275, -0.8299517035484314, "[FF] Overview URL of the Dragon SpX-3 = http://www.spaceflight101.com/dragon-spx-3-cargo-overview.html"]
-[5.042201042175293, 8.32851505279541, "[TT] Operating Frequency of the 183 GHz radiometers = 183 GHz"]
-[9.280651092529297, 2.865940809249878, "[FF] Purpose of the Solar X-ray Spectrometer = Monitor space weather"]
-[7.852272987365723, 3.490725517272949, "[TT] Sensor complement / remarks of the Meteor-2-1 = TV, IR, SM, RMK-2 (experimental)"]
-[7.605476379394531, 4.211094856262207, "[FF] Operating Phases of the NMS = Perigee and near-perigee"]
-[5.6244354248046875, 2.354393243789673, "[FF] Population of the Riyadh = 5.4 million in 2012"]
-[9.265303611755371, -0.3932906985282898, "[TT] Apogee of the FASat-Alfa = 682 km"]
-[7.954977989196777, -0.8897140026092529, "[FF] Image Credit of the ATLAS = NASA Earth Observatory, image by Joshua Stevens, using ICESat-2 data from the National Snow & Ice Center, topographic data from SRTM, and Landsat data from the U.S. Geological Survey"]
-[8.02051830291748, 2.452927350997925, "[FF] Purpose of the MWI = Serve operational meteorology, oceanography, sea-ice/snow/land surface observation and climate applications"]
-[9.611685752868652, 6.7114434242248535, "[TT] Spatial Resolution of the Geodesy Unification of worldwide height systems = 100-20000 km"]
-[9.680839538574219, 0.17574617266654968, "[TT] Parachute Manufacturer of the ExoMars mission = Arescosmo"]
-[7.021766662597656, 4.7053542137146, "[FF] Parameter of the GRS = Value"]
-[10.147436141967773, 7.216670989990234, "[TT] Area Coverage of the MUX = 30 km by 20 km"]
-[5.6269989013671875, 7.165125846862793, "[TT] Data Rate of the WFI = 50 Mbit/s"]
-[9.838720321655273, 4.514648914337158, "[FF] Control Authority Mechanism of the Reaction Wheels = Baseline three axis control authority mechanism at all altitudes"]
-[10.331378936767578, 7.966416835784912, "[TT] Diameter of the Telescope = 12 cm"]
-[9.256141662597656, 3.2088634967803955, "[FF] Purpose of the Compact Coronagraph (CCOR) = Image the solar corona and help detect and characterize CMEs"]
-[6.5421881675720215, 3.192607879638672, "[TT] Operating Stability of the AMS-02 = Stable since May 2011"]
-[8.701445579528809, 4.010758876800537, "[FF] Operation Principle of the LENA = Neutral particles enter the instrument through a collimator which filters charged particles. LENA converts neutrals to negative ions through a near specular glancing reflection from a tungsten surface. Negative ions from the surface are then collected by the extraction lens which focuses all negative ions with the same energy to a fixed location. In the extraction lens, the ions are accelerated by 20 kV prior to entering the electrostatic analyzer (they are detected as they pass through a thin foil and strike an image plane detector). Finally, the ions pass into a time-of-flight/position sensing section where ion mass, energy, and angle are determined"]
-[10.830376625061035, 1.4746577739715576, "[FF] Mass of the Neutron Star = About the same mass as our Sun"]
-[5.2205424308776855, 2.7274539470672607, "[TT] Usage of the EPIRB = Maritime applications"]
-[4.606757640838623, 3.0651140213012695, "[TT] Primary Satellite Operations Control Center Location of the C3S = Suitland, MD"]
-[8.78411865234375, 9.42229175567627, "[TT] Spectral Band 1 Center Wavelength of the TANSO-CAI = 0.380 \u00b5m"]
-[4.5479936599731445, 0.2594640254974365, "[TT] Launch Site of the IDEA-OSG 1 = Vostochny launch site"]
-[4.981226921081543, 1.8295481204986572, "[TT] Operation Status of the RASAT = Nominal"]
-[4.0789313316345215, 6.580646991729736, "[TT] VHF transmitting antennas of the SMDC-ONE = 4"]
-[5.211203575134277, 0.8831531405448914, "[TT] Operation Start Date of the NIRST instrument = Winter of 2012"]
-[3.355318546295166, 5.100541591644287, "[TT] Polarimetry of the SAR-RCM = Hybrid"]
-[10.542410850524902, 4.955544471740723, "[TT] Hosting Payload of the Aalto-2 = m-NLP (Multi-Needle Langmuir Probe)"]
-[8.47265625, 7.469228267669678, "[FF] Scanning Type of the Instrument = 58 pixels / scan line, arranged in 2 x 2 arrays"]
-[6.050519943237305, 3.1150598526000977, "[TT] Satellite Launch of the AMSU = NOAA-15"]
-[7.006773948669434, 4.81444787979126, "[FF] Initiation Connector of the CSD = Unknown"]
-[7.4698591232299805, 3.7651681900024414, "[TT] Camera of the NightPod = Nikon D3s"]
-[3.3702542781829834, 5.2092108726501465, "[TT] Nominal Looking Direction of the SAR = Right"]
-[7.5614142417907715, -2.467982769012451, "[FF] Integration Date of the GOLD = May 23, 2017"]
-[7.743675708770752, 3.001028299331665, "[TT] Atmospheric Sounding Capability of the FY-4 Series = Enabled"]
-[6.096474647521973, 3.4254956245422363, "[TT] Number of Experiments of the D-Sat = 3"]
-[3.2619431018829346, 5.084777355194092, "[TT] Altimeter range RSS error SAR of the Jason-2 = 2.9 cm"]
-[10.84764575958252, 7.5088324546813965, "[TT] Swath Width of the GeoEye-1 = 14.4 km"]
-[9.308956146240234, 5.583652496337891, "[TT] Pointing Stability of the ASTERIA = 0.5 arcseconds RMS"]
-[9.87500286102295, 4.699664115905762, "[TT] Spacecraft Spin Rate of the Spin Track = 1 revolution in 37.5 seconds"]
-[4.926226615905762, 0.581915020942688, "[TT] Scheduled Lift Off of the EM-2 = As soon as 2021"]
-[7.831793308258057, 8.306489944458008, "[FF] Design Purpose of the Data Processing Pipeline = Accommodate both products in each of the six spectral bands"]
-[11.352914810180664, 5.852950096130371, "[TT] Primary Structure Material of the CM (Crew Module) = Aluminum and aluminum-lithium"]
-[5.786197662353516, 2.7270383834838867, "[FF] Developer of the skCube = SOSA (Slovak Organization for Space Activities ) at the University of Zilina"]
-[7.54352331161499, 5.631768703460693, "[FF] Frequency Band of the Microstrip-based L-band radiometer = L-band"]
-[11.376618385314941, 4.324984550476074, "[TT] Size of the CU-E3 = 6U"]
-[6.23955774307251, 4.581782817840576, "[FF] Function of the Vertical installation dolly = Main loading equipment for the satellite integration and testing procedures"]
-[5.78019380569458, -0.4191536605358124, "[TT] Function of the Instrument Package = Serve as reference to determine the aging effects"]
-[8.293444633483887, 2.474198818206787, "[FF] Mission Objective of the PARASOL = Improve the microphysical and radiative property characterization of clouds and aerosols"]
-[14.235122680664062, 3.0581483840942383, "[TT] Mass of the BRITE-CA-2 = 7 kg"]
-[7.8162431716918945, 5.882176876068115, "[TT] Type of the Scanning Radiometer = Total-power passive microwave radiometer/scatterometer"]
-[5.680384635925293, -0.8631595373153687, "[TT] Design Life of the QZS-1 = > 10 years"]
-[10.165729522705078, -2.744032382965088, "[TT] Module size of the SLC NAND-FMM = 200 x 243.5 mm"]
-[4.821017742156982, 4.754663944244385, "[FF] Purpose of the NAVISP = Strengthening European competitiveness in the navigation arena"]
-[7.675222396850586, 1.9659372568130493, "[TT] Coverage of Turkey of the RASAT = 98%"]
-[8.069377899169922, 1.0007965564727783, "[TT] Precipitation Deficit of the Turkey = 48 percent lower than the average for 1981-2010"]
-[6.2977519035339355, 8.637584686279297, "[TT] Function of the OMT = Separate horizontal and vertical polarization components"]
-[5.431640148162842, 7.21329402923584, "[TT] Data Rate (max) of the CanX-2 = 1024 kbit/s"]
-[5.875929832458496, -0.7136054039001465, "[TT] Design Life of the RADARSAT-1 = 5 years"]
-[9.412811279296875, 6.9661383628845215, "[TT] Spatial Resolution - Spotlight of the ALOS-2 = 1 m x 3 m"]
-[4.545877933502197, 7.845404148101807, "[TT] UHF Frequency Last Transmission of the RAX-2 = April 20, 2013"]
-[9.314743041992188, -0.5810335278511047, "[TT] Argument of Perigee of the Molniya Orbit = 270\u00b0"]
-[7.841549873352051, 8.446356773376465, "[TT] Spectral Bands of the MESSR = One visible (VIS) band and three thermal infrared (TIR) bands"]
-[5.559387683868408, 4.712184906005859, "[TT] Percentage of GPS Signal Loss in Strong EPIs of the Swarm = About 95%"]
-[5.60508918762207, 7.250058174133301, "[TT] Bit Rate of the DCP = 12.5 kbit/s"]
-[10.187952041625977, 7.058647632598877, "[TT] FOR in Cross-Track of the MWIR = 1060 km"]
-[9.30273723602295, 2.5969274044036865, "[FF] Flare List Events of the RHESSI = Over 70,000"]
-[6.956009387969971, 6.151353359222412, "[TT] ScanSAR of the Mode = -"]
-[7.3876800537109375, 3.5173532962799072, "[FF] Frequency of the Monitoring of HIS = Daily"]
-[7.94389009475708, 5.948521614074707, "[FF] Purpose of the High-Resolution Video Camera = Zoom in on the actual target of interest"]
-[8.366103172302246, 1.2029590606689453, "[TT] Range of Values of the Precipitation over water = 0 - 25"]
-[8.140632629394531, 2.777559518814087, "[TT] Measurement Domain of the Sentinel-2 = Atmosphere, Land"]
-[5.412003040313721, 3.869443893432617, "[TT] Number of Orbits of the Satellite = 167"]
-[9.068400382995605, -0.3715254068374634, "[TT] Perigee (km) of the Intercosmos- Bulgaria 1300 (Intercosmos-22) = 825"]
-[6.252434730529785, 1.7788286209106445, "[FF] Orbit Information of the SWOT = http://www.aviso.altimetry.fr/es/misiones/future-missions/swot/orbit.html"]
-[9.156868934631348, 7.206996440887451, "[TT] Resolution of the DCG = 20 \u00b5s"]
-[12.701729774475098, 1.9319161176681519, "[FF] Objective of the SAGE-III = Provide global, long-term measurements of key components of the Earth's atmosphere"]
-[9.283193588256836, -0.6573066711425781, "[FF] Path of the Trisat-R's Orbit = Through part of the Van Allen belts"]
-[4.079058647155762, 6.193641662597656, "[FF] Unknown of the Active Phased Array Antenna = Unknown"]
-[7.581264019012451, 5.43331241607666, "[FF] Components of the DLRE = Instrument optics bench assembly (OBA), elevation/azimuth yoke, instrument mount"]
-[4.631034851074219, 6.720787525177002, "[TT] Image Products Downlink of the Aleph-1 satellites = High-speed DVB-S2 (Digital Video Broadcasting-Second Generation) channel operating at 8050-8100 MHz"]
-[7.400523662567139, 3.123383045196533, "[FF] Purpose of the EnviSat = Earth observation"]
-[7.750109672546387, 2.779552459716797, "[FF] Infrared Capability of the Kanopus-V-IK = Detecting sources of fire as small as 5 m x 5 m on a 2,000 km swath of land"]
-[9.538692474365234, 7.031958103179932, "[TT] Resolution of the DPS = 2 - 5 km"]
-[7.422712326049805, 3.633592367172241, "[FF] Operation of the NightPOD = All Crew Members flying to the ISS"]
-[4.783902168273926, 0.60970139503479, "[TT] Operation Date of the Analog-1 = Late 2019"]
-[10.513710975646973, 5.4821696281433105, "[TT] Model Scale of the Juice = 1:18"]
-[6.158502101898193, 3.967782735824585, "[FF] Specifications of the GOES ReBroadcast (GBR) = Unknown"]
-[11.168163299560547, 0.5288130044937134, "[TT] Atmospheric Composition + Structure Observed of the Transiting Exoplanets = Transmission spectrum, emission spectrum, albedo, phase function, clouds, winds"]
-[6.901708126068115, 1.8598425388336182, "[FF] URL of the SOHO = http://www.nasa.gov/content/goddard/soho-captures-jan-14-2014-cme/#.Uz0sNaKegkA"]
-[10.2243013381958, 0.9531984329223633, "[FF] Gravitational Bound Companion of the TOI 451 = Located so far from TOI 451 that its light takes 27 days to get there"]
-[6.38367223739624, -0.49575409293174744, "[TT] Test Duration of the Myriad 2 = 36 straight hours"]
-[11.933755874633789, 4.495437145233154, "[TT] Platform Size of the Genesis spacecraft = 1.7 m diameter x 0.5 m height"]
-[6.203946113586426, 4.786175727844238, "[FF] Multi-Receiver of the GIOVE-M Sensor Station = Unknown"]
-[4.668787479400635, 6.567089080810547, "[TT] RF Communications of the Spacecraft = Up to 4 kbit/s"]
-[5.973400115966797, 4.565875053405762, "[FF] Operator of the Ground Station = ASI (Agenzia Spaziale Italiana)"]
-[7.059277534484863, 1.1855534315109253, "[TT] Launch Date of the Trace Gas Orbiter (TGO) = 2016"]
-[6.521914005279541, 3.1383848190307617, "[TT] Application of the AEISS = Cartography and disaster monitoring"]
-[4.92457389831543, 0.1828605681657791, "[TT] Launch Date of the STRV-1d = Nov. 16, 2000"]
-[6.762972831726074, -0.5723921656608582, "[TT] Expected Orbit Duration of the ChipSats = Merely a few days"]
-[3.5071864128112793, -0.950112521648407, "[TT] Orbit Type of the ALL-STAR-1 = Near-circular orbit"]
-[11.027782440185547, 3.9559695720672607, "[TT] Expected TID Level of the NEA Scout = Exceeding 20 krad (Si)"]
-[6.526921272277832, 3.636784315109253, "[FF] Funding of the SPOT-6 = Government funding or pre-sales agreements"]
-[6.12681770324707, 5.518095970153809, "[FF] FPGA Redundancy of the SMS = Triple Modular Redundant (TMR)"]
-[5.211564540863037, 0.45749619603157043, "[TT] Mission Conception Year of the DSX = 2003"]
-[5.40122127532959, 7.998855113983154, "[TT] Frequency Range of the VLF Experiment = 3-30 kHz"]
-[7.764118671417236, 2.84521484375, "[TT] Sensing Capability of the OLS = Capture city lights and distinguish lights from fires"]
-[6.502081394195557, 5.08070182800293, "[FF] Function of the Data Processing System = Process the raw data"]
-[5.326871395111084, 8.306602478027344, "[FF] Bandwidth of the Channel = <2500"]
-[5.0942301750183105, 4.402129650115967, "[FF] Number of Satellites of the Starlink = More than 500"]
-[5.231271743774414, 7.974793434143066, "[TT] Stiffness of the NAVANT = 145 Hz"]
-[7.039152145385742, 3.1482207775115967, "[FF] Update Frequency of the Maps = Weekly"]
-[9.819140434265137, 4.732600212097168, "[FF] Configuration of the FY-2F = Dual spin-stabilized spacecraft at 100 rpm with a despun antenna platform"]
-[9.088150978088379, 6.300957202911377, "[TT] Slew Rate of the TeLEOS-1 Imager = 2.5\u00ba/s"]
-[5.851180553436279, 3.2922184467315674, "[TT] Funding Requirement of the 90-satellite constellation = Another equity funding round, cash flow from operations and debt"]
-[13.908259391784668, 3.1169981956481934, "[TT] Payload Mass of the RemoveSat = ~40 kg"]
-[8.119731903076172, -0.36644065380096436, "[FF] Decline Rate of the Arctic sea ice cap = 13 percent each decade since 1979"]
-[4.433064937591553, 2.936204671859741, "[TT] Location of the DCT = Happy Jack, Arizona"]
-[5.14327335357666, 1.9310829639434814, "[TT] Mission Status of the CASSIOPE = Operational (extended)"]
-[4.6627888679504395, 7.116914749145508, "[TT] TT&C Uplink of the QSat = S-band, 1 kbit/s"]
-[5.811960220336914, -0.733296811580658, "[TT] Design Life of the DMSP Satellites = 3-5 years"]
-[11.868778228759766, 3.2936744689941406, "[TT] \u0394V Capability of the BIT-3 system = 2.9 km/s"]
-[10.705138206481934, 7.150387287139893, "[TT] Footprint of the 6 = 25.8 x 17.5 km"]
-[9.378571510314941, 6.244930267333984, "[TT] Incidence Angle Range of the Wide Fine Resolution Beams = 20 to 45\u00ba"]
-[7.973414897918701, -2.573326349258423, "[TT] Spectral Range of the GOLD = ~133\u2013165 nm"]
-[4.865584373474121, 2.164348840713501, "[TT] Operational Status of the MTSAT-2 = Operational"]
-[6.072404384613037, 6.108085632324219, "[TT] Operation Commands of the SSRNI = Yes"]
-[7.808980941772461, 6.8253912925720215, "[FF] Temporal Decorrelation of the Interferometric Mode = Within the requirements"]
-[4.084170818328857, 6.3234639167785645, "[FF] Radiation Pattern of the Antenna = Steerable with a gimbal capable of continuously pointing toward the ground station"]
-[5.297959327697754, 1.139298915863037, "[FF] Journal Publication Date of the C/NOFS = November 2004"]
-[11.612688064575195, 4.707825183868408, "[TT] Size of the S/C = Cube with 700 mm length of each side"]
-[4.242660999298096, 4.287909984588623, "[TT] Operational Year of the COSPAS-SARSAT system = 1985"]
-[3.2565557956695557, 5.6525750160217285, "[TT] Array Width of the ICEYE SAR Antenna = 3.2 m"]
-[6.291861057281494, 4.887660980224609, "[FF] Data Types of the GPS Receiver = Time, position, velocity, HDOP, GDOP"]
-[5.324189186096191, 0.7457184791564941, "[FF] Data Processing Chain Delivery Date of the Terma = March 7, 2008"]
-[6.4739251136779785, 4.245924949645996, "[FF] Data Products Distribution of the DSX = To PIs (Principal Investigators) and users at AFRL and the NASA/POCC"]
-[6.609612941741943, -0.04219364747405052, "[FF] Time Reference of the LEO missions = GNSS systems"]
-[9.907807350158691, 7.221025466918945, "[TT] Pixel Sizes of the Instrument = 10 km x 10 km"]
-[3.4908366203308105, -0.8294005393981934, "[TT] Constellation of the Strela-3/Rodnik = Strela"]
-[8.333404541015625, -0.04364047572016716, "[TT] Longitude Spacing of the TOPEX/Poseidon = 1.4\u00ba"]
-[9.028736114501953, 6.76483678817749, "[TT] Vertical Resolutions of the SciSat-1/ACE = One of the world\u2019s highest"]
-[4.388979434967041, 2.1385393142700195, "[TT] Renamed In Honor Of of the KhalifaSat = His Highness Sheikh Khalifa Bin Zayed Al Nahyan"]
-[10.200783729553223, 2.1071863174438477, "[TT] Integration Location of the eROSITA FM (Flight Model) telescope = MPE integration Lab"]
-[8.439512252807617, 6.008055210113525, "[TT] Accuracy of the UFF TLE = Less Accurate"]
-[6.7632060050964355, 5.106293201446533, "[FF] Subsystems of the SSM/I = Radiometers, digital data subsystem, mechanical scanning subsystem, and power subsystem"]
-[7.326958656311035, 7.864302158355713, "[TT] Dynamic Range of the Receiver = \u2264 15 dB"]
-[12.128254890441895, 3.0336647033691406, "[TT] Operational Life of the Propellant = 12 years"]
-[6.177045822143555, 2.9828484058380127, "[TT] Daily Imaging Capacity of the WorldView Legion = 5 million km2"]
-[7.4707417488098145, 4.849734306335449, "[FF] Diode Configuration of the SREM = Two of the three diodes are in-line and operate in `coincidence'"]
-[9.786134719848633, 2.678837537765503, "[FF] Services of the NanoRacks LLC = On-board and on-ground services to the general 'small payload' research community of the International Space Station (ISS)"]
-[8.270867347717285, 7.729969024658203, "[TT] Number of Detector Elements of the Detector Assemblies = 4"]
-[4.6641926765441895, 1.5585745573043823, "[TT] Launch Date and Time of the GHGSat-C2 (Hugo) = January 24, 2021, at 15:00 UTC"]
-[4.329939365386963, 0.7191388607025146, "[TT] Operation Commitment of the EDRS = Next 15 years"]
-[4.3833136558532715, 2.931724786758423, "[FF] Location of the Banks Island = Westernmost island of the Arctic Archipelago"]
-[11.776688575744629, 6.747379779815674, "[TT] Energy Range of the SXG = 0.03 - 100 keV"]
-[8.120368957519531, -0.39940372109413147, "[TT] Projected Growth of the Arctic vessel traffic = 250 percent by 2025"]
-[8.138084411621094, 7.187105655670166, "[TT] Technology of the Analog ASIC = 2 micron CMOS (Orbit) process"]
-[4.73886775970459, 8.008966445922852, "[TT] Signal Frequency of the Matrix Switch = 1.2 GHz or 720 MHz"]
-[6.772199630737305, -0.6371095776557922, "[TT] Orbit of the JPSS = Afternoon (13:30 hours)"]
-[5.5591583251953125, 6.719752788543701, "[TT] Data Delivered of the LRO = 325 TB"]
-[4.581186294555664, 5.133824825286865, "[FF] Objectives of the LUTs = Track COSPAS-SARSAT satellites, recover beacon signals from satellites, perform Doppler processing calculations to locate signal sources, and to relay Doppler solutions to an associated MCC"]
-[10.339668273925781, 7.9860405921936035, "[FF] Telescope Diameter of the Nano-JASMINE = 5cm"]
-[11.76340103149414, 6.6151123046875, "[TT] Energy Range of the HIT = ~2 to ~40 MeV/nuc"]
-[6.489268779754639, 0.04954397678375244, "[TT] Run Frequency of the EDOT = Once per day"]
-[3.2923362255096436, 5.0185017585754395, "[TT] Recording Medium of the SAR Data = Film"]
-[9.75772476196289, -0.8163504004478455, "[TT] Orbit Altitude of the PARASOL = 9.5 km under the A-train"]
-[8.690269470214844, 7.621365547180176, "[TT] CCD Device Resolution of the ASC = 752 x 588 pixel"]
-[9.994662284851074, 7.988418102264404, "[TT] Distance to Focal Plane of the M4 = 10 \u00b5m"]
-[12.107134819030762, 4.539848327636719, "[TT] Primary-Spacecraft Interfaces of the CubeStack = 98.5 cm \u00d8 and 61 cm \u00d8"]
-[8.93224048614502, 4.3484416007995605, "[TT] Function of the Sun Sensor = Provided yaw information"]
-[4.441769123077393, 7.941058158874512, "[TT] Return Link Frequency of the LPT = 2287.5 MHz"]
-[14.307378768920898, 3.0930724143981934, "[TT] Mass of the Weilai-1R = ~40 kg"]
-[10.172229766845703, 1.8529064655303955, "[TT] Number of All-Sky Maps of the eROSITA = 7"]
-[7.933520793914795, 9.147787094116211, "[TT] Wavelength of the Olivine = 2 \u00b5m"]
-[10.115243911743164, -1.4934582710266113, "[TT] Inclination of the Satellites = Mid-inclination"]
-[11.260964393615723, 5.859066486358643, "[TT] Main Structure Material of the UVNS = CFRP (Carbon Fiber Reinforced Polymer)"]
-[6.997039318084717, 3.409909248352051, "[FF] Goal of the EDC = Build and test designs for shields to minimize radiation exposure and damaging human health effects inside NASA's new Orion spacecraft"]
-[5.902493476867676, 5.7627363204956055, "[TT] Ground Coverage Area of the Corvus-BC = 150 million square Kilometres"]
-[9.697410583496094, 8.44265365600586, "[TT] FOV in Transverse Spin Plane of the THD = 6\u00ba"]
-[5.57034158706665, -1.9111565351486206, "[FF] COMS Follow-on Mission of the GEO-KOMPSAT-2 = Unknown"]
-[4.404873847961426, 0.6545792818069458, "[TT] In-Space Disintegration Date of the DMSP-F13 = February"]
-[2.615450382232666, 3.332859992980957, "[FF] Mass of the Flock-4v = Undisclosed"]
-[10.128511428833008, 1.5169882774353027, "[FF] Purpose of the Roman = Make similar measurements of stars in both the Milky Way and other galaxies"]
-[9.820243835449219, 0.399474561214447, "[TT] Satellite Connection Distance of the SpaceDataHighway = Up to 45,000 km"]
-[3.849759101867676, 1.288765549659729, "[TT] Landing Location of the Falcon 9's first stage = \"Just Read the Instructions\" droneship, which was stationed in the Pacific Ocean"]
-[10.684568405151367, 0.8641311526298523, "[FF] Roundness of the Kepler 11145123 = More round than the Sun"]
-[7.210169792175293, 6.892137050628662, "[FF] Background Measurement of the Metrology Laser = Make a background measurement 4 times a second"]
-[7.392503261566162, 3.7362794876098633, "[FF] Design of the NightPod = Combination of custom built parts and ISS compatible COTS items"]
-[9.573054313659668, 7.977712631225586, "[TT] Filter Diameter of the LWIR Camera = 15.5mm"]
-[10.972803115844727, 5.811549186706543, "[FF] Radiation Shielding of the Avionics Box = Graded-Z shield"]
-[7.683917999267578, 6.67239236831665, "[TT] Image Sequence Acquisition Time of the POLDER = 20 seconds"]
-[12.454737663269043, 0.5721705555915833, "[TT] Launch Year of the Plato = 2026"]
-[9.615017890930176, 0.13563154637813568, "[TT] Argument of perigee of the PROBA-3 = 188\u00ba"]
-[11.321800231933594, 5.838914394378662, "[TT] Structure Material of the CeREs = Aluminum"]
-[7.300594329833984, 3.7978832721710205, "[TT] Debris Quantity of the DMSP-F13 = Over 100 pieces"]
-[8.734867095947266, 2.0266990661621094, "[TT] Margin on Wind Direction of the E2E model = Minimum of 20%"]
-[7.953876972198486, 6.290872573852539, "[TT] Type of the MSU-GS = 10-channel radiometer"]
-[9.091529846191406, 1.3738056421279907, "[TT] Image Data Download Completion Date of the Voyager 1 = May 1, 1990"]
-[4.877140998840332, 4.268796443939209, "[FF] Access Method of the Argos = Pure (i.e. unslotted) ALOHA"]
-[8.383225440979004, 6.910887718200684, "[TT] Performance of the Imaging System = Satisfactory"]
-[4.380855083465576, 2.0009260177612305, "[FF] Calibration and Validation Date of the DubaiSat-2 = Early March 2014"]
-[3.8544158935546875, 4.412660121917725, "[TT] Initial Image Acquisition of the RADARSAT-2 = Dec. 18, 2007"]
-[9.346935272216797, -0.764276921749115, "[TT] Quantity of the GEOS-3 = 1"]
-[6.20442533493042, 8.135527610778809, "[TT] Channels of the MWRI-RM = 26"]
-[13.367396354675293, 7.729181289672852, "[TT] Downlink RF Output Power of the RF Communication System = 1 W"]
-[5.416689395904541, 2.6843247413635254, "[TT] Control Facility of the INSAT-3D = ISRO's MCF (Master Control Facility) at Hassan in Karnataka"]
-[11.633549690246582, 3.397135019302368, "[TT] Number of Micronozzles of the CGMS = 8"]
-[9.831833839416504, -0.35287660360336304, "[TT] Altitude of the PAZ = 514 km"]
-[10.49172592163086, 1.2805514335632324, "[TT] Pulsation Patterns of the HD 31901 = 55"]
-[7.131812572479248, 7.8998894691467285, "[FF] Noise Levels of the SOFIE = At or below laboratory values"]
-[8.718585968017578, 7.559951305389404, "[TT] Detector Size of the DIAL Instrument = 200 \u00b5m"]
-[3.9169015884399414, 4.517974853515625, "[FF] Ground Processed Orbit Determination Accuracy Improvement of the RADARSAT-2 = Significant ground processed orbit determination accuracy improvement"]
-[9.271949768066406, 6.211404323577881, "[TT] Observation Direction Angles of the MISR = Nadir, \u00b126.1\u00ba, \u00b145.6\u00ba, \u00b160.0\u00b0 and \u00b170.5\u00ba forward and backward of the local vertical"]
-[9.620552062988281, 8.299126625061035, "[TT] Tracking of the FPM = \u00b120 \u00b5radians"]
-[8.585783004760742, 5.56559944152832, "[TT] Radiometric Accuracy of the Satellite = 0.47 - 0.55 dB pp"]
-[4.929941177368164, 1.7948633432388306, "[FF] Sensor Complement of the Gokturk-2 = EOS-C (Earth Observation Satellite - Camera)"]
-[10.542842864990234, 1.9769165515899658, "[FF] Unknown of the X-ray Pulsars = Unknown"]
-[7.256385803222656, 4.0599236488342285, "[FF] Safety Requirements of the AMS-02 = Less stringent"]
-[7.18223237991333, 2.522925615310669, "[FF] Author of the Observation of the Earth and Its Environment: Survey of Missions and Sensors = Herbert J. Kramer"]
-[7.930734157562256, -2.557870388031006, "[TT] 135.6 nm Emission Production Mechanism of the GOLD = Photoelectron impact on O"]
-[9.67171859741211, -0.303396999835968, "[TT] Altitude of the SARAL/AltiKa = 800 km"]
-[8.38880443572998, 5.544102668762207, "[FF] Geolocation Accuracy of the PROBA-V Mission = RMSE accuracy <50 m"]
-[5.538447856903076, 0.4067398011684418, "[TT] Launch Date of the Flock 1 = December/January"]
-[14.206785202026367, 3.2122175693511963, "[TT] Mass of the CNUSail-1 = 4 kg"]
-[10.372851371765137, 5.75115442276001, "[TT] Maximum Temperature Differential of the PC5 = 85 \u00b0C"]
-[4.922939300537109, 0.2828825116157532, "[FF] Operational Role Transition Time of the GOES-T = Two weeks"]
-[5.315942287445068, 2.3075780868530273, "[FF] Type of the Cesium Mission 1 = On-orbit testbed"]
-[12.453313827514648, 0.6383687853813171, "[TT] Total Spacecraft Image Resolution of the Plato Camera = 2.11 gigapixels"]
-[8.042323112487793, 5.023435592651367, "[FF] Required Precision of the H2CO = 10.0"]
-[7.923620700836182, 5.142485618591309, "[FF] Calibration Procedure of the FLLS = Calibrated separately"]
-[5.354737758636475, 8.538896560668945, "[TT] Filter Bandwidth of the OTD = 8.4\u00c5"]
-[10.136459350585938, -1.343032956123352, "[TT] Orbit Inclination of the MightySat I = 51.6\u00ba"]
-[6.24049711227417, 5.47701358795166, "[FF] Operations Workflow of the Optical Inter-Satellite Links (OISL) = Joint concept for the ASA-S1A Optical Inter-Satellite Links operations, based on the two missions\u2019 planning cycle and operations execution scenario"]
-[5.0267133712768555, 0.5704892873764038, "[FF] Forum Date of the NEC Space Business = December 12, 2010"]
-[7.864691734313965, 4.189508438110352, "[FF] Heat Production of the XO-3b = Unknown"]
-[7.163439750671387, 8.382226943969727, "[TT] Number of Filter Windows of the Filter Wheel = 18"]
-[6.2267985343933105, -1.1136809587478638, "[TT] Minimum Mission Life of the GRACE Follow-On = 5 years"]
-[10.53761100769043, 2.208181142807007, "[FF] Typical Short Outburst Duration of the X-ray Source = Unknown"]
-[7.026090621948242, -0.7226099371910095, "[TT] Orbital Period of the Kepler-438b = 35.2 days"]
-[5.6754255294799805, 0.797747015953064, "[TT] Acquisition Date of the Figure 33 = March 5, 2018"]
-[11.902351379394531, 3.263341188430786, "[TT] Thrust of the DMC Propulsion Subsystem = 50 mN"]
-[10.368392944335938, 5.860351085662842, "[TT] Operating Temperature of the WFS&C = < 45 K"]
-[8.872556686401367, 4.793352127075195, "[FF] Control Requirement of the MGT = Satellite pointing requires knowing the orbit position"]
-[7.081118106842041, 3.7098464965820312, "[FF] Presentation Date of the Proba-3 Formation Flying System = 1-5 October 2018"]
-[6.068864345550537, -1.9653462171554565, "[TT] Member of the Liz Ritchie = True"]
-[12.441180229187012, 0.5626720190048218, "[TT] Launch Date of the SOCRATES = May 24, 2014"]
-[8.7119140625, 2.147275924682617, "[FF] Altitude Range of the Water Vapor VMR = 50 - 110 km"]
-[3.2015039920806885, 5.108561992645264, "[TT] Antenna Beamwidth (Azimuth) of the Seasat SAR sensor = 1\u00ba"]
-[9.710531234741211, 7.191155910491943, "[TT] Resolution Cell, Horizontal of the Instrument = 16 km"]
-[4.023906230926514, 4.3056793212890625, "[FF] Mission Management of the RADARSAT-2 = Unknown"]
-[8.910914421081543, 6.787714004516602, "[TT] Image Rectification Performance of the Meteosat-8 = Met with significant margins"]
-[14.227734565734863, 3.1464550495147705, "[TT] Mass of the S/C = 764 kg (including fuel)"]
-[10.340786933898926, 7.236913204193115, "[FF] Primary Mirror Size of the Telescope System = Larger than 40 cm"]
-[8.388344764709473, 3.5675063133239746, "[FF] Source of Signal Error of the GPS = Ionospheric effects"]
-[8.060708045959473, 4.980145454406738, "[FF] Design Hypothesis of the Geometric Calibration System = Thermoelastic distortions change slowly, smoothly and not a lot"]
-[7.271223068237305, 1.6917393207550049, "[FF] Primary Contribution of the Orbital Astronomical Observatories = Enable humanity to explore beyond our frontier of knowledge"]
-[9.383874893188477, 7.000846862792969, "[TT] Spatial Resolution of the MS = 5 m"]
-[9.124706268310547, 7.370708465576172, "[TT] Resolution of the True Color Composite Image = 250 m"]
-[6.769565582275391, 4.143380641937256, "[FF] Design and Pre-Flight Characterization of the TRUTHS = Will be optimized to fully utilize the benefits"]
-[9.873374938964844, -1.0882762670516968, "[TT] Orbit of the SkySat-16 to -18 = Sun-synchronous circular orbit with an altitude of 575 km, inclination of ~98\u00ba, LTDN (Local Time of Descending Node) of 10:30 hours"]
-[5.624339580535889, 5.778469085693359, "[TT] CMD Schedule Resolution of the C&DH module = 1 s"]
-[9.683103561401367, -1.121423363685608, "[TT] Orbit Longitude of the FY-4B = 123.5\u00ba E"]
-[1.6146271228790283, 3.7641093730926514, "[TT] S-band transmitter of the BEESAT-3 = Yes"]
-[9.581321716308594, 7.007009506225586, "[TT] Spatial Resolution of the Jason and Envisat = 70 - 80 km"]
-[11.889327049255371, 5.419989109039307, "[TT] Size of the Instrument = 45 cm x 35 cm x 30 cm"]
-[3.3508992195129395, 5.301336765289307, "[TT] Signal Wavelength of the S-band SAR = About 4 inches (10 cm)"]
-[11.974918365478516, 6.5421929359436035, "[TT] Energy Range of the Positron spectrum = 1 GeV to 350 GeV"]
-[5.554046154022217, 5.163328647613525, "[TT] Operating System of the OBC = VxWorks RTOS"]
-[10.14827823638916, -2.765467405319214, "[TT] Data Bus Width of the SLC NAND-Flash = 8 bit"]
-[9.498488426208496, 7.044519901275635, "[FF] Angular Resolution of the XRT = Improved"]
-[7.0042219161987305, 3.2119219303131104, "[FF] Purpose of the MANTIS = Monitor climate change, map the environment, forecast the weather, find new resources"]
-[6.492952346801758, 0.022249354049563408, "[TT] Update Frequency of the INR = Daily"]
-[12.044429779052734, 6.2770676612854, "[FF] Flux of Iron Nuclei of the AMS = Identical to the fluxes of the light primary helium, carbon and oxygen cosmic rays"]
-[11.923168182373047, 4.965977668762207, "[TT] Device Size of the TCU/TRC = 380 mm x 60 mm x 90 mm, 173 mm x 18.5 mm x 81 mm"]
-[9.443868637084961, 3.5884695053100586, "[FF] Potential Adjustment of the Magnetic Field Models = Send the pole back to Canada"]
-[10.416790008544922, 2.336538076400757, "[TT] Energy Range of the X-ray Imager = 0.1\u20132 keV"]
-[8.279427528381348, 1.2834045886993408, "[TT] 48-hour Total Precipitation of the Mount Tamalpais = 16.55 inches"]
-[4.974880695343018, 0.37008631229400635, "[TT] Launch Date of the Electron = 17 October, 2019"]
-[5.491452693939209, 0.41701656579971313, "[TT] Launch Date of the Cluster 3 = 2022"]
-[9.313214302062988, 7.609215259552002, "[TT] Time Resolution of the MTEL Space Telescope = 1,000 times better than CCD cameras"]
-[4.931619167327881, -0.9577051997184753, "[FF] Mission Duration of the FengYun-4 series = 17 years"]
-[6.7492876052856445, 7.544055461883545, "[TT] Beam width of the UHF = 3.6 rad"]
-[2.607135772705078, 3.336357831954956, "[TT] Quantity of the Flock-4v = 14"]
-[4.6287126541137695, 4.869715213775635, "[FF] Message Types of the AIS = Position reports and short messages with information about the ship and the voyage"]
-[7.152922630310059, 2.9032816886901855, "[TT] Ground Control Center Budget of the MethaneSAT = $16 million"]
-[9.83967399597168, 4.737466335296631, "[TT] Spin Rate of the Spacecraft = 3 rpm"]
-[8.769610404968262, 1.6014599800109863, "[TT] Mid-course correction burn duration of the Webb = 65 minutes"]
-[8.036430358886719, 5.808230400085449, "[TT] Vertical Resolution of the JPL Microwave Radiometer = 240 m"]
-[5.135477066040039, 0.03586520254611969, "[TT] Agency of the STRV-1a and -1b = UK (Dstl)"]
-[6.206503868103027, 1.8264167308807373, "[TT] Origin of the Sample Return Capsule = NASA Stardust mission"]
-[10.854133605957031, -0.2936110198497772, "[TT] Pursuit Monostatic Phase of the TanDEM-X = Sept. 20, 2014, to the end of March 2015"]
-[4.730352401733398, 0.5194129347801208, "[TT] Launch Date of the GOES-T = December 2021"]
-[9.876546859741211, 8.00765323638916, "[TT] MTF Value of the Telescope = > 0.3"]
-[6.759025573730469, 1.8592907190322876, "[FF] URL of the WIND = http://wind.nasa.gov/"]
-[3.6049561500549316, 2.6694114208221436, "[TT] Total Number in Space of the Iridium NEXT = 55"]
-[5.2809319496154785, 1.3769739866256714, "[FF] Conference Presentation Date of the SMAP Mission = May 4-8, 2009"]
-[8.684962272644043, 7.78917932510376, "[TT] Number of Pixels of the Optics and detector assembly = 900"]
-[11.657404899597168, 4.379150390625, "[TT] Payload Fairing Diameter of the GSLV-F05 = 3.4 m"]
-[8.677523612976074, 5.778893947601318, "[TT] Target Signature Error of the ILRS = 1 mm"]
-[6.057252407073975, 5.550722599029541, "[TT] Redundancy Support of the DPU = Full duplication of DPU hardware"]
-[8.267362594604492, 7.56369686126709, "[TT] Type of the Detector = CdTe Schottky Diode double sided strip (ACRORAD)"]
-[9.888906478881836, 4.730161190032959, "[TT] Spin Rate of the MVIRI = 100 rpm"]
-[14.193960189819336, 3.252830743789673, "[TT] Mass of the CID = 180 g"]
-[7.064341068267822, 6.743869781494141, "[FF] Presentation Date of the Laser Frequency Stabilization = June 21-23, 2010"]
-[3.9481024742126465, 9.703145980834961, "[TT] Frequency (GHz) of the ICI-2 = 183.31\u00b13.4"]
-[4.800820827484131, 6.792165279388428, "[FF] Downlink Transmission of the X-band telemetry subassembly = Stored image data"]
-[6.852261543273926, -0.4355672597885132, "[TT] Cycle of the Solar Maximum = 11 years"]
-[7.93903923034668, 1.7867169380187988, "[FF] Mission Objective of the GOCE = Obtain measurements with high spatial resolution and high accuracy to deduce global and regional models of the Earth's gravity field and geoid with unprecedented precision"]
-[13.904292106628418, 7.183714389801025, "[TT] Output Current of the Buck-Boost Converter = 0 - 8 A"]
-[5.468804836273193, 7.76037073135376, "[TT] Power of the EIRP per channel = > 51 dBW"]
-[8.636784553527832, 6.961556434631348, "[FF] Compensation Methods of the TDI imaging technology = Ground-based input of horizontal frequency data and altimetry data supplementary on board"]
-[4.764741897583008, 3.0116324424743652, "[TT] Location of the MC3 CGA = AFIT (Air Force Institute of Technology), located on Wright-Patterson AFB, Ohio"]
-[3.3427932262420654, 5.116607189178467, "[TT] SAR Payload Polarization of the RCM = Hybrid polarimetry"]
-[5.156604290008545, 7.018270015716553, "[TT] Uplink Speed of the ColKa = Up to 2 Mbit/s"]
-[10.558313369750977, 2.4880447387695312, "[TT] Mirror Shell Thickness of the VNIIEF X-ray module = 250 \u00b5m"]
-[5.0779900550842285, -0.3520362675189972, "[TT] Launch Date of the CBERS-1 = Oct. 14, 1999"]
-[9.419260025024414, -1.1401722431182861, "[TT] Orbit Position of the BeiDou-1C = GEO, 110.5\u00ba E"]
-[6.753169536590576, 5.860948085784912, "[TT] Quantity of the Tx/Rx = 2"]
-[10.41309642791748, 2.1722583770751953, "[TT] Mirror Shells of the eROSITA X-ray telescope = 54"]
-[3.7629947662353516, 4.652047157287598, "[TT] Detection Area of the RADARSAT-2 = 0.5 hectares"]
-[8.293560981750488, 0.13524864614009857, "[FF] Operation of the Meteor-M-2 = Global observations of the Earth\u2019s surface and atmosphere"]
-[5.476552486419678, 5.172603607177734, "[TT] Function of the GAMALINK = Receives and decodes GPS signals"]
-[5.370142936706543, 8.131752014160156, "[TT] Measurement Frequency of the MSC = 2 Hz up to 1 kHz"]
-[9.152327537536621, 4.339394569396973, "[TT] Manufacturer of the Magnetometer = Honeywell"]
-[5.51873779296875, 6.714047431945801, "[TT] Raw Data Size of the QuakeSat = 500 MB"]
-[11.363534927368164, 5.852118015289307, "[FF] Material of the Central Housing = Aluminum"]
-[7.361104965209961, 0.2711378335952759, "[TT] Sample Site Selection Board Chair of the OSIRIS-REx = Heather Enos"]
-[9.400341987609863, 7.065713882446289, "[TT] Spatial Resolution of the SMI = 80 m"]
-[14.035035133361816, 7.157673358917236, "[TT] Output Voltage of the Charge Regulator = Unregulated 14 V"]
-[6.178576946258545, 4.65921688079834, "[FF] User Request of the DPE = Via the Data Delivery subscription service"]
-[8.706250190734863, 7.761353969573975, "[TT] Detector Size of the Short Wavelength Band = 2.5 cm x 2.5 cm"]
-[10.972938537597656, 4.551297664642334, "[TT] Drill Depth of the Rosalind Franklin rover = 2 m underground"]
-[8.21827220916748, 1.2971763610839844, "[TT] Status of the Oceanic Ni\u00f1o Index (ONI) = Dropped below normal in May"]
-[9.839920043945312, 7.394312381744385, "[TT] GSD (Ground Sample Distance) of the ALOS-3/PRISM-2 = 0.8 m"]
-[5.751007556915283, 1.1319199800491333, "[FF] Journal Publication Date of the GPS/MET = 1997"]
-[4.567203998565674, -0.31653541326522827, "[FF] Arrival Date of the Docking Module = 26 November 2021"]
-[10.57309627532959, 3.3936057090759277, "[FF] Objective of the EFILE = Study the thermocapillary effect at the liquid-gas phase-change interface on evaporation in the space environment"]
-[8.758695602416992, 4.815126419067383, "[TT] Size of the Star Tracker = 59 x 56 x 31.5 mm"]
-[8.715417861938477, 7.639015197753906, "[TT] Pixel Size of the Detector = 24 \u03bcm x 24 \u03bcm"]
-[5.325195789337158, 3.948287010192871, "[TT] Number of Satellites per Orbital Plane of the T1TL Prototype Constellation = 21"]
-[7.0500335693359375, 7.119316101074219, "[TT] Pulse Width of the Laser = < 1.5 ns"]
-[9.661062240600586, -0.3738657534122467, "[TT] Altitude of the ADEOS-II = 802.9 km"]
-[7.267283916473389, -0.2366710901260376, "[TT] Number of Orbits Available for UV Measurements of the Tatiana-1 = 3-5"]
-[9.724397659301758, 7.97104549407959, "[FF] Lens Configuration of the WISPR = Split into two separate imaging assemblies"]
-[6.573183536529541, 5.020913124084473, "[FF] Function of the IEU = Receives detector data, formats it and passes it on to the spacecraft data-handling system. It also provides regulated power to all the subsystems, thermal control of the IOU, command and data interfaces and instrument health monitoring and control"]
-[6.161262035369873, 3.1292216777801514, "[FF] Contract with National Reconnaissance Office (NRO) of the BlackSky = Extended"]
-[7.874782562255859, 3.6687023639678955, "[FF] Sensor Complement of the Meteor-3M-2 = MTVZA, MSU-MR (2 instruments), MSU-SR (2 instruments), IKFS-2, MSGI-MKA, KGS-4S, DCS, RRA, SAGE-III"]
-[11.978655815124512, 3.6759870052337646, "[TT] Pressure of the Crew Module Cabin = Maintained"]
-[9.348806381225586, 5.33022403717041, "[TT] Angular Velocity Range of the IRU = 10\u00ba/s to 0.5\u00ba/s"]
-[11.416109085083008, 3.338623046875, "[TT] Method to Counteract External Perturbations of the MicroSCOPE = Micro propulsion system"]
-[6.557918548583984, 4.11289119720459, "[FF] Components of the EPS = Space segment and full ground segment"]
-[11.762585639953613, 6.721841335296631, "[TT] Energy of the TWINS = 10 keV"]
-[8.19954776763916, 7.962749004364014, "[TT] Number of Elements of the VIS and SWIR detectors = 16"]
-[5.853669166564941, 0.9407647848129272, "[FF] Accident Investigation of the Columbia = Help from many other institutions"]
-[11.296258926391602, 3.5147697925567627, "[FF] Formation Control of the OSC = High accuracy actuation using cold gas milli-Newton thrusters"]
-[11.185243606567383, 0.6185932159423828, "[FF] Science Goals of the CHEOPS = Study the structure of exoplanets with radii typically ranging from 1 to 6 Earth radii"]
-[6.8679585456848145, 8.758830070495605, "[TT] Polarization Measurement of the WUPPE = Function of wavelength"]
-[5.091905117034912, 8.32597827911377, "[TT] Frequency Bandwidth of the Frequency bandwidth = < 275 MHz"]
-[10.18472671508789, 9.388205528259277, "[TT] Nominal IGFOV of the Band 7 = 2 km"]
-[5.862582206726074, 5.0336408615112305, "[FF] Experiment of the ISL Tracking Antenna = Bidirectional TM/TC data relay to a LEO satellite"]
-[4.021208763122559, 6.800493240356445, "[FF] Antenna Type of the X-band JPL Iris Radio = Dual patch antennas"]
-[4.525588035583496, 8.103174209594727, "[TT] Ka-band Radar Frequency of the Tomorrow-R1 and -R2 = 35.75 GHz"]
-[9.352489471435547, 7.081022262573242, "[TT] Spatial Resolution of the CZI = 50 m"]
-[6.2071123123168945, 8.027475357055664, "[TT] Redundancy of the Ka-band Channels = 1 standby channel (4 for 3 redundancy)"]
-[8.24073600769043, 5.020442008972168, "[FF] Step 2 Operation of the TRUTHS = HIS (Earth Radiance view) calibrated against the TR at each LD wavelength"]
-[4.508541584014893, -0.8740402460098267, "[TT] Arrival Date of the SpaceX Dragon CRS-14 = April 4, 2018"]
-[8.96273422241211, 4.42752742767334, "[TT] Sensor Suites of the ADCS = Four sun sensor suites and five two-axis magnetic sensors"]
-[4.844611167907715, 7.746697902679443, "[TT] Stiffness of the Antenna = > 40 Hz (during launch in longitudinal direction)"]
-[3.84773588180542, 4.610896110534668, "[TT] Noise Levels of the RADARSAT-2 = Stable and consistent with reported levels"]
-[4.972537040710449, 3.152066707611084, "[TT] Manufacturer of the Trisat-R = University of Maribor in Slovenia with SkyLabs"]
-[10.329811096191406, 5.403000354766846, "[TT] Control Type of the TCS (Thermal Control Subsystem) = Passive control with heaters"]
-[4.507051944732666, -0.9001585245132446, "[FF] Launch Date of the Dragon = 3 April 2018"]
-[7.360349178314209, 1.5493084192276, "[FF] Lead Author of the Kepler space telescope = Steve Bryson"]
-[9.344283103942871, 4.542871475219727, "[TT] Proportional Control of the ADCS = Magnetic field value or sun vector error"]
-[1.9479666948318481, -0.39556780457496643, "[FF] Revolutionize View Date of the Van Allen Probes = Jan. 19, 2016"]
-[11.370475769042969, 5.838228702545166, "[TT] Structure Material of the Bus = Graphite"]
-[13.794285774230957, 3.0223472118377686, "[TT] Mass of the IR Payload = 35 kg"]
-[9.689675331115723, 8.274153709411621, "[TT] Field of View of the POLDER = \u00b143\u00ba along-track"]
-[6.550609588623047, 2.883174419403076, "[FF] Presentation Date of the Small Satellite Constellation for Environment and Disaster Monitoring and Forecasting = Sept. 14-16, 2009"]
-[5.185725212097168, 1.9178266525268555, "[TT] Mission Status of the IMAGE = Cancelled"]
-[4.778180122375488, 0.41127341985702515, "[TT] Launch Date of the Claire = February 2018"]
-[8.70317554473877, 2.024479866027832, "[TT] Wind Direction of the NSCAT = 20\u00ba (rms), 3 - 30 m/s"]
-[8.518698692321777, 2.085841417312622, "[TT] Objective of the SeaWinds = To acquire accurate, high-resolution, global measurements of sea-surface wind vectors in 1 to 2-day repeat cycles"]
-[12.011399269104004, 6.3177595138549805, "[FF] Proton Flux of the AMS = Characteristically different from all the existing experimental results"]
-[4.263538360595703, 2.2236430644989014, "[TT] Launch Site of the SEEDS-2 = SDSC (Satish Dhawan Space Centre), the SHAR launch range (Sriharikota, India)"]
-[6.195948600769043, 4.294459342956543, "[FF] Mission Scope of the OSAM-1 = Refuel a satellite in space, assemble a communications antenna, and manufacture a beam"]
-[4.353709697723389, 7.181009292602539, "[TT] Communication Band of the SPOT-6 & SPOT-7 = S-band"]
-[6.232680797576904, 8.600666999816895, "[TT] Polarization of the AMSR = Dual"]
-[7.917063236236572, 8.0010404586792, "[FF] Instruments of the MTG-S = Infrared Sounder (IRS) and the UV-visible- near infrared imaging spectrometer (UVN)"]
-[6.952308654785156, 1.0029065608978271, "[TT] Landing Date of the Mars 2020 rover = February 2021"]
-[10.191234588623047, 7.513003349304199, "[TT] Configuration of the AstroFein RW-1 = Tetrahedron"]
-[4.697158336639404, 4.140288829803467, "[TT] Auxiliary Payload of the NorSat-3 = Navigation Radar Detector (NRD)"]
-[7.482170581817627, 3.687063455581665, "[FF] Purpose of the NightPod = Take pictures of adjacent areas on the surface"]
-[3.9853758811950684, 6.242404937744141, "[TT] Gain Pattern of the NanoCom Ant430 = Omnidirectional"]
-[5.154575824737549, 2.6960301399230957, "[TT] Sponsor of the Diwata-1 = Philippine government"]
-[9.06076717376709, 2.4570868015289307, "[FF] Purpose of the Athena = Study the hot and energetic Universe"]
-[6.616687774658203, -0.4537864327430725, "[TT] Repeat Cycle of the PanMUX = 52 days"]
-[9.292191505432129, 6.139347076416016, "[TT] Scan Range of the LCS = \u00b13\u00ba"]
-[11.656730651855469, 6.561141490936279, "[TT] Energy Range of the Chandra = 1 to 7 keV"]
-[8.15421199798584, 8.843097686767578, "[TT] Wavelength Range of the Ultraviolet Spectrograph = 132 to 162 nm"]
-[8.413129806518555, 5.793159484863281, "[TT] Positioning Precision of the GAMALINK = 5 m"]
-[5.534005165100098, 0.4027515947818756, "[TT] Operation End Date of the Cluster = December 2014"]
-[8.110353469848633, -0.3706079423427582, "[FF] Next \"Precipitous Drop\" Benchmark of the Arctic Sea Ice = 3 million km2"]
-[8.005936622619629, 5.593115329742432, "[FF] Intersatellite Distance Measurement of the GRACE-FO = Two-way microwave link"]
-[11.126687049865723, 1.0873218774795532, "[TT] Development of the Laser Systems = Pre-developed by ESA, NASA and the LISA consortium of ESA member states"]
-[7.849335193634033, 7.164491653442383, "[TT] Sweep Duration of the FTS Interferometer = 2, 1, 0.5, 0.1 s"]
-[14.638175010681152, 6.644010066986084, "[TT] Battery Capacity of the Block 5D-2 = 25.5 A hr"]
-[10.22247314453125, 7.078583240509033, "[FF] Focusing Method of the Telescope System = Adjustment of distance between the primary mirror and secondary mirrors"]
-[2.0417819023132324, -0.3186395466327667, "[TT] Radiation Belts Crossing of the PROBA-3 = Yes"]
-[4.946434020996094, 3.363736152648926, "[TT] Manufacturer of the ALTIUS = QinetiQ Space"]
-[8.328856468200684, 8.188936233520508, "[TT] Radiometric Accuracy of the IRFS-2 = 0.5 K"]
-[9.734357833862305, 7.087183475494385, "[TT] Spatial Resolution of the SASS = 50 km"]
-[7.625171184539795, 8.026463508605957, "[TT] Sensitivity of the IMI = 0.1-0.2 K"]
-[6.281409740447998, 8.514394760131836, "[TT] Polarimetric Channels of the MWI = 3rd and 4th Stokes"]
-[5.609947204589844, 6.041171550750732, "[TT] Memory of the AIM = 4 M x 16 Flash for storage of multiple Xilinx configurations"]
-[13.321821212768555, 7.614782810211182, "[TT] Transmit Power of the User Terminal = <3 W"]
-[5.339146614074707, 1.3322829008102417, "[TT] Observation Date of the ALOS-2 = 24 December 2018"]
-[7.854781627655029, 6.236400604248047, "[FF] Measurement Accuracy of the ATLAS = Within a billionth of a second"]
-[6.606202125549316, 5.24856424331665, "[FF] Architecture of the NRD Electronics = Multi-board with specific functions"]
-[9.749659538269043, -0.4813153147697449, "[TT] Altitude of the Corvus-BC 4 = 584.8 km"]
-[7.021306991577148, 5.836640357971191, "[TT] Clocks of the QZS-1 = Two rubidium atomic clocks"]
-[4.206599235534668, 2.564910888671875, "[TT] Launch Location of the ShadowCam = Cape Canaveral"]
-[10.107657432556152, -1.4734795093536377, "[TT] Orbit Inclination of the SEOSat = 98\u00b0"]
-[9.705897331237793, 8.446464538574219, "[TT] FOV (Field of View) of the Instrument = 80\u00ba x 80\u00ba"]
-[13.86040210723877, 3.1027655601501465, "[TT] Total Mass of the IPS (Integrated Payload Stack) = 3700 kg"]
-[11.018529891967773, 2.892543315887451, "[TT] Structure Size of the PARASOL microsatellite = 60 cm x 60 cm x 80 cm"]
-[4.151823043823242, 4.846625804901123, "[TT] Pointing Accuracy of the Alphasat TDP1 and Sentinel-1A = Better than 500 \u00b5rad"]
-[6.066232681274414, -1.957983136177063, "[TT] Member of the Peter Cornillon = True"]
-[5.23230504989624, 0.0439356304705143, "[TT] Berthing Date of the Cygnus = November 19, 2018"]
-[7.093274116516113, 3.4684865474700928, "[FF] Data Importance of the ALT = Far more interesting scientifically"]
-[9.90273666381836, 7.304523944854736, "[TT] Diameter of the Sampling Sites = 25 m"]
-[5.243836879730225, 6.980039119720459, "[TT] Downlink Data Rate of the ERBS = 128 kbit/s"]
-[5.173904895782471, 0.5942022204399109, "[TT] International Headquarters Establishment Date of the Spacety = 2019"]
-[9.31444263458252, 4.982594013214111, "[FF] Sensitivity to Multipath of the FFRF Sensor = May lead to initial range biases up to 1 m and bearing bias variations in the 0.5\u00b0 range for 30\u00b0 attitude changes"]
-[7.120481491088867, 3.9498419761657715, "[FF] Activation of the He-repressurization system = Shortly after the LOI maneuver is completed"]
-[7.0438408851623535, 3.4471609592437744, "[TT] Principal Investigator of the PROBA-3 = Andrei Zhukov"]
-[8.403141975402832, 4.160912990570068, "[FF] Calibration Method of the OVIRS = Using NIST traceable calibrated blackbodies and flood sources"]
-[8.98118782043457, -0.7347912192344666, "[TT] Orbit Capability of the Spacecraft = LEO, MEO"]
-[7.657656669616699, 1.9543379545211792, "[FF] Toxin Production of the Blue-Green Algae = Can produce toxins that can make you or your pets sick if swallowed or possibly cause skin and/or eye irritation due to contact"]
-[8.310134887695312, -0.4824059307575226, "[TT] Extent of the Ice Maximum = 14.77 million km2 (5.70 million square miles)"]
-[14.235722541809082, 3.19126558303833, "[TT] Mass of the PicPot = 3 kg"]
-[10.854990005493164, 4.014273166656494, "[TT] Inflatable Mast Extension of the Dragsail = 1m"]
-[5.235836505889893, 1.2774317264556885, "[FF] Conference Date of the LCROSS = April 25-30, 2010"]
-[9.60678768157959, 7.142359733581543, "[TT] Spatial Resolution of the Instrument = 13.5 km horizontal at nadir for IR bands"]
-[6.826337814331055, 7.181374549865723, "[TT] Beam Widening Factor of the BE = More than four times"]
-[4.962693691253662, 3.5814716815948486, "[TT] Manufacturer of the IBIS5-B-1300 = Cypress"]
-[9.37490463256836, 7.352416515350342, "[TT] Spatial Resolution of the AVNIR = ~16 m"]
-[12.062858581542969, 2.0681955814361572, "[TT] Antenna of the CartoSat-2 = Dual-gimballed antenna"]
-[7.740688323974609, 2.301830768585205, "[FF] Data Collection of the Radar Altimeters = Monitor ocean surface topography"]
-[7.554281711578369, 1.9093002080917358, "[FF] Unknown of the Argo = Argo Begins Systematic Global Probing of the Upper Oceans"]
-[6.0428547859191895, 2.5282158851623535, "[TT] Developer of the ROLO = USGS (United States Geological Survey)"]
-[11.148554801940918, 4.196835994720459, "[TT] Design Standard of the Mechanical Chassis = NanoRacks 6U deployer ICD"]
-[4.890904426574707, 3.326636791229248, "[TT] Manufacturer of the OBI = EADS Astrium"]
-[7.57072639465332, 8.839642524719238, "[TT] Spectral Band of the MSGI-5EI = 0.1 keV-90 MeV"]
-[5.526900291442871, -1.8694040775299072, "[FF] Observation Date of the KOMPSAT-3 = Fall of 2012"]
-[3.4391963481903076, -0.8866209983825684, "[TT] Orbit Type of the WorldView-3 = Sun-synchronous orbit"]
-[9.106764793395996, 7.439692497253418, "[TT] Image Resolution of the SCAMP Camera = 640 x 480 pixels"]
-[5.50004768371582, 7.119167327880859, "[TT] Data Rate Requirement of the LCT = 600 Mbit/s"]
-[10.73670482635498, 1.522666335105896, "[FF] Size of the Neutron Star = About the size of a large city"]
-[9.804903030395508, -0.6460637450218201, "[TT] Orbit Altitude of the ResourceSat-1 = 817 km"]
-[3.6067988872528076, 5.457362174987793, "[TT] Pulse Length of the Radar = 15 \u00b5s"]
-[9.075748443603516, 5.609413146972656, "[TT] Fine Pointing Performance of the AOCS = Fully achieved in the Science Observation Mode"]
-[4.882930755615234, 3.3275628089904785, "[TT] Ownership of the TecSAR = Government owned"]
-[4.858783721923828, 0.6106370687484741, "[TT] Launch Date of the GPIM = 25 June 2019"]
-[13.802303314208984, 2.992748260498047, "[TT] Payload Mass of the Meteor-M = ~1,250 kg"]
-[3.3492860794067383, 6.469113826751709, "[TT] Antenna Diameter of the SAS = 1 m"]
-[8.876639366149902, 9.343594551086426, "[TT] Operation Mode of the TANSO-CAI-2 = Nominal"]
-[7.330794811248779, 0.25724872946739197, "[TT] Sample Collection Attempt Date of the OSIRIS-REx = Late August"]
-[5.104022026062012, 3.0001418590545654, "[TT] Payload of the SEOSat/Ingenio = Optical"]
-[11.191091537475586, 4.654857158660889, "[TT] Structure Tolerances of the CXBN-2 = Better than \u00b10.1 mm"]
-[10.210528373718262, 0.9898657202720642, "[TT] Distance from Earth of the HD 260655 b = 33 light-years"]
-[10.952434539794922, 6.362060546875, "[TT] Secondary Mirror Material of the NAOMI = SiC"]
-[8.003321647644043, 5.052213668823242, "[FF] Full Form of the DORIS = Doppler Orbitography and Radiopositioning Integrated by Satellite"]
-[13.296272277832031, 7.23266077041626, "[TT] Steady-State Power of the CAE System = 30W"]
-[4.800836086273193, 0.8185172080993652, "[FF] Launch Date of the GOCE = Unknown"]
-[6.521069526672363, 3.795809507369995, "[TT] Suitability of the DarkCarb = Well suited"]
-[6.555668830871582, 4.84623384475708, "[FF] Description of the SV-6 System Resource Flow Matrix = Tabular description of each data element exchange between two system function actions"]
-[13.248785972595215, 5.265426158905029, "[TT] Solar Array Span of the QuickBird-2 = 5.2 m"]
-[11.385525703430176, 4.33357572555542, "[TT] Size of the Maya-3 = 1U"]
-[5.396220684051514, 5.47290563583374, "[TT] Management Interface of the DCU = PUS (Packet Utilization Standard) TCs"]
-[4.905388832092285, 2.9849698543548584, "[TT] Prime Contractor of the NIRCam = University of Arizona"]
-[11.403861999511719, 4.4025397300720215, "[TT] Size of the StangSat = 1U"]
-[7.889645576477051, 7.2277727127075195, "[TT] Spectral Range of the FTS Interferometer = 2.4-13.3 \u00b5m (or 750-4100 cm -1)"]
-[5.197856426239014, 2.0020620822906494, "[TT] Mission Status of the Buccaneer = Mission complete"]
-[10.921065330505371, 3.411895513534546, "[TT] Size of the CubeSats and smallsats = Up to 50 kg"]
-[9.534455299377441, 7.855083465576172, "[TT] Optics Unit Architecture of the Imager = Extendable"]
-[7.3634490966796875, 8.696704864501953, "[TT] Band of the ALICE = 70-205 nm"]
-[3.02535343170166, 4.761688709259033, "[TT] Centre Frequency of the XSAR = 9.59 GHz"]
-[7.139477729797363, 6.63900899887085, "[TT] Global Detection Threshold of the GLM = 25 counts"]
-[6.5758957862854, 2.65765118598938, "[FF] Program of the MiRaTA = In-Space Validation of Earth Science Technologies"]
-[10.155905723571777, -2.7561514377593994, "[TT] Module power (data retention) of the SLC NAND-FMM = 0 (4) W"]
-[10.0231351852417, -1.517846941947937, "[TT] Inclination of the Orbit = 98.13\u00ba"]
-[6.626889228820801, -0.44909989833831787, "[TT] Potential Repeat Cycle of the MSU-SK = 3-5 days"]
-[10.847414016723633, 5.722201347351074, "[TT] Maximum Temperature of the Avcoat = 2200 \u00b0C"]
-[7.671719074249268, 1.5042308568954468, "[FF] Use of the Concrete = Second only to water in terms of use by humanity"]
-[3.984219789505005, 2.137636184692383, "[TT] Launch Vehicle of the NuSTAR = Pegasus-XL"]
-[6.457477569580078, 4.111506938934326, "[TT] Carried Payload of the Challenger = INMS"]
-[5.294898986816406, 2.402996301651001, "[TT] Mission Type of the IDEA OSG 1 = Non-EO"]
-[7.813425064086914, -2.442913770675659, "[FF] Mission Context of the GOLD = Provides context for ground-based and LEO measurements"]
-[3.411628007888794, 6.45623254776001, "[TT] Pixel Size (km x km) of the Antenna = 16"]
-[5.494532585144043, 5.180854797363281, "[FF] Data Interface of the ESEO-TriTel EQM = CAN (Controller Area Network) open protocol"]
-[7.991818904876709, -0.5459074378013611, "[FF] Event of the Incheon Glacier = Meeting of the IPCC to consider the special report of global warming of 1.5\u00b0C in 2015"]
-[10.24307632446289, 2.967615842819214, "[FF] Design Purpose of the Compact Intersatellite Link Communication System = For satellites operating in swarms"]
-[9.809060096740723, 4.335987567901611, "[FF] DC Measurements Uncertainty of the PNI RM3000 = 0.05% of the field in CuPID's orbit"]
-[14.084832191467285, 3.1902554035186768, "[TT] Mass of the Capability = 14.0 kg"]
-[5.4559454917907715, 6.986326217651367, "[TT] Bus SOH Rate of the Telemetry bus = 90 kB/min"]
-[8.864895820617676, 5.115474700927734, "[FF] Update of the Accelerometer and Gyro = Before the first burn"]
-[5.070960521697998, 3.4701876640319824, "[TT] Manufacturer of the Space Micro \u00b5STDN = Space Micro"]
-[8.913095474243164, 2.5983502864837646, "[FF] Senior Review Date of the Heliophysics Operating Missions = June 11, 2015"]
-[6.570406436920166, -2.0287296772003174, "[TT] Tandem Setup of the Jason-1 = Completed Sept. 16, 2002"]
-[11.533686637878418, 3.4774773120880127, "[FF] Propulsion System of the SES-14 = Electric plasma propulsion system"]
-[11.74771785736084, 4.918966770172119, "[TT] Dimensions of the ChipSats = 3.5 x 3.5 cm"]
-[6.732342720031738, 6.207875728607178, "[FF] Test Number of the File Transfer Test = 1, 2, 3"]
-[10.528060913085938, 3.9743847846984863, "[FF] Illustration of the Drag Augmentation Device = Figure 16"]
-[5.0653791427612305, 3.4112722873687744, "[TT] Manufacturer of the Microthrusters = ENPULSION"]
-[7.401020050048828, 4.481816291809082, "[TT] Pointing Constraints of the RVX = Stringent"]
-[5.979053497314453, 0.9004940390586853, "[TT] Image Acquisition Date of the Karshi Khanabad = 14 Jul. 2014"]
-[8.560611724853516, 7.569445610046387, "[TT] Imaging Bands of the EOS-T = Five bands, one panchromatic as well as four multispectral"]
-[5.71151876449585, 1.0865774154663086, "[FF] Launch Date of the Weather Observation Satellite = April 17"]
-[5.855783939361572, -0.6683907508850098, "[TT] Mission Lifetime of the Satellite = 7.25 years"]
-[4.711294651031494, 0.4858424663543701, "[TT] Launch Date of the SARAL/AltiKa = February 2013"]
-[8.344396591186523, -0.827204167842865, "[TT] Freezing Temperature of the Carbon Dioxide Ice = -193\u00b0C"]
-[8.558844566345215, 1.3796873092651367, "[FF] Measurement of the Aquarius = Sea Surface Temperature"]
-[8.19505500793457, 4.6857805252075195, "[FF] Telescopes, detectors and associated electronics of the Raytheon Space Systems = Unknown"]
-[6.145267009735107, 5.100393772125244, "[FF] Function of the Ethernet LAN analyzer = Log all packets in/out of control center"]
-[4.942239761352539, 0.602873682975769, "[TT] Test Date of the AltiKa = Nov. 17-18, 2009"]
-[5.833625316619873, 6.059782028198242, "[FF] Access Time of the EDRS = Restricted by the visibility time"]
-[6.210442066192627, 4.353350639343262, "[FF] Objective of the DRR = Deliver global SMD (Stored Mission Data) to four US Operational Processing Centers"]
-[6.790706634521484, 4.933649063110352, "[FF] Signal Accuracy of the GPS = Highest\u2010possible"]
-[6.942680358886719, 4.461394309997559, "[FF] Design Requirement of the RVX FDIR = Ensure that the overall RVX SW is single-failure tolerant"]
-[7.747599124908447, 9.448044776916504, "[TT] Center Wavelength of the B1 = 443 nm"]
-[5.427626609802246, -0.7046300172805786, "[TT] Wake Up Time of the Jade Rabbit-2 = 10:51 a.m. last Thursday (28 February)"]
-[8.499800682067871, 5.619573593139648, "[TT] Accuracy of the GPS receiver = 50 m (1\u03c3)"]
-[6.879420757293701, 2.2605249881744385, "[FF] Unknown of the Super Dual Auroral Radar Network = Unknown"]
-[6.121561050415039, 4.580996990203857, "[FF] Processes of the BJ3A1 satellite ground pre-processing system = Image data separation, attitude and orbit parameter analysis, system radiation and sensor geometry correction, band registration, modulation transfer function (MTF) restoration, product packaging and more"]
-[5.3684539794921875, 3.202282428741455, "[TT] Manufacturer of the International Docking Adapters = Boeing"]
-[10.128164291381836, 8.090106010437012, "[TT] Focal Length of the Telescope = 5.6 m"]
-[8.113930702209473, -0.34875139594078064, "[FF] Insulating Effect of the Snow Layer = Insulates sea ice from frigid polar air, slowing ice growth"]
-[7.029585361480713, 4.259131908416748, "[FF] Proximate Cause of the Fairing = Fairing separation failed"]
-[10.293416976928711, 3.9696476459503174, "[TT] Deployment Mechanism of the IXPE observatory = Deployable boom"]
-[5.171140193939209, 0.7591403722763062, "[FF] Publication Date of the DTM-2013 = 2015"]
-[6.904252529144287, 1.6852996349334717, "[FF] URL of the James Webb Space Telescope = http://www.stfc.ac.uk/ukatc/resources/pdf/miri5487-28.pdf"]
-[11.902827262878418, 5.007364749908447, "[TT] TRM size of the HPA = 203 mm x 117 mm x 23.5 mm"]
-[6.532343864440918, 5.7458038330078125, "[TT] Quantity of the CDU = 16"]
-[7.325101852416992, 6.7246479988098145, "[FF] Mirror Actuator Requirement of the Laser frequency stabilization subsystem = Very linear and predictable mirror actuator, or an internal sensor within the actuator that yields an accurate representation of the actual mirror angle"]
-[6.151466369628906, 3.1347155570983887, "[TT] Third-Quarter Revenue of the BlackSky = $7.9 million"]
-[10.762001037597656, 0.9286182522773743, "[TT] Mass of the HAT-P-7 = Somewhat larger than the planet Jupiter"]
-[6.2675557136535645, -0.2548474669456482, "[TT] Duration of the Passivation Phase = About 700 s"]
-[3.4339845180511475, 4.996434688568115, "[TT] SAR system of the Payload = Nominal operations, no redundancy"]
-[8.049230575561523, 6.018233299255371, "[FF] Stability Requirement of the Cameras = High signal-to-noise ratio and long-term photometric stability"]
-[5.318335056304932, 1.0643388032913208, "[FF] Launch Date of the Resourcesat-2A = Unknown"]
-[3.4660120010375977, -0.9164903163909912, "[TT] Orbit Type of the RESURS-O1-4 = Sun-synchronous near-circular orbit"]
-[9.002409934997559, 5.077342510223389, "[TT] Type of the Rate gyro = Gyro chip"]
-[9.122565269470215, 2.753760814666748, "[TT] Suspected Cause of Failure of the KySat-2 = X4.9 solar flare on 25 February"]
-[7.3366522789001465, 4.607735633850098, "[FF] Unknown of the Physik Instrumente = Unknown"]
-[8.288817405700684, -0.4776346981525421, "[TT] Maximum Extent of the Arctic Sea Ice = 14.42 million km2 (5.57 million square miles)"]
-[6.124424934387207, 4.551937103271484, "[FF] Functionality of the Ground Software Architecture = Automatic query and validation of real-time telemetry, downloading stored spacecraft telemetry, and command and control of the platform and its experiments"]
-[5.463608264923096, 5.05084753036499, "[TT] Arbitration System of the CAN Bus = Yes"]
-[4.840185642242432, 4.482145309448242, "[FF] Downlink Function of the Argos System = Acknowledge uplink messages, increase system capacity, transmit broadcasting messages, modulate message length or repetition period"]
-[8.177054405212402, 1.4125927686691284, "[FF] Purpose of the SMOS = Soil moisture and ocean salinity"]
-[6.2422356605529785, 4.631770610809326, "[FF] Function of the SLCPE = Controls all subsystems and manages the data interface with the satellite"]
-[11.68973159790039, 3.301727294921875, "[TT] Redundant Thruster Status of the Meteosat-8 = Performing well"]
-[10.280499458312988, 7.596409797668457, "[TT] Feed Type of the Telescope System = Coud\u00e9 feed"]
-[5.018613338470459, 1.8530851602554321, "[TT] Development Start of the SVM = Phase 2"]
-[5.41343355178833, 6.568490982055664, "[TT] Data Storage Capacity of the RISAT-2 = 240 Gbit"]
-[5.08229398727417, 3.1485395431518555, "[FF] Manufacturer of the Iris V2 CubeSat Deep-Space Transponder = NASA/JPL"]
-[10.203332901000977, 3.8325138092041016, "[FF] Solar Panel Layout of the Coronagraph Spacecraft = Asymmetric solar sail concept"]
-[10.181418418884277, 1.2435964345932007, "[TT] Size of the Cluster XDCPJ0044.0-2033 = Over one and half million light years across"]
-[10.79129695892334, 1.0881931781768799, "[TT] Type of the TOI 270 = M-type dwarf"]
-[6.375194072723389, -1.168173909187317, "[TT] LTAN of the KOMPSAT-5 = 6:00 hours"]
-[10.851911544799805, 7.554636001586914, "[TT] Swath Width of the DMAC = 20 km"]
-[10.007048606872559, -1.4988232851028442, "[TT] Inclination of the Chang'e-1 = 31\u00ba"]
-[6.019862174987793, 2.0548746585845947, "[FF] Sub-Experiments of the EuTEF = DEBIE-2, DOSTEL, EuTEMP, EVC, EXPOSE, FIPEX, MEDET, PLEGPAY, TriboLab"]
-[7.571083068847656, 2.7990198135375977, "[FF] Emissions Cut Target of the U.S. President Joe Biden = At least 50% by 2030"]
-[7.212888240814209, 5.8253173828125, "[FF] Response Time of the MEOLUT = Unprecedented"]
-[6.647238731384277, -0.6244219541549683, "[TT] Actual Orbit Duration of the SMDC-ONE = 35 days"]
-[6.91400671005249, 3.7651050090789795, "[FF] Cocooned of the AGN = Yes"]
-[7.833763599395752, -0.7622120380401611, "[FF] Tracking Duration of the Fletcher's Ice Island = Since 1946"]
-[3.163496255874634, 5.006707191467285, "[TT] MRS Swath of the RISAT-SAR = 115 km"]
-[10.384533882141113, 5.759507179260254, "[TT] Temperature of the Cas A = 50 million degrees"]
-[8.556854248046875, 6.1659088134765625, "[TT] Relative Accuracy of the 268 nm Band = 1000 ppm"]
-[7.4825310707092285, 2.5044851303100586, "[TT] Instrument type of the SMEI = Radar altimeters"]
-[6.605861186981201, 0.41610896587371826, "[TT] Record Duration of the Landsat = Four decades"]
-[13.40260124206543, 5.461391448974609, "[TT] Type of the Solar Array = Single panel"]
-[11.795698165893555, 6.74200439453125, "[FF] Energy Range of the CeREs = ~tens of keV"]
-[7.755890369415283, -0.8621976971626282, "[FF] Data Filter of the ICESat-2 = Month"]
-[7.934785842895508, 4.682408332824707, "[FF] Image Transmission of the STARE satellite = Ground"]
-[10.496816635131836, 2.4116604328155518, "[TT] Resolution of the X-ray Imager = < 0.22\u00ba"]
-[11.791080474853516, 6.691427230834961, "[TT] Energy Range of the RHESSI = 3 keV - 17 MeV"]
-[13.43178653717041, 2.869811534881592, "[TT] Wet Mass of the BIT-3 flight system = 3 kg"]
-[6.133810997009277, 5.267139434814453, "[FF] Processor of the ACS = Dedicated"]
-[11.726627349853516, 7.512026786804199, "[FF] Sampling of the Megha-Tropiques = At 13\u00baN,the various orbits come in one single packet following each other ~100 min apart"]
-[7.428182125091553, 2.873357057571411, "[TT] Emission Reduction Goal of the MethaneSAT = Cut methane emissions by 45% by the year 2025 from the oil and gas industry"]
-[4.469052791595459, 1.839309573173523, "[FF] Conference Date of the RADARSAT-2 = May 16-18, 2006"]
-[11.67783260345459, 3.3526105880737305, "[TT] Number of Rocket Motors of the Super Strypi rocket = 3"]
-[4.870998859405518, 8.252274513244629, "[TT] Frequency Range of the TWTA = 17.7 - 18.8 GHz"]
-[6.187971115112305, 3.151686429977417, "[FF] Capability of the BlackSky platform = Observe, analyze and act on global events"]
-[7.988794803619385, 2.0744059085845947, "[TT] Swath of the Ocean Color Scanner = 3000 km"]
-[8.67974853515625, 7.509239196777344, "[TT] Camera Resolution of the Carbonite-2 = Ultra High Definition (UHD)"]
-[6.843595027923584, 3.477001667022705, "[FF] Mission Purpose of the REX-J = Demonstrate technologies for Astronaut support robots"]
-[9.663365364074707, -0.33945760130882263, "[TT] Altitude Region for OH of the MAHRSI = 38 to 90 km"]
-[4.58581018447876, 7.892296314239502, "[TT] Data Communications Transceiver Frequency of the OSSI-1 = 435 MHz"]
-[8.584136962890625, 1.353777527809143, "[TT] Band of the Aquarius = L-band"]
-[7.099035263061523, 6.894095420837402, "[TT] Operation Frequency of the Laser Altimeter (LALT) = 1Hz"]
-[6.171384334564209, 2.5312507152557373, "[FF] Payload of the SLS = Orion spacecraft, astronauts, and supplies"]
-[9.371271133422852, 9.126544952392578, "[TT] Far-UV Channel Spectral Resolution of the IRIS = 4 x 10-3 nm"]
-[4.981515884399414, 1.7931400537490845, "[FF] Monitoring Activities of the G\u00f6kt\u00fcrk satellite = Control of forestland, tracking illegal construction, rapid assessment of damage after natural disasters, determination of agricultural boundaries and geographical data gathering"]
-[4.884030818939209, 7.701129913330078, "[TT] Frequency Bands of the Galileo/GPS antenna = L1, L2, L5, E5, E6 and E1"]
-[9.061615943908691, 5.0344414710998535, "[TT] Activation of the Gyroscopes = Active"]
-[14.220922470092773, 3.2901368141174316, "[TT] Mass of the MSU-100 = 2.9 kg"]
-[7.734370231628418, 8.280355453491211, "[TT] Visible Channels of the ILAS = 1024"]
-[4.806763172149658, 0.47131580114364624, "[TT] Workshop Date of the GIRO = November 2017"]
-[16.502859115600586, 3.5889089107513428, "[TT] Planned Satellite Launch of the OneWeb = December"]
-[8.912631034851074, 6.465411186218262, "[TT] Operational Orientation of the AgCam/ISSAC = Local-Vertical-Local-Horizontal (LVLH)"]
-[13.316532135009766, 5.521352291107178, "[TT] Solar Arrays of the ISS = Six additional"]
-[7.920272350311279, 5.271609783172607, "[FF] Design of the Radiometric Responsivity Tracking Method = For optical sensors without on-board calibration systems"]
-[3.5215389728546143, -0.7522422671318054, "[TT] Resonance of the Satellite Orbit = 3:1"]
-[8.105269432067871, 1.3196052312850952, "[FF] Data Usage of the SMAP = Analyzing this moisture can tell you whether there is enough water for plants to function properly and to achieve an optimal yield"]
-[5.916497707366943, 0.17661723494529724, "[FF] Anniversary of the TIMED = 10 Years"]
-[7.15794038772583, 4.729316234588623, "[FF] Function of the WTS = Samples the energy distribution"]
-[5.052170276641846, 3.3795018196105957, "[TT] Manufacturer of the SpaceWire ASIC = BAE (British AeroSpace)"]
-[6.488138198852539, 1.1473000049591064, "[TT] Ground System of the FormoSat-7 / COSMIC-2 mission = High degree of automation"]
-[4.1810407638549805, 5.875079154968262, "[TT] Data-Streaming Latency of the ADS-B Receiver = Below 1.5 seconds"]
-[6.499121189117432, -0.09957314282655716, "[TT] Usage of the Short wave references = Once per month"]
-[9.267901420593262, -0.3996415436267853, "[TT] Orbit Perigee of the PROBA-3 = 600 km"]
-[6.627267837524414, -0.5003343820571899, "[TT] Period of the Explorer 36 = 112 minutes"]
-[7.839465618133545, 4.804872989654541, "[FF] Mounting Points of the Bus Structure = Star tracker, gyroscopes, High Gain Antenna, Low Gain Antennae, maneuvering thrusters"]
-[5.818764686584473, -0.8154845833778381, "[TT] Design Lifetime of the TanSat = Three years"]
-[14.303231239318848, 3.0470657348632812, "[TT] Mass of the Global-4 = 60 kg"]
-[14.641988754272461, 6.720143795013428, "[TT] Capacity of the NiH2 Batteries = 8 Ah"]
-[8.160842895507812, 5.88830041885376, "[TT] Orbital Distance Measurement Accuracy of the LASSO = 10 cm"]
-[8.190027236938477, 7.329902648925781, "[FF] Sensitivity of the MCP detectors = Ultraviolet (UV) light, including both EUV and shorter FUV (Far Ultraviolet) wavelengths"]
-[6.401298999786377, 8.089625358581543, "[TT] Number of Channels of the Global Imager (GLI) = 36"]
-[6.615594863891602, 5.43483304977417, "[TT] ACS Reaction Loads of the RBA = Eliminated"]
-[4.98854923248291, 7.174750328063965, "[TT] Data Download Speed of the NEMO-HD = Up to 50 Mbit/s"]
-[7.082306861877441, 1.2755944728851318, "[TT] Function of the Earth Return Orbiter = Rendezvous with the samples in orbit around Mars and take them in a highly secure containment capsule for return to Earth"]
-[13.719575881958008, 2.8633334636688232, "[TT] Mass of the Spacecraft = 670 kg"]
-[4.038728713989258, 6.714233875274658, "[TT] Quantity of the X-band Ground Stations = 4"]
-[7.754143238067627, 6.616003513336182, "[TT] Image Light Time of the Voyager 1 = 5 hours and 36 minutes"]
-[8.13254451751709, -0.3578207790851593, "[FF] Regional Variations of the Sea Ice = Inhibit melting in different parts of the Arctic"]
-[5.576417922973633, -1.9216727018356323, "[TT] Structure of the KOMPSAT-6 = Integrated structure with hexagonal cross section"]
-[8.054510116577148, 0.6569125056266785, "[FF] Water Holding Time of the Lake Eyre = Varies"]
-[6.224996089935303, 2.472200870513916, "[FF] Designation of the Orion Spacecraft = MPCV (Multi-Purpose Crew Vehicle)"]
-[4.015270709991455, 2.1579630374908447, "[TT] Launch Vehicle of the EDRS-C = Ariane-5 ESA"]
-[6.595095157623291, 1.158665418624878, "[FF] Operating Concepts of the PICOSAT1.1 = Unknown"]
-[5.792656898498535, 0.9665251970291138, "[TT] Image Acquisition Date of the HyperScout = 26 March 2018"]
-[10.908561706542969, 7.538044452667236, "[TT] Swath of the MRS = 115 km"]
-[13.845728874206543, 7.016297340393066, "[TT] Actuation of the SU = Quasi DC actuation voltages"]
-[7.516383171081543, 6.304881572723389, "[TT] Mode of the eROSITA = Continuous scanning"]
-[5.268703460693359, 4.368186950683594, "[TT] Global Coverage Requirement of the SpaceLink = 3 satellites"]
-[9.68525218963623, 1.399853229522705, "[FF] Presentation of the POLO = http://smsc.cnes.fr/PLEIADES/Fr/PDF/presentation_pleiades.pdf"]
-[6.989076137542725, 6.146632194519043, "[TT] Data Playback Frequency of the SAMPEX = Twice per day"]
-[5.752645492553711, -0.7845523953437805, "[TT] Actual Operational Life of the BIRD = Just over four years"]
-[10.822542190551758, -0.25505590438842773, "[FF] Mission Concept & Status of the TanDEM-X = Not Provided"]
-[7.077301979064941, 8.333932876586914, "[TT] Estimated SNR of the Band 2 = 797.02 \u00b1 53.34"]
-[12.151907920837402, 3.690159559249878, "[TT] Xenon Pressure of the XTA = 186 bar"]
-[3.498784303665161, 4.762707233428955, "[FF] Program Start of the SIR-C/X-SAR = Seasat Synthetic Aperture Radar (SAR) in l978"]
-[9.672544479370117, 1.4014358520507812, "[TT] Response Time of the Pleiades-1A = Within four hours"]
-[7.977613925933838, 13.683708190917969, "[TT] SSD of the B8a = 20 m"]
-[7.484077453613281, 8.490376472473145, "[TT] Spectral Sensitivity (Source) of the SXI = C (44.7 \u00c5)"]
-[9.25191879272461, 3.1079342365264893, "[FF] Motion of the Solar Plumelets = Move individually, oscillating on its own"]
-[13.069561958312988, 7.7068681716918945, "[TT] Transmit Power of the LCT = 2.2 W"]
-[6.643252849578857, 4.457561016082764, "[FF] Unknown of the Payload = Unknown"]
-[3.5680811405181885, -0.9782379865646362, "[FF] Orbit of the PAMELA = Semi-polar Resurs orbit"]
-[13.37663745880127, 6.75507926940918, "[TT] Power Control Unit (PCU) of the Satellite = 1"]
-[6.041064739227295, 1.2309496402740479, "[FF] Launch Date of the JPL-Built Earth Science Experiment = Nov. 2, 2011"]
-[6.219619274139404, 0.39205753803253174, "[TT] End of Life Date of the ROSE-L = 2035"]
-[8.201491355895996, 8.227438926696777, "[TT] Spectral Range of the Imager = 450-800 nm"]
-[4.719282150268555, 1.4347277879714966, "[TT] PDR Date of the GCOM-W1 = March 2008"]
-[8.41402816772461, 8.67669677734375, "[TT] Spectral Sampling Interval of the Prism Spectrometer = 1.2 nm \u2013 16 nm"]
-[5.66609525680542, 5.514261245727539, "[TT] Industrial grade embedded computers of the Frame Grabber = Industrial grade embedded computers were selected for this application"]
-[14.245729446411133, 3.3024139404296875, "[TT] Mass of the ScaRaB = 40 kg"]
-[10.588847160339355, 2.9530632495880127, "[FF] Mission Purpose of the PACE = Establish more confident simulation models for nanosatellites and/or CubeSats of similar configuration in LEO"]
-[11.903036117553711, 4.95767068862915, "[TT] Dimensions of the PowerCell = ~21 x 29 x 8 cm"]
-[4.506644248962402, 2.9676692485809326, "[TT] Test Location of the CO2M = ESA\u2019s Test Centre in the Netherlands"]
-[9.65214729309082, 1.3804939985275269, "[FF] Launch Date of the Pleiades-1B = More than one and a half years before October 2013"]
-[7.5537428855896, 8.570207595825195, "[TT] Removability of the Optical Filters = Required"]
-[11.657244682312012, 4.633255481719971, "[TT] Dimensions of the Node-3 = Diameter of 4.5 m and length almost 7 m"]
-[3.791316032409668, 4.621405124664307, "[FF] Polarimetric Accuracy of the RADARSAT-2 = Fluctuate seasonally"]
-[8.259696960449219, 8.715789794921875, "[TT] Wavelength Range of the Littrow spectrometers = 1249 \u2013 1305 nm"]
-[3.7339417934417725, -1.073539137840271, "[TT] Initial Orbit Type of the Observatories = Highly elliptical orbits"]
-[9.711417198181152, 8.553472518920898, "[FF] IFOV of the FTS-2 = Unknown"]
-[9.26319694519043, 3.2148945331573486, "[TT] Exposure Time of the Coronal Hole Boundaries = < 10 s"]
-[8.638578414916992, 8.061212539672852, "[TT] VNIR Resolution of the PROBA-V = 5200 pixel"]
-[9.154556274414062, 2.7349300384521484, "[FF] Electron Production Time of the Solar storm = 60 seconds"]
-[6.105085372924805, 1.4657398462295532, "[FF] Image Acquisition Date of the VIIRS = June 3 and 5, 2022"]
-[5.8275227546691895, -0.7604894638061523, "[TT] Lifetime of the MTG-S satellite = Around 8.5 years"]
-[4.0968828201293945, 6.096753120422363, "[FF] Function of the ESS = Deploy the antenna and provide rigid support"]
-[4.191133975982666, 7.353961944580078, "[TT] Band of the CRISTAL = Ku- and Ka-band"]
-[5.933250427246094, 1.3270611763000488, "[FF] Announcement Date of the Tiny NASA Satellite = 28 October 2019"]
-[11.405613899230957, 5.808844566345215, "[FF] Construction of the Central Cylinder = Sandwich construction with aluminum core and CFRP face skin"]
-[12.028164863586426, -0.3435792326927185, "[FF] Event Name of the TESS = ASASSN-19bt"]
-[9.237261772155762, 5.58255672454834, "[TT] Orientation of the \u00b5SCIA = Nadir-oriented"]
-[4.770834445953369, -1.8419092893600464, "[FF] Mission Status of the Chang'e-4 = Unknown"]
-[8.117027282714844, 7.552727699279785, "[FF] Quantum Efficiency of the CCD = Parameter Value"]
-[9.819279670715332, 4.601722717285156, "[FF] Attitude Control of the S/C = 3-axis stabilization with four reaction wheels and three torque rods as actuators"]
-[7.573394775390625, 2.579397201538086, "[FF] Measurement Category of the IRS-P6 = Multi-purpose imagery (land), Vegetation, Albedo and reflectance, Landscape topography, Sea ice cover, edge and thickness, Snow cover, edge and depth"]
-[4.383153438568115, 6.3086957931518555, "[FF] Properties of the Antenna Subsystem = Quick and precise error determination"]
-[10.170114517211914, 5.821876525878906, "[TT] Temperature of the Cold Focal Plane = 91 K"]
-[12.619382858276367, 9.095547676086426, "[TT] Local Equatorial Crossing Time of the Tatiana-2 = 12:00 hours"]
-[7.3408942222595215, 5.409837245941162, "[FF] Contents of the FEEU = Position sensing, analog control loops, Analog to Digital Sigma Delta converters"]
-[8.152624130249023, 7.885348796844482, "[TT] Low Energy Detector Channels of the SSJ/4 = 10 channels centered at 34, 49, 71, 101, 150, 218, 320, 460, 670, and 960 eV"]
-[5.573613166809082, 7.03800106048584, "[TT] VSWR of the SDR = \u22643"]
-[3.7293808460235596, 6.645407199859619, "[TT] VDES Antenna Type of the NorSat-2 = Yagi-Uda antenna"]
-[8.305615425109863, 6.514189720153809, "[FF] Measurement Methods of the LDT Photodiodes = Proton fluence through displacement damage effects, ionizing current"]
-[5.78769588470459, 3.6180882453918457, "[TT] Operational Requests Management of the TDP Operations = Managed at a top level by ESA"]
-[7.653041362762451, 3.2872281074523926, "[FF] Low-Light Imaging Capability of the OLS = Collect low-light imaging data of the Earth during the nighttime period"]
-[8.726930618286133, 7.791008949279785, "[TT] Detector Size of the Long Wavelength Band = 2.5 cm x 2.5 cm"]
-[10.180641174316406, 9.3797025680542, "[TT] Nominal IGFOV of the Band 4 = 2 km"]
-[7.467403888702393, -0.6726709604263306, "[TT] Duration of the Operation IceBridge = 11 years"]
-[13.758804321289062, 7.122450351715088, "[TT] Current range (A) of the PS-1 = 0.2~0.6"]
-[6.570365905761719, 1.875246286392212, "[FF] URL of the GPM = http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20110011761_2011012112.pdf"]
-[7.208992958068848, 0.11251021176576614, "[TT] Rock Deposits Age of the LRO = Less than 100 million years old"]
-[6.749839782714844, 2.042515754699707, "[FF] Survey Purpose of the Nancy Grace Roman Space Telescope = Discern between the leading theories about what's speeding up the universe's expansion"]
-[9.556596755981445, 4.854413986206055, "[TT] Design of the AOCS = Momentum-biased 3-axis stabilized spacecraft"]
-[6.843783378601074, 2.2141273021698, "[FF] Publication Date of the Super Dual Auroral Radar Network = 2007"]
-[9.155017852783203, 0.8814557194709778, "[FF] Ballistic Coefficient of the PUNCH Mission = Increased by adding ballast"]
-[4.1980767250061035, 6.729914665222168, "[FF] Outputs of the Dual-band antenna = Highly isolated"]
-[4.040777206420898, 2.163600444793701, "[TT] Launch Vehicle of the GOES-T = Atlas 5"]
-[10.427433013916016, 5.77591609954834, "[TT] Operating temperature range of the PHA = -30 to +50\u00baC"]
-[4.514018535614014, 6.5932793617248535, "[TT] RF Communications of the Spacecraft = 145.89 MHz"]
-[8.632463455200195, 2.2672581672668457, "[TT] Accuracy of Wind Velocity (Stratosphere) of the Aeolus = 3 m/s"]
-[6.689436912536621, 5.481692314147949, "[TT] Control Type of the TCS = Passive"]
-[11.113574981689453, 4.798085689544678, "[TT] Length of the Tether = 4 km"]
-[8.460489273071289, 5.310983657836914, "[FF] Orbit Determination Accuracy of the AutoNav = Later refinements improved these values substantially"]
-[3.3378944396972656, 1.8546029329299927, "[FF] Image Content of the Sentinel-2C = Part of Mecklenburg\u2013West Pomerania, also known as Mecklenburg-Vorpommern, a state in northeast Germany"]
-[9.960491180419922, 2.784975528717041, "[TT] Function of the RICH = Measure the velocity of charged cosmic particles"]
-[10.168210983276367, 8.208950996398926, "[TT] Ratio of the Aperture Function = D/a"]
-[6.684656143188477, 0.7973342537879944, "[TT] Measurement Date of the On-orbit temperature data = After July 7, 2012"]
-[8.303336143493652, 8.573776245117188, "[TT] Spectral Range of the Fourier transform spectrometer = 645 to 2760 cm-1"]
-[10.203527450561523, 5.8148579597473145, "[TT] Operating Temperature of the SWIR focal plane = -80\u00baC"]
-[8.841029167175293, 4.439044952392578, "[FF] Attitude Sensing of the PARASOL = Star sensor, sun sensors, magnetometer, gyroscopes"]
-[6.533879280090332, -0.32145729660987854, "[TT] Observation Duration of the SLA-1 = Over 80 hours"]
-[8.600640296936035, 0.352297306060791, "[TT] Size of the Hofsj\u00f6kull = Third largest in Iceland"]
-[5.4363908767700195, 5.611823081970215, "[FF] Interface of the Instrument = RS-422 or 1553B"]
-[12.099630355834961, 4.51836633682251, "[TT] Structure Dimensions (Deployed) of the FY-3 series spacecraft = 4.4 m x 10 m x 3.8 m"]
-[5.240837097167969, 6.9901123046875, "[TT] Data Downlink Speed of the Payload = 128/256 kbit/s"]
-[4.933239936828613, 0.332859069108963, "[TT] Launch Date of the Badr-B = 10 December 2001"]
-[10.179924964904785, 5.317983150482178, "[FF] Purpose of the Active Cooling System = Evacuate the heat generated by the STD front-end electronics"]
-[9.832866668701172, 4.248344421386719, "[TT] Quantity of the Magnetorquers = 3"]
-[5.771684646606445, 3.544971227645874, "[TT] Number of Spacecraft of the Landmapper-Demo = 2"]
-[9.952191352844238, -0.5350503325462341, "[TT] Orbit Altitude of the NPSat-1 = 720 km"]
-[7.841516971588135, 1.4917525053024292, "[TT] Number of Land Regions of the RECCAP-2 = 10-14"]
-[4.585029602050781, 4.114898681640625, "[FF] Experiment of the Lunar Pathfinder = Demonstration of GPS and Galileo reception in lunar orbit"]
-[6.326230049133301, -0.6984252333641052, "[TT] LTDN of the Tsubame = 11:00 hours"]
-[8.049022674560547, 1.4185373783111572, "[FF] Importance of the SMAP = Understanding of Earth's cycles"]
-[9.704567909240723, -0.5989505052566528, "[TT] Orbit Altitude of the ASNARO satellite = 504 \u00b1 2 km"]
-[9.435076713562012, 4.830920219421387, "[TT] Attitude Control System Status of the GOSAT-2 = Steady state"]
-[13.420256614685059, 7.321438789367676, "[TT] Power of the Poseidon-1 = 49W"]
-[9.741024017333984, 2.504398822784424, "[TT] Optics Modules of the NuSTAR = Two identical"]
-[9.57435131072998, 9.203474998474121, "[FF] Launch Date of the IRIS = June 27, 2013"]
-[5.006266117095947, 0.4221702516078949, "[TT] Introduction Date of the SASAR = 1992"]
-[4.918413162231445, 2.98095703125, "[TT] Manufacturing Facility of the Pelican = San Francisco"]
-[5.168830394744873, 1.6330952644348145, "[FF] News Release of the TecSAR = IAI news, First Quarter 2008, Issue 25"]
-[8.05819034576416, 8.642765045166016, "[TT] Value of the Spectral Stability = Better than 0.02 nm"]
-[9.561444282531738, 7.057647705078125, "[TT] Spatial Resolution (km) of the Surface type = 25"]
-[4.410471439361572, 1.0044857263565063, "[TT] Launch Date of the IRNSS-1C = Oct. 15, 2014"]
-[5.69461727142334, -0.1304938942193985, "[FF] Deployed Stiffness of the RDA = Not provided"]
-[7.960436820983887, 8.708742141723633, "[TT] Spectral Range of UVIS of the ELVIS = 200-650 nm"]
-[5.78809928894043, 1.7167106866836548, "[FF] Conference Presentation of the MMS Phase 2B Navigation Performance = AAS/AIAA Astrodynamics Specialist Conference"]
-[7.442813396453857, 6.560903549194336, "[TT] Full Latitudinal Coverage Time of the Instrument = 5 successive 100-second intervals"]
-[4.595489501953125, 0.5257765650749207, "[TT] Scheduled Flight Date of the HTV-7 = Sept. 10"]
-[11.892525672912598, 6.6776442527771, "[TT] Energy Range of the HIPS = 10-400 MeV"]
-[4.540431976318359, 1.2478190660476685, "[TT] Launch Date of the AlSat-2B = September 2016"]
-[4.694465160369873, 7.277989387512207, "[TT] X-band Channels Data Rate of the Payload = 105 Mbit/s"]
-[6.258540153503418, -0.36942824721336365, "[TT] Operation Duration of the nanoRTUTM = Six months"]
-[10.397053718566895, 4.0553669929504395, "[TT] Extendible Boom Length of the ACS = 3 m"]
-[12.035223960876465, -0.38166317343711853, "[TT] Mission Lead of the TESS = MIT"]
-[4.346837043762207, 0.4225449860095978, "[TT] Launch Date of the JL-1-GF03D = 03 July 2021"]
-[5.634345054626465, 5.642282009124756, "[TT] Daughter card of the C&DH subsystem = Cortex A8 processor"]
-[9.042179107666016, 0.19003523886203766, "[TT] Size of the Lake Atat\u00fcrk Dam = 817 km2"]
-[6.010016918182373, 5.736799240112305, "[TT] FPGA of the C&DH = Xilinx XCV100"]
-[3.4264402389526367, 5.25881290435791, "[TT] Band Coverage of the SARR = 121.5 MHz"]
-[6.642561912536621, 1.6101844310760498, "[FF] Field of View of the WAC = Large portions of Europa's landscape"]
-[8.221270561218262, 2.7540030479431152, "[TT] Measurement Domain of the TUBSAT = Atmosphere, Ocean, Land, Gravity and Magnetic Fields"]
-[8.165786743164062, 2.125324010848999, "[FF] Purpose of the TROPICS = Study the development of tropical cyclones through rapid-revisit sampling"]
-[10.126428604125977, 7.5456953048706055, "[TT] Swath width at nadir of the Imager = ~57 km"]
-[8.843502044677734, 9.517694473266602, "[FF] Band 2 Spectral Range of the TANSO-FTS-2 = 1.563 - 1.695 \u00b5m"]
-[7.9897356033325195, 8.097548484802246, "[TT] Spectral Band of the Band Photometers = 391.4 nm"]
-[4.19774055480957, 2.0075161457061768, "[TT] Launch Date of the NigeriaSat-2 = November 2011"]
-[8.348441123962402, 8.816156387329102, "[FF] Operation of the OCO-2 = Employ a diffraction grating to separate the inbound light energy into a spectrum of multiple component colors"]
-[10.109537124633789, 1.3239706754684448, "[TT] Maximum Distance of Galaxies of the Euclid = Up to 10 billion light years away"]
-[7.597683429718018, 5.365006923675537, "[FF] Function of the Vision-based Sensor System = Acquire formation and re-acquire it once per orbit"]
-[5.955770015716553, 7.128261089324951, "[TT] Sensor Data Rate (max) of the DACS = 326 Mbit/s (6 bit BAQ), 1562 Mbit/s (3 bit BAQ)"]
-[6.145721435546875, 1.0510796308517456, "[FF] Start of the Science Operations = Main observation periods for GRB events"]
-[8.218992233276367, 7.195326328277588, "[TT] Image Acquisition of the Supervision Cameras = 10 frames/s"]
-[9.50699520111084, 1.376387596130371, "[FF] Ejection Velocity of the Net = Unknown"]
-[13.359655380249023, 7.70242977142334, "[FF] Radio of the PICOSAT = Battery operated, very low power"]
-[8.160334587097168, 5.733297348022461, "[FF] Accuracy of the LUIS = Absolute accuracy traceable to the NIST (National Institute of Standards and Technologies) or equivalent primary standards of radiance scale"]
-[5.568068504333496, 2.4441845417022705, "[FF] Development Team of the PALSAR = Hiroshi Watanabe, Shiro Ohkawa, Kenji Tatsumi, Hidekuni Kikuchi, Yasutaka Onoda"]
-[9.817413330078125, -0.43488746881484985, "[TT] Orbit Altitude of the GF-3 Satellite = 755 km"]
-[9.74675178527832, -0.6277392506599426, "[TT] Orbit Altitude of the GPM Core spacecraft = 400 km"]
-[7.627242565155029, 8.793821334838867, "[TT] Typical Radiance of the COCTS = 27.5 mW/cm2 \u00b5m sr"]
-[5.913198471069336, 2.472245693206787, "[TT] Management Contractor of the IMAP = SwRI (Southwest Research Institute)"]
-[7.098024368286133, 4.543498992919922, "[FF] Data Downlink of the SOLCON-3 = During the mission"]
-[8.839228630065918, 5.391438007354736, "[TT] Measurement Error of the Angular Rate = Random < 0.1\u00ba/s (1\u03c3), Bias < 0.6\u00ba/s, Nonlinearity < 0.5%"]
-[9.760916709899902, 8.173113822937012, "[TT] Focal Length of the Optical Head = 3 mm"]
-[6.994202136993408, 6.093545913696289, "[TT] Number of Instruments of the PIMS = 2"]
-[3.485759973526001, 5.236124038696289, "[TT] Residual Doppler of the SAR payload = 50\u2013150 Hz"]
-[3.6626110076904297, 4.101104736328125, "[TT] Image Capture Date of the RISAT-1 SAR payload = May 4, 2012"]
-[4.377364635467529, 3.0869996547698975, "[TT] Ground Stations of the DEIMOS-2 = Puertollano, Kiruna, and Inuvik"]
-[6.5412397384643555, 6.958314895629883, "[TT] Duty Cycle of the SeaWinds = 100%"]
-[6.948382377624512, 1.271889567375183, "[FF] Investigation Date of the ASGA Solar Cell Experiment = Dec. 05 - 09, 1994"]
-[5.592000484466553, 2.957585334777832, "[TT] Managed By of the TEMPEST-D = NASA/JPL"]
-[8.283368110656738, 2.503662109375, "[FF] Purpose of the PARASOL = Characterisation of clouds and aerosols and their microphysical and radiative properties"]
-[13.691723823547363, 2.9447295665740967, "[TT] Payload Mass of the DSP satellites = 30 kg"]
-[4.333526611328125, 6.82127571105957, "[TT] Downlink Capability of the Malindi station = S-band"]
-[13.110033988952637, 7.381296157836914, "[TT] Digital Data Handling Subsystem Power Consumption of the SIR-C = 800 W"]
-[9.882542610168457, -0.34105607867240906, "[TT] Altitude of the Sentinel-2C = 786 km"]
-[9.127293586730957, 3.270153284072876, "[FF] Observation Target of the IRIS = Sun's lower atmosphere just above the surface (chromosphere)"]
-[6.247781753540039, 4.82621431350708, "[FF] Software of the ACS = ACS flight software (FSW)"]
-[4.916964054107666, 0.34631702303886414, "[TT] Deployment Date of the QARMAN = 2019"]
-[9.159034729003906, 3.069383144378662, "[FF] Objective of the SOSP = Study of solar physics and solar-terrestrial relationships in aeronomy and climatology"]
-[6.922418117523193, -0.6421736478805542, "[TT] Orbit Period of the BX-1 = 90.1 minutes"]
-[8.549572944641113, 8.689576148986816, "[TT] Dispersion Element of the Prism Spectrometer = Direct vision prism"]
-[4.848998069763184, 6.616471290588379, "[FF] Internet Access Disparities Reduction of the KIZUNA = Verified"]
-[8.117271423339844, 8.028329849243164, "[TT] Spectral Band of the MWIR camera = 3.4-4.2 \u00b5m"]
-[8.40972900390625, 7.709243297576904, "[FF] Wavelengths of the Image Quality = 0.540 \u00b5m, 0.555 \u00b5m, 0.570 \u00b5m and 0.588 \u00b5m"]
-[6.88713264465332, 2.15132999420166, "[FF] URL of the STEREO = http://www.nasa.gov/mission_pages/stereo/news/five-years.html"]
-[9.767215728759766, 8.02893352508545, "[FF] Objective Type of the Optics Subsystem = Ritchey-Chr\u00e9tien type with auxiliary lenses"]
-[3.30145263671875, 5.1280598640441895, "[TT] L-band Resolution of the SAR-XL Payload = 5 m class"]
-[6.763099193572998, -0.2350364327430725, "[TT] Temporal Resolution of the Cheollian 2B satellite = 8 times-10 times/day"]
-[5.490707874298096, 1.696410059928894, "[FF] Preliminary Results of the KAGUYA-LALT = Available"]
-[6.933078765869141, 6.923666954040527, "[TT] Type of the TEA-CO2 lasers = Single-longitudinal-mode"]
-[5.492275714874268, 7.710970401763916, "[TT] EIRP of the USAT = > 41.5 dbW"]
-[9.043534278869629, 2.7095210552215576, "[FF] Publication Date of the Can ripples on the sun help predict solar flares? = 21 September 2020"]
-[4.521425247192383, 1.379552960395813, "[FF] Purpose of the AlSat-2 = Widely observe Algeria"]
-[7.800999164581299, 6.484123706817627, "[TT] Time Resolution of the Measurement = Of the order of 1 ms (or less)"]
-[12.467387199401855, 0.5508736968040466, "[TT] Payload Operations Start Date of the PLATO = 2025"]
-[10.92943286895752, 7.513820171356201, "[TT] Swath Width of the TROPOMI = 2600 km"]
-[10.109893798828125, -1.5197700262069702, "[TT] Inclination of the \u00d8rsted satellite = 96.5\u00ba"]
-[5.199601650238037, 0.08473609387874603, "[TT] End of Life Date of the ISS:LIS = 30 Sep 2023"]
-[7.590381145477295, 4.2074151039123535, "[FF] Location of the EARS = Multiple"]
-[3.7373859882354736, 4.619231700897217, "[FF] Data of the ICEYE = SAR data"]
-[5.707516670227051, -0.007468860596418381, "[TT] Power Down Date of the MWI = July 19"]
-[13.599953651428223, 7.326633453369141, "[TT] Input Power of the X-123SDD = +5 VDC, 300 mA"]
-[8.546049118041992, 2.834709644317627, "[FF] Utilization of the ESP-MACCS = Quantify atmospheric processes in the upper troposphere and stratosphere"]
-[5.980408191680908, 4.943286895751953, "[FF] Function of the Communication Network = Provide real-time voice/data/fax connectivity"]
-[5.369898796081543, 0.9763451814651489, "[FF] Opening Date of the ESA Facility = 9 November 2018"]
-[7.453751087188721, -0.1429966539144516, "[TT] Regained Contact Time of the Philae = 22:19 GMT"]
-[10.612622261047363, 7.323343276977539, "[TT] Swath of the NIRST = 180 km"]
-[6.251185894012451, 3.971085548400879, "[FF] Purpose of the COSMOS = Support the development and operations of one or more small spacecraft throughout the life cycle"]
-[6.820106029510498, 7.0049662590026855, "[TT] Number of Beams aiming toward Japan of the MBA System = 12"]
-[8.600083351135254, 0.13768474757671356, "[TT] Water Vapor Emission of the Patch on Comet Surface = 3% of the total amount"]
-[5.083136558532715, 3.3345251083374023, "[TT] Owner of the NeuSAR = DSO National Laboratories, Singapore, with support from the Office for Space Technology and Industry (OSTIn)"]
-[5.710878372192383, 2.194417715072632, "[FF] Supernova Remnant Name of the NuSTAR = Cassiopeia A (Cas A)"]
-[6.053506374359131, -0.2777462899684906, "[TT] Mission Life of the PICOSAT1.1 = About a week"]
-[11.545312881469727, 6.771615028381348, "[TT] Low-Energy Threshold of the Detector = 2.5 keV"]
-[7.891193389892578, -2.4616403579711914, "[FF] Observation of the GOLD = Total solar eclipse in South America"]
-[5.516151428222656, 0.4262920618057251, "[FF] Launch Date of the Atlas V Rocket = Dec. 6, 2013"]
-[10.127071380615234, 6.563125133514404, "[TT] Moving Mirror Unit Location of the MSASI = Russia"]
-[5.210707664489746, 1.3488396406173706, "[TT] Conference Session of the PSAT = Pre-Workshop Session 4: Lessons Learned"]
-[11.902907371520996, 4.982996940612793, "[TT] Dimensions of the Interface Board = 75 mm by 65 mm"]
-[8.021349906921387, 2.911512851715088, "[FF] Purpose of the GLM = Measures lightning activity and ice-phase precipitation"]
-[5.77952241897583, 7.152423858642578, "[TT] Data Rate of the AATSR = 625 kbit/s"]
-[5.037878036499023, 2.3962841033935547, "[FF] Capability of the ORS = Develop the capability to augment or replace space capabilities on very short timescales"]
-[6.0792083740234375, 2.533390998840332, "[TT] Location of the HIFI = SRON Netherlands Institute for Space Research, Groningen, the Netherlands"]
-[12.416402816772461, 3.2407593727111816, "[TT] Maximum Capacity of the Propellant = 300 kg"]
-[5.646892547607422, 2.238781690597534, "[FF] Project Team Member of the SHIZUKU = Matsuaki Kato"]
-[11.09499740600586, 2.861865997314453, "[TT] Maximum Power Budget of the SERB Nanosatellite = 20 W"]
-[-4.064921855926514, 4.482385158538818, "[FF] Support Phase Time Period of the Mango Tango = 03.08 to 10.08.2010"]
-[10.079981803894043, 7.518536567687988, "[TT] Swath Width of the TeLEOS-1 Imager = 12 km"]
-[6.786565780639648, 6.529846668243408, "[TT] Registration Time of the RFA = 50 ms"]
-[12.39837646484375, 0.609926700592041, "[FF] Pointing Performance of the PLATO satellite = Unknown"]
-[3.776251792907715, 6.884939670562744, "[TT] Diagram of the TEC Antennas = Circular with 3 db"]
-[14.186092376708984, 3.192931890487671, "[TT] Total Mass of the Net = Approximately 0.6 kg"]
-[4.403167247772217, 2.200216054916382, "[TT] Operation Status of the DubaiSat-1 = Nominal"]
-[9.846047401428223, 6.425526142120361, "[FF] Authors of the Geostationary Earth Radiation Budget Project = J. E. Harries, J. E. Russell, J. A. Hanafin, H. Brindley, J. Futyan, J. Rufus, S. Kellock, G. Matthews, R. Wrigley, A. Last, J. Mueller, R. Mossavati, J. Ashmall, E. Sawyer, D. Parker, M. Caldwell, P. M. Allan, A. Smith, M. J. Bates, B. Coan, B. C. Stewart, D. R. Lepine, L. A. Cornwall, D. R. Corney, M. J. Ricketts, D. Drummond, D. Smart, R. Cutler, S. Dewitte, N. Clerbaux, L. Gonzalez, A. Ipe, C. Bertrand, A. Joukoff, D. Crommelynck, N. Nelms, D. T. Llewellyn-Jones, G. Butcher, G. L. Smith, Z. P. Szewczyk, P. E. Mlynczak, A. Slingo, R. P. Allan, M. A. Ringer"]
-[12.01689624786377, -0.3480533957481384, "[TT] Discovery Date of the TESS = July 25, 2019"]
-[4.86390495300293, 1.7781167030334473, "[FF] Development Status of the GCOM Satellites = Not provided"]
-[8.672833442687988, 6.372914791107178, "[FF] Optical Path of the IASI-NG = Two opposite prisms moving synchronously with the OPD change"]
-[6.299834728240967, 8.059924125671387, "[TT] Number of Channels of the MWI = 17"]
-[5.910254001617432, 0.8273189067840576, "[FF] Observation Date of the OMI = 15 Dec. 2016"]
-[4.6904072761535645, 7.917226791381836, "[TT] Frequency Range of the RF communications = 4770 - 4800 MHz"]
-[10.541974067687988, 6.871675968170166, "[TT] Transmit Beam Waist Radius of the Triple Mirror = 2.5 mm"]
-[4.846016883850098, 8.577322959899902, "[TT] Center Frequency of the Channel 4 = 1695.7874 MHz"]
-[8.998924255371094, 4.312550067901611, "[FF] Attitude Determination of the Earth sensors, digital sun sensors, star cameras (ASTRA-1A, -1B), IRU (Inertial Reference Unit), and magnetometers = Via"]
-[10.306924819946289, 3.19669771194458, "[FF] Thesis URL of the AAUSAT3 = http://www.crn2.inpe.br/conasat1/projetos_cubesat/projetos/AAUSAT-3%20-%20Aalborg%20University%20-%20Denmark/AAUSAT-3%20-%20ADCS%20-%20Attitude%20Determination%20and%20Control%20System.pdf"]
-[6.187656402587891, 7.962099552154541, "[TT] Signal Reception Capability of the SPAISE2 = 4 channels (simultaneously 2 channels)"]
-[9.799296379089355, 8.591010093688965, "[TT] IFOV of the FTS = 10.5 km"]
-[5.399301052093506, 1.8591686487197876, "[FF] Symposium Date of the Flying Laptop = April 8-12, 2013"]
-[11.80347728729248, 5.002213478088379, "[TT] Elementary Cell Size of the ECAL = 648 mm x 9 mm"]
-[4.0661845207214355, 6.232728481292725, "[FF] Receiving Antenna Location of the Bukittinggi = To cover the far Northwest of Indonesia such as the Aceh province"]
-[10.341024398803711, 8.0134916305542, "[TT] Telescope Diameter of the DIAL Instrument = 40 cm"]
-[9.098663330078125, 1.3328115940093994, "[FF] Extended Mission Objective of the New Horizons = Study the Kuiper Belt environment, observe numerous Kuiper Belt Objects (KBOs) and Centaurs, make the first close flyby of the KBO 486958 2014 MU69"]
-[8.286200523376465, 5.328365802764893, "[FF] NRT Geolocation Accuracy of the RADARSAT-2 = Not provided"]
-[3.906914472579956, 6.431840896606445, "[TT] Ground Incidence Angle of the Antenna = 23\u00ba\u00b13\u00ba cross track"]
-[16.546602249145508, 3.643693208694458, "[TT] Production Capacity of the OneWeb Satellites = Two satellites a day"]
-[13.58536148071289, 6.003254413604736, "[TT] Average On-Orbit Power of the Solar Array = About 700 W"]
-[4.554581165313721, 1.6250941753387451, "[TT] Launch Date of the TanSat = December 2016"]
-[12.089829444885254, 6.3695831298828125, "[TT] Electron Spectrum Turnover of the AMS-02 = Beyond 30 GeV"]
-[9.511982917785645, 6.080349445343018, "[TT] Degrees of Freedom of the VISS = Six"]
-[6.993154048919678, 2.8107175827026367, "[FF] Mission Type of the SEOSAT-Ingenio = Optical Earth-observation"]
-[8.356103897094727, 7.127325057983398, "[TT] Number of Cameras of the MoonKAM = 4 on each vehicle"]
-[8.215441703796387, 0.8961693644523621, "[FF] Science Investigations of the ARTEMIS Probes = 3-D mapping of the lunar wake induced by the solar wind, Measurements of selected lunar crustal magnetic anomalies, Measurements of the lunar exosphere and surface charging, Coordinated measurements with NASA\u2019s forthcoming LADEE mission"]
-[5.74437141418457, 3.1822168827056885, "[FF] Purpose of the NPSAT-1 = Carry several experiments into orbit"]
-[9.750853538513184, 6.407101154327393, "[TT] Maximum View Angle of the MABEL = \u00b11 km"]
-[8.770450592041016, 3.5526716709136963, "[FF] Function of the CERTO/PLUS = Determine integrated ionospheric densities near the satellite orbit plane"]
-[11.792291641235352, 0.5575361847877502, "[FF] Mission Type of the PLATO = Astronomical science mission dedicated to the detection and characterization of exoplanets"]
-[9.995650291442871, 7.674426078796387, "[TT] Observation Swath of the IMI = Wider than real aperture system"]
-[7.357897758483887, 3.7392101287841797, "[FF] Purpose of the GPS Technologies = Atmospheric occultation experiments"]
-[4.607513427734375, 4.824953556060791, "[FF] Objective of the Lemur-2 = Ship tracking via AIS (Automatic Identification System) with SENSE"]
-[11.984416007995605, 4.560355186462402, "[TT] Size of the Spacecraft = 10 cm x 10 cm x 10 cm"]
-[4.909675598144531, 0.48451799154281616, "[FF] Launch Date of the MTVZA-GY = Dec. 10, 2001"]
-[4.4933576583862305, 2.5955631732940674, "[TT] Campaign Location of the KORUS-OC = East Sea (Sea of Japan), South Sea, and Yellow Sea"]
-[7.501215934753418, 3.7253687381744385, "[FF] Motion Compensation of the NightPOD = Yes"]
-[5.999610900878906, 1.5619722604751587, "[FF] Presentation Date of the Small Satellites = Oct. 2-6, 2006"]
-[5.530342102050781, 2.253995656967163, "[FF] EMC Testing Configuration of the MPO Orbiter = Mercury orbiting mode"]
-[7.367236137390137, 4.688953399658203, "[FF] Component of the Side Mount = Unknown"]
-[14.107109069824219, 7.112880706787109, "[FF] Voltage Conversion of the PCDM = Raw 28\u00b15 V battery voltage level to regulated \u00b15 V level"]
-[6.847827911376953, 0.7530637383460999, "[TT] Launch Date of the InSight = May 2018"]
-[7.9263997077941895, 8.265405654907227, "[FF] Spectral Bands of the EarthDaily Optical Imager = 6 bands in each of the visible, near-infrared (NIR) and shortwave infrared (SWIR) spectrums, and 4 in the thermal infrared (TIR) spectrum"]
-[8.039546012878418, -0.11672434955835342, "[TT] Mission Duration of the Meteor M2-2 = Five years"]
-[6.158586502075195, 4.893240928649902, "[FF] Purpose of the TTTC = Commanding tasks with parameters and time tag"]
-[6.875331878662109, 4.4490485191345215, "[FF] FDIR considers all envisaged failures that may affect the safety of the RVX mission and all the SW failures of the RVX GNC of the RVX FDIR = Parameter Value"]
-[12.456062316894531, 0.5840673446655273, "[TT] Mission Duration of the PLATO = Minimum of two years"]
-[14.078695297241211, 4.035854816436768, "[TT] Instrument Mass of the ERIP = 1.80 kg"]
-[6.341557025909424, 5.367988109588623, "[TT] Number of Elements of the Ground Segment = 2"]
-[4.963605880737305, 3.368058681488037, "[TT] Manufacturer of the GIOVE-B = GAIN (Galileo Industries S. A.)"]
-[9.528446197509766, 1.1882237195968628, "[TT] Differential Velocity of the LARES = 0.75 \u00b1 20% m/s"]
-[10.824953079223633, -0.26314231753349304, "[TT] Bistatic Phase of the TanDEM-X = October 2015 to End of the Year"]
-[4.832432270050049, 0.5879634022712708, "[TT] Launch Date of the Resurs-DK1 = 15 Jun 2006"]
-[4.053778171539307, 4.190363883972168, "[FF] Mission Stakeholder of the RADARSAT-2 = Canadian Government"]
-[8.35699462890625, 1.6928480863571167, "[TT] Sky Condition of the Arctic Ocean = Cloudy"]
-[6.46790075302124, 3.556025266647339, "[FF] Usage of the Pelican Satellites = Mapping services, environmental tasks, defense, support rescue operations"]
-[3.2916953563690186, 2.2518293857574463, "[FF] Instrument of the Copernicus Sentinel-6 = Advanced Microwave Radiometer"]
-[3.401721477508545, 5.043887138366699, "[TT] Instrument of the Tandem-L = L-band Synthetic Aperture Radar (L-SAR)"]
-[5.487182140350342, 3.873969078063965, "[TT] Quantity of the SkySat = 21 satellites"]
-[5.590673923492432, -1.9884029626846313, "[FF] Instruments of the GEO-KOMPSAT-2B = Geostationary Environment Monitoring Spectrometer (GEMS) and the Advanced Geostationary Ocean Colour Imager-II (GOCI-II)"]
-[4.519061088562012, 6.164424419403076, "[TT] Beacon Frequency of the RF Communication System = 436.8475 MHz"]
-[8.37020492553711, 9.002260208129883, "[TT] Wavelength Range of the PACS = 55\u2013210 \u00b5m"]
-[10.161663055419922, 1.3569940328598022, "[TT] Variable Stars of the Gaia = 10 million"]
-[5.600057125091553, 2.3918097019195557, "[FF] Development Program Participants of the ABEX = Over 150 undergraduate students, 7 active graduate students, 7 faculty"]
-[6.586453914642334, 0.8588785529136658, "[TT] Launch Site of the Herschel Telescope = Kourou"]
-[10.749917030334473, 7.0851240158081055, "[TT] Footprint of the ATM = 1 m"]
-[5.411662578582764, 1.0007569789886475, "[TT] Coast Phase Dates of the THEMIS Constellation = July 1 to Aug. 31, 2007"]
-[13.33200454711914, 7.823885917663574, "[TT] Maximum Power Output of the S-band transmitter = 27 dBm (0.5 W)"]
-[11.397000312805176, 8.927250862121582, "[TT] Acquisition Date of the MODIS = July 30, 2019"]
-[6.961263179779053, 7.794344425201416, "[TT] Radius of Curvature of the Primary Reflector = 3500 mm"]
-[10.758219718933105, 2.122434377670288, "[FF] EPIC Background of the XMM-Newton observatory = Higher than estimated pre-launch"]
-[14.154826164245605, 3.1541059017181396, "[TT] Mass of the IPEX-II boom = 112 kg"]
-[11.873866081237793, 3.53029465675354, "[FF] Valve Upgrade of the Propulsion System = Number and Flow Capacity"]
-[10.951577186584473, 7.560914039611816, "[TT] Swath Width of the MSU-SK = 600 km"]
-[14.197942733764648, 3.280526876449585, "[TT] Mass of the M2S = 848 kg"]
-[6.080968856811523, 2.684817314147949, "[FF] Workshop Location of the RECCAP-2 = Gotemba, Japan"]
-[6.566900253295898, 7.540639877319336, "[TT] Signal Conversion of the MEV = 12 bit"]
-[7.683361053466797, 4.50870943069458, "[FF] Device Type of the SEM = High energy particles"]
-[5.650764465332031, 0.6463404893875122, "[FF] Announcement Date of the UrtheCast = July 16, 2014"]
-[11.799579620361328, 0.07918907701969147, "[FF] Mission Objective of the TESS = Search for extrasolar planets using the transit method"]
-[8.658637046813965, 7.6210455894470215, "[TT] Array Size of the CMOS Active Pixel Sensor = 1.3 mega pixel (1280 x 1024)"]
-[11.981338500976562, 6.46064567565918, "[FF] Spectra Hardening of the AMS-2 = Above 200 GV"]
-[8.003101348876953, 4.645680904388428, "[FF] Authors of the Multichannel Autocalibration = Luiz F. G. Dos Santos, Souvik Bose, Valentina Salvatelli, Brad Neuberg, Mark C. M. Cheung, Miho Janvier, Meng Jin, Yarin Gal, Paul Boerner and At\u0131l\u0131m G\u00fcne\u015f Baydin"]
-[9.828055381774902, 7.710790157318115, "[TT] Hubble Space Telescope Images Containing Satellite Streaks of the Starlink = Currently 8% of all images"]
-[7.936622142791748, 6.002833843231201, "[FF] Instrumentation of the BIROS = BIROS optical payload, comprising three pushbroom cameras"]
-[5.02797269821167, 8.36210823059082, "[TT] IF Bandwidth (MHz) of the Antenna = 400"]
-[10.09837818145752, 7.879899024963379, "[TT] Spatial Resolution of the DST (Dobson Space Telescope) = 6 m"]
-[8.034025192260742, -0.9616088271141052, "[FF] Global Sampling of the ICESat-2 = Dense"]
-[6.184221267700195, 6.309398174285889, "[FF] Type of the `Hybrid' DCPs = Combination of `alert' and `self-timed' DCPs"]
-[7.272267818450928, 5.330081939697266, "[FF] Function of the MWI = Measure the distance change between the two satellites"]
-[5.670914173126221, -0.8315101861953735, "[TT] Design Life of the SPOT-3 = Four years"]
-[6.714778423309326, 3.58187198638916, "[FF] Successor Instruments of the TES = CrIS instrument on the NOAA-NASA Suomi-NPP satellite and the IASI series"]
-[7.027309894561768, 4.950640678405762, "[FF] Variable Retardance with Applied Voltage of the LCVR = Unknown"]
-[12.617680549621582, 9.093541145324707, "[TT] Local Equator Crossing Time of the PARASOL = 13:30"]
-[10.889687538146973, 7.507392406463623, "[TT] Swath Width of the OMI = 2600 km to 725 km"]
-[4.478363513946533, 2.8999640941619873, "[TT] Location of the GIEN (GESS at IEN) = INRiM, Turin Italy"]
-[14.672342300415039, 6.710141181945801, "[TT] Battery Configuration of the NightPod = Two batteries connected in series"]
-[4.838613986968994, 3.234466552734375, "[TT] Operator of the CASA-212-200 aircraft = Spanish National Institute for Aerospace Technology (INTA)"]
-[6.696974754333496, 0.032654520124197006, "[TT] Measurement Duration of the CryoSat-2 = Seven months"]
-[11.239439964294434, 5.399240970611572, "[TT] LYSO crystals of the Range Calorimeter = Height of 4 cm"]
-[10.300731658935547, 5.870259761810303, "[TT] Temperature Sensitivity of the NEDT (Noise Equivalent Differential Temperature) at 300 K - Band 4 - Band 5 - Band 6 = \u2264 1 K \u2264 0.2 K \u2264 0.2 K"]
-[8.585916519165039, 7.709203720092773, "[TT] Peak Power of the 4-band CCD Imager = 30 W"]
-[11.734139442443848, 4.874171733856201, "[TT] Diameter of the Cathode diameter = 7 mm"]
-[8.844420433044434, 5.824779033660889, "[FF] Measurement of the SCM = Insulator surface potential"]
-[4.632933616638184, 7.792571544647217, "[TT] Clock Rate of the DPSK Transmitter = 2.88 GHz"]
-[11.784341812133789, 3.3030669689178467, "[TT] Thrust of the LAM = 440 N"]
-[9.44989013671875, 3.8128035068511963, "[TT] Purpose of the Magnetometers (MAG) = Earth magnetic field information"]
-[8.573387145996094, 8.613612174987793, "[TT] Instantaneous spectral coverage of the Spectrometer = 1.53 km/s"]
-[6.2801008224487305, 4.628891468048096, "[FF] Components of the MCS = Database and associated programs"]
-[9.212876319885254, 3.0636065006256104, "[FF] Instrumentation of the IMPACT = Solar wind electron and solar energetic particle instrumentation"]
-[10.080446243286133, 8.202369689941406, "[FF] Pre-Flight Performance Characterization of the Medium-sized Aperture Camera = Unknown"]
-[10.343578338623047, 7.1673583984375, "[TT] Data Product Grids of the OSCAT-2 = 25 km and 50 km"]
-[5.493524551391602, 6.127176761627197, "[TT] Memory of the AIM = 128 k x 16 EEPROM for boot and application code"]
-[18.644689559936523, 3.9394800662994385, "[TT] NE\u0394T of the 1 = 0.4 K"]
-[8.508561134338379, 6.904582500457764, "[TT] Imaging Capacity of the Raytheon's Payload = Triples to quadruples the company's capacity to image high-demand areas"]
-[10.878642082214355, 3.5330936908721924, "[TT] Size of the Standard 3U CubeSat = 100 x 100 x 340.5 mm"]
-[8.191508293151855, 3.9113926887512207, "[FF] Unknown of the ASME (Advanced Surface Material degradation Experiment) = Unknown"]
-[11.786516189575195, 6.657677173614502, "[TT] Range of the Incident Particle Energy Range = > 20 MeV (H), > 87 MeV/nucleon (Fe)"]
-[5.071561336517334, 6.588936805725098, "[TT] Design of the Transceivers = Dual receive (Rx)/transmit (Tx)"]
-[3.5557668209075928, 6.487332820892334, "[FF] Antenna Size of the WCOM = Large"]
-[4.915332794189453, 3.427558660507202, "[TT] Manufacturer of the STX = Clyde Space"]
-[3.9066247940063477, 6.585097312927246, "[TT] Type of the Antenna = Dual-feed collocated UHF and L-band antenna"]
-[8.807703018188477, 6.8413262367248535, "[FF] Image Size in Kilometers of the ABI = Based on the conversion factor of 28 \u00b5rad/km"]
-[11.13274097442627, 5.901392459869385, "[TT] Shielding Material Transparency of the CZTI = More transparent above 100 keV"]
-[4.571219444274902, 7.8630499839782715, "[TT] LO Frequency (MHz) of the HRIT HiRID = 1900"]
-[9.060747146606445, 0.5053223967552185, "[TT] Transfer Trajectories to Lunar Orbit of the ARTEMIS = February and March 2010"]
-[10.596056938171387, 5.519075870513916, "[FF] Operation Sensitivity of the Electron Temperature Probe = Less sensitive to the potential sheath structure of its enveloped electrodes"]
-[6.271079063415527, 5.349193572998047, "[FF] Interface of the DACU = BDH unit"]
-[10.471829414367676, 2.260643720626831, "[TT] Mirror Modules of the eROSITA X-ray telescope = 7"]
-[11.686580657958984, 4.580795764923096, "[TT] Diameter of the Didymos = 780 meters"]
-[7.346614360809326, 7.826712131500244, "[TT] Sensitivity of the DPS = 0.5 dB"]
-[3.562432050704956, 4.434802055358887, "[TT] Operation End Year of the SAR-Lupe = 2017"]
-[6.368902683258057, 1.4522608518600464, "[TT] Constellation Status of the Astrocast = Up and running in space"]
-[6.162444114685059, 4.452301502227783, "[FF] Commanding Management of the Ground Schedule Execution System = Nominal"]
-[8.0031156539917, 5.136044979095459, "[FF] Required Precision of the NO2 = 1.00"]
-[12.038315773010254, -0.3737461268901825, "[TT] Mission Extension of the TESS = 2025 and beyond"]
-[4.14280891418457, 5.768973350524902, "[TT] Quantity of the ADS-B Receivers = 12,000+"]
-[11.831510543823242, 4.734208106994629, "[TT] Size of the CEASE-1 = 10 cm x 10 cm x 8.2 cm"]
-[7.612069129943848, 9.002103805541992, "[TT] Spectral Range (\u00b5m) of the Band 8 = 0.48 - 0.53"]
-[8.662413597106934, 3.6640419960021973, "[FF] Measurement of the DIARAD/VIRGO = Total Solar Irradiance"]
-[10.320873260498047, 5.333571910858154, "[FF] Polyimide tape of the Solution = Added to the radiator and chassis in areas where the SMAs may make contact"]
-[9.326464653015137, -0.7497925162315369, "[TT] Quantity of the GEOS-2 = 1"]
-[3.811065196990967, 7.926105499267578, "[TT] Architecture of the DPSK Transmitter = MOPA"]
-[7.162275314331055, 6.588869094848633, "[TT] Detection Threshold of the GLM = 25"]
-[9.2424898147583, 3.209211826324463, "[FF] Purpose of the TESIS = Registration of solar images in narrow spectral bands and monochromatic emission lines of HeII, SiXI, FeXXI \u2013 FeXXIII, MgXII ions in high temperature plasma of the transition region and corona"]
-[13.826193809509277, 3.109834671020508, "[TT] Payload Mass at Liftoff of the LARES-2 = 296 kg"]
-[3.38545298576355, 5.170958042144775, "[TT] BAQ Option of the RISAT-SAR = 2-6 bits"]
-[4.74543571472168, -1.1864972114562988, "[FF] Launch Schedule of the Shenzhou XV = This year"]
-[7.270392417907715, 1.8671084642410278, "[TT] Ground Sample Distance of the Carbonite-1 = 1 m"]
-[7.238339424133301, 4.620145320892334, "[FF] Mounting of the OPSE = Set of screws and spacers"]
-[4.453790187835693, 4.93896484375, "[FF] Purpose of the COSPAS-SARSAT system = Detect and locate transmissions from emergency beacons carried by ships, aircraft, or people"]
-[5.998295783996582, 5.502413749694824, "[TT] Redundancy of the Data Recording System = Dual-redundant"]
-[5.9812421798706055, 3.28190279006958, "[TT] Data Receiver of the TRMM = NASA/GSFC and JAXA/EORC (Earth Observation Research Center)"]
-[7.169513702392578, 4.571305274963379, "[FF] Mounting of the SOLCON-3 = HH Single Bay Pallet (SBP) on top of the HH MPESS"]
-[6.36182165145874, 2.597869396209717, "[TT] Managing Organization of the Solar Probe Cup (SPC) = SAO (Smithsonian Astrophysical Observatory)"]
-[8.711468696594238, 8.84360122680664, "[TT] Grating Type of the MEGS = Dual, holographic, spherical grating"]
-[9.158205032348633, 5.423519611358643, "[TT] Accuracy of the 2-axis gimbal = 0.1\u00ba"]
-[3.1236612796783447, 3.9222490787506104, "[TT] Decommissioned Date of the GEOSAR GOES-7 = April 1, 2003"]
-[3.466515302658081, 4.873922348022461, "[FF] Performance Prediction of the SAR Sensor = Simulation in the system design stage"]
-[14.02702808380127, 3.996506452560425, "[TT] Quantity of Proof Masses of the Electrode Housing Box = 1"]
-[5.607401371002197, 6.573773384094238, "[TT] Daily Capacity of the EDRS-A node = 5.4 TB/day"]
-[9.717782020568848, 0.31647035479545593, "[TT] Proximity GPS Approach of the Mango and Tango = 2 m in Dec. 2010"]
-[10.417991638183594, 1.8220417499542236, "[TT] Function of the NuSTAR = Revealing what lies around the most buried supermassive black holes"]
-[4.799727916717529, 0.15011322498321533, "[TT] End of Life Date of the Buccaneer = 18 November 2022"]
-[5.662168025970459, 5.674934387207031, "[TT] Processor Type of the SCP = Honeywell VHSIC MIL-STD-1750A microprocessor"]
-[9.993852615356445, 0.1536140888929367, "[FF] Distance Between Satellites of the GRACE = Varies ever so slightly depending on the mass of Earth\u2019s surface below"]
-[5.092901706695557, 3.2919232845306396, "[TT] Manufacturer of the iADCS-100 = BST (Berlin Space Technologies) and Hyperion Technologies B.V."]
-[9.878876686096191, 1.7769747972488403, "[TT] Speed of Particles of the SS 433 = Close to a quarter the speed of light"]
-[13.606371879577637, 1.747403621673584, "[TT] Returned Cargo Weight of the Dragon cargo spacecraft = More than 4,000 pounds (1950 kg)"]
-[8.958571434020996, 4.798377990722656, "[TT] Sensor Quantity per Spacecraft of the Tri-TIP = 2"]
-[4.427373886108398, -1.6424148082733154, "[FF] Data of the INTEGRAL\u2019s spectrometer (SPI) = More than 600 individual observations of the nebula"]
-[7.03789758682251, 7.0091657638549805, "[FF] Energy Levels of the Laser002 = Increased and started to oscillate"]
-[4.942885875701904, 5.149011135101318, "[TT] Protocol ID of the GRDDP = 238"]
-[10.406153678894043, 3.250694751739502, "[TT] Number of CubeSat Units of the ChargerSat-1 = 1"]
-[3.3714725971221924, 5.346063137054443, "[TT] Center Frequency of the SAR Antenna = 5.405 GHz"]
-[4.438998222351074, 0.5498916506767273, "[TT] Launch Date of the COSPAS-1 = June 29, 1982"]
-[7.1465959548950195, 6.90811824798584, "[TT] Beam Accuracy of the Metrology Laser = \u2264 130 \u00b5m"]
-[8.800960540771484, 7.127204418182373, "[TT] PAN-F of the CartoSat-1 = Panchromatic Forward-pointing Camera"]
-[7.57877779006958, 6.127840042114258, "[FF] Function of the On-board Processor = Real-time radiometric/geometric calibration and image compression for all imaging data"]
-[8.74920654296875, 1.7774629592895508, "[FF] Wind Speed of the Hurricane Sam = 230 kilometers (145 miles) per hour"]
-[6.295716762542725, 4.437615394592285, "[FF] Verification Process of the ASAP = Closed loop manner, take over control of the satellite by manipulating SONATE\u2019s active command list"]
-[5.972176551818848, 4.218566417694092, "[FF] Function of the TSCT = Allows users to have a real-time interface to the TripleSat constellation database, realizing the enquiry of the data catalog, and purchase of data products online"]
-[9.328789710998535, 3.5208888053894043, "[FF] Objective of the Cluster S/C = Provision of intercalibrated measurements of the magnetic field vector B"]
-[6.449802398681641, 5.835203170776367, "[TT] Number of Paths of the Payload Hosting Paths = Two"]
-[7.642551422119141, 4.949897766113281, "[FF] Navigation Information Utilization Time of the Lander = Unknown"]
-[8.288736343383789, -0.5419126152992249, "[TT] Length of the Glacier = About 13 miles"]
-[8.543587684631348, 5.500059127807617, "[TT] Later Position Accuracy of the Transit Navigation = 15 to 25 meters"]
-[7.62280797958374, 8.837839126586914, "[TT] Spectral Band of the MSU-E = 0.5 - 0.6 \u00b5m"]
-[8.659369468688965, 2.9438982009887695, "[FF] Purpose of the SFx = Researching and characterizing the MEO space weather effects on spacecraft electronics and materials"]
-[14.266325950622559, 3.1996283531188965, "[TT] Mass of the Enxaneta = ~10 kg"]
-[7.905905723571777, 0.176439568400383, "[FF] Data Collection of the GRACE = Monthly variations of the Earth gravity field"]
-[10.911401748657227, 10.092607498168945, "[FF] Debris Shield of the Alpha Magnetic Spectrometer (AMS) = Removed and jettisoned"]
-[14.141467094421387, 3.257659673690796, "[TT] Device Mass of the TCU/TRC = 2 kg, 0.2 kg"]
-[8.070602416992188, 1.0897116661071777, "[TT] Timing of the Calbuco Volcano Eruption = April 2015"]
-[4.830070495605469, 0.7886060476303101, "[TT] Operation End Date of the PROBA-2 = December 31, 2016"]
-[12.020374298095703, -0.3526368737220764, "[FF] Event Start Date of the TESS = September 26, 2019"]
-[7.671875476837158, 8.166022300720215, "[TT] Color of the Electronics Mainboard = Green"]
-[7.8541340827941895, 7.067537784576416, "[TT] Data Recording of the Gamma Detectors (XGRE) = On triggering alerts only"]
-[9.102158546447754, 7.30718469619751, "[TT] Resolution of the DMAC = High-resolution"]
-[9.745942115783691, -0.5554341673851013, "[TT] Orbit Altitude of the ISS = ~400 km"]
-[13.437276840209961, 5.459653377532959, "[FF] Solar Arrays of the TacSat = Thin Film"]
-[8.31412410736084, 8.708661079406738, "[TT] Spectral Resolution of the MEGS = 0.1 nm"]
-[4.191963195800781, 0.6211315989494324, "[FF] Article Date of the INTEGRAL = 2016 April 1"]
-[11.488897323608398, 3.109610080718994, "[TT] Mission Duration of the Electric Thruster = 2.5 years"]
-[8.541687965393066, 5.196446895599365, "[TT] Measurement Range XACC axis of the GFO Accelerometer = \u00b15 x 10-4ms-2"]
-[11.87291431427002, 6.64729642868042, "[TT] Proton Energy Range of the HIPS = 30-300 MeV"]
-[7.959925651550293, 8.586149215698242, "[TT] Spectral Range of the TIR = 8.4-8.5, 10.3-11.3, 11.5-12.5 \u00b5m"]
-[10.783926963806152, 3.915587902069092, "[FF] Drag Sail Deployment Date of the CanX-7 = May 4, 2017"]
-[6.871732234954834, 5.365420341491699, "[FF] Components of the MCCM = Thin film passive circuits, MMIC low-noise amplifiers (LNAs), phase shifter and attenuator chips, ASICs and other discrete components for control and telemetry"]
-[7.049022674560547, 6.066936016082764, "[TT] Instrument Count of the GOES-S = 6"]
-[10.754063606262207, -1.14103364944458, "[FF] Atmospheric Model of the SLATS = NRLMSISE-00"]
-[4.428014278411865, 7.795146942138672, "[TT] Downlink Data Rate of the L-3 Communications Cadet UHF nanosatellite radio = 3 Mbit/s"]
-[11.900458335876465, 3.0934078693389893, "[TT] Delta V of the Satellite = 100 m/s"]
-[9.791357040405273, -0.2818187475204468, "[TT] Freezing Level Height of the GPM = Higher than 4 km"]
-[4.323141098022461, 2.9987165927886963, "[FF] Location of the SAR-VTB = Svalbard site on Spitsbergen in the Norwegian Arctic"]
-[6.897263050079346, 6.82554817199707, "[FF] Implication of the Yaw Rotation Option = Reduces the requirement of the number of beams by half"]
-[8.638765335083008, 0.7274672985076904, "[FF] Impact Point of the Vikram Lander = Unknown"]
-[10.750580787658691, 1.4569844007492065, "[TT] Black Hole Mass of the OJ 287 galaxy = 18 billion times the mass of our Sun"]
-[6.845794677734375, 1.9386250972747803, "[TT] Images Collected per Day of the Landsat-8 = Approximately 1,500"]
-[5.017426490783691, 3.511679172515869, "[TT] Manufacturer of the LISS-II Camera = ISRO"]
-[5.693522930145264, 6.986912250518799, "[TT] Data Stream of the DMSP RTS Mux = 3.072 Mbit/s"]
-[8.415578842163086, 7.207617282867432, "[TT] Number of CCD cameras of the AMI = 2"]
-[7.800357341766357, 5.761950969696045, "[TT] Instrument of the WSF-M = Passive microwave imaging radiometer"]
-[6.91579008102417, -0.7716339826583862, "[TT] Orbit Shape of the WD 1856 b = Elliptical"]
-[6.78026819229126, 5.112672805786133, "[FF] Function of the PMC = Controls all PLM equipment and instruments"]
-[4.94950532913208, 3.208143472671509, "[TT] PI of the CIXS = M. Grande, University of Wales, Aberystwyth, UK"]
-[6.235459327697754, 6.452554225921631, "[TT] Transmission Duration of the Alert DCPs = About 10 seconds"]
-[4.973748683929443, 3.2863998413085938, "[TT] Manufacturer of the QBSout-1S = University of Maryland"]
-[8.129157066345215, 7.520746231079102, "[TT] SNR of the Imager = PAN: \u226548 dB, MS: \u226548 dB"]
-[3.2068839073181152, 1.7576061487197876, "[TT] Data Collection of the Sentinel-2C = 1.5 TB/day"]
-[6.607064723968506, 1.7094216346740723, "[FF] URL of the Rosetta = http://www.esa.int/spaceinimages/Images/2015/08/Rosetta_thermal_louvres"]
-[4.954467296600342, 0.4907940626144409, "[TT] Launch Date of the SwissCube = 2009"]
-[9.578752517700195, 2.7294681072235107, "[TT] Launch Year of the Solar X-ray Spectrometer = 2021"]
-[13.433938980102539, 2.903546094894409, "[TT] Mass of the IITMSAT = 11 kg"]
-[8.448295593261719, 9.011008262634277, "[FF] Observation Wavelengths of the Herschel = 70 \u00b5m (blue), 160 \u00b5m (green) and 250 \u00b5m (red)"]
-[5.79760217666626, 3.0834860801696777, "[TT] Fundraising Goal of the Inspiration4 = $100 million"]
-[13.044034957885742, 7.05729341506958, "[TT] Payload Total Power Requirement of the WCOM = 1300 W"]
-[3.9948296546936035, 3.475890874862671, "[FF] Development of the Galileo App = Internal Competition for ESA Trainees"]
-[5.2026166915893555, 3.6671664714813232, "[TT] Provider of the ADCS = CNES"]
-[6.812341690063477, 5.146297454833984, "[FF] Composition of the NISP Warm Electronics = Two Data Processing Units (NI-DPU) and one Instrument Control Unit (NI-ICU)"]
-[12.207868576049805, -0.21309995651245117, "[TT] Image Frequency of the TESS = Every 30 minutes"]
-[3.149869680404663, 2.2682907581329346, "[FF] Mission Purpose of the Copernicus Sentinel-2 = Mapping differences in land cover, understanding the landscape, mapping how it is used, monitoring changes over time"]
-[5.704352378845215, 3.1051056385040283, "[FF] Expected Profitability of the Astrocast = Loss-making for at least 2022 and 2023"]
-[10.09980583190918, 1.3628321886062622, "[TT] Light Travel Time of the Quasar = More than four billion years"]
-[8.479194641113281, 5.5172319412231445, "[TT] Precision of the Satellite Position = < 10 cm (rms)"]
-[5.6277031898498535, 1.1912517547607422, "[FF] Lift-off Date of the Foton microgravity mission = Sept. 14, 2007"]
-[10.548489570617676, 7.259475231170654, "[TT] Trace H of the APIS Device = 175.2 km"]
-[9.731706619262695, 8.314706802368164, "[TT] FOV in Cross-Track Direction of the MSU-100 = 31\u00ba, 62\u00ba"]
-[10.920792579650879, 10.072982788085938, "[FF] Positron Fraction Measurement of the Alpha Magnetic Spectrometer = 0.5\u2013500 GeV"]
-[7.1925249099731445, 5.569456577301025, "[FF] Quantity of the MTVZA = 1"]
-[4.67793083190918, 7.215958595275879, "[TT] Ka-band of the Downlink communications = 278 Mbit/s (QPSK)"]
-[7.126817226409912, 6.642719268798828, "[FF] Data Output of the GLM instrument = Consists primarily of events, not images"]
-[11.068288803100586, 5.45925235748291, "[TT] Type of the Gamma-radiation detector = Gamma-radiation"]
-[7.721790313720703, -0.8688339591026306, "[FF] Publication Date of the ICESat-2 = 9 December 2020"]
-[6.313568592071533, 3.328815221786499, "[TT] Number of satellites in its constellation by early 2021 of the BlackSky = 16"]
-[9.634903907775879, 4.073868274688721, "[TT] Magnetic Field of the SWFO-L1 = +10"]
-[11.350488662719727, 5.859803199768066, "[TT] Structure Material of the ESTCube-1 & -2 = Aluminum (alloy AW 6082-T6)"]
-[7.8199543952941895, 2.5765562057495117, "[FF] Application of the OLCI = Supporting global land and ocean monitoring services"]
-[3.5807137489318848, -0.9810312390327454, "[FF] Orbit Type of the Secondary Payloads = Near-circular orbit"]
-[5.647401809692383, 4.637780666351318, "[TT] Operation of the Net Technology = Successful"]
-[6.1118950843811035, 4.57267951965332, "[FF] Objective of the DATA-CHASER = Demonstrate distributed, interactive and intelligent control approaches"]
-[8.353909492492676, 7.102683067321777, "[TT] Quantity of Cameras of the Earth Observation Compartment = 3"]
-[12.119864463806152, -0.3427850008010864, "[FF] Operations of the TESS spacecraft = Single 4 hr downlink & repoint every 2 weeks"]
-[8.45589828491211, 7.375589370727539, "[TT] Control of the CMOS Camera = I2C I/F"]
-[6.575474262237549, 2.979043483734131, "[FF] Design, Development and Testing of the TSIS-1 = University of Colorado CU/LASP (Laboratory for Atmospheric and Space Physics), Boulder, CO"]
-[12.045938491821289, 4.541399002075195, "[TT] Payload Volume of the Spacecraft = 46 cm x 46 cm x 25 cm"]
-[8.347060203552246, 8.50911808013916, "[TT] Wavelength Range of the Imaging Spectrometer = 1.61 - 1.68 \u03bcm"]
-[8.19743537902832, 3.5396273136138916, "[TT] Measurement Target of the OCO-3 = Sunlight reflected off the Earth's surface"]
-[4.875173568725586, 1.2303296327590942, "[FF] Launch Dates of the GPSPAC = LS-4, LS-5 in March 1984, DoD host vehicle satellites in 1983 and 1984"]
-[8.767992973327637, 5.986233711242676, "[TT] Maximum Misalignment of the Optical Sensor Systems = 0.001\u00ba"]
-[9.762929916381836, -0.16641446948051453, "[TT] Altitude at Supersonic Parachute Opening of the Experiment Data = 25 km"]
-[7.339798450469971, 3.494403123855591, "[FF] Measurement Frequency of the Satellite = Twice per day"]
-[8.558027267456055, 5.5652689933776855, "[TT] Precision of the Satellite Position = < 1.5 m (rms)"]
-[5.077764987945557, -0.3630179464817047, "[TT] Launch Date of the CBERS-4A = Dec 23, 2019"]
-[14.30012035369873, 3.21197772026062, "[TT] Mass of the CBERS-4A = 1,730 kg"]
-[7.0890069007873535, 4.6719465255737305, "[FF] Point of No Return of the Event Horizon = The point of no return"]
-[5.331590175628662, 0.76178377866745, "[FF] Operation Start Date of the TET-1 = Oct. 16, 2012"]
-[9.430540084838867, 6.923142910003662, "[TT] Intrinsic Range Resolution of the KaRIn = 75 cm"]
-[6.1884379386901855, 4.308134078979492, "[FF] Selected by ESA of the Hylas-3 Ka-band payload = Unknown"]
-[6.925837993621826, 6.996960163116455, "[TT] Quantity of the Laser Beams = 6"]
-[6.808407306671143, -0.5919066071510315, "[TT] General Program Duration of Observation of the SVOM = 1 orbit minimum"]
-[8.505023002624512, 4.710655212402344, "[TT] Manufacturer of the Star Trackers = Leonardo"]
-[8.097185134887695, 6.299263000488281, "[TT] Range Precision of the ATLAS = < 20 cm"]
-[7.869576930999756, -2.497223377227783, "[FF] Observation of the GOLD = Planet-scale waves in the lower atmosphere"]
-[14.26897144317627, 3.160379409790039, "[TT] Mass of the S/C = 125 kg"]
-[4.5293354988098145, 3.326765298843384, "[TT] Data Retrieval Location of the FOS = Ground stations"]
-[5.234603404998779, 8.450629234313965, "[TT] Tunable Bandwidth of the Wideband Radiometer = 6-40 GHz"]
-[7.052642345428467, -0.3393056094646454, "[TT] Tracking Time of the MarCO-B = Several More Weeks"]
-[8.067286491394043, 5.452555179595947, "[FF] Function of the Translation Stage = Shift the alignment of the center of mass relative to the center of pressure"]
-[9.408132553100586, 3.6912026405334473, "[FF] Objective of the NewMag = Measure electrical currents and perturbations in the Earth's magnetic field"]
-[7.87861442565918, 3.9999630451202393, "[FF] Optimization Diameter of the Internal Occulter = 1.02 Rsun"]
-[3.581613779067993, 5.1748433113098145, "[TT] Minimum Looks in Range of the Radar = 12 looks for 3 km cells"]
-[9.502141952514648, 0.9585217237472534, "[FF] Landing Speed of the OMOTENASHI = Approximately 30 m/s"]
-[5.150414943695068, 0.3595885932445526, "[TT] End of Nominal Operations of the Aeolus = 30 April 2023"]
-[9.445928573608398, 4.735289096832275, "[FF] Architecture of the Attitude Control System = FPGA Based"]
-[11.271275520324707, 0.9708386659622192, "[FF] Development and Qualification of the LISA Pathfinder Cage and Vent Mechanism = B. Zahnd, M. Zimmermann, R. Sp\u00f6rri, \"LISA Pathfinder Cage and Vent Mechanism : Development and Qualification,\" Proceedings of the 15th ESMATS (European Space Mechanisms and Tribology Symposium) 2013, Noordwijk, The Netherlands, Sept. 25-27, 2013, ESA, SP-718"]
-[4.685773849487305, 0.5303062796592712, "[TT] Launch Date of the GOES-T = Early 2022"]
-[8.685418128967285, 3.638761281967163, "[FF] Information Source of the Remote Sensing = Reflected light in the solar domain"]
-[13.387959480285645, 7.320613861083984, "[TT] Power of the LIMS = 27 W"]
-[6.557440757751465, 6.929698467254639, "[TT] Duty Cycle of the LINAS = 10%"]
-[9.489606857299805, 3.939131259918213, "[FF] Measurement Principle of the OVM = Proton magnetic resonance"]
-[9.418233871459961, 8.183292388916016, "[FF] Edition of the Introduction to Fourier Optics = 4th"]
-[14.229475975036621, 3.208359479904175, "[TT] Mass of the CP5 = 1.1 kg"]
-[6.405998229980469, 5.661754608154297, "[FF] Conference Presentation of the Lunar Laser Communication Demonstration = Unknown"]
-[6.459336280822754, 7.587563514709473, "[TT] Data of the Data quantization = 10 bit"]
-[10.149662017822266, 5.78354024887085, "[TT] HgCdTe Detectors Cooling Temperature of the MVIRI = 90 K"]
-[10.409029006958008, 5.942935466766357, "[TT] Calibration Target Temperature Difference of the MTVZA-GY Antenna System = 50-60 K"]
-[13.441278457641602, 6.8086042404174805, "[TT] Power Generation of the Spacecraft = 5.2 kW"]
-[7.983741283416748, 5.805908679962158, "[FF] Purpose of the Low-Resolution Video Camera = Spot the general location of interest"]
-[8.690814971923828, 6.437499523162842, "[TT] Range Looks of the HRS = Up to 2"]
-[11.871322631835938, 4.897764205932617, "[TT] Dimensions of the Trius SX9 = 70 mm long and 75 mm in diameter"]
-[9.07128620147705, 4.436272621154785, "[TT] Sun Protection of the AOCS = Always guaranteed"]
-[5.068023681640625, 3.3405637741088867, "[TT] Manufacturer of the SPL = Astro und Feinwerktechnik Adlershof GmbH"]
-[12.677741050720215, 7.577746391296387, "[TT] Instrument power of the Optical System = 200 W"]
-[9.762030601501465, 7.933801651000977, "[TT] Adjustment of the Active Optics =  Misalignment"]
-[5.240695953369141, 0.08306048810482025, "[TT] Retirement Date of the Ikonos = March 31, 2015"]
-[8.204049110412598, 3.1775476932525635, "[FF] Purpose of the SOLSE-2 = O3 retrievals in the lower stratosphere"]
-[9.36977767944336, 8.616421699523926, "[TT] Slit Dimensions of the Imaging Subsystem = 1/2 x 5 arcmin"]
-[8.354701042175293, 1.9312084913253784, "[TT] Sea Surface Temperature Accuracy of the SMMR = 2 K"]
-[8.909811019897461, 7.165848255157471, "[TT] Stripmap Mode Resolution of the Payload = 1-3 m"]
-[9.288201332092285, 3.1518802642822266, "[FF] Unknown of the Genesis Solar Wind Concentrator = Unknown"]
-[9.502486228942871, 3.8872017860412598, "[FF] Measurement Method of the OVM = Proton Larmor precession in a weak magnetic field"]
-[5.56113338470459, 6.373676776885986, "[TT] On-board data storage of the Second generation spacecraft UK-DMC-2 and Deimos-1 = HSDR (High Speed Data Recorder) capable of storing up to 8 GByte worth of data"]
-[10.93054485321045, 6.361440181732178, "[TT] Substrate Material of the Primary Mirror = Fused silica"]
-[14.273158073425293, 3.1732418537139893, "[TT] Mass of the Lemur-2 = 4.5 kg"]
-[8.390716552734375, 6.913845539093018, "[FF] Spatial Resolution of the ABI = Higher than the current imager generation of GOES-N to -P"]
-[4.600909233093262, 7.396376609802246, "[TT] UHF Downlinks of the UoSAT-12 = 3"]
-[3.410947561264038, 1.985079288482666, "[FF] Orbit Analysis and Control of the Sentinel-1 = Unknown"]
-[14.240036964416504, 3.252042770385742, "[TT] Mass of the HSC-III = 2 kg"]
-[6.167728424072266, 4.724290370941162, "[TT] Type of the FY-1C = Feng Yun-1C"]
-[9.72449016571045, 7.150274753570557, "[TT] Cross-track resolution of the L-band = 35-75 km"]
-[8.406628608703613, 7.806581974029541, "[TT] Image Displacement of the Quad-cell = <10 -2\u03c0 sensitivity"]
-[14.218174934387207, 3.323564052581787, "[TT] Mass of the FIBOS = Less than 120 g"]
-[4.904646873474121, 0.513785719871521, "[TT] Launch Date of the TET-1 = 2012"]
-[11.891633033752441, 6.632572650909424, "[FF] Energy Channels of the GALS-VE = > 600 MeV, > 800 MeV, > 1200 MeV"]
-[5.506168365478516, 6.008806228637695, "[TT] Data Transmission Subsystem of the EOS = PDTS"]
-[6.009397983551025, 3.066117286682129, "[FF] Reporting Structure of the NPOESS = Tri-agency office reporting through NOAA to an Executive Committee of representatives from DOC, DoD and NASA"]
-[8.099979400634766, 2.6717677116394043, "[FF] Goal of the RAIDS = Obtain a set of simultaneous airglow profiles at a number of wavelengths"]
-[8.261457443237305, -0.7207558751106262, "[TT] Spatial Resolution of the Ice sheets Ice vertical movements = 100-1000 km"]
-[9.22329330444336, 7.036136627197266, "[TT] Spatial Resolutions of the FGM = About 200 or 100 m"]
-[6.537761688232422, 5.335235118865967, "[FF] Data Flows of the DCS = Unknown"]
-[5.622976779937744, 5.046726703643799, "[TT] Onboard Computer of the Corvus-BC satellites = ARM A8 Linux-based"]
-[5.727200031280518, -0.8835777640342712, "[TT] Lifetime of the Design life = 10 years"]
-[6.634359359741211, 3.554957866668701, "[FF] Data Collection Method of the EARS-ASCAT = Collects ASCAT instrument data from MetOp satellite passes via a network of Direct Readout stations"]
-[13.532776832580566, 2.872528076171875, "[TT] Plasma Density of the Spacecraft = 109 to 1012 m-3"]
-[6.55783224105835, 4.346924781799316, "[FF] Status of the LND = Turned on for testing"]
-[10.90339469909668, 2.0913147926330566, "[TT] Science Data Processing Center of the XMM-Newton = XMM-Newton Survey Science Center at the University of Leicester, England"]
-[8.386077880859375, -2.041269063949585, "[TT] Orbit Position of the GOLD = Geostationary"]
-[10.954715728759766, 6.360957145690918, "[TT] Tertiary Mirror Material of the NAOMI = SiC"]
-[10.471735954284668, 4.791606426239014, "[FF] Attachment Method to SA panel of the Superelastic Springs = Riveted and directly soldered"]
-[1.935010313987732, -0.4042128026485443, "[TT] Expected Operation Duration of the Van Allen Probes = Two years"]
-[3.923253297805786, 2.012207508087158, "[TT] Satellite Launch Vehicle of the Kleos S.A. = SpaceX Falcon 9"]
-[4.226463317871094, 0.12190231680870056, "[TT] Timeline of Events of the SpaceX Falcon-9 = 93 milliseconds from the first sign of anomalous data to the loss of the second stage"]
-[4.888590335845947, 3.8040308952331543, "[TT] Owner of the Deep Space Tracking Antenna = China"]
-[4.343384265899658, 1.2851417064666748, "[TT] Launch Date of the SEOSAT-Ingenio = 24 August 2020"]
-[8.759862899780273, 5.768652439117432, "[TT] Adjustment factor of the ADEOS/TOMS = 1.000"]
-[5.540449619293213, 1.3847801685333252, "[TT] Delivery Date to JAXA of the PROCYON = November 2014"]
-[4.980920791625977, 0.5067751407623291, "[TT] Launch Date of the TSIS = 2017"]
-[9.949145317077637, 5.51645565032959, "[FF] Placement of the Temperature Sensors = Front and back face of the test targets"]
-[6.012559413909912, 7.359451770782471, "[FF] Quantity of the ISP-2 = Unknown"]
-[8.231476783752441, 6.8454790115356445, "[TT] Images per Capture of the EPIC = 10"]
-[5.073390483856201, -0.661737322807312, "[TT] LSDN of the SLATS = 12:00 hours \u00b1 15 min"]
-[10.359306335449219, 2.1420822143554688, "[TT] Detector System of the eROSITA = Based on the successful XMM-Newton pn-CCD technology"]
-[5.081689834594727, 6.943286895751953, "[TT] Data Downlink Frequency of the DMSP = Once per orbit"]
-[2.8354876041412354, 0.09009800851345062, "[TT] J2000 right ascension (deg) of the B1509-58 = 228.48175"]
-[4.424566268920898, 6.254495143890381, "[TT] Patch Antenna Frequency of the GOMX-3 = 1592 MHz"]
-[7.7193498611450195, 8.183445930480957, "[TT] Color of the Optical Elements = Light red"]
-[6.0551862716674805, 1.2849502563476562, "[TT] Launch Date of the Swarm = 2013"]
-[9.943739891052246, 8.989102363586426, "[TT] Effective FOV of the Channel 3 = 42 x 94 km"]
-[10.725847244262695, 5.398459434509277, "[TT] Ion Density of the PAP = 5 x 10^2 ~ 1 x 10^7 cm^-3"]
-[5.781558036804199, 7.189083099365234, "[TT] Data Rate Reduction of the RMC = By a factor of 2"]
-[9.832620620727539, 7.828342914581299, "[TT] Frame Time of the Telescope = 160 minutes for 6000 km x 6000 km area sounding"]
-[8.3541898727417, 2.466472864151001, "[FF] Publication Year of the Case studies of aerosol retrievals = 2002"]
-[10.65142822265625, 1.5859557390213013, "[FF] Interaction in Atmosphere of the Neutrons = Absorption by nuclear reactions, decay, Earth albedo neutron flux"]
-[6.871783256530762, 1.7531790733337402, "[FF] URL of the James Webb Space Telescope = http://www.stsci.edu/jwst/"]
-[8.544760704040527, 2.749476194381714, "[FF] Research Paper of the Picard = Advances in Space Research, Vol. 24, No 2, July 1999, pp. 205-214"]
-[5.4744391441345215, 5.580829620361328, "[TT] Interface of the User Terminal = Standard RS-232"]
-[6.1901679039001465, 4.573039531707764, "[FF] Main Operations Tasks of the LMOC = Monitor payload and ground system telemetry, monitor atmospheric conditions, monitor link status, respond to user service requests, perform ground station handover, execute performance data monitoring, implement scheduling change requests, perform routine housekeeping functions, contact engineering in the event of a significant anomaly"]
-[8.91459846496582, 6.110140323638916, "[TT] Incorporates of the EHIS = ADIS (Angle Detecting Inclined Sensor)"]
-[7.928798198699951, 5.063607692718506, "[FF] Typical Value of the SO2 = 10"]
-[13.870552062988281, 3.049299478530884, "[FF] Size and Mass of the VectorSol = Unknown"]
-[13.682090759277344, 3.074664354324341, "[TT] Payload Mass (max) of the Spacecraft = 170 kg"]
-[5.850276947021484, 4.097497940063477, "[FF] Payloads of the Satellite = IOV, Communication Payload of the German Ministry of Defense"]
-[10.136207580566406, 5.721102714538574, "[TT] Time to Reach Temperature of the PICNIC IR detector = About nine hours"]
-[7.078434944152832, 3.77555513381958, "[FF] Mission Phases of the PROBA-3 = Nominal orbit activity, Formation flying demonstration maneuvers, Coronagraphy"]
-[11.415925979614258, 4.7965521812438965, "[TT] Shape of the FY-2F = Cylindrical"]
-[5.932885646820068, 6.641608715057373, "[FF] Feedback Signal Content of the LCS = Angel error and the received intensity"]
-[8.213698387145996, 2.2056081295013428, "[FF] Science Objectives of the TROPICS = Relate the occurrence of intense precipitation cores (convective bursts) to storm intensity evolution"]
-[9.405814170837402, 3.586803913116455, "[FF] Anomalies of the Earth's Magnetic Field = Deviations from the idealized field of a centered bar magnet"]
-[5.476133823394775, 0.5861125588417053, "[TT] Year of Launch of the Terra = 1999"]
-[9.639039039611816, 5.008138656616211, "[TT] Drift Rate of the AOCS = 5.0 x 10-5 \u00b0/s"]
-[4.5095720291137695, 6.788642406463623, "[FF] Failure Cause of the S-band antenna = Lightning strikes"]
-[8.14022159576416, 3.414393663406372, "[TT] Measurement of the OCO-3 = CO2 Mole Fraction"]
-[8.330992698669434, 5.272293567657471, "[FF] Phase-Delay Sensitivity of the ALISEO = Affected by the overall instrument geometry"]
-[5.814882755279541, 7.1751885414123535, "[TT] 205 kbit/s for each sensor (uncompressed case) of the Data Rate = Data rate 205 kbit/s for each sensor (uncompressed case)"]
-[13.777649879455566, 2.9096953868865967, "[TT] Mass of the Spacecraft = < 2 kg"]
-[4.944033622741699, 3.4994335174560547, "[TT] Manufacturer of the X-band transponder = Lockheed Martin"]
-[13.510417938232422, 2.959625244140625, "[TT] Mass of the RISAT-2 = 300 kg (including a payload mass of 100 kg)"]
-[4.737259864807129, 7.972802639007568, "[TT] Frequency of the Transmitter = 5.84 GHz"]
-[6.715847492218018, 5.200800895690918, "[FF] AFE Type of the N-FEE = Non-integrated 16-bit AFE"]
-[10.04574203491211, -1.5049034357070923, "[TT] Launch Inclination of the Satellite = 57\u00ba"]
-[9.518316268920898, 7.836547374725342, "[TT] Imaging Capability of the CuPID = Yes"]
-[10.835460662841797, 3.493436574935913, "[TT] Size of the EXOpod CubeSat deployers = 12U and 16U"]
-[5.288461685180664, 0.1264965683221817, "[TT] Focus Adjustment of the Ikonos-2 = Not needed since 2006"]
-[9.940040588378906, -0.41652628779411316, "[TT] Altitude of the TanSat = 700 km"]
-[13.47559928894043, 2.8080153465270996, "[TT] Wet Mass of the OSC = ~250 kg"]
-[7.020264625549316, 4.524687767028809, "[FF] Unknown of the MSI = Unknown"]
-[5.232088088989258, 5.228384971618652, "[TT] PCB Design of the Namuru V3.2 GPS Receiver = Consideration of mechanical stresses caused by thermal cycling"]
-[7.427225112915039, 4.585700988769531, "[FF] Function of the Docking Plate = Provides a point of contact on the target for a magnetic capture system, and also provides an optically controlled surface for GNC"]
-[8.584189414978027, 6.924745559692383, "[FF] Imaging Resolution of the PAIS = Higher than an equivalent direct imaging system"]
-[12.176103591918945, -0.24728557467460632, "[TT] Observation Uniformity of the TESS = Very uniform"]
-[5.207079887390137, 3.599292039871216, "[TT] Supplier of the GPSP = NASA"]
-[5.747741222381592, 2.840270519256592, "[FF] Participants of the SRTM = NASA, DoD/NGA, DLR, ASI"]
-[4.750403881072998, 0.41472235321998596, "[TT] Launch Date of the SVOM = No earlier than 2020"]
-[6.668936252593994, 5.24244499206543, "[FF] User Interface Manual Version of the DAPS = 1.1"]
-[13.831977844238281, 2.755647897720337, "[TT] Launch Mass of the SAST-5000 = ~5300 kg"]
-[4.4846343994140625, 5.992309093475342, "[FF] Third-party Payload of the GOMX-3 = Miniaturized high data rate X-band transmitter"]
-[10.41590404510498, 4.017781734466553, "[TT] Maximum Extension of the Deployable Boom = 1.5 m"]
-[6.60080099105835, 6.34050178527832, "[FF] Track Duration of the DSN = 3.5-5 hours"]
-[6.321695327758789, -1.347569465637207, "[TT] Launch Date of the GRACE = August 2017"]
-[4.983207702636719, 3.4991092681884766, "[TT] Manufacturer of the Surface Potential Meter = TREK Inc."]
-[10.226469039916992, 8.421361923217773, "[FF] Pupil Diameter of the NAOMI = Driven by the MTF (Modulation Transfer Function) requirement"]
-[10.049627304077148, 7.536194801330566, "[TT] Contracting Company of the PP Twin Telescopes = SENER"]
-[7.48560905456543, 3.4463002681732178, "[FF] Technique of the Level-2 = Empirical"]
-[9.705635070800781, 7.1417365074157715, "[TT] Spatial Resolution of the Instrument = < 200 m @ 600 km altitude"]
-[9.227278709411621, 7.85120964050293, "[TT] Electrical Isolation of the Focal Plane Assembly = Yes"]
-[8.114649772644043, -1.0430705547332764, "[FF] Function of the NASA Laser = Provide a new look at sea ice"]
-[10.557056427001953, 7.271238327026367, "[TT] Diameter of the Telemetry, Tracking and Command Stations = 13 m"]
-[3.568368673324585, 4.459930419921875, "[TT] Development and Build Contractor of the SAR-Lupe = OHB System AG"]
-[14.262420654296875, 2.9221079349517822, "[TT] Mass of the CINEMA = 2.8 kg"]
-[6.503166675567627, 1.1210471391677856, "[FF] Mission of the CryoSat-2 = Earth Explorer Opportunity Mission-2"]
-[4.83543586730957, 3.140026807785034, "[TT] Manufacturer of the Euclid space telescope = Thales Alenia Space"]
-[9.854341506958008, 4.736440658569336, "[TT] Spin Configuration of the Meteosat = Dual-spin at 100 rpm"]
-[9.622455596923828, 7.129884243011475, "[TT] Spatial Resolution of the MWRI = 15-85 km"]
-[9.301328659057617, 10.72968578338623, "[TT] Polarization of the ICI-1 = V"]
-[12.017189025878906, 4.560382843017578, "[TT] Height of the Large Space Simulator (LSS) = 15 m"]
-[5.114449501037598, 3.3215460777282715, "[TT] Operator of the CPOD Service = GMV-led consortium of Spain"]
-[8.464599609375, 6.4225335121154785, "[FF] Instrument Type of the OSIRIS = Imaging System"]
-[10.169515609741211, 0.9860037565231323, "[TT] Distance from Earth of the Markarian 335 = About 324 million light-years"]
-[5.488229751586914, 4.470702648162842, "[TT] Base Component of the GSCG = ESA SCOS2000 NIS"]
-[6.527709007263184, 1.8541016578674316, "[FF] URL of the Space Shuttle = http://wwlln.net/publications/yair.grl.2005.pdf"]
-[5.81108283996582, 2.0935583114624023, "[FF] Communication of the LightSail 2 = Successful"]
-[5.224204063415527, 0.7700719833374023, "[TT] Product Announcement Date of the Spire Global = September 11, 2019"]
-[14.287887573242188, 2.869288682937622, "[TT] Mass of the CINEMA-2 (KHUSat-1) = 4 kg"]
-[5.13456392288208, 5.536671161651611, "[TT] Operating Modes of the Antenna Subsystem = Searching, Tracking, Gyro-holding"]
-[6.849788188934326, -0.49276551604270935, "[TT] Orbit Raise Rate of the LightSail-2 = Several hundred meters per day"]
-[8.771888732910156, 3.5429751873016357, "[FF] Measurement of the Gaia = The trajectory of the Solar System"]
-[5.974794387817383, 5.973361968994141, "[TT] Type of the HD 21749 = K-type"]
-[6.979130268096924, 6.594013214111328, "[TT] Registration Time of the DUV = 100 ms"]
-[7.854293346405029, 5.450874328613281, "[TT] Interface of the Google Earth = ActiveX server interface"]
-[13.361196517944336, 7.343877792358398, "[TT] Power of the ILAS = 78 W"]
-[9.80172348022461, -0.6715101003646851, "[TT] Orbit Altitude of the Long March 5B = 162 by 306 kilometers"]
-[5.539837837219238, 2.2461581230163574, "[FF] Affiliation of the Steven De Cuyper = Unknown"]
-[9.35157299041748, 4.428923606872559, "[FF] Sun-Earth based spin axis determination of the IKAROS = Not provided"]
-[7.756772518157959, 4.3572096824646, "[FF] Calibration Method of the Meteosat Second Generation (MSG) Radiometer/Imager = Dedicated Moon/Sun/Deep-space Scans"]
-[9.77226734161377, -0.5778685212135315, "[TT] Orbit Altitude of the EAGLE = 39,000 km"]
-[10.17144775390625, 3.1639208793640137, "[FF] Name of the CubeSat = Unknown"]
-[9.706334114074707, -1.0571491718292236, "[TT] Orbital Separation from SPOT-5 of the SPOT-4 = 166\u00ba"]
-[10.458220481872559, 5.673032283782959, "[TT] Surface Temperature of the TOI 700 = About half its surface temperature"]
-[6.908824920654297, -1.7758582830429077, "[TT] Ionosphere of the Jason-2 = 1.2 cm"]
-[3.9239468574523926, 4.767033576965332, "[TT] On-board Location Accuracy Device of the RADARSAT-1 = None"]
-[3.262000560760498, 5.233755588531494, "[TT] Off-nadir Angle of the SAR = 35\u00ba to the right side of the satellite"]
-[5.053914546966553, 7.400699138641357, "[TT] Uplink Data Transmission Rate of the RF = 2400 bit/s"]
-[6.9882612228393555, 4.2270731925964355, "[FF] Unknown of the ASPIICS = Unknown"]
-[3.478799343109131, 6.321401119232178, "[TT] Linear Array Length of the Active Antenna = 1 m"]
-[5.584863185882568, 4.7992329597473145, "[FF] Diagnostic Port Function of the EDSN satellites = Data interface and battery charging during I&T activities"]
-[10.135746955871582, -0.46281155943870544, "[TT] Orbit Altitude of the CubeSats = 550 km"]
-[8.975923538208008, -0.21206073462963104, "[TT] Orbit Altitude of the Meteor-M2 = ~ 825 km"]
-[10.286628723144531, 7.276828765869141, "[FF] Optical System of the PAN Camera = Three-mirror off-axis reflective telescope with an off-axis concave hyperboloidal primary mirror and an off-axis concave ellipsoidal tertiary mirror"]
-[6.84706449508667, 1.7228236198425293, "[FF] URL of the Kepler = https://kepler.nasa.gov/news/nasakeplernews/index.cfm?FuseAction=ShowNews&NewsID=226"]
-[10.391450881958008, 1.6888586282730103, "[FF] Science Outcomes of the NICER = Establishing the existence of intermediate mass black holes, unification of stellar-mass and supermassive black holes, testing models of polar accretion onto magnetic white dwarfs, detecting photon bubble oscillations, probing galaxy evolution in clusters"]
-[4.988160133361816, 1.170745611190796, "[FF] Bulletin Date of the GOCE = February 2008"]
-[8.372827529907227, 7.2506256103515625, "[TT] Sensor Type of the MuREM = Dose rate sensitive photodiode"]
-[3.9181418418884277, 0.18924033641815186, "[TT] End of Mission Date of the SMART-1 = 3 September 2006"]
-[8.237611770629883, 7.50181770324707, "[TT] CCD Detector of the VISIM = Electrim EDC-1000E"]
-[5.760031700134277, 6.439950942993164, "[TT] Raw Data Capacity of the Temporary storage = 5 days"]
-[3.9781851768493652, 6.402394771575928, "[FF] Antennas of the ESPA Ring = 2 S-band omni antennas, and 2 medium-gain horns"]
-[4.608233451843262, 7.092896461486816, "[TT] X-band Data Downlink of the RF communications = 560 Mbit/s"]
-[7.769577980041504, 2.990532875061035, "[FF] Monitoring Capability of the GOSAT-2 = Carbon Monoxide concentrations"]
-[8.186952590942383, -0.4194803833961487, "[FF] Second-Lowest Minimum Extent of the Arctic Ocean = Unknown"]
-[9.222430229187012, 8.363792419433594, "[TT] Optics of the Micro-spectrometer = Infrared optical triplet lens"]
-[4.268116474151611, 7.507375717163086, "[TT] Frequency of the X-band Transmitter = 8.23 GHz"]
-[4.619546413421631, 0.6464448571205139, "[TT] Transfer Date of the POES = May 1998"]
-[9.495341300964355, 1.3396018743515015, "[FF] Previous Believed Speed of the Heliosphere = Faster than 52,000 miles per hour"]
-[9.107587814331055, 1.3588829040527344, "[FF] URL of the New Horizons = http://pluto.jhuapl.edu/News-Center/PI-Perspectives.php?page=piPerspective_01_19_2021"]
-[5.355869770050049, 7.776665210723877, "[TT] Type of the PRARE space segment oscillator = Voltage-controlled"]
-[6.119661808013916, 5.879097938537598, "[TT] AOCS of the MERLIN = Improved"]
-[11.519180297851562, 4.941730499267578, "[TT] Size of the Prototype Chip = 6 x 6 mm"]
-[5.626255035400391, 5.6480302810668945, "[TT] Microprocessor of the CDMU = ERC-32"]
-[7.9490861892700195, 7.980973243713379, "[FF] Type of the MIRI = Mid-Infrared Camera-Spectrograph"]
-[7.760117530822754, 9.122268676757812, "[TT] Wavelength Range of the InSb = 2.08 - 2.35 \u00b5m"]
-[7.217418193817139, 0.9417086243629456, "[TT] Launch Date of the SEASAT = June 27, 1978"]
-[7.602224349975586, 1.469533085823059, "[FF] Use of Shadows of the Bennu Global Mosaic = Needed to make the surface features pop"]
-[12.686761856079102, 1.9163967370986938, "[FF] Data Usage of the SAGE-III on ISS = Help to re-institute aerosol measurements crucial for more-accurate, long-term climate and O3 concentration and distribution models"]
-[11.106170654296875, 4.986380100250244, "[TT] Mass-to-surface ratio relative to LAGEOS of the LARES-2 = 1.5"]
-[3.6330554485321045, 5.024199485778809, "[TT] Steering of the C-RADAR = 2-D electronic"]
-[8.495006561279297, 8.617833137512207, "[TT] Instantaneous spectral coverage of the Spectrometer = 3.58 km/s"]
-[7.156198024749756, 5.578394889831543, "[FF] Quantity of the FIREBIRD-I = 2"]
-[10.123725891113281, -1.5943031311035156, "[TT] Inclination of the Tatiana-2 = 98.8\u00ba"]
-[5.200852394104004, 3.986776351928711, "[TT] Number of Satellites of the Eurostar E3000 = 7"]
-[5.2950005531311035, 3.989345073699951, "[TT] Number of Satellites of the EDSN Swarm = 8"]
-[8.888397216796875, 4.488453388214111, "[TT] Sensors of the Coarse ADCS = Sun sensors and magnetometers"]
-[5.423740386962891, 6.307501316070557, "[TT] Data Volume of the Nancy Grace Roman = 20,000 terabytes (20 petabytes) over the course of its five-year primary mission"]
-[6.981698989868164, 1.2154418230056763, "[FF] Date of the West Lothian Shale Bings = 21 March 2022"]
-[8.000384330749512, 6.877010345458984, "[FF] Image Type of the UV/VIS Camera = UV/VIS"]
-[5.157199382781982, 2.1035892963409424, "[TT] Number of Missions of the Buccaneer = 2"]
-[7.964570045471191, -0.6059482097625732, "[TT] Primary Instrument of the CryoSat-2 = SIRAL (SAR (Synthetic Aperture Radar) Interferometer Radar Altimeter)"]
-[5.326298713684082, 4.597309589385986, "[FF] Scalability of the Open5GCore Rel. 4 = Raspberry PI to a complete rack of servers"]
-[7.829581260681152, 2.6381664276123047, "[FF] Function of the CIRC = Measures land surface temperature and detects active fires"]
-[6.698807716369629, 4.484580993652344, "[FF] Components of the Robotic Servicing Platform = Camera, robotic arm, fuel reserve, GN&C rendezvous and proximity operations capabilities"]
-[4.918752193450928, 0.5637078881263733, "[TT] Launch Date of the ECOSTRESS = June 2018"]
-[6.9064130783081055, 2.312706470489502, "[FF] Development Date of the China High-resolution Earth Observation System (CHEOS) = 2014"]
-[5.463831424713135, 4.688318729400635, "[TT] Monitoring of Technology Advancement of the Proving Ground = Close"]
-[9.296276092529297, 1.2644097805023193, "[TT] Data Transmission Status of the New Horizons = About 80 percent sent to Earth"]
-[9.612974166870117, 1.3393160104751587, "[FF] Speed of the Material from Exploded Star = Faster than 20 million miles per hour"]
-[4.786341667175293, 1.3408923149108887, "[TT] Development Period of the UNITEC-1 = Aug. 2008 to Jan. 2010"]
-[6.904870510101318, 1.5991429090499878, "[FF] Status Update Date of the James Webb Space Telescope = May 19, 2009"]
-[13.73908805847168, 5.430546760559082, "[TT] Solar Panel Type of the Canopus Pipper = Triple-junction 26% efficient solar cells"]
-[9.907752990722656, 5.760623931884766, "[TT] YSI-type Thermistors of the TCS = 128"]
-[10.282279014587402, 8.051274299621582, "[TT] Aperture Diameter of the Telescope = 5 cm"]
-[6.172267436981201, 4.139486312866211, "[TT] Avionics System of the Spacecraft = Modular"]
-[6.735981464385986, 1.341225028038025, "[FF] Publication Date of the Orbit Determination System = 15 January 2016"]
-[7.597641944885254, 8.818843841552734, "[TT] Spectral Bands of the MSI-0 and MSI-1 = 0.45 - 0.52 \u00b5m, 0.52 - 0.60 \u00b5m, 0.63 - 0.69 \u00b5m, 0.76 - 0.90 \u00b5m"]
-[14.105772018432617, 3.0295541286468506, "[TT] Mass of the FY-4B = ~5300 kg"]
-[4.887137413024902, 0.25431740283966064, "[TT] Launch Date of the SPOT-5 = 04 May 2002"]
-[8.202991485595703, 3.6684610843658447, "[FF] Detects of the ABI = Radiation upwelling from the Earth at specific wavelengths"]
-[6.039786338806152, 4.396435737609863, "[TT] Baseline Products of the FY-4A = 28"]
-[4.487002372741699, 2.988834857940674, "[TT] Location of the NSOF = Suitland, MD"]
-[5.703335762023926, -0.9028454422950745, "[TT] Design Life of the S/C = Three years minimum with a goal of five years"]
-[10.160478591918945, -2.7738943099975586, "[TT] Data bus width of the SLC NAND-FMM = 128+24 bit"]
-[5.8835649490356445, 4.927438259124756, "[FF] Function of the LPT = Receives GPS signals (L1 C/A) as input for navigation support and provides low-rate data communications links to ground stations and the TDRS system"]
-[11.211132049560547, 5.145707130432129, "[TT] Structure Type of the WFS&C = Semi-rigid"]
-[7.937040328979492, 6.139683723449707, "[TT] Type of the MWI = Microwave Imager"]
-[7.206249713897705, 8.186473846435547, "[TT] Sensitivity of the Channel 7 = 0.4 K/pixel"]
-[8.018082618713379, 5.106441497802734, "[FF] Data Processing Routines of the NIRST instrument = MWIR cross-talk correction and in-flight calibration protocol"]
-[12.094039916992188, -0.24363979697227478, "[FF] Data Rates at Perigee of the TESS spacecraft = ~100 Mbit s-1"]
-[13.370330810546875, 6.911830902099609, "[TT] Energy Gain of the InSight Mars lander = About 30 watt-hours per sol"]
-[3.377596855163574, 6.154411792755127, "[TT] Size of the Phased Array Antenna (PAA) = 11 m x 3.6 m"]
-[11.261567115783691, 0.9979604482650757, "[FF] Mission Requirements of the LISA = Meet LISA's science requirements"]
-[9.898423194885254, -0.38389986753463745, "[TT] Altitude of the Satellite = 798 km"]
-[7.221543788909912, 8.307737350463867, "[TT] Band Count of the Sounder = 19"]
-[5.879933834075928, 5.390238285064697, "[FF] Secure Commands of the DCU = OTAR (Over-The-Air-Rekeying), key integrity checks and key disabling"]
-[10.006930351257324, 7.19588041305542, "[FF] Observation Data of the DCAM3-D = Size and the angle of the ejecta curtain, and the speed of the ejecta spreading or fragment spattering"]
-[9.367766380310059, 5.0376386642456055, "[FF] Impervious to Tilt of the Spacecraft of the CCRR = Up to a certain angle"]
-[4.422933101654053, 4.6974310874938965, "[FF] Purpose of the Transport Layer Tranche 1 = Support military communications, surveillance and tracking of enemy targets"]
-[6.424785137176514, 3.4748706817626953, "[FF] Function of the HSRC = Demonstrate reentry technology and cargo recovery from the ISS"]
-[6.23023796081543, 2.639275074005127, "[TT] Function of the SM = Contains Orion's propulsion, power and life support systems"]
-[7.990660190582275, 9.200145721435547, "[TT] Wavelength of the CATS = 1.064 \u00b5m"]
-[8.944245338439941, 9.426342010498047, "[FF] Spatial Resolution of the TANSO-CAI = Higher than the FTS"]
-[12.191305160522461, 3.5629162788391113, "[FF] Fuel of the EPPS = Xenon"]
-[5.685827732086182, 2.7815592288970947, "[FF] Primary Industrial Partners of the Nancy Grace Roman Space Telescope = Ball Aerospace and Technologies Corporation, L3Harris Technologies, Teledyne Scientific & Imaging"]
-[13.65925121307373, 6.9875807762146, "[TT] Power Draw of the EPS = < 50 mW"]
-[13.454838752746582, 2.8339664936065674, "[TT] Launch Mass of the DubaiSat-1 = 200 kg"]
-[9.285849571228027, 3.239302158355713, "[FF] Operating Modes of the Coronagraph = \"Video mode\" for display for the astronauts or TV transmission to the ground"]
-[10.320836067199707, 5.889996528625488, "[TT] Black Body Temperatures of the MVIRI = 290 K, 340 K"]
-[4.237223148345947, 2.5878398418426514, "[TT] Launch Location of the SpaceX = Cape Canaveral Air Force Station in Florida"]
-[8.07875919342041, 5.79914665222168, "[FF] Components of the DarkCarb image sensor = Optical elements, detector, temperature sensors"]
-[9.671850204467773, 7.996964454650879, "[TT] Angle of the Nadir FOV = 75\u00ba"]
-[9.32427978515625, 8.232020378112793, "[TT] Spatial Frequency of the Collecting Optics = 70 l/mm"]
-[9.797773361206055, 2.0976216793060303, "[FF] Jet Behavior of the V404 Cygni = Strange"]
-[9.054696083068848, 5.110463619232178, "[TT] Quantity of the Rate gyro = 1 unit"]
-[5.485190391540527, 6.066547870635986, "[FF] Purpose of the SSRB = Evaluate the performance of HCSM (High Capacity Spaceborne Memory) SRAM module in the space environment"]
-[5.697876930236816, 4.471385955810547, "[TT] Control System of the EDRS payload = Fully-automated operations engine"]
-[11.62364673614502, 4.644185543060303, "[TT] Size of the PCU = Compact"]
-[5.501915454864502, 5.139693737030029, "[TT] Operating System of the CANDOS = Red Hat Linux 6.1"]
-[4.559319019317627, 6.981813907623291, "[FF] Communication Experiment of the Q/V-bands = IFMT (Interference and Fading Mitigation Techniques), and site diversity"]
-[10.851849555969238, 3.6964542865753174, "[FF] Mission of the NEA Scout = Rendezvous with an asteroid"]
-[13.477188110351562, 2.806751251220703, "[TT] Dry Mass of the Spacecraft = 2350 kg"]
-[5.946987152099609, 4.392055034637451, "[FF] Mission Scenarios of the Ground Station = Links to and from aircraft, UAVs, and satellites"]
-[4.950944423675537, 1.5217019319534302, "[TT] Operation Start Date of the Tatiana-2 = Sept. 20, 2009"]
-[11.88336181640625, -0.04521939158439636, "[TT] Brightest Stars Observation Cadence of the TESS = 1-minute"]
-[9.756287574768066, 8.10360050201416, "[TT] Focal Length of the Optical Payload = 225 mm"]
-[6.367654800415039, 4.490403175354004, "[FF] Data Processing of the POCs = Pull relevant payload (level 0 and level 1) and ancillary data sets from the ISSDC dissemination server and process the data to generate higher level products"]
-[10.145303726196289, 6.948457717895508, "[TT] East-West Step of the Sounder = 10 km"]
-[5.6025567054748535, 6.348966121673584, "[FF] Tow Capacity of the PistenBullys = Unknown"]
-[14.108834266662598, 3.465230941772461, "[FF] Mass Determination Method of the EIS = Measuring velocity and total energy"]
-[5.276756286621094, 5.522804260253906, "[TT] Transport Layer Protocols of the IXV Communications Network = TCP and UDP"]
-[5.694618225097656, 2.7312867641448975, "[TT] Mission Manager of the NuSTAR = JPL for NASA's Science Mission Directorate"]
-[8.220455169677734, 4.035780429840088, "[TT] Lunar Calibration Frequency of the PACE spacecraft = Once a month"]
-[8.914118766784668, 4.299361705780029, "[FF] Sun Tracking Device of the ORA Instrument = No"]
-[5.241732597351074, 6.580280780792236, "[TT] Number of AIS Transmissions Captured of the AprizeSat-3 and AprizeSat-4 = Over 200,000"]
-[5.882419586181641, -0.014058033935725689, "[TT] Data Collection Period of the DMSP mission (SSM/I & SSMIS) = 40 years"]
-[9.782904624938965, -0.4650125503540039, "[TT] Orbital Altitude of the SSMIS = ~833 km"]
-[3.9072721004486084, 6.2631683349609375, "[TT] Number of Stick Antennas of the SASS = 4"]
-[11.290677070617676, 5.891943454742432, "[TT] Material of the Structural Frame Trusses = Flat stock graphite/epoxy (Gr/E)"]
-[9.329503059387207, 7.150110244750977, "[TT] Spatial Resolution of the PMC = 8 m"]
-[13.860122680664062, 3.0786333084106445, "[FF] Mass of the FY-1C = Unknown"]
-[9.663785934448242, 7.839807510375977, "[TT] Spatial Resolution (IFOV) of the ERIP = 170 km x 70 km"]
-[10.616549491882324, 3.456516742706299, "[FF] Study Phenomena of the RUBI = Phase transition and heat transfer during the evaporation of fluids"]
-[12.024691581726074, 6.258884906768799, "[FF] Anti-proton Fraction of the AMS = Unknown"]
-[3.054748773574829, 2.1709980964660645, "[TT] NDVI Value Representation of the Copernicus Sentinel-2 = Colour"]
-[11.955355644226074, 5.012151718139648, "[TT] Size of the FIBOS = 79 mm x 69 mm x 15 mm"]
-[5.26531457901001, 1.4689422845840454, "[FF] Power Generation Anomaly Date of the DAICHI (ALOS) = April 22, 2011"]
-[5.5801682472229, 3.8619778156280518, "[FF] Satellite Count of the Dnepr Rocket = 37"]
-[11.560505867004395, 4.9267754554748535, "[TT] Size of the MMS = The size of a baseball field"]
-[5.83788537979126, 8.714701652526855, "[TT] Interference filter - Bandwidth of the Instrument = 1 nm"]
-[16.49911117553711, 3.5847225189208984, "[TT] Global Service Target of the OneWeb = 2021"]
-[6.505882263183594, -0.08822720497846603, "[TT] Freeze/Thaw State Refresh Rate of the SMAP = 2 days"]
-[11.144861221313477, 5.8503851890563965, "[TT] Material of the CsI = Cesium Iodide"]
-[6.265047550201416, 5.41172981262207, "[FF] FPGA of the CubeComputer = For flow-through error correction in case of a radiation upset on the memory"]
-[5.032153606414795, 1.055769681930542, "[TT] Launch Status of the Al Amal = Launched"]
-[7.108715057373047, 7.246923446655273, "[TT] Wavelength of the Laser = 1556 nm"]
-[9.589224815368652, 0.12469275295734406, "[TT] Parachute Deployment Time of the MarCO-B = 11:51 am"]
-[8.102389335632324, -1.21271550655365, "[FF] Laser Tests of the ICESat-2 = Preparing"]
-[8.551117897033691, 6.416040420532227, "[TT] Measurement Range of the SSM = \u00b165535 nT"]
-[9.232063293457031, 7.464788436889648, "[TT] Field of View of the Detector = 8 km x 8 km"]
-[9.251787185668945, 0.24024146795272827, "[TT] Main Span Length of the Izmit Bay Bridge = 1688 m"]
-[8.051957130432129, -0.9787128567695618, "[FF] Orbiting Object of the ICESat-2 = Earth"]
-[8.506951332092285, 5.494296550750732, "[TT] Control Mode of the HM = Measurement and Calibration Modes and controlled through CCU-CMN (Correlator and Control Unit-Control and Monitoring Node) chain"]
-[10.762901306152344, 7.48693323135376, "[TT] Swath Width of the MTVZA = 2200 km"]
-[8.037681579589844, 5.083230972290039, "[FF] In-Flight Calibration of the MSU-E = Not Performed"]
-[13.22912883758545, 5.420164585113525, "[FF] Solar Array Deployment of the TSUBAME = Automatically deployed after the rocket separation"]
-[9.130322456359863, 0.4297693073749542, "[TT] Distance from Earth of the Ryugu = 300 million km"]
-[6.046370029449463, 3.2965633869171143, "[TT] Experimenters of the OPS-SAT = Over 200"]
-[5.101232528686523, 7.017766952514648, "[TT] BER (Bit Error Rate) of the Payload Downlink = <10-9"]
-[6.540017604827881, 4.022594451904297, "[FF] Operation of the Antonov 124 = Carry the spacecraft"]
-[7.673365592956543, 8.756636619567871, "[TT] Spectral Range of the MSU-S = 0.58 - 1.0 \u00b5m"]
-[6.404664993286133, 2.4321179389953613, "[TT] Formation Flying of the PRISMA = Autonomous"]
-[11.004514694213867, 7.659655570983887, "[TT] Nominal Swath Width of the Wide fine Quad-Pol = 50 km"]
-[9.652534484863281, 8.071829795837402, "[FF] Composition of the Relay Lens = Doublet, lens, doublet"]
-[9.564720153808594, -0.5833193063735962, "[TT] Plane Spacing of the FormoSat-3/COSMIC-1 = 24\u00ba"]
-[3.9810259342193604, 6.733617305755615, "[TT] Quantity of the S-band patch Rx/Tx antennas = 2"]
-[13.811305046081543, 2.6818952560424805, "[TT] Launch Mass of the Spacecraft = 2040 kg"]
-[8.812326431274414, 3.703907012939453, "[FF] Mass Range of the MIPA = Optimized to cover accelerated ionospheric ions"]
-[10.54816722869873, 6.454753398895264, "[TT] Mirror Module Assemblies Presentation Date of the IXPE = 2019"]
-[9.715580940246582, 0.33282849192619324, "[TT] Maximum Formation Distance of the PROBA-3 = 250 m"]
-[6.9764604568481445, 6.127730369567871, "[TT] Number of Instruments of the JWST = 4"]
-[8.647825241088867, 6.960503578186035, "[FF] Bistatic Imaging of the TDX/TSX = Provides additional observables for the extraction of new scene and target parameters"]
-[4.486519813537598, 0.5290337800979614, "[TT] Launch Date of the HTV-7 = 22 September 2018"]
-[5.8165154457092285, 5.088070392608643, "[FF] Function of the ROSA Radio Occultation Antenna = Receive the strongly attenuated signals coming from the GPS constellation during their occultation time window"]
-[9.514846801757812, 6.182958602905273, "[TT] Incidence Angle of the Wide multi-look fine = 29 - 50\u00ba"]
-[11.726120948791504, 3.4819536209106445, "[TT] Power of the Ion Thruster = 55 W to 585 W"]
-[4.48331356048584, 2.649338483810425, "[FF] Test Location of the AMS-02 = KSC (Kennedy Space Center) in Florida"]
-[7.147131443023682, 2.5212128162384033, "[TT] Publication Year of the Observation of the Earth and Its Environment: Survey of Missions and Sensors = 2002"]
-[5.931783676147461, 1.5570260286331177, "[FF] Milestones of the PRISMA Satellites = Two new milestones achieved"]
-[5.130291938781738, 6.195122718811035, "[FF] Connection of the TTC End-to-End Tests = Hardwired connections to the spacecraft TTC transmitters and the data umbilical will be connected"]
-[11.718250274658203, 3.291203260421753, "[FF] Thruster Quantity of the Eutelsat 172B = Not provided"]
-[9.110494613647461, 1.0798591375350952, "[TT] Arrival at Jupiter of the Juice = July 2031"]
-[8.521280288696289, 4.605630874633789, "[FF] Objective of the ASTERIA = Test miniature telescope components"]
-[10.042510032653809, -1.542052984237671, "[TT] Orbit Inclination of the ASNARO = 97.4\u00b0"]
-[6.235698699951172, 2.44722318649292, "[TT] Partner of the TESS = MIT's Kavli Institute of Technology for Astrophysics (MKI)"]
-[10.945869445800781, 7.54870080947876, "[TT] Swath Width of the HySI = 20 km"]
-[6.537899494171143, -0.5336695909500122, "[TT] Actual Orbit Duration of the ESEO = Almost two years"]
-[10.007329940795898, 4.361479759216309, "[TT] Quantity of the Torque rods = Three"]
-[8.519054412841797, 1.3186163902282715, "[TT] Salt Concentration Units of the Aquarius = Parts per thousand (grams of salt per kilogram of sea water)"]
-[10.223363876342773, -1.3286505937576294, "[TT] Inclination of the CeREs CubeSat = 85\u00ba"]
-[5.13771915435791, 4.538322448730469, "[TT] Function of the MC3 = Signal for assistance if a ground engineer was needed to resolve a problem"]
-[6.30896520614624, 1.8403103351593018, "[FF] URL of the PSLV = https://www.isro.gov.in/2018press15.html"]
-[6.181976795196533, 1.9029628038406372, "[FF] URL of the ILAS-II = http://db.cger.nies.go.jp/ilas2/en/document/usershb/UHB_ALL_E.pdf"]
-[11.299819946289062, 0.9555292129516602, "[TT] Operations Phase Duration of the LISA Pathfinder = 6 months"]
-[6.1875457763671875, 4.1794209480285645, "[FF] Mission Objective of the VELOX-PII = Qualify several in-house built hardware and software components"]
-[9.641286849975586, 8.303165435791016, "[TT] Field of View of the WFI = ~40\u00ba"]
-[3.8690812587738037, 7.903326988220215, "[TT] Modulation Type of the L-band data transmission = PSK (Phase-Shift Keying)"]
-[9.7344970703125, -0.6893627047538757, "[TT] Orbit Altitude of the HY-2B = 963 km"]
-[9.690213203430176, 1.3901739120483398, "[TT] Image Acquisition Capability of the Pleiades System = More than 500 images per day and per satellite"]
-[7.232824325561523, 4.8499979972839355, "[FF] Core Stage of the SLS Rocket = Assembled with four of the five parts"]
-[5.497075080871582, 2.6115033626556396, "[FF] Development Locations of the CPE = ITR of UniSA (University of South Australia), Adelaide, CSIRO (Commonwealth Scientific and Industrial Research Organization) Industrial Physics, Sydney, and at UTS (University of Technology), Sydney"]
-[5.515098571777344, 2.756230354309082, "[FF] Developer of the NRD = Norwegian Defence Research Establishment (FFI) with partners"]
-[6.130191802978516, 6.237813472747803, "[TT] LNA Protection of the TR Module = PIN diode switch"]
-[8.853229522705078, 6.447172164916992, "[FF] Image Color Diversity of the CaSSIS = Present"]
-[5.58895206451416, 1.6366890668869019, "[FF] Software Functionality of the ALOS-2 = Orbit determination, manoeuvre prediction and planning, and manoeuvre executions for both drag-makeup manoeuvres and inclination manoeuvres"]
-[4.917632579803467, 7.847177028656006, "[TT] Stiffness of the Antenna = > 0.1 Hz (in orbit)"]
-[5.837876319885254, -0.7792379260063171, "[TT] Nominal Life of the Spacecraft = 1 year"]
-[14.080458641052246, 7.042579174041748, "[TT] Voltage Output of the PSU = 4.1 V for safe battery charging"]
-[5.928523063659668, -0.6906187534332275, "[TT] Possibly > 10 years of the Spacecraft = Possibly > 10 years"]
-[8.629754066467285, 5.9683122634887695, "[TT] Positional Accuracy of the System = 5-meter CE90 for each individual image"]
-[7.037947177886963, 7.217716217041016, "[TT] Wavelength of the Communications Lasers = 810 nm"]
-[9.770570755004883, 7.496176719665527, "[TT] GSD (Ground Sample Distance) of the NTSIC = Pan: \u2264 0.5 m MS: \u2264 2 m"]
-[10.582439422607422, 1.6653356552124023, "[FF] Surrounding Gas Temperature of the Black Holes = More than a million degrees"]
-[4.9933857917785645, 1.1112090349197388, "[TT] Test Phases of the IEPS = Dec. 10, 2012"]
-[5.175670623779297, 3.0168063640594482, "[TT] Operator of the ICON = UCB/SSL (Space Sciences Laboratory)"]
-[4.996583938598633, 2.87225341796875, "[TT] Developer of the MIRAS Instrument = EADS-CASA in Spain under contract to ESA"]
-[5.415041446685791, 7.18882942199707, "[TT] Error Correction of the Modulator = RS (255, 223)"]
-[5.038150310516357, 7.936490535736084, "[FF] Bandwidth of the Satellite Device = 1500 MHz"]
-[5.708134651184082, 7.156372547149658, "[TT] Date Rate of the TT&C subsystem = 4 kbit/s"]
-[6.39584493637085, 1.5360080003738403, "[FF] Presentation Date of the MICROSCOPE = Sept. 27-Oct. 1, 2010"]
-[10.450456619262695, 6.953791618347168, "[TT] Secondary Mirror Diameter of the Optics Assembly = 56 mm"]
-[9.732501029968262, 6.9463324546813965, "[TT] Value of the Geometric factor = 0.1 cm^2 sr"]
-[5.03728723526001, 1.4257912635803223, "[FF] Role of the MONTE = Independent check of GIPSY-OASIS results"]
-[9.914305686950684, 0.43880173563957214, "[TT] Entanglement Distance of the Satellite = Approximately 500 to 1,400 km"]
-[6.284645080566406, 4.356325149536133, "[FF] Payload Systems of the SPOT-4 = PASTEC, POAM-II"]
-[9.639835357666016, 4.844828128814697, "[TT] Stabilization of the FY-4 = Three-axis stabilized"]
-[4.597627639770508, 7.747195720672607, "[TT] Nominal Carrier Frequency of the L-band data transmission = 1.7 GHz"]
-[9.647639274597168, 8.169220924377441, "[TT] Lens System of the EXI instrument = 48 mm, f/3.6"]
-[7.352908134460449, 0.24199335277080536, "[TT] Sample Return to Earth of the OSIRIS-REx = Sept. 24, 2023"]
-[9.558287620544434, 6.2910027503967285, "[TT] Earth's Surface Angle from GEO of the Scan Mirror Mechanism = 17.4\u00b0"]
-[8.150046348571777, 2.9589202404022217, "[FF] Purpose of the Geostationary Lightning Mapper (GLM) = Improve storm forecasts and warnings"]
-[9.735298156738281, -0.6214041113853455, "[TT] Orbit Altitude of the BRO-4 = 551 km"]
-[3.308760404586792, 1.4424850940704346, "[TT] Operational Lifetime of the Sentinel-2 = At least 15 years"]
-[9.100600242614746, 6.351566791534424, "[FF] Observation Geometry of the Satellite = Limb"]
-[8.292780876159668, 0.4568011164665222, "[FF] Current Elevation of the Lake Powell = Just a few meters from the 'minimum power pool'"]
-[6.448369026184082, -0.8382502198219299, "[TT] LTAN of the RISAT-1 = 6 hours and 18 hours"]
-[5.907585620880127, -0.24271629750728607, "[TT] Deployment Sequence of the SkySat-16 to -18 = SkySat satellites first, about 13 minutes after liftoff, followed by the Starlink satellites about 39 minutes after liftoff"]
-[11.913570404052734, 5.430590629577637, "[TT] Instrument Size of the ScaRaB = 614 x 512 x 320 mm"]
-[4.912131309509277, 0.28764790296554565, "[TT] Launch Date of the Spektr-RG = 13 July 2019"]
-[7.093531608581543, 7.232658386230469, "[TT] Laser Shot Count of the ATLAS laser = ~1 trillion"]
-[12.097394943237305, 3.037147045135498, "[TT] Propellant of the Aquajet = Water & anti-freeze"]
-[5.5192742347717285, 6.427652835845947, "[TT] Data Storage Capacity of the C&DH = 13.4 GB"]
-[8.233997344970703, 2.9679946899414062, "[FF] Measurement of the GLM sensor = Changes in cloud top radiance produced by lightning"]
-[6.69022798538208, 2.421630382537842, "[TT] Daily Image Download Capacity of the COSMO-SkyMed = Up to 1800 images/day"]
-[8.409651756286621, 3.214704990386963, "[TT] Area in 2016 of the Ozone Hole = 23 million km2"]
-[14.228714942932129, 3.0761475563049316, "[TT] S/C Mass of the JL-1-GF03D = <45 kg"]
-[4.766184329986572, 7.893052577972412, "[FF] Radio Frequency Range of the Broad Band Receiver = Not provided"]
-[5.896666526794434, 1.8852638006210327, "[TT] Crew Module Launch Date of the Orion = Dec. 2014"]
-[14.072543144226074, 3.1115880012512207, "[TT] Weight of the ALTIUS = 266 kg"]
-[5.0109381675720215, 3.634906053543091, "[TT] Manufacturer of the ASTERIA Transceiver = Vulcan Wireless"]
-[13.766230583190918, 6.76042366027832, "[TT] Power Source of the EPIRB = Battery-powered"]
-[3.463961362838745, 5.277665615081787, "[TT] Number of SMP Nodes of the SAR Processor = 6"]
-[8.117891311645508, 4.602319240570068, "[TT] Radiation Qualification of the GomX-4 = 20 krad TID (Total Ionizing Dose)"]
-[5.7564544677734375, 1.2546647787094116, "[TT] Observation Frequency of the ALOS-2 = Four times a year"]
-[3.904252290725708, 6.6259446144104, "[TT] Feed Array of the IMI = Tri-frequency patch feed array"]
-[6.935210227966309, 4.9873270988464355, "[FF] Purpose of the MGT = Transition from acquisition or safe-hold mode (MAS) to normal mode (MNO)"]
-[9.553842544555664, 6.926434516906738, "[TT] Spatial Resolution of the SST Product = 2 km"]
-[5.372306823730469, 1.44154953956604, "[FF] Data Collection Dates of the SMAP satellite = May 27\u201331, 2015"]
-[4.7740559577941895, 8.15117073059082, "[TT] Pulse Transmit Frequency of the SASS = 14.599 GHz"]
-[14.205440521240234, 3.1856048107147217, "[TT] Mass of the NewMag = 3 kg"]
-[8.873751640319824, 9.502182006835938, "[FF] Observation Data of the TANSO-3 = AMSR3"]
-[8.6104097366333, 2.265155792236328, "[TT] Accuracy of Wind Velocity (PBL) of the Aeolus = 2 m/s"]
-[8.887917518615723, 4.911407947540283, "[TT] Number of Sensors of the Experiment Layer = Hundreds"]
-[4.535544395446777, 3.021735191345215, "[TT] Ground Segment Sites of the GOES-R = West Virginia, Maryland and Virginia"]
-[4.885677337646484, 3.339977502822876, "[TT] Manufacturer of the VNREDSat-1A = Astrium"]
-[5.862224102020264, 3.1847617626190186, "[FF] Mission of the JPSS-1 through JPSS-4 = Provide operational continuity of satellite-based observations and products from NOAA's POES and S-NPP satellites"]
-[5.238372325897217, 4.98200798034668, "[TT] Communication Distance of the Ground Station = 40-50 k km from Earth"]
-[7.3755106925964355, 8.297952651977539, "[FF] Bands of the GOSAT CAI = 1, 2, 3"]
-[7.567590713500977, 1.238351583480835, "[FF] Presentation Date of the SWIM = Sept. 23-27, 2013"]
-[4.058506011962891, 5.96386194229126, "[TT] Antenna Gain of the ADS-B receiving payload = 10 dB"]
-[10.786678314208984, 1.5974587202072144, "[FF] Energy of the Neutron Star in M82 = Beams with the energy of 10 million Suns"]
-[4.654403209686279, 1.6050150394439697, "[TT] Reentry Date of the HaloSat = January 4, 2021"]
-[14.254800796508789, 3.2284929752349854, "[TT] Mass of the HIA = 3.0 kg"]
-[4.568255424499512, -0.8669422268867493, "[TT] Launch Date of the Crew Dragon = 2:40 a.m. EDT Oct. 31"]
-[7.193427085876465, 8.321409225463867, "[FF] SNR of the UVI instrument = 7.5"]
-[4.885879039764404, -0.874626874923706, "[TT] Mission Duration of the Dragon = 36 days"]
-[13.661478042602539, 7.13655948638916, "[TT] Conversion Efficiency of the DC/DC devices = Exceed 80%"]
-[6.839811325073242, 5.8945207595825195, "[TT] Quantity of the SMARD = 4"]
-[4.57957649230957, 0.09028370678424835, "[TT] Launch Date of the STARSHINE = 27 May 1999"]
-[9.486625671386719, 4.783257961273193, "[FF] Control Capability of the Attitude Control System = Two axes at any given time"]
-[10.366657257080078, 6.700983047485352, "[TT] Intersection Point Location of the Three Mirrors = Outside the mirror device"]
-[7.448614120483398, 9.178950309753418, "[TT] Center Wavelength of the Narrow Band Filter = 587.6 nm"]
-[5.040852069854736, 0.7029317021369934, "[FF] Fly Over Date of the ExoMars 2020 = 16 September 2019"]
-[10.854019165039062, 3.951711654663086, "[TT] Position Control of the CanX-4&5 = 1 m"]
-[9.59969711303711, 8.200916290283203, "[TT] Field of View of the Full Frame Mode = 11.2\u00b0 by 9.6\u00b0"]
-[3.7631800174713135, 4.630203723907471, "[TT] Type of the RADARSAT-1 = Earth-imaging radar satellite"]
-[3.3166656494140625, 5.098248481750488, "[TT] Polarization of the SAR Antenna = HH for medium swath, HH or VV for narrow swath"]
-[8.981679916381836, -0.7792567610740662, "[TT] Constellation Orbit of the SpaceLink = Medium Earth Orbit (MEO)"]
-[8.02248764038086, 5.985835075378418, "[FF] Purpose of the LASSO = Comparing the time at two or more laser-ranging sites"]
-[3.6428065299987793, 5.222611904144287, "[TT] Azimuth Resolution of the Radar = Approximately 400 m"]
-[12.105766296386719, 7.646383285522461, "[TT] Camera Mass of the Pushbroom imager = 13 kg"]
-[14.146265029907227, 2.8172056674957275, "[TT] Payload Mass of the Kondor-E = 350 kg"]
-[4.7920732498168945, -1.8600152730941772, "[FF] Age of Rocks in Landing Zone of the Chang\u2019e-5 = Much younger than those returned by the Apollo astronauts"]
-[8.163280487060547, 1.2469511032104492, "[FF] Data Integration of the SMAP satellite = Soil moisture measurements"]
-[9.413021087646484, 4.265830039978027, "[TT] Number of Fluxgate Sensors of the SOSMAG = 2"]
-[8.159789085388184, 1.2738813161849976, "[FF] Parameter of the IMI = Soil moisture - L band BT sensitive to soil moisture"]
-[10.948759078979492, 5.876821994781494, "[TT] Device Type of the SRM = 4 p-type MOSFET (Metal-Oxide-Semiconductor Field Effects Transistor) devices"]
-[5.552037239074707, 2.8680970668792725, "[TT] Agency of the MidSTAR-1 = USNA (United States Naval Agency)"]
-[10.797586441040039, 7.499951362609863, "[TT] Swath Width of the LIS = 550 km"]
-[3.6983838081359863, 3.8749969005584717, "[TT] Data Release Date of the RISAT-1 = 19 October 2012"]
-[13.830865859985352, 5.674387454986572, "[TT] Cell Efficiency of the Solar Arrays = 27%"]
-[9.764866828918457, 7.8751420974731445, "[TT] Image Resolution of the Herschel = 2 arcmin by 2 arcmin"]
-[9.161794662475586, 5.3523969650268555, "[TT] Pointing Stability of the Spacecraft = 0.3 arcsec/s"]
-[13.842557907104492, 2.889883518218994, "[TT] Dry Mass of the IMP-8 = 371 kg"]
-[10.864395141601562, 0.9896605610847473, "[TT] Temperature of the Red Dwarfs = Roughly a third of our Sun\u2019s temperature"]
-[9.372062683105469, 7.844856262207031, "[TT] Detector Image Circle of the NEA Scout Camera = 24 mm"]
-[6.777833938598633, 0.5156859755516052, "[TT] Deep Space Network Time of the Kepler = Scheduled to begin October 10"]
-[4.852329254150391, 3.3478243350982666, "[TT] Supplier of the MSI = Astrium Toulouse"]
-[7.95208215713501, 5.322625160217285, "[TT] Measurement Accuracy of the FLLS (Fine Lateral and Longitudinal Sensor) = 21 \u00b5m (lateral)"]
-[5.413507461547852, 1.7301924228668213, "[FF] Unknown of the ALOS-3 = Unknown"]
-[3.946610689163208, 2.0237019062042236, "[TT] Launch Vehicle of the Gravity Probe A = Scout-D"]
-[9.704304695129395, 4.088516712188721, "[TT] Magnetic Field Range of the iMTQ = \u00b163 mT"]
-[9.521434783935547, 7.175608158111572, "[TT] Spatial Resolution of the ABI = 0.5 km in VIS and 2 km in IR"]
-[10.801304817199707, 3.4940268993377686, "[TT] CubeSat Size of the RadFxSat = 1U"]
-[5.45334529876709, 0.38704103231430054, "[FF] Watch Start Date of the Space Station = June 15, 2010"]
-[5.793862342834473, 5.331721305847168, "[TT] Interface of the ASIM = CEPA"]
-[9.00190544128418, 6.804261207580566, "[FF] Resolution of the WorldView 4 = High"]
-[14.152581214904785, 3.140028476715088, "[TT] Mass of the Sundancer = about 8,200 kg"]
-[5.017425537109375, 1.7406413555145264, "[TT] Operation Status of the AISSat-1 = Nominal"]
-[13.196752548217773, 7.188235282897949, "[TT] Power Consumption of the SASS = 100 W"]
-[9.507473945617676, 1.1483443975448608, "[TT] Speed Range of the Coronal Mass Ejections = 100 to 3500 km/s"]
-[7.183128356933594, 8.617724418640137, "[TT] Solar Constant Channel FOV of the ISP-2 = 5\u00ba"]
-[4.998929023742676, 0.5543934106826782, "[TT] Data Release Start Date of the RPW = After 15 June"]
-[7.979133129119873, 0.8711192011833191, "[TT] Date of the U.S. Drought Monitor = April 26, 2022"]
-[7.871143817901611, 5.295345783233643, "[FF] Applications of the FLLS = Monitoring displacement between satellites in constellation, measuring structural distortion before, during, and after deployment of large-scale structures, and fine-tuning positioning of telecommunication satellite antennas"]
-[10.374153137207031, 2.211682081222534, "[FF] Observation Capability of the NuSTAR = X-ray vision"]
-[10.135100364685059, -2.7357802391052246, "[TT] Write Speed of the Flash SSD = Up to 1.6 Gbit/s"]
-[6.476779460906982, 3.704793691635132, "[FF] Development Status of the MEP = Not provided"]
-[5.654483795166016, 7.802229404449463, "[TT] Radiometric Gains of the DNB = 119,000:477:1"]
-[4.418320178985596, 7.679840087890625, "[TT] Frequency of the S-band Transmitter = 2234.4 MHz"]
-[9.269786834716797, 3.0896191596984863, "[FF] Perturbation Forces of the Space Environment = Solar pressure, drag"]
-[9.515731811523438, 1.6777726411819458, "[TT] Purpose of the CERN = Simulate conditions within Jupiter's massive magnetic field"]
-[8.554525375366211, 1.3390066623687744, "[FF] Regulation of the Aquarius = 3-dimensional ocean circulation"]
-[5.110260009765625, 3.5190446376800537, "[TT] Manufacturer of the Resistojets = SSTL"]
-[5.978612422943115, 5.821023464202881, "[FF] Data Transfer Method of the TDP-ODP Interface = TDP passes thresholded data to the ODP"]
-[13.453221321105957, 2.82649564743042, "[TT] Maximum Satellite Mass of the ALMASpace AD-SS = 35 kg"]
-[4.459682941436768, 3.232605218887329, "[TT] TT&C Station of the Ground Segment = Kiruna"]
-[4.875499725341797, 3.176643133163452, "[TT] Prime Contractor of the NIRSpec = EADS Astrium GmbH"]
-[7.463351249694824, 5.713965892791748, "[TT] Instrument Type of the CPL = Lidar"]
-[7.5177106857299805, 0.8940253257751465, "[FF] Presentation Authors of the Lunar Reconnaissance Orbiter = Jan McGarry, Tom Zagwodzki, Ron Zellar, Carey Noll, Greg Neumann, Mark Torrence, Julie Horvath, Bart Clarke, Randy Ricklefs, Mike Pearlman"]
-[9.708003044128418, 7.151674270629883, "[TT] Spatial Resolution of the Instrument = 20 m (VIS); 62 m (NIR)"]
-[9.642727851867676, -0.36509275436401367, "[TT] Altitude of the JPSS-1 = 824 km"]
-[5.704732418060303, 2.7563161849975586, "[TT] Funding Agency of the Microage = UK Space Agency"]
-[3.965451955795288, 4.449789524078369, "[TT] Ship Detection Range of the RADARSAT-2 = 1000 nautical miles from Canada's coasts"]
-[5.635138511657715, 5.602439880371094, "[TT] Flash ROM of the OBC = Updated applications"]
-[12.011834144592285, 6.323693752288818, "[TT] Proton Flux of the AMS = 300 million protons"]
-[14.29137134552002, 3.184180736541748, "[TT] Mass of the DIMAC = 9 kg"]
-[13.331727981567383, 6.7780232429504395, "[TT] Average Power of the MightySAT I = 12 W"]
-[6.720771312713623, 5.176006317138672, "[FF] Flow Rate Set Points of the FCA = Two"]
-[11.580782890319824, 4.697691440582275, "[TT] Structure of the Cuboid Module = Cuboid"]
-[11.034987449645996, 3.6342287063598633, "[FF] Propulsion of the CAPSTONE = Solar and the Sun\u2019s gravity"]
-[6.61233377456665, 4.762185573577881, "[FF] Description of the SV-4 diagrams = Hierarchy of systems and system Functions"]
-[10.162971496582031, 2.7308192253112793, "[TT] Field of View of the Meteosat DCS = About 80o great circles of the arc of its subsatellite point"]
-[4.789740562438965, -1.8094611167907715, "[FF] Landing Camera (LCAM) of the Chang\u2019e-4 Lander = Payload"]
-[11.469717025756836, 4.6389994621276855, "[FF] Location of the Sensors and Antennae = Inside the cuboid module"]
-[14.00838565826416, 7.14548397064209, "[TT] Bus Voltage Regulation of the SBVR = 100 V \u00b1 1 V"]
-[5.271007061004639, 4.872838020324707, "[TT] Model of the NovAtel OEM-615 = NovAtel OEM-615"]
-[9.700472831726074, 4.121949672698975, "[TT] Angular Resolution of the Vector Magnetometer = 1 arcsec"]
-[13.513835906982422, 5.341313362121582, "[TT] Impact Features of the Eureca = More than 1000 on the front sides of the solar arrays"]
-[9.840505599975586, 4.773396015167236, "[TT] Spin of the ICU = 1 to 10 rpm"]
-[3.890409469604492, 1.9841670989990234, "[TT] Launch Vehicle of the SpaceX CRS-13 = Falcon-9 FT"]
-[5.633203029632568, 2.6473324298858643, "[TT] Builder of the NuSTAR = Orbital Sciences Corp."]
-[4.903761863708496, 3.4842798709869385, "[TT] Manufacturer of the Magnetorquers = Clyde Space, UK/Scotland"]
-[5.191295623779297, 1.8908318281173706, "[TT] Mission Status of the ZY 1-02C = Operational"]
-[10.130144119262695, -1.499569058418274, "[TT] Inclination of the Satellite = 98\u00ba"]
-[12.678439140319824, 1.9009920358657837, "[FF] Observation Data of the SAGE-II = Stratospheric ozone, aerosol, water vapor, nitrogen dioxide"]
-[8.11592960357666, 3.541147232055664, "[FF] Electromagnetic Emissions of the Instrument = Needed to become sky-noise limited"]
-[9.47314453125, 6.687209129333496, "[TT] Spatial Resolution of the Next Generation Gravity Constellation = 500 km"]
-[8.48611831665039, 6.05131196975708, "[TT] Accuracy of the CERES = 0.5%"]
-[8.114935874938965, 5.877642631530762, "[FF] Camera Data of the PSSCT-2 = Used for Understanding"]
-[7.795261859893799, 1.137757658958435, "[TT] Diameter of the Mars' Core = About 3,660 kilometers"]
-[4.916399955749512, 0.7400283217430115, "[TT] Signing Year of the Paris Agreement = 2015"]
-[10.125679969787598, 8.105757713317871, "[TT] Focal Length of the UVIT Telescope = ~4750 mm"]
-[7.004337310791016, 4.111294746398926, "[FF] Function of the Formation Flying GNC (FF-GNC) = Controls the relative state (position and attitude) of the formation"]
-[8.258252143859863, -0.27406513690948486, "[TT] Sea-Level Rise Contribution of the Greenland and Antarctica = About 11 mm"]
-[11.591922760009766, 6.825949668884277, "[TT] Energy Channels of the Instrument = 5"]
-[4.931268692016602, 2.422715425491333, "[FF] URL of the Eutelsat Quantum = https://www.eutelsat.com/en/news.html#/blog_posts/four-things-you-should-know-about-eutelsat-quantum-69078"]
-[4.336276531219482, 1.2075623273849487, "[TT] Access Time of the SEOSAT-Ingenio = Within three days"]
-[5.8079986572265625, -0.2900529205799103, "[TT] Operational Duration of the MADRAS = Up to the end of January 2013"]
-[6.853598117828369, 0.6679319143295288, "[TT] Retirement Date of the Kepler space telescope = 2018"]
-[7.878382205963135, 8.459541320800781, "[TT] Bands of the CAVIS = 7 VNIR + 5 SWIR"]
-[13.449859619140625, 6.16840124130249, "[TT] Photovoltaic Power Generation of the HORYU-2 = 300 V"]
-[5.519278526306152, 6.335067272186279, "[TT] SD Card Capacity of the Command and Data Handling Board = Pair of SD Cards"]
-[10.110762596130371, -1.4187421798706055, "[TT] Orbit Inclination of the SARSAT-1 = 98.2\u00ba"]
-[4.9491167068481445, 3.002798080444336, "[TT] Manufacturer of the ALOS-2 = Mitsubishi Electric Corporation"]
-[7.984019756317139, 8.951586723327637, "[TT] Spectral Resolution of the SELENE/SP = 6\u20138 nm wavelength intervals"]
-[10.204989433288574, 6.384923934936523, "[TT] Temperature Range of the MABEL = Below -20\u00ba Fahrenheit (-29\u00baC)"]
-[5.1460185050964355, 0.5109690427780151, "[TT] Activation Date of the Range Finder = 11 June 2018"]
-[8.57641887664795, 4.695196628570557, "[FF] Function of the Monochromatic CMOS Imager = Perform star-tracking experiments"]
-[9.899438858032227, 2.662041425704956, "[FF] User of the NanoRacks satellite deployment platforms = High school, university level, professional researchers"]
-[6.850855827331543, 4.797348976135254, "[FF] Usage of the INS = First burn, second burn"]
-[9.666299819946289, 4.125535488128662, "[TT] Resolution of the Magnetic Field Sensor = 100 pT"]
-[6.888941287994385, 4.900380611419678, "[FF] Outputs of the Guidance = Control"]
-[3.6571383476257324, 4.435522556304932, "[FF] Presentation Date of the Capella X-band SAR constellation = 28 July - 2 August 2019"]
-[5.015965461730957, 2.1362409591674805, "[TT] Mission Status of the Eutelsat 172B = Entered full commercial service"]
-[6.876521110534668, 8.842865943908691, "[FF] Electromagnetic Spectrum of the POLDER-P = Visible and near-infrared (VIS/NIR)"]
-[13.825682640075684, 2.708836555480957, "[TT] Launch Mass of the Spacecraft = ~ 450 kg"]
-[6.218533039093018, 3.597975969314575, "[TT] Generation of the DMC (Disaster Monitoring Constellation) = 1st"]
-[9.488853454589844, 7.030229568481445, "[TT] Spatial Resolution of the GHOSt = 8 m"]
-[6.217446804046631, -0.035266634076833725, "[TT] Number of Activations per Day of the LDT = 438"]
-[4.533667087554932, 1.513103723526001, "[TT] Launch Date of the GOSAT = 23 Jan 2009"]
-[8.343194007873535, 4.6278462409973145, "[TT] LOD Improvement of the LARES = 19.8%"]
-[8.943182945251465, 4.3232879638671875, "[FF] Function of the CubeSense = Contains both sun and nadir sensors"]
-[1.314758539199829, 1.897551417350769, "[TT] Waste Capacity of the HTV-6 = Up to 6 metric tons"]
-[6.094229221343994, -1.9692425727844238, "[TT] Member of the Phil Townsend = True"]
-[5.130691051483154, 2.353972911834717, "[TT] Mission Type of the COMS = EO"]
-[5.352555751800537, 2.9254369735717773, "[TT] Funding of the NorSat-3 = NCA (Norwegian Coastal Administration)"]
-[7.654789447784424, 5.577991485595703, "[FF] Purpose of the Optical payload = Observation"]
-[7.490211486816406, 7.9955244064331055, "[TT] Material of the Reflection Diffuser = Spectralon"]
-[7.924709796905518, 6.145692348480225, "[FF] Main Use of the Color Imager = Take snapshots of targets of interest (Earth, moon, etc.)"]
-[6.4910197257995605, 3.3672754764556885, "[TT] Resolution of the BlackSky Satellites = Up to 80 cm"]
-[7.681678295135498, 5.570582866668701, "[FF] Technology of the Vision-based navigation system = Cameras and LiDaR"]
-[7.400546073913574, 4.784156322479248, "[TT] Mounting Location of the Visual Based Sensor (VBS) = OSC"]
-[8.625287055969238, 3.651846408843994, "[FF] Purpose of the SPDC = Trace the solar spectral irradiance to Planck\u2019s constant and photon count number"]
-[5.520914554595947, 6.990466117858887, "[TT] Health and Status Data Transmission Rate of the AMS-02 = 1 kbit/s"]
-[7.65213680267334, 3.4406840801239014, "[FF] Development Date of the In-situ micro-debris measurement system = 1 August 2015"]
-[5.184933185577393, -1.079886794090271, "[TT] Launch Date of the Konnect = 16 January 2020"]
-[6.829870700836182, 3.1393942832946777, "[FF] Meteorological Program of the Meteosat = European meteorological program in GEO (Geostationary Orbit)"]
-[9.765604972839355, -0.5674733519554138, "[TT] Orbit Altitude of the SPOT 6-7 = 694 km"]
-[9.769325256347656, -0.592960000038147, "[TT] Orbit of the BRO-2 and BRO-3 = Sun-synchronous orbit of 500 km altitude"]
-[7.009171962738037, 4.738146781921387, "[FF] Conversion Technology of the OPO = OPO"]
-[8.677728652954102, 7.616592884063721, "[TT] Pixel Size of the Detector = 18 \u00b5m"]
-[7.102362632751465, 3.6567463874816895, "[TT] Payload of the MANTIS = High resolution Earth observation camera"]
-[6.900519371032715, 4.366544246673584, "[FF] Type of the AEEF = Unknown"]
-[10.32348918914795, 3.1297006607055664, "[TT] Number of CubeSats Released of the NRCSD = 33"]
-[5.457664966583252, 6.38370943069458, "[TT] Mass Storage Capacity of the Mass storage capacity = 7 Gbit"]
-[13.389854431152344, 6.840032577514648, "[TT] Power Load (OAP) of the General spacecraft parameters = 90 W bus; 60 W PL"]
-[9.808370590209961, 0.6419321894645691, "[TT] Maximum Distance of the Inter-satellite link = 2-5 km"]
-[9.50150203704834, 7.160086631774902, "[TT] Spatial Resolution of the PMI = 15 x 9 km"]
-[5.515530109405518, -1.8154008388519287, "[TT] Design Life of the KOMPSAT-3 = 4 years"]
-[8.215583801269531, 2.687058925628662, "[FF] Cloud Discrimination of the GOSAT-2 CAI-2 = Unknown"]
-[11.412471771240234, 4.347707271575928, "[TT] Size of the QBus-2 = 2U"]
-[8.973150253295898, -0.797755777835846, "[TT] Orbit of the DSX = Medium Earth Orbit (MEO)"]
-[6.049352169036865, 2.08454966545105, "[FF] URL of the Orion EM-1 = http://www.wrmiss.org/workshops/twentysecond/Gaza.pdf"]
-[7.553298473358154, -2.2848708629608154, "[FF] PI of the ULEIS = G. Mason, U. of Maryland, R. Gold, JHU/APL"]
-[3.4120709896087646, 5.315221786499023, "[TT] SAR Payload Radar Center Frequency of the RCM = 5.405 GHz"]
-[3.3503262996673584, 1.498263955116272, "[TT] Launch Date of the Sentinel-1C = First half of 2023"]
-[14.212984085083008, 3.2144951820373535, "[TT] Mass of the Mass = \u2264 3.36 kg"]
-[6.258116722106934, 1.4591710567474365, "[FF] Progress Update Date of the eROSITA = 18 September 2018"]
-[4.137607574462891, 7.0502095222473145, "[TT] S-band antenna of the TT&C = 1"]
-[6.944671154022217, 9.040119171142578, "[TT] Band Center of the POLDER-1/2 = 763 nm"]
-[5.250635147094727, 8.13650894165039, "[TT] Frequency Range of the IME = DC to 3.3 MHz"]
-[7.529837608337402, 0.1481773853302002, "[TT] Checkpoint Rehearsal Duration of the OSIRIS-REx = Four hours"]
-[5.008501052856445, -0.15724124014377594, "[TT] Launch Time of the BlackSky-1 = 03:42:00 UTC"]
-[4.631956100463867, 0.18376392126083374, "[TT] Launch Date of the ALL-STAR = 18 April 2014"]
-[9.167996406555176, 3.2043120861053467, "[FF] Observation of the Satellite = Particle energization, solar flares, reconnection and plasma jet interaction with the local magnetic field structure"]
-[13.302347183227539, 5.478150844573975, "[TT] Solar Array Placement of the Power subsystem = On the top and side exterior surface of the satellites"]
-[6.157029151916504, 2.3097658157348633, "[TT] Principal Investigator of the AMS-02 = Professor Samuel Ting (MIT/CERN)"]
-[13.66738510131836, 6.89761209487915, "[FF] Electrical Power System of the ESTCube-1 = COTS solution"]
-[6.628176689147949, -0.6334151029586792, "[TT] Expected Orbit Duration of the SMDC-ONE = Approximately 30 days"]
-[5.332000732421875, 2.6249024868011475, "[TT] Led by of the GMES = EC (European Commission)"]
-[7.068905353546143, 8.36308479309082, "[TT] Estimated SNR of the Band 3 = 745.12 \u00b1 92.15"]
-[8.992593765258789, 6.091677188873291, "[TT] Motion Detection of the SU = Capacitive sensors"]
-[5.792983055114746, 1.4621453285217285, "[FF] Mission Start Date of the Eu:CROPIS = April 24, 2014"]
-[6.953248023986816, 1.8593264818191528, "[FF] Publication Date of the Orbiting Carbon Observatory = 2004"]
-[6.770909309387207, -0.6667141318321228, "[TT] Time to Arrive at Halo Orbit of the S/C = Approximately 3 months"]
-[14.065571784973145, 4.037194728851318, "[TT] Mass of the GOLD instrument = 37 kg"]
-[5.939983367919922, 2.9550070762634277, "[TT] Mission Count of the SSTL = 43"]
-[5.153183460235596, 7.674607276916504, "[TT] Signal Path of the Antenna = Separate for E5 and E1-band"]
-[8.683384895324707, 7.626176357269287, "[TT] CCD Pixel Format of the HIRES = 384 x 288"]
-[11.479667663574219, 4.795319557189941, "[TT] Diameter of the FY-2F = 2.1 m"]
-[10.992914199829102, 7.579761028289795, "[TT] Swath of the MSU-SK = 600 km"]
-[13.352051734924316, 5.673321723937988, "[FF] Potential of the Solar Arrays = Most negative potential"]
-[5.720634460449219, -0.896371066570282, "[TT] Design Lifetime of the CIMR = 7 years"]
-[9.721909523010254, 0.7861871123313904, "[FF] Distance from Earth of the Pulsar = Unknown"]
-[9.166526794433594, -0.4727635979652405, "[FF] Reentry Plan of the NPP = Lower the orbit perigee to approximately 50 km and target any surviving debris for open ocean entry"]
-[11.174677848815918, 0.5856230854988098, "[FF] Application of the NIRISS SOSS mode = Atmospheric characterization of transiting exoplanets"]
-[8.539206504821777, 7.685901641845703, "[TT] CCD Array Size of the MEGS = 1024 x 2048 pixels"]
-[9.322924613952637, 5.58343505859375, "[TT] Pointing Stability of the ASTERIA = 0.5 arcsec rms"]
-[4.7578654289245605, 0.5096809267997742, "[TT] Launch Date of the MSG-4 = 15 July"]
-[8.947359085083008, 3.3410511016845703, "[FF] Composition of the Ionosphere = Electrically charged gases or plasma"]
-[9.985308647155762, -0.22901828587055206, "[TT] Altitude of the Harmony satellites = 693 km"]
-[10.029237747192383, 2.738220691680908, "[TT] International Space Station Arrival Date of the NanoRacks CubeSat Deployer Missions = April 18, 2017"]
-[9.843583106994629, 4.481509208679199, "[FF] Attitude Control of the ADCS = Magnetorquers and reaction wheels"]
-[6.1944475173950195, 0.8872631192207336, "[TT] Image License of the CaSSIS = CC BY-SA 3.0 IGO"]
-[4.954806804656982, 7.415161609649658, "[TT] Data Rate of the RF Communications = 2.5 or 15 kbit/s"]
-[3.9845170974731445, 6.741540908813477, "[TT] Antenna Type of the DCS platform = S-band toroidal pattern transmit antenna"]
-[16.490182876586914, 3.575932741165161, "[FF] Launch Date of the OneWeb = 7 February 2020"]
-[7.044244766235352, 7.333816051483154, "[TT] Wavelength of the ATLAS lasers systems = 532.272 nm"]
-[8.603014945983887, 8.07438850402832, "[FF] Image Lines of the Focal Plane Array = Recorded Simultaneously"]
-[7.218198299407959, -0.31182777881622314, "[TT] Years on Orbit of the INSAT-3D = Two"]
-[4.492150783538818, 1.8005262613296509, "[TT] Date of the Bistatic Radar Experiment = April 9-10, 1994"]
-[5.893645763397217, 3.7299399375915527, "[FF] Cost of the Ground Station = As little as \u20ac10"]
-[8.053805351257324, 8.364245414733887, "[TT] Dynamic Range Infrared Channel of the VIRR = 180-330 K (scene temperature)"]
-[6.079666614532471, 4.283904075622559, "[FF] Check-Conflict (National Harmonization) of the CSK GS = Verify if any sensing request is conflicting with any others and submit the final harmonized Service Request list to the FM GS"]
-[8.851075172424316, 9.409247398376465, "[FF] Unknown of the TANSO-CAI-2 = Unknown"]
-[8.669926643371582, 4.628579616546631, "[FF] Redundancy of the Star Sensors = Redundant units may be implemented with some minor penalties"]
-[8.018084526062012, -2.467059373855591, "[TT] Limiting Resolution of the GOLD = ~50 km"]
-[11.087446212768555, 5.425872325897217, "[TT] Sensitivity of the High-Altitude Water Cherenkov Observatory (HAWC) = Very high energy gamma-ray photons"]
-[11.534031867980957, 3.435643196105957, "[TT] Specific Impulse of the CanX-4&5 = 35 s"]
-[8.374434471130371, -0.6344344615936279, "[TT] Thickness of the Iceberg A-76 = About 280 meters"]
-[8.695878982543945, 6.088050842285156, "[TT] Z Accuracy of the Planimetric Accuracy Assessment = <0.3 m"]
-[9.895180702209473, 8.173754692077637, "[TT] Telescope FOV of the Telescope = 166 arcmin x 166 arcmin"]
-[7.745147705078125, 6.059422016143799, "[TT] Measurement Method of the KBR = Dual One Way Ranging (DOWR)"]
-[7.721957206726074, 0.5318238735198975, "[FF] Sensor Complement of the Lunar IceCube = Unknown"]
-[6.178225517272949, 2.7123703956604004, "[FF] Developer of the Ground Segment = Spacebel in Belgium with scientific support from the Belgian institute for Space Aeronomy (BISA) and the University of Saskatchewan (USASK) in Canada"]
-[14.295893669128418, 3.13411545753479, "[TT] Mass of the ICARE = 2.4 kg"]
-[7.161439418792725, 6.15402364730835, "[FF] Function of the PCM Module = Dissipates the thermal power emitted by the lasers during operation, forms the mechanical structure to which the receiver module is attached"]
-[14.261752128601074, 3.2525148391723633, "[TT] Mass of the VPM = 8 kg"]
-[8.1878080368042, 1.1852761507034302, "[TT] Soil Moisture Map Resolution of the SMAP = 9 km"]
-[4.813946723937988, 0.13750803470611572, "[TT] Launch Date of the SpaceX CRS-22 = 03 June 2021"]
-[11.560409545898438, 3.4027459621429443, "[TT] Propulsion System of the Spacecraft = None"]
-[10.432413101196289, 2.290844678878784, "[FF] Data Products of the CRaTER = LET spectra of galactic and solar cosmic rays (particularly above 10 MeV)"]
-[5.649512767791748, 0.7857111096382141, "[FF] Article Date of the H1743-322 = July 2016"]
-[11.360923767089844, 5.8443450927734375, "[TT] Material of the TOGS = Aluminum"]
-[12.984026908874512, 6.961781024932861, "[TT] Requirement of the Power and Thermal Management = Demanding"]
-[3.619070529937744, 2.7189857959747314, "[TT] Number of Satellites of the Iridium NEXT = 72"]
-[5.332076072692871, 4.186399936676025, "[TT] Satellite Bus of the JPSS = \"NPP-like\""]
-[6.192743301391602, 2.4904472827911377, "[FF] Mission Team of the New Horizons = Southwest Research Institute\u2019s Space Studies Department, Boulder, CO; Johns Hopkins University Applied Physics Laboratory in Laurel, Md.; Stanford University, Palo Alto, Calif.; Ball Aerospace Corp., Boulder; NASA Goddard Space Flight Center, Greenbelt, Md.; and the Jet Propulsion Laboratory, Pasadena, Calif"]
-[6.1977972984313965, 2.4930477142333984, "[TT] Joint Project of the GRACE-FO = NASA/JPL (Jet Propulsion Laboratory) and the German Research Center for Geosciences (GFZ)"]
-[11.402347564697266, 4.284181118011475, "[TT] Size of the Eagle-1 (BeakerSat) = 1.5U"]
-[5.383755207061768, 3.8602213859558105, "[TT] Manufacturer of the AD9694 = Analog Devices"]
-[4.146623611450195, 7.36568021774292, "[TT] Instruments of the SARAL = A-DCS3, AltiKa"]
-[14.172808647155762, 6.537164688110352, "[TT] Battery Life of the Telemetry System = Eight hours"]
-[6.915083408355713, 0.03721093013882637, "[TT] Mapping of the Magellan = 1990s"]
-[13.478947639465332, 2.812610149383545, "[TT] Dry Mass of the Spacecraft = 958.5 kg"]
-[8.793331146240234, 5.5083489418029785, "[TT] Pointing Accuracy of the DSP satellites = <5\u00ba"]
-[4.444962024688721, 6.7200493812561035, "[FF] Function of the Drum-shaped Section = Ensure that the main transmissions in S-band are always directed towards the Earth"]
-[8.738152503967285, 2.1208629608154297, "[TT] Antenna Diameter of the WINDS = 2.4m"]
-[3.5154786109924316, 1.8032035827636719, "[FF] URL of the Sentinel-2B = http://m.esa.int/spaceinimages/Images/2017/01/Revealing_Sentinel-2B"]
-[6.382678985595703, -0.19080814719200134, "[TT] Pass-Prediction Frequency of the SpinSat = Once every two weeks"]
-[9.589795112609863, 5.264545917510986, "[FF] Tilt of the Etalon = Mechanically tilted"]
-[5.061688423156738, 0.4887966513633728, "[TT] Launch Date of the Spacecraft = 2019"]
-[12.124920845031738, -0.2771434187889099, "[TT] Observation Duration of the TESS = 27 days"]
-[5.755488395690918, -0.76649409532547, "[TT] Wear-in Test Cycles of the Redesigned SMA = 15 cycles"]
-[5.277512073516846, 7.661555767059326, "[TT] G/T of the Feeder Link = 15 dB/K"]
-[9.551027297973633, 1.0469038486480713, "[TT] Velocity of the QUESS = 8 km/s"]
-[4.922214031219482, -0.6252159476280212, "[FF] RCS Stoppage Period of the SLATS = 9 February to 7 March, 2018"]
-[13.579039573669434, 5.978812217712402, "[TT] Average Power Generation of the MicroMAS-1 = 14.5 W in sunlight (12.7 W orbit average) at a 400 km altitude orbit"]
-[6.184556007385254, 0.3581048846244812, "[TT] FDC (Failure Detection and Correction) Scheme of the Dellingr = 25-hour reset"]
-[5.965941429138184, 2.646531581878662, "[FF] Student Collaboration Goal of the IMAP = Provides students of diverse backgrounds with hands-on experience designing and building a CubeSat and two scientific instruments"]
-[9.525525093078613, 5.009912967681885, "[TT] Attitude Stability of the ACS = 0.03\u00ba/s"]
-[7.048985481262207, 3.664151430130005, "[FF] Collision Risk CONOPS Presentation of the OneWeb = Mike Lindsay, \u201dOneWeb Collision Risk CONOPS,\u201d SSA Operators' Workshop, Denver, Colorado, Nov. 3-5, 2016"]
-[10.07323932647705, 2.9392857551574707, "[FF] Deployment Time of the CubeSat Dispensers = Long after launch"]
-[12.070259094238281, 4.506885051727295, "[TT] Size of the Spacecraft = 7.5 m (high), 4 m x 4 m overall cross section"]
-[13.421226501464844, 6.850078582763672, "[TT] Payload Power of the Heinrich Hertz = 3.6 kW"]
-[5.857172966003418, 4.866086483001709, "[TT] Reliability Impact of the Satlet System = Mitigated by the inherent redundancy of a cellular system"]
-[8.686631202697754, 6.463199615478516, "[TT] Spatial Resolution of the TEMPO instrument = 2.1 km/pixel in the north-south direction, 4.7 km /pixel in the east-west direction"]
-[6.460099697113037, 0.6431174278259277, "[TT] Launch Date of the Landsat 9 = December 2020"]
-[1.7654976844787598, -2.0627894401550293, "[FF] Mission of the Hayabusa-2 = Explore Ryugu"]
-[9.45637321472168, -0.6871147155761719, "[TT] Total Orbits of the Airglow = 2789"]
-[4.7322187423706055, 2.2421841621398926, "[TT] Radio-Frequency Test Completion Date of the Quantum = 27 July 2020"]
-[10.089673042297363, -2.673469305038452, "[TT] Bit Error Rate (GCR) of the Astrium MMFU NAND-Flash SDR-SDRAM = \u2264 9 x 10 -13  / day"]
-[3.8510305881500244, 6.4743781089782715, "[TT] Antenna of the GIOVE-B = 42-element planar array"]
-[6.325167179107666, 6.288468837738037, "[FF] Data Request Time of the CEASE = 72 hours"]
-[9.157154083251953, 5.216363430023193, "[TT] Attitude Knowledge Error of the Spacecraft = 5 arcsec (95%)"]
-[9.46826457977295, 2.3198485374450684, "[TT] Improvement Factor of the ELFIN = Two"]
-[12.006685256958008, -0.3203464448451996, "[FF] Discovery Date of the TESS = January 27, 2021"]
-[7.297523498535156, 8.18094253540039, "[TT] Sensitivity of the Channel 2 = 0.4 K/pixel"]
-[4.177140235900879, 4.221969127655029, "[FF] Primary Mission Goal of the RAX-2 = Assess the generation and distribution of natural ionospheric irregularities"]
-[6.661169528961182, -0.5366231799125671, "[TT] Repeat Cycle of the TanSat = 16 days"]
-[6.493275165557861, 5.117169380187988, "[FF] Data Access of the Vision-1 = Access to a full archive and new acquisition data"]
-[5.165476322174072, -0.5775036215782166, "[FF] Mission Overview of the TARANIS = Lightning Study"]
-[5.6662821769714355, 6.673337936401367, "[TT] Power Supply of the MnACQ-2000 Miniature Network Data Acquisition System = Radiation tolerant"]
-[5.278295040130615, 1.3026189804077148, "[FF] Conference Date of the LUMIO = 1-5 October 2018"]
-[7.98765230178833, 7.920151710510254, "[TT] Noise Performance of the Visible Spectral Band = SNR=6.5 (albedo=2.5%)"]
-[7.782670021057129, 9.139328002929688, "[TT] Wavelength Bands of the SIS = 115 - 180 nm"]
-[6.208286762237549, 0.9572334885597229, "[TT] Eclipses of the Cluster = 19"]
-[13.827715873718262, 7.142529487609863, "[TT] Survive Without Damage of the DC-DC converter = \u00b150 V on input terminals"]
-[4.99802827835083, 7.336956024169922, "[TT] S-band Communication Data Rates of the CanX-2 = 32 kbit/s and 256 kbit/s"]
-[9.045280456542969, 7.58462381362915, "[TT] Pixel Size of the Main Camera = 100 m in its central field of view"]
-[8.849739074707031, 0.07927028834819794, "[TT] Latitude Observation Point of the SHIMMER = Around 55\u00ba"]
-[4.021154403686523, 2.1622822284698486, "[TT] Launch Complex of the Ariane-5 ECA = ELA-3 in Kourou"]
-[5.359050273895264, 5.388743877410889, "[FF] Objective of the STRV-1a and -1b = Evaluate new technologies in the high radiation dose environment of GTO"]
-[7.00473690032959, 8.159186363220215, "[FF] Operation Modes of the POLDER = Two dynamic modes for high SNR and wide dynamic range"]
-[9.709100723266602, 8.4017915725708, "[TT] FOV of the FSS = 128\u00ba x 128\u00ba"]
-[5.66830587387085, 3.861708641052246, "[FF] Objective of the Unseenlabs' Constellation = Create a constellation of 20 to 25 nanosatellites"]
-[6.751873016357422, 5.042888641357422, "[FF] Function of the PSS = Stores, distributes and manages electrical power for all electrical equipment"]
-[6.058385848999023, -0.3121856451034546, "[TT] Duration of the ISS Backup Crew Delivery mission = 216 days (210 quiescent)"]
-[7.535559177398682, 1.3414866924285889, "[FF] User Studies of the SeaSat = 18"]
-[4.409896373748779, 7.5598368644714355, "[TT] Operational Link Frequency of the DASS = L-band"]
-[11.757833480834961, 0.1369830071926117, "[FF] Exoplanet Survey of the TESS = Detects planets via the transit method"]
-[8.831746101379395, 6.124382972717285, "[TT] Camera Position of the PSSCT-2 = +Z face"]
-[9.873465538024902, 4.89900016784668, "[TT] Filter Wheel Rotation Frequency of the GOES Sounder = 10 times per second"]
-[7.644558906555176, 9.291399002075195, "[TT] Band Center Wavelength of the COCTS = 0.865 \u00b5m"]
-[10.32320499420166, 7.198654651641846, "[FF] Type of the VIIRS = Three Mirror Anastigmatic"]
-[5.694559097290039, 3.646533727645874, "[TT] Type of the Test Facility = Vertical test facility"]
-[10.182597160339355, 7.87483024597168, "[TT] Design of the Telescope = Off-axis unobscured TMA without intermediate focus locations"]
-[10.067826271057129, 7.9800310134887695, "[TT] Focal Length of the NuSTAR Optics = 10.15 m"]
-[6.014791488647461, 3.421299934387207, "[FF] Daily Collection Capacity of the Satellite Constellation = Enough to deliver a return on the investment"]
-[5.718008518218994, 0.7340825796127319, "[TT] First Observation Date of the IMG = October 10, 1996"]
-[8.574917793273926, 2.239772319793701, "[FF] Purpose of the Plane = Measure wind speed and direction"]
-[3.992457151412964, 4.384378910064697, "[FF] Purpose of the EMOC = Maximize use of the RADARSAT-2 satellite"]
-[7.110045909881592, 8.320836067199707, "[TT] SNR of the Band 4 = 180"]
-[6.263364791870117, -0.3154807984828949, "[TT] Survey Mode Duration of the C/NOFS = 9 months"]
-[7.972982883453369, 5.232624053955078, "[FF] Calibration Parts of the RSI instrument = Absolute and relative radiometric calibrations"]
-[8.218451499938965, 7.770871162414551, "[TT] Deviation of Center Wavelength of the 4-band CCD Imager = < 5 nm"]
-[13.245417594909668, 7.1697678565979, "[TT] Power Consumption of the PSU = 75 W"]
-[5.7040252685546875, 5.818403720855713, "[TT] Address Space of the LEON3 = >24 bit"]
-[4.9033074378967285, 0.6856426000595093, "[TT] Launch Date of the Aalto-1 = End of 2016"]
-[5.828969955444336, -0.3682498335838318, "[TT] Projected Annual Crewed Missions of the SpaceX = Five or six"]
-[3.871030330657959, 1.9581161737442017, "[TT] Stage Type of the Soyuz = Core stage"]
-[7.679473876953125, -0.8600324988365173, "[TT] Phase C Status Date of the ICESat-2 = December 17, 2012"]
-[7.7145094871521, 2.2986538410186768, "[FF] Current State of the South Atlantic Anomaly = Expanding westward and continuing to weaken in intensity"]
-[8.191123008728027, 3.3277485370635986, "[FF] Components of the Atmospheric Chemistry Suite = Three infrared spectrometers"]
-[6.773690223693848, 4.402255535125732, "[TT] Installation Location of the iROSA = Far port side of the station\u2019s truss"]
-[6.611611843109131, -0.30776315927505493, "[TT] Average of the Observation Time = 16.3 minutes"]
-[6.627922534942627, 0.8228217363357544, "[TT] Agility of the FormoSat-2 = \u00b145\u00ba"]
-[4.10820198059082, 0.2361815869808197, "[TT] Launch Date of the Falcon 9 = March 14, 2021"]
-[8.25918960571289, 2.486100435256958, "[FF] Main Objective of the POLDER = Improve the microphysical and radiative property characterization of clouds and aerosols"]
-[11.517677307128906, 6.417189598083496, "[TT] Energy Range of the NuSTAR = High-energy"]
-[5.251572608947754, 1.0657097101211548, "[FF] Launch Date of the SMOS = May 21, 2010"]
-[6.004219055175781, -0.5360100865364075, "[TT] Mission Duration of the OPAL = > 9 months"]
-[3.470019817352295, -0.9362177848815918, "[FF] Orbit of the Resurs-P1 = Sun-synchronous near circular orbit"]
-[11.971253395080566, 6.452626705169678, "[TT] Gamma-ray Energy Range of the AMS-02 = Up to hundreds of GeV"]
-[9.66384220123291, -0.3749585449695587, "[TT] Baseline Altitude of the SPARCS = 550 km"]
-[4.972590923309326, 7.116555213928223, "[TT] Data Downlink Rate of the SGLS Link = 1024 kbit/s"]
-[12.831202507019043, 7.601734638214111, "[TT] Power of the Instrument = 250 W"]
-[9.511432647705078, 5.851595878601074, "[TT] Parameter of the Tilt angle = +20\u00ba, 0\u00ba, -20\u00ba"]
-[5.43964147567749, 1.2814656496047974, "[FF] Conference Date of the LARES = Sept. 23-25, 2003"]
-[9.013506889343262, 0.19415847957134247, "[TT] Volume of the Lake Atat\u00fcrk Dam = 48.7 km3"]
-[6.209306240081787, 2.023542642593384, "[FF] URL of the RAIDS = http://www.nrl.navy.mil/tira/Projects/raids/"]
-[5.5771284103393555, 5.644269943237305, "[TT] Model of the CPU = PIC16F877A"]
-[13.340577125549316, 6.851376533508301, "[FF] Power Consumption of the Scientific Payload = High"]
-[8.379499435424805, 7.289386749267578, "[TT] Camera Quantity of the LED-arrays = 2"]
-[6.34512186050415, 3.7631852626800537, "[FF] Development Authors of the SpaceCube MINI = Michael Lin, Tom Flatley, Alessandro Geist, Dave Petrick"]
-[8.48111343383789, 1.9512288570404053, "[FF] Purpose of the RapidScat = Spying tropical-storm-force winds"]
-[5.943796634674072, 0.8268449306488037, "[FF] Observation Date of the ISEE-1 and ISEE-2 = 29 September 1978"]
-[9.095133781433105, 1.3867173194885254, "[TT] Telemetry Data Investigation Start Date of the Voyager 1 = 18 May 2022"]
-[6.375256061553955, 4.623898983001709, "[FF] Main Functions of the SCC = Orbit and attitude control, manoeuvre calculations, operational payload configuration, real-time monitoring of the satellite health"]
-[9.967574119567871, 5.389467239379883, "[FF] Thermal Condition of the Satellite = Stable"]
-[8.758695602416992, 2.333071231842041, "[TT] Altitude Range of the Thermosphere = About 53 and 373 miles (85 and 600 km)"]
-[6.020349979400635, -0.3950020372867584, "[TT] Operation Duration of the GIOVE = More than 3 years"]
-[9.0642671585083, 5.5617265701293945, "[TT] Pointing Accuracy of the AOCS = 0.05\u00b0"]
-[9.454710006713867, 6.598532676696777, "[TT] Viewing Geometry of the MRO = West"]
-[10.998270034790039, 5.8026909828186035, "[TT] Gate-Oxide Thickness of the RadFETs = 1 \u00b5m"]
-[8.345612525939941, 7.271916389465332, "[FF] Distance of the Photodiode Pairs = Calculated to avoid light coupling"]
-[8.586002349853516, 8.57867431640625, "[TT] Instantaneous spectral coverage of the Spectrometer = 1.38 km/s"]
-[7.9769487380981445, 5.9856767654418945, "[FF] Components of the Optical Payload = Wide-angle camera (primary) and a telescopic camera (secondary)"]
-[13.725290298461914, 3.046381711959839, "[TT] Payload mass of the DST 35 = < 20 kg electronics inclusive"]
-[4.923154830932617, 3.095259428024292, "[TT] Manufacturer of the CubeSense = University of Stellenbosch, South Africa"]
-[11.869438171386719, 3.076019287109375, "[TT] \u0394V Control of the RVX = Reasonable Margins"]
-[10.086152076721191, -1.5113258361816406, "[TT] Inclination of the Satellite Constellation = 98.2\u00b0"]
-[8.598316192626953, 0.25659191608428955, "[FF] Insight of the Comets = Planetary construction yard at these early times"]
-[12.141477584838867, 1.968973159790039, "[TT] Launch Date of the CartoSat-1 = May 5, 2005"]
-[6.04142427444458, 3.3795387744903564, "[TT] Number of Free Flyers of the ORS-3 Mission = 26"]
-[4.873365879058838, 8.259419441223145, "[TT] Bandwidth of the Radar = 1 MHz"]
-[5.580192565917969, 3.083700180053711, "[FF] Management of the InSight = JPL, a division of Caltech in Pasadena, California"]
-[5.720169544219971, 5.751770973205566, "[TT] Radiation Susceptibility of the SCS750 = 1 uncorrected processor upset every 128 years"]
-[10.37048053741455, 7.338280200958252, "[TT] Secondary Mirror Diameter of the Cassegrain telescope = 50 mm"]
-[5.395909309387207, 5.870205879211426, "[TT] Power of the STRV-1d DHS = 3 W"]
-[8.484739303588867, 6.105576038360596, "[TT] Reliability of the CERES = Highly reliable"]
-[11.71228313446045, 3.2927403450012207, "[TT] RCS Thrusters of the AOCS = 16"]
-[14.1777925491333, 3.1107358932495117, "[TT] Mass of the Poseidon-1 = 24 kg"]
-[7.977834224700928, 13.684720039367676, "[TT] SSD of the B1 = 60 m"]
-[5.269865036010742, 2.2815489768981934, "[FF] Mission Type of the SporeSat = EO"]
-[3.9324591159820557, 4.254693984985352, "[FF] Imaging Capability of the RADARSAT-2 = Full continental coverage of Antarctica"]
-[6.705541133880615, 5.8122735023498535, "[TT] Lead of the CATSat-1, CATSat-2 = Johns Hopkins University Applied Physics Laboratory"]
-[9.837067604064941, 4.281410217285156, "[FF] Vacuum Cases Structures of the AMS-02 = Mechanically identical"]
-[3.957493543624878, 4.22912073135376, "[FF] Mission Objective of the RADARSAT-1 = Monitor environmental change and the planet's natural resources"]
-[5.90107536315918, 1.6257363557815552, "[FF] Workshop Date of the Brazilian EO Satellite Program = April 17-19, 2012"]
-[8.974169731140137, 4.3527398109436035, "[FF] Attitude Sensors of the ANUSat = Tri-axial magnetometer and an optical TWSS (Twin Slit Sun Sensor)"]
-[7.838420867919922, 6.003688812255859, "[FF] Connection of the BSM (Beam Steering Mechanism) = Connected with components on the instrument's telescope receiver"]
-[6.115097522735596, 5.58546781539917, "[FF] Quantity of the SFH4205 = Duplicated in every module"]
-[5.14736795425415, 2.282843589782715, "[TT] Mission Type of the MULA = EO"]
-[11.456127166748047, 6.492474555969238, "[FF] Parameter of the Proton detector (LDT) = Value"]
-[7.450783729553223, 3.5852065086364746, "[FF] Purpose of the SGR-ReSI = Sensing the Earth using GNSS Signals"]
-[6.946575164794922, 1.579880952835083, "[FF] Project Status Presentation of the James Webb Space Telescope = Phil Sabelhaus, \"James Webb Space Telescope (JWST) Project Status for the AAS Town Hall,\" January 5, 2010"]
-[3.3320515155792236, 5.489393711090088, "[TT] RF Bandwidth of the SAR Antenna = 11.6, 17.3, 30, 50, or 100 MHz"]
-[6.436054229736328, 0.9587404131889343, "[TT] Mercury Orbit Arrival Date of the BepiColombo = End of 2025"]
-[6.519893646240234, 4.580283164978027, "[FF] Role of the MiWarS = Backup"]
-[5.3428754806518555, -0.029600538313388824, "[TT] Loss of Contact Date of the TSUBAME = January 27, 2015"]
-[7.328786373138428, 6.314446449279785, "[TT] Timing of the Satnav Signals = Precisely timed to a few billionths of a second"]
-[13.644916534423828, 5.808890342712402, "[TT] Average Power of the Solar Cells = 4 W"]
-[8.28784465789795, 3.1257731914520264, "[TT] Measurement Category of the TEMPO = Ozone, Trace gases (excluding ozone)"]
-[4.598627090454102, 2.5400922298431396, "[FF] Reentry Location of the Skylab-1 = Indian Ocean and parts of sparcely-populated western Australia"]
-[4.822143077850342, -1.8456186056137085, "[TT] Extended Mission of the Chang'e-1 = Crash into the Moon surface"]
-[8.719447135925293, 0.18552327156066895, "[TT] Flyby Distance of the OSIRIS-REx = 2.1 miles (3.5 km)"]
-[7.189150810241699, 5.679990768432617, "[FF] Settings of the RTEP = Adjustable"]
-[9.010024070739746, 5.654077529907227, "[TT] Axis Orientation Accuracy of the Resurs-DK1 = 0.2 arcmin"]
-[10.245485305786133, 7.894576072692871, "[TT] Instrument Size of the Telescope = 430 mm x 190 mm x 135 mm"]
-[5.692685127258301, 4.731278419494629, "[FF] Data Relay of the TGO = Second ExoMars mission"]
-[10.910110473632812, 7.548147201538086, "[TT] Swath width (km) of the VIRR = 10.5-12.5"]
-[6.634006977081299, -0.41728973388671875, "[TT] Cycle Time of the DHS = 60 s"]
-[8.26003360748291, 0.4785407483577728, "[FF] Measurement of the KaRIn = Water level"]
-[12.553218841552734, 6.614185333251953, "[TT] Mass of the Proton Monitor Las Dos Torres = 1.6 kg"]
-[5.591711521148682, 1.8155500888824463, "[FF] Image Acquisition of the ALOS-3 = Satellite body-pointing"]
-[9.660588264465332, -0.6924958229064941, "[TT] Altitude of the Fast-sampling orbit = 857.244 km"]
-[7.683688163757324, -2.537926197052002, "[TT] Scan Start Time of the GOLD = 22:10 UT"]
-[7.816446781158447, 6.31178092956543, "[FF] Integration and Testing Date of the Optical Imaging System = June 14-16, 2007"]
-[8.24574089050293, 3.559626817703247, "[FF] Operation of the RSI = Alternately in eclipsed and sunlight times"]
-[9.003717422485352, 4.975924491882324, "[TT] AOCS Operational Modes of the AlSat-2A = MAS, MGT, MCO, MNO"]
-[4.855133056640625, 7.281468868255615, "[TT] Downlink Data Rate of the RF Communications = 32 kbit/s"]
-[5.775193691253662, 6.982383728027344, "[TT] Instrument Data Rate of the GNSS-RO Receiver = About 53 kbit/s"]
-[10.938575744628906, 7.548847198486328, "[TT] Swath Width of the ATLAS = 17 m"]
-[5.743633270263672, -1.890038251876831, "[TT] Repeat Cycle of the KOMPSAT-3 = 28 days"]
-[9.029709815979004, 8.483487129211426, "[TT] Coherent Laser Light Wavelength of the Telescope = 1.06 \u00b5m"]
-[3.44738507270813, 5.232646942138672, "[TT] Look Direction of SAR Antenna of the RADARSAT-1 = Right"]
-[3.6877808570861816, -0.7120753526687622, "[TT] Orbit of the Spacecraft = SSO"]
-[8.282279014587402, 5.490501880645752, "[FF] Geolocation Accuracy of the Global-1 = Improved"]
-[13.609369277954102, 1.7511498928070068, "[TT] Research and Hardware Facilities Weight of the SpaceX Dragon spacecraft = Approximately 300 kg"]
-[5.989629745483398, 1.887455940246582, "[TT] Inspection Duration of the Orion = Nearly two weeks"]
-[8.614090919494629, 6.205502986907959, "[TT] Far Range LOS Measure of the VBS = 2 DOF"]
-[9.442282676696777, 1.0103979110717773, "[TT] Speed of the New Horizons = Over 30,000 miles per hour"]
-[18.796894073486328, 3.4803547859191895, "[TT] \u0394r (m) of the Marctan = 6.5"]
-[14.300352096557617, 2.7573070526123047, "[TT] Mass of the KOMPSAT-3 = 980 kg"]
-[5.215994834899902, 8.388984680175781, "[TT] Bandwidth of the Instrument = 6 MHz"]
-[9.74968433380127, -0.6056075096130371, "[TT] Target Orbit Altitude of the Bion-M1 = 575 km"]
-[13.449667930603027, 6.813534259796143, "[TT] Power of the Spacecraft = 5.2 kW"]
-[4.969998836517334, 0.37733596563339233, "[FF] Launch Date of the SpaceX = 24 January 2021"]
-[7.890519618988037, 7.9613237380981445, "[FF] Detection Range of the VIIRS = Green to near-infrared"]
-[3.3648250102996826, 6.421722412109375, "[TT] Dish Size of the Stanford Research International = 18.3 m"]
-[14.073075294494629, 3.2306149005889893, "[TT] Mass of the Trailblazer = 110 kg"]
-[4.436628818511963, -0.05547541752457619, "[FF] New Launch Date of the Starliner = Unknown"]
-[10.544572830200195, 6.668686866760254, "[TT] Mirrors of the EGS = 318"]
-[3.416443109512329, 2.3778433799743652, "[TT] Display Location of the Copernicus Sentinel-6 = IAGB space test center in Ottobrunn near Munich"]
-[6.9021100997924805, 7.523946285247803, "[TT] Complex Amplitude Resolution of the Digital Mixer = 16-bit"]
-[3.899789571762085, 3.4473190307617188, "[FF] Testing Start Date of the Galileo Second Generation = 19 July 2021"]
-[6.440563201904297, 3.1068668365478516, "[FF] Service of the Spire Global UK = Manage busy docks safely and market traders to price the goods carried aboard"]
-[8.281661987304688, 7.735074520111084, "[TT] Number of Detectors of the Telescope = 2 (+2 redundant)) 1 (+1 redundant) 1 (+1 redundant)"]
-[9.765204429626465, -0.3190239667892456, "[TT] Altitude Range of the Cluster = 25 000 km to 125 000 km"]
-[4.595943450927734, 4.522678852081299, "[FF] Use of the Lemur-2 = Track maritime, aviation, and weather activity from space"]
-[7.760678291320801, 6.9528326988220215, "[FF] Nominal Value for L of the Michelson Interferometer = Given in the table"]
-[8.708687782287598, -0.22870275378227234, "[TT] Inclina. (\u00ba) of the Meteor-1-1 = 81.2"]
-[7.9224019050598145, 0.5568280816078186, "[TT] Sea Ice Development Revisit Frequency of the ROSE-L = One day"]
-[4.683612823486328, 8.09488296508789, "[TT] Frequency of the Radar = 13.4 GHz"]
-[10.91057300567627, 10.101941108703613, "[TT] Mission Duration of the Alpha Magnetic Spectrometer = 12 years"]
-[10.024604797363281, 2.7085776329040527, "[TT] Launch Time of the Kaber (NanoRacks Microsat Deployer) = 21:44:57 UTC"]
-[9.958463668823242, 8.133832931518555, "[TT] Focal Length of the Stereo 6 and 7 = 237.2 mm"]
-[10.22880744934082, 8.430076599121094, "[TT] Entrance Pupil Diameter (mm) of the FCI-TA = 300"]
-[10.1029052734375, -1.5739383697509766, "[TT] Inclination of the GCOM-W1 = 98.2\u00ba"]
-[12.624002456665039, 3.0796308517456055, "[TT] Dry Mass of the DMC Propulsion Subsystem = < 6 kg"]
-[4.442882537841797, -0.03420489281415939, "[TT] Landing Date of the Starliner = 22 December 2019"]
-[7.721029281616211, 1.7622588872909546, "[FF] Emissions Contribution in 2020 of the Sudd wetlands in South Sudan = Unknown"]
-[7.069491386413574, 7.056578159332275, "[TT] Output Energy of the GEDI Laser = 10 mJ"]
-[7.873531818389893, 8.514731407165527, "[TT] Spectral Range of the Instrument = 0.4 - 2.5 \u03bcm"]
-[16.489608764648438, 3.5959713459014893, "[FF] Purpose of the OneWeb = Provide rural 4G, and one day 5G, Internet signals"]
-[3.9232676029205322, 9.73552417755127, "[TT] Bandwidth (GHz) of the ICI-7 = 3.2"]
-[7.691639423370361, 5.509810447692871, "[FF] Components of the OCE = 6 high-intensity visible LEDs, an infrared LED, a diffuse calibration panel, and an electrical circuit"]
-[9.633403778076172, 4.049363613128662, "[TT] Dynamic Range of the Magnetic Field Sensor = fT - mT"]
-[4.529139518737793, -0.859967827796936, "[FF] Action of the Canadarm2 = Reached into the back of the SpaceX Dragon resupply ship and extracted the new HISUI experiment device"]
-[5.442772388458252, 6.36519193649292, "[TT] Data Storage of the Spacecraft = 500 Mbit bus + 2 Gbit fpr payload data at EOL"]
-[10.12753963470459, 5.559841156005859, "[TT] Cooling Method of the SWIR Detectors = Cryocooler"]
-[6.640149116516113, -0.5005553960800171, "[TT] Table Composition Time of the Inter-satellite Antenna = 8 hours"]
-[5.089000225067139, 0.35631754994392395, "[TT] Launch Date of the TRACE = 2 April 1998"]
-[8.807873725891113, 7.620268821716309, "[TT] Pixel Size of the Point-source Detectors = Tens of meters"]
-[13.41012191772461, 6.886183738708496, "[FF] Power Generation Capability of the SJ-9A = Fairly large"]
-[6.855768203735352, 1.2948096990585327, "[TT] Launch of the Telescope = 2019"]
-[9.64697551727295, 8.311485290527344, "[TT] Field of View (FOV) of the MVIRI = 18\u00b0"]
-[13.429168701171875, 2.8858115673065186, "[TT] Mass of the GHOSt satellites = 91.4 kg"]
-[6.496130466461182, 7.5860466957092285, "[TT] Data Quantization of the Instrument = 12 bit"]
-[8.584864616394043, 5.131570816040039, "[TT] Maximum Acceleration Control Range of the GFO Accelerometer = \u00b12.5 x 10-4ms-2"]
-[13.601383209228516, 1.741895079612732, "[TT] Cargo Capacity of the Dragon = 2625 kg"]
-[5.4561004638671875, 3.90408992767334, "[FF] Number of Satellites of the Indian rocket = 31"]
-[9.91337776184082, -1.3426564931869507, "[TT] Orbit Inclination of the PARASOL = 98.21\u00ba"]
-[5.124540328979492, 8.385869979858398, "[TT] Bandwidth of the EX = 84 MHz, 42 MHz, 28 MHz or 14 MHz"]
-[4.995632648468018, 1.2501455545425415, "[TT] Operational Date of the INSAT-3D = January 15, 2014"]
-[8.877710342407227, 9.451948165893555, "[TT] Expected Improvement of the TANSO-FTS-2 = Substantial"]
-[6.353288650512695, -0.7427644729614258, "[TT] LTDN of the TARANIS = 10:30 hours"]
-[6.103230953216553, 3.3058464527130127, "[FF] Purpose of the OPS-SAT = Enables new ideas, concepts and software to be tested in space"]
-[4.9726362228393555, 0.3218461871147156, "[TT] Launch Date of the AEM-2 = 18 Feb 1979"]
-[8.999124526977539, 5.597221374511719, "[TT] Pointing Control of the Adcole Maryland Aerospace MAI401 ADCS = Better than a tenth of a degree"]
-[14.659762382507324, 6.616654872894287, "[TT] Capacity of the Batteries = 30 W hr"]
-[6.190648078918457, 4.030762195587158, "[FF] Architecture of the MERLIN Satellite = Based on the AS250 (AstroSat) avionics core and integrates all Myriade Evolutions common units"]
-[7.107780456542969, -0.4926801025867462, "[TT] Main Rotation Period of the Philae = 24 seconds"]
-[4.73879861831665, 7.9763031005859375, "[TT] Operational frequency range of the HPA = 28 MHz - 85 MHz"]
-[9.081189155578613, 4.520658493041992, "[TT] Charging and SciD Mode Operation of the ADCS = Solar panels towards the sun with constrain +Y of the spacecraft pointing as close as possible towards the nadir direction"]
-[13.212159156799316, 3.089942216873169, "[FF] Reusability of the Terran R = Both stages and its payload fairing will be reusable"]
-[14.286978721618652, 2.901456832885742, "[TT] Mass of the AprizeSat-7 and AprizeSat-8 = 12 kg"]
-[10.104007720947266, -1.518212080001831, "[TT] Inclination of the GRACE Satellite = 89\u00ba"]
-[5.465093612670898, 6.082713603973389, "[TT] Microcontroller Flash Memory of the CC430 SoC = 32 kB"]
-[13.51077651977539, 7.225958824157715, "[TT] Power (at start of mission) of the S/C = 33 W (at 28 V)"]
-[5.8900370597839355, -0.8404425978660583, "[TT] Design Life of the SARAL spacecraft = 5 years"]
-[9.035429000854492, 4.508093357086182, "[TT] Sensor Quantity of the ADS = 6 sun sensors"]
-[10.47360610961914, 2.2774767875671387, "[FF] X-ray Source Obscuration of the The Teacup = Heavily obscured"]
-[6.780172824859619, 5.988041877746582, "[TT] Quantity of the DSHA = 2"]
-[10.725691795349121, 7.5091071128845215, "[TT] Swath Width of the Spotlight-2A = 10km"]
-[12.735261917114258, 1.9479459524154663, "[TT] Testing Duration of the SAGE-III = Nearly five years"]
-[5.5074615478515625, 5.5371575355529785, "[TT] Serial Interfaces of the ECS = 12"]
-[10.819677352905273, 1.410845398902893, "[TT] Mass of the Swift J1818.0-1607 = Twice the mass of our Sun"]
-[10.196702003479004, 7.532955646514893, "[TT] Design Concept of the Telescope = Foldable truss concept"]
-[7.468728065490723, 6.235783100128174, "[FF] Captures the laser beam of the CCRR = Yes"]
-[9.296786308288574, 0.9363349676132202, "[TT] Impact Speed of the DART = Around 24,000 km/h"]
-[10.90516471862793, 7.541200637817383, "[TT] Swath Width of the KMSS = 960 km"]
-[6.549322605133057, 4.327703952789307, "[FF] Tracking of the Ground System = Imprecise"]
-[6.089862823486328, 1.6632035970687866, "[TT] Launch Date of the Euclid = 2022"]
-[11.489923477172852, 3.3239612579345703, "[TT] Thrust Capability of the MICROSCOPE = Micronewton"]
-[4.569728374481201, 7.783174514770508, "[TT] Data Transmission Band of the RF = UHF-band (306.775 MHz)"]
-[5.852110862731934, -0.6738050580024719, "[TT] Goal of the Satellite = 5 years"]
-[4.740386962890625, 8.128514289855957, "[TT] Center Frequency of the L2C = 1227.6 MHz"]
-[13.431988716125488, 7.299217224121094, "[TT] Power of the COCTS = 70 W"]
-[7.642549991607666, 1.8679090738296509, "[TT] Focus of the Sustainability Tech = Tropical forest ecosystems in Southeast Asia"]
-[7.922399997711182, 6.173544406890869, "[TT] Launch Date of the Imaging multi-spectral radiometers (vis/IR) = December 18, 2012"]
-[13.967852592468262, 3.1441702842712402, "[TT] Mass of the Corvus-BC 1 = 10 kg"]
-[6.281306743621826, 1.1569288969039917, "[FF] Instrument Status of the GEDI = Operational"]
-[14.344351768493652, 2.8147318363189697, "[TT] Mass of the CINEMA-3 (KHUSat-2) = 4 kg"]
-[4.9771928787231445, 3.332571268081665, "[TT] Manufacturer of the GIOVE-A = SSTL (Surrey Space Technology Ltd.)"]
-[8.064077377319336, 4.733935356140137, "[TT] Dose Measurement Range of the MOSFETs = Between rad and Mrad"]
-[6.527515411376953, 2.432009696960449, "[FF] Localization Capability of the ABEX = Rapid"]
-[13.728283882141113, 5.402162075042725, "[FF] Type of the Triple-junction solar cells = Body-mounted"]
-[10.739599227905273, 1.1401959657669067, "[TT] Mass of the TOI 270 b = Around 1.9 times greater than Earth\u2019s"]
-[7.943818092346191, -0.5627343058586121, "[FF] Event of the Glasgow Glacier = COP26 being held in Glasgow, Scotland, UK in October 2021"]
-[7.969446659088135, 4.71255350112915, "[FF] Role of the Central Bulkhead Assembly = Facilitate connectivity of the imager instrument to the spacecraft platform in the desired semi-kinematic configuration"]
-[9.689509391784668, 0.17108070850372314, "[TT] Number of Main Parachutes of the Parachute System = 3"]
-[8.957293510437012, 5.6365132331848145, "[TT] Pointing Accuracy of the ADCS = \u00b13\u00ba"]
-[8.388677597045898, 3.193918466567993, "[TT] Precision of Ozone Density Profile Determination of the ERIP = 10-15%"]
-[10.40386962890625, 7.585488319396973, "[TT] Swath Width of the S-192 optomechanical scanner = 72.4 km"]
-[6.7889862060546875, 1.8095824718475342, "[FF] URL of the SwissCube = https://phys.org/news/2016-09-swisscubeseven-years-space.html"]
-[12.161357879638672, 4.568864345550537, "[FF] Testing Method of the Sample Retrieval Lander = Dropping a prototype lander in a warehouse-like space at JPL"]
-[6.948054313659668, 4.39919900894165, "[FF] TAG Site Flexibility of the Spacecraft = Maximum"]
-[8.521075248718262, 5.590618133544922, "[TT] On-Ground Postprocessing Requirements of the Satellite = < 5 cm 3D rms"]
-[10.154681205749512, 9.332906723022461, "[TT] IGFOV at Nadir for MWIR and TIR of the Instrument = 2.0 km"]
-[7.3573222160339355, 2.0550174713134766, "[FF] Field of View of the NAC = Smaller portions of the landscape"]
-[3.6103527545928955, 5.1114091873168945, "[TT] Instruments of the NeuSAR = SAR"]
-[6.210407257080078, 3.376002788543701, "[FF] Module of the RAIDS = Kibo module of the ISS"]
-[8.277861595153809, 4.734240531921387, "[FF] Components of the Drag-free control system = Shadow sensor, small cold gas thruster, ADACS"]
-[13.74421215057373, 5.383255481719971, "[TT] Solar Array Type of the EPS = Triple-junction solar cells"]
-[1.9422087669372559, -0.40023893117904663, "[TT] Operation Status of the Van Allen Probes = Nominal"]
-[12.000200271606445, 6.305928707122803, "[TT] Proton Flux Accuracy of the AMS = 1%"]
-[5.7103447914123535, 1.2370942831039429, "[FF] Conference Presentation Date of the GPS/MET = Sept. 12-15, 1995"]
-[5.450595378875732, 3.90576434135437, "[TT] Number of Deployed Satellites of the Cygnus = 35"]
-[9.148575782775879, 3.901301860809326, "[FF] Function of the TASC = Measures the local electric field"]
-[5.64054536819458, 6.674267768859863, "[TT] Data Transmission Rate of the EDRS satellites = Up to 1.8 Gbit/s"]
-[3.0756845474243164, 2.436310291290283, "[TT] Wavefront Error of the Sentinel-4 GRU = 6.0 nm (rms)"]
-[7.295001983642578, 6.615940570831299, "[TT] Integration Times of the Argus = Microseconds to seconds"]
-[8.29047679901123, 7.387312412261963, "[FF] Detector Unit Components of the MSASI = High speed CMOS image sensor and an image intensifier"]
-[8.860491752624512, 5.523101806640625, "[TT] Station keeping accuracy of the AOCS = Better than \u00b10.05\u00ba North-South/East-West"]
-[9.597249984741211, -0.4147297441959381, "[TT] Altitude of the SMDC-ONE = ~ 300 km apogee x 275 km perigee"]
-[13.532160758972168, 7.123803615570068, "[TT] Maximum Power (W) of the PS-1 = 660"]
-[7.103005409240723, 4.425017356872559, "[FF] Unknown of the Instrumentation = Unknown"]
-[6.9514994621276855, -0.4497252106666565, "[TT] Orbit Maneuvers Frequency of the GRACE Satellite = About every 50 days"]
-[6.682619094848633, 5.845223903656006, "[FF] Conference Date of the NASA Optical Communications and Sensor Demonstration Program = August 6-11, 2016"]
-[8.377528190612793, 5.513878345489502, "[TT] Geolocation Accuracy of the Sentinel-2 = < 20 m"]
-[3.3011903762817383, 4.94197416305542, "[FF] SAR Operation Swath of the SeaSat-1 = 97 km wide and 4023 km long"]
-[5.176183700561523, 8.411189079284668, "[TT] Bandwidth of the CRISTAL = 500 MHz"]
-[9.717537879943848, -0.6186390519142151, "[TT] Orbit Altitude of the CHORUS = Approximately 588-602 km"]
-[5.494786262512207, 7.113863468170166, "[TT] Rate of the Data Transmission = 12 Mbit/s"]
-[14.367340087890625, 3.051725387573242, "[TT] Mass of the BlackSky-2 = 56 kg"]
-[13.601799964904785, 2.825054407119751, "[TT] Mass at Launch of the Geo Satellite = 6 tonnes"]
-[7.935433387756348, 7.220754623413086, "[TT] False-alarm Ratio of the Sensor = < 10%"]
-[5.276388645172119, 8.13709831237793, "[TT] Frequency of the IME HF 1 = 100 kHz - 30 MHz"]
-[5.620517253875732, -0.07239376753568649, "[TT] Mission Operations Center Support of the TSIS-2 = 3 years"]
-[7.097767353057861, -0.22687563300132751, "[TT] Orbit Count of the Envisat = 50,000"]
-[9.986878395080566, 5.506289958953857, "[TT] Rotation Capability of the JUICE = True"]
-[5.152613162994385, 0.9741511940956116, "[FF] Mission Date of the INTA Picosatellite OPTOS = April 19-21, 2007"]
-[9.105351448059082, 1.3867532014846802, "[TT] Interstellar Space Survey Start Date of the Voyager 1 = 11 May 2021"]
-[7.791202068328857, 3.124941825866699, "[FF] Purpose of the ATANGO = Application of TanSat XCO2 Retrieval Algorithm in GOSAT Observations"]
-[13.255226135253906, 2.932405710220337, "[TT] Mass of the CubeSats = ~2 kg"]
-[14.026383399963379, 7.136347770690918, "[TT] Output Voltages of the EPS = 5 V, 12 V, and 28 V"]
-[9.351088523864746, 7.263423919677734, "[TT] Spatial Resolution of the WPM = 2 m"]
-[10.996601104736328, 7.580631256103516, "[TT] Swath Width of the MSU-E = 76 km within a FOR of 430 km"]
-[10.443007469177246, 5.746654510498047, "[TT] Temperature of the PM = 18.3~26.7\u00ba"]
-[8.461389541625977, 5.019290447235107, "[FF] Unknown of the L-band Brightness Temperature Disaggregation Method = Unknown"]
-[7.023406982421875, -0.8055027723312378, "[TT] Orbital Period of the TOI 2076 c and d = Exceeding 17 days"]
-[11.743837356567383, 6.793274879455566, "[TT] Energy Resolution Improvement of the NICER = A factor of 8 improvement"]
-[3.237321376800537, 1.8396812677383423, "[TT] Image Acquisition Date of the Sentinel-2A = Feb. 11, 2016"]
-[6.894021987915039, 9.487218856811523, "[TT] NEDT at 300 K of the Band 4 = 0.5 K"]
-[6.460353851318359, -0.5682755708694458, "[TT] Average Session Time of the EAN = 1 hour"]
-[7.757576942443848, 1.9836260080337524, "[FF] Conference Location of the High Spatio-Temporal Resolution Land Surface Temperature Mission = Valencia, Spain"]
-[10.413400650024414, 2.799699544906616, "[FF] Source of Skills and Innovation for MDASat-i missions of the CPUT/F'SATI nanosatellite program = Yes"]
-[10.068355560302734, -1.5439070463180542, "[TT] Inclination of the DSX spacecraft = 43\u00ba"]
-[11.666170120239258, 3.7667200565338135, "[TT] Firing Pressure of the Y-axis Bang-Bang Maneuver = 1.62 bar"]
-[10.491146087646484, 1.0214862823486328, "[TT] Host Star System of the WD 1856 b = Triple star system"]
-[8.269268035888672, 2.5883209705352783, "[FF] Atmospheric Measurements of the POPACS = Data"]
-[8.437214851379395, 4.763104438781738, "[FF] Maneuver Name of the Satellite = Z-flip"]
-[9.636761665344238, 0.2532978653907776, "[TT] Semi-major axis of the PROBA-3 = 36943 km"]
-[3.2884812355041504, 5.6728692054748535, "[TT] Size of the SAR Antennas = One of the largest"]
-[11.010397911071777, 5.997871398925781, "[TT] Shield of the MOSFETs = Each MOSFET has a unique shield covering the sensitive device"]
-[8.474954605102539, 5.310502529144287, "[TT] Star Camera Status of the \u00d8rsted spacecraft = Disabled"]
-[5.868775844573975, 2.7601988315582275, "[TT] EMI/EMC Mitigations of the Legion = Integrated"]
-[9.782785415649414, 8.434120178222656, "[TT] FOV of the STORM = 4.6\u00b0 x 4.6\u00b0"]
-[5.990023612976074, -0.38485386967658997, "[FF] Mission Duration of the CASS = Originally planned as a two-year mission"]
-[4.9263105392456055, 0.7530238032341003, "[TT] Operation Start of the Lunar Pathfinder = Q4 2022"]
-[6.540441989898682, 3.1368918418884277, "[FF] Presentation Date of the Disaster Monitoring Constellation Imagers = Oct. 3-7, 2011"]
-[10.373290061950684, 5.314136505126953, "[FF] Kapton Heaters of the Thermal Management Subsystem = Multiple"]
-[13.01402473449707, 7.057940483093262, "[TT] Platform Total Power Requirement of the WCOM = 250 W"]
-[4.992802143096924, 7.378731727600098, "[TT] Data Rate of the RF communications = 100 Mbit/s"]
-[11.466604232788086, 5.729427814483643, "[FF] Main Structure of the CAST968 bus = Aluminum honeycomb sandwich panels"]
-[14.511655807495117, 6.569380283355713, "[TT] Battery Load Rating of the IMPS = Continuous 100 \u03bcA"]
-[13.273703575134277, 7.707542419433594, "[TT] Transmitted Peak Power of the Radar = 1 kW"]
-[10.987345695495605, 6.343178749084473, "[TT] Mirror Material of the Scan Mirror Mechanism = Silicon Carbide"]
-[3.7846853733062744, 7.1730875968933105, "[TT] Gain of the Antenna for Navigation = Greater than \u2013 4 dBic for elevations > 5\u00b0"]
-[3.438884973526001, 3.6261799335479736, "[TT] Status of the PAZ = In launch preparation"]
-[7.910817623138428, 6.31530237197876, "[FF] Chinese Optical instruments of the CBERS = URL: http://dragon2.esa.int/landtraining2008/pdf/D1L3b_Optical_Li.pdf"]
-[8.296937942504883, -0.48111575841903687, "[TT] Minimum Extent of the Sea Ice = Below 4.0 million km2 (1.54 million square miles)"]
-[9.690804481506348, -0.6121855974197388, "[TT] Altitude of the GOES-R = 35,786 km"]
-[11.649847984313965, 6.828242301940918, "[TT] Sensitivity of the ART-XC = Limited above 12 keV"]
-[4.761828422546387, -1.4024373292922974, "[TT] Launch Date of the Tianwen-1 = July"]
-[8.47240161895752, 7.117565631866455, "[TT] Imager Type of the Altius = 2D"]
-[6.918387413024902, 7.767960071563721, "[TT] Reflector Dimension of the PMI = 1.8 m"]
-[7.630198955535889, 1.4460129737854004, "[TT] Availability of the Global Satellite Mapping of Precipitation (GSMaP) = Since March 2000"]
-[4.803068161010742, 5.165835857391357, "[FF] Requirements of the SoL (Safety-of-Life) applications = Interference and multipath robustness"]
-[13.216341018676758, 5.469668865203857, "[FF] Integration of the Reflectarray Antenna = Solar cells have been added on the opposite side"]
-[4.557158946990967, 0.03312127664685249, "[FF] Announcement Date of the Nearby star HR1099 = Jan. 30, 2000"]
-[10.891850471496582, -0.341476172208786, "[TT] Calibration and Mosaicking Chain Operational Date of the TanDEM-X = End of 2013"]
-[5.3866424560546875, 8.76584243774414, "[TT] Bandwidth of the Band 1 = 402-422 nm"]
-[9.03133487701416, 4.4603495597839355, "[TT] Photodiode Cant Angle of the Sun Sensor Suites = 45\u00ba"]
-[9.000434875488281, 4.367114543914795, "[FF] Reference Vector of the Sun Sensor = Coarse sun model from an astronomical almanac"]
-[9.719634056091309, -0.4635811150074005, "[TT] Altitude of the SpinSat = ~359 km"]
-[6.257543563842773, 2.5995261669158936, "[FF] Function of the Orion's service module = Contain the in-space propulsion capability for orbital transfer, attitude control, and high-altitude ascent aborts"]
-[6.733140468597412, 6.9139509201049805, "[TT] Number of Beams of the RISAT-1 = 126"]
-[3.856799840927124, 6.832823276519775, "[TT] Polarization of the VDES Antenna = Circular"]
-[2.040621519088745, -0.3196549415588379, "[FF] First Radiation Belt Discovery of the Van Allen Probes = Data showing, for the first time, the existence of a third radiation belt"]
-[10.075119018554688, -2.6781980991363525, "[TT] Life Time in Orbit of the Astrium MMFU NAND-Flash SDR-SDRAM = Up to 12.5 years"]
-[8.088488578796387, 8.462178230285645, "[FF] View of the VNIR = Spectralon plate at the poles"]
-[4.38787317276001, 2.9391143321990967, "[TT] Location of the HTS: Hawaii Tracking Station, Kaena Point, HI = Kaena Point, HI"]
-[3.297180414199829, 6.49185848236084, "[TT] Antenna Diameter of the VSAT = 1.2 m"]
-[9.022538185119629, 2.916020154953003, "[FF] Presentation Date of the Next-Generation Formation Flying Solar Coronagraph = May 27-28, 2014"]
-[5.2681498527526855, 0.7324745059013367, "[TT] Meeting Date of the ISSP = January 2011"]
-[6.183325290679932, 2.4846508502960205, "[TT] Developers of the Carruthers Geocorona Observatory (GLIDE) = Ball Aerospace and University of California (UC) Berkeley"]
-[4.864725589752197, 7.2923502922058105, "[TT] Data Transmission Rates of the RF radio = FM communication = 1200 bit/s, CW communication (beacon) = 20 wpm"]
-[6.811511039733887, 6.165355205535889, "[FF] Level 1 B Pan-Sharpen Processing Time of the EO System = Unknown"]
-[6.789834499359131, 7.470505714416504, "[TT] Beam width of the SSMIS = 3.3\u00ba-6\u00ba"]
-[6.479427814483643, -0.7676427364349365, "[TT] LTAN of the FTS = 13:00 \u00b1 0:15 hr"]
-[6.329493522644043, 8.216553688049316, "[TT] No of bands/channels of the MWHS = 5"]
-[8.41787338256836, 2.0943098068237305, "[FF] Legacy of the SeaSat = Satellite Scatterometer Wind Vector Measurements"]
-[10.28162670135498, 1.8728166818618774, "[TT] Observation Objective of the NuSTAR = Study the supernova"]
-[5.433654308319092, 2.2116787433624268, "[FF] Team Structure of the HORYU-4 = Professors-staff, and students"]
-[10.898881912231445, 7.506978511810303, "[TT] Swath Width of the JL-1-GF03B = 17 km"]
-[7.902063369750977, 3.720451593399048, "[FF] Instruments of the Meteor M2-2 = Two multi-channel scanners and cameras, microwave radiometer, infrared spectrometer"]
-[7.488648891448975, -0.7736669182777405, "[TT] Contaminant Dissipation Time of the ICESat-2 = Fourteen days"]
-[8.632174491882324, 3.4650611877441406, "[FF] Products of the CERES = Solar-reflected and Earth-emitted radiation from the top of the atmosphere to the Earth's surface"]
-[12.138602256774902, 1.967787504196167, "[FF] Launch Date of the CartoSat-2B = April 2010"]
-[6.0991435050964355, 4.343086242675781, "[TT] Stand on Duty with of the FY-3D = FY-4A"]
-[3.8777899742126465, 3.3918673992156982, "[FF] Test Date of the Galileo Satellites = 4 December 2018"]
-[7.35821008682251, 4.7844648361206055, "[FF] Origin of the SPA = Expanded and refined from the appliqu\u00e9 sensor network"]
-[14.200094223022461, 6.590694904327393, "[TT] Battery Energy of the QuikTOMS spacecraft = 10 Ah"]
-[13.890902519226074, 7.295750141143799, "[TT] Peak Current of the Pulsed Diode Driver = 4 A"]
-[10.016387939453125, -1.5124162435531616, "[TT] Orbit Inclination of the Pegasus rocket = 6\u00ba"]
-[7.714682579040527, 1.6358035802841187, "[FF] Commercial Results of the SeaSat = Improved forecasts lead to better routing of ships with substantial savings in operating costs"]
-[6.762962341308594, -0.4062209129333496, "[TT] Period of the Harmony satellites = 98.74 minutes"]
-[13.277194023132324, 7.58595085144043, "[FF] HPA of the ASCAT = High Power Amplifier"]
-[13.628162384033203, 3.933466672897339, "[FF] Mass Spectrometer of the Kaguya = Present"]
-[6.626627445220947, -1.945982813835144, "[FF] Orbit Duration of the Jason-2 = Three years"]
-[5.242571830749512, 4.5172119140625, "[FF] Purpose of the Advanced Satellite Navigation Receiver = Perform the first ever satnav positioning fix in lunar orbit"]
-[7.588098526000977, 6.385523319244385, "[TT] Acquisition Frequency of the Navigation Images = About every 4 hours"]
-[11.242734909057617, 5.371905326843262, "[TT] Scintillator Material of the Gamma-ray Counter = CsI (Tl)"]
-[5.237626552581787, 6.607728481292725, "[TT] Receiving Sensitivity of the AIS Data Receiver = -112 dBm"]
-[8.338006973266602, 3.27517032623291, "[TT] Ozone Limb Sounding of the SOLSE = 100%"]
-[4.912845611572266, 8.182173728942871, "[TT] Measurement of the MWR = Stoke's parameters at Ka-band"]
-[6.2145538330078125, 7.718337059020996, "[TT] New York Second (NY sec) of the FIELDS Instrument = 217/150,000 ~ 0.873813 sec"]
-[3.8579540252685547, 7.876164436340332, "[TT] Packet modulation of the RF communication subsystem = FSK 1200 baud"]
-[10.363140106201172, 4.050711631774902, "[TT] Lateral Deployable Booms of the DSAT#1 = 2 out of 4 deployed as planned"]
-[9.776662826538086, -0.5459152460098267, "[TT] Altitude of the SPROUT = 628 km"]
-[10.08438491821289, 1.2523705959320068, "[TT] Outflow Length of the Milky Way = Hundreds of light years"]
-[6.187500476837158, 2.0420284271240234, "[FF] URL of the CVX\u20132 = http://library01.gsfc.nasa.gov/host/hitchhiker/cvx_2.html"]
-[9.997563362121582, 2.894986152648926, "[FF] Presentation Date of the HARP CubeSat = 3 Aug 2014"]
-[14.295984268188477, 2.7992734909057617, "[TT] Total Mass of the Kondor-E = 1150 kg"]
-[9.44295597076416, 0.7209349274635315, "[TT] Range of the Unit = 75000 km"]
-[6.126577854156494, 3.5100278854370117, "[FF] Purpose of the Project = Develop and commercialize a range of satellites"]
-[1.9466959238052368, -0.40098899602890015, "[FF] Mission Start Date of the Van Allen Probes = 2012"]
-[11.378382682800293, 5.748462677001953, "[TT] Young's Modulus of the Aluminum foil layers = 68 GPa"]
-[7.748925685882568, 8.290633201599121, "[TT] Sensitivity of the GOME-2 = Negligible"]
-[9.215460777282715, 0.9529176950454712, "[TT] Tail Ray Length of the Parker Solar Probe = Nearly 5,000 miles"]
-[7.233513832092285, 9.13566780090332, "[FF] Band Reflection and Transmission of the Dichroic Filter = 400 to 1,000 nm reflected, 900 to 2,500 nm transmitted"]
-[7.529809474945068, 7.008667469024658, "[TT] Scan Period of the ScaRaB = 6 s"]
-[12.148128509521484, 2.9990084171295166, "[TT] \u03c1Isp of the Thruster = 50% greater than hydrazine"]
-[10.911340713500977, 7.515932559967041, "[TT] Swath of the Vidicons = 2770 km"]
-[8.345600128173828, 9.024616241455078, "[TT] Wavelengths of the PACS = 70 \u00b5m (blue)"]
-[12.15997314453125, 3.6414315700531006, "[FF] Development of the Xenon Gas Flow Control System = First flight test"]
-[7.809019088745117, 2.467374801635742, "[FF] Application of the NIRST = Forest fires detection and monitoring"]
-[8.4216947555542, 1.895128607749939, "[TT] Roundtrip Time to Match OceanSat-2 Angle of the RapidScat = 4.0 ms"]
-[10.172646522521973, 5.729719638824463, "[FF] Mounting of the QWIP Detector = Directly to the 55 K coldfinger of a 1 W tactical cooler"]
-[10.412264823913574, 4.902026176452637, "[FF] Attachment Method to Radiator of the Superelastic Springs = Attached to the radiator with screws"]
-[5.205338954925537, 0.6010932326316833, "[FF] Launch Date of the Psyche spacecraft = Next year"]
-[8.775588989257812, 2.760234832763672, "[TT] Positional Error of the SPG4 = 1000 m"]
-[8.565041542053223, 7.766246795654297, "[FF] Size of the Arrays = 19 meter x 6 meter"]
-[11.926234245300293, 4.983078956604004, "[TT] Volume of the OBC = ~35.4 cm 3"]
-[4.836337566375732, 3.3720428943634033, "[TT] Provider of the S&RSAT = France and Canada"]
-[11.801375389099121, 3.3085367679595947, "[TT] Thrust of the CUS = 73.55 kN"]
-[4.741552829742432, 1.6474074125289917, "[FF] Observation Data of the GCOM-W1 = SHIZUKU"]
-[13.4898681640625, 5.681064605712891, "[TT] Solar Array Power of the MarCO CubeSats = Approximately 35 W (at 1AU)"]
-[9.679104804992676, 6.326549530029297, "[TT] Scan of the VISSR Mirror = 20\u00ba x 20\u00ba"]
-[6.291202068328857, 3.628206729888916, "[FF] Developers of the Spacecraft Design Tool = R. Strunce, F. Eckert, C. Eddy"]
-[4.686245441436768, 8.069911003112793, "[TT] Bandwidths of the Digital Chirp Generator = 225, 75, 37.5 and 18.75 MHz"]
-[11.760592460632324, 3.3253111839294434, "[TT] Maximum Thrust of the Microthrusters = 100 \u00b5N"]
-[7.758834362030029, 4.670244216918945, "[FF] Function of the ECAL = Identify electrons and positrons"]
-[6.370440483093262, 2.521152973175049, "[TT] Mission Count of the Solar Terrestrial Probes (STP) Program = 5"]
-[7.444584846496582, 8.478214263916016, "[TT] Spectral Sensitivity (Spectral Band) of the SXI = 6 to 20 \u00c5"]
-[9.605416297912598, 8.256800651550293, "[TT] Field-of-View of the ISEM = 1\u00b0"]
-[10.19604206085205, 7.820548057556152, "[FF] Size of the Instrument size = Telescope: 170 mm x 420 mm, Electronics: 265 mm x 200 mm x 85 mm"]
-[7.9246320724487305, 7.6088032722473145, "[FF] Function of the Hyperspectral Imaging = Enables the observation and monitoring of surface measurements"]
-[12.369587898254395, 3.1247382164001465, "[TT] Propellant Consumption Rate of the XMM-Newton = Approximately 6 kg per year"]
-[8.38670539855957, 2.613410234451294, "[FF] Cross-Track Error of the Ephemeris = Within \u00b1 100 m"]
-[6.6952385902404785, -0.5330594778060913, "[TT] Orbit Repeat Cycle of the TSX and TDX = 11 days"]
-[5.481703281402588, -1.7384328842163086, "[TT] Design Life of the KOMPSAT-5 = 5 years"]
-[10.883352279663086, 7.490805625915527, "[TT] Swath Width of the Severyanin-M OBRC = 450 - 600 km"]
-[13.42708683013916, 6.740889072418213, "[TT] Operating Power of the Satellite = 8.5 W"]
-[5.713311195373535, -2.101532459259033, "[FF] Geolocation Accuracy of the KOMPSAT-3 = Not provided"]
-[4.413962364196777, 1.866297960281372, "[FF] Interferogram Date of the RADARSAT-2 = March 17, 2014"]
-[8.578880310058594, 0.388775110244751, "[TT] Diameter of the Bennu asteroid = 525-m"]
-[14.100231170654297, 7.191837787628174, "[TT] Voltage of the 28 V bus = 28 V"]
-[3.458587169647217, 3.7447597980499268, "[TT] Payload Location of the AIS = On board PAZ"]
-[8.816767692565918, 0.17089489102363586, "[TT] Comet Distance from Earth of the TESS = About 29 million miles (48 million km)"]
-[5.388293266296387, 1.5522818565368652, "[FF] Imaging Date of the ALOS satellite = September 2013"]
-[5.925221920013428, 0.8030952215194702, "[TT] Image Capture Date of the BepiColombo = 19 April"]
-[5.477275848388672, 0.823148250579834, "[FF] Publication Date of the NICER = 14 August 2018"]
-[8.826971054077148, 0.9427490830421448, "[TT] Affiliation of the Parker Solar Probe = Johns Hopkins University Applied Physics Laboratory"]
-[7.497400760650635, 6.915935039520264, "[TT] Cadence of the Neutral Particle Dose Rate = 1 minute"]
-[3.3779337406158447, 5.28584098815918, "[TT] Ku-band range Noise SAR of the Jason-2 = 1/0.5/0.5 cm"]
-[6.119553565979004, 7.026674270629883, "[TT] PPM Slot Rates of the Optical Downlink = 0.311 \u2013 5 GHz"]
-[4.061619758605957, 2.06658935546875, "[TT] Launch Vehicle of the G\u00f6kt\u00fcrk-1 = Vega VV08"]
-[7.193752765655518, 6.773080825805664, "[TT] Pointing Accuracy of the Laser subsystem = about 100 \u00b5rad"]
-[5.863827228546143, -2.2535109519958496, "[TT] Inclination of the KOMPSAT-6 = 97.42\u00ba"]
-[3.9407296180725098, 0.19321615993976593, "[TT] Launch Date of the SMART-1 = 2003"]
-[5.886916637420654, 4.907559871673584, "[FF] Function of the Anchor Stations = Provide the RF communication link and serve as interface for the satellite payload data"]
-[9.215401649475098, 3.777845621109009, "[FF] Dynamic Testing Actuation of the Solar Array = Sinusoidal actuation at the array root with a motor"]
-[9.215982437133789, 4.172423839569092, "[FF] Components of the Sensor Suite = IMU, magnetometer"]
-[9.725504875183105, 7.562401294708252, "[TT] Scan Period of the Rotating Telescope Scanner = 1.729 s"]
-[10.605600357055664, 3.9286179542541504, "[TT] Flight Heritage of the CanX-2 = 1 mission"]
-[9.923785209655762, 7.314155578613281, "[TT] Ground Sampling Distance of the Deimos-1 = 22 m"]
-[8.157302856445312, -1.0843297243118286, "[FF] Tree Height Measurement of the ICESat-2 = Global"]
-[5.505831241607666, 2.722170352935791, "[TT] Design and Build Contributors of the SAPPHIRE = Students at Stanford University"]
-[6.197725296020508, 2.535703659057617, "[TT] Number of Visitors of the International Space Station = More than 230 people"]
-[6.325005054473877, 2.3515796661376953, "[FF] Window Damage Assessment of the EFT-1 Orion = ORDEM 3 predicted 0.2 features of 0.3 mm and greater diameter"]
-[5.049862861633301, 0.6806958913803101, "[FF] Launch Date of the DSCOVR = Feb. 9, 2015"]
-[7.004838466644287, -0.325531929731369, "[TT] Operation Mode of the ASAR = High-rate mode for up to 30 minutes per orbit, including 10 minutes in the eclipse phase"]
-[8.187047958374023, -1.0056352615356445, "[FF] Measurements of the RA-1 = Precise altitude, Significant wave height, Ocean surface wind speed, Various ice parameters"]
-[12.787586212158203, 7.538611888885498, "[TT] Instrument Power of the Instrument = 35 W"]
-[11.187820434570312, 5.399956703186035, "[TT] Plastic Scintillator of the Range Calorimeter = 1cm thick"]
-[9.330329895019531, -1.2027347087860107, "[FF] X-axis orientation to the station longitude for GOES of the EFC (Earth Centered Fixed) = -"]
-[14.2515287399292, 3.129798650741577, "[TT] Mass of the IRS-1B = 975 kg"]
-[9.999126434326172, 8.188981056213379, "[TT] Aperture of the Optics = 20 mm"]
-[5.447388648986816, 7.301012992858887, "[TT] Data Rates of the Channel = Variable from 37 Mbit/s to 336 Mbit/s"]
-[9.042892456054688, 5.538224697113037, "[TT] Field-of-View of the MEMS device = Greater than \u00b160\u00ba"]
-[8.50434398651123, 1.6808147430419922, "[TT] Range of Values of the Integrated water vapor = 0 - 80"]
-[5.542529582977295, 4.979640007019043, "[FF] Software of the Phoenix GPS Receiver = eXtended Navigation System (XNS)"]
-[6.209322452545166, 0.15658235549926758, "[TT] Crew Capacity of the OWS = 3-person"]
-[8.150115966796875, -2.297152280807495, "[TT] Orbit Altitude of the GOLD = 22,000 miles (35,786 km) above the Earth"]
-[9.621501922607422, 4.727537631988525, "[TT] Attitude Control of the SCD-2 = Spin-stabilized"]
-[9.408501625061035, 6.120120525360107, "[TT] Elevation Angle for Downlink of the ASNARO = 90\u00ba"]
-[9.942510604858398, -0.25819113850593567, "[TT] Altitude of the DMSP Satellites = Ranging between 833 km and 850 km"]
-[5.969322681427002, 5.497104167938232, "[TT] Implementation of the Digital Beamforming = On-board in real time and on the ground in the data processor"]
-[5.323670387268066, 5.647613525390625, "[TT] Data Bus of the JWST Avionics = MIL\u2010STD\u20101553"]
-[5.368487358093262, 0.8394950032234192, "[FF] Senior Review Date of the TIMED = Nov. 15, 2005"]
-[8.234006881713867, 7.435200214385986, "[TT] CCD Detector Light-Sensitive Areas of the DNB = 4"]
-[7.484270095825195, 3.5097153186798096, "[FF] Debris Removal Solution of the Satellite = De/orbiting propulsion system installed on the satellite prior to launch"]
-[6.693068027496338, -0.3074936270713806, "[FF] In-Orbit Results of the AlSat-2A = 6 years"]
-[4.516983985900879, 6.600919246673584, "[TT] Components of the GSVF = RF constellation signal simulator"]
-[10.217403411865234, 8.06418514251709, "[TT] Aperture of the Telescope Assembly = 45 cm"]
-[14.257442474365234, 3.1780083179473877, "[TT] Mass of the CADRE = 4 kg"]
-[8.36357307434082, 7.7115559577941895, "[FF] Power Consumption of the STL-11000M SBIG Camera = Low"]
-[12.425013542175293, 0.6483440399169922, "[TT] Temperature of the PLATO detectors = Lower than \u201365\u00b0C"]
-[11.043824195861816, 0.6574916243553162, "[FF] Newly-Found Planets of the Keck Observatory = Unknown"]
-[6.782398700714111, -0.5453887581825256, "[TT] Orbit Period of the Genesis-2 = 96 minutes"]
-[4.577737808227539, -0.78328537940979, "[TT] Docking Location of the Cargo Dragon = Harmony module"]
-[5.58087682723999, 2.5074405670166016, "[FF] Funding of the Euro-Argo ERIC = Members and observers, European Commission (EC)"]
-[4.313694000244141, 6.09333610534668, "[FF] Purpose of the Patch Antenna = Maintain a radio link between the two satellites"]
-[5.559731483459473, 0.7532318830490112, "[FF] Development Date of the CHRIS = Unknown"]
-[4.971243381500244, 3.301278829574585, "[TT] Manufacturer of the TESIS = LPI (Lebedev Physical Institute)"]
-[10.116440773010254, 3.1576435565948486, "[FF] Technology Readiness Level of the CubeSats = Higher"]
-[8.525394439697266, 0.9108725190162659, "[FF] Desired Quake Magnitude of the InSight = Bigger than 4.0"]
-[11.803365707397461, 6.711988925933838, "[TT] Proton Energy Range of the CPD = 250 keV - 30 MeV"]
-[8.345317840576172, 0.8239327073097229, "[TT] Spatial Resolution (km) of the Snow water content = 25"]
-[5.257198333740234, 4.573358535766602, "[TT] Autonomous Functionality of the Ground Station Receiver = Not autonomous"]
-[5.461334705352783, 3.853527545928955, "[TT] Number of Satellites of the Spacety = 21"]
-[8.420762062072754, 1.7943296432495117, "[FF] Sea-Surface Temperature Accuracy of the VIRR = \u00b1 1.7 \u00baC"]
-[6.431520938873291, 1.107094645500183, "[FF] Presentation Date of the WINDS = Feb. 15, 2006"]
-[2.9562809467315674, 2.371687173843384, "[FF] Nitrogen Dioxide Concentrations Change of the Copernicus Sentinel-5P = Beijing: -35%, Chongqing: -45%"]
-[4.8330488204956055, 2.5272693634033203, "[FF] Program of the Eutelsat Quantum = ESA Advanced Research in Telecommunications Systems (ARTES 33.3) program"]
-[5.148393154144287, 2.5403707027435303, "[FF] Document URL of the EUMETSAT = http://www.eumetsat.int/website/wcm/idc /idcplg?IdcService=GET_FILE&dDocName=PDF_DMT_112370&"]
-[9.718935012817383, 4.616349697113037, "[FF] Torque Type of the Attitude Control System = Attitude control torque"]
-[9.850555419921875, 4.548154830932617, "[FF] Attitude Actuators of the SUNSAT = 3-axis reaction wheels, 3-axis magnetic torquer coils"]
-[11.696099281311035, 0.170793816447258, "[TT] Size Range of the TESS = 80% the size of Earth to comparable to or exceeding the sizes of Jupiter and Saturn"]
-[9.763479232788086, 0.4089456796646118, "[TT] Formation Station Keeping of the PROBA-3 = 25 m to 250 m"]
-[5.147784233093262, 7.01793909072876, "[TT] Downlink Speed of the ColKa = Up to 50 Mbit/s"]
-[10.705981254577637, 5.313963890075684, "[TT] Concentration Range of the DE probe = 10^4 - 10^7 cm^-3"]
-[7.252578258514404, -0.715032696723938, "[TT] Orbit Period of the ICESat-2 = 91 days"]
-[7.952927589416504, 4.533216953277588, "[FF] Conjunction Analysis of the STARE satellite = Higher level of confidence"]
-[12.671954154968262, 3.881214141845703, "[FF] Imaging of the CuPID = Spatial and temporal ion dispersion signatures in the magnetospheric cusps"]
-[10.979826927185059, 7.248393535614014, "[TT] Swath Width of the DubaiSat-2 = 12 km"]
-[6.637613773345947, 6.617671966552734, "[TT] Successful Laser Connections of the EDRS-SpaceDataHighway = 10,000"]
-[7.614614486694336, 1.2138590812683105, "[FF] Symposium Date of the WatER = March 13-18, 2006"]
-[7.309349536895752, 2.7245686054229736, "[FF] Imaging of the DAVINCI and VERITAS missions = Near-infrared imaging"]
-[7.341150283813477, 8.87701416015625, "[TT] Filter Type of the FUV channel = Block with Aluminum"]
-[4.87159538269043, 0.5413780212402344, "[TT] Milestone B Certification Date of the WSF-M = May 15"]
-[7.230504035949707, 6.538976669311523, "[TT] Output of the Timer IC = One pulse lasting one second"]
-[11.788235664367676, 6.715469837188721, "[TT] Energy Range of the IRM = 0.1-100 eV"]
-[9.877294540405273, 6.4842915534973145, "[FF] URL of the Nimbus Earth Radiation Budget (ERB) Experiment = http://journals.ametsoc.org/doi/pdf/10.1175/1520-0477%281993%29074%3C0815%3ATNERBE%3E2.0.CO%3B2"]
-[8.447510719299316, 6.677899360656738, "[FF] Purpose of the IQS (Image Quality Subsystem) = Perform image measurement and payload characterization work"]
-[10.120055198669434, 4.679591655731201, "[TT] Control Speed of the Wheels = 3500 rpm"]
-[7.22887659072876, 3.4184370040893555, "[FF] Tracking Opportunities of the LARES-like satellites = Several times per day"]
-[7.855001449584961, 8.768380165100098, "[TT] Minimum Lower Band Edge of the Pan (WorldView-1) = 400 nm"]
-[8.012787818908691, -0.758824348449707, "[FF] Purpose of Receiving Station in Sodankyl\u00e4, Finland of the COSMO-SkyMed = Monitor ice formation and movements and Arctic changes"]
-[5.613334655761719, 0.2960719168186188, "[FF] Operation Completion Date of the KIKU No. 8 = January 11, 2017"]
-[3.52441143989563, 5.076145648956299, "[TT] Radar Wavelength of the Biomass satellite = Around 70 cm"]
-[9.586470603942871, 4.804907321929932, "[TT] Spacecraft Stabilization of the FY-4 spacecraft series = Three-axis stabilized"]
-[7.874817848205566, 7.270364761352539, "[TT] Data Transmission Rate of the HD-TV Camera = 4 Mbit/s"]
-[10.23607063293457, 7.287262916564941, "[TT] Optics Design of the UV WFOV Imager = Off-axis three-mirror design"]
-[9.009381294250488, 7.170111656188965, "[TT] Camera Position of the DMS = Mounted on the belly of the plane"]
-[7.940891265869141, 6.3744215965271, "[TT] Operation Mode of the PSA = Along-track imaging (default mode)"]
-[5.812958717346191, 3.320885181427002, "[FF] Manufacturer of the GOES Sounder = NASA"]
-[6.380906581878662, -1.2923877239227295, "[TT] Measurement Date of the GRACE-FO = 22 June 2020"]
-[6.462250709533691, 3.537137508392334, "[TT] Installation of the Refabricator = EXPRESS Rack on the space station"]
-[14.234260559082031, 3.1963918209075928, "[TT] Mass of the DIDM = 2.2 kg"]
-[5.119472980499268, 0.4097425043582916, "[TT] Launch Date of the TRACE spacecraft = April 2, 1998"]
-[9.984445571899414, 1.5561858415603638, "[FF] Use of the Quasars = Probes of the expansion history of the Universe"]
-[14.18303108215332, 3.2418179512023926, "[TT] Mass of the COSAC = 4.9 kg"]
-[6.713248252868652, -0.5521737337112427, "[TT] Period of the OrbView-2 = 98.2 minutes"]
-[6.386891841888428, -1.268100619316101, "[TT] Measurement Date of the GRACE-FO = October 26, 2020"]
-[5.302438259124756, 1.1075516939163208, "[FF] Operation Start Date of the SMAP = May 19, 2015"]
-[12.06790828704834, 3.0082595348358154, "[TT] Thrusters of the TESS = Hydrazine"]
-[7.6995062828063965, 0.6585679054260254, "[TT] Water Ice Concentration Measurement Range of the Lunar Flashlight = 5 wt% or less to 0.5 wt%"]
-[7.7572221755981445, -0.8711475133895874, "[TT] Data Release Date of the ICESat-2 = May 2019"]
-[7.540762901306152, 1.2334243059158325, "[FF] Imaging of the Lunar Reconnaissance Orbiter = Yes"]
-[10.3428955078125, 2.0263326168060303, "[FF] Number of Known X-ray Sources of the eROSITA X-ray telescope = Roughly doubling the number of known X-ray sources discovered over the 60-year history of X-ray astronomy"]
-[6.671868801116943, 3.958665132522583, "[FF] User Locations of the OUFTI-1 = Must be within the footprint of the satellite"]
-[3.7513539791107178, -0.7071568965911865, "[FF] Orbit of the Open Cosmos satellite = Low Earth Orbit (LEO) and for any inclination"]
-[3.822509288787842, 0.8939986228942871, "[FF] Launch Date of the PSLV = 12 Jan. 2018"]
-[7.747858047485352, 8.768156051635742, "[TT] Band Range of the Spectral bands = 450-900 nm"]
-[7.9781813621521, 13.686371803283691, "[TT] SSD of the B5 = 20 m"]
-[3.8399112224578857, 7.925651550292969, "[TT] Modulation Scheme of the Link 1 = QPSK (Quadrature Phase-Shift Keying)"]
-[8.041303634643555, 9.28170394897461, "[TT] Wavelength of the Liquid water = 1.9 \u00b5m"]
-[5.168316841125488, -1.0617220401763916, "[TT] Expected Service Start of the Konnect = Fall"]
-[6.723134994506836, 6.42378044128418, "[FF] MSP/MGN Operation Data of the Hitomi = Only HK data during visible time"]
-[11.362092018127441, 4.381804466247559, "[TT] Size of the QBSout-1S = 2.5U"]
-[7.980823040008545, 5.22268009185791, "[TT] Inter-satellite Distance of the FLLS = 25 m to 250 m"]
-[6.083666801452637, 5.667051792144775, "[TT] Performance Advantage of the FPGA based parallel computing = 100 x"]
-[7.452022552490234, -0.4570513367652893, "[TT] Orientation Control of the GRACE satellites = to a level of a few mrad"]
-[6.555804252624512, 2.133908748626709, "[FF] URL of the ATMOS Instrument = http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19880005100_1988005100.pdf"]
-[11.675376892089844, 4.761207103729248, "[TT] Diameter of the Aluminum Spheres = 10 cm"]
-[5.376049995422363, 6.898736476898193, "[TT] Data Rate of the MTG-S Spacecraft = 3 GByte/s at instrument output"]
-[4.768622875213623, 2.954562187194824, "[TT] Development Location of the ABI instrument = Fort Wayne, IN"]
-[8.558855056762695, 3.596322536468506, "[TT] Spectrometer Mounting of the Extinctive Stellar Occultations = Spacecraft"]
-[9.747306823730469, -0.6242601275444031, "[TT] Altitude of the Orbit = 500 km"]
-[8.071492195129395, 3.2331037521362305, "[FF] Rainfall Impact of the OCO-2 = Increased carbon release"]
-[8.084393501281738, 0.5930197834968567, "[FF] Vary the Most of the Reservoirs = Middle East, southern Africa, and the western United States"]
-[7.523354530334473, 5.077625274658203, "[FF] Publication Date of the Copernicus Imaging Microwave Radiometer (CIMR) = December 2021"]
-[13.35393238067627, 7.804955959320068, "[TT] Power of the S-band Transmitter = 5 W"]
-[12.009073257446289, -0.16069012880325317, "[FF] Earth/Moon Stray Light of the TESS spacecraft = ~106 times lower than in low-Earth orbit"]
-[8.201288223266602, 5.4844818115234375, "[FF] Performance Evaluation of the Microhard MHX2420 = Unknown"]
-[3.3600668907165527, 1.4506785869598389, "[TT] Launch Year of the Sentinel-1A/B = 2014"]
-[8.248194694519043, 5.882191181182861, "[TT] RCS Reversely for NDO tracking of the SLATS = 4 times"]
-[4.871871471405029, 0.4817517399787903, "[TT] Launch Date of the ExoMars 2020 = July 2020"]
-[9.552906036376953, 4.041831970214844, "[FF] Components of the GOLF = Sodium vapor resonance scattering filter, Longitudinal magnetic field"]
-[7.926992893218994, 5.846120834350586, "[FF] Purpose of the 3D mode = Acquire the stereo imagery of the target area"]
-[6.354443073272705, 1.4265878200531006, "[TT] Electric Tests Date of the eRosita and ART-XC = May 3 to May 21"]
-[7.593270778656006, 8.981155395507812, "[TT] Spectral Range (\u00b5m) of the Band 2 = 0.84 - 0.89"]
-[5.452393531799316, 3.6396515369415283, "[FF] Contract Release of the JPSS Common Ground System = C18-10"]
-[7.5101823806762695, 3.7533278465270996, "[TT] Axes of the NightPod = 4"]
-[6.675355434417725, 6.165946006774902, "[FF] Sequence of the Optical link = Not provided"]
-[8.642460823059082, 7.470202445983887, "[TT] Sensitivity of the Detector = 10 \u00b5Crab or better"]
-[8.720608711242676, 3.2570183277130127, "[FF] Purpose of the EXIS = Measures ultraviolet flux, crucial for understanding how radiation affects heating in the thermosphere and creating the ionosphere"]
-[7.812437534332275, 2.9934563636779785, "[FF] Observation Type of the TanSat = Similar to Copernicus Anthropogenic Carbon Dioxide Monitoring, CO2M mission"]
-[13.331141471862793, 6.770252704620361, "[TT] Power of the Propulsion = 0.53 W"]
-[1.720462441444397, 6.147234916687012, "[FF] Importance of the Positron Fraction = Understanding the origin of dark matter"]
-[3.34578275680542, 1.4697009325027466, "[TT] Launch Year of the Sentinel-5P = 2016"]
-[11.691885948181152, 6.642417907714844, "[TT] Energy Measurement Range for Protons of the Telescope 2 = 0.8-4 MeV"]
-[4.997108459472656, 2.9886515140533447, "[TT] Operator of the BSOCC = Bowie State University"]
-[6.632502555847168, 4.663049697875977, "[FF] Journal Article of the GPS-aided Automatic Landslide Monitoring System = Pinggen Zhou, Baishen Zhou, Jingjun Guo, Donghang Li, Zhigang Ding, Yanming Feng, \"A Demonstrative GPS-aided Automatic Landslide Monitoring System in Sichuan Province,\" Journal of Global Positioning Systems, 2005, Vol. 4, No. 1-2: pp. 184-191"]
-[11.204060554504395, 1.0122872591018677, "[TT] Proof Mass Distance of the LISA Pathfinder = 35 cm"]
-[3.588470697402954, 5.199422836303711, "[TT] Direction Resolution of the MMW Radar = <\u00b11 arcsec"]
-[9.027166366577148, 3.114414930343628, "[TT] Solar Observations of the FY-4 Series = Enabled for EUV (Extreme Ultraviolet) and X-ray monitoring"]
-[5.290769577026367, 3.3160059452056885, "[TT] Operator of the RemoveDEBRIS = Surrey Satellite Technology Ltd"]
-[5.624106407165527, 1.8844019174575806, "[FF] Deployment Success of the DIWATA-1 = Yes"]
-[7.8406081199646, 8.095072746276855, "[FF] Noise in NIR Channel of the R3 System = Noticeable"]
-[13.906720161437988, 2.947495937347412, "[TT] Mass of the SeaWinds = 205 kg"]
-[9.715044021606445, 8.387463569641113, "[TT] Along-track FOV of the TIR Subsystem = \u00b10.65\u00ba"]
-[7.854560852050781, 8.898449897766113, "[FF] Wavelength Range of the OCO-3 = Entire wavelength range that can be seen by the human eye"]
-[7.025226593017578, 0.8039050698280334, "[FF] Mission Status of the Gravity Probe B = Unknown"]
-[4.750516891479492, -1.8391014337539673, "[TT] Launch Center of the Chang'e-5 = Wenchang Space Center"]
-[10.130996704101562, -2.732548952102661, "[TT] Endurance of the NAND-Flash devices = About 10^5 cycles"]
-[5.427204608917236, 3.0793488025665283, "[TT] Operator of the Hellas Sat 3 = Hellas Sat"]
-[6.614841461181641, 1.6513340473175049, "[FF] URL of the Europa Clipper = https://europa.nasa.gov/spacecraft/instruments/eis/"]
-[6.622453212738037, -0.524456799030304, "[TT] Period of the Tatiana-2 = 101.3 minutes"]
-[9.16763687133789, 5.902109146118164, "[FF] Function of the Calibration Mirror = Block the cold space aperture during Earth view"]
-[8.282812118530273, 6.374203205108643, "[TT] Translation Range of the CCRR = 15 m"]
-[12.179845809936523, 6.922216892242432, "[TT] Charge Separation Range of the STD = Up to Z=26"]
-[3.3416757583618164, 1.549784779548645, "[FF] Application Date of the Sentinel-5P = 17 September 2020"]
-[9.926614761352539, -0.22557978332042694, "[TT] Proposed Altitudes of Operation of the Starlink = Between 340 and 614 kilometers"]
-[4.772585391998291, 2.6151950359344482, "[FF] Beam Reconfiguration of the Eutelsat Quantum = Enabled"]
-[7.588537216186523, 8.630763053894043, "[TT] Number of Bands of the Spectral bands = 5"]
-[5.8009796142578125, 5.321372032165527, "[TT] Function of the OBC = RTC (Real Time Clock)"]
-[4.9691972732543945, 3.417442798614502, "[TT] Manufacturer of the SeaHawk-1 = AAC Clyde Space"]
-[10.230708122253418, 8.047714233398438, "[TT] Optical Telescope Aperture of the Dove-1 = 90 mm"]
-[6.510455131530762, 3.664822578430176, "[FF] Configurations of the Satellite Constellation = Nominal orbital configuration, Interferometric orbital configuration"]
-[1.7297725677490234, 6.13678503036499, "[FF] Purpose of the WFIRST = Explore the nature of dark energy"]
-[5.9766435623168945, -0.5413414835929871, "[TT] Service Life of the CBERS-4A = 5 years"]
-[8.019742965698242, 5.649417877197266, "[FF] Accuracy Improvement of the Map = 10 times more accurate than any previous map"]
-[10.584986686706543, 2.889981985092163, "[FF] Image Taking Condition of the STARE = Nanosatellite\u2019s view must not be obstructed by the Earth or moon"]
-[7.753758907318115, 0.4240323305130005, "[FF] Water Loss Date of the Asteroid 162173 Ryugu = Unknown"]
-[7.806419372558594, 4.851592540740967, "[FF] Function of the INSAT sounder = Measure temperature and humidity profiles"]
-[5.6384663581848145, 5.107614040374756, "[FF] Uplink Verification Method of the Ground System = Transmitting signals in a safe direction while verifying their emissions from the antenna with an on-site technician and a hand-held spectrum analyzer"]
-[6.934589862823486, 1.9320220947265625, "[FF] URL of the Solar Dynamics Observatory = http://sdo.gsfc.nasa.gov/assets/docs/sdo_factsheet.pdf"]
-[9.623292922973633, 3.9980661869049072, "[TT] Servicer Capture Mechanism of the ELSA-d = Magnetic"]
-[4.866387367248535, 7.837014198303223, "[TT] Frequency Bands of the Galileo = E5a, E5b, E6, L1"]
-[8.88079833984375, 0.9642224907875061, "[FF] Responsible Team of the Parker Solar Probe = Modeling teams"]
-[5.254929542541504, 6.757383823394775, "[TT] Science Data Downlink Capacity of the Spacecraft = 105 Mbit/s"]
-[8.634466171264648, 0.1336640566587448, "[TT] Density of the Comet = 470 kg/m3"]
-[4.625713348388672, 2.7136993408203125, "[FF] Direction of the Japan Current = North"]
-[9.6613130569458, 4.045560359954834, "[TT] Stability of the Electrical Field = < 1 mV/m over 1 month"]
-[8.969826698303223, 0.5702592134475708, "[FF] Communication Experiment Date of the ARTEMIS satellite = Sept. 23-27, 2013"]
-[8.663761138916016, 7.604208469390869, "[TT] Pixel Size of the CMOS Active Pixel Sensor = 6.7 \u00b5m x 6.7 \u00b5m"]
-[8.654241561889648, 1.2142192125320435, "[FF] Imaging Concept of the Aquarius = 3-beam pushbroom"]
-[7.576965808868408, 2.7931599617004395, "[FF] Warming Power of the Methane = More than 80 times the warming power of carbon dioxide over 20 years"]
-[8.739493370056152, 7.379334449768066, "[TT] FOR of the Pushbroom imager = \u00b130\u00ba"]
-[6.215603828430176, 5.03740930557251, "[FF] Operation of the OBC Architecture = Independent real time tasks to be executed simultaneously"]
-[9.732565879821777, 8.318894386291504, "[TT] Focal Length of the UVS Instrument = 125 mm"]
-[4.814023494720459, 8.009692192077637, "[TT] Frequency Range of the NCLE = 80 kHz - 80 MHz"]
-[6.471377849578857, 7.593079566955566, "[TT] Data Quantization of the MSU-SK = 8 bits"]
-[8.409200668334961, 7.16982889175415, "[FF] Cameras of the DMSP Block 4 = Two vidicon cameras"]
-[3.8404366970062256, 3.3948678970336914, "[TT] Other Missions of the NewMag = ISEE-1/2 (launch Oct. 2, 1977), AMPTE-UKS (launch Aug. 16, 1984), POLAR (launch Feb. 24, 1996), and Galileo (launch 1989)"]
-[9.948991775512695, 9.021578788757324, "[TT] Effective FOV of the Channel 8 = 21 km x 48 km"]
-[5.755584239959717, 3.7647244930267334, "[FF] Satellite of the Spire Global UK = Nanosatellites"]
-[7.814662933349609, 6.196262836456299, "[FF] Function of the A0 Plotter = Print out the images and analyzed data for the onsite information sharing"]
-[9.094388008117676, 7.550086498260498, "[TT] Fiber Optic Cable Diameter of the Detector Box = 3 mm"]
-[6.0247979164123535, -0.3806830942630768, "[TT] Contact Separation of the PROBA Project = 14h for the nominal operations"]
-[14.275078773498535, 3.2721107006073, "[TT] Total Mass of the ECS = 8 kg"]
-[4.348705291748047, 7.2794928550720215, "[FF] Wavelength of the S-band = 2.5 times shorter than L-band"]
-[10.202686309814453, -0.46259981393814087, "[TT] Altitude of the CeREs CubeSat = 500 km"]
-[7.594257831573486, 1.1304337978363037, "[FF] Water Detection Date of the Bullialdus Crater = August 25, 2013"]
-[14.160391807556152, 3.2064945697784424, "[TT] Mass of the BIROS = 130 kg"]
-[4.612470626831055, 6.587464332580566, "[FF] Data Acquisition Channels of the PDS = X-band channel, ARTEMIS data-relay satellite's Ka-band channel"]
-[7.218076229095459, 4.901468753814697, "[TT] Location of the Puppis-A = Top right"]
-[5.809311389923096, 5.051137924194336, "[FF] Service Spectrum of the NPOESS = Onboard acquisition and transmission (broadcast) of telemetry data in real-time to field terminals of the user community"]
-[13.992980003356934, 3.4941413402557373, "[TT] Losses of the Harness = 1%"]
-[4.397775650024414, 5.44226598739624, "[TT] Release Date of the GomX-3 = October 2015"]
-[8.07054615020752, 8.181963920593262, "[TT] Material of the Infrared Bands = Mercury-cadmium-telluride elements"]
-[10.901918411254883, 2.830686569213867, "[TT] Quantity of the 4 piggyback microsatellites = 4"]
-[6.887962818145752, 7.773059368133545, "[TT] Reflector Dimensions of the SSM/I = 61 cm x 66 cm"]
-[5.220471382141113, 4.0778350830078125, "[TT] Number of active satellites of the MEOSAR Constellation = 17/24"]
-[6.854493618011475, 7.601053237915039, "[TT] Beamwidth of the Reflector = 1.39\u00ba (azimuth) x 1.72\u00ba (elevation) for VV beam"]
-[6.735983371734619, 3.8989500999450684, "[FF] Unknown of the NASA Cargo = Unknown"]
-[14.119401931762695, 3.2191059589385986, "[TT] Mass of the SAS&R Transponder = ~70 kg"]
-[8.787729263305664, 7.669960021972656, "[TT] Control of the CCD system = Prism incidence angle to ~0.5 arc-second rotational resolution"]
-[5.61848783493042, 3.181030511856079, "[TT] Contract Value of the ICON = $50 Million"]
-[12.45714282989502, 0.56524658203125, "[FF] Construction Start Date of the PLATO = 4 October 2018"]
-[14.3500337600708, 3.2445342540740967, "[TT] Mass of the Polizon = 144 kg"]
-[10.154952049255371, 1.3590624332427979, "[TT] Number of Asteroids of the Gaia = 150,000"]
-[10.13144302368164, 1.4722661972045898, "[TT] Number of Galaxies to be Mapped of the Euclid = Up to two billion"]
-[4.532838344573975, 3.4966623783111572, "[TT] Backup of the Ground Station = None"]
-[7.143472194671631, 5.543569564819336, "[FF] Quantity of the MSU-S = Unknown"]
-[12.115022659301758, 7.650712013244629, "[FF] Instrument Mass of the Pushbroom imager = < 41 kg (optics < 35 kg, electronics < 6 kg)"]
-[7.432642936706543, 4.129875183105469, "[FF] Maneuvers of the PROBA-3 = Cooperative far-range hop from WP0 to WP1, Cooperative far-range hop from WP1 to WP2"]
-[9.476038932800293, 0.8549215197563171, "[TT] Road Trip Distance of the Orion = 2,700 miles"]
-[8.0311279296875, 6.254236221313477, "[TT] Earth Imaging Mode of the Imaging System = Scheduled snapshot basis"]
-[13.731197357177734, 2.9425551891326904, "[TT] Mass of the Spacecraft Repeater = 24 kg"]
-[7.873830795288086, -2.4769983291625977, "[TT] Observation Range of the GOLD = Entire Western Hemisphere"]
-[9.674169540405273, -0.4716812074184418, "[TT] Altitude of the LAGEOS = 5858 km x 5958 km"]
-[13.306559562683105, 7.400932312011719, "[TT] Power Range of the ROSA = Hundreds of watts to the megawatt range"]
-[3.969860076904297, 4.253385066986084, "[FF] Radar Image of the ICESat-2 = Acquired on May 18, 2021"]
-[6.733912944793701, 5.2607598304748535, "[FF] Components of the PLC = Motherboard-daughterboard configuration using a single 80C32 microcontroller, a Xilinx XQVR-600 FPGA, a Mil-STD-1553B based control processor and 3 I/O modules along with its power supply"]
-[8.17190170288086, 8.419868469238281, "[TT] Spectral Bands of the VNIR Detector = 10"]
-[9.410709381103516, 5.395696640014648, "[TT] Angular Adjustments of the Mast Alignment = Two"]
-[6.170567989349365, 3.265778064727783, "[TT] Control of the ERA = Can be controlled from both inside and outside the Space Station"]
-[10.822900772094727, 3.915595769882202, "[FF] Reentry Outcome of the Drag Sail = Disintegrate"]
-[8.484089851379395, 2.0335922241210938, "[FF] Function of the OSCAT-3 = Measure wind speeds and vectors at sea level"]
-[4.678640842437744, 3.205876588821411, "[TT] Manufacturer of the TANSO-FTS-2 = Harris Corp. of Melbourne FL, USA"]
-[5.342748641967773, 2.81714129447937, "[TT] Provider of the LICIA = ASI, the Italian Space Agency"]
-[7.671300888061523, 4.647367477416992, "[FF] Secondary Sensor Complement of the DMSP = Now flying on DMSP"]
-[6.481510639190674, 5.07296085357666, "[FF] Function of the IDE = Controls instrument operations and collects instrument telemetry"]
-[9.3707275390625, 6.040476322174072, "[TT] Scanning Mode of the SRG = 6 rotations/day, 1 degree advance per day"]
-[6.498490333557129, 5.544280529022217, "[TT] Mean Availability of the DCS = >95%"]
-[10.001242637634277, -1.48997962474823, "[TT] Inclination of the ICEYE-X14 and ICEYE-X16 = 97.4\u00ba"]
-[3.971073627471924, 6.214992523193359, "[TT] Quantity of the Navigation antennas = 2"]
-[3.4905753135681152, 4.76657772064209, "[FF] Program Start of the SIR-C/X-SAR = MRSE (Microwave Remote Sensing Experiment) flown aboard the Shuttle on the first SPACELAB mission in l983"]
-[4.8233819007873535, -1.580490231513977, "[TT] Components of the Tianwen-1 = Mars orbiter, a lander and a rover"]
-[9.977729797363281, 7.77722692489624, "[TT] Celestial Sphere Coverage of the Telescope = 39.7% at any given time"]
-[8.13676929473877, -1.029618740081787, "[FF] Data Type of the ICESat-2 = Tree Height"]
-[12.170886993408203, -0.20726656913757324, "[TT] Data Collection of the TESS = Light curves on everything in its field of view, every half hour"]
-[10.940598487854004, 7.336761474609375, "[TT] Grid Cell Area of the Satellite Sensors = Roughly 25 km by 25 km (15 miles by 15 miles)"]
-[14.208732604980469, 3.2332003116607666, "[TT] Mass of the Delfi-n3Xt = 3.5 kg"]
-[9.667953491210938, -0.447735458612442, "[TT] Altitude of the Himawari-8 = ~35,800 km"]
-[13.064363479614258, 5.575962066650391, "[TT] External Panels of the GNB = 6"]
-[10.310872077941895, 5.324323654174805, "[FF] Thermal Connection of the Chassis Walls = Well connected"]
-[6.633774757385254, 8.815879821777344, "[FF] Retrieval of Atmospheric Properties and Surface Bidirectional Reflectances of the POLDER = Unknown"]
-[10.395415306091309, 4.043393611907959, "[TT] Length of the Gravity-Gradient Boom = 3 m"]
-[7.318037033081055, 1.033674955368042, "[FF] Requirements of the LunaNet = No extra requirements on the hardware"]
-[8.370589256286621, 7.23897123336792, "[TT] Imaging Modes of the Optical Sensor Assembly (OSA) = Simultaneous imaging in both panchromatic and multispectral modes"]
-[10.97772216796875, 5.655684471130371, "[TT] Heat Shield Material of the Schiaparelli = Norcoat Liege"]
-[4.992656230926514, 8.33611011505127, "[TT] IF Bandwidth (MHz) of the Antenna = 200"]
-[5.826086044311523, 1.153169870376587, "[FF] Meeting Date of the EarthCARE = April 19, 2017"]
-[7.3741135597229, 5.300865173339844, "[FF] Components of the Sounder = EO (Electro-Optics) module, telescope, scan assembly, filter wheel, cooler, detectors, electronics packages"]
-[4.01839017868042, 3.4393715858459473, "[FF] URL of the Galileo = http://m.esa.int/Our_Activities/Navigation/Europe_s_next_Galileo_satellites_in_place_atop_Ariane_5"]
-[8.166735649108887, 5.085883617401123, "[FF] Sensitivity of the SEIS = High"]
-[3.452230453491211, 4.862374782562256, "[TT] Orbital Period of the GOES SAR transponders = 24 hours"]
-[8.780863761901855, 9.431473731994629, "[TT] Spectral Band 1 Bandwidth of the TANSO-CAI = 20 nm"]
-[6.162853717803955, 6.318339824676514, "[TT] Impact Event Record Storage of the MPID = S/C control unit"]
-[6.822783470153809, 4.928249835968018, "[FF] Type of the ABS = Regenerative mode subsystem"]
-[6.501528739929199, 3.548496723175049, "[TT] Activation of the LIRIS Demonstrator = Approach phase with the ISS"]
-[8.522663116455078, 5.393528938293457, "[TT] Position Accuracy (RMS orbit) of the S-2 NRT = < 10 m (2D) 3-sigma"]
-[10.544303894042969, 2.8826591968536377, "[FF] Mission Goal of the Nanosatellite = Micro imaging system, GPS receiver, MEMS based IMU"]
-[5.336716651916504, 4.131410598754883, "[TT] Design of the GETR = Confirmed"]
-[4.52556848526001, 5.658182621002197, "[TT] Beacon Location Accuracy of the SARP-3 = ~ 4 km"]
-[8.472172737121582, 2.0579442977905273, "[FF] Instrument Type of the SeaWinds = Scatterometers"]
-[5.1201372146606445, 8.409212112426758, "[TT] Bandwidth of the MPA = 1.1 GHz"]
-[7.895767688751221, -0.9312587380409241, "[FF] Data Combination of the GRACE = Observations from ICESat and ICESat-2"]
-[5.289580345153809, 7.9924116134643555, "[TT] Frequency Range of the LIGO = 10 Hz to 1000 Hz"]
-[6.811068058013916, 2.1519458293914795, "[FF] URL of the BioSentinel = http://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=3453&context=smallsat"]
-[12.799498558044434, 7.585212230682373, "[TT] Average Power Consumption of the Instrument = 11 W"]
-[8.20573902130127, 0.12063735723495483, "[FF] Heritage of the MTVZA-GY = Meteor-3M-1 mission"]
-[4.961771011352539, 2.1676266193389893, "[TT] Status of the GGAK-M = Functional"]
-[7.0403361320495605, 5.723045825958252, "[TT] Number of \u00b5DPU of the \u00b5ASC = 2"]
-[4.260148525238037, 7.3998003005981445, "[FF] Frequency of the Local oscillator module = X-band local carrier frequency"]
-[6.132314682006836, -0.4150223433971405, "[TT] Operational Service Years of the RADARSAT-2 = 8"]
-[4.392950057983398, 3.018954277038574, "[TT] Ground Control Complex Location of the Kolibri-2000 = Kaluga (Russia)"]
-[10.962467193603516, 2.0701780319213867, "[TT] Image Capture Dates of the XMM-Newton = 19-25 January"]
-[5.0206499099731445, 8.384352684020996, "[TT] Bandwidth of the MWR = 0.5 and 1 GHz"]
-[9.53044319152832, 6.099486351013184, "[TT] Reflector Half Cone Angle of the AMSR-E = 47.4\u00ba"]
-[7.153117656707764, 0.0780521035194397, "[FF] Age of the Fuerteventura = Between 12 and 20 million years"]
-[7.052606582641602, 2.8292031288146973, "[FF] Mission Operations Control Center Creator of the MethaneSAT = Rocket Lab"]
-[5.730909824371338, 6.860957145690918, "[TT] Size of the Raw Science Data Packet = 280 bytes"]
-[7.059910297393799, 6.43032693862915, "[TT] Time Constant of the Fast Shaper = ~300 ns"]
-[8.103537559509277, -1.0954763889312744, "[FF] Function of the Laser Altimeters = Measure how long it takes for light to bounce off the ice and return to the instruments\u2019 sensors"]
-[5.0550856590271, 6.830566883087158, "[TT] Maximum Downlink Rate of the \u00d8rsted satellite = 256 kbit/s"]
-[3.383110284805298, 6.441857814788818, "[TT] Pixel Size (km x km) of the Antenna = 6"]
-[5.333001613616943, 5.615634918212891, "[TT] Interface of the Star Sensor = MIL-STD-1553 bus"]
-[3.495917797088623, 5.374780178070068, "[FF] Support of the SAR antenna = ESS"]
-[10.922451972961426, 3.8990957736968994, "[TT] Avionics/Electronics Stack Size of the InflateSail = Approximately 1U"]
-[8.526124954223633, 8.837823867797852, "[TT] Observation Spectrum of the Herschel = Far-infrared and submillimeter"]
-[10.329045295715332, 1.1866860389709473, "[FF] Red Giant Oscillations of the HD 181068 = Not detected"]
-[6.664796829223633, 8.478975296020508, "[TT] Spectral Channels of the Resurs-P1 = Seven"]
-[4.375949382781982, 3.0142951011657715, "[TT] Location of the GKIR = Kiruna Sweden"]
-[8.952436447143555, 7.139813423156738, "[TT] Camera Properties of the Google Earth = Focus point, range, tilt, azimuth"]
-[3.470740556716919, 4.928287506103516, "[FF] Function of the SAR Controller Electronics = In charge of the command and control of the SSS to achieve the SAR mission"]
-[6.277132987976074, 5.598514080047607, "[TT] Modularity of the BCR = Can be combined in parallel"]
-[10.97015380859375, 5.674286842346191, "[FF] Purpose of the Heat Shield = Extract samples of the ablative material, or Avcoat"]
-[8.1580171585083, -0.3547627627849579, "[TT] Minimum Extent Decline of the Arctic Sea Ice = About 2.7 percent per decade"]
-[7.653602123260498, 8.883567810058594, "[TT] Spectral Range of the Spectral Band D = 0.76 - 0.86 \u00b5m"]
-[8.125273704528809, 7.999551296234131, "[TT] Band of the Camera = TIR (Thermal Infrared)"]
-[11.318317413330078, 2.7917354106903076, "[TT] Mass of the Minisatellite = 383 kg"]
-[3.863163709640503, 6.433006763458252, "[TT] Look Angle of the Antenna = 20\u00ba"]
-[13.383577346801758, 6.750018119812012, "[TT] Power of the Spacecraft = 202 W average (EOL), 254 W max"]
-[6.2925801277160645, 5.607387542724609, "[FF] Memory Module of the MMFU = FMM (Flash Memory Module)"]
-[4.9386420249938965, -2.1612658500671387, "[TT] Propellant Transfer of the Tianzhou-2 = 1.95 tons"]
-[4.987383842468262, 3.893313407897949, "[TT] Manufacturer Location of the Navigation Receiver = Vienna, Austria"]
-[4.413569927215576, 6.747382640838623, "[TT] Communication of the Dove-2 = TT&C over UHF radio"]
-[7.990472793579102, 6.098884105682373, "[FF] Purpose of the Wide view mode = Provide wide area images along with a few sets of neighboring snap shot images"]
-[11.642715454101562, 3.3479583263397217, "[FF] Thrust Capability of the Propulsion System = Variable impulse"]
-[11.700465202331543, 0.13635744154453278, "[TT] Number of Exoplanet Candidates of the TESS = Over 5,000"]
-[13.658214569091797, 2.72033429145813, "[TT] Launch Mass of the TanSat = 620 kg"]
-[4.928375244140625, 5.118751049041748, "[TT] CCSDS ID of the GSAT-0206 = 266"]
-[5.574714660644531, 0.5470898151397705, "[TT] Discovery Date of the NuSTAR = 1 March 2022"]
-[4.589993000030518, 4.6462721824646, "[FF] Purpose of the COSPAS = Support search and rescue operations"]
-[7.547080039978027, 1.3192329406738281, "[FF] Science Requirements Document Release Date of the Surface Water and Ocean Topography (SWOT) = January 26, 2012"]
-[5.701617240905762, -0.9351063370704651, "[TT] Design Life of the ERBS = 2 years"]
-[13.45115852355957, 6.071549892425537, "[FF] Design Conditions of the EPS = 6 hour and 18 hour orbit illumination, large power requirement of the SAR payload, solar eclipse conditions during the summer solstice"]
-[4.782824993133545, 7.982239246368408, "[TT] Frequency Range of the Receiver = 7145 to 7235 MHz"]
-[4.8067169189453125, 0.5483043789863586, "[TT] Rescheduled Launch Date of the OCSD = Late 2017"]
-[10.55534553527832, 5.776147365570068, "[TT] Temperature Control of the Baffle = \u00b10.5 K"]
-[8.76137924194336, 2.343174457550049, "[FF] Composition of the Cloud of gas and dust = Mostly hydrogen and helium, with a small amount of heavier elements such as carbon, nitrogen, oxygen and iron"]
-[8.206949234008789, -0.027053503319621086, "[TT] Operation Duration of the TOPEX/Poseidon = 13 Years (1992 to 2005)"]
-[8.150932312011719, 7.931772232055664, "[FF] Lightning of the Newer neighborhoods = Blue-gray"]
-[14.432713508605957, 6.5596113204956055, "[TT] Outage Duration of the Battery Overvoltage = Approximately 12 hours"]
-[7.48260498046875, 6.429346561431885, "[TT] Image Update Frequency of the GVAR = 30 minutes"]
-[9.108963966369629, 7.476520538330078, "[TT] Pixel Spacing of the MODIS = 300 m"]
-[5.258819103240967, 5.739102840423584, "[FF] Antenna of the EDRS-C = Performance Verification"]
-[5.573642730712891, 5.275538444519043, "[TT] Interface Architecture of the GOES-R Instruments = Point-to-point"]
-[8.717780113220215, 7.533395767211914, "[TT] Format of the Imager = 1280 x 1024"]
-[10.623756408691406, 7.326900959014893, "[TT] Instrument Swath of the Optsat-3000 = 27 km x 27 km"]
-[4.6427998542785645, 2.9600260257720947, "[FF] Operation Status of the Paraguan\u00e1 Refinery Complex = In limbo"]
-[9.57577896118164, -1.004077434539795, "[TT] Orbit Altitude of the GOES-18 = 22,236 miles above the equator"]
-[13.851691246032715, 5.682774066925049, "[TT] Solar Cell Efficiency of the EPS = 26.8%"]
-[10.478759765625, 2.3712308406829834, "[TT] Telemetry of the X-ray Satellite Navigation = 40 kbit/s"]
-[5.501156806945801, -0.18577821552753448, "[TT] Mission Duration of the TSUBAME = 23 December 2017 to 1 October 2019"]
-[7.6629438400268555, 3.231793165206909, "[FF] Objective of the OLS = Day and night cloud cover imagery"]
-[8.355080604553223, 1.2727713584899902, "[FF] Pulse Amplitude of the RainCube = Variable"]
-[3.997676372528076, 6.3274922370910645, "[TT] Antenna Configuration of the Satellite = Single downward pointing antenna"]
-[9.429391860961914, 6.136936187744141, "[FF] Motion of the Scan Mirror = Synchronized with the filter wheel"]
-[11.757271766662598, 3.3396403789520264, "[TT] Isp of the Ion engine = ~2000 s"]
-[3.2453980445861816, 5.707447528839111, "[TT] SAR Antenna Size of the CSG-SAR = ~7.5 m^2"]
-[8.486370086669922, 2.351670980453491, "[FF] Global Wind Field Measurement of the Atmospheric Dynamics Mission = True"]
-[7.321294784545898, 4.967106819152832, "[FF] Primary Structure Components of the S/C = Central cylinder, main platform, propulsion platform, four shear panels"]
-[13.861671447753906, 7.0442962646484375, "[FF] Failure Cause of the MRSE = Arcs of the high-voltage cathode supply at the TWTA connections in the low-pressure environment (vacuum) of the Shuttle orbit"]
-[3.080294370651245, 2.3295366764068604, "[TT] Bands Resolution of the Sentinel-2 = 60 m"]
-[3.868394374847412, 3.4538919925689697, "[TT] Upgrade Start Date of the Galileo = February 2019"]
-[6.9446635246276855, 5.809957981109619, "[TT] Clocks of the GIOVE-B = Better than 1 ns per day"]
-[6.630295276641846, 4.1064887046813965, "[FF] Ground Segment of the SPOT-6 & SPOT-7 = CGS (control ground segment) and EGS (exploitation ground segment)"]
-[8.309757232666016, 1.9962186813354492, "[FF] Measurement Results of the SMMR = Liquid water in clouds and rain was mapped globally"]
-[3.454197406768799, -0.8646377921104431, "[TT] Orbit Type of the Satellite = Sun-synchronous orbit"]
-[9.737933158874512, 1.40455961227417, "[TT] Swath Width of the Pl\u00e9iades = Larger"]
-[7.827425479888916, 9.039043426513672, "[TT] Center Wavelength of the MWIR = 3.8 \u00b5m"]
-[8.607253074645996, 0.32865986227989197, "[TT] Comet Discovery Count of the SOHO = 2875"]
-[5.502964973449707, 1.7051910161972046, "[FF] Wavelengths of the ALOS-2 = Unknown"]
-[6.007879734039307, -0.552014172077179, "[TT] Programming Horizon of the MUS = 72 hours"]
-[4.654520034790039, 0.6808760762214661, "[FF] Development Start Date of the SARah project = 19 September 2013"]
-[13.87126636505127, 7.256046295166016, "[TT] Rise and Fall Times of the Pulsed Diode Driver = \u00b5s class"]
-[10.413944244384766, 5.724206447601318, "[TT] Temperature of the Verkhoyansk = 38\u00b0C"]
-[9.568868637084961, 8.44749641418457, "[TT] Sampling Interval for VIS, SWIR,MIR & TIR-1 / -2 of the Telescope = 1.75 samples / IFOV"]
-[7.40772819519043, 2.5005197525024414, "[TT] Daily Coverage of the GeoCarb = CONUS > once per day"]
-[12.156270027160645, 4.577788829803467, "[TT] Bus Dimensions of the Helios-2 satellites = 3.4 m x 3.1 m x 6 m"]
-[5.151641845703125, 8.42160415649414, "[TT] Bandwidth (MHz) of the PMI = 2000"]
-[5.467558860778809, 1.0223082304000854, "[TT] Launch Date of the EarthDaily Constellation = January 2024"]
-[14.60286808013916, 6.643372535705566, "[TT] Battery Type of the EPS = Rechargeable lithium ion 18650"]
-[3.159456253051758, 4.363519191741943, "[FF] Mission Features of the TerraSAR-X NG = Full polarimetry and improved near-real-time capabilities"]
-[5.891504287719727, -0.43565085530281067, "[TT] Time to Reach Intelsat 10-02 of the MEV-2 = Nearly eight months"]
-[5.156275749206543, 8.23161506652832, "[TT] Frequency of the L-band radiometer = 1.4 GHz"]
-[14.08384895324707, 3.0748772621154785, "[TT] Mass of the ADCS = 0.78 kg"]
-[6.373623371124268, 7.948905944824219, "[TT] Receiver Channels of the DIAL Instrument = 2"]
-[9.483047485351562, -1.3979803323745728, "[TT] Eccentricity of the LARES-2 = 0-0.0025"]
-[5.370602607727051, 2.8421084880828857, "[TT] Coverage of the Konnect = Sub-Saharan Africa"]
-[7.426636695861816, 2.8939473628997803, "[TT] Purpose of the MethaneSAT = Measure methane emissions from human activities"]
-[5.192892074584961, 4.310612201690674, "[FF] Structure of the RADARSAT-2 = Bus module, payload module, ESS"]
-[5.426056861877441, 2.424041748046875, "[TT] Launch Lock of the OSIRISv3 = Not required"]
-[7.358996868133545, 0.23785074055194855, "[TT] Fly-over Date of the OSIRIS-REx = April 7"]
-[9.093445777893066, 5.8458380699157715, "[TT] Calibration Mode Position Angle of the CSM = 55\u00ba"]
-[7.1338677406311035, 7.790055751800537, "[FF] Heat Transfer of the Cube Corner Reflectors (CCRs) = Mainly governed by radiation"]
-[14.317975044250488, 3.0050783157348633, "[TT] Mass of the HORYU-4 = 10 kg"]
-[12.95860767364502, 6.721824645996094, "[TT] Predicted Total \u0394V of the PPT Module = 2.7 m/s"]
-[10.138896942138672, 5.7904253005981445, "[TT] Brightness Temperature Stability of the MWR = 1 K"]
-[7.210801601409912, 2.5746054649353027, "[FF] Key Applications of the GHOSt = Capturing critical environmental and situational awareness information for defence, detecting minute real-time changes in physical infrastructure, monitoring energy infrastructure and regulatory compliance, detecting environmental erosion and degradation, and monitoring crop yield and agriculture"]
-[6.169320106506348, 8.600749969482422, "[TT] Polarization of the Antenna = Linear (V, H)"]
-[9.713552474975586, -0.8664029836654663, "[TT] Orbit Altitude of the PARASOL = 705 km"]
-[10.949734687805176, 0.6552771925926208, "[FF] Position of the Kepler-80g = Sixth planet in the Kepler-80 system"]
-[3.3046584129333496, 0.0801253616809845, "[TT] Phase Angle of the JL-1-GF03B = 60\u00ba"]
-[8.237458229064941, 4.058800220489502, "[FF] Function of the DLP = Surface cleaning"]
-[9.718775749206543, 7.183678150177002, "[TT] 3 m (rg) x 1 m (az) of the Ground resolution = -"]
-[5.146336078643799, 7.684704303741455, "[TT] PRF of the NSCAT = 62 Hz"]
-[5.741146087646484, 2.687297821044922, "[FF] International Contributors of the \u00d8rsted = NASA, CNES, DLR and ESA"]
-[6.186302185058594, 2.557382822036743, "[TT] Development and Construction of the Orion Service Module = November 2014"]
-[11.500725746154785, 5.202701091766357, "[TT] Total Instrumented Surface Area of the STD = 6.45 m2"]
-[11.765589714050293, 6.605838298797607, "[TT] Electron Energy Resolution of the ECAL = 3% at 100 GeV"]
-[5.110966205596924, 3.433120012283325, "[TT] Manufacturer of the GFO-RA = Raytheon's E-Systems Division"]
-[8.01262092590332, 2.1730329990386963, "[FF] Objectives of the AMSR = Measurement of sea surface temperature (SST), soil water content (moisture), sea wind speed, water equivalent of snow cover, precipitation intensity, sea ice distribution, precipitable water"]
-[13.402039527893066, 6.9126482009887695, "[TT] Power Capacity of the Platform = 3 kW"]
-[7.308338165283203, 1.2935372591018677, "[FF] Function of the Ma_MISS = Illuminate the hole's cylindrical wall, capture and analyze reflected light, transfer data to Rover computer"]
-[8.464037895202637, 8.945151329040527, "[TT] Grating Figure of the Long Wavelength Band = Ellipse of rotation"]
-[8.033479690551758, 8.822142601013184, "[TT] Lamps of the SOLSPEC = One cathode"]
-[5.41375207901001, 5.954370021820068, "[TT] PROM of the STRV-1d DHS = 32 k PROM"]
-[12.866920471191406, 7.638425827026367, "[TT] Power of the LCT instrument = 160 W"]
-[6.017047882080078, 0.8956164717674255, "[FF] Image Capture Date of the TopSat = March 2, 2007"]
-[7.58300256729126, 3.8012681007385254, "[FF] Algorithm of the GPS Receiver = Estimate of ionospheric delay and its change"]
-[5.10211706161499, 6.842199802398682, "[TT] Data Rate of the LEO-LEO Inter-satellite Link = 5.625 Gbit/s"]
-[8.853363037109375, 9.518796920776367, "[FF] Band of the FTS-2 = 2.0 \u00b5m"]
-[3.876312017440796, 4.433929443359375, "[FF] TT&C Stations Completion of the RADARSAT-2 = Two decades after completion of the TT&C (Telemetry, Tracking, and Command) stations originally installed for RADARSAT-1"]
-[5.504310131072998, 1.5109648704528809, "[FF] Commissioning Approach of the CLS = Incremental"]
-[7.763894557952881, 2.4407424926757812, "[FF] Complementary Missions of the Aqua and Aura = PARASOL (POLDER) complements CALIPSO (Lidar) and NASA's Aqua and Aura (MODIS, CERES) missions"]
-[5.7024712562561035, 0.3354923725128174, "[TT] Elevation Measurement Date of the ATLAS = October 31, 2018"]
-[7.702343463897705, 0.5407318472862244, "[FF] Mission of the Lunar IceCube = Prospect, locate, and estimate size and composition of water ice deposits on the Moon"]
-[7.06324577331543, 1.4206047058105469, "[FF] Publication Date of the Star-circling bubble of gas = 11 June 2018"]
-[9.079744338989258, 7.166631698608398, "[TT] Supermode Resolution of the Image = About 3 m"]
-[8.89405632019043, 9.553397178649902, "[FF] Band 3 Resolution of the TANSO-FTS-2 = 0.2 cm -1"]
-[4.786214828491211, -1.826859474182129, "[TT] Landing Trajectory Reconstruction of the Chang'e-4 = Completed"]
-[6.3356170654296875, 4.35305118560791, "[FF] Function of the PPS = Create higher-level science data products, deliver science data products to the user community, provide interface to the instrument science teams, and deliver instrument commands and instrument team command requests to the MOC"]
-[11.45840835571289, 5.409811019897461, "[TT] Area of the XGRE = 900 cm2"]
-[3.927464246749878, 6.33095121383667, "[TT] Antennas of the Antenna System = Four broadband feed-horn antennas"]
-[6.719559192657471, 3.855560779571533, "[FF] Equipment Status of the MPO PFM Spacecraft = All platform equipment and payload instruments powered on"]
-[9.703009605407715, 8.447290420532227, "[TT] FOV of the Instrument = 11\u00ba"]
-[7.653846740722656, 4.758970260620117, "[FF] Component of the Main Crates/Radiators = Unknown"]
-[11.548211097717285, 6.465366363525391, "[TT] Energy Range of the NuSTAR = > 25 keV"]
-[4.623961925506592, 6.718613624572754, "[FF] Protocol of the X-band transmission = DVB-S2"]
-[4.171026229858398, 7.197813987731934, "[TT] DT Band of the DTS = X-band"]
-[5.552029132843018, 3.9446773529052734, "[TT] Number of Transponders of the Inmarsat S \u2013 Europasat / Hellas-Sat 3 = 44 Ku and 1 Ka"]
-[6.8089280128479, 7.465808391571045, "[TT] 3db Beamwidth of the MWR = 1.64\u00ba"]
-[10.307783126831055, 4.070410251617432, "[TT] Mounting of the GRNS = 6-foot (2-meter) boom"]
-[11.371743202209473, 5.875326633453369, "[TT] Material of the Izmit Bay Bridge = Steel and concrete"]
-[6.185724258422852, -0.24496181309223175, "[TT] Map Production Time of the SMOS = Within 24 hours"]
-[6.339015960693359, 6.4260358810424805, "[TT] Value of the Group Delay Uncertainty = Few nanoseconds (1-3 ns)"]
-[5.368035316467285, 1.115936279296875, "[FF] Presentation Date of the High Power Distribution, Control and Monitoring ASIC = Sept. 5-8, 2010"]
-[5.951772212982178, 4.949018955230713, "[FF] Designed for of the GPS Receiver = Cubesat Operations"]
-[8.362385749816895, 6.149555206298828, "[TT] Measurement Error of the Overall absolute measurement error at 333 K in bands 4-6 = 0.5 K"]
-[12.029881477355957, 6.474343776702881, "[TT] Observation of the AMS = Fraction decreases with increasing energy from 0.5 to 10 GeV"]
-[10.169928550720215, 8.14541244506836, "[TT] Telescope Aperture of the Pan Camera = 0.5 m"]
-[6.246536731719971, 0.25581151247024536, "[FF] Test Duration of the Modern ICs = Unrealistic 7.6 years"]
-[7.894199371337891, 2.3397510051727295, "[FF] Dissolved Inorganic Carbon of the Marine Chemistry = Unknown"]
-[9.221529960632324, -0.4225051701068878, "[TT] Apogee of the GEOS-1 = 2275 km"]
-[5.094757080078125, 3.266716480255127, "[TT] Prime Contractor of the Swarm Spacecraft = EADS Astrium GmbH, Friedrichshafen, Germany"]
-[9.66331958770752, 7.135136127471924, "[TT] Pixel Spacing of the OLS = 0.5 km"]
-[9.844704627990723, 8.698569297790527, "[TT] Value of the IFOV = 24 \u00b5rad"]
-[12.204998016357422, 3.3510262966156006, "[TT] Propellant Pressure of the IES = Approximately 7MPa"]
-[4.803472995758057, 3.7219810485839844, "[TT] Manufacturer of the Radio Antenna = Tekever in Portugal"]
-[7.9890007972717285, 7.340593338012695, "[TT] Detectors of the FTS Interferometer = InSb, HgCdTe"]
-[7.646655082702637, 0.5367415547370911, "[FF] Mission of the Lunar IceCube = Prospecting for Lunar Water Ice"]
-[6.5153093338012695, 7.03502082824707, "[TT] Transmit Power (average) of the SILEX Optical Terminal = 0.06 W"]
-[4.856218338012695, -1.570644497871399, "[TT] Rover Operation Duration of the Tianwen-1 = About 90 Martian days"]
-[8.585417747497559, 3.977445363998413, "[FF] Function of the Collimator = Collimate the sensor FOV and reject ambient ions and electrons"]
-[14.685275077819824, 6.667943954467773, "[TT] Batteries of the User Terminal = 6 x UM-3"]
-[9.350747108459473, 5.0796074867248535, "[TT] Control Mode of the CMG = Three-axis"]
-[7.0518012046813965, 4.047429084777832, "[FF] Objective of the Rigid Maneuver = Demonstrate operations foreseen from future formation flying missions"]
-[4.649615287780762, 1.5796716213226318, "[FF] Launch Date of the GOSAT-GW = Early 2024"]
-[6.299916744232178, 3.3036293983459473, "[FF] Mission Design of the WSF-M = Next-generation environmental satellite system for the Department of Defense (DoD)"]
-[6.936104774475098, 8.91273307800293, "[TT] Measurement Wavelengths of the POLDER = 443 nm, 670 nm, 865 nm"]
-[13.492895126342773, 2.8300912380218506, "[TT] Mass of the Cospas-Sarsat search and rescue package = 8 kg"]
-[6.933478355407715, 2.512890577316284, "[FF] Role of the Martin Popek = His photographs are proving a very valuable to the team\u2019s research"]
-[13.823890686035156, 2.9083948135375977, "[TT] Mass of the HIT-Sat = 3 kg"]
-[5.204772472381592, 1.3165340423583984, "[FF] Event of the SMOS = SMOS MIRAS - return to nominal data quality"]
-[6.379344463348389, 2.359020471572876, "[FF] Importance of the RRM3 = Enable long duration journeys to destinations, such as the Moon and Mars"]
-[11.183932304382324, 0.6206644177436829, "[FF] Mission Purpose of the CHEOPS = Characterize exoplanets orbiting nearby stars"]
-[4.26422643661499, 0.7340556979179382, "[TT] Launch Year of the EDRS-C = 2018"]
-[10.30104923248291, 3.084014415740967, "[TT] CubeSat Mounting of the Cygnus spacecraft = External"]
-[9.527006149291992, 4.128368377685547, "[TT] Field Change Detection Capability of the SQUID = 5 x 10-14 Gauss"]
-[6.407389163970947, 5.485584259033203, "[FF] Failure of the STM32 microcontroller = Loss of communication"]
-[8.844409942626953, 3.0986459255218506, "[FF] Purpose of the ICON = Explore the boundary between Earth and space \u2013 the ionosphere"]
-[6.804182529449463, 5.9339070320129395, "[TT] Quantity of the No of types of products = 42"]
-[10.472332000732422, 5.649254322052002, "[TT] UK's Record Maximum Temperature of the Meteosat-10 = 38.5\u00b0C"]
-[9.506528854370117, 4.809193134307861, "[TT] Attitude Control of the GFO = Three-axis stabilized"]
-[7.125418663024902, 2.8952465057373047, "[FF] Photo of the TOMS instrument = Image credit: NASA"]
-[4.722684383392334, 4.963524341583252, "[TT] AIS of the LAPAN-A2 = Automatic Identification System"]
-[4.699597358703613, 1.6074885129928589, "[TT] Number of Folders of the GCOM-C/SGLI = 156"]
-[7.6207990646362305, 5.114047527313232, "[FF] Observation Results of the ISUAL = Enormous"]
-[9.967876434326172, 2.008220672607422, "[FF] URL of the Chandra X-Ray Observatory = https://www.nasa.gov/sites/default/files/108075main_REVchandra.pdf"]
-[7.752410411834717, 4.633490085601807, "[FF] Sub-Experiments of the CCA = CREDANCE (Cosmic Radiation Environment Dosimetry and Charging Experiment), DIME-1 (Dosimetry Inter-comparison and Miniaturization Experiment Board #1), DIME-2 (Dosimetry Inter-comparison and Miniaturization Experiment Board #2), ELDRS (Linear Enhanced Low Dose Rate Sensitivity), COTS-2 (Commercial Off the Shelf Technology)"]
-[11.141096115112305, 5.112193584442139, "[TT] Density of the LARES-2 = About 9,000 kg/m3"]
-[10.562590599060059, 2.459251642227173, "[TT] Mirror Module Configuration of the X-ray telescope = Compact hexagonal with 1300 mm diameter"]
-[9.348302841186523, 1.516664981842041, "[FF] Access of the Airbus Constellation = Pl\u00e9iades, SPOT, TerraSAR-X, TanDEM-X radar and DMC Constellation"]
-[6.749335765838623, -1.8642655611038208, "[FF] Inherited Features of the Jason-3 = Orbit, instruments and measurement accuracy"]
-[6.299690246582031, 6.183573246002197, "[TT] Quantity of the 12-Port Ethernet switches = 2 units"]
-[7.7305097579956055, 9.58360481262207, "[TT] Center Wavelength of the B7 = 775 nm"]
-[7.120703220367432, 1.3385168313980103, "[TT] Data Source of the Spitzer Space Telescope = Exoplanet discovery"]
-[9.549538612365723, 0.9660756587982178, "[TT] Satellite Speed of the AIS System = ~7 km/s"]
-[10.084409713745117, 2.9507029056549072, "[FF] Endurance of the CubeSat Dispensers = Up to several months in orbit"]
-[12.117600440979004, 1.9556052684783936, "[TT] LTDN of the CartoSat-2D = Local Time on Descending Node"]
-[12.114888191223145, 3.2371296882629395, "[TT] Propellant of the Cold Gas System = Nitrogen"]
-[6.998316287994385, 4.003817081451416, "[FF] Science Objectives of the ASPIICS = Address the questions listed"]
-[6.271946907043457, 8.622027397155762, "[TT] Polarization of the Spotlight = Single or dual"]
-[5.922558784484863, 0.8342961668968201, "[FF] Ticket Date of the Exoplanet mission = April 6, 2017"]
-[8.515917778015137, 1.5620808601379395, "[TT] Instrument Type of the Aquarius L-Band Scatterometer = Scatterometers"]
-[3.6691672801971436, 2.6043100357055664, "[FF] Signal Strength of the Iridium NEXT = Stronger"]
-[10.913177490234375, 10.099807739257812, "[TT] Lifespan of the Alpha Magnetic Spectrometer (AMS) = Surpassed three years"]
-[3.33872127532959, 5.017020225524902, "[FF] Polarimetry Modes of the SAR (Synthetic Aperture Radar) Instrument = Amplitude and phase information"]
-[6.7313337326049805, 2.165942430496216, "[FF] URL of the STARE = http://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=2991&context=smallsat"]
-[8.644370079040527, 3.2480342388153076, "[FF] Focus of the RAIDS = Remote sensing of the ionosphere"]
-[11.274994850158691, 5.89694356918335, "[TT] Material of the Chimney = CFRP (Carbon Fiber Reinforced Polymer)"]
-[11.92342758178711, -0.1783095896244049, "[FF] URL of the TESS = https://doi.org/10.3847/2041-8213/ab564d"]
-[13.879903793334961, 2.659788131713867, "[TT] Launch Mass of the IRNSS-1D = 1425.4 kg"]
-[6.052114486694336, 1.962978482246399, "[FF] Manufacturer of the SCD-2 = INPE/Brazil"]
-[13.408782005310059, 7.819831371307373, "[TT] RF Output Power of the Channel = 1 W per polarization"]
-[10.846004486083984, -0.35389530658721924, "[TT] Nominal Lifetime of the TanDEM-X = 5.5 years"]
-[5.073241710662842, 2.8010873794555664, "[TT] Designation of the MTSAT = CNS/ATM system"]
-[8.237359046936035, 4.33502197265625, "[FF] Function of the BCA = Minimizes stray-light and includes a protective cover and release mechanism"]
-[11.758382797241211, 0.11224101483821869, "[TT] Mass of the TESS = Ranges from two to 12 times Earth\u2019s"]
-[14.212423324584961, 3.175558567047119, "[TT] Mass of the NEOSSat = ~74 kg"]
-[4.514888763427734, 1.655564546585083, "[TT] Launch Date of the TechnoSat = 14 July 2017"]
-[3.744288921356201, 6.506857395172119, "[FF] Antenna Size of the MWI = Moderate"]
-[4.796091079711914, 7.267790794372559, "[TT] Coded Data Rate of the X-band transmitter = 441.625 Mbit/s"]
-[4.272878170013428, 7.240732669830322, "[TT] Transmission Frequency of the RF Communications = S-band"]
-[5.981799602508545, 5.991626262664795, "[TT] Data/Pilot of the E5b-I = Data"]
-[7.107946395874023, 7.770188808441162, "[TT] Dihedral Angle Offset (DAO) of the Cube Corner Reflectors = 1.5 inch"]
-[11.272371292114258, 5.943326950073242, "[TT] Material of the S/C structure = Graphite fiber"]
-[6.070553302764893, -0.335220605134964, "[TT] Operation Duration of the EDSN = 60 days"]
-[4.176604270935059, 0.6164937019348145, "[FF] Article Date of the INTEGRAL = 26 Jan. 2016"]
-[7.105312824249268, 6.961050510406494, "[TT] Precision of the Laser System = Subatomic scale"]
-[8.037381172180176, 6.527103900909424, "[FF] Unknown of the Multispectral Camera = Unknown"]
-[9.27433967590332, 6.172643184661865, "[TT] Resolution of the Electrostatic Analyzer = 5.2%"]
-[7.828718662261963, 8.501648902893066, "[TT] Spectral Range of the Instrument = 8-12 \u00b5m"]
-[5.71820592880249, 7.0591864585876465, "[TT] Data Output of the REM = 20 kByte/orbit"]
-[6.378635406494141, 4.185732841491699, "[FF] Telecom, Landing Site Tilt Accommodation, Flight Hardware Thermal Safety of the Mission Requirements = Identified and Analyzed"]
-[5.315383434295654, 7.614026069641113, "[TT] Minimum Trigger Level of the Receiver = -96 dBm"]
-[7.833335876464844, 3.0611629486083984, "[FF] Purpose of the Compact Thermal Imager = Observe Earth to detect smoke and fires, as well as measure crop transevaporation"]
-[8.1001558303833, 0.6766049861907959, "[FF] Response Time to Pumping of the Aquifers = Takes a while to compress in response to the weight of land mass pressing down from above"]
-[5.64361572265625, 0.5468813180923462, "[FF] Data Availability of the EPIC = June 2015 through the current day"]
-[6.9106597900390625, -0.4075448215007782, "[TT] Orbit Frequency of the Space Station = About 16 times per day"]
-[13.400171279907227, 2.921266794204712, "[TT] Mass of the StudSat = 1 kg"]
-[5.293087005615234, 0.823485791683197, "[TT] Commercial Service Entry Date of the Data Satellite = 22 July 2022"]
-[4.615474700927734, 7.26911735534668, "[TT] Ka-band of the RF Communications = 350 Mbit/s"]
-[13.252673149108887, 7.296693325042725, "[TT] Power Range of the BIT-3 system = 56-80 W"]
-[7.875913619995117, -0.4309053421020508, "[FF] Freeze-Up Start Date of the Arctic Sea Ice = 9 December 2020"]
-[6.973146438598633, 6.13923454284668, "[TT] Quantity of the Instrument Package = 3 sets of 4"]
-[8.637361526489258, 1.031332015991211, "[TT] Earth Coverage of the SAC-D/Aquarius = Every 7 days"]
-[13.924785614013672, 2.7342398166656494, "[TT] Launch Mass of the INSAT-3D = ~ 6650 kg"]
-[5.392518520355225, 0.9568029642105103, "[FF] Contract Date with Raytheon of the Instrument = January 2018"]
-[9.668221473693848, 8.341687202453613, "[TT] FOV (Field of View) of the XRD = 30 % sky"]
-[7.268734455108643, 8.17496109008789, "[TT] Sensitivity of the Channel 1 = 0.5 K/pixel"]
-[8.663248062133789, 7.078629493713379, "[FF] Box Size of the Image Quality = 30 \u00b5m square"]
-[2.9116692543029785, 4.300105571746826, "[TT] Flood Proxy Map Area of the ALOS-2 PALSAR-2 = 350 km2"]
-[3.7143242359161377, 5.122361660003662, "[TT] Imaging Frequency Band of the ALOS-2 = L"]
-[9.572569847106934, -0.2562732696533203, "[FF] Landing Speed of the EFT-1 = Higher than a low altitude orbital mission"]
-[4.319028377532959, 7.078853607177734, "[TT] Uplink Frequency of the Ground Station = S-band"]
-[4.24397087097168, 2.613471746444702, "[TT] Launch Site of the GeneSat-1 = NASA's Wallops Flight Facility, Wallops Island, VA, USA"]
-[5.952505588531494, 7.145925998687744, "[TT] Data Rate of the Instrument = 1.27 Mbit/s"]
-[4.991283893585205, 3.4787204265594482, "[TT] Manufacturer of the spaceCam c4000 = Theta System Elektronik GmbH"]
-[10.464478492736816, 5.88021183013916, "[TT] Internal Average Temperature of the SVM = 15\u00b0C"]
-[11.913037300109863, 5.0632429122924805, "[TT] Size of the POLDER-2 = 800 mm x 500 mm x 250 mm"]
-[5.769293308258057, 5.3336663246154785, "[TT] PID 238 Implementation of the GOES-R Instruments = FPGA and software on the embedded microcontroller"]
-[14.237102508544922, 3.0248255729675293, "[TT] Mass of the UNISat-6 = 26 kg"]
-[3.1718602180480957, 1.7111477851867676, "[TT] SAR Interferometry Image Pair Time Interval of the Sentinel-1A and Sentinel-1B = 6 days"]
-[3.977278470993042, 6.412650108337402, "[TT] Antenna Type of the ADS = VHF/UHF"]
-[8.834452629089355, -0.5739919543266296, "[TT] Orbit Period of the P35 series = 98.1 min"]
-[8.650421142578125, 0.6301894783973694, "[FF] Magnitude of the Kaik\u014dura earthquake = 7.8"]
-[9.096231460571289, 3.2494072914123535, "[FF] Lithospheric Magnetic Field Resolution of the Swarm = Improved resolution"]
-[8.014747619628906, 2.5541799068450928, "[TT] Measurement Domain of the DMC-3 = Land"]
-[10.937504768371582, 7.640923500061035, "[FF] Swath Width of the Wide Fine Quad-Pol and Wide Standard Quad-Pol modes = Wider than the original modes"]
-[3.0974783897399902, 2.2688395977020264, "[TT] Spatial Resolution of the Sentinel-2 = High"]
-[4.882456302642822, 2.9974963665008545, "[FF] Manufacturer of the ART-XC teleccope = ART-XC consortium"]
-[7.250036716461182, 7.3865275382995605, "[FF] Transmitted Wavefront Error of the Photon Sieve = \u03bb/10"]
-[14.085877418518066, 4.018525123596191, "[TT] Mass of the Instrument = 11.5 kg"]
-[8.588966369628906, 8.05502700805664, "[TT] Number of Pixels of the Band 2 = 1600"]
-[11.900334358215332, 4.63569974899292, "[TT] Size of the TurkSat-3USat = 10 cm x 10 cm x 30 cm"]
-[13.367273330688477, 7.751623153686523, "[TT] Transmission Power of the RF radio = ~1W"]
-[4.569770336151123, 7.896576881408691, "[TT] Downlink Center Frequency of the SAS&R = 4507 MHz"]
-[4.515737533569336, 3.8302230834960938, "[TT] Number of Satellites of the Galileo = 2"]
-[10.143146514892578, 6.948566913604736, "[TT] Ground Track of the MOMS-2P = 2000 km"]
-[4.407349109649658, 4.180006980895996, "[TT] Mission Type of the COSPAS-SARSAT = EO"]
-[9.213210105895996, 5.476578235626221, "[TT] Type of the BSA = 2-axis small range pointing mechanism"]
-[8.21102523803711, 1.3322596549987793, "[FF] Soil Moisture Data of the Aquarius = Coarser than SMOS mission"]
-[3.936124801635742, 9.717805862426758, "[TT] Frequency (GHz) of the ICI-11 = 664\u00b14.2"]
-[10.211316108703613, 7.538263320922852, "[TT] Design of the Telescope = Cassegrain design"]
-[10.1054105758667, 0.4151289165019989, "[FF] Components of the Satellite Breakup Model = Fragment size, A/M (Area-to-Mass ratio), and relative velocity (\u0394V) distributions"]
-[9.430534362792969, 6.205902099609375, "[TT] Viewing Angle of the MWHS-II = \u00b153.35\u00ba"]
-[6.770737171173096, -0.4930260479450226, "[FF] TLE Refresh Frequency of the Prometheus Block 1 = Regularly on orbit"]
-[5.87001895904541, -0.3178543150424957, "[TT] Operational Life of the MWIR = 12 months"]
-[7.729866981506348, 6.902726173400879, "[TT] Imaging Rate of the Instrument = About 60 0.1 second exposures per minute with the NIR camera, and 1/2 second exposure per minute with the VIS camera"]
-[5.793886184692383, 2.1786112785339355, "[FF] URL of the FalconSat-7 = http://www.usafa.edu/df/dfe/dfer/centers/lorc/docs/FalconSAT07.pdf"]
-[9.353562355041504, 6.560251235961914, "[TT] Azimuth Imaging Length of the P Mode = 10 km"]
-[7.720165729522705, -0.6664414405822754, "[TT] Purpose of the Operation IceBridge = Map the snow and ice of Antarctica"]
-[4.552978515625, 6.033718109130859, "[TT] Frequency of the Dual-frequency beacon = 162 MHz and 324 MHz"]
-[7.990564346313477, 7.9893951416015625, "[FF] Spectral Bands of the Satellite = Panchromatic band, 4 MS (Multispectral) bands Pan B, G, R and NIR"]
-[11.712554931640625, 4.496474266052246, "[TT] Length of the Rocket = 9 feet (2.8 meters)"]
-[7.1161980628967285, 7.206805229187012, "[TT] Pulse Width of the LOM = <1.5 ns"]
-[10.497458457946777, 3.354464054107666, "[TT] Power Generation of the ALBus 3U CubeSat = 5 - 20 W"]
-[8.870038986206055, 9.430533409118652, "[TT] Calibration of the Harris TANSO-FTS-2 = Onboard"]
-[8.20786190032959, 1.3706825971603394, "[FF] Rainfall Amount of the IMERG = Up to 10 cm (4 inches)"]
-[9.119606018066406, 2.8091514110565186, "[FF] Authors of the Submerged Sources of Transient Acoustic Emission from Solar Flares = Charles Lindsey, J. C. Buitrago-Casas, Juan Carlos Mart\u00ednez Oliveros, Douglas Braun, Angel D. Mart\u00ednez, Valeria Quintero Ortega, Benjam\u00edn Calvo-Mozo, and Alina-Catalina Donea"]
-[8.335549354553223, 3.175107955932617, "[TT] Manufacturer of the Ozone Mapping and Profiler Suite-Nadir (OMPS-N) = Ball Aerospace"]
-[5.9339494705200195, 2.634974956512451, "[FF] Mission Goals of the ARMADILLO = Train students in best systems engineering practices by executing a complete spacecraft life cycle from concept design to mission operations"]
-[10.138309478759766, -1.4044533967971802, "[TT] Orbit Inclination of the DubaiSat-1 = 98.13\u00ba"]
-[5.903424263000488, 0.37518590688705444, "[TT] Data Collection Period of the Nimbus-7 (SMMR) = 40 years"]
-[5.470239639282227, 1.6773567199707031, "[FF] Orbit Control and Determination of the ALOS-2 = Unknown"]
-[12.22962760925293, 6.941185474395752, "[TT] Charge Range for Isotopes of the LEICA = 2 - 16"]
-[9.053754806518555, 7.654421329498291, "[TT] Pixel Size of the MIR, TIR-1 and TIR-2 = 4 km per side"]
-[5.113344192504883, 2.8647351264953613, "[TT] University of the Delphini-1 = Aarhus University in Denmark"]
-[6.736606597900391, 3.2426068782806396, "[TT] Average Daily Observations of the SBSS = 15,000"]
-[9.72567081451416, -0.5181424021720886, "[TT] Orbit Altitude of the AlSat-2 = 670 km"]
-[14.055495262145996, 3.3376307487487793, "[TT] Mass of the Mass Memory System = 14 kg"]
-[6.581411361694336, 0.9363969564437866, "[FF] Agility Performance of the CSG System = Very high"]
-[4.386409282684326, 7.773409366607666, "[FF] Downlink Frequency of the ANDE-2 = 2 Meters"]
-[5.276073932647705, 3.4288010597229004, "[FF] Manufacturer of the GFO = Unknown"]
-[9.763983726501465, 7.157157897949219, "[TT] Along-track resolution of the L-band = 35 km"]
-[16.496440887451172, 3.613304853439331, "[TT] OneWeb Business of the Hughes = More than $300 million"]
-[6.396024703979492, 1.509948968887329, "[FF] URL of the BepiColombo = http://www.stp.isas.jaxa.jp/mercury/index-e.html"]
-[5.477560043334961, -0.06198718026280403, "[FF] Presentation Date of the RapidEye = Oct. 12-16, 2009"]
-[6.79143762588501, 4.710849761962891, "[TT] Location of the PXA 270 = Payload"]
-[10.902538299560547, 7.477480888366699, "[TT] Swath of the HSC = 700 km"]
-[13.197349548339844, 5.391857624053955, "[FF] Features of the Prometheus Satellite = Four deployable solar arrays and a deployable helix antenna"]
-[8.76302719116211, 5.769702434539795, "[TT] Interbeam Radiometric Stability of the Satellite = 0.33 - 0.41 dB pp"]
-[7.751641750335693, 0.5077557563781738, "[TT] Coverage of the Lunar IceCube = Up to 10% of the lunar surface across all latitudes"]
-[7.591716289520264, 1.4367563724517822, "[FF] Imaging of the Apollo 14 = Yes"]
-[9.796767234802246, -0.5553242564201355, "[TT] Orbit Altitude of the BlackSky-1 = About 450 km"]
-[9.48776626586914, 6.316765785217285, "[TT] Scan Angle of the Rotating Telescope Scanner = \u00b153\u00b0"]
-[7.806056976318359, 8.546602249145508, "[TT] Spectral Range of the Instrument = 400-900 nm"]
-[4.704892158508301, 5.698344707489014, "[TT] ELF Signal Energy of the QuakeSat = Between 10 Hz and 150 Hz"]
-[10.05929946899414, 2.3334431648254395, "[TT] Ability to Capture Nanoflares of the NuSTAR = Potential"]
-[5.965897560119629, 5.16143274307251, "[FF] Realtime Data Exchange of the ISL = Required"]
-[5.335488319396973, 7.948758125305176, "[FF] Design Features of the Receivers = 60 GHz communication receiver, Wideband cueing receiver, >2 GHz chirp bandwidth, Hybrid 9 GHz chan. receiver with MMIC mixer, Low-noise HTS/GaAs down-converter: 7 to 1 GHz"]
-[11.894721031188965, 5.010946750640869, "[TT] Size of the CCE = 235 mm x 205 mm x 85 mm (width x depth x height)"]
-[14.08374309539795, 3.0713586807250977, "[TT] Mass of the Athena = 138 kg"]
-[9.274236679077148, 5.080623149871826, "[TT] Target of the External Calibration = Sky in an inertial attitude"]
-[8.101502418518066, 3.551591157913208, "[FF] Purpose of the Hydrogen Sensor = Monitor for the presence of excess hydrogen in generated oxygen"]
-[3.992692232131958, 6.292606353759766, "[FF] Configuration of the Microstrip Patch = Typical"]
-[6.185222148895264, 4.350219249725342, "[FF] Form of the Procedures = Predefined \u201ctasks\u201d"]
-[9.3396577835083, 4.971311092376709, "[TT] Attitude Knowledge of the AOCS = 0.02\u00ba"]
-[9.6826171875, -0.9936538934707642, "[TT] Orbit of the HORYU-2 = LEO"]
-[8.208806037902832, 8.378925323486328, "[TT] Working f/# of the TOU = 2.06 @ 700 nm"]
-[8.8201904296875, 7.593247890472412, "[TT] Detector Resolutions of the FLIR Boson camera = 640 x 512 or 320 x 256"]
-[5.122729778289795, 2.001680850982666, "[TT] Operational Status of the TSX = Operational"]
-[6.5611114501953125, 0.5841929316520691, "[FF] Daily-Revisit Orbit of the FormoSat-2 = Unknown"]
-[10.837862968444824, 1.402495265007019, "[TT] Mass of the M82 X-2 = About the mass of our sun"]
-[8.569123268127441, 7.517739772796631, "[TT] Detector Areas of the Imager = Two"]
-[13.808439254760742, 5.342705249786377, "[TT] Solar Array Type of the Power subsystem = Triple junction GaAs (Gallium Arsenide) cells"]
-[6.12930154800415, 3.057468891143799, "[TT] Ticker Symbol of the BlackSky Holdings, Inc. = BKSY"]
-[7.301837921142578, 2.9890239238739014, "[FF] Purpose of the Enxaneta = Monitor the flow of rivers and water reserves, monitor and protect wildlife, receive weather data, monitor soil movements, monitor livestock and crops"]
-[7.939187526702881, 3.2083470821380615, "[FF] Purpose of the Instrument = Provide unprecedented imaging of the Earth\u2019s upper atmosphere"]
-[9.873512268066406, 7.745147705078125, "[TT] Spatial Resolution & Stability of the Telescope = PSF stability better than 1%"]
-[4.7237749099731445, 0.5832639336585999, "[TT] Launch Date of the GOES-S = March 2018"]
-[3.596327066421509, 4.441052436828613, "[TT] On-Orbit Service Time of the SAR-Lupe Constellation = More than 20 years"]
-[8.29226303100586, 2.72126841545105, "[FF] Cloud Albedo Measurement of the AIM = Yes"]
-[14.3110990524292, 2.7493648529052734, "[TT] Launch Mass of the KOMPSAT-3 (Arirang-3) = ~ 1990 kg"]
-[7.34512996673584, 3.7160723209381104, "[TT] Daily Radio Occultation Profiles of the Spire = 5,000"]
-[10.99070930480957, 2.9004485607147217, "[TT] Structure Type of the Microsatellite = Hexagonal prism"]
-[14.61726188659668, 6.614963531494141, "[TT] Depth of Discharge of the Battery = Not exceed 20%"]
-[6.439826488494873, 7.609091758728027, "[TT] Data Quantization of the ResourceSat-2 = 10 bit"]
-[8.485550880432129, 6.782511234283447, "[TT] Optical System of the OCTS sensor = Catoptric"]
-[8.705740928649902, 5.924857139587402, "[TT] Axes of the Piezoelectric Positioning Stage = Two-axis"]
-[6.654531478881836, 0.23593632876873016, "[TT] Launch Year of the CryoSat-2 = 2010"]
-[9.699992179870605, 7.640239715576172, "[TT] Distance Between Optical and Electronics Modules of the MCP-MC = 1m"]
-[10.290340423583984, 5.7922282218933105, "[TT] Operating Temperature of the MIRI = 7K"]
-[4.783742427825928, 0.023489011451601982, "[TT] End of Life Date of the SARAL = 31 Dec 2023"]
-[4.175048351287842, 5.674941539764404, "[FF] URL of the Space-based ADS-B = http://www.icao.int/Meetings/anconf12/WorkingPapers/ANConfWP141.1.1.ENonly.pdf"]
-[5.159205436706543, 4.120390892028809, "[TT] Frequency Band of the MEOSAR satellite constellations = 406 MHz"]
-[7.265986442565918, 9.180854797363281, "[TT] Filter Wavelength of the ISUAL instrument = 630 nm"]
-[10.665332794189453, 0.7845179438591003, "[TT] Rotation Period of the Kepler 11145123 = Three times more slowly than the Sun"]
-[5.5800676345825195, 7.118746280670166, "[TT] Usage of the HRIT = High Rate Information Transmission"]
-[4.787512302398682, -1.8143337965011597, "[FF] Candidate Landing Region of the Chang\u2019e-4 = 45\u00b0S-46\u00b0S and 176.4\u00b0E-178.8\u00b0E"]
-[7.381654262542725, 3.4476375579833984, "[TT] Tracking Organization of the Debris = U.S. Air Force's 18th Space Control Squadron"]
-[5.225921154022217, 4.6847004890441895, "[TT] Design Phase Start of the Emergency Egress System = 2019"]
-[11.85582447052002, 6.694340705871582, "[TT] Electron Energy Range of the HIPS = 1-10 MeV"]
-[6.998937606811523, 2.112588882446289, "[FF] Image Source of the Landsat 8 = Images from Landsat 8"]
-[5.155269145965576, 3.214970827102661, "[TT] Manufacturer of the SeaWinds = NASA/JPL"]
-[10.292797088623047, 5.659937858581543, "[FF] Effect of High Beta Angle of the Component Temperatures = Higher"]
-[11.987608909606934, 4.536125659942627, "[TT] Width of the Spacecraft = Approximately 3.5 m"]
-[5.102046489715576, 0.6653459668159485, "[TT] Mission Name of the ExoMars 2020 = ExoMars 2022"]
-[13.361050605773926, 7.730319499969482, "[TT] RF Power of the Unit = 8 W"]
-[4.15271520614624, 7.343203544616699, "[TT] Band of the SARAL/AltiKa = Ka/Ku"]
-[4.397684097290039, 2.839357614517212, "[TT] Location of the Henri = Offshore near the Bahamas"]
-[3.3132925033569336, 5.555772304534912, "[FF] Peak Radiation Power of the L-band SAR antenna = 3,300 W with three panels for Spotlight mode and Ultra-Fine mode, or 5,100 W with full aperture for High sensitive mode, Fine mode and ScanSAR mode"]
-[7.243239402770996, 2.7837941646575928, "[TT] End Date of the Methane Leak = 26 September"]
-[12.801963806152344, 7.617175579071045, "[TT] Power of the Instrument power = \u2264 25 W"]
-[4.348020553588867, 3.073537826538086, "[FF] Location of the Ground Stations = New Norcia, Australia (DSA 1), Cebreros, Spain (DSA 2), Malarg\u00fce, Argentina (DSA 3), Kourou, Maspalomas and Perth"]
-[5.30839204788208, 1.331305742263794, "[FF] Conference Date of the Dellingr = Aug. 5-10, 2017"]
-[4.825101375579834, 7.974192142486572, "[TT] Carrier frequency (MHz) of the E5a-Q = 1176.45"]
-[9.818157196044922, 8.138989448547363, "[TT] Optics Focal Length of the Camera 1 = 2.5 mm"]
-[9.442197799682617, 0.6398221254348755, "[TT] Travel Distance of the Envisat = 2.25 billion km"]
-[3.9343669414520264, 4.90593957901001, "[TT] Signal Reception Frequency Bandwidth of the RISAT-1 DRS = 320 MHz"]
-[5.810225963592529, 4.917241096496582, "[TT] Data Acquisition of the Development Flight Instrumentation (DFI) = Functioned correctly throughout the mission"]
-[7.905180931091309, 6.66460657119751, "[FF] Issue of the Medium-Resolution Camera = Telemetry issues"]
-[4.288595676422119, 7.245246410369873, "[TT] Broadcast Bands of the First Batch of Satellites = \"Ku\" band"]
-[1.777416706085205, -2.0545201301574707, "[FF] Function of the MASCOT = Augment the science capabilities of the Hayabusa-2 mission"]
-[14.022549629211426, 7.143209457397461, "[TT] Regulators of the EPS = 3.3 and 5 V"]
-[5.96449613571167, 1.0806572437286377, "[FF] Readiness Date of the Hispasat-AG1 Redsat component = April 24, 2013"]
-[5.494192600250244, 1.4885236024856567, "[FF] Conference Location of the Trailblazer = St. Louis, Missouri, USA"]
-[6.185206413269043, 2.9891915321350098, "[FF] Imagery Access of the WorldView Legion = Direct task and download 30 cm-class satellite imagery to its ground station"]
-[4.910669803619385, 7.20817756652832, "[TT] Downlink Data Rate of the NEMO-AM = 2Mbit/s"]
-[9.268815994262695, -0.40360864996910095, "[TT] Performance of the Vega-C = 2.3 t in a reference 700 km polar orbit"]
-[5.673629283905029, 7.16117525100708, "[TT] Data Rate of the OGS = 40 Mbit/s"]
-[4.280538082122803, 6.83570671081543, "[FF] Common Functionality of the KazEOSat-2 = Antenna scheduling, user office and image processing facilities"]
-[4.376277923583984, 6.994342803955078, "[TT] RF Communications of the PARASOL = S-band"]
-[9.222819328308105, 1.0441073179244995, "[TT] Arrival Date at Jupiter of the Juno = July 4, 2016"]
-[5.0247955322265625, 7.016964435577393, "[TT] Byte/slot of the Service downlink = 134"]
-[4.732155799865723, -1.1904038190841675, "[TT] Number of Private Launch Companies of the China = More than 10"]
-[11.627605438232422, 0.25248298048973083, "[TT] Planet Size of the TESS = Smaller in size than Neptune, but larger than Earth"]
-[7.815913677215576, 1.5333905220031738, "[FF] Brochure URL of the Global Precipitation Measurement (GPM) = http://www.nasa.gov/sites/default/files/files/GPM_Mission_Brochure.pdf"]
-[10.16181468963623, 3.2937681674957275, "[FF] Payload of the VBN (Vision Based Navigation) CubeSat = VBN payload"]
-[5.436456203460693, 5.173182010650635, "[TT] Operating System of the PhoneSats = Android"]
-[6.059107780456543, 5.483607292175293, "[TT] Redundancy of the OBC = Redundant"]
-[6.955859661102295, 8.430229187011719, "[TT] RIN Performance of the ASM Instrument = -140 dB (Hz)^1/2"]
-[9.604715347290039, -0.13888370990753174, "[TT] Altitude at Touchdown of the Hayabusa-2 = 8.5 m"]
-[13.338818550109863, 7.7655558586120605, "[FF] Transmitting Power of the Transmitter = Use of power monitor"]
-[7.401301860809326, 2.6603033542633057, "[FF] Mission Overview of the STEREO =  Solar Terrestrial Relations Observatory"]
-[13.763915061950684, 5.351327896118164, "[TT] Cell Type of the Photo-Voltaic Array = Triple junction GaAs cells (3G-28%)"]
-[4.6191606521606445, 1.6349254846572876, "[TT] Launch Date of the SkySat 3 = June 22, 2016"]
-[9.644189834594727, 1.412544846534729, "[TT] Data Transfer of the Pl\u00e9iades Neo = Up to 40 terabytes per day"]
-[13.328971862792969, 5.379598140716553, "[TT] Solar Panels of the GaoJing / SuperView minisatellites = Two on each of the pair of solar panel wings"]
-[6.105657577514648, -0.4531574547290802, "[TT] Planned Mission Duration of the Tiangong Space Lab = 40 days"]
-[6.275675296783447, 1.1274547576904297, "[FF] Research Targets of the SJ-10 Satellite = Gene expression pattern, Proteome, Mutation discovery, Embryo development"]
-[7.380186557769775, 9.008407592773438, "[TT] Wavelengths of the Filter = UV"]
-[5.64798641204834, 6.954973220825195, "[TT] Demodulation Scheme MOPS of the DSP System = 350 to 450 MOPS"]
-[7.940110683441162, 8.629813194274902, "[TT] Spectral Range VIS of the MVIRI = 0.5 - 0.9 \u00b5m"]
-[9.9226713180542, 8.99643325805664, "[TT] Effective FOV of the Channel 1 = 89 x 198 km"]
-[7.922729015350342, 5.650941371917725, "[FF] Data Collection of the 3D and 2D cameras = As long as LOS (Line-Of-Sight) is maintained"]
-[7.715871810913086, 4.810779571533203, "[FF] Performance of the OASYS = Solid"]
-[8.49048137664795, 7.4378886222839355, "[TT] Detector of the Instrument = APS (Active Pixel Sensor)"]
-[5.481192111968994, 1.034332513809204, "[FF] Acquisition Date of the OHB AG = June 28, 2011"]
-[8.74051284790039, 7.552534103393555, "[TT] Detector Area of Interest of the BEO = 200 x 200 pixels"]
-[6.353452682495117, 2.0449461936950684, "[FF] URL of the OMI = http://www.atmos-meas-tech.net/9/6035/2016/amt-9-6035-2016.pdf"]
-[8.614192962646484, 2.337934732437134, "[TT] Wind Velocity Range (Troposphere) of the Aeolus = 0 - 2 km"]
-[8.902608871459961, -0.2579944133758545, "[TT] Angular Drift Rate of the Meteor-M2 = 0.0005\u00ba/s"]
-[8.853917121887207, 7.356297492980957, "[TT] Threshold of the High LET Detector = 2 MeV"]
-[11.606562614440918, 6.629713535308838, "[TT] Energy Measurement Range for Electrons of the Telescope 3 = 2-12 MeV"]
-[5.787674903869629, -2.121406078338623, "[TT] Orbit Period of the KOMPSAT-3 = 98.5 minutes"]
-[5.754289150238037, 4.97533655166626, "[FF] Experiment of the STAR-Dundee = Testing a next-gen high-speed communication protocol called SpaceFibre"]
-[11.179311752319336, 0.6372506618499756, "[FF] Mission Objective of the Cheops = Observe bright stars that are already known to host planets"]
-[8.007230758666992, -0.030102556571364403, "[FF] Measurement of the GRACE and GRACE Follow-On = Gravitational pull exerted by massive bodies such as ice sheets"]
-[6.670031547546387, 7.589412689208984, "[TT] Beam width of the W-band = 20 mrad"]
-[6.255227088928223, -0.4346442222595215, "[TT] Arc Duration of the BepiColombo = Two months"]
-[8.23036003112793, 0.01611398160457611, "[FF] Sea Level Rise of the Topex-Poseidon and Jason missions = 3.2 mm per year"]
-[7.983913898468018, 8.721834182739258, "[FF] Spectral Parameters of the FY-4A = LWIR: 700-1130 cm -1  (14.3-8.85 \u00b5m), S/MWIR :  1650-2250 cm -1  (6.06-4.44 \u00b5m), VIS: 0.55-0.75 \u00b5m"]
-[9.840746879577637, 4.907393455505371, "[TT] Antenna Subsystem Rotation Speed of the GMI = 32 rpm"]
-[3.6475794315338135, 4.796794891357422, "[TT] Swath Coverage of the RADARSAT-1/2 = 100 km, 150 km, 170 km, 70 km, 50 km, 500 km, 300 km, 25 km, 25 km, 50 km, 20 km"]
-[7.038615703582764, 3.3310704231262207, "[FF] Technology of the MANTIS = Native multispectral Earth Observation"]
-[11.192410469055176, 1.073940396308899, "[TT] Measurement Method of the LISA = Lasers"]
-[4.767181396484375, 0.02505982667207718, "[TT] End of Life Date of the Sich-2 = 12 Dec 2012"]
-[7.517900466918945, 4.7263617515563965, "[FF] Sensor Development of the DMSP = Primary sensor and developing secondary sensor concepts"]
-[10.238085746765137, 8.087514877319336, "[TT] Clear Aperture of Telescope of the DubaiSat-1 = 30 cm"]
-[9.200325965881348, 3.1095259189605713, "[FF] Objective of the SWEA = Measure the distribution function of the solar wind core and halo electrons from about 1 eV to several keV, with high spectral and angular resolution over practically the full spherical range"]
-[10.111620903015137, 8.06087589263916, "[TT] Focal Length of the Telescope = 167 cm"]
-[9.126391410827637, 4.654938220977783, "[TT] Operational Control of the MEV-1 = Full 6-DOF (Degree of Freedom)"]
-[6.240986347198486, 0.06047994643449783, "[FF] Duration of the Performance Tests = Over long periods of time (many orbits)"]
-[7.646761894226074, 4.586833953857422, "[FF] Performance Evaluation of the ASTER = Not Provided"]
-[9.400235176086426, 6.844947814941406, "[TT] Spatial Resolution of the KazEOSat-1 = 6.5 m"]
-[9.448662757873535, -1.3899755477905273, "[TT] Eccentricity of the Satellite = 0.0024"]
-[6.557503700256348, 0.03573073446750641, "[TT] Activation Duration of the Appleton Anomaly = Much of the night"]
-[6.489932060241699, 6.382951259613037, "[FF] Downlink Method of the Sentinel-1 = Laser Communication Terminal unit allowing downlink of recorded data via the EDRS"]
-[11.767694473266602, 3.361701488494873, "[TT] Thruster of the S/C = 100 mN resistojet"]
-[5.749282360076904, 3.3890624046325684, "[TT] Cost of the Kestrel Eye II = Approximately $2 million per spacecraft"]
-[5.819580078125, 1.2100402116775513, "[FF] Announcement Date of the Galactic GPS = Winter 2018"]
-[14.29366397857666, 3.1719698905944824, "[TT] Mass of the SOLSPC = 32 kg"]
-[9.435142517089844, 6.104131698608398, "[TT] Forward and Aft View Angle of the Instrument = \u00b125.02\u00ba (along-track), \u00b15.7\u00ba (cross-track)"]
-[6.670276165008545, 8.838269233703613, "[FF] Observation of the POLDER = Earth's target reflectance from 12 directions during a single S/C pass"]
-[14.259225845336914, 3.12941312789917, "[TT] Mass of the STRaND-1 = ~ 4.3 kg"]
-[8.371333122253418, 0.8169280290603638, "[TT] Area Covered of the Saltworks = 33,000 hectares (82,000 acres)"]
-[3.1836531162261963, 2.2369933128356934, "[TT] Program of the Sentinel-1C = Copernicus, a joint European Union and European Space Agency (ESA) Earth Observation program"]
-[9.610758781433105, 0.6858314871788025, "[TT] Drift Distance of the ASTRO = More than 6 km"]
-[2.8354811668395996, 0.09658388793468475, "[TT] J2000 right ascension (deg) of the GROJ1744-28 = 266.138"]
-[7.752660274505615, 9.071067810058594, "[TT] Wavelength Range of the Band No 1 = 0.50 \u00b1 0.2 - 0.70 \u00b1 0.2 \u00b5m"]
-[3.8497259616851807, 3.4271669387817383, "[TT] Launch Date of the Galileo = 25 July"]
-[9.597856521606445, 8.256034851074219, "[TT] Field of View of the VISIM = 20\u00ba x 30\u00ba"]
-[5.406381607055664, 2.750244379043579, "[FF] Location of the Lockheed Martin Solar and Astrophysics Lab = USA"]
-[8.028414726257324, 9.251871109008789, "[TT] Wavelength of the Ice = 2.9 \u00b5m"]
-[8.03731632232666, 6.341932773590088, "[TT] Measurement Interval of the ATLAS = 70 cm"]
-[5.491354465484619, 5.9963788986206055, "[TT] Memory of the AIM = 512 k x 16 SRAM for instructions and data for the microcontroller"]
-[9.260641098022461, 1.8617300987243652, "[FF] Calibrations of the HARP-2 = Frequent lunar and solar"]
-[6.417790412902832, -1.3024042844772339, "[FF] Image Credit of the GRACE-FO = GRACE-FO Team"]
-[6.269738674163818, 4.365086078643799, "[FF] Circuitry of the SWEM = Standard designs used extensively in previous missions"]
-[10.431777954101562, 5.787510871887207, "[TT] Temperature of the HD 260655 b = 435 \u00b0C"]
-[6.640002727508545, 4.226785182952881, "[FF] Integration Status of the ALADIN = Second flight model integration was prepared"]
-[5.041631698608398, 0.035252172499895096, "[TT] Shutdown Date of the STRV-1b = September 1998"]
-[5.387748718261719, 8.037720680236816, "[TT] High Power Frequency Range of the VLF transmitter = 3 \u2013 50 kHz"]
-[3.8332064151763916, 6.270423889160156, "[TT] Number of Antennas of the KSAT = More than 130"]
-[5.433379173278809, 6.061095237731934, "[TT] SRAM of the OBC = 2 MB"]
-[4.569320201873779, 5.595667839050293, "[TT] Type of the PLBs = Personal Locator Beacons"]
-[9.435463905334473, 6.060348987579346, "[TT] Off-nadir Angle of the ALOS-2 = 18-35\u00ba"]
-[7.520481109619141, 2.2979536056518555, "[TT] Antenna Coverage of the GVAR = Earth coverage to 5\u00ba"]
-[7.995223045349121, 1.6226811408996582, "[FF] Detection of the DPR = KaPR: snow and light rain, KuPR: heavy rain"]
-[11.675333023071289, 3.388744354248047, "[TT] Thrust Range of the Ion Thruster = 1 to 22 mN"]
-[6.850656509399414, -0.6550872325897217, "[TT] Orbital Period of the Suomi-NPP = 101 minutes"]
-[10.270541191101074, 8.100137710571289, "[TT] Aperture Diameter of the COR1 = 36 mm"]
-[8.011921882629395, 8.627986907958984, "[TT] Spectral Range of the VIS = 350 - 500 nm"]
-[10.888245582580566, 7.5194411277771, "[TT] Swath Width of the Measurements = 20 km"]
-[9.59497356414795, 7.213097095489502, "[TT] Spatial resolution at nadir of the IRAS = 17 km"]
-[8.591678619384766, 3.97652006149292, "[FF] Purpose of the PHA = Monitor the effect of high energy particles on spacecraft electronics"]
-[5.312150955200195, 5.982527732849121, "[TT] Device Parameters of the QLP/NRTP = 8-14 slot cPCI chassis, PE SBC, 96 Tiger SHARC DSP @ 250 MHz, 700 W, 20 kg"]
-[6.41986608505249, 1.430436611175537, "[FF] Conference Date of the COSMO-SkyMed = March 17-18, 2004"]
-[8.08404541015625, 8.601984977722168, "[TT] Wavelength of the VNIR = 1.06 \u00b5m"]
-[10.4176025390625, 7.144001483917236, "[TT] Ground Footprint of the RA = 16 km"]
-[9.748612403869629, -0.5786072015762329, "[TT] Orbit Altitude of the HTV-8 = ~400 km"]
-[11.413854598999023, 3.4825775623321533, "[TT] Maneuvering System of the NEA Scout = Small cold-gas thrusters"]
-[5.581521034240723, 5.2011003494262695, "[TT] Use Case of the CoReCi = First commercial use in an on-board PDHU"]
-[6.352594375610352, 4.65769624710083, "[FF] Purpose of the TeLEOS-1 = Environmental Monitoring"]
-[4.143685340881348, 1.3772892951965332, "[TT] Arrival Date of the Meteosat-8 = 21 September, 2016"]
-[12.107239723205566, 3.19808292388916, "[TT] Propellant of the GPIM = Hydroxyl Ammonium Nitrate fuel/oxidizer blend"]
-[5.715324878692627, 5.7598876953125, "[TT] Processor Configuration of the SCS750 = Triple-modular redundant"]
-[8.644851684570312, 4.736210823059082, "[TT] Star Tracker of the DMSP-19 = Device"]
-[4.962152004241943, 2.0215466022491455, "[FF] Mission Requirements of the GOSAT-2 = Defined by MOE, NIES, and JAXA"]
-[8.14259147644043, 4.744582653045654, "[FF] Components of the AOCS = RWA (Reaction Wheel Assembly), IRU (Inertial Reference Unit), STT (Star Trackers), GPSR (GPS Receiver) and the control S/W"]
-[12.16716480255127, -0.2667454481124878, "[TT] Monitoring Duration of the TESS = About a month"]
-[13.398194313049316, 7.332618236541748, "[TT] Power of the XI-IV = Average power of 1.2 W"]
-[9.877272605895996, 6.446160316467285, "[FF] Duration of the Nimbus Earth Radiation Budget (ERB) Experiment = 1975 to 1992"]
-[8.25842571258545, 3.1484832763671875, "[FF] Utilization of the OMI = Global monitoring system for air quality & health and stratospheric ozone"]
-[4.618142127990723, 5.854501724243164, "[TT] Doppler Shift of the MEOSAR Payloads = Smaller for 406 MHz beacons"]
-[14.158015251159668, 3.211998224258423, "[TT] Mass of the RAAF-M1 = ~4 kg"]
-[5.1121826171875, 1.7100915908813477, "[TT] Conference Date of the TacSat-4 = Aug. 11-14, 2008"]
-[8.986799240112305, 2.5023441314697266, "[TT] Cals of the MEIDEX = 100%"]
-[8.003929138183594, 8.576930046081543, "[TT] Spectral Coverage of the Instrument = 3-12.85 \u00b5m and 753-784 nm"]
-[11.527320861816406, 4.7626495361328125, "[TT] Diameter of the Main Chutes = 35 m"]
-[9.376794815063477, 4.970627784729004, "[TT] Stabilization Accuracy of the Attitude Control System = \u00b110\u00ba"]
-[5.061354160308838, 0.6085019111633301, "[FF] Activation Date of the GOES-13 = April 16, 2010"]
-[4.761672019958496, 7.360430717468262, "[TT] X-band Transmitter Data Rate of the Measurement Data = 10 Mbit/s"]
-[5.0751166343688965, 2.0263047218322754, "[TT] Mission Status of the NeuSAR = Operational (nominal)"]
-[8.38353443145752, 0.8794975280761719, "[TT] Reconstructed Resolution for SWE (Snow Water Equivalent) of the DPS = 2 - 5 km"]
-[6.213043689727783, 2.280545949935913, "[TT] Principal Investigator of the SIMPL = Talbot Jaeger"]
-[4.934861183166504, 1.7035772800445557, "[TT] Mission of the Gokturk-2 = High-resolution optical reconnaissance and Earth observation"]
-[7.318136215209961, 6.647093772888184, "[TT] Integration Time of the Argus = 100 microseconds to 8 seconds"]
-[9.791814804077148, 4.504207134246826, "[TT] Attitude Control of the Satellite = Limited control with magnetorquers"]
-[4.838812351226807, 7.303848743438721, "[TT] CW Beacon Data Rate of the RF Communications = GMSK 9.6 kbit/s / AFSK 1.2 kbit/s"]
-[6.110624313354492, 6.479021072387695, "[TT] Latency Requirement of the S-2 NRT = Within 30 minutes"]
-[9.384228706359863, 5.280502796173096, "[TT] Angular Rate Tolerance of the Procyon = 2\u00b0/s"]
-[5.297807693481445, 5.611376762390137, "[TT] Interface of the STRV-2 DHS = MIL-STD-1553 bus"]
-[4.495366096496582, 1.6508227586746216, "[TT] Launch Date of the NPSat-1 = 2017"]
-[5.00426721572876, 3.3896448612213135, "[TT] Manufacturer of the MMFU = IT"]
-[10.494941711425781, 4.686354637145996, "[TT] Attachment Method of the Separation Panel = Hinges"]
-[3.8209285736083984, 1.2588555812835693, "[TT] First Stage Landing Location of the Falcon 9 = Atlantic Ocean"]
-[14.032533645629883, 7.176346778869629, "[TT] Power Source of the PSM = +28 V"]
-[6.889651298522949, -0.585101842880249, "[TT] Ground Repeat Cycle of the Orbit = 41 days"]
-[6.204104900360107, 1.42391836643219, "[FF] Launch Date of the eROSITA = 26 April 2019"]
-[7.4555487632751465, 2.4739248752593994, "[FF] Strip Map Area Collect Capability of the Satellite = Not a factor of slew rate"]
-[8.073317527770996, 7.8587541580200195, "[TT] Size of the HSC-III optics subsystem = 245 mm x 95 mm x 85 mm"]
-[5.4607672691345215, 6.315920352935791, "[TT] Capacity of the Payload Mass Memory = 16 Gbit"]
-[11.808331489562988, 4.485628128051758, "[TT] Height of the Rocket and Payload = 196 feet"]
-[14.12342357635498, 3.15615177154541, "[FF] Mass of the TigriSat = 3U"]
-[8.062101364135742, 0.9060217142105103, "[TT] 2022 Fires of the U.S. Drought Monitor = 211"]
-[8.934622764587402, 5.604726791381836, "[FF] Altitude Error Type of the OMPS = Rigid vertical shift"]
-[4.483713626861572, 2.907489776611328, "[TT] Location of the F-DUGS = France"]
-[5.419829845428467, 5.974033355712891, "[TT] Operating System (kernel) RAM of the STRV-1b spacecraft = 120 kByte"]
-[7.397800922393799, 9.046926498413086, "[TT] SRF (Solar Rejection Filter) Spectral Width of the GLM = ~30 nm FWHM"]
-[13.200424194335938, 7.33414363861084, "[TT] Power Consumption of the MI Radiometer = < 195 W"]
-[9.328371047973633, 5.0553412437438965, "[TT] Attitude Pointing Accuracy of the CHIPSat = \u00b12\u00ba"]
-[7.894654273986816, 5.0177903175354, "[FF] Typical Value of the NO2 = 6"]
-[9.604077339172363, 8.322312355041504, "[FF] FOV (Field of View) of the VectorSol = Unknown"]
-[6.11548376083374, 0.8166828751564026, "[TT] Image Capture Date of the CaSSIS = 22 December 2018"]
-[4.913485527038574, 3.1412062644958496, "[FF] Prime Contractor of the MSI Instrument = Airbus DS (former EADS Astrium SAS)"]
-[6.7311530113220215, 1.863221287727356, "[FF] URL of the Deep Space 1 = http://nmp.jpl.nasa.gov/ds1/NewsConference/04_06_99DS1.pdf"]
-[7.440589904785156, 5.353304862976074, "[TT] Instrument of the ATLAS-2 = SOLCON-2, ACRIM-II"]
-[9.876144409179688, 1.696105718612671, "[FF] Expansion Rate of the Universe = Accelerating"]
-[5.7444634437561035, -0.8744110465049744, "[TT] Design Life of the WorldView-1 = 7.25 years"]
-[10.420621871948242, 6.103762626647949, "[TT] Cooling Temperature of the eROSITA camera = -80\u00baC"]
-[10.756758689880371, -0.19946250319480896, "[TT] Bus Design of the TanDEM-X = Extended to allow the formation flight of both satellites"]
-[9.625077247619629, 7.4081525802612305, "[TT] Angular Resolution (FWHM) of the Instrument = 9.5 arcsec"]
-[7.037680625915527, 1.1961489915847778, "[FF] Observation Date of the Spitzer = 28 April 2020"]
-[4.915833473205566, 0.4238455593585968, "[TT] Launch Date of the Deployment Systems = July 12, 2006"]
-[7.64561128616333, 6.695274829864502, "[TT] Image Sequence Acquisition Time of the COR1 = \u2264 8 s"]
-[11.336782455444336, 0.4760507643222809, "[FF] Speculated Size of the Planet Candidate = The size of Saturn"]
-[6.650611400604248, 3.306185007095337, "[FF] Imaging Capabilities of the BlackSky Gen-3 satellites = Short-wave infrared (SWIR) for low light and nighttime imaging"]
-[10.466915130615234, 5.391403675079346, "[TT] Type of the Trim Heaters = Trim"]
-[3.8329570293426514, 6.17645263671875, "[TT] Alignment Type of the Helical Antenna = Self-Aligning"]
-[7.993399620056152, 5.889031887054443, "[TT] Sensor Capabilities of the SV-24 = Staring, Motion, Imagery/ Video, Low Light"]
-[7.1731791496276855, 4.762388706207275, "[TT] Sensing Unit of the FIBOS = Two FBGs mounted onto a steel support"]
-[13.351640701293945, 7.8283610343933105, "[TT] Transmitter Output Power of the L-band data transmission = 5 W"]
-[5.594422340393066, 6.560904502868652, "[TT] Data Relay Capacity of the EDRS = Up to 50 TB a day"]
-[14.318490982055664, 3.0659127235412598, "[TT] Mass of the OSIRISv3 = 1.65 kg"]
-[5.606137752532959, 5.675260543823242, "[TT] Processor of the OBC = 80386/80387"]
-[10.139981269836426, 9.999720573425293, "[FF] First European Mission to Launch Multiple Small Satellites Date of the Vega = 3 September 2020"]
-[6.841320514678955, 4.798283100128174, "[TT] Side Panels of the CSTB1 = P0 through P5"]
-[11.732458114624023, 0.11851436644792557, "[FF] Number of Eclipsing Binaries Candidates of the TESS = 450,000"]
-[5.460031032562256, 0.7218661904335022, "[TT] Arrival Date of the Hera = November 2024"]
-[7.964219093322754, 6.541813850402832, "[FF] Elevation Data Resolution of the ATLAS = Higher spatial and vertical resolution"]
-[14.154184341430664, 3.291311740875244, "[TT] Mass of the M1S/M2S = ~1000 kg"]
-[6.525052547454834, 4.87682580947876, "[FF] Control Modes of the IPS = Automatic, Manual"]
-[4.9214982986450195, 4.29015588760376, "[FF] ARGOS Support of the ESEX = Attitude control, communications, radiation-hardened data storage, and housekeeping power"]
-[6.487171173095703, 3.163285255432129, "[FF] URL of the The Charter = http://www.disasterscharter.org/c/document_library/get_file?folderId=33636&name=DLFE-2502.pdf"]
-[7.3674702644348145, 4.440892696380615, "[FF] Design Concept Overview of the ASTER = Not Provided"]
-[13.334574699401855, 2.9097702503204346, "[TT] Weight of the PeruSat-1 = Up to 500 kg"]
-[5.544750213623047, 3.875570297241211, "[TT] Configuration of the Landmapper HD = 20 satellites"]
-[5.6878533363342285, -0.7876874208450317, "[TT] Design Life of the Tsubame = 1 year"]
-[6.342345237731934, 4.022199630737305, "[FF] Type of the SpaceCube2 = Versatile"]
-[8.947113037109375, 4.50217342376709, "[TT] Photodiodes per Suite of the Sun Sensor Suites = 4"]
-[6.547253608703613, -0.41865360736846924, "[TT] Testing Duration of the QUESS satellite = Four months"]
-[10.303565979003906, 5.719879627227783, "[TT] Thermal Stability Requirement of the RFE = Change less than 0.1\u00ba C over 7 days"]
-[8.969663619995117, 2.5932838916778564, "[FF] Observation Area of the IBEX = Outside the heliosphere"]
-[5.367114543914795, 1.7492215633392334, "[FF] Image Content of the ALOS satellite = Al Jawf oasis, city, large, irrigated agricultural plots, Kufra Airport"]
-[6.402919769287109, 5.461716651916504, "[FF] Design of the Signal Processing System = High performance and ultra low-power analog VLSIs that can processes multi signals simultaneously"]
-[10.072265625, -1.524367332458496, "[TT] Orbit Inclination of the HAUSat-2 = 98\u00ba"]
-[5.221974849700928, 0.7409502863883972, "[TT] Phase B Completion of the Spacebus Neo = 2015"]
-[7.58452844619751, 0.6971065998077393, "[FF] Mission of the OMOTENASHI = Demonstrate the technology for low-cost and very small spacecraft to explore the lunar surface"]
-[12.011680603027344, 4.578454971313477, "[TT] Stowed Configuration Size of the KaRIN = 3.0 m x 2.8 m x 2.8 m"]
-[7.0062127113342285, 8.360666275024414, "[TT] Estimated SNR of the Band 5 = 416.39 \u00b1 129.03"]
-[9.324636459350586, 3.1424403190612793, "[FF] Purpose of the Coronagraph = Block out the image of the sun's disc and take pictures of the faint corona"]
-[4.9221086502075195, -2.1318624019622803, "[TT] Launch Mass of the Chang'e-1 = 2350 kg"]
-[9.671463012695312, 6.952426910400391, "[TT] Spatial Resolution of the HIRES = About 2 km at 400 km altitude"]
-[5.53194522857666, -1.8607062101364136, "[TT] Operation Year of the KOMPSAT-3 = 2015"]
-[7.9914445877075195, 2.2816410064697266, "[FF] Imaging Capabilities of the MSU-MR = Cloud cover, surface temperature, vegetation, snow and ice"]
-[4.76320743560791, 0.0702957808971405, "[TT] End of Life Date of the CAS500 = 2029"]
-[13.544045448303223, 5.462681293487549, "[TT] Quantity of the Solar Cells = 64"]
-[9.28948974609375, 4.922816753387451, "[FF] Function of the CMS instrument = Measure attitude changes from a known initial condition without drift"]
-[7.1212477684021, 2.895642042160034, "[TT] Funding of the MethaneSAT = Provided by The Audacious Project"]
-[10.812721252441406, 5.625665664672852, "[FF] Material of the Thermal Protection System = Ceramic materials"]
-[12.061034202575684, 6.421492576599121, "[TT] Positron Annihilation Line Width of the RHESSI = >~5 keV"]
-[4.522364139556885, 1.5196301937103271, "[TT] Launch Date of the TechEdSat = 21 July 2012"]
-[9.932290077209473, 4.969327449798584, "[TT] Revolution Time of the Filter Wheel = 100 ms"]
-[9.34862995147705, 3.2758538722991943, "[FF] Function of the Onboard Software = Tracks the solar wind flow speed and autonomously adjusts the energy range"]
-[6.3485846519470215, 0.4206991493701935, "[TT] Quantity of the ROSE-L SAR = 1"]
-[13.359382629394531, 7.167211055755615, "[TT] Power of the C&DH module = 0.65 W (average)"]
-[6.604940891265869, 6.132295608520508, "[FF] Coverage of the Predictive Avoidance Request Message = Next few days of laser activity by the LCRD payload optical terminal"]
-[11.355986595153809, 3.4578404426574707, "[FF] Propulsion of the Satellite = For orbit establishment, maintenance, collision avoidance, and end-of-life (EOL) disposal"]
-[10.563309669494629, 2.845543146133423, "[FF] Antennas Deployment of the OPTOS nanosatellite = Confirmed"]
-[4.444369792938232, 1.1024906635284424, "[FF] Development Date of the Strategic Sites Monitoring Solution = 8 October 2020"]
-[5.547795295715332, 6.772002220153809, "[TT] Data Volume of the SSI/ES-2 = 12 MByte/satellite-day"]
-[10.765299797058105, -1.0506389141082764, "[FF] Attitude Change Point of the SLATS = D point"]
-[8.05129337310791, 5.090826034545898, "[FF] Calibration of the MADRAS = Unknown"]
-[7.786339282989502, 8.72527027130127, "[FF] Wavelength of the EXI = UV"]
-[9.613741874694824, 7.028414249420166, "[TT] Spectral Resolution of the eROSITA = Unprecedented"]
-[12.703407287597656, 3.887910842895508, "[FF] Evidence of the Ion Dispersion = Multiple ion dispersions observed within a single spacecraft pass through the cusp have been provided as evidence for pulsed magnetopause reconnection"]
-[8.72221851348877, 7.065610885620117, "[FF] Field of View of the Image Quality = 2.7 Rsun"]
-[7.463632583618164, 2.044832229614258, "[FF] Purpose of the CBERS-4A = Monitor water resources, agriculture, urban growth, land use, deforestation and burning of the Amazon rainforest"]
-[10.397042274475098, 5.875383377075195, "[TT] Antenna Temperature of the WISPR = ~1800\u00baC"]
-[14.085296630859375, 3.1562612056732178, "[TT] Mass of the DSX = 600 kg"]
-[7.563701152801514, 1.2412925958633423, "[FF] Presentation Date of the SWIM = July 12-17, 2009"]
-[6.984723091125488, 7.0219807624816895, "[TT] Line Width of the Laser Transmitter = Typically 50 MHz"]
-[6.006781101226807, 1.72059965133667, "[FF] Vision of the Eu:CROPIS = To derive the greatest benefit from long- term human space exploration"]
-[8.238462448120117, 5.836184501647949, "[FF] Observation Region of the Spectrometer = Latitudinal zones 56\u00ba - 70\u00ba N and 63\u00ba - 88\u00ba S"]
-[9.891407012939453, 2.664104461669922, "[TT] Grasp of the HaloSat = 26 cm2deg2"]
-[6.886163711547852, 5.352113723754883, "[FF] Function of the DWP = Data compaction and compression, event selection, particle/wave correlation, and control of WHISPER"]
-[9.25867748260498, 5.334608554840088, "[TT] Average Stabilization Velocity of the Navigation and Stabilization = 0.36 arcsec/s"]
-[5.047097206115723, 0.7243123054504395, "[FF] Date of the Medicane Ianos = 18 September 2020"]
-[3.8568966388702393, 2.0506489276885986, "[TT] Launch Vehicle of the SkySat-16 to -18 = Falcon 9 rocket"]
-[6.25618314743042, 4.484407424926758, "[FF] Functionality of the Mission Control Center = Provides the required TM and TC functions and display capabilities"]
-[4.825676441192627, -1.8153603076934814, "[TT] Mission Duration of the Chang'e-2 = 6 months"]
-[6.204077243804932, 5.829853534698486, "[FF] Function of the E1/E5a Frontend Box = Converts received signals to intermediate frequency, performs signal amplification and filtering"]
-[11.119674682617188, 5.296148777008057, "[TT] Separation of the Primary Objective = 0.5 mm at the edge"]
-[7.424229145050049, 6.443732261657715, "[TT] Event Duration of the XGRE = 10-100 ms"]
-[7.984129428863525, 5.370848655700684, "[TT] Test Length of the FLLS = 16 m"]
-[8.659945487976074, 1.9257712364196777, "[TT] Target Application of the SGR-ReSI receiver = Take wind speed measurements within hurricanes"]
-[10.981948852539062, 4.796913146972656, "[TT] Braking Method of the Tether = Mechanical friction"]
-[3.8920369148254395, 1.9707289934158325, "[TT] Launch Vehicle of the GHOSt = SpaceX's Falcon 9"]
-[5.6511101722717285, 1.2647744417190552, "[FF] Test Date of the Narrow-Band IoT = 17 October 2019"]
-[8.886727333068848, 4.665831089019775, "[TT] Attitude Control of the CeREs = Precision star tracker and two Sun pointers"]
-[4.553737163543701, 5.8685526847839355, "[TT] Ambiguity Resolution of the 406 MHz emergency beacon = 90% on first pass"]
-[7.9637908935546875, 8.448562622070312, "[TT] Spectral Regions of the MVIRI = Thermal infrared region (TIR), water vapour absorption bands (WV), and in the visible range (VIS)"]
-[10.344340324401855, 3.1629912853240967, "[FF] Quantity Needed of the Amazonia-1 = At least 30"]
-[7.0420966148376465, 5.797735691070557, "[FF] Connection of the GESS = Commercial Rubidium clock"]
-[5.989144802093506, 0.062170010060071945, "[TT] Operation Mission of the HAUSat-2 = 1 year"]
-[9.484296798706055, 5.071070194244385, "[TT] Sun-pointing Stability of the AOCS = 1 arcsec over a period of 1.5 minutes"]
-[9.894913673400879, 5.2556047439575195, "[FF] Thermal State of the Celestial Bodies = Unknown"]
-[8.339561462402344, 7.583015441894531, "[TT] Detector Types of the OLS = Silicon photoconductive diode, HgCdTe photoconductive detector, PMT detector"]
-[4.743316173553467, 0.7433946132659912, "[TT] Number of Planned Mission Rehearsals of the GOES-R = 6"]
-[4.5530242919921875, 3.8399758338928223, "[TT] Number of Satellites of the Galileo program = 30"]
-[3.6582024097442627, -1.057298183441162, "[FF] Type of the Satellite = Elliptical polar orbit"]
-[3.756258249282837, 3.897341012954712, "[FF] Event of the RISAT-1 = Floods in Indonesia, February 2015"]
-[7.691858768463135, 0.8878322243690491, "[FF] Area of the Hoinga = About 90 times bigger than the size of the full Moon"]
-[6.938031196594238, -0.2727411985397339, "[FF] Radio Signals of the Hitomi = 3/28 22:06 (for about 10 sec) @ USC"]
-[7.064725875854492, 2.1200242042541504, "[FF] Image Assessment System (IAS) of the Landsat-7 = Provides users with ancillary information needed to generate useful, radiometrically calibrated and geometrically corrected ETM+ digital imagery"]
-[5.7865495681762695, 4.767948150634766, "[FF] User Satellite of the LCT = LEO Sentinel-1A/-2A satellites"]
-[8.713764190673828, 8.380145072937012, "[TT] Depth of Spectrometer Measurements of the Galileo probe = About 75 miles (120 kilometers)"]
-[5.192641735076904, 2.2344696521759033, "[FF] Predecessor of the TOMS = BUV"]
-[7.839364051818848, 8.967601776123047, "[TT] Wavelength Range of the SiPD = 0.50 - 0.90 \u00b5m"]
-[10.186993598937988, 4.419521808624268, "[FF] Actuators of the OceanSat-1 = Reaction wheels, magnetic torquers and hydrazine thrusters"]
-[10.377976417541504, 6.269478797912598, "[TT] Sensitivity Improvement of the NuSTAR = More than 100-fold"]
-[12.84051513671875, 7.594318389892578, "[TT] Power Consumption of the SEIS Instrument = Up to 8.5 W"]
-[13.368517875671387, 5.417191505432129, "[TT] Number of Deployable Wings of the Solar Array = 2"]
-[6.523013591766357, 4.084933757781982, "[FF] Generation of the MetOp = Second"]
-[5.44786262512207, 5.079796314239502, "[TT] Data Bus of the OBC = Dual redundant CAN (Controller Area Network) bus"]
-[8.670655250549316, 4.541097164154053, "[TT] Types of the Sensors = Solar cell voltage & current, Battery voltage & current, Temperature (panel inside x 6, radio, battery x 3), Angular velocity"]
-[7.995357513427734, 2.1634788513183594, "[TT] Sensor Complement of the SeaSat = Active and passive instruments"]
-[10.164020538330078, 3.290996789932251, "[FF] Similarity to CubeSat InflateSAIL of the Dragsail = Very similar"]
-[14.045970916748047, 7.1622538566589355, "[TT] Bus Rail Voltage of the Spacecraft = 26 \u00b16 V"]
-[13.547731399536133, 6.9098219871521, "[TT] Bus Power Consumption of the EROS-A = 300 W"]
-[5.60418701171875, 4.605818748474121, "[FF] Establishment of the State Vectors = Using Deep Space Network (DSN), Orbit Determination and ground uplink"]
-[6.559367656707764, 4.91434383392334, "[FF] Function of the CEU = Provides power and data connections to the IBEX-Hi and IBEX-Lo sensors and stores all mission data, including SCB housekeeping telemetry"]
-[9.787158012390137, 3.7698352336883545, "[TT] Canister Mounting of the CVX-1 experiment = Two adjacent canisters"]
-[4.937111854553223, 7.392886638641357, "[TT] Data Rate of the RF Communications = 1.2 kbit/s"]
-[5.498281002044678, -0.43314218521118164, "[TT] Sail Deployment Time of the LightSail-2 = Roughly two minutes"]
-[7.794712543487549, 5.9344563484191895, "[FF] Measurement of the Vector Sensor = Amplitude and phase of radio emission"]
-[6.5455498695373535, -0.4643312692642212, "[TT] Repeat Cycle of the CERES on TRMM = 46 days"]
-[3.8718721866607666, 6.495498180389404, "[TT] Look Angle of the Antenna = 35.5\u00ba"]
-[7.60854434967041, -0.06465926766395569, "[TT] Flight Above the Surface of the Philae = More than an hour"]
-[4.885745048522949, 0.6356786489486694, "[TT] CME Capture Date of the SUVI = July 10, 2022"]
-[8.883415222167969, 4.909305095672607, "[FF] Measurement of the TWINS Sensor Heads = Trajectory and velocity of each incident ENA"]
-[9.186570167541504, 3.3045709133148193, "[FF] Imaging Target of the COR-2 = Sun\u2019s outer atmosphere, or corona"]
-[3.783726453781128, 6.280406951904297, "[TT] Quantity of the Six helical antennas = 6"]
-[2.9735515117645264, 1.995375633239746, "[TT] Measurement Record Start Date of the Copernicus Sentinel-6 Michael Freilich = 1992"]
-[4.5956902503967285, 1.1886917352676392, "[TT] Number of Computers of the SAOCOM-1A = 6"]
-[10.11286735534668, -1.424149513244629, "[TT] Orbit Inclination of the KySat-1 = 98.2\u00ba"]
-[10.354780197143555, 1.5998932123184204, "[TT] Number of Accreting Supermassive Black Holes of the eROSITA = Around 3 million"]
-[6.910430908203125, 6.781306266784668, "[FF] Technology of the Laser = Monolithic laser oscillator technology"]
-[9.456218719482422, 5.194767951965332, "[TT] Roll Axis Rotation of the TCS = \u00b1 36\u00b0"]
-[3.9998836517333984, 1.9940593242645264, "[TT] Launch Vehicle of the ETS-VIII = H-IIA F11"]
-[3.203916549682617, 4.985877990722656, "[TT] FRS-2 Swath of the RISAT-SAR = 25 km"]
-[6.222914695739746, 4.7810540199279785, "[FF] Function of the Arduino-based processors = Run other activity tasks such as interfacing with the payload, polling sensor data, and interfacing with the GPS"]
-[6.244704246520996, 8.054521560668945, "[FF] Output of the CU = Impulses to all channels"]
-[10.85112190246582, 7.57292366027832, "[TT] Swath Width of the KMS = 940 - 960 km"]
-[6.224126815795898, 8.088848114013672, "[FF] Components of the RWA = One RW and a single channel WDE"]
-[11.98840045928955, 6.477870941162109, "[TT] Positron Annihilation Line Energy of the RHESSI = 511-keV"]
-[8.161086082458496, 1.063978672027588, "[FF] Altitude of Eruption of the CALIPSO = 31 km"]
-[9.415972709655762, 7.112634181976318, "[TT] Spatial Resolution - Pan of the Spacecraft = 1 m GSD"]
-[11.824918746948242, 0.052873026579618454, "[TT] Number of Oscillating Red Giant Stars of the TESS = 158,000"]
-[9.31842041015625, 5.0558552742004395, "[TT] Roll Maneuvers of the RapidEye = \u00b120\u00ba"]
-[8.86974048614502, 3.1057209968566895, "[FF] Purpose of the EUV and X-Ray Irradiance Sensors (EXIS) = Assess space weather"]
-[8.219647407531738, -0.45911240577697754, "[TT] 1981\u20132010 Average of the Antarctic sea ice = 2.8 million km2"]
-[5.741937160491943, 5.682837009429932, "[TT] Power of the Proton P400K-SGMII-2-PCI104S-SD Space Computer = Low"]
-[8.965988159179688, 3.237459659576416, "[FF] Length of Operation of the Solar Measurements = 5\u201310 min per orbit"]
-[13.214529037475586, 7.2668561935424805, "[TT] Power Consumption of the STOs and STAEs = 150.4 W (for 3 STO configuration)"]
-[10.916460990905762, 5.937307357788086, "[TT] Components of the DDM = Four radiation sensitive dual MOSFETs"]
-[14.261948585510254, 3.2877814769744873, "[TT] Mass of the PMI = 200 - 250 kg"]
-[7.151659965515137, 1.3124698400497437, "[TT] Discovery Tool of the Spitzer Space Telescope = Exoplanets"]
-[10.169568061828613, 9.364900588989258, "[TT] Nominal IGFOV of the Band 2 = 0.5 km"]
-[8.234309196472168, -0.6839213371276855, "[TT] Coverage of the Digital Elevation Model = 91% of the total ice on land and 97% of Antarctica's floating ice shelves"]
-[9.535094261169434, 4.500193119049072, "[FF] Spin Rate and Orientation of the LAGEOS 2 = Unknown"]
-[5.653615951538086, 3.7276413440704346, "[TT] Quantity of the SkySats = 18"]
-[8.466670036315918, 7.347048282623291, "[TT] Analog Outputs of the GOCI-II CMOS Imaging Sensor = 10"]
-[9.710561752319336, 7.193161487579346, "[TT] Ground Resolution of the Band 2 = 5.4 km"]
-[4.0951361656188965, 7.87951135635376, "[FF] Modulation Schemes of the MTP = 4"]
-[3.7726681232452393, 4.767864227294922, "[TT] Resolution of the RADARSAT-2 = 3 m"]
-[11.083073616027832, 5.916388511657715, "[TT] Material of the Flywheel = Silicon nitride"]
-[11.23575496673584, 0.9897984862327576, "[FF] Centrifugal Force Cause of the LISA Pathfinder = Combination of the shape of LISA Pathfinder's orbit and the effect of the noise in the signal of the startrackers used to orient it"]
-[5.583804130554199, 2.202380895614624, "[FF] Orbit Confirmation of the YES = Confirmed"]
-[6.170849800109863, 2.966132164001465, "[TT] Resolution of the WorldView Legion Camera = 0.29m"]
-[6.976075649261475, 6.611133575439453, "[TT] Sounding Time of the Sounder = Almost three hours"]
-[4.737957000732422, 0.002718878211453557, "[TT] End of Life Date of the TechEdSat = 5 May 2013"]
-[11.964675903320312, 5.014408111572266, "[TT] Size of the User Terminal = 200 mm x 150 mm x 50 mm"]
-[5.166574478149414, 1.9032645225524902, "[TT] Mission Status of the SARAL = Operational (extended)"]
-[9.50024700164795, 3.8172600269317627, "[FF] Design Evolutions of the Vector Magnetometer = Necessary to comply with the mass and power budgets allocated to the OVM"]
-[11.680888175964355, 3.2614946365356445, "[TT] Impact on Thrusters of the Meteosat-8 = One of the nominal thrusters used for east-west station keeping maneuvers seems affected, possibly damaged"]
-[9.26196575164795, -1.6451241970062256, "[FF] Food Consumption of the Desert Locusts = Same amount of food in one day as about 35,000 people"]
-[9.034775733947754, 6.387670516967773, "[TT] Design of the OMPS = Limb- and nadir-viewing"]
-[9.753303527832031, 8.370319366455078, "[TT] FOV of the FSI dual EUV 174 \u00c5 and 304 \u00c5 alternatively = 5.2\u00ba x 5.2\u00ba"]
-[5.305319786071777, 0.3214082419872284, "[TT] Launch Date of the Cheops = 18 December 2019"]
-[6.760084629058838, 2.246846914291382, "[FF] URL of the PSAT = http://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=3549&context=smallsat"]
-[5.499203681945801, 6.0159478187561035, "[TT] EEPROM of the OBC = 524 kB"]
-[9.11848258972168, 5.700686931610107, "[TT] Area Collection Rate of the Push Frame Framer with a fast steering mirror = Very low"]
-[7.032845973968506, 5.889602184295654, "[TT] Clock Type of the GIOVE-B = Rubidium atomic clock"]
-[9.387471199035645, 6.043306350708008, "[TT] Guard Angle of the MXT = 20\u00b0"]
-[10.769428253173828, 3.469813346862793, "[TT] Size of the ExoCube = 3U CubeSat"]
-[4.816542148590088, 6.178461074829102, "[FF] Purpose of the KNACKSAT = Use of an amateur radio for communication"]
-[7.125077724456787, 5.014275074005127, "[TT] Ultimate Factor of Safety of the ESPA ring = 1.4"]
-[5.998094081878662, -0.4798538386821747, "[TT] Mission Duration of the SPOT-3 = Three years"]
-[11.507556915283203, 3.4887382984161377, "[FF] Testing Method of the ESP Thruster = Firing in pairs and measuring the changes to the spin rate via on-board rate instrumentation"]
-[10.077537536621094, 4.564704895019531, "[TT] Reaction Wheels of the Satellite = 3-axis"]
-[10.141956329345703, 7.048154830932617, "[TT] Across-Track Span of the ILATM2 = Approximately 150 m"]
-[13.24422836303711, 7.136005878448486, "[TT] Power Status of the CATS = On"]
-[8.297595977783203, -0.8620977997779846, "[TT] Presence of the Carbon Dioxide Ice Patch = Isolated rare case"]
-[4.489770412445068, -0.8710418343544006, "[TT] Launch Date of the Crew Dragon = 15 September 2021"]
-[10.268770217895508, 1.0079008340835571, "[FF] Proximity to Star of the HIP 67522 b = Close"]
-[5.815412998199463, 5.692612648010254, "[FF] Operational Protocols of the ISERV = Image data acquisition, storage, and downlink"]
-[3.6569533348083496, 5.221319198608398, "[TT] Polarization of the RISAT-1 = Circular"]
-[8.36479377746582, 5.914828777313232, "[TT] Planned Measurement Rate of the Claire = Double as of early 2017"]
-[9.021710395812988, 8.564809799194336, "[TT] Band 4 Wavelength Range of the Telescope = 6.50 - 7.10 \u00b5m"]
-[5.053037166595459, 1.0479153394699097, "[FF] Mission Date of the O/OREOS Sat = Oct. 12-16, 2009"]
-[1.7239062786102295, 6.140171051025391, "[FF] Existence of the Dark Radiation = Possible in the early cosmos"]
-[6.748379230499268, 6.302119255065918, "[FF] Transaction Time of the CPT = Allocated time"]
-[5.6818132400512695, 11.356693267822266, "[FF] Approx. Peak Sensitivity Altitude of the Channel 5 = Unknown"]
-[7.300820827484131, 2.869962453842163, "[TT] Ground Control Center Location of the MethaneSAT = New Zealand"]
-[6.017947673797607, 3.0082499980926514, "[TT] Imager Manufacturer Experience of the WorldView Legion = 45 years"]
-[4.953454494476318, 4.9661641120910645, "[FF] Function of the Satellite Aided Search and Rescue (SAS&R) = Relays distress signals and detects alerts from beacon transmitters"]
-[5.942224979400635, -0.7128753066062927, "[TT] Stable Electricity Supply Duration of the TSUBAME = At least 80 days"]
-[3.297849655151367, 2.242513418197632, "[FF] Product Type of the Sentinel-1 = SLC (Slant-Range Single-Look Complex)"]
-[6.578666687011719, 1.9008002281188965, "[FF] URL of the Evaluation = https://spacenews.com/nasa-continues-csda-program/"]
-[7.7963643074035645, 8.64859390258789, "[TT] Spectral Range of the Instrument = 3.92-4.64 \u00b5m"]
-[11.780835151672363, 4.99826717376709, "[TT] Size of the MEMS device = 3 cm x 3 cm"]
-[13.347517967224121, 7.13162088394165, "[TT] Projected EOL of the Payload Power = 140 W"]
-[14.307319641113281, 3.2793867588043213, "[TT] Mass of the MuREM = < 1 kg"]
-[14.242837905883789, 3.0780863761901855, "[TT] Mass of the AlSat-2 = 120 kg"]
-[9.66348648071289, 4.80078649520874, "[TT] Stabilization of the TIROS = Spin stabilized to inertial space"]
-[12.102141380310059, 3.7337727546691895, "[TT] Gas Pressure of the Detector = 1.5 bar"]
-[4.345696449279785, -0.09179561585187912, "[TT] Launch Date of the P35 series = Aug. 23, 1962"]
-[7.928583145141602, 8.428190231323242, "[TT] Processing Rate of the Spectral bands = 10 Mpixel/s for PAN, 5 Mpixel/s for MS"]
-[5.065800666809082, 3.5079610347747803, "[TT] Manufacturer of the Weather Program = RCA (Radio Corporation of America)"]
-[10.389922142028809, 4.083583831787109, "[TT] Boom Length of the NewMag = 2.55 m"]
-[8.128389358520508, 4.379120349884033, "[TT] Maneuver Requirement of the Chaser S/C = Relative trajectory that does not advance towards or retreats away from the target over multiple orbits"]
-[9.002552032470703, 7.7048540115356445, "[TT] Spatial Resolution of the INSAT-3D imager = 1 km for VIS and SWIR, 4 km for MWIR, TIR-1 and TIR-2, 8 km for WV"]
-[3.6972343921661377, 5.455424785614014, "[TT] Range Resolution of the Ultrafine and Spotlight = 1.9 m"]
-[8.493627548217773, 1.7431724071502686, "[TT] Integrated water vapor of the Cloud water = 0.1 kg/m 2"]
-[5.282869815826416, 7.691821098327637, "[TT] Isolation of the Diplexer = 60 dB"]
-[10.446578025817871, 5.7727789878845215, "[TT] Storage Temperature of the Integrated Mobile Station = -30\u00ba to 60\u00baC"]
-[9.021188735961914, 5.7266340255737305, "[FF] Boresight Pointing Measurement of the OVIRS = With respect to an optical alignment cube on OVIRS"]
-[4.82231330871582, 1.8022985458374023, "[TT] Launch Date of the HORYU-2 = May 17, 2012"]
-[8.692980766296387, 4.776535511016846, "[TT] Type of the Star sensor = CCD matrix"]
-[6.060714244842529, 0.8983044624328613, "[TT] Image Capture Date of the Advanced Baseline Imager (ABI) = Dec. 14, 2020"]
-[10.276286125183105, 2.1565139293670654, "[FF] Data Type of the Chandra X-ray Observatory = X-ray emission"]
-[10.117939949035645, -1.6190671920776367, "[TT] Inclination of the IDEA-OSG 1 = 98\u00ba"]
-[3.8599941730499268, 2.070305824279785, "[TT] Launch Vehicle of the MethaneSAT = Falcon 9"]
-[8.293992042541504, 3.137603998184204, "[FF] Purpose of the ILAS = Ozone Layer Observation"]
-[6.693687915802002, 5.905830383300781, "[TT] Quantity of the STIM-210 = 2"]
-[3.4958314895629883, 6.5432844161987305, "[TT] Antenna Diameter of the Altimeter Antenna = 1.5 m"]
-[3.769336462020874, 7.158334732055664, "[TT] Peak Gain of the Antenna = 36 dBi"]
-[8.235311508178711, 5.834640026092529, "[FF] Velocity Measurement Range of the NMS = 0.1-2 km/s"]
-[13.7926607131958, 7.1619439125061035, "[TT] Soft Start Up of the DC-DC converter = Typically greater than 1ms/V"]
-[10.458003044128418, 6.633835315704346, "[TT] Number of Mirrors of the NuSTAR Metrology System = 2"]
-[11.980701446533203, 6.430963516235352, "[FF] Rigidity Dependence of the AMS-2 = Above 60 GV"]
-[14.142586708068848, 3.237489938735962, "[TT] Mass of the NAVANT = 21.9 kg"]
-[6.103636264801025, 3.389315128326416, "[TT] Number of Experiments Funded of the OPS-SAT = 12"]
-[7.9823455810546875, 6.241892337799072, "[TT] Instrument Type of the LISS-III = Imaging multi-spectral radiometers (vis/IR)"]
-[8.480565071105957, 7.770499229431152, "[TT] Array of the Fluidic Card = 4 x 12"]
-[9.774574279785156, 7.464967727661133, "[TT] Ground Sample Distance (GSD) of the SWIR Band = 20 m x 20 m"]
-[9.366564750671387, 7.38625431060791, "[TT] Spatial Resolution of the ScaRaB = 48 x 48 mrad"]
-[3.9231598377227783, 5.262187480926514, "[TT] GPS Position Knowledge of the SAR (Synthetic Aperture Radar) Instrument = Real-time within 60 m"]
-[6.1711955070495605, 0.4000037610530853, "[TT] Observation Period of the SoloHI = 17-19 December"]
-[9.849469184875488, 8.732276916503906, "[TT] IFOV of the SiPD = 0.45 - 0.52 \u00b5rad"]
-[8.261767387390137, 3.3152103424072266, "[TT] CWV Retrieval Methods of the MTI = CIBR (Continuum Interpolated Band Ratio) and the APDA (Atmospheric Precorrected Differential Absorption) methods"]
-[7.6570634841918945, 4.995532512664795, "[FF] Purpose of the EOU EQM = Test its performance and to verify its optomechanical design against dynamic loads"]
-[10.12199592590332, -2.712239980697632, "[TT] Technology of the Sentinel-2 MMFU = NAND-Flash Storage"]
-[6.690167427062988, 4.417516231536865, "[FF] Purpose of the Flight Dynamics Tool = Evaluate the navigation data and provides essential data for mission planning"]
-[6.494260787963867, -0.15336298942565918, "[TT] Revisit Time of the OSCAT = 2 days"]
-[7.804133892059326, 5.858236789703369, "[FF] Bias of the Altimeter = Unknown"]
-[13.834846496582031, 3.071009397506714, "[FF] Mass of the SeaHawk-1 = Unknown"]
-[7.453884124755859, 5.23347282409668, "[FF] Components of the CERTO/PLUS = Three-frequency radio-beacon, antenna and an UV photometer"]
-[8.778115272521973, 1.853472352027893, "[TT] Wind Speed of the EF-3 tornado = 140 mile/h (225 km/h)"]
-[8.78864574432373, 0.8462722301483154, "[TT] Touchdown Requirement of the Lander Module = < 5 m/s in vertical and horizontal velocity"]
-[3.983576774597168, 2.124969482421875, "[TT] Type of the Launch Vehicle = EELV medium"]
-[9.13086223602295, 7.575740814208984, "[TT] Coverage of the CCD Camera = 6250 km x 300 km per scan line"]
-[8.170597076416016, 4.462329864501953, "[TT] Update Method of the Spectral Calibration = Vicarious techniques using the measurement of the atmospheric gas and/or the sun Fraunhofer lines"]
-[8.835352897644043, 2.7135908603668213, "[TT] Ionospheric Plasma Survey Hours of the DSLP = 10 thousand hours"]
-[7.314693450927734, 6.899693012237549, "[TT] Measurement Method of the MABEL and ATLAS = Detect just a few photons from each laser pulse and timing their round-trip travel from satellite to earth and back extremely accurately"]
-[1.7503317594528198, -2.072896718978882, "[TT] Communication Disruption of the Hayabusa-2 = During solar conjunction operation"]
-[5.482975006103516, 5.27565336227417, "[TT] Supported RTOS of the RAD750 SBC = VxWorks (versions 5.4, 5.5, and 6.2)"]
-[7.45682954788208, 3.613116502761841, "[FF] Function of the GNSS-POD = Provide with high accuracy and precision a measurement of the orbital position as needed for the conversion of the measurement of altimeter range into a sea level"]
-[8.878588676452637, 8.009894371032715, "[FF] Sextants and Dodecants of the Optic = Unknown"]
-[7.676631927490234, 3.2318665981292725, "[TT] Viewing Capability of the OLS = Nighttime cloud viewing at a lower resolution than daytime visible fine-mode data"]
-[14.047636032104492, 3.554039716720581, "[TT] Mass of the EyeSat = 5 kg"]
-[5.947267055511475, 6.671069622039795, "[TT] Data Retrieval Time of the DMSP and POES systems = About two hours"]
-[13.222137451171875, 5.423936367034912, "[FF] Deployment of the Solar Array = Elastically deployable"]
-[10.739830017089844, 6.582172393798828, "[FF] Machining Process of the OAP = Conventional machining for the mirror blank, single-point diamond turning (SPDT) to achieve the surface figure, and post-polishing to reduce surface scatter"]
-[13.752228736877441, 2.8618106842041016, "[TT] Mass of the Spacecraft = 6 ton"]
-[2.9031472206115723, 4.3791913986206055, "[TT] Calibration Frequency of the PALSAR-2 = Every 3 months"]
-[3.3832218647003174, 1.4732446670532227, "[TT] Launch Date of the Sentinel-1B = April 25, 2016"]
-[8.85249137878418, 5.266440391540527, "[FF] Guidestar Selection of the Spacelab Instrument Pointing System = Improvements"]
-[7.5167131423950195, 4.986084938049316, "[FF] Measurement Modes of the Sensor = Count Mode, List Mode"]
-[5.655837535858154, 6.963042736053467, "[TT] Input Data Rate of the Mass Memory System = 2 x 540 Mbit/s"]
-[7.605105876922607, -2.5106942653656006, "[TT] Data Availability of the GOLD = Through 11/30/2019"]
-[9.229744911193848, 3.466921329498291, "[FF] Purpose of the MMS = Capture the show of charged particles in the magnetosphere"]
-[4.285942077636719, 7.305903434753418, "[TT] Frequency Allocations of the S-band transmitter = Amateur Satellite UHF-band or Space Research S-band"]
-[8.423213005065918, 6.873475074768066, "[FF] Blur Requirement of the Optical System = Must be kept in bounds"]
-[5.167743682861328, 6.9894585609436035, "[FF] Wi-Fi Connection of the FlytLIVE = Always-on high-speed"]
-[4.541400909423828, -0.8631333112716675, "[TT] Splashdown Date of the Crew Dragon spacecraft = Sept. 18, 2021"]
-[6.216703414916992, 8.091398239135742, "[TT] Coding of the Channel = 1/4 to 9/10 FEC"]
-[4.75858736038208, 2.953770637512207, "[TT] Storage Location of the TEMPO = Maxar\u2019s satellite manufacturing facility in Palo Alto, California"]
-[3.0377097129821777, 2.4251511096954346, "[TT] Methane Detection of the Copernicus Sentinel-5P = True"]
-[6.558723449707031, -0.4873020350933075, "[TT] Period of the Resurs-P1 = 94 minutes"]
-[9.515377044677734, 0.7521703839302063, "[TT] Orbit Location Distance of the ACE Mission = About 1% of the way toward the sun on the sun-Earth line"]
-[8.721803665161133, 7.5845160484313965, "[TT] MS MTF of the Imager = >20%"]
-[5.89778995513916, 1.103812575340271, "[FF] Consortium Leadership Date of the Planet = 27 January 2021"]
-[5.822114944458008, 3.3678812980651855, "[TT] Cost per Satellite of the Satellogic = $2 million dollars per year"]
-[9.77021312713623, -0.5586079955101013, "[TT] Orbit Altitude of the SPOT 1-5 = 832 km"]
-[9.592984199523926, -0.4268895387649536, "[TT] S/C Subsatellite Point Travel of the AMSR-E = 10 km in 1.5 seconds"]
-[10.471705436706543, 6.608311653137207, "[TT] Quantity of Mirrors of the LRA = 100"]
-[11.723482131958008, 6.770508766174316, "[FF] Function of the Advanced Resistive Exercise Device (ARED) Knowledge Reaper Asset in a Kinetic Network (KRAKN) Electronics Box = Upgrade the advanced resistive exercise device\u2019s legacy instrumentation box"]
-[7.273880958557129, 0.7734638452529907, "[FF] Operation Status of the China's Lunar Lander = Spotted"]
-[14.109996795654297, 7.19498872756958, "[TT] Operating Voltage Range of the LVPS Board = 26 - 29 V"]
-[9.808209419250488, 4.255581855773926, "[TT] Number of the Magnetorquers = 3"]
-[9.272998809814453, 7.446304798126221, "[TT] Image Size of the CIPS = 1440 km x 960 km"]
-[6.534859657287598, 5.428729057312012, "[TT] Analog Inputs of the C&DH SPAM board = Eight"]
-[5.003808498382568, -0.30616825819015503, "[TT] Launch Time of the TSIS-1 = 15:36 UTC"]
-[12.434541702270508, 0.6258460879325867, "[TT] Readout Modes of the PLATO detectors = Full frame (FF) or frame transfer (FT)"]
-[3.7347328662872314, 4.373314380645752, "[FF] Measurement domain of the SAR (RISAT) = Ocean, Land, Snow & Ice"]
-[5.577851295471191, 5.433450698852539, "[TT] Type of the Instrument's Interfaces = ESA Atmel SMCS-332"]
-[5.4745402336120605, 1.3854509592056274, "[FF] Workshop Date of the MXGS = May 19-22, 2009"]
-[14.439595222473145, 6.499287128448486, "[TT] Battery Strings of the Satellite = 2"]
-[6.2007293701171875, 4.486398220062256, "[FF] Operation of the Satellite to Satellite Tracking Instrument (SSTI) = Provide Satellite-to-Satellite Tracking"]
-[10.187119483947754, 9.387629508972168, "[TT] Nominal IGFOV of the Band 8 = 2 km"]
-[14.234432220458984, 3.1409049034118652, "[TT] Mass of the UNIFORM-1 = ~50 kg"]
-[11.741004943847656, 3.2163116931915283, "[TT] RCS Thrust of the ARTEMIS = 10 N"]
-[10.939001083374023, 7.5848388671875, "[TT] Swath Width of the WFI = 684 km"]
-[9.726445198059082, 7.083548545837402, "[TT] Spatial Resolution (km) of the SASS = 50"]
-[9.48464584350586, 6.233320236206055, "[TT] Look Angle of the MSU-SK = 39\u00ba"]
-[4.4231953620910645, 1.884090542793274, "[FF] Presentation Date of the RADARSAT-2 = Sept. 29 to Oct. 3, 2008"]
-[9.462349891662598, 7.346227169036865, "[TT] Spatial Resolution of the ETM+ = 15 m (PAN band), 30 m (VNIR/SWIR bands), 60 m (TIR band)"]
-[6.457001209259033, 6.095233917236328, "[TT] Position of the AHS = Left-hand port"]
-[6.768375873565674, 5.8814873695373535, "[TT] Quantity of the DGS = 2"]
-[5.158425331115723, 7.6125874519348145, "[TT] Sampling rate of the Cross dipole antenna = 76.8 kHz"]
-[5.569539546966553, 5.645943641662598, "[TT] Processor of the OPS-SAT = Altera Cyclone V System-on-Chip (SoC)"]
-[6.353234767913818, 3.322216510772705, "[FF] Primary Role of the Dextre = ISS Handyman, replacing failed components, unloading cargo, supporting technology demonstrations"]
-[3.8448500633239746, 6.7386860847473145, "[TT] Pulse Duration of the Altimeter Antenna = 102.4 \u00b5s (Ku), 102.4 or 32 \u00b5s (C)"]
-[7.940734386444092, 7.625509738922119, "[FF] Technology Basis of the Hyperspectral Imaging = High spectral resolution measurements of light interacting with matter"]
-[6.094480037689209, 1.1674538850784302, "[FF] Date of the \"NASA Soil Data Joins the Air Force\" = 19 November 2019"]
-[13.891698837280273, 7.0646748542785645, "[TT] Transmission Voltage of the ISS = 120 V"]
-[8.822017669677734, 4.53662109375, "[TT] Type of the Horizon sensor = 2 axis IR pyro array & chopper"]
-[7.440878868103027, 4.857928276062012, "[FF] Observation Scheme of the SSUSI = Not provided"]
-[5.952791690826416, 1.6149250268936157, "[FF] Mission Update Date of the GPM Core = Feb. 27, 2014"]
-[4.562438011169434, -2.7941346168518066, "[TT] Frequency (GHz) of the PMI = 37.0"]
-[6.715869426727295, 1.7423769235610962, "[FF] URL of the ExoMars = http://m.esa.int/Our_Activities/Space_Science/ExoMars/Schiaparelli_crash_site_in_colour"]
-[12.049787521362305, -0.26494142413139343, "[FF] Data Analysis of the TESS = Stream age 120 million years"]
-[12.103372573852539, 4.529640197753906, "[TT] Satellite Dimensions of the Terra Bella = 60 x 60 x 95 cm"]
-[4.845198631286621, 2.9715189933776855, "[TT] Location of the MC3 CGA = UH (University of Hawaii) at Manoa, HI"]
-[14.240031242370605, 3.2417218685150146, "[TT] Mass of the OCM = 78 kg"]
-[13.337531089782715, 7.746328830718994, "[TT] Transmitter Power of the RF Communications = 1.5 W"]
-[6.220289707183838, 5.5101399421691895, "[FF] Components of the Data Handling System (DHS) = Baseband Data Handling (DH) and Solid State Recorder (SSR)"]
-[7.525897979736328, -0.7864004969596863, "[TT] Launch Year of the IceEye-1 = 2018"]
-[6.372577667236328, -1.0989230871200562, "[TT] LTAN of the HORYU-2 = 13:30 hours"]
-[4.905414581298828, 0.6419222354888916, "[TT] Execution Start Date of the CIBORG = Early 2017"]
-[6.377542495727539, 1.8975497484207153, "[FF] URL of the VRSS-1 = http://cn.cgwic.com/VRSS-1/english/focus.html#"]
-[5.862850189208984, 3.3365390300750732, "[TT] Update Frequency of the Cost Model = Throughout development"]
-[5.169435501098633, 0.5361286401748657, "[TT] First Results Date of the RadCube = Next month"]
-[5.812251091003418, 5.719175815582275, "[TT] Data Rate of the Corvus-BC satellites = 19.2kbps"]
-[7.609363555908203, 1.8284962177276611, "[FF] Date of the Pinpointing Tropical Forests with High Ecological 'Quality' = 25 August 2020"]
-[6.495728969573975, 2.0048015117645264, "[FF] URL of the Chinese satellite = http://www.nature.com/news/chinese-satellite-is-one-giant-step-for-the-quantum-internet-1.20329"]
-[5.008873462677002, 3.395082950592041, "[TT] Manufacturer of the Hugo = ABB"]
-[6.852594375610352, -0.5780712366104126, "[TT] Orbital period of the Satellite = 98.8 minutes"]
-[5.831679821014404, 4.001466751098633, "[FF] Unique Payload Services (UPS) of the GOES-R = URL: http://www.goes-r.gov/spacesegment/ups.html"]
-[4.4922895431518555, 3.081983804702759, "[FF] Ground-Based Observation Sites of the ExoCube = Arecibo, Wisconsin, Kitt Peak, and Cerro Tololo"]
-[10.655579566955566, 2.859530448913574, "[FF] Mission Type of the High-Resolution Microsatellite = Earth Monitoring and Observation"]
-[7.490643501281738, 1.3447786569595337, "[FF] OceanObs'09 Presentation Date of the SWOT = Sept. 21-25, 2009"]
-[14.079660415649414, 4.048521518707275, "[TT] Total Mass of the Sounder = ~145 kg"]
-[8.374208450317383, 8.238898277282715, "[TT] Spectral Resolution of the IRFS-2 = 0.4 cm-1"]
-[7.8745903968811035, 7.483062744140625, "[TT] Launch Date of the Hyperspectral imagers = Dec. 14, 1998"]
-[9.627720832824707, -0.42476505041122437, "[TT] Average Altitude of the FY-3D = 836 km"]
-[5.683935165405273, 6.675607681274414, "[TT] Solid State Recorder Speed of the OBC = 300 Mbit/s"]
-[9.531146049499512, 7.1323370933532715, "[TT] Angular Resolution of the Channels = 3''"]
-[4.882808685302734, 7.333273410797119, "[TT] Uplink Data Rate of the RF Communication System = 1.2 kbit/s"]
-[5.489254951477051, 7.520908355712891, "[TT] Receiver Type of the SPOT-2 = 1st generation receiver (18 kg), a bi-frequency system in 1 channel"]
-[5.646471977233887, 7.137165546417236, "[TT] 800 Mbit/s of the Data rate = -"]
-[13.68026351928711, 5.833417892456055, "[TT] Solar Panel Peak Power of the NSat = 28.8 W"]
-[7.078286170959473, 4.207223892211914, "[FF] Unknown of the Spot-1/5 \u2013Spot-6 = Unknown"]
-[10.000873565673828, 5.62998104095459, "[TT] Focal Plane Cooling of the Spectrometers = Passively cooled"]
-[6.323337078094482, 3.9466378688812256, "[FF] Components of the Spacecraft Plug-n-Play Avionics (SPA) = Special test bypass interface"]
-[7.0000410079956055, 1.810593843460083, "[FF] Launch Date of the NASA Orbiting Carbon Observatory-2 = Unknown"]
-[9.21606731414795, 3.9190123081207275, "[FF] Function of the V1-V4 Voltage Probes = Current-biased double probe electric fields sensors and capacitively-coupled radio and plasma wave sensors"]
-[8.145218849182129, 7.9842047691345215, "[TT] Payload of the PLATiNO 2 = Thermal Infrared (TIR)"]
-[4.9691081047058105, 0.4126312732696533, "[TT] Introduction Year of the SASAR = 1992"]
-[13.917581558227539, 7.033360481262207, "[TT] Voltage of the System = 300 V"]
-[8.034415245056152, 8.278426170349121, "[TT] Connection Location of the iROSA = 4B power channel"]
-[8.804078102111816, 5.1589179039001465, "[FF] IMU of the PSSCT-2 = COTS MEMS IMU (Inertial Measurement Unit) from Analog Devices"]
-[7.699613571166992, 0.5166992545127869, "[FF] Mission Type of the Lunar IceCube = Small-scale planetary missions"]
-[13.92413330078125, 7.065187454223633, "[TT] CDH Boot Sector Voltage of the MarCO-B = Approximately 3.3 V"]
-[7.685897350311279, -0.7906723022460938, "[TT] ISRE Date of the ICESat-2 = December 1, 2010"]
-[8.645549774169922, 1.309572458267212, "[FF] Viewing Angle of the Aquarius instrument = Away from the sun"]
-[9.065595626831055, 0.7213111519813538, "[TT] Planned Quantity of the Kinetic Impact/Crater Generation = One"]
-[5.825433731079102, -2.23940372467041, "[TT] Orbit Altitude of the KOMPSAT-3 = 685 km"]
-[5.201301097869873, 1.213815450668335, "[FF] IAC Presentation Date of the D-Sat = 25-29 Sept. 2017"]
-[12.131473541259766, 6.129673480987549, "[TT] Cosmic Ray Elements of the AMS-02 = Up to Z< 27"]
-[13.855868339538574, 3.201042652130127, "[TT] Gravitational Influence of the G229-20 A and B = Less likely"]
-[6.03393030166626, 5.516583442687988, "[TT] Redundancy of the Supervisor = Dual-redundant"]
-[5.839452743530273, 0.6186475157737732, "[FF] Date of the Georegistered CUMULOS data = 17 September 2018"]
-[7.125370025634766, 6.622374057769775, "[FF] Detection Efficiency of the GLM = Unknown"]
-[5.479040622711182, 4.228451728820801, "[TT] Number of Remote Tracking Stations of the DMSP = 4"]
-[9.779805183410645, -0.3536917567253113, "[TT] Altitude Lowering of the Mothercraft = More than 10 km"]
-[5.442507743835449, 3.485440254211426, "[TT] Execution Responsibility of the TDP Operations = Inmarsat"]
-[9.432662010192871, -1.7267216444015503, "[TT] \u0394RAAN of the Swarm-C (Charlie) = ~0-135\u00ba difference wrt mean plane of A/B"]
-[14.002740859985352, 7.187798500061035, "[TT] Power Output of the EPS = 28 \u00b14 VDC"]
-[3.626654624938965, 4.629568099975586, "[FF] On-board Satellite of the Synthetic Aperture Radar = RISAT-1"]
-[7.814878463745117, 8.775352478027344, "[TT] Tilting angle of the Spectral Bands = -20\u00ba, 0\u00ba, +20\u00ba"]
-[7.526643753051758, 5.357440948486328, "[FF] Components of the OTES = Sunshade, telescope, aft optics plate, electronics board, instrument enclosure"]
-[10.71571159362793, 1.8495980501174927, "[FF] First multimessenger observation of the Fermi Gamma-ray Space Telescope = Picked up the first such multimessenger observation just seconds after LIGO detected a merger of two neutron stars through gravitational waves"]
-[4.0143513679504395, 2.1446373462677, "[TT] Flight Number of the Ariane 5 = VA255"]
-[13.279313087463379, 5.506801605224609, "[FF] Solar Panels Configuration of the LF spacecraft = Shown in Figure 2(a)"]
-[4.403597831726074, 7.814725875854492, "[TT] Uplink Frequency of the Cadet-U UHF radio = 449.75 MHz"]
-[9.430105209350586, 0.8251002430915833, "[TT] Peak Distance from the Sun of the Water Production = About 1.7 au"]
-[6.043113708496094, 5.0723466873168945, "[FF] Inter-Orbit Communication Experiment of the Eureca = Unknown"]
-[10.0227689743042, 8.192992210388184, "[TT] Free Aperture of the LRI = > 3 x beam diameter"]
-[3.894627571105957, 4.263538360595703, "[FF] Remote Sensing of the RADARSAT-2 = Ocean, Sea Ice, and Large Water Regions"]
-[5.76702356338501, -2.062080144882202, "[TT] No of revolutions of the KOMPSAT-3A = 15.1 revolutions/day"]
-[5.8849310874938965, 4.322225093841553, "[FF] Components of the Satellite = More than 600 electronic and radio-frequency units"]
-[10.825117111206055, 6.871320724487305, "[FF] Improvement of the DDA = Capturing more reflected energy and requiring smaller transmitted power"]
-[5.151690483093262, 1.0827275514602661, "[TT] Search and Rescue Demonstration Date of the OPS-SAT = 14 October 2021"]
-[4.7484259605407715, 0.4686796963214874, "[TT] Launch Date of the GOES-T = March 2022"]
-[7.953293800354004, 8.95063304901123, "[TT] Wavelength Range of the XRS = 0.05-0.4 nm and 0.1-0.8 nm"]
-[11.34701156616211, 4.293096542358398, "[TT] Size of the OSCAR-QUBE = 1U"]
-[14.010231018066406, 6.32211446762085, "[TT] Built-in Flash of the GomSpace NanoMind A3200 = 512 kB"]
-[9.831653594970703, 3.9102001190185547, "[TT] Location of the Brazilian Hall current magnetometer = In the spacecraft avionics near the wake side of the spacecraft"]
-[5.199434280395508, 3.2678020000457764, "[TT] Manufacturer of the DMSP-14 = Lockheed Martin Space Systems"]
-[5.061511039733887, 7.0664215087890625, "[TT] Downlink Data Rate of the NSat = 9.6 kbit/s"]
-[5.250910758972168, 3.2351505756378174, "[TT] Manufacturer of the WorldView Legion = Maxar-owned manufacturer formerly known as Space Systems Loral"]
-[7.580235958099365, 0.8560885190963745, "[TT] Destination of the MoonLIGHT = Reiner Gamma region of the Moon"]
-[8.831901550292969, 4.453648090362549, "[FF] Sensor Type of the GLI = Core sensor of OCTS heritage"]
-[13.388155937194824, 6.845458507537842, "[TT] Power of the Spacecraft = 600 W"]
-[6.419031620025635, 0.5587678551673889, "[TT] Launch Year of the Landsat-7 = 1999"]
-[10.0003080368042, -0.06930673867464066, "[TT] Proximity to Sentinel-3A of the CDN2 Site = 100 m east"]
-[6.990026473999023, 8.920055389404297, "[TT] Wavelength of the POLDER = 443 nm"]
-[8.827117919921875, 3.410031795501709, "[FF] Purpose of the CIP = In-situ measurements of the ionospheric plasma compositions, ion concentrations, velocities, and temperatures"]
-[3.949763774871826, 0.688919723033905, "[TT] Launches in 2021 of the Falcon 9 = 8"]
-[8.725907325744629, 8.811334609985352, "[TT] Electronics of the Grating Spectrometer = 8 bit microprocessor with 12 bit ADC, 3.6-4.2 V, input rail 250-1000 mA"]
-[6.142575740814209, 2.3243746757507324, "[TT] European Principal Investigator of the MIRI = Gillian Wright"]
-[6.314632415771484, 4.756009101867676, "[FF] Functions of the ALOS-2 ground system = Data processing, archiving, cataloging and user service functions"]
-[9.003255844116211, 8.031332015991211, "[TT] CCD Line Pixel Count of the FPM (Focal Plane Module) = 12,000 pixels"]
-[4.605008125305176, 0.5495205521583557, "[TT] Launch Date of the Sich-2 = April 17, 2007"]
-[5.135339736938477, 8.427631378173828, "[TT] Bandwidth/Passband of the 8 = 1500 MHz"]
-[8.964645385742188, 4.5113115310668945, "[TT] Safe Mode Operation of the ADCS = Coarse sun pointing"]
-[9.290560722351074, 5.189794063568115, "[TT] Re-orientation Velocity (max) of the Navigation and Stabilization = 0.25\u00ba/s"]
-[6.72413969039917, 5.245079517364502, "[FF] Device Type of the QLP/NRTP = cPCI computer system, and a COTS-based DSP (Digital Signal Processor)"]
-[10.167146682739258, 0.9690871238708496, "[TT] Distance from Earth of the HD 93396 = 320 light-years"]
-[6.4513678550720215, 1.2017871141433716, "[FF] Sensor Complement of the FormoSat-7 / COSMIC-2 = Unknown"]
-[6.9270100593566895, 1.5727158784866333, "[FF] Project Status Presentation of the James Webb Space Telescope = Phil Sabelhaus, \"Project Status for the James Webb Space Telescope Partner's Workshop,\" JWST Partner's Workshop, Ottawa, Canada, May 19, 2009"]
-[6.666358947753906, 6.018187999725342, "[FF] Response Time Requirement of the ACC = Fast"]
-[7.418630599975586, -0.8487669825553894, "[TT] Mission Duration of the ICESat-2 = More than 10 years"]
-[6.671203136444092, 6.743685245513916, "[TT] Laser Communication Terminals of the EDRS-D = Multiple"]
-[6.330098628997803, 3.958333730697632, "[FF] Technology of the RCM = Up to date"]
-[10.389854431152344, 4.084713935852051, "[TT] Length of the Booms = 30 cm"]
-[5.968814373016357, 8.129087448120117, "[TT] Number of channels of the Millimeterwave receiver = 4096"]
-[11.181690216064453, 5.011504650115967, "[TT] CCR Diameter of the LARES = 37.5 mm"]
-[9.100876808166504, 8.071629524230957, "[TT] Readout Resolution of the LLNL imaging system = 8 bit"]
-[7.460893154144287, -0.6843670010566711, "[TT] Duration of the Operation IceBridge = Eleven Years"]
-[6.238321781158447, 4.9678778648376465, "[FF] Data Processing Challenge of the INCUS = Technical challenge that\u2019s really fun"]
-[10.683428764343262, 7.139777660369873, "[TT] Footprint of the 4 = 25.8 x 17.5 km"]
-[8.44062328338623, 6.936099052429199, "[FF] Camera of the Pico Dragon = OmniVision CMOS VGA color sensor with low power consumption"]
-[4.3866658210754395, 7.849201202392578, "[TT] Downlink Frequency of the Cadet-U UHF radio = 468 MHz"]
-[8.082096099853516, 1.0910178422927856, "[FF] Importance of the Soil Moisture = Relevant for a variety of applications, particularly farming"]
-[7.933695316314697, 5.310462951660156, "[FF] Purpose of the FLLS = Fine Lateral and Longitudinal Sensor"]
-[7.727829933166504, 5.939219951629639, "[TT] Device Type of the SOLCON = Differential absolute radiometer"]
-[5.360821723937988, 1.0484459400177002, "[TT] Satellite Environment Test Campaign Date of the IASI-NG PFM instrument = 2022 and 2023"]
-[4.803492546081543, 0.6749565601348877, "[FF] Development Start Date of the MMO = March 19, 2015"]
-[5.518991947174072, 6.161890983581543, "[TT] Memory Module Capacity of the IRIS = 8 Gbit"]
-[5.160580158233643, 1.9966187477111816, "[TT] Mission Status of the Satellite = Operational"]
-[7.650279998779297, 6.24635124206543, "[FF] Mapping of the CCRR = From the detector output at a given CCRR position to the corresponding position measurement from the laser tracker"]
-[6.013173580169678, 5.77948522567749, "[TT] Pin Count of the Virtex-4 FPGA = 1140"]
-[9.338418960571289, 8.768376350402832, "[TT] Width of the HXR Flare Ribbons = ~1 arcsec"]
-[5.022024631500244, 7.2625908851623535, "[TT] Telecommand Uplink Data Rate of the GIOVE-B = 2 kbit/s"]
-[7.183260440826416, -0.5682855248451233, "[TT] Rotation Period of the Zeta Puppis = 1.78 d"]
-[5.159666061401367, 6.967945575714111, "[TT] Uplink Speed of the Communication links = 9.6 kbit/s"]
-[11.212162017822266, 5.079100608825684, "[TT] Diameter of the Primary Sensor = 1/8\u201d"]
-[6.476708889007568, 3.2470927238464355, "[TT] Imaging Type of the BlackSky = High-revisit"]
-[10.12314224243164, -1.5037040710449219, "[TT] Quantity of the Satellite = 4 mid-inclination satellites"]
-[5.453409671783447, 6.3577399253845215, "[TT] Mass Memory Capacity of the NIEU = 64 Gbit"]
-[7.750321388244629, 0.5047759413719177, "[FF] Mission Objective of the Lucy = Explore the diversity of Trojan asteroids and their satellites"]
-[5.055273056030273, 3.36301851272583, "[TT] Manufacturer of the MSS = SBRC (Santa Barbara Research Center) of Hughes"]
-[7.340797424316406, 2.1225554943084717, "[FF] Purpose of the SPOT-4 = Environmental studies, crop monitoring and management, environmental forecasting"]
-[5.413015842437744, 4.176826477050781, "[TT] Bus Configuration of the QuikTOMS spacecraft = Two rings stacked together vertically"]
-[4.894012451171875, 7.337268352508545, "[TT] Data Rate of the S-band = 665.4 kbit/s"]
-[7.324578285217285, 7.640814304351807, "[FF] Design of the PHA = Small, low power"]
-[9.298471450805664, 6.426303863525391, "[TT] Sight Axis Angle of the Spectrometer 1 = 60\u00b0 with nadir"]
-[9.39699649810791, -1.6857737302780151, "[TT] Altitude of the Swarm-B = Circa 516 km"]
-[6.620936393737793, -2.0031769275665283, "[FF] Project Status Meeting Date of the Jason-1 = Oct. 19-21, 2011"]
-[5.065655708312988, 0.4218100607395172, "[TT] Launch Date of the Aeolus = August 2018"]
-[4.773828506469727, 3.233933448791504, "[FF] Manufacturer of the TANSO-FTS-2 = Harris"]
-[6.1493754386901855, 5.855538845062256, "[FF] Radio Waves of the Magnetars = Can emit steady beams of radio waves"]
-[4.200325965881348, 2.0965957641601562, "[TT] Ground Stations of the NigeriaSat-2 = Abuja and Guildford"]
-[10.715715408325195, 2.1492350101470947, "[TT] Observed Parts of X-ray Light Spectrum of the XMM-Newton = Low-energy"]
-[4.503119468688965, 0.2413582056760788, "[FF] Delivery Failure Date of the Soyuz = 11 Dec. 2017"]
-[5.432285785675049, 0.060807086527347565, "[FF] Testing Completion Date of the RapidEye = Unknown"]
-[4.429588317871094, 7.804042816162109, "[TT] Uplink Frequency of the RF Communications = UHF band (437.5 MHz)"]
-[3.2617006301879883, 5.613676071166992, "[TT] X-band Downlink Margin of the SAR Antenna = 9 dB"]
-[4.548412322998047, 7.850244522094727, "[TT] Uplink Frequency of the SAS&R = 406.05 MHz"]
-[5.086884498596191, 1.0826866626739502, "[FF] Congress Date of the BEESAT-3 = Sept. 10-12, 2012"]
-[12.409107208251953, 0.6642530560493469, "[TT] Total Image Resolution of the PLATO Satellite = 2.12 gigapixels"]
-[9.820442199707031, 7.089282035827637, "[TT] Beam Resolution of the SASS = Fixed"]
-[5.9173150062561035, 1.1308592557907104, "[FF] Presentation Date of the Michelson Interferometer = May 27-31, 1991"]
-[3.4677646160125732, 5.008411884307861, "[FF] Support of the SARP-2 = Both long and short messages"]
-[1.6051428318023682, 3.762096881866455, "[TT] Fault-tolerant satellite design of the BEESAT-2 = Yes"]
-[4.328938961029053, 2.379673957824707, "[TT] Launch Site of the SOCRATES = TNSC (Tanegashima Space Center), Japan"]
-[7.974547386169434, 4.065464973449707, "[FF] Payload of the Spacecraft = Five scientific instruments to include three cameras, a magnetometer, and a gamma-ray spectrometer"]
-[4.0945916175842285, 6.216141223907471, "[FF] Function of the Antenna = Easily removed from the spacecraft without removing any of the spacecraft panels"]
-[10.649842262268066, 3.843940496444702, "[FF] Control Method of the Solar or drag sails = Constantly controlled relative to either the solar vector for steered sailing or the satellite velocity vector to maximize drag"]
-[10.015628814697266, -1.508122205734253, "[TT] Orbit Inclination of the LARES-2 = 70.16\u00ba"]
-[14.2666015625, 3.0501456260681152, "[TT] Mass of the AlSat-2B = 117 kg"]
-[12.42161750793457, 0.5936197638511658, "[FF] Conference Presentation Date of the PLATO satellite = 1-5 October 2018"]
-[7.847018241882324, 6.867772102355957, "[FF] Detector Function of the Conventional Interferometers = Collects light over the full aperture of the critical optical components"]
-[10.53786563873291, 6.033290863037109, "[TT] Temperature Sensitivity of the NuSTAR = More than 3 million degrees Celsius"]
-[10.865066528320312, 2.0934815406799316, "[FF] X-ray Map of the XMM-Newton = Extensive"]
-[8.131918907165527, 2.6340458393096924, "[FF] Product of the AGRI = Cloud Masks, Cloud Type, Cloud Top Temperature, Cloud Top Pressure, Cloud Optical Depth, Cloud Liquid Water, Cloud Particle Size Distribution, Aerosol Detection, Aerosol Optical Depth, Downward Longwave Radiation, Upward Longwave Radiation, Reflected Shortwave Radiation"]
-[7.2124152183532715, 5.822092533111572, "[FF] Components of the Laser Transmitter = Laser Optical Module (LOM) and Laser Electronics Module (LEM)"]
-[9.314849853515625, -0.5294729471206665, "[FF] Orbit Adjustment of the VNREDSat-1 = Second"]
-[8.349472045898438, 3.008577585220337, "[FF] Requirements of the ISUAL = Determine the location and timing of luminous phenomena above thunder clouds, obtain a global survey of upper atmospheric optical flash transients"]
-[6.762981414794922, -0.4933711588382721, "[TT] Orbit Repeat Time of the SeaHawk-1 = About 18-days"]
-[6.699009895324707, 5.855203151702881, "[FF] Operational Date of the EO-Missions Hybrid Optical/RF Payloads = Oct.12-16, 2015"]
-[5.004715442657471, 7.667378902435303, "[TT] Frequency Bands of the Antenna = E5 and E1-band"]
-[10.174110412597656, 4.563456058502197, "[TT] Maximum Torque Output of the CMG = 0.8 mNm"]
-[5.121294975280762, 3.454745054244995, "[TT] CMG Assembly of the ACS = IMPACT 1.1"]
-[6.298264980316162, 3.2764687538146973, "[TT] Development Location of the Phase Measurement System = Jet Propulsion Laboratory"]
-[4.705993175506592, 3.243406295776367, "[TT] Communications Link of the James Webb Space Telescope = Malindi ground station in Kenya"]
-[3.4651710987091064, -0.937992513179779, "[TT] Orbit of the SMAP = Near-polar, sun synchronous"]
-[7.766659736633301, 7.11135721206665, "[TT] Frame Rate of the Video Product = 30 frames/s"]
-[6.899171352386475, 6.2078118324279785, "[TT] Timers of the MCU = Three 16-bit timers"]
-[6.002276420593262, 7.477135181427002, "[TT] PRF (Pulse Repetition Frequency) of the ATM = 5 kHz"]
-[6.251810073852539, 2.7281439304351807, "[TT] Name of the CERN = VESPER (Very energetic Electron facility for Space Planetary Exploration missions in harsh Radiative environments)"]
-[5.419923305511475, 3.0703423023223877, "[FF] Year of the Maxar Technologies 2019 10-K filing = 2019"]
-[5.0228190422058105, 0.6035327315330505, "[TT] Launch Date of the LADEE = Fall 2013"]
-[9.592384338378906, 8.103689193725586, "[TT] Field of Regard of the NAOMI = \u00b135\u00b0"]
-[14.204071998596191, 3.193483352661133, "[TT] Mass of the FPU = 16 kg"]
-[5.416702747344971, 7.293232440948486, "[TT] Bandwidth of the FODB = Gbit/s"]
-[14.301685333251953, 3.256934642791748, "[TT] Isotope of the RTG = Pu-238"]
-[12.142179489135742, 2.9835002422332764, "[TT] Propulsion System of the GFO = Hydrazine"]
-[6.9042582511901855, 2.8037607669830322, "[FF] Benefits of the Mission = Ecological forecast, water quality, air quality"]
-[5.688559055328369, 7.037573337554932, "[TT] Data Rate of the Command and Data Handling Subsystem = Up to 900 kbit/s"]
-[10.245808601379395, 5.806559085845947, "[TT] Temperature of the Collector Array = < 200 K"]
-[2.9140636920928955, 4.450913429260254, "[TT] Calibrated Beams of the PALSAR-2 = 58"]
-[3.3500709533691406, 1.5326964855194092, "[TT] Launch Date of the Sentinel-5P = Planned for the timeframe 2020"]
-[8.581243515014648, -0.3737603724002838, "[TT] Orbit Latitudes of the CryoSat = 88\u00b0 North and South"]
-[5.4528350830078125, 0.7281574606895447, "[FF] Data Collection Date of the CALIPSO = January 16"]
-[4.8879804611206055, 8.385239601135254, "[TT] Frequency Range of the MTVZA-GY = 52-57, 91 and 183 GHz"]
-[6.103963851928711, 4.621660232543945, "[FF] Interfaces of the HMA = Catalog Service, Ordering Service, Programming Service, Mission Planning Service, Online Data Access Services"]
-[5.12183952331543, 0.10510141402482986, "[TT] Launch Date of the Polar Vigilance Mission = Mid-year"]
-[7.643461227416992, 6.3999481201171875, "[TT] Image Generation Frequency of the VHRR/2 = Every 26 minutes"]
-[9.7470064163208, 7.524422645568848, "[TT] Cross-Track Swath of the Nadir Sensor Wide-Field Telescope = 2800 km"]
-[13.454456329345703, 5.860414981842041, "[FF] Generation Voltage of the High-voltage solar array = Unknown"]
-[5.510806560516357, 3.1860740184783936, "[FF] Vice President of Communication and Strategic Space Systems of the Northrop Grumman = Blake Bullock"]
-[9.444644927978516, -0.9729222059249878, "[TT] Orbit Inclination of the Beijing-3B = 97.94\u00b0"]
-[12.047775268554688, 3.5922114849090576, "[TT] Pressure Exerted by the Pushing Spring of the Separation System = About 2500 N"]
-[5.200858116149902, 0.8232855796813965, "[TT] Launch Schedule of the ECP sensors = Late 2020 and early 2021"]
-[6.970565319061279, -0.42332741618156433, "[TT] Local Sun Time of the ADEOS-II = 10:30 AM \u00b115 minutes"]
-[3.7408227920532227, 4.64756441116333, "[FF] Data Sources of the SARSAT = Imager and Sounder ABI (16 bands), GLM, SEISS, EXIS, SUVI, MAG"]
-[6.407362937927246, 2.93030047416687, "[FF] User Working Group Members of the Seasat = Office of the Oceanographer of the U.S. Navy, Fleet Numerical Weather Center in Monterey, CA, Navy Surface Weapons Center in Dahlgren, VA, Naval Research Laboratory, the Johns Hopkins University Applied Physics Laboratory (APL), the Office of Naval Research, and the Navy/NOAA Joint Ice Center, NOAA Atlantic Oceanic Marine Laboratory (AOML) in Miami, FL, the NOAA weather centre in Suitland, MD, the NOAA Pacific Marine Environmental Laboratory in Seattle, WA, and NOAA's Marine Fisheries office in Bay St Louis, MS; the Defense Mapping Agency, United States Geological Survey (USGS), the U.S. Coast Guard, the Department of the Interior and the Department of Agriculture (AgriStars program)"]
-[6.506652355194092, 7.611364841461182, "[TT] Receive Chain of the Instrument = Single"]
-[4.38478946685791, 7.545249938964844, "[TT] Data Transmission Scheme of the LLMS/IRIS = SSMA (Spread Spectrum Multiple Access)"]
-[4.385875225067139, 7.055779933929443, "[FF] Purpose of the NSLSat-1 = Antenna deployment experiment, Ka-band communications experiment"]
-[13.464763641357422, 7.091414451599121, "[TT] Efficiency of the Secondary Converter = 70%"]
-[14.129693031311035, 3.1195309162139893, "[TT] Mass of the DMSAT-1 = 15 kg"]
-[8.7683744430542, 3.5302696228027344, "[FF] Solar Total Irradiance Variability of the SOVA = Detected"]
-[5.230360507965088, 1.3530372381210327, "[TT] Contract Period of the ELSA-d = 12 months"]
-[7.096720218658447, 3.39613676071167, "[FF] Photo of the C2B flight unit = Figure 3"]
-[4.841764450073242, 1.9134297370910645, "[TT] Operator of the G\u00f6kt\u00fcrk-1 = Turkish Ministry of National Defense"]
-[8.213726997375488, 2.4580636024475098, "[FF] URL of the Aerosol Polarimetry Sensor = http://glory.giss.nasa.gov/aps/docs/SPIE_6786_67865L.pdf"]
-[7.772841453552246, 8.13683032989502, "[TT] Sensitivity of the SIM = 0.2 W m-2"]
-[6.878332138061523, 5.124754428863525, "[FF] Components of the NRD = Industrial, or in some cases automotive, grade commercial off-the-shelf components"]
-[6.824357509613037, 4.410598278045654, "[FF] Control Location of the FORTE = Sandia Labs"]
-[6.004632472991943, 1.2406340837478638, "[TT] Launch Year of the SWARM = 2011"]
-[10.280935287475586, 8.031975746154785, "[TT] Aperture Diameter of the Telescope = 13 cm"]
-[9.277417182922363, 4.7861456871032715, "[TT] Attitude Control of the Monitor-E = Operational"]
-[13.407212257385254, 6.679162979125977, "[FF] Power Budget of the Spacecraft = Low"]
-[8.961027145385742, 0.4466475248336792, "[TT] Boulder Width of the Tycho central peak = Over 100 m"]
-[3.9127142429351807, 3.3997631072998047, "[TT] Transmission Duration of the Galileo probe = 57 minutes"]
-[3.3461849689483643, 5.066023826599121, "[TT] SAR Payload Repeat Cycle of the RCM = 12 days"]
-[3.733771324157715, 2.4455628395080566, "[TT] Announcement Date of the Iridium Certus service providers = February 28, 2018"]
-[6.169836044311523, 4.950727939605713, "[FF] Application of the CMT = Localized Real-Time Security Assessment"]
-[4.23587703704834, 7.251955986022949, "[TT] Frequency Band of the S-band radio frequency = S-band"]
-[10.855833053588867, 7.459683895111084, "[TT] Swath width of the ALOS-3/PRISM-2 = 50 km"]
-[9.521326065063477, 1.636067271232605, "[FF] Observation of the New Horizons = How the volcanic gases from Io are ionized, trapped and energized by Jupiter's magnetic field, then ultimately ejected from the system"]
-[9.006501197814941, 2.8961164951324463, "[TT] Function of the Narrow Band Filter = Energetic electron detector in sprites and aurora"]
-[10.880748748779297, 7.484050273895264, "[TT] Swath of the MWRI = 1400 km"]
-[6.167238712310791, 2.6675286293029785, "[FF] Platform of the CATS = International Space Station"]
-[10.108176231384277, -2.708747148513794, "[FF] Power Consumption of the NAND-Flash = Varies"]
-[3.23952579498291, 5.255013942718506, "[TT] Spotlight Scene Resolution of the SAR Antenna = 0.5 m"]
-[6.69663143157959, 1.679435133934021, "[FF] URL of the THERME experiment = http://esmat.esa.int/Materials_News/ISME09/pdf/10-In-flight/Remaury%20Paper.pdf"]
-[7.951181888580322, 9.131625175476074, "[TT] Wavelength of the Spinels = 2 \u00b5m"]
-[13.747993469238281, 2.964337110519409, "[TT] Mass of the Spacecraft = 47 kg"]
-[6.67650032043457, -0.4078197479248047, "[TT] Checkout Period of the FASTRAC satellites = About two weeks"]
-[3.9559264183044434, 7.084018230438232, "[TT] Bandwidth of the Altimeter Antenna = 320 MHz (Ku), 320 or 100 MHz (C)"]
-[4.652749061584473, 1.5145114660263062, "[TT] Full Operational Service Start Date of the GCOM-W1 = May 17, 2013"]
-[5.294729709625244, 4.29017448425293, "[TT] Rotor Type of the Knudsen Station = AlphaSpid's Big RAS rotor"]
-[10.451183319091797, 2.274357795715332, "[FF] Purpose of the NICER = Observing X-ray MSPs for navigational purposes"]
-[9.671517372131348, 7.144117832183838, "[TT] Resolution Cell, Vertical of the Instrument = 4 km"]
-[5.7240495681762695, 6.373350620269775, "[TT] Capacity of the Solid-State Recorder = 3 Gbit"]
-[5.522743225097656, 1.632988691329956, "[TT] Orbit Control Requirement of the ALOS-2 satellite = Within 500 m orbital tube"]
-[9.432465553283691, 7.069135665893555, "[TT] Spatial Resolution of the Ikonos-2 = 0.82 m"]
-[11.704553604125977, 4.755205154418945, "[TT] Outside Diameter of the Canister = 78 cm"]
-[9.131402015686035, 3.1519196033477783, "[FF] Data Analysis Plan of the THEMIS Probes = Look through archival THEMIS data for more events around Earth and determine how often the magnetopause may be booming like a drum"]
-[7.17112398147583, 6.567052364349365, "[TT] Integrating Time of the GOCI Instrument = Up to 8 seconds"]
-[9.371209144592285, 6.83463716506958, "[TT] Ground Resolution of the Corvus-HD satellites = 2.5 metres"]
-[6.765284538269043, -0.25503700971603394, "[TT] Observation Period of the Gravity Observations = 17 years"]
-[4.594573020935059, 7.763320446014404, "[TT] Downlink Signal Bandwidth of the HRIT HiRID = 1687.1"]
-[3.3557534217834473, 1.472046971321106, "[TT] Expected Operations Start of the Sentinel-2B = Three to four months after launch"]
-[12.613794326782227, 9.089609146118164, "[TT] Equator Crossing Time Deviation of the TanSat = Shorter than 15 minutes"]
-[5.320094108581543, 2.9657094478607178, "[TT] Spacecraft Provider of the PTD series = Terran Orbital"]
-[8.709858894348145, 2.110769271850586, "[FF] Predicted Performance of the E2E simulation = OSVW across the wind speed range of 5 to 25 m/s"]
-[4.955469608306885, 0.15134333074092865, "[TT] Death Date of the Verner Suomi = 1995"]
-[8.707601547241211, 5.310657024383545, "[TT] Design Bandwidth of the Three-axis diagonal gradiometer = 5 x 10 -3 to 10 -1 Hz"]
-[9.669583320617676, 4.788424015045166, "[TT] Stabilization of the DMSP satellites = Three-axis"]
-[7.5154242515563965, 2.907289743423462, "[TT] View Path of the MethaneSat = 200 kilometers"]
-[18.649961471557617, 3.938718795776367, "[TT] Value of the NE\u0394T = 0.2 K"]
-[5.193774223327637, 8.402369499206543, "[TT] Bandwidth of the Channel 5 = 1000 MHz"]
-[4.733268737792969, 7.167634010314941, "[TT] Science Data Rates of the Ka-band Downlink = 7, 14, or 28 Mbit/s"]
-[4.937167167663574, 0.5630824565887451, "[TT] Launch Year of the Kent Ridge 1 = 2013"]
-[7.263918399810791, 1.2634623050689697, "[FF] Objectives of the ExoMars = EDL (Entry, Descent, and Landing) of a payload on the surface of Mars, Surface mobility with a Rover, Access to the subsurface to acquire samples, Sample acquisition, preparation, distribution, and analysis"]
-[3.9185166358947754, 1.9860204458236694, "[TT] Launch Vehicle of the WorldView Legion = Falcon-9"]
-[10.111989974975586, -2.6536176204681396, "[TT] Max Volume of the Astrium MMFU NAND-Flash SDR-SDRAM = 710 mm x 260 mm x 310 mm"]
-[12.067917823791504, 3.672903299331665, "[TT] Pressure of the Gas Tank = 1.78 bar"]
-[7.292450428009033, 1.6152160167694092, "[FF] Goal of the Kepler = Collect and downlink as much science data as possible"]
-[7.910614490509033, 1.7188209295272827, "[FF] Monitoring Purpose of the SMOS = Ocean acidification"]
-[4.3875932693481445, 4.280957221984863, "[TT] Satellite Tracking of the GISAR = Up to 4 satellites"]
-[10.327393531799316, 5.672759056091309, "[TT] Cooling Temperature of the Filter Wheel = 213K"]
-[8.142346382141113, 3.8423142433166504, "[FF] Measurement Type of the TanSat = Maps"]
-[4.617580413818359, 6.249691009521484, "[FF] Emergency Communications Testing of the KIZUNA = Verified"]
-[7.952315807342529, 5.39666223526001, "[FF] Components of the LENA = Collimator, conversion unit, extraction lens, dispersive energy analyzer, time-of-flight mass analyzer with position-sensitive particle detection"]
-[4.979188919067383, 3.366762399673462, "[TT] Manufacturer of the Triton-1 = ISIS-BV, The Netherlands"]
-[8.184205055236816, -1.0897459983825684, "[TT] Melt Pond Depth of the ICESat-2 = About 80 cm"]
-[7.7949910163879395, 3.0068519115448, "[FF] Methane Column-Averaged Dry-Air Mole Fraction (XCH4) of the GOSAT-2 = Parameter Value Unknown"]
-[6.955430030822754, 6.968334674835205, "[TT] Stability of the Laser Transmitter = 50 MHz on one monthly time scale"]
-[4.1355085372924805, 7.301325798034668, "[TT] Bands of the Poseidon 4 = Ku- and C- band"]
-[8.996235847473145, 5.301217079162598, "[TT] Orbit Altitude of the GOMX-1 = 600 km"]
-[11.818225860595703, 6.719226837158203, "[TT] Ion Energy Channels of the EPE = 0.05 - 0.20 MeV, 2.1 - 4.5 MeV"]
-[9.785548210144043, -0.5719490051269531, "[TT] Orbit Altitude of the LitianicaSAT-2 = 505 km"]
-[7.315516471862793, 9.162826538085938, "[TT] Number of Wavelength Positions of the FG (Filtergraph) = One for the continuum"]
-[7.933433532714844, 8.369906425476074, "[TT] Spectral Bands of the Imager = PAN: 0.45-0.90 \u00b5m, B1/blue: 0.45-0.52 \u00b5m, B2/green: 0.52-0.59 \u00b5m, B3/red: 0.63-0.69 \u00b5m, B4/NIR: 0.77-0.89 \u00b5m"]
-[10.942351341247559, 2.0984926223754883, "[FF] Operation of the XMM-Newton = Must be told exactly where to point"]
-[13.38127326965332, 3.0316550731658936, "[TT] Weight of the NorSat-3 = 16 kg"]
-[5.57352876663208, 6.958624362945557, "[TT] Data Delivery Speed of the Quasar 3000 IMU = 100Hz"]
-[11.721207618713379, 6.740864276885986, "[TT] Energy Range of the ELENA = E ~20 eV up to E~5 keV"]
-[5.733646869659424, -0.448782354593277, "[TT] Design Life of the SMDC-One = 1 year"]
-[9.352456092834473, 6.021847724914551, "[TT] Elevation Mask of the GNOMES-1 = 5 degrees"]
-[3.0391886234283447, 2.0957415103912354, "[TT] Along-Track Resolution of the Copernicus Sentinel-6 Poseidon-4 = About 300 m"]
-[9.80307388305664, 7.737901210784912, "[FF] Image Duration/Recurrence of the Telescope = 25 min (scanning), 30 min (duty cycle = 100%), with 5 minutes spare time for a retrace of the scan mirror"]
-[5.450596809387207, 3.9831066131591797, "[TT] Payloads of the NSSL Phase 2 = Large military and intelligence agency satellites"]
-[1.7457575798034668, -2.0754501819610596, "[TT] Travel Time of the Hayabusa-2 = Six years"]
-[7.10746955871582, 4.775667190551758, "[FF] Outer Edge Length of the MLI = Unknown"]
-[7.499124050140381, 3.7581536769866943, "[FF] Compatibility of the NightPOD = Large SLR cameras"]
-[8.63850212097168, 1.1062730550765991, "[FF] PI of the SAC-D/Aquarius = Gary S. E. Lagerloef of ESR (Earth & Space Research), Seattle, WA; Raul F. Colomb of CONAE, Argentina; Sandra Torrusio"]
-[8.554368019104004, 2.7781875133514404, "[TT] Range of measurements of the Atmosphere = 0-5 g/cm2"]
-[4.979518890380859, 2.993297815322876, "[TT] Prime Instrument Contractor of the IASI = Alcatel Space"]
-[12.763553619384766, 1.97747802734375, "[TT] Operational Status of the SAGE-III = Operational"]
-[5.725297927856445, 5.415381908416748, "[FF] Type of the Remote Terminal Unit (RTU) = Implementing all I/O interfaces with the platform subsystems"]
-[5.446023464202881, 1.2512139081954956, "[FF] Presentation Date of the EQUULEUS-CLOTH system = 14-22 July 2018"]
-[10.265175819396973, 8.026643753051758, "[TT] Telescope Aperture Length of the Pushbroom imager = 985 mm"]
-[6.855128765106201, 6.997223377227783, "[TT] Quantity of the Total Beams = 126"]
-[4.850358486175537, -1.8054512739181519, "[FF] Mission Goal of the Chang'e-2 = Collect high-resolution imagery of possible lunar landing sites"]
-[13.549163818359375, 3.0525331497192383, "[TT] Payload Capacity of the ESPAStar = Up to six hosted or 12 separable, free-flyer payloads"]
-[9.726547241210938, 4.854344844818115, "[TT] Stabilization of the ZY-3 = 3-axis"]
-[5.120337963104248, 1.2258892059326172, "[FF] Mission Status of the ADM-Aeolus = Unknown"]
-[7.8673415184021, 2.6933727264404297, "[FF] Complementary Instrument of the CALIPSO = PARASOL (POLDER) complements CALIPSO (Lidar)"]
-[14.08759880065918, 6.595193386077881, "[TT] End-of-life Capacity of the GomSpace NanoPower BPX = 47 Whr"]
-[8.416813850402832, 1.3476920127868652, "[TT] Size of the RainCube = About the size of a cereal box to a toaster oven"]
-[10.806344032287598, 7.476663112640381, "[TT] Swath of the DPS = > 1000 km"]
-[14.238564491271973, 3.191206455230713, "[TT] Mass of the TOMS = 34 kg"]
-[13.615428924560547, 6.983202934265137, "[TT] Power of the EPS = ~ 2 W"]
-[7.521904468536377, 7.925084590911865, "[TT] Radio Emission Confirmation of the Hoinga SNR = Confirmed in 10-year-old surveys"]
-[9.671833038330078, 8.401236534118652, "[TT] FOV (Field of View) of the CIPS = 80\u00ba x 120\u00ba"]
-[12.914773941040039, 7.087316989898682, "[TT] Efficiency of the SABR = Above 95%"]
-[9.308817863464355, 3.1974234580993652, "[TT] Film Roll of the Coronagraph = 229 m long by 35 mm wide"]
-[6.975789546966553, 4.78674840927124, "[FF] Parameter of the Spitzer = Value"]
-[14.234485626220703, 3.2040112018585205, "[TT] Mass of the M3 = 5.1 kg"]
-[10.011825561523438, -1.4921895265579224, "[TT] Inclination of the Beijing-1 = 98.8\u00ba"]
-[3.850648880004883, 4.525606632232666, "[TT] Slew Count of the RADARSAT-2 = 620"]
-[5.314253330230713, 2.239259719848633, "[FF] Mission of the CEDEX Payload = GIOVE-A"]
-[5.42042350769043, 0.41489487886428833, "[TT] Mast Deployment Date of the NuSTAR = June 21, 2012"]
-[8.362849235534668, 7.350255489349365, "[TT] Type of the CMOS Imager = CMOS"]
-[5.92016077041626, 5.727657794952393, "[FF] Supported Navigation Signals of the Signal Generator Subsystem = E5, E6, and L1-bands"]
-[8.031000137329102, 1.132692575454712, "[TT] Forecast of the La Ni\u00f1a = To persist through at least the end of 2020"]
-[8.79502010345459, 2.230912208557129, "[TT] Altitude Range of the Earth\u2019s ionosphere = 50 to 400 miles"]
-[7.414700508117676, 3.901437520980835, "[FF] Activation of the PEPPOD = Command from the GAUSS team ground station"]
-[9.64875602722168, 4.306705474853516, "[FF] ADCS System of the DeorbitSail = Second use of CubeSense after STRaND-1"]
-[4.9542741775512695, 3.359706401824951, "[TT] Manufacturer of the ERNO-Box = Astrium Space Transportation in Germany"]
-[7.889835357666016, 1.9330990314483643, "[FF] Deorbiting Operation of the GOCE = Ongoing"]
-[9.129717826843262, 6.506369590759277, "[TT] Slew Angles of the TeLEOS-1 Imager = Up to \u00b145\u00ba from nadir"]
-[4.750184535980225, 5.790199279785156, "[FF] Packet Periodicity Change of the Stensat Beacon = Observed"]
-[8.301573753356934, 6.437342166900635, "[TT] Maximum Range of the CCRR = 70 m"]
-[9.185093879699707, 7.699653625488281, "[TT] Spatial Resolution of the LWIR Cameras = 348 m"]
-[8.263736724853516, 2.2483654022216797, "[TT] Data Output of the Microwave Imager (MWI) = Ocean Surface Vector Winds (OSVW), Tropical Cyclone Intensity (TCI) and additional EDRs"]
-[5.892168045043945, 3.5717897415161133, "[FF] Goal of the Neosat program = Build a European supply chain which optimizes costs and guarantees on-time delivery of satellites"]
-[6.241728782653809, 0.9329568147659302, "[TT] Launch Date of the Observatory = July 2009"]
-[9.41047191619873, 4.797330379486084, "[TT] Coarse Attitude Knowledge of the MightySAT I = \u00b15\u00ba"]
-[5.357524394989014, 6.288266181945801, "[TT] Module size of the SDR-SMM = 200 x 243.5 mm"]
-[7.016990661621094, 1.9100027084350586, "[FF] Image Credit of the Kepler Mission = NASA"]
-[4.409012317657471, 7.274994850158691, "[TT] Frequencies of the Low Noise Amplifier = L1 and L2"]
-[4.500316143035889, -0.9458044171333313, "[TT] Capture Date of the Dragon = 8 December"]
-[5.525536060333252, 6.128541469573975, "[TT] Non-volatile Memory of the Frame Grabber = Sufficient on-board non-volatile storage"]
-[5.25263786315918, 1.9243606328964233, "[TT] Mission Status of the Rosetta = Active"]
-[8.000923156738281, 6.5250115394592285, "[TT] Detection Method of the Radio Emissions = Juno Waves instrument"]
-[4.924759387969971, 8.307699203491211, "[FF] Frequency of the SSMIS = 85 GHz was changed to 91 GHz"]
-[9.880525588989258, 6.4624433517456055, "[TT] Thermal Operating Range of the Earth Radiation Budget Experiment (ERBE) = 38\u00b10.1\u00baC (detectors)"]
-[14.23842716217041, 3.3057219982147217, "[TT] Mass of the MSI-0 and MSI-1 = 3 kg"]
-[3.6774144172668457, 4.809536457061768, "[TT] Imaging Frequency of the RADARSAT-1 = C-band at 5.3 GHz"]
-[5.445389747619629, 0.6218477487564087, "[TT] Launch Date of the AgilSpace GeoPortal = May 31, 2016"]
-[10.911653518676758, 7.50802755355835, "[TT] Swath Width of the Swath width = 50 km"]
-[6.106536388397217, 6.918247222900391, "[TT] Height Data Echo Rate of the GEOSAT = 10 Hz"]
-[8.622730255126953, 7.978715419769287, "[TT] Spectral Pixel Size after Binning (x5) of the ISRF = 140 \u00b5m"]
-[4.575279712677002, 1.640912652015686, "[TT] Mission Update Date of the GovSat-1 = 31 Jan. 2018"]
-[5.2353668212890625, 5.990749359130859, "[TT] Data Processing of the FPGA = Spacewire packets"]
-[1.3232780694961548, 1.8994832038879395, "[TT] Total Cargo Mass of the HTV-5 = 6,057 kg"]
-[4.590800762176514, 6.759969234466553, "[FF] Network of the KSAT = S-band uplink and X-band downlink"]
-[7.952988147735596, 9.11458683013916, "[TT] Wavelength of the ATLAS = 532 nm"]
-[3.3877861499786377, 1.4674088954925537, "[TT] Liftoff Date of the Sentinel-1B = 22 April"]
-[7.027194023132324, 7.265665054321289, "[TT] Efficiency of the ATLAS lasers systems = >5%"]
-[13.091670989990234, 5.380814075469971, "[TT] Solar Array Rotation of the AlSat-2A = ~ 0.025 \u00ba/s rotation about its \u2013X-axis"]
-[4.766167640686035, -1.4203499555587769, "[TT] Launch Date of the Tianwen-1 = July 23, 2020"]
-[5.591190814971924, 7.891086101531982, "[TT] Precession Frequency of the OVM = 0.8 - 3 kHz"]
-[11.422018051147461, 4.322731971740723, "[TT] Size of the Astrocast-0.1 = 3U"]
-[4.730539321899414, 2.226694345474243, "[TT] Launch Date of the Eutelsat Quantum = 2nd half of 2020"]
-[14.324222564697266, 3.180140495300293, "[TT] Mass of the SSRNI = 9 kg"]
-[11.856115341186523, -0.0412849523127079, "[TT] Maximum Distance to Stars of the TESS = 300 light-years"]
-[5.908447742462158, 4.550512313842773, "[FF] Feature of the Self-organizing network approach = Automatically make use of ground stations or other satellites when available to reach a given target"]
-[6.2666335105896, 4.487842559814453, "[FF] Responsibilities of the SSDC = Science data processing, managing, archiving, permanent preservation and distribution of data"]
-[5.289889335632324, 4.085093021392822, "[FF] Primary Missions of the MEOSAR = Global Navigation Satellite Systems (GPS, Galileo and GLONASS)"]
-[10.97632884979248, 5.093016624450684, "[TT] Sensor #2 Radius of the OPSE = 52 mm"]
-[6.913806915283203, 7.764047145843506, "[TT] Main Reflector Diameter of the MBA = 2.4 m"]
-[10.279641151428223, 3.941617012023926, "[FF] Objective of the SMARD = Demonstration of a new class of low-shock release devices"]
-[7.480892181396484, 6.590247631072998, "[TT] Full Energy and Azimuthal Coverage Time of the Instrument = 100 seconds"]
-[9.184699058532715, 4.916298866271973, "[FF] Function of the PADS = Performs precision attitude determination"]
-[8.108689308166504, 2.954590320587158, "[FF] Completion Date of the Geostationary Lightning Mapper (GLM) = Oct. 9, 2014"]
-[7.002368450164795, 0.22348009049892426, "[TT] Maneuver Time ahead of CALIPSO of the CloudSat = 15 s"]
-[6.0760087966918945, 4.146329402923584, "[FF] Technology of the Radiating Board = Based on the same technology developed in the frame of CSK"]
-[7.61362886428833, 2.3796606063842773, "[FF] Location of the South Atlantic Anomaly = Over South America and the southern Atlantic Ocean"]
-[6.105497360229492, 4.125520706176758, "[TT] Information Representation of the COSMOS Software = JavaScript Object Notation (JSON)"]
-[6.026333808898926, 1.8494477272033691, "[FF] On-Orbit Performance and Application of the HJ-1A and HJ-1B = Proceedings of the 60th IAC (International Astronautical Congress), Daejeon, Korea, Oct. 12-16, 2009"]
-[7.441023349761963, 2.3070595264434814, "[FF] Data of the MODIS = NDVI anomaly: it contrasts vegetation health from March 29 to April 5, 2016, against the long-term average from 2000\u20132015"]
-[12.796835899353027, 7.603936195373535, "[TT] Operational Power Consumption of the MIS Instrument = 357 W"]
-[4.747664451599121, -1.8210885524749756, "[TT] Landing Date of the Chang'e-5 = 1 December 2020"]
-[4.879811763763428, 3.2640910148620605, "[TT] Manufacturer of the AATSR = Astrium Ltd., UK"]
-[11.153986930847168, 5.102117538452148, "[TT] Elastic Modulus of the LARES-2 = > 200 GPa"]
-[11.8440580368042, 3.304569721221924, "[TT] Isp of the Chemical propulsion engine = ~ 200 s"]
-[8.837839126586914, 3.365187406539917, "[FF] Purpose of the NANOhpm = Probe phenomenon by performing satnav fixes in the midst of the ionosphere"]
-[4.2981133460998535, 7.40857458114624, "[TT] TT&C Communication Frequency of the SCD-2 = S-band"]
-[14.271904945373535, 3.155263662338257, "[TT] Mass of the PROITERES-2 = 50 kg"]
-[6.08784818649292, 0.45243969559669495, "[TT] TLE Availability of the ASTERIA = Within 12 hours of deployment"]
-[3.3480896949768066, 1.4629976749420166, "[TT] Launch Date of the Sentinel-3B = 25 April 2018"]
-[8.967326164245605, 5.37090539932251, "[TT] Agility of the SPOT-6 & SPOT-7 = Pitch and roll forward, backwards and sideways by 45\u00b0"]
-[13.250954627990723, 5.243307590484619, "[TT] Total Array Area of the Solar Panels = 9.5 m2"]
-[14.622525215148926, 6.666019916534424, "[TT] Battery Quantity of the HTV = 6"]
-[5.755307674407959, 1.430957555770874, "[FF] Mission Start Date of the Eu:CROPIS = May 24, 2016"]
-[5.243576526641846, 1.564218521118164, "[TT] Dataset Use of the ALOS/ Daichi = No charge"]
-[6.44494104385376, -0.3960767090320587, "[TT] Period of the ALOS-3 = 98 minutes"]
-[13.230310440063477, 7.327723503112793, "[TT] Power of the TANSO-CAI = 100 W"]
-[13.416648864746094, 6.806130886077881, "[TT] Power Generation of the Spacecraft = 450 W @ EOL"]
-[11.48561954498291, 6.565186500549316, "[TT] Measurement Range of the Particle Detector = Proton : 1.5 MeV ~ 250 MeV"]
-[4.9394941329956055, 7.39396858215332, "[TT] S-band TxRx Data Rate (TC) of the RF communications = 64 kbit/s"]
-[7.869997024536133, 6.645432949066162, "[TT] Revisit Time for CCD Camera of the Satellite = Seven days"]
-[4.970776081085205, 0.4875531792640686, "[FF] Article Date of the CXO = 14 February 2019"]
-[14.235024452209473, 3.23930025100708, "[TT] Mass of the PLC = 5 kg"]
-[3.861100196838379, 6.558349132537842, "[TT] HPBW AZ of the Antenna = 33\u00ba"]
-[9.669588088989258, -1.495764136314392, "[TT] True Anomaly of the SMART-1 = 180.000\u00ba"]
-[6.834695816040039, 1.8044484853744507, "[FF] URL of the Dellingr = https://www.nasa.gov/sites/default/files/atoms/files/cuttingedge_-_vol._13_issue_1_-_fall_2016.pdf"]
-[7.188528060913086, 5.184343338012695, "[FF] Across-Track Slope of the ATM = Calculated"]
-[7.6252121925354, 6.517723083496094, "[TT] Relative Accuracy of the Instrument = Better than 1% for 45 s counting time on IP signal"]
-[7.304171085357666, 9.048986434936523, "[TT] NBF (Narrow Band Filter) Spectral Width of the GLM = ~1 nm FWHM"]
-[4.859385967254639, 2.5272228717803955, "[TT] Prime Contractor of the G\u00f6kt\u00fcrk-1 = Telespazio of Italy"]
-[9.352649688720703, 7.09343147277832, "[TT] Spatial Resolution (MS) of the PP = 10 m"]
-[5.775635719299316, -0.856593132019043, "[TT] Design Life of the Resurs-DK1 = 3 years"]
-[9.993894577026367, 2.497631072998047, "[TT] Number of X-ray Sky Fields Observed of the HaloSat = 334"]
-[7.9580230712890625, 6.29791259765625, "[TT] Instrument type of the MVIRI = Imaging multi-spectral radiometers (vis/IR)"]
-[5.280472278594971, 2.8623695373535156, "[TT] Test Location of the EMC Testing = Anechoic chamber either at USSC or SSTL premises"]
-[7.893531322479248, 7.326552867889404, "[TT] Data Rate of the Imager = 7.7 Mbit/s"]
-[3.3200483322143555, 5.0207905769348145, "[FF] Antenna Beam Pointing of the RISAT-SAR = Switches electronically in the elevation direction"]
-[13.262272834777832, 5.242940425872803, "[TT] Total Geometrical Area of Solar Arrays of the CHEOPS = About 2.7 m2"]
-[5.5697126388549805, 5.668040752410889, "[TT] Processor of the OBDH subsystem = Mil-883 68332"]
-[9.231520652770996, 6.933084487915039, "[TT] Image Resolution of the Gen-2 satellites = 1-meter"]
-[8.680315971374512, 4.102737903594971, "[FF] Focal Plane Detectors of the SIM = Three separate photodiode detectors for rapid scan solar measurements and an Electrical Substitution Radiometer (ESR) for long-term SSI calibration maintenance"]
-[4.818207263946533, 0.5160518884658813, "[TT] Launch Date of the FORUM = 2026"]
-[5.416701793670654, 6.027675151824951, "[TT] Processing Power of the OBC = 9 DMIPS/MHz (peak, 4 Cortex A53)"]
-[6.111245155334473, 4.1243133544921875, "[TT] User Interface of the COSMOS Software = Web framework"]
-[9.388118743896484, -1.7086594104766846, "[TT] Total Maneuvering Mass of the Swarm-A = Approximately 80 g"]
-[11.776350021362305, 0.09133090823888779, "[FF] Transiting Exoplanet Survey Satellite of the TESS = Upcoming"]
-[9.05471420288086, 8.681851387023926, "[TT] Imaging Dual-Band Photometry Field of View of the PACS = 1.75 arcmin x 3.50 arcmin"]
-[9.853437423706055, -1.1996448040008545, "[TT] Side to Side of the S-193 = 48\u00ba"]
-[8.676702499389648, 4.792923927307129, "[TT] Technology of the Procyon star tracker = Active Pixel Sensor (APS)"]
-[9.661572456359863, 8.357270240783691, "[TT] Field of View of the FGS = \u00b13 arcmin"]
-[9.236312866210938, 0.21866248548030853, "[TT] Width of the Pas Moraine = Up to 12 miles (20 km)"]
-[8.50866413116455, 8.826215744018555, "[TT] Observation Wavelengths of the Herschel = Far-infrared and sub-millimeter"]
-[12.00096321105957, 4.690225124359131, "[TT] Body Dimensions of the ADEOS = Approx. 4 m x 4 m x 5 m"]
-[5.187878608703613, 2.618678569793701, "[TT] Mission Lead of the SPARCS = Arizona State University"]
-[6.016579627990723, 5.931943416595459, "[TT] Data/Pilot of the E6-B = Data"]
-[3.5856587886810303, -0.8511546850204468, "[FF] Apogee Alignment of the Satellites = HEOs at local midnight over North America in the winter"]
-[8.572826385498047, 5.382842540740967, "[TT] Velocity Accuracy of the Orbit Knowledge = 0.15 m/s"]
-[6.710803508758545, 3.621260404586792, "[FF] Data Source of the IMERG = Integrated Multi-Satellite Retrievals for GPM (IMERG)"]
-[5.143442630767822, 1.9989479780197144, "[TT] Mission Status of the GRIFEX = Operational"]
-[6.48392391204834, -0.12222858518362045, "[FF] Service Life of the Cooling Systems = Wore out in 2017"]
-[6.588953495025635, -2.0350096225738525, "[FF] Project Status Meeting Date of the Jason-1 = Oct. 18-20, 2010"]
-[11.55601692199707, 4.646338939666748, "[TT] PCB Size of the CubeSense = PC104-sized"]
-[4.629307270050049, 0.5649026036262512, "[FF] Renaming Date of the GOES-T = After launch"]
-[5.008823394775391, 0.6107274889945984, "[FF] Press Kit Date of the Global Precjson Measurement = Feb. 27, 2014"]
-[6.457262992858887, -0.2641131579875946, "[TT] Average Period Between Out-of-Plane Orbit Manoeuvres of the ALOS-2 = 176 days"]
-[9.859503746032715, 6.556396484375, "[TT] Deployment Time of the Secondary Mirror Support Structure = Approximately 1 hour and 36 minutes"]
-[6.310971260070801, -0.11520194262266159, "[TT] Maximum Sustained Event Rate of the ISS-LIS = 300 events/s"]
-[8.987796783447266, 8.136468887329102, "[TT] IFOV/line (pixels/scan line) of the MWRI = 240"]
-[4.424086093902588, 7.512402534484863, "[FF] Type of the VHF/UHF uplink and downlink = Redundancy"]
-[6.2569499015808105, -0.06820616126060486, "[TT] Constellation Deployment Timeframe of the Satellite Constellation = Over the course of 24 months"]
-[7.956945419311523, 7.251649379730225, "[TT] Detection Efficiency of the Imager = > 90% of total events"]
-[3.9022727012634277, 6.539927005767822, "[FF] Antenna Type of the AISSat-1 = VHF monopole payload antenna"]
-[11.545465469360352, 2.7663636207580566, "[TT] Launch Mass of the GaoJing / SuperView minisatellites = 560 kg"]
-[4.694570541381836, 7.276327133178711, "[FF] Downlink of the Communication Subsystem = Ku-band transmitter at 10 Mbit/s, BPSK modulation, 0.2 W output"]
-[5.52988338470459, 0.17071470618247986, "[TT] Operation Period of the SAM-II = 1978 to 1995"]
-[4.974281311035156, 0.7984088063240051, "[FF] Development Status of the MULA = In progress"]
-[7.686085224151611, 1.8670161962509155, "[FF] Data Applications of the BeaverCube = Improving the understanding of regional biological productivity and the effects of extreme weather events"]
-[8.11814022064209, 8.731331825256348, "[TT] Spectral Range of the UV to NIR = Ultraviolet (340 nm) to near-infrared (890 nm)"]
-[3.375572443008423, 1.8496251106262207, "[TT] Orbital Phase of the Sentinel-1A and Sentinel-1B = 180\u00ba"]
-[9.414112091064453, 5.03216028213501, "[TT] Attitude Stabilization Time of the GF-2 spacecraft = Within 150 s"]
-[8.88730239868164, 3.2680459022521973, "[FF] Purpose of the STIS = Measures solar energetic particles and provide advance warning if a shock wave produced by those particles is headed for Earth"]
-[8.681729316711426, 4.71122932434082, "[FF] Observation Modes of the TanSat = Nadir mode, Sun-glint mode, Sun glint track, Principle plane track, Target mode, Surface target track, Multi angles for one target"]
-[16.49755096435547, 3.583733558654785, "[TT] Launch Date of the OneWeb = 14th of October"]
-[9.605722427368164, 7.837189197540283, "[TT] Field of View of the OMPS Limb Profiler = 8.5\u00b0"]
-[9.98525619506836, 7.841978073120117, "[TT] Collimation Procedure of the Telescope = Can be performed at any time during the mission"]
-[10.838383674621582, 5.480217456817627, "[TT] Emission Energy of the CuPID = 40.8 eV"]
-[10.12193489074707, 3.218143939971924, "[FF] Transmission Type of the AISat = From space"]
-[10.939072608947754, 7.620009899139404, "[FF] Swath width of the MWTS = "]
-[4.471388339996338, 7.763619899749756, "[TT] Uplink Data Rate of the L-3 Communications Cadet UHF nanosatellite radio = 16 kbit/s with FEC (Forward Error Correction)"]
-[6.979540824890137, 4.281554222106934, "[FF] Unknown of the AIDA = Unknown"]
-[9.011608123779297, 0.5577284097671509, "[FF] Radiation Effects of the THEMIS (and ARTEMIS) spacecraft = No permanent effects, occasional resets due to Single Event Upsets"]
-[6.526574611663818, -0.5292727947235107, "[TT] Science Phase Duration of the EQUULEUS = At least 180 days"]
-[12.0459623336792, 6.29237699508667, "[FF] Antiproton to proton ratio of the AMS = Measured"]
-[8.068180084228516, 4.806972026824951, "[FF] Duration of the Calibration Phases = Not specified"]
-[10.701515197753906, 7.361340522766113, "[TT] Swath Width of the Sensor = 72.4 km"]
-[7.114816665649414, -0.18938474357128143, "[TT] Number of Deployment Orbits of the STP-2 = Three"]
-[7.570110321044922, 2.8048408031463623, "[TT] Measurement Frequency of the Global Oil Storage Monitoring = Weekly"]
-[6.063185214996338, -1.9482887983322144, "[TT] Member of the Ana Barros = True"]
-[11.049376487731934, 6.178714275360107, "[TT] Material of the PO = Radiation resistant glasses"]
-[6.947275638580322, 4.3809380531311035, "[FF] Unknown of the IXV = Unknown"]
-[6.972588062286377, 6.1513752937316895, "[TT] Quantity of the GARI-1 = Two identical GAGG instruments"]
-[5.681262493133545, 2.3601677417755127, "[FF] Project Leadership of the ABEX = Team of graduate students"]
-[7.384464263916016, 3.662367105484009, "[TT] Number of Soundings of the GNOS-2 = 1000 per day"]
-[4.304614543914795, 2.746720552444458, "[TT] Launch Location of the Orbital ATK = Wallops Flight Facility in Virginia"]
-[9.848878860473633, -0.5850783586502075, "[TT] Orbit Altitude of the SAR/Glonass Glonass-K1 No 1 = 19,000 km"]
-[10.301774024963379, 4.445036888122559, "[TT] Momentum Wheels of the NigeriaSat-2 = 4 Microwheel 10SP"]
-[10.259127616882324, 4.545155048370361, "[TT] Maximum Speed of the Reaction Wheels = 3,400 RPM"]
-[8.131603240966797, 3.126518726348877, "[FF] Spectral Filtering of the GLM = Using a narrowband interference filter centered on a strong optical emission line (e.g., OI at 777.4 nm) in the lightning spectrum"]
-[8.787030220031738, 1.9616858959197998, "[TT] Wind Speed of the SAR = 2-15 m/s"]
-[5.235963821411133, 4.097140789031982, "[TT] Number of orbital planes of the GPS-DASS = 3"]
-[6.27979040145874, 4.472073554992676, "[FF] Development Date of the On-board Space Computer Systems = Jan. 1976"]
-[8.793930053710938, 2.121981382369995, "[TT] Amplifier Output of the WINDS = Approximately 280 W"]
-[4.982299327850342, 0.11000160127878189, "[TT] End of Life Date of the TRACE = 21 June 2010"]
-[10.127821922302246, 2.970052719116211, "[TT] Operation Duration of the QB50 CubeSat Constellation = 3 months"]
-[13.615762710571289, 1.7285703420639038, "[TT] Pressurized Cargo Bay Mass of the Dragon Resupply Vehicle = 1530 kg"]
-[7.805065155029297, 8.644083976745605, "[TT] Spectral Bands of the CAPI = Ultraviolet: 0.38 \u00b5m, Visible: 0.67 \u00b5m, Near infrared: 0.87, 1.375 and 1.64 \u00b5m"]
-[12.236737251281738, 3.4479763507843018, "[TT] Propellant Tank Capacity of the Cold Gas System = 132 l"]
-[10.592251777648926, 3.9384539127349854, "[FF] Components of the Dragsail = Deployer, extension mechanism"]
-[4.676243782043457, 6.638862133026123, "[TT] Required Processing System of the UHRIT = Processing system including DVB-S2 equipment"]
-[9.697279930114746, 7.970592975616455, "[FF] Data Collection of the CuPID = Within the cusp"]
-[8.708757400512695, 3.6786327362060547, "[FF] Function of the 782 nm Band = Same \u03bb as SODISM to link diameter and solar irradiance variability"]
-[5.024609565734863, 3.857189416885376, "[TT] Navigation Receiver Manufacturer of the WSF-M = RUAG Space"]
-[4.363733768463135, 7.787563800811768, "[TT] Modulation Index of the DCP = 60o"]
-[6.931642055511475, 5.212512016296387, "[FF] Components of the PMS = TPM (Thermal & Power Module), MCM (Mass storage and Control Module)"]
-[4.004741191864014, 4.829895973205566, "[TT] Radiometric Balance of the RISAT-1 = Within \u00b1 0.5 dB"]
-[4.852975845336914, 0.8376550078392029, "[FF] Adventure Start Date of the TeLEOS-1 = Feb. 6, 2014"]
-[4.700242519378662, 5.656772136688232, "[TT] Doppler Shift of the AIS System = - 4 kHz to + 4 kHz"]
-[13.89407730102539, 2.6786739826202393, "[TT] Launch Mass of the Ascent Vehicle = Roughly 500 kg"]
-[10.8942232131958, 3.9088897705078125, "[TT] Formation Ranges of the CanX-5 = 50 m"]
-[6.294753074645996, 3.959929943084717, "[FF] Ground Segment Ownership of the Helios-2 = Belgium, Spain, Italy, Greece, Germany"]
-[6.445775508880615, 3.246649742126465, "[TT] Constellation of Imaging Satellites of the BlackSky = 6 currently, 12 by year\u2019s end"]
-[11.285981178283691, 4.7512102127075195, "[TT] Size of the Sun Sensor Device = 3 cm x 3 cm x 1.2 cm"]
-[12.106829643249512, 1.9631584882736206, "[TT] Revisit Time with Orbital Manoeuvres of the Cartosat-2E = One day"]
-[7.682012557983398, -0.8697832226753235, "[FF] Imaging Period of the ICESat-2/Sentinel-2 = Contemporary"]
-[11.793367385864258, 3.3280656337738037, "[TT] Thrust of the Propulsion System = 0.3 N"]
-[13.363598823547363, 2.9027726650238037, "[TT] Mass of the HawaiiSat-1 = 40 kg"]
-[8.865850448608398, 3.3070003986358643, "[FF] Position of the WFI Mosaic Plate Assembly = Much farther outboard towards the anti-sun side of the Observatory"]
-[12.059268951416016, 4.3348493576049805, "[TT] Quantity of the SpaceBEE = 12"]
-[4.394401550292969, 5.430139541625977, "[TT] Development Start Date of the GOMX-3 = June 2014"]
-[8.053213119506836, 0.7163662314414978, "[FF] Data Output of the GRACE-FO = Time-varying maps of the distribution of water at three depths: surface soil moisture, root zone soil moisture, and shallow groundwater"]
-[10.106714248657227, 1.023687720298767, "[TT] Distance from Earth of the Carina Nebula = 7500 light-years"]
-[4.62827730178833, 7.196778774261475, "[TT] RF Communications of the IRIS = X-band for payload downlink at 15 Mbit/s"]
-[7.820265769958496, 8.466212272644043, "[FF] Bands of the Advanced Spaceborne Thermal Emission and Reflection Radiometer (ASTER) = 4-2-1"]
-[7.471734523773193, 1.2894519567489624, "[FF] Commercial Users of the SeaSat = 15 companies"]
-[7.332571029663086, 7.9910173416137695, "[TT] Signal-to-Noise Ratio of the Satellite = > 720 @ 320 nm"]
-[3.418715000152588, 1.9748172760009766, "[FF] Operation of the Sentinel-6 = Fly in tandem with the Jason-3 spacecraft"]
-[10.310922622680664, 2.1051714420318604, "[FF] Purpose of the Integral = Observing particles thrown off by extreme phenomena such as black holes, neutron stars, and supernova explosions"]
-[7.747439861297607, 6.121329307556152, "[TT] Instrument Type of the ACE-FTS = Compact high performance instrument"]
-[9.72684383392334, 8.974801063537598, "[TT] Band-to-Band Alignment of the IRIS Instrument = 0.1 pixels"]
-[6.259097099304199, 2.035151481628418, "[FF] Main Port Mechanism of the PRISMA = Unknown"]
-[8.176655769348145, -0.7481356263160706, "[FF] Additional Capability of the SMOS = Map the extent and thickness of sea ice"]
-[4.134898662567139, 1.375489354133606, "[TT] Data Distribution Start Date of the Meteosat-8 = 4 October"]
-[3.4300787448883057, 5.003087043762207, "[TT] Operation Time of the SAR instrument = 10 minutes per orbit"]
-[9.489753723144531, 3.916532278060913, "[TT] Function of the GMAG = Measures magnetic field variations"]
-[5.478957176208496, 3.1890645027160645, "[FF] Platform of the ASNARO = NEXTAR"]
-[10.326333999633789, 5.589001178741455, "[TT] Cooling Power of the Cooler = 5.14 W at 183.1 K"]
-[8.43393325805664, 1.8866723775863647, "[TT] Roundtrip Time to Match Outer OceanSat-2 Angle of the RapidScat = 4.7 ms"]
-[9.686189651489258, 8.254096984863281, "[TT] Accelerators of the NMS and IMS = Two-aperture ion optic lenses"]
-[10.002564430236816, -1.317698359489441, "[TT] Orbital Position of the Meteosat-11 = 0 \u00ba"]
-[5.156374454498291, 2.7503771781921387, "[TT] Affiliation of the ETP = National Central University"]
-[7.60727071762085, 8.017020225524902, "[TT] Sensitivity of the IMI = 0.1~0.2 K 0.3~0.5 K 0.5 dB"]
-[8.5298433303833, 3.5993382930755615, "[FF] Observation of the ILAS-II = Provides information on the altitude distribution of the light-absorbing substances"]
-[8.174418449401855, 3.9958488941192627, "[FF] Trajectory Phases of the EQUULEUS = Science phase, forward transfer phase, backward transfer phase"]
-[5.856690406799316, 1.3831604719161987, "[TT] Launch Date of the IXPE observatory = 2021"]
-[4.014518737792969, 2.0916175842285156, "[TT] Launch Control of the ORS-6 = Not co-lead"]
-[6.432101726531982, 1.4114748239517212, "[TT] Launch Dates of the COSMO-SkyMed = 2007, 2008, 2010"]
-[5.016269683837891, 8.109635353088379, "[TT] Operation Frequency of the Aquarius = 1.41 GHz"]
-[6.505720615386963, -0.0785454511642456, "[TT] Receiver Operation of the ColAIS = Alternating, switching every three months"]
-[4.553244590759277, 2.9334475994110107, "[TT] Location of the Ganges Delta = Bangladesh and the State of West Bengal in India"]
-[7.178863525390625, 6.583930492401123, "[TT] Threshold Control of the GLM = Pixel-by-pixel basis"]
-[5.2559590339660645, 7.041370868682861, "[TT] Downlink Data Rate of the TT&C Communications = Up to 8 kbit/s"]
-[3.3127987384796143, 5.039249420166016, "[FF] Polarization Channel Transition of the SAR Processor = When a transition from quad to single pol (or inversely) happens, the length of the single polarization channel will be increased at the cost of a reduced swath width"]
-[10.374625205993652, 7.9473137855529785, "[TT] Dimensions of the Telescope = 37 x 37 x 188 cm"]
-[5.497269153594971, 2.7444541454315186, "[TT] Led by of the Space component = ESA (European Space Agency)"]
-[10.838906288146973, 7.489485263824463, "[TT] Swath of the SLSTR = 1420 km"]
-[8.989498138427734, 6.494812965393066, "[TT] Time Resolution of the IMAP = Six-month timescales"]
-[10.770597457885742, 7.45255184173584, "[TT] Ground Swath of the AEISS-A = Around 12 km"]
-[10.352021217346191, 5.780477046966553, "[TT] Device Operating Temperature of the Gaia = 130 K"]
-[6.166866302490234, 5.99604606628418, "[TT] Number of T/R modules controlled of the TCU = 24"]
-[6.958302021026611, 5.91359806060791, "[FF] Onboard clock synchronization of the Network Time Protocol (NTP) = Yes"]
-[9.514359474182129, 8.337817192077637, "[TT] Optics Focal Length of the Spectral bands = 2896 mm"]
-[9.451658248901367, 1.2402499914169312, "[TT] Drift Velocity of the DSAT#2 = 2 cm/s"]
-[8.901708602905273, 7.253034591674805, "[TT] MS Camera of the Payload = B1:0.45~0.52 \u00b5m, B2: 0.52~0.59 \u00b5m, B3: 0.63~0.69 \u00b5m, B4: 0.77 ~0.89 \u00b5m"]
-[6.349192142486572, 3.3304901123046875, "[TT] Constellation Expansion of the BlackSky = From 12 to 14 high-resolution satellites"]
-[4.105742454528809, 7.197066307067871, "[TT] Frequency Band of the X-band = EESS X-band"]
-[12.727407455444336, 3.8976995944976807, "[FF] Science Objectives of the CuPID = Determine the cross- or macroscale spatial and temporal properties of magnetic reconnection"]
-[7.243730545043945, 3.4490561485290527, "[FF] Focus of the Astroscale = Developing technologies to service satellites and remove orbital debris"]
-[10.53508186340332, 6.067593097686768, "[FF] Camera Assemblies of the eROSITA = Unknown"]
-[10.394012451171875, 4.556177139282227, "[TT] Quantity of the Reaction Wheel = 4 in hot redundancy"]
-[6.612781524658203, 3.5339879989624023, "[FF] Designer/Developer of the PROBA = Verhaert Design and Development N. V."]
-[7.185848236083984, 3.0811846256256104, "[FF] Unknown of the GeoSTAR-III = Unknown"]
-[5.651808738708496, -2.043339252471924, "[FF] Geolocation Accuracy Evaluation Date of the KOMPSAT-3 = May 4-8, 2015"]
-[5.975159645080566, 0.8332023620605469, "[FF] Image Capture Date of the MarCO = 22 October 2018"]
-[4.5398383140563965, 1.364546537399292, "[FF] Quantity of the AlSat-2 = 2"]
-[5.827306270599365, 2.185856342315674, "[FF] Mission Status of the Satellite = Unknown"]
-[9.060441970825195, 5.127084255218506, "[FF] Measurement Frequency of the Gyro = High-frequency"]
-[9.121935844421387, 6.392297744750977, "[TT] Parallelism of the Optical Window = \u22645 arcsec"]
-[6.499306678771973, 5.681519031524658, "[TT] Number of Boards of the PEB (Payload Electronics Box) = 7"]
-[8.938121795654297, 4.4919819831848145, "[TT] Mission Constraints of the RVX = Sun pointing attitude and Sun-aligned configuration"]
-[13.385641098022461, 7.29895544052124, "[TT] Power of the ISEE-1 = 175 W"]
-[7.922730922698975, 3.1657488346099854, "[FF] Measurement of the GeoCARB = Total concentration of carbon dioxide, methane and carbon monoxide in the atmosphere"]
-[8.977363586425781, 4.816625595092773, "[TT] Quantity of the Horizon sensor = 1"]
-[8.329883575439453, 0.42011260986328125, "[TT] Elevation of the Lake Powell = 1074 m above sea level"]
-[11.536981582641602, 4.692282676696777, "[TT] Diameter of the Dimorphos = 160 meters"]
-[7.394436359405518, 4.557866096496582, "[FF] Configuration of the AMS-02 = PM configuration is technically simpler to operate with respect to the SCM one"]
-[6.932462215423584, 2.404620409011841, "[TT] Mission Type of the Aditya-L1 = Study the Sun"]
-[3.316650152206421, 4.927192211151123, "[FF] Description of the Staggered SAR = Employs multiple elevation beams to map a wide image swath with high resolution"]
-[13.753153800964355, 3.6724109649658203, "[TT] Mass of the SAR Antenna = 547.7 kg"]
-[13.182409286499023, 7.272658348083496, "[TT] Power Consumption of the RCU = < 3 W"]
-[9.732453346252441, 8.443962097167969, "[TT] FOV (Field of View) of the Instrument = 3.0 \u00ba"]
-[7.972560405731201, 7.30886697769165, "[TT] Dynamic Range of the Target Sensor = Six orders of magnitude"]
-[5.851868629455566, -2.2368762493133545, "[TT] Inclination of the KOMPSAT-3A = 97.513\u00ba"]
-[4.4966583251953125, 5.631693363189697, "[TT] SAR Events of the 406 MHz beacons = Approximately 6,200"]
-[4.369731903076172, 2.306854248046875, "[FF] Image Distribution of the DubaiSat-1 = To government agencies, educational institutions, and commercial use"]
-[4.388597011566162, 1.7541968822479248, "[TT] Decommissioned Date of the SARSAT-1 = Dec. 1985"]
-[9.645862579345703, 7.036980152130127, "[TT] Spatial Resolution of the NOAA/AVHRR-2 = 1.1 km LAC, 4.0 km GAC"]
-[8.239837646484375, 8.842057228088379, "[TT] Spectral Sampling of the Ma_MISS = About 20\u2009nm"]
-[8.975248336791992, -0.7486857175827026, "[FF] Orbit of the P3RVX = Highly elliptical"]
-[10.185874938964844, 3.181705951690674, "[FF] Names of the CubeSats = MySat-1 and the second CHEFSat satellite"]
-[5.28898286819458, 4.04036808013916, "[TT] Table Entries of the Inter-satellite Antenna = 1440"]
-[4.5730881690979, 3.0464580059051514, "[TT] Location of the FOS = ESOC in Darmstadt"]
-[5.743078231811523, 2.0575428009033203, "[FF] Mission Status of the LightSail 2 = Unknown"]
-[8.415882110595703, 7.39346170425415, "[TT] Imaging Bands of the DMAC = One panchromatic and four multispectral (MS)"]
-[5.1093854904174805, 5.241275787353516, "[TT] Tracking of the Topstar GPS receiver = Dual-frequency"]
-[12.133904457092285, 2.9866678714752197, "[TT] Propulsion of the Schiaparelli = 3 clusters of 3 hydrazine engines (400 N each), operated in pulse-modulation"]
-[10.248757362365723, 3.1600253582000732, "[FF] Payload of the SciSat/ACE spacecraft = Instruments provide information about more than 30 different molecular species"]
-[5.414284706115723, 0.8326982855796814, "[FF] Senior Review Date of the TRMM = 2011"]
-[9.48227596282959, 0.6066856384277344, "[TT] Velocity Before Engine Shutdown of the Schiaparelli = Nearly 270 km/h"]
-[10.630029678344727, 2.7923853397369385, "[TT] Orbital Life Goal of the Nanosatellite = 25 years"]
-[5.804905414581299, -0.7365304827690125, "[TT] Mission Life of the Telescope = 5-year minimum lifetime"]
-[9.310505867004395, 10.738938331604004, "[TT] Polarization of the ICI-11 = V, H"]
-[4.867950439453125, 3.409243106842041, "[TT] Second Low Flying Customer of the LCT = Sentinel-2A"]
-[13.892373085021973, 3.2037580013275146, "[TT] Mass of the Canadian Advanced Nanospace Experiment 2 = Three-Kilogram"]
-[9.461796760559082, -1.1751259565353394, "[FF] Use of the PistenBully = Traverse along 88 degrees south"]
-[4.98206090927124, -0.34093600511550903, "[TT] Launch Time of the Enxaneta = 7:07:12 am (CET)"]
-[5.580224514007568, 5.731838226318359, "[TT] CPU of the SCU = HD64F7145FW50"]
-[8.189461708068848, 8.378632545471191, "[TT] Spectral Range of the IRFS-2 = 5 to 15 \u00b5m"]
-[6.269552707672119, 6.100255966186523, "[TT] Sync to LOLA of the NGSLR = Yes"]
-[5.182367324829102, 2.4911160469055176, "[TT] Type of the EPIRBs = Maritime"]
-[9.315019607543945, 7.656214714050293, "[TT] Field of View of the 4-band CCD Imager = 36\u00ba, or 500 km swath width"]
-[10.298855781555176, 4.514938831329346, "[TT] Actuators of the iADCS-100 = Miniature reaction wheels"]
-[9.861215591430664, 8.140334129333496, "[TT] Focal Length of the Kowa LM16JC lens = 16mm"]
-[6.897589683532715, 5.84486722946167, "[TT] Quantity of the Perseus-M1 and M2 = 2"]
-[8.418389320373535, 4.068892002105713, "[FF] Publication Date of the The Spectral Irradiance Monitor = Aug. 2005"]
-[6.132877349853516, 3.5223517417907715, "[TT] Number of Experiments of the ORS-3 = 26"]
-[14.483694076538086, 6.593158721923828, "[FF] Battery Status of the Grace Mission = Degraded"]
-[12.176840782165527, 3.146254301071167, "[TT] Propellant Base of the GPIM = Edwards Air Force Base, CA"]
-[8.429957389831543, 8.096661567687988, "[TT] Height of the Spectral Block = 240 pixels"]
-[10.123910903930664, 0.19186575710773468, "[TT] Flight Formation of the Harmony = Approximately 200 - 500 metres apart"]
-[13.98934268951416, 2.706291675567627, "[TT] Launch Mass of the FY-2F = 1380 kg"]
-[8.220613479614258, 3.1003363132476807, "[FF] Algorithm Improvement of the OMI = OMI O2\u2013O2 operational cloud algorithm"]
-[10.876163482666016, 7.536553382873535, "[TT] Swath Width of the CAPI = 400 km"]
-[12.124603271484375, -0.19893166422843933, "[TT] Continuous Viewing Zone of the TESS = Southern continuous viewing zone"]
-[10.819302558898926, 1.0188411474227905, "[FF] Potential Mass of the White Dwarf = Similar to Jupiter"]
-[8.81580924987793, 3.4746015071868896, "[FF] Movement of the Equatorial Ionization Anomaly (EIA) = Symmetrical"]
-[6.501124382019043, -0.7998090386390686, "[TT] LTAN of the JPSS-1 = 13:30 hours \u00b110 minutes"]
-[8.372333526611328, 2.41792893409729, "[FF] Aerosol Types of the CATS = Dust, dust mixtures, smoke, marine aerosols"]
-[10.429609298706055, 2.9858291149139404, "[FF] Affiliation of the MAYA-1 = PHL-Microsat Program of the University of the Philippines Diliman"]
-[9.150298118591309, 3.7542831897735596, "[FF] Position of the SPC (Solar Probe Cup) = Extends beyond the TPS"]
-[6.3242573738098145, 1.83088219165802, "[FF] URL of the SpaceX CRS-6 = http://blogs.nasa.gov/spacex/wp-content/uploads/sites/227/2015/04/SpaceX_CRS-6_Mission_Overview.pdf"]
-[7.095362663269043, 3.2107317447662354, "[FF] System Type of the GeoSTAR = Sparse array synthetic aperture radiometry"]
-[8.239476203918457, 6.704596519470215, "[TT] Provider of the Advanced Baseline Imager = L3Harris Technologies"]
-[7.85884952545166, 9.098664283752441, "[TT] Wavelength of the ISIR = 8.5 \u00b5m"]
-[5.324150085449219, 3.307464122772217, "[TT] Instrument Manufacturer of the OSCAT-3 = ISRO"]
-[7.943958282470703, 9.110568046569824, "[TT] Wavelength of the ADEOS/TOMS = 308.68 nm"]
-[6.039943695068359, -0.35655561089515686, "[TT] Normal Operations Duration of the SELENE/Kaguya = 10 months"]
-[9.709333419799805, -0.6375638246536255, "[TT] Altitude of the Orbit = ~1075 km x 1089 km"]
-[5.208819389343262, 6.001778602600098, "[TT] Communication Protocol of the N-FEE and N-DPU = SpaceWire"]
-[6.044670581817627, 4.326815128326416, "[FF] Elements of the DSX ground segment = Mission control, global telemetry, tracking, and control (TT&C) network, and the remote experiment sites"]
-[5.522030353546143, 6.330505847930908, "[TT] Capacity for MS Imagery of the Memory = 3 Gbit"]
-[3.34798264503479, 4.852099418640137, "[TT] Orbit of the RISAT-1 SAR payload = 536 km"]
-[7.7507524490356445, 6.341477870941162, "[FF] Observation Time of the Helioseismic and Magnetic Imager (HMI) = 11:45 UT"]
-[7.4852213859558105, 0.40632572770118713, "[TT] Laser Altimeter of the OSIRIS-REx = OLA"]
-[6.770555019378662, 7.099676132202148, "[TT] Prototype Name of the BEAM = Bigelow Expandable Activity Module"]
-[12.107975959777832, 3.648906946182251, "[FF] Design Pressure of the Cylinders = More than double normal operation pressure - 1000 times atmospheric pressure"]
-[8.38707447052002, 5.053340911865234, "[FF] Energy Collection of the Reflective Telescope = Collected and focused by the telescope and auxiliary optics"]
-[4.980044841766357, -0.20557352900505066, "[TT] Launch Time of the MicroMAS-2a = 03:59 UTC"]
-[6.307775020599365, 8.040224075317383, "[TT] Channels of the SSMIS = 24"]
-[7.5918169021606445, 6.161234378814697, "[FF] Receiver Operation of the LCT = Optically adding a locally generated field to the receiver field prior to photodetection"]
-[6.18907356262207, -0.3414914608001709, "[TT] Commissioning Time of the AprizeSat-3 and AprizeSat-4 = 1 hour after separation"]
-[5.009400367736816, -0.8184404373168945, "[TT] Duration at Space Station of the Dragon spacecraft = About a month"]
-[6.477565288543701, 3.8173718452453613, "[FF] Functioning of the GOES-16 = Yes"]
-[4.987637519836426, 6.807109832763672, "[FF] BDH Subsystem of the ResourceSat-2 = Baseband Data Handling"]
-[6.866195201873779, 3.2844297885894775, "[FF] Data Usage of the MHS = Provides the operational microwave sounding capability for the NOAA-N, -N' meteorological satellites"]
-[11.732105255126953, 6.637828826904297, "[TT] Energy Range of the High-energy Proton Detector = 1-165 MeV"]
-[11.740466117858887, 3.320462465286255, "[TT] Engine of the TSUBAME = Gas-jet thrusters"]
-[8.436424255371094, 2.113278388977051, "[FF] Calibration Care of the WindSat = Commensurate"]
-[7.506059646606445, 3.5352118015289307, "[FF] Function of the GNSS-RO = Provide (with high vertical resolution) all-weather atmospheric and ionospheric soundings by tracking GNSS satellites"]
-[6.3195929527282715, 1.8311253786087036, "[FF] URL of the eROSITA = http://www.mpe.mpg.de/450698/news"]
-[3.8503923416137695, 4.497619152069092, "[TT] Monitoring Area of the RADARSAT-2 = 3.8 million hectares"]
-[9.120166778564453, 5.578249454498291, "[TT] STARE Pointing Stability of the ADCS = 0.052\u00ba/s"]
-[7.521052360534668, 2.189032554626465, "[TT] Latitude Coverage of the MLS = Complete each orbit"]
-[7.368303298950195, 5.220279216766357, "[FF] Function of the DDA = Measure the across-track angle of the range measurement"]
-[6.967597484588623, 6.044266700744629, "[TT] Quantity of the PPSM = 1"]
-[3.452918291091919, -0.9244242310523987, "[TT] Orbit Type of the JAWSAT = Sun-synchronous near-circular orbit"]
-[8.24164867401123, 6.73826789855957, "[FF] Video Capability of the MWIR Imager = Yes"]
-[8.645430564880371, 8.021330833435059, "[TT] Image Resolution of the MicrOmega/MASCOT = 128 x 128 pixels"]
-[4.603031158447266, 4.432589530944824, "[TT] Spatial Resolution of the DubaiSat-2 = 1.0 m (Pan), 4 m (MS)"]
-[7.714874744415283, -0.8507486581802368, "[TT] Detection Period of the ICESat-2 = October 2019 through April 2020"]
-[5.643238544464111, 7.117499828338623, "[TT] Data Rate of the IPS = 16 Mbit/s"]
-[12.807815551757812, 7.604436874389648, "[TT] Instrument Package Power Consumption of the LCROSS = 27 W"]
-[2.030298948287964, -0.32490119338035583, "[FF] Purpose of the DSX = Advance understanding of the Van Allen radiation belts and their effect on spacecraft components"]
-[12.174059867858887, 3.1606545448303223, "[TT] Propellant of the GPIM = AF-M315E advanced green monopropellant"]
-[8.144075393676758, 8.649377822875977, "[TT] Full Bands of the Spectrometer = 75"]
-[4.761892795562744, 5.437516212463379, "[FF] Function of the LUT = Locates the beacons by Doppler processing"]
-[8.365833282470703, 9.009347915649414, "[TT] Wavelengths of the PACS and SPIRE = 250, 350 and 500 \u00b5m"]
-[8.199809074401855, 3.949289560317993, "[FF] Unknown of the NINA (New Instrument for Nuclear Analysis) = Unknown"]
-[13.258434295654297, 7.087048530578613, "[FF] Power Consumption of the PSA = Unknown"]
-[8.297026634216309, 2.0776453018188477, "[FF] Data Provided of the CFOSAT = Co-located wind vector fields, directional spectra of ocean waves, normalized radar cross-section"]
-[9.666561126708984, 0.16918878257274628, "[FF] Parachute Progress Date of the ExoMars = 15 October 2019"]
-[12.7506685256958, 3.1709611415863037, "[TT] Reserved Quantity of the Fuel = 3.9 kg"]
-[10.459835052490234, -1.3003695011138916, "[TT] \u03b2 Angle of the SLATS = -60\u00ba"]
-[4.849192142486572, 0.3512651324272156, "[FF] Installation Date of the SUVI = Recently"]
-[13.900761604309082, 7.121973514556885, "[FF] Power Supply Card of the ECS = Conditioning raw 28 V spacecraft power to conditioned supply voltages for ECS components"]
-[10.018889427185059, -1.500686526298523, "[TT] Orbit Inclination of the Lunar Landing Vehicle = 45\u00ba"]
-[13.388128280639648, 3.003948450088501, "[TT] Mass (kg) of the Sentinel-1A/B = 2300"]
-[9.390504837036133, 7.095832824707031, "[FF] Spatial Resolution of the EO System = ~50 m (goal)"]
-[6.912788391113281, -0.5062095522880554, "[TT] Local Sun Time of the Orbit = 12:00 \u00b1 15 min"]
-[4.834169387817383, 6.928332328796387, "[TT] X-band Downlink Data Rate of the Spacecraft = 320 Mbit/s"]
-[11.539444923400879, 4.865424156188965, "[TT] Inner Diameter of the PM = 4.2 m"]
-[5.902897834777832, 0.9092588424682617, "[FF] Accident Investigation of the Columbia = Largest investigation ever by NASA"]
-[7.56449031829834, 3.7825088500976562, "[TT] Best Ground Resolution of the NightPod = 10 m/pixel"]
-[12.143928527832031, -0.25149887800216675, "[FF] Imaging Frequency of the TESS spacecraft = Every three hours"]
-[8.058638572692871, 7.473644733428955, "[TT] No of CCD Elements in Cross-Track of the MSU-50 = 8000"]
-[10.235637664794922, 8.084586143493652, "[TT] Telescope Aperture of the PIC = 30 cm"]
-[10.8864164352417, 7.507420539855957, "[TT]  of the Swath-to-Swath Registration = \u00b1 5.2 \u00b5rad"]
-[7.337587356567383, 5.398621082305908, "[FF] On-board Processing Procedures of the Optical Payload = Radiometric correction, Inter-channel co-registration, Geo-referencing, Background classification, Hotspot detection, Consolidation of hot pixels, Extraction of attributes of hot clusters"]
-[7.793791770935059, 7.138735294342041, "[TT] Data Recording of the HF Wave Sensor (IME-HF) = On triggering alerts only"]
-[6.2278852462768555, 2.289658308029175, "[TT] Co-Principal Investigator of the SIMPL = Walt Mirczak"]
-[6.312138557434082, 5.014091968536377, "[FF] Data Storage of the ACOP = Unknown"]
-[13.316534042358398, 5.408700942993164, "[TT] Solar Arrays of the Satellite = Two arrays with a total wingspan of 37 m"]
-[8.53147029876709, 1.3387240171432495, "[TT] Parameter Detected of the Aquarius = Changes in saltiness"]
-[5.644326210021973, 7.033638954162598, "[TT] Data Rate of the SSDRs = 20 Mbit/s"]
-[8.351314544677734, 7.624068737030029, "[TT] Format of the CCD Detector Array = 2 k x 2 k"]
-[7.856944561004639, 9.245444297790527, "[TT] Wavelengths of the ATOMMS = Centimeter and millimeter"]
-[6.78081750869751, 0.02942737191915512, "[TT] Dataset Duration of the Kepler = 4 years"]
-[6.5158843994140625, 7.613254070281982, "[TT] Quantization levels of the Surface type = 12 types"]
-[6.817829132080078, 4.789745807647705, "[FF] Purpose of the NPSCuL = Integrate/package P-PODs as secondary payloads"]
-[7.89037561416626, 8.838953018188477, "[TT] Waveband of the Sensor = 1020 nm"]
-[3.688727855682373, 2.5573840141296387, "[TT] Debut Speed of the Iridium Certus = 352 kbit/s"]
-[11.887073516845703, 4.94883918762207, "[TT] Size (mm) of the M3 = 556 x 291"]
-[10.907556533813477, 0.7644211053848267, "[TT] Growth Requirement of the Space Moss = Only a small area for growth"]
-[8.421585083007812, 7.431668758392334, "[TT] Pixel Pitch of the GOCI-II CMOS Imaging Sensor = 6.8\u03bcm"]
-[13.294865608215332, 2.937011957168579, "[TT] Mass of the FalconSat-7 = 3U CubeSat, 5 kg"]
-[9.53846549987793, 0.972118616104126, "[TT] Velocity of the Zeta Puppis = About 60 km/s"]
-[14.287554740905762, 3.0790176391601562, "[TT] Mass of the UKube-1 = < 1080 g"]
-[10.695114135742188, 3.305302619934082, "[FF] Technology of the Micro-gravity experiment = Important for a better understanding of the characteristics and the mechanisms of the convection movement of the fluid with a free surface or a boundary surface on the ground"]
-[7.75946569442749, 9.13171672821045, "[TT] Wavelength Range of the Band 4 = 1360-1390 nm"]
-[5.612502574920654, 0.9153500199317932, "[TT] Formal Initiation Date of the GeoXO = Nov. 9, 2021"]
-[5.391482353210449, 8.693144798278809, "[TT] Bandwidth of the M2 = 0.018 \u00b5m"]
-[8.397274017333984, 0.0381038635969162, "[FF] Seasonal Cycle of the Carbon Dioxide Ice = Unfolds over the comet's 6.5 year orbit"]
-[11.732650756835938, 6.358645439147949, "[TT] Sensitivity of the XSM = ~ 7000 cps at flux level of 10-4 W m-2 in the range 1-8 \u00c5"]
-[7.042854309082031, 1.367782473564148, "[FF] Background Picture of the Spitzer Space Telescope = Captured in infrared light"]
-[6.801492691040039, 2.6274194717407227, "[FF] Bacteria Test Subject of the Biofilms = Staphylococcus capitis"]
-[8.858480453491211, 8.188288688659668, "[TT] Number of VNIR Focal Planes of the GLI = 2"]
-[6.177877902984619, 7.884353160858154, "[TT] Maximum Simultaneous CDMA Channels of the Mission Uplink Subsystem = 6"]
-[10.18020248413086, 5.509731292724609, "[TT] Cooling Method of the Telescope Tube Assembly = Passively cooled"]
-[6.82003116607666, 4.761195182800293, "[FF] Unknown of the TCU = Unknown"]
-[11.111662864685059, 6.128183364868164, "[FF] Composite Structure of the Mirror = D263 glass; DS-4 graphite; F131 epoxy"]
-[5.552425861358643, 7.572113990783691, "[TT] EIRP of the HDR-VSAT = > 66.9 dBW"]
-[7.442177772521973, 2.2107596397399902, "[FF] Mission Goal of the PROBA-V = Ensure data continuity of global vegetation monitoring and improve data quality"]
-[7.5424299240112305, -0.6662381887435913, "[TT] Start Date of the IceBridge = 2009"]
-[5.413341045379639, 0.9914859533309937, "[FF] Launch Date of the Vietnamese satellite = Unknown"]
-[5.5962815284729, 5.687310218811035, "[TT] Microcontroller of the C&DH Subsystem = 16 bit MSP430F2618"]
-[6.29614782333374, 8.076370239257812, "[TT] Number of Channels of the IIR = 3"]
-[5.505221843719482, 2.2519283294677734, "[FF] Affiliation of the Nico Fleurink = Unknown"]
-[6.359296798706055, 8.515152931213379, "[FF] Observation Functions of the SGLI = NUV and polarization observations"]
-[7.390022277832031, 1.1770358085632324, "[FF] Objective of the MOMA = Analyze volatile and refractory organic compounds in martian surface and subsurface sediments"]
-[2.0134687423706055, -0.33836954832077026, "[FF] Precipitation of Particles from the Van Allen Belts of the Seismic Activity = Can produce the precipitation of particles from the Van Allen belts"]
-[10.646699905395508, 2.2476184368133545, "[TT] Number of X-ray Source Detections of the 3XMM Catalogue = 531 261"]
-[9.240105628967285, 4.7588043212890625, "[FF] Attitude and Pointing Control System of the Skylab = Unknown"]
-[3.3327784538269043, 4.805651664733887, "[TT] Distribution Time of the SAR Data Products = ~ 6 months after launch"]
-[7.93458890914917, 6.6017327308654785, "[FF] Temporal Resolutions of the AGRI = 1 - 5 minutes over a regional domain and 15 minutes over the full-disk domain"]
-[12.087540626525879, 6.385066509246826, "[TT] Observation of the AMS = Slope of the positron fraction decreases by an order of magnitude from 20 to 250 GeV"]
-[6.42868185043335, 0.6635151505470276, "[FF] Lifted atop launcher Date of the Landsat-9 = 21 September 2021"]
-[5.4462785720825195, 3.876281499862671, "[TT] Number of Satellites of the FFRF Subsystem = 2 to 4"]
-[5.804359436035156, 5.404265403747559, "[FF] Processor of the SES-17 = On-board processor"]
-[5.306020736694336, 5.06243371963501, "[TT] Interface of the Phoenix GPS Receivers = AOCS interface box"]
-[8.375617980957031, 1.2661136388778687, "[TT] Pulse Length of the RainCube = Up to 166 \u00b5s"]
-[5.646479606628418, 1.2018321752548218, "[FF] FCI Instrument Testing Date of the MTG = 4 July 2018"]
-[8.177242279052734, 3.425544261932373, "[FF] Measurement Concept of the OCO-3 = OCO-3 will measure the intensity of the sunlight reflected from the presence of CO2 in a column of air"]
-[12.551749229431152, 3.1840739250183105, "[TT] Propellant Mass of the MTM CPS = 157 kg"]
-[9.711445808410645, 1.4100033044815063, "[FF] Image Quality of the Pleiades 1B = Unknown"]
-[5.981489658355713, 0.8580890893936157, "[FF] Image Capture Date of the Small Monitor Camera = August 14, 2018"]
-[4.5915141105651855, 4.711475849151611, "[FF] Function of the MDA Maritime Insights platform = Addresses dark vessel detection and supports maritime enforcement initiatives"]
-[5.899152755737305, 6.401756286621094, "[TT] Latency of the Starlink = 20 milliseconds"]
-[7.35648775100708, 6.82059907913208, "[TT] Measurement Principle of the ATLAS = Sending pulses of light from the satellite to Earth\u2019s surface and measuring how long it takes individual photons to return to the sensor"]
-[9.78732681274414, 7.443450450897217, "[TT] GSD (Ground Sample Distance) of the ALOS/PRISM = 2.5 m"]
-[3.4680702686309814, 6.403968334197998, "[TT] Antenna Aperture of the DPS = 1.5 m x 1.5 m"]
-[5.8756561279296875, -0.6556189656257629, "[TT] Mission Lifetime of the Satellite = ~17 years"]
-[5.947515487670898, 5.466060161590576, "[FF] Processor of the EPS = Dedicated"]
-[1.9350459575653076, -0.4034920334815979, "[FF] Fuel Consumption of the Van Allen Probes = Unknown"]
-[7.944922924041748, 7.620846748352051, "[FF] Optical Performance Test Results of the Hyperspectral Imager = Unknown"]
-[6.322841644287109, 1.5202336311340332, "[FF] URL of the Cluster = http://www.esa.int/Our_Activities/Operations/Rejigging_the_Cluster_quartet"]
-[6.4526567459106445, 6.5740532875061035, "[FF] Function of the Data Compression Core = Achieve on-board data compression"]
-[6.376107692718506, 2.3166961669921875, "[FF] Presentation of the PRISMA = Flight Results from PRISMA Formation Flying and Rendezvous Demonstration Mission"]
-[6.930930137634277, 4.641869068145752, "[FF] Terminal States of the RadFETs = Grounded"]
-[7.798270225524902, 6.969266891479492, "[TT] Pixel Exposure Time of the Instrument = 1.625, 3.25, or 6.5 ms"]
-[6.638132572174072, 6.822235107421875, "[FF] Evaluation of the Small Optical Transponder (SOTA) = Unknown"]
-[13.801009178161621, 2.9102325439453125, "[TT] Mass of the Spacecraft = 1.22 kg"]
-[9.655672073364258, 0.19949780404567719, "[TT] RAAN of the PROBA-3 = 84\u00ba"]
-[10.533552169799805, 6.275488376617432, "[FF] Mounting Method of the Optomechanical System = Epoxy bed of Stycast 2850FT"]
-[10.879108428955078, 2.9229495525360107, "[TT] Type of the PICOSat = Technology demonstration microsatellite of DoD/AFRL"]
-[9.46556282043457, 8.966127395629883, "[TT] Video Imaging Duration of the Iris Video Camera = Up to 60 seconds"]
-[13.158080101013184, 7.275390148162842, "[TT] Power Consumption of the CIRC = <20 W"]
-[10.403583526611328, 1.8333684206008911, "[FF] Penetration Depth of the NuSTAR = Deeper into the region around the black hole"]
-[4.952049732208252, 8.306448936462402, "[TT] RF Bandwidth (MHz) of the Antenna = 600"]
-[9.70115852355957, 7.527534008026123, "[TT] Total Column Ozone Data Resolution of the Nadir Sensor Wide-Field Telescope = About 50 km x 50 km at nadir"]
-[7.871719837188721, 8.676164627075195, "[TT] Spectral Range of the Instrument = 420 nm to 2450 nm"]
-[7.862180709838867, -2.483696222305298, "[TT] Observation Target Changes of the GOLD = Western Hemisphere"]
-[7.3513922691345215, 4.310399532318115, "[FF] Sensor Complement of the GOES-R = Newly defined"]
-[9.397273063659668, -1.7089629173278809, "[TT] Mean Anomaly at Epoch of the Swarm-A (Alpha) = \u0394t = 2-10 s difference between A and B"]
-[6.201116561889648, 8.59901237487793, "[TT] Polarization Options of the Receiver = H and V polarization, or an internal load"]
-[9.315531730651855, -0.4858557879924774, "[TT] Perigee of the Orbit = 108,000 km"]
-[8.32190227508545, 1.5028506517410278, "[TT] Sea Surface Salinity Accuracy of the SMOS = 0.3-0.5 psu"]
-[9.053335189819336, 5.079723358154297, "[FF] Function of the Gyroscopes = Derive the satellite rates"]
-[13.605621337890625, 1.8693363666534424, "[TT] Cargo Capacity of the Cygnus = 3,350 kg"]
-[7.34410285949707, 6.5431060791015625, "[TT] Planning Window Length of the RASP = 240 minutes"]
-[9.676554679870605, 1.411458969116211, "[TT] Ground Resolution of the Pl\u00e9iades-Neo satellites = 30 cm"]
-[8.66645336151123, 3.3948566913604736, "[FF] Sunphotometers of the SOVA = Degradation in Space"]
-[13.137043952941895, 7.714808464050293, "[TT] Optical Transmit Power of the Optical link = 2.2 W"]
-[6.700870513916016, 3.6670219898223877, "[FF] Material of the 3-D Printer = Low-temperature plastic"]
-[9.386338233947754, 7.4681010246276855, "[FF] Ground Pixel Sizes of the MOMS-02 = Unknown"]
-[4.46368408203125, 7.182383060455322, "[TT] Real-time Data Transmission of the RF Communications = S-band"]
-[6.46957540512085, 4.515681266784668, "[FF] Functionality of the DMFC = Perform a variety of mission specific functions"]
-[13.755073547363281, 6.871908187866211, "[TT] Number of PCBs of the EPS = 5"]
-[6.394472599029541, 1.0105836391448975, "[TT] Space Weather Status Website of the FORMOSAT-7/COSMIC-2 Constellation = https://swoo.cwb.gov.tw"]
-[7.28134298324585, 4.560750961303711, "[TT] Instruments of the SPOT-5 = Vegetation, HRS, DORIS-NG (SPOT), HRG"]
-[6.902082443237305, -0.038129016757011414, "[TT] Data Collection of the SOLSE = 20 orbits"]
-[3.4277961254119873, 5.261575698852539, "[TT] Band, Wavelength of the Radar = L-band, 22.9 cm"]
-[11.77139663696289, 6.7194294929504395, "[TT] Energy Range of the XSM = 1-20 keV"]
-[7.445817947387695, 4.565156936645508, "[FF] Environmental Testing of the Monitor = Passed"]
-[9.220104217529297, -0.4364785850048065, "[TT] Apogee of the Molniya Orbit = 39750 km"]
-[9.254075050354004, 7.579234600067139, "[TT] Height of the NETCAM = 220 mm"]
-[8.16763973236084, -0.7303080558776855, "[TT] Thinning Rate of the Crosson ice shelf = About 10 feet (3 meters) per year"]
-[5.824313640594482, 0.9678336977958679, "[FF] Date of the Orbital ATK Resupply Mission = Dec. 6, 2015"]
-[6.209158420562744, 2.48319673538208, "[FF] Capability of the Orion MPCV = Be a backup system for International Space Station cargo and crew delivery"]
-[4.83656120300293, -0.9558724761009216, "[TT] Launch Date of the FY-3 (FengYun-3) = Sep 10, 2023"]
-[7.163186550140381, 8.089369773864746, "[TT] Radiometric Bias of the Instrument = \u2264 0.3 dB"]
-[3.3286120891571045, 5.719099998474121, "[TT] SAR Antenna of the KOMPSAT-6 = Fixed SAR antenna on a panel"]
-[7.610968112945557, 5.71837043762207, "[FF] Field-of-View of the Scanning LIDAR = Ranging between 1\u00b0 x 1\u00b0 and 40\u00b0 x 40\u00b0 degrees maximum"]
-[7.3748459815979, 1.1944520473480225, "[FF] Detection of the MOMA = Direct detection of indigenous martian organic molecules and some thermally released inorganic molecules or laser-desorbed fragments of inorganic minerals"]
-[8.433553695678711, 6.574481964111328, "[FF] Operation of the MSS = Opto-mechanical scanning instrument (whiskbroom technique, unidirectional operation)"]
-[8.733652114868164, 6.03425407409668, "[TT] Depth of Operation of the Coarse Lateral Sensor = 5 m to 80 m"]
-[7.377573490142822, 2.8793625831604004, "[TT] Data Collection of the MethaneSAT = Monitor 50 major oil and gas regions that account for more than 80 per cent of global methane production, revisiting them on intervals of seven days or less"]
-[8.41853141784668, 6.161497116088867, "[TT] Relative Semi-Diameter Precision of the Instrument = Better than 1 marcsec"]
-[5.394792556762695, 3.317796230316162, "[FF] Data Receiving Stations of the JERS-1 = NASDA/EOC (Hatoyama, Japan), Tokai University (Kumamoto, Japan), National Institute of Polar Research, Japan (Syowa, Antarctica), Alaska SAR Facility (ASF, Fairbanks, Alaska), Canada, CCRS (Gatineau, Prince Albert), ESA (Kiruna, Tromsoe), National Research Council of Thailand (Bangkok, Thailand), ACRES (Australia), DLR/DFD station (O'Higgins, Antarctica)"]
-[9.233353614807129, 3.2227025032043457, "[FF] Purpose of the Telescope-coronagraph 132 \u00c5 = Imaging hot plasma (T ~ 10 MK) of the solar corona"]
-[7.677928924560547, 0.8271185755729675, "[FF] Measurement Quality of the Lunar Meteoroid Impact Flash Detection = High signal-to-noise ratios (SNR)"]
-[7.466228008270264, 5.311089992523193, "[FF] Components of the Infrared Imager = Telescope, filter wheel, optical focal plane assembly, cryostat, video proximity electronics unit, payload control unit, X-band payload telemetry chain"]
-[4.60338020324707, 0.4851866066455841, "[FF] Rob Gutro Article Date of the JWST = March 20, 2014"]
-[7.079458713531494, 8.605805397033691, "[TT] Antialiasing Filter Cut-off Frequency of the Rx Module = 18 MHz"]
-[11.586825370788574, 3.4645614624023438, "[TT] Integration Method of the X50 series propulsion system = Sliding it through the opening in the bottom of the separation panel"]
-[6.6330180168151855, 3.3880743980407715, "[FF] Status of the GMR = Providing science data"]
-[13.855778694152832, 7.122056007385254, "[TT] Input Voltage of the Buck-Boost Converter = 60 - 150 V"]
-[5.314803600311279, 0.7857304811477661, "[TT] Commissioning Phase End Date of the SAC-D = July 24, 2011"]
-[13.366942405700684, 7.2281012535095215, "[TT] Maximum Power Draw of the ABEX = 65.5 W"]
-[14.303696632385254, 3.010303258895874, "[TT] Mass of the HORUYU-2 = 7.1 kg"]
-[5.401775360107422, 4.1343994140625, "[TT] Satellite Bus of the EarthDaily Constellation = Modified OneWeb satellite buses"]
-[8.129520416259766, 4.2096381187438965, "[FF] Data Display of the TechDemoSat-1's radiation monitor = Google Earth"]
-[6.669628620147705, 4.337193012237549, "[FF] Data Source of the Map = IBTrACS"]
-[3.3756465911865234, 3.6697194576263428, "[FF] Presentation Date of the PAZ and TerraSAR-X = Sept. 23-27, 2013"]
-[10.212151527404785, 5.762422561645508, "[TT] Temperature Resolution of the AMSU-A = 0.25 - 1.2 K"]
-[8.798493385314941, 5.8455281257629395, "[TT] Misalignment Error Reduction of the Collimation Actuators = From about 1 mm to about 1 \u00b5m"]
-[3.897575616836548, 0.1862279176712036, "[FF] Image Release Date of the SMART-1 = Sept. 29, 2014"]
-[1.7336674928665161, -2.0883853435516357, "[TT] Mission Status Presentation Date of the Hayabusa-2 = 21-25 October 2019"]
-[5.5374755859375, 0.8231536746025085, "[FF] Testing Start Date of the TET-1 = July 24, 2012"]
-[3.393580436706543, 4.922626495361328, "[FF] Sensor of the TanDEM-X = SAR sensors"]
-[6.418951511383057, 1.4298582077026367, "[FF] International Cooperation Presentation of the COSMO-SkyMed = 68th IAC (International Astronautical Congress), Adelaide, Australia, 25-29 Sept. 2017"]
-[5.083963871002197, 1.8129212856292725, "[TT] Operation Status of the ICIR = Normal"]
-[8.590006828308105, 8.061691284179688, "[TT] Pixel Area of the MicrOmega/MASCOT = 20 \u00b5m2"]
-[12.119758605957031, 7.6075897216796875, "[TT] Instrument Mass of the Imager = ~290 kg"]
-[13.378376960754395, 7.67408561706543, "[TT] Power of the DC Power = 12.7 W conditioned power (transmit)"]
-[6.070703983306885, -0.32219013571739197, "[TT] Exploration Mission Duration of the LRO = 9/16/2009 - 9/16/2010"]
-[10.74781322479248, 2.8584423065185547, "[TT] Type of the OTB-1 = Minisatellite"]
-[7.892475605010986, -0.510346531867981, "[FF] Data Transmission of the British Antarctic Survey (BAS) = Remote measurement stations"]
-[7.2403483390808105, 7.570732116699219, "[FF] Surface Requirements of the Reflector = 60 times more stringent than a photon sieve"]
-[8.251602172851562, 6.67138147354126, "[FF] Conference Presentation Date of the Imaging System = Sept. 15-18, 2015"]
-[9.425657272338867, 4.086232662200928, "[FF] Attitude Determination Sensors of the X-ray Telescope = Fine sun sensor, 3-axes magnetometer"]
-[9.282608985900879, 3.136812448501587, "[FF] Value of the Solar Wind Particle Pressure = Unknown"]
-[10.265582084655762, 5.325055122375488, "[FF] Function of the Coldpath Bar = Thermally conductive, yet structurally isolating"]
-[10.495746612548828, 5.759156703948975, "[TT] Temperature of the HD 260655 c = 284 \u00b0C"]
-[5.906162738800049, 1.0753588676452637, "[FF] Mission End Date of the Deep Space 1 = Unknown"]
-[6.026823997497559, 4.958894729614258, "[FF] Risk Mitigation of the On-Board Computer (OBC) = In Progress"]
-[4.5019683837890625, 1.4797402620315552, "[FF] Launch Date of the Intelsat 20 = August 2, 2012"]
-[6.1345624923706055, 2.1482675075531006, "[FF] Principal Investigator of the eROSITA = Andrea Merloni"]
-[5.5022993087768555, 0.5701301693916321, "[TT] First Snapshots Date of the NuSTAR = June 28, 2012"]
-[6.053428649902344, 0.8462929725646973, "[TT] Capture Time of the Image = 07:22 AM local solar time on 2 September 2018"]
-[6.384221076965332, -0.03190300986170769, "[TT] Global Coverage Time of the MSR = 5 days"]
-[6.008031368255615, 4.2125563621521, "[FF] Radiation Levels of the LEO Satellites = More amenable to Commercial-Of-The-Self (COTS) components of automotive or industrial grade"]
-[7.742403030395508, 0.5302779674530029, "[FF] Measurement of the Lunar IceCube = C-, H-, O-, and S-bearing volatiles"]
-[7.6663336753845215, 2.1861038208007812, "[FF] Applications of the NIDEM = Coastal risk mitigation, ecological conservation, habitat mapping, hydrographic surveying"]
-[4.4964919090271, -0.03800124675035477, "[FF] Test Flight Date of the Starliner = Late Summer"]
-[6.59043550491333, 3.152362823486328, "[FF] Evaluation of the Disaster Monitoring Constellation = Utility in Support of Earth Observation Applications"]
-[11.348641395568848, 5.856654167175293, "[TT] Material of the Outer Shield = Aluminum"]
-[9.299324035644531, 5.007956027984619, "[TT] Roll Nadir Pointing Accuracy of the Attitude Control = \u00b115\u00ba"]
-[7.18430233001709, 2.1515302658081055, "[TT] Mission Status of the Biomass = Approved"]
-[4.2657904624938965, 7.088795185089111, "[TT] Operation Frequency of the TT&C Ground Stations (GS) = S-band"]
-[8.140336990356445, 7.094897747039795, "[TT] Technology of the EXI instrument = CMOS"]
-[10.445296287536621, 5.589017391204834, "[TT] Thermal Protection Tiles of the Crew Capsule = 970"]
-[14.287473678588867, 3.060781478881836, "[TT] Mass of the Landmapper-BC = 11 kg"]
-[10.468857765197754, 2.300410747528076, "[FF] Field of View (FOV) of the X-ray telescopes = Energy-dependent"]
-[10.024842262268066, 7.800625324249268, "[TT] Pointing of the Telescope = Within a 40\u00ba cone centered around the anti-sun vector"]
-[7.894939422607422, -0.5223203897476196, "[FF] Preparatory Campaigns of the CryoSat-2 = Arctic Arc Expedition, Antarctic 2008/9 CroVEx campaign"]
-[8.154632568359375, -0.9684087038040161, "[TT] Data Accuracy of the ICESat-2 = Within 4 mm"]
-[6.643685817718506, 4.798427104949951, "[FF] Function of the Instrument Controller Electronics (ICE) = Provides the interface to the spacecraft and is responsible for MWI control"]
-[6.320846080780029, 8.513916969299316, "[FF] Operational Modes of the MIRAS = Dual-polarization mode, Full polarimetric mode, Calibration modes"]
-[7.355104446411133, 3.6565120220184326, "[FF] URL of the Global GNSS Radio Occultation Mission = http://www.intechopen.com/download/pdf/pdfs_id/6844"]
-[7.016849040985107, 2.8290398120880127, "[FF] Design and Verification Status of the EarthCARE/CPR = Unknown"]
-[9.168641090393066, 5.5998640060424805, "[FF] Real-Time Correction of the AOCS = Corrects the scan mirror pointing for the expected spacecraft attitude and orbital effects"]
-[11.36899185180664, 0.659379243850708, "[TT] Size of the Planet Orbiting AU Microscopii = About as large as Neptune"]
-[4.400420665740967, 7.802570343017578, "[TT] Downlink Frequency of the RF Communications = UHF band (437.5 MHz)"]
-[7.444796085357666, 5.312737464904785, "[TT] Instrument of the ATLAS-3 = SOLCON-2, ACRIM-II"]
-[8.878012657165527, 7.650367736816406, "[TT] Pixel Pitch (Pan) of the Pushbroom imager = 12 \u00b5m x 12 \u00b5m"]
-[4.719961166381836, 7.546030521392822, "[FF] Function of the MC34072 Amplifier = Controls the gain of the intermediate amplifier"]
-[5.086309909820557, 1.2311902046203613, "[FF] Conference Presentation Date of the PROBA-2 = April 25-27, 2006"]
-[8.442252159118652, -0.5008916854858398, "[TT] Area Coverage of the CHORUS = 63% of the area around the ice limit border"]
-[6.623833179473877, 1.1160062551498413, "[FF] Resolution of the FormoSat-2 = High"]
-[9.395487785339355, 6.206812858581543, "[TT] Scanning Angle of the Scanning geometry = 108\u00ba, 54\u00ba"]
-[5.03888463973999, 7.079916000366211, "[TT] L (chips) of the Service downlink = 128"]
-[1.36617910861969, 2.7842414379119873, "[TT] Principal Absorbing Constituents of the Band 2 = CO2"]
-[4.573019981384277, 7.124151229858398, "[TT] Leased C-band Capacity to Intelsat of the INSAT-2E = 11 units"]
-[5.783261299133301, 1.0681482553482056, "[FF] Experiment Date of the RIS = 1999"]
-[5.0675811767578125, 0.4081820845603943, "[FF] Launch Date of the SpaceX = 16 August 2021"]
-[14.245321273803711, 3.3754258155822754, "[TT] Mass of the RE (STARE-A) = 4.0 kg"]
-[5.854920864105225, -0.6468519568443298, "[TT] Lifetime of the SmallGEO = Up to 15 years"]
-[8.460917472839355, 7.728791236877441, "[TT] CCD Array of the WFC = 512 x 512"]
-[7.757328510284424, 8.720784187316895, "[TT] Spectral range of the Optical System = 0.37-0.45, 0.45-0.51, 0.58-0.68, 0.68-0.78, 3.55-3.93 \u00b5m"]
-[6.890211582183838, -0.6098676323890686, "[TT] Orbital period of the GPS-DASS = 11 h 15 m"]
-[10.233257293701172, 0.5764192938804626, "[TT] Satellite Separation of the Triple Mirror = 270 km"]
-[6.952920913696289, 5.224991798400879, "[FF] Components of the Group Delay = Clock, code generator, modulator, up-converter, transmitter, satellite antenna"]
-[4.159675121307373, 0.9642585515975952, "[FF] Launch Date of the H-IIB Launch Vehicle No. 6 = Oct. 7, 2016"]
-[10.777176856994629, 0.9224456548690796, "[TT] Size of the TOI-2337b, TOI-4329b, and TOI-2669b = Slightly smaller to more than 1.6 times the size of Jupiter"]
-[7.997951984405518, 7.377087116241455, "[TT] Number of Light Emitters of the OPSE = 3"]
-[9.79687213897705, 8.624171257019043, "[TT] IFOV of the Optical telescope = 24 \u00b5rad"]
-[4.285111427307129, 7.501295566558838, "[TT] Band Frequency of the SARAL/AltiKa = Ka-band"]
-[4.840940475463867, 0.5429708361625671, "[TT] Launch Date of the MMS = March 13, 2015"]
-[10.58953857421875, 1.7216739654541016, "[FF] Surface Temperature of the Black Hole = Millions of degrees"]
-[8.130478858947754, 0.07858071476221085, "[FF] Launch Date of the Meteor-M No.2-1 = Unknown"]
-[7.357146739959717, 3.362790107727051, "[TT] Debris Shield Disposal of the AMS-02 = Eventually burn up harmlessly in Earth\u2019s orbit"]
-[6.947065353393555, 7.103006839752197, "[TT] Sampling Interval of the sADC = 12 \u00b5s"]
-[7.153992176055908, 6.812884330749512, "[TT] Beam Sampling Time of the MWR = 1.92 s"]
-[6.152348041534424, 2.2231297492980957, "[FF] Lead Scientist of the eROSITA = Rashid Sunyaev"]
-[4.299717903137207, 2.9402270317077637, "[TT] Testing Location of the Solar Orbiter = IABG facilities in Ottobrunn, Germany"]
-[8.023591041564941, 3.982200860977173, "[TT] Diffraction Pattern Precision of the External Occulter = \u00b11%"]
-[11.216403007507324, 0.9376727342605591, "[TT] End of Life Date of the LISA = 2038"]
-[8.806400299072266, 4.197474479675293, "[TT] Observation Target of the PROBA-2 = Sun"]
-[9.524726867675781, -1.7207409143447876, "[TT] Orbital Inclination of the Swarm-C (Charlie) = 88\u00ba"]
-[8.149513244628906, -0.6656849384307861, "[TT] Arctic Sea Ice Volume of the CryoSat-2 = 10,200 km3"]
-[4.327571392059326, 7.512387275695801, "[TT] Clock Frequency of the X-band transmitter = 48 MHz"]
-[3.7286481857299805, -0.7352429628372192, "[TT] Orbit of the PhoneSat 2.5 = Low Earth Orbit"]
-[5.21195125579834, 0.5463734269142151, "[TT] Activation Date of the HDEV = April 30, 2014"]
-[5.732943534851074, 12.14820384979248, "[TT] Wavelength FWHM of an unresolved line of the Spectrometer = 0.126 \u00b5m"]
-[9.423149108886719, 8.130776405334473, "[FF] Publisher of the Introduction to Fourier Optics = W. H. Freeman"]
-[5.9813551902771, 0.10215657204389572, "[TT] Hibernation Duration of the Rosetta = 31 months"]
-[6.499391078948975, 1.8994709253311157, "[FF] URL of the MidSTAR-1 = http://en.wikipedia.org/wiki/MidSTAR-1"]
-[6.237307548522949, 1.0033979415893555, "[FF] Progress Update and Launch Plan Date of the FORMOSAT-7/COSMIC-2 = April 16-22, 2015"]
-[5.567073822021484, -1.9362692832946777, "[FF] Unknown of the Kompsat-2 = Unknown"]
-[5.395363807678223, 1.0060794353485107, "[FF] Date of the ICSOS 2014 = May 7-9, 2014"]
-[9.512166976928711, 8.885754585266113, "[TT] Incidence Angle of the Iris Video Camera = < 40\u00ba"]
-[6.639622688293457, 5.478304386138916, "[TT] Type of the Pollux = Passive"]
-[10.083818435668945, -2.6752521991729736, "[FF] Storage of the C2B = Non-volatile flash file-system consisting of two SD cards"]
-[7.540421485900879, 4.651767253875732, "[FF] Function of the Coherency Filter = Remove non-lightning events from the data stream"]
-[13.7649564743042, 2.9107584953308105, "[TT] Mass of the Spacecraft = \u22642480 kg"]
-[4.460201263427734, 0.6383112668991089, "[TT] Data Declassification Date of the DMSP = March 1973"]
-[4.32432222366333, 2.635756492614746, "[TT] Location of the GRACE-FO = VAFB Harris Corporation facility"]
-[6.368656158447266, 0.4988672435283661, "[FF] Data Collection Period of the CPT = Fixed period of time"]
-[5.061908721923828, 0.24485407769680023, "[TT] Launch Date of the Genesis = August 8, 2001"]
-[5.68137264251709, 5.978230953216553, "[TT] Max No of Parameters of the C&DH module = 1500"]
-[9.562143325805664, 7.026261806488037, "[TT] Spatial Resolution at 37 GHz of the SMMR = About 22 km"]
-[10.18957805633545, 3.1830873489379883, "[TT] General Environmental Verification Specification of the Drag-free CubeSat = 14.1 g-rms for the lightest satellites"]
-[7.99493932723999, 9.114534378051758, "[FF] Light Source of the RCA = Phosphor light source with peak emission over the TOMS wavelength range"]
-[5.834046840667725, 4.584564208984375, "[FF] Service of the Ground Station = Tracking, monitoring and control of satellites"]
-[6.034721374511719, 5.756088733673096, "[TT] Information Type of the State-machine sub-experiments = Analog"]
-[11.349390983581543, 5.000542640686035, "[TT] Total Quantity of the Straw Tubes = 5248"]
-[6.937682151794434, 1.2846274375915527, "[FF] Conference Date of the Pico Satellite Solar Cell Testbed = Aug. 10-13, 2009"]
-[13.348941802978516, 7.670978546142578, "[TT] Transmitted Peak Power of the Antenna = 1 kW"]
-[6.82992696762085, 8.446484565734863, "[TT] Number of Channels of the SEDA = Protons: 8, Electrons: 8"]
-[5.296347618103027, 2.740739583969116, "[TT] Location of the Astrobiology Analytical Laboratory = NASA\u2019s Goddard Space Flight Center in Greenbelt, Maryland"]
-[8.69987678527832, 7.608155250549316, "[TT] Detector Pixel Size of the Instrument = 13 \u00b5m x 13 \u00b5m (VIS); 40 \u00b5m x 40 \u00b5m (NIR)"]
-[8.81428337097168, 7.116419792175293, "[FF] Image Resolution of the AlSat-2 = High"]
-[7.496331214904785, 3.4851913452148438, "[FF] Release Method of the Debris Objects = By the main satellite with subsequent recapture"]
-[11.471977233886719, 3.883951425552368, "[TT] Dimensions of the MightySat II.1 = 68.6 cm x 89 cm x 89 cm"]
-[8.293510437011719, 5.378554821014404, "[TT] Radiometric Calibration of the Payload = Continues to be maintained"]
-[8.993587493896484, 1.4316608905792236, "[FF] Program of the New Horizons = New Frontiers Program"]
-[4.860877990722656, 0.5714030265808105, "[TT] Launch Year of the XFM = 2021"]
-[9.864679336547852, 5.557477951049805, "[FF] Thermal Capacitance of the Sensor Node = Large"]
-[7.672786712646484, 2.7124173641204834, "[FF] Location of the The Chinese carbon cycle data-assimilation system (Tan-Tracker) = China"]
-[14.283550262451172, 3.1244680881500244, "[TT] Mass of the S/C = 98 kg"]
-[5.8787336349487305, 0.9694371223449707, "[TT] Image Acquisition Date of the Mosul = 26 Jun. 2014"]
-[4.156526565551758, 7.308887481689453, "[FF] Band of the OneWeb = Ku-band and Ka-band"]
-[7.085875511169434, 7.823661804199219, "[FF] Angular Resolution of the Micropore Reflector = Coarser than Wolter optics"]
-[5.85977029800415, 3.1486141681671143, "[TT] Ownership of the JPSS = NOAA"]
-[10.748982429504395, 2.7750158309936523, "[TT] Microsatellite Lifetime of the BlackSky Constellation = 4 years"]
-[12.44218921661377, 3.3029232025146484, "[FF] Spring Force of the Separation System = Slightly below the weight of the satellite"]
-[12.723337173461914, 3.8980770111083984, "[FF] Nature of the Magnetopause Reconnection = Quasi-periodic"]
-[9.459630012512207, 4.77284049987793, "[TT] Attitude Control Provider of the ADCS = BCT XACT"]
-[5.277501583099365, 0.7502017617225647, "[TT] Commissioning End Date of the RASAT = Late December 2011"]
-[7.5484724044799805, 3.7223145961761475, "[FF] Tracking Targets of the Hexapod = Sun and Moon"]
-[3.5569522380828857, -0.679777979850769, "[TT] Orbit Orientation of the Spacecraft = Parallel to the Sun terminator plane"]
-[11.339387893676758, 2.7764573097229004, "[TT] Analyzer of Particles and Electric Fields Mass of the Microsatellite = 0.8 kg"]
-[8.499120712280273, 9.476682662963867, "[TT] Responsivity Measurement of the Responsivity Measurement = 0.51 A/W"]
-[13.195649147033691, 7.129063606262207, "[FF] Power Consumption of the RDSA = Unknown"]
-[8.72828483581543, 8.639942169189453, "[TT] Pixels per FWHM of the Spectrometer = 1340"]
-[5.207653522491455, 8.420730590820312, "[TT] Bandwidth of the Channel 4 = 1000 MHz"]
-[13.55345630645752, 6.795328617095947, "[TT] Power Source of the RapidScat = Space station"]
-[7.911661148071289, 7.876766681671143, "[TT] Redundancy of the VIS Channel Detector = Yes"]
-[8.50403118133545, 7.340555667877197, "[TT] CCD Cameras of the HJ-1A = 2"]
-[4.508161544799805, 1.6106526851654053, "[TT] Launch Date of the GovSat-1 = 31 Jan. 2018"]
-[6.396305084228516, 0.6456102132797241, "[TT] Launch Date of the Landsat-8 = 2013"]
-[7.284074783325195, 4.012716293334961, "[FF] Ground-Controlled Formation Geometry of the ATI Experiments = Minimum satellite distances of 150 m in the plane perpendicular to the flight direction"]
-[8.841150283813477, 2.7635879516601562, "[FF] Solar Occulting Disk of the SOHO = LASCO C2 and C3 camera"]
-[8.222715377807617, 2.706674575805664, "[FF] Measurement Domain of the CIRC = Atmosphere, Ocean, Land, Gravity and Magnetic Fields, Snow & Ice"]
-[6.769782066345215, 0.7899167537689209, "[FF] First Instrument Placement Date of the InSight = 19 December 2018"]
-[10.170385360717773, 2.80202054977417, "[TT] Version of the NanoSat GSS = 7.1.0"]
-[5.055535316467285, 4.389403343200684, "[TT] Actual Starlink Terminals of the Starlink = Much lower than 200,000 or even zero"]
-[14.20132827758789, 3.274019718170166, "[TT] TRM mass of the HPA = 675 g"]
-[14.166158676147461, 2.816429615020752, "[TT] Mass of the CartoSat-2B = 694 kg"]
-[9.001470565795898, 4.966638565063477, "[TT] Quantity of the Rate sensors = Two 3-axes Inertial Rate Sensors"]
-[9.0751953125, 7.816891670227051, "[TT] Photodetector Sensing Area Size of the Optical Head = 6.66 mm x 5.32 mm"]
-[9.892955780029297, -1.316393494606018, "[TT] Inclination of the BeaverCube = 51.6\u00b0"]
-[7.810752868652344, 9.073421478271484, "[FF] Wavelength Bands of the B. subtilis = 470, 525, and 615 nm"]
-[5.756533622741699, 7.341352939605713, "[TT] Data Rate of the GimmeRF = Up to about 24 Tbit per orbit"]
-[8.96313762664795, 2.6979293823242188, "[FF] Tail Formation of the McNaught = Two distinct tails: an ion tail carried by the solar wind and a dust tail"]
-[4.977198600769043, 3.4016616344451904, "[FF] Acquisition of the EMS Technologies Canada Ltd. = Bought by MDA"]
-[11.025428771972656, 0.5639786124229431, "[TT] Number of Confirmed Planets of the Kepler spacecraft = 2,650"]
-[5.283641815185547, 1.4230190515518188, "[TT] Validated Measurements Availability of the SMAP = Summer of 2016"]
-[8.906164169311523, 5.715188980102539, "[TT] Pointing Accuracy of the Fine Guidance Sensor = Approximately a hundredth of an arcsecond"]
-[7.91684627532959, 6.746393203735352, "[TT] Sensitivity of the Instrument = Compatible with primarily using HH and/or VV imaging"]
-[7.152958869934082, 5.32171106338501, "[FF] Subsystems of the CAST = PRD (Particle Radiation Detector), APD (Aurora Particle Detector), CRED (CMOS-IC Radiation Effect Detector), SDM (SEM Data Memory) and a 4.8 kHz subcarrier modulator"]
-[9.635254859924316, 4.250725746154785, "[TT] Magnetometer of the ADCS = 1.0 V/gauss, \u00b11.9 gauss"]
-[8.544337272644043, 3.576809883117676, "[TT] Mission of the MinXSS-1 = Solar physics"]
-[10.90406608581543, 3.747345447540283, "[FF] Propulsion Method of the LightSail-2 = Solar sailing"]
-[9.247175216674805, -0.39626243710517883, "[TT] Apogee of the BUV = 1108 km"]
-[10.375980377197266, 2.7546324729919434, "[TT] Launch Site of the BRITE/CanX-3 nanosatellites = Yasny Cosmodrome"]
-[4.847798824310303, 3.083911418914795, "[TT] Prime Contractor of the ROSE-L = Thales Alenia Space"]
-[11.489992141723633, 3.4491214752197266, "[FF] Design and Test of the Compact Propulsion System = Complete"]
-[10.46870231628418, 5.688427925109863, "[TT] Surface Temperature of the HD 21749b = Around 300 degrees Fahrenheit (150\u00baC)"]
-[5.942937850952148, 1.2561243772506714, "[FF] Fabrication Project Date of the MIMOSA = April 2-6, 2001"]
-[8.774906158447266, 2.8290843963623047, "[TT] Resolution of the Aurora Sensor = Approximately 30 metres per pixel"]
-[13.807726860046387, 2.6549105644226074, "[TT] Launch Mass of the Spacecraft = 2060 kg"]
-[14.250198364257812, 3.2315869331359863, "[TT] Mass of the PAP = 7 kg"]
-[8.580780982971191, 9.326396942138672, "[TT] Requirement Value of the Level 0 Registration = 0.5pixel RMS (MS)"]
-[9.749998092651367, -0.5287259817123413, "[TT] Orbit of the Restore-L = More than 600 km above Earth"]
-[5.2271246910095215, 0.4265175461769104, "[TT] Authorization Date of the PLB = July 1, 2003"]
-[3.821948289871216, -1.190119743347168, "[TT] Target Orbit of the eROSITA = Lagrange point (L2)"]
-[6.643570899963379, 1.7108174562454224, "[TT] Publication Name of the Astrophysical Journal = Astrophysical Journal"]
-[11.363697052001953, 5.860803604125977, "[TT] Material of the Magnet = AlNiCo"]
-[8.97351360321045, 0.8301355838775635, "[TT] Flybys of the BepiColombo = One at Earth, two at Venus and six at Mercury"]
-[5.141414165496826, 2.399651050567627, "[TT] Mission Type of the SES-17 = Non-EO"]
-[9.568880081176758, 9.108699798583984, "[TT] Mission Type of the IRIS = 3-axis stabilized, sun-pointed"]
-[4.238475799560547, 3.66024112701416, "[TT] Operational of the Galileo Satellites 13 and 14 = Yes"]
-[4.494459629058838, 3.135134220123291, "[TT] Data Processing Location of the Ground Segment = MOC (Mission Operations Center) facility at Cordoba"]
-[7.719044208526611, 2.9094009399414062, "[TT] Mission Scientist of the CO2M = Yasjka Meijer"]
-[7.362067222595215, 2.709099769592285, "[FF] Data of the Magsat = Small-Scale Structure of the Geodynamo"]
-[7.73899507522583, 1.3617585897445679, "[FF] Monitoring of the ROSE-L = Vegetation, ice and oceans"]
-[9.379983901977539, 6.841035842895508, "[TT] Spatial Resolution (km) of the ALT = 7"]
-[7.786881923675537, 6.672571659088135, "[TT] Revisit time of the Imager = 3 days"]
-[7.075088977813721, 1.1487127542495728, "[TT] Arrival of the ERO = Mars orbit"]
-[12.20277214050293, -0.26860594749450684, "[TT] Imaging Duration of the TESS = 1 year"]
-[7.920982360839844, 8.514425277709961, "[TT] Spatial Co-registration of Spectral Bands of the Hyperion = < 20% of pixel"]
-[5.953603744506836, 2.0968716144561768, "[FF] Location of the OSA = Between the ICPS (Interim Cryogenic Propulsion Stage) and Orion"]
-[3.8140413761138916, 7.931551456451416, "[TT] Modulation of the Payload Imagery = OQPSK (Offset Quadrature Phase Shift Keying)"]
-[4.360288143157959, 5.475009441375732, "[TT] Frequency of the COSPAS-1 = 121.5 MHz"]
-[5.108458518981934, 3.2682831287384033, "[TT] Manufacturer of the Landsat-6 = Martin Marietta Astro Space"]
-[11.248642921447754, 4.962061882019043, "[TT] Mast Length of the NuSTAR Metrology System = 10 m"]
-[8.312213897705078, 3.140953779220581, "[FF] Award Date of the Ozone Monitoring Instrument = 1 April 2019"]
-[5.136073112487793, 8.404765129089355, "[TT] Bandwidth/Passband of the 6 = 350 MHz"]
-[13.359955787658691, 7.339791774749756, "[TT] Power of the ILAS = < 120 W"]
-[12.0352783203125, -0.3945285677909851, "[FF] Launch Date of the TESS = 22 June 2020"]
-[11.206818580627441, 1.0890284776687622, "[TT] Performance Requirement of the LISA Pathfinder = As close as possible to 10-12 ms-2 Hz-1/2 in the frequency band 10-3 to 10-1 Hz"]
-[6.990776062011719, -0.7765420079231262, "[TT] Orbital Period of the Beta Pictoris c = 3.3 years"]
-[5.812523365020752, -0.4879210889339447, "[TT] Nominal Mission Lifetime of the PROBA-3 = 2 years"]
-[10.426664352416992, 2.2938649654388428, "[FF] Function of the FM0, FM1 and FM2 = First two modules are the flight units, and the third module is to provide for more extensive X-ray characterization"]
-[8.78251838684082, 5.776881694793701, "[TT] Pointing Knowledge Stability of the Instrument = \u00b19.7 \u00b5radians over 2.5 seconds"]
-[4.995027542114258, 3.28300404548645, "[TT] Manufacturer of the SSTI = Laben, Milan, Italy"]
-[7.2155961990356445, 4.42989444732666, "[FF] Purpose of the VLF Transmitter = Conduct active experiments to quantify spaceborne VLF wave-injection efficiency and determine the details of the wave-particle interactions"]
-[8.185391426086426, 3.129711389541626, "[FF] Function of the OMS Radiometer = Deliver highly-accurate temperature, humidity, and precipitation data"]
-[5.789424419403076, 1.2102019786834717, "[FF] Conference Date of the EarthCARE/CPR = Sept. 24-27, 2012"]
-[3.6065163612365723, 6.998396873474121, "[TT] Polarization of the SAS&R = L-V LHCP"]
-[6.071444511413574, 5.15976619720459, "[FF] Function of the PLC = Transmit beam definition command and switching sequence definitions to the active antenna"]
-[18.799114227294922, 3.479860544204712, "[TT] \u0394r (m) of the Masirah Island = 13.4"]
-[6.101720333099365, -0.3562619984149933, "[TT] Commissioning Phase Duration of the CALIPSO = 38 days"]
-[8.540879249572754, 3.651524305343628, "[FF] Purpose of the RAVAN = Measure the amount of reflected solar and thermal energy that is emitted into space"]
-[5.175745487213135, 3.257312059402466, "[TT] Manufacturer of the RemoveDEBRIS = Surrey Space Centre at the University of Surrey"]
-[7.81316614151001, 2.0137903690338135, "[FF] Observation of the ALT = Oceanic currents, bathymetry, and waves"]
-[7.70502233505249, -0.2685966193675995, "[TT] Peak Season of the AgCam/ISSAC = April - October"]
-[4.458095550537109, 3.214658737182617, "[TT] Location of the ISSDC = IDSN (Indian Deep Space Network) campus in Bangalore"]
-[8.922171592712402, 2.697547435760498, "[TT] Exposure Time of the Solar Flare Sites = < 10 ms"]
-[5.9053425788879395, 5.121113300323486, "[FF] Software of the Modem Processor = Iris software"]
-[5.499326229095459, 5.032704830169678, "[FF] GPS Receiver of the RAX-1 = Operated as predicted and maintained lock in the experimental zones"]
-[5.8229546546936035, 4.793956279754639, "[FF] Navigation Signal Provider of the GPS satellites = Broadcast navigation signals"]
-[4.991257190704346, 3.3971493244171143, "[TT] Manufacturer of the TPS = Herakles-Safran Group"]
-[9.755393981933594, 7.010929584503174, "[TT] Spatial Resolution of the AGRI = 0.5 - 4 km"]
-[7.35300350189209, 3.582949638366699, "[FF] URL of the NightPod = http://www.astrofein.com/astro-und-feinwerktechnik-adlershof/projekte/nightpod/"]
-[14.05024242401123, 4.012147903442383, "[TT] Mass of the Instrument = 205 kg"]
-[6.060352325439453, 5.7483696937561035, "[FF] Data Reception of the DRS = Real-time and playback from the onboard memory"]
-[7.483100414276123, 4.838265895843506, "[FF] ACS Components of the TAIKI = COTS (Commercial Off The Shelf) parts"]
-[6.995229721069336, 1.5444386005401611, "[TT] Purpose of the James Webb Space Telescope = Study other aspects of exoplanets, like the presence and composition of any atmosphere"]
-[5.8295440673828125, 1.7365367412567139, "[TT] Return Date of the Orion = Dec. 18, 2014"]
-[1.7481812238693237, -2.0735294818878174, "[FF] Impact Date of the Hayabusa-2 = 30 October 2020"]
-[7.011685848236084, 1.8419764041900635, "[FF] News Release Date of the NASA's Spaceborne Carbon Counter = Dec. 18, 2014"]
-[6.996222972869873, 7.294338226318359, "[TT] Operational run-time of the ATLAS lasers systems = 3.5 years"]
-[10.097028732299805, 2.956173896789551, "[FF] Deployment Time of the CubeSat Dispensers = Within the first hour of the launch"]
-[13.404210090637207, 2.9344568252563477, "[TT] Mass of the GOSAT-2 = About 1700 kg"]
-[7.184376239776611, 7.364993095397949, "[TT] Resolution of the Beam Modes = 5 m"]
-[9.57058334350586, 4.573204040527344, "[FF] Modes of Operation of the ADCS = Magnetic control, 3-axis control"]
-[8.071702003479004, 2.2236483097076416, "[FF] Data Collection of the Aqua = Cloud formation, precipitation, radiative properties, air-sea fluxes of energy, carbon and moisture, sea ice concentrations and extents"]
-[6.676911354064941, 0.22494806349277496, "[TT] Data Merge Start Year of the CryoSat-2 and SMOS = 2010"]
-[5.217169761657715, 8.256982803344727, "[TT] Bandwidth of the SDR = 175 MHz"]
-[5.704386234283447, 1.2528156042099, "[FF] Publication Date of the LARES satellite = December 2017"]
-[11.092605590820312, 4.845825672149658, "[TT] Voltage of the Electrodynamic Tether = Up to several hundred volts per km"]
-[11.829899787902832, 6.5361857414245605, "[FF] Mass Resolution of the HPCA = Accurately separates and identifies the minute amounts of hydrogen, helium, and oxygen ions"]
-[8.18952751159668, 1.2178339958190918, "[TT] Spatial Resolution (km) of the Soil moisture = 50"]
-[7.165506839752197, 0.21897391974925995, "[TT] Resemblance of the Ichthyosaurs = Modern-day porpoises"]
-[12.129501342773438, 6.113266944885254, "[TT] Detected Events of the AMS-02 = 17 billion cosmic ray events"]
-[4.445440292358398, 1.7827814817428589, "[TT] Antenna Deployment Date of the Radar = July 28, 2018"]
-[11.826177597045898, 6.633736610412598, "[TT] Proton Energy Range of the HEPS = 15-440 MeV"]
-[6.627566337585449, -1.7646243572235107, "[TT] Operating Organizations of the Jason-3 = NOAA, NASA, CNES, EUMETSAT"]
-[4.676891803741455, 1.4688445329666138, "[TT] Publication Date of the Kappa Scheme = July 31, 2020"]
-[10.907233238220215, 10.076889991760254, "[FF] Purpose of the Alpha Magnetic Spectrometer (AMS-02) = Search for antimatter, dark matter, other exotic matter, cosmic ray studies"]
-[8.924749374389648, 7.333548545837402, "[TT] Effective Detector Area of the HXCP = 7 cm 2"]
-[8.997650146484375, 7.392230033874512, "[FF] Horizontal Onboard Accumulation Length of the Detector = 1.0 km and 3.5 km"]
-[8.655707359313965, 2.2667529582977295, "[FF] Altitude Range of the Methane VMR = 40 - 95 km"]
-[10.637838363647461, 8.856303215026855, "[TT] Pixel Size of the Channel 3 = 32 x 32 km"]
-[7.118948936462402, 1.2559748888015747, "[FF] Data Relay of the Trace Gas Orbiter (TGO) = NASA\u2019s Curiosity Mars rover and InSight lander"]
-[5.5895233154296875, 6.541500091552734, "[TT] Daily Capacity of the EDRS-A and EDRS-C nodes = 10.8 TB/day"]
-[8.935785293579102, 6.023575305938721, "[TT] Developer of the Small Analyzer for Neutrals = Sweden"]
-[13.429280281066895, 7.361360549926758, "[TT] Power of the SBUV/TOMS = 20 W"]
-[5.555202960968018, 2.675446033477783, "[TT] Location of the GRNS = Applied Physics Laboratory at Johns Hopkins University"]
-[4.7022833824157715, -1.755730152130127, "[FF] Photogrammetric Processing of the Chang'e-1 = Rigorous"]
-[4.725874423980713, 1.7400851249694824, "[FF] Conference Date of the RazakSAT = Aug. 14-17, 2006"]
-[3.763082265853882, 7.1475830078125, "[TT] Gain of the Antenna = 15 dBi per polarization"]
-[5.252341270446777, 2.633972644805908, "[FF] Operator of the Resurs-P1 = Roscosmos (Russian Federal Space Agency)"]
-[5.209437847137451, 7.83465051651001, "[TT] Master Clock Frequency of the FIELDS Instrument = 38.4 MHz"]
-[8.462973594665527, 2.0136423110961914, "[FF] Channel Purposes of the AMR-2 = Water vapor sensing, Correction for non-raining clouds, Correction for effects of wind-induced enhancements in the sea surface background emission"]
-[7.315791130065918, 6.420130729675293, "[TT] Interval of the Blackbody = 30 minutes"]
-[6.5244646072387695, -0.5803965330123901, "[TT] Orbit Duration of the SMOS = Almost 10 years"]
-[6.867356300354004, 6.116109848022461, "[TT] Number of Pointed Proportional Counters of the IXAE = 3"]
-[11.378312110900879, 4.791035175323486, "[TT] Length of the Hoytether = 10 m"]
-[7.647783279418945, -0.8110782504081726, "[TT] Data Collection Frequency of the ICESat-2 = Every 91 days"]
-[5.153763771057129, 7.4268879890441895, "[TT] Data Rate of the Radio Subsystem = Varying based on the channel capacity"]
-[8.144705772399902, -0.679716169834137, "[TT] Land Ice (small scale) Measurement Accuracy of the CryoSat = 3.3 cm/year"]
-[9.776848793029785, -0.2242516130208969, "[TT] Data Stack Height of the Hubble = About 5,000 miles (8,000 km) high"]
-[16.54717445373535, 3.6435799598693848, "[TT] Number of Planned Satellites of the OneWeb = 1980"]
-[7.814519882202148, 1.7237664461135864, "[FF] Risk-Reduction Studies of the Hydroterra = Will be performed by ESA"]
-[12.73238754272461, 1.9793988466262817, "[TT] Location of the SAGE-III = International Space Station's ExPRESS Logistics Carrier platform"]
-[4.969662189483643, 3.2624597549438477, "[TT] Manufacturer of the UWE-3 = University of W\u00fcrzburg"]
-[6.2940521240234375, 8.066024780273438, "[TT] No of Passbands of the Channel 2 = 1"]
-[9.717608451843262, 2.6153833866119385, "[TT] Operation Start Date of the AlSat Nano = July 24, 2017"]
-[9.858281135559082, 4.737952709197998, "[TT] Spin Rate of the DSP satellites = 15 rpm"]
-[8.627480506896973, 1.0891270637512207, "[FF] Launch Date of the Aquarius = June 10, 2011"]
-[8.089927673339844, -1.2253696918487549, "[FF] Purpose of the IceBridge = Maintain continuity of laser-altimetry measurements between NASA\u2019s ICESat missions"]
-[9.106232643127441, 5.04001522064209, "[FF] Alignment of the Spacecraft = Nominally aligned with the instrument LoS"]
-[6.617680072784424, -0.484053373336792, "[TT] Repeat Cycle of the SPOT-1, -2 and -3 = 26 days"]
-[11.89629077911377, 3.1011674404144287, "[TT] Delta-Velocity of the Onboard Propulsion System = 17 m/s"]
-[4.9568023681640625, -0.5388267040252686, "[TT] Launch Time (JST) of the SLATS / Tsubame = 10:26:22"]
-[6.768802165985107, -0.2800702452659607, "[TT] Years on Orbit of the EO-1 = 13"]
-[8.165358543395996, 0.016492582857608795, "[TT] Launch Date of the TOPEX/Poseidon = Aug. 10, 1992"]
-[8.61374568939209, 1.2256430387496948, "[FF] Performance of the Aquarius sensor = Continues to perform well"]
-[7.8284149169921875, 1.1233947277069092, "[TT] Spatial Resolution for Geohazard Monitoring of the ROSE-L SAR = 5 - 10 m"]
-[8.2344970703125, 7.666914463043213, "[TT] CCD Array Elements of the LISS-3 = 6000"]
-[11.869073867797852, 4.954924583435059, "[TT] Diameter of the Transmitter = 8 mm"]
-[12.031841278076172, -0.286247581243515, "[FF] Observation Date of the TESS = 22 November 2019"]
-[9.750545501708984, 6.4267578125, "[FF] Function of the Mirror = Reflects cold 2.7 K cosmic background radiation into the feedhorn"]
-[10.414231300354004, 2.1258416175842285, "[FF] X-ray Light of the SS 433 = Enough to officially call SS 433 a ULX"]
-[13.417925834655762, 5.477865695953369, "[TT] Solar Array Cells of the MarCO CubeSats = 42"]
-[13.501863479614258, 5.817963600158691, "[TT] Accelerator Grid Voltage of the Solar Wind Concentrator = -8 kV"]
-[9.911005973815918, -0.3611791729927063, "[TT] Altitude for Satellite Release of the Falcon-9 Rocket = 450 km"]
-[9.150259971618652, 7.493716716766357, "[TT] Spatial Resolution of the GOES Imager = 4 km x 4 km on MWIR and TIR bands, 1 km x 1 km on VIS band"]
-[11.021276473999023, 2.9021244049072266, "[TT] Maximum Microsatellite Dimensions of the NanoRacks Microsat Deployer = 95 cm x 83 cm x 64 cm"]
-[9.069805145263672, 3.078658103942871, "[FF] Dominant Dynamics of the Thermosphere = Interaction with charged particles"]
-[5.90196418762207, 4.677343845367432, "[FF] Purpose of the KE Ground Station = Support the singular KE Block I satellite"]
-[5.290663719177246, 4.617457866668701, "[TT] Control Method of the Antenna = Commanded from ground station"]
-[4.749090194702148, 0.46176877617836, "[TT] Launch Date of the GHOSt = End of this year and continuing into 2022"]
-[4.757518768310547, 0.8037503957748413, "[TT] Handover Date of the PROBA-V = April 30, 2014"]
-[5.709611892700195, 2.8762831687927246, "[FF] Name Change of the SRTM = NIMA (National Intelligence Mapping Agency) changed its name to NGA (National Geospatial-Intelligence Agency)"]
-[13.803783416748047, 3.617906093597412, "[TT] Weight of the Antenna Mast = 2.1 kg"]
-[9.588004112243652, 7.026895999908447, "[TT] Spatial Resolution of the LORE = 0.5 km"]
-[8.390840530395508, 7.191791534423828, "[FF] Image Quality of the TRACE instrument = Dependent upon wavelength and required image quality"]
-[7.962361812591553, 0.610745906829834, "[TT] Geospatial Maps of Sea Ice Development Resolution of the ROSE-L SAR = 20 m"]
-[7.839572429656982, 1.361253261566162, "[FF] Data Usage of the WCOM = Improve global hydrological science"]
-[9.013388633728027, 5.452508926391602, "[TT] Body-pointing Capability of the AlSat-2 = \u00b130\u00ba in cross-track"]
-[4.245371341705322, 7.171710014343262, "[TT] Frequency Band of the TT&C = S-band"]
-[6.269134998321533, 8.06320858001709, "[TT] No of Passbands of the Channel 3 = 1"]
-[7.624622821807861, 8.698054313659668, "[TT] Spectral Bands of the ROLO = 32"]
-[10.026504516601562, -1.3975576162338257, "[TT] Pointing Angle of the ADACS = 21.5\u00ba below the orbital normal"]
-[11.112221717834473, 1.006041169166565, "[FF] Orbits of the LISA = Much wider"]
-[7.7212042808532715, 5.6966705322265625, "[FF] Device Type of the SMMR = Radiometer"]
-[11.528299331665039, 3.468709945678711, "[FF] Gas Storage Capability of the Propulsion System = Until it is used for thrusting"]
-[11.999258041381836, 6.539102077484131, "[TT] Energy Range of the AMS-02 = Up to the TeV region"]
-[5.095890045166016, 7.182381629943848, "[FF] Bandwidth Savings of the PhiSat-1 = About 30%"]
-[13.785876274108887, 5.354207515716553, "[TT] Type of the Power System = Dual battery, gallium arsenide triple-junction solar cell based"]
-[9.46667194366455, 5.3683013916015625, "[FF] Rotation of the Mast Alignment = Yes"]
-[7.2872185707092285, 3.1686177253723145, "[TT] Spatial Resolution of the GHGSat's New Satellites = < 25 m"]
-[6.1390790939331055, 1.4961674213409424, "[FF] Image Date of the VIIRS = 7 April 2022"]
-[9.211971282958984, 5.209613800048828, "[TT] Pointing Stability of the LRI = < 20 \u00b5rad over 1 orbit"]
-[5.701805114746094, 1.5580644607543945, "[FF] Development Date of the SWIR Instrument = May 26-30, 2008"]
-[5.354814529418945, 5.609437942504883, "[TT] Data Interface Protocol of the CDMU = 1553 bus protocol"]
-[8.174113273620605, -0.1952286660671234, "[FF] Function of the SSM/I = Define the extent of sea ice and seastate conditions (wave height and patterns) on the world's oceans"]
-[5.381648063659668, 5.783000946044922, "[TT] Radiation hardness of the STRV-2 DHS = about 100 krad"]
-[9.239197731018066, 7.534810543060303, "[TT] GSD at nadir of the Imager = PAN: \u22642.5 m, MS: \u226410 m"]
-[6.601973056793213, 1.0945382118225098, "[FF] Data Collection Area of the FORMOSAT-7/COSMIC-2 = Low- and mid-latitudes"]
-[13.368232727050781, 7.725078105926514, "[TT] Antenna Power of the Transmitter = 2 W"]
-[5.477434158325195, 6.0738444328308105, "[FF] On-board computer of the PCDU = T805, 1 Gbit DRAM/EDAC, 8 Mbit Flash EEPROM"]
-[5.795166969299316, 4.137678623199463, "[TT] System Type of the Mission Control Center = SCOS-2000 (Spacecraft Control & Operation System-2000) EGSE r3.1 system"]
-[3.890925407409668, 2.137101173400879, "[TT] Launch Vehicle of the Galileo FOC satellites = Soyuz ST-B/Fregat-MT"]
-[11.748855590820312, 6.75221061706543, "[TT] Energy Steps of the GIM = 40 per spectrum"]
-[8.168445587158203, -0.6875920295715332, "[FF] Additional Capability of the SMOS = Map the thickness of ice floating in the polar seas"]
-[9.523390769958496, 0.9011366963386536, "[TT] Distance from the Sun of the New Horizons = 50 AU"]
-[8.504923820495605, 7.392735004425049, "[TT] Resolution of the GOCI-II CMOS Imaging Sensor = 2720 rows by 2718 columns"]
-[4.860947132110596, 0.5538973808288574, "[TT] Launch Date of the MULA = 2025"]
-[9.802468299865723, -0.5396928787231445, "[TT] Orbital Height of the HyperScout\u00ae = 500 km"]
-[5.003880977630615, 5.421972751617432, "[TT] Receiver Type of the GTR = Dual-mode receiver"]
-[9.607693672180176, 0.8355000615119934, "[TT] Distance from Earth during Wake-up of the Rosetta = 807 million km"]
-[10.932868957519531, 2.0757181644439697, "[TT] Observation Dates of the XMM-Newton = 2015 and 2017"]
-[6.7390875816345215, 3.5195555686950684, "[FF] Provider of the AMS Experiment = International AMS Collaboration led by the MIT (Massachusetts Institute of Technology)"]
-[6.273673057556152, 0.06509366631507874, "[TT] Years on Orbit of the PARASOL = 6"]
-[8.574387550354004, 5.876158237457275, "[TT] Elevation Pointing Angle Error of the Beam Pointing = Within \u00b11 mrad"]
-[8.69120979309082, -0.17745555937290192, "[TT] Lunar Orbit of the Chang'e-2 = 100 km above the moon's surface"]
-[7.62208890914917, 8.970155715942383, "[TT] Wavelength/Passband of the Instrument = 135.6; 155 nm"]
-[9.360679626464844, -1.390968680381775, "[TT] Orbit Eccentricity of the UniCubeSat = Less than 0.2"]
-[9.113616943359375, 5.068979740142822, "[FF] Shaken but not disturbed of the Inertial Sensor Head = \"Inertial Sensor Head shaken but not disturbed,\" ESA, Dec. 12, 2013"]
-[9.75019359588623, 6.227636337280273, "[TT] Suspension/Drive System of the Moving Mirror = Magnetic"]
-[5.851622104644775, -2.2363052368164062, "[TT] Longitude of the GEO-KOMPSAT-2A = 128.2\u00baE"]
-[5.4427809715271, 3.429058313369751, "[FF] Mission Goals of the Heinrich Hertz = See List"]
-[3.315264940261841, 5.1519646644592285, "[TT] Antenna Roll-Tilting of the RISAT-SAR = \u00b136\u00ba"]
-[3.4231202602386475, -0.889995813369751, "[TT] Orbit Type of the Harmony satellites = Sun-synchronous"]
-[6.8950090408325195, -0.5088241696357727, "[TT] Mean Local Solar Time of the Sentinel-2A = 10:30"]
-[8.08737564086914, -0.43057262897491455, "[FF] Work Progress of the Synthetic Aperture Radar = Analysed less than 0.14 per cent of the lakes in the Arctic"]
-[4.859443664550781, 0.8041588664054871, "[TT] Signing Date of the Statement of Intent = March 28, 2019"]
-[12.20646858215332, -0.10102041065692902, "[TT] Design of the TESS Lens = f=1:4"]
-[11.459689140319824, 5.794291973114014, "[TT] Structure Material of the UniSat-5 = Aluminum honeycomb reinforced by aluminum internal panels"]
-[12.068492889404297, 6.905489921569824, "[TT] Photon Index Below the Break of the Second Broken Powerlaw = 1.96"]
-[4.8227219581604, 0.5513545274734497, "[TT] Launch Year of the SWFO = 2025"]
-[8.456783294677734, 4.295693397521973, "[FF] Purpose of the Shutter Mechanism = Prevent the instrument from direct viewing of the sun in orbit and from contamination during launch"]
-[8.07894229888916, 2.1413698196411133, "[FF] Research Focus of the NASA researchers = Develop new ways to help forecast the intensity of incoming hurricanes"]
-[6.58247709274292, 4.974087715148926, "[FF] Function of the GCS = Monitor and control the entire GATE system"]
-[10.501653671264648, 2.2006680965423584, "[FF] Detection of the X-ray Bubbles = Confirmed"]
-[6.6249284744262695, 4.166705131530762, "[FF] Instrument Configuration of the Ground Segment = Based on predicted crossing times of magnetospheric regions of interest in combination with various on-board trigger algorithms"]
-[9.876480102539062, 7.363129138946533, "[TT] Ground Sample Distance of the Resurs-P1 = 1 m"]
-[9.0521240234375, 0.5220656394958496, "[TT] Maneuvers Events of the ARTEMIS = 170"]
-[5.5775346755981445, -1.9644843339920044, "[FF] Calibration Workshop Date of the KOMPSAT-5 = Aug. 25-27, 2010"]
-[8.21905517578125, 0.04427395015954971, "[FF] Presentation of the Philae = Philae Landing on Comet Churyumov-Gerasimenko: Understanding of Its Descent"]
-[4.566442012786865, -0.797678530216217, "[FF] URL of the SpaceX CRS-25 Dragon = https://www.nasa.gov/mission_pages/station/research/news/spacex-25-research-highlights"]
-[5.360044479370117, 6.878849506378174, "[TT] Peak Detection Rate of the COM DEV NTS Receiver = 35 Messages/s"]
-[8.322216033935547, 7.10234260559082, "[TT] Spatial pixels per frame of the Full-scan Imaging = 24, 8"]
-[6.221253871917725, 4.58837890625, "[FF] Instrument Commands of the Spacecraft = Queued up at the MOC remotely from the SOCs, and uploaded to the spacecraft during the next regular contact"]
-[6.012772560119629, 5.758121967315674, "[TT] FPGA of the SHU = Altera EP3SL70F780I3 (Stratix-III)"]
-[3.44647479057312, -0.9251748919487, "[TT] Orbit Type of the Odin = Sun-synchronous polar orbit"]
-[6.126850605010986, -0.37555280327796936, "[TT] Test Duration of the Large Space Simulator = Weeks at a time"]
-[10.540925025939941, 4.657049655914307, "[FF] Attachment of the ENT = Attached to a spring-loaded pressurized hose"]
-[8.991976737976074, 0.41106516122817993, "[TT] Potential Crater Size of the Wirtanen = Around 20 meters (about 65 feet) across"]
-[5.569766998291016, 5.480846881866455, "[TT] Built-in Radio System of the Command and Data Handling Board = Yes"]
-[6.251306056976318, 6.344350814819336, "[TT] Communication Contact Time of the CANDOS = Almost 60 hours"]
-[8.105175018310547, 6.352427959442139, "[FF] EUV Imager of the SWAP = Unknown"]
-[5.240070819854736, 2.0043540000915527, "[FF] Output of the CEASE = Alerts/warnings in terms of a series of ascending order flags, indicating the likelihood and severity of the forthcoming anomalies"]
-[6.084805011749268, 1.6296391487121582, "[FF] Development Status of the Space Weather Mission = Not Launched"]
-[9.1388578414917, -1.2732378244400024, "[TT] Orbit of the GOES = Geostationary"]
-[5.715580940246582, 5.539047718048096, "[TT] Processor Type of the OBC = Advanced commercial FPGA"]
-[5.882086277008057, 0.8670065999031067, "[TT] Image Acquisition Date of the Bandari = 26 Dec. 2013"]
-[5.671265125274658, 0.7978238463401794, "[FF] Discovery Date of the ASASSN-19bt = Unknown"]
-[9.573175430297852, -0.5243154168128967, "[TT] Altitude of the INSAT-3D = ~35,786 km"]
-[14.259919166564941, 3.180450439453125, "[TT] Mass of the Biobox = 64 kg"]
-[5.577142238616943, 0.5084993243217468, "[TT] End of Operations Date of the GEOS-2 = January 1970"]
-[5.080901622772217, 0.6314203143119812, "[TT] Mission Start Date of the DSCOVR = March 3, 2012"]
-[4.344423294067383, 2.762946844100952, "[FF] Arrival Location of the STPSat-3 = Wallops Flight Facility in Virginia"]
-[8.951595306396484, 4.404925346374512, "[TT] Quantity of the Coarse Sun Sensor Cells = 8"]
-[7.403188705444336, 0.9216565489768982, "[FF] Presentation Date of the GRAIL = March 18-21, 2013"]
-[11.821491241455078, 4.566960334777832, "[TT] Size of the GomX-3 = 10 x 10 x 30 cm"]
-[10.421709060668945, 2.315778970718384, "[FF] Data Transfer of the Soft X-ray telescope = L0 to L1"]
-[6.794934272766113, 5.297950267791748, "[FF] Components of the Digital Back-End (DBE) = Instrument Control Module (ICM), Chirp and Timing Generator (CTG), Digitiser Modules (DGR), Power Conditioning Modules (PCM)"]
-[3.362064838409424, 2.284289836883545, "[FF] Data Processing of the Sentinel-4 = Level-0 data into Level-1B data"]
-[5.129072666168213, 4.387555122375488, "[FF] Orbit Raising Maneuvers of the Starlink Satellites = Failed"]
-[4.650914669036865, 1.554009199142456, "[TT] Patent Filing Date of the GHGSat-D = May 2015"]
-[4.784857749938965, 0.3583146333694458, "[TT] Launch Date of the Prichal Module = 24 November 2021"]
-[10.422723770141602, 6.9766950607299805, "[TT] Meso Height/Width of the ABI instrument = 1.6043\u00ba"]
-[9.357266426086426, -0.4037925899028778, "[TT] Perigee Height of the INTEGRAL = 9,049.6 km"]
-[6.781947135925293, 5.154910564422607, "[FF] DPU of the ASCAT = Digital Processing Unit"]
-[9.12048053741455, 2.523120880126953, "[TT] Strongest X-class flare date of the SOHO = October-November 2003"]
-[8.766334533691406, 4.162078380584717, "[FF] Detector Purpose of the PAMELA = Measure the sign, absolute value of charge and momentum of particles"]
-[14.21849536895752, 3.1161231994628906, "[TT] Mass of the ROBUSTA picosatellite = \u2264 1 kg"]
-[6.594717979431152, 3.718139886856079, "[FF] Purpose of the Portable Water Dispense (PWD) Filter = Remove iodine from water consumed by the crew during nominal operations"]
-[8.275773048400879, 5.483076095581055, "[TT] Size of the DORIS = 385 x 280 x 210 mm"]
-[7.282166957855225, 4.478142261505127, "[FF] Function of the VBS = Render rendezvous and docking navigation information for a formation flying spacecraft"]
-[12.04255199432373, -0.2912881076335907, "[TT] Observation Date of the TESS = Between October and December 2018"]
-[7.698680400848389, 9.209047317504883, "[TT] Wavelength of the Band 2 = 10.0 - 13.4 \u00b5m"]
-[5.354356288909912, 6.98286771774292, "[TT] Speed of the Ground Network = Up to 1 Gbit/s"]
-[6.350798606872559, -0.3148265480995178, "[TT] Revisit Time of the S/C = One day"]
-[11.517090797424316, 5.170155048370361, "[TT] Size of the OMS Radiometer = 10 x 10 x 15cm"]
-[6.435514450073242, -0.696372926235199, "[TT] LTDN of the Resurs-P1 = 10:30 hours"]
-[12.717926025390625, 3.894862413406372, "[FF] Nature of the Magnetopause Reconnection = Ground signatures of bursty reconnection turning on and off at the magnetopause"]
-[5.502716064453125, 7.0001220703125, "[TT] Unidirectional Port Data Rate of the NIC = 40 kbit/s"]
-[14.089642524719238, 3.2315146923065186, "[TT] Mass of the LightSail-2 = 5 kg"]
-[7.584880828857422, -2.4692788124084473, "[FF] Level 1C Data Availability of the GOLD = March 12, 2019"]
-[6.919209957122803, -0.5054556727409363, "[TT] Ascending Nodal Crossing Time of the SSMIS = 20:03 hours local time"]
-[7.493813514709473, 2.1248669624328613, "[FF] Focus Areas of the EDF = Global warming, ecosystem restoration, oceans, and human health"]
-[8.695582389831543, 7.528357028961182, "[TT] Spectral Resolution of the Imager = High"]
-[10.425461769104004, 3.2538769245147705, "[TT] Number of CubeSat Units of the SENSE-A = 3"]
-[8.632132530212402, 5.917637348175049, "[TT] Confidence Level of the GISTEMP = 95 percent"]
-[5.525203227996826, 0.4477229118347168, "[TT] Launch Date of the GeoEye-1 = September 2008"]
-[6.032838821411133, -0.5303726196289062, "[TT] Mission Duration of the AIM = 13 years"]
-[9.804429054260254, 2.4101665019989014, "[TT] Number of Earth-directed (halo) CMEs of the SMEI = 30"]
-[10.09786605834961, -1.5238282680511475, "[TT] Inclination of the Satellite = 99.63\u00ba"]
-[8.371803283691406, 7.156184196472168, "[TT] Quantity of the Cameras = 26 (24 normal cameras and 2 fast cameras)"]
-[13.37549114227295, 6.760488033294678, "[TT] Power of the General spacecraft parameters = 330 W EOL"]
-[5.7617411613464355, 1.9791871309280396, "[TT] Technology Readiness Levels of the SWOT Instruments = 3 to 5"]
-[7.7007622718811035, 9.251782417297363, "[TT] Wavelength Range of the Band 15 = 11.8-12.8 \u00b5m"]
-[6.678778648376465, 3.6256961822509766, "[TT] Robotic Arms of the Satellite = Deployable"]
-[6.576594829559326, 8.361673355102539, "[TT] RIN Performance Frequency of the ASM Instrument = 1 kHz"]
-[6.648866653442383, 8.502775192260742, "[TT] Spectral Channels of the POLDER = 9"]
-[7.499325275421143, 4.7488298416137695, "[FF] Type of the Raytheon Instrument = Advanced instrument"]
-[11.25755500793457, 4.943290710449219, "[TT] Length of the iROSA = 63 feet"]
-[10.21001148223877, 8.101541519165039, "[TT] Aperture Diameter of the DST = 50 cm"]
-[10.309154510498047, 3.198660373687744, "[TT] Platform of the ExoplanetSat = CubeSat"]
-[8.033169746398926, 5.154040813446045, "[FF] Tensional Force Criterion of the Marman Clamp band = Design condition change"]
-[10.089188575744629, 7.999619960784912, "[TT] Focus Distance of the Optoelectronic System = 850 mm"]
-[8.782779693603516, 4.466366767883301, "[TT] Control of the Shutter = Sun Sensor"]
-[7.161508560180664, 0.09842909127473831, "[FF] Age of the Chamaeleon I = Two million years-old"]
-[5.160770893096924, 2.428424596786499, "[TT] Mission Type of the KySat-2 = EO"]
-[10.948016166687012, 3.7560577392578125, "[TT] Solar Sail Area of the NEA Scout = 85 m2"]
-[4.511093616485596, 3.0020720958709717, "[TT] PLSO Location of the FOS = ESTEC"]
-[4.523888111114502, 6.800994396209717, "[TT] Communication of the CICERO satellites = X-band downlink of payload data"]
-[5.704981327056885, 0.8665462136268616, "[TT] Observation Date of the IBEX = Oct. 2009"]
-[9.297720909118652, 4.9991021156311035, "[TT] Cold Face Offset of the SVOM Attitude = 45\u00b0 with respect to the antisolar direction"]
-[10.494855880737305, 2.8928515911102295, "[TT] Platform of the MANTIS = Nanosatellite"]
-[6.908344268798828, 5.8520941734313965, "[TT] Quantity of the PMDs = 2"]
-[8.16694164276123, -1.0459747314453125, "[TT] Vegetation Height Accuracy of the ICESat\u20102 = 3\u2010m"]
-[7.240288734436035, 5.989949703216553, "[FF] Background Value Computation of the RTEP = Exponential moving average with an adjustable time constant k"]
-[5.312618732452393, 0.7622014284133911, "[FF] Research Contract Date of the Capella Space = 17 June 2021"]
-[9.72217082977295, 4.265488147735596, "[FF] Function of the Hysteresis (Memory) Material = Memorizes the current magnetic field and resists changes in KySat-2's orientation"]
-[5.911550521850586, 0.25043952465057373, "[TT] Mission End Date of the Rosetta = September 30, 2016"]
-[4.940601348876953, -2.1403682231903076, "[TT] Mass of the Tianwen-1 = 5 tons"]
-[10.019038200378418, -1.5229735374450684, "[TT] Orbit Inclination of the AlSat-2 = 98.23\u00b0"]
-[3.5536537170410156, -0.9067674875259399, "[TT] Orbit of the DMSP = Polar"]
-[7.744111061096191, 2.373065710067749, "[FF] Objective of the VIRR = Provide images of visual reflection and thermal infrared emission from oceanic, coastal, and atmospheric features"]
-[5.701078414916992, -0.8870123624801636, "[TT] Design Life of the S/C = 1 year + 3 months extension"]
-[5.944057941436768, 0.17963571846485138, "[TT] Deorbiting Date of the PARASOL = Autumn of 2013"]
-[8.317861557006836, 7.112218379974365, "[TT] Nr. of Imaging Tiles per Record of the Camera = 1, 2 or 4"]
-[10.088713645935059, 6.011885166168213, "[TT] Calibration of the Scanning Optical Thermopile = NIST-traceable"]
-[6.237138748168945, 7.267147541046143, "[TT] Sampling Rates of the FGM = 32 Hz (both sensors active) or 64 Hz (one sensor active)"]
-[3.41198992729187, 4.891129493713379, "[FF] L-band Synthetic Aperture Radar of the ROSE-L = Parameter Value Unknown"]
-[7.00292444229126, 5.866189002990723, "[TT] Clocks of the GIOVE-B = 2 RAFS (Rubidium Atomic Frequency Standard)"]
-[8.924692153930664, 7.056539535522461, "[TT] Spectral Resolution of the Satellite = 0.0195/km"]
-[6.295224666595459, 6.4663405418396, "[TT] Signal Delay of the Analog-1 = More than 0.8 seconds"]
-[6.3570075035095215, 8.092109680175781, "[TT] Number of Channels of the CTECS-A = 10"]
-[5.149749755859375, 1.957476019859314, "[TT] Mission Status of the SVOM = Planned"]
-[10.201804161071777, 8.0508394241333, "[TT] Optical Bench Length of the Telescope System = 10 m"]
-[9.890192985534668, 4.527545928955078, "[FF] Attitude Control System of the TanDEM-X = Reaction wheels for fine-pointing with magnet torquers for wheel de-saturation"]
-[5.375759601593018, 3.051936626434326, "[FF] Manufacturer of the InSight = Lockheed Martin Space, Denver"]
-[7.415284156799316, -0.18212540447711945, "[TT] Lander Touchdown Time of the MarCO-B = 11:54 am, November 26th, 2018"]
-[10.72635555267334, 1.1226147413253784, "[TT] Transit of the TOI 700 d = No flares from the star"]
-[7.165565013885498, 2.4377005100250244, "[FF] Service Area of the ASF = North, Central and South America"]
-[9.250545501708984, 3.1166300773620605, "[FF] Content of the Solar Wind = Primordial form of oxygen"]
-[4.879972457885742, 0.6926782727241516, "[TT] Launch Date of the OCO-3 = May 1, 2019"]
-[7.93963098526001, 5.893227577209473, "[TT] Maximum Tracking Rate of the STOs and STAEs = 0.1\u00ba/s"]
-[5.89726448059082, 4.337984085083008, "[FF] Use Case of the Bidirectional IoT = Remote management of equipment"]
-[13.743674278259277, 5.671866416931152, "[TT] Light-Shade Cycle Frequency of the Solar Panels = 16 times per day"]
-[10.887097358703613, 2.9072251319885254, "[TT] Quantity of the CINEMA nanosatellite = 3"]
-[9.467470169067383, 7.103597164154053, "[TT] Spatial Resolution of the OLI-2 = 15 m"]
-[6.7532057762146, 0.9205145835876465, "[TT] First Data Release Date of the Solar Orbiter = September 30, 2020"]
-[10.404054641723633, 1.6832153797149658, "[TT] Rotation of the Delta Scuti stars = Once or twice a day"]
-[8.671830177307129, 3.5753512382507324, "[FF] Measurand of the HIS = Spectrally resolved incoming and Earth-reflected solar radiation"]
-[8.014457702636719, 1.8189365863800049, "[FF] Rate of Increase of the Evapotranspiration = Up to two times higher than previous estimates"]
-[6.296445846557617, 5.938357830047607, "[TT] Late Request Window of the Automator = Up to 45 minutes before execution"]
-[9.637328147888184, 0.7709118723869324, "[TT] Movement Between Observations of the SCIAMACHY = About 1000 km"]
-[9.399718284606934, 7.229292392730713, "[TT] SWIR Spatial Resolution of the iSIM-90 = 13 m"]
-[8.799010276794434, 3.941099166870117, "[FF] Objectives of the S 321 = Measurement of the pitch-angle distribution for electrons (20-300 keV) and protons (20 keV - 3 MeV)"]
-[9.264087677001953, 8.101295471191406, "[TT] Threshold of the Focal Plane Module = 2.5 keV"]
-[4.744104862213135, 3.1491081714630127, "[TT] Manufacturer of the Solar array Photovoltaic Assembly (PVA) = Thales Alenia Space in Belgium"]
-[12.091367721557617, 4.505562782287598, "[TT] Dimensions of the TUBSAT-N = 320 mm x 320 mm x 104 mm"]
-[7.439355850219727, 4.115411758422852, "[FF] Pattern Characteristics of the Flight Feedhorn = To be measured"]
-[14.19742202758789, 6.679309368133545, "[FF] Objective of the BRE = Demonstration of control techniques using conventional constant current battery charging, followed by current tapering"]
-[6.64049768447876, 8.827310562133789, "[TT] Type of the POLDER-2 = Polarization and Directionality of the Earth's Reflectance"]
-[10.567633628845215, 0.9407854080200195, "[FF] Similarity to Earth of the Kepler-1649c = Earth in size and estimated temperature"]
-[10.41466236114502, 5.585212230682373, "[TT] Peak Temperature of the Orion = 2,200\u00b0C"]
-[8.144007682800293, 0.12451927363872528, "[TT] Launch Date of the Meteor-M-2 = July 2014"]
-[7.00453519821167, 3.586714744567871, "[FF] Data Processing of the Satellite Sensors = Daily images"]
-[3.941216230392456, 2.0180447101593018, "[TT] Launch Vehicle of the NPP = Delta-2-7920-10"]
-[3.402495861053467, 5.440324783325195, "[TT] Transmitter Power (Peak) of the SAR Antenna = 1650 W (normal mode), 2280 W (ultra fine mode)"]
-[6.917544364929199, 7.455070495605469, "[TT] ADC Bit Depth of the AEM = 16 bit"]
-[5.322083950042725, 5.226841449737549, "[FF] Planned Connection of the Ground Communication Links = Between ISTRAC and MOSDAC"]
-[10.85086441040039, 2.9907515048980713, "[TT] Nutation Rate of the O/OREOS nanosatellite = 4-5 rpm"]
-[4.176509857177734, 4.036829471588135, "[FF] Objective of the WNISAT-1 = Provide monitoring data to shipping line customers who are interested in the Arctic Sea ice state and the eventual use of the Arctic shipping routes"]
-[4.83338737487793, 5.642909049987793, "[FF] Capability of the ARC = Change the transmit frequency for the evaluation of the Doppler processing"]
-[11.755731582641602, 6.700451374053955, "[TT] Expected energy at LRO (FJ/cm 2) of the NGSLR = 1 to 5"]
-[5.741098880767822, 4.907309055328369, "[FF] Communication Methods of the SSETI Express = Internet, chat sessions, e-mail, news postings, dedicated news server, Internet Relay Chats (IRCs), SSETI website"]
-[8.478910446166992, 8.181706428527832, "[TT] TDI Stage of the VNIR FPA = 1 for 2 lines"]
-[6.760953426361084, 2.7505319118499756, "[FF] Principal Scientific Investigator of the MethaneSAT = Dr Steven C. Wofsy"]
-[5.722946643829346, 1.154017448425293, "[FF] Final Terrestrial Trip Date of the SmallGEO = Dec. 1, 2016"]
-[10.46025276184082, 2.3852386474609375, "[TT] Grasp (500 eV) of the X-ray Imager = 27.5 cm2 deg2"]
-[6.587625980377197, 5.479236602783203, "[TT] State-of-Health of the C&DH = Normal"]
-[6.436188220977783, 5.524549961090088, "[FF] Laser-optical data relay service of the Satellite = Hylas-3 Ka- payload"]
-[5.812160491943359, 2.0465335845947266, "[FF] Mapping of the NuSTAR = Titanium-44 in Cassiopeia A"]
-[5.078378200531006, 0.5575035214424133, "[TT] Operation Start Date of the TSIS-1 SIM = March 2018"]
-[5.060296535491943, 5.298268795013428, "[TT] Tracking Frequencies of the GPS/MET = L1 and L2"]
-[5.815248489379883, 5.059957504272461, "[FF] Software Components of the S-band telemetry data process = Real-time data reception software, real-time data process software"]
-[4.892830848693848, 4.246984004974365, "[FF] Payload Type of the Argos-4 = Wildlife tracking and environmental data"]
-[5.142119884490967, 2.3404042720794678, "[TT] Mission Type of the RHESSI = Non-EO"]
-[5.912590503692627, -1.08828604221344, "[TT] Exceeded Design Life of the Aqua = Yes"]
-[6.509191513061523, 4.287702560424805, "[FF] Data Provided of the REPT = Energy bins, pulse heights, space weather packets, housekeeping telemetry"]
-[13.432271003723145, 6.806164264678955, "[TT] Power Generation Capability of the GOSAT-GW = 5.0 kW"]
-[7.9656081199646, 0.6710435152053833, "[FF] Science Levels of the MASCOT = Context Science"]
-[10.348577499389648, 5.839447975158691, "[TT] Temperature of the NISP = 90 K (-180\u00b0C)"]
-[5.395659446716309, 2.722433090209961, "[FF] CEO of the SpaceLink = David Bettinger"]
-[8.151355743408203, -0.012380161322653294, "[TT] Launch Date of the TOPEX/Poseidon = 1992"]
-[10.10422420501709, 2.4026007652282715, "[FF] X-ray Brightness of the DAXSS = 100 times brighter during flares"]
-[3.1069116592407227, 2.156615734100342, "[FF] Former Name of the Copernicus = GMES"]
-[9.668320655822754, -0.3375154137611389, "[TT] Altitude Increase of the SARAL/AltiKa = 1 km"]
-[11.587512016296387, 4.658746719360352, "[TT] Height of the TOGS = 3.5 m"]
-[8.204313278198242, 2.4309751987457275, "[FF] Estimates of the SCOPE = Cloud top height, cloud thickness, cloud optical depth"]
-[5.9701433181762695, 5.803693771362305, "[TT] Architecture of the QSP-1 = 4-Tray"]
-[10.21839427947998, 8.03369140625, "[TT] Length of the Telescope = 2465 mm"]
-[13.8317232131958, 2.67521595954895, "[TT] Mass at Launch of the Spacecraft = 2093 kg"]
-[12.090685844421387, 4.562255382537842, "[TT] Size of the Satellite = 954 mm x 954 mm x 1000 mm"]
-[8.035009384155273, 2.562403440475464, "[TT] Measurement Domain of the CAS500 = Land"]
-[13.377213478088379, 7.352320671081543, "[TT] Power of the PAP = 7 W"]
-[7.009525775909424, 1.02828049659729, "[FF] Date of the Dungeness Spit = 13 April 2022"]
-[8.375726699829102, 3.7225911617279053, "[FF] Cal_solar data Collection of the OCO-2 = Spectral Wavelength Calibration"]
-[9.085489273071289, 4.808144569396973, "[TT] Sensor Quantity of the MAGIC = 2"]
-[10.064059257507324, 0.9195932149887085, "[TT] Earth Surface Area Observed of the MOMS-2P = 65 million km 2"]
-[12.00822639465332, 6.235164165496826, "[FF] Hypothesis of the AMS-02 = After the Big Bang, identical amounts of matter and antimatter were created"]
-[9.166411399841309, 3.287501811981201, "[FF] Observation of the Satellite = Wave-particle interactions in Earth\u2019s magnetotail"]
-[11.406756401062012, 5.836371421813965, "[TT] Bus Structure Material of the StudSat = High grade aluminum alloy (Al 7075 T6)"]
-[7.679154396057129, 6.561140537261963, "[TT] Scan Time of the MAHRSI = 72 to 202 seconds"]
-[7.691150188446045, 5.291909694671631, "[TT] Function of the Satellite = Performs POD (Precise Orbit Determination)"]
-[5.934799671173096, -0.020344534888863564, "[TT] Activation Times of the LDT = Between 21:00 and 4:18 (UTC), and between 9:00 and 16:18 (UTC)"]
-[5.478944301605225, 2.3600480556488037, "[FF] Target of the Hera = Didymos"]
-[9.084073066711426, 5.104448318481445, "[FF] Output of the Estimator = Estimate of the gyro angular rate bias"]
-[9.448442459106445, 6.131140232086182, "[TT] Incident Angle of the DPS = ~39\u00ba"]
-[7.024544715881348, 7.519850254058838, "[TT] Bit Depth of the Signal Digitization = 10 bit"]
-[6.588185787200928, 4.35695743560791, "[FF] Sample Rate of the QuakeSat = Unknown"]
-[7.97567892074585, 4.52730655670166, "[FF] Lesson Learned of the RASAT = In-orbit calibration is absolutely necessary"]
-[5.201874732971191, 8.38874340057373, "[TT] Bandwidth of the Instrument = 91 to 183.3 GHz"]
-[5.9098591804504395, 2.5600602626800537, "[FF] Student Collaboration Goal of the IMAP = Develop hands-on research experience for students"]
-[3.155080795288086, 4.327600955963135, "[FF] Interferometric Configuration of the TerraSAR-X = Single-pass"]
-[4.898802757263184, 0.5855337977409363, "[TT] Program Start Date of the OICETS = 1993"]
-[8.339198112487793, 7.46692419052124, "[TT] Primary Detector of the Spectrometer = Electrical Substitution Radiometer (ESR)"]
-[6.560082912445068, 4.289205551147461, "[FF] Design Influence of the SWEM = THEMIS, HESSI, STEREO, and MAVEN"]
-[7.691573619842529, 0.822639524936676, "[FF] On-board Image Processing Algorithm of the DELPHINUS = Lunar Impact Flashes Detection"]
-[14.190237998962402, 3.256964683532715, "[TT] Mass of the M1 = 2.3 kg"]
-[8.637706756591797, 1.1819055080413818, "[FF] Data Processing of the Aquarius = Acquiring, processing, analyzing, archiving and distributing scientific data"]
-[9.638864517211914, 4.7650465965271, "[TT] Stabilization of the Satellite = Three axes"]
-[12.154767990112305, 4.65933084487915, "[TT] Dimensions of the CAST968 bus = 1.4 m x 1.1 m x 0.953 m"]
-[8.476215362548828, 3.8343684673309326, "[TT] Imaging Technology of the IBEX = ENA (Energetic Neutral Atom) imaging"]
-[4.445599555969238, 3.2617743015289307, "[TT] Ground Stations of the PROBA Project = ESA station in Redu (Belgium), second ground station used in S-band during LEOP and the first part of the commissioning phase"]
-[3.8965063095092773, 1.9701124429702759, "[TT] Launch Vehicle of the WSF-M = SpaceX Falcon 9"]
-[10.94780445098877, 2.0812721252441406, "[TT] Response Time of the XMM-Newton = A few hours later"]
-[8.599907875061035, 2.180879831314087, "[FF] Purpose of the Plane = Adjust route to fly over sea ice"]
-[14.06316089630127, 7.1723785400390625, "[TT] Power Bus Voltage Range of the EPS = 25-32.8 VDC"]
-[9.803231239318848, -0.3148099482059479, "[TT] Altitude of the LIMS = 153 km"]
-[8.080368995666504, 9.112067222595215, "[FF] Parameter Species Wavelength of the SSUSI = O 911 \u00c5, 1304 \u00c5, 1356 \u00c5"]
-[8.263513565063477, 7.6999711990356445, "[TT] Material of the Visible Band = Silicon photodiodes"]
-[9.97291374206543, 8.991217613220215, "[TT] IGFOV of the Sounder = 280 \u00b5rad"]
-[11.419482231140137, 5.7939581871032715, "[TT] Material of the Platform = Aluminum honeycomb sandwich panels"]
-[4.865009307861328, 0.4203921854496002, "[FF] Launch Date of the SLS = Four years from now"]
-[13.86741828918457, 2.7252864837646484, "[FF] Upper and Lower End Masses Configuration of the ATEx = In orbit as one object connected by a 22 m tether"]
-[11.782598495483398, 4.855932712554932, "[TT] Dimensions of the S/C Structure = 90 cm x 90 cm x 107 cm"]
-[3.0614755153656006, 2.007944107055664, "[FF] Anomaly Updates of the Copernicus Sentinel-1B = 1"]
-[7.531025409698486, 8.247692108154297, "[TT] Point Response (1 x 1 pixel) of the SXI = 25%"]
-[13.262454986572266, 7.094563961029053, "[TT] Power of the IR Payload = < 100 W"]
-[5.809566020965576, 4.489208698272705, "[FF] Data Down-link of the EDRS = Directly to processing and archiving centers"]
-[4.170880317687988, 7.319703578948975, "[TT] Operating Bands of the RCU = K- and Ka-bands"]
-[13.34989070892334, 5.405618667602539, "[TT] Solar Panels of the Picard microsatellite = Single"]
-[9.37691593170166, -1.3467748165130615, "[TT] Eccentricity of the Orbit = < 0.0025"]
-[13.587946891784668, 6.963242530822754, "[TT] Payload Power of the EPS = Up to 130 W average"]
-[3.104424476623535, 1.8398332595825195, "[TT] Global Land Color Data Recording Time of the Sentinel-3B = Less than 1.1 days at the equator, and less than 0.9 days in latitudes higher than 30\u00ba"]
-[8.816100120544434, 8.057985305786133, "[FF] Advantages of the Diffracting Optic = Easing of engineering constraints, reduction in mass"]
-[6.142982006072998, 4.515987396240234, "[FF] Function of the GSD = Provide expertise in satellite ground systems design"]
-[9.186976432800293, 4.684628486633301, "[FF] Attitude Control of the FormoSat-2 = Stabilized to the Sun pointing within 60\u00ba"]
-[5.517284393310547, 1.1052879095077515, "[TT] Test Date of the Optical Bench = September 2021"]
-[8.856623649597168, 7.39907169342041, "[TT] Name of the Image Sampling Mode = THR (Tr\u00e8s Haute R\u00e9solution)"]
-[7.854467391967773, -2.49523663520813, "[FF] Observation Area of the GOLD = Global-Scale"]
-[12.096221923828125, 6.444186687469482, "[TT] Electric Charge of the Neutrinos = Neutral"]
-[4.43874454498291, 2.9411613941192627, "[TT] Location of the WCDAS = Wallops, VA"]
-[5.107466220855713, 2.0411832332611084, "[TT] Mission Status of the CAS500 = Operational (nominal)"]
-[8.996809005737305, 5.671111583709717, "[TT] Pointing Accuracy of the ACS = < 5 arcsec"]
-[18.799335479736328, 3.4784741401672363, "[TT] Mean \u0394E (m) of the Jomo Kenyatta = 3.2"]
-[6.198565483093262, 0.4382809102535248, "[FF] Delivery Date of the ROSE-L = 3 December 2020"]
-[8.920083045959473, 5.663829326629639, "[TT] Pointing Accuracy of the ADCS = \u2264 0.1\u00ba (triaxial, 3\u03c3)"]
-[6.723371982574463, -0.6371283531188965, "[TT] Period of the CBERS-2B = 100.26 minutes"]
-[8.634258270263672, 0.37578141689300537, "[TT] Diameter of the Ryugu asteroid = 1-km"]
-[7.82849645614624, 3.0208044052124023, "[FF] Function of the CO2 retrieval subsystem = XCO2 retrieval based on the observation data, and for the provision of CO2 data products"]
-[3.8344550132751465, 7.165927886962891, "[TT] Amplification of the Patch Array Antenna = Approximately 9.8 dB"]
-[9.526185035705566, 7.606151580810547, "[TT] Spatial Resolution of the SV-24 imager = 1 m"]
-[5.237739086151123, 0.5696459412574768, "[TT] Partnership Date of the SpaceChain = Sept. 28"]
-[8.384865760803223, 7.2429633140563965, "[TT] Number of Pixels of the ABI = Four times the current GOES Imagers"]
-[8.474169731140137, 7.446177959442139, "[TT] Type of the DU = CMOS APS (Active Pixel Sensor)"]
-[8.49279499053955, 7.891207218170166, "[TT] Array Size of the NIR = 80 x 640"]
-[6.5264105796813965, -1.9946720600128174, "[TT] Mission Extension Risk of the Jason-2/OSTM = Low Risk"]
-[7.120832920074463, 6.6285319328308105, "[FF] Detection Efficiency Map of the GLM = Shown in Figure 66"]
-[2.9658823013305664, 1.9739649295806885, "[FF] Image Date of the Copernicus Sentinel-5P = 2 July 2018"]
-[8.339953422546387, 4.732413291931152, "[FF] Components of the AOCS = Four reaction wheels, a dual redundant AIM (AOCS Interface Module), dual redundant gyros, dual redundant ST (Star Trackers) and four sun sensors"]
-[4.381446838378906, 6.951780319213867, "[TT] RF Communications of the Satellite = S-band and X-band"]
-[6.4070281982421875, 2.0280303955078125, "[FF] URL of the SREM = http://www.oerlikon.com/ecomaXL/get_blob.php?name=SREM_Brochure&download=1"]
-[3.703808546066284, 3.827418327331543, "[TT] Launch Date of the RISAT-1 = 2018"]
-[12.14056396484375, 1.9744726419448853, "[TT] Launch Date of the CartoSat-2B = July 21, 2010"]
-[7.060657501220703, 0.8602392673492432, "[FF] Overview Seminar of the Gravity Probe B = June 17, 2009"]
-[5.180923938751221, 0.8217332363128662, "[TT] Launch Date of the ASNARO = November 2014"]
-[14.04538345336914, 3.0316154956817627, "[TT] Mass of the GeoCarb = 138 kg"]
-[5.0335845947265625, 2.876599073410034, "[TT] Managing Contractor of the YES2 = Delta-Utec SRC (Space Research & Consultancy)"]
-[10.79738712310791, 3.903107166290283, "[FF] Deployment Mechanism of the CanX-7 = Stored mechanical energy"]
-[9.096399307250977, 3.8507883548736572, "[FF] Disturbance Models of the Controls = Solar radiation pressure variation, capacitive sensing noise, thruster and star tracker noise, acceleration noise on the test mass"]
-[5.4714531898498535, 3.812307119369507, "[FF] Number of Terran R launches of the Terran R = More than 20"]
-[4.47889518737793, 6.77353572845459, "[FF] RF Communications of the exactView-1 = S-band TM/TC (Telemetry/Telecommand) for satellite operations"]
-[5.193305492401123, 3.0537118911743164, "[TT] Operator of the EDRS = Eutelsat"]
-[10.437443733215332, 5.767402648925781, "[TT] Temperature of the IEC = Room temperature"]
-[6.164012908935547, 2.240572214126587, "[TT] Principal Investigator of the NICER = Keith Gendreau"]
-[5.238188743591309, 2.141394853591919, "[TT] Mission Status of the FalconSat-3 = Mission complete"]
-[7.176447868347168, 2.866175889968872, "[TT] Ground Communications of the MethaneSAT = Commercial ground communications companies"]
-[3.778120279312134, 4.638942241668701, "[TT] Cross-Track Velocity Components of the RADARSAT-2 = 5 m/s"]
-[5.686213970184326, 0.6404291987419128, "[TT] On-orbit Checkout Completion Date of the F-16 = Nov. 20, 2003"]
-[8.602777481079102, 8.780463218688965, "[FF] Function of the Herschel Telescope = Look deep into space by detecting light emitted in the far-infrared and sub-millimeter regions of the spectrum"]
-[13.842264175415039, 6.956004619598389, "[FF] Voltage of the CPU = 300 V"]
-[7.626632213592529, 3.4533724784851074, "[TT] Instrument of the Harmony Satellite = Multibeam Thermal-Infrared Instrument"]
-[13.979228019714355, 7.186526298522949, "[TT] Voltage of the Voltage 5 = 3.8\u00b12%"]
-[7.9556684494018555, 8.657800674438477, "[FF] Visible/Reflected Channels of the AATSR = 0.55, 0.66, 0.87 \u03bcm"]
-[4.803746700286865, -1.8141610622406006, "[TT] Orbit Maintenance of the Chang'e-2 = Three times"]
-[10.627843856811523, 4.179309368133545, "[TT] Formation Resize of the FF mission = 25 to 250 m"]
-[4.978733062744141, 5.8677191734313965, "[TT] Radio Frequency Ranging Algorithms of the GAMALINK Platform = Implemented"]
-[5.4391679763793945, 2.7487680912017822, "[TT] Managed By of the Swift = NASA's Goddard Space Flight Center in collaboration with Penn State in University Park, the Los Alamos National Laboratory in New Mexico and Northrop Grumman Innovation Systems in Dulles, Virginia"]
-[8.158114433288574, 5.082045078277588, "[FF] Purpose of the GIRO = Address the increasingly challenging calibration needs for the next generation of satellite instruments"]
-[5.500589847564697, 0.6808178424835205, "[FF] Data Sharing Date of the ENVISAT-1 = Dec. 1, 2016"]
-[9.365568161010742, 5.923906326293945, "[TT] Close Position Angle of the CSM = 0\u00ba"]
-[7.791370391845703, 7.4969024658203125, "[TT] Data Depth of the Infrared Sensors = 8 bit"]
-[9.679386138916016, 4.130143165588379, "[TT] Range of the Magnetometer = \u00b160 \u00b5Tesla"]
-[13.406140327453613, 5.528924942016602, "[TT] Solar Array Type of the EPS = Fixed"]
-[7.7622504234313965, 5.943987846374512, "[FF] Design Purpose of the CrIS = Provide an optimum combination of optical performance and compact packaging"]
-[10.035372734069824, -1.3564515113830566, "[TT] Orbital Inclination of the ICESat-2 = 92\u00b0"]
-[9.707582473754883, 7.274817943572998, "[FF] Ground Sample Distance of the ASNARO = Comparable to GeoEye-1, WorldView-2 and Pleiades-HR"]
-[3.9528050422668457, 6.188886642456055, "[FF] Hardware of the FFRF Subsystem = One terminal and up to 4 sets of antennas on each satellite"]
-[8.714264869689941, 3.2864303588867188, "[FF] Operation of the SIMBA = Measures the total outgoing flux from the whole Earth"]
-[7.468318939208984, 7.927652359008789, "[TT] Dynamic Range of the EXI instrument = 12 bit, 13,500 e full well"]
-[6.961134433746338, 6.199909210205078, "[TT] Number of Instruments of the AMS-02 = 7"]
-[5.209259510040283, -0.8307662606239319, "[TT] Braking Burn Time of the Queqiao = 13:32 UTC"]
-[3.8820040225982666, 0.18057335913181305, "[FF] Development and Lessons Learnt Presentation Date of the SMART-1 = Oct. 4-8, 2004"]
-[5.878566741943359, 0.886314332485199, "[TT] Stowage Date of the ShadowCam = 12 August 2021"]
-[10.28798770904541, 5.494239807128906, "[TT] Cooler Face Temperature Achievement of the TCS (Thermal Control Subsystem) = 95 K"]
-[11.484156608581543, 5.497036457061768, "[TT] Density of the Haynes 242 = 9050 kg/m3"]
-[4.362543106079102, 0.09973923861980438, "[TT] Starlink Satellites Launch Date of the SpaceX = 14 March 2021"]
-[4.654787540435791, 8.038623809814453, "[TT] Operating Frequency of the ALT Experiment = 13.56 GHz"]
-[10.98785400390625, 5.784267425537109, "[TT] Thickness of the CsI(Na) Shield = 2 cm"]
-[7.673871994018555, 4.94691276550293, "[FF] Navigation of the Lander = Absolute sensors determine the position and velocity with respect to the landing site"]
-[4.5111613273620605, 1.5147000551223755, "[TT] Launch Date of the GEOSAT = 12 March 1985"]
-[8.004631042480469, 8.67153549194336, "[TT] Spectral Range of the TAC = 500 - 800 nm"]
-[8.667069435119629, 5.901189804077148, "[TT] Absolute Calibration Accuracy of the Coarse Lateral Sensor = 0.14 camera pixels (5 arcsec)"]
-[8.727879524230957, -0.22536396980285645, "[TT] Perigee (km) of the Cosmos-1066 (Astrofizika) = 848"]
-[14.25012493133545, 3.2462053298950195, "[TT] Mass of the MISSE-FF = ~435 kg"]
-[8.313945770263672, 0.8730669617652893, "[FF] Purpose of the DCAM3 = Obtain close up views of impact"]
-[9.01255989074707, 7.920567035675049, "[TT] IFOV of the INSAT-3D imager = 28 \u00b5rad for VIS and SWIR, 112 \u00b5rad for MWIR, TIR-1, & TIR-2, 224 \u00b5rad for WV"]
-[1.7687201499938965, -2.0558810234069824, "[FF] Schematic of the Hayabusa and Hayabusa-2 = Figure 3"]
-[4.294687271118164, 2.4322173595428467, "[TT] Launch Site of the Yubileyniy-2/MiR = Plesetsk Cosmodrome, Russia"]
-[4.224929332733154, 2.587756395339966, "[TT] Launch Site of the SpaceX CRS-19 = Space Launch Complex 40 (SLC-40) at Cape Canaveral Air Force Station, Florida"]
-[8.242776870727539, 4.021005153656006, "[FF] Surface Treatment of the ASME = Special surface treatment"]
-[7.252581596374512, 4.284923553466797, "[FF] Unknown of the In Situ Impact Sensor = Unknown"]
-[13.763413429260254, 3.1365087032318115, "[FF] Mass of the ICEcube-1, -2 = Unknown"]
-[12.083250999450684, 4.551095008850098, "[TT] Size of the Spacecraft = 700 mm x 700 mm x 554 mm"]
-[8.117231369018555, -1.0365040302276611, "[FF] Purpose of the ICESat-2 = Measure ice height"]
-[6.91722297668457, 5.691576957702637, "[TT] Quantity of N-DPUs of the Main Electronics Unit (MEU) = 14"]
-[5.195321559906006, 0.549372136592865, "[FF] Launch Date of the SpaceX Satellite = July 14, 2009"]
-[10.030436515808105, -1.5368378162384033, "[TT] Orbit Inclination of the Primary Mission = 98.7\u00ba"]
-[4.995847225189209, 3.295207977294922, "[TT] Manufacturer of the SciSat/ACE = Canadian industry"]
-[8.658029556274414, 7.71847677230835, "[TT] Pixel Count of the Detector array = 1280 x 1024 pixels"]
-[4.912957191467285, 3.292069911956787, "[TT] Fairing Manufacturer of the Ariane 5 = RUAG Space"]
-[3.9381377696990967, 2.0615763664245605, "[TT] Launch Vehicle of the OCO-2 = Delta-2 7320-10C"]
-[8.969931602478027, 5.037569999694824, "[TT] Variation of the Range Correction = From 5.28 m at the zenith to 3.08 m near the horizon"]
-[9.420442581176758, 1.2139354944229126, "[FF] Distance from the Sun of the Voyager 1 = Beyond the heliosphere"]
-[7.5469183921813965, -0.298462837934494, "[TT] Launch Date of the Lunar IceCube = 2021"]
-[7.9242024421691895, 1.9551823139190674, "[FF] Level 1 Calibrated Geolocated Radiances of the ECOSTRESS = 6 months after IOC"]
-[9.509617805480957, 5.475099563598633, "[TT] Integration of the GMR sensors = Chips located on the sides of a cube"]
-[9.614837646484375, 7.06350040435791, "[TT] Angular Resolution of the CIRiS = 0.00122 radians"]
-[7.132806777954102, 5.560929298400879, "[FF] Quantity of the MSU-SR = 2"]
-[13.221632957458496, 5.2694807052612305, "[TT] Solar F10.7 cm fluxes Range of the PEM (Parameterized Exospheric Model) = 80-230 x 10-22 W m-2 Hz-1"]
-[4.888065814971924, 0.2752103805541992, "[TT] Impact Date of the DART = Late 2022"]
-[1.7209235429763794, 6.14219331741333, "[FF] Hypothetical Energy Component of the Dark Energy = Unknown"]
-[9.21866512298584, 5.370736122131348, "[TT] Instrument Boresight of the TanSat = Within 5\u00ba of the principal plane"]
-[9.014799118041992, 2.6481680870056152, "[FF] Mission of the CuSP = Study Solar Particles"]
-[7.711272716522217, 1.7939585447311401, "[FF] Purpose of the Satellite = Monitor soil moisture and groundwater wetness"]
-[8.05959415435791, 6.1800127029418945, "[FF] Analysis of the Unresolved Imagery = Analyzing the spectral frequencies and temporal changes in the intensity"]
-[5.884696006774902, 4.910074710845947, "[FF] Services of the General Purpose Communication Network = Data exchange with any other external system"]
-[13.762232780456543, 5.669843673706055, "[TT] Solar Panel Efficiency of the AprizeSat = 28.3%"]
-[7.873109817504883, 2.1202614307403564, "[TT] Main Measurement Objective of the POLDER-2 = Ocean colour"]
-[11.452589988708496, 4.715327262878418, "[TT] Length of the TT = 6.80 m"]
-[5.310853004455566, 1.2299211025238037, "[FF] Conference Date of the European Re-entry Program = Aug. 19-22, 2013"]
-[5.415772914886475, -0.2733379602432251, "[TT] Deployment Time of the STPSat-6 = About 6 hours, 30 minutes after launch"]
-[3.4944512844085693, 4.918046951293945, "[FF] Digital Technology Elements of the Synthetic Aperture Radar = Advanced"]
-[5.095402717590332, 3.325087785720825, "[TT] Manufacturer of the NEXT-C = NASA's Glenn Research Center"]
-[12.431949615478516, 0.5586937665939331, "[TT] New Lead of the PLATO = Heike Rauer (DLR)"]
-[5.515953540802002, 7.042510986328125, "[TT] Data Transmission Speed of the OceanSat-2 = 4 kbit/s"]
-[4.380780220031738, 4.977523326873779, "[FF] Signal Detection of the COSPAS-SARSAT = Emergency signals"]
-[8.01906967163086, 5.153683662414551, "[TT] Mounting of the CH4 and O2 sensors = Three flexures and an adapter ring"]
-[5.208515167236328, 8.336971282958984, "[TT] Window Channels of the AMSU-A = 23.8, 31.4, 50.3, 89.0 GHz"]
-[6.852415084838867, 1.9251713752746582, "[FF] URL of the NASA's Spaceborne Carbon Counter = http://www.jpl.nasa.gov/news/news.php?release=2014-435"]
-[8.085297584533691, -1.1197104454040527, "[FF] Purpose of the Laser Altimeters = Calculate the distance between the aircraft or the satellite and the ice surface"]
-[4.590510368347168, 0.7004250288009644, "[TT] ADCS Malfunction of the Monitor-E = Sept. 2006"]
-[6.456836223602295, 1.3915882110595703, "[FF] Launch Date of the COSMO-SkyMed Second Generation = 18 December 2019"]
-[8.160205841064453, -0.719520628452301, "[TT] Thinning Rate of the Thwaites ice shelf = About 16 feet (5 meters) per year"]
-[5.338770866394043, 0.4871659576892853, "[TT] Launch Date of the NuSTAR = June 13, 2012"]
-[10.321106910705566, 7.423243999481201, "[TT] Design of the Herschel Telescope = Classic Cassegrain with a 3.5 m primary mirror"]
-[12.457438468933105, 0.5749746561050415, "[TT] Operation Duration of the Plato = 4 years"]
-[13.40265941619873, 6.769124984741211, "[TT] Power of the KOMPSAT-5 = 1.4 kW"]
-[9.298226356506348, 5.44252347946167, "[TT] Pointing Stability of the ASTERIA = Best performance to date for spacecraft of its size"]
-[8.058648109436035, 8.804647445678711, "[TT] Phase of the UV2VIS SO = Engineering and Qualification Model"]
-[11.150053024291992, 3.2451744079589844, "[FF] URL of the \u00b5CAT Micro-Propulsion Solution = https://digitalcommons.usu.edu/cgi/viewcontent.cgi?referer=&httpsredir=1&article=3374&context=smallsat"]
-[6.34753942489624, -0.6416670680046082, "[TT] Acquisition Request Acceptance Time of the ASNARO spacecraft = Until 30 minutes before uplink"]
-[13.27896499633789, 7.051809787750244, "[TT] Power Dissipation of the SVM = 330 W"]
-[5.226754665374756, -0.9507901072502136, "[TT] Communication Sessions of the Kolibri-2000 = Over 230"]
-[13.22909927368164, 7.2867841720581055, "[TT] Power Consumption of the NewMag = 3 W"]
-[8.256861686706543, -0.5961213111877441, "[TT] Dimensions of the Fletcher's Ice Island = 7 kilometres by 12 kilometres"]
-[4.119289875030518, 4.281408309936523, "[FF] Employing Teams of the Radar Remote Sensing = Institute for Telecommunications in Portugal and the University of Stirling in Scotland"]
-[8.086451530456543, 5.825015544891357, "[FF] Detector Alignment of the MVIRI = The misalignment due to these displacements is corrected by central on-ground image processing before the images are distributed to users"]
-[6.065396308898926, 1.876729965209961, "[FF] Mission of the SWOT = Future Project"]
-[4.439990043640137, 1.1102935075759888, "[TT] Establishment Date of the GMES = 1998"]
-[13.754197120666504, 2.874354839324951, "[TT] Mass of the Spacecraft = 1220 kg"]
-[6.727965354919434, 5.531159400939941, "[FF] Real Time Clock and Calendar (RTCC) of the dsPIC33F microcontroller = Unknown"]
-[6.095531940460205, 1.7551209926605225, "[TT] Principal Investigator of the ASTERIA = MIT's Sara Seager"]
-[5.18414306640625, 4.886420726776123, "[FF] GNSS Signals of the Pyxis-RO = GPS (L1 at 1575.42 MHz and L2 at 1227.6 MHz), Galileo (E1 at 1575.42and E5 at 1207.14MHz), GLONASS (FDMA signals centered at L1 at 1602 MHz and L2 at 1246 MHz), and BeiDou (B1 at 1561.1 MHz5and B2 at 1207.14 MHz)"]
-[5.850735664367676, 1.8352491855621338, "[TT] Launch Date of the Orion spacecraft = Nov. 10, 2014"]
-[3.650057315826416, 3.7803452014923096, "[TT] Start of Operations of the CCC (Coordinated Constellation Concept) = 2014"]
-[6.128203868865967, 5.614352703094482, "[TT] Redundant Chains of the G-EPS = 4"]
-[7.360551834106445, 5.536525726318359, "[FF] Failure of the VIRR = Early failure of the instrument limited its usefulness"]
-[6.189560413360596, 3.2194178104400635, "[FF] Refueling of the OSAM-1 = Yes"]
-[8.181024551391602, 5.902924537658691, "[FF] Objective of the CVSE = To demonstrate and to qualify a new vibration suppressing design by employing piezo materials"]
-[10.980705261230469, 2.0521700382232666, "[TT] Launch Date of the XMM-Newton = End of 1999"]
-[10.793893814086914, 2.099865674972534, "[FF] Science Highlights of the XMM-Newton observatory = Various discoveries listed"]
-[5.018002033233643, 1.0472451448440552, "[TT] Launch Date of the ALOS-2 = May 29, 2012"]
-[10.2571439743042, -1.3167002201080322, "[TT] Inclination of the ELaNa-4 CubeSats = 40.5\u00ba"]
-[6.2979021072387695, 0.37750911712646484, "[TT] Lifetime of the ROSE-L = 7.5 years"]
-[14.06793212890625, 4.041269302368164, "[TT] Mass of the Instrument = 51 kg"]
-[5.426578998565674, 3.8786046504974365, "[TT] Number of Doves Onboard of the PSLV-C37 = 88"]
-[9.726799011230469, 4.574397563934326, "[TT] Type of the Attitude Subsystem = Passive magnetic stabilization"]
-[4.3179473876953125, 7.141170978546143, "[TT] Band of the RF Communications = S-Band"]
-[6.117759704589844, 1.5929756164550781, "[FF] Publication Date of the Shuttle Radar Topography Mission = 1998"]
-[11.485548973083496, 4.866119384765625, "[TT] Diameter of the Central Obstruction = 68 mm"]
-[9.523856163024902, 4.835972309112549, "[TT] Stabilization Method of the HAUSat-2 = 3-axis stabilized using bias momentum method in the pitch axis"]
-[5.683812618255615, 3.1663010120391846, "[FF] Program of the InSight = Manages by JPL"]
-[6.875528335571289, 4.282327651977539, "[FF] Type of the MTG-S = Sounder"]
-[5.699483871459961, -0.8662562966346741, "[TT] Design Life of the SEOSat = 7 years"]
-[13.412139892578125, 5.5935797691345215, "[TT] Solar Arrays Type of the Power Subsystem = Sun-tracking"]
-[6.680093765258789, 1.8447133302688599, "[FF] URL of the Exo-Brake = https://gameon.nasa.gov/2016/12/13/nasas-exo-brake"]
-[9.601828575134277, -0.43526747822761536, "[TT] Final Altitude of the FormoSat-2 = 891 km"]
-[4.57293176651001, 0.4384208917617798, "[TT] Next Launch Date of the Soyuz = Spring of 2022"]
-[8.757883071899414, -0.26082348823547363, "[TT] Apogee (km) of the Cosmos-1066 (Astrofizika) = 908"]
-[13.407160758972168, 7.29844331741333, "[TT] Power of the S/C = 65 W"]
-[4.893032550811768, 8.330286026000977, "[TT] Operating Frequencies of the SMMR = 6.6 GHz, 10.7 GHz, 18.0 GHz, 21.0 GHz, 37.0 GHz"]
-[8.599905014038086, 8.334907531738281, "[TT] Spectral Resolution of the Sensor = 20 m"]
-[6.406185626983643, 5.460183620452881, "[TT] Status of the DCS = Fully operative"]
-[4.390706539154053, 7.90699577331543, "[TT] Downlink Frequency of the DRT = 4506.05 MHz"]
-[6.754491806030273, 3.6748688220977783, "[TT] Use of the Robotic Arm = In space"]
-[10.028268814086914, -1.5749655961990356, "[TT] Inclination of the LAGEOS = 109.84\u00ba"]
-[8.126606941223145, 5.872504711151123, "[TT] Orbital Distance Measurement Accuracy of the LASSO = Within 0.1 m"]
-[4.8109846115112305, 0.37669816613197327, "[TT] Launch Date of the Spektr-RG = 21 June"]
-[13.848616600036621, 5.633636474609375, "[TT] Efficiency of the Triple Junction Cells = 24%"]
-[11.280363082885742, 0.48912563920021057, "[FF] Sky Observation Swath of the Transiting Exoplanet Survey Satellite = 24-by-96-degree"]
-[9.123767852783203, 1.3195167779922485, "[FF] Ultima Thule Flyby Date of the New Horizons = Unknown"]
-[9.645715713500977, 6.7341532707214355, "[FF] Shape of the Ceres = Almost spherical"]
-[6.511876106262207, -1.98887300491333, "[TT] Recommended Mission Extension of the Jason-2/OSTM = 2013"]
-[13.850309371948242, 5.6870808601379395, "[TT] Efficiency of the Solar Array Regulator = Above 94%"]
-[8.175273895263672, -0.22689196467399597, "[FF] Minimum Runoff of the Greenland = 247 billion tons in 2017"]
-[6.760365009307861, 6.213433265686035, "[TT] Number of Potential Sites of the Sampling Sites = 12"]
-[8.644911766052246, 1.2163352966308594, "[FF] Data Quality of the Aquarius = Impressive"]
-[11.370058059692383, 4.349453926086426, "[TT] Size of the RSat-P = 3U"]
-[5.437798023223877, 7.046534538269043, "[TT] Transmission Speed of the KIZUNA = 3.2 Gbit/s"]
-[13.980422019958496, 7.18858003616333, "[TT] Voltage of the Voltage 7 = 3.5\u00b12%"]
-[10.153098106384277, 5.348940849304199, "[FF] Components of the Cooling System = Pulse-tube cooler, symmetric compressor"]
-[7.056121826171875, 7.038382530212402, "[FF] Performance Anomaly of the Laser002 = Energy monitors dropped suddenly"]
-[10.232614517211914, 5.695859432220459, "[FF] Temperature Reporting of the CCRR = Thermistors on the CCRR will report the temperature of the CCRR in-flight"]
-[4.488373279571533, 7.7506632804870605, "[TT] Uplink Frequency of the Astrodev Lithium 2 Radio = 449.75 MHz"]
-[9.166383743286133, 6.88682746887207, "[TT] Resolution of the Gen-3 Satellites = 50-centimeter"]
-[8.92449951171875, 4.911169528961182, "[TT] Number of Sensors of the SEIS = Six"]
-[3.937112808227539, 1.985198974609375, "[TT] Launch Vehicle of the CHOMPTT = Rocket Lab USA Electron"]
-[7.710526466369629, -0.8628137111663818, "[TT] Publication Date of the ICESat\u20102 = 10 March 2020"]
-[14.413745880126953, 6.5529913902282715, "[TT] Eclipse Capability of the Satellite = 100 % payload operation; battery max. 75% EOL"]
-[8.884993553161621, 6.820211410522461, "[TT] Image Archive of the SPOT-4 = 100 billion km2"]
-[9.453203201293945, 7.123921871185303, "[TT] Spatial Resolution of the WFC = 125 m"]
-[3.4552736282348633, -0.9060705900192261, "[TT] Orbit Type of the Satellite Constellation = Elliptical sun-synchronous dawn-dusk"]
-[5.956831932067871, 0.28020480275154114, "[TT] End of Operations Date of the Rosetta = 30 September"]
-[8.262747764587402, 7.337929725646973, "[FF] Gain Control of the MCP (Microchannel Plate) Detector = Voltage applied across the MCP"]
-[7.9621171951293945, 5.341639995574951, "[TT] Accuracy of the FLLS = High"]
-[5.516478061676025, 1.241856336593628, "[FF] Presentation Date of the Sapphire = AMOS 2012"]
-[10.789725303649902, 4.630486488342285, "[FF] Simulation of the YES2 satellite = Space Tether Deployment on Earth"]
-[14.263794898986816, 3.2006304264068604, "[TT] Mass of the PSU = 8 kg"]
-[9.234844207763672, 3.19279408454895, "[FF] Article Author of the Magnetospheric Multiscale Mission = Mara Johnson-Groh"]
-[6.66456937789917, 5.1940460205078125, "[TT] Components of the C&DH subsystem = Controller card (CC), data handling card, Power Supply Card (PSC), Input/Output Card (IOC), Mission Interface Card (MIC)"]
-[11.995758056640625, 3.303142786026001, "[TT] Isp of the iodine BIT-3 propulsion system = >2,000 s"]
-[9.482909202575684, 5.989348411560059, "[TT] Angle Between Fixed Panels of the CHEOPS = 67 degrees"]
-[6.28646183013916, -0.4595614969730377, "[TT] Autonomy Duration of the Spacecraft autonomy = Eight hours"]
-[4.881232738494873, 7.123403072357178, "[TT] Nominal Rate of the S-band Uplink = 16 kbit/s"]
-[8.083061218261719, 3.61142635345459, "[TT] Measurement Locations per Day of the OCO-3 = Up to 40"]
-[6.556739330291748, 2.6640288829803467, "[FF] Symposium Date of the Weather Satellite Follow-On \u2013 Microwave (WSF-M) = 13-16 January 2020"]
-[8.725834846496582, 5.941300392150879, "[FF] Measurement Range of the O3 Profile = 0-2 km(ppbv)"]
-[8.29088306427002, 6.403459072113037, "[TT] Measurement Rate of the SSM = 12 readings/s"]
-[7.667651653289795, 8.784859657287598, "[TT] Spectral Ranges of the MSU-E = 0.5 - 0.7 \u00b5m, 0.7 - 0.8 \u00b5m, and 0.8 - 1.0 \u00b5m"]
-[3.7335100173950195, 2.3883888721466064, "[FF] Launch Date of the Iridium NEXT = June 2010"]
-[8.493880271911621, 7.413821220397949, "[TT] Detection Limit at 6 \u00b5m of the Instrument = 3 x 10 -4  W m -2  sr -1  s m"]
-[7.8804612159729, 1.814674735069275, "[TT] Purpose of the Broadband InfraRed Compact High Resolution Explorer Spectrometer (BIRCHES) = Prospect for water in ice, liquid, and vapor forms"]
-[5.284260272979736, 4.609532356262207, "[FF] Issue of the TT&C System = Spacecraft ignoring commands from the ground stations"]
-[7.0443830490112305, 0.845975399017334, "[FF] Mission Update of the Gravity Probe B = Nov. 12, 2009"]
-[5.072276592254639, -0.37836605310440063, "[FF] Joint Tests Date of the CBERS 3 = March 29, 2011"]
-[4.832386493682861, 1.878956913948059, "[FF] Altimetry of the Geosat = W. H. F. Smith, D. T. Sandwell"]
-[5.667507171630859, 2.8690738677978516, "[FF] Funding of the SRTM = NIMA"]
-[9.935677528381348, 4.9106831550598145, "[TT] Rotation Time of the Filter Wheel = 100 ms"]
-[5.173652648925781, 7.568441390991211, "[FF] Function of the MIRU = Is co-integrated with the STR CHU delivering angular rates at high bandwidth"]
-[5.633012771606445, 7.881277084350586, "[TT] Quantity of the Solid state power amplifiers = 1"]
-[10.291938781738281, 1.3643542528152466, "[TT] Star Formation Rate of the Cluster XDCPJ0044.0-2033 = Almost two thousand solar masses per year"]
-[5.397877216339111, 2.331157684326172, "[FF] Agency of the MOMS = DLR"]
-[10.796345710754395, 2.840501308441162, "[TT] Mission Design Life of the PARASOL microsatellite = One year"]
-[4.991955757141113, -0.6218675971031189, "[FF] Perigee Point Wait Time of the SLATS = 15min"]
-[9.633682250976562, -0.320223331451416, "[TT] Altitude of the EFT-1 = Approximately 5800 km"]
-[7.668356895446777, 0.45138871669769287, "[TT] Funding of the Lunar IceCube = NASA\u2019s Next Space Technologies for Exploration Partnerships program"]
-[4.055011749267578, 0.3223954737186432, "[TT] Launch Date of the Corvus-BC 5 = November 20, 2020"]
-[5.834666728973389, 3.228290557861328, "[FF] Number of Spaceships of the Cygnus-15 = 1"]
-[7.615580081939697, 5.217864513397217, "[TT] Acoustics Test of the GOES-S = Completed"]
-[5.122358798980713, 1.1554186344146729, "[FF] Presentation Date of the UniSat-3 = Oct. 2-6, 2006"]
-[5.413488864898682, 0.8551396131515503, "[FF] Launch Date of the Hera = Unknown"]
-[7.666159629821777, 1.9457799196243286, "[FF] Measures of the FLUXNET = Forest canopy fluxes of carbon dioxide and other key environmental variables"]
-[4.931106090545654, -0.02707512304186821, "[FF] Funding Renewal Date of the CUTE = May 2019"]
-[4.836750030517578, 0.5203813314437866, "[TT] Launch Date of the CLARREO Pathfinder = Late CY2022"]
-[4.927048683166504, 3.313446283340454, "[FF] Japanese Contribution to IEOS of the ADEOS-II = WCRP/GEWEX & CLIVAR, IGBP and GCOS"]
-[4.538708209991455, 3.4611899852752686, "[TT] Ground Station of the KySat-1 = Space Science Center at Morehead State University (MSU)"]
-[3.0965747833251953, 1.8641979694366455, "[TT] Global Surface Temperature Data Recording Time of the Sentinel-3B = Less than 0.9 days at the equator and in less than 0.8 days in latitudes higher than 30\u00ba"]
-[10.030095100402832, 7.456225395202637, "[TT] Telescope Offset of the Instrument = 50\u00ba"]
-[7.863658905029297, 0.8745140433311462, "[FF] Date of the Floods Swamp Bangladesh = 24 June 2022"]
-[5.843564510345459, -0.7606847882270813, "[TT] Satellite lifetime of the Legion = >10 years"]
-[7.4507293701171875, 2.5097174644470215, "[TT] Measurement Category of the KySat-2 = Multi-purpose imagery (land)"]
-[4.217148303985596, 4.236880779266357, "[TT] Establishment Year of the Cospas-Sarsat = 1982"]
-[9.856231689453125, 8.777109146118164, "[TT] FOV of the L-band = 1000 km"]
-[9.547928810119629, 0.7721022367477417, "[TT] Distance from the Sun of the Vigil = 150 million km"]
-[8.373971939086914, 5.945938587188721, "[TT] Sensitivity of the STROFIO = 0.14 counts/s when the density is 1 particle/cm3"]
-[4.930160999298096, 8.39522647857666, "[TT] Spectral Band of the MTVZA = 18.7-183.3 GHz"]
-[8.121261596679688, 1.4604196548461914, "[TT] Rainfall Measurement of the GPM = Up to 50 mm per hour"]
-[5.835096836090088, 5.064244747161865, "[FF] Communication of the DSAT-1 = Does not have a communication link directly with Earth"]
-[3.7027194499969482, -1.080472707748413, "[TT] Orbit Type of the Rstar = Elliptical"]
-[9.10543441772461, 2.679837703704834, "[TT] Severity of the Geomagnetic Storm = G2"]
-[5.237288951873779, 3.227769613265991, "[FF] Syndicate Members of the Heinrich Hertz = Tesat-Spacecom GmbH, Audens Telecommunications Consulting, DLR/GSOC, SciSys Deutschland GmbH, HPS, INVENT, Astrium, Inradios GmbH, Dresden, and DLR/IKN"]
-[1.7181038856506348, 6.140143394470215, "[TT] Dark Energy Percentage of the Universe = 70 percent"]
-[8.401792526245117, 7.3867268562316895, "[TT] Fill Factor of the CMOS Image Sensor = 100%"]
-[6.334506988525391, 5.836936950683594, "[TT] Number of Regulators of the BCR Module = 12"]
-[12.361272811889648, 0.5747448205947876, "[FF] URL of the PLATO = https://www.cosmos.esa.int/web/plato/"]
-[9.942434310913086, -1.6239557266235352, "[TT] Orbit Inclination of the Electron rocket = 85\u00ba"]
-[11.266636848449707, 0.9633985161781311, "[FF] Test Date of the LISA Pathfinder = March 11, 2015"]
-[10.508837699890137, 2.2090847492218018, "[TT] Quantity of X-ray Optics of the NICER/SEXTANT = 56"]
-[6.169054985046387, 4.483414173126221, "[FF] Responsibilities of the MC = Mission planning and scheduling, X-band ground stations data reception scheduling, Payload telecommands management, Commands generation for detectors, PMS, and X-band subsystems, Command execution verification, TC plan (telecommands) sending to the CCC, S-band telemetry data and satellite orbit parameters and attitude data reception from the CCC, Science data reception from X-band stations, Payload health & status monitoring"]
-[4.260789394378662, 7.350757598876953, "[TT] X-band Downlink Frequency of the RF Communications = 8192 MHz"]
-[8.05248737335205, 2.2949891090393066, "[FF] Data Production of the INCUS = About 15 times the data of CloudSat"]
-[10.302053451538086, 7.229482650756836, "[TT] Full Disk Circle Size of the ABI = 17.4\u00ba diameter"]
-[10.601710319519043, 3.700392007827759, "[FF] Dragsail of the CubeSat InflateSAIL = Unknown"]
-[8.481671333312988, 3.3416826725006104, "[TT] Processing Levels of the OSIRIS = 1 and 2"]
-[6.051133155822754, 1.304079532623291, "[TT] Meeting Date of the Swarm = April 21, 2017"]
-[13.42623233795166, 7.357529163360596, "[TT] Power of the DORIS = 20 W"]
-[11.127239227294922, 4.663237571716309, "[TT] Maximum Drill Depth of the SD2 = About 0.2 m"]
-[9.437681198120117, 6.302655220031738, "[TT] Scan Mirror Tilt of the GLI = \u00b120\u00ba from nadir"]
-[6.881671905517578, 3.197176933288574, "[FF] Model Building of the Oculus-ASR = 3D Predictive Satellite Models"]
-[4.595356464385986, -0.36136358976364136, "[TT] Docking Date of the REXJ = July 28, 2012"]
-[6.387897968292236, 8.596654891967773, "[TT] Polarization of the Satellite = Vertical"]
-[4.226836204528809, 7.450071334838867, "[TT] Frequency of the X-band = 10.2 GHz"]
-[3.086836338043213, 2.1950180530548096, "[FF] Observation Objective of the Sentinel-4 = Observing the diurnal cycle of the tropospheric composition over Europe and North Africa"]
-[4.62872838973999, 0.863890528678894, "[TT] Launch Date of the ADEOS-II = Dec. 14, 2002"]
-[10.038098335266113, -1.526841163635254, "[TT] Orbit Inclination of the LitianicaSAT-2 = 97.44\u00ba"]
-[13.358171463012695, 5.480858325958252, "[TT] Solar Array of the Starlink Satellite = Single"]
-[10.273629188537598, 2.1476330757141113, "[FF] Imaging of the XRT = Captured the black moon in the shape of a crescent in front of the solar corona brightened by X-rays"]
-[7.187326908111572, 4.641844272613525, "[FF] Function of the S/C Navigation (GNC-NAV) = Computes the absolute position, velocity and attitude of the spacecraft from sensors data and performs Angular Momentum Management (AMM) monitoring"]
-[9.174460411071777, 4.679702281951904, "[TT] Sun-pointed Attitude Acquisition Time of the XACT = Within 150 seconds"]
-[7.274472236633301, 6.023024082183838, "[TT] Quantity of the GRDs = 5"]
-[7.699251174926758, 8.378029823303223, "[TT] Spectral Bands of the EarthDaily Constellation = Over 21"]
-[4.885035991668701, 2.981951951980591, "[TT] Data Archiving Site of the Deployment Systems = Las Vegas"]
-[13.480072021484375, 5.767030239105225, "[TT] Solar Array Power of the EPS = 180 W EOL"]
-[4.695035934448242, 6.559142589569092, "[TT] RF Communications System of the JWST = CCTS (Common Command and Telemetry System)"]
-[7.330142974853516, 8.469108581542969, "[TT] SP Performance of the SEIS Instrument = < 5 x 10-8 m s-2 Hz-\u00bd from 10-2 up to 100 Hz"]
-[8.180734634399414, -0.978914201259613, "[FF] Objective 3 of the ICESat-2 = Estimate sea ice thickness"]
-[5.110599517822266, 4.95896053314209, "[TT] Quantity of the GPS SGR-20 = 1"]
-[8.709440231323242, 3.3484792709350586, "[FF] Purpose of the SUVI = Provide information on solar activity and the effects of the sun on the Earth and the near-earth space environment"]
-[3.483102560043335, 4.840677738189697, "[FF] Contributions of the DLR = X-SAR hardware, ground systems, mission operations and data processing support"]
-[5.765398025512695, -0.25248536467552185, "[TT] Functionality Duration of the SMDC-ONE = Until reentry on 12 January 2011"]
-[7.680729866027832, 2.3757095336914062, "[FF] Expanded Applications of the SMOS = Monitoring and improving forecasting of large storms"]
-[10.975479125976562, 2.0672545433044434, "[TT] Mission Extension Approval Date of the XMM-Newton = November 20, 2014"]
-[9.171895027160645, 5.650084972381592, "[TT] Jitter Values of the ASTERIA = 1\u03c3 ~5\""]
-[11.480986595153809, 4.784389972686768, "[TT] Structure Shape of the WNISAT-1 = Cubic"]
-[5.716676712036133, 6.637028694152832, "[FF] Report Dissemination of the DCP = Occurs in the 27-second intervals between WEFAX transmissions"]
-[6.114079475402832, 0.44771987199783325, "[TT] Successful Contact of the ASTERIA = Approximately 90 minutes later"]
-[4.778183460235596, 5.835126876831055, "[TT] Beacon Packet Content of the StenSat = The most recent science packet"]
-[8.290265083312988, 8.967976570129395, "[TT] Spectral Resolution of the Argus = 6 nm"]
-[11.730360984802246, 6.7868475914001465, "[TT] Energy Range of the SSJ/5 = 0.3-30 keV"]
-[6.845138072967529, 3.3492441177368164, "[FF] Revisit Frequency of the Satellite Constellation = Near the edge of the scan > Near nadir"]
-[6.92962646484375, -0.26255229115486145, "[TT] Orbits/Day of the FormoSat-2 = 14 orbits/day"]
-[9.002456665039062, 0.3759118616580963, "[TT] Diameter of the Crater = 11 km"]
-[8.083476066589355, 4.449319839477539, "[FF] Radiation Dose Measurement of the SREM = Measures the total radiation dose encountered by SREM itself and at different remote locations onboard the satellite, by using RADFETS"]
-[8.378360748291016, 7.238372325897217, "[TT] Yaw Accuracy of the MBA detector = \u00b10.1\u00ba"]
-[10.446688652038574, 2.307497024536133, "[FF] Technology Objective of the NICER/SEXTANT = Demonstrate celestial-based XNAV ( X-ray Navigation)"]
-[4.622970104217529, 6.94292688369751, "[TT] LISS-I Data Downlink of the Satellite = S-band"]
-[7.218302249908447, 8.542606353759766, "[TT] SNR of the RBV Instrument = 33 dB in bands 1 and 2, 30 dB in band 3"]
-[4.441810131072998, 7.0697197914123535, "[TT] Function of the MEXIC = Format and date housekeeping data in S-band"]
-[8.804381370544434, 0.3781251311302185, "[TT] Polar Regions of the Ryugu = Very few craters"]
-[7.974334716796875, 5.168159484863281, "[TT] Dosimeters Quantity of the Tesseract = 10"]
-[7.676671981811523, 8.846671104431152, "[TT] Spectral Band of the Spectral Block = 758 \u2013 768 nm"]
-[13.218701362609863, 7.327584266662598, "[TT] Power Consumption of the OBC = < 6 W"]
-[10.841364860534668, -0.27311211824417114, "[FF] Mission Concept of the TanDEM-X = Not provided"]
-[11.576613426208496, 3.464366912841797, "[TT] Propulsion of the SES-14 = Electric propulsion"]
-[10.975204467773438, 0.8744753003120422, "[FF] Detection Difficulty of the Brown Dwarfs = Easier than planets"]
-[6.567695140838623, 4.996792793273926, "[FF] Architecture of the NNE (Neural Networks Experiment) = Special feed-forward \u201clearning\u201d architecture"]
-[7.05840539932251, 4.702531814575195, "[FF] Operation Modes of the MPO-MAG instrument = Set of science operations modes"]
-[13.190446853637695, 7.267617702484131, "[TT] Power Consumption of the MC-U = < 4.5 W"]
-[14.30683422088623, 2.9142961502075195, "[TT] Mass of the Ten-Koh = 220 kg"]
-[6.662362575531006, 4.143067836761475, "[FF] Data Products Classification of the HY-1C = Level 0-level4"]
-[3.452714681625366, -0.9173324704170227, "[FF] Type of the Orbit = Sun-synchronous near circular orbit"]
-[5.001357555389404, 6.026830196380615, "[TT] Signal Loss of the Schiaparelli module = After one housekeeping data packet"]
-[8.950791358947754, 4.36630916595459, "[TT] Redundancy of the Coarse Earth sun sensor = Internal (2 of 3)"]
-[8.93044662475586, 4.440590858459473, "[TT] Accuracy of the Sun sensors = 0.2\u00ba (3\u03c3)"]
-[7.93582820892334, 8.621792793273926, "[TT] Spectral Range (VIS) of the VHRR = 0.55 - 0.75 \u00b5m"]
-[6.5398359298706055, 1.9362404346466064, "[FF] URL of the Evaluation = https://earthdata.nasa.gov/esds/csdap/csdap-pilot-evaluation"]
-[5.2639617919921875, 6.298037528991699, "[TT] Processor Speed of the MPM = 50 MHz"]
-[3.3438172340393066, 2.211989402770996, "[FF] Data Availability of the Sentinel-3 = Full, free and open basis"]
-[13.393738746643066, 7.666360378265381, "[TT] Power of the Altimeter Antenna = 237 W"]
-[4.767035007476807, -1.8451846837997437, "[TT] Sample Collection of the Chang'e-5 = Completed"]
-[4.217168807983398, 6.203977108001709, "[TT] Antenna Direction of the GPS/MET = Anti-velocity direction"]
-[6.517267227172852, 3.564727783203125, "[FF] Plan Generation of the MPF = Daily"]
-[5.732846736907959, -0.8958893418312073, "[TT] Design Life of the SAST-5000 = 7 years"]
-[10.99010181427002, 6.24827766418457, "[TT] Material of the X-ray mirrors = Nickel"]
-[11.372206687927246, 4.309954643249512, "[FF] Size of the ALICE = 3U"]
-[4.890416622161865, 0.5256162285804749, "[TT] Launch Date of the PACE = 19 June 2014"]
-[13.498151779174805, 2.8703765869140625, "[TT] Ballistic Number of the Satellite = \u2264100 kg/m2"]
-[8.14155387878418, 0.7540723085403442, "[TT] Average Seasonal Fluctuation of the Water Bodies = 8.6 inches (0.22 m)"]
-[4.217352867126465, 7.331263542175293, "[TT] Spectrum of the Starlink and OneWeb = Ku-band"]
-[6.159850120544434, 7.026081562042236, "[TT] Technology of the Rate Measurement Unit = Solid-state rate sensor"]
-[13.221264839172363, 7.231181621551514, "[TT] Power of the SAGE-III = 80 W average"]
-[4.789559364318848, 7.051845550537109, "[TT] Data Transmission of the QARMAN = Iridium telecom satellites"]
-[6.467982292175293, 7.612838268280029, "[TT] Data Quantization of the Satellite = \u2265 12 bit"]
-[4.317383289337158, 5.617342948913574, "[TT] Accuracy of Cloud Echoes of the CPR = 1 m/s"]
-[11.778639793395996, 6.629742622375488, "[TT] Proton Energy Resolution of the REPT = 30%"]
-[8.050421714782715, -0.9353209733963013, "[TT] Data Coverage of the ICESat-2 = Continuous around the globe"]
-[6.327961444854736, 8.594934463500977, "[FF] Operational Modes of the MIRAS = Dual-polarization or full-polarimetric"]
-[5.698011875152588, 3.4130489826202393, "[TT] Aviation Market Ranking of the India = Third largest"]
-[13.584559440612793, 7.20056676864624, "[TT] Charge Confusion of the TRD = Very small"]
-[4.680927753448486, 6.5923051834106445, "[FF] Components of the Antenna and RF Subsystem = S-band transmitter feed, S-band receiver feed, X-band receiver feed, tracking system"]
-[7.750884056091309, 4.051135063171387, "[FF] Objectives of the CEASE = Develop and demonstrate on-orbit, autonomous, compact, light weight, low-power instrumentation to monitor the environment around a spacecraft, and to provide alerts whenever the environment is likely to cause any of the following anomalies: surface charging, deep dielectric charging, single event upsets (SEU's), or radiation dose effects"]
-[8.811076164245605, 6.907386779785156, "[TT] GSD of the DMC-3 = ~1 m"]
-[9.086761474609375, 6.991774082183838, "[FF] Camera Resolution of the Shakuntala = One of the highest"]
-[5.490699291229248, -0.7553168535232544, "[TT] Actual Mission Duration of the Jade Rabbit = 31 months"]
-[10.388737678527832, 7.225081920623779, "[TT] Secondary Mirror Size of the Telescope = 0.3 m"]
-[6.394340515136719, 1.1543515920639038, "[FF] Conference Date of the COSMIC-2 = March 5-12, 2011"]
-[12.122418403625488, 3.4806525707244873, "[TT] Instrument Mass of the PPCU ion thruster = 43 kg"]
-[6.625360488891602, 0.9218198657035828, "[TT] Data Availability of the Landsat 4 = All TM data January 2009"]
-[9.83668327331543, 5.450191020965576, "[FF] Function of the PIU = Provide feedback controls for gain response versus detector temperature"]
-[8.295766830444336, 6.65995454788208, "[FF] Coupling Ratio of the OGS Data Detector = 90% reach the fiber and 10% the ACT"]
-[6.470523357391357, 7.622507572174072, "[TT] Data Quantization of the Instrument = 10 bit"]
-[14.703067779541016, 6.623213768005371, "[TT] Capacity of the Battery Assembly = 15 Ahr"]
-[8.758306503295898, 3.555177688598633, "[FF] Objective of the CERTO/PLUS = To map the ionospheric electron densities in the satellite's orbital plane and to study the evolution of 1-100 km sized low latitude irregularities using radio/optical tomography techniques"]
-[14.532166481018066, 6.681998252868652, "[TT] Power Generation of the S/C = 46 Whr NiCd battery"]
-[9.554449081420898, 0.3040741980075836, "[TT] Closest Distance to Stone of the Yutu-2 = 1.2 meters"]
-[12.154838562011719, 4.847530364990234, "[TT] Volume of the X-band Transmitter = 240 mm x 196 mm x 185 mm"]
-[7.049530982971191, 2.1347033977508545, "[TT] Avionics Suite of the Carbonite-1 = Deep Thought avionics suite"]
-[4.260161876678467, 3.2005932331085205, "[TT] Downlink Frequency Band of the Svalbard Ground Station = S-band"]
-[4.683468341827393, 0.6142908334732056, "[FF] Launch Date of the GOES-U = Unknown"]
-[9.700453758239746, 8.400915145874023, "[TT] Field of View of the FOV = 0.08\u00ba along track and 1.42\u00ba cross track"]
-[11.917145729064941, 5.000487804412842, "[TT] Size of the Gnome Chompski = 150 mm"]
-[3.198861837387085, 3.8088788986206055, "[TT] Data Collection Start Date of the TerraSAR-X = Early 2011"]
-[6.780179023742676, 7.315099239349365, "[TT] Repetition Rate of the ATLAS = 10 kHz"]
-[12.062151908874512, 6.291855812072754, "[FF] Positron Fraction, Antiproton/Proton Ratio, Electron Flux, Positron Flux, Proton Flux, Helium Flux, and other nuclei fluxes of the AMS = Provide precise and unexpected information"]
-[4.274501800537109, 1.9682152271270752, "[FF] Destination of the Falcon-9 = International Space Station"]
-[6.892675876617432, 8.42870807647705, "[TT] RIN Performance of the ASM Instrument = -105 dB (Hz)^1/2 at 2 mW of output power around 1 kHz"]
-[10.896018028259277, 1.6053521633148193, "[FF] Key to Gravitational Waves Study of the Scotland's Space Expertise = Unknown"]
-[7.564082145690918, 8.688055038452148, "[TT] GSD of the Spectral Band D = 5"]
-[8.491360664367676, 5.588163375854492, "[TT] Location Knowledge Accuracy of the GFO = 10 cm (radial component)"]
-[6.24821138381958, 2.0280885696411133, "[TT] Deputy Project Scientist for Applications of the GPM = Dalia Kirschbaum"]
-[4.967975616455078, 0.2924214005470276, "[TT] Arrival Date of the DART = October 2022"]
-[14.17187786102295, 3.248074531555176, "[TT] Mass of the CHEOPS = 300 kg"]
-[5.146852970123291, 2.2586493492126465, "[TT] Mission Type of the PROBA-3 = Non-EO"]
-[7.5373311042785645, 8.839752197265625, "[TT] Radiometric Accuracy of the Spectral Band D = 3"]
-[5.740370750427246, 1.1685079336166382, "[FF] Bulletin Publication Date of the GPS/MET = April 1998"]
-[8.393109321594238, 6.897604942321777, "[TT] Absolute Accuracy of the IMG = <1 K"]
-[13.819873809814453, 7.33113956451416, "[TT] Input Voltage of the Transmitter = +12 V DC"]
-[11.438424110412598, 3.7598652839660645, "[FF] Size of the Cygnus A jet = One of the largest and most powerful"]
-[9.254672050476074, 1.852087378501892, "[TT] Resolution of the HARP-2 = <6 km"]
-[4.964713096618652, 3.242769479751587, "[FF] Manufacturer of the ASIM = Danish company Terma, the Danish Technical University, the University of Bergen in Norway and the University of Valencia in Spain"]
-[11.65200138092041, 4.768783092498779, "[TT] Size of the LCRD = About the size of a king-sized mattress"]
-[4.3987579345703125, 3.153169870376587, "[FF] Stations of the Ground Network = Aussaguel (France), Fairbanks (AK, Poker Flats location), Wallops Island, VA, and Hartebeesthoek, South Africa"]
-[3.2687528133392334, 4.956360340118408, "[TT] Spatial Resolutions of the RISAT = 1-50 m"]
-[4.058565139770508, 2.163867473602295, "[TT] Launch Vehicle of the QBITO = ULA Atlas 5 -401"]
-[3.391901731491089, 4.717924118041992, "[FF] Image Content of the SAR = Various eddies and plumes"]
-[5.4694671630859375, 3.8850982189178467, "[TT] Number of Satellites to Launch in 2022 of the Satellogic = Up to 12"]
-[8.236674308776855, 6.444847583770752, "[TT] Scanning Rate of the SSULI = Up to 6\u00ba per second"]
-[13.239133834838867, 5.259098529815674, "[TT] Solar Arrays Length of the BepiColombo = 15 m"]
-[5.795242786407471, 0.5224233269691467, "[TT] Orbit Date of the Cluster = December 29, 2006"]
-[8.700994491577148, 3.8887155055999756, "[FF] Measurement Range of the SEI = 2-200 eV electrons or ions"]
-[6.675295829772949, 7.5993170738220215, "[TT] A/D Converter of the RCM3400 = 11 bit 8 channel (or 12 bit 4 channel if used in differential mode)"]
-[9.282512664794922, 3.2187981605529785, "[TT] FOV for Broadband Imaging of the 20 cm off-axis internally occulted coronagraph = 1.05 to 3.0 Rsun"]
-[6.470250606536865, 2.041400671005249, "[FF] URL of the CNES = http://www.ies.univ-montp2.fr/robusta/satellite/IMG/pdf/DD_GN_2010.02.16__ISU2010.pdf"]
-[9.375882148742676, 3.635507106781006, "[FF] Measurement Objective of the GMR = Measure the magnetic fluxes produced by Earth's magnetic field"]
-[9.121602058410645, 7.162075996398926, "[TT] Imaging Resolutions of the PanGeo Fleet = From 20 m to 75 cm/ pixel"]
-[7.432764053344727, 2.940157413482666, "[FF] Resolution of the MethaneSAT = High"]
-[7.693274021148682, 3.0402700901031494, "[FF] XCO2 Hotspots of the TanSat = Eastern China, eastern United States, Europe"]
-[10.02878189086914, -1.5298094749450684, "[TT] Orbit Inclination of the Genesis-2 = 64.5\u00ba"]
-[4.939298629760742, 7.3730058670043945, "[TT] Data Rates (Uplink) of the RF Communications = 1.2 kbit/s"]
-[8.920525550842285, 7.56848669052124, "[TT] Spatial Resolution of the CCD Camera = <= 1 km"]
-[4.828958511352539, -0.30390268564224243, "[TT] Upper Stage Engine Ignition Time of the Falcon 9 = 4:29 a.m. EST"]
-[6.814886093139648, 0.8003233671188354, "[FF] Image Span of the Herschel = 2 x 2 degrees"]
-[5.906987190246582, 1.105755090713501, "[FF] Discovery Date of the NASA Satellite = June 1, 2016"]
-[7.87494421005249, 6.530877590179443, "[TT] Temporal Resolution of the ABI = Every fifteen or five minutes"]
-[4.586931228637695, 1.656006097793579, "[FF] Mission Status Presentation Date of the TanSat = Sept. 9-11, 2015"]
-[14.333890914916992, 6.491087436676025, "[TT] Battery Life of the Astrocast\u2019s devices = Up to 10 years"]
-[5.8561482429504395, 1.989659070968628, "[TT] Landing Method of the Orion = Water"]
-[5.88796854019165, 7.142701625823975, "[TT] Source Data Rate of the Instrument = 20 MByte/s"]
-[3.443220615386963, 6.383002281188965, "[TT] Length of the RF Antenna Mast = Nearly 12 m"]
-[8.715347290039062, 4.954844951629639, "[TT] Bias Error of the Aeolus = 0.4 m/s"]
-[5.413546562194824, 8.735176086425781, "[TT] Bandwidth of the COCTS = 0.027 \u00b5m"]
-[6.7704291343688965, 2.4171900749206543, "[FF] Image Credit of the MODIS = NASA Earth Observatory image by Lauren Dauphin"]
-[6.9885969161987305, 6.118851184844971, "[TT] Number of Instruments of the ISEE-3 = 13"]
-[5.2035908699035645, 2.5817084312438965, "[TT] Mission Type of the MTSAT = EO"]
-[13.440555572509766, 5.455233097076416, "[TT] Solar Array of the Orion = 1242 cells per panel"]
-[10.123820304870605, 2.5833165645599365, "[FF] Calibration of the ART-XC instrument = Unknown"]
-[5.405785083770752, 2.9064574241638184, "[TT] Development Location of the SPIDER = Advanced Technology Center in Silicon Valley"]
-[6.720623970031738, 4.199667930603027, "[FF] Installation Location of the ELF = Upper part of MSPR-2, called the Work Volume (WV)"]
-[9.305830955505371, 1.8147501945495605, "[TT] Quantity of the Harpoon capture system = 1"]
-[10.084904670715332, -2.6845791339874268, "[FF] Advantages of the NAND-Flash technology = Non-volatile data storage capability and substantially higher storage density"]
-[7.342413902282715, 2.825472593307495, "[FF] Purpose of the Satellite = Monitor wildfires"]
-[6.077167510986328, 0.03330479562282562, "[FF] Mapping Duration of the TIMED = 10 Years"]
-[7.603288173675537, 8.147868156433105, "[TT] Color of the Driver Electronics = Green"]
-[4.514112949371338, 1.6410589218139648, "[TT] Launch Date of the NPSat-1 = 25 June 2019"]
-[9.728034973144531, 7.552504539489746, "[TT] Along-Track Resolution of the Nadir Sensor Wide-Field Telescope = 50 km at nadir"]
-[6.119112968444824, 5.041222095489502, "[FF] Process Management of the FreeRTOS = Separation of a program in several processes, managing the assignment of processor internal resources like processor time and memory to the various processes"]
-[10.914119720458984, 7.4858598709106445, "[TT] Swath Width of the Sentinel-2 = 290 km"]
-[10.780928611755371, 1.7926466464996338, "[FF] Mission Type of the XMM-Newton = Follow-up of Gravitational Wave Detections"]
-[7.301620960235596, 4.373096466064453, "[FF] SDR Validation of the VIIRS = Unknown"]
-[1.37093985080719, 2.782057523727417, "[TT] Principal Absorbing Constituents of the Band 6 = Water vapor"]
-[10.142940521240234, 5.381694793701172, "[FF] Function of the HCU = Controls the heaters to maintain the operating temperature"]
-[11.251054763793945, 5.86111307144165, "[TT] Material of the Printed Antenna = CFRP (Carbon Fiber Reinforced Plastic)"]
-[6.082259654998779, 0.45636460185050964, "[TT] Extended Mission Duration of the ASTERIA = Nearly two years"]
-[6.183464050292969, 5.334566593170166, "[FF] Hardware and Software Design of the OBC = Exactly the same as PDH"]
-[3.3957362174987793, 6.434724807739258, "[TT] Diameter of the Antenna = 0.65 m"]
-[6.998810291290283, 7.281274795532227, "[TT] Continuous Operation of the ATLAS laser = 3 years"]
-[9.812216758728027, -0.5692939758300781, "[TT] Orbit Altitude of the ALMASat-1 = 354 km x 1450 km"]
-[9.810897827148438, 4.719233989715576, "[TT] Stabilization of the AOCS = 3 axis stabilized with 4 Reaction Wheels"]
-[11.88351821899414, 3.048494577407837, "[TT] Bipropellant System Total \u0394V Capability of the Clementine = About 1900 m/s"]
-[10.541322708129883, 7.42547082901001, "[FF] Observation Goal of the DELPHINUS = Detect over a hundred LIFs in a month"]
-[7.133129119873047, 7.285806655883789, "[TT] Optical Pulse Size of the LI = 10 km - 100 km circular pulse diameter"]
-[7.7756028175354, 8.039947509765625, "[TT] Sensitivity of the SSULI = 0.5 counts per second per Rayleigh at 83.4 nm"]
-[3.329932451248169, 5.749091625213623, "[TT] Number of Panels of the SAR Antenna = 3"]
-[6.060476303100586, 1.0666594505310059, "[FF] Presentation Date of the Xatcobeo = May 12-14, 2010"]
-[13.24601936340332, 5.4267096519470215, "[TT] Array Configuration of the Solar Cell Experiment = Two parallel arrays"]
-[3.8012654781341553, -1.0773983001708984, "[TT] Orbit Decay of the LAGEOS = Won't decay"]
-[9.610645294189453, 8.189818382263184, "[TT] Field of View of the ABI = 17.76\u00b0"]
-[9.596024513244629, 8.26601505279541, "[TT] Field of View (FOV) of the PamCam = 20\u00ba x 16\u00ba"]
-[9.211074829101562, 5.300348281860352, "[TT] Scanning Range of the SSULI = 10\u00ba - 40\u00ba below of spacecraft horizon (y-direction)"]
-[8.750190734863281, 5.907810211181641, "[TT] Acquisition Range of the GT = Slightly >15 arcmin"]
-[6.008574962615967, 1.7575746774673462, "[TT] Hitchhiker Video Interface Units (HVIUs) of the MEIDEX = 2"]
-[6.086559295654297, -0.4478724002838135, "[TT] On-Orbit Duration of the CanX-5 = More than one year"]
-[10.449332237243652, 5.771331310272217, "[TT] Transit of the KELT-9 b = Lopsided"]
-[10.823895454406738, -0.3179343640804291, "[TT] Years in Orbit of the TanDEM-X = 8 years"]
-[10.44796085357666, 7.071181297302246, "[TT] CONUS Width of the ABI instrument = 8.0215\u00ba"]
-[6.273124694824219, 4.390228271484375, "[FF] Operator of the DSDS = Four National data centers"]
-[6.046613693237305, 4.704888820648193, "[FF] Communications Capability of the Variable Attitude Spacecraft = Omni-Directional"]
-[7.05989933013916, 8.000829696655273, "[FF] Impact of the Signal to Noise Ratio (SNR) = The higher the SNR, the smaller the bandwidth and the highest spatial resolution the better"]
-[5.896546840667725, -0.8666494488716125, "[FF] Lifetime Mechanism of the SWIM RMA = Unknown"]
-[5.678140640258789, 5.681600093841553, "[TT] Model of the Proton P400K-SGMII-2-PCI104S-SD Space Computer = Proton P400K-SGMII-2-PCI104S-SD"]
-[4.92310094833374, 3.052399158477783, "[TT] Manufacturer of the Meteosat = Aerospatiale of Cannes (France)"]
-[5.768016338348389, 5.980528831481934, "[FF] Digital VCR (Video Cassette Recorder) of the MEIDEX = Data Recording System"]
-[3.3673903942108154, 6.2334794998168945, "[TT] Antenna Size of the Biomass = 12 m diameter"]
-[10.209709167480469, 8.218235969543457, "[TT] Diameter of the Aperture Function = D"]
-[8.956180572509766, 2.2561819553375244, "[FF] Study Location of the Stardust Grain = University of Arizona"]
-[5.4167704582214355, 8.723647117614746, "[TT] Bandwidth of the COCTS = 0.041 \u00b5m"]
-[6.094461917877197, 2.2286453247070312, "[FF] Mission of the POLDER = Observation"]
-[4.873193264007568, 0.5680723786354065, "[TT] Launch Date of the STARE-A = September 13, 2012"]
-[5.553313732147217, 2.8277766704559326, "[TT] Agency of the Arachne = USAF"]
-[7.022839069366455, -0.20121771097183228, "[TT] Journey Time towards the Sun of the ISON = About 3 million years"]
-[7.672490119934082, 8.613940238952637, "[TT] No of Spectral Bands of the ABI = 16"]
-[5.027514934539795, 3.4761898517608643, "[TT] Manufacturer of the CMV4000 = CMOSIS"]
-[9.115621566772461, 6.990554332733154, "[TT] Digital Resolution of the Cluster S/C = 7.813 x 10 -3 nT, 3.125 x 10 -2 nT, 0.125 nT, 0.5 nT, 8 nT"]
-[3.9134104251861572, 3.5006752014160156, "[FF] Name of the GSTB = Galileo System Test Bed"]
-[8.541558265686035, 5.439787864685059, "[TT] Real-Time Orbit Determination Accuracy of the GF-3 Satellite = Better than 10 m (1\u03c3)"]
-[9.32006549835205, 3.2311558723449707, "[TT] Imaging of the 20 cm off-axis internally occulted coronagraph = [Fe xiv] at 5303 \u00c5 and [Fe x] at 6374 \u00c5"]
-[7.222123622894287, 8.206162452697754, "[TT] SNR for Bright Objects of the MSU-50 = 200"]
-[8.158658027648926, 1.1596996784210205, "[FF] Level-2 Data Reprocessing of the SMAP (Soil Moisture Active Passive) = From March 31, 2015 to Sept. 9, 2015"]
-[9.680638313293457, 8.226412773132324, "[FF] Field of View of the MEPED = 15\u00ba full angle, -x, -x + 90\u00ba, 120\u00ba full angle, -x"]
-[9.21064281463623, 7.109720706939697, "[TT] SWIR Range Ground Resolution of the WorldView-3 = 3.7 m"]
-[6.594732761383057, 4.015486240386963, "[FF] Deployment Attempt of the HTV-6 = Unsuccessful"]
-[10.10372257232666, 8.137724876403809, "[TT] Aperture of the Shutter = 35 mm"]
-[6.72857141494751, 1.8349801301956177, "[FF] URL of the Xatcobeo = http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20100021944_2010023813.pdf"]
-[7.972548484802246, -0.6567320823669434, "[TT] Instruments of the CryoSat = DORIS-NG, Laser Reflectors (ESA), SIRAL"]
-[5.381791591644287, 1.671913981437683, "[FF] URL of the ALOS-2 = http://global.jaxa.jp/press/2014/05/20140524_daichi2.html"]
-[7.633533954620361, -0.8392496109008789, "[TT] Mission End Date of the ICESat = Aug. 31, 2010"]
-[9.11308765411377, 3.911799907684326, "[FF] Function of the Optical Solar Reflectors = Deliver additional heat protection"]
-[8.649332046508789, 5.262258529663086, "[TT] Gradiometer Instrument Position of the GOCE = Near the Centre of Mass"]
-[8.073654174804688, -1.0906773805618286, "[FF] Application of the Radar and laser altimeters = Measure changes to ice elevation"]
-[10.482231140136719, 5.562640190124512, "[FF] Surface Temperature of the TOI 270 = About one-third cooler than the Sun\u2019s"]
-[5.262308597564697, 3.068155527114868, "[TT] Partnership of the ESA and EDA = Solid"]
-[8.355269432067871, 6.727838516235352, "[TT] Temporal Resolution of the EIS = 30 s"]
-[7.390933513641357, 3.5148138999938965, "[FF] Data Return of the Corona Satellites = Film canisters were jettisoned and returned to Earth via parachute and recovered by aircraft"]
-[7.445971488952637, 0.26195886731147766, "[FF] Mission Status of the OSIRIS-REx = One Step Closer to Touching Asteroid Bennu"]
-[14.525473594665527, 6.554575443267822, "[TT] Battery Type of the CubeSat power module = Lithium-polymer"]
-[9.353582382202148, 2.603631019592285, "[FF] Flare List Events with Emission above 12 keV of the RHESSI = Over 14,000"]
-[7.992530822753906, 5.352227687835693, "[TT] Extrapolation Range of the FLLS = 250 m"]
-[9.1975679397583, 8.52086067199707, "[TT] Wavelength of the Lens 5 = 1.64 \u00b5m @ 60\u00ba"]
-[8.362296104431152, 6.785943984985352, "[TT] Sensor Mode of the HyperScout\u00ae = Pushbroom"]
-[9.548937797546387, 8.183667182922363, "[TT] Field of View of the Camera System = 15\u00b0 x 20.2\u00b0"]
-[6.248302459716797, 2.6619365215301514, "[TT] Design Basis of the Orion Service Module = ATV (Automated Transfer Vehicle)"]
-[6.396427154541016, -0.9290628433227539, "[TT] In Orbit Checkout Duration of the GRACE-FO = 8 months"]
-[7.540984153747559, -0.6783787608146667, "[TT] Launch Date of the ICEYE-X2 = December 2018"]
-[6.214339256286621, 0.13923008739948273, "[TT] Full-Time Crew Capacity of the International Space Station (ISS) = 6"]
-[6.3754401206970215, 6.519926071166992, "[TT] Message Duration of the ODB = 0.8 seconds"]
-[4.9981513023376465, 0.6217454075813293, "[TT] Launch Date of the ICARE = Nov. 21, 2000"]
-[9.326125144958496, -0.8901672959327698, "[TT] Position of the INSAT-3D = 82\u00b0 East, over the equator"]
-[9.039051055908203, 7.513152599334717, "[TT] Spatial Resolution of the FTHSI = Variable"]
-[8.762677192687988, 2.7314906120300293, "[FF] Measurement of the WINCS = In-situ density, temperature and composition of the thermosphere"]
-[9.75560188293457, -0.5780127048492432, "[TT] Orbital Altitude of the HPT = 400 km"]
-[8.568320274353027, 8.11073112487793, "[TT] Image Cube Build Time of the MicrOmega/MASCOT = About 10 mn"]
-[10.70935344696045, 3.004992961883545, "[TT] Quantity of the ISL (Intersatellite Link) = 1"]
-[9.945094108581543, 9.019594192504883, "[TT] Effective FOV of the Channel 7 = 24 x 43 km"]
-[10.727020263671875, 1.0826345682144165, "[TT] Size of the TOI 700 b = Almost exactly Earth-size"]
-[7.015514373779297, -0.03725316375494003, "[TT] Time Reference of the CryoSat-2 = TAI (International Atomic Time)"]
-[5.008975982666016, 4.308318614959717, "[TT] Preorder Count in India of the Starlink = Over 5,000"]
-[8.14625358581543, 7.630587577819824, "[TT] Number of Analyzers of the FlaPS = 16"]
-[5.042487621307373, 0.0974172055721283, "[TT] License to Operate of the CALIPSO = Through February 2018, perhaps longer"]
-[3.273621082305908, 5.0908331871032715, "[TT] Required Tapes of the Digital SAR Scene = 6 magnetic tapes of 1600 BPI"]
-[10.742877960205078, -1.1305487155914307, "[TT] Altitude Keeping Period of the SLATS = 633 days"]
-[6.1965155601501465, 2.607292413711548, "[TT] Managing Organization of the SWEAP Investigation = SAO (Smithsonian Astrophysical Observatory)"]
-[7.864770412445068, 3.0225298404693604, "[FF] Mission Objectives of the TanSat = Improve the understanding of the global carbon dioxide distribution and its contribution to climate change, and also monitor the carbon dioxide variation on seasonal time scales"]
-[5.762848377227783, 7.163875579833984, "[TT] Data Rate Decrease of the OLS = Factor of 25"]
-[3.8551175594329834, 4.526682376861572, "[TT] Population Standard Deviation of the RADARSAT-2 = 0.3 dB"]
-[13.549874305725098, 5.7465596199035645, "[TT] Current of the Solar Panels = 0.86 A"]
-[10.455759048461914, 2.886693239212036, "[TT] Communication Protocol of the Nanosatellite = FMCW"]
-[7.241698741912842, 4.716684341430664, "[TT] Mounting Location of the SPS = COB"]
-[8.216328620910645, 7.414535999298096, "[TT] Type of Detector of the Instrument = Solar blind MgF2 / CsI Cathode - Multi-anode MCP"]
-[9.396946907043457, 4.947870254516602, "[TT] Attitude Knowledge/Control of the MightySat II.1 = 0.15\u00ba/0.18\u00ba"]
-[10.84416675567627, -0.28978803753852844, "[TT] Earth's Entire Land Mass Mapping Completion Date of the TanDEM-X = By the end of 2014"]
-[9.101580619812012, 6.926464080810547, "[TT] Vertical Error 90% (VE90) of the WorldView-3 = 2.7 m"]
-[5.4871506690979, 6.329156398773193, "[TT] Capacity of the Rolling Memory = 32 Mbit"]
-[5.10993766784668, 6.059954643249512, "[FF] Signal Processing of the NTS AIS Receiver = Attempt to unravel the overlapping messages"]
-[7.2050700187683105, 3.1498794555664062, "[TT] Environmental Qualification of the Prometheus = GEVS (General Environmental Verification Specification)"]
-[6.4056267738342285, 1.4103678464889526, "[FF] Constellation Maintenance Presentation Date of the COSMO-SkyMed = Feb. 24-26, 2003"]
-[8.157548904418945, 4.061546802520752, "[FF] Lunar Calibration Frequency of the Satellite = Monthly"]
-[9.351940155029297, 7.655129909515381, "[TT] Diameter of the NETCAM = 275 mm"]
-[10.660128593444824, 0.8995172381401062, "[TT] Orbit Distance of the Kepler-1658b = Only twice the star's diameter"]
-[4.335362911224365, -0.07998508960008621, "[FF] Reentry Date of the P35-3 = 26.12.1979"]
-[5.336289882659912, 4.763757228851318, "[TT] Number of GPS Signal Losses of the Swarm = 166"]
-[11.724884986877441, 4.586413860321045, "[TT] Secondary Diameter of the Didymos = 160 m"]
-[4.38112211227417, 1.3916257619857788, "[TT] Orbit Position of the GCOM-W1 = International A-Train orbit"]
-[10.065516471862793, 1.7200050354003906, "[FF] Source of Scatter for L\u03b1D of the IMAP = Dim unresolved stars"]
-[5.234359264373779, 3.424398422241211, "[FF] Supplier of the TDP = Unknown"]
-[6.994820594787598, 7.051846981048584, "[TT] Design of the ATLID Power Laser Head = Sealed and pressurized"]
-[3.389822006225586, 6.322549819946289, "[TT] Antenna Mounting Plane Dimensions of the KySat-1 = Maximum 10 x 10 x 10cm"]
-[7.958430290222168, 4.6100006103515625, "[FF] Calibration Activities Duration of the SGLI = First year"]
-[10.938655853271484, 7.530503273010254, "[TT] Swath Width of the SMAP = Approximately 1000 km"]
-[7.442817687988281, 6.0825700759887695, "[FF] Output of the MCP = Proportional to the number of ions at its input"]
-[8.571616172790527, 0.27452099323272705, "[TT] Non-Group Comet Sightings per Year of the SOHO = Over 100"]
-[7.9073262214660645, -0.3795173168182373, "[TT] Date of the Arctic Sea Ice = 6 January 2021"]
-[11.70165729522705, 0.16448575258255005, "[TT] Size of the TESS = 1.9 times Earth\u2019s size"]
-[4.557579040527344, 2.9142115116119385, "[FF] Locations of the LAPAN = Rumpin and Rancabungur (Bogor), Bukittinggi (West Sumatra), Pontianak (West Borneo)and Biak (Papua)"]
-[8.673890113830566, 1.8304955959320068, "[TT] Flash Rate During Weakening of the Hurricane Dorian = More than three times that during rapid intensification"]
-[9.32419490814209, 7.576454162597656, "[TT] Size of the PAN Camera = 150 cm x 850 cm x 100 cm"]
-[7.6591715812683105, 6.229382514953613, "[FF] Goal of the BSM (Beam Steering Mechanism) = Automatically point the lasers at the exact spot on the ground where the telescope is observing"]
-[4.745347023010254, 0.47635960578918457, "[TT] Launch Date of the SpIRIT = 2023"]
-[5.647491931915283, 6.299125671386719, "[TT] Processing Capacity of the OBC = 2 MIPS"]
-[10.863570213317871, -0.3228763937950134, "[TT] Global DEM Acquisition Start Date of the TanDEM-X = December 2010"]
-[12.441901206970215, 5.037091255187988, "[TT] Location of the Solar Arrays = Inside the cuboid module"]
-[7.643865585327148, 5.313322067260742, "[FF] Components of the PCM = Steering mirror mechanism, angular sensor, electrical unit"]
-[14.092863082885742, 7.198765754699707, "[TT] Input Voltage of the LVPS Board = 26 - 29 V"]
-[6.836702346801758, 8.49089241027832, "[FF] Bands of the Spectral bands = 23 bands (380 - 830 nm), 18 channels with 10 nm bandwidth - 6 bands (1050 - 2215 nm) - 7 bands (3.715 - 11.95 \u00b5m)"]
-[13.153421401977539, 5.178079128265381, "[TT] Solar Array Span of the SOHO = 9.5 m"]
-[13.975662231445312, 7.166947841644287, "[TT] Voltage of the Voltage 6 = 3.8\u00b12%"]
-[4.387947082519531, 1.6413805484771729, "[TT] Launch Date of the SARSAT-1 = Mar. 28, 1983"]
-[10.863805770874023, 5.267139434814453, "[TT] Pressure Range of the DN probe = 10^-7 - 10^-2 Pa"]
-[10.847759246826172, -0.26858341693878174, "[FF] Product Definition of the TanDEM-X = Not provided"]
-[11.241426467895508, 5.3938727378845215, "[TT] Size of the Scintillation Detector = 400 cm2"]
-[12.764552116394043, 7.414698600769043, "[FF] Output Power of the InnoSlab amplifier = Scalable"]
-[4.267060279846191, 4.2589192390441895, "[FF] Installation of the SARP-1 = On all early spacecraft in the COSPAS as well as in the SARSAT series"]
-[9.35548210144043, 6.821351051330566, "[TT] Pan Spatial Resolution of the KazEOSat-2 = 1 m"]
-[10.195184707641602, 8.170726776123047, "[TT] Height in Stowed Configuration of the Aperture Stop = 0.83 m above the focal plane surface"]
-[8.73291015625, 0.9157021045684814, "[TT] Final Flyby Date of the Parker Solar Probe = November 2024"]
-[7.205852508544922, 1.670295000076294, "[FF] Technology of the SporeSat = Variable-rate centrifuge"]
-[4.877739906311035, 0.49271178245544434, "[TT] Launch Date of the MEV-2 = August 2020"]
-[10.076454162597656, -1.5071656703948975, "[TT] Orbit Inclination of the Harmony = 98.19\u00b0"]
-[8.531915664672852, 2.0963220596313477, "[FF] Wind and Temperature Observations of the GomX-3 = Mode-S"]
-[8.391814231872559, 7.427661418914795, "[TT] Bit Depth of the CMOSIS CHR70M Image Sensor = 12-bit"]
-[4.724636554718018, 6.249667644500732, "[TT] Average Level of the Beacon Level = -46.4 dBm"]
-[4.934267997741699, 0.03687412664294243, "[TT] End-of-life Date of the SPOT-4 = June 29th, 2013"]
-[14.631599426269531, 6.7470622062683105, "[TT] Battery Nominal Capacity of the EPS = 4.55Ah"]
-[6.536536693572998, 2.6024670600891113, "[FF] Development Date of the Microsized Microwave Atmospheric Satellite (MicroMAS) = April 28, 2013"]
-[8.761137962341309, 9.3998441696167, "[TT] Spectral Band 4 Center Wavelength of the TANSO-CAI = 1.620 \u00b5m"]
-[5.161348819732666, 7.629292964935303, "[TT] Data Output Rate of the I-Q Channel = 31.25 MHz"]
-[4.264610767364502, 7.281094551086426, "[TT] Downlink Frequency of the RF communications = X-band"]
-[4.41815710067749, 7.827154636383057, "[TT] Frequency of the RF radio = Uplink = 145 MHz, downlink = 437.375 MHz"]
-[8.420421600341797, 5.532484531402588, "[TT] Geo-location Accuracy of the Satellite = <50 m without GCP, 20 m with GCP"]
-[7.327976226806641, 5.302371025085449, "[FF] Transmission Profile of the FG = Unknown"]
-[5.824153423309326, 6.782960414886475, "[TT] Data Transmission Cadence of the Data Processing Unit (DPU) = Every 25 s"]
-[10.606471061706543, 3.372445821762085, "[TT] Type of the TechEdSat-10 = 6U CubeSat"]
-[18.798879623413086, 3.4801671504974365, "[TT] \u0394r (m) of the Mosul = 7.7"]
-[7.784209728240967, 3.033985137939453, "[FF] Data Usage of the AVHRR/3 = Provide image data in the visible and infrared spectral bands, information on cloud coverage within the footprints of the various sounding instruments"]
-[6.541924953460693, 1.9161195755004883, "[FF] URL of the Dellingr = http://spaceflight101.com/dragon-spx12/dellingr/"]
-[7.536176681518555, 4.483853340148926, "[FF] Objective of the SMX-1 = Evaluate the ESA ERC32 chip set and advanced processing technologies and shielding experiments in the harsh space environment"]
-[4.231368064880371, 7.369163990020752, "[TT] Type of the K/Ka-Band Ranging (KBR) = Gravity instruments"]
-[8.43697738647461, 2.0623953342437744, "[TT] Control System of the RapidScat = LVLH system"]
-[9.435210227966309, -0.026492591947317123, "[TT] Altitude of the SWIM = 519 km"]
-[10.574471473693848, 1.9406601190567017, "[FF] Non-Thermal Radiation Creation Processes of the Pulsars = Synchrotron emission and curvature emission"]
-[10.350747108459473, 3.268111228942871, "[FF] Type of the Twin 6U CubeSats = CubeSat"]
-[6.767731189727783, 8.491962432861328, "[TT] Data Channels of the SAGE-III = 8 spectral channels + 1 zero-order light channel"]
-[5.39998722076416, 0.18563373386859894, "[TT] Extra Flight Schedule of the Space Shuttle = 2010"]
-[1.3269118070602417, 1.9007564783096313, "[TT] Late-load Cargo Mass of the HTV-5 = 215 kg"]
-[13.94528865814209, 3.017336368560791, "[FF] Mass of the ROSE-1 = Unknown"]
-[8.343134880065918, 8.656342506408691, "[TT] Spectral Resolution of the Littrow spectrometers = 0.3 nm"]
-[8.989032745361328, 7.23729944229126, "[TT] Operational Capability of the MRC (Medium-Resolution Camera) = Achieved"]
-[7.619630813598633, 3.0127182006835938, "[FF] Purpose of the Sensing Instrument = Locate and measure methane emissions"]
-[4.304259777069092, 0.8905613422393799, "[TT] Launch Date of the HY-2 (Haiyang-2) = Aug. 15, 2011"]
-[7.797304630279541, 5.706003189086914, "[FF] Image Navigation of the ABI = Ground processing algorithms to decompress, calibrate and navigate the image samples"]
-[6.109951019287109, 0.756893515586853, "[FF] Publication Date of the Vidal C. Lozada = Dec. 2011"]
-[5.658346176147461, 1.2288576364517212, "[FF] Development and Operations Authors of the EO-1 Hyperion = J. Pearlman, C. Segal, L. Liao, S. Carman, M. Folkman, B. Browne, L. Ong, S. Ungar"]
-[8.55874252319336, 1.3599382638931274, "[TT] Swath Coverage of the Aquarius instrument = 88\u00ba N over the Arctic, and about 79.6\u00ba S over the Antarctic"]
-[9.978344917297363, 6.898095607757568, "[FF] Design Concept of the DST = On-axis, two-mirror, and two-lens corrector system"]
-[6.76237678527832, 2.6272881031036377, "[FF] Number of Lunar Transit Images of the EPIC = Two"]
-[3.4590084552764893, -0.9338775873184204, "[TT] Orbit Type of the FY-3E = Sun-synchronous near-circular orbit"]
-[8.085715293884277, 9.297578811645508, "[TT] Wavelength of the Ice = 1.5 \u00b5m"]
-[6.357961177825928, 0.6923466324806213, "[TT] Monitoring Period of the Gaia = 5 years"]
-[8.747251510620117, 0.1632157862186432, "[TT] Perihelion Distance of the Comet 67P/C-G = 1.24 au"]
-[6.837038040161133, 5.05889892578125, "[FF] Data Transmission of the DCS = In-situ environmental sensor data"]
-[8.589152336120605, 3.4028255939483643, "[FF] Example of the Coordinated Observations = Study of trans-ionospheric radio propagation using the RRI on e-POP in conjunction with SuperDARN and CADI (Canadian Advanced Digital Ionosonde) transmitters on the ground"]
-[9.034032821655273, 6.217617511749268, "[TT] Slot Compatibility of the ArgUS = Slot 1, 2, 3, 4, 5, 6"]
-[5.050390720367432, 1.1544140577316284, "[FF] Conference Presentation of the ADM Aeolus = ADM-Aeolus: an Innovative Operations Concept"]
-[5.1523847579956055, 2.3148279190063477, "[TT] Mission Type of the SPIDER = EO"]
-[6.746296405792236, 6.117698669433594, "[TT] Number of Elements of the PAA = 64"]
-[7.767348289489746, 9.060541152954102, "[TT] Wavelength Range of the HIRES = Wide"]
-[8.450754165649414, 6.384117603302002, "[TT] Residual Phase Error of the Instrument = \u226410\u00ba"]
-[4.958237648010254, 1.487981915473938, "[TT] First TLE Payload Data Received of the Tatiana-2 = Oct. 21, 2009"]
-[8.275920867919922, 7.442974090576172, "[TT] Detector of the VIS/UV Czerny-Turner imaging spectrometer = CCD array"]
-[10.161580085754395, 5.816549777984619, "[TT] Temperature Stability of the HyperScout\u00ae Telescope = Within 2.5\u00b0C"]
-[7.2438764572143555, 5.626717567443848, "[FF] Payloads of the Landmapper-Demo = Optical communication system; and a high-performance payload data processor"]
-[5.6962890625, -0.9040600657463074, "[TT] Design Life of the STPSat-3 = 2-3 years"]
-[8.550512313842773, 5.68237829208374, "[TT] RMSE of the Geometry = 5.34m(L1.1) / 6.73 m (L2.1)"]
-[6.061926364898682, 6.4481377601623535, "[TT] Latency of the TBS Product latency = Near real-time to 15 minutes (product dependent)"]
-[5.866970539093018, 4.793483257293701, "[FF] Control of the Anchor Stations = Remote supervision and control functions are provided by the MCC"]
-[10.294042587280273, 3.995404005050659, "[TT] Deployment Status of the AstroTubeTM Boom = Deployed to full length"]
-[10.47474479675293, 6.6317219734191895, "[TT] Number of Flat Mirrors of the Refocus Mechanism Assembly = 2"]
-[8.163778305053711, 0.008769365958869457, "[TT] Decommission Date of the TOPEX/Poseidon = January 18, 2006"]
-[5.4933671951293945, -0.10736709833145142, "[TT] Departure Time of the Cygnus = 11:10 a.m. EST"]
-[4.843326091766357, 7.305144309997559, "[TT] Downlink Data Rate of the RF Communications = 320 Mbit/s"]
-[5.203188896179199, 3.043966054916382, "[TT] Operator of the EDDS = IWF (Institut f\u00fcr Weltraumforschung), Graz, Austria"]
-[11.937878608703613, 4.572620391845703, "[TT] Size of the SeaHawk-1 = 30 x 10 x 10 cm"]
-[5.1329240798950195, -0.5914071202278137, "[FF] Project Date of the TARANIS = Sept. 25-29, 2006"]
-[4.725889205932617, 5.517967224121094, "[FF] Location Information Encoding of the 406 MHz beacon = GPS, Glonass or the future Galileo system"]
-[10.977484703063965, 7.58365535736084, "[TT] Swath Width of the MSC = 15 km"]
-[5.213477611541748, 6.95265007019043, "[TT] Downlink Data Rate of the Tape Recorder = 15 Mbit/s"]
-[5.432344436645508, 6.314274787902832, "[FF] Memory Space of the NanoSat MO Framework = Dedicated memory space allocated specifically for them"]
-[8.913762092590332, 4.082061290740967, "[FF] Sensor Types of the InSight = Wind, temperature, pressure, magnetometer"]
-[8.83027458190918, 4.075199604034424, "[FF] Function of the Magnetic Spectrometer = Track charged particles and determine the sign of their charge and their rigidity"]
-[14.091266632080078, 2.9912188053131104, "[TT] Freshwater Release of the A-68A = 152 billion (152 x 10^9) tonnes"]
-[6.46190071105957, 4.588939666748047, "[FF] Levels of the Specification Tree = Spacecraft, Subsystem and Unit level"]
-[9.36322021484375, 7.07907772064209, "[TT] Resolution of the COSI = 20 m"]
-[8.795897483825684, 7.510929584503174, "[TT] Inter-strip Distance of the Detector = 75 \u00b5m"]
-[5.200270175933838, 0.8772174119949341, "[TT] Delivery Date of the IASI-NG = Early 2022"]
-[9.641434669494629, 6.991375923156738, "[TT] Spatial Matchup Window of the CYGNSS = 25 km"]
-[5.685095310211182, 0.557853102684021, "[TT] Discovery Year of the Itokawa = 1999"]
-[8.542773246765137, 2.0247690677642822, "[TT] Spatial Resolution of the SeaWinds scatterometer = 50 km"]
-[5.258894443511963, 4.8160929679870605, "[TT] Harmful Interference to Starlink Users of the 5G Network = 77% of the time"]
-[8.296323776245117, 3.998370885848999, "[FF] Pre-flight Calibration Target of the ARTEMIS = Specially-coated panel with known absorption features"]
-[8.474722862243652, 1.2692463397979736, "[TT] Environmental Testing Location of the SAC-D/Aquarius observatory = INPE/LIT facility in Sao Jose dos Campos, Brazil"]
-[9.76313304901123, 8.191781044006348, "[TT] Angle of the Zenith FOV = 35\u00ba"]
-[8.227025985717773, 7.55172061920166, "[TT] Detector of the ELVIS = UV coated back-illuminated e2V CCD 30-11"]
-[9.532614707946777, 4.893971920013428, "[FF] Cone Tilt of the SS 433 = Periodically tilts slightly toward Earth"]
-[5.2855329513549805, 1.5884907245635986, "[FF] Presentation of the Global Change Observation Missions = June 25-29, 2007"]
-[10.190413475036621, 5.819230556488037, "[TT] Range of Radiation Temperature Measured in Bands 4-6 of the Scanning geometry = 213-313 K"]
-[11.671862602233887, 3.3328263759613037, "[FF] Thrusting Modes of the T3\u00b5PS = Continuous thrust mode, Burst thrust mode"]
-[12.176913261413574, 3.7979989051818848, "[TT] Volume of the Gas Cartridge = 20 ml"]
-[7.59301233291626, -2.3058061599731445, "[FF] Principal Investigator of the GOLD = Richard Eastes of UCF"]
-[3.875703811645508, 3.4420742988586426, "[TT] Initial Operations Start Date of the Galileo = December 2016"]
-[4.613797664642334, 6.715721607208252, "[FF] Receiver of the RF Electronic Assembly = Receives uplinked command stream"]
-[5.704773426055908, 2.7878921031951904, "[FF] Funding Amount of the UK Space Agency = More than two million British pounds"]
-[7.186765193939209, 1.8573698997497559, "[FF] Launch Confirmation Date of the CARBONITE-2 = 12 Jan. 2018"]
-[6.294577598571777, 1.4849367141723633, "[FF] Mission of the MERTIS = BepiColombo"]
-[14.049731254577637, 3.2006733417510986, "[TT] Total Mass of the RASAT = ~95 kg"]
-[1.936108112335205, -0.40418902039527893, "[FF] Antenna Fields of View of the Van Allen Probes = Initially from boresight to 70\u00ba"]
-[5.410921573638916, -0.2592772841453552, "[TT] Launch Date of the Block 5D-2 satellite = 1982"]
-[10.572444915771484, 2.4535014629364014, "[TT] Mirror Shells per Module of the X-ray telescope = 54"]
-[14.257002830505371, 3.2151567935943604, "[TT] Mass of the QB50P1 and QB50P2 = 2 kg each"]
-[13.885808944702148, 7.13916540145874, "[TT] Power Lines of the ICU = +3.3 V, +5 V, \u00b115 V, \u00b148 V"]
-[8.49480152130127, 7.057888031005859, "[TT] Camera Type of the ASTERIA = Visible-light camera"]
-[8.979443550109863, 4.233666896820068, "[FF] Vector Inputs of the Slew Mode = Magnetometer and sun sensor vectors"]
-[9.090928077697754, -0.5461925268173218, "[FF] Orbit Phase of the PROBA-3 = Apogee"]
-[3.756828546524048, 4.551800727844238, "[TT] Polarimetric SAR Test Data Availability of the RADARSAT-2 = May 2008"]
-[13.622003555297852, 5.454759120941162, "[TT] Type of the Solar Panels = Silicon solar cells"]
-[7.8734517097473145, 3.112549066543579, "[FF] XCO2 Changes of the CO2 = < 1 ppm"]
-[6.443597793579102, 0.8672613501548767, "[FF] Power Supply of the FormoSat-2 = IRU power supply failed in 2006"]
-[3.6322240829467773, -1.0392364263534546, "[TT] Orbit Type of the Explorer 36 = Elliptical polar retrograde orbit"]
-[4.6947221755981445, 0.5385400652885437, "[TT] Launch Date of the MOMS = 18 June 1983"]
-[11.44987678527832, 3.968701124191284, "[TT] In-track Separation of the AeroCube-OCSD-B and -C = 151 meters"]
-[9.419028282165527, 4.999169826507568, "[TT] Attitude Control Stability of the GF-2 spacecraft = 5 x10-4 \u00ba/s"]
-[8.991759300231934, 4.517793655395508, "[TT] Sun edge sensor array size of the Sun tracker = 512 elements"]
-[9.961760520935059, 4.406105995178223, "[FF] Actuation of the ADCS = 3 MTQs (Magnetic Torquer) and a MW (Momentum Wheel)"]
-[9.644124984741211, -0.45202404260635376, "[TT] Altitude of the ResourceSat-2 = 817 km"]
-[9.037456512451172, 3.38317608833313, "[FF] Objective of the Variant = Investigation of the lithosphere-atmosphere-ionosphere-magnetosphere coupling"]
-[10.117704391479492, 8.04069709777832, "[TT] Aperture of the DST 35 = 35 cm"]
-[10.887453079223633, 7.487245559692383, "[TT] Swath of the CZI = 950 km"]
-[7.854790687561035, 6.918314456939697, "[FF] Operation of the Interferometer Arrays = Take a snapshot, process it and there's your image"]
-[10.670262336730957, 0.9171741604804993, "[TT] Size of the Kepler-1658b = Three times larger than previously thought"]
-[8.230722427368164, 2.843381404876709, "[TT] Measurement Domain of the CATS = Atmosphere"]
-[8.632319450378418, 1.0828880071640015, "[FF] Design Life of the SAC-D spacecraft = 3 years for Aquarius and 5 years for the SAC-D instruments"]
-[13.400412559509277, 7.325993061065674, "[TT] Power of the COPPER = 2 W"]
-[7.737927436828613, 9.551161766052246, "[TT] Center Wavelength of the B4 = 665 nm"]
-[8.166438102722168, -1.0615577697753906, "[TT] Precision of Height Change Measurements of the ICESat-2 = Less than 2.5 cm"]
-[5.276303768157959, 2.0803096294403076, "[TT] Mission Status of the SpaceX CRS-16 = Mission complete"]
-[8.709492683410645, 3.379749298095703, "[TT] Number of Instruments of the Solar Ultraviolet Imager (SUVI) = 1"]
-[14.035758972167969, 6.318253993988037, "[TT] Architecture of the GomSpace NanoMind A3200 = AVR32"]
-[1.3636457920074463, 2.7834973335266113, "[TT] Principal Absorbing Constituents of the Band 3 = CO2"]
-[13.4718656539917, 2.820528507232666, "[TT] Dry Mass of the Spacecraft = 322 kg"]
-[10.763246536254883, 7.460019588470459, "[TT] Swath Width of the SASS = 500 km on either side of the ground track"]
-[13.374082565307617, 2.9044766426086426, "[TT] Mass of the TechnoSat = 18 kg"]
-[7.977252960205078, 7.682459354400635, "[FF] Payload Qualification of the Hyperspectral Imager = Unknown"]
-[4.899540424346924, -0.8453078269958496, "[FF] Models of the FengYun LEO satellites = FY-3A/B, FY-3C/D/E/F"]
-[7.968860149383545, -2.576399564743042, "[TT] Light Wavelength of the GOLD = 135.6 nm"]
-[10.902304649353027, 7.531350612640381, "[TT] Swath Width of the WorldView Legion = 9km"]
-[7.917751312255859, 4.8616414070129395, "[TT] Quantity of the RADFET dosimeters = 2"]
-[10.4108304977417, 2.1257143020629883, "[TT] Uniform Exposure of the eROSITA X-ray telescope = About 150-200 seconds"]
-[6.4081950187683105, 4.446498870849609, "[FF] Content of the Email = Excel spreadsheet with CM data and value-added analysis results including PoC and delta-V tradespace"]
-[10.633184432983398, 0.012433452531695366, "[TT] Formation of the CloudSat = Close formation with CALIPSO"]
-[4.716106414794922, -1.9010738134384155, "[TT] Launch Date of the Chang'e-5 = Late November 2020"]
-[9.378024101257324, 7.17752742767334, "[TT] Spatial Resolution of the WFI = 16 m"]
-[7.6448845863342285, 8.521139144897461, "[FF] Application of the Platinum-based multilayers = First 7 groups"]
-[5.366347789764404, 0.9421038627624512, "[FF] Announcement Date of the SmallGEO Extension = Sept. 30, 2011"]
-[10.944924354553223, 0.5405144095420837, "[FF] Number of Transiting Super-Earths of the K2-155 = 3"]
-[3.4865646362304688, 4.919309139251709, "[TT] SAR of the RISAT-1 = C-band"]
-[8.328862190246582, 4.532219409942627, "[FF] Purpose of the Unresolved Imagery = Observe and characterize orbiting objects with the goal of determining their attitude and detecting configuration changes"]
-[3.264547109603882, 1.7975214719772339, "[TT] Ship Detection Information Availability of the Sentinel-1A = 18 minutes"]
-[11.860541343688965, -0.015393750742077827, "[FF] Data Usage of the TESS = Detecting pulsation patterns in young, rapidly rotating stars"]
-[8.056309700012207, -0.8634821176528931, "[TT] Measure Area Frequency of the Sentinel-3 = More frequent than ICESat-2"]
-[6.937316417694092, 1.4517457485198975, "[FF] Spacecraft Operations Location of the Spitzer Space Telescope = Lockheed Martin Space in Littleton, Colorado"]
-[9.506341934204102, -0.551950216293335, "[TT] Mission Orbit Altitude of the FormoSat-2 = 888 km"]
-[4.560263156890869, 0.5991185903549194, "[FF] Launch Date of the ANGELS = 2019"]
-[6.644427299499512, 4.458253860473633, "[TT] Recovery Actions of the FDIR = Reconfigurations or mode change"]
-[6.281742095947266, 1.9148892164230347, "[FF] URL of the SpaceX 2 = http://www.nasa.gov/pdf/729030main_spacex_2_cargo_manifest.pdf"]
-[3.878354549407959, 3.3973875045776367, "[TT] Delay of the Galileo program = 3 years"]
-[11.20248031616211, 1.03382408618927, "[FF] Centrifugal Force of the LISA Pathfinder = Small"]
-[9.357101440429688, 5.2888407707214355, "[TT] Solar Elevation Angle of the Instrument = 30-90\u00ba"]
-[5.1318159103393555, 1.7789286375045776, "[TT] Operational of the Resurs-P3 = True"]
-[3.589303731918335, 4.917530059814453, "[TT] Incidence Angle Range of the RISAT-1 = 12\u00b0 to 55\u00b0"]
-[5.867236614227295, 1.3659615516662598, "[FF] Paper Number of the ERG Satellite = 2011-r-51"]
-[3.63582706451416, 2.643630027770996, "[TT] Inter-satellite Links of the Iridium PRIME = 4"]
-[8.145147323608398, 8.404134750366211, "[TT] VNIR Channels of the PROBA-V = 3"]
-[8.579455375671387, 5.50565242767334, "[TT] Pointing Accuracy of the GP-B satellite = 0.97 \u00b5rad RMS (0.2 arcsec RMS)"]
-[6.456624984741211, 1.4277358055114746, "[FF] Control Presentation Date of the COSMO-Skymed = Oct. 4-8, 2004"]
-[9.741559982299805, 4.547450542449951, "[TT] Control System of the S/C = Four reaction wheels and gyro-stellar attitude determination"]
-[5.481093883514404, 6.0366363525390625, "[TT] ROM/RAM of the SHU = EEPROM(128KB x 2), SRAM(8MB x 4), FROM(128MB)"]
-[3.4477386474609375, 6.432074546813965, "[TT] Antenna aperture of the Mobile Link = 13 m diameter"]
-[14.183377265930176, 3.2335143089294434, "[TT] Mass of the Tether = 5.5 kg"]
-[4.695676326751709, 5.701516151428223, "[TT] Doppler Frequency Shifts Setup of the GATE Signal Generator = Independent"]
-[4.397736072540283, 7.747292518615723, "[TT] Ka-band Frequency of the SARAL/AltiKa = 35.75 GHz"]
-[8.159303665161133, -0.6410208940505981, "[FF] Main Role of the CryoSat = Provide detailed measurements of the height of the world\u2019s ice"]
-[5.185343265533447, 0.16642852127552032, "[TT] Retirement Date of the TRACE = June 2010"]
-[8.648345947265625, 3.6839632987976074, "[TT] Measurement Type of the Energetic Charged Particle (ECP) sensor = In-situ space weather measurements, ECP flux and warnings"]
-[5.330566883087158, 3.367013692855835, "[TT] Platform of the SEOSat = AstroBus-250"]
-[6.492213249206543, 5.104097843170166, "[FF] Data Processing of the RPW = Relatively easy and quick once behavior is known"]
-[18.79833221435547, 3.4805893898010254, "[TT] Mean \u0394E (m) of the Menara = -8.4"]
-[4.488120079040527, 6.926403522491455, "[FF] Measurement of the Ka-band ground station = High data rate by SNR (Signal-to-Noise) measurement"]
-[6.255650997161865, 0.4197314381599426, "[FF] Expected Duration of the ABEX = 18 months"]
-[4.8096604347229, 7.2654900550842285, "[TT] Digital Recorder Dump Rate of the X-band = 61.44 Mbit/s"]
-[4.022212028503418, 3.5153064727783203, "[FF] URL of the Galileo = http://m.esa.int/Our_Activities/Navigation/Android_smartphone_app_connects_you_to_Galileo"]
-[6.069128036499023, -0.22304311394691467, "[TT] Maximum Crew Duration of the OWS = 84 days"]
-[3.7328906059265137, -0.7685163021087646, "[FF] Orbit Type of the ELV = Low Earth Orbit"]
-[5.77116060256958, 7.1215596199035645, "[TT] Data Rate of the HI-SCALE = 160 bit/s"]
-[8.10643482208252, 7.156975269317627, "[TT] Transmission Success of the HD-TV Camera = Most cases"]
-[6.490686893463135, 0.02421935647726059, "[TT] Update Frequency of the Active Schedule = Minimum of once per week"]
-[8.625911712646484, 7.584181785583496, "[TT] Area of the CCID-80 = 20.4 cm2"]
-[5.33988618850708, 3.9574496746063232, "[TT] Number of Satellites of the First Batch of Satellites = 1600"]
-[5.0477070808410645, 0.3783278167247772, "[TT] Installation Date of the TSIS-1 = 30 December 2017"]
-[4.4813642501831055, -0.9254093766212463, "[FF] Symposium Date of the Dragon 3 = June 25-29, 2012"]
-[5.004687786102295, 3.372709035873413, "[TT] Manufacturer of the Gaia = ESA"]
-[6.638145923614502, 3.6205244064331055, "[FF] Filters of the Water Machines = Ultrafiltration and reverse osmosis"]
-[10.71223258972168, 3.4319546222686768, "[TT] Bus Assembly Type of the LunIR = 6U CubeSat"]
-[8.292623519897461, 3.9108762741088867, "[FF] Non-cooperative Mode Operation of the RVX = Not during eclipses, when large shadows are cast on the CSC, or in the case specular reflections on the CSC cause the sunlight to mirror back to the OSC"]
-[5.651641368865967, 4.903670310974121, "[FF] Impact on ACS Algorithm Test-Replace Cycle of the Ground Station = Almost twice as fast"]
-[9.448787689208984, 3.6200380325317383, "[FF] Long-wavelength Magnetizations of the Vertically-integrated magnetization model = Dominated by the continent-ocean contrast"]
-[3.6414289474487305, 5.661757469177246, "[TT] Technology of the Multimode radar = APAA (Active Phased Array Antenna)"]
-[10.412961959838867, 1.7764173746109009, "[FF] Brightness of the ULX-pulsar = Hundreds of times brighter than the Eddington luminosity"]
-[4.847932815551758, 8.180461883544922, "[TT] Signal Frequency of the Clementine = 2.273 GHz"]
-[5.993480205535889, 5.203139305114746, "[TT] Type of the CANOE = Multithreaded"]
-[5.638303756713867, 5.2657790184021, "[TT] Redundancy of the Phoenix GPS Receivers = Cold redundant pair"]
-[10.437286376953125, 5.743868350982666, "[TT] Maximum Temperature of the GOES-R satellite = 87\u00baC"]
-[9.873308181762695, 2.850579023361206, "[FF] Launch Date of the Estonia's student cubesat satellite = Unknown"]
-[5.066775798797607, 0.6048789024353027, "[FF] Launch Date of the ExoMars = 2020"]
-[4.252713203430176, 2.6004319190979004, "[TT] Launch Site of the OCO-2 = VAFB, CA"]
-[7.7625274658203125, 1.6851856708526611, "[FF] Purpose of the Atlantic Basin Facility = Simulate the deep ocean environment"]
-[8.880593299865723, 4.554353713989258, "[TT] Function of the Earth Sensor = Furnished pitch and roll information"]
-[8.320748329162598, 7.2585129737854, "[FF] Family of the COBRA = COBRA, a CMOS Space Qualified Detector Family"]
-[6.812562465667725, 0.992094874382019, "[TT] Renaming Date of the Solar Probe Plus = May 31, 2017"]
-[6.371322154998779, 2.003784418106079, "[FF] URL of the RADARSAT Constellation Mission = http://www.asc-csa.gc.ca"]
-[5.378757476806641, 7.883937835693359, "[FF] Oscillation Frequencies of the GOLF = Between 10-7 and 6 x 10-2 Hz"]
-[7.067731857299805, 4.963068008422852, "[FF] Powering of the Valves Controller Board = Telecommands"]
-[9.454996109008789, 7.370054244995117, "[TT] Resolution of the SXI = 7 arcsec (on axis)"]
-[5.483596324920654, 3.0322701930999756, "[TT] Manufacturer of the COWVR = NASA\u2019s Jet Propulsion Laboratory"]
-[10.588521957397461, 2.7809340953826904, "[TT] Orbit Altitude of the Nanosatellites = 500 km"]
-[8.504653930664062, 9.232135772705078, "[TT] Inefficiency Requirement of the ACC = < 10-4"]
-[7.901226997375488, 7.604160785675049, "[TT] End of Life Date of the Hyperspectral imagers = Nov. 12, 2002"]
-[13.4269380569458, 5.462680816650391, "[TT] Redundancy of the Solar Array = 4 strings loss allowed"]
-[4.718145370483398, 0.8115323781967163, "[TT] Launch Approval Date of the PROCYON = September 2013"]
-[5.732064723968506, 12.149713516235352, "[TT] Wavelength FWHM of an unresolved line of the Spectrometer = 0.098 \u00b5m"]
-[6.756534576416016, 5.031208038330078, "[FF] Electric Field of the FSU = Set up between the modulator grid and the adjacent ground grids"]
-[7.423038959503174, 2.291499614715576, "[TT] Global Coverage of the Satellite System = True"]
-[6.690279483795166, 1.825978398323059, "[FF] URL of the Reentrynews = http://reentrynews.aero.org/26414.html"]
-[10.910903930664062, 10.104459762573242, "[TT] Service Date of the Alpha Magnetic Spectrometer (AMS) = December 3, 2019"]
-[4.613194942474365, 1.5268086194992065, "[FF] Launch Date of the GOSAT-GW = 2024"]
-[8.257476806640625, 0.7878879308700562, "[TT] 2022 Acres Burned of the U.S. Drought Monitor = 230,000 acres"]
-[6.146147727966309, 4.772515296936035, "[FF] MCS of the FOS = Multi-domain distributed system"]
-[5.7374773025512695, 5.880828857421875, "[FF] Transmission Configuration of the Data Download System = All files (already downloaded and not yet downloaded) or only not yet downloaded files"]
-[11.923065185546875, 5.015124797821045, "[TT] Size of the MEPSI = 100 mm x 100 mm x 125 mm"]
-[10.835186004638672, 2.1287076473236084, "[FF] Data Type of the XMM-Newton = X-ray emission"]
-[4.462350845336914, 7.873003005981445, "[TT] Intermediate Frequency of the Receive Downmixer Board = 420 MHz"]
-[6.674905300140381, 5.001614570617676, "[FF] Functions of the ICU = Controlling the detector modules, reading-out, processing and forwarding science data, providing thermal control to all instrument units, controlling the calibration light sources and mechanisms, providing engineering data for instrument health status"]
-[3.6727004051208496, 6.505167484283447, "[TT] Type of the RA/SCAT = Paraboloidal reflector antenna"]
-[6.883724212646484, 3.392484664916992, "[FF] Purpose of the Engineered Heart Tissues (EHTs) study = Looks at how human heart tissue functions in space"]
-[11.289306640625, 6.390235424041748, "[TT] Density of the Proton Component Measurement Range of the DSCOVR = 1 \u2013100 particles/cm3"]
-[5.248397350311279, 2.72377347946167, "[TT] Number of Universities of the ESEO = 13"]
-[5.658320903778076, 1.290675401687622, "[FF] Presentation Date of the Sapphire = April 23, 2012"]
-[7.479611396789551, 0.14237704873085022, "[TT] Signal Travel Time of the OSIRIS-REx = Just over 18.5 minutes"]
-[8.448649406433105, 5.349895000457764, "[TT] Orbital Accuracy of the STARE = \u2264 50 m"]
-[4.884974002838135, 7.272840976715088, "[TT] Nominal Mode Downlink Data Rate of the ASTERIA Transceiver = 1 Mbit/s"]
-[8.47647762298584, 8.222612380981445, "[TT] Spectral Resolution of the Instrument = 0.625 cm -1"]
-[5.432679176330566, 0.19952663779258728, "[TT] Operation End Date of the SAMS = April 9, 1985"]
-[4.611649990081787, 4.788610935211182, "[FF] Purpose of the AIS = Improve the maritime safety and efficiency of navigation, safety of life at sea and the protection of the marine environment"]
-[10.345876693725586, 4.519586563110352, "[TT] Reaction Wheels Quantity of the AOCS = 4"]
-[10.22123908996582, 4.555074691772461, "[TT] Wheel Design of the ADCS = Custom (scalable) motor design"]
-[1.7453958988189697, -2.0757863521575928, "[TT] Journey Duration of the Hayabusa-2 = 42 months"]
-[8.073299407958984, 8.918041229248047, "[TT] Wavelength Range of the SUVI = 9.4 nm - 30.4 nm"]
-[8.107442855834961, -1.1871000528335571, "[FF] Laser Altimetry of the ICESat-2 = Measure loss of the floating ice shelves around Antarctica"]
-[4.566277980804443, 5.846255779266357, "[TT] Number in Use of the 406 MHz beacons = Over 600,000"]
-[9.294610977172852, 3.2068405151367188, "[FF] Components of the Coronagraph = Four coaxial occulting discs and photodetectors"]
-[6.799978733062744, 3.9981932640075684, "[TT] Retirement Reason of the DMSP F-19 = Power failure"]
-[13.26896858215332, 7.158090591430664, "[TT] Average Power Consumption (Observation Mode) of the COMIS = 14 W"]
-[7.81054162979126, 5.998027324676514, "[FF] Type of the EOVSA's Images = Radio emissions"]
-[5.573121547698975, -1.9582314491271973, "[FF] Applications of Data of the KOMPSAT-2 = Unknown"]
-[5.068218231201172, 3.596963405609131, "[TT] Engineering Model Availability of the EDR-2 = Available at CADMOS"]
-[13.896021842956543, 2.7038426399230957, "[TT] Launch Mass of the EduSat = 10 kg"]
-[9.442831993103027, 4.682677745819092, "[FF] Computer Interface of the ADCS = Attitude sensors and actuators"]
-[13.520265579223633, 6.647749423980713, "[TT] Average On-Orbit Power of the EPS = 42-52 W"]
-[8.095775604248047, 7.0090484619140625, "[TT] Components of the Sensor = Four optical and electronic chains"]
-[5.127068042755127, 1.83688223361969, "[TT] NRL Review Date of the TacSat-4 = 2009"]
-[8.434476852416992, 6.965108871459961, "[TT] Instrument type of the MS = High resolution optical imagers"]
-[8.573687553405762, 4.84067964553833, "[TT] Type of the Star Camera Assembly (SCA) = Star Camera Assembly"]
-[5.020975589752197, 7.527286052703857, "[TT] Link Margin of the RF = 20 dB"]
-[10.072003364562988, -1.5381460189819336, "[TT] Inclination of the Shakuntala = 97.4\u00b0"]
-[14.087148666381836, 4.0615739822387695, "[TT] Instrument Mass of the Instrument = 20.45 kg"]
-[10.411803245544434, 3.2316744327545166, "[TT] Number of CubeSat Units of the COPPER = 1"]
-[9.252727508544922, 10.696711540222168, "[TT] Polarisation of the PMI = V, H"]
-[8.021700859069824, 8.489144325256348, "[TT] Vibration Isolation of the VISS = >20 dB"]
-[5.27810001373291, 1.5856596231460571, "[TT] Copyright of the ALOS/ Daichi = \u00a9 JAXA"]
-[8.747668266296387, 6.728344917297363, "[TT] OAP Increase of the UK-DMC-2 = 60%"]
-[5.6867780685424805, 1.208163857460022, "[FF] Delivery Date of the Sapphire Satellite = January 30, 2014"]
-[8.348750114440918, 7.796961307525635, "[TT] Absorber Material of the Imaging Calorimeter = Tungsten"]
-[4.2593770027160645, 0.3303156793117523, "[TT] Launch Date of the JPSS-2 = 2019"]
-[5.777308940887451, 4.500699996948242, "[TT] Validation Data Source of the CYGNSS = GPS dropsondes"]
-[3.3678359985351562, 0.10361428558826447, "[TT] LTDN of the JL-1-GF03D = 10:00"]
-[5.984828472137451, 7.166708946228027, "[TT] Instrument Package Data Rate of the LCROSS = 554.5 kbit/s"]
-[6.028127193450928, 7.04481315612793, "[TT] Data Rate of the Optical ISL forward service = 500 bit/s or 4 kbit/s"]
-[9.837428092956543, 2.715118885040283, "[TT] Number of Satellites Deployed from Cygnus of the NanoRacks = 35"]
-[7.879701137542725, 3.5063259601593018, "[FF] Application of the Compact Infrared Camera (CIRC) = Earth Observation"]
-[9.001294136047363, 5.576279163360596, "[TT] Earth Pointing Accuracy of the Resurs-O1 spacecraft = 6 arcmin"]
-[9.19860553741455, 7.396144866943359, "[TT] GSD (Multispectral) of the EOS = 4 m"]
-[6.483928203582764, 7.613274574279785, "[TT] Data Quantization of the NTSIC = 12 bit"]
-[7.550042152404785, 3.8168985843658447, "[FF] Instruments of the FORUM = Cloud Radar, Imager, Sounder"]
-[7.643119812011719, 0.44029706716537476, "[FF] Manufacturer of the Lunar IceCube = Morehead State University, NASA/GSFC, Busek Company"]
-[3.4012887477874756, 4.584146499633789, "[FF] Image Content of the SAR = Large-scale, tongue-like feature protruding from the coast into the ocean"]
-[8.085905075073242, 4.605034351348877, "[FF] Testing of the Prometheus = 3-axis random vibration and lengthy thermal vacuum cycling"]
-[5.092471599578857, 3.4541773796081543, "[TT] Model of the USRP = USRP N210"]
-[8.046714782714844, 8.862793922424316, "[TT] Spectral Bandwidth of the MAHRSI = About 4 nm"]
-[7.942899227142334, 6.279845237731934, "[TT] Type of the TANSO-FTS = Imaging multi-spectral radiometers (vis/IR)"]
-[9.099822044372559, 7.5014801025390625, "[TT] MWIR Band Resolution of the Imager = 4 km"]
-[7.722401142120361, 9.351065635681152, "[TT] Center Wavelength of the Band 3 = 0.885 \u00b5m"]
-[10.480417251586914, 2.2796268463134766, "[TT] Telescope Type of the ASTRO-H = SXTs (Soft X-ray Telescopes)"]
-[3.120709180831909, 2.1691393852233887, "[FF] Catalyst of the Copernicus = Nicolaus Copernicus"]
-[3.4642767906188965, 4.590579032897949, "[FF] Applications of the SeaSat SAR = Determine the directional spectra of ocean waves, surface manifestations of internal waves, polar ice-cover motion, geological structural features, soil moisture boundaries, vegetation characteristics, urban land-use patterns, and other geoscientific features of interest"]
-[6.8975067138671875, -0.3460029661655426, "[TT] Orbit Period of the SeaSat = 101 minutes"]
-[9.326111793518066, 7.153848648071289, "[FF] Resolution of the Thorium Distribution Map = Unknown"]
-[11.197371482849121, 5.70697021484375, "[TT] Flexural Rigidity of the Aluminum-polymer laminate = 5.6 x 10-4 Nm"]
-[8.184536933898926, 7.170335292816162, "[FF] Conference Presentation of the EarthCARE Multi Spectral Imager = SPIE Remote Sensing Conference, Toulouse, France, Sept. 20-23, 2010"]
-[7.850096702575684, 4.77180290222168, "[FF] Execution Location of the Image acquisition and HSI calibration = Anywhere on the satellite orbit"]
-[9.476606369018555, 7.562103271484375, "[FF] Goal of the SV-24 = Provide high spatial resolution imaging"]
-[8.08710765838623, 7.452303886413574, "[TT] Grounding of the Modulator Assembly = Niobium outer tube"]
-[9.237015724182129, 3.1429128646850586, "[FF] Purpose of the Solar Wind = Give insight into birth of solar system"]
-[6.993910789489746, -0.05801154300570488, "[TT] Orbit Duration of the CryoSat-2 = A decade"]
-[8.62870979309082, 1.1586287021636963, "[FF] Sensor Complement of the SAC-D/Aquarius = Unknown"]
-[2.551802396774292, 0.1661047339439392, "[TT] Pulse period (ms) of the B1758-250 = 3.000"]
-[8.176958084106445, 1.2158085107803345, "[FF] Data Type of the SMAP = Soil moisture data"]
-[7.624289035797119, 2.9593448638916016, "[FF] Mission Goal of the GOSAT = Provide policy makers with observed and analyzed data on climate changes"]
-[11.761475563049316, 3.349313259124756, "[TT] Engine Type of the EDRS-C = Liquid apogee engine"]
-[5.090612888336182, 1.388508915901184, "[FF] URL of the INSAT-3D = http://www.imd.gov.in/section/satmet/dynamic/insat_3d.htm"]
-[6.325044631958008, 5.462192058563232, "[FF] Computational Units of the Electrical System = Distributed processors and FPGAs"]
-[10.024073600769043, -1.497811198234558, "[TT] Parking Orbit Inclination of the Spacecraft and Propulsion Module = 63\u00ba"]
-[5.864780902862549, -0.4146164059638977, "[TT] Expected Deployment Duration of the Spaceflight SSO-A: SmallSat Express = Six hours"]
-[4.7558698654174805, -1.6264084577560425, "[FF] Purpose of the Tianyan-1 / Yizheng-1 = Technology verification"]
-[7.270069599151611, 7.965777397155762, "[TT] Signal-to-Noise Ratio of the Atmospheric-sounding instrument = High"]
-[11.174511909484863, 5.798246383666992, "[TT] Material of the Net = Kevlar"]
-[8.79104232788086, 6.407930850982666, "[TT] Uncertainty of Altimeter Height Data Corrections of the TMR = 1.2 cm"]
-[13.563789367675781, 5.481960296630859, "[TT] Number of Solar Cells of the SCTE = Up to 47"]
-[3.9251813888549805, 4.410266399383545, "[TT] Surveillance Capabilities of the RADARSAT-2 = Global high-resolution surveillance"]
-[8.108325958251953, -1.0603634119033813, "[TT] Sea Ice Detection of the ICESat-2 = The comparatively textured surface of sea ice"]
-[13.071685791015625, 7.238738059997559, "[FF] Collection Power of the IMAP = ~15 x, ~25 x, ~ 35 x"]
-[6.888822078704834, -0.5375269651412964, "[TT] Orbit Determination Frequency of the ASNARO Ground Segment = Twice per day"]
-[7.476943016052246, 0.367450475692749, "[TT] Thermal Spectrometer of the OSIRIS-REx = OTES"]
-[5.611441135406494, 5.754575252532959, "[TT] Processor of the PROBA-2 = 32-bit LEON2-FT RISC processor with up to 100 MIPS"]
-[4.3863606452941895, 0.9569188356399536, "[TT] Launch Date of the IRNSS-1D = March 27, 2015"]
-[6.440401077270508, 2.6069607734680176, "[TT] Responsible Organization of the SPAN (Solar Probe Analyzers) = UCB/SSL (University of California, Berkeley /Space Sciences Laboratory)"]
-[7.22019624710083, 2.5929970741271973, "[FF] Publisher of the Observation of the Earth and Its Environment: Survey of Missions and Sensors = Herbert J. Kramer"]
-[13.291605949401855, 7.704366207122803, "[TT] Transmit power of the Downlink (Ku-band) = 0.2 W"]
-[11.293656349182129, 0.9500935673713684, "[TT] Lifetime of the LISA = Four years, with possible six-year extension"]
-[5.179692268371582, 6.85344123840332, "[TT] Downlink Data Rate of the Spacecraft = 1 Mbit/s"]
-[3.4673614501953125, 5.573356628417969, "[TT] Type of the SAR Antenna = 2-D active phased array antenna"]
-[8.539885520935059, -0.16274374723434448, "[TT] Map of the Moon's Surface Observation Period of the Chang'e-2 = October 2010 and May 2011"]
-[9.941546440124512, 9.019586563110352, "[TT] Effective FOV of the Channel 7 = 24 km x 43 km"]
-[5.549932479858398, 6.3961286544799805, "[TT] Solid State Storage of the Command and data handling subsystem = 380 MByte"]
-[7.469735622406006, 3.6746914386749268, "[FF] Purpose of the NightPod = Crew Earth Observations"]
-[12.393696784973145, 0.6018224954605103, "[FF] MAIT Phase of the PLATO Satellite = Parallel and independent for Payload and Service modules"]
-[4.713803291320801, 8.359560012817383, "[TT] Center Frequency of the 5 = 55.5 GHz"]
-[9.288002967834473, 5.268651485443115, "[TT] Rate Stability of the QuikTOMS spacecraft = < 0.01\u00ba/s"]
-[6.266034126281738, 8.06661605834961, "[TT] Number of Passbands of the Channel 2 = 1"]
-[5.062221527099609, 3.4607443809509277, "[TT] Satellite of the Sentinel-4 = MTG"]
-[7.42012357711792, 0.8097058534622192, "[FF] Meeting Location of the LunaH-Map = Columbia, Maryland"]
-[7.6358513832092285, 2.145763874053955, "[FF] Additional Information Source of the Remote Sensing = Emission of fluorescence from the chlorophyll of assimilating leaves"]
-[4.493797779083252, 1.567589521408081, "[TT] Deployment Date of the LituanicaSat-1 = February 28, 2014"]
-[10.207266807556152, 3.216360569000244, "[FF] Purpose of the AERO-VISTA Interactive Spectrogram Display = Scientific Operations of Twin 6U CubeSats"]
-[7.943873405456543, 0.9335848689079285, "[FF] Date of the Volcanic Eruption Lights Up Iceland = 23 March 2021"]
-[13.868372917175293, 2.9700307846069336, "[TT] S/C Launch Mass of the Payload = 1,900 \u2013 2,100 kg"]
-[8.969962120056152, 4.341544151306152, "[TT] Measurement of the FSS (Fine Sun Sensor) = 2-axis sun vector"]
-[9.521081924438477, 4.8002448081970215, "[FF] Operational Modes of the ACS = Momentum biased stabilization, Nadir optimized pointing, Fixed scan angle"]
-[6.267850399017334, 4.628823757171631, "[FF] Function of the Database Services = Enable element-level databases through the use of relational database clusters"]
-[8.255112648010254, 2.502027750015259, "[FF] Usage of the CAI-2 = Used for cloud discrimination except thin cirrus"]
-[10.703750610351562, 7.185582637786865, "[TT] Footprint of the SMAP = 9 km"]
-[3.3530683517456055, 4.854568958282471, "[FF] SAR Techniques of the TanDEM-X = Digital beamforming (DBF) with two satellites, single-pass polarimetric SAR interferometry, single-pass along-track interferometry with varying baseline"]
-[13.5951509475708, 7.556316375732422, "[TT] Voltage Output of the PSU = 5 V to supply the RF power amplifiers in C&CS"]
-[8.417682647705078, 8.035629272460938, "[TT] Spectral Range of the LWIR Camera = 8-9.5 \u00b5m"]
-[8.47778606414795, 6.514085292816162, "[TT] TGFs Detected of the RHESSI = Over 1000"]
-[5.8929595947265625, 2.765937089920044, "[TT] Installation Location of the CATS = JEM-EF (Japanese Experiment Module-Exposed Facility) of JAXA"]
-[13.745866775512695, 7.400381088256836, "[TT] Transmitter Voltage of the DSX = 5 kV"]
-[3.637855052947998, 4.811838150024414, "[TT] Imaging Frequency Band of the Sentinel-1A/B = C"]
-[8.991212844848633, -0.2884604036808014, "[FF] SMIM Location of the LUMIO = Periselene of the transition orbit"]
-[4.158934593200684, 1.9143788814544678, "[TT] Launch Vehicle of the HORYU-2 = H-IIA of Japan"]
-[5.117300987243652, -0.27382954955101013, "[TT] Retirement Date of the CBERS-1 = Aug. 2003"]
-[9.410799026489258, 0.7435937523841858, "[TT] Impact Speed of the SMART-1 = 2 km/s"]
-[3.6704800128936768, 4.045360565185547, "[FF] Unknown of the GEOSAR = Unknown"]
-[5.482328414916992, 1.6443545818328857, "[TT] Mission Status of the WorldView-1 = Fully operational as of 2008"]
-[3.455852508544922, 4.876056671142578, "[FF] Ground SAR Image Processor of the X-band SAR payload system = Included"]
-[5.394852161407471, 0.053745996206998825, "[TT] Operation Start Year of the IRS = 1988"]
-[5.987890243530273, 3.277625322341919, "[FF] Number of Spacecraft of the ASTERIA = Dozens"]
-[7.635315895080566, 8.395747184753418, "[TT] Number of Bands of the GLI = 4"]
-[8.37424087524414, 2.1682989597320557, "[FF] Mission Objective of the MWR = Investigate the use of microwave radiometers and to measure both wind speed and direction over the ocean"]
-[4.945949077606201, 0.5074121952056885, "[FF] Launch Date of the Glory = March 4, 2011"]
-[7.837312698364258, 8.86131763458252, "[TT] Wavelength Range of the SWIR Filter Assembly = 1375 nm to 2190 nm"]
-[14.384750366210938, 6.518165111541748, "[TT] Battery Endurance of the Satellite = 5 years"]
-[9.839632987976074, 5.499598979949951, "[TT] Thermistor Telemetry Data of the Satellite = Stable"]
-[9.453230857849121, 4.858692169189453, "[TT] Axes of the Attitude Determination and Control System = Full 3-axis"]
-[4.726336479187012, 1.5596750974655151, "[FF] Launch Date of the GHGSat's Second Satellite = August"]
-[3.818474769592285, 7.171066761016846, "[TT] Gain of the C-band Antenna = More than 32.5dB"]
-[4.6616411209106445, 2.9939639568328857, "[FF] Headquarters Locations of the SAR Satellites = San Francisco, California; Denver, Colorado; Washington, D.C."]
-[5.20288610458374, 0.9498941898345947, "[FF] Construction Completion Date of the BDS-3 = June 2020"]
-[9.47534465789795, -1.0681872367858887, "[TT] Location of the GOES-West = 137\u00ba W"]
-[13.785210609436035, 3.0120768547058105, "[TT] Total payload mass of the Repeater subsystem = 400 kg"]
-[7.655073165893555, 8.396150588989258, "[TT] Number of Bands of the SWIR = 80"]
-[6.598653793334961, 2.8457231521606445, "[TT] Number of Experiment Cultures of the Biofilms = 24"]
-[5.639815807342529, 6.454324722290039, "[TT] Conditions of the Sample Storage = Ultra-pure clean room"]
-[9.235356330871582, -0.6263022422790527, "[TT] Orbit Perigee of the BX-1 = 280 km"]
-[8.596341133117676, 5.9347429275512695, "[FF] Accuracy of the SSAS = 0.1\u00ba to 1\u00ba"]
-[10.84818172454834, 0.9823176264762878, "[FF] Light Production of the Brown Dwarfs = Weaker than stars"]
-[10.451449394226074, 5.775126934051514, "[TT] Temperature Range of the GOES-R satellite = -15 \u00baC to 50 \u00baC"]
-[6.042609214782715, 2.279787540435791, "[TT] Affiliation of the eROSITA = IKI (Space Research Institute), Moscow"]
-[6.457798957824707, -0.8119568824768066, "[TT] LTAN of the Main Payload = 10:39 hours"]
-[6.127594470977783, 8.32082748413086, "[TT] Channels of the RFE = 4 (vertical, horizontal and the sum and difference which is equivalent polarization at \u00b145\u00ba)"]
-[6.3100996017456055, 4.482335567474365, "[FF] Function of the HRIT/EMWIN = High rate information transmission / Emergency managers weather information network"]
-[13.853706359863281, 3.7698910236358643, "[TT] Mass of the Starfire Optical Reflectors = 1.76 kg"]
-[6.226678371429443, 2.973073959350586, "[TT] Imagery Resolution of the WorldView Legion = 30 cm"]
-[6.144887924194336, 6.441420555114746, "[TT] Data Processing of the MODEX-2 = Toggle mode data processing and waveform diversity processing"]
-[8.135793685913086, 8.97421932220459, "[FF] Spectral Domains of the Sentinel-4/UVN = UV (305-400 nm), VIS (400-500 nm) and NIR (750-775 nm)"]
-[5.95556640625, -0.46669235825538635, "[TT] Mission Duration of the ERO = 1 year"]
-[13.605340003967285, 6.892097473144531, "[TT] Power Generation Capacity of the EPS = At least 5 kW (EOL)"]
-[6.230091094970703, 1.9564419984817505, "[FF] URL of the RAIDS = http://ccar.colorado.edu/muri/DoD%20Missions-Budzien.pdf"]
-[7.545902252197266, 5.381519794464111, "[FF] Components of the ORA Instrument = UV-visible module, infrared unit, electronics unit"]
-[6.909293174743652, 4.797476291656494, "[FF] Used of the Racetrack Configuration = Alternative design"]
-[10.56768798828125, 1.9543508291244507, "[FF] Spectrum of the X-ray pulsars = Almost the same as predicted by the model"]
-[7.181098937988281, -0.4116578996181488, "[TT] Gravitational Field Model Update Frequency of the GRACE-FO = Every 30 days"]
-[5.114517688751221, 0.7339268922805786, "[FF] Newsletter Issue of the SHADOZ = 11"]
-[6.692008018493652, 5.397033214569092, "[FF] Devices of the Baseband module = WizardLink family of multi-Gigabit Serializer/Deserializers (Ser/Des), SRAM-based FPGA (Virtex-4QV), High-speed Digital-to-Analog Converter (DAC5675A-SP), antifuse-FPGA, TCXO (Temperature Compensated Crystal Oscillator)"]
-[10.921405792236328, 2.067077159881592, "[FF] Mission of the XMM-Newton = European Space Agency's"]
-[11.775819778442383, 3.233537435531616, "[TT] Central Thruster of the AOCS = One (1) central 11 N thruster"]
-[5.552619457244873, 0.48686572909355164, "[TT] Measurement Start Date of the SOVAP = 21/7/2010"]
-[4.737029075622559, -0.28812092542648315, "[TT] Launch Date of the CATS = January 10, 2015"]
-[5.441831588745117, 6.491692066192627, "[TT] Yearly Capacity of the CLASS data storage per satellite = 670 TB"]
-[7.379260063171387, 0.3091680705547333, "[FF] URL of the OSIRIS-REx = https://earthobservatory.nasa.gov/IOTD/view.php?id=91494&src=iotdrss"]
-[7.252752304077148, 4.488603115081787, "[FF] Complementary Data Source of the VIIRS = AIS and VMS data"]
-[9.525354385375977, 6.825168609619141, "[TT] Range Resolution of the Wide fine = 5.2-15.2 m"]
-[5.61853551864624, -0.14659062027931213, "[TT] Operational Period of the TSIS-1 = 5 years"]
-[10.945749282836914, 7.577526092529297, "[FF] Swath Width of the Back-end electronics = Can easily be adjusted"]
-[10.965397834777832, 6.361917972564697, "[TT] Telescope Material of the RSI = SiC (Silicon Carbide)"]
-[13.164444923400879, 7.279307842254639, "[TT] Power Consumption of the Power consumption = \u2264 25.5 W"]
-[7.3633646965026855, 7.039700984954834, "[TT] ADC Cadence of the AEM = 40 samples/s"]
-[3.4658334255218506, 1.7602163553237915, "[FF] Mission Overview Date of the Sentinel-1 = July 12-17, 2009"]
-[8.258528709411621, 7.453248500823975, "[FF] Technology of the CIRC = Uncooled infrared array detector (microbolometer)"]
-[8.043606758117676, 5.2051310539245605, "[FF] Calibration of the PIANO Airglow Camera = Pre-Flight"]
-[8.361361503601074, 6.9878034591674805, "[TT] Camera Type of the SLIM6 = Multispectral scanning camera"]
-[4.801267147064209, -1.8862264156341553, "[FF] Components of the Chang'e-5 = Lander, orbiter, ascender, returner"]
-[6.978810787200928, 7.012932300567627, "[TT] Beam Type of the Fiber-coupled laser-diode bar = Diverging"]
-[11.69091796875, 2.901123523712158, "[TT] Hydrazine Quantity of the PARASOL microsatellite = 4.5 kg"]
-[6.743524551391602, 1.5204243659973145, "[FF] Symbolism of the Emirates Mars Mission = Named as a symbol of hope for all Arab youth"]
-[14.099763870239258, 7.205438613891602, "[TT] Voltage of the Main Power Bus = 28 to 33 V"]
-[4.1771392822265625, 5.5173516273498535, "[TT] Distress Signal Location Accuracy of the SAR Network = Approximately 100 meters"]
-[13.252264976501465, 5.247702121734619, "[TT] Area of the Solar Panels = 2.44 m2"]
-[5.390710830688477, 0.47624728083610535, "[FF] Mission Expansion Date of the Juno = 13 January 2021"]
-[4.251331806182861, 0.7735574841499329, "[TT] Launch Year of the EDRS-A = 2016"]
-[10.414091110229492, 2.1355702877044678, "[FF] Detection Capability of the NuSTAR = Dark matter particle called the axion"]
-[6.366880416870117, 1.8980690240859985, "[FF] URL of the AVNIR = http://www.eorc.jaxa.jp/ADEOS/Project/Avnir.html"]
-[14.247652053833008, 3.171082019805908, "[TT] Mass of the BIROS = Roughly 130 kg"]
-[14.29570484161377, 3.048215389251709, "[TT] Mass of the BRITE-CA-1 = 7 kg"]
-[5.735397815704346, 0.5275393724441528, "[FF] Largest Commercial ISS User of the UrtheCast = True"]
-[6.520690441131592, 4.417229175567627, "[FF] Function of the Spacecraft Operation Planning System = Planning of the maintenance of the solar array paddle and the battery"]
-[10.533356666564941, 3.3475918769836426, "[TT] CubeSat of the Satellite = 2U"]
-[8.007193565368652, 7.934765815734863, "[TT] No. of Detectors/Channels of the Visible Spectral Band = 4 (+4 spare)"]
-[4.527301788330078, -0.8754422068595886, "[TT] Recovery Location of the Dragon = Southern California"]
-[13.522207260131836, 2.9692323207855225, "[TT] Payload Mass of the Eutelsat 172B = 10,865 kg"]
-[10.446394920349121, 5.786597728729248, "[TT] Low Temperature Limit of the Batteries = -10\u00b0C"]
-[5.410681247711182, 7.708266735076904, "[TT] EIRP/Carrier of the Satellite = 49 dBW"]
-[6.730367183685303, 6.0499587059021, "[TT] Quantity of the Subsystems = 8"]
-[6.203054428100586, 1.7471058368682861, "[FF] URL of the ESTCube-1 = http://icubesat.files.wordpress.com/2012/06/icubesat-org-2012-c-1-3-_presentation_noorma_201205301151.pdf"]
-[11.048652648925781, 1.492469310760498, "[TT] Diameter of the STARSHINE = 47.5 cm"]
-[4.72166633605957, 8.020366668701172, "[TT] Pointing Stability of the LCT LOS = 1 \u00b5rad peak-to-peak for frequencies greater than 100 Hz"]
-[9.696205139160156, 4.14618444442749, "[TT] Spatial Resolution of the Three-axis magnetometer = 38 km"]
-[5.43069314956665, 2.334872245788574, "[FF] Affiliation of the C\u00e9line C\u00e9nac-Morth\u00e9 = Unknown"]
-[6.989666938781738, 7.153876304626465, "[TT] Laser Pulse Footprint of the ATM = 1m"]
-[5.87360954284668, 6.8844804763793945, "[TT] Source Data Rate of the Telescope = 4.0 Mbit/s"]
-[4.429335594177246, 2.8813846111297607, "[TT] Location of the GTHT = Tahiti French Polynesia"]
-[7.939675807952881, 7.646331310272217, "[FF] Purpose of the Hyperspectral Imaging = Characterization and quantification of Earth's surface materials"]
-[4.946653842926025, 2.9830050468444824, "[TT] Prime Contractor for B series of the MetOp-SG = Airbus Defence and Space of Germany"]
-[5.123231410980225, 6.931304931640625, "[TT] Payload Data Downlink Rate of the MightySat II.1 (Sindri) = 1 Mbit/s"]
-[4.958704948425293, 0.8568665981292725, "[TT] Launch Date of the AISSat-1 = July 2010"]
-[5.1246442794799805, 8.47404670715332, "[TT] Spectral range of the MWHS = 150-183 GHz"]
-[9.08456039428711, 7.0046539306640625, "[TT] Resolution of the TeLEOS-1 Imager = 1m nominal at nadir"]
-[9.669066429138184, 8.369040489196777, "[FF] FOV Support Mode of the ABI instrument = 0.5 km resolution, 1 km resolution, 2 km resolution"]
-[6.9931182861328125, 4.256793022155762, "[FF] Unknown of the SAC-A = Unknown"]
-[7.829643249511719, 5.7254180908203125, "[TT] Operation of the INR = Ground-based real time image navigation process"]
-[6.946284294128418, 4.388446807861328, "[FF] Unknown of the MAXI/SEDA = Unknown"]
-[3.0356316566467285, 4.607271671295166, "[TT] Signal In Space Acquisition Band of the GISAR = 1544.05 \u2013 1544.15 MHz"]
-[7.376348495483398, 5.253016471862793, "[FF] Upper Module Components of the Merlin = `sensor board', detectors, associated front-end electronics"]
-[13.37650203704834, 2.1152853965759277, "[TT] Number of Objects of the StrayCats = About 80"]
-[8.718920707702637, 2.6326420307159424, "[FF] Expected Parameter Measurement of the CDE = Cosmic dust influx, PMC nucleation sites"]
-[6.622866630554199, -0.02298692613840103, "[TT] Operation Time of the Cryogenic Coolant System = 3 days out of 13 days"]
-[10.255098342895508, 8.077333450317383, "[TT] Aperture of the NESSI = 15 cm"]
-[13.508749961853027, 2.884124279022217, "[TT] Mass at Launch of the Eutelsat Quantum = 3.5 tons"]
-[3.8493173122406006, -1.1388627290725708, "[TT] Orbit of the Telescope = Lissajous orbit about L2"]
-[6.2571563720703125, 5.533949375152588, "[FF] Start of the Data Compression = Autonomously as soon as the acquisition of data is stopped"]
-[7.726888656616211, 0.4819600284099579, "[TT] Propulsion System of the Lunar IceCube = Miniaturized electric thrusters"]
-[4.4084014892578125, 2.051607370376587, "[FF] Anniversary Date of the Dubaisat-1 = Aug.9"]
-[7.382876396179199, 3.9302186965942383, "[FF] Observation of the GMI (GPM Microwave Imager) = Precipitation across a broad swath"]
-[3.6340794563293457, 4.823537826538086, "[FF] Polarimetric Data of the RISAT-1 = Available in Spotlight and in ScanSAR mode"]
-[9.13769245147705, -1.2743943929672241, "[TT] Orbit Type of the GOES-S = Geostationary"]
-[7.815890312194824, 8.539250373840332, "[TT] Spectral Range of the IIM instrument = 0.48-0.96 \u00b5m"]
-[8.87297534942627, 2.771374225616455, "[FF] URL of the Cluster = http://www.esa.int/Our_Activities/Space_Science/Cluster/Origin_of_high-latitude_auroras_revealed"]
-[6.794795989990234, 1.3538835048675537, "[FF] Agility of the FormoSat-2 = Able to take imagery over the disaster area during its first pass"]
-[10.193243980407715, 7.246492862701416, "[TT] Ground Range x Product Length of the ScanSAR = 100 x 150 km"]
-[14.244744300842285, 3.318145275115967, "[TT] MLI Mass of the MPO TCS = 94 kg"]
-[4.679887771606445, 7.778930187225342, "[TT] Data Reception Frequency from DCPs of the Onboard data collection and transmission system = 401.2-402.0 MHz"]
-[9.24337100982666, 2.295436382293701, "[FF] Authors of the \"Discrete and broadband electron acceleration in Jupiter's powerful aurora\" = B. H. Mauk, D. K. Haggerty, C. Paranicas, G. Clark, P. Kollmann, A. M. Rymer, S. J. Bolton, S. M. Levin, A. Adriani, F. Allegrini, F. Bagenal, B. Bonfond, J. E. P. Connerney, G. R. Gladstone, W. S. Kurth, D. J. McComas & P. Valek"]
-[10.749713897705078, -1.1396969556808472, "[TT] Altitude of the SLATS = 268 km"]
-[5.954231262207031, -0.4944957196712494, "[TT] Mission Duration of the NuSTAR = 10 Years"]
-[4.830228328704834, 0.5959977507591248, "[TT] Launch Date of the Rocket 3.3 = 20 November 2021"]
-[4.152143478393555, 5.740387916564941, "[FF] Operation of the ADS-B = Aircraft determines its position via satellite navigation and periodically broadcasts it"]
-[6.616966724395752, 5.398234844207764, "[TT] Type of the TCS = Semi-active"]
-[8.719054222106934, 5.4866557121276855, "[TT] Pointing Accuracy of the Block 5D satellites = Greater"]
-[3.306572675704956, 2.261514186859131, "[FF] Data Access of the Sentinel-2 = Full and open"]
-[7.068465709686279, 6.850191116333008, "[TT] Stability Requirement of the Laser = Up to 16 years"]
-[5.851075172424316, -0.40220415592193604, "[TT] Deployment Time of the NPSat-1 = 1 hour and 22 minutes"]
-[5.516488552093506, 0.9980205297470093, "[TT] Thermal Vacuum Testing Start Date of the GOES-R satellite = July 1"]
-[2.9819445610046387, -0.36712169647216797, "[TT] Targeted Orbit Altitude of the OneWeb satellites = Roughly 450 km above Earth"]
-[3.6762807369232178, 4.598988056182861, "[FF] Imaging Mode of the RADARSAT-2 = TOPS (Terrain Observation by Progressive Scans)"]
-[9.60402774810791, 4.482512950897217, "[FF] Maneuver Scheme of the P2 = Spin control maneuver scheme"]
-[7.7975263595581055, 4.78778600692749, "[FF] Data Collection of the Sounder = Vertical temperature and moisture profile"]
-[9.046111106872559, 3.6835780143737793, "[TT] Optical Design of the COR2 = Externally occulted Lyot design"]
-[4.509927749633789, 6.007077217102051, "[FF] Algorithms of the Array signal processing = Minimum Mean Squared Error (MMSE) beamforming, DOA (Direction of Arrival) estimation"]
-[7.310610771179199, 4.0988874435424805, "[FF] Purpose of the IGOR+ = Allows the tracking of occulting signals"]
-[5.565567970275879, 0.34833964705467224, "[TT] Reentry Date of the SpinSat = March 15, 2017"]
-[7.882830619812012, 8.297588348388672, "[TT] Normalized to of the PRI = 570 nm"]
-[8.451135635375977, 5.551800727844238, "[TT] Geolocation accuracy of the ALOS/PRISM = 6.1 m (rms)"]
-[12.124977111816406, 1.982200026512146, "[FF] Data Processing of the CartoSat-1 = Advanced"]
-[6.860574722290039, -0.6074724793434143, "[TT] Period of the Satellite Orbit = 9.03 days"]
-[13.798130989074707, 2.6851859092712402, "[TT] Launch Mass of the QuikTOMS spacecraft = 166 kg"]
-[5.706188201904297, -0.6394780874252319, "[TT] Operation Duration of the Block 5D-2 Satellite = Nearly five years"]
-[6.401890277862549, 2.057452917098999, "[FF] URL of the WorldView Legion Satellite Constellation = https://www.businesswire.com/news/home/20170706005679/en/DigitalGlobe-Selects-SSL-Build-Industry-Leading-WorldView-Legion"]
-[10.76312255859375, 1.284453272819519, "[TT] Size of the Parent Star GJ 367 = About half the size of the Sun"]
-[13.368280410766602, 7.361557483673096, "[TT] Power of the HAUSat-2 = > 20 W"]
-[9.650843620300293, 7.9600911140441895, "[TT] f/number of the 50 mm camera = f/1.8"]
-[13.825577735900879, 2.974588394165039, "[TT] Mass of the Meteor-M = ~2,800 kg"]
-[6.265130043029785, 4.80279541015625, "[FF] Data-handling infrastructure of the LIS = TRMM"]
-[8.902175903320312, 7.382385730743408, "[TT] Thickness of the Low LET Detector = 1000 \u00b5m"]
-[7.458680629730225, -0.13169758021831512, "[TT] Final Location Time of the Philae = 17:32 GMT"]
-[13.24445915222168, 5.248832702636719, "[TT] Size of the Solar Panels = 0.81m x 0.72 m"]
-[5.64517068862915, 1.0074260234832764, "[FF] Mission End Date of the IBEX = Unknown"]
-[11.875191688537598, 4.705752372741699, "[TT] Vacuum Chamber Dimensions of the Test Setup = 1.2 m in length and 1 m in diameter"]
-[5.938294887542725, -0.3609503209590912, "[TT] Operation Period of the STRV-2 = 6 months"]
-[6.989584922790527, 0.12752924859523773, "[TT] Travel Duration of the SeaSat = 61 days"]
-[9.781745910644531, 6.9155988693237305, "[TT] ESA: 2.8 x 10 -4 [cm 2 str eV/eV/10\u00ba], ISA: 4.9 x 10 -4 [cm 2 str eV/eV/10\u00ba] of the Geometrical Factor = Geometrical factor ESA: 2.8 x 10 -4 [cm 2 str eV/eV/10\u00ba], ISA: 4.9 x 10 -4 [cm 2 str eV/eV/10\u00ba]"]
-[6.85931921005249, 2.674673557281494, "[FF] Photo of the MEOLUT = Image credit: ESA"]
-[5.5289201736450195, 4.028742790222168, "[TT] Number of Earth Stations of the LAGEOS = 14"]
-[4.325730323791504, 7.536418437957764, "[TT] Frequency of the S-band = 2 GHz"]
-[6.880171298980713, 2.9046974182128906, "[FF] Uplink Sites of the MDD = Bracknell (UK Meteorological Office), Rome (Italian Meteorological Service), Toulouse (France)"]
-[10.358744621276855, 2.3421525955200195, "[FF] Purpose of the Soft X-ray Imager = Make measurements of the Earth's space environment in soft X-rays"]
-[13.365665435791016, 5.475694179534912, "[TT] Solar Arrays of the SEOSat = Fixed body mounted"]
-[5.4922776222229, 0.3801916241645813, "[TT] Launch Date of the GEOS-2 = 11 January 1968"]
-[4.955028533935547, 0.49813368916511536, "[TT] Launch Date of the BeiDou-1A = Oct. 31, 2000"]
-[8.135724067687988, 1.4654942750930786, "[FF] Radar Signature Change of the ENVISAT satellite = Increased with rainfall, then shrank at a rate of 2.4 cm/hr"]
-[9.284104347229004, 5.436338424682617, "[TT] Axis of the ISA = Three"]
-[6.862491607666016, 4.447481632232666, "[TT] Programmable of the RVX FDIR = Yes"]
-[4.990015029907227, 7.887861728668213, "[TT] Output Frequency of the PRARE space segment oscillator = 5 MHz"]
-[7.604555606842041, 0.8333848714828491, "[FF] Mission of the LunaH-Map = Map hydrogen within craters and other permanently shadowed regions throughout the moon\u2019s south pole"]
-[4.196599006652832, 0.5937958359718323, "[TT] Discovery Date of the Integral = 20 Oct. 2003"]
-[11.809507369995117, 0.06136896461248398, "[TT] Number of Pulsating Red Giants Identified of the TESS = More than 158,000"]
-[4.826577663421631, 7.345137596130371, "[TT] TM Rate of the S-band transceivers = 25-384 kbit/s"]
-[7.771202087402344, 5.768451690673828, "[FF] Function of the Processor = Control and synchronise the camera electronics, the SPS, the thermal control and the mechanisms control"]
-[8.354517936706543, 2.2821476459503174, "[FF] Development Team of the SMOG-P = Students supervised by University professors from the Faculty of Electrical Engineering and Informatics (VIK) of BME"]
-[10.586950302124023, 4.984630107879639, "[TT] Height of the Langmuir Probe Assembly = 10 mm"]
-[14.302407264709473, 6.633633136749268, "[TT] Battery Capacity of the Avionics bus = 80 Whr"]
-[10.459226608276367, 2.1505331993103027, "[FF] X-ray Emission of the RCW 89 = Glows with lower-energy X-ray light"]
-[4.627921104431152, 6.248020648956299, "[TT] Beam Control of the APAA = Independently, flexibly and rapidly"]
-[6.024279594421387, 1.1589703559875488, "[FF] Confirmation Decision Date of the NASA = 2033"]
-[6.214727878570557, 3.522932767868042, "[TT] Number of Fixed Experiments of the EAGLE = 4"]
-[13.163057327270508, 7.02921199798584, "[TT] Power/energy provider for EDM of the TGO = Yes"]
-[4.856308460235596, 6.047402381896973, "[FF] Purpose of the Frontier Software Defined Radio = Communication"]
-[12.111395835876465, 4.47064733505249, "[TT] Size of the Spacecraft Repeater = 0.034 m3"]
-[8.476300239562988, 0.33950483798980713, "[TT] Diameter of the Asteroid 1999JU3 = About 900 m"]
-[4.803884983062744, 0.7412031888961792, "[TT] Cease Processing Date of the 121.5 MHz Analog Signals = 1 February 2009"]
-[11.263126373291016, 0.9536989331245422, "[FF] Presentation Date of the LISA = 05-05-2017"]
-[13.745699882507324, 5.393996238708496, "[FF] MZ-Surface Function of the H3 and H4 = Location of solar cells"]
-[7.6831841468811035, -0.8229906558990479, "[FF] Applications Team of the ICESat-2 = Organize and develop a mission applications program"]
-[13.729522705078125, 3.0735559463500977, "[TT] Maximum Mass of the Payload = Up to 600 kg"]
-[6.925492763519287, 4.868506908416748, "[FF]  of the CGG & valve control board = "]
-[8.753121376037598, 8.394204139709473, "[TT] Resolution of the Imaging Spectrometer = 100 m x 400 m"]
-[7.103898048400879, 1.8660074472427368, "[FF] Launch Date of the Carbon Mapper = April 2021"]
-[7.002456188201904, 4.987401485443115, "[FF] Configuration of the OPSIM = One RTU in the loop and the other RTUs are simulated"]
-[7.9128098487854, 4.50388765335083, "[FF] Navigation Method of the Interplanetary spacecraft = Pulsars"]
-[5.416274070739746, 7.198216915130615, "[TT] Bitrate of the EWC27 = Up to 100 Mbit"]
-[9.518553733825684, 7.855243682861328, "[TT] Field of View of the LI = 16\u00ba \u00d8 shifted northward or 84% of visible Earth disk"]
-[7.968711853027344, 2.5981101989746094, "[TT] Accuracy of the Space Weather Models = Not yet exist"]
-[6.717250823974609, -0.2906569540500641, "[TT] Peak of the Observation Time = 31 minutes"]
-[10.991902351379395, 6.31697940826416, "[TT] Material of the Multispectral Imager = Silicon carbide ceramic"]
-[10.938777923583984, 0.5705504417419434, "[TT] Confirmed Transiting Planets of the Kepler-11 = 6"]
-[10.242182731628418, 2.169236183166504, "[FF] X-ray Study of the Chandra X-ray Observatory = Low-energy X-rays from Jupiter's auroras"]
-[8.167730331420898, 2.5680158138275146, "[FF] Product of the GIIRS = Atmospheric Temperature, Humidity and Ozone Profiles (Clear), Atmospheric Temperature and Humidity Profiles"]
-[6.422747611999512, 7.594978332519531, "[TT] Data Quantization of the DubaiSat-1 = 8 bit"]
-[4.146232604980469, 6.540210723876953, "[TT] Beam Type of the Downlink = Narrow"]
-[9.477380752563477, 6.009795188903809, "[TT] Near Incidence Angle of the Instrument = >23\u00ba"]
-[8.746670722961426, 7.207980632781982, "[TT] Measurement Error of the Particle Detectors = < 1%"]
-[4.567409992218018, 7.911316394805908, "[TT] Interference Analysis Frequency of the uFDS = Daily"]
-[8.044861793518066, 3.4267866611480713, "[TT] Spatial Variations in XCO2 of the OCO-2 = <2%"]
-[5.671530723571777, 4.260152339935303, "[FF] Service of the KSAT = Satellite operations as-a-service for ESA's Arctic Weather Satellite"]
-[4.765613555908203, 8.199310302734375, "[TT] Frequency of the SIRAL = 13.575 GHz"]
-[3.334080219268799, 1.709405779838562, "[TT] Realtime Data Availability of the SAPHIR = Since May 2013"]
-[8.550978660583496, 6.151264667510986, "[TT] Accuracy of the CERES = 0.3 Wm -2  sr -1"]
-[8.623345375061035, 1.1270551681518555, "[FF] URL of the Aquarius/SAC-D = http://www.tos.org/oceanography/issues/issue_archive/issue_pdfs/21_1/21.1_lagerloef.pdf"]
-[7.680910587310791, 5.091145992279053, "[TT] Vibration Testing of the TEMPEST-D = Passed"]
-[7.587220668792725, 5.445789813995361, "[FF] Components of the Electro-optical assembly = Off-axis TMA (Three Mirror Anastigmat) optical telescope unit, focal plane assembly, baffle"]
-[10.168312072753906, 5.499057769775391, "[TT] Thermal Control of the Detector = Passive cooling using a space-facing radiative surface"]
-[8.763002395629883, 4.994406700134277, "[TT] Accuracy of the Star Tracker = < 7 arcsec RMS cross-boresight, < 70 arcsec RMS around boresight"]
-[1.6113979816436768, 3.760091543197632, "[TT] Universal TC/TM system of the BEESAT-3 = Yes"]
-[7.539689540863037, 5.3448686599731445, "[FF] Components of the Astro-APS = Camera head, electronics, and a shorter baffle"]
-[11.446817398071289, 4.3643035888671875, "[TT] Size of the SPACE HAUC = 3U"]
-[5.7161688804626465, -0.8045812249183655, "[TT] Design Life of the SPOT-1 = Three years"]
-[8.001837730407715, 2.4005796909332275, "[FF] Observation Parameters of the MWRI = Precipitation, cloud feature, vegetation, soil humidity, sea ice, etc"]
-[8.023056030273438, 5.188335418701172, "[FF] AOI Sensitivity of the PF1 = Unknown"]
-[5.899438858032227, 4.650083541870117, "[FF] Functionality of the Ground Station = Collect satellite telemetry data, send satellite tasking requests, retrieve relayed data, and extract ground sensor data"]
-[5.686853408813477, 7.080975532531738, "[TT] Information Rate of the LRIT = 256 kbit/s"]
-[6.861004829406738, 3.5187511444091797, "[FF] Purpose of the Sabatier Main Controller = Used in conjunction with the Oxygen Generation System (OGS) for water production needs on-orbit"]
-[6.854754447937012, 1.9417061805725098, "[FF] NASA URL of the BioSentinel = https://www.nasa.gov/centers/ames/engineering/projects/biosentinel.html"]
-[5.648346424102783, 2.709118366241455, "[TT] Agency of the CubeRRT = NASA"]
-[9.248602867126465, -0.7176177501678467, "[TT] Orbit of the MTCube-2 (ROBUSTA 1F) = LEO (~ 500 km)"]
-[7.826869487762451, 1.6597040891647339, "[TT] Regeneration Area of the Mangrove Forests = 48 km2"]
-[12.445696830749512, 0.6222121119499207, "[FF] CCDs Procurement of the PLATO = Study of the CCDs procurement was issued by ESA"]
-[5.429129600524902, 3.8128042221069336, "[TT] Number of Satellites of the GRACE-FO = 2"]
-[5.888876438140869, 3.036393642425537, "[TT] Total system cost of the WorldView Legion = $600 million"]
-[5.70444393157959, 5.437459468841553, "[TT] Redundancy of the INSPIRE = Two spacecraft"]
-[3.870022773742676, 6.921915054321289, "[TT] Polarization of the Antenna = Right Hand Circular"]
-[14.053001403808594, 4.145395278930664, "[FF] Mass, Power Consumption of the Instrument mass, power consumption = 6.5 kg, 22 W"]
-[1.7557843923568726, -2.067417860031128, "[FF] Presentation Date of the Hayabusa-2 = Jan. 8-9, 2014"]
-[5.566370487213135, 5.006577968597412, "[TT] Use of the Receiver = Real-time orbit determination, Use of GPS C/A signal observations and navigation messages"]
-[7.752308368682861, 9.064881324768066, "[TT] Wavelength of the Band 1 = 0.4 - 1.1 \u00b5m"]
-[2.988873243331909, -0.3709508776664734, "[TT] Operational Altitude of the OneWeb = Around 1,200 km"]
-[3.278177261352539, 5.19484281539917, "[TT] Roll Bias Requirement of the SAR payload = \u00b1 36\u00b0"]
-[4.539068222045898, 1.8299062252044678, "[TT] Cloud Profiling Radar (CPR) Transition to Operate Mode Date of the CloudSat = May, 20, 2006"]
-[11.196185111999512, 5.840795993804932, "[TT] Material of the C2B = Polycarbonate"]
-[10.819313049316406, 7.4961700439453125, "[TT] Swath Width of the MTVZA-GY = 1500 km"]
-[2.9686450958251953, -0.3610842227935791, "[TT] Altitude of Initial Orbit of the OneWeb Satellites = 450 kilometers"]
-[12.456268310546875, 0.5626453757286072, "[TT] Launch Opportunity of the PLATO = 2022\u20132024"]
-[10.427743911743164, 2.308213949203491, "[TT] Number of X-ray detector arrays of the IXPE observatory = 3"]
-[5.557706832885742, 6.768805503845215, "[TT] Downlink Acquire Time of the IXPE = 60 s"]
-[8.218000411987305, 1.9400144815444946, "[FF] Influence on Storm Growth of the Drop Size Distribution = Changes the rate of evaporation of rain, affects storm structure and behavior"]
-[8.057579040527344, 7.884245872497559, "[TT] Noise performance of the Channel = 6 : 1 min at 2.5% albedo"]
-[9.182854652404785, 4.749698638916016, "[TT] Sun Aspect Angle of the Attitude control = 90\u00ba \u00b1 10\u00ba"]
-[10.387256622314453, 2.3005309104919434, "[FF] Energy Range of the RHESSI = Soft X-rays (about 3 keV) to gamma-rays (up to about 17 MeV)"]
-[9.01636791229248, 3.2601959705352783, "[FF] Meeting Date of the Swarm Magnetometry Package = June 24-26, 2009"]
-[14.641871452331543, 6.648502826690674, "[TT] Battery of the IOD-1 GEMS = CSL 30 Whr Battery"]
-[10.596990585327148, 2.1093027591705322, "[FF] X-ray emission source of the Einstein Observatory = First identified in the 1970s"]
-[5.134801864624023, 8.259065628051758, "[TT] Frequency of the Radiometers = 1.413 GHz"]
-[10.083145141601562, -1.5470155477523804, "[TT] Final Inclination of the FormoSat-2 = 99.14\u00ba"]
-[9.066011428833008, 7.565654754638672, "[TT] Multispectral Resolution of the Resurs-P1 = 3-4 m"]
-[6.192556858062744, 4.389816761016846, "[FF] User Interface of the Gaia = GUI (Graphical User Interface)"]
-[9.78287124633789, 6.320949077606201, "[FF] Components of the Uplink = Slow tip/tilt mirror, dichroic mirror"]
-[5.85910701751709, -0.30336642265319824, "[TT] Deorbit Timeline of the NRCSD = Within 18 months"]
-[9.166655540466309, 4.6959757804870605, "[TT] Perigee Pass Sun Pointing of the Activity Attitude = 360\u00ba"]
-[6.609294891357422, 4.517849922180176, "[FF] Application of the Spaceborne GPS = Limb sounding and global monitoring"]
-[6.4993743896484375, 3.4905903339385986, "[FF] Task Execution of the Dextre robotic arm = Carry out tasks using a suite of three primary tools"]
-[9.809192657470703, 8.77564811706543, "[TT] IFOV of the INSAT sounder = 290 \u00b5rad x 280 \u00b5rad"]
-[8.065500259399414, 0.9847736358642578, "[TT] Start Date of the Cerro Pelado fire = April 22"]
-[7.645922660827637, 6.5858025550842285, "[TT] Image Production of the SECCHI = About 7 images/hour"]
-[10.737826347351074, 3.4667632579803467, "[TT] Size of the Cubesats = 3U"]
-[9.867680549621582, 2.919902801513672, "[TT] Flight Selection of the UNITE = NASA's CubeSat Launch Initiative (CSLI)"]
-[4.396030426025391, 0.6828552484512329, "[TT] Explosion Date of the DMSP-F13 = Feb. 3, 2015"]
-[4.930631160736084, -2.137753963470459, "[TT] Launch Mass of the Chang'e-2 = 2480 kg"]
-[5.6472978591918945, -1.9545694589614868, "[TT] Repeated ground track of the KOMPSAT-3 = 28days/423revolutions"]
-[4.496669292449951, 4.292074680328369, "[FF] Timing of the GPS and Galileo = Different but each system will transmit timing offsets"]
-[5.877172946929932, 1.3492310047149658, "[TT] M-CDR Date of the IXPE observatory = July 10, 2019"]
-[7.934608459472656, 1.178454041481018, "[TT] Observation Date of the Eruption = March 12 and 13, 2016"]
-[4.234978199005127, 5.629830360412598, "[TT] ADS-B Receiver of the CanX-7 = Included"]
-[5.339172840118408, 3.923748016357422, "[TT] Orbital Planes of the T1TL Prototype Constellation = 2"]
-[10.143269538879395, 8.002665519714355, "[TT] Front Face Diameter of the MoonLIGHT Retroreflector = 100 mm"]
-[6.312541484832764, 8.093008995056152, "[TT] Number of Passbands of the Channel 7 = 1"]
-[14.075841903686523, 4.049506187438965, "[TT] Total mass of the eROSITA instrument = ~ 750 kg"]
-[9.221321105957031, 3.050781488418579, "[TT] Rate of Change of the Delta in Solar Phase of Apsides = 0.8\u00ba/year"]
-[9.911223411560059, 2.8471248149871826, "[TT] Launch Date of the Polar Scout 6U CubeSat = December 3, 2018"]
-[9.308448791503906, 3.6797008514404297, "[FF] Earth Magnetic Field Sensor of the NanoSat-1B = COTS AMR magnetic sensor"]
-[4.467504024505615, 3.2554373741149902, "[TT] Location of the RF Backup Station = Matsumoto"]
-[5.677101135253906, 11.36217975616455, "[FF] Approx. peak sensitivity altitude of the Channel 8 = Unknown"]
-[4.7199625968933105, 6.111748695373535, "[FF] TX Power of the Software-Defined Radio (SDR) = Likely need to be increased to close the link at apogee"]
-[4.578900337219238, 7.105009078979492, "[TT] TT&C Subsystem of the CBERS-1 = S-band and UHF-band data transmission"]
-[9.080626487731934, -0.5087433457374573, "[TT] Science Target Orbit Apogee of the ABEX = 60,000 km"]
-[7.501420021057129, -0.8442460298538208, "[TT] End of Life Date of the ICESat-2 = 6 years (Expected)"]
-[7.777082443237305, 1.9821940660476685, "[FF] Warming Cause of the Earth = Human influences, such as deforestation, particulate pollution, and the release of greenhouse gases from the burning of fossil fuels"]
-[9.408255577087402, 6.995700836181641, "[TT] Spatial Resolution - Strip map of the ALOS-2 = 3 m /6 m /10 m"]
-[5.090269088745117, 0.45779505372047424, "[TT] Launch Date of the TSIS-1 = December 2017"]
-[9.234395980834961, 3.4721193313598633, "[FF] Objectives of the EFI = Study of the ambient vector electric field structure of the high-latitude magnetosphere, the cusp, and the plasma mantle"]
-[10.290458679199219, 0.32698550820350647, "[FF] Formation Geometry of the TDX and TSX Satellites = Bistatic Close formation with Large Perpendicular Baseline"]
-[8.32535171508789, 6.045904636383057, "[FF] Image Enhancement of the ISS Crew Earth Observations = Contrast improvement, lens artifacts removal"]
-[5.497949123382568, 1.317163109779358, "[TT] EMC Qualification Date of the Instrument = Summer 2021"]
-[6.9545979499816895, 6.213215351104736, "[TT] Number of Preamplifiers of the Preamp Board = Up to four"]
-[9.636401176452637, -0.16845080256462097, "[TT] Height of the Hunga Tonga-Hunga Ha\u2018apai = More than 120 meters over the surrounding terrain"]
-[9.9271240234375, 1.4931734800338745, "[FF] Mission Type of the Gaia = Astrometric Survey"]
-[13.946959495544434, 7.13078498840332, "[TT] Output Voltage of the Buck-Boost Converter = 65 - 106.6 V"]
-[3.3418216705322266, 5.101590156555176, "[TT] SAR Payload Mass of the RCM = Approximately 600 kg"]
-[4.405529499053955, 3.103168487548828, "[TT] Location of the Ground Station = Guildford, UK"]
-[9.595629692077637, 0.786733865737915, "[TT] Orbital Speed of the Satellite = High"]
-[9.138206481933594, 7.345090389251709, "[TT] Geometric Factor of the Particle Detector = 0.0442 cm 2  sr"]
-[11.793450355529785, 5.424919128417969, "[TT] Bus Structure of the SOHLA-1 = Isogrid panels"]
-[6.275097370147705, 5.129236698150635, "[TT] Function of the Antenna Control Unit (ACU) = Control the antenna"]
-[7.855573654174805, 8.701972961425781, "[TT] NIR Bands Spectral Range of the MTI = 850-1050 nm"]
-[9.662335395812988, -0.37085944414138794, "[TT] Mean Altitude of the RESURS-O1-4 = About 650 km"]
-[5.081345081329346, 8.161574363708496, "[TT] Frequency of the Millimeterwave receiver = 188.5 \u2013 191.5 GHz"]
-[6.115830898284912, 3.4765255451202393, "[FF] Cost of the CubeSat = Low"]
-[7.433435440063477, 8.75869083404541, "[TT] Band 5 of the MSS Instrument = 0.6 - 0.7 \u00b5m"]
-[6.667674541473389, 8.484152793884277, "[TT] Spectral Channels of the POLDER = Eight"]
-[6.402690887451172, -0.6888120770454407, "[TT] LTDN of the LitianicaSAT-2 = 9:30 hours"]
-[11.431751251220703, 4.203803062438965, "[TT] Size of the Sunstorm = 2U"]
-[11.141826629638672, 1.048316240310669, "[FF] Resolution of the LISA = Ten times smaller than an atom"]
-[10.501916885375977, 2.3634042739868164, "[TT] Optic Configuration of the CuPID X-ray telescope = Kirkpatrick/Baez system"]
-[5.637659549713135, 1.3459256887435913, "[FF] Mission Date of the LARES-2 = 21-25 October 2019"]
-[4.557135581970215, 1.4614876508712769, "[TT] Launch Date of the GOSAT-2 = 2018"]
-[10.245153427124023, 7.530636787414551, "[TT] Telescope Type of the GOES Sounder = Cassegrain telescope"]
-[9.539525985717773, 5.320286273956299, "[TT] Alignment of the CRBF and ORBF = Parallel to each other"]
-[10.103551864624023, 7.08607816696167, "[TT] Spatial Resolution of the OSCAT-3 = 25 km"]
-[10.151250839233398, 5.675596714019775, "[FF] Thermal Power Dissipation of the Focal Plane Assembly = Evacuated to the telescope structure"]
-[10.937586784362793, 2.049412727355957, "[FF] Fact Sheet URL of the XMM-Newton = http://sci.esa.int/xmm-newton/47370-fact-sheet/"]
-[5.355498313903809, 8.447965621948242, "[TT] Bandwidth of the DNB = 0.40 \u00b5m"]
-[8.301101684570312, 1.4028451442718506, "[TT] Spatial Resolution (km) of the Precipitation over land ares = 25"]
-[6.055581569671631, 7.9091081619262695, "[TT] Phase Variable Range/Step of the D-Amps = Range: 0 to 360\u00ba; Step: 90\u00ba"]
-[8.318924903869629, 1.7673259973526, "[TT] Unbalance of the Land and Sea Contamination = 2%"]
-[8.257208824157715, 6.660094261169434, "[FF] Instrument Architecture of the OMPS = Staring spectrometer"]
-[7.7015485763549805, 6.501972198486328, "[TT] CONUS Image Collection Interval of the ABI = 5-minute (300-second)"]
-[10.393898010253906, 0.5356966853141785, "[FF] Solar Maximum of the Starshine-2 = Double-peaked"]
-[4.862325668334961, 4.168853282928467, "[TT] Manufacturer of the EPS = GomSpace"]
-[10.102932929992676, 8.062037467956543, "[TT] Size of the VSAT (Very Small Aperture Terminal) = 1.2 m"]
-[2.605280637741089, 3.3310704231262207, "[TT] Quantity of the Flock-2e = 12"]
-[9.248147010803223, 2.600341558456421, "[TT] Number of Witnessed Flare of the NASA spacecraft = Four"]
-[4.789271831512451, 6.31865119934082, "[TT] Mode of the Frontier Radio LT = 1W receive mode"]
-[6.384626865386963, -1.0805258750915527, "[TT] LTAN of the SCATSat-1 = 9:20 hours"]
-[7.205186367034912, 3.8863131999969482, "[FF] Rendezvous Experiment of the PROBA-3 = P3RVX"]
-[6.93480110168457, 0.9711743593215942, "[FF] Solar Panel Dust Accumulation Date of the InSight = June 22, 2021"]
-[8.89406681060791, 2.257253408432007, "[FF] Interstellar Dust Measurements of the Ulysses = October 20, 2015"]
-[6.203287601470947, 4.62894344329834, "[FF] Basic Tasks of the Onboard Data Handling = Storage of housekeeping data, storage and processing of payload data, transition between the satellite modes, execution of the attitude control algorithm, detection and correction of device malfunctions, execution of telecommands, preparation of data for the transmission to the ground station"]
-[12.162962913513184, -0.2961382269859314, "[TT] Sector Monitoring Duration of the TESS = 27 days"]
-[9.00821590423584, 4.436478614807129, "[TT] Photodiode Rotation of the Sun Sensor Suites = 90\u00ba"]
-[14.458999633789062, 6.834039688110352, "[TT] Voltage of the Li-ion battery assembly = 24 V"]
-[8.619277954101562, 3.333041191101074, "[FF] Measurement Objective of the EPISEM = Measure the omnidirectional integral flux"]
-[4.978785514831543, -0.2741280496120453, "[TT] Liftoff Time of the Antares 230 = 04:01:22 EST (09:01:22 UTC)"]
-[4.869085311889648, 2.7925641536712646, "[TT] Market of the EarthSTAR Inc. = People's Republic of China, including Hong Kong and Macao"]
-[6.048558235168457, 2.2086877822875977, "[FF] Primary Objective of the Starshine-3 = Involve more school children in radio science"]
-[8.742318153381348, 6.807607650756836, "[TT] Instrument of the DMC-3 = MSI (BJ-2)"]
-[6.277428150177002, 6.395929336547852, "[TT] Data File Duration of the MABEL = 1 minute"]
-[8.986823081970215, 4.419053077697754, "[FF] Performance of the EKF = Good to around 1.5\u00ba in sunlight"]
-[12.001133918762207, -0.3269549310207367, "[TT] Publication Date of the TESS = 15 April 2019"]
-[13.344229698181152, 7.348670959472656, "[TT] Power Requirement of the MDIM = 1.5 W"]
-[9.696004867553711, -0.5193926692008972, "[TT] Altitude of the SuperView 1A and 1B = 514 km"]
-[11.530943870544434, 3.4487500190734863, "[FF] Operation of the Tsubame = Gas jet is turned on in addition to the ion engines to withstand the drag"]
-[14.473856925964355, 6.585027694702148, "[TT] Battery Location of the Spacecraft = Anti-nadir panel"]
-[13.360274314880371, 6.798633098602295, "[TT] Thermionic Emission Power Draw of the SPC = No more than 0.1 mW"]
-[9.014042854309082, 8.55022144317627, "[TT] Band 3 Wavelength Range of the Telescope = 3.80 - 4.00 \u00b5m"]
-[5.122669219970703, 0.6732600927352905, "[FF] Status Report Date of the PRARE = Sept. '90"]
-[6.1823015213012695, 3.999626874923706, "[FF] Background Removal of the Software Tools = Flexible"]
-[6.964303970336914, -0.346273809671402, "[TT] Satellite Configuration Frequency of the HyperScout\u00ae = Once per day"]
-[8.219095230102539, 1.419534683227539, "[TT] Summer Rainfall of the Cedar City, Utah = 0.05 inches"]
-[3.085167169570923, -0.043840162456035614, "[TT] Orbital Slot of the GSAT-0203 = B08"]
-[13.40146541595459, 7.149828910827637, "[TT] Energy Storage Margin (60 minute window) of the RASP = 62.9%"]
-[10.914920806884766, 7.456666469573975, "[TT] Swath of the OLCI = 1270 km"]
-[3.939328670501709, 9.713361740112305, "[TT] Frequency (GHz) of the ICI-7 = 325.15\u00b11.5"]
-[4.773558616638184, 8.580757141113281, "[TT] Center Frequency of the Channel 4 = 31.5 GHz"]
-[5.277748107910156, 8.114648818969727, "[TT] Sensitive Frequency Range of the Phasemeter = Approximately 2 - 15 MHz"]
-[4.8130269050598145, 8.26225471496582, "[TT] Frequency of the HSB = 183.3 GHz"]
-[4.726851940155029, 0.8670915365219116, "[TT] Phase CD/E1 Proposal Start Date of the PROBA-3 = Autumn 2013"]
-[9.725284576416016, -0.5811638832092285, "[TT] Orbit Altitude of the VesselSat-1 = ~ 865 km"]
-[8.286519050598145, 1.9912760257720947, "[FF] Data of the RapidScat = Semi-diurnal differences"]
-[7.117819786071777, 6.750815391540527, "[TT] Integration Time of the N-FEE = 22.5 s"]
-[6.95520544052124, 1.2567020654678345, "[TT] Mission of the Mars Hope probe = Orbit Mars"]
-[7.895893096923828, 8.263736724853516, "[FF] Spectrum of the FCI = Visible, near-infrared and infrared"]
-[10.293646812438965, 7.369561672210693, "[TT] Design of the Optical Payload = Two-mirror telescope"]
-[8.082723617553711, 4.554782867431641, "[FF] Design Hypothesis of the Geometric Calibration System = Seasonal change can be sufficiently modelled for a pair of months with a 1st order polynomial against sun \u03b2 angle"]
-[13.810111045837402, 2.9005541801452637, "[TT] Mass of the Spacecraft = 6.5 kg"]
-[7.798276424407959, 5.766366481781006, "[FF] Type of the FPP = Housing two filtergraphs and a spectro-polarimeter"]
-[5.6517252922058105, 0.7431510090827942, "[FF] Delivery Date of the FORMOSAT-7 = May 1, 2015"]
-[10.493878364562988, 3.3743033409118652, "[TT] Power Source of the CubeSats = Does not require any extra power from the rocket"]
-[2.9077930450439453, 4.468285083770752, "[TT] LOS Distance Change of the PALSAR-2 = At least 1.5 metres"]
-[5.912724018096924, 1.8658311367034912, "[FF] Launch Date of the Orion Capsule = December"]
-[6.7291178703308105, 4.010775566101074, "[FF] Symposium Location of the HSC-III = Berlin, Germany"]
-[5.2052998542785645, -0.9678875207901001, "[TT] Launch Date of the Kolibri-2000 = March 20, 2002"]
-[11.778908729553223, 3.250173330307007, "[TT] Development Status of the 20 N Thruster = Near-flight-ready"]
-[9.654152870178223, -0.6979197263717651, "[TT] Orbit Altitude of the GeoCARB = Approximately 35,786 km above the equator"]
-[7.682271480560303, 0.4590838551521301, "[FF] Attitude Determination and Control Subsystem of the Lunar IceCube = BCT's (Blue Canyon Technologies) XACT attitude determination and control subsystem"]
-[4.910778522491455, 3.163593292236328, "[TT] Manufacturer of the Net = Airbus (Germany)"]
-[10.391045570373535, 4.461855888366699, "[TT] Quantity of the Landing Legs = 4"]
-[14.032815933227539, 7.106544494628906, "[TT] Output Voltages of the EPS Card = 3.3, 5 and 12 V"]
-[7.057791709899902, 0.9189935922622681, "[FF] X-band radio of the InSight = Measure the \"wobble\" of Mars as it spins"]
-[5.204685211181641, 1.7520101070404053, "[TT] AIS Status of the AISSat-1 = Fully operational"]
-[9.260982513427734, 3.209644079208374, "[TT] Developer of the Solar Wind Monitors = Los Alamos National Laboratory"]
-[7.837543487548828, 8.429381370544434, "[TT] Bands of the OLS = Three bands in the visible (VIS) and thermal infrared (TIR) ranges"]
-[5.049331188201904, 0.6154712438583374, "[TT] New Deadline for Completion of the SpaceIL = December 2017"]
-[10.657808303833008, 7.349823951721191, "[TT] Swath Width of the Instrument = 1650 km for IR bands"]
-[7.410194396972656, 1.014603853225708, "[FF] URL of the GRAIL = http://moon.mit.edu/index.html"]
-[7.053864479064941, 0.26003503799438477, "[TT] Study Duration of the SeaSat = Two years"]
-[5.907638072967529, 7.1555256843566895, "[TT] Data Rate of the POLDER-P = 883 kbit/s"]
-[10.198253631591797, 4.062803745269775, "[TT] Mounting Location of the VMAG = On the tip of the -Z boom"]
-[7.454394817352295, 0.36215776205062866, "[TT] X-ray Spectrometer of the OSIRIS-REx = REXIS"]
-[10.50385856628418, 1.7174216508865356, "[TT] Brightness of the Companion Star = five times fainter than the primary star"]
-[4.730944633483887, 0.7771050930023193, "[TT] Phase A Start Date of the PROBA-3 = October 2006"]
-[5.088659763336182, 2.9613404273986816, "[TT] Consortium of the Meteosat = European subcontractors"]
-[18.647525787353516, 3.9392037391662598, "[TT] NE\u0394T of the 6 = 0.5 K"]
-[4.284876823425293, 0.3586229383945465, "[FF] Deployment Date of the JPL = 7 Dec. 2017"]
-[4.928826332092285, 3.3457577228546143, "[TT] Manufacturer of the NewMag = UCLA (C. T. Russell)"]
-[8.771147727966309, 3.4074370861053467, "[FF] Function of the HPD (High-energy Particle Detector) = Probe the near-moon space environment"]
-[5.747743129730225, 0.440639853477478, "[TT] Decommissioned Date of the FormoSat-2 = August 22, 2016"]
-[7.819282531738281, 3.0627264976501465, "[TT] January 2016 Value of the CO2 Concentration = 401.1 ppm"]
-[9.585002899169922, 0.5970791578292847, "[TT] Distance from the Moon of the Satellite = 18,000 km"]
-[6.447569847106934, -1.2571289539337158, "[TT] First Science Data Release of the GRACE-FO = About seven months"]
-[5.495527744293213, 0.7699836492538452, "[TT] Critical Design Review Date of the Instrument = Early 2020"]
-[6.0242228507995605, 5.665546894073486, "[TT] Redundancy of the SSTL Signal Generator Chain = One chain"]
-[4.5473127365112305, 1.480565071105957, "[TT] Launch Date of the GOSAT-2 = 29 Oct 2018"]
-[7.724703311920166, 0.5425282120704651, "[FF] Science Goal of the Lunar IceCube = Investigate the distribution of water as a function of time of day, latitude, and regolith composition"]
-[9.429082870483398, 5.423360824584961, "[TT] Acceleration Rate of the APM = 0.4\u00ba s-2"]
-[10.552220344543457, 4.9168620109558105, "[FF] Deployment of the Langmuir Probe = Must be made deployable"]
-[9.151473045349121, 6.4666428565979, "[TT] Inertial Reference Unit Resolution of the TDP = 1 m/s"]
-[5.2089948654174805, 4.877477169036865, "[TT] Type of the GPS-In ATT = GPS-In"]
-[10.364972114562988, 5.754077911376953, "[TT] Temperature of the Passive Radiator = 150 K"]
-[4.223570346832275, 7.25618839263916, "[TT] Developer of the X-band transmitter = Syrlinks in France"]
-[5.336329936981201, 8.06105899810791, "[TT] Dynamical Disturbances of the Test Masses = < 3 x 10-14 m s-2 Hz1/2 @ 1 mHz"]
-[7.448282718658447, 7.724849700927734, "[TT] Dynamic Range of the Kruiz CCD = 2500"]
-[5.958135604858398, 1.537268877029419, "[TT] Detectors Service Unit Status of the IXPE observatory = Complete"]
-[1.7158910036087036, 6.140616416931152, "[TT] Ordinary Matter Percentage of the Universe = 5 percent"]
-[9.341623306274414, 4.5661492347717285, "[TT] Number of Units Fabricated of the MinXSS = 3"]
-[6.067746162414551, -1.9468425512313843, "[TT] Member of the Richard Bevilacqua = True"]
-[10.492914199829102, 2.365781307220459, "[FF] Throughput of the Cupid X-ray telescope = Unknown"]
-[3.530973434448242, 3.5630366802215576, "[TT] Owner of the PAZ = Ministry of Defence"]
-[5.53350305557251, -0.696022629737854, "[TT] Design Life of the Yutu-2 = Three months"]
-[6.796357154846191, 3.2269465923309326, "[FF] Purpose of the EDC = Investigating how best to safeguard the health of America's future astronauts"]
-[9.570817947387695, 9.181391716003418, "[TT] Eclipse-Free Viewing of the IRIS = 7 months per year"]
-[6.023502349853516, 7.144530773162842, "[TT] Data Rate of the Instrument = 40 kbit/s"]
-[6.722627639770508, -0.1463429033756256, "[TT] Refresh Rates of the Satellite System = 2 hours typically in equatorial regions"]
-[13.21767807006836, 7.246490001678467, "[TT] Power Consumption of the Total = < 75 W"]
-[7.916238307952881, -0.8900790810585022, "[TT] Measurements of the ICESat-2 = More than 2 billion in its first week"]
-[9.3914155960083, 0.02303401008248329, "[TT] Height of the Pas Moraine = About 30 meters (100 feet)"]
-[6.54539680480957, 5.490472316741943, "[FF] Function of the SSRU = Receive, process, store and transmit the image data"]
-[9.607813835144043, 7.127643585205078, "[TT] Spatial Resolution of the OLS = 2.7 km"]
-[6.713788986206055, -0.29050615429878235, "[FF] Time Period of the Broad Band Receiver = 7 seconds"]
-[10.46533203125, 3.4069700241088867, "[TT] Model of the Syrlinks EWC27 CubeSat X-band transmitter = EWC27"]
-[5.2187418937683105, 0.8188533782958984, "[FF] Presentation Date of the Agile data downlink solutions = June 4-8, 2012"]
-[8.91294002532959, 6.859253883361816, "[FF] Image Resolution of the OSIRIS-REx = High enough to produce digital terrain maps and global image mosaics"]
-[9.538654327392578, -0.4980199635028839, "[TT] Orbit of the ERBS satellite = 507 km x 559 km"]
-[5.798005104064941, 1.6831215620040894, "[TT] Arrival Date at NASA Plum Brook of the Orion = November 22, 2019"]
-[7.83242654800415, 8.468692779541016, "[TT] Emissive Band Wavelengths of the VIIRS = 3.74, 11.45, 3.75, 4.05, 8.55, 10.76, and 12.01 \u00b5m"]
-[5.594700813293457, 0.6099652647972107, "[FF] Operational Date of the ERS-1 = Unknown"]
-[5.740188121795654, 0.46690165996551514, "[FF] Data Collection of the SSM/I and SSMIS = 1991-1997 and 2009-2015"]
-[8.193345069885254, 5.218865394592285, "[TT] Blackbody Calibration Target of the ISIR = Included"]
-[11.98424243927002, -0.4059087634086609, "[TT] Mission Operator of the TESS = MIT"]
-[8.60841178894043, 0.47383004426956177, "[TT] Area of the Victoria Island = Around 200,000 km2"]
-[10.660270690917969, -0.16288840770721436, "[FF] Observation Target of the Tandem-L = Earth\u2019s surface"]
-[10.905065536499023, 7.536558628082275, "[TT] Swath Width of the ATM = 40 m"]
-[9.1954345703125, 7.458249568939209, "[TT] Distance Range of the Camera = A few km to ~50 km"]
-[6.985818862915039, -0.7076761722564697, "[TT] Orbital Period of the Eta Carinae = 5.5 years"]
-[3.5737061500549316, 4.791682720184326, "[TT] Instrument Type of the GF-3 = Imaging microwave radars"]
-[9.189801216125488, 6.072299480438232, "[TT] Control of the Argus = 3-axis"]
-[11.776456832885742, 6.633612155914307, "[TT] Energy Range of the Proton spectrum = 1 GV to 1.8 TV"]
-[5.809930801391602, 4.279648303985596, "[TT] Instrument Type of the ADEOS Comms = Communications"]
-[5.955178737640381, 8.748147964477539, "[TT] MTF of the Satellite = > 0.3 in N/S direction @ Nyquist frequency"]
-[7.63321590423584, 0.9834912419319153, "[FF] URL of the Gravity Recovery and Interior Laboratory (GRAIL) = http://www.lpi.usra.edu/meetings/lpsc2013/pdf/1777.pdf"]
-[6.6602091789245605, 5.3731369972229, "[FF] Advantages of the LCT = Higher data rate, larger link distance, lower size, weight and power"]
-[8.698775291442871, 7.643472194671631, "[TT] Pixel Size of the Kruiz CCD = 9 \u00b5m x 9 \u00b5m"]
-[8.327054977416992, 7.471148490905762, "[TT] Number of Elements of the InGaAs photodiodes = 8"]
-[4.8211469650268555, 0.5906251668930054, "[TT] Planned Operation of the GOES-T = On-orbit storage until it transitions to operational service"]
-[13.514571189880371, 7.408405303955078, "[TT] Output Power of the HPAs = 28 dBm"]
-[5.402359485626221, 4.200606822967529, "[FF] Variant of the A2100 geosynchronous spacecraft bus = GOES-R"]
-[5.507887840270996, 2.2944743633270264, "[TT] Agency of the SpaceX CRS-16 = NASA"]
-[6.382241249084473, 3.4541895389556885, "[FF] Purpose of the WSF-M = Mitigate DoD Space-Based Environmental Monitoring gaps"]
-[12.04716682434082, 4.568166255950928, "[TT] Width of the Large Space Simulator (LSS) = 10 m"]
-[9.81312370300293, 5.5602521896362305, "[TT] Decenter of the M1 = 10 \u00b5m"]
-[6.449965000152588, 5.1904802322387695, "[FF] Components of the Avionics bus = Three main PCBs \u2013 EPS, C&DH, and Backplane"]
-[7.39573335647583, 4.361376762390137, "[FF] Sensors of the SPOT-4 = Unknown"]
-[11.969136238098145, 4.987704277038574, "[TT] PCB Volume of the MPPT = 50 mm x 82,4 mm"]
-[6.205251693725586, 2.417476177215576, "[FF] Software Load of the EFT-1 = About 50% of the entire software load that is required for crewed flight on EM-2"]
-[6.790133476257324, 5.979745864868164, "[TT] Quantity of the MC3 = 6"]
-[8.710094451904297, 7.799561500549316, "[FF] Manufacturer of the UL 03041 pixel ULIS microbolometer array = ULIS"]
-[6.404076099395752, -0.01675606332719326, "[TT] Global Coverage Time of the MESSR = 17 days"]
-[5.356333255767822, 0.6282626390457153, "[FF] Reentry Date of the Long March 5B = 9 March 2021"]
-[5.320045471191406, 1.0808937549591064, "[FF] Mission Date of the FireBird = May 11-15, 2015"]
-[8.13183879852295, 0.7083348631858826, "[FF] Groundwater Storage Measurement of the GRACE-FO = Blue areas have more water than usual, and orange and red areas have less"]
-[6.771280765533447, 4.797942161560059, "[FF] Functionality of the AOCS = Variable"]
-[13.586302757263184, 6.99946403503418, "[TT] Power System of the GNB = Direct energy-transfer"]
-[13.745427131652832, 5.3888773918151855, "[TT] Solar Cells Type of the Power Subsystem = Triple-junction"]
-[11.837030410766602, 6.751180171966553, "[TT] Energy Range of the EPD-E = 50 keV \u2013 4 MeV"]
-[10.593539237976074, 3.36922287940979, "[TT] Type of the LituanicaSAT-2 = 3U CubeSat"]
-[8.442455291748047, 7.683149337768555, "[TT] Detector Type of the Instrument = 2D CCD of 1024 x1024 pixels in VIS; 2D InGaAs detector of 320 x 240 pixels in NIR"]
-[5.358175277709961, 3.8986384868621826, "[TT] Number of Sprite satellites of the KickSat = 104"]
-[9.775359153747559, -0.36202794313430786, "[TT] Altitude of the RemoveDebris = <400km"]
-[11.656620979309082, 4.781306743621826, "[TT] Shape of the S/C structure = Hexagon with a diameter of 50 cm and a height of 53 cm"]
-[13.619190216064453, 5.429981708526611, "[TT] Provider of the Next generation solar cells / Azur = Azur Space GmbH"]
-[3.6700267791748047, -1.0501827001571655, "[TT] Orbit Type of the MMO = Polar elliptical orbit"]
-[6.617598533630371, 0.20604905486106873, "[TT] Operation Start Date of the CryoSat-2 = April 8, 2010"]
-[10.755990028381348, 0.9365596771240234, "[TT] Size of the WD 1856 b = Jupiter-size"]
-[6.178136825561523, 2.986281156539917, "[FF] Monitoring Capabilities of the WorldView Legion = High-agility point collects for monitoring targets and large-area collects for mapping missions"]
-[5.695032119750977, 5.527312755584717, "[FF] Core Processors of the Hayabusa-1 SRC = Discontinued"]
-[3.668027877807617, 5.3023152351379395, "[TT] Number of Cores per Node of the SAR Processor = 8"]
-[8.106703758239746, 0.6820619106292725, "[TT] Groundwater Storage Measurement Date of the GRACE-FO = January 11, 2021"]
-[6.174374103546143, -0.5988126397132874, "[TT] Collection Mode Duration of the Genesis spacecraft = 2 years"]
-[10.010238647460938, -1.567029595375061, "[TT] Inclination of the ADEOS-II = 98.62\u00b0"]
-[13.315718650817871, 5.70275354385376, "[TT] Connection of the TJ Array = Connected via the switches (MOSFET, for biasing) to the negative end of the high-voltage solar array"]
-[9.648236274719238, 1.3961405754089355, "[TT] Daily Revisit Frequency of the Pleiades Neo-3 = At least twice a day"]
-[9.438323974609375, -1.2460604906082153, "[TT] Orbit Direction of the Space Station = From west to east"]
-[10.078529357910156, 2.9353599548339844, "[TT] Development Time of the CubeSat = 2 years"]
-[10.197442054748535, 4.56677770614624, "[TT] Momentum wheel of the ADCS = 0.002 Nms at 2000 rpm"]
-[4.562886714935303, 0.1466025710105896, "[FF] Press Release Date of the Smile = 30 July 2019"]
-[13.802437782287598, 3.9890780448913574, "[TT] Mass of the Micro-spectrometer = 0.250 kg"]
-[8.516294479370117, 4.174331188201904, "[FF] Measurement Principle of the SREM = Examining the sizes of charge pulses generated by charged particles in silicon diodes polarized in reverse by a high voltage"]
-[11.216525077819824, 5.671444416046143, "[TT] Material of the Wire = Teflon-coated 29 gauge copper-stranded wire"]
-[6.705473899841309, 2.2929275035858154, "[FF] Additional Experiments of the Kounotori = Upgrade to the Cell Biology Experiment Facility (CBEF-L), a small-sized satellite optical communication system (SOLISS), and a payload for testing the effects of gravity on powder and granular material (Hourglass)"]
-[11.755550384521484, 6.64411735534668, "[TT] Energy Range for Protons of the Spectrometer = 8 to 120 MeV/(mg/cm2)"]
-[9.209471702575684, -0.4024353325366974, "[TT] Apogee of the Geotail = 870,000 miles (1.4 million km)"]
-[3.761920690536499, -0.8370172381401062, "[FF] Status of the LCTs = In orbit"]
-[9.691000938415527, -0.3272564113140106, "[TT] Altitude Range of the LF = 12.6 to 52.4 km"]
-[13.347082138061523, 7.849271774291992, "[TT] Power Consumption of the X-band transmitter = Below 10 W peak, 1 W mean/orbit"]
-[6.342936992645264, 4.7065534591674805, "[FF] Functionality of the Software = Object recognition, satellite alignment, fine pointing, target recognition, stage recognition, image capture, image transmission, attitude acquisition"]
-[4.486558437347412, 2.989739418029785, "[FF] Location of the Command/Readout Stations = Fairchild Air Force Base (FAFB), near Spokane, Washington, and Loring Air Force Base, Limestone, Maine"]
-[5.674585342407227, 11.350631713867188, "[FF] Approx. peak sensitivity altitude of the Channel 4 = Unknown"]
-[10.737154006958008, 3.4675819873809814, "[TT] Size of the APSS-1 = 1U CubeSat"]
-[12.090888977050781, -0.3664979338645935, "[TT] Primary Mission Duration of the TESS = Two-year period"]
-[4.833726406097412, 0.1342557668685913, "[TT] End of Life Date of the ST5 = 30 June 2006"]
-[6.059357643127441, 4.605777263641357, "[FF] Concept of the Data Center = Compactness, self-automation, high speed, user oriented"]
-[6.105734825134277, 1.8174235820770264, "[TT] URL of the Peter Wegner = https://web.archive.org/web/20150423114038/http://www.responsivespace.com/Papers/RS2012/SPECIAL%20SPEAKERS/Dr.%20Peter%20Wegner/Dr.%20Peter%20Wegner.pdf"]
-[9.711338996887207, 1.39362370967865, "[TT] Resolution of the Pleiades-1A = 50 cm"]
-[8.396803855895996, 4.896521091461182, "[FF] Glint Handling of the VBS = Special filter attempts to recover optical information from the non-affected parts of the image"]
-[5.546349048614502, 2.218838930130005, "[FF] Affiliation of the Kazifumi Fukuda = Unknown"]
-[7.201055526733398, 6.749892711639404, "[TT] Laser Transmitter Range of the OLA = ~7.5 km down to ~1km"]
-[7.806424140930176, 7.150254726409912, "[TT] Frame Rate of the Camera = 15, 30, 60, 110 frames/s"]
-[9.601438522338867, 4.227382659912109, "[TT] Quantity of the Magnetometers = Several sensors"]
-[9.468008995056152, 5.549266338348389, "[TT] Maximum Elevation Slewing Rate of the OCTL = 10\u00ba/s"]
-[3.736069917678833, -0.737991213798523, "[TT] Orbit Type of the LEO Satellites = Low Earth Orbit (LEO)"]
-[7.829402446746826, 2.934962034225464, "[FF] Team Leader of the CO2 Flux inversion = Xiangjun Tian"]
-[9.225321769714355, 7.258824348449707, "[TT] Image Resolution of the EROS-B = Up to 50 cm"]
-[9.754505157470703, 0.7669942378997803, "[TT] Orbit Distance of the 55 Cancri e = 0.015 astronomical units from its Sun-like star"]
-[14.663671493530273, 6.674013137817383, "[TT] Capacity of the NiCd batteries = 4 Ah"]
-[5.943450450897217, 2.506237745285034, "[FF] Dragsail of the Spaceflight Industries\u2019 SSO-A mission = Unknown"]
-[3.2405831813812256, 4.956754684448242, "[TT] Range Coverage of full-pol. in fine mode of the ALOS-2 SAR = 30 km"]
-[12.246689796447754, 3.6856625080108643, "[TT] Critical Viscosity of Xenon of the CVX-2 = 100%"]
-[14.315351486206055, 2.7681655883789062, "[TT] Mass (kg) of the KOMPSAT-5 = 1400"]
-[7.091268539428711, 3.441213846206665, "[FF] Objective of the ScaRaB = Collection of data on shortwave and longwave radiation"]
-[6.292786121368408, 8.11359691619873, "[TT] No of Passbands of the Channel 5 = 1"]
-[10.414838790893555, 5.622042655944824, "[FF] Temperature of the Jupiter's Atmosphere = Much higher than it is at the top"]
-[9.5285005569458, 6.32374906539917, "[TT] Viewing Angle of the ELENA = 4.5\u00ba x 76\u00ba"]
-[6.399484157562256, 1.0619713068008423, "[FF] Mission Overview and Status Date of the WindSat = June 5, 2006"]
-[7.720156669616699, 6.392754554748535, "[TT] Mesoscale #2 of the ABI = 1 minute"]
-[16.499059677124023, 3.6050407886505127, "[TT] Ownership of the OneWeb = Partly owned by the British government"]
-[11.237435340881348, 5.784147262573242, "[FF] Flaps Material of the Thermal Control Louvers = Aluminum"]
-[6.95062255859375, 8.826278686523438, "[TT] Saturation Level of the POLDER-1/2 = 1.1"]
-[9.292832374572754, -1.191774606704712, "[TT] Orbit of the Eutelsat 172B = GEO at 172\u00baE longitude"]
-[7.224693775177002, 1.7023009061813354, "[FF] Investigating Parameter of the SporeSat = Gravitational Threshold for Calcium Ion Channel Activation"]
-[13.520805358886719, 2.806533098220825, "[TT] Wet Mass of the CSC = ~300 kg"]
-[6.530929088592529, -1.9571539163589478, "[TT] Bus Type of the Jason-2 = Proteus"]
-[5.973230838775635, 0.5157278776168823, "[FF] Publication Date of the Rosetta = 26 January 2015"]
-[6.02835750579834, 0.9769682288169861, "[FF] Comparison Date of the AGRI = 11 January 2019"]
-[9.673247337341309, 8.115781784057617, "[FF] Wavefront Sensing of the DeMi = Image plane and pupil plane (Shack-Hartmann)"]
-[4.383686065673828, 6.800528049468994, "[TT] Frequency Bands of the Antenna for Navigation = L1/L2"]
-[4.423835754394531, 5.828362941741943, "[TT] Receiver Reconfiguration of the GomX-3 = Recorded the information in the aircraft signals needed by the UK Met Office"]
-[4.277037620544434, 0.7270750403404236, "[TT] Launch Date of the EDRS-C satellite = 24 July 2019"]
-[5.894445896148682, -0.01499965414404869, "[FF] Number of CRs collected in 10 years of the PM = Greater than the number of CRs that could be collected in the SCM scenario"]
-[9.106803894042969, 3.190885305404663, "[FF] Objective of the TRACE = Collect comprehensive multispectral images of solar plasmas at temperatures from 104 - 107 K with 1 arcsecond spatial resolutions and excellent temporal resolution and continuity"]
-[5.041848182678223, 0.8461215496063232, "[FF] Operations Date of the MCubed-2 = April 22, 2014"]
-[5.940861701965332, 1.5790868997573853, "[FF] Conference Date of the Multi-satellite Operations System = April 25-30, 2010"]
-[8.458443641662598, 8.064659118652344, "[TT] Detectors of the Grating Spectrometer = 256 element InGaAs diode arrays"]
-[6.813287258148193, 4.194805145263672, "[FF] Symposium Date of the HSC-III = May 4-7, 2009"]
-[10.476842880249023, 2.341691017150879, "[FF] Data Telemetry of the Cupid X-ray telescope = Time and position information of every photon measured by the MCP"]
-[6.645025253295898, 2.7556097507476807, "[FF] Design Date of the Weather Ssystem Follow-On \u2014 Microwave = December 2017"]
-[4.7931365966796875, 0.5439974665641785, "[TT] Launch Date of the Inspiration4 = Sept. 15"]
-[7.420425891876221, 4.737775802612305, "[FF] Conference Presentation Date of the Appliqu\u00e9 Sensor Interface Module = Aug. 13-16, 2007"]
-[2.847388744354248, 0.08956850320100784, "[TT] J2000 right ascension (deg) of the B0540-69 = 85.04668"]
-[5.903602123260498, -0.4046817719936371, "[TT] Nominal Operations Duration of the PROBA-3 = About 22 months"]
-[2.3320651054382324, 1.2975893020629883, "[TT] Deployment Time of the NanoSail-D2 = 30-45 seconds"]
-[6.820568084716797, 0.8653410077095032, "[FF] Article Date of the Tooley Crater = 26 January 2021"]
-[4.894030570983887, 7.371120452880859, "[TT] S-band transceivers Data Rate of the PCDU = 20 kbit/s TC"]
-[9.754023551940918, -0.5776955485343933, "[TT] Orbit Altitude of the PACE = 600-800 km"]
-[13.18795108795166, 7.291713237762451, "[TT] Power Consumption of the PCDM = 164.2 W"]
-[5.64063835144043, 1.9471653699874878, "[FF] Development of the RISING-2 = By Tohoku University and Hokkaido University"]
-[8.611532211303711, 4.066136360168457, "[FF] Principle of the Sensor = Amperometric three electrode principle"]
-[8.165797233581543, 6.641275405883789, "[FF] Optical Performance of the ASPIICS = Unknown"]
-[4.439970970153809, 7.840228080749512, "[TT] Microwave Link Frequencies of the GRACE-FO = 24 GHz (K-band) and 32 GHz (Ka-band)"]
-[9.096061706542969, -1.1846450567245483, "[TT] Orbit of the EDRS-A = Low"]
-[8.84730339050293, 7.2297682762146, "[TT] Differential Photometry of the BRITE = < 0.1%"]
-[6.296332359313965, 2.9741077423095703, "[FF] Centrals of the DRR = NOAA/NESDIS (National Environmental Satellite, Data, and Information Service), NCEP (National Centers for Environmental Prediction), AFWA (Air Force Weather Agency), FNMOC (Fleet Numerical Meteorology and Oceanography Center), NavOceano (Naval Oceanographic Office)"]
-[11.747349739074707, 3.3208279609680176, "[TT] Engines of the Propulsion Qualification Model = 21"]
-[7.636361122131348, 5.569018840789795, "[FF] Components of the VBN (Visual Based Navigation) system = LiDAR and 2D camera"]
-[3.08600115776062, 1.7709122896194458, "[TT] Repeat Intervals of the Copernicus Sentinel-1A and -1B = Six to 30 days"]
-[11.608475685119629, 3.239081859588623, "[TT] Number of Activation Cycles of the Electric Thruster = About 2500"]
-[8.368966102600098, 5.741487503051758, "[FF] Data Product Accuracy of the EUVS = \u226420% over mission life, 18% over mission life"]
-[8.154234886169434, 8.454069137573242, "[TT] Spectral Range of the KMS = Visible and near-infrared (VNIR)"]
-[4.369407653808594, 2.084177017211914, "[FF] Launch Date of the Dubaisat-1 = Aug.9, 2010"]
-[5.255695819854736, 7.849931240081787, "[FF] Frequency Range of the Variant = 0.1 Hz to 40 kHz"]
-[9.319275856018066, 7.351418495178223, "[TT] Spatial Resolution of the Pan Imager = 8 m"]
-[9.656418800354004, -1.4996488094329834, "[TT] Argument of Pericenter of the SMART-1 = 292.930\u00ba"]
-[5.656227111816406, 4.501944065093994, "[FF] Application of the 5G Protocol = Internet of Things (IoT) connectivity"]
-[5.822300434112549, 2.8867080211639404, "[FF] Funding Raised of the Xona = About $10 million"]
-[4.409531593322754, 2.0798420906066895, "[TT] Launch Date of the KhalifaSat = 29 October 2018"]
-[3.3084590435028076, 3.7751965522766113, "[FF] Presentation of the TerraSAR-X, TanDEM-X, EnMAP = GSCB (Ground Segment Coordination Body) Workshop"]
-[6.641605854034424, 6.841610908508301, "[TT] Design of the SILEX = ESA"]
-[5.00177001953125, 8.265564918518066, "[TT] Bandwidth of the CubeRRT RFE = 1 GHz"]
-[9.679401397705078, 2.3572824001312256, "[FF] Data Loss of the FREESTAR = Varies"]
-[5.004979610443115, -0.33015576004981995, "[TT] Launch Time of the CartoSat-2D = 3:58 UTC"]
-[4.58612060546875, 2.847224712371826, "[TT] Location of the HIRES = W. M. Keck Observatory (Mauna Kea, Hawaii)"]
-[5.30037784576416, 0.8445417881011963, "[FF] Observation Date of the ICON = December 10, 2019"]
-[6.981141567230225, 7.0283660888671875, "[FF] Heat Source of the Laser Diode = Significant"]
-[5.2204084396362305, 4.5665788650512695, "[TT] Number of Receiver Antennas of the Geostationary Relay Satellites = 4"]
-[5.489299774169922, 0.3115670382976532, "[FF] Launch Date of the Atlas Cygnus = Dec. 6, 2015"]
-[10.963481903076172, 0.7645413875579834, "[FF] Habitable Zone of the Red Dwarf Star = Requires planets to orbit extremely close"]
-[8.55054759979248, 8.810235023498535, "[TT] Emission Band of the Herschel = Far-infrared (at 100 \u00b5m)"]
-[5.423398971557617, 1.715563178062439, "[FF] Objective of the ALOS-2 = Provide data continuity to be used for cartography, regional observation, disaster monitoring, and environmental monitoring"]
-[10.920154571533203, 7.570466995239258, "[TT] Swath Width of the WFC = 61 km"]
-[4.286563873291016, 4.817917823791504, "[TT] Minimum Beam Mode Detectable Ship Length (MDSL) of the ScanSAR narrow = 51-190 m"]
-[3.724591016769409, 5.440266132354736, "[TT] Azimuth Resolution of the High Resolution Spotlight = 1.1 m (single pol.)"]
-[7.235844612121582, 2.5917420387268066, "[FF] Documentation Source of the MEVI\u00b5S = \"Observation of the Earth and Its Environment: Survey of Missions and Sensors\" (Springer Verlag)"]
-[6.375678062438965, 5.347130298614502, "[FF] Function of the FPGA = Receives command packets from the DPU and timing and synchronization data from the AEU"]
-[6.6898193359375, 4.448545455932617, "[FF] Backup for Rumpin of the Rancabungur = True"]
-[7.27687931060791, 3.09261417388916, "[FF] Mission Goals of the GOES-R = Maintain continuous, reliable operational environmental, and storm warning systems to protect life and property; Monitor the Earth's surface and space environmental and climate conditions; Introduce improved atmospheric and oceanic observations and data dissemination capabilities; Develop and provide new and improved applications and products for a wide range of federal agencies, state and local governments, and private users"]
-[4.962528228759766, 0.6077471375465393, "[FF] Delivery Date of the WINCS = Fall"]
-[4.207775592803955, 2.3657264709472656, "[TT] Launch Vehicle of the BRITE/CanX-3 nanosatellites = Dnepr-1"]
-[5.686903476715088, -0.9206188321113586, "[TT] Design Life of the S/C = 3 years"]
-[11.03526496887207, 0.5634464025497437, "[TT] Number of Monitored Stars of the Kepler Space Telescope = More than 150,000"]
-[10.357754707336426, 2.8318111896514893, "[TT] Launch Date of the CADRE nanosatellite = December 6, 2015"]
-[9.142200469970703, 5.181562900543213, "[FF] Purpose of the VISS = Steering about any or all of the three rotational axes"]
-[6.001041889190674, 6.334493637084961, "[TT] Latency Requirements of the ISLs = Not compromised"]
-[3.816617965698242, 1.405072808265686, "[TT] First Stage Engine of the Falcon 9 = Merlin"]
-[12.12286376953125, 4.455067157745361, "[TT] Dimensions of the NOAA POES series fifth generation satellites = 4.18 m length, 1.88 m diameter, 7.4 m with solar paddles"]
-[10.529569625854492, 3.158909320831299, "[FF] Attitude Stability of the Nanosatellite = Arc-Minute"]
-[10.74894905090332, 0.9201827049255371, "[TT] Classification of the HAT-P-7 = Hot Jupiter"]
-[5.980273246765137, 2.393104076385498, "[FF] Expected Orbit Date of the Legion Constellation = 2022"]
-[5.66094970703125, 2.969407558441162, "[FF] Consortium of the ASPIICS = European Institutes and Industries from Belgium, Czech Republic, France, Germany, Greece, Italy, Luxembourg, Russia, and the UK"]
-[4.455595970153809, 7.840936183929443, "[TT] Uplink Frequency of the DCS = 401.55 MHz"]
-[7.711667060852051, -0.8346070051193237, "[TT] Data Collection Start Date of the ICESat-2 = Early 2019"]
-[4.118085861206055, 4.094449520111084, "[FF] Emergency Message Collection of the LEOSAR = Yes"]
-[13.241876602172852, 7.209173679351807, "[TT] Power Consumption of the FPU = 85 W"]
-[8.812987327575684, 2.6220552921295166, "[FF] Objective of the SOAR = Investigate the interaction between different materials and the atmospheric flow regime in very low Earth orbits (VLEO)"]
-[8.301567077636719, 2.2321932315826416, "[FF] Cloud Penetration of the Lasers = Cannot penetrate thick clouds"]
-[5.508462429046631, -0.6098856329917908, "[TT] Mode of the Yutu-2 = \"Napping\" mode"]
-[9.823057174682617, 2.6876132488250732, "[FF] Update of the NanoCom ADS-B = More resilient to single-event upsets"]
-[13.433231353759766, 2.9339632987976074, "[TT] Mass (kg) of the RISAT-1 = 300"]
-[7.468626976013184, 8.773896217346191, "[TT] Band 6 of the MSS Instrument = 0.7 - 0.8 \u00b5m"]
-[6.4412736892700195, 6.118433952331543, "[TT] Position of the SASI-600 = Right-hand port"]
-[13.740874290466309, 3.114274740219116, "[TT] Mass of the Total Payload = < 100 kg"]
-[5.374600410461426, 7.2561726570129395, "[TT] Bit Rate of the Receiving Signal Bit Rate = 400bit/s"]
-[6.946781158447266, 2.2976958751678467, "[FF] Publication Date of the Experimental Satellite System for Earth Monitoring = 1981"]
-[5.208723545074463, 7.0088114738464355, "[TT] Bent-pipe Mode Up to of the Communication Modes = 1.2 Gbit/s"]
-[7.609059810638428, 6.749693393707275, "[TT] Video Capture Time of the Carbonite-2 = Up to two minutes"]
-[5.829370498657227, -0.7593192458152771, "[TT] Lifetime of the Satellite = 7 years"]
-[8.7853422164917, 3.595292568206787, "[FF] Leading Noise Terms of the Satellite = Thermal effects"]
-[8.641031265258789, 7.010899543762207, "[TT] Field of Regard of the WV60 imager = 900 km"]
-[10.146655082702637, 8.152366638183594, "[TT] Aperture Diameter of the Optics = 80 cm"]
-[13.44738483428955, 6.706253528594971, "[TT] Average Consumption per Burn of the Spacecraft = 0.011 kg"]
-[9.958060264587402, 6.519028186798096, "[TT] ILP of the Instrument = 0.5 cm -1"]
-[5.4603495597839355, 0.43758195638656616, "[TT] Mission Start Date of the Triana = October 2, 2000"]
-[10.346142768859863, 2.3709053993225098, "[FF] Spectroscopy of the RHESSI = Up to \u03b3-ray energies of about 17 MeV"]
-[8.784029960632324, 7.475819110870361, "[TT] Radiometric Resolution of the Raw Video Product = 11 bit"]
-[6.501007080078125, 3.554150104522705, "[FF] Primary Objectives of the Refabricator = Demonstrate repeatable, closed-loop recycling plastic materials for additive manufacturing in the microgravity environment of the ISS a minimum of seven times"]
-[10.937835693359375, 6.38759183883667, "[TT] Primary Mirror Material of the NAOMI = SiC"]
-[3.212012529373169, 4.982081413269043, "[TT] Spatial Resolution of the SAR Sensor Subsystem = 3 m x 3 m"]
-[5.542247772216797, 0.8541646599769592, "[FF] Publication Date of the Kris Fury = April/May 2012"]
-[3.8761606216430664, -2.168732166290283, "[FF] Purpose of the Specialized Asset Tracking = Gather lots of data for a specific asset"]
-[14.203474044799805, 3.21053147315979, "[TT] Total Mass of the X50L = 150 kg"]
-[7.141175746917725, 6.636529922485352, "[TT] Integration Time of the GLM = 2 ms"]
-[6.34766960144043, 3.287299633026123, "[FF] Data Collection of the BlackSky Constellation = Commercially available"]
-[7.628629207611084, -0.08638115972280502, "[TT] Initial Touchdown Point of the Philae lander = Agilkia"]
-[8.319405555725098, 7.994311332702637, "[TT] Wire Bond Pitch of the SWIR Detector = 50 \u00b5m"]
-[12.435603141784668, 0.5504694581031799, "[TT] Long-Term Pointing Stability of the PLATO = 3.85 days"]
-[6.965193748474121, 0.0031948634423315525, "[TT] Age of the AU Mic = 20 million to 30 million years"]
-[5.96012020111084, -0.4694175124168396, "[TT] Mission Duration of the NuSTAR = 10 years"]
-[5.351842403411865, 6.808556079864502, "[TT] Data Rate of the Spacecraft = 100 Mbit/s"]
-[13.562543869018555, 7.151560306549072, "[TT] Efficiency of the DC-DC converter = Greater than 85% across load range of 75% to 100%"]
-[7.603976249694824, 8.679254531860352, "[TT] OLI Bands of the Landsat-8 = 7-5-2"]
-[5.314136505126953, 5.2895283699035645, "[FF] Prime Objective of the STRV-1a and -1b = Provide opportunities for the evaluation of several new technologies in-orbit"]
-[5.01710319519043, 3.1174707412719727, "[FF] Image Credit of the NAOMI = EADS Astrium SAS"]
-[8.52490520477295, 1.8521811962127686, "[TT] Absolute accuracy of the Cloud amount = \u00b120%"]
-[6.274051666259766, 5.652990341186523, "[TT] Former Name of the GIOVE-A = GSTB-V2/A"]
-[4.878655910491943, 2.1988000869750977, "[FF] Website of the TUBSAT = http://www.raumfahrttechnik.tu-berlin.de/tubsat"]
-[3.9367847442626953, 4.210114479064941, "[FF] Test Plan Presenters of the RADARSAT-2 GMTI Capabilities = P. D. Beaulne, C. E. Livingstone"]
-[9.152196884155273, -1.2550150156021118, "[TT] Orbit Type of the GOES-18 = Geostationary"]
-[7.5690460205078125, -0.9100266695022583, "[TT] Design Life of the ICESat-2 = 3 years"]
-[14.265199661254883, 3.171950578689575, "[TT] Mass of the YES-2 = 36 kg"]
-[5.288808822631836, 6.62899112701416, "[FF] Data Transport Standards of the SPA = USB 1.1 limited to 12 Mbit/s, SpaceWire 400~600 Mbit/s"]
-[7.7210774421691895, 0.70453941822052, "[FF] Wavelengths of the Lunar Flashlight = ~1.495 \u00b5m, ~1.990 \u00b5m, ~1.064 \u00b5m, ~1.850 \u00b5m"]
-[7.766978740692139, 2.0520122051239014, "[TT] Primary Use of the Band 7 = Ocean color"]
-[13.393471717834473, 7.331921100616455, "[TT] Power of the TRSR = 7-15 W"]
-[14.046878814697266, 7.193140983581543, "[TT] Unregulated Bus Voltage of the Power Subsystem = 14 V"]
-[6.950761795043945, 2.394272804260254, "[FF] Presentation Date of the Remote Sensing Activities = Feb. 6-17, 2012"]
-[4.8079962730407715, 7.107633590698242, "[TT] Downlink Data Rate of the Frontier Radio = Up to 2 Mbit/s"]
-[9.397581100463867, 6.986945152282715, "[TT] Spatial Resolution of the MSU-MR Scanning Radiometer = 1 km"]
-[8.994994163513184, 5.8180718421936035, "[TT] Angular Accuracy Requirement of the Optical System = 5 arcsec"]
-[4.891358852386475, 3.0104963779449463, "[TT] Prime Contractor of the QZS-1 = MELCO (Mitsubishi Electric Corporation) Kamakura Works, Kamakura-City, Japan"]
-[6.132220268249512, 1.3757398128509521, "[FF] Meeting Date of the Swarm = June 24-26, 2009"]
-[5.701713562011719, 5.547830104827881, "[TT] Function of the OBC = RF communication subsystems"]
-[9.493925094604492, 4.218111991882324, "[FF] Angle of the Solar Panel = Optimization"]
-[13.772543907165527, 2.8718647956848145, "[TT] Mass of the Spacecraft = 495 kg"]
-[8.706552505493164, 5.012916564941406, "[TT] Object Detection Threshold of the Star Tracker = Visual (or apparent) magnitude Mv 11"]
-[4.476879596710205, 7.087428569793701, "[TT] NRT Data Downlink Frequency of the Sentinel-6 = X-band contact"]
-[7.6424880027771, 8.938891410827637, "[TT] Spectral Bands of the MISR = 0.45, 0.56, 0.67 and 0.87 \u00b5m"]
-[9.173072814941406, 3.1654157638549805, "[FF] Determines of the A/M Distribution = Solar radiation pressure and atmospheric drag perturbations on the fragments"]
-[8.775222778320312, 1.937760353088379, "[TT] Link Speed of the WINDS = 1.2 Gbit/s"]
-[10.135644912719727, 7.558383941650391, "[TT] Image Swath-Width of the ISIR = 85 km"]
-[9.80502700805664, 7.151846408843994, "[TT] Along-track resolution of the S-band = 20 km"]
-[11.405141830444336, 4.350033283233643, "[TT] Size of the Dove-3 = 3U"]
-[5.832169055938721, 8.009468078613281, "[FF] Spin Frequency of the MicroSCOPE = Twice the Orbital Frequency"]
-[11.98818302154541, 4.985339641571045, "[TT] Volume of the MiniCOR = ~2U"]
-[3.3869714736938477, 5.1939802169799805, "[TT] Required Radiometric Accuracy of the SAR System = 1 dB (3\u03c3)"]
-[10.166459083557129, 5.806154727935791, "[TT] IR Detector Temperature of the OCTS sensor = 100 K"]
-[11.18873119354248, 1.0442438125610352, "[FF] Image Credit of the LISA = AEI/MM/exozet; GW simulation: NASA/C. Henze"]
-[8.098116874694824, 8.94151782989502, "[TT] Wavelength Range of the BIRCHES = 1 to 4 \u00b5m"]
-[5.072690486907959, 1.74559485912323, "[TT] Deployment Date of the TacSat-4 = October 8, 2011"]
-[5.109609127044678, 0.2459285706281662, "[TT] Deployment Date of the LDEF = April 7, 1984"]
-[7.174264430999756, 6.55850076675415, "[TT] Signal Threshold of the GMOD = 10 sigma"]
-[4.864910125732422, 7.337997913360596, "[TT] Data Transmission Rate of the L-band data transmission = 665.4 kbit/s"]
-[8.746183395385742, 3.9566423892974854, "[FF] Operation of the SUVI = Solar-pointing"]
-[8.70797061920166, 4.7557053565979, "[TT] Observation Mode of the TanSat = Sun-glint observation mode"]
-[7.2464919090271, 7.013878345489502, "[TT] Non-operating Survival Temperature of the Laser = 0 \u2013 50\u00baC"]
-[1.9464954137802124, -0.3943534195423126, "[FF] Orbit of the Van Allen Probes = Stable, circular orbit around Earth"]
-[7.1836838722229, 7.405198097229004, "[TT] Signal Photon Density of the MABEL = 3.9 photons per 70 cm"]
-[9.736740112304688, 4.227975845336914, "[FF] ADCS System of the DeorbitSail = First demonstration of this Cubesat-specific ADCS"]
-[6.294693946838379, 7.127142429351807, "[TT] Projected Counting Rate of the Instrument = 0.5 counts/pixel/exp/R"]
-[8.185876846313477, 1.150695562362671, "[TT] Soil Moisture Measurement Period of the RISAT-1 = April to October"]
-[14.18298053741455, 3.1456499099731445, "[TT] Mass of the RemoveDebris = 100 kg"]
-[4.784971237182617, -1.8376846313476562, "[TT] Sample Collection Time of the Chang'e-5 Lander = 20 hours"]
-[10.319707870483398, 5.698451995849609, "[TT] Temperature Stability of the Filter Wheel Casing = \u00b11 K"]
-[5.831974983215332, -0.7364434599876404, "[TT] Life Expectancy of the Almaz-1B = 5 years"]
-[3.5544896125793457, 5.070085048675537, "[TT] Swath Width of the C-RADAR = 225 km"]
-[4.9393510818481445, 0.7735458016395569, "[TT] Availability of the European Aviation Network = 18 July 2019"]
-[9.411266326904297, 3.8338589668273926, "[FF] Function of the ISIS = Provide access to the nominal direction of the Parker Spiral magnetic field"]
-[14.121472358703613, 3.154644250869751, "[TT] Mass of the ORA = 16 kg"]
-[7.39995813369751, 1.1948392391204834, "[FF] Journal Publication Date of the OCEANSAT-2 = October, 2007"]
-[5.458607196807861, -1.7375116348266602, "[TT] End of Life Date of the KOMPSAT-3 = 18 May 2022"]
-[7.774209022521973, 3.0620718002319336, "[TT] Concentration Measurement Precision of the GOSAT = 4 ppm (CO2), 34 ppb (CH4)"]
-[3.9002768993377686, 4.294942855834961, "[FF] Purpose of the Radar Payload = Understand climate change and support sustainable ecological transition"]
-[9.12777042388916, 1.429334044456482, "[TT] Current Location of the Voyager 1 = Interstellar space"]
-[10.848625183105469, 7.472559928894043, "[TT] Swath Width of the Visible Band = 1500 km"]
-[6.734899520874023, 6.512391090393066, "[TT] Prime Developer of the Laser Transmitter = Selex Galileo"]
-[12.05170726776123, 4.501917839050293, "[TT] Dimensions of the Autonomous spaceport drone ship = 90 m x 30 m"]
-[12.683795928955078, 1.9239035844802856, "[TT] Type of the SAGE I = Atmospheric chemistry"]
-[7.61276388168335, 1.4992605447769165, "[FF] Operation of the GOES-16 = Captured images of the shadow of the Moon crossing the face of Earth"]
-[11.779232025146484, 3.29223895072937, "[TT] Development Status of the 1 N Thruster = Flight-ready"]
-[12.074888229370117, -0.24258442223072052, "[TT] Northern Sky Study Duration of the TESS = Second year of operations"]
-[5.396185874938965, 0.0892157182097435, "[TT] Operation Start Date of the RAIDS = October 23, 2009"]
-[7.453293323516846, 1.2110741138458252, "[FF] Data Release of the SeaSat = 1977"]
-[5.38858699798584, 5.695400238037109, "[TT] SCI ports of the STRV-1d DHS = Eleven RS-422"]
-[7.007608413696289, 0.7592734694480896, "[TT] Microchip Quantity of the InSight = 2"]
-[7.575826168060303, 3.6566882133483887, "[FF] Grabber of the CleanSpace One = Demonstrate capture"]
-[7.117829322814941, 1.8344378471374512, "[TT] Launch Year of the Carbonite-2 = 2018"]
-[9.065540313720703, 6.164483070373535, "[FF] Mechanism of the IASI-NG = Patented mechanism allows performing simultaneously the OPD scan and the compensation using a single actuator"]
-[9.410103797912598, 8.075355529785156, "[TT] Number of Channels of the Telescope = 15"]
-[8.64058780670166, 1.0824570655822754, "[TT] Launch Date of the Aquarius/SAC-D = 10 June 2011"]
-[11.85855484008789, 4.9010009765625, "[TT] Base Dimensions of the CMS = 380 mm x 315 mm x 186 mm"]
-[9.281728744506836, 5.101059913635254, "[TT] Attitude Subsystem Knowledge of the Spacecraft = 0.1\u00ba (3\u03c3)"]
-[11.940906524658203, 4.557980537414551, "[TT] Deployed Configuration Size of the KaRIN = 5.0 m x 10.6 m x 1.5 m"]
-[4.746679306030273, 0.65804123878479, "[TT] Operational Services Start of the MSG = 2004"]
-[5.4022626876831055, 3.9714183807373047, "[TT] Quantity of the Earth observation satellites = At least six"]
-[7.895637512207031, 7.532811641693115, "[FF] Publication Date of the Hyperspectral sensor HSC3000 = Nov. 2008"]
-[13.212964057922363, 7.255035400390625, "[TT] Power Consumption of the LISS-3 = 70 W"]
-[8.552887916564941, 4.699462413787842, "[TT] Manufacturer of the MST Star Tracker = TU Graz"]
-[8.053683280944824, 3.262920379638672, "[FF] Measurement Category of the Imager = Atmospheric Temperature Fields"]
-[13.288063049316406, 7.383103847503662, "[TT] Power of the MSI = 170 W"]
-[6.682309627532959, -0.6022294759750366, "[TT] On Orbit Duration of the SwissCube = 4 years"]
-[3.2143187522888184, 5.055868148803711, "[FF] Resolution of the PMI = Unfocused SAR"]
-[5.367431163787842, 0.27713674306869507, "[TT] Launch Date of the SRL-1 (STS-59) = April 9, 1994"]
-[10.859609603881836, 7.593053817749023, "[TT] Swath width (km) of the ALT = 2.8"]
-[10.047540664672852, 2.6764986515045166, "[TT] \u03b2 Angle Variation of the NanoRacks-QB50 CubeSats = 0-75\u00ba"]
-[5.884616374969482, 1.365355134010315, "[FF] Presentation Date of the ERG Satellite = Oct. 3-7, 2011"]
-[9.989594459533691, 7.2116379737854, "[TT] Ground Coverage of the Scanner Assembly = 96 km"]
-[5.247316837310791, 0.5029028058052063, "[FF] Deployment Orbit of the OG2-1 = Lower than intended"]
-[9.608890533447266, -0.43600401282310486, "[TT] Perigee Altitude of the IDEA-OSG 1 = 600 km"]
-[8.531195640563965, 1.9421749114990234, "[TT] Absolute Accuracy of the Ocean surface wind speed = \u00b1 2 m/s"]
-[7.860748767852783, 1.3605560064315796, "[FF] Mission of the IMI = Water Cycle Observation"]
-[10.728802680969238, 1.170274019241333, "[TT] Mass of the HD 21749b = 23 times as massive as the Earth"]
-[7.577414512634277, 7.33975076675415, "[TT] Maximum Imaging Range of the CHORUS = \u00b162.5\u00b0"]
-[5.395959854125977, 6.552830696105957, "[TT] Microcontroller Speed of the CDHS = 16 MIPS when run at 32 MHz"]
-[5.86993408203125, 4.8919854164123535, "[TT] Data Recording of the Development Flight Instrumentation (DFI) = Redundantly recorded all data as planned"]
-[10.91879940032959, 0.8726868033409119, "[TT] Formation of the LISA = Three spacecraft flying in a triangular formation with 2.5-million kilometre-long sides"]
-[6.066338062286377, 2.244354009628296, "[FF] URL of the SSMI = http://nsidc.org/data/docs/daac/ssmi_instrument.gd.html"]
-[5.065673351287842, -0.16452673077583313, "[TT] Launch Time of the Aeolus = 21:20 GMT"]
-[3.965505838394165, 3.5100696086883545, "[TT] Operational Since of the Galileo = December 2016"]
-[11.78395938873291, 6.7416768074035645, "[FF] Energy Range of the MERiT = Below 30 keV"]
-[4.966684341430664, 0.4930974543094635, "[TT] Launch Date of the VRSS-1 = Sept. 28, 2012"]
-[5.2540669441223145, 6.917795181274414, "[TT] Downlink Capacity of the Bartolomeo = Up to 1 GB per day"]
-[8.07998275756836, -1.2227027416229248, "[FF] Laser Altimeter of the ICESat-2 = Records the length of time it takes to make that round trip"]
-[6.855765342712402, -0.42120206356048584, "[TT] Orbital Period of the ASTERIA = 92.6 minutes"]
-[7.946412086486816, 0.40470170974731445, "[TT] Glacier and Ice Cap Surface Velocity Revisit Time of the ROSE-L = Six days"]
-[10.446441650390625, 2.287295341491699, "[FF] Image Blur Metrics of the X-ray telescopes = FWHM (Full Width Half maximum), RMS (Root-Mean-of Squares)"]
-[5.562597274780273, 2.2337982654571533, "[FF] Affiliation of the Toshinori Kuwahara = Unknown"]
-[13.827753067016602, 3.0907044410705566, "[TT] Payload Mass of the Spacecraft = 35 kg"]
-[11.433835983276367, 0.7721900343894958, "[TT] Mass of the AU Mic b = Less than 58 times Earth's mass"]
-[11.504461288452148, 3.4207236766815186, "[FF] Conference Presentation Date of the Micro-Cathode Arc Thruster = 5-12 March 2016"]
-[3.832026243209839, 3.4169554710388184, "[TT] Service Restoration Date of the Galileo = July 22, 2019"]
-[4.409280300140381, 5.440359592437744, "[TT] Technology Demonstration Phase Duration of the GomX-4B = 6 months"]
-[5.355456829071045, 7.098815441131592, "[TT] Baud Rates of the High-speed link = 600 - 19200 baud"]
-[9.573393821716309, 8.117388725280762, "[TT] Hydrogen Cell of the Instrument = Pyrex vessel (MgF 2  lens windows-distance 76 mm)"]
-[5.370476722717285, 5.611754894256592, "[TT] Interface of the STRV-1d spacecraft = RS-422"]
-[8.99718189239502, 0.5142176747322083, "[TT] Maximum Displacement of the Disturbed Areas = 10 cm"]
-[9.76725959777832, -0.4224684536457062, "[TT] TGF Altitude of the RHESSI = Around 15 km"]
-[9.452812194824219, 6.131144046783447, "[TT] 8\u00ba to 70\u00ba of the Incidence angle = -"]
-[4.844827651977539, 0.6906381249427795, "[FF] Availability Date of the FM (Flight Model) = 2009"]
-[11.594688415527344, 4.82637882232666, "[TT] Cylinder Diameter of the ACC = 1.1 m"]
-[11.425407409667969, 4.357316970825195, "[TT] Size of the Triton-1 = 3U"]
-[6.180788516998291, 6.919931411743164, "[FF] Data Rate of the Space to Ground Bidirectional Optical Communication Link = 5.6 Gbit/s"]
-[5.733236312866211, 2.559968948364258, "[TT] Test Modes of the MPO spacecraft = Launch mode operations and science operation"]
-[10.878679275512695, -0.31098833680152893, "[TT] Number of Tiles of the TanDEM-X = More than 19,000"]
-[9.044285774230957, 6.479252815246582, "[TT] Data Acquisition of the MMS = Simultaneously at multiple points in space"]
-[6.908099174499512, 4.873918056488037, "[FF] Flight Hard Drive Data Recovery of the CVX-2 = Successful"]
-[5.487725734710693, 2.4428353309631348, "[TT] Mission Name of the \u00d8rsted = \u00d8rsted"]
-[5.626173973083496, 2.2300612926483154, "[FF] Status of the YOUTHSAT = Functioning Satisfactorily"]
-[8.000434875488281, -0.5450132489204407, "[FF] Location of the Land Glacier = West Antarctica"]
-[4.758455753326416, 4.937166213989258, "[TT] Sensor of the ESAIL = AIS (Automatic Identification System)"]
-[4.821025848388672, 0.18650996685028076, "[TT] Target Launch Date of the Crew-5 = Fall of '22"]
-[9.227910995483398, 1.3402636051177979, "[FF] Data Transmission of the New Horizons = Ongoing"]
-[9.488598823547363, -1.0711005926132202, "[TT] Orbital Location of the GOES-T = 137\u00ba west"]
-[5.381532669067383, 3.092299699783325, "[TT] Developer of the CZI = Beijing Institute of Space Machines and Electricity"]
-[14.015412330627441, 2.743029832839966, "[TT] Launch Mass of the WNISAT-1 = 10 kg"]
-[4.930188179016113, 1.4623125791549683, "[TT] End of Life Date of the Tatiana-2 = 16 January 2010"]
-[4.002893924713135, 2.1800575256347656, "[TT] Launch Vehicle of the Starliner = United Launch Alliance Atlas 5 rocket"]
-[5.523349761962891, 5.838253021240234, "[TT] CPU of the On-board computers = 80C186, 16 MHz"]
-[10.190043449401855, 1.5326918363571167, "[TT] Number of Clusters of Galaxies Detected of the eROSITA = More than 100,000"]
-[11.34673023223877, 5.860680103302002, "[TT] Structure Material of the SRMSat = Al-6061 alloy"]
-[6.788825511932373, 6.058016300201416, "[TT] Operation Mode of the DOTs = Continuous when they detect some requests or when they need to transmit their data"]
-[5.765071392059326, 3.4357504844665527, "[TT] # satellites to collect 106 sqkm/day @ 50 cm GSD of the Legion = 1"]
-[6.892090320587158, -0.6164475083351135, "[TT] Period of Orbit of the ICIR = Approximately 1.55 hours"]
-[6.50966215133667, 2.0918920040130615, "[FF] URL of the Microsat = https://web.archive.org/web/20180125015338/https://www.isro.gov.in/Spacecraft/microsat-0"]
-[9.195914268493652, 7.4290242195129395, "[TT] Spatial Resolution of the MP-900M TV Camera = 1.6 km x 1.8 km"]
-[4.790952682495117, 0.4507526159286499, "[TT] Launch Date of the Stingray = Early 2024"]
-[6.315654277801514, 7.228143692016602, "[FF] Error Reduction of the DS-BAQ = Better than BAQ"]
-[14.741830825805664, 6.615127086639404, "[TT] Total Capacity of the Li-ion batteries = 102 Ah @ EOL"]
-[13.83448314666748, 2.749288320541382, "[TT] Launch Mass of the Genesis spacecraft = 636 kg"]
-[9.165090560913086, -0.3882095515727997, "[FF] Apogee Alignment of the MMS and THEMIS = 180\u00ba apart"]
-[5.905980587005615, 1.0335614681243896, "[FF] Date of the SOLSE/LORE-2 Experiment = April 25, 2006"]
-[8.367732048034668, 0.835322380065918, "[FF] Additional Observation of the DCAM3-D = Low-speed ejecta (dust) spreading will possibly be observed around the DCAM3 in a few hours after the impact"]
-[6.0839972496032715, -0.4906659722328186, "[TT] Flight Duration of the Spacecraft = About two months"]
-[8.927165031433105, 4.499334335327148, "[FF] Purpose of the OB = Transference of the attitude from the star trackers to the magnetometer field components"]
-[13.771468162536621, 2.712040901184082, "[TT] Launch Mass of the Helios-2 satellites = Approximately 4200 kg"]
-[4.876136779785156, 0.16713592410087585, "[TT] Launch Date of the STPSat-3 iMESA = Nov. 2013"]
-[10.269068717956543, 5.320390224456787, "[FF] Maximum Admissible Heat Load of the RVX = Unknown"]
-[6.071153163909912, -0.42219769954681396, "[TT] Operation Duration of the SPOT-VEGETATION = 16 years"]
-[11.989130020141602, 5.0684590339660645, "[TT] Size of the FREND = 465 x 380 x 370 mm"]
-[7.241735935211182, 3.9472713470458984, "[FF] Maneuvers of the OMOTENASHI = Two deterministic maneuvers"]
-[8.788463592529297, 4.612943172454834, "[FF] Pointing Restrictions of the CHIPSat = Sun, Earth, moon and in the orbital RAM direction"]
-[13.349929809570312, 7.666732311248779, "[TT] Signal Power of the ITUs = 5 W (+37 dBm)"]
-[4.757294178009033, 7.985254287719727, "[FF] Function of the Chirp generator = Generate the high-power radar transmit signal"]
-[8.657970428466797, 6.125784397125244, "[TT] Accuracy of the SubWave = 10m"]
-[14.076862335205078, 4.030991554260254, "[TT] Electronic Unit Mass of the Instrument = 2.82 kg"]
-[8.129911422729492, 1.8265657424926758, "[TT] Spacecraft Body Shape of the GOCE = Aerodynamic"]
-[10.033750534057617, 3.006446599960327, "[FF] Conference Presentation Date of the Dynamic Ionosphere Cubesat Experiment (DICE) = Aug. 9-12, 2010"]
-[6.19954252243042, 0.2893642783164978, "[TT] Communication Pass Duration of the ASTERIA = 8 to 10 minutes"]
-[7.70722770690918, 6.52921199798584, "[TT] Mosaic Image Tile Time of the EUI = About 10 minutes"]
-[5.075295925140381, 3.510063648223877, "[TT] Manufacturer of the SGR-ReSI = SSTL"]
-[5.07537841796875, 7.087111949920654, "[TT] Data Rate (Uplink) of the S-band telemetry system = 256 kbit/s"]
-[2.898651361465454, 4.382430076599121, "[TT] Calibration Time of the PALSAR-2 = 3 and a half months"]
-[6.412620544433594, 4.698352813720703, "[FF] Function of the ISSAC SOC = Receive ISSAC imagery requests"]
-[6.258526802062988, 3.376065492630005, "[FF] Mission Phase of the PROBA-V = Operational"]
-[8.23349380493164, 3.963771104812622, "[FF] Function of the ASME = Measures the surface degradation of a material sample exposed to the space environment"]
-[9.62129020690918, 1.4116806983947754, "[TT] Launch Year of the Pl\u00e9iades Neo constellation = 2020"]
-[3.455341100692749, -0.8376333117485046, "[TT] Orbit of the GF-3 Satellite = Sun-synchronous orbit"]
-[4.438153266906738, 1.851711392402649, "[FF] Conference Date of the RADARSAT-2 = June 4-7, 2018"]
-[6.074043273925781, 2.199645519256592, "[FF] Test Flight of the Orion MPCV = Uncrewed"]
-[3.2270970344543457, 5.000339508056641, "[TT] Line-of-Sight Deformation Rate Maps Generation Period of the SAR = One year"]
-[3.4720005989074707, 5.192429542541504, "[FF] Designers of the CSG SAR waveform generator and echo digitizer = Francesco Spadoni, Antonio Delfino, Francesco Richichi, Roberto Capezzali, Isaia Martinazzo, Francesco Quaranta, Mario Frezzini"]
-[5.568063259124756, 7.606446743011475, "[TT] Sampling Speed of the RFA = Highest"]
-[3.5388500690460205, 4.741983890533447, "[FF] Operation of the RISAT-1 SAR payload = Ground-based"]
-[4.876933574676514, 7.160894870758057, "[TT] Downlink Data Rate of the TT&C S-band Link = 2 Mbit/s"]
-[3.1405887603759766, 2.3721253871917725, "[FF] Straylight Measurement of the Sentinel-5 = Laser and filter measurements"]
-[6.526768207550049, -1.2677088975906372, "[FF] Data Consistency of the GRACE-FO = Consistent with GRACE data"]
-[11.753880500793457, 3.340339422225952, "[FF] Impulse Density of the Thruster = High"]
-[6.04782772064209, 5.500695705413818, "[TT] Redundancy of the Magnetometer = Cold redundancy"]
-[4.629153728485107, 7.255367755889893, "[FF] Communication of the ACS = RF communications TM: 4.5 W RF, 40 kbit/s TM at 387.1 MHz; TC at 400 MHz. S-band TM-TC at 2.043 & 2.223 GHz 40-175 kbit/s"]
-[9.59054946899414, 4.069746494293213, "[TT] Type of the Magnetometer (NOAA) = Magnetic field"]
-[8.14656925201416, 7.172964096069336, "[TT] Imaging Type of the R3 spacecraft = Multispectral"]
-[9.933053016662598, -1.4656243324279785, "[TT] Orbit Inclination of the ISS = 51.6\u00ba"]
-[10.29376220703125, 1.7651785612106323, "[FF] 3D Visualization of the Exploded Star = Built with Help from NASA's Great Observatories"]
-[7.880730628967285, 8.298431396484375, "[FF] Spectral Bands of the Sensor = Not specified"]
-[6.337782382965088, 4.731632232666016, "[FF] Function of the UIS = User Interface"]
-[6.603355884552002, 4.77039098739624, "[FF] Unknown of the FlexRX Receiver = Unknown"]
-[6.449020862579346, -0.6663995385169983, "[TT] Reconnection Duration of the In-situ spacecraft = Hours"]
-[7.18232536315918, 7.358127593994141, "[FF] Photon Types of the MABEL = Signal photons, noise photons"]
-[5.062337398529053, 0.5460272431373596, "[FF] Shipment Date of the TSIS = 4 Aug. 2017"]
-[4.822781085968018, 8.557511329650879, "[TT] Center Frequency of the Channel 7 = 48 GHz"]
-[3.1210203170776367, 2.2018661499023438, "[FF] Land-surface Temperature Imaging of the Copernicus Sentinel-3 = Data"]
-[5.762909412384033, 0.9240562319755554, "[TT] Imaging Date of the KMSS = Jan. 13, 2015"]
-[10.539878845214844, 2.8637053966522217, "[FF] Mission Objective of the Small or Nanosatellite = Reach the surface of Mars and other planetary bodies"]
-[6.273800373077393, 5.579518795013428, "[FF] Memory Module of the MMFU = SMM (SDR-SDRAM memory module)"]
-[6.996822357177734, 7.101329803466797, "[TT] Laser Diode Stacks Output Power of the Power Laser Head (PLH) = About 700 W"]
-[4.591436862945557, 2.690685987472534, "[TT] CEO of the Iridium = Matt Desch"]
-[5.774514198303223, 2.752930164337158, "[TT] Cooperative Research and Development Agreement Partner of the SpaceX = U.S. Space Force"]
-[5.797232151031494, 3.3914411067962646, "[TT] Revenue Projection of the Satellogic = $7 million in 2021 to $787 million in 2025"]
-[5.615738868713379, 6.752623558044434, "[TT] Data Throughput of the AIS Data Collection System = 30 MB per day"]
-[3.812847852706909, 6.257360935211182, "[TT] Number of Linear Arrays of the Radiating Board = 8"]
-[10.53195571899414, 2.2522549629211426, "[FF] X-Ray Jet of the M87 = Superluminal Motion"]
-[4.665459632873535, 7.205671787261963, "[TT] Data Transmission Rate of the X-band = 5 Mbit/s"]
-[7.925191879272461, 7.033156871795654, "[TT] Type of the PH-U = Photometer"]
-[8.856611251831055, 3.129671812057495, "[FF] In-situ Measurements of the ICON = Provide the ability to explain how energy and momentum from the lower atmosphere propagate into the space environment"]
-[11.126663208007812, 3.6623928546905518, "[FF] Operation of the E-Sail = Repelled charged plasmas found in space"]
-[4.586212635040283, 7.51605224609375, "[TT] Data Rate of the VHF-band communications = 9.6 kbit/s"]
-[11.692337036132812, 6.596760272979736, "[TT] Energy Ranges of the Chandra = 0.5 to 2 keV and 2 to 4 keV"]
-[13.237227439880371, 5.236349582672119, "[TT] Size of the Solar Panels = 10 m2"]
-[6.405233383178711, 1.3869044780731201, "[TT] Launch Provider of the COSMO-SkyMed-1 = ULA"]
-[7.829899311065674, 9.067599296569824, "[TT] Wavelength of the Master Oscillator = ~ 1550 nm"]
-[13.611520767211914, 1.8679615259170532, "[TT] Cargo Removal of the Cygnus = More than 2,500 kg"]
-[8.666828155517578, 5.896777153015137, "[TT] Localization Performance of the Spacecraft = 300 m CE90"]
-[3.1646788120269775, 2.2942895889282227, "[FF] Data Usage of the Sentinel-1 = Hydrological variations monitoring"]
-[3.84505558013916, 6.4857378005981445, "[TT] Offset Angle of the Antenna = 52.5\u00ba"]
-[3.7524733543395996, 4.738092422485352, "[TT] Phase-Center Distance of the RADARSAT-2 = 3.75 m"]
-[14.049592971801758, 7.160775661468506, "[TT] Secondary Voltages of the PCM = +28 V, \u00b15 V, \u00b115 V, and \u00b112 V"]
-[2.6126821041107178, 3.33441424369812, "[TT] Quantity of the Flock 4v SuperDoves = 26"]
-[11.937697410583496, 3.381098508834839, "[TT] Propellant Status of the CanX-5 = Very large fraction remaining"]
-[8.13128662109375, 2.8438432216644287, "[FF] Purpose of the OLCI = Provide atmospheric information"]
-[6.60412073135376, -0.5555224418640137, "[TT] Orbit Duration of the LF = Two months"]
-[4.869546413421631, 7.956132411956787, "[TT] Carrier frequency (MHz) of the E5b-I = 1207.14"]
-[3.4691851139068604, 6.418967247009277, "[TT] Antenna Diameter of the Integrated Mobile Stations = 4.6 m"]
-[1.6181808710098267, 3.7612016201019287, "[TT] Sun sensors of the BEESAT-1 = Yes"]
-[13.25224781036377, 7.0792155265808105, "[TT] Power Demand of the CMA/CM = 7.3 kW"]
-[6.147597312927246, 4.73886251449585, "[FF] Service Level Agreement of the DPCC = Continuous payload utilization, up to 200 links per day and communication channel, over the expected lifetime of 15 years, with a targeted service availability of at least 99.6% over 60 days and an order reaction time well below one hour"]
-[13.293862342834473, 6.954070091247559, "[TT] Power Consumption of the SpaceCube 2 = 14 W"]
-[4.943159103393555, 5.12285041809082, "[TT] CCSDS ID of the GSAT-0208 = 268"]
-[4.589056968688965, 3.0378105640411377, "[TT] Location of the MOC = Darmstadt"]
-[7.849914073944092, 6.6293864250183105, "[FF] Image Duration of the VIRR = 62 days"]
-[3.847317695617676, 1.1425889730453491, "[TT] Speed of the Falcon-9 first stage = Around 2 m/s"]
-[6.5997490882873535, 7.715217590332031, "[TT] Data Channels of the Sensor = 24"]
-[6.682438850402832, 3.4941189289093018, "[FF] Network of Direct Readout Stations of the EARS = Around the Atlantic and Arctic Oceans"]
-[7.950863838195801, 8.589384078979492, "[TT] Wavelength Separation Direction of the HyperScout\u00ae = Along track"]
-[8.624935150146484, 5.0324015617370605, "[TT] Star Sensitivity Range of the STOs and STAEs = 4 ~6.5 magnitude"]
-[4.04645299911499, 4.468282699584961, "[FF] Ship Detection of the RADARSAT Constellation Mission = Operational"]
-[10.348823547363281, 6.675932884216309, "[TT] Positional Repeatability of the Mirror = Better than 5arcsec"]
-[9.702489852905273, 7.233694076538086, "[TT] Ground Resolution of the P Mode = 2.29 m~0.98 m"]
-[8.677010536193848, 5.909696102142334, "[TT] Calibration Type of the SSM/I = Absolute"]
-[11.439126968383789, 4.891448974609375, "[TT] Depth of the HXT-S = 223 mm"]
-[10.01810359954834, 4.588138103485107, "[TT] Friction of the SADM = Very low"]
-[9.186627388000488, 2.8877015113830566, "[FF] IRIS of the NASA = Largest Solar Flare"]
-[8.69186782836914, 7.669692516326904, "[TT] Detector Array of the Payload 2 = 640 x 480 pixels"]
-[5.230371475219727, -0.8826715350151062, "[FF] Mission Date of the Kolibri-2000 = April 4-8, 2005"]
-[4.720454216003418, -0.03689443692564964, "[TT] End of Life Date of the FedSat = 14 Dec 2005"]
-[4.5229811668396, 4.190218925476074, "[TT] Number of Operational Satellites of the LEOSAR spacecraft = 5"]
-[14.20351505279541, 3.2461156845092773, "[TT] Mass of the FSS = 87.5 g"]
-[10.45907974243164, 7.3361496925354, "[TT] NETD of the MWIR = < 0.5 K @ 400 K scene"]
-[8.704533576965332, 2.01004695892334, "[TT] Wind Speed Measurement Range of the SeaWinds = 3-20 m/s"]
-[13.374410629272461, 2.9131929874420166, "[TT] Mass of the SkySat-2 = 83 kg"]
-[8.754921913146973, 0.13634565472602844, "[TT] Altitude of Checkpoint Rehearsal of the OSIRIS-REx = 246 feet (75 meters)"]
-[11.07818603515625, 2.972386360168457, "[TT] Dimensions of the NanoRacks Kaber Microsat Deployer = 40 cm x 42 cm x 31 cm"]
-[9.070056915283203, 8.526945114135742, "[TT] Wavelength Range of the Lens = 600 - 1000 nm"]
-[7.466727256774902, 2.1976420879364014, "[TT] Measurement Category of the Biomass = Vegetation"]
-[14.660682678222656, 6.671109676361084, "[TT] Capacity of the NiCd Batteries = 18 Ah"]
-[14.105877876281738, 3.2016897201538086, "[TT] Mass of the EPS = 0.28 kg"]
-[8.056099891662598, 8.04692554473877, "[FF] Quantity of the ILAS-II = 3 IR spectrometers, 1 VIS spectrometer"]
-[3.2057509422302246, 5.0882649421691895, "[FF] Image Resolution of the SAR = Not specified"]
-[11.355433464050293, 5.792774677276611, "[TT] Nozzle Material of the Propulsion System = Aluminum"]
-[6.331709861755371, 8.01534652709961, "[TT] Number of Parallel Readout Channels of the CAMEX chip = 128"]
-[10.263026237487793, 5.763012886047363, "[TT] Operating Temperature of the Near-infrared instruments = About 30 K"]
-[4.789401054382324, -1.7837738990783691, "[FF] Terrain Camera (TCAM) of the Chang\u2019e-4 Lander = Payload"]
-[9.146257400512695, 1.2649821043014526, "[TT] Estimated End of the Oort Cloud = About 100,000 AU"]
-[3.43143630027771, 4.847933292388916, "[FF] Objective of the Sentinel-1 = Assure C-band SAR data continuity for the user community currently provided by Envisat and ERS-2"]
-[5.508689880371094, 6.134583950042725, "[TT] Data Storage of the ASAP-Light = Non-volatile memory"]
-[6.415221691131592, 4.398592472076416, "[FF] Data Products of the DPE = RDRs (Raw Data Records), Sensor Data Records, EDRs (Environmental Data Products), TDRs (Temperature Data Records)"]
-[10.564501762390137, 2.8938889503479004, "[FF] Mission Objective of the FASTRAC = Demonstrate two-way intersatellite crosslink with verified data exchange"]
-[3.4982872009277344, -0.9511741399765015, "[TT] Orbit Type of the Yubileyniy-2/MiR = Near-circular orbit"]
-[10.463008880615234, 3.956050157546997, "[FF] Formation of the Shocks = When a supersonic \u2013 faster-than-sound \u2013 flow encounters an obstacle"]
-[7.033246994018555, 2.8446850776672363, "[FF] Observation System of the SEOSAT/Ingenio = Combined radar and optical images"]
-[9.828958511352539, -0.3392459452152252, "[TT] Altitude of the Computer System = 120,000 feet"]
-[8.441207885742188, 1.785044550895691, "[FF] Sea-Surface Temperature Accuracy of the VIRR = \u00b1 1.5\u00baC"]
-[7.971507549285889, 7.983960151672363, "[FF] Noise of the NISP IR Detector = CDS readout noise shows the same performances demonstrated during the NRE phase"]
-[6.117107391357422, -0.5402055382728577, "[TT] On-Orbit Duration of the ACE Mission = 18 years"]
-[7.358941078186035, 0.22379070520401, "[TT] Departure Date from Bennu of the OSIRIS-REx = 2021"]
-[14.24478816986084, 2.978501319885254, "[TT] Mass of the Global-1 = 44 kg"]
-[6.880641937255859, 2.991394281387329, "[TT] Mission Type of the Global GHG Monitoring Constellation = EO"]
-[1.7513694763183594, -2.071488618850708, "[FF] Conference Date of the Hayabusa-2 = June 18-20, 2013"]
-[5.719315528869629, 3.1114630699157715, "[TT] Ownership Acquisition Cost of the Vricon = $140 million"]
-[11.196391105651855, 5.346045017242432, "[FF] Spectrometer Components of the Natalya-2M = Two spectrometers, eight scintillation modules with CsI(Tl) crystals each, anti-coincident protection detectors from polystyrene"]
-[8.188365936279297, 8.201630592346191, "[FF] Technology of the VNIR Range = Photodiode-silicon readout"]
-[7.951327800750732, -2.5690109729766846, "[FF] Imaging Wavelength of the GOLD = Ultraviolet light"]
-[7.485055446624756, 8.788308143615723, "[TT] Band 1 of the Instrument = 0.5 - 0.6 \u00b5m"]
-[3.632155656814575, 4.4778900146484375, "[FF] Function of the Dual-Frequency Synthetic Aperture Radar (DF-SAR) = Studying planetary surfaces and subsurface"]
-[8.082952499389648, 8.529712677001953, "[TT] Spectral Band of the AVNIR = 0.42-0.50 \u00b5m"]
-[11.423579216003418, 6.623899459838867, "[TT] Cadence of the Proton Energy Spectra = Up to around 20 MeV"]
-[8.682008743286133, 2.0363659858703613, "[TT] Wind Vector Directions Accuracy of the SeaWinds scatterometer = 20\u00b0"]
-[7.492025375366211, 9.048102378845215, "[TT] Tuned Wavelengths of the FUV Instrument = 135.6 and 155.0 nm"]
-[5.824268341064453, 2.2267251014709473, "[FF] Project Contributor of the MIMOSA = Ladislav Sehnal"]
-[7.061037063598633, 3.8123135566711426, "[FF] Trajectory Designers of the OMOTENASHI = Javier Hernando-Ayuso, Yusuke Ozawa, Shota Takahashi, Stefano Campagnola, Toshinori Ikenaga, Tomohiro Yamaguchi, Tatsuaki Hashimoto, Chit Hong Yam, Bruno V. Sarli"]
-[8.253866195678711, 9.076189041137695, "[TT] Wavelength Calibration of the Argus = 1064 nm and 1532 nm"]
-[9.249114036560059, 1.8596622943878174, "[FF] Location of the HARPS = European Southern Observatory's 3.6m Telescope"]
-[8.898008346557617, 4.64687442779541, "[TT] Attitude Determination of the S/C = Two STA (Star Tracker Assembly)"]
-[9.560696601867676, -0.504387617111206, "[TT] Orbital Altitude of the FormoSat-2 = 891 km"]
-[11.881758689880371, 3.305224895477295, "[TT] Nozzle Throat Diameter of the Propulsion System = 700 \u00b5m"]
-[6.646574020385742, 4.069659233093262, "[FF] Development Status of the Intermediate Experimental Vehicle = Unknown"]
-[14.021634101867676, 3.973881483078003, "[TT] Instrument Mass of the OVM = 2.5 kg"]
-[10.933798789978027, 7.421084880828857, "[TT] Swath of the TANSO-CAI = 1000 km"]
-[8.671794891357422, 9.00532054901123, "[TT] Sensitivity of the NIRSpec MIRI = 368 nJy (3.5 \u03bcm, \u03c4 i =10,000 s, and \u03bb/\u0394\u03bb = 100)"]
-[9.566792488098145, 4.2578349113464355, "[TT] Magnetometers of the S/C = Two 3-axis magnetometers"]
-[14.065658569335938, 4.0282464027404785, "[TT] Instrument Mass of the RAMIS = 540 g"]
-[9.200599670410156, 6.542473793029785, "[TT] PUI Measurement Resolution of the IMAP = < 1 min"]
-[5.369205951690674, 0.4296185076236725, "[TT] Date of first successful ranging to LRO of the NGSLR = 30-June-2009"]
-[8.573612213134766, 6.153281211853027, "[TT] Relative Accuracy of the 535 nm Band = 100 ppm"]
-[7.416014194488525, 2.927076578140259, "[TT] Purpose of the MethaneSAT = Detect global methane emissions"]
-[7.921118259429932, 5.924940586090088, "[FF] Purpose of the Onboard Cameras = Look back at the plywood and take pictures to see how it is behaving"]
-[4.617543697357178, 7.407939434051514, "[TT] Downlink Frequency of the NEMO-AM = S-band"]
-[6.160384178161621, 5.245944499969482, "[FF] Data Transmission of the GOLD = Transmit data from a geostationary orbit"]
-[4.776879787445068, 1.8868910074234009, "[FF] Operational Mandate of the EUMETSAT = 1993"]
-[6.646340370178223, 0.6531108617782593, "[FF] Data Collection Period of the AMS = Complete solar cycle"]
-[14.074210166931152, 4.04171895980835, "[TT] Mass of the Instrument = 38.7 kg"]
-[7.745334625244141, 3.4028842449188232, "[FF] Test Objectives of the RemoveDebris = Practice hitting an onboard target with a harpoon, jettison a small piggyback satellite and then try to bag it up with a net"]
-[14.08031940460205, 3.206791639328003, "[TT] Mass of the DataLogger = 2 kg"]
-[5.575227737426758, 5.627666473388672, "[TT] Processor of the ICM = Leon ll processor"]
-[5.734036922454834, 6.895840167999268, "[TT] Size of the Processed Science Data Packet = 60 bytes"]
-[4.813107967376709, 0.8380674123764038, "[TT] Launch Date of the TeLEOS-1 = Dec 16, 2015"]
-[4.71030330657959, 7.074920177459717, "[TT] X band downlink Data Rate of the Payload data management = 60 Mbit/s"]
-[10.187031745910645, 5.770965576171875, "[TT] Temperature Retrievals of the Sensor = Extended up to about 80 km"]
-[6.5013346672058105, 2.0474538803100586, "[FF] URL of the NuSTAR = http://www.nustar.caltech.edu/news/nustar170131"]
-[13.823216438293457, 6.932545185089111, "[TT] Nominal Generation Voltage of the ISS = 160 V"]
-[3.4990572929382324, -0.8729215264320374, "[TT] Orbit of the Satellite = Sun-synchronous dawn-dusk"]
-[13.953498840332031, 3.09344482421875, "[TT] Mass of the SeaHawk-1 = ~5 kg"]
-[18.799182891845703, 3.4795925617218018, "[TT] Mean \u0394N (m) of the Masirah Island = -7.1"]
-[10.23878002166748, -1.3050140142440796, "[TT] Inclination of the 46 nanosatellites = 97.51\u00ba"]
-[4.4433369636535645, 7.5805583000183105, "[TT] Gain on receive of the Uplink (VHF) = 2.15 dBi"]
-[8.568050384521484, 8.573572158813477, "[TT] Instantaneous spectral coverage of the Spectrometer = 2.37 km/s"]
-[5.280113220214844, 0.5237395167350769, "[FF] Update Date of the Juno = 11 December 2020"]
-[3.182046890258789, 4.465266704559326, "[TT] Band of the TerraSAR-X = X-band"]
-[6.7748799324035645, 6.207082271575928, "[TT] Number of the TDI Stages = 8"]
-[6.478909015655518, 5.886363506317139, "[FF] Components of the RFE = Dicke switch, reference load, coupler to a noise diode"]
-[6.351750373840332, 3.6340837478637695, "[TT] Expected Operational Position of the GOES-T = GOES-WEST"]
-[11.307262420654297, 5.8567657470703125, "[TT] Type of the Lutetia = M-type (metallic)"]
-[8.540912628173828, 7.010850429534912, "[FF] Camera Type of the Chang'e-2 = Micro CMOS-camera"]
-[3.4095535278320312, 4.397982120513916, "[TT] Immunity of the Interferometer = Immune to damage or misalignment during launch and on-orbit operations"]
-[5.350628852844238, 3.9608047008514404, "[TT] Number of Satellites of the V-band Constellation = 13,000"]
-[7.950831413269043, 8.818713188171387, "[TT] Spectral Signature of the Osprey = Carbon-rich material"]
-[7.975744247436523, 5.851166725158691, "[TT] Radar Sensitivity of the JPL Microwave Radiometer = 12 dBZ"]
-[9.20881175994873, 2.8356499671936035, "[FF] Justification of the ACE = New science that can be accomplished with three solar wind satellites near L1"]
-[7.697469711303711, 5.608861923217773, "[FF] Development of the MONTE = Precision one-way radiometric measurement modeling, high fidelity clock modeling, and appropriate filter methods"]
-[3.8862648010253906, 4.483582496643066, "[TT] Imaging Capacity of the RADARSAT-2 = More than 250,000 km2 of the ocean in less than a minute"]
-[5.697896957397461, 4.560273170471191, "[TT] Purpose of the ADR1EN = Testing net technologies on the ground"]
-[4.98682165145874, 0.08389431983232498, "[TT] Expected Return near to Earth of the Satellite = 2029"]
-[8.651247024536133, 5.458268642425537, "[TT] Residual Acceleration of the GP-B satellite = 4\u00d710-11 m s-2"]
-[10.957313537597656, 5.098212718963623, "[TT] Sensor #1 Radius of the OPSE = 42 mm"]
-[12.438071250915527, 0.6295276880264282, "[TT] CCDs per Camera of the Plato Camera = 4"]
-[6.008757591247559, 5.342177391052246, "[FF] Antenna Operation of the LPT = Prohibited"]
-[5.597385406494141, 1.107896089553833, "[FF] Meeting Date of the ECOSTRESS = 15 - 17 May 2017"]
-[9.91413688659668, 2.661323070526123, "[FF] Triple-Altitude Delivery of the NanoRacks = Yes"]
-[9.36669921875, 4.856028079986572, "[TT] Filter of the ACS = Extended Kalman filter"]
-[7.343608379364014, 8.841156005859375, "[TT] Configuration of the Filter = Telecentric"]
-[8.72035026550293, -0.22787201404571533, "[TT] Apogee (km) of the Meteor-2-1 = 906"]
-[4.818049907684326, 0.5732907652854919, "[TT] Launch Date of the STARE-A = Sept. 13, 2012"]
-[9.616642951965332, 8.337518692016602, "[TT] Camera FOV of the Observation of non-cooperative objects = 14o"]
-[9.239530563354492, 8.330743789672852, "[TT] No of Simultaneous Soundings of the Telescope = 4 per band"]
-[11.799434661865234, 0.06638828665018082, "[FF] Mission Name of the TESS = Transiting Exoplanet Survey Satellite"]
-[5.587594509124756, -2.01405668258667, "[FF] Imaging Capability of the KOMPSAT-3 = Afternoon"]
-[8.060521125793457, 8.620814323425293, "[TT] Wavelength Range of the VNIR = 0.45 - 0.905 \u03bcm"]
-[6.943905830383301, 7.742245197296143, "[FF] Size of the Reflector Deployment Assembly = Scaled from the GMI RDA"]
-[6.506367206573486, 1.4034603834152222, "[FF] Availability of the U.S. forecast and global maps = Freely available"]
-[9.71503734588623, 4.8357319831848145, "[TT] Stabilization of the FORTE = Momentum-biased, gravity-gradient stabilized (nadir-pointing)"]
-[10.343045234680176, 4.551694869995117, "[TT] Size of the Reaction Wheels = Large (0.2 Nm, 12 Nms)"]
-[8.722294807434082, -0.26327964663505554, "[TT] Latitude of the ICESat-2 = 88 degrees south"]
-[8.77737808227539, 0.843967616558075, "[TT] Reach of the InSight lander = Nearly 2 meters"]
-[11.356528282165527, 2.7944176197052, "[TT] Payload Accommodation of the Minisatellite = 50 kg (max)"]
-[8.742806434631348, 8.030845642089844, "[TT] Digital Lines of the EPH = Sixteen"]
-[7.530486583709717, 8.371740341186523, "[TT] Observation Band of the TRACE = 171 \u00c5"]
-[7.974475383758545, 6.9806084632873535, "[TT] Operation of the Imager = Operates continuously"]
-[10.083856582641602, -1.5610955953598022, "[TT] Inclination of the Vstar = 90\u00ba"]
-[9.337998390197754, 6.393854141235352, "[FF] Measurement Range of the IMAP-Ultra = Extends the measurements through the range covered previously by Cassini/INCA"]
-[13.224409103393555, 5.247630596160889, "[TT] Solar Array Size of the DSP satellites = 6.33 m2"]
-[5.493930339813232, 7.075101852416992, "[TT] Baud Rate of the Science Data Interface = 1 Mbit/s"]
-[10.0816011428833, 6.961989879608154, "[TT] Spatial Resolution of the INSAT sounder = 10 km x 10 km"]
-[6.137826919555664, 0.8387548923492432, "[FF] First Light Date of the CaSSIS = Unknown"]
-[5.770194053649902, 7.161149978637695, "[TT] Data Rate (max) of the HiSPiCO = 2000 kbit/s"]
-[10.385741233825684, 2.0622544288635254, "[TT] Sky Sweep Duration of the eROSITA X-ray telescope = 182 days"]
-[14.03355884552002, 7.173710346221924, "[TT] Output Voltage of the PPM = 28 V"]
-[7.08173131942749, 7.0313005447387695, "[FF] Optical Slab Fracture of the Laser002 = The crystal optical slab within the pre-amplifier assembly fractured towards the center at a point where thermal stress is low"]
-[13.537989616394043, 7.239955425262451, "[TT] Power (at start of mission) of the S/C = 31 W (at 28 V)"]
-[14.264522552490234, 3.2116920948028564, "[TT] Mass of the MiniCOR = <3.6 kg"]
-[10.00533676147461, -0.4457378089427948, "[TT] Secondary Orbit Altitude Goal of the HAPS = 1200 km"]
-[4.799744129180908, 0.550148069858551, "[TT] Instrument Delivery Date of the SUVI = Oct. 2013"]
-[7.625025272369385, 9.187066078186035, "[TT] Band 5 Wavelength of the AEISS = 760 nm - 900 nm"]
-[3.9121854305267334, 3.5145576000213623, "[TT] Program Name of the SAR/Galileo = SAR/Galileo"]
-[7.979342937469482, -0.5822147727012634, "[FF] Event of the Paris Glacier = Agreement of a legally binding treaty in 2015"]
-[5.409878253936768, 5.449106693267822, "[TT] Radiation Exposure of the STRV-1a = Very high"]
-[8.433717727661133, 2.0330841541290283, "[FF] Purpose of the COWVR = Forecast ocean surface winds"]
-[3.666792869567871, -0.8835591077804565, "[TT] PI of the SPARCS = Evgenya Shkolnik"]
-[14.273578643798828, 3.0543501377105713, "[TT] Mass of the ALSAT-2B = 125 kg"]
-[8.374483108520508, 7.1848931312561035, "[TT] Quantity of the WFOV cameras = 4"]
-[6.316247463226318, 8.645967483520508, "[TT] Polarization of the Severyanin-M = Vertical"]
-[6.306356430053711, -0.3143194019794464, "[TT] Revisit Time of the DMAC = Four days"]
-[5.652281761169434, 5.4023284912109375, "[FF] Ground Terminals of the ETS-VIII LRRA = Portable terminal, Handheld terminal"]
-[3.461397409439087, 5.253538131713867, "[FF] Bandwidth of the CSG-SAR = Programmable"]
-[5.237996578216553, 6.243264675140381, "[TT] Core Speed of the BILGE = 200 MHz"]
-[4.569770336151123, -0.8943722248077393, "[FF] Launch Time of the SpaceX Dragon spacecraft = 1:16 p.m. EST (18:16 GMT) Dec. 5, 2018"]
-[4.504617691040039, 4.205626487731934, "[TT] Number of Operational Spacecraft of the LEOSAR = 5"]
-[7.486276626586914, 8.66480541229248, "[FF] Band of the UVI instrument = 0.375-0.395 \u00b5m"]
-[8.25162410736084, 2.127490520477295, "[FF] Output Data of the Poseidon-1 = Sea state and wind speed"]
-[7.107574462890625, 6.837840557098389, "[TT] Dicke Load Phases of the MWR = Three"]
-[9.863053321838379, 2.2981176376342773, "[FF] Sensitivity of the NuSTAR = Cannot view the larger flares"]
-[5.674383640289307, 6.380300045013428, "[TT] Capacity of the S/C Data Recorders = 54 Gbit"]
-[9.497384071350098, 6.905213832855225, "[TT] Range Resolution of the Wide multi-look fine = 3.1-10.4 m"]
-[9.483057022094727, 0.8750974535942078, "[TT] Distance from Earth of the New Horizons = More than 5 billion miles"]
-[11.674956321716309, 3.333010196685791, "[TT] Thruster Type of the Eutelsat 172B = Electric"]
-[5.95261812210083, 8.74524974822998, "[TT] MTF at Nyquist Frequency of the Spacecraft = > 10% for Pan"]
-[11.882257461547852, 4.712764263153076, "[TT] Size of the CEASE = 10 cm x 10 cm x 8.2 cm"]
-[7.841494083404541, 7.738532066345215, "[FF] Color in Image of the Was 49a = Greenish"]
-[4.2039690017700195, 7.305253028869629, "[TT] Band of the EUTELSAT KONNECT = Ka-band"]
-[8.913431167602539, 7.155447006225586, "[TT] Calibration Status of the HRC (High-Resolution Camera) = Ongoing"]
-[7.173387050628662, 5.013411998748779, "[FF] Function of the VBN = Provide on-board processing function in order to support navigation"]
-[10.568733215332031, 4.937942028045654, "[TT] Placement of the Langmuir Probe = On long protruding booms"]
-[6.335613250732422, -1.3115159273147583, "[TT] Mission of the ACC = GRACE\u2010Follow\u2010on"]
-[13.975312232971191, 3.0017430782318115, "[TT] Mass of the OPS-SAT = 6 kg"]
-[6.182763576507568, 2.425848960876465, "[FF] Coordination Office of the ARTEMIS = Air Force International Affairs Office"]
-[6.978010177612305, 1.030669093132019, "[FF] Arrival Date at Mars of the ExoMars 2020 mission = March 2021"]
-[10.583782196044922, 2.189910650253296, "[TT] Time Delay of the X-ray binaries = About one-tenth of a second"]
-[11.127490997314453, 1.0659241676330566, "[FF] Cosmic Horizon of the LISA = Expands"]
-[13.351819038391113, 2.9037630558013916, "[TT] Mass of the TUBSAT-N = 8.5 kg"]
-[13.213481903076172, 7.249894618988037, "[TT] Power Consumption of the VIRR = 7.3 W"]
-[5.0733723640441895, 2.6449689865112305, "[FF] Predecessor Organization of the Meteosat = ESRO (European Space Research Organization)"]
-[5.851756572723389, 2.2124688625335693, "[TT] Location of the ICARE = USTL (Universit\u00e9 des Sciences et Techniques de Lille), Lille, France"]
-[10.13647747039795, 0.9308788776397705, "[TT] Distance from Earth of the HAT-P-7 = About 1,000 light years"]
-[11.036333084106445, 6.1127142906188965, "[TT] Material of the Focal Plane Assembly = Titanium"]
-[5.802771091461182, 6.3013811111450195, "[TT] Capacity of the SSR = 300 Gbit"]
-[6.4033331871032715, 7.965631008148193, "[TT] Number of Channels of the FODB = 12"]
-[7.714995384216309, 9.119996070861816, "[TT] Wavelength Range of the Band 2 = 0.59-0.69 \u00b5m"]
-[6.681266784667969, -0.3076257109642029, "[TT] Programming Loop Operation of the Helios-2 = Daily"]
-[2.895108699798584, 4.541407108306885, "[TT] Frequency of the PALSAR-2 = 1257.5 MHz"]
-[10.135390281677246, -1.6284592151641846, "[TT] Inclination of the Bion-M1 = 64.9\u00ba"]
-[10.368194580078125, 5.5458173751831055, "[TT] Thermal Control Range of the SU = \u00b1 0.1\u00baC"]
-[4.86833381652832, -1.8714666366577148, "[TT] Design Life of the Chang'e-4 lunar probe = Three years"]
-[4.51987361907959, 7.715269565582275, "[TT] Receiver noise temperature of the Uplink (VHF) = 23 dBK"]
-[5.671935081481934, 1.2010118961334229, "[TT] Proto-flight Tests Completion Date of the Optical Sensor = 2011"]
-[5.356872081756592, 6.211780548095703, "[TT] RAM of the SDR Host Computer = 8 GB"]
-[11.543733596801758, 6.6752753257751465, "[TT] Energy Range of the eROSITA = Up to 10 keV"]
-[11.454140663146973, 5.812458038330078, "[TT] Structure Material of the New Horizons = Aluminum honeycomb core with ultra-thin aluminum face sheets"]
-[5.685900688171387, -0.9007756114006042, "[TT] Design Life of the SwissCube = 1 year"]
-[6.226135730743408, 1.0760685205459595, "[FF] Progenitor Type of the GRB 130925A = PopIII-like"]
-[5.8473005294799805, -0.04828618839383125, "[TT] Activation Times of the LDT = Between 1:00 and 4:18 (UTC), and between 13:00 and 16:18 (UTC)"]
-[5.46571683883667, 7.138335704803467, "[TT] Data Exchange Speed of the LCTs = Up to 1800 Mbit/s"]
-[5.446852684020996, 3.7862179279327393, "[TT] Number of Pieces of the Iceberg A-76 = 3"]
-[6.674989700317383, 0.24012447893619537, "[TT] Publication Date of the CryoSat = 15 September 2018"]
-[8.174310684204102, 7.438984394073486, "[TT] SNR of the PMC-2 Imagers = 23~43 db for PAN and 25~43db for MS data"]
-[8.199790000915527, -0.24607889354228973, "[FF] Velocity Measurement of the Amundsen Sea Embayment sector of West Antarctica = Logarithmic scale"]
-[7.641406536102295, 5.8147687911987305, "[FF] Camera Activation of the HORYU-2 = Command from the ground station"]
-[8.09924602508545, -1.2213287353515625, "[TT] Instrument of the ICESat-2 = Laser altimeter"]
-[9.290435791015625, 7.149285793304443, "[TT] Image Resolution of the Ikonos-2 = 1 m"]
-[5.783444404602051, 0.7349852919578552, "[FF] Publication Date of the ISEE-C = July 1978"]
-[8.973331451416016, 5.300025939941406, "[TT] Orbit Shift Distance of the GomX-4A = Up to 2000 km"]
-[8.088027954101562, 3.3729419708251953, "[FF] Purpose of the OCO-2 = Making unprecedented, accurate global measurements of carbon dioxide levels in the atmosphere and providing unique information on the natural processes controlling carbon exchange between land and air and between the atmosphere and ocean"]
-[7.258721351623535, 4.626399040222168, "[FF] Function of the VT = Provide GRB alerts with sub-arcsec accuracy"]
-[12.40322208404541, 0.6171725988388062, "[FF] Components of the PLATO Satellite = Optical Bench Assembly (OBA), Payload Thermal shield, Payload Electronics panel, Central Module - Structure and Propulsion, Avionics and Electronics panels, Sunshield (SS) and Solar Array"]
-[10.185537338256836, 5.802619457244873, "[TT] Temperature of the VIS Focal Plane = 155 K (-115\u00b0C)"]
-[6.68039083480835, 8.472393989562988, "[FF] Photon Flow Direction of the New lighthouse model = At a right angle to the polar beams expected in a standard pulsar model"]
-[4.470288276672363, 3.095898151397705, "[TT] Location of the EDRS MOC = Ottobrunn (Germany)"]
-[5.3480544090271, 3.9300358295440674, "[TT] Number of Satellites of the NSPO = 12"]
-[3.9838898181915283, 6.02470064163208, "[TT] Antenna Type of the ADS-B receiving payload = Helical antenna"]
-[10.112896919250488, -1.5746443271636963, "[TT] Inclination of the Satellite = 80\u00ba"]
-[5.843435287475586, 6.024437427520752, "[FF] Message Format Elements of the DCP = Unmodulated carrier for 5 seconds, 250-bit preamble, 15-bit synchronization word, DCP address, Data field, 31-bit End of Transmission (EOT) sequence"]
-[5.756883144378662, 2.7392067909240723, "[TT] Assistants of the COMS = Astrium, KARI (Korean Aerospace Research Institute), and KIOST (Korean Institute of Ocean Science and Technology)"]
-[8.07080078125, -0.9880006313323975, "[FF] Orbit of the ICESat-2 = Over sea and land ice"]
-[8.207124710083008, 7.125821113586426, "[FF] Latchup Event of the CMOS Sensors = Produces an increase in current consumption, and the device becomes un-responsive"]
-[5.924295902252197, 6.235811710357666, "[TT] Connection Delay of the EDRS = Up to 90 minutes"]
-[8.634908676147461, 3.039970636367798, "[FF] Impact of the EUVS = Excess EUV radiation can result in radio blackouts of terrestrial high frequency communications at low latitudes"]
-[10.899561882019043, 0.6488756537437439, "[TT] Number of Lowest-Mass, Tiniest, and Dimmest Cluster Members' Rotation Rates Measured of the Kepler = About 500"]
-[5.473405838012695, 7.15058708190918, "[TT] User Data Link Speed of the GEO LCT = 1.8 Gbit/s"]
-[9.05018424987793, 7.065576553344727, "[TT] Spatial Resolution of the SLIM6 = 32 m GSD"]
-[14.192962646484375, 3.3426263332366943, "[TT] Mass of the Experiment = 11 kg"]
-[13.540822982788086, 5.54086971282959, "[FF] Purpose of the SFINKS = Test the efficiency of thin film solar arrays"]
-[10.798194885253906, 1.488106608390808, "[FF] Mass of the J1820 = Lower than supermassive black holes"]
-[5.662950038909912, 7.123520851135254, "[TT] Data Rate of the 16QAM = 800 Mbit/s"]
-[10.265454292297363, 5.8805341720581055, "[TT] Temperature Range of the Telescope = Much wider"]
-[6.04715633392334, 5.381040573120117, "[FF] Branch of the Level-1 Processor v700 = ALL-LICEF"]
-[6.326691150665283, 1.5521080493927002, "[FF] Calibration Approach Date of the MICROSCOPE = 2003"]
-[5.312234878540039, 2.142185688018799, "[TT] Mission Type of the FormoSat-7 / COSMIC-2 = Non-EO"]
-[5.493511199951172, 0.6530967354774475, "[FF] Data Release Date of the EPIC = July 20, 2016"]
-[8.071049690246582, 7.8136725425720215, "[TT] Dynamic range of the Channel = approx. 0-100% albedo"]
-[7.307372570037842, 5.647118091583252, "[FF] Detector of the Tatiana = On-board"]
-[7.610988616943359, 0.27619075775146484, "[TT] Development Cost of the Lucy = Approximately $450 million"]
-[5.160949230194092, 2.326948404312134, "[TT] Mission Type of the LADEE = Non-EO"]
-[10.520905494689941, 1.9052493572235107, "[FF] Mission Purpose of the ABEX = Investigate Gamma-Ray Bursts (GRB) through spectral analysis and localization of joint gravitational-wave GRB mergers using wavefront timing analysis"]
-[13.848248481750488, 5.676608562469482, "[FF] Production Speed Improvement of the Solar Cells = More than 20 times faster than the process now commonly used"]
-[5.488327980041504, 1.9482256174087524, "[TT] Mission Name of the ABEX = Alabama Burst Energetics eXplorer (ABEX)"]
-[5.192870140075684, 8.428696632385254, "[TT] Bandwidth of the Channel 8 = 400 MHz"]
-[5.500677585601807, 6.506771564483643, "[TT] Storage Capacity of the TUBSAT-N = Over 6000 messages at 134 bytes in length"]
-[7.53985071182251, 0.8417168259620667, "[FF] Mission of the LunaH-Map = Lunar Polar Hydrogen Mapper"]
-[7.611278533935547, 8.427680969238281, "[TT] Bands of the WFI = Three visible bands and one NIR band"]
-[7.762547492980957, 5.1026177406311035, "[FF] Flight Performance Analysis of the GRACE K-band ranging instrument = Unknown"]
-[8.150003433227539, -0.900027871131897, "[FF] Snow and Ice Thickness Measurement of the Airborne Topographic Mapper = Unknown"]
-[5.452123641967773, 3.0443973541259766, "[TT] Developer of the AstroRad vest = StemRad"]
-[6.107097625732422, 4.241111755371094, "[FF] Contact Operations of the COSMOS = Pre-contact operations, real-time contact operations, and post-contact operations"]
-[4.75319242477417, 2.430854320526123, "[FF] Technology of the OSCAR-QUBE = Diamond-based quantum technology"]
-[8.968270301818848, 7.387258052825928, "[TT] Resolution of the intensified sprite imager = 512 x 80 pixels"]
-[5.143103122711182, 4.0567946434021, "[TT] Bus Name of the NorSat-1 = GNB (Generic Nanosatellite Bus)"]
-[9.005585670471191, 3.1323392391204834, "[FF] Trajectory Deflection of the Solar System = Diameter of an atom every second"]
-[7.044842720031738, 3.8019635677337646, "[FF] Flight Heritage of the HiSPiCO = Sounding rocket"]
-[8.197511672973633, 8.2732515335083, "[TT] Resolving Power of the IR Channel = 70"]
-[6.229948997497559, 4.879748344421387, "[FF] Location of the DCS = LEO"]
-[10.890090942382812, 7.54512882232666, "[TT] Swath Width of the WFI = 800 km"]
-[4.5499396324157715, 2.9842171669006348, "[TT] Operator of the GPC (GIOVE Processing Center) = GAIN in Noordwijk (The Netherlands)"]
-[5.934762954711914, 4.617134094238281, "[TT] Developer of the Flight Computer = GSFC"]
-[4.393429279327393, 2.1835520267486572, "[TT] Renamed By of the KhalifaSat = His Highness Sheikh Mohammed Bin Rashid Al Maktoum"]
-[8.921630859375, 4.314050674438477, "[FF] Purpose of the VLBI = Inertial direction of the Earth rotation vector determination"]
-[7.800909519195557, 3.03786563873291, "[FF] Purpose of the CO2M = Distinguish between natural sources of carbon dioxide and sources that are a result of human activity"]
-[6.723387241363525, 2.676327705383301, "[FF] Symposium Date of the Earth Observation Payload Instruments = April 8-12, 2013"]
-[6.108325958251953, 3.299943685531616, "[FF] Investment Focus of the UrtheCast = Constellation of Earth-imaging satellites"]
-[4.676365375518799, 5.74722957611084, "[TT] Downlink Frequency Band of the GPS-DASS = 2226 MHz (S-band)"]
-[13.669073104858398, 5.904288291931152, "[TT] Power Output of the Solar Panels = 20 KW"]
-[7.813440322875977, 6.592951774597168, "[TT] Repeatability of the Imaging Mode = 33 min"]
-[8.350942611694336, 2.7783291339874268, "[TT] Measurement Category of the Badr-B = Gravity, Magnetic and Geodynamic measurements"]
-[5.731001853942871, 7.061563968658447, "[TT] Data Rate of the ABI = 75 Mbit/s"]
-[8.530914306640625, 6.12555456161499, "[TT] Accuracy of the CERES = 1.0%"]
-[9.038519859313965, 2.599966049194336, "[FF] Mission Objective of the IMAP = Understand the boundary of the heliosphere"]
-[5.211400032043457, 1.38673734664917, "[TT] Launch Date of the ELSA-d = March 2021"]
-[6.328225135803223, -1.3163138628005981, "[TT] Launch Date of the GRACE Satellite = March 17, 2002"]
-[4.006158351898193, 3.554166793823242, "[TT] Mission Status of the Galileo = Operational (nominal)"]
-[11.361991882324219, 3.3323047161102295, "[FF] Conference Date of the \u00b5CAT Micro-Propulsion Solution = August 6-11, 2016"]
-[5.491525173187256, 7.083458423614502, "[TT] Baud Rate of the Command and Telemetry Interface = 19.2 kbit/s"]
-[13.956011772155762, 2.8651835918426514, "[TT] Mass at Launch of the S/C = 1360 kg"]
-[4.470037460327148, -0.21987424790859222, "[TT] Launch Date of the Nauka = July 21"]
-[10.027655601501465, 1.433892846107483, "[FF] Unique Capability of the Gaia = Performing the most precise astrometric survey ever realized"]
-[7.536829471588135, 2.8846988677978516, "[FF] Emission Source Detection of the MethaneSat = Small emission sources over large areas"]
-[7.745709419250488, 2.54587721824646, "[FF] Radiation-Intense Areas of the ABEX = South Atlantic Anomaly and Van Allen Belts' High-Latitude Zones"]
-[8.122154235839844, -0.4664268493652344, "[TT] Multi-Year Ice Amount of the Sea Ice = Second-lowest on record"]
-[6.898905277252197, 6.154194355010986, "[TT] Operation Mode of the GR700XD grism = Slitless"]
-[10.748326301574707, 1.0505986213684082, "[TT] Size of the TOI 700 d = About the size of Earth"]
-[8.590514183044434, 8.406103134155273, "[TT] Spectral Resolution of the OMPS Limb Profiler = 0.75 nm to 25 nm"]
-[6.607689380645752, 1.839228630065918, "[FF] URL of the SMAP = http://smap.jpl.nasa.gov/mission/description"]
-[6.657156944274902, -0.05669832602143288, "[FF] Mission Duration of the SeaWiFS = Thirteen Years"]
-[5.995484352111816, 0.9481143951416016, "[FF] First Earth Imagery Release Date of the UrtheCast = April 3, 2014"]
-[8.894868850708008, 5.3844218254089355, "[FF] Attitude of the GOMX-3 = Ram pointing"]
-[6.557558059692383, -0.9386131167411804, "[FF] Observation Continuity of the WFIRST = More-or-less continuously"]
-[9.46021556854248, -1.3964478969573975, "[TT] Eccentricity of the PROBA-3 = 0.8111"]
-[4.202729225158691, 7.29719352722168, "[TT] Link Type of the Ka-band table management = Bidirectional"]
-[8.507347106933594, 5.788219451904297, "[TT] Tracking Passes Occurrence of the CAPSTONE = When nearer to periapse"]
-[10.312182426452637, 4.393711090087891, "[TT] Planned Quantity of the Surface Rovers Deployment = Four"]
-[9.403755187988281, 8.160124778747559, "[TT] Weak Lens Defocus of the ZnSe prism = ~25 pixels"]
-[5.601307392120361, 5.497700214385986, "[FF] Function of the SRX = Uplink redundancy"]
-[8.156350135803223, 2.051426410675049, "[FF] Outline of the KIZUNA(WINDS) = Unknown"]
-[9.732781410217285, 6.774179935455322, "[TT] Stereo Image Dimensions of the Satellite = 100 km x 20 km"]
-[7.737123966217041, -2.5331568717956543, "[FF] Observing Modes of the GOLD = Disk images and limb scans, dayside: T and O/N2, nightside: O+ density, stellar occultations, full disk maps and limb scans with 30 minute cadence"]
-[11.117552757263184, 0.6511899828910828, "[FF] Purpose of the Next-generation telescopes = Directly image Earth-size exoplanets"]
-[7.713386535644531, 0.5186724066734314, "[TT] Development Status of the Lunar IceCube = Passed essential environmental testing"]
-[5.2592573165893555, 0.6974157094955444, "[FF] Activation Date of the ISERV Pathfinder = March 3, 2013"]
-[4.818325519561768, 0.25957632064819336, "[TT] Launch Date of the SPOT-1 = February 1986"]
-[6.301621437072754, 1.720751404762268, "[FF] URL of the AISsat-1 = http://www.km.kongsberg.com/ks"]
-[6.668798446655273, 4.7705512046813965, "[FF] Structure of the OSC = Essentially a cube"]
-[8.514121055603027, 6.930462837219238, "[TT] Instrument Type of the DMC-3 = High resolution optical imagers"]
-[10.44052505493164, 7.194622039794922, "[TT] Area Coverage of the WFI = 330 km by 200 km"]
-[5.433686256408691, 0.7313456535339355, "[TT] Arrival Date of the NICER = June 8, 2016"]
-[10.009576797485352, 1.9712951183319092, "[FF] URL of the Chandra = https://www.nature.com/articles/s41467-018-06558-7.pdf"]
-[5.019453048706055, 1.4461055994033813, "[FF] Communication Link Establishment of the INSAT3D = Operation since 1999"]
-[5.915686130523682, 0.8326626420021057, "[TT] Product Specification Date of the RadidEye Imagery = January 2016"]
-[4.824102401733398, 6.458627700805664, "[FF] Protocol of the RF Communications Subsystem = Strandatoga"]
-[7.396254062652588, 4.913279056549072, "[FF] Operational Modes of the ALOS-2 = Rate Damping Mode, Sun Acquisition Mode, Earth Acquisition Mode, Fine Normal Mode"]
-[7.97764253616333, 0.10383164882659912, "[FF] Measurement of the GRACE and GRACE Follow-On = Weight, or mass, of the object below"]
-[6.736221790313721, 4.482596397399902, "[FF] Design Principle of the FDIR System = Lowest-level isolation and recovery is attempted first"]
-[12.040528297424316, 6.283990859985352, "[FF] Helium Flux of the AMS = Exhibits nearly identical and equally unexpected behavior as the proton flux"]
-[9.224321365356445, 3.0872678756713867, "[FF] Interaction of the Magnetosphere = Penetrated by the solar wind's onslaught of charged particles"]
-[8.814360618591309, 7.383996963500977, "[TT] Translation of the Detector = ~ 25 \u00b5m"]
-[7.523443698883057, 2.9207708835601807, "[FF] Measurement Types of the MethaneSAT = Global mapping, point-source detection, area-source detection"]
-[6.438004493713379, -0.35905277729034424, "[TT] Revisit Time of the LIS = 4 days"]
-[10.512964248657227, 2.944650650024414, "[FF] Data Rate of the S/X-band architecture = Considerable increase for nanosatellites"]
-[5.075972080230713, 7.136412143707275, "[TT] Uplink Data Rate of the NSat = 1.2 kbit/s"]
-[5.23061990737915, 3.1687259674072266, "[TT] Manufacturer of the LunIR = Lockheed Martin"]
-[6.581287384033203, 6.790730953216553, "[TT] Laser Beam Capacity of the EDRS-A = Up to 1.8 Gbit/s of user data"]
-[11.448484420776367, 3.6413469314575195, "[TT] Number of Fires of the Fregat = Two"]
-[6.896786689758301, 4.209253787994385, "[FF] Design of the OMI = Conceptual"]
-[8.225605964660645, 5.33719539642334, "[FF] Components of the HISUI = Reflective telescope, two spectrometers"]
-[8.720320701599121, 7.075160503387451, "[FF] Image Resolution of the On-board Image Processing = Better than 100 m/pixel"]
-[9.267205238342285, 3.1924116611480713, "[FF] Purpose of the Bragg-crystal telescope-spectrometer Mg1 and Mg2 = Imaging hot plasma (T ~ 10 MK) of the solar corona"]
-[7.398438930511475, 0.25170648097991943, "[TT] Departure from Bennu of the OSIRIS-REx = Mid-2021"]
-[7.56273078918457, 3.465552568435669, "[FF] Presentation Title of the Marshall Polk = DebriSat: data from Destruction"]
-[6.697881698608398, 1.9310214519500732, "[FF] URL of the SwRI-led team = https://www.swri.org/press-release/high-fidelity-images-sun-atmosphere?"]
-[10.811347007751465, 5.657770156860352, "[FF] Polyimide Thermal Shield of the Optic = Unknown"]
-[9.337656021118164, 3.365901470184326, "[FF] Peak strength of the EEJ (Equatorial Electrojet) = ~80 nT at 12:00 hours LT (Local Time)"]
-[5.678943157196045, 2.554541826248169, "[TT] Population of the Kiribati = 100,000 citizens"]
-[6.355251312255859, 4.4088006019592285, "[FF] Instrument Type of the ADEOS Comms = Communications"]
-[8.686219215393066, 4.740053653717041, "[TT] Quantity of the Autonomous star tracker (AST) = 2"]
-[10.743758201599121, 1.4416793584823608, "[TT] Black Hole Mass of the OJ 287 galaxy = Over 18 billion times the mass of our Sun"]
-[5.0566325187683105, 0.14203916490077972, "[TT] Launch Date of the Cygnus CRS-4 = 2016"]
-[6.188266277313232, 5.953514575958252, "[TT] Function of the TCU = Provides synchronization of the TR modules with a master reference"]
-[5.55937385559082, 2.2786331176757812, "[FF] Affiliation of the Carlos Flores = Unknown"]
-[10.986467361450195, 5.777733325958252, "[TT] Function of the Baffle = Thermal"]
-[4.915159702301025, 1.8040353059768677, "[FF] Purpose of the G\u00f6kt\u00fcrk-1 = reconnaissance, homeland surveillance, intelligence, environmental monitoring, forest control, cadastral surveys, identifying illegal construction sites, crop management, damage assessment after natural disasters, and management of natural resources"]
-[5.291783809661865, 1.2352299690246582, "[FF] Meeting Date of the SMOS = Sept. 30, 2015"]
-[6.515911102294922, 7.320949077606201, "[TT] Transmitting Pulses of the Instrument = H or V"]
-[5.173900604248047, 3.4952590465545654, "[TT] Manufacturer of the BILSAT-1 = BILTEN"]
-[7.045061111450195, 2.9096455574035645, "[TT] Payload Provider of the MethaneSAT = Ball Aerospace"]
-[13.392145156860352, 2.912317991256714, "[FF] Design Class of the QSAT = 50 kg"]
-[13.781900405883789, 2.8503756523132324, "[TT] Total Rock Mass Returned of the Apollo Missions = 382 kg"]
-[6.999072551727295, 5.397571563720703, "[FF] Tracking Loss of the SST = Transition to survival mode"]
-[6.1632795333862305, 0.35774466395378113, "[TT] Extended Mission Phase of the FormoSat-2 = Ongoing"]
-[3.8988025188446045, 0.9517889022827148, "[TT] Time to First Stage Landing of the Falcon 9 = Eight and a half minutes"]
-[5.837533950805664, 3.4134902954101562, "[TT] Aviation Market Growth of the India = Sustained double-digit growth for the last 50 months"]
-[8.091602325439453, 8.21114730834961, "[FF] Channels of the SEVIRI = VIS 0.6 \u00b5m, VIS 0.8 \u00b5m, IR 1.6 \u00b5m, HRV (High Resolution Visible), IR 3.9 to IR 13.4 \u00b5m"]
-[3.6131534576416016, 5.259800434112549, "[FF] Detection Objective of the MMW Radar = Debris of size 3-10 cm or larger"]
-[4.933115005493164, 2.0015695095062256, "[TT] Mission Status of the GovSat-1 = Operational (nominal)"]
-[8.632922172546387, 3.4294166564941406, "[FF] UV Light Absorption of the Earth = Absorbs UV light from the Sun and re-emits it to space"]
-[10.074216842651367, 4.550452709197998, "[TT] Pointing System of the EDSN = Reaction wheel based"]
-[5.858994960784912, 0.7177548408508301, "[TT] First Photo of the MarCO-B = 9 May"]
-[6.907960414886475, 1.5988216400146484, "[FF] Observatory Presentation of the James Webb Space Telescope = Rob Garner, \"The James Webb Space Telescope Observatory,\" NASA, July 28, 2013"]
-[5.366298675537109, 4.574887275695801, "[FF] Integration with 5G New Radio of the Open5GCore Rel. 4 = NSA [S1-MME, S1-U] and SA [N1, N2, N3]"]
-[9.761402130126953, -0.7905731201171875, "[TT] Orbit Altitude of the FY-4A = 35786 km"]
-[18.79743766784668, 3.4803311824798584, "[TT] \u0394r (m) of the Menara = 9.4"]
-[7.245475769042969, 7.795539855957031, "[TT] Number of dual-gain PHAs of the PHA = 16"]
-[14.090237617492676, 7.198554039001465, "[TT] Voltage of the MTM main power bus = 28 V"]
-[11.995210647583008, 6.53275728225708, "[TT] Energy Range of the AMS-02 = Up to 400 GeV/c2"]
-[3.203472375869751, 4.924338340759277, "[FF] Swath of Compact Polarimetry of the ALOS-2 = Wider than that of full-pol."]
-[13.64142894744873, 6.788406848907471, "[TT] Power Capacity of the Bus = 140 W"]
-[9.190620422363281, 3.063568592071533, "[FF] URL of the Magnetospheric Multiscale Mission = https://www.nasa.gov/feature/goddard/2018/nasa-s-magnetospheric-multiscale-mission-locates-elusive-electron-act"]
-[6.75427770614624, 1.856661319732666, "[FF] URL of the NICER = https://smd-prod.s3.amazonaws.com/science-red/s3fs-public/atoms/files/nicer-factsheet-final.pdf"]
-[4.9259185791015625, -2.1412296295166016, "[TT] Fuel Mass of the Chang'e-2 = 1300 kg"]
-[4.02144193649292, 6.686818599700928, "[TT] Pointing of the X-band antenna = Body-pointing"]
-[3.83184552192688, 3.422309398651123, "[TT] Launch Date of the Galileo = Sept. 9, 2015"]
-[9.878764152526855, 0.044677261263132095, "[TT] Operational Orbit of the Spacecraft = Lissajous orbit at an average distance of 800,000 km from L2"]
-[2.839367389678955, 0.08882003277540207, "[TT] J2000 declination (deg) of the B1509-58 = -59.13583"]
-[13.568652153015137, 2.7827658653259277, "[TT] Mass at Launch of the Satellite = Dry mass = 750 kg"]
-[8.714770317077637, 2.7380645275115967, "[TT] Temperature Accuracy of the Lower atmosphere = 4 K at 1000 mb"]
-[9.155797958374023, -1.3041551113128662, "[TT] Orbit of the GOES SAR transponders = Geostationary"]
-[9.101733207702637, 5.39209508895874, "[TT] Pointing Rate of the Spacecraft = 1\u00ba/s (average)"]
-[12.149068832397461, 3.8486177921295166, "[TT] Stress Level of the Reflector Film = 82.5 bar (1200 psi)"]
-[8.569897651672363, 4.8580474853515625, "[TT] Absolute Accuracy of the Instrument = Checked at regular time intervals with stellar calibrations"]
-[7.429530620574951, 2.9634761810302734, "[TT] Liquid Methane Capacity of the RRM3 = 42 liters"]
-[7.714449405670166, 9.31714153289795, "[TT] Maximum Upper Band Edge of the MS8 (NIR2) = 1043 nm"]
-[10.28297233581543, 8.001972198486328, "[TT] Length of the Telescope Assembly = 100 cm"]
-[6.159849166870117, 4.413377285003662, "[FF] Operation of the F-DUGS = Request programming and pre-feasibility analysis, satellite data acquisition, data processing and distribution, archiving and cataloguing"]
-[3.116762161254883, 2.20041823387146, "[TT] Temporal Resolution of the Sentinel-2 = High"]
-[10.909469604492188, 10.101234436035156, "[TT] Repair Date of the Alpha Magnetic Spectrometer (AMS) = January 25, 2020"]
-[6.909065246582031, -0.3138176500797272, "[FF] Radio Signals of the Hitomi = 3/27 01:23~01:27 (for 4 min) @USC, 01:21~01:27 (for 6 min) @ KTU"]
-[5.563597202301025, 2.0234217643737793, "[FF] Mission Phase of the ABEX = Science Operations"]
-[10.150202751159668, 3.212156295776367, "[FF] Measurement Parameters of the TROPICS CubeSat = Temperature, Humidity, Precipitation"]
-[7.058828353881836, 4.917752742767334, "[FF] Component of the Remotely Operated Electrical Umbilical (ROEU) Payload Disconnect Assembly (PDA) = Unknown"]
-[6.58474588394165, 5.255774021148682, "[FF] Purpose of the LCT = Combines and encodes data streams, performs data rate adaptation"]
-[6.645859718322754, 6.6560163497924805, "[TT] Technology of the EDRS = Laser"]
-[4.439449787139893, -0.060702063143253326, "[FF] Launch Date of the Starliner = Mid-May 2022"]
-[10.538143157958984, 2.4256680011749268, "[TT] Mirror Modules of the X-ray telescope = 7"]
-[9.508561134338379, 0.9714754819869995, "[TT] Reentry Speed of the Orion = 32,200 km/hr"]
-[10.093329429626465, 1.0675219297409058, "[FF] Length of the Hyades Tidal Tails = Thousands of light years"]
-[4.996663570404053, 2.8212180137634277, "[TT] Manufacturer of the Sich-2 = Yuzhnoye State Design Office (SDO)"]
-[11.769911766052246, 3.23701810836792, "[TT] Thrust of the ADCS Thrusters = 150 N"]
-[11.99549388885498, 3.477771282196045, "[TT] Chamber Pressures of the LM thruster = Approximately 700,000-2,100,000 Pa"]
-[3.3730309009552, 4.9799275398254395, "[FF] Advantage of the Staggered SAR = Allows the imaging of a wide continuous swath without the need for a long antenna with multiple apertures"]
-[6.805798530578613, 3.3470396995544434, "[FF] Data Source of the Ursa Space Systems = Space-based data from satellites"]
-[3.5056378841400146, 4.8947954177856445, "[FF] Processing Mode of the SAR Processor = Complete processing for the trigger application and possibly repeated processing for other applications"]
-[8.489705085754395, 4.847827911376953, "[FF] Image Processing of the VBS = If the glint is massive, the image will be suppressed from further processing"]
-[6.569371223449707, -2.028616189956665, "[TT] Program Timeframe of the Jason-CS = 2015-2020"]
-[5.536979675292969, 5.164942264556885, "[TT] Provider of the RTOS = VxWorks"]
-[4.4424333572387695, 7.575270175933838, "[TT] Downlink Frequency of the S-band = 2.402 GHz"]
-[8.722228050231934, 7.865232944488525, "[TT] Pixels per Line of the CZI = 21800 pixels/line"]
-[9.37524127960205, 5.031085014343262, "[TT] Attitude Knowledge Stability of the ADCS = \u2264 0.12 \u00b5rad in 2.5 seconds"]
-[4.408491611480713, 0.10967123508453369, "[TT] Starlink Satellites Launch Date of the SpaceX = 4 March 2021"]
-[5.452329158782959, 8.601741790771484, "[TT] Bandwidth of the SAW Filters = 14 MHz"]
-[9.42310905456543, 3.290778875350952, "[FF] Collector Arrays of the Solar Wind Concentrator = Deployed from the SRC (Sample Return Capsule) which faces the sun"]
-[8.79908275604248, 0.5086292028427124, "[TT] Descent Speed of the MASCOT = Slower than an earthly pedestrian"]
-[9.030526161193848, 3.503929376602173, "[TT] Arc Duration of the High-voltage solar array = 3 hours"]
-[6.927191257476807, 2.274482011795044, "[TT] Mission Type of the Biomass = EO"]
-[9.966156959533691, -1.4414883852005005, "[TT] Orbit Inclinations of the Constellations = Different"]
-[7.838148593902588, 3.7312240600585938, "[FF] Instrument Type of the MITA = Other, Atmospheric chemistry, Communications, Data collection, Gravity instruments, Lightning sensors"]
-[6.920759201049805, 1.0629600286483765, "[TT] Launch Date of the Mars Hope probe = February 2021"]
-[6.087001800537109, -0.0740453228354454, "[FF] Design Life of the FormoSat-2 = 5 years"]
-[8.968681335449219, 5.619386196136475, "[TT] Sensor Read Noise of the Sensor = 2.48 ADU"]
-[8.22211742401123, 0.8032847046852112, "[TT] 2021 Acres Burned of the U.S. Drought Monitor = 124,000 acres"]
-[5.055243968963623, 3.3480677604675293, "[TT] Manufacturer of the OPTSAT 3000 = IAI"]
-[13.227185249328613, 5.221242427825928, "[TT] Area of the Solar Panels = 14.5 m2"]
-[8.486480712890625, 1.7189456224441528, "[TT] Spatial Resolution (km) of the Integrated water vapor = 25"]
-[4.731449604034424, -1.1915596723556519, "[TT] Based on of the Beijing-3B = Beijing-3A"]
-[5.490532398223877, 1.2434165477752686, "[FF] Presentation Date of the INDEX (REIMEI) = Sept. 24-28, 2007"]
-[7.994917392730713, -0.052537962794303894, "[FF] Purpose of the GRACE-FO = Measure the mass loss of glaciers and ice sheets"]
-[9.22227954864502, 5.6083807945251465, "[FF] Function of the Image Motion Compensation Mirror = Compensate for the satellite's orbital motion"]
-[12.365713119506836, 7.537899494171143, "[TT] Power Supply of the LinkSprite JPEG color VGA camera = 3.3 -5 V"]
-[12.0291748046875, 3.044684648513794, "[FF] Propulsion System of the Clementine = Non-propellant hydrazine system for attitude control"]
-[5.555636405944824, 0.5543028712272644, "[TT] Observation Period of the STEREO-A = May 25 \u2013 June 1"]
-[10.354345321655273, 5.666767120361328, "[TT] Thermal Survival Range of the Instrument = -50 / +40\u00baC"]
-[4.9401164054870605, 3.3191041946411133, "[TT] Manufacturer of the EFP = Utah State University"]
-[4.442490100860596, 2.7414379119873047, "[TT] Development Location of the CuPID = Goddard and Wallops Flight Facility on Wallops Island, Virginia"]
-[12.421623229980469, 0.6234549283981323, "[TT] Telescope and Camera System of the PLATO = 34 separate small telescopes and cameras"]
-[11.393009185791016, 4.435660362243652, "[TT] Size of the Wren = 1U"]
-[3.8715479373931885, 6.477923393249512, "[TT] Antenna Angle of the SWOT = \u00b1 60\u00ba"]
-[10.177423477172852, 5.353195667266846, "[FF] Function of the PHCE = Controls other heaters"]
-[5.0364089012146, 3.375309944152832, "[TT] Manufacturer of the FPA = e2v (UK)"]
-[5.027257442474365, 8.369037628173828, "[TT] Bands of the MWRI-RM = 54, 118 and 183 GHz"]
-[11.718884468078613, 6.727863788604736, "[TT] Energy Range of the EPIC Cameras = 0.15 to 15 keV"]
-[6.896646022796631, 6.543124675750732, "[TT] Operation Time of the Spectrometer = 12 minutes per occultation (limb observations)"]
-[10.144339561462402, 5.421752452850342, "[FF] Aim of the Structural & Thermal Model (S/C STM) = Qualification with respect to environmental requirements relevant to the spacecraft structure and the thermal control system"]
-[8.847426414489746, 4.6590471267700195, "[FF] Primary Attitude Determination of the Star Tracker = Method"]
-[10.439105987548828, 5.7796125411987305, "[TT] Operating Temperature Range of the Integrated Mobile Station = -30\u00baC to 45\u00baC"]
-[9.865849494934082, 0.604610025882721, "[FF] Activation Distance of the LIRIS = 3500 m from the Space Station"]
-[6.234753608703613, 2.4710023403167725, "[TT] Location of the CARMENES spectrographs = Calar Alto Observatory (Almeria, Spain)"]
-[5.649538040161133, 4.290721893310547, "[FF] Program Name of the Satellite for 5G = Satellite for 5G (S45G)"]
-[6.341351509094238, 7.379953861236572, "[TT] Repetition Rate of the MABEL = Variable (between 5 and 25 kHz)"]
-[8.609859466552734, 7.149080276489258, "[TT] Instrument Banks of the SLIM6 = 2"]
-[5.694452285766602, 7.134790420532227, "[TT] Data Rate of the PAD = 4.0 Mbit/s"]
-[8.355525970458984, 8.321074485778809, "[TT] Spectral Range of the MicrOmega/MASCOT = 0.9 to 3.5 \u00b5m"]
-[8.506407737731934, 8.637392044067383, "[TT] Magnification of the Prism Spectrometer = 1:1"]
-[8.808124542236328, 0.02771957777440548, "[TT] Sampling Latitude Range of the OSIRIS-REx = 85\u00ba North to 85\u00ba South"]
-[6.617217063903809, 1.6656540632247925, "[FF] Propulsion System Contract Date of the Skybox Imaging = Jan. 15, 2013"]
-[11.681132316589355, 3.194883346557617, "[TT] Number of Attitude Control Thrusters of the GN2 Reaction Control System = 12"]
-[6.101052761077881, 5.628885269165039, "[TT] FPGA of the CCM = Microsemi RTAX"]
-[7.142180442810059, 2.7638509273529053, "[TT] Launch Date of the MethaneSAT = 2023"]
-[5.292839050292969, 7.1483378410339355, "[TT] Downlink Baud Rate of the CMC Transceiver = 9600 baud"]
-[8.067521095275879, 6.447991847991943, "[FF] Data Collection of the Advanced Baseline Imager (ABI) = Information collected by the Advanced Baseline Imager (ABI)"]
-[13.83390998840332, 3.3550896644592285, "[TT] Mass of the NovAtel OEMV-2 L1/L2-F GPS unit = 56 g"]
-[7.97611141204834, 8.13715934753418, "[TT] Spectral Band of the Band Photometers = 650-740 nm"]
-[6.92818021774292, 1.6064682006835938, "[FF] Payload of the Ariane 5 = NASA\u2019s space telescope, James Webb"]
-[7.335478782653809, 4.598632335662842, "[FF] Behavior of the SAA = Gradually weakening"]
-[8.628951072692871, 3.6097500324249268, "[FF] Objective of the TSIS = Acquire measurements of total and spectral solar irradiance"]
-[7.71722412109375, 6.534817218780518, "[TT] Fast Imaging Time of the AMI = Within 10 minutes for FD (Full Disk) observations"]
-[7.682292461395264, 3.1491801738739014, "[FF] Payloads of the FY-3E = Microwave and infrared sounders, instrument to derive atmospheric conditions and ocean winds, spectral imager"]
-[6.868228912353516, 7.469377040863037, "[TT] ADC Resolution of the SEVIRI = 12 bit"]
-[10.280259132385254, 7.998024940490723, "[TT] Telescope Aperture of the QuickBird-2 = 60 cm \u00d8"]
-[5.46852970123291, 6.348769664764404, "[TT] Data Capacity of the SB = 64 Gbit"]
-[9.752676010131836, -0.4218568503856659, "[TT] Altitude of the SARAL spacecraft = ~800 km"]
-[7.861595630645752, 2.6528139114379883, "[FF] Monitoring of the ISS LIS = Occurrence and changes in extreme storms"]
-[7.554197311401367, 4.645827770233154, "[FF] Inspection Cone Angle of the RVX = Limited to meet non-cooperative VBS constraints"]
-[8.334132194519043, -0.43091681599617004, "[TT] Measurement of the Sea Ice Extent = 2.04 million square miles"]
-[7.026706695556641, 2.06894850730896, "[FF] URL of the NASA Satellite = http://www.nasa.gov/press-release/nasa-satellite-finds-unreported-sources-of-toxic-air-pollution"]
-[7.249995708465576, 3.3689351081848145, "[FF] Operation of the Cryogen servicing tool = Uses a hose to connect the tank filled with liquid methane to the empty tank"]
-[4.937864780426025, 0.49978551268577576, "[TT] Clock 2 Anomaly Date of the QZS-1 = Dec. 19, 2012"]
-[12.381475448608398, 0.601068377494812, "[TT] Consortium Size of the PLATO = More than 350 scientists and engineers"]
-[10.178279876708984, 8.258974075317383, "[TT] Telescope Aperture of the IRIS = 20 cm"]
-[7.699711322784424, 8.540960311889648, "[TT] Spectral Bands of the WFI = VIS to NIR"]
-[4.595736980438232, 1.6507368087768555, "[TT] XCO2 Maps Date of the TanSat = April and July 2017"]
-[2.330186605453491, 1.3075217008590698, "[TT] Mission Duration of the NanoSail-D2 = 70 and 120 days"]
-[5.403591632843018, 0.2693338096141815, "[TT] Landing Time of the Space Shuttle Endeavour = June 1, 2011, at 6:35 GMT"]
-[8.771476745605469, -0.14263293147087097, "[TT] Perigee of the Chang'e-2 = 200 km"]
-[9.948675155639648, 8.928786277770996, "[TT] Parameter of the IFOV = 1.25 mrad (or 1 km at nadir) for 28 bands 0.3125 mrad (or 250 m at nadir) for 6 bands"]
-[4.178640365600586, 7.1760478019714355, "[TT] Communication Bands of the KOMPSAT-3 = S-band, X-band"]
-[8.021958351135254, 8.381250381469727, "[FF] Spectrum of the Imaging Spectrometer = Short-wave infrared (SWIR)"]
-[8.267833709716797, 7.28484582901001, "[FF] Gain Control of the MCP (Microchannel Plate) Detector = Voltage applied to the front surface"]
-[6.631199359893799, 2.853261709213257, "[FF] Purpose of the CBPSS = Support scientific progress in space research in the biological, medical, and physical sciences"]
-[13.606467247009277, 2.8409383296966553, "[TT] Total Allowable Mass of the Supernova-Beta = 12 kg"]
-[3.784546375274658, 6.658121585845947, "[TT] VDES Antenna Operating Band of the NorSat-2 = VHF maritime band"]
-[6.462070465087891, 4.063043117523193, "[FF] Segments of the MANTIS = Space, Ground, User and Launch"]
-[6.903891086578369, -0.32561013102531433, "[FF] Importance of Temporal Domain of the SVOM = Recognized in recent reports by the Chinese Space and Technology Roadmap, the European Union ASTRONET group and the USA National Research Council Decadal Survey"]
-[8.169574737548828, 5.791498184204102, "[FF] Challenge of the DarkCarb image sensor = Wavelengths to which it is sensitive are emitted by all objects that are at the Earth\u2019s temperature"]
-[5.6402997970581055, -0.18016700446605682, "[TT] Expected Mission Duration of the RapidEye = Through 2020"]
-[9.953189849853516, 8.199873924255371, "[TT] Aperture of the NUV & VIS Channels = ~380 mm"]
-[9.1467924118042, 5.620532512664795, "[TT] Jitter performance of the DST 35 = 0.185 arcmin/s"]
-[4.900156497955322, 7.330698490142822, "[TT] BER (Bit Error Rate) of the S-band Transmitter = 10 -5"]
-[5.576891899108887, 5.32274866104126, "[TT] Network Communication of the COSMOS Software = IPV4 UDP packets"]
-[10.940340995788574, 2.0750558376312256, "[FF] Article URL of the XMM-Newton = https://doi.org/10.1051/0004-6361/201832664"]
-[11.91050910949707, 6.789833068847656, "[TT] Output Voltage of the High Voltage Power Supplies = Fixed (adjustable) bias voltages for the MCP detectors"]
-[10.371997833251953, 2.1321332454681396, "[TT] Energy Measurement Accuracy of the eROSITA X-ray telescope = 2% - 6%"]
-[10.732165336608887, 0.9011886119842529, "[TT] Type of the Kepler-1658b = Hot Jupiter-like planet"]
-[8.066661834716797, 4.462306022644043, "[TT] Type of the LRA (Laser Retroreflector Array) = Precision orbit"]
-[7.844093322753906, -0.8044919371604919, "[FF] Collaboration of the IceBridge Plane = ESA\u2019s CryoSat-2 and the European Union\u2019s Sentinel-3 satellites"]
-[7.940577983856201, 6.306302547454834, "[TT] Type of the DCS = Imaging multi-spectral radiometers (vis/IR)"]
-[8.521156311035156, 6.235598564147949, "[TT] Measurement Range of the VMAG = 100-10000 nT"]
-[4.121368885040283, 2.007101058959961, "[TT] Launch Provider of the SOCRATES = MHI (Mitsubishi Heavy Industries, Ltd.)"]
-[6.770747184753418, 4.8985276222229, "[FF] Tracking and Cataloging of the CSpOC = Immediate"]
-[9.469179153442383, 3.632681131362915, "[FF] Magnetization Dominance of the Vertically-integrated magnetization model = Areas of negative magnetization are dominated by magnetizations in directions oblique and opposite to that of the present Earth's field"]
-[4.870143413543701, 8.348762512207031, "[TT] Frequency Range of the MTVZA-GY = 10-48 GHz"]
-[9.375532150268555, 4.725358963012695, "[TT] Attitude Control System of the F-15 and F-16 DMSP satellites = Advanced"]
-[12.455559730529785, 0.5853434801101685, "[TT] Observation Duration of the PLATO = One to two years"]
-[7.076967239379883, 3.764162540435791, "[FF] Formation Flying Technology Demonstration of the PROBA-3 = In Flight"]
-[4.621494770050049, 0.4833917021751404, "[TT] Integration Date of the SpIRIT = 2022"]
-[13.641071319580078, 3.0321602821350098, "[TT] Payload of the Solar Orbiter = 180 kg"]
-[10.471641540527344, 1.8218042850494385, "[TT] Spectrum of the Swift J0042.6+4112 = Very similar to known pulsars in the Milky Way"]
-[12.135080337524414, 1.969361424446106, "[FF] DEM Extraction of the CartoSat-1 = Not Available"]
-[6.455755233764648, 5.794085502624512, "[FF] Number of Products of the EnMAP = 3 + 1 internal product"]
-[8.63378620147705, 0.1472954899072647, "[TT] Boulder Strength of the Comet 67P/C-G = One hundred times weaker than freshly packed snow"]
-[13.742206573486328, 3.808286190032959, "[TT] Mass of the Reflector Mesh = < 0.5 kg"]
-[6.337480545043945, 4.52961540222168, "[TT] Development Tool of the ACS = Matlab/Simulink"]
-[9.430444717407227, 3.8353936672210693, "[FF] Readings of the Magnetometer = Unknown"]
-[6.017584800720215, 0.8365575671195984, "[FF] Image Capture Date of the DESIS = 29 November 2019"]
-[4.171297073364258, 7.732082366943359, "[TT] Modulation Technique of the LCS = IM/DD (Intensity Modulation / Direct Detection)"]
-[8.135920524597168, 3.079998016357422, "[FF] Purpose of the ASIM = Shed more light on the lightning phenomena"]
-[6.525776386260986, -0.10215282440185547, "[TT] Observation Time of the ILAS = 10 minutes per occultation"]
-[4.048335075378418, 6.720846652984619, "[FF] Quantity of the Antenna = 2 fixed X-band Low Gain, 1 steerable K-band High Gain, 1 steerable X-band Low Gain"]
-[10.040900230407715, 2.952934980392456, "[FF] Launch Date of the QB50-ISS CubeSats = Dec. 9, 2016"]
-[5.883245944976807, 2.049389362335205, "[FF] Utilization of the Columbus Laboratory = By the European Union"]
-[4.964745044708252, 0.4259903132915497, "[TT] Launch Date of the VRSS-1 = September 29, 2012"]
-[8.733482360839844, 6.453512191772461, "[TT] Echo Samples Spacing of the ALT = 3.125 ns"]
-[9.137469291687012, 7.0119428634643555, "[TT] Multitemporal Registration of the VSSC = Better than 3 m"]
-[6.6947102546691895, 2.367457628250122, "[FF] Data Sheet URL of the ADIS16250_16255 = http://www.analog.com/static/imported-files/data_sheets/ADIS16250_16255.pdf"]
-[4.807175636291504, -0.030703766271471977, "[TT] End of Life Date of the ZACUBE-2 = 27 Dec 2022"]
-[7.052062511444092, 3.5109500885009766, "[FF] URL of the PROBA-3 = http://www.esa.int/Our_Activities/Technology/Proba_Missions/About_Proba-3"]
-[4.979930400848389, 1.17341947555542, "[TT] Launch Date of the INSAT-3DR = Sep 9, 2016"]
-[5.405113697052002, 5.645195007324219, "[TT] Onboard Data Recording of the RADARSAT-1 = Tape recorder (analog)"]
-[5.741896629333496, 7.376175403594971, "[TT] Telemetry Bit Rates of the MPO-MAG instrument = 64, 32, 16, 8, 4, 2, 1, and 0.5 Hz"]
-[7.506248950958252, 5.6790924072265625, "[FF] Payload Data of the ASAP = High-resolution image data, in the order of 100 MB/day"]
-[8.573132514953613, 6.722183704376221, "[TT] Monitoring Frequency of the OSIRIS Narrow Angle and Wide Angle Cameras = Weekly"]
-[8.710763931274414, 3.9623005390167236, "[FF] Measurement of the PHA = Spectrum of ionizing particle energy, charge, and mass"]
-[10.44935131072998, 5.978890895843506, "[TT] Brigthness Temperature (BT) Sensitivity of the Antenna = \u00b10.42 K"]
-[11.440047264099121, 5.822345733642578, "[FF] Material of the Antenna structure = Aluminum honeycomb"]
-[8.953946113586426, 8.572225570678711, "[TT] Spectral Line of the Deployable Membrane Telescope = Hydrogen-alpha spectral line of 656.46 nm"]
-[13.360494613647461, 7.351995468139648, "[TT] Power of the RPU = 36 W"]
-[4.818836212158203, 8.06484603881836, "[TT] Frequencies of the DORIS = 400 MHz and 2 GHz"]
-[11.040017127990723, 4.6441874504089355, "[FF] Current Flow of the Electrodynamic Tether = Determines if the interaction contributes to drag or to propulsion"]
-[8.861992835998535, 0.858374834060669, "[FF] Purpose of the ARTEMIS probes = Monitor solar wind input at lunar distances sunward of Earth or provide observations of plasma structures when crossing through the Earth magnetotail at lunar distances once per lunar cycle"]
-[4.619941234588623, 7.078124523162842, "[TT] Signal Format of the Downlink = NRZ (Non-Return Zero)"]
-[6.492183685302734, 4.918351650238037, "[FF] ACS Parameters of the MarCO = Working for both TCMs and flight"]
-[6.172872543334961, 4.185105323791504, "[FF] Architecture of the COSMOS = Provides a number of software tools to serve well defined operational roles and applications"]
-[5.841405391693115, -0.7737709283828735, "[TT] Satellite lifetime of the SkySat = <<5 years"]
-[9.805387496948242, -0.577415406703949, "[TT] Altitude in Orbit of the Electric Thruster = 410 km"]
-[9.278670310974121, 6.827545166015625, "[TT] Planned Image Resolution Improvement of the Satellite Constellation = 70 centimeters"]
-[5.510859966278076, 2.4361391067504883, "[FF] Country of the LAPAN-A3/IPB = Republic of Indonesia"]
-[4.78827428817749, 5.352136135101318, "[FF] Function of the AMU = Emits a high-power beacon that enables target acquisition at far range with Earth in the background of CSC"]
-[5.147202491760254, 2.29563307762146, "[TT] Mission Type of the Arachne = Non-EO"]
-[7.821900844573975, 2.5644702911376953, "[FF] Image Detail of the TEMPEST-D = Similar to existing weather satellites"]
-[4.52028751373291, 1.9654161930084229, "[TT] Launch Date of the NorSat-2 = July 2017"]
-[2.9621968269348145, 2.3769466876983643, "[FF] Monitoring of the Copernicus Sentinel-4 and Sentinel-5 = Key air quality trace gases, stratospheric ozone, and aerosols"]
-[7.480490684509277, 3.7761476039886475, "[FF] Tracking Device of the NightPod = Accommodates commercial optical cameras"]
-[9.41183853149414, 6.573855400085449, "[TT] Step Size of the Scan Mirror = 1120 \u00b5rad"]
-[4.418733596801758, 0.6359975934028625, "[TT] Launch Date of the DMSP-F13 = March 1995"]
-[10.54815673828125, 3.9972808361053467, "[FF] Mechanism of the Dragsail = Mechanical two stage ejector, extension mechanism with four booms rolled into a central distributor"]
-[9.299687385559082, 5.065989017486572, "[TT] Attitude Control Accuracy of the BRITE spacecraft = better than 1.0\u00ba"]
-[6.854084491729736, 5.63856840133667, "[FF] Data Processing of the Delay/Doppler Altimeter = Unknown"]
-[8.270155906677246, 2.079002618789673, "[TT] Cloud Profiling Signal Attenuation of the CloudSat = From the surface to 5-6 km"]
-[5.011097431182861, 3.3661394119262695, "[TT] Manufacturer of the NewSat-6 = Satellogic S.A."]
-[7.84343957901001, 3.0186424255371094, "[FF] Background Concentration of the CO2 = 415 ppm"]
-[8.955510139465332, 4.860588550567627, "[TT] Number of Piezoelectric Sensors of the IS = 5"]
-[5.562808036804199, 3.8467612266540527, "[TT] Expected Number of Connected Devices by 2025 of the Satellite IoT Market = Surpass 30 million"]
-[6.074230670928955, -0.07508327811956406, "[TT] Peak Manufacturing Rate of the SSTL-300 S1 = 4 units per year"]
-[7.218488693237305, 7.527579307556152, "[TT] Radiometric Resolution of the Optoelectronic System = 8 bit"]
-[8.003294944763184, 8.585348129272461, "[TT] Performance Range of the VIS = 365 - 500 nm"]
-[3.6692285537719727, 4.970602035522461, "[TT] Spotlight Mode Resolution of the RADARSAT-2 = Better than one meter in azimuth"]
-[7.167915344238281, 1.2782624959945679, "[FF] Transfer Method of the Orbiting Sample (OS) = STA will transfer the sample tubes into the Orbiting Sample (OS)"]
-[3.3374829292297363, 4.969977378845215, "[FF] 3-D Structure Mode of the Tandem-L = Fully-polarimetric SAR interferometry"]
-[4.948051452636719, 7.3536272048950195, "[TT] Uplink Data Rate of the RF Communications = 9.6 kbit/s"]
-[7.734588623046875, 2.5323891639709473, "[FF] Purpose of the Nimbus-7 = Testing of advanced systems for sensing and collecting data in the atmospheric, oceanographic and meteorological disciplines"]
-[3.871907949447632, 7.879459381103516, "[TT] Modulation Type of the Modulation scheme = 16QAM, QPSK"]
-[8.614835739135742, 1.0894811153411865, "[TT] Range of measurements of the Land = Up to 1.5 m"]
-[3.831749439239502, 7.903993606567383, "[TT] Modulation of the X-band Transmitter = BPSK or QPSK"]
-[5.67418098449707, 6.136013031005859, "[FF] Data Storage of the Mikulski Archive for Space Telescopes = Raw and processed data"]
-[11.931920051574707, 3.0637221336364746, "[TT] \u0394V Savings of the KPLO = About 165 m/s"]
-[4.359376430511475, 3.3073294162750244, "[TT] Ground Station Location of the TanDEM-X = Neustrelitz, Germany"]
-[10.016773223876953, -1.5220112800598145, "[TT] Inclination of the Science Orbit = 77.6\u00ba"]
-[10.736471176147461, 5.561825275421143, "[TT] Design of the TEMBOTM EMC = Elastic Memory Composite"]
-[7.929739475250244, 7.92821741104126, "[TT] Quantum Efficiency of the HSC-III optics subsystem = 0.36 @ 620 nm"]
-[10.375062942504883, 2.3105854988098145, "[TT] Quantity of Telescopes of the Imaging X-ray Polarimetry Explorer (IXPE) = 3"]
-[9.143556594848633, 7.4994611740112305, "[TT] Spatial Resolution of the Panchromatic Wide-Scan Camera = 2-8 m"]
-[11.717552185058594, 4.621667861938477, "[TT] Dimensions of the Atlantic Basin Facility = 75 m long 9 m wide"]
-[9.775270462036133, -0.6114377379417419, "[TT] Orbit Altitude of the MicroMAS-2a = 550 km"]
-[7.300379276275635, 9.135388374328613, "[TT] Filter Wavelength of the ISUAL instrument = 427.8 nm"]
-[10.832380294799805, 3.921238422393799, "[TT] Drag Sails Deployment Date of the CanX-7 = May 3, 2017"]
-[3.1715543270111084, 4.388157367706299, "[TT] Interferometry Mode of the TerraSAR-X = ATI (Along Track Interferometric) mode"]
-[6.44331693649292, -0.2286261022090912, "[TT] Delivery Frequency of the SpinKF = Daily"]
-[5.21215295791626, 6.483402729034424, "[TT] Storage Capacity of the Spacecraft 406 MHz Processor = 324 kbit"]
-[8.506680488586426, 8.046778678894043, "[TT] Number of Pixels of the Band 4 = 800"]
-[8.262879371643066, 8.740180969238281, "[TT] Imaging Wavelength of the PROBA-2 = Extreme ultraviolet"]
-[5.946308135986328, 7.102327346801758, "[TT] Source Data Rate of the Instrument = ~600 kbit/s"]
-[7.318382740020752, 9.152560234069824, "[TT] Wavelength Range of the Wide Band Filter = 540 nm \u2013 590 nm"]
-[11.738025665283203, 7.532121181488037, "[TT] Launch Date of the Megha-Tropiques = 12 Oct 2011"]
-[7.940367698669434, 2.0588417053222656, "[FF] Data Distribution of the SeaSat = Real-time weather data"]
-[10.426615715026855, 1.554180383682251, "[FF] Transit of the KELT-9 b = Begins near the star's bright poles and then blocks less and less light as it travels over the star's dimmer equator"]
-[7.967855930328369, 2.838658571243286, "[FF] Function of the CAPI = Compensate the CO2 measurement errors by high-resolution measurement of cloud and aerosol"]
-[5.08521842956543, 5.200326919555664, "[TT] Channels of the GPS receiver = 24 channels"]
-[9.82375717163086, 4.131028652191162, "[FF] Cirrus Cloud Properties of the POLDER-1/ADEOS = Derived"]
-[8.044673919677734, 6.061398506164551, "[FF] Advanced Baseline Imager (ABI) of the GOES-18 = Captured stunning views of Earth"]
-[14.065787315368652, 4.035688877105713, "[TT] Mass of the Instrument = 96 kg"]
-[7.397782802581787, 0.27529197931289673, "[FF] Purpose of the OSIRIS-REx = Measure the Yarkovsky effect"]
-[8.178544998168945, 7.149260520935059, "[TT] Image Sequence Specification of the COR1 = 3 white light images at 3 different polarization angles"]
-[6.930276870727539, 4.738887786865234, "[FF] Data of the CHAMP = +16"]
-[7.884466648101807, 2.6478159427642822, "[FF] Complementary Instrument of the CloudSat = PARASOL (POLDER) complements CALIPSO (Lidar) and NASA's Aqua and Aura (MODIS, CERES) missions, it also makes use of the CloudSat (CPR) radar data"]
-[9.283066749572754, 1.7711139917373657, "[TT] Speed of the Harpoon = 20 m/s"]
-[11.128000259399414, 4.066338062286377, "[TT] Sail Material Surface Area Reduction of the DSAT-1 = 25%"]
-[10.107044219970703, -1.54916250705719, "[TT] Orbital Inclination of the DMSP Satellites = 98.7\u00b0"]
-[5.704723358154297, 4.205805778503418, "[FF] Purpose of the Hiber = Track and monitor machines and devices for a wide range of IoT solutions in some of the world's hardest-to-reach places"]
-[10.797286033630371, 2.137380599975586, "[FF] Principal Investigator of the XMM Newton = Nanda Rea"]
-[11.479732513427734, 6.443354606628418, "[TT] Energy Band of the NuSTAR Optics = 6-79 keV"]
-[7.115405082702637, 5.837655544281006, "[FF] Functionality of the NTP = Maintain the processor clock and provide accurate time stamps"]
-[9.241045951843262, -0.41063791513442993, "[TT] Apogee of the Satellite = 257 km"]
-[14.310857772827148, 2.7757046222686768, "[TT] Mass of the KOMPSAT-5 = 1400 kg"]
-[8.686543464660645, 7.146064758300781, "[TT] Camera Type of the GF-2 = PAN/MS"]
-[13.381559371948242, 7.344610691070557, "[TT] Power of the Power = 0.5 W"]
-[8.1949462890625, 0.09067536890506744, "[TT] Launch Date of the Meteor-3-1 = 24.10.1985"]
-[5.991565227508545, 4.945810317993164, "[FF] Purpose of the LPT/CANDOS = Supporting communications and/or navigation functions of mission applications"]
-[8.03303337097168, 8.604552268981934, "[TT] Spectral Range of the SWIR Spectrometer = 900 nm to 2450 nm"]
-[4.607990741729736, 0.5009160041809082, "[TT] Launch Date of the GOES-U = 2024"]
-[6.818759441375732, 4.448965072631836, "[FF] Unknown of the DSX = Unknown"]
-[10.400303840637207, 2.145423650741577, "[FF] Travel Path of the X-ray emission = Towards us through dusty regions of our Galaxy"]
-[8.109450340270996, -1.025445818901062, "[FF] Measurement of the ICESat-2 = Height of Earth\u2019s surfaces"]
-[6.417530536651611, 1.0618109703063965, "[FF] Image of Los Angeles 1 of the ASTERIA = 16 May 2019"]
-[9.669864654541016, 5.522607326507568, "[TT] Orientation Requirement of the Radiator = Oriented on cold, deep space"]
-[10.759644508361816, 3.497081756591797, "[TT] CubeSat Size of the FITSat-1 = 1U"]
-[13.465429306030273, 7.306814193725586, "[TT] Maximum Current of the ArgUS = 5 A"]
-[7.537040710449219, 8.06551742553711, "[FF] Polarisation Effects of the CCRs = Reduces the intensity of the central peak of the Airy pattern by approximately a factor of four"]
-[10.287909507751465, 2.3479323387145996, "[FF] Objective of the CXBN = Make precise measurements of the cosmic X-ray background in the 30-50 keV range"]
-[7.426175117492676, 6.094641208648682, "[FF] Objectives of the SLA sensor package = In-space engineering testbed for future spaceborne laser altimeters, acquire samples of land topography and vegetation data, measure cloud and aerosol layers in the atmosphere"]
-[9.269697189331055, 5.111719608306885, "[TT] Pointing Stability of the TanSat = \u2264 0.001\u00ba/s"]
-[9.53309440612793, 0.954840362071991, "[TT] Speed of the Rosetta = 31 000 km/h"]
-[6.398325443267822, 1.0392863750457764, "[FF] Mission Status of the FormoSat-7 / COSMIC-2 = Unknown"]
-[6.992947578430176, -0.729637086391449, "[TT] Orbital Period of the Kepler-186f = 130 days"]
-[4.475991725921631, 0.11289115250110626, "[FF] Travel Date of the Smile = 16 March 2022"]
-[11.259013175964355, 4.152848243713379, "[TT] Inflatable Mast Length of the Spacecraft = 1 m"]
-[10.955845832824707, 6.3683247566223145, "[TT] Folding Mirror Material of the NAOMI = SiC"]
-[6.696969985961914, 3.841040849685669, "[FF] Alert Production of the Ground Software = Produce and distribute alerts to the world-wide astronomical community"]
-[12.048016548156738, -0.3285509943962097, "[TT] Age of the TESS = 120 million years"]
-[9.435312271118164, 0.9751251935958862, "[TT] Closest Approach Time of the New Horizons spacecraft = 10:29 a.m. EST"]
-[11.640324592590332, 4.702270030975342, "[TT] Diameter of the Secondary Body = 160 m"]
-[5.237929344177246, 0.9928402900695801, "[TT] First Measurement Date of the Poseidon-1 instrument = 21 August 1992"]
-[11.006512641906738, 7.579178810119629, "[TT] Swath Width of the MSU-MR = 2800 km"]
-[5.312984943389893, 0.4334574341773987, "[FF] Debut Flight Date of the Rail-guided space launcher = October"]
-[6.099265098571777, 2.3005707263946533, "[FF] Mission Status of the Orion MPCV = Unknown"]
-[9.589956283569336, 3.7290146350860596, "[TT] Typical Magnetic Field Strength of the Sunspot = 3,000 gauss"]
-[9.036317825317383, 7.330432415008545, "[TT] Image Resolution of the EXI = 12 megapixels"]
-[7.05363130569458, 6.9997382164001465, "[TT] Size of the LISA Laser Prototype = About half the volume of a typical shoe box"]
-[7.660876274108887, 5.677325248718262, "[FF] Sensor Types of the VBN = Standard camera, flash imaging LiDAR"]
-[14.289538383483887, 6.87470817565918, "[TT] Battery Voltage of the SBVR = 55 to 96 V"]
-[9.970412254333496, 5.603574275970459, "[TT] Decenter of the M3 = 20 \u00b5m"]
-[5.252895832061768, 2.2668986320495605, "[FF] Mission Type of the MITA = EO"]
-[10.13334846496582, 8.10041332244873, "[TT] Focal Length of the Telescope = 12 cm"]
-[11.409132957458496, 4.3431854248046875, "[TT] Size of the ICE-Cap = 3U"]
-[4.762510299682617, 0.2827839255332947, "[TT] Launch Date of the RemoveDebris = Q3 2016"]
-[8.106637001037598, 2.5231258869171143, "[FF] Mission Objective of the Terra = Obtain information about the physical and radiative properties of clouds, air-land and air-sea exchanges of energy, carbon, and water, measurements of trace gases, and volcanology"]
-[7.286039352416992, 5.764967918395996, "[FF] Flashes Measurement of the Tatiana-2 = More than 1000"]
-[10.201129913330078, 8.414432525634766, "[TT] Pupil Diameter for LR of the Instrument = 36.1 mm"]
-[6.5888590812683105, 3.628537178039551, "[FF] Development Status of the PROBA-V plus one = In the process of developing"]
-[6.0753607749938965, -0.3385680317878723, "[TT] Operation Duration of the Experiments = 1 year to 3 years"]
-[10.87094497680664, 3.7168796062469482, "[FF] URL of the Electric Solar Wind Sail (E-sail) = http://www.electric-sailing.com/"]
-[10.945904731750488, 7.504842758178711, "[TT] Swath Width of the EOS = 12 km"]
-[3.6792585849761963, -1.0408751964569092, "[TT] Orbit Stability of the EQUULEUS = Quasi-periodic"]
-[8.80678653717041, 1.0062071084976196, "[FF] URL of the Parker Solar Probe = https://blogs.nasa.gov/parkersolarprobe/2021/11/10/space-dust-presents-opportunities-challenges-as-parker-solar-probe-speeds-back-toward-the-sun/"]
-[4.375288009643555, 7.777116775512695, "[TT] Uplink Frequency of the TT&C = 2.0 GHz"]
-[8.598440170288086, 5.577544689178467, "[TT] Time Error of the GPSR = < 0.2 \u00b5s (1\u03c3)"]
-[14.33425235748291, 2.7958528995513916, "[TT] Mass of the KOMPSAT-2 = 770 kg"]
-[8.566900253295898, 5.937515735626221, "[TT] Accuracy of the CTECS-A = 10-20 m"]
-[8.387650489807129, 6.246290683746338, "[FF] Observation Capabilities of the TWINS = 3D spatial, energy, and pitch angle distributions of the terrestrial ring current (RC)"]
-[6.727180004119873, 1.9381717443466187, "[FF] Survey Date of the Nancy Grace Roman Space Telescope = March 22, 2022"]
-[7.8978962898254395, 8.604156494140625, "[TT] Spectral Range of the ELVIS = 200-650 nm"]
-[8.284067153930664, 0.4417373538017273, "[FF] Elevation of the Lake Powell = Around 1120 m"]
-[5.063102722167969, 0.7474972605705261, "[FF] Launch Date of the ZACUBE-01 = Unknown"]
-[8.092850685119629, 0.7990583777427673, "[TT] Lowest Water Storage Levels Timeframe of the Turkey = 15 years"]
-[6.569304943084717, 4.988001823425293, "[FF] Selects the interesting opportunities to execute links during increment N of the LCT Operations Team = The LCT Operations Team at TES selects the interesting opportunities to execute links during increment N"]
-[7.586806297302246, 1.8246620893478394, "[FF] Coverage of the WatER = Fresh water bodies cover at least 4% of Earth's terrestrial surface"]
-[7.122158050537109, 4.517326354980469, "[FF] Component of the Flight Releasable Grapple Fixture (FRGF) = Unknown"]
-[8.969243049621582, -0.8284808993339539, "[TT] Orbit of the Spacecraft = MEO"]
-[13.777325630187988, 3.6772429943084717, "[TT] Instrument Mass of the SAR Antenna = 350 kg"]
-[7.931050777435303, 9.003716468811035, "[TT] Wavelength of the Sensor = 777.4 nm"]
-[13.668399810791016, 7.101934909820557, "[TT] Capacity of the Power = 70 Ah"]
-[5.731711387634277, 4.179224014282227, "[FF] Purpose of the Challenge One smallsat = Internet of Things"]
-[4.573254585266113, 2.6863853931427, "[FF] Historical Use of the Bran Castle = Often cited as Vlad\u2019s home and as the inspiration for Stoker\u2019s gothic novel"]
-[4.8058648109436035, 1.3905704021453857, "[TT] Launch Date of the G\u00f6kt\u00fcrk-2 = December 2012"]
-[6.714370250701904, 4.49479341506958, "[FF] Structure of the Payload Module = Provides structural support"]
-[6.992565155029297, -0.7916908264160156, "[TT] Orbital Period of the L 98-59c = 3.7 days"]
-[14.260356903076172, 3.240485191345215, "[TT] Mass of the UGATUSat = 30 kg"]
-[8.41413688659668, 1.7104833126068115, "[TT] Ocean Surface Currents Measurement Accuracy of the SAR = \u00b10.2 m/s"]
-[6.248986721038818, 3.9062702655792236, "[TT] Data Sets of the NPOESS = 55 EDRs (Environmental Data Records)"]
-[5.747779846191406, 3.3440449237823486, "[TT] Data Recipient of the GCOM-W and GCOM-C = NOAA"]
-[12.147344589233398, -0.11674514412879944, "[FF] Field of View of the TESS Cameras = Not specified"]
-[7.109088897705078, 7.225818634033203, "[TT] Wavelength of the Laser = 1570 nm"]
-[7.900247573852539, 8.807695388793945, "[TT] Maximum Upper Band Edge of the Pan (WorldView-1) = 900 nm"]
-[4.5837578773498535, 0.6574166417121887, "[TT] Test Campaign Date of the QBITO = May 30-June 3, 2016"]
-[8.313558578491211, -0.49958986043930054, "[FF] Sea Ice Extent of the GCOM-W1 = 19.47 million km2"]
-[3.3960697650909424, 1.4973161220550537, "[TT] Arrival Date of the Sentinel-1B = March 22, 2016"]
-[5.9389328956604, -0.4374098479747772, "[TT] Natural Re-entry Time of the PROBA-3 = About 30 months"]
-[4.967663288116455, 0.5941693186759949, "[TT] Scheduled Lift Off of the EM-1 = November 2018"]
-[3.657616138458252, 4.544370174407959, "[FF] Mission of the RISAT-1 = SAR Imagery"]
-[10.920171737670898, 4.286647796630859, "[FF] Ion Pump of the SU = Used to maintain the vacuum and monitor the level of residual pressure"]
-[4.752327919006348, 0.04877939447760582, "[TT] End of Life Date of the PhoneSat-1 and -2 = 27 April 2013"]
-[6.135684013366699, 4.654346466064453, "[FF] Purpose of the KSU CubeSat = Sending telemetry data and photos from the space to the ground station"]
-[9.361222267150879, 3.931245803833008, "[TT] Electric Field Measurement Range of the Plasma Wave Instrument = 0.5 Hz to 400 kHz"]
-[4.2283525466918945, 2.571894645690918, "[TT] Launch Site of the Falcon 9 = Launch Complex 39A (LC-39A) at NASA\u2019s Kennedy Space Center in Florida"]
-[8.282684326171875, 6.467636585235596, "[FF] Dark Current Source of the Photodiode = Thermal and ionizing radiation effects"]
-[9.165620803833008, 4.595422267913818, "[FF] Attitude Control Parameters of the NuSTAR = Unknown"]
-[5.622956275939941, 6.101014137268066, "[TT] Storage Location of the Processed science data = DAAC located at GSFC"]
-[1.9330921173095703, -0.40473049879074097, "[TT] Data Return of the Van Allen Probes = More than twice the expected"]
-[6.476991653442383, 3.866664171218872, "[FF] Data Products of the PARASOL = Unknown"]
-[9.354147911071777, 6.342382431030273, "[FF] Complementarity of the IMAP-Ultra = Complements the measurements of IMAP-Lo and IMAP-Hi"]
-[9.54455280303955, 8.110406875610352, "[FF] Objective of the APIS = Study the degradation of lenses in the space environment"]
-[7.537349700927734, 3.758908748626709, "[FF] Instrument of the Gravity Satellites = Observations"]
-[8.904159545898438, 4.580071449279785, "[TT] Mode of the XACT = Sun Point"]
-[6.895842552185059, 4.857383728027344, "[FF] Function of the TEDA = Measure the space environment surrounding the S/C"]
-[7.295118808746338, 0.23981231451034546, "[TT] Sample Delivery Date to Earth of the OSIRIS-REx = September 2023"]
-[10.88182258605957, 6.06154727935791, "[TT] Thermal Expansion Coefficient of the Optical Cavity = 3 x 10-8/K"]
-[6.739111423492432, -0.3074452877044678, "[TT] Time Between Observations of the SCIAMACHY = 150 seconds"]
-[10.040264129638672, -1.4847300052642822, "[TT] Inclination of the ICEYE-X10 = 97.4\u00ba"]
-[3.4672961235046387, 1.5976063013076782, "[FF] Mission Date of the Sentinel-2 = Oct. 15-16, 2007"]
-[18.646224975585938, 3.940680742263794, "[TT] NE\u0394T of the 5 = 0.4 K"]
-[13.40422534942627, 5.468178749084473, "[TT] Solar Panels of the ICESat-2 = 4"]
-[6.6618266105651855, 1.9016845226287842, "[FF] URL of the SOLSE/LORE-2 Experiment = http://earthobservatory.nasa.gov/Features/SOLSE/"]
-[5.4213995933532715, 5.896579265594482, "[TT] Power of the STRV-2 DHS = 6 W"]
-[6.275186538696289, 4.173223495483398, "[FF] Components of the GS = Mission management, product generation, product distribution, enterprise management"]
-[10.111242294311523, 4.303898334503174, "[FF] Function of the Release Levers = Release the system"]
-[13.924437522888184, 7.191163539886475, "[TT] Charge Pump Voltage of the Sensor Board = 100 V"]
-[5.601461410522461, -0.3939056396484375, "[TT] Deployment Time of the Kibo module = 14:40 UTC"]
-[9.030573844909668, 8.678510665893555, "[TT] Entrance Slit Dimensions of the Spectrometer = 0.3 mm x 7 mm"]
-[5.105612754821777, 2.370530366897583, "[TT] Mission Type of the Genesis = Non-EO"]
-[5.266436576843262, 7.137119293212891, "[TT] Downlink Speed of the CXS-810C = Up to 2 Mbit/s"]
-[9.131359100341797, 5.677920818328857, "[TT] Jitter of the GOCI Instrument = Less than 10 \u00b5rad"]
-[13.307106971740723, 7.453371047973633, "[TT] Transmission Power of the SSRNI = 8 W"]
-[7.090241432189941, 2.6817870140075684, "[FF] Imaging Mission of the SEOSAT\u2013Ingenio = High-resolution images of Earth's land cover"]
-[3.2452852725982666, 5.682673454284668, "[TT] Area of the SAR Antenna = 23 m2"]
-[6.884416103363037, 9.515867233276367, "[TT] NEDT at 300 K of the Band 5 = 0.5 K"]
-[7.399248123168945, 3.986894130706787, "[FF] Calibration Function of the GMI Radiometer = Constellation precipitation transfer standard"]
-[7.859498977661133, 8.136825561523438, "[TT] Band 1 of the R3 Sensor = Pan"]
-[5.356723785400391, 0.7099310159683228, "[FF] Technical Digest Date of the TIMED = 2003"]
-[6.588340759277344, -2.0439581871032715, "[FF] Mission Start Date of the Jason-1 = May 4, 2012"]
-[8.164100646972656, 5.153463840484619, "[FF] Calibration Method of the ALRad = Three-position Dicke switching method"]
-[10.169922828674316, 5.444460868835449, "[TT] Function of the New Screwdriver Bits = Working on the cooling lines"]
-[10.039711952209473, -1.5355278253555298, "[TT] Orbit Inclination of the SeaSat = 108\u00b0"]
-[4.000943660736084, 2.2060279846191406, "[TT] Launch Vehicle of the Galileo = Ariane 5"]
-[4.576433181762695, 7.168135166168213, "[TT] Ka-band System of the STPSat-6 = Transmit up to 622 Mbit/s"]
-[4.443367004394531, 0.39134499430656433, "[FF] Installation Date of the GMAG = Unknown"]
-[6.75653600692749, 8.454720497131348, "[TT] Spectral Channels of the Alice = 1,024"]
-[13.859128952026367, 3.6865580081939697, "[TT] Full-Scale Unit of the MEMS Cantilever Beam Accelerometers = 5 gram"]
-[9.33169174194336, -0.29242902994155884, "[TT] Perigee of the UK-DMC-2 = ~ 632 km"]
-[6.9439191818237305, 1.9404308795928955, "[TT] Image Credit of the Orbiting Carbon Observatory-2 (OCO-2) = NASA/JPL-Caltech/University of Utah"]
-[9.401909828186035, 6.2080512046813965, "[TT] Incident Angle of the Reflection Diffuser = \u03b8 inc. = 65\u00ba"]
-[5.066405296325684, 8.333612442016602, "[TT] Frequency Bands of the Scanning Radiometer = Near 90 GHz, 118 GHz, 183 GHz, 206 GHz"]
-[8.685189247131348, 4.701048851013184, "[TT] Quantity of the Star Trackers = 2"]
-[4.719109535217285, 0.4751635789871216, "[TT] Launch Date of the GOES-T = March 1"]
-[4.49312686920166, 5.405129909515381, "[FF] Development Standards of the GOMX-3 = ESA-tailored ECSS (European Cooperation for Space Standards) engineering standards and product/quality assurance requirements"]
-[9.69226360321045, 7.164520263671875, "[TT] Spatial Resolution of the Instrument = \u2264 60 m x 50 m"]
-[6.519578456878662, 5.14968204498291, "[FF] Components of the ECSE = Number of switches, several electronic devices, and interfaces to the Sparc processor with the relevant software loaded"]
-[5.419295310974121, 4.1793646812438965, "[TT] Bus Provider and Integrator of the ALTAIR and AQUILA satellites = Millennium"]
-[13.32137680053711, 5.442668437957764, "[TT] Quantity of the Solar Arrays = 2"]
-[7.8406596183776855, 4.116339683532715, "[FF] Drifted Orbit of the ERS-2 = Reference Orbit"]
-[13.84353256225586, 3.081751585006714, "[TT] Mass of the Service Module = 35 ton"]
-[8.488276481628418, 7.535650253295898, "[TT] Detector Elements of the Imager = 8"]
-[8.206646919250488, 6.608035564422607, "[TT] Imaging Capability of the RSI = 8 minutes per orbit"]
-[7.35544490814209, 6.624386310577393, "[TT] Sampling duration of the FTS = 4 s"]
-[10.641016006469727, 8.767133712768555, "[TT] 3 dB Footprint Size of the Channel = 21 x 13 km"]
-[14.257834434509277, 3.1492199897766113, "[TT] Mass of the BILSAT-1 = Around 120 kg"]
-[6.766592979431152, -0.6481102108955383, "[TT] Repeat cycle of the GOSAT-2 = 6 days"]
-[6.688704013824463, -0.39021551609039307, "[TT] Period of the Satellite = 103 minutes"]
-[5.008492469787598, 0.43355825543403625, "[FF] Launch Date of the QZS-3 = June 16, 2017"]
-[5.4942626953125, 1.8134770393371582, "[TT] Mission Concept Review Completion Date of the ABEX = Spring of 2021"]
-[9.976372718811035, -0.5009921193122864, "[TT] Altitude of the PeruSat-1 = 695 km"]
-[4.770297050476074, 0.25542980432510376, "[TT] Launch Date of the RemoveDebris Mission = 2 April 2018"]
-[8.678229331970215, 4.665038108825684, "[TT] Redundancy of the Autonomous star tracker (AST) = Cold redundancy"]
-[3.9666030406951904, 4.253418445587158, "[FF] Documentation of the RADARSAT-2 = Observation of the Earth and Its Environment: Survey of Missions and Sensors"]
-[3.4373397827148438, 4.976157188415527, "[TT] Type of the L-SAR Instrument = SAR"]
-[5.4598708152771, 3.308290719985962, "[FF] Manufacturer of the ALICE = SwRI"]
-[7.793539047241211, 7.525308609008789, "[TT] Image Rejection of the Receiver = 60 dB"]
-[7.9687275886535645, 5.434178352355957, "[FF] Detectors of the INTEGRAL = Imager (IBIS) and a Spectrometer (SPI)"]
-[10.461995124816895, 4.667726039886475, "[TT] Deployment Mechanism of the DST = Trusses and hinges"]
-[5.849918842315674, 4.205204963684082, "[FF] Use Cases of the Satellite for 5G = Disaster response, relieving ground network congestion, serving areas with poor terrestrial links"]
-[7.865381240844727, 8.711349487304688, "[TT] Spectral Range of the Ma_MISS = 0.4\u20132.2\u2009\u00b5m"]
-[8.26993179321289, -0.40145400166511536, "[TT] Air Temperatures of the Antarctic Sea Ice = 2 to 4 degrees Celsius above average"]
-[7.476504325866699, 2.643684148788452, "[FF] Data of the \u00d8rsted = Small-Scale Structure of the Geodynamo"]
-[10.316808700561523, 5.639558792114258, "[TT] Reentry Temperature of the EFT-1 = Up to 2,200\u00ba C"]
-[8.957648277282715, 4.360990524291992, "[TT] Attitude Sensing Subsystem of the S/C = V-slit sun/Earth sensors and analog sun sensors"]
-[9.702888488769531, -0.5348883867263794, "[TT] Orbit Altitude of the HAUSat-2 = 650 km"]
-[5.4880051612854, 5.5801286697387695, "[TT] Communication Interfaces of the MCU = Up to 8 communication interfaces"]
-[13.417487144470215, 7.333771705627441, "[TT] Power of the MuREM = Low"]
-[5.750908374786377, 7.166255950927734, "[TT] Data Rate of the WFC = 26 kbit/s"]
-[7.946006774902344, 9.087377548217773, "[TT] Bands of the LORE = Up to 760 nm"]
-[5.867470741271973, 1.5144978761672974, "[FF] Workshop Date of the PRISMA = 28-30 March 2017"]
-[8.162504196166992, 0.0008487855084240437, "[TT] Launch Date of the TOPEX/Poseidon = 10 Aug 1992"]
-[5.074877738952637, 0.348380446434021, "[TT] Launch Date of the Trasser = July 5, 1988"]
-[4.3831329345703125, 2.172302722930908, "[FF] Transport U.S. Crews to and from the space station of the CST-100 = Boeing"]
-[11.368292808532715, 4.088640213012695, "[FF] Length of the IEM = Specified length"]
-[5.349271774291992, 7.163562297821045, "[TT] Data Rate of the Ka-ISL return service = 300 Mbit/s"]
-[12.127986907958984, 1.9760940074920654, "[FF] Data Availability of the CartoSat-1 = Unknown"]
-[6.93306827545166, 1.0639387369155884, "[TT] Launch Date of the Mars 2020 Perseverance rover = July"]
-[13.530084609985352, 5.441709995269775, "[TT] Manufacturer of the Solar Panels = Spectrolab"]
-[8.159414291381836, 7.870959758758545, "[TT] Channel Detectors of the SEVIRI = 42"]
-[5.849048614501953, 3.1721222400665283, "[TT] Operator of the COMS = Korean Meteorological Association (KMA)"]
-[8.033710479736328, 0.9518687129020691, "[FF] Fine-Tuning of the Irrigation in Asia = Unknown"]
-[6.7869648933410645, 5.952089786529541, "[TT] Engineering Model Quantity of the C2B = 2"]
-[5.170516014099121, 6.952341556549072, "[TT] Intersatellite Link Data Rate of the CNAPS = 10 kbit/s"]
-[9.892585754394531, 7.96696138381958, "[TT] Field of Incident Angle of the Optical telescope = 0\u00ba to 0.69\u00ba"]
-[9.296664237976074, 0.11376235634088516, "[TT] Length of the Scandinavian Peninsula = Approximately 1850 km"]
-[6.238008499145508, 0.2018747329711914, "[TT] Crew Size of the ISS = Three-person"]
-[8.6306791305542, 3.059171199798584, "[TT] Vertical Resolution of the ROSA = 300 m"]
-[6.859143257141113, -0.10296755284070969, "[TT] Revisit Cycle of the Satellite = 1-3 days (for observations at 40\u00ba latitude or higher)"]
-[3.9243433475494385, 2.034773111343384, "[TT] Launch Vehicle of the Jugnu = ISRO PSLV launcher"]
-[9.01255989074707, 2.5997517108917236, "[FF] Current Purpose of the CRS = Study the heliosphere\u2019s charged particles and the particles in the interstellar medium"]
-[8.450887680053711, 1.9344213008880615, "[TT] Measurement Category of the ISS-RapidScat = Ocean surface winds"]
-[4.195438385009766, 2.493680715560913, "[TT] Launch Site of the SkySat-16 to -18 = Cape Canaveral"]
-[3.3303840160369873, 5.742092132568359, "[TT] Number of Panels of the SAR Antenna = 8"]
-[11.195596694946289, 1.079498291015625, "[TT] Operating Spectrum of the LISA Laser Prototype = Near-infrared"]
-[5.825664520263672, 3.4175326824188232, "[TT] Net Loss of the Satellogic = $117.7 million"]
-[6.0991435050964355, 5.7811689376831055, "[TT] Type of the ABI = Data collection"]
-[9.57730484008789, 6.990447044372559, "[TT] 30 bins in polar angle direction of the Angular Resolution = Angular resolution 30 bins in polar angle direction"]
-[7.489384651184082, 2.367295503616333, "[FF] Purpose of the Observation Data = Detecting oil and mineral resources in the ground and seabed"]
-[8.33291244506836, 7.589478969573975, "[TT] Element Size of the CCD Detector Matrix = 22.5 \u00b5m x 22.5 \u00b5m"]
-[13.560497283935547, 5.813529014587402, "[TT] Power Source of the Satellite = 5 solar panels"]
-[3.295109510421753, 6.490859508514404, "[TT] Antenna Diameter of the SDR-VSAT = 2.4 m"]
-[13.446661949157715, 6.9095282554626465, "[TT] Power Output of the IPS = Up to 1.25 kW"]
-[6.93634033203125, 1.768882393836975, "[FF] URL of the James Webb Space Telescope = http://www.roe.ac.uk/ukatc/consortium/miri/index.html"]
-[4.97578763961792, 4.3668317794799805, "[TT] Service Cost of the Starlink = $99 per month"]
-[4.784538269042969, 0.38331300020217896, "[TT] Launch Date of the SPARCS = Not earlier than October 2021"]
-[6.909645080566406, 4.0505290031433105, "[FF] Unknown of the Land Contamination Analysis = Unknown"]
-[6.612105369567871, -0.2639859914779663, "[TT] Trip Duration of the ATLAS = Four and a half days"]
-[10.066761016845703, 2.419962167739868, "[FF] Observation Purpose of the Integral = Measure the cosmic X-ray background"]
-[11.773334503173828, 3.5354721546173096, "[TT] Diameter of the T5 thruster = 10 cm"]
-[14.318862915039062, 3.1046812534332275, "[TT] Mass of the UK-DMC-2 = ~ 96 kg"]
-[8.559978485107422, 8.60497760772705, "[TT] Instantaneous spectral coverage of the Spectrometer = 2.16 km/s"]
-[9.525031089782715, 6.185306072235107, "[TT] Incidence Angle Range of the Wide Ultra-Fine Mode = 30 -50\u00ba"]
-[6.725214004516602, -0.5541641116142273, "[TT] Orbital Period of the NigeriaSat-2 = About 99.5 min"]
-[8.304102897644043, 7.03048038482666, "[TT] Spectrometer Type of the INMS = Gated time-of-flight"]
-[9.368538856506348, 7.008273601531982, "[TT] Resolution of the ScanSAR-1 = 4 x 20m"]
-[5.958178997039795, -0.535483717918396, "[FF] Expected Mission Duration of the Worldview-4 = 10 to 15 years"]
-[5.319972038269043, 6.793605327606201, "[TT] Data Downlink of the BRITE spacecraft = up to 256 kbit/s"]
-[7.357681751251221, 6.57230806350708, "[TT] Sampling Duration of the TAGSAM = About five seconds"]
-[3.063124656677246, 2.192121982574463, "[FF] Mission Purpose of the Copernicus Sentinel-2 = Provide detailed information about Earth\u2019s vegetation, play a key role in mapping differences in land cover, understand the landscape, map how it is used and monitor changes over time"]
-[4.8148651123046875, 0.4135405421257019, "[TT] Kurs-NA Radio System Test Start Date of the Prichal = October 20"]
-[9.97530746459961, 8.139978408813477, "[TT] Focal Length of the MSU-100 = 100 mm"]
-[10.890706062316895, 7.504920482635498, "[TT] Swath Width of the EOS-T = 14 km"]
-[10.812750816345215, 3.7913670539855957, "[FF] Mission of the NEA Scout = Reconnaissance of an asteroid, take pictures and observe its position in space"]
-[4.893294811248779, 0.15317898988723755, "[TT] Launch Date of the Observer Mission (KSF3) = Mid-2022"]
-[7.85592794418335, 2.9510130882263184, "[TT] Global Carbon Dioxide Maps Data Collection Dates of the TanSat = April and July 2017"]
-[5.92262601852417, 2.615201711654663, "[FF] Mission Developer of the \u00d8rsted = NBI (Niels Bohr Institute) of the University of Copenhagen, the Technical University of Denmark (DTU), the Solar-Terrestrial Physics Division of DMI (Danish Meteorological Institute), the Danish Space Research Institute (DSRI) of Copenhagen, Terma A/S, and Computer Resources International (now part of Terma A/S)"]
-[9.550910949707031, 0.9320506453514099, "[TT] Speed of the GEO Satellite = About 3 km/s (11,000 km/h)"]
-[4.840373992919922, 0.9007323384284973, "[TT] Satellite Launch Dates of the AMSU = NOAA-15 (1998), NOAA-16 (2000), NOAA-17 (2002)"]
-[3.505877733230591, 5.334085941314697, "[TT] PRF of the CSG-SAR = Programmable (500-7000 Hz)"]
-[11.396157264709473, 6.7007341384887695, "[TT] Electrical Noise Measurement of the ELS-A = 16.3 keV"]
-[11.539234161376953, 3.3679699897766113, "[TT] Propulsion System of the BIROS = Equipped"]
-[5.464571475982666, 7.749978065490723, "[TT] EIRP of the Ground terminal = 9 dBW"]
-[6.570279598236084, 7.9541401863098145, "[TT] Filter Wheel Filters of the GOES Sounder = 18"]
-[8.967761039733887, 4.534528732299805, "[FF] Attitude Determination Control System (ADCS) of the OPS-SAT = Gyroscopes, accelerometers, magnetometers, reaction wheels, magnetorquers, and a star tracker"]
-[9.727177619934082, -0.13161514699459076, "[TT] Altitude of the BEESAT-4 = 515 km"]
-[5.207469940185547, 2.4818971157073975, "[TT] Agency of the GIOVE = ESA"]
-[13.888216018676758, 3.0662295818328857, "[TT] Mass of the OCULUS-ASR = 70 kg"]
-[5.271034240722656, 0.5920386910438538, "[TT] Recording Date of the SEIS = July 25, 2019"]
-[8.778550148010254, 5.428499221801758, "[TT] ADCS Status of the AlSat Nano = Verified and activated"]
-[16.5416259765625, 3.638768434524536, "[FF] Number of Gateway Stations of the OneWeb = Unknown"]
-[7.052581787109375, 6.767002105712891, "[FF] Function of the Beam-splitter = Mixes light output from the cavity with the input light from the laser"]
-[6.597594738006592, 0.16029684245586395, "[TT] Revisit Time of the Satellite Constellation = Better than 10 hours globally"]
-[5.53848934173584, 2.696491241455078, "[TT] Technology Mission of the CADRE = University of Michigan"]
-[8.07654094696045, -1.0411577224731445, "[FF] Orbit Determination of the ICESat-2 = High-precision GPS receiver and laser ranging"]
-[8.86665153503418, 0.046221714466810226, "[TT] Ecliptic Latitude Range of the NEOSSat = Tentatively \u00b1 40\u00ba"]
-[5.1428141593933105, 1.1734215021133423, "[FF] Participants Meeting Date of the PROBA-3 = March 13, 2008"]
-[9.9776611328125, 7.733264446258545, "[TT] Telescopes of the CREDO-II = Two telescopes"]
-[5.613681316375732, 0.8929958343505859, "[FF] Viasat Partnership Date of the Satellite Vu = 28 September, 2022"]
-[8.289910316467285, 6.354634761810303, "[TT] Lateral Range of the CCRR = \u00b125 mm in Z and Y axes"]
-[5.899750709533691, 2.8830807209014893, "[TT] Developer of the CIP = Space Payload Laboratory at NCU (National Central University) of Taiwan"]
-[9.947843551635742, 4.576910495758057, "[TT] Control of the Reaction Wheels = Coarse three-axis control of the spacecraft body"]
-[11.381503105163574, 5.885526180267334, "[TT] Structure Material of the QuakeSat = 6061 aluminum"]
-[5.58500337600708, 5.487032890319824, "[TT] Interface Type of the OD (Order Desk) system = Web services"]
-[9.142404556274414, 3.1484122276306152, "[FF] Objective of the Cluster = Observation of key interaction processes between two cosmic plasmas"]
-[6.872580051422119, 7.093915939331055, "[TT] Beam Incidence Span of the SWIM = Up to 10\u00ba"]
-[9.914382934570312, -0.5299822092056274, "[TT] Orbit Altitude of the SARSAT-1 = 801 x 826 km"]
-[9.437481880187988, -1.3924343585968018, "[TT] Orbit Eccentricity of the ASNARO satellite = 0.00125\u00b10.0008"]
-[3.2181315422058105, 5.079071521759033, "[TT] Resolution of the SAR Image = 3-meter"]
-[6.262040138244629, 1.770509958267212, "[FF] Mission of the BRITE = BRIght Target Explorer"]
-[8.02740478515625, 8.701873779296875, "[TT] Precision of the SOLSPEC = 0.01 nm"]
-[6.248690128326416, 1.0256401300430298, "[TT] Launch Date of the Sample Retrieval Lander = Summer 2028"]
-[13.471835136413574, 1.8993148803710938, "[TT] Live Mammals of the Dragon = 20 rodents"]
-[8.114341735839844, -1.164077877998352, "[FF] Laser Instrument of the ICESat-2 = Can directly measure both the height of the top of the melt pond and of the ice below"]
-[9.500883102416992, 6.368460178375244, "[TT] Scan Fields of Regard of the Scan Mirror = 1\u00ba x 0.75\u00ba, 1\u00ba x 1.5\u00ba, or 1\u00ba x 3\u00ba"]
-[6.707205772399902, -0.6549992561340332, "[TT] Flight Time to Second Transfer Orbit of the Fregat upper stage = 1 minute 6 seconds"]
-[4.408396244049072, 1.4214142560958862, "[TT] Launch Year of the SARLupe = 2006"]
-[5.067774295806885, 1.119246244430542, "[TT] Presentation Date of the UniSat-5 = April 23-25, 2014"]
-[9.612985610961914, 7.094579219818115, "[TT] Spatial Resolution of the AMSR3 = 3 km x 5 km to 34 km x 58 km"]
-[4.6058878898620605, 1.1869975328445435, "[TT] Number of Professionals of the SAOCOM-1A = As many as 600"]
-[6.499871730804443, 4.940902233123779, "[FF] System Architecture of the GATE = GATS (GATE Transmit Segment), GAMS (GATE Mission Segment)"]
-[5.878704071044922, 1.2454683780670166, "[FF] Purpose of the GeoXO = Advance Earth observations from geostationary orbit"]
-[6.166269302368164, 2.279235363006592, "[TT] Principal Investigator of the TROPICS = William Blackwell of MIT/LL (Massachusetts Institute of Technology'/Lincoln Laboratory)"]
-[4.909643650054932, 0.5567690134048462, "[TT] Launch Date of the MoonLIGHT = 2024"]
-[8.142101287841797, 0.495204359292984, "[TT] Highest Water Level of the Lake Mead = June 2019"]
-[6.281676769256592, 8.068187713623047, "[TT] Number of Passbands of the Channel 3 = 1"]
-[8.369489669799805, 2.743098735809326, "[TT] Measurement Domain of the Badr-B = Gravity and Magnetic Fields"]
-[10.45840835571289, 6.848923206329346, "[TT] Focal Length of the Mirror System = 2700 mm"]
-[8.78380012512207, 3.547656297683716, "[FF] Objective of the CERTO = Observe ionospheric densities and irregularities"]
-[8.54914665222168, 0.3594437837600708, "[FF] Diameter of the Potentially Hazardous Asteroid (PHA) = ~140 m or larger"]
-[7.56503438949585, 2.6991193294525146, "[FF] Radar Altimeter System of the Envisat = RA-2"]
-[5.642014503479004, 4.575431823730469, "[FF] LRIT and HRIT Broadcasting Service Provider of the GK2A satellite = KMA (Korean Meteorological Administration)"]
-[7.065920352935791, 4.278077602386475, "[FF] Function of the VISTA = Complement AERO"]
-[5.193812370300293, 0.6913959980010986, "[FF] Article Date of the TCarta = 27 October 2020"]
-[5.191694259643555, 5.166314125061035, "[FF] Ground-Station Uplink Passes of the SpinSat = Within the preceding 5 days"]
-[4.2169575691223145, 4.292304039001465, "[FF] Status and Developments Meeting Date of the Cospas-Sarsat Program = 25 \u2013 29 January 2015"]
-[6.207250595092773, -0.29065006971359253, "[TT] Backup Power Duration of the RTC = At least 24 hours"]
-[7.831415176391602, 0.675967812538147, "[TT] Size of the Lunar Flashlight = About the size of a briefcase"]
-[10.62421703338623, 3.939000368118286, "[FF] Dragsail Deployment of the DSAT-3 = After DSAT-3 deploys a dragsail"]
-[9.780978202819824, 4.572636127471924, "[TT] Attitude Control of the ASTRO-SPAS platform = Cold-gas system"]
-[14.265724182128906, 3.1976191997528076, "[TT] Mass of the CMS = 4 kg"]
-[6.026324272155762, 7.502167701721191, "[TT] Sample Rate of the Angular Rate = 125 Hz"]
-[8.34793758392334, 3.0610716342926025, "[FF] Topic of the SCISAT = Ozone depletion"]
-[8.072187423706055, 4.230281829833984, "[TT] Instrument Type of the GPIM = Earth radiation budget radiometers, Other, Data collection"]
-[5.933786869049072, 2.343209981918335, "[TT] Mission of the Orion MPCV = EM-2 (Exploration Mission-Two)"]
-[6.948953628540039, 3.6594018936157227, "[FF] Design Material of the PROBA-3 = Plastic"]
-[10.705806732177734, 1.0790109634399414, "[TT] Size of the L 98-59b = Around 80% Earth\u2019s size"]
-[7.613027572631836, -0.3288535475730896, "[TT] De-orbit of the Gnome Chompski = With Electron\u2019s Kick Stage"]
-[6.635436058044434, 4.2788238525390625, "[FF] Design Incorporations of the Automated Transfer Vehicle = About 30"]
-[5.051586627960205, 7.339725017547607, "[TT] ILAS Data Rate of the RF communications = 0.517 Mbit/s"]
-[13.381814956665039, 7.418886184692383, "[TT] Total Output Power of the TWTA = > 54.5 dBm (about 280 W)"]
-[4.489001274108887, -0.2400503009557724, "[TT] Docking System Compatibility of the MEV-1 = 80 percent of all geosynchronous satellites"]
-[9.402746200561523, 3.7798776626586914, "[FF] Function of the Tool = Compute the strength and direction of the magnetic field along animal migratory paths"]
-[5.092756271362305, 0.41379284858703613, "[TT] Year of Launch of the TRMM = 1997"]
-[5.624697208404541, 4.442229747772217, "[TT] Roaming Capability of the Cellular Telephones = U.S., Europe and Asia"]
-[9.939006805419922, -1.4632444381713867, "[TT] Orbit Inclination of the BX-1 = 42.4\u00ba"]
-[13.237781524658203, 5.251142978668213, "[TT] Solar Arrays Area of the Spacecraft = 144 m2"]
-[6.6550374031066895, 6.377913951873779, "[TT] Number of Off-Source Pointings of the Mode 2 = 24"]
-[7.709954261779785, 2.9549691677093506, "[FF] Purpose of the GOSAT-2 = Monitoring greenhouse gases such as methane, ozone, water vapour, carbon monoxide and nitrogen dioxide levels"]
-[4.891603469848633, 7.3265485763549805, "[TT] Command Data Rate of the S-band transponder = 2 kbit/s"]
-[8.775129318237305, 6.322703838348389, "[TT] Calibration Images of the PROBA-V = 2.622"]
-[5.968890190124512, 6.266839504241943, "[TT] Communication Delay of the EDRS-C = Up to 90 minutes"]
-[3.494342803955078, 6.449400424957275, "[TT] Swath Width of the Antenna Subsystem = 180 km"]
-[3.572042942047119, 4.409116268157959, "[TT] Retirement Date of the SAR-Lupe Constellation = After November 2017"]
-[5.587846755981445, 5.093474388122559, "[FF] Data Relay of the EDRS-C terminal = Relaying in excess of 500 TB of the Earth observers\u2019 findings"]
-[6.309272766113281, 6.5619120597839355, "[TT] Optical Inter-satellite Links of the EDRS-A = Almost 30,000"]
-[4.452346324920654, 7.360414505004883, "[TT] X-band links Frequencies of the Science data transmission = 8.15, 8.25, 8.35 GHz"]
-[9.830994606018066, 8.262066841125488, "[TT] Across-track FOV of the Telescope = \u00b11.31\u00b0"]
-[7.546546459197998, 2.4425466060638428, "[TT] Value of the GRDs Sky Coverage = ~80%"]
-[7.731297016143799, 6.553043365478516, "[TT] First Tb Image Production Time of the MWR = ~ 6 hours after the data reception on August 31, 2011"]
-[8.616215705871582, 4.731310844421387, "[TT] Star Trackers of the DSX = None"]
-[7.5686845779418945, 2.138993740081787, "[FF] Science Objectives of the ADEOS-II = Acquire data contributing to international global change research (carbon cycle and the water and energy cycle), as well as for applications in such fields as meteorology and fishery"]
-[7.596500873565674, 4.675248622894287, "[FF] TEB Detector Nonlinearity of the VIIRS = Excellent"]
-[5.100765228271484, 3.528780937194824, "[TT] Manufacturer of the SSP Altimeter = SSTL/Astrium"]
-[10.557455062866211, 7.208461761474609, "[TT] Tube-shaped Corridor Radius of the ALOS-2 satellite = 500 m"]
-[8.048164367675781, 2.993076801300049, "[FF] Function of the Atmosphere Measuring Devices = Characterizing the location"]
-[7.910044193267822, 6.67667818069458, "[TT] Interface Type of the FODB = Fiber Optic"]
-[13.969865798950195, 7.32037353515625, "[TT] Power Output of the PDC = Conditioned 28 VDC and 12 VDC"]
-[3.6156811714172363, 2.7089388370513916, "[TT] Number of Satellites of the Iridium Next = 66"]
-[5.9262800216674805, 2.3438127040863037, "[TT] Science Team Lead of the MIRI = George Rieke with the University of Arizona"]
-[6.693310737609863, -0.6484955549240112, "[TT] Functionality Duration of the S/C and ground segment = Up to 1 orbit before the final breakup"]
-[10.230097770690918, 3.088009834289551, "[TT] Operation Frequency of the SONATE CubeSat = Daily"]
-[8.204891204833984, -1.0748416185379028, "[TT] Measurement Depth of the ICESat-2 = Up to 140 feet (43 meters)"]
-[9.747346878051758, -0.5552631616592407, "[TT] Orbital Altitude of the DST = 550 km"]
-[6.295709133148193, 6.328492164611816, "[FF] Data Collection Timestamp of the CANDOS = SYSLOG facility or application logs"]
-[9.01338005065918, 4.886082649230957, "[TT] Range of the Horizon sensor = \u00b15.5\u00ba"]
-[5.935176849365234, 4.747463226318359, "[FF] Interface Requirements of the Satellite Bus = Power interface requirements, data storage requirements and payload control requirements"]
-[4.88006067276001, 0.7756491303443909, "[TT] Launch Date of the PW-Sat = February 13, 2012"]
-[4.875049114227295, 0.5520129203796387, "[TT] Launch Date of the CFOSAT = 2018"]
-[8.314726829528809, -0.5386121273040771, "[TT] Width of the Glacier = 7 miles"]
-[8.380133628845215, 4.34174108505249, "[TT] Calibration Method of the OBC = LED + solar calibration"]
-[4.9613213539123535, 0.5007205605506897, "[TT] Launch Date of the BIROS = 2016"]
-[7.663707256317139, 4.199215412139893, "[FF] Grid of the Phantoms = Three-centimeter grid embedded throughout the torsos"]
-[11.3841552734375, 0.7078666687011719, "[TT] Orbital Period of the AU Mic b = 8.5 days"]
-[5.556857585906982, 0.9032702445983887, "[TT] Arrival Date at NASA/MSFC of the Heat Shield = March 9, 2015"]
-[8.941686630249023, -0.24442461133003235, "[FF] Kinematic properties of the \u03b2 meteoroid = > 77 km/s"]
-[7.089972972869873, 2.4256861209869385, "[FF] Mission Title of the Firefly Satellite = Understanding Earth\u2019s most Powerful Natural Particle Accelerator"]
-[5.817034721374512, 7.171950340270996, "[TT] Parameter of the Data Rate = 4 kbit/s max"]
-[8.19422435760498, -0.287840873003006, "[FF] Meltwater Runoff Increase of the Greenland = 21% over the past 40 years"]
-[10.744892120361328, 2.778557538986206, "[FF] Design Presentation Proceedings Date of the Microsatellites = Jan. 2005"]
-[5.307528972625732, 1.8440406322479248, "[TT] Mission Status of the GeoEye-1 = Operational (extended)"]
-[11.608229637145996, 6.6971235275268555, "[TT] Energy Measurement Range for Nuclei of the Telescope 3 = 20-500 MeV/n"]
-[8.86839485168457, 3.173201084136963, "[FF] Study of the ISEE-1/2 spacecraft = An unusual flux transfer event"]
-[12.717294692993164, 1.931268334388733, "[FF] Measurement Range of the SAGE-II = Earth's upper troposphere and stratosphere in the altitude range of 10-40 km"]
-[6.999320983886719, 5.13728666305542, "[TT] Structure Type of the Satellite = Monoblock frame"]
-[9.861838340759277, 8.042268753051758, "[TT] Beam of the STARE telescope = f/2.5"]
-[9.256437301635742, 1.8439159393310547, "[TT] Quantity of the HTA (Harpoon Target Assembly) = 1"]
-[5.736704349517822, 5.9625091552734375, "[TT] Data Access of the SOAR = Research and testing purposes"]
-[4.559554576873779, 3.4013733863830566, "[TT] Ground Station Location of the CFESat = LANL"]
-[11.53664493560791, 6.895787715911865, "[TT] High Energy Detector Channels of the SSJ/4 = 10 channels centered at 1.0, 1.4, 2.1, 3.0, 4.4, 6.5, 9.5, 14.0, 20.5 and 29.5 KeV"]
-[10.64216136932373, 8.866490364074707, "[TT] Pixel Size of the Channel 5 = 32 x 32 km"]
-[13.808692932128906, 7.1211628913879395, "[TT] Ripple (%) of the PS-2 = 5"]
-[7.591037750244141, 6.222737789154053, "[TT] Measurement Accuracy of the Advanced Topographic Laser Altimeter System (ATLAS) = About 10 vertical centimeters"]
-[8.019888877868652, 5.151945114135742, "[FF] Typical Value of the AAOD = 0-0.05"]
-[5.636953353881836, 0.9932168126106262, "[FF] Commissioning and Operations Support Date of the Orbital Test Bed Satellite = 23 July 2019"]
-[5.385715007781982, 0.9064241051673889, "[FF] Opening Date of the ESA's first UK Center = July 9, 2015"]
-[6.862849235534668, 4.445079803466797, "[FF] Main Control Station of the Rumpin = True"]
-[5.953787326812744, 8.749509811401367, "[TT] Value of the MTF = Better than 0.3 Nyquist"]
-[7.901716709136963, 5.124828338623047, "[FF] Mission Operations Blocks of the HyperScout\u00ae = Radiometric Calibration, Line of Sight Model Correction and Instrument Functionality Testing; Intensive Observations L2 Data Validation; On Board Processing Experiments"]
-[8.170010566711426, -0.9250908493995667, "[FF] Sub-ice-shelf Bathymetry Measurement of the Airborne Topographic Mapper = Unknown"]
-[12.01159381866455, 6.489898204803467, "[TT] Observation of the AMS = Spectrum appears to flatten above 250 GeV"]
-[9.659940719604492, 8.348159790039062, "[FF] Field of View (FOV) of the AMSU-A = Varies with angle about 48 km at nadir about 150 km at limb"]
-[10.786137580871582, 1.3670117855072021, "[TT] Mass of the HD 21749 = About 70% of the Sun\u2019s mass"]
-[4.952876567840576, 3.2704288959503174, "[TT] Manufacturer of the PUCPSat-1 = Pontificia Universidad Cat\u00f3lica del Per\u00fa-Satellite"]
-[5.887357711791992, 1.4795706272125244, "[TT] Commissioning Date of the PRISMA POD = Fall of 2010"]
-[9.975428581237793, 4.4417033195495605, "[TT] Winding of the Torque Rods = Dual-wound"]
-[7.905335426330566, 6.932828903198242, "[TT] Status of the Spectrophotometer sensor head = Operational"]
-[14.10383415222168, 3.2425544261932373, "[TT] Mass of the CICERO-6 = ~10 kg"]
-[9.894577980041504, 2.7530527114868164, "[FF] End Date of the CubeRRT mission = 30 November 2020"]
-[4.449960708618164, 7.048443794250488, "[TT] DVB-RCS/DVB-S2 On-Board Processors (OBPs) of the Repeater subsystem = 4 channels in Ku-band"]
-[6.395124912261963, 0.8011730909347534, "[FF] Early Data Release 3 (EDR3) of the Gaia = Data processed, validation ongoing"]
-[10.912885665893555, 4.498366832733154, "[FF] Working Depth of the Surveyor = Shallow water"]
-[8.083209037780762, 8.368264198303223, "[FF] Spectrometer Regions of the HISUI = VNIR (Visible and Near Infrared Region), SWIR (Shortwave Infrared Region)"]
-[9.73018741607666, 3.7464523315429688, "[FF] Model of the Pulsars = \"Accretion columns\" model where the infalling gas is guided by the pulsar's strong magnetic field so that it lands on the magnetic poles"]
-[5.511238098144531, 6.765066623687744, "[TT] Daily Data Volume of the WCOM = 291.6GB"]
-[5.218118190765381, 0.7940437197685242, "[FF] Mission Profile Presentation Date of the SVOM = 10-15 April 2016"]
-[8.310705184936523, 2.4651925563812256, "[TT] Number of Stacer Boom Systems of the THEMIS Constellation = 10"]
-[10.948177337646484, 0.8683488965034485, "[TT] Spacecraft Separation of the LISA = 2.5 million km"]
-[7.572751045227051, 8.96777629852295, "[TT] NER of the Spectral Band C = 1.7 x 10^-5 W/(cm^2 sr \u00b5m)"]
-[11.810312271118164, 4.720706462860107, "[TT] Column Dimensions of the UniSat-3 = Aluminium threaded rods, 6 mm in diameter"]
-[4.760571002960205, 5.836262226104736, "[TT] Frequency (MHz) of the Compass-BeiDou B2a = 1175.00"]
-[10.86545467376709, -0.3031744360923767, "[FF] T/R Modules Design and Performance Presentation Date of the TanDEM-X = June 2-5, 2008"]
-[5.388434410095215, 4.38799524307251, "[TT] Ground System Component of the MEOLUTs = MEOLUTs"]
-[7.5801191329956055, 5.82794713973999, "[FF] Operational Modes of the VRSS-1 = Real-time imaging mode, Quasi real-time imaging mode, Recording mode, Replay mode"]
-[13.165698051452637, 2.9210803508758545, "[FF] Launch Mass of the VELOX-PII CubeSat = Unknown"]
-[4.019904613494873, 1.5774455070495605, "[TT] Launch Failure Issue Time of the Global-9 = Shortly after stage two ignition"]
-[6.89569616317749, 6.919730186462402, "[TT] Pause Time of the Lasers = 1 to 6 ms"]
-[7.1924896240234375, 2.7309622764587402, "[FF] Objectives of the INSAT3D = Monitor earth's surface, carryout oceanic observations, provide data dissemination capabilities, provide BSS (Broadcast Satellite Services)"]
-[4.237306118011475, 2.61944842338562, "[TT] Launch Site of the Landsat-6 = Vandenberg Air Force Base (VAFB)"]
-[8.052459716796875, 5.9896392822265625, "[FF] Off-nadir tilted field of view of the OLCI = Implemented for OLCI cameras"]
-[4.645223140716553, 7.9821906089782715, "[TT] Operating Center Frequencies of the Satellite = 13.575 GHz (Ku-band), and 3.2 GHz (S-band)"]
-[9.603767395019531, 8.29379653930664, "[TT] Field of View (FOV) of the WISPR = 180\u00ba"]
-[5.9136128425598145, 2.5965025424957275, "[FF] Collaboration of the JEM-EUSO = T. Ebisuzaki, H. Mase, Y. Takizawa, Y. Kawasaki, H. Miyamoto, K. Shinozaki, H. Ohmori, Hachisu, S. Wada, T. Ogawa, F. Kajino, N. Inoue, N. Sakaki, J. Adams, M. Christl, R. Young, M. Bonamente, A. Santangelo, M. Teshima, E. Parizot, P. Gorodetzky, O. Catalano, P. Picozza, M. Casolino, M. Bertaina, M. Panasyuk, B.A. Khrenov, I.H. Park, A. Neronov, G. Medina-Tanco, D. Rodriguez-Frias, J. Szabelski, P. Bobik R. Tsenov"]
-[5.509372234344482, 2.3387765884399414, "[TT] Mission Type of the LAPAN-A2 = EO (Earth Observation)"]
-[6.700438976287842, 5.4314494132995605, "[FF] Board Types of the PEB (Payload Electronics Box) = Bus interface board, Solid state data recorder, Digital board, LED and heater control board, 2 x focal plane bias boards, Low-voltage power supply board"]
-[3.410590887069702, 6.362349033355713, "[TT] Antenna Size of the Antenna and RF Subsystem = 11.3 m"]
-[9.284157752990723, -0.429902583360672, "[TT] Apogee Altitude of the IDEA-OSG 1 = 800 km"]
-[5.051809787750244, -0.7245338559150696, "[TT] Launch Time of the Kounotori = 11:50:49 UTC"]
-[7.374262809753418, 3.728792905807495, "[FF] Mission Goals of the ARMADILLO = Demonstrate ionospheric radio-occultation within a single CubeSat volume (10 cm x 10 cm x 10 cm) using a software-defined dual frequency GPS receiver"]
-[10.075749397277832, -1.502394199371338, "[TT] Inclination of the DMC-3 Constellation = 97.8\u00ba"]
-[6.404780864715576, 6.94062614440918, "[TT] Fiber Optics Links of the MIRAS = 144"]
-[5.976931571960449, 6.429128170013428, "[TT] Science Data Collection Modes of the DPU = Two"]
-[7.018594741821289, -0.45917463302612305, "[TT] Local Solar Time (LST) of the ADEOS-II = 1030 \u00b1 15 minutes"]
-[4.897765636444092, 3.307269334793091, "[TT] Manufacturer of the SIMBA = Royal Meteorological Institute Belgium"]
-[3.471395254135132, 4.854253768920898, "[TT] Radar Imagery Capability of the SIR-C/X-SAR = Multifrequency (3) and multipolarization"]
-[13.34993839263916, 7.301079750061035, "[TT] Input Power of the HET-X = 350 - 2500 W"]
-[4.627158164978027, 2.9488718509674072, "[TT] Data Management Center of the ALT = Wallops Flight Center, VA"]
-[14.226990699768066, 3.2305827140808105, "[TT] Total Mass of the CAE System = 3.25 kg"]
-[9.378251075744629, 6.165118217468262, "[TT] Rotation of the Scanning Platform = Continuous"]
-[6.806429386138916, -0.5756519436836243, "[TT] Orbital Period of the Satellite = 97.7 minutes"]
-[7.214278221130371, 0.9988506436347961, "[TT] Launch Date of the OceanSat-1 = May, 26, 1999"]
-[6.269736289978027, 4.829921722412109, "[FF] Function of the MIP = Reconfigured the data paths between the control center and the payload automatically"]
-[7.01304817199707, 5.135117053985596, "[TT] ADCS Systems of the OPS-AT = Two"]
-[8.420310974121094, 2.5662412643432617, "[FF] Science Objectives of the THEMIS = Onset and evolution of the macroscale substorm instability, production of storm-time MeV electrons, control of the solar wind-magnetosphere coupling"]
-[5.521841526031494, 6.257070064544678, "[TT] Data Storage of the Satellite = At least two and a half orbits of mission data"]
-[5.23599100112915, 0.33949780464172363, "[TT] Last Observation Date of the TRACE = June 21, 2010"]
-[3.447679281234741, 2.0180230140686035, "[FF] Mission Type of the Sentinel-6 = Reference"]
-[9.900741577148438, 8.216941833496094, "[FF] Issue of the Coded aperture correlation holography system = 13"]
-[11.746086120605469, 6.57343053817749, "[TT] Gamma-ray Energy Resolution of the MGNS = Approximately 3.5% at the energy of 662 keV"]
-[5.766899108886719, 5.110053539276123, "[FF] Capability of the SCPS = Aggregate telecommand and telemetry data into recognizable files and transport them end-to-end through the data networks"]
-[8.199373245239258, 7.649392604827881, "[FF] Function of the 215 nm Band = Monitors the UV flux and estimate possible degradations of the SODISM CCD detectors"]
-[7.4197096824646, 1.9396214485168457, "[FF] Applications of the Landsat TM = Global change research, agriculture, forestry, geology, resources management, geography, water quality, and oceanography"]
-[7.2630133628845215, 4.373941898345947, "[FF] Unknown of the NMS = Unknown"]
-[10.159266471862793, 1.4683507680892944, "[TT] Data of the Roman = More than 10 million galaxies"]
-[9.78908634185791, 7.6339216232299805, "[FF] Design and Test of the BRITE Constellation Space Telescope = Wide Field, High Resolution, Low Noise"]
-[7.640634059906006, 2.2310550212860107, "[TT] Spatial Coverage of the ILAS-II = 10 - 60 km"]
-[6.174267768859863, 4.797963619232178, "[FF] Usage of the Serial Communication = For some specialized payloads"]
-[4.962497234344482, 3.254905939102173, "[TT] Manufacturer of the OMPS = BATC (Ball Aerospace & Technologies Corp.)"]
-[10.12108325958252, 5.307105541229248, "[TT] Vibration Reduction of the Cryocooler = Factor of about 75"]
-[10.839557647705078, 2.1310226917266846, "[FF] X-ray emission source of the XMM-Newton = Detected"]
-[3.4310290813446045, 4.730518341064453, "[TT] Observation Modes of the StriX-\u03b1 = Stripmap and Sliding Spotlight mode"]
-[6.466952323913574, 4.916895389556885, "[FF] Functions of the OBC = Sensor electronics, command processing, telemetry and housekeeping, attitude and orbit control, thermal management"]
-[8.303014755249023, 4.59426212310791, "[FF] Calibration Method of the OMPS = Solar illuminated diffusers"]
-[6.505277633666992, 0.5526648759841919, "[TT] Explosion Date of the Cassiopeia A = 320 years ago"]
-[5.495115756988525, 4.881185054779053, "[TT] Communication Network Type of the EDSN Swarm = Hub-and-spoke network"]
-[9.436890602111816, -1.1403331756591797, "[TT] Orbit Position of the BeiDou-1A = GEO, 140\u00ba E"]
-[8.718607902526855, 7.24945592880249, "[TT] Detector Orientation of the DIDM = Facing the S/C ram direction"]
-[11.373510360717773, 5.8377156257629395, "[TT] Structure Material of the Payload Module = Aluminum core and aluminum face skin"]
-[11.764875411987305, 3.2766783237457275, "[TT] Thruster Type of the NanoPS = Liquid-fueled cold-gas"]
-[5.542400360107422, 1.2160683870315552, "[FF] Conference Date of the IR-sounder IRFS-2 = 4-8 February 2013"]
-[5.510064125061035, 6.363450050354004, "[TT] On-board Storage of the CDSU = 2 GB"]
-[8.409798622131348, 3.9425718784332275, "[FF] Measurement Type of the NINA-2 = Light high-energy ions"]
-[7.191427707672119, 3.440744400024414, "[FF] Imaging Frequency of the Dove Satellites = Once a day for the entire planet, up to 10 times a day for a particular location"]
-[5.962181568145752, 4.433319091796875, "[FF] Architecture of the GIOVE system = Ground Mission Segment, GESS network, GIOVE Mission segment"]
-[7.144465923309326, 0.02466427907347679, "[TT] Record Days Above 110\u00b0F of the Phoenix = 34"]
-[4.561957836151123, 6.428986549377441, "[FF] RF Communications Radios of the Neutron-1 = Gamalink Radio, GlobalStar radio, GlobalStar simplex radio"]
-[5.209532260894775, 4.4600830078125, "[TT] Ground Station Interface of the TROPICS = KSAT-lite ground station network"]
-[9.98516845703125, 4.5892767906188965, "[TT] Attitude Control of the PhoneSat-2.5 = Reaction wheels"]
-[5.233983993530273, 8.397831916809082, "[TT] Bandwidth of the HDR Terminal = 900 MHz"]
-[13.35563850402832, 6.905193328857422, "[TT] Power of the RISAT-2 = 750 W"]
-[6.137524604797363, 1.7445615530014038, "[FF] URL of the LUMIO = https://iafastro.directory/iac/proceedings/IAC-18/"]
-[7.8724260330200195, 7.936458110809326, "[FF] Effect of Diffraction of the Geostationary Infrared Sounder = Increased compared to sounding from LEO"]
-[9.464201927185059, 7.436742305755615, "[TT] Ground Pixel Size of the HORUS = 14.6 m"]
-[14.405677795410156, 3.262442111968994, "[TT] Mass of the LISS-4 = 169.5 kg"]
-[3.8881518840789795, 1.9908925294876099, "[TT] Launch Vehicle of the LightSail-2 = SpaceX Falcon Heavy rocket"]
-[12.013607025146484, -0.3520909249782562, "[TT] Discovery Date of the TESS = January 7, 2020"]
-[8.548612594604492, 7.752237319946289, "[TT] Data Product of the DHU = Subarrays (nominally 10 x 10 pixels)"]
-[7.84329891204834, 9.286601066589355, "[TT] Center Wavelength of the Green = 555.0 \u00b5m"]
-[8.979448318481445, 5.691401481628418, "[TT] Pointing Range of the ADCS = \u00b132\u00ba"]
-[9.354697227478027, 6.868350505828857, "[TT] Resolution of the Radiometer = 40 km"]
-[3.8688154220581055, 3.4534335136413574, "[FF] Launch Date of the Galileo = Unknown"]
-[6.179332256317139, 5.217319011688232, "[FF] I/O Capabilities of the OBC = Provided"]
-[3.145962715148926, 2.2708122730255127, "[FF] Mission Goals of the Sentinel-6 Michael Freilich = Gather data for atmosphere information, climate change, and environment monitoring"]
-[6.041781425476074, 5.467587471008301, "[TT] Redundancy of the Central Computers = Two redundant central computers"]
-[3.8761889934539795, 4.269214153289795, "[FF] Application Areas of the RISAT = Vegetation, agriculture, forestry, soil moisture, geology, sea ice, coastal processes, and man-made object identification"]
-[13.397317886352539, 7.368982791900635, "[TT] Power of the LISS-IIM = 34 W"]
-[3.8742334842681885, 6.334352493286133, "[TT] Quantity of the TT&C Antennas = 4"]
-[11.411537170410156, 4.410587787628174, "[TT] Form Factor of the Doublewide Deployers = 2U x 3U"]
-[5.144282341003418, 3.375784158706665, "[TT] Collaboration of the OSAM-1 = Maxar Technologies"]
-[11.030996322631836, 7.403442859649658, "[TT] Swath of the Sentinel-2 satellites = 290 km"]
-[3.6873536109924316, 4.777317523956299, "[FF] Functionalities of the ICPS = Generation of image collection plan, management of image collection planning status, managing resources related to the SAR payload operation"]
-[10.372469902038574, 3.205249071121216, "[FF] Quantity of the SmallSats = 38"]
-[6.329931259155273, -1.3739343881607056, "[FF] Launch Date of the GRACE Follow-On = Unknown"]
-[9.920392036437988, 8.187488555908203, "[TT] FOV of the Mirror System = \u220534 arcmin"]
-[6.337871551513672, 7.29683780670166, "[TT] Input Data Stream of the LIAU = 8-bit wide"]
-[5.898841857910156, 3.473233938217163, "[FF] Target Market of the ANGELS = Small satellite market for in orbit operational missions"]
-[12.020334243774414, -0.41833752393722534, "[FF] Launch Date of the TESS = 28 March 2018"]
-[10.220457077026367, 7.226476192474365, "[TT] Resolution of the APIS Device = 273.7 m"]
-[4.979390621185303, 3.2500765323638916, "[TT] Manufacturer of the AAUSat-2 = Aalborg University, Denmark"]
-[6.950490951538086, 4.147677421569824, "[FF] Autonomy of the SIRDARIA = Autonomous"]
-[5.386855125427246, -0.029011335223913193, "[TT] Attachment Time of the NG-10 Cygnus = 7:31 a.m. EST"]
-[5.271839618682861, 8.160941123962402, "[TT] Antenna Preamp of the IME-HF instrument = Equipped"]
-[8.65530014038086, 7.963087558746338, "[FF] Radiometric Resolution of the Instrument = 0.34 K, 0.7 K, 0.7 K, 0.6 K, 0.7 K, 1.8 K, 1.6 K, 1.2 K, 1.2 K"]
-[8.180229187011719, -0.4229898154735565, "[FF] Average Concentration of the Arctic Sea Ice = At least 15 percent"]
-[13.846821784973145, 5.654890537261963, "[TT] Cell Efficiency of the Solar Array = 28.7%"]
-[9.467472076416016, 1.078371524810791, "[TT] Speed of the Reverse Shocks = Between about 5 and 9 million miles per hour"]
-[5.971560478210449, 5.725556373596191, "[TT] Identical Payload of the CBERS-2A = CBERS-1"]
-[7.007170677185059, 7.140779495239258, "[TT] Divergence of the Communications Lasers = 80 \u00b5rad"]
-[5.293684005737305, 3.248856544494629, "[TT] Manufacturer of the Gonets-M No.3 = JSC Academician M.F. Reshetnev Information Satellite Systems"]
-[10.049111366271973, 1.816939353942871, "[FF] Mission Type of the eROSITA = All-sky survey"]
-[10.347612380981445, -1.2989531755447388, "[TT] Value of the Maximum \u03b2 angle = -62 \u00ba"]
-[3.6906230449676514, 5.443368911743164, "[FF] Resolution of the Spotlight-1B = Finest"]
-[5.497389316558838, 6.435861110687256, "[TT] Storage Capacity of the Data Buffer Board = Up to 46+46 averaged frames with telemetry and ancillary data"]
-[4.746095657348633, -1.7989144325256348, "[TT] Launch Date of the Chang'e-2 = October 1, 2010"]
-[13.474878311157227, 2.8210761547088623, "[TT] Mass (Dry) of the Satellite = \u2264 1700 kg"]
-[4.614837169647217, 2.830596446990967, "[TT] Mission Operations Center of the XMM-Newton = ESA/ESOC (European Spacecraft Operations Center) in Darmstadt, Germany"]
-[13.771902084350586, 3.4213154315948486, "[TT] Mass of the Receiver = 200 g"]
-[13.52624225616455, 2.9931182861328125, "[TT] Bus Mass of the SAC-D spacecraft = 800 kg"]
-[9.257292747497559, -0.27937933802604675, "[TT] Perigee of the Explorer 36 = 1082 km"]
-[5.46426248550415, 5.420766830444336, "[TT] Data Link Error Detection of the GOES-R Instruments and Spacecraft = Implemented"]
-[10.110509872436523, 1.9680628776550293, "[TT] Launch Date of the Chandra X-ray Observatory = July 23, 1999"]
-[5.8211989402771, -0.7821175456047058, "[TT] Lifetime of the Satellite = Up to 12 years"]
-[10.448758125305176, 5.842487335205078, "[TT] Interface Temperature Requirement of the LCT = Lower than 15\u00baC"]
-[7.479828834533691, 5.326717376708984, "[FF] Components of the Imager = EO (Electro-Optics) module, telescope, scan assembly, detectors, cooler, power-supply modules"]
-[7.236512184143066, 4.012304306030273, "[FF] Unknown of the Small Optical Sensor Satellite ASNORO = Unknown"]
-[5.411104679107666, 3.110938787460327, "[TT] Developer of the Electronic Unit = Shandong Institute of Aerospace Engineering"]
-[8.819437026977539, 2.919092893600464, "[FF] Mission of the ALPHA = Understand phenomena related to Earth's auroras"]
-[8.391032218933105, 4.819207668304443, "[FF] Disturbance Source of the VBS = Short-lived glints from the target"]
-[6.476311206817627, 2.1165237426757812, "[FF] URL of the Advanced Communication Technology Satellite (ACTS) = http://acts.grc.nasa.gov/experiments/acts_exp_opportunity_guide.pdf"]
-[10.739200592041016, 3.847705364227295, "[FF] Reentry Outcome of the InflateSail = Destroyed"]
-[6.518339157104492, 5.150842666625977, "[FF] Instrument Control Document of the Advanced Data Collection System = Advanced Data Collection System Instrument Control Document, (A-DCS ICD)"]
-[10.180727005004883, 8.121885299682617, "[TT] Telescope Aperture of the OGS = 1 meter"]
-[4.247114658355713, 6.250863552093506, "[TT] Antenna of the Lunar Pathfinder's Receiver = High-gain satnav antenna"]
-[9.218634605407715, 6.651856422424316, "[TT] Position Knowledge of Imagery of the S/C = 9 m"]
-[7.539315700531006, -0.6798762083053589, "[FF] Image Capture Date of the ICEYE-X2 = Four days after the satellite's launch"]
-[4.948766708374023, 0.42821866273880005, "[TT] Launch Date of the CASSIOPE = 29 Sep 2013"]
-[10.79586410522461, 0.715955913066864, "[FF] Oblateness of the Kepler 11145123 = Less than implied by its rotation rate"]
-[8.187423706054688, 7.774505138397217, "[TT] Detector Size of the HSC-III optics subsystem = 640 x 480 pixels"]
-[14.275014877319336, 3.093482494354248, "[TT] Mass of the ZACube-2 = 4 kg"]
-[5.986603736877441, -2.337571144104004, "[TT] Angular Drift of the Kondor-E = <0.001\u00ba/s"]
-[9.284626960754395, -0.4802982807159424, "[TT] Perigee of the GEOS-1 = 1113 km"]
-[6.922149181365967, 6.4383931159973145, "[TT] Time Constant of the Slow Shaper = ~1 \u00b5s"]
-[12.748122215270996, 7.438068389892578, "[TT] Power Consumption of the Spectral bands = 161 W for imaging, 73 W for standby"]
-[8.915611267089844, 4.804787635803223, "[TT] Accuracy of the Horizon sensor = 0.06\u00ba (3\u03c3)"]
-[6.819732666015625, 5.620540618896484, "[TT] Value of the System Availability = > 0.82"]
-[9.2318115234375, 0.21296562254428864, "[TT] Tower Height (Asian side) of the Yavuz Sultan Selim Bridge = 318 m"]
-[6.402050971984863, 4.659565448760986, "[FF] Operation of the Payload Data = Continuous throughout the mission life"]
-[7.261566638946533, 4.173016548156738, "[FF] Unknown of the NanoRacks Kaber system = Unknown"]
-[9.24112606048584, 7.767429351806641, "[TT] Focal Length of the Pushbroom imager = 5131 mm"]
-[10.192062377929688, 6.998587131500244, "[TT] Cross-Track Speed of the WTS1 and WTS2 = ~2 km/s"]
-[13.793928146362305, 3.0398366451263428, "[TT] Mass of the Plato\u2019s payload = 600 kg"]
-[4.2778730392456055, 7.180041790008545, "[TT] Signal Frequency of the Ground Station Antenna System = 8200.5 MHz"]
-[7.049200534820557, 1.8282815217971802, "[FF] Benefits Categories of the Landsat 7 = Technical, Scientific, Programmatic, Organizational"]
-[5.72874641418457, 4.722381591796875, "[FF] Data Transmission of the EDRS = User data will be transmitted from LEO user satellites to either of the EDRS payloads (i.e., EDRS-A, EDRS-C) and relayed to the DGS and/or FLGS/B-FLGS on the ground"]
-[10.071324348449707, -1.5525799989700317, "[TT] Inclination of the INTEGRAL = 52.246\u00ba"]
-[9.151479721069336, 2.977344512939453, "[FF] Formation of the Solar System = Violent wind of particles"]
-[7.196752548217773, 2.20755672454834, "[FF] Science Instruments of the Landsat-9 = Operational Land Imager 2 (OLI-2) and the Thermal Infrared Sensor 2 (TIRS-2)"]
-[7.399170398712158, 1.6554573774337769, "[TT] Latency of the Argo buoys = 1 day"]
-[8.054243087768555, 5.8464837074279785, "[TT] Swath Width of the JPL Microwave Radiometer = 9 km"]
-[7.764584064483643, 2.2425193786621094, "[TT] Data Coverage of the AMSU = Vertical temperature profiles up to 50 km"]
-[11.6725435256958, 6.6418046951293945, "[TT] Energy Measurement Range for Protons of the Telescope 1 = 0.05 and 25 MeV"]
-[5.477346897125244, 4.21258544921875, "[TT] Bus Design of the ERG = Small science satellite bus design"]
-[5.709844589233398, 1.0324517488479614, "[FF] NASA Feature Date of the IBEX = 5 August 2020"]
-[10.621284484863281, 7.314952850341797, "[TT] Swath Width of the Instrument = 2500 km"]
-[6.614617347717285, -0.2831162214279175, "[TT] Slew Maneuvers Frequency of the RADARSAT-2 = 150 times a month"]
-[6.929018497467041, 0.9248405694961548, "[FF] Mission of the Kepler = K2"]
-[5.181509971618652, 2.7583301067352295, "[TT] Designing Institution of the WeissSat 1 = Weiss School"]
-[5.160637378692627, 3.3267276287078857, "[TT] Manufacturer of the BEPT = Bradford Engineering"]
-[7.361018657684326, 4.629014492034912, "[FF] Function of the MPACS = Attitude control of the spacecraft"]
-[9.717443466186523, -0.5311052203178406, "[TT] Altitude of the STPSat-3 = 500 km"]
-[4.8314948081970215, 0.5333561301231384, "[TT] Launch Date of the BRO-1 = 20 August 2019"]
-[3.771984100341797, -0.7307466268539429, "[TT] Location of the NCLE = Low Earth Orbit"]
-[7.961119651794434, -2.5821070671081543, "[TT] Imaging Wavelength of the GOLD = 135.6 nm"]
-[11.43908405303955, 5.791906356811523, "[TT] Structure of the Schiaparelli = Aluminum sandwich with CFRP skins"]
-[10.633318901062012, 3.218879461288452, "[TT] Quantity of the AMICalSat = 1"]
-[7.387883186340332, 8.749770164489746, "[TT] Band 4 of the MSS Instrument = 0.8 - 1.1 \u00b5m"]
-[5.015363693237305, 0.7507078647613525, "[FF] Completion Date of the CMIP6 = Recent"]
-[9.616146087646484, 7.024267196655273, "[TT] Resolution of the KLIMAT = 3 km x 3 km"]
-[6.126037120819092, 5.272120952606201, "[FF] Function of the RFDN = Route the RF signal"]
-[6.044887542724609, 6.574344158172607, "[FF] Layout of the Transponder = Downconverter, LNA, RF switch matrix, Upconverter, channel amplifier, TWT"]
-[4.4073028564453125, 3.070981502532959, "[TT] Operation Location of the Ground Segment = CONAE Control Center at Cordoba, Argentina"]
-[10.578276634216309, 4.997742652893066, "[TT] Spacecraft Potential of the Langmuir Probe = \u00b15 V"]
-[7.8524489402771, 6.27137565612793, "[TT] Imaging Opportunity of the R3 = Landsat equivalent time-of-day"]
-[8.377355575561523, 8.147175788879395, "[FF] Spectral Resolution of the ABI = Increased"]
-[5.704823017120361, 3.963813304901123, "[TT] Payloads of the Spaceflight SSO-A: SmallSat Express = 64"]
-[5.8187255859375, 3.549499988555908, "[FF] Mission of the ArgoMoon = Demonstrate the ability to perform operations in close proximity of the ICPS"]
-[8.467585563659668, 1.93058180809021, "[TT] Roll of the RapidScat = Generally be less than 1\u00ba"]
-[5.503118991851807, 1.4715880155563354, "[FF] Commissioning Status of the EGG = Successful"]
-[6.886800765991211, 3.0005688667297363, "[FF] Data Sharing of the ISS LIS = National forecast offices, NOAA/AWA"]
-[4.557060241699219, 5.89277458190918, "[TT] Transmission Interval of the 406 MHz beacons = Approximately every 50 seconds"]
-[9.353474617004395, 7.051828861236572, "[TT] Angular Resolution of the IBEX-Lo sensor = 3.5\u00ba x 3.5\u00ba FWHM"]
-[7.865160942077637, 7.23874044418335, "[TT] Noise Equivalent Radiance of the FTS Interferometer = <0.5% of the radiance of a blackbody at 5800 K"]
-[5.2419257164001465, 7.22332239151001, "[TT] Downlink Data Rate of the DCS = 200 bit/s"]
-[7.314976692199707, 5.237481117248535, "[FF] Performance of the CIMERA = Testing and monitoring of Single Event Upsets (SEUs), Multiple Bit Upsets (MBUs), Single Event Functional Interrupts (SEFIs) and Latch-Ups"]
-[3.7630808353424072, 1.1444900035858154, "[TT] First Stage Length of the Falcon 9 = 42 m"]
-[8.364076614379883, 8.020368576049805, "[FF] IM Spacers of the Optic = Light Blue"]
-[9.231731414794922, 1.01323401927948, "[TT] Orbit Insertion Burn Duration of the Juno spacecraft = 30 minutes"]
-[10.444779396057129, 1.7473753690719604, "[FF] X-ray Emission of the Ophiuchus galaxy cluster = Reveals the edge of a large cavity, carved in the hot gas by the black hole jets"]
-[7.7638936042785645, 8.980545997619629, "[FF] Wavelength Bands of the Hrr. chaoviatoris = 470, 525, and 615 nm"]
-[7.270396709442139, 2.6959714889526367, "[FF] Deployed Teams of the Optical Instrumentation = University of Leiden, the University of Oldenburg in Germany and the ITC Faculty of Geo-Information Science and Earth Observation of the University of Twente"]
-[6.04347038269043, 4.343790531158447, "[TT] Reconfigurability of the Software = Can be reconfigured on orbit"]
-[5.99953556060791, 5.574921607971191, "[TT] Reprogrammable of the FPGA based parallel computing = Yes"]
-[9.624174118041992, 4.744266033172607, "[TT] Spin Stabilized Control of the Attitude control = \u00b1 3\u00ba"]
-[7.695584297180176, 6.541855812072754, "[TT] Image Capture Period of the DEIMOS-2 = 12 hours"]
-[4.859992980957031, 8.166455268859863, "[TT] Frequency Tuning Method of the CubeRRT RFE = Phased-locked oscillator (PLO) and sub-harmonic image rejection (IR) mixer"]
-[8.334114074707031, -0.6208478212356567, "[FF] Largest Iceberg of the Iceberg A-76 = No"]
-[8.318575859069824, 2.13358736038208, "[FF] Input Data of the CYGNSS = Winds"]
-[7.940853595733643, 1.0238133668899536, "[FF] Observation Tool of the Satellite = Global view of water mass changes"]
-[3.116736888885498, 2.292170763015747, "[FF] Data Contribution of the Sentinel-6 = Sea-level rise estimates"]
-[3.824392795562744, -1.1507498025894165, "[TT] Orbit Type of the SWFO-L1 = L1"]
-[10.648904800415039, 2.6965367794036865, "[TT] Orbit Altitude of the BlackSky microsatellite = Approximately 430 km"]
-[12.441083908081055, 0.5733504295349121, "[TT] Potential Mission Extension of the PLATO = 4 years"]
-[13.018205642700195, 7.1413774490356445, "[FF] Usage of the RADMON = Used sporadically and depending on the system's instantaneous power demands"]
-[6.51953649520874, 6.664549350738525, "[TT] Capture Time of the Bitgrabber = Up to 400 ms"]
-[6.972374439239502, -0.7004107236862183, "[TT] Orbital Period of the XMM-Newton = Exactly two times the Earth rotation period"]
-[5.4725446701049805, 6.390427589416504, "[FF] Data Storage of the EPICHyper Constellation = At least 4 GB on platform and 128 GB on payload"]
-[13.810419082641602, 6.942350387573242, "[TT] Required Voltage of the Future 1 MW-class spacecraft = 300 - 400 V"]
-[5.795828342437744, -0.8040384650230408, "[TT] Development Phase of the Spacebus Neo = Passed the Preliminary Design Review in early 2015"]
-[7.673053741455078, 2.1617648601531982, "[TT] Primary Use of the Band 5 = SST, day/night clouds"]
-[14.093971252441406, 4.039309501647949, "[TT] Mass of the Instrument = 25 kg"]
-[11.689815521240234, 4.342923641204834, "[TT] Size of the CICERO-4 = 3U"]
-[5.332070827484131, 1.6860450506210327, "[FF] Date of the Ground Segment Coordination Body Workshop = June 19-20, 2007"]
-[13.291227340698242, 5.482635021209717, "[TT] Solar Array Deployment Mechanism of the RISAT-1 = Employed"]
-[7.387079238891602, 4.120131969451904, "[FF] Capture and De-Orbit Capabilities of the ELSA-M = Innovative rendezvous, capture and de-orbit capabilities with a full-size constellation client"]
-[6.763607501983643, 3.4237987995147705, "[FF] Application of the AMS = Manned Interplanetary Flight"]
-[9.111985206604004, 4.348025321960449, "[TT] Sun Model of the ADCS = Computes sun vectors"]
-[8.693453788757324, 7.218564033508301, "[FF] Temporal Resolution of the GK-2A = Improved"]
-[10.014068603515625, 2.684583902359009, "[TT] Grapple Type of the NanoRacks Kaber Deployment System = Micro fixture"]
-[5.72343111038208, 8.016838073730469, "[TT] Inertial Mode Test Frequency of the MicroSCOPE = fep \u2248 1.7 x 10-4 Hz"]
-[5.07914924621582, 2.5994725227355957, "[FF] Design Center of the Mars Ascent Vehicle = NASA\u2019s Marshall Space Flight Center in Huntsville, Alabama"]
-[8.071406364440918, 8.170235633850098, "[FF] Sensor of the LunIR = New technology mid-wave infrared camera and micro-cryocooler"]
-[5.367396354675293, 8.741083145141602, "[TT] Bandwidth of the Band 4 = 545-565 nm"]
-[6.435739040374756, 3.4058992862701416, "[FF] Based on the Ball Configurable Platform of the WSF-M bus = Proven, agile spacecraft with 50 years of on-orbit operations for affordable remote sensing applications"]
-[8.756653785705566, 6.334955215454102, "[TT] Backscatter Coefficient Accuracy of the ALT Experiment = 1.0 dB"]
-[10.853997230529785, -0.3287711441516876, "[TT] Launch Year of the TanDEM-X = 2010"]
-[4.720495700836182, 0.007918904535472393, "[TT] End of Life Date of the GOSAT-2 = Dec 2023"]
-[5.453653812408447, 8.513189315795898, "[TT] Front-End Filters Bandwidth of the TOTEM SDR = 10 MHz"]
-[11.731290817260742, 3.268946647644043, "[FF] Thrusters of the ICESat-2 = Four 22 N thrusters and eight 4.5 N thrusters"]
-[5.2166829109191895, 2.074143886566162, "[TT] Status of the Vesselsat-1 & -2 = Still counting"]
-[7.114582061767578, 5.01814079284668, "[FF] Maximum Speed of the PistenBullys = Unknown"]
-[9.591218948364258, 7.029437065124512, "[TT] Spatial Resolution of the CERES = 20 km"]
-[11.045960426330566, 1.3582909107208252, "[FF] Purpose of the LISA = Study gravitational waves produced by merging stellar mass black holes, supermassive black holes, white dwarfs, neutron stars, or small black holes"]
-[3.475781202316284, 4.781637668609619, "[FF] Imaging Modes of the PAZ = Four"]
-[14.261617660522461, 2.98140287399292, "[TT] Mass of the BlackSky-1 = About 44 kg"]
-[7.981017589569092, 2.5075435638427734, "[TT] Measurement domain of the DMAC = Land"]
-[14.232730865478516, 3.2757070064544678, "[TT] Mass of the Test Masses = 1.96 kg"]
-[8.404094696044922, 7.432729721069336, "[TT] Type of the CLS detector unit = Cypress HAS2 CMOS APS detector"]
-[9.555700302124023, 4.144556999206543, "[TT] Type of the Magnetometer = Triaxial"]
-[8.345252990722656, 7.4756927490234375, "[TT] Sensor Layers of the STD = 8 double-sided silicon sensor layers"]
-[8.012751579284668, 1.852889060974121, "[FF] Rate of Change of the Evapotranspiration = Increased from 405 mm per year in 2003 to 444 mm per year in 2019"]
-[13.897880554199219, 3.247893810272217, "[TT] Mass of the FUNCube-1 = 1.2 kg"]
-[4.858193397521973, 0.4817054569721222, "[TT] Launch Date of the INSAT-2A = July 9, 1992"]
-[6.353652477264404, 1.7712000608444214, "[FF] URL of the HICO = http://cioss.coas.oregonstate.edu/CIOSS/Documents/HICO_Overview_Presentation.pdf"]
-[7.531935214996338, 5.272350788116455, "[FF] Components of the Receiver Module = OAP mirror, receiver housing, detector subassembly, cryoradiator"]
-[4.99932336807251, -0.05059957504272461, "[TT] Inauguration Date of the Kleos Headquarters = December 14, 2021"]
-[10.381298065185547, 7.583268642425537, "[TT] Band 13 Detector of the S-192 optomechanical scanner = Photoconductive HgCdTe"]
-[8.602224349975586, 7.743597984313965, "[FF] Purpose of the FREND = Fine-Resolution Epithermal Neutron Detector for ExoMars Project"]
-[4.575300693511963, 1.0298144817352295, "[TT] Launch Date of the SAOCOM-1A = 2015"]
-[5.1390180587768555, 3.240603446960449, "[TT] Manufacturer of the AMBER IOD-3 = Horizon Space Technologies (UK)"]
-[10.752257347106934, -1.131842851638794, "[TT] Altitude Descent of the SLATS = From 393 km to 270 km"]
-[4.949639320373535, 3.345414638519287, "[TT] Manufacturer of the OCO-2 = JPL"]
-[4.993430137634277, 0.5646319389343262, "[FF] Deployment Date of the DSX = 12 July 2019"]
-[5.752763271331787, -0.8959417343139648, "[TT] Solar Panels Lifespan of the InSight = Over four years"]
-[5.247548580169678, 3.3753514289855957, "[TT] Lead Contractor of the Heinrich Hertz = OHB System AG"]
-[10.693853378295898, 3.0991506576538086, "[TT] Form Factor of the PACE nanosatellite = 2U CubeSat standard"]
-[5.655253887176514, 4.503925800323486, "[FF] Impact of the 5G = Drive a convergence of fixed and mobile services, introduce a new set of technologies and standards, create a network of networks and facilitate communications between everyone and everything"]
-[5.349782466888428, 3.33988618850708, "[TT] Operator of the GRACE-FO = DLR/GSOC"]
-[4.734415054321289, 8.149194717407227, "[TT] Center Frequency of the L6 (LEX) = 1278.75 MHz"]
-[8.16618537902832, 8.780444145202637, "[TT] Performance Range of the UV-2 = 310 - 365 nm"]
-[9.847508430480957, 4.398501873016357, "[TT] Manufacturer of the Torque Rod = SSTL"]
-[8.051973342895508, 0.8587450981140137, "[FF] Number of Observers of the U.S. Drought Monitor program = More than 350 federal, state, and local observers"]
-[13.730231285095215, 2.41650652885437, "[TT] Cargo Mass of the SpaceX = 2,910 kg"]
-[5.341421604156494, 3.8808257579803467, "[TT] Number of Satellites of the FormoSat-7/COSMIC-2 = 6"]
-[7.309343338012695, 5.69032096862793, "[FF] Power Delivery of the PCM = Primary power to the Ancillary Electronics Module (AEM), power the camera, power the MCM"]
-[4.601429462432861, 8.047101974487305, "[TT] Frequency of the AltiKa = 35.75 GHz"]
-[6.860072612762451, 5.995916366577148, "[TT] 3He Separation of the LET = ~1%"]
-[4.8891119956970215, 7.317548751831055, "[TT] Safe Mode Uplink Data Rate of the ASTERIA Transceiver = 4 kbit/s"]
-[10.727119445800781, 1.7572251558303833, "[FF] Signal Trigger of the LIGO = Merging of two black holes"]
-[8.23625373840332, 4.4957275390625, "[FF] Orbit Design of the Chang'e-2 = Nonlinear system manifold design, low energy transfer orbit control technology"]
-[13.417216300964355, 2.9016757011413574, "[TT] Mass of the GRACE-FO Satellites = Around 580 kg"]
-[5.574326515197754, 5.1735429763793945, "[TT] Tracking System of the DORIS = CNES"]
-[6.135424613952637, 3.8331117630004883, "[FF] Development Status of the GOES-R = Under development"]
-[7.2305731773376465, 7.937788963317871, "[TT] Preamp feedback capacitance of the PHA = 5\u201375 pF"]
-[6.281031131744385, -1.1744956970214844, "[TT] Mission Duration of the GRACE = 2002 to 2017"]
-[8.075395584106445, 8.864328384399414, "[TT] Signal-to-Noise Ratio of the BIRCHES = >400"]
-[10.059881210327148, -1.5371850728988647, "[TT] Inclination of the ALOS-2 = 97.9\u00b0"]
-[12.102160453796387, -0.34818676114082336, "[FF] Launch Windows of the TESS spacecraft = 20 days per lunation"]
-[10.506022453308105, 4.73577880859375, "[TT] Hinge Type of the Closeout Panels = Spring loaded"]
-[6.410587310791016, -0.6859233379364014, "[TT] Orbit Time of the TanSat = 13:30 hours"]
-[3.8437020778656006, 5.457950592041016, "[TT] Minimum Radar Reflectivity of the CPR = -35 dBZ"]
-[5.159581184387207, 2.3266828060150146, "[TT] Mission Type of the Kondor-E = EO"]
-[6.18153715133667, 1.7002179622650146, "[FF] Configuration of the RISESat = Launch and deployed"]
-[4.744721412658691, 0.6080366373062134, "[FF] Launch Date of the HREP = Sept. 10, 2009"]
-[8.340164184570312, 7.3177409172058105, "[TT] Sensor of the Longitudinal System = Photodiode"]
-[2.918950080871582, 4.421402454376221, "[FF] Observation Performance of the PALSAR-2 = Improved"]
-[6.914005756378174, 7.765185356140137, "[TT] Reflector Size of the IMI = 6 m x 6 m"]
-[5.827184677124023, 0.4245019257068634, "[TT] Origin of the ERA = Europe"]
-[9.070985794067383, 5.676874160766602, "[TT] Steering Rate of the VISS = 2 Hz"]
-[12.055767059326172, -0.20135356485843658, "[FF] Observation Target of the TESS = L 98-59"]
-[8.216480255126953, 2.721522331237793, "[FF] Measurement Domain of the ERS-2 = Atmosphere, Ocean, Land, Gravity and Magnetic Fields, Snow & Ice"]
-[10.965899467468262, 3.7212727069854736, "[TT] Thrust Source of the LightSail-2 = Solar sails"]
-[11.241203308105469, 4.090940952301025, "[TT] Height of the CubeStack = 10 inches (25 cm)"]
-[10.125295639038086, -1.4675111770629883, "[TT] Orbit Inclination of the TARANIS = 98\u00ba"]
-[10.605563163757324, 2.042025089263916, "[FF] Detection of the X-ray pulsars = Detected"]
-[8.998865127563477, 4.326176643371582, "[FF] Attitude Measurement Devices of the Spacecraft = Miniature Spinning Sun Sensor (MSSS), two single-axis Inertial Reference Units (IRU), and a Flux Gate Magnetometer (FGM)"]
-[10.598063468933105, 1.8470134735107422, "[FF] Mission of the XMM-Newton = Observation of ultra-fast winds from supermassive black holes"]
-[4.928613662719727, 8.321736335754395, "[TT] Center Frequency of the Radiometer = 1.41 GHz"]
-[5.068732261657715, 2.1476328372955322, "[FF] Imagery Assessment of the TacSat-2 = Useful to the tactical operator"]
-[7.303987503051758, 3.50661563873291, "[FF] Conference Frequency of the JFCT = Once a week"]
-[5.556787490844727, 1.624326467514038, "[FF] Observation Frequency of the ALOS-4 = More frequent than ALOS-2"]
-[5.433229923248291, 2.6279444694519043, "[FF] Affiliation of the SwissCube = EPFL (Ecole Polytechnique Federale de Lausanne)"]
-[5.144681930541992, 8.425405502319336, "[TT] Bandwidth/Passband of the 3 = 400 MHz"]
-[7.814712047576904, 8.972752571105957, "[TT] Band Spacing of the VNIR = 11.4 nm"]
-[3.339245319366455, 2.3368613719940186, "[TT] Budget of the Copernicus Programme = EUR 4.3 billion"]
-[7.251042366027832, 5.8765387535095215, "[FF] Effect on Displacement Measurement of the Clock = Can be accounted for"]
-[6.370938777923584, -0.15888376533985138, "[FF] Shift Length of the On-call Operations = 12 hours"]
-[9.040228843688965, 8.522147178649902, "[TT] Wavelength of the Telescope = 0.6 - 29 \u00b5m"]
-[9.020570755004883, 7.323390007019043, "[TT] Image Resolution of the PMC = 10 m"]
-[6.419821739196777, 4.469852447509766, "[FF] Function of the SOC = Process and validate the data, and distribute products to the science team"]
-[8.297857284545898, -0.5538580417633057, "[FF] Sea Ice Coverage of the Global Change Observation Mission 1st \u2013 Water \u201cSHIZUKU\u201d = 19.47 million km2"]
-[6.043386459350586, -0.44187358021736145, "[TT] Demonstration Duration of the BEAM = Two years"]
-[5.293803691864014, 2.9739603996276855, "[TT] Platform of the Alphasat = Alphabus"]
-[7.643279552459717, 2.278841495513916, "[TT] Resolution of the Global coverage = 2.7 km"]
-[10.077372550964355, -1.5744173526763916, "[TT] Inclination of the CICERO-4 = 85\u00ba"]
-[14.268798828125, 3.2508704662323, "[TT] Mass of the CIVA = 3.4 kg"]
-[7.655374526977539, 6.6897783279418945, "[TT] Sensitivity of the eROSITA = High"]
-[5.6656718254089355, 6.994451522827148, "[TT] Data Input Data Rate of the Data Handling System = 336 Mbit/s"]
-[7.7325310707092285, 5.56332540512085, "[FF] Model of the SAC-D/NIRST Radiometer = Engineering Model"]
-[3.9196321964263916, 6.509136199951172, "[TT] Elevation of the Antenna = 20\u00ba~90\u00ba"]
-[4.707059860229492, 2.486773729324341, "[TT] Location of the Dasht-e Lut salt desert = Iran"]
-[5.555073261260986, 5.717405319213867, "[FF] MOPS of the TI C6701 DSP processor = Unknown"]
-[5.077878475189209, 3.0460925102233887, "[FF] Export Approval of the MMS = Provided by the French government"]
-[5.529755592346191, 5.077488422393799, "[FF] Data Handling Functionality of the NANOsky I = On-board data handling functionality exploits the advantages of the reliable hot redundant CAN networking with built-in error detection mechanisms and a ruggedized and fail-safe harness"]
-[12.963114738464355, 7.27987813949585, "[TT] Power Consumption of the LEID = 2.9 W"]
-[10.0254545211792, 2.904318332672119, "[FF] Launch Date of the TROPICS cubesats = 12 June 2022"]
-[10.270309448242188, 5.873233318328857, "[TT] Temperature Range of the Range of radiation temperature measured in bands 4-6 = 213-313 K"]
-[7.912184715270996, 6.357645034790039, "[FF] Function of the Imager Driver Board = Powering, configuring, and reading pixel data from the imager"]
-[5.575786590576172, 3.902717351913452, "[TT] Number of Partially Operational Satellites of the DMSP Satellite Series = 3 (F-13, F-15)"]
-[4.7649359703063965, 3.265756845474243, "[TT] Development Location of the EDRS Control Center = DLR's GSOC"]
-[5.979684352874756, 4.797558784484863, "[FF] Function of the Global Positioning System (GPS) Receiver = Receives tracking signals transmitted by GPS satellites"]
-[8.213820457458496, 2.0706281661987305, "[TT] Ephemeris Accuracy of the SeaSat = 50-70 cm"]
-[8.657999992370605, 4.792183876037598, "[TT] Acquisition Mode Duration of the Star Tracker = 2-3 seconds"]
-[8.31105899810791, 1.2539665699005127, "[TT] Build, Deployment, and Operations Cost of the RainCube = Less than $10 million"]
-[11.870888710021973, 5.422911643981934, "[TT] Size of the Instrument = 30 cm x 30.8 cm x 37 cm"]
-[9.623156547546387, 4.362297534942627, "[TT] Accuracy of the Magnetometer = 30 nT (3\u03c3)"]
-[9.940572738647461, -0.3502982556819916, "[TT] Altitude of the Satellite = 630 km"]
-[8.67708969116211, 5.738550662994385, "[TT] Function of the Coarse Pointer = Hemispherical tracking of the counter terminal"]
-[4.529356956481934, 3.8373217582702637, "[TT] Number of Satellites of the Galileo = 26"]
-[4.9510345458984375, 1.062447428703308, "[TT] Launch Year of the ALOS = 2006"]
-[5.186277866363525, 4.993046760559082, "[TT] Provider of the Two-frequency GPS (NOX) = DLR/GSOC"]
-[10.265098571777344, 3.441635847091675, "[FF] Mission Objectives of the ITUpSat-1 = Capture imagery of the CMOS payload and to study the behavior of the passive stabilization system of the CubeSat"]
-[3.7566940784454346, 6.397400379180908, "[TT] Antenna Quantity of the MC3 CGA = 2"]
-[9.207402229309082, 3.9158661365509033, "[FF] Components of the BF-Analyzer = Electric field antenna, magnetic field antenna, Ion probe"]
-[11.353453636169434, 2.763230323791504, "[TT] Total Mass of the Microsatellite = 40 kg"]
-[11.820231437683105, 6.713753700256348, "[TT] Energy Range of the EPI-Hi = MeV"]
-[10.096738815307617, 3.11240553855896, "[FF] Development Workshop of the UNISAT = 5th Annual CubeSat Developers' Workshop"]
-[4.484996318817139, 0.6903685927391052, "[TT] Acceptance Date of the DMSP F-19 = August 19, 2014"]
-[4.550279140472412, 7.049358367919922, "[TT] Data Downlink Band of the SWFO-L1 = X-band"]
-[5.99634313583374, 2.93597674369812, "[TT] Deployment Location of the ECOSTRESS = JEM (Japanese Experiment Module) External Facility on the ISS"]
-[9.832893371582031, 8.223315238952637, "[TT] FOV of the Telescope = 4.4\u00ba"]
-[6.08935022354126, 4.175556659698486, "[TT] Command and Control of the COSMOS Software = Native OS programs"]
-[7.969527721405029, -0.3815888464450836, "[TT] Annual Maximum Extent Timeframe of the Arctic Sea Ice = February and April"]
-[5.649824619293213, 5.22892951965332, "[TT] Setup Time of the Mobile IP = ~50 ms"]
-[6.870302200317383, -0.5178899765014648, "[TT] Orbital Period of the OceanSat-1 = 99.31 min"]
-[9.67408561706543, 8.130279541015625, "[TT] Optics of the CIRC = f/1"]
-[5.274592876434326, 1.4876278638839722, "[TT] Report Recommendation of the SMAP = Recommended for implementation in the first phase of new missions (2010-2013)"]
-[8.560735702514648, 5.677580833435059, "[TT] Telemetered Data Accuracy of the Payload = 0.2\u00ba in all axes"]
-[7.277194023132324, 4.376312732696533, "[FF] Orbit Determination Method of the WEOS = Uses the Keplerian elements of the satellite which are estimated from its locations measured by the onboard GPS receiver"]
-[6.1583685874938965, -0.3563116788864136, "[TT] Revisit Time of the Platform = Within 3 days"]
-[3.277794599533081, 5.167681694030762, "[TT] Wind Direction Blur of the SAR Image = 180\u00b0"]
-[6.8762431144714355, 4.602832794189453, "[FF] Design Method of the LTI MIMO Controller = Optimization problem aimed to ensure the CL robustness to complex-valued model uncertainty, as well as uncertain parameters"]
-[8.052297592163086, 5.523715972900391, "[FF] Sensor Type of the RPA = Planar sensor with a circular aperture"]
-[5.709623336791992, 1.169339895248413, "[FF] Constellation Update Date of the Planet = 24 January 2021"]
-[11.078225135803223, 6.043246746063232, "[TT] Mask Material of the Optical Head = Steel"]
-[7.458895683288574, 2.1788716316223145, "[TT] Amazon Basin Size of the Biomass satellite = Over six million km2"]
-[3.16845440864563, 2.36362361907959, "[FF] Objective of the Sen2Coral = Preparation of the exploitation of the Sentinel-2 mission for coral reefs"]
-[10.429974555969238, 7.165360450744629, "[TT] CONUS Rectangle Width of the ABI = 5000 km"]
-[13.948634147644043, 7.124964714050293, "[FF] Power Bus System of the SpriteSat = Experienced a low voltage condition"]
-[5.842736721038818, 6.528263568878174, "[TT] Encryption of the TT&C = NSA Type-1/2 encryption"]
-[5.550634860992432, 5.597201824188232, "[TT] Processor of the Spacecraft = Xilinx Virtex 4FX / PowerPC405"]
-[8.153706550598145, 8.422542572021484, "[TT] Global MTF of the WPM = > 0.23 at 38.5 lp/mm for B13, B14 and B15 bands, and > 0.18 at 38.5 lp/mm for B16 band"]
-[8.124364852905273, 8.320253372192383, "[TT] IR Channels of the Spectrometer = 22 channels from 3.0 - 5.7 \u00b5m (1754-3330 cm -1 )"]
-[10.060620307922363, -1.539041519165039, "[TT] Orbit Inclination of the SeaSat = 108\u00ba"]
-[6.594123840332031, -2.046635389328003, "[FF] Launch Date of the Jason-3 = March 16, 2016"]
-[9.030439376831055, 3.1294026374816895, "[FF] Solar Activity Model of the SLATS = Marshall solar activity future estimation model"]
-[9.602643966674805, 8.246716499328613, "[TT] Field of View Directions of the CIRiS = Four orthogonal directions"]
-[9.712776184082031, 8.424973487854004, "[TT] FOV of the HIRES = 0.3\u00ba x 0.4\u00ba"]
-[7.054985046386719, 8.36043930053711, "[TT] Nominal SNR of the Band 1 = 1000"]
-[4.293549060821533, 7.56245231628418, "[TT] Uplink Frequency of the Iris Radio = Standard X-band"]
-[8.203429222106934, 7.907253742218018, "[FF] Purpose of the Resurs-DK1 = Multispectral and spectrozonal mapping of the Earth's surface in the visible and near IR bands"]
-[11.798567771911621, 3.248140811920166, "[TT] Thrusters of the AOCS = Eight 11 N canted thrusters"]
-[8.224517822265625, -0.48749834299087524, "[FF] 1981\u20132010 Average Extent of the Antarctic Sea Ice = 18.6 million km2"]
-[9.023029327392578, 3.0541000366210938, "[FF] Objectives of the EXIS = Solar flare warnings for communications and navigation"]
-[5.097553253173828, 1.0975404977798462, "[FF] Year of the PROBA-3 = 2013"]
-[10.628790855407715, 7.332678318023682, "[TT] Swath Width of the Instrument = 7-29 km"]
-[10.176712989807129, -0.47935882210731506, "[TT] Altitude of the ELaNa-4 CubeSats = 500 km"]
-[7.81655216217041, 8.634779930114746, "[TT] Spectral Band Centers of the Instrument = 415,750,900,950,1000 nm (VIS); 1000,1050,1250,1550 nm (NIR)"]
-[5.799403667449951, 0.9765784740447998, "[TT] Image Acquisition Date of the Dobbins = 14 Mar. 2013"]
-[8.632538795471191, 3.536968231201172, "[FF] Function of the TSIS Instrument = Measure the energy output from the sun and its interaction with the atmosphere"]
-[5.901988506317139, -0.12776528298854828, "[TT] Power On of the Smartphone = 45 minutes after deployment"]
-[13.978599548339844, 3.3093037605285645, "[TT] Mass of the Harness = 3 kg"]
-[3.897019147872925, 6.533749580383301, "[FF] Deployment Phases of the VDES Antenna = Two phases of approximately two seconds and 30 seconds duration"]
-[8.219354629516602, 4.265054702758789, "[TT] On Orbit Star Calibration of the Instrument = Once per week"]
-[8.296107292175293, 8.59483814239502, "[TT] SNR of the Spectrometer = Drops to rather low levels if a constant spectral sampling level is maintained"]
-[6.966982364654541, -0.6118025183677673, "[TT] Orbital Period of the Starshine = 90 minutes"]
-[7.879067897796631, -0.3845174312591553, "[TT] Peak of the Drift Ice Season = February"]
-[6.412769794464111, 5.121220588684082, "[TT] Communication of the LAGEOS = None"]
-[10.093326568603516, -2.67874813079834, "[TT] User Storage Capacity of the Astrium MMFU NAND-Flash SDR-SDRAM = 2.4 Tbit (EoL)"]
-[12.725591659545898, 3.8960225582122803, "[FF] Duration of the Reconnection Process = More than 10 RE"]
-[9.9116849899292, 7.695574760437012, "[TT] Scan Step Angle of the Telescope = 8 \u00b5rad step size"]
-[5.224607467651367, 0.3693261444568634, "[TT] Operation Start Date of the MAP-PACE = 14 December 2007"]
-[8.210698127746582, 2.525740623474121, "[TT] Measurement Category of the CATS = Cloud type, amount and cloud top temperature, Atmospheric Temperature Fields, Cloud particle properties and profile, Aerosols"]
-[5.833494663238525, 2.9470176696777344, "[TT] Primary Partner Agencies of the DASS = NASA, NOAA, USAF, and USCG"]
-[8.348127365112305, 6.429392337799072, "[TT] Type of the TEMPO = Spaceborne ultraviolet/visible light air quality spectrometer"]
-[8.12201976776123, 6.5701375007629395, "[TT] Imaging Camera of the DSCOVR satellite = Earth Polychromatic Imaging Camera"]
-[13.809500694274902, 2.6767144203186035, "[TT] Total Satellite Launch Mass of the Vega Rideshare Mission = 1,327 kg"]
-[8.493111610412598, 7.446232318878174, "[TT] Sensor Type of the Astro-APS = CMOS Active Pixel Sensor"]
-[7.920623302459717, 5.232125759124756, "[FF] Application of the FLLS = Position-monitoring, monitoring the relative positions between craft in the constellation, monitoring the structural distortion before, during, and after deployment"]
-[5.178255558013916, 4.92632532119751, "[TT] Model of the GPS Receiver = SGR-10"]
-[13.415682792663574, 6.92909049987793, "[TT] Power of the EDRS-C = 3 kW"]
-[8.399992942810059, 1.9458814859390259, "[FF] Swath Width of the ISS-RapidScat = Similar to the EUMETSAT ASCAT (Advanced Scatterometer)"]
-[6.350868225097656, 1.615660548210144, "[TT] Project Manager of the Europa Clipper = Jan Chodas"]
-[5.534887790679932, 6.5414204597473145, "[TT] Total Volume of Stored Data for One Orbital Revolution of the Onboard data collection and transmission system = 300 kByte"]
-[4.832081317901611, 0.5738943219184875, "[TT] Launch Year of the SORCE = 2003"]
-[11.409923553466797, 4.352985382080078, "[TT] Size of the Audacy-0 = 3U"]
-[7.084519863128662, 3.6990110874176025, "[FF] Issue of the PROBA-3 = 1"]
-[5.19896125793457, 1.3866660594940186, "[TT] Prototype Development Status of the ELSA-M = Ongoing"]
-[9.465914726257324, 6.18455696105957, "[FF] Angular Coverage of the STAFF/DWP = Polar(range/interval) = 180\u00ba/12 (IIMS), = 180\u00ba/9 (IES)"]
-[5.778905868530273, 7.183467864990234, "[TT] Data Increase of the VCM Mode = 60%"]
-[8.660303115844727, 4.7243971824646, "[TT] Quantity of the Star trackers (STR) = 3 on each S/C"]
-[10.285000801086426, 5.3945631980896, "[TT] Type of the Thermal control = Passive thermal control on the external surfaces"]
-[8.800430297851562, 1.877039909362793, "[TT] Strongest Winds of the Nor'easter = 78 miles per hour"]
-[6.053099632263184, 7.1362104415893555, "[TT] Data Collection Rate of the GIOVE = 1 Hz"]
-[14.66373062133789, 6.663992881774902, "[TT] Capacity of the Batteries = 4Ah"]
-[4.318113327026367, 2.366170644760132, "[TT] Launch Location of the RADARSAT-2 = Baikonur, Kazakhstan"]
-[7.102555274963379, 4.701203346252441, "[FF] Interest of the SDA = Algorithms and compute capabilities on orbit"]
-[6.62835168838501, 5.372021198272705, "[FF] Data Tagging of the CDMS = Time tag and spin phase tag"]
-[8.62514591217041, 3.7242565155029297, "[FF] Objective of the SOLCON-3 = Accurately measure the solar constant and identify variations in the value during a solar cycle"]
-[7.204938888549805, 3.221280097961426, "[FF] Instrument Concept of the GeoSTAR-III = Unknown"]
-[9.676304817199707, 4.331295490264893, "[FF] ADCS System of the DeorbitSail = Stabilized"]
-[4.546977996826172, 7.075960636138916, "[TT] Ka-band System of the STPSat-6 = Ability to be reconfigured on orbit"]
-[10.177214622497559, 8.215963363647461, "[TT] Bandwidth of the Aperture Function = 2D"]
-[6.692248344421387, 0.7791662812232971, "[FF] Image of the Week Date of the Herschel = Jan. 18, 2016"]
-[5.786352157592773, 4.718997478485107, "[FF] Link Direction of the Payload link configuration request = EDRS to LEO, LEO to EDRS, or bidirectional"]
-[8.567578315734863, 3.770287036895752, "[TT] Science Payload of the EDSN = EPISEM (Energetic Particle Integrating Space Environment Monitor)"]
-[8.466983795166016, 5.108838081359863, "[FF] EM Build Year of the GFO accelerometer = 2013"]
-[5.19242000579834, 0.6413832902908325, "[TT] Service Start Date of the Lightspeed Satellites = 2023"]
-[4.812040328979492, 4.334627628326416, "[FF] Phased-Array Technology of the SARah = Developed by Airbus DS GmbH"]
-[4.480248928070068, 4.232911586761475, "[TT] Number of Satellites of the SAR-Lupe Constellation = 5"]
-[4.76454496383667, 7.385685443878174, "[TT] Data Rate of the Ku-band transmitter = 10 Mbit/s"]
-[7.298951148986816, 7.654793739318848, "[FF] Purpose of the PHA = Improved dosimetry and measurement of linear energy transfer (LET) value"]
-[11.825003623962402, 6.712489604949951, "[FF] Composition Energy Range of the ECT Suite = Up to 50 keV for ions, from a few to 50 MeV/nucleon for ions"]
-[8.600259780883789, 3.6247875690460205, "[FF] Conference Presentation of the Solar Orbiter/METIS = The optimization of the inverted occulter"]
-[6.269466876983643, 8.066171646118164, "[TT] No of Passbands of the Channel 1 = 1"]
-[8.964966773986816, 4.524784564971924, "[TT] Attitude Control Subsystem of the TanSat = 3 sun sensors, 2 three-axial magnetometers, 2 star trackers, 2 gyros, 1 GPS receiver"]
-[8.83105182647705, 6.441186904907227, "[TT] Data Accuracy of the SLA-1 = Meter-level"]
-[6.731400012969971, 8.373679161071777, "[FF] Requirement of the Spectral Channel = >200"]
-[9.774648666381836, -0.5682840943336487, "[TT] Orbit Altitude of the TEMPO = 35,786 km"]
-[7.569340229034424, 5.4676713943481445, "[FF] Components of the PIC = Back-illuminated scene, projector, lenslets, PIC interferometers, detector, thermoelectric phase modulators, Fast-Steering Mirror, three-row mask"]
-[3.1208927631378174, 2.2388112545013428, "[FF] Glacier Monitoring of the Copernicus Sentinel-2 = Monitors changes in glacier mass, extents, trace area and length of glacier changes through time and derive surface velocity"]
-[10.943229675292969, 7.521347522735596, "[TT] Swath width of the MERSI = 2800 km"]
-[9.39935302734375, -0.4706748425960541, "[TT] Altitude Adjustment of the CryoSat-2 = Just more than half a mile (900 meters)"]
-[13.61750602722168, 5.475561141967773, "[TT] Type of the Solar Panels = Silicon cells"]
-[12.139589309692383, 6.113376617431641, "[TT] Number of Cosmic Rays Tracked of the Alpha Magnetic Spectrometer = More than 69 billion"]
-[5.636500358581543, 6.295041084289551, "[TT] AIS Message Latency of the AISSat-1 = < 1sec"]
-[4.818572521209717, -1.7567315101623535, "[TT] Attitude Transition of the Chang'e-2 = Twice"]
-[5.798166751861572, 8.17030143737793, "[TT] Footprint of the Millimeterwave receiver = 15 m"]
-[5.583553314208984, 5.6672282218933105, "[TT] Microcontroller of the TCA = P89C51"]
-[5.663362979888916, 5.390578269958496, "[TT] Delivery of the UDP = One-way only path through NASA firewall"]
-[6.891721248626709, 1.797476887702942, "[FF] Data Distribution of the Landsat-7 = ETM+ data will be distributed from the archive in an essentially raw form"]
-[8.30453109741211, 1.532345175743103, "[TT] Absolute Accuracy of the Precipitation over land ares = \u00b1 5 mm/hr"]
-[11.80311107635498, 3.2789180278778076, "[TT] Force of the Thrusters = 10 Newton"]
-[5.260888576507568, 2.398761510848999, "[TT] Mission Type of the ArgoMoon = EO"]
-[6.955492973327637, 4.346790313720703, "[FF] Unknown of the NBR = Unknown"]
-[3.596618175506592, 5.253218650817871, "[TT] Integration Distance of the Radar = 10 km"]
-[10.788333892822266, 4.000068664550781, "[TT] Module Assembly of the CanX-7 = Two decks"]
-[10.969998359680176, 6.338576316833496, "[TT] Mirror Surface Roughness of the SiC = A few angstrom (1\u00c5= 10-10 m)"]
-[5.368139266967773, 5.652101993560791, "[TT] SCI ports of the STRV-2 DHS = Six RS-422, MIL-STD-1553 S/C bus"]
-[13.902342796325684, 3.105802059173584, "[TT] Payload Mass of the Priroda module = About 7,000 kg"]
-[11.447698593139648, 3.373401403427124, "[FF] Objective of the UniSat-2 = Develop and demonstrate an onboard micro-propulsion system"]
-[9.099797248840332, 4.4483866691589355, "[FF] Orientation of the OSC = Same face facing the Sun at all times"]
-[5.901951313018799, -0.8386703133583069, "[TT] Goal Life of the Spacecraft = 7 years"]
-[6.364273548126221, 1.891343116760254, "[FF] URL of the Arctide2017 = https://tinyurl.com/y2axpw8c"]
-[8.123672485351562, 8.265020370483398, "[FF] Design Drivers of the ACE-FTS = Sensitivity (SNR), Spectral Resolution, Large Spectral Coverage"]
-[4.783701419830322, 7.984261512756348, "[TT] Frequency of the Unit = 435 MHz"]
-[8.671682357788086, 8.453125, "[FF] Imaging Spectrometer of the PROBA = CHRIS"]
-[14.21887493133545, 3.2223575115203857, "[TT] Mass of the KaRIN = ~294 kg"]
-[6.856290817260742, 2.0154147148132324, "[FF] URL of the Hinode = http://www.isas.ac.jp/home/solar/"]
-[5.468653202056885, 7.206635475158691, "[TT] Data Transmission Rate of the OCM = 0.3 Mbit/s"]
-[8.16557788848877, 2.252336263656616, "[FF] Purpose of the Temporal Experiment for Storms and Tropical Systems (TEMPEST) = Investigate atmospheric humidity"]
-[6.580878257751465, 1.6970175504684448, "[FF] URL of the Rosetta = http://www.esa.int/Our_Activities/Space_Science/Rosetta/Rosetta_factsheet"]
-[5.802224159240723, 2.0933666229248047, "[FF] Mission Location of the eROSITA = Russia"]
-[5.768518447875977, 0.6226953268051147, "[TT] Quarantine Period of the Probe = Two weeks"]
-[8.28628921508789, 5.763195991516113, "[FF] Accuracy of the Geoid = cm"]
-[5.313289642333984, 1.0113643407821655, "[FF] Office Launch Date of the ESA = 9 February 2022"]
-[6.4737396240234375, 7.616746425628662, "[TT] Data Quantization of the AATSR = 12 bit"]
-[5.168909072875977, 4.861603260040283, "[TT] Type of the GPS Receiver = NovAtel OEMV-1"]
-[7.834832668304443, 6.845911502838135, "[FF] Test Status of the Interferometer = Completed"]
-[6.173373699188232, 4.4377007484436035, "[FF] Original Purpose of the ERNO-Box = Assess a new processor and other technologies in the space environment"]
-[7.744107246398926, 6.639382839202881, "[TT] 20 ms / 16 energy steps of the Time Resolution = Time resolution 20 ms / 16 energy steps"]
-[10.105825424194336, 1.3411325216293335, "[FF] Number of Stellar Streams of the Milky Way = At least 70"]
-[8.561766624450684, 5.50419807434082, "[TT]  of the Landing Accuracy = 10 m"]
-[11.948512077331543, 5.005675315856934, "[TT] Size of the CPD = 260 mm x 199 mm x 113 mm"]
-[9.068721771240234, 6.654228210449219, "[FF] Acceleration Distance of the Small density \u201cblobs\u201d = Up to 30 Rs"]
-[11.770295143127441, 6.775575160980225, "[TT] Energy Range of the DSX Sensor Suite = < 1000 keV"]
-[7.904077529907227, 1.098588228225708, "[TT] Start Date of the Cooks Peak fire = April 17"]
-[7.3583574295043945, 5.825387954711914, "[TT] Absolute Radiometric Error of the MSU-SK = 1%"]
-[6.234440803527832, 4.934273719787598, "[FF] No Influence Condition Monitoring of the Bus system = Required"]
-[8.045703887939453, 8.748395919799805, "[TT] Spectral Range of the VIS = 403-803 nm"]
-[4.7833638191223145, -0.8219811320304871, "[TT] Capture Time of the Dragon spacecraft = 5:57 a.m. EST"]
-[5.037604808807373, 0.7434186339378357, "[FF] Year of the WISE = 2003"]
-[10.456618309020996, 3.2483582496643066, "[TT] Toolkit of the Ubotica CogniSAT-XE1TM CubeSat Board = Intel\u00ae\u2019s OpenVINO\u2122"]
-[6.221091270446777, 7.9792866706848145, "[TT] Channels of the LAGRANGE receiver = 12"]
-[6.803374290466309, 6.004215240478516, "[TT] Multi-Look of the Capella = 10"]
-[10.017255783081055, 0.2087147831916809, "[TT] Closest Approach Distance of the GRACE Satellites = 406 meters"]
-[9.298629760742188, 10.731118202209473, "[TT] Polarization of the ICI-3 = V"]
-[8.94072151184082, 5.668768405914307, "[TT] Pointing Accuracy of the S/C = Within 5-10\u00ba"]
-[11.092081069946289, 5.780726432800293, "[TT] Alu Shielding Thickness of the CID = 2 mm"]
-[5.450860977172852, 5.44154691696167, "[TT] Architecture of the MOC = An evolution of the proven design currently supporting SAC-C"]
-[7.020960330963135, 2.278057813644409, "[FF] URL of the Medium Energy Neutral Atom (MENA) Imager = http://twins.swri.edu/pubs/MENA.pdf"]
-[12.475769996643066, 7.547451972961426, "[TT] Power of the Pushbroom Imager = 250 W"]
-[8.757649421691895, -0.12400934100151062, "[TT] Expected Distance from Earth in 2029 of the Chang'e-2 = 7 million km"]
-[4.892731666564941, 0.21294166147708893, "[TT] Launch Date of the NeuSAR = June 30, 2022"]
-[5.715809345245361, 6.948333263397217, "[TT] Data Transmission Rate of the Telescope = 333 kbit/s (normal), 2.7 Mbit/s (burst mode)"]
-[5.074653148651123, 4.381799221038818, "[FF] Number of Passes over Stations of the SPOT-6 = 4 passes over the Toulouse station and 8 passes over the Kiruna station"]
-[8.423357963562012, 5.558650493621826, "[TT] Position Accuracy of the GPS = 20-30 m"]
-[6.353979110717773, 8.054586410522461, "[TT] Number of Regional Channels of the DCP = Up to 33"]
-[6.377317428588867, 1.9703634977340698, "[FF] URL of the DEIMOS-2 = http://www.elecnor.es/en/press/press/elecnor-deimos-inaugurates-its-puertollano-integration-and-satellite-operation-centre-and-presents-its-deimos-2-satellit"]
-[3.097583055496216, 4.360007286071777, "[FF] Coherence Change Detection of the TerraSAR-X = Significantly Enhanced"]
-[10.47722053527832, 2.2113795280456543, "[FF] Duration of Brightness Change of the X-ray Source = About five minutes"]
-[11.98840045928955, 6.5751824378967285, "[FF] Energy Range of the AMS = 0.5 to 200 GeV"]
-[6.872784614562988, 5.0434980392456055, "[FF] Function of the MSPR-2 = Provides power and communication interface to each experiment device"]
-[12.119638442993164, 6.793292999267578, "[TT] Bias Voltage of the SDEA = Typically < 10 V"]
-[14.109944343566895, 7.219448566436768, "[TT] Bus Voltage of the BDR = 70 V"]
-[6.460180759429932, 4.736929893493652, "[FF] Data Delivery of the LIS = Once operations begin"]
-[3.6486072540283203, 6.599569320678711, "[TT] Shortest Adjacent Feed Distance of the L/S/C tri-frequency feed array = 0.13 m"]
-[5.459052085876465, 3.8656246662139893, "[TT] Planned Number of Satellites for 2020 of the Satellite Constellation = 16"]
-[6.983480930328369, 1.5422914028167725, "[FF] Observational Target of the James Webb Space Telescope = Rocky Exoplanets"]
-[7.752842903137207, 0.7606936097145081, "[TT] Spatial Resolution of the Lunar Flashlight = 10 km or better"]
-[7.571073532104492, 2.193612575531006, "[TT] Target Coverage of the OneWeb = All regions north of 50 degrees latitude"]
-[11.55176067352295, 4.905476093292236, "[TT] Effective Diameter of the RIS = 0.5 m"]
-[8.596975326538086, 3.428237199783325, "[TT] Measurement of the SSUSI = UV radiation from the Earth's atmosphere and ionosphere"]
-[4.666767120361328, 0.725016176700592, "[TT] Mission End Date of the COSPAS GOMS-1 = Nov. 2000"]
-[9.07193374633789, 7.405854225158691, "[TT] Spatial Resolution of the MWIR Imager = 3.5 m"]
-[5.063011646270752, 8.433331489562988, "[TT] Spectral range of the MWTS = 50-57 GHz"]
-[11.467606544494629, 5.6477484703063965, "[FF] Admissible Yield of the Inconel alloy = 400 MPa"]
-[5.487203598022461, 6.766250133514404, "[TT] Downlink Frequency of the Data = Every 13.7 days at perigee"]
-[7.9463725090026855, 1.1014046669006348, "[FF] Date of the Manam Volcano, Papua New Guinea = 30 May 2022"]
-[4.1837005615234375, 6.967717170715332, "[TT] Downlink Frequency of the Ground Station = S-band, X-band"]
-[8.415019035339355, 5.524227142333984, "[TT] Standard Deviation of Error (Slant-range) of the Geolocation Testing = 0.1-0.3 m"]
-[11.00149917602539, 7.358974933624268, "[TT] Swath Width of the Satellite = 48 km"]
-[4.594187259674072, 2.916609287261963, "[TT] Flight Control Team Location of the Gaia = ESA's ESOC mission control center in Darmstadt"]
-[11.567829132080078, 4.729333877563477, "[TT] Size of the OS = Basketball-size"]
-[14.256680488586426, 3.1835522651672363, "[TT] Mass of the DACS = 4.6 kg"]
-[3.454310894012451, -0.9110286235809326, "[TT] Orbit Type of the Satellite = Sun-synchronous dawn-dust orbit"]
-[5.280471324920654, 4.579675197601318, "[FF] Deployment Options of the Open5GCore Rel. 4 = Containers or virtual machines on top of a large number of virtualization environments"]
-[9.716053009033203, 4.215641498565674, "[TT] Quantity of the Magnetometers = 3"]
-[10.819562911987305, 1.39268958568573, "[FF] Mass of the Stars = As little as a tenth of our sun\u2019s mass"]
-[6.065013885498047, 3.892374038696289, "[FF] Definition of the Situation Awareness = The perception of the elements in the environment within a volume of time and space, the comprehension of their meaning and the projection of their status in the near future"]
-[5.558753490447998, 1.7152695655822754, "[FF] Activities of the Commissioning and IOT = Initialization and commissioning"]
-[6.251026153564453, 5.663303852081299, "[TT] Redundant Branches of the CGS = 2"]
-[8.999166488647461, 6.719404220581055, "[TT] Main Imager Spatial Resolution of the PROBA-1 = 17 m"]
-[4.999722480773926, 3.3543787002563477, "[FF] Manufacturer of the CDHS = University of Tartu"]
-[4.870556354522705, 7.294275283813477, "[TT] Back-up Channel Data Rates (Downlink) of the RF Communications = 38.8 kbit/s"]
-[5.796102046966553, 0.595090389251709, "[TT] Data Production Period of the IMERG = Seven day period from 23-30 November 2018"]
-[8.046133995056152, 5.814499378204346, "[FF] Attachment Method of the LF Reflectometer Assembly = Semi-kinematic"]
-[9.088741302490234, 7.5683979988098145, "[TT] Spatial Resolution of the Multispectral Camera = 16 m"]
-[8.069084167480469, 5.390784740447998, "[TT] Testing Range of the FLLS = 140 m"]
-[7.149236679077148, 0.05953836441040039, "[TT] Age of the Manatee Nebula = Around 30,000 years"]
-[4.453854084014893, 7.8282670974731445, "[TT] Frequency of the Ka-band = 32 GHz"]
-[5.532365798950195, 0.5138098001480103, "[TT] Extended Mission Start Date of the SELENE/Kaguya = November 2008"]
-[7.865790367126465, -2.48628830909729, "[TT] Thermosphere Temperature Increase of the GOLD = Over 160 \u00b0F (90 \u00b0C)"]
-[10.001904487609863, 2.9111571311950684, "[TT] Launch Date of the AQT-D 3U CubeSat = 24 September 2019"]
-[5.345001697540283, 5.405540466308594, "[TT] Receiver Usability of the STRV-1a = One receiver on each spacecraft remained usable"]
-[5.39633321762085, 6.852054119110107, "[TT] Data Rate of the MTG-S Spacecraft = Around 60 Mbit/s"]
-[6.111062049865723, 5.528443336486816, "[FF] Redundancy of the KBR = The IPU, SPU, KBR and ACC are internally redundant, and the ultra-stable oscillator (USO) is redundant"]
-[5.212786674499512, 4.943536758422852, "[TT] Primary System of the GPS = GPS"]
-[10.87171459197998, 3.9405910968780518, "[TT] Formation Control of the TSX and TDX = Precise"]
-[9.928863525390625, 1.5259225368499756, "[FF] Function of the Gaia = Scans the sky"]
-[4.326679229736328, 0.7728105783462524, "[TT] Cease Transmitting Weather Data of the DMSP F-19 = August 4, 2017"]
-[11.2611665725708, 5.347686767578125, "[TT] Quantity of Scintillators of the Absorber = 28"]
-[9.748152732849121, 8.460210800170898, "[TT] FOV of the WPM = \u00b128.63\u00ba"]
-[11.386686325073242, 0.7147172689437866, "[TT] Orbit Period of the AU Mic b = 8.5 days"]
-[7.427950859069824, 2.1342484951019287, "[TT] Earth Coverage of the Planet = At least 85% of the Earth\u2019s landmass every 15 days"]
-[6.4232401847839355, 1.5397439002990723, "[FF] URL of the MICROSCOPE = http://missions-scientifiques.cnes.fr/MICROSCOPE/GP_segment_sol.htm"]
-[5.183538913726807, 0.6785932779312134, "[FF] Launch Date of the CanX-2 = 28 April 2008"]
-[7.980767250061035, 0.8440504670143127, "[FF] Reporting Date of the U.S. Drought Monitor program = August 11, 2020"]
-[8.089900970458984, 6.861632823944092, "[TT] Maximum Range of the TDC-GPX = 7 \u00b5s"]
-[6.090656280517578, 6.42321252822876, "[TT] Data Collection to Estimate Extension of the C/NOFS = 24 hours"]
-[13.325132369995117, 5.489657878875732, "[FF] Type of the Solar Arrays = Articulating"]
-[14.065195083618164, 3.9751315116882324, "[TT] Mass of the Instrument = < 10 kg (with MI)"]
-[9.689224243164062, -0.5569065809249878, "[TT] Altitude of the Orbit = 720 km"]
-[6.532381057739258, 5.181152820587158, "[FF] Algorithm Design Status of the FY-4A = Completed"]
-[5.9039201736450195, -0.65199214220047, "[TT] Operational Lifetime of the MicroMAS-1 = One year"]
-[5.391087532043457, 2.5193991661071777, "[TT] Information Provider of the SwissCube = Muriel Richard of EPFL"]
-[7.618009567260742, 5.710778713226318, "[FF] Control of the Scanning LIDAR = Predefined timeline"]
-[6.562587261199951, 3.216233015060425, "[FF] Revisit Time of the BlackSky Gen-2 satellites = One-hour average dawn-to-dusk imaging revisits"]
-[10.309466361999512, 1.5517734289169312, "[FF] Formation Scenario of the Black Hole = Runaway merger of massive stars lying within dense star clusters"]
-[8.299818992614746, 4.526752471923828, "[TT] Techniques of the LARES = SLR, VLBI, GNSS"]
-[5.199040412902832, 2.715074300765991, "[TT] Affiliation of the MRM = National Central University"]
-[4.670197486877441, 1.7570722103118896, "[FF] Presentation Date of the Navy GEOSAT follow-on altimeter = Feb. 1-8, 1997"]
-[8.699552536010742, 7.690489292144775, "[TT] Pixel Size of the LISS-3 = 13 \u00b5m"]
-[4.945310115814209, 1.2921130657196045, "[TT] Patent Date of the DST = June 1, 2007"]
-[9.424117088317871, 4.883805274963379, "[FF] Angular Momentum Management of the AOCS = Relies solely upon EPPS in the nominal modes"]
-[8.119400978088379, 6.526079177856445, "[FF] Technical Requirements Document of the GOES Advanced Baseline Imager = S-415-200, March 2000"]
-[8.272905349731445, 8.661422729492188, "[TT] Linearity of the UV/VIS Spectrometer = 0.5%"]
-[6.176362991333008, 3.217241048812866, "[TT] Control of the Dextre = NASA"]
-[14.180937767028809, 3.2632365226745605, "[TT] Mass of the CanX-7 = 3.5 kg"]
-[8.68143081665039, 7.625243663787842, "[TT] MS Image Detector Size of the OIS = 2048 pixels x 2048 lines"]
-[7.128859043121338, 6.030245304107666, "[FF] Quantity in Lot of the CCRs = 10"]
-[8.55406665802002, 1.3574494123458862, "[FF] Purpose of the Aquarius = Provide maps of salt concentration on the ocean surface"]
-[7.06721305847168, 3.5189270973205566, "[FF] URL of the PROBA-3 = http://www.sffmt2013.org/PPAbstract/4067p.pdf"]
-[11.422625541687012, 3.5054056644439697, "[FF] Functions of the Electric Propulsion Test Subsystem = Measurement of the plasma parameters around the satellite (exhaust plume) during the operation of electric propulsion, Directly measure pollution caused by electric propulsion, Monitor satellite floating potentials influenced by electric propulsion"]
-[5.149799823760986, 5.193124294281006, "[TT] Frequency Tracking of the Phoenix GPS Receivers = Single-frequency"]
-[9.651089668273926, 7.087656497955322, "[TT] Spatial Resolution of the OLS = 560 metres in fine mode and 2.7 km in smooth mode"]
-[8.110857963562012, 2.6492414474487305, "[TT] Measurement Domain of the MTSAT = Atmosphere, Ocean"]
-[7.099660396575928, 0.2751999497413635, "[TT] Overpass Time Offset of the CloudSat = About 4 minutes"]
-[13.192200660705566, 5.21170711517334, "[TT] Panel Size of the Solar Panels = 432 mm x 243 mm"]
-[5.435781478881836, 6.9502949714660645, "[TT] Data Download of the STRaND-1 = 274 kB over 65 k packets"]
-[7.9635748863220215, 8.54619026184082, "[TT] Spectral Range of the SWIR bands = Shortwave (SW) infrared (IR) bands include: 940, 1038, 1250, 1378, 1615, 2130, and 2260 nm"]
-[8.595807075500488, 3.787116050720215, "[FF] Objective of the APD = Observe the low energy charged particle density distribution in LEO (Low Earth Orbit)"]
-[7.381246089935303, 6.778698921203613, "[FF] Temperature Measurement of the FIBOS = Laser beam wavelengths"]
-[10.19485092163086, 5.543962001800537, "[TT] Thermal Design of the Antennas, Solar Array, Sun Sensors, MLI = Dedicated high temperature technologies"]
-[14.680876731872559, 6.6381449699401855, "[TT] Quantity of the Li-Ion Battery = 1"]
-[10.31838321685791, 2.3350048065185547, "[TT] Optics Presenter of the Imaging X-ray Polarimetry Explorer = Brian D. Ramsey"]
-[7.85518217086792, 4.234010696411133, "[FF] Types of the Rendezvous Maneuvers = Radial (R-bar) or velocity (V-bar) burns"]
-[9.23782730102539, 6.959916591644287, "[TT] Imagery Resolution of the ALOS-3 = 0.8 m"]
-[7.305910110473633, 5.019820213317871, "[FF] Component of the Umbilical Mechanism Assembly (UMA) = Unknown"]
-[6.724813938140869, 4.501039028167725, "[FF] Design Verification of the FDIR = Standalone or integrated GNC/FDIR test environments"]
-[7.800018310546875, 5.878231525421143, "[TT] Type of the Severyanin-M = Imaging multi-spectral radiometers (passive microwave)"]
-[7.765106678009033, 0.03552236407995224, "[FF] Date of the Mackenzie River = 01 October 2021"]
-[6.984457492828369, 4.791158199310303, "[FF] Tests of the Characterization Process = Repeatability and reproducibility tests"]
-[9.232486724853516, 0.22486771643161774, "[TT] Total Length of the Yavuz Sultan Selim Bridge = 2,164 m"]
-[7.82696008682251, 7.17959451675415, "[TT] Frame Rate of the intensified sprite imager = 180 frames/s"]
-[4.798079013824463, 0.012670653872191906, "[TT] End of Life Date of the GF-3 = 10 Aug 2024"]
-[6.122272968292236, 0.7257198095321655, "[FF] Publication Date of the SpooQy-1 = 2017"]
-[6.968964576721191, -0.7686280012130737, "[TT] Orbit Period of the TOI 700 c = 16 days"]
-[5.713490009307861, 4.461226940155029, "[FF] Ground Segment of the EDRS = EDRS Services"]
-[10.964641571044922, 1.0881853103637695, "[TT] Mass Accuracy of the Planets = 10%"]
-[13.6908540725708, 2.792922019958496, "[TT] Launch Mass of the Satellite = ~5.8 tons"]
-[7.003662586212158, 2.555198907852173, "[FF] Applications of the LAPAN-TUBSAT = Disaster monitoring, vegetation monitoring"]
-[7.937777996063232, 9.1279296875, "[TT] Wavelength of the OH (surface or structural) = 3.6 \u00b5m"]
-[6.843094825744629, 2.027228832244873, "[FF] URL of the STEREO = http://science.nasa.gov/science-news/science-at-nasa/2011/06feb_fullsun/"]
-[5.042479991912842, 0.5984290242195129, "[FF] Deactivation Date of the GOES-10 = Dec. 7, 2009"]
-[6.295438766479492, -1.2650063037872314, "[TT] Preliminary Design Review Date of the GRACE = January"]
-[5.5306715965271, 3.155385732650757, "[TT] Shareholding of the Eutelsat Communications = 22.9%"]
-[7.02830696105957, 8.140091896057129, "[TT] Noise performance of the Channel = 0.25 K at 300 K"]
-[4.881650447845459, 6.589061260223389, "[FF] Usage of the USRP = Access the RF signals, demodulate, and decode the signals"]
-[7.803884506225586, 1.9817582368850708, "[FF] Mission Goals of the PACE = Making climate-quality global ocean color measurements, understanding the carbon cycle and global ocean ecology, determining the ocean\u2019s role in global biogeochemical cycling and ocean ecology in relation to climate change"]
-[10.697930335998535, 1.1114311218261719, "[TT] Size of the TOI 700 d = Earth-size"]
-[10.46042537689209, 3.3525197505950928, "[TT] Capability of the iADCS100 = Precisely pointing and slewing a 3U CubeSat"]
-[7.7115607261657715, 2.249696731567383, "[TT] Data Coverage of the Sounder = Clear sky region of the data-sparse Indian Ocean"]
-[13.142047882080078, 6.961556434631348, "[TT] Power of the Telescope = 100 W"]
-[10.617679595947266, 4.000258922576904, "[FF] Properties of the Cryogenic Fluid = Produces high thrust or acceleration"]
-[7.354129314422607, 5.814841270446777, "[TT] Energy Release Range for UV Flashes of the Tatiana-1 = 10 kJ - 1MJ"]
-[5.5535688400268555, 3.8683512210845947, "[TT] Access to Satellites of the Satellogic = 10 satellites"]
-[7.367580413818359, 2.0059897899627686, "[TT] Subject of the UMAMI Study = Bobtail squid and bacteria"]
-[6.626450538635254, 1.9003483057022095, "[FF] URL of the ExoMars = http://www.jpl.nasa.gov/news/news.php?feature=6663&utm_source=iContact&"]
-[10.448152542114258, 1.739700198173523, "[FF] Ability of the Black Hole = Pulling things toward it and blasting material away from itself"]
-[5.069741249084473, 7.008391857147217, "[TT] Brute bit rate (bit/s) of the Service downlink = 8,414"]
-[8.436629295349121, 6.029531955718994, "[FF] Ground Measurements of the TRUTHS = SI-traceable ground measurements of RadCalNet"]
-[8.020792961120605, 8.082605361938477, "[TT] Bandwidth of the Band Cameras = 5.0 nm"]
-[13.590326309204102, 5.48127555847168, "[TT] Total Number of Solar Cells of the TCS = 190"]
-[5.221804141998291, 1.64113450050354, "[TT] Dataset Availability of the ALOS/ Daichi = Public download"]
-[8.048254013061523, 0.8597704768180847, "[FF] Data Source of the U.S. Drought Monitor = Climate, soil, and water conditions"]
-[10.418473243713379, 2.2215895652770996, "[FF] Nature of the X-ray Light = Reflected off the accretion disk"]
-[10.54207992553711, 3.3281280994415283, "[TT] Satellite Type of the PROBA-V plus one = 12U CubeSat"]
-[4.497736930847168, 5.280179977416992, "[FF] Data Source of the Flightradar24 = Crowdsourced information gathering by volunteers with ADS-B receivers"]
-[3.106462001800537, 2.2494869232177734, "[FF] Mission of the Copernicus Sentinel-3 = Measure Earth\u2019s oceans, land, ice and atmosphere"]
-[7.688711643218994, 0.4802158772945404, "[FF] Mission Type of the Lunar IceCube = Science"]
-[8.144685745239258, -0.9725544452667236, "[TT] Orbit Type of the ICESat-2 = Near polar LEO frozen orbit"]
-[8.002955436706543, 5.755420684814453, "[TT] Calibration Mode of the LISS-3 camera = Pulsed"]
-[4.560278415679932, 6.739204406738281, "[FF] Communication Links of the TT&C subsystem = S-band (2 GHz, command uplink and telemetry downlink)"]
-[5.448132514953613, 7.09739875793457, "[TT] Data Transmission Rate of the ITU = 160 Mbit/s"]
-[5.635420322418213, 7.145643711090088, "[TT] Data Rate of the MBA System = 1.2 Gbit/s"]
-[11.25283432006836, 5.547990322113037, "[TT] Aerogel Tile Thickness of the RICH = 25 mm"]
-[10.75900936126709, 1.0332481861114502, "[TT] Diameter of the KELT-11b = 181,600 km"]
-[7.596315383911133, 3.210339307785034, "[FF] Function of the AMR-C = Provide a correction for the wet tropospheric path delay for the altimeter range measurement"]
-[6.976733684539795, 5.924015045166016, "[TT] Operation Modes of the PDHS = Real-time, real-time stretch mode, record, and playback"]
-[12.805821418762207, 7.595065116882324, "[TT] Power Consumption of the Instrument = 4 W"]
-[7.087710380554199, 3.034255266189575, "[FF] Operation Mode of the GeoSTAR = Nowcasting and very short range weather forecasts"]
-[4.242952346801758, 0.31646162271499634, "[TT] Launch Date of the JPSS-1 = 2016"]
-[5.1058807373046875, 1.0344467163085938, "[TT] Launch Date of the SMOS = Nov. 2, 2009"]
-[3.238304376602173, 5.034806251525879, "[TT] Imaging Data of the Synthetic Aperture Radar (SAR) = High-resolution"]
-[10.358195304870605, 5.730190753936768, "[TT] Phase Transition Temperature of the Gallium Black Bodies = 29.76\u00b0C"]
-[6.531260013580322, -0.39575058221817017, "[TT] Descent Phase Duration of the MIP = About 20 minutes"]
-[5.191110134124756, 1.2207268476486206, "[FF] Conference Date of the STRaND-1 = Oct. 3-7, 2011"]
-[7.416827201843262, 2.544074296951294, "[FF] Observation Target of the Satellite = Sea wave, sea surface wind field, internal wave, frontal surface, shallow sea topography, sea surface oil spill, sea ice, green tide, coastal zone and sea surface targets, Flood submerged area, debris flow, landslide, ice or snow, extent of sea ice, drought scope, buildings, temporary housing, traffic, agricultural and land use, flood control facilities, Characteristics of river basin systems, surface water distribution, flood range, soil moisture content, land use and vegetation coverage. Surface water indicators, lakes, reservoirs (dams), rivers, wetlands, glaciers, snow, other important water sources, irrigation areas, groundwater remote sensing monitoring indicators, karst, phreatic water, springs, geological landforms, High resolution regional surface soil moisture monitoring, rainstorm triggered landslides and debris flow and other geological disaster prediction and warning"]
-[11.273149490356445, 6.372746467590332, "[TT] Bulk Velocity of the Proton Component Measurement Range of the DSCOVR = 200 \u2013 1250 km/s"]
-[10.752196311950684, -0.20648831129074097, "[FF] Vertical Separation of the TanDEM-X = Achieved by a relative shift of the eccentricity vectors of the satellites"]
-[9.626816749572754, 8.214630126953125, "[FF] Field of View of the SEM-2 = Two at 15\u00ba full angle, -x, -x + 30\u00ba"]
-[5.159971237182617, 6.421422004699707, "[TT] Size of the Spacecraft 406 MHz Processor = 0.034 m3"]
-[9.384485244750977, 3.679866313934326, "[FF] Observation Date of the Magnetometer = Aug. 1, 2002"]
-[13.375702857971191, 7.370492935180664, "[TT] Power of the QC40 = 17 W"]
-[4.143711566925049, 7.331125736236572, "[TT] Band of the SWIM Instrument = Ku-band"]
-[3.219198703765869, 1.6321622133255005, "[TT] Downlink Time of the Sentinel-1, -2 = Approximately 16-18 minutes per orbit"]
-[11.71825885772705, 6.661123275756836, "[TT] Energies Sampled Per Spin of the Genesis Electron Monitor = 4"]
-[13.406879425048828, 5.761418342590332, "[FF] Voltage of the Solar Array = High-voltage"]
-[8.355961799621582, 8.631158828735352, "[TT] Spectral Sampling Interval of the Spectrometer = 1.2 nm to 16 nm"]
-[6.257329940795898, 6.35129451751709, "[FF] Data Retrieval Time Improvement of the SafetyNet = More than 32 minutes"]
-[6.61715841293335, 7.694313049316406, "[TT] Data Quantization of the 4-band CCD Imager = 12 bit"]
-[8.99792194366455, 8.011735916137695, "[TT] CCD Packages of the Focal Plane Module = 2"]
-[6.33674955368042, 0.6268125176429749, "[TT] New Orbit Date of the SPOT-4 = Jan. 29, 2013"]
-[8.30064582824707, 6.369194507598877, "[TT] Displacement Intervals of the CCRR = 0.2 m (TBC)"]
-[2.870516777038574, 4.216979026794434, "[FF] Observation of the ALOS/PALSAR = Magnitude-6.5 Earthquake in Southeastern Iran, 2010"]
-[6.86630916595459, 7.5795793533325195, "[TT] Resolution of the A/D converter = 16 MHz"]
-[6.432527542114258, 3.348412036895752, "[TT] Additional Features of the BlackSky Next Generation Satellites = Infrared sensors, inter-satellite links, on-board data processing enabled by artificial intelligence"]
-[10.75289249420166, 3.2739429473876953, "[FF] Purpose of the MICS (Microgravity Investigation of Cement Solidification) = Studied cement solidification in microgravity"]
-[5.700067043304443, -0.3976871073246002, "[TT] Installation Time of the iROSA = 7 hours and 15 minutes"]
-[6.260644435882568, 4.00398063659668, "[FF] Type of the Software development kit = Software development kit"]
-[5.724262237548828, -0.68817138671875, "[TT] On-Orbit Spare Lifetime of the GOES-R = 5 years"]
-[9.331005096435547, 6.887573719024658, "[TT] Spatial Baseline of the GF-3 = 250 m"]
-[6.125946521759033, 4.292274475097656, "[FF] Purpose of the Computer = Provide the interface between COSMOS and the ground station for data management, monitor and possibly control the operations of the ground station"]
-[8.592045783996582, 4.46604061126709, "[TT] Trajectory Correction Maneuver of the MarCO-B = Completed with Unexpected Challenges"]
-[6.047994613647461, 7.112819194793701, "[FF] Data Rate of the POLDER = 0.882 Mbit/s"]
-[9.035358428955078, 7.003159046173096, "[TT] Resolution of the OSIRIS = About 3 m per pixel"]
-[5.036479473114014, 0.5767055153846741, "[TT] Launch Date of the MESA = Aug. 2013"]
-[5.392186641693115, 4.900025367736816, "[TT] Data Bus of the OBDH Subsystem = Dual redundant CAN bus"]
-[9.401154518127441, 6.871640682220459, "[TT] Pan Spatial Resolution of the KazEOSat-1 = 1 m"]
-[6.242009162902832, 6.376712322235107, "[TT] Duration of the Planned data outage = > 300 hrs / yr"]
-[6.112652778625488, 7.759986400604248, "[TT] Number of Channels of the OPS (Onboard Packet Switch) = 128 packets/carrier (max)"]
-[13.56002140045166, 5.696975231170654, "[TT] Solar Array Power of the UK-DMC-2 = 65 W at AM0 and 25\u00baC"]
-[9.337213516235352, 7.0525288581848145, "[TT] NDVI Map Spatial Resolution of the RISING-2 = About 10 m"]
-[9.444260597229004, 7.417370319366455, "[TT] Multispectral GSD at Nadir of the NAOMI = 2 m to 10 m"]
-[5.729958534240723, 4.250726222991943, "[FF] Purpose of the Hiber-3 = Providing connectivity for IoT sensors and devices"]
-[14.256063461303711, 3.3025171756744385, "[TT] Mass of the IMI = 250 - 300 kg"]
-[10.66450309753418, 4.008028984069824, "[FF] Folding Method of the Inflatable boom = Origami pattern"]
-[8.834357261657715, 6.174731731414795, "[FF] Measurement Technique of the SOLSE-2 = Limb-sounding"]
-[7.836287021636963, 6.048705101013184, "[FF] Components of the Image Processing Payload = Multi-anode photon multiplier tube(MaPMT), a camera, and a real-time image processing engine"]
-[6.2338995933532715, 4.2675251960754395, "[FF] Operation System of the ADEOS-II = Central-core system for the mission operation"]
-[4.153348445892334, 5.8769402503967285, "[TT] Symbol Rate of the ADS-B receiving payload = 1 MHz"]
-[13.34080982208252, 2.843005418777466, "[TT] Launch Mass of the DubaiSat-1 = < 200 kg"]
-[5.516268253326416, 0.24134695529937744, "[TT] Launch Date of the ISS-RapidScat = 20 Sep 2014"]
-[10.836236000061035, 7.563869476318359, "[TT] Swath Width of the DMC-2 = 650 km"]
-[3.3088390827178955, 4.962143421173096, "[FF] Imaging Modes of the TSX-SAR = Spotlight (SL), Spotlight High Resolution (HS), Experimental Mode"]
-[4.592800617218018, 2.663623332977295, "[FF] North Polar Region Name of the Charon = Mordor Macula"]
-[3.0601017475128174, 1.8266379833221436, "[TT] Image Capture Date of the Sentinel-2 = 25 January 2022"]
-[9.1725492477417, 1.0373187065124512, "[TT] Date of the Next Flyby of Jupiter = July 21"]
-[4.564365386962891, 4.769654273986816, "[FF] Objective of the AIS = Provide a SAR data fusion capability for maritime surveillance from space with AIS data services"]
-[10.018298149108887, 4.366858959197998, "[TT] Torque of the Magnetic torquers = 100 Am 2"]
-[11.873830795288086, 6.628787040710449, "[FF] Proton Energy of the GALS-VE = > 1200 MeV"]
-[10.13748836517334, -1.4537569284439087, "[TT] Inclination of the PeruSat-1 = 98.3\u00b0"]
-[11.72549057006836, 5.284270763397217, "[TT] Power Lines for SVM-PDU and FPA-PDU of the MRU = 2 x 2"]
-[5.234740257263184, 2.0448625087738037, "[TT] Functionality Verification of the BIRCHES = Completed"]
-[12.756117820739746, 7.613160610198975, "[TT] Power Consumption of the Instrument = 50 W"]
-[5.302577972412109, 3.889397382736206, "[TT] Number of Satellites of the Sentinels Satellites = Up to four"]
-[5.185046672821045, 2.7471694946289062, "[TT] Agency of the Monitor-E = ROSKOSMOS"]
-[6.135495662689209, 1.5022283792495728, "[TT] Mission Duration of the Euclid = 6 years"]
-[9.159018516540527, 3.1770949363708496, "[FF] Environment of the Cluster = Magnetosheath"]
-[9.462916374206543, 7.0784220695495605, "[FF] Spatial Resolution Comparison of the GMI = 50-60% better than TMI on TRMM"]
-[5.290217876434326, 0.7853201031684875, "[TT] Recovery Date of the EFT-1 = Dec. 10, 2014"]
-[6.2159037590026855, 5.786628246307373, "[TT] Data Relay of the Laser Communication Terminal (LCT) = More than 10,000 successful links to the European Union\u2019s Copernicus Sentinels-1 and -2"]
-[9.041077613830566, 4.23349142074585, "[TT] Solar Temp. Range of the TRACE = 3.6 - 3.8"]
-[5.275476455688477, 3.2482054233551025, "[FF] Satellite Manufacturer of the Surrey Satellite Technology Limited = True"]
-[10.29179859161377, 5.370253086090088, "[TT] Heat Dissipation Method of the Spacecraft = Heat pipes"]
-[7.677560329437256, 6.7035722732543945, "[FF] Test Mass Relative Displacement Measurement of the Laser Interferometer = High resolution"]
-[4.9666666984558105, 0.5011904835700989, "[TT] Separation Date of the Schiaparelli = 16 October"]
-[9.566956520080566, 0.7199124097824097, "[TT] Distance from Earth for First Image of Earth and Moon of the Voyager 1 = About 7.3 million miles (11.66 million kilometers)"]
-[7.13388729095459, 3.942777633666992, "[TT] Number of Fragments Larger than 1 mm of the DMSP-F13 = More than 50,000"]
-[5.477621078491211, 6.42263650894165, "[TT] Data Storage Capacity of the Data Handling System = 64 Gbit"]
-[5.236852169036865, 0.9019960761070251, "[FF] Program Date of the ASNARO = June 4-8, 2012"]
-[7.432196140289307, 2.2945687770843506, "[TT] Global Coverage of the Visible Band = Daily"]
-[5.559009075164795, 1.0521585941314697, "[FF] Presentation Date of the Tuomas Tikka = October 14-16, 2014"]
-[4.831657409667969, 7.870186805725098, "[TT] Frequency Band of the GETR (Galileo Experimental Test Receiver) = E5a+b (AltBOC) 1191.795 MHz"]
-[9.044231414794922, 4.260597229003906, "[TT] Attitude Determination of the S/C = Magnetometer and sun sensors"]
-[5.448163986206055, 5.005621433258057, "[TT] Bus of the Payload Instruments = Redundant CAN (Control Area Network) bus"]
-[10.798135757446289, 7.504886150360107, "[TT] Multispectral Mode Swath Width of the LISS-4 = 23.9 km"]
-[8.14052677154541, 1.397068738937378, "[FF] Mission of the SMOS = Soil Moisture and Ocean Salinity"]
-[9.063767433166504, 5.855119228363037, "[TT] Coarse Pointing Accuracy of the NEMO-AM = Better than 5\u00b0"]
-[5.922637939453125, 0.8356417417526245, "[TT] Image Capture Date of the LRO = October 12, 2014"]
-[6.279313564300537, 3.0390379428863525, "[FF] Staff Count of the GHOSt Constellation = Unknown"]
-[5.236584186553955, 5.4429121017456055, "[TT] Type of the Network Fabric = IP (Internet-Protocol)-based"]
-[9.016695022583008, 7.379802703857422, "[TT] Image Resolution of the NAVCAM = 84.6 cm/pixel"]
-[7.8791913986206055, 8.424866676330566, "[TT] Integration Time of the Spectral bands = 0.308 ms for PAN, 1.232 ms for MS"]
-[5.463281154632568, 2.5649139881134033, "[TT] Managing Center of the SMAP = NASA's Jet Propulsion Laboratory in Pasadena, California"]
-[3.4670534133911133, 5.341611385345459, "[FF] Orientation of the SAR Antenna = Nadir (left) and in right-side looking direction"]
-[4.5100812911987305, -0.9040737152099609, "[TT] End of Life Date of the Dragon spacecraft = 10 July 2021"]
-[4.413815498352051, 7.863083839416504, "[TT] Downlink Frequency of the RF Communications = 430 MHz"]
-[6.36466646194458, 3.0426807403564453, "[TT] Daily system capacity of the WorldView-4 = 1x"]
-[7.897426128387451, -0.6444271206855774, "[FF] Collaboration of the IceBridge = International Thwaites Glacier Collaboration"]
-[13.644468307495117, 5.820866107940674, "[TT] Average Power of the Solar Cell Assemblies = ~1.5 W"]
-[6.098618984222412, -0.08406029641628265, "[FF] Duration of the OSCAR-QUBE = 8 months"]
-[13.495318412780762, 6.591396808624268, "[FF] Compatibility of the EPS (Electrical Power Subsystem) = Low Earth orbit to deep space exploration missions"]
-[7.404587745666504, 4.675187587738037, "[FF] Data Collection Detail of the ASAS-SN = Collects less detail on individual outbursts"]
-[5.743610382080078, 4.131965637207031, "[FF] Objective of the MidSTAR-1 = Fly two payloads: ICSat (Internet Communications Satellite) and CFTP (Configurable Fault Tolerant Processor)"]
-[11.846052169799805, 3.2500898838043213, "[TT] Thrust of the Chemical propulsion engine = 1 N x 4 engines"]
-[14.006958961486816, 2.9346847534179688, "[TT] Masses of the Aluminum Spheres = 1 kg, 1.5 kg, 2 kg"]
-[4.77030086517334, 7.818730354309082, "[TT] Operating Frequency of the C&DH Subsystem = 8 MHz"]
-[6.460682392120361, 7.618141174316406, "[TT] Data Quantization of the MI Radiometer = 10 bit"]
-[4.771076679229736, 0.7157334685325623, "[TT] Malfunction Date of the OHRIS = March 4, 2007"]
-[10.72446060180664, 1.1140403747558594, "[TT] Size Compared to Earth of the TOI 270 d = 2.1 times larger"]
-[8.730881690979004, 7.757602214813232, "[TT] Element Size of the S7 detector = 200 x 200 \u00b5m"]
-[8.911386489868164, 3.7657670974731445, "[FF] NLC Observation Peak of the AIM spacecraft = During solar minimum"]
-[8.145522117614746, 6.476015090942383, "[FF] Image Distribution of the CBERS = Approximately 90,000 images"]
-[7.0552449226379395, 6.93411111831665, "[TT] Quantity of the Metrology Laser Subsystems = 2"]
-[7.52473258972168, 5.457826137542725, "[FF] Contents of the FEEU = Precise and stable references voltages Vp for actuation linearization, Vd for position sensing and Vref for Analog to Digital accurate conversion"]
-[10.769803047180176, 2.7566981315612793, "[TT] Intersatellite Link Range of the CNAPS = 5 km"]
-[7.617059230804443, 6.605367183685303, "[TT] Image Delivery Time of the RISAT-1 MRS = Typically within 1 hour"]
-[8.679564476013184, 4.751944541931152, "[TT] Quantity of the STR (Star Tracker) = 3 x Optical Heads + 2 x electronics"]
-[5.156797409057617, 8.387961387634277, "[TT] Bandwidth of the MWR = 500 MHz"]
-[14.285722732543945, 3.29563307762146, "[TT] Mass of the SGR-ReSI = 1.5 kg"]
-[9.834033966064453, -0.6492635607719421, "[TT] Orbit Altitude of the Argos-4 = 850 km"]
-[8.380842208862305, 1.7552870512008667, "[TT] Percentage from Oil and Gas Sector of the Kayrros Studies = Around 50%"]
-[6.585498809814453, 5.366735458374023, "[FF] Components of the ADE = Single ferrite switch on the transmit path and four ferrite switches on the receive path"]
-[7.282537460327148, 6.742157936096191, "[FF] Pointing Error of the Laser frequency stabilization subsystem = Residual errors and offsets in the beam steering control loop and optics"]
-[8.510003089904785, 8.942002296447754, "[TT] Spectroscopy Wavelength Range of the PACS = 55 and 210 \u00b5m"]
-[8.36306381225586, 2.535778045654297, "[FF] Aerosol Typing Algorithm of the CATS = CALIOP instrument aerosol typing algorithm"]
-[9.093212127685547, 5.099633693695068, "[TT] Gyroscope Range of the ACS = \u00b1 200\u00ba/s"]
-[5.200531005859375, 7.918763160705566, "[TT] Reporting Frequency of the GT = 250 Hz"]
-[8.498042106628418, 5.916123390197754, "[TT] Predicted Target Error of the LRR = Below 6 mm"]
-[10.905755996704102, 4.9692535400390625, "[TT] Computed optical cross-section of the LARES-2 = 3.92 x 10^6 m^2"]
-[4.748596668243408, 0.7091670632362366, "[TT] Operational Date of the F-DUGS = 2010"]
-[5.019692420959473, 3.347791910171509, "[TT] Manufacturer of the LINAS = Cannon Corp."]
-[5.196037292480469, 0.23942831158638, "[FF] Presentation Date of the NEMO Bus = April 4-8, 2011"]
-[5.867366790771484, 5.117883205413818, "[FF] Function of the ROSA Radio Occultation Antenna = Receive signals from the GPS constellation during their occultation time window"]
-[4.881855010986328, 8.298768997192383, "[TT] Center Frequencies of the SSMIS = 19.35 GHz to 183.31 GHz"]
-[14.620410919189453, 6.65655517578125, "[TT] Type of the Energy Storage = NiCd batteries"]
-[4.801116943359375, 0.25858351588249207, "[FF] Deployment Date of the RemoveDEBRIS = 20 June 2018"]
-[4.850001335144043, 7.433977127075195, "[TT] Data Rates of the CC1101 UHF transceiver = Up to 500 kbit/s"]
-[7.109399795532227, 0.06475286185741425, "[TT] Age of the HIP 67522 b = About a few million years"]
-[10.71252727508545, 5.2908735275268555, "[FF] Function of the ETFE film and the semi-conductive coating = Mitigate arcing under a LEO plasma environment"]
-[7.112092018127441, 6.590250015258789, "[FF] URL of the Laser Frequency Stabilization = https://trs.jpl.nasa.gov/handle/2014/41635"]
-[4.662198543548584, 5.462339401245117, "[TT] Function of the GOES Search and Rescue Transponders = Detects beacon signals"]
-[5.37945556640625, 0.779689371585846, "[TT] Arrival Date of the European Service Module = November 7, 2018"]
-[8.012939453125, -0.9373147487640381, "[TT] Data Densities of the MABEL = 46% of the expected ICESat-2 data densities"]
-[8.032913208007812, 4.749344348907471, "[TT] Component of the MuREM = Radiation effects board"]
-[4.120860576629639, 6.353872776031494, "[FF] Antenna Pattern of the Antenna = Cross-track direction"]
-[9.1505765914917, -1.2138501405715942, "[TT] Orbit of the Himawari-8 = Geostationary orbit"]
-[7.881939888000488, 6.068427562713623, "[TT] Operation Mode of the Vision-based sensor = Uncooperative"]
-[8.627695083618164, 7.677210330963135, "[TT] Detector Pixels per Spot of the ATLAS instrument = Multiple"]
-[6.564999580383301, 4.655375003814697, "[TT] Operation Management of the CAPSTONE = Advanced Space and Terran Orbital"]
-[9.90674877166748, -0.41733652353286743, "[TT] Altitude of the Satellite = 572 km"]
-[4.680055141448975, 5.427280902862549, "[FF] Purpose of the Automated Beacon Network = Provide cost-effective anomaly detection and notification capabilities"]
-[6.959169387817383, 6.162358283996582, "[TT] Quantity of the Instrument Package = 4"]
-[4.843046188354492, 2.9667932987213135, "[TT] Prime Contractor of the CHEOPS = Airbus in Spain"]
-[8.90565013885498, 4.197998523712158, "[FF] Earth Pointing Mode Function of the H3 and H4 = PZ-Surface faces into the nadir direction during observations"]
-[6.574245929718018, -0.491590678691864, "[TT] Orbital Period of the ISS = 90 minutes"]
-[7.992425918579102, 9.181994438171387, "[TT] Wavelengths of the CATS = 532 nm and 1064 nm"]
-[7.042430877685547, 7.342432498931885, "[TT] Pulse rate of the ATLAS lasers systems = 10 kHz"]
-[14.094011306762695, 3.2482755184173584, "[TT] Payload Mass of the IMS-2 = 147 kg"]
-[8.615626335144043, 3.2513959407806396, "[FF] Measurement of the ROSA = Total Electron Count"]
-[6.341891765594482, 8.416730880737305, "[TT] Polarization Purity of the Array Radiator = Cross-polar better than -20 dB"]
-[8.101916313171387, -0.7058261632919312, "[FF] Sea ice identification of the Cryosphere = Creates monthly ScanSAR mosaics for both polar regions and temporal changes for glacier movement"]
-[11.79308795928955, 3.264158010482788, "[TT] Number of Thrusters of the LAM = 12"]
-[7.462188243865967, 1.1880519390106201, "[TT] Number of Colloquiums of the SeaSat = 2"]
-[7.336309909820557, 2.642894983291626, "[FF] Overview Date of the Terrestrial Imaging Spectroscopy Missions = 21\u201326 July 2013"]
-[6.480315685272217, 2.92985200881958, "[FF] Purpose of the International Space Station (ISS) = On-orbit research and discovery"]
-[11.244732856750488, 0.9858765006065369, "[FF] Abstract URL of the LISA = https://journals.aps.org/prl/abstract/10.1103/PhysRevLett.120.191103"]
-[5.54429292678833, 0.8398513197898865, "[TT] Orbital Commissioning Finish Date of the Satellite = September 29, 2013"]
-[5.882023334503174, 5.7297139167785645, "[FF] Type of the Network data recorder = Network data recorder"]
-[3.4455111026763916, 6.460808753967285, "[TT] Pixel Size (km x km) of the Antenna = 32"]
-[11.655619621276855, 6.728819847106934, "[TT] Energy Resolution of the Detector = 10% at 14 keV"]
-[8.371590614318848, 0.23972488939762115, "[FF] Observation of the FAUST = Gas trail behind the cloud"]
-[5.372926712036133, 4.1639885902404785, "[TT] Bus Design of the QuickBird-2 = BCP 2000 (Ball Commercial Platform 2000)"]
-[5.7540106773376465, 1.0572788715362549, "[TT] Geostationary Observations Maintenance Period of the GeoXO = Through 2055"]
-[6.686320781707764, 4.9019012451171875, "[FF] Activation Sequence of the ISM = Two diagonal corners, then the other two"]
-[10.062173843383789, 2.888951301574707, "[FF] On-Orbit Duration of the HRBE (E1-P) CubeSat = Nine Months"]
-[11.115315437316895, 5.9558491706848145, "[TT] Material of the Desiccant Bed = Silica gel"]
-[5.7967047691345215, 3.9095396995544434, "[FF] Target Markets of the Satellite for 5G = Transport sector (maritime, aviation and land), public safety, and media and broadcasting"]
-[8.284913063049316, 7.417232513427734, "[TT] Data Type of the CMOS Camera = UYVY, 8 bit"]
-[5.747312545776367, 4.855465412139893, "[FF] Hardware Changes of the Satellite = Addition of a bolt-hole pattern and two ruggedized connectors"]
-[5.769875526428223, 4.719351291656494, "[FF] Compliance of the QPSK = Existing ground stations and improve robustness"]
-[13.944785118103027, 3.0440146923065186, "[TT] Mass of the GPSDR = 28 kg"]
-[7.7120513916015625, 1.9314216375350952, "[FF] Carbon Dioxide Absorption of the Earth's Forests = Around 8 Gigatons a year"]
-[7.2958173751831055, 1.6320139169692993, "[FF] Imagery Capture Date of the WorldView-3 and GeoEye-1 = Northern California Firestorm"]
-[3.432892084121704, 6.322164535522461, "[TT] Tile Size of the Active Antenna = 1 m x 1 m"]
-[6.185845375061035, 4.369674205780029, "[FF] Ground System of the UNIFORM-1 = Mission Planning, Scheduling, Control, and Data Processing"]
-[9.014041900634766, 4.368063926696777, "[TT] DSS of the AOCS = Digital Sun Sensor"]
-[6.382952690124512, 1.1015063524246216, "[FF] Constellation Operations of the FormoSat-7 / COSMIC-2 mission = 6 satellite constellation operations"]
-[10.040363311767578, 4.3677849769592285, "[FF] Function of the Pinpuller = Provides a reliable launch locking device and allows after pin retraction the mechanism to rotate in both senses"]
-[4.309711933135986, 4.810868740081787, "[TT] Minimum Beam Mode Detectable Ship Length (MDSL) of the ScanSAR wide = 61-639 m"]
-[12.002452850341797, 4.827654838562012, "[TT] Dimensions of the LLITED = Approximately 100 x 100 x 170 mm"]
-[10.019206047058105, 8.481563568115234, "[TT] Value of the Sprite Volume Radiance = ~9 x 10-7 W/m2 on the entrance pupil"]
-[5.18500280380249, 8.104239463806152, "[TT] Frequency Range of the Spectrum Analyzer = \u00b1 7 MHz"]
-[10.58182430267334, 5.493793964385986, "[FF] Function of the TEMBOTM EMC = Allows for strain energy to be \"frozen\" into an EMC structure by cooling the deformed laminate below the critical temperature"]
-[13.431732177734375, 7.47107458114624, "[TT] Output Power of the CanX-2 = 27 dBm"]
-[8.37356185913086, 6.156637191772461, "[TT] Sensor Type of the ISIS = Piezoelectric devices"]
-[4.913899898529053, 3.397073745727539, "[TT] Manufacturer of the ERNO-Box = Astrium Space Transportation"]
-[3.3467955589294434, 5.0349345207214355, "[TT] X-band Resolution of the SAR-XL Payload = 1m class"]
-[5.293976306915283, 0.8491255044937134, "[FF] Partnership Date of the Capella Space = August 5, 2019"]
-[5.551089286804199, 3.400913953781128, "[FF] Broadband Networking and Video Distribution Services Coverage of the Intelsat 39 = Africa, Europe, the Middle East and Asia"]
-[6.128114700317383, -0.44636523723602295, "[TT] Single Event Effect Correction Time of the TechEdSat = 87 days"]
-[5.724679470062256, 5.566324234008789, "[TT] Data Interface of the NSat = UART and I2C"]
-[5.597198009490967, 6.402841091156006, "[TT] HSDR Capacity of the SSTL-100 = Up to 48 GByte"]
-[9.997802734375, 4.555330753326416, "[FF] Components of the Superconducting Magnet = 2 main dipole coils and 12 racetrack coils, a superfluid helium vessel and a cryogenic system, all enclosed in an aluminum vacuum tank"]
-[4.265258312225342, 7.1834397315979, "[TT] Band of the RF Communications = X-band"]
-[14.17685604095459, 2.980264186859131, "[TT] Mass (kg) of the ALOS-2 = 2120"]
-[9.28221607208252, -1.0659359693527222, "[TT] Final Geostationary Orbital Location of the INSAT-3D = 82\u00ba East longitude"]
-[9.669316291809082, 6.9077582359313965, "[TT] SST Spatial Resolution of the CIMR = 15 km"]
-[6.5545268058776855, 0.23636074364185333, "[TT] Age of the Landsat 7 = Nearing nineteenth year in orbit"]
-[6.0690131187438965, 2.5972843170166016, "[TT] Managing Organization of the SWEAP Science Operations Center (SOC) = SAO (Smithsonian Astrophysical Observatory)"]
-[6.258012294769287, 5.529223442077637, "[FF] Purpose of the Data Compression Method = Prevent crowding out payload data"]
-[6.642178535461426, 1.8314892053604126, "[FF] URL of the Landsat 9 = https://www.nasa.gov/press-release/nasa-launches-new-mission-to-monitor-earth-s-landscapes"]
-[7.461061954498291, 3.64886474609375, "[FF] Application of the NightPOD = Optical observation"]
-[6.0911126136779785, 5.4939799308776855, "[TT] Redundancy of the CIB = Cold"]
-[5.708117961883545, 0.7630784511566162, "[FF] Discovery Date of the TGFs = Unknown"]
-[6.389220714569092, 4.321331024169922, "[FF] Purpose of the FFS = Maintain the satellites in the desired relative configuration"]
-[3.5106008052825928, 4.88784646987915, "[TT] Instrument Type of the Biomass = Imaging microwave radars"]
-[11.807612419128418, 0.0653548538684845, "[TT] Number of Stars Identified in Catalog of the TESS = 1,822"]
-[10.07001781463623, 8.182700157165527, "[TT] Lens Aperture of the MSI-0 and MSI-1 = 180 mm"]
-[13.37578010559082, 7.336367130279541, "[TT] Power of the BHT-200 = 200 W"]
-[9.352821350097656, 0.8563634753227234, "[FF] Venus Zone of the L 98-59b = Range of stellar distances where a planet with an initial Earth-like atmosphere could experience a runaway greenhouse effect"]
-[4.568850040435791, 3.0152833461761475, "[TT] Location of the Tyvak 61C = Irvine CA, USA"]
-[5.513088226318359, 3.201847791671753, "[FF] Amount of the Maxar\u2019s $140 million buyout of 3D analytics firm = $140 million"]
-[9.048229217529297, 7.566620349884033, "[TT] Resolution of the Multispectral Bands = 1.16 m"]
-[10.119839668273926, 8.150432586669922, "[FF] Optimal Size of the Photometric Aperture = Unknown"]
-[11.18276309967041, 5.960918426513672, "[TT] Material of the Quasi-Isostatic Bipods = Titanium"]
-[4.804204940795898, 0.11895228177309036, "[TT] End of Life Date of the SWFO-L1 = 31 December 2029"]
-[4.514786243438721, 4.652310848236084, "[TT] Usage Increase of the Maritime Surveillance modes = Quick ramp up"]
-[7.871253967285156, 0.9249348044395447, "[FF] Date of the Rain Drenches Kauai = 2 May 2018"]
-[11.890172958374023, -0.011405219323933125, "[FF] Monitoring Method of the TESS = Capturing changes in stellar brightness"]
-[8.132469177246094, 5.2280402183532715, "[TT] Calibration Algorithm Version of the MWR = v2.2"]
-[14.028507232666016, 7.158215522766113, "[TT] Output of the DC/DC converter = +5 V, +3.3 V"]
-[9.504302024841309, 7.210559368133545, "[FF] Nadir Angular Resolution of the VIRR = 2.3 km and 4.4 km"]
-[11.707825660705566, 4.679281711578369, "[TT] Structure Shape of the Baumanets-2 = Regular hexagon"]
-[13.612990379333496, 5.878183364868164, "[FF] Power Source of the Electrical Power Subsystem (EPS) = Solar arrays and rechargeable batteries"]
-[6.006819725036621, 2.930168867111206, "[FF] Development Organizations of the NINA-2 = INFN (Italian National Institute of Nuclear Physics) of Rome, Italy and MEPhI (Moscow Engineering and Physics Institute)"]
-[10.374251365661621, 4.412130832672119, "[FF] Wheels of the ESA rover = Designed by engineers at NASA\u2019s Glenn Research Center in Cleveland, Ohio"]
-[8.231491088867188, 6.992152214050293, "[TT] Number of Images Received by CIFAS of the PAZ = 30 of the 100 high-resolution images captured daily"]
-[10.205204010009766, 3.1192362308502197, "[FF] Risk Reduction of the MicroMAS-2 = NASA TROPICS , NOAA EON-MW CubeSat missions"]
-[5.189556121826172, 5.826129913330078, "[FF] Number of Nodes of the TacSat-4 SpaceWire Link = 2"]
-[9.590313911437988, 7.456877708435059, "[TT] Angular resolution (2 px) of the HRI dual EUV 174 \u00c5 and 335 \u00c5 alternatively = 1 arcsec"]
-[13.216243743896484, 7.4600629806518555, "[TT] Tx Power of the HDR-VSAT = 100 W"]
-[5.090640544891357, 7.014552116394043, "[TT] Net bit rate (bit/s) of the Service downlink = 4,709"]
-[6.959662914276123, -0.668708086013794, "[TT] Orbit Period of the KELT-9 b = 9 hours"]
-[5.875461101531982, 0.08981508761644363, "[FF] Timeframe of the Operation Practice/Rehearsal = Year 2017"]
-[4.7702836990356445, 0.0631742924451828, "[TT] End of Life Date of the PROBA-3 = 2026"]
-[4.80959939956665, 3.2493796348571777, "[FF] Locations of the Indian Coast Guard and Rescue Coordination Centers (RCCs) = Mumbai, Kolkata, Delhi and Chennai"]
-[10.06154727935791, 1.373755931854248, "[FF] Discovery of the Gaia = Detection of Starquakes"]
-[5.368852138519287, 0.534519612789154, "[TT] Event Date of the LROC = October 13, 2014"]
-[9.841350555419922, 4.263164520263672, "[TT] Quantity of the Suspension Electromagnets = 8"]
-[9.71219253540039, 6.249050140380859, "[FF] Issue of the Moving Mirror Alignment System = Occasional sticking at anomalous alignment position"]
-[5.256634712219238, 7.088348865509033, "[TT] Data Transmission from S/C to Ground of the Onboard data collection and transmission system = 1690-1710 MHz"]
-[6.496936321258545, 4.618457794189453, "[FF] Reason for Incomplete Flight Objectives of the OCSD = Software anomaly in the ACS"]
-[8.146407127380371, 8.543950080871582, "[TT] Roughness of the Ir Layer = 1.3 nm rms"]
-[14.598835945129395, 6.618039608001709, "[TT] Battery Type of the Spacecraft = Li-ion"]
-[5.3255205154418945, 0.9060032367706299, "[FF] Launch Date of the ELISA = Unknown"]
-[5.694317817687988, 1.1662107706069946, "[FF] Launch Date of the Copernicus Environmental Satellite = April 3, 2014"]
-[7.232010364532471, 8.593502044677734, "[TT] Spectral Channel 1 of the Satellite = 0.50 - 0.59 \u00b5m"]
-[8.909852027893066, 4.916690826416016, "[TT] Sensor Units of the CDMS = 2"]
-[7.791037082672119, 6.611950874328613, "[TT] Number of Images Processed by ECMWF of the SMOS = Some 600 images every day"]
-[4.849949359893799, -1.7832635641098022, "[TT] Orbit Duration of the Chang'e-2 = More than 2 years"]
-[10.99986743927002, 7.643060684204102, "[TT] Swath Width for Regular Corresponding Mode of the Wide fine = 50 km"]
-[7.509040832519531, 7.144826889038086, "[TT] Signal Inputs of the AEM = 8 differential signals from light sensors, 2 temperature signals"]
-[9.345110893249512, 6.520236015319824, "[TT] Field of View of the OMPS Nadir Sensor = 110\u00b0"]
-[8.767391204833984, 6.373593807220459, "[TT] Accuracy of the Altimeter = \u00b1 1 m"]
-[14.229132652282715, 3.216395139694214, "[TT] Mass of the FGM = 3.0 kg"]
-[10.256403923034668, 2.3575336933135986, "[FF] Ability of the INTEGRAL = Detect polarized gamma-radiation"]
-[4.976325511932373, 4.356439590454102, "[TT] Ground Station Operator of the RF Communications = TI-Tech"]
-[8.363218307495117, 3.6009891033172607, "[FF] Measurement of the MHS = Microwave radiation emitted from Earth\u2019s surface"]
-[9.390152931213379, 7.050302028656006, "[TT] Value of the Spatial Effective Resolution = 50-60 m"]
-[5.647320747375488, 5.9813032150268555, "[FF] Primary Objective of the SDA = Speed"]
-[7.120293617248535, 6.413524627685547, "[TT] Number of Stations of the Satellite Laser Ranging Stations = 3 in Russia, 10 outside Russia"]
-[13.883270263671875, 3.0490472316741943, "[FF] Mass Control Requirement of the Invar = Careful attention to mass control"]
-[10.948108673095703, 3.7162084579467773, "[FF] Propulsion of the LightSail = Solar sailing"]
-[6.704850673675537, 4.461070537567139, "[FF] Data of the GRB = Processed mission data"]
-[7.312088966369629, 4.104105472564697, "[FF] Calibration Function of the GMI Radiometer = Transfer standard for the other radiometers of the GPM constellation"]
-[6.721038341522217, 7.538593292236328, "[TT] A/D Conversion of the Satellite = 8 bit"]
-[6.488681793212891, 2.0263943672180176, "[FF] URL of the ACTS = http://acts.grc.nasa.gov/about/operations/index.shtml"]
-[10.241369247436523, 7.895086765289307, "[TT] Instrument Type of the RadMon = Miniature Particle Telescope"]
-[8.372509956359863, 1.153558611869812, "[TT] Quantization Levels of the Soil moisture = 1"]
-[8.21056079864502, -1.09467613697052, "[TT] Ground Path Height Measurement of the ICESat-2 = Every 2.3 feet (70 cm)"]
-[8.391161918640137, 4.556478023529053, "[FF] General Relativistic Effect Test of the LARES = Frame-dragging"]
-[10.062403678894043, -1.5937752723693848, "[TT] Inclination of the Primary Payload = 69.5\u00ba"]
-[8.798968315124512, 2.710831642150879, "[TT] Error of the Atmosphere = \u00b13.0 K"]
-[4.6157050132751465, 1.6740835905075073, "[FF] Conference Date of the Alphasat Concept = May 5-9, 2014"]
-[7.860316276550293, 8.493621826171875, "[TT] Spectral Range of the Instrument = 8.80-15.39 \u00b5m"]
-[3.4019577503204346, 3.631340980529785, "[FF] Document Date of the Paz ground segment = May 31, 2011"]
-[6.295504093170166, 5.431819438934326, "[FF] Function of the TCU = Control the beam pointing and the beam setting in a tile"]
-[7.4801249504089355, 0.1830829381942749, "[TT] Flyby Duration of the OSIRIS-REx = 5.9 hours"]
-[5.2961039543151855, 1.0282613039016724, "[FF] Launch Date of the IASI-NG = Unknown"]
-[5.574836254119873, -1.9212985038757324, "[FF] Data Collection Objective of the KOMPSAT-1 = Provide information on the LEO particle environment and globally on the plasma distribution in the ion layer"]
-[10.214606285095215, 5.4277448654174805, "[FF] Operation of the SIMBA = Swivels out to deep space, just a few degrees from absolute zero, to learn the maximum level of heat we need to apply to keep it there"]
-[5.860182285308838, 6.322122097015381, "[TT] Number of Files per Input Port of the SSR = Up to 32"]
-[8.488715171813965, 5.085965633392334, "[FF] Development Status of the GRACE Follow-On accelerometer = Unknown"]
-[8.065842628479004, 2.5530078411102295, "[TT] Measurement Domain of the GPIM = Ocean, Land"]
-[8.564698219299316, 7.0598883628845215, "[FF] Modulation Transfer Function of the UK-DMC-1 = Improved compared to the first generation 32 m DMC imagers"]
-[5.384275913238525, 3.2056620121002197, "[TT] New Debt Issued of the Maxar Technologies = $150 million"]
-[7.898202419281006, -0.6501696705818176, "[FF] Observation Date of the Wilkins Ice Shelf = Dec. 1, 2016"]
-[7.760746955871582, 5.754222393035889, "[TT] Manufacturer of the Passive Microwave Imaging Radiometer = Harris Corp."]
-[5.506646156311035, 7.509119510650635, "[TT] XPD of the SWOT = ~25dB"]
-[13.76834487915039, 3.090606689453125, "[TT] Payload Mass of the Heinrich Hertz = 435 kg"]
-[4.3529582023620605, 0.6805934906005859, "[TT] Launch Date of the DMSP-F19 = April 2014"]
-[3.789854049682617, 6.934881210327148, "[TT] Gain of the KhalifaSat Antennas = 18 dBi"]
-[7.008718967437744, 7.158202171325684, "[TT] Tx Pulse Width of the KaRIn = 4.5 \u00b5s"]
-[11.25797176361084, 5.853949069976807, "[TT] Interface Bracket Material of the ASM = CFRP (Carbon Fiber Reinforced Polymer)"]
-[5.237649440765381, 3.6221249103546143, "[FF] Composition of the RCC = Formed from a variety of different state rescue services, depending on the responding nation"]
-[5.493093967437744, 3.311077356338501, "[TT] Sensor Provider of the DMSP-14 = Northrop Grumman"]
-[5.679905891418457, -0.1345812827348709, "[FF] Deployment Duration of the RDA = Not provided"]
-[11.748090744018555, 6.573145389556885, "[TT] Neutron Converter of the LND = Natural Gd foil"]
-[6.756864070892334, 4.353654861450195, "[FF] Location of the RSC = RSC"]
-[4.216652870178223, 6.719386100769043, "[FF] Dual Receive Antenna Configuration of the TanDEM-X = Introduced during the TanDEM-X Science phase"]
-[7.8075995445251465, 2.616323947906494, "[FF] Applications of the SWIR band = Daytime cloud/snow/ice discrimination, total cloud cover, aviation weather analysis for icing, smoke from low-burn-rate fires"]
-[9.265259742736816, 1.8487398624420166, "[FF] Composition of the Harpoon Concept System (HCS) = Deployer, Projectile and Tether"]
-[9.774870872497559, -0.5386300683021545, "[FF] Orbital Altitude of the International Space Station = Relatively low over our planet"]
-[7.5611701011657715, 6.845616340637207, "[TT] Temporal Cadence of the TRACE instrument = About 20-30 seconds"]
-[8.620192527770996, 5.940425395965576, "[TT] Requirement Value of the Ortho-image accuracy = 3.5 m CE90 (Horizontal)"]
-[3.3584609031677246, 1.5440101623535156, "[FF] Launch Date of the Sentinel-1C = 7 April 2022"]
-[11.287473678588867, 5.839092254638672, "[TT] Foil Material of the Dosimeter A = Aluminum"]
-[4.688584327697754, 5.912109851837158, "[TT] Type of the GomSpace SDR (Software Defined Radio) module = Software Defined Radio"]
-[9.260504722595215, 3.2026784420013428, "[FF] Purpose of the Coronagraph = Taking pictures of the inner solar corona"]
-[5.052948474884033, 1.683397889137268, "[FF] Launch Date of the TacSat-4 = Unknown"]
-[7.029255390167236, 5.881056308746338, "[FF] Hardware of the NTP = Simple PC104 computer clock, no thermal control, no 1 PPS source"]
-[6.939091205596924, 4.260669708251953, "[FF] Docking Maneuver of the ATV = Fully autonomous"]
-[9.492229461669922, -0.8117245435714722, "[TT] Nominal Position of the MVIRI = 0o longitude"]
-[8.234685897827148, 6.244250774383545, "[FF] Output Voltage Behavior of the OPS systems = Decreases for distances smaller than 10 mm"]
-[12.103240013122559, -0.20804384350776672, "[TT] Sector Observation Time of the TESS = 1 year for southern sky, 1 year for northern sky"]
-[3.699925422668457, 4.68604850769043, "[TT] Speed Estimation Accuracy of the In-flight simulated radar interferometry experiment = 0.05 m/s"]
-[10.73538589477539, 1.124833106994629, "[TT] Size Compared to Earth of the TOI 270 c = 2.4 times larger"]
-[6.438356876373291, 1.1425937414169312, "[FF] Ground Network of the FormoSat-7 / COSMIC-2 mission = U.S., European, Asian, and polar ground networks"]
-[5.178375720977783, 8.262943267822266, "[FF] Bandwidth of the Instrument = 350 MHz, 100 MHz, 200 MHz, 400 MHz, 1000 MHz, 200 MHz, 400 MHz, 3000 MHz, 3000 MHz"]
-[6.042407989501953, 1.2486062049865723, "[FF] Date of the Autonomous Sciencecraft Experiment = June 27-29, 2006"]
-[6.25355863571167, 1.917801022529602, "[FF] URL of the AAUSat3 = http://www.space.aau.dk/aausat3/index.php?n=Tech.AAUSAT3InDetails"]
-[9.911413192749023, 3.097111463546753, "[TT] Full Form of the ESP-MACCS = Earth System Processes Monitored in the Atmosphere by a Constellation of CubeSats"]
-[7.737292289733887, 1.4132437705993652, "[FF] Goals of the ROSE-L = Geohazards monitoring, land use monitoring, soil moisture monitoring, Arctic and cryosphere monitoring, maritime surveillance"]
-[3.117036819458008, 2.223914623260498, "[FF] Measurement Capabilities of the Copernicus Sentinel-3 = Earth\u2019s oceans, land, ice and atmosphere"]
-[6.387872219085693, 0.7911162376403809, "[TT] Health Status of the FormoSat-2 = Nominal"]
-[9.447052955627441, 1.339233160018921, "[TT] Deployment Velocity of the Net Demonstration = 5 cm/s"]
-[10.651549339294434, 1.9043370485305786, "[FF] Observed Phenomenon of the XMM-Newton = Winds emanate from the black hole not in a beam, but in a nearly spherical fashion"]
-[10.247782707214355, 5.740450382232666, "[TT] Cold Finger Temperature of the AIM SX030 microcryocooler = \u2264 115 K"]
-[13.537447929382324, 7.122724533081055, "[TT] Efficiency of the Diode Power Module = >87%"]
-[11.793388366699219, 3.2648379802703857, "[TT] Thrusters of the Propulsion = 20 x 20 N"]
-[8.750412940979004, 6.770516872406006, "[TT] Cross-Track Scanning Technique of the MERSI-RM = 4096 samples"]
-[5.161391735076904, 3.3457353115081787, "[TT] Manufacturer of the Heinrich-Hertz satellite = DLR-RfM (German Aerospace Center \u2013 Space Administration)"]
-[9.294249534606934, 6.053152561187744, "[FF] Incidence Angle Measurement of the Radiometer = From the surface"]
-[5.108565330505371, 3.2926459312438965, "[TT] Manufacturer of the GEMS = Ball Aerospace"]
-[13.498041152954102, 5.471231460571289, "[FF] Application of the Optically Clear Silicone Rubber = Fabricating solar concentrator lenses"]
-[13.587674140930176, 5.458845138549805, "[TT] Quantity of the Dual-junction solar cells = Six strings of 18 GaInP cells"]
-[9.458723068237305, 7.3167643547058105, "[TT] Ground Resolution of the VIS Camera = 150 m"]
-[8.425554275512695, 8.270737648010254, "[TT] Spectral Cube Size of the Observation Instrument = 1900 (spectral) x 1150 (spatial)"]
-[7.771763324737549, 0.3491365313529968, "[FF] Status of the Lamp system = Damaged on the ScaRaB/Meteor-3-7 mission"]
-[8.338611602783203, 7.078590393066406, "[TT] Number of Photographs of the Metric Camera = 1019"]
-[6.872103214263916, 7.747534275054932, "[FF] Volume Efficiency of the Reflectarray Antenna = Leaves plenty of room for payloads such as science instruments or imaging systems"]
-[11.890109062194824, 6.665541648864746, "[TT] Energy of the Sub-mm = 1.4 meV"]
-[5.301651477813721, 4.005228042602539, "[TT] Number of Supported Satellite Missions of the KSAT = More than 100"]
-[9.909749031066895, 8.191340446472168, "[TT] Focal Length of the Vidicons = 2.5 cm"]
-[14.2037935256958, 3.426812171936035, "[TT] Mass of the EPP device = 1.1 kg"]
-[10.05767822265625, -1.5080121755599976, "[TT] Inclination of the FormoSat-3/COSMIC-1 = 72\u00ba"]
-[9.519193649291992, 8.198159217834473, "[TT] Field of View of the Camera = 15 degrees"]
-[8.905407905578613, -0.23066186904907227, "[FF] Orbit Insertion of the Periselene-1 = Lunar orbit"]
-[8.320549964904785, 2.8007900714874268, "[TT] Measurement Domain of the FORUM = Atmosphere, Gravity and Magnetic Fields"]
-[4.801224231719971, 6.63820219039917, "[FF] Data Transmission of the Block 5 = Encrypted S-band digital data links"]
-[6.8217997550964355, -0.5814022421836853, "[TT] Orbital period of the Satellite = 24 hours"]
-[7.884575843811035, 7.22686767578125, "[FF] Distortion of the SHS Interferograms = Figure errors distort the individual (carrier) fringes to a greater extent than the envelope (visibility) of the fringes"]
-[4.495265483856201, 1.681734561920166, "[TT] Launch Vehicle of the TanSat = Chinese Long March 2D"]
-[8.866259574890137, 8.20921516418457, "[TT] Visible Energy Transmission of the Optics Assembly = 75%"]
-[7.579165458679199, 6.424610614776611, "[TT] Scenes Recorded per Scan of the TOMS = 35"]
-[3.2091176509857178, 3.8886849880218506, "[TT] Operation Start Year of the TerraSAR-X and TanDEM-X = Since 2010"]
-[14.648019790649414, 6.7561163902282715, "[TT] Battery Capacity of the EPS = 2600 mAh"]
-[14.381050109863281, 3.319718599319458, "[TT] Mass of the SDS-4 = ~48 kg"]
-[11.483864784240723, 5.076561450958252, "[TT] Guard Ring Diameter of the LPE = 100 mm"]
-[10.415091514587402, 7.602425575256348, "[TT] IFOV of the S-192 optomechanical scanner = 79 m"]
-[9.242281913757324, -0.32201993465423584, "[TT] Apogee of the Orion EFT-1 = 5800 km"]
-[3.3001630306243896, 6.487905025482178, "[TT] Antenna Diameter of the VSAT = 120 cm"]
-[10.854384422302246, 3.9742813110351562, "[TT] Drag Sail Modules of the CanX-7 = 4"]
-[13.223060607910156, 5.224945545196533, "[TT] Size of the Solar Array = 8.9 m x 3.3 m"]
-[5.470967769622803, -0.4801484942436218, "[TT] Separation Time of the GCOM-W1 = 23 minutes after launch"]
-[8.029814720153809, -0.6810041069984436, "[TT] Radar of the CryoSat-2 = Measures height"]
-[8.938888549804688, 3.0483083724975586, "[FF] Impact of the EUVS = EUV flares also deposit large amounts of energy in Earth\u2019s upper atmosphere (thermosphere) causing it to expand into Low Earth Orbiting satellites"]
-[7.625823974609375, 7.652002811431885, "[FF] Sensitivity of the SSM/I = Factor two better over a conventional Dicke-switched system"]
-[10.366589546203613, 6.590627670288086, "[TT] Number of Mirrors of the Laser Retroreflector Array (LRA) = 9"]
-[7.203319549560547, 6.8510823249816895, "[FF] Power Consumption of the APD detector = Low"]
-[5.246193885803223, 1.2447967529296875, "[FF] Conference Date of the PLEGPAY = Oct. 15-19, 2001"]
-[8.378472328186035, 3.9525840282440186, "[TT] Manufacturer of the Total Irradiance Monitor and Spectral the Irradiance Monitor = University of Colorado Laboratory for Atmospheric and Space Physics"]
-[6.871555805206299, 1.766168236732483, "[FF] URL of the Star-circling bubble of gas = http://m.esa.int/spaceinimages/Images/2018/06/Star-circling_bubble_of_gas"]
-[3.294649124145508, 6.4865264892578125, "[TT] Antenna Diameter of the HDR-VSAT = 1.2 m"]
-[4.779970645904541, 0.49413439631462097, "[TT] Launch Date of the CHAMP = July 2000"]
-[8.897736549377441, 7.908328056335449, "[TT] MTF of the Optoelectronic System = ~ 40%"]
-[9.8103609085083, -0.583755373954773, "[TT] Orbit Height of the TerraSAR-X = 514 km"]
-[7.096971035003662, 3.0684330463409424, "[FF] Photo of the SREM = Figure 19: Photo of the SREM instrument"]
-[5.762073040008545, 4.634312629699707, "[FF] Purpose of the MEO = Cellular telephone communication and navigation"]
-[6.6226091384887695, 5.8978071212768555, "[TT] Quantity of the Feed-OMT Assemblies = 3"]
-[6.593475341796875, 1.9736857414245605, "[TT] Official Data Archive of the NuSTAR = NASA's High Energy Astrophysics Science Archive Research Center"]
-[5.323160648345947, 3.2954697608947754, "[TT] Operator of the MSX = APL"]
-[3.5764272212982178, 6.420690536499023, "[TT] Antenna of the Communications = 12 m antenna at DERA Lasham ground station (26 m DSN antennas)"]
-[14.354308128356934, 3.2728445529937744, "[TT] Mass (kg) of the ERS-2 = 2384"]
-[7.684584140777588, 8.731452941894531, "[TT] Spectral Bands of the MSU-MR = 6 bands in the Visible (VIS) and Infrared (IR)"]
-[5.310598373413086, 3.9515717029571533, "[TT] Number of Satellites of the ICEYE Constellation = Approximately 18"]
-[8.779172897338867, 8.810304641723633, "[TT] Face Sheet Thickness of the Grating = 1mm"]
-[5.722689151763916, 0.9873978495597839, "[FF] Rendezvous Sensor Test Date of the ATV-5 = March 18, 2014"]
-[9.604682922363281, 6.834301471710205, "[TT] Range Resolution of the Wide ultra fine = 1.6 - 3.3 m"]
-[5.124565601348877, 3.293081045150757, "[TT] Manufacturer of the Terra = Lockheed Martin Missiles and Space (LMMS)"]
-[5.528883934020996, 1.0023256540298462, "[TT] First Picture Acquisition Date of the D-Sat = June 26, 2017"]
-[9.796835899353027, -0.4189545214176178, "[TT] Altitude of the TRACE spacecraft = 602 km x 652 km"]
-[6.204620838165283, 7.278656959533691, "[TT] Sampling Rate of the ULF Sensor = 10 Hz"]
-[10.827022552490234, 7.398697853088379, "[TT] Width of the Penumbra = 100+ km"]
-[5.348092079162598, 6.903074264526367, "[TT] Realtime Access Link Speed of the IRIS = 81 Mbit/s"]
-[7.387211799621582, 5.139471054077148, "[FF] Probability Threshold of the Coherency Filter = Adjustable"]
-[6.416760444641113, -0.5888843536376953, "[TT] Observation Time of the TANSO-CAI-2 = Day time"]
-[9.483084678649902, 4.7911200523376465, "[TT] Controller of the ADCS = Kalman Estimator"]
-[8.321454048156738, 6.756580829620361, "[TT] Scan Speed of the PIC = 30 - 750 line/s"]
-[5.667360782623291, 4.379087924957275, "[FF] Satellite Network Provider of the SES = True"]
-[5.620319843292236, 1.1172009706497192, "[TT] Imaging Date of the MSU-MR = Jan. 14, 2015"]
-[8.30644416809082, 2.535973072052002, "[FF] Mission of the Cloud-Aerosol Transport System (CATS) = Unknown"]
-[3.5022082328796387, 5.320106506347656, "[TT] Frequency of the SARP = 406.025 MHz"]
-[10.878464698791504, -0.3170478641986847, "[TT] Available DEM Geocells of the TanDEM-X = Over 15,000 geocells or nearly 80%"]
-[7.529748439788818, 3.7534146308898926, "[TT] Tracking Range of the NightPod = \u00b1 18\u00ba"]
-[8.452163696289062, 1.3467273712158203, "[FF] Objectives of the Aquarius = Understanding ocean circulation, global water cycle and climate interaction. Soil moisture measurements over Argentina"]
-[5.039538860321045, 3.4191441535949707, "[TT] Manufacturer of the Hyperion = Northrop Grumman (formerly TRW)"]
-[4.806674003601074, -1.8398367166519165, "[TT] Sampling Time of the Chang'e-5 Lander = 48 hours"]
-[4.314150810241699, 7.208422660827637, "[TT] Band of the Eutelsat Quantum = Ku-band"]
-[9.0677490234375, 9.996028900146484, "[TT] Pixel Size of the Eastman Kodak KLI14403 linear CCD sensor = 5.0 x 5.0 \u00b5m"]
-[11.841774940490723, 6.71605110168457, "[TT] TGF Energy of the RHESSI = Beyond 20 MeV"]
-[5.708409309387207, 4.638452053070068, "[FF] Ground Station of the ARTEMIS = UHF tactical communications ground station"]
-[5.587862491607666, -1.9872164726257324, "[FF] Instrument of the KOMPSAT-2 = MSC (Multispectral Camera)"]
-[9.970309257507324, -0.32804009318351746, "[TT] Wave Height of the Satellite = 0.5 m to 20 m"]
-[11.175588607788086, 3.0975680351257324, "[FF] Mission of the Colloid Microthruster = Space Technology 7 and LISA"]
-[4.87491512298584, 0.4592759907245636, "[TT] Launch Date of the MAIA = 2022"]
-[8.732970237731934, 3.7558319568634033, "[FF] Measurement of the Electric Field Instrument = 25 km-wide ribbon of gas flowing westward at about 6 km/s"]
-[9.095888137817383, 7.407074451446533, "[TT] Air Pressure of the Metric Camera = About 1020 mbar"]
-[4.798548221588135, 8.002251625061035, "[TT] 1257.5 MHz of the Frequency = -"]
-[10.394632339477539, 5.751487731933594, "[TT] Predicted Temperature Range of the DSX = -116\u00baC to 45\u00baC"]
-[16.49896240234375, 3.5842435359954834, "[TT] Test Service Start of the OneWeb = Late 2021"]
-[9.208450317382812, 5.309823989868164, "[TT] Range of the Acceleration = -50 to +50 G (3-axis)"]
-[5.350660800933838, 0.7353639006614685, "[TT] Arrival Date at NASA/KSC of the TSIS-1 = August 4, 2017"]
-[4.885302543640137, 0.35929062962532043, "[TT] Launch Date of the Rocket Lab\u2019s Electron rocket = April 2"]
-[6.877101898193359, -0.6312931776046753, "[TT] Orbit Period of the ResourceSat-2A = 101.35 minutes"]
-[6.99816370010376, 7.173129558563232, "[TT] Wavelength of the Micropulse Laser Transmitter = 532 nm"]
-[7.764248847961426, -0.8542658686637878, "[FF] Discovery Year of the ICESat-2 = 2007"]
-[5.485447406768799, 6.245678424835205, "[TT] EEPROM of the SMX-2 = 2 MByte"]
-[6.4402313232421875, 4.421901702880859, "[FF] Modules of the Spacecraft = Service module (bus) and payload module"]
-[8.965299606323242, 3.348792791366577, "[FF] Application of the Miniaturized In-Situ Plasma Sensors = NSF Small Satellite program"]
-[8.544998168945312, 5.399938583374023, "[FF] Rigidity Evaluation Relative Error of the STD = \u0394R/R"]
-[6.685128211975098, 4.43098783493042, "[FF] Payload Volume of the STACEM = Not provided"]
-[8.119317054748535, 0.6590444445610046, "[FF] Mission Objective of the Psyche spacecraft = Explore a metal-rich asteroid in the main asteroid belt between Mars and Jupiter"]
-[9.212827682495117, -0.40030959248542786, "[TT] Updated Apogee of the \u00d8rsted satellite = 845 km"]
-[9.126814842224121, 8.073860168457031, "[TT] Exposure Time of the LLNL imaging system = 1 s"]
-[11.482783317565918, 4.813377380371094, "[TT] Shape of the M2 = Aspheric on-axis convex"]
-[7.1066975593566895, 1.7328304052352905, "[FF] Imagery Usage of the FormoSat-2 = Planning field interventions to stop illegal deforestation in progress in the Amazon basin"]
-[8.211430549621582, 7.2949628829956055, "[TT] Technology of the C3D Instrument = CMOS"]
-[10.023388862609863, -1.532103180885315, "[TT] Orbit Inclination of the ASNARO satellite = 97.42 \u00b10.1\u00ba"]
-[4.843114852905273, 0.8200595378875732, "[TT] Launch Year of the UWE-2 = 2006"]
-[7.268656253814697, 5.62144660949707, "[FF] Function of the Front-End Electronics Module (F2EM) = Provides the detectors with all the necessary biasing and clocking signals and performs preamplification and transmission of the video signal to the MEV"]
-[5.100448131561279, 8.33852481842041, "[TT] IF bandwidth of the Millimeterwave receiver = 1 \u2013 1.5 GHz"]
-[13.410125732421875, 7.4704389572143555, "[TT] Output Power of the TXS = 28 dBm"]
-[7.8077497482299805, 1.6128642559051514, "[FF] Test Date of the Dual-frequency Precipitation Radar = July 24-29, 2011"]
-[7.760867118835449, 7.916608810424805, "[TT] Sensitivity of the SCM = 100 nT"]
-[6.37534236907959, 1.8700050115585327, "[FF] URL of the POPSAT-HIP1 = http://blog.isilaunch.com/?p=885"]
-[5.138355731964111, 0.7159910202026367, "[FF] News Release Date of the WFIRST = 30 March 2020"]
-[8.931558609008789, 2.205698013305664, "[FF] Study Level of the Stardust Grain = Atomic"]
-[11.841381072998047, 4.6551032066345215, "[TT] Physical Baseline Length of the KaRIn = 10 m"]
-[12.138842582702637, 4.631970405578613, "[FF] Size of the GOES-T = Small school bus"]
-[8.373993873596191, 4.2575297355651855, "[FF] Measurement of the SRM = Ionizing dose of charged particles"]
-[8.508572578430176, 5.866063117980957, "[TT] Geolocation Accuracy of the Imager = \u2264 3 m"]
-[5.075016498565674, 2.033616781234741, "[TT] Mission Status of the THEOS-2 = Operational (nominal)"]
-[10.773749351501465, -1.1217740774154663, "[FF] Initial Orbit Control of the SLATS = Atmospheric Drag"]
-[5.006397724151611, 6.8458251953125, "[TT] Uplink Date Rate of the \u00d8rsted satellite = 4 kbit/s"]
-[3.3614132404327393, 4.71951150894165, "[FF] Imaging Capability of the NovaSAR-1 = SAR and AIS (Automatic Identification System) data"]
-[8.386792182922363, 4.195818901062012, "[FF] Function of the Charge Sensitive Preamplifier = Convert total charge Q created by the passage of ionizing radiation to an electric impulse"]
-[5.366674900054932, 6.269166946411133, "[TT] Microprocessor Speed of the RAD750 SBC = 132 MHz"]
-[3.4707860946655273, 6.4153852462768555, "[TT] Antenna Size of the Antenna = 3m2"]
-[8.114144325256348, 3.3515801429748535, "[FF] Purpose of the OCO-2 and OCO-3 = Monitor global carbon dioxide emissions"]
-[6.9538421630859375, 7.416192531585693, "[TT] Beam Propagation Factor of the LRI = M 2 < 1.2"]
-[6.244637489318848, -0.2892754375934601, "[TT] Emergency Observation Command Ready Time of the ALOS-2 = Within 60 minutes"]
-[8.890472412109375, 5.3038129806518555, "[FF] Collector Segments Arrangement of the IDM = Along the satellite nadir and the orbit normal"]
-[7.990889549255371, 4.588067531585693, "[FF] Radiation Monitoring of the SPA-1 Dosimeter = Depletion mode, p-channel RADFET from REM"]
-[5.6096696853637695, 6.7662553787231445, "[TT] Daily Data Volume of the Instrument = 50 Gbit"]
-[3.8017380237579346, 4.726229190826416, "[TT] Payload of the Resurs-O spacecraft = Radar instrument, RLSBO"]
-[4.654289245605469, 0.1262345314025879, "[TT] Launch Date of the STARS spacecraft = January 23, 2009"]
-[7.94943904876709, 1.7531862258911133, "[FF] Measurement Type of the Argo = Subsurface-salinity"]
-[8.892580032348633, 7.613358020782471, "[TT] Pan of the Pushbroom imager = 0.45-0.9 \u00b5m"]
-[2.85609769821167, 0.0836327075958252, "[TT] J2000 right ascension (deg) of the B1617-155 (Sco X-1) = 244.979"]
-[7.744643211364746, -0.8508421778678894, "[FF] DOI of the ICESat-2 = 10.1029/2019JC016008"]
-[5.36110782623291, 2.5367839336395264, "[FF] Agency of the MITA = ASI"]
-[5.286441326141357, 5.661235809326172, "[TT] Data Bus of the Payload = LEON II FT MIL-STD-1553, CAN, SpaceWire"]
-[6.57824182510376, 2.91764497756958, "[TT] Image Credit of the DMS = NASA/Digital Mapping System"]
-[6.908987522125244, 3.0556445121765137, "[FF] Mission Type of the MetOp Second Generation = Weather forecast and climate monitoring"]
-[3.4257423877716064, 5.271810054779053, "[TT] Power Consumption of the SAR instrument = 216 W"]
-[1.7207798957824707, 6.137884616851807, "[TT] Hot, Diffuse Gas in the Haloes Percentage of the Universe = 5 percent"]
-[9.440415382385254, -0.25842830538749695, "[TT] Sampling Interval of the Satellite = 25 km"]
-[9.374964714050293, 7.007020950317383, "[TT] Spatial Resolution of the TOMS = 3o x 3o"]
-[6.959907054901123, 3.372694492340088, "[FF] Considered Data of the NOAA = Microwave Sounding Data"]
-[7.893137454986572, 7.243550777435303, "[TT] Compressed Data Rate of the Camera = 105 Mbit/s"]
-[8.109713554382324, 8.60599422454834, "[TT] SNR of the UV/VIS Spectrometer = >12"]
-[14.031237602233887, 7.153425693511963, "[TT] Power Bus Voltage of the MuREM = +5V"]
-[7.352910041809082, 0.2700622081756592, "[FF] Sample Collection Sites of the OSIRIS-REx = Nightingale, Kingfisher, Osprey and Sandpiper"]
-[10.813053131103516, 1.4103827476501465, "[TT] Mass of the ASASSN-19bt = 6 million times the Sun\u2019s mass"]
-[3.935211181640625, 2.0068130493164062, "[TT] Launch Vehicle of the ResourceSat-2A = PSLV-C36"]
-[6.536931991577148, -1.9867439270019531, "[TT] Contract Signing Date of the Jason-CS / Sentinel-6 = May 11, 2015"]
-[7.69550085067749, 5.390971660614014, "[TT] Vibration Test Frequencies of the FPM = 5 Hertz and 2000 Hertz"]
-[8.571703910827637, 5.465290069580078, "[TT] Velocity Determination of the Transit Navigation = Not permitted"]
-[11.960587501525879, 4.9278130531311035, "[TT] Dimensions of the SCDE = about 100 mm x 150 mm x 30 mm"]
-[4.561059474945068, 6.217512607574463, "[FF] X-band Downlink Capability of the GOMX-3 = High-speed"]
-[11.902899742126465, 5.4429097175598145, "[TT] Instrument Size of the SBVR = 750 mm x 247 mm x 348 mm"]
-[6.622952461242676, -0.43032822012901306, "[TT] Period of the FASat-Alfa = 98.7 minutes"]
-[4.611701011657715, 1.6153148412704468, "[TT] Launch Date of the SkySat-16 to -18 = 13 June 2020"]
-[9.820886611938477, 2.6599340438842773, "[FF] Deployment Date of the NanoRacks = March 11, 2015"]
-[7.847300052642822, 7.177365303039551, "[TT] Mode of the EPIC CCDs = Photon counting mode"]
-[8.248363494873047, 4.232950687408447, "[FF] Probe Tips Contamination Mitigation of the m-NLP = Protective covers, replacement tips, or repeated cleaning"]
-[13.855009078979492, 3.290706157684326, "[TT] Electronics Package Mass of the FlaPS = 0.5 kg"]
-[10.280256271362305, 5.75633430480957, "[TT] Measurement Methods of the Temperature = 2 ways"]
-[8.945884704589844, -0.7022784352302551, "[TT] On-Orbit Performance of the ATMS = Superior to AMSU"]
-[3.3572781085968018, 6.474878311157227, "[TT] Diameter of the Receiving Antenna = 100 cm"]
-[7.06653356552124, 1.2878018617630005, "[TT] Retirement Date of the Spitzer Space Telescope = Jan. 30, 2020"]
-[7.3216376304626465, 1.045292854309082, "[TT] Budget Cap of the SeaSat = $68 M plus launch vehicle costs"]
-[4.518191337585449, 3.23934268951416, "[TT] Prime Contractor of the Galileo 2nd Generation Satellites = Thales Alenia Space in Italy"]
-[3.7477400302886963, -1.0146859884262085, "[TT] Trajectory Profile of the RVX = Highly elliptical orbit"]
-[12.075021743774414, 4.502545356750488, "[TT] Size of the Spacecraft = 2 m x 3 m x 8 m"]
-[7.835377216339111, 9.089097023010254, "[TT] Wavelength of the PH3 = 762 \u00b1 5 nm"]
-[8.083902359008789, 2.4065096378326416, "[FF] Unique Feature of the CALIPSO = First satellite to provide information on the vertical structure of clouds and aerosols, as well as provide vertically-resolved estimates of the amount of rain and ice in clouds"]
-[4.787725925445557, -1.5373467206954956, "[FF] Landing Technology Status of the Tianwen-1 = Ready for 2020"]
-[10.241817474365234, 6.0379204750061035, "[TT] Temperature of the VNIR FPA = 293K"]
-[10.98270320892334, 3.553443193435669, "[TT] Cube Volume of the E1P-2 CubeSat = 10 cm"]
-[4.9375457763671875, 0.4756116271018982, "[TT] Launch Year of the TecSAR = 2008"]
-[9.274581909179688, 0.14933061599731445, "[TT] Length of the Pas Moraine = 300 kilometers (185 miles)"]
-[10.393914222717285, 2.977308988571167, "[FF] AI Model Testing of the \u03a6sat-2 = Run on generic GPU, Tested in targeted hardware Intel\u00ae Movidius\u2122 Myriad\u2122 2 on Neural Compute Stick with OpenVINO (2020.3), Tested with FlatSat in real configuration"]
-[14.054661750793457, 3.5562479496002197, "[TT] Mass of the Iris Radio = 0.4 kg"]
-[10.220874786376953, 5.721574306488037, "[FF] Radiometric Performance of the EO Module = Maintained by limiting the temperature change between views of cold space"]
-[7.370687961578369, 5.145831108093262, "[FF] Configuration of the STOs and STAEs = 3 on but 2 in operation"]
-[6.774774074554443, 7.336650371551514, "[TT] ADC Sampling Rate of the Rx Module = 40 Msamples/s"]
-[9.90749454498291, 7.215750217437744, "[TT] Observed Area of the MUX = 20 x 11 km"]
-[4.019327640533447, 2.1712257862091064, "[TT] Launch Vehicle of the MSG-3 = Ariane-5 ECA"]
-[8.37131118774414, 3.7180209159851074, "[FF] CRISM Spectrometer of the Mars Reconnaissance Orbiter = Spectrometer"]
-[11.288866996765137, 3.330660104751587, "[TT] Development Location of the Precision Micropropulsion System = Jet Propulsion Laboratory"]
-[13.774701118469238, 2.969144105911255, "[TT] Mass of the Spacecraft = 80 kg"]
-[12.385284423828125, 3.210252523422241, "[TT] Remaining Propellant of the Advanced Composition Explorer = Approximately 46 kg"]
-[13.241023063659668, 7.2169342041015625, "[TT] Power Consumption of the OSDP = 28 W"]
-[6.134432792663574, 4.926447868347168, "[FF] Function of the C&DH = Serves as the hub for all data received by and sent from the spacecraft"]
-[5.240326881408691, 3.1563780307769775, "[TT] Activation Location of the LCT = Alphasat"]
-[9.458270072937012, 7.273510456085205, "[TT] Ground Resolution of the Corvus-HD = 2.5 m"]
-[8.086710929870605, -1.2129533290863037, "[TT] Pulse Rate of the ICESat-2's instrument = 10,000 pulses of light a second"]
-[6.7569899559021, 5.101166248321533, "[FF] Control Hierarchy of the RISAT-SAR = PLC (Payload Controller) > RF and baseband subsystems > DCG (Digital Chirp Generator), the V and H receivers, the FG (Frequency Generator), Feeder SSPA (Solid\u2010State Power Amplifier), CAL (Calibration Switch Matrix) and four DACSs (Data Acquisition and Compression Subsystems)"]
-[8.368059158325195, 7.0675458908081055, "[FF] Technologies of the Micro-CMOS Cameras = Auto-exposure, high-speed compression of color imagery and static gray image, and sub-sampling methods"]
-[5.541408061981201, 8.054444313049316, "[TT] Measurement Range of the Cluster S/C = DC to 10 Hz"]
-[5.443269729614258, 6.2993011474609375, "[TT] Memory Capacity of the CoReCi = Various capacities"]
-[9.545740127563477, 3.842132091522217, "[FF] Operational Environments of the Vector Magnetometer = Various environments, in particular for aeromagnetic surveys"]
-[11.808903694152832, 6.620434284210205, "[TT] Proton Dynamic Pressure of the ACE = ~1.4 nPa"]
-[13.448797225952148, 2.9144046306610107, "[TT] Mass of the Satellite = 90 kg"]
-[14.639102935791016, 6.6524248123168945, "[TT] Power Storage of the EPS = Li-ion battery of 9 Ah capacity"]
-[5.794884204864502, 3.3742265701293945, "[FF] Development Cost of the BRITE = Minimized"]
-[8.895477294921875, 2.854276418685913, "[FF] Support Goal of the MinXSS mission = To study the \"dynamics and energetics of the upper atmosphere, with particular emphasis on the hard to observe region between 80 and 150 km\""]
-[7.7653093338012695, -2.387636184692383, "[TT] Instrument Type of the GOLD = Space environment, Magnetic field"]
-[4.7206034660339355, 2.766993999481201, "[TT] Launch Contractor of the OCO-2 = ULA (United Launch Services LLC)"]
-[6.146354675292969, -0.588768720626831, "[TT] Operation Time of the TanSat = At least three years"]
-[5.41762638092041, 1.697281837463379, "[FF] Mission Status of the ALOS-2 = Unknown"]
-[6.028825759887695, 2.219045400619507, "[TT] Next Flight Type of the Orion = Uncrewed"]
-[4.55458927154541, 8.011646270751953, "[TT] Rx frequency of the Antenna = 18.25 GHz\u00b1550 MHz"]
-[6.740041732788086, 2.603834867477417, "[FF] Mission of the UrtheCast = Earth Observation"]
-[8.250858306884766, 6.279803276062012, "[FF] Objective of the HIP (Heterojunction Internal Photoemission) Infrared Sensors = Determine if exposure of the HIP sensor to the complex spectrum of incident radiation might result in increased sensitivity"]
-[5.181005477905273, 2.3371975421905518, "[FF] Usage of the TacSat-4 = SATCOM between many platforms"]
-[4.158811569213867, 7.178658485412598, "[TT] Band of the Frontier Radio = X-band"]
-[9.360467910766602, 5.095695495605469, "[TT] Attitude Control Stability of the BRITE spacecraft = 1 arcmin rms"]
-[11.380598068237305, 2.7855217456817627, "[TT] Total Mass of the Minisatellite = 150 kg"]
-[7.210484027862549, 5.9924163818359375, "[TT] Accuracy of the Clock = 100 parts per billion"]
-[13.519327163696289, 5.764066696166992, "[TT] Power Generation of the SPOT-2 = Solar array"]
-[5.781989574432373, 0.9986149072647095, "[FF] Launch Date of the BepiColombo = February 2007"]
-[9.787220001220703, 8.481621742248535, "[TT] IFOV of the Telescope = 0.004\u00ba"]
-[5.90080451965332, -0.48007985949516296, "[TT] Expected Fate of the ChipSats = Burning up"]
-[9.60461139678955, 4.788903713226318, "[TT] Stabilization of the TARANIS spacecraft = 3-axis"]
-[6.429788112640381, 3.5777876377105713, "[TT] Function of the CM = Houses and transports NASA's astronauts during spaceflight missions"]
-[8.868241310119629, 6.9120564460754395, "[TT] GSD of the DMC-2 = 2.5 m"]
-[10.332786560058594, 5.430715560913086, "[TT] Heater Control of the Payload Thermal Control = Precision"]
-[10.90306568145752, 2.0759077072143555, "[TT] Commissioning Start Date of the XRS instrumentation = End of November 2007"]
-[6.681288242340088, 7.527131080627441, "[TT] Digitization of the Observation Data = 12 bit"]
-[7.618340492248535, 5.738133907318115, "[TT] TRL Level of the Flash Imaging LiDAR = 7"]
-[7.096757888793945, 3.730933904647827, "[FF] Unknown of the ZY-1-02C Satellite Images = Unknown"]
-[5.379114627838135, 8.051912307739258, "[TT] Low Power Frequency Range of the VLF transmitter = 50 \u2013 750 kHz"]
-[2.5664281845092773, 0.16068816184997559, "[TT] Pulse period (ms) of the J1846-0258 = 325.684"]
-[9.482993125915527, 7.031886100769043, "[TT] Spatial Resolution of the MSI-0 and MSI-1 = 32.5 m"]
-[6.1272969245910645, 6.473167419433594, "[TT] Latency Requirement of the S-3 NRT = Within 30 minutes"]
-[8.058134078979492, 9.294702529907227, "[TT] Wavelength of the Liquid water = 2.903 \u00b5m"]
-[6.925395488739014, -0.6719633936882019, "[TT] Cold Start Time of the DORIS = Less than 1 orbit"]
-[4.794588565826416, 7.107754230499268, "[TT] X-band Transmission Speed of the NigeriaSat-2 = Up to 210 Mbit/s"]
-[11.808375358581543, 0.056520238518714905, "[TT] Discovery Tool of the TESS = Exoplanets"]
-[4.399297714233398, 3.1113550662994385, "[TT] Location of the Ground Station = Villafranca, Spain"]
-[11.748682975769043, 7.522740840911865, "[FF] Congress Date of the Megha-Tropiques = Sept. 29 to Oct. 3, 2008"]
-[6.365701675415039, 0.07877177745103836, "[TT] Ready Time of the 90-satellite constellation = 24 months later"]
-[3.420743465423584, 3.612259864807129, "[TT] Launch Date of the PAZ = February 2018"]
-[10.127707481384277, 1.5856410264968872, "[FF] Light Baseline of the Quasar = Gray line"]
-[8.498690605163574, 9.489238739013672, "[TT] Responsivity Measurement of the Responsivity Measurement = 106 A/W"]
-[3.2822017669677734, 1.5311778783798218, "[TT] Testing Duration of the Sentinel-2C = Until the end of 2021"]
-[6.176614761352539, 4.877560615539551, "[FF] Function of the Automation Engine = Supervise the complete cycle of telecommand uplink and execution, as well as reaction monitoring of telemetry"]
-[9.988236427307129, 7.756752014160156, "[FF] Telescope Optics of the EUVI = Fully baffled"]
-[8.576754570007324, 8.416030883789062, "[FF] Specialization of the LET spectrometer = Highly specialised"]
-[10.064045906066895, 2.255406379699707, "[FF] Optics URL of the Imaging X-ray Polarimetry Explorer = https://doi.org/10.1117/12.2275502"]
-[8.43000602722168, 7.692222595214844, "[TT] Detector Type of the OSIRIS = One-dimensional InGaAs (128 pixel) linear arrays"]
-[7.007633686065674, 7.739887714385986, "[TT] Reflector Quantity of the Mayak = 4"]
-[4.85320520401001, 7.969385147094727, "[TT] Carrier frequency (MHz) of the E5b-Q = 1207.14"]
-[8.345343589782715, 0.4308866858482361, "[TT] Previous Record Crest Height of the Yellowstone River = 11.5 feet"]
-[6.000802040100098, -0.4635017216205597, "[TT] Mission Duration of the DSX spacecraft = 23 months"]
-[8.928661346435547, 0.2983025014400482, "[TT] Orbital Range of the Ryugu = Mostly between Earth and Mars"]
-[9.183941841125488, 4.14321231842041, "[TT] Observation Capability of the STEREO spacecraft = More than 270\u00ba of solar longitude"]
-[4.694522857666016, 4.913926601409912, "[FF] Software of the TIE = AIS (Automated Identification System)"]
-[9.792275428771973, -0.427812784910202, "[TT] Altitude of the Landsat-9 = 705 km"]
-[9.416306495666504, 4.754180431365967, "[TT] Attitude Control of the LAGEOS = None"]
-[8.548564910888672, 7.415504455566406, "[TT] Image Size of the Supervision Cameras = 1280 x 1024 pixels"]
-[8.205690383911133, 5.471329212188721, "[FF] Aperture Area of the IBEX-Lo sensor = Fourth of the aperture area for IBEX-Lo"]
-[8.381021499633789, 5.780698299407959, "[FF] Metrology Metric of the Drag-Free Technology = Measurement of the absolute position of a drag-free test mass or the differential measurement of the distance between two drag-free test masses"]
-[4.577625274658203, 7.328129291534424, "[TT] S-band 1Mbit/s Downlink of the UoSAT-12 = 1"]
-[13.380274772644043, 7.334238052368164, "[TT] Power of the PLC = 15 W"]
-[6.154460906982422, 2.950153350830078, "[TT] Daily system capacity of the WorldView Legion = 3x"]
-[5.194055080413818, 7.025274753570557, "[TT] Downlink Speed of the Communication system = 2.25 Mbit/s"]
-[6.4532952308654785, -0.5602299571037292, "[TT] Time in Spacecraft of the Valves = 46 days"]
-[3.5733959674835205, -0.713807225227356, "[TT] Resonance Ratio of the Satellite Orbit = 3:1"]
-[9.100605964660645, 0.8648401498794556, "[FF] Key Unknown of the Kinetic Impactor Technique = Beta"]
-[9.683210372924805, 4.393209934234619, "[TT] DC Measurements Uncertainty of the PNI RM3000 = 14 nT"]
-[3.102670907974243, 2.2263104915618896, "[TT] Area Coverage of the Copernicus Sentinel-3 = 100 000 km2"]
-[11.460854530334473, 5.534940242767334, "[TT] E of the Haynes 242 = 220-230 GPa"]
-[5.0993266105651855, 3.3747987747192383, "[TT] Manufacturer of the Landsat-9 = Northrop Grumman"]
-[10.633197784423828, 3.941042900085449, "[TT] Anomalies of the Dragsail = Manifested"]
-[7.009880542755127, 7.01582145690918, "[FF] Number of Sensors of the Laser Control Board = 20"]
-[6.76088809967041, -0.3203285336494446, "[TT] Period of the \u00d8rsted satellite = 100 min"]
-[11.776101112365723, 6.769577503204346, "[TT] Energy Range of the Instrument = 43 and 300 keV"]
-[5.242065906524658, 8.418020248413086, "[TT] Bandwidth of the Channel = 500 MHz"]
-[5.349003314971924, 0.026465533301234245, "[TT] End of Life Date of the IRS-P6 = 07 Dec 2013"]
-[8.063101768493652, 2.48537015914917, "[FF] Data Collection of the Resurs-O1 = Atmosphere, Cloud type, amount and cloud top temperature, Radiation budget"]
-[10.437463760375977, 5.782591342926025, "[TT] Operational Temperature of the Supercapacitor = -40\u00b0C to +70\u00b0C"]
-[5.88927698135376, 0.8549161553382874, "[FF] Launch Date of the KANOPUS-V-IK = July 14, 2017"]
-[8.033092498779297, 8.835906028747559, "[TT] Wavelength Stability of the LD Output = <0.1%"]
-[5.101122856140137, 1.279045581817627, "[FF] Conference Presentation Date of the CDHS = Oct. 2-6, 2006"]
-[6.34910249710083, -1.3497576713562012, "[TT] Re-Entry Date of the GRACE 1 = 11 March 2018"]
-[7.69943904876709, 2.243872880935669, "[FF] Function of the Open Loop tracking mode = Exploits an on-board DEM (Digital Elevation Map) to adapt the PRI (PRI=1/PRF) for the elevation of inland waters"]
-[11.409485816955566, 5.003658771514893, "[TT] Overall Length of the COR2 = 1348 mm"]
-[6.392828941345215, 1.74898362159729, "[FF] URL of the Cluster = http://www.esa.int/Our_Activities/Operations/Cluster_satellite_catches_up"]
-[8.763646125793457, 8.521995544433594, "[TT] Field of View of the Spectrometer = 3.5 x 3.5 to 7 arcsec x 7 arcsec"]
-[9.092247009277344, 7.12575626373291, "[TT] Image Resolution of the ASAP-Light = 4 Mpixels"]
-[5.189814567565918, 5.3730082511901855, "[TT] Tracking Systems of the Antenna Subsystem = Mono-pulse and gyro-tracking systems"]
-[3.925161123275757, 3.4321227073669434, "[FF] Program Completion of the Galileo = May 2003"]
-[8.953150749206543, 5.5102434158325195, "[TT] Pointing Accuracy of the Spacecraft = < 0.02\u00ba"]
-[9.937758445739746, 1.4219001531600952, "[TT] Sky Area of the Coma galaxy cluster = Roughly the size of four full Moons"]
-[9.400045394897461, 5.987957000732422, "[TT] Open Position Angle of the CSM = 63\u00ba"]
-[8.188702583312988, 2.926565408706665, "[FF] Measurement Domain of the LMI = Atmosphere"]
-[7.268110275268555, 1.8612996339797974, "[TT] Ground Sample Distance of the Carbonite-1 = 1 meter"]
-[3.611459732055664, 6.491343021392822, "[TT] Antenna Diameter of the X-band ground station = 11 m"]
-[8.438369750976562, 3.175191640853882, "[TT] Ozone Concentration Measurement Altitudes of the UVSP = 50 - 75 km"]
-[11.652750968933105, 6.6757612228393555, "[TT] Energy Range of the Telescope = 1/4 keV"]
-[8.71893310546875, 3.010453939437866, "[FF] Connection of the ICON = Physical connection between our world and the immediate space environment around us"]
-[7.144226551055908, -0.7452329993247986, "[TT] Host Star Consumption Time of the TOI-2337b = Less than 1 million years"]
-[11.872391700744629, 3.0537054538726807, "[TT] Total \u0394V of the Perigee Raising = 40 m/s"]
-[4.314435958862305, 7.400069236755371, "[TT] Convolutional Encoding of the X-band Transmitter = \u00bd rate k=7"]
-[7.814604759216309, 2.0793352127075195, "[TT] Instrument Type of the COCTS = Ocean colour instruments"]
-[5.107486724853516, 5.800353527069092, "[TT] Protocol of the TT&C S-band Communications = CCSDS"]
-[7.877861499786377, 3.080491304397583, "[FF] Range of CO2 Absorption Bands of the TanSat = Unknown"]
-[10.613614082336426, 3.423909902572632, "[TT] Design of the BRO-1 = 6U CubeSat"]
-[7.614382266998291, 4.496211528778076, "[FF] Unknown of the AMS-02 Transition Radiation Detector = Unknown"]
-[7.0503106117248535, 2.0963945388793945, "[FF] Price of the Landsat-7 = The price tag for Landsat-7 imagery is substantially lower than for the commercial products of Landsat-4 and -5"]
-[10.921506881713867, 7.532738208770752, "[TT] Swath Width (Simultaneous) of the HRV = 117 km"]
-[11.803778648376465, -0.0680912435054779, "[TT] Closest Approach to Earth of the TESS = Once per orbit"]
-[9.226285934448242, 4.227384090423584, "[TT] Manufacturer of the COMPASS-1 = University of Applied Science, Aachen, Germany"]
-[9.288832664489746, 6.99770975112915, "[TT] Resolution of the DST = 1 m GSD"]
-[5.704135894775391, 7.1989006996154785, "[TT] Data Rate of the WPM = 240 Mbit/s"]
-[8.714400291442871, -0.23117098212242126, "[TT] Apogee (km) of the Meteor-3-1 = 1263"]
-[9.626307487487793, 6.925088882446289, "[TT] Grid Resolution of the L2SMP = 36 km EASE-2"]
-[3.3332138061523438, 5.0201005935668945, "[TT] Imaging Modes of the RISAT-SAR = Co-polarisation and cross-polarisation"]
-[10.52235221862793, 3.322787046432495, "[TT] Type of the Hiber-3 = 3U CubeSat"]
-[11.789812088012695, 6.4654154777526855, "[FF] Energy Loss of the Neutron-Element Collisions = More like a ping pong ball hitting a bowling ball"]
-[10.953052520751953, 7.468855857849121, "[TT] Swath Width of the BIROS = 211 km"]
-[14.067757606506348, 4.03906774520874, "[TT] Instrument Mass of the AATSR = 101 kg"]
-[7.858486652374268, 5.164292812347412, "[FF] Test Type of the Konnect satellite = Vibration"]
-[5.873538494110107, -0.40861624479293823, "[TT] Lifetime Revolutions of the MWI Instrument = 180 million cycles"]
-[5.6418280601501465, 7.161035537719727, "[TT] Data Rate of the OGS = 80 Mbit/s"]
-[9.576190948486328, 4.1663641929626465, "[TT] Type of the SSM = Magnetic field"]
-[4.9791483879089355, 3.506662607192993, "[TT] Manufacturer of the EPS = Tiger Innovations"]
-[4.647709846496582, 5.091235637664795, "[FF] Basic Tasks of the LUTs = Track Cospas and Sarsat satellites, Recover beacon signals from satellites, Perform Doppler processing to determine geographic location, Send resulting Doppler solutions to the associated MCC"]
-[9.427789688110352, 5.325836181640625, "[TT] Mounting of the TWINS = Rotating actuator platform"]
-[8.313002586364746, 2.458115816116333, "[TT] Number of Substorms Observed of the THEMIS Constellation = 57"]
-[10.884359359741211, 3.8071165084838867, "[FF] Ride Capability of the CubeStack = Tertiary canisterized"]
-[6.655257225036621, -0.4223193824291229, "[TT] Period of the GEOS-1 = 120.3 minutes"]
-[8.455835342407227, 5.542942523956299, "[TT] Orbit Position Accuracy of the GPS Receiver = 50 m (1\u03c3)"]
-[7.487211227416992, 5.020904064178467, "[FF] Alignment of the FG = Unknown"]
-[13.226754188537598, 5.542582035064697, "[FF] Installation Date of the ISS Roll-out Solar Arrays (iROSA) = June 16 and 20"]
-[5.742099285125732, 3.7829926013946533, "[TT] Number of Satellites of the Sateliot IoT Nanosatellite Constellation = Up to 100"]
-[6.974694728851318, 2.42465877532959, "[FF] URL of the Remote Sensing Activities = http://www.oosa.unvienna.org/pdf/pres/stsc2012/tech-24E.pdf"]
-[8.257509231567383, 2.453186273574829, "[TT] Number of Pristine Vantage Points of the THEMIS Constellation = 12"]
-[7.644092082977295, 5.7164835929870605, "[FF] Validation Tool of the Ground-Based Lidar Network = Used"]
-[4.064681053161621, 0.33102911710739136, "[TT] Launch Date of the Corvus-BC 3 = August 2, 2017"]
-[4.856385707855225, 0.5122400522232056, "[TT] Launch Date of the ALTIUS = May 2025"]
-[7.311737060546875, 7.516122341156006, "[FF] Uplink Frequency of the Imager Sounder = 4781 MHz"]
-[5.032830715179443, 1.8680585622787476, "[FF] Naming of the Giove = Italian word for \"Jupiter\""]
-[3.4724438190460205, -0.8934530019760132, "[TT] Orbit of the IRIS = Polar sun-synchronous orbit"]
-[8.596290588378906, 2.378910541534424, "[FF] Impact of the EMIT = Help scientists understand which kinds of dust dominate each region and advance their understanding of dust\u2019s impact on climate and the Earth system"]
-[5.513607501983643, 0.36333855986595154, "[TT] Launch Date to ISS of the Flock 1b = July 13, 2014"]
-[10.740315437316895, -0.18182508647441864, "[TT] Formation Flight Separation of the TanDEM-X = 200 m"]
-[5.879251003265381, 3.4764230251312256, "[FF] Operator of the TIM and SIM instruments = NOAA"]
-[9.616644859313965, 2.4883689880371094, "[FF] Data Color of the NuSTAR = Green"]
-[9.190957069396973, 4.279912948608398, "[TT] Attitude Determination of the UniSat-3 = Magnetometer readings and the telemetry data of three solar panels"]
-[7.9347825050354, 5.436725616455078, "[TT] Range-independent Noises of the FLLS = \u00b5m"]
-[4.222481727600098, 0.3703064024448395, "[FF] Launch Date of the JPSS-1 = 2016"]
-[4.186967849731445, 6.942950248718262, "[TT] Frequency Band of the ICEYE Constellation = X-band"]
-[11.815303802490234, 6.736867904663086, "[TT] Ion Energy Range of the SWEPAM = 0.26 - 35 keV"]
-[11.424720764160156, 4.343299865722656, "[TT] Size of the Tyvak 61C = 3U"]
-[9.791610717773438, 8.14978313446045, "[TT] Focal Length of the Lenses = 2.6 m"]
-[12.035040855407715, 5.00375509262085, "[TT] Volume of the DPU = 230 x 300 x 250 mm"]
-[7.161245346069336, 5.135811805725098, "[FF] Components of Flight Prototype Model of the MinXSS = Structure, CDH custom board, EPS custom board, custom motherboard, custom battery pack, and plastic 3D printed prototypes of the secondary instrument housing and antenna deployment module"]
-[7.4535322189331055, 3.475086212158203, "[FF] Study Subject of the Proba-3 = Sun\u2019s inner corona"]
-[14.150691032409668, 3.3008954524993896, "[TT] Mass of the TXS = 75 g"]
-[9.579804420471191, 3.7518558502197266, "[TT] Strength of the Earth's Magnetic Field = 0.5 gauss, 5 x 10-5 tesla"]
-[8.278142929077148, -0.6066209077835083, "[FF] Collision Date of the A-74 iceberg = 20 August 2021"]
-[12.056188583374023, 6.259467124938965, "[TT] Antiproton Sample of the AMS = 349,000 antiprotons"]
-[9.460347175598145, 7.030818939208984, "[TT] Resolution of the IMI = 15 - 50 km"]
-[7.817327976226807, 8.625595092773438, "[TT] Spectral Range of the M16 filter = 11.5 - 12.5 \u00b5m"]
-[9.943180084228516, 5.696156024932861, "[TT] Focal Plane Temperature Stability of the ASTERIA = Better than \u00b10.01 K"]
-[9.05368709564209, 2.613368272781372, "[TT] Duration of the Geomagnetic Storm = Feb. 2"]
-[11.098458290100098, 4.984712600708008, "[FF] Tether Composition of the ProSEDS = 10 km of nonconducting Spectra tether for ballast and to begin the deployment, and of a 5 km of aluminum wire (1.2 mm diameter)"]
-[14.207978248596191, 3.1440398693084717, "[TT] Mass of the CONSERT = 1.8 kg"]
-[5.1998419761657715, 2.957702398300171, "[TT] Operator of the SEOSAT-Ingenio = ESA"]
-[4.794764041900635, 0.27961844205856323, "[TT] Launch Date of the Crew-4 = Spring of 2022"]
-[6.853719234466553, 4.6547136306762695, "[FF] Unknown of the DSP ASIC = Unknown"]
-[9.608636856079102, 8.222309112548828, "[TT] Field of View of the EPD-E = < 28\u00b0"]
-[7.977152347564697, 7.422693729400635, "[TT] Hyperspectral Imager of the HJ-1A = 1"]
-[4.246688365936279, 0.7341229319572449, "[TT] Operation Period of the EDRS Space Data Highway = 2015 until 2021, with an option for extension until 2028"]
-[6.4996442794799805, -0.545181393623352, "[TT] Period of the Spacecraft = 97.34 minutes"]
-[4.983027458190918, 1.4718031883239746, "[FF] Image Acquisition Date of the Gokturk-2 = June 23, 2013"]
-[7.493684768676758, 5.97650146484375, "[FF] Objective of the LRR = Spacecraft POD (Precise Orbit Determination) to cm-level accuracy by SLR (Satellite Laser Ranging)"]
-[5.0042290687561035, 0.5383888483047485, "[TT] Maneuver Date of the P2 = Early May 2012"]
-[5.469790935516357, 1.1427708864212036, "[FF] Publication Date of the Supercapacitors = 2009"]
-[4.293228626251221, 7.303431510925293, "[FF] Ka-band Disadvantages of the SARAL/AltiKa = Attenuation due to water/water vapour in case of rain, resulting loss of data"]
-[6.581172943115234, -2.041703462600708, "[TT] Year of Launch of the Jason-2 = 2008"]
-[10.070560455322266, -1.5643855333328247, "[TT] Inclination of the BIROS = 97.56\u00ba"]
-[6.554771900177002, -0.80921471118927, "[TT] Data Release Frequency of the GRACE = Weekly"]
-[8.107170104980469, -1.1672319173812866, "[TT] Laser Instrument (Lidar) of the ICESat-2 = Measures height by sending out signals and timing how long they take to reflect off Earth\u2019s surface and return to their respective satellites"]
-[6.062376976013184, 0.5553784966468811, "[TT] Last Communication Date of the ASTERIA = Dec. 5, 2019"]
-[8.806593894958496, 0.25025391578674316, "[TT] Basalt Flows Fill Time of the Von K\u00e1rm\u00e1n crater = ~3.35 Ga"]
-[9.690855026245117, 0.16107141971588135, "[FF] Parachutes of the CM (Crew Module) = 11"]
-[8.325774192810059, 6.635571479797363, "[FF] Type of the SPOT-6 = Optical imaging specialist"]
-[6.720182418823242, 2.0766727924346924, "[TT] Number of Standard Images in December 2012 of the COSMO-SkyMed = More than 300,000"]
-[4.711946964263916, 8.076617240905762, "[TT] Chirp Signal Bandwidth of the P Mode = 240 MHz"]
-[8.269655227661133, 8.068755149841309, "[TT] Quantum Efficiency Improvement of the Device = Over 20% at 1000 nm"]
-[9.562468528747559, 2.729774236679077, "[FF] Purpose of the Dual Aperture X-ray Solar Spectrometer (DAXSS) = Measure the soft X-ray (SXR) spectrum of the sun during a quiescent period through the solar maximums"]
-[11.211358070373535, 5.882421970367432, "[TT] Material of the Adsorbent Bed = Zeolite"]
-[10.030850410461426, 0.5364621877670288, "[TT] Separation Distance of the Satellite Constellation = 100-1000 km"]
-[7.857480525970459, 1.5994932651519775, "[FF] Purpose of the GPM = Vertical structure and distribution of precipitation"]
-[6.100519180297852, 4.725931644439697, "[FF] Autonomy of the Link Management System = Fully autonomous"]
-[8.991811752319336, 8.558056831359863, "[TT] Calibration Lamp Wavelength of the Telescope = 546.1 nm"]
-[14.06395435333252, 4.030789375305176, "[TT] Instrument Package Mass of the LCROSS = 12.4 kg"]
-[6.759011268615723, -0.6581678986549377, "[FF] Orbit Intersections of the PREFIRE = Intervals of 1-12 h"]
-[9.711915016174316, -0.425003319978714, "[TT] Operational Altitude of the GNOMES-1 = 650 km"]
-[6.882856845855713, 4.968619346618652, "[FF] Status of the P-PODs = Needed to be de-manifested"]
-[6.963489532470703, 1.198251485824585, "[FF] Solar Wing Deployment Test of the BepiColombo = March 6, 2017"]
-[10.889830589294434, 3.7441248893737793, "[TT] Solar Sail Deployment Test Date of the NEA Scout = 28 June 2018"]
-[5.1122941970825195, 4.381880283355713, "[FF] Reentry of the Starlink Satellites = Up to 40 satellites"]
-[7.482681751251221, 4.719761371612549, "[FF] Type of the REIS (JSS-56) instrument = REIS (JSS-56)"]
-[8.862915992736816, 2.4452879428863525, "[FF] Solar Observation of the SOHO = March 19, 2015"]
-[7.180398941040039, 7.070900917053223, "[TT] Interface Temperature of the Power Laser Head = 0.5 K"]
-[3.358870506286621, 1.4609534740447998, "[TT] Launch Year of the Sentinel-1A/B = 2016"]
-[6.849593162536621, 3.532442569732666, "[TT] Source of the Induced Pluripotent Stem Cells = Adult cells genetically programmed to return to an embryonic stem cell-like state"]
-[4.923367500305176, 8.26740837097168, "[TT] Frequency of the MWR = 23.8 GHz"]
-[9.018131256103516, 5.870391368865967, "[TT] Absolute Pointing Required of the COR1 = 7 arcsec"]
-[13.391742706298828, 5.471240520477295, "[TT] Type of the Solar array = Fixed, single wing, three panel"]
-[5.520256042480469, 2.8429996967315674, "[TT] Number of Formal Cooperation Projects of the ESA and EDA = Eight"]
-[8.632513046264648, 5.735665321350098, "[TT] Relative Position Measurements Accuracy of the CanX-4&5 = Centimeter-levels"]
-[7.9200897216796875, 7.862906455993652, "[TT] No of detectors of the Channel = 1 + 1 redundant"]
-[6.40170955657959, 4.15973424911499, "[FF] Usage of the MDA = Dock for the command and service modules"]
-[4.911612033843994, 0.6292688846588135, "[TT] Launch Date of the DSCOVR = February, 11, 2015"]
-[8.446281433105469, 1.8139533996582031, "[FF] Role of the Thermohaline Circulation = Supplying heat to the polar regions"]
-[4.877275466918945, 5.855775833129883, "[TT] Link Establishment of the LLITED satellites = Beacon and proper serial number code"]
-[7.1716814041137695, 5.026732921600342, "[FF] Operational Modes of the LUTI = Survival mode, Standby mode, Ready mode, Imaging mode, Diagnostic mode"]
-[9.389202117919922, 6.191094398498535, "[TT] Sensor Type of the LINAS = Hot-filament ionization gauge"]
-[8.144838333129883, 0.11144176125526428, "[FF] Launch Date of the Meteor-M2-2 = 5 July 2019"]
-[9.315296173095703, 4.946956634521484, "[TT] Attitude of the Satellite = BBQ-attitude"]
-[12.074376106262207, 3.7012927532196045, "[TT] First Actuation Pressure of the T3\u00b5PS = 711 mbar"]
-[4.935710906982422, 3.367422342300415, "[TT] Manufacturer of the IVM = University of Texas, Dallas"]
-[13.344647407531738, 7.701106071472168, "[TT] Power of the Transmitters = 40 W"]
-[7.942906856536865, 0.14488700032234192, "[FF] Monitoring of the GRACE-FO = Monthly changes in the distribution of mass within and among Earth's atmosphere, oceans, land and ice sheets, as well as within the solid Earth itself"]
-[8.555782318115234, 3.8223628997802734, "[FF] Observed Atoms of the IBEX = Hydrogen, oxygen, neon and helium"]
-[13.210872650146484, 6.265866279602051, "[FF] Risk of the HORYU-2 = Electrostatic discharge"]
-[10.326284408569336, 2.2590720653533936, "[FF] Purpose of the RHESSI = Imaging spectroscopy of hard X-ray (HXR) and gamma-ray continua emitted by energetic electrons, and gamma-ray lines produced by energetic ions"]
-[6.972188949584961, 7.117295742034912, "[TT] Number of Beams for HR Mode of the COSI = 19"]
-[3.0022566318511963, 2.3604822158813477, "[FF] Mission Type of the Sentinel-5 = European operational atmospheric chemistry mission in polar orbit"]
-[7.539690017700195, 2.3766300678253174, "[FF] Function of the MDA Maritime Insights platform = Provides near real-time monitoring of fishing activity"]
-[14.17701244354248, 3.153637409210205, "[TT] Mass of the AltiKa = 150 kg"]
-[7.015928268432617, 1.6209899187088013, "[FF] URL of the Kepler = http://www.nasa.gov/mission_pages/kepler/news/41-new-transiting-planets.html"]
-[9.983291625976562, 7.769726753234863, "[TT] Celestial Sphere Coverage of the Telescope = 100% of sphere has at least 51 contiguous days visibility"]
-[4.416921615600586, 7.831988334655762, "[TT] Frequency of the Downlink frequency = 26 GHz"]
-[8.149386405944824, 6.761692047119141, "[TT] Usage of the Portable ultrasound device = Medical imaging"]
-[14.668397903442383, 6.643742084503174, "[TT] Battery Capacity of the NSat = 5.2 Ah"]
-[11.589221954345703, 3.324530601501465, "[TT] Operation Hours of the Ion Engine = 1346 hours"]
-[4.4467973709106445, 6.748077392578125, "[TT] RF Communications of the Meteosat = L-band"]
-[6.602439880371094, 4.099836826324463, "[FF] Unknown of the Ground Segment = Unknown"]
-[4.891982078552246, 0.5947542786598206, "[FF] Launch Date of the MITA = 15 July 2000"]
-[13.441377639770508, 2.879152536392212, "[TT] Satellite Mass of the Terra Bella = ~120 kg"]
-[6.82697868347168, 3.3386027812957764, "[FF] Purpose of the BioFabrication Facility (BFF) = Printing of human organs and tissues in microgravity"]
-[5.950133323669434, 0.8314365148544312, "[FF] Image Capture Date of the SOHO = Jan. 14, 2014"]
-[9.291741371154785, 4.881887435913086, "[TT] Autonomous Rotation Angle of the Spacecraft = Within 35\u00b0 of the sun"]
-[10.88805866241455, 7.4868245124816895, "[TT] Swath Width of the MUX = 120 km"]
-[9.31590747833252, 10.742209434509277, "[TT] Polarization of the ICI-9 = V"]
-[10.30649185180664, 8.069784164428711, "[TT] Entrance Aperture Diameter of the COR2 = 30.5 mm"]
-[5.546469688415527, 3.3884356021881104, "[FF] Manufacturer of the Robotic Arm = MAXAR"]
-[11.124543190002441, 1.0009956359863281, "[TT] Mission Type of the LISA = Non-EO"]
-[7.855671405792236, 7.484537124633789, "[FF] Energy Spectrum of the SWAP = Unknown"]
-[8.57081127166748, 8.580151557922363, "[TT] Instantaneous spectral coverage of the Spectrometer = 1.56 km/s"]
-[7.597283840179443, 3.4614789485931396, "[FF] Operation of the Net = Successfully snares space debris"]
-[7.942583084106445, 6.2377190589904785, "[TT] Instrument Type of the MSU-SK = Imaging multi-spectral radiometers (vis/IR)"]
-[7.5301833152771, 2.4833593368530273, "[TT] Data Collection of the Radar altimeters = Since 1991"]
-[9.618412017822266, 8.108908653259277, "[TT] F Number of the Optics = f/12"]
-[11.803057670593262, 3.180748701095581, "[TT] Thrusters of the RADARSAT-2 = Six 1 N thrusters"]
-[6.141386032104492, 8.055750846862793, "[TT] Number of Channels of the Dual-channel Receiver Unit (DRU) = 2"]
-[10.052165031433105, 1.4318643808364868, "[TT] Peak Brightness Time of the GRB 191016A = Between 1,000 and 2,600 seconds"]
-[9.290590286254883, 3.314127206802368, "[FF] Calibration Maneuver of the Voyager = Spin around to differentiate between the spacecraft's own magnetic field and the magnetic fields of the space it\u2019s traveling through"]
-[10.014989852905273, 2.9099462032318115, "[FF] Launch Status of the TROPICS cubesats = Failed"]
-[8.780509948730469, 3.5425920486450195, "[FF] Frequency of the Solar Measurements = Every orbit"]
-[5.403111934661865, 7.6878342628479, "[FF] Transmit Operation of the T/R Module = Can alternate between H and V on alternate pulses"]
-[8.7490816116333, 7.287906169891357, "[TT] L1 Detectors Thickness of the HIT = 1000 \u00b5m"]
-[10.149471282958984, 5.867871284484863, "[TT] CCD Detector Temperature of the MEGS = -100\u00ba C"]
-[9.82945728302002, -0.5718395709991455, "[TT] Orbit Altitude of the LEOSAR = > 2000 km"]
-[6.881505489349365, 4.602509498596191, "[FF] Application of the Supercapacitor = Launchers and satellites"]
-[12.718398094177246, 3.8934526443481445, "[FF] Evidence of the Ion Dispersion = Multiple overlapping dispersions have also been presented as evidence for multiple discontinuous reconnection sites along the magnetopause"]
-[9.676482200622559, 4.5655107498168945, "[TT] Control Method of the ADCS = Magnetic torque control"]
-[5.553057670593262, 2.704909324645996, "[TT] Partnership of the Unicorn-1 = European Space Agency (ESA)"]
-[10.769563674926758, 1.2611993551254272, "[TT] Size of the Thuban = 4.3 times bigger than the Sun"]
-[4.790494918823242, 0.5454071164131165, "[TT] Launch Date of the PhoneSat-1 and -2 = 21 April 2013"]
-[10.238529205322266, -1.293515682220459, "[TT] Inclination of the PhoneSat-2.5 1U CubeSat = 51.6\u00b0"]
-[5.619106769561768, 0.9929177761077881, "[TT] Proto-flight Tests Completion Date of the Spacecraft = Q2 of 2012"]
-[9.423901557922363, 4.742525100708008, "[TT] Function of the OASYS = Command actuators to attain a desired attitude state"]
-[13.619481086730957, 6.872897148132324, "[TT] Power Source of the RapidScat = Columbus module power circuit"]
-[13.792240142822266, 6.874083042144775, "[TT] Voltage Limit of the ISS = 160 V"]
-[8.355504035949707, 7.537269592285156, "[TT] Detector Types of the Instrument = NIR and narrow-band VIS (630 nm)"]
-[5.499926567077637, -0.5926768779754639, "[TT] Operating Status of the Yutu 2 = Operating"]
-[10.577298164367676, 6.746764659881592, "[TT] Mirror Thickness of the Mirror = 0.21 mm"]
-[5.639280319213867, 2.3763785362243652, "[FF] Educational Mission of the ABEX = Develop in-house engineering solutions for ABEX lead by student design teams"]
-[8.54693603515625, 8.483755111694336, "[TT] Resolving Power of the Spectrometer = R = 100"]
-[13.404426574707031, 6.7099432945251465, "[TT] Power Generation of the SPOT satellite constellation = 1,000 W"]
-[11.831006050109863, 6.70319128036499, "[TT] Energy Range for Charged Particles of the FREND = 0.5\u201310 MeV"]
-[9.280248641967773, 3.1364917755126953, "[FF] Measurement of the WISPR = Solar Wind Structures"]
-[8.270590782165527, 7.509564399719238, "[FF] CCD Detector Assembly of the EUVI = Backside-illuminated, backside-thinned and pacified array of size 2k x 2k with an EUV quantum efficiency >70%"]
-[6.709348678588867, 5.601574897766113, "[FF] Contents of the RF Module = Input and reference switching networks, the mixer-IF preamplifiers, and the Gunn local oscillators"]
-[7.750768184661865, 3.5357179641723633, "[FF] Additional Payloads of the Meteor M2-2 = Search-and-rescue radio transponder, data relay payload"]
-[9.62619400024414, 7.155604839324951, "[TT] Main Mode Ground Resolution of the MRSE = 25 m"]
-[9.495922088623047, 6.220626354217529, "[TT] Incidence Angle of the MTVZA-GY = 65\u00ba"]
-[9.758161544799805, -0.5509439706802368, "[TT] Orbit Altitude of the RemoveDebris = 405 km"]
-[8.328011512756348, 3.746359348297119, "[FF] Purpose of the AMO = Monitor Atomic Oxygen"]
-[8.519481658935547, 6.728749752044678, "[TT] Required Spacecraft Stability of the Pushbroom Scanner = High"]
-[10.726855278015137, 3.275883436203003, "[FF] Purpose of the SUBSA-BRAINS = Examine differences in capillary flow, interface reactions, and bubble formation during the solidification of brazing alloys in microgravity"]
-[8.095634460449219, -1.2564376592636108, "[TT] Laser Pulse Footprint of the ICESat-2 = 17 m in diameter"]
-[7.2033233642578125, 7.035747051239014, "[TT] Operating Temperature of the Laser = 10 \u2013 40\u00baC"]
-[13.341984748840332, 7.345637321472168, "[TT] Power of the EXIS = 40 W"]
-[14.317669868469238, 3.158336639404297, "[TT] Mass of the Tsubame = 48.6 kg"]
-[13.387042999267578, 7.308738708496094, "[TT] Power of the DPU = 10 W"]
-[3.63081955909729, 5.608521938323975, "[TT] PRF of the Radar = 2.9 kHz"]
-[8.137537002563477, 2.0936474800109863, "[FF] Measurement Parameters of the SSM/I = Sea surface winds, rain rates, cloud water, precipitation, soil moisture, ice edge, and ice age"]
-[5.927273273468018, 1.8769086599349976, "[FF] Test Schedule of the Orion Spacecraft = Accelerated"]
-[5.22780704498291, 3.220252752304077, "[TT] Manufacturer of the OSIRIS-REx = Lockheed Martin"]
-[8.185359001159668, 8.626827239990234, "[TT] Spectral Range of the Spectrometer = 450 -1000 nm"]
-[4.236595630645752, 2.665771007537842, "[TT] Launch Site of the Galileo FOC-3 and FOC-4 satellites = Europe's Spaceport (Kourou, ELS) in French Guiana"]
-[5.388083457946777, 1.298134684562683, "[FF] Conference Date of the Dove = Aug. 5-10, 2017"]
-[11.235509872436523, 0.9961382150650024, "[FF] Mission Design Feasibility of the LISA = Confirmed"]
-[5.167877674102783, 2.305335760116577, "[TT] Mission Type of the THEOS-2 = EO"]
-[5.279479026794434, 3.907717227935791, "[TT] Demonstration Satellites of the Falcon 9 rocket = Two"]
-[4.977222442626953, 3.40364146232605, "[TT] Manufacturer of the OHU = Micos"]
-[10.0205717086792, 2.928466320037842, "[FF] Presentation Date of the NANOSATC-BR Cubesat Program = Oct. 10-13, 2012"]
-[8.177726745605469, -0.28305092453956604, "[FF] Maximum Meltwater Runoff of the Greenland = 527 billion tons in 2012"]
-[13.82278060913086, 2.684072494506836, "[TT] Launch Mass of the Spacecraft = 696 kg"]
-[5.866583824157715, -0.7774739265441895, "[TT] On-Orbit Useful Life of the SXI = 3 years with a goal of 5 years"]
-[9.466663360595703, -0.5396843552589417, "[TT] Argument of periapsis of the Satellite = 270\u00ba"]
-[5.725390434265137, 5.084133625030518, "[FF] Data Acquisition of the Telemetry, Tracking and Command (TT&C) Ground Stations = Raw data from the CBERS data collection system in the S-band"]
-[10.7657470703125, 1.0280735492706299, "[TT] Mass of the GJ 367 b = 55 percent that of Earth's"]
-[14.001297950744629, 4.033133506774902, "[TT] Mass of the Field Measurement Device = < 0.5 kg"]
-[4.795875549316406, 5.349820613861084, "[TT] Antennas of the GPS receiver = 4 antennas"]
-[7.89351224899292, 6.265124320983887, "[FF] Instrument Type of the POLDER-2 = Imaging multi-spectral radiometers (vis/IR)"]
-[13.962859153747559, 3.5162222385406494, "[TT] Mass of the MEMS device = 24 gram"]
-[8.324110984802246, 2.491699695587158, "[TT] Aerosol Layer Height of the CATS = 5 km"]
-[13.236283302307129, 7.259549617767334, "[TT] Power Consumption of the WPIx = > 650 W peak"]
-[6.733419895172119, 7.553696632385254, "[TT] Beam width of the X-band = 0.15 rad"]
-[13.736211776733398, 7.117475986480713, "[TT] Current range (A) of the PS-2 = 0.001~0.1"]
-[3.521242380142212, 6.305618762969971, "[TT] Diameter of the Net = 5 m"]
-[4.897530555725098, 2.72739577293396, "[TT] Promoter of the SOHLA-1 = NEDO"]
-[6.892723560333252, 4.0730671882629395, "[FF] Type of the Astrolabe Rupes = Lobate scarp"]
-[8.706829071044922, 8.60870361328125, "[TT] Pixels per FWHM of the Spectrometer = 1220"]
-[4.793083667755127, -1.883009672164917, "[FF] Components of the Chang'e-5 = Orbiter, lander, ascender and reentry module"]
-[5.567744731903076, 5.919351577758789, "[TT] Processor of the Command and Data Handling Subsystem = 32-bit"]
-[4.617481708526611, 3.062854528427124, "[TT] Manufacturer of the Iridium NEXT = Thales Alenia Space"]
-[11.974135398864746, 3.1861438751220703, "[FF] Propellant of the OSAM-1 = Bi-propellant and mono-propellant"]
-[5.273690700531006, 0.8124696016311646, "[TT] Year of Launch of the EO-1 = 2000"]
-[7.617863655090332, 3.42783260345459, "[TT] Detection of the Debris Cloud = Mid-2018"]
-[4.49321985244751, 2.819394826889038, "[TT] Installation Location of the SCRI = Sydney, Australia"]
-[7.7507123947143555, -0.8520915508270264, "[FF] Date of the ICESat-2 Applications Workshops = May-June 2014"]
-[4.823985576629639, 7.921423435211182, "[TT] Excitation Frequency of the MCAc = 0.005 Hz"]
-[8.34844970703125, 2.7181220054626465, "[FF] Measurement Domain of the MITA = Atmosphere, Gravity and Magnetic Fields"]
-[7.881441116333008, 5.102018356323242, "[FF] Calibration Data Acquisition of the Mini-RF = During spacecraft integration and test"]
-[4.959704399108887, -0.3184677064418793, "[TT] Launch Time of the GRIFEX = 14:22:00 UTC"]
-[4.775763511657715, 2.4287827014923096, "[FF] Capacity Reservation of the Eutelsat Quantum = Majority"]
-[5.458963394165039, 6.1183295249938965, "[TT] Microcontroller RAM of the On-board Computer = 1 MB"]
-[11.995057106018066, -0.11527366191148758, "[TT] Angular Field of View of the TESS = 6 degrees"]
-[7.907257556915283, 1.729109764099121, "[FF] Mission Name of the GOCE = Gravity field and steady-state Ocean Circulation Explorer"]
-[8.215678215026855, 2.3007726669311523, "[FF] Affected by of the DETER = High frequency of clouds over the Amazon region"]
-[5.43967342376709, 6.083139896392822, "[TT] RAM of the Model calculator = 512 kB"]
-[8.877909660339355, 9.571599006652832, "[FF] Band 5 Wave Numbers of the TANSO-FTS-2 = 700 - 1183"]
-[14.254505157470703, 3.08379864692688, "[TT] Mass of the TurkSat-3USat = ~ 4 kg"]
-[6.338059902191162, 1.872493863105774, "[FF] URL of the Alphabus = http://www.esa.int/esaTE/SEMSIGKTYRF_index_0.html"]
-[5.30609655380249, 2.5788981914520264, "[TT] Mission Type of the GEOSAT = EO"]
-[3.8610177040100098, 1.2442635297775269, "[TT] Version of the PSLV-C19 = PSLV-XL"]
-[9.773079872131348, -0.5780106782913208, "[TT] Orbital Altitude of the NAOMI = 695 km"]
-[12.438237190246582, 0.6388815641403198, "[TT] Model of the PLATO detectors = CCD270"]
-[9.832503318786621, 7.72175931930542, "[TT] Turnaround Time of the Telescope = 0.1 s per scan"]
-[7.566370010375977, 3.263425588607788, "[TT] Stray Light of the GHGSat-D = Up to 5%"]
-[8.980661392211914, 7.346194267272949, "[TT] Area of the High LET Detector = 9.6 cm^2"]
-[9.30594539642334, 6.796147346496582, "[TT] Goal Image Resolution of the Satellite Constellation = 1 meter"]
-[13.275533676147461, 2.9150631427764893, "[TT] Mass of the MicroSat-2b = 400 kg"]
-[3.8549134731292725, -1.1061104536056519, "[FF] Orbit of the Genesis = Halo orbit around the Lagrangian point L1"]
-[10.758378028869629, -0.21372470259666443, "[FF] Orbit Concept of the TanDEM-X = Double helix formation"]
-[7.109772682189941, 7.490598678588867, "[TT] Logarithm Resolution Adjustment of the RFA Computer = 8 bits"]
-[10.26229476928711, 3.96687912940979, "[TT] Deployment Position Reporting of the AstroTubeTM Boom = Yes"]
-[7.740118980407715, 0.5129756331443787, "[TT] Power Generation of the Lunar IceCube = 120 W"]
-[8.373106956481934, 3.1782431602478027, "[TT] Accuracy of the Ozone Measurement Instrument = 15 DU or better"]
-[10.896787643432617, 7.52107572555542, "[TT] Swath Width of the OLS = 3000 km"]
-[4.824497699737549, 0.5209142565727234, "[TT] Proposed Launch Year of the e.Deorbit = 2023"]
-[9.600370407104492, 7.04197883605957, "[TT] Resolution of the T2 = 5 km x 5 km"]
-[9.23629093170166, -0.5739073157310486, "[TT] Orbiter Orbit of the Tianwen-1 = Polar elliptical orbit (265 km x 12,000 km)"]
-[11.3194580078125, 0.9529883861541748, "[TT] Nominal Mission Lifetime of the LISA Pathfinder = 180 days"]
-[7.474457740783691, 2.2982730865478516, "[FF] Monitoring and Modeling of the Hunga Tonga Hunga Ha'apai = High Spatial Resolution Satellite Observations"]
-[4.881019592285156, 0.4244156777858734, "[TT] Launch Date of the CAPSTONE = June 28, 2022"]
-[8.674396514892578, 2.3791863918304443, "[FF] Purpose of the EMIT = Map the world\u2019s mineral dust source regions and provide information on the color and composition of dust sources"]
-[8.250265121459961, 2.967104196548462, "[FF] Observed Phenomena of the ASIM = Wide variety of phenomena in Earth's upper atmosphere"]
-[8.070850372314453, -0.4095878601074219, "[TT] Annual Minimum Extent Date of the Antarctic Sea Ice = February"]
-[11.856912612915039, 3.1027657985687256, "[FF] Attitude Control of the Attitude Control Subsystem (ACS) = Hydrazine reaction control thrusters"]
-[4.544543266296387, 0.5736274123191833, "[FF] Launch Date of the M3MSat = Unknown"]
-[5.305633068084717, 4.004434585571289, "[TT] Number for Coverage Match of the LEO Satellites = Around 300"]
-[13.655228614807129, 7.018335819244385, "[TT] Power Generation of the EPS = 7.2 W"]
-[7.934365749359131, 7.953402996063232, "[FF] Development Challenges of the Infrared Sounder (IRS) = Utilizing a corner cube mechanism design with successful IASI flight heritage for the Infrared Sounder (IRS) on MTG; recurrent mechanical design not correlated to recurrent development"]
-[6.358425617218018, -0.10374072939157486, "[TT] Frequency of the Request for Information = Every 12 to 18 months"]
-[13.246515274047852, 5.267155647277832, "[TT] Solar Array Span of the S/C = 13 m"]
-[8.099443435668945, 2.2979650497436523, "[FF] Indicators of the Atmospheric Measurements = Surface temperature, water vapor, sea ice"]
-[3.644970417022705, 4.674937725067139, "[FF] SAR Processor Upgrade of the RADARSAT-2 = New and improved image products"]
-[8.054109573364258, 8.095056533813477, "[TT] Bandwidth of the Band Cameras = 90 nm"]
-[5.503577709197998, 6.7209601402282715, "[TT] Maximum Data Volume of the ALOS-3 = 1400 Gbit per day"]
-[9.651493072509766, 7.241017818450928, "[TT] Vertical Sampling of the Instrument = \u22641 km"]
-[6.212213516235352, 3.7944464683532715, "[FF] Operation of the DMC Constellation = Share unused capacity with other Members"]
-[10.08725643157959, 1.4086624383926392, "[TT] Quasar Diminishment of the The Teacup = Only fading by a factor of 25 or less over the past 100,000 years"]
-[5.983859539031982, 4.933435440063477, "[FF] Self-management of the Network = Required"]
-[5.626988887786865, 5.011920928955078, "[TT] Function of the MEXIC = Provide secondary voltage to the various instruments"]
-[8.993566513061523, 5.074098587036133, "[TT] Quantity of the Gyroscopes = Three"]
-[7.306905269622803, 8.765470504760742, "[TT] Development Status of the Master Oscillator Power Amplifier (MOPA) = In Progress"]
-[7.820555686950684, 2.9979002475738525, "[FF] Mission of the TanSat = Carbon Dioxide (CO2) detection and monitoring"]
-[8.740631103515625, 2.040628671646118, "[TT] Margin on Wind Speed of the E2E model = Minimum of 70%"]
-[9.37150764465332, 3.4489192962646484, "[FF] Product of the SEP = Distribution of High Energy Particle Products, Intensity of Magnetic Field, Effects of Spatial Environment"]
-[3.3745641708374023, 1.4654183387756348, "[TT] Launch Date of the Sentinel-1A = Expected in 2014"]
-[7.551880836486816, 6.99525260925293, "[TT] Typical high cadence of the HRI dual EUV 174 \u00c5 and 335 \u00c5 alternatively = 2 s"]
-[3.434302568435669, 6.298577308654785, "[TT] Antenna Booms Length of the DSX spacecraft = 80-meter and 16-meter"]
-[8.897404670715332, 0.9576511979103088, "[FF] Team Effort of the Parker Solar Probe = Yes"]
-[7.752194404602051, 5.767961025238037, "[FF] Components of the Angular Sensor = 2D-PSD (2 dimensional Position Sensitive Detector) and low power laser diode"]
-[6.638200283050537, 4.946281909942627, "[FF] Integration Status of the Electronics Module = Ongoing"]
-[5.914034366607666, 1.1330777406692505, "[FF] Launch Date of the Space Weather Mission = Unknown"]
-[7.9131550788879395, -0.534188985824585, "[TT] Trend of the Freeze-up = Nearly one month later since the start of the satellite record in 1979"]
-[5.511634349822998, 3.7443575859069824, "[FF] Backlog Value of the Terran R = More than $1.2 billion"]
-[10.146732330322266, 7.551085948944092, "[TT] Swath Width of the SIR-C = 15 to 65 km for calibrated images"]
-[5.1167521476745605, 2.8752102851867676, "[TT] Institute of the CIP = NCU (National Central University), Taiwan"]
-[9.992286682128906, 5.7084150314331055, "[TT] Temperature Stability of the ASTERIA = mK (milliKelvin)-level"]
-[6.871089458465576, 3.437443971633911, "[FF] Purpose of the Kidney Cells-02 study = Improve treatments for kidney stones and osteoporosis"]
-[8.115599632263184, 4.558180809020996, "[TT] Full Calibration Mode Frequency of the TRUTHS = Bi-monthly"]
-[10.1779146194458, 3.219146728515625, "[FF] Type of the Iris V2 CubeSat Deep-Space Transponder = Deep-Space"]
-[3.0910513401031494, -0.05472448468208313, "[TT] Orbital Slot of the GSAT-0211 = A06"]
-[13.39007568359375, 7.364749431610107, "[TT] Power of the MAG = 0.2 W"]
-[11.201672554016113, 3.3758301734924316, "[FF] Development Date of the Microelectromechanical System = May 6, 2004"]
-[9.786892890930176, 8.549132347106934, "[TT] IFOV for MWIR, TIR-1, & TIR-2 of the Telescope = 112 \u00b5rad (4 km)"]
-[9.681591033935547, -0.621540904045105, "[TT] Orbit of the PSLV-C40 = Polar orbit of 365 km height"]
-[6.915535926818848, -0.6745838522911072, "[FF] Inner Quadruple Orbit Period of the TYC 7037-89-1 = Every four years or so"]
-[7.572713851928711, 3.483152151107788, "[FF] Conference Presentation of the Net Capture Mechanism = 7th European Conference on Space Debris, ESA/ESOC, Darmstadt/Germany, 18 - 21 April 2017"]
-[6.273397922515869, 5.555456638336182, "[FF] Redundancy of the MMU = Two MSM (Memory System Module) in cold redundancy"]
-[4.486863136291504, 7.1187615394592285, "[FF] Research Activities of the Q/V-bands = Needed"]
-[6.604971885681152, 3.786785364151001, "[FF] Gas Purification of the LAXPCs = Onboard purifier"]
-[5.2064642906188965, 7.15036153793335, "[TT] Telemetry Bit Rates of the S-band = Few Mbit/s"]
-[8.15099048614502, 4.638750076293945, "[FF] Calibration Frequency of the OMPS = Weekly for working diffuser, Twice annually for reference diffuser"]
-[6.845688819885254, 3.792583465576172, "[FF] Experiment of the Tokyo Institute of Technology = Evaluation of the robot arm's vibrations"]
-[5.7244977951049805, 2.986241340637207, "[TT] Payload Development Manager of the CloudSat = NASA/JPL"]
-[4.553825378417969, 2.9480626583099365, "[TT] Location of the GUSN = USNO, Washington USA"]
-[4.862010478973389, 0.4408354163169861, "[TT] Launch Date of the OFEQ-3 = April 15, 1995"]
-[9.6836576461792, -0.4904422163963318, "[TT] Altitude of the ADEOS = 797 km"]
-[4.667454719543457, 7.6810173988342285, "[TT] Data Rate of the Astrodev Lithium 2 Radio = 9.6 kbit/s"]
-[10.823675155639648, 1.0237942934036255, "[FF] Composition of the White Dwarf = Rich in helium"]
-[4.622666835784912, 8.02023983001709, "[TT] Chirp Bandwidth of the SAR = 225 MHz 75 MHz 37.5 MHz 18.75 MHz"]
-[5.5426435470581055, 2.764571189880371, "[TT] Manager of the WFIRST = NASA's Goddard Space Flight Center"]
-[5.207935333251953, 8.287784576416016, "[TT] Performance Requirement of the LISA LTP = \u2264 10-15 ms-2 Hz-1/2 in the bandwidth 10-3 to 10-1 Hz"]
-[8.942865371704102, 4.381866455078125, "[TT] Purpose of the CESS (Coarse Earth Sun Sensors) = Coarse Earth and Sun direction determination"]
-[7.5895256996154785, 6.859029769897461, "[TT] Exposure Time of the CCD = 50 ms"]
-[9.38928508758545, 6.771189212799072, "[FF] Cross-Strapping of the KazEOSat-2 = Provides Redundancy"]
-[4.503722667694092, 1.675537109375, "[TT] First FM Beacon Signal Date of the LituanicaSat-1 = February 28, 2014"]
-[5.998509407043457, 1.8937338590621948, "[FF] Workshop Date of the GPM Program = June 16-18, 2009"]
-[9.115753173828125, -1.2776086330413818, "[TT] Orbit of the Satellites = Geostationary"]
-[4.830498218536377, 0.5120891332626343, "[TT] Launch Date of the OFEQ-2 = April 1990"]
-[3.5024962425231934, 6.658655166625977, "[TT] Polarization Modes of the RISAT-1 SAR payload = RHCP and LHCP"]
-[4.98198938369751, 5.939873218536377, "[TT] Link Reversion of the LLITED satellites = Passive receive mode"]
-[3.3700380325317383, 4.836890697479248, "[FF] Application of the PPT = SAR application such as interferometry, ATI/GMTI, the fusion of SAR data with AIS data"]
-[5.219513416290283, 5.835092544555664, "[TT] Number of Networks of the GSM = 200"]
-[8.526726722717285, 6.355049133300781, "[TT] Sensor Type of the IDM = Planar sensor"]
-[4.615875244140625, 6.320275783538818, "[TT] Beacon Transmission Rate of the ELFIN-B = 9600 baud"]
-[7.733784198760986, 6.725517749786377, "[TT] Sensitivity of the eROSITA = 30 times more than ROSAT"]
-[8.577276229858398, 2.765983819961548, "[TT] Range of measurements of the Atmosphere = Up to 45 km"]
-[5.330691814422607, 0.502359926700592, "[TT] Launch Date of the Envisat = March 1, 2002"]
-[6.455273628234863, 4.674269676208496, "[FF] Function of the POCC = AMS operations take place, including commanding, storage and analysis of housekeeping data and partial science data analysis for rapid quality control and feedback"]
-[6.113633632659912, 0.8054754137992859, "[FF] Image Capture Date of the CaSSIS = 18 November 2018"]
-[6.693837642669678, -0.6698663234710693, "[TT] Flight Time to Kanopus-V-IK separation orbit of the Fregat upper stage = 1 minute 26 seconds"]
-[5.026015758514404, 1.0441863536834717, "[FF] Presentation Date of the ADM-Aeolus = April 24-28, 2006"]
-[9.574851989746094, 5.064320087432861, "[TT] Relative Position of the AC4-B = Catch up with and pass AC4-A"]
-[13.4426908493042, 2.8079662322998047, "[TT] Wet Mass of the Spacecraft = 2712.5 kg"]
-[5.207181453704834, 0.7413681745529175, "[TT] Delivery Date of the LAS = 2014"]
-[6.399600028991699, 1.248059630393982, "[FF] Workshop Date of the COSMIC-II = October 21-22, 2010"]
-[8.802350044250488, 1.9450807571411133, "[TT] Communication Speed of the WINDS = 155 Mbit/s for residential use and 1.2 Gbit/s for office use"]
-[8.005276679992676, -0.4471907615661621, "[FF] Satellite Record Start Year of the Arctic Sea Ice = 1979"]
-[4.707284450531006, 0.5671093463897705, "[TT] Launch Date of the GOES-18 = March 1, 2022"]
-[10.413776397705078, 5.776733875274658, "[TT] Temperature Range of the SLC NAND-Flash = - 40\u00baC to + 85\u00baC"]
-[5.83117151260376, 0.7672402858734131, "[FF] Publication Date of the ISEE-1 = July 1978"]
-[3.8617517948150635, 0.8971408605575562, "[FF] Launch Date of the PSLV-C31/IRNSS-1E = January 20, 2016"]
-[8.130977630615234, 0.6995885372161865, "[TT] Global Variability of Water Storage of the Reservoirs = 57%"]
-[12.982572555541992, 6.769869327545166, "[FF] Event Probability of the Safe Mode = Sufficiently low and only possible under very special initial conditions"]
-[8.141376495361328, 3.5131335258483887, "[TT] Number of Atmosphere Passes of the OCO-3 = 2"]
-[5.848350524902344, 3.3830132484436035, "[TT] Future Test Plan of the VECTOR system = Toss a heavier rocket even higher"]
-[6.364882469177246, 4.175973415374756, "[FF] Intended Use of the Bartolomeo = Technology testing and validation"]
-[6.110240459442139, 5.421346187591553, "[FF] Configuration of the CFTP = TMR (Triple-Modular Redundant) computer"]
-[9.90080738067627, 7.883405685424805, "[TT] FMC Mode Rotation Speed of the Telescope = 0.6\u00ba/s"]
-[6.242813587188721, 4.358114719390869, "[FF] Activities of the PDGS = Coordinated planning of the mission subsystems, automated and recurrent planning of the satellite observations, systematic acquisition and safeguarding of all spacecraft acquired data, recurrent calibration of the instrument, automated product circulation across PDGS distributed archives, long-term archiving of all mission data"]
-[8.278454780578613, 4.732811450958252, "[FF] Calibrators of the Instrument = Solar diffuser, solar diffuser stability monitor, blackbody"]
-[6.336452960968018, -1.3530402183532715, "[TT] Launch Date of the GRACE-FO = May 22"]
-[6.6028828620910645, 3.9718968868255615, "[FF] Development Status of the TRUTHS = Preliminary design phase"]
-[9.565474510192871, 7.315350532531738, "[TT] Ground Resolution of the Mars Express = Approximately 20 m/pixel"]
-[3.5926804542541504, 4.752758502960205, "[FF] Acquisition Modes of the ASNARO spacecraft = Snapshot mode (10 km x 10 km), StripMap mode, Skew mode"]
-[5.2939887046813965, 5.6810221672058105, "[FF] Interface of the OBC = 1553 RIU interface with the S-band transceiver"]
-[3.797349691390991, 4.500180721282959, "[FF] Image Quality of the RADARSAT-2 = Maintained or improved"]
-[5.28968620300293, 2.7288074493408203, "[FF] Navigation Payload Builder of the MTSAT-1R = Alcatel Space of France"]
-[5.985182285308838, 4.984629154205322, "[FF] ADCS Suite of the CanX-4 or CanX-5 = Tray Housing"]
-[11.857625961303711, 5.425513744354248, "[TT] Connection of the SOLID Panels = Two panels are connected to each of the two busses"]
-[9.284335136413574, 1.2552286386489868, "[TT] Image Transmission Time of the New Horizons = More than four hours"]
-[13.827169418334961, 3.0992329120635986, "[FF] Mass of the MicroMAS-2a = Not provided"]
-[12.445430755615234, 0.5693823099136353, "[FF] Delivery Date of the PLATO = 11 April 2019"]
-[4.71536111831665, 3.162184715270996, "[TT] Manufacturer of the Lightspeed Satellites = Thales Alenia Space"]
-[13.633166313171387, 5.517170429229736, "[TT] Solar Panels of the EPS = 5 GaAs panels"]
-[8.560288429260254, 4.945756435394287, "[FF] Sensitivity of the ASTRO-H = 2 orders of magnitude better than previous instruments"]
-[8.793802261352539, 8.42060375213623, "[TT] Ground Swath of the Miniature High-Resolution Imaging Spectrometer = 15 km"]
-[8.159676551818848, -1.0343186855316162, "[TT] Height Measurements of the ICESat-2 = Thousands"]
-[3.812744617462158, 4.676463603973389, "[TT] Sensor Module Frequency of the RADARSAT-2 = 5.4GHz"]
-[5.075949192047119, -0.3649443984031677, "[TT] Launch Date of the CBERS-3 = December 09, 2013"]
-[6.960200309753418, 1.0858818292617798, "[TT] Arrival Date at Mars of the ExoMars 2020 = March 2021"]
-[4.147141456604004, 1.3780815601348877, "[TT] Operational Service Start Date of the Meteosat-8 = Jan. 29, 2004"]
-[11.99950122833252, 4.5008625984191895, "[TT] Spacecraft Volume (Before Inflatable and Sail Deployment) of the Spacecraft = 34 cm x 10 cm x 10 cm"]
-[8.894285202026367, 3.569037437438965, "[FF] Measurement Comparison of the Science Question Methodology = Plasma density profile and line of sight scintillations at different latitudes in the target longitude region may be compared with the latitude profile of the plasma density, drift and structures observed earlier in time by the satellite"]
-[6.6615753173828125, 0.7367255687713623, "[TT] Lunar Eclipse Date of the Spacecraft = June 4"]
-[10.013338088989258, -1.473489761352539, "[TT] Orbital Inclination of the Long March 5B = 41.5 degrees"]
-[4.221917629241943, 2.567345380783081, "[TT] Launch Site of the GRACE-FO Satellites = Vandenberg Air Force Base"]
-[13.659687042236328, 6.986783981323242, "[TT] Power of the EPS = > 330 W"]
-[9.759628295898438, -0.5891880393028259, "[TT] Orbital Altitude of the LDEF = 477 km"]
-[7.138106822967529, 6.7204179763793945, "[FF] Beam Collimation of the OHU = Maintains approximately the same diameter"]
-[3.852567672729492, 3.4293179512023926, "[TT] Orbit Placement Date of the Galileo 2nd Generation Satellites = End of 2024"]
-[8.079010009765625, 8.803747177124023, "[TT] Spectral Range of the SOLSE-2 = 530 - 850 nm"]
-[8.82813549041748, 3.212428569793701, "[FF] Objectives of the PIXIE = Study of the morphology and spectra of energetic electron precipitation and its effect on the atmosphere. Derivation of the total electron energy deposition rate, the energy distribution of the precipitating electrons, and the altitude profile of ionization and electrical conductivity"]
-[3.480611801147461, 5.388455867767334, "[TT] PRF of the SAR = About 9 kHz"]
-[6.490936756134033, 1.0597001314163208, "[FF] Image of the Day Date of the NASA Earth Observatory = 17 May 2022"]
-[4.7505784034729, -1.840667963027954, "[TT] Launch Date of the Chang'e-5 = Nov. 23"]
-[4.4891676902771, -0.2567489743232727, "[TT] Planned Docking Date of the Nauka = 23 July 2021"]
-[5.699578762054443, 1.5485413074493408, "[FF] Operational of the WorldView 4 = Yes"]
-[16.545894622802734, 3.6402339935302734, "[TT] Number of Satellites of the OneWeb = 322"]
-[5.731834888458252, 7.150787830352783, "[TT] Data Rate of the TT&C = 4 Kbit/s"]
-[5.610727310180664, 6.415877342224121, "[FF] Data Transmission of the EDRS = Few TB (terabyte) of data every day"]
-[7.859189033508301, 1.9910411834716797, "[FF] Dead Zone Area of the Gulf of Mexico = Variable, average size about the same as the state of Connecticut"]
-[13.223785400390625, 7.1980485916137695, "[TT] Power Consumption of the Module = < 3.5 W"]
-[6.501919269561768, -0.19510896503925323, "[TT] Monitoring Frequency of the RADARSAT-2 = Every 24 days"]
-[5.316158294677734, 1.3361114263534546, "[FF] Impact Site of the MRO = Confirmed"]
-[8.84900188446045, 2.982259511947632, "[FF] Unknown of the Auroral Particle Instrument = Unknown"]
-[7.952454090118408, 9.17347240447998, "[TT] Wavelength of the OH (surface or structural) = 2.2-2.3 \u00b5m"]
-[9.266175270080566, 3.200005531311035, "[FF] Coronagraph Instrument of the CSC = Observation of Sun\u2019s corona during artificial eclipse"]
-[3.232703447341919, 1.6180331707000732, "[TT] Average Communication Time of the Sentinels Satellites = 10 minutes per orbit"]
-[5.1660590171813965, 0.636562168598175, "[TT] Mission End Date of the DSCOVR = Unknown"]
-[6.988424301147461, 4.983311653137207, "[FF] Components of the HH canister = Canister extension ring, HMDA"]
-[7.311019420623779, 6.264192581176758, "[TT] Time Synchronization Accuracy of the LCT = Better than 0.5 seconds"]
-[10.013314247131348, 5.637340545654297, "[FF] Function of the TechEdSat-10 = High temperature, accurate deorbit reentry"]
-[8.647623062133789, 4.768770694732666, "[TT] Star Tracking Capability of the Monochrome Imager = Yes"]
-[9.746893882751465, 5.278837203979492, "[TT] Equipment Health of the Satellite = Nominal"]
-[7.647881984710693, 0.7911941409111023, "[FF] Effect of the Solar Storms = Cause the regolith in the moon's PSRs to accumulate charge in two layers until explosively released"]
-[4.992921352386475, 3.4592862129211426, "[TT] Manufacturer of the Advanced Sensor = Harris"]
-[14.192522048950195, 3.1557822227478027, "[TT] Mass of the DPU = 15 kg"]
-[10.691156387329102, 7.504846572875977, "[TT] Swath Width of the Wide Fine Resolution Beams = 170 km, 150 km, 120 km"]
-[6.985305309295654, 4.415562629699707, "[FF] Unknown of the DLTU = Unknown"]
-[5.319291114807129, 1.3291552066802979, "[FF] Mission Operation Phase of the TET-1 = One Year"]
-[6.673003673553467, 5.135917663574219, "[FF] Link Types of the LCT links = Return, forward, bidirectional"]
-[3.906665802001953, 3.446173906326294, "[FF] Lives Saved Annually of the Galileo = More than 2000"]
-[4.596994876861572, 0.040488846600055695, "[TT] End of Life Date of the STARSHINE = 21 January 2003"]
-[11.19191837310791, 1.0123125314712524, "[FF] Prototype Laser Delivery Date of the LISA = May, 2021"]
-[5.238585948944092, -0.2972312867641449, "[TT] Jettison Time of the Launch Abort System = 6 minutes and 20 seconds"]
-[7.229860782623291, 0.9438658356666565, "[FF] Earthquake Date of the Southern California = Early July 2019"]
-[11.219372749328613, 0.9750531315803528, "[TT] Type of mission of the LISA = L-class mission"]
-[5.323042869567871, 5.648187637329102, "[TT] Data Bus of the Command and Data Handling Subsystem = MIL-STD-1553"]
-[7.3412251472473145, 2.322136878967285, "[TT] Crosses the Equator of the JPSS-1/NOAA-20 = About 14 times daily"]
-[4.062822341918945, 3.5779976844787598, "[FF] Compliance of the GGTO = Feasible compliance to the Galileo requirements"]
-[6.187939167022705, 5.442384243011475, "[FF] Function of the Antenna System = Front-end for transmission and receipt of the RF signals"]
-[9.413542747497559, -0.19701114296913147, "[TT] Perigee of the Starlink Satellites = 210 kilometers"]
-[4.937329292297363, 8.2877779006958, "[TT] Bandwidth of the Antenna = 19.077 MHz"]
-[7.267043113708496, 4.152444362640381, "[TT] Design of the Formation Flying Control (FF-C) = Robust structured 6DoF controller using H-infinity and mu-tools"]
-[7.0988922119140625, 3.473857879638672, "[TT] Planned Number of Satellites of the TROPOMI = 1"]
-[6.2526702880859375, 1.195696234703064, "[FF] Conference Presentation Date of the SJ-9 Technology Demonstration Satellite = Sept. 23-27, 2013"]
-[11.823458671569824, 3.2836501598358154, "[TT] LAM Thrust of the Propulsion = 440 N"]
-[5.914453983306885, 2.2424590587615967, "[FF] Image Credit of the GLI = JAXA"]
-[3.0745043754577637, -0.04616271331906319, "[TT] Orbital Slot of the GSAT-0208 = C07"]
-[7.949518203735352, 7.968996524810791, "[TT] Spectral Resolution of the HSC-III optics subsystem = 5 or 10 nm"]
-[3.76637864112854, -0.7549946904182434, "[FF] Orbit of the SuperView-1 = Low Earth"]
-[6.916140556335449, -0.2799301743507385, "[FF] Radio Signals of the Hitomi = 3/29 00:33 (for about 6 sec) @ SNT"]
-[6.777838706970215, 1.5664461851119995, "[FF] Design Purpose of the First Arab mission to Mars = To inspire youth"]
-[8.153322219848633, 2.586188793182373, "[FF] Measurement Capability of the CATS = Fly on the International Space Station"]
-[5.077704906463623, 3.3008105754852295, "[TT] Manufacturer of the DESIS = German Aerospace Center (DLR)"]
-[9.487817764282227, 7.169075965881348, "[TT] Spatial resolution at nadir of the MERSI = 1.1/0.250 km"]
-[10.005889892578125, 4.395301342010498, "[TT] Torque Provider of the Permanent Magnets = Small amount"]
-[11.135660171508789, 5.537132263183594, "[TT] Material of the Tether = Spectra woven around yarn"]
-[4.704028606414795, 0.8108066320419312, "[TT] Launch Date of the ArgoMoon = 16 November 2022"]
-[9.898523330688477, 0.7510982751846313, "[TT] Observation Distance of the GOSAT-2 = 500 km"]
-[4.524085998535156, 6.437991619110107, "[FF] Communication Links of the Lunar Pathfinder = S-band and UHF to lunar assets, X-band to Earth"]
-[4.746804237365723, 8.097430229187012, "[TT] Frequency of the DASS = 1544 MHz"]
-[8.672951698303223, 5.076517581939697, "[TT] Star Position Accuracy (3\u03c3) of the STOs and STAEs = Random Bias 3.1 arcsec (4 mag), 9 arcsec (6 mag); 13.7 arcsec (6.5 mag)"]
-[5.137424945831299, 3.2565200328826904, "[TT] Owner of the RapidEye = BlackBridge"]
-[3.3716325759887695, 2.1020023822784424, "[FF] System Overview of the Sentinel-1 = Unknown"]
-[3.3519558906555176, 5.223011016845703, "[TT] Polarization Isolation of the SAR Antenna = \u226525 dB"]
-[3.902371406555176, 0.18522466719150543, "[FF] Image Release Date of the SMART-1 = March 03, 2008"]
-[11.96941089630127, 4.9300432205200195, "[TT] Size of the Receiver = 70 mm x 60 mm x 30 mm"]
-[11.932296752929688, 4.9708685874938965, "[TT] Volume Comparison of the MiniCOR = ~10 smaller volume than LASCO C3"]
-[5.685636043548584, 5.492594242095947, "[TT] Processor Generation of the SES-17 = Fifth-generation"]
-[8.622352600097656, 7.513841152191162, "[TT] Detector Type of the NEA Scout Camera = CMV20000 CMOS"]
-[11.507152557373047, 3.4338903427124023, "[TT] Propulsion System of the DFACS = CGPS (Cold Gas Propulsion System)"]
-[7.753149509429932, 8.810870170593262, "[TT] Spectral Band Interval of the SMI = 13 nm"]
-[7.156708240509033, 1.0802695751190186, "[FF] Flood Mapping Date of the Satellites = 16 July 2021"]
-[6.719448566436768, 4.482178211212158, "[FF] Description of the FDIR (Failure Detection, Isolation and Recovery) test maneuvers = FDIR (Failure Detection, Isolation and Recovery) test maneuvers"]
-[3.153885841369629, 2.3314452171325684, "[TT] Imagery Type of the Sentinel-2 = Optical"]
-[6.970869541168213, 5.083755970001221, "[FF] Function of the CMART = Generate anomaly trouble tickets and support the prioritization, tracking, and resolution of anomalies"]
-[9.899815559387207, -0.3439706563949585, "[TT] Altitude of the Primary Payload = 1450 km"]
-[4.786267280578613, -0.02261962927877903, "[TT] End of Life Date of the ITUpSat-1 = 2030"]
-[7.527547836303711, 3.741489887237549, "[FF] Mode Function of the NightPod = Manually pointing the camera to specific targets and making single-shot pictures"]
-[8.12758731842041, 3.5295701026916504, "[FF] Operation of the OCO-2 = Pass through the atmosphere twice"]
-[7.952317714691162, 8.584769248962402, "[TT] Spectral range of the VIRR = 0.43-12.5 \u00b5m"]
-[14.277127265930176, 2.971376895904541, "[TT] Mass of the AprizeSat-9 and -10 = 12 kg"]
-[9.902289390563965, 7.731701374053955, "[FF] Telescope Sensitivity of the EUVI = Higher sensitivity"]
-[3.1858155727386475, 5.049446105957031, "[TT] Experimental Mode Coverage of the TSX-SAR = 5 x 10"]
-[13.577448844909668, 5.85628080368042, "[TT] Power Source of the Gaia = Solar power"]
-[9.997852325439453, -1.5057084560394287, "[TT] Orbit Inclination of the VesselSat-1 = 20\u00ba"]
-[13.331412315368652, 7.310235023498535, "[TT] Power of the NINA = 40 W"]
-[11.39277458190918, 8.921822547912598, "[FF] Image Acquisition Date of the MODIS = January 30, 2022"]
-[5.253819942474365, 7.702698707580566, "[TT] E5 to E1 Port Isolation of the Antenna = Better than 20 dB"]
-[10.21558666229248, 5.642594337463379, "[FF] Temperature of the SWAP = One million degrees"]
-[2.2914013862609863, 2.7677149772644043, "[TT] SSM of the EPI-Lo = Robert Gold"]
-[10.666184425354004, 1.0421687364578247, "[FF] Loop Span of the TRACE = 30 or more times the diameter of planet Earth"]
-[7.792773723602295, 7.1732282638549805, "[TT] Compression Algorithm of the COTS Cameras = JPEG"]
-[6.314262866973877, 8.103110313415527, "[TT] Number of Passbands of the Channel 5 = 1"]
-[3.629136562347412, 5.338842868804932, "[TT] Power of the MMW Radar = 120 W"]
-[5.087080955505371, 3.080075263977051, "[TT] Affiliation of the CubeBug-2 = Argentina (sponsored by the Argentinian Ministry of Science, Technology and Productive Innovation)"]
-[5.4590067863464355, 1.1501131057739258, "[TT] Commissioning Result of the QUESS = Successful"]
-[6.570403099060059, 5.091427803039551, "[FF] Map Projection of the L1C Products = User Selectable"]
-[5.812922954559326, 6.227348327636719, "[TT] Storage Capacity of the SSR = 3.1 Tbit @ EOL"]
-[4.719638347625732, 7.204493999481201, "[TT] X-band Link Data Rate of the Onboard Storage and Communication Subsystem = 64Mbit/s"]
-[8.756829261779785, 6.808242321014404, "[TT] Generation of the DMC-2 = Current"]
-[6.477555751800537, 7.638505458831787, "[TT] Data Quantization of the Scanning geometry = 10 bit"]
-[4.796656131744385, -0.012083140201866627, "[TT] End of Life Date of the GPIM = 14 October 2020"]
-[5.599462509155273, 5.6792449951171875, "[TT] Microprocessor of the C&DH subsystem = Rabbit 3000 8-bit microprocessor"]
-[4.3354878425598145, 2.6861209869384766, "[TT] Launch Location of the Astra's Rocket = Kodiak Island, Alaska"]
-[9.153962135314941, 6.091662406921387, "[TT] Moving Warm Start Acquisition Time of the Antenna Subsystem = < 300 s"]
-[3.4615235328674316, -0.8941981196403503, "[TT] Orbit Type of the CALIPSO = Sun-synchronous"]
-[3.4224212169647217, 4.93423318862915, "[TT] Payload of the PAZ = X-band SAR (Synthetic Aperture Radar)"]
-[13.796170234680176, 2.72587251663208, "[TT] Launch Mass of the Resurs-O1 spacecraft = About 1800-1900 kg"]
-[9.295660018920898, 4.891586780548096, "[TT] Performance of the Vehicle Attitude Control = Nominal"]
-[4.687568187713623, 0.15485291182994843, "[TT] End of Life Date of the IDEA OSG 1 = 28 November 2017"]
-[5.676445484161377, 6.3892903327941895, "[TT] Data Recorder Capacity of the C&DHS = >30 GByte"]
-[8.910188674926758, 7.9839606285095215, "[TT] Number of CCDs of the Focal Plane Array = 36"]
-[6.079102039337158, 7.060959815979004, "[TT] Modulation of the Optical Downlink = 16-ary PPM format"]
-[7.94675874710083, 9.151395797729492, "[TT] Wavelengths of the LRR = \u03bb = 694 nm and \u03bb = 532 nm"]
-[6.289797306060791, 1.1965852975845337, "[FF] Adverse Influences of the SJ-9A = Interference with in-situ environment, electromagnetic interference"]
-[4.771674633026123, 8.030145645141602, "[TT] Frequency of the L-band real-aperture scatterometer = 1.26 GHz"]
-[9.45402717590332, 4.97548246383667, "[TT] Attitude Stability of the AOCS = \u2264 0.01\u00ba/s (3\u03c3)"]
-[13.296602249145508, 2.9464917182922363, "[TT] Mass of the MicroMAS-2 CubeSat = 3.8 kg"]
-[4.54740571975708, 6.936789035797119, "[FF] Capability of the TacSat-4 = Transmitting and receiving multiple carriers simultaneously"]
-[8.573486328125, 3.7189531326293945, "[FF] Advance in Accuracy Over Current Instruments of the CLARREO\u2019s infrared and reflected solar spectrometers = Unknown"]
-[9.034065246582031, 5.566450119018555, "[TT] Pointing Solution Update Rate of the Adcole Maryland Aerospace MAI401 ADCS = 10 Hz"]
-[8.067399024963379, 6.488357067108154, "[TT] Scan Mode of the SSULI = Every 90 seconds"]
-[3.8778538703918457, 4.996622085571289, "[TT] Calibration Stability for 7 days of the Radar (ALScat) = 0.13 dB"]
-[10.049385070800781, 4.330494403839111, "[TT] Quantity of the Ithaco Inc. 60 Am2 electromagnetic torque rods = Three"]
-[5.287461280822754, 3.207500696182251, "[TT] Manufacturer of the Lucy = Lockheed Martin Space"]
-[7.454672336578369, 3.2971911430358887, "[FF] Description of the Level-6 (L6) = Thematic map (classification)"]
-[5.7719902992248535, 2.861018180847168, "[TT] Preference for Working with U.S. companies of the NASA = Strong"]
-[8.496211051940918, 1.4036699533462524, "[FF] Sea Surface Salinity Measurement of the Aquarius/SAC-D = Unknown"]
-[4.374454975128174, 3.1757287979125977, "[TT] Location of the Goonhilly Earth Station = UK"]
-[5.594631671905518, 2.4715254306793213, "[TT] Test Team of the FFRF = CNES team"]
-[8.8313570022583, 7.628629207611084, "[TT] Pixel Array Pitch of the MWIR Imager = 8 \u03bcm"]
-[6.733895778656006, 5.854380130767822, "[TT] Quantity of the OBC750 = 2"]
-[9.79500675201416, 8.203386306762695, "[TT] Lens Focal Length of the Instrument = 14 cm"]
-[4.86480712890625, 6.737733364105225, "[TT] Transceivers of the RF Subsystem = Two"]
-[11.380125045776367, 2.8117451667785645, "[TT] Transmitter/Receiver and the Buffer Store Mass of the Microsatellite = 12.5 kg"]
-[9.157343864440918, 7.227663516998291, "[TT] Nominal Vertical Resolution of the Detector = 1 km"]
-[8.108135223388672, 2.2276508808135986, "[FF] System Level Specifications Retained of the SCATSat-1 = OSCAT instrument"]
-[8.683363914489746, 3.9131577014923096, "[TT] Field of View of the TRACE instrument = 1/10th of the solar disk"]
-[7.610477924346924, 8.714120864868164, "[TT] Total Number of Spectral Bands of the MSU-100 = 6"]
-[8.71996784210205, 6.794082164764404, "[FF] Scale of the Image = Indicated on the image"]
-[7.728712558746338, 2.1361918449401855, "[FF] Purpose of the Global Carbon Cycle = Understanding the global carbon cycle and how it responds to human and natural forcing"]
-[5.071760654449463, 4.412978649139404, "[TT] Number of DASS POC payloads with S-band of the GPS II = 16"]
-[6.601635456085205, 0.2568548321723938, "[TT] Mission Start Date of the CryoSat-2 = June 21, 2011"]
-[8.416929244995117, 7.86061954498291, "[TT] Spectral Range of the Detector = 0.25-50 \u00b5m"]
-[8.503952980041504, 6.0551886558532715, "[TT] Accuracy of the TSIS-1 SIM = uc < 0.25%"]
-[13.378847122192383, 7.345119476318359, "[TT] Power of the GeoCarb = 128 W"]
-[7.321829319000244, 9.172810554504395, "[TT] Wavelength Shift of the FG (Filtergraph) = Up to 26 km/s"]
-[10.256933212280273, 4.502250671386719, "[FF] Actuators of the IRS-1C and IRS-1D = Four reaction wheels, two magnetic torquers, 16 one Newton hydrazine trusters, one 11 Newton thruster"]
-[7.701674938201904, 6.457859992980957, "[FF] Function of the Detection Circuit = Counts the number of arcs"]
-[11.01414966583252, 0.5872533917427063, "[TT] Number of Planets of the TOI-178 = 6"]
-[4.519110679626465, -0.88850998878479, "[TT] Berthing Date of the Dragon C2/3 spacecraft = May 25, 2012"]
-[5.511842250823975, 3.2917823791503906, "[TT] Platform of the Heinrich-Hertz satellite = SmallGEO (SGEO)"]
-[10.828619956970215, 1.3957518339157104, "[TT] Mass of Stars of the Eta Carinae = 90 and 30 times the mass of our Sun"]
-[7.706484794616699, -0.8932618498802185, "[TT] Instrument PDR Date of the ICESat-2 = Nov. 18, 2011"]
-[10.005322456359863, -1.5121495723724365, "[TT] Orbit Precession of the TRUTHS = 90 degrees"]
-[4.648362159729004, 6.922514915466309, "[TT] Telemetry Downlink of the Aleph-1 satellites = X-band feeds, one at 8030 MHz using a custom protocol for 100 kbit/s"]
-[8.275845527648926, 7.566443920135498, "[TT] CCD Detector of the NMS = 256 x 256 elements"]
-[9.640176773071289, 7.818686485290527, "[TT] Quantity of the Telescopes = 26"]
-[7.787473678588867, 2.5375583171844482, "[FF] Data Usage of the ISS LIS = Air-traffic advisories, climate monitoring"]
-[8.903386116027832, 8.090731620788574, "[FF] Glass Segmentation of the Optic = Unknown"]
-[10.179604530334473, 5.929887294769287, "[TT] Operating Temperature of the VNIR focal plane = 20\u00baC"]
-[10.054884910583496, -1.5530381202697754, "[TT] Maximum Slope of the Schiaparelli = 12.5\u00ba"]
-[6.031187057495117, -0.23063646256923676, "[TT] Design Life of the FormoSat-2 = 5 years"]
-[9.406095504760742, -0.38411909341812134, "[TT] Apogee of the SCD-2 = 768 km"]
-[6.904306411743164, 1.4973655939102173, "[FF] Development Status of the Webb = Not provided"]
-[6.164089679718018, 1.0419570207595825, "[FF] Capture Date of the Earth from Space = 30 January 2022"]
-[11.218225479125977, 5.93133020401001, "[FF] Design of the Cupola Windows = Four layered front to potential impactors: a debris pane, two pressure panes, and an inner scratch pane"]
-[3.6450014114379883, 6.967514991760254, "[TT] Polarization of the Antenna for Navigation = RHCP (Right Hand Circular Polarization)"]
-[5.684207439422607, 4.391116142272949, "[TT] Number of Checkouts of the EDM = Three"]
-[6.607595443725586, 5.807693958282471, "[TT] Quantity of the Total Board Count = 18"]
-[13.766100883483887, 3.667820692062378, "[TT] Mass of the Antenna = < 400 kg"]
-[9.244050979614258, 7.123963356018066, "[TT] Measurement Resolution of the Cluster S/C = >= 6 pT"]
-[14.491515159606934, 6.534947872161865, "[TT] Battery Capacity (BOL) of the CubeSat power module = 7.2 Whr"]
-[5.925105571746826, 0.7575003504753113, "[TT] Launch Date of the Transiting Exoplanet Survey Satellite = Oct. 28, 2014"]
-[5.110674858093262, 5.19058895111084, "[TT] GPS Receivers of the TanDEM-X = Dual-frequency"]
-[7.537108898162842, -2.4802803993225098, "[TT] Launch Date of the GOLD = 25 January 2018"]
-[5.315427780151367, 0.2964940667152405, "[TT] Launch Year of the Ikonos = 1999"]
-[5.696420192718506, 2.835285186767578, "[FF] Developer of the CVX = NASA/GRC"]
-[5.38067626953125, 8.406654357910156, "[TT] Bandwidth of the Instrument = 20 nm (for 415, 750, 900,950 nm); 30 nm (for 1000, 1050, 1250 nm)  50 nm (1550 nm)"]
-[5.75445556640625, 4.977878093719482, "[FF] Downlink Verification Method of the Ground System = Playing back the recorded signal to the flight unit or an engineering unit and verifying the uplinked commands"]
-[8.931370735168457, 4.664592742919922, "[TT] Quantity of the Earth Horizon Sensors = 2"]
-[5.8186445236206055, 2.4579458236694336, "[FF] Platform of the RemoveDebris Mission = EU (European Union) Framework 7 (FP7) research project"]
-[7.730072021484375, 0.3030596971511841, "[TT] Main Belt Asteroid Flyby Date of the Lucy = 2025"]
-[9.977616310119629, 2.9278972148895264, "[TT] Launch Date of the STARE-B 3U CubeSat = November 20, 2013"]
-[5.027715682983398, 3.3093669414520264, "[TT] Manufacturer of the DTUSat-2 = DTU (Technical University of Denmark)"]
-[9.841106414794922, 3.8048582077026367, "[TT] Mounting Location of the Collector Arrays = Within the sample canister"]
-[7.894765377044678, 5.223435401916504, "[FF] Error Sources of the FLLS = Unknown"]
-[5.533141613006592, 1.1722713708877563, "[FF] Publication Date of the Supercapacitors = 1999"]
-[9.652693748474121, 0.22464331984519958, "[TT] Parachute of the Schiaparelli = Disk-Gap-Band canopy, 12 m diameter"]
-[12.083000183105469, 3.007389783859253, "[TT] Thruster Type of the Propulsion Subsystem = 1N hydrazine"]
-[8.65158748626709, 7.995409965515137, "[TT] Pixel Offset of the Band-64 = 34 pixels out of 256 pixels"]
-[5.206984043121338, 0.9558693170547485, "[TT] Mission of the MANTIS = Demonstration"]
-[3.4544951915740967, -0.9018823504447937, "[TT] Orbit Type of the ICEYE-X14 and ICEYE-X16 = Sun-synchronous"]
-[6.2173357009887695, 4.194925308227539, "[FF] Overview of the ASNARO Ground System = An overview of the ASNARO ground system"]
-[6.391813278198242, 3.191220283508301, "[TT] Revisit Time of the BlackSky's Satellites = Every 30 minutes"]
-[10.27612590789795, 1.9336150884628296, "[TT] Brightness Outburst of the GX 339-4 = Less than 1 percent of its maximum expected brightness"]
-[9.563972473144531, 9.06950855255127, "[TT] Spatial Resolution of the IRIS = 0.33 arcsec"]
-[8.196578025817871, 7.349395275115967, "[FF] Sensor Complement of the HJ-1A = Wide View CCD Cameras (WVC), Hyperspectral Imager(HSI)"]
-[5.417187690734863, 3.119722843170166, "[TT] Partner of the ROSA = Deployable Space Systems"]
-[10.31573486328125, 3.635969877243042, "[TT] Location of the Solar Cells = Five sides of the nanosatellite, sun-facing -Z surface of the spacecraft"]
-[10.248688697814941, 4.211340427398682, "[TT] Movement Direction of the CCRR = +X direction and then back again along the same path in the -X direction"]
-[11.98204517364502, 5.076993465423584, "[TT] Size of the EPS = 96 x 90 x 20 mm"]
-[7.925230503082275, 8.334524154663086, "[TT] CCD Type of the Pan band = PhotoMOS-type"]
-[6.092405319213867, 1.3482736349105835, "[FF] Image Creation Date of the SwRI-led team = 18 July 2018"]
-[5.46476411819458, 6.5429534912109375, "[TT] Mass Data Storage of the DubaiSat-1 = 32 Gbit"]
-[6.520915508270264, -1.9688798189163208, "[TT] Design Life of the Jason-1 = 5 years"]
-[9.963933944702148, -0.3850461542606354, "[TT] Orbit Altitude of the Secondary Payloads = ~820 km"]
-[5.842345237731934, 0.9799527525901794, "[FF] Last Chance to View of the BepiColombo = 14 June 2017"]
-[11.987370491027832, -0.3314765691757202, "[TT] Project Scientist of the TESS = Patricia Boyd"]
-[8.028458595275879, 0.8375630974769592, "[FF] Drought Observation of the GRACE = 2018 - 2020"]
-[7.360703945159912, 0.18796557188034058, "[TT] Mission Duration of the OSIRIS-REx = Two years"]
-[7.068806171417236, 5.075328350067139, "[FF] Modes of the Operational modes = ON, Standby, Survival"]
-[7.692553997039795, 9.383148193359375, "[TT] Center Wavelength of the MS8 (NIR2) = 908 nm"]
-[7.628346920013428, 0.8517730832099915, "[FF] Coverage of the Permanently Shadowed Regions = About three percent of the moon's south pole"]
-[8.99909496307373, 5.116456031799316, "[TT] Accuracy Range of the MEMS-based rate gyroscope assembly = \u00b15\u00ba/s"]
-[7.34335994720459, 8.444727897644043, "[TT] Number of IR spectral filters of the Filter Wheel = 18"]
-[5.345749855041504, 0.9984189867973328, "[FF] Presentation Date of the STSat-1 = Dec. 13-17, 2004"]
-[5.2083210945129395, 2.203840494155884, "[TT] Mission Status of the Myriade/AstroSat-100 = Operational (extended)"]
-[13.464491844177246, 2.892425775527954, "[TT] Mass of the Satellite = 100-400 kg"]
-[9.681715965270996, 7.413887023925781, "[TT] Performance Area of the Nadir Profile Spectrometer = 250 km x 250 km"]
-[10.298436164855957, 5.174854278564453, "[FF] Loading Temperature of the Helium = Cold"]
-[13.88794994354248, 2.7131028175354004, "[TT] Launch Mass of the Spektr-RG = ~2650 kg"]
-[11.447944641113281, 3.505154609680176, "[TT] Design Completion of the Solar Electric Propulsion (SEP) Chassis = Nearly complete"]
-[8.673240661621094, 2.7352497577667236, "[TT] Temperature Accuracy of the Lower atmosphere = 3 K at 850 mb"]
-[5.40399169921875, 3.923837661743164, "[TT] Number of Satellites of the Landsat Next = 3"]
-[11.218716621398926, 5.701818466186523, "[TT] Thickness of the Device Wafer = 100 \u00b5m"]
-[10.06816291809082, -1.5210859775543213, "[TT] Orbit Inclination of the HY-2B = 99.3\u00ba"]
-[7.662358283996582, 8.089098930358887, "[TT] Color in Image of the Swift J0042.6+4112 = Blue"]
-[8.957663536071777, 7.969213962554932, "[TT] Technology of the ISIR = Microbolometer Focal Plane Arrays"]
-[4.0866923332214355, 6.299290180206299, "[TT] Antenna Type of the APAA = Transmitting and receiving"]
-[7.473631858825684, 7.370278358459473, "[FF] Journal Article of the Demeter = Chorus and chorus-like emissions"]
-[10.329371452331543, 6.275906085968018, "[TT] Sensitivity Improvement of the NuSTAR = 50 - 100"]
-[6.674469947814941, 5.218930244445801, "[FF] Components of the PMS = TPU (Thermal Power Unit) and MMU (Memory Management Unit)"]
-[8.304622650146484, 6.358520030975342, "[TT] Maximum Longitudinal Displacement of the CCRR = 6 m (TBC)"]
-[6.427424907684326, 6.283592700958252, "[TT] Continuous Receive of the User Terminal = 5 hrs"]
-[3.939854621887207, 2.0017662048339844, "[TT] Serial Number of the Astra's Rocket = LV0007"]
-[8.478344917297363, 8.652851104736328, "[TT] Measurement Range of the Ultraviolet Spectrometer = Up to 43,000 km from the surface"]
-[8.792075157165527, 0.0532364547252655, "[TT] Bipropellant System Lunar Departure \u0394V of the Clementine = About 540 m/s"]
-[14.260761260986328, 3.125020742416382, "[TT] Mass of the Shakuntala = Less than 15 kg"]
-[13.140606880187988, 7.320633888244629, "[TT] Power Consumption of the CEASE-1 = 1 W"]
-[7.669464111328125, 0.7212582230567932, "[FF] Enrichment of the Moon = Heat-producing elements"]
-[7.387948513031006, 1.1880900859832764, "[FF] Status Update Date of the SeaWiFS = Jan. 24, 2011"]
-[11.818538665771484, 6.728307247161865, "[TT] Photon Energy Range of the XGRE = 20 keV \u2013 10 MeV"]
-[7.3107500076293945, 9.08774185180664, "[TT] Filter Wavelength of the ISUAL instrument = 337.0 nm"]
-[6.705198287963867, 4.423823833465576, "[FF] Purpose of the HDR Mechanism = Provide fault tolerance against premature deployment"]
-[4.506107807159424, -0.9079540967941284, "[FF] Symposium Date of the Dragon 2 = June 25-29, 2012"]
-[2.907620906829834, 4.508328437805176, "[TT] Signal-to-Noise Ratio of the PALSAR-2 = 13 dB"]
-[5.7664594650268555, 0.5852749347686768, "[TT] Launch Date of the SuperView-1 01 and Superview-1 02 = December 28, 2016"]
-[11.552268028259277, 3.0782060623168945, "[TT] Incident Cause of the Meteosat-8 = Likely hit by a micro-meteorite or space junk"]
-[5.41856050491333, 1.0441160202026367, "[FF] Date of the IGARSS = July 26-31, 2015"]
-[11.553144454956055, 3.5638887882232666, "[FF] Setup of the Integrated Firing Test = Spacecraft installed the propulsion system was mounted on the thrust stand"]
-[11.175284385681152, 5.923527240753174, "[TT] Material of the HiRAIS = CFRP"]
-[7.241953372955322, 5.898813247680664, "[TT] Design/Qualification Approach of the LCT = Identical for GEO and LEO application"]
-[11.074955940246582, 0.647296667098999, "[FF] Observation of the ExoplanetSat = Exoplanets"]
-[4.373945713043213, 2.344081163406372, "[TT] Launch Site of the TanSat = JSLC (Jiuquan Satellite Launch Center), China"]
-[7.24233341217041, 8.526020050048828, "[TT] VBB Performance of the SEIS Instrument = -9 m s-2 Hz-\u00bd from 10-3 up to 10 Hz"]
-[5.086166858673096, 0.5458272695541382, "[FF] Launch Preparations Date of the Mission Extension Vehicle = 30 June 2020"]
-[8.099369049072266, -0.29508787393569946, "[FF] Weather Pattern of the Greenland = Lower rates of snowfall compared to the long-term average in 2019"]
-[5.49019718170166, 7.153358459472656, "[TT] Data Transmission Rate of the HGAA = Up to 72 Mbit/s"]
-[11.196420669555664, 5.39202880859375, "[TT] Plastic Scintillator of the Range Calorimeter = 16 planes"]
-[8.884014129638672, 9.472695350646973, "[FF] Anomalies of the TANSO-FTS = Present"]
-[9.01686954498291, 4.444011688232422, "[FF] Required Spacecraft Orientation for Stability of the Kepler Space Telescope = Nearly parallel to its orbital path around the sun"]
-[5.731168746948242, 12.150063514709473, "[TT] Wavelength FWHM of an unresolved line of the Spectrometer = 0.013 \u00b5m"]
-[8.31295108795166, 8.709736824035645, "[TT] Operation of the UV/VIS Spectrometer = Continuously over full orbit"]
-[11.307478904724121, 3.4402220249176025, "[FF] Propulsion System Control of the BepiColombo = Mercury Planetary Orbiter\u2019s onboard computer"]
-[5.737957954406738, 1.3532252311706543, "[FF] Launch Date of the SWOT = Unspecified"]
-[6.909321308135986, 1.0127952098846436, "[TT] Landing Date of the Perseverance rover = Feb. 18, 2021"]
-[5.340551376342773, 0.369577556848526, "[TT] End Date of the SRL-1 (STS-59) = April 20, 1994"]
-[5.191498756408691, 1.8839035034179688, "[TT] Mission Status of the Resurs-P1 = Operational"]
-[9.533425331115723, 8.170700073242188, "[FF] Field of View of the Roman = Wide"]
-[9.385747909545898, 5.392815113067627, "[TT] Angular Random Walk of the IRU = 0.008\u00ba/sqrt hr"]
-[6.876397132873535, 7.025089740753174, "[TT] Repetition Rate of the Laser Transmitter = 51 Hz"]
-[11.978689193725586, 3.0398271083831787, "[TT] Total \u0394V of the Station keeping = 85 m/s"]
-[7.402868270874023, 2.4015114307403564, "[TT] Sampling of the Satellite = Poor spatial and temporal sampling: each point on globe sampled just once every day on dayside, once nightside"]
-[6.483127593994141, 3.6567955017089844, "[FF] Use of the DMSP-20 = Support military operations"]
-[5.523014545440674, 5.080814838409424, "[TT] Platform of the IOD-1 GEMS = CSL 3U structure"]
-[13.784846305847168, 5.334367752075195, "[FF] Cell Type of the AzurSpace 3G30 Triple Junction GaAs/Ge cells = AzurSpace 3G30 Triple Junction GaAs/Ge cells"]
-[4.409952163696289, 5.426845550537109, "[FF] Mission Results Presentation Date of the GomX-3 = August 6-11, 2016"]
-[7.662469863891602, 0.8233916759490967, "[FF] Detection Method of the Lunar Meteoroid Impact Flash Detection = Light flashes at the Moon are typically observed by detecting a local spike of the luminous energy in the visible spectrum when pointing a telescope at the lunar night side"]
-[9.07103443145752, 3.2218947410583496, "[FF] Magnetic Waves Discovery Date of the Swarm = 23 May 2022"]
-[11.11804485321045, 5.970451354980469, "[TT] Window Damage of the Cupola = Minor"]
-[5.04923152923584, -0.2777455151081085, "[TT] Launch Time of the TanSat = 19:22 UTC"]
-[4.734799385070801, 2.777010679244995, "[TT] CEO of the Lacuna Space = Rob Spurrett"]
-[8.608098030090332, 7.654870510101318, "[TT] Die Size of the CCID-80 = 32 (W) x 64 (H) mm"]
-[4.949013710021973, -0.07155802845954895, "[TT] Launch Window of the Launch = 12 days"]
-[7.474853515625, -0.6562624573707581, "[TT] Data Size of the Operation IceBridge = Hundreds of terabytes"]
-[8.108144760131836, 7.27614688873291, "[TT] Stability of the Radiometer stability for 7 days = 0.12 K"]
-[9.505536079406738, 6.260769367218018, "[FF] Control of the Precision Flat Scan Mirror = Scan mechanism assembly"]
-[6.404618740081787, 3.6409990787506104, "[FF] Purpose of the SSIKLOPS = Provide means to release small satellites from the ISS"]
-[9.161526679992676, 5.35142707824707, "[TT] Pointing Error of the AOCS = \u00b1 0.05\u00ba in roll and pitch"]
-[9.002086639404297, 8.016728401184082, "[TT] CCD Line Pixel Count of the Focal Plane Module = 12,000 pixels"]
-[6.237504959106445, 3.908078193664551, "[FF] Project Role of the UAH = Management, System Engineering, Science & Payload"]
-[8.086020469665527, -1.0099709033966064, "[TT] Data Collection of the ICESat-2 = Elevation measurements of Earth\u2019s surface"]
-[3.455812454223633, -0.9133607745170593, "[TT] Orbit of the MinXSS-2 = Sun-synchronous, polar orbit"]
-[8.148797988891602, -0.886134147644043, "[FF] Measurement Type of the Microwave instruments = Arctic sea ice extent"]
-[6.767405986785889, 1.9760960340499878, "[FF] Survey Content of the Nancy Grace Roman Space Telescope = Analyze millions of galaxies"]
-[8.47928237915039, 4.599045753479004, "[FF] Components of the Integrated Navigation System = INS, star tracker (2), altimeter (2), velocimeter (2) and image sensor (2)"]
-[8.022270202636719, 2.621853828430176, "[TT] Team Leader of the CAPI (Cloud and Aerosol Polarization Imager) = Zhongdong Yang"]
-[7.106463432312012, -0.6378946304321289, "[TT] Rotation Period of the Zeta Puppis = 1.78 days"]
-[7.949049949645996, 8.680118560791016, "[FF] Sensitivity of the VT = High sensitivity, in particular at long wavelength"]
-[6.698467254638672, 6.153193950653076, "[TT] Number of L2+ End-Products Requiring Ancillary Data Inputs of the ADRS = 20"]
-[8.5833740234375, 7.111204624176025, "[TT] Image Generation of the MVIRI = Simultaneous"]
-[10.09390640258789, 2.036109209060669, "[FF] Parameter Measurement of the NuSTAR = Distance particles in jets travel before they \"turn on\""]
-[8.073145866394043, 2.721787691116333, "[FF] Measurement Domain of the Satellite = Atmosphere, Ocean, Land, Gravity and Magnetic Fields, Snow & Ice"]
-[8.712539672851562, 2.4404423236846924, "[FF] Sample Capture Method of the TAGSAM = Nitrogen gas will blow onto the surface to roil up dust and small pebbles, which will then be captured in the TAGSAM head"]
-[3.9287779331207275, 2.0631818771362305, "[TT] Launch Vehicle of the NeuSAR = ISRO Indian Polar Satellite Launch Vehicle"]
-[7.406179904937744, 3.6698782444000244, "[TT] BeiDou Occultations of the GNOS Instrument = About 200 per day"]
-[7.019415855407715, 5.142397880554199, "[FF] Mode of the LISS-4 = Mx mode"]
-[6.475587844848633, 5.690120220184326, "[TT] Door Latch of the CSD = Automatically resettable"]
-[7.866643905639648, 8.670047760009766, "[TT] Spectral Range of the MWIR = 3.4-4.2 \u00b5m"]
-[8.036890983581543, 5.916957378387451, "[FF] Objective of the CMOS Camera = Take occasional snapshot imagery of Earth and to use the camera for onboard event verification"]
-[4.886709213256836, -0.5849255919456482, "[FF] Development Date of the SLATS = June 5-12, 2011"]
-[10.796248435974121, 3.4672048091888428, "[TT] Size of the SPORT 6U CubeSat = 6U"]
-[8.179962158203125, -1.1071890592575073, "[FF] Function of the Multispectral Bathymetric Tool for Esri ArcPro = Process Satellite Derived Bathymetry data, assess accuracy, and output as .BAG files"]
-[5.225471019744873, 8.07959270477295, "[TT] Frequency of the IME-BF 1 = DC - 1 MHz"]
-[9.778547286987305, 7.463308334350586, "[TT] Cross-Track Swath of the OMPS Nadir Sensor = 2800 km"]
-[5.904742240905762, 0.39333245158195496, "[FF] Discovery Date of the Rosetta = 26 Oct. 2017"]
-[9.586101531982422, 8.217720985412598, "[TT] IFOV of the 16 mm camera = 9.2 x 10 -3  degrees"]
-[5.8983988761901855, 6.2836198806762695, "[TT] Data Delivery of the OPSE = Not usable onboard in real time"]
-[6.009671688079834, 2.973437786102295, "[TT] Developer of the EMIT = NASA\u2019s Jet Propulsion Laboratory"]
-[8.923622131347656, 5.682663917541504, "[TT] Drift Angle Correction Accuracy of the ADCS = \u2264 0.1\u00ba (3\u03c3, correction based on nadir camera)"]
-[5.034623622894287, 3.390130043029785, "[TT] Manufacturer of the PIMS = Johns Hopkins Applied Physics Laboratory (APL)"]
-[5.198947429656982, 5.831307888031006, "[TT] Onboard Communication Bus of the SAST-5000 = 1553B+SpaceWire"]
-[8.961712837219238, 4.407635688781738, "[TT] Type of the Sun Sensors = Dual axis"]
-[12.14047622680664, 1.9711047410964966, "[TT] Launch Date of the CartoSat-2 = Jan. 10. 2007"]
-[5.241382122039795, 0.8912858963012695, "[FF] Presentation Date of the CNES = Feb. 16-18, 2010"]
-[8.628941535949707, 4.503945350646973, "[FF] Purpose of the Arkyd-6A = Test attitude control, power, and communication systems as well as a photo-display-and-retransmission system"]
-[6.960382461547852, 4.226503372192383, "[FF] Unknown of the BELA = Unknown"]
-[3.6085751056671143, 6.251953125, "[TT] Location of the ESA\u2019s three 35 m dish antennas = Australia, Spain and Argentina"]
-[6.183155536651611, 0.3786149024963379, "[FF] Test Cost of the Modern ICs = >$46 M"]
-[9.746655464172363, -0.392712265253067, "[TT] Reentry Altitude of the First Stage = 70 km"]
-[4.927426338195801, 2.8684630393981934, "[TT] Provider of the Roskosmos = Roskosmos"]
-[6.254420280456543, 5.131546497344971, "[FF] Data Transmission of the ACOP = HRDL"]
-[10.373153686523438, 2.181344509124756, "[FF] Brightness Change of the X-ray Source = Up to 50 times its normal level"]
-[9.205982208251953, -0.4180898070335388, "[TT] Phase 2 Apogee Altitudes of the MMS = 25 Re"]
-[9.302099227905273, 3.1943540573120117, "[FF] Fabrication Status of the Compact Coronagraph (CCOR) = Ready to proceed with full-scale fabrication, assembly, integration and test"]
-[9.2084321975708, -0.410083144903183, "[TT] Apogee of the \u00d8rsted satellite = 857 km"]
-[10.518083572387695, 5.498942852020264, "[TT] Activation Method of the TEMBOTM EMC = Heat-activated"]
-[11.383378028869629, 4.431049823760986, "[TT] Size of the CP5 = 1U"]
-[5.4174885749816895, 5.122834205627441, "[TT] Tracking Method of the GPSDR = Track the satellite"]
-[6.6749701499938965, -0.4720006585121155, "[TT] Break-out Time of the Hitomi = 10:42\u00b111M"]
-[6.650994300842285, 3.6228110790252686, "[FF] Forward Bay Cover of the CM (Crew Module) = Protects the top of the spacecraft during flight and reentry through Earth's atmosphere"]
-[5.555514812469482, 1.0861780643463135, "[FF] Vibration Testing Date of the CuPID = April 2021"]
-[9.06775188446045, 7.071026802062988, "[TT] ScanSAR Mode Resolution of the Payload = 5-30 m"]
-[5.7042317390441895, 4.464657306671143, "[FF] Connectivity of the Ground Operations Networks = Spacecraft to the PCC (Payload Control Center) at a specific test site; to the Command Center at the Air Materiel Command's Detachment 2/Space and Missile Center, Onizuka AFB, CA; or to the MCC (Mission Control Center) at APL"]
-[6.864787578582764, 7.256112098693848, "[TT] Repetition Rate of the ATLAS instrument = 10 kHz"]
-[6.801877021789551, 5.827634334564209, "[TT] Number of Units of the GEMS = 2"]
-[6.751184940338135, 1.1932027339935303, "[FF] Date of the New NASA Model Finds Landslide Threats = 22 March 2018"]
-[8.332118034362793, 2.82424259185791, "[FF] Altitude of the Atmospheric Chemistry Experiment (ACE) satellite = Low"]
-[7.775768756866455, 8.374688148498535, "[TT] Resolution of the GOME-2 = 0.22-0.50 nm"]
-[9.308186531066895, 4.980023384094238, "[TT] Attitude Information Source of the ABI = Spacecraft"]
-[13.745223045349121, 5.386683464050293, "[TT] Solar cells of the EPS = 20 x Triple Junction GaAs"]
-[5.649057388305664, 7.101626396179199, "[TT] Data Rate of the APAA subsystem = Up to 6.5 Mbit/s"]
-[4.1216583251953125, 4.742288112640381, "[FF] Beam Modes of the RADARSAT-2 sensor = 450 km wide ship detection optimized beam mode in the HH polarization channel, and a 530 km wide multi-purpose beam mode in the HH and HV polarization channels"]
-[6.521740913391113, 5.609892845153809, "[FF] Data Rate of the DCS = Unknown"]
-[8.59186840057373, 1.295307993888855, "[TT] Calibration Stability Requirement of the Aquarius = 0.15 K over two days"]
-[4.940328598022461, 7.372954368591309, "[TT] Data Rate of the RF Communications = 9.6 kbit/s"]
-[5.618691444396973, -1.895050287246704, "[FF] Operation Duration of the KOMPSAT-2 = Until the mission end"]
-[8.106337547302246, -0.1348787546157837, "[FF] Impact of Climate Change of the Arctic = Increased occurrence of droughts and wildfires"]
-[5.984302520751953, 2.379765272140503, "[FF] First Launch of the Legion spacecraft = Early 2021"]
-[6.499682903289795, 0.01948278769850731, "[TT] Feasibility Analysis Frequency of the MUS = Daily"]
-[7.807182788848877, 0.5937279462814331, "[FF] DOI of the Near Earth Asteroid Scout = https://doi.org/10.2514/6.2014-4435"]
-[7.867109775543213, 2.1208722591400146, "[TT] Measurement Category of the FormoSat-1 = Ocean colour/biology"]
-[5.786933898925781, 3.7859697341918945, "[TT] Constellation Size of the Astrocast's Nanosatellites = 100 satellites"]
-[4.74642276763916, 2.177379608154297, "[TT] Vibration Test Completion Date of the Quantum = 2 March 2020"]
-[10.503612518310547, 6.893444538116455, "[TT] Diameter of the Secondary Mirror = 308 mm"]
-[3.641474485397339, 4.888949394226074, "[TT] Left or Right Looking Modes of the RADARSAT-2 = Available"]
-[5.190353870391846, 5.798412799835205, "[TT] Downlink Subsystem Interface of the Frame Grabber = Ethernet"]
-[14.0707426071167, 4.052928447723389, "[TT] Instrument Mass of the STOs and STAEs = 39.8 kg (for 3 STO configuration)"]
-[4.278969764709473, 1.5762639045715332, "[FF] Sensor Update Date of the ROCSat-1 = Unknown"]
-[5.87831449508667, 3.3013129234313965, "[TT] Number of SSEP Payloads on STS-134 and STS-135 missions of the Dragon C2/3 spacecraft = 2"]
-[5.042508125305176, 0.6519871950149536, "[FF] Asia-Pacific Region Service Start Date of the BDS = 2012"]
-[3.0954318046569824, 3.8927812576293945, "[TT] Launch Date of the NISAR = 2020"]
-[6.837100982666016, 4.412306308746338, "[FF] Not specified of the EXIS = Not specified"]
-[11.257246017456055, 2.807387590408325, "[TT] Mass of the Flock-2b nanosatellites = 5 kg"]
-[11.00523853302002, 6.215968608856201, "[TT] Coating of the Glass Layers = Depth-graded multilayers"]
-[8.056739807128906, 0.6961681842803955, "[FF] Reaching Unusually Low Levels of the Reservoirs, Lakes, and Streams = Yes"]
-[4.337286472320557, 7.0878119468688965, "[FF] Elements of the Ka-band experiments = Data rate capability, antenna gain, antenna pattern"]
-[8.022363662719727, 8.491755485534668, "[TT] Wavenumber of the Instrument = 4250\u20132630 cm -1"]
-[7.481086254119873, 4.743103981018066, "[FF] Orthorectification Requirement of the EROS-A PIC = Required"]
-[14.452725410461426, 6.558631420135498, "[TT] Battery Discharge of the Integral = Increased to more than six hours"]
-[9.181580543518066, 8.100139617919922, "[TT] Pixel Size of the LLNL imaging system = 6.7"]
-[8.572141647338867, 4.620039463043213, "[FF] Function of the STR CHU = Observes the stellar sky to resolve the inertial pointing of the spacecraft"]
-[10.130650520324707, -2.737788677215576, "[TT] Endurance of the SLC NAND-Flash = > 10 5 \u221e"]
-[5.025889873504639, 1.0697007179260254, "[FF] Telemetry Data of the Hitomi = Not Received"]
-[14.17929744720459, 3.2404592037200928, "[TT] Mass of the MBA = 418 kg"]
-[10.10246467590332, 3.1703169345855713, "[FF] Conference Presentation of the EDSN Intersatellite Communications Architecture = AIAA/USU Pre-Conference: CubeSat Developers' Workshop, Logan, Utah, USA, August 2-3, 2014"]
-[8.236064910888672, 8.34862232208252, "[TT] Sample Rate of the VNIR Detector = 4.8MHz"]
-[4.377598285675049, 7.127411365509033, "[TT] Command Communication Band of the SWFO-L1 = S-band"]
-[7.463836193084717, 3.688638687133789, "[FF] Usage of the NightPod = Aid in taking astronaut photos"]
-[11.447216033935547, 4.729683876037598, "[TT] Length of the Arm = 4 m"]
-[8.743033409118652, 2.5920250415802, "[FF] Measurement of the WINCS = Neutral winds and ion flows"]
-[7.113054275512695, -0.22258563339710236, "[TT] Number of MWR Orbits Gathered of the MWR = 65"]
-[8.048404693603516, 2.3506569862365723, "[FF] Usage of the MVIRI = Day/Night Cloud Coverage, Cloud Motion Winds, Cloud Top Heights, Upper Tropospheric Humidity, Precipitation and Sea Surface Temperature"]
-[6.668076992034912, 0.6073946356773376, "[TT] Launch Date of the Kepler = March 7, 2009"]
-[8.1329927444458, -1.024075984954834, "[FF] Application of the Lidar Instrument = Determine the seasonal cycle of ice sheet changes"]
-[5.249457359313965, -0.9988314509391785, "[TT] Launch Date of the Kolibri-2000 = 20 March 2002"]
-[11.677242279052734, 6.724545955657959, "[FF] Neutron Measurement of the SEDA-AP = Unknown"]
-[4.239400386810303, 2.257488489151001, "[TT] Launch Site of the GHGSat-D = Satish Dhawan Space Center (SDSC) in India"]
-[9.290549278259277, 2.1160643100738525, "[FF] Publication Date of the \"Discrete and broadband electron acceleration in Jupiter's powerful aurora\" = 7 September 2017"]
-[10.811403274536133, -0.26106199622154236, "[TT] Cumulated Absolute Height Error of the TanDEM-X = 3.5 m"]
-[6.764401435852051, -0.053815796971321106, "[FF] Observation Time of the Tycho = More than four centuries"]
-[5.511299133300781, 2.203254461288452, "[FF] Affiliation of the Dr Sara Mikaloff-Fletcher = NIWA"]
-[7.529963493347168, 1.3947290182113647, "[FF] Program of the ERS-l = Very similar to SeaSat"]
-[10.035416603088379, 2.924578905105591, "[TT] Release Date of the CubeSats = January 16, 2017"]
-[6.806446075439453, 4.467691898345947, "[FF] Location of the RCS Components = On one of the shear webs and the exterior surface of the triangular bottom deck"]
-[8.005732536315918, 4.160532474517822, "[TT] Thermal-Vacuum Testing Location of the AMS-02 = ESA's the LSS (Large Space Simulator)"]
-[7.533044815063477, 2.113041400909424, "[FF] Biomass Estimate Accuracy of the GEDI = Well-described uncertainty for its estimates using advanced statistical models"]
-[7.691170692443848, 5.885271072387695, "[FF] Methods of the Image Smearing Correction = Fast readout, binning, skipping rows outside the region of interest, post-processing"]
-[16.55227279663086, 3.6443028450012207, "[TT] Number of Satellites of the OneWeb = 648"]
-[9.266059875488281, 6.442048072814941, "[TT] Sight Axis Angle of the Spectrometer 2 = 30\u00b0 with the anti-nadir direction"]
-[6.212850570678711, 0.7615523338317871, "[FF] Data Publication Date of the Gaia = February 13, 2020"]
-[7.283028602600098, 3.766592502593994, "[TT] Number of Debris Pieces Produced of the DMSP-F13 = 43"]
-[8.981865882873535, 6.414195537567139, "[TT] Mounting Location of the CaSSIS = Mars-surface-facing side of the orbiter"]
-[3.2316129207611084, 1.8046693801879883, "[FF] Scheduled Launch Date of the Sentinel-6 Michael Freilich = Nov. 10"]
-[6.7927751541137695, -0.5762850046157837, "[TT] Orbital Period of the IBEX = 7.5 days"]
-[5.829469203948975, -0.7564325928688049, "[TT] Design Life of the Satellite = 1 year"]
-[9.8873291015625, 4.5144476890563965, "[FF] Control Method of the AOCS = Reaction wheels and magneto torquers"]
-[7.410140514373779, 6.1162638664245605, "[FF] Measurement Method of the Radar and laser altimeters = By measuring the time between the outgoing and returning signal, and knowing the precise altitude of the satellite above ground"]
-[8.858868598937988, -0.3118290305137634, "[TT] Inclination of the Meteor-M2-2 = 98.8\u00ba"]
-[5.749295234680176, 1.1200470924377441, "[TT] Development Status of the GeoXO = In progress"]
-[12.811532974243164, 2.0553159713745117, "[TT] FOV Azimuth of the SAGE-III = \u00b1 185\u00ba"]
-[5.670932292938232, -0.05068496987223625, "[FF] Mission Condition of the PROBA-V Mission = Excellent after six months of operations and one year after launch"]
-[9.391295433044434, 4.906833171844482, "[FF] Attitude Dynamics Analysis Presentation of the Aalto-1 = Oct. 1-5, 2012"]
-[9.007183074951172, 0.46125727891921997, "[FF] Orbit Raise Maneuver Sequence of the ARTEMIS = Maneuver the two spacecraft into the Earth-Moon Lagrangian points and eventually into lunar orbit"]
-[6.245844841003418, 4.613710880279541, "[FF] Function of the User Services = Allows end users to select which product they want to visualize or to download"]
-[5.597091197967529, 5.641430854797363, "[TT] Processor of the MPM = LEON2-E Sparc V8 processor"]
-[8.335686683654785, 7.087014675140381, "[TT] Pixel step period of the Full-scan Imaging = 0.112 s, 0.112 s"]
-[10.758173942565918, 3.9384028911590576, "[FF] Precision Formation Flight of the CanX-4 & CanX-5 = Demonstrated"]
-[6.004011154174805, 6.473855972290039, "[TT] Real-Time Data Delivery of the CATS = Less than six hours"]
-[7.427102565765381, 2.901688814163208, "[FF] Field of View of the MethaneSAT = Wider than a point-source system"]
-[11.353575706481934, 2.7841830253601074, "[TT] Mass of the BlackSky microsatellite = 56 kg"]
-[6.225834369659424, 5.789920806884766, "[TT] Component Type of the INMTX = Matrix"]
-[10.411569595336914, 5.830012321472168, "[TT] Operating Temperature of the Myriad RF board = -40\u00b0C to 85\u00b0C"]
-[8.084630012512207, 3.3159618377685547, "[FF] Rainfall Impact of the OCO-2 = More carbon being released into the atmosphere"]
-[8.199135780334473, 5.195992946624756, "[TT] Calibration Scheme of the In-flight Radiometric Calibration = Two points calibration"]
-[5.9307541847229, 2.4965555667877197, "[FF] Funding of the Euclid Consortium = National space agencies and national research organizations"]
-[6.3492584228515625, 3.0095415115356445, "[TT] Test Beam Incident Angles and Positions of the AMS-02 = Thousands"]
-[7.826539516448975, 2.020048141479492, "[FF] Objectives of the Seasat = Collect data on sea-surface winds, sea-surface temperatures, wave heights, ocean topography, internal waves, atmospheric water, and sea ice properties"]
-[10.672069549560547, -0.18407288193702698, "[TT] Number of Preliminary Geophysical Products of the Tandem-L = 26"]
-[4.733473777770996, 0.8577615022659302, "[TT] Announcement Date of the PROBA-V = 20 April 2020"]
-[4.19105339050293, 7.23887300491333, "[TT] Frequency Band of the X-band transmitter = X-band"]
-[12.124585151672363, 2.9818038940429688, "[TT] Thruster System of the ERG = Hydrazine"]
-[4.901789665222168, 1.0840846300125122, "[TT] Launch Year of the ALOS-1 = 2006"]
-[5.822163105010986, 1.0193684101104736, "[FF] Eclipse Observation Date of the PROBA-2 = Sept. 14, 2015"]
-[13.455215454101562, 2.8018083572387695, "[TT] Dry Mass of the Satellite = 270 kg"]
-[5.937156677246094, 4.737277984619141, "[TT] Performance of the Flight Software = Excellent"]
-[7.166177272796631, 1.861867070198059, "[TT] Launch Date of the CARBONITE-2 = January 12, 2018"]
-[14.617598533630371, 6.631906986236572, "[FF] Cargo of the Kounotori = Six new lithium-ion batteries and corresponding adapter plates"]
-[7.867950916290283, 3.558140993118286, "[FF] Main Goal of the NCLE = Registering the hydrogen line at different frequencies"]
-[7.51863431930542, 5.023141860961914, "[FF] Design Advantage of the PCM = Low internal disturbance, lightweight"]
-[5.251677989959717, 0.6043193936347961, "[TT] Mission Overview Date of the ICON = 3 Nov. 2017"]
-[5.909764766693115, 6.435560703277588, "[TT] Data Transmission of the CATS = Ongoing"]
-[5.2614240646362305, 3.234797477722168, "[TT] Manufacturer of the MPCV = Lockheed Martin"]
-[8.034124374389648, 4.254169940948486, "[TT] Testing Location of the ATLAS = Temperature-controlled vacuum chamber at Goddard"]
-[9.42960262298584, -1.704167366027832, "[TT] \u0394RAAN of the Swarm-A (Alpha) = 1.4\u00ba difference between A and B"]
-[5.189778804779053, 3.324099063873291, "[TT] Owner of the WorldView-1 = Maxar Technologies Inc."]
-[5.971334457397461, 4.699465751647949, "[TT] Original Design Application of the Sabertooth = Machine-learning"]
-[8.391359329223633, 1.2657498121261597, "[TT] Range Compression Gain of the RainCube = 26 dB"]
-[11.640542984008789, 3.7166032791137695, "[TT] Firing Duty Cycle of the Y-axis Bang-Bang Maneuver = 90%"]
-[5.768280506134033, 2.139308452606201, "[FF] Mission Status of the CBERS-4A = Unknown"]
-[9.973419189453125, -1.540879249572754, "[TT] Orbit Type of the CHORUS = Inclined"]
-[11.893963813781738, 5.084056377410889, "[TT] Size of the Rosetta Stone = 114.4 cm x 72.3 cm x 27.93 cm"]
-[9.617283821105957, 8.311005592346191, "[TT] FOV of the 16 mm camera = 6.9\u00ba x 5.336\u00ba"]
-[5.477688312530518, 7.013338088989258, "[TT] Data Transmission Rate of the AMS-02 = 4 Mbit/s"]
-[3.2889420986175537, 1.565900444984436, "[TT] Orbit Period of the Sentinel-2C = 100 minutes"]
-[9.548529624938965, 7.053219318389893, "[TT] Spatial Resolution of the SAM-II = 1 km (vertical)"]
-[10.417576789855957, 5.162208557128906, "[FF] Heaters Addition of the Valves = Under Consideration"]
-[4.514848709106445, 7.0265021324157715, "[FF] Design Approaches of the Q/V-bands = FMT(Fade Mitigation Technique), lower QoS (Quality of Service)"]
-[6.370007038116455, 4.820618629455566, "[FF] Function of the Monitor and Control System = Monitor and control ground station operations"]
-[10.157182693481445, 6.560381889343262, "[TT] Graze Angles of the Mirror = 1.3 - 4.7 mrad"]
-[5.608054161071777, 2.652958631515503, "[FF] Project Management of the Communication subsystem = Kagoshima University Soka University, Akita University"]
-[6.801239490509033, 7.536151885986328, "[TT] Beam width of the VIS (red) = 3.4 \u00b5rad"]
-[5.073474407196045, 4.042931079864502, "[TT] Manufacturer of the GPS Receiver = Surrey"]
-[13.430882453918457, 2.8946785926818848, "[TT] Mass of the Satellite = \u2264100 kg"]
-[5.0415825843811035, 2.821263074874878, "[TT] Location of the Science Operations Center (SOC) = Boston University (BU)"]
-[6.467685699462891, 2.0527524948120117, "[FF] Performance of the eROSITA = Demonstrated"]
-[7.847242832183838, -2.4762802124023438, "[TT] Measurement Domain of the GOLD = Atmosphere"]
-[6.546280384063721, -2.0026092529296875, "[FF] Development Start Date of the Jason-CS / Sentinel-6 = Late 2013"]
-[4.895454406738281, 0.6658715605735779, "[TT] Launch Date of the TEMPO = 2022"]
-[7.649706840515137, 7.997594833374023, "[TT] Sensitivity of the PMI = 0.3-0.5 K"]
-[9.548599243164062, 7.359333038330078, "[TT] Ground Resolution of the PAN = 1m"]
-[11.896116256713867, 3.1157002449035645, "[TT] Delta Velocity of the Steam Propulsion Unit = Up to 10 meter per second"]
-[5.6657209396362305, 6.863383769989014, "[TT] Data Size of the Telecommands = 62 bytes"]
-[7.950873851776123, 1.8750218152999878, "[FF] Level 4 Water use efficiency and evaporative stress index of the ECOSTRESS = 2 months after Level 3 data products are available"]
-[10.754972457885742, -0.17196932435035706, "[TT] Formation Flight Mode of the TanDEM-X = Close formation"]
-[8.297990798950195, 7.58546781539917, "[TT] Detector Systems of the Spectrometer = 7"]
-[6.169029235839844, 0.8571265935897827, "[TT] Observation Date of the NGC 1068 = August 2014"]
-[6.660142421722412, 8.768203735351562, "[FF] Single-Angle Polarization Reflectance Sensitivity Analysis of the Unknown = Unknown"]
-[4.993329048156738, 6.824485778808594, "[FF] Function of the Baseband Processor = Demodulation, storage and remodulation of LBR (Low Burst Rate) data"]
-[7.808224201202393, 5.845276832580566, "[TT] Type of the Imaging multi-spectral radiometers = Imaging multi-spectral radiometers (passive microwave)"]
-[5.7108473777771, -0.2929430603981018, "[TT] Separation Time of the EDRS-C = 33 minutes after liftoff"]
-[4.977965831756592, 0.5981835126876831, "[TT] Final Preparations Date of the ESAIL = 8 July 2019"]
-[12.020427703857422, 6.878396034240723, "[FF] Charge Range of the ULEIS = He through Ni"]
-[9.138726234436035, 7.462319850921631, "[TT] Camera Resolution of the PhoneSats = 5 Mpixel"]
-[7.984626293182373, 6.321749687194824, "[TT] Instrument Type of the RASAT VIS Multispectral = Imaging multi-spectral radiometers (vis/IR)"]
-[4.876138210296631, 0.9250534176826477, "[TT] Launch Year of the AMSU = 1998"]
-[6.223274230957031, 4.762972831726074, "[FF] Computer of the FCM (Flight Control Module) = GN&C flight software"]
-[7.577968597412109, 8.93175983428955, "[TT] Spectral Range of the Spectral Band C = 0.62 - 0.68 \u00b5m"]
-[14.520237922668457, 6.591048717498779, "[FF] Energy Storage of the Electric Power Subsystem = Lithium-ion batteries"]
-[4.798808574676514, 0.43021008372306824, "[TT] End of Mission Date of the CHAMP = September 19, 2010"]
-[9.181713104248047, 7.506647109985352, "[TT] VNIR Spatial Resolution of the iSIM-90 = 1.65 m"]
-[6.343443870544434, 4.386274814605713, "[FF] Status of the ADCS = Nominal operation"]
-[10.10006332397461, -1.5406084060668945, "[TT] Inclination of the Landsat-9 = 98.2\u00ba"]
-[6.166243076324463, 4.270770072937012, "[FF] Acquisition Planning follow-up of the CSK GS = Provide the S-IM with the planning of its acquisition requests"]
-[14.440564155578613, 6.514504432678223, "[TT] Battery Life of the AAUSat-1 = Two and a half months"]
-[5.441734790802002, 5.303880214691162, "[FF] Security of the QKD = Provable security against future hacks from advanced computers"]
-[7.778019428253174, 6.834187984466553, "[TT] Camera Exposures of the S-052 = 0.5, 1.5, and 4.5 seconds duration"]
-[11.0756254196167, 4.782549858093262, "[TT] Tether Length of the ATEx = 22 m"]
-[7.3193864822387695, 6.343826770782471, "[TT] Overpass Timing Prediction Accuracy of the ARC = Less than 1 second"]
-[8.234187126159668, 3.1014962196350098, "[FF] Purpose of the Spectrometer = Separation of atmospheric extinction along the line-of-sight due to Rayleigh scattering, aerosols, ozone, nitrogen dioxide, water vapor concentration profiles, and aerosol detection"]
-[7.192930698394775, 5.272322177886963, "[FF] Tracking Reliability of the CHOMPTT = Only reliable when the SLR facility is in darkness"]
-[6.384469985961914, 8.644070625305176, "[FF] Polarization Measurement of the Sentinel-5 = First three elements of the M\u00fcller matrix"]
-[7.729454040527344, 9.52823543548584, "[TT] Center Wavelength of the B3 = 560 nm"]
-[8.634871482849121, 5.663863658905029, "[TT] Pointing Accuracy of the Antenna = 0.1\u00ba"]
-[8.291369438171387, 7.5087809562683105, "[TT] Number of Lines of the CCDs = 576"]
-[10.119359970092773, -1.4840784072875977, "[TT] Orbit Inclination of the STARE Satellite = 98\u00ba"]
-[10.500375747680664, 7.348455429077148, "[TT] Covers an Area of the WFI = 620 x 180 km"]
-[5.752831935882568, 4.3620195388793945, "[FF] Operation of the EDRS = LEO-GEO OISL"]
-[11.102596282958984, 5.514770984649658, "[TT] Quantity of the Aluminum Spheres = 3"]
-[6.954286098480225, 3.2425010204315186, "[FF] Ground-Truth Characterization of the Oculus-ASR = Successful"]
-[10.013076782226562, -1.5267939567565918, "[TT] Orbital Inclination of the LDEF = 28.5\u00ba"]
-[9.301197052001953, 10.722981452941895, "[TT] Polarisation Mode of the IMI = Full-polarisation Full-polarisation for selected frequencies Full-polarisation"]
-[9.218343734741211, -1.1561691761016846, "[TT] Orbit of the GOES-S = Geostationary orbit of 35,786 km above Earth"]
-[13.443501472473145, 5.515089511871338, "[FF] Examples of Technologies of the CubeSats = Advanced multi-junction solar cells and carbon nanotube batteries"]
-[12.031501770019531, 4.582663536071777, "[TT] Dimensions, stowed of the General spacecraft parameters = 0.67 m W x 0.83 m L x 0.86 m H"]
-[5.011956691741943, 4.155401706695557, "[FF] Application of the Argos DCS = Environmental monitoring, Wildlife monitoring, Oceanography, Climatology"]
-[4.989816188812256, 3.20711350440979, "[TT] Provider of the LRR = GFZ Potsdam"]
-[4.893070697784424, 0.67854905128479, "[TT] Launch Date of the OCO-2 = July 2, 2014"]
-[8.243244171142578, 7.8549275398254395, "[TT] MWIR/TIR Detector Material of the GLI = CMT"]
-[5.169854164123535, 6.850546836853027, "[TT] Uplink Data Rate of the TRACE spacecraft = 2 kbit/s"]
-[6.803912162780762, 2.745300531387329, "[FF] Filming Locations of the UrtheCast\u2019s Proprietary HD Video Camera = More than 10 countries across four continents"]
-[10.14329719543457, 5.6838812828063965, "[TT] Operation Temperature of the Calibration Motor Home Sensor = Low temperatures"]
-[9.739328384399414, 7.301642894744873, "[TT] Image Scene Length of the Image scene length = 500 km"]
-[5.965686798095703, 3.2270774841308594, "[FF] Impact of the EMOC = Eliminated the need for the use of higher priority programming levels"]
-[3.0985517501831055, 1.786069393157959, "[TT] Global Coverage Time for Altimetry Observations of the Sentinel-3B = After completion of the reference ground track of 27 days"]
-[10.9517822265625, 4.540130615234375, "[TT] Drill Length of the Rosalind Franklin ExoMars rover = 2 m"]
-[5.852548122406006, -0.7993825674057007, "[TT] Years of the Spacecraft Design Life = 15 years (10 operational, after 5 years on-orbit spare)"]
-[7.183680057525635, 2.78448748588562, "[TT] Completion of CDR of the MethaneSAT = September 21, 2020"]
-[6.012779235839844, 6.85144567489624, "[TT] Data Storage of the ScaRaB = Up to 12 hours"]
-[1.7204210758209229, 6.138026237487793, "[TT] Cold Interstellar Gas Percentage of the Universe = 1.8 percent"]
-[14.590188026428223, 6.607850551605225, "[FF] Battery of the XI-IV = Manganese type lithium-ion battery"]
-[14.24129581451416, 3.151158094406128, "[TT] Mass of the ICEYE-X1 = <100 kg"]
-[11.229886054992676, 4.679344654083252, "[TT] Depth of the Great Blue Hole = About 123 m"]
-[6.900623321533203, 7.41650390625, "[TT] Width of the Multi-purpose beam mode = 530 km"]
-[11.361637115478516, 3.6305618286132812, "[FF] Neutralizer hollow-cathode activation of the ACTV_N = PS-6 on, high level"]
-[5.300285339355469, 4.598793983459473, "[FF] Hardware Platforms of the Open5GCore Rel. 4 = Common hardware platforms"]
-[8.15459156036377, -0.1659083515405655, "[TT] Period (min) of the Meteor-1-1 = 97.9"]
-[5.918638706207275, 1.596497654914856, "[FF] Workshop Date of the Small Satellite Platforms = Oct. 13-15, 2008"]
-[8.286467552185059, 1.8198809623718262, "[TT] Intersection Frequency of the ISS-RapidScat = Approximately every hour"]
-[10.135836601257324, 8.17164134979248, "[TT] Size of the Aperture = Slightly below 1 meter"]
-[5.899326801300049, 3.5154097080230713, "[FF] Cost-Benefit Analysis Factors of the Satellite = Fuel use, satellite destruction cost, collision probability"]
-[11.104551315307617, 5.968235015869141, "[TT] Shielding of the LDT = In first approximation, the same for all the floors in the rest of directions"]
-[3.7528769969940186, 4.958456039428711, "[TT] Multi-Look of the Non-Capella radar = 1"]
-[8.313949584960938, 7.369824409484863, "[TT] CCD Detector Stability of the CHEOPS = Stabilized within ~10 mK"]
-[8.323945999145508, 2.493089437484741, "[FF] Measurement Range of the Aerosol Index (AI) = -1 to +5"]
-[4.845288276672363, 1.8177849054336548, "[TT] End of Life Date of the HORYU-2 = Operational as of December 2022"]
-[9.40228271484375, 2.358093738555908, "[FF] Halos of the ISUAL = 6.00%"]
-[8.040669441223145, 1.651111364364624, "[FF] Radar Signature of Rain Falling on Water of the Radar = Article"]
-[7.905490875244141, 1.3474177122116089, "[FF] Purpose of the JUICE = Explore Callisto, Europa and Ganymede"]
-[5.821780204772949, 1.168511152267456, "[FF] Advisory Group Call Date of the EarthCARE = April 4, 2017"]
-[4.726335525512695, 0.9166145324707031, "[TT] Project Agreement Date of the YouthSat = January 25, 2007"]
-[13.464744567871094, 6.907407760620117, "[TT] Generating Capacity of the Power = 2.2 kW"]
-[7.075705051422119, 8.261103630065918, "[TT] SNR Saturation of the SCATSat-1 = 50%"]
-[8.92566204071045, 8.602788925170898, "[TT] Grating Angle of the UVS Instrument = 22.7\u00ba"]
-[6.542113304138184, -0.4834849536418915, "[TT] Period of the Yubileyniy-2/MiR = 115.8 minutes"]
-[11.733365058898926, 6.783830165863037, "[TT] Minimum Energy Threshold of the CID = Approximately 750 keV"]
-[8.201345443725586, -0.2768576443195343, "[FF] Melting Effect of the Ice = Earth re-adjusts and immediately rises by a few millimeters"]
-[10.12906551361084, 5.826038837432861, "[TT] Focal Plane Temperature of the GIIRS = Constantly low temperature"]
-[5.24173641204834, -0.320141077041626, "[TT] Maturity Prediction of the SPIDER = Five to ten years away from being fully matured"]
-[10.27017879486084, 5.735182285308838, "[TT] Thermosphere Temperature of the Instrument = Typically > 600 K"]
-[11.565728187561035, 3.6703872680664062, "[TT] Firing Durations of the IEPS = Three 3-minute firings, eighteen 10-minute firings"]
-[6.2190842628479, 2.6474595069885254, "[FF] Conference Presentation of the DoD Space Test Program = Barbara Manganis Braun, Sam Myers Sims, James McLeroy, Ben Brining, \"Breaking (Space) Barriers for 50 Years: Past, Present, and Future of the DoD Space Test Program,\" 31st Annual AIAA/USU Conference on Small Satellite, Logan UT, USA, Aug. 5-10, 2017"]
-[10.510472297668457, 7.453245639801025, "[TT] Swath Width of the ScanSAR-2 = 200 x 2500 km"]
-[5.395132541656494, 1.0295127630233765, "[FF] Launch Date of the LunaH-Map = Second half of 2021"]
-[5.659032344818115, 1.8482708930969238, "[FF] Durability of the LED = Confirmed"]
-[8.745405197143555, 6.34718132019043, "[TT] Backscatter Coefficient Measurement Accuracy of the Altimeter = \u00b1 1.0 dB"]
-[10.505959510803223, 1.4290547370910645, "[TT] Flash Brightness of the OJ 287 galaxy = Brighter than a trillion stars"]
-[8.179006576538086, 2.4793689250946045, "[FF] Objective of the ISIR = Measurement of the infrared brightness temperature of cloud tops as well as the Earth's surface"]
-[4.870550632476807, 0.5749229788780212, "[TT] Launch Date of the ExoMars = September 2022"]
-[4.146026611328125, 0.1884775161743164, "[TT] Launch Date of the Falcon 9 = Early 2018"]
-[8.36937141418457, 6.729895114898682, "[TT] Imaging Capacity of the Satellite = 2.5 x 10^6 km^2 / day"]
-[7.089621543884277, 8.09976577758789, "[TT] Signal-to-Noise Ratio of the AEISS = > 100"]
-[9.488874435424805, 7.2187676429748535, "[TT] Spatial Resolution of the TanDEM-X = 0.4 arcseconds (12 m at the equator)"]
-[10.94436264038086, 7.553104400634766, "[TT] Limited Swath of the QLP/NRTP = 4096 range gates, 15-240 km in width"]
-[7.997917175292969, -0.3162102699279785, "[FF] Weather Pattern of the Greenland = Unusually cold and snowy in 2017 and 2018"]
-[8.014859199523926, 5.713834762573242, "[FF] Measurement Rate of the SPAN Sensors = Constant"]
-[5.842845916748047, 6.299020767211914, "[TT] Storage Capacity of the SSR = 4 Tbit @ BOL"]
-[12.10882568359375, 3.1981911659240723, "[TT] Number of Propellant Tanks of the XMM-Newton = 4"]
-[13.347434997558594, 5.551657199859619, "[TT] Quantity of the ISS Roll-out Solar Arrays (iROSA) = Six"]
-[9.040107727050781, 4.974319934844971, "[FF] Orbit Control Maneuvers of the AlSat-2A = 10 regular station keeping OCM performed for ground track corrections and 2 OCMs were performed as emergency collision avoidance maneuvers"]
-[7.550990581512451, 7.402079105377197, "[TT] Digitization of the Camera Electronics = 10 bits"]
-[3.938697099685669, 9.713830947875977, "[TT] Frequency (GHz) of the ICI-3 = 183.31\u00b12.0"]
-[5.5279221534729, 5.537885665893555, "[TT] Microprocessor of the Beresheet lander = GR712RC"]
-[3.8901660442352295, 2.0324926376342773, "[TT] Launch Vehicle of the Meteor-M2 spacecraft = Soyuz-2.1b/Fregat"]
-[5.389320373535156, 0.5961293578147888, "[TT] Launch Date of the Terra = February 1999"]
-[8.62045669555664, 8.073821067810059, "[TT] Spectral Resolution (5-30 keV) of the Detector = 500 eV FWHM"]
-[4.701288223266602, 1.6052385568618774, "[TT] IAC Presentation Date of the HaloSat = 21-25 October 2019"]
-[8.784906387329102, 7.104706764221191, "[TT] Image Capture of the Rosetta = 76,000 high-resolution images"]
-[9.699860572814941, 8.032870292663574, "[FF] Optics of the Instrument = f/0.73, 50 mm focal length, 68 mm diameter"]
-[4.162672519683838, 4.2569684982299805, "[FF] Participating Countries and Organizations of the COSPAS-SARSAT = Canada (CRC), France (CNES), Russia (ROSHYDROMET), and the USA (NOAA)"]
-[5.395639896392822, 2.70617938041687, "[TT] Responsible Organization of the Operational and Precise Orbits = Goddard Space Flight Center"]
-[6.078568458557129, 2.117422103881836, "[FF] URL of the Orion spacecraft = http://www.nasa.gov/exploration/systems/mpcv/test_flight_2014.html#.UyqgYM52H5p"]
-[5.57427978515625, 0.5393531918525696, "[TT] Observation Date of the ENVISAT satellite = 2006"]
-[9.383301734924316, 5.7081146240234375, "[FF] Actuation of the Rotary Stage = Non-linear rotation of the camera to compensate for the ISS orbital motion"]
-[4.2448811531066895, 7.412405014038086, "[TT] Downlink Frequency of the GRB = L-band"]
-[11.713788986206055, 0.1306656450033188, "[TT] Number of Transiting Exoplanet Candidates of the TESS = More than 1,500"]
-[4.026883602142334, 2.1873834133148193, "[TT] Launch Vehicle of the CubeSat - Launch 4 = Dnepr"]
-[3.377612590789795, 4.972441673278809, "[TT] L0 and L1A Processing Time of the SAR = About 3 days"]
-[8.515132904052734, 5.367273330688477, "[TT] Radial Accuracy of the Orbits = 2.5 cm"]
-[10.15286922454834, 5.732691764831543, "[TT] Detector Temperature of the Ricor Cryocooler = Below 120 K"]
-[8.802974700927734, 4.724973201751709, "[FF] Pointing Modes of the TanSat = Principal plane nadir, Sun-glint pointing, Forward nadir, Backward nadir, Target pointing, Area steering, Direct solar pointing, Diffusion solar pointing, Moon pointing, Solar panel pointing, Attitude slew"]
-[7.4014434814453125, 0.7628452181816101, "[FF] Operation Status of the China's Moon Rover = Awaken"]
-[7.063162803649902, 8.274740219116211, "[TT] SNR of the COCTS = 995"]
-[7.480433940887451, 8.368663787841797, "[TT] Number of Occluded Rows per Filter Band of the QWIP Array = 76"]
-[5.161725997924805, 5.679409503936768, "[FF] Function of the TTC Rx = Acquire the residual carrier from the ground station and extract the 16 kHz subcarrier for the telecommand demodulator inside the CCSDS processor"]
-[8.229640007019043, 4.97714376449585, "[FF] Purpose of the Gallium Black Bodies = Track the long-term degradation of the radiometer sensors"]
-[5.399991989135742, 4.524049758911133, "[TT] Configuration of the Corvus-BC = 10 satellites"]
-[5.444631099700928, 6.838346481323242, "[FF] Peak Detection Rate of the Simple Receiver = Not tabulated"]
-[9.670613288879395, 4.109701156616211, "[FF] Components of the ULF Sensor = Search coil, calibration coil, amplifier/filter circuit"]
-[12.214066505432129, 3.2445929050445557, "[TT] Propulsion System Capacity of the ESPA Ring = 344 kg"]
-[6.37298583984375, 8.412030220031738, "[TT] Channels of the PolaRx2 = 9"]
-[9.254972457885742, 1.8653883934020996, "[FF] Purpose of the HARP-2 = Improve OCI measurements"]
-[9.745129585266113, 0.7371748089790344, "[TT] Closest Approach to Earth of the Bennu = Every 6 years"]
-[10.958494186401367, 0.8725540041923523, "[TT] Spacecraft Separation of the LISA = 2.5 million kilometers"]
-[3.6746914386749268, 6.510322570800781, "[TT] Reflector Type of the Antenna Subsystem = 1m parabolic dish"]
-[3.971031665802002, 4.420496463775635, "[FF] Plan of the USA = Incorporate Canada-supplied L-band SAR repeaters on 24 GPS satellites"]
-[3.8384134769439697, 3.3852267265319824, "[TT] Launch Date of the Galileo FOC satellites = 22 August 2014"]
-[8.667821884155273, 4.6317219734191895, "[FF] Configuration of the Star Sensors = Hot redundant, cross-strapped"]
-[10.905016899108887, 7.262132167816162, "[TT] Width of the Dimorphos = 160 meters"]
-[6.356193542480469, 2.723083019256592, "[FF] Testbed of the International Space Station = Perfect testbed for those that are new to space and to those that have a long history in orbit"]
-[13.441314697265625, 7.346159934997559, "[TT] Power of the XRD = 0.45 W"]
-[8.5576753616333, 6.574092864990234, "[TT] Post-facto baseline reconstruction accuracy of the TDX/TSX = 1 mm"]
-[5.11610746383667, 4.328787803649902, "[TT] Number of Orbited Satellites since May of the Starlink = 420"]
-[8.286396026611328, 8.536386489868164, "[TT] FPA Cutoff of the HyperCube Instrument = 9.5 \u00b5m"]
-[4.979313373565674, 1.6538892984390259, "[TT] Reconnaissance Missions of the Gokturk-2 = Over 4800"]
-[5.342779636383057, 0.7547963261604309, "[TT] Planned Operation Date of the METimage = 2021"]
-[16.481788635253906, 3.6153721809387207, "[FF] User Terminals Contract Value of the OneWeb = $73 million"]
-[11.759634017944336, 6.628443241119385, "[TT] Energy Range of the Helium spectrum = 2 GV to 3 TV"]
-[5.186165809631348, 4.08005952835083, "[TT] Number of GPS II satellites of the MEOSAR satellite constellation = 16"]
-[10.524429321289062, 2.33082914352417, "[FF] Integration of the X-ray photon = Not conducted on the spacecraft"]
-[13.782825469970703, 5.3541083335876465, "[TT] Solar Cell Type of the EPS = Triple junction solar cells (GaInP 2 /GaAs/Ge)"]
-[8.985993385314941, 8.549422264099121, "[TT] Band 2 Wavelength Range of the Telescope = 1.55 - 1.70 \u00b5m"]
-[14.245234489440918, 3.2704296112060547, "[TT] Mass of the EXIS = 30 kg"]
-[7.0670623779296875, 4.637840747833252, "[TT] Mounting Location of the CEASE = Exterior panel of the payload module"]
-[5.121323585510254, 1.6922358274459839, "[TT] Testing Status of the Pathfinder 2 = In the process of final testing and checkout"]
-[7.793117523193359, 5.865085124969482, "[TT] Type of the SMMR = Scanning Multichannel Microwave Radiometer"]
-[3.4286892414093018, 6.3532490730285645, "[TT] Dish Size of the NASA Wallops field = 18.29 m"]
-[4.5015869140625, 7.746032238006592, "[TT] Transmit power of the Uplink (VHF) = 50 W"]
-[7.645414352416992, 4.201810359954834, "[FF] Transfer Phase End of the LUMIO = Halo Injection Maneuver"]
-[10.380025863647461, 4.49700927734375, "[TT] Quantity of the Reaction Wheels = 3"]
-[8.124197006225586, 3.037374496459961, "[FF] Measurement Components of the LI System = IC (Intra Cloud) and CG (Cloud Ground)"]
-[5.722516059875488, 6.29795503616333, "[FF] Data Recording Capacity of the ODR = High-speed, large-volume data recorder"]
-[13.875829696655273, 7.194453239440918, "[TT] Power of the Voltage 2 = 0.055"]
-[7.9337382316589355, 8.43847370147705, "[TT] Wavelength Bands of the VHRR/2 = Visible, shortwave infrared, middle infrared, water vapor and two bands in thermal infrared"]
-[8.611557960510254, 4.855705738067627, "[TT] Observation Mode of the TanSat = Nadir observation mode"]
-[9.644669532775879, 0.1307302564382553, "[TT] Parachute Manufacturer of the ExoMars mission = Airborne Systems"]
-[7.805478572845459, 3.0478341579437256, "[FF] Purpose of the GeoCarb = Distinguish between man-made and natural emissions"]
-[5.766803741455078, 3.0615901947021484, "[FF] BAA Framework Name of the NRO = Framework for Strategic Commercial Enhancements"]
-[3.2854878902435303, 5.242468357086182, "[TT] Imaging Mode Delay Time of the SAR Antenna = 10 ms"]
-[11.197294235229492, 5.976080417633057, "[TT] Material of the Titanium Mandrel = Titanium"]
-[5.013964653015137, 4.329171657562256, "[TT] Preorder Count of the Starlink = Over 750,000"]
-[5.96772575378418, 5.546632766723633, "[FF] Function of the Control Center = Downloaded files collected and stored by pass for later analysis"]
-[12.054883003234863, 6.389458179473877, "[TT] Interaction with Matter of the Neutrinos = Incredibly rarely"]
-[5.571983814239502, 5.984722137451172, "[TT] Programming Space of the SCP = 64K words"]
-[7.029539585113525, -0.796967625617981, "[TT] Orbital Period of the TOI 2076 b = 10 days"]
-[6.153729438781738, 0.4572932720184326, "[TT] Mission Extension of the Megha-Tropiques = 2 years"]
-[7.561697483062744, 3.0035762786865234, "[TT] Methane Detection Sensitivity of the Imaging Spectrometer = 3 parts per billion"]
-[6.665438652038574, 0.7754579186439514, "[FF] Online Publication Date of the Herschel and Planck = 12 September 2019"]
-[9.558003425598145, 8.197938919067383, "[TT] Pixel IFOV of the Full-scan Imaging = 10 km x 10 km"]
-[9.690583229064941, 1.4228075742721558, "[TT] Number of Satellites of the Pl\u00e9iades Neo = 4"]
-[9.875285148620605, 2.452847719192505, "[FF] Light Blocking of the 55 Cancri e = 0.04% of its host star's light"]
-[8.117574691772461, -1.01852548122406, "[FF] Mission Goal of the ICESat-2 = Provide high-quality topographic measurements for estimating ice sheet volume change"]
-[5.8267316818237305, 5.156020164489746, "[TT] Design of the ECS = Highly generalized"]
-[6.27490234375, 3.082439661026001, "[FF] Revisit Times of the BlackSky Events = Very short"]
-[6.6100945472717285, 6.674156188964844, "[TT] Laser Terminal Type of the EDRS-A = Autonomous state-of-the-art telescope"]
-[4.557001113891602, 0.15918418765068054, "[FF] Delay Date of the Soyuz/Fregat = Sept. 27, 2013"]
-[6.892387866973877, 3.469289779663086, "[FF] 10-day Global Syntheses of the PROBA-V = 6"]
-[8.42149829864502, 2.116957426071167, "[FF] Mission Objectives of the WSF-M = Address three critical SBEM gaps: ocean surface vector winds, tropical cyclone intensity, and LEO energetic charged particle characterization"]
-[4.623232364654541, 0.5951640605926514, "[TT] Integration Date of the Mynaric\u2019s CONDOR Mk3 = 2022"]
-[5.019035339355469, 3.4136898517608643, "[TT] Manufacturer of the MCU = Texas Instruments"]
-[7.69273042678833, 7.022407531738281, "[FF] CCD Well Depth of the GLM = Unknown"]
-[8.710467338562012, 8.834115982055664, "[TT] Flatness of the Grating = 1 \u03bb (634.8 nm)"]
-[10.963327407836914, 5.593388080596924, "[TT] Thickness of the Heat Shield = 1.6 inches"]
-[13.374632835388184, 7.65494441986084, "[TT] Power Output of the Antenna System = 37.8 W"]
-[4.32127046585083, 2.4538323879241943, "[TT] Manufacturer of the ATLAS = NASA"]
-[7.617441177368164, 4.910524368286133, "[FF] Importance of the Stepper Motor = Mission critical part"]
-[5.537715911865234, 5.110311508178711, "[FF] Software of the TriTel CPU = CAN communication protocol"]
-[7.977409839630127, 0.8669167757034302, "[FF] Date of the \"Drought in the Northern Great Plains\" = 19 October 2021"]
-[11.469322204589844, 3.3667404651641846, "[FF] Propulsion System of the New Horizons = Small thrusters"]
-[4.155137062072754, 5.791594982147217, "[TT] ADS-B Messages Received of the Aireon = 6,935"]
-[7.677574634552002, 0.5525522828102112, "[FF] URL of the NASA Mission = http://www.nasa.gov/content/goddard/new-nasa-mission-to-help-us-learn-how-to-mine-asteroids/#.U4s2hXbwUkA"]
-[4.256813049316406, 2.5680246353149414, "[TT] Launch Site of the CADRE nanosatellite = SLC-41 (Space Launch Complex-41) at CCAFS (Cape Canaveral Air Force Station), FL"]
-[8.450067520141602, 5.541463375091553, "[TT] Localization Accuracy of the Satellite = 4.4 km"]
-[8.110129356384277, -1.2033008337020874, "[FF] Highest-resolution laser altimeter of the ICESat-2 = Yes"]
-[9.304316520690918, -0.3302064836025238, "[TT] Perigee of the BUV = 1092 km"]
-[6.037206649780273, 7.028875350952148, "[TT] Quantity of the Rate Measurement Unit = 1"]
-[14.592402458190918, 6.601784706115723, "[TT] Battery Type of the GHGSat-D = Li-Ion"]
-[7.189576625823975, 8.5869140625, "[TT] Spectral Channel 2 of the Satellite = 0.61-0.69 \u00b5m"]
-[5.494165420532227, 0.6519750356674194, "[TT] Last ?V Maneuver Date of the Satellite = July 8, 2014"]
-[6.968425750732422, 4.168961048126221, "[TT] Loss of Attitude Control of the DMSP F-19 = Predicted to occur late next month"]
-[9.571669578552246, 9.196247100830078, "[TT] Eclipse Operation of the IRIS = Not operated for 4 months"]
-[9.080410957336426, 3.935257911682129, "[FF] Mounting of the Sun-shade = Optical element"]
-[4.923561096191406, 3.3036534786224365, "[TT] Manufacturer of the ABI instrument = ITT Industries"]
-[1.3160320520401, 1.8997150659561157, "[TT] Supplies Capacity of the HTV = Up to 6,000 kg"]
-[8.662936210632324, 6.09124755859375, "[TT] Accuracy of the GaAs cells = 0.2\u00ba"]
-[8.98605728149414, 4.409394264221191, "[TT] SPSS of the AOCS = Solar Panel Sun Sensor"]
-[9.191804885864258, 7.498297214508057, "[TT] Panchromatic Resolution of the SuperView 1A and 1B = 0.5 m"]
-[4.564030647277832, 1.4880753755569458, "[TT] Launch Date of the Alphasat = July 25, 2013"]
-[6.220925807952881, 6.008204936981201, "[TT] Performance of the FACT = Fine"]
-[5.078869819641113, 5.087607383728027, "[TT] Quantity of the GPS Receiver = 2"]
-[8.698105812072754, 5.866382598876953, "[TT] Co-Alignment of the OSIRIS = With a reference spot in the measurement devices"]
-[12.724270820617676, 3.905190944671631, "[FF] Nature of the Magnetopause Reconnection = Bursty or pulsed"]
-[5.492711067199707, 1.2262758016586304, "[FF] Conference Presentation Date of the EO-1 = June 22-24, 2004"]
-[6.424214839935303, -0.40754038095474243, "[TT] Total Hours of the Total = 12405.95"]
-[9.855438232421875, 4.903069496154785, "[TT] Rotation Rate of the Antenna = 14.6 rpm"]
-[6.6786041259765625, 0.7686124444007874, "[FF] Discovery Date of the Herschel = November 27, 2017"]
-[7.048484802246094, 4.377523899078369, "[FF] Experiment of the CNES = Automatic spacecraft maneuver planning and collision prediction in space"]
-[9.907387733459473, -0.4786120653152466, "[TT] Altitude of the SkySat-16 to -18 = 575 km"]
-[4.388067245483398, 4.116328239440918, "[FF] Purpose of the Jamming and Spoofing Protection Mechanisms = Safeguard Galileo signals"]
-[5.158534526824951, -0.10948940366506577, "[TT] Time Laboratories of the Coordinated Universal Time (UTC) = About 90"]
-[7.678863048553467, 8.957531929016113, "[TT] Spectral Range (\u00b5m) of the Band 3 = 3.55 - 3.93"]
-[10.721512794494629, 5.366219997406006, "[TT] Scattered Emission Energy of the CuPID = 10.2 eV"]
-[7.458049297332764, 4.288825511932373, "[FF] Information Source of the Sensor Complement = Herbert J. Kramer"]
-[7.868954658508301, 9.112164497375488, "[TT] Wavelength of the PH1 = 260 nm"]
-[8.418149948120117, 2.0421438217163086, "[TT] Achieved Accuracy of the SSH (Sea Surface Height) = 4.3 cm"]
-[7.0130109786987305, 7.168623447418213, "[TT] Beam Divergence of the Micropulse Laser Transmitter = 20 \u00b5rad"]
-[11.87819766998291, 3.0662214756011963, "[TT] \u0394V of the RemoveSat = Up to 6 m/s"]
-[7.455968379974365, 2.4318041801452637, "[FF] Data Usage of the BIRD = Measurements of vegetation, albedo and reflectance, surface temperature on land, and multi-purpose imagery"]
-[13.495976448059082, 5.4475812911987305, "[TT] Solar Cell Quantity of the TUBSAT-N = 34 cells per string"]
-[8.3120698928833, 7.796520233154297, "[TT] Detector Type of the BIRCHES instrument = Teledyne H1RG HgCdTe FPA"]
-[4.649863243103027, 5.4905686378479, "[TT] Alert Method of the JAC = Email"]
-[5.915621757507324, -0.3900509178638458, "[TT] Operation Duration of the STRV-1b = 4 years"]
-[14.03931999206543, 6.327245712280273, "[TT] FRAM of the GomSpace NanoMind A3200 = 32 kB"]
-[8.638422012329102, 7.705524921417236, "[TT] Pixel Count of the Detector = 1024 x 1024"]
-[5.357941150665283, 2.8523192405700684, "[FF] Program Partners of the SloshSat-FLEVO = ESA, the (Dutch) Ministry of Economic Affairs, NIVR (Netherlands Agency for Aerospace Programs), and NRL (National Aerospace Laboratory)"]
-[10.9662446975708, 0.8804550766944885, "[TT] Distance to LPF of the LISA = 50 million km"]
-[9.888516426086426, 4.187781810760498, "[TT] Operation of the ULF Sensor = Continuous"]
-[9.045317649841309, -0.8107737898826599, "[TT] Spacecraft of the Orbital ATK = Cygnus"]
-[4.389159202575684, 7.823999404907227, "[TT] Downlink Frequency of the RF Communications = UHF (436 MHz)"]
-[5.448668003082275, 3.8845906257629395, "[TT] Number of Satellites of the Planet SkySats = 21"]
-[5.893016338348389, 5.064844131469727, "[FF] Conference Presentation Date of the ROSA Radio-Occultation Receiver = Dec. 8-10, 2010"]
-[18.802715301513672, 3.4758336544036865, "[TT] Mean \u0394N (m) of the Dobbins = -12.5"]
-[10.281675338745117, 3.1720821857452393, "[TT] Deployment Type of the CubeSat = Doublewide"]
-[8.441054344177246, 5.522426605224609, "[TT] Relative Geometric Accuracy of the GCP Extraction Approach = 10 m RMSE"]
-[8.208823204040527, 8.833456993103027, "[TT] Spectral Resolution of the MAHRSI = 0.026 nm at 215 nm"]
-[5.491004943847656, -0.027391444891691208, "[FF] Presentation Date of the RapidEye = Sept. 29 to Oct. 3, 2008"]
-[10.666460990905762, 2.087390661239624, "[TT] Operation Start Date of the NICER X-ray telescope = June 2017"]
-[6.417062282562256, -0.44874367117881775, "[TT] Forecast Duration of the HWRF = 24 hours"]
-[9.384852409362793, 7.621644020080566, "[TT] Width at 1000 km distance of the LWIR Camera = About 17.5 km"]
-[9.616347312927246, 4.809774398803711, "[TT] Stabilization of the Spacecraft = 3-axis stabilized"]
-[9.46925163269043, 4.992489337921143, "[TT] Roll-Tilt Angle of the Spacecraft = \u00b1 34\u00ba"]
-[2.4139397144317627, 1.2582721710205078, "[FF] Orbit Operations Duration of the Canadian Advanced Nanospace Experiment 2 = Two Years"]
-[6.53730583190918, 3.096001148223877, "[FF] Objective of the HJ-1 minisatellite constellation = Establish an operational Earth observing system for disaster monitoring and mitigation using remote sensing technology and to improve the efficiency of disaster mitigation and relief"]
-[8.989301681518555, 5.847978591918945, "[TT] Pointing Range of the HSC-III = > 5\u00ba /s"]
-[10.87509822845459, 7.503816604614258, "[TT] Swath Width of the TOMS = 2795 km"]
-[7.690412998199463, 7.145369529724121, "[TT] Stability of the Satnav Signals = Highly stable"]
-[9.224435806274414, 10.64567756652832, "[TT] Polarization Observation Data of the CAPI = 0.67 \u00b5m and 1.64 \u00b5m in three angles"]
-[7.47750997543335, 3.764835834503174, "[FF] Compatible Physical Lengths of the NightPod = Unknown"]
-[11.524391174316406, 3.4633426666259766, "[TT] Propulsion System of the CanX-2 = Custom cold-gas"]
-[10.01622200012207, -1.5193169116973877, "[TT] Orbit Inclination of the GPM Core spacecraft = 65\u00ba"]
-[8.4847993850708, 1.5961729288101196, "[TT] Radiometer Type of the Aquarius = Pushbroom-type polarimetric microwave radiometer in L-band"]
-[4.426042079925537, 1.3110826015472412, "[FF] Launch Date of the SEOSat = Unknown"]
-[3.1822242736816406, 2.3412394523620605, "[FF] Objective of the Algorithm Development & Data Processing = Develop and validate new algorithms relevant for coral reef monitoring based on Sentinel-2 observations"]
-[14.229185104370117, 2.9430809020996094, "[TT] Mass of the KAUSAT-5 = 4 kg"]
-[8.787826538085938, 4.7753143310546875, "[TT] Size of the BOKZ-M star tracker = 37 cm x 23 cm x 23 cm"]
-[5.173073768615723, 2.3950486183166504, "[TT] Mission Type of the SMART = Non-EO"]
-[4.56270170211792, -2.7971606254577637, "[TT] Frequency (GHz) of the PMI = 6.8/7.2"]
-[4.636717319488525, 0.8291724920272827, "[TT] Operational Date of the FY-4A = May.8, 2018"]
-[6.1073198318481445, -0.5222201347351074, "[TT] Mission Duration of the LADEE spacecraft = ~160 days"]
-[6.794033527374268, 5.848387718200684, "[TT] Quantity of the CM1 and CM2 = 2"]
-[4.8398261070251465, 0.07702457904815674, "[TT] End of Life Date of the SpaceX CRS-19 = 7 January 2020"]
-[13.516593933105469, 6.468568325042725, "[TT] Generation Voltage of the HORYU-2 = Above 300 V"]
-[7.864211559295654, 0.990090548992157, "[FF] Gravity Experiment of the Kaguya (SELENE) = Four-Way Doppler Measurement"]
-[8.065600395202637, 8.59384536743164, "[TT] Range of the Spectral Range (VNIR) = 400-1000 nm"]
-[11.735593795776367, 4.699533462524414, "[TT] Shape of the UniSat-3 = Octagonal prism"]
-[9.972633361816406, 2.748295307159424, "[FF] Role of the NanoRacks = Launch integration and deployment partner for the QB50 CubeSat Constellation Mission"]
-[6.162389755249023, -0.4096969962120056, "[TT] On-Orbit Duration of the CanX-4 = More than one year"]
-[5.198410511016846, 6.984842777252197, "[TT] Options of the Downlink data rates = 24, 48, or 96 kbit/s"]
-[8.364068031311035, 3.169372320175171, "[FF] Objectives of the ACE-FTS = Measure the vertical distribution of atmospheric trace gases, in particular the regional ozone budget, as well as temperature and pressure"]
-[5.456698417663574, -0.5821771025657654, "[TT] Wake Up Time of the Yutu-2 = 1:45 p.m. Sunday"]
-[5.980539321899414, 8.674737930297852, "[FF] Modulation Transfer Function of the MTF = Pan: 8%, MS: 15%"]
-[11.46308422088623, 4.883234024047852, "[TT] Diameter of the Holes = 60-centimeter"]
-[7.764569282531738, 1.8768199682235718, "[FF] Effect on Pteropods of the Ocean Acidification = Shell damage has been observed"]
-[9.806256294250488, 2.7205917835235596, "[FF] Manufacturer of the NanoRacks Airlock Module = NanoRacks"]
-[5.3755059242248535, 3.16872239112854, "[TT] Host of the Bartolomeo = ESA"]
-[8.363208770751953, 0.5550939440727234, "[FF] Purpose of the OLA = Provide high accuracy range data of Bennu for navigation and long-range scans of the asteroid surface to establish the shape and model the gravity of Bennu"]
-[3.8554270267486572, 4.513668537139893, "[TT] Acquisition Success Rate of the RADARSAT-2 = Above 98%"]
-[6.459903717041016, 0.6186590790748596, "[TT] Launch Date of the Landsat 9 = 16 September 2021"]
-[5.925362586975098, 1.5595691204071045, "[FF] Presentation Date of the CMC Windward TPS and Nose of the IXV Vehicle = Oct.12-16, 2015"]
-[8.523353576660156, 7.698263168334961, "[TT] Detector Line Array of the SLIM6 = 10,000 silicon element cells in cross-track"]
-[7.01006555557251, 6.952319622039795, "[TT] Confidence Level of the IRS Sounder = 68.26%"]
-[4.805967330932617, 8.222975730895996, "[TT] Frequency of the RA-1 = 13.8 GHz"]
-[8.243712425231934, 8.893229484558105, "[TT] Wavelengths of the Telescope = Fe XIV 530.3 nm; He I 587.6 nm"]
-[6.248013973236084, 0.4966951906681061, "[FF] Development Status of the FormoSat-5 = In process of developing"]
-[7.997939109802246, 5.413896560668945, "[FF] Function of the Sensor Aperture = Allows a significant fraction of the ENAs to pass"]
-[5.427425861358643, -0.1355888396501541, "[TT] Test Results of the TSUBAME = Successful"]
-[13.375256538391113, 6.841614723205566, "[FF] Expected Electrical Power Levels of the GSE Power Supplies = Not provided"]
-[13.296000480651855, 2.9458844661712646, "[TT] Launch Mass of the GHGSat-D = 15 kg"]
-[7.571250915527344, 1.2488679885864258, "[FF] Proposal Date of the Surface Water and Ocean Topography (SWOT) = Sept. 24-29, 2012"]
-[13.375572204589844, 6.9569993019104, "[TT] Payload Power of the RemoveSat = 8 W"]
-[5.141769886016846, 2.927398920059204, "[TT] Provider of the MetOp-A = EUMETSAT"]
-[9.451104164123535, 3.9103634357452393, "[FF] Parameter of the Experimental Magnetic Sensor (MI) = Value"]
-[11.53084659576416, 5.0169830322265625, "[TT] Size of the ASPIICS = ~1.5 m"]
-[4.4604034423828125, 0.7722022533416748, "[TT] Launch Date of the HySIS = 29 November 2018"]
-[8.648120880126953, -0.5933340787887573, "[TT] Data Delivery of the ICEYE = Near real-time"]
-[10.92626953125, 5.637030601501465, "[FF] Coatings of the EIRSAT-1 = Protective oxide coatings"]
-[10.824959754943848, 0.9923416376113892, "[TT] Classification of the TOI-148, TOI-587, TOI-681, TOI-746, TOI-1213 = Borderline between brown dwarfs and stars"]
-[5.958637714385986, 0.967483401298523, "[TT] Start of Full-Scale Simulations of the BepiColombo = May 28, 2018"]
-[8.334739685058594, 8.285137176513672, "[TT] Detector Element Spacing of the VNIR FPA = 12 \u00b5m"]
-[9.991214752197266, -1.3051443099975586, "[TT] Orbit Inclination of the SAC-D/Aquarius = 98\u00ba"]
-[9.437762260437012, 5.989985942840576, "[TT] Angle Measurements of the TED = 0\u00ba and 30\u00ba from the local vertical"]
-[10.8829345703125, 7.499238014221191, "[TT] Swath Width on the Ground of the OLS = 2960 km"]
-[6.491201400756836, -0.7056676149368286, "[TT] Revisit Period of the RISAT-1 = 25 days"]
-[5.7550811767578125, 4.658349990844727, "[TT] Purpose of the HADR = Examined trade-offs for different ADR technologies, especially including flexible link capture systems"]
-[8.56113338470459, 7.771218299865723, "[TT] Correction Scheme of the CGI = Pairwise probing and electric field conjugation"]
-[10.415603637695312, 6.85137414932251, "[TT] Number of Mirrors of the Shafer Telescope = 5"]
-[13.750714302062988, 2.90012788772583, "[TT] Mass of the Spacecraft = 2290 kg"]
-[13.21553897857666, 7.230873107910156, "[TT] Power Consumption (Nighttime) of the TANSO-CAI-2 = 220 W"]
-[8.452862739562988, 7.768364906311035, "[TT] LWIR Camera Settings of the CUMULOS = High gain, 200 ms exposure"]
-[7.177721977233887, 2.6885859966278076, "[FF] Mission Purpose of the INSAT-3D = Provide enhanced meteorological observations and monitoring of land and ocean for weather forecasting and disaster warning"]
-[5.412715911865234, 4.153004169464111, "[TT] Bus Design of the QZS-1 = ETS-8 (Engineering Test Satellite-8) heritage"]
-[4.9270195960998535, 0.8667492866516113, "[TT] Fifth Flight Date of the MEPSI = 2007"]
-[12.054530143737793, 4.48496150970459, "[TT] Lunar Disk Size of the PACE spacecraft = 0.5\u00ba"]
-[7.170968532562256, 2.147402048110962, "[TT] Launch Date of the Biomass = 2023"]
-[6.606335639953613, 6.928404808044434, "[TT] Percentage of Components with No New Technology of the Instrument Assembly = 80%"]
-[13.319911003112793, 6.709278583526611, "[FF] Energy Comparison of the Transient Luminous Event = Energy produced by a transient luminous event would be enough to charge more than 800 vehicles"]
-[3.4334216117858887, 4.508601665496826, "[FF] Studied Phenomena of the SAR = Surface waves, internal waves, currents, upwelling, shoals, sea ice, wind, and rainfall"]
-[6.323614120483398, 4.50588846206665, "[FF] Function of the On-orbit Reprogramming = Can save a mission if the software is not perfect at orbital insertion"]
-[5.93421745300293, 2.994241952896118, "[TT] Collaboration with Other Government Agencies of the NASA = National Oceanic and Atmospheric Administration (NOAA) and the National Reconnaissance Office (NRO)"]
-[8.213615417480469, 1.265489935874939, "[TT] Observation Location of the RainCube = Sierra Madre Oriental, near Monterrey, Mexico"]
-[7.94741678237915, 4.271934986114502, "[FF] Purpose of the Radiation Monitor = Measure radiation"]
-[5.785150527954102, 1.0672446489334106, "[TT] Launch Date of the EROS-B = April 25, 2006"]
-[6.103484153747559, 8.54011058807373, "[TT] Polarization of the Communications Signal = Right-hand circular"]
-[8.48100471496582, 5.115739822387695, "[FF] Development Status of the GFO accelerometer = Delivered in December 2015"]
-[6.5471367835998535, 3.3346800804138184, "[FF] Use of the CRISTA-SPAS-2 = Simulation exercises for ISS assembly flight"]
-[8.905500411987305, 4.573473930358887, "[FF] Attitude Determination of the ASTRO-SPAS platform = Star field camera and a gyro package in combination with a GPS (global positioning system) position determination"]
-[4.730648040771484, 4.766115188598633, "[FF] Percentage of Detections from Vessels without AIS or VMS of the VIIRS = More than 85 percent"]
-[13.12490177154541, 7.3006439208984375, "[TT] Power Usage of the Micro-electromechanical system chip = 8.5 times less than proven systems"]
-[6.882278919219971, 3.692697286605835, "[FF] Ground Segment of the CO2Image = DLR\u2019s Space Operations facility"]
-[4.212156295776367, 7.083965301513672, "[TT] Band of the Telemetry Data = X-band"]
-[10.706147193908691, 7.551924705505371, "[TT] Swath Width of the PamCam = Approximately 250 km"]
-[8.073602676391602, 0.8818434476852417, "[TT] Drought Level of the United States = Extreme or exceptional"]
-[4.96238899230957, 6.131805419921875, "[TT] Data Receiver of the APL = Prime science data"]
-[12.104279518127441, 7.642947196960449, "[TT] Mass of the Pushbroom imager = 18.5 kg"]
-[7.827064514160156, 4.849404335021973, "[FF] Components of the Deployment Monitoring System = Cameras, limit switches, eddy current damper voltage, accelerometers"]
-[8.147958755493164, 8.879956245422363, "[TT] Spectral Resolution of the BIRCHES = 10 nm"]
-[13.068144798278809, 7.15679931640625, "[TT] Collection Power of the IMAP-Hi = ~25 x"]
-[13.72010612487793, 5.408145904541016, "[TT] Type of the Solar Panels = Triple junction solar cells"]
-[8.878324508666992, 1.446879506111145, "[TT] Centrifuge of the MVP-Cell 05 = Provides a variable gravity environment"]
-[8.427489280700684, 8.558855056762695, "[TT] Spectral Resolution of the OVIRS = R>2,000"]
-[7.057857036590576, 2.063922166824341, "[FF] Data Quality of the Landsat = Unmatched in quality, detail, coverage, and length"]
-[8.21953296661377, -0.5023849010467529, "[TT] Location of the Tyndall Glacier = Chile"]
-[5.753339767456055, 5.888573169708252, "[TT] Memory of the AIM = 64 kbyte I/O space mapped into Xilinx FPGA"]
-[6.448577404022217, 1.1073291301727295, "[FF] URL of the SphinX = http://www.cbk.pan.wroc.pl/body/publikacje/2008/JC_JS_Sphinx_2008_11_06.ppt"]
-[3.8543431758880615, 4.347553253173828, "[FF] Examples of InSAR and other land applications of the RADARSAT-2 = Unknown"]
-[8.834867477416992, 6.9385576248168945, "[TT] Image Compression of the HyperScout = 2x2"]
-[8.251385688781738, 2.531719923019409, "[FF] Team Leader of the Aerosol and cloud Retrieval Algorithm for CAPI = Chengcai Li"]
-[8.374147415161133, 6.182699680328369, "[FF] Purpose of the TRIO-CINEMA = Provide stereo ENA imaging of the ring current"]
-[6.849023342132568, -0.6513499021530151, "[TT] Orbit Period of the SEOSat = 98 minutes"]
-[11.62409782409668, 3.440765142440796, "[TT] Thrust of the CanX-4&5 = 5 mN"]
-[13.004335403442383, 7.040367126464844, "[TT] IMI Power Requirement of the WCOM = 250 W"]
-[6.3836669921875, 4.066497325897217, "[FF] Data Range of the SERVIR = Not entirely available through non-commercial entities"]
-[12.099754333496094, 4.570992946624756, "[TT] Stowed Dimensions of the Spacecraft = 239 mm x 116 mm x 366 mm"]
-[9.929130554199219, 6.791596412658691, "[TT] Detection Depth of the SMAP = Top 5 cm (2 inches) of the ground"]
-[8.161896705627441, -1.1012580394744873, "[FF] Bathymetry Models of the ICESat-2 = Unknown"]
-[1.6567378044128418, 3.744889259338379, "[FF] Development Team of the BEESAT-3 = Merlin F. Barschke, Frank Baumann, Klaus Briess, Christian Nitzschke"]
-[11.721868515014648, 0.13557986915111542, "[TT] Number of Earth-sized and \u2018Super Earth\u2019 planets of the TESS = ~500"]
-[14.271627426147461, 3.2349720001220703, "[TT] Mass of the \u00d8rsted = 60.7 kg"]
-[5.731398105621338, 12.150359153747559, "[TT] Wavelength FWHM of an unresolved line of the Spectrometer = 0.039 \u00b5m"]
-[10.21196460723877, 7.961131572723389, "[TT] Stray Light/Sun Disk Light Rejection of the Telescope = 5 x 10^8"]
-[8.655713081359863, 7.678268909454346, "[TT] Pixel Size of the CCID-80 = 15 x 15 \u00b5m"]
-[9.1397066116333, 3.105559825897217, "[FF] Effect of the Clusters = Generates an enhanced particle acceleration compared to the isolated plasma cloud"]
-[7.284267902374268, 8.733489036560059, "[TT] Band 3 of the RBV Instrument = 0.70 - 0.83 \u00b5m"]
-[6.136052131652832, 1.3551414012908936, "[FF] Activation Date of the Deep Space Atomic Clock = 26 August 2019"]
-[8.258515357971191, 0.44579920172691345, "[TT] Previous Record Discharge of the Yellowstone River = 32,200 cubic feet per second"]
-[10.13107967376709, -1.380523681640625, "[TT] Orbit Inclination of the TanSat = 98.2\u00ba"]
-[6.594815731048584, 4.177021503448486, "[FF] Operation of the JEMRMS = Catches EP and carries it to EFU"]
-[12.306966781616211, 3.1789374351501465, "[FF] Revision Decision of the SLATS = Revise the NDO to cut off the future fuel of RCS"]
-[7.018173694610596, 7.9716010093688965, "[TT] Ranging Noise of the LRI = < 80 nm/\u221aHz"]
-[9.061306953430176, 4.95919132232666, "[TT] Accomplished ?V Maneuver of the Satellite = 0.15 m/s"]
-[5.118849754333496, 1.8767786026000977, "[FF] Conference Presentation Date of the TacSat-4 = Feb. 24-26, 2009"]
-[4.936169624328613, 0.9846667647361755, "[TT] Launch Date of the Dellingr = 2017"]
-[6.885632038116455, 1.9279935359954834, "[FF] URL of the Electron Tunneling Infrared Detector = http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910005078_1991005078.pdf"]
-[10.818943977355957, -0.25305917859077454, "[TT] Baseline Vector Accuracy of the TanDEM-X = 1 mm"]
-[11.991103172302246, 6.5573601722717285, "[TT] Energy Range of the AMS-02 = 0.5 to 350 GeV"]
-[8.410672187805176, 1.779456377029419, "[TT] Range of measurements of the Ocean SST = 20%"]
-[9.461103439331055, 6.963116645812988, "[TT] Spatial Resolution - ScanSAR of the ALOS = 100 m"]
-[13.685769081115723, 6.980632305145264, "[TT] PCDU Outlets of the EPS = Over 150"]
-[5.302298069000244, 0.624152421951294, "[TT] First Contact Date of the RASAT = August 17, 2011"]
-[4.729523658752441, 8.366223335266113, "[TT] Center Frequency of the 3 = 53.596 GHz"]
-[11.702746391296387, 3.3419926166534424, "[TT] Time to Reduce Pressure from 95% to 80% of the Thruster = Approximately two seconds"]
-[7.836096286773682, 4.604062557220459, "[FF] Impact on Results of the Subapertures = Larger subapertures yield better results than smaller subapertures"]
-[4.815375804901123, 0.5177047848701477, "[FF] Launch Date of the OSCAR-QUBE = 29 August 2021"]
-[8.883179664611816, 7.361886501312256, "[TT] Detection Area of the Detector = 1000 cm2"]
-[6.175212383270264, 2.330465793609619, "[FF] Project Scientist of the Airborne Topographic Mapper (ATM) = Michael Studinger"]
-[7.104538917541504, 3.9365649223327637, "[FF] Trajectory Analysis and Design Presentation of the OMOTENASHI = 26th International symposium on Space Flight Dynamics"]
-[10.782281875610352, 1.7150605916976929, "[FF] Role of the INTEGRAL and XMM-Newton = Follow-up of recent gravitational wave detections"]
-[5.76483154296875, 5.284011363983154, "[FF] Telemetry Protocol of the LPT = UDP (User Datagram Protocol)"]
-[4.856287479400635, 7.2747039794921875, "[TT] Downlink Data Rate of the RF Communications = 270 Mbit/s"]
-[8.144946098327637, -0.6699643731117249, "[TT] Land Ice (small scale) Temporal Sampling of the CryoSat = 1 year"]
-[7.689411640167236, -2.3576114177703857, "[TT] Principal Investigator of the GOLD Instrument = Richard Eastes"]
-[14.292404174804688, 3.1644411087036133, "[TT] Mass of the SCDE = 0.6 kg"]
-[9.3292875289917, 6.390190601348877, "[TT] Scan Rate of the Scan Mirror = 0.46\u00ba/s"]
-[13.499826431274414, 5.378359317779541, "[TT] Subject of the Cell Science-04 = Tardigrades"]
-[10.244806289672852, 8.41385269165039, "[TT] Diameter of the Entrance Pupil = 320 mm"]
-[10.831634521484375, 3.4942874908447266, "[TT] Bus Size of the CubeSat = 6U"]
-[8.872035026550293, 7.354631423950195, "[FF] Payload of the ZACube-2 = Medium resolution matrix imager and a number of communication subsystems"]
-[8.31715202331543, -0.5822365880012512, "[TT] Edge location of the Ice = \u00b112.5 km"]
-[8.091863632202148, 2.036672353744507, "[TT] Operation of the Seasat-A Scatterometer System (SASS) = Simultaneous operation with all sensors"]
-[4.689139366149902, 2.2430849075317383, "[TT] Landing Site of the Capsule = Southern Australian desert"]
-[11.552536010742188, 5.1858296394348145, "[TT] Size of the SMOG-P = 5 x 5 x 5 cm"]
-[8.500198364257812, 6.150138854980469, "[TT] Accuracy of the VMAG = \u00b1 0.1 nT"]
-[3.379859685897827, 1.564428448677063, "[FF] Launch Plans of the Sentinel-1C = In force to launch as soon as possible"]
-[3.762223720550537, 2.418858289718628, "[TT] Deployment Timeframe of the Iridium NEXT = 2015-2017"]
-[8.570252418518066, 7.935295581817627, "[TT] Spectral resolution (nm) of the Full-scan Imaging = 1.2, 1.9, 4.2"]
-[5.096060752868652, 0.3852466642856598, "[TT] Deployment Date of the nSight-1 = 16 to 25 May 2017"]
-[9.460821151733398, -0.5595092177391052, "[TT] Altitude of the ICEYE-X14 and ICEYE-X16 = Approximately 500 km"]
-[3.649209976196289, 6.92399787902832, "[FF] Antenna Polarization of the GPS Reflectometry Receiver = RHCP (Right-Hand Circular Polarization) and LHCP (Left-Hand Circular Polarization)"]
-[12.702188491821289, 7.6265950202941895, "[TT] Resolving Power of the Instrument = 10,000"]
-[5.449463844299316, 2.546811819076538, "[TT] Data Evaluation Teams of the TRISHNA = French team, Indian team"]
-[6.902626991271973, 2.2417643070220947, "[TT] Role of the Hinode = Sun-watching"]
-[9.861437797546387, 5.584919452667236, "[TT] Decenter of the M2 = 8 \u00b5m"]
-[5.317232131958008, 3.4851036071777344, "[TT] Type of the Terminator Tape Deorbit Module = Passive de-orbit device"]
-[7.011504173278809, 3.064131498336792, "[FF] Capabilities of the EON-MW = Microwave Atmospheric Remote Sensing"]
-[7.3968729972839355, 6.580656051635742, "[TT] Accuracy of the Laser Rangefinder = Better than 1 meter"]
-[6.9964799880981445, 1.2837903499603271, "[FF] Final Report Date of the Solar Mass Ejection Imager (SMEI) = Oct. 25, 2007"]
-[14.225666999816895, 3.1349568367004395, "[TT] Mass of the SHFT = 5 kg"]
-[9.454151153564453, 4.954453468322754, "[FF] Airplane (AP) Mode of the ICESat = XG axis (plus or minus) is closely aligned with the velocity vector"]
-[4.963286399841309, 0.9912282824516296, "[TT] Data Acquisition Period of the TANSO-FTS-2 = 5 March to 3 April 2019"]
-[8.421600341796875, 6.550471782684326, "[FF] Scanning Pattern Loss of the OGS = Applies during initial acquisition"]
-[13.392518997192383, 7.343119144439697, "[TT] Power of the SCD-2 = 110 W"]
-[6.927478313446045, 7.053527355194092, "[TT] Components of the LCEU = 980 nm continuous-wave laser diode and signal processing electronics"]
-[6.504330158233643, 1.1288776397705078, "[FF] Date of the Dynamic Dunes = 15 March, 2021"]
-[6.888904571533203, 6.163924694061279, "[TT] Stripmap of the Mode = -"]
-[14.243457794189453, 3.282250165939331, "[TT] Mass of the Jugnu = 3 kg"]
-[5.319003105163574, 0.7002472281455994, "[TT] Data Collection Start Date of the TIM = January 11th"]
-[4.6587324142456055, 2.901749849319458, "[TT] Control Center of the Aeolus = ESA's ESOC (European Space Operations Center) in Darmstadt, Germany"]
-[14.180469512939453, 2.994262933731079, "[TT] Mass of the Deimos-2 = 310 kg"]
-[4.796698570251465, 0.07419988512992859, "[TT] End of Life Date of the SES-17 = 24 October 2036"]
-[7.159280300140381, 5.7954277992248535, "[FF] Stability of the DSAC = 100 times more stable than today\u2019s best navigation clocks"]
-[9.110257148742676, 8.323387145996094, "[TT] Spectral Data Utilization of the Focal Plane = Less than 20%"]
-[6.069352149963379, 5.721151351928711, "[TT] Regulated Voltages of the COVE Board = FPGA: 3.3 V, 2.5 V, 1.0 V; Configuration PROM: 3.3 V, 1.8 V; Magnetoresistive RAM: 3.3 V; Flash memory: 3.3 V; ADCs: 3.3 V, 1.25 V; Buffers, muxes: 3.3 V"]
-[11.681981086730957, 3.4011282920837402, "[TT] Propellant Ionization of the Ion Thruster = DC discharge, Kaufman configuration"]
-[9.437246322631836, 5.368041038513184, "[TT] Mechanism Type of the SMA = Two-axis mechanism involving two flex pivots per axis"]
-[13.854680061340332, 5.679062843322754, "[TT] Efficiency of the Solar Panels = 27.5%"]
-[1.723549723625183, 6.133450508117676, "[TT] Stars in Galaxies Percentage of the Universe = 7 percent"]
-[6.7057952880859375, 4.705333232879639, "[FF] Objective of the CAPS SW = Provide full autonomous navigation onboard the CAPSTONE spacecraft"]
-[10.747397422790527, 3.919077157974243, "[FF] Formation Flight of the CanX-4 & CanX-5 = Accomplished"]
-[4.962200164794922, 3.1048622131347656, "[TT] Manufacturer of the Multispectral Instruments = Airbus Defence and Space in France"]
-[5.352797031402588, 0.8125066757202148, "[FF] Date of the EFT-1 = Unknown"]
-[3.8483622074127197, 1.1193236112594604, "[TT] Number of Launches for Booster of the Falcon 9 = Fifth flight"]
-[5.464557647705078, 6.020506381988525, "[TT] ROM of the OBC = 16 kB"]
-[6.773844242095947, -0.6697566509246826, "[TT] Orbital Period of the PROBA-3 = 19.5 hours"]
-[6.605238914489746, 4.632519245147705, "[FF] Backup Purpose of the CIRAS = Gap filler in the event of a failure of the CrIS"]
-[13.683095932006836, 6.861833095550537, "[TT] Power Generation Capability of the SBVR = 20.3 kW max"]
-[5.711511135101318, -0.09203879535198212, "[TT] Repeat Cycle of the IRS-1B = 22 days"]
-[5.05238151550293, 4.154745578765869, "[TT] Service Name of the XPOD = NLS-6 (Nanosatellite Launch Service-6)"]
-[6.962661266326904, 4.909084320068359, "[FF] Objective of the GAGE = To characterize the GPS signal availability at selected altitudes up to GEO"]
-[8.859048843383789, 7.064245223999023, "[FF] Imagery Objective of the AlSat-2A = Provide medium resolution satellite imagery as well as expertise to identify locust breeding areas"]
-[8.933113098144531, 4.4907145500183105, "[FF] Attitude and Orbit Control Subsystem Components of the FormoSat-2 = Star sensors, gyroscopes, IRU (Inertial Reference Unit)"]
-[6.264040946960449, 6.1045613288879395, "[TT] INR Performance of the GOES N-P series = Improved"]
-[8.335437774658203, 7.565080165863037, "[FF] Operation of the MVIRI = One infrared detector, one water vapour detector and one pair of visible detectors will be in operation"]
-[6.071556568145752, -1.9453591108322144, "[TT] Member of the Gary Egbert = True"]
-[5.866001605987549, 0.9102529287338257, "[FF] First Image Transmission Date of the LADEE = Feb. 13, 2014"]
-[8.827783584594727, 3.206874370574951, "[FF] Ambient Ionosphere Forecast of the C/NOFS = Several hours ahead"]
-[14.308696746826172, 3.2182741165161133, "[TT] Mass of the DebriSat = 56 kg"]
-[7.515252590179443, 1.324689269065857, "[FF] Detection Date of the Offshore Platform in the Gulf of Mexico = June 9, 2022"]
-[1.7538950443267822, 4.565481662750244, "[FF] N/A of the microthruster = N/A"]
-[12.10848617553711, 4.128220081329346, "[TT] Volume of the CROP Filter = 600 mL"]
-[10.070051193237305, 1.422516107559204, "[FF] Purpose of the Euclid = Measure the shapes and distances of billions of galaxies"]
-[7.537999629974365, 0.9680156111717224, "[TT] Depth Scales of the Surface Topography of the GRAIL = About 4 km"]
-[7.9898681640625, -0.6159007549285889, "[TT] Instrument 1 of the CryoSat-2 = DORIS"]
-[3.950479507446289, 7.83610200881958, "[TT] Uplink Modulation of the Iris Radio = BPSK"]
-[7.978488922119141, 8.04290771484375, "[FF] Instrument Type of the IRFS-2 = Advanced infrared sounder"]
-[6.1813178062438965, 1.061342716217041, "[FF] Establishment Date of the WINDS broadband link = March 15"]
-[9.746797561645508, 4.222762584686279, "[TT] Principle of the PNI RM3000 = Magneto-inductive"]
-[6.528170108795166, 3.9399757385253906, "[TT] Instrument Status of the GOES-17 = Turned off"]
-[7.725835800170898, 3.833624839782715, "[FF] Instrument Type of the Satellite = Cloud profile and rain radars, High resolution optical imagers, Earth radiation budget radiometers, Space environment, Magnetic field, Other, Atmospheric chemistry, Communications, Precision orbit, Data collection, Radar altimeters, Imaging microwave radars, Gravity instruments, Lightning sensors"]
-[5.988276481628418, -0.41508087515830994, "[TT] Temporal Baseline of the GF-3 = Nearly 4 months"]
-[7.362584590911865, 0.3842209279537201, "[FF] URL of the Jason-2 = http://www.aviso.oceanobs.com/fileadmin/documents/newsstand/Newsletter/aviso_special_issue_3years_Jason2.pdf"]
-[8.359101295471191, 0.13565871119499207, "[FF] Release Date of the Comet landscape = 01 October 2018"]
-[6.79862117767334, 4.180041313171387, "[FF] Design Goals Met of the SHIMMER = Yes"]
-[5.947913646697998, 5.405107498168945, "[TT] Activation of the Redundant Series Separation Switches = After spacecraft deployment"]
-[5.584604263305664, 0.8400216698646545, "[FF] Contract Date of the Satellite Vu\u2019s first satellite = December 16, 2021"]
-[8.395941734313965, 3.5665104389190674, "[FF] Measurement of the Sea and Land Surface Temperature Radiometer = Real amount of energy radiating from Earth"]
-[9.30079174041748, 1.1660598516464233, "[TT] Velocity Regime of the Austfonna = Predominantly slow (~ 101\u2009m/yr) to fast (~ 103\u2009m/yr)"]
-[5.638366222381592, 2.881380558013916, "[FF] Design of the ASTROhead = Jena-Optronik\u2019s existing ASTROhead design"]
-[5.942422866821289, 0.4730314016342163, "[TT] Observation Period of the RECCAP-2 = 2009-2018"]
-[13.836048126220703, 3.0998857021331787, "[TT] Mass of the Payload = 100 kg"]
-[4.7842698097229, 0.4354170560836792, "[TT] Launch Date of the FORUM = July 2027"]
-[3.527613878250122, 6.351922512054443, "[TT] Size of the DSN Antennas = 34 m"]
-[7.6621623039245605, -2.3770534992218018, "[FF] Mission Status of the GOLD instrument = Unknown"]
-[3.431703805923462, 6.416114330291748, "[TT] Antenna Diameter of the Satellite = 1.5 m"]
-[5.791515350341797, 7.168399333953857, "[TT] Data Rate of the HEPD = 0.19 kbit/s"]
-[9.44590950012207, 6.313581943511963, "[TT] LOS IAR Rotation Angle of the Integer Ambiguity Resolution = 50o"]
-[9.690961837768555, -0.8471714854240417, "[TT] Orbit of the Spacecraft = SSO, altitude of 623 km x 650 km, inclination = 98\u00ba, LTDN= 10:30 hours"]
-[6.11349630355835, 3.013068199157715, "[FF] Challenge of the Legion satellites = Miniaturizing electronics while maintaining the performance of the high-resolution optics and keeping cost under control"]
-[9.212116241455078, 2.473315954208374, "[TT] Total of the Sprites = 2048"]
-[9.325209617614746, 3.3667919635772705, "[FF] Paper Title of the Nikolai A. Tsyganenko = Data-based modeling of the geomagnetosphere with an IMF-dependent magnetopause"]
-[8.157909393310547, 7.887163162231445, "[TT] NIR Channel Detectors of the SEVIRI = InGaAs photovoltaic diodes"]
-[5.393927097320557, 4.639667510986328, "[FF] Implementing control-user plane split of the Open5GCore Rel. 4 = PFCP [N4]"]
-[8.746088981628418, 2.612900495529175, "[FF] Accuracy of Flow Angle and Flux Measurements of the SPC = Decoupled from any thermal or mechanical changes within the modulator assembly"]
-[6.896679878234863, 6.5885748863220215, "[TT] Dynamic Spectrum Production of the SWAVES = 1 minute averaged"]
-[7.379306316375732, 1.0185985565185547, "[TT] Support of the LRO = Future human missions to the moon"]
-[9.98468017578125, 2.248182773590088, "[FF] Capability of the NuSTAR = Pinpointing the location of the radioactivity, creating maps"]
-[7.461246490478516, 2.302687168121338, "[TT] Region of the FlytLIVE = Americas and the Atlantic Ocean region"]
-[5.570067405700684, 7.5264058113098145, "[TT] G/T of the HDR-VSAT = > 19.0 dB/K"]
-[4.553160667419434, 0.34989118576049805, "[TT] Launch Date of the Soyuz-2.1b rocket = 6 February 2020"]
-[10.068917274475098, 5.3122663497924805, "[FF] Cryocooler of the WFIRST = Eliminated in favor of passive cooling of the WFI cold electronics"]
-[6.521970272064209, 4.80348014831543, "[FF] Unknown of the GATE Receiver = Unknown"]
-[5.257669448852539, 0.7478176951408386, "[FF] Re-entry Date of the HITSAT = June 18, 2008"]
-[7.012362003326416, 4.314809322357178, "[FF] Unknown of the IMS = Unknown"]
-[9.13928508758545, 7.412273406982422, "[TT] Panchromatic Band Off-nadir Resolution of the WorldView-3 = 0.34 m"]
-[9.212214469909668, 2.9146156311035156, "[FF] Associated Event of the Solar Flare = Fast coronal mass ejection (CME)"]
-[7.967449188232422, 6.500895977020264, "[TT] Duty Cycle of the Satellite = 30 min imaging + 30 min rest"]
-[9.179696083068848, 7.442399501800537, "[TT] Panchromatic Spatial Resolution of the DMAC = 2.5 m"]
-[12.00190544128418, -0.3256898820400238, "[TT] Discovery Date of the TESS = July 29, 2019"]
-[8.996014595031738, 6.423122406005859, "[FF] Image Orientation of the CaSSIS = North is up"]
-[13.755901336669922, 2.96006441116333, "[TT] Booster Segments Weight of the SLS = 180 tons"]
-[9.694354057312012, -0.5307227373123169, "[TT] Altitude of the Earth Orbit = 833 km"]
-[7.100438594818115, -0.7648367285728455, "[FF] Transit Period of the GJ 367b = Ultrashort"]
-[6.142890930175781, 2.835237503051758, "[FF] Technology Generation of the X-Series Missions = Next-generation"]
-[8.630648612976074, 0.9252620935440063, "[TT] Published Article Date of the Eugene Parker = 1958"]
-[6.814977645874023, 5.912353992462158, "[TT] Quantity of the bioCDs = 3"]
-[5.323610782623291, 0.09842826426029205, "[TT] Calibration Update of the Ikonos-2 = 2007"]
-[9.497048377990723, 5.605993270874023, "[TT] Moon Angle Constraint of the CHEOPS = Larger than 5\u00ba"]
-[2.9255270957946777, 4.252803325653076, "[FF] Emergency Observation of the PALSAR-2 = Mount Agung in Bali Island, Indonesia"]
-[10.415699005126953, 5.6998419761657715, "[FF] Building Exterior Temperature of the ECOSTRESS = A few degrees cooler than paved surfaces"]
-[8.282927513122559, 0.12329789251089096, "[TT] Discovery Date of the Comet ATLAS = Dec. 28, 2019"]
-[5.525271415710449, 2.641523838043213, "[TT] Agency of the FalconSat-3 = USAF"]
-[6.453728675842285, 2.6302685737609863, "[FF] Principal Investigators of the Rhodium Synthetic Cryptobiology = Drs. Heath Mills and Aindrila Mukhopadhay"]
-[9.953751564025879, 6.644272804260254, "[TT] FOV of the Earth Radiation Budget Experiment (ERBE) = \u00b178\u00ba cross-track, 360\u00ba azimuth"]
-[6.298577308654785, 7.4400715827941895, "[TT] Data Quantization of the CSG-SAR = 10 bit"]
-[13.917695999145508, 3.4545886516571045, "[TT] Material of the Canopy = 1/4 mil mylar"]
-[11.415635108947754, 5.7145094871521, "[TT] Composition of the Cobalt Alloy = 13% W"]
-[6.319863796234131, 3.9037725925445557, "[FF] Benefits of the ASAP = Fast response to external events, reduces overall mission costs"]
-[12.017882347106934, -0.4301936626434326, "[TT] Mission Start Year of the TESS = 2018"]
-[13.074972152709961, 5.453394889831543, "[FF] Configuration of the MPO = Equipment panel perpendicular to radiator"]
-[7.2962493896484375, 3.80066180229187, "[FF] Metrology Sensor Suite of the PROBA-3 = Acquiring the formation and providing relative position determination with micrometric precision"]
-[6.672226905822754, 5.367236614227295, "[FF] Optimization Contributions of the Advanced Digital Subsystems = Size, mass, and power"]
-[8.961484909057617, 4.404026985168457, "[TT] Type of the Sun sensors = 2 axis slit & photo cell"]
-[8.03242015838623, 4.670461654663086, "[FF] Calibration Views of the CIRiS = 1) deep space 2) an on-board source at a selectable and controlled temperature and 3) an on-board source at the instrument temperature"]
-[4.301894187927246, 7.249711036682129, "[FF] Band of the Ka-band High Power Multi-Port Amplifier = Ka-band"]
-[8.633149147033691, 7.728062152862549, "[TT] Detector Array Size of the HySI = 512 x 512 pixels"]
-[9.491806030273438, 6.397005558013916, "[TT] Time of the Mirror Retrace = 2.5 minutes"]
-[7.823111534118652, 4.069492340087891, "[TT] Size of the Internal Occulter (IO) = 1.04 Rs"]
-[6.9161376953125, 4.060085296630859, "[FF] Field of View of the ASPIICS = Unprecedented"]
-[11.756136894226074, 3.267055034637451, "[TT] Thrust of the Chemical Propulsion Thrusters = 6 to 12.5 N"]
-[7.49294376373291, 1.4478363990783691, "[TT] Forecast Date of the Hurricane Michael = 8 Oct 2018"]
-[13.202064514160156, 7.2663350105285645, "[TT] Power Consumption of the AMU = < 39 W"]
-[6.911471366882324, 2.5244483947753906, "[FF] Role of the Martin Popek = Scientific team member"]
-[7.777562141418457, 6.485947608947754, "[TT] Power Cycle Frequency of the Metrology System = 4 times a second"]
-[5.44769811630249, 1.4653136730194092, "[FF] Conference Presentation Date of the EnMAP = March 6-13, 2010"]
-[8.114691734313965, 5.165491580963135, "[FF] Calibration Process of the PNI RM3000 = Subtracted off from the DC measurements"]
-[8.809182167053223, 7.602008819580078, "[TT] MS B1 of the Pushbroom imager = 0.45-0.52 \u00b5m"]
-[5.83513069152832, 4.9354400634765625, "[FF] Control Method of the Barber Pole = Tether deployment"]
-[14.592350006103516, 6.64314079284668, "[TT] Battery Type of the EPS = Lithium-ion"]
-[7.1896257400512695, 7.484861373901367, "[TT] Optical Pulse Spectral Range of the LI = 777.4 \u00b1 0.17 nm"]
-[10.08549976348877, 8.430424690246582, "[TT] Aperture Diameter of the IRIS Instrument = 120 mm"]
-[6.420266628265381, 1.8984663486480713, "[FF] Public Science Archive Location of the NuSTAR = HEASARC"]
-[7.910120964050293, 0.14334824681282043, "[FF] Monitoring Capability of the GRACE-1 = Mass motions in the Earth system with unprecedented accuracy and temporal resolution"]
-[4.207693576812744, 2.600299596786499, "[TT] Launch Site of the AeroCube-4 = VAFB, CA"]
-[8.849602699279785, 5.801808834075928, "[TT] Sensor Pointing Accuracy of the STARE = 1\u00ba"]
-[10.129651069641113, 1.9672423601150513, "[TT] Anomaly Date of the Chandra X-ray Observatory = Aug. 24"]
-[5.745803356170654, 3.4588565826416016, "[FF] Requirement of the EUMETCast = Users to purchase new satellite reception equipment and pay for the transmission fee"]
-[8.376350402832031, -2.0592520236968994, "[TT] Orbit of the GOLD = Geostationary"]
-[5.841439247131348, 4.862061023712158, "[FF] Function of the L1-SAIF+ = Augmentation of satellite-positioning signal and shortening the TTFF (Time To First Fix)"]
-[5.7190775871276855, 1.3290207386016846, "[TT] Presentation Date of the Peter Wegner = May 7-10, 2012"]
-[8.62423038482666, 1.9566320180892944, "[TT] Grid Size of the ASCAT coastal winds = 12.5 km"]
-[7.3950910568237305, 5.4809794425964355, "[FF] Sub-Assemblies of the FLLS = LCEU (Laser Control Electronics Unit), the OHU (Optical Head Unit), and the CCRR (Corner Cube Retroreflector)"]
-[3.2617111206054688, 4.138474464416504, "[TT] Operation as Radar Interferometer of the TerraSAR-X and TanDEM-X = Since December 2010"]
-[5.316253185272217, 0.28981730341911316, "[TT] Approach Date to ISS of the Cygnus Orbital ATK CRS-4 = Dec. 9, 2015"]
-[3.5133485794067383, -0.8376500010490417, "[TT] Orbit Type of the SPARCS = Sun-synchronous terminator orbit"]
-[7.786250114440918, 8.675690650939941, "[TT] Spectral Ranges of the Dichroics = 4"]
-[8.172544479370117, 8.795644760131836, "[TT] Performance Range of the UV-1 = 270 - 310 nm"]
-[4.943276882171631, 0.49704989790916443, "[TT] Launch Date of the ARMADILLO = 25 June 2019"]
-[3.2525222301483154, 5.168117046356201, "[TT] Spotlight (SL) Spectral Resolution of the TSX-SAR = 2m"]
-[8.190773010253906, 6.691262722015381, "[TT] Data Transmission of the Imaging Plan = 1.6 TB per orbit"]
-[9.83987045288086, -0.20469504594802856, "[TT] Orbit Altitude of the GRACE = Same altitude"]
-[5.1771345138549805, 2.4478752613067627, "[TT] Acoustic Chamber Testing Location of the Crew Dragon = NASA\u2019s Plum Brook Station test facility at Glenn Research Center in Ohio"]
-[10.39125919342041, 4.538283348083496, "[TT] Redundancy of the Reaction Wheels = 1 RW loss allowed"]
-[8.958532333374023, 0.937721848487854, "[TT] Model of the Parker Solar Probe = WSA model"]
-[6.291339874267578, 4.2558369636535645, "[FF] Feasibility Analysis of the CSK GS = Check the possibility to perform sensing on the selected Area of Interest during the selected Time Window and according to the chosen mission/satellite acquisition parameters"]
-[7.068285942077637, 4.577188968658447, "[FF] Selection Basis of the RVX equipment = Needs of several systems"]
-[8.099469184875488, 3.3298256397247314, "[FF] Drought Impact of the OCO-2 = Increased carbon dioxide release"]
-[14.250219345092773, 3.1965725421905518, "[TT] Mass of the TRSR = 4 kg"]
-[5.3712358474731445, 5.621737003326416, "[TT] Standard Interface of the CEASE-2 = RS-422 or MIL-STD-1553B"]
-[6.989359378814697, -0.3516082167625427, "[TT] Number of Orbits per Day of the Tatiana-1 = 14"]
-[7.914313793182373, 4.427667617797852, "[FF] Interferometry Concept of the CE-2 Navigation Project = Employed for orbit determination"]
-[9.444626808166504, 5.956348419189453, "[TT] Cross-Track Tilt of the Geoton-1 = \u00b1 30\u00ba"]
-[6.320611476898193, -1.3257699012756348, "[TT] Launch Year of the GRACE = 2002"]
-[11.185428619384766, 4.996824264526367, "[TT] CCR Diameter of the LARES-2 = 25 mm"]
-[9.283669471740723, 4.55670690536499, "[FF] Operation of the ACS = Mostly passive during transfer orbit"]
-[7.362520217895508, 2.104682445526123, "[FF] Objective of the Landsat Next = Extend the ability to detect and quantitatively characterise changes on the global land surface"]
-[4.312386512756348, 7.563108921051025, "[TT] Frequency of the S-band Uplink = 2061.976 MHz"]
-[7.709932804107666, 6.790088176727295, "[FF] Purpose of the DWS = Measuring with high sensitivity the angle between two wavefronts in a laser interferometer"]
-[9.844178199768066, 8.185388565063477, "[TT] Focal Length of the HR5 or Stereo 5 = 660 mm"]
-[8.105027198791504, -1.2251780033111572, "[FF] Laser Altimetry Mission of the ICESat-2 = Proceedings of the IEEE. Vol 98, No. 5, May 2010. Pages 735-751"]
-[4.771913528442383, 0.4787536859512329, "[TT] Launch Date of the SVOM = Scheduled for Mid-2023"]
-[9.665200233459473, 7.3363752365112305, "[TT] Ground Resolution of the StriX-\u03b1 = 1-3 m"]
-[8.130213737487793, 3.026655912399292, "[TT] Resolving Power of the Atmospheric Chemistry Suite = 10,000 or more"]
-[4.827671527862549, 1.3189283609390259, "[FF] Launch Date of the OPTSAT-3000 = Aug. 2, 2017"]
-[9.935917854309082, 4.6125688552856445, "[TT] Attitude Control Components of the STPSat-1 = Momentum wheel, two smaller reaction wheels"]
-[8.820176124572754, 2.490781784057617, "[FF] Mission Type of the SOHO = Solar Study"]
-[13.033767700195312, 7.3784379959106445, "[TT] Power of the SeaWinds = 250 W"]
-[5.2471923828125, 0.8219122886657715, "[TT] Commissioning Phase of the RPW = Before 15 June"]
-[6.255121231079102, 7.419698715209961, "[TT] Data Quantization of the SAR = 2/3 BAQ 2/3/4/5/6 bit BAQ"]
-[6.963863849639893, 4.173672199249268, "[FF] MMOD of the Spacecraft = Unseen threat that all spacecraft need to be protected from"]
-[8.456299781799316, 0.829919695854187, "[TT] Utilization of the ICI-11 = Quasi-window, cirrus clouds, cloud ice water path"]
-[7.485269069671631, 6.960629940032959, "[TT] Read-out Time of the CCD = 2.1 s"]
-[9.481266975402832, 4.116304874420166, "[TT] Type of the Magnetometer = Flux gate"]
-[5.404213905334473, 3.9837844371795654, "[TT] Number of Earth observation satellites of the Ground Station = More than 16"]
-[9.130285263061523, -0.37500372529029846, "[FF] Apogee Alignment of the MMS = Opposing"]
-[7.440268039703369, 4.511287212371826, "[FF] Execution Dates of the RVX = Critical aspect in the definition of the trajectory profile"]
-[8.454324722290039, 2.272090196609497, "[FF] Minimum Variance Wind Speed Estimator of the Spaceborne GNSS-R = Spaceborne GNSS-R Minimum Variance Wind Speed Estimator"]
-[8.137699127197266, 5.606377124786377, "[FF] Data Transfer of the Webb's Fine Guidance Sensor (FGS) = Up to two science instruments at a time"]
-[5.8198933601379395, 4.869002342224121, "[TT] New Program Segments Languages of the ESA = Dutch, French, German, Italian and Spanish"]
-[5.19473123550415, 6.076529026031494, "[TT] Data Input Interface of the Modem Processor = SpaceWire over LVDS (Low Voltage Differential Signaling) link"]
-[4.000839710235596, 6.495042324066162, "[TT] Location of the X-band antenna = Nadir face"]
-[9.485130310058594, 7.106780529022217, "[TT] Radiometric Resolution (K) of the PMI = 0.5"]
-[6.947734832763672, 7.805221080780029, "[TT] Optical Retro Reflector Diameter of the ANDE-2 = 12.7 mm"]
-[6.492288112640381, 5.027920722961426, "[FF] Technologies of the CFESat = Supercomputer equipped with field-programmable gate arrays (FPGAs), new power supply, inflatable antennas, deployable booms, new type of launch-vehicle separation system, high-density pack of AA lithium-ion batteries"]
-[6.009749889373779, 7.5073747634887695, "[TT] Sampling Rate of the RTEP = 500 Hz"]
-[8.961112976074219, 5.606171131134033, "[TT] Knowledge of the Pointing requirements = 0.1\u00ba"]
-[3.9270806312561035, 6.574879169464111, "[TT] HPBW EL of the Antenna = 73\u00ba"]
-[6.932000637054443, 4.2615485191345215, "[TT] Mounting Location of the CREAM = Externally to the ISS"]
-[10.876720428466797, 3.8968918323516846, "[TT] ISL Range of the CanX-4&5 = 5 km"]
-[9.901816368103027, 1.4366976022720337, "[FF] Number of Stars of the Pleiades = Several hundred"]
-[10.064982414245605, -1.4567172527313232, "[TT] Final Orbit Inclination of the FormoSat-7/COSMIC-2 satellites = 24\u00ba"]
-[9.669633865356445, -0.11990145593881607, "[TT] Ascent-Back \u0394V of the Hayabusa-2 = 0.64 m/s"]
-[8.983654975891113, 4.906474590301514, "[TT] Measurement Principle of the Honeywell QA-2000 Accelerometer = Actively centered proof mass on a deflection beam"]
-[8.324426651000977, 2.5177454948425293, "[TT] Impact of the CATS = Enabled more accurate aerosol modeling and forecasting"]
-[6.640287399291992, -0.6338226199150085, "[TT] Orbital Period of the STRV-1c and -1d = About 10.5 hours"]
-[10.049113273620605, -1.546284794807434, "[TT] Orbit Inclination of the GOMX-3 = 51.6\u00b0"]
-[3.4301321506500244, 6.371951580047607, "[TT] Length of the DSX Z antenna = 16 m"]
-[10.419913291931152, 2.1485369205474854, "[TT] Light Detection of the NuSTAR = X-rays"]
-[4.812417507171631, -1.8615645170211792, "[TT] Re-Entry Speed of the Chang\u2019e-5 = Approximately 40,000 km/hr"]
-[9.069766998291016, 7.275341987609863, "[TT] Sensitive Area of the IS = 100 cm2"]
-[5.942094802856445, 5.072335243225098, "[FF] Function of the Strain Relief Connector Saver = Alleviate issues and protect the access port"]
-[7.177866458892822, 4.473823547363281, "[FF] Function of the CMS = Analysis of orbit data and planning of orbit correction maneuvers"]
-[16.501949310302734, 3.5881614685058594, "[TT] Global Services Delivery of the OneWeb = 2022"]
-[8.242557525634766, -0.466279000043869, "[TT] Coverage of the NSCAT = 90% of ice-free ocean surface every two days"]
-[6.617799758911133, 2.4474380016326904, "[FF] Optical Performance of the Euclid = Very stable under extreme attitude changes"]
-[9.735821723937988, -0.5557633638381958, "[TT] Altitude of the Orbit = 400 km"]
-[6.066214561462402, 3.026946544647217, "[FF] User Agencies of the SeaSat = NOAA, Navy, Coast Guard, Geological Survey, NSF"]
-[7.66173791885376, -0.5448493361473083, "[FF] Collaboration Members of the IceCube-Gen2 = M. G. Aartsen, R. Abbasi, M. Ackermann, .... M. Z\u00f6cklein"]
-[13.535768508911133, 5.286504745483398, "[TT] Solar Panels of the CartoSat-2B = Deployed"]
-[9.750688552856445, 4.481166362762451, "[TT] Spin System Rate of the Starshine-2 = 5\u00ba/s"]
-[7.1552510261535645, 7.138506889343262, "[TT] Compressed Pulse Width of the ALT = 3.125 ns"]
-[8.442790031433105, 0.8826600313186646, "[TT] Utilization of the ICI-1 = Water vapor profile and snowfall"]
-[8.17944049835205, 7.869749069213867, "[FF] Key Technology Elements of the MWIR Sensor = Integrated micro-cryocooler and a high temperature nBn based 1-Megapixel focal plane"]
-[7.073896884918213, 2.343064546585083, "[FF] Field of View of the Solar-B / Hinode = Unknown"]
-[9.441703796386719, 6.239031791687012, "[TT] Scan Angle of the ScaRaB = 100\u00ba"]
-[5.614451885223389, -1.913649559020996, "[TT] Repeated ground track of the KOMPSAT-3A = 28days/409revolutions"]
-[4.535195827484131, 1.557344913482666, "[TT] Mission Date of the FedSat = 1998"]
-[3.9774818420410156, 4.482483386993408, "[FF] Applications of the SAR Satellites = Defense and intelligence, supply chain, insurance, maritime"]
-[8.05160140991211, -0.1298864334821701, "[TT] Body Condition Scale of the Polar Bears = 1 to 5"]
-[10.286693572998047, 5.711245536804199, "[TT] Operating Temperature of the CCD = 155 K"]
-[10.820093154907227, -0.2556585967540741, "[TT] Horizontal Sampling of the TanDEM-X = 12 m by 12 m"]
-[8.551340103149414, 7.380619049072266, "[TT] Gain Levels of the eROSITA pnCCD detector = 16 discrete levels"]
-[8.005759239196777, 0.8766085505485535, "[FF] Forecasted Drought Impacts of the GEOGLAM Crop Monitor = Potential drought impacts on wheat production"]
-[5.390632152557373, 8.174370765686035, "[TT] Sensor Type of the IME-HF instrument = Double-wire Hertz dipole"]
-[5.177939414978027, 0.5329113602638245, "[TT] Mission Support Start Date of the RRA = 1 May 2002"]
-[7.025082111358643, 2.439838409423828, "[FF] Imagery of the ResourceSat-2 LISS-3 = Data"]
-[11.138435363769531, 5.24825382232666, "[FF] In-flight Performance of the Gas Scintillation Proportional Counter = Unknown"]
-[4.846041679382324, 8.207319259643555, "[TT] System Bandwidth of the Radar = 19 MHz"]
-[12.139922142028809, 2.9771158695220947, "[TT] Propulsion System of the Jason-3 = Hydrazine"]
-[16.551036834716797, 3.643813371658325, "[TT] Total Satellites of the OneWeb = 218"]
-[8.336162567138672, 2.497678518295288, "[TT] Observation of the CATS = Aerosol Vertical Distribution"]
-[10.885723114013672, 7.448872089385986, "[TT] Swath of the FRS-1 = 25 km"]
-[8.793957710266113, 2.352011203765869, "[TT] Dust Grain Width of the COSIMA = About 50 \u00b5m and 70 \u00b5m"]
-[13.220552444458008, 7.235012054443359, "[TT] Power Consumption of the WFI = 70 W"]
-[9.588449478149414, 8.338293075561523, "[TT] Ion Acceleration of the Extraction Lens = 20 kV"]
-[7.8405537605285645, 2.114835262298584, "[FF] Mission Objective of the PACE = Measure ocean color and have secondary objectives"]
-[10.06213665008545, 7.565844535827637, "[TT] Mirror Tilt of the Telescope = Approximately 4.5\u00ba"]
-[3.6690304279327393, 6.3601155281066895, "[TT] Antenna Aperture of the XPAA = 8 x 8 array of modules"]
-[2.8880128860473633, 2.413144826889038, "[FF] Function of the Copernicus Sentinel-5P = Maps a multitude of air pollutants around the globe"]
-[9.714906692504883, -0.6610594987869263, "[TT] Injection Orbit Lower Than Target Orbit of the PSLV-C15 = 33 km"]
-[10.33491039276123, 4.518186569213867, "[TT] Reaction Wheels Capacity of the AlSat-2 = 0.12 Nms"]
-[12.224635124206543, -0.2025710791349411, "[TT] Camera Capture Interval of the TESS = Every 10 minutes"]
-[14.276415824890137, 3.2097890377044678, "[TT] Mass of the Teplo = 10 kg"]
-[3.7235794067382812, 6.656046390533447, "[TT] IFOV (beam width) of the Antenna = 0.94\u00ba"]
-[6.797573566436768, 5.0860981941223145, "[FF] ICU of the ASCAT = Instrument Control Unit"]
-[9.406357765197754, -0.7705325484275818, "[TT] Orbit Parameters of the GEOS-3 = 816 km x 850 km x 115.0\u00ba"]
-[7.550009727478027, 2.067505359649658, "[FF] Data Validation of the TanDEM-X = Used additional remote sensing data to validate the calculated results and differentiate forest areas from non-forested regions"]
-[3.2709755897521973, 3.839097499847412, "[TT] Formation Maintenance of the TanDEM-X and TerraSAR-X = 3 months"]
-[7.836909294128418, 8.693336486816406, "[TT] Spectral Bands of the Microbolometer Array = 3.8, 10.85, and 11.85 \u00b5m"]
-[13.274396896362305, 7.272202491760254, "[TT] Power Requirement of the MTVZA-GY = 80 W"]
-[8.63459587097168, 3.7614316940307617, "[FF] Objective of the APD detector = Observe the low energy charged particle density distribution in LEO (Low Earth Orbit)"]
-[6.659468650817871, 5.71530294418335, "[TT] Number of Essential Ground-Support Equipment Containers of the BepiColombo = Approximately 40"]
-[4.37608003616333, 1.8276606798171997, "[TT] First Image Delivery Date of the PeruSAT-1 = October 5, 2016"]
-[4.59129524230957, 1.5050348043441772, "[TT] Development Date of the FedSat = 1998"]
-[3.5050923824310303, 2.328340768814087, "[FF] Relation to Sentinel-4A of the Sentinel-4B = Follow up satellite"]
-[4.5225300788879395, 7.578977584838867, "[FF] Modulation Type of the Downlink Modulation = EO slice"]
-[14.271456718444824, 3.1282036304473877, "[TT] Mass of the SCCO = 28 kg"]
-[7.834009647369385, 7.504050254821777, "[TT] Dynamic Range of the Imager = > 100"]
-[8.632970809936523, 1.215815544128418, "[FF] Function of the ACCS = Operating and monitoring the Aquarius Instrument's health"]
-[9.45772933959961, 6.170176029205322, "[TT] Angle Bin Interval of the PR = 0.71\u00ba"]
-[7.706462860107422, 0.71384596824646, "[FF] Regions of Interest of the Lunar Flashlight = Permanently shadowed and occasionally sunlit regions poleward of 80\u00ba S latitude"]
-[9.750476837158203, 5.900118350982666, "[TT] Projection of the CUTE = 23 arcminutes (23')"]
-[6.1687726974487305, 5.0579304695129395, "[FF] Main Control Capabilities of the Antenna = Providing the TM (Telemetry), Processing the TC (Telecommands), Controlling the switching on/off of the active subassemblies"]
-[6.372591018676758, 8.61241626739502, "[TT] Polarization of the MTVZA-GY = Horizontal"]
-[5.285048961639404, 1.3497380018234253, "[FF] Event of the SMOS = SMOS gains clearer view as illegal transmitters shut down"]
-[13.980033874511719, 3.0531575679779053, "[TT] Total Mass of the PSLV-C38 = ~955 kg"]
-[11.112677574157715, 3.0493149757385254, "[TT] Size of the SERPENS nanosatellite = 3U"]
-[6.938337802886963, 6.274402618408203, "[TT] Quantity of the SDEA instrument = 2"]
-[11.222355842590332, 0.9160280823707581, "[TT] Location of the LISA Pathfinder = L1 (Lagrangian Point 1)"]
-[3.3365042209625244, 5.066583156585693, "[FF] Imaging Modes of the SAR-RCM = Single or dual polarisation, quad-polarisation"]
-[8.727214813232422, -0.6668909192085266, "[TT] Data Resolution of the ICEYE-X1 = 10 x 10 meters"]
-[3.844226837158203, 1.344052791595459, "[TT] First Stage Landing Location of the Falcon 9 = \"Just Read the Instructions\" droneship, Pacific Ocean"]
-[5.357226371765137, 6.896966457366943, "[TT] Global Average Detection Rate of the COM DEV NTS Receiver = 14.8 Messages/s"]
-[9.950933456420898, 8.188811302185059, "[TT] Focal Length of the AEISS = 8.6 m"]
-[5.355287551879883, 6.611734867095947, "[TT] Payload Data Storage of the MERLIN = Increased"]
-[5.9989519119262695, 1.048820972442627, "[FF] Presentation Date of the Compact Infrared Camera (CIRC) = June 2-8, 2013"]
-[9.25910472869873, 1.0126746892929077, "[TT] Number of Orbits around Jupiter of the Juno = 35 times"]
-[4.661856651306152, -0.048851530998945236, "[TT] End of Life Date of the TechnoSat = Operational as of February 2023"]
-[4.56952428817749, 0.4160483181476593, "[FF] Installation Date of the STP-H7 and H8 = Unknown"]
-[7.050613880157471, 7.000447750091553, "[TT] Laser Type of the Laser Head Unit (LHU) = Narrow linewidth NPRO laser"]
-[7.678961277008057, 9.406171798706055, "[TT] Center Wavelength of the Band 14 = 11.2 \u00b5m"]
-[6.945704460144043, 4.109077453613281, "[FF] Interface of the Formation Flying Computer = Propulsion system and GPS receiver"]
-[7.101490020751953, -0.18532751500606537, "[TT] Number of Orbits of the Envisat = 10,000"]
-[9.285868644714355, 8.682896614074707, "[TT] Dimensions of the Slits = 84 \u00b5m x 44.1 mm"]
-[9.560458183288574, 0.4295332133769989, "[TT] Distance Range of the MCAM-3 = Approximately 984 km \u2013 6194 km"]
-[4.240802764892578, 7.199416637420654, "[TT] Type of the Ka-band payload = Circularly polarized"]
-[5.641860008239746, 0.8136482238769531, "[FF] Calibration and Validation Approach Date of the Envisat = Oct. 2000"]
-[3.8803956508636475, 6.342733383178711, "[TT] Antenna Quantity of the Ground Segment = 2"]
-[7.936634540557861, 8.630298614501953, "[TT] SWIR Spectral Range of the GLI = 1050 - 2215 nm"]
-[5.082871437072754, 2.779871702194214, "[TT] Workshop Location of the SUM = Cal Poly State University, San Luis Obispo, CA, USA"]
-[9.129329681396484, 2.8118927478790283, "[FF] Publication Date of the Submerged Sources of Transient Acoustic Emission from Solar Flares = 20 September 2020"]
-[6.495880126953125, 6.2565484046936035, "[TT] Manufacturer of the Laser Communication Terminal (LCT) = Airbus subsidiary Tesat Spacecom"]
-[5.3235249519348145, 7.386754989624023, "[TT] Bandwidth of the Communication Bus = 100 Mbit/s"]
-[8.7567777633667, 7.182179927825928, "[TT] Camera of the OPS-SAT = High-resolution"]
-[6.84604024887085, 6.0858378410339355, "[TT] Daily Global Composite Products of the PROBA-V = 728"]
-[9.783317565917969, 3.944523811340332, "[FF] Design of the MAG Instrument = \"Dual mag\" implementation of two identical racetrack magnetometers on a 6-meter boom"]
-[4.757338523864746, 2.7758240699768066, "[TT] Founder of the Kleos Space = Luxembourg government"]
-[6.2499566078186035, -0.237634539604187, "[TT] Operation Duration of the EXCISS = In the first hour"]
-[3.486882209777832, 5.296212673187256, "[FF] Function of the SAR Antenna Assembly = The SAA is an active phased array and it is able to operate different beam characteristics for transmission and reception"]
-[12.01175594329834, -0.32953768968582153, "[TT] NASA Feature Date of the TESS = 12 February 2021"]
-[10.129634857177734, 3.074582815170288, "[FF] X-SAT Saturn-Class Platform Adapter of the Blue Canyon Technologies = Unknown"]
-[9.433996200561523, 8.236091613769531, "[TT] IFOV cross-track of the Full-scan Imaging = 0.3\u00ba"]
-[4.6618218421936035, 3.8997642993927, "[TT] Number of Cicero Satellites of the GeoOptics = At least two"]
-[5.345727920532227, 2.693455457687378, "[TT] Affiliation of the OSCAR-QUBE = Hasselt University (Belgium)"]
-[13.203269958496094, 7.404486179351807, "[TT] DC Power Consumption of the Channel = 50 W"]
-[13.926995277404785, 7.170335292816162, "[TT] Potential Difference of the DSLP = A few tenths of Volts"]
-[6.85741662979126, -0.4944206774234772, "[TT] Orbit Repeat Cycle of the Altimetry Satellites = Every ten days"]
-[13.199212074279785, 5.531085014343262, "[FF] Components of the Solar Panels (SPs) = Photovoltaic assembly, solar panel deployment mechanisms, PDM (Pyro Drive Module) electronics"]
-[5.434998989105225, 7.556492328643799, "[FF] Bandwidth of the OCM = Not specified"]
-[6.303849220275879, 5.702301025390625, "[TT] Quantity of the On-board computers = 2"]
-[9.181198120117188, 4.921099662780762, "[FF] Purpose of the Attitude Determination Quaternion Filter = Perform spacecraft attitude tests in LEO"]
-[4.135874271392822, 0.6736416220664978, "[TT] Autonomous Functionality of the INTEGRAL = Yes"]
-[5.97951602935791, 3.1239426136016846, "[TT] Acquirer of the JPSS-1 = NOAA (National Oceanic and Atmospheric Administration)"]
-[8.103516578674316, 2.1657395362854004, "[FF] Cross-Calibration of the CloudSat = Additional Funds"]
-[3.9662439823150635, 6.350896835327148, "[TT] Connector Type of the Antennas = MMCX"]
-[7.6819539070129395, 4.473266124725342, "[FF] Silicon Tracker of the AMS-02 = Constant Temperature"]
-[6.128683567047119, 4.2799577713012695, "[FF] Ground Segment Architecture of the RCM = Modular distributed system"]
-[10.589226722717285, 6.709730625152588, "[TT] Ion Concentration Factor of the Electrostatic Mirror = >20"]
-[9.41455078125, -0.489665150642395, "[TT] Orbit Altitude of the MEOSAR satellites = 19,000 to 24,000 kilometers"]
-[7.339306354522705, 6.148403644561768, "[TT] Time Synchronization Accuracy of the Data Handling Subsystem = < 10 \u00b5s"]
-[11.824464797973633, 4.74058723449707, "[TT] Platform Size of the Tsubame = 45 cm x 45 cm x 56 cm (H)"]
-[13.893054008483887, 7.216721534729004, "[TT] Power Supply of the Coarse Lateral Sensor = Unregulated 28 V"]
-[9.353485107421875, 6.031667709350586, "[FF] Emissivity of the Calibration Mirror = Near-perfect zero radiance reference"]
-[6.474521636962891, 3.76243257522583, "[FF] Approach of the Development Plan = Classical V-approach"]
-[9.45616340637207, 6.905704021453857, "[TT] Down-track Resolution of the MAHRSI = 8\u00ba - 12\u00ba"]
-[10.123411178588867, 6.96327543258667, "[TT] Along-track Segment Duration of the SIMPL = 0.125 s"]
-[11.665117263793945, 3.3833351135253906, "[FF] Components of the Stack Level = MPO (and Japanese orbiter MMO), MTM ion propulsion with twin thruster operation"]
-[10.368942260742188, 4.4956560134887695, "[TT] Number of Wheels of the Reaction Wheels = 3"]
-[5.1166863441467285, 3.2195205688476562, "[TT] Designer of the CIXS = RAL (Rutherford Appleton Laboratory), UK"]
-[9.73973274230957, 0.8132447004318237, "[TT] Orbital Speed of the Cluster spacecraft = Up to 23,000 km/h"]
-[9.533367156982422, 7.1742682456970215, "[TT] Resolution of the Spatial resolution at nadir = 1 km"]
-[7.707408905029297, 0.7117465734481812, "[FF] Volume of the Lunar Flashlight = 255"]
-[7.679304599761963, 4.968208312988281, "[FF] Observation Results of the RSI = Significant"]
-[5.029983997344971, 5.021051406860352, "[TT] Quantity of the GPS Receivers = 2"]
-[14.099512100219727, 3.230445384979248, "[TT] Mass of the HID = 2.2 kg"]
-[6.853004455566406, 6.462536811828613, "[TT] Processing Time of the Ortho = 90 s"]
-[5.676974773406982, 2.47745943069458, "[TT] Managing Entity of the MoonLIGHT = ESA"]
-[8.313596725463867, 7.182309150695801, "[TT] Technology of the Supervision Cameras = COTS"]
-[9.513388633728027, 8.178037643432617, "[TT] Field of View of the LWIR Camera = 1\u00ba x 1\u00ba"]
-[8.623515129089355, 7.901951789855957, "[TT] Spectral Pixel Size after Binning (x1) of the ISRF = 28 \u00b5m"]
-[6.162116527557373, 1.1518641710281372, "[FF] Image Pair Date of the Satellite = September 2020 (left) and February 2021 (right)"]
-[7.638728618621826, 8.74533462524414, "[TT] Spectral Ranges of the MSU-SK = 0.5 - 0.6, 0.6 - 0.7, 0.7 - 0.8, 0.8 - 0.9 \u00b5m"]
-[4.64937162399292, 0.5861579179763794, "[TT] Launch Year of the GOES-U = 2024"]
-[6.396632671356201, 5.034156322479248, "[FF] Function of the DPCC = Stop internal processing if request is deleted"]
-[7.3176350593566895, 1.997395396232605, "[FF] Imagined View of the Planet Kepler-10b = Artist's depiction"]
-[5.729990482330322, 3.811065912246704, "[FF] Satellite Configuration of the OptiSAR\u2122 Constellation = 8 X- and L-band SAR satellites and 8 high-resolution optical satellites"]
-[6.616543769836426, 1.0215002298355103, "[TT] Spotting Date of the Neil Gehrels Swift Observatory = March 12"]
-[3.681966543197632, 6.655126571655273, "[TT] Azimuth Width of the Transmitting Beam of the UF Mode = Broadened 1.7 times"]
-[5.0154805183410645, 0.7448127269744873, "[FF] Close-Up Date of the Arrokoth = 13 February 2020"]
-[8.626410484313965, 4.690335273742676, "[FF] Function of the ASTERIA = Holds the temperature of the telescope detector constant"]
-[4.790942668914795, 0.006642848253250122, "[TT] End of Life Date of the COMS = 1 April 2021"]
-[5.087791919708252, 2.3055427074432373, "[TT] Mission Type of the LunIR = Non-EO"]
-[5.861049175262451, 1.8150091171264648, "[TT] Return Date of the Orion = Sept. 1, 2015"]
-[10.090429306030273, -1.5643149614334106, "[TT] Inclination of the GCOM-C = 98.6\u00ba"]
-[4.739404678344727, 0.5193484425544739, "[TT] Launch Date of the SARAL = 2012"]
-[6.174546241760254, 2.1683831214904785, "[FF] Award of the eROSITA = Marcel Grossmann Award"]
-[6.36892032623291, 8.18670654296875, "[TT] Pass Band Channels of the DCS = 66"]
-[12.070674896240234, 3.673226833343506, "[TT] Pressure Change of the Airtight Vessel = 1.6%"]
-[8.368285179138184, 7.173445224761963, "[TT] Quantity of the Monitoring Cameras (CAM) = 3"]
-[5.807937145233154, 1.531160593032837, "[TT] Ground Station Operators of the ASTERIA = Half-dozen talented students"]
-[8.443178176879883, 2.121839761734009, "[FF] Calibration/Validation of the WindSat = Special Issue (18 papers) on the WindSat Spaceborne Polarimetric Radiometer -Calibration/Validation and Wind Vector Retrieval"]
-[5.083915710449219, 1.9309792518615723, "[TT] Status of the Carmen 1 = Fully operative"]
-[6.830235004425049, -0.47717392444610596, "[TT] Measurement Frequency of the Dark Reference = Every 2\u20133 orbits"]
-[13.744009971618652, 5.377878189086914, "[TT] Quantity of the Dual-junction solar cells = 13 strings of 40 GaAs cells"]
-[7.969462871551514, 4.310208797454834, "[FF] Mission of the MTCube-2 = Study the effects of radiation on electronic systems"]
-[9.268242835998535, 4.34057092666626, "[FF] Solar panel pointing of the TanSat = -Xs points to the sun, Ys is parallel to Earth equator plane"]
-[7.145548343658447, 8.279630661010742, "[TT] SNR in Nadir of the ELVIS = >500"]
-[9.84854793548584, 7.830074787139893, "[TT] Line Step of the Telescope = 224 \u00b5rad in N-S direction"]
-[5.705960273742676, 7.127883434295654, "[TT] Data Rate of the Resurs-O1-4 = 15.36 or 61.44 Mbit/s"]
-[10.231664657592773, 6.13341760635376, "[TT] Temperature Range of the LWIR Cameras = -59\u00b0C to 113\u00b0C"]
-[5.443367004394531, 0.38588449358940125, "[FF] Article Date of the Clyde Space Rocket = Feb. 1, 2011"]
-[4.280303001403809, 0.939984917640686, "[FF] Voyage Article Date of the Argo = Feb. 28, 2002"]
-[6.020412445068359, 1.5009002685546875, "[TT] Anniversary of the Swarm = 4th"]
-[4.1214823722839355, 1.386187195777893, "[TT] Date of Malfunction of the MeteoSat-8 = Oct. 17, 2002"]
-[5.8224287033081055, 7.2298808097839355, "[TT] Isp of the BIT-3 system = 1,400-2,640 s"]
-[4.714295387268066, 1.5562090873718262, "[TT] Launch Date of the GCOM-C = 23 December 2017"]
-[5.8885602951049805, 2.3592634201049805, "[TT] Image Source of the PLEGPAY = ESA"]
-[5.1176066398620605, 1.933077335357666, "[FF] Transportation of the Genesis Sample Return Capsule = Flown to Ellington Field in Houston, then shipped by van for the short ride to JSC"]
-[6.451687335968018, 0.0009514898410998285, "[TT] Patent Number of the Helix Orbit = EP 1 273 518 A2"]
-[11.724660873413086, 3.374605894088745, "[FF] Development Date of the Resistojet Thruster Propulsion Systems = Aug. 11-14, 2003"]
-[10.412837028503418, 5.713888645172119, "[FF] Record Temperature of the Concordia station = -11.8\u00baC"]
-[5.263984203338623, 2.25268816947937, "[FF] Mission Type of the ITASat-1 = EO"]
-[6.834181308746338, 6.372206687927246, "[TT] Operation Time of the HPS = Under 10 minutes"]
-[11.95862865447998, -0.15455234050750732, "[FF] Research Area of the TESS = Asteroseismology"]
-[8.651942253112793, 1.0997298955917358, "[FF] Publication Date of the Aquarius = July 2007"]
-[5.585855960845947, 3.8893978595733643, "[TT] Constellation Size of the NewSat = 38 operating satellites"]
-[9.234861373901367, 4.967408180236816, "[TT] Number of Algorithms of the Attitude Determination Quaternion Filter = Four"]
-[8.083441734313965, 8.19764232635498, "[FF] Channels of the VISSR = Water vapor (6.5 - 7.0 \u00b5m), Infrared (10.5 - 11.5 \u00b5m), Infrared (11.5 - 12.5 \u00b5m)"]
-[16.491952896118164, 3.580312490463257, "[TT] Launch Date of the OneWeb = 2022"]
-[7.4344162940979, -0.17203110456466675, "[TT] Instrument Operation Time of the Philae = First 60 hours following the touch-down"]
-[10.233319282531738, 6.170192718505859, "[TT] Slew Rate Enhancement of the NuSTAR = Factor of two"]
-[13.37770938873291, 6.848445892333984, "[TT] Payload Power of the Spacecraft = 32 W"]
-[11.317987442016602, 5.813222885131836, "[TT] Seal Material of the Sample Container = Aluminum metal"]
-[11.009016990661621, 3.613201856613159, "[TT] Size of the PhiSat-1 = About the size of a cereal box"]
-[6.138681888580322, 4.037403106689453, "[FF] Use Case of the Bidirectional IoT = Water management systems control"]
-[6.055136203765869, 1.7254213094711304, "[TT] Mission Selection Date of the Euclid = October 2011"]
-[8.062725067138672, 8.08881664276123, "[TT] Spectral Band of the Band Cameras = 762.4 nm"]
-[10.155701637268066, 5.355551719665527, "[TT] Displacer Unit of the Stirling Cycle Cooler = Single, similarly driven, displacer unit orthogonal to the compressor axis"]
-[4.184464931488037, 2.5540995597839355, "[TT] Launch Site of the SMART-1 = Kourou, French Guiana"]
-[8.530189514160156, 5.320613384246826, "[TT] Accelerations of the GPS Receiver = Up to 20 g"]
-[10.541667938232422, 7.341156482696533, "[TT] GSD of the Instrument = 32m to 22m"]
-[6.762884140014648, 4.248111248016357, "[FF] Design Philosophy of the SMEX = Emphasis on design simplicity, functional independence at subsystem level, and flexibility to accommodate growth"]
-[8.078935623168945, 8.61005687713623, "[TT] Wavelength Range of the VNIR Filter Assembly = 443 nm to 945 nm"]
-[8.666943550109863, 8.850203514099121, "[TT] Grating Structure of the OCO-3 = Very regularly-spaced series of grooves on a very flat surface"]
-[13.785147666931152, 6.942745685577393, "[TT] Potential of the SCM = Near 200 V"]
-[8.100560188293457, 3.610501766204834, "[TT] Instrument Type of the ILAS = Atmospheric chemistry"]
-[5.416234970092773, 3.952639579772949, "[TT] Number of Satellites of the FY-3 = 4"]
-[10.256255149841309, 1.676032543182373, "[FF] Observation Target of the eROSITA = Galaxy Clusters, Active Galactic Nuclei, X-ray Sources, Double Stars, Supernovae, Neutron Stars"]
-[10.011687278747559, 7.5431647300720215, "[TT] Swath Width of the Pushbroom imager = 10.15 km"]
-[11.015429496765137, 2.059326171875, "[FF] Announcement Date of the XMM Newton = 04 February, 2000"]
-[8.900861740112305, 6.854874134063721, "[TT] Number of CMEs Observed of the SMEI = Over 200"]
-[4.836042881011963, 0.25811484456062317, "[TT] Launch Date of the SPOT-6 = September 2012"]
-[5.11433744430542, 5.0449724197387695, "[TT] Quantity of the Space GPS Receivers = 1"]
-[13.338924407958984, 6.485713481903076, "[TT] Predicted Pmp at EOL of the KOMPSAT-6 = 2,258 W"]
-[7.165573596954346, 2.6092419624328613, "[FF] Focus of the Elecnor Deimos = Development of future internet technologies to improve Earth Observation Data processing and distribution"]
-[5.347991943359375, 6.163447380065918, "[TT] Processor Speed of the Safe-mode Computer = 400 MHz"]
-[12.097428321838379, 4.506782531738281, "[TT] Dimensions of the DART spacecraft with ROSA = 12.5 meters by 2.4 meters"]
-[5.293972015380859, 2.6014015674591064, "[FF] Affiliation of the ITUpSat-1 = Istanbul Technical University"]
-[8.563323020935059, 3.2893645763397217, "[FF] Measured Parameters of the Special Sensor Ultraviolet Spectrographic Imager (SSUSI) = Composition of the upper atmosphere and ionosphere"]
-[7.794593811035156, 8.730390548706055, "[TT] Spectral Region of the ERIP = 252 - 340 nm"]
-[8.681824684143066, 5.874092102050781, "[TT] Positional Accuracy of the System = 1-meter CE90 when suitable elevation data is available"]
-[7.650379180908203, 0.47321614623069763, "[TT] Flight Computer of the Lunar IceCube = Proton 400K made by Space Micro, Inc."]
-[5.557001113891602, -1.9137426614761353, "[FF] Support Plan of the KOMPSAT-2 = Support key technologies for application in the private sector and to promote the relevant industries"]
-[9.626704216003418, 8.251459121704102, "[TT] Field of View of the BIROS = 19.6\u00ba"]
-[6.797972679138184, 6.149924278259277, "[TT] Location of the OSIRIS laser communications terminal = Bartolomeo from 2021"]
-[9.180071830749512, 3.109846830368042, "[FF] Objective of the SWOOPS = Observation of the solar-wind flow at middle-to-high solar latitudes for the construction of a representative model of the heliosphere"]
-[9.369686126708984, 6.051691055297852, "[TT] Cross-Track Pointing of the HRG Sensors = \u00b1 27\u00b0"]
-[8.972115516662598, 3.384570598602295, "[FF] New Finding of the Plasma Sheet = Higher-energy O+ (1\u201310 keV) ions"]
-[10.050741195678711, -1.5456044673919678, "[TT] Inclination of the Ariane 5 = 20 degrees"]
-[10.737699508666992, 6.521141529083252, "[TT] Multilayer Thickness (layer 1-89) of the Mirror = ~0.7 \u00b5m"]
-[6.944093704223633, 6.3274736404418945, "[TT] Number of Windows of the Windowed Mode = Up to eight"]
-[4.341991424560547, 7.045759201049805, "[TT] Frequency Band of the AIS = VHF"]
-[11.062356948852539, 3.6495161056518555, "[TT] Size of the CubeSats = 10 cm x 10 cm x 15 cm"]
-[5.309254169464111, 7.692324161529541, "[FF] Transmit Signal Distribution of the PAA (Power Amplifier Assembly) = Distributes low power transmit signal pulses to each T/R module"]
-[13.28400707244873, 7.298470973968506, "[TT] Power Consumption of the STAFF/DWP = 4.5 W"]
-[7.757077693939209, 1.7302148342132568, "[TT] Regeneration Percentage of the Mangrove Forests = 2 percent"]
-[8.010804176330566, 0.11234326660633087, "[TT] Measurement Type of the GRACE = Satellite gravimetry"]
-[8.288776397705078, 3.07377290725708, "[FF] Objectives of the MAESTRO = Measuring ozone, nitrogen dioxide and aerosol/cloud extinction in the atmosphere"]
-[10.04709529876709, 3.1432995796203613, "[FF] Survey Date of the CubeSat Communication Systems = April 18, 2008"]
-[5.5860066413879395, 3.855471611022949, "[TT] Number of Retired Satellites of the DMSP (Defense Meteorological Satellite Program) = 16"]
-[10.461524963378906, 6.912771224975586, "[TT] Focal length of the Mirror = 1600 mm"]
-[9.717212677001953, 8.460862159729004, "[TT] FOV of the BIRCHES instrument = 100 mrad (6\u00ba)"]
-[6.496066570281982, 1.6913857460021973, "[FF] URL of the EO-1 = http://ase.jpl.nasa.gov/public/papers/chien_aamas2005_lessons.pdf"]
-[9.402668952941895, 8.129355430603027, "[TT] Optics System of the Collecting Optics = f/5"]
-[8.618132591247559, 6.027891635894775, "[TT] Accuracy of the CESS = ~5\u00ba"]
-[5.224271774291992, -1.2266757488250732, "[TT] Launch Date of the Kondor-E1 = 19 December, 2014"]
-[6.019958019256592, 5.7703070640563965, "[FF] Qualification Program of the Virtex-4 FPGA = Undergoing vibration and thermal cycling tests"]
-[9.36350154876709, 9.122641563415527, "[TT] Near-UV Channel Spectral Resolution of the IRIS = 8 x 10-3 nm"]
-[5.389721393585205, 7.849513530731201, "[TT] RF Power of the Ka-band Channels = 46 W/channel"]
-[13.720357894897461, 5.401179790496826, "[TT] Solar Cells of the SCARAB = Spectrolab triple-junction CIC solar cells (body-mounted)"]
-[5.186748027801514, 0.5621907711029053, "[FF] Project Overview Date of the TSIS-1 = Nov. 10-13, 2015"]
-[8.726205825805664, 6.094098091125488, "[FF] Instrument Type of the SOLSE-2 = Limb scattering instrument"]
-[10.631733894348145, 6.500988006591797, "[TT] MA-CA pairs of the eROSITA = 7"]
-[6.206103324890137, -0.27596738934516907, "[TT] Duration of the BLT = Three to four months"]
-[3.5071394443511963, 1.7420614957809448, "[TT] Mission Status of the Sentinel-5P = Pre-operational"]
-[5.758160591125488, 6.135103702545166, "[TT] Backup of the Instrument Processing Unit = Active"]
-[6.209955215454102, 1.7292046546936035, "[FF] Image Credit of the RISESat = RISESat consortium"]
-[7.292840003967285, 3.4726691246032715, "[TT] Observation Resolution of the TROPOMI = 49 km2"]
-[9.512206077575684, 7.085545539855957, "[TT] Resolution of the ABI = 1 km"]
-[4.1389007568359375, 3.6494390964508057, "[TT] Availability of the Galileo Service = > 99.5%"]
-[8.530653953552246, 4.58325719833374, "[FF] Components of the BepiColombo = Star trackers, spectrometer, magnetometer boom"]
-[9.313362121582031, 6.842793941497803, "[TT] Mass Resolution of the STROFIO = m/Dm = 60"]
-[14.191866874694824, 3.278795003890991, "[TT] Mass of the STAFF/DWP = 5.0 kg"]
-[7.262567520141602, 2.760282516479492, "[TT] Revisit Interval of the MethaneSAT = Seven days or less"]
-[11.583971977233887, 3.4100263118743896, "[FF] Components of the Ion engine = Ion generator, ion acceleration system, neutralizer, power sources, controller"]
-[10.644664764404297, 3.922410011291504, "[TT] Deployment Status of the Dragsail = Partial"]
-[6.008158206939697, 5.724621295928955, "[TT] Manufacturer of the Second FPGA = Xilinx"]
-[9.661502838134766, 4.417694568634033, "[FF] Publication Date of the Active magnetic attitude control algorithms for a CubeSat for astrophysics research = 2014"]
-[5.3815131187438965, 6.219571590423584, "[TT] Start-up ROM Capacity of the RAD750 SBC = 64 KB"]
-[8.575292587280273, 0.17548495531082153, "[FF] Encounter of the Solar Orbiter = First time that we have encountered a comet tail inside Earth's orbit"]
-[4.418352127075195, 1.8315318822860718, "[TT] Launch Date of the RADARSAT-2 = Dec. 14, 2007"]
-[6.102336883544922, 6.597723007202148, "[FF] Operation of the TTC Buffer = Constantly kept as full as possible"]
-[4.99367618560791, 7.666472911834717, "[FF] UHF Lithium-1 Radio of the RAX-1 = Performed extremely well"]
-[8.47591781616211, 8.158150672912598, "[TT] Detectors of the NIRSpec = Two"]
-[10.026598930358887, 7.743852138519287, "[TT] Lightweighting of the PP Twin Telescopes = Up to 72%"]
-[10.628012657165527, 7.326046943664551, "[TT] Swath Width of the Instrument = 19.3 km"]
-[6.0446672439575195, 7.279355049133301, "[TT] Sample Rate of the MGF = 160 per second"]
-[10.853899955749512, 7.44153356552124, "[FF] Diameter Range of the Kuiper Belt Object = 50 to 2,000 kilometers"]
-[7.4297285079956055, 4.568636417388916, "[FF] Objectives of the RVXC = Regulate the spacecraft translational and rotational states around the guidance reference; Compute commands for the spacecraft actuators, based on the processing of the control error"]
-[9.80636978149414, 4.280335903167725, "[TT] Magnetorquer Coils Max. Magnetic Dipole of the ADCS = 0.13 A m2"]
-[10.03145694732666, 2.9230966567993164, "[TT] Deorbiting Date of the CubeSats = 2 March 2019"]
-[7.634639739990234, 1.0257834196090698, "[FF] Conference Presentation Date of the Gravity Recovery and Interior Laboratory (GRAIL) = March 18-22, 2013"]
-[5.0592451095581055, 1.374597191810608, "[FF] Conference Presentation Date of the GIOVE-A = Sept. 26-29, 2006"]
-[6.850086212158203, 6.322328090667725, "[FF] Beam Splitter of the OBA = Unknown"]
-[9.442085266113281, 4.512938499450684, "[TT] Primary Attitude Sensor of the ADCS = Magnetometer"]
-[6.1667585372924805, 1.7773663997650146, "[FF] URL of the IAC-18-C1.5.10 = https://iafastro.directory/iac/proceedings/IAC-18/IAC-18/C1/5/manuscripts/IAC-18,C1,5,10,x47313.pdf"]
-[12.032225608825684, 4.524448394775391, "[TT] Size of the Spacecraft = 21 m length, 1.5 m diameter"]
-[4.747934341430664, -1.8161542415618896, "[TT] Landing Date of the Chang'e-3 = December 2013"]
-[8.481788635253906, 6.047722339630127, "[TT] Range Precision Requirement of the GFO-RA = 3.5 cm"]
-[4.77155876159668, 0.5030430555343628, "[TT] Launch Date of the GOES-T = 1 March 2022"]
-[8.494220733642578, 0.1870550960302353, "[FF] Dust Trail of the Wirtanen = A field of larger debris that traces the comet\u2019s orbital path as it travels around the sun"]
-[8.254598617553711, 8.34572696685791, "[FF] Straylight Rejection of the VNIR Detector = High"]
-[4.016517639160156, 2.166616678237915, "[TT] Launch Vehicle of the GOES-S = Atlas V 541 rocket"]
-[8.63766098022461, 4.245615005493164, "[TT] Sensor Type of the AeroCube-11B/TOMSat R3 = Multispectral"]
-[11.84904670715332, 6.695713043212891, "[FF] Energy Levels of the MEPED = Electrons: 30-7000 keV, Protons: 30 - 6900 keV, Above >16, >35, >70, >140 MeV"]
-[10.062533378601074, -1.5455378293991089, "[TT] Inclination of the SPROUT = 97.9\u00ba"]
-[11.483590126037598, 4.915633201599121, "[FF] Size of the BIROS = About the size of a washing machine"]
-[2.8984262943267822, 4.462582111358643, "[TT] Chirp Signal Management of the ALOS-2 PALSAR-2 = Up/down chirp signals alternatively"]
-[10.930426597595215, 2.088897943496704, "[TT] Observation Duration of the XMM-Newton = 18 days"]
-[6.360779285430908, 6.282951354980469, "[TT] Maximum Event Processing Rate of the FPGA-embedded microprocessor = 400 cps"]
-[11.998400688171387, 3.293318748474121, "[TT] Propellant of the Busek\u2019s miniaturized electric thrusters = Iodine"]
-[13.834024429321289, 2.6554737091064453, "[TT] Launch Mass of the KPLO = Approximately 678 kg"]
-[6.284759998321533, 8.050741195678711, "[TT] Channels of the FCI = 16"]
-[10.107194900512695, 1.9312392473220825, "[FF] Black Hole Jet Discovery Date of the Chandra X-ray Observatory = 9 January 2019"]
-[5.567171573638916, 7.415043354034424, "[TT] G/T of the SDR-VSAT = > 24.5 dB/K"]
-[8.900091171264648, -0.35714492201805115, "[TT] Inclination of the Meteor-M2 = 98.8\u00ba"]
-[8.54918098449707, 1.4419158697128296, "[TT] Quantization Levels of the Cloud water = 0.05"]
-[12.05344009399414, 6.288355827331543, "[FF] Measurement of the AMS = Electron flux and positron flux"]
-[8.087834358215332, -0.5624558925628662, "[FF] Event of the Land Glacier = Part of the glacier\u2019s ice tongue crumbled away"]
-[5.354402542114258, 1.381361722946167, "[FF] Conference Date of the CHIPS = Aug. 11-14, 2003"]
-[4.766234397888184, -1.7781989574432373, "[FF] Operation Status of the Chang'e-3 = Devices still work well"]
-[11.515107154846191, 4.709983825683594, "[TT] Board Standard of the MuREM = PC104"]
-[8.643534660339355, 5.292812347412109, "[TT] Resolution of Accelerometer Measurements of the Three-axis diagonal gradiometer = < 2.0 x 10 -12  m s -2  Hz -1/2"]
-[5.373449802398682, 7.658535957336426, "[TT] Maximum Firing Rate of the CU = 55 Hz"]
-[5.531852722167969, 6.146997928619385, "[TT] Data Transmission Mode of the Satellite = Recording (R) with subsequent reproduction(DR)"]
-[6.222690105438232, 7.947454452514648, "[FF] Downlink Channels of the MDD = 4"]
-[5.028740406036377, 3.6824989318847656, "[TT] Backup Satellite of the Sentinel-2 = 1"]
-[8.386137008666992, 2.910477638244629, "[FF] Measurement Category of the Kolibri-2000 = Radiation budget, Gravity, Magnetic and Geodynamic measurements"]
-[4.7136616706848145, 0.010977549478411674, "[TT] End of Life Date of the GEOSAT = January 1990"]
-[6.338210582733154, 4.134535789489746, "[FF] Payload of the Satellite = Unknown"]
-[7.789206504821777, 8.328113555908203, "[FF] Alignment and Testing of the NIRSpec Filter and Grating Wheel Assembly = Unknown"]
-[8.441276550292969, 3.5072457790374756, "[FF] Purpose of the CLARREO = Accurately measuring and attributing climate change"]
-[6.492024898529053, 5.062469959259033, "[FF] Type of the Data Flow = Continuous"]
-[7.359433650970459, 8.828202247619629, "[TT] Filter Type of the VIS channel = VIS 3"]
-[8.240753173828125, 3.4253270626068115, "[FF] Observed Emissions of the MIGHTI = O(1D)@630.0 nm, O(1S) @ 557.7 nm, 0-0 band of O2(b1Sg+) @762.0 nm"]
-[8.094183921813965, 6.426827430725098, "[FF] Imaging Instruments of the CBERS-4A = Unknown"]
-[13.306169509887695, 2.903944730758667, "[TT] Mass of the MethaneSAT = 350 kg"]
-[11.775187492370605, 5.009710311889648, "[TT] Size of the POLDER-P = 80 cm x 50 cm x 25 cm"]
-[10.76986026763916, 1.2160881757736206, "[TT] Density of the TOI-2337b, TOI-4329b, and TOI-2669b = From styrofoam-like to three times denser than water"]
-[9.576302528381348, 8.18140983581543, "[TT] Field-of-view of the CuPID = Wide"]
-[10.761234283447266, -1.1128077507019043, "[FF] Specific Goals of the SLATS = Verification of super low altitude satellite system, Measurement of atmospheric density in super low altitude, On-orbit monitoring of atomic oxygen"]
-[5.564528942108154, -1.9216439723968506, "[FF] Mission Status of the KOMPSAT-2 = Unknown"]
-[8.811285018920898, 6.407261848449707, "[TT] Height Measurement Accuracy of the ALT = \u00b1 10 cm"]
-[5.1459856033325195, 0.6661567687988281, "[TT] Meeting Date of the ICON = Dec. 3-7, 2012"]
-[4.778721332550049, 3.7247283458709717, "[TT] Country of Manufacture of the Antennas = Spain"]
-[5.8258538246154785, -0.7606651186943054, "[TT] Design Life of the Satellite = > 10 years"]
-[6.65742826461792, 0.7706540822982788, "[FF] Workshop Date of the Herschel = Dec. 17-18, 2009"]
-[3.4054248332977295, 5.103095531463623, "[TT] Operation Mode of the C-band synthetic aperture radar = Transmit-receive or receive-only"]
-[9.302797317504883, 4.236751079559326, "[FF] Orientation of the Solar Panels = Perpendicular to the sun direction"]
-[7.736435413360596, 5.6518473625183105, "[FF] Publication Date of the Nimbus-7 SBUV radiometer = 1988"]
-[5.562687873840332, 6.707635402679443, "[TT] Downlink Contact Duration of the IXPE = 8 minutes"]
-[4.622742652893066, 1.421840786933899, "[TT] Development Contract Date of the Alphasat = November 2007"]
-[6.50578498840332, 3.517103910446167, "[FF] Dynamic Range of the NOAA/AVHRR-2 = N/A"]
-[6.965818405151367, 5.847501754760742, "[TT] Number of PHM Clocks of the GIOVE-A = 2"]
-[6.087314128875732, 4.139709949493408, "[TT] Device Generalization of the COSMOS Software = All devices are simplified to their most general basics"]
-[7.889365196228027, 6.0915632247924805, "[FF] Lateral Movement of the CCRR = Twice the movement imaged on the lateral sensor"]
-[11.358869552612305, 4.9763360023498535, "[TT] Subaperture Radius of the PAIS = 0.2 mm"]
-[9.031291961669922, 7.507789611816406, "[TT] TIR Channel Resolution of the Imager = 4 km"]
-[7.63206672668457, 2.2129478454589844, "[FF] Function of the Landsat\u2019s Thermal Infrared Sensor (TIRS) = Find overwatering farms"]
-[4.414305686950684, -1.648088812828064, "[FF] Frequency of Stellar Mergers of the Blue Ring Nebula = Once every 10 years in our Milky Way galaxy"]
-[14.49824047088623, 6.659406661987305, "[TT] Type of the Lithium ion battery = Rechargeable"]
-[8.046075820922852, 0.566413164138794, "[FF] Authors of the Double Asteroid Redirection Test (DART) = Justin A. Atchison, Matthew Abrahamson, Martin T. Ozimek, Brian L. Kantsiper, Elena Y. Adams, Andrew F. Cheng, Andrew S. Rivkin, Cheryl L. Reed, Shyam Bhaskaran, Zahi Tarzi, Dianna Velez, Julie Bellerose, Frank Laipert, Daniel Grebow"]
-[10.384300231933594, 5.667247295379639, "[FF] Average High Temperatures in March of the Concordia station = Around -48\u00baC"]
-[8.139737129211426, 3.670353651046753, "[FF] Data Collection of the OCO-3 = Denser data set than OCO-2"]
-[5.826323509216309, 2.7388319969177246, "[TT] Funding Source of the CATS = International Space Station Program"]
-[13.301612854003906, 7.744065284729004, "[TT] Low Power Output of the VLF transmitter = 1 W"]
-[7.181554317474365, 6.9234490394592285, "[TT] Sun Exclusion Angle of the Metrology Laser = < 15\u00ba"]
-[10.091450691223145, 5.5710601806640625, "[TT] Accuracy Range of the Surface temperature = 2 K"]
-[13.403434753417969, 6.7762532234191895, "[TT] Power of the Spacecraft = 1260 W"]
-[7.934369087219238, 8.513772010803223, "[TT] Spectral Range of the Instrument = 5.0-15 \u00b5m (2000-667 cm -1)"]
-[8.50335693359375, 5.731547832489014, "[TT] Precision of the Onboard Receiver = <5 cm"]
-[8.435108184814453, 1.1588646173477173, "[TT] Spatial Resolution of the Solid Earth Lithosphere and upper mantle density structure = 100 km"]
-[4.66992712020874, 8.293022155761719, "[TT] Center Frequency (GHz) of the Antenna = 19.35"]
-[9.902297019958496, -0.40121275186538696, "[TT] Satellite Altitude of the MXT = 600 km"]
-[9.016607284545898, 5.301459312438965, "[TT] Attitude Uncertainty Bounds of the GOMX-3 = 1\u03c3 (68%)"]
-[9.78248119354248, -0.5560896992683411, "[TT] Orbital altitude of the FTS = 613 km"]
-[10.404353141784668, 2.0264384746551514, "[TT] Dynamic Range of the eROSITA X-ray telescope = More than one billion"]
-[10.109551429748535, -1.488081455230713, "[TT] Orbit Inclination of the CartoSat-2D = 97.44\u00ba"]
-[14.325701713562012, 2.8893532752990723, "[TT] Mass of the CINEMA-3 = 4 kg"]
-[4.860894680023193, 1.5408560037612915, "[TT] Launch Date of the Tatiana-2 = 17 September 2009"]
-[9.780420303344727, -0.34065717458724976, "[TT] Height of the Lightning Flashes = 10 to 20 km altitude"]
-[4.929853916168213, 5.232752323150635, "[TT] Quantity of the GPS = 2 x receivers + 2 x Antennas"]
-[7.000087261199951, 5.275339603424072, "[FF] Class of the Power Processing Control Unit = 20 mN"]
-[11.676158905029297, 4.812567234039307, "[TT] Dimensions of the TEP Absorber 1 = 5.4 cm cylinder"]
-[8.172018051147461, 4.530213832855225, "[TT] Total Ionizing Dose (TID) of the DSX spacecraft = 10 krad/year behind 8 mm of aluminum shielding"]
-[4.019654750823975, 1.7808102369308472, "[TT] Launch Vehicle of the Kounotori = H-IIB vehicle of MHI (Mitsubishi Heavy Industries, Ltd.)"]
-[4.841813087463379, 7.973484039306641, "[TT] Signal Frequency of the ATSR = 145.860 MHz"]
-[11.389567375183105, 4.882033824920654, "[TT] Tube Capacity of the Picosa Launcher = 2 short picosats or 1 long picosat"]
-[4.863592147827148, 8.264524459838867, "[TT] Frequency (GHz) of the SSMIS = 91.655, 150.0, 183.310"]
-[3.4420039653778076, 5.278585433959961, "[TT] SAR Payload Chirp Bandwidth of the RCM = 100 MHz"]
-[13.357949256896973, 6.906622886657715, "[TT] Power Consumption of the Plato\u2019s payload = 800 W"]
-[5.518558025360107, 7.139515399932861, "[TT] Expected Data Rate of the Data Transmission Test = 24 Mbit/s"]
-[5.773460865020752, 2.347094774246216, "[FF] Integration and Testing Team Size of the ATLAS = 250 engineers, fabricators and scientists"]
-[7.8546624183654785, 8.70159912109375, "[TT] Wavelength Range of the Visible Channel = 0.4-1.0 \u00b5m"]
-[8.095577239990234, 4.412231922149658, "[FF] Information Collected of the TechDemoSat-1's radiation monitor = Total ionizing dose, dose rate, and particle flux (protons and heavy ions)"]
-[7.813366889953613, 1.8335845470428467, "[FF] Effect on Marine Ecosystem of the Ocean Acidification = Potential damaging knock-on effects"]
-[5.335451126098633, 0.8985434174537659, "[FF] Mission Definition Date of the NICER = June 22, 2014"]
-[7.361364841461182, 4.512920379638672, "[TT] Mounting Location of the VWFC = Spacelab scientific airlock"]
-[4.457865238189697, 1.7700080871582031, "[TT] Launch Date of the KySat-2 = 20 November 2013"]
-[7.657273769378662, -0.866916835308075, "[FF] Launch Date of the ICESat-2 = 15 September 2018"]
-[4.5581536293029785, -0.7670260071754456, "[TT] Docking Port of the Dragon = Space-facing port on the station\u2019s Harmony module"]
-[6.454944610595703, 6.232186317443848, "[TT] Standby Autonomy of the User Terminal = 100 hrs"]
-[5.929929256439209, 4.429708480834961, "[FF] Payload of the EDRS-C = Hosted steerable Ka-band communications payload named HYLAS-3 for Avanti Communications"]
-[9.661253929138184, -0.618312656879425, "[TT] Altitude of the ETS-VIII = 35,786 km above the equator"]
-[10.659286499023438, 3.799967050552368, "[FF] Purpose of the Aerothermodynamics = Validation of design tools and improvement of design performance"]
-[9.442245483398438, 4.669620990753174, "[FF] Attitude Control Performance of the ADCS = Suffers from worse performance when the orientation vectors (magnetic and sun) are close together or during the eclipse"]
-[4.0559492111206055, 5.292763710021973, "[TT] Detection and Location of the GPS-SAR = Global near-instantaneous"]
-[11.250585556030273, 0.6400809288024902, "[TT] Purpose of the HARPS = Identifies exoplanets by their gravitational tug on their host stars"]
-[9.999653816223145, 2.854356288909912, "[TT] Launch Date of the CANYVAL-X CubeSats = 12 January 2018"]
-[6.462118625640869, 3.2854113578796387, "[TT] Operation of the AMS-02 = On the International Space Station (ISS)"]
-[6.27095365524292, 2.439019203186035, "[FF] Quote Source of the Carruthers Geocorona Observatory = Dr. Mackenzie Lystrup"]
-[7.838531970977783, 2.5690979957580566, "[FF] Data Use of the GLM = Long-term trending and climate understanding"]
-[5.407420635223389, 6.356112003326416, "[TT] Partition net capacity of the SDR-SMM = 64 Gbit"]
-[9.933563232421875, 6.3815507888793945, "[TT] Rotation Range of the Beryllium mirror = \u00b115\u00ba around its 45\u00ba position"]
-[8.682982444763184, 3.2251360416412354, "[FF] Sensor Complement of the LAICE = In-situ measurements of wave perturbations in the ionosphere and remote sensing of the middle atmosphere"]
-[6.717823505401611, 5.169370174407959, "[FF] User's Interpretation Guide Revision of the SSM/I = C"]
-[7.265219688415527, 5.343969821929932, "[TT] Operating Modes of the VBS = Cooperative Mode, Non-cooperative Mode"]
-[10.610030174255371, 7.3156867027282715, "[TT] Swath Width of the IIM instrument = 25.6 km"]
-[10.839171409606934, 3.7632813453674316, "[FF] Simulation Study of the Solar Wind Electric Sail = P. Janhunen, A. Sandroos"]
-[10.009303092956543, 1.3556327819824219, "[FF] Age of the Cosmic Microwave Background (CMB) = 380,000 years"]
-[6.556757926940918, 4.133545875549316, "[FF] Payload of the MPQ442 = SuperSprite"]
-[7.491974353790283, 6.3348846435546875, "[TT] Absolute Time Accuracy of the TARANIS Instruments = Less than 1 ms"]
-[13.229585647583008, 7.2732253074646, "[TT] Power Consumption of the ECAL Electronics = Limited to 100 W"]
-[9.855836868286133, 2.7000861167907715, "[TT] Size of the Nanoracks BlackBox = Locker-sized"]
-[5.398074626922607, 2.638606548309326, "[TT] Number of Students of the University of Sankore = 25,000"]
-[7.285553455352783, 5.156315326690674, "[FF] Components of the PMC = Camera mainframe, camera management & control unit, DC/DC converter, baffle"]
-[4.279049873352051, 0.715308666229248, "[TT] Launch Date of the EduSat = 2012"]
-[5.465999126434326, 1.6656782627105713, "[FF] Follow-on Satellite of the ALOS = ALOS-2"]
-[5.710195064544678, 4.173325061798096, "[FF] Purpose of the Military Payload = Provision of military Satcom services over the whole visible Earth"]
-[10.224016189575195, 4.320675373077393, "[TT] Quantity of the Coils = 2"]
-[10.136313438415527, -2.7500925064086914, "[TT] Operating Voltage of the SLC NAND-Flash = 2.7 V \u2013 3.6 V"]
-[10.951655387878418, 7.5421342849731445, "[TT] Swath of the MSU-E1 = 105 km"]
-[9.070629119873047, 0.5095037817955017, "[TT] Maneuvers per Year of the ARTEMIS = Approximately two"]
-[5.146295070648193, 1.0566389560699463, "[TT] Launch and Early Orbit Phase (LEOP) Completion Date of the SMOS = Early December 2009"]
-[4.5953545570373535, 2.690356969833374, "[FF] Conference Location of the SWAP = Toulouse, France"]
-[13.513428688049316, 2.878591299057007, "[TT] Total Mass of Satellites of the PSLV-C40 = 1323 kg"]
-[6.228417873382568, 6.054361343383789, "[FF] Link Speed of the Payload link configuration request = Unknown"]
-[7.105895042419434, 4.3988165855407715, "[FF] Unknown of the CFE = Unknown"]
-[7.604438781738281, 8.747093200683594, "[TT] Spectral Bands of the MTG-S Spacecraft = 16"]
-[4.720010280609131, 6.2538886070251465, "[TT] Power Requirement of the APL\u2019s Frontier radio = Less than other deep-space radios"]
-[6.977295875549316, 4.621419906616211, "[FF] Function of the GRB = Provide full resolution, calibrated, navigated, near-real-time direct broadcast data"]
-[8.992950439453125, 8.535117149353027, "[TT] Band 1 Wavelength Range of the Telescope = 0.55 - 0.75 \u00b5m"]
-[14.656658172607422, 6.782776355743408, "[TT] Battery Capacity of the EPS = 4 Ah"]
-[9.43350887298584, 5.3558268547058105, "[FF] Additional Feature of the AMI-302 = Small temperature sensor (PT-1000)"]
-[4.5135393142700195, 6.734059810638428, "[TT] RF Communications of the Spacecraft = 0.5 W (S-band downlink)"]
-[11.864580154418945, 6.78031587600708, "[TT] Photon Energy Range of the XGRE = 20 keV-10 MeV"]
-[3.5145177841186523, -0.8856156468391418, "[TT] Orbit Type of the ABEX = Sun-synchronous"]
-[6.371127128601074, 4.467000484466553, "[FF] Project Role of the UA = Power Systems, Command & Data Handling"]
-[3.7392303943634033, 6.333236217498779, "[TT] Antennas of the ASCAT = 6"]
-[3.379685878753662, 1.435463786125183, "[TT] Launch Date of the Sentinel-1D = First half of 2024"]
-[8.082809448242188, 8.893085479736328, "[TT] Refraction Angle Measurement of the MSX/UVISI = Visible Wavelengths"]
-[9.136569023132324, 7.639874458312988, "[TT] MS (Multispectral) of the Medium resolution = 0.60-0.70 \u00b5m (red)"]
-[9.033288955688477, 3.3327605724334717, "[FF] Objective of the FlaPS = To provide a solution to the investigation of plasma distributions in space - to characterize the effects of charged particles on the formation, propagation and decay of ionospheric plasma bubbles"]
-[3.5764849185943604, 4.888670444488525, "[FF] Mode of Operation of the Poseidon 4 = SAR and pulse-width limited modes"]
-[4.730146408081055, 0.6577720642089844, "[TT] Launch Year of the GOES-R = 2016"]
-[6.672780513763428, 0.7650153636932373, "[FF] Image of the Week Date of the Herschel = March 29, 2016"]
-[13.804220199584961, 5.352945327758789, "[TT] Solar Panel Type of the AprizeSat = UTJ (Ultra Triple Junction) GaAs"]
-[13.899799346923828, 3.670759916305542, "[TT] Mass of the Telescope = 1.7 kg"]
-[4.4362921714782715, 7.808276176452637, "[TT] Uplink Frequency of the DCS = 402 MHz"]
-[10.981545448303223, 5.9888715744018555, "[TT] Material of the Faraday Cup = Refractory metals and sapphire crystal insulators"]
-[9.042313575744629, 5.134757041931152, "[FF] Operation Principle of the Gyro Unit = Electrically-excited vibration of a solid cylindrical element"]
-[9.444618225097656, 4.7066779136657715, "[FF] Control Strategy of the Passive Attitude Control System = Robust, simple"]
-[5.17362117767334, 2.2861428260803223, "[TT] Mission Type of the FormoSat-1 = EO"]
-[14.058589935302734, 7.158412456512451, "[TT] Fully Charged Bus Voltage of the EPS = 33.6 V"]
-[11.866676330566406, 4.844360828399658, "[TT] Dimensions of the CSM = ~ 80 cm x 30 cm"]
-[8.567667007446289, 2.2961483001708984, "[FF] Local Effects of the DIBS = Lingering dust, affect forecasts of temperature and precipitation"]
-[6.463444232940674, 2.0445399284362793, "[FF] URL of the MidSTAR-1 = http://www.usna.edu/Satellite/midstar/downloads/ops/MidSTAR-1%20Ops%20Concept.doc"]
-[11.792034149169922, 6.7269206047058105, "[TT] Measurement Range of the EIS = ~45 keV to 500 keV"]
-[7.465922832489014, 8.94338321685791, "[TT] Bandpass of the OLS = 0.5 - 0.85 \u00b5m"]
-[13.438551902770996, 5.434412479400635, "[TT] Type of the Solar Panel = Single articulating"]
-[7.767006874084473, 1.832240343093872, "[FF] Response to Stresses of the Phytoplankton = Varying greatly in size, function, and response to environmental and ecosystem changes or stresses such as ocean acidification"]
-[6.828268527984619, 5.72332763671875, "[TT] Phase Control Interval of the BSC = 2 ms"]
-[5.696700572967529, 2.8150665760040283, "[TT] Funding of the SEXTANT = NASA funded"]
-[8.189385414123535, 6.301769256591797, "[FF] Dominant Uncertainty Component of the Multi-Spectral Imager (MSI) = In-flight, radiometric calibration"]
-[8.919535636901855, 3.237823724746704, "[FF] Imaging Purpose of the Deployable Membrane Telescope = Narrow-band imaging of the sun's chromosphere"]
-[7.635933876037598, 8.78145980834961, "[TT] Spectral Bands of the MSU-S = 2"]
-[5.164608478546143, 1.0582557916641235, "[FF] Launch Date of the Hisea-1 = 6 November 2020"]
-[11.22830867767334, 5.361242771148682, "[TT] Plastic Scintillator Counters of the Veto System = 5"]
-[10.687797546386719, 3.921156644821167, "[FF] Formation Flight Mission of the CanX-4/CanX-5 = Unknown"]
-[13.51170825958252, 6.894973278045654, "[TT] Power Generation of the Power System = 215 kW"]
-[7.336405277252197, 1.1702830791473389, "[TT] Mission of the OSCAT-3 = Oceansat-3"]
-[5.554398059844971, 5.403983116149902, "[TT] Flight Computers of the Payload Instruments = Dual redundant flight computers based on Intel 80386EX processors, configured with 32 MByte capacity"]
-[4.40535306930542, 5.425008296966553, "[FF] Conference Presentation Date of the GOMX-1 = April 23-25, 2014"]
-[8.557220458984375, 7.833674907684326, "[TT] Array Size of the VISIM = 652 x 492 pixels"]
-[6.835357189178467, 7.427856922149658, "[TT] ADC Resolution of the Rx Module = 14 bit"]
-[4.859608173370361, 7.943878650665283, "[TT] Carrier frequency (MHz) of the E5a-I = 1176.45"]
-[5.975780010223389, -0.3979881703853607, "[TT] Commissioning Duration of the PROBA-3 = About 2 months"]
-[8.672358512878418, 4.769508361816406, "[TT] Quantity of the Star Tracker Optical Heads (STR) = 3"]
-[7.881213188171387, 5.804835319519043, "[FF] Device Type of the ISIR = Radiometer"]
-[12.06519603729248, 4.89870023727417, "[TT] Size of the S-band transceiver = 106 mm x 166 mm x 90 mm"]
-[8.148043632507324, 1.2580569982528687, "[FF] Purpose of the SMAP = Measure soil moisture"]
-[10.840005874633789, -0.2814520001411438, "[FF] Mission Objectives of the TanDEM-X = Generating a global HRTI-3 DEM"]
-[7.456587791442871, 5.1955132484436035, "[FF] Transmission Profile of the PF1 = Unknown"]
-[10.169659614562988, 8.096292495727539, "[TT] Effective Focal Length of the Telescope = 466.7 mm"]
-[5.911917209625244, 1.0557823181152344, "[FF] Publication Date of the GNSS in Space = Nov/Dec. 2008"]
-[8.157835960388184, 8.329076766967773, "[TT] Emissivity of the CrIS-based target = >995%"]
-[5.21646785736084, 1.204186201095581, "[FF] Submission Deadline of the OPS-SAT = 13 June"]
-[7.097945213317871, 6.17227029800415, "[TT] Fundamental Timing Unit of the Hardware = 10 ms"]
-[5.430929660797119, 6.736900329589844, "[TT] Science Archive Size of the LDCM = ~ 400 TB"]
-[11.55060863494873, 3.4113516807556152, "[TT] Performance of the CNAPS Propulsion System = Out-performed expectations"]
-[3.449977397918701, 6.4372477531433105, "[TT] Antenna Diameter of the Integrated Mobile Station = 4.6 m"]
-[7.872006893157959, 3.0883283615112305, "[FF] Units of the CO2 Concentration = ppm (parts per million)"]
-[10.701803207397461, 5.552231311798096, "[FF] Design of the TCS = Passive methods with MLI (Multi-Layered Insulation) blankets and thermal coatings"]
-[10.955525398254395, 2.0616607666015625, "[FF] Catalogue Release Date of the XMM-Newton = May 15, 2017"]
-[9.110595703125, 4.893867015838623, "[FF] Quantity of the Temperature Sensors = 2"]
-[7.688666343688965, -2.540773868560791, "[TT] Cadence of the GOLD = 30 minutes"]
-[10.21291446685791, 1.3992271423339844, "[TT] Star Formation Rate Discrepancy of the Cluster XDCPJ0044.0-2033 = Four times the rate found in its outer regions"]
-[11.766440391540527, 6.805370330810547, "[TT] Energy Range of the ELS-A = 400 \u2013 490 keV"]
-[9.777942657470703, 7.018433094024658, "[TT] Ground Distance per Step of the Scan Mirror Mechanism = 8 km"]
-[4.773191928863525, 7.185105323791504, "[TT] Uplink Rate of the S-band = 20 kbit/s"]
-[13.718260765075684, 2.7985000610351562, "[TT] Mass of the TSX-5 spacecraft = 249.5 kg"]
-[3.182297945022583, 3.9945802688598633, "[TT] Number of Data Takes of the TerraSAR-X = Over 12000"]
-[12.052781105041504, 4.578359603881836, "[TT] Size of the Spacecraft = 80 cm x 60 cm x 60 cm"]
-[5.428954124450684, 4.038022518157959, "[TT] Number of Supersites of the MAPS = 19"]
-[1.367087960243225, 2.782139301300049, "[TT] Principal Absorbing Constituents of the Band 7 = Water vapor"]
-[5.151220798492432, 3.2721426486968994, "[TT] Manufacturer of the LWFT = Space Research Center of the University of Leicester, UK"]
-[5.549345970153809, 1.9831255674362183, "[FF] Mission Phase of the ABEX = Science Commissioning"]
-[8.11047649383545, 7.244389533996582, "[FF] Components of the Prime Instrument = Two nadir-pointing UV cameras, one operating with CCD detectors, the other with UV photodiodes"]
-[5.359066963195801, 0.4864243268966675, "[FF] Launch Date of the ASTRO-H = Feb. 17, 2016"]
-[9.581686019897461, 4.861331939697266, "[TT] Stabilization of the ADCS = 3-axis stabilized with RWA's, Zero Momentum Biased (ZMB)"]
-[8.856915473937988, 3.2772462368011475, "[FF] Purpose of the SUVI = Provides information on solar activity such as solar flares and its impacts on the Earth"]
-[10.376490592956543, 6.979679584503174, "[TT] Pointing mirror size of the Sun tracker = 18 x 18 cm"]
-[9.470016479492188, 8.9545259475708, "[TT] Dynamic Range of the Iris Video Camera = 16 bit"]
-[6.2815423011779785, 8.665444374084473, "[TT] Polarization of the MWR = H+V"]
-[3.23439884185791, 1.7615691423416138, "[TT] Image Acquisition Date of the Sentinel-2A = Jan. 31, 2016"]
-[6.03503942489624, -0.24298112094402313, "[TT] Design Life of the Genesis-2 = 5 years"]
-[7.1170334815979, -0.13491250574588776, "[TT] Number of Orbits of the Part B2 = 2"]
-[4.737951755523682, 8.39539623260498, "[TT] Center Frequency of the 4 = 54.4 GHz"]
-[6.456060409545898, -0.02013278193771839, "[TT] Contact Check Frequency of the CSpOC = Daily"]
-[10.494745254516602, 1.8248026371002197, "[FF] Mission of the NuSTAR = Observation of ultra-fast winds from supermassive black holes"]
-[9.8021240234375, -0.4164704978466034, "[TT] Altitude of the BIROS = 515 km"]
-[5.719680309295654, 6.373533725738525, "[TT] Capacity of the Solid-state Recorder = 192 Gbit"]
-[4.394660949707031, 1.879609227180481, "[FF] Service Date of the RADARSAT-2 = 26 February 2019"]
-[7.862351894378662, -2.489874839782715, "[FF] Purpose of the GOLD = Track changes in the ionosphere\u2019s temperature, density and composition"]
-[4.433769702911377, 7.475739479064941, "[TT] Uplink Frequency of the HRIT/EMWIN = S-band"]
-[3.7539286613464355, 6.794362545013428, "[TT] Antennas of the Ground Station = UHF/VHF high-gain cross Yagi-Uda antennas"]
-[9.110127449035645, 7.293268203735352, "[TT] Imager Resolution of the Satellite Vu = 3.5 m"]
-[4.605353832244873, 0.8837608098983765, "[TT] Communication Experiment Date of the ADEOS-II = Feb. 19, 2003"]
-[9.444510459899902, 7.460353374481201, "[TT] Spatial Resolution of the HXR Flare Ribbons = ~2 arcsec"]
-[7.210505485534668, 4.795449256896973, "[FF] Component Detection of the SPA System = Automatic"]
-[11.597710609436035, 6.629857540130615, "[TT] Electrostatic Energy Analyzer Passband of the CID = DE/E = 0.14"]
-[6.939827919006348, -0.4647238552570343, "[TT] Descending Node Time of the Sun-synchronous orbit = 10:30"]
-[9.753317832946777, 4.0325093269348145, "[TT] Surface Field of the Neodymium Block Magnets = 144.6 mT"]
-[9.32461166381836, 2.613548517227173, "[FF] X-Ray Flares Count of the RHESSI = Forty Thousand"]
-[5.194293022155762, 1.01670503616333, "[FF] Launch Date of the D-Sat = June 27, 2017"]
-[8.62777042388916, 7.430777549743652, "[TT] Detection Limit of the VIS = AB 24.5 magnitude"]
-[10.375181198120117, 2.1544950008392334, "[TT] Energy Range of the NuSTAR = High-energy X-rays"]
-[10.523240089416504, 2.3416261672973633, "[FF] Resolution of the Spacecraft Module = Eight-times greater than any previous X-ray telescope"]
-[5.332775592803955, 7.718868732452393, "[TT] EIRP of the Antenna = >55.0 dBW"]
-[11.005228996276855, 3.787816047668457, "[TT] Size of the TechEdSat-8 = 6U"]
-[4.923679828643799, -2.139496088027954, "[TT] Rocket Weight of the Chang'e-5 = 870 metric tons"]
-[7.104625225067139, 7.0003662109375, "[TT] Nominal Faint-Source Count Rate Dead Time of the Readout System = < 2%"]
-[5.48019552230835, 2.6544272899627686, "[TT] Graduate Student Contributors of the SAPPHIRE = Dozen graduate students"]
-[3.312251091003418, 5.297140121459961, "[TT] Incidence Angle of the SAR Antenna = 8\u00ba to 70\u00ba"]
-[12.004204750061035, 4.885083198547363, "[TT] Volume of the PROBA-1 = 1 m3"]
-[8.297218322753906, 3.2178502082824707, "[FF] Function of the TES = Collecting measurements of ozone's greenhouse effect"]
-[13.266831398010254, 7.313364505767822, "[TT] Power Consumption of the MSU-100 = 6.8 W"]
-[9.866777420043945, 4.988204479217529, "[TT] Rotational Coupling Factor of the LRI = < 200 \u00b5m/rad"]
-[14.631837844848633, 6.750930309295654, "[TT] Battery Capacity of the EPS = 15 Ah"]
-[7.865470886230469, 0.966701328754425, "[TT] Spatial Resolution of the ROSE-L = 5 m - 10 m"]
-[11.162028312683105, 7.495095729827881, "[TT] Swath of the Megha-Tropiques = ~2200 km"]
-[11.619233131408691, 6.650750160217285, "[TT] Energy Measurement Range for Particles of the Telescope 1 = 1.6-12 MeV/n"]
-[6.216595649719238, 2.173259735107422, "[TT] Principal Investigator of the GIADA = Luigi Colangelo"]
-[5.910909175872803, 0.5635333061218262, "[FF] Number of Interferometric Pairs of the ERS Tandem Mission = Five or six for Europe and North America"]
-[8.833633422851562, 5.3296027183532715, "[FF] Imaging Modes of the Dove-1 = Nadir pointing, Upwards pointing"]
-[7.964378833770752, 4.450656414031982, "[FF] Test Locations of the FG = Air, vacuum conditions, 10000-class clean room, solar telescope"]
-[5.183393478393555, 8.417604446411133, "[TT] Bandwidth of the Channel 7 = 1000 MHz"]
-[12.345698356628418, 3.2223589420318604, "[TT] Wet Mass of the iodine BIT-3 flight system = 3 kg"]
-[9.438325881958008, 4.760830879211426, "[FF] Fuel Consumption of the Attitude Control System = None"]
-[10.588099479675293, 2.889655351638794, "[TT] Photometer Field-of-View of the Nanosatellite = 24\u00ba"]
-[7.996387958526611, -0.4467964172363281, "[TT] Boiling Point of the Cryogens = Extremely low"]
-[6.8669610023498535, 0.7634271383285522, "[FF] Landing Date of the InSight = 29 November 2018"]
-[6.162880897521973, 2.5244534015655518, "[FF] Authors of the Rosetta = J.-B. Vincent, M. F. A'Hearn, Z.-Y. Lin, M. R. El-Maarry, M. Pajola, H. Sierks, C. Barbieri, P. L. Lamy, R. Rodrigo, D. Koschny, H. Rickman, H. U. Keller, J. Agarwa, M. A. Barucci, J.-L. Bertaux, I. Bertini, S. Besse, D. Bodewits, G. Cremonese, V. Da Deppo, B. Davidsson, S. Debei, M. De Cecco, J. Deller, S. Fornasier, M. Fulle, A. Gicque, O. Groussin, P. J. Gutierrez, P. Gutierrez-Marquez, C. G\u00fcttler, S. H\u00f6fner; M. Hofmann, S. F. Hviid, W.-H. Ip, L. Jorda, J. Knollenberg, G. Kovacs, J.-R. Kramm, E. K\u00fchrt, M. K\u00fcuppers, L. M. Lara, M. Lazzarin, J. J. Lopez Moreno, F. Marzar, M. Massironi, S. Mottola, G. Naletto, N. Oklay, F. Preusker, F. Scholten, X. Shi, N. Thomas, I. Toth, C. Tubiana"]
-[6.924131870269775, 1.7235721349716187, "[FF] URL of the Kaik\u014dura earthquake = http://science.sciencemag.org/content/early/2017/03/22/science.aam7194"]
-[10.72105598449707, 1.0753345489501953, "[TT] Size of the TOI 1807 b = About twice Earth\u2019s size"]
-[9.242831230163574, -0.41069284081459045, "[FF] Safe Orbit Range of the PROBA-3 = < 1 km"]
-[4.589259147644043, 1.6624950170516968, "[FF] Launch Date of the TANSAT = January 2017"]
-[5.613970756530762, 4.234252452850342, "[FF] Status of the EDRS-C = On the home stretch"]
-[10.204510688781738, 5.7551045417785645, "[TT] Operating Temperature of the Detector Cooler = 95 K"]
-[8.885161399841309, 7.3940300941467285, "[TT] Background Area of the Detector = 10 x"]
-[8.668778419494629, 2.6612465381622314, "[TT] Measurement of the K-band channel = Water vapor content of the atmosphere"]
-[9.34769058227539, 6.433291912078857, "[TT] Geoid Height Accuracy of the Next Generation Gravity Constellation = 1 mm"]
-[6.4944939613342285, 4.563404560089111, "[FF] Distribution of the AWIPS = Subset of product generation element"]
-[10.821206092834473, 7.494598388671875, "[TT] Swath Width of the NSCAT = 600 m"]
-[1.9418197870254517, -0.40218061208724976, "[TT] Extended Mission End Date of the Van Allen Probes = June 2019"]
-[5.633474826812744, 3.237006187438965, "[TT] Contract Value of the TSIS-1 = Approximately $16.2 million"]
-[11.41191291809082, 4.329521179199219, "[TT] Size of the CINEMA = 3U"]
-[7.387060642242432, 4.227844715118408, "[FF] Description of the Rendezvous experiment and Realistic Collision Avoidance = Rendezvous experiment and Realistic Collision Avoidance"]
-[7.538293838500977, -2.494337797164917, "[TT] Launch Year of the GOLD = 2018"]
-[12.077064514160156, -0.19714045524597168, "[TT] Observation Sectors of the TESS = 26"]
-[9.70074462890625, 6.989920616149902, "[TT] Integral Geometric Factor of the ELENA = 6 x 10 -4 cm 2 sr"]
-[8.042046546936035, 5.752349376678467, "[TT] Calibration Cycle Time of the LISS-3 camera = 7.3 s"]
-[11.735185623168945, 3.271850109100342, "[TT] Minimum Impulse Time of the PROP unit = 40 ms"]
-[6.340876579284668, 6.04177188873291, "[TT] Number of Systems of the Data Center = 7"]
-[4.826754570007324, 7.98814058303833, "[TT] Spectral Recommended Occupation Bandwidth of the EESS S-band = 6 MHz maximum"]
-[10.808613777160645, 7.421281814575195, "[TT] Impact of Sector Blanker of the RapidScat = Reduce the swath up to approximately 50 km"]
-[10.634659767150879, 8.885370254516602, "[TT] Pixel Size of the WV channel = 8 km on a side"]
-[3.74984073638916, -0.6616437435150146, "[TT] Orbit of the Iridium NEXT = Low Earth Orbit"]
-[3.8004400730133057, 1.1790034770965576, "[TT] Booster Reuse of the Falcon 9 = 7 trips to space and back"]
-[13.7609224319458, 3.67914080619812, "[TT] Mass of the SAR Antenna = 750 kg"]
-[10.032511711120605, 2.796036720275879, "[TT] Mission Type of the NanoSat-1B = Non-EO"]
-[5.355656623840332, 5.534599781036377, "[FF] Data Interfaces of the EuTEF = MIL-STD-1553B data bus and a redundant Ethernet"]
-[6.058432102203369, 0.8259311318397522, "[FF] Release Date of the Zaatari Refugee Camp, Jordan = May 23, 2014"]
-[5.013935089111328, 3.341167449951172, "[TT] Information Usage of the IIS = Co-registration with the AVHRR"]
-[8.626219749450684, 2.4665427207946777, "[FF] Function of the FDA = Protect the instrument against dust particles"]
-[7.081199645996094, 3.892791271209717, "[TT] Function of the Formation flying technology = Demonstrate a high-precision formation flight in space"]
-[1.7180203199386597, 6.145230770111084, "[FF] Composition of the Dark Matter = ~27%"]
-[5.666935443878174, 0.6646721363067627, "[TT] Return Date of the Probe = February 2021"]
-[8.092353820800781, 7.3354811668396, "[TT] Device Type of the CCID-80 = Deep-depletion, frame-transfer CCD"]
-[9.313446998596191, -0.8725707530975342, "[TT] Orbit of the Kestrel Eye-2M = Near the ISS"]
-[8.368136405944824, 1.8928191661834717, "[TT] Calibration and Validation Duration of the RapidScat = Two weeks"]
-[5.461398124694824, 1.6125963926315308, "[TT] Development Date of the ABI instrument = Sept. 2004"]
-[4.614279270172119, 6.6120829582214355, "[TT] RF Communications of the Spacecraft = 2 MByte (typical)"]
-[13.471360206604004, 2.901437520980835, "[TT] Educational Satellites Mass of the VEGA C = About 50 kg"]
-[5.008466720581055, 3.2070209980010986, "[TT] Lead Investor of the EDRS-C = Germany"]
-[8.740350723266602, 4.851174354553223, "[TT] Pointing Accuracy (Roll Axis) of the Star Tracker = 0.2\u00ba (3\u03c3)"]
-[14.304034233093262, 3.368608236312866, "[TT] Mass and Volume of the HTA = Low"]
-[6.4621429443359375, 1.98545503616333, "[FF] URL of the NuSTAR = http://airex.tksc.jaxa.jp/dr/prc/japan/contents/AA0064574157/64574157.pdf"]
-[8.500585556030273, 3.0205025672912598, "[FF] Atmosphere of the 55 Cancri e = Possibly made of oxygen or nitrogen, or a very thin atmosphere of mineral vapor, such as silicon oxide"]
-[8.634864807128906, 4.569441318511963, "[FF] Sensors of the ACS = Fine and Coarse Sun Sensors (FSS & CSS), Magnetometers (MAG), Fiber-optical Gyros (Gyro), and Star Sensors (STS)"]
-[11.539039611816406, 4.782811641693115, "[TT] Length of the Cygnus = 17.6 m"]
-[8.428895950317383, 7.852456569671631, "[FF] Power Consumption of the FLIR Boson camera = Low"]
-[8.944883346557617, 5.295721530914307, "[TT] Orbit Altitude of the GOMX-3 = ~400 km"]
-[12.92764949798584, 6.74776029586792, "[TT] Predicted Specific Impulse of the PPT Module = 320 s"]
-[5.964040756225586, -0.4951699674129486, "[TT] Journey Duration of the NEA Scout = Approximate two years"]
-[7.717381477355957, 7.606207847595215, "[TT] Dynamic Range of the Detector = 16 bit"]
-[5.6131062507629395, 4.541751861572266, "[FF] Communication Network of the SBSS = Air Force Satellite Control Network and commercial USN (Unified Space Network) ground stations"]
-[6.8214826583862305, 5.372855186462402, "[TT] Type of the Sun Sparc microprocessor = Radiation-hardened"]
-[9.937914848327637, -0.43260666728019714, "[TT] Altitude of the Satellite = 1012 km"]
-[9.434134483337402, 3.8040990829467773, "[FF] Calibration of the \u00d8rsted Vector Magnetometer = Unknown"]
-[6.0403313636779785, 5.505062103271484, "[TT] Redundancy Approach of the SSTL = High degree of cold parallel redundancy"]
-[3.4318716526031494, -0.8876451849937439, "[TT] Orbit of the Kleos Patrol Mission (KSF2) = Sun synchronous"]
-[6.380389213562012, 3.8700757026672363, "[FF] Additional Capabilities of the GOES-R = GBR (GOES-R Re-Broadcast), S&R (Search & Rescue), DCS (Data Collection System), EMWIN (Emergency Managers Weather Information Network), and LRIT (Low Rate Information Transmission) communications"]
-[5.195328235626221, 3.6423027515411377, "[TT] Developer of the Image Processing Software = CNES"]
-[8.634773254394531, 1.1449066400527954, "[FF] Mission Status of the Aquarius = Unknown"]
-[5.8977789878845215, -0.33676615357398987, "[FF] Partnership Duration of the DMSP = More than 50 years"]
-[8.938831329345703, 5.6266865730285645, "[TT] In-Flight Pointing Control Accuracy of the EFI (Electrical Field Instrument) = 5\u00ba"]
-[4.488766670227051, 0.9961346387863159, "[TT] Integration Date with GEOSS of the GMES = 2016"]
-[6.925709247589111, 3.354647159576416, "[FF] Data Processing of the ECP = Products that support host satellite anomaly resolution, and state of health trending and analysis"]
-[5.84767484664917, 3.336010456085205, "[TT] Total Cost of the LEO Constellation = $5 billion"]
-[8.209127426147461, 4.768871784210205, "[FF] Components of the Automatic target pointing mode = Star sensor assembly, GPS receiver, attitude control actuator"]
-[10.311643600463867, 3.7911224365234375, "[FF] Shock Front Formation of the Accreting Gas = Yes"]
-[13.644854545593262, 5.923282623291016, "[TT] Power Sources of the PSU = Solar panels, battery"]
-[5.1286516189575195, 2.314556360244751, "[TT] Status of the Severjanin = Functional with limitations"]
-[8.660603523254395, -0.11638490110635757, "[TT] Keel Depth of the A-68A = 141 metres below the ocean surface"]
-[13.557686805725098, 7.073495388031006, "[TT] Quantity of the Power Converters = 2"]
-[6.219743251800537, 5.759958744049072, "[TT] Status of the LRPT transmission = Functional"]
-[4.30360746383667, 5.408154487609863, "[FF] Frequency Compatibility of the TUC Transponder = European and international altimetry missions in the microwave range"]
-[5.785656452178955, 1.454465627670288, "[FF] Conference Date of the WorldView-1 = Nov. 11-14, 2007"]
-[5.478915691375732, 0.7226125597953796, "[FF] Design Date of the CHRIS = Unknown"]
-[7.714267730712891, 0.4247124195098877, "[TT] Orbit Type of the Lunar IceCube = Highly elliptical, equatorial periapsis"]
-[8.991928100585938, 4.400697231292725, "[TT] Digital Sun Sensor FOV of the AOCS = 37\u00ba"]
-[9.807616233825684, 6.947332382202148, "[TT] Vertical Resolution (PBL) of the Aeolus = 0.5 km"]
-[8.506278991699219, 7.008156776428223, "[TT] C3D2 Camera Images of the AlSat Nano = 105 image files downloaded in total so far, including 16 full size images"]
-[4.9895339012146, 0.3541681170463562, "[TT] Launch Date of the Jugnu = October 12, 2011"]
-[7.2264533042907715, 4.590800762176514, "[FF] Component of the Power Video Grapple Fixture (PVGF) = Unknown"]
-[8.418832778930664, 7.876331806182861, "[TT] FPA of the MWIR = Two staggered CMT arrays, each of size 2 x 512 elements"]
-[4.090329647064209, 4.279321193695068, "[FF] Mission Operations of the RADARSAT-2 = Day-to-day end-to-end system operations and maintenance of the satellite and ground segment"]
-[4.728837966918945, 2.425096273422241, "[FF] TT&C Station of the Maroc-TUBSAT = Not needed within the target region"]
-[5.240153789520264, 6.958653450012207, "[TT] Max Data Rate (Mbit/s) of the HDR-VSAT = Uplink: 155 Downlink: 155"]
-[6.473405361175537, 2.533470630645752, "[FF] Missions of the Solar Terrestrial Probes (STP) Program = STEREO, MMS, Hinode, TIMED"]
-[11.193365097045898, 0.6451655030250549, "[TT] Signal to Noise of the CHEOPS = 5 for a transit of an Earth-sized planet orbiting a solar-sized star (0.9 solar radii)"]
-[14.734126091003418, 6.621502876281738, "[TT] Capacity of the Li-ion battery assembly = 5.8 Ah"]
-[5.9444403648376465, 0.6011399626731873, "[TT] Launch Date of the ASTERIA = Aug. 14, 2017"]
-[6.295947551727295, 2.571624755859375, "[FF] Design Purpose of the Orion = Carrying crew to space, providing emergency launch abort capabilities, sustaining the crew during space travel, and providing reentry from deep space return velocities"]
-[5.144222259521484, 8.162766456604004, "[TT] Frequency of the VIS (red) = 460 THz"]
-[7.564208030700684, -0.10192873328924179, "[TT] Last Signal Date of the Philae lander = 9 July 2015"]
-[6.374206066131592, 6.3789777755737305, "[TT] Search Duration of the YES = About 96 hours"]
-[13.135716438293457, 5.36752462387085, "[TT] Solar Array Rotation of the ALSAT-2B = ~ 0.025 deg/sec"]
-[3.269550085067749, 4.988964080810547, "[TT] Polarimetry Modes of the ALOS-2 SAR = Single, dual, quad (full-pol.), compact (or hybrid)"]
-[7.23179292678833, 1.2472422122955322, "[FF] Components of the Sample Retrieval Lander = Mars Ascent Vehicle, Sample Transfer Arm, two sample recovery helicopters"]
-[6.767127513885498, -0.3698617219924927, "[TT] Flyover Time of the LEO Satellite = Minutes"]
-[9.218498229980469, 8.033007621765137, "[TT] Pixel Size of the Focal Plane Module = 600 \u00b5m"]
-[6.1672749519348145, -0.5304273366928101, "[TT] Continuous Operation Hours of the TechEdSat = 2000"]
-[4.487959861755371, 2.9700582027435303, "[TT] Location of the CMC = Moscow, Russia"]
-[9.54969310760498, 4.197572708129883, "[TT] Type of the Magnetic Field Sensor = Two-axis"]
-[8.774870872497559, 9.405488014221191, "[TT] Spectral Band 1 Number of Pixels of the TANSO-CAI = 2000"]
-[4.483299255371094, 1.4539260864257812, "[TT] Program Start Year of the MightySat = 1994"]
-[5.268991947174072, 1.2731159925460815, "[FF] Conference Date of the Resurs-P1 = Feb. 28 - March 2, 2007"]
-[8.580863952636719, 2.264503002166748, "[FF] Frequency of the Dust Storm = Somewhat unusual"]
-[13.853144645690918, 2.7113571166992188, "[TT] Launch Mass of the Flight System = 366 kg"]
-[3.438093900680542, -0.881043016910553, "[TT] Orbit type of the GOSAT-2 = Sun synchronous"]
-[5.8600969314575195, 7.182990074157715, "[TT] Nominal Average of the Data Generation Rate = 120 kbit/s"]
-[7.388908863067627, 5.236428260803223, "[FF] Component Manufacturing of the Structure = Machining components from solid"]
-[2.896489143371582, 4.526419639587402, "[FF] Wind speed distribution of the Marine = LMOD (L-band modulation function) developed for PALSAR will be improved by using the dual-polarized PALSAR-2"]
-[7.696590900421143, 6.778533458709717, "[TT] Exposure Time of the VIS = 565 seconds"]
-[9.270398139953613, 5.9208269119262695, "[FF] Position of the Reference Absorbers = Mounted on the non-rotating part of the instrument"]
-[7.421308517456055, 5.3401875495910645, "[FF] Purpose of the LRI = Precision distance measurements in space"]
-[7.405683994293213, 8.807611465454102, "[TT] Band 7 of the MSS Instrument = 0.8 - 1.1 \u00b5m"]
-[14.243154525756836, 3.2284655570983887, "[TT] Total Mass of the ASAP = About 3 kg"]
-[6.788227081298828, 4.0987701416015625, "[FF] Power Production with One Wing Failed of the SAWs = Unknown"]
-[6.470757007598877, -0.6937847137451172, "[TT] LTDN of the Optsat-3000 = 10:30 hours"]
-[7.412535667419434, 0.32952189445495605, "[FF] URL of the OSIRIS-REx = https://www.asteroidmission.org/asteroid-operations/"]
-[5.948478698730469, 2.9097800254821777, "[TT] Project Manager of the Fission Surface Power System = Todd Tofil"]
-[3.9417436122894287, 2.1791510581970215, "[TT] Launch Vehicle of the Starshine-3 = Athena-1"]
-[5.6411237716674805, 3.7086191177368164, "[TT] Total Impulse of the SkySat-6 = 269 Ns"]
-[10.42448902130127, 3.3093924522399902, "[FF] Payload of the Iraz\u00fa CubeSat = Secondary OBC which acts as an IMU"]
-[7.075415134429932, 1.2637231349945068, "[TT] Observation Period of the Spitzer = 2015-2019"]
-[5.580350875854492, 5.694577217102051, "[TT] Processor of the CubeComputer = 32 bit ARM Cortex-M3"]
-[12.449265480041504, 0.5861693024635315, "[TT] Pointing Stability of the PLATO = High"]
-[8.762468338012695, 3.444150686264038, "[FF] Ionospheric Perturbations of the Seismic Activity = Can produce ionospheric perturbations"]
-[8.657215118408203, 4.713578701019287, "[TT] Anomaly Compensation of the Astro-APS = White spots"]
-[6.71802282333374, 6.1596760749816895, "[TT] Default Mode of the TRXU = Receive mode"]
-[14.222323417663574, 3.238077163696289, "[TT] Total Mass of the TiPS = 54 kg"]
-[9.005908966064453, 0.5528246760368347, "[TT] End of Life Date of the Artemis-I = 11 December 2022"]
-[13.447453498840332, 5.408640384674072, "[TT] Manufacturer of the Solar Panels (SPs) = STI (SpaceTech GmbH Immenstaad), Germany"]
-[7.455773830413818, 0.7412315607070923, "[FF] Observation Date of the Lake Okeechobee = July 3, 2022"]
-[6.263778209686279, 8.652832984924316, "[TT] Polarization of the Stripmap = Single or dual"]
-[5.122567176818848, 3.2922756671905518, "[TT] Manufacturer of the WSF-M = Ball Aerospace"]
-[8.063297271728516, 7.366209983825684, "[TT] Pixel Response Time of the Detector = < 6 ms"]
-[8.895974159240723, 3.1470606327056885, "[FF] Objectives of the SEISS = Energetic particle forecasts"]
-[7.499203205108643, 3.5782949924468994, "[FF] Data of the NightPod = Images of Earth at night"]
-[4.938844680786133, 0.5754789710044861, "[TT] Launch Date of the ZY 1-02C = Dec. 22, 2011"]
-[5.8499064445495605, -0.769524872303009, "[TT] Lifetime of the HaloSat = Two and a half years"]
-[5.677130222320557, 2.6635584831237793, "[TT] Title of the Kevin Murphy = NASA Earth Science Division chief science data officer"]
-[8.212757110595703, 5.986117362976074, "[FF] Interferometric Baseline of the ERS-2 = Optimal with 30 min. separation"]
-[8.150344848632812, 0.10355035960674286, "[FF] Launch Date of the Meteor-M #2 = July 8, 2014"]
-[3.894974708557129, 4.293270587921143, "[FF] Primary Objective of the RISAT-1 = Earth observation"]
-[3.624061107635498, 2.706468343734741, "[TT] Number of Satellites of the Iridium NEXT = 81"]
-[7.6415510177612305, 1.5353502035140991, "[TT] Maturity of the Marine litter aggregation forecast = Not Mature"]
-[8.575227737426758, 5.859436511993408, "[TT] Systematic Radial Bias of the Baseline Products = About ten times lower than cross-track bias"]
-[10.271566390991211, 3.1950111389160156, "[FF] URL of the TOPCAT = https://web.archive.org/web/20120306134455/http://www.bis.gov.uk/assets/bispartners/ukspaceagency/docs/space%20science/cubesats/topcat%20text%20and%20picture.pdf"]
-[10.839540481567383, 1.0153671503067017, "[TT] Primary Mass of the White Dwarfs = About three times as massive as the secondary"]
-[12.202445983886719, -0.19886723160743713, "[TT] Responsible for the Cameras of the TESS = MIT/LL (Lincoln Laboratory)"]
-[10.030046463012695, -1.5304827690124512, "[TT] Orbit Inclination of the EAGLE = 0\u00ba"]
-[13.533787727355957, 2.7893760204315186, "[TT] Mass of the Comet = 10 billion tons"]
-[5.0389885902404785, 7.166588306427002, "[TT] Telemetry Downlink Data Rate of the NEMO-HD = 8 kbit/s"]
-[4.867761135101318, 0.9158197045326233, "[TT] International Designation of the GFO = 1998-007A"]
-[8.668453216552734, 2.0526697635650635, "[TT] IFOV of the SeaWinds scatterometer = \u00b152\u00b0"]
-[3.1294960975646973, 2.241924285888672, "[FF] Monitoring Capabilities of the Copernicus Sentinel-3 = Wildfires, land use, vegetation state, sea surface temperature, sea surface color, sea surface height"]
-[10.134947776794434, 3.2135417461395264, "[FF] Function of the Juventas CubeSat = Perform the first radar probe of an asteroid"]
-[11.647562980651855, 3.6981050968170166, "[TT] Total Firing Time of the Y-axis Bang-Bang Maneuver = 60 seconds"]
-[5.397177696228027, 2.6716277599334717, "[TT] Manufacturer of the OceanSat-2 = Indian Space Research Organization (ISRO)"]
-[14.031320571899414, 7.130358695983887, "[TT] Power Bus of the EPS = Unregulated 22 V - 36 V"]
-[9.614399909973145, 7.047563076019287, "[TT] Spatial Resolution of the ECOSTRESS = 38 m in-track by 69 m cross-track"]
-[8.037581443786621, -0.9452518820762634, "[TT] Measurement of the ICESat-2 = Around the clock"]
-[10.194657325744629, 1.3995797634124756, "[TT] Number of Stars of the Gaia EDR3 = More than 1.8 billion"]
-[5.013985633850098, 4.316473960876465, "[TT] Preorder Deposit of the Starlink = USD 99"]
-[11.750514030456543, 4.796638488769531, "[TT] Size of the UniSat-5 = 50 cm x 50 cm x 50 cm"]
-[5.4612274169921875, 7.133435249328613, "[TT] Test Transmission Data Rate of the Herschel = 1.5 Mbit/s"]
-[5.846368789672852, 6.53427791595459, "[TT] Latency of the ATL00 Telemetry Data = Downlinked 8 times/day"]
-[9.957380294799805, 0.13112680613994598, "[TT] Orbit Distance of the GRACE-FO satellites = 220 km"]
-[10.773355484008789, 3.279364585876465, "[FF] Technology of the Micro-gravity experiment = Important for improving the quality of crystals"]
-[6.586798667907715, -2.047492504119873, "[FF] Update Date of the Jason-3 = Feb. 11, 2016"]
-[8.60243034362793, 6.116484642028809, "[TT] Deviation from Omni-directionality of the OVM = Less than 0.2 nT"]
-[8.392582893371582, 3.9148097038269043, "[FF] Particles Detected of the Carmen-2 = e-, p+ (high-energy particle flux of electrons and protons) and ion fluxes"]
-[4.862950801849365, 0.10245656222105026, "[TT] Launch Date of the SpaceX CRS-16 = 5 December 2018"]
-[8.238838195800781, 6.9996724128723145, "[TT] Number of Images Transmitted of the Tyvak-0130 = More than 4,500"]
-[13.437675476074219, 5.757474422454834, "[FF] Open Circuit Voltage (Voc) of the Solar Panel = Variable"]
-[11.194388389587402, 5.381274700164795, "[TT] Plastic Scintillator of the Range Calorimeter = Side of 15 cm"]
-[4.054863929748535, 6.355909824371338, "[TT] Antenna Location of the NanoCom SDR = -Z face of the satellite"]
-[9.096006393432617, 3.176866292953491, "[FF] Objective of the EPAM = Measurement of solar and interplanetary particle fluxes with a wide dynamic range and a directional coverage of nearly a full unit sphere"]
-[8.340278625488281, 7.749306678771973, "[TT] SWIR Camera Settings of the CUMULOS = Low-gain, 32 ms exposure"]
-[6.9767842292785645, 0.7971533536911011, "[FF] Launch Date of the InSight Mars Lander = May 5, 2018"]
-[12.130112648010254, 6.156487464904785, "[TT] Helium Events of the AMS-02 = 3.7 billion"]
-[4.660189151763916, 0.8869951367378235, "[TT] Development Time Frame of the GOME = 1990-1994"]
-[8.964978218078613, 4.396142959594727, "[FF] Function of the Sun sensor = Determine accurately the yaw orientation"]
-[8.948437690734863, 7.508524417877197, "[TT] Size of the Particle Detectors = 95 mm x 122 mm x 217 mm"]
-[3.49674391746521, 1.9217007160186768, "[FF] Electrical/Functional Allocation of the Sentinel-5P = Classical architecture"]
-[9.351542472839355, 4.9836249351501465, "[FF] Measurement Model of the ADCS = Comprised of sensory inputs and computed attitudes"]
-[9.422215461730957, 3.99695086479187, "[FF] Magnetic Impulse of the Ground-based sensors = Recorded"]
-[10.276601791381836, 7.976276874542236, "[TT] Diodes Area of the Telescope = 3cm2"]
-[9.398609161376953, 3.2888259887695312, "[FF] Manufacturer of the Solar Wind Concentrator = Los Alamos National Laboratory"]
-[5.47438907623291, 4.114389896392822, "[FF] Capacity of the SES-17 = Up to ten times more than traditional satellites"]
-[9.521974563598633, 4.799952983856201, "[TT] Attitude Control of the AOCS = 3-axis"]
-[9.743195533752441, -1.3831636905670166, "[TT] Orbital Inclination of the International Space Station = Between 52 degrees north and 52 degrees south latitudes"]
-[5.109883785247803, 4.669589519500732, "[TT] Tracking Station Passes of the Odin = 10 per day"]
-[13.953573226928711, 7.149116039276123, "[TT] Microcontroller Power of the C&DH Subsystem = +5 volt input"]
-[13.015542984008789, 3.1287550926208496, "[TT] Fuel Capacity of the Sentinel-2A = 123 kg"]
-[5.209933757781982, 0.15780875086784363, "[TT] Death Year of the Max Valier = 1930"]
-[3.4063901901245117, 4.9159770011901855, "[FF] SAR Data Acquisition of the X-UGS = Absence of acquisition and processing functionalities"]
-[8.613550186157227, 7.068770408630371, "[TT] Spectral Range of the WV60 imager = 0.45 \u00b5m- 0.90 \u00b5m"]
-[5.2781081199646, 1.3140839338302612, "[FF] Conference Presentation of the SWAP = March 30-April 2, 2004"]
-[5.0374298095703125, 0.5629899501800537, "[FF] Tracking Task Completion Date of the VLBI system = November 2, 2010"]
-[5.837141036987305, 2.553088426589966, "[FF] Award Abstract Number of the OPAL = 1242901"]
-[9.34107494354248, 4.661956787109375, "[FF] Architecture of the AOCS = Three-axis stabilized system using a reaction wheel assembly for attitude control, star trackers for attitude control, and the EPPS for orbit maintenance"]
-[3.655728816986084, 5.251467227935791, "[TT] Azimuth Dwell Time of the Radar = 42 ms"]
-[11.039726257324219, 6.0897908210754395, "[FF] Width of the Cover Glass = Smaller than the silicon substrate"]
-[6.341769695281982, 1.0309138298034668, "[TT] Imaging Date of the Landsat 8 = October 31, 2021"]
-[5.218780517578125, 8.2500638961792, "[TT] Bandwidth of the Ranging Channel = Approximately 800 kHz"]
-[10.728349685668945, 5.568915367126465, "[FF] Isolation Solutions of the SMA = Polyimide tape layer covered by a heat shrink sleeve, G10 composite bushings"]
-[5.075534343719482, 3.4110970497131348, "[TT] Manufacturer of the Optical Communication Payload = Tesat Spacecom GmbH"]
-[6.0712199211120605, 1.3683667182922363, "[TT] Mission Duration of the EURECA = 336 days"]
-[5.1972174644470215, 7.0340070724487305, "[TT] Data Rate of the Data Downlink = Up to 640 Mbit/s"]
-[6.597851276397705, 5.194175720214844, "[FF] Provides of the PIH = Structural, electrical, and C&DH interfaces"]
-[10.725982666015625, 2.800945281982422, "[FF] Acta Astronautica Publication Date of the STRV 1 microsatellite series = August 1997"]
-[10.998832702636719, 2.0550923347473145, "[FF] Article Date of the XMM-Newton = 21 November 2018"]
-[10.569413185119629, 2.3146352767944336, "[FF] Data Products of the X-ray and Microdosimeter = Survey level X-ray and microdosimeter measurements"]
-[9.495850563049316, 0.9733676910400391, "[FF] Size of the OMOTENASHI = Unknown"]
-[3.7281744480133057, 6.431308746337891, "[TT] Off-Nadir Intervals of the Active Antenna = ~ 9 km"]
-[4.939456939697266, 1.7886942625045776, "[FF] Responsibilities of the TURAF = Planning, data acquisition, processing and distribution of the G\u00f6kt\u00fcrk-2 satellite data"]
-[11.146570205688477, 5.987306594848633, "[TT] Shielding of the LDT = Different for each floor at right angles to the sensors"]
-[9.124217987060547, 2.8674890995025635, "[FF] Technique Developer of the Solar Flare = Alina-Catalina Donea"]
-[8.02857494354248, 5.0452165603637695, "[FF] Precision Measurement Method of the Servo-system = Measurement of the electrical power applied to each channel for the two cases"]
-[7.3098530769348145, 2.5459256172180176, "[FF] Purpose of the TRISHNA = Climate monitoring and operational applications"]
-[10.724900245666504, 1.399276852607727, "[TT] Size of the Manatee Nebula = Spanning the equivalent size of four full Moons"]
-[9.858522415161133, 6.484930992126465, "[TT] Size of the Earth Radiation Budget Experiment (ERBE) = 60 cm x 60 cm x 57.6 cm/unit"]
-[7.44375467300415, 5.035303115844727, "[FF] Alignment Requirement of the RTA = Perfect"]
-[7.810910224914551, 5.5785369873046875, "[FF] Components of the GFI = Metrology optics, scanning actuator"]
-[8.319890975952148, 2.3429677486419678, "[FF] Formation Process of the Above-anvil cirrus plumes = Intense updrafts puncture the tropopause and airflow draws cirrus cloud tops into the stratosphere"]
-[5.308966636657715, 8.683252334594727, "[TT] Bandwidth of the Band 6 = 675-685 nm"]
-[5.003097057342529, 3.3472909927368164, "[TT] Manufacturer of the BPA-3 = Hartron-Arkos"]
-[4.643216133117676, 7.6734724044799805, "[TT] Pulse Repetition Frequency (PRF) of the Satellite = 1795.33 Hz (Ku-band), 448.83 Hz (S-band)"]
-[7.929202556610107, 9.090928077697754, "[FF] Wavelength of the FAI = 630 nm"]
-[5.007673263549805, 3.5357863903045654, "[TT] Manufacturer of the ADCS = XACT, Blue Canyon Technology"]
-[5.556482315063477, 6.160315036773682, "[TT] Type of the OBCM = Enhanced by a mass memory"]
-[11.93509578704834, 4.807380199432373, "[TT] Dimensions of the VELOX-PII = 10 cm x 10 cm x 11.35 cm"]
-[7.948450565338135, 6.470139503479004, "[FF] Image Type of the Long-Range Reconnaissance Imager (LORRI) = Color"]
-[10.045016288757324, 7.5503764152526855, "[TT] Swath Width of the Imager = 290 km"]
-[9.407940864562988, 7.3051838874816895, "[TT] Spatial Resolution of the Spectral Channels = 28 \u00b5rad (1 km x 1 km at nadir) (+0-10%)"]
-[8.941980361938477, 2.7480554580688477, "[FF] Image Content of the INTEGRAL = Shows the auroras forming a rough semi-circle at Earth\u2019s northern latitudes"]
-[9.977010726928711, -1.4832650423049927, "[TT] Inclination of the Orbit = 40.5\u00ba"]
-[7.179511547088623, 5.381816864013672, "[FF] Micro-Switch Location of the ISM = Adjacent to the ISM"]
-[5.749629974365234, 2.682070255279541, "[FF] Consortium of the RemoveDEBRIS spacecraft = Surrey Space Center at the University of Surrey and co-funded by the EC (European Commission)"]
-[8.430193901062012, 3.1555325984954834, "[FF] URL of the Solar Backscatter Ultraviolet/Total Ozone Mapping Spectrometer (SBUV/TOMS) = http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1978-098A-09"]
-[14.237316131591797, 3.1877760887145996, "[TT] Mass of the CanX-7 = 8 kg"]
-[8.053901672363281, 4.378751277923584, "[FF] Design and Performance of the Dual-channel Radiometers for Earth and Atmosphere Monitoring (DREAM) = Protoflight Model"]
-[6.075037479400635, 4.40940523147583, "[FF] Purpose of the GFP = FSS (Fixed Service Satellite), DBS (Direct Broadcast Satellite) and broadband missions"]
-[7.557762622833252, 7.072887420654297, "[TT] Levels of the CSI = 4"]
-[9.035911560058594, 3.3193631172180176, "[FF] Associated Plasma Dynamics of the Plasma Blobs = Investigated in the topside ionosphere"]
-[4.858840465545654, 0.1748875081539154, "[TT] End of Life Date of the CXBN-2 = 1 March 2019"]
-[13.560245513916016, 5.469797611236572, "[TT] Solar Cell Sections of the BCR Module = Twelve solar cell sections in total on three solar panels"]
-[7.997705459594727, 7.709552764892578, "[TT] Spectral Bands of the High-Resolution Hyperspectral Imager = 220 bands"]
-[3.451662540435791, 6.42941427230835, "[TT] Length of the X-band antenna = 3.3 m"]
-[8.504364967346191, 3.6158483028411865, "[FF] Mission Date of the Total Solar Irradiance Calibration Transfer Experiment (TCTE) = July 31, 2012"]
-[14.643037796020508, 6.759222507476807, "[TT] Battery Capacity of the EPS = 108 Wh"]
-[7.266963005065918, 2.880125045776367, "[TT] Data Availability of the MethaneSAT = Freely available"]
-[13.461870193481445, 2.8322272300720215, "[TT] Mass of the Starlink Satellite = ~227 kg"]
-[4.952449321746826, 3.354004383087158, "[TT] Manufacturer of the PPS-1350-G = SNECMA of France"]
-[7.68377161026001, 0.2562871277332306, "[TT] L5 Cloud Encounter Date of the Lucy = 2033"]
-[9.947914123535156, 8.060434341430664, "[TT] Focal Ratio of the Telescope = F/5"]
-[5.4140214920043945, 4.940397262573242, "[FF] Operation Setup Time of the Integrated Mobile Station = Short"]
-[4.805325984954834, 0.034068863838911057, "[TT] End of Life Date of the Satellite = 30 Sep 2023"]
-[8.656506538391113, 7.686814785003662, "[TT] Detector Size of the MSI-0 and MSI-1 = 1024 x 1024 pixels"]
-[4.92925500869751, -2.141441822052002, "[TT] Weight of the Chang'e-5 = 8.2 tons"]
-[7.506880283355713, 2.005154848098755, "[FF] Purpose of the CBERS-4A = Monitor water resources, agriculture, urban growth, and land use, with a large focus on the preservation of the Amazon rainforest"]
-[7.0217108726501465, 3.7393317222595215, "[FF] Redundancy Approach of the PROBA-3 = Cold redundancy and use radiation-hardened qualified components"]
-[6.449951171875, -0.08633597195148468, "[TT] Manual Operations Frequency of the AISSat-1 = Once a week"]
-[9.264636039733887, 7.250113487243652, "[TT] Geometric Factor of the NINA = 8.6 cm 2 sr for low energy particles to 1 cm 2 sr for particles crossing the detector"]
-[3.7256288528442383, 5.6872992515563965, "[TT] PRF of the Radar = 1464-1640 Hz"]
-[3.363658905029297, 6.348984241485596, "[TT] Dimensions of the Antenna Mast = 16 x 16 x 6 cm"]
-[3.814073324203491, 7.957217216491699, "[TT] Modulation of the ITUs = QPSK (Quadra-Phase Shift Keying)"]
-[7.628233432769775, 8.895421028137207, "[FF] Bands of the CLAUDIA-CAI = 0.67, 0.87 and 1.60 \u00b5m"]
-[10.346658706665039, 5.896496772766113, "[FF] Qualification Tests of the Antenna = Temperature cycling, vibration, thermal vacuum"]
-[9.32563591003418, 6.946151256561279, "[TT] Position Resolution of the STD = 8.5 \u00b5m"]
-[5.227301120758057, 1.0202000141143799, "[FF] Approval Date of the SMC-S-016 = 5 September 2014"]
-[8.025508880615234, 3.2236719131469727, "[FF] Method of the Retrieval of column-averaged volume mixing ratio of CO2 = Ground-based high spectral resolution solar absorption"]
-[7.929703235626221, 3.164626121520996, "[FF] Detection Capability of the Harris TANSO-FTS-2 = Precise locations of greenhouse gas emissions"]
-[9.628264427185059, 8.342853546142578, "[TT] Full Angle of the Pixel FOV = 2\u00ba"]
-[6.016711711883545, 1.6313257217407227, "[FF] Presentation Date of the Small Satellites = Sept. 29 to Oct. 3, 2008"]
-[5.434309482574463, 2.7289257049560547, "[TT] Lead Organization of the LCRD = NASA\u2019s Goddard Space Flight Center"]
-[10.835054397583008, 7.492011070251465, "[TT] Swath of the SLSTR = 750 km"]
-[9.310107231140137, 7.422327995300293, "[TT] Ground Resolution of the NAOMI = 0.7 m in the panchromatic channel"]
-[5.380669116973877, 1.7475556135177612, "[FF] Presentation of the Global Change Observation Mission = Unknown"]
-[5.632876396179199, 2.8177130222320557, "[TT] Funding of the NIRCam = NASA"]
-[6.624873638153076, 2.7735276222229004, "[FF] Development Team of the Microsized Microwave Atmospheric Satellite (MicroMAS) = K. Cahoy, R. Kingsbury, E. Peters, A. Marinan, M. Prinkey, E. Wise, P. Dave, S. Paek, C. Pong, D. Miller, D. Sklair, B. Coffee, L. Orrego, E. Main, K. Frey, R. Aniceto, P. Vaidyanathan"]
-[6.3059492111206055, 3.3036930561065674, "[TT] Number of Operational Satellites of the BlackSky Constellation = 17"]
-[12.186521530151367, 3.1113789081573486, "[TT] Propellant of the DMC Propulsion Subsystem = Butane"]
-[3.779831647872925, 4.754337787628174, "[TT] Yaw Steering of the RADARSAT-1 = None"]
-[7.083247661590576, 5.372779369354248, "[FF] Operation Principle of the STROFIO = The start time is imprinted on the trajectory of the particle by a radio frequency electric field, that bends the trajectory in a given plane, and the stop time is the time when the particle reaches the detector"]
-[10.100715637207031, 1.0916774272918701, "[TT] Distance from the Sun of the Galactic Center = Almost 30,000 light years"]
-[6.103359222412109, 3.1305758953094482, "[TT] Number of Scientists and Engineers of the ASTRO-H = 266"]
-[8.048511505126953, 8.824492454528809, "[TT] Spectroscopy Range of the CUTE = 255 to 330 nm"]
-[8.164417266845703, 5.659780025482178, "[TT] GPS/UTC Accuracy of the Data Handling Subsystem = 100 \u00b5s"]
-[10.445000648498535, 7.267691135406494, "[TT] Ground Swath of the Payload = 15 km"]
-[14.400339126586914, 3.3107879161834717, "[TT] Mass of the SD2 = 4.8 kg"]
-[8.095820426940918, 0.5353261232376099, "[FF] Orbit of the Lutetia = Main asteroid belt between Mars and Jupiter"]
-[8.849946022033691, 4.256017684936523, "[FF] Perigee Phase of the S/C = Free flight and Sun pointing"]
-[12.034148216247559, 4.976692199707031, "[TT] Volume of the RCU = 300 x 240 x 80 mm"]
-[10.907678604125977, 10.099133491516113, "[TT] Installation Date of the Alpha Magnetic Spectrometer (AMS) = May 2011"]
-[13.38007926940918, 7.383662223815918, "[TT] Power of the HID = 2.0 W"]
-[10.94741439819336, 4.275933742523193, "[TT] Decks of the Bus = Bottom deck, top deck and payload deck"]
-[4.801274299621582, 0.5020354986190796, "[TT] Development Time of the CuPID = Sixteen years"]
-[7.54931640625, 4.744624614715576, "[FF] Conference Presentation of the Sensor Web = First IEEE International Conference on Sensors 2002"]
-[7.60377836227417, 3.374985694885254, "[FF] Purpose of the CiELO = Assess the collision risk to space missions from small-sized debris"]
-[8.82723617553711, 6.381518363952637, "[TT] Height Bias of the ALT = 0.0 \u00b1 0.07 m"]
-[12.00027084350586, 0.5508166551589966, "[FF] Sensor Complement of the PLATO = Detection and characterization of terrestrial exoplanets around bright solar-type stars"]
-[5.689154624938965, 1.9800869226455688, "[TT] Splashdown Location of the Orion = Pacific Ocean"]
-[6.504961013793945, 3.6622977256774902, "[FF] Services of the Data Collection, Rescue = Search & Rescue, Data Collection, Emergency Manager\u2019s Weather Information Network (EMWIN)"]
-[8.44692611694336, 6.086544513702393, "[TT] Measurement Accuracy - Location of the Instrument = 1 pixel"]
-[5.007688999176025, 0.09176480770111084, "[TT] End of Operations of the SPOT-1 = November 2003"]
-[7.988647937774658, 4.597925186157227, "[FF] Total Ionizing Dose Measurement of the RADMON = Unknown"]
-[7.393982410430908, 0.2564529478549957, "[FF] Mission Status of the OSIRIS-REx = Ready for Touchdown on Asteroid Bennu"]
-[7.563094139099121, -2.4719772338867188, "[FF] Launch Date of the GOLD = July 31, 2015"]
-[5.1950507164001465, 2.76119065284729, "[TT] Mission Lead of the TEMPEST-D = Colorado State University"]
-[8.546808242797852, 8.734549522399902, "[FF] Function of the Diffraction Grating = Disperses the light"]
-[16.473464965820312, 3.5692427158355713, "[FF] Launch Date of the UWE-1 = Unknown"]
-[7.314796447753906, 7.76780366897583, "[FF] Instrument Performance Parameters of the HIT = Summarized in Table 10"]
-[7.9695143699646, 6.3994855880737305, "[FF] Measurement Accuracy of the Imager = Location: 1 pixel; intensity: 10%; time tag at frame rate"]
-[5.004279613494873, 0.37932103872299194, "[TT] Launch Date of the DSX spacecraft = June 25, 2019"]
-[13.982542037963867, 7.094028472900391, "[TT] Bias Voltage of the Suppressor Grid = -12 V"]
-[14.522244453430176, 6.590625762939453, "[TT] Battery Capacity of the Genesis spacecraft = 448 Whr at 100% SOC and 313 Whr at 70% SOC"]
-[9.309935569763184, 6.7733845710754395, "[TT] Resolution of the Satellite = 10 meters"]
-[9.33963394165039, 5.031506061553955, "[TT] Attitude Pointing Control of the Spacecraft = 1\u00ba in pitch, roll, yaw"]
-[10.398591995239258, 2.072683811187744, "[TT] Number of X-ray Sources of the eROSITA X-ray telescope = More than one million objects"]
-[8.524669647216797, 3.120143175125122, "[FF] Build Date of the IUE (International Ultraviolet Explorer) = 1970s"]
-[10.350886344909668, 8.00919246673584, "[TT] Telescope Diameter of the Submillimeterwave receiver = 30 cm"]
-[6.799476623535156, -0.5676376223564148, "[TT] Repeat Cycle of the MTG-S Spacecraft = 10 minutes"]
-[5.732278823852539, 6.1159987449646, "[TT] Devices per Partition of the SDRAM based memory module = 8 SDRAM chips with a capacity of 512 Mbit each"]
-[4.847843170166016, 0.9470986723899841, "[TT] Telescience Support Unit Presentation Date of the Foton = Oct. 2-6, 2006"]
-[6.433530330657959, 6.375301361083984, "[TT] Response Time of the System = Less than 36 hours"]
-[4.865880966186523, 0.507234513759613, "[TT] Launch Date of the CADRE = 6 December 2015"]
-[4.793497562408447, 5.552848815917969, "[FF] Location Technique of the PTT-HD or PMT-HD = Not designed to be autonomously located by Doppler technique"]
-[8.725504875183105, 8.646409034729004, "[TT] Pixels per FWHM of the Spectrometer = 580"]
-[9.065821647644043, 0.5293012261390686, "[FF] Types of Maneuvers of the THEMIS (and ARTEMIS) spacecraft = 4 orbit change maneuvers, one attitude, and one spin rate adjustment per probe"]
-[5.346465587615967, 2.527794599533081, "[FF] Modes of Operation of the CXBN-2 = Failure recovery, standby/uplink, downlink, and full science modes"]
-[7.862864017486572, 0.1447998732328415, "[FF] Input Data of the Goddard Earth Observing System, Version 5 = GRACE-FO data"]
-[6.191331386566162, 2.315563201904297, "[FF] Image Credit of the OMI = KNMI"]
-[10.03747272491455, 2.953415870666504, "[FF] Development Start Year of the CubeSat = 2015"]
-[5.0702223777771, -0.008043593727052212, "[TT] End of Life Date of the STRV-1a and -1b = 2001"]
-[8.638761520385742, 8.790363311767578, "[FF] Sensitivity of the Interferometric Spectroscopic Instruments = Typically 100 times those of conventional grating spectroscopic instruments of similar size"]
-[5.40100622177124, 1.6878868341445923, "[FF] Ability of the ALOS-2 = Penetrate rain and clouds, penetrate forest canopies"]
-[9.420820236206055, -1.3591796159744263, "[TT] Eccentricity of the GEOS-1 = 0.07193"]
-[4.597322463989258, 2.9302704334259033, "[TT] Location of the HSC = ESAC (ESA/European Space Astronomy Centre) in Villafranca, Spain"]
-[9.253829956054688, 7.321300029754639, "[TT] Resolution of the AEISS-A = 0.5 m for panchromatic imagery"]
-[5.638873100280762, 2.4972329139709473, "[FF] Partners of the Rosalind Franklin = ESA and the Russian State Space Corporation, Roscosmos"]
-[4.685839653015137, 0.4878087043762207, "[TT] Reaction Wheel Problem Start Date of the SARAL/AltiKa = July 2016"]
-[6.115534782409668, 6.4239091873168945, "[TT] Latency Requirement of the S-1 NTC = Within 20 days"]
-[8.317465782165527, 7.752181053161621, "[TT] Detector Technologies of the Imager = Monolithic Si (VNIR); hybrid HgCdTe CMOS (SWIR)"]
-[9.534683227539062, 0.7016785740852356, "[TT] Closest Approach Distance of the BepiColombo = 199 km"]
-[11.985079765319824, -0.16611769795417786, "[FF] Observation Data of the TESS = Used to create an asteroseismic model"]
-[5.849842548370361, 3.3693840503692627, "[TT] Cost of the Full-size Earth-observing satellite = Hundreds of millions of dollars to build, launch, and operate"]
-[7.337153434753418, 1.0976253747940063, "[FF] Science Objective of the Ma_MISS = Study the Martian subsurface"]
-[9.341169357299805, 5.9408793449401855, "[TT] Onboard Sensors of the SPOT 6-7 = HRV, HRVIR, HRG and NAOMI"]
-[5.878349781036377, 0.3417942523956299, "[TT] Data Collection Duration of the GPM = Last 19 years"]
-[7.166942596435547, 0.8830297589302063, "[TT] Operation Period of the SeaSat = 26 June - 10 October 1978"]
-[12.428092956542969, 0.6349291801452637, "[TT] Optically Sensitive Surface of the PLATO CCDs = 0.74 m2"]
-[6.965360164642334, 5.656389236450195, "[TT] Quantity of the IOV Units = 10"]
-[5.43132209777832, 1.6331923007965088, "[TT] Field of Regard (FOR) of the ALOS-2 = Up to about 3 times (from 870 km on Daichi to 2,320 km)"]
-[10.63565731048584, 1.511864185333252, "[FF] Black Hole Size of the Was 49b = Unknown"]
-[9.56214714050293, -0.46084314584732056, "[TT] Initial Orbit Altitude of the FormoSat-7/COSMIC-2 satellites = 720 km"]
-[6.297934055328369, 2.5738368034362793, "[TT] Program Affiliation of the IMAP = Solar Terrestrial Probes (STP) Program"]
-[8.675357818603516, 8.768197059631348, "[TT] Grating Order of the Spectrometer = 2"]
-[8.930702209472656, 6.957787990570068, "[TT] Imaging Resolution of the NEMO-HD = 2.8 m GSD"]
-[3.5886857509613037, 6.453444004058838, "[TT] Antenna Diameter of the Earth station = 5 m"]
-[4.4510908126831055, 3.020598888397217, "[TT] Location of the CMCC = Trenton, Ontario"]
-[6.535711288452148, -0.5381491780281067, "[TT] Period of the WorldView-3 = 97 minutes"]
-[9.74185848236084, 1.3935232162475586, "[TT] Total Imaging Area of the Pleiades = 40,000 km2"]
-[4.973235607147217, 3.242884635925293, "[TT] Manufacturer of the SEEDS-2 = Nihon University, Japan"]
-[9.864301681518555, 7.038344860076904, "[TT] Stereo Observations Area of the GIS Instrument = Up to 6270 km2 daily"]
-[6.064610004425049, 5.031012535095215, "[FF] Control Subsystem of the Active Antenna Subsystem = Distributed embedded control subsystem"]
-[7.2353339195251465, 6.260337829589844, "[FF] Measurement Interval of the FTS = Approximately every two minutes"]
-[9.053985595703125, 5.181093215942383, "[TT] Technology of the Inertial reference unit (IRU) = Fiber Optic Gyro"]
-[4.3617777824401855, 3.9120869636535645, "[FF] Data Characterization of the Sensor Station = In-depth validation of Galileo Mission Segment key technology and design aspects"]
-[9.537997245788574, 7.1038818359375, "[TT] Spatial Resolution of the PMI = 34 x 19 km"]
-[7.96572208404541, 2.924530267715454, "[FF] Requirement of the United States = Measure atmospheric carbon with great precision and high spatial resolution"]
-[7.211937427520752, 1.885264277458191, "[TT] Construction Time of the Carbonite-1 = 6 months"]
-[8.587418556213379, 5.468634128570557, "[FF] Curvature Determination Error of the STD = \u0394R/R"]
-[11.993982315063477, -0.14341233670711517, "[FF] Follow-up Observations of the TESS = Spectroscopy"]
-[14.074179649353027, 6.797568321228027, "[TT] Voltage Range of the GomSpace NanoPower BPX = 24 V to 32.8 V"]
-[3.888669967651367, 6.297985553741455, "[TT] Number of Antennas of the MEOLUT = 4"]
-[10.13818359375, 6.487328052520752, "[TT] Distance from Other People of the MABEL = A hundred miles"]
-[7.142947673797607, 6.490248203277588, "[FF] Effect of the SM = Makes the outgoing beam parallel to the incoming beam"]
-[7.506932735443115, 4.793681621551514, "[TT] Mounting Location of the Shadow Position Sensor (SPS) = CSC"]
-[6.180917263031006, 4.026006698608398, "[FF] Purpose of the SSN dedicated satellites = Observe other satellites and orbital debris"]
-[4.898312568664551, 5.091391086578369, "[TT] CCSDS ID of the GSAT-0101 = 3A5"]
-[13.24016284942627, 5.437702178955078, "[FF] Configuration of the Solar Array = Deployed and stowed"]
-[10.168416976928711, 5.775875568389893, "[TT] FPA Cooling of the Camera = Passively cooled"]
-[14.303325653076172, 3.007997751235962, "[TT] Mass of the HORYU-2 = 7.1 kg"]
-[4.745116233825684, -1.8160876035690308, "[TT] Launch Date of the Chang'e-1 = Oct. 24, 2007"]
-[10.102402687072754, 1.5176961421966553, "[FF] Survey Map Feature of the eROSITA = Huge circular structure of hot gas below the plane of the Milky Way"]
-[6.463064193725586, -0.617796003818512, "[TT] Repeat Cycle of the CBERS-3 = 26 days"]
-[5.288303375244141, 1.5662562847137451, "[FF] Operation Completion Date of the DAICHI (ALOS) = May 12, 2011"]
-[7.3726420402526855, 6.245448112487793, "[FF] Integration Time of the Responsivity Measurement = Almost cancel the noise on the measurements"]
-[4.816412448883057, 0.5544888973236084, "[TT] Launch Date of the ANUSat = April 20, 2009"]
-[8.401959419250488, 8.197042465209961, "[TT] Multispectral Band: Red of the NAOMI = 0.62 \u00b5m - 0.69 \u00b5m"]
-[1.947251319885254, -0.39236482977867126, "[FF] Risk of the Van Allen Probes = Earth could be at risk for up to trillions of dollars of damage"]
-[12.055133819580078, 4.9294023513793945, "[TT] PCB Layers of the MPPT = 6"]
-[9.05273723602295, 3.1547327041625977, "[FF] Objectives of the ISEE-1 = Observation of the near-Earth magnetosphere and its boundaries, better understanding of many phenomena, such as the Earth's bow shock, the magnetosheath and magnetopause, interactions between the tail and aurorae, and particle populations and flows in the tail"]
-[8.13422679901123, -1.0856928825378418, "[FF] Measurement Capability of the ICESat-2 = All of these lakes and reservoirs"]
-[9.612109184265137, 7.130206108093262, "[TT] Resolution (Smoothed images) of the OLS = 2.8 km"]
-[6.612020492553711, -0.5600388050079346, "[TT] Mission Period of the Corvus-BC 4 = 3 minutes"]
-[10.161957740783691, 4.596231460571289, "[TT] Reaction Wheel Rotation of the Integral = Roughly one rotation every 21 minutes"]
-[5.706582546234131, -0.8729544281959534, "[TT] Design Life of the MERLIN = Approximately three years"]
-[8.947164535522461, 7.69321346282959, "[TT] Triangulation Results of the RASAT = 1-1.5 pixels"]
-[5.170020580291748, 0.29151979088783264, "[TT] Deployment Order of the SAPPHIRE = After PICOSat"]
-[7.82144021987915, 2.110811948776245, "[FF] Purpose of the SGLI = Provide ocean color capability not accomplished by NPP, plus augment other VIIRS capabilities"]
-[4.360537528991699, 3.05975604057312, "[TT] Tracking Stations of the QZS-1/Michibiki = Chofu, Singapore, Sydney, Maui, and Tahiti"]
-[8.159281730651855, 6.646551609039307, "[TT] Maximum Acquisition Capability of the Satellite = 1800 images in a 24 hour period"]
-[11.319390296936035, 5.766161918640137, "[TT] Structure Material of the Payload Module = CFRP face skin"]
-[13.951045989990234, 7.183691501617432, "[TT] Power of the Voltage 7 = 1.66"]
-[8.61922550201416, 2.2913103103637695, "[TT] Wind Velocity Range (PBL) of the Aeolus = \u00b1150 m/s"]
-[5.843626499176025, 4.449418544769287, "[FF] Validation Data Source of the CYGNSS = GPS dropsondes, SFMR, IWARP"]
-[7.041675090789795, 7.0779128074646, "[TT] Peak Fluency of the InnoSlab laser = Smaller than 2.5 J/cm2"]
-[9.462890625, -1.0822067260742188, "[TT] Longitude of the GOES-S = 137\u00ba W"]
-[5.4545793533325195, 2.676764965057373, "[TT] Builder of the ISEE-1 = NASA"]
-[7.529099464416504, 5.086644172668457, "[FF] Purpose of the VECTION = Estimate the distance to an object, length of an object and orientation of their bodies in space"]
-[5.025652885437012, 3.58258056640625, "[TT] Developers of the Level 2 products = KNMI, SRON, DLR and BIRA"]
-[4.759169101715088, -1.837285041809082, "[TT] Sample Transfer Date of the Chang'e-5 = Around Dec. 15-16"]
-[11.310866355895996, 3.4762637615203857, "[FF] Purpose of the Electric Propulsion = Propel the satellites from the orbit in which they will be launched to the final operational orbits"]
-[10.849101066589355, 1.4512290954589844, "[FF] Mass of the Neutron Star = One to two times the mass of the Sun"]
-[7.915910720825195, 6.699338436126709, "[FF] Function of the PH-A = Driving the HVs of the photomultipliers, Driving the power supply of the calibration sources, Providing the necessary power lines (+5V, \u00b112 V) and switching them on and off, Acquiring (including data quantization) signals from the sensor"]
-[6.934761047363281, 3.833902359008789, "[FF] Operation of the Robotic arms and space vehicles = Remotely operated using virtual reality and haptics interfaces"]
-[6.498603343963623, 3.4814746379852295, "[TT] Payload Condition of the AMS-02 = Good"]
-[9.467306137084961, 0.8321036100387573, "[TT] Journey Distance of the Orion = 3,300 miles above Earth"]
-[7.5503435134887695, 3.403325080871582, "[FF] Description of the Orthorectified and Atmospheric Corrected Product (L1A) = The product is derived from the LevelC product, atmospherically corrected and the data converted to ground surface reflectance values"]
-[5.6183342933654785, 0.7741334438323975, "[FF] Unveiling Date of the ZACUBE-01 = Oct. 1, 2011"]
-[9.33460807800293, 8.011921882629395, "[TT] Field of View of the Data Receiver = 15 \u00b5rad"]
-[10.366146087646484, 7.953265190124512, "[TT] Telescope Diameter of the ATLAS = 0.8 m"]
-[6.4260969161987305, 4.938153266906738, "[TT] Carries of the nSight-1 = FIPEX"]
-[10.153512001037598, 0.9837606549263, "[FF] Distance from Earth of the TYC 7037-89-1 = About 1,900 light-years"]
-[7.9159255027771, 7.395191192626953, "[TT] Data Output of the TDI Detector = 290 Mpixel/s total"]
-[5.132645606994629, 7.194619655609131, "[TT] Impact on NGSO Terminals of the 5G Network = Fewer than 1%"]
-[14.635087966918945, 6.752781867980957, "[TT] Battery Capacity of the EPS = < 7600 mAhr"]
-[5.456055641174316, 7.112524032592773, "[TT] Data Rate from OBC to FPGA of the Transmission Module = 10 Mbit/s"]
-[10.467632293701172, 6.843807697296143, "[TT] Mirror Path Length of the IMG = 10 cm"]
-[8.383056640625, 4.106772422790527, "[FF] Design Date of the Uniform Spectral Radiance source = May 2008"]
-[8.78232192993164, 7.721979141235352, "[TT] MS B2 of the Pushbroom imager = 0.53-060 \u00b5m"]
-[9.007594108581543, 4.396815299987793, "[FF] Robotic Arms Function of the Satellite = Orientation of the satellite's electric propulsion thrusters and to control thrust direction and attitude"]
-[8.649544715881348, 2.901136875152588, "[FF] Mission Type of the CADRE = Space weather"]
-[9.196710586547852, 1.8208534717559814, "[TT] Lunar Disk Area on HARP-2 Detector of the PACE spacecraft = 10 x 10 pixel area"]
-[9.68819808959961, 4.839021682739258, "[TT] Type of the Stabilization = 3-axis stabilized"]
-[10.090392112731934, 5.371059894561768, "[FF] Heat Up Monitoring of the S/C = Yes"]
-[4.881124973297119, 1.7873055934906006, "[FF] On-Orbit Experiment Date of the HORYU-II = Oct. 1-5, 2012"]
-[10.424100875854492, 2.912670135498047, "[FF] S-band communications link of the Nanosatellites = For increased data transmission"]
-[5.481276512145996, 5.095538139343262, "[TT] Communication Protocol of the PIC microcontroller = CAN bus"]
-[11.992330551147461, 4.641997814178467, "[TT] Dimensions of the G\u00f6kt\u00fcrk-1A = 4.2 m x 2.5 m x 1.6 m"]
-[4.7974700927734375, -1.8115471601486206, "[FF] Technical Characteristics of the Chang'e 4 = Unknown"]
-[5.971710205078125, 3.929262161254883, "[FF] Integration of Physical Components of the Cooperation by Federation = Not Required"]
-[7.956502437591553, -0.11970365792512894, "[TT] Average Time Spent on Land of the Polar Bears = 30 more days than in the 1990s"]
-[9.39488697052002, 0.578938901424408, "[TT] Length of the Current Sheet = More than 40,000 kilometers"]
-[10.631654739379883, 8.873150825500488, "[TT] Pixel size of the Channel 6 = 32 km x 32 km"]
-[9.678544998168945, -0.3371521830558777, "[TT] Altitude of the JL-1-GF03B = 535 km"]
-[1.3160932064056396, 1.8993537425994873, "[TT] ULC Cargo of the HTV-7 = 1.9 metric tons"]
-[14.724961280822754, 6.466465473175049, "[TT] Mass of the Li-ion batteries = 51 kg"]
-[7.247623443603516, 5.059055805206299, "[FF] Electronics of the MPPT = COTS (Commercial-of-the-Shelf) components"]
-[4.948914051055908, 2.999418020248413, "[TT] Location of the SOC = VITO (Flemish Institute for Technological Development)"]
-[3.6086814403533936, 2.6976070404052734, "[TT] Number of Satellites of the Iridium NEXT = 70"]
-[8.340060234069824, 2.081393241882324, "[FF] Data Usage of the CFOSAT = Improve the inversion algorithms for estimating wind speed and significant wave height, characterize the small scale roughness of all types of surfaces"]
-[5.4886040687561035, -0.5297996401786804, "[TT] Mission Success of the MightySat II.1 = 100%"]
-[10.846681594848633, 2.1152727603912354, "[FF] Detector Type of the XMM-Newton = Absorption"]
-[7.189964294433594, 2.767251491546631, "[FF] Purpose of the CHRIS = Terrestrial and aquatic observation"]
-[9.804686546325684, 8.629176139831543, "[TT] FOV of the Short Wavelength Band = 4\u00ba x 5'"]
-[6.8320183753967285, -0.6514155268669128, "[TT] Orbital Period of the CBERS-3 = 100.26 minutes"]
-[5.137945175170898, 1.6909557580947876, "[TT] Testing Status of the Pathfinder 1 = In the process of final testing and checkout"]
-[7.614784240722656, -2.524704694747925, "[TT] Observation Date of the GOLD = December 10, 2019"]
-[4.942526340484619, 1.3595869541168213, "[TT] Development Start Year of the MiRaTA = 2012"]
-[3.3889756202697754, 5.1427001953125, "[TT] Frequency of Operation of the SAR instrument = C-band"]
-[5.113564491271973, 2.4610559940338135, "[TT] Mission Type of the EDRS = Non-EO"]
-[6.981451034545898, -0.4092911183834076, "[TT] Number of Orbits/Day of the Orbit = 15 3/14"]
-[5.054776668548584, 3.060835838317871, "[TT] Manufacturer of the CINEMA-2 (KHUSat-1) = KHU (Kyung Hee University), Seoul, Korea"]
-[8.422224998474121, 3.94488263130188, "[FF] Flux Limitation of the Sensor = Limits the oxygen flux to the cathode"]
-[4.5212507247924805, -0.21949633955955505, "[FF] Docking Target of the MEV = Main engine of Intelsat-901 and other future client satellites"]
-[9.73505973815918, 3.9955804347991943, "[TT] Magnetic Field Strength of the AMS-02 = 4000 times stronger than the magnetic field of Earth"]
-[5.1613287925720215, 3.75366473197937, "[TT] Space Segment of the Sentinel-6 = Two successive Jason-CS satellites (A and B)"]
-[13.632641792297363, 5.71327543258667, "[TT] End of Life Power Generation of the Solar Panels = 1790 W"]
-[13.678319931030273, 2.8013205528259277, "[TT] Launch Mass of the WINDS satellite = 4850 kg"]
-[10.443266868591309, 1.6951751708984375, "[TT] Difficulty of Pulsation Interpretation of the Delta Scuti stars = Complicated and difficult"]
-[6.6326003074646, 4.25473690032959, "[FF] Payloads of the Aditya-L1 = Particle payloads, magnetometer payload"]
-[12.721391677856445, 3.8952457904815674, "[FF] Basis of the Kappa Scheme = Theory of \"double-arc instability,\" a magnetohydrodynamic (MHD) instability triggered by magnetic reconnection"]
-[10.06640625, -1.4930062294006348, "[TT] Orbit Inclination of the ResourceSat-1 = 98.7\u00b0"]
-[6.358224868774414, -0.754413366317749, "[TT] Required Tracking Interval of the TIRA = 12 hours"]
-[5.321648120880127, 0.681755781173706, "[FF] Release Date of the Arctide2017 = 15 September 2018"]
-[7.291937351226807, 8.24198055267334, "[FF] SNR of the GOSAT-2 = b2: >200 (79/0.144)"]
-[13.765437126159668, 5.939681529998779, "[TT] Nominal Operating Voltage of the GHGSat-D = 12.3 V"]
-[10.906792640686035, 7.542504787445068, "[TT] Swath Width of the SAM-II = 5 - 40 km vertical"]
-[7.0784382820129395, 8.05137825012207, "[TT] Channel Imbalance of the Instrument = \u2264-34 dB"]
-[7.781223773956299, 6.745765209197998, "[TT] Detection Threshold of the TROPOMI = 12 ppb"]
-[5.355556964874268, 3.948744535446167, "[TT] Number of Satellites of the SARah = 3"]
-[4.708353519439697, 8.113417625427246, "[TT] Chirp Parameters of the DCG = 2-75 MHz"]
-[7.680281162261963, 0.7968436479568481, "[FF] Mission Objectives of the LADEE = Determine the composition of the lunar atmosphere and investigate the processes that control its distribution and variability, including sources, sinks, and surface interactions. Characterize the lunar exospheric dust environment and measure any spatial and temporal variability and impacts on the lunar atmosphere. Demonstrate that Lunar Laser Com Demonstration (LLCD) can operate at high data rates from lunar distances. Create a low-cost reusable spacecraft architecture that can meet the needs of certain planetary science missions. Demonstrate the capability of the Minotaur V as a launch vehicle for planetary missions."]
-[7.496928691864014, 6.4072065353393555, "[TT] GNOS and Radiosonde Refractivity Profile Difference of the GNOS Instrument = <3%"]
-[12.17667293548584, 3.6348893642425537, "[TT] Gas of the CAE System = Xenon"]
-[7.478521347045898, 4.682830333709717, "[FF] Acceptance Matching of the STD = ECAL"]
-[8.225515365600586, 5.579761028289795, "[TT] Location of the Spectral Calibration = Ground"]
-[5.899412155151367, 6.09102201461792, "[TT] Ports of the MPA = 8"]
-[8.083902359008789, 8.80201530456543, "[TT] Spectral Region of the MEIDEX = 340-860 nm"]
-[9.063082695007324, 3.2296993732452393, "[FF] Imaging Capability of the Hubble Space Telescope = Shows only blurry patches of light and dark materials on Pluto\u2019s surface"]
-[13.340571403503418, 7.240503311157227, "[TT] Power of the ASC (Advanced Stellar Compass) = 37 W EOL"]
-[8.171615600585938, 6.6229095458984375, "[TT] Manufacturer of the Advanced Baseline Imager (ABI) = L3Harris"]
-[4.774832725524902, 1.6869689226150513, "[FF] Possibility to Cooperate of the TanSat = Participants in the A-Train"]
-[11.065174102783203, 0.9065872430801392, "[TT] Arm Length of the LISA = About a million miles"]
-[5.234805583953857, 0.963555634021759, "[TT] Commissioning Phase End Date of the SMOS = April"]
-[5.400703430175781, 4.256191730499268, "[TT] Planned Number of Satellites of the Corvus-BC 3 = 10"]
-[3.5513648986816406, 5.2986321449279785, "[TT] Dimensions of the MMW Radar = 400 mm x 350 mm x 350 mm"]
-[4.798006057739258, 0.5964773297309875, "[FF] Development End Date of the MOMS-02 = Dec. 20, 1993"]
-[8.929874420166016, 3.2384514808654785, "[FF] Fast Plasma Experiment of the SEE-1 and ISEE-2 = Unknown"]
-[5.308398246765137, 1.0652005672454834, "[TT] Imaging Date of the OPS-SAT = 14 August 2020"]
-[6.386700630187988, 3.6524558067321777, "[TT] Planned Name of the GOES-T = GOES-18"]
-[9.953878402709961, 0.6535006761550903, "[TT] Travel Direction of the Cluster 3 = From low to high latitude"]
-[5.480777740478516, 5.060299396514893, "[TT] Interface of the EPH = CAN bus"]
-[5.292852878570557, 6.477010726928711, "[TT] Tx-TNC Cache Memory of the RF Communication System = 128 byte"]
-[6.126299858093262, -0.43782904744148254, "[TT] Mission Duration of the TIMED = Ongoing"]
-[9.379742622375488, 7.044975757598877, "[TT] Resolution of the CRS = 50 m"]
-[8.751328468322754, 5.099747180938721, "[TT] Performance of the ST (Star Tracker) = 10 arcsec"]
-[7.723001003265381, 9.006098747253418, "[TT] Amplified Output Quality of the LOM = Near diffraction-limited beam quality (M2 < 1.4)"]
-[6.511711120605469, -0.261155366897583, "[TT] Duration of the SJ-10 Satellite = About two weeks"]
-[7.076657295227051, 5.892299652099609, "[TT] Stability of the Cesium Atomic Clock 5585B = High"]
-[8.691930770874023, 1.826395869255066, "[TT] Rapid Intensification Definition of the Hurricane Dorian = An increase in 30 kts (35 mph) in sustained winds over 24 hours"]
-[13.852534294128418, 3.0570828914642334, "[TT] Mass of the Astrium Sentinel 2 MMFU = 14 Kg"]
-[9.908384323120117, -0.39243435859680176, "[TT] Altitude of the Satellite = 686 km"]
-[8.476737022399902, 7.634618759155273, "[TT] Resolution of the CCD Array = 1024 x 1024"]
-[4.922209739685059, 8.29470157623291, "[TT] Frequency of the MWR = 36.5 GHz"]
-[5.441961288452148, -0.01855325698852539, "[TT] Launch Date of the IRS-1B = August 29, 1991"]
-[5.130426406860352, 1.3726563453674316, "[FF] User Workshop Date of the GOCE = Nov. 6-8, 2006"]
-[6.022497653961182, 1.6394087076187134, "[TT] Data Products Archive of the IXPE Observatory = NASA's HEASARC"]
-[9.054900169372559, 0.5211847424507141, "[TT] Earth Departure Maneuvers of the ARTEMIS = Over forty maneuvering events"]
-[4.948462009429932, 2.0987088680267334, "[TT] Status of the MTVZA-GY = Fully functional"]
-[5.76033353805542, 7.162728786468506, "[TT] Data Rate of the Unit = 1000 bit/s"]
-[7.557729721069336, 8.876688003540039, "[TT] Radiometric Accuracy of the Spectral Band B = 3"]
-[9.040569305419922, 3.195286989212036, "[FF] Activity Level of the Solar Activity = Exceptionally low and practically constant"]
-[4.6646223068237305, 0.18322253227233887, "[TT] End of Life Date of the ALOS-3 = 7 March 2023"]
-[13.42219352722168, 5.899484157562256, "[FF] Low Voltage Occurrence of the SpriteSat = After the deployment of the gravity mast"]
-[3.2127554416656494, 3.8610105514526367, "[TT] LEOP Completion Date of the TerraSAR-X = June 21, 2007"]
-[9.87026596069336, 4.596282958984375, "[TT] Spin Rate of the AlSat Nano = Low"]
-[4.46552038192749, 3.1835286617279053, "[TT] Location of the Ground Station = Tarusa (Russia)"]
-[4.495269298553467, 1.5381070375442505, "[TT] Launch Date of the SciSat-1/ACE = 12 August 2003"]
-[6.915472030639648, 7.770230293273926, "[TT] Reflector Size of the Harris Corporation = 12-meter"]
-[4.537287712097168, 7.786616325378418, "[TT] Downlink Frequency of the Astrodev Lithium 2 Radio = 401.3 MHz"]
-[5.428435802459717, 5.137632846832275, "[TT] Communications and Navigation of the LPT/CANDOS = 100%"]
-[5.01719331741333, 1.199798345565796, "[FF] Workshop Date of the UniSat-3 = Oct. 9-11, 2006"]
-[13.483333587646484, 7.161039352416992, "[TT] Power Supply of the GNB = 8 W peak and 5.6 W nominal"]
-[5.038114070892334, 2.9213595390319824, "[TT] Funding Source of the MOMS = German Ministry for Research and Technology"]
-[5.483725547790527, 6.109735488891602, "[TT] Memory Use Capability of the SPOT-4 = Lost"]
-[3.8585848808288574, 3.4164912700653076, "[TT] Integration Dates of the Galileo Satellites = July 11, 2018"]
-[5.036640644073486, 3.084139347076416, "[FF] Financing of the LLMS/IRIS = Mainly financed by the Federal Office for Scientific, Technical and Cultural Affairs (OSTC) of Belgium, with a contribution from its German counterpart (DLR)"]
-[13.389848709106445, 2.866969108581543, "[TT] Instrument Mass of the DubaiSat-1 = 38.67 kg"]
-[3.324589490890503, 5.731930255889893, "[TT] Panel Quantity of the SAR Antenna = 5"]
-[11.602091789245605, 6.522047996520996, "[TT] Energy Range of the NuSTAR = Greater than 10 keV"]
-[1.609208583831787, 3.7597601413726807, "[TT] 3-axis stabilization of the BEESAT-1 = Yes"]
-[6.88075065612793, 0.7343600988388062, "[TT] Landing Date of the InSight = 26 November"]
-[13.42384147644043, 6.805425643920898, "[TT] Total Power of the Spacecraft = 5.4-11 W (6 W average)"]
-[5.076815605163574, 1.0262444019317627, "[FF] Launch Date of the PW-Sat = Unknown"]
-[4.8600077629089355, 2.225529432296753, "[TT] Platform of the G\u00f6kt\u00fcrk-1A = Proteus"]
-[7.685818672180176, 2.920745611190796, "[FF] Use of the Images = Estimating the types of light sources, comparing the lighting and the economic health of a city, evaluating lighting for road and public safety, correlating light pollution with effects on human health and biodiversity"]
-[8.735123634338379, 7.5657196044921875, "[TT] CCD Sensor Pixels of the COTS Cameras = 640 x 480"]
-[6.768373012542725, 3.236964225769043, "[TT] Deep-Space Observations of the SBSS-1 = 3.8 million in first year"]
-[10.887109756469727, 6.073190212249756, "[TT] Design of the Optical Benches = Truss-type"]
-[4.228641986846924, 7.3160858154296875, "[TT] Function of the Antenna System = Receive GRB and legacy GVAR downlinks"]
-[5.674816608428955, 11.345198631286621, "[FF] Approx. Peak Sensitivity Altitude of the Channel 1 = Unknown"]
-[6.449981212615967, 7.57078218460083, "[TT] Signal Quantization of the DACS = 8 bit I/Q"]
-[14.083603858947754, 4.031580924987793, "[TT] Total Mass of the Instrument = 13.25 kg"]
-[7.911858558654785, 3.1308584213256836, "[FF] Carbon Monoxide Column-Averaged Dry-Air Mole Fraction (XCO) of the FTS-2 = Parameter Value Unknown"]
-[9.051424980163574, 4.568079948425293, "[TT] Operation Attitude of the Satellite = Maximum power generation attitude with the \u2013Z satellite face sun pointing"]
-[4.987245559692383, 0.8350067138671875, "[TT] Observations for Performance Verification Dates of the Hitomi = March 25 & 26, 2016"]
-[6.825760364532471, -0.4012046754360199, "[TT] Local Time of Imaging of the Satellites = Varies"]
-[8.831092834472656, -1.1996562480926514, "[TT] Time to Reach Geostationary Orbit of the SES-14 = Four months"]
-[11.181174278259277, 4.984298229217529, "[TT] Size of the CCRs = One inch"]
-[7.768893718719482, 4.718189716339111, "[FF] Environment Requirement of the CITRIS = Electromagnetically pristine"]
-[9.711446762084961, 7.151463985443115, "[TT] Ground Resolution of the NIUSAT = 25 m"]
-[9.635852813720703, -0.45417773723602295, "[TT] Mean Altitude of the FormoSat-2 = 888 km"]
-[7.424670696258545, 2.9537320137023926, "[TT] Data Sharing Resolution of the MethaneSAT = 1 km"]
-[8.205564498901367, -1.0989348888397217, "[TT] Bathymetry Visibility of the ICESat-2 = Up to 25 meters"]
-[10.532472610473633, 5.755385875701904, "[TT] Number of Summers and Winters of the KELT-9 b = 2 each"]
-[3.1875, 5.001387596130371, "[TT] FRS-1 Resolution of the RISAT-SAR = 3 m x 2 m (Az x Range)"]
-[4.8738532066345215, 0.9370633363723755, "[FF] Flight Operation Date of the Cute-1.7+APD = June 25-29, 2007"]
-[5.018017768859863, 0.8606310486793518, "[TT] Launch Date of the AFSPC-11 = 14 April 2018"]
-[7.874144077301025, 6.414380073547363, "[FF] Data Collection Time of the Advanced Baseline Imager (ABI) = About 45 minutes before the tornado touched down"]
-[5.218690872192383, -0.8384881615638733, "[FF] Mission Type of the Kolibri-2000 = EO"]
-[5.609365463256836, 4.983696460723877, "[TT] Data Relay Service of the EDRS = Sentinel-1 and -2"]
-[5.445825576782227, 4.180516242980957, "[TT] Common Ground System of the JPSS and DWSS = Yes"]
-[8.039777755737305, 2.4702634811401367, "[FF] Measurement Domain of the AGRI = Ocean, Land"]
-[7.219820022583008, 3.675640344619751, "[FF] Predecessor of the WSF-M = Suomi National Polar-orbiting Partnership (Suomi NPP), Joint Polar Satellite System (JPSS)-1, and the Global Precipitation Measurement (GPM) Microwave Imager (GMI) sensor"]
-[7.194904327392578, 5.455140590667725, "[FF] Demonstration Requirement of the DSAC = In-orbit demonstration of the precision timing and navigation capabilities"]
-[8.190157890319824, 4.468962669372559, "[FF] Environmental Monitoring of the LARES = Unknown"]
-[3.788269519805908, -1.0662237405776978, "[TT] Orbit Type of the DSX spacecraft = Elliptical MEO"]
-[5.562731742858887, 7.223882675170898, "[TT] Maximum Bit Rate of the VBR = 50 Mbit/s"]
-[5.047142505645752, 1.1302518844604492, "[TT] Launch Date of the INSAT-3D = July 25, 2013"]
-[9.716414451599121, 1.4120168685913086, "[TT] Resolution of the Pl\u00e9iades Neo = 30cm"]
-[9.817337989807129, 8.593012809753418, "[TT] IFOV of the IMG = 10 mrad"]
-[4.174880504608154, 3.7962324619293213, "[FF] Unknown of the Galileo Reference Receiver = Unknown"]
-[8.581291198730469, 1.5185743570327759, "[TT] Quantization levels of the Integrated water vapor = 0.10"]
-[8.082152366638184, 8.75830364227295, "[FF] Model of the UVIT = Engineering model"]
-[6.490767002105713, 3.043552875518799, "[FF] Program Components of the NPOESS = NOAA POES, DoD DMSP, NASA\u2019s long-term continuous climate record collection"]
-[5.70388126373291, 4.746882915496826, "[FF] Telemetry of the YES = Not Switched On"]
-[14.277771949768066, 3.2840514183044434, "[TT] Mass of the CVX = < 1 mg"]
-[9.017640113830566, 4.901819705963135, "[FF] Acquisition Failure Reason of the Satellite Terminal = Ephemeris and spacecraft attitude control was out of specification"]
-[5.286713600158691, 4.022075653076172, "[TT] Number of Satellites of the Lightspeed Satellites = Nearly 300"]
-[9.899734497070312, 7.673110008239746, "[FF] Telescope Image Cadence of the EUVI = Higher image cadence"]
-[7.543118953704834, 4.412109851837158, "[FF] Objective of the QWIP = Demonstrate and assess QWIP FPA uniformity, stability, and repeatability and responsivity in a space radiation environment"]
-[7.361670017242432, 6.8650288581848145, "[TT] Measurement Method of the ATLAS = Sending pulses of light to Earth\u2019s surface and measuring the time for individual photons to return to the sensor"]
-[7.975337505340576, 1.9633197784423828, "[FF] Surface Type of the TOI 700 d = Ocean-covered, all-land"]
-[4.89677619934082, 1.222579836845398, "[FF] Presentation Date of the Delfi-n3Xt = June 3-5, 2013"]
-[7.444525718688965, 3.518829822540283, "[FF] PZ-Surface Function of the H3 and H4 = Location of major mission instruments"]
-[6.312943458557129, 4.685338020324707, "[FF] Reprocessed Data of the EDOT = Entire mission orbit telemetry"]
-[14.169589042663574, 3.0957820415496826, "[FF] Quantity of the KGS-4S = 1"]
-[10.98972225189209, 6.10212516784668, "[TT] Material of the Optical Components = BK7G18"]
-[5.0310444831848145, 0.7689749598503113, "[FF] Change 1 Approval Date of the STD-8719.14A = 2012-05-25"]
-[8.352720260620117, 4.167952537536621, "[TT] Calibration Method of the CAPI = LED +lunar + solar calibration"]
-[6.17903995513916, 5.450667858123779, "[FF] Redundancy of the TCU = Internally redundant"]
-[3.5687501430511475, -0.8612545132637024, "[TT] View of the TIROS = Only an oblique swath of the Earth's surface occasionally in each orbit"]
-[7.282113552093506, 6.503149509429932, "[TT] Overpass Duration of the ARC = Less than 1 second"]
-[10.870899200439453, 7.574123382568359, "[TT] Swath Width of the SLIM6 = 600 km"]
-[5.779898166656494, 8.045267105102539, "[FF] Equivalence Principle Frequency Value of the MicroSCOPE = Unspecified"]
-[7.902259349822998, 3.4699769020080566, "[FF] Data Collection of the Neil Gehrels Swift Observatory = Sensitive to different wavelengths of light"]
-[10.449828147888184, 1.8239246606826782, "[FF] Speed of the Spinning Black Hole = Approaches the speed of light"]
-[11.520742416381836, 4.653894424438477, "[FF] Shape of the Procellarum = Rectangular"]
-[11.056828498840332, 1.4895578622817993, "[TT] Outer Diameter of the Starshine-1 = 47.5 cm"]
-[8.84344482421875, -0.08852249383926392, "[TT] Distance from Earth of the Chang'e-2 = Over 100 million km"]
-[11.129988670349121, 4.800934791564941, "[FF] Power Requirement of the Electrodynamic Tether (Thrust System) = Requires power to be injected into the tether system from an on-board power supply"]
-[5.28116512298584, 7.73785924911499, "[TT] Isolation of the Waveguide Radiating Element = Better than -25 dB"]
-[5.871734619140625, 7.158555507659912, "[TT] Rate of the Material Release Rate = One ton per second"]
-[7.384559631347656, 6.68286657333374, "[TT] Integration Time of the Pixel integration time = 1.0 s"]
-[5.12105131149292, 6.2850775718688965, "[TT] Operator of the MSG-3 = Hughes Network Systems"]
-[11.611038208007812, 6.642868518829346, "[TT] Detection Energy of the CZTI = Greater than about 60 keV"]
-[4.752674579620361, 0.4460887312889099, "[TT] Launch Date of the PAMELA = June 15, 2006"]
-[4.956563949584961, 0.7798521518707275, "[TT] Maiden Flight Date of the Automated Transfer Vehicle = March 9, 2008"]
-[8.702427864074707, 1.9885679483413696, "[TT] Wind Speed Range of the Scatterometer = 3-16 m/s"]
-[6.704992771148682, 6.82652473449707, "[TT] Performance of the LAS (Launch Abort System) = Successful"]
-[5.560333728790283, 0.5149306654930115, "[FF] Evaluation Date of the SSM/I = Sept. 1990"]
-[5.404877662658691, 3.1474053859710693, "[TT] Mission Integration Provider of the GHOSt = Maverick Space Systems"]
-[10.243353843688965, 5.751523494720459, "[TT] High-Temperature Calibration Source Temperature of the AMSR = About 340 K"]
-[7.065219402313232, 7.765195369720459, "[FF] Location of the Reflector Cubes = Precise latitude, longitude, and elevation"]
-[5.995911121368408, -0.4536108672618866, "[TT] Mission Duration of the UKube-1 = Over 14 months"]
-[5.17483377456665, -1.1043736934661865, "[TT] Launch Time of the Kondor-E1 = 16:53 UTC"]
-[7.629117012023926, -0.5028113126754761, "[FF] URL of the IceCube = https://icecube.wisc.edu"]
-[4.251655578613281, 6.6586222648620605, "[TT] Frequency Bands of the ROSA = L1 and L2"]
-[4.872856616973877, 0.4812457859516144, "[TT] Launch Date of the VELOX-PII = 21 November 2013"]
-[9.562458992004395, 7.312501907348633, "[TT] Angular Resolution of the RHESSI = Few arcseconds"]
-[6.7967209815979, 4.447004795074463, "[FF] Design Challenges of the INTEGRAL = Mechanical and electrical interfaces, environmental requirements, spacecraft envelope"]
-[4.499443531036377, 6.968559741973877, "[TT] Signal Type of the Ground Stations = 16 QAM"]
-[8.251028060913086, 0.2973910868167877, "[FF] Overall Objective of the T/P = Provide high-accuracy global sea level (ocean height) measurements"]
-[10.095044136047363, 7.645105361938477, "[TT] Radius of Curvature of the Image Surface = -165 mm"]
-[9.469727516174316, 0.47406288981437683, "[TT] Perihelion Radius of the Solar Orbiter = < 0.25 AU and > 0.20 AU"]
-[6.847800254821777, 4.778843402862549, "[FF] Architecture of the ICE = Modular design with integrated RF and digital design technologies"]
-[6.155885696411133, 6.613672256469727, "[TT] Service Types of the EDRS = Optical and Ka-band"]
-[9.615779876708984, 7.212093830108643, "[FF] Ground Spatial Resolution of the POLDER = 7 km x 6 km at nadir"]
-[6.394149303436279, 2.087817668914795, "[FF] URL of the FedSat = https://web.archive.org/web/20110603203559/http://www.ips.gov.au/IPSHosted/NCRS/wars/wars2000/invited/fraser.pdf"]
-[9.319070816040039, 5.062312602996826, "[TT] Attitude Accuracy of the TAIKI = \u00b12\u00ba"]
-[6.336637496948242, 8.085005760192871, "[TT] Number of Channels of the AGRI = 14"]
-[5.540544033050537, 6.238733291625977, "[TT] Type of the Mass memory = Mass memory"]
-[5.534595966339111, 3.844233274459839, "[TT] Goal of the Satellogic = Fly about 300 satellites"]
-[8.369195938110352, 7.452645778656006, "[TT] Receiver Unit of the FIBOS = Pigtailed PIN InGaAs photodiode (model EPM605 from JDSU)"]
-[13.983821868896484, 7.101475715637207, "[TT] Regulated Output of the EPS = +5 Vdc"]
-[8.166438102722168, -0.6084612607955933, "[TT] Measurement Coverage of the SMOS = Arctic"]
-[10.18135929107666, 2.2370009422302246, "[FF] Capability of the NuSTAR = Taking detailed pictures of radioactive material"]
-[14.217631340026855, 3.1961629390716553, "[TT] Mass of the LAP = 6.3 kg"]
-[3.533784866333008, 5.15775203704834, "[TT] Orientation of the RADARSAT-2 = Both left- and right-looking"]
-[11.835884094238281, 0.04182332754135132, "[FF] Purpose of the TESS = Monitor transits, periodic dips in a star\u2019s brightness"]
-[9.010847091674805, 5.105162143707275, "[TT] Power Consumption of the MEMS-based rate gyroscope assembly = < 80 mA at \u00b15 V for each gyro"]
-[9.620587348937988, -0.24569326639175415, "[TT] Altitude Above Ground of the Lunar Landing Vehicle = 4 m"]
-[5.431817054748535, 7.136849880218506, "[TT] User Data Rate of the 2nd generation Tesat LCT = 600 Mbit/s"]
-[5.17358922958374, 4.5414228439331055, "[TT] Number of Satellites of the GPS Receiver = 4 or more"]
-[4.400550842285156, 1.8341295719146729, "[TT] Decommission Date of the RADARSAT-1 = 29 March 2013"]
-[8.623106002807617, 6.940850257873535, "[FF] Quantity of the Scientific Instrument = 26 cameras and electronic units"]
-[14.579267501831055, 6.6166672706604, "[TT] Battery Type of the ALP = Li-ion"]
-[5.445436477661133, -0.5747135877609253, "[TT] Expected Wake Up Date of the Yutu-2 = 28 April"]
-[6.199990749359131, -0.5028541088104248, "[TT] Years on Orbit of the RADARSAT-2 = 10 years"]
-[6.563928127288818, 5.061958312988281, "[FF] Functionality of the DHU = Control & Monitoring, Generation of camera syncs, Interface to VNIR/SWIR, Sorting of incoming data, Storage of data, Compression, Generation of source packets, Interface for control & monitoring from S/C, RTC, Acquisition of HK data"]
-[7.5872602462768555, 4.8566436767578125, "[TT] Installation Location of the Metric Camera = Inside the pressurized cabin of the Spacelab module"]
-[6.903481960296631, 8.978288650512695, "[TT] Bandwidth of the POLDER-1/2 = 20 nm"]
-[9.87499713897705, -1.362527847290039, "[TT] Eutectic Point of the Galinstan = T= -19.5\u00b0C"]
-[10.887158393859863, 3.920109748840332, "[FF] Function of the Drag Sail = Deorbit the satellite"]
-[8.992852210998535, 5.662456512451172, "[TT] Pointing Performance of the S/C = Better than 0.05\u00ba (3 \u03c3)"]
-[7.159137725830078, 4.595442295074463, "[FF] Purpose of the GRD = Simulate GRB detection"]
-[6.409506797790527, -0.7593733072280884, "[TT] LTAN of the NEMO-HD = 10:30 hours"]
-[8.130900382995605, 3.3881468772888184, "[FF] Function of the OCO-3 = Monitors carbon dioxide and its changes throughout space and time"]
-[8.549742698669434, 3.5893397331237793, "[TT] Absorption Cell of the Extinctive Stellar Occultations = Intervening Atmosphere"]
-[11.435615539550781, 6.396202087402344, "[TT] Data Wavelength of the NuSTAR = 10 to 35 keV"]
-[6.660533428192139, 2.1783556938171387, "[FF] Availability of the Visualization = Worldwide to planetariums and other centers of informal learning"]
-[9.457768440246582, 0.8609540462493896, "[FF] Closest Approach to the Sun of the ISON = Unknown"]
-[14.308794021606445, 3.1299946308135986, "[TT] Mass of the ITASAT-1 = ~8kg"]
-[7.839898586273193, 2.0604748725891113, "[TT] Instrument Type of the OCTS = Ocean colour instruments"]
-[11.529044151306152, 3.4041035175323486, "[TT] Specific Impulse of the CNAPS = 40 s"]
-[4.798115253448486, -1.8716728687286377, "[TT] Previous Lunar Landings of the Chang'e-5 = Chang\u2019e-3 and Chang\u2019e-4 missions"]
-[7.230863571166992, 8.106151580810547, "[TT] ISLR of the Instrument = \u2264-9 dB"]
-[9.630141258239746, 7.0009989738464355, "[TT] Spatial Resolution of the L2SMP = About 40 km"]
-[7.839865684509277, 2.205106019973755, "[FF] Data Types of the Cheollian 2B = Marine image data, Ocean color images"]
-[4.712224960327148, 1.5487598180770874, "[TT] Update Frequency of the GCOM-C/SGLI = Two times during the five-year mission period"]
-[11.737650871276855, 7.510445594787598, "[FF] Observation Frequency of the Megha-Tropiques = Up to 5 (3) observations per day"]
-[14.080129623413086, 4.049919128417969, "[TT] Mass of the Instrument = 6.0 kg"]
-[7.454092025756836, 1.0013465881347656, "[TT] Purpose of the LRO = Observing the moon"]
-[11.362383842468262, 3.517289161682129, "[FF] Propulsion of the ACS = Hot gas jets"]
-[5.83977746963501, -2.249816656112671, "[TT] Altitude of the KOMPSAT-6 = 505 km"]
-[5.434754848480225, 6.305859565734863, "[TT] Capacity of the DDR2 SDRAM = 1 GByte"]
-[4.455676555633545, 3.098731756210327, "[TT] Location of the DPS = Balanagar"]
-[5.683859348297119, 0.49839508533477783, "[FF] Testing Date of the GEOS-1 = Unknown"]
-[10.65253734588623, 7.341518878936768, "[TT] Swath Width of the MIS Instrument = ~1,700 km"]
-[11.55312728881836, 4.812385082244873, "[TT] Height of the Sample Return Capsule (SRC) = 1.31 m"]
-[7.062366962432861, 8.184518814086914, "[TT] SNR of the Instrument = > 100"]
-[6.273863792419434, 8.656350135803223, "[TT] Polarization of the AMSU-A = Mixed V & H (V only for 22.2)"]
-[5.4115095138549805, 0.019429534673690796, "[TT] Launch Date of the IRS-P6 = 17 Oct 2003"]
-[9.100661277770996, -0.5750764608383179, "[TT] Orbit Apogee of the P35 series = 752 km"]
-[7.91369104385376, 7.177391052246094, "[TT] Interferometers of the LTP = 4"]
-[9.869999885559082, -1.5374014377593994, "[TT] Inclination of the SMART-1 = 90.188\u00ba"]
-[4.19343376159668, 6.355154514312744, "[FF] Placement of the S-band antennas = On the top and bottom of the spacecraft"]
-[12.13806438446045, 3.035313606262207, "[TT] Hydrazine Mass Flow Rate of the Microthrusters = 0.1 mg/s"]
-[9.758899688720703, 8.036263465881348, "[TT] Focal length of the 1000 mm camera = 1000 mm"]
-[6.390772342681885, 1.1692242622375488, "[TT] Start Date of the Weather Program = 1962"]
-[4.548540115356445, 7.723676681518555, "[TT] Frequency Selectivity of the LICEF = High"]
-[14.008665084838867, 3.009878396987915, "[TT] Mass of the D-SAT = 3.5 kg"]
-[8.634023666381836, 0.14055617153644562, "[TT] Total Volume of the Comet = 21.4 km3"]
-[8.857588768005371, 9.528647422790527, "[FF] Band 3 Spectral Range of the TANSO-FTS-2 = 1.923 - 2.381 \u00b5m"]
-[9.312529563903809, 5.21469783782959, "[TT] Surface Solar Zenith Angle of the TanSat = < 80\u00ba"]
-[5.485069274902344, 8.720830917358398, "[TT] Bandwidth (\u00b5m) of the Spectral Bands = 0.020, 0.020, 0.020, 0.018, 0.020, 0.020, 0.040, 0.040"]
-[13.543060302734375, 2.84684157371521, "[TT] Mass of the DMSP Block 5B and Block 5C satellites = 193 kg"]
-[5.547876834869385, 2.7063987255096436, "[FF] Development of the TRISHNA = Joint by the French Space Agency (CNES) and the Indian Space Research Organization (ISRO)"]
-[7.198947429656982, 0.9043831825256348, "[TT] Launch Date of the SeaSat = June 27 (UTC), 1978"]
-[3.3576548099517822, 1.4766614437103271, "[TT] Launch Date of the Sentinel-2B = March 7, 2017"]
-[7.196532249450684, 1.090780258178711, "[TT] Mars Atmosphere Entry of the Schiaparelli = 19 October, 14:42 GMT"]
-[6.286238670349121, 8.042502403259277, "[TT] Channels of the BlackJack = 16"]
-[9.700149536132812, 5.704268932342529, "[TT] Tilt of the M1 = 5 \u00b5rad"]
-[8.34104061126709, 6.802087306976318, "[TT] Data Collection Mode of the VIRR = Pushbroom"]
-[14.010418891906738, 3.506564140319824, "[TT] Mass of the High-Voltage Array = 186 g"]
-[5.655977725982666, 7.142727375030518, "[TT] Data Rate of the VIS = 7.2 Mbit/s"]
-[6.369828224182129, 3.4021403789520264, "[TT] Control Center of the AMS-02 = POCC (Payload Operation Control Center) from NASA/JSC, Houston"]
-[5.917577266693115, 1.149067997932434, "[FF] Innovation Spin-off of the BepiColombo = Terrestrial industry products"]
-[5.356960296630859, 3.9426419734954834, "[TT] Quantity of the Dove satellites = 88"]
-[7.198911666870117, 1.8912142515182495, "[TT] Satellite Design Lifetime of the Carbonite-1 = 5 years"]
-[3.8997321128845215, 4.649737358093262, "[TT] Noise Levels of the RADARSAT-2 = Within approximately 1 dB of the calibrated noise level of each pulse"]
-[5.282353401184082, 7.860233306884766, "[TT] Chopping Frequency of the Mechanical choppers = 10 Hz"]
-[10.112398147583008, 3.0494229793548584, "[FF] Door Opening of the PEPPOD#1 = Initiating the deployment of the CubeSats: ICube-1, HumSat-D and PUCPSat-1"]
-[8.07443904876709, 2.289419651031494, "[FF] Parameters of the MWR = Precipitation rate, wind speed, sea ice concentration, water vapor, clouds"]
-[9.421685218811035, 4.096001625061035, "[TT] Frequency Range of the Field Measurement Device = DC to 10 Hz"]
-[9.675586700439453, 6.602416038513184, "[TT] HST Loss Cone of the LCI = 6.5\u00ba"]
-[5.848933219909668, 6.101067066192627, "[FF] Delivery Time of the EDRS (European Data Relay System) = Within 18 minutes"]
-[9.31290054321289, 1.453979253768921, "[TT] Firing Speed of the HTA = High"]
-[9.076824188232422, 7.052194595336914, "[TT] Image Resolution of the SPOT-6 = 1-5 m"]
-[4.6159749031066895, 4.743903636932373, "[FF] Function of the RLS = Relays Return Link Messages from the RLSP to new generation beacons through the Galileo navigation signal"]
-[8.207942962646484, 7.341671466827393, "[TT] FPA Format of the CIRiS = 640 x 480"]
-[2.887216806411743, 4.2385149002075195, "[FF] Imagery Acquisition Date of the PALSAR-2 = June 27, 2014"]
-[7.239365100860596, 3.580840826034546, "[TT] Launch Date of the NightPod = December 21 2011"]
-[7.839693546295166, 4.935731887817383, "[FF] Components of the TEPCE = High voltage supplies, magnetorquers, GPS, camera, plasma sensors"]
-[10.94157886505127, 4.009161949157715, "[TT] Orientation of the Drag Sail = Convex side faces the sail"]
-[10.627922058105469, 5.309360027313232, "[TT] Electron Temperature Range of the Langmuir Probe = 500 - 10,000 K"]
-[5.326962947845459, 6.187246322631836, "[TT] Speed of the BILGE processor = 200 MHz"]
-[5.76540470123291, 1.920558214187622, "[FF] Status of the ExoMars = Performing flawlessly"]
-[8.42163372039795, 5.520666599273682, "[TT] Accuracy of the Radiation Budget Estimation Device = Better than 5%"]
-[3.979326009750366, 3.4744081497192383, "[TT] Development Oversight of the Galileo Second Generation = ESA"]
-[4.375802993774414, 3.1317591667175293, "[TT] Location of the NHS: New Hampshire Station, New Boston, NH = New Boston, NH"]
-[3.4691455364227295, 4.8600029945373535, "[FF] Data Importance of the SMMR = Far more interesting scientifically than the data from SAR"]
-[5.766704082489014, 7.046965599060059, "[TT] LVDS Serial Data Recording Port Speed of the PIC = 2 Mbit/s"]
-[5.903350830078125, 0.8214216232299805, "[FF] Observation Date of the ISEE-1 and ISEE-2 = July 1978"]
-[7.653910160064697, 4.614872455596924, "[FF] Function of the AMS-02 transition radiation detector (TRD) = Unknown"]
-[12.320252418518066, 2.9644691944122314, "[TT] Hydrazine Fuel Mass of the MERLIN = 28 kg"]
-[4.798708438873291, 0.45177972316741943, "[TT] Launch Date of the LIBRA = 2025"]
-[14.203975677490234, 3.2068798542022705, "[TT] Mass of the Stone = 1 kg"]
-[4.544372081756592, 3.094309091567993, "[TT] Location of the PDGS = DLR in Oberpfaffenhofen"]
-[6.535851955413818, 4.177447319030762, "[FF] Operational Interface of the SWOT = Unique"]
-[10.27353286743164, 3.2058792114257812, "[FF] URL of the TOPCAT = https://web.archive.org/web/20120306134438/http://www.bis.gov.uk/assets/bispartners/ukspaceagency/docs/space%20science/cubesats/cmos%20imager%20text.pdf"]
-[9.30548095703125, 3.6766083240509033, "[FF] Geomagnetic Field Data Capture of the \u00d8rsted Satellite = High-Precision"]
-[5.220191955566406, 2.4049072265625, "[TT] Agency of the DeMi = MIT"]
-[13.783591270446777, 3.4488930702209473, "[TT] Mass of the Transmitter = 700 g"]
-[6.803921699523926, -0.35336217284202576, "[TT] Exact Repeat Cycle of the Satellite = 8 days"]
-[7.129417896270752, 1.2368038892745972, "[TT] Operating Period of the Spitzer = 2003 until its decommissioning on Jan. 30, 2020"]
-[6.978196620941162, 6.276710510253906, "[TT] Number of Systems of the Dichroic Systems = 5"]
-[8.026005744934082, 1.7936114072799683, "[TT] Azimuth Coverage of the SWIM = 180 km"]
-[7.465615749359131, 5.549712181091309, "[TT] Contact Attempt Elevation Angle of the Polar Scout = Above 10 \u00ba"]
-[10.112061500549316, 5.779587745666504, "[FF] Standby Mode of the CAMEX = Minimize the average heat dissipation to the focal plane CCD"]
-[4.949234962463379, 7.395166873931885, "[TT] Data Rates of the RF communications = 9.6 kbit/s"]
-[5.350412368774414, 8.722723960876465, "[TT] Bandwidth of the Band 7 = 735-755 nm"]
-[8.405570030212402, 8.116679191589355, "[TT] Spectral Range of the QWIP Detector = 11-17 \u03bcm"]
-[5.055099964141846, 8.216792106628418, "[TT] Bandwidth of the RF communications = 30 MHz"]
-[10.39146900177002, 7.351896286010742, "[TT] Primary Mirror Diameter of the Telescope = 30 cm"]
-[6.660478115081787, 0.10423368215560913, "[TT] Revisit Time of the Landsat-9 = 16 days"]
-[1.7651081085205078, -2.063743829727173, "[FF] Mission of the Hayabusa = Itokawa, an S-type asteroid"]
-[7.699321746826172, 6.872441291809082, "[TT] Exposure Time of the NISP Spectrograph = About 4000 seconds"]
-[6.648704528808594, -0.2537049651145935, "[TT] Yaw Maneuver Frequency of the SABER = Once every sixty days"]
-[5.852513313293457, 4.740233898162842, "[TT] Reliability Impact of the Satlet System = Not impacted in many uses"]
-[7.732059478759766, 0.4552907347679138, "[FF] Trajectory of the Lunar IceCube = Low energy trajectory using gravitational manifolds"]
-[11.382179260253906, 4.743122577667236, "[TT] Diameter of the Great Blue Hole = Over 300 m"]
-[4.559179306030273, 7.8698601722717285, "[TT] Data Communications Transceiver Frequency of the OSSI-1 = 437.525 MHz"]
-[13.124836921691895, 7.6289167404174805, "[TT] Energy of the W-band = 0.3 meV"]
-[9.870481491088867, -1.4271199703216553, "[TT] Orbit of the Kounotori-5 = Near-circular orbit, altitude of ~400 km to ISS, inclination =51.6\u00b0"]
-[9.07550048828125, 5.598188877105713, "[TT] Cost (sensor + spacecraft) of the Push Frame Framer with a fast steering mirror = Very low"]
-[11.359780311584473, 4.400997161865234, "[TT] Size of the PSat-2 = 1.5U"]
-[3.879852294921875, 6.052732944488525, "[TT] Antenna Location of the Voyager 2 = Canberra, Australia"]
-[13.829320907592773, 5.685809135437012, "[TT] Solar Cells Efficiency of the EPS = 28%"]
-[5.37606143951416, 7.13129997253418, "[TT] User Data Rate of the Ka-ISL RTN service = Up to 300 Mbit/s"]
-[5.273857593536377, 0.6976919174194336, "[TT] Launch Date of the Satellite = April 26"]
-[8.642833709716797, -0.014243075624108315, "[TT] Asteroid Flyby of the Chang'e-2 = 1 km-level"]
-[5.72435998916626, 0.887074887752533, "[TT] Operation Status of the IBEX = Nominal in 2012"]
-[5.467371463775635, 5.2969160079956055, "[TT] OS of the RF communications = VxWorks"]
-[5.082983016967773, 3.1981778144836426, "[FF] Partners of the EDRS Space Data Highway = ESA, Airbus DS, DLR, 50 companies in 13 European countries"]
-[4.9880523681640625, 0.3738178610801697, "[TT] Launch Date of the SOHO = December 2, 1995"]
-[7.599360466003418, 1.2052961587905884, "[FF] Function of the Lunar Ops E/PO = Image the lunar surface"]
-[8.428301811218262, 7.151719570159912, "[FF] Design of the Micro-CMOS Cameras = Smart and low mass, low power, and highly-integrated"]
-[8.320008277893066, 1.6484580039978027, "[FF] Effect on Jet Stream of the La Ni\u00f1a = Pushes the jet stream north and causes it to curve"]
-[13.321212768554688, 7.4581708908081055, "[TT] Tx Power of the USAT = 5-10 W"]
-[5.826910495758057, 0.8408331274986267, "[FF] Launch Date of the Exoplanet mission = Unknown"]
-[6.457221031188965, 7.532620906829834, "[FF] Data Quantization of the FY-4A = 13 bit"]
-[8.512125968933105, 4.701848983764648, "[TT] Manufacturer of the Star Trackers = CAL Corp, Canada"]
-[8.119367599487305, 8.276263236999512, "[TT] Spectral Coverage of the ILAS = 44 infrared channels in the range from 6.21-11.77 \u00b5m (850-1610 cm"]
-[9.797330856323242, 4.209012985229492, "[TT] Quantity of the Magnetorquers = 5"]
-[5.409402370452881, 6.000582218170166, "[TT] On-board Data Storage of the STRV-1d DHS = 1 MB"]
-[3.8639495372772217, 4.494258880615234, "[TT] Data Products of the RADARSAT-2 = High-quality"]
-[4.896245002746582, 0.49189838767051697, "[TT] Scheduled Launch of the Patrol Mission = End of 2021"]
-[9.093411445617676, 3.153143882751465, "[FF] Global Picture of Mantle Conductivity of the Swarm = Can only be obtained from space"]
-[9.202481269836426, -1.0605326890945435, "[TT] Orbit of the ECOSTRESS = Precessing orbit of the ISS"]
-[8.313952445983887, 4.700621128082275, "[FF] Components of the ACS = One digital sun sensor, six coarse sun sensors, one three-axis magnetometer, three two-axis inertial gyros, TRACE instrument, three magnetic-torquer coils, four reaction wheels"]
-[6.447301387786865, -0.5267469882965088, "[TT] Forecast Duration of the JPSS = 3-7 days"]
-[3.793647050857544, -1.2077720165252686, "[TT] Orbit of the eROSITA = Second Lagrange point of the Earth-Sun-system"]
-[9.092885971069336, 1.3469785451889038, "[TT] Next Proposal Due Date of the New Horizons = Early 2022"]
-[8.632344245910645, 2.9522480964660645, "[FF] Purpose of the Taranis MCP = Accurate monitoring of Transient Luminous Event in the upper atmosphere"]
-[6.966212749481201, 4.438789367675781, "[FF] Level of the S/C TRD = Spacecraft Level"]
-[5.32056188583374, 0.7629544734954834, "[FF] Data Collection Period of the TROPOMI = January 1-20, 2020 and February 10-25, 2020"]
-[9.113697052001953, 3.313025712966919, "[FF] Calibration Date of the Swarm Magnetometry Package = Pre-Flight Calibration"]
-[5.069103240966797, 7.071478366851807, "[TT] Data Rate of the Uplink = 1 kbit/s"]
-[6.63361930847168, 4.874748706817627, "[FF] Framework of the Model = LFT (Linear Fractional Transformation)"]
-[9.7344970703125, -0.6263478398323059, "[TT] Orbit of the LADEE spacecraft = Low-altitude (50 km) retrograde equatorial orbit"]
-[8.34346866607666, 6.692838668823242, "[TT] Temporal Resolution of the ELENA = 40 s"]
-[12.091024398803711, 6.922823429107666, "[TT] Photon Index Below the Break of the First Broken Powerlaw = 1.54"]
-[8.979876518249512, -0.7342368364334106, "[TT] Ground Track Repeat of the MEO Constellation = ~ 10 days"]
-[3.1879429817199707, 5.076962947845459, "[TT] Experimental Mode Spatial Resolution of the TSX-SAR = 1m"]
-[2.884822368621826, 4.501059532165527, "[TT] Radiometry of the PALSAR-2 = 0.4 dB"]
-[6.065742492675781, 3.5237045288085938, "[FF] Cost of the RemoveDebris = Low"]
-[5.415862560272217, 2.6327645778656006, "[TT] Mission of the MTG-I = Imaging"]
-[5.504619121551514, 5.131763935089111, "[FF] Better Uplink Verification Method of the Ground System = Recording the uplink RF signal at the ground site using a software-defined radio"]
-[12.672859191894531, 7.524402618408203, "[TT] Power of the eROSITA instrument = 405 W"]
-[6.631200790405273, 2.128570556640625, "[FF] URL of the TGO Electra radios = http://www.esa.int/spaceinimages/Images/2016/03/TGO_Electra_radios"]
-[10.156656265258789, 2.2553927898406982, "[FF] Localization of the Swift = Very precise"]
-[6.890247821807861, 7.0167131423950195, "[TT] Modulation of the Laser Diodes = Power switching (on-off keying)"]
-[12.834566116333008, 7.587439060211182, "[TT] Power of the Total instrument = <256 W"]
-[7.986692428588867, 5.860527038574219, "[TT] Function of the Optical visual sensors = Close-up maneuvering"]
-[5.521264553070068, 5.700211524963379, "[TT] Processor of the OBC = 32-bit ARM-7"]
-[8.127835273742676, 4.4185261726379395, "[FF] Purpose of the Electromagnetic Calorimeter = Detecting and measuring the energy of particles"]
-[8.928210258483887, 4.7992072105407715, "[FF] Mounting Configuration of the Honeywell QA2000-030 accelerometers = One measures spin rate and the other measures nutation"]
-[5.646618366241455, -0.8580723404884338, "[TT] Design Life of the RASAT = 3 years"]
-[7.676560878753662, -0.8309022784233093, "[FF] Image of the Day Date of the ICESat-2 = 29 January 2019"]
-[5.060891151428223, 0.5584799647331238, "[FF] Launch Date of the TSIS-2 = Unknown"]
-[9.58521842956543, 8.228875160217285, "[TT] Field of View of the CHIPS = 5\u00ba \u00d7 26.7\u00ba"]
-[5.974756717681885, 4.870297908782959, "[FF] Design and Performance Presentation of the QZSS = ION NTM (National Technical Meeting) 2007, San Diego, CA, USA, January 22-24, 2007"]
-[13.741487503051758, 2.8496546745300293, "[TT] Mass of the SARAL spacecraft = 407 kg"]
-[5.428301811218262, 3.1232330799102783, "[TT] Heat Shield Manufacturer of the Orion = Lockheed Martin"]
-[13.282322883605957, 2.905557632446289, "[TT] Mass of the Microsat of ISRO = 100 kg"]
-[8.424415588378906, 3.8380513191223145, "[FF] Calibration Method of the ARTEMIS = Solar radiation-based"]
-[7.713387489318848, -0.4944758713245392, "[FF] Detection Date of the IceCube = 10 March 2021"]
-[8.55412769317627, 7.051027774810791, "[FF] L1 Detectors Purpose of the HIT = Sweep out a 4\u03c0, full-sky coverage"]
-[9.556848526000977, 5.665745258331299, "[TT] Performance of the MAG = \u00b130 nT"]
-[14.075695037841797, 3.0288195610046387, "[TT] Mass of the TechDemoSat-1 = 150 kg"]
-[7.423976898193359, 5.338474750518799, "[FF] Purpose of the LRI = Measure distance variations between remote spacecraft"]
-[12.693517684936523, 1.9165105819702148, "[FF] Monitored Parameters of the SAGE-III = Aerosols, ozone and other gases in Earth\u2019s high atmosphere"]
-[4.609419822692871, 0.6341214179992676, "[TT] Uplink Test Date of the QBITO = May 2016"]
-[8.016425132751465, 5.305006504058838, "[FF] Design Components of the CHRIS = Catadioptric telescope, imaging spectrometer, area detector array"]
-[8.460692405700684, 6.813714981079102, "[TT] Scanning Technique of the WFI = Pushbroom"]
-[8.051464080810547, 6.460291862487793, "[TT] Sensor Type of the SSULI = Ultraviolet Limb Imager"]
-[8.455615997314453, 6.956517696380615, "[TT] Instrument Type of the MR-900B = High resolution optical imagers"]
-[5.108297348022461, 2.4164092540740967, "[TT] Agency of the Sich-2 = NSAU"]
-[5.761034965515137, 6.981484413146973, "[TT] Data Rate of the CATS = ~2 Mbit/s"]
-[13.927696228027344, 3.0731959342956543, "[FF] Mass of the RinconSat = Unknown"]
-[10.102350234985352, -1.4746142625808716, "[TT] Orbit Inclination of the Sentinel-2 satellites = 98.6\u00b0"]
-[9.502702713012695, 3.934281349182129, "[FF] Components of the Test Equipment = Two sets of two magnetometer sensors denoted as MAG1 and MAG2 and a digital E-Box"]
-[10.864579200744629, -0.2932981550693512, "[FF] Mission Overview and Status of the TanDEM-X = Not Provided"]
-[7.992314338684082, -1.0039615631103516, "[FF] Ground Track of the ICESat-2 = Exactly repeating"]
-[3.453878164291382, 1.7261344194412231, "[FF] Workshop Date of the Sentinel-2 MMFU = Oct.23-25, 2012"]
-[6.00183629989624, -0.47341305017471313, "[TT] Mission Duration of the TRACE = 12 years"]
-[14.287757873535156, 3.00063419342041, "[TT] Mass of the HORYU-2 = ~ 7 kg"]
-[5.991491317749023, 3.577683687210083, "[FF] Program Objectives of the MightySat = Provide an environment for frequent, inexpensive, on-orbit demonstrations of emerging space system technologies and to accelerate their transition into operational use"]
-[10.152727127075195, 4.060895919799805, "[TT] Booms of the Spacecraft = Four 60 m wire booms in the spin plane for electric field sensors"]
-[5.780213832855225, 0.5250045657157898, "[FF] SAR Tandem Mission Date of the ERS-2 = September 2007 to February 14, 2008"]
-[8.139911651611328, 5.778092384338379, "[TT] Operation Mode of the SLATS = NDO tracking"]
-[5.203457832336426, 8.425127983093262, "[TT] Channel of the Broadband Applications Experiment = 450 MHz broadband channel"]
-[10.373051643371582, 2.2763633728027344, "[FF] Sensitivity of the SSD\u2019s = X-rays to visible wavelengths"]
-[3.6040658950805664, 4.857423782348633, "[FF] Linear Polarimetric Mode of the RISAT-1 = Restricted coverage of 20\u00b0 to 30\u00b0 incidence angle"]
-[8.126461029052734, 0.6366192102432251, "[TT] Groundwater Storage Comparison Period of the GRACE-FO satellites = 1948-2010"]
-[5.956757545471191, 4.815183639526367, "[FF] Type of the P-SBAS service = On-demand processing"]
-[5.317533493041992, 0.31765612959861755, "[TT] Launch Date of the RAVAN = Nov. 11, 2016"]
-[12.026820182800293, 2.13848614692688, "[TT] Wheel Configuration of the CartoSat-2 = Tetrahedral"]
-[6.809389114379883, 4.7201738357543945, "[FF] Measurement of the Global Positioning System = Geopotential Heights"]
-[7.531836986541748, 4.78120231628418, "[TT] Mounting Location of the Photodetector = Vacuum flange"]
-[13.550382614135742, 5.300097942352295, "[TT] Manufacturer of the Solar Panels = PrecizikaMET SC"]
-[8.582188606262207, 2.035243272781372, "[FF] Measurement of the Compact Ocean Wind Vector Radiometer (COWVR) = Direction and speed of winds at the ocean surface"]
-[5.794418811798096, 7.184762477874756, "[TT] Nominal Mode Data Rates of the LunaH-Map = 1 kbit/s to 128 kbit/s"]
-[8.331868171691895, 1.0521149635314941, "[TT] Quake Magnitude of the SEIS = 3.3"]
-[8.134839057922363, 8.37663745880127, "[TT] Number of Bands of the VNIR Filter Assembly = 10"]
-[13.801885604858398, 5.672506809234619, "[FF] Goal of the Solar Cells = Enable high-efficiency space solar cells and panels to be produced in large quantity and at lower cost"]
-[13.99035358428955, 3.119630813598633, "[TT] Digital Data Handling Subsystem Mass of the SIR-C = 145 kg"]
-[5.292534351348877, 0.616694986820221, "[TT] Archival Data Collection Date of the NEOWISE = Between 2009 and 2011"]
-[4.599162578582764, 1.7855826616287231, "[FF] Conference Presentation Date of the JC2Sat & MIRAD = Sept. 29 to Oct. 3, 2008"]
-[9.281813621520996, 7.984115123748779, "[TT] Focal Planes of the ETM+ Scanner = 2"]
-[6.786660671234131, 2.826767683029175, "[FF] Sponsors of the RECCAP-2 = Global Carbon Project, European Space Agency, National Institute for Environmental Studies, International Carbon Coordination Project"]
-[5.950292587280273, 7.139970302581787, "[TT] Data Rate of the GOLD instrument = ~6 Mbit/s"]
-[5.94366979598999, -0.5278245806694031, "[TT] Development Schedule of the ANGELS = Particularly short"]
-[13.315340995788574, 7.7521796226501465, "[TT] Amplifier Power of the Knudsen Station = 500 W"]
-[6.582427978515625, 2.1070313453674316, "[FF] Mission of the IMP = On-orbit verification and the monitoring of the secular change of the materials exposed to space"]
-[5.39971399307251, -0.0003369616169948131, "[FF] Data User's Manual of the IRS-P6 = Unknown"]
-[4.52094030380249, 5.4134650230407715, "[FF] Orbit Track of the GomX-3 = Not provided"]
-[4.66505765914917, 5.510732650756836, "[FF] Function of the Master Beacon (MB) = Transmit instructions for on-board programming and time-tagging information"]
-[5.397797107696533, 0.6965385675430298, "[FF] Mission Status Report Date of the QuikSCAT = Nov. 23, 2009"]
-[6.492342948913574, 7.5882887840271, "[TT] Data Quantization of the SXI = 10 bits"]
-[11.00631332397461, 0.8569265007972717, "[TT] Satellite Triangle Side Length of the LISA = Approx. 2.5 million kilometers"]
-[8.501218795776367, 6.670535564422607, "[TT] Daily Imaging Capacity of the SEOSat = 2,500,000 km2"]
-[9.56179141998291, 8.20689582824707, "[TT] Field of View of the Camera 1 = 84.6\u00ba"]
-[6.574948787689209, 5.438608646392822, "[FF] Components of the DACS = Atmel's high speed ADC (Analog Digital Converter) & demultiplexer and a Xilinx XQVR-600 FPGA-based BAQ and formatter"]
-[8.464502334594727, 7.8829426765441895, "[FF] Challenge of the WCOM = Insufficient resolutions of the instruments"]
-[5.146154403686523, -0.34760916233062744, "[TT] Retirement Date of the CBERS-2B = May 10, 2010"]
-[13.744016647338867, 2.87890625, "[TT] Weight of the Windsat = 450 kg"]
-[9.207372665405273, 4.322403907775879, "[FF] Solar Panel Orientation of the X-Sat = Pointed towards the sun, except during imaging or downlinking operation during certain orbits over a small portion of its period"]
-[5.605630397796631, 1.2945269346237183, "[FF] LRIT and HRIT Broadcasting Service Start Date of the GK2A satellite = 2011"]
-[7.728578567504883, 1.5817099809646606, "[FF] Purpose of the SWOT = Study small-scale features of ocean surface"]
-[4.464630603790283, -0.8621301651000977, "[FF] Arrival Method of the Dragon CRS-14 = Snagged by the orbiting lab's huge Canadarm2 robotic arm"]
-[8.17346477508545, 8.775236129760742, "[FF] Function of the MOH = Emits a pulsed infrared signal. Combined, the MOHs enable 6 DOF resolution of the relative state when operating in cooperative mode"]
-[14.063617706298828, 3.4323573112487793, "[TT] PCB Mass of the MPPT = ~ 50 g"]
-[4.675085067749023, 6.621029376983643, "[TT] Technology of the EARS = DVB-S2"]
-[9.250648498535156, 0.24331378936767578, "[FF] Location of the Izmit Bay Suspension Bridge = Gulf crossing Izmit Bay"]
-[5.93244743347168, 2.434157371520996, "[FF] Possibility of Earlier Launch of the Worldview Legion = Possibly pull that into the back end of 2020"]
-[9.506139755249023, 6.196188926696777, "[TT] Incidence Angle Range of the Wide Standard Quad-Polarisation Mode = 18-42\u00ba"]
-[14.253303527832031, 3.142343521118164, "[TT] Mass of the ASTERIA = 10 kg"]
-[10.889086723327637, -0.3382052183151245, "[FF] Conference Date of the Tandem-L = June 4-7, 2018"]
-[14.301591873168945, 3.2871932983398438, "[TT] Mass of the VPU = 3.2 kg"]
-[3.8126027584075928, 7.921161651611328, "[TT] Modulation of the CBERS-1 = QPSK for HRCC and WFI data streams and BPSK for IRMSS"]
-[5.354487419128418, 1.0705479383468628, "[FF] Departure Date of the CuPID = July 2021"]
-[8.655943870544434, 0.8030767440795898, "[TT] Date of the Proximity Flyby = June 3, 2018"]
-[4.344920635223389, -0.11093129962682724, "[TT] Launch Date of the P35-6 = 19.1.1964"]
-[6.662575721740723, -0.35508662462234497, "[TT] Connection Period of the Satellite Link = March 20 to April 5"]
-[10.708799362182617, 3.301011562347412, "[FF] Field of the Micro-gravity experiment = Fluid mechanics"]
-[4.878104209899902, 3.103231191635132, "[TT] Manufacturer of the ROSE-L SAR = Airbus"]
-[13.609502792358398, 1.7452938556671143, "[TT] Combined Mass of the Dragon\u2019s Trunk = 645 kg"]
-[6.542277812957764, 5.352542400360107, "[FF] Function of the DAQ (Data Acquisition) System = Digitization of the signals from the straw tubes"]
-[7.916773319244385, 8.46364688873291, "[TT] Scanning angle of the Spectral Bands = ~\u00b140\u00ba (1400 km)"]
-[4.659497261047363, 0.9340437054634094, "[TT] Agreement Date of the BRITE-PL = May 2010"]
-[10.02840518951416, 4.396059036254883, "[FF] Deployment Time of the SpinSat = Few minutes after the plunger inhibit switches disengage from the Cyclops pusher plate"]
-[9.309343338012695, 6.001514434814453, "[TT] Heating Power of the Shutter = Lower than 0.5 W"]
-[8.080002784729004, 8.023606300354004, "[TT] Spectral Band of the Camera = 762 nm"]
-[5.677172660827637, -0.12286017835140228, "[FF] Deployment Over Operating Temperature of the RDA = Not provided"]
-[6.748921871185303, 8.46341323852539, "[TT] Spectral Channels of the SEVIRI = 12"]
-[9.111371040344238, 2.7803919315338135, "[FF] Interaction of the IBEX = Solar wind pushes up against the interstellar material"]
-[8.435830116271973, 7.387919902801514, "[FF] Optical Performance of the DST = Limits to some extent the optical performance with regard to maximum swath width, MTF degradation, and stray light problems"]
-[6.408996105194092, 5.0000786781311035, "[FF] Components of the Ground Station = Receiving antenna, antenna rotating and control system, low noise amplifier, receiver, ground station control software"]
-[8.570387840270996, 4.454286575317383, "[FF] Function of the Space Observatory = Continuous photometric monitoring of stars"]
-[9.43384075164795, -0.7106476426124573, "[TT] Orbit Parameters of the GEOS-2 = 1,079 km x 1,572 km x 105.8\u00ba"]
-[10.747377395629883, -1.0708129405975342, "[TT] Attitude Mode of the SLATS = NM-Z"]
-[14.26939868927002, 3.0132718086242676, "[TT] Mass of the Global-7 = 56 kg"]
-[7.662651538848877, 9.231292724609375, "[TT] Wavelength Range of the Band No 6 = 11.5 \u00b1 0.50 - 12.5 \u00b1 0.50 \u00b5m"]
-[14.108659744262695, 3.411065101623535, "[TT] Mass of the Battery = About 3.5 kg"]
-[9.778270721435547, -0.6492006778717041, "[TT] Orbit Altitude of the GeoEye-1 = 681 km"]
-[7.981472492218018, 7.399191856384277, "[TT] Image Video Stream Capacity of the MSI instrument = 1.4 Tbit"]
-[7.500644683837891, 4.755666732788086, "[FF] Function of the Coherency Filter = Rely on the fact that true lightning events are coherent in time and space, whereas noise events are not"]
-[3.3197226524353027, 4.734100818634033, "[FF] Sensitivity of the SeaSat SAR = Surface roughness, slope, and land-water boundaries"]
-[7.760256290435791, 8.640384674072266, "[TT] Nr. of spectral or frequency bands of the Optical System = 4 in VIS and 1 in SWIR"]
-[3.6341495513916016, 4.814920902252197, "[TT] Vertical Accuracy of the In-flight simulated radar interferometry experiment = 1 m"]
-[10.227557182312012, 8.05648422241211, "[TT] Aperture Range of the Telescope = 30 cm to 2 m"]
-[8.01845645904541, 3.0958383083343506, "[FF] Application of the Falcon Neuro = Sprite and lightning detection on the International Space Station"]
-[3.411930561065674, 6.422872066497803, "[TT] Mounting Plate Diameter of the SciSat/ACE = 1.12 m"]
-[4.727018356323242, -1.3560941219329834, "[TT] Transport Destination of the Yuanwang-21 and -22 = Qinglan, Hainan island"]
-[6.923183917999268, 8.512534141540527, "[FF] Channel Centre Wavelengths of the LIMS = 6.25, 6.75, 9.65, 11.35, 15.25 \u00b5m and one broad channel from 13.3 - 17.2 \u00b5m"]
-[6.8077192306518555, 4.570746421813965, "[FF] Flexibility of the Coprocessor = Can be programmed in orbit for different purposes"]
-[4.194100856781006, 7.382711410522461, "[TT] Frequency of the X-band phased array antenna = 8125 MHz"]
-[9.47264289855957, 6.3063788414001465, "[TT] Field of Regard of the Scan Mirror Mechanism = \u00b16\u00b0"]
-[5.7828593254089355, 5.511250019073486, "[FF] Function of the SoCWire = Attach to the running system by a flexible and glitch-free on-chip communication architecture"]
-[4.990407943725586, 2.8770692348480225, "[TT] Provider of the NSSL Phase 2 = ULA and SpaceX"]
-[7.918025970458984, 4.882229804992676, "[FF] Evaluation Method of the Precise Position Determination System = GCPs (Ground Control Points) prepared for the calibration will be used as true value"]
-[11.463020324707031, 4.585218906402588, "[TT] Mechanical Standard of the CubeLCT = PC/104"]
-[5.978346347808838, 3.5185704231262207, "[FF] Launch Options of the MightySat = STS (Shuttle) or with multi-service launch systems"]
-[5.4923505783081055, 7.616971969604492, "[TT] Pulse Repetition Frequency of the Radar = 189 Hz"]
-[4.806994438171387, 0.027702797204256058, "[TT] End of Life Date of the EXPORTS = July, 2025"]
-[7.405248641967773, 3.585233688354492, "[FF] Purpose of the STRATOS instrument = Makes use of GPS occultation measurements to determine temperature, pressure and humidity profiles of Earth's atmosphere for application in operational meteorology"]
-[7.785921573638916, 7.175879001617432, "[TT] Frame Rate of the Video Camera = 10/s"]
-[9.980125427246094, -0.5147181153297424, "[TT] Altitude of the RISAT-1 = 543 by 539 km"]
-[5.032024383544922, 7.805785179138184, "[TT] Power of the 406 MHz EPIRB = 5 W"]
-[4.865785121917725, 0.49317923188209534, "[TT] Launch Date of the GeneSat-1 = December 16, 2006"]
-[8.12268352508545, -0.49770185351371765, "[TT] Ice Loss of the GRACE-FO = 600 billion tons"]
-[7.743953704833984, 1.928198218345642, "[FF] Impact of the Climate Models = Helped scientists separate natural changes in the Earth's climate from human influences"]
-[6.642165184020996, 6.398679733276367, "[TT] ToO Exceptional Programming Delay of the SVOM = <12h"]
-[8.07373332977295, 7.862009525299072, "[TT] Detector Elements of the VIS Channel Detector = 4"]
-[11.868237495422363, -0.018945273011922836, "[FF] Function of the TESS = Planet-hunting"]
-[13.405997276306152, 2.8896539211273193, "[TT] Satellite Class of the Cheollian 2B = 3.4-ton class"]
-[3.855536937713623, 3.4302279949188232, "[FF] Image Release Date of the Galileo = 28 March 2018"]
-[7.541517734527588, 6.459470272064209, "[TT] Relative Time Resolution of the XGRE = 1 \u00b5s"]
-[8.73604965209961, 6.5927042961120605, "[FF] Anomaly of the ISUAL = Dark line appears in the images"]
-[9.400392532348633, -1.7227113246917725, "[TT] Mean Anomaly at Epoch of the Swarm-C (Charlie) = N/A"]
-[5.473865509033203, 6.139301300048828, "[TT] RAM of the SMX-2 = 4 MByte"]
-[5.551270484924316, 5.669139862060547, "[TT] Processor of the Spacecraft = Mongoose V processor"]
-[13.772090911865234, 5.361466884613037, "[TT] Type of the Solar Cells = GaInP/GaAs/Ge triple junction solar cells"]
-[7.546212673187256, 2.963529586791992, "[FF] Measurement Capability of the Synthetic Aperture Radar = Measure methane emissions"]
-[10.289871215820312, 2.7375881671905518, "[FF] Catalyst for Establishing a Nanosatellite Manufacturing Sector of the MDASat-1 = Yes"]
-[7.344155311584473, 4.107607364654541, "[FF] Performance of the GEOSAT Follow-On Water Vapor Radiometer = Not Specified"]
-[13.786192893981934, 2.8230509757995605, "[TT] Mass of the Spacecraft = 95 kg"]
-[7.0519185066223145, 8.212371826171875, "[TT] SNR (Signal-to-Noise Ratio) of the O2-A = 360"]
-[7.281600475311279, 2.0512356758117676, "[TT] Capability of the Carbonite Smallsat = Multi payload"]
-[4.549870491027832, 3.821763038635254, "[TT] Number of Satellites of the Galileo = 14"]
-[9.201311111450195, 6.224429607391357, "[TT] Plane Orientation of the Imaging Calorimeter = x-plane, y-plane"]
-[8.807278633117676, 6.468909740447998, "[TT] Calibration Images of the PROBA-V = 2.674"]
-[9.10129165649414, -1.2345044612884521, "[TT] Orbit of the EDRS-C = Geostationary"]
-[6.57395601272583, -0.43229949474334717, "[TT] Repeat Cycle of the Resurs-P1 = 3 days"]
-[5.525376796722412, 0.718407392501831, "[TT] International ID of the SpriteSat = 2009-002C 33494"]
-[5.966644763946533, -0.6621894836425781, "[TT] Mission Life of the ECS = 1 year"]
-[4.923794746398926, 0.6890727877616882, "[TT] Launch Year of the Electro-L2 = 2015"]
-[7.948522090911865, 0.18298177421092987, "[FF] Detection Capability of the GRACE-FO = Month-to-month variations in Earth's gravity field caused by the movement of mass as small as about a 1 cm of water over an area of about 320 km in diameter"]
-[7.899526596069336, 7.134250640869141, "[TT] Detection Efficiency of the Instrument = ~90%"]
-[4.526435852050781, -0.8443394899368286, "[TT] Docking Date of the Dragon spacecraft = June 5"]
-[7.885793209075928, -0.15275168418884277, "[TT] Latency of the ATL06 Land Ice Height = 45 days"]
-[4.480011940002441, 7.793886184692383, "[TT] Range of the S-band = 2098 - 2110 MHz"]
-[7.275334358215332, 1.2634137868881226, "[FF] Function of the SFR = Collect Martian samples"]
-[4.46742582321167, 2.887296438217163, "[FF] Location of the Margarita Island = Venezuela"]
-[8.70569133758545, 7.039127826690674, "[TT] Field of View of the WV60 imager = 2.12\u00b0"]
-[7.244446277618408, 3.630730152130127, "[FF] Manufacturer of the NightPod = ESA"]
-[8.614686012268066, 2.561610221862793, "[TT] Vertical Scan Emphasis of the MLS = Lower stratosphere and upper troposphere"]
-[11.204004287719727, 5.043038368225098, "[TT] Mass-Cage Contact of the Inertial Sensors = 5 \u00b5m diameter gold wire"]
-[3.3431105613708496, 4.961928367614746, "[FF] Calibration Modes of the SAR Instrument = Interferometric calibration mode, Amplitude/phase distortions measurement mode"]
-[13.842303276062012, 2.9763195514678955, "[TT] Payload Mass of the ADEOS-II = 1300 kg"]
-[3.592514991760254, 6.9743266105651855, "[TT] Polarizations of the RF communications = RHCP and LHCP"]
-[6.335817813873291, 4.499838829040527, "[FF] Function of the Order Handling and Distribution System = Accepts and handles acquisition request and send them to Mission Planning System as data acquisition requests"]
-[10.176481246948242, 5.779702186584473, "[TT] Temperature of the PICNIC IR detector = Around 90 K"]
-[9.512232780456543, 1.1072741746902466, "[TT] Outward Speed of the Blast Wave = About 11 million miles per hour"]
-[14.306815147399902, 3.35322904586792, "[TT] Mass of the TANSO-CAI = 40 kg"]
-[3.6325061321258545, 4.606018543243408, "[FF] Interferometry Technique of the Synthetic Aperture Radar = More sensitive to the motion of the ice"]
-[5.1604533195495605, 4.001929759979248, "[TT] Number of Satellites in Production of the Eurostar E3000 = 6"]
-[5.0999860763549805, 7.661978244781494, "[TT] Amplifier Efficiency of the Ka-band = 13%"]
-[14.256210327148438, 3.232140064239502, "[TT] Total Mass of the XPAA = 5.5 kg"]
-[6.09635591506958, 0.5308560729026794, "[FF] Test Standards of the PCU EQM = MIL-STD-461E, ECSS-E-10-03A"]
-[13.460679054260254, 2.7980518341064453, "[TT] Wet Mass of the Coronagraph Spacecraft = 300 kg"]
-[5.678152084350586, 3.665846109390259, "[TT] Support Level of the Test Station = Subsystem to SV (Space Vehicle) I&T (Integration and Test) level"]
-[7.343050003051758, 3.723940849304199, "[FF] Occultations per Day of the MetOp-SG Radio Occultation = More than 1300"]
-[9.269414901733398, 1.033575415611267, "[TT] Orbital Path of the Juno spacecraft = Over Jupiter's poles"]
-[5.964585781097412, 0.7841432094573975, "[FF] Testing Date of the Camera = 2012"]
-[9.717811584472656, -0.6256023049354553, "[TT] Orbit Altitude of the Enxaneta = Approximately 550 km"]
-[10.298919677734375, 3.291189432144165, "[TT] Communication Frequency of the Sunstorm CubeSat = S-band"]
-[8.752511024475098, -0.23531119525432587, "[TT] Lunar Orbit Inclination of the Chang'e-1 = 90\u00ba"]
-[5.200761318206787, 0.7013201117515564, "[TT] Mission Status of the CYGNSS = On Track"]
-[5.54055118560791, 1.3116503953933716, "[TT] Development Start Year of the SMOG-P = 2014"]
-[9.05251693725586, 4.5158915519714355, "[FF] Safe Attitude Mode of the TIMED = \u2013y side of the spacecraft is pointed at the Sun and the solar arrays are rotated to face the Sun"]
-[6.149885177612305, 2.9706859588623047, "[FF] Imagery Refresh Rate of the WorldView Legion = Unprecedented speed in the industry"]
-[6.6445088386535645, 5.549713611602783, "[TT] State-of-Health of the AOCS = Normal"]
-[11.992444038391113, 4.900208950042725, "[TT] Dimensions of the Saffire Experiment Module = Approximately 53 x 90 x 133 cm"]
-[7.347517013549805, 0.23336321115493774, "[TT] TAG Date of the OSIRIS-REx = Up to asteroid departure in March 2021"]
-[9.546117782592773, 4.284619331359863, "[TT] Attitude Sensor of the UniSat-3 = COTS three-axes magnetoresistive magnetometer (TAM)"]
-[5.797692775726318, 1.2511260509490967, "[TT] Image Acquisition Date of the Suomi NPP satellite = April 24, 2022"]
-[3.9687817096710205, 7.248468399047852, "[TT] Gain of the LNA = 43 dB"]
-[6.845664978027344, 5.869192600250244, "[TT] ISPR of the PM = 12"]
-[3.75533390045166, -0.7264269590377808, "[FF] Orbit of the Telesat LEO Phase 1 = Low Earth Orbit (LEO)"]
-[9.82799243927002, -0.28446677327156067, "[TT] Altitude of the Main Payload = ~661 km"]
-[5.140073776245117, 2.1643877029418945, "[FF] Mission Selection Criteria of the TacSat-3 = Specific capabilities to meet user needs"]
-[6.867788314819336, 4.213589191436768, "[FF] Unknown of the USMCC = Unknown"]
-[6.18166446685791, 6.819068431854248, "[TT] Optical Link Bandwidth (Uplink) of the OICETS satellite = 2 Mbit/s"]
-[3.4678103923797607, 6.363857269287109, "[TT] Aperture Size of the Antenna = 13 m"]
-[9.324081420898438, 4.193682670593262, "[TT] Technology of the Magnetometers = Magneto resistive device of Honeywell HMC 2003"]
-[7.971214294433594, 8.691324234008789, "[TT] Resonance of the TOI-178 = Laplace"]
-[9.847122192382812, 4.68549108505249, "[TT] Spin Rate of the SCD-2 = 32 - 36 rpm"]
-[5.365959167480469, 0.8533834218978882, "[FF] Internet Demonstration Time Frame of the UoSAT-12 = April-June 2000"]
-[9.287383079528809, 7.331599235534668, "[TT] Resolution of the IRMSS = 150 m"]
-[5.631336688995361, 2.795757532119751, "[TT] Funding of the FGS = CSA (Canadian Space Agency)"]
-[6.2185282707214355, 7.897819519042969, "[TT] UART Interface Channels of the SpaceCube 2 = 2"]
-[7.860646724700928, 1.7542258501052856, "[FF] Mission of the GOCE = Gravity field and steady-state Ocean Circulation Explorer"]
-[7.38075590133667, 5.785223960876465, "[FF] Sampling Time Offset of the Science Question Methodology = 1 hour and 40 minutes"]
-[6.155206680297852, 5.488097190856934, "[FF] Signal Processing of the TriG receiver = Multiple reconfigurable FPGAs"]
-[8.99876880645752, 5.622753620147705, "[TT] Pointing Accuracy of the Spacecraft = 0.24 arcsec relative pointing accuracy over 1 minute"]
-[7.589176177978516, 1.4405750036239624, "[FF] Presentation of the SWOT = Engaging the applications community of the future Surface Water and Ocean Topography (SWOT) mission"]
-[8.383846282958984, 7.54600191116333, "[TT] Detector Type of the CERES = Thermistor bolometers"]
-[11.610882759094238, 3.4128339290618896, "[TT] Ion Electric Propulsion of the Electric Propulsion Test Subsystem = Isp = 3000 s \u00b1 300 s"]
-[6.626361846923828, 0.5187503099441528, "[TT] Term of the Landsat Science Team = Five years"]
-[8.000456809997559, 1.8215875625610352, "[FF] Increase of the Evapotranspiration = About 10% since 2003"]
-[6.7776055335998535, 5.956021308898926, "[TT] Subaperture Quantity of the SMART = Four and eight"]
-[13.921570777893066, 7.252981185913086, "[TT] Power of the Voltage 5 = 2"]
-[6.924928188323975, 4.324392318725586, "[FF] Unknown of the SLA = Unknown"]
-[6.68513298034668, 4.70667839050293, "[FF] Function of the NGA = Ensures safety of navigation in the air and on the seas"]
-[6.156205177307129, 1.9766701459884644, "[FF] URL (presentation) of the Cute-1.7+APD = http://lss.mes.titech.ac.jp/ssp/cute1.7/paper/aca2007_p.pdf"]
-[5.656338691711426, 5.6691179275512695, "[TT] Microprocessor of the ADCS = 32-bit ARM"]
-[7.7630228996276855, 9.418163299560547, "[TT] Band Center Wave of the M1 = 0.412 \u00b5m"]
-[5.963157653808594, 7.530549049377441, "[TT] Signal Sampling of the MWI = Digital"]
-[10.359732627868652, 2.113635778427124, "[TT] Brightness of the Swift J0042.6+4112 = Brighter in high-energy X-rays than anything else in the galaxy"]
-[4.510527610778809, -0.8905845880508423, "[FF] Arrival Date of the SpaceX Dragon = 4 April 2018"]
-[7.921548366546631, 5.972135066986084, "[FF] Components of the DDS = COTS camera"]
-[11.400891304016113, 6.63742208480835, "[TT] Particle Contamination Level of the VSSC = Maximum of 300 ppm"]
-[11.431419372558594, 5.71673583984375, "[TT] Main Metal Percentage of the Nickel Alloy = 74%"]
-[8.178411483764648, 2.944019317626953, "[FF] Purpose of the ARI = Optimize measurement of the long-term changes of Earth\u2019s atmosphere and surface"]
-[6.128060817718506, 2.5270438194274902, "[TT] Development Program of the HAUSat-2 = SSRL (Space System Research Laboratory) at Hankuk Aviation University"]
-[10.352269172668457, 5.736810684204102, "[TT] B1 and B2 Tank Temperatures Increase of the Advanced Composition Explorer = By 5\u00b0 C"]
-[6.025094032287598, 6.901917934417725, "[TT] Data Compression of the PLDHS = From 1.3 Gbit/s to 450 Mbit/s"]
-[4.723396301269531, 2.9246885776519775, "[TT] Manufacturer of the ART-XC telescope = Russia"]
-[10.395360946655273, 5.936305522918701, "[TT] Mounting Range of the WFI = -24\u00ba to +24\u00ba"]
-[7.856571197509766, 9.013306617736816, "[TT] Wavelength of the MWIR = 4 to 6 \u00b5m"]
-[6.086400032043457, 5.461874008178711, "[TT] FPGA of the OBC = Radiation-hardened"]
-[9.769715309143066, -0.6509243845939636, "[TT] Orbit Altitude of the ProSEDS = 400 km"]
-[8.171036720275879, 1.1975164413452148, "[TT] Soil Moisture Accuracy of the SMOS = 4%"]
-[4.861661434173584, 7.209815502166748, "[TT] Uplink Beacon Data Rate of the RF Communications = 20 bit/s"]
-[5.749313831329346, 5.424609661102295, "[FF] Data Throughput of the Ground Station = Doubled"]
-[7.486072063446045, 5.570985794067383, "[FF] Modules of the EOS = OM (Optical Module) and CEU (Camera Electronics Unit)"]
-[11.427908897399902, 3.929164409637451, "[TT] Program of the AeroCube-7 = OCSD (Optical Communication and Sensor Demonstration)"]
-[3.462526559829712, -0.9190928936004639, "[TT] Orbit of the SMDC-ONE = Non-sun-synchronous orbit"]
-[5.800126075744629, 7.225358009338379, "[TT] Data Rate of the GeoEye-1 = 740 Mbit/s"]
-[7.433793544769287, 7.99754524230957, "[FF] Dynamic Range of the Instrument = 2.7 K to 340 K"]
-[13.213286399841309, 7.342312335968018, "[TT] Power Consumption of the OBC = 6 W max"]
-[7.706336975097656, 1.895162582397461, "[FF] Measurement Types of the Argo Array = Temperature, salinity, pressure, and velocity"]
-[12.092759132385254, 3.216359853744507, "[TT] Propellant of the BIT-3 = Iodine"]
-[9.057787895202637, 4.562978744506836, "[TT] Attitude Profile of the S/Cs = Sun-pointing"]
-[4.518885135650635, 7.740964889526367, "[TT] Frequency Band of the TOTEM SDR = 400-440 MHz"]
-[4.850037574768066, -1.5069477558135986, "[TT] Expected Mars Orbit Entry Date of the Tianwen-1 = February 10"]
-[6.714718818664551, 4.054266929626465, "[FF] Unknown of the Ground-based experimental facility = Unknown"]
-[13.57150650024414, 5.885188102722168, "[TT] Power of the Solar arrays = 750 W (600 W average)"]
-[8.374229431152344, 2.3640620708465576, "[FF] Objectives of the ROSA = Atmospheric properties Measurements of atmospheric temperature, pressure profiles, and water vapor content"]
-[7.574681758880615, 6.482675075531006, "[FF] Time Resolution of the MCP = Better than several hundred \u00b5s"]
-[10.90444278717041, 5.459094047546387, "[TT] Transition Temperature of the Superelastic SMA = Below 0\u00baC"]
-[8.225412368774414, 7.3885087966918945, "[FF] Type of the MCP Detector = 1D position-sensitive \"stop\" anode"]
-[4.264132499694824, 7.261797904968262, "[TT] Downlink Frequency of the PARASOL = X-band"]
-[8.015830993652344, -0.4030936658382416, "[FF] Average Age of the Arctic Sea Ice = Younger"]
-[8.847138404846191, 0.23368604481220245, "[TT] Distance from Earth of the OSIRIS-REx = More than 200 million miles (321 million km)"]
-[3.8659772872924805, 4.582015514373779, "[TT] Mean Radiometric Error of the RADARSAT-2 = Approximately -0.1 dB on ascending passes and +0.15 dB on descending passes"]
-[5.024076461791992, 3.0714027881622314, "[FF] Integration Location of the GOLD instrument = Airbus Defence and Space in Toulouse, France"]
-[9.50187873840332, -1.0922226905822754, "[TT] Longitude of the On-orbit Storage Position = 105\u00ba W"]
-[8.48669719696045, 7.310561656951904, "[TT] Type of the Focal Plane Receiver = Multi-chromatic TDI"]
-[12.808268547058105, 7.58815336227417, "[TT] Power Consumption of the OBRC instrument = Not more than 1 kW"]
-[5.376888275146484, 7.061005592346191, "[TT] Communication Rate of the TSUBAME = More than 10 kbit/s"]
-[11.12996768951416, 5.2422871589660645, "[FF] Scintillation Counter Hodoscopes of the AMS-02 = Determines particle time of flight (TOF) and velocity"]
-[5.418380260467529, 2.0311038494110107, "[FF] Mission Objectives of the SOHLA-1 = Completed"]
-[5.129791259765625, 6.955790042877197, "[TT] Downlink Data Rate of the LDCM = 384 Mbit/s"]
-[5.194345951080322, 2.276653289794922, "[TT] Support Mission of the CRISTA/MAHRSI = STS-85"]
-[10.806272506713867, 2.091418504714966, "[TT] Operation Time of the XMM-Newton observatory = More than 15 years"]
-[6.713346004486084, 3.3479115962982178, "[FF] Concept Interest of the Satellite Constellation = High"]
-[10.27033805847168, 5.434548854827881, "[FF] Battery Thermal Regulating System of the Neutron-1 = Active internal system with a sensor, heater, and controller"]
-[7.3874359130859375, 2.899935007095337, "[FF] Purpose of the MethaneSAT = Assess methane emissions at every stage in the U.S. oil and gas supply chain"]
-[8.892879486083984, 7.163829803466797, "[TT] Imagery Resolution of the AlSat-2A = High-resolution"]
-[8.878215789794922, 5.5528564453125, "[TT] Pointing Accuracy of the FormoSat-2 = < 0.7 km (0.12\u00ba)"]
-[5.144557476043701, 1.3348910808563232, "[FF] Conference Date of the GIOVE-B = Sept. 22-25, 2009"]
-[7.006170749664307, 4.360325813293457, "[FF] Unknown of the SEM = Unknown"]
-[11.726153373718262, 3.2761573791503906, "[TT] Propulsion of the Spacecraft = Slanted N2H4 monopropellant thrusters"]
-[6.622997283935547, 1.723308801651001, "[FF] URL of the Entice = https://www.entice-project.eu/"]
-[10.209141731262207, 7.952101230621338, "[TT] Separation of the Telescope = 1.75 mm"]
-[8.284071922302246, 8.611144065856934, "[TT] Spectral Resolution of the CO2Image = 1.0 nm - 1.3 nm"]
-[10.285111427307129, 5.752006530761719, "[TT] Operating Temperature of the CCD = -10\u00baC"]
-[11.729470252990723, 5.447985649108887, "[TT] Instrument Module Length of the Resurs-P1 = About 1 m"]
-[3.229743003845215, 5.007936477661133, "[TT] Swath Width of the SAR = 100 km"]
-[9.930789947509766, 4.455949306488037, "[TT] Attitude Control Subsystem (ACS) of the S/C = Magnetorquer coils & cold gas thruster"]
-[13.688769340515137, 3.0338525772094727, "[TT] Total Mass of the Secondary Payloads = 243 kg"]
-[14.26550579071045, 3.056276321411133, "[TT] Mass of the Deimos-2 = 300 kg"]
-[7.714113235473633, 8.696868896484375, "[TT] Filter Spectral Bands of the EXI instrument = UV1: 245-275 nm, UV2: 305-335 nm Blue: 427-447 nm, Green: 536-556 nm, Red: 625-645 nm"]
-[5.476861000061035, 6.116835594177246, "[TT] RAM of the OBC = 2MByte payload data"]
-[5.383973121643066, 3.9307825565338135, "[TT] Number of Satellites of the Unseenlabs constellation = Between 20 and 25 by 2025"]
-[3.8051233291625977, 1.1711875200271606, "[TT] First Stage Flights of the Falcon 9 = 7"]
-[4.333406448364258, 4.138382434844971, "[FF] Introduction of the SARP-3 = On the MetOp-A spacecraft of EUMETSAT (launch October 19, 2006)"]
-[8.175436973571777, 0.02029244601726532, "[TT] Mission Duration of the TOPEX/Poseidon = 13 years"]
-[10.480260848999023, 6.624816417694092, "[TT] Number of Mirror Systems of the Mirror System = 7"]
-[9.768360137939453, 6.265079021453857, "[FF] Final Alignment Step of the Webb = Adjust any small, residual positioning errors in the mirror segments"]
-[8.832415580749512, 2.2595648765563965, "[TT] Interstellar Dust Measurement Period of the Ulysses = 16 years"]
-[5.819039821624756, 4.854434490203857, "[FF] Function of the RLS = Provide the user in distress with a confirmation that its call for help has been received and that aid is underway"]
-[9.398695945739746, 7.208138942718506, "[FF] Spatial Resolution of the FY-4A = LWIR/S/MWIR : 16 km, VIS : 2 km"]
-[8.340150833129883, 7.192473411560059, "[TT] Stability of Measurement of the IMG = <0.1K"]
-[9.507479667663574, 6.171887397766113, "[TT] Incidence Angle Range of the Wide Multi-Look Fine Mode = 29-50\u00ba"]
-[4.401736736297607, 1.5368555784225464, "[FF] Image Credit of the ROCSat-2 = NSPO"]
-[7.028896808624268, 8.320745468139648, "[TT] SNR of the CZI = 2.46-4.57"]
-[7.080522060394287, -0.6938246488571167, "[TT] Nodal Period of the Fast-sampling orbit = 6131.25 s"]
-[9.734550476074219, -0.5726723074913025, "[TT] Orbit Altitude of the ISS = 405km"]
-[4.42581844329834, 7.7859110832214355, "[TT] Frequency of the Ka-band payload = 30 GHz (receive) and 20 GHz (transmit)"]
-[13.857155799865723, 5.692135810852051, "[TT] Solar Panel Conversion Efficiency of the EPS = 26.8%"]
-[9.748170852661133, 8.549321174621582, "[TT] IFOV (Instantaneous Field of View) of the Instrument = 0.0058\u00ba or 0.0029\u00ba"]
-[7.694283962249756, 9.399901390075684, "[TT] Center Wavelength of the Band 12 = 9.61 \u00b5m"]
-[3.22737979888916, 5.001333713531494, "[TT] Spatial Resolution of the SAR = 5-30 m"]
-[6.608701705932617, 1.9275741577148438, "[TT] URL of the CATS = http://cats.gsfc.nasa.gov/index.html"]
-[9.00645923614502, 4.865182399749756, "[TT] Internal Sensor of the Honeywell QA-2000 Accelerometer = Temperature sensor"]
-[10.11008358001709, -1.4777934551239014, "[TT] Inclination of the Harmony satellites = 98.19\u00b0"]
-[4.545228481292725, 0.4854396879673004, "[TT] Cooperation Agreement Date of the Astroscale UK = December 2018"]
-[7.055820465087891, -0.5324656367301941, "[TT] Observation Duration of the SPARCS = 1 to 3 stellar rotations"]
-[10.946172714233398, 7.593900203704834, "[TT] Swath Width of the AMSU-A = About 2000 km"]
-[9.393011093139648, 5.358865737915039, "[TT] Mounting of the LAD = Rotating actuator platform"]
-[10.000616073608398, 8.07622241973877, "[TT] Volume of the Optics volume = 180 mm diameter x 530 mm"]
-[8.978461265563965, 4.40142822265625, "[FF] Attitude Determination of the MPID = Data from the coarse sun sensors is used to help determine attitude of the spacecraft"]
-[14.082436561584473, 4.003551959991455, "[TT] Mass of the Instrument = < 10 kg"]
-[6.742986679077148, -0.4250468313694, "[TT] Nodal Period of the Satellite = 100.8 minutes"]
-[6.379944801330566, 3.452047348022461, "[FF] Testing Purpose of the Flying Laptop = New technologies and scientific Earth observation"]
-[5.8618927001953125, 1.8711473941802979, "[FF] Presentation Date of the SLS-Orion Missions = Oct.12-16, 2015"]
-[11.849047660827637, 0.005729130934923887, "[FF] Discovery of the TESS = Transiting Super-Earth in the pi Mensae System"]
-[8.460601806640625, 5.807504177093506, "[TT] Fine Localization Accuracy of the LLMS/IRIS = <1 km"]
-[8.161117553710938, 8.23563289642334, "[TT] Spectral Range of the TrueColour Imager = 433 nm - 907 nm"]
-[3.183711528778076, 1.6911866664886475, "[TT] Data Stream Availability of the Sentinel-6 = A couple of days after collection"]
-[5.538522720336914, 0.11819721013307571, "[TT] Last Command Date of the Ulysses = June 30, 2009"]
-[7.460237503051758, 2.0762171745300293, "[FF] Vegetation of the Tuscany = Lush green"]
-[5.103729724884033, 3.1431262493133545, "[TT] Developer of the Transponder = Italian company IDS"]
-[9.724920272827148, -0.17963959276676178, "[TT] Altitude of the Tsubame satellite = 271.5 km"]
-[10.324031829833984, 3.169128656387329, "[TT] Mechanism Failure Rate of the CubeSats = Less than 10%"]
-[8.024859428405762, 5.969760417938232, "[FF] URL of the Miniature Integrated Camera and Imaging Spectrometer = http://nmp.nasa.gov/ds1/tech/micas.html"]
-[3.7873313426971436, 6.440247535705566, "[TT] Type of the Antenna subsystem = Fixed offset system with three beams"]
-[9.843574523925781, 3.953472137451172, "[TT] Solar Panel Orientation of the STRaND-1 nanosatellite = +Y body direction"]
-[10.215814590454102, 7.557685375213623, "[TT] Telescope Type of the CaSSIS = Three-mirror off-axis telescope with an additional slightly powered folding mirror"]
-[7.388252258300781, 4.235777378082275, "[FF] Rendezvous Demonstration of the ETS-VII = Robotic rendezvous using chaser and target satellites"]
-[13.85677719116211, 6.8528618812561035, "[TT] Maximum Voltage of the LEO = 200 V"]
-[10.265473365783691, 0.9707778692245483, "[TT] Distance from Earth of the Kepler-1649c = 300 light-years"]
-[6.210445404052734, 4.502737998962402, "[FF] Key Features of the Flight Operations Segment = Re-use the AIV system in operations, Limited number of satellite contacts, Autonomous contact execution, Fast data distribution after a satellite contact, Automated handling of scientific requests (nominal and calibrations), Direct data distribution from the DRS (Data Reception Station) to the SOC, Limited number of routine tasks for the operators"]
-[3.975416898727417, 6.424320697784424, "[TT] Antenna Type of the Spacecraft = Steerable medium gain antenna"]
-[7.168563365936279, 2.5294089317321777, "[FF] Publisher of the Observation of the Earth and Its Environment = Herbert J. Kramer"]
-[5.954627513885498, 6.003195285797119, "[TT] Number of Active Modules (Flash) of the Memory Modules = 2"]
-[4.753048419952393, 7.244480609893799, "[TT] Ka-Band Link of the Corvus-BC = 170 Mbps"]
-[9.725934982299805, 6.204202175140381, "[FF] Issue of the Dynamic Alignment System = Slippage when the moving mirror vibrated"]
-[7.499435901641846, -0.17038150131702423, "[TT] Touchdown Time of the Philae = 17:25:26 GMT"]
-[11.165801048278809, 5.127795219421387, "[TT] Diameter of the Sensor Module = 25.4 cm"]
-[5.646645545959473, 3.689455270767212, "[TT] Number of Maneuvers of the SkySat-3 = 13"]
-[9.183547973632812, -0.3486919701099396, "[TT] Apogee of the Deimos-1 = 680 km"]
-[8.982666969299316, 7.662001132965088, "[TT] Seeing Diameter of the Acquisition and Tracking Camera (ATC) = 1 arcsec = 65 \u00b5m"]
-[11.352320671081543, 2.7793729305267334, "[TT] Service System Mass of the Microsatellite = 18.2 kg"]
-[5.573866367340088, 0.06432978063821793, "[TT] Operation Period of the MAG = January 2012 to May 2014"]
-[8.990779876708984, 8.028339385986328, "[TT] CCD Lines of the FPM (Focal Plane Module) = 3 linear CCD lines"]
-[9.707462310791016, 8.362822532653809, "[TT] Field of View of the XRD = 3% sky"]
-[4.645686626434326, 4.453244209289551, "[TT] Spatial Resolution of the DubaiSat-1 = 2.5 m (Pan), 5 m (MS)"]
-[10.110591888427734, 5.722212791442871, "[TT] Operation of the ISIR = Infrared imaging without external cooling"]
-[8.040738105773926, 5.537660121917725, "[FF] Function of the Intelligent pointing function = Detects cloud-free areas and repoints scanner in real time"]
-[13.447555541992188, 6.636274337768555, "[TT] Solar Array Capacity of the KOMPSAT-6 = 2.250 kW"]
-[11.2314453125, 1.0476833581924438, "[FF] Test of the LISA Pathfinder = Acoustic test"]
-[9.446765899658203, -1.1711244583129883, "[TT] Direction of the FWD = From GEO to the LEO user"]
-[10.29849910736084, 5.384599208831787, "[TT] Orbit Control and Maintenance of the Spacecraft = TCS (Thermal Control Subsystem)"]
-[4.9912214279174805, 0.701088547706604, "[TT] Deployment Date of the MicroMAS-1 = March 4, 2015"]
-[8.722925186157227, -0.6885701417922974, "[TT] Resolution of the ICEYE = 25 cm"]
-[11.821120262145996, 3.256991147994995, "[TT] Engine Thrust of the Change'4 = 7500 N"]
-[8.520017623901367, 7.64075231552124, "[TT] Pixel Count of the Kruiz CCD = 1024 x 128"]
-[6.9566192626953125, 3.5605785846710205, "[FF] Concept Presentation of the ALTIKA = Unknown"]
-[4.87653112411499, 4.282462120056152, "[FF] Alias of the ARGOS-4 = Advanced Data Collection System (ADCS-4)"]
-[7.6591410636901855, 1.886062741279602, "[FF] Carbon Source of the Tropical Forests = True"]
-[8.731193542480469, 7.041238784790039, "[TT] Swath of the WV60 imager = 17.9 km"]
-[10.104371070861816, -0.10961414128541946, "[TT] Height of the Block 5 Satellite = 122 cm"]
-[3.790294885635376, 4.309614658355713, "[FF] Measurement category of the SAR (RISAT) = Multi-purpose imagery (land), Vegetation, Albedo and reflectance, Ocean topography/currents, Sea ice cover, edge and thickness, Soil moisture, Snow cover, edge and depth, Ice sheet topography"]
-[6.3205084800720215, 6.874213695526123, "[FF] Technology Demonstration Boards of the AEEF = SIOS (Sistema de Interconexiones \u00d3pticas para Sat\u00e9lites) optical link demonstration board and one GaN (Gallium Nitride) board"]
-[11.538637161254883, 6.666380405426025, "[TT] Range of the LET Range = 0.2 - 7 MeV/\u00b5m"]
-[9.599167823791504, 7.188085556030273, "[TT] Spatial Resolution of the Instrument = 8 m"]
-[4.8489274978637695, 7.327491760253906, "[TT] Nominal Downlink Data Rate of the RF communications = 5 kbit/s"]
-[6.838017463684082, 3.0148067474365234, "[FF] Impact of Satellite Constellations of the ESO Telescopes = Not specified"]
-[5.588016033172607, 6.321715831756592, "[TT] Manufacturer of the Data Storage System = RUAG Space"]
-[3.8591244220733643, 4.600905418395996, "[TT] Antenna Pattern Measurement of the RISAT-1 = During IOT (In-Orbit Test)"]
-[8.963875770568848, 5.657627582550049, "[TT] Pointing Accuracy of the TRACE = 20 arcseconds"]
-[7.174031734466553, 2.534111261367798, "[TT] Publisher of the Observation of the Earth and Its Environment: Survey of Missions and Sensors = Springer Verlag"]
-[10.744110107421875, 0.9864490628242493, "[TT] Mass of the TOI-2337b, TOI-4329b, and TOI-2669b = Between 0.5 and 1.7 times Jupiter\u2019s mass"]
-[8.214078903198242, 3.330657958984375, "[TT] Measurement Category of the OCO-3 = Trace gases (excluding ozone)"]
-[7.698580741882324, 5.379937648773193, "[FF] Usage of the Vision Aiding or Terrain Sensor = Landing phase"]
-[8.791155815124512, 5.469611644744873, "[TT] Navigation Accuracy of the Spacecraft = 60 m"]
-[6.75498104095459, 0.6275460124015808, "[FF] Launch Date of the Kepler Mission = March 7, 2009"]
-[10.399629592895508, 2.8487470149993896, "[FF] Publication Date of the Galassia Nanosatellite = 31 May 2016"]
-[10.25327205657959, 5.323735237121582, "[FF] Attachment Method of the Thermal Control System = Off the side of AMS and plug it into the existing system"]
-[8.509663581848145, 1.3604413270950317, "[FF] Purpose of the Aquarius = Monitor ocean salinity features"]
-[7.958471298217773, 4.70247220993042, "[FF] Components of the ODM (OPTOS Dose Monitoring) System = Two on-board units, commercial RadFETs, thermistor"]
-[6.158096790313721, 5.092338562011719, "[FF] Functionality of the Core-DHS = Same level as heritage equivalent avionics stack"]
-[4.899004936218262, 6.253638744354248, "[TT] Protocol of the RF communications = AX.25 packet protocol"]
-[7.21117639541626, 4.366301536560059, "[FF] Transfer Parameters of the LUMIO = Cj = 3.09"]
-[7.93277645111084, -0.980323076248169, "[FF] Data Collection of the ICESat-2's instrument = Tracks of ICESat-2 measurements from 2019"]
-[11.591755867004395, 4.734403133392334, "[TT] Structure of the Lander = Truncated pyramid around a cylinder"]
-[5.759415149688721, 3.1133363246917725, "[TT] Development Cost of the SAOCOM-1A = $500 million"]
-[9.385193824768066, 4.795811176300049, "[FF] Design Tolerance of the D3 = The alignment of the motor with the spacecraft's center of gravity resulted to be outside the designed tolerance"]
-[8.679849624633789, 7.647727966308594, "[TT] Resolution of the CCD = 512 x 2048 image pixels"]
-[10.22419261932373, 8.4242525100708, "[TT] Diameter of the Pupil = 50 mm"]
-[8.043362617492676, 0.6098385453224182, "[FF] Closure Status of the North and northeast entrances to Yellowstone National Park = Closed indefinitely"]
-[4.630143642425537, 0.26056742668151855, "[FF] Launch Date of the AstroSat = Unknown"]
-[5.563345432281494, 5.928528308868408, "[TT] Usage of the SSH and SCP = Successful"]
-[4.540685653686523, 7.872048854827881, "[TT] Frequency of the RF communications = 437.27 MHz"]
-[5.244704246520996, 4.894421577453613, "[TT] Pass Duration of the Ground Stations = 2.5 hours"]
-[9.075713157653809, 2.867867946624756, "[FF] Publication Date of the Solar XUV grazing incidence spectrograph = April 1977"]
-[12.93188762664795, 6.996088027954102, "[TT] Attitude Control Power Requirement of the WCOM = 70 W"]
-[6.417240619659424, 5.564328670501709, "[FF] Operation of the OGS = Ground segment laser communication experiment of SOTA/SOCRATES mission"]
-[9.392881393432617, -0.3162136971950531, "[TT] Perigee of the FASat-Alfa = 651 km"]
-[5.725878715515137, 2.7564196586608887, "[FF] Program Manager of the DSX = Jeffrey Christmas"]
-[12.111626625061035, 0.5794283151626587, "[FF] Purpose of the PLATO = Provide precise characteristics of thousands of exoplanet systems"]
-[7.497890472412109, 5.486948013305664, "[FF] Angular Speed of the Polar Scout = Higher at high elevation angles"]
-[4.559054851531982, 6.082150936126709, "[TT] Morse Code Beacon Frequency of the OSSI-1 = 145.980 MHz"]
-[4.647877216339111, 1.5440579652786255, "[TT] Launch Date of the GCOM-W1 = May 17, 2012"]
-[4.815622329711914, 7.401808738708496, "[TT] Downlink Data Rate of the RF communications = 9.6 kbit/s"]
-[6.437429904937744, 2.307605028152466, "[FF] Unknown of the eROSITA = Unknown"]
-[12.540133476257324, 7.486771106719971, "[TT] Power Consumption of the Imager = 85 W"]
-[7.529759883880615, 1.043110728263855, "[FF] Purpose of the Ground-Penetrating Radar = Scan subsurface layers of the Martian crust in search of water ice deposits"]
-[11.592698097229004, 4.325832366943359, "[TT] Fairing Envelope Requirement of the TacSat-4 = Must fit within the fairing envelope of the Minotaur IV launch vehicle"]
-[7.611627101898193, 3.3976364135742188, "[TT] Debris Shield Exposure of the AMS-02 = Eight years"]
-[14.171360969543457, 3.115983486175537, "[TT] Mass of the CALET = 650 kg"]
-[7.510025978088379, 6.995633125305176, "[TT] Typical cadence of the FSI dual EUV 174 \u00c5 and 304 \u00c5 alternatively = 600 s"]
-[10.751327514648438, -1.1564244031906128, "[TT] Altitude of the SLATS = 393 km"]
-[7.437724590301514, 2.930269718170166, "[TT] Annual Methane Release of the Kayrros Studies = 20 megatons"]
-[8.22553825378418, 2.8162825107574463, "[TT] Measurement Domain of the LAICE = Atmosphere"]
-[6.967919826507568, 6.529480457305908, "[FF] Data Transmission of the GLM = Near real-time"]
-[5.782917499542236, 3.3595433235168457, "[TT] Total Addressable Market of the Satellogic = $140 billion"]
-[8.929647445678711, 7.781616687774658, "[TT] Focal Length of the 4-band CCD Imager = 32 mm"]
-[9.13107681274414, 7.2849884033203125, "[TT] Pixel-Binning Spatial Resolution of the EyeSat = 0.5\u00b0-2\u00b0"]
-[8.448098182678223, 0.7183899879455566, "[TT] Utilization of the ICI-5 = Cloud ice effective radius"]
-[4.828970432281494, 0.7578325867652893, "[TT] Launch Year of the OCO-2 = 2014"]
-[4.195820331573486, 0.9660659432411194, "[FF] Launch Date of the H-IIB Launch Vehicle No. 3 = July 21, 2012"]
-[5.0324883460998535, 1.254616379737854, "[TT] Launch Year of the Suomi NPP = 2011"]
-[8.839309692382812, 4.5252156257629395, "[FF] Pointing Method of the ASTRO-1 UV payload = Shuttle maneuvers and slews of the IPS"]
-[9.50127124786377, 5.020841121673584, "[TT] Spin Axis Tilt Angle of the Cluster spacecraft = 45\u00ba"]
-[7.939647197723389, 3.125232458114624, "[FF] Measurement Uncertainty of the CO2 = Unknown"]
-[4.935817718505859, 5.336862564086914, "[TT] Antenna of the Phoenix GPS Receivers = L1/L2 antenna"]
-[14.298179626464844, 3.0376200675964355, "[TT] Mass of the UniSat-4 = 10 kg"]
-[5.285780429840088, 2.0104868412017822, "[TT] Mission Status of the Vesselsat-1 & -2 = Completed"]
-[5.945577144622803, 6.264122009277344, "[TT] Data Transfer Time of the Ground Station = About 2 minutes per day"]
-[6.355207443237305, 7.3357062339782715, "[TT] Output Signal of the THD = Analog signal"]
-[8.770364761352539, 4.488811016082764, "[FF] Sensor Suite of the NEMO-AM = SFL sun sensors, SFL magnetometer, SI star tracker"]
-[3.1232895851135254, 2.2364675998687744, "[FF] Data Comparison of the HyperScout\u00ae = Copernicus data, in-situ ground truth measurements and an airborne campaign"]
-[10.0120210647583, 1.2738450765609741, "[TT] Drift Time of the Galaxy-15 = Almost a year"]
-[10.35026741027832, 2.0602145195007324, "[FF] Purpose of the NuSTAR = Detects high-energy X-ray light and studies some of the most energetic objects and processes in the universe"]
-[9.863926887512207, 8.75329303741455, "[TT] IFOV of the HgCdTe = 170 \u00b5rad"]
-[7.599432468414307, -0.36334913969039917, "[FF] Funding of the IceCube = Co-funded by ESTO (Earth Science Technology Office)"]
-[12.140179634094238, 6.157659530639648, "[TT] Events Collected of the AMS-02 = 60 billion"]
-[8.23858642578125, 7.505614757537842, "[TT] Detector of the Instrument = E2V CCD67"]
-[6.461579322814941, 0.023945126682519913, "[TT] Temporal Resolution of the Next Generation Gravity Constellation = Three and ten day solutions"]
-[13.728008270263672, 5.402747631072998, "[TT] Solar Panel Type of the EPS = Triple-junction solar cells"]
-[11.186173439025879, 0.6634224653244019, "[FF] Photometric Precision of the CHEOPS = Similar to the Kepler mission of NASA"]
-[7.620288372039795, 8.927682876586914, "[TT] Polarization Angle of the Band 2 = 0/60/120 \u00ba"]
-[6.18604040145874, 4.3500800132751465, "[FF] Delivery of the CSG GS = Responsible for the delivery to the final user"]
-[9.235429763793945, 1.8712247610092163, "[FF] Project Role of the HTA (Harpoon Target Assembly) = HTA payload development"]
-[8.074652671813965, -0.9337015748023987, "[FF] Objectives of the ICE-Cap = Demonstrate a cross-link from LEO to MUOS WCDMA in GEO"]
-[2.3282485008239746, 1.3128504753112793, "[FF] Article Publication of the NanoSail-D = October 2008"]
-[8.815014839172363, 1.8935763835906982, "[TT] Speed of the Easterly Winds = 0 to 2.5 m/s"]
-[12.182245254516602, -0.24771644175052643, "[TT] Image Capture Time of the TESS = Over the course of 17 hours on July 25"]
-[3.07504940032959, 2.355149507522583, "[TT] Spectral Bands of the Sentinel-2C = 13"]
-[8.261064529418945, 7.335602760314941, "[TT] Carries of the LilacSat-1 = INMS (Ion-Neutral Mass Spectrometer)"]
-[5.652279853820801, 3.181837797164917, "[FF] Value of the Agreement with ABDAS = $38 million"]
-[8.07375431060791, 0.7687913775444031, "[FF] Composition of the Fortescue Group = Volcanic and sedimentary rocks"]
-[9.260175704956055, -1.0880717039108276, "[TT] Orbit Altitude of the EDRS-C = 36,000 km"]
-[8.779296875, -0.3919264078140259, "[TT] Period (min) of the Intercosmos- Bulgaria 1300 (Intercosmos-22) = 101.9"]
-[10.954158782958984, 7.577633857727051, "[TT] Swath Width (Individual) of the HRV = 60 km"]
-[5.519152641296387, 6.828896999359131, "[TT] Data Transmission Speed of the European Data Relay System (EDRS) = 1.8 Gbit/s"]
-[4.8910136222839355, 2.929126501083374, "[TT] Location of the Weather Satellite = Lockheed Martin facility near Moffett Field in Sunnyvale, California"]
-[4.756274700164795, -1.8373773097991943, "[TT] Landing Date of the Chang'e-4 = January of this year"]
-[12.37802791595459, 0.5751057863235474, "[FF] Mission Operation of the PLATO = URL: http://www.oact.inaf.it/plato/PPLC/ScientificProgramTao_files/2014-12-03Gondoin.pdf"]
-[5.492983818054199, 5.090712547302246, "[TT] Interface of the MuREM = CAN bus"]
-[13.31207275390625, 2.946042537689209, "[TT] Mass of the Inmarsat S \u2013 Europasat / Hellas-Sat 3 = About 5.8 tons"]
-[10.073392868041992, 1.9140989780426025, "[FF] Launch Date of the Chandrayaan-1 = Oct. 22, 2008"]
-[8.509511947631836, 5.435928821563721, "[TT] Position Fix Availability of the Transit Navigation = Every 35 to 100 minutes"]
-[11.46883773803711, 5.104246139526367, "[TT] Size Requirement of the ETB sub-experiment = Fitting within 17.6 cm2"]
-[6.985767841339111, 2.5174474716186523, "[FF] Role of the Martin Popek = Passionate about capturing sprites, jets and elves on camera"]
-[3.577263593673706, 6.486011028289795, "[FF] Antenna Size of the Altimetry Instrument = 1.2 m"]
-[6.0511884689331055, 3.9212887287139893, "[FF] Avionics of the AstroSat-250 = Astrium AS250 new generation avionics"]
-[8.494393348693848, 5.373080253601074, "[FF] Rigidity Resolution of the STD = Unknown"]
-[7.443091869354248, 5.783198833465576, "[FF] Vibration Robustness of the FPA = Guaranteed"]
-[4.9679975509643555, 3.3994905948638916, "[TT] Purchase of the THEMIS = Alliant Techsystems Inc. (ATK)"]
-[7.0889434814453125, 2.245070457458496, "[TT] Structure Designer of the Biomass = OHB in Italy"]
-[8.223801612854004, 8.232185363769531, "[TT] Spectral Range of the Panchromatic Imager = 400 to 900 nanometers"]
-[7.9216203689575195, 3.760345935821533, "[FF] Ephemeris Source of the Prometheus Block 1 = Ground-based tracking and TLE sets provided by JSpOC"]
-[3.854405641555786, 6.5964436531066895, "[TT] F/D of the Antenna = 0.8"]
-[5.207878112792969, 1.2255184650421143, "[FF] Status Presentation Date of the SMOS = Nov. 18-20, 2009"]
-[11.14396858215332, 5.157217979431152, "[TT] Yield Strength of the LARES-2 = > 500 MPa"]
-[13.79207706451416, 2.8244311809539795, "[TT] Total Mass of the Spacecraft = 600 kg"]
-[4.412354469299316, 0.9823595285415649, "[TT] Launch Date of the IRNSS-1E = January 20, 2016"]
-[9.234997749328613, 6.639148235321045, "[FF] Purpose of the ALMA = High-resolution observations"]
-[7.093302249908447, 6.7504119873046875, "[TT] Light Source Unit of the FIBOS = Pigtailed tunable laser"]
-[5.294356822967529, 1.0118606090545654, "[TT] Test Phase Start Date of the IASI-NG = Early 2021"]
-[8.834548950195312, 4.716259479522705, "[TT] Attitude Update Mode Rate of the Star Tracker = 1.7 Hz"]
-[2.0476460456848145, -0.3128494322299957, "[FF] Radiation Belt Remediation (RBR) effort Leader of the DSX spacecraft = Dr. Michael Starks"]
-[8.929116249084473, 4.002574920654297, "[FF] MZ-Surface Function of the H3 and H4 = Faces to the sun"]
-[6.827054977416992, 3.146481990814209, "[FF] Integration Objective of the NPOESS = Integrate separate meteorological programs into a single program"]
-[13.811772346496582, 6.866372585296631, "[TT] Capacity of the Energy Storage System = 70 AH"]
-[5.564120292663574, 4.853325843811035, "[FF] Future Enhancements of the EDSN = Implementation of an ACK/NACK system, or via delay tolerant networks"]
-[6.154603481292725, 0.2522449493408203, "[FF] Resilience Strategy of the Dellingr = 25-hour reset"]
-[5.39800500869751, 6.9261155128479, "[TT] Data Download Rate of the Second generation spacecraft UK-DMC-2 and Deimos-1 = Up to 80 Mbit/s"]
-[8.662189483642578, 0.5309698581695557, "[TT] Tree Height of the Pongara National Park = Up to 60 meters"]
-[14.642465591430664, 6.7086873054504395, "[TT] Capacity of the NiCd Cells = 46 Whr"]
-[8.676146507263184, 3.4890379905700684, "[FF] Objective of the SREM = To map the radiation environment of GTO with high temporal and spatial resolution at post-solar minimum conditions"]
-[7.005181789398193, 7.0342183113098145, "[TT] Power of the Acquisition/Tracking Lasers = 100 mW"]
-[8.975778579711914, 2.7073588371276855, "[FF] Mission Purpose of the ASTRO-H = Give us a new view of the non-thermal processes taking place in the universe"]
-[8.214850425720215, 8.479146957397461, "[FF] Critical Parameter of the Primary Objective = Micro-roughness of each surface"]
-[5.962721347808838, 0.8965670466423035, "[TT] Image Capture Date of the MSG-3 = April 22, 2015"]
-[8.360559463500977, 7.613455295562744, "[TT] Detector Array of the PAN Band = Dual array of 12,000 charge coupled device (CCD) detectors"]
-[3.0643651485443115, 2.1208245754241943, "[TT] Announcement Date of the Copernicus = December 11, 2012"]
-[8.339516639709473, 6.037353992462158, "[TT] Overall Relative Measurement Error of Radiance in Bands 1-3 of the Scanning geometry = 10%"]
-[8.136319160461426, 7.55217981338501, "[FF] Signal of the Photomultiplier = Few tenths of a \u00b5W/m2"]
-[7.092811107635498, 6.200305938720703, "[TT] BCP Distribution Interval of the INTEGRAL = Every 8 s"]
-[3.931368350982666, 0.1978093683719635, "[TT] Launch Date of the SMART-1 = September 27, 2003"]
-[8.676058769226074, 8.64211368560791, "[TT] Pixels per FWHM of the Spectrometer = 1420"]
-[8.108015060424805, 8.63282585144043, "[TT] Full Bands Range of the Spectrometer = 550-1000 nm"]
-[5.911206245422363, 1.531003713607788, "[FF] Separation Date of the PRISMA Satellites = August 12, 2010"]
-[8.11933422088623, 8.344621658325195, "[TT] Imager Ranges of the HySIS = Visible Near Infrared (VNIR) range and the other in the Shortwave Infared (SWIR) range"]
-[8.274263381958008, 2.8999624252319336, "[TT] Missed Lightning in Northern Hemisphere of the ISS-LIS = Nearly all of that lightning"]
-[5.75236177444458, 0.6954424381256104, "[FF] Exploration Start Date of the Cluster = July 1, 2015"]
-[6.485747337341309, 4.46090030670166, "[FF] Unknown of the Multiple-Payload Processing System = Unknown"]
-[10.184804916381836, 2.800478219985962, "[TT] Qualification Nanosat Quantity of the SMDC-ONE program = 1"]
-[5.8182172775268555, 5.340567111968994, "[TT] Type of the ASCE = Advanced"]
-[6.411568641662598, -0.6575708389282227, "[TT] Revisit Period of the TanSat = Shorter than 16 days"]
-[9.605664253234863, -0.5481671690940857, "[TT] GEO Altitude of the INSAT-3D = 35,786 km"]
-[10.350489616394043, 3.19783616065979, "[TT] TRL of the CubeSat = 7"]
-[4.821664333343506, 0.5767095685005188, "[TT] Launch Date of the Resurs-P2 = December 2014"]
-[5.996003150939941, 4.728198051452637, "[FF] Fine Tuning Frequency of the AI Apps = As often as necessary during the visibilities over the ground stations"]
-[5.964583873748779, 7.1567254066467285, "[TT] Source Data Rate of the Instrument = 200 bit/s"]
-[11.994105339050293, 4.54158353805542, "[TT] Radius of the Spacecraft = 21 cm"]
-[6.208302021026611, 4.383162975311279, "[FF] Task of the OPS&GRND = Automate as much work as possible to simplify the future operation of the satellite"]
-[5.602926254272461, -2.0313682556152344, "[FF] Imaging Objective of the KOMPSAT-1 = Provide high-resolution imagery of the Korean Peninsula"]
-[6.3580522537231445, 0.16516652703285217, "[FF] Achievements of the Skylab = Unknown"]
-[6.346686363220215, 2.0545494556427, "[FF] URL of the RADARSAT Constellation Mission = http://eofsac.org/sites/default/files/2018-02/McNairn%20Delisle%20RADARSAT%20Constellation_0.pdf"]
-[6.188154220581055, 8.600444793701172, "[TT] Polarized Signals of the T/R Module = V and H"]
-[5.3872175216674805, 0.49385595321655273, "[TT] Launch Date of the Alba Cluster 3 = Q2 2021"]
-[10.280344009399414, 2.134551763534546, "[TT] Resolution of High-Energy X-ray Background of the Chandra mission = 2 percent to 35 percent"]
-[9.664444923400879, -0.7122809290885925, "[TT] Orbital Altitude of the IceCube = Approximately 400 km"]
-[14.314580917358398, 3.2462480068206787, "[TT] Mass of the LIMS = 68.4 kg"]
-[6.316845893859863, 5.217144966125488, "[FF] Malfunction of the OBC = None"]
-[5.999788284301758, 4.957837104797363, "[TT] Function of the OCL = In-flight reprogrammable procedures"]
-[7.314512252807617, 2.610630989074707, "[FF] Data Requirements of the EOS-C = Disaster and emergency response, environment, mapping, urban planning, landcover, geology, coastal zone monitoring, ecosystem, and water resource management"]
-[8.997785568237305, 4.520294189453125, "[TT] Quantity of the Sun Sensors = 2"]
-[11.489094734191895, 6.337201118469238, "[TT] Energy Output of the Pulsar = About 10 million suns"]
-[4.971188545227051, 0.4414668083190918, "[TT] Birth Date of the Verner Suomi = 1915"]
-[3.728501319885254, 4.15102481842041, "[FF] Agreement Date of the SAR Satellite Imagery = 17 December 2018"]
-[8.636907577514648, 7.823678493499756, "[TT] Average Power of the LWIR Camera = 13 W"]
-[6.772512435913086, 6.138305187225342, "[FF] Processing Time for One Snapshot Scene of the EO System = Unknown"]
-[10.43417739868164, 2.963951349258423, "[TT] Radio Performance of the CanX-2 = Unprecedented for an operational nanosatellite"]
-[4.010726451873779, 7.834233283996582, "[FF] Modulation Schemes of the Transponder = PCM/PSK/PM, PSK"]
-[11.79939079284668, 6.763668537139893, "[TT] Effective Energy Range of the Instrument Suite = 2 keV to 1 MeV"]
-[4.274733543395996, 7.135459899902344, "[TT] TT&C Transmission of the PRISMA = S-band"]
-[6.244145393371582, 1.413808822631836, "[TT] First Look Date of the eROSITA = 22 October 2019"]
-[3.792848825454712, 4.704707145690918, "[TT] Azimuth Resolution of the RADARSAT-2 = Stable"]
-[8.091036796569824, -0.694035530090332, "[TT] Measure Area Frequency of the CryoSat-2 = More frequent than ICESat-2"]
-[2.962800979614258, 4.431032657623291, "[TT] Ground Resolution (ScanSAR mode) of the XSAR = Varying between 8 m and 20 m"]
-[8.161663055419922, 1.1779507398605347, "[FF] Level-3 Data Reprocessing of the SMAP (Soil Moisture Active Passive) = From March 31, 2015 to Sept. 9, 2015"]
-[10.485564231872559, 5.71871280670166, "[TT] Temperature Range of the Juice = -180\u00baC to 250\u00baC"]
-[6.113216876983643, -0.05024619400501251, "[TT] Expected Data Transmission of the GRIFEX = Many months"]
-[7.3315935134887695, 4.349442958831787, "[FF] Calibration of the Suomi NPP VIIRS = Unknown"]
-[8.627077102661133, 5.542185306549072, "[TT] Linear Velocity Error of the GPSR = 1 m/s (1\u03c3)"]
-[8.934210777282715, 2.7777466773986816, "[FF] Observation Result of the Integral = Unexpectedly strong auroras illuminating the Earth"]
-[7.690726280212402, 2.6134419441223145, "[FF] Earth Observation Applications of the Aurora = Energy, mining and defence sectors, oil and gas pipeline monitoring, methane mapping, clean-energy resource exploration, sustainable mining practices and wildfire risk mitigation"]
-[5.5570902824401855, 5.239206314086914, "[FF] Services of the EuTEF = Delivers EuTEF downlinked TM Data to EuTEF Ground Segment"]
-[4.459013938903809, -0.8810093998908997, "[TT] Launch Date of the SpaceX-CRS-4 Dragon capsule = Sept. 21, 2014"]
-[8.10209846496582, 5.134057521820068, "[TT] Calibration Method of the MWHS-II = Two points periodically"]
-[5.211514472961426, 3.537281036376953, "[TT] Provider of the RS2000 = NASA"]
-[10.70300006866455, 2.813304901123047, "[TT] Mission Life of the Minisatellite = ~2 years or longer"]
-[6.956182479858398, 0.796434760093689, "[TT] Marsquake Discovery Date of the InSight = 22 September 2021"]
-[5.560577392578125, 2.745363235473633, "[TT] Post-Project Careers of the SAPPHIRE = Nine hold significant spacecraft systems or management responsibilities with aerospace contractors, the Air Force or academia"]
-[5.550159931182861, 1.0961380004882812, "[FF] Launch Date of the LARES satellite = Unknown"]
-[11.85525131225586, 0.015334025956690311, "[FF] Purpose of the TESS = Study exoplanets"]
-[9.417487144470215, 5.0655107498168945, "[TT] Attitude Knowledge Precision of the ADCS Unit = Better than 2\u00ba"]
-[3.5858864784240723, 4.659645080566406, "[FF] Imaging Products of the RISAT-1 = SAR data"]
-[6.1099114418029785, 2.448852300643921, "[FF] Project Scientist of the Rosetta = Matt Taylor"]
-[8.978261947631836, 5.535385608673096, "[TT] Orientation Accuracy of the GOMS-1 = \u00b12-5 arcmin"]
-[9.331299781799316, 5.135183334350586, "[FF] Yaw Control of the Spacecraft = Within 1.0\u00ba"]
-[5.882812976837158, 7.77158784866333, "[TT] Component Type of the D-Amp = Amplifier"]
-[5.742514610290527, 2.819563627243042, "[TT] Space Act Agreement Partner of the SpaceX = NASA"]
-[9.506446838378906, 7.184674263000488, "[TT] Spatial Resolution of the ISIR = 250 m"]
-[3.280935525894165, 1.5764987468719482, "[TT] Orbit Period of the Sentinel-2 satellites = 101 minutes"]
-[3.4546473026275635, -0.48380231857299805, "[TT] Orbit Type of the JL-1-GF03D = SSO"]
-[8.116281509399414, -0.7126602530479431, "[FF] Objectives of the CRISTAL = Survey the sea ice, its snow cover and the land ice, support maritime operations in the polar oceans, better understand the climate processes"]
-[6.445530414581299, -0.643336832523346, "[TT] LTDN of the Satellite = 10:30 hours"]
-[9.28095531463623, 4.835415363311768, "[TT] Operation Start of the Attitude Determination and Control System = Since 2014"]
-[3.2985737323760986, 5.012836933135986, "[TT] Swath Width of the L-band Synthetic Aperture Radar (SAR) = 260 km"]
-[6.870995044708252, -1.7725987434387207, "[FF] Data Products of the Jason-1 Mission = Sea surface topography, Significant wave height, Surface wind speed, Ocean tides, Vertically integrated atmospheric water vapor, Vertically integrated ionospheric electron content"]
-[7.9449286460876465, 8.698577880859375, "[TT] Spectral Range of the TROPOMI = Ultraviolet to visible and selected bands in near-infrared"]
-[5.548603057861328, 2.422301769256592, "[FF] Affiliation of the SPADUS = A. J. Tuzzolino, R. B. McKibben, J. A. Simpson, S. BenZvi, H. D. Voss, H. Gursky"]
-[13.369309425354004, 7.837682723999023, "[TT] RF Output Power of the Zonal Beam = 32 W"]
-[8.857421875, 3.3940258026123047, "[TT] Accuracy of the Ionosphere Plasma Density = < 20% (\u03c1=10 9  -10 11  m -3 ) \u2013 5% (\u03c1 >10 11  m -3 )"]
-[7.334449768066406, 8.702604293823242, "[TT] Band 1 of the RBV Instrument = 0.48 - 0.58 \u00b5m"]
-[3.566511869430542, 4.4136271476745605, "[FF] Contents of the Biosphere = 25-m spaced annual global mosaics (using orthorectified slope corrected SAR)"]
-[6.93262243270874, 4.602743148803711, "[FF] Parameter of the RadFET = Value"]
-[7.9682745933532715, 7.404590129852295, "[TT] Video Data Conversion Rate of the MS Detectors = 7 Mpixel/s"]
-[8.30892562866211, 6.137712478637695, "[TT] Control Precision of the PCS = One thousandth of a degree"]
-[7.756994247436523, 5.802224636077881, "[FF] Product Line of the NAOMI instrument = Compact & versatile cameras"]
-[9.436088562011719, 7.058923244476318, "[TT] Spatial Resolution of the MSI = 10 m, 20 m, 60 m"]
-[7.605109214782715, 7.573107719421387, "[FF] Size of the PSF = Must be balanced against the increase in other noise sources such as read noise and dark current"]
-[7.210896968841553, 7.889309883117676, "[TT] Dynamic Range (Far) of the Satellite = -28.6 - -8.8 dB"]
-[14.21207046508789, 3.22383975982666, "[TT] Mass of the OBIS = 20 kg"]
-[3.882293224334717, 3.4210727214813232, "[TT] Deployment Start Date of the Galileo Second Generation Satellites = By 2024"]
-[9.587757110595703, 9.071602821350098, "[FF] Design Reference of the IRIS spacecraft = Prior missions and design studies"]
-[10.879074096679688, -0.3197215497493744, "[TT] Data Acquisition Period of the TanDEM-X = 2011 and 2015"]
-[12.446915626525879, 0.5743749737739563, "[TT] Mission Lifetime of the PLATO Spacecraft = Up to 8.5 years"]
-[8.224740982055664, 7.263707637786865, "[TT] Quantity of the Teledyne e2v CCDs = 104"]
-[5.014593124389648, 3.109250783920288, "[FF] Operation Contract of the LLMS/IRIS = SAIT Systems has also a contract from ESA to operate LLMS/IRIS for a period of three years"]
-[6.3899359703063965, 0.2238800972700119, "[TT] Design of the Skylab-1 = Use leftover Apollo lunar hardware"]
-[9.153697967529297, 2.685276746749878, "[FF] Magnetic Field Study of the Voyager = Heliosphere and beyond"]
-[13.492815971374512, 2.9523439407348633, "[TT] Weight of the Satellite = 770 kg"]
-[7.424563884735107, 6.3208208084106445, "[FF] Ranging Noise Requirement of the Laser Ranging Instrument (LRI) = Unknown"]
-[7.72532844543457, 6.748260974884033, "[FF] Delay Measurement of the ULTRACAM = 30,000 km"]
-[10.392056465148926, 1.957719326019287, "[TT] Brightness Profile Correlation of the ASTER = More than 0.99"]
-[13.214730262756348, 7.261686325073242, "[TT] Power Consumption of the CMGs = 220 W"]
-[6.741367816925049, 2.0493228435516357, "[TT] Field of View of the Nancy Grace Roman Space Telescope = Nearly 100 times larger than Hubble Space Telescope"]
-[5.763861179351807, 0.9019999504089355, "[FF] Publication Date of the G11.2-0.3 = 9 March 2016"]
-[11.301692008972168, 5.890323638916016, "[TT] Material of the Proof Masses = Gold/platinum alloy"]
-[10.254611015319824, 7.865211009979248, "[TT] Aperture of the Optical Parabolic Mirror or Telescope = ~1 m"]
-[13.938624382019043, 3.8682360649108887, "[TT] Sensor Mass of the OVM = 1 kg"]
-[10.073823928833008, -1.578012466430664, "[TT] Inclination of the ANUSat = 41\u00ba"]
-[6.752838134765625, 8.831422805786133, "[TT] Polarized Wavelengths of the POLDER = 3"]
-[9.247830390930176, 3.168879270553589, "[FF] Purpose of the Solar Wind Monitor Instruments = Detect the solar wind regime"]
-[3.921208143234253, 6.509119510650635, "[TT] Incidence Angle of the Antenna = 40.0\u00ba"]
-[8.560917854309082, 2.858473300933838, "[FF] Observation Contribution of the MAHRSI = Help quantify the contribution of water vapor exhaust injected into the upper atmosphere from the space shuttle to PMCs"]
-[11.279312133789062, 2.8227131366729736, "[TT] Mass of the Diamond nanosatellites = 6 kg"]
-[5.61915397644043, 5.654143333435059, "[TT] Microprocessor of the PCU = 16 bit microprocessor (H8/3048F)"]
-[8.965668678283691, 5.6040568351745605, "[TT] Pointing Accuracy of the CADRE = 1.0\u00ba"]
-[5.2205939292907715, 0.3894176781177521, "[TT] Installation Date of the Y-3 = January 1974"]
-[5.4102888107299805, 6.492920398712158, "[TT] Mass Data Storage of the DubaiSat-2 = 256 GBit"]
-[4.728450298309326, 7.333171367645264, "[TT] Data Rate of the X-band Transmitter = Up to 100 Mbit/s"]
-[9.57823657989502, 6.950610637664795, "[TT] Resolution of the Digital Elevation Model = 2 km"]
-[9.715521812438965, -0.22379070520401, "[TT] Altitude Range of the SOFIE = 40-95 km for T, 55-95 km for O3, 20-95 km for H2O, 20-75 km for CH4"]
-[8.086798667907715, 4.3743205070495605, "[TT] Frequency of the External Calibration = Two events every two weeks"]
-[5.970992088317871, 1.147455096244812, "[FF] Validation Date of the NASA ESTO technologies = July 22-27, 2012"]
-[10.043563842773438, 7.261238098144531, "[TT] Field of Regard of the Satellite = > 5,000 km(N/S) x 5,000 km(E/W)"]
-[7.727774143218994, 2.137808084487915, "[TT] Application of the VIS band (0.86 \u00b5m) = Determining vegetation amount, aerosols and ocean/land studies"]
-[9.796911239624023, 4.317645072937012, "[FF] Cryomag with planes of detectors of the AMS-02 = Above, inside and below the magnet"]
-[13.836684226989746, 7.194512367248535, "[TT] Input Current of the Buck-Boost Converter = 0 - 16 A"]
-[4.748508930206299, 6.312281608581543, "[TT] Frequency Range of the APL\u2019s Frontier radio = Wide range of frequencies"]
-[4.3942790031433105, 7.069515228271484, "[TT] Communication of the GPM Core = S-band RF"]
-[5.783532619476318, 0.6331462264060974, "[FF] Discovery Date of the Cluster = Spring of 2009"]
-[10.293173789978027, 4.0406904220581055, "[TT] Mounting of the MFI = 12 m radial boom"]
-[13.014974594116211, 7.259782791137695, "[TT] Power Consumption of the Vector Magnetometer = 1.1 W"]
-[9.083399772644043, 5.0749945640563965, "[FF] Stabilization of the ACS = Gyro reference unit"]
-[9.49079704284668, 3.707974672317505, "[FF] Projection of the Vertically-integrated magnetization model = Orthographic, centered at 90\u00ba West, 30\u00ba North"]
-[9.611491203308105, -0.5758435726165771, "[TT] Orbit Altitude of the CartoSat-2D = 506 km"]
-[8.164165496826172, 7.951553821563721, "[TT] IR Channel Detectors of the SEVIRI = HgCdTe"]
-[7.000921249389648, 4.4941558837890625, "[FF] Priority of the LEP-EA and LEP-E = High"]
-[8.263731002807617, 4.481805801391602, "[FF] Total Ionizing Dose Measurement of the Thermometers = Unknown"]
-[12.039872169494629, -0.41520094871520996, "[TT] Launch Date of the TESS = 18 April 2018"]
-[8.596802711486816, 0.14454832673072815, "[FF] Interaction of the Solar Orbiter = Crossed one of the comet\u2019s two tails"]
-[6.8261399269104, 5.864731311798096, "[TT] Quantity of the XPODs = 3"]
-[5.026866436004639, 8.271645545959473, "[TT] Bandwidth of the Linear FM Transmitter = 320 MHz"]
-[11.508682250976562, 4.736527919769287, "[TT] Size of the 5.2 m 2 = 5.2 m 2"]
-[5.704018592834473, 6.088178634643555, "[FF] Image Data Storage of the ISERV = Compact Flash memory, WORF laptop hard disk"]
-[9.583341598510742, 5.041904926300049, "[TT] Short Term Stability of the AOCS = 56 \u00b5rad"]
-[5.6091179847717285, 2.5967142581939697, "[TT] Population of the Timbuktu = About 55,000"]
-[9.286351203918457, 1.0190349817276, "[TT] Planned Trajectory Correction Maneuvers of the Juno spacecraft = 13"]
-[7.381300449371338, 3.162430763244629, "[FF] Objective 2 of the EPS (EUMETSAT Polar System) = Provide enhanced monitoring capabilities (complimentary to ENVISAT) to fulfil the requirements to study the Earth climate system"]
-[7.765061378479004, 6.5729546546936035, "[TT] Distance IAR Duration of the Integer Ambiguity Resolution = Roughly 15 minutes"]
-[10.977231979370117, 7.652945041656494, "[TT] Nominal Swath Width of the Wide standard Quad-Pol = 50 km"]
-[4.422827243804932, 0.6311209797859192, "[TT] Integration Completion Date of the ABI = Jan. 12, 2015"]
-[4.958358287811279, 3.37455677986145, "[TT] Manufacturer of the OAPs = Thorlabs Inc"]
-[10.099894523620605, 2.4549553394317627, "[FF] Objective of the S-020 = Record on photographic film a spectrum of the X-ray and ultraviolet radiation from the sun in the 1-20 nm (or 10 - 200 \u00c5) region, with modest angular resolution"]
-[5.9398651123046875, 4.160103797912598, "[TT] Replacement of the FY-3D = FY-3B"]
-[5.656209945678711, 4.964868545532227, "[FF] Data Transmission of the McMurdo Ground Station = Real-time"]
-[13.956064224243164, 2.8441052436828613, "[TT] Launch Mass of the DMSP F-17 = 1154 kg"]
-[5.687899112701416, 7.052002906799316, "[TT] Input Data Rate of the CoReCi = Up to 1.4 Gbit/s"]
-[9.683674812316895, 7.237194061279297, "[TT] Ground Resolution of the OCTS = 700 m"]
-[8.327535629272461, 7.346358776092529, "[TT] Payload of the THEA = Proprietary spectrometer and components"]
-[-4.065065383911133, 4.4823899269104, "[FF] Support Phase Time Period of the Mango Tango = 20.06 to 01.07.2010"]
-[9.3060941696167, -0.5817468762397766, "[TT] Orbit of the Prox-1 = Circular, 720-kilometer-high"]
-[5.349101543426514, 7.753204822540283, "[TT] Isolation Between Ports of the Array Radiator = Better than -22 dB"]
-[4.562780857086182, 6.5592498779296875, "[TT] Antenna Performance Verification of the Spacecraft = TRL 7"]
-[9.290719985961914, -0.3479439914226532, "[TT] First Orbit Apogee Altitude of the EFT-1 Orion = 890 km"]
-[8.090876579284668, 4.609316825866699, "[TT] Orbit Tracking Method of the LARES-2 = Laser"]
-[9.206831932067871, 3.0841355323791504, "[FF] Solar Wind Measurements of the IMAP = Electron, proton, heavy ion, and magnetic field"]
-[7.087133407592773, 3.9746649265289307, "[FF] Social Value of the COS = Lost if information is not used"]
-[5.091790676116943, 5.203133583068848, "[TT] GPS Receiver of the KOMPSAT-6 = Dual-frequency GPS receiver for POD generation"]
-[3.8396871089935303, 4.3270978927612305, "[FF] Purpose of the RADARSAT-1 = Produced radar imagery for applications in agriculture, cartography, hydrology, forestry, oceanography, geology, ice and ocean monitoring, arctic surveillance, and detecting ocean oil slicks"]
-[11.46514892578125, 3.937647819519043, "[FF] Range of the AeroCube-OCSD-B and -C = Unknown"]
-[6.28369665145874, 4.8876776695251465, "[FF] Application of the CMT = Support for Local Emergencies"]
-[14.297144889831543, 3.1595346927642822, "[TT] Mass of the Capella-1 = 37 kg"]
-[3.875208616256714, 7.859619617462158, "[TT] Modulation Type of the AX100 = G3RUH FSK"]
-[5.587402820587158, 6.277754783630371, "[TT] File System of the Data Storage = FAT32"]
-[6.321924209594727, 0.1223469004034996, "[TT] Observation Period of the BRITE = Six-month"]
-[18.79836654663086, 3.479896306991577, "[TT] Mean \u0394E (m) of the Nellis = -0.2"]
-[9.573874473571777, 9.193523406982422, "[FF] Funding of the IRIS Imager = DSO National Laboratories"]
-[7.930377960205078, 6.533524036407471, "[TT] Time Resolution of the SEM-2 = 500 s, 600 s, 30-minute averages"]
-[8.78393840789795, 4.48500919342041, "[FF] Maximum Angular Limit Away from Sun-pointing Direction of the RVX = Unknown"]
-[5.233651161193848, 0.5323827266693115, "[TT] Switch On Date of the LRI = July 2, 2018"]
-[14.287403106689453, 3.016375780105591, "[TT] Mass of the UniSat-5 = 28 kg"]
-[5.436014175415039, 2.4084625244140625, "[TT] Status of the MSU-MR = Fully functional"]
-[7.1932902336120605, 4.471202373504639, "[FF] Unknown of the SOLCON-3 = Unknown"]
-[10.58676528930664, 5.169967174530029, "[FF] Probe Types of the ISL Instrument = One cylindrical, one spherical with a 6 cm diameter segmented probe"]
-[6.886683940887451, 6.098679065704346, "[TT] Number of Instruments of the JEM-X = 2"]
-[4.145694255828857, 7.006083011627197, "[FF] Splitting of the Baseband Signal = Three ways"]
-[6.794740676879883, 6.858445167541504, "[TT] Number of Laser Terminals of the EDRS-D = 3"]
-[9.280625343322754, 3.202550172805786, "[TT] Function of the Coronagraph = Take images of the Sun's corona"]
-[3.550234794616699, 6.443453788757324, "[TT] Antenna Mast Height of the ASAL Ground Station = 10 m"]
-[3.7866365909576416, 7.950406551361084, "[TT] Modulation Scheme of the Link 2 and 3 = UQPSK (Unbalanced Quadrature Phase-Shift Keying)"]
-[6.937556266784668, 2.0641632080078125, "[FF] URL of the GFO = http://ibis.grdl.noaa.gov/SAT/gfo/"]
-[8.785411834716797, 2.685809373855591, "[TT] Error of the Atmosphere = \u00b10.25 g/cm2"]
-[3.6674344539642334, 4.846274375915527, "[TT] Incidence of the RADARSAT-2 = 20\u00ba - 49\u00ba"]
-[8.150494575500488, 8.74597454071045, "[TT] Redshift Range of the NISP Spectrograph = 0.7 to 2.0"]
-[13.717135429382324, 2.9469823837280273, "[TT] Mass of the Spacecraft = 3.2 kg"]
-[9.459268569946289, 4.087670803070068, "[TT] Electric Field Measurement Frequency Range of the IOF = 40 Hz and 178 kHz"]
-[2.929809093475342, 4.465034484863281, "[TT] ScanSAR Mode Swath of the PALSAR-2 = 490 km"]
-[6.567372798919678, 1.667391300201416, "[FF] URL of the DeorbitSail = http://www.athena-spu.gr/projects/DeOrbit"]
-[5.311838626861572, 3.140768527984619, "[TT] Procurement of the DWSS = DoD"]
-[9.277945518493652, 9.133589744567871, "[TT] Near-UV Channel Range of the IRIS = 278.0\u2013284.0 nm"]
-[14.126511573791504, 7.1426167488098145, "[TT] Bus Voltage of the EPS = 28 to 33 V"]
-[4.685307025909424, 6.63502836227417, "[TT] RF Communications of the Spacecraft = 32 to 256 kbit/s"]
-[13.123579025268555, 7.313193321228027, "[TT] Design of the MTVZA-GY = Total-power radiometer"]
-[8.441679000854492, 4.919354438781738, "[FF] Channel E0 of the Telescopes = Monitors the instrument thermal noise but can register ions above the background if the ion flux is sufficiently high"]
-[4.9193501472473145, 3.3534491062164307, "[TT] Manufacturer of the Tyvak 61C = Tyvak Inc."]
-[10.010771751403809, -1.5283280611038208, "[TT] Orbit Inclination of the FREESTAR = 39\u00ba"]
-[6.148257732391357, 3.1390535831451416, "[TT] Cash Infusion of the BlackSky 7 = $450 million"]
-[6.988882064819336, 7.791131496429443, "[TT] Reflector Optical Prescription of the SweepSAR = F/D=0.75"]
-[6.526912689208984, 3.5805749893188477, "[FF] Purpose of the DMSP-20 = Provide information on cloud cover over the Soviet Union"]
-[6.899297714233398, 5.17339563369751, "[FF] Function of the PIU = Provide high voltage supplies for both the SiPMs and Si-PIN sensors on the GRD and XRD respectively"]
-[9.464839935302734, 7.284549713134766, "[TT] Resolution of the NAOMI = 2.5 m"]
-[8.106029510498047, 8.343951225280762, "[TT] IR Channels of the Spectrometer = 44 channels from 6.21-11.76 \u00b5m (850-1610 cm -1 ) with 0.1296 \u00b5m interval"]
-[11.479815483093262, 5.8093976974487305, "[TT] Structure of the OceanSat-1 = Aluminum/aluminum honeycomb structure with CFRP elements"]
-[5.568161964416504, 6.562445640563965, "[TT] Data Usage by Scientists of the SMOS = Around 13 TB per year"]
-[6.5392584800720215, 1.3251953125, "[FF] Image Credit of the FormoSat-2 = NSPO"]
-[5.530169486999512, -1.8288171291351318, "[TT] Design Life of the KOMPSAT-1 = 3 years"]
-[11.008992195129395, 2.9096291065216064, "[TT] Structure Dimensions of the PSSCT Nanosatellite = 12.5 cm x 12.5 cm x 25 cm"]
-[1.7446168661117554, 4.56205415725708, "[FF] N/A of the mechanical interface = N/A"]
-[9.691889762878418, 8.186476707458496, "[TT] Field of View (Cross-track) of the MSU-100 = 31\u00ba"]
-[9.731401443481445, 8.463210105895996, "[TT] FOV of the Instrument = 19.3\u00ba"]
-[7.214303493499756, 5.180540084838867, "[FF] Purpose of the COTS-2 = Collects information on the frequency of single event effects and how to mitigate them, especially in specialized computer chips"]
-[6.015047073364258, 4.142093181610107, "[FF] Supported Services of the APT web server = Catalog query, receiving acquisition coverage"]
-[8.345755577087402, 2.598848342895508, "[FF] Objective of the CATS = Demonstrate the utility of state-of-the-art multi-wavelength laser technology to study aerosol distribution and transport in the atmosphere"]
-[14.033690452575684, 6.306588172912598, "[TT] Manufacturer of the NanoMind A3200 = GomSpace"]
-[4.588512420654297, 0.8710094690322876, "[TT] Launch Date of the FY-3E = 4 July 2021"]
-[8.531001091003418, 5.547670841217041, "[TT] Geolocation Error Requirement of the Satellite = Smaller than approximately 10% of the footprint size"]
-[5.6839470863342285, 4.663000106811523, "[FF] Provided through a secure communication channel via VPN of the Real-time network communications = Links the SCC of GISTDA to the RTS of NSPO and the SOCC of NSPO to the SBS of GISTDA"]
-[7.561293125152588, 6.948497772216797, "[TT] Cadence of the SUVI = Up to 3 images/s"]
-[5.150730609893799, 6.001668453216553, "[FF] SpaceWire Deterministic Implementation of the NEXTAR = Unknown"]
-[5.5133538246154785, 2.652873992919922, "[FF] Outreach Program of the EduSat = Italian Space Agency"]
-[6.279745101928711, -0.11595799028873444, "[TT] Revisit Time of the WCOM = 2-3 days"]
-[6.728977203369141, 5.382412910461426, "[FF] Features of the Control Units = A/D (Analog-to-Digital) converters"]
-[6.088767051696777, 3.314239501953125, "[FF] Real-Time Data Broadcast of the WSF-M = Equipped Department of Defense (DoD) direct readout sites"]
-[11.135152816772461, 5.71869421005249, "[TT] Gd Foil Thickness of the LND = 20 \u00b5m"]
-[8.528482437133789, 7.884948253631592, "[FF] Remaining Challenge of the CGI = Instrument-model mismatch"]
-[8.747593879699707, 0.6548956632614136, "[TT] Current Speed of the Gulf of Khambhat = 1.5 to 2 m/s (3.3 to 4.5 miles per hour)"]
-[4.916305065155029, -2.105841875076294, "[TT] Mass of the Chang'e-4 lunar probe = 400 kg"]
-[4.776850700378418, 0.5543857216835022, "[TT] Launch Year of the ARIEL = 2029"]
-[8.00918960571289, 0.7474106550216675, "[FF] Running Above the 95th Percentile of the River Levels = Yes"]
-[4.480816841125488, 4.2087721824646, "[TT] Number of Satellites of the GEOSAR space segment = 7"]
-[8.415979385375977, 5.780848503112793, "[TT] DOFs Measured of the Metrology System = Translation in 2 axes, clocking angle"]
-[7.755413055419922, 8.071746826171875, "[TT] SNR of the Telescope = 205"]
-[8.271943092346191, 6.653866291046143, "[FF] Stereo Imaging Capability of the WV60 = Yes"]
-[13.654716491699219, 6.9954633712768555, "[TT] Power Output of the EPS = 20 W"]
-[10.158317565917969, 5.5586090087890625, "[TT] Thermal Operational Stability of the Instrument = \u00b11\u00baC"]
-[11.861054420471191, 4.948982238769531, "[TT] Size of the PCB = 115 mm x 190 mm"]
-[9.772098541259766, 8.540785789489746, "[TT] IFOV N/S x E/W (\u00ba) of the FCI-TA = 0.40 x 0.40"]
-[7.905953407287598, 7.195249080657959, "[TT] Data Recording of the Electron Detectors (IDEE) = On triggering alerts only"]
-[7.078827857971191, 7.088422775268555, "[TT] Wavelength Stability/Linewidth of the Laser = < 60 pm"]
-[11.825933456420898, 6.726592063903809, "[TT] Mass Range of the IRM = 1-40 amu/q"]
-[9.62031078338623, 8.266380310058594, "[TT] Field of View of the MEIDEX = 16\u00ba"]
-[7.757666110992432, 7.882436275482178, "[TT] Sensitivity of the Sensitivity = 5 counts/s/Rayleigh"]
-[8.893842697143555, 3.282763719558716, "[FF] Impact on Satellites of the Earth's Magnetic Field = Can cause big headaches for satellites"]
-[6.992963790893555, 6.142435073852539, "[TT] Operating Modes of the CATS = Six science modes"]
-[8.784463882446289, 4.470498085021973, "[TT] Safe Mode Attitude Sensing System of the SPOT-6 = Magnetometer (MAG) / Sun Sensor (BASS) system or optionally a Magnetometer / Coarse Earth Sun Sensor (CESS) system"]
-[3.6946394443511963, -1.1117408275604248, "[TT] Orbit Type of the \u00d8rsted satellite = Elliptical polar orbit"]
-[10.407398223876953, 2.3755807876586914, "[FF] Attitude Sensing of the X-ray Navigation = High-accuracy without optics"]
-[6.045551776885986, 3.7087628841400146, "[FF] Ground Segment and Distributed Operations Concept of the BRITE-Austria = Unknown"]
-[12.103904724121094, 2.9986932277679443, "[TT] Delta V of the Hydrazine Propulsion Subsystem = 70 m/s"]
-[7.875851154327393, 1.9569276571273804, "[FF] Marine Geoid of the SeaSat = Data"]
-[14.6434907913208, 6.663080215454102, "[TT] Capacity of the Batteries = 50 Ah"]
-[5.250738620758057, 1.2520643472671509, "[FF] Conference Date of the SOTA = May 11-13, 2011"]
-[7.091087818145752, 2.472170829772949, "[FF] Mission Name of the Satellite = Wildfire Observations"]
-[10.048746109008789, 4.272964954376221, "[TT] Deployment Shock of the SADM = Low"]
-[3.741499662399292, 4.436291217803955, "[TT] Program Name of the SAR/GLONASS = SAR/GLONASS"]
-[4.521292209625244, 3.8151180744171143, "[TT] Ground Segment Operator of the Galileo = European Global Navigation Satellite System Agency (GSA)"]
-[8.031782150268555, 4.692680835723877, "[FF] Power Initialization of the Satellite = Autonomously perform the initialization sequence"]
-[9.418330192565918, 3.9919960498809814, "[TT] Launch Date of the Fluxgate magnetometer = 25 June 2019"]
-[6.470297813415527, -1.2472150325775146, "[FF] Data Gap of the GRACE-FO = July 2017 to May 2018"]
-[5.56303596496582, 7.04930305480957, "[TT] Telemetry of the LEICA = 1.3 kbit/s"]
-[13.317919731140137, 5.464990139007568, "[TT] Solar Array of the EPS = Articulated, 1 wing, 2-axis tracking"]
-[9.775935173034668, 7.498696804046631, "[TT] GSD of the Spacecraft = 1 m (PAN), ~ 4 m (MS) @ 600 km altitude, nadir view"]
-[9.565055847167969, 9.089585304260254, "[TT] Image Area Coverage of the IRIS = 175 arcsec x 175 arcsec"]
-[10.369787216186523, 3.191896438598633, "[TT] Number of CubeSats of the PSLV-C37 = 88"]
-[5.6118340492248535, 4.705728054046631, "[FF] Signal-In-Space Test Activity of the GIOVE-A = Unknown"]
-[13.773811340332031, 2.8883633613586426, "[TT] Mass of the Spacecraft structure = 0.48 kg"]
-[8.566019058227539, 4.5883660316467285, "[FF] Target Star Monitoring of the ASTERIA = One star at a time"]
-[13.872363090515137, 3.653275728225708, "[TT] Mass of the Telescope = 63 kg"]
-[4.535061836242676, 2.937366485595703, "[TT] Location of the PDCC = ESA/ESRIN, in Frascati, Italy"]
-[5.826160430908203, -0.8009696006774902, "[TT] Operational Life of the Spacecraft = \u2265 7.5 years from the end of IOT"]
-[7.70924186706543, 0.5535797476768494, "[FF] Purpose of the LDEX = Detect presence of water ice in the permanently shadowed lunar craters"]
-[6.787648677825928, 1.0747101306915283, "[FF] Conference Date of the Solar Orbiter = Oct. 14-17, 2008"]
-[14.258405685424805, 3.304072380065918, "[TT] Mass of the MSI = 275 kg"]
-[9.230240821838379, 8.621766090393066, "[TT] Slit Height of the Long Wavelength Band = 2.75 cm; 1/33 for bright target"]
-[6.471376419067383, 4.899603366851807, "[FF] Subsystems of the IRPS = UIS (User Interface Subsystem), ICPS (Image Collection Planning Subsystem), DIS (Direct Ingestion Subsystem), PMS (Product Management Subsystem)"]
-[4.712229251861572, 7.962135314941406, "[TT] Operating Frequency of the SAS&R = 406 MHz"]
-[12.179119110107422, 6.113467216491699, "[TT] Events Collected of the AMS = 54 billion"]
-[10.78262710571289, 2.803619861602783, "[FF] Laboratory and Flight Testing of the Chibis-M Microsatellite = Unknown"]
-[5.618590831756592, 1.0944596529006958, "[TT] Imaging Date of the MSU-MR = July 25, 2014"]
-[6.422553539276123, 1.9941645860671997, "[FF] URL of the MidSTAR-1 = http://www.usna.edu/Satellite/midstar/downloads/main/PDRfinal.ppt"]
-[4.610901832580566, 2.769519805908203, "[TT] Development Location of the ART-XC = Russia"]
-[4.385730266571045, 3.104201555252075, "[TT] Ground Station of the SAOCOM-1A = ETC (Estaci\u00f3n Terrena de C\u00f3rdoba), Argentina"]
-[3.861539602279663, 5.444551467895508, "[TT] Illumination Diameter of the Radar Altimeters = 1700-meter"]
-[6.328186988830566, 3.533658742904663, "[FF] Data Repository Demonstration of the Space Traffic Management = Planned for the next several weeks"]
-[8.968157768249512, 6.855106830596924, "[FF] Covered Area of the Image = Approximately 30 km x 50 km"]
-[8.597319602966309, 1.4406180381774902, "[TT] Quantization levels of the Cloud water = 0.05"]
-[4.424100875854492, 5.191285610198975, "[FF] Phased Out Devices of the COSPAS-SARSAT = 121.5 and 243 MHz emergency beacons"]
-[9.55821704864502, 5.029993057250977, "[FF] Pointing Stability of the VT = High"]
-[4.478638648986816, 6.858627796173096, "[TT] Beacon Ku-band of the RF communications = 1 mW"]
-[3.199739694595337, 1.6610854864120483, "[TT] Image Coverage Time of the Sentinel-2B = 5 days"]
-[6.591637134552002, 5.891498565673828, "[TT] Payloads of the TDS-1 = 8"]
-[7.854684352874756, 8.022831916809082, "[TT] CCD Array Elements of the LISS-4 = 12,288 elements for each band"]
-[8.130624771118164, 6.037735462188721, "[TT] Camera of the Occulter satellite = A set of cameras"]
-[10.076727867126465, -1.5760061740875244, "[TT] Inclination of the Spacecraft = 98.09\u00ba"]
-[11.6845703125, 4.6793975830078125, "[TT] Cylinder Height of the ACC = 0.83 m"]
-[10.37071704864502, 2.1304073333740234, "[FF] Purpose of the NuSTAR = Take focused pictures of the cosmos in high-energy X-ray light"]
-[10.867499351501465, 6.423398494720459, "[TT] Manufacturing Process of the Mirror = Electroforming"]
-[5.289801120758057, 3.112272024154663, "[FF] GaN Manufacturing Process of the UMS = Placed onto the European Preferred Parts List of the European Space Components Coordination"]
-[7.185415267944336, 5.163362503051758, "[FF] Components of the IEPS = IT (Ion Thruster), PPU (Power Processing Unit), ECU (Electric-propulsion Control Unit), XT (Xenon Tank), PRU&FCU (Pressure Regulation Unit and Flow Control Unit), LCU (Line Connection Unit)"]
-[9.192987442016602, 7.590431213378906, "[TT] Spatial Resolution (Multispectral Band) of the NAOMI = 10 m"]
-[9.563512802124023, 1.0070774555206299, "[TT] Speed of the CME = Between 1.5 and 1.8 million miles an hour (700 and 800 km/s)"]
-[8.851729393005371, 2.872110605239868, "[FF] Objectives of the Deployment Mechanism = 1) Deploy each pair of nodes on command, so as to guarantee appropriate formation on orbit; 2) Do so without inducing a torque on the mule; and 3) Ensure appropriate deployment velocity for ideal cross-track separation while traversing the Auroral region"]
-[6.801365852355957, 3.105236768722534, "[TT] Lower Refresh Rates of the Satellite System = Much lower rates at the higher latitudes"]
-[6.471400737762451, 6.252155780792236, "[TT] TRL Level of the Computer System = 5"]
-[7.500235557556152, 0.9570493102073669, "[FF] Purpose of the GRAIL Probes = Learn about the moon's internal structure and composition"]
-[9.677655220031738, 4.0709757804870605, "[TT] Vector Components Random Error of the Magnetic Field = < 1 nT"]
-[6.010270595550537, 4.723052501678467, "[FF] Function of the SSPA-C = Rebroadcast data processed by the EUMETSAT control center"]
-[6.70435905456543, 4.7523980140686035, "[FF] Function of the DIS = Direct Ingestion"]
-[4.031194686889648, 4.165403842926025, "[TT] Image Content of the RADARSAT-2 = Vancouver harbor, Canada"]
-[10.931923866271973, 7.552852153778076, "[TT] Swath Width of the TAC = 52 km"]
-[5.807134628295898, 6.461153030395508, "[TT] Data Storage Duration of the C&DH = More than 28 days"]
-[7.256834030151367, 7.502129554748535, "[FF] Downlink Frequency of the Imager Sounder = 4798 MHz"]
-[8.083136558532715, -0.11729349941015244, "[TT] Normal Cub Litter Size of the Polar Bears = Two"]
-[6.476414680480957, 5.128434181213379, "[FF] Module Type of the PIU = Unknown"]
-[8.584753036499023, 1.5009406805038452, "[TT] Quantization Levels of the Integrated water vapor = 0.10"]
-[10.88368034362793, 5.48185396194458, "[TT] Diameter of the Heat Shield = 8 feet (2.44 m)"]
-[13.854320526123047, 5.670802593231201, "[FF] Efficiency Comparison of the Solar Cells = 24% efficient under air mass zero (AM0) compares favorably to silicon solar cells that are 16% efficient or GaAs cells at 20% efficiency"]
-[6.604419708251953, 8.147196769714355, "[TT] Polarimetric Imaging of the Instrument = Incoherent"]
-[12.075139045715332, 7.641375541687012, "[TT] Mass of the FLIR Boson camera = <38 g"]
-[8.439517974853516, 7.551632881164551, "[TT] Detector Readouts of the ASTERIA = 20 Hz"]
-[6.217517375946045, -0.2656405568122864, "[TT] Operation Period of the IMA = Limited to several hours/day"]
-[13.455422401428223, 7.369186878204346, "[TT] Power of the S/C = 693 W (EOL)"]
-[3.6284019947052, -0.9897680282592773, "[TT] Orbit of the ProSEDS = Circular"]
-[10.263110160827637, 5.759528636932373, "[TT] Operating Temperature of the Telescope = 150 K"]
-[4.40087890625, 3.1302876472473145, "[TT] Ground Station Location of the PROBA-3 = Santa-Maria in the Azores (in Portugal)"]
-[8.364706039428711, 1.265260934829712, "[TT] Transmit-Mode Duty Cycle of the RainCube = 25%"]
-[6.629571437835693, 2.0179004669189453, "[FF] URL of the NuSTAR = https://www.nasa.gov/feature/jpl/andromedas-bright-x-ray-mystery-solved-by-nustar"]
-[5.812058925628662, 2.49115252494812, "[TT] Launch Partner of the WorldView Legion = SpaceX"]
-[5.674331188201904, 11.349189758300781, "[FF] Approx. Peak Sensitivity Altitude of the Channel 3 = Unknown"]
-[6.0297932624816895, 3.0861284732818604, "[TT] Operations Manager of the GOES-O = National Oceanic and Atmospheric Administration (NOAA)"]
-[7.907222747802734, 7.905017852783203, "[FF] Temporal Coverage of the Geostationary Infrared Sounder = Good"]
-[13.273283958435059, 2.9212818145751953, "[TT] Mass of the SaudiSat-2 = 15 kg"]
-[8.357314109802246, 5.294301986694336, "[TT] Accuracy of the Satellite Tracking = Centimeter-scale orbital checks"]
-[5.145501613616943, 1.911373257637024, "[TT] Mission Status of the HJ-1 = Operational (extended)"]
-[13.59878921508789, 2.0014054775238037, "[TT] Payload Capacity of the Cygnus cargo = More than 400 kg"]
-[5.897186756134033, 1.532982349395752, "[FF] Presentation Date of the PRISMA mission = May 29-31, 2013"]
-[13.24488639831543, 5.441639423370361, "[TT] Product of the Deployable Space Systems = Canister, frame and solar array blanket"]
-[10.13405990600586, 6.496493816375732, "[TT] Survey Date of the MABEL = April 8, 2012"]
-[9.777217864990234, -0.57623690366745, "[TT] Orbit Altitude of the BlackSky Pathfinder-1 = 690 km"]
-[9.770071029663086, 7.08884334564209, "[TT] Spatial Resolution of the LISS-4 = 5.8 m"]
-[5.56035852432251, -1.932916522026062, "[TT] Type of the KOMPSat-5 = SAR"]
-[6.473569869995117, 7.81088399887085, "[TT] Number of CHUs of the \u00b5ASC = Up to 4"]
-[8.026853561401367, -0.3625853657722473, "[FF] Minimum Extent Date of the Arctic Sea Ice = September 15, 2020"]
-[10.41959285736084, 2.291635751724243, "[TT] Spectral Resolution of the X-ray telescopes = 500 eV at energies below ~30 keV, 1.2 keV at the upper end of the energy range"]
-[5.275880813598633, 0.40764370560646057, "[TT] Launch Date of the TIROS = April 1, 1960"]
-[8.496315956115723, 5.099534511566162, "[FF] Development Status of the GRACE Follow-On accelerometers = Unknown"]
-[8.975187301635742, 0.5206728577613831, "[FF] Launch Date for Artemis 1 of the SLS Rocket = Unknown"]
-[12.201708793640137, 3.674395799636841, "[FF] Objective of the LPE = Xenon plasma diagnostic instrument for CAE"]
-[14.578554153442383, 6.663342475891113, "[FF] Purpose of the NiMH Battery = Functional test"]
-[7.17692232131958, 2.712433338165283, "[FF] Imaging Capability of the SEOSAT-Ingenio = High-resolution images of Earth's land cover"]
-[10.058096885681152, 4.007593154907227, "[TT] Location of the SCM = In the shade of the spacecraft, at the end of the magnetometer boom"]
-[8.438899040222168, 5.51824426651001, "[TT] Geolocation Accuracy Test Location of the Ikonos-2 = Big Spring, TX"]
-[3.5327932834625244, 5.637307167053223, "[TT] Antenna Type of the XSAR = Active phased array antenna"]
-[9.470120429992676, 7.049065113067627, "[TT] DEM Resolution of the Terra/ASTER system = 30 m"]
-[8.076674461364746, 9.117392539978027, "[TT] Ellipse Axis A of the Long Wavelength Band = 180 mm"]
-[9.549365043640137, 4.4405083656311035, "[FF] Ballistic Coefficient of the SpinSat = Well-determined and characterized"]
-[9.116199493408203, 0.21584896743297577, "[FF] Elevation Difference of the Burroughs Crater = About 400 km"]
-[5.024168491363525, 0.015720460563898087, "[TT] Satellite Launch Date of the Kleos S.A. = Mid-2021"]
-[6.038452625274658, 4.2908735275268555, "[FF] Purpose of the CIL = Enable operators from one nation to order image products from the other nation\u2019s system, task the satellites of the other nation, receive the image products and store them in a fully secure way"]
-[7.940674781799316, 9.142881393432617, "[TT] Wavelengths of the AVGS = 808 nm and 850 nm"]
-[6.9311137199401855, 7.068933963775635, "[TT] Number of Beams of the ATLAS = 9"]
-[10.313264846801758, 7.364522933959961, "[TT] Design of the Limb Imager = Single off-axis three-mirror reflective telescope"]
-[4.743535041809082, 7.887999534606934, "[TT] Transmitter Frequencies of the ODB = 401.25 MHz, 2036.25 MHz"]
-[9.157885551452637, -0.44310489296913147, "[TT] Apogee of the IBEX = 319,000 km"]
-[6.490148067474365, 3.4109175205230713, "[TT] Resolution of the BlackSky Gen-3 satellites = 50 cm"]
-[3.7856154441833496, 1.1958916187286377, "[FF] Reusability of the Falcon 9 = Fully and rapidly reusable"]
-[7.30120325088501, 3.5359861850738525, "[FF] Pass Frequency of the Satellite = Between two and four times per day"]
-[14.165616989135742, 2.843170404434204, "[TT] Launch Mass of the HORYU-2 = ~ 7.1 kg"]
-[6.396291732788086, 2.006035804748535, "[FF] URL of the RADARSAT Constellation Mission = https://www.youtube.com"]
-[8.236170768737793, 4.134260654449463, "[TT] Spectral Calibration of the SUCHI = On orbit using atmospheric absorption features"]
-[5.554995536804199, 2.264159917831421, "[FF] Names of the Phantoms = Helga and Zohar"]
-[7.4528117179870605, 7.084640026092529, "[TT] Frame Rate of the GLM = 500 Hz"]
-[3.7362983226776123, 4.933733940124512, "[FF] Purpose of the Beamformers = Maximize their gain towards the direction of arrival of the desired radar echo and suppress, at the same time, range ambiguities arriving from different directions"]
-[3.3912646770477295, 5.067151069641113, "[TT] Observation Capability of the SIR-C/X-SAR = Two-frequency"]
-[8.488923072814941, 5.518040657043457, "[TT] Orbit Localization Accuracy of the WEOS = About 30 m"]
-[10.989419937133789, 7.641506195068359, "[TT] Swath Width for Regular Corresponding Mode of the Wide standard Quad-Pol = 25 km"]
-[9.840450286865234, 4.54389762878418, "[TT] Attitude Control Scheme of the GRACE-FO = Magnetic torque rods and cold gas thrusters"]
-[6.739134311676025, -0.33813318610191345, "[TT] Revisit Cycle of the Satellite = 5 day"]
-[9.014193534851074, 2.6082868576049805, "[FF] Observation Location of the IBEX = About 30 degrees south of the interstellar upwind direction"]
-[9.149293899536133, 3.113272190093994, "[FF] Importance of the Cluster = Study turbulence and its role in fundamental processes"]
-[7.9743266105651855, 1.9815645217895508, "[FF] Data Application of the CYGNSS = Flood Inundation Mapping"]
-[6.6909613609313965, 3.900803565979004, "[FF] Operation End of the Experiment = Mid-1975"]
-[4.935715198516846, 3.0037338733673096, "[TT] Prime Contractor of the ISS = Boeing"]
-[14.281469345092773, 3.205254077911377, "[TT] Mass of the Tsubame = 49 kg"]
-[4.0705342292785645, 6.56971549987793, "[TT] UHF receiving antennas of the SMDC-ONE = 4"]
-[12.619735717773438, 9.098007202148438, "[TT] Local Equator Crossing Time of the QuakeSat = 6:00 and 18:00"]
-[11.955528259277344, 6.551607608795166, "[TT] Energy Range of the Positron+Electron spectrum = 0.5 Gev to 700 GeV"]
-[8.754021644592285, 8.760451316833496, "[TT] Instrument Mass of the Grating Spectrometer = 0.230 kg"]
-[10.62742805480957, 6.82765531539917, "[TT] Transmit Efficiency of the Triple Mirror = 50%"]
-[10.42308235168457, 3.1664066314697266, "[TT] Type of the GOMX-3 = CubeSat nanosatellite"]
-[3.143608331680298, 2.3688931465148926, "[FF] Purpose of the Sentinel-2 MSI = Mapping (habitat, bathymetry, and water quality) and detection change for coral reef health assessment and monitoring"]
-[6.677372455596924, 2.9883339405059814, "[TT] Data Service of the Spire = Provides reliable and accurate global weather forecast"]
-[4.510494709014893, 1.4995167255401611, "[FF] Launch Date of the VNREDSat-1A = Unknown"]
-[9.705429077148438, -0.28320273756980896, "[TT] Mean Altitude of the Vstar = ~100 km"]
-[6.58244514465332, 0.7663043737411499, "[FF] Observation Date of the Herschel = 24 September 2018"]
-[4.873514652252197, 8.028497695922852, "[TT] Stable Roll Frequency of the GP-B satellite = 0.081 rad/sec (13 mHz)"]
-[6.133558750152588, 5.856022357940674, "[TT] System Control Module (SCM) of the SAMMES = 1 unit"]
-[9.874090194702148, -0.44428977370262146, "[TT] Orbit Altitude of the Harmony = 693 km"]
-[5.2841644287109375, 1.1417186260223389, "[FF] ICSO 2010 Presentation Date of the ASPIICS/PROBA-3 = Oct. 4-8, 2010"]
-[6.608736515045166, -0.3920244574546814, "[TT] Repeat Cycle of the POLDER-P = 16 days"]
-[8.06452751159668, 4.974570274353027, "[FF] Receiver Type of the CryoSat = DIODE added another feature: inertial J2000 on-board position and velocity bulletins to be used by the AOCS"]
-[8.044975280761719, 4.472862720489502, "[FF] Unknown of the Electromagnetic Calorimeter Trigger System = Unknown"]
-[7.0624589920043945, 0.05099400877952576, "[TT] Age of the LAGEOS-1 = 40 years"]
-[10.058512687683105, 1.6202853918075562, "[FF] Article Title of the Daniel Wang = Chandra large-scale mapping of the Galactic Centre: probing high-energy structures around the central molecular zone"]
-[6.871352195739746, 3.9075005054473877, "[FF] Function of the Vent = Allow venting after launch"]
-[6.3096489906311035, 4.794182777404785, "[FF] Function of the Peregrine Electronics = Provide C&C (Command and Control) of the payload, as well as data handling"]
-[8.199331283569336, 8.546236038208008, "[TT] End of Life Date of the Multi-band UV/VIS Spectrometer (ACE) = 31 December 2023"]
-[4.91878080368042, 0.447961688041687, "[TT] Launch Date of the MarCO = November 27, 2018"]
-[8.308197021484375, 3.1483254432678223, "[FF] Purpose of the SOLSE-2 = Provide stratospheric ozone profile information"]
-[13.516454696655273, 2.983079671859741, "[TT] Mass of the GOSAT-GW = 2900 kg"]
-[10.014106750488281, 6.109905242919922, "[TT] Background Albedo of the GLM = 80%"]
-[10.709344863891602, 2.8133485317230225, "[FF] URL of the FASat-Bravo microsatellite = http://rsta.royalsocietypublishing.org/content/361/1802/71.full.pdf"]
-[5.4479475021362305, 1.2683860063552856, "[FF] Deployment Date of the DIWATA-1 = April 27, 2016"]
-[10.914860725402832, 6.414750576019287, "[TT] Secondary Mirror Material of the Optical telescope = Fused silica"]
-[5.351101398468018, 3.1356446743011475, "[TT] Provider of the GPM Core spacecraft = NASA"]
-[5.137883186340332, 7.055592060089111, "[TT] Telemetry Downlink Rate of the SGLS Link = 32 kbit/s"]
-[3.4140472412109375, 6.402840614318848, "[TT] Size of the Antenna = 10.74 m x 2.16 m"]
-[13.568370819091797, 5.945756912231445, "[TT] Power Output of the Solar Array = ~1000 W at the beginning of the mission, varying throughout the mission to ~ 700 W"]
-[5.859888553619385, 2.5578999519348145, "[FF] Director of the ArgoMoon = David Parker"]
-[11.442573547363281, 4.554996967315674, "[TT] Gas Volume of the DSAT-1 = Minimal"]
-[4.13673210144043, 0.1279306262731552, "[TT] Proposed Doubleheader Launch Date of the Falcon 9 = February 4"]
-[7.666202068328857, 2.4620277881622314, "[FF] Radar Altimeter of the SeaSat = Device"]
-[5.6052985191345215, 6.883066654205322, "[TT] Archive Size of the SeaSat = Exceeds 1.5 PB (1015 Byte)"]
-[6.5467047691345215, 4.0995049476623535, "[FF] Design, Fabrication, and Testing Responsibility of the Payload = NASA Ames"]
-[5.147543907165527, -0.12716741859912872, "[TT] End of Life Date of the AeroCube-11/TOMSat = 5 years"]
-[6.951052188873291, 2.1883575916290283, "[FF] Mission of the Satellogic = Build an accurate and up-to-date picture of our planet"]
-[5.124076843261719, 0.6330052018165588, "[FF] Mission Move Forward Date of the DSCOVR = 2015"]
-[7.309165000915527, 9.13855266571045, "[TT] Filter Wavelength Range of the ISUAL instrument = 150-280 nm"]
-[4.5378851890563965, 1.1142216920852661, "[FF] Design and Implementation Date of the Argo = 1998"]
-[7.458189487457275, 3.0823144912719727, "[FF] Purpose of the GOES-S = Provide faster, more accurate data for tracking lightning, storm systems, wildfires, dense fog and other hazards"]
-[6.864686965942383, 7.121834754943848, "[TT] Size of the Additional Beams = 6 m x 1 m each"]
-[4.2895989418029785, 1.2153695821762085, "[FF] Industry Day Date of the SEOSat/Ingenio = Nov. 17, 2008"]
-[10.136953353881836, 0.973615288734436, "[TT] Distance of the ASASSN-14ko = 570 million light-years"]
-[4.062383651733398, 3.835481882095337, "[TT] Data Reception Location of the RISAT-1 = Shadnagar GS (Ground Station) of NRSC (National Remote Sensing Center)"]
-[14.475030899047852, 6.538744926452637, "[TT] Battery Status of the VELOX-PII CubeSat = Fully charged"]
-[12.767885208129883, 7.607104301452637, "[TT] Instrument Power of the Hyperion = 78 W"]
-[10.04761791229248, 2.991428852081299, "[FF] Design Date of the CubeSat Guidance, Navigation, and Control Module = August 2011"]
-[5.880721569061279, 6.277618408203125, "[TT] Number of Supported Devices of the SSRNI = Up to 24"]
-[6.521337985992432, -0.14662210643291473, "[TT] Frequency of the EMOC = Monthly"]
-[4.510140419006348, 0.5189292430877686, "[TT] Debut Date of the CIMON = 15 November 2018"]
-[9.06035327911377, 4.546648025512695, "[FF] Development and Operations of the Advanced Stellar Compass = 1996"]
-[13.595483779907227, 2.8322582244873047, "[TT] Chassis Mass of the Supernova-Beta = 1.64 kg"]
-[3.868084669113159, 7.867092609405518, "[TT] Modulation Mode of the Data Transmission = BPSK"]
-[7.161311149597168, 7.795999050140381, "[FF] Infrared Emissivity of the Cube Corner Reflectors (CCRs) = \u03b5"]
-[11.151599884033203, 4.7768025398254395, "[TT] Designed Depth of the \"the mole\" = 5 meters underground"]
-[5.775354385375977, 6.802884101867676, "[TT] Downlink Data Rate of the Telescope = 40 kbit/s"]
-[3.4563565254211426, -0.9283117651939392, "[TT] Orbit Type of the SeaSat = Non-sun-synchronous near circular polar orbit"]
-[5.99356746673584, 1.6122663021087646, "[FF] Critical NASA Review Date of the TEMPO = May 6, 2015"]
-[10.885087013244629, -0.3259681463241577, "[TT] Expected Number of Final DEM Geocells of the TanDEM-X = Nearly 20,000"]
-[10.1163969039917, -1.5039337873458862, "[TT] Inclination of the Satellite = 99.049\u00ba"]
-[5.005169868469238, -0.1952570080757141, "[TT] Launch time (UTC) of the GOSAT-2 = 04:08:00"]
-[6.415026664733887, 8.59380054473877, "[FF] Polarization of the Instrument = H/V (horizontal and vertical), H (vertical), H/V"]
-[11.91489028930664, 3.327007293701172, "[TT] Maneuvers Performance of the Advanced Composition Explorer = Periodically underperform by as much as 50% in 2014"]
-[5.427535057067871, 4.111969947814941, "[TT] Number of Bus Components of the MightySat I = 2"]
-[10.285401344299316, 3.170722246170044, "[FF] Payload of the Atlas V = Classified NROL-39 & 12 CubeSats"]
-[5.326355934143066, 5.720339775085449, "[TT] Communication of the DCAM3 = One-way to the mother ship"]
-[3.856290340423584, 3.4235503673553467, "[FF] Service Interruption Date of the Galileo = Unknown"]
-[11.511768341064453, 5.7094831466674805, "[FF] Platform Type of the G\u00f6kt\u00fcrk-1A = Aluminium chassis with honeycomb panels"]
-[8.034832954406738, 0.7171797156333923, "[FF] Mission Type of the Hera = Rendezvous with a binary asteroid system"]
-[5.505173206329346, 7.103984832763672, "[TT] Rate of the Data Transmission = 3 Mbit/s"]
-[5.406835079193115, 0.5566174387931824, "[TT] Planned Date of the Maneuvers = June 2015"]
-[11.836472511291504, 3.3534023761749268, "[TT] Thrust of the Steam Propulsion Unit = 4 mN"]
-[9.587444305419922, 4.225761890411377, "[TT] Sensor Quantity of the ADS = 3-axis magnetometer"]
-[4.089965343475342, 2.1113176345825195, "[TT] Launch Vehicle of the SEOSAT-Ingenio = Vega"]
-[6.493692874908447, 8.690913200378418, "[TT] Parameter of the Polarization sensitivity = < 2%"]
-[9.216347694396973, 6.841639995574951, "[FF] Vertical Resolution Requirement of the OMPS = Not provided"]
-[7.176855564117432, 5.388948440551758, "[FF] Quantity of the MP-900B = Unknown"]
-[4.6557793617248535, 4.836611270904541, "[TT] Monitoring of the AIS = Ships"]
-[6.0539937019348145, 3.4253249168395996, "[FF] Cost of the 3U Cubesat = Cheap"]
-[8.444189071655273, 3.1599934101104736, "[TT] Average Concentrations in 1960s of the Ozone Layer = 260 to 320 Dobson Units"]
-[5.948680877685547, -0.41700735688209534, "[TT] Expected Mission Duration of the DSX = At least a year"]
-[9.54684066772461, 7.110158443450928, "[TT] Spatial Resolution of the Global DEMs = About 30 m"]
-[6.710827350616455, 4.3831305503845215, "[FF] Project Role of the TU = Structural Design"]
-[10.913809776306152, 7.541025638580322, "[TT] Swath Width of the HRMX = 10 km"]
-[14.101393699645996, 3.09364914894104, "[TT] Mass of the Prichal Module = 4 metric tons"]
-[13.298320770263672, 7.454312324523926, "[TT] Power of the SSPA = 8 W"]
-[8.806396484375, 2.862302303314209, "[FF] Mission Goal of the SMEI = Understand and predict solar effects"]
-[9.60906982421875, 8.169775009155273, "[TT] Field Illumination of the WPM = Constant within \u00b1 3.0%"]
-[5.464995384216309, 6.094615459442139, "[TT] Memory of the OBC = Radiation-hardened SDRAMs (Synchronous Dynamic Random Access Memory)"]
-[7.639720439910889, -0.12738317251205444, "[FF] Contract Signing Date of the Arctic Weather Satellite = 09 March 2021"]
-[5.0644989013671875, 5.492856979370117, "[TT] Error Handling of the Tracking Mode = If the beacon strength suddenly drops, the control system sends a command to mute the Tx and switches to the gyro-holding mode"]
-[9.692090034484863, 8.295792579650879, "[TT] Field of View of the POLDER = \u00b151\u00ba across-track"]
-[9.487472534179688, 5.632506847381592, "[TT] CPA Azimuth Rotation Axis Distance of the LCT = More than 3\u00ba"]
-[8.68449878692627, 1.8104345798492432, "[TT] Storm Surge of the Hurricane Laura = 9 to 15 feet (3 to 5 meters)"]
-[13.532535552978516, 2.9270949363708496, "[TT] Payload Mass of the Satellite = ~1200 kg"]
-[13.45196533203125, 5.755921363830566, "[TT] Nominal Open Circuit Voltage of the Solar Array = 7.6 V"]
-[8.735555648803711, 7.844784259796143, "[TT] Channel of the INSAT-3D Imager = SWIR"]
-[8.095129013061523, 2.6425650119781494, "[FF] Orbit of the ISS = Permits study of diurnal (day to night) changes due to the effects of aerosols and clouds in the atmosphere"]
-[6.724854469299316, 2.9304280281066895, "[FF] Image Catalog of the DigitalGlobe\u2019s Geospatial Big Data platform = Expanded"]
-[11.036795616149902, 1.4862860441207886, "[TT] Mass of the Star Tracker = ~90 gram"]
-[5.460649490356445, -0.16180184483528137, "[FF] Current Status of the AeroCube-3 = Operating nominally as of summer 2009"]
-[9.297091484069824, 5.0898942947387695, "[TT] Attitude Determination of the BRITE spacecraft = 10 arcseconds"]
-[11.160780906677246, 5.22053337097168, "[FF] Post-flight Calibration of the Gas Scintillation Proportional Counter = Unknown"]
-[11.125179290771484, 5.041173458099365, "[TT] Open Pores Fraction of the MXT = 50"]
-[10.111339569091797, -2.700850486755371, "[TT] Quantity of the MMFU with NAND-Flash = 2"]
-[9.535511016845703, 8.291325569152832, "[TT] Field of View of the SSM/T-1 = 14.4\u00ba"]
-[11.550291061401367, 5.706247806549072, "[FF] Structure Components of the HIT-Sat = Four angle bars, six surface panels and two inner panels"]
-[5.492981910705566, 6.246465682983398, "[TT] Local Memory of the Optoelectronic System = 128 MB"]
-[3.3909225463867188, 4.646958351135254, "[FF] Synthetic Aperture Radar (SAR) of the Copernicus Sentinel-1A = Unknown"]
-[7.571422100067139, -0.599258542060852, "[FF] Public Archive Images of the ICEYE = Nearly 18,000 images taken between mid-2019 and the present"]
-[10.211979866027832, 5.738449573516846, "[TT] Cooling Temperature of the Focal Plane = 150 K"]
-[13.305195808410645, 6.717281818389893, "[TT] Power Supply for ISM Release of the Satellite = Two activations"]
-[4.6047844886779785, 1.2471767663955688, "[TT] Operational Date of the AlSat-2A = Feb. 2015"]
-[5.142935276031494, 0.5401343107223511, "[TT] Return Date of the NRCSD = Mid-September"]
-[6.135479927062988, 6.3754987716674805, "[TT] Report Schedule of the DCPs = Several times per hour to once every 24 hours"]
-[10.096210479736328, 0.9015234112739563, "[TT] Distance from Earth of the Thuban = About 270 light-years"]
-[5.558141708374023, 5.655553340911865, "[TT] Processor of the SCB = Motorola 68302"]
-[10.7735013961792, -0.2562999725341797, "[TT] Autonomy of the X-UGS = Full"]
-[9.150044441223145, 4.672565937042236, "[TT] Maximum Sun Off-Point of the Activity Attitude = 30\u00ba"]
-[7.815385341644287, 3.0101544857025146, "[FF] Content of the L2A Products = Ground reflectance cube, maps for estimated WV, AOT and image masks for land, water, haze, clouds, cloud-shadows and snow"]
-[10.723868370056152, 7.4935078620910645, "[TT] Swath Width of the SASS = 500 km"]
-[16.551633834838867, 3.64473819732666, "[TT] Number of Satellites in Orbit of the OneWeb = 74"]
-[4.32464599609375, 0.7257735729217529, "[FF] Break-up Date of the DMSP satellite = July 24, 2015"]
-[9.35595989227295, 6.069785118103027, "[TT] Image Orientation of the Galileo = The north pole of the moon is to the right"]
-[5.8831400871276855, 4.56685733795166, "[FF] Functionality of the SatBus 3C1 = On-board computer, Attitude determination & control subsystem, Communication subsystem"]
-[7.111649990081787, 5.888034343719482, "[FF] Predictability of the Clock = Errors at 100 minutes clearly below the nanosecond"]
-[14.619767189025879, 6.775940418243408, "[TT] Battery Capacity of the EPS = 125 Ah"]
-[6.211582183837891, 6.16060209274292, "[TT] Data Processing Time of the Ground Segment = Within an hour"]
-[10.252188682556152, 7.560237884521484, "[TT] Mount Type of the Telescope = English mount"]
-[12.785276412963867, 7.618263244628906, "[TT] Power of the Instrument = 35 W average"]
-[7.058009147644043, 7.3077592849731445, "[TT] Linewidth of the ATLAS lasers systems = <30 pm"]
-[7.341968059539795, 2.8077290058135986, "[FF] Purpose of the PIRPL = Collect data on the low Earth orbit environment"]
-[8.908195495605469, 4.382246494293213, "[FF] Reference Trajectory of the SASK = Constant relative range and with a direction that ensures the S/C are Sun aligned"]
-[9.700918197631836, -0.4189152717590332, "[TT] Perigee Altitude of the Satellite Constellation = ~ 300 km"]
-[8.268993377685547, -0.9825446605682373, "[TT] Ice Thickness of the Landsat 8 = 12 to 28 inches (30 to 71 cm)"]
-[3.3782968521118164, 5.295170307159424, "[TT] Transmission Frequency of the SAR = 1.275 GHz"]
-[10.156654357910156, -1.6573784351348877, "[TT] Inclination of the UniSat-3 = 98\u00ba"]
-[8.492244720458984, 8.136726379394531, "[TT] Spectral Resolution of the IMG = 0.1 cm-1"]
-[10.124619483947754, 5.829404830932617, "[TT] Primary Function of the JMR = Measure brightness temperatures"]
-[8.958416938781738, 0.9477836489677429, "[FF] Mission Purpose of the Parker Solar Probe = Study the Sun"]
-[9.647136688232422, 7.080577850341797, "[TT] Linear Resolution of the OLS = 0.56 km"]
-[6.169982433319092, 4.42084264755249, "[FF] Purpose of the SIM = Testing and validation of operational procedures and databases, support the training of operators, and execution of simulation campaigns"]
-[5.474521160125732, -0.07467764616012573, "[TT] Launch Date of the RapidEye = August 2008"]
-[7.654852390289307, 4.378973007202148, "[FF] Environmental Requirement of the ISL = Survive the harsh radiation environment"]
-[5.923068523406982, -0.5063560009002686, "[TT] Operation Requirement of the Laser = 24/7 for five years for the initial mission, with a possible six to seven years of extended mission after that"]
-[6.960799217224121, -0.7331404089927673, "[TT] Orbital Period of the Juno = 43 days"]
-[7.354597568511963, 0.24855506420135498, "[FF] Status Report Date of the OSIRIS-REx = Sept. 15, 2016"]
-[3.427201509475708, 5.005545616149902, "[FF] Bandwidth Transition Processing of the SAR Processor = Process for the \"lower performance\" i.e. when a switch occurs between 84 MHz and lower bandwidth, it extends the acquisition with the lowest bandwidth"]
-[6.884128570556641, 9.515279769897461, "[TT] NEDT at 300 K of the Band 9 = 0.2 K"]
-[10.184752464294434, 5.718240737915039, "[TT] Detector Cooling Temperature of the SWIR Spectrometer = 120 K"]
-[4.39891242980957, 6.8873724937438965, "[TT] Communication Frequency of the Spacecraft = S-band RF (radio frequency)"]
-[5.091004848480225, 3.0987918376922607, "[TT] Development Program of the HSB = ESA-ARTES program"]
-[11.571139335632324, 6.737349510192871, "[TT] Energy resolution of the Mirror = 138 eV @ 6 keV"]
-[9.716513633728027, -0.45769214630126953, "[TT] Altitude of the AOE-2 = Around 600km"]
-[7.233234882354736, 6.202220916748047, "[TT] Modes of the Payload 2 = VGA/QVGA"]
-[10.677398681640625, 4.040396213531494, "[FF] Attitude Demonstration Operations of the CanX-2 = Third quarter of 2008"]
-[11.495526313781738, 6.6670613288879395, "[TT] Energy Band of the eROSITA = 0.5-11 keV"]
-[5.4242167472839355, 2.988483190536499, "[TT] Program Manager of the WSF-M = Lt. Col. Wilfredo Ruiz"]
-[4.9662580490112305, 8.316242218017578, "[TT] RF Bandwidth (MHz) of the Antenna = 800"]
-[5.492127895355225, 7.025527000427246, "[TT] Payload Data Transmission Rate of the ResourceSat-1 = 105 Mbit/s"]
-[9.73930835723877, -1.1895414590835571, "[TT] Orbital inclination of the MEOSAR Constellation = 55\u00ba"]
-[6.879029750823975, -0.6303103566169739, "[TT] Orbital Period of the MPO = 2.3 hours"]
-[10.946420669555664, 1.4456175565719604, "[FF] Weight of the Neutron Stars = A teaspoon of one would weigh about a billion tons on Earth"]
-[6.016509056091309, 5.977441310882568, "[TT] Number of Modules of the T/R Modules = 512"]
-[3.3635077476501465, 5.259877681732178, "[TT] Number of TRMs of the CSG-SAR = 1280 @ H polarization and 1280 @ V polarization"]
-[3.937034845352173, 6.515301704406738, "[TT] UHF/VHF omnidirectional antennas of the TT&C = 2"]
-[7.955570697784424, 4.336388111114502, "[FF] Next Testing Steps of the TEMPEST-D = TVAC (Thermal Vacuum) testing and antenna radiation pattern testing"]
-[4.724737644195557, 0.9663493633270264, "[TT] End of Operations of the Resurs-P1 = 2021"]
-[7.79376220703125, 6.672026634216309, "[TT] Image Processing Rate of the ASAP-Light = 100 images/s"]
-[5.653584957122803, 3.7045276165008545, "[TT] Number of Maneuvers of the SkySat-7 = 14"]
-[9.873592376708984, 4.912712574005127, "[TT] Antenna Rotation Rate of the SAS = 18 rpm"]
-[8.978837013244629, 8.105056762695312, "[TT] IFOV/line (pixels/scan line) of the MWTS = 15"]
-[3.755504608154297, -1.0790883302688599, "[TT] Orbit Type of the STRV-1a = Elliptical GTO"]
-[4.7273030281066895, -0.2885446846485138, "[TT] Launch Date of the CATS = 10 Jan 2015"]
-[9.9318265914917, 7.504520416259766, "[FF] Swath Width of the Pushbroom imager = 20 km x 640 km (one pass)"]
-[8.330192565917969, 2.445627212524414, "[FF] URL of the Case studies of aerosol retrievals = http://glory.giss.nasa.gov/publications/2002_JAS_59_383.pdf"]
-[6.615813255310059, -0.4983070194721222, "[TT] Mission Duration of the WIND = Almost two complete solar cycles"]
-[12.930391311645508, 7.437544822692871, "[TT] Average power of the Spectrometer = 124 W"]
-[10.366203308105469, 1.7685177326202393, "[FF] Studies of the NuSTAR = Objects outside our solar system, such as exploding stars and disks of hot gas accelerated by the gravity of massive black holes"]
-[7.653135776519775, 3.4362244606018066, "[TT] Impact Experiment Initiation Year of the DebriSat = 2011"]
-[13.7538480758667, 3.6548309326171875, "[TT] Mass of the Cross dipole antenna = 7 kg"]
-[4.580512523651123, 0.9573768973350525, "[TT] Planned Launch Date of the SAOCOM-2A = 2025"]
-[8.099861145019531, 6.40259313583374, "[FF] Bidirectional Scanning of the Imager = Employed"]
-[9.828134536743164, 8.789730072021484, "[TT] IFOV of the Spectral Bands = 0.85 mrad (~700 m)"]
-[9.076029777526855, 2.9911272525787354, "[FF] Effect of the Solar Storms = Affected a variety of technological systems around the world"]
-[7.564739227294922, 7.663316249847412, "[TT] Dynamic Range of the RASAT = 6 bits"]
-[9.913045883178711, 7.01959753036499, "[TT] Spatial Resolution of the SeaHawk-1 = 130 meters"]
-[4.724344730377197, -1.229691743850708, "[TT] Mission Status of the Beijing-1 = Operating nominally in 2012"]
-[3.3681886196136475, 6.384427547454834, "[TT] Size of the 16.4 m antenna = 16.4 m"]
-[5.481490135192871, 1.323325514793396, "[TT] Image Acquisition Date of the ALOS = May 30, 2010"]
-[6.085170269012451, 3.419508934020996, "[FF] Satellite Quantity of the ASTERIA = 6"]
-[5.345208168029785, 3.1184937953948975, "[TT] Collaboration of the AstroRad vest = Lockheed Martin"]
-[7.172901153564453, 7.046818733215332, "[TT] Operating Temperature of the GEDI Laser = 350 (\u00b12)\u00baC"]
-[3.474090099334717, 6.43449068069458, "[TT] Length of the Antenna = 0.5m"]
-[6.0011420249938965, 5.113138198852539, "[FF] Digital Subsystem of the SCATSat-1 = Redesigned leveraging some of the recent efforts that have resulted in a smaller form factor for the digital system"]
-[8.124930381774902, -0.6741887331008911, "[TT] Arctic Sea-Ice Temporal Sampling of the CryoSat = 1 month"]
-[5.187495708465576, 6.973233222961426, "[TT] Downlink Data Rate of the Payload = 278 Mbit/s"]
-[9.281768798828125, 6.553116321563721, "[TT] Angle Resolution of the FSS = Up to 0.03\u00ba"]
-[9.289179801940918, 4.103172302246094, "[TT] Magnetometer Status of the Solar Orbiter = Good health"]
-[7.6707234382629395, 2.1792612075805664, "[TT] Primary Use of the Band 1 = Daytime clouds, ice and snow, vegetation"]
-[4.215473651885986, 7.348480701446533, "[TT] Spectrum of the Starlink and OneWeb = Ka-band"]
-[9.859478950500488, 2.691600799560547, "[FF] Deployment Services of the NanoRacks LLC = Small satellites"]
-[8.60487174987793, 2.0276501178741455, "[TT] Post-Processing of the Wind Vector Resolution = 12.5 km"]
-[12.03555679321289, -0.4122464656829834, "[TT] Mission Start Date of the TESS = April 15, 2019"]
-[3.465390920639038, 4.878178596496582, "[FF] Instrument Segments of the RISAT-SAR = Deployable SAR antenna subsystem, RF and baseband subsystems"]
-[9.005423545837402, 7.3750224113464355, "[TT] Resolution of the Optical Payload = 29 \u00b5rad/pixel"]
-[9.572064399719238, -1.1984025239944458, "[TT] Shift of the Launcher Trajectory = 20-degree to the south"]
-[13.187630653381348, 7.203091621398926, "[TT] Power Consumption of the FPA = < 1 watt"]
-[11.842144012451172, 0.028018780052661896, "[FF] Purpose of the TESS = Exoplanet Survey"]
-[7.554945468902588, 6.502074241638184, "[TT] Image Frequency of the Data Flow = One image per minute"]
-[13.466902732849121, 2.929124355316162, "[TT] Weight of the SPOT satellite constellation = 1869 kg"]
-[4.347488880157471, 7.095274448394775, "[TT] Communication of the SEOSat = S-band RF for TT&C data transmissions"]
-[4.8504557609558105, 3.3243443965911865, "[TT] Manufacturer of the SARah system = OHB and Astrium"]
-[4.465317726135254, 2.9582607746124268, "[TT] Location of the USMCC = NOAA in Suitland, MD"]
-[10.026008605957031, 7.82996940612793, "[TT] Optics Design of the ACE-FTS = Highly folded design"]
-[7.523133277893066, 3.8598549365997314, "[TT] Modes of Operation of the Alice = Airglow, Occultation"]
-[8.15504264831543, 6.8083600997924805, "[FF] Maximum Distance to Targets of the Cypress IBIS-5B CMOS sensor = Unknown"]
-[3.0784530639648438, 2.3565633296966553, "[TT] Frequency Bands of the Copernicus Sentinel-6 Poseidon-4 = C- and Ku-band"]
-[7.882989883422852, 9.010860443115234, "[TT] Wavelength of the Second Stage = 1645 nm"]
-[5.464524745941162, 6.019579887390137, "[TT] Static RAM of the C&DH subsystem = 512 kM"]
-[9.69101333618164, 0.32259759306907654, "[TT] Separation of the PROBA-3 = -145 m"]
-[10.2071533203125, 1.5288982391357422, "[TT] Number of Clusters of Galaxies of the eROSITA = More then 400"]
-[6.633249282836914, 5.7885236740112305, "[TT] Quantity of the RAMs = 6"]
-[4.90885066986084, 3.499720335006714, "[TT] Manufacturer of the Hiber-1 and-2 = Hiber Global"]
-[8.151205062866211, 7.942214488983154, "[TT] HRV Channel Detectors of the SEVIRI = 9"]
-[9.509065628051758, -1.399727463722229, "[TT] Eccentricity of the Explorer 36 = 0.03165"]
-[9.368959426879883, 5.077719688415527, "[TT] Yaw Axis Attitude Change of the TanSat = Approximately for 160\u00ba"]
-[8.192225456237793, 8.29715347290039, "[FF] Sensitivity Adjustment of the VNIR Detector = Through CVF (Charge to Voltage conversion Factor)"]
-[8.778764724731445, 9.430376052856445, "[TT] Spectroscopic System of the TANSO-CAI = Band pass filter"]
-[10.928739547729492, 7.587324142456055, "[TT] Swath Width of the AMSR3 = 1535 km"]
-[9.992618560791016, -1.6532381772994995, "[TT] Inclination of the CBERS-3 = 98.5\u00ba"]
-[13.616179466247559, 1.731242060661316, "[TT] Unpressurized Trunk Mass of the Dragon Resupply Vehicle = 960 kg"]
-[3.4349560737609863, 5.349236488342285, "[TT] Wavelength of the L-band Synthetic Aperture Radar (SAR) = 24 cm"]
-[5.87019157409668, -0.20102594792842865, "[TT] Time on ISS of the CIMON-1 = 14 months"]
-[7.804954528808594, 4.911235809326172, "[TT] Mounting of the Outer enclosure structure = Four corner flexures"]
-[11.304566383361816, 5.063803195953369, "[TT] Straw Tubes of the TRD = 5248 straw tubes"]
-[5.310708999633789, 0.7515372037887573, "[FF] Merger Date of the Spire = Aug. 17"]
-[5.661350727081299, 0.57618647813797, "[FF] Review Date of the GEOS-1 = 1978"]
-[7.843122482299805, 9.149908065795898, "[TT] Center Wavelength of the Red = 657.5 \u00b5m"]
-[3.7459633350372314, 4.5595197677612305, "[TT] SAR Videos Creation Time of the ICEYE = At least 20 seconds"]
-[6.4831390380859375, 5.816161155700684, "[TT] PRN of the GSAT-0211 = 2"]
-[4.880748748779297, 7.14550256729126, "[TT] S-band Uplink Data Rate of the Payload = 4 kbit/s"]
-[9.231325149536133, 8.103358268737793, "[TT] Target Distance of the LLNL imaging system = \u2264 300 km"]
-[13.410808563232422, 7.146031379699707, "[TT] Power of the PPL1 and PPL2 = 30 W peak power"]
-[5.894919395446777, 0.5922201871871948, "[FF] Data Collection Period of the OMI = More than 15 years"]
-[11.314545631408691, 4.155644416809082, "[TT] Size of the Eagle-2 ($50SAT) = 2.5U"]
-[8.389742851257324, 7.748233318328857, "[TT] Detector of the Spectral Band D = Si-PIN"]
-[7.014127254486084, -0.5110210180282593, "[TT] Ascending Node Time of the Odin = 18:00 hrs"]
-[11.719650268554688, 4.820828437805176, "[TT] Longitudinal Dimension of the HXT-C = 1400 mm"]
-[11.111628532409668, 5.873786449432373, "[TT] Shape of the Baffle = Closely follows the RX beam"]
-[13.836670875549316, 5.306875705718994, "[TT] Type of the Solar Arrays = Triple junction solar cells (GaAs)"]
-[3.833383798599243, 4.309988498687744, "[FF] Measurement domain of the SAR (RADARSAT-2) = Atmosphere, Ocean, Land, Snow & Ice"]
-[11.263228416442871, 0.9499247670173645, "[FF] Publication Date of the LISA = 15 May, 2018"]
-[3.899480104446411, 6.8967061042785645, "[TT] Polarization of the UHF transmitting antenna = Circular"]
-[10.050430297851562, 7.921844005584717, "[FF] Importance of the Full Width at Half Maximum (FWHM) = Critical for telescope performance"]
-[9.414344787597656, -0.6488705277442932, "[TT] Orbit of the AVUM = Required Disposal Orbit (1450 km x 304 km, i=69.5\u00ba)"]
-[4.802635669708252, -1.7733139991760254, "[FF] Panorama Camera (PCAM) of the Chang\u2019e-4 Rover = Payload"]
-[5.9981184005737305, 0.30532968044281006, "[TT] Image Time Interval of the Rosetta = 25 and 27 February 2015"]
-[7.639166355133057, 6.515796184539795, "[TT] Scan Mode 3 (Flex Mode) of the ABI = 15 minutes"]
-[14.593729972839355, 6.621211528778076, "[TT] Energy Storage of the AlSAT-1 = 4 Ah NiCd rechargeable battery"]
-[6.585227012634277, -0.2294960469007492, "[FF] Length of Operation of the Monitoring of HIS = Few minutes"]
-[6.127077102661133, -0.20929664373397827, "[TT] Testing Duration of the JUICE = Several weeks"]
-[8.427273750305176, 5.37343168258667, "[TT] Orbit Knowledge Accuracy of the Satellite = < 3 m rms in each axis"]
-[6.993795394897461, 7.772644519805908, "[TT] Reflection Coefficient of the Mayak = 95%"]
-[5.663746356964111, 2.2371060848236084, "[FF] Contact of the LAPAN = Robertus Heru Triharjanto"]
-[10.221441268920898, 5.4720139503479, "[TT] Thermal Dissipation Function of the APAA = Self-controlled"]
-[13.389355659484863, 7.263838291168213, "[TT] Peak Power of the DPS = 200 W/150 W"]
-[9.539641380310059, 4.0335774421691895, "[TT] Magnetic Field Measurement Channels of the IOF = 7"]
-[5.283071517944336, 4.5765604972839355, "[FF] Data path diversity of the Open5GCore Rel. 4 = Supporting local offloading and backhaul control"]
-[12.010074615478516, -0.4021749496459961, "[TT] Lunar Flyby Date of the TESS = 17 May"]
-[9.258683204650879, 7.107272624969482, "[TT] SWIR Off-nadir Resolution of the WorldView-3 = 4.1 m"]
-[6.328269004821777, 2.0914106369018555, "[FF] Reference Architecture of the PDHT = RADARSAT-2, COSMO SkyMed Constellation (FM1, FM2, FM3)"]
-[4.886515140533447, 7.257656574249268, "[FF] Data Transfer Rate of the XCOM = Gigabits per second"]
-[10.44520092010498, -1.3282842636108398, "[TT] Inclination of the SLATS = 98.3\u00ba"]
-[5.876528739929199, 4.345551490783691, "[FF] Function of the System satlets = Designed so each satlet constitutes a complete standalone system"]
-[7.72453498840332, 8.98659610748291, "[TT] Spectral Range (Band 3) of the MUX = 0.63-0.69 \u00b5m"]
-[3.4500503540039062, -0.8993813395500183, "[TT] Orbit Type of the MightySat II.1 (Sindri) = Sun-synchronous circular orbit"]
-[11.800178527832031, 6.755370140075684, "[TT] ESA: 12 eV-12 keV, ISA: 10 eV/ q-12 keV/q of the Energy Range = Energy range ESA: 12 eV-12 keV, ISA: 10 eV/ q-12 keV/q"]
-[9.339906692504883, -0.7866340279579163, "[TT] Quantity of the GEOS-1 = 1"]
-[9.011128425598145, 4.063533782958984, "[FF] Constraint of the Instrument = Avoid the sunlight intrusion in the payload CCD"]
-[9.552671432495117, 4.197684288024902, "[TT] Technology of the Magnetometer = Three-axis Anisotropic magneto-resistor"]
-[11.218952178955078, 4.94761848449707, "[TT] Size of the CCR = 1.0 inch"]
-[8.498443603515625, 5.1174163818359375, "[TT] Number of Micro-g Accelerometers of the Boom = 24"]
-[4.960243225097656, 1.6577599048614502, "[TT] Ground Surface Coverage of the Gokturk-2 = 9,850,000 km2"]
-[6.48063850402832, -0.7203459143638611, "[TT] LTDN of the WorldView-3 = 13:30 hours"]
-[9.273681640625, 2.2157235145568848, "[TT] Source of the Most Intense Auroras of the Jupiter = Not the observed electric potentials"]
-[5.582577705383301, -0.05973602458834648, "[FF] Mission Design of the RapidEye = G. Tyc, J. Tulip, D. Schulten, M. Krischke, M. Oxfort"]
-[13.966131210327148, 7.188077449798584, "[TT] Current of the Voltage 7 = 475"]
-[3.992949962615967, 4.197193622589111, "[TT] Operation Status of the RISAT-1 = Nominal"]
-[3.4551661014556885, -0.8460910320281982, "[TT] Orbit of the Synthetic Aperture Radar Instrument = 690 km polar orbit"]
-[5.394160270690918, 1.4638763666152954, "[TT] Launch Date of the OrbView-2 = August 1, 1997"]
-[10.941829681396484, 7.555065631866455, "[TT] Swath Width of the COSI = 100 km"]
-[8.882230758666992, 3.3418056964874268, "[FF] Purpose of the Ionosphere = Study its changes"]
-[8.948309898376465, 5.327754497528076, "[TT] Orbit Shift Distance of the GomX-4B = 300 km"]
-[6.621208667755127, 5.509579181671143, "[TT] Type of the Castor = Active"]
-[6.65968132019043, 4.098272323608398, "[FF] Operation Life of the FG = Unknown"]
-[7.720321178436279, 9.383889198303223, "[TT] Center Wavelength of the MS1 (NIR1) = 831 nm"]
-[4.929372310638428, 1.082003116607666, "[TT] Copyright of the eoPortal = 2024"]
-[5.480053424835205, 6.375334739685059, "[TT] On-board Data Storage of the Spacecraft = 2 GByte"]
-[5.261316299438477, 0.45408162474632263, "[FF] Mission Presentation Date of the CYGNSS = March 2-9, 2013"]
-[12.721097946166992, 1.9556728601455688, "[FF] Science Objectives of the SAGE-III = Extend the SAM II, SAGE I and SAGE II self-calibrating solar occultation data sets"]
-[13.773025512695312, 2.9006388187408447, "[TT] Mass of the Spacecraft = 447 kg"]
-[4.7239861488342285, 7.058119773864746, "[TT] Data Rate of the X-band downlink system = Up to 80 Mbit/s"]
-[14.205967903137207, 3.2838926315307617, "[TT] Mass of the MSU-SK = 21kg"]
-[5.385765552520752, 8.7775297164917, "[TT] Bandwidth of the Band 3 = 0.256 \u00b5m (13 cm -1)"]
-[9.45447063446045, 3.595259666442871, "[FF] Potential Return of the Magnetic Pole = Canada"]
-[7.222684383392334, 5.3936309814453125, "[TT] Data Transmission Frequency of the HRC Instrument = At least once per orbit, or every 90 minutes"]
-[8.465847969055176, 4.641916275024414, "[FF] Sensor Complement/Experiment of the TechnoSat = Camera, Fluiddynamic Actuator, S-band transmitter HISPICO, Laser Retroreflectors, Solar Generator Impact Detector, Star Tracker STELLA, Reaction Wheel System"]
-[7.093100547790527, 2.4317338466644287, "[FF] Imaging of the Ikonos-2 = Continues to provide imagery of the Earth"]
-[8.888420104980469, 9.542386054992676, "[FF] Band 4 Resolution of the TANSO-FTS-2 = 0.2 cm -1"]
-[5.0184149742126465, 8.00916862487793, "[TT] Frequency source of the NGSLR = Maser"]
-[10.187328338623047, 7.560239791870117, "[TT] Optics System of the Telescope = Ritchey-Chretien type, with 2 aspherical mirrors and 3 folding mirrors"]
-[12.69681453704834, 1.9123756885528564, "[FF] Measurements of the SAGE-III = Vertical distribution of aerosols and ozone, temperature in the stratosphere and mesosphere, profiles of trace gases such as water vapor and nitrogen dioxide"]
-[6.01320219039917, 3.286485433578491, "[TT] Satellites of the MHS = NOAA-N (NOAA-18) and NOAA-N' (NOAA-19)"]
-[11.436549186706543, 3.5298328399658203, "[TT] Manufacturer of the Solar Electric Propulsion (SEP) Chassis = Maxar Technologies"]
-[5.310642719268799, 3.3786909580230713, "[FF] Technology Management Contractor of the Heinrich Hertz satellite = OHB"]
-[5.7328996658325195, 1.6847821474075317, "[FF] URL of the ALOS PRISM = http://www.isprs-ann-photogramm-remote-sens-spatial-inf-sci.net/II-4/71/2014/isprsannals-II-4-71-2014.pdf"]
-[8.130804061889648, 2.178288698196411, "[FF] FY22 Budget of the CloudSat = Unknown"]
-[9.46627426147461, 7.103586673736572, "[TT] Spatial Resolution of the GLI = 7.8 km"]
-[8.896925926208496, 7.716915130615234, "[TT] Focal Plane Size of the CMOS Active Pixel Sensor = 4.3 mm x 3.2 mm"]
-[10.014375686645508, 2.7149746417999268, "[TT] Orbit Type of the NanoRacks-QB50 CubeSats = Near-circular"]
-[7.0672407150268555, 1.4364655017852783, "[FF] Release Date of the Wide-Field Imager for Solar Probe Plus = July 2016"]
-[5.36696720123291, 3.869171380996704, "[TT] Number of Satellites of the FORMOSAT-7/COSMIC-2 = 6"]
-[9.312439918518066, 5.106268882751465, "[TT] Pointing/Attitude Error Signal Cadence of the Data Processing Unit (DPU) = 2.5 s"]
-[4.860011100769043, -0.03791183605790138, "[TT] End of Life Date of the TAIKI = 31 December 2028"]
-[13.285874366760254, 7.033755779266357, "[FF] Power Transmission of the IOV Payload = Flexible"]
-[6.165650844573975, -0.46381211280822754, "[TT] Time Span of the GF-3 = 29 days"]
-[10.933956146240234, 7.493125915527344, "[TT] Swath Width of the SSM/T-1 = 1500 km"]
-[8.270021438598633, 3.4598236083984375, "[FF] Purpose of the TOPCAT = Ionospheric study based on GPS measurements"]
-[11.643094062805176, 4.526862621307373, "[TT] Min. Depth of the Shipboard Thermosalinograph = 5 m"]
-[6.0022783279418945, 1.778464674949646, "[FF] Deployment and Retrieval of the Eureca = Unknown"]
-[9.961587905883789, 3.107250213623047, "[FF] Mission Objectives of the BeaverCube = Demonstrate the use of a CubeSat platform to gather important ocean and atmospheric measurements, support teaching and outreach"]
-[9.756942749023438, -0.5601056218147278, "[TT] Orbit Altitude of the T/P = 1336 km"]
-[4.467835426330566, 2.9895639419555664, "[TT] Location of the BSOCC = Just about 10 miles northeast of the GSFC"]
-[4.595810890197754, 7.407716751098633, "[TT] VHF-band FSK Channels Data Rate of the UoSAT-12 = 9.6 kbit/s"]
-[9.454055786132812, 3.6199026107788086, "[FF] Shape of the Earth\u2019s magnetic field = Not specified"]
-[8.309289932250977, 5.380111217498779, "[TT] Orbit Accuracy of the DORIS = 3-10 cm radial distance"]
-[7.237983703613281, 8.17742919921875, "[FF] Parameter of the GOSAT-2 CAI-2 = Value"]
-[10.699502944946289, 1.0913761854171753, "[TT] Diameter of the 55 Cancri e = Almost twice that of Earth"]
-[7.578453063964844, 8.01220989227295, "[TT] Dynamic Range (solar) of the ScaRaB = up to 425 W m -2  sr -1"]
-[11.091060638427734, 5.339128017425537, "[TT] Material of the LARES-2 = Single block of material"]
-[9.406356811523438, 0.9948660135269165, "[TT] Measurement Depth of the Juno = About 3,000 km"]
-[4.910064220428467, 5.725711345672607, "[FF] Payload of the MDASat-1 = SDR-based payload that will provide AIS and VDES services"]
-[9.00342082977295, 7.409112453460693, "[TT] Pixel Resolution of the GLI = 400 x 600 pixels"]
-[5.09879207611084, 2.9595563411712646, "[TT] Provider of the MetOp-B = EUMETSAT"]
-[5.857933044433594, 1.1529217958450317, "[FF] Operation Support of the GeoXO = Weather, ocean, and climate operations in the United States"]
-[10.659280776977539, 1.0897988080978394, "[TT] Size of the HD 260655 c = 1.5 times as big around as Earth"]
-[10.784004211425781, -0.2447148561477661, "[TT] Magnetic Storm Observation Date of the TWINS = 22 July 2009"]
-[7.314343452453613, 8.842541694641113, "[TT] Filter Type of the VIS channel = Block with Aluminum"]
-[5.678971290588379, 2.1742494106292725, "[TT] Operations Team Size of the ASTERIA = 7 to 10 JPL staff members"]
-[8.520589828491211, 7.430676460266113, "[TT] Architecture of the DU = Figure 37"]
-[4.567592620849609, 0.1076463982462883, "[FF] Test Campaign Date of the Smile = 21 April 2022"]
-[4.178099632263184, 1.3156864643096924, "[TT] Operational Duration of the Meteosat-7 = 17 years"]
-[4.814934730529785, 0.6118578910827637, "[TT] Launch Date of the F-16 = Oct. 18, 2003"]
-[8.491195678710938, -0.08977126330137253, "[TT] Diameter of the South Pole-Aitken Basin = Roughly 2,500 km"]
-[8.707329750061035, 8.61600112915039, "[TT] Pixels per FWHM of the Spectrometer = 1400"]
-[13.80661678314209, 2.672966241836548, "[TT] Launch Mass of the Kanopus-V = ~ 450 kg"]
-[8.447582244873047, 2.164215087890625, "[FF] Purpose of the SeaWinds scatterometer = Earth observation"]
-[8.076114654541016, 0.11109413206577301, "[TT] Predecessor Missions of the TOPEX/Poseidon = GEOS-3, SEASAT, GEOSAT"]
-[8.150069236755371, 6.515033721923828, "[FF] Problem of the Advanced Baseline Imager (ABI) = Blockages in its radiator by FOD (Foreign Object Debris)"]
-[7.621992588043213, 0.6746349334716797, "[FF] Purpose of the Queqiao = Bridge between Earth and the far side of the moon"]
-[3.4847493171691895, -0.8498519062995911, "[TT] Orbit Type of the PARASOL = Sun-Synchronous Orbit (SSO)"]
-[4.703539848327637, 6.469489574432373, "[TT] Telemetry of the RF Communications = CW"]
-[3.7554080486297607, 6.489471912384033, "[TT] Antenna Type of the AMSR = Offset Parabolic"]
-[3.7279369831085205, -1.0830262899398804, "[TT] Orbit Type of the MPO = Lower elliptical orbit"]
-[3.652857780456543, 6.519068717956543, "[TT] Antenna Type of the SMMR = Parabolic reflector"]
-[5.149399280548096, 1.0219521522521973, "[FF] Announcement Date of the European Commission = 8 October 2018"]
-[5.902336597442627, 1.5306406021118164, "[FF] Propulsion System Commissioning Date of the PRISMA Satellites = June 24, 2010"]
-[7.78041934967041, 8.982768058776855, "[TT] Value of the Sprite Volume Radiance = 1.1 x 1012 photons/s/m3/sr at 762 nm"]
-[9.179999351501465, 3.4227206707000732, "[FF] Objective of the TRACE = Study the three-dimensional magnetic structures of the sun"]
-[5.421632766723633, 4.544681549072266, "[TT] Operation Mode of the Ground Segment = Store-and-forward"]
-[8.820999145507812, 3.3810408115386963, "[FF] Measurement of the DCP = In-situ ionosphere plasma density"]
-[9.020430564880371, 3.3392350673675537, "[FF] Plasma Irregularities Model of the C/NOFS = Equatorial plasma bubbles age and irregularity spectra evolution"]
-[4.013130187988281, 2.139444589614868, "[FF] Launch Manifest of the Ariane = Unknown"]
-[4.463406562805176, 7.599919319152832, "[TT] Bandwidths of the Ku-band = 320, 80 and 20 MHz"]
-[13.324713706970215, 2.9545302391052246, "[TT] Payload Mass of the GHGSat-D = 9 kg"]
-[3.9362568855285645, 9.717672348022461, "[TT] Frequency (GHz) of the ICI-4 = 243.2\u00b12.5"]
-[9.510674476623535, 7.035942554473877, "[TT] Vertical Resolution of the MAHRSI = 2 km"]
-[5.105391502380371, 4.350180149078369, "[TT] Number of Satellites of the Starlink Group 4-14 = 53"]
-[5.022955894470215, 1.0394631624221802, "[TT] Debut Flight Date of the Dellingr = 2 Aug.2017"]
-[6.417268753051758, 0.8845855593681335, "[FF] Mission Status of the FormoSat-2 = Currently operating"]
-[9.512470245361328, 7.134142875671387, "[TT] Spatial Resolution of the Stripmap = 10 m"]
-[5.519119739532471, 3.1459479331970215, "[FF] Design and Build of the GLM = Lockheed Martin"]
-[4.141104221343994, 2.2410550117492676, "[TT] Launch Vehicle of the DubaiSat-2 = Dnepr"]
-[8.097281455993652, 4.26905632019043, "[TT] Type of the TSIS-1/SIM = Earth radiation budget radiometers"]
-[6.7525458335876465, -1.8624995946884155, "[FF] Components of the Jason-1 Ground Segment = Altimetric and Orbitography Mission Center (SSALTO), located in Toulouse and the Jason Science Data System at JPL in Pasadena"]
-[7.000491142272949, 1.888179898262024, "[FF] Instrumentation of the SAC-D = CONAE and NASA"]
-[9.123546600341797, 2.8522064685821533, "[FF] Technique Developers of the Solar Flare = Charles Lindsey and Douglas Braun"]
-[6.367670059204102, -1.1638069152832031, "[TT] LTAN of the KOMPSAT-1 = 10:50 hours"]
-[9.994918823242188, 3.8054721355438232, "[FF] Potential Use of the UniSat-2 = Future precise attitude control of a nanosatellite"]
-[7.263864994049072, 7.422468662261963, "[FF] Drawback of the Photon Sieve = Limited bandwidth"]
-[10.37649917602539, 3.29781174659729, "[FF] Type of the GRIFEX = 3U CubeSat flight test experiment"]
-[3.5992090702056885, 5.144611835479736, "[TT] Single-look Resolution of the Radar = 250 m x 400 m"]
-[8.691174507141113, 5.948484897613525, "[TT] Centroidization Accuracy of the Coarse Lateral Sensor = 0.1 camera pixels (3.5 arcsec)"]
-[9.988001823425293, 4.6058220863342285, "[TT] Attitude Actuation of the QuickBird-2 = Reaction wheels"]
-[9.848359107971191, 4.895737171173096, "[TT] Antenna Rotation Speed of the SeaWinds = 18 rpm"]
-[6.553028106689453, -0.5498409271240234, "[TT] Total Transfer Time of the Transfer Orbit = 3 to 4 months"]
-[6.852895259857178, -0.6858800053596497, "[TT] Orbit Raising Time of the Safran/Snecma PPS-5000 = Approximately four months"]
-[7.674373149871826, 8.533452033996582, "[TT] Bandpass Filters of the EXI = 3 UV bands and 3 visible (RGB) bands"]
-[6.934558868408203, 1.5456924438476562, "[TT] Observation Target of the James Webb Space Telescope = TOI-4329"]
-[6.270487308502197, 8.066804885864258, "[TT] Channels of the AMSU = 20"]
-[5.37026834487915, 3.937998056411743, "[TT] Number of Satellites of the Terra Bella = 13"]
-[10.748034477233887, 7.317249774932861, "[FF] Footprint Size of the Footprint size of beams = 76 km x 94 km, 84 km x 120 km, 96 km x 156 km"]
-[5.802779674530029, 3.2555203437805176, "[FF] Size of the Legion satellites = Smaller than the earlier generations"]
-[5.417288303375244, 2.7629849910736084, "[FF] Operator of the MEIDEX = Israeli Payload Specialist (PS) or a backup crew member"]
-[11.800944328308105, 4.969163417816162, "[TT] Size of the PICOSAT = 25 mm x 75 mm x 100 mm"]
-[5.323730945587158, 0.6080172657966614, "[TT] Discovery Date of the 2020 GE = March 12, 2020"]
-[5.7251434326171875, -0.16742730140686035, "[TT] Mission Life of the GeoEye-1 = 7 years"]
-[4.41792631149292, 0.12708745896816254, "[TT] Starlink Satellites Launch Date of the SpaceX = 16 February 2021"]
-[10.281323432922363, 5.5375566482543945, "[TT] Cooler of the Argus = Programmable Peltier-effect cooler"]
-[7.5038743019104, 6.9127302169799805, "[TT] Cadence of the Dose Rate = 1 minute"]
-[13.770356178283691, 3.1357204914093018, "[TT] Mass of the CICERO satellites = Approximately 10 kg"]
-[6.979971885681152, 1.961764931678772, "[FF] Data Quality Assessment of the Landsat-7 ETM+ = Not provided"]
-[10.898781776428223, 7.372518539428711, "[TT] Swath of the Sentinel-2 = 290 km"]
-[4.777665138244629, 7.409130096435547, "[TT] Frequency Bandwidth Allocation of the XMOD = 375 MHz"]
-[8.954615592956543, 9.384410858154297, "[TT] Spatial resolution of the TANSO-CAI = 500 m"]
-[11.010555267333984, 4.773910045623779, "[TT] Tether Pull Force of the ENT = Up to 40-50 N"]
-[10.716936111450195, 1.116966962814331, "[TT] Size of the TOI 270 b = 25% larger than Earth"]
-[7.450859069824219, 0.7563356757164001, "[FF] Orbit of the LunaH-Map = Stable circular orbit"]
-[3.4700264930725098, 1.7491049766540527, "[FF] Conference Presentation Date of the Sentinel-1 = July 22-27, 2012"]
-[4.8363847732543945, 0.4995318055152893, "[TT] Launch Date of the PSat-2 = June 25, 2019"]
-[7.042199611663818, 4.410977840423584, "[FF] Quantity of the RMK-2 = Unknown"]
-[6.3935370445251465, -0.48948049545288086, "[TT] Duration of the Satellite Orbit = Ten years"]
-[5.060959815979004, 1.9707133769989014, "[TT] Status of the MWR = Fully operative"]
-[10.534957885742188, 1.9751079082489014, "[FF] Description of the Model = Describes the gamma-ray emission of pulsars detected by Fermi and combines this information with three parameters that determine the pulsar emission"]
-[6.610790252685547, 3.9722328186035156, "[FF] User Segment Responsibility of the MANTIS = Creation and distribution of added-value products (Level 2+)"]
-[10.903550148010254, 7.561184883117676, "[TT] Swath Width of the POLDER-2 = 2400 km"]
-[3.7565226554870605, -1.0786762237548828, "[TT] Orbit Type of the S/C = High elliptic"]
-[7.950911998748779, 6.2793121337890625, "[TT] Type of the KMSS = Imaging multi-spectral radiometers (vis/IR)"]
-[11.738485336303711, 3.2924869060516357, "[TT] Quantity of the Thrusters = 4"]
-[5.64616060256958, -0.8217916488647461, "[TT] Nominal Design Life of the INSAT-3D = 7.7 years"]
-[5.324634075164795, 1.4119051694869995, "[FF] Conference Date of the CHIPS = Aug. 21-24, 2000"]
-[5.478869915008545, 6.435940265655518, "[TT] Data Storage Capacity of the SET = Up to 10 GByte"]
-[9.878076553344727, 2.811441659927368, "[FF] Functionality of the HISat = Complete satellite functionality in a nanosat-scale package"]
-[13.875951766967773, 2.7676498889923096, "[TT] Launch Mass of the MSG-3 = ~2000 kg"]
-[12.213038444519043, -0.20841462910175323, "[TT] Image Capture Frequency of the TESS = Every 10 minutes"]
-[10.155165672302246, 1.5513986349105835, "[FF] Image Content of the eROSITA = A3391/3395 system of interacting clusters of galaxies"]
-[9.598068237304688, -0.3786846697330475, "[TT] Altitude of the COMPASS-1 = 830 km"]
-[7.910820960998535, 8.844483375549316, "[TT] Center Wavelength of the Pan (WorldView-1) = 650 nm"]
-[5.101790904998779, 1.1151063442230225, "[TT] Development Start Date of the SMOS = 1992"]
-[10.984810829162598, 6.331111907958984, "[TT] Structure Material of the Infrared Imager = CeSiC (Carbon-fiber reinforced Silicon Carbide)"]
-[8.169663429260254, 0.09095083177089691, "[TT] Launch Date of the Meteor-2-1 = 11.07.1975"]
-[5.230374336242676, 3.1102936267852783, "[TT] Operator of the Bartolomeo = Airbus"]
-[7.202969551086426, 4.48231840133667, "[FF] Component of the Worksite Interface Fixture (WIF) = Unknown"]
-[7.978092193603516, 13.68568229675293, "[TT] SSD of the B6 = 20 m"]
-[9.87596607208252, -0.43042340874671936, "[TT] Altitude of the BlackSky Global Satellite = 450 km"]
-[12.172953605651855, -0.12709352374076843, "[TT] Camera of the TESS = Single detector"]
-[9.418071746826172, 7.060449123382568, "[TT] Spatial Resolution of the MSI = 10 meter"]
-[3.3094115257263184, 5.112702369689941, "[TT] Incidence Angle Coverage of the RISAT-SAR = 12\u00b0- 55\u00b0"]
-[8.643793106079102, 8.789443969726562, "[TT] Spectral Resolution of the Grating Spectrometer = Approximately 6nm"]
-[6.248068809509277, 1.5168532133102417, "[TT] Observation Status of the GPM Core Observatory = Normal"]
-[6.319338321685791, 1.918511152267456, "[FF] Report URL of the AAUSAT3 = http://zcuba.dk/reports/08gr633.pdf"]
-[5.1001973152160645, 1.0668785572052002, "[TT] Flight Unit Fabrication and Testing Completion Date of the OCSD = Mid 2016"]
-[4.112277984619141, 4.3777174949646, "[TT] Subsystems of the RISAT-1 = Around 1400"]
-[10.051461219787598, 1.4467425346374512, "[FF] Purpose of the Gaia = Measure the positions and motions of stars in our Milky Way galaxy"]
-[6.398956775665283, 2.7249951362609863, "[TT] Daily Revisit of the RCM (RADARSAT Constellation Mission) = Average daily revisit"]
-[10.076559066772461, 1.3106547594070435, "[TT] Distance of A3391/3395 system of the eROSITA = About 800 million lightyears"]
-[8.008965492248535, 8.93825912475586, "[TT] Emission Wavelength of the CuPID = 30.4 nm"]
-[10.221579551696777, 2.7442126274108887, "[TT] Launch Date of the NanoSat-1B = 29 July 2009"]
-[10.773774147033691, 3.8670318126678467, "[FF] Technology of the LOFTID = Hypersonic Inflatable Aerodynamic Decelerator (HIAD)"]
-[4.8192524909973145, 0.5280476212501526, "[TT] First launch date of the GPS III (9+) = Planned 2020"]
-[10.545119285583496, 6.010107040405273, "[TT] Temperature Sensitivity of the NuSTAR = More than 5.4 million degrees Fahrenheit"]
-[4.943481922149658, 8.011760711669922, "[TT] Length of Transmit Signal of the ALScat = 1 ms"]
-[5.7373480796813965, 4.839308738708496, "[FF] Netherlands-China Low-Frequency Explorer (NCLE) of the Relay Satellite = International Joint Collaboration Payload"]
-[7.855929851531982, 1.607651948928833, "[FF] Mission Type of the GPM = Rainfall Measurement"]
-[4.725125789642334, 8.157354354858398, "[TT] Range of Bandwidths of the Radar = 14 / 28 / 42 / 84 MHz"]
-[6.876617908477783, 7.473214626312256, "[TT] Bit Resolution of the ADCs = 16 bit"]
-[5.55893611907959, 0.6694179177284241, "[TT] Exploration Date of the Ultima Thule = January 1, 2019"]
-[7.839877605438232, 5.687765598297119, "[FF] Modes of the Camera System = Automatic target pointing, Interactive operation"]
-[5.4909820556640625, 0.35231250524520874, "[TT] Launch Date of the GEOS-1 = 6 November 1965"]
-[5.334792613983154, 1.114393949508667, "[FF] Operation Guide Date of the SOMP = March 5, 2013"]
-[10.139813423156738, 8.085082054138184, "[TT] Effective Focal Length of the Telescope = 8.66 m"]
-[7.938333511352539, 2.3690786361694336, "[FF] Application of the NIRST = Fire and sea surface temperature measurement"]
-[8.91297435760498, 3.150357484817505, "[FF] Objectives of the SUVI = Power blackout forecasts due to solar flares"]
-[4.784435749053955, 7.13923978805542, "[TT] Downlink Rate Support of the X50 S-band transceiver = 2-4 Mbit/s"]
-[6.442576885223389, 1.4111992120742798, "[FF] Conference Date of the COSMO-SkyMed = Nov. 27-29, 2006"]
-[11.213281631469727, 5.87066125869751, "[FF] Thermal Coatings of the Spacecraft = 27% gold, 25% silvered Teflon, and 48% polished Al 6061-T6"]
-[7.514339923858643, 2.084104061126709, "[FF] Product of the Climate Change Initiative = Maps that provide a global view of above-ground biomass"]
-[7.552002429962158, -2.463675022125244, "[FF] Launch Date of the GOLD = Unknown"]
-[1.3248125314712524, 1.9007775783538818, "[TT] Total Cargo Delivery of the HTV-7 = 6.2 metric tons"]
-[5.377251625061035, 1.4142684936523438, "[FF] Observation Date of the ACE - Advanced Composition Explorer = April 21, 2016"]
-[5.01518440246582, 2.5948374271392822, "[FF] Location of the GOLD = Goddard Space Flight Center in Greenbelt, MD"]
-[13.879549980163574, 2.785236358642578, "[TT] Launch Mass of the Resurs-DK1 = about 6570 kg"]
-[5.578960418701172, 0.5499659776687622, "[TT] Mapping Completion Date of the ERS-1 = March 1995"]
-[8.09891414642334, 9.220739364624023, "[TT] Wavelength of the Responsivity Measurement = 1064 nm"]
-[10.327960968017578, 4.537168979644775, "[TT] Reaction Wheels Torquing Capability of the RISAT = 0.3 Nm"]
-[13.29839038848877, 7.482338905334473, "[TT] Amplification of the SSPA = 2 W"]
-[4.782052516937256, 7.892279624938965, "[TT] Frequency of the 406 MHz EPIRB = 406 MHz"]
-[10.263317108154297, 2.155609369277954, "[TT] Imaging Capability of the Chandra = Capturing intricate details in X-rays"]
-[14.189504623413086, 3.1643195152282715, "[TT] Mass (kg) of the IceEye-1 = 80"]
-[11.408966064453125, 5.32611083984375, "[TT] Area of the GDS = 100 cm2"]
-[10.755597114562988, -1.1385222673416138, "[TT] Altitude of the SLATS = 268 and 220 km for more than 31days, 250, 240, 230, 220 and 180 km for more than 7 days"]
-[4.380222797393799, 0.6314527988433838, "[TT] Launch Date of the DMSP-F17 = November 2006"]
-[8.592580795288086, 3.8496081829071045, "[TT] Number of Instruments of the Space Environmental In Situ Suite (SEISS) = 1"]
-[7.172031402587891, 3.8966822624206543, "[FF] Trajectory Analysis and Design Presentation of the OMOTENASHI = 31st ISTS (International Symposium on Space Technology and Science)"]
-[5.885731220245361, 3.096320629119873, "[TT] Responsible Agency of the JPSS = NOAA"]
-[9.35424518585205, -0.31686875224113464, "[TT] Perigee of the COMPASS-2 = 402 km"]
-[5.189160346984863, 0.4660840928554535, "[FF] Establishment Timeline of the PROSWIFT Act = Within 12 months of its enactment"]
-[5.6935601234436035, 0.6241180896759033, "[FF] Data Return of the LIRIS = September 2014"]
-[3.5567097663879395, 6.446583271026611, "[TT] Size of the Ground station antenna = 21 m"]
-[4.339136600494385, 6.835965633392334, "[TT] VHF-UHF Transceiver of the IOD-1 GEMS = CPUT (Cape Peninsula University of Technology) VHF-UHF Transceiver (VUTRX) with CSL ADM (Antenna Deployment Mechanism)"]
-[5.514990329742432, 5.659276485443115, "[TT] Processor of the ROSA = ADSP 21020"]
-[9.805174827575684, 8.126764297485352, "[TT] Optics Focal Length of the Camera 2 = 6 mm"]
-[11.668405532836914, 4.583667278289795, "[TT] Primary Semi-Major Axis of the Didymos = 1.1 km"]
-[8.960068702697754, 4.468172073364258, "[TT] Quantity of the Sun sensors = 5 (1 Fine and 4 Coarse)"]
-[7.893987655639648, 3.0963592529296875, "[TT] Tracked Gases of the GeoCarb = Atmospheric carbon dioxide, carbon monoxide and methane"]
-[8.5001859664917, 1.942659616470337, "[FF] Kinematic properties of the Ejecta cloud = > 0 km/s"]
-[4.523657321929932, 7.838010311126709, "[FF] Band of the DTL = UHF band (467.7 MHz)"]
-[7.518569469451904, 9.030138969421387, "[FF] Optics Components of the MSASI = Fabry-Perot etalon and a temperature-stable narrow band filter"]
-[5.200819492340088, 2.300668239593506, "[TT] Mission Type of the NeuSAR = EO"]
-[6.396176815032959, 2.9547650814056396, "[FF] Contains of the Ralph = SEDS (Small Expendable Tether Deployer System) box"]
-[13.867949485778809, 3.5602731704711914, "[TT] Launch Mass of the Telescope = 4166 kg"]
-[13.388340950012207, 6.876158714294434, "[TT] Transponder Power of the TRACE spacecraft = 5 W"]
-[4.844426155090332, 3.0865395069122314, "[TT] Company Headquarters of the SAR Satellites = San Francisco, California"]
-[5.778660774230957, 4.848529815673828, "[FF] Ground Contact Reset of the C&DH = Full reset after a prolonged period without ground contact"]
-[13.256888389587402, 5.25339412689209, "[FF] Margins of Safety of the AM structure, PM structure, ESPA ring, solar array panels, bulkheads, brackets = 8.5 g\u2019s in two directions simultaneously, 12 g\u2019s in each of three directions individually"]
-[4.280299663543701, 3.299994468688965, "[FF] Control Centers Locations of the Galileo = Fucino (Italy) and at the DLR site in Oberpfaffenhofen"]
-[7.388947486877441, 4.208165645599365, "[FF] Calibration Status of the GMI (GPM Microwave Imager) = Continued"]
-[3.5228734016418457, -0.8848400712013245, "[TT] Orbit Type of the AlSat-2B = Sun-synchronous orbit"]
-[6.353218078613281, 5.63890266418457, "[TT] Outputs of the CDSU = Pulsed power outputs (both at 12 V and at the bus voltage)"]
-[7.111167907714844, 2.720015525817871, "[FF] Imaging Mission of the SEOSAT-Ingenio = High-resolution land imaging"]
-[11.750290870666504, 6.540924072265625, "[TT] Monitor of the MPS-HI = Medium and high energy protons and electrons"]
-[7.3955488204956055, 2.387701988220215, "[TT] Data Sampling Rates of the \u00d8rsted satellite = 1 to 100 samples/s"]
-[8.495229721069336, 5.38357400894165, "[TT] Position Accuracy (RMS orbit) of the S-1 NTC = 5 cm (3D)"]
-[7.9878411293029785, 5.329568862915039, "[TT] Mid-range of the FLLS system = 7 \u2013 70 m"]
-[7.601241111755371, 6.4642109870910645, "[FF] Function of the Arc Monitoring Circuit = Detects arc"]
-[8.899076461791992, 0.5371438264846802, "[TT] Location of the ALICE = Boulder, CO, USA"]
-[6.650639057159424, 0.8131391406059265, "[TT] Launch Date of the Herschel Telescope = May 14, 2009"]
-[11.18643569946289, 0.6161936521530151, "[FF] Capability of the CHEOPS = Determine accurate radii for exoplanets"]
-[10.020735740661621, -1.5737236738204956, "[TT] Inclination of the COMPASS-1 = 98.85\u00ba"]
-[9.04243278503418, 0.5756680965423584, "[FF] Orbit Raising of the ARTEMIS = In-Flight Experience with Ion Propulsion"]
-[6.045105934143066, 1.2514605522155762, "[TT] Expected Return Date of the ERNO-Box = Not earlier than February 2010"]
-[5.2516188621521, 6.356502532958984, "[TT] Processor Speed of the Spacecraft = 12 MHz"]
-[5.146644592285156, 3.963592767715454, "[TT] Number of Satellite Operations Centers of the C3S = 2"]
-[12.156269073486328, 3.217756748199463, "[TT] Propellant of the CGS = Nitrogen gas"]
-[11.960311889648438, -0.14184805750846863, "[TT] View Angle of the TESS = About three degrees above the stars\u2019 orbital plane"]
-[9.994054794311523, -1.5814288854599, "[TT] Inclination of the IRS-1B = 99.09\u00ba"]
-[4.575847148895264, 6.755516052246094, "[FF] Communication of the OPS-SAT = S-band transponder, Telemetry and Telecommand (TM/TC), X-band transmitter, optical uplink"]
-[13.759629249572754, 2.779395341873169, "[TT] Launch Mass of the LEOStar-3 = 1387 kg"]
-[12.429234504699707, 0.6418055891990662, "[TT] Image Resolution of the PLATO Telescope = About 80 Mpixels"]
-[4.305747985839844, 7.140800952911377, "[FF] Frequency Band of the Ka-band Mobile Earth Station = Ka-band"]
-[3.1876769065856934, 4.824365139007568, "[TT] Observation Mode of the ALOS-2 = DRC and full-pol. observation simultaneously"]
-[16.55339241027832, 3.6449320316314697, "[TT] Number of Satellites with FCC Application of the OneWeb = 48000"]
-[8.148849487304688, -1.08417546749115, "[FF] Data Usage of the ICESat-2 = Accurately measure the depths (bathymetry) of shallow coastal waters"]
-[4.787967681884766, 3.018021583557129, "[TT] Manufacturer of the Sentinel-5 = Airbus DS"]
-[10.591662406921387, 0.9797667264938354, "[FF] Type of the GJ 367b = Sub-Earth"]
-[5.211618423461914, 3.0034048557281494, "[FF] Consortium of the Izmit Bay Bridge = Kvaerner-led Joint Venture, the Anglo-Japanese-Turkish Consortium"]
-[7.907604694366455, 4.807087421417236, "[TT] Location of the RADFET dosimeters = ESS (Experiment Support System) PCB"]
-[10.879484176635742, 6.155619144439697, "[TT] Quantity of Faraday Cup Ion Detectors of the SWE Instrument = 2"]
-[6.349707126617432, 5.358962535858154, "[TT] Type of the VIRR = Cassegrain-type"]
-[12.074125289916992, 3.4625375270843506, "[TT] Thrust of the PPCU ion thruster = 11.5~17mN"]
-[8.263136863708496, 4.425666332244873, "[FF] Orbit of the LARES-2 = Unique"]
-[4.837124347686768, 5.711848258972168, "[TT] Frequency L1 of the GPS receiver = 1575.42 MHz"]
-[5.217668056488037, 7.150078296661377, "[TT] Data Transmission Speed of the Baseband Switching Router = Up to 155 Mbit/s"]
-[7.591845989227295, 4.704703330993652, "[FF] Description of the Part B2 = An identical maneuver is performed but at a later stage when the perigee is illuminated and the VBS can operate in non-cooperative mode"]
-[7.139410972595215, 0.04981602355837822, "[FF] Age of the HD 31901 = Initially estimated at 1 billion years, later estimate of about 120 million years"]
-[11.227755546569824, 5.8202924728393555, "[TT] Type of the DERA-patented carbon-composite joint = Novel"]
-[13.549890518188477, 6.53560733795166, "[FF] Worst-Case Depth-of-Discharge of the Power Subsystem = Well below the limit allowed by FP (Fault Protection)"]
-[9.006545066833496, 3.3392202854156494, "[FF] Composition of the Plasmasphere = Low-energy (low-temperature) plasma"]
-[6.648640155792236, 5.35781717300415, "[TT] Design Type of the TCS = Passive and Active"]
-[10.378307342529297, 2.1301701068878174, "[TT] X-ray Emission of the Swift = Low level"]
-[10.405319213867188, 2.324974536895752, "[TT] Field-of-View of the Soft X-ray Imager = Wide"]
-[4.930922508239746, 2.97965669631958, "[TT] Prime Contractor of the Jason-CS / Sentinel-6 = Airbus Defence and Space"]
-[4.782908916473389, 3.1255698204040527, "[TT] Location of the SDC = LASP"]
-[7.253568649291992, 7.787827968597412, "[TT] Deadtime per trigger of the PHA = 4\u201367 \u00b5s"]
-[9.477851867675781, 2.7859463691711426, "[FF] Measurement Task of the SIXS = Measurement of solar X-rays on the dayside of Mercury's surface"]
-[9.808959007263184, 8.608173370361328, "[TT] IFOV of the SGLI = 250 m"]
-[14.69632625579834, 6.647549629211426, "[TT] Batteries Capacity of the EROS-A = 14 Ah"]
-[5.800858497619629, -0.7997347116470337, "[TT] Design Life of the GEISAT Constellation = Five years"]
-[5.641160488128662, 4.296239376068115, "[FF] Technology of the EDRS = Developed by European industry"]
-[4.459452152252197, 7.695408821105957, "[TT] Frequency of the S-band = 2067 MHz"]
-[14.240839004516602, 3.0660977363586426, "[TT] Mass of the TISat-1 = 1 kg"]
-[7.621029853820801, 3.8906147480010986, "[FF] Purpose of the STR = Removing non-stellar objects"]
-[11.032503128051758, 0.6882454752922058, "[FF] Definition of the Habitable Zone = The area around a star at which water can be liquid on a rocky planet's surface"]
-[7.822388172149658, 7.054008960723877, "[TT] Design of the Interferometer = Solid block design"]
-[9.792016983032227, 8.427074432373047, "[TT] IFOV of the TOMS = 50 km at nadir"]
-[5.114729881286621, 2.3611507415771484, "[TT] Mission Operator of the SPOT 1-5 = CNES"]
-[5.3751540184021, 6.245625019073486, "[TT] SDRAM of the Stamp9G20 = 54 MB"]
-[5.733563423156738, 5.067534446716309, "[FF] Requirements of the GRDDP = Be flexible so that it can be adapted as needed to different host data throughput requirements and resources"]
-[10.830510139465332, 4.027279853820801, "[TT] Boom Material of the Drag Sail = Tape-springs"]
-[6.8394775390625, 6.00229549407959, "[TT] Quantity of the Rubidium frequency standards = 2"]
-[4.658471584320068, 7.115045070648193, "[TT] Downlink of the Miniaturized X-band transponders = 100 kbit/s"]
-[9.00046443939209, -0.7629285454750061, "[TT] Orbit Type of the PROBA-3 = Highly elliptical"]
-[13.717240333557129, 5.424331188201904, "[TT] Solar Array Type of the UK-DMC-2 = GaAs/Ge single-junction solar cells"]
-[12.040870666503906, -0.1795417219400406, "[TT] Sky Area Coverage of the TESS = 400 X larger than Kepler"]
-[7.192971706390381, 4.43172025680542, "[FF] Mounting of the SEP = On the spacecraft body"]
-[3.4294445514678955, 4.918675899505615, "[FF] Architecture of the SAR Instrument = Front-end and back-end"]
-[5.884790897369385, 1.0313987731933594, "[FF] Date of the Wolf Awakens at Night = 8 January 2022"]
-[10.656039237976074, 3.8847217559814453, "[FF] Mission of the CANYVAL-X = Technology demonstration"]
-[9.90861988067627, 8.023699760437012, "[TT] PSF (Point Spread Function) of the Telescope = 1.5 - 2.5 arcmin (rms)"]
-[10.309338569641113, 2.1056244373321533, "[TT] Purpose of the NuSTAR = Confirm hypothesis of higher-energy X-rays from Jupiter"]
-[9.515636444091797, 4.773263454437256, "[TT] Attitude Control of the Spacecraft = 3-axis stabilization (zero momentum control)"]
-[8.619240760803223, 7.4533371925354, "[TT] Detection Threshold of the Instrument = 4.7 \u00b5J m -2  sr -1"]
-[9.898285865783691, 5.179844856262207, "[FF] Thermal-optical design for one millimeter accuracy of the LARES-2 = Advances in Space Research, Volume 65, Issue 10, 2020, Pages 2276-2289"]
-[13.492709159851074, 2.8207802772521973, "[TT] Mass of the Block 5 Satellite = 104 kg"]
-[13.841021537780762, 3.6484382152557373, "[TT] Payload Mass of the Telescope = 2191 kg"]
-[5.992220878601074, 4.362918853759766, "[FF] Disaggregation Capability of the Cellular Satellite Architecture = Allows the disaggregation of typical space vehicles into as many or as few cardinal pieces (called satlets) as required"]
-[8.14101791381836, 1.2103025913238525, "[FF] URL of the Soil Moisture Active Passive (SMAP) = http://secure.ntsg.umt.edu/publications/2010/ENOKCEEGJJKPKMMMMRSSTTV10/Entekhabi_IEEEProceedings_05_10.pdf"]
-[13.664889335632324, 6.97849178314209, "[TT] Power Generation of the EPS = ~50-100 W"]
-[4.2959794998168945, 7.081045627593994, "[TT] Transmission Band of the TT&C = S-band"]
-[6.606329917907715, 2.811084032058716, "[FF] Image Source of the DMS = NASA, Nathan Kurtz"]
-[6.7071075439453125, 1.829508662223816, "[FF] URL of the NICER = https://heasarc.gsfc.nasa.gov/docs/nicer/gallery/slides/NICER_Science_Overview.pdf"]
-[5.9381103515625, 2.414870262145996, "[TT] Launch Date of the WorldView Legion = 2021"]
-[8.301796913146973, 4.705350875854492, "[FF] Components of the iADCS100 = ST200 star tracker, RW200-series of reaction wheels, MTQ200 series of magnetorquers"]
-[5.849620819091797, 2.954329490661621, "[FF] Funding of the MAST = Combination of private and government research funds"]
-[9.5687255859375, -0.7524426579475403, "[TT] Orbit Parameters of the DSX spacecraft = Perigee of 6000 km, apogee of 12000 km, inclination of 43\u00ba"]
-[11.665284156799316, 4.79741907119751, "[TT] Dimensions of the TEP Absorber 2 = 2.7 cm cylinder"]
-[6.111693859100342, 1.4185261726379395, "[FF] Operation End Date of the Midcourse Space Experiment = July 22, 2008"]
-[5.98933219909668, 3.3617498874664307, "[TT] Number of Spacecraft of the THEMIS = Three"]
-[9.412821769714355, 8.131649017333984, "[FF] Mounting Ring Location of the LWIR Camera = Blue"]
-[7.007503986358643, 5.1880269050598145, "[FF] Components of the HH-J interface = HH Remote Interface Unit (HRIU), LEP (Lower End Plate) electronics"]
-[8.414570808410645, 8.70837688446045, "[TT] Effective Area at 40 nm of the EUV Simulation = 28 cm2"]
-[3.7836570739746094, -0.6856532096862793, "[TT] Service Area of the Bartolomeo = Low Earth Orbit"]
-[9.641013145446777, 6.872251510620117, "[TT] Freeze/Thaw State Resolution of the SMAP = 3 km"]
-[3.4144158363342285, -0.9038705229759216, "[TT] Orbit Type of the MethaneSAT = Sun-synchronous polar orbit"]
-[4.410246849060059, 7.233325004577637, "[TT] Ku-band Transponders of the Eutelsat-9B = Up to 66"]
-[4.893933296203613, 8.324376106262207, "[TT] Frequency Bands of the JMR = 18.7, 23.8, and 34 GHz"]
-[13.413772583007812, 5.508493423461914, "[TT] Quantity of the Solar panels = 3"]
-[9.381677627563477, 7.095760822296143, "[TT] Spatial Resolution of the SPOT 1-5 = From 20 m to 1.5 m"]
-[7.663015365600586, 5.7032551765441895, "[FF] Transmission Concept of the PRARE = Microwave"]
-[1.6099790334701538, 3.759319543838501, "[TT] 3-axis stabilization of the BEESAT-2 = Yes"]
-[4.641242504119873, 1.7316173315048218, "[FF] Conference Presentation Date of the TechnoSat = Aug. 10-15, 2013"]
-[6.213815689086914, 6.45137882232666, "[TT] Number of Digital Delays of the TTDL = 5"]
-[5.274045467376709, 2.5009918212890625, "[TT] Mission Type of the SciSat-1/ACE = EO"]
-[5.326827049255371, 0.048209547996520996, "[FF] End of Mission of the Cygnus NG-10 = Unknown"]
-[6.719265460968018, 0.8419214487075806, "[TT] Close Pass of the Sun Date of the Solar Orbiter = 26 March 2022"]
-[5.882763385772705, 4.2702460289001465, "[TT] Operation Start of the Flight Computer = Since 2017"]
-[4.7571492195129395, -0.26537972688674927, "[TT] End of Life Date of the CATS = 30 Sep 2018"]
-[7.57373046875, 4.572231292724609, "[FF] Parameter of the Sensors = Unknown"]
-[10.015203475952148, -1.6142206192016602, "[TT] Inclination of the Secondary Payloads = ~51.6o"]
-[5.669983863830566, 3.34145188331604, "[TT] Operator of the DMSP = NOAA"]
-[4.935658931732178, 4.103590488433838, "[TT] Countries of the IC Stations = 23"]
-[6.861519813537598, 3.3597352504730225, "[FF] Purpose of the Rodent Research-19 = Investigating two proteins that may prevent muscle and bone loss in space"]
-[9.68791389465332, 8.344037055969238, "[TT] Field of View at Nadir of the SBUV = 0.20 rad"]
-[9.638992309570312, 7.6570916175842285, "[FF] Spot Size of the Optical Telescope = Smaller than the pixel size of the detector"]
-[9.583087921142578, 7.355003356933594, "[TT] Angular Resolution of the JEM-X = 3 arcmin"]
-[11.539924621582031, 3.4802591800689697, "[FF] Propulsion Subsystem of the SGEO = Electric"]
-[7.8714985847473145, 1.4185491800308228, "[FF] Mission Focus of the Aqua = Multidisciplinary study of the Earth's water cycle"]
-[5.3947038650512695, 1.3904966115951538, "[FF] Impact Status of the LADEE = Planned"]
-[5.1576032638549805, 5.77011251449585, "[TT] Protocol of the RF Communications = CCSDS compatible"]
-[4.472295761108398, 1.0336378812789917, "[TT] Upgrade Year of the GMS = 2005"]
-[6.471226215362549, 5.830461025238037, "[TT] PRN of the GSAT-0205 = 24"]
-[6.189742565155029, 7.004093170166016, "[TT] Data rate of the Optical System = 665.4 kbit/s"]
-[8.853060722351074, 2.8884353637695312, "[FF] Importance of the Frictional heating = Strongly controls the mass density of the thermosphere"]
-[11.963813781738281, -0.34527459740638733, "[FF] Development Status of the TESS = Arrived in Florida"]
-[3.4691452980041504, -0.9242987632751465, "[TT] Orbit Type of the OrbView-2 = Sun-synchronous polar circular orbit"]
-[11.009211540222168, 7.675807476043701, "[TT] Swath Width for Regular Corresponding Mode of the Wide fine Quad-Pol = 25 km"]
-[5.414708614349365, 1.0058064460754395, "[FF] Date of the IGARSS = July 21-26, 2013"]
-[6.83013916015625, 1.1784124374389648, "[FF] Launch Date of the Emirates Mars Mission (Hope) = 17 April 2020"]
-[8.069825172424316, 9.068227767944336, "[FF] Parameter Species Wavelength of the SSUSI = O 989 \u00c5, 1304 \u00c5, 1356 \u00c5, 1641 \u00c5"]
-[5.851943016052246, 1.993470549583435, "[FF] Contribution of the SPEXone = PACE mission"]
-[10.955424308776855, 6.340909004211426, "[TT] Optics System Material of the NAOMI = SiC-100 (silicon carbide)"]
-[9.487309455871582, 8.945820808410645, "[TT] Pointing Platform Provider of the Iris video camera = RSC Energia of Kaliningrad, Russia"]
-[6.2897419929504395, 1.9067445993423462, "[FF] URL of the eROSITA = http://arxiv4.library.cornell.edu/PS_cache/arxiv/pdf/1004/1004.5219v1.pdf"]
-[8.49721622467041, 1.7423232793807983, "[TT] Accuracy of Water Vapor Measurement of the TMR = 0.2 gm/cm2"]
-[11.921531677246094, 4.986917972564697, "[TT] Size of the ASAP = 175 x 245 x 100 mm3"]
-[4.729612350463867, 7.967081546783447, "[TT] Frequencies of the DOR Tones = Typically at 1 MHz and 2f0"]
-[3.399481773376465, 4.926686763763428, "[FF] Features of the ASAR = A digital chirp generator and an improved linear dynamic range, Flexible swath positioning, Dual polarization capability, Wide-swath coverage, Enhanced wave-mode, Extended duty cycle, Global SAR coverage"]
-[14.053879737854004, 4.047631740570068, "[TT] Instrument Mass of the SEVIRI = 270 kg"]
-[9.541184425354004, 4.091688632965088, "[FF] Components of the Wave Probe (WP) = SLP (Split Langmuir Probe), search-coil magnetometer, and electric probe"]
-[6.5143866539001465, 5.372198581695557, "[FF] Data Collection of the DCS = From DCPs (Data Collection Platforms)"]
-[4.7731170654296875, 7.284848213195801, "[TT] X-band Data Rate of the VRSS-1 = 190 Mbit/s"]
-[5.782173156738281, 7.150519371032715, "[TT] Bit Rate of the LIMS = 4 kbit/s"]
-[10.01860523223877, -1.568020224571228, "[TT] Inclination of the Rideshare mission = 97.6\u00ba"]
-[13.25396728515625, 5.244607448577881, "[TT] Total Array Area of the Solar Array = 7.1 m2"]
-[3.254929542541504, 5.042887210845947, "[TT] Resolution of the SAR = 25 km"]
-[8.612998008728027, 2.4276533126831055, "[TT] Vertical Resolution (Stratosphere) of the Aeolus = 2.0 km"]
-[4.799620628356934, 2.9516632556915283, "[FF] Responsibility of the Airbus = Responsible for the spacecraft or payload on 3 of the 6 new generation Copernicus Environment and Earth observation missions: LSTM, CRISTAL and ROSE-L"]
-[11.65456771850586, 4.4482574462890625, "[TT] Size of the GOMX-1 = 2U"]
-[9.354421615600586, 5.232789039611816, "[FF] Principle-plane Nadir Observation of the Satellite = Slowly slews for about 160\u00ba around the yaw axis"]
-[11.592780113220215, 4.690316677093506, "[TT] Size of the Barge = 90 m x 50 m"]
-[4.368229389190674, 0.09854289144277573, "[FF] Launch Date of the Starlink Satellites = February 3, 2022"]
-[7.931977272033691, 1.8480830192565918, "[FF] Marine Geoid of the GOCE = Knowledge of the marine geoid to 1 cm at a scale of 100 km"]
-[4.393828392028809, 0.6269076466560364, "[FF] Integration Date of the TROPOMI = May 26-30, 2014"]
-[7.982969284057617, 4.5969767570495605, "[FF] Radiation Protection of the CUTE-1.7 = Mentioned"]
-[7.286339282989502, 2.3170700073242188, "[TT] Objective of the GEOSAT Radar Altimeter (GRAS) = Study the marine gravity field as accurately as possible"]
-[9.363861083984375, 4.923588752746582, "[TT] Attitude Restitution of the Attitude Control Subsystem (ACS) = 6 x 10-5 radians"]
-[7.842580318450928, 3.04231858253479, "[FF] Function of the TROPOMI = Bring a significant improvement in the precision as well as temporal and spatial resolution of derived atmospheric constituents"]
-[6.569723129272461, 1.89207923412323, "[FF] URL of the SARah project = https://www.army-technology.com/news/newsastrium-german-third-sarah-reconnaissance-satellite/"]
-[5.754952430725098, 0.5330447554588318, "[TT] Observation Period of the ERS-1 and -2 = 1992 and 2011"]
-[6.2152886390686035, 1.1131101846694946, "[FF] Observation Date of the Earth from Space: Lofoten, Norway = 11 March 2022"]
-[14.242951393127441, 3.1109776496887207, "[TT] Mass of the IDEA OSG-1 = 22 kg"]
-[5.506749629974365, 0.36786261200904846, "[TT] Launch Date of the GEOS-1 = Nov. 6, 1965"]
-[9.131854057312012, 7.2431488037109375, "[TT] Image Resolution of the VSSC = 10 m"]
-[10.569439888000488, 3.3282127380371094, "[TT] Form Factor of the C2B = 3U CubeSat"]
-[11.337545394897461, 3.678110361099243, "[FF] Neutralizer discharge on of the NEUT = PS-7 on"]
-[4.9395751953125, 2.1737451553344727, "[FF] Mission Manager of the RADARSAT Constellation Mission = Daniel De Lisle"]
-[8.017390251159668, 4.102432727813721, "[FF] Side Slither Calibration Frequency of the Satellite = Quarterly"]
-[7.211250305175781, 1.2760697603225708, "[FF] Purpose of the Sample Transfer Arm (STA) = Transfer the samples from the SFR to the Mars Ascent Vehicle (MAV)"]
-[10.145194053649902, 6.969789028167725, "[TT] FOR Size of the Sounder = 24\u00ba (E-W) x 19\u00ba (N-S)"]
-[4.167854309082031, 7.192015647888184, "[TT] Frequency Band of the X-band transponder = X-band"]
-[7.367608070373535, 1.1220391988754272, "[TT] Users of the SeaSat = 16"]
-[4.024717330932617, 2.1516027450561523, "[TT] Launch Vehicle of the GeneSat-1 = Minotaur"]
-[3.3348429203033447, 5.200165748596191, "[TT] Data Link Frequency of the Seasat SAR sensor = 2.265 GHz"]
-[10.052435874938965, -1.6376731395721436, "[TT] Inclination of the Secondary Payloads = 69.5\u00ba"]
-[7.2643561363220215, 4.342763423919678, "[FF] Unknown of the EROS-B = Unknown"]
-[6.939462184906006, 6.333779811859131, "[FF] Data Processing of the HyperScout = Onboard image processing and data compression"]
-[9.834989547729492, 2.680481195449829, "[TT] Statistical Accuracy Goal of the HaloSat = \u00b10.5 LU"]
-[8.648752212524414, 3.676457166671753, "[FF] Purpose of the MIPA = Provide monitoring of the precipitating ions"]
-[9.701004981994629, -0.4798670709133148, "[TT] Altitude of the Anand = Approximately 510 km"]
-[13.357614517211914, 5.479984283447266, "[TT] Quantity of the Solar Arrays = 6"]
-[10.152531623840332, -2.7622320652008057, "[TT] Max. Input data rate of the SLC NAND-FMM = 800 Mit/s"]
-[12.23989486694336, 0.5713012218475342, "[FF] Target of the PLATO = Earth-sized planets and super-Earths"]
-[8.953431129455566, 5.840434551239014, "[FF] Scan Mechanism Assembly of the TEMPO = Provides high-precision pointing"]
-[10.853370666503906, 5.744248867034912, "[TT] MLI Surface Material of the ERG = Black polyimide film"]
-[8.141697883605957, 5.689513683319092, "[FF] Calibration Steps of the Detector Calibration = Apply bad pixel map, followed by gain and offset correction to flat-field the sensor output"]
-[4.855289936065674, 0.5156365633010864, "[TT] Deployment Date of the BRO-2 and BRO-3 = November 20, 2020"]
-[5.746777057647705, 7.134690761566162, "[TT] RDS Data Rate of the DMSP = 88.75 kbit/s unencoded, 177.5 kbit/s encoded"]
-[10.43950366973877, 2.8537542819976807, "[TT] Communication Protocol of the Nanosatellite = FM"]
-[3.8499279022216797, 4.586331844329834, "[TT] Collision Avoidance Maneuvers of the RADARSAT-2 = 2"]
-[8.323782920837402, 7.545804023742676, "[TT] Measurement Stability of the IMG = < 0.43 K (band 3); <1.59 K (band 2), < 1.58 K (band 1)"]
-[5.036635875701904, 1.2118537425994873, "[FF] Operational Date of the INSAT-3D = Feb. 5, 2014"]
-[7.658203125, 8.701769828796387, "[TT] Radiance (W/m/sr/\u00b5m) of the Spectral Bands = 145, 150, 130, 120, 90, 60, 40, 20"]
-[8.329436302185059, 3.8258979320526123, "[FF] Natural Targets for Calibration of the EarthCARE satellite = Sea surface, Desert"]
-[10.242947578430176, 8.042131423950195, "[TT] Telescope Primary Aperture Diameter of the MVIRI = 400 mm"]
-[7.745206356048584, 2.963376760482788, "[FF] Support Initiative of the Copernicus program = Stocktaking exercise with a new observation-based service to monitor CO2 emissions resulting from human activities"]
-[11.010299682617188, 1.5108568668365479, "[TT] Size of the Starshine-2 = Same as Starshine-1"]
-[8.111522674560547, 2.4341979026794434, "[FF] Objective of the MWI = Measure precipitation, provide measurements of cloud products, water vapor and temperature profiles, and surface imagery"]
-[6.834352970123291, 6.016143321990967, "[TT] Multi-Look of the Capella = 20"]
-[10.00294303894043, -1.6178265810012817, "[TT] Orbit Inclination of the SuperView-1 01 and Superview-1 02 = 98\u00ba"]
-[4.821694374084473, 2.326507568359375, "[FF] Disadvantage of the Maroc-TUBSAT = Onboard storage capacity is still too small"]
-[11.655932426452637, 5.074454307556152, "[TT] Area of the Silicon Die = 0.75 cm x 0.85 cm"]
-[7.505170822143555, 4.617344856262207, "[FF] Usage of the Testing Filters = During testing in ambient conditions"]
-[3.7482168674468994, 2.388967275619507, "[TT] Shipping Schedule of the Iridium NEXT = This week"]
-[6.472742080688477, 1.5310863256454468, "[FF] URL of the BepiColombo = http://www.issfd22.inpe.br/S10-Orbit.Determination-OD/S10_P4_ISSFD22_PF_065.pdf"]
-[8.567899703979492, 4.555664539337158, "[FF] Purpose of the ASTERIA = Monitor nearby stars for orbiting exoplanets"]
-[6.740931034088135, 0.3991219401359558, "[FF] URL of the CryoSat = http://tinyurl.com/y2uzf5xr"]
-[9.699851036071777, 6.257782936096191, "[TT] Bearings of the Steering Mirror Mechanism = Four rod-end-bearings"]
-[10.045014381408691, -1.4903587102890015, "[TT] Orbit Inclination of the GRIFEX = 99.12\u00ba"]
-[8.303498268127441, 1.2768710851669312, "[TT] 24-hour Total Precipitation on October 24-25 of the Blue Canyon, California = 10.4 inches"]
-[6.998504638671875, 4.0469818115234375, "[TT] Series of the DMSP-F13 = DMSP-5D2"]
-[5.980795860290527, -2.3260865211486816, "[TT] Orbit Inclination of the Kondor-E1 = 74.9\u00ba"]
-[14.15762710571289, 3.2581326961517334, "[TT] Mass of the GPIM = ~180 kg"]
-[5.313320636749268, 8.338698387145996, "[TT] Waveform Sampling Bandwidth of the ALT = 312.5 kHz"]
-[9.281611442565918, 6.648126602172852, "[TT] Resolution of the HRS = 1 m (Azimuth) x 0.67 m (Range)"]
-[12.21687126159668, -0.19903814792633057, "[TT] Snapshot Rate of the TESS = 10-minute"]
-[13.60346508026123, 5.78260612487793, "[FF] Energy Source of the Electric Power Subsystem = Solar cells"]
-[8.328542709350586, 4.894944190979004, "[FF] Inputs of the C&DH SPAM board = Up to 24 temperature sensor inputs including AD590 temperature transducers, PRTs (Platinum Resistance Thermometers), and standard NTC thermistors"]
-[1.6097291707992554, 3.7583816051483154, "[TT] 3-axis stabilization of the BEESAT-3 = Yes"]
-[3.903536319732666, 3.46681809425354, "[TT] Upgrade Name of the Galileo = Galileo System Build 1.5.1"]
-[9.493468284606934, 7.160048007965088, "[TT] Resolution of the Spatial resolution at nadir = 25 km"]
-[4.956089019775391, -0.022603439167141914, "[FF] End of Life Date of the MITA = 15 August 2001"]
-[11.177703857421875, 5.597721099853516, "[TT] Thickness of the Separation Panel = 30 mm"]
-[6.316450119018555, 4.626511096954346, "[FF] Function of the Data Center = Monitoring and control of orbit and attitude of the satellite, planning and management of the satellite bus operation plan, reception and management of imaging plan, processing of the image data and storage and management of the product"]
-[11.435212135314941, 4.822691917419434, "[TT] Length of the Rods = 25 cm"]
-[4.364475250244141, 5.335683345794678, "[TT] Beacon Type of the COSPAS-SARSAT = Digital 406 Mhz"]
-[4.225862979888916, 2.5723299980163574, "[TT] Launch Site of the TSIS-1 = Cape Canaveral Air Force Station, SLC-40"]
-[8.966097831726074, 3.3542613983154297, "[FF] Mission Purpose of the SPORT = Understand the preconditions leading to equatorial plasma bubbles"]
-[6.2572712898254395, 6.75881290435791, "[TT] Location Accuracy of DCP of the Onboard data collection and transmission system = 3.6 km (for one session)"]
-[8.282464981079102, 6.6694769859313965, "[TT] Temporal Resolution of the IMI = 2-3 days 2-3 days 2-3 days"]
-[9.631077766418457, 6.996798992156982, "[TT] Angular Resolution of the ECAL = < 1\u00ba @ E > 50 GeV"]
-[6.486232280731201, 4.054619312286377, "[FF] Responsibilities of the ESA = Payload Module, launcher, AIT facilities for spacecraft integration and testing"]
-[5.345411777496338, 3.965388536453247, "[TT] Number of Satellites of the Satellite Constellation = 3-5"]
-[11.349790573120117, 5.847949028015137, "[TT] Material of the Enclosure = Black anodized aluminum"]
-[10.043477058410645, 2.4987149238586426, "[FF] Purpose of the DAXSS = Observe Solar X-rays, specifically soft X-rays"]
-[5.470425128936768, 2.9632413387298584, "[FF] Designers of the Small Satellite Platform = F. Dannemann, M. Jetzschmann"]
-[13.31557846069336, 7.240041732788086, "[TT] Power Consumption of the EPP device = 4 W"]
-[5.607850551605225, 5.611654281616211, "[TT] Main Processor System of the CCM = LEON-3 based"]
-[3.2708890438079834, 2.1399128437042236, "[FF] Bathymetry Models of the Sentinel-2 = Unknown"]
-[14.276978492736816, 3.18737530708313, "[TT] Mass of the DoT-1 = 18 kg"]
-[13.98934268951416, 3.0830631256103516, "[FF] Mass of the STP-H5 = Unknown"]
-[5.424318313598633, 2.9491167068481445, "[FF] Sponsor of the EXCISS = DLR, the German Space Agency, and DreamUp"]
-[5.5324788093566895, 1.7542790174484253, "[TT] Mission Status of the CryoSat = Mission complete"]
-[10.694933891296387, 1.9665485620498657, "[FF] Description of the Gravitational Lensing Method = Photons deviate from the rectilinear direction when passing near a massive body under the influence of its gravitational field"]
-[11.286290168762207, 0.9590950608253479, "[TT] Test Center of the LISA Pathfinder = IABG (Industrieanlagen-Betriebsgesellschaft), Ottobrunn, Germany"]
-[11.724710464477539, 3.2989604473114014, "[TT] Time to Refill the Plenum back to 95% of the Thruster = Approximately three seconds"]
-[12.057016372680664, -0.34926819801330566, "[TT] Lunar Flyby Time of the TESS = 06:34:35 UTC (2:34 AM EST)"]
-[6.3938422203063965, 1.868659496307373, "[FF] URL of the PSLV = https://spaceflightnow.com/2018/01/12/pslv-c-40-coverage/"]
-[4.896492958068848, 8.28187084197998, "[TT] Frequency Range of the SSM/IS = 19-184 GHz"]
-[14.286860466003418, 3.1922192573547363, "[TT] Mass of the ICARE-NG = 2 kg"]
-[5.17197847366333, 6.852367877960205, "[TT] Uplink Data Rate of the Spacecraft = 32 kbit/s"]
-[6.222010135650635, 5.719748497009277, "[TT] Late Request Window of the LMS = 45 minutes"]
-[11.401399612426758, 3.4973926544189453, "[FF] Ignition Capability of the Propulsion System = All CGGs individually upon request"]
-[8.047884941101074, 2.623492956161499, "[TT] Measurement Domain of the SPOT-5 = Ocean, Land, Snow & Ice"]
-[3.447631597518921, -0.8991690874099731, "[TT] Orbit Type of the Anand = Sun-synchronous"]
-[4.339507579803467, 0.802869975566864, "[TT] Launch Year of the HJ-1C = 2012"]
-[13.394862174987793, 5.690490245819092, "[FF] Unknown of the Solar Power Technology = Unknown"]
-[5.42216682434082, 7.113900661468506, "[TT] ISL Data Rate of the CanX-4&5 = 10 kbit/s"]
-[6.872217178344727, 3.190946102142334, "[FF] Forecasting Needs of the National Operational Meteorological Satellite System (NOMSS) = Civil and military"]
-[5.551539897918701, 6.3332719802856445, "[TT] Function of the MEXIC = Manage the transfer of data to the mass storage"]
-[6.931703567504883, 1.5335464477539062, "[TT] Launch Date of the James Webb Space Telescope = Later this year"]
-[7.662414073944092, 2.118972063064575, "[TT] Primary Use of the Band 2 = Daytime clouds, vegetation, water"]
-[9.531359672546387, -0.6613143682479858, "[TT] Height of the ICESat-2 = 500 km in space"]
-[7.966403961181641, -0.9728181958198547, "[FF] Data Integration of the ICESat-2 = ICESat-2\u2019s predecessor, the original ICESat mission, as well as the European Space Agency\u2019s satellite dedicated to monitoring polar ice thickness, CryoSat-2"]
-[3.823645830154419, 4.27688455581665, "[FF] Measurement category of the SAR (RADARSAT-2) = Multi-purpose imagery (ocean), Multi-purpose imagery (land), Vegetation, Albedo and reflectance, Landscape topography, Ocean topography/currents, Sea ice cover, edge and thickness, Soil moisture, Snow cover, edge and depth, Ocean surface winds, Atmospheric Winds, Ocean wave height and spectrum, Ice sheet topography"]
-[6.246890544891357, 5.724836349487305, "[TT] L1B, L1C and L2A Product Destination of the EnMAP = Temporary storage on the pick-up points for delivery"]
-[13.450264930725098, 6.782653331756592, "[TT] Payload Power of the Inmarsat S \u2013 Europasat / Hellas-Sat 3 = About 12.3 kW"]
-[8.843427658081055, 1.4425771236419678, "[FF] Accuracy of the Gravity = mgal"]
-[8.496557235717773, 6.876077651977539, "[TT] Temporal Resolution of the MSASI = 2 ms"]
-[13.387009620666504, 5.46120023727417, "[TT] Solar Array of the KOMPSAT-6 = Fixed solar array with one deployable wing"]
-[5.704189300537109, 4.496422290802002, "[FF] Data Availability of the EDRS = It will be made available through terrestrial network to the users\u2019 sites"]
-[4.3215107917785645, 7.554691791534424, "[TT] S-band Uplink Frequency of the MSX = 1827.8 MHz"]
-[3.3648314476013184, 5.048396110534668, "[FF] Synergy of the Copernicus L-band SAR = Works in synergy with other Copernicus SAR-based space elements operating at a different frequency"]
-[7.746522903442383, 4.757390975952148, "[FF] Device Type of the CIMERA = Radiation Assurance"]
-[4.60013484954834, 6.767367839813232, "[FF] Function of the NanoCom AX100 = Primary RF communications method"]
-[10.403491973876953, 7.606408596038818, "[TT] Power of the S-192 optomechanical scanner = 266 W"]
-[13.372486114501953, 2.8958446979522705, "[TT] Mass of the HawaiiSat-1 = 55 kg"]
-[8.951268196105957, -0.19839900732040405, "[FF] Target of the Periselene-1 = Sun-Earth WSB (Weak Stability Boundary)"]
-[9.84831428527832, 8.153038024902344, "[TT] Focal Length of the Custom design lens = 155.9 mm"]
-[5.03428316116333, 8.419301986694336, "[TT] Bands of the MicroMAS-2 = 89 GHz (window), 118 (temp), 183 GHz (humidity), 207 GHz (cloud ice)"]
-[7.301991939544678, 4.386374473571777, "[TT] Space Experiment Module of the SEM = 100%"]
-[10.483803749084473, 6.897613048553467, "[TT] Diameter of the Main Mirror = 64 cm"]
-[10.37853717803955, 2.278679609298706, "[FF] Energy of the X-rays = Higher energy, longer penetration depth"]
-[5.3805952072143555, 0.4062899053096771, "[TT] In Orbit Commissioning (IOC) Start Date of the CHEOPS = 7th January"]
-[6.599904537200928, 6.054903030395508, "[TT] Position of the CASI-1500i = Left"]
-[7.901966094970703, 1.078963279724121, "[FF] Date of the NASA Adds Up Alberto's Soaking Rainfall = 31 May 2018"]
-[13.528619766235352, 5.545790672302246, "[TT] Solar Panels of the EPS = 5 surface-mounted solar panels"]
-[9.336525917053223, 6.978887557983398, "[TT] Resolution of the MSU-E = 38 m"]
-[9.32461929321289, 6.186224937438965, "[TT] Scan Geometry of the SSM/I = Conical 45 \u00ba"]
-[1.7521108388900757, -2.0701651573181152, "[FF] Presentation Date of the Hayabusa-2 = March 5, 2011"]
-[8.966177940368652, 7.333339214324951, "[TT] Detection Area of the HXD = 16cm2"]
-[4.985415458679199, 1.18483567237854, "[FF] Brochure Date of the GOCE = June 2006"]
-[13.772439002990723, 5.950352191925049, "[TT] Sunlight Power Conversion Efficiency of the SBVR = 98%"]
-[8.013654708862305, -0.20240063965320587, "[FF] Monitoring of the GRACE-FO = Changes in ice mass"]
-[5.3020172119140625, 5.62239408493042, "[TT] Data Bus of the Suomi-NPP = MIL-STD-1553"]
-[11.150455474853516, 0.4736006557941437, "[TT] Study Duration of the Exoplanets = More than 27 months"]
-[9.195053100585938, 8.483966827392578, "[TT] Wavelength of the Lens 4 = 1.375 \u00b5m and 1.64 \u00b5m"]
-[7.679605484008789, 2.2148265838623047, "[TT] Coverage Area of the Ikonos = More than 400 millionkm2"]
-[10.062445640563965, 5.513899326324463, "[FF] Thermal Gradients of the Etalon = Unknown"]
-[8.051346778869629, 4.365915298461914, "[FF] Study Topic of the MSI and Proba-V = Radiation Influence"]
-[4.460562705993652, 1.453647255897522, "[TT] Reentry Date of the MightySat II.1 = Nov. 12, 2002"]
-[12.801868438720703, 3.1662092208862305, "[TT] Quantity of the Fuel = 6.38 kg"]
-[6.76069450378418, 5.693390369415283, "[TT] Phase Data Number of the BSC = 4,096"]
-[5.173098564147949, 3.116786241531372, "[TT] Pipeline Software Developer of the GBOT = GBOT group in Paris"]
-[14.06445598602295, 4.023579120635986, "[TT] Mass of the Instrument = < 7 kg"]
-[5.847471237182617, -0.7042770385742188, "[TT] Orbital Lifetime of the Geotail = 20 years"]
-[8.33456039428711, 7.54964017868042, "[TT] Detector Type of the Instrument = 1D CCD (4098 pixels)"]
-[11.070940017700195, 6.047812461853027, "[TT] Material of the Optical Benches = Composite tubes with titanium fittings"]
-[5.823501110076904, -0.6485698223114014, "[TT] Mission Life of the CLARREO Pathfinder = 1 year"]
-[11.663593292236328, 6.755833148956299, "[TT] Detection Range of the ABEX = Under 15 keV"]
-[14.220603942871094, 3.2477617263793945, "[TT] Mass of the SEAM = 4.7 kg"]
-[8.247573852539062, 2.396486520767212, "[FF] Effect of the Clouds = Can cause scattered clouds resulting in links that are only partly available"]
-[7.585943698883057, 2.433105945587158, "[FF] Evolution of the Poseidon-4 radar altimeter = Evolved significantly from the Poseidon-3A and -3B instruments"]
-[7.8816680908203125, 8.644097328186035, "[TT] Number of Colors of the OCO-3 = 17,500"]
-[9.339032173156738, 6.084472179412842, "[TT] Field of View of the HRG Sensors = 4.13\u00b0"]
-[6.4652252197265625, 1.9921934604644775, "[FF] URL of the Intermediate Experimental Vehicle = http://www.spaceflight101.com/ixv.html"]
-[11.581228256225586, 4.885333061218262, "[TT] Central Hole Diameter of the XMM Service Module = 2.10 m"]
-[11.992384910583496, -0.36347365379333496, "[TT] Spacecraft Builder and Operator of the TESS = Orbital ATK (OA)"]
-[5.030923366546631, 6.077680587768555, "[FF] Signal Spectrum of the AIS = Entire signal spectrum is downloaded for de-collision of the AIS messages"]
-[12.143742561340332, 6.139029502868652, "[TT] Events Analyzed of the AMS = 41 billion"]
-[3.467973232269287, 5.029900550842285, "[FF] Instrument Subsystems of the CSG-SAR = SES (SAR Electronic Subsystem) and SAS (SAR Antenna Subsystem)"]
-[3.6181769371032715, -0.7872951626777649, "[TT] Satellite Orbit of the Satelles = LEO"]
-[9.721043586730957, -0.5424286127090454, "[TT] Orbit Altitude of the AlSat-2A = ~670 km"]
-[8.357986450195312, 3.288907527923584, "[FF] Composition of the Ozone = Three oxygen atoms"]
-[5.008701801300049, 0.5330131649971008, "[TT] Commencement Date of the SERVIR = 2004"]
-[6.847384452819824, 5.253688335418701, "[FF] IPU Components of the RSI = Video electronics, sequencer, DC/DC converter, compression cards"]
-[13.429326057434082, 6.7695746421813965, "[TT] Power of the Spacecraft = 357 W (long-term), 1350 W (short-term)"]
-[4.907961368560791, 0.4661490321159363, "[TT] Launch Date of the SES-14 = Late 2017"]
-[3.825570583343506, 6.389933109283447, "[TT] Installation of the ISL Antennas = +X surface and -X surface"]
-[5.961060047149658, 2.4206697940826416, "[FF] Launch Date of the WorldView Legion = Unknown"]
-[5.786777019500732, 2.8332622051239014, "[FF] Cooperation Agreement of the OICETS = JAXA (formerly NASDA) and the ESA signed an agreement regarding cooperation in optical communications in space"]
-[4.386025428771973, 1.1081526279449463, "[TT] Capacity Establishment Deadline of the GMES = 2008"]
-[12.043387413024902, -0.3177669644355774, "[TT] Data Release of the TESS = Sectors 1 and 2, observed between July 25 and September 20, 2018"]
-[11.032118797302246, 2.130011558532715, "[TT] Number of Thermistors of the XMM-Newton = 8"]
-[4.6483941078186035, 8.079163551330566, "[TT] Chirp Bandwidth of the RA-1 = 330 MHz (for ocean mode) and 82.5 MHz (for ice mode)"]
-[3.969228744506836, 4.34820032119751, "[FF] Performance Monitoring Campaign of the RADARSAT-2 = Ongoing"]
-[9.410516738891602, 7.040422439575195, "[TT] Vertical Resolution of the Tomorrow-R1 and -R2 = 250 m"]
-[12.064566612243652, 6.250058650970459, "[TT] Antihelium Candidate Rate of the AMS-02 = Approximately one per year"]
-[8.170673370361328, 8.543804168701172, "[FF] Spectral Resolution of the ICON FUV instrument = High enough to reject unwanted contamination by the bright optically thick 130.4 nm O line"]
-[4.238636016845703, 2.6177666187286377, "[TT] Launch Site of the GFO = VAFB (Vandenberg Air Force Base), CA"]
-[5.084503650665283, 0.7401443719863892, "[TT] Launch Date of the Astra's Rocket = Expected in the next week"]
-[10.093561172485352, 7.186143398284912, "[TT] Scene Length Range of the Instrument = 10 km to 473 km"]
-[10.78614616394043, 1.0338844060897827, "[TT] Mass Loss of the Star = About three times the mass of Jupiter"]
-[7.739634990692139, 6.913055419921875, "[TT] Recording Duration of the Camera = 10 minutes"]
-[7.183348178863525, 1.0591331720352173, "[TT] Missions of the ROSA = OceanSat-2 of ISRO, SAC-D of CONAE and NASA, Megha Tropiques of ISRO and CNES"]
-[6.9002509117126465, -0.6158143281936646, "[TT] Orbit Period of the AlSat-2 = 98 minutes"]
-[5.820457935333252, 3.6697542667388916, "[TT] Number of Experiments of the MightySat I = 5"]
-[4.737740516662598, 7.905610084533691, "[TT] Clock Signals of the CIB = 1 Hz and 220 Hz"]
-[6.000245094299316, 1.6603925228118896, "[FF] News Date of the SCD-2 = Dec. 17, 2014"]
-[8.085960388183594, -0.33124154806137085, "[TT] Velocity Derivation Date of the Amundsen Sea Embayment sector of West Antarctica = Winter 1996"]
-[8.529340744018555, 6.089232444763184, "[TT] Pointing Accuracy of the CeREs = Exceeds mission requirements"]
-[9.538983345031738, 3.9509613513946533, "[TT] Heritage of the NewMag = MFI (Magnetic Fields Instrument)"]
-[3.7190849781036377, 6.516631603240967, "[TT] Material of the Sprite\u2019s antenna = Nitinol"]
-[3.812934160232544, 7.854982852935791, "[TT] Modulation of the RF communications = Asynchronous GMSK"]
-[8.430744171142578, 0.9708144068717957, "[TT] Quantization Levels of the Snow water content = 1"]
-[3.165027141571045, 4.969022750854492, "[TT] CRS Swath of the RISAT-SAR = 223 km"]
-[10.48516845703125, 5.73622989654541, "[TT] Dayside Temperature of the 55 Cancri e = 4,400\u00ba Fahrenheit (about 2,400\u00ba Celsius)"]
-[3.8833868503570557, 3.449218273162842, "[FF] Development Date of the New maritime Galileo receiver = 24 June 2021"]
-[6.76646089553833, 8.670265197753906, "[FF] Filters of the POLDER-P = Spectral and polarized"]
-[6.540968894958496, 7.662969589233398, "[TT] Quantization of the Imager = 14 bit"]
-[5.786189079284668, 0.7181990742683411, "[FF] Validation Date of the SCARLET Advanced Array = Aug. 2, 1999"]
-[5.291900634765625, 2.898946762084961, "[TT] Platform of the Deimos-2 = SpaceEye-1"]
-[8.300806045532227, 6.937501430511475, "[TT] Number of Images of the MWIR = Over 300"]
-[8.242987632751465, 2.911407470703125, "[FF] Age of the Atmospheric Chemistry Experiment (ACE) satellite = 15 years"]
-[6.169376373291016, 6.040003299713135, "[TT] Operator Requirement of the Data Center = 4"]
-[6.727110385894775, 2.7633121013641357, "[FF] Destination of the Biofilms experiment = International Space Station"]
-[8.892407417297363, 4.2396464347839355, "[FF] Function of the 607 nm Band = Used to constrain the temperature determination of the sun"]
-[6.930778503417969, 7.537477016448975, "[TT] Number of Beams of the Reflector = Two (inner \u2013 HH, outer \u2013 VV)"]
-[10.128021240234375, -1.3831682205200195, "[TT] Orbit Inclination of the RISAT-1 = 97.552\u00ba"]
-[3.1987359523773193, 5.069907188415527, "[TT] Length of a Scene of the SAR = Up to 4000 km"]
-[11.25306510925293, 5.932088851928711, "[FF] Primary Structure of the Terra = Truss-like structure built of graphite-epoxy tubular members"]
-[13.658092498779297, 5.770993232727051, "[TT] Solar Panels Power Generation of the EURECA = 1.5 kW at 28 VDC"]
-[4.008103847503662, 6.197791576385498, "[TT] Range Direction Beam Steering of the SIR-C = 123\u00ba"]
-[8.989386558532715, 4.375640392303467, "[TT] Field of View of the Coarse Earth sun sensor = 4 pi steradian"]
-[6.487122058868408, 3.29394268989563, "[FF] Imaging of the BlackSky Constellation = High temporal and spatial resolution"]
-[10.50354290008545, 3.2952561378479004, "[TT] Satellite Type of the Hyper-Angular Rainbow Polarimeter = 3U CubeSat"]
-[9.712064743041992, -0.6500994563102722, "[TT] Orbit Altitude of the ResourceSat-2A = 817 km"]
-[4.389247417449951, 1.8697426319122314, "[TT] Number of Conflicts of the RADARSAT-2 = 395 in August 2014"]
-[8.911964416503906, 3.6511170864105225, "[FF] Location of the COR-2 = On board NASA\u2019s STEREO-A (Solar and Terrestrial Relations Observatory-A)"]
-[10.40147876739502, 5.631131649017334, "[TT] Temperature of the Hot Intergalactic Gas = Around a million degrees or more"]
-[4.842196464538574, 3.0244228839874268, "[TT] Prime Contractor of the Earth Return Orbiter (ERO) = Airbus"]
-[10.18869400024414, 1.3880655765533447, "[TT] Percentage of Stars within 100 parsecs of the Gaia Catalogue of Nearby Stars = 92%"]
-[6.897572040557861, -0.6595385074615479, "[TT] Orbit of the HaloSat = 93-minute orbit around Earth"]
-[4.934915542602539, 3.3106489181518555, "[TT] Developer of the HRS Instrument = EADS Astrium SAS"]
-[8.851927757263184, 2.4202287197113037, "[TT] Solar Cycle Observation of the SOHO = 24"]
-[12.411919593811035, 0.6210834980010986, "[FF] Thermal Isolation of the PLATO Satellite = Maximum"]
-[9.932066917419434, 2.690659761428833, "[TT] Field of View of the HaloSat = Near 100 square degrees"]
-[5.715989112854004, 4.325778007507324, "[FF] Unknown of the EDRS-A = Unknown"]
-[5.310159206390381, 1.256289005279541, "[FF] AIAA Meeting Date of the C/NOFS = January 10-13, 2005"]
-[4.925198554992676, 0.4978426992893219, "[TT] Launch Date of the Intercosmos- Bulgaria 1300 (Intercosmos-22) = 07.08.1981"]
-[13.794899940490723, 6.8979902267456055, "[FF] Voltage Threshold of the Power Cut-off = Below the security margin set by the ISS safety policy"]
-[5.98159122467041, 7.965595722198486, "[TT] Control Type of the Dual-channel Receiver Unit (DRU) = Manual or Automatic"]
-[6.5270843505859375, 0.6696236729621887, "[TT] Communication Status of the Landsat-6 = Never established"]
-[5.597523212432861, -0.06656134128570557, "[TT] Operation Duration of the RAIDS = Eight months"]
-[6.206942081451416, 6.664737224578857, "[FF] Data Rate of the ROSA = Unknown"]
-[8.430984497070312, 2.2121851444244385, "[FF] Observation of the Suomi NPP satellite = Huge Saharan dust plume streaming over the North Atlantic Ocean"]
-[11.709468841552734, 3.297569751739502, "[TT] Redundancy of the Thrusters = 1 THR loss allowed"]
-[11.698225975036621, 4.670067310333252, "[TT] Structure Dimensions of the Baumanets-2 = 460 mm in diameter and 530 mm high"]
-[3.6562929153442383, 5.193532943725586, "[TT] Altitude of the Ground Penetrating Radar = about 3 km"]
-[14.052865982055664, 4.029949188232422, "[TT] Instrument Mass of the Scanning geometry = \u2264 70 kg"]
-[7.116499900817871, 4.471365928649902, "[FF] Instrumentation of the EOS/ACRIM III = Unknown"]
-[8.073798179626465, 2.4179046154022217, "[TT] Measurement Domain of the EXPORTS = Ocean"]
-[10.289595603942871, 2.312438488006592, "[FF] Scientific Goals of the INTEGRAL = High resolution spectroscopy with fine imaging and accurate positioning of celestial sources in the gamma-ray domain"]
-[7.925718784332275, 1.7793617248535156, "[TT] Purpose of the GOCE = Measuring Earth's gravity"]
-[13.701896667480469, 2.7269396781921387, "[TT] Launch Mass of the Satellite = 3100 kg"]
-[8.014410018920898, 5.889612674713135, "[FF] Function of the High-Resolution Camera = Capture Earth imagery"]
-[13.321937561035156, 5.6644392013549805, "[FF] Temperature of the Solar Panel = Variable"]
-[7.592154026031494, -0.8353074193000793, "[TT] Launch Year of the ICESat-2 = 2018"]
-[8.707597732543945, 8.212060928344727, "[TT] Optical Efficiency of the Overall = 0.6"]
-[8.099645614624023, 3.0823702812194824, "[FF] Accuracy of the Infrared Spectrometer = Increases with the length of the climate record"]
-[14.074593544006348, 4.05557107925415, "[TT] Instrument Mass of the HySI = 4 kg"]
-[7.651069641113281, 3.6712257862091064, "[FF] Purpose of the Bipods = Minimize the thermal conductive leaks between the COB and the OBA"]
-[8.994512557983398, 4.934494972229004, "[TT] Quantity of the 3-axes Inertial Rate Sensors = Two on each S/C"]
-[8.799066543579102, 2.8612570762634277, "[FF] Mission of the THEMIS = Uncover the mysteries behind the formation of auroral beads"]
-[8.412586212158203, 0.4072362780570984, "[TT] Maximum Depth of the Lake Cedar = 10 meters (32 feet)"]
-[7.948639869689941, 8.590062141418457, "[TT] Spectral range of the IRAS = 0.69-15.5 \u00b5m"]
-[5.221336364746094, 3.0831613540649414, "[TT] Operator of the Bartolomeo = Airbus DS"]
-[8.666258811950684, 9.036967277526855, "[TT] Sensitivity of the NIRSpec MIRI = 560 nJy (10 \u03bcm, \u03c4 i =10,000 s, and \u03bb/\u0394\u03bb = 5)"]
-[8.103799819946289, -1.2046635150909424, "[TT] Laser Altimeter of the ICESat-2 = Measures the height of the first substance it hits"]
-[7.1782755851745605, 4.637692928314209, "[TT] Attachment Method of the Payload Panel = Support Rods"]
-[6.156143665313721, 5.153298377990723, "[TT] Equipped with of the ExAlta-1 = m-NLP"]
-[8.008841514587402, 9.201658248901367, "[TT] Depolarization Measurements of the CATS = At all wavelengths"]
-[7.863266468048096, 8.636624336242676, "[TT] Spectral Bands of the Hyperion = 220"]
-[6.307553291320801, 5.645965576171875, "[TT] Communication Relay Terminals of the Pl\u00e9iades-Neo satellites = Tesat Spacecom laser"]
-[14.100010871887207, 7.196513652801514, "[TT] Nominal Bus Voltage of the OBDH = 28 V"]
-[11.794295310974121, 6.655823230743408, "[TT] Electron Energy Range of the SWEPAM = 1 - 1240 eV"]
-[14.283663749694824, 3.035860061645508, "[TT] Sample Mass of the OSIRIS-REx = At least 60 gram"]
-[9.127641677856445, 3.4012598991394043, "[FF] Purpose of the FIELDS = Measure electric and magnetic fields in the Sun's atmosphere"]
-[6.4134931564331055, 6.986685752868652, "[TT] Link Distance of the Optical link = > 45,000 km"]
-[8.553967475891113, 3.0733590126037598, "[FF] Review Date of the Solar Ultraviolet Imager = Jan. 8, 2013"]
-[5.611528396606445, 6.880456924438477, "[TT] Data Rate of the Solar Orbiter = 100 kbit/s"]
-[5.879064083099365, 1.3578706979751587, "[FF] Paper Number of the ERG Satellite = 2011-r-50"]
-[4.369701385498047, 6.21433162689209, "[FF] Destination of the Dutch Radio Antenna = Moon"]
-[10.238937377929688, 8.188237190246582, "[TT] Opening Diameter of the Aperture Stop = 4\u00ba"]
-[13.828591346740723, 3.241943359375, "[TT] Total Mass of the NanoPS = < 0.5 kg"]
-[5.066624641418457, -0.35063010454177856, "[TT] Planned Launch Date of the CBERS-4 = 2013"]
-[3.8926279544830322, 3.4103972911834717, "[TT] Launches of the Galileo Satellite = 11 in 10 years"]
-[5.380958557128906, 3.9582512378692627, "[TT] Number of Satellites of the Spire = Over 100"]
-[10.100778579711914, -1.5963083505630493, "[TT] Inclination of the FY-3D = 98.75\u00ba"]
-[7.598355770111084, 2.645036458969116, "[FF] Data Collection of the Mission = Atmospheric and oceanic data"]
-[4.425496578216553, -1.6313073635101318, "[TT] Publication Date of the Blue Ring Nebula = Nov. 18"]
-[5.581112861633301, -1.984868049621582, "[FF] Function of the IPRE = Provides data reception and storage processes of KOMPSAT-3 spatial data and allows for the distribution of imagery products to end-users"]
-[9.599644660949707, -0.43996769189834595, "[FF] Altitude of the Ballast = MEO (6-12,000 km)"]
-[11.34144115447998, 6.525000095367432, "[TT] Design of the LINAS = IGS (Ionization Gauge Streak)"]
-[10.023456573486328, -1.5162091255187988, "[TT] Orbital Inclination of the Solar Orbiter = 17\u00ba (by 2025), 33\u00ba (by the end of the decade)"]
-[4.719785690307617, 1.6712894439697266, "[FF] Mission Overview of the GCOM-W = Not provided"]
-[4.38109016418457, 7.823877334594727, "[TT] Frequency of the Uplink = 749f0"]
-[2.0262370109558105, -0.32589444518089294, "[TT] Number of Radiation Belts Discovered of the Van Allen Probes = 3"]
-[9.32199478149414, 4.833341598510742, "[FF] Attitude Control System Testing Date of the Odin = Oct. 18-21, 1999"]
-[7.521381855010986, 2.502156972885132, "[TT] Measurement Category of the GPIM = Multi-purpose imagery (ocean), Multi-purpose imagery (land)"]
-[4.252594947814941, -1.4894167184829712, "[FF] Lagrangian Point Flyby of the Chang'e-2 = Realized"]
-[14.181253433227539, 3.147812604904175, "[TT] Mass of the ASC = 1.647 kg"]
-[8.465511322021484, 1.8987038135528564, "[TT] 18.7 GHz Channel Function of the JMR = Correction for effects of wind-induced enhancements in the sea surface background emission"]
-[9.337015151977539, -0.5678578615188599, "[TT] Orbit of the INTEGRAL = Highly eccentric 64-hour orbit, coming as close as 10,000 km and as distant as 140,000 km from Earth"]
-[7.969457149505615, 2.4631640911102295, "[TT] Measurement Category of the SARAL = Atmospheric Humidity Fields, Ocean topography/currents, Ocean surface winds, Ocean wave height and spectrum"]
-[12.445892333984375, 0.6409958004951477, "[TT] Image Resolution of the PLATO CCDs = 20 megapixels"]
-[9.02291202545166, 6.843324661254883, "[TT] Image Size of the OSIRIS = About 96 cm across"]
-[5.2758917808532715, 3.993955373764038, "[TT] Platform of the WSF-M Space Vehicle = BCP (Ball Configurable Platform)"]
-[9.241783142089844, 4.816749572753906, "[TT] CSC Rotation of the Activity Attitude = 180\u00ba around xRBF"]
-[6.405937194824219, -0.5718086957931519, "[TT] Time of the Spacecraft Stabilization = 2.5 minutes"]
-[5.07389497756958, 2.879206895828247, "[TT] Agency of the Myriade/AstroSat-100 = CNES, ASTRIUM"]
-[11.662280082702637, 6.718203544616699, "[TT] Energy Range of the Detector = 5-30 keV"]
-[7.235297679901123, 2.354468822479248, "[TT] Primary Instrument of the GEOSAT = GEOSAT Radar Altimeter (GRAS)"]
-[8.174988746643066, 0.03902202844619751, "[TT] Design Life of the TOPEX/Poseidon = 5 years"]
-[6.015279293060303, -0.5417405962944031, "[TT] Mission Duration of the ADEOS-II = 10 months"]
-[7.157989501953125, 3.944061517715454, "[TT] Potential Substitute for of the AMSR2 = JPSS (Joint Polar Satellite System), the former NPOESS MIS (Microwave Imager Sounder)"]
-[5.869743824005127, 0.5744808912277222, "[TT] Number of ERS SAR Pairs of Data of the ERS Tandem Mission = About 110,000"]
-[4.989403247833252, 3.3993773460388184, "[TT] Manufacturer of the Argus = Thoth Technology Inc."]
-[9.301445960998535, 3.1738293170928955, "[FF] Components of the ASPIICS Coronagraph System = CI (Coronagraph Instrument), OD (Occulter Disk), metrological sensors"]
-[10.196062088012695, 4.545349597930908, "[TT] Reactive Control Torque of the RWAs = 0.2 Nm"]
-[7.801425457000732, 2.2643158435821533, "[FF] Climate Patterns of the XO-3b = Map provided by Spitzer data"]
-[9.72159194946289, 6.265287399291992, "[FF] Adjustment of the Moving Mirror Alignment Control Bias = Related to the slippage margin"]
-[5.100869655609131, 6.942519187927246, "[TT] Data downlink of the DST 35 = 10-50Mbit/s"]
-[5.467364311218262, 6.388786315917969, "[TT] Capacity of the Onboard data storage = 2.4 Tbit"]
-[8.40439510345459, 2.492424488067627, "[FF] Purpose of the MAIA = Observations of small atmospheric aerosols will be combined with health information to determine the toxicity of different particulate matter types in airborne pollutants over the world's major cities"]
-[6.0500688552856445, 7.876955986022949, "[TT] Phase Variable Range/Step of the D-Amps = Range: 0 to 45\u00ba"]
-[6.288760662078857, 8.072561264038086, "[TT] Main Channels of the ScaRaB = Channels 2 and 3"]
-[7.7689924240112305, 1.2271722555160522, "[FF] Measurement of the Electrostatic Gravity Gradiometer (EGG) = Gravitational field of the Earth"]
-[4.889500141143799, 0.20981663465499878, "[TT] Launch Date of the SPOT-3 = September 1993"]
-[6.3527936935424805, -1.2237861156463623, "[TT] Trailing Satellite of the GRACE-1 = December 10, 2005"]
-[7.622889041900635, 5.397464752197266, "[TT] Objective of the KBR = Ultra-precise satellite-to-satellite tracking in low-low orbit"]
-[5.576808452606201, 4.826972007751465, "[TT] Communication Network of the Spacecraft = NASA's Deep Space Network"]
-[4.312967777252197, 2.458681344985962, "[TT] Launch Site of the CHAMP = Plesetsk Cosmodrome in Russia"]
-[12.042989730834961, 3.4326283931732178, "[FF] Refueling Capability of the MEV = None"]
-[5.809247016906738, 7.200827121734619, "[TT] Data Compression Steps of the RFA Computer = 3"]
-[4.974933624267578, 3.4977779388427734, "[TT] Manufacturer of the C3D Imager = Clyde Space"]
-[9.635071754455566, 4.872053623199463, "[TT] Stabilization of the ALTIUS = Three-axis"]
-[11.08720874786377, 4.045054912567139, "[TT] Sail Surface Area of the SIRDARIA = 1.2 m2"]
-[2.9180006980895996, 1.9673105478286743, "[TT] Image Capture Date of the Copernicus Sentinel-2 = 29 November 2021"]
-[8.169276237487793, 1.3296310901641846, "[FF] Effect on Sea Levels of the El Ni\u00f1o = More than a 30 cm higher than normal"]
-[6.404403209686279, 2.4068758487701416, "[FF] In-Flight Test of the Orion = Micrometeoroid Orbital Debris Vulnerability"]
-[18.798330307006836, 3.4804534912109375, "[TT] Mean \u0394E (m) of the Kirkuk = -3.0"]
-[3.3784255981445312, 4.89705753326416, "[FF] Real-time SAR Data Downlinks of the Oakhanger = 272 minutes"]
-[7.529314994812012, -0.9042966961860657, "[TT] Instrument Optimization Time of the ICESat-2 = About one month after launch"]
-[5.799454212188721, 2.1500461101531982, "[FF] Operation of the APMIR = Provided SSMIS underflights during the March/April 2004 field campaign"]
-[13.22313404083252, 5.269280433654785, "[TT] Array of the Spacecraft = 3 panel/Si with GaAs/articulating/5.25 m"]
-[9.107104301452637, -1.2076244354248047, "[TT] Orbit Position of the EDRS-C satellite = Geostationary orbit at 31\u00b0 East"]
-[9.435312271118164, 5.754992961883545, "[TT] Earth Illumination Angle Constraint of the CHEOPS = Larger than 35\u00ba"]
-[9.558916091918945, 4.804893493652344, "[TT] Control of the Spacecraft = 3-axis stabilized"]
-[6.339356899261475, -1.3481541872024536, "[TT] Launch Date of the GRACE-FO = Early 2018"]
-[5.431816101074219, 1.7186154127120972, "[FF] Commercial Operations Start Date of the HawkEye 360's Third Satellite Cluster = 12 October 2021"]
-[5.817477703094482, 6.501223564147949, "[TT] Data Latency of the GOMX-3 = <5 minutes"]
-[7.961836814880371, -2.5789847373962402, "[TT] Imaging Wavelength of the GOLD = Far ultraviolet light"]
-[14.592239379882812, 6.6196675300598145, "[TT] Type of the Battery = Li-ion"]
-[3.7861275672912598, 5.430870056152344, "[TT] L-band Radar Frequency of the SMAP = 1.26 GHz"]
-[4.97694730758667, 7.902179718017578, "[TT] Control Loop Frequency of the XACT = 20 Hz"]
-[10.926041603088379, 7.551990032196045, "[TT] Swath Width of the COSI = 30 km"]
-[14.236355781555176, 3.192028045654297, "[TT] Mass of the SAOCOM-1A = 3,000 kg"]
-[5.51511287689209, 6.035406112670898, "[TT] Memory of the OBC = 2 x 16 MB SPI NOR-flash data memory"]
-[9.13430118560791, 1.3215676546096802, "[TT] Struggle Duration of the New Horizons = 17 years"]
-[13.465263366699219, 3.0480501651763916, "[TT] Total Mass of the Bus = 128 kg"]
-[4.826493740081787, 0.48265737295150757, "[TT] Launch Date of the WSF-M = January 2024"]
-[8.191359519958496, 0.7429620027542114, "[FF] Mission Goals of the Psyche = Understand the building blocks of planet formation, determine Psyche's age and formation process, and study its surface"]
-[12.100775718688965, -0.350368857383728, "[TT] Mission Duration of the TESS = 2 years"]
-[2.94693922996521, 0.1482059806585312, "[TT] Number of Collision Warnings Provided in 2014 of the JSpOC = 671,727"]
-[9.90174388885498, 2.111065149307251, "[FF] Purpose of the NISS = Star formation history"]
-[5.215266227722168, 8.348793983459473, "[TT] Horizontal Resolution of the MWI = Less than 30 km for the 10 GHz channel"]
-[8.665560722351074, 4.730241775512695, "[FF] Science Objective of the BRITE Constellation = Provide milli-magnitude (0.1% error) differential photometry of bright stars"]
-[7.659383296966553, 6.4556708335876465, "[FF] Trigger of the Arcing Detection Circuit = Voltage across the inductor"]
-[16.551578521728516, 3.6444449424743652, "[TT] In-Orbit Fleet of the OneWeb = 110 satellites"]
-[5.627898693084717, 5.0776591300964355, "[FF] Interface of the ACU = CAN bus"]
-[8.242816925048828, 7.525716781616211, "[TT] Type of the MIR channel detector = InSb (Indium Antimonide) photodiode"]
-[6.2090606689453125, 4.042784690856934, "[FF] FDIR Concept of the AstroBus-L = Hierarchically structured and can easily be adapted to specific mission needs"]
-[6.4838643074035645, 5.608220100402832, "[FF] Concept Developed of the CubeSat-based Optical Crosslink Nodes = Yes"]
-[6.349174976348877, 4.842174530029297, "[FF] Program Motivation of the ISERV = Timely access to data"]
-[5.579264163970947, 0.8855963349342346, "[TT] Global Coverage Date of the BeiDou-2 Navigation Satellite System = 2020"]
-[3.669578790664673, 6.508073329925537, "[FF] Radiating Element of the Parabolic Antenna = Parabolic antenna, a deployable umbrella reflector, with a rigid CFRP (Carbon Fiber Reinforced Plastic) central dish and a set of knitted mesh gores stretched by skeleton ribs"]
-[6.2878313064575195, -0.7447317242622375, "[FF] Duration of the Spacewalk Duration = Six hours and two minutes"]
-[9.579484939575195, 7.051950454711914, "[TT] Resolution of the Measurements = 8 km"]
-[4.813802719116211, -0.9811158776283264, "[TT] Planned Launch Year of the FengYun-4G = 2033"]
-[8.466169357299805, 6.079016208648682, "[TT] Accuracy of the VMAG = \u00b10.1 nT"]
-[8.60272216796875, 7.582483291625977, "[TT] MTF of the CCD Camera = <=0.23"]
-[12.06646728515625, 4.395176410675049, "[TT] Size (deployed) of the Heritage Orbital LEOStar-2 = 3.9 m x 1.2 m x 1.5 m"]
-[13.23338508605957, 7.267537593841553, "[TT] Value of the Peak Power Consumption = < 35 W"]
-[3.4858450889587402, 6.449566841125488, "[TT] Distance of the Antennas = 300 m"]
-[6.854975700378418, 6.555514335632324, "[FF] Data Downlink of the Lasercom = Via Lasercom"]
-[4.863816261291504, 3.7576990127563477, "[TT] Manufacturer of the Antenna = TICRA"]
-[5.767298221588135, 1.2338380813598633, "[FF] Publication Date of the Ministers back ESA's bold ambitions for space with record 17% rise = 23 November 2022"]
-[6.83659029006958, 7.0172834396362305, "[TT] Number of Ka-band user beams of the Al Yah-3 = 53"]
-[7.776599884033203, -0.11954894661903381, "[TT] Daily Downlink Time of the Arctic Ground Station = Approximately 93 minutes"]
-[6.0268707275390625, 1.4302771091461182, "[FF] Recommendations of the IRB = Provided to NASA"]
-[12.457215309143066, 4.8619184494018555, "[TT] Width with Solar Paddles Extended of the Nimbus-7 S/C = 3.96 m"]
-[7.804505348205566, 6.532066345214844, "[TT] Imaging Frequency of the Meteosat-10 = Every five minutes"]
-[10.180156707763672, 8.177618026733398, "[TT] Aperture of the GT = 2.5 cm"]
-[5.80413818359375, 7.118627548217773, "[TT] Data Rate of the OPAL = 9.6 kbit/s"]
-[6.575345993041992, 4.224085330963135, "[FF] Operation of the HTV = Unloading and Loading"]
-[10.635785102844238, 8.8831148147583, "[TT] Pixel size of the Channel 8 = 48 km x 48 km"]
-[4.269257545471191, 4.472479343414307, "[FF] Function of the BRO-1 = Maritime monitoring"]
-[7.192939758300781, 3.0326175689697266, "[TT] Purpose of the ECP-Lite = Provide a focused subset of space environmental data"]
-[10.093757629394531, -1.5913989543914795, "[TT] Inclination of the BUV = 80.1\u00ba"]
-[8.101238250732422, 7.80830717086792, "[TT] Material of the Primary Sensor = Niobium C-103"]
-[9.780754089355469, -0.5398526191711426, "[TT] Orbit Altitude of the WFIRST = One million miles"]
-[14.240701675415039, 3.1965219974517822, "[TT] Mass of the CanX-2 = Unknown"]
-[4.26347541809082, 7.454893112182617, "[TT] Nominal Carrier Frequency of the X-band data transmission = 8192 (T1); 8320 (T2) MHz"]
-[16.549379348754883, 3.6424615383148193, "[TT] Planned Number of Satellites of the OneWeb = Up to 672"]
-[7.931735992431641, 4.917443752288818, "[FF] Calibration Validation of the AirHARP = Ongoing"]
-[10.202052116394043, 1.493453860282898, "[TT] Distance of Interacting Clusters of Galaxies of the eROSITA = About 800 million lightyears"]
-[5.855933666229248, 4.900998115539551, "[FF] Content of the L1-SAIF+ = Differential correction information, information for correcting orbital position and clock errors for 10 satellites, short messages for emergency cases"]
-[9.147034645080566, 5.511260509490967, "[FF] Off Nadir Acquisition Capability of the Satellite = Up to 1 path off nadir"]
-[4.832430839538574, 1.8166327476501465, "[TT] De-orbit Requirement of the HORYU-2 = Within 25 years after launch"]
-[8.885863304138184, 6.466866493225098, "[TT] Primary Images of the PROBA-V = 8.345"]
-[5.687328338623047, 0.2766140401363373, "[TT] Mission Operation Start Date of the WINDS/Kizuna = 2008"]
-[9.128074645996094, 5.503720760345459, "[TT] ACS Jitter of the Spacecraft = \u00b10.125 arcsec/s"]
-[5.059765815734863, 0.7158622741699219, "[FF] Year of the 4th Edition = 2002"]
-[11.416125297546387, 5.701237201690674, "[TT] Material of the Haynes 242 = Nickel-based superalloy"]
-[13.48059368133545, 2.94498348236084, "[TT] Bus Dry Mass of the Spacecraft = 410 kg"]
-[7.770360946655273, 5.436117649078369, "[FF] Sensor Data of the PSSCT-2 = Collected"]
-[5.321836948394775, 1.0955613851547241, "[FF] Assembly Date of the MARFEQ = 10-19 Oct. 10-19, 2002"]
-[12.724590301513672, 3.898730516433716, "[FF] Length of the Reconnecting Lines = A few RE or smaller"]
-[6.2840704917907715, 8.680636405944824, "[TT] Polarizations of the SASS = VV, HH"]
-[5.011710166931152, 3.2196691036224365, "[TT] Manufacturer of the DRF = Nuclear Physics institute (NIIYaF) of the Moscow State University (MSU)"]
-[7.302665710449219, 7.3924407958984375, "[TT] Controller of the HSC-III = Microcomputer: 32bit RISC (SH2)"]
-[6.584044933319092, 5.764458656311035, "[TT] Number of Boards of the OBC = 4"]
-[12.096416473388672, 4.541971683502197, "[TT] Size of the Satellite = 954 mm x 954 mm x 1218 mm"]
-[6.27992057800293, -0.11567211896181107, "[TT] Workshop Frequency of the SSETI Express = Twice a year"]
-[4.913222312927246, 8.283390045166016, "[TT] Frequency Range of the CubeRRT = 6-40 GHz"]
-[5.3753767013549805, 3.8647992610931396, "[TT] Number of Planes of the FormoSat-3/COSMIC-1 = 6"]
-[5.433892250061035, 2.420217275619507, "[FF] Location of the King Saud University campus = Arabic Language Institute"]
-[10.385422706604004, 2.135862350463867, "[TT] Imaging Capability of the NuSTAR = High-energy X-rays"]
-[7.976459980010986, 9.06995677947998, "[TT] Measurement Wavelengths of the TOMS = 308.6, 312.5, 317.5, 322.3, 331.2 and 360 nm"]
-[9.82272720336914, 7.730569839477539, "[TT] Coincidence of the Telescope = Two pin diodes in coincidence"]
-[8.24056625366211, 6.380158424377441, "[FF] Scan Components of the SSM/I = Cold reading, warm load reading, and the scene stations"]
-[8.439494132995605, 1.8596352338790894, "[FF] Function of the CIRAS = Measuring temperature and water vapor profiles"]
-[5.108152389526367, 3.579030990600586, "[TT] Manufacturer of the FR-lite satellite radio = Johns Hopkins University Applied Physics Laboratory"]
-[10.33532428741455, 5.8178277015686035, "[TT] Temperature Sensitivity of the NEDT = 0.01 K to 0.06 K"]
-[7.060703754425049, 5.457123756408691, "[FF] Quantity of the SMDC-ONE-2.3 and SMDC-ONE-2.4 = 2"]
-[6.6502766609191895, 0.24751760065555573, "[TT] Launch Date of the CryoSat = 08 Oct 2005"]
-[5.569847583770752, 2.7976574897766113, "[TT] Managed By of the TESS = NASA's Goddard Space Flight Center"]
-[4.84345006942749, 5.675537586212158, "[TT] Frequency (MHz) of the GPS L1C = 1575.42"]
-[13.193696975708008, 7.249875545501709, "[TT] Power Consumption of the Transponders = 2.7 W"]
-[3.729536294937134, 2.4111459255218506, "[TT] Launch Date of the Iridium NEXT = January 8, 2017"]
-[4.7170090675354, 7.931767463684082, "[TT] Synchronization Signal Frequency of the F-FEE = 50 MHz"]
-[6.925032615661621, 7.832180023193359, "[FF] Linearity/Noise Level or Bias/NF of the Receiver = Use of noise sources"]
-[5.915741443634033, 2.8568735122680664, "[FF] Mission Objectives of the NPSat-1 = Provide hands-on education in space systems for NPS students, demonstrate COTS technology in a spacecraft architecture, provide a more capable platform for spaceflight experiments"]
-[9.998930931091309, -1.5277925729751587, "[TT] Orbital Inclination of the Geotail = About \u20137 degrees"]
-[14.258054733276367, 3.4632606506347656, "[TT] Mass of the Gyro Unit = 1.5 kg"]
-[11.151952743530273, 1.1027770042419434, "[TT] Test Masses Relative Acceleration of the LISA Pathfinder = Lower than ten millionths of a billionth of Earth's gravity"]
-[3.602674722671509, 2.082016944885254, "[TT] Structure of the Sentinel-5P = Hexagonal"]
-[18.803640365600586, 3.467197895050049, "[TT] Mean \u0394N (m) of the Jomo Kenyatta = -11.1"]
-[7.042019367218018, 6.962182521820068, "[TT] Recording Frequency of the Laser Beams = High"]
-[7.970551490783691, 0.7263699173927307, "[FF] Measurement Method of the Gravity satellite = Global mass changes"]
-[5.426334857940674, 1.226505994796753, "[TT] Renaming Date of the Suomi NPP (National Polar-orbiting Partnership) = January 2012"]
-[5.37285041809082, 0.9648827910423279, "[TT] Development and Testing Completion Date of the GLM = Oct. 9, 2014"]
-[8.274190902709961, 7.899448871612549, "[TT] Housing Material of the Detector Stack = Tungsten"]
-[7.284743309020996, 4.686836242675781, "[FF] Function of the NuDose = Force a specified current through the RADFET"]
-[4.970376491546631, 3.4167983531951904, "[TT] Manufacturer of the GESS stations = Indra Espacio"]
-[4.791293621063232, 0.4421616792678833, "[TT] Launch Date of the CuPID = 27 September 2021"]
-[11.231813430786133, 1.8725745677947998, "[FF] Objective of the PR_CuNaR2 = Increase understanding of the outcomes of relevant collisions among millimeter-sized particles, or \u201cpebbles\u201d, in a protoplanetary disk"]
-[10.100480079650879, 2.9378485679626465, "[FF] Launch Date of the Hyper-Angular Rainbow Polarimeter (HARP) CubeSat = Feb. 2015"]
-[7.6817731857299805, 9.428813934326172, "[TT] Center Wavelength of the Band 9 = 6.95 \u00b5m"]
-[11.906332015991211, 5.340237617492676, "[TT] Dimensions of the Instrument Interface Module = 90 mm x 95 mm x 12 mm"]
-[4.373105525970459, 3.1502726078033447, "[TT] Location of the Monitoring and Control Segment = Troms\u00f8, Norway"]
-[14.046293258666992, 7.154681205749512, "[TT] Output Voltage (Nominal) of the LVPS Board = +3.3 V"]
-[5.401905059814453, 6.133923053741455, "[TT] Technology Type of the SDR-SDRAM = SDR-SDRAM"]
-[4.784635543823242, 3.0481929779052734, "[TT] Platform of the BRITE Satellites = GNB (Generic Nanosatellite Bus)"]
-[4.439298629760742, 4.192533493041992, "[TT] Number of GEOLUTs of the LEOSAR = 23"]
-[9.186928749084473, 3.2577970027923584, "[FF] Unique Capability of the Cluster = Allows multipoint measurements of the magnetosphere in different regions and at different scales"]
-[7.94882345199585, 5.92259407043457, "[FF] Production, Assembly, and Testing of the Cameras = Successfully Exercised"]
-[5.386440277099609, 6.560932159423828, "[TT] Total Capacity of the EUTELSAT KONNECT = 75 Gbit/s"]
-[12.094862937927246, 7.619537353515625, "[TT] Instrument Mass of the Imager = 125 kg"]
-[10.620388984680176, 4.4929304122924805, "[TT] Locomotion Mode of the Rosalind Franklin ExoMars rover = Wheel walking"]
-[9.198784828186035, 7.772477626800537, "[TT] Coverage of the Imaging Mode = 20\u00ba N-S and 20\u00ba E-W"]
-[7.2078857421875, 7.602470874786377, "[TT] Data Quantization of the WiFS camera = 7-bit (radiometric resolution of 128 grey levels)"]
-[8.291791915893555, 3.544844388961792, "[FF] Operation Mode of the TSIS-1 = Follows the Sun from sunrise to its sunset, which occurs every 90 minutes"]
-[7.119829177856445, 3.202279567718506, "[FF] Imagery of the GOES-18 SUVI Instrument = First Imagery"]
-[8.735211372375488, 7.106382369995117, "[TT] Data Density of the DMC-2G imager = Doubled"]
-[7.433694839477539, 5.237022876739502, "[TT] Mode of the Satellite = Observation"]
-[5.5649285316467285, 5.713034629821777, "[TT] Processor of the ODHS Processor Module = Atmel 32 bit processor of ARM9 architecture"]
-[7.868462085723877, 5.862562656402588, "[FF] Function of the Payload Cameras = Provide optical imaging"]
-[8.794363021850586, 8.68379020690918, "[TT] Average Efficiency of the Grating = Greater than 60%"]
-[10.345101356506348, 5.624255657196045, "[TT] Nominal Temperature of the Passive Radiant Cooler = 95 K"]
-[9.784079551696777, 7.149394512176514, "[TT] Ground Resolution of the Instrument = 6 km x 7 km"]
-[2.424362897872925, 2.779391288757324, "[TT] PI of the CRaTER = Harlan E. Spence"]
-[6.483480930328369, 4.471359729766846, "[TT] Development Environment of the Attitude Control Software = Matlab-Simulink based simulation"]
-[5.516152858734131, 6.607865333557129, "[TT] Data Volume of the Mini-RF = 200 GB"]
-[6.819577217102051, 4.676798343658447, "[TT] Structure of the Payload Module = Triangular"]
-[12.400385856628418, 3.930798292160034, "[TT] Payload Space of the Bartolomeo = 50+ liters"]
-[4.54573917388916, 1.8940470218658447, "[FF] Launch Date of the ECSAT = 14 June 2017"]
-[9.090652465820312, -1.2236359119415283, "[TT] Orbit of the EDRS = Geostationary"]
-[3.912851333618164, 4.409336090087891, "[FF] Operations of the RADARSAT-2 = Intensive, highly automated, intermittent TT&C pass operations"]
-[11.100912094116211, 5.52915096282959, "[TT] Composition of the Superelastic SMA = Ni50.7Ti49.3 (atomic %)"]
-[6.293062210083008, 4.560320854187012, "[FF] User Interface of the CMS = Simple and robust"]
-[8.72255802154541, 2.0048768520355225, "[TT] Wind Velocity of the Integrated Mobile Station = 25 m/s"]
-[13.899100303649902, 2.738182783126831, "[TT] Launch Mass of the INSAT-3D = Approximately 2060 kg"]
-[12.054713249206543, 3.4643540382385254, "[TT] Signal Interface of the PPCU ion thruster = RS422"]
-[8.042425155639648, 1.237250566482544, "[FF] Dryness of the Atacama Desert = One of the driest places on Earth"]
-[14.2350435256958, 3.185155153274536, "[TT] Mass of the DeOrbitSail = 7 kg"]
-[9.60566520690918, 0.36811619997024536, "[TT] Distance from BEESAT-4 of the BEESAT-4 = 67 m"]
-[4.707055568695068, 6.51401948928833, "[FF] Components of the LPT = Electronics stack, three S-band antennas, one L-band antenna"]
-[9.288202285766602, 0.2689981162548065, "[TT] Side Span Length of the Izmit Bay Bridge = 560 m"]
-[14.469097137451172, 6.59878396987915, "[FF] Battery Storage of the EPS = Capable of sustaining subsystems during operating loads and orbit eclipses"]
-[10.925592422485352, 3.5727832317352295, "[TT] Size of the CubeSats = About the size of a boot box"]
-[5.057648181915283, 3.2361233234405518, "[TT] Contractor of the M3MSat = COM DEV International Ltd."]
-[11.844610214233398, 4.591653347015381, "[TT] Shape of the Spacecraft = Octagonal"]
-[5.666121482849121, 4.609151840209961, "[TT] Source of the Positioner = NASA Deep Space Network (DSN)"]
-[5.962453842163086, 5.406727313995361, "[FF] Type of the TT&C and Payload Data Communication System = Flexible"]
-[5.4049882888793945, 0.28312137722969055, "[TT] Mission Timeframe of the RAVAN = Six months"]
-[7.348654747009277, 2.2988176345825195, "[TT] Global Coverage of the JPSS-1/NOAA-20 = Twice a day"]
-[6.137305736541748, 2.0991132259368896, "[FF] Authors of the ACES = L. Cacciapuoti, Ch. Salomon"]
-[9.746297836303711, -0.7081459760665894, "[TT] Orbit Altitude of the HY-2A = 971 km"]
-[6.673604965209961, 1.8214479684829712, "[TT] URL of the NASA Space Laser Missions = https://www.jpl.nasa.gov/news/news.php?release=2020-086"]
-[7.042471885681152, -0.19376155734062195, "[TT] Peak Totality Duration of the Solar Eclipse = About 2 minutes 40 seconds"]
-[11.11001205444336, 6.106843948364258, "[FF] Material of the Glass and graphite layers = Glass and graphite"]
-[7.043126106262207, 5.8825154304504395, "[TT] Clocks of the GIOVE-B = PHM (Passive Hydrogen Maser)"]
-[4.81381893157959, 0.2697744071483612, "[TT] Launch Date of the ST5 = 22 March 2006"]
-[10.01131534576416, 2.8966472148895264, "[TT] Launch Date of the Sunstorm CubeSat = 17 August 2021"]
-[3.4845495223999023, 6.4169182777404785, "[TT] Antenna Thickness of the Subarray = 9 mm"]
-[8.362544059753418, 3.966008424758911, "[FF] Calibration Methods of the SeaWiFS = Short-period solar calibration, long-term lunar calibration"]
-[8.558722496032715, 2.0743658542633057, "[FF] Effect of the Stratospheric Polar Vortex = Trapped cold air in the Arctic"]
-[7.372629642486572, 3.806939125061035, "[FF] Exposure Orientations of the MISSE Flight Facility = Ram, wake, zenith, and nadir"]
-[5.923558235168457, 3.411302328109741, "[TT] Quantity of the Flights Tracked = 150,000+ per day"]
-[6.805365085601807, 2.832319736480713, "[FF] Collaboration Partner of the MethaneSAT = MBIE (Ministry of Business Innovation & Employment)"]
-[10.095151901245117, -1.587404727935791, "[TT] Inclination of the ZY 1-02C = 98.5\u00ba"]
-[9.225310325622559, 3.9186739921569824, "[FF] Photoresistor of the Solar Panel = Mounted to its outer face"]
-[9.134681701660156, 8.053324699401855, "[TT] Focal Plane Array of the ISIR = 327 x 240 pixel"]
-[5.076751232147217, 7.341561317443848, "[TT] Command Bit Rate of the RF communications = 500 bit/s"]
-[9.488332748413086, 5.0379204750061035, "[TT] Attitude Pointing Knowledge of the QuickBird-2 = \u00b10.0008o (3? steady state in all three axes)"]
-[7.717797756195068, 9.083847999572754, "[TT] Wavelength Range of the Band No 3 = 1.60 \u00b10.50 - 1.80 \u00b1 0.50 \u00b5m"]
-[6.185561656951904, 2.618762493133545, "[FF] Service Module of the Orion Multi-Purpose Crew Vehicle = Unknown"]
-[4.332062721252441, 3.9740493297576904, "[TT] Number of Galileo Channels of the GETR (Galileo Experimental Test Receiver) = 7"]
-[2.838369846343994, 0.08529844135046005, "[TT] J2000 declination (deg) of the B1617-155 (Sco X-1) = -15.640"]
-[5.415157318115234, 0.43586236238479614, "[TT] Mission End Date of the Triana = Unknown"]
-[8.410344123840332, 4.670365333557129, "[FF] Components of the ACS = Three magnetic torquers (MTQ, total mass of 90 gram), a magnetometer (Honeywell HMC2003), a sun sensor (FOV \u00b145\u00ba) and a gyroscope (range of \u00b1 200\u00ba/s)"]
-[5.003811836242676, -0.6267112493515015, "[TT] Release Time of the SLATS = Less than 6,700 seconds"]
-[9.534505844116211, 7.2063775062561035, "[TT] Nadir Visual Imaging Resolution of the Westinghouse OLS = 0.55 km during daytime and 3.7 km at night"]
-[5.189420223236084, 8.376166343688965, "[TT] Channel Bandwidth of the TT&C = 25 kHz"]
-[5.724395275115967, 7.312532901763916, "[TT] Specific Impulse (Isp) of the BIT-3 = 2,250 s"]
-[7.538028717041016, 2.3849735260009766, "[TT] Temporal Resolution of the GIIRS = 55 minutes (China area mode), 30 minutes (Mesoscale mode)"]
-[12.303284645080566, 0.5739949941635132, "[FF] Purpose of the PLATO = Find the second Earth"]
-[3.0807034969329834, 2.1790125370025635, "[FF] Ocean Measurements of the Copernicus Sentinel-3 = Temperature, colour and height of the sea surface"]
-[13.362037658691406, 2.8625316619873047, "[TT] Average Crust Density of the InSight = 2,582 kg/m3"]
-[7.866568565368652, 6.118953704833984, "[FF] Type of the MUX = Multi-spectral radiometers"]
-[14.620323181152344, 6.658905029296875, "[TT] Battery Type of the EPS = 2 x 66 Ah Li-ion batteries"]
-[4.712540626525879, 7.944718837738037, "[TT] Frequency of the Transmitting Frequency = 465.9875 MHz"]
-[8.526535987854004, 1.3648896217346191, "[TT] Average Salinity of the Aquarius = About 35"]
-[9.40905475616455, 6.705874443054199, "[TT] Azimuth Resolution of the ScanSAR = 18.5 m"]
-[6.202490329742432, 2.513906240463257, "[FF] Symposium Date of the Air Force Academy Department of Physics Space Technologies Development and Research = May 19-22, 2014"]
-[5.583648681640625, 6.181951999664307, "[TT] Operating Modes of the FTHSI = 512 x 512, 512 x 1024, and 1024 x 1024"]
-[11.460847854614258, 4.520373344421387, "[FF] Shape of the Plasmasphere = Doughnut-shaped"]
-[9.803245544433594, -0.24340245127677917, "[TT] Peaking Measurement Heights of the SSM/T-2 = 0 to 10 km"]
-[6.312168121337891, 3.313434362411499, "[FF] Purpose of the Tools = Future spacewalks to prepare the station for the installation of the new international docking adapters"]
-[4.279470443725586, 7.236147880554199, "[TT] Ka-Band Terminal of the Astro Digital Satellites = Second-generation"]
-[5.392102241516113, 3.9107697010040283, "[TT] Number of Satellites of the FY-4 = 7"]
-[10.115754127502441, -1.4754921197891235, "[TT] Inclination of the RISAT-1 = 97.6\u00b0"]
-[11.5418119430542, 3.4638161659240723, "[FF] Current Design of the DFACS = CGPS (Cold Gas Propulsion System)"]
-[8.85361099243164, 6.941771507263184, "[TT] GSD of the DMC-2 = 22 m"]
-[7.778237819671631, 8.804718017578125, "[TT] Spectral Band Wavelengths of the ERIP = 252.0, 273.5, 283.0, 292.2, 301.9, 320.0, 340.0 nm"]
-[3.5574283599853516, 3.831981897354126, "[FF] Constellation Concept of the PAZ-TerraSAR Constellation = Coordinated Constellation Concept (CCC)"]
-[10.555137634277344, 5.763594150543213, "[TT] Type of the KELT-9 b = Hot"]
-[8.883557319641113, -0.0011165643809363246, "[TT] Latitude Range of the TanSat = -82\u00ba to 79\u00ba"]
-[8.130274772644043, 5.874342441558838, "[FF] FPN Measurement Method of the Sensor = Capturing and averaging a series of 50 dark images, each containing 10 \u00b5s exposure time"]
-[6.036005973815918, -1.902260661125183, "[TT] Board Member of the Viasat = Jim Bridenstine"]
-[10.291149139404297, 7.889171123504639, "[TT] Instrument Size (Unfolded) of the DST (Dobson Space Telescope) = 100 mm x 100 mm x 210 mm"]
-[12.619086265563965, 9.094748497009277, "[TT] Equatorial Crossing Time of the Orbit = 12:00 hours"]
-[9.60150146484375, 7.100063800811768, "[TT] Spatial Resolution of the PMI = 4 x 2 km"]
-[6.438784122467041, 0.6099145412445068, "[TT] Launch Date of the Landsat-9 = September 2021"]
-[7.178035736083984, 5.169763565063477, "[FF] Stacking Components of the Modulator Assembly = Niobium spacer rings, individual grids, sapphire spacer rods and rings"]
-[5.042543411254883, 7.4099249839782715, "[TT] Polder Data Rate of the RF communications = 0.882 Mbit/s"]
-[5.897560119628906, 0.8519609570503235, "[FF] Meeting Date of the Nigerian National Geospatial Data Infrastructure Programme = March 1-2, 2007"]
-[4.996184825897217, -0.19634303450584412, "[TT] Launch time (JST) of the GOSAT-2 = 13:08:00"]
-[6.624017238616943, 6.038050174713135, "[FF] Reliability Requirements of the LRI = Less stringent than the primary KBR instrument"]
-[13.987753868103027, 2.8658692836761475, "[TT] Mass of the BRITE spacecraft = about 7 kg"]
-[12.619853973388672, 9.097622871398926, "[FF] Cross Equator Time of the VIIRS = Early in the morning local time"]
-[7.074954509735107, 3.594820261001587, "[FF] Acta Astronautica Vol. of the PROBA-3 = 82"]
-[6.321128845214844, 4.070170879364014, "[FF] Heritage of the Avionics Core = Multi-mission version of avionics"]
-[7.198635578155518, 2.759854793548584, "[FF] Phase 2 Date of the MethaneAIR = July and August 2021"]
-[6.880425930023193, -0.2919703423976898, "[TT] Years on Orbit of the AISSat-1 = 3 years"]
-[7.910337448120117, 9.105161666870117, "[TT] Wavelength of the Wavelength = 427.8 nm"]
-[7.967581272125244, 5.128512382507324, "[FF] Calibration of the DDM = Absolute"]
-[7.8622026443481445, 1.0810011625289917, "[FF] Doppler and differential VLBI techniques of the Kaguya (SELENE) = 4-way"]
-[4.864251136779785, 8.274353981018066, "[TT] Frequency of the IceCube = 883-GHz"]
-[8.176299095153809, 6.369048118591309, "[TT] Measurement Frequency of the TEMPO = Hourly"]
-[8.508631706237793, 0.18893539905548096, "[FF] Solar Wind Behavior of the Comet 67P = Beforehand, particles had been slower-moving, and the solar wind had been generally weaker"]
-[7.710509300231934, 3.918917655944824, "[FF] NASA Instruments of the Rosetta spacecraft = Three"]
-[5.2757062911987305, 0.30476415157318115, "[TT] Operation Start Date of the RAVAN = Jan. 25"]
-[5.778546333312988, -0.6224042773246765, "[FF] Development Time of the NPSAT-1 = Years"]
-[6.152726650238037, 4.095853328704834, "[FF] Modularity of the Open Cosmos satellite = Achieved by standardisation of interfaces between subsystems and within them"]
-[6.218770503997803, -0.3293359577655792, "[TT] Expected Lifetime of the SpinSat = >6 months"]
-[10.558419227600098, 3.3283939361572266, "[TT] Form Factor of the Spacecraft = 12U CubeSat"]
-[11.714560508728027, 4.60186243057251, "[TT] Diameter after Expansion of the Genesis-2 = 2.54 m"]
-[5.235550403594971, 0.6300598978996277, "[FF] Launch Date of the Minotaur-C rocket = Nov. 1, 2017"]
-[3.757504463195801, 4.575160980224609, "[FF] Image Type of the ICEYE-X2 = Radar"]
-[3.8279213905334473, 0.8981567621231079, "[FF] User Manual Date of the PSLV = 15 December 2014"]
-[3.2916579246520996, 2.269319772720337, "[FF] Product Type of the Sentinel-1 = GRD (Ground Range Detected)"]
-[6.6213579177856445, 3.626922369003296, "[FF] Data Provided of the MetOp Satellites = ATOVS, AVHRR, ASCAT and IASI Data"]
-[9.417423248291016, -0.6770117282867432, "[TT] Orbit of the AstroBio CubeSat (ABCS) = MEO (~5900 km)"]
-[11.423530578613281, 4.847973346710205, "[TT] Diameter of the DSS 43 = 70-meter"]
-[9.620621681213379, 8.230294227600098, "[TT] Field of View of the SCA = 18\u00ba x 16\u00ba"]
-[4.67141056060791, 5.472148895263672, "[FF] Operation of the Automated Beacon Network = Broadcasts a health message periodically"]
-[11.417258262634277, 4.325701713562012, "[TT] Size of the RadCube = 3U"]
-[10.524869918823242, 4.8949713706970215, "[FF] Development Date of the Multi-Needle Langmuir Probe System = May 25, 2009"]
-[4.782576084136963, 0.20468994975090027, "[TT] End of Life Date of the FORUM = December 2031"]
-[9.692741394042969, -0.5967841744422913, "[TT] Altitude of the ICESat-2 = 496 km"]
-[7.516655921936035, 2.1617555618286133, "[FF] \u00b150\u00b0 latitude of the Satellite = Population distribution"]
-[5.855199337005615, -0.03986211121082306, "[TT] Identification Time of the CSpOC Catalog = 8 days after launch"]
-[8.252854347229004, 7.77169132232666, "[TT] Number of Detectors of the AGRI = 216"]
-[6.027763366699219, 4.704736709594727, "[FF] Function of the BJ3A1 satellite ground pre-processing system = Receives raw data received by the ground station for processing"]
-[8.576650619506836, 6.011667251586914, "[TT] Systematic Cross-Track Bias of the Baseline Products = At most 2 mm"]
-[6.917259693145752, -1.7732988595962524, "[TT] Sea-state bias of the Jason-2 = 1.8 cm"]
-[5.20878791809082, 1.237321376800537, "[FF] Conference Date of the AISsat-1 = June 11-15, 2012"]
-[9.907218933105469, 4.586336612701416, "[TT] Attitude Control of the STARE-B = Full set of reaction wheels"]
-[12.935269355773926, 7.099926471710205, "[TT] Power Consumption of the Proton Monitor Las Dos Torres = 1.56 W"]
-[5.495376110076904, 6.298611164093018, "[TT] Status of the M3MSat = In storage"]
-[9.752803802490234, -0.590292751789093, "[TT] Orbit Altitude of the PRISMA = ~725 km"]
-[11.631508827209473, 4.652453899383545, "[TT] Total Height of the ESM = 4.0 m"]
-[9.097182273864746, 1.3652838468551636, "[TT] Communication Status During Upgrade of the Voyager 2 = Still be able to receive science data from Voyager 2"]
-[4.756992340087891, 8.5534086227417, "[TT] Center Frequency of the Channel 6 = 42 GHz"]
-[10.994294166564941, 6.3057684898376465, "[TT] Material of the TPS = C-SiC (Carbon-Silicon Carbide)"]
-[4.238543510437012, 3.0898373126983643, "[FF] Ground Stations of the Sentinel-1 = Svalbard, Maspalomas, Matera"]
-[10.045393943786621, 7.552199363708496, "[TT] Manufacturer of the PP Twin Telescopes = SAGEM-REOSC"]
-[4.113189220428467, 5.283370018005371, "[TT] Frequency of the SARSAT payload = 406 MHz"]
-[6.33197021484375, -1.329765796661377, "[TT] MWI Switchover Date of the GRACE-FO = November 01, 2018"]
-[8.956119537353516, 7.369335651397705, "[TT] Resolution of the Imager = 2592 by 2192 pixels"]
-[7.273263931274414, 5.290714263916016, "[TT] Qualification Approach of the Curtiss Wright = Space COTS Qualification"]
-[13.791462898254395, 3.0683677196502686, "[TT] Payload Mass of the SV-24 = < 10 kg"]
-[7.0050225257873535, 8.390536308288574, "[TT] Nominal SNR of the Band 7 = 860"]
-[6.785313606262207, 4.146015644073486, "[FF] Instrument Provider of the Ball Aerospace = Unknown"]
-[10.124419212341309, -2.718369245529175, "[FF] Radiation Sensitivity of the NAND-Flash devices = High"]
-[4.731616020202637, 3.227236032485962, "[FF] In Charge of of the Thales Alenia Space = Avionics and integration for the service module (SVM)"]
-[10.41360855102539, 3.3473923206329346, "[TT] Receiver of the CTECS-A = The Aerospace Corporation\u2019s PNT CubeSat receiver"]
-[9.933123588562012, 9.008261680603027, "[TT] Effective FOV of the Channel 1 = 89 km x 198 km"]
-[6.701679229736328, -0.23212465643882751, "[TT] Revisit Time of the Capella's Satellites = 2-5 hours"]
-[10.100725173950195, -0.5020946264266968, "[TT] Orbit Altitude of the Polar Scout 6U CubeSat = 575 km"]
-[8.145018577575684, -0.8691602945327759, "[TT] Greenland and Antarctic Ice Sheets Elevation Change Measurement of the ICESat-2 = Over 16 years"]
-[11.80426025390625, 6.746707439422607, "[TT] Energy Range of the XGRE = 20 keV-12 MeV"]
-[4.279945373535156, 0.7489379644393921, "[TT] Integration Date of the EDRS-C terminal = March 2017"]
-[6.7122931480407715, 4.808733940124512, "[FF] Function of the EM = Monitor, report, and enable an operator response to anomalous conditions"]
-[7.693870544433594, 7.123706340789795, "[TT] Point Source Sensitivity of the eROSITA = ~30 times better than ROSAT (soft band 0.5-2 keV) and ~100 times better than HEAO/RXTE (hard band 2-10 keV)"]
-[10.010967254638672, 1.6488237380981445, "[FF] Discovery of the Hubble = Myriad galaxies beyond our own"]
-[13.811478614807129, 2.939401865005493, "[FF] Mass of the Voyager = Unknown"]
-[9.136844635009766, 7.352761268615723, "[TT] Resolution of the Camera = 1 km"]
-[5.1164960861206055, 4.137183666229248, "[FF] Ground Segment Platforms of the Argos/DCS = Buoys, free-floating balloons, wildlife, remote weather stations"]
-[5.104242324829102, 5.865510940551758, "[TT] Number of Users of the GSM = 480 million"]
-[8.872984886169434, 9.56692886352539, "[FF] Band 4 Wave Numbers of the TANSO-FTS-2 = 1183 - 1800"]
-[9.677738189697266, 5.3525214195251465, "[TT] Pair Orientation of the DBCP = The wedges of a pair are bonded with crossed crystal axes, and the first pair is rotated by 45\u00b0 w.r.t. the second one"]
-[5.265737056732178, 0.7029705047607422, "[TT] Data Collection Start Date of the COWVR = Jan. 7, 2022"]
-[3.648869276046753, 5.019164085388184, "[FF] Instruments of the JERS-1 = L-band SAR, OPS, JERS-1 Comms"]
-[8.329774856567383, 7.083099365234375, "[TT] Sensor of the Lateral System = CMOS sensor"]
-[9.195380210876465, 4.777601718902588, "[TT] Attitude Data Acquisition Time of the Procyon = 8 seconds from power-on"]
-[4.543301582336426, 6.275111198425293, "[TT] Solving Scheme of the MLFMM (Multilevel Fast Multipole Method) = Recursive"]
-[6.975673198699951, 3.851336717605591, "[FF] URL of the Anti-Coincidence Counter = http://ams.cern.ch/AMS/Reports/TIMOct05/TOF/03_ACC_Wallraff.ppt"]
-[5.631385326385498, 2.402989387512207, "[FF] Affiliation of the Ayyoob Sharifi = Urban Knowledge-Action Network"]
-[6.122890949249268, 5.7636847496032715, "[TT] Data/Pilot of the L1-A = Classified"]
-[9.88329792022705, 2.70715594291687, "[FF] Testing and On-orbit Performance of the Micro/Nano Satellites = Unknown"]
-[9.731324195861816, 5.785994052886963, "[TT] Number of Thermistors of the Dosimeter Suite = 2"]
-[6.256230354309082, 6.461836338043213, "[TT] Group Delay of the Receiver = \u2264 13 \u00b5s"]
-[7.93988561630249, 4.725894927978516, "[FF] Measurement of the DFACS = Accurately measures the spacecraft accelerations in 6-DoF (Six Degrees of Freedom)"]
-[10.298081398010254, 6.141647815704346, "[TT] Average Cabin Temperature of the Metric Camera = 22\u00ba C"]
-[6.192293643951416, 1.3955787420272827, "[TT] Launch Date of the eROSITA = 13 July 2019"]
-[5.924991607666016, 2.785283088684082, "[TT] Electronic Parts of the Legion = Rad-hard/tolerant level 1/2"]
-[5.711925506591797, 6.8737711906433105, "[TT] Data Acceptance Rate of the SSR = Up to 400 Mbit/s"]
-[12.125513076782227, 3.6828184127807617, "[TT] Xenon Pressure of the EPTA = 150 bar BOL"]
-[6.12196683883667, -0.5307499766349792, "[FF] End-of-Mission (EOM) Altitude of the PUNCH Mission = Passivated and naturally reenter within 22 years"]
-[6.174067974090576, 5.820047855377197, "[TT] Quantity of the FPGAs = 6"]
-[6.140315532684326, 4.981770038604736, "[FF] Software of the TIE = Payload Control (PLC) software"]
-[3.397488832473755, 6.409298419952393, "[TT] Diameter of the Antenna dish = 10 m"]
-[5.7609710693359375, 4.8311357498168945, "[FF] Data Relay Method of the DMSP Ground Stations = Commercial communications satellites"]
-[6.620810508728027, 5.624709606170654, "[FF] Data Sensitivity of the PAMELA = Exceeds current data by several orders of magnitude"]
-[13.57296085357666, 5.863119602203369, "[TT] Power Output of the Solar Array = 2.2 kW"]
-[5.532558441162109, 5.988516330718994, "[TT] Computer Memory Interfaces of the SMEX = Four EIA RS422 Direct Memory Access (DMA) interfaces"]
-[6.069699764251709, 5.502192974090576, "[TT] Redundancy Type of the RPU = Cold internal redundancy"]
-[9.66569709777832, 8.357758522033691, "[TT] Mask at Intermediate Image Plane FOV of the TIR Subsystem = \u00b111.3\u00ba"]
-[8.70242977142334, 7.01018762588501, "[TT] Resolution of the TDI imaging technology = 1.3 m"]
-[4.90781831741333, -0.6096016764640808, "[FF] URL of the SLATS = http://global.jaxa.jp/projects/sat/slats/"]
-[4.540095329284668, 5.6991424560546875, "[FF] External Configurations of the GomX-4 = Antennas, sensors, solar panels, radiation shields and radiative surfaces"]
-[7.074337005615234, 6.580076694488525, "[FF] Total Noise of the GLM = Varies by several counts over small spatial scales"]
-[12.04501724243164, 3.150644540786743, "[TT] Propellant Type of the Chemical Propulsion Thrusters = Monomethylhydrazine and nitrogen tetroxide"]
-[4.885769367218018, 0.66981440782547, "[TT] Launch Date of the AAUSat-1 = June 30, 2003"]
-[9.129195213317871, 7.00497579574585, "[TT] Imagery Resolution of the WorldView-3 = 30 cm"]
-[9.436880111694336, 2.282219648361206, "[TT] Total of the Elves = 23104"]
-[6.165998935699463, 4.796629905700684, "[FF] Operation Type of the FOP = Telemetry verification"]
-[10.22618293762207, 4.013523578643799, "[FF] Mounting Technique of the MPO-MAG instrument = Boom mounting technique"]
-[5.237548828125, 0.7717623710632324, "[TT] Agreement Date of the Spire Global = August 14, 2019"]
-[7.05898380279541, 6.814052581787109, "[FF] Response of the APD = High-speed"]
-[7.843019962310791, 3.5007259845733643, "[TT] Sensor complement / remarks of the Cosmos-1066 (Astrofizika) = Exp. payload on Meteor-1 satellite technology,special geophysical experiment (look for artificial light sources on Earth)"]
-[4.551584720611572, 3.002053737640381, "[TT] Operation Center of the SAOCOM-1A = Mission Operation Center in CETT (Centro Espacial Te\u00f3filo Tabanera), CONAE \u2013Cordoba"]
-[5.180647373199463, 5.302380084991455, "[TT] Connection Type of the Ground Station = Ethernet over IP (Internet)"]
-[8.939300537109375, 5.631167411804199, "[TT] Self-Position Accuracy of the ADCS = < 50 m"]
-[9.793137550354004, 8.721776008605957, "[TT] FOV of the Visible Band = 1 mradian"]
-[7.05196475982666, 3.7134530544281006, "[FF] Formation Flying of the DelFFi = QB50 Constellation"]
-[4.919346809387207, 3.2005953788757324, "[FF] Cooperation Agreement of the SSOT = Includes provision for Chilean engineers to work alongside the Astrium development team"]
-[11.221290588378906, 5.939451217651367, "[TT] Coating of the Aluminum Spheres = Space-rated flat white paint (AZ-93 white paint)"]
-[10.919456481933594, 0.8417351841926575, "[TT] Orbited by of the Red Dwarfs = An average of two to three planets"]
-[7.385183334350586, 7.7076416015625, "[FF] Spectral Efficiency of the VCM Mode = Better"]
-[5.536404609680176, 3.896010637283325, "[TT] Number of Satellites of the OptiSAR\u2122 Constellation = 16"]
-[1.9434598684310913, -0.4017219543457031, "[TT] Shutdown Date of the Van Allen Probes = July 19, 2019"]
-[13.168323516845703, 7.185324192047119, "[TT] Power Consumption of the REM = 5 W"]
-[12.165033340454102, 3.0018746852874756, "[TT] Type of the Monopropellant hydrazine = Monopropellant hydrazine"]
-[14.609063148498535, 6.6681413650512695, "[TT] Battery Capacity of the S/C = 920 mAh"]
-[3.5916452407836914, -0.9948426485061646, "[TT] Orbit of the GRACE-FO = Circular polar orbits"]
-[9.039740562438965, 7.342041492462158, "[TT] Resolution of the Optical Payload = 2.9 m/pixel"]
-[11.417532920837402, 4.360367298126221, "[TT] Size of the Shields-1 = 3U"]
-[14.213729858398438, 3.257488965988159, "[TT] Mass of the Freqbone = 10 kg"]
-[5.342649936676025, 6.850714683532715, "[TT] RF Carrier Data Rate of the RISAT-1 DRS = 160 Mbit/s"]
-[9.367148399353027, 4.2999396324157715, "[TT] Manufacturer of the 3-axis magnetometer = Honeywell"]
-[5.0978217124938965, 0.22249773144721985, "[TT] Launch Date of the LDEF = April 6, 1984"]
-[4.950502872467041, 1.3471065759658813, "[TT] Long-Term Stability of the MIRAS = 0.18 K/year"]
-[6.570757865905762, 3.5343050956726074, "[TT] Data Source of the IMERG = GPM Core Observatory, GPM Constellation"]
-[5.137945652008057, 2.3057761192321777, "[TT] Mission Type of the ZACUBE-2 = Non-EO"]
-[8.486095428466797, 7.055176734924316, "[FF] Detector of the Image Quality = Up to 3 Rsun"]
-[4.816487789154053, 7.024885177612305, "[TT] Model of the BayPac BP-96A modem = BayPac BP-96A"]
-[5.503203868865967, 1.2773252725601196, "[FF] Modules Integration Date of the ExoMars = 6 September 2019"]
-[6.998012542724609, 4.6679368019104, "[FF] Parameter of the LRO, LEND, LAMP, DVNR, LOLA, LROC, LADEE = Value"]
-[6.581537246704102, -0.7357255220413208, "[TT] Anomaly Investigation Duration of the NextSat = Additional week"]
-[11.46484661102295, 4.811558723449707, "[TT] Shape of the M1 = Aspheric of-axis concave"]
-[3.5738065242767334, 4.900443077087402, "[FF] Processing Modes of the Poseidon-4 radar altimeter = Conventional pulse-width limited processing (low-resolution mode) and simultaneous high-resolution (HR) processing (SAR mode)"]
-[8.467720031738281, 0.8199428915977478, "[TT] Total Land Area of the Kiribati = 800 km2"]
-[7.429913520812988, 3.5139660835266113, "[FF] Collision Avoidance Requirement of the IDEA OSG 1 = If there is sufficient probability that IDEA OSG 1, during its operations, will collide with an uncontrollable resident space object, then IDEA OSG 1 should control its own orbit to the best of its ability to avoid the collision"]
-[4.942837238311768, 3.2978732585906982, "[TT] Manufacturer of the Nauka = RSC Energia"]
-[8.200789451599121, 4.466534614562988, "[TT] Usage of the Gray lamps = Turned on during the calibration session (typically once per day)"]
-[8.202879905700684, 6.123051166534424, "[TT] Accuracy of the Rangefinder Module = 20 cm"]
-[9.30369758605957, -0.5206999778747559, "[TT] Maximum Cube Size of the Orbit Your Thesis! 2019 program = 4U"]
-[4.41195011138916, 7.726413726806641, "[TT] Frequency of the Downlink (Ku-band) = 20 GHz"]
-[8.58010482788086, 5.227229118347168, "[TT] Resolution of the GFO Accelerometer = Better than 10-10 ms-2 Hz-1/2"]
-[6.090446472167969, 5.235214710235596, "[FF] Telemetry Transfer of the Interfaces = Flawless"]
-[7.871555328369141, 2.1303775310516357, "[FF] URL of the Ocean Color and Temperature Scanner (OCTS) = http://www.eorc.jaxa.jp/en/hatoyama/etc/images/adeos_first/octs_ir_e3.html"]
-[5.457077980041504, 6.2074456214904785, "[FF] Memory of the Avionics bus = microSD (2 GB), and 3Mbit FRAM"]
-[7.722745418548584, 6.228812217712402, "[FF] Image Acquisition Time of the VIIRS = 1:35 p.m. local time (19:35 Universal Time) on May 30, 2022"]
-[3.270794153213501, 5.228106498718262, "[TT] Look Angle of the SAR = 20\u00ba"]
-[3.461461305618286, 1.6553443670272827, "[FF] Bulletin Publication Date of the Sentinel-2 = May 11, 2015"]
-[12.059683799743652, 3.405241012573242, "[TT] Mass of the Ion Thruster = 2 kg"]
-[9.581088066101074, 8.268228530883789, "[TT] Field of View of the ISO Instrument = 0.65\u00ba x 0.01\u00ba"]
-[3.4205081462860107, 1.7746403217315674, "[FF] Implementation of the Sentinel Asia = First Step"]
-[5.174294471740723, 6.365252494812012, "[TT] Communication Speed of the SpaceWire NEXTAR = Up to 400Mbit/s per channel"]
-[6.293084144592285, 4.043825149536133, "[FF] Hosted Payloads of the Prometheus Satellite = 1.5U payload module can be added to each satellite"]
-[9.3707275390625, 5.060605525970459, "[TT] Attitude Control Accuracy (Roll, yaw) of the HAUSat-2 = < \u00b13\u00ba"]
-[8.3643159866333, 8.765323638916016, "[TT] Dust Measurement Altitude of the UVS = Down 300 m"]
-[7.598505973815918, 6.897877216339111, "[TT] Cadence of the MiniCOR = ~15 images/hour"]
-[11.94812297821045, 4.966328144073486, "[TT] Form Factor Dimensions of the Myriad RF board = 50 mm x 55 mm"]
-[5.228254318237305, 2.3260252475738525, "[TT] Mission Type of the ALL-STAR = Non-EO"]
-[8.662707328796387, 8.23255729675293, "[TT] Light Diffraction Reduction of the ASPIICS = 2 to 5 times"]
-[5.834353923797607, -0.17923465371131897, "[TT] Operation Period of the CEASE = 6 months"]
-[6.281660079956055, 2.5006039142608643, "[TT] Managing Institution of the Carruthers Geocorona Observatory = University of California, Berkeley (UC Berkeley)"]
-[6.9914374351501465, 6.915318012237549, "[TT] Use of the TEA-CO2 lasers = Spectroscopic measurements"]
-[8.127625465393066, 0.9435489177703857, "[TT] Soil Moisture Measurement Date of the GRACE-FO = August 10, 2020"]
-[10.102156639099121, -1.486807107925415, "[TT] Inclination of the FASat-Alfa = 82.5\u00ba"]
-[13.52394962310791, 2.9257915019989014, "[TT] Platform Weight of the Satellite Vu = 100 kg"]
-[9.003501892089844, 4.500539779663086, "[TT] Quantity of the Sun sensors = 6 units"]
-[9.981033325195312, -1.4043304920196533, "[TT] Orbit Inclination of the SCATSat-1 = 98.1\u00ba"]
-[8.703128814697266, 2.0178842544555664, "[TT] Accuracy of the Wind Direction Measurements = 20\u00ba"]
-[8.163626670837402, 0.09317340701818466, "[FF] URL of the Meteor-M No.2-1 = https://en.wikipedia.org/wiki/Meteor-M_No.2-1"]
-[12.311269760131836, 0.5701443552970886, "[FF] Transit Signal Detection Method of the PLATO = Measurement of the so-called transit signal"]
-[7.778800010681152, 8.833962440490723, "[TT] MWIR Band Wavelength Range of the OHIS = 3.0 - 5.0 \u03bcm"]
-[10.286888122558594, 3.237144708633423, "[FF] Mission Goals of the ALBus 3U CubeSat = Technology demonstration, Power distribution, Battery charging, Shape Memory Alloys deployment"]
-[6.65710973739624, 3.561558961868286, "[FF] Information Stream of the EMWIN = Live stream of weather and other critical information"]
-[3.115001916885376, 4.52217435836792, "[FF] Data Link Subsystem of the XSAR = DLS"]
-[11.157140731811523, 0.7326001524925232, "[TT] Photometric Signal Precision of the CHEOPS = 20 ppm in 6 hours of integration time for a 9th magnitude star"]
-[6.224632740020752, 4.507730484008789, "[FF] Instrument Operations of the Spacecraft = Performed \"offline\" of the MOC"]
-[8.202698707580566, 7.235869407653809, "[FF] Operational Modes of the GIS Instrument = Simultaneous panchromatic and multispectral (pan-sharpened), Panchromatic only, Multispectral only"]
-[7.8027663230896, 2.987293004989624, "[TT] CO2 Annual Flux Estimation Error of the GOSAT = 0.54GtC/yr to 0.27GtC/yr"]
-[6.796701431274414, 1.828383207321167, "[FF] URL of the WIND = http://www-spof.gsfc.nasa.gov/istp/wind/wind_inst.html"]
-[6.613256931304932, 5.228910446166992, "[TT] SASAR System of the DRT = Not Carried"]
-[10.18056869506836, 4.417342662811279, "[TT] Actuation Control of the Canopus Pipper = 3-axis"]
-[7.678258419036865, 8.759251594543457, "[TT] Channel Wavelengths of the IIR = 8.65 \u00b5m, 10.6 \u00b5m, 12.05 \u00b5m"]
-[9.146805763244629, 6.887388706207275, "[TT] Ground Instantaneous Field of View (GIFOV) of the Climate Observatory = 50 m"]
-[8.372730255126953, 3.2300236225128174, "[TT] Long-term Stability of the Ozone Measurement Instrument = 1% over 7 years or better"]
-[8.632575988769531, 7.818064212799072, "[TT] Maximum Count of the Maximum count per pixel = 500,000"]
-[5.990004539489746, 1.705946683883667, "[FF] Web Source of the MEIDEX = No longer available"]
-[9.042914390563965, 2.6564888954162598, "[FF] Mission Objective of the IMAP = Learn more about the generation of cosmic rays in the heliosphere"]
-[4.825750827789307, -1.0344302654266357, "[FF] Launch Date of the Chinese satellite = Aug. 16, 2016"]
-[8.508749008178711, 6.629981517791748, "[FF] Stability of the Scanner = Highly accurate and stable"]
-[7.798013210296631, 5.897886753082275, "[FF] Components of the Multispectral Camera = Electrooptical assembly, management and control unit, signal processing unit"]
-[5.216302871704102, 2.803781270980835, "[TT] Collaborating Organizations of the MySat-1 = Yahsat, Khalifa University of Science and Technology, and Northrop Grumman"]
-[10.406428337097168, 2.288055658340454, "[FF] Event Identification of the CZTI = Compton scattering criteria"]
-[5.342365264892578, 7.682992935180664, "[TT] EIRP of the Mobile Link = 65 dBW @ NPR=16 dB"]
-[11.151504516601562, 5.5096540451049805, "[TT] Thickness of the Ejecta Deposits at TD2 = Between 1.0 mm to 1.8 cm"]
-[9.449219703674316, 2.324291706085205, "[TT] Count of the Blue Jets = 4,720"]
-[4.258280277252197, 4.311715602874756, "[TT] SAR Events of the Cospas-Sarsat System = 10385"]
-[10.202019691467285, 5.767146587371826, "[TT] Detector Temperature of the OCO-3 = -120\u00b0 C (-184\u00b0 F)"]
-[4.82275915145874, 0.06802549213171005, "[TT] End of Life Date of the Resurs-DK1 = 01 Mar 2016"]
-[5.792996406555176, 0.5190019607543945, "[TT] Date of the North Pole Observations = 23 and 24 April 1994"]
-[5.493802070617676, 5.138692378997803, "[TT] Tracking Software of the Rotator controller = Gpredict"]
-[8.694515228271484, 8.414362907409668, "[TT] Velocity Resolution of the Spectrometer = ~100 km/s"]
-[7.936746120452881, 7.879159927368164, "[FF] Components of the Wolf-Rayet bubble = Blue, Yellow-Green, Red"]
-[11.706986427307129, 6.668927192687988, "[TT] Energy Range of the High-energy Electron Detector = 0.4 - 4 MeV"]
-[5.188555717468262, 8.40976333618164, "[TT] Bandwidth of the Channel = 370 MHz"]
-[8.503218650817871, 1.3707623481750488, "[FF] Purpose of the Aquarius = Soil moisture and ocean salinity"]
-[7.156641960144043, 1.528059959411621, "[FF] Deployment Sequence of the Dobson Space Telescope = Launch configuration, solar array deployment, telescope deployment, in-orbit collimation"]
-[7.4615654945373535, 6.5596771240234375, "[TT] Manufacturing Process of the Radiation-resistance devices = SOI (silicon on Insulator)"]
-[5.473121166229248, 1.1337279081344604, "[TT] Regular Technology Demonstration Mode Start Date of the ICIR = June 16, 2017"]
-[4.91180944442749, 0.42824408411979675, "[TT] Installation Date of the MDA MOC = May 2006"]
-[5.131380558013916, 3.3078010082244873, "[TT] Manufacturer of the SBSS = Boeing Space and Intelligence Systems"]
-[4.652523517608643, 0.7194077968597412, "[FF] Additional Contract Award Date of the SARah project = 7 August 2019"]
-[4.735703468322754, 7.354833602905273, "[TT] X-band Data Rate of the RF communications = 26 kbit/s"]
-[7.1276445388793945, 5.866028308868408, "[TT] Stability of the Deep Space Atomic Clock = Time deviation of less than four nanoseconds after more than 20 days of operation"]
-[7.872994422912598, 8.133196830749512, "[TT] Band 3 of the R3 Sensor = CA"]
-[14.293632507324219, 3.0584046840667725, "[TT] Mass of the BRITE-Austria = 6.5 kg"]
-[4.639599323272705, 1.3334835767745972, "[FF] Publication Date of the Superconducting Submillimeter-Wave Limb-Emission Sounder = Dec. 7, 2010"]
-[3.0150699615478516, 1.998969316482544, "[TT] Integration Completion Date of the Copernicus Sentinel-2C = July 29, 2021"]
-[10.118033409118652, -2.709336280822754, "[FF] Technology of the Sentinel 2 MMFU = NAND-Flash Storage"]
-[10.349647521972656, 6.697221755981445, "[TT] Configuration of the Three Mirrors = Corner cube"]
-[8.200540542602539, 8.819234848022461, "[TT] Spectral Sampling Distance of the UV-2 = 0.15 nm"]
-[4.562802791595459, 0.16220663487911224, "[TT] Kick-off Meeting Date of the SMILE = Sept. 3-4, 2015"]
-[13.605814933776855, 1.7488696575164795, "[TT] Cargo Weight of the Dragon = More than 5,700 pounds"]
-[6.897100925445557, 8.984890937805176, "[TT] Bandwidth of the POLDER-2 = 20 nm"]
-[7.673823356628418, 4.201260089874268, "[FF] Purpose of the AMS-01 = Test particle physics technology in LEO"]
-[7.058660507202148, 8.352226257324219, "[TT] Estimated SNR of the Band 6 = 427.81 \u00b1 136.32"]
-[4.905554294586182, 3.661235809326172, "[TT] Developer of the ODTML = Praxis Inc."]
-[5.463627338409424, 5.087314128875732, "[TT] Bus Type of the OBCom = Wireless CAN (Controller Area Network)"]
-[7.672451496124268, 9.435925483703613, "[TT] Center Wavelength of the Band 3 = 14.06 \u00b5m (711 cm -1)"]
-[5.795959949493408, 3.3793373107910156, "[FF] Economic Impact of the Silkworm = More than 30 billion dollars income for silkworm breeders, commercial as well as industry"]
-[5.7380475997924805, 6.195867538452148, "[FF] Capacity of the Tape Recorder = Stored pictures of the entire northern hemisphere each day"]
-[7.073747634887695, 1.283881664276123, "[TT] Observation Date of the Spitzer Space Telescope = 2019 and 2020"]
-[3.6741578578948975, 2.6139214038848877, "[FF] Signal Speed of the Iridium NEXT = Faster"]
-[8.2003755569458, 7.017436981201172, "[TT] TDI (Time Delay Integration) of the Imager = 6 selectable levels from 8 to 64 in Pan and MS"]
-[8.347208023071289, 7.275835037231445, "[TT] Image Type of the Supervision Cameras = 8 bit"]
-[5.369525909423828, 6.947007656097412, "[TT] Downlink Data Rate of the IXPE = 2.0 Mbit/s"]
-[4.35143518447876, 7.455652236938477, "[TT] Uplink Modulation of the S-band transponder = NRZ (Non-Return to Zero) bi-phase modulated synchronously on a 16 kHz subcarrier"]
-[6.1537766456604, 0.9998036623001099, "[TT] Gamma-Ray Measurement of the GRB 031203 = About one thousand times less than expected"]
-[5.946594715118408, -0.491446316242218, "[TT] Mission Duration of the MATS = Two years"]
-[5.30687952041626, 1.5142302513122559, "[FF] Observation Date of the ALOS-2/Daichi-2 = August 19, 2015"]
-[13.291441917419434, 3.453559160232544, "[TT] Sub-payload Volume of the ArgUS = 3U up to Single payload maximum volume"]
-[6.977694988250732, 6.1681437492370605, "[TT] Number of Instruments of the MetOp = 11"]
-[7.599217891693115, 2.1516432762145996, "[TT] Area Coverage of the EROS-B = 450 km"]
-[5.113590240478516, 1.431894302368164, "[FF] Known For of the Carrara = World-famous marble"]
-[6.752439498901367, 1.7980902194976807, "[FF] URL of the MEOSAR = http://www.navnin.nl/NIN/Downloads/SARl.pdf"]
-[10.335585594177246, 2.3701906204223633, "[FF] Energy Range of the Satellite = Hard X-ray"]
-[7.547554016113281, -0.8924490213394165, "[TT] Propellant Onboard of the ICESat-2 = 7 years"]
-[7.880305767059326, 4.097535133361816, "[FF] Component of the ABEX = Thermal component"]
-[10.00527572631836, -1.5091158151626587, "[TT] Orbit Inclination of the AFSPC-11 = 0\u00ba"]
-[5.708494663238525, 7.070213794708252, "[TT] Data Rate of the MUX = 68 Mbit/s"]
-[6.850970268249512, 2.2643580436706543, "[FF] Conference Presentation Date of the Radio Aurora Explorer = Aug. 8-11, 2011"]
-[14.695674896240234, 6.673098564147949, "[TT] Configuration of the Lithium-ion batteries = 3 parallel cells"]
-[11.750166893005371, 7.520125389099121, "[FF] Precession Cycle of the Megha-Tropiques = Clearly seen"]
-[4.730175971984863, 7.379364490509033, "[TT] Data Rate of the X-band transmitter = Up to 384Mbit/s"]
-[10.336188316345215, 4.319769859313965, "[TT] Attitude Control Subsystem of the TanSat = 4 reaction wheels, 4 torque-rods, 4 hydrazine thrusters"]
-[7.020269870758057, 5.2352986335754395, "[FF] Function of the Watchdogs = Mitigate the risk of single-event upsets by resetting parameters, subsystems, or the entire system in the case of anomalous behaviour"]
-[7.1734724044799805, 5.729313373565674, "[FF] Operation of the Optical Encoder = Tailored to the operation in a LCT under harsh environmental conditions outside the spacecraft in GEO"]
-[14.209208488464355, 3.2362918853759766, "[TT] Mass of the COCTS = 50 kg"]
-[8.250648498535156, 5.543056488037109, "[FF] Pointing Accuracy of the LRI = Not accurate enough"]
-[3.595651865005493, -0.9919395446777344, "[TT] Science Mission Orbit of the LRO = Quasi-circular orbit (50 \u00b1 15km)"]
-[13.774030685424805, 3.01810359954834, "[TT] Payload Mass of the Spacecraft = 33.3 kg"]
-[4.453444480895996, 0.6155551671981812, "[TT] Operational Period of the COSPAS-1 = Until December 1987"]
-[13.203495025634766, 7.762343883514404, "[TT] Energy of the X-band = 42 \u00b5eV"]
-[7.5062336921691895, 4.123584747314453, "[FF] Purpose of the Additional Payloads = Performing a radiation census of this segment of space"]
-[6.208957672119141, 1.3735910654067993, "[FF] Date of the Space-based Automatic Identification System Experiment (SPAISE) = June 5-12, 2011"]
-[10.88034725189209, 1.1361198425292969, "[FF] Weight of the V404 Cygni = 3 million Earths"]
-[10.803855895996094, 2.8205268383026123, "[FF] Complex Investigation of the Chibis-M Microsatellite = Unknown"]
-[4.3491644859313965, 2.6477129459381104, "[FF] Location of the Coastal Eddies = Off Point Arena, California"]
-[11.209172248840332, 5.6971845626831055, "[FF] Composition of the Laminate Material = Two 14.5 \u00b5m aluminum layers sandwich 16 \u00b5m of Mylar and adhesive"]
-[9.186056137084961, 5.569565296173096, "[TT] Pointing Repeatability of the ASTERIA = 1 milliarcsecond rms"]
-[11.614723205566406, 3.3706676959991455, "[FF] Presentation Date of the Miniature Ion Propulsion System = Oct. 10-13, 2012"]
-[9.127379417419434, 4.674881935119629, "[TT] Attitude Control of the GCOM-W1 = 4 reaction wheels in response to the signal from IRU (Inertial Reference Unit) calibrated by Star Trackers and GPS receivers"]
-[6.9607110023498535, 4.637962818145752, "[FF] Parameter of the HSPD = Value"]
-[5.419862747192383, 6.247735977172852, "[TT] SRAM Capacity of the RAD750 SBC = 36 MB"]
-[10.03657054901123, -1.6006834506988525, "[TT] Inclination of the Tandem-L = 98.4\u00ba"]
-[6.926705360412598, -0.47098103165626526, "[TT] Revolutions per Day of the Satellite = 14+3/10"]
-[10.425360679626465, 5.880710601806641, "[TT] Operating Temperature of the Antenna = 0~70\u00baC -10~70\u00baC"]
-[10.394168853759766, 2.116093397140503, "[FF] X-ray Spectrum of the SXT = Provides both the continuum spectrum which is indicative of the temperature of the plasma and the lines of the elements which are expected to be formed during the final evolution before the supernova explosion"]
-[8.401217460632324, 6.905611038208008, "[TT] Instrument Type of the GeoEye-1 = High resolution optical imagers"]
-[8.449755668640137, 6.908339500427246, "[TT] Scanning Technique of the WV-3 Imager = Pushbroom"]
-[7.338134765625, 6.249948024749756, "[FF] Unknown of the BepiColombo Laser Altimeter = Unknown"]
-[12.088274955749512, 6.315960884094238, "[TT] Electron+Positron Flux Measurement of the AMS-02 = Up to 1 TeV"]
-[16.475738525390625, 3.6141583919525146, "[TT] Ownership Stake in OneWeb of the Eutelsat = 17.6%"]
-[3.4167022705078125, 5.012320518493652, "[TT] SAR Bands of the SAR Satellite = X-band and L-band"]
-[13.488459587097168, 5.935258388519287, "[TT] Voltage of the High-voltage solar array = 350 V"]
-[14.632464408874512, 6.759096145629883, "[TT] Cd-Ni Battery Capacity of the EPS = 55 Ah"]
-[7.996652603149414, 8.873406410217285, "[FF] Measurement Types of the MSX/UVISI = Refraction and Extinction"]
-[14.112512588500977, 3.348048686981201, "[FF] Mass Resolution of the GEMS = Enables mass resolution of the particles"]
-[11.453978538513184, 5.232789039611816, "[TT] Area of the Effective Collecting Area = 767.93 cm2"]
-[5.446133136749268, 0.7133950591087341, "[TT] Arrival Date of the CALET = August 19, 2015"]
-[6.90801477432251, 1.8329955339431763, "[FF] URL of the Solar Dynamics Observatory = http://science.nasa.gov/science-news/science-at-nasa/2010/05feb_sdo/"]
-[6.286892414093018, -0.40173599123954773, "[TT] Orbit Duration of the Ikonos-2 = 10 years"]
-[5.244515419006348, 3.801070213317871, "[TT] Architecture of the SSTI = Lagrange architecture"]
-[12.712387084960938, 1.934078335762024, "[FF] Expected O3 Recovery of the SAGE-III on ISS = About half of the amount lost from pre-1980 levels by the 2020s"]
-[8.404974937438965, 2.7774739265441895, "[FF] Cloud Brightness Trend of the AIM = Getting brighter"]
-[12.039814949035645, 4.4785847663879395, "[TT] Size of the Spacecraft = 2.6 m x 1.8 m x 2.8 m"]
-[8.539704322814941, 6.372552871704102, "[TT] Type of the AMSU-A = Cross-track, line-scanning instrument (whiskbroom type)"]
-[7.666530609130859, 6.404430866241455, "[TT] IR Stars Observation Frequency of the ABI = On average at least every 300 s"]
-[5.034931659698486, 1.2020831108093262, "[FF] Launch Date of the GIOVE-B = October 13, 2008"]
-[6.477555274963379, 5.130590438842773, "[TT] Long-Term Tracking of the LAGEOS = Yes"]
-[7.959690093994141, 8.559969902038574, "[TT] Spectral Range of the TSI = 0.2-35 \u03bcm"]
-[13.347363471984863, 7.258031845092773, "[TT] Electronics Package Power of the FlaPS = 1.5 W"]
-[6.3429274559021, 3.488790988922119, "[FF] Assembly of the SIMPL-Microsat = Manual crew member assembly in microgravity of eight subassemblies utilizing minimal tools and simple mechanical and electrical connections"]
-[5.156271934509277, 0.44924047589302063, "[TT] Issued Date of the Hazards Outlook = December 7"]
-[5.387715816497803, 1.6973541975021362, "[TT] Mission Type of the ALOS-2 = Earth observation and disaster monitoring"]
-[10.93019962310791, 7.565952301025391, "[TT] Swath Width of the MWIR = 182 km"]
-[8.363739013671875, 6.095157623291016, "[TT] Accuracy at 20 keV of the XGRE = 30%"]
-[9.738262176513672, -0.6674595475196838, "[TT] Orbit Altitude of the HORYU-2 = ~680 km"]
-[5.818013668060303, 3.625922679901123, "[TT] Availability of the PARASOL = Near 90%"]
-[10.801899909973145, 7.29600191116333, "[TT] Length of the Nix = 42 km"]
-[5.544944763183594, 2.893864631652832, "[TT] Host of the OSIRISv3 = ISS"]
-[6.596989631652832, 1.8263229131698608, "[FF] URL of the TOPCAT = http://www.bath.ac.uk/elec-eng/invert/topcat.html"]
-[8.19685173034668, -1.1270145177841187, "[FF] Bathymetric Mapping Technology of the ICESat-2 = Machine Learning-based"]
-[4.80640983581543, 7.327971935272217, "[TT] Downlink Data Rate of the RF Communications = 9.6 or 38.4 kbit/s"]
-[9.972633361816406, -0.4836840331554413, "[TT] Altitude of the RADARSAT-2 = 798km"]
-[6.8523125648498535, 3.372105836868286, "[FF] Interface of the Kaber = JEM airlock slide table and the ISS SPDM"]
-[5.612491607666016, 7.065347194671631, "[TT] Power Consumption of the CoReCi = 75 W during simultaneous data record / data compression / data replay"]
-[7.773076057434082, 7.257104396820068, "[TT] Frame Rate of the Detector assembly = > 500 Hz"]
-[3.3978421688079834, 1.6749860048294067, "[FF] Establishment Date of the Sentinel Asia = May 2005"]
-[9.75609302520752, 7.167721271514893, "[TT] Ground Resolution of the MWNIR = 100 km - 18 km"]
-[4.280930995941162, 7.325817108154297, "[TT] S/C Body Pointing Capability of the Spectral bands = \u00b145\u00ba in the roll and pitch axis"]
-[10.187091827392578, 8.09623908996582, "[TT] Objective Aperture Diameter of the VSSC = 0.25 m"]
-[9.126325607299805, -1.1876535415649414, "[TT] Orbit Location of the EDRS-C = 9\u00baE"]
-[7.9392876625061035, 3.954240560531616, "[FF] Purpose of the Mouse Cells and Fruit Flies = Obtain gene expression profiles and identify sensitive biological molecules as space radiation markers"]
-[5.154435634613037, 2.372227668762207, "[FF] Mission Type of the Deimos-1 = Fully Commercial EO Mission"]
-[10.771768569946289, -1.062972068786621, "[FF] Aero Attitude Control Modes of the SLATS = Aero-braking mode, Aero-through mode"]
-[10.146588325500488, 2.037900686264038, "[FF] Data Source of the Chandra X-ray Observatory = Astronomers obtained this result using data from NASA's Chandra X-ray Observatory"]
-[11.731610298156738, 6.637613296508789, "[TT] Energy Range of the Genesis Electron Monitor = 1 eV to 1400 eV"]
-[11.084235191345215, 4.6386308670043945, "[FF] Data Acquisition of the Ma_MISS = Exploits the movement of the drill to acquire data from all around the borehole"]
-[9.152573585510254, 7.833406448364258, "[TT] Rotation per Image of the M-CAM 1 = 3\u00ba"]
-[11.408446311950684, 4.352259159088135, "[TT] Size of the CUAVA-1 = 3U"]
-[10.901865005493164, 2.081724166870117, "[FF] Manufacturer of the XMM-Newton telescope = European Space Agency"]
-[10.968295097351074, 7.332019805908203, "[TT] Sample Width of the BIROS = 42.4 m"]
-[6.982952117919922, 4.764340877532959, "[FF] Based on of the Navigation Function = Extended Kalman Filtering (EKF) theory"]
-[9.666293144226074, 0.12348657101392746, "[TT] Testing Start Date of the Parachute System = 2016"]
-[8.256467819213867, 6.519038200378418, "[FF] Spectrometer of the The Rossi Explorer = Device used to uncover properties of the light source, such as speed and rapid variations in the order of milliseconds"]
-[8.058024406433105, 8.094228744506836, "[TT] SIF Emission Data Micro-Windows of the IAPCAS/SIF = 757 nm and 771 nm"]
-[5.700512409210205, 5.9585490226745605, "[TT] Processing Power of the QC40 = 120 Megaflop"]
-[9.808396339416504, -0.45652931928634644, "[TT] Orbit Altitude of the NEMO-HD = 600 km"]
-[8.823019027709961, 3.586470365524292, "[FF] Instrument Types of the Voyager 1 = Cosmic ray instrument, one plasma instrument, magnetometer, low-energy charged particle instrument"]
-[8.480002403259277, 2.254645347595215, "[FF] Mode of the WINDS = Bent-pipe and Regenerative"]
-[5.056945323944092, 3.3157877922058105, "[TT] Manufacturer of the Minotaur-1 = Orbital Sciences Corporation"]
-[6.041688919067383, 1.0078147649765015, "[TT] Image Acquisition Date of the AGRI = 1 February 2019"]
-[8.485917091369629, 1.3650784492492676, "[FF] Salinity Measurement Mission of the Aquarius = Ongoing"]
-[9.298521041870117, -1.0461405515670776, "[FF] Formation Configuration Parameters of the SJ-9A and SJ-9B = Eccentricity difference, phase difference, ascending node difference, argument of perigee difference"]
-[8.674162864685059, 3.1483967304229736, "[FF] Formation of the Ionosphere = Photodissociation of thermospheric air by solar extreme ultraviolet radiation"]
-[6.508828163146973, 3.3704874515533447, "[FF] Search and rescue capabilities of the Weather satellites = Aid"]
-[9.26789379119873, 8.6506986618042, "[TT] Entrance Slit of the UVS Instrument = 0.31 x 3.2 mm"]
-[7.358932018280029, 0.2640349566936493, "[TT] Instrument Install/Assembly Completion Date of the OSIRIS-REx = October 22, 2015"]
-[2.9269907474517822, 1.9700508117675781, "[TT] Image Capture Date of the Copernicus Sentinel-2 = 25 January"]
-[11.215828895568848, 1.0464067459106445, "[FF] Demonstration of the LISA Pathfinder = Precision laser metrology"]
-[7.045651912689209, 4.097254753112793, "[FF] Unknown of the SCIAMACHY = Unknown"]
-[10.185608863830566, -2.796043634414673, "[TT] Accessible unit (erase) of the SLC NAND-FMM = 16 MByte"]
-[5.3754167556762695, 7.179656982421875, "[TT] Data Rate of the Ka-ISL forward service = 1 Mbit/s"]
-[7.736660003662109, 1.4162640571594238, "[FF] Purpose of the ROSE-L = Better understand climate change and simulate its impact on humankind"]
-[4.497838497161865, 5.450181484222412, "[FF] Product Assurance/Quality Assurance Standards of the GomX-4 = ESA on nanosatellite missions"]
-[5.882727146148682, -0.33635857701301575, "[TT] Safety Period of the RVX Profile = At least 5 days"]
-[11.043635368347168, 5.802123546600342, "[TT] Cu Foil Thickness of the RADFET Dosimeters = 50 \u00b5m"]
-[8.132722854614258, -1.0509651899337769, "[TT] Laser-Illuminated Area Movement Time of the Spectral Bands = Corresponding to the desired mapping resolution of water ice (10 km or less)"]
-[8.035943984985352, 5.554335594177246, "[FF] Components of the Camera Unit = Filters, spectral calibration sources (PTFE sun diffusers)"]
-[4.305211067199707, 2.508841037750244, "[TT] Launch Provider of the Delfi-n3Xt = ISC Kosmotras of Moscow"]
-[2.294677257537842, 2.7721033096313477, "[TT] Co-PI of the EPI-Lo = Bill Matthaeus"]
-[2.474919557571411, 2.8295743465423584, "[TT] PI of the SOLSPC = G. O. Thuillier"]
-[5.898213863372803, 1.798546314239502, "[TT] Test Flight Date of the Orion = Fall 2014"]
-[5.3060784339904785, 1.2480067014694214, "[FF] Conference Date of the SMEX-LITE = Sept. 16-19, 1996"]
-[6.461323261260986, 7.628438472747803, "[TT] Data quantization of the ALOS/PRISM = 8 bit"]
-[8.985677719116211, 4.759174346923828, "[TT] Quantity of the LEP Sensor Units = Three"]
-[10.984994888305664, 1.3346368074417114, "[FF] Mission Objectives of the LISA = Study the formation and evolution of compact binary stars in the Milky Way galaxy; Trace the origin, growth and merger history of massive black holes across cosmic ages; Probe the dynamics of dense nuclear clusters using extreme mass-ratio inspirals (EMRIs); Understand the astrophysics of stellar-origin black holes; Explore the fundamental nature of gravity and black holes; Probe the rate of expansion of the Universe; Understand stochastic gravitational wave backgrounds and their implications for the early Universe and TeV-scale particle physics; Search for gravitational wave bursts and unforeseen sources"]
-[4.987648963928223, 0.9886614084243774, "[TT] Deployment Status of the MicroMAS-2 = Working splendidly"]
-[9.071609497070312, 5.496539115905762, "[TT] Steering Capability of the LISS-4 = \u00b126\u00ba in the cross-track direction"]
-[5.320250511169434, 1.556746244430542, "[FF] Check-out Result Date of the ALOS Ground Data System = July 31-Aug. 4, 2006"]
-[10.078730583190918, -1.5193122625350952, "[TT] Orbit Inclination of the KSF1 satellites = 97.6\u00ba"]
-[8.583663940429688, 7.261867523193359, "[TT] Transmission Failure of the HD-TV Camera = Cases with obstacles such as buildings, pedestrian overpasses and utility poles"]
-[8.33756160736084, -0.8125338554382324, "[TT] Resolution of winter and summer ice\u2010sheet elevation change of the ATLAS = 10 cm at 25 km x 25 km spatial scales"]
-[5.100668907165527, 0.6401639580726624, "[TT] Health Check Date of the SEIS = July 19"]
-[5.6286540031433105, 3.7423317432403564, "[TT] Total Impulse of the SkySat-7 = 317 Ns"]
-[5.04123592376709, 6.123198986053467, "[TT] Expected Number of AIS Signals of the ZACUBE-2 = 6000"]
-[8.24721622467041, -0.37252599000930786, "[FF] Water Content of the Micro Cold Traps = Approximately 10 to 20% of the permanent cold-trap area"]
-[8.817466735839844, 5.676676273345947, "[TT] Measured Position Accuracy of the DIOGENE = ~ 5 m (3D, 1\u03c3)"]
-[6.319116115570068, 4.097638130187988, "[FF] Ground Segment Operation of the Helios-2 = Image acquisition, priority discussion, transmission of plans, satellite control, image processing"]
-[14.081509590148926, 3.1152679920196533, "[TT] Servicer Mass of the ELSA-d = ~175 kg"]
-[6.959124565124512, 0.1329343169927597, "[TT] Mission Duration of the SeaSat = 110 days"]
-[9.54152774810791, 0.7406694889068604, "[TT] Mission Position of the IMAP = One million miles (1.5 million kilometers) away from Earth towards the Sun"]
-[2.0327305793762207, -0.32186728715896606, "[FF] Purpose of the DSX = Operate spacecraft in the harsh radiation environment of the Van Allen radiation belts"]
-[5.255423069000244, 4.794496059417725, "[TT] BCRs Configuration of the DubaiSat-2 = Three BCRs in a hot redundancy configuration"]
-[11.95130443572998, 3.5386478900909424, "[TT] Mass Flow Rate of the IES = 10.5 cm3/s"]
-[6.17176628112793, 2.2794065475463867, "[TT] Principal Investigator of the LOLA = David E. Smith"]
-[5.70121955871582, 3.697885513305664, "[TT] Number of Maneuvers of the SkySat-6 = 5"]
-[7.089786529541016, 2.988515853881836, "[FF] Data Type of the Sloan Digital Sky Survey = Optical data"]
-[8.818530082702637, 0.0424068309366703, "[TT] Latitude Range of the LF = 10\u00ba of latitude from the lunar South Pole"]
-[6.930334568023682, 6.329586029052734, "[TT] Number of 'Original Design' Arrays of the MSA = Three"]
-[5.545130729675293, -1.8606693744659424, "[TT] Participating Companies of the KOMPSAT-5 = Korea Aerospace Industries, Korean Air, Hanwha, Doowon Heavy Industries, and SI (Satrec Initiative)"]
-[5.994836330413818, -0.4194846749305725, "[TT] Mission Duration of the LLITED = One year"]
-[6.59363317489624, 0.8226569294929504, "[TT] Side-Looking Capability of the FormoSat-2 = \u00b145\u00ba"]
-[6.2338385581970215, 7.989151477813721, "[TT] Channels of the Communication System = Two"]
-[5.565132141113281, 5.452920436859131, "[FF] Interface of the PLC = DC Power and a 1553 interface with the BMU (Bus Management Unit) of the spacecraft"]
-[8.33932113647461, 3.9207541942596436, "[FF] Lunar Calibration Method of the SeaWiFS = S/C maneuver to view the moon during the nighttime portion of an orbit"]
-[8.140247344970703, 5.642749786376953, "[TT] Microwave Ranging Instruments Precision of the GRACE-FO = Better than one micron"]
-[6.724329471588135, 3.903233051300049, "[TT] Location of the Robotic Arm = On board the ISS"]
-[6.515689373016357, 8.683064460754395, "[TT] Minimum Detectable Polarization of the HXCP = 6.2%"]
-[5.742845058441162, 6.890853404998779, "[TT] Data Amount of the Experiment Data = 130 Mbit"]
-[4.254941463470459, 3.047250986099243, "[FF] Observation Modes of the AISSat-1 = Autonomous, Svalbard ground station contact"]
-[5.249743461608887, 3.5030221939086914, "[TT] Platform Shape of the Spacelab Pallet = Open, U-shaped"]
-[9.833296775817871, -0.32196980714797974, "[TT] Altitude of the IVM = Above 250 km"]
-[8.53918170928955, 9.448028564453125, "[TT] Responsivity Requirement of the Responsivity Measurement = >0.47 A/W"]
-[8.303128242492676, 0.060206089168787, "[TT] Average Temperature Increase of the Earth = More than 2 degrees Fahrenheit (1.2 degrees Celsius) since the late 19th century"]
-[10.913691520690918, 3.9730308055877686, "[TT] Deorbit System of the Spacecraft = Sail"]
-[10.624308586120605, 7.337360858917236, "[TT] View Swath of the TIR Instrument = 68 degrees-wide nadir cross-track swath"]
-[5.636134624481201, 7.683140277862549, "[TT] G/T of the VSAT (Very Small Aperture Terminal) = >18.0 dB/K"]
-[6.541697025299072, 6.890252590179443, "[TT] Duty Cycle of the T/R module = ~7-8%"]
-[8.745529174804688, 5.0798516273498535, "[TT] Mode of the TanSat = Nadir"]
-[10.355395317077637, 4.047377586364746, "[TT] Length of the Gravity Gradient Boom = 1.4 m"]
-[11.460640907287598, 5.7231340408325195, "[TT] Design of the UniSat-4 = Four aluminum sandwich \u201ctrays\u201d assembled and kept together by four aluminum columns"]
-[8.898548126220703, -0.5594211220741272, "[TT] Orbit Type of the P35 series = Sun-synchronous"]
-[7.9621171951293945, 5.374990940093994, "[FF] Range of the FLLS = \u00b5m"]
-[8.329397201538086, 1.3155187368392944, "[TT] Spatial Resolution (km) of the Precipitation over water = 25"]
-[11.210002899169922, 4.065543174743652, "[TT] Volume Occupation of the Solar Sail Subsystem = Lower 2/3 of the spacecraft"]
-[3.676908493041992, 4.482567310333252, "[FF] Application of the RISAT-2 = Radar satellite imagery for assessing cyclone damages"]
-[11.46033763885498, 3.4882824420928955, "[FF] Propulsion System of the CanX-2 = Custom cold-gas propulsion system"]
-[8.608325958251953, 1.8958195447921753, "[TT] Pointing Accuracies of the OceanSat-1 = \u00b10.15\u00ba in pitch/roll and \u00b10.20\u00ba in yaw"]
-[7.875619411468506, 2.831035852432251, "[FF] Citation of the SOLSPEC = E. Hilsenrath, in Optical Remote Sensing of the Atmosphere, 1990 Technical Digest Series of the Optical Society of America, Vol. 4, pp. 409-412"]
-[10.912663459777832, 7.541985511779785, "[TT] Swath Width of the MWR = 380 km"]
-[9.655454635620117, 8.20350170135498, "[TT] Field of View of the Focal Plane = 0.4\u00ba"]
-[8.75832462310791, 5.684876441955566, "[TT] Maximum Pointing Error of the Tracking Accuracy = 0.064\u00b0"]
-[3.4101264476776123, 5.323559284210205, "[TT] Center Frequency of the CSG-SAR = 9.6 GHz"]
-[5.106420993804932, 8.406257629394531, "[TT] Bandwidth/Passband of the 1 = 400 MHz"]
-[7.172982215881348, 4.69951057434082, "[FF] Unknown of the Power Supply System = Unknown"]
-[9.502141952514648, -0.5064026713371277, "[TT] Orbit Altitude of the Tiangong = About 400 kilometers"]
-[13.25213623046875, 5.280463218688965, "[TT] Total Solar Array Size of the Resurs-DK1 = 36 m2"]
-[3.7740116119384766, -1.1638729572296143, "[TT] Position of the Spektr-RG (SRG) = Lagrange point L2 of the Sun-Earth system"]
-[6.1717529296875, -0.456041544675827, "[TT] Orbit Decay Time of the MicroMAS-1 = Within the required 25 year time period"]
-[9.528864860534668, 5.9608659744262695, "[TT] Cross-Track of the HORUS = 1.6\u00b0"]
-[6.9635210037231445, -0.728557288646698, "[TT] Orbit Period of the HIP 67522 b = About seven days"]
-[4.871732711791992, 0.4681987166404724, "[TT] Retrieval Date of the CRISTA-SPAS-2 = Aug. 16, 1997"]
-[6.335471153259277, 5.132858753204346, "[FF] Purpose of the OBDH = Load the software experiment"]
-[5.87760066986084, 1.201696753501892, "[FF] Conference Date of the EarthCARE = Dec. 8, 2011"]
-[4.7492499351501465, 2.2287724018096924, "[TT] Technology Presentation Date of the Quantum = 21 November 2019"]
-[13.229511260986328, 5.542325973510742, "[FF] Solar Environment of the Electric Field Antennas = More severe than all previous experience"]
-[11.449944496154785, 3.3809406757354736, "[FF] Thrusters of the Satellite = Micro-newton (\u00b5N) cold gas thrusters"]
-[3.9823412895202637, 6.547284126281738, "[TT] Accuracy of the Onboard Antenna = 5\u00ba"]
-[13.665911674499512, 5.794773578643799, "[TT] Solar Panel Power Output of the AprizeSat = 7.7 W"]
-[9.657739639282227, 4.1803998947143555, "[TT] Uncertainty of the Magnetometer = \u00b114 nT"]
-[5.3173112869262695, 8.105411529541016, "[TT] Frequency Range of the IMM = 10kHz \u2013 1MHz"]
-[4.341490745544434, 1.1854164600372314, "[TT] Repeat Cycle of the SEOSAT-Ingenio = 38 days"]
-[4.293794631958008, 3.0326170921325684, "[TT] Testing Location of the Galileo Satellites 13 and 14 = Oberpfaffenhofen, Germany"]
-[5.157211780548096, 1.1045781373977661, "[FF] Conference Presentation Date of the SEXTANT = 5-9 Jan. 2015"]
-[4.673702239990234, 1.185671091079712, "[FF] In-Orbit Performance of the ALSAT-2B = 2 years"]
-[4.985285758972168, 1.7455050945281982, "[TT] Operation Status of the Ikonos-2 = Nominal"]
-[5.188868999481201, -1.2055753469467163, "[FF] Launch Date of the Kondor-E = June 27, 2013"]
-[5.745841979980469, -0.8904760479927063, "[TT] Design Lifetime of the FLP = Two years"]
-[6.007989406585693, 2.713808536529541, "[TT] Affiliation of the JEM-X = DSRI (Danish Space Research Institute), Copenhagen, Denmark"]
-[7.340660095214844, 8.702116966247559, "[FF] ROIC Components of the VIS channel = Capacitive trans-impedance amplifiers, 8:1 multiplexer, output buffer"]
-[4.819892406463623, 7.151600360870361, "[TT] Nominal Rate of the S-band Downlink = 40 kbit/s"]
-[4.895010948181152, 0.665439248085022, "[TT] Launch Date of the DMC-3 = 10 Jul 2015"]
-[9.923529624938965, 6.6803669929504395, "[TT] Full Width at Half Maximum (FWHM) of the Dosimeter Suite = 38\u00b0 and 32\u00b0"]
-[7.833317279815674, 3.5680184364318848, "[FF] Components of the ETB = MDIM (Meteoroid and Debris Impact Monitor) and the Meteoroid Impact Sensor of BMDO"]
-[8.315343856811523, -0.49562501907348633, "[TT] Minimum Extent of the Arctic sea ice = 3.74 million km2 (1.44 million square miles)"]
-[6.219674110412598, 0.07764242589473724, "[TT] Observation Duration of the IBEX = Six months"]
-[4.735260963439941, 1.3413163423538208, "[TT] First Signal Received of the Robusta = Feb. 16, 2012"]
-[8.144314765930176, 1.7941497564315796, "[FF] Drag-Free Attitude and Orbit Control System Performance of the GOCE = Unknown"]
-[4.548300743103027, 6.109542369842529, "[TT] Beacon Frequency of the OSSI-1 = 145 Mhz"]
-[4.127854824066162, 6.30734920501709, "[FF] Enhancement of the Navigation Antenna = More powerful"]
-[11.641996383666992, 3.397599935531616, "[FF] Development Date of the Miniature Ion Propulsion System = Unknown"]
-[10.492240905761719, 4.024105072021484, "[FF] Deployment of the Origami booms = Straight-line"]
-[5.818551063537598, 3.1746914386749268, "[FF] Number of Satellites of the WorldView Legion = Not announced"]
-[7.737390518188477, 9.142032623291016, "[TT] Wavelength Range of the Band No 4 = 3.50 \u00b1 0.50 - 4.10 \u00b1 0.50 \u00b5m"]
-[5.926325798034668, -0.12717226147651672, "[FF] Software Shutdowns of the IPA = Twice in 20 months of operation"]
-[8.740447998046875, 7.848100662231445, "[TT] IR Sample Size of the INSAT-3D Imager = 64 \u00b5rad E/W"]
-[5.850988864898682, -0.49286749958992004, "[TT] Time to Reach Intelsat 901 of the MEV-1 = Approximately four months"]
-[9.640823364257812, 4.0845046043396, "[TT] Dynamic Range of the Magnetometer = 160 dB (ELF/VLF range), 130 dB (LF/MF range)"]
-[5.077513217926025, 0.021069372072815895, "[FF] Delivery Date of the CUTE = Mid-September 2021"]
-[7.651391506195068, 5.5200886726379395, "[FF] Components of the CLS telescope unit = 5 lenses, 2 filters, an alignment cube and a divergent lens"]
-[7.735413074493408, 1.9567484855651855, "[FF] Data Provided of the EXPORTS = Role of phytoplankton and plankton in the biological pump, export of carbon"]
-[10.174761772155762, 5.806577205657959, "[TT] Temperature Corrections of the Detector = Small adjustments over the course of an observation"]
-[9.97921085357666, 2.845747947692871, "[TT] Airlock Cycle Dates of the NanoRacks CubeSat Deployer Missions = May 16-17, 2017"]
-[5.4748077392578125, 6.457211971282959, "[TT] Data Storage Capacity of the ResourceSat-2 = 400 GB"]
-[14.72812271118164, 6.6098737716674805, "[TT] Li-ion Battery Capacity of the GNB = 5.3 Ah"]
-[4.770127296447754, -1.8707308769226074, "[TT] Rocket Type of the Chang'e-5 = Long March 5"]
-[10.683942794799805, 4.062679767608643, "[FF] Attitude Pointing Requirements of the CanX-4&5 = Placed on the attitude determination and control system for accurate thruster pointing"]
-[7.0860514640808105, 0.2825884521007538, "[FF] Age of the Site Kingfisher = Relatively young"]
-[12.091594696044922, -0.3118881583213806, "[TT] Southern Hemisphere Mapping of the TESS = Second year"]
-[9.036698341369629, 2.5995607376098633, "[FF] Purpose of the IBEX = Images the outer boundary of the heliosphere"]
-[8.322932243347168, 0.34166035056114197, "[TT] Number of Lunar Flybys of the ICE (International Cometary Explorer) = 5"]
-[7.26905632019043, 4.2700934410095215, "[FF] Ground Segment of the ERS-2 = Unknown"]
-[12.021832466125488, 4.242531776428223, "[TT] Satellite Size of the ANGELS = 12U"]
-[7.138136863708496, 4.620150089263916, "[TT] Location of the IDA = Installed on the bottom side of the S/C deck"]
-[9.238367080688477, 7.506643772125244, "[TT] Ground Pixel Size of the HSRS = 372 m"]
-[5.197779655456543, 4.344648838043213, "[TT] Number of Satellites per ESPA port of the GHOSt = Two"]
-[7.924678802490234, 0.593226432800293, "[TT] Landing Date of the MASCOT = October 3, 2018"]
-[10.743358612060547, 1.4568248987197876, "[TT] Orbiting Black Hole Mass of the OJ 287 galaxy = About 150 million times the Sun's mass"]
-[4.878240585327148, 0.4434293508529663, "[TT] Launch Date of the FTHSI = July 19, 2000"]
-[11.244876861572266, 5.361659049987793, "[FF] Effective Area Falloff of the Crystal Scintillator = Approximately cosine"]
-[7.213422775268555, 2.060945749282837, "[FF] Scope of the CBPSS = Plant and microbial biology, animal and human physiology, and basic and applied physical sciences"]
-[5.892937183380127, 4.6782755851745605, "[FF] Ground Station Contact of the Satellite = Maintained"]
-[3.6697323322296143, 4.710478782653809, "[FF] Dual-receive aperture balance of the RADARSAT-2 = Some RADARSAT-2 modes (including Multi-Look Fine, Ultra-Fine and Spotlight) use dual receive apertures to double the effective pulse repetition frequency without needing to sacrifice swath width"]
-[9.303292274475098, 5.109158992767334, "[TT] Attitude Subsystem Agile Platform of the Spacecraft = \u00b145\u00ba pointing in cross-track (max), \u00b130\u00ba pointing in cross-track (nominal)"]
-[6.7145915031433105, -0.39530447125434875, "[TT] Repeat Cycle of the Satellite = 22 days"]
-[8.317904472351074, 5.39147424697876, "[TT] Radiometric Calibration Accuracy (Relative) of the TanSat = 3%"]
-[4.860575199127197, -0.31377410888671875, "[TT] Launch Time of the Falcon 9 = 1:19 a.m. Eastern (06:19 UTC)"]
-[4.715152740478516, 0.5437110066413879, "[TT] Launch Date of the CO2M = 2025"]
-[10.303177833557129, 7.239885330200195, "[TT] Ground Range x Product Length of the Spotlight = 10 x 10 km"]
-[6.285110950469971, 8.009576797485352, "[TT] Close Passes of the Messenger = 3"]
-[4.5022382736206055, 1.3191800117492676, "[TT] Scheduled Launch Year of the AlSat-2B = 2014"]
-[4.709172248840332, 0.24613818526268005, "[TT] Launch Date of the Arktika-M N1 = February 2021"]
-[4.852733135223389, 4.108920574188232, "[TT] Leading Company of the EPS-MACCS = GomSpace in Denmark"]
-[5.161510944366455, 2.0405571460723877, "[TT] Operational Capability of the GATE = Full"]
-[8.882620811462402, 2.733794927597046, "[FF] East/West Extents of the Aurora = Relatively small"]
-[7.926236629486084, 8.78560733795166, "[TT] Spectral Coverage of the WFC = 620-670 nm"]
-[7.384710311889648, 6.540907382965088, "[FF] Function of the BSM (Beam Steering Mechanism) = Directs the laser at the ground below and has fine control over where the laser is pointing"]
-[8.538224220275879, 8.42588996887207, "[TT] Resolving Power of the Spectrometers = 15 x 10^3 for the broadband measurements"]
-[8.229911804199219, 3.3644278049468994, "[FF] Measurement of the TanSat = Solar-induced Chlorophyll Fluorescence"]
-[10.322443962097168, 3.067347288131714, "[FF] URL of the MicroMAS-2 = https://tropics.ll.mit.edu/CMS/tropics/The-MicroMAS-2-Cubesat"]
-[7.933647632598877, 1.3343427181243896, "[FF] Temperature Shifts of the Unknown = Give Rise to Eruptions"]
-[9.08176040649414, 3.7233386039733887, "[FF] Affected by of the SSMIS = Solar intrusions into the warm load, and thermal emission from the reflector"]
-[7.492700099945068, 8.410770416259766, "[TT] Spectral Sensitivity of the SXI = 6 to 20 \u00c5"]
-[3.8910553455352783, 6.278468132019043, "[TT] Quantity of the Zenith antennae = 2"]
-[5.254013538360596, 1.141477108001709, "[FF] Mission Date of the JEM-EUSO = June 5-12, 2011"]
-[5.1833930015563965, -1.1950559616088867, "[TT] Launch Date of the Kondor-E1 = June 27, 2013"]
-[9.449739456176758, 5.607480525970459, "[TT] Lunar Exclusion Angle of the STARE satellites = 1\u00ba"]
-[11.177632331848145, 4.09658670425415, "[TT] Sail Surface Area of the Spacecraft = 10 m^2"]
-[8.654823303222656, 1.1503210067749023, "[FF] Verification of the Aquarius testbed = Each Aquarius instrument command activity, nominal or contingency, is verified using the Aquarius testbed"]
-[4.989387512207031, 0.7151766419410706, "[TT] Operation Start Date of the Hitomi = March 26, 2016"]
-[11.789651870727539, 6.760782718658447, "[TT] Energy Range of the MPS-LO = 30ev to 30kev"]
-[11.669986724853516, 6.753777027130127, "[TT] Energy range of the Mirror = ~0.2 to 10 keV"]
-[8.789031028747559, 8.43580436706543, "[TT] Spatial Resolution of the Miniature High-Resolution Imaging Spectrometer = Under 50 m"]
-[5.54887580871582, 7.786276340484619, "[TT] EIRP of the Steerable Beam = 57 dBW"]
-[7.1865129470825195, 6.316623210906982, "[FF] Data Acquisition Start Timing of the ARC = Adequate"]
-[11.264493942260742, 5.814423561096191, "[TT] Sample Clamping of the Bartolomeo = Between two aluminum plates"]
-[10.315804481506348, 4.530708312988281, "[FF] Reaction Wheels of the NEMO-AM = Quantity: 3, Manufacturer: SI, Momentum Storage: 60 Nms, Maximum Torque: 2 mNm, Maximum Torque Jitter: 5 x 10-5Nm"]
-[2.8938043117523193, 1.9359478950500488, "[TT] Image Capture Date of the Copernicus Sentinel-2 = January 28, 2022"]
-[13.428525924682617, 5.499680995941162, "[TT] Number of Solar Panels of the Yutu 2 = 2"]
-[5.631905555725098, 7.204158306121826, "[TT] Data Rate of the Rebroadcast = 2.11 Mbit/s (GVAR)"]
-[10.342522621154785, 1.9279900789260864, "[FF] Number of X-ray Stars of the eROSITA = Most of the remainder X-ray stars"]
-[11.71187973022461, 3.3845274448394775, "[TT] Total Impulse Capability of the Ion Thruster = > 3 x 10^6 Ns @ 20 mN"]
-[5.292556285858154, 4.752933025360107, "[FF] Purpose of the Emergency Egress System = Provide quick escape in the unlikely event of an emergency"]
-[10.221661567687988, 2.071444511413574, "[FF] Published Date of the Photospheric Emission of Gamma-Ray Bursts = 28 March 2017"]
-[8.81628704071045, 7.716099739074707, "[TT] Pixel Pitch (MS) of the Pushbroom imager = 48 \u00b5m x 48 \u00b5m"]
-[10.186525344848633, -1.3687227964401245, "[TT] Orbit Inclination of the CubeSat satellites = ~28\u00ba"]
-[9.268996238708496, 8.140105247497559, "[TT] Dead Time Fraction of the Focal Plane Module = 2%"]
-[10.174761772155762, 5.79487419128418, "[TT] Cooling Temperature of the HgCdTe detector = About 95 K"]
-[4.840875625610352, 3.7739181518554688, "[TT] Manufacturer of the S-band antennas = Victory Industrial Corp."]
-[5.926610946655273, 1.8060113191604614, "[FF] Testing Date of the Orion = May 11, 2016"]
-[8.949554443359375, 2.692093849182129, "[FF] Observation Target of the IBEX = Heliosheath"]
-[5.8258280754089355, 2.7376184463500977, "[FF] Collaborative Institutions of the TEMPO = NASA/GSFC, NOAA, EPA, NCAR, Harvard, UC Berkeley, St. Louis University, University of Alabama, Huntsville, and the University of Nebraska, KARI, NIER, ESA, and Canada"]
-[9.508429527282715, 8.318703651428223, "[TT] Field of View of the EXI instrument = 19.0\u00ba"]
-[8.044017791748047, -0.14658872783184052, "[TT] Period of the Meteor-M-2 = 101.41 minutes"]
-[10.1265287399292, 6.930408477783203, "[TT] East-West Block of the Sounder = 640 km"]
-[9.673933982849121, 7.2782464027404785, "[TT] Angular Resolution (HPD) of the Instrument = 45 arcsec"]
-[13.503771781921387, 3.5027146339416504, "[FF] Quantity of the Kuiper Belt Object = More than 100,000 objects"]
-[8.610010147094727, 3.5618038177490234, "[FF] Science Objectives of the TSIS-1 = Quantify variability in incoming solar radiation, determine regions/layers of Earth\u2019s atmosphere that are affected by solar variability, determine whether the Sun\u2019s spectral ultraviolet output is in- or out-of-phase with visible wavelength output, provide TSI and SSI data to support community science in climate, atmosphere, solar physics, and radiative transfer modeling"]
-[10.144425392150879, 7.5201311111450195, "[TT] Swath of the Imaging Plan = 290 km"]
-[5.8077473640441895, 5.36083984375, "[TT] Redundancy of the Data Handling Unit = Half Satellite"]
-[6.291908264160156, 8.666997909545898, "[TT] Polarization of the MWR = V and H"]
-[5.297290802001953, 6.759332180023193, "[TT] Download Speed of the Starlink = 100-200 Mbit/s"]
-[5.056240558624268, 7.262313365936279, "[TT] S-band Communication Data Rate of the CanX-2 = 1000 kbit/s"]
-[4.632659435272217, -0.006349172443151474, "[FF] Expected End of Life Date of the STARLETTE and Stella = At least 2050"]
-[12.614718437194824, 9.086722373962402, "[TT] Equatorial Nodal Crossing Time of the NigeriaSat-2 = 10:15 LTAN"]
-[6.053757667541504, 5.514134883880615, "[TT] Redundancy of the ADCS Mainboard = Cold redundant units"]
-[8.67839527130127, 4.735694885253906, "[TT] Quantity of the Star tracker = Single unit"]
-[13.330280303955078, 5.7261881828308105, "[FF] Function of the Space Solar Power System = Collect solar energy, convert it to RF and beam it to a receiving station on the ground for conversion to clean, usable power"]
-[9.244816780090332, -0.5196190476417542, "[TT] Perigee of the Molniya Orbit = 1043 km"]
-[8.148579597473145, 7.804095268249512, "[FF] Spectral Bands of the CCD Camera = 0.62 - 0.68 \u00b5m, 0.77 - 0.86 \u00b5m, 1.55 - 1.69 \u00b5m"]
-[5.563014984130859, 6.950072765350342, "[TT] Emergency Support Data Rate of the IXPE = 32 kbit/s"]
-[10.840590476989746, 3.947190999984741, "[FF] Deorbiting Technology of the CanX-7 = Drag Sail"]
-[6.530920505523682, -1.9701448678970337, "[TT] Design Life of the Jason-2 = 3 years"]
-[8.794672012329102, 3.637639284133911, "[FF] Objective of the HI-SCALE = Measurement of interplanetary ions and electrons"]
-[8.526190757751465, 4.571463584899902, "[FF] Telescope Size of the ASTERIA = Small"]
-[5.722268104553223, 4.05361270904541, "[FF] Design Approach of the Satellite Bus = Commercial-off-the-shelf (COTS) products"]
-[5.480010032653809, 1.5633703470230103, "[TT] Image Capture Date of the ALOS satellite = February, 2014"]
-[5.911683082580566, 1.1340794563293457, "[FF] Publication Date of the Satellite = 20 February 2020"]
-[11.788286209106445, 4.724945545196533, "[TT] Dimensions of the UniSat-3 = 40 cm in diameter and a height of 25 cm"]
-[10.013333320617676, 6.788630485534668, "[TT] Average Spacing of the GNOS-2 = 710 km"]
-[7.149796009063721, 4.990305423736572, "[FF] Speed of the Motor = Not specified"]
-[3.81858491897583, 7.156293869018555, "[TT] Antenna Gain (dB) of the Antenna = 29.3"]
-[7.342902183532715, 3.690669536590576, "[FF] GNSS Systems of the MetOp-SG Radio Occultation = Galileo, GLONASS, Beidou/Compass"]
-[9.3875093460083, -0.02943309023976326, "[TT] East to West of the Aso Caldera = 18 km"]
-[13.878070831298828, 3.6790449619293213, "[TT] Mass of the Telescope = 315 kg"]
-[14.279440879821777, 3.2652697563171387, "[TT] Mass of the HI-SCALE = 5.8 kg"]
-[10.141111373901367, -1.3175650835037231, "[TT] Orbit Inclination of the Optsat-3000 = 98.28\u00ba"]
-[9.751669883728027, 7.643968105316162, "[FF] Image Quality of the Telescope = Exceeds prelaunch expectations"]
-[10.080551147460938, 8.046406745910645, "[TT] Effective Focal Length of the Telescope = 1150 mm"]
-[4.832224369049072, 7.8782830238342285, "[TT] Frequency (MHz) of the Galileo E5a = 1176.45"]
-[11.236481666564941, 2.826348066329956, "[TT] Mass of the Nanosatellites = < 10 kg"]
-[14.562101364135742, 6.650069236755371, "[TT] Actual Battery DoD of the IXV = 10%"]
-[5.057841777801514, 8.654306411743164, "[FF] Center Frequency of the Channel = 18\u03bd, 18h"]
-[7.701848983764648, 9.22604751586914, "[TT] Wavelength Range of the Band 10 = 7.24-7.44 \u00b5m"]
-[11.410301208496094, 4.8464765548706055, "[FF] Structure of the Core module = 12-sided structure measuring 0.95 m point to point"]
-[6.295797824859619, 8.179408073425293, "[TT] No of bands/channels of the MWTS = 4"]
-[9.495569229125977, 7.93548583984375, "[TT] Field of View Resolution of the IBEX-Lo sensor = 7\u00b0 x 7\u00b0 FWHM"]
-[9.211708068847656, 6.20754861831665, "[FF] Observation Angle of the VSSC = Constant for all data acquisition at a given site"]
-[5.740414619445801, 1.1751190423965454, "[FF] Agreement Date of the GPS = June 26, 2004"]
-[8.729422569274902, -0.6182107329368591, "[FF] Imaging Modes of the ICEYE-X2 = High resolution and very wide swath"]
-[13.12166976928711, 3.180873155593872, "[TT] Sulfur Dioxide Content of the Dobson Unit = 0.0285 grams of sulfur dioxide/m2"]
-[7.8247809410095215, 8.906819343566895, "[FF] Spectral Bands of the MCP-PH = PH1: 160 to 260 nm, PH2: 337 \u00b1 5 nm, PH3: 762 \u00b1 5 nm, PH4: 600 to 900 nm"]
-[8.026413917541504, 8.773261070251465, "[TT] Spectral Coverage of the Blue = 440-510 nm"]
-[11.705058097839355, 3.9119129180908203, "[FF] Quantity of the AeroCube-5a and -5b = 2"]
-[14.038724899291992, 7.1673583984375, "[TT] Supply Voltage of the Power Supply = 27 \u00b1 1.35 V"]
-[6.468917369842529, 3.08434796333313, "[FF] URL of the Space Plug and Play Compatible Earth Observation Payload Instruments = http://media.dlr.de:8080"]
-[10.15757942199707, 5.678676605224609, "[FF] Detector Cooler of the SWIR Spectrometer = Stirling cooler"]
-[7.317966938018799, 5.477654457092285, "[FF] Components of the LCT instrument = Data electronics, laser and fiber amplifiers, computer, mechanisms, beam expander optics"]
-[10.316035270690918, 5.38662576675415, "[FF] Thermal Control of the OMT Assembly = Cold-biased passively and actively controlled using heaters"]
-[5.8672685623168945, 3.252145767211914, "[FF] Net Present Value (NPV) of the Climate Damages = Tens of trillions of US dollars"]
-[3.3487565517425537, 5.3137664794921875, "[TT] Wavelength of the SAR = 23.5 cm"]
-[6.214233875274658, 1.9610140323638916, "[FF] URL (paper) of the Cute-1.7+APD = http://lss.mes.titech.ac.jp/ssp/cute1.7/paper/aca2007.pdf"]
-[8.33617877960205, 7.741734027862549, "[TT] Intensity Variation of the STL-11000M SBIG Camera = Approximately 6%"]
-[5.056351184844971, 1.1869077682495117, "[FF] Workshop Date of the PROBA-1 = April 28, 2004"]
-[9.289863586425781, 5.3066935539245605, "[TT] Attitude Navigation Solution of the NEMO-AM = 0.036\u00b0 (2\u03c3)"]
-[6.084870338439941, 4.161350727081299, "[FF] Produces of the Services component = Information services in response to European policy priorities in environment and security"]
-[8.171659469604492, 8.885194778442383, "[FF] Wavelengths of the SOHO's EIT = 171 \u00c5, 195 \u00c5, 284 \u00c5 and 304 \u00c5"]
-[9.864645957946777, 8.781991004943848, "[TT] FOV of the Band 1 = 400 km x 0.5 km"]
-[4.598276615142822, 6.456422805786133, "[TT] RF Communications of the Spacecraft = 0.1 W (VHF beacon)"]
-[8.053362846374512, 6.245303153991699, "[FF] Payload of the AlSat-1B = Earth imaging payload with panchromatic and multispectral cameras"]
-[7.5891804695129395, 2.0141453742980957, "[FF] Purpose of the Biomass satellite = Chart all the forests on Earth"]
-[9.451735496520996, 5.7799391746521, "[TT] Exclusion Angles of the STOs and STAEs = \u00b135\u00ba (sun), \u00b125\u00ba (S/C secondary reflection) \u00b125\u00ba (moon), \u00b135\u00ba (Earth)"]
-[8.096122741699219, 7.3348188400268555, "[TT] Imaging System of the NewSat = Hyperspectral imagery"]
-[5.674833297729492, 11.346856117248535, "[FF] Approx. Peak Sensitivity Altitude of the Channel 2 = Unknown"]
-[6.177743911743164, -0.15749798715114594, "[TT] Time in Orbit of the Aeolus = 20 months"]
-[10.112351417541504, 1.1665557622909546, "[TT] Distance from Earth of the Ophiuchus galaxy cluster = 390 million light years"]
-[8.290055274963379, -0.6275722980499268, "[TT] Average Ice Thickness of the Vatnaj\u00f6kull Glacier = More than 900 m"]
-[8.03979778289795, 7.786605358123779, "[TT] Detector Elements of the SEVIRI = 3"]
-[6.5557146072387695, 4.127013206481934, "[FF] Payload of the MPQ442 = Qubduino"]
-[7.698838710784912, 8.940086364746094, "[FF] Spectral Bands of the NIRST = 3.8, 10.85, and 11.85 \u00b5m"]
-[10.870447158813477, 3.7247862815856934, "[FF] Deployment Method of the NEA Scout = From a dispenser attached to the adapter ring that connects the rocket and Orion spacecraft"]
-[13.250750541687012, 7.208538055419922, "[TT] Maximum of the Power Consumption = 12 W"]
-[3.7546191215515137, 6.650468349456787, "[TT] Beam Width of the Antenna = 0.4\u00ba-1.9\u00ba"]
-[7.001308441162109, 2.3745198249816895, "[FF] Conference Presentation Date of the Earth Observation System of the Republic of Kazakhstan = Sept. 23-27, 2013"]
-[12.778447151184082, 7.607885360717773, "[TT] Instrument Power of the HySI = 16 W"]
-[5.136435031890869, -0.5214703679084778, "[TT] Launch Date of the TARANIS = 17 Nov 2020"]
-[9.023893356323242, 0.5255180597305298, "[TT] Launch Date of the ARTEMIS = July 12, 2001"]
-[8.450021743774414, 1.9466781616210938, "[FF] Measurement Results of the SMMR = Water vapour measurements proved to be at least as accurate as radiosondes"]
-[5.489804744720459, 1.027877688407898, "[TT] Handover Date of the Diwata-1 = January 13, 2016"]
-[9.113868713378906, 7.2034430503845215, "[TT] Imaging System Resolution of the GOMX-1 = 35 m"]
-[6.026057243347168, 4.677572727203369, "[FF] Alert System of the MCP = Alerts the TARANIS payload of a TLE occurrence"]
-[14.665962219238281, 6.740992546081543, "[TT] Battery System of the EPS = 2 NiCd batteries of 19 Ah each"]
-[14.269044876098633, 3.252448797225952, "[TT] Mass of the P35 series = 91 kg"]
-[7.767482280731201, 5.074757099151611, "[TT] Reference Frame of the FF-G = Local Vertical Local Horizontal (LVLH)"]
-[12.016596794128418, -0.42583832144737244, "[TT] Launch Year of the TESS = 2018"]
-[4.792643070220947, 2.9708638191223145, "[TT] Production Location of the Airbus Arrow 450 = Airbus OneWeb Satellites factory in Merritt Island, Florida"]
-[6.20048713684082, 4.343979835510254, "[FF] Ground Segment Components of the TEMPO = IOC (Instrument Operations Centre) and the interface to the host SOC (Spacecraft Operations Centre)"]
-[7.551461219787598, 6.4500508308410645, "[TT] Measurement of Rise Time of the XGRE = 10-100 \u00b5s"]
-[6.8267292976379395, 0.6442329287528992, "[FF] Second Reaction Wheel Failure Date of the Kepler Space Telescope = Unknown"]
-[7.108516216278076, 8.430185317993164, "[TT] Spectral Channels of the CAPI instrument = 0.38, 0.67, 0.87, 1.375, and 1.64 \u00b5m"]
-[3.4494500160217285, -0.9259565472602844, "[TT] Orbit Type of the ZY 1-02C = Sun-synchronous near circular orbit"]
-[10.678998947143555, 5.637544631958008, "[TT] Electron Temperature of the Test Setup = 1.0 eV"]
-[9.763256072998047, -0.6045608520507812, "[TT] Altitude of the Orbit = 490 \u00b110 km"]
-[7.313440322875977, 2.2779266834259033, "[FF] Global Coverage of the MERSI-RM = Once per day on VIS/NIR/SWIR channels, and twice per day on MWIR/TIR"]
-[8.517404556274414, 6.894981384277344, "[TT] Image Types of the Wide Fine Resolution Beams = Single-pol (HH, VV, HV or VH) image or two dual-pol images (HH+HV or VV+VH)"]
-[8.091775894165039, -0.38533011078834534, "[FF] Refreezing Rate of the Arctic Sea Ice = Did not see its typical rate of refreezing in 2020"]
-[7.36172342300415, 7.554023742675781, "[TT] Average AOI Coverage of the CHORUS = 92.6%"]
-[5.851970672607422, 4.871538162231445, "[FF] Contact Method of the LPT = Ground stations or TDRS"]
-[5.824830532073975, 1.1862832307815552, "[FF] Experiment Date of the ETS-VII = March 14, 2000"]
-[6.371496200561523, -1.2527333498001099, "[FF] URL of the Grace Mission = https://web.archive.org/web/20230406203004/http://www.csr.utexas.edu/grace/operations/"]
-[9.351845741271973, -0.2821694612503052, "[TT] Perigee of the Satellite = 324 km"]
-[5.8332061767578125, 3.204712152481079, "[TT] Cost of the NPOESS = Exceed $14 billion"]
-[3.8431928157806396, 6.276547908782959, "[TT] Antenna Arms of the MIRAS = Three"]
-[5.224079132080078, 7.529219150543213, "[FF] Planned Improvement of the Radio Subsystem = Adapting the waveform for better channel capacity utilization"]
-[9.778996467590332, 5.421884059906006, "[FF] Thermal Gradients of the PF1 = Unknown"]
-[14.19709587097168, 3.179060220718384, "[TT] Mass of the Total = 7.49 kg"]
-[11.761885643005371, 3.291276693344116, "[TT] Thrust of the Propulsion System = 10 N"]
-[7.585511684417725, 7.077465057373047, "[TT] Cadence of the Alpha-Particle Spectrum = Up to around 20 MeV /nuc"]
-[9.85245132446289, 8.192350387573242, "[FF] Function of the Array of Cylindrical Lenses = Image the telescope pupil onto the detector"]
-[5.947845935821533, -0.6131170392036438, "[TT] Number of Years for Spacewalk Planning of the AMS-02 = 4 years"]
-[10.451743125915527, 5.752831935882568, "[TT] Temperature Range of the Battery = -5\u00ba to +25\u00ba C"]
-[8.070801734924316, 9.12757682800293, "[TT] Wavelengths of the SPIRE = 160 \u00b5m (green)"]
-[13.944836616516113, 6.202389240264893, "[FF] Power Source of the Lander = Lithium ion battery"]
-[7.1393890380859375, 3.1000618934631348, "[FF] Purpose of the LEO = Weather and reconnaissance"]
-[6.98209810256958, 4.352163791656494, "[FF] Unknown of the SPOC = Unknown"]
-[7.311090469360352, 2.296858310699463, "[FF] Mission Objectives of the ADEOS = Observe environmental changes to Earth\u2019s atmosphere, with particular areas of focus being deforestation, reduction of the ozone layer and a wider study of global warming"]
-[9.34256649017334, 5.192083358764648, "[FF] Experiment Time of the Sloshsat-FLEVO = Until the gas supply of the cold-gas reaction control system is exhausted"]
-[8.576443672180176, 6.688014507293701, "[FF] Camera Suite of the OSIRIS-REx = OCAMS"]
-[5.843815803527832, 4.178925037384033, "[TT] Type of the SEISS = Space environment"]
-[3.9507431983947754, 2.06671142578125, "[TT] Launch Vehicle of the GRACE-FO = Dnepr rocket"]
-[7.927140235900879, 2.1206324100494385, "[FF] Identification Method of the Small- and Meso-scale Ocean Features = Solely using sea surface temperature properties"]
-[11.525091171264648, 5.745549201965332, "[TT] Material of the Bus = Aluminium honeycomb panels"]
-[8.49948501586914, 7.189859867095947, "[TT] Image Transfer Modes of the Payload 2 = 8/16 bit"]
-[9.287064552307129, 6.297770023345947, "[TT] Scan Width of the SSMIS = 144\u00ba"]
-[8.748620986938477, 4.695583820343018, "[TT] Star Sensors of the R3 Spacecraft = Two 90\u00b0 offset star sensors"]
-[7.873087406158447, -0.326236367225647, "[TT] Date of the Arctic Sea Ice = 23 September 2021"]
-[11.146773338317871, 1.0107730627059937, "[TT] Relative Acceleration of the LISA Pathfinder = Lower than ten millionths of a billionth of Earth's gravitational acceleration"]
-[10.878593444824219, 5.532734394073486, "[FF] Material of the Ribbon Cable = Unknown"]
-[5.414621353149414, 6.397587776184082, "[TT] Onboard Data Storage of the QuickBird-2 = 128 Gbit"]
-[6.550729751586914, 0.3106634020805359, "[FF] Mission Start Date of the CryoSat = Unknown"]
-[13.354703903198242, 7.4683027267456055, "[TT] Input Power Range of the TWTA = -8 to -22 dBm/port"]
-[9.329205513000488, 6.6199164390563965, "[TT] Resolution of the Satellite = \u0394x = 1.2 km for \u0394\u03b8 = 0.1\u00ba"]
-[6.654003143310547, -0.4273030459880829, "[TT] Telemetry Data Acquisition Time of the CSG-1 satellite = 26 minutes after the launch"]
-[10.866562843322754, 7.511694431304932, "[TT] Swath of the Extra Fine mode = 125 km"]
-[6.534124851226807, 4.611852645874023, "[FF] Role of the GIPSY-OASIS = Simulating DSAC\u2019s expected PCD performance"]
-[7.69908332824707, 9.388444900512695, "[TT] Center Wavelength of the Band 13 = 10.35 \u00b5m"]
-[7.079476356506348, 7.247110843658447, "[TT] Minimum Optical Pulse Duration of the LI = 0.6 ms"]
-[8.587876319885254, 1.2062387466430664, "[TT] Integration Location of the Aquarius = INVAP facility in Bariloche, Argentina"]
-[4.455938816070557, 0.6600915789604187, "[TT] Entry Date of the DFM-COARSE = 5th May"]
-[7.527816295623779, 0.18516185879707336, "[TT] Sampling Mechanism Duration of the OSIRIS-REx = Approximately five seconds"]
-[9.759307861328125, -0.5888269543647766, "[TT] Orbit Altitude of the GEISAT Precursor = 520 km"]
-[5.796016216278076, 3.3956103324890137, "[TT] Satellite Cost of the Astrocast = Half a million dollars"]
-[6.016183376312256, -0.47018712759017944, "[TT] Mission Duration of the LCROSS = 26 months"]
-[6.715569019317627, 1.3033677339553833, "[TT] Image Revisit Time of the Landmapper BC = One to four-day"]
-[5.822808265686035, -2.227036237716675, "[TT] Ground speed of the KOMPSAT-3A = 7.02 km/second"]
-[7.096972942352295, 7.765763759613037, "[TT] Mount of the Cube Corner Reflectors = Floating mount"]
-[4.954043388366699, 5.035755634307861, "[FF] Communication Technology of the Quango = 5G connection and Quantum Key Distribution"]
-[7.841867446899414, 2.0849788188934326, "[FF] Purpose of the OCI = Derive optical properties of chlorophyll-sensitive species in the ocean and ocean color"]
-[6.995650291442871, 4.610367774963379, "[FF] Complement of the NIRST = Unknown"]
-[7.813457489013672, 4.517161846160889, "[FF] Orbit Computation of the Laplace = Angles-only-method"]
-[4.477977275848389, 3.178123950958252, "[TT] Main Node Location of the Ground System = IKI of Moscow"]
-[3.479177236557007, 6.406436443328857, "[TT] Antenna Size of the Reception Station = 2.4 m"]
-[9.992570877075195, 5.518269062042236, "[FF] Features of the MFCBS = Integrated thermal management system, robust structural integrity, high-attitude control accuracy, and precision three-axis stabilization"]
-[8.999343872070312, 6.86835241317749, "[TT] Observation Range of the WAC = 12 - 100 m"]
-[6.154611110687256, 1.6846027374267578, "[FF] URL of the TSU = http://www.prismasatellites.se/?id=8202"]
-[5.233687877655029, 7.145336151123047, "[TT] Downlink Margin of the CXS-810C = 5.0 dB for safe mode at 500 bit/s and 5.1 dB in nominal operations at 1 Mbit/s"]
-[13.628958702087402, 5.941713333129883, "[TT] Capacity of the Solar Power = 3.4 kW (BOL)"]
-[10.886054039001465, 7.526645660400391, "[TT] Swath Width of the WPM = 92 km"]
-[9.682124137878418, 0.3330143988132477, "[TT] Length of the PROBA-3 = 150-m"]
-[7.789212703704834, 5.863111972808838, "[TT] Type of the SSM/T-2 = Imaging multi-spectral radiometers (passive microwave)"]
-[10.89876651763916, -0.2956556975841522, "[TT] Data Acquisition of the TanDEM-X = 300 TByte"]
-[7.423347473144531, 6.4760355949401855, "[TT] Imaging to Availability Time of the Ground Network = <1 minute"]
-[5.2872748374938965, 8.425220489501953, "[TT] Bandwidth of the Radiometers = 3 kHz"]
-[4.209641933441162, 7.2085700035095215, "[TT] Band of the RLSBO = L-band"]
-[8.431859016418457, 2.819577932357788, "[TT] Daily Atmospheric Profiles of the TOR = About 250"]
-[7.275596618652344, -0.2495070844888687, "[TT] Atmosphere and Ionosphere Profiles Creation Frequency of the GRACE-FO = Up to 200 profiles per day"]
-[14.273804664611816, 3.252920150756836, "[TT] Mass of the Jugnu = ~ 3 kg"]
-[8.276639938354492, 2.8338379859924316, "[TT] Measurement Domain of the STARSHINE = Atmosphere"]
-[6.600663661956787, 6.884077072143555, "[TT] Data Reception Capacity of the Laser Terminal = 1.8 Gbit/s"]
-[11.341418266296387, 2.7813634872436523, "[TT] Mass at Launch of the PARASOL microsatellite = 120 kg"]
-[7.066433429718018, 3.522887706756592, "[FF] Page Numbers of the PROBA-3 = 38-46"]
-[5.880867958068848, 6.126898288726807, "[FF] Redundancy Principle of the SSR = Division of the total storage space into several banks of memory"]
-[6.549522399902344, 0.36673057079315186, "[TT] Impact on Ganymede's Surface of the Juice = Late 2035"]
-[6.187798023223877, 0.40680763125419617, "[FF] Mission Start Date of the ROSE-L = 29 October 2012"]
-[12.099555969238281, 7.607053279876709, "[TT] Mass of the NETCAM = 6.5 kg"]
-[10.589005470275879, 5.496260643005371, "[TT] Temperature Range of the DE probe = 0.1 - 1.5 eV"]
-[4.882966995239258, 1.7679414749145508, "[FF] Power Subsystem of the Gokturk-2 = Unknown"]
-[7.990204334259033, 5.168415069580078, "[FF] Calibration Types of the ICU = Absolute and relative radiometric calibrations and spectral calibrations"]
-[8.23183536529541, -0.0005234545678831637, "[FF] Date of the Taking a Measure of Sea Level Rise: Gravimetry = 11 November 2020"]
-[6.277225494384766, 4.4687981605529785, "[FF] Components of the MOC = Mission planning software, data management system, spacecraft ground terminal"]
-[7.3472442626953125, 3.686539888381958, "[FF] Observation Capabilities of the TriG = POD (Precise Orbit Determination), GNSS-RO (GNSS Radio Occultation), Neutral Atmosphere, Ionosphere, and Scintillation, GNSS-R (GNSS Reflections)"]
-[4.925920009613037, 0.48629358410835266, "[TT] Launch Date of the DICE = October 2011"]
-[4.6919732093811035, 4.624889373779297, "[FF] Purpose of the S&RSAT = Support search and rescue operations for aviators, mariners, and land travellers in distress"]
-[4.870487689971924, 0.8605203628540039, "[TT] Launch Date of the AMSU-A = May 13, 1998"]
-[14.017245292663574, 6.971758842468262, "[TT] Development Location of the Charge Management System = University of Florida"]
-[6.737034320831299, 4.0724005699157715, "[TT] Installation Location of the EMIT = International Space Station"]
-[7.157425880432129, 3.6744580268859863, "[FF] Frequency of the Formation Flying Maintenance = Once per week or longer"]
-[10.0050687789917, 1.9880766868591309, "[FF] URL of the Chandra = http://chandra.harvard.edu/press/18_releases/press_101218.html"]
-[7.848261833190918, 8.543545722961426, "[TT] Spectral Range of the Instrument = 350 - 1050 nm"]
-[5.457876682281494, 6.373640537261963, "[TT] Onboard Storage of the SSMI = Lost in August 2008"]
-[6.079338073730469, -0.4821230471134186, "[TT] Estimated Mission Duration of the Spacecraft = \u2264 1 month"]
-[8.459875106811523, 7.394344806671143, "[TT] Number of Segments of the Photodetector = 4"]
-[9.49378776550293, 7.165615558624268, "[TT] Resolution of the MUX = 16 m"]
-[10.207223892211914, 1.5372908115386963, "[FF] Sensitivity of the eROSITA = Enough to detect the most distant clusters of galaxies in the Universe"]
-[6.901594161987305, 1.814244031906128, "[FF] URL of the Wide-Field Imager for Solar Probe Plus = http://www.nrl.navy.mil/ssd/branches/7680/WISPR"]
-[1.933430552482605, -0.39966440200805664, "[FF] Measurement of the Van Allen Probes = Sudden pulse of electrons energized to extreme speeds"]
-[9.312451362609863, 3.29516863822937, "[TT] Exposure Time of the Coronal Loops = < 1 second"]
-[10.422967910766602, 2.813497304916382, "[FF] Design, AIT, Launch & Early-Operations of the Galassia Nanosatellite = Unknown"]
-[6.17090368270874, 0.25767824053764343, "[TT] Backup Crew Member of the Crew-4 = Assigned to fill that seat"]
-[7.183270454406738, 2.992306709289551, "[FF] Purpose of the Global GHG Monitoring Constellation = Space-based monitoring of air quality, greenhouse gases, the ozone layer and natural climate drivers like solar energy"]
-[8.164064407348633, 8.286079406738281, "[FF] Components of the FGS = Two Guider channels and one Near-Infrared Slitless Spectrometer (NIRISS) channel"]
-[14.263402938842773, 3.14261794090271, "[TT] Mass of the AISSat-2 = ~7 kg"]
-[9.197933197021484, 1.4977151155471802, "[FF] Current Location of the Voyager 2 = Beyond the heliopause"]
-[12.071682929992676, 3.7545413970947266, "[TT] Initial Plenum Pressure of the T3\u00b5PS = 1 bar"]
-[8.61338996887207, 2.3263192176818848, "[TT] Wind Velocity Range (Stratosphere) of the Aeolus = 2 - 16 km"]
-[6.20076322555542, 1.0433140993118286, "[TT] Acquisition Date of the Operational Land Imager (OLI) = October 15, 2017"]
-[5.714748382568359, 7.936866283416748, "[TT] Stabilization Rate of the FORTE = 1 Hz"]
-[8.318097114562988, 7.921853542327881, "[TT] Manufacturer of the SWIR Detectors = Sofradir"]
-[7.827536582946777, 8.890315055847168, "[FF] Center Wavelengths of the AATSR = 0.55 \u00b5m, 0.66 \u00b5m, 0.87 \u00b5m, 1.6 \u00b5m, 3.7 \u00b5m, 11 \u00b5m, 12 \u00b5m"]
-[9.002131462097168, -0.5008665919303894, "[TT] Super-Synchronous Deployment Apogee of the ABEX = 60,000 km"]
-[4.2330169677734375, 7.290482997894287, "[TT] Band Frequencies of the SweepSAR = L-band and S-band"]
-[3.849590301513672, 7.9143171310424805, "[TT] Modulation of the TT&C Data = MSK (Minimum Shift Keying)"]
-[5.889955043792725, 5.573505401611328, "[FF] Data Access of the Twinkle = Exclusive access, via encrypted transfer, to the data within days of the observation"]
-[9.000384330749512, 5.82647180557251, "[TT] Precision of the ASC = Few arcseconds"]
-[8.031681060791016, 6.373682022094727, "[FF] Target Tracking Capability of the BILSAT-1 = Yes"]
-[9.038496017456055, 5.072749137878418, "[FF] Estimated Drift of the Gyro = Standard deviation"]
-[5.397088050842285, 5.4327263832092285, "[TT] Operating System (kernel) of the STRV-1b spacecraft = Developed by the Mitre Corporation"]
-[9.916413307189941, -0.3717021644115448, "[TT] Altitude of the Secondary Payloads = 354 km x 1450 km"]
-[8.928567886352539, 7.457833290100098, "[TT] Resolution of the PamCam = 1280 x 1024 pixels"]
-[6.8844075202941895, 9.508798599243164, "[TT] NEDT at 300 K of the Band 6 = 0.3 K"]
-[8.993942260742188, 2.5141053199768066, "[FF] Mission Aim of the SOAR = Test and characterize new materials that can reduce the experienced drag and increase aerodynamic performance in low altitude orbits"]
-[10.628613471984863, 6.676252841949463, "[TT] Mirror Shape Defect of the MSI = Few tens of a \u00b5m"]
-[9.158859252929688, -1.270161509513855, "[TT] Orbit Type of the GOES-R = Geostationary"]
-[14.231552124023438, 3.166196346282959, "[TT] Mass of the ISEE-1 = 340 kg"]
-[10.157954216003418, 5.761031150817871, "[TT] Detector Temperature of the TIR Subsystem = 80 K"]
-[11.767712593078613, 3.236621856689453, "[TT] COVP of the Propulsion Subsystem = 1"]
-[7.9442667961120605, 2.5596656799316406, "[FF] Measurement Category of the MTSAT = Cloud type, amount and cloud top temperature, Liquid water and precipitation rate, Surface temperature (ocean), Atmospheric Humidity Fields, Atmospheric Winds"]
-[9.464253425598145, 4.843672275543213, "[TT] Attitude Control of the Payload = 3-axis control"]
-[7.6187872886657715, 3.42913556098938, "[FF] URL of the Space Debris IADC Assessment Report for 2010 = http://www.iadc-online.org/Documents/IADC-2011-04,%20IADC%20Annual%20Report%20for%202010.pdf"]
-[5.334314346313477, 7.301150321960449, "[TT] Bit Rate of the Transmitting Signal Bit Rate = 200 bit/s"]
-[7.884845733642578, 9.13397216796875, "[TT] Wavelength of the Sulfide = 3 \u00b5m"]
-[4.1234564781188965, 0.14785924553871155, "[FF] Launch Date of the Falcon 9 = Unknown"]
-[4.010956287384033, 6.104914665222168, "[FF] Deployment of the Antenna Dish = Outer portion of the rib must be folded before the inner portion of the rib"]
-[8.964484214782715, 3.1410531997680664, "[FF] Purpose of the DSLP = Studying characteristic macroscopic properties of ionospheric plasmas and identifying observed irregularities with possible solar-terrestrial connection related to sudden space weather events"]
-[6.2333760261535645, 3.134706974029541, "[FF] Product Integration of the BlackSky = Customer\u2019s system or BlackSky\u2019s Spectra platform"]
-[12.798543930053711, 7.617988586425781, "[TT] Power of the Aquarius instrument assembly = 375 W duty cycle, 50 W standby"]
-[8.025732040405273, -0.4067210555076599, "[TT] Annual Maximum Extent Date of the Antarctic Sea Ice = August 31"]
-[4.285171031951904, 0.7997448444366455, "[FF] Launch Year of the EDRS-A = 2016"]
-[4.5227460861206055, 1.4969406127929688, "[TT] Launch Date of the TechEdSat = March 21, 2012"]
-[3.759432077407837, 4.361947059631348, "[FF] Purpose of the RADARSAT = SAR surveys of land and ice"]
-[13.804802894592285, 6.92584753036499, "[FF] Potential of the 300 V system = Measurable"]
-[10.077680587768555, -1.503898024559021, "[TT] Inclination of the Satellite = 57\u00ba"]
-[4.3804707527160645, 6.844299793243408, "[TT] TT&C System Band of the PAZ spacecraft = S-band"]
-[9.578022003173828, 8.182997703552246, "[TT] Field of View of the WISPR = 13.5\u00ba - 105\u00ba from the Sun"]
-[11.4829683303833, 4.672961235046387, "[TT] Length of the Block 5D-2 = 6.85 m"]
-[10.361740112304688, 5.448213577270508, "[TT] Heater Circuits of the TCS = 96"]
-[9.270856857299805, 5.0752973556518555, "[TT] Attitude Measurement Accuracy of the TanSat = \u2264 0.03\u00ba"]
-[4.958622455596924, 8.02023983001709, "[TT] Frequency Range of the SAAMD = Low"]
-[5.94659423828125, 5.825231075286865, "[TT] Module Type of the RFM69HCW module = RFM69HCW"]
-[4.783752918243408, 2.8089747428894043, "[TT] Location of the Argus = York University, Toronto, Canada"]
-[6.390650272369385, -0.48149415850639343, "[TT] Transit Duration of the KELT-11b = Eight hours"]
-[5.291206359863281, 5.384345054626465, "[TT] Interface Standard of the GSCG = CCSDS SLE"]
-[10.358747482299805, 5.598439693450928, "[TT] Power of the 1 W Tactical Cooler = 1 W"]
-[5.917502403259277, 3.01705265045166, "[TT] Quantity of the WorldView Legion = 6"]
-[6.39352560043335, -0.23645834624767303, "[TT] Pass Prediction Accuracy of the SpinSat = About three weeks"]
-[11.77979850769043, 3.2771105766296387, "[TT] Thrust of the Thrusters = 10 N"]
-[5.740691661834717, 0.6585900783538818, "[FF] Status Update Date of the Cluster = July 2015"]
-[6.702243804931641, 5.230411529541016, "[FF] Distribution Function of the PDU = Distributes power to the equipment"]
-[6.769193649291992, 3.5528366565704346, "[FF] Data Type of the GPM = Three-dimensional snapshots of drop size distribution"]
-[6.550313949584961, -0.8006734251976013, "[TT] LTAN of the MetOp-B satellite = 0930 hours"]
-[7.041409492492676, 7.169154644012451, "[TT] Center Wavelength of the Laser = 1020 - 1080 nm"]
-[6.064346790313721, 2.3434629440307617, "[TT] Mission Principal Investigator of the IMAP = David McComas"]
-[6.962404251098633, 4.9417924880981445, "[TT] Joint Instrument of the MIRI = JPL and ESA"]
-[6.370486259460449, -0.2918996214866638, "[TT] Timer Validity of the MOBC = 200 days"]
-[5.308173656463623, 1.0740907192230225, "[FF] Date of the SMAPVEX12 = 2012"]
-[10.598369598388672, 2.796875476837158, "[TT] Orbit of the Astrocast's Nanosatellites = About 500 km from Earth"]
-[10.090185165405273, 7.571641445159912, "[TT] Swath Width of the TrueColour Imager = 120 km"]
-[4.787059307098389, 7.848607540130615, "[FF] DF (Direction Finder) of the 406 MHz EPIRB = 406 MHz signal"]
-[3.801809310913086, 6.726284027099609, "[TT] Antenna Type of the Knudsen Station = Two phased 2MCP8A circularly polarized VHF yagis with polarizer switching capabilities"]
-[4.024356365203857, 6.383768558502197, "[FF] Quantity of the Communication Antennas = Steerable high-gain antenna dish and two omni antennas"]
-[10.720232009887695, 1.2369613647460938, "[TT] Size of the TOI 700 = Roughly 40% of the Sun\u2019s size"]
-[8.431736946105957, 3.198993444442749, "[TT] Horizontal Cell Size of the Ozone Measurement Instrument = 250 km"]
-[6.9540300369262695, 4.28058385848999, "[FF] Unknown of the AVNIR = Unknown"]
-[10.326798439025879, 3.188009023666382, "[TT] Free Flyers Quantity of the CubeStack = 26"]
-[6.832975387573242, 4.640877723693848, "[FF] Operation of the Multi-function tool 2 = Operates smaller specialized tools to prepare for the fluid transfer"]
-[5.053948879241943, 0.6035885214805603, "[TT] Installation Date of the AMS-02 = 2011"]
-[5.307990550994873, 4.9442877769470215, "[TT] Euclidean Difference of the NovAtel GNSS receiver = 4 to 10 km"]
-[9.691664695739746, 7.162556171417236, "[TT] Ground Resolution (Fine Observation Mode) of the \u00b5SCIA = 12 km x 4 km"]
-[8.36268138885498, 5.080787658691406, "[FF] Subsystems of the GFO Accelerometer = SU (Sensor Unit) and the ICU (Interface Control Unit)"]
-[10.946606636047363, 5.650563716888428, "[TT] Erosion of the Avcoat = Roughly 20 percent"]
-[6.257907390594482, 7.9938578605651855, "[TT] Design Feature of the C-shaped channels = Engages with tabs"]
-[5.047002792358398, 8.018644332885742, "[TT] Operating Frequency of the SeaWinds = 13.402 GHz"]
-[9.083822250366211, 0.20396871864795685, "[TT] Length of the Krishna River = 1,300 km"]
-[4.8243231773376465, 7.759603023529053, "[FF] Additional Feature of the 406 MHz devices = 121.5 MHz homing transmitter"]
-[5.200740337371826, 2.7093632221221924, "[FF] Integration and Testing of the BRITE-PL = By the Polish team with mentoring and supervising support from UTIAS/SFL"]
-[12.21249008178711, -0.21484272181987762, "[TT] Image Capture Frequency of the TESS = Every 30 minutes"]
-[7.340077877044678, 2.399179220199585, "[FF] Coverage Zone of the SES-17 = North, South and Central America, the Caribbean and the Atlantic Ocean"]
-[5.131410598754883, 0.9524261355400085, "[FF] Flight Experience Presentation Date of the BIRD Onboard Navigation System = Dec. 3-7, 2001"]
-[6.293364524841309, 0.40534234046936035, "[TT] Launch Year of the ROSE-L = 2028"]
-[5.714818477630615, 5.293415069580078, "[TT] Purpose of the SES-17 and Syracuse-4E = Connectivity and security"]
-[5.996816158294678, 3.640228271484375, "[TT] Task of the Restore-L = Lock on to it"]
-[8.230426788330078, 8.821203231811523, "[TT] Spectral Sampling Distance of the UV-1 = 0.32 nm"]
-[7.862827301025391, 2.580054998397827, "[FF] Impact of the Aeolus = Comparable to the impact from other satellite-based observations which have been assimilated for many years and have much larger data volumes"]
-[12.75821304321289, 7.583527565002441, "[FF] Power Consumption of the Instrument = <1.5 W"]
-[10.177953720092773, 8.405981063842773, "[TT] Pupil Diameter of the Spectral bands = 600 mm"]
-[5.4933180809021, -1.8357795476913452, "[TT] Launch Date of the KOMPSat-5 = August 22, 2013"]
-[7.1202850341796875, 5.164332389831543, "[FF] Purpose of the MOIS Event Monitor = React to different types of events, Check the consistency of the anomaly, Request the start of the contingency recovery procedure"]
-[12.093730926513672, 3.55893874168396, "[TT] Location of the Propellant Tank = Inside the main cylinder"]
-[6.984294891357422, 4.41826057434082, "[FF] Unknown of the LCI = Unknown"]
-[9.756420135498047, 2.6391232013702393, "[TT] Flux Measurement Error of the HaloSat = 2.5%"]
-[13.638323783874512, 5.814275741577148, "[TT] Average Power of the Solar Panels = 28.5 W"]
-[5.4354119300842285, 5.134340286254883, "[TT] GPS L1 Complementary Signal Improvement of the QZS-1 = Approximately 1.7 to 2.5 times"]
-[9.22780704498291, 0.22022482752799988, "[TT] Length of the Kurushima Kaikyo Bridge = 4,015 meters (13,173 feet)"]
-[3.651503801345825, 4.670502185821533, "[TT] Constellation Type of the ICEYE = Synthetic-aperture radar (SAR)"]
-[5.924482345581055, 7.176301956176758, "[TT] Data Rate of the OBRC instrument = 10 kbit/s"]
-[4.778418064117432, 6.179436206817627, "[FF] Communication Equipment of the UNITEC-1 = Simple and inexpensive radio equipment"]
-[10.064714431762695, 7.540058135986328, "[TT] Swath Width of the Wide Field Imager = 684 km"]
-[9.529389381408691, 0.32243621349334717, "[TT] Distance Traveled of the Yutu 2 = 565.9 meters"]
-[10.075711250305176, 5.451388359069824, "[TT] Thermal Stability Requirement of the PAS = Better than 2 mK at fep (peak to peak value)"]
-[13.353435516357422, 7.602362155914307, "[TT] Transmit Power of the KaRIN = ~1.5 kW"]
-[6.901127338409424, 4.360874176025391, "[TT] Autonomously Performed by the Satellite of the RVX FDIR = Yes"]
-[9.673578262329102, 0.615471363067627, "[TT] Operating Distance of the OE = Up to 7 km"]
-[9.516378402709961, 4.937093734741211, "[TT] Attitude Control of the ACS = \u00b10.05\u00ba"]
-[5.51006555557251, 0.49681180715560913, "[TT] Checkout Date of the Y-3 = January 15 to 17, 1974"]
-[7.627044677734375, 8.75646686553955, "[TT] Bands of the MSU-MR = Six bands in the VIS and IR spectral regions"]
-[9.754325866699219, -0.4191018044948578, "[TT] Altitude of the SCI = Approximately 500 m"]
-[8.036639213562012, 7.4708781242370605, "[FF] Sub-Tasks of the Systematic and Radiometric Correction Processor = Saturated pixel detection, Suspicious pixel detection and dead pixel registration, Nonlinearity response correction, Electronic offset correction and dark current subtraction, Photo response non-uniformity (PRNU) correction, Gain matching for the VNIR spectrometer, Spectral stray-light correction, Spatial stray-light correction, Spectral referencing, Radiometric conversion, Annotation of data quality information"]
-[5.79467248916626, 3.3377597332000732, "[FF] Investment Raised of the Sateliot = 10 million euros ($11.4 million)"]
-[6.535437107086182, 7.645181179046631, "[TT] Signal Quantization of the Telescope = 13 bit/sample"]
-[4.707605361938477, 0.06874856352806091, "[TT] End of Life Date of the JPSS-2/NOAA-21 = 10-11-2029"]
-[6.345704555511475, 6.567624568939209, "[FF] Data Rate of the NIRST = Unknown"]
-[11.750410079956055, 3.3160998821258545, "[TT] Thruster Quantity of the EPPS = 8"]
-[8.174172401428223, 8.788899421691895, "[TT] Bands of the CAI-2 = Near infrared (NIR, 0.87 \u00b5m) and shortwave infrared (SWIR, 1.60 \u00b5m)"]
-[6.8089189529418945, 6.0929694175720215, "[TT] Number of Built Units of the ABI = 7"]
-[7.3008503913879395, 6.265388488769531, "[TT] Sampling Frequency of the Precipitation Data = Every half hour"]
-[11.840558052062988, 4.704941749572754, "[TT] Dimensions of the PRIMA = 3.7 m (height) by 1.36 m (diameter)"]
-[9.663474082946777, 1.3885115385055542, "[FF] Imagery of the Pleiades = Not Free"]
-[5.1369218826293945, 0.7117511034011841, "[TT] Mission Start Date of the HEOSS = Late 2015"]
-[7.026243209838867, 4.5871124267578125, "[TT] Accommodation Location of the ASIM = Starboard deck of the CEPF"]
-[8.750419616699219, 3.9111363887786865, "[FF] Function of the SDEA instrument = Deflect the ambient ions and to ionize neutrals"]
-[9.308490753173828, 8.144054412841797, "[TT] Focal Length of the LLNL imaging system = 225 mm"]
-[7.474068641662598, 2.887695074081421, "[TT] Volume Range of the Methane Leak = Between five and 20 tonnes of methane per hour"]
-[3.8868727684020996, 7.855470180511475, "[TT] Modulation Scheme of the S-band transmitter = BPSK"]
-[4.3184099197387695, 1.4272410869598389, "[TT] Launch Vehicle of the FY-3E = Long March 4C"]
-[3.8616983890533447, 6.441119194030762, "[TT] Antenna Beam Surface Incidence Angle of the SMAP = Approximately 40\u00ba"]
-[4.366392612457275, 6.261117935180664, "[FF] Operation of the ALISEO = Collects radiation and produces interference fringes"]
-[9.730154991149902, 8.318997383117676, "[TT] Optics Field-of-View of the POLDER-P = \u00b1 51\u00ba cross-track and \u00b1 43\u00ba along-track"]
-[7.703028202056885, 5.737576007843018, "[TT] Manufacturer of the Passive Microwave Imaging Radiometers = Harris Corp."]
-[5.438928127288818, 0.606488823890686, "[TT] Mission Date of the NuSTAR = March 23, 2017"]
-[11.76612663269043, 6.710129737854004, "[FF] Energy Cutoff of the SPC = Does not change"]
-[7.775587558746338, 3.1011505126953125, "[TT] XCO2 Retrieval Algorithm of the TanSat = IAPCAS"]
-[8.906442642211914, 4.660044193267822, "[FF] Components of the Sundancer = Life support systems, attitude control, three windows, on-orbit maneuverability, reboost, and de-orbit capability"]
-[8.692092895507812, 8.868725776672363, "[TT] Spectroscopy Field of View of the PACS = 47 arcsec x 47 arcsec"]
-[4.6042280197143555, 6.276222229003906, "[TT] Beacon Transmission Rate of the ELFIN-A = 9600 baud"]
-[5.312178134918213, 0.03236399218440056, "[TT] Operation Start Date of the BIRD = October 2001"]
-[4.5509209632873535, 6.653127670288086, "[FF] Communication Protocol of the Deployment Systems = RF, UHF/VHF, S-band"]
-[7.639554500579834, 5.644872665405273, "[TT] Radiometer Instrument Status of the SMAP = Active"]
-[9.715306282043457, 7.134915351867676, "[TT] Vertical Resolution of the Instrument = 1 km"]
-[6.832335948944092, -0.4509598910808563, "[TT] Duration of the Solar Cycle = 11 years"]
-[14.274065017700195, 3.1894924640655518, "[TT] Mass of the ARMADILLO = ~ 4 kg"]
-[12.079517364501953, 6.2930989265441895, "[TT] Second Event of the AMS-02 = 42 GeV Carbon nucleus"]
-[6.965575695037842, 7.085654258728027, "[TT] Number of Radar Beams of the COSI = 50"]
-[10.693305969238281, 0.9321572780609131, "[TT] Appearance from the planet of the Kepler-1658 = 60 times larger in diameter than the Sun as seen from Earth"]
-[10.823417663574219, 7.521289348602295, "[TT] Mono Mode Swath of the LISS-4 = 70 km"]
-[8.360973358154297, 3.255676031112671, "[FF] Point Spread Function Assessment of the OVIRS = Using collimated point and extended sources"]
-[11.071674346923828, 5.778838157653809, "[TT] Material of the Delrin Spacers = Delrin"]
-[14.237399101257324, 3.1864309310913086, "[TT] Mass of the Aeneas = 3.7 kg"]
-[13.59232234954834, 1.7387874126434326, "[TT] Cargo Capacity of the SpaceX Dragon spacecraft = More than 2540 kg"]
-[6.884209632873535, 7.414436340332031, "[TT] ADC type of the PHA = Wilkinson ADC"]
-[10.834348678588867, 7.451993465423584, "[TT] Swath of the CRS = 223 km"]
-[6.4539361000061035, 3.490320920944214, "[TT] Number of Primary Tools of the Dextre robotic arm = 3"]
-[4.886751651763916, 0.4350803792476654, "[TT] Launch Date of the EXPORTS = July, 2018"]
-[6.567547798156738, 5.844286918640137, "[TT] Quantity of the Payload Interface Unit = 2"]
-[8.923637390136719, 5.590845584869385, "[TT] Gaia's Position Accuracy of the GBOT = Good to 20 m arcsec"]
-[10.909424781799316, 10.088619232177734, "[FF] Unknown of the Alpha Magnetic Spectrometer - 02 (AMS-02) = Unknown"]
-[5.579949855804443, 5.631759166717529, "[TT] Microcontroller of the On-board Computer = Motorola 68332"]
-[6.940607070922852, 8.89736270904541, "[TT] Wavelength Range of the POLDER-2 = 443 - 910 nm"]
-[4.566343307495117, 0.5113269090652466, "[TT] Mission Objectives Completion Date of the M3MSat = May 2021"]
-[9.257401466369629, -0.34904131293296814, "[TT] Perigee of the Deimos-1 = ~ 642 km"]
-[6.318456172943115, 4.516871452331543, "[FF] Function of the CMART = Distribute software and database updates throughout the GS"]
-[10.818004608154297, 3.515336751937866, "[TT] Size of the AESP-14 CubeSat = 1U"]
-[9.605550765991211, 4.619757175445557, "[FF] Synthesis Approaches of the Controller = H\u221e unstructured control, mixed-\u00b5 control synthesis"]
-[7.716302394866943, 9.158075332641602, "[TT] Wavelength Range of the Band 5 = 1.58-1.64 \u00b5m"]
-[11.583287239074707, 6.640632152557373, "[TT] Energy Range of the Electrostatic Analyzer = ~100 eV to 14 keV"]
-[5.578676223754883, 5.780048847198486, "[TT] Microcontroller of the AIM = Intel 80C196 architecture"]
-[7.978894233703613, 3.1342663764953613, "[FF] Objective of the GLO-5 and GLO-6 = Measure Earth's atmospheric emissions, day and night glow, and aurora"]
-[12.810752868652344, 7.619997024536133, "[TT] Power of the Instrument = 135 W"]
-[6.954373359680176, 4.121284008026123, "[FF] Unknown of the Kaber = Unknown"]
-[9.475545883178711, 0.6279776096343994, "[TT] Operating Distance from Earth of the Euclid = 1.5 million km"]
-[8.295012474060059, 4.528886318206787, "[FF] Design of the LARES-2 = Special"]
-[8.360740661621094, 6.308794021606445, "[FF] Measurement Error of the Instrument = Slightly deteriorated when no ground echo was retrieved"]
-[5.235203266143799, 2.0702900886535645, "[TT] Mission Status of the FITSat-1 = Mission complete"]
-[8.090937614440918, 8.721940040588379, "[TT] Spectral bands of the UV/VIS Spectrometer = 248-371/387-693 nm"]
-[5.201141834259033, 7.010400772094727, "[TT] Downlink Speed of the EV-9 = 2 Mbit/s"]
-[7.687201976776123, 8.627229690551758, "[TT] Spectral Bands of the TOMS = 6"]
-[8.033644676208496, 8.663065910339355, "[TT] Spectral Range of the TOU = 500 \u2013 1000 nm"]
-[5.938056468963623, -0.5766801238059998, "[TT] Service Life of the LCT = 15 years"]
-[8.990118980407715, 5.087606906890869, "[TT] Quantity of the Gyroscopes = Three 1-axis gyroscopes"]
-[3.3722293376922607, 4.992502212524414, "[TT] SAR Bands of the NISAR = L and S-band"]
-[6.666443824768066, 6.504312038421631, "[FF] Data Time Resolution of the TRITEL = 1 minute for count rate measurements, 10 minutes for spectrum acquisition"]
-[5.576239585876465, 0.6369245052337646, "[FF] Data Acquisition Period of the ISDA = Sept.-2019 to Feb.-2020"]
-[4.994185924530029, 7.0866265296936035, "[TT] Downlink Bandwidth of the AMS-02 = 2 Mbit/s"]
-[5.985766887664795, 1.6997932195663452, "[FF] Observation Date of the Orion A = 18 November 2019"]
-[2.9126627445220947, 4.425507068634033, "[FF] Schematic Diagram of the PALSAR-2 = Not Applicable"]
-[4.805660247802734, 8.253785133361816, "[TT] Frequency Conversion of the Microwave Assembly = 24 and 32 GHz"]
-[7.240818500518799, 5.187723636627197, "[FF] Quantity of the IKFS-2 = 1"]
-[6.929782867431641, 4.409426212310791, "[FF] Failure Response of the RVX FDIR = Trigger a CAM (Collision Avoidance Maneuver) in case of imminent risk of collision"]
-[5.391286849975586, 6.434753894805908, "[TT] Module power (data retention) of the SDR-SMM = 8 W"]
-[7.631496429443359, 0.7861071825027466, "[FF] Mission Type of the Moon Impact Probe = Surface Impact"]
-[14.184638977050781, 3.227506160736084, "[TT] Mass of the Telesupport = 27 kg"]
-[5.967106819152832, 6.925490856170654, "[TT] Lossless Compression Ratio of the HSDR FPGA = 2.8:1"]
-[8.946100234985352, 7.332202434539795, "[TT] Area of the Low LET Detector = 9.6 cm^2"]
-[13.284220695495605, 5.473962306976318, "[FF] Solar Panel Configuration of the C2B = Double-deployed in cross-axis direction and two single deployed in axial direction"]
-[9.146227836608887, 7.947725772857666, "[TT] Read-out Integrated Circuit of the Focal Plane Assemblies = GeoSnap"]
-[7.7087225914001465, 1.989881992340088, "[FF] Conference Presentation Date of the High Spatio-Temporal Resolution Land Surface Temperature Mission = 22-27 July 2018"]
-[8.116137504577637, 2.740959882736206, "[TT] Measurement Domain of the GOSAT = Atmosphere, Land"]
-[9.885778427124023, 8.00727367401123, "[TT] Field of View of the NuSTAR Optics = 12 arcminutes by 12 arcminutes"]
-[4.385609149932861, 5.420282363891602, "[TT] Delivery Schedule of the GOMX-3 = About 1 year after project kickoff"]
-[5.162878036499023, 8.1663179397583, "[TT] Bandwidth (\u00c5) of the TRACE = 1700"]
-[11.155651092529297, 5.924391269683838, "[TT] Shielding Material of the LDT Sensors = Aluminum foils of different thicknesses"]
-[11.908368110656738, 5.046236038208008, "[TT] Size of the MSU-100 = 210 x 200 x 200 mm"]
-[3.587454319000244, -0.828497052192688, "[TT] Orbit Type of the CeREs CubeSat = Circular"]
-[9.939324378967285, 9.007756233215332, "[TT] Effective FOV of the Channel 3 = 42 km x 94 km"]
-[10.225156784057617, 7.867533206939697, "[FF] Optics of the Pushbroom imager = Korsch telescope with a TMA design in SiC"]
-[7.1734819412231445, 5.569293975830078, "[FF] Quantity of the MSU-SK = Unknown"]
-[6.007195472717285, 1.133284091949463, "[FF] Article Date of the NASA = 23 July 2021"]
-[5.116390705108643, 1.9210773706436157, "[TT] Status of the HSC = Operating nominally"]
-[8.46423053741455, 1.956913948059082, "[TT] Yaw of the RapidScat = Around -6\u00ba"]
-[13.483905792236328, 5.775666236877441, "[FF] Purpose of the Solar Arrays = Ensure a sufficient power supply for NASA\u2019s exploration technology demonstrations for Artemis and beyond as well as utilization and commercialization"]
-[8.33281135559082, 7.012783527374268, "[TT] Design of the O2 sensor assembly = Athermalised optical design"]
-[13.609870910644531, 5.905372619628906, "[TT] Solar Power Generation of the EPS = 48 W"]
-[9.610379219055176, 7.035747528076172, "[TT] Spatial Resolution of the OPS = Proportional to the altitude"]
-[9.085104942321777, 7.100191593170166, "[TT] Image Resolution of the RISING-2 = ~5m"]
-[3.068279504776001, 1.861511468887329, "[TT] Mission Duration of the Copernicus Sentinel-2 = 17 March to 21 April 2019"]
-[5.1902241706848145, 8.399648666381836, "[TT] Bandwidth of the Wideband Radiometer = 1 GHz"]
-[5.409449577331543, 6.39270544052124, "[TT] Device capacity of the SDR-SMM = 4 Gbit"]
-[9.976447105407715, 6.1732282638549805, "[TT] Albedo of the Lutetia = Unusually low"]
-[9.972137451171875, 7.727087497711182, "[FF] Telescope Heritage of the EUVI = EIT (EUV Imaging Telescope) heritage on SOHO and of TRACE (Transition Region and Coronal Explorer) mission heritage"]
-[7.416483402252197, 4.343764305114746, "[FF] Sensor Complement of the GOMX-3 = Unknown"]
-[5.062813758850098, 8.321686744689941, "[TT] Bandwidth Range of the AMSR3 = 200 MHz to 4000 MHz"]
-[5.85432767868042, 3.7242252826690674, "[FF] Constellation Configuration of the UrtheCast = 16-satellite constellation of eight optical and eight SAR (Synthetic Aperture Radar) satellites in LEO (Low Earth Orbit)"]
-[7.9335126876831055, -0.6542841792106628, "[TT] Contact Establishment of the Aeolus = Through the Troll ground station in Antarctica"]
-[7.00584077835083, 6.413583755493164, "[TT] Test Time of the TJ array = 60 minutes"]
-[5.964272499084473, 5.442227363586426, "[TT] Capability of the Payload OBC = Support of payloads with FPGA computing capability"]
-[7.900585174560547, 5.855401039123535, "[FF] Purpose of the Lateral Calibration Model = Establishes a mathematical model that describes the relationship between the position of the CCRR and the position of the return beam on the sensor"]
-[7.407563209533691, 6.89811372756958, "[FF] Data Analysis of the ATLAS = Analyzing the latitude, longitude and elevation represented by each photon"]
-[6.11419677734375, 4.132411956787109, "[TT] Modularization of the COSMOS Software = Subsystems and/or Devices are broken out as Agents"]
-[9.559999465942383, 9.181943893432617, "[FF] Purpose of the IRIS = Observe the transition region"]
-[5.301405429840088, 0.4350338876247406, "[TT] Launch Date of the NuSTAR = June 2012"]
-[9.151765823364258, 3.4755454063415527, "[FF] Objective of the VEFI = Provide in-situ measurements of Vector AC and DC electric fields related to plasma drift and irregularity development, Vector magnetic fields related to plasma irregularities"]
-[5.866058349609375, 0.7492059469223022, "[FF] Wind Sensor Failure Date of the QuikSCAT = Nov. 24, 2009"]
-[3.742647647857666, 3.862338066101074, "[TT] Calibration Experiment Date of the RISAT-1 MRS = Nov. 2014"]
-[10.982775688171387, 5.681963920593262, "[TT] Percentage Burned Away of the Avcoat = 20%"]
-[5.604694843292236, 0.37765270471572876, "[TT] Launch Date of the Cosmos-1066 (Astrofizika) = 23.12.1978"]
-[8.95289421081543, 9.371685981750488, "[FF] Field of View of the TANSO-CAI = Wider than the FTS"]
-[6.445931911468506, 3.3055946826934814, "[FF] Real-time Image Acquisition of the BlackSky platform = Available"]
-[8.006135940551758, 7.285039901733398, "[TT] Data Block Length of the Camera = 0 to 134 MByte"]
-[5.762519359588623, 4.6891279220581055, "[FF] Role of the CE-4R satellite = Relay satellite for a rover"]
-[5.975939750671387, -0.5083833932876587, "[TT] Mission Duration of the OPTOS = 1 year"]
-[8.093061447143555, 2.585841417312622, "[FF] Observation Objective of the UVI instrument = Atmospheric correction of turbid water, dissolved organic matter"]
-[9.41922664642334, 3.906287908554077, "[FF] Function of the STD = Measures the particle's momentum in the strong magnetic (B) field of the AMS"]
-[5.19711446762085, 0.8531664609909058, "[FF] Launch Date of the Hitomi = Unknown"]
-[11.983534812927246, -0.31557977199554443, "[TT] Northern Hemisphere Mapping of the TESS = First year"]
-[7.352614402770996, 5.927605628967285, "[FF] Proportional Function of the Extinction = exp(\u2013\u03c4(\u03bb))"]
-[7.4660420417785645, 5.41847038269043, "[FF] Design of the ALRad = Polarimetric with four separate channels and four noise diode calibration sources"]
-[3.3224258422851562, 1.421978235244751, "[TT] Design Life of the Sentinel-2B = Seven years"]
-[9.513439178466797, 6.648308277130127, "[TT] Azimuth Resolution of the Wide fine Quad-Pol = 7.6 m"]
-[6.397210121154785, -0.24564668536186218, "[TT] Bus Calibration and Validation Duration of the TeLEOS-1 = Two weeks"]
-[7.2688703536987305, 6.9640679359436035, "[TT] Electrical Noise of the APS-A and APS-B = Smaller than a digit of the ADC"]
-[4.331141471862793, 2.889923572540283, "[TT] Location of the Reykjav\u00edk = Seltjarnarnes Peninsula, in southwest Iceland"]
-[10.08439826965332, -0.050444841384887695, "[TT] Height of the DMSP Block 5B and Block 5C satellites = 214 cm"]
-[5.584672451019287, 4.288059234619141, "[FF] Extension of the EDRS = GlobeNet program by 2020"]
-[4.752890110015869, 0.38389572501182556, "[TT] Launch Date of the LAICE = > 2023"]
-[9.394516944885254, 4.986629962921143, "[TT] Attitude Control Accuracy (Pitch) of the HAUSat-2 = < \u00b11\u00ba"]
-[7.27353048324585, 5.056495189666748, "[FF] Operating Modes of the ADEOS/TOMS = Standby mode, Scan mode, Solar calibration mode, Wavelength monitoring mode, Electronic calibration mode, Reflectance calibration mode, Direct control mode"]
-[7.134998798370361, 6.564383029937744, "[TT] Target of Opportunity Duration of the INTEGRAL = 100,000 seconds"]
-[3.920893907546997, 6.4213433265686035, "[TT] Antenna Purpose of the PROBA-V plus one = Downlink large amounts of imagery to users"]
-[10.978106498718262, 1.4907875061035156, "[TT] Size of the STARLETTE and Stella = 24 cm in diameter"]
-[7.095271110534668, 6.352717876434326, "[TT] Micro-switches of the Mechanism = Array of micro-switches"]
-[6.835536003112793, 8.02232837677002, "[TT] Noise Figure of the Low Noise Amplifier (LNA) = 0.9 dB"]
-[6.100280284881592, 3.5334854125976562, "[FF] Hardware Maintenance Costs of the MEOLUT Next = The lowest on the market"]
-[11.534199714660645, 4.847330570220947, "[TT] Maximum Diameter of the Agena = 1.5 m"]
-[8.527782440185547, 6.150489330291748, "[TT] Relative Deviation of the PREMOS = At most 50 ppm after 2 years"]
-[7.68572473526001, 9.05044937133789, "[TT] Wavelength Range of the Spectral band 2 = 0.2 - 4 \u00b5m"]
-[4.607607841491699, 7.033117294311523, "[TT] Data Transmission of the Landsat-5 = X-band direct downlink only"]
-[13.384716987609863, 7.337525844573975, "[TT] Nominal Power of the ArgUS = 140 W"]
-[10.841012954711914, 0.9971736073493958, "[FF] Composition of the Brown Dwarfs = Mainly made of hydrogen and helium"]
-[6.061059951782227, 5.790505409240723, "[TT] Quantity of the Virtex-4 FPGA = 2"]
-[10.527359962463379, 2.153109312057495, "[TT] Survey Duration of the ART-XC telescope = 8 December 2019 till 10 June 2020"]
-[4.648001194000244, 5.044203758239746, "[TT] Manufacturer of the GomSpace ADS-B receiver = GomSpace"]
-[5.3692450523376465, 0.20908202230930328, "[TT] Birth Year of the Max Valier = 1895"]
-[8.524605751037598, 3.7271008491516113, "[FF] Absolute Accuracy Requirement of the CLARREO\u2019s infrared and reflected solar spectrometers = Unknown"]
-[5.769978046417236, 0.5185198783874512, "[TT] Tandem Mission Start Date of the Envisat / ERS-2 SAR = Nov. 23, 2008"]
-[6.595349311828613, 0.4390186369419098, "[TT] Orbital Insertion at Ganymede of the Juice = December 2034"]
-[7.127209663391113, 7.755095958709717, "[FF] Asymmetry of the Cube Corner Reflectors = Present when linear polarisation is used in an uncoated retroreflector"]
-[5.579529285430908, 2.2077598571777344, "[FF] Lead Author of the OMI = Xiaomeng Jin"]
-[6.439891338348389, 0.6209007501602173, "[TT] Liftoff Date of the Landsat-9 = Sept. 27"]
-[6.292081832885742, 1.6803374290466309, "[FF] Data Release of the eROSITA = First public release of eROSITA data"]
-[6.1835551261901855, 5.82155179977417, "[FF] Latency of the ISL = Critical for formation flying missions"]
-[8.821209907531738, 5.083334445953369, "[TT] Accuracy for 2000 kg payload of the IPS = 0.4 arcseconds lateral and 11.2 arcseconds for roll under star tracker control"]
-[9.372400283813477, 4.0468621253967285, "[FF] Components of the PM = HSB Magnetometer and IMU (Inertial Measurement Unit)"]
-[11.246233940124512, 5.2392168045043945, "[TT] Plasma Density of the Test Setup = 1.3 x 1012 m-3"]
-[9.725181579589844, -0.5654170513153076, "[TT] Orbit Altitude of the HY-1C = 780 km"]
-[6.086716175079346, -0.2394997924566269, "[FF] Growth Test Times of the Experiment = Within 1-2 weeks, three months, six months after launch"]
-[6.299964904785156, 5.306605339050293, "[FF] Function of the IM = Combines and splits the RF energy and serves as the interface between the transmitter, receiver, and antenna"]
-[7.028778553009033, 3.276965856552124, "[FF] Purpose of the Land Information System = Integrate satellite and ground-based data using advanced mathematical techniques to improve performance of weather and climate computer models"]
-[7.018842697143555, 4.1286301612854, "[FF] Project of the CFOSAT = Unknown"]
-[6.968055725097656, 7.756878852844238, "[TT] f/d Ratio of the Reflector Assembly = 0.5"]
-[9.114527702331543, 0.470895379781723, "[TT] Original Orbit Parameters of the ARTEMIS = Perigee: 592 km, Apogee: 17,518 km, Inclination: 3\u00ba"]
-[6.8268513679504395, 4.660013675689697, "[FF] Regulator of the IMSO = GMDSS"]
-[9.35783576965332, 5.188534259796143, "[TT] Maximum Yaw Axis Slew Rate of the TanSat = 0.2\u00b0/s"]
-[5.678664207458496, 5.500518321990967, "[TT] Architecture of the OBC = ERC32 PM"]
-[5.795135498046875, -2.1923844814300537, "[TT] Thrusters of the KOMPSAT-6 = 1 N thrusters for precise orbit correction"]
-[7.40533971786499, 3.7219104766845703, "[FF] Description of the RO Proposals = Polarimetric Global Navigation Satellite System (GNSS) Radio-Occultation (RO) payload"]
-[4.828982830047607, 6.339298248291016, "[TT] Protocol of the CW transmitter = AX.25"]
-[13.924220085144043, 3.0211215019226074, "[TT] Mass of the PW-Sat 2 = ~4 kg"]
-[5.866533279418945, 7.736012935638428, "[TT] Component Type of the TWTA = Amplifier"]
-[10.05148696899414, 1.7563966512680054, "[FF] Completeness of the Einstein's theory of gravity = May be incomplete"]
-[7.821822166442871, 0.2928068935871124, "[TT] Mission of the GRACE-FO = Gravity Recovery and Climate Experiment Follow-On"]
-[13.781052589416504, 2.9648959636688232, "[TT] Payload Mass of the Meteor-M-2 = 1200 kg"]
-[8.75991439819336, 2.781125068664551, "[FF] Telescopes Coordination of the NASA = Best-ever flare observations"]
-[12.05743408203125, 4.4666032791137695, "[TT] Spacecraft Type of the CHOMPTT = 3U"]
-[13.19057846069336, 7.550932884216309, "[TT] Tx Power of the SDR-VSAT = 200 W"]
-[4.824042320251465, -0.31083443760871887, "[TT] Upper Stage Engine Orbit Adjustment Burn Time of the Falcon 9 = One-second"]
-[7.704745769500732, 9.389871597290039, "[TT] Center Wavelength of the Band No. 17 = 644.64 nm"]
-[5.034924507141113, 3.4310836791992188, "[TT] Manufacturer of the Instrument = Northrop Grumman"]
-[10.053506851196289, 0.11876673251390457, "[TT] Satellite Position of the Harmony = 350 km in front of and behind the Sentinel-1 satellite"]
-[5.499172210693359, 2.274163246154785, "[FF] Affiliation of the Stephane Dussy = Unknown"]
-[7.237656116485596, 7.764698028564453, "[TT] Cross-talk between PHAs of the PHA = <0.2%"]
-[5.760976314544678, 0.631842851638794, "[TT] Days of data collection of the ALT = 63.5"]
-[9.175344467163086, 3.024467706680298, "[FF] Role of the Sun = Generates (regular and irregular) variations of the lithosphere-ionosphere-magnetosphere parameters by impulsive events as solar Coronal Mass Ejections and Solar Flares"]
-[6.336350440979004, 5.159745216369629, "[TT] Possibility of Cross-Tagging of the UFF TLE = Good"]
-[9.473194122314453, 0.9209177494049072, "[FF] Distance from the Sun of the Juno = Orbiting Jupiter 10 times closer to the Sun than New Horizons"]
-[4.121662616729736, 7.336353778839111, "[FF] Band of the IOCS = S-band and Ka-band"]
-[6.898802280426025, 3.2874913215637207, "[FF] Goal of the Satellite Constellation = Measure the Earth radiation imbalance"]
-[5.221942901611328, 1.2525759935379028, "[FF] Event of the SMOS = SMOS Results and MIRAS Evolution Studies"]
-[8.640691757202148, 1.1103401184082031, "[FF] Ground Segment of the SAC-D/Aquarius = Unknown"]
-[4.925864219665527, 5.479759216308594, "[TT] Frequency of the GPS Receiver = L1/L2 code"]
-[4.7821269035339355, 4.885283946990967, "[TT] Type of the NorAIS = Norwegian Automatic Identification System"]
-[13.25017261505127, 7.1941304206848145, "[TT] Maximal Power Consumption of the PPU = 22 W"]
-[7.53972053527832, 4.654654026031494, "[FF] On-Orbit Performance of the ATMS = All performance parameters are within expected values"]
-[9.965377807617188, 0.7124087810516357, "[TT] Separation Distance of the ASTRO and NextSat = 10 m"]
-[5.539034366607666, 7.063061237335205, "[TT] Data Rates of the LPT Modulator = Up to 5 Mbit/s"]
-[8.956206321716309, 6.105922698974609, "[TT] Diodes Intensity Difference Range of the Limb Sensor Unit = \u00b1120 arcseconds"]
-[5.898319721221924, -0.6288801431655884, "[TT] Mean Mission Life of the SBSS = 5.5 years"]
-[4.684922218322754, 7.962612628936768, "[TT] Frequency of the ICOM-9100 transceiver = 144 MHz (Tx), 434MHz (Rx)"]
-[13.507270812988281, 6.815131664276123, "[TT] Power Draw of the LEOStar-2 bus = 290 W"]
-[5.574425220489502, 5.545021057128906, "[TT] Bus Type of the PIC microcontroller = SPI (Serial Peripheral Interface)"]
-[12.948381423950195, 7.493389129638672, "[TT] Signal Power Boost of the GPS/Galileo E1/E5a receiver = Approximately 6 dB"]
-[4.974255084991455, 2.9106593132019043, "[TT] Prime Contractor of the Meteosat = ESA (later Alcatel Space)"]
-[12.180292129516602, -0.27452749013900757, "[TT] Ka-band Science Data Downlink Period of the TESS = 4 hr"]
-[6.829048156738281, 1.8787450790405273, "[TT] Total Photos of the FormoSat-2 = 2.55 million"]
-[4.451320171356201, 7.064640522003174, "[FF] TT&C Subsystem of the TanSat = S-band link"]
-[10.554327011108398, 4.948719024658203, "[TT] Type of the Langmuir probe = Langmuir probe"]
-[10.367478370666504, 2.7561652660369873, "[TT] Launch Date of the OTB-1 minisatellite = 25 June 2019"]
-[14.264182090759277, 3.0093038082122803, "[TT] Mass of the Global-8 = 56 kg"]
-[9.302659034729004, 5.426579475402832, "[TT] Actuation of the 2-axis gimbal = \u00b110\u00ba"]
-[4.908405303955078, 0.020635537803173065, "[TT] Launch Date of the STPSat-3 = November 20, 2013"]
-[5.974819660186768, 5.762734413146973, "[TT] Interface of the Xilinx XCV600 FPGA = 16-bit PC/104 bus"]
-[7.110131740570068, 4.546031475067139, "[TT] Mounting Location of the SSULI = +x panel of the spacecraft"]
-[7.856054306030273, 8.44485092163086, "[TT] Spectral Range of the Satellite = 300 nm to 500 nm"]
-[8.13100814819336, 8.554976463317871, "[TT] Spectral Range of the VNIR Spectrometer = 420 nm to 1000 nm"]
-[8.211213111877441, -1.0959068536758423, "[TT] Bathymetry Mapping Depth of the ICESat-2 = 26 meters"]
-[8.12138557434082, 8.595477104187012, "[TT] Spectral Resolution of the Hyperion = 10 nm in VNIR and SWIR"]
-[4.871662616729736, 0.4712214171886444, "[TT] Insertion Date of the P2 = October 22, 2010"]
-[3.571073055267334, -0.9745659828186035, "[TT] Orbit Type of the ANUSat = Near-circular"]
-[8.32227897644043, 6.5965986251831055, "[TT] Status of the STEREO-A = Operating fully"]
-[6.695489883422852, 1.8299990892410278, "[FF] URL of the Copernicus = http://m.esa.int/Our_Activities/Observing_the_Earth/Copernicus"]
-[5.2564568519592285, 7.265582084655762, "[TT] Data Rate of the LCS transmitter = 100 Mbit/s"]
-[10.892836570739746, -0.3425421714782715, "[FF] Mission Operations Segment Date of the TanDEM-X = April 25-30, 2010"]
-[10.47659969329834, 6.2996087074279785, "[TT] Total of the IASI-NG Instrument = About 8 cm"]
-[7.839979648590088, -2.4728779792785645, "[FF] Purpose of the GOLD = Examine the response of the upper atmosphere to forcing from the Sun, the magnetosphere and the lower atmosphere"]
-[7.677789688110352, 3.4290053844451904, "[FF] Additional Information Needed of the Spacecraft (S/C) OD Impact Damage Assessments = Shape and material density of the impacting debris"]
-[8.736324310302734, 8.44577407836914, "[TT] Pointing Axis Off-Pointing Angle of the Spectrometer (SPI) = 2.17\u00ba"]
-[9.271245956420898, 3.183420181274414, "[FF] Measurement of the WISPR = SEP-Producing Shocks and CME Drivers"]
-[5.634681224822998, 2.3956313133239746, "[FF] Educational Mission of the ABEX = Provide graduate students with early-career leadership roles in the project and system management roles"]
-[4.99356746673584, 3.1473045349121094, "[TT] Quantity of the Airbus space engineers and technicians = 15"]
-[6.329267978668213, 4.627222537994385, "[FF] Functions of the Satellite Management Unit = Onboard Data Handling, power and control distribution"]
-[5.419198989868164, 1.1995069980621338, "[FF] Conference Date of the Supercapacitors = 2011"]
-[9.564552307128906, 4.183717250823975, "[TT] Magnetometer of the AOCS = Magnetometer"]
-[3.4065420627593994, 5.162923812866211, "[TT] Polarization of the SAR = HH"]
-[10.107431411743164, -1.4119170904159546, "[TT] Orbit Inclination of the RISAT-1 = 97.55\u00b0"]
-[7.785881519317627, 2.710753917694092, "[FF] Purpose of the ABI = Provides high-resolution imagery and atmospheric measurements for short-term forecasts and severe weather warnings"]
-[9.847723007202148, -0.42477697134017944, "[TT] Orbit Altitude of the GNSS Satellites = 20,000-23,000 km"]
-[5.655359268188477, 3.8861477375030518, "[TT] Number of Satellites of the Sateliot IoT = At least 250"]
-[8.326664924621582, 7.0398335456848145, "[FF] Sensitivity of the BARNES pyroelectric detectors = AC component of the signal"]
-[5.670042514801025, 7.76102352142334, "[FF] RF Receive Interfaces of the T/R module = HP and VP 50 ohm"]
-[7.16792106628418, 3.6294453144073486, "[FF] Data Usage of the MATS = Produce a climatology on wave spectra"]
-[8.306962966918945, -0.8460755944252014, "[TT] Accuracy of Land Ice Surface Elevation Changes Measurement of the ATLAS = 0.4 m/year"]
-[5.541069984436035, 2.3898658752441406, "[FF] Affiliation of the Shobhakar Dhakal = Asian Institute of Technology"]
-[5.919805526733398, 6.444354057312012, "[TT] Bit Error Rates of the ISLs = Lower"]
-[13.245450019836426, 2.9018280506134033, "[TT] Mass of the CubeSats = 14 kg"]
-[7.970868110656738, 2.4204111099243164, "[FF] Impact on Numerical Weather Prediction Models of the MiniRad = Largest positive impact of any assimilated observation"]
-[11.574329376220703, 4.843931198120117, "[TT] Base Diameter of the Carrot Sprites = 3 km"]
-[11.186307907104492, 4.087666988372803, "[TT] Volume Occupation of the Sail = Lower 2/3 of the spacecraft"]
-[8.47485637664795, 0.8482304811477661, "[TT] Quantization Levels of the Ice: area covered = 1"]
-[5.422331809997559, 3.9309961795806885, "[TT] Number of Satellites of the SkySat-16 to -18 = 3"]
-[13.387127876281738, 6.715970516204834, "[TT] Power Generation of the Meteosat = 200 W average"]
-[9.056326866149902, 4.752198219299316, "[FF] Performance of the Attitude & Pointing Control Subsystems = On-Orbit"]
-[4.876783847808838, 1.7036340236663818, "[FF] Earth Observation of the Gokturk-2 = Parameter Value"]
-[9.546073913574219, 7.630606651306152, "[FF] CCD Pixel Measurements of the Nadir Sensor Wide-Field Telescope = Summed into 35 bins"]
-[5.749948978424072, 3.6450040340423584, "[TT] Cost of the Cellular Telephones = Below $100"]
-[7.027663230895996, -0.5908973813056946, "[TT] Rotation Period of the Didymos = 2.26 hours"]
-[6.9563775062561035, 4.7311530113220215, "[FF] Parameter of the LCROSS = Value"]
-[4.31884241104126, 0.9734682440757751, "[TT] Launch Date of the Argos-4 = November 26, 2022"]
-[6.568268299102783, 2.3015880584716797, "[TT] Flatness Target of the Euclid = Less than 50 microns"]
-[9.93456745147705, 2.8298585414886475, "[TT] Deployment Date from Cygnus of the VPM CubeSat = Early February 2020"]
-[3.399091958999634, 6.404708385467529, "[TT] Diameter of the Antenna dish = 11.28 m"]
-[7.892161846160889, 4.415487289428711, "[TT] Role of the CSC = Chaser spacecraft"]
-[6.542318344116211, 4.750763893127441, "[FF] Hardware Paths of the IRNSS Navigation Signal = Main and redundant"]
-[9.2009859085083, -0.41431546211242676, "[FF] Mounting of Liquid Apogee Engine of the Communications Satellites = Base of about 80 percent of the communications satellites in geosynchronous orbit"]
-[7.829812049865723, 4.9811906814575195, "[FF] Integration of the MIRU and VBS = The strategies for integrating the measurements from the available sensors (MIRU and VBS) must be carefully considered"]
-[6.557468414306641, 0.14219392836093903, "[TT] Absorbed Effects of the Constellations = Daily and Subdaily Phenomena"]
-[6.8433074951171875, 5.847728252410889, "[FF] Integration Status of the Optical Module = Completed"]
-[7.9017133712768555, 7.484057426452637, "[TT] Hyperspectral Instruments of the 90-satellite constellation = Yes"]
-[7.8363776206970215, 2.0527775287628174, "[TT] Instrument Type of the OCI = Ocean colour instruments"]
-[8.730579376220703, 3.596359968185425, "[FF] Mounting of the Solar Orbiter /PHI Full Disk Telescope = Unknown"]
-[10.303571701049805, 2.7514147758483887, "[TT] Launch Date of the BRITE/CanX-3 nanosatellites = June 19, 2014"]
-[5.453669548034668, 6.433626174926758, "[TT] Onboard Storage Capacity of the Onboard Storage and Communication Subsystem = 128 Gbit"]
-[7.124185562133789, 6.533736705780029, "[FF] Function of the PBC = Ensure primary and backup lasers head down the same path"]
-[3.6783061027526855, 4.637143135070801, "[TT] X-band Synthetic Aperture Radar (SAR) of the CHORUS = ICEYE"]
-[7.518801689147949, 2.3143301010131836, "[FF] Distribution Potential of the MDD = Particularly across Africa and the Middle East"]
-[5.274260997772217, 2.2364606857299805, "[FF] Mission Type of the JERS-1 = EO"]
-[8.199398040771484, 7.622596263885498, "[TT] SNR of the 4-band CCD Imager = 641"]
-[9.978100776672363, -0.4285591244697571, "[TT] Orbit Altitude of the Secondary Payloads = ~ 635 km"]
-[7.086198806762695, 1.307534098625183, "[FF] Image Release Date of the Spitzer Space Telescope = 27 January 2020"]
-[3.4413840770721436, 5.156122207641602, "[FF] Capability of the SAR antenna = Beam steering, multi-beam operations, large bandwidth and high efficiency"]
-[10.137173652648926, 4.3553032875061035, "[FF] Ejection Mechanism of the Picosat Launcher = Latched door with a dual-release mechanism"]
-[5.151699066162109, -0.528311014175415, "[TT] End of Life Date of the TARANIS = 17 Nov 2020"]
-[5.406052112579346, 6.992926597595215, "[TT] Speed of the LET = 1244 Mbit/s"]
-[10.216943740844727, 0.9534162282943726, "[TT] Geographic Site Sizes of the PUTC = Vary from 100 km2 up to 3500 km2"]
-[5.901910305023193, -0.4311061501502991, "[TT] Planned Operation Duration of the Tiangong = 15 years"]
-[4.784520626068115, 0.4529644250869751, "[TT] Start Year of the MDPP-2 = 2000"]
-[6.279781341552734, 4.587579250335693, "[FF] Architecture Components of the MSAS = MRS (Monitor and Ranging Stations), GMS (Ground Monitor Stations), MCS (Master Control Stations)"]
-[7.64874267578125, 4.3001179695129395, "[FF] Purpose of the Helix Orbit = Close formation flight, maintenance of baselines of a cluster of spacecraft in orbit for cross-track and along-track interferometric observations"]
-[5.608056545257568, 2.5683281421661377, "[FF] Name Change of the \u00d8rsted = DNSC (Danish National Space Center), DTU Space"]
-[11.476926803588867, 5.647784233093262, "[TT] Yield of the Inconel 718 = 1034 MPa"]
-[6.949269771575928, 4.361481666564941, "[FF] Unknown of the CVX-1 = Unknown"]
-[9.68369197845459, -0.5548226833343506, "[TT] Altitude of the OrbView-3 = ~435 km"]
-[7.933771133422852, -2.5650532245635986, "[TT] 135.6 nm Emission Contribution of the GOLD = ~10% from radiative recombination (RR) of O+"]
-[10.458431243896484, 5.975931644439697, "[TT] Brigthness Temperature (BT) Sensitivity of the Antenna = \u00b10.18 K"]
-[3.669339895248413, -0.484162837266922, "[FF] Orbital Solution of the Gaia16aye = Full"]
-[7.951945781707764, 1.777174949645996, "[FF] Mission Objectives of the GOCE = Determine the stationary gravity field - geoid and gravity anomalies with high accuracy (1 cm of geoid heights, and 1 mgal) at spatial grid resolutions of 100 km or less over the Earth's surface"]
-[5.478230953216553, 6.090084075927734, "[TT] Flash Memory of the OBC = 16 MB"]
-[5.453775882720947, 0.33443593978881836, "[FF] Crew of the STS-107 = Rick D. Husband, William C. McCool, Kalpana Chawla, David M. Brown, Michael P. Anderson, Laurel B. Clark, and Ilan Ramon"]
-[6.130885124206543, 7.445584774017334, "[TT] Number of MEMS RF switches of the Sensor Board = 4"]
-[9.240662574768066, 7.2734456062316895, "[TT] Image Resolution of the OIS = Pan images with a resolution of 7.5 m, MS images with a resolution of 15 m"]
-[6.0184478759765625, 4.750046730041504, "[FF] Communication of the BIROS = On board AVANTI experiment programs"]
-[9.67756175994873, 5.4531168937683105, "[FF] Equipped Devices of the Low Noise Amplifier = Temperature sensor, switched load"]
-[7.297867298126221, 5.657495498657227, "[FF] Function of the Instrument = Monitor instrument response and enable high data quality and reliability"]
-[12.039387702941895, 4.546341896057129, "[TT] Tray Depth of the Exposure of Spacecraft Coatings = 15.2 cm"]
-[5.9998297691345215, 4.118569374084473, "[FF] Information Delivery of the Satellite = Actionable, affordable and timely"]
-[6.175436019897461, 2.1719119548797607, "[FF] Design Basis of the Euclid = Experience gained with ESA\u2019s Herschel and Planck missions"]
-[5.57401704788208, 7.069090366363525, "[TT] Data Rate of the CBERS-4A = 900 Mbit/s"]
-[8.27333927154541, 2.526329278945923, "[FF] Secondary Objective of the CATS = Support operational applications such as air quality and special event monitoring"]
-[6.710644245147705, 5.909867763519287, "[TT] Quantity of the Hiber-1 and Hiber-2 = 2"]
-[7.823694705963135, 6.304150104522705, "[TT] Output of the HET-X = 20 - 150 millinewtons"]
-[7.754450798034668, 0.388044148683548, "[FF] Discovery Date of the Asteroid 162173 Ryugu = Unknown"]
-[7.82180118560791, 3.077522039413452, "[FF] Parameter Retrieved of the TANSO-FTS-2 = Methane column-averaged dry-air mole fraction (XCH4)"]
-[6.748386383056641, 3.116018295288086, "[TT] Program of the MetOp = Meteorological Operational Satellite Program of Europe"]
-[6.210605621337891, 4.5536088943481445, "[FF] Monitoring Function of the SPACON = Spacecraft's status in telemetry as well as the state of the ground components"]
-[9.720450401306152, -0.31807613372802734, "[TT] Value of the Altitude = 268 km"]
-[9.179879188537598, 2.9313440322875977, "[FF] Science Focus of the IMPACT = Magnetic connections to the sun, topology of interplanetary CME-related interplanetary disturbances, and the energetic particles"]
-[7.266867637634277, 4.791386127471924, "[FF] Data Processing of the EPD Sensors = Manual for first data release, future automation planned"]
-[8.983081817626953, 4.350769519805908, "[FF] Attitude Measurement of the OceanSat-1 = Earth sensors, sun sensors, a magnetometer and gyros"]
-[8.104562759399414, -1.097257375717163, "[FF] Measurement Capability of the ICESat-2 = Trace individual waves"]
-[10.267170906066895, 2.3049590587615967, "[FF] URL of the An Efficient Photoelectric X-ray Polarimeter = https://doi.org/10.1038/35079508"]
-[5.692127227783203, 4.722448825836182, "[FF] Function of the Electra = Relay data from a rover or stationary lander to an orbiter passing overhead"]
-[5.529211044311523, 4.040739059448242, "[FF] Bus Concept of the MS-2 = Modular platform capable to accommodate various types of payloads within the minisatellite class and to permit various versions and modifications of the onboard supporting subsystems"]
-[8.262770652770996, 4.5128984451293945, "[FF] Cost of the Radiation Effects Tests = On the order of $400,000"]
-[6.0453410148620605, 3.636235475540161, "[TT] Stationkeeping Maneuvers of the ISEE-3 = 15"]
-[5.592319488525391, 4.6170477867126465, "[FF] First spacecraft to have an Internet Protocol (IP) address of the STRV-1b = 1996"]
-[5.494389533996582, 6.2814412117004395, "[TT] Memory Capacity of the SLIM6 = 2 x 2 GByte"]
-[7.6494364738464355, 6.471606731414795, "[TT] Images Collected of the ABI = 5-minute Full Disk images"]
-[6.235986232757568, 2.22476863861084, "[FF] Product Line of the AstroSat = High Resolution Small and Micro Satellites"]
-[8.107150077819824, 2.374856948852539, "[TT] Data Processing Provider of the CloudSat = CIRA (Cooperative Institute for Research in the Atmosphere) of CSU (Colorado State University)"]
-[8.953240394592285, 7.464494705200195, "[TT] Resolution of the M-CAM 1 = 1024 x 1024 pixels"]
-[2.070796251296997, -0.2994055151939392, "[FF] Mission Name of the Radiation Belt Storm Probes = Radiation Belt Storm Probes"]
-[7.0094428062438965, 3.769335985183716, "[FF] Operation Priority of the PROBA-3 = FF demonstration first, then science and finally experiments"]
-[6.19927978515625, 3.922240734100342, "[FF] Data Usage of the Resurs-DK1 = Update and improvement of the existing geographic digital maps, offer an opportunity to enter the global market, to conduct surveys, to provide environmental monitoring, and to acquire real-time information on natural disasters or emergencies"]
-[6.058967113494873, 8.025012969970703, "[TT] FEC Coding Scheme of the Transmitter = 5/6 TCM"]
-[7.995258331298828, -0.3460790514945984, "[TT] Annual Minimum Date of the Arctic sea ice = September 15, 2020"]
-[6.235034942626953, 4.593658924102783, "[FF] Software Expertise of the AOCS = Over the last 20 years"]
-[11.765802383422852, 4.965697765350342, "[TT] Size of the Chipsats = 3.5 cm2 per side"]
-[14.158709526062012, 3.182339906692505, "[TT] Weight of the HRC = 2.1 kg"]
-[10.021965980529785, -1.5187042951583862, "[TT] Inclination of the Orion EFT-1 = 28.6\u00ba"]
-[6.324365139007568, 4.74401330947876, "[FF] Image Processing Chain of the EO-ALERT = Payload on-board the satellite, on-board data processing unit, flight-to-ground communications subsystem, ground units for decryption/decompression"]
-[11.608577728271484, 4.602538108825684, "[TT] Quantity of the Unpressurized Pallet Segments = 5"]
-[9.640310287475586, 7.67678689956665, "[TT] FPA Size of the Telescope = 1056 (spatial) x 256 (spectral) pixel"]
-[8.22265911102295, 3.3953213691711426, "[FF] Measurement Type of the CDMS = Impact momentum detection, penetration measurement, impact plasma detection"]
-[4.640532970428467, 0.5329819917678833, "[TT] Launch Timeframe of the BA 330 module = 2012/14"]
-[8.151172637939453, 5.076202392578125, "[TT] Calibration of the MAC = In-orbit radiometric calibration"]
-[6.3772077560424805, 3.1355130672454834, "[FF] Service of the Spire Global UK = Track the identity, position, course and speed of each vessel"]
-[5.433234691619873, 1.0574408769607544, "[TT] Public Listing Date of the Astrocast = August 2021"]
-[8.400899887084961, 2.022196054458618, "[FF] Measurement Goals of the SMMR = Obtain all-weather measurements of ocean surface temperature and wind speed"]
-[9.450311660766602, 3.365110397338867, "[TT] Mounting Location of the Solar Wind Concentrator = Within the sample canister"]
-[4.28894567489624, 7.432160377502441, "[TT] Frequency of the S-band RF Communications = 2.2 GHz"]
-[4.845067024230957, 7.182281494140625, "[TT] Data Rate of the S-band Uplink = 9.6 kbit/s"]
-[4.842530250549316, 3.101348876953125, "[TT] Developer of the WALIS (Wide Angle Localization Integrated System) = Airbus"]
-[6.208139896392822, 4.803885459899902, "[FF] Function of the CPU Board = Controls the detector and communicates with the platform of the satellite via CAN BUS interface"]
-[7.879382133483887, 2.4291129112243652, "[FF] Objective of the NIRST = Detect high temperature thermal events (HTE) such as biomass burning and volcanic ash regions"]
-[12.021203994750977, 6.391086101531982, "[FF] Be/B Ratio of the AMS = Increases with energy"]
-[5.2782511711120605, 2.665497303009033, "[FF] Agency of the Resurs-DK1 = ROSKOSMOS, ROSHYDROMET"]
-[10.029674530029297, -1.5341174602508545, "[TT] Inclination of the LARES-2 = 70.16\u00ba"]
-[12.832322120666504, 6.720020294189453, "[TT] Type of the PCDU = Miniaturized pulsed EPC"]
-[7.651832580566406, 5.681951999664307, "[FF] Technology of the Flash Imaging LiDAR = Flash imaging LiDAR"]
-[5.541083812713623, -1.9051473140716553, "[FF] Image Capture Date of the KOMPSAT-3 = Dec. 14, 2015"]
-[8.239505767822266, 7.6023783683776855, "[TT] Detector Type of the NuSTAR Metrology System = Cadmium-zinc-telluride pixel detectors"]
-[6.555943965911865, -0.5954299569129944, "[TT] Attachment Time of the Centaur Second Stage and Spacecraft = 4 minutes, 33 seconds after launch"]
-[7.716503143310547, 2.162604331970215, "[FF] Measurement of the GEDI = Forest canopy height, canopy vertical structure, and surface elevation"]
-[10.4937105178833, 5.68098783493042, "[TT] Top Temperature of the Meteosat-10 = 33.5 \u00b0C"]
-[9.069640159606934, -1.2143977880477905, "[TT] Position of the EDRS-A = Geostationary orbit with visibility over central Europe"]
-[4.489467144012451, 6.664956092834473, "[TT] RF Communications of the Spacecraft = UHF"]
-[5.145010948181152, 4.6891021728515625, "[TT] Manufacturer of the NovAtel GPS receiver = NovAtel"]
-[8.728530883789062, 7.0274176597595215, "[TT] Spatial Resolution at 20\u00b0 off-nadir of the WV60 imager = 0.55 m"]
-[10.658202171325684, 8.724433898925781, "[TT] 3 dB Footprint Size of the Channel = 15 x 10 km"]
-[10.32421875, 5.347845554351807, "[TT] Thermal Control of the KOMPSAT-6 = Passive & processor-controlled thermal control"]
-[6.739964962005615, 2.3560328483581543, "[TT] Percentage of Sky Observed in Three Exposures of the Euclid Reference Survey = 47%"]
-[5.771329402923584, 7.167303085327148, "[TT] Source Data Rate per Band of the MSU-100 = 9.8 Mbit/s"]
-[3.305293560028076, 5.269597053527832, "[TT] Wave Height of the SAR = 1.5-5 m"]
-[6.378391742706299, 3.1208746433258057, "[TT] Daily Revisit Rate of the BlackSky = 8 to 10 times a day"]
-[10.482745170593262, 5.423119068145752, "[FF] Control Method of the TCS = Passive thermal control is implemented based in the selection of materials, internal arrangement and paints or MLI (Multi-Layered Insulation)"]
-[9.284588813781738, 6.787313938140869, "[FF] Data Resolution of the GeoSTAR = Very high temporal resolutions"]
-[5.61433744430542, 3.322561264038086, "[TT] Total Value of the Joint Polar Satellite System Common Ground System contract = Approximately $1,919,705,269"]
-[6.692133903503418, 1.1003758907318115, "[FF] Mission Start Date of the Solar Dynamics Observatory = Feb. 5, 2010"]
-[4.788935661315918, 0.08148897439241409, "[TT] End of Life Date of the FITSat-1 = 4 July 2013"]
-[4.619364261627197, 1.6505374908447266, "[FF] First Pictures Date of the SkySat-3 = July 1, 2016"]
-[8.367422103881836, 7.313711166381836, "[TT] Image Gain of the PMC-2 Imagers = 1~5 levels"]
-[13.248115539550781, 7.761873245239258, "[TT] Energy of the S-band = 10 \u00b5eV"]
-[6.257976055145264, -0.1710904836654663, "[TT] Lag Time of the International Bureau of Weights and Measures = About six weeks"]
-[7.9068989753723145, 2.3772265911102295, "[FF] Purpose of the Infrared cameras = Read surface temperatures of sea and land ice"]
-[7.799935340881348, 7.608134746551514, "[FF] Color of the ATLAS = Blue, green, and purple"]
-[5.880173206329346, 3.424971342086792, "[TT] Cost of the Prometheus Satellite = Less than $100,000"]
-[7.873035907745361, 7.041272163391113, "[TT] Maximum Optical Path Difference of the Michelson Interferometer = \u00b10.8 cm"]
-[3.83132266998291, 1.2053323984146118, "[TT] Configuration of the PSLV-C38 = XL"]
-[4.6892571449279785, 7.293848514556885, "[TT] Antenna Data Rate of the X-band JPL Iris Radio = 128 kbit/s with the 34 m DSN antennas and 64 kbit/s with the MSU 21 m Ground Station"]
-[4.70257043838501, 7.345776557922363, "[TT] Ka-band Data Rate of the IOCS = 120 Mbit/s max"]
-[10.143891334533691, 1.3733867406845093, "[TT] Distance Limit of the Gaia Catalogue of Nearby Stars = 326 light years"]
-[9.008734703063965, 8.01814079284668, "[TT] Focal Plane of the Camera = 3 CCD lines"]
-[8.719259262084961, -0.22195374965667725, "[TT] Inclina. (\u00ba) of the Meteor-1-2 = 81.2"]
-[5.2147321701049805, 2.1769962310791016, "[TT] Status of the SwissCube = Active"]
-[7.107816696166992, -0.10265722870826721, "[TT] Rotation Period of the Crab Nebula = About 30 times a second"]
-[12.654013633728027, 3.1737060546875, "[TT] RCS Fuel Capacity of the SLATS = 34.3 kg"]
-[14.278867721557617, 3.233811616897583, "[TT] Mass of the P35 series = 40 kg"]
-[13.253301620483398, 5.261422157287598, "[TT] Span of the Solar Panel = 7.9 m"]
-[7.924405097961426, 4.625168800354004, "[FF] Internal Calibration Modes of the MIRAS = Short duration, full orbit"]
-[6.582917213439941, -0.5020807385444641, "[TT] Period of the RESURS-O1-4 = 97 minutes"]
-[3.900371551513672, 1.9709755182266235, "[TT] Launch Vehicle of the Launch Segment = Soyuz 2-1b"]
-[6.551483154296875, 4.362836837768555, "[FF] AWiFS Data Access of the Resourcesat-1 = Unknown"]
-[5.6561808586120605, 7.0437726974487305, "[TT] Data Rate of the GSN = Up to 622 Mbit/s"]
-[4.362733364105225, 3.7646007537841797, "[FF] Number of Devices Served of the Galileo = More than 1.5 billion smartphones and devices"]
-[12.2286376953125, 3.425882577896118, "[TT] Propellant Tank Capacity of the Propulsion Subsystem = 20 liter"]
-[7.059886932373047, 8.334272384643555, "[TT] SNR of the Band 3 = 400"]
-[8.166255950927734, 5.222904205322266, "[FF] Selectable Positions of the Onboard calibration wheel = Open (nominal), closed (testing) and X-ray source (calibration)"]
-[8.360931396484375, 1.5079545974731445, "[TT] Accuracy Range of the Surface specific humidity = 0.4 g/kg 2-20 g/kg"]
-[7.439296722412109, 2.9917376041412354, "[TT] Measurement Precision of the GHGSat's New Satellites = 1% of background for methane"]
-[8.144278526306152, 9.09724235534668, "[FF] Parameter Species Wavelength of the SSUSI = O + 834 \u00c5"]
-[3.2491204738616943, 5.657138824462891, "[TT] Length of the SAR Antenna = 9.9 m"]
-[8.568973541259766, 8.611710548400879, "[TT] Instantaneous spectral coverage of the Spectrometer = 1.37 km/s"]
-[6.841854095458984, 0.5872875452041626, "[TT] Retirement Date of the Kepler = September 28, 2018"]
-[9.737972259521484, 3.9983432292938232, "[TT] Spatial Extent of the Magnetic Null = 500 km"]
-[9.26245403289795, 4.921492099761963, "[TT] Gyroscopic Attitude Control Channels of the Electro-L = 4"]
-[4.226956367492676, 7.323046684265137, "[TT] Frequency Bands of the RA/HY-2 = Ku-band and C-band"]
-[9.279403686523438, 4.983304023742676, "[FF] Objective of the Slew Mode = Slew the satellite from its arbitrary attitude after detumble into an attitude where the correct body panel is nadir-pointing and the satellite is oriented correctly along-track"]
-[6.919984340667725, -0.7456373572349548, "[FF] Orbital Period of the A and C systems = About every four years"]
-[10.25081729888916, 7.858742713928223, "[TT] Downlink Telescope Size of the GS-2 = 60 cm"]
-[8.410740852355957, 7.021769046783447, "[TT] Type of the Imaging Detector Array = Pushbroom"]
-[5.277338027954102, 6.786314964294434, "[TT] Data Bus Speed of the Spacecraft = 1 Mbit/s"]
-[5.84382438659668, 1.914202094078064, "[FF] Mission Status of the BRITE-Austria = Unknown"]
-[7.0472588539123535, 3.440183401107788, "[FF] Purpose of the Catalytic Reactor = Provide critical sparing support for the water production capability for the environmental control and life support system (ECLSS)"]
-[10.394920349121094, 7.582529544830322, "[TT] Spectral Range of the S-192 optomechanical scanner = 0.4-12.5 \u00b5m"]
-[9.143263816833496, 1.3780409097671509, "[FF] Publication Date of the New Horizons = 15 November 2021"]
-[7.741199493408203, 5.140234470367432, "[TT] Number of RadFETs of the CDE = 8"]
-[5.494704246520996, 0.6296064257621765, "[FF] Date of the A Data With Destiny = 9 December 2021"]
-[9.279290199279785, 7.052265167236328, "[FF] Measurement Scenario of the MIPAS = Enhanced Vertical Resolution and Regularization"]
-[9.475250244140625, 6.9882988929748535, "[TT] Spatial Resolution - Strip map of the ALOS = 10 m"]
-[8.713556289672852, 2.0094261169433594, "[TT] Wind Direction Range of the SCAT = \u00b120\u00ba"]
-[7.07576322555542, 0.24747306108474731, "[TT] Formation Time Offset of the CloudSat = 12.5 \u00b1 2.5 s ahead of CALIPSO"]
-[3.255436897277832, 4.854216575622559, "[TT] SAR Data Collection of the SeaSat = Approximately 42 hours"]
-[8.032133102416992, 9.020418167114258, "[TT] Wavelength of the Fe XIV = 530.285 nm"]
-[9.289936065673828, 6.427181243896484, "[TT] Scan Time of the VISSR Mirror = 30 minutes"]
-[5.969223499298096, 2.665166139602661, "[FF] Development Consortium of the HyperScout = cosine, VITO, S&T, Technical University of Delft"]
-[5.276356220245361, 3.22878360748291, "[FF] Partner of the GFO satellite system = Astrium GmbH"]
-[9.660347938537598, -0.41986769437789917, "[TT] Altitude of the LARES-2 = 5893 km"]
-[4.955100059509277, 0.730704665184021, "[TT] Initial Services in the United Kingdom of the Lightspeed = 2026"]
-[9.984282493591309, -1.4223518371582031, "[TT] Orbit Inclination of the COSPAS-1 = 83\u00ba"]
-[11.710103034973145, 7.505960464477539, "[TT] Provider of the Megha Tropiques = CNES and ISRO"]
-[10.37061882019043, 1.840274453163147, "[FF] Probes of the NuSTAR = Black Hole Jet Mystery"]
-[3.4984872341156006, 6.447140693664551, "[TT] Swath Width of the Antenna = 1000 km"]
-[11.068199157714844, 4.7922587394714355, "[FF] Operation of the Tether System = Voltage is on when the tether moves downwind with respect to the plasma ram flow and off when it moves upwind"]
-[9.872220993041992, -0.44302576780319214, "[TT] Orbit Altitude of the Satellite = 786 km"]
-[7.435379981994629, 1.4159178733825684, "[FF] Symposium Date of the ECOSTRESS = July 23\u201328, 2017"]
-[4.665806770324707, 3.391568660736084, "[TT] Raw Data Processing Location of the CBERS-4A = S\u00e3o Jos\u00e9 dos Campos, SP"]
-[6.8207573890686035, 7.431545257568359, "[TT] Digitizer of the Data Acquisition Unit = 8 bit"]
-[5.297207355499268, 4.4981207847595215, "[TT] Mission Ground Segment of the Ground Segment = CLS network"]
-[10.157560348510742, -2.7819652557373047, "[TT] Erase Time of the SLC NAND-Flash = 2 ms on block level (256 k x 8)"]
-[4.606116771697998, 1.151681900024414, "[TT] Launch Date of the PhiSat-2 = End of 2023/beginning of 2024"]
-[4.71034574508667, 0.6847972869873047, "[TT] Launch Date of the FY-2 = May 29, 2012"]
-[8.113739967346191, 3.364976167678833, "[FF] Purpose of the OCO-3 = Response to growing populations and varying patterns of fossil fuel consumption"]
-[5.011417388916016, 3.400803327560425, "[TT] Manufacturer of the GEMS = GSFC"]
-[7.702186107635498, 6.077148914337158, "[TT] Description of the Searching Mode = Open loop tracking mode for initial acquisition and re-acquisition"]
-[4.562315464019775, 3.0863759517669678, "[TT] Control Center of the GIOVE-A and GIOVE-B = SSTL in Guildford (UK)"]
-[7.08309268951416, 0.86834317445755, "[FF] NASA Announcement of the Gravity Probe B = May 4, 2011"]
-[6.53981876373291, 6.036839962005615, "[FF] RF Emissions of the DSX = Flow Diagram"]
-[6.649117469787598, 5.446953773498535, "[FF] Quantity of the PDGS = 1"]
-[5.65806770324707, 7.884428024291992, "[TT] Design of the Power Amplifier (PA) = Robust mechanical design based on fiber components"]
-[7.6605682373046875, 1.9015229940414429, "[FF] Greening of the Northern Forests = Rare benevolent effects of our warming climate"]
-[7.186499118804932, 4.945091724395752, "[FF] Parameter of the DeCor-type instrument = Value"]
-[4.813534736633301, -1.888374924659729, "[TT] Number of International Joint Collaboration Payloads of the Chang\u2019e-4 = 3"]
-[5.35941219329834, 2.6054275035858154, "[TT] Number of Koranic schools of the University of Sankore = 180"]
-[11.493683815002441, 5.777905464172363, "[TT] Structure of the SCD-2 = Aluminum honeycomb"]
-[5.55394983291626, -1.9123982191085815, "[FF] Mission Status of the KOMPSAT-3 = Fully operational in its 7th year of service"]
-[6.5489182472229, 4.349028587341309, "[FF] Development Units of the OCSD = Two flight units and an engineering model"]
-[4.640847682952881, 8.047561645507812, "[TT] Transponder Frequency of the DASS = 1544-1545 MHz"]
-[5.440438270568848, 6.860298156738281, "[TT] Bidirectional Port Baud Rates of the NIC = 9600 to 115,200 baud"]
-[8.424947738647461, 7.522346496582031, "[TT] Ground Resolution of the CCD Detector System = 0.65 m"]
-[9.305220603942871, -1.6464375257492065, "[TT] Number of Maneuvers of the Swarm-A = 9"]
-[12.263175010681152, 6.935816287994385, "[TT] Energy Range for Fe of the LEICA = 0.21 - 3.1 11 - 90 27 - 450 70 - 270 MeV/n"]
-[4.2188944816589355, 5.396232604980469, "[TT] Frequency of the GPS-SAR = 406 MHz"]
-[4.615280628204346, 2.7416131496429443, "[TT] Filter of the BRITE = Different from Another BRITE Satellite"]
-[2.9630062580108643, -0.3585624098777771, "[TT] Altitude of Final Orbit of the OneWeb Satellites = 1,200 kilometers"]
-[6.511027812957764, 1.9225140810012817, "[FF] URL of the SARah-1 = https://www.airbus.com/en/newsroom/press-releases/2022-06-airbus-built-earth-observation-satellite-sarah-1-ready-for-launch"]
-[6.3482160568237305, 4.617374897003174, "[FF] Function of the MCE = Provides the planning and satellite command, control functions and the maintenance of the satellite systems"]
-[6.214890956878662, 4.760015487670898, "[TT] Designations of the FengYun-4 = FengYun-4A through -4G"]
-[3.2704920768737793, 5.044733047485352, "[TT] Swath of the Seasat SAR sensor = Extends from 290 km to 390 km to the right of the S/C ground track"]
-[7.692512512207031, 8.740944862365723, "[TT] NEDT of the Spectral Bands = 3.55 - 3.88, 8.25 - 8.80, 10.3 - 11.4, 11.4 - 12.7"]
-[5.757471561431885, 1.0356196165084839, "[FF] International Astronautical Congress Date of the Odin = October 6-10, 1997"]
-[7.031158447265625, 6.141908645629883, "[TT] Data Update Frequency of the GPM = Every half-hour"]
-[6.4858832359313965, 3.032080888748169, "[FF] Imagery Remapping Goals of the Satellogic = Weekly remapping of the entire globe with high-resolution imagery in 2023, daily remapping when the full constellation is in place in 2025"]
-[7.968959808349609, -2.563175916671753, "[TT] Brightness Unit of the GOLD = R (1R = 1010 photons m-2 s-1 steradian-1)"]
-[5.781380653381348, 7.061066627502441, "[TT] Data Rate of the HSDR = 80 Mbit/s"]
-[6.0196213722229, 1.9701274633407593, "[FF] Mission Status of the MASCOT Sample Return Capsule = Unknown"]
-[4.759882926940918, -1.8728255033493042, "[TT] Resumed Work Days of the Chang'e-4 = 21"]
-[10.430115699768066, 5.403026103973389, "[TT] Heater Lines of the OTC = 13"]
-[3.6429567337036133, 2.7013559341430664, "[TT] Number of Warnings of the Iridium constellation of satellites = About 10 per day"]
-[6.796621799468994, 2.7287065982818604, "[FF] Test Subject of the Biofilms = Laser-structured metal surfaces such as steel, copper and brass"]
-[5.207685470581055, 3.317095994949341, "[TT] Manufacturer of the MATHS = ISRO"]
-[8.02022933959961, 9.000334739685059, "[TT] Wavelength Range of Sensitivity of the MAHRSI = 195-320 nm"]
-[10.346424102783203, 4.119968414306641, "[TT] Direction of the Spool = Counterclockwise"]
-[6.1129350662231445, 6.14484167098999, "[TT] Data Processing Algorithm of the V5QV FPGA = MSPI algorithm"]
-[4.969025135040283, 6.766707420349121, "[TT] Bit Error Rate of the LEO-LEO Inter-satellite Link = < 10-9"]
-[10.904027938842773, 7.544254779815674, "[TT] Width of the Swath width = 2800 km"]
-[8.162461280822754, 7.89503288269043, "[TT] Bands of the CCD Camera = 430-520 nm, 520-600 nm, 630-690 nm, 760-900 nm"]
-[10.758594512939453, -1.1389386653900146, "[TT] Altitude of the SLATS = ~200 km"]
-[3.6324124336242676, 2.6933541297912598, "[FF] Number of Satellites of the Iridium-4 NEXT Mission = 10"]
-[4.866387367248535, 0.3858471214771271, "[TT] End Date of the SLA = About 2030"]
-[7.6905388832092285, 2.9352598190307617, "[FF] Mission of the GOSAT = Greenhouse Gases Observing"]
-[5.020278453826904, 0.7134642004966736, "[TT] First Flight Date of the SLS = 2020"]
-[10.07052993774414, -1.5273962020874023, "[TT] Inclination of the Satellite = 56.2\u00ba"]
-[9.82178020477295, 7.642218112945557, "[TT] Image Stabilization of the Telescope = \u00b10.1 arcsec"]
-[5.819925308227539, 5.437587738037109, "[TT] Reprogrammable of the MCU = Reprogrammable"]
-[6.246777057647705, 5.846227169036865, "[TT] Component Type of the OUTMTX = Matrix"]
-[8.633092880249023, 7.702969551086426, "[TT] Array Size of the Detector = 1024 x 1024 pixels"]
-[8.14490795135498, 4.323437213897705, "[FF] Purpose of the Mechanical model = Stray light analysis"]
-[6.7394208908081055, 1.8664218187332153, "[FF] URL of the NASA Orbiting Carbon Observatory-2 = http://meetingorganizer.copernicus.org/EGU2015/EGU2015-6804.pdf"]
-[9.862016677856445, -1.573886752128601, "[TT] Eccentricity of the Secondary Payloads = 0.075"]
-[4.997828483581543, 0.9932044148445129, "[TT] Communication Failure of the Hitomi = March 26, 2016"]
-[6.045857906341553, 7.158730506896973, "[TT] Range Measurement of the KBR = To the \u00b5m level"]
-[6.5451178550720215, 0.581784725189209, "[TT] Dark Sky Park Designation Date of the Watoga State Park = October 2021"]
-[8.673827171325684, 1.1206899881362915, "[TT] Commissioning Completion Date of the Aquarius = Aug. 24, 2011"]
-[10.122184753417969, 7.071645736694336, "[TT] On-Ground Footprint Range of the MWI = 50 km down to 10 km"]
-[8.73052978515625, 0.04609072208404541, "[TT] Orbit Altitude of the Rosetta = Less than 10 km from the comet's surface"]
-[8.405609130859375, 7.384422302246094, "[TT] Analog Output Frequency of the CMOSIS CHR70M Image Sensor = 30MHz"]
-[7.4772562980651855, 6.918408393859863, "[TT] Cadence of the Housekeeping = 1 minute"]
-[13.978487968444824, 7.1862993240356445, "[TT] Supply Voltage of the GAMALINK = 3.3 V or 5 V"]
-[13.370821952819824, 2.8832039833068848, "[TT] Mass of the DubaiSat-1 = ~ 190 kg"]
-[11.497587203979492, 3.5146493911743164, "[TT] Propulsion System of the MERLIN = Newly adapted"]
-[4.729670524597168, 7.3467116355896, "[TT] Data Rate of the X-band Transmitter = Up to 210 Mbit/s"]
-[5.212929725646973, 6.989419937133789, "[TT] Downlink Speed of the AprizeSat-3 and AprizeSat-4 = Up to 300 kbit/s"]
-[14.089136123657227, 7.165712833404541, "[TT] Voltage of the S/C Power = 28 V"]
-[8.729729652404785, 3.6539645195007324, "[FF] Function of the EFP = Measure only one component of both DC and AC electric fields for identifying disturbed regions of the ionosphere"]
-[8.035940170288086, 4.576051235198975, "[FF] Purpose of the Scanning Radiometer = Observes the radiance of the atmosphere at microwave wavelengths"]
-[5.5946221351623535, 0.02335156872868538, "[TT] End of Operation of the LS-7 = 2012"]
-[5.755690097808838, 7.158412933349609, "[TT] Data Rate (max) of the TXS = 100 kbit/s"]
-[5.650915622711182, 3.281661033630371, "[TT] Quantity of the Satellite = 2 sun-synchronous Legions"]
-[10.446955680847168, 1.6207462549209595, "[FF] Definition of the Eddington luminosity = Luminosity upper limit at which the radiation pressure balances the gravitational force"]
-[7.090958118438721, 3.7011096477508545, "[FF] Purpose of Models of the PROBA-3 = Visualize orientation and explain the mission easily"]
-[10.041881561279297, 2.6782751083374023, "[TT] Launch Date of the Kaber (NanoRacks Microsat Deployer) = December 6, 2015"]
-[9.204526901245117, 6.062507152557373, "[TT] Static Cold Start Acquisition Time of the Antenna Subsystem = < 720 s"]
-[14.05165958404541, 4.048278331756592, "[TT] Mass of the LCT instrument = 53 kg"]
-[7.706790924072266, -0.8447477221488953, "[FF] Publication Date of the ICESat-2 = 10 March 2020"]
-[4.7364325523376465, -1.8198204040527344, "[FF] Imaging of the Chang\u2019e-3 = Yes"]
-[13.592218399047852, 3.4088351726531982, "[TT] Mass of the MMW Radar = 50 kg"]
-[10.384705543518066, 5.7844038009643555, "[TT] Electronics Temperature of the VIS = 290 K (20\u00b0C)"]
-[7.545217037200928, -2.4532511234283447, "[FF] Level 2 Data Release Date of the GOLD = June 3, 2019"]
-[8.580252647399902, 3.8977091312408447, "[FF] Energy Suppression of the IBEX-Lo sensor = External electrons below ~600 eV and the external ions below 10 keV"]
-[8.762073516845703, 9.409830093383789, "[TT] Spectral Band 4 Bandwidth of the TANSO-CAI = 90 nm"]
-[8.27254867553711, 6.4523138999938965, "[FF] Purpose of the LDT = Measure the effect of protons on photodiodes and LEDs"]
-[4.223128318786621, 0.7162750363349915, "[TT] Launch Date of the EDRS-A = Late January 2016"]
-[8.508230209350586, 1.8015981912612915, "[TT] Landfall Location of the Tropical Storm Fred = Florida Panhandle near Apalachicola"]
-[4.367488384246826, 4.272126197814941, "[TT] Number of LEOSAR satellites of the COSPAS-SARSAT system = 5"]
-[11.816704750061035, 0.06406796723604202, "[FF] Purpose of the TESS = Find Earth-sized planets orbiting nearby stars"]
-[3.580477476119995, -0.8106316328048706, "[TT] Orbit Type of the ELaNa-4 CubeSats = Near-circular orbit"]
-[5.377399444580078, 4.098170280456543, "[TT] Satellite Constellation of the EDRS = 3 satellites"]
-[4.799502372741699, -1.8136389255523682, "[TT] Landing Accuracy of the Chang'e-3 lander = Better than 0.6 km"]
-[3.2341151237487793, 3.840764045715332, "[TT] Operation Status of the TerraSAR-X = Nominal as of 2010"]
-[5.432064056396484, 7.170239448547363, "[TT] High-Voltage Transmission of the Modulator Assembly = Niobium wire"]
-[10.832015037536621, -0.28240707516670227, "[FF] Objective of the TerraSAR-X and TanDEM-X = Generate an updated global DEM which exceeds the presently available global data sets in terms of resolution, coverage, and quality by orders of magnitude"]
-[9.256264686584473, -0.6397159099578857, "[TT] Orbit of the Tianzhou-2 = 343 by 371 kilometers"]
-[4.4825334548950195, 6.756107330322266, "[TT] Transceiver of the SCARAB = AstroDev Helium-100 UHF/VHF transceiver"]
-[13.614020347595215, 2.982382297515869, "[TT] Payload Capacity of the X-SAT Saturn-Class = Up to 200 kg"]
-[7.9294538497924805, 0.18057265877723694, "[FF] Mission Purpose of the GRACE-FO = Measuring changes in high-resolution monthly global models of Earth\u2019s gravitational field"]
-[6.829634189605713, -0.5542352199554443, "[TT] Observation Duration of the HD 31901 = 27 days"]
-[9.784530639648438, -0.43048566579818726, "[TT] Altitude of the Landsat 9 = 705 km"]
-[5.0573577880859375, 3.3649721145629883, "[FF] Supplier of the TT&C transponders = COM DEV"]
-[7.202442169189453, 8.44548225402832, "[TT] Filter Wheel of the MWIR = 6 filters"]
-[8.412675857543945, 8.210497856140137, "[TT] Multispectral Band: Green of the NAOMI = 0.53 - 0.60 \u00b5m"]
-[6.440806865692139, 1.5209729671478271, "[FF] Development Date of the Microscope Mission = Unknown"]
-[11.95400333404541, -0.2578480541706085, "[FF] Project Scientist of the TESS = Stephen Rinehart"]
-[10.136185646057129, 7.917969703674316, "[TT] Telescope Separation of the Gaia = 106.5\u00ba"]
-[9.594976425170898, 1.4635705947875977, "[TT] Ejection Velocity of the DSAT-2 = Low"]
-[6.277882099151611, 3.268117904663086, "[TT] Long-Term Goal of the BlackSky = Deploy 30 satellites by 2023, and possibly 60 in the years after"]
-[7.284040451049805, 3.942640542984009, "[FF] Stray Light Analysis of the ASPIICS/PROBA-3 = Optimization"]
-[9.405221939086914, 7.3230743408203125, "[TT] Resolution of the MSC = 1 m (Pan)"]
-[4.56035041809082, 5.919497489929199, "[TT] Old Frequency of the Distress Beacons = 121.5 MHz"]
-[5.614099502563477, 5.672983646392822, "[TT] CPU of the OBC (On-Board Processor) module = TSC695F"]
-[4.306131839752197, 2.5589025020599365, "[TT] Launch Site of the GOES-R = Kennedy Space Center, Florida"]
-[6.907909393310547, 0.02816479094326496, "[FF] Purpose of the Cheollian 2B satellite = Observing the ocean and atmospheric environment around East Asia, including the Korean Peninsula"]
-[4.98411750793457, 8.234508514404297, "[TT] Surface Acoustic Wave Generator Frequency of the Poseidon-1 = 900 MHz"]
-[5.0510945320129395, 7.352540493011475, "[TT] RF Trunkline of the LCRD = High data rate"]
-[4.887557506561279, 3.15674090385437, "[TT] Manufacturer of the SES-14 = Airbus DS"]
-[9.322550773620605, 2.5759503841400146, "[FF] Flare List Events with Emission above 300 keV of the RHESSI = 35"]
-[3.956230878829956, 6.507081508636475, "[TT] Antenna Type of the XTU = One-axis (\u00b190\u00ba) steerable antenna"]
-[11.474839210510254, 3.442690134048462, "[FF] Initial Design of the DFACS = FEEP (Field Emission Electric Propulsion)-type system"]
-[8.97382926940918, 7.475558757781982, "[TT] Image Sensor Resolution of the Wide-angle camera = VGA resolution (640 x 480 pixels)"]
-[10.429888725280762, 1.220617651939392, "[FF] Evolutionary State of the HD 203949 = Red-giant phase"]
-[6.20257568359375, 5.951226234436035, "[TT] Quantity of the Battery Charge Modules = 3"]
-[14.144804000854492, 3.315765142440796, "[TT] Mass of the SAC = 0.74 kg"]
-[14.289450645446777, 3.336885690689087, "[TT] Mass of the REM = 3 kg"]
-[4.875669002532959, 3.0458970069885254, "[TT] Platform of the SES-14 = Eurostar E3000 EOR"]
-[8.009297370910645, 0.5091948509216309, "[FF] Wetness Percentile of the GRACE-FO satellites = Varies"]
-[7.502240180969238, 3.70869517326355, "[FF] Operation Mode of the NightPod = Semi-automatic mapping mode"]
-[3.3746814727783203, 6.368902683258057, "[TT] Dimensions of the Antenna = 73.5 x 73.5 m x 6.8 mm"]
-[5.327478885650635, 0.8623006343841553, "[FF] Satellite Launch Date of the Capella Space = December 2018"]
-[9.280792236328125, 7.388241767883301, "[TT] Resolution of the Panchromatic Band = 0.29 m"]
-[4.433504581451416, 7.858839511871338, "[TT] Downlink Frequency of the DCS = 1675 MHz"]
-[9.370098114013672, 2.3992345333099365, "[TT] Value of the Straylight = Less than 2%"]
-[6.926523685455322, -1.744164228439331, "[FF] Objective 3 Purpose of the Jason-CS = For determining tides, ocean circulation, climate change and sea level rise"]
-[8.190400123596191, -1.11958909034729, "[FF] Commercial Application of the ICESat-2 = Bathymetric Mapping"]
-[10.949316024780273, 7.556573390960693, "[TT] Swath Width of the TopSAR wide = > 350 km"]
-[6.391358375549316, -0.5760010480880737, "[TT] Orbit Duration of the International Gamma-Ray Astrophysics Laboratory = 1 Year"]
-[7.327922344207764, 4.53955078125, "[FF] Risk Assessment Parameters of the Collision Avoidance Strategy = Miss distance of 200 m radial and 1000 m in-track and cross-track"]
-[4.925102710723877, 3.416940689086914, "[TT] Manufacturer of the EC = TI"]
-[5.147171974182129, 0.6436155438423157, "[TT] Launch Date of the CanX-2 = April 28, 2008"]
-[9.699409484863281, 0.15632489323616028, "[FF] Location of the Parafoil Main Parachute = Packed around the drogue canister"]
-[9.012873649597168, 5.6305832862854, "[TT] Pointing Accuracy of the IPS = Within 2 arcseconds"]
-[4.724242210388184, -1.2302149534225464, "[FF] Strategic Cooperation Sign Date of the Beijing Space View = 5 Dec. 2017"]
-[4.940211296081543, 0.20955388247966766, "[FF] Original Launch Date of the Crew-1 = Oct. 31"]
-[9.634182929992676, 6.982255935668945, "[TT] SSS Spatial Resolution of the CIMR = 5 km"]
-[9.47746753692627, 7.939310073852539, "[TT] Optics Lens Field of View of the NEA Scout Camera = 27\u00ba"]
-[9.364617347717285, 6.351197242736816, "[TT] Moving Mirror Scan Time of the MSASI = 80 seconds"]
-[3.679377555847168, 4.653144359588623, "[FF] Radar Type of the SWIMSAT = Real-Aperture"]
-[7.804662227630615, 6.596563816070557, "[TT] Number of Channels of the MSU-MR Scanning Radiometer = 6"]
-[7.680327415466309, 6.762834072113037, "[TT] Exposure Time Range of the COR1 = (0.1, 1)"]
-[9.506656646728516, 2.774937629699707, "[FF] Type of the MinXSS-2 = Miniature X-ray Solar Spectrometer-2"]
-[6.644352912902832, -0.4024731516838074, "[TT] Measurement Duration of the Plane = Few seconds"]
-[14.114716529846191, 7.018281936645508, "[FF] Output Channels of the EPS = Raw battery voltage, regulated 3.3 V, 5 V, and 12 V channels"]
-[9.434762001037598, -1.1786136627197266, "[TT] Orbit Position of the BeiDou-1D = GEO, 58.75\u00ba E"]
-[4.829100608825684, 1.2831984758377075, "[FF] Conference Presentation Date of the Delfi-C3 = June 9-11, 2005"]
-[5.617386817932129, 6.708593368530273, "[TT] Downlink Contacts per Day of the IXPE = Up to 9"]
-[8.524352073669434, 7.574216842651367, "[TT] Array Size of the Camera Sensor = 578 x 576 array"]
-[8.141571998596191, 4.0004167556762695, "[FF] Function of the Internal Occulter = Blocks the direct light from the external occulter"]
-[6.043163776397705, 4.999087810516357, "[FF] Function of the AFSCN = Global data reception/communication"]
-[7.4194560050964355, 1.6083201169967651, "[FF] Presentation Date of the Global Climate Observing System (GCOS) = July 21, 1999"]
-[11.246941566467285, 5.354026794433594, "[TT] Plastic Scintillator Counters of the Veto System = 5 mm thick"]
-[3.4973089694976807, 4.56870698928833, "[FF] Payloads of the PAZ = Synthetic Radar Aperture (SAR) as primary and sole payload, and included an IGOR+ advanced GPS (Global Positioning System) receiver and corresponding antennas for precise orbit determination"]
-[9.170222282409668, 7.492292881011963, "[TT] Spatial Resolution of the GK-2A = 2 km for the 10 infrared channels and 1 km for 6 visible channels"]
-[6.1987433433532715, 2.127516508102417, "[FF] Presentation of the GPM = 14th European Space Mechanisms & Tribology Symposium \u2013 ESMATS 2011"]
-[9.116748809814453, 5.466611385345459, "[TT] Pointing or Orientation Time of the ADCS = Less than 24 hours"]
-[4.900733470916748, 0.6365868449211121, "[TT] Official Launch Date of the IMEO = Toward the end of the third quarter \u2014 or early in the fourth quarter \u2014 of this year"]
-[7.323217868804932, 2.5614309310913086, "[FF] Applications of the TRISHNA = Peat or coal fires mapping, geothermal exploration, possibly earthquake precursors, monitoring of volcanic activity, monitoring of snow and ice in polar regions, monitoring of glaciers and glacial high altitude lakes, deriving information on atmosphere and clouds"]
-[6.9950642585754395, -0.2674451172351837, "[TT] Start Time of the Solar Eclipse = 11:00 UTC"]
-[4.957573890686035, 0.08968456089496613, "[TT] End of Life Date of the FormoSat-1 = June 17, 2004"]
-[9.296438217163086, 3.196972370147705, "[FF] Function of the ASPIICS CCB = Control the Externally Occulted Solar Coronagraph Instrument"]
-[5.501314640045166, 7.1207709312438965, "[TT] Data Rate of the GEO LCT = 600 Mbit/s"]
-[9.90764045715332, -0.622530460357666, "[TT] Mission Altitude of the MicroSat-2a = 1125 km"]
-[6.092720031738281, -0.43507856130599976, "[TT] Funding Duration of the Participating Scientists = Three years"]
-[10.107758522033691, -1.3902270793914795, "[TT] Orbit Inclination of the DubaiSat-2 = 97.8\u00ba"]
-[7.778861045837402, 1.0549944639205933, "[TT] Spatial Resolution of the ROSE-L = 25 m2 for regional coverage, 50 m2 for global coverage"]
-[13.819109916687012, 2.648754358291626, "[TT] Launch Mass of the Falcon-9 Rocket = 13,620 kg"]
-[6.989473342895508, 3.569124221801758, "[FF] Test Results of the ALTIKA = Unknown"]
-[7.681745529174805, -0.7110661864280701, "[TT] URL of the ICESat\u20102 = https://doi.org/10.1029/2019JC015764"]
-[6.744652271270752, 5.943436622619629, "[TT] Quantity in PPU of the StrongARM SA1110 = 20"]
-[5.5699872970581055, 7.027886867523193, "[TT] Continuous Transmission of the LRDL = 10 byte/s"]
-[10.545822143554688, 2.8909966945648193, "[TT] Configuration of the SONATE nanosatellite = ASAP-L (light)"]
-[11.892027854919434, 5.422898769378662, "[TT] Size of the Instrument = 180 mm x 110 mm x 230 mm"]
-[1.7598413228988647, -2.0620031356811523, "[TT] Catcher Compartments of the Hayabusa-2 = Three compartments"]
-[5.531085014343262, 6.278294086456299, "[TT] PROMs Capacity of the DHS = 32 kbyte"]
-[6.938089847564697, 4.1229634284973145, "[FF] Purpose of the Team Miles = Demonstrate navigation in deep space using innovative plasma thrusters"]
-[4.240580081939697, 6.855823993682861, "[TT] Sensor of the ESAIL = VDES (VHF Data Exchange System)"]
-[11.739930152893066, 3.3136751651763916, "[TT] Thrust of the CNAPS = 10 mN/thruster"]
-[7.739339828491211, 8.419356346130371, "[TT] IR Bands of the CrIS = 3"]
-[8.201864242553711, -0.5490882992744446, "[FF] Collision Date of the A-74 iceberg = 19 May 2021"]
-[9.646315574645996, 5.500335693359375, "[FF] Functions of the Electronics = Detector and image data operation, calibration mechanism operation and temperature control, cryocooler operation and supervision"]
-[8.292709350585938, 1.3521419763565063, "[FF] Effect of the Rain Clouds = Changes ocean's temperature and salinity profiles, affects the circulation of deep water and can even affect global climate events like El Ni\u00f1o"]
-[9.263997077941895, 3.21486759185791, "[FF] Objectives of the EUI = 1. Provide EUV imagery with at least a factor 2 higher spatial resolution than currently available, to reveal the fine-scale structure of coronal features. 2. Provide full-disc EUV imagery of the sun to reveal the global structure and irradiance of inaccessible regions such as the \u201dfar side\u201d of the sun and the polar regions. 3. Study the connection between in-situ and remote-sensing observations"]
-[5.746243476867676, 4.037089824676514, "[TT] Reference of the Procedures = ID"]
-[11.35420036315918, 4.926631927490234, "[TT] Diameter of the LAGEOS = 60 cm"]
-[9.816707611083984, 4.738525390625, "[FF] Spin Frequency of the Myriade series spacecraft = Orbital Frequency"]
-[9.586179733276367, 8.764232635498047, "[TT] Number of IFOVs of the Spectrometer = 3 x 3 at 14 km diameter for each band"]
-[6.83632230758667, 4.7565999031066895, "[FF] Function of the Control Box = Provides containment for inadvertent flame and shatters"]
-[9.648490905761719, 5.193310737609863, "[TT] Stability of the ADCS = \u2264 5 x10-4 \u00ba/s"]
-[4.663244247436523, 5.426096439361572, "[FF] Function of the MEOLUTs = Recovering the message and locating the emergency beacon"]
-[6.113646507263184, 3.552619218826294, "[FF] Conference Location of the Space Plug-and Play Avionics = Los Angeles, CA, USA"]
-[6.026413917541504, -0.564004123210907, "[TT] Science Mission Duration of the RapidScat = Two years"]
-[9.942617416381836, 9.049131393432617, "[TT] Effective FOV of the Channel 5 = 30 x 67 km"]
-[3.225688934326172, 5.060572624206543, "[TT] Spatial Resolution of the SAR = 1-5 m"]
-[5.347348690032959, 7.957014560699463, "[FF] Frequency Range of the NewMag = 0.1 Hz to 1 kHz"]
-[9.273163795471191, 0.1293397843837738, "[TT] Length of the Tianhe = 16.6 meters"]
-[5.041849613189697, 1.2163385152816772, "[TT] Decommission Date of the GIOVE-A = 24 November 2021"]
-[9.05350112915039, 0.8581826686859131, "[FF] Venus Flyby Types of the V7GA = Resonant and non-resonant"]
-[9.668048858642578, 8.376708030700684, "[TT] FOV (Field of View) of the DST 35 = 1,87\u00ba"]
-[11.579253196716309, 5.155550956726074, "[TT] Spacer Length of the Cavity = 77.5 mm"]
-[3.7295212745666504, 4.352182388305664, "[FF] Application Topics of the Pol-InSAR = Forest, Agriculture, Snow and ice, Ship detection, Wind and waves, Geological mapping, Urban areas, Landslides/subsidence, Earthquakes/volcanoes, Development of new SAR techniques"]
-[10.05485725402832, -2.642853260040283, "[FF] Use of the NAND-Flash Technology = Storing larger quantities of data"]
-[7.801069259643555, 5.672192573547363, "[FF] Purpose of the LED target plate = Vision-based sensor system testing"]
-[4.246821403503418, 7.057016849517822, "[TT] Transmission Band of the Delft ground station = S-band"]
-[8.216986656188965, 0.7334105968475342, "[FF] Purpose of the GRNS = Detect, measure, and map Psyche\u2019s elemental composition"]
-[7.3056182861328125, 8.815585136413574, "[TT] Passband of the FUV channel = >125 nm"]
-[6.528810977935791, -0.7037256360054016, "[TT] Local Time of the Tandem-L = 6 h / 18 h"]
-[10.150684356689453, 5.56962776184082, "[TT] Cooling System of the Detector = Two-stage TEC (Thermoelectric Cooler)"]
-[6.287299156188965, 0.4341457486152649, "[FF] Data Collection of the ROSE-L = 24/7"]
-[9.471129417419434, 7.993413925170898, "[FF] Telescopes of the IPDA LIDAR = Two separate telescopes for the transmission (TX) and reception (RX) of the laser"]
-[6.560708999633789, 7.087510108947754, "[TT] Transmission x QE of the Instrument = 3%"]
-[9.240348815917969, -0.41408446431159973, "[TT] Apogee of the RBSP spacecraft = ~ 5.8 RE"]
-[8.418255805969238, 3.8189351558685303, "[FF] Imager of the IBEX = Energetic Neutral Atom Imager"]
-[9.533082962036133, 6.66991662979126, "[TT] Azimuth Resolution of the Wide fine = 7.7 m"]
-[1.6107455492019653, 3.759634494781494, "[TT] Reaction wheels of the BEESAT-1 = Yes"]
-[6.859671592712402, 3.7458572387695312, "[FF] Function of the Pelican Satellites = Distinguish road markings on the ground"]
-[7.157338619232178, 4.273434162139893, "[FF] Configuration of the SARAL spacecraft = Overview shown in Figure 2"]
-[11.626829147338867, 4.558177471160889, "[TT] Internal 'Bulk' Cohesion of the Didymos = 11 to 17 Pascals"]
-[7.983364105224609, 4.243200302124023, "[TT] Frequency of the Dark Current Measurements = Twice a day"]
-[9.038130760192871, 0.9198724031448364, "[FF] Imaging of the Parker Solar Probe = Night Side of Venus"]
-[7.2059197425842285, 4.8048624992370605, "[FF] Features of the Avionics Section = Interfacing port with the deployer, a camera, burn wire, avionics boards, central inflation connector system, CGG (Cold Gas Generator), solenoid valve"]
-[5.2363200187683105, 6.7352986335754395, "[TT] Data Downlink of the AstroBus-L = 560 Mbit/s"]
-[4.372848987579346, 4.299907684326172, "[TT] Number of Spacecraft of the COSPAS-SARSAT = 4"]
-[5.7507004737854, 4.857884883880615, "[TT] Method of the Satellite Relay = Relay via satellite"]
-[9.90550708770752, 8.212459564208984, "[TT] Effective Focal Length of the WPM = 149.85 mm"]
-[5.497947692871094, 5.012917995452881, "[TT] On-board Computer of the IOD-1 GEMS = CSL On-board Computer (OBC) with integrated GPS receiver"]
-[6.507503986358643, 5.987308025360107, "[TT] Mode of the Radio = Cyclic on/off cycle"]
-[5.300242900848389, 7.1186347007751465, "[TT] Uplink Baud Rate of the CMC Transceiver = 1200 baud"]
-[5.349708557128906, 6.4009528160095215, "[TT] Bus Speed of the RAD750 SBC = 66 MHz"]
-[6.9943647384643555, 0.8101575374603271, "[FF] Presentation Date of the Gravity Probe B = 23-24 July 1992"]
-[7.846604824066162, 8.756351470947266, "[TT] Resolving Power of the O2 A-band channel = > 17,000"]
-[5.699693202972412, -0.9026170969009399, "[FF] Design Competition Duration of the EDC = One year"]
-[11.228507041931152, 2.8261477947235107, "[TT] Mass of the PSSCT Nanosatellite = 6.5 kg"]
-[6.135560989379883, 6.8201704025268555, "[FF] Compression Type of the DHU = Online lossless and lossy"]
-[7.139743804931641, 3.832336902618408, "[FF] Mission Objectives of the PROBA-3 = Demonstrate formation flying technologies, obtain scientific results from a coronagraph science payload, including also dedicated rendezvous demonstration"]
-[6.384961128234863, 2.5678601264953613, "[TT] Chief Scientist of the QUESS = Jianwei Pan from the University of the Science and Technology of China"]
-[9.497013092041016, 5.039373397827148, "[TT] Stabilization of the AOCS = Three-axis stabilized within 10 arcsec"]
-[9.734619140625, -0.5681425333023071, "[TT] Orbit Altitude of the SuperView-1 01 and Superview-1 02 = 530 km"]
-[5.629035949707031, 2.8064961433410645, "[TT] Development Partner of the Land Information System = NASA's Goddard Space Flight Center"]
-[5.82567024230957, 3.1943886280059814, "[FF] Number of Spaceships of the SpaceX Crew Dragon = 2"]
-[6.623387813568115, 4.64886999130249, "[TT] Relative Navigation of the PRISMA = GPS- and FFRF-based"]
-[5.712723255157471, 3.1980674266815186, "[FF] Ownership Stake of the Indra = Approximately 10.5%"]
-[9.980046272277832, -1.504224419593811, "[TT] Orbit Inclination of the STS-85 = 51.6\u00ba"]
-[8.87986946105957, 0.9762744307518005, "[TT] Project Scientist of the Parker Solar Probe = Nicola Fox"]
-[9.499282836914062, 0.99770587682724, "[TT] Reentry Speed of the Orion Capsule = 32,000 km/hr"]
-[6.294209003448486, 1.2601124048233032, "[TT] Date of the Electrodynamic Tethers for Space Propulsion = Jan. 12-15, 1998"]
-[5.5309739112854, -1.868590235710144, "[TT] Manufacturer of the KOMPSAT-1 = KARI (Korea Aerospace Research Institute)"]
-[7.138401031494141, 5.778695106506348, "[FF] Stability of the DSAC = Orders of magnitude more stable than current spaceborne navigation clocks"]
-[9.580819129943848, 0.15484203398227692, "[TT] Perigee of the PROBA-3 = 600 km"]
-[10.262453079223633, 3.9984946250915527, "[TT] Family of the TEMBOTM EMC = Booms"]
-[9.54927921295166, 8.300432205200195, "[TT] Wide-Angle Video Camera Field of View of the MEIDEX = 60\u00ba"]
-[5.184718132019043, 5.996199131011963, "[FF] Performance of the SpaceWire = Not provided"]
-[10.409690856933594, 1.6750568151474, "[TT] Pulsation Patterns of the Delta Scuti stars = Regular"]
-[8.188590049743652, 4.781071186065674, "[FF] Calibration Device Quantity of the OMPS = Two diffusers for each sensor"]
-[5.9827423095703125, 7.077179908752441, "[TT] User Data Rate of the Optical RTN service = 600 Mbit/s"]
-[11.963635444641113, 5.037077903747559, "[TT] Size of the CIRC = 110 mm x 180 mm x 230 mm"]
-[10.910202026367188, 5.643682479858398, "[TT] Impact Punctures of the Eureca = 71 in the outer layer of the thermal blankets"]
-[6.888418674468994, 4.61086893081665, "[TT] Location of the Subsystem Electronics Packages = Equipment decks/panels"]
-[9.78772258758545, -0.5540788769721985, "[TT] Orbit Altitude of the IRIS = 620 km x 670 km"]
-[7.107752323150635, 6.6837286949157715, "[TT] False Event Rate of the GLM = Below 100 events/s"]
-[4.355353355407715, 6.905972003936768, "[TT] Communication System of the TanDEM-X = X-band inter-satellite link"]
-[7.5964531898498535, -2.5129172801971436, "[TT] Observation Start Date of the GOLD = October 2018"]
-[7.8439812660217285, 2.1015701293945312, "[FF] Calibration of the Ocean Color and Temperature Scanner (OCTS) = Unknown"]
-[14.45781135559082, 6.789883136749268, "[TT] Full Charge Voltage of the Li-ion battery = 29.4 V"]
-[7.317246913909912, 3.2550671100616455, "[FF] Definition of the Level 3 = Projection of the future status"]
-[9.980179786682129, -1.4919337034225464, "[TT] Orbit Inclination of the Dragon = 51.6\u00ba"]
-[5.639358043670654, 0.4256146550178528, "[FF] Arrival Date of the ATLAS = May 2014"]
-[6.4787516593933105, 5.948509216308594, "[FF] Application of the Optical Terminal = Support a user forward and/or return relay service, Support user-to-user relays"]
-[8.740948677062988, 5.450070858001709, "[FF] Conductive Surface Area Requirement of the m-NLP = Not provided"]
-[6.545933246612549, 6.8033447265625, "[TT] Duty Cycle of the TR Module = ~ 7%"]
-[5.671385765075684, 6.332726001739502, "[TT] On-board data storage of the First DMC generation = SSDRs (Solid State Data Recorders) capable of storing up to 1.5 GByte of imagery"]
-[12.882710456848145, 5.53774356842041, "[TT] Number of Panels of the Collector Arrays = 4"]
-[5.900317192077637, 0.8574471473693848, "[FF] Camera Deployment Date of the TechDemoSat-1 = 31 May 2019"]
-[4.756908893585205, 1.1108310222625732, "[TT] Communication Loss Date of the STEREO-B = Oct. 1, 2014"]
-[6.42084264755249, 4.708063125610352, "[FF] Function of the Mission Data Archiving System = Manages the archiving and backup of all processed image data"]
-[6.229584693908691, 4.763638496398926, "[FF] Type of the Onboard Computer = Custom"]
-[9.287134170532227, 1.8455349206924438, "[FF] Presentation Date of the Robot Harpoon and Net System = 5 April 2018"]
-[6.333958148956299, 2.6920652389526367, "[TT] Manufacturer of the GOLD = University of Colorado Boulder\u2019s Laboratory for Atmospheric and Space Physics (LASP)"]
-[4.332158088684082, 1.4287683963775635, "[TT] Position in Constellation of the GCOM-W1 = Prior to the Aqua spacecraft"]
-[6.107967853546143, 1.3533239364624023, "[FF] Presentation Date of the Swarm = March 20-24, 2017"]
-[13.981401443481445, 3.9265785217285156, "[TT] Instrument Mass of the JPL Microwave Radiometer = 7 kg"]
-[8.27188777923584, 3.2395246028900146, "[FF] Observing Capability of the Ground-based Telescopes = Decreases as air mass increases at low altitudes"]
-[5.532594680786133, 5.5147857666015625, "[TT] Magnetic Onboard Recorders of the SPOT-4 = Operational"]
-[4.523343563079834, 6.363617897033691, "[TT] Uplink Beacon of the RF Communications = CW (Continuous Wave) UHF beacon"]
-[13.531994819641113, 5.729717254638672, "[FF] Power Source of the Spacecraft Module = Solar arrays and three nickel-hydrogen batteries"]
-[10.836801528930664, -0.28316208720207214, "[FF] Effective Baselines of the TanDEM-X = Required for DEM acquisition at different latitudes"]
-[5.017589092254639, 6.74605131149292, "[FF] Data Transmission of the CubeRRT = On-board filtering requires 99% less data to be downlinked"]
-[4.512739658355713, -0.8765319585800171, "[FF] Launch of the CRS-12 Dragon = Unknown"]
-[9.467689514160156, 8.960886001586914, "[TT] GSD of the Iris Video Camera = Resampled to 1 meter"]
-[9.02947998046875, 5.110310077667236, "[FF] Engineering Challenges of the GP-B probe = Measurement requirements of extremely minute changes in the orientation of gyroscopes"]
-[8.783780097961426, 5.952081203460693, "[TT] Range of Values of the Surface type = 12 types"]
-[9.005626678466797, 8.134079933166504, "[TT] IFOV/line (pixels/scan line) of the TOU = 31"]
-[6.6578898429870605, 3.7054710388183594, "[FF] Resonant Frequency of the 3D Printed Polymers = Unknown"]
-[3.4794962406158447, 6.456768989562988, "[TT] Access Width of the Antenna = 165 km"]
-[6.068566799163818, 0.9581128358840942, "[FF] Purpose of the Kanopus-V-IK = Earth-observation"]
-[10.0211181640625, 5.595771789550781, "[TT] Temperature Stabilization of the UVNS = Better than 1oK during one orbit"]
-[6.0346150398254395, -0.051392603665590286, "[TT] Power On Time of the MWR = 81 days"]
-[5.176512718200684, 4.656777858734131, "[TT] Ground Command Acceptance of the TT&C radio = Yes"]
-[4.4831671714782715, 3.1169302463531494, "[FF] Location of the Ground Segment = Belgian user Support and Operation Centre (B.USOC) in Brussels, Belgium"]
-[8.019622802734375, 5.142734527587891, "[FF] Calibration Step of the Sensor Counts to Radiance Conversion = May be applied for calibration"]
-[13.388134002685547, 6.824358940124512, "[TT] Power of the Spacecraft = 1400 W"]
-[12.120802879333496, -0.42978397011756897, "[TT] Extended Mission Duration of the TESS = Until September 2022"]
-[5.09548807144165, 1.8870911598205566, "[TT] Operational Status of the OFEQ-3 = Operational as of 2002"]
-[13.631610870361328, 6.969761371612549, "[TT] Power Topology of the Bus = Direct Energy Transfer (DET)"]
-[9.187016487121582, -0.38110873103141785, "[TT] Apogee of the Explorer 36 = 1570 km"]
-[5.945322513580322, 0.6807273626327515, "[FF] Discovery Date of the Andrew Vanderburg, Pamela Rowden, Steve Bryson, Jeffrey Coughlin, Natalie Batalha, Karen A. Collins, David W. Latham, Susan E. Mullally, Knicole D. Col\u00f3n, Chris Henze, Chelsea X. Huang, and Samuel N. Quinn = 28 February 2020"]
-[3.109212636947632, 2.1320087909698486, "[FF] Operational Experience of the Copernicus POD Service = Not provided"]
-[9.000685691833496, 4.390946388244629, "[TT] Sensors of the ADCS = Redundant set of sun sensors and magnetometers"]
-[5.170199394226074, 7.052778720855713, "[TT] Data Rate of the TT&C Downlink = 38.4 kbit/s"]
-[9.449511528015137, -1.1477160453796387, "[TT] Orbit Position of the BeiDou-1B = GEO, 80\u00ba E"]
-[4.830763339996338, 0.6402988433837891, "[TT] Launch Date of the Resurs-O1 = Jun 13, 2012"]
-[8.834039688110352, 5.690994739532471, "[TT] Knowledge of the 0.002\u00ba (3\u03c3) = 0.002\u00ba (3\u03c3)"]
-[7.015533447265625, 1.8225674629211426, "[FF] Delay Announcement Date of the Orbiting Carbon Observatory-2 = Feb. 10, 2012"]
-[8.76239013671875, 0.1434207409620285, "[TT] Matchpoint Maneuver Altitude of the OSIRIS-REx = Approximately 246 ft (75 m)"]
-[8.882333755493164, 5.8300461769104, "[TT] Nominal Pointing Range of the Guider = \u00b130 arcsec"]
-[13.944575309753418, 7.050785064697266, "[TT] Output Voltage of the High Voltage Power Supplies = Sweeping (lookup table-driven) voltages for the inner hemisphere, electrostatic deflectors and spoiler electrostatic attenuator"]
-[8.627224922180176, 2.0940043926239014, "[TT] Data Swath of the SeaWinds = Continuous 1800 km swath, centred about nadir"]
-[7.211918830871582, 4.733639717102051, "[FF] Ground Commanding of the Spacecraft = Uploading Steering Coefficients and Bias Commands"]
-[9.345247268676758, 3.2737045288085938, "[FF] Nitrogen Enrichment of the Sun = Unknown"]
-[10.008322715759277, 2.8845062255859375, "[TT] Launch Date of the R3 CubeSat = December 16th, 2018"]
-[9.020525932312012, -0.21447348594665527, "[TT] Altitude of the Meteor-M-2 = 825 km"]
-[4.319201469421387, 6.3282694816589355, "[FF] Function of the Tether = Antenna"]
-[7.408942222595215, 4.475305557250977, "[FF] Use as Transfer Radiometer of the S-NPP VIIRS = Unknown"]
-[4.162671089172363, 3.7038986682891846, "[FF] Oxygen Variation of the Galileo probe = Up to 7 percent"]
-[5.811732292175293, 4.566423416137695, "[FF] Use of the ROBUSTA ground station = Future GENSO (Global Educational Network for Satellite Operation) use"]
-[8.602564811706543, 6.115941524505615, "[TT] Accuracy of the SA Drive Mechanism = > 1%"]
-[4.901989459991455, 6.427932262420654, "[TT] Receiver Frequency of the CTECS-A = L2"]
-[8.421730041503906, 7.525527000427246, "[TT] Detector Type of the NINA = Silicon"]
-[8.782848358154297, 2.87549090385437, "[FF] Mission Objective of the THEMIS Probes = Determine what physical process in near-Earth space initiates the auroras"]
-[9.514826774597168, 6.204029560089111, "[TT] Angle of Incidence of the Stripmap = 20\u00b0 - 50\u00b0"]
-[7.129122734069824, 3.2162926197052, "[FF] Data Source of the GEOS-FP = Satellite, aircraft, and ground-based observing systems"]
-[11.916918754577637, 4.661485195159912, "[TT] Size of the HawkEye = 10 x 10 x 10 cm"]
-[7.957237243652344, 7.392359733581543, "[TT] Modulation of the Imager = PCM"]
-[10.016549110412598, 7.920679569244385, "[TT] MCP Optics per Telescope Module of the LWFT instrument = Approximately 60"]
-[3.849277973175049, 4.462770462036133, "[TT] Operation Status of the RADARSAT-2 = Nominal"]
-[4.241307735443115, 7.105350494384766, "[TT] RF Communications Band of the ETS-VIII = S-band"]
-[5.535177707672119, 6.894414901733398, "[TT] Pulsation Speed of the HD 31901 = Sped up by 54,000 times"]
-[6.984714984893799, 1.6879286766052246, "[TT] Imagery Coverage of the FormoSat-2 = ~8 times the land area of the Earth"]
-[4.720954418182373, -0.7933827638626099, "[TT] Launch Time of the Crew Dragon = 8:02 p.m. EDT"]
-[9.93203353881836, -0.2500523030757904, "[TT] Orbit Altitude of the Starlink Satellite = 550 km"]
-[9.389181137084961, 4.731904983520508, "[TT] Structure of the MTG-S Spacecraft = Two-winged satellite configuration"]
-[5.355260372161865, 4.087744235992432, "[TT] Number of Satellites in Orbit of the Corvus-BC 3 = 3"]
-[8.906095504760742, 5.700273036956787, "[TT] Pointing Accuracy of the ADCS = 0.02\u00ba (3\u03c3)"]
-[8.040422439575195, 9.268471717834473, "[TT] Wavelength of the Liquid water = 3.106 \u00b5m"]
-[5.4543328285217285, 3.5134365558624268, "[TT] Host of the GOLD = SES-14, a commercial communications satellite"]
-[5.527466773986816, 4.240515232086182, "[TT] Bus Platform of the Restore-L = 1300-class"]
-[3.799578905105591, 7.171584606170654, "[TT] Antenna Gain (dB) of the Antenna = >30"]
-[9.247628211975098, -0.41716697812080383, "[TT] Apogee Height of the TESS = 400,000 km"]
-[6.2357258796691895, 3.4564919471740723, "[FF] Expertise of the Artificial intelligence solutions = Based on space technology"]
-[6.115015506744385, 0.8182530403137207, "[TT] Image Capture Date of the CaSSIS = 15 January 2019"]
-[8.105053901672363, 4.436668395996094, "[FF] Usage of the CST Microwave Studio\u00ae = Electric field calculation"]
-[13.436768531799316, 2.847273111343384, "[TT] Mass of the Sloshsat-FLEVO = 50-150 kg"]
-[9.51457405090332, 1.0501292943954468, "[TT] Speed of the Proximity Flyby = 800 m/day"]
-[5.8289031982421875, 1.3838063478469849, "[FF] Conference Date of the MTG Satellites = June 22-24, 2010"]
-[6.984097003936768, 8.077642440795898, "[TT] Noise Level of the RASAT = Relatively low"]
-[8.934555053710938, 4.345761299133301, "[TT] Tracking Capability of the Hinode = Continuous tracking of sunspots with high spatial resolution for several days"]
-[7.6505327224731445, -2.3521134853363037, "[FF] URL of the GOLD = http://www.nasa-usa.de/mission_pages/sunearth/missions/mission_gold.html"]
-[6.021853923797607, 6.0213727951049805, "[TT] Operating Mode of the Antenna = SS-TDMA"]
-[9.098751068115234, 7.758512020111084, "[TT] Requirement Value of the MTF = 8%(PAN) 12%(MS)"]
-[6.9643235206604, 7.213022708892822, "[TT] Quantity of the Corner-cube Emitter (laser) and Sensor = 1"]
-[10.712370872497559, 5.596546173095703, "[TT] Properties Below Critical Temperature of the TEMBOTM EMC = Comparable to the conventional \"rigid\" composite structures"]
-[5.3306145668029785, 2.2253730297088623, "[FF] Mission Type of the MOMS = EO"]
-[6.270572662353516, 8.186342239379883, "[TT] No of bands/channels of the VIRR = 10"]
-[8.592910766601562, 4.409933567047119, "[FF] Operation Modes of the ABEX = Sun-pointing Idle mode, Earth-pointing Communications modes, Safety and Reaction Wheel Desaturation modes"]
-[7.660218715667725, 5.752151966094971, "[FF] Function of the Closed Loop tracking mode = Automatic echo recognition and tracking"]
-[5.532427787780762, 5.4933295249938965, "[TT] Interface Type of the HMA Project = Machine-to-machine"]
-[13.944207191467285, 4.032596588134766, "[TT] Instrument Mass of the Vector Magnetometer = 2.1 kg"]
-[10.301541328430176, 4.0573039054870605, "[TT] Booms of the Spacecraft = 8"]
-[6.271032810211182, 7.110082626342773, "[TT] Compression Mode of the BAQ = 4 bit, 2 bit, and no compression with or without the improved compression mode"]
-[12.187376022338867, 2.9882662296295166, "[TT] Type of the Hydrazine Propellant System = Hydrazine"]
-[5.718903541564941, 2.4213528633117676, "[FF] Land Coverage of the LAPAN-A3/IPB = 1/3 of the country is land mostly covered by forest and agriculture"]
-[9.69483757019043, -0.012386428192257881, "[TT] Trigger Altitude of the Parachute = About 5 km"]
-[14.243440628051758, 3.240013599395752, "[TT] Mass of the CCE = 3.8 kg"]
-[7.113972187042236, 2.867978096008301, "[FF] Mission of the NAOMI instrument = High resolution missions in Earth observation"]
-[7.870858669281006, 5.783798694610596, "[FF] Features of the Optical bench = Ultra-stable fiber injector (FIA), beam fine steering mirror (FSM), imaging optics, photoreceiver frontends (PRFs) with the quadrant photodiodes"]
-[7.596773624420166, 6.970925807952881, "[TT] Data Delivery of the SWAP = About 70 images per contact, delivered within 30 minutes to the SOC"]
-[6.143301963806152, 5.253398895263672, "[TT] Features of the DUTHSat = M-NLP"]
-[7.420457363128662, 3.236104965209961, "[FF] Purpose of the TROPOMI and TEMPO = Provide improved satellite observations for health studies beneficial to societal concerns"]
-[10.222111701965332, 7.518313407897949, "[TT] Telescope Type of the OGS = Cassegrain reflector"]
-[2.285550117492676, 2.769315242767334, "[TT] Co-PI of the EPI-Lo = Mark Wiedenbeck"]
-[7.8030595779418945, 4.97542142868042, "[FF] Purpose of the DSX = Test methods to control the orientation of very large structures in space"]
-[5.509857654571533, 6.393398284912109, "[TT] SD Card Capacity of the On-board data handling = 2 GB"]
-[3.5398285388946533, 6.512589454650879, "[FF] Antenna of the Instrument = Parabolic, Aperture Diameter = 2 m, Conical Scan"]
-[8.149394035339355, 5.100467681884766, "[TT] Calibration of the CarbonSpec instrument = Spectrometric calibration, Radiometric calibration"]
-[6.623765468597412, 6.613737106323242, "[FF] Technology of the EDRS = Laser communication technology"]
-[3.770034074783325, 2.5025105476379395, "[TT] GMDSS Service Provider of the Iridium = Iridium"]
-[4.681116104125977, 0.3093985915184021, "[TT] End of Life Date of the OSCAR-QUBE = 29 August 2026"]
-[4.853193759918213, 7.9124345779418945, "[TT] Clock Frequency of the AIM = 48 MHz"]
-[9.461684226989746, 6.0617852210998535, "[TT] Incidence Angle Range of the OBRC instrument = 25-48\u00ba"]
-[16.49692153930664, 3.5915369987487793, "[FF] Technology of the OneWeb = Progressive pitch technology"]
-[13.636171340942383, 5.81195068359375, "[TT] Power of the Solar Panels = 14 W (max)"]
-[5.60986852645874, 6.3496856689453125, "[FF] Memory Capacity of the TARANIS Instrument Analyzers = Includes memory to store high resolution data for a time interval including the event detection time"]
-[11.722817420959473, 7.513091087341309, "[FF] Observation Frequency of the Megha-Tropiques = Up to 6 overpasses per day"]
-[5.000146865844727, 8.328609466552734, "[TT] RF Bandwidth (MHz) of the Antenna = 400"]
-[7.250516891479492, 2.583526372909546, "[FF] Edition of the Observation of the Earth and Its Environment: Survey of Missions and Sensors = 4th"]
-[13.137264251708984, 7.266833305358887, "[TT] Power Consumption of the UVS = 1 W"]
-[4.561788558959961, -2.7922520637512207, "[TT] Frequency of the PMI = 6.8 to 150 GHz"]
-[4.381849765777588, 7.424705982208252, "[TT] Downlink Frequency of the Payload = Ka-band"]
-[8.46057415008545, 1.7762092351913452, "[TT] Cloud Water Accuracy of the Lower atmosphere = 0.10 kg m -2"]
-[7.838259696960449, 1.2534265518188477, "[FF] Productivity Decline of the Cropland = 15 percent in 2019 from 2018 levels"]
-[13.831160545349121, 2.7047338485717773, "[TT] Mass at Launch of the Spacecraft = 2388 kg"]
-[6.396224021911621, 1.3952642679214478, "[TT] Launch Year of the COSMO-SkyMed = 2007"]
-[4.923685550689697, 0.7702215313911438, "[TT] CCD Delivery of the Teledyne e2v = Mid March"]
-[7.3199028968811035, 0.2335009127855301, "[TT] Departure Date from Bennu of the OSIRIS-REx = May 10"]
-[9.067036628723145, 5.131943702697754, "[TT] Range of the Rate gyro = \u00b15\u00ba/s"]
-[4.7415080070495605, -1.8216967582702637, "[FF] Launch Date of the Chang'e-1 = Oct. 24, 2007"]
-[12.055709838867188, -0.20244790613651276, "[TT] Imaging Coverage of the TESS = 75% of the starry sky"]
-[10.599275588989258, 2.2133357524871826, "[FF] Anniversary of the X-ray Astronomy = 50th anniversary in June 2012"]
-[7.6741204261779785, 0.7131510376930237, "[FF] Propellant of the Lunar Flashlight = \"Green\" propellant"]
-[7.6649370193481445, 8.786993980407715, "[FF] Function Shape of the ISRF = Quasi-trapezoidal for almost all bands and quasi-triangular for the LR 500\u2013697 nm bands"]
-[8.00657844543457, 1.0668407678604126, "[TT] Volumetric Soil Moisture Products Spatial Resolution (Regional Scale) of the ROSE-L SAR = 25 m2"]
-[8.010269165039062, 2.666152000427246, "[TT] Instruments of the AIM = CIPS (Cloud Imaging and Particle Size) high spatial resolution camera and SOFIE (Solar Occultation For Ice Experiment)"]
-[7.519101142883301, -0.14657217264175415, "[TT] Final Parking Time of the Philae = 17:31:17 GMT"]
-[5.258363246917725, 1.2813810110092163, "[FF] Conference Date of the SPARCS = Aug. 4-9, 2018"]
-[10.20382022857666, 3.1639368534088135, "[FF] Type of the Cube and nanosatellites radios = Unknown"]
-[7.080657482147217, 3.031984329223633, "[FF] Interface Type of the GS PD element = Sectorized cloud and moisture imagery directly to the NWS via the AWIPS interface"]
-[6.5098466873168945, 8.34149169921875, "[TT] Channels of the POLDER = 15"]
-[7.5958685874938965, 2.2357633113861084, "[FF] Purpose of the SLSTR = Retrieve vegetation information"]
-[5.908495903015137, -0.4519249498844147, "[TT] Maximum Mission Duration of the PROBA-3 = About 2.5 years"]
-[7.849337100982666, 7.455324649810791, "[FF] Data Usage of the TRUTHS = Global hyperspectral data"]
-[11.003497123718262, 5.790744304656982, "[TT] CsI Shield Thickness of the GRS = Approximately 3 cm"]
-[3.2050113677978516, 4.995255470275879, "[TT] Range Coverage of single/dual-pol. in fine mode of the ALOS-2 SAR = 70 km"]
-[13.451577186584473, 2.9204347133636475, "[TT] Total of the Satellite = 500 kg"]
-[5.981106281280518, 1.401313066482544, "[FF] Conference Date of the Earth Observation Constellation Satellites = 14-16 May 2013"]
-[8.807388305664062, 4.64522123336792, "[TT] Correction Factor of the Sun and Galactic Glint = 0.98"]
-[8.190110206604004, -0.9413429498672485, "[FF] Freeboard of the Sea Ice = Total height of the snow cover and sea ice that floats above the ocean"]
-[5.780732154846191, 7.162230968475342, "[TT] Data Rate of the ASPOC = 0.13 kbit/s"]
-[4.253903865814209, 0.7623754739761353, "[TT] Launch Date of the EDRS = Jan 28, 2013"]
-[5.920196533203125, -0.5451276302337646, "[TT] Operational Service Life of the WNISAT-1 = 2 years"]
-[6.251011371612549, -0.5678579807281494, "[FF] Duration of the Spaceflight\u2019s 64-satellite rideshare mission = Five hours"]
-[8.457300186157227, 2.1318936347961426, "[FF] Signal Saturation of the CYGNSS = Not saturate, even at surface wind speeds up to 60 m/s"]
-[10.400104522705078, 2.131746768951416, "[TT] Resolution of High-Energy X-ray Background of the NuSTAR = 35 percent"]
-[6.682492733001709, 1.9104883670806885, "[FF] URL of the HITSAT = http://astronomy.activeboard.com/forum.spark?aBID=58381&p=3&topicID=18351197&page=1&sort=newestFirst"]
-[9.208780288696289, 5.287055015563965, "[TT] Pointing Accuracies of the AOCS = Pitch and roll = 0.2\u00ba, yaw = 0.4\u00ba"]
-[10.280356407165527, 5.322456359863281, "[FF] Function of the Radiator Thermal Shield = Shields the cryogenic radiator from the warm Earth and all direct sun"]
-[7.796335220336914, 4.188604354858398, "[FF] Description of the 6DOF Control = 6 Degree of Freedom control with thrusters"]
-[5.066225051879883, 5.902702808380127, "[FF] Compatibility of the EWC31 S-band equipment = Fully CCSDS compatible with ranging and coherent transmission capabilities"]
-[8.791176795959473, 1.9227782487869263, "[TT] Windspeed of the Jason-2 = 1.6/1.5/1.5 m/s"]
-[12.085065841674805, 6.26826810836792, "[TT] Identified Electrons and Positrons of the AMS = 10 million"]
-[8.600825309753418, 2.7603299617767334, "[TT] Range of measurements of the Atmosphere = 0-5 kg/m2"]
-[9.148651123046875, -0.5035458207130432, "[TT] Orbit Apogee of the BX-1 = 296 km"]
-[3.6097147464752197, -0.7869687676429749, "[TT] Reference Orbit of the Spacecraft = SSO (Sun-synchronous Orbit)"]
-[6.451013565063477, -0.9345808625221252, "[TT] MLST Excursion of the Envisat = 10 minutes"]
-[9.826796531677246, 8.529974937438965, "[TT] IFOV of the Satellite = Very large"]
-[4.5605950355529785, 3.13954758644104, "[TT] Structure and Power Systems Provider of the SloshSat-FLEVO = Dutch Space, Leiden, The Netherlands"]
-[8.23844051361084, 7.540033340454102, "[TT] Detector of the SAGE-III = CCD and photodiode"]
-[14.280214309692383, 3.2458317279815674, "[TT] Mass of the HEED = 2.2 kg"]
-[13.979843139648438, 7.132818222045898, "[TT] Voltage Output of the PSU = 3.3 V"]
-[7.26160192489624, 4.728240013122559, "[TT] Mounting Location of the Bottom Plate = Internal components"]
-[5.216576099395752, -1.2260282039642334, "[TT] End of Life Date of the Kondor-E = 27 June 2019"]
-[13.625450134277344, 5.724725246429443, "[TT] Power Source of the PhoneSat-2.5 = Solar cells"]
-[3.178737163543701, 2.3355181217193604, "[FF] Mission Capability of the Sentinel 2 = Tropical coral reef mapping and coral bleaching detection"]
-[9.421309471130371, 7.375356197357178, "[TT] Image Resolution of the BlackSky Pathfinder-1 = ~2 m/pixel"]
-[3.813291311264038, 7.927046298980713, "[TT] Modulation of the X-band Transmitter = QPSK/OQPSK (Quadrature Phase Shift Keying / Offset Quadrature Phase Shift Keying)"]
-[10.363288879394531, 7.3256516456604, "[TT] Telescope Primary Mirror Aperture Diameter of the WV-3 Imager = 110 cm"]
-[5.222466945648193, 2.325894832611084, "[TT] Mission Type of the AstroSat = Non-EO"]
-[6.406996250152588, 0.6556746959686279, "[FF] Launch Date of the Landsat 9 = 16 September 2021"]
-[10.906773567199707, 3.073253870010376, "[TT] Magnetic-Gravitational Stabilization and One-Axis Orientation System Mass of the Microsatellite = 2.7 kg"]
-[7.707935333251953, 0.933155357837677, "[FF] Background Components of the Optical Receiver = Detector dark current, detected thermal emission of the receiver, detected solar illumination reflected from the lunar surface"]
-[6.611690044403076, 2.181987762451172, "[FF] URL of the WorldView Legion = https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=4709&context=smallsat"]
-[6.244413375854492, 8.122416496276855, "[TT] Channels of the MWRI = 10 channels"]
-[7.42797327041626, 4.271641254425049, "[FF] Sensor Complement of the SAC-D = Unknown"]
-[5.048183441162109, 6.343628883361816, "[TT] Remote Operation of the TUC Transponder = Yes"]
-[10.90340805053711, 7.521660804748535, "[TT] Swath Width of the SPOT 1-5 = 60 km"]
-[9.682299613952637, 7.027584552764893, "[TT] Floating Distance of the Orihime = About 200 mm"]
-[5.567187786102295, 3.775697946548462, "[TT] New Factory Production Capacity of the Satellogic = 25 satellites a quarter"]
-[8.583468437194824, 0.30950167775154114, "[TT] Travel Distance of the SeaSat = 157 km"]
-[8.053177833557129, 5.447397708892822, "[FF] Description of the At-Sensor-Radiance Product (L1B) = The product is radiometrically calibrated, spectrally characterized, geometrically characterized, quality controlled and annotated with preliminary pixel classification (usability mask)"]
-[9.91893196105957, 4.311443328857422, "[TT] Magnet Temperature of the AMS-02 = 1.8\u00ba C above absolute zero"]
-[8.619479179382324, 2.665698528289795, "[FF] Purpose of the CDE = Measure the temporal variability of meteoric material"]
-[6.156139373779297, 8.502557754516602, "[TT] Polarimetric Capability of the 10, 18, and 36 GHz channels = V, H, 3rd and 4th Stokes"]
-[4.495034217834473, 7.8415327072143555, "[TT] Data Collection Frequency of the DCS = UHF (~401 MHz)"]
-[7.5443620681762695, 6.87513542175293, "[TT] Operational Cadence of the Instrument = Rotate to 120\u00ba in < 2 minutes to nadir view"]
-[6.228323459625244, 8.589481353759766, "[TT] Polarization of the High Resolution Spotlight = Single or dual"]
-[6.326429843902588, 4.7924065589904785, "[FF] Function of the SGR-ReSI = Collect more data and allow processing on-board"]
-[11.342394828796387, 5.869748592376709, "[TT] Material of the Platform = Machined aluminum"]
-[13.331385612487793, 7.7919816970825195, "[TT] Output Power of the Ku-band transmitter = 200 mW"]
-[4.930929183959961, 3.4402501583099365, "[TT] Manufacturer of the Composite Dispenser = RUAG Space in Sweden"]
-[7.945239067077637, 8.602202415466309, "[TT] IR Bands Wavelength of the Instrument = 0.86 \u00b5m to 13.3 \u00b5m"]
-[6.380094528198242, -1.1458600759506226, "[TT] LTAN of the KOMPSAT-6 = 6 hours"]
-[5.363293170928955, 4.0870890617370605, "[TT] Platform Type of the Satellite Vu = DarkCarb satellite bus"]
-[12.806321144104004, 3.135348320007324, "[TT] Maximum Sulphur Dioxide Content of Ship Fuels of the International Shipping Emission Regulations = 0.5%"]
-[13.828795433044434, 2.671882152557373, "[TT] Launch Mass of the IRNSS-1E = 1425.4 kg"]
-[10.030875205993652, 7.896934509277344, "[TT] Telescope Type of the R3 spacecraft = Refractive"]
-[14.189481735229492, 3.311225175857544, "[TT] Estimated Mass of the Subarray = 80 gram"]
-[9.541886329650879, 3.8989851474761963, "[FF] Omnidirectionality of the Vector Magnetometer = Ensured by the coils design"]
-[7.495269298553467, 3.128864049911499, "[FF] Target-Point Observation Capabilities of the GOSAT-2 = Enhanced"]
-[5.659533500671387, 1.8866074085235596, "[TT] EMC Test Dates of the MPO spacecraft = 2015"]
-[7.919837951660156, -0.9346548914909363, "[TT] Users of the ICESat-2 = More than 350"]
-[7.681345462799072, 6.836441993713379, "[TT] Combined Sensitivity Improvement of the eROSITA = Factor of 5"]
-[10.326027870178223, 5.7628984451293945, "[TT] Apparent Cooling of the GeoSTAR = Can exceed 100 K"]
-[7.260322570800781, 5.847845554351807, "[TT] Quantity of the CERES = 2"]
-[9.377455711364746, 7.373682975769043, "[TT] Ground Resolution of the Panchromatic Imager = One meter"]
-[4.17853307723999, 7.1583452224731445, "[TT] Frequency Bands of the SIR-C = C-band, L-band, X-band"]
-[14.168009757995605, 3.174028158187866, "[TT] Mass of the HSC-III = ~ 10 kg"]
-[3.8516132831573486, 3.839723825454712, "[TT] Test Download Location of the RISAT-1 = Troms\u00f8, Norway"]
-[7.580273151397705, -2.504396438598633, "[TT] Operation Start Date of the GOLD = Early October 2018"]
-[11.586721420288086, 6.903143882751465, "[TT] NH Parameter of the ART-XC = \u2265 3 x 1023 cm-2"]
-[12.131263732910156, 4.530111312866211, "[TT] Largest Satellite Deployed from ISS of the RemoveDebris satellite = True"]
-[5.416146278381348, -0.5161384344100952, "[TT] Expected Resume Date of the Yutu-2 = Next Thursday (10 January)"]
-[9.514318466186523, 0.8223804235458374, "[FF] Closest Approach to the Sun of the Rosetta = Perihelion"]
-[14.302726745605469, 2.7902588844299316, "[TT] Mass of the KOMPSAT-1 = 470 kg"]
-[5.388513565063477, 3.943403959274292, "[TT] Quantity of the SuperDove satellites = 150"]
-[7.848316192626953, 1.5227925777435303, "[FF] Purpose of the GPM = Provide advanced measurements about the rain and snow particles within clouds, Earth\u2019s precipitation patterns, extreme weather and myriad ways precipitation around the world affects society"]
-[13.105101585388184, 3.091468572616577, "[TT] Fuel of the Satellite = Limited amount"]
-[5.199358940124512, 5.179323673248291, "[TT] Tracking System of the MMS = GPS signals"]
-[8.690662384033203, 7.151709079742432, "[FF] Active Diameter of the L3 Detector = Large enough to intercept even the widest-angle trajectories defined by the L1\u2022L2 coincidence"]
-[6.504680156707764, -0.23940163850784302, "[TT] Observation Duration of the Roman = Several days"]
-[7.761265277862549, 6.702659606933594, "[TT] Based on of the VNIIEF and MSFC designs = Single spider scheme"]
-[4.329948425292969, 0.7370488047599792, "[TT] Unveiling Date of the DMSP-20 = December 20, 2017"]
-[8.417986869812012, 7.311244964599609, "[TT] System Dynamic Range of the PMC-2 Imagers = 20~800 DN"]
-[9.410534858703613, 7.036801338195801, "[TT] Spatial Resolution (TIR) of the MSU-SK1 = 700 km"]
-[9.858185768127441, 7.686633586883545, "[FF] Observation Capability of the MTEL Space Telescope = Space-time development of TLEs"]
-[6.134134292602539, 6.4583001136779785, "[TT] Latency Requirement of the S-1 NRT = Within 3 hours"]
-[5.1894917488098145, 2.22268009185791, "[FF] Mission Payloads of the HORYU-4 = Multiple"]
-[6.3517255783081055, 8.643593788146973, "[TT] Polarization of the 5 = Horizontal"]
-[7.8668646812438965, 8.647443771362305, "[TT] Optical Configuration of the ELVIS = Czerny-Turner"]
-[8.178934097290039, 8.484321594238281, "[TT] Bandwidth of the VNIR = 0.40 \u00b5m"]
-[6.6500935554504395, 1.706403374671936, "[FF] URL of the Rosetta = http://sci.esa.int/rosetta/12198-new-louvers-ensure-that-rosetta-is-real-cool/"]
-[6.431759357452393, 3.9834940433502197, "[TT] Number of Runs of the Monte Carlo Simulation = 3000"]
-[7.46858549118042, 5.3301544189453125, "[FF] Purpose of the COTS #3 = Examine new photonics technologies, in particular optocoupler components"]
-[9.513712882995605, 3.9078235626220703, "[FF] Measurement of the Search-coil magnetometers = Alternative magnetic field in the low and medium frequency ranges"]
-[6.521645545959473, 4.5107598304748535, "[FF] Unknown of the Direct Readout Data Users = Multiple"]
-[5.402341842651367, 1.0765702724456787, "[FF] Mission Start Date of the SMOS = Unknown"]
-[12.205862045288086, 3.6906492710113525, "[TT] Xenon Critical Temperature of the CVX\u20132 Device = Tc=16.6\u00baC"]
-[12.460926055908203, 0.6433994770050049, "[TT] Focusing Length Adjustment of the Plato Camera = 1 \u00b5m"]
-[7.838390350341797, 3.033714771270752, "[FF] Monitoring Program of the MicroCarb = CNES / MicroCarb Atmospheric CO2 Monitoring Program"]
-[7.977253437042236, 1.6724075078964233, "[FF] Backscattering from Water Surface of the Radar = Study Conducted"]
-[5.0875139236450195, 6.763899803161621, "[TT] TT&C Uplink of the Spacecraft bus = 2 kbit/s"]
-[7.960136890411377, 8.263330459594727, "[FF] Purpose of the Dichroic Systems = Separate the scene radiance into the spectral bands of interest"]
-[7.671863555908203, -0.0964498221874237, "[FF] Operator of the IceCube = NASA and GSFC (Goddard Space Flight Centre)"]
-[6.4867048263549805, -0.5454086065292358, "[TT] Period of the RADARSAT-2 = 100.7 min"]
-[8.034517288208008, 4.520535469055176, "[FF] Radiation Resistance of the Bdelloids = Extremely resistant to radiation"]
-[5.985439300537109, 6.8760857582092285, "[TT] Data Compression of the Onboard Data Handling Subsystem (OBDH) = Achieving compression ratios of 2.28 - 2.8"]
-[4.330165863037109, -0.020268963649868965, "[FF] Reentry Date of the P35-6 = Unknown"]
-[10.414788246154785, 4.4340596199035645, "[TT] Reaction Wheel of the CanX-2 = 30 mNms"]
-[13.46497917175293, 3.050078868865967, "[TT] Mass of the S-band Broadcast Satellite Services Transponder = ~70 kg"]
-[4.901630401611328, -0.8755994439125061, "[TT] Orbit Period of the Dragon = ~92 minutes"]
-[8.656755447387695, 1.222916841506958, "[FF] Coordination of the ACCS = Coordinates with the Aquarius Science Team and the SAC-D Operations personnel"]
-[6.63407039642334, 0.8245764374732971, "[TT] Launch Date of the Solar-B / Hinode = 23 September 2006"]
-[5.768364906311035, -0.8153115510940552, "[TT] Operational Lifespan of the Flock-1d' satellites = Around six months"]
-[10.376738548278809, 4.452855587005615, "[FF] Components of the PCS separation system = Two spring loaded rings and a motorized release mechanism"]
-[8.46314811706543, 6.6789774894714355, "[FF] Time Between Monitoring Campaigns of the OSIRIS Narrow Angle and Wide Angle Cameras = Reduced to a few days"]
-[8.533047676086426, 7.4309210777282715, "[TT] Binning Modes of the Camera = 1 x 1, 1 x 2, 2 x 1, 2 x 2"]
-[9.900690078735352, 8.118428230285645, "[TT] F/No of the Telescope = 2.8"]
-[3.4149560928344727, 5.283350467681885, "[TT] Frequency of the SAR = 3.13 GHz"]
-[4.970656871795654, 8.139846801757812, "[TT] Receiver Type of the CubeRRT RFE = Single tunable superheterodyne"]
-[9.490772247314453, 6.099461078643799, "[TT] Cross-Track of the HSRS = 19\u00b0"]
-[6.704087257385254, -0.35645896196365356, "[TT] Period of the Satellite = 89.5 minutes"]
-[7.148775100708008, 2.5268714427948, "[TT] Publisher of the Observation of the Earth and Its Environment = Springer Verlag"]
-[9.86381721496582, -0.3657054305076599, "[TT] Altitude of the TSX and TDX = About 514 km"]
-[5.604548454284668, 1.2655936479568481, "[FF] Development Date of the ETS-VIII Satellite = 2003"]
-[5.123525619506836, 2.959041118621826, "[TT] Operator of the GovSat-1 = LuxGovSat S.A."]
-[9.802176475524902, 1.0695923566818237, "[TT] Journey Distance of the eROSITA = 1.5 million kilometers"]
-[10.796835899353027, 3.4873006343841553, "[TT] CubeSat Size of the BRRM = 3U"]
-[5.8683953285217285, 2.4590256214141846, "[TT] Technology Readiness Level of the Legion = High"]
-[9.43086051940918, 3.841670274734497, "[TT] Measurement Type of the \u00d8rsted spacecraft = Magnetic field intensity"]
-[6.718857765197754, -0.47425830364227295, "[TT] Repeat Cycle of the Harmony = 12 days"]
-[4.843008518218994, 7.151905536651611, "[TT] Data Rate of the S-band downlink system = 8 Mbit/s"]
-[6.911736965179443, 2.675150156021118, "[FF] Mission of the INSAT-3DR = Improve upon observation capabilities of its predecessors"]
-[13.832117080688477, 2.7194859981536865, "[TT] Mass at Launch of the Spacecraft = ~4850 kg"]
-[8.326623916625977, 5.876511573791504, "[TT] Distance Measurement Accuracy of the LRI = Up to 0.000001 mm"]
-[8.927326202392578, 5.971775054931641, "[TT] Direction of the Beam = 45\u00ba to nadir"]
-[7.228376388549805, 3.2306580543518066, "[FF] Instrument of the GeoSTAR = Utilizes the same established approach as is being used with the AMSU instrument"]
-[13.357925415039062, 7.428159236907959, "[TT] TWTA Output Power of the TWTA = 90 W max (saturation)"]
-[3.7875852584838867, 6.243535041809082, "[TT] Number of Radiators of the NAVANT = 36"]
-[5.391193866729736, 4.1689372062683105, "[TT] Spacecraft Bus Type of the QuickBird-2 = BCP-2000"]
-[4.929030418395996, 0.5162031054496765, "[TT] Launch Year of the TCTE = November 2013"]
-[6.482962608337402, 4.852614402770996, "[FF] Transmission Capacity of the IOV Payload = Dynamic allocation"]
-[6.143099308013916, 5.125863552093506, "[FF] Receiver Locking Sequence of the Transponder = Residual carrier, command subcarrier"]
-[6.966727256774902, 4.6798014640808105, "[FF] Long Range Navigation of the ATV-5 = Relative GPS navigation"]
-[8.89958381652832, 3.9782772064208984, "[TT] Spectral Region of the Sun of the ISO Instrument = 30 - 125 nm"]
-[18.803619384765625, 3.476043701171875, "[TT] \u0394r (m) of the Dobbins = 13.1"]
-[5.087391376495361, 0.40745294094085693, "[TT] Launch-readiness Date of the TSIS-2 = February 2023"]
-[6.814380645751953, 5.691621780395508, "[FF] Purpose of the VCU (Video and Compression Unit) = Process the video signals delivered by the FEEs : digitization on 12 bits, numerical processing, compression and image CCSDS packet generation"]
-[5.676713943481445, 0.3073938488960266, "[TT] Orbit Reach Date of the Cheollian 2B = March 6"]
-[4.976083278656006, 0.5928518772125244, "[TT] Launch Date of the UKube-1 = July 2014"]
-[8.497708320617676, 5.34879207611084, "[TT] Orbit Determination Accuracy of the GF-3 Satellite = 4 cm"]
-[5.807528972625732, 3.397778034210205, "[TT] Adjusted EBITDA of the Satellogic = \u2013$30.7 million"]
-[5.536675930023193, -0.034885793924331665, "[FF] Mission Design of the RapidEye = Acta Astronautica Volume 56, Issues 1-2, January 2005, pp. 213-219"]
-[4.824869155883789, -0.9904386401176453, "[FF] Launch Date of the Fengyun-4B = 2 June 2021"]
-[12.144968032836914, 5.118934631347656, "[TT] Size of the High-Voltage Array = 122 mm x 214 mm"]
-[11.297195434570312, 5.666543006896973, "[TT] Material of the Torus/Strut Structures = 12 mil thick neoprene coated Kevlar"]
-[5.720228672027588, 0.6452445387840271, "[TT] On-orbit Checkout Completion Date of the F-17 = Jan. 29, 2007"]
-[5.449271202087402, 6.202686786651611, "[TT] Memory of the Transceivers = 2 Mbit"]
-[9.664510726928711, 8.297078132629395, "[TT] Lens System of the Color Imager = Wide field-of-view (FOV) lens of 30\u00ba"]
-[13.389705657958984, 6.930572032928467, "[TT] Power Requirement of the Severyanin-M = 1 kW"]
-[5.916834831237793, 4.435098648071289, "[FF] Purpose of the Automator = Commanding and monitoring the EDRS-A payload"]
-[7.958202362060547, 6.610033988952637, "[TT] Scan Rate of the MSU-SK = 50 lines/s in channels 1-4 and 12.5 lines/s in channel 5"]
-[10.075547218322754, -1.5494931936264038, "[TT] Inclination of the S/C = 80.2\u00ba"]
-[5.433071136474609, 1.388230800628662, "[FF] Presentation of the NROL-36/OUTSat = Workshop"]
-[8.230937004089355, 7.484504699707031, "[TT] Detector of the DubaiSat-2 = TDI CCD detectors"]
-[11.900869369506836, 4.5227885246276855, "[TT] Span of the Spacecraft = 14.67 m"]
-[5.705936908721924, -0.7236204147338867, "[TT] Mission Duration of the Kolibri-2000 = 45 days"]
-[6.600351810455322, 0.010007505305111408, "[FF] Operation Duration of the Landsat 5 = Unknown"]
-[13.398100852966309, 7.320277214050293, "[TT] Power of the XRD = 2.245 W (BOL)"]
-[9.51657485961914, 0.8906236886978149, "[TT] Distance from New Horizons of the Hydra = About 231,000 km"]
-[8.05391788482666, 5.9080119132995605, "[FF] Thermal Environment Requirement of the Cameras = Stable measurements over long periods of time (months)"]
-[5.179433345794678, 0.5773677229881287, "[FF] Announcement Date of the 30 Doradus in LMC = Jan. 30, 2000"]
-[6.079832077026367, 0.8668649196624756, "[TT] Discovery Date of the GRB 150101B = January 2015"]
-[5.881494045257568, 0.9003651142120361, "[FF] Failure Date of the Sensor Flipper = March 23, 1978"]
-[6.474488735198975, 5.1007537841796875, "[FF] Operation Type of the DPCC = LCT time synchronization, On-orbit propagator, LCT alignment matrix, LCT park and unpark, Ka-band antenna steering pause"]
-[4.522500038146973, 1.2980741262435913, "[FF] Presentation Date of the AlSAT-1 = Unknown"]
-[3.7957959175109863, 6.447912216186523, "[TT] Antenna Type of the MSR = Offset Cassegrain-type antenna"]
-[10.143033981323242, 1.5673810243606567, "[FF] Discovery of the eROSITA = Large-scale bubbles in the halo of the Milky Way"]
-[13.623741149902344, 5.877171516418457, "[TT] Power of the Solar panels = 2 kW (BOL)"]
-[5.183079242706299, 0.8962175846099854, "[FF] Launch Date of the FireBird = April 8, 2013"]
-[5.052098274230957, 0.48405224084854126, "[FF] Launch Date of the EPICHYPER-1 = July 5, 2023"]
-[8.191044807434082, 8.00418472290039, "[TT] Number of Bands of the SWIR Detector = 3"]
-[11.847362518310547, 6.572236061096191, "[TT] High Energy Particle Strikes of the Computer System = 2"]
-[6.317256927490234, 3.114750385284424, "[TT] Nadir resolution of the WorldView Legion = 29 cm"]
-[6.912846565246582, 4.253691673278809, "[FF] GIFOV of the TRUTHS = Unknown"]
-[10.0518798828125, 4.873244285583496, "[TT] Number of Redundant Cooling Pumps of the AMS-02 = 4"]
-[4.629007339477539, 7.0555806159973145, "[TT] Downlink Rate of the Sentinel-1 = Very high X-band downlink rate"]
-[4.5324907302856445, 0.3366955518722534, "[FF] Success Date of the Soyuz = April 19, 2013"]
-[9.658726692199707, 8.391193389892578, "[TT] Field of View (FOV) of the Instrument = 52\u00ba"]
-[7.390035152435303, 3.5725743770599365, "[FF] Length of Operation of the Internal Satellite Diffuser = 30 min, one or two wavelengths per orbit"]
-[7.022558689117432, 3.8555586338043213, "[FF] Mission of the ASPIICS = ESA PROBA-3 Formation FlighT"]
-[7.527739524841309, 7.005199909210205, "[TT] Cadence of the Electron Spectrum = 5 minutes"]
-[8.95435905456543, 5.466198921203613, "[TT] Pointing Precision of the FY-3 series spacecraft = 50 m on the ground"]
-[10.927824020385742, 3.6985981464385986, "[TT] Flyby Speed of the NEA Scout = Less than 100 feet [30 meters] per second"]
-[8.384562492370605, 6.628775119781494, "[FF] Performance of the Scanner = Stable scanner performance over life"]
-[7.7263994216918945, -0.7835657596588135, "[FF] URL of the ICESat-2 = http://www.nasa.gov/feature/goddard/lasers-path-through-icesat-2"]
-[7.427043437957764, 2.3482613563537598, "[TT] Global Mapping Achievement of the Satellite = 97.4%"]
-[8.538833618164062, 2.3354477882385254, "[FF] Wind Measurement of the InSight = Continuous"]
-[9.450919151306152, 5.935225486755371, "[TT] Incidence Angle of the Satellite = 25\u00ba"]
-[5.30122184753418, 2.5360116958618164, "[FF] Development Institution of the e-st@r program = Politecnico di Torino"]
-[7.889230728149414, -2.4763660430908203, "[FF] Observation of the GOLD = Total solar eclipse"]
-[4.181582450866699, 1.873718023300171, "[TT] End of Life Date of the NigeriaSat-X = 31 Dec 2021"]
-[11.7711181640625, 0.04701820760965347, "[TT] Additional Partners of the TESS = Northrop Grumman, NASA\u2019s Ames Research Center, Harvard-Smithsonian Center for Astrophysics, MIT\u2019s Lincoln Laboratory, Space Telescope Science Institute"]
-[13.355596542358398, 5.419921398162842, "[FF] Additional Solar Panel of the MicroMAS-1 = Another 2U solar panel will be body-mounted on the zenith side of the satellite bus"]
-[11.509511947631836, 3.9930367469787598, "[TT] Balloon Diameter of the AeroCube-3 = ~ 60 cm"]
-[13.800249099731445, 2.814359426498413, "[TT] Liftoff Mass of the SRG spacecraft = 2,704 kg"]
-[13.264702796936035, 5.290902614593506, "[TT] Largest Crater Diameter of the Eureca = 6.4 mm on the solar arrays"]
-[13.97193431854248, 3.0234179496765137, "[TT] Take-off Weight of the SES-14 = 4,200 kg"]
-[4.425381660461426, 1.8471879959106445, "[TT] Launch Date of the RADARSAT-2 = December, 2007"]
-[10.395663261413574, 4.491757869720459, "[TT] Quantity of the Momentum Wheels = Three"]
-[4.505845546722412, -0.17693638801574707, "[FF] Docking Date of the Intelsat 901 Satellite = 27 February 2020"]
-[6.361954212188721, 1.9563941955566406, "[FF] URL of the WorldView Legion = https://tinyurl.com/y8f8qhrb"]
-[9.039985656738281, 7.728017330169678, "[FF] Spectral Resolution of the HPT = Multispectral"]
-[8.701233863830566, 5.669045448303223, "[TT] Post-processed position knowledge of the POD software = \u00b1 15 m (3\u03c3 in each axis)"]
-[5.017738342285156, 0.3192351162433624, "[TT] Scheduled Operational Date of the Polar Epsilon = 2010/11"]
-[9.352089881896973, 0.9138820767402649, "[TT] Distance from Sun at Arrival of the Parker Solar Probe = 18.8 solar radii (around 8.1 million miles)"]
-[7.006397247314453, 2.550107717514038, "[TT] Experiments per Day of the Satellite = 2-3"]
-[8.099186897277832, 2.7127797603607178, "[FF] Purpose of the CAPSat = Perform quantum annealing experiments"]
-[10.83206844329834, 7.105381011962891, "[TT] Remaining ?V Capability of the PRISMA = More than 50 m/s"]
-[6.413105487823486, -0.6902432441711426, "[TT] LTDN of the DubaiSat-2 = 10:30 hours"]
-[7.425967693328857, 3.7400102615356445, "[TT] Developer of the Neutron Dosimeter = Germany"]
-[6.058541297912598, 1.1434743404388428, "[FF] Date of the Hunting Milky Seas by Satellite = 2 November 2021"]
-[10.083856582641602, 5.672656059265137, "[FF] CCD Detector Assembly Cooling of the EUVI = Passively cooled by a radiator"]
-[7.084166526794434, 6.812955379486084, "[FF] Frequency Locking of the Master Laser = On-board reference cavity"]
-[10.655266761779785, 4.086436748504639, "[TT] Attitude Determination and Control Subsystem of the CanX-2 = Demonstrated"]
-[5.044179439544678, 4.884204864501953, "[FF] Mission Objective of the SpooQy-1 = Demonstrate an entangled photon light source"]
-[3.4272263050079346, 6.411978244781494, "[TT] Thickness of the Antenna = 7 mm"]
-[4.569464683532715, 0.5474368333816528, "[TT] Prototype Duration of the CIMON = 2 July 2018 to 27 August 2019"]
-[5.080916881561279, 6.888246536254883, "[TT] Capability of the RF communications = 300 Gbit"]
-[5.409643173217773, 2.1566779613494873, "[FF] Team Communication of the HORYU-4 = Problems"]
-[5.1981916427612305, 2.485058069229126, "[TT] Agency of the PhoneSat-1 and -2 = NASA"]
-[14.222461700439453, 3.2913100719451904, "[TT] Mass of the Experiment = 55 kg"]
-[5.503392696380615, 5.545641899108887, "[TT] CPU Cores of the Mission Operation System = More than 3000"]
-[8.176304817199707, 5.60184907913208, "[FF] Function of the CAMS = Help better calibrate the observatory's main telescope"]
-[6.684384346008301, 1.7719208002090454, "[FF] URL of the Rosetta = http://www.esa.int/spaceinimages/Images/2014/11/Rosetta_solar_wing"]
-[13.393632888793945, 7.340287208557129, "[TT] Power of the Power = 1164 W"]
-[8.058913230895996, 3.653493881225586, "[TT] Instrument Type of the LORAAS = Low Resolution Airglow/Aurora Spectrograph"]
-[7.940517425537109, 7.950520992279053, "[TT] Power of the HSC-III optics subsystem = 3.3 W"]
-[8.508781433105469, 4.292655944824219, "[FF] Sun Azimuth and Elevation of the RVX = Wrt the orbital perigee direction"]
-[3.9213037490844727, 9.737860679626465, "[TT] Bandwidth (GHz) of the ICI-1 = 6"]
-[9.682387351989746, 5.5587382316589355, "[TT] Actuation Method of the Electrodes = Electrostatic force"]
-[10.351642608642578, 2.102703809738159, "[TT] X-ray Source of the NuSTAR = Sun, Jupiter"]
-[8.373640060424805, 4.397385120391846, "[FF] Development Date of the USNA MIDN Microdosimeter Instrument = Unknown"]
-[7.305008888244629, 2.794440269470215, "[TT] Revisit Time of the MethaneSAT = Every few days"]
-[7.644069194793701, 8.948628425598145, "[TT] Spectral Range of the Spectral Band B = 0.52 - 0.60 \u00b5m"]
-[6.2564005851745605, 6.447719573974609, "[TT] Guard Time of the DCPs = At least 30 seconds"]
-[4.844454765319824, -1.8513542413711548, "[TT] Journey Time to the Moon of the Chang'e-5 = Estimated 112 hours"]
-[14.211423873901367, 3.21034836769104, "[TT] Mass Limit of the Tyvak 12U dispenser = 25 kg"]
-[4.658134937286377, 6.599697113037109, "[TT] Technology of the EUMETCast = Standard DVB-S2"]
-[8.030659675598145, 5.274975299835205, "[FF] Components of the Spectral Calibration = ISRF Shape, SSI, SR, Smile, CU"]
-[3.5277721881866455, 1.6474759578704834, "[TT] Launch Site of the Sentinel-1B = Kourou"]
-[7.8506245613098145, -2.508939743041992, "[FF] Measurement Techniques of the GOLD = Temperature obtained on disk from rotational shape of N2 LBH (Lyman-Birge-Hopfield) bands, O/N2 composition measured using ratio of 135.6 doublet to LBH bands, Temperature on limb determined by slope of emission altitude profile, O+ at night observed using 135.6 recombination emission, O2 profile on limb from stellar occultations"]
-[9.781042098999023, 7.049894332885742, "[TT] Observation Modes of the AGRI = 2"]
-[6.157325744628906, 1.3839337825775146, "[FF] Collision Avoidance Date of the Swarm = 14 July 2022"]
-[3.2105960845947266, 4.9739813804626465, "[TT] Mapped Area of the SAR = 100 million km2"]
-[9.354328155517578, 5.3187737464904785, "[TT] Slew Rate of the Spacecraft = 15\u00ba / minute"]
-[6.939280033111572, 0.4954814910888672, "[TT] Tasks of the Kepler = 4"]
-[5.129824161529541, 8.431241035461426, "[TT] Bandwidth/Passband of the 4 = 400 MHz"]
-[8.324891090393066, 7.531787395477295, "[TT] Detector Type of the Imager = CCD"]
-[4.102815628051758, 4.828405857086182, "[TT] Total Uncertainty Cone of the Alphasat TDP1 and Sentinel-1A = Initially set to 2250 \u00b5rad and reduced to 1000 \u00b5rad"]
-[8.278261184692383, 3.6836354732513428, "[FF] Data Acquired of the TSUBAME = Atmospheric density, atomic oxygen density, and the level of deterioration of material samples"]
-[5.24744987487793, 3.3025176525115967, "[TT] Manufacturer of the NRTP = MRSA/SAC team"]
-[9.992613792419434, 2.866856813430786, "[TT] Launch Date to ISS of the VPM CubeSat = 5 December 2019"]
-[5.639858245849609, 3.308537483215332, "[FF] Operator of the SEOSat = Unknown"]
-[10.237715721130371, 3.259692668914795, "[TT] Spectrometer Frequency of the MicroMAS-2 CubeSat = Near 90 and 206 GHz"]
-[4.649720191955566, 1.5485495328903198, "[TT] Observation Time of the TanSat = April and July 2017"]
-[4.561682224273682, 7.707250118255615, "[FF] Configuration of the Spare Lithium-1 Radio = Reconfigured to monitor the crosslink activity"]
-[9.617899894714355, -0.39654627442359924, "[TT] Altitude of the FY-3E = ~ 800 km"]
-[6.6881632804870605, -0.36589086055755615, "[TT] Orbit Maneuver Frequency of the RADARSAT-2 = Once every 3 weeks"]
-[5.828773021697998, 5.459494590759277, "[TT] Type of the OBC = High-grade main OBC"]
-[13.947299003601074, 3.063283920288086, "[FF] Mass of the TSAT = Unknown"]
-[4.576254367828369, 0.11571169644594193, "[TT] Launch Date of the Starshine-3 = Sept. 30, 2001"]
-[4.5047502517700195, 1.399355173110962, "[FF] Launch Date of the LambdaSat = Unknown"]
-[7.389134883880615, 4.949765205383301, "[FF] Data Processing of the LUTI = ICAS (Image Calibration and Analysis Subsystem) in KDGS (KPLO Deep-space Ground System)"]
-[8.24289321899414, 5.904672145843506, "[FF] Use of the CVSE = To use these low-power flight piezo drivers and control systems in zero-g environments"]
-[5.5446085929870605, 1.7415498495101929, "[FF] Autonomous Precision Orbit Control of the ALOS-2 = Unknown"]
-[8.051937103271484, 1.7751466035842896, "[FF] Orbit Decay Cause of the GOCE mission = Uncompensated atmospheric drag"]
-[3.2720279693603516, 5.039346218109131, "[TT] Single Pol Swath Width of the SAR Processor = 350 km"]
-[8.766144752502441, 2.077826738357544, "[TT] S/C Size of the WINDS satellite = 2 m x 3 m x 8 m"]
-[9.80215072631836, 8.247925758361816, "[TT] FOV of the SXI = 42 arc min x 42 arcmin"]
-[4.3824381828308105, 3.112800359725952, "[FF] Ground Station Location of the Enxaneta = Sant Esteve de la Sarga, in the Pallars Juss\u00e0"]
-[9.474294662475586, 1.371727466583252, "[TT] Low Speed Deployment Functionality of the Dispensers = As low as 5 cm/s"]
-[5.1718974113464355, 4.214405059814453, "[TT] Maximum Satellites Launched of the New Glenn rocket = Around 30"]
-[13.834495544433594, 2.693265438079834, "[TT] Launch Mass of the Spacecraft = 116 kg"]
-[6.056128025054932, 7.118036270141602, "[TT] Data Rate of the Instrument = 600 kbit/s"]
-[14.22605037689209, 3.0923380851745605, "[TT] Mass of the ZACUBE-1 = 1.2 kg"]
-[7.544829845428467, 4.812994480133057, "[FF] Data Collection Method of the Radiometer Sensor = Sweeping perpendicular to the groundtrack"]
-[6.211916446685791, 5.174465656280518, "[FF] Categories of the L1-SAIF+ = \"SBAS-compatible\" and \"SBAS-incompatible\""]
-[7.995692253112793, 5.147010803222656, "[FF] Datasheet Revision of the QubeAIS = 1.4"]
-[6.555272102355957, 0.27912333607673645, "[TT] Data Posting Time of the FORMOSAT-7/COSMIC-2 Constellation = 02:00 UTC"]
-[6.876957416534424, 4.820412635803223, "[FF] Functions of the Data Handling Computer (DHC) = Flare detection, exposure evaluation, time averaging, spatial averaging, sub-field extraction, and JPEG compression"]
-[9.012024879455566, 0.5388773679733276, "[FF] International Participants of the ARTEMIS = The United Kingdom, Canada, and Australia"]
-[6.024433135986328, 0.5444096922874451, "[TT] Mission Status of the ASTERIA = Operating on an extended mission"]
-[9.958477020263672, -1.4361572265625, "[TT] Orbit Inclination of the SpaceX CRS-17 = 51.6\u00ba"]
-[3.2383618354797363, 5.091815948486328, "[TT] Incidence Angle of the SeaSat SAR = Near-nadir"]
-[6.37982177734375, -0.15065769851207733, "[TT] Expected Orbit Duration of the Skylab-1 = 8-10 years"]
-[7.491959095001221, 2.922593116760254, "[FF] Methane Emissions of the Hugo = Approximately 4000 kg per hour"]
-[13.2609224319458, 5.4454731941223145, "[FF] Function of the Canadarm2 = Stage the new pair of solar arrays in time for the installation spacewalks"]
-[5.030708312988281, 6.295665264129639, "[FF] Transmission Protocol of the MDD = GTS (Global Telecommunication System of WMO)"]
-[9.372197151184082, 4.794579029083252, "[FF] Pointing Control of the Attitude System = One arc-minute"]
-[5.75258731842041, 6.839352607727051, "[TT] Data Delivery of the Science Data Interface = 1/8/64 science data packet(s) every 3 seconds"]
-[8.416178703308105, 3.229550838470459, "[TT] Precision of the Ozone Measurement Instrument = 3 DU+0.5% total ozone or better"]
-[9.891358375549316, 5.5755486488342285, "[FF] Function of the AEM = Data acquisition and treatment, temperature control"]
-[9.67990779876709, 4.088804721832275, "[TT] Magnitude Random Error of the Magnetic Field = < 0.3 nT"]
-[10.320230484008789, 3.296109199523926, "[FF] Fine Pointing Control of the CubeSat = Detect 55 Cancri e via the transit method"]
-[8.292258262634277, -0.4772092401981354, "[TT] Comparison of the Sea Ice Extent = 3.07 million km2 (1.19 million square miles) lower than the 1981-2010 average extent"]
-[10.33193588256836, 7.10310173034668, "[TT] Ground Area Coverage of the TIR Subsystem = 156 km by 8 km"]
-[8.430261611938477, 7.963109970092773, "[TT] Array Size of the VNIR = 40 x 640"]
-[6.230221748352051, 5.28843879699707, "[FF] Objective of the FITSat-1 = Demonstrate a high-speed transmission module for a small satellite and a visible light communication experiment using high power LEDs"]
-[7.524980545043945, 2.8830604553222656, "[FF] Warming Power of Methane of the MethaneSAT = More than 80 times the warming power of carbon dioxide during its first 20 years"]
-[10.063705444335938, -1.5119150876998901, "[TT] Orbit Inclination of the KSM-1 satellites = 37\u00ba"]
-[5.404453754425049, 5.965598106384277, "[TT] Data Transmission of the EUMETCast = Multicast files"]
-[3.98331618309021, 1.8803551197052002, "[TT] Launch Provider of the TEMPO = SpaceX Falcon-9"]
-[3.667602062225342, 6.524180889129639, "[TT] Antenna Type of the Antenna = Dual Paraboloidal Reflector"]
-[4.2481207847595215, 7.251675128936768, "[TT] Downlink Frequency of the EROS-A = X-band"]
-[6.463934421539307, 5.808790683746338, "[TT] PRN of the GSAT-0101 = 11"]
-[7.029381275177002, 6.8765869140625, "[TT] Pointing Stability (long-term) of the Laser = < 20% of divergence"]
-[4.020667552947998, 3.493577718734741, "[FF] URL of the Galileo = http://www.esa.int/Our_Activities/Navigation/Galileo_to_spearhead_extension_of_worldwide_search_and_rescue_service"]
-[4.707172393798828, 4.950176239013672, "[FF] Information Provided of the Flightradar24 = Flight tracks, origins and destinations, flight numbers, aircraft types, positions, altitudes, headings and speeds"]
-[11.70989990234375, 3.283496856689453, "[TT] Thrust Time of the RCS = About 80 sec in the one cycle"]
-[4.2813520431518555, 2.4340574741363525, "[TT] Launch Site of the Enxaneta = Baikonur Cosmodrome, Kazakhstan"]
-[11.61788558959961, 3.3153505325317383, "[TT] Propulsion System of the Satellites = Mono-propellant"]
-[13.639095306396484, 3.5406699180603027, "[TT] Mass of the X-band Transmitter = 2.7 kg"]
-[9.602608680725098, 8.169102668762207, "[TT] Field of View of the MSC = 6\u00b0 x 0.3\u00b0"]
-[11.114117622375488, 6.409982681274414, "[TT] Halo Temperature of the eROSITA = Millions of degrees"]
-[10.717771530151367, 1.5867443084716797, "[FF] Magnetic Field of the Neutron Star = Strong, complex"]
-[8.378518104553223, 0.2610877454280853, "[FF] Composition of the Meteorites = Unknown"]
-[5.823203086853027, 4.7079758644104, "[FF] Data Encryption Capability of the NPOESS = Capable of encrypting selected mission data in all satellite links, excluding the S&RSAT and ADCS real-time downlinks"]
-[5.467921733856201, 6.081554412841797, "[TT] Flash Memory of the OBC = 256 MB"]
-[5.144655227661133, 3.236253261566162, "[TT] Owner of the Beijing-3 = Twenty First Century Aerospace Technology Co., Ltd (21AT)"]
-[4.264898300170898, 2.5285274982452393, "[TT] Launch Site of the Deployment Systems = Dombarovsky Missile Site, Yasny"]
-[4.606880187988281, 2.658428430557251, "[TT] Funding Date of the BRITE Satellites = 2010"]
-[3.8827362060546875, -1.2463390827178955, "[TT] Placement of the Aditya-L1 = Lagrangian point L1"]
-[11.300326347351074, 2.8186893463134766, "[TT] Power of the Microsatellite = 30 W (max)"]
-[3.3671627044677734, 1.4367682933807373, "[TT] Launch Dates of the Sentinel-2 = 23 June 2015 (Sentinel-2A), end of 2016 (Sentinel-2B)"]
-[10.897834777832031, 7.519372463226318, "[TT] Swath Width of the AATSR = 500 km"]
-[5.940027236938477, 1.9386693239212036, "[TT] Deployment Window of the OSA (Orion Space Adapter) = From the time ICPS disposal maneuver is complete to up to 10 days after launch"]
-[6.54823637008667, 7.659621715545654, "[TT] Quantization of the Instrument = 12 bit"]
-[7.828413963317871, 7.120774745941162, "[TT] Frame Rate of the Video Camera = 30 frames/s"]
-[8.659740447998047, 8.774954795837402, "[FF] Components of the Offner Spectrometer = Relay mirror and a spherical convex diffraction grating"]
-[7.9290771484375, 2.310074806213379, "[FF] Monitoring Capabilities of the MTVZA-GY = Atmospheric temperature and humidity profiles, precipitation, sea-level wind speed and snow/ice coverage"]
-[9.808812141418457, 2.351655960083008, "[FF] Calibration of the NuSTAR = First light pictures"]
-[4.672749042510986, 1.522789478302002, "[TT] Launch Date of the GCOM-C = 27 October, 2017"]
-[6.061216831207275, 1.434091567993164, "[FF] Radioactive 44Ti of the Cassiopeia A = Detected"]
-[5.171393871307373, 6.505518913269043, "[TT] Output Data Rate of the Spacecraft 406 MHz Processor = 2.4 kbit/s"]
-[3.938323736190796, 2.024951219558716, "[TT] Launch Vehicle of the BlackSky-1 = PSLV-C35"]
-[10.031556129455566, 6.982124328613281, "[TT] Spatial Resolution of the IRS Sounder = 800 m at SSP"]
-[9.559775352478027, 7.189340114593506, "[TT] Spatial resolution at nadir of the VIRR = 1.1 km"]
-[3.4484336376190186, 4.972374439239502, "[TT] Mission Phase of the Copernicus L-band SAR = Preliminary design phase"]
-[3.721972703933716, -1.0728557109832764, "[TT] Orbit Type of the Orion EFT-1 = Elliptical orbit"]
-[4.326848983764648, 2.4840803146362305, "[TT] Launch Site of the Probe = Tanegashima Space Center"]
-[6.321784496307373, 7.2809529304504395, "[FF] Error Reduction of the DS-BAQ = More than the BAQ technique"]
-[3.242570638656616, 4.957005023956299, "[TT] Field of Regard of the SAR = 500 km"]
-[5.807886123657227, 5.3573317527771, "[TT] Redundancy of the GPS receiver = Cold redundancy"]
-[8.052078247070312, 3.25622820854187, "[FF] Objective of the LI System = Deliver information on total lightning over the full disk"]
-[11.575860977172852, 4.723883152008057, "[TT] Structure Length of the STRV-2 = 0.82 m"]
-[11.444263458251953, 2.2076969146728516, "[TT] \u0394V (cm/s) of the Cosmos 1302 = 1.40"]
-[4.1964497566223145, 2.3515658378601074, "[TT] Separation Status of the BRITE-Montreal satellite = Did not separate from its Dnepr launch vehicle"]
-[8.063921928405762, 4.131636142730713, "[FF] Operating Principle of the SEVIRI = Collecting radiation from a target area and focusing it on detectors sensitive to 12 different bands of the electromagnetic spectrum by means of a telescope"]
-[2.343245506286621, 1.3176952600479126, "[TT] Launch Site of the NanoSail-D = Omelek Island in the Kwajalein Atoll"]
-[10.94228458404541, 2.102381706237793, "[FF] Manufacturer of the XMM-Newton = ESA"]
-[13.371520042419434, 2.878943681716919, "[TT] Instrument Mass of the DubaiSat-2 = 50 kg"]
-[8.260307312011719, 3.1566121578216553, "[FF] Data Collection Period of the Ozone Monitoring Instrument (OMI) = 150-day period from 2015 through 2019"]
-[7.8751678466796875, 2.001132011413574, "[FF] Mean Sea Surface Topography of the SeaSat = Data"]
-[6.037600517272949, 4.973758697509766, "[FF] Function of the Space-ground communications hardware = Turns RF signals into information to be sent throughout the system"]
-[5.109057903289795, 4.690413951873779, "[TT] Emergency Number of the eCall = 112"]
-[3.945509433746338, 6.72157096862793, "[TT] Design of the Antenna = Square array of tunable inverted F UHF antennas, and of one stacked circularly polarized L-band patch"]
-[9.768763542175293, 2.7574892044067383, "[FF] Fault Tolerant Features of the NANOsky I = SEE immunity, innovative error mitigation techniques, sophisticated three-level FDIR policy, redundancy on all critical functions"]
-[4.505916595458984, 7.869024753570557, "[TT] Transmit and Receive Frequencies Offset of the Satellite = 0.5 MHz in the 24 GHz channel, and by 0.67 MHz in the 32 GHz channel"]
-[6.361391067504883, 0.1544845551252365, "[FF] Repair Effectiveness of the Skylab = Exceeded expectations"]
-[3.319845676422119, 1.5666279792785645, "[FF] Application Date of the Sentinel-5P = 19 October 2020"]
-[7.449107646942139, 8.592434883117676, "[FF] Feature of the SGD = Greatest sensitivity in this band"]
-[3.4614577293395996, -0.8930354714393616, "[TT] Orbit Type of the CBERS-3 = Sun-synchronous orbit"]
-[12.828131675720215, 7.5991082191467285, "[TT] Power of the Instrument = 6 W"]
-[7.141703128814697, 8.24665641784668, "[FF] Function of the Filter Wheel Assembly = Defines the channels in each band"]
-[5.392502307891846, 3.312260627746582, "[FF] Heritage of the Deployable mast = SRTM"]
-[4.943096160888672, 0.6777625679969788, "[TT] Transition Date of the Pilot Program = CSDA"]
-[8.714766502380371, 8.662986755371094, "[TT] Pixels per FWHM of the Spectrometer = 715"]
-[8.140708923339844, -0.6487921476364136, "[FF] Measurement Importance of the CryoSat-2 = Understanding the links between ice and climate"]
-[4.523530006408691, 1.2937965393066406, "[TT] Launch Date of the AlSat-2B = September 26, 2016"]
-[6.946371078491211, 6.1392316818237305, "[TT] Number of Instruments of the AMS = 7"]
-[10.183819770812988, 9.387197494506836, "[TT] Nominal IGFOV of the Band 3 = 1 km"]
-[3.615025520324707, 6.999863147735596, "[TT] Polarization of the DRT = L-V LHCP"]
-[7.0580525398254395, 0.22080621123313904, "[FF] Bedrock Formation Age of the CaSSIS = Between 3.7 and 4.1 billion years ago"]
-[8.518275260925293, 8.030221939086914, "[TT] Number of Pixels of the Band 5 = 800"]
-[7.418356418609619, 2.802025079727173, "[TT] Global Mapping Frequency of the MethaneSAT = Every 3 - 4 days"]
-[13.779093742370605, 5.349353313446045, "[TT] Type of the Multi-junction GaAs = Multi-junction GaAs"]
-[10.099349021911621, 6.480145454406738, "[FF] Across-Track Slope of the MABEL = Calculated"]
-[5.407915115356445, 2.6282925605773926, "[TT] Back Up User of the Canadarm2 = ESA astronaut Thomas Pesquet"]
-[4.646493434906006, 0.5760874152183533, "[TT] Launch Date of the Sich-2 = 17 Aug 2011"]
-[8.812862396240234, 6.369243621826172, "[TT] Significant Wave Height Estimate Accuracy of the ALT = 0.5 m or 10%"]
-[4.594664096832275, 6.592717170715332, "[FF] Communication System of the Spacecraft Bus = S-band TT&C (Telemetry, Tracking and Command) transceivers and X-band data downlink transmitters"]
-[7.785704612731934, 6.087416648864746, "[TT] Operation of the ABI = Earth scene collection"]
-[6.044619083404541, 0.8079013228416443, "[FF] Orbit Parameters of the Kanopus-V-IK = i=97.44\u00b0; H = 522.5km; h = 478.6km"]
-[7.569604873657227, 7.656795978546143, "[TT] Sensitivity of the MTVZA-GY = Factor 2"]
-[5.671224117279053, 5.544780731201172, "[TT] Type of the OBC = Dual-redundant GEC/Plessey Mil Std SOS 1750a microprocessor"]
-[3.511841297149658, 5.969471454620361, "[FF] Mechanical Configuration of the Antenna = Three panels per twelve tiles"]
-[8.237284660339355, 7.258654594421387, "[TT] Sensitivity of the Visible Light and Infrared Point Detectors = Highly sensitive"]
-[10.09728717803955, -1.5905723571777344, "[TT] Inclination of the FormoSat-2 = 97.7\u00ba"]
-[8.206404685974121, 7.509082794189453, "[TT] Signal Processing of the CCD Detector = Fast electronics near the detector head"]
-[9.34631633758545, -0.4131501615047455, "[TT] Apogee Altitude of the Satellite Constellation = ~ 4,500 km"]
-[6.990836143493652, 5.6567816734313965, "[TT] Availability of the SST = 66%"]
-[10.09309196472168, 0.26614826917648315, "[TT] Formation Distance (Cross-track) of the Harmony satellites = 200 - 500 m"]
-[8.412923812866211, 2.9856231212615967, "[FF] Purpose of the Odin = Aeronomy and astronomy minisatellite with applications for atmospheric research, stratospheric ozone chemistry, mesospheric ozone science and summer mesospheric science"]
-[5.188425064086914, 2.725167751312256, "[TT] Agency of the SMART = Ben-Gurion University (BGU)"]
-[10.76097583770752, -1.1430877447128296, "[TT] Altitude of the SLATS = 368 km"]
-[9.02627944946289, 5.093353271484375, "[TT] Design and Testing Duration of the Gyro Unit = Three and a half years"]
-[5.697808742523193, -0.9029877185821533, "[TT] Design Life of the GEISAT Precursor = Four years"]
-[4.565980911254883, 6.758332252502441, "[TT] Communication of the CICERO satellites = UHF up/downlink for TTC data"]
-[4.656280040740967, 7.112252235412598, "[TT] X-band, Downlink Data Rate of the Data Transmission Subsystem = 190 Mbit/s"]
-[5.5318145751953125, 6.516671180725098, "[TT] Data Volume of the Vricon\u2019s products = 110-petabyte"]
-[14.136624336242676, 3.214550733566284, "[TT] Mass of the DMSP Block 4 = About 80 kg"]
-[12.41069507598877, 0.6169284582138062, "[FF] Telescope Sensitivity of the PLATO = 1 m-class"]
-[9.048233985900879, 6.479612827301025, "[TT] Imager Coverage of the CaSSIS = Eight-kilometer-wide swath of the planet's surface"]
-[9.552735328674316, 6.2064433097839355, "[TT] Incidence Angle of the Wide standard Quad-Pol = 18 - 42\u00ba"]
-[12.699536323547363, 1.9090094566345215, "[FF] Science Objectives of the SAGE-III = Characterize tropospheric and stratospheric aerosols and upper tropospheric and stratospheric clouds"]
-[3.8205690383911133, 1.2243143320083618, "[FF] Fairing Recovery of the Falcon 9 = Two recovery vessels were dispatched to sea to retrieve the fairing halves from Tuesday night\u2019s mission"]
-[6.1558709144592285, 4.2084832191467285, "[FF] Objective of the CIL = Preserve confidentiality for requests and products"]
-[11.989154815673828, 3.184034585952759, "[TT] Propellants of the Bipropellant propulsion system = MMH (fuel) and N2O4 (oxidizer)"]
-[7.663234710693359, 2.963928461074829, "[FF] Expected Nitrogen Dioxide Emissions Restriction of the International Shipping Emission Regulations = Coming years"]
-[5.266991138458252, 7.731927871704102, "[TT] EIRP of the UHF Antenna = over 27.1 dBm"]
-[9.150121688842773, 5.758253574371338, "[TT] Cant Angle of the Pointing Mechanism = About 1\u00ba"]
-[4.681388854980469, 4.977846145629883, "[TT] Information Received of the SDR = Aircraft identification, position, altitude, and intent"]
-[7.204983711242676, 4.931545257568359, "[FF] Design of the MPPT = Onboard"]
-[8.477899551391602, 8.520179748535156, "[TT] Spectral Resolution of the Spectrometer = <0.625 cm -1"]
-[9.426517486572266, 3.955894947052002, "[TT] Magnetic Field Measurement Range of the Plasma Wave Instrument = 1 Hz to 10 kHz"]
-[6.198249816894531, 5.964529991149902, "[TT] Function of the TRC = Controls both H and V TR modules and the PCPU"]
-[8.928799629211426, 5.665868759155273, "[TT] Pointing Accuracy of the ADCS = \u00b1.14 arcsec (1\u03c3)"]
-[8.618424415588379, 8.285789489746094, "[FF] Upgrades of the NIRSpec = New detectors and microshutters"]
-[8.2086763381958, 6.7382307052612305, "[TT] Revisit Time at 1 m - 0.5 m GSD of the WV60 imager = 1.7 days"]
-[9.258773803710938, -1.1560373306274414, "[TT] Orbit of the GOES-T = Geostationary orbit 22,236 miles above Earth"]
-[8.065592765808105, 4.740019798278809, "[FF] Output of the TRITEL = Dose Equivalent"]
-[8.029374122619629, 2.605053424835205, "[TT] Measurement Category of the VHRR = Cloud type, amount and cloud top temperature, Liquid water and precipitation rate, Radiation budget, Multi-purpose imagery (land), Surface temperature (land), Albedo and reflectance, Surface temperature (ocean), Atmospheric Winds"]
-[5.385078430175781, 3.9245221614837646, "[TT] Number of Satellites of the WorldViews 1, 2 and 3 = 3"]
-[9.756020545959473, 0.6331192851066589, "[FF] Measurement Distance of the Autonomous Wireless Payload = 635 km"]
-[6.298142910003662, 8.117053985595703, "[TT] Channels of the AMSR3 = 10"]
-[5.132536888122559, 1.564939260482788, "[FF] Website of the GOCE = http://op.gfz-potsdam.de/champ/systems/main_SYSTEMS.html"]
-[8.373502731323242, 2.4070255756378174, "[FF] Effect Size of the Aerosol Direct Radiative Effect = Unknown"]
-[5.45978307723999, 0.5246441960334778, "[TT] Last Data Received of the MaSat-1 = January 9, 2015"]
-[8.05924129486084, 7.375626564025879, "[TT] Data Rate of the CCD Camera = 1.3 Mbit/s"]
-[4.381948947906494, 0.6657865643501282, "[TT] Launch Date of the DMSP-F19 = April 19, 2014"]
-[11.140218734741211, 1.5511454343795776, "[TT] Mass of the BOKZ-M star tracker = 4 kg"]
-[9.779908180236816, 4.2884840965271, "[TT] Magnetorquer of the ADCS = \u00b10.2 Am 2"]
-[6.560297012329102, 2.6899290084838867, "[TT] Potential Use of the Space Moss = Space and future bases on the Moon or Mars"]
-[5.803803443908691, 0.8201863169670105, "[FF] Operational Declaration Date of the Kanopus-V = Jan. 29, 2013"]
-[9.631098747253418, 4.635455131530762, "[FF] Control Methods of the ADCS = Unique control method using aerodynamic drag"]
-[4.663623809814453, 3.2654192447662354, "[FF] Data Transmission Destination of the SAS&R = INMCC (Indian Mission Control Center), located at ISTRAC (ISRO Telemetry, Tracking and Command Network), Bangalore"]
-[5.389524936676025, 1.144006609916687, "[TT] Mounting Date of the IASI-NG PFM instrument = 2022"]
-[7.4403276443481445, 5.27945613861084, "[FF] Performance of the ILAS Instrument = Not specified"]
-[5.182332515716553, 1.2753218412399292, "[TT] Report Release Date of the SMAP = January 2007"]
-[10.230560302734375, 5.66638708114624, "[TT] Temperature Stability of the Filter Wheel = \u00b11 K"]
-[6.070127487182617, 6.4854559898376465, "[TT] Latency Requirement of the S-2 NRT = Restituted 90 minutes before Sentinel-2 A/B ANX is crossed"]
-[7.57468843460083, -0.6362523436546326, "[TT] Launch Date of the ICEYE = January 2018"]
-[9.256180763244629, 6.838629722595215, "[FF] Spatial Resolution of the Satellite = High"]
-[6.288907527923584, 8.62600040435791, "[TT] Polarization Mode of the TopSAR narrow = HH or HV or VH or VV"]
-[9.851017951965332, 8.217737197875977, "[TT] FOV Resolution of the WAOSS-B = 1.11 arcmin"]
-[7.373470783233643, 4.073796272277832, "[FF] Sensor Complement of the Satellite = Unknown"]
-[9.610272407531738, 4.075355529785156, "[TT] Interplanetary Vector Magnetic Field Measurement Accuracy of the DSCOVR = \u00b11 nT"]
-[6.587206840515137, 3.395134925842285, "[FF] Collaboration of the AMS-02 = AMS Collaboration"]
-[6.105769634246826, 6.785010814666748, "[FF] Data Acquisition of the PROBA-V = >1015 bytes"]
-[8.136346817016602, 3.4890177249908447, "[TT] Measurement Target of the OCO-2 = Gases"]
-[6.9495720863342285, 0.8313040137290955, "[FF] Mission End Date of the Gravity Probe B = Unknown"]
-[3.8521528244018555, 1.1411293745040894, "[TT] Number of Launches of the Falcon 9 = Three"]
-[4.7557373046875, 0.6852918863296509, "[TT] Remaining CCD Delivery of the Teledyne e2v = Before the end of 2020"]
-[6.010350227355957, 2.445361375808716, "[TT] Design Provider of the LRI = Max-Planck-Institute for Gravitational Physics (Albert-Einstein-Institute)"]
-[7.490203380584717, 5.285045146942139, "[FF] Development Areas of the Prototype hardware = RF Digital Polarimetric Receivers, Main Reflector, Reflector Deployment Assembly, Instrument Controller Electronics"]
-[11.450939178466797, 2.7621541023254395, "[TT] Mass of the NanoSat-1B = 23.5 kg"]
-[5.9255876541137695, -0.28829824924468994, "[FF] Mission Extension Period of the Aura spacecraft = Ongoing"]
-[5.859595775604248, 7.782262325286865, "[TT] Design of the OTA = Truly differential amplifier"]
-[14.330056190490723, 3.041952133178711, "[TT] Mass of the Baumanets-2 = 86 kg"]
-[7.619997024536133, 9.04203987121582, "[TT] Spectral Range (\u00b5m) of the Band 4 = 10.3 - 11.3"]
-[5.519360542297363, 2.2808542251586914, "[FF] Mission Type of the Hera = Surveying Didymos"]
-[6.023252487182617, -0.34320783615112305, "[TT] Operation Duration of the SWFO = 5 years"]
-[12.825258255004883, 7.5993499755859375, "[TT] Power of the Instrument = 50 W"]
-[9.611751556396484, 4.892608642578125, "[TT] Stabilization of the AOCS = 3-axis stabilized"]
-[10.342181205749512, 7.93184232711792, "[TT] Envelope Dimensions of the AEISS telescope = \u00d8 1.3 m x 2.1 m"]
-[6.7019243240356445, 4.052098751068115, "[FF] Formation of the B612 Foundation = Unknown"]
-[4.376411437988281, 7.874483108520508, "[FF] Downlink Frequency of the DRT = Extended C -band"]
-[7.614990234375, -0.8946364521980286, "[TT] Launch Date of the ICESat-2 = September 15th 2019"]
-[9.518595695495605, 2.742988109588623, "[TT] Solar X-ray Flux Level of the XRS instrumentation = A0.3"]
-[4.4481635093688965, 2.934199571609497, "[TT] Location of the Transponder = Australia"]
-[6.25100564956665, 6.002170085906982, "[TT] Phase Shifter Control of the TR Module = 6 bit"]
-[13.615850448608398, 5.767127513885498, "[FF] Power Source of the XI-IV = Body-mounted solar cells"]
-[11.890250205993652, 4.751497745513916, "[TT] Dimensions of the CanX-2 = 10 cm x 10 cm x 34 cm"]
-[6.156023025512695, 2.216125249862671, "[TT] Principal Investigator of the TEMPO = Kelly Chance"]
-[4.7352614402771, 8.08358383178711, "[TT] Center Frequencies of the EX = 1257.5, 1236.5 or 1278.5 MHz"]
-[10.26163101196289, 8.079379081726074, "[TT] Telescope Diameter of the SILEX Optical Terminal = 250 mm"]
-[6.23826265335083, 7.996263027191162, "[TT] Port Configuration of the Prototype Channelizer = 3 x 3"]
-[7.016657829284668, 4.4257612228393555, "[FF] Unknown of the Automatic Registration Method = Unknown"]
-[5.045061111450195, 2.7151589393615723, "[TT] Focal Point of the SWAVES = University of Minnesota"]
-[10.205190658569336, 4.599948883056641, "[TT] Rotation Rate of the Reaction Wheels = Up to 60,000 rpm"]
-[7.844357490539551, 3.0740838050842285, "[FF] Monitoring of the TanSat = Greenhouse gases"]
-[3.8721179962158203, 6.426865577697754, "[TT] Beam-Pointing Positions of the Active Antenna = 61"]
-[6.888134956359863, 8.910067558288574, "[TT] Spectral Region of the POLDER-P = 443 to 910 nm"]
-[5.685610294342041, 5.175386428833008, "[TT] Network Redundancy of the MTG satellites = Full cross-strapping redundancy with SpW-10X routers"]
-[6.3593339920043945, 5.81026554107666, "[TT] RPO Capability of the GSSAP = Yes"]
-[8.307344436645508, 0.520767331123352, "[FF] Hydropower of the Glen Canyon Dam = Electricity to about 5 million people in seven states"]
-[6.499242782592773, 1.5146141052246094, "[FF] Studies of the Faraday-Girl Scouts = Plant growth, ant colonization, brine shrimp lifecycle"]
-[7.032982349395752, -0.21247060596942902, "[TT] Total Crossing Time of the Solar Eclipse = About 1.5 hours"]
-[4.689464092254639, 7.04519510269165, "[TT] Data Transmission of the Landsat-6 = X-band direct downlink"]
-[5.514839172363281, 6.351556301116943, "[TT] Data Storage of the ISUAL instrument = Separate 128 MByte memory"]
-[4.521491527557373, -0.8838325142860413, "[FF] Splashdown Date of the SpaceX Crew Dragon = 8 March 2019"]
-[8.752791404724121, 5.790072917938232, "[TT] Confidence Limits of the CLARREO = 3\u03c3 or 99%"]
-[9.308572769165039, -1.6899014711380005, "[TT] LTAN Evolution of the Swarm-C (Charlie) = 9 hours of separation between lower pair and upper satellite at end of life"]
-[8.43942642211914, 1.1519981622695923, "[TT] Spatial Resolution of the Solid Earth Continental lithosphere = 50-100 km"]
-[6.406048774719238, 0.4819430708885193, "[TT] Landing Year of the Venera 9 = 1975"]
-[4.977943420410156, 6.223728656768799, "[TT] Receiver Type of the CTECS-A = Custom"]
-[6.556059837341309, 6.4069929122924805, "[FF] Robustness of the SMA Antenna Connection = Robust"]
-[4.7453460693359375, 7.2426066398620605, "[TT] Ka-band Data Rate of the CASCADE = Up to 1.4 Gbit/s (QPSK modulation)"]
-[5.140291213989258, 2.6675679683685303, "[TT] Affiliation of the OSIRIS = PSU (Penn State University), University Park, PA, USA"]
-[8.356951713562012, 3.9645910263061523, "[TT] Calibration Targets of the TRUTHS = Deserts and the moon"]
-[4.1559224128723145, 0.1824622005224228, "[TT] Launch Pad Explosion Date of the SpaceX Falcon-9 = Sept. 1, 2016"]
-[10.717708587646484, 2.944495677947998, "[TT] Resonance Survey Requirement of the SERB Nanosatellite = First resonant frequency > 90 Hz"]
-[11.194127082824707, 3.444521903991699, "[FF] Function of the Micro-propulsion thrusters = Control the spin and precession motion of the spacecraft"]
-[8.26697826385498, 4.083394527435303, "[FF] Observation Modes of the OCO-2 = Nadir, Glint, Target"]
-[3.7750120162963867, -1.0713783502578735, "[TT] Orbit Type of the P3RVX = Highly elliptical"]
-[5.675571918487549, 0.4579658508300781, "[TT] Operation Extension Date of the Cluster = December 31, 2009"]
-[9.179431915283203, 4.481719017028809, "[FF] Control Method of the Attitude Control System = Solar radiation pressure, Optical parameters control"]
-[7.765892028808594, 5.953848361968994, "[FF] Operation of the MODEX = Sequentially observe the same scene from the same spatial point"]
-[6.43335485458374, 8.152647972106934, "[FF] Communication Bands of the BioSentinel = Higher frequency bands"]
-[5.276991844177246, 5.364109039306641, "[TT] Tracking Method of the Cassegrain antenna = Closed-loop tracking"]
-[4.1936845779418945, 7.335753917694092, "[TT] Axial Ratio of the X-band Transmitter = <3dB"]
-[3.851712226867676, 3.399012565612793, "[TT] Launch Date of the Galileo = Dec. 17, 2015"]
-[9.276955604553223, 0.9538369178771973, "[TT] Impact Speed of the DART = 6.6 km/s"]
-[6.752049922943115, 4.467666149139404, "[FF] Unknown of the IPEX-II = Unknown"]
-[3.64401912689209, 4.763157844543457, "[TT] Payload of the Resurs-O spacecraft = Radar instrument, RLSBO (Side Looking Real Aperture Radar)"]
-[9.469137191772461, 4.714951515197754, "[FF] Attitude Control of the AOCS = Three-axis attitude control"]
-[8.24181079864502, 4.095906734466553, "[FF] Sensor Head Heritage of the Genesis Electron Monitor = SWEPAM-E and BAM-E flown on the ACE and the Ulysses missions"]
-[8.575200080871582, 3.079357862472534, "[FF] Measurement of the MAHRSI = Nitric oxide"]
-[6.463039875030518, 7.636689186096191, "[TT] Quantization of the LICEF = 1 or 0"]
-[9.629732131958008, 7.168233394622803, "[TT] Spatial resolution at nadir of the MWRI = 15-70 km"]
-[7.0015082359313965, 7.137020587921143, "[TT] Wavelength of the Acquisition/Tracking Lasers = 852 nm"]
-[5.857118129730225, 1.7893054485321045, "[FF] Altitude Data of the PRISM = Acquired by PRISM aboard ALOS-2"]
-[9.409414291381836, 0.8985031843185425, "[TT] Drift Speed of the Great Red Spot = Circling the planet in about four-and-a-half years"]
-[11.844948768615723, 3.3238418102264404, "[TT] Leak of the MarCO-B = Thruster Valve"]
-[5.755703926086426, 0.626902163028717, "[FF] Observation Date of the NOMAD-TGO = 15 June 2020"]
-[5.742481231689453, 6.897324562072754, "[TT] Header Size of the Processed Science Data Packet = 23 bytes"]
-[8.219032287597656, 1.954456090927124, "[FF] Objectives of the MWR = Precipitable water, winds speed, sea ice concentration, water vapor, cloud liquid water Measurements of precipitable water and sea surface wind speed (which will enhance the results of Aquarius measurements). Measurements of water vapor, cloud liquid water and sea ice concentration"]
-[8.805497169494629, 5.90711784362793, "[TT] Pointing Accuracy of the HSC-III = < 300 \u00b5rad (3\u03c3)"]
-[3.22110915184021, 5.037939548492432, "[TT] Spatial Resolution of the SAR Sensor Subsystem = 1 m x 1 m"]
-[5.0863261222839355, 2.039632797241211, "[TT] Mission Status of the QBITO = Mission complete"]
-[7.064026832580566, 8.154691696166992, "[TT] Signal-to-Noise Ratio (SNR) of the MSU-SK = 80 dB"]
-[3.169006109237671, 2.1977972984313965, "[FF] Affiliation of the CRISTAL = Copernicus program"]
-[7.6435465812683105, -0.49003446102142334, "[FF] URL of the IceCube-Gen2 = https://arxiv.org/pdf/2008.04323.pdf"]
-[9.388627052307129, -0.9876055717468262, "[TT] Mean semi-major axis of the Fast-sampling orbit = 7235379.8 m"]
-[10.452136039733887, 7.07847785949707, "[TT] CONUS Height of the ABI instrument = 4.8129\u00ba"]
-[4.582277774810791, 5.511592388153076, "[TT] Average Pass Length of the GOMX-3 = 7.4 minutes"]
-[4.366092205047607, 7.507183074951172, "[TT] Frequency Bands of the IMI = S- and C-band"]
-[6.302367210388184, -0.4129207730293274, "[TT] Total Duration of the STP-2 = Over six hours"]
-[7.722258567810059, 0.5176881551742554, "[FF] Measurement of the Lunar IceCube = 3 \u00b5m band absorption by several forms of water"]
-[9.069483757019043, 7.36285400390625, "[TT] Resolution of the False Color Composite Image = 250 m"]
-[7.499758243560791, 0.7803105711936951, "[FF] Unknown of the Lunah-Map = Unknown"]
-[5.254251003265381, 5.642021179199219, "[TT] Data Transmission Protocols of the ETS-VIII = CCSDS"]
-[8.783299446105957, 2.056290626525879, "[FF] Observed Altitudes of the MIGHTI = 200-300 km altitude, ~100 km altitude, 100 km altitude region"]
-[14.192049026489258, 3.2821996212005615, "[TT] Mass of the EPS = 167 g"]
-[8.290252685546875, 5.480240345001221, "[TT] Stand on Duty at of the FY-3D = 36,000 km"]
-[7.535238742828369, 3.757488489151001, "[FF] Usage of the NightPOD = Accurately track a SLR camera"]
-[5.426367282867432, 1.9367284774780273, "[TT] Image Credit of the TEMPO = BATC"]
-[7.00115966796875, 4.407954216003418, "[FF] G/T of the System = Unknown"]
-[5.481376647949219, 0.4019898772239685, "[FF] Definition and Upload of the Custom Timelines = Any time during the mission life"]
-[11.375306129455566, 6.354040622711182, "[TT] Minimum Proton Energy Detection of the LDT Sensors = Different for each floor"]
-[8.251582145690918, 5.891003608703613, "[FF] Measurement Principle of the SPS = Light received by this sensor evolves nearly linearly with the distance with the full umbra"]
-[5.182321071624756, 6.926624298095703, "[TT] Average Download Capacity of the Panama ground station = 1.2 GB/day"]
-[6.814433574676514, 6.39547061920166, "[TT] Activation Window of the Experiment Data = 1200 seconds"]
-[7.905942440032959, 0.9131234288215637, "[FF] Date of the \"Drought Hits Thailand\" = 15 February 2020"]
-[6.692727565765381, 2.175344467163086, "[FF] URL of presentation of the STARE = http://digitalcommons.usu.edu/cgi/viewcontent.cgi?filename=0&article=2991&context=smallsat&type=additional"]
-[6.579821586608887, 4.125854969024658, "[FF] Mission Type of the CHIPS = Small spacecraft with a single instrument payload"]
-[9.745565414428711, 6.926825046539307, "[TT] Calibration of the AGRI = Full-path on-orbit"]
-[6.387011528015137, 1.5060741901397705, "[TT] Expected End of Operations of the MICROSCOPE = Autumn 2018"]
-[5.182445526123047, 5.9652533531188965, "[TT] Router Internal Connections of the SpaceWire ASIC = 2"]
-[5.30658483505249, 7.288405418395996, "[TT] Interface of the Modem Processor = SPI (Serial Peripheral Interface) running at 1 MHz line rate"]
-[6.134429931640625, 5.506098747253418, "[FF] Redundancy of the USO = Redundant"]
-[6.2695746421813965, 4.504250526428223, "[FF] Function of the Mission Control = Command generation, telemetry analysis"]
-[11.692024230957031, 3.4107089042663574, "[FF] Ion Propulsion Technology of the Linar Cube = Mission Enabling"]
-[16.49565887451172, 3.595625162124634, "[FF] Purpose of the OneWeb = Broadband connectivity in unserved or underserved regions, cellular backhaul, mobility services, community and residential Internet access, and emergency communications"]
-[10.068768501281738, 1.2863883972167969, "[TT] Frequency of the Tidal Disruptions = Once every 10,000 to 100,000 years in a galaxy the size of our own Milky Way"]
-[9.67527961730957, 4.054711818695068, "[TT] Response Time of the Magnetic Field Sensor = <200 ns"]
-[8.624128341674805, 3.8839809894561768, "[TT] Solar Constant of the SOLCON = 100%"]
-[8.296991348266602, -0.5524749755859375, "[TT] Minimum Sea Ice Coverage of the Satellite Sensors = 15 percent of the water"]
-[7.047111988067627, 8.253195762634277, "[TT] Requirement Value of the SNR = 100"]
-[5.900542736053467, -0.23669478297233582, "[TT] Mission Design Life of the HAUSat-2 = 2 years"]
-[8.067336082458496, 8.277502059936523, "[FF] Output Signal of the Tunneling Infrared Sensor = 3.0 V signal + 1/400 of the tunneling high voltage + the tunneling signal disturbance"]
-[10.604257583618164, 5.496984481811523, "[TT] Inventor of the Electron Temperature Probe = K. Hirao"]
-[7.513460636138916, 2.3618505001068115, "[FF] Observation Modes of the GIIRS = China area mode, Mesoscale mode"]
-[9.400810241699219, 7.985576629638672, "[FF] Nominal Focal Parameters of the PamCam = Unknown"]
-[9.120659828186035, 7.212204933166504, "[TT] Resolution of the Imaging Payload = 22 metres"]
-[6.888542175292969, 9.506038665771484, "[TT] NEDT at 300 K of the Band 2 = 1 K"]
-[9.965923309326172, 7.910497665405273, "[TT] Field of View of the Telescope = Below 75 \u00b5rad"]
-[6.012755870819092, -0.44080692529678345, "[TT] Commissioning Duration of the Webb = Two months"]
-[3.08760929107666, 2.154059886932373, "[TT] Data License of the Copernicus Sentinel-3 = CC BY-SA 3.0 IGO"]
-[5.100672721862793, 3.4269306659698486, "[TT] Data Processor Developer of the GOME = German Remote Sensing Data Center (DFD) of DLR"]
-[3.4070913791656494, 5.084347248077393, "[FF] Frequency Band of the L-band SAR = L-band"]
-[6.127160549163818, 6.063656806945801, "[TT] Number of Sub-Processes of the EMOC = 5"]
-[9.733599662780762, -0.7695983648300171, "[TT] Orbit Altitude of the BeaverCube = Approximately 410 km"]
-[4.677277565002441, 0.9126648902893066, "[FF] Phase C Review Date of the SVOM = Unknown"]
-[9.46927261352539, -0.11514926701784134, "[TT] Height of the Sand Dunes = Up to 300 m"]
-[10.091023445129395, 5.535860538482666, "[TT] Mechanical, Thermal and TED Qualification of the PLM = Completed"]
-[8.734617233276367, 8.754012107849121, "[TT] Instrument Size of the Grating Spectrometer = 40 mm x 45 mm x 80 mm"]
-[6.570459365844727, 2.0597405433654785, "[FF] URL of the NuSTAR = http://www.jpl.nasa.gov/news/news.php?feature=6760&utm_source=iContact&utm_medium=email&utm_campaign=NASAJPL&utm_content=daily20170228-2"]
-[8.884343147277832, 7.621468544006348, "[FF] Design of the NAOMI = High-resolution pushbroom imager"]
-[9.769150733947754, -0.584373414516449, "[TT] Altitude in Orbit of the Electric Thruster = 720 km"]
-[5.257373332977295, 1.413877010345459, "[FF] Image Date of the ALOS-2 = July 25, 2019"]
-[5.574696063995361, -1.9164865016937256, "[FF] Role of the Kimiya Yui = Manipulate the SSRMS (Space Station Remote Manipulator System) for the operation of capturing Kounotori-5"]
-[7.67336893081665, 5.637555122375488, "[FF] Conference Date of the L-band Radiometers = Sept. 20\u202224, 2004"]
-[9.109539031982422, -1.2807778120040894, "[TT] Radiation Environment of the Instrument = GEO and LEO orbit"]
-[5.668476104736328, 5.0936360359191895, "[FF] Activation of the EPIRB = Can be activated in times of trouble to send out help signals"]
-[4.188665866851807, 1.9614777565002441, "[TT] Image Capture Date of the NigeriaSat-2 = 8 days after launch"]
-[8.708008766174316, 2.749352216720581, "[TT] Temperature Accuracy of the Lower atmosphere = 1 K at 700-10 mb"]
-[6.398184299468994, 2.073166608810425, "[FF] Presentation Date of the Taiwan Weather Monitoring Satellites = March 1-8, 2008"]
-[13.84242057800293, 7.118969440460205, "[TT] Topology of the Buck-Boost Converter = Buck-Boost"]
-[8.394116401672363, 8.223701477050781, "[TT] Spectral Resolution of the FTS = 0.04 to 1 cm-1"]
-[5.23598575592041, 6.725628852844238, "[TT] Download Speed of the Starlink Premium = 150-500 Mbit/s"]
-[4.909685134887695, 3.1840200424194336, "[TT] Manufacturer of the PeruSAT-1 = Airbus Defence and Space"]
-[8.42684555053711, 3.8382527828216553, "[FF] Function of the Earth horizon sensor = Use the infrared spectrum corresponding to the H2O absorption bands"]
-[7.4957122802734375, 8.461099624633789, "[TT] Color Filters of the LORRI = No"]
-[18.79827308654785, 3.479269504547119, "[TT] Mean \u0394N (m) of the Karshi Khanabad = 22.0"]
-[9.778374671936035, 4.118930339813232, "[TT] Magnet Strength of the PAMELA = 0.48 T"]
-[9.701885223388672, 7.092499732971191, "[TT] Resolution of the MWR = 50 km"]
-[5.974704742431641, -2.328010320663452, "[TT] Orbit Altitude of the Kondor-E1 = 464 km x 552 km"]
-[5.42617130279541, 3.066762685775757, "[TT] Vice President and General Manager of the WSF-M = Mark Healy"]
-[11.191150665283203, 0.6536059379577637, "[TT] Photometric Signal Precision of the CHEOPS = 85 ppm in 3 hours integration time for Neptune-size planets orbiting 12th magnitude star"]
-[8.009256362915039, 4.8027753829956055, "[FF] Components of the ADCS = Attitude sensor, actuator interface assembly, four digital sun sensors, magnetic coils, momentum wheel"]
-[11.904261589050293, 4.388824939727783, "[TT] Cion Size of the CICERO-6 = 30 x 10 x 6 cm"]
-[9.17164421081543, 3.792093276977539, "[FF] On-Orbit Calibration Method of the RAX-1 = Used the IGRF magnetic field model and current satellite measurements"]
-[5.81549072265625, 3.2648563385009766, "[FF] Development Partners of the Telerobotics = ESA, DLR"]
-[5.935703277587891, 1.97476065158844, "[FF] Contact Email of the MEVI\u00b5S = eoportal@symbios.space"]
-[7.930514812469482, 1.8268284797668457, "[FF] Purpose of the GOCE = Measure the pull of Earth's gravity"]
-[5.465668678283691, 6.210621356964111, "[TT] Memory Storage of the CPU Board = 128 MB of DRAM for data memory storage and cache memory storage"]
-[6.83440637588501, -0.6944595575332642, "[TT] Start Time of the Quasi-Halo Orbits = 2020 August 30 00:00:00.00 dynamical barycentric time (TDB)"]
-[7.554612636566162, 1.626180648803711, "[FF] Purpose of the Kepler Mission = Detection of extra-solar planetary systems"]
-[9.080806732177734, 3.370081901550293, "[FF] Transverse Propagation of Wave-like Drift Perturbations of the Plasma Drifts = Account for a phase difference between local maxima in the plasma drift and the plasma density"]
-[7.07130765914917, 5.9037766456604, "[FF] Purpose of the Atomic Hydrogen-Maser Oscillator System = Measure the effect of the gravitational potential on the frequency of a proper clock"]
-[10.4138765335083, 5.736294746398926, "[TT] Cooling Temperature of the Baseplate of the Vessel = 15\u00b0C"]
-[6.5469970703125, 4.845187664031982, "[FF] Assembly State of the EM (Engineering Model) = In the assembly state"]
-[6.4165472984313965, 2.0306620597839355, "[FF] URL of the RADARSAT Constellation Mission = http://www.asc-csa.gc.ca/eng/search/images/watch.asp?id=4247"]
-[9.238595008850098, 7.036355972290039, "[TT] Spatial Resolution of the Chang'e-1 = 120 m"]
-[4.555874824523926, 6.151266574859619, "[TT] Morse Code Rate of the VHF Beacon = 15 words/minute"]
-[8.915192604064941, 5.7092204093933105, "[TT] Accuracy of the GT = 0.4 arcsec, 3\u03c3"]
-[6.71284294128418, 4.576538562774658, "[TT] Carried Payload of the Aoxiang-1 = FIPEX (Flux-Phi Probe Experiment)"]
-[9.759242057800293, -0.2784847915172577, "[TT] Peaking altitude (km) of the SSMIS = 0-10"]
-[4.813786506652832, 0.5418481826782227, "[TT] Launch Dates of the iMESA = MISSE-7(ISS), iMESA 2009-2011"]
-[12.906030654907227, 7.098413944244385, "[FF] Function of the SWEM = Load new high voltage lookup tables, trigger a switch between the operative high voltage table, load and trigger a switch between the lookup tables that determine how counts are accumulated and binned in the SPAN sensor FPGAs"]
-[9.485713005065918, 5.378202438354492, "[TT] Orientation of the CRBF and ORBF = The corresponding x-axes are oriented along the relative motion line"]
-[10.113142967224121, -2.709418773651123, "[TT] Data Storage of the C&DH SPAM board = 16 GB of on-board NAND Flash"]
-[13.876627922058105, 6.972103118896484, "[TT] Breakdown Voltage of the Zener Diode = 356 V"]
-[3.796184778213501, -1.1182225942611694, "[TT] Orbit of the DSCOVR = Lissajous orbit about L1"]
-[8.402769088745117, 1.1595262289047241, "[TT] Spatial Resolution of the Solid Earth Rifts = 100-500 km"]
-[5.791000843048096, 2.079444646835327, "[FF] Program Overview of the CBERS = URL: http://www.dpi.inpe.br/gilberto/present/cbers_overview.ppt"]
-[8.153697967529297, 6.7963948249816895, "[TT] Number of Images of the MWIR = 90 in first 6 months"]
-[10.762578964233398, -1.0686312913894653, "[FF] Attitude Mode of the SLATS = NM-PX or the NM-MX"]
-[3.2551627159118652, 5.719156742095947, "[TT] Radar Reflector Antenna Diameter of the NISAR = 40 feet (12 meters)"]
-[4.434063911437988, 7.773813724517822, "[TT] Frequency of the VHF Transmitter = 137 MHz"]
-[8.08575439453125, 8.723755836486816, "[TT] Spectral Range of the EUVS = 5 - 127 nm"]
-[11.701298713684082, 3.2785918712615967, "[TT] Functionality of the NANOPS Propulsion System = Undegraded after 1.5+ years in orbit"]
-[10.438191413879395, 2.275463581085205, "[TT] Energy Range of the X-ray Background Spectrum = 3-300 keV"]
-[5.526955604553223, 3.8363420963287354, "[TT] Number of Satellites Sold of the Neosat = 15"]
-[5.954280376434326, -0.13911640644073486, "[FF] Command Preparation Time of the Malindi, Kenya = Up to 12 hours"]
-[6.959129810333252, 2.3915228843688965, "[FF] Conference Presentation Location of the Earth Observation System of the Republic of Kazakhstan = Beijing, China"]
-[14.032861709594727, 3.176225423812866, "[TT] Servicer Mass of the ELSA-d = ~180 kg"]
-[8.634507179260254, 7.150873184204102, "[TT] Optics Type of the Imager Suite = All-reflective"]
-[4.925510883331299, 3.381091356277466, "[TT] Manufacturer of the Safran/Snecma PPS-5000 = Safran/Snecma"]
-[10.51990795135498, 6.927489757537842, "[TT] Diameter of the Mirror Shell = 50 to 150 mm"]
-[10.092421531677246, -1.5821393728256226, "[TT] Inclination of the FY-3E = 98.7\u00ba"]
-[5.553769588470459, 7.184676647186279, "[TT] Data Rate of the Rebroadcast = ~30 Mbit/s (GRB)"]
-[10.126317977905273, 1.1006982326507568, "[TT] Distance to Galaxy of the GRB 031203 = Less than 1300 million light years"]
-[9.718283653259277, 8.444073677062988, "[TT] FOV of the Instrument = 4 x 150 arcmin"]
-[10.92585563659668, 4.73042106628418, "[TT] Edition of the Tethers In Space Handbook = Third"]
-[7.690273761749268, 4.955845832824707, "[TT] Radiation Tolerance of the GPS Receiver = 13 kRads"]
-[6.758881092071533, -0.6196486949920654, "[FF] Orbit of the JPSS = Afternoon (13:30 hours)"]
-[5.844850540161133, 4.501392364501953, "[FF] Purpose 3 of the PW-Sat = Testing of the satellite communication system"]
-[7.965572357177734, 5.953600883483887, "[TT] Conical scanning period of the Microwave System = 2.88 s"]
-[8.490541458129883, 6.4215521812438965, "[TT] Estimated Uncertainty of the EDOT = Below 1 m"]
-[8.638957977294922, 2.506640911102295, "[FF] URL of the Hyper-Angular Rainbow Polarimeter-2 = https://iafastro.directory/iac/proceedings/IAC-19/IAC-19/B1/2/manuscripts/IAC-19,B1,2,7,x52335.pdf"]
-[7.136834621429443, 5.6058454513549805, "[FF] Function of the On-board Science Algorithm = Autonomously adjusts the receiver detection threshold levels and detector gain"]
-[9.939574241638184, -1.0859452486038208, "[TT] Acceleration of the NigeriaSat-2 = 0.35\u00b0/s2"]
-[10.628125190734863, 7.3298726081848145, "[TT] Swath Width of the Instrument = 20 km"]
-[10.506561279296875, 2.2707672119140625, "[TT] Manufacturer of the X123 X-ray Spectrometer = Amptek"]
-[6.348898887634277, -1.2160143852233887, "[TT] Local Access Time of the KOMPSAT-3 = 13:30 hours"]
-[5.401947498321533, -0.23592378199100494, "[TT] Launch Date of the Block 5D satellites = Fall of 1974"]
-[4.125675678253174, 4.275234222412109, "[FF] Secondary Goals of the RAX-2 = Training the next generation of space engineers and monitoring amateur radio frequency bands"]
-[8.772480964660645, 2.783740520477295, "[FF] Mission Objectives of the TIMED = Determine the relative importance of the various radiative, chemical, electrodynamical, and dynamical sources or sinks of energy for an understanding of the thermal structure of the MLTI"]
-[5.523728847503662, 2.9365735054016113, "[TT] Agencies of the MSOC = Department of National Defence (DND), the Royal Canadian Mounted Police, Canada Border Services Agency, the Canadian Coast Guard, the Department of Fisheries and Oceans and Transport Canada"]
-[3.810028314590454, 6.048403739929199, "[TT] Manufacturer of the Helical Antenna = SENER Aeroespacial"]
-[6.977484226226807, 4.312343597412109, "[FF] Unknown of the IDS = Unknown"]
-[8.575112342834473, 6.412221431732178, "[TT] Location of the SHM = Close to the intermediate focus"]
-[5.798740386962891, 1.0127562284469604, "[FF] Launch Date of the Deep Space 1 = Unknown"]
-[6.061432838439941, 0.8448648452758789, "[TT] Discovery Date of the GRB 191016A = Oct. 16"]
-[9.163677215576172, 7.126944065093994, "[TT] Camera Resolution of the Change-2 Satellite = One Meter"]
-[3.562793016433716, 3.8865931034088135, "[FF] Concept Type of the PAZ-TerraSAR Constellation = Coordinated Constellation Concept (CCC)"]
-[5.140312194824219, 4.203181266784668, "[TT] Number of L-band MEOSAR payloads of the Glonass-K1 = 2"]
-[11.972039222717285, 5.014397621154785, "[TT] Size of the Size = 277 mm x 106 mm x 186 mm"]
-[5.460872650146484, 1.496190071105957, "[FF] Workshop Presentation Date of the EnMAP = March 16-18, 2009"]
-[10.255361557006836, 8.094917297363281, "[TT] Diameter of the Telescope Aperture = 150 mm"]
-[5.213436603546143, 6.967405319213867, "[TT] Max Data Rate (Mbit/s) of the USAT = Uplink: 1.5-6 Downlink: 1.5-6"]
-[6.285133361816406, 8.080732345581055, "[TT] No of Passbands of the Channel 4 = 1"]
-[5.358422756195068, 4.000196933746338, "[TT] Number of Satellites of the Beijing-3 = 2"]
-[4.357092380523682, 6.994139671325684, "[TT] Purpose of the S-band station = Telemetry, Tracking and Control (TT&C)"]
-[10.18217658996582, 0.9212621450424194, "[TT] Distance from Earth of the WD 1856 b = 80 light-years"]
-[10.25991439819336, 7.531752109527588, "[TT] Telescope Type of the MSI instrument = Mirror silicon carbide off-axis telescope (TMA)"]
-[8.270605087280273, 8.413228034973145, "[TT] VIS Channels of the Spectrometer = 1024 channels from 0.753 - 0.784 \u00b5m with 0.1 nm FWHM resolution"]
-[7.243252277374268, 7.854395866394043, "[TT] Preamp full scale output swing of the PHA = 4.0 V"]
-[7.2018303871154785, 1.8610581159591675, "[TT] Decommission Date of the Carbonite-1 = November 2018"]
-[3.4896652698516846, 1.5036944150924683, "[TT] Anomaly Date of the Sentinel-1B = 23 December 2021"]
-[6.054790496826172, 4.097365856170654, "[FF] Organizational Interfaces of the MSX Flight Operations Team = Figure 38"]
-[4.846983909606934, -0.014577838592231274, "[TT] Data Delivery of the SPOT-4 = Unreliable"]
-[7.207520484924316, 1.9216630458831787, "[FF] Data Usage of the Carbonite-2 = UK\u2019s Royal Air Force (RAF) for use by the Joint Force Command National Centre for Geospatial Intelligence"]
-[3.7659459114074707, 4.684528827667236, "[TT] X-band SAR Data Reception Stations of the RADARSAT-2 = 26 sites"]
-[5.555931568145752, 1.0482312440872192, "[FF] Launch Date of the Satellite = Unspecified"]
-[8.03884506225586, 5.023022174835205, "[FF] Total O3 of the O3 Profile = 9 x 10 3"]
-[4.222659111022949, 7.22867488861084, "[TT] Frequency Band of the S-band Transmitter = S-band"]
-[13.427857398986816, 7.317906379699707, "[TT] Power of the DACS = 27 W"]
-[7.037324905395508, 4.290279865264893, "[FF] Unknown of the CEASE = Unknown"]
-[9.314215660095215, -0.676406741142273, "[FF] Orbit Parameters of the 5 smallsats = i=97.61\u00b0; H = 601.5-600.1km; h = 600.0-590.1km"]
-[9.798563957214355, 8.256030082702637, "[TT] FOV of the Telescope = 1.02 R sun \u00b1 2.7/3 R sun"]
-[4.288349628448486, 4.8158793449401855, "[TT] Minimum Beam Mode Detectable Ship Length (MDSL) of the ScanSAR wide = 29-358 m"]
-[10.418971061706543, 7.426397323608398, "[TT] Swath Width of the ScanSAR-1 = 100 x 2500 km"]
-[4.848411560058594, 3.1547417640686035, "[TT] Manufacturer of the NAOMI = Airbus DS (former EADS Astrium SAS)"]
-[9.669235229492188, 7.006422519683838, "[TT] SIC Spatial Resolution of the CIMR = 5 km"]
-[5.740277290344238, 6.277193546295166, "[TT] Processing Power of the VPU = More than 1000 MIPS"]
-[3.93381404876709, 3.4392290115356445, "[FF] Stakeholder Involvement Timeline of the Galileo Second Generation = In the next eight months"]
-[9.241153717041016, 4.415691375732422, "[FF] Primary Sensor of the SpinSat = The spacecraft itself"]
-[9.199369430541992, 7.445218086242676, "[TT] Image Resolution of the Satellogic = 1 meter"]
-[6.2503228187561035, 1.8148425817489624, "[FF] URL of the PSLV = https://www.isro.gov.in/mission_PSLV_C40.html?timeline=timeline#:~:text=PSLV%2DC40%2FCartosat%2D2%20Series%20Satellite%20Mission&text=India's%20Polar%20Satellite%20Launch%20Vehicle,613%20kg%20at%20lift%2Doff"]
-[7.948598861694336, 7.23270320892334, "[FF] Command Interface of the CCD (Charge-Coupled Device) = UART type"]
-[3.3474202156066895, 1.7458795309066772, "[FF] Calibration Date of the Sentinel-1 = Sept. 9-13, 2013"]
-[7.938885688781738, 2.8606574535369873, "[FF] Steps of the Level 2 image processing = Cloud screening, Atmospheric corrections, Geophysical variables retrieval algorithms"]
-[9.363268852233887, 6.786910057067871, "[TT] Imaging Modes of the KazEOSat-2 = Agile"]
-[3.5351979732513428, 4.416967391967773, "[TT] Operation Start Year of the SAR-Lupe = 2008"]
-[7.874558925628662, -0.716376543045044, "[TT] Discovery Year of the Fletcher's Ice Island = 1946"]
-[9.526909828186035, 4.9879913330078125, "[TT] Long-Term Stability Drift of the MIRAS = 0.49 K or 1.46 K"]
-[3.9225001335144043, 9.736223220825195, "[TT] Bandwidth (GHz) of the ICI-8 = 6"]
-[10.931842803955078, 3.7355196475982666, "[TT] Solar Sail Flyby Velocity of the NEA Scout = Less than 100 feet, or 30 meters, per second"]
-[14.361572265625, 3.1729331016540527, "[TT] Mass of the MKA-N 2 = 10 kg"]
-[4.9569621086120605, 8.348506927490234, "[TT] Channel Frequency of the MHS = 183.311 GHz"]
-[6.836111545562744, 7.125160217285156, "[TT] Length Increase of the BEAM = Nearly doubled"]
-[9.140875816345215, 4.952236175537109, "[TT] Gyroscope of the ADCS = 12.5 mV/\u00ba/s, \u00b1150\u00ba/s"]
-[3.8244946002960205, -1.2122020721435547, "[TT] Orbit of the Gaia = Second Lagrange point, L2, of the Sun-Earth system"]
-[5.706295967102051, 7.060772895812988, "[TT] Peak Data Rate of the EAN = 100 Mbit/s"]
-[8.38669204711914, 1.8792880773544312, "[FF] Effect of Traffic Levels of the Model = Increased coverage from contrail cirrus clouds, with an increased optical thickness of the ice clouds"]
-[7.325936317443848, 5.074934959411621, "[FF] Sensor Complement of the ResourceSat-2 = Two AWiFS cameras (AWiFS-A and AWiFS-B) and LISS-4"]
-[5.3648481369018555, 4.828024387359619, "[FF] Supported Signals of the TriG receiver = GPS, Galileo, CDMA GLONASS, Compass"]
-[7.602664947509766, 7.71234655380249, "[TT] Dynamic Range of the XRS = 10^-9 - 10^-3 W/m^2"]
-[5.287654876708984, 8.303128242492676, "[FF] Bandwidth of the Channel = <6000"]
-[6.135716438293457, 7.7052106857299805, "[FF] Signal Amplification Approach of the ATMS = Amplify first and then split into the various channels"]
-[13.358731269836426, 7.747713565826416, "[TT] Energy of the UHF = 1.8 \u00b5eV"]
-[8.213924407958984, 5.646435260772705, "[TT] Range Rate Accuracy of the DORIS = 0.3 mm/s"]
-[11.80661678314209, 3.999354124069214, "[TT] Mezzanine Size of the GHGSat-D = 7 x 18 x 42 cm"]
-[8.699060440063477, 4.470045566558838, "[FF] Magnetometer, 4\u03c0 Sun Sensor, Temperature Sensor of the AOCS = Data are processed in the OBC"]
-[3.5736300945281982, 4.311866760253906, "[FF] Image Location of the SAR = Coastal waters south of Point Arena, California"]
-[6.087978839874268, 3.6891682147979736, "[TT] Task of the Restore-L = Refuel"]
-[9.254931449890137, 1.8695614337921143, "[FF] Ground Resolution of the HARP-2 = Narrow"]
-[8.51627254486084, 8.647906303405762, "[FF] Design Concept of the SHIMMER FTS = Diffraction at the gratings results in a wavenumber-dependent tilt of the wavefronts recombining at the beamsplitter, and interference of the tilted wavefronts creates Fizeau fringes at the instrument's CCD detector"]
-[8.635464668273926, 6.629683494567871, "[TT] Imagery Geolocation Accuracy without GPCs of the WV60 imager = 5.8 m-7.6 m"]
-[9.586791038513184, 9.223008155822754, "[FF] Acquisition Date of the Iris = January 15, 2016"]
-[13.204615592956543, 7.385917663574219, "[TT] Power Consumption (Transmit/Receive Mode) of the NSX = 23.2 W"]
-[5.7645263671875, 4.789313793182373, "[FF] Function of the Data Relay Transponder (DRT) = Receives and relays metrological, hydrological and oceanographic data"]
-[4.628106117248535, 0.6474607586860657, "[TT] INMS Science Unit Interface Control Document Issue Date of the QBITO = Nov. 23, 2015"]
-[3.909769296646118, 2.0006651878356934, "[TT] Launch Vehicle of the ART-XC = Proton rocket"]
-[13.827323913574219, 3.6652183532714844, "[TT] Mass of the SAR ELU = 109.1 kg"]
-[7.172369956970215, 6.659041404724121, "[TT] Detection Efficiency of the GLM = 80%"]
-[3.5509092807769775, 5.213757514953613, "[FF] Endurance of the Low-noise Amplifier = Against SAR signal"]
-[12.173094749450684, -0.22087126970291138, "[TT] Fast Mode Brightness Measurement Interval of the TESS = Every 20 seconds"]
-[8.996910095214844, 7.2369208335876465, "[TT] Group Offset Angle of the Camera = 9.2\u00b0 from the PLM (Payload Module) +Z axis"]
-[9.697705268859863, -0.4587695896625519, "[TT] Altitude of the DMC-3 Constellation = 651 km"]
-[7.924633026123047, 5.602751731872559, "[FF] Use of the 2D map = Great for positional location and relative distance from one feature to another"]
-[7.164371013641357, 2.5427613258361816, "[FF] Editor of the Observation of the Earth and Its Environment = Herbert J. Kramer"]
-[10.81863784790039, -0.2604997754096985, "[TT] Height Error Requirement of the TanDEM-X = 10 m"]
-[7.1047210693359375, 7.205272674560547, "[TT] Laser Pulse Photon Count of the ATLAS = More than 200 trillion"]
-[8.383072853088379, 6.182018280029297, "[TT] Measurement Accuracy - Intensity of the Instrument = 10%"]
-[8.944022178649902, 8.69129467010498, "[FF] Tolerable Misalignment of the Spectrometer Channel = On the order of the slit width"]
-[3.190202474594116, 4.9972920417785645, "[TT] MRS Resolution of the RISAT-SAR = 25 m x 8 m (Az x Range)"]
-[5.526121616363525, 2.274169921875, "[TT] Mission Type of the Solar-B / Hinode = Non-EO"]
-[7.903417110443115, 0.771138608455658, "[FF] Completion Date of the Freshwater Fluctuation = 3 March 2021"]
-[5.550285339355469, 7.102076053619385, "[TT] Global Capacity of the Telesat Lightspeed = 15 terabit/s (Tbit/s)"]
-[4.137438774108887, 6.294885635375977, "[TT] Antenna Type of the ROSA = Directive velocity antenna"]
-[9.990036964416504, 3.1050078868865967, "[FF] Mission of the RSP-00 = Demonstrate technology aimed at electron density measurement and three-dimensional mapping of ionosphere and chip scale (ultra-small) atomic clock for CubeSats"]
-[4.860544681549072, 4.2381768226623535, "[TT] Ground Station Contact of the CanX-2 = Second pass after deployment"]
-[3.523390293121338, -0.8202950358390808, "[TT] Orbit of the SkySat 3 = Sun-synchronous orbit of ~ 500 km"]
-[9.193572044372559, 0.14105309545993805, "[TT] Embankment Height of the Ataturk Dam = 184 m"]
-[5.434407711029053, 1.7064634561538696, "[FF] Ground Segment Design Presentation Date of the EnMAP = March 17-19, 2010"]
-[9.602248191833496, 1.9305124282836914, "[TT] Detection Announcement of the Hubble Space Telescope = 2013"]
-[7.639622211456299, 0.23195579648017883, "[TT] Age of the Ryugu asteroid = 100 million years old"]
-[13.49245834350586, 6.782616138458252, "[TT] Power of the GOMS-1 = 1.5 kW"]
-[5.25292444229126, 3.564577579498291, "[TT] Qualification of the Electronics Components = Space qualified"]
-[4.261849880218506, 7.181509494781494, "[TT] Communication System of the CAPSTONE = S-band telecommunication system"]
-[13.384031295776367, 5.487301349639893, "[FF] Quantity of the Solar array = 3 body mounted and 2 deployable panels"]
-[6.534974098205566, 2.8692739009857178, "[FF] Deployment Method of the SEDS = Deployer system"]
-[9.107909202575684, 4.587203502655029, "[FF] Attitude of the Spacecraft = Spin-stabilized and nominally sun-pointing"]
-[7.751745223999023, 3.6518120765686035, "[FF] Purpose of the Bipods = Minimize the transfer of OBA deformations to the coronagraph structure"]
-[9.71362590789795, 6.2584123611450195, "[FF] Alignment Bias of the Moving Mirror Alignment and Suspension Control System = Offset angle of the moving mirror"]
-[6.9579315185546875, 4.270373344421387, "[FF] Unknown of the DART = Unknown"]
-[6.902544021606445, -0.6349532008171082, "[TT] Orbit Period of the T/P = 112.4 min"]
-[10.394329071044922, 3.2346670627593994, "[TT] Number of CubeSat Units of the SPA\u00bf1 Trailblazer = 1"]
-[5.897057056427002, 3.4789159297943115, "[TT] Number of Spacecraft of the INSPIRE = 2"]
-[11.635127067565918, 6.652201175689697, "[TT] Energy Measurement Range for Nuclei of the Telescope 2 = 4-20 MeV/n"]
-[14.12863826751709, 3.2209222316741943, "[TT] Maximum Allowable Mass of the BeaverCube = 4.8 kg"]
-[5.434137344360352, 8.667640686035156, "[TT] Bandwidth of the Crystal Filter = 3 kHz"]
-[6.002381324768066, -0.47893381118774414, "[TT] Duration of the POCC = Five years renewable"]
-[9.896258354187012, 7.781314849853516, "[TT] Random Acceleration of the PP Twin Telescopes = Up to 88.1g"]
-[11.743766784667969, 3.2744905948638916, "[TT] Thrusters of the MTM CPS = 12 x 10 N bipropellant thrusters"]
-[10.090157508850098, 3.2179791927337646, "[FF] Components of the CubeSat = Off-the-shelf"]
-[8.168521881103516, 5.7001214027404785, "[FF] Sensitivity of the GOLF = 1 mm/s"]
-[5.925203800201416, -0.2753559350967407, "[FF] Mission Duration of the DMSP = Over the past two decades"]
-[7.527502059936523, 7.778181076049805, "[TT] Effective for sensors with few channels of the CAPI = True"]
-[9.451855659484863, 2.3216941356658936, "[TT] Count of the Gigantic Jets = 104"]
-[7.219579696655273, 4.756336212158203, "[FF] Reel in the neck of the net of the Motor Driven Winches = Unknown"]
-[5.045868873596191, 3.5876200199127197, "[TT] Provider of the CVSE = BMDO"]
-[6.174415588378906, 5.371002674102783, "[FF] Type of the Second FPGA = Co-processor"]
-[9.851907730102539, 8.236468315124512, "[TT] FOV of the Telescope = 8.5 x 8.5 arcmin"]
-[6.768057346343994, 6.23909854888916, "[TT] Activation Time of the Initial Mode = 30 minutes"]
-[9.674698829650879, 7.725707054138184, "[TT] Spatial Scale of the Telescope = 2.8 arcsec/pixel"]
-[12.169309616088867, 4.583522796630859, "[TT] Bus Diameter of the LADEE spacecraft = 117 cm"]
-[5.120014190673828, 3.335951805114746, "[TT] Manufacturer of the CAPSTONE = Rocket Lab"]
-[4.803144931793213, -1.8444628715515137, "[FF] Low Frequency Spectrometer (LFS) of the Chang\u2019e-4 Lander = Payload"]
-[6.404979228973389, 2.8153717517852783, "[FF] Purpose of Funding of the Brazilian Ministry of Defense = Buy an undisclosed satellite imaging system for Amazon monitoring, both for civilian and military use"]
-[5.099081039428711, -0.3550325334072113, "[TT] Launch Date of the CBERS-2B = Sept. 19, 2007"]
-[7.434542655944824, 3.6825966835021973, "[TT] Display Type of the NightPod = OLED (Organic Light Emitting Diode)"]
-[3.5200376510620117, -0.7924628853797913, "[TT] Orbital Plane of the CSG and CSK satellites = Same"]
-[6.9627299308776855, 1.8675230741500854, "[TT] Observation Location of the Orbiting Carbon Observatory-2 (OCO-2) = Las Vegas"]
-[4.309616565704346, 7.389793395996094, "[TT] Uplink Frequency of the Communication = S-band"]
-[8.580252647399902, 2.972341299057007, "[FF] Measurement of the MAHRSI = OH distribution in the mesosphere and upper stratosphere"]
-[6.51865291595459, 5.20554256439209, "[FF] Design of the TCS = Incorporates passive and active elements"]
-[7.5584211349487305, 3.5018703937530518, "[FF] Steps of the Level-1 image processing = Radiometric corrections, Geometric corrections"]
-[4.819846153259277, 8.016711235046387, "[TT] Carrier frequency (MHz) of the E6-A = 1278.750"]
-[11.503557205200195, 6.475631237030029, "[TT] Energy Band of the NuSTAR = 5 - 80 keV"]
-[7.289558410644531, 2.74660325050354, "[FF] Purpose of the InSAR = Deformation forecast/monitoring"]
-[5.605785846710205, 2.174184560775757, "[FF] Affiliation of the Hiroyuki Shindou = JAXA"]
-[5.750438213348389, 6.890895366668701, "[TT] Checksum Size of the Raw Science Data Packet = 1 byte"]
-[10.096566200256348, 3.1066737174987793, "[FF] Role of the UNM (University of New Mexico) team = Integrators of the CubeSat"]
-[9.461606979370117, -1.3391401767730713, "[FF] Orbit of the Galileo Navigation = Low-Earth orbit"]
-[10.121878623962402, 7.578452110290527, "[TT] Swath Width of the Imaging Payload = 220 Kilometres"]
-[4.521784782409668, 1.3049633502960205, "[FF] Presentation Date of the AlSat-2 = Oct. 2-6, 2006"]
-[5.774991989135742, 5.020135879516602, "[FF] Supported Protocols of the Standard routers and Frame Relay equipment = UDP/IP"]
-[10.181449890136719, 6.58212423324585, "[TT] South Movement of the Mirror = 1120 \u00b5rad"]
-[4.649630546569824, 7.252206802368164, "[TT] X-band Channels of the Payload = 2 parallel"]
-[3.8530426025390625, 4.482782363891602, "[TT] Collection Capacity of the RADARSAT-2 = Large"]
-[9.202980041503906, 3.0923192501068115, "[FF] Measurement Data of the Solar Orbiter = Solar wind, coronal mass ejection"]
-[3.947824001312256, 4.268841743469238, "[FF] Data Capture of the RADARSAT-2 = From the South Pole to the coast"]
-[4.246014595031738, 7.2142133712768555, "[TT] TT&C Frequency of the Payload = S-band"]
-[8.808176040649414, 3.4463486671447754, "[FF] Measurement Capabilities of the DE-2 = Density, temperature, and winds of ions and neutrals"]
-[11.080333709716797, 3.9324405193328857, "[FF] Sail Size of the Solar Cruiser = 16 times larger"]
-[5.017385005950928, 4.865021228790283, "[FF] Size, Weight and Power (SWaP) of the Small Photon Entangling Quantum System (SPEQS) = Miniaturized"]
-[4.908699989318848, -0.29344677925109863, "[TT] Launch Time of the NeuSAR = 0832 EDT"]
-[7.39984130859375, 4.7292609214782715, "[FF] Oscillation Modes of the Gaia = Radial and Nonradial"]
-[10.350615501403809, 4.2096028327941895, "[TT] Number of Degrees of Freedom of the Grid Fins = Two"]
-[3.5338010787963867, -0.7789162397384644, "[TT] Orbit Type of the Rideshare mission = SSO (Sun-Synchronous Orbit)"]
-[7.939097881317139, 4.251780033111572, "[TT] Instrument type of the LRR (SeaSat) = Precision orbit"]
-[6.478037357330322, -0.23808453977108002, "[TT] Observation Duration of the Observation Region = One year"]
-[10.158178329467773, 4.504751205444336, "[FF] Momentum Wheel of the DSAT-2 = Activated just before leaving the platform"]
-[4.921713829040527, 1.93942391872406, "[FF] Mission Status of the TanSat = Complete"]
-[9.52688980102539, 8.072189331054688, "[TT] f/number of the 1000 mm camera = f/11"]
-[10.228744506835938, 8.341617584228516, "[TT] Pupil Diameter of the Telescope = 75.6 mm"]
-[8.448057174682617, 2.1364800930023193, "[FF] Deep-Space Calibration of the WindSat = Not provided"]
-[7.474118709564209, -0.556307852268219, "[FF] Date of the NASA IceBridge Flight = 23 October 2018"]
-[8.374166488647461, 7.181077480316162, "[TT] Imaging System of the NewSat = Panchromatic imager"]
-[4.939919948577881, 7.845778465270996, "[TT] Wide Band Mode of the Receiver = \u00b1 10.0 kHz (- 3 dB )"]
-[11.894571304321289, 5.546277046203613, "[TT] Pore Size of the ICON FUV Instrument = 6 mm"]
-[10.647829055786133, 2.008204698562622, "[FF] Measure of Precision Cosmology of the Gravitational Weak Lensing = Yes"]
-[8.288753509521484, 1.7707514762878418, "[TT] Spatial Resolution of the Sea Surface Temperature (SST) = 15 km"]
-[11.115028381347656, 5.709496974945068, "[FF] Type of the LAM = Liquid"]
-[10.122210502624512, 2.7793831825256348, "[TT] Flight Nanosats Quantity of the SMDC-ONE program = 8"]
-[4.295528888702393, 1.2186264991760254, "[FF] Revisit Time of the SEOSAT-Ingenio = Within three days"]
-[12.160062789916992, -0.12955592572689056, "[TT] Camera of the TESS = 4 cameras"]
-[6.711580276489258, 3.980271577835083, "[TT] Operation Location of the ERNO-Box = Columbus module of the ISS"]
-[11.564532279968262, 3.359687566757202, "[TT] Flight Time for Ions of the COSIMA = 16 \u00b5s"]
-[8.217849731445312, -0.24036124348640442, "[TT] Global Sea Level Rise Contribution from Greenland and Antarctic ice sheets of the GRACE = 1.2 mm per year"]
-[5.620041847229004, 5.942895412445068, "[FF] Memory Types of the CIB = EEPROM and SRAM"]
-[3.432051420211792, 3.616950035095215, "[FF] Operational Status of the PAZ = Unknown"]
-[8.594327926635742, 0.6562528014183044, "[TT] Debris Field Location of the Vikram Lander = About 750 meters northwest of the main crash site"]
-[6.337439060211182, 5.539921760559082, "[FF] Mission Goal of the OICETS = Conduct interorbit laser communications experiments with ARTEMIS of ESA"]
-[9.689335823059082, 4.878122806549072, "[TT] Stabilization of the Tsubame = 3-axis"]
-[3.8334193229675293, -0.6226068735122681, "[TT] Mission Service of the Bartolomeo = Fast, cost-efficient and reliable access to low Earth orbit"]
-[7.876713752746582, 7.13312292098999, "[TT] Data Recording of the Photometers (MCP-PH) = On triggering alerts only"]
-[10.974581718444824, 4.051556587219238, "[TT] Enclosure Shape of the CanX-7 = Circular"]
-[8.276854515075684, 5.413390636444092, "[TT] Calibration of the MIS Instrument = 2-point"]
-[9.283018112182617, 5.155220985412598, "[TT] Alignment of the GT = Nominally aligned with the spacecraft axes"]
-[10.507119178771973, 6.618696212768555, "[TT] Degree of nesting (mirror shells/module) of the Mirror = 54"]
-[3.8113324642181396, 4.490823745727539, "[FF] SAR Imagery of the RADARSAT-2 = Vessel Detection Applications"]
-[9.728432655334473, 2.375426769256592, "[FF] Total Effective Area of the NuSTAR = Unknown"]
-[3.4634625911712646, -0.9070987105369568, "[TT] Orbit Type of the SPOT 1-5 = Sun-synchronous"]
-[6.87087869644165, -0.6214761137962341, "[TT] Orbital Period of the ADEOS = 100.8 minutes"]
-[4.945981502532959, 8.204511642456055, "[FF] Frequency Bands of the CITRIS = 401.25 and 2036.25 MHz, 150, 400 and 1067 MHz"]
-[5.61320161819458, 5.598304271697998, "[FF] Communication Links of the SSR = UART link to OIM module, high speed differential LVDS links to XBT subsystem and IRIS and PPU payloads"]
-[11.804940223693848, 6.72257137298584, "[TT] Energy Range of the EPD-I = 50 keV \u2013 300 keV"]
-[5.5371551513671875, 7.08798360824585, "[TT] Telemetry Rate of the Langmuir Probe = 80 kbit/s"]
-[3.532128095626831, 4.786566734313965, "[FF] Precision of the Synthetic-aperture radar phase interferometry = Up to two orders of magnitude better than speckle tracking"]
-[6.2757978439331055, 8.648544311523438, "[TT] Polarisation of the DPS = HH, VV, HV, VH"]
-[14.220646858215332, 3.13272762298584, "[TT] Mass of the SOHLA-1 = 50 kg"]
-[3.8744590282440186, -2.1719369888305664, "[FF] Use Case of the Specialized Asset Trackers = Knowing where your assets are and how your assets are being treated"]
-[6.1279616355896, 2.5150303840637207, "[FF] Radiation Environment Analysis of the HAUSat-2 = Implemented"]
-[7.295560359954834, 8.025301933288574, "[TT] Dynamic range of the Channel = approx. 4-320 K"]
-[6.712112903594971, -0.006823957897722721, "[TT] Observation Cycle of the Landsat-8 = Every eight days"]
-[9.285642623901367, 3.1336517333984375, "[FF] Purpose of the WISPR = Study the solar wind"]
-[4.610281944274902, 4.783173561096191, "[FF] Intended Use of the AIS = Maritime traffic awareness, collision avoidance, vessel traffic management"]
-[6.015361309051514, 5.100180625915527, "[FF] Symposium Presentation Date of the Centralized Computation Service Architecture = April 4-8, 2005"]
-[6.740715980529785, 5.331408977508545, "[FF] Components of the BSA = BSMFE, BSME, BSH"]
-[9.03605842590332, 8.151776313781738, "[TT] IFOV/line (pixels/scan line) of the SBUS = 240"]
-[11.676368713378906, 3.3439173698425293, "[TT] Maximum Thrust of the Field Emission Electric Propulsion System = 350 micronewtons"]
-[5.77091121673584, 3.7829742431640625, "[TT] Constellation Size for Weekly Remapping of the Satellite Constellation = About 90 satellites"]
-[3.443657159805298, 6.430500507354736, "[TT] Pixel Size (km x km) of the Antenna = 8"]
-[9.703042030334473, -0.8641281723976135, "[TT] Orbit of the PARASOL = Lower orbit (3.9 km below the orbit of the A-train)"]
-[9.360505104064941, 4.805179595947266, "[FF] Activation Sequence of the Attitude Determination and Control System = Enabled and sensors are given a warm-up period"]
-[11.850374221801758, 6.61114501953125, "[TT] Neutron Energy Range of the Natalya-2M = 20 \u2013 300 MeV"]
-[7.365539073944092, 1.030951738357544, "[FF] Purpose of the Lunar Pathfinder = Perform satnav fixes in lunar orbit"]
-[11.476943969726562, 4.376498699188232, "[FF] Size of the HyperScout = Milk-carton-sized"]
-[5.156652450561523, 2.3180391788482666, "[TT] Mission Type of the FITSat-1 = Non-EO"]
-[6.256026268005371, 4.901288032531738, "[FF] Function of the OBCS = Main flight computer which runs the flight software (FSW)"]
-[3.762209177017212, 5.222952365875244, "[TT] Imaging Frequency Band of the TanDEM-X = X"]
-[5.146485328674316, 3.2064249515533447, "[FF] Export License of the DASA/DSS = Refused by the German government"]
-[7.994901180267334, 7.931751251220703, "[FF] Payload of the STACEM = Miniaturized multi-spectral payload for the acquisition of imagery in the visible and near infrared wavelengths and hyperspectral channels"]
-[13.99598217010498, 3.3785274028778076, "[TT] Mass of the ChipSats = Just a few grams"]
-[11.395805358886719, 8.926112174987793, "[TT] Image Acquisition Date of the MODIS = May 16, 2022"]
-[8.87664794921875, 9.567995071411133, "[FF] Band 3 Wave Numbers of the TANSO-FTS-2 = 4200 - 5200"]
-[5.231738090515137, 3.176107406616211, "[TT] Program Manager of the ATMS = Danielle Gallegos"]
-[8.29732608795166, 0.7642965912818909, "[TT] Firefighters of the Calf Canyon-Hermits Peak fire = 1,800"]
-[9.583272933959961, 2.901242256164551, "[FF] Understanding of the Galactic Cosmic Rays = Remains poorly understood and controversial"]
-[5.610031604766846, 1.1858810186386108, "[FF] RF Model Date of the MTG-I = 03 July 2019"]
-[11.635878562927246, 4.862888336181641, "[TT] Diameter of the Collector = 73 cm"]
-[10.116174697875977, 5.487030029296875, "[FF] Operation of the SIMBA = Looks down at Earth for a long time to see what temperature it stabilizes at"]
-[10.086968421936035, -1.5567148923873901, "[TT] Inclination of the Anand = 97.4\u00b0"]
-[5.234941482543945, 2.668545961380005, "[FF] Program of the MYriade = Performances, Missions, Tool for education and cooperation"]
-[7.907525539398193, 5.299915790557861, "[FF] Parameter of the FLLS = High-accuracy, displacement-measuring sensor"]
-[3.443936824798584, -0.8967049717903137, "[TT] Orbit of the IRS-1B = Polar sun-synchronous orbit"]
-[6.25821590423584, -0.5140045881271362, "[TT] Years on Orbit of the RADARSAT-2 = 6 years"]
-[11.743638038635254, 7.519335746765137, "[FF] Observation Period of the Megha-Tropiques = December 28, 2013 to January 4, 2014"]
-[9.5363130569458, 9.025005340576172, "[TT] Spectrograph Slit Width of the IRIS = 0.33 arcsec"]
-[7.027073383331299, 7.744476795196533, "[TT] Number of Optical Retro Reflectors of the ANDE-2 = 30"]
-[8.501047134399414, 7.417532920837402, "[TT] Data Size of the Camera = 14 bit/pixel"]
-[5.993509292602539, 1.5373947620391846, "[TT] Mission Start Date of the EURECA = August 7, 1992"]
-[8.912053108215332, 3.209129571914673, "[FF] Imaging Capability of the ICON = Provide the ability to explain how these drivers set the stage for the extreme conditions of solar-driven magnetic storms"]
-[4.746609210968018, 0.917136013507843, "[TT] PDR Date of the PROBA-3 = Fall of 2012"]
-[6.317649841308594, 8.064945220947266, "[TT] Number of Channels of the ABI = 16"]
-[4.624706745147705, 2.9385461807250977, "[TT] Science Operations Centre Location of the Integral = ESAC, Madrid"]
-[4.2238898277282715, 0.7517735958099365, "[TT] Launch Date of the EDRS-C = 6 August 2019"]
-[7.571417808532715, 6.85543966293335, "[TT] Wavelength Stability of the LRI (Laser Ranging Interferometer) = Excellent"]
-[4.394252777099609, 5.425176620483398, "[TT] Deployment Date of the GomX-3 = 5 October 2015"]
-[10.591320037841797, 4.935912609100342, "[TT] Boom Length of the Langmuir Probe = 50 cm"]
-[14.451278686523438, 6.55799674987793, "[TT] Battery Backup Duration of the IMPS = 90 days"]
-[11.768281936645508, 3.256157398223877, "[TT] Thrust of the RCS (Reaction Control System) = 1 N"]
-[6.358996391296387, 3.333350896835327, "[TT] Number of Satellites of the BlackSky = 2"]
-[3.4066519737243652, 6.420014381408691, "[TT] Pixel Size (km x km) of the Antenna = 11"]
-[4.244182586669922, 3.330312728881836, "[TT] CEO of the Galileo 2nd Generation Satellites = Herv\u00e9 Derrey"]
-[5.6113457679748535, 5.654567241668701, "[FF] Method of the Data Transmission = Placing it into an ftp-site with password protection"]
-[11.030936241149902, 1.4607948064804077, "[TT] Mass of the Starshine-2 = Same as Starshine-1"]
-[9.482834815979004, 7.953161716461182, "[TT] Optics Lens Focal Length of the NEA Scout Camera = 50.2 mm"]
-[8.97873592376709, 4.4951043128967285, "[TT] Quantity of the SAS (Sun Acquisition Sensor) = 6"]
-[7.738918304443359, 1.3654507398605347, "[FF] Target Applications of the ROSE-L = Measurement of surface deformation of vegetated terrain, soil moisture, land cover classification, crop type discrimination, Polar ice sheets and ice caps monitoring, sea-ice conditions monitoring, European maritime situational awareness"]
-[5.335450649261475, 0.5036070942878723, "[TT] Operational Date of the MaSat-1 = Feb. 2014"]
-[4.615062236785889, 7.493784427642822, "[TT] Data Rate of the VHF COTS transmitter = 1200 to 9600 bit/s"]
-[10.374679565429688, 3.219346284866333, "[TT] Quantity of the CubeSats = 2"]
-[5.817533493041992, -2.254218816757202, "[TT] Ground Target Coverage of the KOMPSAT-5 = Up to 490 km width in a single orbit"]
-[6.335922718048096, 1.4504590034484863, "[FF] URL of the Swarm = https://earth.esa.int/c/document_library/get_file?folderId=131556&name=DLFE-3101.pdf"]
-[5.307401180267334, 3.8289430141448975, "[TT] Number of Satellites of the MetOp-SG = 6"]
-[8.310858726501465, 2.4856326580047607, "[FF] Primary Objective of the CATS = Continue the CALIPSO aerosol and cloud profile data record"]
-[7.019720077514648, 4.966598033905029, "[FF] Function of the FPGA Code = Did not allow the motor to move without a valid home command"]
-[4.66072416305542, 7.971591472625732, "[TT] Frequency Band of the TT&C = 435-438 MHz"]
-[8.035228729248047, 9.03181266784668, "[TT] Spectral Range of the TOMS = 312-380 nm"]
-[9.555473327636719, 0.6644521355628967, "[TT] Test Transmission Distance from Earth of the Herschel = 280,000 km"]
-[5.791443824768066, 5.962500095367432, "[TT] TM/TC Interface of the RAMIS = RS-485"]
-[5.7131242752075195, -0.833346426486969, "[TT] Design Life of the TRACE = 1 year"]
-[9.026449203491211, 5.318484306335449, "[TT] Inertial Measurement Unit of the ADCS = 1"]
-[5.651151180267334, 7.06521463394165, "[TT] Data Rate of the Payload Imagery = 32.72 Mbit/s"]
-[13.549825668334961, 5.860644340515137, "[TT] Power Output of the Solar Arrays = > 330 W"]
-[5.813217639923096, 5.390028953552246, "[TT] Redundancy of the TT&C Transmitter = Half Satellite"]
-[6.061866760253906, -0.5120951533317566, "[TT] Planned Science Mission Duration of the GOLD = Two years"]
-[11.33087158203125, 5.902499675750732, "[TT] Material of the WISA Woodsat = Plywood"]
-[5.90207052230835, 5.189960479736328, "[FF] Functions of the ARF = Second level of synchronization, generation of ISP files and routing to the Nominal PDGS or the Defence one"]
-[8.51633071899414, 6.125278949737549, "[TT] Accuracy of the CERES = 0.8 Wm -2  sr -1"]
-[4.875375270843506, 7.454360008239746, "[TT] C/N of the Downlink (Ku-band) = 96.862 dB"]
-[7.028942108154297, 4.255913734436035, "[FF] Eclipsing of the TIC 168789840 = Sextuply"]
-[5.64725399017334, 7.0876688957214355, "[TT] Data Rate of the MBA subsystem = Up to 24 Mbit/s"]
-[8.796142578125, 0.3913729190826416, "[TT] Formation of the Equatorial Ridge = During a period when it only took Ryugu 3 hours to rotate"]
-[4.667079448699951, 0.5377817153930664, "[TT] Launch Date of the Mey-Lin (C6) = 15th April"]
-[4.970617771148682, 6.080124378204346, "[TT] Protocol of the High-speed link = AX.25 packet protocol"]
-[7.030336856842041, 8.11617374420166, "[FF] Definition of the Signal to Noise Ratio (SNR) = Commensurate with the overall uncertainty required by the application and its observational characteristics"]
-[6.672527313232422, 5.306085109710693, "[FF] Function of the DPP = Digitizes the preamplifier output, applies real-time digital processing to the signal, detects the peak amplitude, and bins this in its histogram memory"]
-[5.502592086791992, 7.793163299560547, "[TT] Transmit EIRP of the Wide Beam = 36 dBW"]
-[8.43520736694336, 6.966197490692139, "[TT] Camera Operation of the ResourceSat-2 = 'pushbroom scanning' concept"]
-[8.976018905639648, 0.46587225794792175, "[TT] Size of the Boulder = 10 m-wide"]
-[5.422502517700195, 0.20510177314281464, "[TT] Mission Status of the IRS-P6 = Mission Complete"]
-[5.819748878479004, 2.957707166671753, "[TT] Mission Cost Cap of the IMAP = $492 million"]
-[3.5841867923736572, 1.5880658626556396, "[FF] Presentation Date of the GMES Missions Sentinel-4, Sentinel-5 and Sentinel-5p = June 18-22, 2012"]
-[4.898653984069824, 0.9047713875770569, "[TT] Contract Signing Date of the Alphabus = June 2005"]
-[7.358917713165283, 5.272469997406006, "[TT] Position of the DSCOVR = L1"]
-[5.470672130584717, 6.364778518676758, "[TT] Volatile Mass Storage of the ECS = 10 GByte"]
-[11.745072364807129, 4.9164509773254395, "[TT] Size (mm) of the M2 = 147 x 118"]
-[12.06955337524414, 4.4980878829956055, "[TT] Size of the Spacecraft = 5.5 m x 6.6 m x 2.8 m"]
-[3.3807501792907715, 1.4715858697891235, "[TT] Launch Date of the Sentinel-2B = March 2017"]
-[7.718729019165039, 5.608893394470215, "[FF] Control System of the Shutter = Control loops and position encoder"]
-[9.058585166931152, 7.341078758239746, "[TT] Demonstration Contrasts of the CGI = Below 5 x 10-9 for SPC bowtie mode, Below 1 x 10-9 for HLC mode"]
-[8.89922046661377, 7.604693412780762, "[TT] Pixel Size of the pnCCD camera = 75 \u00b5m by 75 \u00b5m"]
-[8.409585952758789, 5.477607727050781, "[TT] Geolocation Accuracy of the LEOSAR = 2km"]
-[5.565554141998291, 4.537482738494873, "[FF] Revival Possibility of the MarCO = Uncertain"]
-[9.533549308776855, 4.6653547286987305, "[TT] Control Law of the ADCS = B-dot control law"]
-[6.401909351348877, 1.3883668184280396, "[TT] Leaders of the Cosmological Simulations Working Group = Pablo Fosalba (ICE, IEEC-CSIC) and Romain Teyssier (Institute for Computational Science at the University of Zurich)"]
-[8.487149238586426, 3.2425413131713867, "[FF] Purpose of the MAHRSI = Measure ultraviolet radiation emitted and scattered by the Earth's atmosphere"]
-[5.158999919891357, 6.999316692352295, "[TT] Downlink Data Rate of the EROS-A = 70 Mbit/s"]
-[7.034107685089111, 4.441412925720215, "[FF] Not specified of the HTSSE-II = Not specified"]
-[3.7727980613708496, 2.3393025398254395, "[TT] Targeted Date of the Iridium-5 = March 29, 2018"]
-[13.613704681396484, 1.7628926038742065, "[TT] Cargo Capacity of the Dragon = Over 1630 kg"]
-[10.030901908874512, 2.636705160140991, "[TT] Inclination of the NanoRacks-QB50 CubeSats = 51.6\u00ba"]
-[16.549034118652344, 3.64316463470459, "[TT] Planned OneWeb Constellation Size of the Airbus = 648-satellite"]
-[5.881685733795166, -0.41258305311203003, "[TT] Deployment Time of the TechEdSat = 60 minutes"]
-[7.011034965515137, 5.276452541351318, "[FF] Components of the C&DH Subsystem = IEM (Integrated Electronics Module), PIE (Payload Interface Electronics), SSR, and two OCXO (Oven Controlled Crystal Oscillators)"]
-[13.387070655822754, 2.849790573120117, "[TT] Adapter and Separation System Mass of the ALMASat-1 = 20.5 kg"]
-[8.422417640686035, 6.132704734802246, "[TT] Radiometric Absolute Accuracy of the AVNIR = \u00b110%"]
-[9.31613540649414, 5.124260425567627, "[TT] Attitude Pointing Accuracy of the AOCS = \u2264 0.4\u00ba (3\u03c3)"]
-[8.821653366088867, 0.9562332630157471, "[FF] Award Date of the Parker Solar Probe = 1 July 2021"]
-[5.441577434539795, 0.5006713271141052, "[TT] Launch Year of the NuSTAR = 2012"]
-[9.795960426330566, 7.622070789337158, "[TT] Along-Track Slit Width of the Nadir Sensor Wide-Field Telescope = 0.27\u00ba"]
-[5.339287757873535, 0.2780954837799072, "[FF] Heritage of the DOSTEL = Mir station (Oct. 1997 - Jan. 1998), Shuttle flights STS-76, -81, and -84, US Lab of the ISS (March to August 2001)"]
-[8.168255805969238, 1.2042442560195923, "[TT] Seismometer of the InSight Lander = SEIS (Seismic Experiment for Interior Structure)"]
-[13.831063270568848, 3.0701422691345215, "[TT] Mass of the Payload = 1300 kg"]
-[6.817188739776611, 4.567359924316406, "[FF] Application of the Supercapacitors = Space"]
-[10.103352546691895, 1.3016390800476074, "[TT] Arrival Time of the Dwarf galaxies in the new study = In the last few billion years"]
-[13.524683952331543, 5.774758815765381, "[TT] Voltage of the Solar Panels = 6.9 V"]
-[10.066784858703613, 5.600050926208496, "[FF] Thermal Environment After Separation of the MMO = High temperature, illuminated by sunlight"]
-[9.605006217956543, 3.7209765911102295, "[FF] Operating Principle of the GMR = Change in electrical resistance experienced by a multilayer structure in the presence of a magnetic field"]
-[9.479789733886719, 7.34811544418335, "[TT] Resolution Requirement of the Optical System = 30 cm ground sampled distance"]
-[9.05507755279541, 5.108651638031006, "[TT] Accuracy of the Rate gyro = 0.02\u00ba/s"]
-[9.415218353271484, -1.017937421798706, "[TT] Orbit Longitude of the SASAR INSAT-2 = 93.5\u00ba E"]
-[11.814943313598633, 0.0760665088891983, "[FF] Observation Method of the TESS = Measured the \u201cwobble\u201d of the star, caused by the gravitational tugs from orbiting planets (radial velocity)"]
-[12.82088565826416, 7.612791061401367, "[TT] Power of the Instrument = < 17 W"]
-[4.89420223236084, 1.0898652076721191, "[TT] Launch Year of the ALOS-2 = 2014"]
-[7.9969305992126465, -0.7244294881820679, "[TT] Radar of the CryoSat-2 = Measures height by sending out signals and timing how long they take to reflect off Earth\u2019s surface and return to their respective satellites"]
-[10.432526588439941, 5.695423603057861, "[TT] Equilibrium Temperature of the TOI 270 b = Around 490 \u00ba Fahrenheit (254\u00baC)"]
-[3.368419647216797, 1.4825568199157715, "[FF] Launch Date of the Sentinel-1A = 2013+"]
-[7.472288131713867, 3.979329824447632, "[TT] Type of the Radio-occultation instrument = Radiomet"]
-[10.134615898132324, 1.4690207242965698, "[TT] Official Name of the Whirlpool galaxy = M51a"]
-[7.084591865539551, 4.316760540008545, "[FF] Unknown of the SFE (Scatterometer Front End) = Unknown"]
-[6.286395072937012, 6.224806785583496, "[TT] Part Quantity of the DAQ (Data Acquisition) System = 2"]
-[7.605356693267822, 6.636575222015381, "[TT] Distribution of the MET data = HRIT/LRIT transmission within 15 minutes after image acquisition"]
-[10.460528373718262, 2.196133613586426, "[TT] Survey Frequency of the ART-XC telescope = Eight all-sky surveys for the next four years"]
-[10.54843807220459, 6.5643181800842285, "[TT] Number of mirror modules of the Mirror = 7"]
-[16.552724838256836, 3.644523859024048, "[TT] Number of Satellites of the OneWeb = 650"]
-[8.180624008178711, 1.1848770380020142, "[FF] Workshop Report URL of the Soil Moisture Active Passive (SMAP) = http://nasascience.nasa.gov/earth-science/decadal-surveys/Volz1_SMAP_11-20-07.pdf"]
-[8.076729774475098, 4.496387958526611, "[FF] Component of the Electromagnetic Calorimeter (ECAL) = Unknown"]
-[9.488572120666504, 4.950759410858154, "[TT] Attitude Control System Stability of the CFESat = Up to 60% of the orbit"]
-[5.492051124572754, 2.241222381591797, "[FF] Affiliation of the David Granena = Unknown"]
-[5.5960469245910645, 5.719408988952637, "[TT] CPU of the SHU = HD64F7145FW50"]
-[7.921032428741455, 2.521435022354126, "[FF] Product of the LMI = Derived Motion Winds, Lightning Detection, Rainfall Rate /QPE, Convective Initiation, Tropopause Folding Turbulence Prediction, Sea Surface Temperature (skin), Fire/Hot Spot Characterization, Land Surface (Skin) Temperature, Land Surface Emissivity, Snow Cover"]
-[14.047219276428223, 3.3821043968200684, "[TT] Mass Resolution of the GEMS = 1/50"]
-[9.689459800720215, 8.369913101196289, "[TT] Corrected FOV of the SPARCS = 1\u00b0"]
-[6.326138973236084, 5.828954219818115, "[TT] Internal Trays of the GNB = 2"]
-[4.200474262237549, 2.5446701049804688, "[TT] Launch Site of the SpaceX CRS-13 = Cape Canaveral SLC-40"]
-[6.0870585441589355, 1.5555387735366821, "[FF] Status Report Date of the Space Situational Awareness = Oct. 8, 2015"]
-[3.4207403659820557, 4.888305187225342, "[TT] Development Company of the SAR Processor = MDA (MacDonald Dettwiler)"]
-[5.508203983306885, 1.0832147598266602, "[FF] Functional Demonstration Date of the OHB Telecommunications Satellite = June 2, 2017"]
-[4.397475719451904, 2.9145326614379883, "[FF] Location of the GS operators = Wallops, VA"]
-[8.587860107421875, 1.147895097732544, "[TT] Global Coverage of the Aquarius = Monthly"]
-[6.543486595153809, -1.2312649488449097, "[FF] Data Continuity of the GRACE-FO = Continuation of GRACE data record"]
-[6.938991546630859, 1.2504785060882568, "[FF] Conference Date of the Pico Satellite Solar Cell Testbed = May 7-12, 2006"]
-[5.1769185066223145, 3.6166677474975586, "[TT] Camera Supplier of the OPTSAT 3000 = Elop"]
-[9.825469970703125, 4.185765266418457, "[TT] Nominal Magnetic Moment of the MTs = 1 Am2"]
-[9.73458194732666, 5.7619147300720215, "[TT] FUS Baseplate Tilt of the LCT = 15\u00ba"]
-[3.2132999897003174, 1.6657980680465698, "[TT] Separation Time of the Sentinel-2B = 57 min 57 seconds"]
-[11.391186714172363, 4.329006671905518, "[TT] Size of the EQUULEUS = 6U"]
-[7.011937618255615, -0.8051828742027283, "[TT] Orbital Period of the Beta Pictoris b = 21 years"]
-[5.267297744750977, 4.664364337921143, "[TT] Redundancy Requirement of the SpaceLink = 4 satellites"]
-[7.646485328674316, 0.8143380284309387, "[FF] Objective of the CRaTER = Characterize the global lunar radiation environment and its biological impacts"]
-[9.020806312561035, 5.635620594024658, "[TT] X Axis Alignment of the SSM = Downward and aligned to local vertical within 0.01 degree"]
-[8.632545471191406, 7.8915839195251465, "[TT] Spectral Range of the LWIR Cameras = 7.5 - 13.5 \u00b5m"]
-[8.401694297790527, 2.878858804702759, "[FF] Atmosphere of the NRLMSISE\u201000 = Statistical Comparisons and Scientific Issues"]
-[6.794867038726807, 1.9768314361572266, "[FF] Mission Prediction of the Roman Space Telescope = Find 100,000 Transiting Planets"]
-[9.633116722106934, 5.356514930725098, "[TT] Period of the Lateral Shearing Angular Period = 200 \u00b5rad"]
-[6.24342155456543, 3.4054622650146484, "[TT] Number of Satellites of the BlackSky Satellite Constellation = 14"]
-[10.5472412109375, 4.924291133880615, "[TT] Manufacturer of the Langmuir Probe = Utah State University"]
-[9.895126342773438, 2.574251651763916, "[TT] Number of Referred Papers Produced of the HaloSat = 7"]
-[9.359362602233887, 6.887759685516357, "[TT] Range Resolution of the SIRAL = Approximately 0.45 m"]
-[5.752813339233398, 2.464406728744507, "[FF] Objective of the LAPAN-A3/IPB = Monitor food resources in Indonesia and provide environmental monitoring"]
-[4.245611190795898, 3.9226489067077637, "[TT] Signal Components of the Galileo = 10"]
-[11.522039413452148, 3.385000228881836, "[FF] Technology Demonstrations of the BeaverCube = Use of low-cost commercial cameras to obtain measurements and operation of Tiled Ionic Liquid Electrospray (TILE) propulsion technology"]
-[5.788437843322754, 4.174181938171387, "[FF] Purpose of the LacunaSat2-B = Provides global connectivity for Internet-of-Things devices"]
-[3.990885019302368, 4.307878017425537, "[FF] Maintenance Policy of the RADARSAT-2 = Adopted early in development"]
-[9.902413368225098, -1.3679014444351196, "[FF] Orbit of the Dnepr Launch Vehicle = Sun-synchronous orbit, altitude altitude = 700 km, inclination = 98.25\u00ba"]
-[9.115134239196777, 4.291858196258545, "[FF] Three-axis accelerometer of the Spacecraft = Mounted to the inside face of each solar panel"]
-[5.853482723236084, 0.5392320156097412, "[FF] Drift Start Date of the ERS-2 = After the completion of the tandem mission"]
-[9.331521987915039, 5.099431991577148, "[TT] Nominal Attitude of the AOCS = Nadir orientation"]
-[5.566779613494873, 2.3884775638580322, "[FF] Affiliation of the \u015eiir K\u0131lk\u0131\u015f = Urban Knowledge-Action Committee Network"]
-[6.477334976196289, 7.599987983703613, "[TT] Data Quantization of the GIIRS = 13 bit"]
-[8.173232078552246, 6.631199359893799, "[TT] Manufacturer of the Advanced Baseline Imager = L3Harris Technologies"]
-[5.970117568969727, 8.753986358642578, "[TT] MTF of the Instrument = > 0.2 @ Nyquist frequency"]
-[4.908518314361572, 0.5949685573577881, "[TT] Launch Date of the NRCSD = January 9, 2014"]
-[7.895835876464844, -0.331163614988327, "[TT] Date of the Arctic Sea Ice = 19 April 2021"]
-[11.204379081726074, 4.11954402923584, "[FF] Failure Cause of the COPV = Accumulation of oxygen between the COPV liner and over-wrap in a void or a buckle in the liner"]
-[9.100510597229004, 7.012077808380127, "[TT] Spatial Resolution of the DMC-3 = 1 m"]
-[9.3362398147583, 4.8378472328186035, "[TT] Function of the Startrackers = Provide attitude information"]
-[4.045012474060059, 1.8102585077285767, "[TT] Launch Provider of the H-IIA launch vehicle No. 37 = Mitsubishi Heavy Industries, Ltd."]
-[3.179255962371826, 2.3243401050567627, "[FF] User Consultation Working Groups of the Sentinel-1 = Marine Core Services, Land Monitoring and Emergency Services"]
-[6.155040740966797, 4.380674362182617, "[FF] Inputs of the Active Schedule = Mission Timeline, LMOC downtimes, OGS availability schedules, external interfaces availability, predictive avoidance constraints, experiment plans, user service requests"]
-[6.215068817138672, 3.0812292098999023, "[FF] URL of the BlackSky = http://www.blacksky.com/"]
-[9.580735206604004, 4.916217803955078, "[TT] Stabilization of the AOCS = 3-axis"]
-[8.8174409866333, 0.9171541333198547, "[FF] Publication Date of the Parker Solar Probe = 10 January 2022"]
-[6.6544108390808105, 0.7823840975761414, "[TT] Date of the Solar Eclipse = 21 August 2017"]
-[11.55620288848877, 4.8216071128845215, "[TT] Top Diameter of the Carrot Sprites = 15 km"]
-[8.232965469360352, 0.10947570949792862, "[FF] Mission Type of the Meteor-1/Meteor-2/Meteor-Priroda Series = EO"]
-[4.37839412689209, 4.269044399261475, "[TT] Number of GEOSAR satellites of the COSPAS-SARSAT system = 5"]
-[10.347505569458008, 4.499889850616455, "[TT] Quantity of the Reaction Wheels = 4"]
-[10.485501289367676, 2.1919355392456055, "[FF] X-ray Blocking Property of the SS 433 = Acts like lead paneling"]
-[7.77376651763916, 6.517505645751953, "[TT] Mode 3 Imaging Frequency of the ABI = 1 FD image, 3 CONUS and 30 Mesoscale images, every 15 minutes"]
-[8.2808837890625, -0.055098216980695724, "[TT] Sea Level Rise of the GRACE-FO = 2.2 millimeters in two months"]
-[8.93405818939209, 5.364709377288818, "[TT] Relative Motion of the GOMX-3 = About 1 m/s"]
-[5.408735752105713, -0.10256719589233398, "[TT] Arrival Time at Space Station of the Cygnus = Around 6:10 a.m. Thursday, Aug. 12"]
-[10.875946998596191, 7.509210109710693, "[TT] Swath Width of the ERIP = 170 km"]
-[5.2302470207214355, 4.7389655113220215, "[TT] Type of the Tri-GNSS (GPS+Galileo+GLONASS) = GNSS"]
-[10.294601440429688, -0.3029067814350128, "[TT] Altitude of the Tandem-L satellites = 745 km"]
-[6.444875717163086, 3.523074150085449, "[FF] Access of the HTV = ISS crew will be able to enter and remove the supplies"]
-[6.022506237030029, 5.236373424530029, "[TT] Designation of the DFACS = DFACS (aka AACS)"]
-[5.28302526473999, 2.934950113296509, "[FF] Entities of the GMES program = ESA, CNES, DLR, EUMETSAT, ASI, INTA, CSA, DMCii"]
-[8.285284042358398, 7.163246154785156, "[FF] Microchannel Plate Detector of the CID = Records the impact of the particles"]
-[10.18787670135498, 0.9776617884635925, "[TT] Distance from Earth of the Cassiopeia A = 11,000 light-years"]
-[4.742883682250977, 6.808165073394775, "[TT] Payload Uplink of the Dove-2 = 30 kbit/s over 2.4 GHz radio"]
-[3.645458221435547, 2.806659460067749, "[TT] Number of Atomic Clocks of the IRNSS = 3 per satellite"]
-[10.05551528930664, -1.5959833860397339, "[TT] Inclination of the CBERS-2B = 98.5\u00ba"]
-[5.925375461578369, 3.507918357849121, "[FF] Goal of the IRAS project = Reduce manufacturing costs for satellites by using commercial components"]
-[10.309218406677246, 5.76832914352417, "[TT] Maximum Operating Temperature of the RDM Sensor = +80\u00baC"]
-[7.370302200317383, 2.9035589694976807, "[FF] Mission Purpose of the MethaneSAT = Provide global emissions data"]
-[8.419977188110352, 2.0209226608276367, "[FF] Scatterometer of the CYGNSS = OSCAT and ASCAT"]
-[10.13944149017334, 1.030051589012146, "[TT] Distance from Earth of the GRB 150101B = About 1.7 billion light years"]
-[13.687666893005371, 5.791215419769287, "[TT] Solar Panel Power of the Canopus Pipper = 15 W"]
-[9.67557144165039, 4.16837215423584, "[TT] Ranges of the MAG Sensor = \u00b11024, \u00b14096, \u00b116,384, \u00b165,536 nT"]
-[5.017823219299316, 3.39644193649292, "[TT] Manufacturer of the PM = Thomson & Nielsen Electronics Ltd, Canada"]
-[5.5523681640625, 6.051979064941406, "[TT] EEPROM of the OBDH = 128 kB"]
-[3.1335110664367676, 2.177762508392334, "[TT] Crop Type Detection of the Sentinel-2 = Yes"]
-[9.44399642944336, 3.075629711151123, "[FF] Effect of the Galactic Cosmic Rays = Penetrate Earth's magnetic fields and interact with the atmosphere"]
-[4.342761516571045, 4.7931318283081055, "[TT] Scene Size of the Ship Detection mode = 450 km x 500 km"]
-[9.938921928405762, -0.5424180030822754, "[TT] Orbit Altitude of the Trisat-R = Close to 6000 km"]
-[7.337714195251465, 3.5981831550598145, "[FF] Presentation Date of the GNSS Reflectometry Instrument = Sept 18-20, 2012"]
-[5.585578441619873, 2.6820175647735596, "[FF] Project Management of the C&DH subsystem = University of Tokyo, Hokkaido Institute of Technology, Tokyo Metropolitan College"]
-[8.641504287719727, 8.265715599060059, "[TT] IR Energy Reflection of the Optics Assembly = 85%"]
-[5.375072479248047, 4.182180404663086, "[TT] Bus Type of the GFO = BCP 600 (Ball Commercial Platform)"]
-[5.2022480964660645, 3.637007713317871, "[TT] Developer of the ADCS = SENER, Spain"]
-[8.559062004089355, 7.546275615692139, "[TT] Panchromatic Image Data of the Optical Sensor Assembly (OSA) = 6500 lines/s"]
-[5.849234104156494, -0.8357990980148315, "[TT] Design Lifetime of the Rover = Around 90 Earth days"]
-[5.942995548248291, 8.707991600036621, "[TT] Modulation Transfer Function (MTF) of the System = 9-10% at Nyquist"]
-[5.674347877502441, 2.568997383117676, "[TT] Affiliation of the CATSat-1 = JHU/APL (Johns Hopkins University /Applied Physics Laboratory)"]
-[6.2896013259887695, 3.1813089847564697, "[TT] Responsible Organization of the Sensor and Geophysical Data Records = Jet Propulsion Laboratory"]
-[5.481695652008057, 4.896583080291748, "[FF] GPS receiver of the TDX/TSX = IGOR GPS receiver"]
-[13.882080078125, 3.0295815467834473, "[TT] Mass of the Dove-1 = ~ 5.8 kg"]
-[4.267834663391113, 2.644691228866577, "[TT] Launch Site of the STPSat-3 = MARS (Mid-Atlantic Regional Spaceport) on Wallops Island, VA"]
-[8.412376403808594, 2.102869987487793, "[FF] Calibration Quality of the WindSat = Extremely demanding"]
-[4.521509647369385, 2.960569381713867, "[TT] Location of the Hertz Chamber = ESA's ESTEC technical center in the Netherlands"]
-[6.3895368576049805, 7.398642539978027, "[TT] Pulse Repetition Frequency of the LOM = 10 kHz"]
-[8.402885437011719, 1.9400919675827026, "[TT] Instrument Type of the ISS-RapidScat = Scatterometers"]
-[12.478445053100586, 3.203746795654297, "[TT] Remaining Useable Propellant of the OrbView-3 = 22.98 kg"]
-[6.399450302124023, 3.2420732975006104, "[TT] Potential Servicing of the AMS-02 = Future spacewalk"]
-[9.549314498901367, 7.09504508972168, "[TT] Ground Resolution of the SLA-2 = 1-10 m"]
-[4.630624771118164, 7.209365367889404, "[TT] Performance of the S-band link = Successfully established even in elevations below 20 degrees"]
-[6.765346050262451, 6.3384623527526855, "[TT] Number of 'New Design' Array of the MSA = One"]
-[6.985517501831055, 4.317465305328369, "[FF] Unknown of the BRICSAT-2 = Unknown"]
-[6.536526679992676, 3.2559878826141357, "[FF] Data Sharing of the Earth-observing satellites = With colleagues around the world, including disaster response agencies"]
-[11.847765922546387, 2.8682568073272705, "[TT] \u0394V (cm/s) of the Pegasus R/B (2) = 0.56"]
-[6.842945098876953, 6.105710983276367, "[TT] Operation Mode of the DP5G = List mode"]
-[7.061167240142822, 0.8790714740753174, "[FF] Mission Requirements Document of the Next Generation Gravity Mission = URL:\u00a0https://www.asi.it/wp-content/uploads/2021/03/MAGIC_NGGM_MCDO_MRD_v1_0-signed2.pdf"]
-[3.934560537338257, 6.527272701263428, "[FF] Configuration of the VDES Antenna = Stowed and deployed"]
-[5.891986846923828, 7.188570976257324, "[TT] Data Rate of the POLDER-2 = 883 kbit/s"]
-[4.633965969085693, 0.8545595407485962, "[FF] Mission Failure of the ADEOS = June 1997"]
-[8.322745323181152, 5.033891201019287, "[FF] Device Type of the Electrostatic Accelerometer = Electrostatic"]
-[12.05640983581543, 4.55768346786499, "[TT] Payload Volume of the TCS = 279 x 406 x 254 mm"]
-[3.233494520187378, 5.7301154136657715, "[TT] Dimensions of the SAR Antenna = 6 m x 6 m"]
-[8.184112548828125, -0.7665108442306519, "[TT] Composition of the Layered Mounds = Nearly pure water ice"]
-[3.772437334060669, 4.560755252838135, "[FF] Reprogrammable Parameters of the RADARSAT-2 SAR sensor = Resolution, swath width, polarization"]
-[6.400157928466797, 4.800073623657227, "[FF] Data Delivery of the DPE = HDF-5 formatted file"]
-[14.14699649810791, 3.224165916442871, "[TT] Mass of the TCS = 0.15 kg"]
-[8.339600563049316, 7.686746120452881, "[TT] Detector Array Bands of the FTS = 194-324 \u00b5m and 316-672 \u00b5m"]
-[5.1410040855407715, 0.7025395631790161, "[FF] Impact Date of the LADEE = April 18, 2014"]
-[8.159478187561035, -0.9516661167144775, "[TT] Draining Period Frequency of the Conway and Mercer lakes = Third time since the original ICESat mission began measuring elevation changes on the ice sheet\u2019s surface in 2003"]
-[7.800048351287842, 1.970672369003296, "[FF] Purpose of the OceanSat-2 = Provides data for the study of surface wind, ocean surface strata, observation of chlorophyll concentrations, monitoring phytoplankton blooms, study of atmospheric aerosols and suspended sediments in the water"]
-[11.329645156860352, 5.829779624938965, "[TT] Material of the SAS Subassemblies = Aluminum brackets parts attached to supporting sandwich structures"]
-[8.563227653503418, 4.6989545822143555, "[FF] Integration of the \u00b5ASC = Integrated with the STR (Star Tracker) package"]
-[5.392900466918945, 8.775009155273438, "[TT] Bandwidth of the Band 10 = 0.304 \u00b5m (55 cm -1)"]
-[6.185361385345459, 2.203735828399658, "[FF] URL of the Docking Module = https://blogs.nasa.gov/spacestation/2021/11/26/russias-new-docking-module-arrives-at-station/"]
-[5.533142566680908, 7.170921325683594, "[FF] Download Capacity Multiplier of the VBR = 1.6 with Nbr=2, and multiplied by 2 with Nbr=3"]
-[6.763726711273193, 0.7687743306159973, "[FF] Views of Star Formation Date of the Herschel and Planck = 5 July 2020"]
-[8.876847267150879, 5.545466899871826, "[TT] Pointing Knowledge of the DSP satellites = <0.5\u00ba"]
-[8.201708793640137, 8.175153732299805, "[TT] Type of the GeoCarb = 4-Infrared channel, single-slit imaging spectrograph"]
-[9.148014068603516, 1.2588777542114258, "[FF] Time to Fly Beyond Oort Cloud of the Voyager 2 = Possibly 30,000 years"]
-[5.834675312042236, 2.6079649925231934, "[FF] Program Theme of the UniSat = Education and hands-on experience of students and faculty in the field of aerospace engineering"]
-[10.115743637084961, 0.6830160617828369, "[TT] Minimum Separation for Distinguishing Spacecraft of the TIRA = 5 km"]
-[6.8946356773376465, 9.505130767822266, "[TT] NEDT at 300 K of the Band 11 = 0.2 K"]
-[4.672626972198486, 0.8281363844871521, "[TT] Announcement Date of the PROBA-V = 9 July 2020"]
-[8.823685646057129, 3.775447130203247, "[FF] Systematic Error of the MIRAS = Several Kelvin"]
-[5.366527080535889, 5.7264180183410645, "[FF] Protocol of the N-FEE and N-DPU = Simulated RMAP with e.g. control registers, HK data, memory mapped for simple access"]
-[5.6922993659973145, -0.774164617061615, "[TT] Design Life of the DubaiSat-1 = 6 years"]
-[4.906599998474121, 0.36946436762809753, "[FF] Launch Date of the DART = Last November"]
-[13.419163703918457, 7.358670234680176, "[TT] Power of the Total with contingency = 18 W"]
-[5.182316780090332, 7.061395645141602, "[TT] Downlink Data Rate of the TT&C Subsystem = 8.192 kbit/s"]
-[4.766571998596191, 7.956234455108643, "[TT] Frequency (MHz) of the GLONASS L5 OC = 1176.45"]
-[8.13692569732666, 1.2938443422317505, "[FF] Purpose of the SMAP = Provide information on water availability and environmental stress for estimating plant productivity and potential yield"]
-[5.275697231292725, 7.52699613571167, "[TT] Free Space Loss of the Unit = 182.7 dB"]
-[6.3681721687316895, 5.048435688018799, "[FF] Function of the OBC = Collects housekeeping data from all subsystems and provides it to subscribing subsystems locally"]
-[12.078195571899414, 4.556209087371826, "[TT] Size of the GeoCarb = 1.3 m x 1.14 m x 1.3 m"]
-[5.585927486419678, 6.409915924072266, "[TT] Storage Capacity of the IDEE = 200 000 photons"]
-[5.409369945526123, 2.197695016860962, "[FF] Technology Transfer Program of the SOHLA-1 = Ongoing"]
-[7.0767741203308105, 1.279722809791565, "[FF] Mission of the Spitzer Space Telescope = 2003 - 2020"]
-[8.0161771774292, 1.7811102867126465, "[FF] Increase of the Global Land Evapotranspiration = 10 per cent"]
-[8.610922813415527, 3.7029354572296143, "[FF] Solar Spectral Irradiance Measurement Range of the SOLSPEC = 200 to 2400 nm"]
-[5.695839881896973, 4.85465669631958, "[FF] Service Type of the EDRS = Data-Relay"]
-[12.336404800415039, 0.6167627573013306, "[TT] Number of Stars of the PLATO = Up to a million"]
-[5.50416374206543, 7.223798751831055, "[TT] Set Bitrate of the EWC27 = 3 Mbit"]
-[4.353965759277344, 0.7815137505531311, "[TT] Launch Date of the HJ-1 = 06 Sep 2008"]
-[9.767770767211914, 1.3604177236557007, "[TT] Planned Imaging Area of the Pleiades = 150,000 km2"]
-[7.443906307220459, 6.361596584320068, "[FF] Function of the Advanced Topographic Laser Altimeter System (ATLAS) = Sends pulses of laser light toward Earth and precisely times each photon\u2019s round-trip journey as it bounces off a surface and returns to the sensor"]
-[6.210543155670166, 4.293698310852051, "[FF] Function of the European Mission Tasking Center = Receives observation requests and incorporates them into its tasking/planning cycle"]
-[4.690144062042236, 7.20505428314209, "[TT] Command S-band of the RF communications = 1.2 kbit/s"]
-[13.419665336608887, 6.732446670532227, "[TT] Power of the KOMPSAT-1 = 636 W"]
-[10.665793418884277, 1.3068815469741821, "[TT] Energy Received from Star of the L 98-59b = 22 times the amount of energy Earth receives from the Sun"]
-[7.2987236976623535, 3.845409631729126, "[FF] Purpose of the NEMO Bus = Earth Monitoring and Observation"]
-[9.426739692687988, 1.345596432685852, "[TT] Launch Speed of the Rocket = 16 feet (5 meters) per second"]
-[4.246752738952637, 0.8269972205162048, "[TT] Founded of the EDF = 1967"]
-[5.987196922302246, 2.8974804878234863, "[TT] Manufacturing of the Legion = Cleanliness standards appropriate for optical payloads"]
-[13.383748054504395, 7.771328926086426, "[TT] RF Output Power of the Transmitter = 12 W"]
-[3.5758109092712402, 5.101841926574707, "[TT] Spatial Resolution of the Severjanin X-band Side-Looking Radar = 500 m and 1000 m"]
-[14.106565475463867, 7.18191385269165, "[TT] Bus Voltage of the S/C = 28 V"]
-[7.579696178436279, 2.1952004432678223, "[FF] Testing Location of the Marine Plastic Detection = Ocean Wave Facility"]
-[5.933558940887451, 2.699035406112671, "[TT] Mission Assurance Standards of the Legion = Class B"]
-[7.0294060707092285, 8.133857727050781, "[TT] Noise Equivalent Temperature of the MSU-SK = 0.5 K"]
-[10.861592292785645, 1.4699652194976807, "[TT] Mass of the Infinity-shaped loop = 30 million solar masses"]
-[7.349419116973877, 0.24544095993041992, "[TT] Science Deck Population Date of the OSIRIS-REx = Aug. 29, 2015"]
-[9.189058303833008, 7.191648483276367, "[TT] Fast Imager Resolution of the FY-4B = About 250 meters"]
-[4.687156677246094, -0.30325937271118164, "[TT] Docking Date of the CATS = Jan. 12, 2015"]
-[7.798168659210205, 5.322279930114746, "[FF] Issue of the Control System = Insufficient gain leading to induced vibration"]
-[9.184127807617188, 7.583239555358887, "[TT] Frame Coverage of the spaceCam c4000 = 12 km x 12 km"]
-[8.633545875549316, 7.849009990692139, "[TT] Digitization Interval of the Instrument = 0.25 s m -1"]
-[8.949004173278809, 6.522724628448486, "[FF] Image Resolution of the CaSSIS camera = Unknown"]
-[4.69135046005249, 5.949870586395264, "[FF] SDR of the GOMX-3 = Software Defined Radio"]
-[7.6230363845825195, -0.3384249210357666, "[TT] Event Nickname of the IceCube Detector = Hydrangea"]
-[8.971009254455566, 0.6260207295417786, "[FF] Support Tools of the ARTEMIS = Tools developed under multiple airborne experiments"]
-[13.878069877624512, 3.1481785774230957, "[TT] Platform Mass of the MERLIN = 260 kg"]
-[5.0285234451293945, 8.144173622131348, "[TT] Switch Positions of the CubeRRT RFE = 4"]
-[6.152393341064453, 4.550673484802246, "[FF] Function of the PTT = Collect and process relevant environmental data and transmit them to the NOAA-POES satellites"]
-[5.882873058319092, -0.021636316552758217, "[TT] Operation Period of the S-191 and S-192 experiments = May 1973 to Feb. 1974"]
-[9.274041175842285, 3.0996358394622803, "[FF] Impact of the Solar Wind Concentrator = Revealed differences between the sun and planets in oxygen and nitrogen"]
-[5.914649963378906, 3.1065495014190674, "[FF] Focus of the EMOC = Coordinating orders for maritime GoC users"]
-[6.951646327972412, 7.78744649887085, "[TT] Aperture Size of the Reflector Assembly = 14 m"]
-[11.772446632385254, 4.346571445465088, "[TT] Overall Volume of the TanSat = 150 cm (Ys) x 180 cm (Zs) x 185 cm (Xs)"]
-[4.408899784088135, 2.9641239643096924, "[TT] Location of the TIRA = FGAN site in Wachtberg near Bonn, Germany"]
-[8.413100242614746, 4.597654342651367, "[FF] Frame-Dragging Accuracy of the LARES = 2%"]
-[5.402646541595459, 6.261551856994629, "[TT] Model of the SDR Host Computer = Intel Core i5"]
-[6.109631061553955, 5.455411434173584, "[TT] Redundancy of the OBC = Cold dual-redundant"]
-[3.829375743865967, 7.915844440460205, "[TT] Type of the OQPSK = Offset Quadrature Phase Shift Keying"]
-[11.172653198242188, 1.5451953411102295, "[TT] Mass of the ST (Star Tracker) = 1.2 kg"]
-[9.419007301330566, 4.969801425933838, "[TT] Attitude Stability of the ADCS = \u22640.001\u00ba/s (3\u03c3, 3-axis)"]
-[7.534122943878174, 8.110626220703125, "[TT] Color of the Transmit Collimator = Yellow"]
-[3.196235179901123, 5.024266242980957, "[TT] Footprint Diameter of the COSPAS-SARSAT Visibility = 4000 km"]
-[7.083063125610352, 2.0300843715667725, "[TT] End of Life Date of the Biomass = April 2029"]
-[5.695076942443848, 1.090016484260559, "[FF] Satellite Delivery Date of the International Partners = May 26, 2016"]
-[5.2446370124816895, 0.1051056757569313, "[TT] Planned Launch Date of the Heinrich Hertz = 2016"]
-[2.8313021659851074, 0.08633407205343246, "[TT] J2000 declination (deg) of the B1758-250 = -25.079"]
-[5.563540935516357, 3.452706813812256, "[FF] Antenna Chips Sales of the Astrocast = Sells the antenna chips to the clients"]
-[11.798839569091797, 6.825653076171875, "[TT] Energy Optimization of the MEG = Medium"]
-[8.520315170288086, 0.621701717376709, "[FF] Objective of the LALT = Measure the vertical distance between the Main Orbiter and the subsatellite point on the lunar surface"]
-[5.9613871574401855, 3.5545127391815186, "[TT] Receiver Prices of the Transit Navigation = As low as $1000"]
-[3.7419190406799316, 2.3964033126831055, "[TT] Age of the Iridium 33 = Modern"]
-[4.356135845184326, 3.076615333557129, "[TT] Locations of the Ground Stations = Oberpfaffenhofen, Neustrelitz, Adelaide/Australia and Iza\u00f1a/Tenerife"]
-[7.754079818725586, 3.046224594116211, "[FF] Instrument Functions of the GOES-S = Provide advanced imagery and atmospheric measurements, real-time mapping of lightning activity, and improved monitoring of solar activity and space weather"]
-[7.162579536437988, 8.607073783874512, "[TT] Solar Constant Channel Spectral Band of the ISP-2 = 0.2 - 10.5 \u00b5m"]
-[5.110335826873779, 1.112221121788025, "[TT] Initial Launch of the NPOESS = 2014"]
-[10.565474510192871, 2.244281053543091, "[FF] Future Investigator of the Athena X-ray observatory = ESA\u2019s future Athena X-ray observatory"]
-[5.016561031341553, -0.6208216547966003, "[TT] IOC Operation Period LSDN of the SLATS = 16:00 hours"]
-[8.087804794311523, 8.319405555725098, "[FF] Signal Type of the Spectral Lines = Distinct"]
-[3.9151790142059326, 3.408895492553711, "[TT] Flight Name of the Galileo FOC-3 and FOC-4 satellites = VS-11"]
-[9.495916366577148, 8.946747779846191, "[TT] Frame Coverage of the Iris Video Camera = Approximately 3.8 km x 2.2 km (UHD); Approximately 1.9 km x 1.1 km (HD)"]
-[5.183371543884277, 0.4041955769062042, "[FF] Launch Date of the TRACE = Feb. 14, 1980"]
-[8.175107955932617, 7.421731948852539, "[TT] Function of the Photo MOSFET Switch = Capacitor discharge"]
-[5.6330695152282715, 5.3467020988464355, "[TT] Data Interfaces of the OBC = I2C, CAN and UART"]
-[9.133572578430176, 1.325345516204834, "[FF] Launch Date of the New Horizons = 19 January 2006"]
-[5.986232280731201, 0.26623353362083435, "[TT] Closest Approach Date of the Rosetta = 13 November 2007"]
-[7.837864398956299, 2.1871252059936523, "[TT] Latitude Coverage of the LIS = \u00b154.33\u00ba"]
-[5.729429244995117, 1.2342332601547241, "[FF] Mission Analysis Presentation Date of the EQUULEUS and OMOTENASHI = 1-5 October 2018"]
-[9.079224586486816, 7.81535530090332, "[TT] Lens Type of the MOMS-02 = 3 for stereoscopic applications, 2 for multispectral data sets"]
-[9.375045776367188, 8.460456848144531, "[TT] Ensquared Energy of the Lens = 90% within 60 x 60 \u00b5m"]
-[9.352066040039062, 6.8868727684021, "[TT] Spatial Resolution of the MSU-SK = 175-243 m (in VIS) and 500 m (in IR)"]
-[6.304611682891846, 1.8541077375411987, "[FF] URL of the VAMOS = http://elib.dlr.de/84313/1/IFAC2013_VAMOS_03.pdf"]
-[3.1916394233703613, 1.6903700828552246, "[TT] Imaging Frequency of the Sentinel-1 = Every few days"]
-[5.800492763519287, 1.2277381420135498, "[FF] Capture and Berthing Experiment Date of the ETS-VII = Aug. 14-17, 2000"]
-[8.155101776123047, 2.1665961742401123, "[FF] Function of the Kazachok = Remain stationary to investigate the climate, atmosphere, radiation and possible presence of subsurface water"]
-[7.638277530670166, 3.4344420433044434, "[FF] Conference Presentation of the Harpoon Capture System = 7th European Conference on Space Debris, ESA/ESOC, Darmstadt/Germany, 18 - 21 April 2017"]
-[9.06551742553711, 2.642629623413086, "[FF] Impact Time of the Geomagnetic Storm = Less than a day"]
-[6.763734817504883, 6.404896259307861, "[TT] Processing Time of the Level 1A = 60 s"]
-[5.678300380706787, 8.195174217224121, "[TT] Spectral resolution of the Millimeterwave receiver = 44 kHz"]
-[7.022636890411377, 8.374463081359863, "[TT] Nominal SNR of the Band 8 = 750"]
-[9.417257308959961, 3.7781167030334473, "[FF] Measurement of the MAG = Space environment magnetic field"]
-[4.823883056640625, 0.43860605359077454, "[TT] Launch Start Date of the Transport Layer = Late 2024"]
-[10.683273315429688, 0.927177906036377, "[FF] Type of the Kepler-80g = Earth-sized"]
-[7.741890907287598, 2.1374716758728027, "[FF] Members of the A-train = Aqua, CloudSat, CALIPSO, PARASOL, and Aura spacecraft"]
-[4.777132511138916, 0.37879884243011475, "[TT] End of Life Date of the MOMS = 16 August 1999"]
-[11.430864334106445, 4.415136814117432, "[TT] Size of the TEPCE = 3U"]
-[3.8369433879852295, 7.907631874084473, "[TT] Modulation of the Channel = QPSK, 8PSK, 16APSK, 32APSK"]
-[8.642309188842773, 3.3141286373138428, "[FF] Purpose of the Solar Ultraviolet Imager (SUVI) = Space weather monitoring"]
-[6.210616111755371, 5.536779880523682, "[FF] Redundancy Concept of the Redundancy Switch Assembly (RSA) = 5 out of 6 redundancy concept is applied for the RXMs and DGRs"]
-[3.3063831329345703, 2.2608063220977783, "[FF] Access of the Sentinel Data Policy = Full and open access to the data"]
-[7.242027282714844, 8.608582496643066, "[TT] Antialiasing Filter Poles of the Rx Module = 19"]
-[8.420174598693848, 4.067863464355469, "[FF] Function of the EIS (Extreme Ultraviolet Imaging Spectrometer) = Scanned the active region, breaking the light into spectral lines used to identify specific elements"]
-[8.132347106933594, 8.895774841308594, "[TT] Spectral Resolution of the BIRCHES = 5 nm"]
-[9.135966300964355, 6.912995338439941, "[FF] Tradeoffs of the Ground-based Analysis Techniques = Between spatial and temporal resolution"]
-[2.9667606353759766, 0.10322213917970657, "[FF] - of the J2000 = -"]
-[4.7972564697265625, 7.338866710662842, "[TT] RF Communications Data Rate of the Kanopus-V 1 = 300 Mbit/s"]
-[8.44533634185791, 3.1975083351135254, "[TT] Range of the Ozone Measurement Instrument = 0.1 - 15 ppmv"]
-[10.415046691894531, 6.695549964904785, "[TT] Mirror Position Measurement of the SMA = Differential Impedance Transducers"]
-[8.04074764251709, 7.243857383728027, "[TT] Type of the GLI = CCD (Charge Coupled Device)"]
-[4.569187164306641, 3.055053472518921, "[TT] PGDS Location of the FOS = ESRIN"]
-[5.122129440307617, 2.489724636077881, "[TT] Type of the ELTs = Aviation"]
-[13.617095947265625, 5.7468647956848145, "[TT] Power Source of the GHGSat-D = Body-mounted solar cells"]
-[7.77577543258667, 3.2237980365753174, "[TT] Instruments of the GOES-S = Earth-sensing, lightning-detecting, solar imaging and space weather monitoring instruments"]
-[8.096884727478027, 7.617839336395264, "[TT] Spatial Resolution of the High-Resolution Hyperspectral Imager = 30-meter"]
-[5.27117395401001, 0.6397882699966431, "[TT] Launch Date of the Simon Bolivar Satellite (VeneSat-1) = October 29, 2008"]
-[10.669069290161133, 3.328129529953003, "[FF] Scientific Objectives of the EFILE = Development of the phase-change interfacial hydrodynamic theory by using microgravity environment, to obtain the novel knowledge on the coupling mechanism of evaporation and convection; Understand the gravity effects on the heat and mass transfers of evaporation and improve the development of Space Thermal Engineering and Space Life System"]
-[9.25475025177002, 1.8674079179763794, "[FF] Calibration Validation of the HARP-2 = Ongoing"]
-[8.966023445129395, -1.3177088499069214, "[TT] Tracking Direction for Geostationary satellites of the NEOSSat and Sapphire = Antisolar direction"]
-[7.677237510681152, 0.28469187021255493, "[FF] Destination Count of the Lucy = Unknown"]
-[9.949270248413086, 1.5391227006912231, "[FF] Observation of the FAUST = Large Magellanic Cloud galaxy"]
-[3.445349931716919, 5.016095161437988, "[TT] Backup Station Frequency Bands of the PAZ SAR Processor = S/X-band"]
-[3.171483039855957, 4.171644687652588, "[TT] Bistatic X-band Experiment Date of the TerraSAR-X = November 2007"]
-[7.512937545776367, 5.722497940063477, "[FF] Function of the Video Proximity Electronics Unit = Conversion of the analog signal coming from the focal plane assembly into digital signals"]
-[4.536635398864746, 0.5792023539543152, "[FF] Contract Award Date of the M3MSat = June 23, 2008"]
-[5.796090602874756, -0.8204318881034851, "[TT] Design Life of the MEV-1 = Redundant and high reliability 15+ years"]
-[9.02328109741211, 5.191411018371582, "[TT] Type of the FOG 120 HR = High precision Fiber Optic Gyro"]
-[4.442656993865967, 1.806607723236084, "[TT] Launch Date of the RADARSAT-2 = December 2007"]
-[6.945465564727783, 1.3016809225082397, "[FF] Publication Date of the Solar Mass Ejection Imager = 1997"]
-[7.81948709487915, 3.8444669246673584, "[FF] Type of the LRA, GPSDR = Ocean colour instruments, Magnetic field, Other, Data collection, Atmospheric temperature and humidity sounders, Gravity instruments"]
-[9.849725723266602, 1.3296152353286743, "[FF] Diameter of the Pleiades = About 35 light years"]
-[9.795339584350586, 6.193684101104736, "[TT] Mirror Angle of the SUNSAT = 45\u00ba"]
-[4.829174041748047, -1.8405462503433228, "[FF] Lunar Lander Neutrons and Dosimetry(LND) of the Chang\u2019e-4 Lander = International Joint Collaboration Payload"]
-[6.042569160461426, 2.4513001441955566, "[TT] Acquisition Date of the WorldView Legion Satellite Constellation = 06 July 2017"]
-[5.221093654632568, -1.062103271484375, "[FF] Test Completion Date of the Konnect satellite = 6 September 2019"]
-[10.081486701965332, 1.9193463325500488, "[FF] Mission Date of the Chandrayaan-1 = April 25-30, 2010"]
-[4.934264659881592, -0.3135365843772888, "[TT] Launch Time of the Rocket 3.3 = 1:16 a.m. EST (06:16 UTC)"]
-[11.063750267028809, 5.995498180389404, "[TT] Coating Materials of the AOE = Polyethylene, PTFE, carbon, and silica"]
-[9.493611335754395, 8.126252174377441, "[TT] Depth of Field of the CMOS Camera = 120 cm"]
-[6.412644386291504, 0.4865490198135376, "[TT] Profiles Per Day of the FormoSat-7 / COSMIC-2 mission = 8,000 (threshold)"]
-[7.282339096069336, 7.501898288726807, "[FF] Bump Height of the Photon Sieve = h< 8\u2205(f/D)2"]
-[11.21948528289795, 5.884279251098633, "[FF] Properties to Investigate of the Bricks = Number and orientations of protein bridges, compressive strength, and porosity"]
-[7.094334125518799, 5.829492092132568, "[FF] Time Delay of the Deep Space Atomic Clock = About five times better than what the team reported in the spring of 2020"]
-[14.2454252243042, 3.1409056186676025, "[TT] Mass of the S/C = 3700 kg"]
-[4.431439399719238, 1.2600544691085815, "[TT] Handover Date to EUMETSAT of the MSG-4 = 26 July, 2015"]
-[5.959500789642334, 2.4034337997436523, "[TT] Location of the PACS = MPE (Max Planck Institute for Extraterrestrial Physics), Garching, Germany"]
-[8.440166473388672, 5.355459690093994, "[TT] Orbit Prediction Accuracy of the Picosatellite = Meter Level"]
-[10.163908958435059, 8.084901809692383, "[TT] Telescope/Spectrograph Assembly of the MAHRSI = f/7.5 Czerny-Turner spectrograph with a 75 cm focal length behind a 50 cm focal length telescope (57 cm2 aperture)"]
-[8.212307929992676, 1.430411696434021, "[FF] Mission of the SMOS = Measuring Ocean Salinity from Space"]
-[11.361437797546387, 5.742705821990967, "[TT] Material of the Heatshield = Al honeycomb structure"]
-[10.381601333618164, 3.260047435760498, "[TT] Number of CubeSat Units of the Prometheus-1 = 1 x 3"]
-[8.347184181213379, 7.393836498260498, "[TT] Contract Value of the Teledyne e2v CCD Bruy\u00e8res Image Sensors = \u20ac42 M"]
-[11.306058883666992, 5.148063659667969, "[TT] Wall Material of the Straw Tubes = 72 \u00b5m kapton foil"]
-[6.901992321014404, -1.7885587215423584, "[FF] Data Type of the Jason-3 satellite = Sea surface height anomalies"]
-[7.249885082244873, 7.811058044433594, "[TT] Shaping of the PHA = Bipolar, 1.9 \u00b5s to peak"]
-[3.617363691329956, -0.8088423013687134, "[TT] Orbit Sunlight of the ALMASat-1 = About 75%"]
-[14.032350540161133, 7.078681945800781, "[TT] Regulated Voltages of the EPS = +3.3 V, +4 V, +5 V, +5.5 V, \u00b1 12 V"]
-[10.868884086608887, -0.3212882876396179, "[TT] Global DEM Production Completion Date of the TanDEM-X = September 2016"]
-[7.038234233856201, 4.290188789367676, "[FF] Unknown of the StangSat = Unknown"]
-[6.808859825134277, -0.4095364212989807, "[TT] Orbital Period of the Landsat-9 = 99 minutes"]
-[1.7355910539627075, 6.116700172424316, "[TT] Lyman-alpha Forest Percentage of the Universe = 28 percent"]
-[6.926638603210449, 6.157412052154541, "[TT] Number of Instruments of the Nimbus-7 = 9"]
-[10.175871849060059, 0.9903275370597839, "[TT] Distance from Earth of the GW170817 = About 130 million light years"]
-[12.035026550292969, 4.601180076599121, "[TT] Size of the Spacecraft = 98 cm x 107 cm x 115 cm"]
-[6.585407257080078, 2.9569051265716553, "[TT] Various Code Names of the Weather Program = Program 2, Program 694BH, and Program 417"]
-[5.973460674285889, 5.288636207580566, "[FF] Functions of the SMC = TC authentication/ciphering and key management"]
-[7.9663262367248535, -2.5769639015197754, "[TT] Wavelength of the GOLD = 135.6 nm"]
-[7.754408359527588, 8.263924598693848, "[TT] Band Count of the Six-band Imager = 6"]
-[8.143049240112305, 2.240200996398926, "[FF] Purpose of the Humanity Star = Purely artistic"]
-[8.712672233581543, 3.4078686237335205, "[FF] Purpose of the THEMIS = Study the energy and particle flow in the Sun-Earth system"]
-[5.635795593261719, -0.7421462535858154, "[TT] Design Life of the MightySAT I = One year"]
-[13.327468872070312, 7.038212299346924, "[TT] TWTA Output of the LDCM spacecraft = 62 W"]
-[10.321763038635254, 5.752206325531006, "[TT] NE\u0394T @ specified scene temperature of the Instrument = 0.1-0.7 K @ 250 K"]
-[6.758244037628174, 5.096863269805908, "[FF] Subsystems of the STRV-2 = EPS (Electrical Power Subsystem, C&DH (Command and Data Handling), communications, and an attitude determination and control subsystem"]
-[8.719429969787598, -0.22154487669467926, "[TT] Inclina. (\u00ba) of the Intercosmos- Bulgaria 1300 (Intercosmos-22) = 81.2"]
-[8.934514045715332, 7.426185131072998, "[TT] Multispectral Imagery Resolution of the Raytheon imagers = 50 cm"]
-[9.605974197387695, 8.02119255065918, "[TT] Focal Length of the LWIR Cameras = 13.5 mm"]
-[6.856783866882324, 4.129760265350342, "[FF] Performance Options of the LEOStar-2 = Redundancy, propulsion capability, high data rate communications, high-agility/high-accuracy pointing"]
-[5.5169525146484375, 7.025439262390137, "[TT] Baud Rate of the RS-422 UARTs = 115 kbit/s"]
-[13.458879470825195, 5.589907169342041, "[TT] Grids Number of the Solar Wind Ion Entry = 3"]
-[6.979185104370117, 2.515078067779541, "[FF] Role of the Martin Popek = His photos add another dimension to the research"]
-[5.5500383377075195, 4.659229755401611, "[FF] Software of the HISat = App-based, open-source approach to core resource-sharing cellular firmware"]
-[9.477678298950195, 3.8599956035614014, "[FF] Measurement of the MFI = Intensity and direction of magnetic field vector"]
-[4.487842082977295, 3.079200506210327, "[FF] Data Routing of the EV-9 = From Panama to the NOC (Network Operations Center) located at the exactEarth facilities in Cambridge, Ontario"]
-[8.08885383605957, -1.1299598217010498, "[FF] Surface Wave Frequency of the ICESat-2 = Unknown"]
-[6.631547451019287, 3.9019312858581543, "[FF] Payload of the AlSat-2B = NAOMI (New AstroSat Optical Modular Instrument)"]
-[11.201169967651367, 6.455623626708984, "[TT] Gas Temperature of the eROSITA = Tens of millions of degrees"]
-[5.877867221832275, 4.972849369049072, "[FF] Software Protocol of the C2B = Unknown"]
-[14.075571060180664, 4.056434154510498, "[TT] Mass of the SEIS Instrument = 29.5 kg"]
-[9.77532958984375, -0.5548495650291443, "[TT] Orbit Altitude of the Odin = 600 km"]
-[8.782078742980957, 2.3023900985717773, "[TT] Dust Measurement Period of the Ulysses = 1992 to 1998"]
-[9.059557914733887, 5.312004089355469, "[TT] Attitude Accuracy of the Procyon = 5 arcsec on X/Y and 50 arcsec on Z"]
-[6.253318786621094, 8.024821281433105, "[TT] Number of Passbands of the Channel 4 = 1"]
-[10.736930847167969, 0.9245025515556335, "[TT] Size of the WD 1856 b = No more than 14 times Jupiter\u2019s size"]
-[4.781166076660156, 0.612516462802887, "[TT] Launch Date of the OPAL = Late 2016"]
-[5.73801326751709, 3.530271291732788, "[TT] Number of Spacecraft of the Cislunar Explorers = 2"]
-[6.0455851554870605, 1.3539412021636963, "[FF] Conference Date of the Swarm = Oct. 4-8, 2010"]
-[7.77555513381958, 1.2506219148635864, "[FF] Endured Unusually Active and Destructive Fire Seasons of the States, particularly California = Yes"]
-[11.734606742858887, 7.525209426879883, "[FF] Presentation Date of the Megha-Tropiques = November 7-11, 2011"]
-[4.688314914703369, 0.13865521550178528, "[TT] Launch Date of the FREESTAR = 16 January 2003"]
-[8.036831855773926, 0.590241551399231, "[FF] Conference Presentation of the MASCOT Lander = May 16-20"]
-[3.1298155784606934, 4.333425045013428, "[FF] Radiometric Sensitivity of the TerraSAR-X = Improved"]
-[6.862792015075684, -0.7229185104370117, "[TT] Orbital Period of the GRACE-FO = Once every 90 minutes"]
-[8.661894798278809, 6.742096900939941, "[FF] Number of Images of the SPOT-6 = More than 100 million km2"]
-[8.817296028137207, 2.8764774799346924, "[FF] Impact of the XFM = Provide autonomy over Europe's space weather forecasts and redundancy for space weather forecasters globally"]
-[6.843500137329102, 7.3731369972229, "[TT] Thickness of the Beamsplitter = 7 mm"]
-[5.160995960235596, 2.28833270072937, "[TT] Mission Type of the Rosetta = Non-EO"]
-[10.15323257446289, 4.061855316162109, "[TT] Position of the Magnetometer = Deployed on a relatively short boom (~20 cm)"]
-[7.730904579162598, 8.385126113891602, "[TT] MWIR and TIR Bands of the GLI = 7"]
-[4.847799777984619, 7.5956645011901855, "[TT] Bandwidth of the RF Ground Network = Up to ten times the UHF radio"]
-[8.260366439819336, 5.341240882873535, "[FF] Geolocation Method of the NigeriaSat-2 = Precise measurement of the position and attitude of the payload"]
-[10.397170066833496, 5.5392608642578125, "[TT] Temperature at Closest Approach to the Sun of the Heat Shield = Nearly 2,500 degrees Fahrenheit (1370 \u00baC)"]
-[6.78989315032959, 1.829715609550476, "[FF] URL of the Roman Space Telescope = https://www.nasa.gov/feature/goddard/2021/nasa-s-roman-mission-predicted-to-find-thousands-of-transiting-planets"]
-[13.725410461425781, 5.40177583694458, "[TT] Deployable Solar Array Type of the UK-DMC-2 = Emcore triple-junction InGaP/InGaAs/Ge solar cells"]
-[5.522631645202637, 6.4203009605407715, "[TT] Data Capacity of the CDMU = 25 GByte"]
-[11.195920944213867, 5.929383277893066, "[TT] Grids of the FSU = Monolithic grids etched from single wafers of high purity W"]
-[4.95658016204834, 3.3369405269622803, "[TT] Manufacturer of the Fregat = RUAG Space in Sweden"]
-[10.074542999267578, 4.583311557769775, "[TT] Temperature of the Superconducting Magnet = 1.8 K"]
-[11.905078887939453, 5.360376358032227, "[TT] Dimensions - Electronics box of the Instrument = 31 x 22 x 27 cm"]
-[9.575377464294434, 0.6835461854934692, "[TT] Additional Velocity of the Objects Orbiting at LEO = ~7700 m s-1"]
-[3.115194320678711, 2.339019536972046, "[TT] Spectral Bands of the Sentinel-2 = 13"]
-[13.39603328704834, 5.401977062225342, "[TT] Type of the Solar panel release mechanism = New implementation method"]
-[8.947164535522461, 5.197755336761475, "[TT] Configuration of the IRU = PS2/CPU2 and gyro A/B/C"]
-[6.831592559814453, 1.723670482635498, "[FF] URL of the James Webb Space Telescope = http://www.stsci.edu/jwst/operations"]
-[6.049063205718994, 2.4352762699127197, "[TT] Managing Entity of the New Horizons = NASA's Science Mission Directorate"]
-[12.391173362731934, 7.5354084968566895, "[TT] Instrument Power of the Imager = < 266 W"]
-[6.949336051940918, 6.9071221351623535, "[TT] Memory Compression of the TRACE instrument = 12 bit JPEG compression"]
-[8.28951358795166, 9.069196701049805, "[FF] Instrument Overview of the Argus = Not Applicable"]
-[4.938220500946045, 0.5398533344268799, "[TT] Launch Date of the NICER-SEXTANT = 3 June"]
-[13.514354705810547, 2.9495978355407715, "[TT] Heaviest Satellite Mass of the PSLV-XL = 1858 kg"]
-[8.559571266174316, 8.80113410949707, "[FF] Function of the Rowland circle = Determines the locations of slit, grating, and detector in a concave grating spectrograph"]
-[9.47162914276123, -0.5788217186927795, "[TT] Canadian Core Area of Interest of the CHORUS = 11.5M km2"]
-[9.45181941986084, 6.0409722328186035, "[TT] Stereo Angles of the Instrument = \u00b115\u00ba (fore and aft)"]
-[4.249358654022217, 7.373754501342773, "[TT] Uplink Frequency of the GRB = X-band"]
-[5.589789390563965, 0.8279786705970764, "[FF] Test Date of the ISIM = Summer 2015"]
-[4.151350975036621, 7.327051162719727, "[TT] Band of the KaRPDA = Ka-band"]
-[13.395256996154785, 7.385701656341553, "[TT] Power Amplification of the TRMs = Higher"]
-[9.008244514465332, 0.5579886436462402, "[FF] Mission Start Date of the ARTEMIS = 2010"]
-[18.66632843017578, 3.9354171752929688, "[TT] NE\u0394T (K) of the ICI-6 = 1.2"]
-[8.80724811553955, 2.4006361961364746, "[FF] Purpose of the MEIDEX = Study desert dust in the Mediterranean"]
-[9.08061408996582, 5.072772026062012, "[FF] Function of the GYRO = Pick up the resulting angular rates of the system"]
-[6.9150543212890625, 7.096540451049805, "[TT] Laser Diodes Wavelength of the SILEX = 0.8 to 0.86 \u00b5m"]
-[9.823262214660645, -0.4001912474632263, "[TT] Altitude of the Satellite = 764 - 824 km"]
-[10.377706527709961, 2.1489338874816895, "[FF] Ability of the NuSTAR = See the highest energy X-rays in the universe"]
-[7.1618971824646, 5.102676868438721, "[FF] Function of the DWS = Differential Wavefront Sensing"]
-[7.822266101837158, 0.03271261602640152, "[TT] Duration of the Asteroid Day TV = Five hours"]
-[6.501833438873291, 7.041378021240234, "[TT] Power Consumption (average) of the SILEX Optical Terminal = 150 W"]
-[9.544912338256836, 7.180035591125488, "[TT] Spatial Resolution at Nadir VIS of the MVIRI = 2.5 km"]
-[13.35372543334961, 7.526426792144775, "[TT] Peak Pulse Output Power (Low Power Mode) of the T/R module = +38 dBm (6.3 W)"]
-[6.298642635345459, 1.2252240180969238, "[FF] Experiment Focus of the SJ-10 satellite = Study on the pre-ignition characteristics, soot emission, and smoke distributions of the overload wire insulation"]
-[13.194846153259277, 5.496422290802002, "[TT] Deployment Strategy of the Solar arrays = Passive deployed"]
-[7.37758731842041, 3.8951237201690674, "[FF] Publication Date of the Intercalibration of Satellite Instruments = March 2013"]
-[9.296154022216797, 4.9955878257751465, "[TT] Tolerance of the SVOM Attitude = 5\u00b0"]
-[4.725869655609131, 8.336305618286133, "[TT] Center Frequency of the KaRIn = 35.75 GHz"]
-[6.832019805908203, -0.46274277567863464, "[TT] Autonomous Operations of the Solar Orbiter = 15 days without ground contact"]
-[4.2580976486206055, 7.487454414367676, "[TT] Frequency of the XBT = 8.3025 GHz"]
-[7.580105781555176, 1.2353363037109375, "[FF] Symposium Location of the WatER = Venice, Italy"]
-[11.765313148498535, -0.058487795293331146, "[TT] Closest Star Distance of the TESS = Approximately 6 light-years from Earth"]
-[8.222366333007812, 8.71315860748291, "[TT] Spectral Resolution of the SSULI = 1.5 nm or less"]
-[9.18528938293457, 6.94128942489624, "[TT] Resolution of the Global-1 = 1-meter"]
-[9.718749046325684, -0.36512261629104614, "[TT] Altitude of the AMSR-E = 705 km"]
-[10.867637634277344, 1.4208039045333862, "[TT] Mass of the Crab Nebula = Mass of the Sun"]
-[4.695664882659912, 0.7185280919075012, "[TT] Operation Start Date of the SARah system = End of 2019"]
-[5.477864742279053, 0.9261977076530457, "[TT] Thermal Vacuum Testing End Date of the GOES-R satellite = August 24"]
-[7.38859748840332, 8.650812149047852, "[TT] Width of the Instrumental Profile = 0.02 nm"]
-[13.365323066711426, 7.165409564971924, "[TT] P/L Power of the Repeater subsystem = < 3500 W (EOL)"]
-[5.647546768188477, 2.640610933303833, "[FF] Mission Director of the DSX spacecraft = Lt. Col. James Caldwell"]
-[6.813448429107666, 4.578681945800781, "[FF] Location of the VIS = Payload Module"]
-[6.840569496154785, 0.8468136787414551, "[TT] Launch Date of the Gravity Probe A = Nov. 9, 2015"]
-[4.080222129821777, 2.2110254764556885, "[TT] Rocket of the CST-100 = Atlas V"]
-[7.174811363220215, 6.790650844573975, "[TT] Nominal Value of the FPA to FEE Distance = 65 mm"]
-[6.2159905433654785, 5.898694038391113, "[TT] Quantity of the Flight Modules = 3"]
-[10.113563537597656, -1.6073760986328125, "[TT] Inclination of the STRV-1a = 7.3\u00ba"]
-[3.8660266399383545, 4.482355117797852, "[TT] Availability Requirement of the RADARSAT-2 = Above 97%"]
-[9.312637329101562, 7.03376579284668, "[FF] Spatial Resolution of the GMI = Excellent"]
-[8.742064476013184, 7.6213483810424805, "[TT] Large Window Imaging Area Pixels of the CCD = 300 x 300"]
-[8.073426246643066, 3.1669411659240723, "[FF] Detection Capability of the OMI = Gas and Oil Facilities Emissions"]
-[6.063985824584961, -1.1232125759124756, "[TT] Design Life of the GRACE = 8 years"]
-[4.764825344085693, 7.955233573913574, "[TT] Carrier frequency (MHz) of the L1-C = 1575.420"]
-[10.791062355041504, 4.057321071624756, "[FF] Performance Impact of the Inflatable Boom = Affected by the mechanical properties of the laminate material"]
-[7.298690319061279, 5.068030834197998, "[TT] Location of the Receiver Sensor = Back side of the terminal"]
-[5.384324550628662, 8.780120849609375, "[TT] Bandwidth of the Band 2 = 0.268 \u00b5m (13 cm -1)"]
-[7.75615119934082, 5.905486583709717, "[FF] Processed Images of the Image Processing = Level 1 image, ortho-image, pan-sharpen image and DSM (Digital Surface Model)"]
-[11.835963249206543, 4.899186134338379, "[TT] Dimensions of the S/C = 440 mm x 440 mm x 420 mm"]
-[1.7891066074371338, -2.035597562789917, "[FF] Edge Design of the Hayabusa-2 = Folded back inward"]
-[5.507776737213135, 0.42140987515449524, "[FF] Blog Post Date of the International Space Station = 27 April 2023"]
-[5.856359004974365, 3.5570530891418457, "[TT] Number of Tests Conducted of the VECTOR system = 23"]
-[6.7522430419921875, 5.874881267547607, "[TT] Quantity of the TSAT = 1"]
-[14.183358192443848, 3.281003475189209, "[TT] Mass of the TANSO-CAI-2 = 137 kg"]
-[6.020865440368652, 4.782203197479248, "[TT] Software Heritage of the AOCS = PROBA program"]
-[10.544754028320312, 6.881036281585693, "[TT] Target Diameter of the Electrostatic Mirror = 6 cm"]
-[10.302227020263672, 5.380963325500488, "[TT] Type of the Multiview Thermal-Infared = Multiview Thermal-Infared"]
-[3.374793767929077, 1.4576174020767212, "[TT] Launch Date of the Sentinel-2 = 23 June 2015"]
-[6.320605754852295, 2.5248682498931885, "[FF] Purpose of the Orion spacecraft = Return astronauts to the Moon and eventually take the first humans to Mars"]
-[10.110492706298828, 1.4371049404144287, "[FF] Structure of the Milky Way = Warped galactic disc with hundreds of billions of stars"]
-[6.284249305725098, 1.9043035507202148, "[FF] URL of the Resurs-P1 = http://eng.ntsomz.ru/news/news_center/resurs-p_images_gallery_201308"]
-[6.944860458374023, 1.6008384227752686, "[TT] Ground Control of the James Webb Space Telescope = Space Telescope Science Institute in Baltimore"]
-[8.81423568725586, 4.677535057067871, "[TT] Function of the Star Sensor = Update attitude position"]
-[7.422168254852295, 2.5926949977874756, "[FF] Applications of the HyperScout = Monitoring of natural disasters such as floods delineation, forest fires hazard and desertification"]
-[6.225895404815674, 6.09421968460083, "[TT] Quantity of the TRMs (T/R module) = Three"]
-[6.376039505004883, 8.117671966552734, "[TT] Noise of the EZ probe = 0.4 \u00b5V/Hz^(1/2)"]
-[10.717487335205078, 1.107129693031311, "[TT] Size of the TOI 700 d = 20% larger than Earth"]
-[5.376347541809082, 5.667965412139893, "[FF] Interface of the S-band transceiver = UART link with the RIU, 1553 RIU interface with the OBC"]
-[7.381631851196289, 4.526296138763428, "[FF] Unknown of the Multispectral Instrument = Unknown"]
-[3.45328950881958, 1.678632378578186, "[FF] Presentation Date of the Sentinel-2 MMFU = Aug. 22-25, 2011"]
-[5.992166519165039, 0.9367029666900635, "[FF] Image Acquisition Date of the OLI = January 11, 2017"]
-[4.0770111083984375, 2.2145957946777344, "[FF] Rocket of the CST-100 spacecraft = United Launch Alliance Atlas V rocket"]
-[7.006701946258545, 4.182173252105713, "[FF] Unknown of the CATS = Unknown"]
-[13.41677474975586, 2.9090988636016846, "[TT] Mass of the GRACE-FO satellites = ~600 kg"]
-[8.098873138427734, -0.9975847005844116, "[FF] Data Collection of the ICESat-2 = Detailed elevation measurements over tropical and temperate latitudes"]
-[6.799322605133057, -0.5978070497512817, "[TT] Expected Orbit Duration of the ChipSats = Only a few days"]
-[11.401374816894531, 8.930781364440918, "[FF] Observation Dates of the MODIS = February 8-12, January 22-29, and January 14-17"]
-[9.823164939880371, -1.1875112056732178, "[TT] Forward of the S-193 = 48\u00ba"]
-[6.367321968078613, 5.727789402008057, "[FF] Conference Date of the High Data Rate Optical Inter-Satellite Links = Sept. 20-24, 2009"]
-[8.109006881713867, -0.659906268119812, "[TT] Sea Level Rise Contribution of the CryoSat = 0.21 mm per year for Gulf of Alaska, 0.05 mm per year for High Mountain Asia"]
-[9.042251586914062, -0.22072173655033112, "[TT] Altitude of the Meteor-M2 = ~ 825 km"]
-[9.207808494567871, 6.090359210968018, "[TT] Boresight Pointing of the MWIR = \u00b130\u00ba from nadir"]
-[4.247498035430908, 7.4435319900512695, "[TT] Clock Source of the X-band transmitter = Local TXCO (Thermally Controlled Crystal Oscillator)"]
-[10.156683921813965, 1.6244099140167236, "[FF] Image Content of the eROSITA = LMC (Large Magellanic Cloud)"]
-[7.715387344360352, 8.728975296020508, "[TT] Spectral Bandpass of the Instrument = 400 nm to 850 nm"]
-[10.309945106506348, 1.897105097770691, "[FF] Emission of the Black Hole = Flare"]
-[11.574126243591309, 5.726349353790283, "[FF] S/C Structure of the IRS-1C and IRS-1D = Main platform and the payload platform (aluminium honeycomb structure)"]
-[6.770543098449707, 5.542949676513672, "[TT] Control Type of the Tom = Active"]
-[8.091202735900879, 1.4355230331420898, "[FF] Extension of the Navigable Area Limit Lines (NALL) = Can extend significant distances from shore"]
-[7.097007751464844, 8.642314910888672, "[TT] Spectral Channel 3 of the Satellite = 0.79 - 0.92 \u00b5m"]
-[6.020293712615967, 1.1634520292282104, "[FF] Announcement Date of the NASA Mission = August 8, 2013"]
-[5.809601306915283, -2.218364715576172, "[TT] Orbit velocity of the KOMPSAT-3A = 7.60 km/second"]
-[3.7555882930755615, 4.67160701751709, "[FF] Type of the OBRC = Radar"]
-[9.222514152526855, 5.911561965942383, "[FF] Components of the Microwave Calibration System = Small mirror and a hot reference absorber"]
-[9.461493492126465, 6.977705478668213, "[TT] Spatial Resolution of the MSU-SK = 170 m (in VIS) and 600 m (TIR)"]
-[13.158472061157227, 5.447235584259033, "[FF] Function of the Canadarm2 = Extract the new pair of solar arrays from Dragon\u2019s trunk"]
-[9.713531494140625, 4.744009971618652, "[FF] Spin Rate Change of the Satellite = Large, easily detectable change in the spin rate after a few hours or less"]
-[9.186256408691406, 4.75505256652832, "[FF] Attitude Control of the OPTOS = Required for the operation of an imaging camera"]
-[4.27176570892334, 3.328909397125244, "[FF] Ground Stations of the PRISMA = DLR antennas at Weilheim and the antennas operated by SSC in Sweden"]
-[10.665586471557617, 1.1114805936813354, "[TT] Size of the HD 21749b = About three times the size of Earth"]
-[5.477035999298096, 2.7338948249816895, "[TT] Host of the MOCC = University of Auckland\u2019s Te P\u016bnaha \u0100tea-Auckland Space Institute"]
-[3.7917845249176025, 6.073969841003418, "[TT] Deployment Type of the Helical Antenna = Self-Deploying"]
-[12.00086784362793, -0.3241124153137207, "[FF] Publication Date of the TESS = 30 November 2018"]
-[4.957784175872803, 0.40542885661125183, "[TT] Installation Date of the NICER-SEXTANT = June 13"]
-[7.522073268890381, 5.1877241134643555, "[FF] Short Range Navigation of the ATV-5 = Optical sensors on ATV"]
-[4.383180141448975, 7.815720081329346, "[TT] Downlink Frequency of the CMC Transceiver = 430-440 MHz"]
-[5.935659885406494, 2.4675707817077637, "[FF] Mission Outcome of the ESEO = Reduced success in achieving the science objectives"]
-[6.506389141082764, 5.834322452545166, "[TT] PRN of the GSAT-0204 = 22"]
-[8.198430061340332, -1.0378952026367188, "[FF] Measurement of the ICESat-2 = Arctic Snow Depth and Sea Ice Thickness"]
-[6.809708595275879, 4.263489246368408, "[FF] Safety Measures of the ELSA-d = Safety evacuations and passively safe trajectories, Collision Avoidance Maneuvers, Ground segment and operator oversight, Protected critical mission functions, Safety critical computing, Architectural redundancy, High-fidelity ground-based simulation"]
-[8.797263145446777, 7.644591331481934, "[TT] Pixel Size of the ABI = 14 \u00b5rad"]
-[6.4418864250183105, 6.422869682312012, "[FF] Growth Rate Approximation of the C/NOFS = Linear"]
-[11.741490364074707, 3.407851219177246, "[TT] Number of Valves of the PROP unit = 6"]
-[8.871933937072754, 4.759057998657227, "[FF] Control Method of the GSS = Attitude and orbit commands from SATSIM"]
-[13.251840591430664, 7.313655376434326, "[TT] Power of the \u00d8rsted = 54 W (40 W average load)"]
-[7.93379020690918, 8.668293952941895, "[TT] Spectral Range of the SWIR = 843-1043 nm"]
-[6.635157585144043, 1.8811196088790894, "[FF] URL of the ISIM = http://www.jwst.nasa.gov/isim.html"]
-[4.351455211639404, 5.267592430114746, "[TT] Frequency of the COSPAS-SARSAT beacons = 121.50 mHz"]
-[14.158502578735352, 3.12913179397583, "[TT] Cargo Mass of the CREAM = 1,258 kg"]
-[7.547274112701416, 1.3577591180801392, "[FF] Dark-Adapted Experiment of the Apollo 9 mission = Unknown"]
-[9.004338264465332, 5.393118381500244, "[TT] Cross-Track Pointing Capability of the Spacecraft = \u00b130\u00ba from nadir"]
-[3.6583404541015625, 5.41265344619751, "[TT] Coverage of the Ultrafine and Spotlight = From 49.54\u00ba to 54.2\u00ba"]
-[1.719507098197937, 6.137179851531982, "[TT] Warm Component Percentage of the Universe = 15 percent"]
-[8.727116584777832, 8.796984672546387, "[TT] Grating Angle of the Offner-type spectrometer = 5\u00ba at 325 nm"]
-[5.41826868057251, 0.34138619899749756, "[FF] Reentry Date of the STS-107 = Feb.1, 2003"]
-[8.32655143737793, 3.1827428340911865, "[FF] Chemical Composition of the OMC2 FIR4 = Nitrogen compound, hydrogen, carbon and oxygen compound"]
-[7.686467170715332, 5.456264019012451, "[FF] Components of the FTHSI instrument = Monolithic Sagnac interferometer, Fourier transform lens, cylindrical lens"]
-[5.296802997589111, 1.2482366561889648, "[FF] Presentation Date of the e-st@r program = Sept. 27-Oct. 1, 2010"]
-[8.080551147460938, 1.0374966859817505, "[TT] Eruption Start Time of the Anak Krakatoa Volcano = Around 16:15 local time"]
-[13.4628267288208, 5.824851989746094, "[TT] Open Circuit Voltage of the High-voltage solar array = Approximately 7V"]
-[4.796892166137695, 3.238553524017334, "[TT] Manufacturer of the FTHSI = Kestrel Corporation of Albuquerque, NM, and the Florida Institute of Technology, Melbourne, FL"]
-[7.619928359985352, 1.9188867807388306, "[FF] Service Impact of the Lacuna Space = Monitor peatland restoration impact"]
-[3.837770462036133, 7.902362823486328, "[FF] Operation Locations of the OQPSK = Transmitter, Mass Memory, Processor"]
-[5.4361677169799805, 3.9167990684509277, "[TT] Number of Satellites in Constellation of the Satellogic = 34"]
-[4.443665027618408, 2.8577005863189697, "[TT] Location of the FAI = Novaya Zemlya, Russia"]
-[9.74855899810791, 6.260565757751465, "[TT] Rotation Range of the Pointer Mirror = 0 to 360\u00ba"]
-[7.702016830444336, 8.004526138305664, "[TT] Sensitivity of the DWS = Few nrad/\u221aHz"]
-[8.08514404296875, 2.5789084434509277, "[TT] Measurement Domain of the GF-3 = Land"]
-[5.994075775146484, 4.564297676086426, "[FF] Navigation Message of the GIOVE-A = Not representative from structure and contents viewpoint"]
-[12.078960418701172, 5.019084453582764, "[TT] Face sheets thickness of the Bus structure = t = 0.8 mm"]
-[6.073015213012695, 3.326521635055542, "[FF] Project of the SumbandilaSat = First national satellite, First opportunity for SAC to operate a satellite, First opportunity to put the newly developed MCS architecture to test, First time in SunSpace's history where the day-to-day health monitoring of a satellite had to be transferred to an entity which is not the design authority, First time that remote sensing data products from a local source had to be integrated with historical non-African sources in the MES of SAC"]
-[5.665743827819824, 1.0401787757873535, "[FF] Meeting Date of the Rosalind = 13 December 2019"]
-[8.633813858032227, 1.1155718564987183, "[TT] Data Collection Duration of the Aquarius = Four-months"]
-[7.093373775482178, 2.492934226989746, "[FF] Edition of the Observation of the Earth and Its Environment = 4th"]
-[4.579479217529297, 0.4882223308086395, "[TT] Launch Date of the M3MSat = April 28, 2008"]
-[11.41690444946289, 5.724095821380615, "[TT] Main Metal Percentage of the Copper Alloy = 62%"]
-[5.145812034606934, 2.2633392810821533, "[TT] Mission Type of the Spektr-RG/SRG = Non-EO"]
-[4.591340065002441, 2.6750309467315674, "[FF] Historical Use of the Poenari Castle = Home and stronghold for Vlad Tepe\u015f"]
-[8.097366333007812, 4.033679008483887, "[FF] Steps of the Diffraction Computation = 1) Diffraction by the external occulter based on the Fresnel-Kirchhoff theory at the pupil and the primary objective level. 2) Propagation of the diffracted light in the instrument with ASAP"]
-[13.246370315551758, 2.915335178375244, "[TT] Satellite Mass of the GHGSat = 15 kg"]
-[13.650490760803223, 5.779982089996338, "[TT] Power of the Power GaAS body-mounted solar panels = 37 W EOL"]
-[11.648438453674316, 4.726349830627441, "[TT] Structure Shape of the UniSat-5 = Cuboid"]
-[4.915979385375977, 7.386110782623291, "[TT] Uplink Data Rate of the RF communications = 1.2 kbit/s"]
-[10.470067024230957, 6.532003879547119, "[FF] Retroreflectors of the Ralph and Norton = Mounted on the exterior surfaces"]
-[12.18871784210205, -0.26935872435569763, "[TT] Data Transmission Frequency of the TESS = Every 13.5 days"]
-[8.66689682006836, 1.9781503677368164, "[TT] Nominal of the Wind Vector Resolution = 25 km"]
-[8.228105545043945, 7.610891342163086, "[TT] Type of the TIR-1 and TIR-2 channel detector = Photo-conductive HgCdTe (Mercury Cadmium Telluride) detectors"]
-[12.091644287109375, 4.356544494628906, "[TT] Cion Power of the CICERO-6 = 8 W"]
-[6.066573143005371, 6.0343780517578125, "[FF] Microcontroller/Processors of the SSR = None"]
-[10.74586296081543, 2.1286778450012207, "[TT] Distance of X-ray jet from the Manatee\u2019s head of the XMM-Newton = About 100 light years"]
-[6.142353057861328, 2.482693672180176, "[FF] Development Purpose of the HAUSat-2 = Educational tool and a technology testbed"]
-[11.13033390045166, 7.193371772766113, "[TT] Swath Width of the Spacecraft = 23 km"]
-[8.455718040466309, 0.11900642514228821, "[TT] Study Subject of the Rosetta spacecraft = Comet 67P/Churyumov-Gerasimenko"]
-[5.169821262359619, 3.232177257537842, "[TT] Manufacturer of the Weather Satellite = Lockheed Martin"]
-[7.993697643280029, 2.7695770263671875, "[FF] Coverage of the International Space Station = Areas where thunderstorms are common"]
-[7.957906723022461, 6.213233470916748, "[FF] Imaging Concept of the OCM = Extension of the imaging concept adopted for the IRS LISS instruments"]
-[11.333261489868164, 4.7396955490112305, "[TT] Depth of the Misteriosa Bank = 9 to 12 fathoms"]
-[9.00153923034668, 4.399447917938232, "[TT] Angle Accuracy of the Sun Sensor Device = < 0.15\u00ba"]
-[5.834468841552734, 5.112855434417725, "[FF] Data Transmission of the EDRS = High speed OISL (Optical Intersatellite Links) between LEO and GEO relay satellite and multi channel RF downlinks in Ka-band for the GEO to ground links"]
-[13.466510772705078, 5.535514831542969, "[TT] Number of Solar Panels of the AprizeSat = 6"]
-[5.6638360023498535, 4.492480754852295, "[FF] Connectivity of the 5G Network = Reliable connection for people and devices, anytime and anywhere, with increased security"]
-[11.865145683288574, 6.7461934089660645, "[TT] Bias Voltages of the EPE = 1.25-1.5 times the values required for full depletion"]
-[8.515482902526855, 1.6862770318984985, "[TT] Range of values of the Integrated water vapor = 0-80"]
-[8.776774406433105, 5.171752452850342, "[TT] Quantity of the IMU (Inertial Measurement Unit) = 2"]
-[12.945697784423828, 7.385344982147217, "[TT] Instrument Power of the DST (Dobson Space Telescope) = < 0.5 W"]
-[3.82041597366333, 1.2351313829421997, "[FF] First Stage Landing of the Falcon 9 = Land safely on Earth to be refueled and fly again"]
-[4.837895393371582, 1.2479504346847534, "[FF] Operational of the GENSO = By the time that Delfi-n3Xt is launched"]
-[6.598325729370117, 0.8146581053733826, "[TT] Launch Date of the Solar-A / Yohkoh = 30 August 1991"]
-[11.239931106567383, 5.844696044921875, "[FF] Construction of the Thermal Strap = Pyrolytic graphite film for the flexible section and aluminum terminals on each end"]
-[13.807168006896973, 3.133371353149414, "[TT] Mass of the Payload = 149 kg"]
-[9.81668472290039, 2.6435437202453613, "[FF] Launch Date of the NanoRacks-QB50 = April 5, 2017"]
-[8.565888404846191, 2.8411664962768555, "[FF] Purpose of the MI = Monitor clouds, atmosphere, snow cover, and Earth surface radiation"]
-[14.251895904541016, 3.0975327491760254, "[TT] Mass of the CEASE-2 = 1.3 kg"]
-[7.509900093078613, 3.385929584503174, "[FF] Definition of the Level 1 = Perception of the elements in the environment"]
-[4.121728897094727, 0.1795625239610672, "[TT] Launch Date of the Falcon 9 = February 4, 2021"]
-[6.113158702850342, 6.421859264373779, "[TT] Latency of the TBS Product latency = Near real-time to hrs (product dependent)"]
-[7.407266616821289, 1.8247919082641602, "[FF] Forest Cover Loss of the Forest Alert Service (FAS) = 5-6 per cent to just 0.06 per cent"]
-[4.39841890335083, 7.927450656890869, "[TT] Forward Link Frequency of the LPT = 2106.40625 MHz"]
-[6.230984210968018, 4.8792195320129395, "[FF] Function of the OBC = Interfaces with all the subsystems on CanX-2, responsible for all normal satellite operations, including telemetry collection, execution of attitude determination and control algorithms, commanding of experiment payloads, communication with the ground"]
-[10.386933326721191, 7.157642841339111, "[TT] Primary Mirror Size of the Telescope = 40 cm"]
-[4.6183366775512695, 7.3471879959106445, "[TT] Quantity of the S-band transceivers = 2"]
-[14.26868724822998, 3.1219685077667236, "[TT] Mass of the DCG = 4 kg"]
-[4.750508785247803, 8.327579498291016, "[TT] Center Frequency of the 1 = 50.3 GHz"]
-[13.414584159851074, 6.768892765045166, "[TT] Power of the Spacecraft = 3.4 kW (BOL), 2.1 kW (after 5 years)"]
-[2.530698299407959, 0.16988538205623627, "[TT] Pulse period (ms) of the B1813-140 = 3.300"]
-[6.520707130432129, 2.3373565673828125, "[TT] Displacement between Exposures of the Euclid Reference Survey = 100 arcsec"]
-[5.1762166023254395, 2.2770488262176514, "[TT] Mission Type of the MidSTAR-1 = Non-EO"]
-[5.7683868408203125, 5.829885005950928, "[TT] Data Interface of the SAMPEX = SEDS (Small Explorer Data System)"]
-[10.777996063232422, 1.3792964220046997, "[TT] Mass of the Markarian 335 = 10 million times the mass of our sun"]
-[10.866155624389648, 3.997586727142334, "[TT] Drag Sails of the CanX-7 = 4"]
-[9.520467758178711, 4.816152572631836, "[TT] Stabilization of the Resurs-O1 spacecraft = Three-axis"]
-[6.9171977043151855, 2.8967175483703613, "[TT] Mission Type of the HySIS = Earth Observation"]
-[5.355941295623779, 3.136340856552124, "[TT] Manufacturer of the AstroRad vest = ISA"]
-[13.669013023376465, 6.996553421020508, "[TT] PPTs of the EPS = 4 independent PPTs"]
-[4.125121116638184, 1.3852488994598389, "[TT] Operation Start Date of the Meteosat First Generation = November 1977"]
-[5.664753437042236, 7.038976192474365, "[TT] Data Rates of the OBC = 130 Mbit/s"]
-[7.730318546295166, 9.497038841247559, "[TT] Center Wavelength of the B11 = 1610 nm"]
-[9.750712394714355, -0.6015021800994873, "[TT] Orbit Altitude of the ALOS-3 = 618 km"]
-[13.547900199890137, 5.478309631347656, "[TT] Quantity of the Solar cells = 5 parallel strings of 4 series connected"]
-[6.970225811004639, 6.364150047302246, "[TT] Number of Flight Models of the MWI Instrument = Three"]
-[8.9082670211792, 4.35084342956543, "[FF] Attitude Sensing of the OceanSat-2 = Earth horizon sensors, digital sun sensors, triaxial magnetometers and a gyroscope-based inertial reference unit"]
-[6.449742794036865, 1.445013403892517, "[TT] Prime Phase Duration of the eROSITA = Four years"]
-[11.474026679992676, 3.453155517578125, "[TT] Position Control of the CNAPS = 1 m"]
-[5.058901309967041, 0.2900001108646393, "[TT] Deployment Date of the CYGNSS = Dec. 15, 2016"]
-[11.781824111938477, 3.261021852493286, "[TT] Thrust of the Main Thrusters = 10 N"]
-[4.920662879943848, 1.5481541156768799, "[TT] Geometric Calibration of the G\u00f6kt\u00fcrk-2 = Yearly basis"]
-[4.89744234085083, 7.356728553771973, "[TT] Uplink Data Rates of the RF Communications = 1.2 or 9.6 kbit/s"]
-[12.698737144470215, 1.9026397466659546, "[FF] Objective of the SAGE-II = Monitoring of concentrations and distributions of stratospheric aerosols, nitrogen dioxide, and water vapor"]
-[7.4203386306762695, 5.13719367980957, "[FF] Alignment Mechanism of the DST = Fine precision mechanism"]
-[9.677999496459961, 7.106497287750244, "[TT] Spatial Resolution of the Instrument = 10 m"]
-[8.365751266479492, 7.115820407867432, "[TT] Number of BW Photographs of the Metric Camera = 473"]
-[11.95949649810791, 4.8804144859313965, "[TT] Dimensions of the GaInP cells = 2 cm x 2 cm"]
-[6.7773332595825195, 4.101803779602051, "[FF] Command Processor of the DMSP-19 = Unreachable"]
-[9.147459030151367, 7.62082576751709, "[TT] Spatial Sampling Distance of the Imager = 10 m (VNIR), 20 m (SWIR), 60 m (3 bands)"]
-[8.267375946044922, 6.438050746917725, "[TT] Accuracy of the PM and SCM = Equivalent at high energies, 10% difference at low energies"]
-[4.965847015380859, 3.2216603755950928, "[FF] Supplier of the AOCS = OHB-Sweden"]
-[4.703746795654297, -0.06126109138131142, "[TT] End of Life Date of the GovSat-1 = 2033"]
-[7.84874963760376, 1.1624356508255005, "[TT] Gravity of the Mars = About one-third that of Earth\u2019s"]
-[14.198173522949219, 3.145740032196045, "[TT] Mass of the ESEO = ~40 kg"]
-[7.8932342529296875, 5.9047040939331055, "[FF] Grid Positions of the CCRR = Constructed to cover the field of view of FLLS"]
-[6.895310878753662, 3.477431058883667, "[FF] Movement of the REXJ = Can theoretically move around the space station"]
-[6.514437675476074, 3.929746389389038, "[FF] Purpose of the Tyvak 61C = Technology demonstration and astronomy mission"]
-[6.905674934387207, 1.9164682626724243, "[FF] URL of the SP-402 A New Sun = http://history.nasa.gov/SP-402/ch4.htm"]
-[8.1346435546875, -0.32437968254089355, "[TT] Trend of the Arctic Sea Ice = Decline"]
-[6.148322582244873, 5.867475986480713, "[FF] Function of the RF front-end = Amplification and initial down-conversion of the signal"]
-[10.628913879394531, 1.2652521133422852, "[TT] Energy Received from Star of the Kepler-186f = One-third of the energy Earth gets from the sun"]
-[6.719693183898926, 1.6193749904632568, "[FF] Purpose of the Emirates Mars Mission = Accelerate the development of the UAE\u2019s space sector, education and science community"]
-[12.98416519165039, 7.355061054229736, "[TT] Current of the GPS OEM Sensor = About 0.15 A"]
-[9.816529273986816, 8.103750228881836, "[TT] Focal length of the 16 mm camera = 16 mm"]
-[13.832693099975586, 6.299632549285889, "[FF] Functions of the GomSpace NanoPower P60 = Conditioning the solar array input, regulating the battery charge/discharge cycle, and providing power to the other subsystems"]
-[7.971001148223877, 8.572554588317871, "[TT] Spectral range of the MERSI = 0.41-12.5 \u00b5m"]
-[8.550498008728027, 1.8616138696670532, "[TT] Error of the Ocean SST = \u00b12 m/s"]
-[9.099947929382324, 6.761239051818848, "[TT] Vertical Accuracy of the WorldDEM4Ortho = 4 meters"]
-[13.806113243103027, 5.344389915466309, "[TT] Cell Type of the Solar Arrays = Triple-junction GaAs design"]
-[14.620248794555664, 6.722529888153076, "[TT] Battery Packs Capacity of the Electrical Power Subsystems (EPS) = 14.4 Ah"]
-[11.463899612426758, 3.941859722137451, "[FF] Risk of Collision of the AeroCube-OCSD-B and -C = Little risk"]
-[6.438726425170898, 6.999283790588379, "[TT] Range of Optical Link of the SILEX Optical Terminal = Up to 45000 km"]
-[10.632062911987305, 8.858113288879395, "[TT] Pixel size of the Channel 3 = 32 km x 32 km"]
-[3.570774793624878, -1.0623210668563843, "[TT] Orbit of the GRACE = Pole to pole"]
-[5.612987041473389, 2.54600191116333, "[FF] Developers of the Timepix = Carlos Granja, Michal Platkevic, Daniel Turecek, Vaclav Kraus, Michael Holik, Jan Jakubek, Zdenek Vykydal, Stanislav Pospisil, Toshinori Kuwahara"]
-[9.562321662902832, 9.097319602966309, "[TT] Resolution of the Iris = 100 times higher than any other satellite"]
-[9.371299743652344, 7.083460330963135, "[TT] Resolution of the Severyanin = Up to 400 m"]
-[4.56911563873291, 6.736046314239502, "[FF] Purpose of the RF Crossover Switch = Hedge against loss of one of the redundant UHF command and telemetry transceivers"]
-[10.131328582763672, -1.666245460510254, "[TT] Inclination of the Resurs-P1 = 97.3\u00ba"]
-[12.831156730651855, 7.601437568664551, "[TT] Output Power of the Instrument Power Unit = 463 W"]
-[9.665682792663574, -0.37037715315818787, "[TT] Pass Elevation Sequence of the ASTERIA = High, Low, High"]
-[8.014659881591797, 5.126138210296631, "[FF] Vibration Design of the Instrument = 150 g static, random 24.7 g rms"]
-[9.56067943572998, 4.041937828063965, "[TT] Dynamic Range of the Magnetic Field Measurement System = 60 dB"]
-[3.2806334495544434, 5.15710973739624, "[TT] Incidence Angles of the SAR = 20-55\u00ba"]
-[9.429637908935547, 3.8337278366088867, "[FF] Measurement Type of the Overhauser Magnetometer = Magnetic field (scalar), Magnetic field (vector)"]
-[8.904359817504883, 4.545459747314453, "[FF] Attitude Control of the Satellite = Hybridization of star sensor and accelerometer measurements"]
-[10.087536811828613, 4.453946590423584, "[FF] Torque Margin of the RDA = Not provided"]
-[8.297292709350586, 7.754884243011475, "[TT] Multispectral Bands Detector Array of the WV-3 Imager = 9,300 pixel"]
-[5.877058029174805, 2.918132781982422, "[FF] Advancement of the NPSAT-1 = Provides university students and faculty with a unique platform on which they can conduct science and engineering experiments"]
-[6.019700050354004, 5.560391426086426, "[TT] Redundancy of the Transmit chain = Two chains"]
-[8.934664726257324, 5.401706218719482, "[TT] Pointing of the Orbiter = Primarily nadir pointing"]
-[10.172019958496094, 1.0304969549179077, "[TT] Distance from Earth of the The Teacup = 1.1 billion light years"]
-[5.683993816375732, 1.084588646888733, "[FF] Mission Update Date of the IBEX = Nov. 14, 2011"]
-[7.986030578613281, 5.07697868347168, "[FF] Calibration of the DDM = Relative"]
-[4.767276287078857, 0.1821620911359787, "[TT] Deployment Date of the RemoveDEBRIS spacecraft = 20 June 2018"]
-[6.0437774658203125, -0.53762286901474, "[TT] Mission Duration of the RBSP spacecraft = 2 years"]
-[3.727374315261841, 6.660748481750488, "[TT] Beamwidth of the Antenna = 1.1\u00ba"]
-[8.859007835388184, 4.691191673278809, "[TT] Quantity of the Star sensor = 2 units"]
-[3.4496896266937256, -0.9319460391998291, "[TT] Orbit Type of the Landsat-9 = Sun-synchronous near-circular orbit"]
-[6.6073832511901855, 1.904590368270874, "[FF] URL of the Space Based Space Surveillance (SBSS) = http://www.afspc.af.mil/library/factsheets/factsheet.asp?id=20523"]
-[5.880472183227539, -0.7333212494850159, "[TT] Reliability of the OCI = 0.991 at the end of two years in orbit"]
-[9.624814987182617, 4.810732841491699, "[TT] Stabilization of the LEOStar-3 = 3-axis, zero momentum bias, nadir pointing"]
-[9.75987720489502, 4.227484226226807, "[TT] Quantity of the Magnetometers = Three rods"]
-[5.05375862121582, 2.390676736831665, "[TT] Mission Type of the STRV-1a and -1b = Non-EO"]
-[9.767831802368164, 5.8167548179626465, "[TT] Module Rotation of the ECAL = 90\u00ba"]
-[5.164688587188721, 0.47829458117485046, "[TT] Launch Date of the CALIPSO = April 28, 2006"]
-[13.603301048278809, 6.893270492553711, "[TT] Power, Thermal, Propulsion, Mechanisms of the Bus = Nominal"]
-[7.619011402130127, 3.428487777709961, "[TT] Impact Test Outcome of the DebriSat = Planned catastrophic outcome"]
-[5.382059574127197, 4.918310165405273, "[FF] Radius of the Ground Station Coverage = 2000 km"]
-[3.4659693241119385, -0.8828572034835815, "[TT] Orbit Type of the GCOM-W1 = Sun-synchronous orbit"]
-[16.48828887939453, 3.5740222930908203, "[FF] Serial Production Initiation Date of the OneWeb = June 27, 2017"]
-[8.975436210632324, 8.58657455444336, "[TT] Band 5 Wavelength Range of the Telescope = 10.3 - 11.3 \u00b5m"]
-[13.669729232788086, 3.067408323287964, "[TT] Payload Capacity of the Super Strypi launcher = 300 kg"]
-[11.134390830993652, 3.007993698120117, "[TT] Solar Power of the PARASOL microsatellite = 180 W"]
-[7.291445732116699, 1.3082973957061768, "[TT] Principal Investigator of the Kepler Space Telescope = William Borucki"]
-[11.073713302612305, 6.0034356117248535, "[TT] Material of the Cavity = Zerodur"]
-[4.375865459442139, 6.859584808349609, "[TT] Telecom Frequency of the Spacecraft = S-band"]
-[7.953643798828125, -0.4458027184009552, "[FF] Ice Loss Detection of the GRACE-FO satellites = Yes"]
-[5.939579963684082, 1.5872130393981934, "[FF] Presentation Date of the SI-200 Mini-Satellite Platform = Oct. 12-16, 2009"]
-[5.794666290283203, 4.456376552581787, "[FF] Purpose of the LEO Network = Minimize or eliminate the need for new satellite companies to develop their own ground network"]
-[3.460298538208008, 1.6241573095321655, "[FF] Mission Date of the Sentinel-2 = June 28-July 2, 2010"]
-[7.649962425231934, 3.337982177734375, "[FF] Purpose of the AMSR-E = Measure geophysical data related to the Earth's environment"]
-[5.926004409790039, 3.042274236679077, "[FF] Coordination Responsibilities of the Executive = Coordination with EC and GSA, analysis of operational requirements, dissemination of joint information papers at IMO and IALA"]
-[10.880287170410156, -0.3177872896194458, "[TT] Conference Date of the TanDEM-X = April 25-30, 2010"]
-[8.136886596679688, -1.0987144708633423, "[FF] Snow Depth of the ICESat-2 = 14 cm (5.5 inches) in October, 27 cm (10.6 inches) in April"]
-[8.277496337890625, 2.625157117843628, "[TT] Cloud Discrimination Algorithm of the GOSAT = CLAUDIA (Cloud and Aerosol Unbiased Decision Intellectual Algorithm)"]
-[7.523311138153076, 4.347829818725586, "[FF] Sensor Complement of the AMS-02 = Unknown"]
-[13.381834983825684, 6.91733980178833, "[TT] Power of the Spacecraft Repeater = 53 W"]
-[6.5110554695129395, 4.1872639656066895, "[FF] Payload of the MPQ442 = SuperLab"]
-[5.017266273498535, 0.45067018270492554, "[TT] Launch Date of the Aeolus = 2018"]
-[7.456212520599365, 0.3852691054344177, "[FF] Instrument of the OSIRIS-REx = OTES spectrometer"]
-[7.822635650634766, 5.755868434906006, "[TT] Developer of the Vision-based sensor system = Technical University of Denmark (DTU)"]
-[12.873149871826172, 7.093362331390381, "[TT] Efficiency of the 27% = 27%"]
-[13.65616512298584, 3.074903964996338, "[TT] Payload Capability of the PSLV-XL = 1750 kg in 600 km SSPO"]
-[4.544593334197998, 7.795472145080566, "[TT] Frequency Band of the CW transmitter = UHF (437.375MHz)"]
-[10.449767112731934, 5.711374282836914, "[TT] Equilibrium Temperature of the TOI 270 d = 150\u00ba Fahrenheit (66\u00ba C)"]
-[6.349400520324707, 0.7421213388442993, "[TT] Global Coverage of the GNOS-2 = 2 weeks"]
-[9.855470657348633, -0.3654613792896271, "[TT] Altitude of the Satellite = 904 km"]
-[4.880199909210205, 8.311071395874023, "[TT] Operation Frequencies of the TMR = 18, 21, and 37 GHz"]
-[10.749317169189453, 1.092871069908142, "[TT] Mass Compared to Earth of the TOI 270 d = 5 times Earth\u2019s mass"]
-[9.034297943115234, -0.7823672890663147, "[TT] Orbital Period of the MEO Constellation = 5/3 revolutions/day"]
-[13.386298179626465, 5.4755425453186035, "[TT] Number of Panels of the Solar Array = 8"]
-[10.795547485351562, 5.218977928161621, "[TT] Distance to M2 of the M1 = 3 \u00b5m"]
-[6.772112846374512, 0.11174905300140381, "[TT] Mission Duration of the Kepler = Three-and-a-half years"]
-[8.784866333007812, 2.6911516189575195, "[TT] Error of the Atmosphere = \u00b10.2 kg/cm2"]
-[6.140437602996826, 5.509975910186768, "[FF] Memory of the CubeComputer = Flash for in-flight reprogramming (dual redundant)"]
-[13.502952575683594, 2.9915595054626465, "[TT] Mass of the Spacecraft bus = 1750 kg"]
-[5.30486536026001, 5.660617828369141, "[TT] Data Bus of the C&DH Subsystem = MIL-STD-1553B"]
-[9.098684310913086, 6.53911018371582, "[TT] Performance of the FSS = \u00b10.35\u00ba"]
-[5.699486255645752, 4.867190837860107, "[FF] Data Downlink Frequency of the GFO = Real-time at sea, approximately every 12 hours at CONUS ground sites"]
-[9.869426727294922, -0.6125926971435547, "[TT] Orbit Altitude of the MicroSat-2a = 514 km"]
-[5.816135406494141, -0.7664788365364075, "[TT] Orbital Lifetime of the KE-2M satellite = Approximately six months"]
-[7.64554500579834, 4.918377876281738, "[FF] Navigation of the Lander = Configured for inertial navigation from separation to the end of rough braking"]
-[8.357806205749512, 4.624534606933594, "[TT] Polar Motion Improvement (x-component) of the LARES = 24%"]
-[8.639618873596191, 1.0808615684509277, "[FF] Launch Date of the Aquarius = Unknown"]
-[5.972978115081787, 2.791032314300537, "[TT] Deployment Count of the J-SSOD (JEM Small Satellite Orbital Deployer) = 10"]
-[4.541348934173584, 3.0186924934387207, "[TT] Location of the Tracking and Control Center (TACC) = Tsukuba Space Center"]
-[7.123845100402832, 2.3803467750549316, "[FF] Sensitivity of the Solar-B / Hinode = Unknown"]
-[7.741684913635254, -0.9078946709632874, "[FF] Status Updates of the ICESat-2 = Ongoing"]
-[11.248308181762695, 5.613689422607422, "[TT] Material of the Propulsion System = Plastic"]
-[5.8563337326049805, 4.793076515197754, "[TT] Programming Language of the SCIP = Forth"]
-[4.286688804626465, 1.2033069133758545, "[FF] Current Policy of the Meteosat Satellites = Keep two operable satellites in orbit and to launch a new satellite close to the date when the fuel in the elder of the two starts to run out"]
-[9.765951156616211, -0.6190555095672607, "[TT] Altitude of the Orbit = 575 km"]
-[10.730425834655762, 1.0605539083480835, "[TT] Size of the TOI 700 c = 2.6 times larger than Earth"]
-[5.3635573387146, 1.48829984664917, "[FF] Phase B2/C/D/E1 Contract of the OPS-SAT = Kicked off in February 2015"]
-[9.25300407409668, 6.900307655334473, "[TT] Spatial Resolution of the Radiometer = 90 \u00b5rad"]
-[7.922384738922119, 4.400300025939941, "[FF] Function of the SEM-2 = Investigate the link between deep dielectric charging and the spacecraft anomalies"]
-[5.315592288970947, 3.1688120365142822, "[FF] Software Platform of the DLR Compact-Satellite Series = Unknown"]
-[10.040243148803711, -1.5239317417144775, "[TT] Inclination of the Corvus-BC 5 = 97.5\u00b0"]
-[9.115511894226074, 7.557541370391846, "[TT] Multispectral Resolution of the SuperView 1A and 1B = 2 m"]
-[8.802401542663574, 2.2783355712890625, "[FF] Observation Duration of the SOHO = 10 years"]
-[9.091059684753418, 1.3801380395889282, "[TT] Test Message Date of the Voyager 2 = October"]
-[6.308297634124756, 5.429126262664795, "[TT] Architecture of the UVNS = Modular"]
-[14.235686302185059, 3.2123782634735107, "[TT] Mass of the FREND = 36 kg"]
-[8.71894645690918, 0.18982672691345215, "[TT] Distance from Bennu of the OSIRIS-REx = 328,000 miles"]
-[5.935249328613281, 3.0438363552093506, "[TT] Staff Count of the Orbital Sidekick = 33"]
-[6.292749404907227, 0.623652994632721, "[TT] Launch Date of the Gaia = December 19, 2013"]
-[7.021535396575928, -0.18658840656280518, "[TT] Eclipse Duration at \u03b2=0\u00b0 of the ASTERIA = 35.8 minutes"]
-[10.110899925231934, -0.5034295916557312, "[TT] Orbit Altitude of the R3 CubeSat = 500 km"]
-[13.568626403808594, 5.788617134094238, "[FF] Power Source of the Lander = Body mounted solar panels"]
-[10.035133361816406, 5.546431541442871, "[FF] Thermal Environment Before Separation of the MMO = Low temperature, not illuminated by sunlight"]
-[6.01715612411499, -0.6711769700050354, "[TT] Mission Life of the Spacecraft = 1 year min (2 year goal)"]
-[4.401181697845459, 2.0898382663726807, "[FF] URL of the Dubaisat-1 = http://www.arabianaerospace.aero/article.php?section=technology&article=eiast-celebrates-first-anniversary-of-dubaisat-1-launch"]
-[18.64566421508789, 3.939401865005493, "[TT] NE\u0394T of the 2 = 0.4 K"]
-[9.322038650512695, 4.866103172302246, "[FF] Spatial Resolution of the Attitude Determination & Control System = Better than 100 m"]
-[4.4756245613098145, 1.7326726913452148, "[FF] Launch Date of the NorSat-2 = Unknown"]
-[8.426545143127441, 7.174506187438965, "[TT] Number of Normal Cameras of the Payload = 24"]
-[9.066085815429688, 5.740050315856934, "[TT] Random Error of the NSTT = < 4 arcsec (3\u03c3)"]
-[7.006805896759033, 7.032191276550293, "[TT] Intensity of the Laser Beams = Much higher than normal"]
-[6.89503812789917, -0.538066029548645, "[TT] Retargeting Frequency of the Platform = Twice per orbit"]
-[6.391133785247803, 0.32009971141815186, "[TT] Revisit Time of the ROSE-L = Three days for both regional and global coverage"]
-[10.14960765838623, 8.071194648742676, "[TT] Focal Length of the Telescope = 2000 mm"]
-[9.545421600341797, 4.816119194030762, "[TT] ADCS of the DSX = 3-axis stabilized"]
-[8.662947654724121, 4.753086566925049, "[TT] Star Tracker of the SPOT-6 = HYDRA"]
-[5.670776844024658, 7.963626861572266, "[TT] Measurement Rate of the CESS = 1 Hz"]
-[10.37318229675293, 5.554703235626221, "[TT] Plasma Temperature of the Perseus galaxy cluster = Around 50 million degrees"]
-[11.006933212280273, 6.278761863708496, "[TT] SiC Strength of the OPS = Two to three times higher than a conventional sintered SiC"]
-[7.4601359367370605, 7.974564552307129, "[TT] Color of the Laser Source = Orange"]
-[9.40027141571045, 8.616761207580566, "[FF] Entrance Slit of the SDEA = Horizontal from the upper (lower) left"]
-[7.5797834396362305, 6.872828483581543, "[TT] Operational Cadence of the Instrument = Rotate 120\u00ba in < 2 minutes to blackbody view"]
-[5.200117588043213, 2.4804494380950928, "[TT] Mission Type of the Myriade/AstroSat-100 = EO"]
-[7.973032474517822, 5.8492560386657715, "[FF] Function of the NICER = Measure light echoes"]
-[8.465686798095703, 3.550726890563965, "[FF] Function of the Chibis-M = Monitor electromagnetic environment of the Earth at ionospheric altitudes and produce simultaneous measurements of electromagnetic emissions"]
-[10.437336921691895, 5.792577266693115, "[TT] Temperature Range of the Instrument = -30\u00baC \u2264 T \u2264+70\u00baC"]
-[3.774019718170166, 7.989896774291992, "[TT] Modulation Type of the QPSK modulation = QPSK (Quadrature Phase Shift Keying)"]
-[6.714536666870117, 3.972245216369629, "[FF] Deployment Location of the Astro Pi = Columbus module and looking through a hatch window towards the Earth"]
-[8.68857479095459, 2.6582367420196533, "[TT] Constellation Size of the Aurora = Six-satellite"]
-[11.283768653869629, 0.6856572031974792, "[FF] Atmospheric Phenomenon of the Planets with One Side Permanently Facing Their Star = Clouds of different compositions might be visible, depending on the side observed"]
-[9.382293701171875, 6.4483137130737305, "[TT] Azimuth Resolution of the P Mode = 1 m"]
-[9.674790382385254, 0.14302660524845123, "[FF] Function of the Mortar = Propels the drogue parachute out"]
-[13.108282089233398, 7.347695827484131, "[TT] Power Consumption of the BIRCHES = 10-15 W"]
-[3.332484245300293, 1.4650380611419678, "[TT] Launch Year of the Sentinel-4B = 2032"]
-[6.899034023284912, 9.501452445983887, "[TT] NEDT at 300 K of the Band 3 = 0.5 K"]
-[3.565990686416626, -0.8711689114570618, "[TT] Orbit of the NOAA = Polar"]
-[11.512687683105469, 3.368290424346924, "[FF] Type of the Miniature Propulsion System = Miniature"]
-[4.3820576667785645, 7.811666965484619, "[TT] Uplink Frequency of the RF communications = 2.0 GHz"]
-[9.199522018432617, 7.450479984283447, "[TT] Panchromatic of the Medium resolution = 0.43-0.7 \u00b5m"]
-[9.170147895812988, 5.640545845031738, "[TT] Pointing Jitter of the ASTERIA = 1\u03c3 ~0.5\""]
-[5.056229591369629, 0.334236204624176, "[TT] Test Date of the SpaceWire = December 2010"]
-[5.5249199867248535, 2.6313421726226807, "[TT] Control of the JEM/RMS = JAXA (Japanese Aerospace Exploration Agency)"]
-[5.701756000518799, 6.882192611694336, "[TT] Control and Communication MOPS of the DSP System = 10 to 20 MOPS"]
-[7.964890480041504, 0.11796710640192032, "[TT] Purpose of the GRACE-FO = Measure changes in gravitational pull"]
-[5.375614643096924, 3.8559978008270264, "[FF] Constellation Expansion Plan of the ICEYE = More satellite additions later this year"]
-[4.772317409515381, 4.576811790466309, "[FF] Purpose of the GMDSS = Rescue mariners in emergency situations while at sea"]
-[7.513984203338623, 7.734569549560547, "[TT] Dynamic Range of the SXI = 1000"]
-[7.321224689483643, 7.8534932136535645, "[TT] Dynamic Range of the FIELDS suite = 140 dB"]
-[7.943633079528809, 3.1557929515838623, "[FF] Purpose of the IMG = Interferometric Monitor for Greenhouse Gases"]
-[4.430246353149414, 7.508120059967041, "[TT] Downlink Frequency of the HRIT/EMWIN = L-band"]
-[8.632888793945312, 8.749652862548828, "[TT] Spectral Coverage of the Instrument = 3.74 - 15.4 \u00b5m for the array grating spectrometer (IR bands)"]
-[9.829961776733398, -0.23757228255271912, "[TT] Data Stack Height of the Nancy Grace Roman = 330 miles (530 km) high after a single day"]
-[6.343934059143066, 4.816405296325684, "[FF] Function of the Payload Control Unit = Provide the command and control interface between the platform and the payload"]
-[9.668899536132812, 8.196263313293457, "[TT] Depth of Field of the Telecentric lens and camera = 25 m to 250 m"]
-[5.454414367675781, 5.055900573730469, "[TT] Unique Label of the CAN Bus = Yes"]
-[8.075627326965332, 8.989757537841797, "[TT] Wavelengths of the CarbonSpec = 1.61 \u00b5m, 2.06 \u00b5m, 0.76 \u00b5m"]
-[5.443862438201904, 0.9903025031089783, "[FF] Arrival Date at Launch Site of the OHB Communications Satellite = Dec. 1, 2016"]
-[7.250088691711426, 1.6927169561386108, "[FF] Function of the SporeSat = Study the gravity response of ion channels"]
-[8.082270622253418, 4.241367816925049, "[TT] Instrument Type of the ScaRaB = Earth radiation budget radiometers"]
-[13.308500289916992, 5.465828895568848, "[TT] Solar Array of the EPS = Single deployable with single-axis articulation capability"]
-[10.63370418548584, 8.884486198425293, "[TT] Pixel Size of the Channel 4 = 32 x 32 km"]
-[13.178401947021484, 7.302067756652832, "[TT] Power Consumption of the RMU = < 4 W"]
-[9.772544860839844, 7.512449264526367, "[TT] Ground Sample Distance (GSD) of the GLM CCD = Approximately 8 km"]
-[9.944927215576172, -0.476211279630661, "[TT] Orbit Altitude of the GOSAT-GW = 666 km"]
-[3.7307653427124023, 6.659712314605713, "[TT] IFOV (beam width) of the Antenna = 1.81\u00ba"]
-[9.966429710388184, -1.4277722835540771, "[TT] Orbit Inclination of the STP-S26 mission = 72\u00ba"]
-[5.091095924377441, 1.6070497035980225, "[TT] Development Status of the VBN = Currently being developed"]
-[4.757564067840576, 7.6561150550842285, "[FF] Gain Control Method of the Ranging Channel = Apportioning the ranging channel the correct predetermined modulation index in the transmit modulator"]
-[5.33683967590332, 6.656357288360596, "[TT] Onboard Data Storage of the RF Communication System = Up to 64 kbyte"]
-[3.471808671951294, 5.101398468017578, "[TT] Instrument Type of the C-band synthetic aperture radar = C-band synthetic aperture radar"]
-[3.9786362648010254, 2.0514492988586426, "[TT] Manufacturer of the Falcon 9 = SpaceX"]
-[3.9484808444976807, 7.824920177459717, "[TT] Modulation Schemes of the GATE Signal Generator = AltBOC and CASM (Coherent Adaptive Subcarrier Modulation)"]
-[5.40785551071167, 7.818012237548828, "[TT] Sampling Frequency of the fADC = 80 MHz"]
-[6.10457706451416, 5.990845203399658, "[TT] Performance of the TPS = Excellent"]
-[4.854313850402832, -0.8647449612617493, "[TT] Reentry Duration of the Dragon = About 30 minutes"]
-[13.344901084899902, 6.960583209991455, "[TT] Onboard Power of the FY-2F = 300 W"]
-[10.177519798278809, 4.663686752319336, "[TT] Nominal Angular Momentum of the MW = 0.125 Nms"]
-[11.676246643066406, 5.080178260803223, "[TT] Dimensions of the MTF Target = 30 m x 30 m"]
-[6.094625473022461, 5.439544677734375, "[TT] Operation of the OHRIS = Can be operated in parallel with OHIS"]
-[6.900230884552002, 2.510625123977661, "[FF] Impact of the Remote Sensing Space Systems Act = Imposed new regulatory requirements"]
-[13.836525917053223, 3.344942569732666, "[TT] Mass of the Data Relay Transponder = ~70 kg"]
-[5.504265785217285, -1.8019553422927856, "[TT] Launch Date of the KOMPSAT-3 = 18 May 2012"]
-[3.4586329460144043, -0.9049319624900818, "[TT] Orbit Type of the ResourceSat-2A = Sun-synchronous orbit"]
-[3.7130181789398193, 4.737586975097656, "[FF] Sensor Types of the EO ASI = SAR and hyperspectral"]
-[4.437070369720459, 5.4315338134765625, "[TT] Number of Beacons Received of the KySat-2 = Over 12,000"]
-[4.380877494812012, 4.600677490234375, "[FF] Local User Terminals (LUTs) of the COSPAS-SARSAT = Over 40"]
-[6.240852355957031, 6.014467716217041, "[TT] Design and Production Location of the TR modules = India"]
-[4.609086036682129, 2.888582229614258, "[TT] Offices of the EROS-B = Limassol, Cyprus, and in Tel Aviv, Israel"]
-[4.90981388092041, 1.482614278793335, "[TT] Image Acquisition Date of the Gokturk-2 = April 5th, 2016"]
-[5.498615741729736, 7.043853282928467, "[TT] Data Transmission Speed of the ITU = 320 Mbit/s"]
-[8.306573867797852, 7.5351996421813965, "[TT] CCD Detector of the NTSIC = 12 bit CCD detector with TDI (Time Delay Integration) capability for Pan and MS"]
-[10.528197288513184, 1.8318164348602295, "[FF] Description of the Pulsar = Pulsars are the collapsed remains of stars that exploded in supernova blasts. They can spin extremely fast and send out intense beams of radiation"]
-[14.246058464050293, 3.290276288986206, "[TT] Mass of the QC40 = 1.4 kg"]
-[1.6115771532058716, 3.757777690887451, "[TT] Multi-function component assembly of the BEESAT-3 = Yes"]
-[8.114571571350098, -0.8451917767524719, "[FF] Surface Elevation Measurement of the Airborne Topographic Mapper = Unknown"]
-[5.792170524597168, 3.0093183517456055, "[FF] Funding Amount of the Pixxel = $25 million"]
-[8.262465476989746, -0.006847002077847719, "[TT] Global Average Sea Level Rise of the TOPEX/Poseidon = 7 cm"]
-[7.129053592681885, 0.8977851867675781, "[FF] URL of the Next Generation Gravity Mission Elements of the Mass Change and Geoscience International Constellation = URL:\u00a0https://www.mdpi.com/2072-4292/13/19/3935"]
-[6.004275321960449, 4.145223617553711, "[FF] Owner of the Hylas-3 payload = Avanti Communications (UK)"]
-[9.227258682250977, 6.412910461425781, "[TT] Limb-Viewing Imagery Range of the SIS = -72.8\u00ba from nadir to -63.2\u00ba from nadir"]
-[6.753218173980713, 5.561172008514404, "[TT] P-PODs Quantity of the Secondary Payloads = 4"]
-[11.414443969726562, 6.623840808868408, "[TT] Energy Release of the eROSITA = 1056 ergs"]
-[8.114803314208984, 8.07530403137207, "[TT] Spectral Bands of the WV-3 Imager = 29"]
-[8.847395896911621, 3.3607709407806396, "[FF] Study Parameters of the Compact Ionosphere Probe (CIP) = Ion composition, density, velocity, and temperature"]
-[5.089155673980713, 3.299722194671631, "[TT] Manufacturer of the LRI = BATC (Ball Aerospace & Technologies Corporation)"]
-[8.902852058410645, 5.631028175354004, "[TT] Requirement Value of the Pointing accuracy = 1.2 km"]
-[9.93354320526123, 7.863386154174805, "[TT] Optics System of the Telescope = f/8 RC (Ritchey/Chretien)"]
-[4.58149528503418, 6.775166988372803, "[FF] Function of the S-band Transmitters and Receivers = Provide the communications link for engineering and payload data"]
-[9.138025283813477, 7.400039196014404, "[TT] Multispectral Bands Ground Resolution of the WorldView-3 = 1.24 m"]
-[5.3751091957092285, 6.1764302253723145, "[TT] Front End Modules of the NanoCom SDR = Up to 3"]
-[3.60360050201416, 4.495351314544678, "[TT] SAR Constellation Frequency of the Spacety = Day and night"]
-[8.187889099121094, 8.55659294128418, "[TT] Imaging Wavelength of the Solar Orbiter = 17 nm"]
-[3.32616925239563, 5.674047470092773, "[TT] Number of Antenna Partitions in Receive of the L-band SAR antenna = 2"]
-[6.11184549331665, 1.922851324081421, "[FF] URL of the GPM = http://www.esmats.eu/esmatspapers/pastpapers/pdfs/2011/sexton.pdf"]
-[12.041816711425781, -0.38546857237815857, "[TT] Mission Selection Year of the TESS = 2013"]
-[10.402237892150879, 2.348557472229004, "[FF] Principle of the TRD = Detects soft x-rays emitted when charged particles traverse the boundary between two media with different dielectric constants"]
-[6.585893154144287, -2.024831771850586, "[TT] Year of Launch of the Jason-1 = 2001"]
-[8.282327651977539, -0.06528119742870331, "[TT] Accelerating Rate of the Sea Level = 3 mm/year"]
-[3.17093563079834, 2.3133718967437744, "[FF] Application of the Sentinel-2 = Plant health monitoring"]
-[8.797843933105469, 3.419736862182617, "[FF] Purpose of the CIRCE = Understanding the dynamics of the ionosphere"]
-[6.736032009124756, 0.8296541571617126, "[TT] Dust Tail Crossing Date of the Solar Orbiter = June 6"]
-[10.703556060791016, 1.0641354322433472, "[TT] Host Star Size of the Kepler-186 = Half the size of the sun"]
-[8.122757911682129, 5.882885932922363, "[FF] Accuracy of the LASSO = 1.5 ns"]
-[5.915861129760742, 2.531229019165039, "[FF] Orbit Type of the Spacecraft = Pyramid"]
-[6.927659511566162, 7.14804744720459, "[TT] Laser Pulses Per Second of the ATM = Thousands"]
-[9.655709266662598, -0.3570118546485901, "[TT] Altitude Range of the NEOSSat = 15,000 and 40,000 km"]
-[5.662219524383545, -0.28077101707458496, "[TT] Deployment Wait Time of the Payloads = 15 seconds"]
-[8.783141136169434, 4.6105427742004395, "[FF] Function of the GT (Guide Telescope) = Directs pointing maneuvers to the desired solar targets"]
-[12.059277534484863, -0.40341052412986755, "[TT] Launch Time of the TESS = 22:51 UTC"]
-[7.655694484710693, 3.7078356742858887, "[FF] Purpose of the Bipods = Ensure system rigidity and required first eigenfrequency of the COB"]
-[7.564483165740967, 4.811709403991699, "[FF] Operating Modes of the iADCS100 = Tracking mode"]
-[7.103472709655762, 7.770205020904541, "[FF] Reflecting Performances Evaluation of the Cube Corner Reflectors (CCRs) = Through the analysis of the FFDP (Far Field Diffraction Pattern)"]
-[8.906542778015137, 6.486874103546143, "[TT] Footprint Diameter of the SLA altimeter = 100 m"]
-[8.256712913513184, 2.851207733154297, "[TT] Measurement Domain of the QBITO = Atmosphere"]
-[7.010051727294922, 1.292008638381958, "[FF] Publication Date of the Solar Mass Ejection Imager = Jan. 22, 2002"]
-[5.008533000946045, 3.318330764770508, "[TT] Manufacturer of the ArgoMoon = Argotec S.r.I."]
-[6.577744960784912, -0.46585193276405334, "[TT] Repeat Cycle of the SPOT 1-5 = 26 days"]
-[8.786346435546875, 9.424885749816895, "[TT] Spectral Bands of the TANSO-CAI-2 = 5"]
-[4.502146244049072, -0.8914074897766113, "[TT] Launch Date of the SpaceX Dragon = October 8, 2012"]
-[6.978465557098389, 5.522097110748291, "[FF] Effectiveness Demonstration of the LRI = Improving the low-low SST measurement performance"]
-[6.550454139709473, 3.5888702869415283, "[TT] Function of the Refabricator = Recycles waste plastic materials into high-quality 3D-printer filament"]
-[6.23206901550293, 6.413517951965332, "[TT] Transmission Time of the `Alert' DCPs = About 10 seconds"]
-[9.082782745361328, 1.3445934057235718, "[TT] Funding Cycle of the New Horizons = Every three years"]
-[4.099633693695068, 6.240165710449219, "[FF] Components of the APAA Antenna = 128 horn antennas, 128 high power amplifiers (HPAs), and a beam forming network (BFN) with 256 digital phase shifters (PSs)"]
-[8.284709930419922, 8.37317943572998, "[TT] Radiometric stability of the Spectrometer = <0.65% (SWIR, <0.5% (MWIR), <0.4% (TIR)"]
-[9.910730361938477, 5.440866470336914, "[FF] Thermal Gradients of the FG = Unknown"]
-[2.9141149520874023, 1.957451343536377, "[FF] Image Capture Date of the Copernicus Sentinel-2 = March 2021"]
-[3.8770999908447266, 1.9851046800613403, "[TT] Launch Vehicle of the ICEYE-X2 = SpaceX Falcon 9 rocket"]
-[11.419584274291992, 4.37032413482666, "[TT] Size of the SHFT = 3U"]
-[7.670482158660889, 2.9215707778930664, "[FF] Purpose of the VIIRS = Characterize clouds and provide imagery in theaters of combat"]
-[9.996511459350586, 2.8917832374572754, "[FF] Launch Date of the CubeSats = 26 May 2016"]
-[9.21087646484375, -0.06596600264310837, "[TT] Height of the Prometheus Volcano Plume = 60 km (40 miles)"]
-[5.688150405883789, 1.3665562868118286, "[FF] Last Accessed Date of the JAXA Missions = March 2015"]
-[5.3705549240112305, 6.469305038452148, "[TT] Data Generation of the WPIx = Up to 5 GB per orbit"]
-[9.310589790344238, 4.07459831237793, "[FF] Components of the SEP = Flux Gate Magnetometer (FGM), radiation dosimeter and surface charging sensors"]
-[3.6021904945373535, 1.5940227508544922, "[FF] Meeting Date of the GMES Sentinel-3 = Sept. 16, 2010"]
-[5.024631500244141, 4.806188583374023, "[FF] Goal of the Small Photon Entangling Quantum System (SPEQS) = Enable a QKD link between satellites, or between a satellite and an optical ground station"]
-[5.346776962280273, 0.05159830302000046, "[TT] Focus Assessment of the Ikonos-2 = Yearly"]
-[9.156076431274414, 7.016481399536133, "[TT] Ground Instantaneous Field of View (GIFOV) of the Climate Observatory = ~250 m spatial resolution"]
-[4.427926063537598, 0.4737510085105896, "[FF] Target Launch Date of the MMO = JFY 2016"]
-[5.122767925262451, 6.86192512512207, "[TT] Downlink Data Rate of the Satellite = 620 Mbit/s"]
-[6.142185688018799, 6.5669779777526855, "[TT] Transmission Duration of the DCP = About 1 minute"]
-[11.71860408782959, 4.650572299957275, "[TT] Dimensions of the DMSP Block 4 = 76 cm in diameter and 74 cm high"]
-[7.713610649108887, 0.5257896184921265, "[FF] Water Ice Deposits of the Lunar IceCube = Unknown"]
-[7.00028133392334, 0.820056140422821, "[FF] Detection Capability of the InSight = Marsquakes every day"]
-[8.655119895935059, 2.335482120513916, "[FF] Atmospheric Properties of the GOE = TEC of the ionosphere and tropospheric water vapor as a function of altitude"]
-[8.108264923095703, 1.5992088317871094, "[FF] Measurement of the SMAP = Land and ocean measurements"]
-[5.168795108795166, 0.30748677253723145, "[TT] Operational Period of the Trasser = Until 1990"]
-[7.824679374694824, 5.82778787612915, "[TT] Frequency of the Advanced Microwave Scanning Radiometer (AMSR) = Eight"]
-[5.552955150604248, 6.4086174964904785, "[TT] Capacity of the Image Storage = 8 GB + 32 GB of science data"]
-[4.7858567237854, 2.920738935470581, "[TT] Developer of the ART-XC = IKI RAN"]
-[5.525465965270996, 5.613357067108154, "[TT] MCU of the C&DH = Freescale MCU (HCSX12)"]
-[13.889777183532715, 3.7151224613189697, "[TT] Mass of the Optical Telescope Assembly = 109 kg"]
-[8.99307632446289, 0.43577343225479126, "[TT] Displacement Resolution of the Boulders = ~1 cm"]
-[8.601226806640625, 6.464247226715088, "[FF] Imaging Capability of the WorldView-1, WorldView-2 and GeoEye-1 = To be replaced"]
-[6.265867233276367, -0.1102636307477951, "[TT] Number of Profiles/Hour of the Aeolus = 100"]
-[10.891557693481445, 4.027368068695068, "[FF] Sail Assembly and Boom Mechanical Assembly of the Sail Subsystem = Two primary components"]
-[8.676527976989746, 8.727081298828125, "[TT] Grating Type of the Offner-type spectrometer = Mechanically ruled"]
-[7.128438472747803, 4.585966110229492, "[TT] Mounts of the Separation Panel = ISS deployment specific mounts"]
-[13.457836151123047, 6.802774906158447, "[TT] Spacecraft Power of the QuickBird-2 = 1.14 kW (EOL)"]
-[12.033804893493652, 6.309831619262695, "[FF] Proton-to-Helium Flux Ratio of the AMS = Decreases with rigidity"]
-[5.084516525268555, 1.9162406921386719, "[TT] Decommissioned Status of the Pirs = True"]
-[9.810541152954102, 4.725611209869385, "[TT] Spin Rate of the ELFIN = 20 rpm"]
-[11.443058013916016, 5.774119853973389, "[TT] Face sheets material of the Bus structure = Aluminum (AA2024-T3)"]
-[13.417084693908691, 6.453316688537598, "[TT] Power Generation Test of the HORYU-2 = 300 V"]
-[6.871453762054443, 1.5744894742965698, "[FF] Daily Image Coverage of the FormoSat-2 = Taiwan and the surrounding region"]
-[5.810624122619629, 1.3135960102081299, "[TT] I&T Start Date of the IXPE observatory = March 2020"]
-[4.076174259185791, 1.446456789970398, "[TT] SEVIRI HRV Image Date of the Meteosat-10 = 19 July 2016"]
-[8.321452140808105, 7.050655841827393, "[TT] Number of Cameras of the KMSS = 3"]
-[7.222801208496094, 6.233448505401611, "[FF] Signal Injection Window of the Time Delaying Transponder = Noise measurement slot"]
-[10.861393928527832, 7.500183582305908, "[TT] Swath of the AVHRR/3 = 2900 km"]
-[4.19633674621582, 3.883793354034424, "[TT] Pilot Component of the Galileo Signal = Included"]
-[4.806755065917969, 0.08093325793743134, "[TT] End of Life Date of the HySIS = 5 years"]
-[5.171989440917969, 0.5431387424468994, "[FF] Launch Date of the EyeSat = 18 December 2019"]
-[16.488006591796875, 3.57253098487854, "[FF] Groundbreaking Date of the OneWebSatellites = March 16, 2017"]
-[9.014444351196289, 7.701802730560303, "[TT] Pan MTF of the Imager = >10%"]
-[8.569961547851562, 5.433701992034912, "[TT] Precision of Post Event Processing of the GF-3 Satellite = Better than 20 cm (1\u03c3)"]
-[13.3871431350708, 7.598718643188477, "[TT] TX Power of the Myriad RF board = Max. 10 dBm"]
-[7.825107574462891, 1.402992606163025, "[FF] Mission Purpose of the WCOM = Improve observation capabilities and understanding of water cycle"]
-[8.969486236572266, 7.55787467956543, "[TT] Fiber Optic Cable Type of the Detector Box = Various lengths"]
-[8.112059593200684, 6.619263648986816, "[TT] Data Downlink of the SOLSE = About 10-12% of the scans"]
-[5.171005725860596, 2.3695027828216553, "[TT] Mission Type of the DeMi = Non-EO"]
-[3.937148332595825, 3.4796347618103027, "[FF] Potential Use of the OneWeb's Gen2 satellite = Galileo replacement with groundbreaking technology to meet the needs of Government, military, maritime and first responder customers"]
-[6.461388111114502, 1.8732072114944458, "[FF] URL of the FireBird = http://www.int-arch-photogramm-remote-sens-spatial-inf sci.net/XL-7-W3/461/2015/isprsarchives-XL-7-W3-461-2015.pdf"]
-[6.688179969787598, -0.5728079080581665, "[TT] LEOP Duration of the PROBA-3 = Less than 2 days"]
-[6.126011371612549, 0.8771025538444519, "[FF] Data Gathering Start Date of the GEDI = 1 February 2019"]
-[9.401190757751465, 0.429008811712265, "[TT] Apocenter Distance of the SMART-1 = 4644.004 km"]
-[12.172707557678223, -0.09828711301088333, "[TT] Lens Assembly Elements of the TESS Camera = 7"]
-[6.965169906616211, 0.09795325249433517, "[FF] Mission Duration of the Seasat = 105 days"]
-[10.408714294433594, 2.368915557861328, "[FF] X-ray Generation of the CuPID = Soft X rays imaged by the spacecraft"]
-[8.175788879394531, 7.29261589050293, "[TT] Type of the HISUI = Hyperspectral and multispectral pushbroom imager"]
-[6.99000883102417, 6.955960750579834, "[TT] Operation Duration of the CATS = More than 200 billion laser pulses"]
-[5.068765640258789, 2.2412898540496826, "[TT] Program of the TacSat-3 = ORS (Operational Responsive Space)"]
-[3.2664072513580322, 1.4368207454681396, "[TT] Nominal Lifetime of the Sentinel-6 = 5.5 years"]
-[7.119701862335205, 7.301080703735352, "[TT] Optical Pulse Dynamic Range of the LI = 6.7 - 670 mW/m 2 /sr"]
-[9.820544242858887, 7.029035568237305, "[TT] Co-registration of the Instrument = 10% of the footprint size"]
-[11.66969108581543, 6.843413829803467, "[TT] Energy Coverage of the ART-XC = Up to 30 keV"]
-[5.931743621826172, 5.87401819229126, "[FF] Function of the Consolidated Storage = Enable short-term and long-term storage within the GS"]
-[5.99265193939209, -0.31645283102989197, "[TT] Required Contacts of the PROBA Project = 2 or 3 per day for S-band (U/D)"]
-[6.255415439605713, 8.04850959777832, "[TT] Location of the Channelizer = On the ground"]
-[5.632584095001221, 2.564756393432617, "[FF] Access Capability of the JAXA Flight Controller = Laptops in JEM"]
-[9.873173713684082, 6.4684858322143555, "[TT] Power of the Earth Radiation Budget Experiment (ERBE) = 50 W (average) per scanner"]
-[11.49741268157959, 6.583109378814697, "[TT] Measurement Range of the Particle Detector = Tritium : 9.2 MeV/n ~ 21 MeV/n"]
-[8.635592460632324, 1.0793944597244263, "[TT] Operational Date of the Aquarius = August 25, 2011"]
-[9.753253936767578, -0.6032581329345703, "[TT] Altitude of the Orbit = 628 km"]
-[10.1036958694458, 5.418032169342041, "[FF] Function of the ACC = Provides better thermal stability and characterisation"]
-[11.990398406982422, 4.9806809425354, "[TT] Volume of the MC-U = 125 mm x 180 mm x 165 mm"]
-[11.940305709838867, 3.5412991046905518, "[TT] Mass Flow Rate for Neutralizer of the IES = 2 cm3/s"]
-[7.983625411987305, 0.5751828551292419, "[TT] Record Low Water Levels Date of the Po River = June 27, 2022"]
-[7.489801406860352, 1.856946349143982, "[FF] Publication Date of the System Concept for Wide-Field-Of View Observations of Ocean Phenomena from Space = 1987"]
-[6.469139099121094, 5.164478302001953, "[FF]  of the CubeComputer = "]
-[6.795295715332031, 6.048567295074463, "[TT] Operation Mode of the DOTs = Periodic on/off to save energy"]
-[8.066953659057617, 9.192001342773438, "[TT] Wavelength of the Responsivity Measurement = 1495 nm"]
-[8.187801361083984, 4.529342174530029, "[FF] Contribution of the LARES = Laser Relativity Satellite"]
-[4.236965179443359, 7.309815406799316, "[TT] Radio Frequency of the PhoneSat-2.5 = S-band"]
-[8.293868064880371, 8.766379356384277, "[TT] Dust Measurement Concentration of the UVS = As low as 10-4 per cc"]
-[4.887497425079346, 2.4019272327423096, "[FF] Planned of the T\u00dcRKSAT 6A = First Indigenous Satellite Build Is Planned By Turkey\u2014T\u00dcRKSAT 6A"]
-[6.70035457611084, 1.5060378313064575, "[FF] Launch Readiness of the Emirates Mars Mission = Ready for Launch"]
-[8.24974536895752, 4.524823188781738, "[FF] Data Improvement of the LARES 2 = Order of magnitude"]
-[8.933357238769531, 0.9471924901008606, "[TT] Field of Research of the Parker Solar Probe = Heliophysics"]
-[7.996426105499268, 7.221240043640137, "[FF] Operation Modes of the CCD Detector = TDI"]
-[7.96229362487793, -0.9087058901786804, "[TT] Data Processing Location of the ICESat-2 = NASA Goddard"]
-[3.768768072128296, 7.1737165451049805, "[TT] Gain of the Antenna = Maximum gain normal to the spin axis of the bus"]
-[10.186280250549316, 5.41620397567749, "[FF] Cooling of the FPA = Cryogenic module (three-stage radiative cooler)"]
-[10.261449813842773, 2.0465266704559326, "[FF] Purpose of the SVOM = Observe and characterize gamma-ray bursts"]
-[10.404624938964844, 2.1259841918945312, "[TT] X-ray Cameras of the eROSITA X-ray telescope = 7"]
-[8.394562721252441, 7.305393695831299, "[TT] Stability of the Detector = To the required precision"]
-[6.680706977844238, 5.224034786224365, "[FF] Function of the Power Distributor Unit (PDU) = Distributes the platform power bus to all units of the SAR electronics subsystem, as well as AIU and TGCUs of the antenna subsystem, and powers up these units"]
-[8.094655990600586, 5.701578617095947, "[FF] URL of the JWST Fine Guidance Sensor = http://www.stsci.edu/jwst/instruments/fgs"]
-[4.27863883972168, 4.820431232452393, "[TT] Minimum Beam Mode Detectable Ship Length (MDSL) of the ScanSAR narrow = 25-95 m"]
-[10.418108940124512, 5.854257106781006, "[TT] Operating temperature of the Antenna = -20\u00baC ~+40\u00baC"]
-[4.7045063972473145, 6.245121002197266, "[TT] Communication Subsystem Radio of the Hope Probe = APL\u2019s Frontier radio"]
-[6.9282546043396, -1.7476904392242432, "[TT] Dry troposphere of the Jason-2 = 0.3 cm"]
-[5.538832664489746, 3.923170566558838, "[TT] Number of Primary Operational Satellites of the DMSP Satellite Series = 2 (F-16, and F-17)"]
-[6.012901782989502, 5.905040740966797, "[TT] Data/Pilot of the E6-A = Classified"]
-[7.815253257751465, 5.921935081481934, "[TT] Timing Accuracy of the STOs and STAEs = \u00b11 \u00b5s"]
-[5.785495758056641, -0.7822675108909607, "[FF] Lifespan of the Dove Satellites = Five to six years"]
-[6.474550247192383, -0.7693256139755249, "[TT] LTAN of the Spacecraft = 11 hours"]
-[5.401334285736084, 5.736046314239502, "[TT] Data Interface of the Command and Data Handling Subsystem = RS-422"]
-[7.748867511749268, 2.0035808086395264, "[FF] Purpose of the OCI = Examine and monitor phytoplankton communities in the ocean"]
-[5.630098342895508, 1.5565658807754517, "[TT] Operational Status of the WorldView-1 = Operational as of July 2022"]
-[9.407774925231934, 2.7775845527648926, "[FF] Science Objective of the MinXSS = Better understand the solar irradiance energy distribution of solar flare SXR (Soft X-Ray) emission and its impact on Earth's ITM (Ionosphere, Thermosphere, and Mesosphere)"]
-[8.651601791381836, 7.349054336547852, "[TT] Imagers of the HySIS = Two pushbroom imagers"]
-[10.42982006072998, 5.755007743835449, "[TT] Working Temperature of the TOU = -80\u00baC"]
-[5.047555446624756, 4.3090691566467285, "[TT] Number of Ground Stations of the Ground Station Subsystem (GSSS) = 3"]
-[4.78386116027832, 0.5666226148605347, "[TT] Launch Date of the Resurs-P3 = March 2016"]
-[8.035734176635742, 6.3280463218688965, "[FF] Sensor Type of the TANSO-FTS = Fourier Transform Spectrometer"]
-[7.41145658493042, 4.128557205200195, "[FF] Flight Performance of the MOPITT = Unknown"]
-[7.816002368927002, 5.54996395111084, "[TT] Build Timeline of the Passive Microwave Imaging Radiometer = Approximately two years"]
-[6.463311195373535, 3.403862953186035, "[FF] Components of the Orion spacecraft = Avionic computers, harnesses, propulsion system, 12 engines, 11 parachutes, 16-foot-diameter heat shield, forward bay cover and numerous other systems and components"]
-[6.514463901519775, 7.181675910949707, "[TT] Count Rate of the Instrument = From 200/s (IP) to 104 /s (solar corona) per pixel"]
-[11.50775146484375, 5.1569719314575195, "[TT] NaF Tile Area of the RICH = 34 cm x 34 cm"]
-[4.351097106933594, 2.9148895740509033, "[TT] Location of the Svalbard = 78\u00ba North"]
-[5.874882698059082, -0.7899453043937683, "[TT] Design Life of the Resurs-O1 spacecraft = 2 years"]
-[4.864189624786377, 0.5109029412269592, "[TT] Launch Date of the FITSat-1 = 21 July 2012"]
-[5.709839344024658, 5.04413366317749, "[FF] Objectives of the SCPS = Demonstrate and test a full space implementation of the Space Communications Protocol Standards"]
-[9.113903045654297, 1.0816502571105957, "[TT] Orbital Energy Source of the Juice mission = Earth, Venus and Mars"]
-[9.716293334960938, -0.4552212357521057, "[TT] Altitude of the BeaverCube = 410 km"]
-[5.903433799743652, -0.540211021900177, "[TT] Mission Life of the YouthSat = 2 years"]
-[5.745744705200195, 4.923615455627441, "[TT] TT&C of the Bus = Nominal operations"]
-[4.3575897216796875, 2.744236469268799, "[FF] Location of the DSX = Kirtland AFB, New Mexico"]
-[7.910834312438965, -0.9655531048774719, "[TT] Data Products Availability of the ICESat-2 = Now available for free from the National Snow and Ice Data Center"]
-[4.633347511291504, 8.089566230773926, "[TT] Operating Frequency of the OSCAT = Ku-band of 13.515 GHz"]
-[5.604371547698975, 6.804399013519287, "[TT] Data Delivery of the GBOT = One set of data per day"]
-[8.019619941711426, 4.613564968109131, "[TT] Radiation Hardened of the OBC = 15 krad, SEL and SEU immune"]
-[8.438694953918457, 7.649816989898682, "[TT] CCD Array Detector of the OTD = 128 x 128 pixels"]
-[6.39701509475708, 1.6385842561721802, "[FF] Calibration Plan Presentation of the Microscope = Oct. 1-5, 2012"]
-[9.702727317810059, 7.437661647796631, "[TT] Ground Sample Distance (GSD) - Single Image Mode of the PAN Band = 5 m x 5 m"]
-[6.283848762512207, 2.5790059566497803, "[FF] Conference Presentation of the Space Test Program-1 = J. S. Wisecup, S. Stephens, \"Space Test Program-1 (STP-1) - Raising the Standard,\" Proceedings of the 57th IAC/IAF/IAA (International Astronautical Congress), Valencia, Spain, Oct. 2-6, 2006"]
-[14.630343437194824, 6.74963903427124, "[TT] Battery Capacity of the EPS = ~ 10 Whr"]
-[8.730999946594238, 1.814894437789917, "[TT] Wind Speed Increase of the Hurricane Eta = 80 miles (130 km) per hour in one day"]
-[10.941046714782715, 4.861606121063232, "[TT] Structure of the Tether = Mesh"]
-[5.071223258972168, 1.1696162223815918, "[TT] Phase B of the SMOS = 2002"]
-[13.343914985656738, 7.297120094299316, "[TT] Power of the GaN-based Power Transistors = 15W and 80W"]
-[4.430131435394287, 1.8524556159973145, "[TT] Launch Date of the RADARSAT-2 = Jun 12, 2012"]
-[5.845915794372559, 4.50478458404541, "[FF] Purpose of the HEO = Communications services and other uses at high northern latitudes"]
-[4.428870677947998, 1.2622257471084595, "[TT] Arrival Date at Guiana of the SEOSAT-Ingenio = September 25, 2020"]
-[5.2047247886657715, 1.8806391954421997, "[TT] Operation Status of the PREMOS = Continuously operating since the launch, except for mission interruption due to operational constraints"]
-[7.345773696899414, 4.967783451080322, "[FF] Additional Mode of the EPI-Lo = Requires a Start pulse along with the SSD pulse"]
-[13.728191375732422, 2.901768922805786, "[TT] Mass of the Spacecraft = 23.9 kg"]
-[3.431823968887329, -0.8556994199752808, "[TT] Orbit Type of the DMC-3 Constellation = Sun-synchronous orbit"]
-[11.235054969787598, 5.338871002197266, "[TT] Calorimeter Diameter of the Microcalorimeter = 5.6 cm"]
-[4.937951564788818, 7.434257984161377, "[TT] Uplink Data Rate of the RF Communications = 15 kbit/s"]
-[10.901751518249512, 7.510807514190674, "[TT] Swath Width of the JL-1-GF03D = 17 km"]
-[13.941261291503906, 3.119812488555908, "[TT] Mass of the Dove-2 = ~ 5.8 kg"]
-[8.62522029876709, 5.575126647949219, "[TT] Positioning Accuracy of the Argos DCS = Up to 150 m"]
-[8.600956916809082, 6.170327186584473, "[TT] Measurement Accuracy of the SSALT = 2.5 cm"]
-[11.822340965270996, 6.721086025238037, "[TT] Electron Energy Range of the REPT = 1.6 to 18.9 MeV"]
-[9.374759674072266, 3.514432430267334, "[FF] Shape of the Earth's Magnetosphere = Artist's Rendition"]
-[8.297884941101074, 2.065612316131592, "[TT] Instrument Type of the OSCAT-3 = Radar scatterometer"]
-[8.507584571838379, 7.40385103225708, "[TT] Sensor of the ZY 1-02C = PMS (Panchromatic/Multispectral) Camera"]
-[10.602428436279297, 3.8959126472473145, "[FF] Deployment Status of the Dragsail = Not fully deployed"]
-[5.643286228179932, 0.6526690721511841, "[TT] Last Spinup Maneuver Date of the Satellite = July 2, 2014"]
-[13.124757766723633, 7.2558979988098145, "[TT] Power Consumption of the CPD = 1 W"]
-[8.97631549835205, 7.56632661819458, "[TT] Spatial Resolution of the CCD Camera = 1 km x 1 km"]
-[11.36029052734375, 3.565953493118286, "[FF] Orientation of the ESP Thrusters = For the spin-up maneuver, pairs of thrusters will be co-aligned 180\u00ba apart; for de-spin, a 2nd pair of thrusters will provide the opposite force; for the normal thrust maneuver, the thrusters will be oriented perpendicular to the exterior of the satellite"]
-[4.3282952308654785, 7.2091755867004395, "[TT] Band of the RF Communications = Ku-band and S-band"]
-[10.343846321105957, 4.528406143188477, "[TT] Quantity of the RW (Reaction Wheel) = 4"]
-[4.9841532707214355, 7.39786958694458, "[TT] AVNIR (M) Data Rate of the RF communications = 60 Mbit/s"]
-[10.051468849182129, 3.07501220703125, "[FF] Development Authors of the CubeSats for Technology Maturation = Charles D. Norton, Steve A. Chien, Paula J. Pingree, David M. Rider, John Bellardo, James W. Cutler, Michael P. Pasciuto"]
-[10.726454734802246, 3.4581596851348877, "[TT] Size of the 3U CubeSat = 3U"]
-[13.404001235961914, 5.475420951843262, "[TT] Solar Panels of the Sunstorm CubeSat = Four"]
-[3.4078400135040283, 6.448802947998047, "[TT] Diameter of the 21m diameter parabolic antenna = 21m"]
-[9.125382423400879, 8.186312675476074, "[TT] UV Detection Capabilities of the Hubble Space Telescope = Yes"]
-[5.9436798095703125, 6.498910427093506, "[TT] Data Upload Frequency of the Base Station = Every half an hour"]
-[4.33007287979126, 2.492062568664551, "[TT] Launch Site of the HTV = Tanegashima Space Center"]
-[11.149871826171875, 5.876340866088867, "[FF] Hardening Process of the Bricks = Water evaporation"]
-[6.048853397369385, 7.1505632400512695, "[TT] Rates of the Gimbal = 1 rad/s (max)"]
-[9.886164665222168, 3.6261179447174072, "[TT] Pointing Direction of the X-ray telescope = Radially outward from the center of the Earth"]
-[11.225992202758789, 0.6175985932350159, "[FF] Target Stars of the CHEOPS = Small exoplanets previously detected by accurate Doppler surveys and known transiting Neptune-size planets detected by ground-based photometric surveys"]
-[6.1845622062683105, 2.9472546577453613, "[FF] Imaging Purpose of the WorldView Legion = Identify vehicle types, create detailed 3-dimensional maps of terrain and infrastructure, simulate future battlegrounds for soldiers, and observe enemy activity"]
-[7.383498191833496, 3.650259256362915, "[FF] Data Gathered of the Global Navigation Satellite System - Radio Occultation (GNSS-RO) = Temperature and humidity"]
-[6.61074161529541, 1.9765450954437256, "[FF] URL of the CATS = http://www.nasa.gov/mission_pages station/research/experiments/1037.html"]
-[5.08164119720459, 1.5544054508209229, "[TT] Launch Status of the Galaxy = Not Launched"]
-[10.300993919372559, 0.9264434576034546, "[TT] Distance from Earth of the Kepler-186 = About 500 light-years"]
-[9.411724090576172, -0.2973251938819885, "[TT] First Orbit Perigee Altitude of the EFT-1 Orion = 200 km"]
-[6.212688446044922, 7.604614734649658, "[TT] Maximum Signals Tracked of the BlackJack = 48"]
-[8.564553260803223, 6.384343147277832, "[TT] Scan Mechanism of the SSM/T-2 = Step-scan motion in the cross-track direction of \u00b1 40.5\u00ba"]
-[5.814774990081787, 2.9821770191192627, "[FF] Goal of the EIAST = Establish a complete Space Industry within the UAE"]
-[4.482960224151611, 1.7717159986495972, "[FF] Data Collection of the Radarsat-1 = 25 years"]
-[6.219100475311279, 8.590363502502441, "[TT] Receiver Type of the AIS = Dual polarization"]
-[4.716217994689941, 2.9477243423461914, "[FF] Data Fusion Center of the Satellite = ADFC (Altimeter Data Fusion Center) also located at NavOceano"]
-[4.74749755859375, -1.8153924942016602, "[TT] Departure Date from L2 of the Chang'e-2 = April 15, 2012"]
-[9.1842622756958, 6.803879737854004, "[TT] Analysis Resolution of the SLA-1 = ~ 1.5 m (vertically) within each 100 m diameter footprint"]
-[8.01297378540039, 9.179505348205566, "[TT] Wavelengths of the CATS = 1064, 532, 355 nm"]
-[4.230391025543213, 0.5484402179718018, "[TT] Launch Date of the Integral = 2002"]
-[10.89508056640625, 7.511940002441406, "[TT] Swath Width of the CO2Image = 50 km"]
-[7.563127040863037, 6.1836981773376465, "[TT] Timing Accuracy of the ATLAS = Within a billionth of a second"]
-[9.003678321838379, 5.638702869415283, "[TT] Pointing Accuracy of the SILEX = Better than 1 arc second"]
-[6.426027774810791, 1.9864810705184937, "[FF] URL of the IXV = http://www.esa.int/Our_Activities/Launchers/IXV/IXV_spacecraft"]
-[4.732798099517822, 3.120589256286621, "[FF] Senior Executive Vice President of the Thales Alenia Space = Massimo Comparini"]
-[7.573164939880371, 4.2991156578063965, "[FF] Sensor Complement of the S/C = OLS, SSH, SSJ/3, SSB, Contamination Monitor"]
-[4.713390827178955, 7.919434070587158, "[TT] Frequency of the Receiver = 435 MHz"]
-[9.232220649719238, 3.045666456222534, "[FF] Observation Capabilities of the Aditya-L1 = Sun's Photosphere (soft and hard X-ray), Chromosphere (UV) and corona (Visible and NIR)"]
-[6.638639450073242, 4.545711994171143, "[FF] Payload Handling of the Vega-C = Handles larger payloads"]
-[9.801082611083984, 7.8409104347229, "[TT] Aperture of the SV-24 imager = 0.24 m"]
-[6.513583660125732, -0.6053535342216492, "[FF] WDT Function of the Phoenix EPS = Count up to 12 hours then power cycle the entire spacecraft for 10 seconds"]
-[8.937264442443848, 8.573771476745605, "[TT] Wavelength Range of the Telescope = 600 -1000 nm"]
-[11.228554725646973, 5.869804382324219, "[TT] Material of the Main Tank = Ti"]
-[5.402866840362549, 6.903855323791504, "[TT] C&DH Data Rate of the LDCM = 260.92 Mbit/s"]
-[8.245828628540039, -0.04757630452513695, "[TT] Orbit Count of the TOPEX/Poseidon = Nearly 62,000 orbits of Earth"]
-[6.082863807678223, 4.825040340423584, "[FF] Issue of the Diagnostic Port = Beginning to separate the mechanical ground connectors from the PCB"]
-[4.5252685546875, 1.2827037572860718, "[TT] Launch Date of the AlSat-1 = Nov. 28, 2002"]
-[6.952539443969727, 7.741697311401367, "[TT] Reflector Area of the Mayak = 4 m2"]
-[12.619342803955078, 9.094409942626953, "[TT] ECT (Equatorial Crossing Time) of the WV-1 = 1030 hours on a descending node"]
-[13.962181091308594, 3.1415038108825684, "[TT] Mass of the ESTCube-1 & -2 = 1.050 kg"]
-[8.368593215942383, -0.8450012803077698, "[TT] Mass of the Carbon Dioxide Ice Patch = 57 kg"]
-[9.684885025024414, 8.347524642944336, "[TT] FOV Motion of the MAHRSI = 0.01\u00ba x 1.13\u00ba"]
-[5.198943614959717, 1.4766566753387451, "[FF] Inauguration Date of the DEIMOS-2 = October 8, 2013"]
-[3.6584129333496094, 4.736240386962891, "[FF] Modes of the RADARSAT-1/2 = Standard, Wide, Low incidence, High incidence, Fine, ScanSAR wide, ScanSAR narrow"]
-[6.169185638427734, 0.47724324464797974, "[TT] Data Availability of the ATMS = For at least 98% of all observations over an annual basis"]
-[13.656440734863281, 6.859674453735352, "[TT] Eclipse Power Conversion Efficiency of the SBVR = 97%"]
-[6.603894233703613, 3.010246515274048, "[TT] Daily Revisit Rate of the Some of the company\u2019s current satellites = 15 times a day"]
-[10.028407096862793, 2.876401662826538, "[TT] Launch Date of the VELOX-PII CubeSat = Nov. 21, 2013"]
-[6.202673435211182, -0.49397411942481995, "[TT] Original Design Orbit Duration of the ESEO = 6 months"]
-[5.180044651031494, 2.8385493755340576, "[TT] Nationality of the Max Valier = Italian"]
-[12.151412010192871, 4.601578712463379, "[TT] Dimensions of the Spacecraft Bus = 1.34 x 1.34 x 3.2m"]
-[3.835211992263794, -1.162276268005371, "[TT] Orbit of the Queqiao = Halo orbit around the second Lagrangian (L2) point of the Earth-moon system"]
-[10.244000434875488, 1.973301887512207, "[FF] Brightness of the McNaught = High"]
-[13.65592098236084, 5.813939571380615, "[TT] Maximum Power Output of the Polarization Separation Grid Panel = 10.5 W"]
-[11.96126651763916, 6.577869415283203, "[TT] Energy Range of the AMS = 60 to 500 GeV"]
-[5.841001510620117, -0.7971628904342651, "[TT] Design Life of the Spacecraft = 2 years"]
-[13.543217658996582, 5.700494289398193, "[TT] Power Source of the 3U CubeSat = Fixed solar panels along with a 30 Wh battery"]
-[5.698197364807129, 2.881683826446533, "[FF] Project Management of the Power subsystem = Osaka Prefecture University, Kagawa University, Keio University, Tokyo Metropolitan College, Osaka Prefecture College"]
-[8.832804679870605, 9.515780448913574, "[FF] Polarization Measurement of the TANSO-FTS = P and S polarization"]
-[4.455334186553955, 3.1574299335479736, "[TT] Location of the Ground Station = Malindi, Kenya"]
-[5.645506381988525, 2.8847498893737793, "[TT] Developer of the Polar Vigilance Mission = ISISPACE"]
-[5.329302787780762, 2.019771099090576, "[FF] Mission Status of the MITA = Cancelled"]
-[10.76323127746582, 0.8456714749336243, "[TT] Sun Size Comparison of the TRAPPIST-1 = Not much bigger than Jupiter"]
-[10.724041938781738, 3.4488070011138916, "[TT] Size of the GRIFEX = 3U CubeSat"]
-[7.814189434051514, 5.882017612457275, "[TT] Type of the SEM = Multiple direction/polarisation radiometers"]
-[10.388175010681152, 6.997961521148682, "[TT] Earth Footprint of the NEMO-AM = 35 km x 95 km"]
-[8.095654487609863, 4.989600658416748, "[TT] Time of the Calibration Cycle = Approximately 1.8 s"]
-[5.5795769691467285, 6.207763195037842, "[FF] Ring Memory (RM) of the Groza = Fixed size sufficient to record a few events"]
-[6.579277992248535, 5.313011646270752, "[FF] Function of the DCS = Data collection"]
-[6.038122177124023, 5.073845863342285, "[FF] Functions of the RF Transceiver = Activates the antenna deployment mechanism, Receives and decodes data from the ground, Encodes and transmits data to the ground, Transmits a beacon, Transmits and receives data to/from the OBC via the spacecraft\u2019s I2C bus, Includes the ability to reconfigure the OBC via a dedicated UART interface"]
-[8.250273704528809, -0.6057389974594116, "[TT] Detection Limit for Water Ice of the LEND = ~0.1 wt%"]
-[5.889989852905273, 4.758052349090576, "[TT] Power Cycle Sequences of the Development Flight Instrumentation (DFI) = Executed as planned"]
-[5.211088180541992, 2.046168804168701, "[TT] Mission Status of the ITASat-1 = Operational"]
-[10.041646957397461, 6.984055519104004, "[TT] Ground Resolution of the Sounder = 10 km"]
-[9.058758735656738, 1.3453617095947266, "[FF] Mission of the New Horizons = Explore the Kuiper Belt"]
-[6.06837797164917, 2.3180606365203857, "[TT] Recovery Process of the Orion = Powered down, put in a safe mode"]
-[14.065512657165527, 4.035567760467529, "[TT] Mass of the Instrument = 9.4 kg"]
-[5.828394412994385, 6.0744171142578125, "[TT] Number of Partitions of the FMM (Flash Memory Module) = 4"]
-[6.99398946762085, 2.022808313369751, "[FF] Image Credit of the Helix Orbit = DLR"]
-[8.433619499206543, 6.008865833282471, "[TT] Data Product Accuracy of the XRS = \u226420% over mission life"]
-[3.177536964416504, 4.964786529541016, "[TT] CRS Resolution of the RISAT-SAR = 50 m x 8 m (Az x Range)"]
-[9.222724914550781, 3.1657960414886475, "[FF] Article Publication Date of the Magnetospheric Multiscale Mission = 3 Jan. 2018"]
-[4.135974407196045, 5.737709999084473, "[FF] Datasheet Release Date of the ADS-B Receiver = 22 Sept. 2015"]
-[7.5322442054748535, -0.5825591683387756, "[TT] Manufacturer of the ICEYE-X2 = ICEYE Ltd."]
-[9.587228775024414, 8.207559585571289, "[TT] Field of View, vertical of the Instrument = -8 to -32 (20\u00ba)"]
-[10.704423904418945, -0.14799529314041138, "[TT] Formation Time of the TanDEM-X and TerraSAR-X = ~ 3 seconds"]
-[8.534274101257324, 4.488840103149414, "[FF] Function of the Astronode S = Allow remote monitoring and significant maintenance cost reduction"]
-[6.001240253448486, 2.698855400085449, "[TT] Manufacturer of the Orion Service Module = Airbus Defence and Space"]
-[9.038508415222168, -0.775819718837738, "[TT] Orbit of the Alpha = MEO (~5900 km)"]
-[10.518515586853027, 4.920143127441406, "[FF] Functions of the Langmuir Probe = Measure plasma density, Ne and Ni, as well as temperature, Te, the floating potential, Vf, and the space potential, Vs"]
-[8.519447326660156, 7.411858081817627, "[TT] f/No of the CMOS Camera = 2.8"]
-[7.793785095214844, 7.995838165283203, "[TT] Sensitivity of the THD = 1,500 V/W"]
-[7.728410243988037, 0.5104337334632874, "[FF] Testing of the Lunar IceCube = Thermal vacuum, instrument testing and calibration"]
-[5.836687088012695, 2.1138312816619873, "[FF] URL of the NRL Miniature SGLS Transponder = http://www.nrl.navy.mil/pao/pressRelease.php?Y=2000&R=54-00r"]
-[11.81696891784668, 6.773331642150879, "[TT] Energy Optimization of the HEG = High"]
-[8.2660551071167, 4.468396186828613, "[TT] Contribution of the LARES = ITRF, Earth's gravitational field, Earth Orientation Parameters"]
-[6.109370708465576, -0.4438822865486145, "[TT] Expected Operation Duration of the MASCOT = Approximately 16 hours"]
-[16.50935935974121, 3.596463680267334, "[FF] Launch Plan of the Arianespace = Launch the rest of OneWeb\u2019s constellation this year"]
-[9.42482852935791, 9.157649040222168, "[FF] Spectral Signatures of the IRIS = Oxygen and heavier silicon ions"]
-[5.99429988861084, -2.3394877910614014, "[TT] Orbit Inclination of the Kondor-E1 = 74.75\u00ba"]
-[9.070635795593262, 2.878181219100952, "[FF] Diagnostic Technique of the Solar Flare = Helioseismic holography"]
-[13.434260368347168, 2.904546022415161, "[TT] Mass of the GRACE-FO satellites = Around 580 kg"]
-[6.9719319343566895, 6.303745269775391, "[FF] Transmission Interval of the GLB = Once, twice, or three times every minute"]
-[6.3206634521484375, 0.1257077306509018, "[TT] Reentry Date of the Skylab-1 = July 11, 1979"]
-[9.894816398620605, -1.3038082122802734, "[TT] Orbit Inclination of the PARASOL = 98.21\u00b0"]
-[5.286341667175293, 0.7536370158195496, "[TT] Data Collection Date of the GOCI = May 12, 2016"]
-[7.807009696960449, 6.933670520782471, "[FF] Descoped of the Fabry-Perot interferometer = Yes"]
-[5.56643009185791, -0.593152642250061, "[TT] Operation Duration of the Yutu = 972 days"]
-[10.277432441711426, 4.051405429840088, "[TT] Nuisance Objective of the SSM-Boom = Source 3"]
-[4.491240501403809, 6.361454963684082, "[TT] Telemetry Receiver Status of the \u00d8rsted spacecraft = Problematic"]
-[9.11795711517334, 0.22765065729618073, "[TT] Length of the Ganges River = Over 2400 km"]
-[8.34668254852295, 7.197742462158203, "[TT] Sensor Type of the MuREM = Two large area PIN diodes"]
-[5.204225540161133, 0.39631861448287964, "[TT] Operation Period of the ADM/Aeolus = 2018 to 2022"]
-[9.345733642578125, 7.115469932556152, "[TT] Resolution of the Spatial resolution = 1 mrad"]
-[9.264430046081543, 3.1070563793182373, "[TT] Energy Dissipation Location of the Cluster = Swirling vortices, or O-lines"]
-[8.141199111938477, 0.5305683016777039, "[FF] Second-Largest Humanmade Reservoir in the United States of the Lake Powell = "]
-[4.960606575012207, 3.3978018760681152, "[TT] Manufacturer of the NESSI = Spectral Applied Research Inc."]
-[8.684988975524902, 3.5619237422943115, "[FF] Measurement of the LYRA = Sun's energy intensity"]
-[7.42324686050415, 2.9649438858032227, "[TT] Size Comparison of the MethaneSAT = 10 times bigger than GHGSat"]
-[8.202896118164062, 5.496232032775879, "[TT] Stand on Duty at of the FY-3D = 800 km"]
-[9.935113906860352, 7.037623882293701, "[TT] Resolution of the NSCAT = 50 km"]
-[8.698991775512695, 5.326645851135254, "[TT] Baseline Length of the Three-axis diagonal gradiometer = 0.5 m"]
-[3.6459028720855713, 6.531674385070801, "[TT] Mirror Type of the Long Wavelength Band = Off-axis parabolic cylinder"]
-[7.330117702484131, 3.4235141277313232, "[FF] Function of the Level 3 = Spatio-temporal synthesis"]
-[5.218740463256836, 0.7409391403198242, "[TT] Launch Date of the GF-3 Satellite = 9 August 2016"]
-[3.868588447570801, -2.1752665042877197, "[FF] Practicality of the Specialized Asset Trackers = Not always the most practical solution"]
-[13.7067232131958, 5.3673787117004395, "[TT] Solar Cell Material of the LFSA = Copper Indium Diselinide (CuInSe2)"]
-[7.3179240226745605, 8.689261436462402, "[TT] Band 2 of the RBV Instrument = 0.58 - 0.68 \u00b5m"]
-[8.841019630432129, 7.288660049438477, "[TT] Visual Magnitude Limit of the BRITE = +3.5"]
-[8.937954902648926, 4.736484050750732, "[FF] Function of the SSTs = Derive the satellite attitude"]
-[4.801422595977783, 0.5957298278808594, "[TT] Planned Launch of the Resurs-P5 = 2023"]
-[8.150201797485352, 7.669730186462402, "[TT] Detector of the HSC-III optics subsystem = CCD image sensor"]
-[6.261813163757324, 0.6765906810760498, "[TT] Launch Window of the Gaia = 17 December to 5 January 2014"]
-[8.706029891967773, 2.0294582843780518, "[TT] Accuracy of the Wind Direction = 20\u00ba"]
-[10.895459175109863, 7.523669719696045, "[TT] Swath Width of the AEISS = 15 km"]
-[5.680400848388672, 6.660444736480713, "[FF] Transmission Schedule of the WEFAX = 4-minute slots with a break of 27 seconds between two transmissions"]
-[8.107401847839355, 1.3026918172836304, "[FF] Soil moisture of the Geosphere = To be generated from PolSAR data"]
-[9.88891315460205, 4.90899133682251, "[TT] Rotation Speed of the AMSR-E = 40 rpm"]
-[10.13951301574707, -2.7606143951416016, "[TT] Error Correction of the NAND-Flash based system = Complete"]
-[6.30280876159668, -1.3932621479034424, "[TT] Launch Year of the GRACE-FO = 2018"]
-[6.467254161834717, 3.577080011367798, "[TT] Current Challenges of the Refabricator = Quality control and consistency of feedstock material"]
-[8.708539009094238, -0.16503146290779114, "[FF] Lunar Orbit Insertion Location of the Chang'e-2 = Sinus Iridum (Bay of Rainbows, 43\u00b0N 31\u00b0W)"]
-[7.708166599273682, 2.3383736610412598, "[TT] Data Coverage Area of the OCO-3 = 80 km2"]
-[8.196404457092285, -0.4264051020145416, "[TT] Total Extent Increase of the Antarctic Sea Ice = About 1 percent per decade since 1979"]
-[4.5412139892578125, 2.624685525894165, "[FF] Launch Location of the Italian mini-satellite = Russia"]
-[11.776000022888184, 6.7783050537109375, "[TT] Energy Range of the HXCP = 30-100 keV"]
-[3.464442014694214, -0.8736116886138916, "[TT] Orbit of the nSight-1 = 500 km Sun synchronous polar orbit"]
-[7.936492919921875, 2.1413023471832275, "[FF] Alkalinity of the Marine Chemistry = Unknown"]
-[10.091656684875488, -2.6757357120513916, "[TT] Instrument Input Data Rate of the Astrium MMFU NAND-Flash SDR-SDRAM = 490 Mbit/s + 80 kbit/s (housekeeping)"]
-[11.71301555633545, 3.3516712188720703, "[TT] Engine of the TSUBAME = Ion engine"]
-[7.233790874481201, 1.276655673980713, "[FF] Function of the Sample Fetch Rover = Collect and deliver samples"]
-[11.719555854797363, 3.381119728088379, "[TT] Specific Impulse of the Ion Thruster = 500 - 3000 s"]
-[7.338478088378906, 5.7591962814331055, "[TT] Number of UV Flashes Detected of the Tatiana-1 = More than 300"]
-[13.910356521606445, 2.898488998413086, "[TT] Mass of the GCOM-W1 = About 1991 kg at launch"]
-[8.243696212768555, 3.1175365447998047, "[FF] Data Collection Period of the Ozone Monitoring Instrument (OMI) = March 25 through April 25 for 2020"]
-[14.043105125427246, 4.007083415985107, "[TT] Mass of the Instrument = 202 kg with the NG reflector and 275 kg with the HC reflector"]
-[10.359410285949707, 5.6249518394470215, "[TT] Temperature of Spacecraft and Instruments at Closest Approach to the Sun of the Heat Shield = About 85 degrees Fahrenheit (29\u00baC)"]
-[3.1396634578704834, 2.24041748046875, "[FF] Plant Indices of the Sentinel-2 = Leaf area index, leaf chlorophyll content, leaf water content"]
-[6.7655839920043945, 5.871335983276367, "[TT] Quantity of the XTA = 2"]
-[5.927130222320557, 4.399648666381836, "[FF] Modules of the TSCT = Data enquiry, data purchase, data acceptance, and the personal center"]
-[6.9572882652282715, 1.6758280992507935, "[FF] Imagery Usage of the FormoSat-2 = Providing imagery of the stricken region to the Chinese Academy of Sciences"]
-[2.907747983932495, 1.9390605688095093, "[TT] Image Capture Date of the Copernicus Sentinel-2 = June 17, 2022"]
-[13.866077423095703, 7.015596866607666, "[TT] Voltage Ripple of the SBVR = < 600 mVpp"]
-[5.366824626922607, 1.4362837076187134, "[TT] Reentry Date of the OrbView-3 = March 13, 2011"]
-[8.08372688293457, 9.144697189331055, "[TT] Ellipse Axis C of the Long Wavelength Band = 242.6 mm"]
-[5.154516220092773, 3.263465166091919, "[TT] Manufacturer of the GF-2 = CAST (China Academy of Space Technology)"]
-[9.577162742614746, 9.200105667114258, "[FF] CME Observation Date of the IRIS = May 9, 2014"]
-[4.860929012298584, 0.6235944628715515, "[TT] Launch Date of the OCO-3 = May 2019"]
-[8.048145294189453, 1.821601152420044, "[FF] Application of the HISEA-1 = Ocean and coastal observations"]
-[3.901801347732544, 7.915663242340088, "[TT] TC Demodulation Scheme of the TT&C subsystem = PSK (Phase Shift Keying)/PCM (Pulse Code Modulation)"]
-[10.007675170898438, 3.0182411670684814, "[FF] Publication Date of the National Scientific Foundation (NSF) CubeSat-based science missions for Geospace and Atmospheric Research = October 2013"]
-[10.451380729675293, 2.9367408752441406, "[FF] Nanosatellite of the GPS = CanX-2"]
-[5.19376802444458, 8.420074462890625, "[TT] Bandwidth of the Channel 3 = 400 MHz"]
-[9.383524894714355, 8.59865951538086, "[TT] Slit Length of the Instrument = 150 arcmin"]
-[9.326497077941895, 6.6079888343811035, "[TT] Resolution of the Satellite = \u0394x = 62 km for \u0394\u03b8 = 0.1\u00ba"]
-[12.186728477478027, -0.26775485277175903, "[TT] Monitoring Duration of the TESS = Nearly a month"]
-[7.745447158813477, 0.4789702296257019, "[TT] Trajectory of the Lunar IceCube = Low-thrust trajectory to lunar orbit with very little propellant"]
-[6.7136311531066895, 4.80166482925415, "[FF] Function of the GAMS = Generate navigation messages and steering commands"]
-[11.837260246276855, 3.161311626434326, "[TT] Thruster of the Clementine = 489 N"]
-[8.802494049072266, 6.37589168548584, "[TT] Wave Height Measurement Accuracy of the ALT = \u00b1 10% or 0.5 m, whichever is greater"]
-[8.513723373413086, 6.04813289642334, "[TT] Measurement Accuracy of the GRACE = Within one micron (1 \u00b5m)"]
-[6.320057392120361, 1.9088789224624634, "[TT] Developer of the eROSITA = MPE Garching"]
-[9.386642456054688, 5.79021692276001, "[TT] Measurement Method of the Electrodes = Differential capacitive measurement"]
-[9.885374069213867, 4.476446151733398, "[FF] Control Systems of the ANUSat = Magnetic torquers"]
-[10.96899700164795, 0.886729896068573, "[TT] Orbit of the LISA = Heliocentric Earth-trailing orbit"]
-[9.198445320129395, 3.068204879760742, "[FF] Structure of the Solar Plumes = Bundle of denser, flowing plumelets"]
-[8.902788162231445, 7.33784818649292, "[FF] Image Sensor Resolution of the Corvus = Higher resolution images"]
-[5.029140949249268, 2.172940969467163, "[TT] Operator of the TacSat-2 = US military"]
-[9.520960807800293, 8.157456398010254, "[TT] Field of View of the Imager = 28.6\u00ba"]
-[5.144634246826172, 1.9615968465805054, "[TT] Operational Status of the Geotail = Operational"]
-[6.820734024047852, 3.4867773056030273, "[TT] Location of the Kaber = JEM airlock"]
-[9.61089038848877, 4.1677165031433105, "[TT] Belongs to of the Swift J1818.0-1607 = Special class of objects called magnetars"]
-[8.61616325378418, 0.31045910716056824, "[TT] Number of Sun-grazing comets discovered by amateurs of the SOHO = Over 1100"]
-[8.7047758102417, 7.035394668579102, "[TT] Resolution of the TDI imaging technology = 7 m"]
-[9.691902160644531, 8.041035652160645, "[TT] FOV of the COR1 = 1.25 - 4 R sun"]
-[5.04135274887085, 2.9587454795837402, "[FF] Program Partners of the MYriade = CNES, Alcatel, Astrium"]
-[9.4246244430542, 0.6219214797019958, "[TT] Final Impact Velocity of the Schiaparelli = Just under 11 km/h"]
-[9.508967399597168, 0.7534316182136536, "[TT] Distance from Earth of the Voyager 1 = About 5.9 billion km"]
-[14.27855396270752, 3.1160597801208496, "[TT] Mass of the EDRS-C = 3500 kg"]
-[3.4682276248931885, 5.034880638122559, "[FF] Function of the SAR payload = Determine the coordinates of the emergency signal"]
-[8.257640838623047, 1.277745246887207, "[TT] 24-hour Total Precipitation on October 24-25 of the Downtown Sacramento = 5.44 inches"]
-[9.025659561157227, 7.24871826171875, "[FF] Image Resolution of the RapidEye = 30 cm"]
-[7.000673294067383, 7.043939590454102, "[TT] Maximum Source Flux Count Rate of the Readout System = 104 cps"]
-[4.743321895599365, -0.28349289298057556, "[TT] Construction Timeline of the CATS = Only two years"]
-[5.435685634613037, 6.418123245239258, "[TT] Data Storage Capacity of the SGR-ReSI = 1 GByte"]
-[8.034927368164062, 9.225188255310059, "[TT] Wavelength of the Carbonate = 2.5 \u00b5m"]
-[8.689352989196777, 2.70833420753479, "[TT] Geometric Accuracy of the Atmospheric Correction Processor = ~10 m RMSE linear"]
-[7.4401092529296875, 1.026228427886963, "[FF] Date of the Mapping Shallow Seafloors = 29 September 2020"]
-[9.827116966247559, 8.154189109802246, "[TT] Focal Ratio of the Lens = f/1.4"]
-[6.018051624298096, -0.5902438759803772, "[TT] Mission Life of the QSat = 2 years"]
-[5.428954124450684, 0.585501492023468, "[FF] Release Date of the Papette Uplink Station = 14 January 2015"]
-[3.5254313945770264, 6.328890323638916, "[TT] Ground Station Antenna of the KySat-1 = 21 m SPA (Space Tracking Antenna)"]
-[3.463345527648926, -0.8911843299865723, "[TT] Orbit of the ROSE-L = 690 km polar orbit"]
-[5.50533390045166, 6.0294036865234375, "[TT] Type of the Flash Memory Controller = DMA"]
-[11.801064491271973, 3.3665854930877686, "[TT] Thruster Temperature of the BepiColombo = Minus 150 C"]
-[9.235017776489258, 3.2475626468658447, "[FF] Purpose of the PlasMag Fluxgate Magnetometer = Provide crucial continuity of observation of interplanetary solar wind parameter"]
-[4.956400394439697, 6.3719892501831055, "[TT] Receiver of the CTECS-A = NovAtel receivers"]
-[11.224310874938965, 5.91387939453125, "[TT] Material of the Optical telescope = CFRP (Carbon Fiber Reinforced Plastic)"]
-[7.617652893066406, 8.729094505310059, "[TT] Total No of Spectral Bands of the MSU-100 = 6"]
-[2.289907217025757, 2.766526222229004, "[TT] SSM of the EPI-Lo = Ed Stone"]
-[10.004755020141602, 4.375150203704834, "[FF] Functionality of the CANOE = Turns the torquers off while reading from the magnetometer"]
-[6.835418224334717, 5.097210884094238, "[FF] Function of the MCP = Multiplier"]
-[9.624845504760742, -0.45653730630874634, "[TT] Altitude of the FormoSat-3/COSMIC-1 = 800 km"]
-[7.526710510253906, 7.951621055603027, "[TT] B/H of the Instrument = 0.57"]
-[5.08026123046875, 3.326343536376953, "[TT] Manufacturer of the GFO = BATC (Ball Aerospace & Technology Corporation)"]
-[6.852521896362305, 6.958134651184082, "[TT] Expansion Time of the BEAM = Seconds"]
-[5.789673805236816, 5.115838050842285, "[FF] Error Detection and Correction Scheme of the SSR = EDAC (Error Detection and Correction)"]
-[6.361084938049316, 4.871788501739502, "[FF] FDC Algorithms of the ACS = Included in ACS flight software (FSW)"]
-[10.997952461242676, 2.9011712074279785, "[TT] Body Dimensions of the Nanosatellite = 20 x 20 x 20 cm"]
-[7.53355073928833, 2.4074313640594482, "[FF] Image Capture of the OLI-2 = During the wildfires"]
-[14.637267112731934, 6.690980911254883, "[TT] Li-ion Battery Capacity of the EPS = ~20 Ah"]
-[5.223342418670654, 2.7440006732940674, "[TT] Location of the NASA's Jet Propulsion Laboratory = Pasadena, California"]
-[7.57621955871582, 5.717219829559326, "[FF] Data Density of the Scanning LIDAR = Provided data at a reasonable density for the last 30 m"]
-[9.437447547912598, 6.1324782371521, "[TT] Rotation of the Scan Assembly = 360\u00ba"]
-[11.926657676696777, 6.201512336730957, "[FF] Antimatter Detection of the AMS-02 = Unknown"]
-[6.552240371704102, 4.839671611785889, "[FF] Resource Requirement of the ACE (Adaptive Controls Experiment) = Downlink of data generated from ACE"]
-[5.628394603729248, 5.028679370880127, "[FF] Signal of the FFRF Subsystem = GPS C/A navigation signal modulated on two S-band carrier frequencies (S1 and S2) with BPSK/QPSK modulation"]
-[10.624942779541016, 8.890003204345703, "[TT] Pixel size of the Channel 4 = 32 km x 32 km"]
-[9.373088836669922, 4.815864086151123, "[FF] Attitude Controller Design Presentation Date of the IKAROS = July 20-22, 2010"]
-[10.939208984375, 7.522817611694336, "[TT] Swath Width of the MESSR = 200 km"]
-[4.73464298248291, -1.8165640830993652, "[FF] Tracking Support of the ESA = Essential to Chinese mission"]
-[12.02191162109375, 4.545193672180176, "[TT] Volume of the Spacecraft = 20 cm x 20 cm x 20 cm"]
-[9.577865600585938, 8.141563415527344, "[TT] Lens Assembly of the OTA = Custom 5-element refractive design"]
-[12.10319709777832, 3.335604667663574, "[TT] Fuel Tank Distribution of the Advanced Composition Explorer = One pair having approximately 20% more propellant than the other pair"]
-[4.733279228210449, 5.798677444458008, "[TT] Measurement Types of the LAGRANGE receiver = Pseudorange and Doppler phase"]
-[6.13279390335083, 4.2556071281433105, "[FF] Interaction of the Mission Planning = Uptakes CTDA requests into its planning cycle"]
-[7.22272253036499, 7.03488826751709, "[TT] Survival Temperature Range of the GEDI Laser = 50\u00baC to -10\u00baC"]
-[6.914880752563477, 1.4886281490325928, "[FF] Alignment Milestone Date of the Webb = 16 March 2022"]
-[4.517683029174805, -0.9005909562110901, "[FF] Berthing Date of the Dragon spacecraft = 2 July 2018"]
-[6.142358303070068, 4.806868076324463, "[FF] Type of the Telemetry/Command interface module = Telemetry/Command interface module"]
-[9.314295768737793, 5.206081867218018, "[TT] Platform of the CASPR = Gimbal-actuated platform"]
-[6.996245861053467, 4.5671563148498535, "[FF] Function of the CEASE = Provide essential knowledge about surrounding space"]
-[6.210716247558594, 5.016438961029053, "[FF] Function of the CPOD Service = Generating precise orbital products and auxiliary data files"]
-[7.105495452880859, 4.655246734619141, "[FF] Attachment of the Payload Panel = Cylindrical tube"]
-[8.107564926147461, 6.693012714385986, "[TT] Frame Capacity of the Satellite = Up to 45 frames"]
-[8.454401969909668, 1.0757800340652466, "[TT] Year of Launch of the Aqua = 2002"]
-[9.651360511779785, 8.338702201843262, "[TT] FOV of the CuPID = 4.6\u00b0 x 4.6\u00b0"]
-[14.322477340698242, 3.2096710205078125, "[TT] Mass of the MinXSS-2 = 4 kg"]
-[4.921608924865723, 0.9644829034805298, "[TT] Communication Reestablishment Date of the STEREO-B = Aug. 21, 2016"]
-[7.419618129730225, 1.654600739479065, "[TT] Quantity of the Argo buoys = ~300/day"]
-[7.947566986083984, 6.288549900054932, "[TT] Type of the Imaging multi-spectral radiometers (vis/IR) = Imaging multi-spectral radiometers (vis/IR)"]
-[13.640753746032715, 5.670321464538574, "[TT] Design Life of the Solar Panels = Up to 15 years"]
-[3.1841139793395996, 3.8093628883361816, "[TT] Nominal Lifetime of the TerraSAR-X = 5.5 years"]
-[14.070585250854492, 7.1660871505737305, "[TT] Input Voltage of the Instrument Power Unit = 28 V DC"]
-[10.204026222229004, 3.225909948348999, "[FF] Flight Software of the SOURCE 3U CubeSat = Being developed and tested in parallel"]
-[8.492664337158203, 6.83463716506958, "[TT] Area Collection Rate of the Pushbroom Scanner = Very high"]
-[8.904926300048828, 9.378645896911621, "[TT] Type of the TANSO-CAI = Atmospheric chemistry"]
-[13.341684341430664, 7.821194648742676, "[TT] S-band TxRx Power of the RF communications = 5W"]
-[11.345955848693848, 4.29963493347168, "[TT] Size of the AISTechSat-2 = 6U"]
-[11.40680980682373, 4.317162036895752, "[TT] Size of the Al Farabi-2 = 3U"]
-[3.0754761695861816, 2.2396929264068604, "[TT] Fire Front Length of the Copernicus Sentinel-2 = More than four km"]
-[9.635483741760254, 1.375343918800354, "[FF] Launch Date of the Pl\u00e9iades Neo = 17 August 2021"]
-[5.739909648895264, 2.768556594848633, "[FF] Sponsor of the CADRE = National Science Foundation (NSF)"]
-[6.876801013946533, 4.964337348937988, "[FF] Type of the LCT = Unknown"]
-[13.828746795654297, 6.982795238494873, "[TT] Power Delivery of the Spacecraft Plug-n-Play Avionics (SPA) = Separate 28V power delivery"]
-[11.613912582397461, 6.625280380249023, "[TT] Telescope Energy Range of the ASTRO-H = E ~ 0.3-12 keV"]
-[5.045797824859619, 1.0105550289154053, "[FF] Copyright Year of the eoPortal = 2024"]
-[8.32043170928955, 7.146706581115723, "[TT] Coverage Rate of the ABI = Six times the current GOES Imagers"]
-[14.194548606872559, 3.2242467403411865, "[TT] Mass of the DORIS = 15 kg"]
-[8.549748420715332, 5.405862331390381, "[TT] Accuracy for Stationary Users of the Transit Navigation = Order of 5 m"]
-[3.3333470821380615, 6.035487651824951, "[TT] Size of the Radar Antenna = 11 metres by 3.6 metres"]
-[5.002708911895752, 3.2877023220062256, "[TT] Manufacturer of the ILAS-II = Japanese Environment Ministry"]
-[7.567415714263916, -0.6491387486457825, "[FF] Launch Date of the ICEYE = June 13, 2023"]
-[4.597437381744385, 5.746826171875, "[FF] Divergence of the Ground Terminal Beacons = Designed to the ephemeris specification"]
-[5.915383338928223, 0.9606554508209229, "[TT] Image Acquisition Date of the Dyess = 20 Jan. 2014"]
-[13.346877098083496, 5.436629772186279, "[FF] Solar Generator Configuration of the MicroSCOPE = Two identical wings of one panel each, mounted on Y panels and directed toward +X"]
-[8.129548072814941, -0.9864524602890015, "[FF] Function of the Gravimeter = Map the bedrock below the ice shelf and the water"]
-[14.579024314880371, 6.604857921600342, "[TT] Battery Type of the Spacecraft = Li-ion 12 Ah"]
-[5.199837684631348, 3.2456514835357666, "[TT] Manufacturer of the NOAA-20 = Ball Aerospace"]
-[13.620100021362305, 5.8562541007995605, "[TT] Power Supply of the SI-300 = Li-ion battery and four deployable solar panels"]
-[10.35092830657959, 5.249504089355469, "[FF] Location of the Heat pipes = Embedded in the North and East panels"]
-[11.401899337768555, 4.3320417404174805, "[FF] Size of the SNaP = 3U"]
-[5.950249195098877, 0.27443644404411316, "[TT] Trajectory Change Start Date of the Rosetta = August"]
-[8.12897777557373, 2.6540651321411133, "[TT] Measurement Domain of the VHRR = Atmosphere, Ocean, Land"]
-[8.052785873413086, 6.1881232261657715, "[TT] Precision of the Time-to-Digital Converters = < 0.5 ns"]
-[2.8424994945526123, 0.09317392855882645, "[TT] J2000 right ascension (deg) of the B1813-140 = 274.006"]
-[8.797443389892578, 2.161796808242798, "[FF] Current Distance of the IC 4665 and Collinder 350 = More than twice as large as the diameters of the biggest molecular clouds"]
-[9.409010887145996, 7.526346683502197, "[TT] Field of View of the DMAC = 720 km"]
-[13.539447784423828, 2.86626935005188, "[TT] Mass of the DMSP satellites = ~1220 kg"]
-[11.327739715576172, 2.7964372634887695, "[TT] Scientific Payload Mass of the Microsatellite = 10.8 kg"]
-[6.4264235496521, 1.783859133720398, "[FF] URL of Presentation of the RISESAT = http://digitalcommons.usu.edu/cgi/viewcontent.cgi?"]
-[8.485267639160156, 6.144222259521484, "[TT] Accuracy of the CCRs = One-millimetre"]
-[5.527981758117676, 6.613430023193359, "[TT] Minimum Detectable Size of the SDS = 50 \u00b5m"]
-[12.063213348388672, 2.9891891479492188, "[TT] Onboard Propulsion of the QuickBird-2 = 4 x 4.4 N hydrazine thrusters"]
-[8.009501457214355, 3.9609780311584473, "[FF] On-Orbit Spectral Characterization Duration of the Terra MODIS = Five Years"]
-[8.231830596923828, 2.9875967502593994, "[FF] Objective of the ISUAL = Observe the natural upward lightning discharge phenomena toward the ionosphere on top of the troposphere"]
-[3.2327232360839844, 3.8223624229431152, "[TT] Fuel Supply of the TSX (TerraSAR-X) = Until at least 2026"]
-[10.117401123046875, 1.3195974826812744, "[TT] Radiation Diminishment of the The Teacup = 50 to 600 times over the last 40,000 to 100,000 years"]
-[10.237500190734863, 3.2567832469940186, "[TT] Spectrometer Channels of the MicroMAS-2 CubeSat = 12"]
-[9.694392204284668, 0.1413152664899826, "[TT] Parachute Quantity of the ExoMars mission = Two main parachutes"]
-[4.984752178192139, 0.501482367515564, "[TT] Deployment Date of the DarkCarb MWIR Payload = 2022"]
-[9.094433784484863, -1.2383737564086914, "[TT] Orbit of the ETS-VIII = Geostationary orbit at 146\u00ba E longitude"]
-[5.967395305633545, 2.402006149291992, "[FF] Second Launch Timing of the WorldView Legion satellites = Approximately three to six months after the first launch"]
-[7.4736528396606445, 2.303715467453003, "[TT] Data Source of the IBTrACS = International Best Track Archive for Climate Stewardship"]
-[10.796003341674805, -0.3753218352794647, "[TT] Launch Year of the Tandem-L = 2022"]
-[4.647641658782959, 0.9005881547927856, "[TT] Communication Experiment Date of the ADEOS-II = March 28 to 30, 2003"]
-[8.485676765441895, 7.694620132446289, "[TT] Line Array of the MS CCD detector module = 6,000 pixels"]
-[7.7167487144470215, 5.518579006195068, "[FF] Function of the S-193 = Combination of passive microwave radiometer with an active scatterometer, and radar altimeter"]
-[11.097155570983887, 5.040709495544434, "[TT] Length of the Primary Sensor = 2 m"]
-[8.171175003051758, 5.404651165008545, "[FF] Unknown of the DORIS = Unknown"]
-[4.65131139755249, 6.925942420959473, "[FF] Function of the PDD = Payload data acquisition and high rate downlink in Ka-band"]
-[3.5933432579040527, 6.995353698730469, "[TT] Polarizations of the Antenna = Ch 0, 1, 2: RHCP, Ch 3, 4, 5: LHCP"]
-[5.664592742919922, 2.305312395095825, "[TT] Project Team Size of the CIMON = Approximately 50"]
-[4.783931255340576, 0.5141788125038147, "[TT] Launch Date of the COMS = 26 June 2010"]
-[8.154565811157227, 7.706192970275879, "[TT] Noise Performance of the CCD Camera = SNR <= 128 at 100% albedo"]
-[7.4078288078308105, 5.536279201507568, "[FF] Modules of the CEU = CEUP (CEU Power supply), CC (Camera Controller), and FPA"]
-[6.691537857055664, 1.1160842180252075, "[FF] Image Capture Date of the Solar Dynamics Observatory = March 31, 2022"]
-[7.985255718231201, 9.03395938873291, "[TT] Observation Wavelength of the DCAM3 = Visible"]
-[13.704469680786133, 7.0019402503967285, "[TT] Stored Energy of the NanoPower P31us = 38 Wh"]
-[7.5746750831604, 6.63001823425293, "[TT] Data Delivery Time of the HRFI Imagery = 150 seconds"]
-[5.826235771179199, 5.4069976806640625, "[TT] Interface of the Instrument Control Unit (NI-ICU) = 1553 bus"]
-[4.94034481048584, 5.100295543670654, "[TT] CCSDS ID of the GSAT-0102 = 3A6"]
-[3.120738983154297, 1.7277196645736694, "[TT] Revisit Time of the Copernicus Sentinel-3 = Every two days"]
-[5.672883987426758, 4.807021141052246, "[FF] Purpose of the EDRS = Relay data between satellites in low orbit and Earth via satellites in geostationary orbit"]
-[7.268701076507568, 8.16380500793457, "[TT] Sensitivity of the Channel 4 = 0.3 K/pixel"]
-[5.634405136108398, 0.9611806273460388, "[FF] Inter-Calibration Date of the COCTS = 25 July 2018"]
-[7.463776588439941, 2.041383743286133, "[FF] Mission of the Biomass = Deliver crucial information on how the world's forests are changing"]
-[5.142301559448242, 0.7844913601875305, "[FF] Year of the \u00a9 2024 = 2024"]
-[8.845378875732422, 7.486855506896973, "[TT] Be Window Thickness of the Detector = 100 \u00b5m"]
-[7.145256042480469, -0.06619826704263687, "[FF] Data Collection Focus of the CIP = Eclipse time and the transition time from sunlight to eclipse time"]
-[5.9612932205200195, 7.094287395477295, "[FF] Data Rates of the STAFF/DWP = 1.024 kbit/s, or 4.627 kbit/s"]
-[5.479568004608154, 5.198521614074707, "[TT] Firing Tests of the AQT-D = Standalone and Integrated"]
-[11.974651336669922, 4.685068607330322, "[TT] Mainframe Launch Size of the SRMSat = 286 mm x 286 x 294 mm"]
-[5.88350772857666, -0.05254204198718071, "[FF] Life Extension of the ESA's science missions = Extended"]
-[5.821364879608154, 1.2056896686553955, "[FF] Conference Date of the EarthCARE = Oct. 4-8, 2010"]
-[9.90103816986084, 5.580904960632324, "[FF] Components of the PLM Structural & Thermal Model (PLM STM) = Optical Bench Assembly STM with thermal mass dummies of the cameras"]
-[9.564194679260254, 7.170517921447754, "[TT] Spatial resolution at nadir of the MWHS = 15 km"]
-[8.625612258911133, 3.6735424995422363, "[FF] Citation of the SOLSPEC = G. Thuillier, M. Herse, D. Labs, T. Foujols, W. Peetermans, \u201cThe Solar Spectral Irradiance from 200 to 2400 nm as measured by the SOLSPEC spectrometer from the ATLAS and EURECA missions,\u201d Solar Physics, Vol. 214, pp. 1-22, 2003"]
-[10.977242469787598, 5.156002044677734, "[TT] Periherm of the MMO = 400 km"]
-[3.4535300731658936, 1.8509210348129272, "[FF] Registration Process of the Sentinel-1 = Online self-registration accessible via the Sentinel Data Hub"]
-[8.040977478027344, 0.7186028361320496, "[TT] Flooding Frequency of the Lake Eyre = Few times per century"]
-[2.976486921310425, -0.3650478720664978, "[TT] Operational Orbit Altitude of the OneWeb satellites = 1,200 km"]
-[5.870048999786377, 5.948995590209961, "[FF] Speed Requirement of the MOBC = Modest"]
-[4.894519329071045, 0.4435117542743683, "[TT] Launch Date of the Galaxy = Late 2008"]
-[4.851150035858154, 0.6835972666740417, "[TT] Launch Date of the GPM Core spacecraft = 2014"]
-[4.568258285522461, 8.006335258483887, "[TT] Frequency (Ka-band) of the Antenna = 18 GHz (17.7-18.8)"]
-[8.132678985595703, 5.911940097808838, "[FF] Dark Current of the Sensor = Negligible"]
-[6.3166632652282715, 0.07793953269720078, "[TT] Operation Period of the Skylab-1 = Up to 84 days"]
-[4.168496131896973, 2.1160457134246826, "[FF] Mission Type of the NigeriaSat-2 = Imaging"]
-[8.241421699523926, 3.9124395847320557, "[FF] Measurement Method of the ASME = The electrical resistance is measured over time for a deduction in sample volume changes"]
-[12.11832332611084, -0.3191221356391907, "[FF] Short-term Oscillations Period of the TESS spacecraft = Six months"]
-[9.379558563232422, 4.703763008117676, "[FF] Issue of the Attitude Control System = Eclipse attitude control not achieved"]
-[5.039938926696777, 0.6799162030220032, "[FF] Launch Date of the Ven\u00b5s = Aug. 2, 2017"]
-[4.7792439460754395, 0.3112928569316864, "[TT] Launch Date of the CAS500 = 22 March, 2021"]
-[5.2430853843688965, 0.0914575606584549, "[TT] Launch Date of the AeroCube-4 = Sept. 13, 2012"]
-[11.698805809020996, 4.689281940460205, "[TT] Upper Plate Shape of the Baumanets-2 = Hexagonal"]
-[8.084196090698242, 2.628861904144287, "[FF] Purpose of the RAIDS = Acquire a global database of airglow intensities"]
-[11.813948631286621, 3.276890277862549, "[TT] Thruster of the PLATiNO-2 = HT 100"]
-[13.482856750488281, 5.4607014656066895, "[FF] Components of the IRAS project = Efficient type of solar cell by AzurSpace, a smart heater which self regulates the heat output and a multifunctional sandwich structure with built in radiometry sensors, inertial measurement units (IMUs) and strain gauges"]
-[6.540507793426514, 6.859482288360596, "[FF] Performance of the Tesat laser communication terminal = 5.6 Gbit/s"]
-[5.583817005157471, -1.9952410459518433, "[FF] Observation Applications of the KOMPSAT-3 = GIS, environmental monitoring, agricultural monitoring, oceanographic monitoring"]
-[4.507734775543213, 1.5134292840957642, "[TT] Launch Date of the TechEdSat = July 31, 2012"]
-[6.002048969268799, 5.925637245178223, "[TT] Number of Docking Ports of the Prichal Module = 5"]
-[8.473794937133789, 5.042790412902832, "[FF] Sensitivity of the Electrostatic Accelerometers = Ultra-sensitive"]
-[9.197540283203125, -1.1945698261260986, "[TT] Motion of the LEO satellite = Moves relative to the Earth"]
-[9.06607723236084, 3.66524600982666, "[TT] Arc Detection Monitoring Frequency of the High-voltage solar array = Every second"]
-[9.289172172546387, 10.721573829650879, "[TT] Polarization of the ICI-4 = V, H"]
-[5.55465841293335, -0.06917845457792282, "[FF] Period of Performance of the TSIS-2 = Ending with on-orbit acceptance by the government"]
-[3.608928918838501, 6.988073825836182, "[TT] Polarization of the X-band Transmitter = RHCP"]
-[7.799692153930664, 2.068192720413208, "[TT] Latitude Coverage of the ERS-1 = \u00b1 81.5\u00ba"]
-[8.410758018493652, 7.458284378051758, "[TT] Detector Types of the Imager = CMOS detector, smaller CMOS sensor"]
-[13.802395820617676, 2.678677797317505, "[TT] Launch Mass of the Spacecraft = 720 kg"]
-[3.4374632835388184, 6.312145709991455, "[TT] Length of the LMAG (Lunar Magnetometer) mast = 12 m"]
-[4.246120929718018, 7.847590923309326, "[TT] Clock 1 Function of the QZS-1 = Generating positioning signals"]
-[10.24647331237793, 1.6084827184677124, "[TT] Number of Active Stars of the eROSITA = Half a million"]
-[7.938065528869629, 6.259608268737793, "[TT] End of Life Date of the Imaging multi-spectral radiometers (vis/IR) = 2025"]
-[10.164976119995117, 1.6962532997131348, "[TT] Number of Extended Sources of the eROSITA = Tens of thousands"]
-[7.283007621765137, 5.643624305725098, "[FF] Detection Filter of the Tool = Constant False Alarm Rate (CFAR) filter using a K distribution"]
-[4.382754802703857, 1.891758918762207, "[TT] Image Acquisition Date of the RADARSAT-2 = October 8, 2019"]
-[5.909829139709473, 4.402474403381348, "[FF] Function of the Single-function satlets = Incorporate one individual satellite subsystem function per satlet"]
-[6.2670087814331055, 2.5583364963531494, "[FF] Function of the Orion = Provide emergency abort during the launch ascent phase, sustain the crew during space travel, and provide safe reentry from deep space return velocities"]
-[5.164820671081543, 4.588765621185303, "[TT] Antennas of the Starlink Satellite = Multiple high-throughput"]
-[9.853550910949707, 0.6500996351242065, "[TT] Link Distances of the 1st generation Tesat LCT = About 5000 km"]
-[8.548630714416504, 7.7011823654174805, "[FF] Film Transmission of the MXT = t70"]
-[5.8766655921936035, -0.7584988474845886, "[TT] Mission Design Life of the Spacecraft = 1.5 years"]
-[14.082648277282715, 7.199162006378174, "[TT] Power Bus Voltage of the PCDU = 28 V"]
-[9.1130952835083, 4.531309604644775, "[FF] Design Concept of the AOCS = Gyro stellar hybridation with reaction wheel actuators unloaded through magnetotorquer bars, safe hold mode only relies on kinetic momentum, coarse sun sensors and magnetic sensors and actuators, four 1N thrusters in blow down mode limited to orbit control manoeuvres"]
-[6.2073140144348145, 8.044178009033203, "[TT] Number of Channels of the RF D/L channels = 2"]
-[11.28222370147705, 0.9637700915336609, "[TT] Start of Science Mission of the LISA Pathfinder = 1 March 2016"]
-[11.626712799072266, 4.757087707519531, "[TT] Size of the OPS-SAT = 30 cm tall"]
-[10.984420776367188, 5.321140766143799, "[FF] Mission of the IST = Verify the long-term (~six months) retainment of pressurized membrane structure"]
-[6.404232978820801, -0.25508803129196167, "[TT] Mean Revisit Time of the TeLEOS-1 = 12-16 hours"]
-[11.429697036743164, 4.796451091766357, "[TT] Side Length of the HIT-Sat = 12 cm"]
-[11.912930488586426, 5.407495975494385, "[TT] Dimensions of the CLARA Instrument = 114 mm x 141 mm x 155 mm"]
-[8.288873672485352, 7.246264457702637, "[FF] Camera Type of the Gaia = CCDs"]
-[3.34309458732605, 5.6746931076049805, "[TT] Number of Radiating Elements of the SAR Antenna = 8192"]
-[4.847711086273193, 0.026360249146819115, "[TT] Launch Date of the SpaceX CRS-13 = December 15, 2017"]
-[5.136244773864746, 2.32256817817688, "[TT] Mission Type of the TAIKI = EO"]
-[10.919045448303223, 3.685410499572754, "[TT] Size of the TechEdSat-6 = 4U"]
-[5.3689069747924805, 3.262051820755005, "[TT] Operator of the DSAS = CSSAR, Beijing, China"]
-[10.109227180480957, 3.2361717224121094, "[FF] Use of the CubeSats = Artificial debris targets"]
-[5.674363613128662, 2.3693912029266357, "[TT] Reduced Size of the Upgrade Team = Four"]
-[7.341038227081299, 3.715405225753784, "[FF] Purpose of the GNSS = Polar motion determination"]
-[4.320018768310547, 3.123837471008301, "[TT] Test Transmission Location of the Herschel = ESA's ESTRACK (ESA Tracking stations network) station at New Norcia, Australia"]
-[5.034080982208252, 4.345553398132324, "[TT] Total Number of Stations in North America of the Mesonet = Nearly 1,500"]
-[6.561916828155518, 7.66495943069458, "[TT] Data Quantization of the Imager = 12 bit"]
-[7.940073490142822, 9.219026565551758, "[TT] Wavelength of the Hydroxyl ion = 2.7-2.8 \u00b5m"]
-[5.977530002593994, 0.25803717970848083, "[TT] Descent Date of the Rosetta = 30 September"]
-[10.155367851257324, 0.6867057681083679, "[TT] Spacecraft Separation of the Tri-TIP = 250-500 km"]
-[9.745511054992676, 4.858790874481201, "[FF] Required Rotation Rate Knowledge of the ANDERR-MAA spacecraft = Yes"]
-[8.574380874633789, 4.653686046600342, "[FF] Design Presentation Date of the Star Tracker = March 3-10, 2012"]
-[4.8150315284729, 3.242711305618286, "[TT] Manufacturer of the TANSO-FTS = Harris Corp."]
-[8.947044372558594, 5.688368320465088, "[TT] Accuracy of the Unit = \u00b110 arcsec"]
-[8.017983436584473, 4.3222551345825195, "[FF] Transfer Phase Start of the LUMIO = Stable Manifold Injection Maneuver"]
-[3.882697105407715, 6.46827507019043, "[TT] Antenna Type of the CTAGS Antenna Array = Patch antennas"]
-[5.145306587219238, 4.4969916343688965, "[TT] Manufacturer of the GNSS Receiver = Syrlinks"]
-[10.15114974975586, 9.323016166687012, "[TT] IGFOV at Nadir for SWIR of the Instrument = 1.0 km"]
-[4.470200538635254, 7.857790946960449, "[TT] Frequency of the K-band = About 24 GHz"]
-[4.951750755310059, 3.7248241901397705, "[TT] BSL Entry of the MCU = Provides BSL (BootStrap Loader) entry for payload and EPS"]
-[5.339731693267822, 0.7701897025108337, "[FF] Third Birthday of the SmallGEO = 14 September 2020"]
-[7.048800468444824, 8.337296485900879, "[TT] Estimated SNR of the Band 4 = 544.65 \u00b1 88.66"]
-[13.2819185256958, 5.7058234214782715, "[TT] Maximum Depth Of Discharge of the Solar Array = 1% outside of eclipse and 8% during eclipse"]
-[5.283730506896973, 2.8387999534606934, "[FF] Composition of the SloshSat Investigators' Working Group (IWG) = Academic researchers from Groningen State University (NL), Delft Technical University (NL), Technion (Israel), and investigators from ESA, NASA and NLR"]
-[9.449517250061035, 1.2716161012649536, "[TT] Release Speed of the DSAT#1 = 5cm/s"]
-[5.5602617263793945, 0.4973892271518707, "[TT] Discovery Year of the 1999JU3 = 1999"]
-[7.8702006340026855, 2.1450717449188232, "[FF] Manufacturer of the Ocean Color and Temperature Scanner = Unknown"]
-[10.193181037902832, 9.398965835571289, "[TT] Nominal IGFOV of the Band 9 = 2 km"]
-[5.844038963317871, 7.156008243560791, "[TT] Max. Data Rate of the RA-1 = 15 kbit/s"]
-[9.979790687561035, 2.9122490882873535, "[FF] Maiden Flight Date of the CubeSat = Unknown"]
-[8.62157154083252, 6.801454067230225, "[TT] Imaging System of the Rosetta = OSIRIS camera"]
-[6.77335786819458, 1.0849254131317139, "[FF] Unboxing Date of the Mercury Magnetospheric Orbiter = April 29, 2015"]
-[7.703736782073975, 9.234195709228516, "[TT] Wavelength Range of the Band 8 = 5.77-6.6 \u00b5m"]
-[12.138476371765137, 1.9750022888183594, "[FF] Data Reception and Distribution Agreement Date of the CartoSat-1 = January 14, 2008"]
-[7.51169490814209, 3.437448263168335, "[FF] Description of the Level-1 (L1) = Radiometric corrected image (image without detector and atmospheric defects removed, shadow, noise and blur removed, no projection information in the projection system)"]
-[5.009963035583496, 3.2804319858551025, "[TT] Manufacturer of the MOMA = ESA"]
-[10.364961624145508, 5.815180778503418, "[TT] Mean Temperature of Operation of the WPM = 17.5\u00baC"]
-[8.037725448608398, 5.840731143951416, "[TT] Intensity Levels of the LISS-3 camera = Six"]
-[5.069423675537109, 3.3596272468566895, "[TT] Manufacturer of the STACEM = SDL (Space Dynamics Laboratory) of USU (Utah State University)"]
-[9.080795288085938, 4.591127395629883, "[TT] Sun Elevation for Operations of the Metric Camera = Never exceeded 30\u00ba"]
-[7.99069881439209, 8.201038360595703, "[TT] Channels of the IR Instrument = Channel 1, Channel 2"]
-[7.093809127807617, 7.9035773277282715, "[TT] Backscatter Coefficient of the Satellite = -10 dB to +50 dB"]
-[11.849017143249512, 6.765865802764893, "[TT] Ion energy of the Microdosimeter A = > 1 MeV"]
-[14.103403091430664, 7.162129878997803, "[TT] Voltage of the ESSM = 28\u00b15 V"]
-[7.567641735076904, 4.716656684875488, "[FF] Component of the ECAL electronics boxes = Unknown"]
-[7.9626312255859375, -0.5722833871841431, "[FF] Data Tracking of the GRACE = Ice Loss at the Poles"]
-[5.510410308837891, 4.942529201507568, "[TT] Operation of the CGA = Can be run autonomously"]
-[13.374739646911621, 7.339694023132324, "[TT] Power of the HIA = 3.0 W"]
-[4.140170574188232, 0.6396467685699463, "[TT] Project Scientist of the INTEGRAL = Chris Winkler"]
-[8.830622673034668, 5.803121089935303, "[FF] Measurement of the SCM = Potential"]
-[11.80235481262207, 3.2600350379943848, "[TT] Force of the Thrusters = 5 N"]
-[8.356915473937988, 7.921292781829834, "[TT] Number of Arms of the Spectrometer Arms = 4"]
-[5.1241068840026855, 2.2514994144439697, "[TT] Mission Type of the INSAT-3D = EO"]
-[5.183043479919434, 0.5958194136619568, "[TT] USC Operation End Date of the Hitomi = March 26"]
-[9.873238563537598, 8.196091651916504, "[TT] Focal Length of the Instrument = 72.5 mm"]
-[11.115195274353027, 0.5527440905570984, "[FF] Number of Confirmed Exoplanets of the Kepler = 100+"]
-[11.814887046813965, 6.552719593048096, "[TT] Energy Threshold of the CRaTER = >10 MeV"]
-[8.751493453979492, 8.747512817382812, "[FF] Design of the Supermirror = Periodic length decreases from the top surface to the base substrate"]
-[4.248537540435791, 7.224604606628418, "[TT] Frequency Bands of the GovSat-1 = X-band and Military Ka-band"]
-[8.280150413513184, 5.938409328460693, "[TT] Measurement Rate of the Claire = 500th measurement on 09 December 2016"]
-[4.607907295227051, 1.6233742237091064, "[TT] Project Status Presentation Date of the GOSAT-2 = May 5-7, 2014"]
-[8.334085464477539, 8.493328094482422, "[TT] Micro-Roughness of the Primary Optics = Better than 0.2 nm"]
-[10.728059768676758, -0.19837598502635956, "[TT] Formation Control Accuracy of the TanDEM-X = 10 m (1\u03c3)"]
-[11.580756187438965, 3.29231595993042, "[FF] Propulsion System of the AOCS = Bi-propellants"]
-[9.949250221252441, 8.197185516357422, "[TT] Focal Length of the VSSC = 1.75 m"]
-[9.826671600341797, -0.29999038577079773, "[TT] Altitude of the DMSP = 811 - 853 km"]
-[11.524221420288086, 5.907803058624268, "[FF] Type of the Fermi Gamma-ray Burst Monitor (GBM) = Sodium Iodide (NaI)"]
-[10.036211013793945, -1.544065237045288, "[TT] Orbit Inclination of the Monitor-E = 97.5\u00ba"]
-[8.976967811584473, 4.554448127746582, "[FF] Impact on Measurements of the Thermal Effects = Systematic errors"]
-[4.642213821411133, 6.69195556640625, "[FF] Telemetry Standard of the X Band Transmitter = DVB-S2 CCSDS"]
-[5.532285213470459, 6.53565788269043, "[TT] Packet Storage of the LT = Queue"]
-[5.0269951820373535, 3.434356927871704, "[TT] Manufacturer of the Adcole Maryland Aerospace MAI401 ADCS = Adcole Maryland Aerospace"]
-[10.152731895446777, 7.445687294006348, "[TT] Image Size of the AMI = 17.8 degree diameter circle"]
-[11.35729694366455, 4.0955610275268555, "[FF] Size of the Solar Flare = X8.2-sized"]
-[11.764286041259766, 6.731898307800293, "[TT] Energy Range of the Measurement = ~ 150 keV to 4 MeV"]
-[7.030158996582031, 4.063669204711914, "[TT] Sensor Payloads of the DMSP-19 = Larger"]
-[11.724350929260254, 0.11486712843179703, "[TT] Number of Confirmed Exoplanets of the TESS = 175"]
-[3.926042079925537, 6.592304706573486, "[TT] Phase Shift Bit Number of the Antenna = 5"]
-[9.033596992492676, 0.5335233807563782, "[FF] Operational Orbit Reach Date of the Artemis = Jan. 31, 2003"]
-[10.291200637817383, 7.099793910980225, "[TT] Atmospheric Volume Footprint of the MEIDEX = 100 km x 100 km"]
-[6.595418930053711, -2.045973062515259, "[FF] Update Date of the Jason-3 = Feb. 12, 2016"]
-[6.337586402893066, 5.461353302001953, "[FF] Purpose of the NICT's New OGS = Satellite Laser Communication and SOTA/Socrates experiment"]
-[13.767472267150879, 2.6935198307037354, "[TT] Launch Mass of the SEOSat = Approximately 830kg"]
-[5.1360554695129395, 1.1233296394348145, "[TT] Program Status of the NPOESS = Cancelled in 2010"]
-[13.712753295898438, 5.407110691070557, "[TT] Solar Cells Type of the EPS = Triple-junction surface-mounted"]
-[10.539740562438965, 3.3248953819274902, "[TT] Form Factor of the MicroMAS = 3U CubeSat"]
-[3.1894264221191406, 4.9958624839782715, "[TT] FRS-2 Resolution of the RISAT-SAR = 6 m x 4 m (Az x Range)"]
-[6.806910991668701, 1.6293249130249023, "[FF] URL of the NASA Moon Mission = http://www.jpl.nasa.gov/news/news.php?feature=6662&utm_source=iContact&utm_medium=email&utm_campaign=NASAJPL&utm_content=weekly20161028-5"]
-[10.94025707244873, 7.5465803146362305, "[TT] Swath Width of the MESSR = 100 km"]
-[4.572883129119873, 0.05763617530465126, "[TT] Reentry Date of the Starshine-2 = April 26, 2002"]
-[9.724141120910645, 5.310416221618652, "[TT] Yaw Coupling Factor of the Compensation Plate = 10 \u00b5m/rad"]
-[10.55101203918457, 7.486724376678467, "[TT] Monoscopic Area Coverage of the QuickBird-2 = 1 x > 4 x"]
-[3.270092248916626, 5.023383617401123, "[TT] PRF of full-pol. mode of the ALOS-2 SAR = Doubled as that of single/dual-pol."]
-[9.247445106506348, 3.238259792327881, "[FF] Purpose of the Telescope-coronagraph 304 \u00c5 = Imaging hot plasma (T ~ 10 MK) of the solar corona"]
-[9.288869857788086, 8.113595008850098, "[TT] Instrument Mass of the LLNL imaging system = < 1.83 kg"]
-[7.6392436027526855, 4.547272682189941, "[FF] Houses of the AM = HEPS instrument, the ECS (Experimental Computer System), and the radiometers and photometers"]
-[5.651412010192871, 7.020546913146973, "[TT] Data Rate of the SDS = 2.66 Mbit/s"]
-[5.391262054443359, 5.432859897613525, "[TT] Error Handling of the Tracking Mode = If the estimated pointing error is too large, the control system sends a command to mute the Tx"]
-[8.160564422607422, 2.317580461502075, "[TT] Prediction Accuracy of the Weather Information = Better than 90%"]
-[5.973076343536377, 0.32045039534568787, "[TT] Image Posting Date of the Rosetta = March 4, 2015"]
-[13.955948829650879, 3.9428513050079346, "[TT] Mass of the ATLAS instrument = 298 kg"]
-[5.559701442718506, 5.707891941070557, "[TT] CPU of the ACU = HD64F7145FW50"]
-[7.79656982421875, 9.049363136291504, "[FF] Emission Wavelengths of the PREFIRE = Greater than 15 \u03bcm"]
-[10.236773490905762, 8.053165435791016, "[TT] Telescope Aperture of the NEOSSat = 15 cm"]
-[10.734323501586914, 2.8062174320220947, "[FF] Avionics of the Microsatellite = PUNCH avionics"]
-[6.255144119262695, 3.7003815174102783, "[FF] Risk Mitigation of the Autonomous Satellite Avoidance Program (ASAP) = In Progress"]
-[7.4964518547058105, 3.786306142807007, "[FF] Components of the NightPod = \"head\", \"legs\", lens support"]
-[7.889954090118408, 5.980478286743164, "[FF] Video Camera Assembly of the LAPAN-A2 = Two cameras, featuring analog and digital outputs respectively"]
-[5.220252990722656, 4.0349650382995605, "[TT] Bus of the Essaim-1, -2, -3, and -4 = Myriade microsatellite bus of CNES"]
-[4.655615329742432, 7.37396240234375, "[TT] Uplink and Downlink Frequency of the NEMO-AM = S-band"]
-[5.486600875854492, 5.714704513549805, "[TT] Model of the Tekk T-Net mini 960 radio = Tekk T-Net mini 960"]
-[10.845091819763184, 2.117326498031616, "[FF] Detected Atoms of the XMM-Newton = Iron atoms"]
-[9.80434513092041, 5.018428802490234, "[FF] Stressful Periods of the Power Subsystem = Low beta angle (long eclipse)"]
-[8.268715858459473, 2.400006055831909, "[FF] Cloud Cover Impact of the CHOMPTT = Preventing lasing from the Mount Stromlo site"]
-[5.489663124084473, 0.3800060451030731, "[TT] Launch Date to ISS of the Flock 1d = October 28, 2014"]
-[14.190990447998047, 3.316157817840576, "[TT] Mass of the SFINKS = 30 grams"]
-[9.584519386291504, 7.047791957855225, "[TT] Spatial Resolution of the KMS = 60 - 120 m"]
-[8.000678062438965, 4.258163928985596, "[FF] Mission of the Celesta = Study the effects of radiation on electronic systems"]
-[10.980348587036133, 5.706345558166504, "[TT] Material of the Heat Shield = Avcoat"]
-[3.7405335903167725, -0.8070209622383118, "[FF] Baseline Orbital Parameters of the ABEX = Shown in Table 2"]
-[3.3610360622406006, 1.4090794324874878, "[TT] End of Life Date of the Sentinel-2 = 2038"]
-[3.87605619430542, 7.864796161651611, "[TT] Modulation Type of the Resurs-O1-4 = BPSK (NRZ-M)"]
-[11.721932411193848, 3.5018310546875, "[TT] Grid Diameter of the Ion Thruster = 100 mm"]
-[6.757848262786865, 5.052244663238525, "[FF] Components of the IMS-2 System = EPS (Electric Power Subsystem) with battery and solar arrays, AOCS (Attitude and Orbit Control Subsystem), TT&C (Telemetry, Tracking & Command) subsystem, RCS (Reaction Control Subsystem), thermal subsystem for bus, mechanisms"]
-[8.334785461425781, 8.283203125, "[TT] Wavebands of the R3 spacecraft = Visible to near-IR"]
-[6.426107406616211, 1.577233076095581, "[TT] Survey Duration of the eROSITA = 4 years"]
-[8.91555118560791, 4.838371276855469, "[FF] Avoidance Targets of the SVOM Attitude = Sco X1 source, Galactic Plane"]
-[6.490391731262207, 0.7142724990844727, "[FF] Long-Term Acquisition Plan Publication Date of the Landsat-7 = Oct. 2006"]
-[4.892416477203369, 0.34058791399002075, "[TT] Launch Date of the CXBN-2 = 18 April 2017"]
-[4.748682975769043, -0.26476341485977173, "[TT] Installation Date of the CATS = Jan. 22, 2015"]
-[3.289740800857544, 2.277571678161621, "[FF] Assets Ownership Transfer of the Copernicus Space Component = Defined in Agreement"]
-[13.820270538330078, 2.7578413486480713, "[TT] Launch Mass of the SAST-5000 = Approximately 5300 kg"]
-[5.9381818771362305, -0.4573737680912018, "[TT] Duration of the TAKE5 mission = Jan. 31, 2013 - June 19, 2013"]
-[8.495288848876953, 0.13694967329502106, "[TT] Porosity of the Comet 67P/Churyumov-Gerasimenko = High"]
-[1.7609261274337769, -2.061347484588623, "[FF] Size of the Hayabusa-2 = Fridge-sized"]
-[9.414328575134277, 7.3571062088012695, "[TT] Spatial Resolution (Band 1) of the PanMUX = 5 m"]
-[12.79901123046875, 7.5947465896606445, "[TT] Power Consumption of the Instrument = < 24 W"]
-[5.920492649078369, 2.609243631362915, "[FF] Mission Regions of Interest of the HyperScout\u00ae = Identified by the consortium partners"]
-[8.573124885559082, 5.663319110870361, "[TT] Horizontal Accuracy of the Galileo Service = 4 m"]
-[8.849883079528809, 7.595186233520508, "[TT] Temporal Resolution of the Visible Spectral Band = 30 minutes (frame time)"]
-[5.311524868011475, 3.958859920501709, "[TT] Number of Satellites of the PanGeo Fleet = 9"]
-[5.094458103179932, 2.1281721591949463, "[FF] Software Code Reuse of the VMOC = About two-thirds between TacSat-4 and ORS-1 missions"]
-[5.147764205932617, 3.673912286758423, "[TT] Provider of the SSU = BMO"]
-[10.407326698303223, 7.616534233093262, "[TT] Radius of Circular Scan of the S-192 optomechanical scanner = 42 km"]
-[5.3781867027282715, 2.441608428955078, "[FF] Educational Mission of the Irvine 02 = Irvine Public School Foundation"]
-[12.08140754699707, 3.456904888153076, "[TT] Proof Pressure of the PPCU ion thruster = >1.5 x MEOP"]
-[10.131439208984375, 8.1738862991333, "[TT] Aperture Size of the SSJ/4 = About 20 x 10 (FWHM)"]
-[10.19007682800293, 5.785427570343018, "[TT] Detector's Temperature of the EyeSat = 0\u00b0C"]
-[10.152522087097168, 1.9562878608703613, "[TT] Resumption of Science Observations Date of the Chandra X-ray Observatory = Sept. 12"]
-[7.9958176612854, 5.366715908050537, "[TT] Accuracy of the FLLS = 300 \u00b5m"]
-[6.247299671173096, 1.0508441925048828, "[TT] Image Acquisition Date of the Landsat-8 = May 21, 2022"]
-[5.342018127441406, 8.725075721740723, "[TT] Bandwidth of the Band 8 = 845-885 nm"]
-[5.9035186767578125, -0.649878203868866, "[FF] Ballistic Coefficients Comparison of the POPACS = DANDE mission results"]
-[8.618473052978516, 1.2810451984405518, "[FF] Operation Frequency of the Aquarius = Not specified"]
-[6.922144889831543, 4.174528121948242, "[FF] Purpose of the Proto-Flight Model (PFM) = The final Spacecraft to be launched"]
-[5.625120639801025, 5.975425720214844, "[TT] Components of the PM = Dynamic RAM"]
-[8.540218353271484, 3.1487557888031006, "[FF] Integration Date of the NASA ultraviolet space spectrograph = May 23, 2017"]
-[5.458486557006836, 3.9807050228118896, "[TT] Number of Geographic Sites of the PUTC = 69"]
-[4.669724464416504, 0.46627184748649597, "[TT] Launch Date Control of the ORS-6 = Not have the ability to dictate launch date"]
-[7.858550548553467, -2.4921553134918213, "[TT] Ion Type of the GOLD = Oxygen ions"]
-[4.733476638793945, 7.878433704376221, "[TT] Clock Basis of the DOT = Several MHz"]
-[8.488970756530762, 8.010615348815918, "[TT] Width of the Spectral Block = 100 pixels"]
-[6.7847137451171875, 2.0074896812438965, "[TT] Eclipse Encounters of the Hinode = Total: 3"]
-[4.120736122131348, 1.3775213956832886, "[TT] Operation End Date of the Meteosat First Generation = 2017"]
-[8.698687553405762, -0.17065690457820892, "[TT] Lunar Working Orbit of the Chang'e-2 = 100 km x 100 km"]
-[5.342103004455566, 3.9783973693847656, "[TT] Number of Satellites of the BDS-3 = 30"]
-[11.007380485534668, 0.5591575503349304, "[TT] Number of Candidate Planets of the Kepler Space Telescope = More than 4,000"]
-[6.651975631713867, 0.7626244425773621, "[FF] Retired Date of the Herschel and Planck = Unknown"]
-[6.160895347595215, 0.6030615568161011, "[FF] Data Revealed of the Hinode = The source of the SEP events"]
-[7.55294132232666, -0.3191351592540741, "[TT] Local Time on Ascending Node (LTAN) of the Meteor-M-2 = 0930 hours"]
-[4.472687721252441, 6.978183269500732, "[TT] Back-up Channel of the RF Communications = S-band"]
-[8.752038955688477, 6.522566795349121, "[TT] Resolution of the TEMPO = 10 km2"]
-[2.923116683959961, 4.2179179191589355, "[TT] Emergency Observation Date of the PALSAR-2 = November 13, 2016"]
-[4.30007266998291, 7.066256523132324, "[FF] Architecture of the X-band system = Not specified"]
-[11.4940767288208, 3.2986807823181152, "[TT] Orbit Maintenance System of the GOCE = Ion Propulsion Unit"]
-[6.361130714416504, -0.5270387530326843, "[TT] On-Orbit Duration of the TRACE = 10 years"]
-[8.530978202819824, 4.8569416999816895, "[FF] Inertia Tensor of the AGS = Best available"]
-[7.61570405960083, 4.458649158477783, "[FF] Location of the ISIS = As far aft on the spacecraft body as possible, on the ram side, just inside the umbra line"]
-[11.270828247070312, 0.962610125541687, "[FF] Conference Date of the LISA Pathfinder = Oct. 17-20, 2005"]
-[10.9881010055542, 6.350413799285889, "[TT] Coating Material of the Primary Mirror = Boron carbide (B4C)"]
-[5.241746425628662, 3.006957530975342, "[TT] Contractor of the CAPSTONE = Advanced Space of Boulder, Colorado"]
-[4.615989685058594, 5.4467082023620605, "[TT] Signal Types of the QuakeSat = Approximately 25"]
-[6.327507972717285, 8.600122451782227, "[FF] Polarization Modes of the TRMs = Single (HH/VV/HV), dual (HH + HV=VV + VH), quad (HH + HV + VV + VH), and compact polarimetry (Tx: oriented 45\u00ba or circular, Rx: H or V)"]
-[5.287607669830322, 2.06461501121521, "[TT] Deputy Director of the Roman = Nancy Levenson"]
-[6.360601902008057, 7.410246849060059, "[FF] Output Signals of the AHM = 10 MHz frequency and 1 pulse per second (1 PPS)"]
-[8.488446235656738, 6.013864040374756, "[TT] SST Accuracy of the AATSR = Better than 0.3 K"]
-[5.996923923492432, 1.621485948562622, "[FF] Date of the 5th International Conference on Spacecraft Formation Flying Missions and Technologies = May 29-31, 2013"]
-[9.985334396362305, 1.4361178874969482, "[TT] Explosion Frequency of the Massive Star = About every fifty years"]
-[12.082290649414062, 3.4747581481933594, "[TT] Propellant of the PPCU ion thruster = Xenon"]
-[4.505144119262695, 2.966482639312744, "[TT] Location of the SOC = Villafranca near Madrid"]
-[3.8212201595306396, 7.929119110107422, "[TT] Modulation of the S-band Transmitter = DQPSK (Differential Quadrature Phase Shift Keying)"]
-[10.294018745422363, 3.198546886444092, "[TT] Telemetry Frames Received of the SONATE CubeSat = More than 5000"]
-[5.783738136291504, 2.20005202293396, "[FF] Communications Snapshot of the CADRE = URL: https://web.archive.org/web/20190716185147/http://mstl.atl.calpoly.edu/~bklofas/Presentations/DevelopersWorkshop2012/CHDC_Provost_CADRE.pdf"]
-[9.584159851074219, -0.7244940400123596, "[TT] Orbit Altitude of the GOES-S = 35,786 km"]
-[4.905971527099609, 0.4414161145687103, "[TT] Scheduled Launch of the Space Comb = 2017"]
-[5.912673473358154, 3.0374934673309326, "[TT] Awarded Funding of the OPS-SAT = 12"]
-[3.73040771484375, -1.0817369222640991, "[TT] Orbit Type of the ExoMars Orbiter = Elliptical"]
-[13.46181583404541, 7.259106159210205, "[TT] Ignition Power of the T3\u00b5PS = 10.1 W"]
-[10.104965209960938, -1.4494470357894897, "[TT] Orbit Inclination of the GOSAT-GW = 98.06\u00b0"]
-[3.7232465744018555, 2.543351173400879, "[TT] Network Type of the Iridium NEXT = IP-based, broadband"]
-[6.114126682281494, -0.39924755692481995, "[TT] Program Duration of the SOHLA-1 = 5 years"]
-[9.511603355407715, 6.994653224945068, "[TT] Angular Resolution of the eROSITA = Unprecedented"]
-[8.733688354492188, 2.107025623321533, "[TT] Business Terminal Diameter of the WINDS = 5 m"]
-[8.244485855102539, 3.2393226623535156, "[TT] Purpose of the RIS = Laser long-path absorption measurements of atmospheric trace species"]
-[7.952914237976074, -0.39214685559272766, "[FF] Maximum Extent Date of the Arctic Sea Ice = March 9, 2018"]
-[7.44945764541626, 4.302506446838379, "[FF] Sensor Complement of the OPAL = Not provided"]
-[3.092207670211792, 2.2757461071014404, "[FF] Multispectral Data of the Copernicus Sentinel-2 = Parameter Value Unknown"]
-[8.250359535217285, 0.1500541865825653, "[TT] Mission Type of the Meteor-M-2 = Meteorological"]
-[5.43874454498291, 0.6249685287475586, "[FF] Commissioning Phase Date of the Envisat = June 2001"]
-[5.2467427253723145, 4.6792755126953125, "[FF] Construction Completion of the Emergency Egress System = TBD"]
-[6.07529878616333, 0.24283580482006073, "[TT] Age of the Rosetta = Over 12 years"]
-[8.855338096618652, 3.109060049057007, "[FF] Description of the R. R. Hodges-model = Describes the terrestrial hydrogen exosphere up to ~60,000 km from the geocenter, based on a third-order spherical harmonic expansion"]
-[7.46292781829834, 2.2509615421295166, "[FF] Function of the Transponder = Track the Biomass satellite"]
-[4.746237277984619, 3.1969480514526367, "[FF] Avionics architecture of the Thales Alenia Space (France and UK) = Responsible"]
-[1.7397459745407104, 4.563898086547852, "[FF] N/A of the TLE micro-camera = N/A"]
-[9.645853042602539, 7.093867301940918, "[TT] Resolution of the OLS = 0.55 km"]
-[7.0825324058532715, 7.021710395812988, "[TT] Pulse Pileup Threshold of the Readout System = ~ 105 cps"]
-[10.319257736206055, 7.15203332901001, "[TT] Full Disk Circle Height of the ABI = 3000 km"]
-[5.433559417724609, 0.07586599886417389, "[FF] Operation Start Date of the RapidEye = Unknown"]
-[10.572220802307129, 2.8956592082977295, "[FF] Imaging Improvement of the Nanosatellite System = Better imagery at lower cost"]
-[5.28264856338501, 1.9091546535491943, "[TT] Mission Status of the Megha-Tropiques = Operational (extended)"]
-[7.727179050445557, 9.220037460327148, "[TT] Band Centers of the NIRST = 3.8 \u00b5m (MWIR), 10.85 \u00b5m and 11.85 \u00b5m (TIR)"]
-[7.9794416427612305, 3.9324140548706055, "[FF] Disposal of the Monitor-E mock-up = De-orbit together with Breeze into the atmosphere"]
-[12.723885536193848, 1.947277545928955, "[FF] Science Objectives of the SAGE-III = Investigate the spatial and temporal variability of the measured species"]
-[6.769565582275391, 5.866928577423096, "[TT] Quantity of the OBC = 3"]
-[8.316610336303711, 8.443012237548828, "[TT] Pitch of the VNIR FPA = 7.5-15 \u00b5m"]
-[6.739741325378418, -0.5664088726043701, "[TT] Orbital Period of the Main Payload = About 97.7 minutes"]
-[5.737304210662842, 2.0196032524108887, "[FF] Mission Status of the SAC-D = Unknown"]
-[5.542269229888916, 3.7985661029815674, "[TT] Satellite Constellation Goal of the Satellogic = 300 satellites by 2025"]
-[4.608264446258545, 7.08254337310791, "[TT] Raw Data Transmission of the SAST-5000 = X-band"]
-[9.71972942352295, 8.434859275817871, "[TT] FOV in Vertical Plane of the THD = 22\u00ba"]
-[6.765072822570801, 5.915956497192383, "[TT] Quantity of the XRDs = 6"]
-[11.757786750793457, 3.315944194793701, "[TT] Thruster Type of the Starlink Satellite = Hall thrusters powered by krypton"]
-[8.390145301818848, 2.789881706237793, "[TT] Measurement Domain of the OSCAR-QUBE = Gravity and Magnetic Fields"]
-[12.037009239196777, 6.463027000427246, "[TT] Turning Point Energy of the Positron Fraction = 275+32 GeV"]
-[7.795862197875977, 4.905860900878906, "[FF] Control Electronics of the Lander = Provide the interface to all the sensors and the actuator drives"]
-[5.800375461578369, 7.156971454620361, "[TT] Data Rate of the LEID = 1 kbit/s"]
-[10.422845840454102, 5.630674362182617, "[TT] Surface Temperature of the HD 21749c = Perhaps as high as 800\u00ba F (427 \u00baC)"]
-[7.623604774475098, 5.575817108154297, "[FF] Sampleability of the Site Nightingale = High"]
-[5.87112283706665, 1.8664621114730835, "[TT] Splashdown Date of the Orion = Dec. 5, 2014"]
-[3.2835261821746826, 0.1260429322719574, "[TT] Phase Angle of the JL-1-GF03D = 120\u00ba"]
-[6.443061351776123, -0.5280438661575317, "[TT] Landing Site Data Transfer Time of the Spacecraft = Two days"]
-[6.386501312255859, 7.656120300292969, "[TT] 25 dB of the S/A: range = -"]
-[5.722838401794434, 0.5067160725593567, "[TT] Tandem Mission End Date of the Envisat / ERS-2 SAR = Late April 2009"]
-[8.563886642456055, 5.515102386474609, "[TT] Radiometric Resolution at Low Wind of the Satellite = 2.5 - 7.1%"]
-[11.209344863891602, 5.761389255523682, "[TT] Joint Type of the Structure = Brazed joint"]
-[6.128536224365234, 5.4953293800354, "[FF] Reliability of the ISL = Critical"]
-[18.79043960571289, 3.4787638187408447, "[TT] \u0394r (m) of the Bandari = 3.3"]
-[9.738778114318848, -0.31759369373321533, "[TT] Altitude of the NEMO-AM = 650 km"]
-[7.568966388702393, 2.171891689300537, "[TT] Geographical Coverage of the Satellite = World coverage, with latitudes from 83\u00baN to 56\u00baS"]
-[7.435340881347656, 8.572432518005371, "[FF] Band of the UVI instrument = 0.345-0.365 \u00b5m"]
-[9.284756660461426, 3.143157720565796, "[FF] Value of the Solar Wind Dynamic Pressure = Unknown"]
-[10.597396850585938, 2.849865436553955, "[FF] Fault Location of the Tsubame microsatellite = Peripheral circuit for communication"]
-[12.071647644042969, 3.4352123737335205, "[TT] Leakage of the PPCU ion thruster = internal: <0.5 Pa m3/h(Ghe), external: <1x10 -7 Pa m3/s(Ghe)"]
-[9.500986099243164, 7.477781295776367, "[TT] Ground Swath of the Multispectral Imager = 5 km"]
-[5.354915618896484, 6.542401313781738, "[TT] Max. Input data rate of the SDR-SMM = 2400 Mit/s"]
-[8.620986938476562, 4.93203592300415, "[TT] Location of the Star Tracker Camera = On the optics (outboard) bench"]
-[5.464791774749756, 1.136966586112976, "[FF] Presentation Date of the CEBRAS = July 26-31, 2015"]
-[7.665335655212402, 6.7140607833862305, "[TT] Mean Revisit Time of the TeLEOS-1 Imager = 12 to 16 hours"]
-[7.6871232986450195, 6.830127239227295, "[TT] Minimum Exposure Time of the Sensor = 10 \u00b5s"]
-[10.49721908569336, 4.018059253692627, "[TT] CFRP Booms Deployment of the Dragsail = Radially outwards"]
-[9.099346160888672, 5.458350658416748, "[TT] Pointing Knowledge of the HY-2A = < 0.05\u00ba"]
-[10.411500930786133, 2.0254342555999756, "[FF] Purpose of the NuSTAR = Capture X-ray light from regions near a supermassive black hole"]
-[5.793313980102539, 0.9588786959648132, "[TT] Image Acquisition Date of the GOES-16 = September 14, 2020"]
-[4.941032409667969, 8.306012153625488, "[TT] Frequency (GHz) of the SSM/T-2 = 50.5, 53.2, 54.35, 54.9, 58.4, 58.825, 59.4"]
-[5.3452935218811035, 3.924855947494507, "[TT] Number of Satellites of the Enxaneta = At least 250"]
-[6.519759654998779, -1.9839961528778076, "[TT] System Availability of the Jason-2/OSTM = 99.9%"]
-[10.727084159851074, 3.462987184524536, "[TT] CubeSat Size of the LEDSAT = 1U"]
-[4.261447906494141, 7.472239017486572, "[TT] Frequency of the X-band = 8.320, 8.064 or 8.192 GHz"]
-[12.218863487243652, 6.195296764373779, "[TT] Mass of the Neutrinos = Nearly massless"]
-[6.769298076629639, 1.8633599281311035, "[FF] URL of the FORUM = https://www.esa.int/Our_Activities/Observing_the_Earth/Two_new_Earth_Explorer_concepts_to_understand_our_rapidly_changing_world"]
-[6.913543701171875, 8.033318519592285, "[TT] On Orbit Noise Power of the RAX-1 = -113 dBm"]
-[8.265393257141113, 3.348531723022461, "[FF] Measurement of the FORUM = Far-infrared radiation emitted from Earth"]
-[7.398086071014404, 3.6638779640197754, "[TT] Installation Year of the NightPod = 2012"]
-[4.552212238311768, 0.5693168044090271, "[FF] Extension Date of the ANGELS = 13 October 2020"]
-[9.579850196838379, -1.6884394884109497, "[TT] Orbital Inclination of the Swarm-A (Alpha) = 87.4\u00ba"]
-[2.8818399906158447, 4.223432540893555, "[TT] Observation Image Date of the ALOS-2 PALSAR-2 = 4th August 2017"]
-[5.767762184143066, 7.163087844848633, "[TT] Data Rate of the GVAR = 2.11 Mbit/s"]
-[9.307376861572266, -1.2122429609298706, "[TT] Orbital Position of the ACTS/TOS = GEO (Geosynchronous Earth Orbit) at longitude 100\u00ba West"]
-[12.070038795471191, -0.11704380810260773, "[TT] Wide Field of View of the TESS Camera = 24\u00ba x 24\u00ba"]
-[6.795483112335205, 3.696300745010376, "[FF] Purpose of the Avionics Air Assembly (AAA) Fans = Critical high speed fan spares that provides cooling to support continued operations for Environmental Control and Life Support System (ECLSS) Temperature and Humidity Control (THC) across the space station"]
-[3.372277021408081, 6.3525495529174805, "[TT] Dimensions of the Antenna = 10.74 m x 2.16 m"]
-[8.554484367370605, 1.090120553970337, "[TT] Quantization levels of the Precipitation over water = 0.5,10,15,20, \u226525"]
-[11.75931167602539, 3.2806053161621094, "[TT] Thrust Measurement Method of the AQT-D = Direct"]
-[4.560384273529053, 7.577643394470215, "[TT] Data Rate of the VHF links = 9.6 kbit/s"]
-[3.464137315750122, 6.437310218811035, "[TT] Antenna Length of the Instrument = 60 m"]
-[5.053124904632568, 6.857968807220459, "[TT] LISS-I Data Downlink Transfer Rate of the Satellite = 5.4 Mbit/s"]
-[7.5006256103515625, 3.496051788330078, "[TT] Debris Removal Capability of the ELSA-M = Multiple defunct satellites in a single mission"]
-[5.016820907592773, 1.5954878330230713, "[FF] Meeting Date of the Global Change Observation Mission (GCOM) = 24-26 April 2018"]
-[13.782303810119629, 3.0751965045928955, "[TT] Mass of the TriG GNSS-RO payload = 115 kg"]
-[6.106260776519775, 4.694607257843018, "[FF] Flight Software of the ABEX = F\u2019 (pronounced F prime) framework from JPL"]
-[9.980738639831543, 2.718273639678955, "[TT] CubeSat Deployments of the NanoRacks = 185th from the Space Station"]
-[10.812003135681152, 7.5567121505737305, "[TT] Swath Width of the DMC-3 = 20 km"]
-[6.127229690551758, 5.3608927726745605, "[FF] Hardware and Software Design of the PDH = Exactly the same as OBC"]
-[6.188461780548096, 2.266127347946167, "[FF] Principal Investigator of the CuPID = Brian Walsh"]
-[4.563582420349121, 5.513892650604248, "[FF] Conference Presentation of the GOMX-1 = 4S (Small Satellites Systems and Services) Symposium"]
-[11.999176979064941, 4.887887954711914, "[TT] Structure of the S/C = Box-shaped three-axis bus"]
-[4.39125919342041, 3.0415842533111572, "[TT] Ground Stations of the Colony I = Melbourne, Florida, and Fort Huachuca, Arizona"]
-[5.2861714363098145, 3.9377641677856445, "[TT] Total Satellite Missions of the ICEYE = 10"]
-[4.8424859046936035, 7.959447860717773, "[FF] Components of the DORIS = Receiver, ultra-stable oscillator, antenna"]
-[6.099421977996826, 5.543107032775879, "[FF] Beamforming Technology of the TriG receiver = Digital"]
-[8.705581665039062, -0.19997644424438477, "[TT] Lunar Orbit Altitude of the Chang'e-1 = 200 km"]
-[6.810607433319092, 1.9177683591842651, "[FF] URL of the Cosmic Ray Isotope Spectrometer = http://www.srl.caltech.edu/ACE/CRIS_SIS/cris.html"]
-[9.344966888427734, 4.9217681884765625, "[TT] Orbit Normal of the Attitude control = \u00b1 10\u00ba"]
-[11.969430923461914, 3.252816915512085, "[TT] \u0394V of the EP (Busek BIT-3 Iodine engine) = 1.2 km/s-1"]
-[7.452892780303955, 5.339363098144531, "[FF] Components of the SLA instrument = 38 cm telescope, diode-pumped Nd:YAG laser transmitter, altimeter receiver electronics package, 250 MHz waveform digitizer"]
-[7.757719039916992, 6.807510852813721, "[FF] Measurement Concept of the KaRIn = Interferometric"]
-[7.418259143829346, 4.792794227600098, "[FF] Instruments of the SciSat-1/ACE = MAESTRO, ACE-FTS"]
-[5.802452564239502, 4.305948257446289, "[FF] Feasibility of the Global Satnav System = Unfeasible"]
-[8.21075439453125, 8.762089729309082, "[TT] Wavelength Resolution of the ISO Instrument = 0.2 - 0.6 nm"]
-[8.734606742858887, 2.8550002574920654, "[FF] Test Satellite Deployment of the Xona Space Systems = Recently deployed"]
-[13.776222229003906, 3.608459949493408, "[TT] Antenna Weight of the PRARE ground transponder = 42 kg including gearing unit"]
-[4.286013126373291, 0.8649020195007324, "[FF] Launch Date of the HY-1B = October 4, 2007"]
-[9.819530487060547, -0.6724587678909302, "[TT] Orbit Altitude of the CBERS-4A = 628.6 km"]
-[5.145044326782227, 1.1803396940231323, "[TT] Phase A Feasibility Study of the SMOS = 2000-2001"]
-[9.162415504455566, 7.362542152404785, "[TT] GSD (Panchromatic) of the EOS = 1 m"]
-[6.161802291870117, 5.35230016708374, "[TT] Name of the STCUI-RAS = STCUI-RAS"]
-[6.339293956756592, 1.959525227546692, "[FF] Calibration Activities of the GCOM-C = On-orbit"]
-[5.135826110839844, 6.90870475769043, "[TT] Data Downlink Speed of the NorSat-3 = Up to 2 Mbit/s"]
-[14.088859558105469, 7.182615756988525, "[TT] Unregulated Bus Voltage of the EPS = 28V \u00b16 V DC"]
-[6.598084926605225, 4.447113990783691, "[FF] Data Products Distribution of the HY-1C = Free"]
-[5.389220714569092, 5.812857151031494, "[TT] Radiation hardness of the STRV-1d DHS = about 100 krad"]
-[6.101966857910156, 5.550349235534668, "[FF] Development Location of the TriG receiver = Moog Broad Reach (formerly Broad Reach Engineering)"]
-[6.423429489135742, -0.5830960869789124, "[TT] Duration of the Orbital Express = 3 months"]
-[2.9909849166870117, 4.643314361572266, "[TT] Band of the PALSAR-2 = L-band"]
-[1.7195063829421997, 6.139228820800781, "[TT] Dark Matter Percentage of the Universe = 25 percent"]
-[10.292505264282227, 4.547072410583496, "[TT] Output Torque of the Reaction Wheel (RW) = More than 0.9 Nm"]
-[8.187409400939941, 0.18390603363513947, "[FF] Subsystems of the TOPEX/Poseidon = Command and data handling, Attitude determination and control, Electrical power"]
-[11.875932693481445, 4.168464660644531, "[TT] Payload Envelope Size of the MightySat II.1 = 61 cm x 61 cm x 46 cm"]
-[5.810446739196777, -0.3953149616718292, "[TT] Deployment Time of the Spaceflight SSO-A: SmallSat Express = Approximately 13 to 43 minutes after liftoff"]
-[13.23458480834961, 7.102662563323975, "[FF] Power Consumption of the Core-DHS = Reduced"]
-[14.718649864196777, 6.6142730712890625, "[TT] Capacity of the Lithium-ion battery = 60 Ah"]
-[9.93324089050293, -0.34741806983947754, "[TT] Average Altitude of the COSPAS Satellites Altitude = 1000 km"]
-[9.41283893585205, 3.7303683757781982, "[FF] Purpose of the Spaceborne scalar magnetometers = Map the Earth\u2019s magnetic field"]
-[11.48349666595459, 5.146120071411133, "[TT] Collecting Area of the Collector = 3500 cm2"]
-[9.310392379760742, 0.8886709809303284, "[TT] Closest Approach to Sun of the Parker Solar Probe = 4 million miles"]
-[5.029356479644775, 0.42405420541763306, "[TT] Design Completion Date of the Development Status = June 16, 2016"]
-[8.63754653930664, 1.0961344242095947, "[TT] Launch Date of the SAC-D/Aquarius = June 10, 2011"]
-[9.420309066772461, 6.104565620422363, "[TT] Azimuth Angle of the SASS = 45\u00ba, 135\u00ba"]
-[8.303720474243164, 0.6733447909355164, "[FF] Composition of the Rocklea Dome = Light-colored granites"]
-[8.071284294128418, 8.099565505981445, "[TT] Spectral Band of the Camera = 744-826 nm"]
-[9.999370574951172, 2.886070966720581, "[TT] End of Life Date of the Sunstorm CubeSat = Operational as of February 2023"]
-[3.431098222732544, 4.835729122161865, "[TT] Operation Modes of the RISAT-SAR = HRS (High Resolution Spotlight), FRS-1 (Fine Resolution Stripmap-1), FRS-2 (Fine Resolution Stripmap-2), MRS (Medium Resolution ScanSAR), CRS (Coarse Resolution ScanSAR)"]
-[8.1240816116333, 3.217860221862793, "[FF] Data of the LI = Real-time data on the location and intensity of lightning flashes"]
-[14.263870239257812, 3.1887545585632324, "[TT] Mass of the Bayi Kepu Weixing-1 = 2 kg"]
-[7.148076057434082, 3.827749729156494, "[FF] Source of the Arrokoth = AAAS"]
-[5.38077449798584, 0.8245705366134644, "[TT] International Code of the BX-1 = 2008-047G"]
-[7.71490478515625, 8.459653854370117, "[TT] Bands of the INSAT sounder = 19 bands, with 18 Infrared(IR) bands, and one visible (VIS) band"]
-[9.669448852539062, 4.089629650115967, "[TT] Field Range of the Magnetic Field Sensor = 64 \u00b5T"]
-[13.579715728759766, 2.778961181640625, "[TT] Mass of the Satellite = 2388 kg (launch mass) and 2169 kg of dry mass"]
-[3.3387811183929443, 5.741822242736816, "[FF] Antenna Scalability of the NovaSAR-1 = Larger antenna can easily be realized simply by building more of the same phase center units and configuring them with the required number of rows and columns"]
-[10.74895191192627, 3.4676711559295654, "[TT] Size of the Cesium Satellite 1 = Six-unit CubeSat"]
-[7.450797080993652, 8.48981761932373, "[TT] Spectral Sensitivity (Spectral Band) of the SXI = 6 to 60 \u00c5"]
-[4.221647262573242, 6.9975972175598145, "[TT] Payload of the VESTA = Two-way VHF Data Exchange System (VDES)"]
-[5.8179731369018555, 2.631833076477051, "[FF] Deployment Services of the NanoRacks LLC = J-SSOD (JEM-Small Satellite Orbital Deployer) of JAXA"]
-[5.436672210693359, 5.169217109680176, "[FF] Potential Applications of the STP-H6-XCOM = Deep space probes, communicating with hypersonic vehicles"]
-[12.270001411437988, 6.945648670196533, "[TT] Energy Range for He of the LEICA = 0.45 - 6.1 4.3 - 38 7 - 20 18 - 350 MeV/n"]
-[9.591476440429688, 7.223333358764648, "[TT] Resolution of the Band 2 = 0.56 km"]
-[4.541518688201904, 6.885906219482422, "[TT] Backup Communication System of the RAX-2 = Microhard S-band radio"]
-[8.071759223937988, 8.204976081848145, "[FF] Sensor of the LunIR = Miniature high-temperature MWIR (Mid-Wave Infrared) sensor"]
-[6.273505687713623, 7.033786773681641, "[FF] Compression Modes of the Data Compression Module = DS-BAQ, the original BAQ, and direct output without data compression"]
-[6.425878047943115, 0.9048648476600647, "[TT] Data Distribution of the Gaia = ESAC"]
-[10.592958450317383, 5.456484317779541, "[TT] Type of the Cryogenic Multi-layer Insulation = Specialized"]
-[5.63751745223999, 1.125497579574585, "[FF] Science Operations Support Conference Date of the IBEX = March 3-10, 2012"]
-[6.732784748077393, 3.542684555053711, "[FF] Latency of the Earth Observation Services = Large"]
-[11.412325859069824, 3.9440274238586426, "[FF] Capability of the AeroCube-4 = Can slew and maintain pointing at a specific ground target"]
-[10.005800247192383, 7.154458045959473, "[TT] Scene Size of the Instrument = 5 km x 20 km"]
-[13.6271390914917, 5.836960315704346, "[TT] Power of the Solar Panels = About 230 W"]
-[5.203345775604248, 0.7795861959457397, "[TT] Milestone Date of the EGNOS V3 = March 28, 2017"]
-[11.579720497131348, 5.115720748901367, "[TT] Length of the CID = 120 mm"]
-[11.528084754943848, 6.574131488800049, "[TT] Measurement Range of the Particle Detector = Helium-4 : 10 MeV/n ~ 400 MeV/n"]
-[8.724776268005371, 0.1882474273443222, "[TT] Distance from Bennu of the OSIRIS-REx = 155 miles (250 km)"]
-[9.421693801879883, 3.684201240539551, "[FF] Purpose of the MGF = Measure deviations of the magnetic fields during space storms"]
-[12.147171020507812, 3.27976131439209, "[TT] Propellant of the Second Stage = Solid"]
-[5.799474716186523, 0.0881601944565773, "[TT] Operation Period of the TOMS = October 1978 to May 1993"]
-[13.261823654174805, 7.606407165527344, "[TT] Power Consumption of the Receiver = 0.125 W"]
-[8.291238784790039, 5.435967922210693, "[TT] Calibration Equipment of the Monochromator = \u201cHP 70950A\u201d"]
-[11.932402610778809, 5.007530689239502, "[TT] Size of the OSC = 1378mm x 1069 mm x 1160 mm"]
-[9.85039234161377, -0.6361355781555176, "[TT] Orbit Altitude of the TARANIS = 670 km"]
-[4.61408805847168, 0.8175283074378967, "[TT] Launch Date of the ADEOS 1 = May 27, 2012"]
-[5.076988697052002, 0.9099065065383911, "[TT] Retirement Date of the ALOS = May 12, 2011"]
-[8.497668266296387, 9.473115921020508, "[TT] Responsivity Measurement of the Responsivity Measurement = 1.37 A/W"]
-[11.901994705200195, 5.010916233062744, "[TT] Size of the ILAS = 800 x 1630 x 550 mm"]
-[4.996003150939941, 3.47648549079895, "[TT] Manufacturer of the Navigator platform = Russia"]
-[10.585197448730469, 1.96273934841156, "[FF] Purpose of the Model = Predict whether pulsars detected in gamma-rays could also be expected to appear in X-rays"]
-[6.622562885284424, 3.942288398742676, "[FF] Experiment Approach of the Scientific Payload = Baseline is to run most of the experiments sequentially"]
-[5.39107608795166, 8.728720664978027, "[TT] Bandwidth of the Band 3 = 480-500 nm"]
-[9.70992660522461, 6.723934650421143, "[TT] HST Geometric Factor of the LCI = 0.1 cm2 str"]
-[5.233213901519775, 5.165795803070068, "[TT] RF Front End of the Namuru V3.2 GPS Receiver = Zarlink GP2015 L1 RF front end"]
-[11.472270965576172, 6.628121852874756, "[TT] Energy Band of the eROSITA = 0.3\u201311 keV"]
-[7.660630226135254, 8.348252296447754, "[FF] Spectral Ranges of the GOSAT-2 = Backward viewing (-20\u00ba) b6: 370-390 nm, b7: 540-560 nm, b8: 664-684 nm, b9: 859-879 nm, b10: 1585-1675 nm"]
-[6.217754364013672, 2.474043130874634, "[FF] Capability of the Orion MPCV = Conduct regular in-space operations (rendezvous, docking, extravehicular activity) in conjunction with payloads delivered by the Space Launch System (SLS) for missions beyond LEO"]
-[3.072404146194458, -0.046151719987392426, "[TT] Orbital Slot of the GSAT-0210 = A02"]
-[4.392074108123779, 7.724715709686279, "[TT] Frequency Range of the S-band antenna = 2226.42 \u2013 2226.52 MHz"]
-[7.295008182525635, 6.742480754852295, "[TT] Measurement Interval of the ODM (OPTOS Dose Monitoring) System = Periodically (in minutes)"]
-[4.681596755981445, 0.3462740480899811, "[TT] End of Life Date of the QBITO = 16 February 2019"]
-[11.628114700317383, 3.6700375080108643, "[FF] Mass Balance Usage of the Integrated Firing Test = Not used"]
-[4.467824935913086, 7.1366286277771, "[TT] Ku-band repeater of the Repeater subsystem = 24 (BOL) / 20 (EOL) simultaneously operating transponders at saturation"]
-[7.80075216293335, 4.942930221557617, "[FF] Purpose of the SPEXone = Improve OCI measurements"]
-[4.896173000335693, 0.5983951091766357, "[FF] Planned Launch Year of the ProSEDS = 2003"]
-[9.326650619506836, 3.5923924446105957, "[FF] Affiliation of the DTU's Geomagnetic Measuring Stations = DTU"]
-[7.962357044219971, 1.6239709854125977, "[FF] Calibration Status of the DPR (Dual-frequency Precipitation Radar) = Continued"]
-[7.681323051452637, 9.428672790527344, "[TT] Center Wavelength of the Band 7 = 12.02 \u00b5m (832 cm -1)"]
-[8.164155006408691, 7.024077415466309, "[FF] Catastrophic Burnout of the CMOS Sensors = Did not occur"]
-[7.437119960784912, -0.3243412971496582, "[FF] Announcement Date of the Thales Alenia Space = 9 October 2018"]
-[7.463222026824951, 4.898592472076416, "[FF] Purpose of the IPEX-II = Measure the vibration of the SPAS structure"]
-[4.722829341888428, 0.7542933821678162, "[TT] Retirement Date of the FY-3A = January 5, 2015"]
-[11.338675498962402, 3.6406383514404297, "[FF] Neutralizer and main hollow-cathode heating of the IDLG = PS-4 and PS-6 on, low level"]
-[9.987653732299805, 4.8679518699646, "[TT] Rotation Speed of the Filter Wheel = 600 rpm"]
-[10.106388092041016, -2.6826417446136475, "[TT] Mass of the Astrium MMFU NAND-Flash SDR-SDRAM = \u2264 29 kg"]
-[5.311367988586426, 0.22315572202205658, "[TT] Operation Period of the ACLS = Until the end of 2019"]
-[11.725565910339355, 6.471748352050781, "[TT] Gamma-Ray Regime of the ABEX = 50-500 keV"]
-[7.3293046951293945, 8.833126068115234, "[TT] Filter Thickness of the NUV channel = 3.00 mm"]
-[7.437900543212891, 3.7167062759399414, "[TT] Measurement Precision of the GNSS-RO Instrument = Higher than other radio occultation instruments"]
-[7.504814147949219, 6.7127203941345215, "[TT] Integration Time of the PIC = 18 to 1.3 ms"]
-[4.359809875488281, 7.777320861816406, "[TT] Uplink Frequency of the LLMS/IRIS = 388 MHz"]
-[5.632024765014648, 5.706230163574219, "[FF] Processor of the OBC = 80C186+16 MByte, 80C386+64 MByte"]
-[12.687040328979492, 3.8859736919403076, "[FF] Purpose of the MMS = Study magnetic reconnection in collisionless plasmas"]
-[8.03869915008545, -0.12565582990646362, "[TT] Period of the Meteor-M2 = 101.41 minutes"]
-[8.564568519592285, 1.9423869848251343, "[TT] Range of Values of the Ocean surface wind speed = 3 - 25"]
-[7.729176998138428, 9.503700256347656, "[TT] Center Wavelength of the B12 = 2190 nm"]
-[9.225663185119629, 3.2501161098480225, "[TT] Exposure Time of the Coronal Loops = < 1 s"]
-[6.705339431762695, -0.3123251497745514, "[TT] Time Delays of the LEOSAR = Minutes to hours"]
-[11.78825569152832, 4.546366214752197, "[TT] Deployed Length of the Genesis spacecraft = 7.9 m"]
-[6.265548229217529, 8.563780784606934, "[FF] Polarities of the Overhauser Nuclear Magnetic Resonance Autooscillator = Positive or negative"]
-[5.797989845275879, 7.163105010986328, "[TT] Parameter of the Data rate = 4 Mbit/s (for 1 km resolution), 16 Mbit/s (250 m resolution)"]
-[13.436792373657227, 7.423880100250244, "[TT] Generated Power of the CBERS-4A = 2100 W"]
-[9.575782775878906, 7.5849528312683105, "[TT] Swath Width of the Panchromatic Wide-Scan Camera = 92 km"]
-[4.349613666534424, 7.76790714263916, "[TT] Downlink Frequency of the RF communications = 2.2 GHz"]
-[10.815783500671387, 3.4685096740722656, "[TT] Platform Size of the 6U CubeSat = 6U"]
-[13.462573051452637, 7.388099193572998, "[TT] Electrical Power of the STX-01 = 6 W"]
-[8.644640922546387, 8.9507417678833, "[TT] Sensitivity of the NIRSpec MIRI = 5.2 x 10 -22  Wm -2  (2 \u00b5m, \u03c4 i =100,000 s, R=1000)"]
-[7.794934272766113, 5.881791114807129, "[TT] Instrument Type of the MWR = Multiple direction/polarisation radiometers"]
-[8.194700241088867, 1.160738229751587, "[TT] Soil Moisture Estimation Error of the RISAT-1 = 6.2 to 8.5 volume percent"]
-[9.633721351623535, 7.57576847076416, "[TT] Ground Sample Distance (GSD) of the NAOMI = 2.5 m in Pan and 10 m in 4 multispectral (MS) bands"]
-[7.492788791656494, 3.3934543132781982, "[FF] Description of the Level-3 (L3) = Geo-calibrated and orthorectified image using Ground Control Points"]
-[9.01675796508789, 2.611135482788086, "[FF] Purpose of the IBEX = Examine how our heliosphere interacts with interstellar space"]
-[13.116789817810059, 5.674001216888428, "[FF] Test of the TJ Array = Discharge test will be performed on each TJ array when the biasing switch is activated"]
-[13.380077362060547, 7.369259834289551, "[TT] Power of the HEED = 2.0 W"]
-[6.64959192276001, 4.578139781951904, "[TT] Carried Payload of the Atlantis = FIPEX"]
-[9.851175308227539, 4.918117046356201, "[TT] Rotation Speed of the Antenna Subsystem = 5.6 rpm"]
-[8.93843936920166, 0.3718928098678589, "[TT] Gravitational Attraction of the Ryugu = 1/66,500th of the Earth's"]
-[6.674195289611816, -0.5666331648826599, "[TT] TLE Maintenance of the Orbit Dynamic System = 5.5 hours to 10 hours"]
-[9.770597457885742, -0.39457568526268005, "[TT] Periapsis Altitude of the Satellite = 879 km"]
-[5.168394565582275, 0.5988577604293823, "[FF] Instrument History of the CREDO-II = Flown on aircraft [the Concorde (BA) and Boeing-767 (SAS)], on the Shuttle (STS-48, -44, -53, -56, -68, and -63), in sun-synchronous orbit (UoSat-3, since Jan. 23, 1990), and on the USAF APEX satellite"]
-[6.254787921905518, 3.3299498558044434, "[FF] Installation of the MSPR-2 = Already installed to Kibo"]
-[8.105046272277832, -0.3676896095275879, "[TT] Losses Comparison of the GRACE-FO = More than double Greenland's 2002-2019 yearly average"]
-[11.80234146118164, 6.760413646697998, "[TT] Ion and Electron Pass Energy of the Dosimeter B = Greater than 50 keV"]
-[8.172410011291504, 1.3576077222824097, "[FF] Mission of the SMOS = Soil moisture and ocean salinity data"]
-[6.861181259155273, -0.6404493451118469, "[TT] Orbit Period of the ALMASat-1 = 103 minutes"]
-[8.478943824768066, 4.553106784820557, "[FF] Field-of-view of the ASTERIA payload = Wide"]
-[7.499967575073242, 2.4885261058807373, "[TT] Measurement category of the DMAC = Multi-purpose imagery (land)"]
-[5.351445198059082, 3.950934410095215, "[TT] Operations with 2 satellites of the Dove-2 = True"]
-[9.465015411376953, 6.713561058044434, "[TT] Azimuth Resolution of the SIR-C = 7 m for the selected area"]
-[5.258589267730713, 0.6212499737739563, "[FF] Facilities Launch Date of the UK space industry = July 9, 2015"]
-[6.491311550140381, 6.1447343826293945, "[FF] Data Relay Method of the Sentinel-1B = Highly precise lasers"]
-[4.9628520011901855, 3.04343318939209, "[TT] Data Distribution Center of the SAMPEX = UMSOC (University of Maryland Science Operation Center)"]
-[8.122586250305176, 5.1820902824401855, "[FF] Typical Value of the AOD = 0.1-1"]
-[8.841958999633789, 6.924002170562744, "[TT] GSD of the DMC-1 = 32 m"]
-[9.294815063476562, 5.178360939025879, "[TT] Attitude Jitter of the ADCS = \u2264 0.28 \u00b5rad, 0.1-1.0 Hz"]
-[6.767897129058838, 4.513923168182373, "[FF] Type of the DECA = Descent"]
-[5.30174446105957, 7.179989814758301, "[TT] Channel Speed of the UniSat bus communication system = 9600 bit/s"]
-[9.363659858703613, 4.6255106925964355, "[TT] Algorithm Type of the Control algorithm = B-dot based algorithm"]
-[14.259882926940918, 3.2314059734344482, "[TT] Mass of the NRA = 230 kg"]
-[3.478633165359497, 5.383121490478516, "[TT] Data Rate (max) of the SAR Antenna = 105 Mbit/s"]
-[6.92434024810791, 4.687379837036133, "[FF] System Focus of the Xona = Satellite navigation system"]
-[7.732951641082764, 6.7754011154174805, "[TT] Science Sensor Integration Times of the Imager = Longer"]
-[5.402072906494141, 2.8603854179382324, "[TT] Developer of the PHI = Consortium with major contributions from institutes in Germany, Spain and France, and smaller contributions from Sweden, Norway and Switzerland"]
-[11.82536506652832, 6.766884803771973, "[TT] Total Energy Channels of the GRS = 512"]
-[4.324110984802246, 1.233290672302246, "[TT] Launch Date of the SEOSAT/Ingenio = First half of 2020"]
-[5.913134574890137, 5.128089427947998, "[FF] Functions of the Layer 1 = Interface to the H/W, Real-time operating system and driver software, I/Fs to both the RTOS and the driver S/W"]
-[8.556751251220703, 7.518196105957031, "[TT] Shadow of the Debris = One pixel"]
-[5.78579044342041, 2.544227123260498, "[FF] Operational of the Lockheed Martin Weather Satellite = Yes"]
-[3.4206721782684326, -0.8593696355819702, "[TT] Orbit Type of the RADARSAT-2 = Sun-synchronous polar"]
-[4.5050129890441895, 2.95042085647583, "[TT] Location of the GMAL = Malindi Kenya"]
-[5.742660045623779, 7.144354820251465, "[TT] Data Rate of the Level 1b products = 2.11 Mbit/s (GVAR)"]
-[6.332313537597656, 8.058122634887695, "[TT] No of Passbands of the Channel 6 = 1"]
-[3.6708946228027344, 6.531345844268799, "[TT] Type of the IMI antenna = Deployable parabolic cylinder mesh reflector"]
-[9.586444854736328, 7.091031074523926, "[TT] Spatial Resolution of the LORE = 0.75 km"]
-[5.718221664428711, 0.918313205242157, "[FF] Merger Date of the Planet = 7 July 2021"]
-[6.395070552825928, 0.5358925461769104, "[TT] Profiles Per Day of the FormoSat-3 / COSMIC mission = 1,600~1,800"]
-[6.944908142089844, -0.5118268132209778, "[TT] Orbit Revolutions/Day of the ALMASat-1 = 14"]
-[5.677134037017822, 6.6794819831848145, "[TT] Quantity of the MnACQ-2000 Miniature Network Data Acquisition System = 9 units"]
-[5.571558475494385, 6.763418197631836, "[TT] Data Throughput of the AIS Data Collection System = 16 MB per day"]
-[7.599272727966309, 8.42635440826416, "[FF] Polarization Measurements of the GOME-2 = Advanced"]
-[7.719803810119629, 6.823239326477051, "[TT] Exposure Time of the M-CAM 1 = 20 ms"]
-[14.296802520751953, 3.1193833351135254, "[TT] Mass (kg) of the HJ-1C = 890"]
-[11.242378234863281, 3.321263551712036, "[FF] Type of the ENPULSION Micro R3 = Microsat propulsion technology"]
-[7.44810676574707, 3.0599348545074463, "[FF] Data and Imagery of the GOES-S = Near-realtime on severe weather events such as thunderstorms, tornadoes, hurricanes and flash floods, as well as hazards like fog, aerosols, dust storms, volcanic eruptions and forest fires"]
-[6.062600612640381, 1.8245025873184204, "[TT] Restart Time of the Orion's Computer = 15 seconds"]
-[8.928754806518555, 5.65585470199585, "[TT] Pointing Accuracy of the ADEOS-II = < 0.3\u00b0"]
-[7.132790565490723, 7.786230564117432, "[FF] Solar Absorptivity of the Cube Corner Reflectors (CCRs) = \u03b1s"]
-[10.898698806762695, 7.5346245765686035, "[TT] Swath Width of the AVNIR = 80 km"]
-[8.73025894165039, 7.29824686050415, "[TT] Body-Pointing Capability of the Pushbroom Imager = \u00b140\u00ba into the along-track and cross-track directions"]
-[8.529930114746094, 7.444774150848389, "[TT] Detection Limit at 13 \u00b5m of the Instrument = 1 x 10 -4"]
-[3.786461353302002, 7.154716491699219, "[TT] Gain of the Onboard Antenna = 13.5 dBi"]
-[6.297881126403809, 4.528162479400635, "[FF] Function of the CMART = Manage the configuration of software builds, licenses, and database schema"]
-[4.983685493469238, 1.8383005857467651, "[FF] URL of the Gokturk-2 = http://www.airforce-technology.com/projects/-gktrk-2-earth-observation-satellite/"]
-[4.358548164367676, 1.361324429512024, "[FF] Security System of the SEOSat/Ingenio = SEOSat/Ingenio Security System"]
-[9.430171966552734, 7.0420756340026855, "[TT] Spatial Resolution of the MSU-100 = 60 m"]
-[3.815473794937134, 4.316194534301758, "[FF] Purpose of the PAZ = Produces radar imagery of the Earth for government and commercial use, as well as ship tracking and weather sensors, enabling high-resolution mapping of large geographical areas"]
-[3.186850070953369, 2.2532060146331787, "[FF] Purpose of the Copernicus Programme = Monitor and collect information across different parts of the Earth"]
-[7.967962265014648, 1.0631170272827148, "[TT] Eruption Date of the Calbuco volcano = April 22, 2015"]
-[6.823894500732422, 1.9554071426391602, "[FF] URL of the SCARLET Advanced Array = http://nmp.nasa.gov/ds1/tech/scarlet.html"]
-[5.037117004394531, 0.7519465088844299, "[TT] Date of the MC3E = April 15 -June 1, 2011"]
-[4.158192157745361, 5.782952308654785, "[TT] Signal Type of the SDR = ADS-B (Automatic Dependent Surveillance-Broadcast) signals"]
-[7.915900707244873, 7.276074409484863, "[TT] Raw Video Data Bandwidth of the Camera = 12.5 Gbit/s"]
-[9.594353675842285, 7.126612186431885, "[TT] Spatial Resolution of the MUX = 16 m"]
-[11.444833755493164, 6.5355682373046875, "[FF] Observable Particle of the Particle Detector = Proton, deuteron, tritium, helium"]
-[11.238160133361816, 0.9648321866989136, "[TT] Extended Mission Start Date of the LISA Pathfinder = 1 November"]
-[10.292594909667969, 4.53685998916626, "[TT] Torque of the Honeywell 25 Nms reaction wheels = 25 Nms"]
-[10.636866569519043, 5.378871917724609, "[TT] Concentration Ratio of the SAC = 3:1"]
-[9.978715896606445, 7.984307289123535, "[TT] Distance to Focal Plane of the M5 = 10 \u00b5m"]
-[9.557921409606934, 7.109002590179443, "[TT] Spatial Resolution of the WFC = 1 km"]
-[5.034158229827881, 3.4827823638916016, "[TT] Manufacturer of the CHIPSat = SpaceDev, Inc."]
-[5.192018032073975, 7.108157634735107, "[TT] Command Uplink Speed of the CXS-810C = 2 kbit/s"]
-[5.434816360473633, 6.434027194976807, "[TT] Capacity of the Onboard Mass Data Storage = 24 GByte"]
-[3.3281190395355225, 6.095327377319336, "[TT] Antenna Size of the Radar Instrument = 11 m by 3.6 m"]
-[5.6400146484375, 0.6333948969841003, "[FF] Data Capture Date of the NuSTAR = February 19, 2014"]
-[6.9231390953063965, -0.5541171431541443, "[TT] Orbit Period of the VesselSat-1 = ~ 102 minutes"]
-[10.273404121398926, 1.6853249073028564, "[FF] Source Types of the eROSITA = Active galactic nuclei, accreting supermassive black holes, clusters of galaxies, stars with strong, magnetically active hot coronae, X-ray binary stars containing neutron stars, black holes or white dwarves, and spectacular supernova remnants"]
-[10.19918155670166, 4.16706657409668, "[TT] Stabilization of the \u00d8rsted = Gravity gradient boom and active magnetic torquing"]
-[6.324341297149658, 8.095690727233887, "[TT] Channels of the GOLD = 2"]
-[7.363912582397461, 0.2663033902645111, "[FF] Sample Stowage of the OSIRIS-REx = Originally scheduled for Nov. 2"]
-[18.665813446044922, 3.93550443649292, "[TT] NE\u0394T (K) of the ICI-8 = 1.3"]
-[9.537191390991211, 4.7420854568481445, "[TT] Attitude Control System of the LEOStar-2 bus = Three-axis controlled, zero-momentum"]
-[6.112853527069092, 1.9647605419158936, "[TT] Test Flight of the Orion = Artemis I"]
-[5.159420967102051, 2.398911952972412, "[TT] Mission Type of the Oculus-ASR = Non-EO"]
-[4.872129917144775, 0.5767815113067627, "[FF] Launch Provider Announcement Date of the TEMPO = 18 March 2020"]
-[4.730860710144043, 7.112419605255127, "[TT] Mission Data Downlink of the QSat = Ku-band, 30 Mbit/s"]
-[6.194845676422119, 2.2709250450134277, "[TT] Principal Investigator of the IMPACT = Janet G. Luhmann"]
-[5.131885051727295, -0.019465114921331406, "[FF] Final Report Date of the STRV-1A and -1B = August 1995"]
-[2.02182674407959, -0.3332831561565399, "[FF] Purpose of the Van Allen Probes = Investigating Earth's radiation belts"]
-[10.317583084106445, 4.516178131103516, "[TT] Manufacturer of the Reaction Wheel = AstroFein (Astro und Feinwerktechnik Adlershof GmbH,)"]
-[5.9650444984436035, 2.2768752574920654, "[TT] Mission of the Orion MPCV = EM-1 (Exploration Mission-One)"]
-[8.42143726348877, 5.8977580070495605, "[FF] Absolute Accuracy of the Instrument = 1 K (1 sigma)"]
-[1.361946940422058, 2.7836787700653076, "[TT] Principal Absorbing Constituents of the Band 5 = CO2"]
-[10.251924514770508, 4.534823894500732, "[FF] Phases 2 and 8 Activity of the S/C = Roll flip and a roll flip back"]
-[7.650193214416504, 9.027715682983398, "[TT] Dynamic Range of the Band 1 = Approximately 107"]
-[2.919509172439575, 1.9769734144210815, "[TT] Image Capture Date of the Copernicus Sentinel-3 = 3 January"]
-[8.99117660522461, 10.257307052612305, "[TT] Pixel Resolution of the SPIM4 = 14 bit"]
-[8.284529685974121, 5.002418518066406, "[FF] Calibration Uncertainty of the E2E simulation = Unknown"]
-[9.554652214050293, 0.621285617351532, "[TT] Communication Range of the SATTLA-2 = Over 600 km"]
-[6.340176582336426, 2.5253803730010986, "[FF] Inspection Areas of the EFT-1 Orion = Back shell thermal protection system tiles, back shell thermal barriers, reaction control system thruster nozzles, base heat shield acreage, docking hatch thermal protection system blankets, docking hatch window, and crew module windows"]
-[4.972329616546631, -0.007152522448450327, "[TT] Launch Date of the Kleos Patrol Mission (KSF2) = April 2022"]
-[3.2508351802825928, 2.2096264362335205, "[FF] Design Approach of the Sentinel FOS = Extensive re-use of elements developed in the context of previous Earth Observation ground segments"]
-[9.381438255310059, 5.030092716217041, "[TT] Attitude Variation During Docking Operations of the ISS = Several degrees"]
-[4.516226768493652, 3.813868284225464, "[TT] Number of Batch 3 Satellites of the Galileo = 12"]
-[5.855113506317139, -0.7684365510940552, "[TT] Build Cycle of the Legion spacecraft = 24-36 months"]
-[7.924200534820557, 8.877009391784668, "[TT] Wavelength Range of the SSULI = 80 - 170 nm"]
-[7.57063627243042, 5.779026031494141, "[FF] Bias Histograms of the MWR = Zero mean and of Gaussian shape"]
-[4.3283772468566895, 0.3667753338813782, "[TT] Launch Date of the JL-1-GF03B = 15 September 2020"]
-[13.728968620300293, 2.925386428833008, "[TT] Total Mass of the Spacecraft = 25.5 kg"]
-[5.006914138793945, 3.501450777053833, "[TT] Manufacturer of the Stamp9G20 = Taskit"]
-[7.9774861335754395, 7.268244743347168, "[TT] Readout Capability of the CCD Array = 12 bit full-frame at up to 120 frames/s"]
-[4.384264945983887, 0.9593280553817749, "[TT] Number of Launches of the Arianespace = Fourth launch of the year"]
-[7.998888969421387, 7.411956787109375, "[TT] Type of the Hyperspectral imagers = Hyperspectral imagers"]
-[9.127952575683594, 6.837954044342041, "[FF] Lava Area of the Image = Roughly 10 km2"]
-[5.406447410583496, 4.192831516265869, "[TT] Bus Type of the GF-2 = CAST-CS-L3000A"]
-[5.737702369689941, -0.9676451683044434, "[TT] Design Life of the SORCE = 5 years"]
-[14.631234169006348, 6.699378490447998, "[TT] Li-ion Battery Capacity of the EPS = 30 Ah"]
-[12.087299346923828, 3.2789783477783203, "[TT] Fuel System of the XMM = Specially designed tank fuel system"]
-[4.609328269958496, 2.944472074508667, "[FF] Regional Hubs of the SERVIR = CATHALAC in Panama, RCMRD in Nairobi, ICIMOD in Kathmandu"]
-[1.3162606954574585, 1.899133324623108, "[TT] Transportation Capacity of the HTV-9 = World's largest"]
-[8.519149780273438, 2.069460868835449, "[FF] Measurement of the NASA\u2019s Scatterometer (NSCAT) = Wind speeds over bodies of water"]
-[9.409940719604492, 5.670444011688232, "[TT] View Angle Range of the TanSat = -60\u00b0 to 60\u00b0"]
-[11.88991928100586, -0.1360889971256256, "[FF] URL of the TESS = https://www.nasa.gov/feature/goddard/2021/nasa-s-tess-discovers-stellar-siblings-host-teenage-exoplanets"]
-[6.501516819000244, 5.596660614013672, "[FF] Conference Location of the CubeSat Laser Communication Crosslink Pointing Demonstration = Logan, UT, USA"]
-[9.48717212677002, 6.98796272277832, "[TT] Resolution of the Kuzgun = 20 m"]
-[7.918479919433594, 4.486136436462402, "[FF] In-Orbit Calibration Types of the MIRAS = External, internal"]
-[5.991601943969727, 7.217440128326416, "[TT] Data rate of the Spectrometer = 1.5 Mbit/s (average), 1.5 Mbit/s (max)"]
-[9.342658996582031, 6.232875347137451, "[TT] Scanning Type of the MTVZA-GY = Conical"]
-[6.058568477630615, 3.9912891387939453, "[TT] Architecture of the AstroBus-L = Modular with a standard mission and hardware independent core"]
-[12.204207420349121, 0.5784553289413452, "[FF] Science Goals of the PLATO = Explore the conditions for planet formation and the emergence of life, the solar system origin and its behavior, fundamental physics of the universe, its origin and composition"]
-[8.2213716506958, 8.71708869934082, "[TT] Spectral Sampling Distance of the VIS = 0.21 nm"]
-[10.283753395080566, 4.541030406951904, "[TT] Quantity of the ADCS = 100-SP(O) wheels"]
-[5.101060390472412, 0.6356386542320251, "[TT] Launch Date of the CanX-6/NTS = Apr. 28, 2008"]
-[7.658639430999756, 0.2489277869462967, "[TT] Launch Date of the Lucy = January 31, 2019"]
-[9.712751388549805, -0.35948899388313293, "[TT] Longitude of the Meteosat-7 = 57.5 \u00b0E"]
-[9.879721641540527, 0.23644888401031494, "[FF] Orbit of the Herschel Telescope = Large Lissajous orbit around the L2 point at a distance of around 1.5 million km from Earth"]
-[5.765366554260254, 5.782467365264893, "[FF] Data Downlink of the ISERV = Via TDRSS"]
-[9.606258392333984, 7.062196731567383, "[TT] Image Footprint of the HyperScout = Approximately 200 x 150 km2"]
-[8.278695106506348, 2.444845199584961, "[FF] Challenges of the LCRD = Susceptibility to cloud cover, scintillation, scattering and other atmospheric effects"]
-[5.905049800872803, -0.8564086556434631, "[TT] Condition of the Genesis spacecraft collectors = Excellent"]
-[3.4370269775390625, 6.341923236846924, "[TT] Dimensions of the Active Antenna Panels = 2.2m x 3.6m"]
-[5.515083312988281, 4.744777679443359, "[FF] LRIT and HRIT Broadcasting Service of the GK2A satellite = L-band"]
-[5.231247425079346, 2.71490478515625, "[TT] Development Center of the GeoXO = NASA's Goddard Space Flight Center in Greenbelt, Maryland"]
-[9.56721019744873, 9.034610748291016, "[TT] Velocity Resolution of the IRIS = 0.4 km/s"]
-[7.992833137512207, 2.7039692401885986, "[FF] Data Products of the Sentinel-4 = Ozone total column and tropospheric sub-column, nitrogen dioxide total column and tropospheric sub-column, sulphur dioxide total column, formaldehyde total column, glyoxal total column, cloud optical thickness, fraction and altitude, aerosol column thickness, type, layer height, and absorbing index and surface and aerosol characteristics"]
-[8.721277236938477, 1.847456455230713, "[TT] Wind Speeds of the Hurricane Models = Up to category 5 strength"]
-[11.850786209106445, 5.425490856170654, "[TT] Size of the Instrument = Microwave oven"]
-[12.00863265991211, 4.764133453369141, "[TT] Dimensions of the Namuru V3.2 GPS Receiver = 82 \u00d7 82 mm"]
-[8.82995319366455, 7.655045509338379, "[TT] Photodetector Resolution of the Optical Head = 1280 x 1024 pixels"]
-[9.633722305297852, 7.104633808135986, "[TT] Mean Spatial Resolution of the IMI = 15~50 km 4~50 km 2~5 km"]
-[8.636453628540039, 4.724664211273193, "[TT] Quantity of the Star Tracker (STR) = 3"]
-[8.918889999389648, 3.947477340698242, "[FF] Measurement Locations of the IMPACT = Two STEREO spacecraft locations"]
-[9.459420204162598, 5.640676975250244, "[TT] Maximum Azimuth Slewing Rate of the OCTL = 20\u00ba/s"]
-[6.272080898284912, -0.3632049262523651, "[TT] Duration of the CALET = Two to five years"]
-[3.8625473976135254, 1.1485859155654907, "[TT] Falcon Rocket Landings of the SpaceX = 75"]
-[13.867785453796387, 7.246109485626221, "[TT] Power Generation of the IRIS = 28 V"]
-[3.9638512134552, 4.340152263641357, "[FF] System Specifications of the RISAT-1A = Virtually the same as those of RISAT-1"]
-[7.820504188537598, 8.636056900024414, "[FF] Spectral Index of the AMS = Varies"]
-[7.190194606781006, 1.8395001888275146, "[FF] Function of the bioCDs = Integrate the sensors that allow for real-time measurement of calcium signaling"]
-[2.97023868560791, 4.496501922607422, "[TT] ScanSAR Mode Spatial Resolution of the PALSAR-2 = 60 m"]
-[8.947760581970215, 4.395833969116211, "[TT] Sun Sensors of the DSX = 3"]
-[8.786270141601562, 4.571369171142578, "[FF] Sensor Subsystems of the SEEDS-2 = 3-axis geomagnetic sensors, 3-axis gyro sensors, temperature sensors, solar battery cell galvanometers, and voltage sensors"]
-[6.927990913391113, 4.130186080932617, "[FF] Design Evolution of the ASPIICS = Not provided"]
-[4.730640888214111, -1.2153323888778687, "[TT] Launch Date of the Beijing-3A = 11 June 2021"]
-[9.35385513305664, -0.44865682721138, "[TT] Apogee Altitude of the STRV-1a = 35,818 km"]
-[4.875107765197754, 8.285941123962402, "[TT] Centre Frequency Range of the AMSR = 6.925 - 89.0 GHz"]
-[5.07221794128418, 1.9256579875946045, "[FF] Type of the CARMEN-1 = Unknown"]
-[5.075935363769531, 6.338006973266602, "[TT] Mass of the Spacecraft 406 MHz Processor = 27.5 kg"]
-[11.116809844970703, 6.013010025024414, "[TT] Material of the Electrodes = Dielectric material (resin-glass)"]
-[7.707948684692383, 2.369112968444824, "[TT] Data Coverage of the AMSU = Up to 50 km"]
-[9.197546005249023, 3.1489739418029785, "[FF] Scientific Objectives of the ASPIICS = Understand the physical processes that govern the quiescent solar corona and determine space weather"]
-[12.449856758117676, 0.6329683661460876, "[TT] Image Acquisition Frequency of the Plato Camera = Every 25 seconds"]
-[4.97518253326416, 3.4493801593780518, "[TT] Developer of the OMU = Acer Inc."]
-[11.820894241333008, 3.297358512878418, "[TT] Configuration of the Propulsion System = ESPA and T2E-compatible"]
-[10.284652709960938, 1.792328953742981, "[FF] Observation Plan of the eROSITA = Discover many X-ray sources, including double stars and the remains of stellar explosions (supernovae). Rare objects such as isolated neutron stars"]
-[6.583350658416748, 5.458566188812256, "[FF] Quantity of the LPT = 1"]
-[1.3161826133728027, 1.8990627527236938, "[TT] PLC Cargo of the HTV-7 = 4.3 metric tons"]
-[6.322520732879639, -1.3189964294433594, "[TT] Operation Start Date of the GRACE = March 2002"]
-[13.421896934509277, 2.976682424545288, "[TT] Mass of the NorSat-2 = 16 kg"]
-[10.81997299194336, 2.1139585971832275, "[TT] Cataloged X-ray Sources of the XMM-Newton = 71,951"]
-[6.856793403625488, 3.1657304763793945, "[TT] Planned Number of Satellites of the GHGSat = >10"]
-[9.618247032165527, -0.45247629284858704, "[TT] Altitude of the ALOS-2 = 628 km"]
-[9.192782402038574, 4.852818965911865, "[FF] Anomaly of the EAIM = Occurred on the wheels command of satellite attitude control"]
-[9.193300247192383, 3.177706718444824, "[FF] Measurement of the SWAP = Interactions of Pluto with the solar wind"]
-[5.183494567871094, 5.870021820068359, "[FF] Type of the SpaceWire bus = High-speed"]
-[7.995451927185059, 5.152654647827148, "[FF] Mechanical Tests of the Biomass = Sine vibration, acoustic, shock and clamp-band release tests"]
-[14.256946563720703, 3.270209789276123, "[TT] Mass of the MEPSI = < 1 kg"]
-[7.964510917663574, 8.587599754333496, "[TT] Spectral Range of the TIR = 2.15-2.25 \u00b5m"]
-[9.71158218383789, 7.623255252838135, "[TT] Observation Field Tilt Capability of the AVNIR = \u00b140\u00ba"]
-[4.794325828552246, 0.45298561453819275, "[TT] Launch Date of the LCT = Q2 2013"]
-[7.147313117980957, 2.108154773712158, "[FF] Image Type of the Image = 360\u00b0 colored image of the Milky Way"]
-[6.986494064331055, 4.109258651733398, "[TT] Power Subsystem of the DMSP-19 = More capable"]
-[8.433172225952148, 6.8913655281066895, "[TT] Imaging Mode of the Stereo Camera = Pushbroom"]
-[13.299736976623535, 7.157375335693359, "[TT] Power of the Average Payload = < 100 W"]
-[6.556187629699707, 6.37736177444458, "[FF] Delayed TM Playbacks of the Telemetry = Five complete during the visibility window"]
-[10.20976734161377, 1.5475324392318726, "[TT] Number Found in Other Galaxies of the ULXs = About 500"]
-[4.529284477233887, 1.2417680025100708, "[TT] Design Life of the ALSAT-2B = 5 years"]
-[8.57850456237793, 5.567403316497803, "[TT] Roll Phase Error of the GP-B satellite = 0.13 mrad RMS"]
-[9.815526008605957, -0.5047788619995117, "[TT] Orbit Altitude of the KSM-1 satellites = 500 km"]
-[8.021573066711426, 4.843340873718262, "[FF] Design Hypothesis of the Geometric Calibration System = Change across the swath can be modelled with 8th order polynomials"]
-[14.094395637512207, 7.166963577270508, "[TT] Nominal Voltage Range of the ArgUS = 28 V \u00b1 2 V"]
-[4.20046854019165, 5.422980308532715, "[TT] Communication of the CAPSTONE = Two-way, coherent range and Doppler measurements"]
-[4.278137683868408, 7.499871253967285, "[TT] Main Mode Frequency of the MRSE = X-band (9.6 GHz)"]
-[8.270334243774414, 0.08276015520095825, "[TT] El Ni\u00f1o Anomaly of the TOPEX/Poseidon = More than 20 cm"]
-[8.111397743225098, -0.958619236946106, "[TT] Pass Separation of the ICESat-2 = About a half-mile"]
-[14.246176719665527, 3.218292474746704, "[TT] Mass of the CXBN = 2.8 kg"]
-[8.608176231384277, 1.271600365638733, "[TT] Measurement Depth of the Aquarius = Top 5 cm of the land"]
-[8.240015029907227, 2.6657052040100098, "[TT] Measurement Domain of the Resurs-DK1 = Land, Gravity and Magnetic Fields"]
-[11.794576644897461, 6.7441511154174805, "[TT] Energy Range of the SEDA = Protons: 15 MeV \u2013 100 MeV, Electrons : 0.2 MeV \u2013 5 MeV"]
-[13.598475456237793, 5.779452323913574, "[TT] Power Source of the Rosetta = Solar cells"]
-[5.974606513977051, 4.851282119750977, "[FF] Message Bus Function of the MCS = Provides a publish/subscribe mechanism"]
-[10.433730125427246, 6.890091419219971, "[TT] Receive Aperture Radius of the Triple Mirror = 4 mm"]
-[13.04673957824707, 7.0833001136779785, "[TT] TC/TM Power Requirement of the WCOM = 25 W"]
-[9.973511695861816, 4.696690559387207, "[TT] Motor Step Angle of the SADM = 1.5\u00ba"]
-[8.368208885192871, 3.1588222980499268, "[FF] Objective of the OMPS = Measure the total amount of ozone in the atmosphere and the ozone concentration variation with altitude"]
-[6.973326206207275, 4.700595378875732, "[FF] Unknown of the DM of power controller = Unknown"]
-[5.174290180206299, 0.48995503783226013, "[TT] Launch Date of the Juno = Aug. 5, 2011"]
-[4.281994342803955, 7.157578945159912, "[FF] Radiation Pattern of the Ka-band payload = Modified to distribute higher power at angles \u00b1 50\u00ba from boresight"]
-[9.502816200256348, 4.06428337097168, "[FF] Type of the Space Magnetometer = Anisotropic magnetoresistive hybrid sensor"]
-[5.684264659881592, 6.984475135803223, "[TT] Data Stream Rate of the DPU = 1800 Mbit/s"]
-[11.90866470336914, 3.343379497528076, "[TT] Propulsion System Performance of the Advanced Composition Explorer = Nominally for the first 16 years of the mission"]
-[10.045816421508789, -1.5425461530685425, "[TT] Orbit Inclination of the P35 series = 98.5\u00ba"]
-[9.414562225341797, 7.6529717445373535, "[TT] Requirement Value of the GSD = 0.7 m(PAN), 2.8 m(MS)"]
-[7.607541561126709, -0.8646746277809143, "[TT] Mission Start Year of the ICESat-2 = 2003"]
-[13.530112266540527, 3.3081085681915283, "[FF] Mass of the AeroCube-6 = 1U"]
-[3.3560116291046143, 1.4497566223144531, "[TT] Launch Date of the Sentinel-2C and -2D = 2020/2021"]
-[12.135149002075195, 6.150251388549805, "[TT] Cosmic-Ray Hits of the AMS-02 = ~10,000 hits per minute"]
-[5.36458158493042, 0.737186849117279, "[TT] Arrival Date at Wallops Flight Facility of the LADEE = June 2013"]
-[10.139315605163574, 10.002850532531738, "[TT] Launch Date of the Vega = 29 April 2021"]
-[9.071110725402832, 5.40984582901001, "[TT] S/C Pointing of the Spacecraft = 1.0\u00ba, 1.0\u00ba"]
-[7.81941032409668, 6.262929439544678, "[FF] Measurement Method of the LOLA = Pulse waveform integration"]
-[8.173990249633789, 3.2047359943389893, "[FF] Required Climate Record of the Infrared Spectrometer = 20 years for a 95% confidence level of 0.1 K/decade"]
-[2.833465337753296, 0.08774954080581665, "[TT] J2000 right ascension (deg) of the B1758-250 = 270.284"]
-[5.845615386962891, 4.93562650680542, "[FF] Methods of Communication of the MCS = Point-to-point client-server communication and communication on a message bus"]
-[5.6822919845581055, 3.7241830825805664, "[TT] Constellation Size of the Kleos Space S.A. = Up to 20 clusters"]
-[5.960517883300781, 4.822977542877197, "[FF] Telemetry Submission Method of the GeneSat-1 = Web site"]
-[3.451857328414917, -0.9096986651420593, "[TT] Orbit Type of the Shakuntala = Sun-synchronous"]
-[5.9108991622924805, 2.9235496520996094, "[TT] Mission Number of the Swarm = 4th"]
-[7.76364278793335, 5.748899936676025, "[FF] Instrument Type of the GLI = Imaging multi-spectral radiometers (passive microwave)"]
-[6.770644664764404, 1.0498266220092773, "[FF] Date of the Super Typhoon Rai = 18 December 2021"]
-[4.851851463317871, 7.234737396240234, "[TT] Data Download Capacity of the EWC27 HDR-TM X-band transmitter = Up to 17 GB/day"]
-[13.35139274597168, 7.247608661651611, "[TT] Average Power of the S/C Power = 171 W"]
-[10.285162925720215, 6.235749244689941, "[TT] Sensitivity of the NuSTAR = More than 100 times greater than previous missions"]
-[4.660694599151611, 6.876755714416504, "[TT] Ground Station-pointing Mode Downlink Data Rate of the S-band system = Up to 204 MB/day"]
-[4.9073991775512695, 6.922447204589844, "[TT] Number of RF Hybrids of the TTDL = 3"]
-[13.810835838317871, 2.697387218475342, "[TT] Launch Mass of the Helios-2A = 4200 kg"]
-[6.004936218261719, 1.5261136293411255, "[FF] Collaboration Invitation Date of the SWOT = 2 January 2019"]
-[3.1188106536865234, 2.19732403755188, "[TT] Data Sources of the Green City Watch = Copernicus Sentinel-2 mission, Sentinel-1 SAR imagery, SkySat and RapidEye"]
-[8.368507385253906, 4.609457492828369, "[FF] Function of the Optical Telescopes = Determine the trajectory of an orbiting object, determine the object's attitude, physical profile, and features"]
-[11.596728324890137, 4.595597267150879, "[FF] Shape of the DMSP Block 4 = Spin-stabilized octagon"]
-[5.9551682472229, 0.20480570197105408, "[TT] Arrival Date of the Juice = 2029"]
-[6.940330982208252, 3.097383975982666, "[FF] Based on of the Ground data management system = FY (Feng Yun) satellite series of China"]
-[9.08102035522461, 3.483905553817749, "[FF] Solar Environment of the SPC (Solar Probe Cup) = More severe than all previous experience"]
-[5.867690086364746, 3.3358969688415527, "[TT] Cost per Flight of the Super Strypi = $15 million"]
-[6.112244606018066, 0.38620245456695557, "[FF] Hold Period of the RISESAT = True"]
-[6.092111587524414, 2.17295503616333, "[FF] Participating Countries of the Euclid Mission Consortium = Italy, France, Germany, Denmark, Portugal, Spain, The Netherlands, Norway, Romania, United Kingdom, Finland"]
-[9.858436584472656, 7.107724189758301, "[TT] Ground Resolution of the Scanner Assembly = 1 km"]
-[5.948085308074951, 1.9957218170166016, "[FF] Contact Email of the eoPortal = eoportal@symbios.space"]
-[4.148285388946533, 1.4118767976760864, "[TT] Launch Date of the Meteosat-7 = September 1997"]
-[13.218521118164062, 5.475147247314453, "[TT] Deployment of the Solar Array = Included in Launch and early operations"]
-[4.2059173583984375, 1.8415950536727905, "[TT] Orbit Estimator of the NigeriaSat-2 = Recursive orbit estimator"]
-[10.91047477722168, 10.088521957397461, "[FF] Team Composition of the Alpha Magnetic Spectrometer (AMS-02) = 600 physicists and 56 institutes and organizations from 16 countries"]
-[9.600525856018066, 7.095248222351074, "[TT] Spatial Resolution of the PMI = 10 x 6 km"]
-[4.654688358306885, 1.576293706893921, "[FF] Presentation Date of the GCOM-W1 = June 5-12, 2011"]
-[8.028257369995117, 7.208339214324951, "[TT] Frame Rate of the Supervision Cameras = 10 frames/s"]
-[7.021296977996826, 7.085495948791504, "[TT] Output Power of the Laser = 1.5 W"]
-[11.736503601074219, 4.917850017547607, "[TT] Transverse Dimensions of the HXT-C = 417 mm x 376 mm"]
-[5.736991882324219, -0.9093981981277466, "[TT] Design Life of the BIRD = 1 year"]
-[5.778903007507324, 7.122698783874512, "[TT] Data Rate of the TT&C Data = 32 kbit/s"]
-[13.318602561950684, 7.417715549468994, "[TT] TWTA Output Power of the TWTA = Nominal operation: 50 W (MPA operation in linear range)"]
-[11.423644065856934, 2.164938449859619, "[TT] \u0394V (cm/s) of the Cosmos 2251 Debris = 0.67"]
-[5.6690826416015625, 0.6753854155540466, "[FF] - of the True of date frame = -"]
-[13.27739429473877, 2.90549898147583, "[TT] Weight of the MethaneSAT = 350 kg"]
-[8.33561897277832, 7.719851016998291, "[TT] Detector of the Spectral Band C = Si-PIN"]
-[7.579465389251709, 3.45491623878479, "[FF] Presentation Title of the J.-C. Liou = USA Space Debris Environment, Operations, and Measurement Updates"]
-[10.938863754272461, 7.544057846069336, "[TT] Swath Width of the COSI = 5 km"]
-[5.931540489196777, 1.2674016952514648, "[TT] Launch Date of the Carruthers Geocorona Observatory (GLIDE) = 2025"]
-[8.938185691833496, 5.749929904937744, "[TT] Pointing Accuracy of the ADCS = 648 arcsec"]
-[4.187801837921143, 1.8561240434646606, "[TT] On-Orbit Life of the NigeriaSat-2 = 5th year"]
-[7.653487682342529, -0.7135933041572571, "[TT] URL of the ICESat\u20102 = https://doi.org/10.1029/2019JC016008"]
-[12.491518020629883, 6.660325050354004, "[TT] Dimensions of the Proton Monitor Las Dos Torres = 180 mm length, 130 mm width, and a maximum height of 56 mm"]
-[8.442627906799316, 1.7061976194381714, "[TT] Uncertainty of the Sea Surface Temperature (SST) = <0.3 K"]
-[5.2163801193237305, 1.5103228092193604, "[FF] On-Orbit Verification Mission of the TET-1 = IAC 2013"]
-[4.757188320159912, 3.8902382850646973, "[TT] Availability of the European Ground Motion Service = Public"]
-[10.275558471679688, 4.056635856628418, "[TT] Secondary Objective of the SSM-Boom = Source 1"]
-[4.033246040344238, 3.483001470565796, "[FF] URL of the Galileo = http://m.esa.int/Our_Activities/Space_Engineering_Technology/Combined_orbital_Galileo-GPS_position_fix_achieved_aboard_ISS"]
-[10.401076316833496, 1.616597056388855, "[FF] Cause of the ULXs = Object with strong gravity accreting gas from a companion star"]
-[4.477982044219971, 5.493590354919434, "[FF] Mission Purpose of the GomX-1 = Demonstrate Improved Situational Awareness for Air Traffic Control"]
-[6.668547630310059, 2.7902910709381104, "[FF] Mission Type of the CO2M = Two-satellite mission, with the option of a third satellite"]
-[4.125113487243652, 1.0885848999023438, "[FF] Undock Date of the H-II Transfer Vehicle \"KOUNOTORI3\" (HTV3) = Sept. 17, 2012"]
-[3.091278076171875, -0.06679107248783112, "[TT] Orbital Slot of the GSAT-0204 = B03"]
-[11.761488914489746, 3.2439937591552734, "[TT] Number of Orbit Control Thrusters of the GN2 Reaction Control System = 2"]
-[9.477760314941406, 4.957613468170166, "[TT] Stability of the Attitude Control = \u22640.005\u00ba/s"]
-[6.365303993225098, -0.13912220299243927, "[FF] Actual Orbit Duration of the Skylab-1 = Prematurely decayed"]
-[6.806119441986084, 3.957247018814087, "[FF] Quake Duration of the SEIS = Unknown"]
-[7.894571304321289, 6.700016021728516, "[TT] Instrument Type of the AaSI = Fabry-P\u00e9rot Interferometer (FPI)"]
-[14.118939399719238, 7.179823875427246, "[TT] Voltage of the Voltage 1 = 22-28 adjustable"]
-[7.681323051452637, -0.8855597972869873, "[TT] Aliveness Tests Completion of the ICESat-2 = End of July"]
-[8.332778930664062, 5.570206642150879, "[FF] Objective of the CVE = Calibration of the COSI payload and maintaining its long-term system performance"]
-[13.700318336486816, 3.0822455883026123, "[TT] Mass of the GOMS-1 = 2580 kg"]
-[14.251752853393555, 3.1354973316192627, "[TT] Mass of the ROLIS = 1.4 kg"]
-[7.9937744140625, 8.978809356689453, "[TT] Wavelength Range of the SUSIM = 110 to 410 nm"]
-[8.863951683044434, 5.652406215667725, "[TT] Pointing Accuracy of the APM = Better than 0.1\u00ba"]
-[4.468601703643799, 7.705938816070557, "[TT] Bandwidth of the Uplink (VHF) = 16 MHz"]
-[7.060130596160889, 1.3660670518875122, "[FF] Science Operations Location of the Spitzer Space Telescope = Spitzer Science Center at IPAC at Caltech"]
-[3.1278882026672363, 3.9229514598846436, "[FF] Authors of the NISAR = Paul Rosen, Yunjin Kim, Howard Eisen, Scott Shaffer, Louise Veilleux, Scott Hensley, Manab Chakraborty, Tapan Misra, R. Satish, Deepak Putrevu, Rakesh Bhan"]
-[11.5884428024292, 3.1695098876953125, "[TT] Orbit Maneuver Support of the INSAT-2A/2B = Integral apogee boost motor"]
-[6.199629783630371, 8.598733901977539, "[TT] Polarization of the Radar = Single / dual / full / compact"]
-[3.2919609546661377, 5.80305290222168, "[TT] Tile Size of the SAR antenna subsystem = 1 m x 1 m"]
-[3.784973621368408, -1.20842444896698, "[TT] Orbit of the SRG = L2 (Lagrangian Point 2)"]
-[11.5548095703125, 4.819839000701904, "[TT] Diameter of the SHIROP = 20 cm"]
-[5.130663871765137, 2.002840757369995, "[TT] Mission Status of the DMC-3 = Operational (nominal)"]
-[4.153094291687012, 0.6659718751907349, "[TT] Operations Manager of the Integral = Richard Southworth"]
-[4.875973701477051, 7.2763543128967285, "[TT] Data Downlink Speed of the RF Communications = > 100 Mbit/s"]
-[11.862283706665039, 4.81746768951416, "[TT] Dimensions of the DECA = about 9 cm x 9 cm x 9 cm"]
-[7.682948112487793, -0.8237273693084717, "[FF] Campaign Team of the ICESat-2 = Four-person team"]
-[8.586774826049805, 6.696224689483643, "[FF] Observation Geometry of the MOMS-02 = Stereo Triplets"]
-[8.500442504882812, 6.726781368255615, "[FF] Capability of the TDI Feature = Low-light observations of imagery"]
-[10.467395782470703, 5.467560768127441, "[TT] Heat Shield Type of the Skylab = Temporary parasol-type"]
-[11.808999061584473, 0.07331066578626633, "[FF] Purpose of the TESS = Hunts for exoplanets and studies stellar oscillations"]
-[8.92020320892334, 4.571996212005615, "[TT] Pointing Modes of the AlSat-2A = Sun pointing (heliocentric pointing) or toward Earth (geocentric pointing)"]
-[12.017740249633789, 0.581345796585083, "[TT] Observation Method of the Plato = Looking for regular dips in starlight caused by the transit of a planet across the star\u2019s disc"]
-[10.03830623626709, 1.6132248640060425, "[TT] Bubble Size of the eROSITA = Several kiloparsecs (or up 50,000 light-years) across"]
-[5.437560558319092, 0.1865481585264206, "[TT] Possible Extension of the SAMPEX = One year"]
-[7.116910457611084, 6.632411003112793, "[FF] Detection Efficiency of the GLM = Maximize"]
-[5.896435737609863, 4.472806453704834, "[FF] Functionality of the Bidirectional IoT = Send commands back to assets"]
-[5.596543788909912, 0.48253950476646423, "[FF] Deployment of the Flock-4v = ISL\u2019s QuadPack deployers and D-Orbit\u2019s InOrbit Now (ION) free-flying deployment platform"]
-[5.2775559425354, 0.9180522561073303, "[FF] Meeting Date of the BioSentinel = 2-3 September 2-3 2015"]
-[3.9165871143341064, 2.0255486965179443, "[TT] Launch Vehicle of the RADARSAT-2 = Soyuz"]
-[13.32521915435791, 7.426642417907715, "[TT] Power of the DC Power = 1.0 W conditioned power (standby)"]
-[5.4932780265808105, 3.887688159942627, "[TT] Goal for Number of Satellites by 2025 of the Satellogic = 200 or more"]
-[8.715438842773438, 2.222022294998169, "[FF] Altitude Range of the Nitric Oxide VMR = 80 - 120 km"]
-[3.5582239627838135, 5.128004550933838, "[TT] X-band of the Multimode radar = Spatial resolution from 1 to 500 m"]
-[6.032522201538086, 4.680145740509033, "[FF] Operational Modes of the Ground Station = Command and Control (C2) and UGS (Unattended Ground Sensor)"]
-[6.667429447174072, 5.868003845214844, "[TT] Quantity of the OBC = 1"]
-[12.186331748962402, 4.670840263366699, "[TT] Dimensions of the Corvus-XL bus = 52.4 cm by 52.4 cm by 62 cm"]
-[9.265355110168457, 5.057440280914307, "[TT] Attitude Control Accuracy of the GFO = 0.25\u00ba (3\u03c3)"]
-[6.228409290313721, 5.056687355041504, "[FF] Interface Specification of the QZSS = http://qzss.jaxa.jp/is-qzss/index_e.html"]
-[4.842779159545898, 8.289304733276367, "[TT] Frequencies of the MSR = 24 GHz and 31 GHz"]
-[4.47578763961792, 2.989243984222412, "[FF] Test Location of the OSIRIS = Stuttgart and Oberpfaffenhofen"]
-[10.010969161987305, -0.529967725276947, "[TT] Nominal Altitude of the DubaiSat-2 = 600 km"]
-[5.1404595375061035, 0.403088241815567, "[TT] Separation Date of the STRaND-1 = February 25, 2013"]
-[4.726201057434082, 8.340667724609375, "[TT] Central Transmission Frequencies of the RA = 13.58 GHz and 5.25 GHz"]
-[9.380586624145508, 5.152592658996582, "[TT] Yaw Axis Slew of the Satellite = 180\u00ba in five minutes"]
-[5.5606608390808105, -1.9195159673690796, "[TT] Mission Status of the KOMPSAT-2 = Operational"]
-[8.233180046081543, 7.525888919830322, "[TT] Detector of the DubaiSat-1 = CCD (Charged Coupled Device)"]
-[11.566054344177246, 3.62337589263916, "[TT] Firing Direction of the Micronozzle = +Y"]
-[5.405795574188232, 3.9647364616394043, "[TT] Number of Satellites of the Global-5 and Global-19 = 2"]
-[11.811930656433105, 4.729798316955566, "[TT] Size of the Jugnu = 10 cm x 10 cm x 32 cm"]
-[7.866175174713135, 6.8789262771606445, "[TT] Spectrometer Type of the ACE-FTS = Adapted version of the classical Michelson interferometer"]
-[7.709897518157959, -2.341151475906372, "[TT] Manufacturer of the GOLD Instrument = LASP (Laboratory for Atmospheric and Space Physics) at the University of Colorado, Boulder, CO"]
-[5.750763416290283, 6.340103626251221, "[TT] Capacity of the Onboard data storage = 41 Gbit on SSR (Solid State Recorder)"]
-[5.168578624725342, 1.0202808380126953, "[FF] EOL Operations Date of the D-Sat = October 10, 2017"]
-[6.966766834259033, 5.790612697601318, "[TT] Number of RAFS Clocks of the GIOVE-A = 2"]
-[5.1477885246276855, 2.3453128337860107, "[FF] Owner of the GOSAT-2 = Japan Aerospace Exploration Agency (JAXA)"]
-[5.087308883666992, 0.6539239287376404, "[TT] Operational Alerts Availability of the MEOSAR = 2014-2016"]
-[5.96455192565918, 6.6760759353637695, "[TT] Transmission Path OPS per symbol of the DSP System = 3-5 OPS per transmitted symbol"]
-[4.463486194610596, 2.4311773777008057, "[TT] Image Capture of the DubaiSat-1 = More than 10,000 images of the globe"]
-[5.583586692810059, 0.8635019063949585, "[TT] Launch Date of the BepiColombo = October 2018"]
-[11.256827354431152, 5.380541801452637, "[TT] Scintillation Panels Thickness of the ACC = 8 mm"]
-[5.181430816650391, 5.9272074699401855, "[FF] Not Used for Payload Synchronization of the SpaceWire = Not used for payload synchronization"]
-[10.696579933166504, 7.150842666625977, "[TT] Footprint of the 2 = 25.8 x 17.5 km"]
-[10.063437461853027, 7.998479843139648, "[TT] Imager Size of the STARE telescope = 8.6 mm x 6.9 mm"]
-[6.432464122772217, 4.87493896484375, "[FF] Development Methodology of the TCS = Corresponded to the recommendations of the ECSS"]
-[9.655003547668457, 7.024108409881592, "[TT] Geometric Factor of the Instrument = 0.52 sr cm2"]
-[6.88280725479126, -0.6188119649887085, "[TT] Orbital Period of the MMO = 9.2 hours"]
-[4.474074363708496, 7.747608661651611, "[TT] Frequency Band of the CW transmitter = VHF (144 MHz)"]
-[5.547566890716553, 6.431435585021973, "[TT] Data Storage Capacity of the Instrument = 64 Gbit"]
-[7.14607572555542, 6.576183319091797, "[FF] Function of the PBC = Use a periscope to pick off a fraction of the laser light and direct it to the LSA"]
-[2.947268486022949, 4.466578483581543, "[TT] Spotlight Mode Spatial Resolution of the PALSAR-2 = 1 m x 3 m"]
-[9.51719856262207, 6.010922908782959, "[TT] Scan Geometry of the AMSU-A = Cross-track \u00b148.33 \u00ba"]
-[7.543064117431641, 3.1202194690704346, "[FF] Function of the GEDI = Produces detailed observations of the three-dimensional structure of the Earth's surface"]
-[13.378972053527832, 6.825875282287598, "[TT] Power On of the Watchdog = Immediately after the spacecraft has been ejected from the launch vehicle"]
-[7.6879191398620605, 3.1644163131713867, "[FF] Light Pollution of the Satellites = Not specified"]
-[8.50406551361084, 5.402760028839111, "[TT] Position Accuracy of the Orbit Knowledge = 10 m"]
-[9.024721145629883, 7.243367671966553, "[TT] Resolution of the Instrument = < 0.5 \u00b5rad"]
-[9.131047248840332, 3.148329973220825, "[FF] Mission of the MMS = Magnetospheric Multiscale Mission"]
-[14.72541332244873, 6.622308254241943, "[TT] Quantity of the Lithium-cobalt cells = 8"]
-[13.641480445861816, 3.205648899078369, "[TT] Sub-payload Mass of the ArgUS = 4 - 100 kg"]
-[7.620351314544678, 8.455533981323242, "[TT] Number of Elements of the MS Bands = 1,500"]
-[9.224672317504883, 8.679783821105957, "[TT] Dimensions of the Slit = 50 mm x 5 \u03bcm"]
-[5.5417094230651855, 6.386012554168701, "[TT] Capacity for Pan Imagery of the Memory = 4 Gbit"]
-[8.206218719482422, 2.839332103729248, "[FF] Measurement Importance of the FORUM = Important for understanding atmospheric processes linked to climate change"]
-[6.51936149597168, -0.5307493805885315, "[TT] Repeat Cycle of the CBERS-4A = 31 days"]
-[6.333690166473389, 0.7618526220321655, "[TT] Data Release Dates of the Gaia = 2016, 2018"]
-[3.848602771759033, 3.3975276947021484, "[TT] Launch Date of the Galileo Satellites 13 and 14 = 24 May"]
-[7.632556438446045, -0.8447204232215881, "[TT] Launch Date of the ICESat-2 = 2018"]
-[3.8866019248962402, 1.0864969491958618, "[FF] Launches Planned of the Falcon 9 = At least a dozen"]
-[13.804130554199219, 3.095151424407959, "[TT] Mass of the Payload = 3.00 kg"]
-[7.118259906768799, 3.7592763900756836, "[FF] Formation Flying Technology Demonstration of the PROBA-3 = In-Orbit"]
-[11.312612533569336, 2.888784885406494, "[TT] Power of the Minisatellite = 50 W"]
-[6.3381500244140625, 8.097253799438477, "[TT] Number of Channels of the GLI = 36"]
-[5.096556663513184, 5.182364463806152, "[TT] Communication Status of the UWE-1 = No communication signals can be received"]
-[13.741744041442871, 7.017704010009766, "[TT] Configuration of the SABR = Synchronous buck converter"]
-[13.314757347106934, 7.5177998542785645, "[TT] SSPA Power of the USAT = 20 W"]
-[5.167731285095215, 1.2379404306411743, "[FF] Launch Date of the ALOS-2 = Between 2009 and 2012"]
-[5.032561779022217, 1.3918653726577759, "[TT] Launch Date of the Flying Laptop = 2017"]
-[11.818458557128906, 4.764157295227051, "[TT] Size of the CanX-2 = 10 cm x 10 cm x 34 cm"]
-[13.69935417175293, 3.0891833305358887, "[TT] Payload Capacity of the STPSat-5 = 50-100 kg"]
-[5.905351161956787, 1.5022763013839722, "[FF] Mission Date of the PRISMA = Sept. 25-29, 2006"]
-[5.909916400909424, 7.724224090576172, "[TT] Signal Transmission of the GIOVE-B satellite = MBOC modulation scheme standard"]
-[5.781357765197754, 0.8590704798698425, "[FF] Installation Date of the UrtheCast Cameras = Jan. 28, 2014"]
-[5.1905412673950195, 1.1146374940872192, "[TT] Full Implementation Approval Date of the SMOS = Nov. 2003"]
-[5.1388068199157715, 1.0417332649230957, "[FF] Launch Date of the OPS-SAT = 18 December 2019"]
-[8.771645545959473, 2.9854538440704346, "[FF] Proposed Mission of the Aditya-L1 = Conference on Coupling and Dynamics of the Solar Atmosphere\", Pune, India, Nov. 10-14, 2014"]
-[9.731589317321777, 8.279012680053711, "[TT] IFOV of the DORIS = 125\u00ba centered on nadir"]
-[8.628238677978516, 3.6132068634033203, "[TT] Measurement Category of the TSIS-1/TIM = Downwelling (Incoming) solar radiation at TOA"]
-[5.0616583824157715, 3.1757335662841797, "[TT] CubeSat Structure Manufacturer of the Iraz\u00fa CubeSat = Costa Rica"]
-[10.003454208374023, 0.16247709095478058, "[TT] Spacing of the GRACE-FO satellites = 220 km"]
-[14.020031929016113, 2.739978790283203, "[TT] Launch Mass of the CartoSat-2D = 1378 kg"]
-[4.89094877243042, 8.27575969696045, "[TT] Frequency of the SSALT = 13.65 GHz"]
-[13.772852897644043, 3.1545491218566895, "[TT] Payload Capacity of the AlSat-2 = Up to 50 kg"]
-[7.611579895019531, 8.56942367553711, "[TT] Number of Usable Spectral Bands of the Instrument = 256"]
-[4.666769027709961, 3.225656032562256, "[FF] Expertise of the Thales Alenia Space = Satellite avionics development and testing"]
-[6.55720329284668, 4.639258861541748, "[FF] Function of the Mission Data Processing System = Performs the geometric correction of the image data according to the processing planning from Order Handling and Distribution System and the stores the data into Mission Data Archiving System"]
-[9.7316255569458, -0.7634867429733276, "[TT] Orbit Altitude of the FY-4B = 35786 km"]
-[7.8865156173706055, 3.1625945568084717, "[TT] Absorption Band of the FTS = CO2"]
-[8.984747886657715, 5.686849594116211, "[TT] Pointing Accuracy of the Kondor-E = \u2264 6 arcmin"]
-[8.7490816116333, 6.36121129989624, "[TT] Measurement Accuracy of the Altimeter = \u00b1 10 cm"]
-[10.147953987121582, 0.9670879244804382, "[TT] Distance from Earth of the M82 X-2 = About 12 million light-years away"]
-[6.17757511138916, 0.01761273853480816, "[TT] Activation Frequency of the LDT = Every 2 minutes"]
-[4.131677627563477, 7.311525344848633, "[TT] Bands of the Star One D2 = Ku-, Ka-, C- and X-band"]
-[8.201738357543945, 6.592607498168945, "[FF] Description of the Spectroscopy Technique = Uses a laser to zap a pinhead-size portion of a rock, and a spectrometer to analyze the light given off by plasma generated by the laser\u2019s interaction with the rock\u2019s surface"]
-[5.833847522735596, -0.7800494432449341, "[TT] Actual Lifetime of the QuakeSat = 1 \u00bd years"]
-[5.9545416831970215, 5.463923931121826, "[FF] Technology of the GALANT = Digital beamforming (DBF)"]
-[4.272100448608398, 0.34293270111083984, "[TT] Launch Date of the JPSS-1 = 18 November 2017"]
-[7.630327224731445, 5.293546199798584, "[FF] Assembly of components of the Metering Truss = Brazed assembly of components"]
-[9.290081024169922, 3.1945908069610596, "[FF] Image Recording of the Coronagraph = 35 mm film"]
-[5.8582444190979, 3.8464014530181885, "[TT] Alias of the AstroBus-L platform = AstroSat-250 (AS250)"]
-[13.859267234802246, 5.658332824707031, "[TT] Cell Efficiency of the Solar Panels = 26%"]
-[6.805054187774658, 2.4760303497314453, "[FF] Backup Location of the Meteosat = 63o E over the Indian Ocean"]
-[8.161848068237305, 3.794968605041504, "[FF] On Board Calibrator (OBC) of the OCO-2 = Calibration Data Collection"]
-[12.215802192687988, 3.6805601119995117, "[FF] Critical Viscosity of Xenon-2 of the CVX-2 = Unknown"]
-[12.172330856323242, 4.625049591064453, "[TT] Size of the Bus = 1.2 m in diameter, 1.35 m high"]
-[9.776944160461426, 7.495569229125977, "[TT] Ground Sample Distance (GSD) of the MS Bands = 10 m x 10 m"]
-[6.895339012145996, 5.6791090965271, "[TT] Quantity of the PEPPODs = 2"]
-[13.713271141052246, 3.462477445602417, "[TT] Mass of the S-band Transmitter = 0.1 kg"]
-[5.1971869468688965, 0.8315269947052002, "[FF] Submission Date of the MinXSS = August 15, 2013"]
-[5.6126861572265625, 2.7732481956481934, "[FF] Status of the X-SAT = Functioning Satisfactorily"]
-[7.474584579467773, 2.524235725402832, "[TT] Measurement Category of the Kondor-E = Multi-purpose imagery (land), Soil moisture"]
-[9.87972354888916, 4.406374931335449, "[FF] Redundancy of the ADCS = Full redundant backup with magnetorquers and reaction wheels"]
-[10.832059860229492, 4.008672714233398, "[TT] Drag Sails of the CanX-7 = Four"]
-[7.510389804840088, 3.4079573154449463, "[FF] Deliverable of the Product Level 2A (L2A) = Earth located pixel values converted to ground surface reflectance"]
-[8.436362266540527, 8.7206392288208, "[TT] Effective Area of the EUV Simulation = 43 cm2"]
-[5.911225318908691, 1.5112015008926392, "[FF] Collision Avoidance Maneuver Date of the PRISMA Satellites = July 7, 2010"]
-[8.64974308013916, 7.718663215637207, "[TT] Number of Pixels of the OLS = 7,325 pixels"]
-[7.3167266845703125, 2.4126501083374023, "[FF] Global Coverage of the TOPEX/Poseidon = Yes"]
-[7.611351013183594, 5.170133590698242, "[TT] Environmental Testing of the GOES-S = Undergoing"]
-[4.44040584564209, 3.3069469928741455, "[TT] Location of the DLR ground station = Neustrelitz"]
-[8.512615203857422, 6.882913112640381, "[TT] Scanning Technique of the PRISM-2 = Pushbroom"]
-[5.618549823760986, 6.549238681793213, "[TT] Buffering Capacity of the DHS = Three days worth of science data"]
-[3.287607192993164, 5.234248638153076, "[TT] Incidence-angle Range of the SAR-10 = 20-55\u00ba"]
-[11.484354019165039, 4.888047695159912, "[TT] Length of the New Depression = 210 m"]
-[8.174787521362305, 7.827704429626465, "[TT] Number of Detectors of the VIS Channel Detector = 4"]
-[5.542229652404785, 1.6401821374893188, "[FF] Availability of the HEASARC = Public"]
-[9.834251403808594, 1.6063036918640137, "[FF] Conference Presentation of the TESIS = Proceedings of the International Astronomical Union (IAU), 2006"]
-[9.896328926086426, 8.02050495147705, "[FF] Dominant Lines of the Telescope = Fe(8+ through 11+), Mg(8+ through 10+), O(6+ and 7+), Si(8+ and 9+), C(6+ and 5+), O7+ and O 8+"]
-[8.044011116027832, -0.5413511395454407, "[TT] Ice Loss of the ICESat = 200 gigatons per year"]
-[10.114208221435547, -1.5768569707870483, "[TT] Inclination of the Yubileyniy-2/MiR = 82.5\u00ba"]
-[6.49382209777832, 6.288796424865723, "[FF] Intensity of the RFI Sources = Very strong power emitters"]
-[9.774323463439941, -0.6058264970779419, "[TT] Orbit Altitude of the WCOM = 645 km"]
-[8.178851127624512, 8.571050643920898, "[TT] Micro-Roughness of the ASPIICS = 0.5 nm RMS"]
-[9.200681686401367, 4.911442756652832, "[FF] Image Registration Accuracy of the Attitude Determination & Control System = 100 m"]
-[8.510343551635742, 1.5857350826263428, "[TT] Scatterometer Type of the Aquarius = S-band scatterometer"]
-[5.430794715881348, 5.5696892738342285, "[TT] Communication Interface of the EC = 16-bit parallel port"]
-[9.617749214172363, -0.5479158163070679, "[TT] Orbit Altitude of the PICOSat = 800 km"]
-[8.41301155090332, 1.145064115524292, "[TT] Spatial Resolution of the Solid Earth Seismic hazards = 100-200 km"]
-[8.338521957397461, 1.6868901252746582, "[TT] Spatial Resolution of the Oceanography Basin scale = 200 km"]
-[5.343461036682129, 0.8074153065681458, "[FF] Experiment Start Date of the AMS-02 = September 2011"]
-[5.861177921295166, 3.558227300643921, "[FF] Design of the SSTE-4 = Low-Cost, R&D Space Mission with Responsive Enabling Technologies"]
-[8.395452499389648, 8.760625839233398, "[TT] Effective Area at 80 nm of the EUV Simulation = 6 cm2"]
-[10.49807071685791, 0.950474202632904, "[TT] Host Star Diameter of the WD 1856 b = Roughly 11,000 miles (18,000 km)"]
-[3.532626152038574, 6.412001132965088, "[TT] Antenna Diameter of the Ground Segment = As small as 2.4 m"]
-[9.037942886352539, 5.5158233642578125, "[TT] Off-nadir Body-pointing Capability of the AODCS = \u00b130\u00ba in all directions"]
-[10.278583526611328, 5.397939682006836, "[TT] Thermal Control Type of the CASSIOPE spacecraft = Passive, supplemented with software-controlled operational heaters"]
-[8.945351600646973, 2.4672622680664062, "[TT] Dust of the MEIDEX = 56%"]
-[10.432785987854004, 2.8867290019989014, "[FF] Software defined radio of the Nanosatellites = For greater transceiver frequency flexibility"]
-[9.678108215332031, 4.8425188064575195, "[TT] Stabilization of the COMS = 3-axis"]
-[6.892457485198975, 4.975930690765381, "[FF] Canister Equipment of the CVX-2 = UEPs (Upper End Plates)"]
-[9.898975372314453, 0.8739522099494934, "[TT] Capture Method of the ASTRO and NextSat = Docking mechanism"]
-[6.231949806213379, 0.9816979169845581, "[FF] Observation Date of the Murchison Widefield Array (MWA) = Unknown"]
-[8.120646476745605, 8.344356536865234, "[TT] Sensitivity (NE\u0394T) Infrared Channel of the VIRR = 4 K with a scene at 185 K, 1 K with a scene at 300 K"]
-[8.82923412322998, 0.09476572275161743, "[TT] Altitude at Checkpoint of the OSIRIS-REx = Approximately 410 feet (125 m)"]
-[4.8715500831604, 0.5881394743919373, "[FF] Launch Date of the MULA = 2025"]
-[5.081326961517334, 3.396077871322632, "[TT] Manufacturer of the Landsat-9 = Northrop Grumman Innovation Systems"]
-[6.720066547393799, 5.900864601135254, "[TT] Quantity of the TDU = 2"]
-[5.606269359588623, 7.025665760040283, "[TT] Telemetry Data Rate Range of the TTCS = 4-16 kbit/s"]
-[8.116657257080078, -1.0507837533950806, "[FF] Data Detection of the ICESat-2 = Lakes filling and draining"]
-[5.00437593460083, 0.4685412049293518, "[FF] Press Release Date of the University of Zurich and Airbus = 26 August 2021"]
-[9.543302536010742, 8.029603958129883, "[TT] f/D of the Limb Imager = 7.3"]
-[10.933856010437012, 2.8808300495147705, "[TT] Pointing Accuracy of the PARASOL microsatellite = 0.1\u00ba"]
-[7.071846961975098, 2.426128625869751, "[FF] Publication Date of the Superresolution far-field imaging by coded phase reflectors = 18 December 2018"]
-[10.011507034301758, 2.8932580947875977, "[TT] Launch Date of the CubeSat - Launch 4 = 17 April 2006"]
-[8.432333946228027, 5.118575096130371, "[TT] Number of Accelerometers of the Accelerometer Suite = 6"]
-[11.843265533447266, 6.7574262619018555, "[TT] Energy Range of the IDEE = 70 keV \u2013 4 MeV"]
-[5.222026824951172, 1.5533204078674316, "[TT] Dataset Update of the ALOS/ Daichi = March 2017"]
-[7.082863807678223, 5.912060260772705, "[TT] Accuracy of the Atomic Clock = One second in three million years"]
-[5.413740158081055, 3.920628070831299, "[TT] Number of Satellites in Orbit of the Satellogic = 68"]
-[4.79307746887207, 5.499085903167725, "[FF] Frequency of the Pyxis-RO = 1575.42 MHz (L1 GPS), 1227.6 MHz (L2 GPS), 1575.42 MHz (E1 Galileo), 1207.14MHz (E5 Galileo), 1602 MHz (L1 GLONASS), 1246 MHz (L2 GLONASS), 1561.1 MHz (B1 BeiDou), 1207.14 MHz (B2 BeiDou)"]
-[7.928557872772217, 7.621469020843506, "[TT] Objective of the FTHSI = Demonstrate spaceborne hyperspectral imaging technologies"]
-[8.746052742004395, 5.2521748542785645, "[TT] SIF Products Agreement of the TanSat = Strong, higher than 0.73"]
-[7.818093299865723, 5.859250545501709, "[TT] Instrument type of the VIRR (SeaSat) = Imaging multi-spectral radiometers (passive microwave)"]
-[5.079257488250732, 0.9436837434768677, "[TT] Launch Date of the SMAP = 2015"]
-[5.801736354827881, 0.5310766100883484, "[TT] Tandem Passes Separation of the Envisat / ERS-2 SAR = 28 minutes"]
-[7.930771350860596, 8.671903610229492, "[FF] Spectral Response of the VACNTs = Extremely flat over a wide wavelength range"]
-[6.104686260223389, 3.13266658782959, "[TT] Contract with National Geospatial-Intelligence Agency (NGA) of the BlackSky = $30 million, five-year indefinite delivery indefinite quantity contract"]
-[10.033500671386719, -1.5409204959869385, "[TT] Orbit Inclination of the NRCSD = 51.6\u00ba"]
-[13.32358455657959, 7.314197063446045, "[TT] Power of the MSU-100 = 6.8 W"]
-[5.453832149505615, 6.211660861968994, "[TT] Capacity of the Memory = Dual-redundant 128 kBytes SOS RAM, 64 kBytes ROM"]
-[6.183574199676514, 4.563302993774414, "[FF] Operation of the Command and Data Handling Subsystem = Autonomously schedules GPS acquisitions and uplink/downlink operations"]
-[13.609054565429688, 1.7421765327453613, "[TT] Return Cargo Weight of the Cargo Dragon = 5,200 pounds"]
-[7.850274085998535, 8.111637115478516, "[TT] Function of the Bandpass Filter = Detect N2 1st positive emission from sprites"]
-[5.94014310836792, 4.422517776489258, "[FF] Purpose of the Secure Communications Satellite = Provide secure and resilient satellite communications"]
-[6.583698272705078, -0.570903480052948, "[TT] Mission Period of the Corvus-BC 5 = 3 minutes"]
-[10.25900936126709, 2.057114839553833, "[FF] Published Date of the Prompt thermal emission in gamma-ray bursts = 5 March 2013"]
-[7.048133850097656, 5.882761001586914, "[TT] Clock Type of the GIOVE-B = Hydrogen-maser clock"]
-[3.60750675201416, 4.641417026519775, "[FF] Flexibility of the RISAT-1 = Reconfigurable to meet different imaging requirements"]
-[9.30029296875, 5.34193754196167, "[TT] Type of the AMI-302 = 3-axis"]
-[8.637063026428223, 7.686695098876953, "[TT] Pixel Count of the Detector Array (MS) = 3375 pixels cross-track"]
-[10.75632095336914, -1.138055682182312, "[FF] Atmospheric Density Comparison of the SLATS = NRLMSISE-00 has more than +20% bias, JB2008 and DTM2013 correspond well with the SLATS data"]
-[4.753715991973877, 7.300766944885254, "[TT] Bandwidth of the Ground Station = 19.2 kbit/s CPFSK and 38.4 kbit/s BPSK/QPSK \u00bd k=7"]
-[9.392151832580566, 5.650498390197754, "[TT] Probe Orientation of the TPMU = In the direction of the velocity vector"]
-[10.752902030944824, 2.847210645675659, "[TT] Planned Number of Microsatellites of the PlanetIQ = 12"]
-[11.77931022644043, 3.326421022415161, "[TT] Apogee Motor Type of the Propulsion Subsystem = Bipropellant liquid"]
-[6.358100891113281, 6.121326446533203, "[TT] Configuration of the NGAVGS = One box"]
-[5.973154544830322, 0.68096923828125, "[FF] Mission of the Year Award of the ASTERIA = 14 August 2018"]
-[11.902416229248047, 3.1043245792388916, "[TT] Delta-V of the DMC Propulsion Subsystem = 10 m/s"]
-[6.294210433959961, 8.658026695251465, "[TT] Polarization of the MWR = V"]
-[9.619354248046875, 6.941411972045898, "[TT] Angular Resolution of the ELENA = 4.5\u00ba x 4.5\u00ba"]
-[5.814335823059082, 5.225757122039795, "[FF] Network Configuration of the MEOLUT = Networked to share raw data"]
-[12.131973266601562, 4.602018356323242, "[TT] Size of the Spacecraft = 2000 mm x 1720 mm x 2200 mm"]
-[5.843568325042725, 7.002473831176758, "[TT] Data Rate of the WINDS = 1.2 Gbit/s"]
-[8.363576889038086, 8.253384590148926, "[FF] Bands of the NAOMI = Over five different bands, one panchromatic band and four multispectral bands (blue, green, red, and near-infrared)"]
-[4.86876106262207, -0.9089382290840149, "[FF] Measurement Resolution of the Fengyun-4B = Doubled compared with the Fengyun-4A satellite"]
-[7.6603264808654785, 3.7152116298675537, "[TT] Size of the Debris = About 1.3 meter pixels"]
-[6.88963508605957, 4.924952030181885, "[FF] Function of the ToF (Time-of-Flight) counter = Measure the velocity of particles"]
-[8.717618942260742, 8.77856731414795, "[TT] Gratings of the Grating Spectrometer = 12 mm x 12 mm plane gratings, 200 to 600 g/mm"]
-[10.531638145446777, 1.77438223361969, "[FF] Observation Target of the NICER/SEXTANT = Neutron stars and pulsars"]
-[5.841474533081055, 6.093421459197998, "[FF] Bandwidth Demand of the ISL Communications = Increased"]
-[6.882248878479004, 2.303553342819214, "[FF] URL of the China High-resolution Earth Observation System (CHEOS) = http://www.oosa.unvienna.org/pdf/pres/stsc2014/tech-47E.pdf"]
-[5.665444374084473, -0.10071691125631332, "[TT] Departure Time from Space Station of the Cygnus = About three months after arrival"]
-[7.9588847160339355, 8.397836685180664, "[TT] Spectral Coverage of the ILAS = 1024 visible channels in the range of 0.753 - 0.784 \u00b5m"]
-[10.061821937561035, 1.3984771966934204, "[FF] Distance Scale of the Gaia mission = Each kiloparsec equal to 3,260 light-years"]
-[3.3430488109588623, 5.086550235748291, "[TT] Operation Modes of the RISAT-SAR = Simultaneous co- and cross-polarization"]
-[8.573893547058105, 5.631323337554932, "[TT] Position Accuracy of the NavIC = 5 m"]
-[8.478240013122559, 0.16603218019008636, "[FF] Presentation of the Rosetta = Rosetta: Imaging Tools, Practical Challenges and Evolution of Optical Navigation Around a Comet"]
-[11.970698356628418, 4.535508155822754, "[TT] Target Diameter of the Psyche spacecraft = About 140 miles, or 226 kilometers"]
-[14.218816757202148, 3.1406090259552, "[TT] Mass of the AISSat-1 = 6.5 kg"]
-[6.734840393066406, -0.5890563130378723, "[TT] Repeat Cycle of the GOSAT-GW = Three days"]
-[10.106051445007324, -1.524893879890442, "[TT] Along-Track of the WAOSS-B = \u00b125\u00b0"]
-[6.588855743408203, -2.0398337841033936, "[TT] Launch Date of the Jason-1 = Dec. 7, 2001"]
-[10.630817413330078, 2.8696415424346924, "[FF] Based on of the RASAT microsatellite = BILSAT bus and module heritage"]
-[4.510936260223389, -0.9065518379211426, "[TT] Launch Date of the Dragon C2/3 spacecraft = May 22, 2012"]
-[6.839549541473389, 2.8340933322906494, "[FF] Focus of the RECCAP-2 = Reconcile and constrain the global GHGs budget with the aggregation of regional budgets"]
-[3.7057454586029053, 5.0980119705200195, "[TT] Imaging Frequency Band of the ERS-1 = C"]
-[5.992924690246582, 3.17309308052063, "[TT] Operation Agency of the GOES-16 = NOAA"]
-[7.310568809509277, 6.295178413391113, "[TT] Quantity of the CCDs = 104"]
-[11.791093826293945, 4.791116237640381, "[TT] Size of the CADRE = 10 cm x 10 cm x 34 cm"]
-[7.986133575439453, -0.5348612070083618, "[TT] Take Measurements Through Clouds of the CryoSat-2 = Yes"]
-[11.695758819580078, 6.440577030181885, "[FF] Flux Variations of the LDT = Can also be obtained"]
-[9.41541576385498, 5.971255302429199, "[FF] Views of the Calibration Mirror = Cold space, \"warm\" blackbody"]
-[8.679717063903809, 8.813790321350098, "[TT] Grating Type of the Grating Reflection Unit = Dielectric reflection grating"]
-[9.16472339630127, 6.82363224029541, "[TT] Resolution of the FSS = 0.005\u00ba"]
-[6.360434532165527, 4.9810075759887695, "[FF] Function of the C&DH = Receives and decodes command signals, communicates with instruments, edits temperature, voltage, and status, transmits telemetry signals"]
-[7.4454498291015625, 2.9144532680511475, "[TT] Spatial Resolution of the MethaneSAT = 100 x 400 meters"]
-[12.832254409790039, 7.592160701751709, "[TT] Power of the Instrument = 129 W"]
-[5.417490005493164, 0.14972823858261108, "[TT] Operation Start Date of the RAIDS = October 22, 2009"]
-[7.977948188781738, 3.0623912811279297, "[FF] Purpose of the ISUAL = Imager of Sprites and Upper Atmospheric Lightning"]
-[9.226449012756348, 6.076502799987793, "[TT] Sweep Angle of the Sensor = 10.4\u00ba"]
-[10.868600845336914, 5.605031490325928, "[TT] Heat Shield of the EFT-1 Orion = Avcoat"]
-[7.800167560577393, 2.8391642570495605, "[FF] Purpose of the ABI = Provides high-resolution imagery and radiometric information of the Earth\u2019s surface, atmosphere and cloud cover"]
-[4.777815818786621, -1.8385025262832642, "[TT] Lunar Orbit Entry Date of the Chang'e-5 = Nov. 28"]
-[4.440342426300049, 6.2022223472595215, "[TT] UHF Transceiver Frequency Range of the GOMX-3 = 435-438 MHz"]
-[6.005076885223389, -0.3702591359615326, "[TT] Commissioning Duration of the QUESS = 5 months"]
-[7.596904754638672, 2.202134847640991, "[TT] Global Coverage of the Antenna Subsystem = \u00b180\u00ba latitude"]
-[4.369190216064453, 4.304141521453857, "[TT] Number of Operational Satellites of the COSPAS-SARSAT = 62"]
-[6.988978862762451, 1.8436241149902344, "[FF] Data Access of the Landsat-7 = Free access to the entire user community"]
-[4.153855800628662, 2.282984972000122, "[TT] Launch Provider of the GRACE-FO = ISC (International Space Company) Kosmotras"]
-[1.4411031007766724, 2.770174741744995, "[TT] Primary Use of the Band 10 = Water vapor"]
-[3.880157947540283, 2.011251211166382, "[TT] Launcher of the Sentinel-1B = Soyuz-STA/Fregat vehicle (VS 14) of Arianespace"]
-[9.465145111083984, 7.051403045654297, "[TT] Resolution of the ALI = 30 m"]
-[7.661960601806641, 5.629263401031494, "[FF] Main Challenges of the MERLIN = Implementing a complex LIDAR instrument on a small satellite platform with limited resources"]
-[4.759920597076416, 1.8027082681655884, "[FF] Ground Segment Establishment Date of the EUMETSAT = 1995"]
-[5.579131126403809, 5.638591766357422, "[TT] Processor of the MCM = TS68EN360 and XPC860"]
-[9.768044471740723, -0.5899389386177063, "[TT] Orbit Altitude of the CanX-2 = 635 km"]
-[7.951490879058838, 9.285345077514648, "[TT] Wavelength of the Hydroxyl ion = 2.81 \u00b5m"]
-[7.785111904144287, 2.0560812950134277, "[FF] Purpose of the EXPORTS = Advance the utility of NASA ocean color assets to predict how changes in ocean primary production will impact the global carbon cycle"]
-[13.352994918823242, 7.034003257751465, "[TT] Power Requirement of the Payload = 100 W"]
-[7.375273704528809, 5.262163162231445, "[TT] Components of the EQB (EQuipments Box) = Relay lens(es), FPA and its radiator, filter wheel and the Lyot stop assemblies, shutter mechanisms, venting systems"]
-[8.89488697052002, 9.534904479980469, "[FF] Band 5 Resolution of the TANSO-FTS-2 = 0.2 cm -1"]
-[10.143385887145996, 8.0742769241333, "[TT] Focal Length of the Telescope = 150 mm"]
-[5.029156684875488, 4.482701301574707, "[TT] Number of Stations in Oklahoma of the Mesonet = More than 100"]
-[12.09121036529541, -0.2177860289812088, "[TT] Monitoring Region of the TESS = 24-by-96-degree"]
-[3.9641356468200684, 5.41449499130249, "[TT] Signal Type of the Radar Altimeters = Pulses of radio waves (microwaves)"]
-[10.370741844177246, 5.697684288024902, "[TT] Thermal Operating Range of the SAGE-III = 10-30\u00ba C"]
-[11.406636238098145, 3.4832923412323, "[FF] Mission of the CU-E3 = Use solar radiation pressure rather than an onboard propulsion system"]
-[12.217730522155762, 3.6903510093688965, "[FF] Temperature of the CVX = Very near Xenon's liquid-vapor critical point"]
-[6.674498558044434, 3.5480871200561523, "[FF] Data Latency of the MetOp Satellite = 65 minutes"]
-[13.452714920043945, 6.9506964683532715, "[TT] Power Output of the Fission Surface Power System = Up to 10 kilowatts"]
-[6.167359352111816, 0.7704845666885376, "[FF] Publication Date of the Gaia16aye = January 2020"]
-[5.2566046714782715, 7.007039546966553, "[TT] Telemetry Downlink Speed of the Communication links = 20 kbit/s"]
-[4.56462287902832, 1.4306100606918335, "[TT] Launch Year of the GOSAT-2 = 2018"]
-[8.925777435302734, 4.372293472290039, "[FF] Type of the Coarse Sun Sensors = Unknown"]
-[6.285088062286377, 3.9616706371307373, "[TT] Program of the MetOp-SG = MetOp-Second Generation Program"]
-[6.501118183135986, 1.987722396850586, "[FF] URL of the Chinese satellite = http://www.spaceflightinsider.com/"]
-[5.27764368057251, 7.660058498382568, "[TT] G/T of the Mobile Link = 15 dB/K"]
-[8.303878784179688, 7.510317802429199, "[TT] Detector Types of the MSI instrument = CMOS and hybrid HgCdTe (MCT)"]
-[6.941215991973877, 4.180586814880371, "[FF] Website of the SCARAB = http://smsc.cnes.fr/SCARAB/"]
-[5.50466775894165, 2.745561361312866, "[FF] Development Status of the Arachne = Unknown"]
-[8.557147979736328, 2.3689112663269043, "[FF] Objective 2 of the EMIT = Predict how future climate scenarios might change the amount and type of mineral dust emitted into the Earth\u2019s atmosphere"]
-[4.608804702758789, 4.78737735748291, "[FF] Challenges of the Maritime AI-NAV = Significant increases in transport volumes, more stringent environmental requirements and a shortage of seafarers in the future"]
-[3.8199360370635986, 4.597617149353027, "[FF] Phase imbalances of the RADARSAT-2 = Can arise due to differences in component temperatures between wings, among other factors"]
-[6.49290657043457, 0.7370485663414001, "[FF] Mission Status of the Landsat-9 = Continuing the legacy - 2020 and beyond"]
-[8.990203857421875, 7.236361503601074, "[TT] Resolution of the AlSat-2A = 2.5 m"]
-[8.404607772827148, 6.718903541564941, "[TT] Sensor Type of the TANSO-CAI-2 = Push-broom imaging sensor"]
-[9.867114067077637, 4.265169143676758, "[TT] Magnet Type of the AMS-02 = Permanent"]
-[12.69624137878418, 4.949726581573486, "[TT] Solar Paddle Dimensions of the ADEOS = Approx. 3 m x 26 m"]
-[5.40433931350708, 5.877211570739746, "[TT] CPU of the STRV-1d DHS = 8051 rad-hard"]
-[11.722156524658203, 6.6748175621032715, "[FF] Energy Range of the ELENA = <0.02-5 keV"]
-[5.444794654846191, 6.073083877563477, "[TT] SRAM Memory of the OBC = 6 MB"]
-[7.235709190368652, 6.861684799194336, "[TT] CCD Readout Interval of the F-FEE = 2.5 s"]
-[9.394658088684082, 5.255739212036133, "[TT] Roll Angle of the TanSat = About 20\u00b0"]
-[5.065584659576416, 5.935975551605225, "[FF] Function of the AIS Data Receiver = Collect, store, and forward AIS messages globally"]
-[5.588287353515625, -2.0085785388946533, "[FF] Purpose of the KOMPSAT-3 = High-resolution optical imagery for applications in environmental, oceanographic and agricultural monitoring"]
-[5.441749095916748, 5.2046799659729, "[TT] Onboard Computer of the PhoneSat 2 = Samsung Nexus S phone"]
-[4.11862850189209, 2.091364860534668, "[TT] Launch Vehicle of the NigeriaSat-1 = Kosmos-3M"]
-[3.372722864151001, 6.470409870147705, "[TT] Diameter of the Antenna = 1 m"]
-[5.345582485198975, 0.6535983085632324, "[FF] Launch Date of the EnviSat = Unknown"]
-[6.814376354217529, 6.431552410125732, "[TT] Processing Time of the DSM = 180 s"]
-[11.6381254196167, 3.729205369949341, "[TT] Firing Duty Cycle of the X-axis Bang-Bang Maneuver = 90%"]
-[5.676957607269287, 0.8885785341262817, "[FF] Contract Signing Date of the BepiColombo = Dec. 5, 2012"]
-[7.847836971282959, 1.6575276851654053, "[TT] Regeneration Area of the Mangrove Forests = 148 km2"]
-[11.809309005737305, 6.618759632110596, "[TT] Ionization Efficiency of the MCP = 80-120 eV"]
-[10.974577903747559, 3.7774696350097656, "[TT] Solar Sail Size of the NEA Scout = 925 square feet (86 m2)"]
-[8.181251525878906, 2.1495273113250732, "[FF] Science Objectives of the TROPICS = Relate the precipitation structure evolution, including the diurnal cycle, to the evolution of the upper-level warm core and associated intensity changes"]
-[5.90504264831543, 1.5762748718261719, "[FF] Presentation Date of the MEIDEX = 2003"]
-[9.127732276916504, 0.4138702154159546, "[TT] Parking Orbit Altitude of the ARTEMIS = 31,000 km"]
-[7.714903354644775, 9.358750343322754, "[TT] Center Wavelength of the Band 2 = 0.64 \u00b5m"]
-[5.719453811645508, 6.858797073364258, "[TT] Data Packet Size of the Processor-based sub-experiments = Up to 255 bytes"]
-[7.585263252258301, 4.243138313293457, "[FF] Function of the RC = Analysis facilities to support physicists from geographically close AMS universities and laboratories, provide access to the AMS-02 data for visualization, detector verification studies and status of data processing, processing sites for the AMS-02 Monte Carlo production and AMS-02 Data reproductions"]
-[14.070405006408691, 4.049594879150391, "[TT] Instrument Mass of the GGAK-M = 90 kg"]
-[5.090766906738281, 3.46417498588562, "[TT] Manufacturer of the Imaging Payload = SI (Satrec Initiative Co. Ltd.)"]
-[9.477330207824707, 7.064248085021973, "[FF] L3 Data Grid Resolution of the HY-1C = 4 km and 9 km"]
-[7.679293632507324, 5.535340785980225, "[FF] Purpose of the VBN Demonstration = Assess the state-of-the-art of Image Processing (IP) and navigation algorithms"]
-[8.156132698059082, 7.257359504699707, "[FF] Conference Presentation of the EarthCARE Multispectral Imager = ICSO 2010 (International Conference on Space Optics), Rhodes Island, Greece, Oct. 4-8, 2010"]
-[18.796722412109375, 3.479750394821167, "[TT] Mean \u0394N (m) of the Dyess = 5.2"]
-[5.187350749969482, 4.78578519821167, "[TT] Minimum BCRs for Normal Function of the DubaiSat-2 = Two BCRs"]
-[4.53509521484375, 4.131223678588867, "[FF] Signal Transmission of the GIOVE-A = Galileo spreading codes"]
-[3.9389116764068604, 9.712309837341309, "[TT] Frequency (GHz) of the ICI-6 = 325.15\u00b13.5"]
-[7.968937873840332, 8.333127975463867, "[FF] Minimum Value of the Spectral Angle = Achieved when the blue panel is prominent"]
-[11.243267059326172, 0.942383348941803, "[TT] Launch Date of the LISA = 2034"]
-[11.259943962097168, 0.9754139184951782, "[FF] Requirements Maturity of the LISA = Adequate to the current phase"]
-[5.96366548538208, -0.2792719900608063, "[TT] Test Duration of the EDRS-C = Two weeks"]
-[14.102476119995117, 3.1413652896881104, "[TT] Mass of the ELSA-d = 180 kg (Chaser/Servicer), 20 kg (Target/Client)"]
-[7.639097213745117, 8.755338668823242, "[FF] Spectral Bands of the MSU-MR = Six bands in the VIS and IR spectral regions"]
-[7.906245231628418, 7.107831954956055, "[TT] Quantity of the MCP-PH = 4 photometers"]
-[8.113869667053223, 5.259453296661377, "[FF] Function of the SES = Validate the optical and thermal performance of the instrument"]
-[6.5810723304748535, 0.9778600335121155, "[FF] Daily Revisit Capability of the FormoSat-2 = Yes"]
-[10.464887619018555, 5.772263050079346, "[TT] Temperature Difference of the KELT-9 b = Almost 1,500\u00ba F (800\u00ba C)"]
-[3.48276686668396, -0.8570011258125305, "[TT] Orbit of the EarthDaily Constellation = Sun-synchronous"]
-[6.997337341308594, 0.16010241210460663, "[TT] Lifetime of the SeaSat = 110 days"]
-[4.1629133224487305, 0.6585967540740967, "[FF] URL of the INTEGRAL = http://iopscience.iop.org/article/10.3847/2041-8205/820/2/L36/pdf"]
-[5.210911273956299, 6.002326011657715, "[FF] SpaceWire Interfaces of the PDHU = Performed thanks to a specific FPGA"]
-[9.167780876159668, 5.282708644866943, "[TT] Pointing Accuracy of the Payload = 0.5\u00ba in roll, pitch and yaw"]
-[14.05424976348877, 4.010357856750488, "[TT] Mass of the Instrument Interface Module = 75 g"]
-[6.733650207519531, 4.011788368225098, "[FF] Failure of the DMSP F-19 = Unknown"]
-[5.35782527923584, 0.22757668793201447, "[TT] Launch Date of the STS-85 = Aug. 7-19, 1997"]
-[10.887784004211426, 2.110106945037842, "[FF] Data Archive of the XMM-Newton = Rich"]
-[6.334061622619629, 2.2794034481048584, "[FF] Image of the SEOSAT/Ingenio = SEOSAT in the cleanroom"]
-[4.806488513946533, 0.24468432366847992, "[TT] Launch Date of the RemoveDebris = 2 April 2018"]
-[9.676051139831543, 1.3833637237548828, "[FF] Unknown of the Pleiades = Unknown"]
-[12.156076431274414, -0.1123785749077797, "[FF] Photometric Performance of the TESS Cameras = Not specified"]
-[8.72863483428955, 1.5123231410980225, "[TT] Access of the Copernicus EMS = Planet\u2019s SkySat constellation"]
-[5.523754119873047, 2.404914617538452, "[FF] Targets of the GSPC = Cyg X-2, 4U1636-53, Her X-1, Coma, Cyg X-3, Perseus, Cyg X-1, Cas A, Crab, Cen X-3, Cen X-2, and Vela X-1"]
-[10.969476699829102, 2.8928375244140625, "[TT] Dimensions of the Picard microsatellite = 90 cm x 80 cm x 110 cm"]
-[11.98577880859375, 3.0663461685180664, "[FF] Attitude Control System of the Bus = Reaction Control Subsystem (RCS) - a hydrazine blowdown system pressurised with helium"]
-[14.067341804504395, 4.043020725250244, "[TT] Mass of the Instrument = < 300 g"]
-[6.508004188537598, 8.597082138061523, "[TT] Polarization Factor of the Satellite = < 2% (310-500 nm)"]
-[11.922381401062012, 4.874209880828857, "[TT] Enclosure Size of the XPAA = 30.5 cm x 33 cm x 7.4 cm"]
-[5.537777423858643, 6.512927532196045, "[TT] Data Storage Volume of the MDHS = 130 GB"]
-[8.297927856445312, -0.611556887626648, "[TT] Absolute Accuracy of the Ice: edge location = \u00b1 12.5 km"]
-[9.907414436340332, 2.2868666648864746, "[FF] Design Quirk of the NuSTAR = Allows study of previously unwanted light"]
-[8.438823699951172, 7.204317092895508, "[TT] Number of Photo Diodes of the Limb Sensor Unit = Four pairs"]
-[6.074702739715576, 7.078103065490723, "[TT] Count Rate of the EPD-E = 10,000 to 50,000 counts/s"]
-[8.301897048950195, 4.702541828155518, "[FF] Data Collection of the EPIC248847494 star = Light Curve"]
-[10.20201301574707, 7.582902908325195, "[TT] Type of the Telescope Type = Cassegrain reflective telescope with correcting lenses (a catadioptric optical system)"]
-[3.081808090209961, 2.2218477725982666, "[FF] Coverage Area of the Copernicus Sentinel-2 = Puglia (Apulia)"]
-[6.153718948364258, 7.209939956665039, "[TT] Sampling Rate of the GPS OEM Sensor = 1/60 Hz"]
-[7.518984317779541, 3.7131831645965576, "[FF] Purpose of the NightPod = Compensate for orbital motion during imaging"]
-[12.204817771911621, 3.6256234645843506, "[TT] Potable Water Volume of the Pressurized Cargo = 600 liter"]
-[4.981082916259766, 3.065514326095581, "[TT] Prime Contractor of the THEMIS = Swales Aerospace"]
-[9.888701438903809, -1.4685280323028564, "[TT] Science Target Orbit Inclination of the ABEX = >27\u00ba"]
-[10.117588996887207, 3.287400484085083, "[FF] Affiliation of the CubeSat ADCS hardware and software = Stellenbosch University \u2013 Electronic System Laboratory (ESL), South Africa"]
-[6.019570827484131, 5.337177753448486, "[FF] Subsystem of the C&DH = Dedicated processor"]
-[5.523442268371582, 6.362100124359131, "[TT] Capacity of the Solid State Mass Memory = 2.4 Tbit"]
-[3.8059072494506836, 4.220455646514893, "[TT] Antenna Pattern Update of the RISAT-1 = Sept-Oct 2013"]
-[5.814820289611816, 2.5437827110290527, "[FF] Post-EPS VII Mission of the METimage = Unknown"]
-[7.109283924102783, 8.297674179077148, "[TT] SNR of the Spectral Bands = 450, 500, 500, 500, 500, 500, 500, 450"]
-[6.6088337898254395, -0.37525224685668945, "[TT] Repeat Cycle of the ResourceSat-1 = 24 days"]
-[3.0486299991607666, 1.928301215171814, "[TT] Data Availability of the Copernicus Sentinel-6 Poseidon-4 = Now"]
-[5.831789016723633, 5.862967491149902, "[TT] Number of Processors of the EnMAP = 4"]
-[8.18132495880127, 6.598036289215088, "[TT] Type of the TROPOMI = Pushbroom type imaging spectrometer"]
-[10.466094017028809, 3.334669828414917, "[TT] Architecture of the TechEdSat = 1U cubesat"]
-[7.442246437072754, 1.216135859489441, "[FF] Announcement Date of the OceanFinder = 18 September 2019"]
-[7.650304317474365, 6.379511833190918, "[TT] CONUS Observation Frequency of the ABI = Every 5 minutes (goal of 1 minute)"]
-[5.516999244689941, 5.098416328430176, "[TT] Operating System of the CGA = CentOS (Linux)"]
-[9.497684478759766, 9.073542594909668, "[TT] Data Rate for Images of the IRIS = Every 5\u201310 s"]
-[11.53171157836914, 6.487592697143555, "[TT] Energy Band of the NuSTAR = 3 to 79 keV"]
-[7.51047945022583, 1.8397334814071655, "[FF] Unknown of the Argo Profiling Floats = Argo Profiling Floats Bring New Era of In Situ Ocean Observations"]
-[8.648268699645996, 3.6537437438964844, "[FF] Measurement of the TSIS-1 = Sun's energy input to Earth"]
-[2.8637337684631348, 4.5771379470825195, "[TT] Bandwidth of the PALSAR-2 = 1.2 GHz"]
-[8.030842781066895, 6.140350341796875, "[FF] Instruments of the CAS500 = CSAR, Compact Advanced Payload Wide Swath, High Resolution Optical Sensor"]
-[7.840511798858643, 6.683557033538818, "[TT] Interferogram Scan Time of the IMG = \u2264 10 s"]
-[6.164649486541748, 6.992547512054443, "[TT] Data Rate of the Optical link = 2.8 Gbit/s (1.8 Gbit/s user data)"]
-[10.279107093811035, 3.2475922107696533, "[TT] Architecture of the CubeSat = Decentralized"]
-[10.137395858764648, 7.639833450317383, "[FF] Design of the Telescope = Compact, folded optical path, no optical obstruction"]
-[6.806617736816406, 4.3813157081604, "[FF] Type of the Payload Accommodation = Large"]
-[12.133149147033691, 7.606902122497559, "[TT] Mass of the IMG = 130 kg"]
-[5.432368755340576, 7.757915019989014, "[TT] EIRP of the Antenna = \u2265 54.6 dBW/ 1 beam \u2265 52.1 dBW/ 2 beams"]
-[3.9436259269714355, 1.400571584701538, "[FF] Objective of the SpaceX Falcon Heavy = Demonstrate performance"]
-[8.294347763061523, 6.221480846405029, "[FF] Clarity of the EPIC Data = Exceptionally clear view of Earth, largely unfettered by light from other sources"]
-[13.926490783691406, 7.173776149749756, "[TT] Power Input Voltage Range of the COVE Board = 6.0-8.4 V"]
-[7.948803901672363, 7.885061264038086, "[FF] Multispectral Mode Bands of the SPOT satellite constellation = Red, green and infrared bands of the visible spectrum"]
-[12.409579277038574, 7.003914833068848, "[TT] Anticoincidence Efficiency of the GRS = \u226590%"]
-[6.637300491333008, 8.809897422790527, "[FF] Measurement of the POLDER-P = Multidirectional and polarised solar radiation reflected by the atmosphere and Earth\u2019s surface"]
-[5.954168319702148, 7.585756778717041, "[TT] Sampling Rate of the OVM = 1 Hz"]
-[14.286038398742676, 3.1282460689544678, "[TT] Mass of the UKube-1 = ~3.5 kg"]
-[13.552371978759766, 5.890975475311279, "[TT] Solar Array Demand of the MTM = 2 x 5 kW"]
-[8.847339630126953, 5.567803382873535, "[TT] Performance of the Guidance Navigation and Control = Excellent"]
-[4.2849531173706055, 4.345919132232666, "[TT] Number of LEOLUTs of the COSPAS-SARSAT system = 45"]
-[9.166418075561523, 7.105515003204346, "[TT] Spatial Resolution of the HSC = 200-300 m"]
-[3.545370578765869, -0.9132139682769775, "[TT] Orbit of the STPSat-3 = Near-circular orbit"]
-[7.551905155181885, 6.898958683013916, "[TT] Operational Cadence of the Instrument = Stare for ~30 seconds"]
-[6.7149810791015625, 1.8474159240722656, "[FF] URL of the Communications with Earth = https://mars.nasa.gov/insight/mission/communications/"]
-[5.956173419952393, 5.3212456703186035, "[TT] Configuration of the IEPS = Single-string system"]
-[9.718901634216309, 8.478938102722168, "[TT] Instantaneous Field of View of the IFOV = 14.60 \u00b5rad"]
-[3.659029483795166, 4.74660062789917, "[TT] Imaging Modes of the RADARSAT-1 = Multiple"]
-[3.8792786598205566, 7.875006198883057, "[FF] Modulation Schemes of the Lithium 2 radio = GMSK for low Earth to near Earth orbit, theoretically supports BPSK"]
-[8.625983238220215, 1.138094186782837, "[FF] Interruptions of the Aquarius sensor = During much of the second half of 2012 there were interruptions in the precise geodetic pointing, and some safe hold events"]
-[10.996330261230469, 0.6430956125259399, "[FF] Location of Exoplanets of the WFIRST = Between three and 10 times Earth\u2019s distance from the Sun"]
-[5.470162868499756, 6.272064208984375, "[TT] EEPROM Capacity of the RAD750 SBC = 4 MB"]
-[6.439886569976807, 7.605220317840576, "[TT] Dat Quantization of the Instrument = 10 bit"]
-[11.062954902648926, 5.863860130310059, "[FF] Requirement of the Candidate Materials = Resistant to the effects of AO"]
-[8.379300117492676, 7.9660234451293945, "[TT] Type of Array of the SWIR = HgCdTe"]
-[10.813677787780762, -0.2682996690273285, "[FF] Mission Status of the Tandem-L = Proposal"]
-[7.403181076049805, 2.335820436477661, "[TT] Global Mapping Achievement of the Satellite = 43.6%"]
-[10.285819053649902, 3.958463668823242, "[TT] Retraction Status of the AstroTubeTM Boom = Retracted"]
-[4.727836608886719, 0.5631217360496521, "[TT] Operational Date of the GOES-18 = Early 2023"]
-[5.368507385253906, 5.523758411407471, "[TT] Message Format of the SpW = ECSS PUS"]
-[4.6446919441223145, 7.949034690856934, "[TT] Operating Frequency of the UHF Transceiver = 435-438 MHz"]
-[4.979624271392822, 1.4955339431762695, "[TT] Funding Approval Year of the MiRaTA = 2013"]
-[6.729257106781006, 6.406063556671143, "[TT] Cycle Time of the Event Processor = 50 ms"]
-[10.795297622680664, 7.484738826751709, "[TT] Swath of the LISS-3 = 140 km"]
-[6.047819137573242, -0.4920305907726288, "[TT] Mission Duration of the Spacecraft = Minimum of 3 years"]
-[6.041610240936279, 4.69117546081543, "[FF] Function of the Housekeeping Computer = Responsible for communications with the ground station and collecting satellite telemetry"]
-[5.341817855834961, 2.6594276428222656, "[TT] Agency of the KySat-2 = MSU (Morehead State University), University of Kentucky (UKy), Kentucky Space LLC"]
-[9.063267707824707, -1.151125431060791, "[TT] Orbit of the INSAT-3D = Elliptical GTO (Geosynchronous Transfer Orbit)"]
-[6.297159671783447, 1.1793653964996338, "[FF] Environment Density of the GRB 130925A = Low"]
-[5.59081506729126, -1.9927153587341309, "[FF] Instruments of the GEO-KOMPSAT-2A = Advanced Meteorological Imager (AMI) and the Korean Space Environment Monitor (KSEM)"]
-[6.328859329223633, 6.482170104980469, "[FF] Duration of the TTTC = Longer than the data take itself"]
-[9.084352493286133, 5.006862640380859, "[FF] Operation of the Attitude & Pointing Control Subsystems = ASTERIA"]
-[6.8545098304748535, 5.547003746032715, "[TT] Quantity of the P-PODs = 4"]
-[6.944314956665039, -0.5204253792762756, "[TT] Local Solar Time on Descending Node of the CBERS-2B = 10:30 hours"]
-[4.852169513702393, 3.2851223945617676, "[TT] Manufacturer of the AlSat-2A = Astrium"]
-[6.9998555183410645, -0.8142369985580444, "[TT] Orbital Period of the TOI 1807 b = 13 hours"]
-[10.08527660369873, -1.4814021587371826, "[TT] Inclination of the COSPAS Satellites Inclination = 83\u00ba"]
-[13.36881160736084, 6.815605163574219, "[TT] Spacecraft Power of the Telescope = 2.5 kW"]
-[10.791666030883789, 7.424531936645508, "[TT] Swath Width of the TeLEOS-1 = 12 km"]
-[6.83067512512207, 5.906630039215088, "[TT] Quantity of the Mandrels = 54"]
-[5.026015281677246, 7.574581146240234, "[FF] Components of the E1/E5 active antenna array = E1/E5 active antenna array with calibration network"]
-[13.40539264678955, 6.760913848876953, "[TT] Power Generation of the Resurs-O1 spacecraft = 500 W (average), 1200 W (peak)"]
-[10.575803756713867, 5.491873264312744, "[TT] Principal Investigator of the Heat Probe = Tilman Spohn"]
-[9.153694152832031, 7.644461154937744, "[TT] MS (Multispectral) of the Medium resolution = 0.8-0.9 \u00b5m (NIR2)"]
-[7.6750054359436035, 2.150315046310425, "[TT] Primary Use of the Band 3 = Heat source, night cloud"]
-[14.678756713867188, 6.656295299530029, "[TT] Capacity of the Battery = 11.8 Ahr"]
-[9.009594917297363, 7.6457977294921875, "[TT] Pixel Size of the IIR = 1 km"]
-[6.700721740722656, 4.50083589553833, "[FF] Design and Analysis of the FDIR = Ongoing"]
-[4.953836441040039, 8.270448684692383, "[TT] Transmit Bandwidth of the Radar = 1 MHz"]
-[5.6703643798828125, 6.2203569412231445, "[TT] Data Storage of the ISIR = Two standard Exabyte-8505c 8mm tape recorders"]
-[4.308675765991211, 4.342842102050781, "[TT] Number of GEOLUTs of the COSPAS-SARSAT system = 19"]
-[4.274749279022217, 7.3951096534729, "[TT] Frequency Allocation of the Antennas = 437.575 MHz (downlink), 145.860 MHz (uplink)"]
-[5.394611835479736, 2.222238540649414, "[FF] Flown Mission of the MOMS-02 = MIR/Priroda"]
-[9.091442108154297, 4.499661445617676, "[TT] Sun Direction Tolerance of the SCTE = 5\u00ba"]
-[6.680237770080566, 4.48568058013916, "[FF] Operation Mode of the SMOS = Autonomous mode using the FDIR (Failure Detection Isolation and Recovery) concept"]
-[5.909149646759033, 2.033860683441162, "[FF] Monitored Regions of the GEOGLAM Crop Monitor = Central and Eastern Europe, Southwestern Russia"]
-[4.525843143463135, 3.122004985809326, "[TT] CEO of the CesiumAstro = Shey Sabripour"]
-[9.765869140625, -0.575473427772522, "[TT] Orbit Altitude of the Fregat = Around 450 km"]
-[10.7892427444458, -1.1593613624572754, "[TT] Altitude of the SLATS = 643 x 450 km"]
-[8.373673439025879, 1.2916004657745361, "[TT] Range Sidelobes Suppression of the RainCube = Less than -55 dB at 500 m and -70 dB at 1 km"]
-[8.2044038772583, 1.909820556640625, "[TT] Typical Number of Storms Per Year of the Arabian Sea = One or two"]
-[6.052418231964111, 6.173894882202148, "[TT] Data Transfer Time to Ground of the Satellite = More than an hour"]
-[7.539843559265137, 3.7969536781311035, "[FF] Planned Instruments of the FY-3RM = Ku/Ka band radar, microwave sounding and imaging instruments"]
-[10.54382610321045, 2.1441879272460938, "[FF] X-ray Emission Models of the XMM-Newton = Clouds of dust and gas partially block the X-ray light, emission is reflected off the inner edge of the accretion disk"]
-[4.879966735839844, 1.39948308467865, "[TT] Heritage of the ADCS = Previous GNB missions"]
-[4.178165912628174, 0.973325788974762, "[FF] Launch Date of the H-IIA Launch Vehicle No. 23 = Dec. 26, 2013"]
-[8.603361129760742, 0.2880266606807709, "[TT] Comets Discovered of the SOHO = More than 3000"]
-[3.8478686809539795, 4.389836311340332, "[TT] Image Acquisition Frequency of the RADARSAT-2 = Almost every 24 days"]
-[9.242799758911133, 7.055418014526367, "[FF] Spatial Resolution of the SGR-ReSI = Lower"]
-[9.425549507141113, 6.075382232666016, "[TT] Incidence Angle Range of the Scatterometer = 0 to 48\u00ba"]
-[2.9019110202789307, 4.213707447052002, "[TT] Emergency Observation Period of the PALSAR-2 = January 6-16, 2016"]
-[7.4650373458862305, 2.4774749279022217, "[TT] Value of the Joint Sky Coverage = ~18%"]
-[3.4472391605377197, 3.616999387741089, "[FF] Design and Status Presentation Date of the PAZ Ground Segment = June 3-5, 2014"]
-[7.2359538078308105, 5.120055675506592, "[FF] Transmission Profile of the Etalon = Unknown"]
-[4.912021636962891, 0.293708860874176, "[FF] Impact Date of the DART = Coming September"]
-[7.127956867218018, 6.614008903503418, "[TT] Threshold Tables of the GLM = Can be uploaded to the instrument"]
-[4.348345756530762, 7.149412631988525, "[FF] Application of the Mie Scattering Theory = Estimation of specific attenuation and radar reflectivity for Ku-band"]
-[4.881772041320801, 0.5441002249717712, "[TT] Launch Date of the Beresheet = Mid-February"]
-[11.299431800842285, 5.325828552246094, "[FF] Size of the Chondrules = Submillimeter to millimeter"]
-[10.277195930480957, 5.16808557510376, "[TT] Number of HTS Experiments of the HTSSE-II cryogenic subsystem = 8"]
-[4.762063503265381, 6.754745960235596, "[FF] Communication of the ALOS-2 ground system = Data relay communication and very fast X-band direct downlink"]
-[6.220006942749023, 6.297074317932129, "[TT] On-Station Time of the DSCOVR = 110 days"]
-[6.399684906005859, 1.5299001932144165, "[TT] Expected Completion Date of the Europa Clipper = End of 2022"]
-[6.097898483276367, 7.013798236846924, "[TT] Data Compression of the Instrument = None"]
-[8.14831256866455, 3.972025156021118, "[FF] Purpose of the SEISS = Monitors near-Earth particles and the electromagnetic environment, which includes electrons, protons and heavy ions"]
-[9.776690483093262, -0.39496272802352905, "[TT] Altitude of the Spacecraft = 645 km"]
-[4.92390251159668, 1.1705368757247925, "[TT] Operation Date of the TANSO-FTS-2 = 12-14 December 2018"]
-[3.2804179191589355, 5.010003089904785, "[TT] SAR Payload Accessible Swath Width of the RCM = 500 km"]
-[11.362018585205078, 5.866866111755371, "[TT] MLI Material of the Spacecraft = Aluminum"]
-[8.026658058166504, 5.070501327514648, "[FF] Required Precision of the O3 Profile = 3%"]
-[7.876325607299805, 8.825419425964355, "[TT] Wavelength Interval of the PAN = 0.50 - 0.85 \u00b5m"]
-[10.92070484161377, 4.078239440917969, "[TT] Formation of the TSX and TDX = Close Helix"]
-[4.509174346923828, 3.353628396987915, "[TT] Location of the Ground Station = NTU"]
-[9.303964614868164, 3.9042625427246094, "[FF] Magnetometer Suite of the RAX-1 = Two internally mounted tri-axial magnetometers and four dual axis magnetometers mounted on external faces of the satellite"]
-[6.54135799407959, 6.4862470626831055, "[FF] Communication of the EDRS-A = Secure laser communication to receive data from the low-Earth orbiting satellites and beams the information back to Earth via radio frequency"]
-[13.170931816101074, 7.353824615478516, "[FF] Power Savings of the ADCS = Individual OBCs can be powered off without the operation of the others"]
-[9.65311336517334, 8.008590698242188, "[TT] Mechanism of the Active Optics = Actuators"]
-[10.071006774902344, 4.371936321258545, "[TT] Usage of the Magnet-Torquer Bars = Unload the kinetic momentum of the 3 RWs"]
-[6.327480316162109, 1.1538033485412598, "[FF] Observation Period of the NASA Satellite Sensors = May 29 to June 6"]
-[7.280833721160889, 1.676649570465088, "[FF] Scientific Instruments of the Trace Gas Orbiter = High-resolution color imaging system, High-resolution neutron detector, Two spectrometer suites"]
-[10.812128067016602, -0.2702264189720154, "[TT] Operator of the TanDEM-X = German Space Operations Center (GSOC)"]
-[2.310016393661499, 2.7748396396636963, "[TT] Co-PI of the EPI-Lo = Ralph McNutt"]
-[8.270578384399414, 3.723677158355713, "[FF] Objective of the ASME = Monitor the changes in sample thickness as a result of atomic oxygen erosion"]
-[6.1729512214660645, 4.732115745544434, "[FF] Function of the GEOLUTs = Process the satellite signal"]
-[14.212227821350098, 3.1351966857910156, "[TT] Mass of the TechDemoSat-1 = 157 kg"]
-[4.920398712158203, 8.329586029052734, "[TT] Frequencies of the SMMR = 6.6 GHz, 10.7 GHz, 18.0 GHz, 21.0 GHz, 37.0 GHz"]
-[9.277612686157227, 3.197629928588867, "[FF] Optical Design of the ASPIICS = Classically occulted Lyot coronagraph"]
-[6.849003314971924, 7.754178047180176, "[TT] Reflector Dimension of the Antenna System = 60 cm"]
-[6.095390796661377, 5.187074184417725, "[FF] Interfaces of the Mission Data Sources = Two cold redundant interfaces and harnesses"]
-[9.430081367492676, 6.929973602294922, "[TT] Spatial Locations of the Alice = 32"]
-[8.923849105834961, 2.7932193279266357, "[FF] Purpose of the IBEX = Provide images of the solar system's boundaries"]
-[9.097647666931152, 8.17928695678711, "[TT] Number of Groups of the Optic\u2019s Layers = 10"]
-[11.192703247070312, 3.639309883117676, "[TT] Attitude Control of the CNAPS = 5\u00ba (3\u03c3)"]
-[5.19995641708374, 6.974684238433838, "[TT] Downlink Speed of the GOMX-3 = 19.2 kbit/s"]
-[5.1298747062683105, 7.149555683135986, "[TT] Telemetry Downlink Data Rate of the GIOVE-B = 31.250 kbit/s"]
-[10.452089309692383, 6.375161647796631, "[FF] Mirror Technology Workshop Date of the JWST = June 16-18, 2009"]
-[7.694705009460449, -0.8697149753570557, "[TT] Ground Systems CDR Date of the ICESat-2 = Sept. 6, 2013"]
-[6.6568732261657715, 0.24977128207683563, "[TT] Launch Date of the CryoSat-2 = April 8, 2010"]
-[4.447195053100586, 3.767930269241333, "[TT] Space Infrastructure of the Galileo = 26 satellites"]
-[3.8571910858154297, 6.495151519775391, "[TT] Look Angles of the Antenna Subsystem = 42.62\u00ba and 49.38\u00ba"]
-[8.016794204711914, 8.95406723022461, "[FF] Extinction Cross Sections of the Species = Wavelength Dependent"]
-[10.03664493560791, 3.773872137069702, "[FF] Orientation of the SERB Nanosatellite = +Z pointing to the Sun, +Y along the longitudinal nanosatellite axis, and +X along the deployed solar arrays"]
-[5.245750904083252, 0.5879009962081909, "[TT] Test Period of the TOR = January 15 through February 15, 2008"]
-[13.164294242858887, 7.28032112121582, "[TT] Power Consumption of the CEASE-2 = 1.7 W"]
-[3.0756266117095947, -0.052351854741573334, "[TT] Orbital Slot of the GSAT-0209 = C02"]
-[11.459299087524414, 3.9799349308013916, "[TT] ACS Testing Device of the AeroCube-4 = Simple single degree-of-freedom hanging string"]
-[10.815372467041016, 7.453775405883789, "[TT] Swath of the MWR = 390 km"]
-[5.849170207977295, 0.2405480295419693, "[TT] Launch Window of the Juice = 5\u201325 April 2023"]
-[8.916119575500488, 7.705044269561768, "[FF] Spatial Resolution of the Pushbroom imager = Pan = 2.5 m, MS = 10 m, SWIR = 20 m"]
-[8.839893341064453, 3.434520721435547, "[FF] Mission of the SPATIUM-I = Demonstrate technology aimed at electron density measurement and three-dimensional mapping of ionosphere"]
-[10.301469802856445, 8.032546043395996, "[TT] Aperture Diameter of the Telescope = 310 mm"]
-[6.633112907409668, 5.159500598907471, "[FF] Complement of the DCS = Unknown"]
-[8.936962127685547, 7.993013858795166, "[FF] Type of the BLITS = Ball Lens In The Space"]
-[5.132996082305908, 7.6818461418151855, "[TT] Minimum receiver sensitivity of the Cross dipole antenna = -112 dBm"]
-[3.614731788635254, 4.689817905426025, "[FF] SAR Elements of the SAR-VTB = Existing developments"]
-[6.317885875701904, -1.3061858415603638, "[TT] Launch Campaign of the GRACE-FO Satellites = 2018"]
-[8.574089050292969, 7.998653411865234, "[TT] Spectral resolution of the Imager = 0.2 cm -1"]
-[8.118205070495605, 0.9763728976249695, "[FF] Soil Moisture Measurement of the GRACE-FO = Unknown"]
-[8.314225196838379, 6.335142612457275, "[TT] X Axis Reporting Rate of the SSM = 10 readings/s"]
-[6.980857849121094, 7.036046981811523, "[TT] Type of the Master Oscillator (MO) = Low-mass, compact micro non-planar ring oscillator (m- NPRO) laser"]
-[14.11676025390625, 3.071444034576416, "[TT] Mass of the \u00b5SCIA = 6 kg"]
-[10.963412284851074, 2.0641610622406006, "[FF] Article Date of the XMM-Newton = 20 January 2020"]
-[10.076654434204102, 1.2631945610046387, "[TT] Galaxy Light Travel Time of the GRB 191016A = 11.7 billion years"]
-[11.35161304473877, 5.869485378265381, "[TT] Composition of the Galinstan = Gallium, Indium, Tin"]
-[9.04123592376709, 1.466552972793579, "[FF] Navigation of the New Horizons = State-of-the-art"]
-[4.8516764640808105, -1.7259416580200195, "[FF] Image Credit of the Analog-1 rover = ESA\u2013A. Koehler"]
-[10.218733787536621, 5.793562889099121, "[TT] Temperature Derivation Samples of the Instrument = 20 samples per spectrum"]
-[3.8175129890441895, -0.7123117446899414, "[FF] Orbit of the TET-1 = Low Earth Orbit"]
-[8.589256286621094, 2.2105579376220703, "[TT] Operation Status of the WIND = Nominally"]
-[11.300250053405762, 6.488305568695068, "[TT] Measurement Range of the Faraday Cup Ion Detectors = Up to 8 keV"]
-[7.780332088470459, 4.80021333694458, "[FF] Step 1 Operation of the TRUTHS = LDs illuminate (underfill) first the CSAR cavity and then the transfer radiometer (TR)"]
-[7.6167073249816895, 1.948715329170227, "[TT] Orbit Coverage of the CATS = Tropics and mid-latitudes"]
-[9.24301815032959, 3.184173822402954, "[FF] Presentation Date of the Magnetospheric Multiscale (MMS) = Feb. 24-27, 2014"]
-[6.881824016571045, 7.490983963012695, "[TT] ADC Resolution of the MuREM = 10 bit"]
-[4.717996120452881, -1.2122818231582642, "[TT] Launch Date of the Beijing-3 = 11 June 2021"]
-[5.6298017501831055, 6.553666591644287, "[FF] Data Stream of the MDHS = 1.23 Gbit/s"]
-[8.325268745422363, 7.104171276092529, "[TT] Number of Images Selected of the PolyCam = Just over 2,100 images"]
-[5.690316677093506, 5.3339152336120605, "[FF] Connectivity of the SES-17 = High-speed connectivity with a high degree of flexibility"]
-[7.1385297775268555, 6.922433853149414, "[TT] Operating Range of the Metrology Laser = ~ 6 mm"]
-[13.208229064941406, 7.24398946762085, "[TT] Power Consumption of the KGI-4C = 6.8 W"]
-[6.859730243682861, 2.926560878753662, "[TT] Budget of the MethaneSAT = $88 million"]
-[7.724185466766357, 0.4613810181617737, "[TT] Orbit of the Lunar IceCube = Highly inclined elliptical lunar orbit"]
-[5.218415260314941, 3.0352022647857666, "[TT] Type of the EARS = EUMETSAT Advanced Retransmission Service"]
-[9.165785789489746, 5.244405269622803, "[TT] Pointing Accuracy of the IRS-1C and IRS-1D = Roll and pitch = \u00b10.15\u00ba, yaw = \u00b10.2\u00ba"]
-[6.445641994476318, 5.9305500984191895, "[TT] Quantity of the Clock monitoring and control units = 2"]
-[8.524977684020996, 8.929758071899414, "[FF] Spectrometer Resolution of the PACS = Lower than HIFI"]
-[4.497135639190674, 3.016122341156006, "[FF] Location of the NSOF = Suitland, MD"]
-[4.494637966156006, 7.073277473449707, "[TT] Data Downlink of the ISUAL instrument = S-band"]
-[13.477474212646484, 2.903588056564331, "[TT] Mass of the Satellite = 250 kg"]
-[9.480484962463379, 6.99521017074585, "[TT] Spatial Resolution of the SLSTR = 1 km"]
-[9.026764869689941, 6.931215286254883, "[TT] Image Scale of the OSIRIS = About 2 mm/pixel"]
-[5.108314514160156, 3.4434170722961426, "[TT] Manufacturer of the CMS instrument = SSBV SGS (Space & Ground Systems)"]
-[7.447850704193115, 4.179742813110352, "[FF] Sensor Complement of the RaInCube = Unknown"]
-[9.545888900756836, 6.225268363952637, "[TT] Incidence Angle of the Wide ultra fine = 30-50\u00ba"]
-[7.064218521118164, 7.220118999481201, "[TT] Wavelength of the Laser = 830 nm"]
-[8.285253524780273, 8.143467903137207, "[TT] Detector Count of the VNIR and SWIR focal plane assemblies = 12"]
-[5.037480354309082, 8.352494239807129, "[TT] Bandwidth of the MWR = 1 GHz"]
-[5.541449546813965, 6.436879634857178, "[TT] Capacity of the HSDR = 8 GByte"]
-[6.167805194854736, 3.1370553970336914, "[TT] Third-Quarter Operating Loss of the BlackSky = $48.9 million"]
-[10.091800689697266, -2.6677212715148926, "[TT] Quantity of the MMFU with SDR-SDRAM = 2"]
-[2.285327196121216, 2.7715325355529785, "[TT] Co-PI of the EPI-Lo = Don Mitchell"]
-[4.6981587409973145, 0.7299224734306335, "[TT] Launch Failure Date of the HAUSat-1 = July 26, 2006"]
-[8.97894287109375, 0.4593313932418823, "[TT] Mass of the Boulder = 230 tons"]
-[4.317446708679199, 7.279792308807373, "[TT] Frequency Bands of the Communication System = Ku-/Ka-bands"]
-[9.483555793762207, 7.116539001464844, "[TT] Resolution of the MI = 500 m"]
-[10.014671325683594, -1.5672959089279175, "[TT] Orbit Inclination of the Odin = 97.77\u00ba"]
-[7.28631067276001, 2.981891632080078, "[TT] Total Cost of the GHGSat-D = 1% of other greenhouse gas measurement missions"]
-[5.743125915527344, 1.2202521562576294, "[TT] First 883-GHz Cloud Radiance Map Date of the ICIR = June 20, 2017"]
-[9.905738830566406, 0.7828326225280762, "[TT] Measurement Area of the GOSAT-2 = 10 km diameter"]
-[7.460063457489014, 2.4145333766937256, "[TT] Measurement Category of the TAIKI = Multi-purpose imagery (land), Vegetation"]
-[4.159359931945801, 6.234396457672119, "[TT] Location of the GPS patch antenna = Wake surface of the satellite"]
-[4.959077835083008, 5.638850212097168, "[FF] Payload of the ZACUBE-2 = SDR-based payload that will provide AIS and VDES services"]
-[5.792433738708496, -0.8956774473190308, "[TT] Design Life of the Terra = 6 years"]
-[6.693581581115723, 8.722586631774902, "[TT] Polarization sensitivity of the Spectral Bands = Band 1 \u2264 5%, Band 2-8 \u2264 2%"]
-[8.455352783203125, 1.9779139757156372, "[TT] Cloud Deck Resolution of the CIPS = 2 km"]
-[7.143002510070801, 8.553837776184082, "[TT] Reflected Radiation Channel Accuracy of the ISP-2 = 1%"]
-[13.712060928344727, 2.776582956314087, "[TT] Launch Mass of the NOAA POES series fifth generation satellites = 2232 kg"]
-[8.846270561218262, 5.655162811279297, "[TT] Pointing Control of the LRI instrument = Internal"]
-[9.571589469909668, 7.180171012878418, "[TT] Spatial Resolution at Nadir WV and TIR of the MVIRI = 5 km"]
-[11.40677547454834, 5.723231315612793, "[TT] Composition of the Copper Alloy = 8% W, 9% Ag, 5% Pb"]
-[8.880623817443848, 7.907238960266113, "[TT] Number of Pixels of the MWHS-II = 98/scan"]
-[4.839661121368408, -0.3064728081226349, "[TT] Launch Time of the Falcon 9 = 12:16 UTC"]
-[4.644081115722656, 0.7029215693473816, "[TT] Launch Date of the SARah-1 = 13 June 2022"]
-[8.502490043640137, 3.096282720565796, "[FF] Page Numbers of the Very-Wide-Filed Ultraviolet Sky Survey = 179-180"]
-[11.982084274291992, -0.35519951581954956, "[TT] Mission Manager of the TESS = NASA's Goddard Space Flight Center"]
-[3.6433920860290527, 4.558912754058838, "[TT] Location of the Synthetic Aperture Radar (SAR) = Cloudy tropical location like the Tonga archipelago"]
-[12.435120582580566, 0.6295363306999207, "[TT] Number of Cameras of the PLATO = 24, 18, 12 or 6"]
-[8.16191291809082, 7.913310527801514, "[TT] Measurement Range of the Spectral Channels = 1.6 to100% albedo"]
-[9.977739334106445, 3.2079732418060303, "[FF] Primary Goals of the Dellingr = Develop a cost-effective Center model for CubeSat development, Develop tailored, lean, and scalable end-to-end systems, Determine lessons learned, and apply them to the next generation of satellites"]
-[5.0620293617248535, 4.427000045776367, "[TT] Number of Satellites of the Starlink = 835"]
-[7.04439115524292, 2.603689670562744, "[FF] Purpose of the ZACube-2 = Track boats along South Africa's coasts and detect forest fires"]
-[1.7440425157546997, 4.561846733093262, "[FF] N/A of the gas tank = N/A"]
-[5.142094612121582, 0.6587947607040405, "[TT] Observation Start Date of the SUVI = June 24, 2022"]
-[9.05335807800293, 8.055307388305664, "[TT] CCD Line Read-Out Rate of the Focal Plane Module = 6.5 MHz"]
-[5.666743278503418, 0.9694693088531494, "[TT] Engagement Date of the SES-14 Satellite = 4 September 2018"]
-[12.023848533630371, 6.317768096923828, "[FF] B/C Flux Ratio of the AMS = Well described by a single power law B/C= kRd with d = -0.333\u00b10.015"]
-[13.479433059692383, 6.911806106567383, "[TT] Charge Carrier of the ASPOC = Indium"]
-[5.561269283294678, 5.6836347579956055, "[TT] Model of the OHDH = Motorola 68332 microprocessor"]
-[5.6415910720825195, 6.083859443664551, "[FF] Memory Type of the PDHS = Memories for burst data formatting"]
-[10.507771492004395, 2.4081876277923584, "[TT] Number of X-ray mirror module assemblies of the IXPE observatory = 3"]
-[10.304896354675293, 3.1386911869049072, "[TT] Unknown Failure Rate of the CubeSats = 33%"]
-[7.718177795410156, 4.534048080444336, "[FF] Silicon Tracker of the AMS-02 = Measures charged particle bending"]
-[5.975187301635742, 2.4018592834472656, "[TT] Launch Date of the WorldView Legion satellites = September 2021"]
-[7.77358865737915, 1.9760940074920654, "[FF] Spectral Range and Resolution of the OCI = Advance the ability to distinguish between different species of phytoplankton compared to predecessor satellite instruments"]
-[8.561660766601562, 4.670295238494873, "[FF] Components of the ADCS = Sun sensors, magnetometers, rate gyro"]
-[7.7719316482543945, 8.62452507019043, "[TT] Band of the Microbolometer = LWIR"]
-[3.8424601554870605, 1.1388858556747437, "[TT] Speed of the Falcon-9 first stage = Upwards of 1300 m/s"]
-[3.7872314453125, 6.669826507568359, "[TT] VDES Antenna Polarization of the NorSat-2 = Circular"]
-[6.013945579528809, 5.6707539558410645, "[TT] Redundancy of the CFI Signal Generator Chains = Two chains"]
-[7.365278720855713, -0.16641759872436523, "[TT] Hibernation Start Time of the Philae = 00:36 GMT"]
-[4.37730073928833, 7.8974409103393555, "[TT] Uplink Frequency of the DRT = 402.75\u00b10.1 MHz"]
-[11.489936828613281, 3.5138614177703857, "[TT] Type of the UK-10 ion thruster hollow cathode = UK-10"]
-[7.938011646270752, 5.775742530822754, "[FF] Rescaling Method of the Landsat images = Bilinear interpolation"]
-[7.2642436027526855, 6.025890827178955, "[FF] Quantity of the VIS = 5"]
-[11.161441802978516, 1.2209675312042236, "[FF] Sensitivity of the LISA = Lower frequency than LIGO"]
-[3.9233787059783936, 9.735565185546875, "[TT] Bandwidth (GHz) of the ICI-5 = 6"]
-[5.229062080383301, 1.4134690761566162, "[FF] Deployment Date of the HawkEye 360 = Not Provided"]
-[4.77781867980957, 0.4549679160118103, "[TT] Launch Date of the Earth Return Orbiter = Fall 2027"]
-[5.02302360534668, 3.510533571243286, "[TT] Manufacturer of the GTR = NovAtel Inc."]
-[8.129350662231445, 1.202659010887146, "[TT] First Precipitation Observation Date of the RainCube = August 27, 2018"]
-[13.529708862304688, 2.8253443241119385, "[TT] S/C Mass at Launch of the RADARSAT-1 = 2750 kg"]
-[11.946616172790527, 4.978281497955322, "[TT] Electronics Package Volume of the FlaPS = 290 cm3"]
-[4.171063423156738, 7.325233459472656, "[TT] Band of the WINDS/Kizuna = Ka-band"]
-[6.5827860832214355, 5.696582317352295, "[FF] Custom Design of the Actel RH1280 = Digital square-law processor module and the RFI-threshold detection circuitry"]
-[5.615128040313721, 6.3622355461120605, "[TT] Capacity of the SSB (Solid-State Buffer) cards = 192 GB"]
-[5.5756449699401855, 6.993278503417969, "[TT] Telecommand Data Rate Range of the TTCS = 2-8 kbit/s"]
-[8.468192100524902, 8.34886646270752, "[TT] Spectral Resolution of the Instrument = 85.4 cm -1 (1.7 nm @ 450 nm)"]
-[4.921882152557373, 2.115999698638916, "[FF] Mission Design of the Geosat ERM = G. H. Born, J. L. Mitchell, G. A. Heyler"]
-[4.5926737785339355, 5.848710060119629, "[FF] Main Payload of the GOMX-3 = SDR (Software Defined Radio)"]
-[10.72895336151123, 2.740654230117798, "[TT] Altitude of the 7 microsatellites = 515 km"]
-[4.607317924499512, 0.5291211009025574, "[TT] Launch Date of the M3MSat = June 2016"]
-[4.790663719177246, 7.301079750061035, "[TT] Ka-band Data Rate of the CASCADE = Up to 2.1 Gbit/s using higher order modulations"]
-[6.824281215667725, 3.117098569869995, "[FF] Simulation and Materials Database of the Oculus-ASR = Improved"]
-[7.313478946685791, 4.829798221588135, "[FF] Function of the Reflector Deployment Assembly (RDA) = Stows the MR and deploys it to the on-orbit configuration"]
-[5.304520130157471, 0.4190307557582855, "[TT] Reentry Date of the Long March 5B = May 8"]
-[5.92523193359375, 6.871697425842285, "[TT] Data Volume of the ScaRaB = 18 Mbit/orbit"]
-[8.92612361907959, 5.714413166046143, "[TT] Position Accuracy of the Detector = 30 arcsec"]
-[8.928387641906738, 7.591063499450684, "[TT] Pixel Size of the Main Camera = 300 m"]
-[8.395639419555664, 5.469282627105713, "[TT] Calibration Accuracy of the IMI = Higher than two-dimensional interferometric radiometers"]
-[7.60131311416626, 1.9603900909423828, "[FF] Unknown of the Argo Project = Global ocean observations for understanding and prediction of climate variability"]
-[9.73051929473877, -0.6247451305389404, "[TT] Orbital Altitude of the SZ-7 = ~330 km"]
-[11.930180549621582, 5.032430171966553, "[TT] Size of the HORYU-2 = 350 mm x 310 mm x 315 mm"]
-[6.607669353485107, 1.6914955377578735, "[FF] DOI of the NICER = 10.1117/12.2056811"]
-[3.824220657348633, 7.926007270812988, "[TT] Modulation of the Modulator = QPSK"]
-[1.3266322612762451, 1.899300456047058, "[TT] Cargo Weight of the HTV-7 = 6200 kg"]
-[8.9799222946167, -1.1642589569091797, "[FF] Final Position of the EDRS-A = 9\u00b0E, over Europe"]
-[5.280483722686768, -0.32605957984924316, "[TT] End of Life Date of the Odin = Dec 2023"]
-[6.401107311248779, 3.739713430404663, "[TT] Backup of the GOES-15 = Available"]
-[5.054502487182617, 1.9998899698257446, "[TT] Operation Status of the TacSat-2 = Nominal as of 2007"]
-[5.976652145385742, 1.471129059791565, "[FF] Collision Date of the Small Near-Earth Objects = 21 November 2002"]
-[7.933976650238037, 2.3411600589752197, "[FF] Parameter of the 3D Climate Models = Various"]
-[5.370981693267822, 1.1298032999038696, "[FF] Presentation Date of the ASIM = Sept. 24-28, 2007"]
-[5.248777389526367, 6.608611106872559, "[FF] Data Distribution Telemetry of the MTG SpaceWire Architecture = 295 Mbit/s (Imager S/C) and 557Mbit/s (Sounder S/C)"]
-[5.213871955871582, 2.818887233734131, "[TT] Testing Location of the GOES-T = Lockheed Martin Corporation\u2019s Littleton, Colorado, facility"]
-[8.217857360839844, 7.12259578704834, "[TT] Output word size of the Full-scan Imaging = 6 bits, 6 bits"]
-[8.439570426940918, 4.846451759338379, "[FF] Tracking Method of the Aluminum Spheres = Radar tracked by the U.S. Space Command and optically tracked by a world-wide network of university students and amateur observers with \"Go To\" telescopes"]
-[6.383402347564697, 4.796173095703125, "[FF] Estimated Code Reuse of the VMOC = Soon approach 95%"]
-[6.00526762008667, -0.3738820254802704, "[TT] Operation Duration of the EO-1 = 10 years"]
-[4.899163246154785, 7.226699352264404, "[TT] RF Link Speed of the BILSAT-1 = 2 Mbit/s"]
-[6.805770397186279, 4.815085411071777, "[FF] GMU Modification of the I-COUPS = Addition of CTU and modification of GMU"]
-[6.019954204559326, 5.1605448722839355, "[TT] Platform of the AOCS = Standard platform AOCS"]
-[5.915741443634033, 2.476619005203247, "[FF] Planned Launch Quarter of the WorldView Legion satellites = First quarter of 2021"]
-[6.940739631652832, 7.054878234863281, "[FF] Reliability of the Laser Diodes = Equally reliable"]
-[9.239343643188477, 7.036280155181885, "[TT] Resolution of the Extra Fine mode = 5 m"]
-[10.114594459533691, 8.092626571655273, "[TT] Focal Length of the Optical Telescope Assembly = 10 m"]
-[7.619311809539795, 8.834315299987793, "[TT] Spectral Bands of the LISS-IIM = 0.45-0.52 \u00b5m, 0.52-0.59 \u00b5m, 0.62-0.68 \u00b5m, 0.77-0.86 \u00b5m"]
-[9.288155555725098, 3.1084160804748535, "[TT] Integrated Irradiance Values of the Solar SXR Spectra = 0.1-7 nm"]
-[8.50156307220459, 7.446270942687988, "[TT] Type of the Camera Sensor = EEV CCD04-06 image sensor + chip set"]
-[7.908951759338379, 0.3997349143028259, "[TT] Moon Azimuth of the CUMULOS = 188.2\u00b0"]
-[3.999720335006714, 6.459814071655273, "[TT] Antenna Array of the OBRC instrument = Uncontrolled"]
-[4.6231369972229, 7.142249584197998, "[TT] TT&C Downlink of the QSat = S-band with a data rate of 1 or 100 kbit/s"]
-[9.794469833374023, -0.543125569820404, "[TT] Altitude of the Science Orbit = 891 km"]
-[8.149507522583008, -1.0823462009429932, "[TT] First Height Measurements of the ICESat-2 = 3 October"]
-[14.563994407653809, 6.665519714355469, "[TT] Battery Capacity of the Power subsystem = 66 Ah"]
-[7.62376594543457, 6.861724376678467, "[TT] Exposure Time of the CCDs = 2 seconds"]
-[4.769053936004639, 8.041533470153809, "[TT] Center Frequency of the Instrument = 435 MHz"]
-[13.879563331604004, 5.673800468444824, "[TT] Efficiency of the Solar array = 28.5% at BOL"]
-[6.802832126617432, -0.7098811268806458, "[TT] Orbital Period of the SARAL spacecraft = 100.6 minutes"]
-[7.584457874298096, 2.1185410022735596, "[TT] Application of the CZI = Monitor vegetation and the coastal zone"]
-[8.11269760131836, 4.443943977355957, "[FF] URL of the 3D Imaging Electromagnetic Calorimeter = http://www.pg.infn.it/"]
-[9.775917053222656, 6.958278179168701, "[TT] Geometry Factor of the LEICA = 0.8 cm^2 sr"]
-[5.323112487792969, 4.8992815017700195, "[TT] Daily Downlink Time of the Ground Stations = About 102 minutes"]
-[3.2253150939941406, 5.014293670654297, "[TT] Spatial Resolution of the SAR Sensor Subsystem = 20 m x 20 m"]
-[9.588850021362305, -0.36579281091690063, "[TT] High-Elevation Pass Selection of the ASTERIA = Once per day"]
-[11.310405731201172, 5.08976936340332, "[TT] Size of the Integrated Sensor = 8 mm x 3 mm x 19 mm"]
-[4.411412715911865, 6.5982489585876465, "[TT] Beacon modulation of the RF communication subsystem = OOK 15 WPM"]
-[10.102686882019043, -1.4192544221878052, "[TT] Inclination of the RADARSAT-2 = 98.6\u00b0"]
-[9.60059642791748, 8.169073104858398, "[TT] Lens System of the Instrument = f/4 telecentric lens system with a 5:1 fiber-optic taper"]
-[8.049474716186523, 6.108756065368652, "[FF] Function of the KMSS = Mounting fixture of three separate cameras"]
-[3.669398307800293, 2.6157994270324707, "[TT] Upgradable Speed of the Iridium Certus = 704 kbit/s"]
-[5.255216121673584, 4.9004669189453125, "[TT] Detection Time of the Ground System = 7 days"]
-[9.525308609008789, 5.373836994171143, "[FF] Components of the Focal Plane Cryostat Assembly = Infra-red detectors, cold optics, cryocoolers, detection chain electronics"]
-[8.70648193359375, 1.6562594175338745, "[TT] Altitude of the Noctilucent Clouds = 50 miles (80 km)"]
-[5.1519012451171875, 0.32857877016067505, "[TT] Operation Start Date of the AOCS = Day 5"]
-[6.466182231903076, -0.29192501306533813, "[TT] Revisit Time of the SuperView-1 01 and Superview-1 02 = 4 days"]
-[7.1419148445129395, 8.343696594238281, "[TT] SNR in SO of the ELVIS = >1000"]
-[4.196341514587402, 2.535173177719116, "[TT] Launch Site of the OPAL = VAFB, CA"]
-[6.2609944343566895, -1.1358240842819214, "[TT] Operation Duration of the GRACE-1 = More than 10 years"]
-[4.750696182250977, 3.1030423641204834, "[TT] Backup Environmental Satellite Operations Center Location of the C3S = SOC 81, Shriever (Falcon) AFB, Colorado Springs, CO"]
-[14.327359199523926, 3.0896177291870117, "[TT] Mass of the AlSat-1B = 103 kg"]
-[6.761745929718018, 2.222893714904785, "[FF] URL of the Dellingr = http://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=3614&context=smallsat"]
-[5.99011754989624, 5.166311264038086, "[FF] Components of the ECSE = Telecommand and telemetry security layer software integrated into the primary STRV TM/TC processor workstation"]
-[6.289069652557373, 2.5505642890930176, "[FF] Purpose of the SLS = Carry astronauts to destinations beyond LEO"]
-[4.69413423538208, 0.6056836843490601, "[FF] Date of the Without Mission A Beat = 2 April 2022"]
-[5.2681684494018555, 1.7554349899291992, "[FF] Purpose of the HawkEye 360 = Deliver RF data and analytics to the agency and combatant commands"]
-[10.907096862792969, 7.549751281738281, "[TT] Swath Width of the ScaRaB = 3200 km"]
-[6.818810939788818, 4.9016523361206055, "[FF] Definition of the OHU = Position of its alignment cube"]
-[10.178186416625977, 1.3569190502166748, "[TT] Number of Stars of the M33 galaxy = Forty billion"]
-[8.06798267364502, 8.414002418518066, "[TT] Spectral Region Infrared Channel of the VIRR = 10.5 - 12.5 \u00b5m"]
-[8.256613731384277, 8.737082481384277, "[TT] Wavelength of the EUV Simulation = 80 nm"]
-[6.266162872314453, 4.851491928100586, "[FF] Function of the Relative GPS (rGPS) = Computing the relative position and velocity during perigee pass based on GPS measurements"]
-[5.830866813659668, 6.1489410400390625, "[FF] Raw Data Rates of the ISL Communications = Increased"]
-[7.0106353759765625, 4.883195400238037, "[FF] Test Equipment of the ICI Instrument = Unknown"]
-[4.138198375701904, 3.3517637252807617, "[TT] Estimated Cost of the Galileo program = \u20ac 3.4 billion"]
-[7.918952465057373, 3.0947790145874023, "[FF] Measurement Type of the Carbon Dioxide Spectrometer = Near-infrared absorption by CO2"]
-[5.690771102905273, 4.680030345916748, "[FF] Internet Protocol (IP) address of the STRV-1b = Unknown"]
-[6.9733428955078125, 5.105984687805176, "[TT] Configuration of the Platform = Open \u201cflower petal\u201d configuration"]
-[10.801957130432129, 2.919556140899658, "[TT] Structure of the SciSat/ACE = Minisatellite"]
-[5.1904616355896, -1.2060353755950928, "[TT] Launch Date of the Kondor-E = 27 June 2013"]
-[6.723860740661621, -0.297536700963974, "[TT] Average Duration of the LEO-LEO Inter-satellite Link = About 20 minutes"]
-[12.619917869567871, 7.462714195251465, "[TT] Contract Volume of the MWI Instrument = \u20ac 134 million"]
-[4.602107524871826, 7.390799522399902, "[TT] Return Loss of the X-band Transmitter = <12 dB"]
-[9.622416496276855, 4.8316168785095215, "[TT] Stabilization of the Spacecraft = 3-axis"]
-[6.589233875274658, 5.220463275909424, "[TT] Function of the Instrument Control Unit (NI-ICU) = General power supply"]
-[6.819024085998535, 4.547346591949463, "[FF] Data Set of the RAVAN = Episodic"]
-[11.924278259277344, 5.022375106811523, "[TT] Size of the \u00b5SCIA = 130 mm x 80 mm x 50 mm"]
-[6.39884090423584, -0.22700470685958862, "[FF] Operation Duration of the SuperDARN = Not specified"]
-[5.504216194152832, 0.5825926661491394, "[TT] Data Collection Start of the ERBE = 1984"]
-[8.088027000427246, 8.343366622924805, "[TT] Measurement Range of the SSI = 200 \u2013 2400 nm"]
-[7.801257610321045, 4.63861608505249, "[FF] Heritage of the OMA = Long lived commercial instrument series which started in the mid 80's"]
-[6.455151557922363, 1.879215121269226, "[FF] URL of the SWOT Satellite = https://swot.jpl.nasa.gov/flight_systems.htm"]
-[7.598415374755859, -2.514235258102417, "[TT] Commissioning Period of the GOLD = 4 September to early October"]
-[8.278006553649902, 0.05164260417222977, "[TT] Number of Contacts with the Comet of the Philae lander = Four times"]
-[8.001116752624512, 1.9710091352462769, "[TT] Channels of the Coastal Zone Scanner = 4"]
-[9.743551254272461, 1.3883945941925049, "[TT] Agility Range of the Pleiades-1A = Up to 1500 km on either side of their path"]
-[3.7007482051849365, 1.495573878288269, "[FF] Industry Day Date of the GMES Sentinel-1 = Nov. 2007"]
-[9.382858276367188, 3.970871925354004, "[FF] Calibration of the MAG Sensor = Performed over a wide range of temperatures"]
-[6.257592678070068, 4.4271979331970215, "[FF] Development and Flight Results of the On-Board Computer = Unknown"]
-[4.485625267028809, 1.5524473190307617, "[TT] Launch Date of the MightySat II.1 (Sindri) = July 19, 2000"]
-[4.519726276397705, -0.8900251984596252, "[TT] Launch Date of the Dragon cargo capsule = June 3, 2021"]
-[8.143980026245117, 2.7712221145629883, "[FF] Purpose of the MicroMAS = Provide near-continuous views of severe weather"]
-[6.005043029785156, 5.73203182220459, "[TT] FPGA of the CIB = ACTEL's ProAsic3"]
-[7.997000217437744, 8.778640747070312, "[TT] Spectral Coverage of the Green = 520-590 nm"]
-[6.7283172607421875, 2.790703296661377, "[TT] Funding of the MethaneAIR = Environmental Defense Fund (EDF) and private philanthropy"]
-[7.105368614196777, 6.907851219177246, "[FF] Energy Readings of the Laser002 = Stabilizing at lower than nominal values (~70 to 80% of nominal)"]
-[6.7982401847839355, 1.4825853109359741, "[FF] Imagery Reception of the FormoSat-2 = Available to third parties with their own ground stations through cooperative agreements"]
-[13.661617279052734, 5.412868022918701, "[TT] Fabrication Technology of the Solar Cells = D-HVPE (Dynamic Hydride Vapor Phase Epitaxy)"]
-[8.55879020690918, 5.5333051681518555, "[TT] Radiometric Resolution at High Wind of the Satellite = 2.0 - 2.7%"]
-[6.054966449737549, -0.2817589044570923, "[FF] Operations Duration of the MOPITT = 2.5 Years"]
-[5.457204818725586, 4.320735931396484, "[FF] Authorized Service of the COMPASS/BeiDou = Commercial Basis"]
-[5.805045127868652, -0.7617259621620178, "[TT] Design Life of the Satellite = 3-5 years"]
-[5.879258155822754, 1.3370814323425293, "[TT] PDR Date of the IXPE observatory = August 8, 2018"]
-[9.74964714050293, 7.030893802642822, "[TT] Spatial Resolution of the CAPI instrument = 0.5 km"]
-[7.5902628898620605, 5.58117151260376, "[FF] Modules of the IASI-NG Instrument = Optical Head (I-OH) and Electronics Module (I-EM)"]
-[12.066414833068848, 4.505445957183838, "[TT] Body Size of the Spacecraft = 2.5 m x 1.2 m x 1.1 m"]
-[8.41260051727295, 7.51977014541626, "[TT] Detector Type of the PAMELA = Double-sided silicon detectors"]
-[5.13967227935791, -0.5947718024253845, "[FF] Project Date of the TARANIS = July 16-23, 2006"]
-[10.155405044555664, 1.6908378601074219, "[TT] Number of Compact Sources of the eROSITA = More than a million"]
-[5.458419322967529, 6.3951849937438965, "[TT] Onboard Data Storage Capacity of the XMM-Newton = None"]
-[6.665725231170654, 3.064279317855835, "[FF] Simulation Models of the PRISMA project = Reaction Wheels (RW), Magnet Torquers (MT), Hydrazine Thrusters, Micro propulsion Thrusters, Sun Sensors (SS), Magnetometer (MAG), Accelerometer (ACC), GPS models, FFRF (Formation Flying Radio Frequency) model, Startracker (ST) and Visual based sensor (VBS), Intersatellite link (ISL), Solar panels, Batteries, Power conditioning and distribution unit (PCDU), All RTUs"]
-[4.085269451141357, 4.194746017456055, "[TT] Radar Scatter Detection of the RAX-2 = June 12, 2012"]
-[8.148786544799805, 1.1859130859375, "[FF] Potential Misidentification of the DIBS = Volcanic ash"]
-[13.980831146240234, 2.8017425537109375, "[TT] On-orbit Mass of the INSAT-2A/2B = 911 kg"]
-[3.0654027462005615, 2.0074682235717773, "[FF] Mission of the Copernicus Sentinel-2 = Detect the slight signs of change that may foretell an eruption"]
-[4.990610122680664, 3.129497766494751, "[TT] Manufacturer of the SEOSAT/Ingenio = Airbus"]
-[5.641175746917725, 4.7161078453063965, "[FF] Connection of the SATLAB = SATSIM is connected with the OBC through the CAN bus"]
-[6.810100555419922, -0.5930965542793274, "[TT] Orbit Period of the ERBS = 96.8 min"]
-[5.081281661987305, 2.1617608070373535, "[TT] Mission Type of the QBITO = EO"]
-[8.153395652770996, 8.893972396850586, "[TT] Instrument Payload of the Sentinel-4 = Passive UVN (Ultraviolet-Visible-Near-Infrared) hyperspectral imaging spectrometer"]
-[7.40742826461792, 2.32978892326355, "[TT] Global Mapping Achievement of the Satellite = 56.9%"]
-[7.802306652069092, 8.249948501586914, "[TT] Spectral Range of the HSC-III = 400-1000 nm"]
-[9.985578536987305, -1.52767014503479, "[TT] Orbit Inclination of the ProSEDS = 35\u00ba"]
-[13.48141860961914, 6.992147922515869, "[TT] Power Output of the Fission Surface Power System = At least 40 kilowatts"]
-[4.385250091552734, 7.837346076965332, "[TT] Frequency of the RF communication subsystem = 437 MHz (UHF), in uplink and downlink"]
-[6.43698787689209, 0.11092964559793472, "[TT] Global Coverage Time of the DMAC = Four months"]
-[10.199629783630371, 5.481833457946777, "[TT] Thermal Design of the Instrument Equipment = Classical thermal environment"]
-[6.666351795196533, 2.4287960529327393, "[TT] Peak Daily Acquisition Capability of the COSMO-SkyMed = 10 minutes of continuous operation in Stripmap or ScanSAR modes or alternatively 20 spotlight images"]
-[7.099827289581299, 5.13474178314209, "[FF] Components of the SMX-1 = ESA ERC32 chip set and components"]
-[4.135937690734863, 0.1788274198770523, "[FF] Launch Campaign Thread Date of the Falcon Heavy = 3 June 2019"]
-[5.7510223388671875, 7.159138202667236, "[TT] Data Rate of the NSCAT = 3.2 kbit/s"]
-[7.249131679534912, 9.03675365447998, "[TT] Filter Center of the MCE = 777 nm"]
-[8.990666389465332, 4.466455936431885, "[FF] Sensors of the Attitude Control Subsystem = Sun sensors, star sensors and gyroscopes"]
-[5.848638534545898, -0.8110631108283997, "[TT] Predicted Operational Life of the SAR spacecraft = Three years"]
-[8.254714965820312, 5.910040855407715, "[TT] Precision of the Bulk Parameters = 2%"]
-[7.731173515319824, 8.789478302001953, "[TT] Wavelength Range of the Spectral Channels = 0.55 - 0.75 \u00b5m"]
-[12.366576194763184, 0.6142933964729309, "[FF] ICUs of the PLATO = Two ICUs used in cold redundancy"]
-[5.3845295906066895, 5.118886470794678, "[FF] Sensor Complement of the Namuru GPS Receiver = Optical Payload, Namuru GPS Receiver"]
-[4.9768548011779785, 3.356428384780884, "[TT] Manufacturer of the MicrOmega = ESA"]
-[3.721223831176758, 6.646895885467529, "[TT] IFOV (beam width) of the Antenna = 5.3\u00ba"]
-[9.7836332321167, -0.596244752407074, "[TT] Orbit Altitude of the Electron rocket = 500 km"]
-[13.445703506469727, 6.881396293640137, "[TT] Power Generation of the MTM = More than 11 kW"]
-[8.915626525878906, 8.349201202392578, "[TT] Iron Particle Speeds of the WISPR Optics = 0.5 - 8 km/s"]
-[8.110638618469238, 8.987663269042969, "[TT] Wavelength Range (UV) of the Sentinel-4/UVN = 305-400 nm"]
-[5.066378116607666, 7.270273208618164, "[TT] Max. Data Rate of the RF Communications = 100 kbit/s"]
-[6.5135416984558105, 0.6962778568267822, "[FF] Observation Record of the Landsat-9 = Last half-century"]
-[11.506682395935059, 4.82344388961792, "[TT] Size of the OPS-SAT = 30-cm"]
-[8.609823226928711, 6.951557159423828, "[TT] Data Volume Reduction of the Stereo Camera = Two-line pushbroom scheme"]
-[9.049039840698242, 5.088231086730957, "[TT] Test Range of the Gyroscopes = About 12,270 km"]
-[7.79439640045166, 8.438874244689941, "[TT] Number of Thermal Emissive Bands of the VIIRS = 7"]
-[5.857057094573975, 3.7642085552215576, "[TT] Constellation Size of the ESAIL = More than 60"]
-[9.710339546203613, -0.5986009240150452, "[TT] Orbit Altitude of the ASNARO = 504 km"]
-[11.856499671936035, 6.768913745880127, "[TT] Relativistic e- Energy Range of the XGRE = 1 MeV \u2013 10 MeV"]
-[7.5713019371032715, 3.1755785942077637, "[FF] Visibility of the Satellite = Certain recurring morning and evening twilight periods"]
-[4.662198543548584, 7.13217306137085, "[TT] X-band Downlink Data Rate of the RF communications = 30 Mbit/s"]
-[14.631407737731934, 6.668576240539551, "[TT] Battery Type of the Energy Storage System = NiH2"]
-[5.877653121948242, -0.28998133540153503, "[TT] Acoustic Test Duration of the EDRS-C = Two days"]
-[5.365663528442383, 0.22695215046405792, "[TT] Launch Date of the STS-56 = April 8-17, 1993"]
-[4.893890857696533, -0.042679931968450546, "[TT] End of Life Date of the SPOT-5 = 30 Mar 2015"]
-[9.609476089477539, 4.208532333374023, "[TT] Magnetometer of the DSX = Present"]
-[13.388627052307129, 5.475594997406006, "[TT] Quantity of the Solar Panels = 2 sets"]
-[8.503379821777344, 2.9687705039978027, "[FF] Journal Article of the ROCSat-2 Satellite = J. L. Chern, R. R. Hsu, H. T. Su, S. B. Mende, H. Fukunishi, Y. Takahashi, L .C. Lee, \"Global Survey of Transient Luminous Events by ROCSat-2 Satellite,\" Journal of Atmospheric and Solar-Terrestrial Physics, Vol. 65, 2003, pp. 647\u2013 659"]
-[3.0790672302246094, 1.975573182106018, "[FF] Working Life of the Copernicus Sentinel-1 = Exceeded"]
-[5.4289164543151855, 0.18339253962039948, "[TT] Launch Date of the SAMPEX = July 3, 1992"]
-[5.680615425109863, 4.704657554626465, "[FF] Data Relay of the TGO = NASA rovers"]
-[8.427741050720215, 4.01781702041626, "[FF] Measurement Record of the SIM = Extends a 15-year record of spectral irradiance measurements"]
-[10.409363746643066, 2.1758310794830322, "[FF] Sensitivity of the NuSTAR = Detecting the highest-energy X-rays"]
-[10.069208145141602, 1.9361469745635986, "[FF] Creation Technique of the Synthetic Galaxy Catalog = Halo Occupation Distribution technique"]
-[14.389286994934082, 3.3705379962921143, "[TT] Mass of the SDR = 547 g"]
-[4.395902633666992, 4.863570690155029, "[TT] Incidence Angles of the Vessel detection optimized beam mode = 34\u00ba to 57\u00ba"]
-[11.155594825744629, 6.027863502502441, "[TT] HV Grid Insulation of the Modulator Assembly = Sapphire tubes"]
-[7.943559646606445, 7.699157238006592, "[FF] Panchromatic Mode Band of the SPOT satellite constellation = Single wide band in the visible part of the spectrum"]
-[4.962838649749756, 4.745216369628906, "[TT] QKD Channel Collaborator of the QUESS = Anton Zeilinger and colleagues at the University of Vienna"]
-[5.807267189025879, 6.228126525878906, "[TT] Processing Power of the GS (Ground System) = Approximately 40 trillion floating point operations per second"]
-[6.759310722351074, 2.1037614345550537, "[FF] Mission Overview of the Hinode = June 2007"]
-[6.792911052703857, 5.854772090911865, "[TT] Predicted Quantity of the Fragments = 85 k"]
-[5.460453987121582, 5.979040622711182, "[TT] ROM of the OBDH = 64kB"]
-[9.381479263305664, 7.202210903167725, "[TT] Resolution of the WPM = 8 m"]
-[4.886219501495361, -0.5932897925376892, "[FF] Operational Update Date of the SLATS = 1 June 2018"]
-[4.891316890716553, 0.6482309103012085, "[TT] Launch Date of the TechDemoSat-1 = 2014"]
-[5.205615520477295, 4.223547458648682, "[TT] Minimum Number of Satellites for Navigation Fix of the T3000G2 receiver = 4"]
-[5.815783500671387, -2.242588520050049, "[TT] Orbital Altitude of the KOMPSAT-5 = 550 km"]
-[3.7422494888305664, 2.489119529724121, "[TT] Commercial Availability of the Iridium Certus = Mid-2018"]
-[8.38765811920166, 4.684197902679443, "[FF] Components of the G&C system = Sun sensors, a ST (Star Tracker), redundant IMUs (Inertial Measurement Units), the GT, reaction wheel assemblies, and a monopropellant hydrazine propulsion system"]
-[4.758782863616943, 6.993842124938965, "[TT] X-band Downlink of the Satellite = 280 Mbit/s"]
-[11.069891929626465, 3.776611804962158, "[TT] Size of the MySat-1 = 1U"]
-[7.688757419586182, 6.384228229522705, "[FF] Imaging Mode of the FAI = Slew"]
-[5.288414001464844, 0.4958288073539734, "[FF] Radio Trigger Date of the Juno = 15 July 2021"]
-[5.328239917755127, 7.580043792724609, "[TT] PRF of the KaRIn = 2 x 4420 Hz"]
-[7.839753150939941, 8.699918746948242, "[FF] Bandwidths of the AATSR = 20 nm, 300 nm, 1000 nm"]
-[4.892059803009033, -1.9724230766296387, "[TT] Rocket Height of the Chang'e-5 = 57 meters"]
-[8.054890632629395, 7.998813152313232, "[FF] Type of the Medium Wave Infrared Imager = Medium Wave Infrared"]
-[4.9231181144714355, 0.5149051547050476, "[TT] Start Date of the SLA = 2015"]
-[8.166773796081543, -0.957462728023529, "[FF] Application of the Lidar Instrument = Determine topographic character of ice sheet changes"]
-[3.6794354915618896, 4.531230926513672, "[FF] Image Recording Capability of the SAR Antenna = All weather conditions, both during the day and the night"]
-[10.953133583068848, 4.819185733795166, "[TT] Orientation Accuracy of the Tethered System = Within \u00b110 degrees of the vertical"]
-[8.938050270080566, 5.325669288635254, "[FF] Pointing Mode of the Spacecraft = View the cusp from different perspectives"]
-[5.766506195068359, 0.8576465249061584, "[FF] Discovery Date of the Blue Jets = Unknown"]
-[8.242563247680664, 1.8933703899383545, "[TT] Spatial Resolution of the Oceanography Short scale = 100 km"]
-[6.757692813873291, 7.577091693878174, "[TT] Receive Options of the Instrument = H or V"]
-[5.468291759490967, 0.5466179847717285, "[TT] Mission Start Date of the FormoSat-2 = June 2004"]
-[3.851153612136841, 7.90008544921875, "[TT] Modulation Scheme of the Real-time data = BPSK (Bi-Phase-Shift Keying)"]
-[6.214478015899658, 3.125257730484009, "[TT] Science Payload Developer of the Neutron-1 = Arizona State University (ASU)"]
-[10.42313003540039, 5.732661724090576, "[FF] Temperature Increase Objective of the Paris Agreement = Well below 2\u00b0C above pre-industrial levels and pursuing efforts to limit the temperature increase to 1.5\u00b0C above pre-industrial levels"]
-[6.298345565795898, 3.8285248279571533, "[FF] Sections of the DMSP Block 5D-1 = Three sections: a square precision-mounting platform, a five-sided equipment-support module, a circular reaction and control-equipment support structure"]
-[5.689366340637207, 2.6528029441833496, "[FF] Collaborators of the CADRE = University of Michigan (UMich), NASA/GSFC, NRL (Naval Research Laboratory)"]
-[2.6045775413513184, 3.333735942840576, "[TT] Quantity of the Flock-3p x 4 = 4"]
-[13.647708892822266, 2.7422409057617188, "[TT] Launch Mass of the Meteosat = 696 kg"]
-[6.435288429260254, -0.2989747226238251, "[TT] Revisit Time of the ALOS-2 = 14 days"]
-[9.486028671264648, 1.0752623081207275, "[TT] Drift Speed of the Great Blue Spot = About 2 inches (4 cm) per second"]
-[7.748359203338623, 3.6287715435028076, "[TT] Data Processing Unit of the PLASTIC = IMPACT IDPU"]
-[6.083597660064697, 4.488000392913818, "[FF] Functions of the Integrated Mobile Stations = Mission control, mission planning, ground station, mission data processing and GIS"]
-[5.715037822723389, 6.312266826629639, "[TT] Processing Power of the CCM = 20-30 MIPS"]
-[11.850971221923828, 0.01337924413383007, "[FF] Purpose of the TESS = Discovering new Earths and Super-Earths in the solar neighborhood"]
-[4.815462589263916, -0.262473464012146, "[TT] Launch Time of the Soyuz MS-17 = 1:45 a.m. Eastern Oct. 14"]
-[8.041613578796387, 6.069484710693359, "[FF] Sensor Complement of the BX-1 = WFOV (Wide Field of View) and a NFOV (Narrow Field of View) camera"]
-[9.340411186218262, 2.6386728286743164, "[FF] Flare List Events with Gamma-ray Line Emission of the RHESSI = 27"]
-[7.039203643798828, 7.199927806854248, "[TT] Laser Pulses Per Second of the ATLAS altimeter = 10,000"]
-[8.684630393981934, 5.538278579711914, "[TT] Altitude Measurement Accuracy of the NRA = 2.4 cm"]
-[4.9771294593811035, -0.4476456940174103, "[TT] Launch Date of the SLATS / Tsubame = 23 December 2017"]
-[7.91890811920166, 4.976509094238281, "[FF] Change of the Test Profile = Started on a warm temperature plateau to enable a valid home command"]
-[6.532272815704346, 0.3357366919517517, "[TT] Revisit Time of the Terra Bella = Three times per day"]
-[8.370150566101074, 4.044885635375977, "[FF] Parameters Measured of the SpaceRadMon = Total Ionization Doze (TID), Single Event Upsets (SEUs), Single Event Latchups (SELs), HEH fluence"]
-[7.823411464691162, 6.42235803604126, "[FF] Image Capture Time of the ABI (Advanced Baseline Imager) = 5 and 8 p.m. local time (04:00 to 07:00 Universal Time)"]
-[11.176398277282715, 3.813493490219116, "[FF] Tether Break of the AeroCube-3 = The tether to the upper stage broke within hours"]
-[8.84432315826416, 5.3333420753479, "[TT] Measurement Error of the Acceleration = Random <0.1 G (1\u03c3), Bias < 0.25 G, Nonlinearity < 2%"]
-[7.555250644683838, 4.688377857208252, "[FF] Component of the Transition Radiation Detector (TRD) = Unknown"]
-[6.078974723815918, 1.6178439855575562, "[FF] Science Requirements Document Date of the SWOT = March 19, 2009"]
-[10.43490982055664, 2.156726598739624, "[TT] Sensitivity of the eROSITA X-ray telescope = 25 times more sensitive than its predecessor ROSAT"]
-[11.394322395324707, 4.308939456939697, "[TT] Size of the Phoenix = 2U"]
-[6.565760135650635, 3.9461309909820557, "[TT] Science Instruments of the Spacecraft = Built into the chassis"]
-[13.58694076538086, 5.519346714019775, "[TT] Cells in Series of the Solar Panels = 34"]
-[7.653782367706299, 1.9336862564086914, "[FF] Source of Carbon of the Northern Forests = Potential future outcome"]
-[5.523259162902832, 0.5343565344810486, "[TT] Launch Date of the ERS-2 = 21 Apr 1995"]
-[6.628060817718506, 0.13099543750286102, "[TT] Repeat Coverage of the Landsat 9 = 16 days"]
-[11.337742805480957, 1.1208984851837158, "[TT] Cube Mass of the LISA Pathfinder = 2 kg"]
-[9.0405855178833, 5.8092169761657715, "[TT] Pointing Accuracy of the NEMO-HD = 1.5 arcmin"]
-[10.275071144104004, 5.592128753662109, "[FF] Temperature of the Tank B2 = Increased"]
-[4.7643890380859375, 0.6000697612762451, "[TT] First Launch of the MSG = 2002"]
-[10.782431602478027, -0.2153175324201584, "[FF] Formation Flying of the TanDEM-X = Yes"]
-[5.004924297332764, 7.301369667053223, "[TT] Bit Rate of the S-band Transmitter = Up to 1 Mbit/s"]
-[8.017935752868652, 9.142212867736816, "[TT] Wavelength for Ozone Measurement of the LORE = 322 nm"]
-[7.110004425048828, 5.8361897468566895, "[FF] Stability of the DSAC = 100 times more stable than today's best navigation clocks"]
-[10.726455688476562, 2.881978750228882, "[TT] Resonance Survey Requirement of the SERB Nanosatellite = First global mode > 250 Hz"]
-[8.149130821228027, 2.0883023738861084, "[FF] Cross-Calibration Frequency of the CloudSat = Once in 3 days"]
-[12.779810905456543, 7.231612682342529, "[TT] Main Beam Efficiency (%) of the Antenna = 86"]
-[8.28787612915039, 0.4571663737297058, "[TT] Discharge of the Yellowstone River = 51,400 cubic feet per second"]
-[5.171043395996094, 8.090556144714355, "[TT] Frequency Requirement of the SRMSat = > 90 Hz in longitudinal and > 45 Hz in lateral directions"]
-[13.77232551574707, 2.896507740020752, "[TT] Mass of the Trailblazer spacecraft = 83.5 kg"]
-[6.428686141967773, -1.215804100036621, "[TT] Data Collection Period of the GRACE and GRACE-FO = 17 years"]
-[4.911877155303955, 5.1218485832214355, "[TT] CCSDS ID of the GSAT-0203 = 263"]
-[10.111071586608887, -1.398012399673462, "[TT] Orbital Inclination of the TanSat = 98.2\u00b0"]
-[10.039247512817383, 4.522751331329346, "[TT] Detector Type of the AMS-02 = Particle physics detector containing a large, cryogenic superfluid helium superconducting magnet"]
-[9.709386825561523, -0.5390140414237976, "[TT] Altitude of the OrbView-2 = 705 km"]
-[5.121520042419434, 6.9740118980407715, "[TT] Downlink Chains Data Rate of the ResourceSat-2 = 105 Mbit/s"]
-[11.822242736816406, 2.846928834915161, "[TT] \u0394V (cm/s) of the Orbcomm FM30 = 0.65"]
-[9.481078147888184, -1.120104193687439, "[TT] Nominal Position of the MFG series = 0\u00b0 longitude"]
-[9.05419921875, 5.680552005767822, "[TT] Boresight Pointing Accuracy of the SXI = Within 3 arcmin elevation, within 3.5 arcmin azimuth"]
-[4.79024076461792, 1.7519865036010742, "[FF] URL of the GOSAT-2 = http://global.jaxa.jp/projects/sat/gosat2/"]
-[8.419130325317383, 7.319233417510986, "[TT] CCDs of the Camera = 4"]
-[12.894014358520508, 7.563570499420166, "[TT] Instrument Power Requirements of the FLP = Approximately 100 W"]
-[10.137641906738281, 9.987150192260742, "[TT] Mission Number of the Vega = 18"]
-[9.87313175201416, 8.949939727783203, "[TT] IGFOV of the VIS and SWIR detectors = 28 microradians (\u00b5rad)"]
-[7.203111171722412, 8.442676544189453, "[TT] C-band range Noise of the Jason-2 = 3.5/2/2 cm"]
-[3.440495491027832, -0.9274076819419861, "[TT] Orbit Type of the Satellite = Sun-synchronous near-circular orbit"]
-[10.57230281829834, 2.8948726654052734, "[FF] Illustration of the STARE nanosatellite = Figure 4"]
-[5.084125995635986, 3.205503463745117, "[TT] Manufacturer of the Eagle-2 ($50SAT) = MSU (Morehead State University)"]
-[7.052157878875732, 4.17454195022583, "[FF] Unknown of the GOMOS = Unknown"]
-[9.891762733459473, 2.7118799686431885, "[TT] Number of Satellites Deployed of the NanoRacks = 231"]
-[10.1842041015625, 1.015857458114624, "[TT] Distance of the Cassiopeia A = 10,000 light years"]
-[11.382024765014648, 3.4982757568359375, "[FF] Propulsion Subsystem of the AOCS = Cold gas propulsion subsystem and magnetic torquers"]
-[5.8251729011535645, 3.057344675064087, "[TT] Number of Missions of the MISSE = Nine"]
-[13.173219680786133, 5.481563091278076, "[FF] Components of the European Service Module = Built and integrated in Italy and Germany, with smaller components delivered from several European nations, including the solar arrays from the Netherlands"]
-[4.350069522857666, 1.6237088441848755, "[FF] Development Date of the ROCSat-1 = Unknown"]
-[6.031680583953857, -0.3497835099697113, "[TT] Operation Duration of the CanX-7 = Approximately six months"]
-[7.455634593963623, 2.9523515701293945, "[TT] Pixel Size of the MethaneSAT = 400 x 100 m"]
-[5.9264326095581055, 4.679702281951904, "[TT] Type of the SCIP = Stack based"]
-[14.046890258789062, 7.159244537353516, "[TT] Regulated Bus Voltage of the Power Subsystem = 5 V"]
-[9.863883018493652, 7.920991897583008, "[TT] Aperture of the SV-24 = 24 cm diameter"]
-[9.795097351074219, 8.579551696777344, "[TT] IFOV for WV of the Telescope = 224 \u00b5rad (8 km)"]
-[6.271521091461182, 0.40422841906547546, "[FF] Launch Date of the ROSE-L = Mid-2027"]
-[4.295781135559082, 7.480501174926758, "[TT] Frequency Band of the AltiKa = Ka-band"]
-[7.547053337097168, 0.7947453856468201, "[FF] Purpose of the OMOTENASHI = Demonstrate the technology for low-cost and very small spacecraft to explore the lunar surface"]
-[8.717772483825684, 7.6370463371276855, "[TT] Imaging Area Pixels of the CCD = 600 x 600"]
-[4.610952377319336, 7.118663311004639, "[FF] Downlink Transmission Rate of the X-band transmitter = Efficient"]
-[11.366349220275879, 3.46760892868042, "[FF] Expected Outcome of the TEPCE = New propulsion capability for spacecraft"]
-[5.085018634796143, 0.8596059083938599, "[FF] Network Completion Date of the EAN = 5 Feb. 2018"]
-[5.171795845031738, -0.5555083155632019, "[FF] Inquiry Commission Appointment of the TARANIS = 17 November 2020"]
-[5.769608020782471, 2.9742431640625, "[TT] Ground Operations Provider of the CloudSat = USAF/STP (Space Test Program)"]
-[7.5027570724487305, 5.143299102783203, "[TT] Operation Mode of the IXAE = Pointed mode observations"]
-[6.035311698913574, -0.07881322503089905, "[TT] Mission Lifetime of the FormoSat-2 = 5 years"]
-[6.584070205688477, 5.289970397949219, "[FF] Components of the NRD = Antenna and receiver electronics"]
-[4.454681396484375, 5.402837753295898, "[TT] Manufacturer of the GomX-4A and GomX-4B = GomSpace"]
-[5.417682647705078, 3.6706273555755615, "[TT] Platform of the DoT-1 satellite = SSTL-Micro"]
-[10.833417892456055, 7.525649070739746, "[TT] Swath Width of the IMI = >1000 km > 1000 km > 1000 km"]
-[8.349156379699707, 2.7710654735565186, "[TT] Measurement Domain of the FedSat = Gravity and Magnetic Fields"]
-[5.464678764343262, 0.7375833988189697, "[TT] De-orbit Date of the GFO = End of 2008"]
-[10.190152168273926, 3.1550889015197754, "[FF] Conference Presentation of the GOMX-1 = 11th Annual CubeSat Developers\u2019 Workshop"]
-[6.239059925079346, 4.945934295654297, "[FF] Function of the PERL/SNMP program = Monitor router interface traffic, data rates, error indicators, and MIP tunnel status"]
-[9.032660484313965, 0.45587682723999023, "[FF] Diameter of the Ryugu = 900 m"]
-[13.578947067260742, 7.068007946014404, "[TT] Peak Power of the EPS = 2.4 W"]
-[5.247659683227539, 2.0343923568725586, "[TT] Mission Status of the ALL-STAR = Unknown"]
-[7.649133682250977, 1.851061463356018, "[FF] Greenness Increase of the Amazon forests = About 10 to 15 percent on average"]
-[6.649181842803955, 5.80281400680542, "[TT] Board Quantity of the MuREM = 3"]
-[7.720603942871094, 4.726263046264648, "[FF] Sensor of the SWOT = KaRIn (Ka-band Radar Interferometer)"]
-[5.804329872131348, 6.477853775024414, "[TT] Access Method of the OPS (Onboard Packet Switch) = Slotted ALOHA"]
-[3.457813024520874, -0.9195641875267029, "[FF] Type of the Orbit = Sun-synchronous near-circular orbit"]
-[5.6360979080200195, 2.586035966873169, "[TT] Mission Management Provider of the Lucy = Goddard"]
-[16.555280685424805, 3.6453142166137695, "[TT] Total Satellites in Orbit of the OneWeb = 182"]
-[5.627323627471924, -1.769878625869751, "[FF] URL of the KSAT-HP = http://leo.sci.kagoshima-u.ac.jp/~n-lab/KSAT-HP/Ksat2_E.html"]
-[7.223550319671631, 1.2357922792434692, "[FF] Function of the Sample Fetch Rover (SFR) = Navigate, locate and collect the sample tubes"]
-[5.818681716918945, -0.7899532318115234, "[TT] Expected Lifetime of the MetOp-SG = 7.5 years"]
-[7.676450252532959, 4.966038703918457, "[FF] Measurement Date of the Microwave instruments = September 18, 2019"]
-[9.918919563293457, 1.6267123222351074, "[FF] Observation Results of the Herschel = Intricate network of gas filaments and dark bubbles interspersed by bright hotspots"]
-[13.744178771972656, 5.457708835601807, "[TT] Power Generation of the S/C = Four body-mounted GaAs solar panels"]
-[10.516072273254395, 7.432377338409424, "[TT] Beam Width of the SASS = 500 km"]
-[7.556910037994385, 2.1542129516601562, "[TT] Coverage of the TeLEOS-1 = Equatorial belt"]
-[10.065133094787598, -1.5021283626556396, "[TT] Inclination of the GEOS-1 = 59.3\u00ba"]
-[11.001962661743164, 2.044816493988037, "[FF] Launch Date of the XMM-Newton = April 2, 2015"]
-[10.318801879882812, 5.604067325592041, "[TT] Cooling Power of the Cooler = 2.27 W at 53.0 K"]
-[5.777588367462158, 7.132622718811035, "[TT] Rate of the Data rate = 660 kbit/s"]
-[9.299118995666504, 2.804201364517212, "[TT] Solar Wind Speed and Beta of the ACE = ~40% lower on average from 2009 through the day 79 of 2013"]
-[10.247493743896484, 4.032812595367432, "[TT] Mounting of the MAG = Boom mounted on GOES-R"]
-[8.729715347290039, 5.976447582244873, "[TT] Field of Operation of the Coarse Lateral Sensor = 10 arcdeg"]
-[5.702256202697754, 0.6220672726631165, "[TT] Observation Date of the NuSTAR = April 29, 2015"]
-[4.676811218261719, 5.429327487945557, "[FF] Operation of the Automated Beacon Network = Receives the health message"]
-[6.920632362365723, 1.386626124382019, "[TT] Destination of the Sample Return Capsule = Earth"]
-[8.817689895629883, 6.257837295532227, "[TT] Scan Rate of the VIRR = 48 rpm"]
-[3.4774584770202637, 6.32209587097168, "[TT] Antenna Area of the Capella's Satellites = Approximately 8 square meters"]
-[10.413636207580566, 2.16964054107666, "[FF] Detection Capability of the NuSTAR = High-energy X-rays"]
-[10.083569526672363, -1.4180999994277954, "[TT] Inclination of the SkySat-16 to -18 = ~98\u00ba"]
-[7.974141597747803, 7.221303462982178, "[TT] False Alarm Rate of the Imager = <5% of total events"]
-[7.329296112060547, 8.267202377319336, "[TT] PSLR of the Instrument = \u2264-16 dB"]
-[5.0854926109313965, 0.2533376216888428, "[TT] Launch Date of the NEA Scout = No earlier than March 2022"]
-[9.61101245880127, 4.048158645629883, "[TT] Magnetic Field Measurement Rate of the ULF Sensor = 0.03 to 3 Hz"]
-[5.539731025695801, 7.0360918045043945, "[TT] LVDS Link Speed of the IRIS = 50 Mbit/s"]
-[7.400615692138672, 0.7069413065910339, "[FF] Operation Status of the China's Moon Rover = Sleeps"]
-[8.996109008789062, 8.141067504882812, "[TT] IFOV/line (pixels/scan line) of the IRAS = 56"]
-[6.080734729766846, 4.523600101470947, "[FF] Location of the GPS Network GNET = Greenland"]
-[4.004907131195068, 1.7022144794464111, "[TT] Launch Failure Investigation Status of the Global-9 = Under investigation"]
-[9.597064971923828, 7.094022750854492, "[TT] Spatial Resolutions of the AMSR = 3 x 6 km - 40 x 60 km"]
-[9.593029975891113, 7.688536643981934, "[TT] Spatial Pixels of the Telescope = 1024"]
-[3.955636739730835, 9.691526412963867, "[TT] Frequency (GHz) of the ICI-10 = 448\u00b11.4"]
-[10.265944480895996, 8.034960746765137, "[TT] Telescope Secondary Aperture Diameter of the MVIRI = 140 mm"]
-[8.08743953704834, -1.225446105003357, "[FF] Laser Beams of the ICESat-2 = Can show the dramatic change in the terrain before and after the lake drained"]
-[7.159909248352051, 2.67918062210083, "[FF] Objective of the MSS = Provide repetitive daytime acquisition of high-resolution, multispectral data of the Earth's surface on a global basis and to demonstrate that remote sensing from space is a feasible and practical approach to efficient management of the earth's resources"]
-[9.741935729980469, 5.083251476287842, "[FF] Stressful Periods of the Power Subsystem = High beta angle"]
-[11.495671272277832, 4.800693511962891, "[TT] Length of the PM = 11.2 m"]
-[7.43419885635376, 0.9699814915657043, "[FF] DOI of the GRAIL = 10.1038/nature13697"]
-[9.187597274780273, 7.265668869018555, "[TT] Spatial Resolution of the EarthDaily Optical Imager = 5 m"]
-[5.900608539581299, 3.619784116744995, "[FF] Planned Satellite Constellation Size of the Capella Space = 36"]
-[13.652274131774902, 2.9717752933502197, "[FF] Number of Modules of the Astrium Sentinel 2 MMFU = Reduced"]
-[6.150429725646973, 4.3286004066467285, "[FF] Function of the Satellite = Create a random string of numbers to represent an encryption key"]
-[4.378331184387207, 2.091909408569336, "[TT] Launch Date of the DubaiSat-1 = 29 July, 2009"]
-[14.23265552520752, 3.3142080307006836, "[FF] Mass and Volume of the Core-DHS = Reduced"]
-[8.14271354675293, 6.849382400512695, "[FF] Signal Requirement of the Optical System = Must be enough"]
-[6.590750217437744, 2.038498878479004, "[FF] URL of the NuSTAR = https://www.jpl.nasa.gov/news/news.php?release=2017-088"]
-[6.307888031005859, 8.67548942565918, "[TT] Polarization, Left Swath of the KaRIn = HH"]
-[11.529889106750488, 3.47940993309021, "[TT] Flight Test of the UK-10 Ion Thruster Hollow Cathode Assembly = First"]
-[5.3087263107299805, 6.8259687423706055, "[TT] Serial Data Output of the LDCM spacecraft = 440.825 Mbit/s"]
-[9.407356262207031, -1.369917869567871, "[TT] Eccentricity of the GRACE-FO Satellites = Less than 0.0025"]
-[11.809569358825684, 3.309037685394287, "[TT] Thrust of the BIT-3 system = 0.66-1.24 mN"]
-[13.667261123657227, 3.5475871562957764, "[TT] Mass of the X-band Transmitter = 3.25 kg"]
-[6.806293487548828, -0.5857100486755371, "[TT] Orbit Period of the Satellite = 97 minutes"]
-[2.964022397994995, 4.351687908172607, "[FF] Development Date of the PALSAR Ground Data System = 2004"]
-[5.135004997253418, 3.5677998065948486, "[TT] Manufacturer of the exactView-1 = SSTL"]
-[7.205357074737549, 8.174549102783203, "[TT] Signal-to-Noise Ratio for Bright Objects of the MSU-100 = 200"]
-[5.035101413726807, -0.7585975527763367, "[TT] Function of the EDOT = Generate definitive orbit files"]
-[9.801380157470703, -0.554912269115448, "[TT] Orbit Altitude of the SeaHawk-1 = ~590 km"]
-[11.34609317779541, 5.835565567016602, "[TT] Trays Material of the QSP-1 = Aluminum"]
-[7.742087364196777, 1.589619755744934, "[FF] Capturing Shadows from a Solar Eclipse of the Satellite = Unknown"]
-[8.575936317443848, 4.503811359405518, "[FF] Components of the VELOX-PII = Fault tolerant power system, attitude determination & control algorithms, fine sun sensor, solar panel"]
-[6.901792526245117, 5.313226699829102, "[FF] Components of the MCCM = Digital/analogue ASIC electronics"]
-[5.817817211151123, -0.5297897458076477, "[TT] Lifetime of the Instrument = 15 years"]
-[6.679098129272461, 5.157902240753174, "[FF] Control Function of the PCU = Controls the power supply subsystem"]
-[14.341532707214355, 6.5440263748168945, "[TT] Maximum Battery Power Before 100% Depletion in Orbits of the Satellite = 2 orbits"]
-[13.999425888061523, 6.631476402282715, "[TT] Power Source of the Telemetry System = Non-rechargeable battery"]
-[10.077615737915039, 0.2944706082344055, "[TT] Satellite Separation of the GRACE-FO = 170 and 270 km"]
-[9.213479042053223, 2.7866692543029785, "[FF] Technology of the X-Ray Flux Monitor (XFM) = Highly miniaturized"]
-[9.289595603942871, 1.7474051713943481, "[TT] Travel Speed of the Harpoon = 19m/s"]
-[7.479703903198242, 3.737898826599121, "[FF] Technology of the MSAS = Advanced technologies such as satellite orbit ranging, and ionospheric and tropospheric delay estimation assumption"]
-[6.310522556304932, 6.487709999084473, "[FF] Data Rate of the LLCD = High"]
-[7.683701038360596, -0.8264894485473633, "[TT] KDP-A Review Date of the ICESat-2 = December 11, 2009"]
-[6.2995285987854, 0.9612655639648438, "[FF] Mission Overview Date of the WindSat = Polar Max 2006"]
-[11.759446144104004, 4.784544467926025, "[TT] Canister Size of the IAE Experiment = 2.04 m x 1.08 m x 0.5 m"]
-[13.536974906921387, 6.836971759796143, "[TT] Power Generation of the Existing Arrays = 160 kW"]
-[5.166867256164551, 2.7458691596984863, "[TT] Agency of the QBITO = UPM (Universidad Polit\u00e9cnica de Madrid)"]
-[8.482719421386719, 6.5204243659973145, "[FF] Scanning Method of the OLS = Whiskbroom fashion"]
-[14.278504371643066, 3.0237483978271484, "[TT] Mass of the Global-2 = 56 kg"]
-[6.207861423492432, 6.045272350311279, "[TT] Attenuator Control of the TR Module = 6 bit"]
-[9.15114974975586, 7.432831764221191, "[TT] Ground Resolution of the Multispectral Imager = One meter"]
-[11.2147855758667, 0.9404749870300293, "[TT] Expected Launch Date of the LISA = 2034"]
-[11.383858680725098, 4.987725257873535, "[TT] Length Range of the Straw Tubes = 0.8 m to 2.0 m"]
-[4.56276273727417, -2.793684720993042, "[TT] Frequency (GHz) of the PMI = 10.7"]
-[8.002140045166016, 3.7236549854278564, "[FF] Purpose of the EQUULEUS = Understand the radiation environment in the region of space around Earth"]
-[14.114931106567383, 3.096134662628174, "[TT] Mass of the STF-1 = 4 kg"]
-[6.2906036376953125, 3.6659398078918457, "[FF] Ground Segment of the BRITE-Austria = Unknown"]
-[5.232223987579346, 6.141773223876953, "[TT] Function of the GAMALINK = Communications and networking platform"]
-[8.850200653076172, 3.1128790378570557, "[FF] Purpose of the ICON = Retrieve all of the properties of the system that both influence and result from the dynamical and chemical coupling of the atmosphere and ionosphere"]
-[10.064864158630371, 4.949502944946289, "[TT] Required Operating Cooling Pumps of the AMS-02 = 1"]
-[12.067200660705566, 2.1926302909851074, "[TT] Structure of the CartoSat-2 = Hexagonal-shaped, light weight and compact"]
-[2.999669313430786, 2.238420009613037, "[TT] Pixel Size of the Copernicus Sentinel-1 = About 30 m"]
-[2.9648375511169434, 4.648951053619385, "[TT] Bandwidth Allocation of the TerraSAR-NG System = 1,200 MHz"]
-[9.126399993896484, 7.4860029220581055, "[TT] Resolution of the AEISS-A = 2.0 m for multispectral MWIR images"]
-[7.061402320861816, 0.8492582440376282, "[FF] Research Area of the B2-1 = Gravitational Biology"]
-[13.974780082702637, 7.048703670501709, "[TT] Operating Voltage of the SDR-SDRAM = 3.0 V \u2013 3.6 V"]
-[13.698899269104004, 6.863502025604248, "[TT] Bus Power of the Avionics bus = Less than 50 mA (without radios)"]
-[4.201775550842285, 3.6198182106018066, "[TT] Number of Users of the Galileo = Over 400 million"]
-[5.922562122344971, 7.168594837188721, "[TT] Data Rate of the DH = 4.2 Msample/s"]
-[13.477123260498047, 5.899994373321533, "[TT] Generation Voltage Regulation of the High-voltage solar array = Up to 350 V"]
-[8.29325008392334, 7.204468727111816, "[TT] Light Measurement of the RICH = Photomultiplier tubes"]
-[8.315840721130371, 0.03425266966223717, "[FF] Science Goals of the Philae Lander = Study the elemental, isotopic, molecular and mineralogical composition of the cometary material, the characterization of physical properties of the surface and subsurface material, the large-scale structure and the magnetic and plasma environment of the nucleus"]
-[5.8321709632873535, 3.776228189468384, "[FF] Operator of the Sateliot IoT nanosatellite constellation = Open Cosmos Ltd. (UK)"]
-[8.710793495178223, 8.620284080505371, "[TT] Pixel Sampling Interval of the Spectrometer = 28 \u00b5m"]
-[9.71008586883545, 0.83458012342453, "[TT] Distance from Earth of the Didymos = Within 0.08 AU"]
-[7.942126750946045, 1.1056321859359741, "[FF] Threat of the U.S. Midwest = Agricultural productivity is being threatened by climate change"]
-[9.51067066192627, 7.121877193450928, "[TT] Spatial Resolution of the Stripmap = < 10 m"]
-[11.395431518554688, 8.926279067993164, "[TT] Image Acquisition Date of the MODIS = May 5, 2022"]
-[5.52754020690918, 0.042394187301397324, "[TT] Mission Planned Life-cycle of the SAMPEX = Three years"]
-[6.733999729156494, 1.6071292161941528, "[FF] URL of the First Arab mission to Mars = https://www.marsdaily.com/reports/First_Arab_mission_to_Mars_designed_to_inspire_youth_999.html"]
-[5.299402713775635, 0.7902100086212158, "[TT] Commissioning Phase Start Date of the Electro-L = March 2011"]
-[11.871966361999512, 5.440767288208008, "[TT] Size of the BIRCHES instrument = 10 x 10 x 15 mm"]
-[6.209441661834717, -0.5970933437347412, "[TT] Test Duration of the Tianzhou 2 = 47 minutes"]
-[10.102863311767578, 1.9813097715377808, "[FF] Discovery Date of the Chandra X-Ray Observatory = 31 March 2021"]
-[10.116020202636719, -1.562328577041626, "[TT] Inclination of the Reflector = 23\u00ba"]
-[7.854060173034668, 1.1518580913543701, "[FF] Material of the Habitat = Regolith mixed with water and bovine serum albumin"]
-[10.132156372070312, 1.0338517427444458, "[TT] Distance from Earth of the NGC 5907 ULX = 50 million light years"]
-[3.9150497913360596, 4.248292922973633, "[FF] Operational Modes of the RISAT-1 = Multiple"]
-[6.567778587341309, 2.4141955375671387, "[TT] Affiliation of the MCP = CEA (Commissariat Energie Atomique - or the Atomic Energy Commission of France) + Tohoku University and Riken University (Japan)"]
-[14.258801460266113, 2.9015135765075684, "[TT] Mass of the AprizeSat-4 = 12 kg"]
-[5.798464298248291, -0.8085160255432129, "[TT] Lifetime of the Satellite = 15 years design after IOT"]
-[7.97482967376709, 5.318304061889648, "[TT] Calibration Distance of the FLLS = 7 m and 70 m"]
-[8.127486228942871, 2.9037280082702637, "[FF] Parts Issues of the Geostationary Lightning Mapper (GLM) = Required the GOES-R Program to re-plan the GOES-T schedule"]
-[10.95981502532959, 2.118436098098755, "[TT] Number of Main Sections of the XMM-Newton spacecraft = 4"]
-[4.542595863342285, 5.842987060546875, "[TT] Location Probability of the 406 MHz emergency beacon = Better than 90% on one pass"]
-[4.526697635650635, 6.248215198516846, "[TT] Beacon Frequency of the CUTE-1.7+APD = UHF (437.385 MHz)"]
-[3.4642534255981445, -0.9059291481971741, "[TT] Orbit Type of the ICEYE-X10 = Sun-synchronous"]
-[6.762247562408447, -0.5846005082130432, "[TT] Orbit Period of the Odin = 97.6 minutes"]
-[12.029399871826172, 3.580583095550537, "[TT] Shock Tolerance of the IES = > 1000 G srs"]
-[14.612363815307617, 6.6487956047058105, "[TT] Battery Type of the TUBSAT-N = NiCd"]
-[5.2840447425842285, 0.7741602659225464, "[TT] Commissioning Date of the SSR = April 27-28, 2012"]
-[9.431646347045898, 2.2925617694854736, "[FF] Speed of the Solar Particles = Fastest"]
-[9.585954666137695, 8.098505020141602, "[TT] Optics Type of the CIRC = Athermal"]
-[8.389358520507812, 3.9744632244110107, "[FF] Design Basis of the SWiPS = IES (Ion and Electron Sensor) flown on ESA's comet mission, Rosetta"]
-[8.105860710144043, 4.325672626495361, "[FF] Comparison of the CUMULOS = VIIRS, MODIS, DMSP, CIRC, and related on-orbit microbolometers"]
-[5.598779678344727, 0.10841533541679382, "[TT] Operation Authorization of the ISS = Through 2024"]
-[13.954202651977539, 4.022747993469238, "[TT] Total Instrument Mass of the Detector = 350 kg"]
-[5.308921813964844, 1.0069345235824585, "[FF] Conference Date of the CanX-4 & CanX-5 = April 25-27, 2006"]
-[6.607937335968018, -0.1270464062690735, "[TT] Anomaly Duration of the ASTRO = 22 hours"]
-[10.361366271972656, 7.145220756530762, "[TT] Mesoscale Square Height of the ABI = 1000 km"]
-[8.122692108154297, 2.6897635459899902, "[TT] Measurement Domain of the Sich-2 = Ocean, Land, Snow & Ice"]
-[7.936608791351318, 5.447666645050049, "[TT] Range-independent Biases of the FLLS = \u00b5m"]
-[8.879881858825684, 9.544103622436523, "[FF] Band 1 Resolution of the TANSO-FTS-2 = 0.2 cm -1"]
-[7.82948112487793, 8.72054386138916, "[TT] Spectral Range of the CLARREO = 0.32 to 2.3 \u00b5m"]
-[3.824951410293579, 1.221756100654602, "[FF] Boosters First Stage Recovery of the Falcon 9 = Via an unprecedented precision guided landing on an ocean-going \"drone\""]
-[8.867762565612793, 4.395689964294434, "[FF] Usage of the Sun sensors and gyros = Safe modes"]
-[10.427552223205566, 2.356903314590454, "[TT] X-ray Type of the CuPID = Soft"]
-[11.981240272521973, -0.07323388010263443, "[FF] Purpose of the TESS = Collects light curves on everything in its field of view"]
-[6.184974670410156, -0.3031157851219177, "[TT] Operation Duration of the AMS-01 = 10 days"]
-[9.026904106140137, -1.2745869159698486, "[TT] Orbit Type of the XMM-Newton = Highly eccentric"]
-[8.692378044128418, 8.133291244506836, "[TT] Optical Efficiency of the Overall = 0.4"]
-[6.024179935455322, 3.4400668144226074, "[FF] Cost of the Satellite Constellation = Less than previous constellation cost"]
-[4.778025150299072, 3.2091009616851807, "[FF] Contract of the Thales Alenia Space = Won the first Spacebus Neo commercial satellite contract for a Broadband for Africa mission with Eutelsat (BB4A) to be launched in 2019"]
-[7.506564617156982, 2.8381175994873047, "[FF] Purpose of the Satellite = Pinpoint Methane and CO2 Super Emitters"]
-[8.514592170715332, 1.9358761310577393, "[TT] Spatial resolution of the Ocean surface wind speed = 25 km"]
-[7.759425163269043, 8.029868125915527, "[TT] NEDT System Sensitivity Performance of the ISIR = 0.1 K"]
-[4.443926811218262, 3.1924095153808594, "[FF] Ground Stations of the EDRS = Redu (BE), Harwell (UK), Weilheim (DE), Matera (IT)"]
-[7.837960243225098, 6.029277801513672, "[FF] Purpose of the Lateral System = Map the calculated centroid of the imaged beam, in detector coordinates, to the position of the CCRR"]
-[11.939641952514648, 4.9651899337768555, "[TT] Overall Dimensions of the X50M = 550 x 550 x 760 mm"]
-[3.181558847427368, 4.982473373413086, "[TT] FRS-1 Swath of the RISAT-SAR = 25 km"]
-[4.212970733642578, 4.932981014251709, "[TT] Link Performance of the Alphasat TDP1 = More than 200 successful links"]
-[8.600956916809082, 0.08069043606519699, "[TT] Customization of the Comet = Available"]
-[5.541525840759277, -1.936287522315979, "[FF] Image Release Date of the KOMPSAT-3 = Jan. 03, 2014"]
-[5.190786361694336, 0.4199569523334503, "[TT] Delta-Critical Design Review Completion Date of the TSIS-1 = July 2015"]
-[9.623311042785645, 6.85714054107666, "[TT] Spatial Resolution of the Geodesy Inertial navigation system = 100-1000 km"]
-[10.916472434997559, 10.074707984924316, "[FF] Antiproton-to-Proton Flux Ratio of the Alpha Magnetic Spectrometer = Unknown"]
-[5.731532573699951, 12.150383949279785, "[TT] Wavelength FWHM of an unresolved line of the Spectrometer = 0.020 \u00b5m"]
-[3.744601011276245, 3.9251599311828613, "[TT] Emergency Observation Request Date of the RISAT-1 = Feb 12, 2015"]
-[3.716146230697632, 6.3511176109313965, "[TT] Antenna Quantity of the NSCAT = 6"]
-[7.983157634735107, 6.362875461578369, "[FF] Video Capabilities of the Carbonite Series = High-performance"]
-[4.251022815704346, 0.25261390209198, "[FF] Mission Presentation Date of the FalconSat-7 = Oct. 1-5, 2012"]
-[6.667671203613281, -0.3988480269908905, "[TT] Direct Transmission Delivery Time of the Polar Satellite Data = Virtually at the time of measurement"]
-[13.386944770812988, 7.339832782745361, "[TT] Power of the RA-1 = 130 W"]
-[5.719132900238037, 2.30526065826416, "[TT] Team Size of the New Horizons = About 200"]
-[9.92626953125, -0.29000967741012573, "[TT] Altitude of the Secondary Payloads = ~325 km"]
-[5.375544548034668, 0.8846763372421265, "[TT] Launch Year of the ERO = 2026"]
-[5.1851301193237305, 2.1812691688537598, "[TT] Mission Status of the Sich-2 = Mission complete"]
-[10.235904693603516, 8.049684524536133, "[TT] Aperture of the Telescope = 12 cm"]
-[6.249392032623291, 4.959430694580078, "[FF] Function of the MIU = Provides the interface to the S-band transceiver to receive uplinked commands and downlink telemetry and science data"]
-[6.574540138244629, 4.62677001953125, "[FF] Relative Movement of the LEO Platform = With regard to the payload"]
-[10.081305503845215, 0.9635575413703918, "[TT] Distance from Earth of the Eta Carinae = 7,500 light-years"]
-[9.582111358642578, 8.264341354370117, "[TT] Field of View of the LSI-1 = 29\u00ba"]
-[3.2701241970062256, 5.217458724975586, "[TT] Wave Direction of the SAR = 15\u00ba 360\u00ba"]
-[10.535040855407715, 5.5629353523254395, "[TT] Operating Temperature Range of the CubeSat = -5\u00baC to 20\u00baC"]
-[5.217107772827148, 4.884263038635254, "[TT] GPS Receiver of the ACS = NovAtel OEMV-1"]
-[4.042928695678711, 0.3243807852268219, "[TT] Launch Date of the Corvus-BC 3 = November 28, 2017"]
-[5.150111198425293, 6.994271278381348, "[FF] Data Downlink Intervals of the Transmitter = 4 hr intervals at each perigee"]
-[5.867178440093994, 1.7186589241027832, "[FF] Presentation Location of the MEIDEX = Versailles, France"]
-[12.484402656555176, 0.6518648862838745, "[TT] Image Resolution of the Plato Camera = 20.3 megapixels"]
-[5.906121730804443, -0.6126060485839844, "[TT] Service Life of the Spacelab-1 = 50 missions"]
-[9.718379974365234, 5.252490997314453, "[TT] Platform Fixings of the Hard Stack = Torqued to correct levels"]
-[9.871123313903809, -0.23170986771583557, "[TT] Altitude of the ROSE-L = 693 km"]
-[4.680603981018066, 0.05200941860675812, "[TT] End of Life Date of the Myriade/AstroSat-100 = June 2030"]
-[9.232553482055664, 3.8708178997039795, "[FF] Tuning of the AOCS = Solar array natural mode damping, optimised wheel zero crossing management"]
-[11.794921875, 6.705938339233398, "[TT] Energy of Low Energy Electrons of the SPC = Several eV"]
-[5.105283737182617, 3.3167035579681396, "[TT] Manufacturer of the TRMM = NASA\u2019s Goddard Space Flight Center"]
-[8.786539077758789, 4.990899562835693, "[TT] Pointing Accuracy (Yaw and Pitch Axis) of the Star Tracker = 30 arcsec (3\u03c3)"]
-[9.59100341796875, 4.080515384674072, "[TT] Magnetic Field Alignment of the Dove-1 = About 1\u00ba"]
-[6.719489574432373, 2.214845895767212, "[FF] URL of the Dove = https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=3797&context=smallsat"]
-[7.478251934051514, 4.367652893066406, "[FF] Unknown of the EREP sensors = Unknown"]
-[3.330383777618408, 4.768342971801758, "[FF] SAR Instrument Data Collection of the SeaSat-1 = About 60 hours of data"]
-[8.771814346313477, 6.379742622375488, "[TT] Measurement Methods of the Wave height = 3 ways"]
-[11.082499504089355, 5.4684295654296875, "[TT] Thickness of the Superelastic SMA = 0.2 mm"]
-[10.750661849975586, 1.204593539237976, "[FF] Mass Compared to Sun of the TOI 270 = About 40% smaller"]
-[10.604117393493652, 3.9308159351348877, "[FF] Purpose of the 10 m2 dragsail = Testing"]
-[4.4151387214660645, 1.0969358682632446, "[TT] Establishment Date of the GMES = 2006"]
-[7.4902496337890625, 4.860294342041016, "[FF] Purpose of the MEV = Steering, pointing and relocating another spacecraft"]
-[5.7015228271484375, -0.9326651096343994, "[TT] Design Life of the EO-1 = 2 years"]
-[5.648354530334473, 6.815650939941406, "[TT] Data of the UKube-1 = < 36 kB per orbit"]
-[4.895628929138184, 0.1457950472831726, "[TT] Duration of the NSSL Phase 2 = 2022 until 2027"]
-[10.170435905456543, 1.0069873332977295, "[FF] Distance from Earth of the M83 = 15 million light-years"]
-[11.045673370361328, 5.721260070800781, "[TT] Structure Material of the CeREs = Teflon"]
-[7.985611915588379, 0.052561964839696884, "[FF] Missions of the Altimetry Satellites = TOPEX/Poseidon (1992-2006), Jason-1 (2001-2013), Ocean Surface Topography Mission/Jason-2 (2008-2019), and Jason-3 (2016 to present)"]
-[6.101022720336914, -0.19311903417110443, "[TT] Operation Duration of the FormoSat-2 = 9 years"]
-[6.419049263000488, 3.569894552230835, "[FF] Use of the DMSP-20 = Help plan future launches"]
-[8.284250259399414, 7.057040214538574, "[TT] Number of CIR Photographs of the Metric Camera = 546"]
-[11.024316787719727, 4.832986354827881, "[TT] Tether Length of the TEPCE = 1 km"]
-[14.011520385742188, 3.2690019607543945, "[TT] Total Mass of the MERLIN = 430 kg"]
-[6.302478790283203, 5.575112819671631, "[FF] Memory Module of the MMFU = TFGs (Transfer Frame Generators)"]
-[7.857666492462158, 2.542201280593872, "[TT] Measurement Domain of the Kondor-E = Land"]
-[8.919272422790527, 7.899912357330322, "[FF] Spatial Resolution of the VNIR FPA = Unknown"]
-[6.045042514801025, 4.721604347229004, "[FF] Function of the Satellite Communication Protocol Experiment = Allows satellites to dynamically transfer data"]
-[14.168012619018555, 3.0781219005584717, "[TT] Mass of the HY-2A = ~ 1500 kg"]
-[13.337259292602539, 5.570524215698242, "[FF] Technology of the ROSA = Scalable solar power array"]
-[5.829706192016602, 5.10920524597168, "[FF] Data Encryption of the SeaWiFS = Real time LAC data are encrypted"]
-[7.455524444580078, 6.441269874572754, "[FF] Receiver Function of the SILEX = Power detection device"]
-[12.005133628845215, -0.3332843780517578, "[TT] Start of Science Operations of the TESS = July 25, 2018"]
-[6.369150638580322, -1.153924822807312, "[TT] Mean LTAN of the KOMPSAT-3A = 13:30 hours"]
-[10.236857414245605, 8.096192359924316, "[TT] Clear Aperture of Telescope of the DubaiSat-2 = 40 cm"]
-[3.3338303565979004, 6.080328941345215, "[TT] Radar Antenna Length of the Spacecraft = 16 m"]
-[4.752401828765869, -1.8261336088180542, "[FF] Midway Correction Control of the Chang'e-2 = October 2, 2010"]
-[4.704744338989258, 7.180778503417969, "[TT] Uplink Power of the SARSAT transponder = 32 dBm"]
-[8.16706657409668, 2.998605728149414, "[FF] Primary Objective of the AMSU-A = Provide significantly improved temperature soundings"]
-[6.210410118103027, 4.721554756164551, "[FF] Navigation System of the GIOVE-M = Unknown"]
-[6.253889560699463, 3.9099619388580322, "[FF] Benefits of the EGS-CC = Faster transitions between the life stages of a mission, reduced cost and risk for missions, evolving ground systems for missions of the future, working towards a \u2018European Network of Centers\u2019, providing European industry with a powerful tool with which they can compete on the global market"]
-[3.2122058868408203, 4.941404819488525, "[TT] FRS-1 (Fine Resolution Stripmap Mode-1) of the RISAT-1 SAR instrument = 25 km swath with 3 meter resolution"]
-[5.760204315185547, 7.361274242401123, "[TT] On-board Data Analysis of the GimmeRF = Up to 2 TFLOPs"]
-[8.950234413146973, 5.040344715118408, "[TT] Number of Gyroscopes of the SloshSat = 3"]
-[7.108374118804932, 8.229047775268555, "[TT] SNR of the Instrument = \u2265900"]
-[8.082076072692871, 4.905670166015625, "[TT] Duration of the Calibration Sequence = 2.5 minutes"]
-[9.501709938049316, 0.9776670932769775, "[TT] Speed of the Orion-EFT-1's = 32,000 km/h"]
-[9.284276962280273, 6.951379776000977, "[FF] NDVI Map Spatial Resolution of the Landsat-8 = Unknown"]
-[5.2240142822265625, 0.07621540129184723, "[TT] Launch Date of the KazSTSAT = 3 December 2018"]
-[5.071305751800537, 0.00378412869758904, "[TT] End of Life Date of the Ikonos-2 = 31 Mar 2015"]
-[13.414580345153809, 7.452662467956543, "[TT] Output Power of the MHX-2400 = 30 dBm"]
-[5.584054470062256, -1.9321249723434448, "[FF] Publication Date of the Atlas zur Interpretation von kosmischen Scanneraufnahmen = 1989"]
-[5.787064075469971, 4.430008888244629, "[FF] Monitoring of the EDRS = Not specified"]
-[7.91636848449707, -0.4354403614997864, "[TT] Date of the Ice Maximum = March 21, 2021"]
-[5.646430015563965, 2.7097878456115723, "[FF] Consortium Lead of the Satellites around the Moon = SSTL Lunar"]
-[4.930652141571045, 0.05096695199608803, "[TT] End of Life Date of the Cygnus NG-10 = 25 February 2019"]
-[6.888343334197998, 7.649748802185059, "[TT] Gain of the Reflector = 39 dBi for both beams"]
-[10.950469017028809, 5.636166572570801, "[TT] Erosion Percentage of the Heat Shield = 20%"]
-[3.6370391845703125, 5.4054155349731445, "[TT] Resolution of the Spotlight-2B = 1m"]
-[10.148024559020996, 10.00778579711914, "[FF] Return to Flight Date of the Vega = 3 September 2020"]
-[9.697478294372559, -0.6260775327682495, "[TT] Altitude of the ExoMars Orbiter = Approximately 400 km"]
-[10.319005966186523, 4.530745506286621, "[FF] Type of the Astrofein momentum wheels = Unknown"]
-[8.994866371154785, 5.431427478790283, "[TT] Pointing Agility of the S/C = Roll 10\u00ba in 25 s and 30\u00ba in 45 s, pitch 45\u00ba in 60 s"]
-[4.60612154006958, 5.531601905822754, "[TT] Function of the Beacons with integrated GPS technology = Sends location data through GOES to the SAR network"]
-[10.021286010742188, 4.493483066558838, "[TT] Magnet Power Source of the AMS-02 = Superfluid helium"]
-[6.708075046539307, 4.615472316741943, "[FF] Location of the Payload Modules = Section close to the antenna"]
-[5.896991729736328, 3.004300355911255, "[TT] Projected Price Tag of the WorldView Legion = $600 million"]
-[7.88165807723999, 8.328435897827148, "[TT] Imaging Spectrum of the VIIRS = Longwave infrared (thermal)"]
-[4.844956398010254, 3.2467100620269775, "[TT] Manufacturer of the ETB = AFRL, Kirtland AFB, NM"]
-[7.58988094329834, 7.179855823516846, "[TT] Scanning Period of the MWHS-II = 2.667 s \u00b1 50 ms"]
-[4.787613868713379, 2.5908679962158203, "[FF] Beam Tracking of the Eutelsat Quantum = Enabled"]
-[8.212623596191406, 7.838149070739746, "[TT] VIS Channel Detectors of the SEVIRI = Photo-voltaic silicon diodes"]
-[13.921006202697754, 3.676265239715576, "[TT] Instrument Mass of the DST (Dobson Space Telescope) = < 0.5 kg"]
-[10.756650924682617, 1.2900021076202393, "[TT] Mass of the TOI 700 = Roughly 40% of the Sun\u2019s mass"]
-[11.11172866821289, 0.6406000852584839, "[FF] Imager Stabilization Requirement of the ExoplanetSat = Same fraction of a pixel"]
-[8.278664588928223, 2.5265257358551025, "[FF] Publication Year of the Aerosol Polarimetry Sensor = 2007"]
-[9.381672859191895, 4.335753917694092, "[TT] Sensor Type of the GAS = 3-axis"]
-[9.639762878417969, -0.6744814515113831, "[TT] Orbit of the Dove-2 = 575 km x 575 km"]
-[6.4499735832214355, 4.8071818351745605, "[FF] Function of the HHC = Power, control, command, and telemetry"]
-[9.978145599365234, 5.517948627471924, "[TT] Equipment Temperatures of the Satellite = Stable"]
-[13.864152908325195, 7.043778896331787, "[TT] Operation End Cause of the SeaSat = Abrupt power system failure in the Agena bus"]
-[9.478198051452637, 5.509331703186035, "[TT] Slew Rate of the ISS Platform = 0.067\u00ba/s"]
-[6.9864349365234375, -0.2182348221540451, "[TT] Eclipse Duration at \u03b2=75\u00b0 of the ASTERIA = 0 minutes"]
-[10.753402709960938, -1.1476629972457886, "[FF] Altitude of the SLATS = -60\u00ba"]
-[10.502470016479492, 2.300875425338745, "[FF] Function of the MXS = Demonstration of X-ray communication in space"]
-[10.804584503173828, 6.8618388175964355, "[TT] Effective Received Power (a) of the Triple Mirror = ~200 pW"]
-[5.523691654205322, 4.091075420379639, "[TT] Number of X-Y Planes of the NINA = 16"]
-[10.842377662658691, 1.0313851833343506, "[TT] Primary Temperature of the White Dwarfs = Nearly 50,000 K"]
-[9.424788475036621, 6.899595737457275, "[TT] Field of View of the OMPS Nadir Profile Spectrometer = 16.6\u00b0"]
-[9.19892406463623, 3.1145784854888916, "[FF] Characteristics of the Eruption = Ejection of a hot layer of solar material above a magnetically active region on the Sun's surface"]
-[13.716938018798828, 2.8756580352783203, "[TT] Mass of the Spacecraft = 1700 kg"]
-[5.336923599243164, 5.616944313049316, "[TT] Protocol of the OBC = MIL STD 1553B"]
-[5.678676128387451, 1.6124088764190674, "[TT] Status of the ROSA = Operating nominally"]
-[6.878916263580322, 4.421534538269043, "[FF] Purpose of the Iceberg = Support expanded payload operations"]
-[9.565796852111816, 7.050480365753174, "[TT] Resolution of the MUX = 20 m"]
-[7.881079196929932, 9.100525856018066, "[TT] Wavelength of the SOTA = 1.5 \u00b5m"]
-[5.660763263702393, 7.027673721313477, "[TT] Data Input Rate of the Data Handling System = 336 Mbit/s"]
-[4.872128009796143, 0.3661155104637146, "[TT] Launch Date of the NewMag = Aug. 21, 1996"]
-[11.20498275756836, 4.747673511505127, "[TT] Pit Depth of the Ma'at = 50\u201360 m"]
-[8.14759635925293, 3.1246495246887207, "[TT] Data Focus of the GLM = Near real-time lightning data"]
-[1.7457972764968872, -2.0754597187042236, "[TT] Arrival Date of the Hayabusa-2 = December 7, 2020"]
-[5.735603332519531, 1.0682787895202637, "[FF] International Astronautical Congress Date of the VRSS-1 = Sept. 23-27, 2013"]
-[7.892510890960693, 7.956051349639893, "[FF] Spectral Ranges of the WorldView-110 camera = Eight bands of the short-wave infrared range"]
-[4.319201946258545, 7.378985404968262, "[TT] Downlink Frequency of the TT&C = S-band"]
-[5.593912124633789, 5.712428569793701, "[TT] Type of the Microprocessor = 32-bit ~200 MHz ARM"]
-[5.629080295562744, 0.9693842530250549, "[FF] Test Date of the LARES = 7-14 March 2015"]
-[5.987858295440674, -0.6146929860115051, "[TT] Mission Life of the S/C = Two years (min)"]
-[9.512216567993164, 8.909812927246094, "[TT] Altitude of the Iris Video Camera = 360-460 km"]
-[7.754193305969238, 9.11160659790039, "[TT] Wavelength Range of the InSb = 1.55 - 1.75 \u00b5m"]
-[3.36604380607605, 1.519942283630371, "[FF] Replacement Date of the Sentinel-2A and Sentinel-2B = Unknown"]
-[7.771541118621826, 9.247143745422363, "[TT] Signal Wavelength of the Clementine = 13.19 cm"]
-[8.956221580505371, 0.682745635509491, "[FF] ICDS Redundancy of the ARTEMIS = All units have a redundancy"]
-[10.77815055847168, 7.408892631530762, "[TT] Swath of the ALOS-2 = 40-50 km"]
-[6.691122531890869, 3.7544283866882324, "[FF] URL of the SPOT 6 = http://www.astrium-geo.com/files/pmedia/edited/r18072_9_spot_6_technical_sheet.pdf"]
-[8.287725448608398, 6.860509395599365, "[TT] Imager Type of the Satellite Vu = MWIR"]
-[8.272887229919434, 8.73081111907959, "[TT] Spectral Resolution of the UV-1 = 0.42 nm"]
-[7.378016471862793, 4.058391571044922, "[FF] Performance Simulation of the SWIMSAT = URL: http://journals.ametsoc.org/doi/pdf/10.1175/1520-0426(2001)018%3C0421%3ASARART%3E2.0.CO%3B2"]
-[11.6688232421875, 4.836451053619385, "[TT] Throat Dimension of the CGM = 0.02 mm diameter"]
-[4.402948379516602, 0.7067171931266785, "[TT] Transfer Date of the DMSP = May 1998"]
-[12.163076400756836, 1.94535231590271, "[FF] Presentation Date of the CartoSat-2 = Sept. 29 to Oct. 3, 2008"]
-[3.8853564262390137, 7.847461223602295, "[TT] Modulation Scheme of the VHF COTS transmitter = BPSK"]
-[5.104661464691162, 7.061041355133057, "[TT] Downlink Rates of the LLCD PAT Systems = Up to 311 Mbit/s"]
-[3.2240405082702637, 5.759154796600342, "[TT] Dimensions of the SAR antenna = 2.1 m x 10.7 m"]
-[7.94668436050415, 9.174962043762207, "[TT] Wavelength of the LORE = 675 nm"]
-[3.912310838699341, 6.328385829925537, "[TT] Quantity of the Two omni patch antennas = 2"]
-[8.973149299621582, 1.5698996782302856, "[TT] Observation Speed of the Solar Dynamics Observatory = 200 times faster than real time"]
-[7.493677616119385, 3.0722978115081787, "[FF] Observation Capability of the GEO Satellite = Constant monitoring of quickly developing weather phenomena or diurnal variations in weather events"]
-[3.8233935832977295, 3.4075875282287598, "[TT] Launch Date of the Galileo Second Generation (G2) = 31 December 2024"]
-[6.260537147521973, 0.9496759176254272, "[FF] Suitability for Satellite Flight of the Silkworm = Duration of the development of each stage, especially, the embryo state is well matched with the satellite flight period of SJ-10"]
-[4.443105220794678, -0.23379261791706085, "[FF] Launch Date of the Nauka Development = Unknown"]
-[3.363762140274048, 1.4498441219329834, "[TT] End of Life Date of the Sentinel-5P = September 2027"]
-[6.085105895996094, 6.361569404602051, "[TT] Data Transfer Time of the FTHSI instrument = 6-30 s"]
-[7.574371814727783, 6.98120641708374, "[TT] Frame Rate of the SIS = One frame in 22 seconds"]
-[9.573949813842773, 6.117595672607422, "[TT] Sensor Area of the XGRE = 300 cm2"]
-[8.187602996826172, 0.17635613679885864, "[TT] Operational Status of the Meteor-M-2 = Yes"]
-[4.681516170501709, 0.778113067150116, "[TT] Launch Date of the GOMS-1 = October 31, 1994"]
-[9.828093528747559, 4.483025074005127, "[FF] Control Authority Mechanism of the Magnetorquers = Primary control authority and reaction wheel desaturation at low orbital altitudes"]
-[9.565072059631348, 9.104763984680176, "[TT] Field of View of the IRIS = 171 arcsec"]
-[5.611241817474365, 4.991359710693359, "[TT] Function of the MEXIC = Serve as a host structure for instrumentation analyzers"]
-[13.859350204467773, 3.095144748687744, "[FF] Mass of the ION = Unknown"]
-[7.199076175689697, 4.5629448890686035, "[FF] Design Constraint of the RVX = VBS mounted on the OSC"]
-[5.041495323181152, 3.173295497894287, "[TT] Manufacturer of the Prometheus Block 2 CubeSats = LANL (Los Alamos National Laboratory)"]
-[13.768926620483398, 2.7870616912841797, "[TT] Launch Mass of the Heritage Orbital LEOStar-2 = 325 kg"]
-[10.42355728149414, 1.821135401725769, "[FF] Observation Capability of the NuSTAR = Peered inside dense doughnuts surrounding supermassive black holes"]
-[9.729057312011719, 7.838852882385254, "[TT] FOV Overlap of the COR1 = Pointing stability required 1.5 arcsec over pB sequence (7 s)"]
-[3.923898458480835, 4.302196025848389, "[FF] Purpose of the RADARSAT-2 = Environmental monitoring, natural resource management, and coastal surveillance"]
-[6.053441047668457, 5.487663745880127, "[TT] Redundancy of the EPPS = Fully redundant system"]
-[11.389010429382324, 4.366218090057373, "[TT] Size of the Delphini-1 = 1U"]
-[3.108126401901245, 2.2731876373291016, "[FF] Application Categories of the Sentinel-3 = Marine meteorology, Operational oceanography, Climate change"]
-[13.336362838745117, 6.717970848083496, "[FF] Budgets of the Spacecraft = Mass, Power, Data"]
-[6.474197864532471, 4.341921329498291, "[FF] Ground Systems of the CU-E3 = Two separate ground systems"]
-[11.303545951843262, 5.073975563049316, "[TT] Separation of the OB = About 40 cm"]
-[3.6553845405578613, 6.949596881866455, "[TT] Polarization of the Galileo/GPS antenna = RHCP (Right Hand Circular Polarized)"]
-[6.444585800170898, 6.23978853225708, "[TT] Additional Downlink Subsystem of the Sentinel-1, -2 = Laser Communication Terminal (LCT)"]
-[9.05987548828125, 4.557805061340332, "[TT] Attitude Mode of the SLATS = SPM (Sun Pointing Mode)"]
-[3.4706921577453613, 4.0633649826049805, "[TT] Launch Date of the SAR/Glonass Glonass-K1 No 1 = Feb. 26, 2011"]
-[10.17273998260498, 9.372307777404785, "[TT] Nominal IGFOV of the Band 1 = 1 km"]
-[10.319487571716309, 5.666735649108887, "[TT] Temperature of the 1 W Tactical Cooler = 55 K"]
-[4.888626575469971, 7.398718357086182, "[TT] S-band TxRx Data Rate (TM) of the RF communications = 1.91 Mbit/s or 329 kbit/s"]
-[10.156424522399902, -2.762434959411621, "[TT] Module power (max data rate) of the SLC NAND-FMM = 10.5 W"]
-[8.16966724395752, 0.8069380521774292, "[FF] Composition of the Hamersley Group = Iron-rich rocks, banded iron formations, dolomites, shales, and volcanics"]
-[5.317197799682617, 5.641798973083496, "[TT] Communication Interface of the DCU = Mil-STD-1553 bus"]
-[8.395614624023438, 8.350650787353516, "[FF] Point Spread Function of the IR Instrument = Determines Spectral Resolving Power"]
-[12.25462818145752, 6.929258823394775, "[TT] Energy Range for C of the LEICA = 0.44 - 11.4 7.2 - 160 14 - 210 34 - 120 MeV/n"]
-[5.397645473480225, 3.756589412689209, "[TT] Number of Spacecraft of the Constellation Size = 1 spacecraft cluster at each orbital slot"]
-[5.9550065994262695, -0.4774952232837677, "[FF] Mission Tenure of the RHESSI = 10 Years"]
-[5.054660320281982, 3.4563915729522705, "[TT] Manufacturer of the Drag Augmentation Device = Ryokeiso CO., Ltd."]
-[5.873788833618164, -0.7955443859100342, "[TT] Vehicle Dockings Per Year of the Orion spacecraft = 12-15"]
-[9.675095558166504, 0.15332454442977905, "[FF] Deployment Speed of the Parachute System = 32 km/h"]
-[5.428021430969238, 3.291834831237793, "[FF] Owner of the Lemur-2 = Spire Global"]
-[11.1111421585083, 4.658445835113525, "[TT] Depth of the Firn Drill = About 50 meters"]
-[10.91011905670166, 10.054805755615234, "[FF] Purpose of the Alpha Magnetic Spectrometer (AMS) = Looks for dark matter, antimatter and measures cosmic rays"]
-[10.912537574768066, 7.5425124168396, "[TT] Value of the Swath Width = 15 km"]
-[5.075460910797119, 0.5756194591522217, "[FF] Contract Announcement Date of the Transport Layer Tranche 1 = By the end of the month"]
-[9.261761665344238, 7.057744026184082, "[TT] Raster Resolution of the WorldDEM4Ortho = 24 m"]
-[4.4100565910339355, 7.628242492675781, "[TT] Frequency of the S-band = 1.67-1.71 GHz"]
-[3.4940121173858643, 5.367487907409668, "[TT] Downlink Frequency of the SARR = 1544.5 MHz"]
-[5.828943729400635, 5.041886329650879, "[TT] Software Language of the BMU = ADA"]
-[6.489956855773926, -0.4861607253551483, "[TT] Period of the IRS-1B = 103.2 minutes"]
-[6.6860737800598145, 5.530484676361084, "[FF] Clock Frequency of the dsPIC33F microcontroller = Unknown"]
-[8.656283378601074, 2.374042510986328, "[FF] Data Collection of the ISS-EMIT = Composition of minerals that become airborne dust"]
-[5.407591342926025, 4.17955207824707, "[TT] Constellation Architecture of the CIRCE = Dual satellite bus"]
-[4.972544193267822, 5.737030982971191, "[TT] Operating Mode of the T3000G2 receiver = Dual-frequency mode"]
-[6.532704830169678, 3.1046290397644043, "[FF] Symposium Date of the Space Plug and Play Compatible Earth Observation Payload Instruments = April 8-12, 2013"]
-[9.345791816711426, -1.2300333976745605, "[FF] Eccentricity and Argument of Perigee Adjustment Method of the SJ-9A and SJ-9B = Adjusting the speed increment (position and time) and the semi-major axis"]
-[13.131782531738281, 7.292598724365234, "[TT] Power Consumption of the \u00b5SCIA = 4 W"]
-[7.44705867767334, 3.0068423748016357, "[FF] Importance of the Satellites = Crucial for monitoring climate-related phenomena"]
-[8.870132446289062, 5.847235679626465, "[TT] Pointing Knowledge Stability of the Instrument = \u00b19.7 \u00b5radians over 34 minutes"]
-[7.315649509429932, 6.695400714874268, "[TT] Relation to Single-Detector Integration Time of the Integration Time = m times longer, where m is the number of stages in a row"]
-[1.3697290420532227, 2.780845880508423, "[TT] Principal Absorbing Constituents of the Band 11 = Water vapor"]
-[5.3556718826293945, 2.55062198638916, "[FF] Type of the Princess Nora Bint Abdul Rahman University = Largest all-female university in the world"]
-[5.180612564086914, 2.3561904430389404, "[TT] Mission Type of the ARMADILLO = Non-EO"]
-[9.699604034423828, 4.120030403137207, "[TT] Range of the Magnetometer = \u00b1 100,000 nT"]
-[6.690968990325928, 5.8237624168396, "[TT] Number of OCMs of the Transfer Phase = 14"]
-[8.86713981628418, 6.493056774139404, "[TT] Primary Images of the PROBA-V = 14.021"]
-[6.539535999298096, 5.618172645568848, "[FF] Conference Date of the CubeSat Laser Communication Crosslink Pointing Demonstration = August 3-8, 2019"]
-[6.572247505187988, -0.4917173385620117, "[TT] Days in Space of the Genesis-2 = More than 150 days"]
-[8.15552806854248, 8.278508186340332, "[TT] Resolving Power of the Visible Channel = 300"]
-[6.411221027374268, 1.3801498413085938, "[TT] Launch Date of the COSMO-SkyMed-4 = Nov. 6, 2010 (UTC)"]
-[5.108458995819092, 8.391836166381836, "[TT] Pulse Bandwidth of the SIRAL = 320 MHz"]
-[9.278339385986328, -0.4794687032699585, "[TT] Orbit Altitude of the MEOSAR = 2000 - 35,786 km"]
-[7.759705543518066, 1.5164417028427124, "[FF] Memorandum of Understanding Date of the Global Precipitation Measurement (GPM) = Aug. 3, 2009"]
-[6.659919261932373, 5.289412021636963, "[FF] Function of the Analog I/O power switch board = Control instrument power"]
-[3.369363307952881, 5.337384223937988, "[FF] Reference Position of the EDOT = Center of the SAR antenna"]
-[9.178325653076172, 4.727934837341309, "[FF] Attitude and Orbit Control System of the CHAMP = Unknown"]
-[9.433320045471191, 7.058533191680908, "[TT] Spatial Resolution of the OLCI = 300 m"]
-[5.618495941162109, 5.687163829803467, "[TT] Microcontroller Architecture of the CDHS = 16 bit, modified Harvard architecture"]
-[10.656434059143066, 0.9694067239761353, "[TT] Diameter of the Kepler-442b = 33% bigger than Earth"]
-[6.003945350646973, -0.5897703766822815, "[TT] Deorbiting Time of the IDEAS = Within about 25 years"]
-[5.068678379058838, 2.013050079345703, "[TT] Mission Status of the GOLD = Operational (nominal)"]
-[4.836780548095703, -0.9785645604133606, "[FF] Launch Date of the FengYun 4 = April 3, 2012"]
-[11.003280639648438, 4.041260242462158, "[TT] Inflatable and Sail Payloads Size of the InflateSail = 2U"]
-[8.395270347595215, 5.5670905113220215, "[TT] Precision of the TanSat = 1%"]
-[5.535449981689453, -1.873152256011963, "[TT] Country of Origin of the KOMPSat-5 = South Korea"]
-[6.644969940185547, -0.49750879406929016, "[TT] Period of the SPROUT = 97.4 minutes"]
-[6.947671413421631, 7.530282020568848, "[FF] 3 dB Beamwidth of the Satellite Device = 2.0\u00ba\u00b10.1\u00ba"]
-[12.859681129455566, 7.540061950683594, "[TT] Power Consumption of the SEIS Instrument = Around 1W"]
-[5.3435187339782715, 1.0480023622512817, "[FF] Development Date of the ABI = Nov. 3-5, 2009"]
-[3.0501062870025635, 4.488581657409668, "[TT] TOA/FOA Measurement of the GISAR = High accuracy"]
-[11.710328102111816, 4.678874969482422, "[TT] Bottom Plate Shape of the Baumanets-2 = Hexagonal"]
-[5.189894676208496, 3.8549091815948486, "[TT] Number of Satellites of the Sentinel-2 = 4"]
-[8.432217597961426, 6.340020179748535, "[FF] Image Capture of the Worldview-4 = SpaceX's first stage"]
-[5.228524684906006, 8.361186027526855, "[TT] Channels of the MWI = 10 GHz to 89 GHz"]
-[10.137031555175781, 4.604008674621582, "[TT] Reaction Wheel Spin Rate of the Integral = About 17 degrees per minute"]
-[4.850860595703125, 7.208639621734619, "[TT] Maximum Daily High-Speed Downlinks of the NEMO-AM = 2"]
-[5.356794834136963, 7.2492523193359375, "[TT] Minimum SNR of the NEMO-HD = 75"]
-[6.37577486038208, 2.9414753913879395, "[FF] Operation and Control of the Satellite = Brazil, China"]
-[6.45427131652832, -0.2683868706226349, "[TT] Repeat Period of the T/P = About 10-day"]
-[8.71627140045166, 3.270287036895752, "[FF] Objective of the EPP = Measure electron density and temperature in the upper atmosphere"]
-[4.2419047355651855, 1.9040919542312622, "[FF] Launch Date of the NigeriaSat-X = Unknown"]
-[5.01819372177124, 0.5234726071357727, "[TT] Start Date of the ELFIN = 2012"]
-[7.628307342529297, 0.834596574306488, "[FF] Symposium Date of the Space based observation of lunar impact flashes = 3-9 June 2017"]
-[12.009223937988281, 6.5418500900268555, "[TT] Energy at Which Fraction Starts to Increase of the AMS = 8 GeV"]
-[5.3529181480407715, 3.971623420715332, "[TT] Number of Satellites of the Unseenlabs' Constellation = 3"]
-[11.813629150390625, 6.70070743560791, "[TT] Energy Range for Ions of the MagEIS = 20 keV to 1 MeV"]
-[7.985159397125244, 4.351119041442871, "[FF] Objective of the CREDO-II = Characterize the radiation dose received by the spacecraft"]
-[9.907493591308594, 2.7901527881622314, "[TT] Launch Date of the CubeRRT = 21 May 2018"]
-[3.6843953132629395, 5.444586753845215, "[FF] Resolution of the Spotlight-1A = Finest"]
-[9.28437328338623, 3.2019400596618652, "[TT] Instrument Type of the COR1 = Internally occulted Lyot coronagraph"]
-[4.524991989135742, 7.707337379455566, "[TT] Frequency of the Antenna = 1090 MHz"]
-[10.074015617370605, 1.4220337867736816, "[FF] Function of the Gaia = Measure the position, movement, distance, and characteristics of billions of stars"]
-[8.036820411682129, 7.1711015701293945, "[TT] Variation of the TSI Monitoring Device = Approximately \u00b10.05%"]
-[6.7341203689575195, -0.38114094734191895, "[TT] Period of the Satellite = 98.5 minutes"]
-[4.264583110809326, 7.106675624847412, "[TT] TT&C Function of the COSMO-SkyMed-1 = S-band"]
-[4.501358985900879, 0.6465643644332886, "[TT] Integration Date of the SUVI = 2014"]
-[7.930609703063965, 0.08166341483592987, "[TT] Asteroid Spin of the TAG = 1.4\u00ba/min"]
-[16.50069808959961, 3.598386287689209, "[TT] Next Satellite Launch Date of the OneWeb = July 1"]
-[5.323442459106445, 3.3903615474700928, "[FF] Closure Reason of the Factory = Pandemic"]
-[6.429252624511719, -0.6501574516296387, "[TT] LTDN of the SuperView-1 01 and Superview-1 02 = 10:30 hours"]
-[9.77874755859375, -0.38127413392066956, "[TT] Flight Altitudes of the MERLIN = Low"]
-[8.070260047912598, 3.492624521255493, "[FF] Transmission Spectra of the Altitude Range = 1 to 99%"]
-[7.8558030128479, -0.9365389943122864, "[TT] Measurement Comparison of the ICESat-2 = February/March 2019 ICESat-2 measurements with those calculated using ICESat in February/March 2008"]
-[8.126612663269043, -0.6558542847633362, "[TT] Ice Volume of the CryoSat = 1Gt corresponds to a volume of 1 km3"]
-[13.000686645507812, 7.0753278732299805, "[TT] DFPSCAT Power Requirement of the WCOM = 800 W"]
-[7.9389824867248535, -1.0233103036880493, "[TT] Computer Algorithms of the ICESat-2 = Being refined"]
-[10.644189834594727, -1.2122480869293213, "[FF] Change of \u03b2 Angle of the SLATS = Consists mostly of the long-term change of right ascension of the ascending node by geopotential (d\u03a9/dt)"]
-[9.51262378692627, 4.709849834442139, "[FF] Doppler Shift of the Spinning Disk = Happening due to the spinning disk"]
-[6.78740930557251, 6.636289119720459, "[FF] Successful Laser Links of the European SpaceDataHighway = 20,000"]
-[11.847665786743164, 4.746752738952637, "[TT] Outer Diameter of the Vacuum Tank = 2.7 m"]
-[5.635072708129883, 5.738285541534424, "[TT] Microprocessor of the PCU = 16 bit Microprocessor (H8/3048F)"]
-[10.97292423248291, 7.581362724304199, "[TT] Swath Width of the MSC = 51 km"]
-[6.026269912719727, 0.7439096570014954, "[FF] Data Collection Duration of the OMI = Over a decade"]
-[11.924825668334961, 4.942509174346924, "[TT] Size of the TDU = 370 mm x 350 mm x 130 mm (width x depth x height)"]
-[7.528718948364258, 4.861874103546143, "[FF] Match Process of the VBS = Equipped with a suite of filters, testing the match between the measured and the reference target model"]
-[5.588221073150635, 6.5605034828186035, "[TT] Advanced Mode Daily Capacity of the EDRS-A node = 16.2 TB/day"]
-[5.483928680419922, 7.155006408691406, "[TT] Receiver Data Rate of the LCT = 1.8Gbit/s"]
-[5.761953830718994, 6.724802494049072, "[TT] Average Data Rate of the Telescope = 3.6 Gbit/day"]
-[7.742731094360352, 0.35606932640075684, "[TT] Dry Conditions Frequency of the GRACE-FO = Once every 50 years"]
-[6.203463077545166, 3.5462594032287598, "[TT] Quantity of the Auxiliary demonstration experiments = 5"]
-[9.374621391296387, 3.713717222213745, "[FF] Function of the Magnetometer = Measure the Earth's magnetic field (strength and direction)"]
-[11.212462425231934, 3.6709065437316895, "[FF] Effectiveness of the Hollow Cathode Plasma Contactor = Most effective technology for mitigating charging effects"]
-[10.399271965026855, 7.492978096008301, "[TT] Swath Width of the Scanning geometry = 2800 km"]
-[4.4982218742370605, 3.0071396827697754, "[TT] Location of the GFZ = Potsdam, Germany"]
-[5.264432430267334, 4.041493892669678, "[TT] Number of Satellites of the Lightspeed = 198"]
-[11.435513496398926, 2.168766498565674, "[TT] \u0394V (cm/s) of the Cosmos 2251 Debris = 1.80"]
-[4.432544708251953, 7.792187213897705, "[TT] Frequency of the Ka-band Channels = 30 GHz uplink, 20 GHz downlink"]
-[11.803982734680176, 6.722874164581299, "[TT] Alpha-particle Energy Range of the CPD = 1-100 MeV"]
-[9.695775032043457, 4.639529705047607, "[TT] Attitude Control of the UniSat-1 = Spin-stabilized at 5 rpm with the spin-axis normal to the orbital plane"]
-[6.313869953155518, 3.6743693351745605, "[TT] Operational Name of the GOES-T = GOES-18"]
-[5.736693859100342, 1.024911642074585, "[FF] International Astronautical Congress Date of the 3MI = 25-29 Sept. 2017"]
-[10.84589958190918, 7.506859302520752, "[TT] Swath Width of the QuickBird-2 = 16.5 km"]
-[11.178617477416992, 5.939630031585693, "[TT] Material of the HiRAIS = Zerodur"]
-[8.22201156616211, 5.651040554046631, "[TT] Absolute Accuracy of the FFRF sensor = 1o on LOS"]
-[3.3680360317230225, 5.21046257019043, "[TT] Radio frequency (GHz) of the SAR = 1.3"]
-[7.980470180511475, 0.11842755973339081, "[TT] Operation of the GRACE-FO = Orbit Earth and measure changes in mass below"]
-[8.378607749938965, 4.749406337738037, "[FF] Components of the ADCS = 1 GPS receiver, 2 IMUs, 1 dual-FOV sun sensor, 5 coarse sun sensors, 3 magnetic torquers"]
-[9.513833045959473, 4.621560573577881, "[FF] Attitude Control Algorithms of the ADCS = Runs"]
-[8.964847564697266, 5.693570613861084, "[TT] Bore Site Shift of the OCO Instrument = ~70 arcsec"]
-[8.672697067260742, 7.5638604164123535, "[TT] ROIC Size of the CMOS Active Pixel Sensor = 640 x 480 pixels"]
-[8.3261137008667, 1.4437509775161743, "[FF] Salinity of the Bay of Bengal = Low"]
-[6.914306163787842, 7.389462947845459, "[TT] Beam Diameter of the LRI = 5\u00b10.5 mm"]
-[8.639616012573242, 2.3779139518737793, "[FF] Objective 1 of the EMIT = Deliver a new improved assessment of the heating and cooling effects of mineral dust in the Earth\u2019s atmosphere"]
-[6.1898674964904785, 4.479334354400635, "[FF] Functional Areas of the MM = Space-ground communications, Command generation, Telemetry (TT&C) processing, Mission operations, Product monitoring"]
-[3.703187942504883, 6.576653957366943, "[TT] Antenna Beam Width of the NSCAT = 25\u00ba (3 dB broad beam) =0.42\u00ba (3 dB narrow beam)"]
-[9.365487098693848, 8.62488842010498, "[TT] Slit Width of the Instrument = 4 arcmin"]
-[6.883650779724121, 4.134184837341309, "[TT] On-board Computer of the DMSP-19 = Upgraded"]
-[9.224113464355469, 7.107410907745361, "[TT] Image Resolution of the MTG-S Spacecraft = 0.5 to 2 km"]
-[10.38558292388916, 7.266495704650879, "[TT] M1 Mirror Diameter of the TX Telescope = ~220 mm"]
-[6.908979892730713, 8.912262916564941, "[TT] Wavelength of the POLDER-2 = 443 nm"]
-[10.191534042358398, 5.7932257652282715, "[TT] Temperature Errors of the CrIS-based target = <100 mK"]
-[7.74038553237915, 1.3928929567337036, "[FF] Measurement Capabilities of the ROSE-L = Land, disasters, geohazards, and the cryosphere"]
-[3.6870367527008057, 3.8156888484954834, "[TT] Launch Year of the RISAT-1 = 2012"]
-[8.683998107910156, 4.8959784507751465, "[TT] Star Magnitude Registration of the Camera System = 4 and brighter"]
-[7.564136028289795, 3.4531707763671875, "[TT] Sensor Payloads Capability of the Gen-3 Satellite = See at nighttime, in low light conditions and in bad weather"]
-[4.973243236541748, -0.40702131390571594, "[TT] Launch Time (UTC) of the SLATS / Tsubame = 01:26:22"]
-[9.25469970703125, 5.092151165008545, "[TT] Angular Velocity of the Maneuver Rate = 3\u00ba/s"]
-[8.080195426940918, -0.43902724981307983, "[TT] Greenland Ice Loss of the GRACE = 600 gigatons in two months"]
-[13.347488403320312, 7.068657875061035, "[TT] Power of the QSat = 74 W"]
-[8.080103874206543, -1.0156456232070923, "[FF] Data Type of the ICESat-2 = Elevation"]
-[8.052978515625, 6.627776145935059, "[TT] Junction Type of the Device = P-type in an n-type substrate"]
-[8.022732734680176, 2.0140228271484375, "[FF] Ephemeris Improvement of the SeaSat = Expected"]
-[5.381893157958984, 8.776354789733887, "[TT] Bandwidth of the Band 9 = 0.235 \u00b5m (25 cm -1)"]
-[7.121729373931885, 1.8513535261154175, "[FF] URL of the Solar X-ray Imager = http://goes.gsfc.nasa.gov/text/databook/section06.pdf"]
-[13.522217750549316, 6.0109381675720215, "[TT] Voltage of the High-voltage solar array = 300 V"]
-[10.192214965820312, 4.5618815422058105, "[TT] Wheel Type of the ADCS = 30 mNms wheel"]
-[7.165756702423096, 2.7634129524230957, "[TT] On-orbit operations start date of the MethaneSAT = Q4 2022"]
-[8.170317649841309, 8.51223373413086, "[FF] Micro-Roughness of the ASPIICS = 1 nm RMS"]
-[7.8039469718933105, 7.524478912353516, "[TT] LVDS Image Data Ports of the CSM = Quantity: 4"]
-[8.77164363861084, 7.756026268005371, "[TT] Detector Output Sampling Rate of the INSAT-3D Imager = 5460 samples/s for MIR, WV, TIR-1 and TIR- 2 channels and 21840 samples/s for the VIS and SWIR channels"]
-[13.763540267944336, 5.971197128295898, "[TT] Regulated Voltage of the GHGSat-D = 5 and 3.3 V"]
-[8.301030158996582, -0.07342095673084259, "[TT] Event Cause of the LROC = Hit by a tiny meteoroid"]
-[11.424570083618164, 3.5045223236083984, "[TT] Maximum Relative Distance of the CNAPS = 1000 m"]
-[6.231215476989746, 0.1812441051006317, "[TT] Crew Capacity of the MPCV = 2\u20136 astronauts"]
-[7.353055477142334, 4.963382244110107, "[TT] Instrument of the TEMPEST-D = Radiometer"]
-[7.818944931030273, 6.9291582107543945, "[FF] Instrument Concept of the IASI-NG = Mertz Interferometer allowing to assess the Self Apodization issue by a Field Effect Compensation"]
-[5.950372695922852, 0.6964165568351746, "[FF] Discovery Date of the TLE Phenomenon = Sept. 22, 1989"]
-[4.879946231842041, 0.4818219840526581, "[TT] Launch Date of the SPIRRAL = 2023"]
-[1.7444032430648804, 6.156237602233887, "[FF] Interaction of the DM particles = Very weakly with normal matter"]
-[9.417886734008789, 0.9014310240745544, "[TT] Closest Approach to Sun's Surface in 2022 of the Solar Orbiter = Within 48 million km"]
-[7.897483825683594, 5.1035261154174805, "[FF] Geometric Calibration/Validation of the PROBA-V = Implemented"]
-[5.706823348999023, -0.9251202344894409, "[TT] Design Lifetime of the ERBE = 3 years"]
-[7.578093528747559, 2.1848666667938232, "[FF] Purpose of the Satellites = Detect and reduce plastic pollution in the ocean"]
-[11.73450756072998, 4.331616401672363, "[TT] Dimensions of the TanSat = 150 cm x 180 cm x 185 cm"]
-[5.492021083831787, 4.906455993652344, "[FF] Signal Tracking of the TriG receiver = GPS, Galileo, CDMA GLONASS, Compass"]
-[3.5923891067504883, 1.5955396890640259, "[FF] IAC Presentation Date of the GMES Sentinel-1 = Oct. 12-16, 2009"]
-[6.510678291320801, 7.466966152191162, "[TT] Useful Data Bits of the MEV = 10"]
-[10.655957221984863, 5.758459091186523, "[TT] Measurement Range - Electron Temperature of the ISL Instrument = 500-3000 K"]
-[8.619281768798828, 3.591111898422241, "[TT] Observation Method of the ILAS-II = Solar occultation"]
-[9.668469429016113, 1.80563223361969, "[FF] Type of the Orphan Cloud = Isolated cloud in a galaxy cluster"]
-[11.818778991699219, 5.036211013793945, "[TT] Structure Size of the AlSat-2 = 60 cm x 60 cm x 100 cm"]
-[8.380334854125977, 2.7568936347961426, "[FF] Detection of the ILAS = Polar Stratospheric Cloud"]
-[5.923268795013428, 0.9544209837913513, "[FF] Image Acquisition Date of the PROBA-V = Feb. 7, 2014"]
-[12.128313064575195, 6.093717098236084, "[TT] Data Collected of the AMS Experiment = More than 90 billion cosmic rays"]
-[10.088260650634766, 4.54323673248291, "[FF] Activation Method of the Gas Generator = Gas release into the chamber volume"]
-[3.8651247024536133, 7.876025199890137, "[TT] Modulation of the RF Communications = BPSK"]
-[10.466034889221191, 2.8061180114746094, "[FF] Construction Time of the Nanosatellite Tracking Ships = Seven Months"]
-[6.27698278427124, -0.096181720495224, "[TT] Temporal Sampling of the Aeolus = 12 hours"]
-[8.049273490905762, 5.089721202850342, "[FF] Required Precision of the O3 Profile = FT (ppbv)"]
-[7.551884651184082, 3.2864973545074463, "[FF] Contents of the Level-2 = Granule scene and global (tile) data of geophysical parameters"]
-[9.574584007263184, 7.062294960021973, "[TT] Resolution of the VISIM = < 1 km"]
-[11.66496467590332, 6.837308883666992, "[TT] Energy Resolution of the ART-XC = 10% at 14 keV"]
-[9.415401458740234, 3.7266552448272705, "[FF] Contribution of the Scalar Magnetometer (OVM) = Improved understanding of ionospheric and magnetospheric current systems"]
-[7.614654541015625, 1.2815290689468384, "[FF] Water Points Connection Goal of the Astrocast = 150 water points in 2022 in Senegal"]
-[5.382213115692139, 7.712355613708496, "[TT] EIRP of the Feeder Link = 44 dBW @ NPR=20 dB"]
-[10.115633010864258, -1.5088832378387451, "[TT] Inclination of the Satellite = 97.44\u00ba"]
-[11.31482219696045, 5.851812839508057, "[TT] Truss Structure Material of the ALI = Invar"]
-[10.415783882141113, 7.57335090637207, "[TT] Number of Spectral Bands of the S-192 optomechanical scanner = 13"]
-[11.99743938446045, 3.5100903511047363, "[TT] Plenum Pressure Threshold of the Thruster = 80% of the current main tank pressure"]
-[7.3128581047058105, 2.874159336090088, "[FF] Function of the INSAT-3D imager = Provide accurate and higher resolution meteorological observations"]
-[10.081121444702148, -1.568939447402954, "[TT] Inclination of the CALIPSO = 98.05\u00ba"]
-[8.08101749420166, 1.2957866191864014, "[FF] Rainfall Accumulation of the IMERG = April 12 to April 19"]
-[9.503110885620117, 0.8670760989189148, "[TT] Distance from Pluto of the New Horizons = Nearly 500 million km"]
-[10.65910530090332, 7.430698394775391, "[TT] High Wind Swath Width of the SASS = 250 km"]
-[10.469236373901367, 7.225096225738525, "[TT] CONUS Sector Area of the Instrument = 5000 km x 3000 km"]
-[4.815976619720459, 2.9237637519836426, "[TT] Location of the Deployable Space Systems = Santa Barbara, California"]
-[6.336492538452148, 3.980219602584839, "[FF] Main Payload of the Eutelsat 9B = Unknown"]
-[5.208327293395996, 0.8227420449256897, "[TT] Launch Date of the ASNARO = Nov. 6, 2014"]
-[6.299857139587402, 4.774147033691406, "[FF] Operator of the MOC/DC = AFRL"]
-[6.3004631996154785, 5.381623268127441, "[FF] Components of the TAMU = 8051 microcontrollers, 4 Mbit Magnetic RAM, and CAN-bus interface"]
-[13.774343490600586, 6.7643585205078125, "[FF] Type of the P31us EPS = Power System"]
-[9.66677474975586, 1.404811143875122, "[TT] Service Continuity of the Pl\u00e9iades Neo = 15 years"]
-[10.227251052856445, 8.352720260620117, "[TT] Entrance Pupil Diameter of the Telescope Optical Unit (TOU) = 120 mm"]
-[7.8910651206970215, 2.339609146118164, "[FF] Objectives of the NIRST = Hot spot events, sea surface temperature measurements Monitoring of hot spots caused by biomass fires and volcanic eruptions, estimation of fire radiative power Measurements of sea surface temperature"]
-[9.77269458770752, -0.34042200446128845, "[TT] Altitude of the Shakuntala = 480 km"]
-[6.705510139465332, -0.658726692199707, "[TT] Orbit File Generation Period of the EDOT = 24 hours"]
-[4.529065132141113, 7.005555152893066, "[TT] Communication System of the TRMM = Four radio frequency (RF) links"]
-[6.422877311706543, 5.317646026611328, "[FF] Base carrier board of the C&DH subsystem = Contains all the peripheral ports"]
-[7.951269149780273, 1.3695738315582275, "[FF] Aerosol Events of the SAGE III = Wildfires in the Pacific Northwest in 2017, Alberta, Canada and Siberia, Russia in mid to late 2019, eruptions of Ambae on the south Pacific island of Vanuatu in mid-2018, and Ulawun in Papua New Guinea in mid-2019, Raikoke volcano on the northwest Pacific Kuril Islands erupted in June 2019"]
-[7.986398696899414, 5.379132270812988, "[FF] Quantity of the OSL Dosimeter = 1"]
-[6.821058750152588, 5.718960762023926, "[TT] Total of the Total = 31369"]
-[4.549807548522949, 5.78639554977417, "[TT] Location Accuracy of the 121.5 MHz emergency beacons = About 20 km"]
-[4.671555042266846, 3.167642116546631, "[TT] Manufacturer of the Syracuse 4A = Thales Alenia Space"]
-[4.931270122528076, 8.218941688537598, "[TT] Frequency Range of the CubeRRT RFE = 6 to 40 GHz"]
-[6.890631675720215, 2.2109038829803467, "[FF] Mission Type of the Hinode = Solar Study"]
-[5.54435920715332, 2.9209258556365967, "[FF] Affiliated Organizations of the InSight Lander = NASA, German Aerospace Center (DLR)"]
-[4.359433174133301, 7.396388530731201, "[FF] Communication Link Frequency of the DRTS = Ka-band for mission data and S-band for TT&C data"]
-[13.850412368774414, 5.954857349395752, "[TT] Continuous Peak Demand Operations with Solar Power of the Daughter Battery Module = ~20 Whr"]
-[7.636773586273193, 0.7653012871742249, "[FF] Volcanic Activity of the Moon = Prolonged"]
-[10.571715354919434, 2.9415555000305176, "[TT] Platform of the GaoJing / SuperView minisatellites = CAST3000B light agile platform"]
-[8.396565437316895, 5.522346496582031, "[TT] Velocity of the GPS Receiver = Up to 10,000 m/s"]
-[11.102158546447754, 5.530789852142334, "[TT] PCB Technology of the OPSE = Flex-rigid"]
-[7.609240531921387, 5.078171253204346, "[TT] Number of RADFETS of the SMX-1 = Three"]
-[10.202961921691895, -0.4486042857170105, "[TT] Orbit Altitude of the CubeSat satellites = ~300 x 860 km"]
-[6.836167335510254, -0.6471012234687805, "[TT] Orbital Period of the Orbit = 100.8 min"]
-[11.405086517333984, 4.353050231933594, "[TT] Size of the QBus-1 = 2U"]
-[11.596007347106934, 3.8543336391448975, "[TT] Value of the Use ratio of IES = 0.3"]
-[4.7629804611206055, 0.41247671842575073, "[TT] Launch Date of the Priroda module = April 23, 1996"]
-[9.40287971496582, 6.108024597167969, "[TT] Downlink Elevation Angle of the GRB = 5\u00ba"]
-[5.710050582885742, 4.045199871063232, "[TT] Instrument Type of the XRD and GRD instruments = XRD and GRD"]
-[8.506597518920898, 9.487071990966797, "[TT] Responsivity Measurement of the Responsivity Measurement = 1.36 A/W"]
-[8.803362846374512, 6.846271514892578, "[FF] Image Resolution of the RISING-2 = Unknown"]
-[8.197410583496094, -0.45293042063713074, "[FF] February Extent Deviation of the Arctic Sea Ice = 1.35 million km2 below the 1981\u20132010 average"]
-[11.09675121307373, 5.3484344482421875, "[TT] Pore Size of the Membranes = 100 nanometers or smaller"]
-[7.738156795501709, 5.80903434753418, "[FF] Operation of the Radiometers = Alternated at a rapid rate"]
-[5.933846473693848, 4.904470443725586, "[FF] Function of the Enterprise Service Bus = Support a common set of message exchanges for both intra-and inter-element communication"]
-[12.873601913452148, 7.55302095413208, "[TT] Power Subsystem Requirement of the BIRCHES instrument = 10-15 W"]
-[5.60312032699585, -0.8053672909736633, "[TT] Design Life of the GOES-R = At least 14 years"]
-[5.77645206451416, 7.167273044586182, "[TT] Data Rate of the HEED = 0.19 kbit/s"]
-[6.5854268074035645, 4.571105480194092, "[FF] Components of the FDIR System = On-ground system, Automation system, MOIS Event Monitor"]
-[6.456465244293213, 3.2619497776031494, "[TT] Imaging Conditions of the BlackSky Satellite Constellation = Variety of conditions"]
-[5.100340843200684, 8.329076766967773, "[TT] Bandwidth of the SLA-1 = Up to 250 MHz"]
-[11.109823226928711, 1.31306791305542, "[FF] Gravitational Wave Detection of the LISA = Yes"]
-[8.831271171569824, 7.743161678314209, "[TT] VIS and SWIR Sample Size of the INSAT-3D Imager = 16 \u00b5rad E/W"]
-[8.898792266845703, -0.30260539054870605, "[TT] Pointing Accuracy of the Meteor-M2 = 0.1\u00ba"]
-[9.215279579162598, 4.324182510375977, "[FF] Orientation of the SA (Solar Array) = 40\u00ba ahead of the +Y axis and 40\u00ba behind the -Y axis"]
-[2.8661816120147705, 0.09147365391254425, "[TT] J2000 right ascension (deg) of the J1846-0258 = 281.60392"]
-[10.545011520385742, -0.28774404525756836, "[TT] Orbital Height of the Tandem-L = 745 km"]
-[5.867684841156006, -0.6239649653434753, "[TT] Passes in 1-year mission lifetime of the Satellite = ~1000"]
-[3.3578908443450928, 5.314979076385498, "[TT] Reflector Diameter of the L-band SAR instrument = 12-m"]
-[9.203907012939453, 1.9052435159683228, "[FF] Target of the Harpoon = Structural panels on old, large satellites"]
-[3.3831987380981445, 5.0449113845825195, "[FF] Operation of the Staggered SAR = Continuously varying the PRI in a cyclic manner"]
-[7.47108268737793, 4.3422417640686035, "[FF] Operations Concept of the ABEX = Wavefront timing for sGRB detection"]
-[6.728545665740967, 4.965970993041992, "[FF] Control Algorithm of the EIRSAT-1 = \u2018Wave based control' algorithm"]
-[6.164058685302734, 2.7654788494110107, "[FF] Team Members of the Advanced On-Board Calibration of Space Systems = John C. Fleming, Sandra Collins, Beth Kelsic, Nathan Schwartz, David Osterman, Bevan Staple"]
-[7.007654666900635, 6.787591934204102, "[FF] Dicke Load Measurement of the MWR = During the second half of the Dicke cycle"]
-[9.515276908874512, 6.054677963256836, "[TT] Collimator Angle of the Instrument = Nominal 10o full angle"]
-[11.533880233764648, 4.7943196296691895, "[TT] Formation Shape of the MMS = Tight pyramid"]
-[4.5192179679870605, 1.5372402667999268, "[TT] Launch Date of the TUBSAT = September 13-16, 1993"]
-[5.724038600921631, 3.2342567443847656, "[TT] Grant Amount of the SpaceChain = $596,000"]
-[9.297809600830078, 5.08598518371582, "[TT] Attitude Control Error of the ETS-VIII LRRA = Roll (< \u00b10.05\u00ba), Pitch (< \u00b10.05\u00ba), Yaw (< \u00b10.15\u00ba)"]
-[5.808155059814453, 7.147035121917725, "[TT] Data Rate of the FGM = 0.80 kbit/s"]
-[9.545388221740723, 0.9607998728752136, "[TT] Closest Edge Distance from Earth of the Heliosphere = More than ten billion miles"]
-[6.307603359222412, 5.478400707244873, "[TT] Initiator of the CSD = Reusable"]
-[13.780620574951172, 2.9187839031219482, "[TT] Mass of the Spacecraft = 138 kg"]
-[10.350452423095703, 2.112206220626831, "[TT] Function of the NuSTAR = Collects X-rays"]
-[12.038469314575195, 6.240872383117676, "[FF] Observation of the AMS-01 = Millions of helium nuclei, but no antihelium"]
-[5.21858024597168, 1.9855530261993408, "[TT] Mission Status of the RemoveDebris Mission = Ongoing"]
-[5.005063533782959, 7.304736614227295, "[TT] Maximum Data Rate of the RF communications = 640 Mbit/s"]
-[4.174479961395264, 6.412813186645508, "[FF] Radiation Pattern of the Antenna = Broad-beam"]
-[8.683738708496094, 0.660112202167511, "[TT] Depth of the Tohoku-Kanto earthquake = 32 km"]
-[5.612194538116455, 2.399939775466919, "[TT] Number of Teams of the PRISMA = 3"]
-[5.561859130859375, 3.6017818450927734, "[TT] Generations of the SkySat = A and B generation, C generation"]
-[8.275461196899414, 8.573296546936035, "[TT] Channel 5 Altitude Range of the FT Spectrometer = 10 to 40 km"]
-[4.758350372314453, 7.3650007247924805, "[TT] Rate of the Data Output to X-band Transmitter = 30.72 Mbit/s"]
-[7.743247032165527, 3.365725517272949, "[FF] Darkening of the Satellite = Surfaces on the satellite that scatter light or reflect light diffusely"]
-[9.426528930664062, 7.113720893859863, "[TT] Spatial Resolution of the OLI-2 = 30 m"]
-[9.67310905456543, 3.952725887298584, "[TT] Magnetic Field Strength of the Oersted = 20000 - 70000 nT"]
-[5.566037654876709, -1.9209527969360352, "[TT] Bus Design, Development and Integration of the KOMPSAT-5 = Led by KARI"]
-[9.135802268981934, 6.967418193817139, "[FF] Data Resolution of the GRACE-FO = High-resolution"]
-[5.51922082901001, 1.9284534454345703, "[FF] Mission Objectives Achievement of the Alexander = More than 100%"]
-[7.4873223304748535, 2.2213754653930664, "[FF] System Name of the Whale Ecology Observation Satellite = Kanta-kun"]
-[10.006877899169922, 2.3701765537261963, "[FF] Ability of the NuSTAR = Measure the energy of smaller microflares"]
-[8.062764167785645, 4.998129844665527, "[FF] Calibration Time of the LD Output = Unknown"]
-[7.392231464385986, 0.3065543472766876, "[FF] URL of the OSIRIS-REx = http://www.spacedaily.com/reports/OSIRIS_REx_cruising_towards_rendezvous_with_Asteroid_Bennu_999.html"]
-[10.976585388183594, 3.782116174697876, "[FF] Size Comparison of the ORS-3/STPSat-3 = 6 times bigger than TechEdSat"]
-[11.831338882446289, 0.04965399205684662, "[FF] Goal of the TESS = Build a catalog of small, rocky planets on short orbits around very bright, nearby stars for atmospheric study by NASA's upcoming James Webb Space Telescope"]
-[8.596375465393066, 4.0425124168396, "[FF] Design of the Electron Sensor = Specialized"]
-[5.968149185180664, 3.7783219814300537, "[FF] Operational Modes of the TechEdSat = Basic operation and computationally demanding payloads"]
-[5.4271368980407715, 0.2349807471036911, "[FF] Mission Preprint of the SAMPEX = 93-128"]
-[11.694400787353516, 5.033855438232422, "[TT] Printed Circuit Board Area of the Sprite = 3.5 by 3.5 cm"]
-[4.402569770812988, 3.012178897857666, "[TT] Location of the MBB = Ottobrunn, Germany"]
-[6.184851169586182, 7.007139682769775, "[TT] Phase Change Sample Rate of the Satellite = 10 Hz"]
-[9.655302047729492, 8.136438369750977, "[TT] Hole Diameter of the Optical Head = 0.2 mm"]
-[8.700154304504395, 4.9912848472595215, "[FF] Bias Correction of the Aeolus = Temperature variations across the instrument's telescope"]
-[8.008747100830078, 8.749107360839844, "[TT] Spectral Coverage of the Red edge = 690-730 nm"]
-[8.173602104187012, 3.4404172897338867, "[FF] Auto Capture of the SADA = Initiation during the sunlit period"]
-[4.6190571784973145, 4.801446437835693, "[FF] Information Provided of the AIS = Ship identity, location, size, speed, heading, cargo, destination"]
-[5.460064888000488, 6.121784210205078, "[TT] Memory of the Controller card = Several MB of RAM and EEPROM"]
-[13.611446380615234, 1.7479166984558105, "[TT] Cargo Weight of the Dragon CRS-14 = More than 2630 kg"]
-[7.5772833824157715, 9.106147766113281, "[TT] Bandpass of the CIPS = UV bandpass of 265 nm (\u00b15 nm)"]
-[5.227494716644287, 2.161116600036621, "[TT] Mission Type of the Flying Laptop = EO"]
-[6.380088806152344, 6.299538612365723, "[FF] Advantages of Optical Communications of the OICETS = Support of much higher data rates and transmission capacities than in conventional radio links, lower risk of link interference with other optical communication systems, as well as in more compact and lighter designs of communication equipment"]
-[7.861176013946533, 7.141712665557861, "[TT] Maximum Frame Rate of the Frame Store Operation = Up to 200 X-ray images per second"]
-[6.634762287139893, -1.9978057146072388, "[FF] URL of the Jason-1 = http://www.aviso.oceanobs.com/en/missions/current-missions/jason-1/index.html"]
-[7.385073184967041, 3.6624181270599365, "[TT] Installation Date of the NightPOD = February 24, 2012"]
-[10.3627290725708, 2.038135290145874, "[FF] Scientific Objectives of the NuSTAR = Probe the obscured AGN activity, study the population of hard X-ray-emitting compact objects, study the non-thermal radiation in young supernova remnants, observe blazars"]
-[6.307398319244385, 5.145164966583252, "[FF] Function of the Interface Chip = Provides a convenient breakout interface"]
-[6.514761924743652, 4.691716194152832, "[FF] Services of the MSS = Power, video and data transfer functions, robotic manipulation"]
-[6.363112449645996, -0.6818504929542542, "[TT] LTDN of the FormoSat-2 = 10:00 hours"]
-[6.928626537322998, 7.4990410804748535, "[TT] ADC resolution of the PHA = 11 bits, 12th bit overflow"]
-[13.147492408752441, 7.255463123321533, "[TT] Power Consumption of the SMMR = ~60 W"]
-[13.637563705444336, 5.600078582763672, "[FF] Objective of the LCE = To measure the IV curves and to determine the pointing sensitivity of a new linear concentrator solar cell assembly"]
-[10.630311012268066, 7.224600791931152, "[TT] Trace V of the APIS Device = 131.4 km"]
-[9.381583213806152, 4.8804144859313965, "[TT] Function of the OASYS = Calculate attitude state vector"]
-[7.278903007507324, 5.207295894622803, "[FF] Components of the OMA = Metrology detection, laser source, actuator drive, servo control, housekeeping, telemetry and command/data handling"]
-[8.05920124053955, -0.6154255270957947, "[TT] Ice Loss of the ICESat-2 = 118 gigatons per year"]
-[12.69817066192627, 1.921415090560913, "[FF] Purpose of the SAGE-III on ISS = Monitor the health of the ozone layer and track the recovery of stratospheric O3"]
-[9.749874114990234, 2.6490118503570557, "[TT] Launch Date of the AlSat Nano = September 2016"]
-[9.768314361572266, 4.296998977661133, "[TT] Energy Dissipation System of the UniSat-3 = Three magnetic hysteresis rods"]
-[5.741350173950195, -0.9129295945167542, "[TT] Design Life of the SA-200HP = 5 years"]
-[9.374141693115234, 8.020587921142578, "[FF] Position of the Side-Looking Camera = Right Side"]
-[8.12229061126709, 3.2426412105560303, "[FF] Detection Capability of the OMI = Emissions Changes"]
-[5.019346714019775, 3.534296751022339, "[TT] Manufacturer of the LISS-I Camera = ISRO"]
-[6.306275367736816, 5.464600563049316, "[FF] Standard of the OOK Modulated Optical Satellite Communications System = CCSDS"]
-[7.0914154052734375, 2.4265670776367188, "[FF] Sensor Complement of the Solar-B / Hinode = Unknown"]
-[6.6444501876831055, -1.9258776903152466, "[FF] Project Management of the Jason-2 = NASA and CNES"]
-[10.535325050354004, 2.1952431201934814, "[TT] Average Turnaround Time of the X-ray telescopes = Typically within 6 hours"]
-[7.972479343414307, 2.8948562145233154, "[TT] Purpose of the SCRI = Space Weather Monitoring"]
-[7.061121463775635, 1.3191659450531006, "[FF] Mission Type of the MSR = Multiple missions to the Red Planet to collect samples, launch them into space and return them safely to Earth"]
-[5.657853126525879, 0.7488280534744263, "[TT] Initial Checkout Date of the IMG = Between September 20 and October 10, 1996"]
-[6.57066535949707, 5.880511283874512, "[FF] Anticipated Users of the LCRD = NASA, future users of optical communications, commercial operators"]
-[11.488055229187012, 5.664331912994385, "[TT] E of the Inconel 718 = 195-200 GPa"]
-[5.31268310546875, 7.6897735595703125, "[TT] Inter Port Isolation of the TWTA = > 25 dB"]
-[8.484874725341797, 1.9023842811584473, "[TT] Pitch of the RapidScat = Roughly 0\u00ba to -10\u00ba"]
-[11.529274940490723, 4.496960639953613, "[TT] Shape of the Payload Deck = Rectangular"]
-[8.925948143005371, 1.0752878189086914, "[FF] Solar Wind Source Prediction of the Parker Solar Probe = Daily"]
-[7.903729438781738, 8.175907135009766, "[TT] TDI Levels of the Pan band = 5 selectable levels from 7 to 20"]
-[4.185302734375, 7.181448936462402, "[TT] TT&C of the Chang'e-1 = S-band"]
-[5.283902168273926, 5.636748313903809, "[TT] Interface Protocol of the DHU = 1553 link"]
-[5.71795654296875, 6.0244269371032715, "[TT] Data Speed of the Corvus-HD satellites = Up to 1Gbps"]
-[13.889718055725098, 3.0208840370178223, "[TT] Mass of the Airbus Arrow 450 = 300 kg to 500 kg"]
-[6.184839725494385, 0.8619773387908936, "[TT] Image Date of the CaSSIS = February 4, 2021"]
-[8.673908233642578, 8.776483535766602, "[TT] Integration Time of the Grating Spectrometer = 100 \u00b5s to 8 s"]
-[8.021084785461426, 3.774404764175415, "[FF] Mission of the EQUULEUS = Understand the radiation environment in the region of space around Earth"]
-[6.658961772918701, 6.100471019744873, "[TT] Number of TRMs of the HPA = 80"]
-[11.57443904876709, 4.834566116333008, "[TT] Diameter of the Hoinga = About 4.4 degrees"]
-[7.022724151611328, 5.764926433563232, "[TT] General Program Percentage of the SVOM = 90%"]
-[5.5535502433776855, 5.669077396392822, "[TT] Processor of the C&DH = 2 x C8051F120 microcontroller"]
-[8.099294662475586, 3.178490161895752, "[FF] Type of the IME-HF, MEXIC, IMM, IDEE, MCP, XGRE, IME-BF = Lightning Detection"]
-[7.459744930267334, 3.470803737640381, "[FF] Purpose of the IDEA OSG 1 = Tracking and mapping of space debris"]
-[6.896617889404297, 9.497103691101074, "[TT] NEDT at 300 K of the Band 10 = 0.2 K"]
-[5.241042137145996, 5.356530666351318, "[TT] Description of the Tracking Mode = Beacon is used to estimate the pointing error, which is then used to continuously steer the antenna back to the satellite"]
-[10.942158699035645, 7.565169334411621, "[TT] Swath Width of the TopSAR wide = 220 - 350 km"]
-[14.683938026428223, 6.708611965179443, "[TT] Quantity of the Battery = 3 parallel of 3 series"]
-[8.301932334899902, 3.784322738647461, "[TT] Objective of the Essaim-1, -2, -3, and -4 = Analysis of the electromagnetic environment (military use)"]
-[6.759621620178223, 5.199328899383545, "[FF] Components of the CDMS = SCP (Spacecraft Process Controller), SCC (Serial Communication Card), DAC (Data Acquisition Card), HSF (High Speed Formatter)"]
-[5.835978031158447, 0.7159277200698853, "[TT] First Image Taken Date of the RSI = 4 June 2004"]
-[6.115977764129639, 4.644679546356201, "[FF] Communication Ability of the Propulsion System = With the satellite to get instructions and to send telemetry data"]
-[3.9078826904296875, 3.403806209564209, "[TT] Contract Award Date of the Galileo = January 7, 2010"]
-[10.157797813415527, 1.3613648414611816, "[TT] Binary Star Catalogue of the Gaia = More than 800 thousand binary systems"]
-[14.455323219299316, 6.55457067489624, "[TT] Battery Discharge of the Integral = The first estimates of the charge remaining before blackout and the loss of the satellite was just three hours"]
-[10.126338005065918, -1.6174570322036743, "[TT] Inclination of the DMSP = 98.9\u00ba"]
-[3.657015562057495, 5.302894115447998, "[TT] SNR of the MMW Radar = 6.9 dB"]
-[9.831488609313965, 7.052596092224121, "[TT] Measurement Scales of the CAPI instrument = Regional (500 km x 500 km) and monthly"]
-[8.570825576782227, 6.424474716186523, "[TT] Shutter Operation Frequency of the ELENA = Above 20 kHz and up to 50 kHz"]
-[7.460535526275635, 2.249664306640625, "[FF] Ability of the Normalized Difference Vegetation Index (NDVI) = Can detect subtle seasonal cycles"]
-[6.351256370544434, 4.885716438293457, "[FF] Mission Objectives of the GATE = Signal experiments, receiver testing, user applications"]
-[7.21118688583374, 8.642354965209961, "[TT] Reflected Radiation Channel FOV of the ISP-2 = 60\u00ba"]
-[13.666319847106934, 3.3423619270324707, "[TT] Magnitude of the Gaia = G=20"]
-[3.2334647178649902, 3.8271870613098145, "[FF] Presentation Date of the TerraSAR-X, TanDEM-X, EnMAP = June 18-19, 2009"]
-[3.447404146194458, -0.8781701326370239, "[TT] Orbit of the ROSE-L = Sun-synchronous orbit of 693 km"]
-[7.658087730407715, 1.0411778688430786, "[FF] Parameter of the LunIR = Perform a lunar flyby of the moon"]
-[7.99747371673584, -0.9945164322853088, "[FF] Data Collection of the ICESat-2 = Freshwater from the surface of the ice shelf into the ocean below within three days"]
-[10.939806938171387, 2.070735216140747, "[TT] Observation Date of the XMM-Newton = 2013 and 2014"]
-[8.979937553405762, 3.3016021251678467, "[FF] Associated Density Perturbation of the Plasma Drifts = Indicated by the circled arrow"]
-[3.3881781101226807, 5.114558696746826, "[FF] Observation Capabilities of the L-band SAR = Longer wavelength and enhanced penetration"]
-[8.048372268676758, 9.228174209594727, "[TT] Wavelength for Ozone Measurement of the LORE = Near 600 nm"]
-[5.772541046142578, 1.0679118633270264, "[FF] Launch Date of the EarthCARE = Unknown"]
-[8.585399627685547, 6.268972396850586, "[TT] Estimated Uncertainties of the TIM = Around 160 ppm"]
-[7.845270156860352, 2.1710927486419678, "[TT] Measurement Category of the EXPORTS = Ocean colour/biology, Multi-purpose imagery (ocean)"]
-[14.232016563415527, 3.136665105819702, "[TT] Mass of the TAIKI = 2.7 kg"]
-[13.357015609741211, 7.660641670227051, "[TT] Power of the Radar = 110 W"]
-[8.663867950439453, 4.743855953216553, "[TT] Quantity of the ST-16 star tracker = 1"]
-[5.1732635498046875, 4.4354143142700195, "[TT] Number of Prisms of the LAGEOS = 426"]
-[5.352720260620117, 7.602066516876221, "[FF] Data Frequency of the FGS = 1 Hz"]
-[9.481000900268555, 6.0542097091674805, "[TT] Incidence Angle of the ALOS-2 = 8-70\u00ba"]
-[9.365124702453613, -0.7121050357818604, "[TT] Orbit of the Trisat-R = 530 km low-Earth orbit"]
-[9.374435424804688, 6.250031471252441, "[TT] Forward Used Angle of the Scan Assembly = 110\u00ba"]
-[4.276419162750244, 0.8697863817214966, "[FF] Meeting Date of the HY-1B = Feb. 12-14, 2008"]
-[3.7298641204833984, 4.555148601531982, "[FF] Imaging Geometry of the RADARSAT-2 = Varies"]
-[5.829607009887695, -2.219785690307617, "[TT] Orbit Inclination of the KOMPSAT-3 = 98.13\u00ba"]
-[8.3438720703125, 2.0455024242401123, "[TT] Required Accuracy of the SSH (Sea Surface Height) = 13.4 cm"]
-[4.387283802032471, 2.874065637588501, "[TT] Location of the NewMag = New South Wales, Australia"]
-[8.173567771911621, 3.322922468185425, "[TT] Measurement Domain of the OCO-3 = Atmosphere"]
-[5.177824974060059, 2.283020496368408, "[TT] Mission Type of the HJ-1 = EO"]
-[3.6032915115356445, 5.240101337432861, "[TT] Time Resolution of the MMW Radar = <1 s"]
-[9.269953727722168, 5.025054454803467, "[TT] Attitude Measurement Accuracy of the Spacecraft = 1-2\u00ba"]
-[14.508110046386719, 6.54777717590332, "[FF] Payloads of the MySat-1 = Camera module, small lithium-ion coin cell battery"]
-[3.848881244659424, 4.502694606781006, "[TT] Slew Count of the RADARSAT-2 = 570"]
-[8.70263671875, -0.2329774647951126, "[TT] Inclina. (\u00ba) of the Meteor-3-1 = 82.5"]
-[6.411795616149902, 3.732440233230591, "[TT] Designation of the GOES-S = GOES-17"]
-[5.605041980743408, 1.444516897201538, "[FF] Ops Renewal Contract of the SeaHawk-1 = Received"]
-[6.0976643562316895, 7.048277854919434, "[TT] Data Rate of the ScaRaB = 3 kbit/s"]
-[4.2583818435668945, 4.356739044189453, "[TT] Individuals Rescued of the Cospas-Sarsat System = 2156"]
-[9.078084945678711, 2.653533458709717, "[TT] Coronal Mass Ejections Observed of the SOHO = More than 20,000"]
-[7.7998199462890625, 1.4852534532546997, "[FF] Bloom Intensity Change of the Phytoplankton = Rose considerably in 48 out of the 71 lakes (68 percent)"]
-[6.213354110717773, 4.6420745849609375, "[FF] Functions of the OpenMCT = Plot and analyze spacecraft health and safety telemetry as a function of time, view GDS logs, view raw file and telemetry downlink, and create command products to downlink telemetry"]
-[4.6483259201049805, 0.8661099076271057, "[TT] Launch Date of the FY-4B = June 02, 2021"]
-[5.864145278930664, -0.8211740851402283, "[TT] Design Life of the Spacecraft = 7 years"]
-[7.5228986740112305, 2.5431296825408936, "[FF] Development Time of the NASA Radar Altimeter = 25 Years"]
-[4.663553714752197, 6.748555660247803, "[TT] Transponders of the S/C Communication Subsystem = 2"]
-[3.833190679550171, 6.328824520111084, "[TT] Antenna Selection of the ISL = Autonomous and seamless"]
-[6.810591220855713, -0.598773717880249, "[TT] Orbit Period of the ResourceSat-1 = 101.35 minutes"]
-[8.996447563171387, 7.44138240814209, "[TT] Panchromatic GSD of the CCD Pushbroom Camera = 5m"]
-[8.89412784576416, 2.884115695953369, "[FF] Purpose of the XFM instrument = Space weather in-orbit demonstration"]
-[10.775041580200195, 2.954038381576538, "[FF] Development of the PACE nanosatellite = Carried out by students of the PACELAB research laboratory at NCKU"]
-[10.378110885620117, 7.9409613609313965, "[TT] Acquisition Telescope Size of the OCTL = 20 cm"]
-[8.041929244995117, 7.501406192779541, "[TT] FPA of the COR1 = 1024 x 1024 (2k x 2k array summed 2 x 2)"]
-[6.874630928039551, -1.7920585870742798, "[TT] Topography Measurement Data of the Jason-1 = High-resolution"]
-[9.338955879211426, 7.006417274475098, "[TT] Resolution of the MERSI-RM = 500 m"]
-[7.7703022956848145, 1.123574137687683, "[TT] Atmospheric Water Equivalent of the Mars = Global layer 10 \u00b5m thick"]
-[11.798104286193848, -0.030602209270000458, "[TT] Earth-sun L-5 Lagrange point Distance of the TESS-L5 = One astronomical unit, or about 150 million kilometers"]
-[11.111576080322266, 5.943247318267822, "[TT] Equivalent Shieldings of the LDT = Different for each floor"]
-[4.903863906860352, 3.0821988582611084, "[FF] Prime Contractor of the ILAS-II = MEI (Matsushita Electric Industrial Co. Ltd.)"]
-[5.269283771514893, 4.523006916046143, "[TT] Controller Type of the Knudsen Station = Green Heron RT-21 Az-El controller"]
-[5.005507469177246, 5.372917652130127, "[TT] Amplifier of the Phoenix GPS Receivers = Independent low noise amplifier (LNA)"]
-[5.157799243927002, 6.1931233406066895, "[TT] Data Input Interface of the Modem Processor = SpaceWire over LVDS (Low Voltage Differential Signaling) link with minimal NRE (Non-Recurring Engineering)"]
-[9.16272258758545, 7.207161903381348, "[TT] Spatial Resolution of the Imaging Plan = As high as 10 m"]
-[5.522284507751465, 0.45969125628471375, "[TT] Deployment Date of the Flock 1a = February 2014"]
-[6.263888835906982, 4.9522294998168945, "[TT] Framework of the FSW = F Prime"]
-[11.640251159667969, 3.400866985321045, "[TT] Thrust of the Electric Propulsion Test Subsystem = 40 mN\u00b14mN"]
-[9.889864921569824, 4.292595863342285, "[FF] Configuration of the AMS-02 = Superconducting Magnet (SCM)"]
-[7.41480016708374, 3.6807267665863037, "[TT] Design of the NightPod = Crew-attended and operated device"]
-[8.43120002746582, 0.14252343773841858, "[FF] Comet of the Rosetta = 67P/Churyumov-Gerasimenko"]
-[6.713001728057861, -0.3327416479587555, "[TT] Time of the South Stepping = 200 ms"]
-[13.466588973999023, 2.8010058403015137, "[TT] In-Orbit Dry Mass of the Spacecraft = ~2750 kg"]
-[10.781115531921387, 5.924965858459473, "[TT] Radiation Mitigation of the Observation Instrument = Contiguous High-Z shielding (4\u03c0 sr @detector and electronics)"]
-[11.44041919708252, 3.592463493347168, "[FF] Test Location of the Power Subsystem = Thruster manufacturer's vacuum chamber"]
-[8.26148796081543, 9.191669464111328, "[TT] Observation Wavelengths of the CAI-2 = 0.67 \u00b5m, 0.87 \u00b5m, 1.60 \u00b5m"]
-[7.32496452331543, 8.611408233642578, "[TT] Design Change of the ABI = Eliminates the filters that are susceptible to debris"]
-[6.747437477111816, 6.019582748413086, "[TT] Number of TWTA of the TWTA = 8"]
-[10.140449523925781, 3.055328845977783, "[TT] Deployment Mission of the CubeSats = 14th"]
-[7.873114585876465, 8.016640663146973, "[TT] Signal-to-Noise Ratio of the NISP Photometer = At least 5"]
-[10.856376647949219, 6.105349063873291, "[FF] Housing Material of the eROSITA camera = Titanium"]
-[12.038128852844238, 4.929806232452393, "[TT] Electronics Unit Dimensions of the PRARE ground transponder = 560 x 560 x 300 mm"]
-[9.400381088256836, 7.723238468170166, "[TT] Detector Pixel Count of the Telescope = 2 k x 1 k pixels"]
-[6.0994873046875, 0.6023691892623901, "[TT] Launch Date of the GRIFEX = January 31, 2015"]
-[8.137944221496582, 7.757254123687744, "[FF] TDI of the Pushbroom imager = The Pan band offers TDI services for SNR improvement of the signal"]
-[9.869255065917969, 0.7582107186317444, "[TT] Mesh Size of the GOSAT = 1,000 km (terrestrial region), 4,000 km (ocean)"]
-[7.707005500793457, 5.925960063934326, "[TT] Instrument Type of the ROSA = Multiple direction/polarisation radiometers"]
-[8.997428894042969, 8.024494171142578, "[TT] CCD Lines per Package of the Focal Plane Module = 3"]
-[9.961313247680664, -1.4681382179260254, "[TT] Orbit Inclination of the ISS-RapidScat = Lower than polar sun-synchronous satellites"]
-[13.494266510009766, 6.880688190460205, "[TT] Power Requirement of the AMS-02 = 2.4 kW @ 28 V"]
-[8.883225440979004, 2.674828290939331, "[TT] Total Hours of the Aurora = 12405.95"]
-[6.836616516113281, 4.0298638343811035, "[FF] Status and Performance of the CALIOP = Unknown"]
-[6.303643703460693, 8.057758331298828, "[TT] Number of Channels of the AMSU = 15"]
-[4.8297224044799805, 2.953481674194336, "[TT] Prime Contractor of the Sentinel-1 = TAS-I (Thales Alenia Space Italia)"]
-[4.225854873657227, 3.889375925064087, "[FF] Receiver Sensitivity of the Galileo = Millions of times weaker than the ones received on Earth"]
-[7.694945335388184, 9.235237121582031, "[TT] Wavelength Range of the Band 13 = 10.1-10.6 \u00b5m"]
-[16.492998123168945, 3.5784058570861816, "[FF] Launch Date of the OneWeb = 7 February, 2020"]
-[5.805801868438721, 4.1098480224609375, "[TT] Number of Payloads of the FY-3E = 11"]
-[7.977836608886719, 13.686050415039062, "[TT] SSD of the B3 = 10 m"]
-[9.482487678527832, -0.5862042903900146, "[TT] Altitude of the ICEYE-X10 = 500 km"]
-[9.067030906677246, 4.718189716339111, "[FF] Function of the Scanwheels = Provide pitch and roll references viewing the Earth's horizon and pitch and roll fine control"]
-[4.545139312744141, 7.161598205566406, "[TT] Experimental Uplink of the QSat = Ku-band, 10 Mbit/s"]
-[8.035724639892578, 8.712728500366211, "[TT] Measurement Range of the SOLSPC = 200-2400 nm"]
-[7.1142897605896, 6.754905700683594, "[TT] Pointing Stability (shot-to-shot) of the Laser = < 10% of divergence"]
-[10.406238555908203, 2.1019344329833984, "[TT] Purpose of the NuSTAR = Detect highest-energy X-ray light in great detail"]
-[8.34640884399414, 7.093008995056152, "[TT] Number of Cameras of the LROC = 3"]
-[10.90886116027832, 10.101460456848145, "[TT] Installation Date of the Alpha Magnetic Spectrometer (AMS) = 2011"]
-[11.966726303100586, 6.46777868270874, "[TT] Quantity of the Passive hydrogen maser = 1"]
-[9.991539001464844, -1.5206866264343262, "[TT] Orbit Inclination of the EURECA = 28.45\u00ba"]
-[4.812076091766357, 0.39245617389678955, "[TT] Launch Date of the TIMED = December 2010"]
-[8.967549324035645, 4.5165557861328125, "[FF] Pointing Modes of the ALSAT-2B = Heliocentric, Geocentric"]
-[6.553678035736084, 6.661585807800293, "[TT] Data Transmission of the MSI = X-band, laser link through EDRS"]
-[8.099579811096191, 7.376974582672119, "[TT] Number of CCD Elements in Cross-track of the MSU-100 = 8000"]
-[5.357729911804199, 6.819173812866211, "[TT] XDA Data Rate of the PAZ spacecraft = 300 Mbit/s"]
-[6.31056547164917, -0.6902680397033691, "[TT] LTDN of the Polar Scout 6U CubeSat = 10:30 hours"]
-[9.663822174072266, 6.997071266174316, "[TT] Angular Resolution of the ECAL = Around 1\u00ba"]
-[6.4850873947143555, 1.789583444595337, "[FF] URL of the Fengyun 4B = https://space.oscar.wmo.int/satellites/view/fy_4b"]
-[9.034613609313965, 0.5649003386497498, "[TT] Goal of the Artemis Program = Land the first woman and next man on the Moon by 2024"]
-[10.97912883758545, 5.661171913146973, "[TT] Filling Method of the Avcoat = Filled by hand"]
-[10.591936111450195, 3.361011505126953, "[TT] Form Factor of the LINAS = 1U CubeSat"]
-[8.124434471130371, 3.1397011280059814, "[FF] Detection of the LI = Cloud to cloud, cloud to ground, and intra-cloud flashes"]
-[5.05935525894165, 2.1144628524780273, "[FF] Ground Segment of the Himawari-8/9 = Unknown"]
-[10.03842544555664, 0.24690428376197815, "[TT] Separation Distance of the GRACE Satellite = Between 170 to 270 km"]
-[7.844620227813721, 3.046999931335449, "[FF] Function of the Interferometric Monitor for Greenhouse Gases (IMG) = Map greenhouse gas ratios on a global scale"]
-[8.168394088745117, 8.63260269165039, "[TT] Spectral Ranges of the Spectrometer Modules = 190-735 nm (UV-VIS) and 350-1100 nm (VNIR)"]
-[8.020302772521973, 6.454412460327148, "[FF] Instruments of the MTG-I = Flexible Combined Imager (FCI) and Lightning Imager (LI)"]
-[13.506640434265137, 5.809042453765869, "[TT] Solar Power of the EPS = at BOL: 1390 W (max), at EOL: 1100 W"]
-[5.824498176574707, 2.2615749835968018, "[FF] Geopotential Mission of the CHAMP = Unknown"]
-[9.429116249084473, 4.8506760597229, "[FF] Attitude Determination and Control System Performance of the Claire = Exceeded specifications"]
-[3.8781440258026123, 6.37788724899292, "[TT] Antennas of the FFRF = Nominally seven"]
-[10.187138557434082, 8.10819149017334, "[TT] Telescope Aperture of the Pan Camera = 0.7 m"]
-[4.665627956390381, 7.944360733032227, "[TT] Frequency Band of the ELFIN-A = 435-438 MHz"]
-[7.613039016723633, 5.540225982666016, "[FF] Focal Plane Components of the NAOMI = Detectors, filters, front-end electronics"]
-[14.082542419433594, 3.412158250808716, "[TT] Mass of the HSC-III optics subsystem = 1.5 kg"]
-[5.839349269866943, 4.424401760101318, "[FF] Types of the Satlet = Single-function satlets, System satlets"]
-[5.438380718231201, 5.7310967445373535, "[TT] Serial Port Hardware Layer of the NIC = RS-422"]
-[9.527167320251465, 0.6768914461135864, "[TT] Distance from Mars of the TGO = About 41 million km"]
-[7.878184795379639, 2.0880818367004395, "[FF] Image Color Representation of the Shikisai = Coolest waters in blue, warmest temperatures in red"]
-[5.095649242401123, 2.0838985443115234, "[TT] Mission Status of the ZACUBE-2 = Operational (nominal)"]
-[9.229058265686035, 4.646811008453369, "[FF] Outputs of the ADCS = Estimated attitude, orbital position, magnetorquer control signals"]
-[3.1196846961975098, 2.150951862335205, "[FF] Program of the CRISTAL = Copernicus Expansion program"]
-[8.393454551696777, 7.376511573791504, "[FF] Device Type of the CMOS/APS Imagers = CMOS/APS"]
-[3.546091318130493, 4.950353622436523, "[TT] Incidence Angles of the RADARSAT-1/2 = 20\u00ba - 49\u00ba, 20\u00ba - 45\u00ba, 10\u00ba - 23\u00ba, 50\u00ba - 60\u00ba, 37\u00ba - 49\u00ba, 20\u00ba - 49\u00ba, 20\u00ba - 46\u00ba, 20\u00ba - 41\u00ba, 20\u00ba - 41\u00ba, 30\u00ba - 50\u00ba, 30\u00ba - 40\u00ba"]
-[10.87469482421875, -0.30510395765304565, "[FF] Data Acquisition and Processing Concepts Presentation Date of the TanDEM-X = July 4-6, 2006"]
-[7.604135990142822, 1.790360450744629, "[FF] Content of the Dataset = Location and crown diameter of trees in western Africa"]
-[4.797275066375732, 2.27117919921875, "[TT] Revenue Start of the Eutelsat Quantum = Fiscal 2021"]
-[6.9408674240112305, 6.949409484863281, "[TT] Quantity of the Lasers = 2"]
-[8.877578735351562, 4.426767349243164, "[FF] Components of the Attitude Sensing System = Sun sensors, a three-axis magnetometer, and a star-tracker"]
-[8.308945655822754, 3.9511525630950928, "[TT] Calibration Targets of the XGRE = Dark oceans, well known desert areas under moonlight"]
-[5.365391254425049, 0.4724269509315491, "[TT] Launch Date of the NuSTAR = Q1 2012"]
-[6.797876358032227, 2.298445224761963, "[FF] URL of the China High-resolution Earth Observation System (CHEOS) = http://spacenews.com/article/civil-space/39665china-pushing-ahead-on-hi-res-satellite-system"]
-[6.487686634063721, -0.7250678539276123, "[TT] LTDN of the HY-1C = 10:30 \u00b130 min"]
-[9.001070022583008, 4.410591125488281, "[FF] Orientation Stabilization of the Solar Orbiter = After the first command was sent"]
-[7.484082221984863, 6.866513252258301, "[TT] Measurement Cadence of the DSCOVR = 1 sample per minute"]
-[4.858704566955566, 8.557501792907715, "[TT] Center Frequency of the Channel 1 = 1695.6938 MHz"]
-[6.816898345947266, 0.6330292224884033, "[TT] Original Mission End Date of the Kepler Space Telescope = 2013"]
-[9.329533576965332, 3.7621569633483887, "[FF] Function of the OSCAR-QUBE = Perform extremely rapid and precise magnetic field measurements"]
-[13.271869659423828, 5.291738033294678, "[TT] Solar Panel Size of the EPS = 2.4 m2"]
-[10.88916015625, 0.9500265717506409, "[TT] Mass Precision of the Exoplanet GJ 367 b = 14 percent"]
-[11.172706604003906, 5.289519786834717, "[FF] Component of the Time of Flight Scintillator Counters (TOF) = Unknown"]
-[4.504327774047852, 6.130080223083496, "[FF] Components of the GOE = Dual-frequency receiver and a directional antenna"]
-[11.702239990234375, 6.615800857543945, "[TT] Energy Measurement Range of the ECAL = 1 GeV to few TeV"]
-[3.9281227588653564, 0.19415995478630066, "[TT] Launch Date of the SMART-1 = 27 September 2003"]
-[5.932945251464844, 3.5793418884277344, "[TT] Name Change of the OSAM-1 = Restore-L to OSAM-1"]
-[10.896368026733398, 2.0840115547180176, "[FF] Exposures of the XMM-Newton = Long, uninterrupted, detailed"]
-[7.828939437866211, 3.1339774131774902, "[TT] Absorption at 1.67 \u00b5m of the Methane (CH4) = 10 -20 mol cm -2"]
-[6.0762529373168945, 5.679025650024414, "[FF] Data Storage of the CubeComputer = MicroSD card"]
-[5.615691661834717, 5.644925117492676, "[TT] Type of the ERC-32 = Radiation-tolerant processor"]
-[8.564841270446777, 7.027528285980225, "[TT] Photographic Modes of the S-052 = 4"]
-[7.414100646972656, 8.40762710571289, "[TT] Filter of the BRITE = Single Color"]
-[5.871314525604248, -0.5217602252960205, "[TT] Tracking Duration of the TiPS Assembly = One year"]
-[8.324153900146484, 4.491350173950195, "[FF] Calibration Sources of the Gray lamps and blackbodies = Gray lamps and blackbodies"]
-[10.140369415283203, 8.119394302368164, "[TT] Aperture of the Optical telescope = 150 mm"]
-[7.9738335609436035, 7.484498500823975, "[TT] Operation Mode of the Detection subassembly = NIMO (Non Inverted Mode Operation)"]
-[6.819571495056152, 7.0440168380737305, "[TT] Coverage of the Payload = Eight spot beams"]
-[14.280179023742676, 3.2280449867248535, "[TT] Mass (kg) of the ERS-1 = 2384"]
-[8.424206733703613, 7.529379844665527, "[TT] Detector Unit of the DOSTEL = Five silicon sensors"]
-[10.725244522094727, 7.281143665313721, "[TT] Footprint of the TOMS = 50 km x 50 km"]
-[8.192853927612305, 1.1835570335388184, "[TT] Soil Moisture Accuracy of the Lower atmosphere = \u00b1 10%"]
-[6.986430644989014, 3.8134453296661377, "[FF] Purpose of the Tactile and Visual Feedback Device = Provide tactile and visual feedback to astronauts during robotic operations"]
-[5.900846481323242, 1.5446827411651611, "[FF] Predecessor of the ROBUSTA-1B = ROBUSTA satellite, which was launched in February 2012"]
-[7.671896457672119, 7.933660984039307, "[TT] Sensitivity of the LEND = 100 ppm or better"]
-[11.079983711242676, 5.985751152038574, "[TT] Manufacturing Location of the Optical Bench Assembly (OBA) = SENER Aeroespacial facility in Bilbao (Spain)"]
-[8.029754638671875, 7.430556774139404, "[FF] Imaging Capabilities of the NewSat-6 = Multispectral and hyperspectral"]
-[4.927919864654541, 5.144624710083008, "[TT] CCSDS ID of the GSAT-0204 = 264"]
-[8.974797248840332, 4.838409423828125, "[TT] Model of the Honeywell QA-2000 Accelerometer = QA-2000"]
-[16.544038772583008, 3.646138906478882, "[FF] Number of OneWeb Gen 2 satellites of the Terran R = Not Disclosed"]
-[4.338396072387695, 4.110973834991455, "[FF] Modulation Schemes of the Galileo Signal = Result in significant reduction of both tracking and multipath noise"]
-[4.492873191833496, 2.833453416824341, "[FF] Sample Image Locations of the NovaSAR-1 = Cebu city and the nearby Mactan-Cebu International Airport, Masbate Island in the Bicol region of the Philippines"]
-[8.681509017944336, 4.26988410949707, "[TT] Sensor Type of the AeroCube-11A/TOMSat EagleScout = Multispectral"]
-[5.719627857208252, 2.8516435623168945, "[FF] Focus of the Bigelow Aerospace = Space Agencies, Commercial Users"]
-[10.455464363098145, 1.5120600461959839, "[TT] Number of Stars of the Upper Scorpius = 83"]
-[4.508114814758301, -0.9199793934822083, "[TT] Program Inception Date of the Dragon C2/3 spacecraft = June 2010"]
-[4.395196914672852, 3.741948366165161, "[FF] Ground Segment Infrastructure of the Galileo program = Included"]
-[4.926167011260986, -2.146301507949829, "[TT] Spacecraft Weight of the Tianwen-1 = Five-ton"]
-[11.688309669494629, 5.02142858505249, "[TT] Circuit Board Area of the ChipSat = 3.5 cm2"]
-[6.2708282470703125, 4.719683647155762, "[FF] Function of the Proton 400 k single board computer = Responsible for commanding, communicating with the spacecraft master avionics unit, and interfacing with the Ka-band transmitter"]
-[10.619394302368164, 3.3565351963043213, "[TT] Form Factor of the CubeSats = 1.5U"]
-[4.555607795715332, 5.905908107757568, "[TT] Doppler Beacon of the GFO = CW (Continuous Wave) transmitter"]
-[9.364908218383789, 7.141368865966797, "[TT] Resolution of the WFI = 55 m"]
-[4.192712306976318, 0.9633036851882935, "[FF] Launch Date of the H-IIB Launch Vehicle No. 2 = Jan. 22, 2011"]
-[8.058595657348633, 9.230834007263184, "[TT] Wavelength of the Water vapor = 2.738 \u00b5m"]
-[11.53933048248291, 4.23208475112915, "[TT] Size of the BeaverCube = 3U"]
-[9.749046325683594, 7.178881645202637, "[TT] Horizontal Spatial Resolution of the MTVZA-GY = 16 - 198 km"]
-[7.561656475067139, -2.474126100540161, "[FF] Launch Schedule of the GOLD = 24 to 36 months from satellite contract to launch"]
-[6.800426006317139, 0.5524343848228455, "[TT] Mission Extension Approval Date of the Kepler = April 4, 2012"]
-[10.249293327331543, 5.346162796020508, "[TT] Location of the Heaters and Temperature Sensors = Near the top and the bottom of the outer aluminum enclosure"]
-[8.910564422607422, 0.5002302527427673, "[FF] Hazard of the Site Nightingale = Building-size boulder on the eastern rim"]
-[5.612088203430176, 1.043749213218689, "[FF] Presentation Date of the ExoMars 2016 Mission = Oct.12-16, 2015"]
-[7.419821262359619, 1.1674169301986694, "[FF] Status Update Date of the SeaWiFS = Feb. 5, 2010"]
-[9.84941291809082, 4.464752674102783, "[FF] Backup of the Cold Gas Attitude Control Subsystem (ACS) = For the magnetorquers for control of S/C precession"]
-[6.38303279876709, 2.4538750648498535, "[FF] Assessment Tool of the EFT-1 Orion = Bumper 3 code and the ORDEM 3 orbital debris environment"]
-[9.052705764770508, 7.162229537963867, "[TT] Resolution of the Chang'E-2 stereo camera = 7 m"]
-[8.154869079589844, 7.758448123931885, "[FF] Quantum Efficiency of the MAPMT = High"]
-[6.173868656158447, 4.504546165466309, "[FF] Size of the Flight Unit = About the size of a desktop computer"]
-[9.470867156982422, 4.841464519500732, "[TT] Attitude Control Performance of the ADCS = Capable of periods of 1 degree pointing (1\u03c3)"]
-[5.21315860748291, 3.2664833068847656, "[TT] Manufacturer of the SeaWiFS = Raytheon SBRC"]
-[3.8117761611938477, -1.1316221952438354, "[TT] Orbit Type of the Euclid = Large-amplitude libration halo orbit"]
-[10.290548324584961, 2.3408541679382324, "[TT] Energy Resolution of the SXD and Solar X-ray monitor = \u2264 600 eV at 5.95 keV"]
-[3.814887285232544, 7.945578098297119, "[TT] Modulation Format of the Flight Modem = DPSK (Differential Phase Shift Keying)"]
-[9.791407585144043, 8.607575416564941, "[TT] IFOV of the Argus = 1 mrad"]
-[6.71235990524292, 0.8733739852905273, "[TT] Launch Date of the Solar Orbiter = February 2020"]
-[6.478711128234863, 4.704115390777588, "[FF] Functionalities of the PMS = Catalog data generation, product generation status control and monitoring, standard product generation"]
-[8.322392463684082, 8.018233299255371, "[TT] Kovar Package Length of the SWIR Detector = ~103 mm"]
-[9.738779067993164, 7.183168888092041, "[TT] Ground Resolution of the InSb = 30m"]
-[3.124173164367676, 1.8910152912139893, "[TT] Global Ocean Color Data Recording Time of the Sentinel-3B = Less than 1.9 days at the equator, and in less than 1.4 days at latitudes higher than 30\u00ba"]
-[3.8759641647338867, 1.9983230829238892, "[TT] Stage Type of the Soyuz = Payload shroud"]
-[12.499005317687988, 3.203915596008301, "[TT] Total propellant used of the Station keeping = 28.6 g"]
-[10.351359367370605, 3.1873748302459717, "[TT] Number of CubeSats of the EM-1 = 13"]
-[9.077637672424316, 2.876889705657959, "[FF] Observation Focus of the Solar Dynamics Observatory = Solar flares and sunquakes"]
-[5.774797439575195, 7.236837863922119, "[TT] Data Rate of the HID = 0.64 kbit/s"]
-[13.477856636047363, 3.0378174781799316, "[TT] Mass of the Corvus-XL bus = Approximately 80 kg"]
-[10.950577735900879, 6.256738662719727, "[TT] Coefficient of Thermal Expansion of the SiC = Low"]
-[5.1673359870910645, 4.223978519439697, "[TT] Space Segment Host of the DASS = GPS-III satellites"]
-[9.203227043151855, 7.26584005355835, "[TT] GSD (Panchromatic) of the GF-2 = 0.81 m"]
-[7.492258071899414, 5.892345905303955, "[FF] Potential Applications of the Optical Encoder = High precision, long life space instruments"]
-[9.737948417663574, -0.5719046592712402, "[TT] Orbit Altitude of the STSAT-3 = ~600 km"]
-[5.831015586853027, 2.7842252254486084, "[FF] Role of the Space Development Agency = Accelerate delivery of needed space-based capabilities to the joint warfighter"]
-[4.657901287078857, 6.032872676849365, "[FF] Function of the MCCM = Control the illumination coefficients (attenuation or phase) of the RF signal received from each subarray for the beam synthesis"]
-[6.581989765167236, 1.0644137859344482, "[FF] Data Collection of the Landsat series of satellites = Decades-long record"]
-[9.313430786132812, 3.1703498363494873, "[TT] Photographs of the Coronagraph = More than 35,000"]
-[6.573094367980957, -2.046555995941162, "[TT] Launch Date of the Jason-3 = 2014"]
-[5.262181282043457, 1.5041712522506714, "[TT] Preliminary Data Availability of the SMAP = August 2015"]
-[10.643659591674805, 1.0865119695663452, "[TT] Diameter of the HD 21749c = 89% of Earth\u2019s diameter"]
-[13.418109893798828, 6.623676776885986, "[TT] Maximum Satellite Demand of the Satellite = 850 W"]
-[3.6501028537750244, 4.137558937072754, "[TT] SAR Imagery Collection Start Date of the RISAT-1 = July 1, 2012"]
-[8.058855056762695, 2.821164131164551, "[FF] Function of the GLM = Improve storm hazard identification and increase warning lead-time"]
-[5.922764778137207, -0.6266590356826782, "[TT] Mission Lifetime of the NEMO-HD = One year"]
-[9.723355293273926, 4.913444995880127, "[TT] Peak Rotation Rate of the SMAP spacecraft = Up to 11 degrees per second"]
-[7.720254421234131, 2.270285129547119, "[FF] Additional Data Sources of the TanDEM-X = \u2018global urban footprint\u2019, a global map of settlements created at the DLR Earth Observation Center (EOC), as well as the mapping of water bodies by ESA\u2019s Climate Change Initiative"]
-[7.453797817230225, 5.744427680969238, "[FF] Repeatability of the MWI Instrument = Unknown"]
-[8.23814582824707, 6.025606155395508, "[FF] Degradation of the Piezoelectric Cantilevers = Systematic errors"]
-[5.3294758796691895, 7.498788356781006, "[TT] C/N0 of the Beacon Level = 47.4 dB"]
-[13.411723136901855, 5.539641857147217, "[TT] Solar Arrays Quantity of the EPS = 3"]
-[5.494785785675049, 0.5502586364746094, "[TT] Operation Stop Date of the ERB = Jan. 4, 1994"]
-[6.913746356964111, 4.11445426940918, "[FF] Website of the SCARAB = http://www.lmd.polytechnique.fr/~Scarab/english/Orbs.htm"]
-[13.529650688171387, 5.836284637451172, "[TT] Total Power (EOL) of the Solar Array = 1730 W"]
-[6.414366245269775, 4.732141494750977, "[FF] Continuation of the TIM = Provided by TSIS"]
-[7.558493137359619, -0.4110403060913086, "[FF] Expertise of the ICEYE = Risk finance, climate risk management"]
-[8.440381050109863, 6.546175479888916, "[TT] Spectral Range of the TEMPO instrument = 290\u2013740 nm (UV, VIS)"]
-[5.407374382019043, 4.3068461418151855, "[TT] Number of Satellites of the Corvus = 10 medium-resolution satellites (Corvus-BC) and 20 high-resolution satellites (HD)"]
-[11.418368339538574, 2.164365768432617, "[TT] \u0394V (cm/s) of the Cosmos 2251 Debris = 0.92"]
-[8.87946891784668, 4.557894706726074, "[FF] Attitude and Orbit Measurement System of the TanDEM-X = GPS/Star Tracker system during nominal operation and a CESS (Coarse Earth and Sun Sensor) in safe mode situations and during the initial acquisition"]
-[6.566059589385986, 6.64998722076416, "[TT] Communication Technology of the EDRS-C = Laser"]
-[5.564255714416504, 2.628085136413574, "[TT] Number of Participating Students of the YES2 = About 400"]
-[8.966967582702637, -0.626762866973877, "[FF] Orbit of the MEOSAR = Mid-Earth"]
-[5.528199672698975, 5.334466457366943, "[TT] Usage of the TRON = About 60% of the RTOS implementations in the embedded equipment market"]
-[7.2298359870910645, 1.220116138458252, "[TT] Propulsion Systems Provider of the Mars Ascent Vehicle (MAV) = Northrop Grumman"]
-[3.851405382156372, 7.883756637573242, "[TT] Modulation of the RF Communications = Bell 202"]
-[7.807796478271484, 9.076310157775879, "[TT] Input Angle alpha of the Short Wavelength Band = 21.9\u00ba"]
-[12.41771125793457, 3.2025327682495117, "[TT] Propellant Quantity of the Propulsion Subsystem = 10 kg"]
-[7.245135307312012, 0.9423668384552002, "[TT] Launch Date of the SeaSat-1 = 1978"]
-[8.258489608764648, 8.092452049255371, "[TT] Type of Array of the VNIR = Si"]
-[7.565258502960205, 1.001603126525879, "[FF] Water Decomposition Time Scale of the Mars = Centuries"]
-[5.327983379364014, -0.2437208890914917, "[TT] First Launch Date of the Block 5D-1 = September 11, 1976"]
-[11.845446586608887, 6.707819938659668, "[TT] Energy Range of the IDEE = < 1 MeV to >10 MeV"]
-[9.109360694885254, -1.2298436164855957, "[TT] Orbit Location of the EDRS-C = 31\u00baE"]
-[7.413931846618652, 2.6484458446502686, "[FF] Imaging Capabilities of the Severyanin-M OBRC = Land and sea surface monitoring"]
-[4.852733135223389, 6.783294200897217, "[TT] Purpose of the XSTP = Data transport errors correction in LEO satellite links"]
-[13.898502349853516, 7.092653751373291, "[TT] Current of the Voltage 3 = 350"]
-[7.436872959136963, 4.232438087463379, "[FF] Update Contact of the Sensor Complement = eoportal@symbios.space"]
-[10.346685409545898, 5.800917625427246, "[TT] Gain temperature coefficient of the PHA = <50 ppm/\u00baC"]
-[8.019625663757324, 5.362233638763428, "[TT] Measurement of the FLLS = Three axes of movement"]
-[11.427275657653809, 4.361318588256836, "[TT] Size of the Dellingr = 6U"]
-[8.342206001281738, 7.536247253417969, "[TT] Bands of the Optical Sensor Assembly (OSA) = Four multispectral bands and one panchromatic band"]
-[4.763675212860107, 5.574644565582275, "[FF] Doppler Correction Errors of the Prometheus Block 1 = Cause of Communications Failure"]
-[2.285719871520996, 1.26858389377594, "[FF] Deployment Event of the NanoSail-D2 = Missed"]
-[8.382608413696289, 1.945145606994629, "[FF] Instrument of the ISS-RapidScat = QuikSCAT scatterometer"]
-[5.3551130294799805, 5.471924304962158, "[FF] Availability of the Strandatoga protocol = Available"]
-[13.280701637268066, 5.457294464111328, "[TT] Type of the Solar Arrays = Deployable sun-tracking"]
-[5.477079391479492, 2.8732755184173584, "[TT] Funding of the NIRSpec = ESA"]
-[13.998760223388672, 3.9656405448913574, "[TT] Mass of the OBRC instrument = Not more than 150 kg"]
-[3.4107658863067627, 1.6755094528198242, "[FF] Approval Date of the Sentinel Asia = October 2005"]
-[3.553877592086792, -0.8459876775741577, "[TT] Orbit of the TRUTHS = Asynchronous"]
-[8.861729621887207, 3.7366535663604736, "[FF] Measurement of the Electric Field Instrument = Temperature 300 km above Earth\u2019s surface jumped by 3000\u00baC"]
-[5.078812122344971, 1.1741015911102295, "[FF] Workshop Date of the PROBA-3 = March 13-15, 2013"]
-[12.020045280456543, -0.37028172612190247, "[TT] Mission Lead of the TESS = MIT in Cambridge, Massachusetts"]
-[11.561514854431152, 4.852359294891357, "[TT] Diameter of the TMR = 79 cm"]
-[10.751192092895508, 4.476621150970459, "[TT] Rover Name of the ExoMars = Rosalind Franklin"]
-[10.824156761169434, -0.2997337877750397, "[TT] Image Date of the TWINS = June 15, 2008"]
-[11.628417015075684, 4.688936710357666, "[TT] Structure Diameter of the Clementine = 1.14 m"]
-[7.473718643188477, 3.6612284183502197, "[TT] Mission Objective of the NightPod = Assist the crew in taking high-resolution (long exposure) picture tracking of Earth targets at night from the Cupola"]
-[10.150618553161621, -2.764831781387329, "[TT] Maximum Read Performance of the SLC NAND-Flash = < 250 Mbit/s @ 40 MHz on page level (4 k x 8)"]
-[3.8684871196746826, 4.355111598968506, "[FF] Future Plans of the Synthetic Aperture Radar = Analyse Alaska, Canada and Greenland as well as eventually Russia"]
-[8.42261028289795, 6.445004940032959, "[TT] Instrument Type of the AVHRR/3 = Whiskbroom-type"]
-[7.332577228546143, 3.548882484436035, "[FF] Purpose of the Enhancing Space Situational Awareness using a 3U CubeSat with Optical Imager = Enhancing Space Situational Awareness"]
-[11.958069801330566, 0.5540566444396973, "[FF] Exoplanet Detection of the PLATO = Terrestrial exoplanets in the habitable zone of solar-type host stars"]
-[5.28410005569458, 8.440469741821289, "[TT] Bandwidth of the A/D converter = 500 MHz"]
-[4.648460865020752, 7.15416955947876, "[TT] Uplink of the Communications = S-band at 1 kbit/s"]
-[7.604045867919922, 3.988218069076538, "[FF] Instruments of the FedSat = Communications payload (Ka and UHF band), GPS receiver, Fluxgate magnetometer"]
-[5.885682106018066, 5.1917405128479, "[FF] Data Flow Architecture of the LPT = Standard IP protocols and HDLC data framing"]
-[2.8809876441955566, 1.9501932859420776, "[FF] Image Capture Date of the Copernicus Sentinel-2 = 19 January 2022"]
-[8.02549934387207, 4.055987358093262, "[FF] EECC of the Exposure of Spacecraft Coatings = Experiment Exposure Control Canister"]
-[9.366867065429688, 8.260723114013672, "[TT] FOV of the LLNL imaging system = 2.08\u00ba x 1.67\u00ba"]
-[10.101261138916016, -1.6062747240066528, "[TT] Inclination of the RESURS-O1-4 = 98\u00ba"]
-[5.000343322753906, -0.3069196343421936, "[TT] Launch Time of the Cesium Satellite 1 = 18:12 UTC"]
-[8.06690788269043, 8.722125053405762, "[TT] Error of Amplitude Spectrum of the BRITE = 2 x 10-5 (20 ppm)"]
-[9.447357177734375, 4.829784870147705, "[TT] Attitude Control Mode of the Hayabusa-2 = One wheel control mode"]
-[8.456860542297363, 1.9597193002700806, "[FF] Primary Usage of the QuikSCAT = Measure winds inside distant hurricanes"]
-[4.807131290435791, -0.011328939348459244, "[TT] End of Life Date of the LARES-2 = March 2062"]
-[6.016839981079102, 1.4515981674194336, "[FF] On-Orbit Operations of the SENSE Satellites = August 8-13, 2015"]
-[6.6521806716918945, 3.092154026031494, "[FF] Goal of the SERVIR = Supplement local facilities, technology, and skills with expanded satellite imagery and tools"]
-[4.892731666564941, 0.559165894985199, "[FF] Launch Date of the POPSAT-HIP1 = June 3, 2014"]
-[9.692906379699707, 0.9914490580558777, "[TT] Heliocentric Range of the S/C = 1.34 to 5.4 AU"]
-[5.681619644165039, 3.8886682987213135, "[TT] Equipped with of the NJUST-1 = INMS"]
-[5.926239013671875, 0.8453586101531982, "[TT] Image Date of the AWiFS = May 4, 2011"]
-[5.592958927154541, 0.583208441734314, "[TT] ERBS S/C Operational on One Battery Date of the ERBE = June 2001"]
-[7.584811687469482, -0.7252243161201477, "[TT] Resumption Date of the Operation IceBridge = Late March 2018"]
-[5.241023540496826, 3.374220609664917, "[TT] AVGS Manufacturer of the ASTRO = NASA/MSFC"]
-[10.410825729370117, 7.166306972503662, "[TT] Primary Mirror Size of the Telescope = 3.5 m"]
-[8.7314453125, 3.797255277633667, "[TT] Instrument Types of the Solar Orbiter = In situ and remote sensing"]
-[5.218532085418701, 3.1587963104248047, "[TT] Operator of the RapidEye = BlackBridge"]
-[4.102303981781006, 0.1854790300130844, "[TT] Launch Date of the Falcon 9 = 21 April 2022"]
-[11.6829195022583, 3.3125360012054443, "[TT] Propulsion Systems Quantity of the MTG Satellites = 6"]
-[9.261557579040527, 3.2120180130004883, "[TT] Exposure Time of the Coronal Hole Boundaries = < 10 seconds"]
-[14.192268371582031, 2.9818263053894043, "[TT] Mass of the Deimos-2 = ~310 kg"]
-[7.115988731384277, 5.914431571960449, "[FF] Purpose of the Texas Instruments MSP-430 = Count clock cycles over the entire lifetime of the mission"]
-[8.944664001464844, 7.405647277832031, "[TT] Optomechanical Stability of the Multispectral Imager = Extremely high"]
-[7.6468377113342285, 0.6938377022743225, "[FF] Measurement Goal of the Lunar Flashlight = Measure the surface abundance of water ice on the lunar South Pole with concentrations of 5 wt% or less, down to as little as 0.5 wt%, with a spatial resolution of 10 km or better"]
-[9.86843490600586, -0.36074522137641907, "[TT] Altitude of the MetOp-B satellite = 827 km"]
-[7.602295398712158, 3.511964797973633, "[FF] Space Debris Capture of the RemoveDEBRIS = Successful"]
-[13.60526180267334, 1.7481293678283691, "[TT] Cargo Capacity of the SpaceX Cargo Dragon = Over 7,300 pounds"]
-[10.635285377502441, 1.3609871864318848, "[TT] Energy Received from Star of the L 98-59d = 4 times the radiant energy as Earth"]
-[10.733478546142578, 7.437473773956299, "[TT] Swath Width of the Spectral bands = 24 km"]
-[7.071873664855957, -0.2578032314777374, "[TT] Orbits Completed of the MaSat-1 = 10,000"]
-[7.417305946350098, 3.198408365249634, "[TT] Detection Threshold of the GHGSat = ~100 ppb"]
-[11.90383529663086, 4.969394207000732, "[TT] Dimensions of the CVX cell = 62 mm long by 38 mm wide"]
-[6.344754695892334, 4.702010154724121, "[FF] Subsystems of the Ground Station = Monitor and Control, Atmospheric Monitoring Instruments, Laser Safety Systems"]
-[4.396059036254883, 3.7665748596191406, "[TT] Number of Phase-B Contracts of the Galileo Second Generation = 11"]
-[4.823657035827637, 1.7830873727798462, "[TT] Climb Duration of the Eutelsat 172B = Approximately four months"]
-[3.382885456085205, 6.455855846405029, "[TT] Diameter of the Antenna = 61 cm"]
-[4.435462474822998, 1.586593747138977, "[TT] Launch Date of the First SARSAT Equipment Launch Date = March 1983"]
-[8.374821662902832, 3.5753402709960938, "[FF] Measurement of the AOE-2 = Flux of atomic oxygen (AO)"]
-[5.8988823890686035, 4.3275346755981445, "[FF] Purpose 2 of the PW-Sat = Demonstration of a satellite deorbit structure"]
-[10.187704086303711, 3.272623062133789, "[FF] Fundraising of the Iraz\u00fa CubeSat = Aluminum plate is placed on one of the sides of the CubeSat and another one inside of the spacecraft for fund-raising purposes"]
-[6.308446407318115, 2.5466606616973877, "[FF] Purpose of the Orion = Protect the crew for re-entry velocities that are higher than any human spacecraft in history"]
-[4.808749675750732, 1.321799874305725, "[FF] Technology Demonstrator Mission of the Delfi-C3 = April 6-8, 2005"]
-[3.2144505977630615, 5.041403770446777, "[TT] HRS Spotlight Target of the RISAT-SAR = 10 km (azimuth) x 10 km (ground range)"]
-[7.6133832931518555, 3.441577196121216, "[FF] Conference Presentation Date of the DebriSat Fragments = 25-29 Sept. 2017"]
-[9.415800094604492, 6.633155345916748, "[TT] Scanning Mode of the SASS = Fan-beam (2 sides)"]
-[9.140754699707031, 4.746840000152588, "[FF] Attitude Control Software of the CRISTA mission satellite = Available"]
-[5.194038391113281, 2.3131279945373535, "[FF] Technology and Resource Legacy of the ZACUBE-1 = Leveraged for ZACUBE-2"]
-[9.018237113952637, 0.9400897026062012, "[TT] Successful Swings around the Sun of the Parker Solar Probe = 7"]
-[8.78416919708252, 5.614907741546631, "[TT] Antenna Control Pointing Accuracy of the NRA = 0.14\u00ba (1 \u03c3)"]
-[5.415711879730225, 5.333090305328369, "[FF] Enhancement of the STRV-1c and -1d Spacecraft = Introduction of full dual-redundancy"]
-[10.254375457763672, 5.315192699432373, "[FF] HTS Condenser Plate Interface of the LCT = Connected to dedicated radiators through heat pipe networks"]
-[7.334509372711182, 3.2307467460632324, "[FF] Data of the Tropomi = Used to combine with GHGSat's unique fleet of high-resolution satellites"]
-[14.14366626739502, 3.2752466201782227, "[TT] Mass Measurement Unit of the GRACE = Gigatons (Gt)"]
-[10.237743377685547, 5.3233184814453125, "[FF] Function of the TET Radiator = Allows the complete radiation of all thermal energy into free space during the \"hot\" phases"]
-[11.265860557556152, 5.871973037719727, "[TT] Material of the 3D-printed metal antenna = Metal"]
-[8.330690383911133, 2.783478021621704, "[TT] Measurement Domain of the ST5 = Atmosphere, Gravity and Magnetic Fields"]
-[7.566562652587891, 8.516396522521973, "[TT] Band Number of the Himawari-8 = 16 bands"]
-[7.674648284912109, 9.445181846618652, "[TT] Center Wavelength of the Band 9 = 9.71 \u00b5m (1030 cm -1)"]
-[5.177806854248047, 4.4175705909729, "[TT] CGA Implementation of the MC3 = Allowed for the ground stations to be unmanned 24/7"]
-[5.311026573181152, 0.25331541895866394, "[TT] Arrival Date of the ISS = Monday (Nov. 19)"]
-[6.072103977203369, 4.175171852111816, "[FF] Ground Segment Components of the JUICE Mission = Mission Operation Center (MOC) and the Science Operation Center (SOC)"]
-[10.149044036865234, 5.9624152183532715, "[TT] Temperature Range of the Miniature High-Resolution Imaging Spectrometer = -40\u00b0C to +80\u00b0C"]
-[11.351573944091797, 5.8592376708984375, "[TT] Material of the Mandrels = Aluminum"]
-[10.244855880737305, 4.6089348793029785, "[TT] Maximum Momentum of the Reaction Wheel (RW) = 40 Nms"]
-[5.043899059295654, 5.229286193847656, "[TT] Modulation of the GPS L1C signal = MBOC waveform"]
-[2.917926073074341, 4.377798557281494, "[FF] Calibration and Validation Team of the PALSAR = M. Shimada, H. Wakabayashi, T. Tadono, A. Rosenqvist, T. Igarashi"]
-[6.027155876159668, 2.6525559425354004, "[FF] Project Partners of the SPORT = NASA, the Brazilian National Institute for Space Research (INPE), and the Technical Aeronautics Institute under the Brazilian Air Force Command Department (DCTA/ITA)"]
-[8.29673957824707, 5.072739124298096, "[TT] Calibration Duration of the ADCS = About one month"]
-[4.197225093841553, 2.9609291553497314, "[TT] Test Location of the GRACE-FO Satellites = IABG in Ottobrunn near Munich"]
-[8.13941764831543, 4.547613143920898, "[FF] Radiation Exposure of the O/OREOS = Unknown"]
-[8.247803688049316, 6.3524651527404785, "[TT] Translation Intervals of the CCRR = 0.5 m"]
-[6.43966817855835, 8.62307071685791, "[FF] Polarization Modes of the Coronagraph = Unpolarized light or one of three possible orientations of plane polarized light"]
-[10.37269115447998, 5.475448131561279, "[TT] Surface Temperature of the Sun = 6,000 degrees Celsius"]
-[6.515254497528076, 2.20855712890625, "[FF] Science Team of the Nancy Grace Roman Space Telescope = Scientists from various research institutions"]
-[4.80168342590332, 0.3880179822444916, "[TT] Initial Scheduled Launch Date of the OFT-2 = July 30"]
-[11.741138458251953, 3.3094871044158936, "[FF] Endurance of the TSUBAME = Able to endure the Dnepr rocket vibrations"]
-[7.035371780395508, 4.331360816955566, "[FF] Unknown of the VMAG = Unknown"]
-[4.598910331726074, 7.027293682098389, "[TT] Data Downlink of the Payload = X-band"]
-[11.116833686828613, 1.5235316753387451, "[TT] Mass of the STARSHINE-3 = 91 kg"]
-[8.058300971984863, 6.379349231719971, "[FF] Imaging Capability of the Terra Bella = Sub-meter color imagery and up to 90-second clips of HD video with 30 frames/s"]
-[5.369776725769043, 0.4381203055381775, "[TT] In Orbit Commissioning (IOC) End Date of the CHEOPS = March 26, 2020"]
-[10.567748069763184, 1.8496628999710083, "[FF] Measurement of the XMM-Newton = Black hole's spin rate"]
-[2.7841320037841797, 0.09466920047998428, "[TT] J2000 declination (deg) of the B0531+21 (Crab) = 22.01449"]
-[3.8932156562805176, 1.981145977973938, "[TT] Launch Vehicle of the KazSTSAT = SpaceX Falcon-9 Block 5"]
-[9.984023094177246, 2.9332470893859863, "[FF] Launch Date of the CubeSat = July 21, 2010"]
-[8.600968360900879, 3.673992395401001, "[TT] Measurement Category of the TSIS-1/SIM = Downwelling (Incoming) solar radiation at TOA"]
-[10.137171745300293, 6.958206653594971, "[TT] Footprint Positioning of the Sounder = Anywhere in the FOR"]
-[10.292607307434082, 5.788156986236572, "[TT] Temperature of the Instrument = 130 K"]
-[3.852170705795288, 4.6126203536987305, "[TT] Radiometric Accuracy of the RADARSAT-2 = Stable and within expectations"]
-[13.442084312438965, 5.468430519104004, "[TT] Number of Arrays of the Solar Panel = 6"]
-[4.238947868347168, 2.1734344959259033, "[TT] Launch Site of the AlSat-2A = Satish Dhawan Space Centre (SDSC) SHAR, Sriharikota, India"]
-[8.007226943969727, 5.932567596435547, "[FF] Components of the SSUSI = SIS (Scanning Imaging Spectrometer), NPS (Nadir-looking Photometer System), Support module"]
-[13.432991027832031, 6.832722187042236, "[TT] Power of the INSAT-3D = ~1.1 kW"]
-[8.557609558105469, 8.073606491088867, "[TT] Spectral Resolution (60 keV) of the Detector = 1.0 keV"]
-[4.9582133293151855, 7.337377548217773, "[TT] TRM Phase/Amp Update Rate of the TCU/TRC = 18 \u00b5s @ PRF rate"]
-[6.409899711608887, -0.6346499919891357, "[TT] Revisit Period of the CBERS-2B = 26 days"]
-[5.11874532699585, 8.358777046203613, "[TT] Bandwidth of the NRA = 320 MHz"]
-[8.39207935333252, 7.630242347717285, "[TT] Pixel Size of the CCD Detector Array = < 12 \u00b5m"]
-[3.851041078567505, 7.903696060180664, "[TT] Modulation of the Ku-band transmitter = BPSK (Binary Phase Shift Keying)"]
-[8.35700511932373, 8.30334758758545, "[TT] Filters of the VNIR FPA = 10"]
-[7.221978664398193, 8.691553115844727, "[TT] Dynamic Range (Normalized Radiance) of the POLDER = 0.05-0.22"]
-[5.201844692230225, 2.335888624191284, "[TT] Constellation of the ESO 253-3 = Pictor"]
-[6.181278705596924, -0.3995508551597595, "[TT] Minimum Duration of the PACE = Three years"]
-[9.4150390625, 7.262851238250732, "[TT] Ground Coverage of the Detector = 79 m"]
-[3.877854108810425, -1.2727755308151245, "[TT] Lagrange Point of the SWFO = Lagrange Point 1"]
-[5.1883769035339355, 2.0043866634368896, "[TT] Mission Status of the ISS:LIS = Operational (extended)"]
-[10.111461639404297, -1.6112723350524902, "[TT] Inclination Difference of the PSLV-C15 = 0.1\u00ba"]
-[9.445145606994629, 6.07742166519165, "[FF] Incidence Angle of the Instrument = 55\u00ba, 54.5\u00ba"]
-[8.455032348632812, 5.540091514587402, "[TT] Positioning Errors Reduction with QZSS of the QZS-1 = More than 30%"]
-[11.604204177856445, 4.7395405769348145, "[TT] Shape of the SVM = Irregular hexagonal base"]
-[9.269617080688477, 1.0079718828201294, "[TT] Impact Speed of the DART = Approximately 3.7 miles per second"]
-[2.886540412902832, 0.0956890806555748, "[FF] Discovery of the MAXI J1820+070 = Newly discovered"]
-[11.752461433410645, 3.2702319622039795, "[TT] Total Impulse of the Mono-propulsion Chemical System = 1000 Newton-seconds"]
-[2.2971835136413574, 2.7699642181396484, "[TT] Co-PI of the EPI-Lo = Nathan Schwadron"]
-[4.419543743133545, 7.9078779220581055, "[TT] Frequency of the Downlink = 880f0"]
-[7.538364410400391, 9.261985778808594, "[TT] Band 3 of the CIRiS = 11.77 \u00b5m to 12.6 \u00b5m"]
-[14.226146697998047, 3.0692033767700195, "[TT] Mass of the Phoka-D = 3 kg"]
-[5.896697998046875, 3.7735977172851562, "[FF] Cost Scaling of the Ground Station Network = Does not scale with the size of the satellites"]
-[7.668397426605225, 9.447322845458984, "[TT] Center Wavelength of the Band 11 = 8.5 \u00b5m"]
-[6.704443454742432, 1.044944167137146, "[TT] Data Availability of the Landsat 7 ETM+ SLC-off and Landsat 5 TM = All data September 2008"]
-[6.295072555541992, 4.630788326263428, "[FF] Function of the MOT = Communicates with spacecraft engineers to assist in SOH (State-of-Health) matters, such as anomaly resolution, and reports of the condition of the spacecraft and receives in return any constraints or tasking that may be required"]
-[13.546524047851562, 5.473624229431152, "[TT] Number of Cells of the Solar Array = 14"]
-[11.158502578735352, 6.319473743438721, "[TT] Temperature of the Proton Component Measurement Accuracy of the DSCOVR = 50%"]
-[8.046341896057129, 8.47456169128418, "[TT] Effective Emissivity of the MLI = \u03b5 < 0.05"]
-[11.899418830871582, -0.06662599742412567, "[TT] Target Stars Brightness of the TESS = 30-100 times brighter than those surveyed by the Kepler satellite"]
-[7.438682556152344, 5.364663124084473, "[FF] Components of the SOLCON-3 = Substitution radiometer (absolute cavity device) and a digital processor unit"]
-[10.010594367980957, 6.6361870765686035, "[FF] Function of the Secondary Mirror = Reflects the beam towards the focal plane"]
-[14.221562385559082, 3.1753973960876465, "[TT] Mass of the exactView-1 = 100 kg"]
-[7.299820423126221, 0.362671434879303, "[TT] Science Team Leader of the OSIRIS-REx = University of Arizona, Tucson"]
-[8.888944625854492, 4.105583190917969, "[TT] Observation Target of the EXIS = Sun"]
-[7.193369388580322, 7.547645568847656, "[FF] NE\u0394T of the Satellite Device = 1.0 K"]
-[8.042793273925781, 1.0474220514297485, "[FF] Description of the Centre-pivot irrigation systems = Equipment rotates around a central pivot and crops are watered with sprinklers"]
-[5.547412872314453, 6.965867042541504, "[TT] Data Download Rate of the First DMC generation = 8 Mbit/s"]
-[13.243741989135742, 7.233950138092041, "[TT] Power Consumption of the Mass Memory System = < 35 W"]
-[5.759129047393799, 3.5328125953674316, "[FF] Return on Investment of the Neosat programme = Predicted to be more than 20 times"]
-[5.420059680938721, 3.471601724624634, "[TT] Design of the Terminator Tape Deorbit Module = Cubesat tether design"]
-[11.183502197265625, 0.5690092444419861, "[TT] Function of the ASTERIA = Study exoplanets via the transit method"]
-[12.413654327392578, 7.016655921936035, "[TT] Power of the LEICA = 4.9 W"]
-[13.85494327545166, 7.114920616149902, "[TT] Output Voltage of the High Voltage Power Supplies = Utilize the primary 22 V from the SWEM"]
-[4.867953300476074, 7.880406379699707, "[TT] Frequency Band of the GETR (Galileo Experimental Test Receiver) = L1 1574.42 MHz"]
-[10.104826927185059, 8.061869621276855, "[TT] Effective Focal Length of the Telescope = 1600 mm"]
-[7.211751937866211, -0.784580409526825, "[FF] Data Improvement of the Spitzer = Sharpened their measurements of its orbital period by 56% and its size by 38%"]
-[7.375336647033691, 2.9485702514648438, "[FF] Agreement of the ABB = Signed with GHGSat to deliver the payloads for GHGSat\u2019s next 3 methane detecting satellites"]
-[8.78935432434082, 3.544907331466675, "[FF] Leading Noise Terms of the Satellite = Self gravitation to the satellite"]
-[6.64134407043457, 6.200532913208008, "[FF] Cumulative Processing Time from Raw Data of the EO System = Unknown"]
-[6.4574995040893555, 5.135140419006348, "[FF] Function of the AIU = Monitors the operating state of the electronics subsystem and the operating state of the antenna subsystem"]
-[7.455150604248047, 3.679964780807495, "[FF] Safety Compliance of the NightPod = Human spaceflight safety for pressurized payloads"]
-[13.34736156463623, 7.2308669090271, "[FF] Power Collection Strategy of the ABEX = Relying on stored power for burn maneuvers"]
-[8.310099601745605, 2.5381886959075928, "[TT] Particle Heights of the CATS = 4 -5 km, 16 km, closer to the ground"]
-[14.048415184020996, 7.224594593048096, "[TT] DET System of the EPS = 21-35 V"]
-[9.391792297363281, 6.992170810699463, "[TT] Resolution of the MSU-S = 240 m"]
-[4.806148529052734, 5.6403703689575195, "[TT] Operating Frequency of the GPSDR = 1227.6 MHz and 1575.4 MHz"]
-[4.225234031677246, 7.230862617492676, "[TT] Frequency Band of the S-band system = S-band"]
-[5.347375392913818, 6.47713041305542, "[TT] On-board Data Storage and Downlinking Interval of the \u00d8rsted satellite = Every 12 hours or less"]
-[6.48665714263916, 5.921117305755615, "[TT] Paths of the BPFs = Six paths"]
-[11.565367698669434, 6.418956756591797, "[TT] Energy Output of the NuSTAR = 10 million suns"]
-[8.324737548828125, 3.1390013694763184, "[FF] Award Date of the Ozone Monitoring Instrument = 29 April 2019"]
-[10.032632827758789, 4.435388088226318, "[FF] De-tumble mode function of the Torque Rods = Reduce rates on all three axes to<1\u00ba/s"]
-[7.22255277633667, 5.055186748504639, "[FF] Components of the ESEX = PFS (Propellant Feed System), power subsystem, command and telemetry modules, onboard diagnostics, arcjet assembly"]
-[13.755366325378418, 3.435786247253418, "[TT] Mass of the Meteorological Transmitter = ~70 kg"]
-[5.751945495605469, 3.263969659805298, "[TT] Operator of the Bluecrab supercomputer cluster = Maryland Advanced Research Computing Center"]
-[8.141268730163574, -0.372348427772522, "[TT] Maximum Extent Decline of the Arctic Sea Ice = Roughly 13 percent per decade"]
-[7.951836585998535, 7.544047832489014, "[FF] Development Team of the EnMAP Hyperspectral Imager = S. Hofer, H. J. Kaufmann, T. Stuffler, B. Penn\u00e9, G. Schreier, A. M\u00fcller, A. Eckardt, H. Bach, U. C. Benz, R. Haydn"]
-[4.787424564361572, -1.7825944423675537, "[TT] Landing Site Name of the Chang'e-4 = Statio Tianhe"]
-[7.453245639801025, 2.4770593643188477, "[TT] Measurement Category of the SPOT-5 = Multi-purpose imagery (ocean), Multi-purpose imagery (land), Vegetation, Albedo and reflectance, Landscape topography, Sea ice cover, edge and thickness, Ice sheet topography"]
-[5.950577735900879, 1.9629178047180176, "[TT] Recovery Time of the Orion = One hour after splashdown"]
-[3.409097194671631, 5.160958290100098, "[FF] Measurement Concept of the Integrated SAR Antenna = PNF (Planar Near-Field) concept"]
-[10.344040870666504, 2.7930917739868164, "[FF] Launch Date of the Nanosatellite = 22 March 2021"]
-[12.156229019165039, 2.9633731842041016, "[FF] Tank Type of the ACE propulsion system = Blow-down hydrazine tanks"]
-[11.615825653076172, 5.105395317077637, "[TT] Size of the Silicon drift diode = Barely bigger than an ant"]
-[9.140990257263184, 7.524840354919434, "[TT] Resolution of the PolyCam = >5 cm"]
-[16.53350067138672, 3.635496139526367, "[FF] Number of User Terminals of the OneWeb = Unknown"]
-[4.976334571838379, 4.0240888595581055, "[TT] AIS Receiver of the NorSat-3 = ASR x50"]
-[7.058480739593506, 1.4569413661956787, "[TT] Solar Array Deployment Time of the James Webb Space Telescope = Approximately 30 minutes after launch"]
-[7.928581714630127, 3.548665761947632, "[TT] Sensor complement / remarks of the Meteor-1-1 = TV, IR, AC"]
-[8.423791885375977, 8.036198616027832, "[TT] Nr. of Samples of the IMG = Band 1: 1.6 x 10 5 ; band 2 & 3: 1.0 x 10 5"]
-[4.408149242401123, -1.6544194221496582, "[FF] Time Since Formation of the Blue Ring Nebula = Millennia"]
-[8.149776458740234, 4.812710762023926, "[FF] Technology Areas of the GP-B probe = Cryogenics, magnetics, quantum devices, telescope design, control systems, quartz fabrication techniques, metrology, and gyroscope technology"]
-[5.311980724334717, 2.2179245948791504, "[FF] Agency of the ITASat-1 = AEB"]
-[6.175017833709717, 4.706042766571045, "[FF] Routine Activities of the DPCC = Nominal activities related to the provision of the link service, management of payload configuration and maintenance activities"]
-[13.59100341796875, 6.986227989196777, "[TT] Power of the EPS = < 8.6 W"]
-[6.324335098266602, 8.063711166381836, "[TT] Channels of the ROSA = 16 dual-frequency channels (4 AGGA chips)"]
-[13.262516975402832, 5.237478733062744, "[TT] Solar Panel Length of the Landmapper-Demo6 = 1.2 m"]
-[10.025336265563965, 2.832221031188965, "[TT] Total Deployed of the NRCSD (NanoRacks CubeSat Deployer) = 176"]
-[5.914990425109863, 1.776258111000061, "[FF] Meeting Date of the VIIRS M-Band = July 2014"]
-[4.701125621795654, 7.048356533050537, "[TT] Communication of the SEOSat = X-band for downloading imagery"]
-[7.790345668792725, 4.998627185821533, "[TT] Reference Frame of the rGPS = WGS84 Earth centered fixed frame"]
-[10.211886405944824, 1.5338917970657349, "[TT] Galaxy Cluster Detection of the eROSITA = Redshifts z > 1"]
-[7.654147148132324, 6.419580936431885, "[TT] Imaging Frequency of the PROBA-V = Every two days"]
-[7.997905254364014, 3.1168253421783447, "[FF] Objective of the GAS = Measurement of CO2, CH4, CO, N2O"]
-[5.528077602386475, 2.672915458679199, "[TT] Total Student Contributors of the SAPPHIRE = More than 70 Stanford students and 30 WU students"]
-[4.769494533538818, 0.35281383991241455, "[TT] Launch Date of the AIM = 2007"]
-[6.395814895629883, -0.4779127538204193, "[TT] Mission Duration of the Cheollian 2B satellite = Eight months"]
-[5.314237594604492, 5.549561023712158, "[TT] Standard of the Communications = ESA packet TM/TC CCSDS standard"]
-[9.507370948791504, 8.177777290344238, "[TT] Field of View of the Supervision Cameras = 65\u00ba x 54 \u00ba"]
-[8.156416893005371, -1.093375563621521, "[TT] Lidar of the ICESat-2 = Measures height"]
-[6.08027982711792, 2.461017370223999, "[TT] Designer of the New Horizons = Johns Hopkins University Applied Physics Laboratory"]
-[9.479557991027832, 6.1485209465026855, "[TT] Incidence Angle of the P Mode = 20\u00ba~50\u00ba"]
-[13.527761459350586, 3.071615695953369, "[TT] Payload Capacity of the Terran R = More than 20,000 kg"]
-[9.798510551452637, -0.40025970339775085, "[TT] Target Altitude of the CHEOPS = Equal or higher than 100 km"]
-[4.756371021270752, 7.322096824645996, "[TT] K-band Data Rate of the RF communications = 72 Mbit/s"]
-[4.414846420288086, 7.035072326660156, "[FF] Data Transmission of the ACOP = Ku-band"]
-[9.071025848388672, 7.347877502441406, "[TT] Tube Diameter of the Detector = 6 mm"]
-[3.250270128250122, 4.516490936279297, "[TT] Imaging Frequency Band of the TerraSAR-X = X"]
-[7.659980297088623, 1.2389475107192993, "[TT] Data Set Duration of the Global Satellite Mapping of Precipitation (GSMaP) = Less than twenty years"]
-[8.056522369384766, 6.334442138671875, "[TT] Type of the SSJ/5 = Imaging multi-spectral radiometers (vis/IR)"]
-[10.168949127197266, 5.822482109069824, "[TT] Nonlinearity Temperature of the MCT detector = Higher than 280 K"]
-[5.351978778839111, 6.370031833648682, "[TT] Die capacity of the SDR-SMM = 0.5 Gbit"]
-[4.283798694610596, 0.7985687255859375, "[TT] Start of Services of the EDRS = 2014"]
-[10.436198234558105, 7.432229518890381, "[TT] Coded Masks Distance of the JEM-X = 3.2 m"]
-[14.649598121643066, 6.675564289093018, "[TT] Battery of the UniSat-1 = NiMH batteries of 2.4 Ah capacity"]
-[4.923159122467041, -2.132296085357666, "[TT] Payload Mass of the Chang'e-2 = 140 kg"]
-[10.996990203857422, 0.7705563306808472, "[FF] Commonality of Earth-size exoplanets of the Red Dwarf Star = Increasing evidence"]
-[5.788409233093262, -0.3637962341308594, "[TT] Follow-up Period of the SRG = 3 years"]
-[10.4530668258667, 5.7847442626953125, "[TT] Interface Temperature of the HTS = Between -10\u00baC and +15\u00baC"]
-[10.418898582458496, 7.262505531311035, "[TT] Area Coverage of the WPM = 5 km by 3 km"]
-[10.152846336364746, 1.4886322021484375, "[TT] Number of Clusters of Galaxies of the eROSITA = Approximately 100,000"]
-[4.877816200256348, 0.09891073405742645, "[TT] Launch Date of the STPSat-3 = 20 Nov 2013"]
-[9.433916091918945, 2.9711005687713623, "[FF] Impact on Xenon Consumption of the Solar Activity = Lower than what was expected in the mission design phase"]
-[7.936402320861816, 6.928467273712158, "[FF] Image Type of the LROC = Black-and-white and color"]
-[5.902837753295898, -0.25265181064605713, "[TT] Mission Life of the ANUSat = 2 years"]
-[11.447040557861328, 0.7489422559738159, "[TT] Size of the AU Mic b = About 8% larger than Neptune"]
-[11.53725528717041, 6.88823938369751, "[TT] FOV of the SEDA = Protons: \u00b1 39.35\u00ba, Electrons: \u00b178.3\u00ba"]
-[11.054720878601074, 5.821972370147705, "[TT] Cover Glass Thickness of the TFSC = 0.1 mm"]
-[12.197476387023926, -0.20303742587566376, "[TT] Full Frame Images Cadence of the TESS = 30-minute"]
-[3.853361129760742, 6.430596828460693, "[TT] Array of the Onboard Antenna = 2 x 2 patch array"]
-[4.3346662521362305, -0.09862373024225235, "[TT] Launch Date of the P35 series = Feb. 19, 1963"]
-[11.686750411987305, 0.1751956343650818, "[TT] Size of the TESS = Four times the size of our planet"]
-[12.106435775756836, 6.0037055015563965, "[FF] Age of Cosmic Rays in the Galaxy of the AMS = ~12 million years"]
-[10.005533218383789, 8.230728149414062, "[TT] Aperture of the FUV Channel = ~380 mm"]
-[11.622060775756836, 4.329649448394775, "[TT] Extension Length of the Fairing = 1.5 m"]
-[7.49323034286499, 8.848437309265137, "[FF] Electromagnetic Spectrum Range of the LISS-3 = Unknown"]
-[5.666243076324463, -0.9025769829750061, "[TT] Design Life of the HY-1C = 5 years"]
-[10.140957832336426, 5.727045059204102, "[TT] Temperature Stability of the Detector Cooler = Better than \u00b10.25 K"]
-[3.2351467609405518, 3.8071227073669434, "[TT] Years on Orbit of the TerraSAR-X = 10"]
-[5.405205726623535, 8.262215614318848, "[TT] Frequencies of the MWRI-RM = 17"]
-[6.682249069213867, 5.3525543212890625, "[FF] Development, Test and Flight Results of the RF Systems = Unknown"]
-[4.6536545753479, 7.941787242889404, "[TT] Frequency of the RF communication subsystem = 435.325 MHz/145.95 MHz"]
-[6.473916530609131, 8.741503715515137, "[TT] Polarization of the POLDER = yes"]
-[6.820705890655518, 5.34822416305542, "[FF] Design of the SMS = Radiation-hardened system"]
-[4.662904739379883, 7.118869781494141, "[TT] Downlink Data Rate of the X-band phased array antenna = 105 Mbit/s"]
-[9.141840934753418, 2.782520055770874, "[FF] Observation Type of the RHESSI = Global wave generation"]
-[14.784391403198242, 6.476288795471191, "[TT] Mass Comparison of the Lithium Ion Battery = Half the mass of a conventional nickel-cadmium battery"]
-[6.513916015625, -0.25946149230003357, "[TT] Global Occurrence Rate of the FORMOSAT-2 = 24 TLEs per minute"]
-[7.9629716873168945, 7.924263954162598, "[FF] Device Type of the VIRR = Visible and Infrared"]
-[13.606636047363281, 1.7375861406326294, "[TT] Return Cargo Capacity of the Dragon = More than 1800 kg"]
-[11.40156364440918, 4.429883003234863, "[TT] Size of the OptiCube-1 = 3U"]
-[7.91616678237915, 5.143258571624756, "[FF] Internal Calibration of the Mini-RF = Acquired every time that Mini-RF takes a data collect; a chirp, noise, and tone calibration is done both immediately before and immediately after a data collect"]
-[4.961516380310059, 0.06308023631572723, "[TT] End of Operations of the SPOT-2 = July 2009"]
-[5.184035778045654, 6.105337142944336, "[FF] Radiation Sensitivity of the SDR-SDRAM devices = General"]
-[11.964811325073242, 6.607072353363037, "[TT] Sine Burst Levels of the AM and PM flight structures = Up to 14.4 g"]
-[4.699777603149414, 7.2348833084106445, "[FF] Data Rate of the X-band transmitter = Up to 100 Mbit/s"]
-[13.28855037689209, 6.977172374725342, "[TT] Capacitance of the PPTs = 0.76 \u00b5F"]
-[9.706461906433105, -0.42936044931411743, "[TT] Orbit Altitude of the Crew Dragon = Approximately 575 kilometers"]
-[7.894721031188965, 3.0877206325531006, "[FF] Measurement Type of the TanSat = Carbon Dioxide Maps"]
-[7.962719440460205, 7.676463603973389, "[FF] Purpose of the Hyperspectral imager = Takes measurements over hundreds of wavelengths"]
-[5.415542125701904, 1.1780177354812622, "[FF] Presentation Date of the DLR FireBird Constellation = May 30-June 3, 2016"]
-[10.137203216552734, 5.496279239654541, "[TT] Purpose of the HS = Keep equipment temperatures above the minimum non-operational limits (\u201320 \u00baC for most of the units) during satellite SHM and PLM Off modes"]
-[6.83112096786499, 5.993086814880371, "[TT] Multi-Look of the Capella = 30"]
-[9.635140419006348, 5.311150550842285, "[TT] Theoretical Performance of the Lateral Shearing Angular Period = 41 mas"]
-[8.585540771484375, 1.7320846319198608, "[TT] Range of Values of the Cloud amount = 0 - 100%"]
-[10.256847381591797, 3.158541202545166, "[TT] Number of CubeSat P-PODs of the CubeSat - Launch 4 = 3"]
-[7.663416862487793, 1.9086281061172485, "[FF] Function of the Amazon Rainforest = Draws carbon out of the atmosphere and stores it in plant matter or the soil"]
-[6.6569437980651855, 5.772805690765381, "[TT] Number of Sets of the HETG = 2"]
-[9.854561805725098, -1.323461651802063, "[TT] Orbital Planes Inclination of the MEO Constellation = 56\u00ba"]
-[8.124188423156738, -1.0277361869812012, "[TT] Application of the ICESat-2 = Investigate coastal ecosystems, measure mangrove forests, measure sea level rise in coastal regions, improve nearshore bathymetry maps"]
-[7.358198165893555, 4.614863395690918, "[FF] Function of the Spacecraft GNC (SC-GNC) = Controls the absolute attitude of the spacecraft and estimates its absolute position"]
-[4.044075012207031, 6.981029510498047, "[TT] Antenna Type of the S-band Transmitter = SFL-developed patch antennas"]
-[6.854400157928467, 6.031749725341797, "[TT] Planned Quantity of the Touch Downs/Sample Collections = Three"]
-[13.969011306762695, 7.102365493774414, "[TT] Power Source of the Electronics = Spacecraft 28 V bus"]
-[13.881158828735352, 3.052554130554199, "[TT] Mass of the Main Platform = 800 - 900 kg"]
-[4.452838897705078, 6.79393196105957, "[TT] RF Communications of the Spacecraft = S-band for TT&C support"]
-[10.25351333618164, 7.991833209991455, "[TT] Aperture Diameter of the DST (Dobson Space Telescope) = 80 mm"]
-[5.425127029418945, 0.016135158017277718, "[FF] Acta Astronautica Publication Date of the IRS-P6 = Jan. 2007"]
-[9.323908805847168, 5.095737457275391, "[TT] Attitude Pointing Error of the AOCS = < 0.3\u00ba"]
-[7.255303859710693, 4.677711009979248, "[FF] Mounting of the FBGs = Steel mounting with a cantilever"]
-[8.017865180969238, 8.679832458496094, "[TT] Spectral Range of the AaSI = Visible"]
-[8.294259071350098, 8.717591285705566, "[TT] Spectral resolution of the UV/VIS Spectrometer = 0.89 nm"]
-[4.792288780212402, -0.13041970133781433, "[TT] End of Life Date of the NPSat-1 = 18 Months"]
-[6.564001083374023, 5.559855937957764, "[TT] Operational Status of the CDH and EPS subsystems = Always ON"]
-[5.277911186218262, 1.2634334564208984, "[FF] Conference Date of the SOMP = September 8-9, 2009"]
-[13.460320472717285, 5.478128910064697, "[TT] Solar Panels of the Meteosat = More than 8000 cells"]
-[8.915502548217773, 6.135843276977539, "[TT] Scanning Rate of the AMSR = 40 rpm"]
-[7.745813369750977, 2.6898975372314453, "[FF] Objectives of the HSC = Urban lights, electric storms, polar regions, snow cover Measurements of light intensity (urban areas, detection of electric storms, snow coverage, detection of fishing boats and aurora studies)"]
-[11.929247856140137, 4.996456146240234, "[TT] Size of the TIDM = 46 mm x 27 mm x 18.5 mm"]
-[5.5074782371521, 2.289712905883789, "[FF] Affiliation of the Nobuo Sugimura = Unknown"]
-[8.147974014282227, 2.9069018363952637, "[FF] Coverage of the GLM = Earth's radius down to individual thunderstorms"]
-[9.030330657958984, 2.592904567718506, "[FF] Mission of the IBEX = Outer heliosphere research"]
-[5.118643760681152, 8.226347923278809, "[TT] Purpose of the RF Filter Box = Mitigate strong pulsed interference from the Aquarius instrument"]
-[8.042280197143555, 3.8208303451538086, "[FF] Function of the CARMEN-3 = Space environment measurement: orbital debris, high and low energy particles"]
-[7.234447479248047, 5.243200302124023, "[FF] Purpose of the COTS #2 = Examine synergistic radiation effects on a variety of newer state-of-the-art digital microcircuit and multi-chip module (MCM) technologies"]
-[8.243191719055176, 8.160905838012695, "[TT] Resolving Power of the CHIPS = f/150"]
-[5.7519330978393555, 7.425504207611084, "[FF] Frequency Range of the GimmeRF = Unknown"]
-[13.579739570617676, 2.871436595916748, "[TT] Payload Volume of the Supernova-Beta = 7000 cm3"]
-[6.924701690673828, 3.627039909362793, "[FF] Requirement of the Caging System = Prevent damage to the sphere during launch and to release the sphere after arrival of the satellite on orbit"]
-[9.694316864013672, 2.6852149963378906, "[FF] Purpose of the COBE (COsmic Background Explorer) = Measure the leftover radiation from the big bang"]
-[7.978080749511719, 13.68582534790039, "[TT] SSD of the B4 = 10 m"]
-[9.980270385742188, 5.4287919998168945, "[FF] Health Monitoring of the C&DH = Temperature, battery voltage"]
-[10.826494216918945, 7.1734747886657715, "[TT] Target Size of the PRISMA Payload = 30 km x 30 km"]
-[8.680879592895508, 5.090873718261719, "[TT] Star Intensity Accuracy (3\u03c3) of the STOs and STAEs = Random Bias -0.26 ~ +0.28 mag ((@ 6 mag) -0.4 ~ +0.65 mag (@ 6 mag)"]
-[4.873747825622559, 7.341545104980469, "[TT] Data Rate of the S-band = 4 kbit/s"]
-[5.992467880249023, 5.178664684295654, "[FF] Data Interface of the OBC = I2C bus"]
-[5.931741714477539, -0.06654594093561172, "[TT] Extended Mission Duration of the Juno = Through September 2025"]
-[5.138391494750977, 2.9903526306152344, "[TT] Major Contribution of the LRI = Provided by Germany"]
-[7.966892242431641, -2.5663068294525146, "[TT] Resolution of the GOLD = 0.21, 0.35, or 2.16 nm"]
-[11.114282608032227, 5.288228511810303, "[TT] Core Diameter of the Graded Index Multimode Fiber = 200 \u00b5m"]
-[5.578750133514404, 6.97264289855957, "[TT] Speed of the ASIC = Up to 25 Mpixel/s"]
-[4.185718536376953, 2.1072003841400146, "[TT] Software Load Location of the NigeriaSat-2 = On-Board Computer"]
-[7.808804512023926, 2.1540212631225586, "[TT] Revisit Time for Ocean Color Scanner of the Satellite = Every day"]
-[11.941679000854492, 5.040796279907227, "[TT] Size of the STAFF/DWP = 351 mm x 200 mm x 208 mm"]
-[8.099160194396973, 8.737516403198242, "[TT] Wavelength Range of the RAVAN = UV (200 nm) to far infrared (200 \u00b5m)"]
-[4.968578815460205, 0.669246256351471, "[FF] Mission Launch Date of the PACE = 2023"]
-[8.97375774383545, 3.13250994682312, "[FF] Detection Capability of the TimePix radiation sensors = Able to detect radiation flux spikes of over 1000 times the background level during a single solar particle event (SPE)"]
-[7.516820907592773, 5.116428852081299, "[FF] Scan Modes of the DMSP SSM/I sensor = Two alternating modes"]
-[5.027672290802002, 3.322197675704956, "[TT] Manufacturer of the VRSS-1 = CGWIC (China Great Wall Industry Corporation)"]
-[4.187549114227295, 2.5159785747528076, "[TT] Launch Site of the Falcon 9 rocket = Vandenberg Air Force Base"]
-[9.633444786071777, 6.397665023803711, "[FF] Control Loop of the SM = Rotates the steering mirror until the local and incoming beams are parallel on the photodetector"]
-[5.8352885246276855, 0.0778665617108345, "[TT] Identification Time of the CSpOC Catalog = L+20"]
-[8.092742919921875, 3.3614444732666016, "[TT] Spectral Measurement of the Lightning camera = Broad band"]
-[4.550711631774902, 5.700349807739258, "[TT] Distress Signal Detection Range of the MEOLUT Next = More than 5,000 km"]
-[1.6223149299621582, 3.7584264278411865, "[TT] Multi-function component assembly of the BEESAT-1 = Yes"]
-[8.70150375366211, -0.22450439631938934, "[TT] Inclina. (\u00ba) of the Cosmos-1066 (Astrofizika) = 81.2"]
-[6.82045316696167, 5.2586164474487305, "[FF] Performance of the RAFS = Excellent frequency stability"]
-[4.491397857666016, 1.5867029428482056, "[TT] Launch Date of the GovSat-1 = 31 Jan 2018"]
-[13.506549835205078, 6.180807590484619, "[TT] Payload Power of the Solar Orbiter = 180 W"]
-[8.556153297424316, 2.0137736797332764, "[TT] Spatial Resolution of the SeaWinds = 50 km"]
-[9.110831260681152, 3.152970314025879, "[FF] Measurement Regions of the Cluster = Solar wind and bow shock, magnetopause, polar cusps, magnetotail, auroral zone"]
-[8.17319393157959, 2.977864980697632, "[FF] Purpose of the ASIM = Surveys severe thunderstorms in Earth\u2019s atmosphere and upper-atmospheric lightning"]
-[8.509427070617676, 5.350181579589844, "[TT] Position Accuracy (RMS orbit) of the S-1 NRT = < 10 cm (2D)"]
-[6.5001726150512695, 3.364252805709839, "[TT] Imaging Resolution of the BlackSky Next Generation Satellites = 35 cm at nadir, 50 cm on average"]
-[8.747810363769531, 7.596410751342773, "[TT] Format of the Detector = 600 x 600 pixels"]
-[5.5496745109558105, 2.8805480003356934, "[TT] Development Funding of the iMESA = AFOSR and AFRL"]
-[6.3697333335876465, 0.9007557034492493, "[TT] Data Set of the Gaia = Third"]
-[6.005132675170898, -0.4307425916194916, "[TT] Mission Duration of the Worldview-4 = 10 to 15 years"]
-[3.817584276199341, 7.908520221710205, "[TT] Modulation Scheme of the Software-Defined Radio (SDR) = Digital QPSK"]
-[6.976778507232666, -0.7855259776115417, "[TT] Orbit Period of the TOI 700 b = 10 days"]
-[3.392291784286499, 5.269043922424316, "[TT] Observing Frequency of the L-SAR = 1.275 GHz"]
-[7.557675838470459, 8.594467163085938, "[TT] Band Number of the Spectral Bands = 1, 2, 3, 4, 5, 6, 7, 8"]
-[7.747754096984863, 3.1158065795898438, "[FF] Evaluation Data of the AVTP and AVMP retrievals = Global ECMWF analysis fields, radiosonde (RAOB) measurements, and AIRS (Aqua-Atmospheric Infrared Sounder) heritage algorithm retrievals"]
-[14.327272415161133, 3.1730356216430664, "[TT] Mass of the KELT-9 b = 2.9 times its mass"]
-[10.540409088134766, 5.277454853057861, "[FF] Components of the Maeva Hinges = Carpentier elastic blades, SMA strings, Cerafil heater wires"]
-[5.778203010559082, 2.525117874145508, "[FF] Team Members of the Dellingr = Larry Kepko, Chuck Clagett, Luis Santos, Behnam Azimi, Daniel Berry, Todd Bonalsky, Dean Chai, Matthew Colvin, Alan Cudmore, Allison Evans, Scott Hesh, Sarah Jones, James Marshall, Nicholas Paschalidis, Zach Peterson, Juan Rodriquez, Marcello Rodriquez, Salman Sheikh, Scott Starin, Eftyhia Zesta"]
-[8.997941017150879, 0.5419546961784363, "[TT] Launch Date of the Artemis-I = 16 November 2022"]
-[12.398910522460938, 0.6043304800987244, "[TT] Sky Coverage of the PLATO = Half of the sky"]
-[6.595987319946289, 5.732892036437988, "[TT] Number of Science Boards of the MakerSat = 4"]
-[13.325593948364258, 7.711206912994385, "[TT] Power of the Transmitting Power = over 5 W"]
-[7.7667236328125, 6.112739562988281, "[FF] Operation of the THEIA = Image Capture"]
-[6.180281162261963, 5.953577995300293, "[FF] Components of the SSRU = 2 CIBs (Control Interface Boards), 4 SBs (Storage Boards), 2 PBs (Power Boards), and a backplane"]
-[10.01220417022705, 1.8189412355422974, "[TT] All-Sky Survey Date of the eROSITA = 19 June 2020"]
-[7.4945454597473145, 3.303746461868286, "[FF] Description of the Level-5 (L5) = Mosaic image"]
-[4.8771562576293945, 7.363832950592041, "[TT] S-band transceivers Data Rate of the PCDU = 25-384 kbit/s TM"]
-[10.862493515014648, 6.380425930023193, "[TT] Coating of the Mirror = Gold (> 50 nm)"]
-[6.290550708770752, -0.25938498973846436, "[TT] Launch Timeframe of the Lightspeed Satellites = Around two years"]
-[11.779524803161621, 3.2680935859680176, "[FF] Propulsion Efficiency of the DRACO = Two to five times the efficiency of chemical propulsion"]
-[5.323408603668213, 1.0015939474105835, "[FF] Mission Extension Announcement Date of the LADEE = Jan. 31, 2014"]
-[7.3689093589782715, 2.4389309883117676, "[FF] Monitoring Area of the PROBA-V = Europe and Africa"]
-[1.9368454217910767, -0.40330350399017334, "[TT] Mission Duration of the Van Allen Probes = 2 years"]
-[4.735903263092041, -0.2835017740726471, "[FF] Status Update Date of the CATS = Feb. 16, 2015"]
-[9.553919792175293, 4.742796897888184, "[TT] Attitude Control of the ADCS unit = 3-axis stabilization"]
-[10.369714736938477, 3.2119250297546387, "[TT] Quantity of the CubeSats = 12"]
-[5.946715354919434, -0.5741170048713684, "[TT] Mission Life of the TechEdSat-1 = 7-8 months"]
-[4.896705150604248, 3.2740845680236816, "[TT] Manufacturer of the RadFET = Tyndall National Institute in Ireland"]
-[5.918169021606445, 1.5456032752990723, "[FF] Presentation Date of the Prisma Satellites = June 4-8, 2012"]
-[6.893977642059326, 7.96298885345459, "[TT] Noise figure of the HPA = 2.9 dB"]
-[5.397158145904541, 1.1792014837265015, "[FF] Project Date of the Small Explorer (SMEX) = March 28, 1994"]
-[4.996245861053467, 3.294926166534424, "[TT] Manufacturer of the Delfi-C3 = Technical University of Delft, The Netherlands"]
-[8.350650787353516, -0.6448014378547668, "[FF] Size of the Iceberg A-76 = Largest iceberg floating anywhere in the world"]
-[9.695165634155273, -0.12919211387634277, "[TT] Lowest Altitude of the TSUBAME = 167.4 km"]
-[3.1264915466308594, 2.209639310836792, "[TT] Data Source of the Green City Watch = Copernicus Sentinel satellite data"]
-[4.794294357299805, 0.4670664668083191, "[TT] Launch Date of the MSG-3 = July 5, 2012"]
-[13.41351318359375, 7.390279769897461, "[TT] Power of the LISS-4 = 216 W"]
-[10.453391075134277, 5.775130748748779, "[TT] Temperature Range of the Operating temperature = -30\u00ba - -20\u00ba C"]
-[10.727089881896973, 1.1811105012893677, "[TT] Size Compared to Sun of the TOI 270 = About 40% smaller"]
-[14.260741233825684, 3.2122294902801514, "[TT] Mass of the ROMAP = 0.7 kg"]
-[5.004253387451172, 0.4804419279098511, "[TT] Re-Entry Survival of the QARMAN = Yes"]
-[8.653364181518555, 1.0836542844772339, "[TT] Data Collection Start Date of the Aquarius/SAC-D satellite = August 25, 2011"]
-[6.742159366607666, 4.988236904144287, "[TT] Processing Unit of the FIBOS = PCB (Printed Circuit Board)"]
-[8.5049409866333, 6.123135089874268, "[TT] Measurement Method of the SRM = Measure the current-voltage (I-V) characteristics"]
-[3.5316646099090576, 5.3682451248168945, "[TT] Pulse Transmission Rate of the SAR = 1,500 pulses/s"]
-[11.487593650817871, 5.673089504241943, "[TT] Hardness of the Inconel 718 = >33.4 HRC"]
-[8.472548484802246, 8.592591285705566, "[TT] Order Filter of the Micro-spectrometer = Prevents visible radiation (below 900 nm) from entering the spectrometer chamber"]
-[6.506340980529785, -0.441142737865448, "[TT] Uptime of the AlSat Nano = 27.4 days"]
-[4.600074291229248, 7.165420055389404, "[TT] Data Transfer of the NEXTAR-300L = X-band communication"]
-[13.973240852355957, 3.0143589973449707, "[TT] Total mass of assembly of the STRV-2 DHS = 2 kg"]
-[4.74264669418335, -0.2667819857597351, "[FF] Status Update Date of the CATS = Feb. 26, 2015"]
-[10.883288383483887, -0.29497963190078735, "[FF] Data Acquisition Plan of the TanDEM-X = Not provided"]
-[6.325693130493164, 1.779836893081665, "[FF] Presentation URL of the SVOM = https://indico.in2p3.fr/event/12490/session/3/contribution/7/material/slides/0.pdf"]
-[4.372602462768555, 2.0511667728424072, "[TT] Revisit Time of the DubaiSat-2 = < 8 days"]
-[13.331377029418945, 2.8545660972595215, "[TT] Mass of the DubaiSat-2 = ~ 300 kg"]
-[5.092553615570068, 1.258628487586975, "[TT] Conference Date of the PSAT = Aug. 5-10, 2017"]
-[13.344555854797363, 2.8748891353607178, "[TT] Mass of the TechEdSat = 1.2 kg"]
-[8.968475341796875, 4.571425914764404, "[FF] Safe Mode Attitude Control Principles of the SPOT-6 = Sun oriented, magnetic field spin controlled, or Earth oriented"]
-[11.02940559387207, 7.653024673461914, "[TT] Swath Width of the POLDER-P = 2400 km"]
-[8.75338363647461, 7.669906139373779, "[TT] Data Tile Size of the EnMAP = 1000 x 1024 pixels"]
-[5.706483364105225, 4.820183277130127, "[FF] Application of the Geostationary Communication Relays = Communication"]
-[5.338771343231201, 4.936454772949219, "[TT] Daily Downlink Time of the Ground Station Subsystem (GSSS) = About 102 minutes"]
-[4.133553504943848, 1.3828835487365723, "[FF] Launch Confirmation Date of the MeteoSat Third Generation = 23 March 2021"]
-[4.727567195892334, -1.8064000606536865, "[FF] Landing Date of the Chang'e-3 = Dec. 14, 2013"]
-[5.795928001403809, 0.9568191766738892, "[TT] Launch Date of the WorldView-3 = August 13, 2014"]
-[9.066081047058105, 9.99051284790039, "[TT] GSD of the Eastman Kodak KLI14403 linear CCD sensor = 22 m"]
-[9.170683860778809, 6.091284275054932, "[TT] Observation Angles of the Sensor = Various"]
-[4.6704301834106445, 7.569982528686523, "[TT] Amplifier Gain of the Ka-band = 36 dB"]
-[7.197999954223633, 1.9784268140792847, "[TT] Target Tracking of the Carbonite-2 = Supported"]
-[11.24356460571289, 3.338761329650879, "[FF] Unknown of the Micropropulsion Experiment = Unknown"]
-[9.52331829071045, 7.115340709686279, "[TT] Absolute INR of the ABI = 54 \u00b5rad (EW), 21 \u00b5rad (NS)"]
-[10.064369201660156, -1.5580949783325195, "[TT] Inclination of the TSX-5 = 68\u00ba"]
-[5.68255615234375, 8.177300453186035, "[TT] DSB noise temperature of the Millimeterwave receiver = 1000 K"]
-[10.20089054107666, 5.422060966491699, "[FF] Thermal Coupling of the Flight Computer, Payload Electronics, Radio = Well-coupled to the bottom plate"]
-[8.713689804077148, -0.21360675990581512, "[TT] Perigee (km) of the Meteor-1-1 = 644"]
-[4.8386406898498535, -1.8358230590820312, "[TT] Earth-to-Moon Cruise Time of the Chang'e-1 = 12 days"]
-[6.8589606285095215, 3.2834880352020264, "[FF] Services of the MTSAT = Aeronautical communications and navigation, and meteorological observations"]
-[9.500861167907715, 6.157534599304199, "[TT] Incidence Angle Range of the Stripmap = 21\u00ba - 50\u00ba"]
-[14.17463207244873, 3.123931407928467, "[TT] Mass (kg) of the ALOS-1 = 4000"]
-[8.568519592285156, 8.622747421264648, "[FF] Design of the Interferometer = Birefringent gratings, Wollaston prisms, and LSI spacers to create the grating lateral shearing interferometer"]
-[7.553826332092285, 2.982553005218506, "[TT] Methane Detection Resolution of the Iris = 25 m on the ground"]
-[5.642253875732422, 4.681513786315918, "[FF] Data Transmission of the McMurdo Ground Station = NOAA in Suitland"]
-[14.231521606445312, 6.748149394989014, "[TT] Type of the Charging circuit = Constant current/constant voltage charging"]
-[8.311905860900879, 4.820633888244629, "[FF] Modes of the Satellite = Open-loop, Interactive mode, Closed-loop, Automatic target pointing"]
-[7.9279584884643555, 4.713937759399414, "[FF] Characteristics of the Detector = High MTF and high quantum efficiency"]
-[6.430464267730713, 5.709272384643555, "[FF] Purpose of the E-cal Signal = Checking the stability of the amplifiers and of the data stream"]
-[5.816293239593506, -0.8201999664306641, "[TT] Service Life of the Prometheus Satellite = 3 to 5 years"]
-[9.870972633361816, 4.397453784942627, "[TT] Sampling Coordination of the PNI RM3000 = With pulsing by the magnetorquers"]
-[4.909083366394043, 0.46867889165878296, "[TT] Launch Date of the SASAR INSAT-2 = July 9, 1992"]
-[9.24448299407959, 3.140847682952881, "[FF] Nature of the Corona = Cloud of particles traveling near the speed of light"]
-[11.739035606384277, 6.754826068878174, "[TT] Momentum Range of the TRD = 10 to 300 GeV/c"]
-[13.497620582580566, 6.717612266540527, "[TT] Maximum Orbit-Average Power Dissipation of the ASTERIA = 24 W"]
-[8.435511589050293, 6.919381141662598, "[FF] Type of the MSC = High resolution optical imagers"]
-[5.7287750244140625, -0.36217930912971497, "[TT] Deployment Time of the iROSA = 10 minutes"]
-[6.75683069229126, -0.6371979117393494, "[TT] Orbit Reach Time of the Kick Stage = About 10 minutes later"]
-[4.811621189117432, 0.4500207304954529, "[TT] Launch Date of the CuPID = 27 Sept 2021"]
-[6.625838279724121, 5.078300476074219, "[FF] Data Collection of the DCS = In-situ data from Data Collection Platforms (DCPs) in the ground segment with location capability"]
-[13.250072479248047, 5.237276554107666, "[TT] Size of the Solar Array = 9.29 m2"]
-[5.742725372314453, 7.764667987823486, "[FF] Phase-matched v-pol and h-pol channels of the RF front ends = Based on the heritage GMI design"]
-[7.468458652496338, 2.919180154800415, "[TT] Monitoring Target of the MethaneSAT = Methane emissions"]
-[13.010271072387695, 7.320888042449951, "[TT] Power Consumption of the Micro-spectrometer = < 1 W"]
-[6.218551158905029, 0.8140889406204224, "[FF] Activity Date of the GIADA = March 17-21, 2014"]
-[11.218523979187012, 1.016470193862915, "[FF] Purpose of the LISA Pathfinder = Measure how well we can isolate a macroscopic body from all external forces except gravity"]
-[10.187337875366211, 9.394383430480957, "[TT] Nominal IGFOV of the Band 11 = 2 km"]
-[3.781238079071045, 4.556297302246094, "[FF] Data and Satellite Solutions of the SAR Satellites = Government and commercial use"]
-[9.52625560760498, 0.760008692741394, "[TT] Trip Distance of the ATLAS = 2,000 miles"]
-[11.644915580749512, 6.736260890960693, "[TT] Spectral Resolution of the XSM = ~ 250 eV at 6 keV"]
-[9.974991798400879, 4.606451988220215, "[FF] Orientation Control of the GomX-3 = Spinning miniaturized \u2018reaction wheels' at varying speeds"]
-[9.504084587097168, 4.130867004394531, "[TT] Type of the GSFC Fluxgate = Miniature vector fluxgate"]
-[5.182801246643066, 6.445596694946289, "[TT] Data Transmission of the Optoelectronic System = 25MHz LVDS, 100 MHz SpaceWire, Real-time LVDS"]
-[3.4073872566223145, -0.7486674785614014, "[TT] Orbit Type of the NigeriaSat-2 = Sun-synchronous circular orbit"]
-[5.301554203033447, 4.073858737945557, "[TT] Platform of the SAR spacecraft = CAST-2000 bus with necessary modifications and upgrades"]
-[9.34801959991455, 6.763892650604248, "[TT] Resolution of the MAG = 0.016 nT"]
-[9.888510704040527, 7.020774841308594, "[TT] Ground Sampling Distance of the NEMO-AM = Approximately 42 m"]
-[6.2461652755737305, 4.326321601867676, "[FF] Important Feature of the Mission Control Center = TOPE scripting IF"]
-[9.285665512084961, -0.651730477809906, "[TT] Orbit of the TSX-5 = Elliptical orbit of 410 km x 1710 km"]
-[7.177577972412109, 2.7886123657226562, "[TT] Launch Date of the MethaneSAT Instrument = October 1, 2022"]
-[7.852569580078125, 6.459345817565918, "[TT] Imaging Opportunities of the TeLEOS-1 = Up to 6 within a day"]
-[4.876664638519287, 0.17103490233421326, "[TT] Installation Date of the SpaceX CRS-17 = May 6"]
-[8.210187911987305, 2.7718546390533447, "[FF] Cloud Discrimination Processing Time of the ABO2 = Longer than using CAI-2"]
-[13.34520149230957, 2.903099775314331, "[TT] Mass of the MightySAT I = 63 kg"]
-[8.251899719238281, 4.479920864105225, "[FF] Purpose of the LARES-2 = Testing general relativity"]
-[7.930992603302002, 7.159241676330566, "[TT] Saturation Limit of the CCD = IC = 7:5"]
-[11.95781135559082, -0.14432887732982635, "[FF] Parameter of the TESS = Value"]
-[6.594361305236816, 7.690093040466309, "[TT] Data Quantization of the Imager = 11 bit"]
-[12.086244583129883, 4.552206993103027, "[TT] Size of the ADEOS spacecraft = 4 m x 4 m x 5 m"]
-[3.3418357372283936, 1.5048341751098633, "[TT] Launch Date of the Sentinel-5P = 13 October 2017"]
-[10.90195083618164, 7.3785400390625, "[TT] Width of the iROSA = 20 feet"]
-[11.180079460144043, 0.9377503991127014, "[TT] Launch of the LISA = 2034"]
-[7.914544105529785, 7.182094097137451, "[TT] Flash Efficiency of the Imager = 80%"]
-[6.494317054748535, 5.455957412719727, "[FF] Down converted to an intermediate frequency of the Analog outputs = Enabling sampling by a high-speed analog-to-digital converter and processing by the digital backend"]
-[8.408023834228516, 1.1958775520324707, "[TT] Range of values of the Precipitation over water = 0-25"]
-[7.6085052490234375, 8.46778392791748, "[TT] Bands of the AaSI = One to three"]
-[4.989621162414551, 0.12038952857255936, "[TT] End of Life Date of the IMAGE = 18 December 2005"]
-[11.12075424194336, 5.452121734619141, "[TT] Hamamatsu PMTs of the Range Calorimeter = 2 per plane"]
-[13.429549217224121, 6.690453052520752, "[FF] Output Power of the Satellite = Equivalent to the light from a 60 watt lamp"]
-[9.588109016418457, 8.2618408203125, "[TT] Field of View of the Xybion camera = 10.7\u00ba x 14.0\u00ba"]
-[7.692997932434082, 6.576955795288086, "[TT] Scanning Time per Image of the VHRR = 30 minutes"]
-[8.14548110961914, -0.6780602335929871, "[FF] Observation Data of the CryoSat-2 = Arctic sea-ice thickness measurements"]
-[3.403890371322632, 5.028661251068115, "[FF] Input of the MDA Tool = Relevant characteristics of a proposed SAR beam mode"]
-[13.24459457397461, 7.334157466888428, "[TT] Power consumption of the DST 35 = 20 W average 50 W peak including downlink"]
-[6.114679336547852, 7.717731475830078, "[TT] Signal Transmission of the GIOVE-A = L1 and E5"]
-[8.797250747680664, 4.677341461181641, "[TT] Purpose of the Star Tracker = Fine-attitude determination"]
-[4.5991926193237305, 6.57914924621582, "[FF] Function of the SCP = Provide a UHF link for the ODTML services and to function as an internal S&F subsystem"]
-[5.379629135131836, 0.5017351508140564, "[TT] Hydrazine Exhaustion of the Envisat = End of 2010"]
-[9.705830574035645, 7.160292148590088, "[TT] Ground Resolution of the HgCdTe = 120m"]
-[6.371833801269531, 0.619785487651825, "[FF] Power Protection Design of the FormoSat-5 = Unknown"]
-[13.971867561340332, 7.036365985870361, "[TT] Power Source of the Spacecraft = 28V battery"]
-[4.871468544006348, 7.232839584350586, "[TT] Downlink Data Rates of the NEMO-AM = 32kbit/s to 2Mbit/s"]
-[4.625110149383545, 4.752557754516602, "[FF] Boat Detection of the VIIRS = 10,000 to 20,000 boats every night"]
-[9.458693504333496, 6.983780860900879, "[TT] Spatial Resolution of the MSU-MR = 1 km"]
-[8.170309066772461, 2.513295888900757, "[FF] General Objective of the PARASOL = Study the Earth's atmosphere"]
-[4.611221790313721, 1.6257621049880981, "[TT] HPGP Commissioning Date of the SkySat-3 = August 3, 2016"]
-[8.817733764648438, 6.4540300369262695, "[FF] Imaging Subject of the PROBA-V = Drakensberg mountains"]
-[7.950248718261719, 9.105775833129883, "[TT] Wavelength of the ATM = 532 nm"]
-[9.09362506866455, 8.49704647064209, "[FF] Design of the Optical Telescope = Nearly diffraction-limited system close to the near-infrared band"]
-[8.93988037109375, 7.492164611816406, "[TT] Image Resolution of the Infrared Sensors = 6688 x 2500 pixels"]
-[10.909440040588379, 10.099116325378418, "[TT] Data Collection Upgrade of the Alpha Magnetic Spectrometer - 02 (AMS-02) = Needed"]
-[4.454079627990723, -0.22402873635292053, "[TT] Arrival Year of the Nauka mini-research module = 2021"]
-[8.35104751586914, 2.5458285808563232, "[FF] Nominal Mission Focus of the THEMIS = Time line of macroscale interactions during substorm onsets"]
-[5.359380722045898, 2.790342330932617, "[TT] Operator of the Hinode = JAXA/NASA"]
-[13.594590187072754, 6.635222434997559, "[TT] Average Payload Power of the QuikTOMS spacecraft = 107 W"]
-[8.159123420715332, -1.002630591392517, "[FF] Purpose of the ICESat-2 = Make detailed global elevation measurements, including over Earth's frozen regions"]
-[8.384318351745605, 7.700466632843018, "[TT] Number of Detectors of the Focal Plane Module = ~500 multispectral, 1000 panchromatic"]
-[9.406529426574707, -1.7044683694839478, "[TT] Orbital Altitude of the Swarm-A (Alpha) = \u2264 460 km"]
-[5.446215629577637, 6.353658676147461, "[TT] SDRAM Mass Storage of the PIC = 10 GByte"]
-[10.023236274719238, -1.5239863395690918, "[TT] Inclination of the IBEX = 11\u00ba"]
-[8.783428192138672, 8.269073486328125, "[TT] MTF of the WPM = > 0.65 at 38.5 lp/mm"]
-[7.6304097175598145, 6.51533317565918, "[TT] Scan Mode 6 (Super Flex Mode) of the ABI = 10 minutes"]
-[13.541058540344238, 5.7697577476501465, "[FF] Power Source of the ISS = Solar Panels"]
-[11.063997268676758, 7.706791877746582, "[TT] Swath Width for Regular Corresponding Mode of the Wide multi-look fine = 50 km"]
-[3.4738271236419678, 5.137750625610352, "[TT] Swath Width of the Multimode radar = 10 - 750 km"]
-[3.5617504119873047, 4.7572784423828125, "[TT] SAR Instrument of the RISAT-1 = Synthetic Aperture Radar"]
-[8.694501876831055, 3.4448602199554443, "[FF] Observation Modes of the Trace Gas Orbiter = Solar occultation, Nadir, Nightside"]
-[5.893105983734131, -0.556329607963562, "[TT] Mission Lifetime of the CHIPSat = One year"]
-[5.084530830383301, 3.24206280708313, "[TT] Manufacturer of the ICube-1 = PIST (Pakistan Institute of Space Technology)"]
-[7.897684097290039, 1.1857845783233643, "[FF] Age of the Tropical Rainfall Measuring Mission = 15 years"]
-[4.52133846282959, 1.026975154876709, "[TT] Anomaly Found of the IRU = February 7, 2006"]
-[3.027409553527832, 1.8356152772903442, "[FF] Image Capture Date of the Sentinel-2 = March 30, 2022"]
-[8.119868278503418, -1.265390157699585, "[FF] Pre-launch Activities of the ICESat-2 = Assessment of Arctic sea ice freeboard from photon-counting laser altimetry"]
-[8.65939998626709, 1.2488229274749756, "[TT] Spatial Resolution of the Aquarius = 150 km"]
-[10.652175903320312, 8.775806427001953, "[TT] 3 dB Footprint Size of the Channel = 38 x 23 km"]
-[4.8308424949646, 0.6648866534233093, "[TT] Launch Date of the MetOp-A = Oct. 19, 2006"]
-[7.671718597412109, 9.203676223754883, "[TT] Wavelength Range of the Band No 5 = 10.5 \u00b1 0.50 - 11.5 \u00b1 0.50 \u00b5m"]
-[9.341182708740234, 2.368558168411255, "[FF] Red Sprites of the ISUAL = 6.53%"]
-[13.862218856811523, 2.8040990829467773, "[TT] Launch Mass of the ADEOS = 3560 kg"]
-[4.901424884796143, 0.4370659291744232, "[TT] Launch Date of the SES-17 = 24 October 2021"]
-[5.799391746520996, 0.8906569480895996, "[FF] Mission Date of the ASPIICS = July 16-23, 2006"]
-[5.781701564788818, 7.416214942932129, "[TT] Preamplifier IP3 of the GimmeRF = +30 dBm"]
-[6.433676242828369, 1.774450659751892, "[FF] URL of the ANTRIX Corporation Limited = http://www.antrix.gov.in/irsonline/eosatellites.html"]
-[4.291189670562744, 0.3907502591609955, "[FF] Launch Date of the JJ-FAST = November 2016"]
-[8.970324516296387, 8.0094575881958, "[TT] Number of CCDs of the Focal Plane Assembly = 4"]
-[4.2192206382751465, 4.294250011444092, "[FF] Year of the Cospas-Sarsat rescues in 2021 = 2021"]
-[7.542396545410156, 5.414421081542969, "[FF] Components of the SWIR Camera System = Integrated detector cooler assembly, MCT photodiode array, ROIC, pulse tube cooler"]
-[13.332259178161621, 7.100133895874023, "[TT] Primary Power of the SPAN Sensor = Regulated 22 V from the SWEM"]
-[4.570478916168213, 2.877612590789795, "[TT] Headquarters of the EROS-B = Netherlands Antilles (Cayman Islands)"]
-[9.02122974395752, 6.453189849853516, "[TT] Image Segment Location of the CaSSIS = Margin of the South PLD"]
-[6.745416641235352, 4.983214378356934, "[FF] Usage of the IU = Only during launch and the initial phases of operation"]
-[6.899112224578857, -0.6818379759788513, "[TT] Orbital Plane Interval of the S/C = 19 minutes"]
-[10.673646926879883, 3.901787281036377, "[FF] Purpose of the CanX-2 = Demonstrate several technologies critical for the CanX-4/5 formation flying mission"]
-[3.750112295150757, -0.730750322341919, "[TT] Orbit of the CM1 = Low Earth Orbit (LEO)"]
-[6.313234806060791, 1.8192939758300781, "[FF] URL of the Jaan Praks = https://web.archive.org/web/20160304222738/http://tstc2014.to.ee/download/m5429b9e5144f8"]
-[6.393239974975586, 7.282740116119385, "[TT] Signal Type of the Output signal = Pulse"]
-[3.9871127605438232, 2.0000553131103516, "[TT] Launch Vehicle of the SOCRATES = H-IIA"]
-[6.436072826385498, 4.535717010498047, "[FF] Function of the KBR = Provides precise Satellite to Satellite Tracking (SST) in low-low orbit"]
-[5.385745048522949, 8.776615142822266, "[TT] Bandwidth of the Band 5 = 0.286 \u00b5m (16 cm -1)"]
-[9.279653549194336, 3.7747907638549805, "[FF] Function of the Magnetometer = Earth horizon sensors and sun sensors"]
-[9.067408561706543, 4.7721757888793945, "[FF] Temperature Sensors of the SEEDS-2 = Installed in 14 locations within the spacecraft"]
-[8.041962623596191, 3.0841400623321533, "[FF] CO2 Reactivity of the AIRS = Does not react with other gases in the atmosphere"]
-[9.585269927978516, 6.8327836990356445, "[TT] Spatial Resolution of the CERES on TRMM = Approximately 10 km"]
-[8.396721839904785, 8.222447395324707, "[TT] Spectral resolution of the FTS = 0.2 cm -1"]
-[3.3991260528564453, 5.070140361785889, "[TT] Frequency Band of the SAR = C-band"]
-[4.34475040435791, 7.805372714996338, "[TT] Uplink Frequency of the L-3 Communications Cadet UHF nanosatellite radio = 450MHz"]
-[8.949018478393555, 8.529472351074219, "[TT] Spectral Range of the Telescope = 400-1000 nm"]
-[8.016499519348145, 6.7650017738342285, "[FF] Data Acquisition Method of the CCD Detector = Rotating the imaging system, including the CCD, at a rated synchronization with a vertical charge transfer of the CCD detector"]
-[12.794618606567383, 7.631017208099365, "[TT] Electric Power of the Instrument = < 3 W"]
-[5.119484901428223, 8.361577987670898, "[TT] 84 MHz of the Bandwidth = -"]
-[6.122381687164307, 0.8338544368743896, "[TT] Imaging Date of the CaSSIS Camera = 7 June 2021"]
-[7.812984466552734, 5.105608940124512, "[FF] Function of the FRAM = Allows configurations, calibrations, and more to be modified easily without a lengthy software upload"]
-[4.873718738555908, 8.14097785949707, "[TT] Band of the LNA = 8400 to 8500 MHz"]
-[8.676849365234375, 7.728017807006836, "[TT] Detector Array Pixels of the PIC = 7490 pixels per line"]
-[4.389659881591797, 5.422618865966797, "[TT] Deployment Date of the GOMX-3 = October 5, 2015"]
-[8.122777938842773, 0.7395782470703125, "[FF] Unknown of the Asteroid Deflection Mission = Unknown"]
-[8.318391799926758, 8.985658645629883, "[FF] Wavelengths of the Herschel = 70 \u00b5m (blue), 160 \u00b5m (green) and 250 \u00b5m (red)"]
-[7.697226047515869, 1.4502440690994263, "[FF] Function of the Baffle = Blocks stray light from the Moon and the Earth limb"]
-[9.590578079223633, 1.392476201057434, "[TT] Visits per Day of the Pl\u00e9iades Neo constellation = Doubles the number of visits per day anywhere on Earth"]
-[5.316718101501465, 1.610709547996521, "[TT] Mission Status of the ALOS-2 = Operating nominally"]
-[3.213653564453125, 5.079217433929443, "[TT] Radiometric Resolution of the SAR = 5 bits"]
-[5.277920246124268, 2.1167757511138916, "[TT] Missions of the CEASE = TSX-5, STRV-1c, DSP-21"]
-[7.647752285003662, -0.4548923075199127, "[FF] Publication Date of the IceCube = 16 May 2018"]
-[5.564197063446045, 4.182297706604004, "[FF] Coverage of the EDRS = Wide European"]
-[6.4063239097595215, 4.926793098449707, "[FF] Requirement of the Data Processing System = Complex and robust"]
-[8.51503849029541, 3.886723041534424, "[FF] Monitored Particles of the SEISS = Geomagnetically trapped electrons and protons; electrons, protons, and heavy ions of direct solar origin; and galactic background particles"]
-[7.94246244430542, 8.93266487121582, "[TT] Wavelength of the VIS = 20 nm"]
-[8.598999977111816, 4.739473819732666, "[TT] Guide Stars Selection of the DPU = Up to 10 stars from the full OM image"]
-[4.914157867431641, 2.7232437133789062, "[FF] Centers of Expertise Locations of the YES2 = Fachhochschule Rhein/Ahr Campus, Remagen/Krefeld, Germany; University of Modena & Reggio Emilia, Italy; University of Patras, Greece; and Volgaspace (Samara State Aerospace University SSAU), Samara, Russia"]
-[6.376680850982666, 8.464299201965332, "[TT] Polarization Channels of the SGLI = 2"]
-[9.170494079589844, 7.5420098304748535, "[TT] Visible Band Resolution of the Imager = 1 km"]
-[8.32175064086914, 6.718069553375244, "[TT] Instruments of the THEOS-2 = Imager"]
-[6.825634002685547, 0.6761361360549927, "[TT] Operation Pause Date of the InSight = Around Oct. 7"]
-[7.688991546630859, 4.902210235595703, "[FF] Monitoring Devices of the IEM = Camera and accelerometer"]
-[11.442712783813477, 3.5095489025115967, "[TT] Main Structure of the Psyche spacecraft = Solar Electric Propulsion (SEP) Chassis"]
-[11.318648338317871, 5.848000526428223, "[FF] External Parts of the WISA Woodsat = Corner aluminum rails, metal selfie stick"]
-[6.401676654815674, 3.970942735671997, "[FF] ELEGANT Framework of the SpaceCube 2 = Unknown"]
-[7.029013633728027, 0.8310142159461975, "[FF] Mission Start Date of the Gravity Probe B = Unknown"]
-[6.7365593910217285, 6.420180797576904, "[FF] Listening Duration of the CPT = Entire transaction duration"]
-[6.182994365692139, 0.9100285172462463, "[TT] Agreement Date of the FormoSat-7/COSMIC-2 Satellite = October 2017"]
-[8.640417098999023, 2.691037654876709, "[TT] Measurement Height of Atmosphere of the ERIP = 0 - 55 km"]
-[6.81186580657959, 0.7447089552879333, "[TT] Safe Mode Entry Date of the InSight = 11 January 2022"]
-[8.787787437438965, 7.0513224601745605, "[FF] Resolution of the Imager = High"]
-[5.142723083496094, 3.1739866733551025, "[TT] Manufacturer of the Icarus-1 = Cranfield University"]
-[13.251266479492188, 5.246664524078369, "[TT] Solar Arrays Surface Area of the Kondor-E = 9.2m2"]
-[13.907770156860352, 3.0555567741394043, "[FF] Mass of the MEROPE = Unknown"]
-[5.24267053604126, 8.144062995910645, "[TT] Frequency Range of the IME_HF = 100 kHz \u2013 35 MHz"]
-[3.3886568546295166, 6.393270492553711, "[TT] Length of the Spin Plane Dipole Antenna = 90 m"]
-[5.676172733306885, 3.0211939811706543, "[TT] Managing Agencies of the DASS = NOAA, the USAF, and the USCG"]
-[6.8606133460998535, 1.5646238327026367, "[FF] Imagery Usage of the FormoSat-2 = Disaster monitoring, land-use (change) detection, environmental monitoring"]
-[5.819154262542725, -0.850527822971344, "[TT] Design Life of the Spacecraft = 7.25 years"]
-[10.205153465270996, 5.727382659912109, "[TT] Cooling Temperature of the CCD detector array = -65\u00baC"]
-[5.012463569641113, 0.4480901062488556, "[FF] Control Date of the QZS-1 = Feb. 22, 2017"]
-[10.189427375793457, -0.5152825713157654, "[TT] Altitude of the PhoneSat-2.5 1U CubeSat = ~400 km"]
-[5.926071643829346, 0.8669961094856262, "[TT] Image Capture Date of the Small Monitor Camera (CAM-H) = 14 August"]
-[9.099954605102539, 5.289547443389893, "[TT] Attitude Accuracy of the SAST-5000 = 3 arcsec"]
-[9.662555694580078, 1.3860327005386353, "[TT] Launch Date of the Pl\u00e9iades = Dec. 17, 2011"]
-[8.831746101379395, 3.271406412124634, "[FF] Observation Target of the EUV Imager = Plasmasphere"]
-[4.830493450164795, 0.06261058151721954, "[TT] End of Life Date of the Genesis = September 8, 2004"]
-[7.198314189910889, 4.838140487670898, "[TT] Location of the Avionics Stack = Below the laser"]
-[4.272337913513184, 2.736328125, "[TT] Location of the GKOU = Kourou French Guyana"]
-[11.405787467956543, 5.89649772644043, "[FF] Material of the Cold Plates = Stainless steel channelling enclosed in an aluminum casting"]
-[6.380105018615723, 1.9362664222717285, "[FF] URL of the VRSS-1 = http://cn.cgwic.com/VRSS-1/english/satellite.html"]
-[6.181764602661133, 4.2822160720825195, "[FF] Responsible Teams of the ADCS = Mission Operations (health monitoring and reporting), ADCS team (performance maintenance)"]
-[5.4801716804504395, 0.7592636346817017, "[FF] Public Listing Date of the Astra = July 1"]
-[8.898387908935547, 0.968374490737915, "[FF] Purpose of the Parker Solar Probe = Answer questions about solar physics"]
-[7.224768161773682, 1.610764980316162, "[FF] Reproduction of the Bdelloids = Produce offspring from unfertilized eggs"]
-[10.623807907104492, 7.344656467437744, "[TT] Swath Width of the Instrument = 35 km (nominal mode)"]
-[8.194023132324219, 2.1592702865600586, "[FF] Science Objectives of the TROPICS = Relate the retrieved environmental moisture measurements to coincident measures of storm structure (including size) and intensity"]
-[6.8130574226379395, -0.6749023795127869, "[TT] Orbit MLST of the Envisat = 22:00 ANX \u00b1 5 minutes"]
-[6.131383895874023, 6.189581871032715, "[TT] Onboard Time Code of the SSRNI = Yes"]
-[6.317625522613525, 4.288082599639893, "[FF] Operations Concept of the Spacecraft = Unattended with distributed science operations"]
-[7.9750471115112305, 1.8507249355316162, "[FF] Level 3 Evapotranspiration of the ECOSTRESS = 2 months after Level 2 data products are available"]
-[8.467354774475098, 3.246281385421753, "[TT] Altitude Range of the Atomic Oxygen (AO) Density Measurement Device = 180-200 km"]
-[9.498797416687012, 6.1677093505859375, "[TT] Incidence Angle Range of the TopSAR narrow = 25\u00ba - 45\u00ba"]
-[3.8399851322174072, 6.931351184844971, "[TT] Polarization of the TEC Antennas = Right, circular"]
-[7.683182716369629, 0.6636593341827393, "[FF] Measurement Goal of the Lunar Flashlight = Identify locations where water ice is present at the surface of the Moon as a frost"]
-[3.3592193126678467, 4.994935035705566, "[TT] Operating Mode of the SAR = HRS FRS-1 FRS-2 MRS/CRS"]
-[6.959721088409424, 1.4724775552749634, "[FF] Demonstration Date of the Space Weather Observation System = August 18, 2010"]
-[9.30612850189209, 10.736059188842773, "[TT] Polarization of the ICI-10 = V"]
-[8.19861888885498, 6.733796119689941, "[TT] Type of the MAESTRO = Dual channel optical spectrometer"]
-[6.221560001373291, 7.035561561584473, "[TT] Attitude Data Sampling Rate of the Satellite = 1 sample every 10 minutes"]
-[4.761263370513916, 7.152499675750732, "[TT] Downlink, uplink of the RemoveSat = 2 Mbit/s (S-band), 19.2 kbit/s"]
-[7.089373588562012, 1.225390911102295, "[FF] Discovery Date of the Spitzer = 24 June 2020"]
-[13.474117279052734, 2.8267786502838135, "[TT] Mass (Wet) of the Satellite = \u2264 3200 kg"]
-[14.157087326049805, 3.292807102203369, "[TT] Mass of the OBCom module = 8 gram"]
-[13.798962593078613, 2.688755750656128, "[TT] Launch Mass of the General spacecraft parameters = 123.7 kg"]
-[9.769689559936523, 2.696563482284546, "[FF] URL of the NanoRacks Airlock Module = http://nanoracks.com/wp-content/uploads/NanoRacks-Airlock-Presentation.pdf"]
-[8.484658241271973, 3.142941474914551, "[FF] Average Concentration of the Ozone Layer = 220 Dobson Units"]
-[11.800228118896484, 0.08474655449390411, "[TT] Stellar Spectral Types of the TESS = F5 to M5"]
-[14.246519088745117, 3.0787439346313477, "[TT] Mass of the Tyvak-0171 = 138 kg"]
-[9.897790908813477, 1.743344783782959, "[FF] Time to be Pulled towards the Black Hole of the Earth-sized clump of matter = About a day"]
-[6.3004560470581055, 4.806017875671387, "[FF] Function of the ISSAC SOC = Convert these requests into specific sets of commands for uplink to ISSAC"]
-[8.672877311706543, 4.591275691986084, "[TT] Slope Error of the Aeolus = 0.7%"]
-[11.693122863769531, 6.824657440185547, "[TT] Energy Range of the ART-XC = 5 to 30 keV"]
-[3.5677356719970703, 6.448662757873535, "[FF] Deployed Antenna Size of the IAE Experiment = Roughly the size of a tennis court"]
-[5.268683910369873, 1.514970064163208, "[TT] Operating Status of the SMOS mission = Nominally"]
-[10.436640739440918, 2.281087875366211, "[FF] Observation Mode of the IXPE = Pointed viewing of known X-ray sources"]
-[7.968185901641846, 9.026739120483398, "[TT] Wavelength Channels of the TOMS = Six"]
-[10.136752128601074, 1.700520396232605, "[TT] Number of Detected Sources of the eROSITA = About one million"]
-[10.661873817443848, 5.2401957511901855, "[FF] Background of the CuPID = Due to energetic particles striking the detector"]
-[13.326706886291504, 6.9094014167785645, "[TT] Control Method of the PCU = PPT (Peak Power Tracking)"]
-[3.371955633163452, 5.002499580383301, "[FF] Instrument Calibration of the SAR = Performed in HF part of the equipment"]
-[9.840557098388672, 2.6702115535736084, "[TT] Small Satellite Deployments of the NanoRacks = 217th overall"]
-[9.238578796386719, 8.275321960449219, "[TT] Number of Elements of the Collecting Optics = 8"]
-[11.889273643493652, 4.732641220092773, "[TT] Mass of the PCU = Low"]
-[5.546286106109619, 4.544519901275635, "[FF] Coverage of the 5G Network = Global, always-on network"]
-[7.931309223175049, 7.188545227050781, "[TT] Interferometer Throughput of the FTS = Factor of two higher than for the M-P"]
-[10.633152961730957, 1.5490833520889282, "[FF] Quantity of the Black Hole Detector = > 170000"]
-[7.218581676483154, 7.210829257965088, "[FF] Photon Detection of the GLAS = Thousands of photons per laser fire"]
-[8.163331985473633, 7.289681911468506, "[TT] Imaging System of the NewSat = Visible and near-infrared spectrum"]
-[7.873762130737305, 7.30112361907959, "[TT] Data Rate of the Imager = ~3.9 Mbit/s"]
-[10.969978332519531, 4.208093166351318, "[FF] Status of the Vacuum Valve and Ion Gage = Will be removed"]
-[4.708237171173096, 1.8887587785720825, "[TT] Launch Date of the Eutelsat 172B = June 1, 2017"]
-[5.519096374511719, -1.8487929105758667, "[TT] Development Location of the KOMPSAT-1 = Taejon"]
-[5.910777568817139, 1.345861792564392, "[FF] Publication Year of the Satellite = 1996"]
-[13.927196502685547, 2.9922823905944824, "[TT] Total mass of assembly of the STRV-1d DHS = 1.2 kg"]
-[4.842268466949463, 0.2887616455554962, "[TT] Deployment Date of the RemoveDebris satellite = 20 June 2018"]
-[7.222513198852539, 2.7591419219970703, "[TT] Start Date of the Methane Leak = 4 July 2020"]
-[7.934850692749023, -0.31199899315834045, "[TT] Location of the High-Latitude Cold-Season Snowfall Campaign = Ontario, Canada"]
-[3.672260046005249, 5.0816450119018555, "[FF] Availability of the Matera ground station = For L-band SAR imagery downlinks"]
-[9.414141654968262, 6.189548015594482, "[TT] Viewing Angle of the SCIAMACHY = 55\u00ba"]
-[9.863126754760742, 4.449972152709961, "[FF] Components of the ADCS = Three magnetorquers, a single momentum wheel, a translation stage"]
-[11.977754592895508, 6.4873127937316895, "[TT] Neutrino Energy of the Glashow Resonance = 6.3 PeV"]
-[10.341689109802246, 7.999945163726807, "[TT] Telescope Diameter of the TRACE instrument = 30 cm"]
-[7.843982219696045, -0.6274440884590149, "[TT] Orbit of the CryoSat = Polar"]
-[7.53902530670166, 2.0131845474243164, "[FF] Band 6 of the Landsat TM = Plant heat stress, thermal mapping, soil mapping"]
-[5.902135372161865, -0.7428922057151794, "[TT] Mission Life of the Telescope = 11 years for fuel"]
-[7.091119289398193, 5.085291385650635, "[FF] Voltage Conversion of the LCT instrument = Yes"]
-[5.707974433898926, 7.136719703674316, "[TT] Information Rate of the OBP (Onboard Processor) = 5.6 kbit/s (voice)"]
-[4.834681034088135, 6.206024646759033, "[FF] Operation Environment of the Frontier Radio = Very harsh environment"]
-[10.14639663696289, 3.243363618850708, "[FF] EMC Design of the CubeSats = Not designed to be as clean as possible"]
-[4.78771448135376, 7.152914047241211, "[TT] Data Download Rate of the X-band = 60 Mbit/s"]
-[3.8717269897460938, 6.534518718719482, "[TT] Antenna Type of the SPS = Micro-strip patch antenna"]
-[4.756453514099121, 5.615671634674072, "[FF] Zero Doppler Calibration of the Overall System = Use of Tx leak signal"]
-[5.302148342132568, 5.627246379852295, "[TT] Flash Memory of the Namuru V3.2 GPS Receiver = 1 MB"]
-[13.446770668029785, 6.922247886657715, "[TT] Power of the GCOM-W1 = 4.05 kW at EOL (End of Life)"]
-[3.199225425720215, 1.681344747543335, "[TT] Data Processing Time to Level 1 Image of the Sentinel-1A = 13 minutes"]
-[7.98016357421875, 6.284971714019775, "[TT] Type of the TANSO-FTS = Thermal and Near-Infrared Sensor for carbon Observation-Fourier Transform Spectrometer"]
-[9.000347137451172, 6.096267223358154, "[TT] MTF of the NEMO-HD = 0.10"]
-[14.023122787475586, 3.206090211868286, "[TT] Mass of the GCOM-W1 = ~1990 kg"]
-[6.8677592277526855, 6.129464626312256, "[TT] Operation Mode of the GEMS = Low-voltage mode"]
-[9.794366836547852, 7.45751428604126, "[FF] Ground Sample Distance of the GSD = Pan: 7.5 m, MS: 15 m"]
-[7.98538875579834, 3.083972692489624, "[FF] Measures of the WAF-P = Vertical column densities of CO2 and CH4"]
-[7.417734622955322, 1.1570326089859009, "[FF] Publication Date of the OceanSODA-ETHZ = 02 Mar 2021"]
-[4.863814830780029, 3.026751756668091, "[FF] Manufacturer of the ICESat-2 spacecraft = Orbital ATK"]
-[4.964261054992676, 1.2278834581375122, "[FF] Mission Success Confirmation Date of the GIOVE-A = April 2, 2008"]
-[5.730158805847168, 3.2743349075317383, "[TT] Number of Satellites of the WorldView Legion satellites = 6"]
-[5.859993934631348, 3.538036346435547, "[FF] Production Rate of the Factory = About one satellite per week"]
-[9.291200637817383, 4.911703109741211, "[FF] Point-Spread-Function Hold Requirement of the Attitude System = Within 3 pixels of the original point locations"]
-[3.2953238487243652, 6.489614486694336, "[TT] Antenna Diameter of the VSAT = 2.4 m"]
-[6.4838948249816895, 7.614485740661621, "[TT] Data Quantization of the Hyperion = 12 bit"]
-[5.451889514923096, 7.122036933898926, "[TT] Telemetry Data Frequency of the DRS = 70 MHz"]
-[8.575250625610352, 6.106510639190674, "[TT] Absolute Measurement Error of the OVM = < 0.5 nT"]
-[4.221335411071777, 3.9132771492004395, "[TT] Comments of the L6 (LEX) = Compatibility with Galileo E6 signal"]
-[6.544572830200195, 2.469142198562622, "[FF] Testing Status of the Euclid = Thermal qualification tests completed, mechanical vibration tests upcoming"]
-[9.037487983703613, -1.187243938446045, "[TT] Operating Position of the EDRS = 9\u00ba longitude over Europe"]
-[7.655014514923096, 3.6302430629730225, "[FF] Instrument of the Aeolus satellite = Space Doppler wind lidar"]
-[9.072630882263184, 7.455811023712158, "[TT] Resolution of the Camera 1 = 0.8 km/pixel"]
-[7.871047496795654, 3.397970676422119, "[FF] Mission of the Medium Energy Neutral Atom (MENA) Imager = IMAGE"]
-[7.73227596282959, 9.112284660339355, "[TT] Wavelength Range of the PH4 = 600 to 900 nm"]
-[5.4339118003845215, 3.1932201385498047, "[FF] Service Prime Capacity of the Surrey Satellite Technology Limited = Lunar services brand SSTL Lunar"]
-[5.734264850616455, -0.8685164451599121, "[TT] Design Life of the ADEOS = 3 years"]
-[5.259115219116211, 2.378375768661499, "[TT] Agency of the Enxaneta = Sateliot"]
-[3.9624884128570557, 6.744434833526611, "[TT] Operating Band of the VDES Antenna = VHF maritime band"]
-[10.173776626586914, 1.016204833984375, "[TT] Distance from Earth of the NGC 3603 = 20,000 light-years"]
-[9.754895210266113, -0.3827216923236847, "[TT] Altitude of the ANUSat = 550 km"]
-[13.92883586883545, 7.208095550537109, "[TT] Current of the Voltage 5 = 525"]
-[5.407811164855957, 0.8803991079330444, "[FF] Satellite Launch Date of the Capella Space And Rocket Lab = Not Provided"]
-[4.771357536315918, 7.490267276763916, "[TT] Data Transmission Rate of the RF Communications = 1.2 kbit/s for the UHF band"]
-[8.81258773803711, 7.641788959503174, "[TT] Photodetector Pixel Size of the Optical Head = 5.2 \u00b5m x 5.2 \u00b5m"]
-[5.286613464355469, 7.033369064331055, "[TT] Downlink Data Rate of the Telemetry, Tracking, and Command (TT&C) = 6 Mbit/s"]
-[8.448027610778809, 8.190159797668457, "[FF] Unapodized Spectral Resolution Requirement of the CrIS Instrument = I/(2L)"]
-[8.141757011413574, -0.6677029132843018, "[FF] Additional Role of the CryoSat-2 = Measure the height of the surface of the sea"]
-[12.0401611328125, -0.24080389738082886, "[TT] Duration of All Sky Survey of the SRG = 4 years"]
-[3.8358852863311768, 1.9436817169189453, "[TT] Vehicle of the SpaceX = Falcon 9"]
-[10.515819549560547, 2.2421412467956543, "[FF] Integration Times of the X-ray images = User-defined or variable"]
-[14.215502738952637, 3.3123321533203125, "[TT] Mass of the OBC = 129 g"]
-[6.687221050262451, 5.860109806060791, "[FF] Conference Date of the NASA Optical Communications and Sensor Demonstration Program = Aug. 4-9, 2018"]
-[8.324462890625, -0.6076319813728333, "[TT] Ice Cover of the Landsat 8 = 82 percent"]
-[10.052227020263672, 4.725773811340332, "[TT] Chopper Wheels Frequency of the SBUV = 25 Hz"]
-[13.640549659729004, 2.7811179161071777, "[TT] Total Mass of the DSP satellites = 330 kg at launch"]
-[7.754678249359131, 9.156373977661133, "[TT] Wavelength Range of the Band 4 = 1.371-1.386 \u00b5m"]
-[3.8575446605682373, 6.462690830230713, "[TT] Antenna Offset of the SMMR = 42\u00b0 from the nadir"]
-[8.137799263000488, 4.420340538024902, "[FF] Function of the Electromagnetic Calorimeter = Measure the energy of particles interacting in its sensitive volume and image the shape of these interactions"]
-[12.494401931762695, 6.654489994049072, "[FF] Stacks of the Proton Monitor Las Dos Torres = \u2018dark\u2019 and \u2018light\u2019 towers"]
-[3.5243282318115234, 5.213247299194336, "[TT] Hardware Location of the L-band Radar = JPL"]
-[4.987595558166504, 3.292630910873413, "[TT] Manufacturer of the RTAFSAT-1 = Royal Thai Air Force"]
-[9.320425987243652, 3.2911794185638428, "[FF] Science Objectives of the CuPID = Answer fundamental questions in plasma physics and space weather"]
-[6.580779075622559, 4.6084442138671875, "[FF] Conference Presentation of the GPS Navigation = 22nd International Technical Meeting of The Satellite Division of the Institute of Navigation (ION GNSS 2009)"]
-[5.86627197265625, -1.1027538776397705, "[TT] Exceeded Design Life of the QuikSCAT = Yes"]
-[5.032473564147949, 3.328193426132202, "[TT] Manufacturer of the Suomi-NPP = Ball Aerospace and Technologies Corporation (BATC)"]
-[2.9107301235198975, 4.464341640472412, "[TT] Daily Data Acquisition Volume of the PALSAR-2 = 800 GB"]
-[5.586655139923096, -0.37074437737464905, "[TT] Upper Stage Deployment Time of the Rocket = More than a half-hour"]
-[8.539831161499023, 0.3382788598537445, "[FF] Depth of the Lake Balkhash = Around 6 m"]
-[10.69424819946289, 4.061097621917725, "[TT] Attitude Control of the CanX-4&5 = 1.0\u00ba"]
-[6.805140018463135, -0.4050532579421997, "[FF] Lag Period of the Pelican Satellites = Less than two hours"]
-[6.00581693649292, 6.540469646453857, "[FF] Configuration of the \u00b5SDTN transponder = Core transponder on the left; diplexer, RF switch and test couplers on the right"]
-[10.886054039001465, 5.887735366821289, "[TT] Effective Area of Main CsI Crystal of the GRS = 118 mm"]
-[4.9889678955078125, 7.432556629180908, "[TT] Noise Figure of the Uplink Receiver = < 4 dB"]
-[10.354350090026855, 4.513922214508057, "[TT] Type of the Reaction Wheels = Commercial"]
-[10.73672866821289, 1.4148533344268799, "[TT] Mass of the Giant Molecular Clouds = Up to 10 million times the mass of the Sun"]
-[10.987272262573242, 2.9419565200805664, "[TT] Size of the Astrocast's Nanosatellites = 10x10x10 centimeters"]
-[7.402547836303711, 3.0403659343719482, "[FF] Cryogenic Liquid Methane Transfer of the RRM3 = Objective"]
-[10.904873847961426, 5.605894565582275, "[FF] Test Article of the Heat Shield = Water impact testing"]
-[5.095765590667725, 3.1819028854370117, "[TT] Manufacturer of the Satellite = Nanyang Technological University"]
-[5.510431289672852, 1.8797438144683838, "[FF] Deployment Status of the Aireon = Closer to Complete"]
-[9.713878631591797, 0.35147830843925476, "[TT] Minimum Formation Distance of the PROBA-3 = 25 m"]
-[7.034796237945557, 1.3656538724899292, "[TT] Observation Type of the Spitzer = Infrared"]
-[5.065769195556641, 3.3470168113708496, "[TT] Provider of the CAVIS = BATC (Ball Aerospace and Technologies Corporation)"]
-[14.656407356262207, 6.671318054199219, "[TT] Capacity of the NiCd Battery = 4 Ah"]
-[10.803581237792969, 3.476381540298462, "[FF] Size of the SporeSat = 3U CubeSat"]
-[5.541800022125244, -1.884329080581665, "[TT] Operation Year of the KOMPSAT-3 = 2014"]
-[4.45002555847168, -0.21131151914596558, "[TT] Planned Launch Date of the Nauka = 15 July 2021"]
-[4.870283126831055, 8.462202072143555, "[TT] Frequency Channels of the AMR-2 = 18.7 GHz, 23.8 GHz, 34 GHz"]
-[7.708284378051758, 5.828473091125488, "[FF] Processing Steps of the Image Processing Software = Interleaving, Interpolation, Restoration"]
-[3.84106707572937, -1.0841783285140991, "[TT] Jacobi Constants Range of the Quasi-Halo Orbits = Cj = 3.04 to Cj = 3.1613263"]
-[8.173693656921387, -1.078741431236267, "[TT] Water Level Height Uncertainty of the ICESat-2 = Roughly 4 inches (10 cm)"]
-[7.941488742828369, 8.657015800476074, "[TT] Spectral Bands of the HyperScout = 400-600 nm"]
-[9.10516357421875, 7.734560966491699, "[TT] MS (Multispectral) of the Medium resolution = 0.51-0.58 \u00b5m (green)"]
-[9.071268081665039, 4.460053443908691, "[TT] Mode of the Solar Panels = Nominally in sun-pointing mode"]
-[7.052838325500488, 3.495995283126831, "[FF] URL of Paper of the PROBA-3 = http://www.sffmt2013.org/PPAbstract/4069p.pdf"]
-[4.639970302581787, 5.350331783294678, "[FF] Signal Overlap of the GPS Receiver = ALOS-2 SAR frequency"]
-[8.643677711486816, 1.9946156740188599, "[FF] Changes of the Neutral winds = Sluggish"]
-[8.78412914276123, 6.335033893585205, "[TT] Position Accuracy of the ALT Experiment = 0.1 m"]
-[6.9110307693481445, 7.73041296005249, "[TT] Main Reflector Size of the MIS Instrument = 1.8 m"]
-[7.91314172744751, 9.044328689575195, "[TT] Wavelength Range of the OMI = 270 nm to 500nm"]
-[8.122714042663574, 4.910362243652344, "[FF] Noise Temperature of the System = Unknown"]
-[13.389455795288086, 7.382410526275635, "[TT] Power of the Power = 1466 W"]
-[10.911880493164062, 0.8542768955230713, "[TT] Inter-spacecraft Separation of the LISA = 2.5 million km"]
-[11.441071510314941, 5.758657932281494, "[FF] Concepts Investigated of the ALBus = Piston design, Collet design"]
-[8.458072662353516, 3.9605796337127686, "[FF] Current Dependence of the Sensor = Linear dependence on the oxygen partial pressure"]
-[10.82343864440918, 7.4348344802856445, "[TT] Swath Width of the ALOS-3 = 50 km"]
-[6.453373432159424, 1.2887136936187744, "[FF] Mission of the CryoSat = Earth Explorer Opportunity Mission-1"]
-[6.1970014572143555, 4.4919657707214355, "[TT] Subsystems of the AVUM = GNC (Guidance Navigation and Control), SAS (Electric Safeguard Subsystem), TMS (Telemetry Subsystem)"]
-[9.008069038391113, 5.189043045043945, "[TT] Sensor Volume of the R3 spacecraft = Less than 1.5U"]
-[9.863329887390137, -0.345441073179245, "[TT] Orbit Altitude of the STARE Satellite = 700 km"]
-[5.607934474945068, 6.695703029632568, "[TT] Data Collected of the eROSITA = 165 GB"]
-[7.018219470977783, 4.647057056427002, "[FF] Parameter of the Cassini VIMS = Value"]
-[8.995494842529297, 5.344895362854004, "[FF] Pointing Ability of the ASTERIA = Coarse pointing control"]
-[10.050475120544434, -1.556893229484558, "[TT] Orbit Inclination of the ADEOS-II = 98.62\u00ba"]
-[11.516057014465332, 4.958011150360107, "[TT] Diameter of the MCP = 40 mm"]
-[9.662322998046875, 1.4042139053344727, "[TT] Daily Acquisition Capacity of the Pl\u00e9iades Neo = More than double"]
-[14.672419548034668, 6.741899490356445, "[TT] Battery Configuration of the EPS = 5 parallel sets of 2-series batteries"]
-[4.711357593536377, 3.7505149841308594, "[TT] Provider of the European Ground Motion Service = European Union"]
-[6.876711845397949, 4.760735034942627, "[FF] Lack of Attitude Control of the \u00d8rsted = Resulted in an almost total lack of GPS timing information"]
-[9.726171493530273, 7.041895389556885, "[TT] Resolution of the LISS-4 = 6 m"]
-[4.397937297821045, 2.924713134765625, "[FF] Locations of the Test Sites = La Crau test site (43.56\u00baN, 4.86\u00baE), Libya 1 (24.42\u00baN, 13.35\u00baE), Libya 2 (25.05\u00baN, 20.48\u00baE), Libya 3 (23.15\u00baN, 23.1\u00baE), Mauritania 2 (20.85\u00baN, 8.78\u00baW)"]
-[3.1995997428894043, 5.076981067657471, "[TT] Spotlight High Resolution (HS) Image Size of the TSX-SAR = 5-10km x 5km"]
-[5.673327445983887, 1.0107508897781372, "[FF] Calibration Date of the Resourcesat-2A = July 12-19, 2016"]
-[10.263574600219727, 5.206356048583984, "[FF] Purpose of the Heat Transfer Host = Investigate convection and heat transfer through air and liquids"]
-[8.475071907043457, 7.053565979003906, "[TT] Spatial Resolution of the ABI = Twice the current GOES Imagers"]
-[7.8582940101623535, -0.9392566084861755, "[FF] Technical Status Summary of the ICESat-2 = Sept. 1, 2016"]
-[11.41401481628418, 4.3688130378723145, "[TT] Size of the VisionCube-1 = 2U"]
-[7.743607521057129, 8.383031845092773, "[TT] SWIR Bands of the GLI = 6"]
-[10.488237380981445, 2.300161838531494, "[FF] Operating Wavelengths of the X-ray Navigation = Ground cannot be seen"]
-[7.208715915679932, 2.770825147628784, "[FF] Phase 1 Date of the MethaneAIR = October and November 2019"]
-[8.698652267456055, 3.6172187328338623, "[FF] Objective of the SOVA = Measurement of the solar constant, its variability and its spectral distribution"]
-[5.038687705993652, 3.351973533630371, "[TT] Manufacturer of the DSAC = SST-US"]
-[6.824399471282959, 7.774294853210449, "[TT] Reflector Diameter of the Antenna subsystem = 2.5 m"]
-[13.324859619140625, 7.584407329559326, "[TT] SSPA Output Power of the USAT (Ultra Small Aperture Terminal) = 20 W"]
-[5.957571029663086, -0.40114736557006836, "[TT] Operation Duration of the STRV-1a = 4 years"]
-[9.564224243164062, 7.070371150970459, "[TT] Spatial Resolution of the SMMR = Ranged from 22 km at 37 GHz to 100 km at 6.6 GHz"]
-[8.340215682983398, 1.4484010934829712, "[TT] Quantity of the TAO/Triton = ~70 with salinity"]
-[6.10198450088501, 0.7961091995239258, "[TT] Image Capture Date of the CaSSIS = 18 May 2018"]
-[11.900237083435059, 3.0836663246154785, "[TT] Delta V of the Propulsion Subsystem = 20 m/s"]
-[8.53559684753418, 1.4828813076019287, "[FF] Development and Integration of the Aquarius Scatterometer Processor/Control Electronics = Unknown"]
-[8.568353652954102, 1.9773348569869995, "[TT] Absolute accuracy of the Ocean surface wind speed = \u00b12 m/s"]
-[7.955812454223633, 8.308741569519043, "[TT] Sensitivity of the MWIR (Midwave Infrared) = NEDT \u2264 0.7 K"]
-[9.162534713745117, -1.3042179346084595, "[TT] Orbit of the Spacecraft = GEO (Geostationary Orbit)"]
-[6.651068687438965, 5.192387580871582, "[FF] Components of the Spacecraft Emulator = Flight representative STRx Transceiver, OBC emulator development board, Antennas"]
-[7.701835632324219, 8.68884563446045, "[TT] Spectral Bands of the IRS = 4"]
-[6.872985363006592, 0.6610119938850403, "[TT] Mission Status of the Kepler Space Telescope = Retired"]
-[9.128061294555664, 5.559170246124268, "[TT] Gimbal Tracking of the SOTA = \u00b1100 \u00b5radians"]
-[6.192100524902344, 5.980372428894043, "[TT] Performance of the Avcoat = Excellent"]
-[5.384712219238281, 1.1553289890289307, "[FF] Date of the WCOM = November 20-21, 2014"]
-[7.880198955535889, 4.665795803070068, "[FF] Relative to the spacecraft body axis frame of the IMF (Instrument Mounting Frame) = -"]
-[10.059544563293457, 3.158243179321289, "[FF] Mission of the Cubesats = Intelligence, surveillance, and reconnaissance"]
-[6.268083572387695, 3.071927309036255, "[FF] Tasking of the BlackSky Spectra = Available"]
-[3.9084742069244385, 6.5125956535339355, "[TT] Type of the Antennas = Microstrip"]
-[11.373675346374512, 4.327676773071289, "[TT] Size of the CIRAS = 6U"]
-[3.730501413345337, -0.7460862398147583, "[TT] Orbit of the LIBRA = Low Earth Orbit (LEO)"]
-[9.206655502319336, 5.169565677642822, "[FF] Pointing and Stabilization System of the ExoplanetSat = Sub-arcsecond"]
-[6.4605231285095215, 2.9357569217681885, "[FF] Image Source of the NOAA-20 = VIIRS"]
-[5.022608757019043, 2.8188095092773438, "[FF] Owner of the Meteosat = EUMETSAT"]
-[5.090162754058838, 1.001227855682373, "[FF] Health Status of the Hitomi = Not Confirmed"]
-[4.669920444488525, 7.142216205596924, "[TT] Uplink of the Miniaturized X-band transponders = 1 kbit/s"]
-[5.456579685211182, 6.298952102661133, "[TT] Capacity of the 768 Mbit = 768 Mbit"]
-[8.260820388793945, 4.1712141036987305, "[FF] Operation Mode of the CAPI instrument = Moon observation"]
-[10.234029769897461, 8.396965980529785, "[TT] Effective Pupil Diameter of the TESS Camera = 100 mm"]
-[9.957991600036621, 0.0013239351101219654, "[TT] Orbit Altitude of the GRACE-FO satellites = Around 500 km"]
-[6.659749984741211, 8.044069290161133, "[TT] Noise Figure of the TOTEM SDR = 2 dB"]
-[6.701798915863037, 3.7083516120910645, "[FF] Purpose of the Urine Processing Assembly (UPA) Distillation Assembly = Used for urine distillation, processing, and future use"]
-[4.350400447845459, 2.5029282569885254, "[TT] Launch Site of the ART-XC = Baikonur in Kazakhstan"]
-[13.438867568969727, 2.999483346939087, "[TT] Bus Mass of the Spacecraft = 180 kg"]
-[7.916993141174316, 1.8419815301895142, "[FF] Data of the GOCE = Unique models of the Earth's gravity field and of its equipotential reference surface, as represented by the geoid"]
-[8.614278793334961, 4.763730049133301, "[FF] Sensitivity of the Instrument = Detects an Earth-size transit of an mv=12 G2V star at 4 \u03c3 in 6.5 hours of integration"]
-[5.106111526489258, 8.421300888061523, "[TT] Bandwidth/Passband of the 2 = 400 MHz"]
-[8.610296249389648, 9.216386795043945, "[FF] Spectral Ranges of the TANSO-CAI = Ultraviolet (UV), visible, and SWIR"]
-[9.38747501373291, 0.9764079451560974, "[TT] Distance from Jupiter's Cloud Tops of the Juno = 2,100 miles (3,400 km)"]
-[8.052594184875488, 7.806975841522217, "[TT] Detector Channels of the REM = 16"]
-[8.927000045776367, 6.696995735168457, "[TT] Resolution of the SSM = 2 nT"]
-[10.26735782623291, 5.771390438079834, "[TT] Temperature of the Primary Sensor = >1300\u00baC"]
-[6.591557502746582, 4.950377464294434, "[FF] Bus Subsystems of the INSAT-3D = Thermal Control Subsystem (TCS), Bus Management Unit (BMU), Electrical Propulsion Subsystem (EPS), Attitude and Orbit Control Subsystem (AOCS ), Liquid Apogee Motor (LAM) and Radio Frequency (RF) communications"]
-[7.465980052947998, 2.0941317081451416, "[FF] Full Name of the FLORIS = FLuORescence Imaging Spectrometer"]
-[5.597350597381592, 6.26629114151001, "[TT] Data Storage of the Instrument = On the spacecraft"]
-[5.7990241050720215, 3.6596105098724365, "[TT] Funds Needed of the Sateliot IoT Nanosatellite Constellation = $35 million to deploy an initial 16 satellites by the end of 2022"]
-[6.042449474334717, 1.7787271738052368, "[FF] Dosimetric Results of the Eureca = Unknown"]
-[10.265286445617676, 8.037880897521973, "[TT] Aperture Diameter of the Telescope = 0.7 m"]
-[7.834914684295654, 3.7245569229125977, "[FF] Type of the Imager = Earth radiation budget radiometers, Space environment, Magnetic field, Other, Atmospheric chemistry, Communications, Data collection, Hyperspectral imagers, Gravity instruments"]
-[8.968046188354492, 8.18070125579834, "[FF] Component of the Ring Imaging Cherenkov Counter (RICH) = Unknown"]
-[5.321206569671631, 6.938717365264893, "[FF] Speed of the 5G Network = Faster than current data speeds"]
-[6.1775803565979, 5.1470489501953125, "[FF] Function of the Microprocessor = Grouping the measurements into a packet and sending them over the I2C bus to the OBC for downlink transmission"]
-[4.36826229095459, 2.403325080871582, "[TT] Launch Site of the HORYU-2 = TNSC (Tanegashima Space Center), Japan"]
-[9.242334365844727, 6.115753650665283, "[TT] Angle of Incidence of the Sensor = 53.1\u00ba"]
-[8.903999328613281, -0.9959275126457214, "[TT] Orbit Shape of the XO-3b = Eccentric (oval)"]
-[3.5795047283172607, 3.85330867767334, "[FF] Components of the CCC (Coordinated Constellation Concept) = German TerraSAR-X/TanDEM-X and the Spanish PAZ satellite"]
-[7.71405029296875, 3.247340440750122, "[FF] Facilities of the Coordinated Observations = Magnetic and optical observatories, radars, receivers and heaters"]
-[6.706162929534912, 6.215825080871582, "[FF] Test Number of the File Transfer Test = 4"]
-[9.215670585632324, 7.159974098205566, "[TT] GSD (Multispectral) of the GF-2 = 3.24 m"]
-[8.647177696228027, 7.689150333404541, "[TT] Array Size of the Detector = 256 x 256 pixels"]
-[13.52294635772705, 5.798136234283447, "[TT] Solar Array Power of the DSP satellites = 260 W (BOL) and 210 W (EOL)"]
-[3.684861183166504, 5.132472515106201, "[TT] Imaging Frequency Band of the ALOS-1 = L"]
-[5.170120716094971, 8.417223930358887, "[TT] Bandwidth of the Spectrometer = 1 GHz or more"]
-[5.375392436981201, 1.2832692861557007, "[FF] Conference Date of the LPT9310 COTS cooler = May 23-27, 2016"]
-[5.056107044219971, 3.053704023361206, "[TT] Manufacturer of the CINEMA-3 (KHUSat-2) = KHU (Kyung Hee University), Seoul, Korea"]
-[5.513862133026123, 5.7269816398620605, "[TT] Architecture of the Data Handling Computer (DHC) = AMD 2910 bit-slice"]
-[13.353082656860352, 5.624661445617676, "[TT] Efficiency of the ISS Roll-out Solar Array (iROSA) = Higher than existing arrays"]
-[6.670966625213623, 3.048611640930176, "[FF] Purpose of the ISS = Conducting experiments and research in microgravity environment"]
-[8.337969779968262, 0.1183815598487854, "[FF] Outburst Date of the Comet 67P = 2016 July 03"]
-[6.676729679107666, 4.6912617683410645, "[FF] Application of the GPS = Navigation"]
-[4.834944248199463, 2.9836008548736572, "[TT] Prime Contractor of the Spacecraft = Airbus UK"]
-[9.040911674499512, 7.546909809112549, "[TT] Spatial Resolution of the WiFS camera = 188 m"]
-[7.984911918640137, 8.2004976272583, "[FF] Bandpass Filters of the Camera = Blue, Red"]
-[5.8137526512146, 5.168715000152588, "[FF] Design Requirement of the GALANT = Provides access to each part in the receiver to take appropriate counter measures against almost any kind of interference and jamming"]
-[5.441094875335693, 5.512401103973389, "[TT] Communication Interface of the EC = Serial port"]
-[10.77263069152832, 3.8913958072662354, "[TT] Re-entry Date of the Drag de-orbit sail = 72 days later"]
-[6.453652381896973, 3.928753614425659, "[FF] Experiment of the VisionSpace = Testing the use of artificial intelligence to allow a spacecraft to analyze images on board and schedule and plan activities autonomously"]
-[8.344496726989746, 7.614410877227783, "[TT] Counting Ability of the Particle Detector = 5 x10 4  event/s"]
-[3.801342487335205, 5.057804584503174, "[TT] Polarization Selections of the RADARSAT-2 = Multiple options"]
-[10.666699409484863, 7.437643527984619, "[TT] Swath Width of the Stripmap = > 40 km"]
-[13.53286361694336, 5.858044147491455, "[FF] Function of the MPPT = Track the solar panels to obtain the maximum power operative condition"]
-[7.448522567749023, 2.9072265625, "[TT] Intended Measurement Scales of the MethaneSAT = Regional (100s of km) and fine scales (< 1 km)"]
-[4.872454643249512, 0.07350749522447586, "[TT] End of Life Date of the AEM-2 = 19 Nov 1981"]
-[9.9542818069458, 8.21607494354248, "[FF] Volume of the Coded aperture correlation holography system = 56"]
-[9.427178382873535, 2.308910369873047, "[TT] Total of the Gigantic Jets = 95"]
-[4.86030912399292, 7.356005668640137, "[TT] Data Rates (Downlink) of the RF Communications = 9.6 kbit/s"]
-[4.1403303146362305, 1.3868025541305542, "[FF] Program Date of the Meteosat Third Generation (MTG) = Oct. 1-5, 2012"]
-[3.7071738243103027, 5.435575008392334, "[TT] Azimuth Resolution of the High Resolution Spotlight = 2.2 m (dual pol.)"]
-[9.566045761108398, 4.870501518249512, "[TT] Stabilization of the Adcole Maryland Aerospace MAI401 ADCS = Three-axis"]
-[9.429033279418945, 3.7997844219207764, "[FF] URL of the Magnetometer (MAG) = http://www.goes-r.gov/spacesegment/mag.html"]
-[8.272626876831055, 2.5552186965942383, "[FF] Maximum Altitude of the Thunderstorms = Tropopause"]
-[3.7828454971313477, 4.104475021362305, "[FF] Emergency Message Collection of the GEOSAR = Yes"]
-[13.366883277893066, 7.345985412597656, "[TT] Power of the HI-SCALE = 4.0 W"]
-[7.337252616882324, 7.203369140625, "[FF] Type of the ATLAS = Optical"]
-[4.503353595733643, 2.899834632873535, "[TT] Location of the DMMC = Toulouse"]
-[6.379642009735107, -0.4548730254173279, "[TT] Operational Autonomy Period of the Spacecraft = 24 hours"]
-[10.596684455871582, 2.1895525455474854, "[FF] X-ray Source of the MAXI J1820+070 = Point source"]
-[12.004745483398438, 3.1768856048583984, "[TT] Delta-V Capacity of the Bus = More than 154 m/s"]
-[4.787522792816162, 5.685197830200195, "[TT] Frequency L2 of the GPS receiver = 1227.6 MHz"]
-[14.155440330505371, 3.0275087356567383, "[TT] Mass of the WNISAT-1R = 43 kg"]
-[10.357213973999023, 7.14992094039917, "[TT] Mesoscale Square Width of the ABI = 1000 km"]
-[11.275887489318848, 3.3083860874176025, "[FF] Challenges of the Micropropulsion = Special manufacturing technologies for the construction of the micronozzles, resistance of launchers to allow the presence of a propellant"]
-[10.188870429992676, 5.784238338470459, "[TT] Temperature Requirement of the Focal Plane Assemblies = At or below 190 K"]
-[9.874215126037598, -0.5408505797386169, "[TT] Orbital altitude of the Imager = 666 km"]
-[8.320637702941895, 7.564149856567383, "[TT] Detector Type of the EPI-Lo = SSDs (Solid State Detectors)"]
-[10.757654190063477, 2.8023765087127686, "[FF] Secondary Objective of the BIRD = Demonstrate new microsatellite technologies"]
-[4.72752046585083, -1.2214722633361816, "[TT] Launch Date of the Beijing-1 = 2005"]
-[10.245874404907227, 5.326444149017334, "[FF] Issue of the SMA = Can contact the radiator and chassis in other areas, causing an electrical short"]
-[6.725740432739258, 4.688145160675049, "[FF] Role of the OSC = Target"]
-[6.794161796569824, 4.764702796936035, "[FF] Objectives of the DCS = Collection of data from the ground segment Collect environmental measured parameters (e.g. meteorological)"]
-[8.587678909301758, 5.373350620269775, "[TT] Pointing Accuracy of the Satellite = Better than 200 m"]
-[3.870351552963257, 7.879580497741699, "[TT] Modulation Type of the TM-D710G = FM modulation with two-tone AFSK encoding"]
-[7.468975067138672, 2.409320116043091, "[TT] Measurement Category of the GF-3 = Multi-purpose imagery (land), Landscape topography"]
-[7.612203598022461, 5.660153865814209, "[FF] Approach of the Instrument = Micro-pulse multi-beam"]
-[7.627961158752441, 5.122415542602539, "[FF] URL of the Copernicus Imaging Microwave Radiometer (CIMR) = https://agupubs.onlinelibrary.wiley.com/doi/epdf/10.1029/2021JC017610"]
-[7.935174465179443, 7.196507453918457, "[TT] Data Rate of the WiFS camera = 2.06 Mbit/s"]
-[5.590137004852295, 5.1107401847839355, "[TT] OBC OS of the Spacecraft = VxWorks"]
-[8.728438377380371, 3.8672945499420166, "[FF] Measurement Type of the EIS = Ion Composition and Angular Distributions"]
-[10.251514434814453, 0.932344377040863, "[TT] Distance from Earth of the Kepler-442b = Around 1,200 light years"]
-[3.51029634475708, 5.143431663513184, "[TT] Swath Width of the Radar = 100 km"]
-[4.867032051086426, 3.8512330055236816, "[TT] Provider of the Antenna System = USA"]
-[11.024103164672852, 3.6314940452575684, "[TT] Size of the CubeSat = 10 cm x 10 cm x 10 cm per 'U'"]
-[5.493663311004639, 2.2432100772857666, "[FF] Affiliation of the Laurence Lorda = Unknown"]
-[5.332327842712402, -0.3030725419521332, "[TT] Life Expectancy of the SPOT-4 = Unchanged at the end of 2012"]
-[4.880565643310547, 0.8614897727966309, "[TT] First Flight Date of the MEPSI = February of 2000"]
-[4.726093769073486, 8.348934173583984, "[TT] Center Frequency of the 8 = 150.0 GHz"]
-[3.3845105171203613, 6.402944564819336, "[TT] Diplexer Height of the Syrlinks EWC31 TT&C transceiver = About 2.5 cm"]
-[6.310930252075195, 8.028741836547852, "[TT] Channels of the DAC = 4"]
-[4.941450595855713, 3.3957719802856445, "[TT] Manufacturer of the IXV Recorder = Curtiss Wright"]
-[7.89058780670166, 6.647932052612305, "[TT] Ecliptic Pole Observation Time of the Cameras = More than 300 days"]
-[14.31020736694336, 3.046961784362793, "[TT] Mass of the AlSat-2A and -2B = 116 kg"]
-[6.641929626464844, -0.47572508454322815, "[FF] Orbit Coverage of the JPSS = Global"]
-[4.95867919921875, 1.3136484622955322, "[TT] Design Copyright of the BRITE-PL = SFL"]
-[9.990747451782227, 1.6651413440704346, "[FF] General Theory of Relativity of the Gaia = Test"]
-[9.034263610839844, 2.6146113872528076, "[FF] Potential Cost of the Geomagnetic Storm = Up to several trillion dollars"]
-[9.140241622924805, -0.5558763146400452, "[TT] Orbit Altitude of the CryoSat-2 = 700 km"]
-[6.387568473815918, -0.4756971597671509, "[TT] Initial Acquisition Time of the CAPSTONE = Six days"]
-[7.544650077819824, 0.7460257411003113, "[FF] Mission Objective of the OMOTENASHI = Land the smallest lander to date on the lunar surface to demonstrate the feasibility of the hardware for distributed cooperative exploration systems"]
-[9.906816482543945, 1.4669286012649536, "[FF] Observation of the FAUST = Galaxy clusters in the Virgo, Telescopium, Dorado, and Ophicus constellations"]
-[10.909647941589355, 10.095415115356445, "[FF] Cooling Pipes of the Alpha Magnetic Spectrometer (AMS) = Housed in the service channel"]
-[9.985974311828613, 9.053353309631348, "[TT] Effective FOV of the Channel 5 = 30 km x 67 km"]
-[4.067815780639648, 1.570308804512024, "[TT] Landing Location of the Starliner = White Sands Space Harbor in New Mexico"]
-[10.558810234069824, 5.574986934661865, "[TT] Accuracy of the Ion & Electron Temperature = < 20% (\u03c1 >10 10  m -3 )"]
-[10.175300598144531, -2.734221935272217, "[TT] Module mass of the SLC NAND-FMM = 0.85 kg"]
-[6.888232707977295, 4.412398815155029, "[FF] Functions of the FF-G = Computes the reference state, position, velocity and attitude; and feed forward action in case of forced continuous phases (formation acquisition, coronagraphy, formation flying maneuvers), and calculates the orbital maneuvers and application times and direction in case of impulsive maneuvers (perigee pass DTMs, CGC, Go to Safe, CAM)"]
-[9.361333847045898, 3.6435976028442383, "[FF] Measured Parameters of the Special Sensor Magnetometer (SSM) = Geomagnetic fluctuations associated with solar geophysical phenomena"]
-[10.362442970275879, 4.060635566711426, "[TT] Direction of the Wire Boom = Counterclockwise"]
-[10.826948165893555, 1.4136773347854614, "[TT] Volume of the Crab Nebula = About 10 km radius"]
-[7.078303813934326, 1.264132022857666, "[FF] Last Update of the Spitzer = 16 December 2020"]
-[5.848744869232178, 7.11446475982666, "[TT] Data Rate of the STAFF/DWP = 3.00 kbit/s"]
-[9.271212577819824, 1.87532377243042, "[FF] Swath of the HARP-2 = Wide"]
-[5.150964736938477, 2.3347578048706055, "[TT] Mission Type of the Sich-2 = EO"]
-[9.67862319946289, 1.3676462173461914, "[TT] Image Receiving Stations of the Pleiades System = Japan, China and Canada"]
-[6.371216773986816, 0.4427170157432556, "[TT] Orbit Raise Maneuver No. 2 Completion Date of the CloudSat = 27 May, 2006"]
-[11.194991111755371, 5.16811466217041, "[TT] Alloy Density of the LARES and LARES-2 = Close to 10,000 kg/m3"]
-[7.654808044433594, 1.4719970226287842, "[FF] Mission of the SWOT = Surface Water and Ocean Topography"]
-[6.0369553565979, -0.2863422632217407, "[TT] Operation Duration of the PRARE = Over a year"]
-[6.673815727233887, 0.08292315155267715, "[TT] Years in Orbit of the Landsat 7 = 20 Years"]
-[3.2225053310394287, 5.12105655670166, "[TT] Boresight Orientation of the Seasat SAR sensor = 20\u00ba from the vertical direction"]
-[8.229393005371094, 6.2272539138793945, "[TT] Correct Identification Rate of the Neural Network = 96 percent"]
-[3.420567512512207, 5.055611610412598, "[TT] Radar Measurements Spatial Resolution of the L2SMAP = About 9 km"]
-[4.409299373626709, 1.9740349054336548, "[FF] Launch Date of the EgyptSat-2 = May 5, 2014"]
-[6.304378032684326, 8.103137969970703, "[TT] Number of Channels of the MTVZA-GY = 29"]
-[6.268439292907715, -0.7671657800674438, "[FF] Related to of the Orbital Lifetimes = A/M distribution"]
-[7.814238548278809, 1.5655782222747803, "[FF] Rainfall Data URL of the TRMM = http://pmm.nasa.gov/TRMM/realtime-3hr-7day-rainfall"]
-[4.518897533416748, 1.5355017185211182, "[TT] Launch Date of the VNREDSat-1A = January 08,2013"]
-[4.140218257904053, 1.3858840465545654, "[TT] MSG-1 Operational Date of the Meteosat-8 = January 9, 2004"]
-[5.284350872039795, -1.195977807044983, "[TT] Goal Life of the Kondor-E = 7 years"]
-[10.034855842590332, -1.536250114440918, "[TT] Inclination of the Orbit = 97.9\u00ba"]
-[6.361889839172363, -1.189481496810913, "[TT] LTAN of the KOMPSAT-3 = 13:30 hours"]
-[5.670019626617432, 2.757282257080078, "[TT] Funding Source of the ELFIN = NASA/NSF"]
-[10.233633995056152, 8.045365333557129, "[TT] Telescope Aperture Diameter of the GLM instrument = 12 cm"]
-[7.919386863708496, 9.014822959899902, "[TT] Panchromatic Wavelength Range of the NAOMI = 0.45 \u00b5m - 0.75 \u00b5m"]
-[7.650998592376709, -0.8603531122207642, "[TT] Operation Period of the ICESat-2 = Since 2018"]
-[9.906794548034668, 4.1868414878845215, "[TT] Search Coil Diameter of the ULF Sensor = 5 cm"]
-[7.390970706939697, 0.2594809830188751, "[FF] NASA's upcoming asteroid sample return mission of the Rosetta spacecraft = OSIRIS-REx"]
-[7.270242214202881, 4.999082088470459, "[FF] Full Swap Angle of the Motor = Not specified"]
-[9.692192077636719, 7.1738152503967285, "[TT] Ground Resolution (Normal Observation Mode) of the \u00b5SCIA = 20 km x 20 km"]
-[11.675922393798828, 4.783268451690674, "[TT] Diameter at the Base of the Nimbus-7 S/C = 1.52 m"]
-[5.398115158081055, 5.297736644744873, "[FF] Objective of the STRV-1c and -1d Spacecraft = Demonstrate emerging technologies"]
-[11.780474662780762, 0.0859011709690094, "[TT] Number of Stars with Potential Earth-like Planets of the TESS = 408"]
-[7.841705322265625, 4.441477298736572, "[TT] Measurement Frequency of the TIM = 15 measurements per day"]
-[6.897701740264893, 2.3631701469421387, "[FF] Imaging Services of the Beijing-1 = Monitoring land and water resources, agriculture, urban development, desertification, earthquake and snow disasters, pollution, and environmental impact assessment"]
-[4.910512447357178, 8.153477668762207, "[TT] Frequency of the Scatterometer = 1.26 GHz"]
-[11.030008316040039, 4.768157482147217, "[TT] Deployment Method of the Tether = Rolled up and housed within the end mass of the EDT system"]
-[5.521666526794434, 2.6867282390594482, "[TT] Senior Director of Human Spaceflight Programs of the SpaceX = Benji Reed"]
-[10.644268035888672, 7.480566501617432, "[TT] Single Pass Mono Coverage of the QuickBird-2 = 1 strip of 350 km"]
-[12.159917831420898, -0.2831440269947052, "[TT] Sector Data Collection Time of the TESS = 27 days"]
-[1.764216423034668, -2.0640811920166016, "[FF] Conjunction Transition Orbit of the Hayabusa-2 = Placed slightly further away from the asteroid"]
-[8.002899169921875, 3.1518547534942627, "[FF] Purpose of the Atmospheric Spectrometer = Detect greenhouse gases"]
-[9.560340881347656, 6.729642391204834, "[TT] Spatial Resolution of the Geodesy Levelling by GPS = 100-1000 km"]
-[11.007621765136719, 3.7734885215759277, "[FF] Size of the CUNYSAT-1 = 1U"]
-[4.763657093048096, 0.6100800037384033, "[TT] Launch Year of the MSG-4 = 2015"]
-[11.134383201599121, 0.5433879494667053, "[FF] Mission Objective of the ARIEL = Measure the chemical composition and thermal structures of exoplanets, linking them to the host star\u2019s environment"]
-[7.486632347106934, 8.90754508972168, "[TT] Band of the CLAUDIA-CAI = 1.60 \u00b5m"]
-[6.634334564208984, 5.979403495788574, "[TT] Quantity of the Transfer Frame Generators = 4"]
-[6.324949264526367, 2.5048370361328125, "[TT] Quantity of Femtosatellites of the KickSat = About 250"]
-[12.217703819274902, -0.213402658700943, "[TT] Snapshot Frequency of the TESS = Every two minutes"]
-[4.720891952514648, 4.201368808746338, "[TT] Development Organization of the SiREUS = AIS (Atlantic Inertial Systems - formerly BAE Systems of Plymouth)"]
-[7.771429061889648, 2.52919602394104, "[FF] Effect of the CH4 = Lower summertime CH4"]
-[7.080011367797852, 5.536511421203613, "[FF] Quantity of the RRA = 1"]
-[8.01833438873291, 5.1994476318359375, "[FF] Function of the CAL LR = Provide an alternate load path to support the mass of the calibration targets without over loading the Despin Assembly"]
-[14.25168514251709, 3.1661386489868164, "[TT] Mass of the AIST-2 = 39 kg"]
-[11.794034004211426, 0.10724961757659912, "[FF] Method of Exoplanet Detection of the TESS = Measuring small dips in stellar brightness caused when a planet crosses in front of, or transits, its star"]
-[6.472779273986816, 8.59953498840332, "[FF] Polarization Dependence of the Scanning Systems = Problematic"]
-[7.468396186828613, 2.3006465435028076, "[FF] Coverage of the Map = Shows flows over 80% of the continent"]
-[8.19864273071289, 4.781818866729736, "[FF] URL of the Spectrometer Telescope = http://www.esep.pro/sites/esep/IMG/pdf/poster_spie12_stix_8443-131_v3.pdf"]
-[3.6911888122558594, 4.601004600524902, "[TT] Earth Observation Constellation Type of the Spacety = Microwave-based (Synthetic Aperture Radar) satellite"]
-[4.713910102844238, 6.9543657302856445, "[FF] BDH Subsystem of the ResourceSat-2 = X-band data transmission system"]
-[2.334624767303467, 1.304020643234253, "[TT] Orbit Duration of the NanoSail-D2 = 95 days"]
-[5.256594181060791, 0.7303016781806946, "[FF] Installation Date of the Capella = 9 November 2021"]
-[4.359347820281982, 5.417798042297363, "[FF] Flight Model Delivery Date of the GOMX-3 = One year later"]
-[4.366615295410156, 0.12781015038490295, "[FF] Anticipated Global Connectivity Timeline of the Starlink = A few months after the 28th launch"]
-[6.476725101470947, 1.6788398027420044, "[TT] Surveys of the eROSITA = Eight surveys"]
-[9.60832405090332, 8.26199722290039, "[TT] Field of View of the VectorSol = 0,1\u00ba in 120\u00ba"]
-[6.274291515350342, 4.944070816040039, "[FF] Components of the On-board software controller = CAN drivers, TTC drivers, the operating system kernel, ADCS software, and the application software"]
-[7.41743278503418, 2.93646502494812, "[TT] Field of View of the MethaneSAT = 260 km"]
-[5.297159194946289, 6.342553615570068, "[TT] Core Speed of the Stamp9G20 = 400 MHz"]
-[7.041372299194336, -0.17430298030376434, "[TT] Solar Eclipses Duration of the SPARCS = 25 minutes per year"]
-[5.071743965148926, 6.972466468811035, "[TT] Uplink TT&C Data Rate of the MightySat II.1 (Sindri) = 2 kbit/s"]
-[6.261191368103027, 5.801887035369873, "[TT] Version of the GPWv4 = 4"]
-[13.617748260498047, 5.5643157958984375, "[FF] Parts of the SCTE = Flight demonstration of advanced cells on the power generating panels of STRV-1c/d and in-flight measurement of the current-voltage characteristics of 38 individual solar cells"]
-[7.496729850769043, 3.102954864501953, "[FF] Purpose of the ELDRS = Study the ELDRS effect"]
-[8.514371871948242, 1.6774637699127197, "[TT] Accuracy Range of the Integrated water vapour = 20%"]
-[5.046928882598877, 3.4284238815307617, "[TT] Manufacturer of the Phasemeter Assembly = University of Birmingham"]
-[5.0386552810668945, 3.3974411487579346, "[TT] Manufacturer of the TIRS = Northrop Grumman"]
-[8.689666748046875, 5.983433246612549, "[TT] Precision-Pointing Accuracy of the Primary Imager = 0.01\u00ba"]
-[8.289128303527832, 2.8568356037139893, "[TT] Measurement Domain of the Tatiana-2 = Atmosphere"]
-[10.710200309753418, 7.585183620452881, "[TT] Grid Size of the RAS Product = 25 km"]
-[6.466686725616455, 4.714771270751953, "[TT] Modules of the PRIMA = Propulsion module (PPM), service module (SVM), payload module (PLM)"]
-[10.77740478515625, -0.34836137294769287, "[TT] Operation Duration of the TanDEM-X = 10 years"]
-[4.607320308685303, 0.8194358944892883, "[TT] Service Start Year of the Satelles = 2016"]
-[6.554007530212402, 1.9497833251953125, "[FF] URL of the Satellite = http://journals.ametsoc.org/doi/pdf/10.1175/1520-0477%281979%29060%3C1038%3ASSOTSA%3E2.0.CO%3B2"]
-[6.9094061851501465, 7.781418800354004, "[TT] Diameter of the Secondary Reflector = 308.12 mm"]
-[7.7432756423950195, 3.496516704559326, "[FF] Objective of the GOE = Perform refractive radio occultation measurements of Earth's atmosphere"]
-[8.6146821975708, 1.9298300743103027, "[TT] Sustained Surface Winds of the RapidScat = 46.9 mph (21 meters per second/75.6 kph)"]
-[9.395573616027832, 4.7798027992248535, "[FF] Operating Modes of the IPS = Dependent on whether the gimbal resolver or gyro was used for feedback control of attitude"]
-[8.056089401245117, -1.0121490955352783, "[TT] Data Collection of the ICESat-2 = Thin ice, thick ice, and features such as ice ridges"]
-[10.58157730102539, 4.761033058166504, "[TT] Coil Windings of the VLF Experiment = 1000"]
-[9.278873443603516, 6.67561149597168, "[TT] Imaging Capacity of the KazEOSat-2 = Up to 1,000,000 km2 per day"]
-[5.964223384857178, 0.8021061420440674, "[TT] Launch Date of the FormoSat-3/COSMIC-1 = April 15, 2006"]
-[9.30575942993164, 3.686319351196289, "[FF] Data of the \u00d8rsted satellite = High precision scalar magnetic data"]
-[11.918050765991211, 3.503762722015381, "[FF] Pressure and Temperature Monitoring of the Propulsion System = Inside the plenum"]
-[6.500804424285889, 1.9294074773788452, "[FF] Presentation Date of the Indian Remote Sensing Satellite Missions (IRS) = Sept. 24-28, 2007"]
-[7.743001937866211, 3.1550776958465576, "[FF] Capability of the Visible and SWIR Cameras = Imaging the Earth's surface and clouds when illuminated by moonlight and the airglow"]
-[6.018152713775635, 5.0537800788879395, "[FF] Purpose of the ISL = Exchange data between the different elements of the constellation or network spacecrafts"]
-[8.688089370727539, 0.40313175320625305, "[TT] Water Depth of the Gulf of Khambhat = Less than 20 meters (65 feet)"]
-[7.882495880126953, -0.08863957226276398, "[FF] Date of the Cloud-free Iceland = 28 August 2020"]
-[8.715371131896973, 7.705319881439209, "[TT] Array Size of the Microbolometer Detectors = 512 x 2 pixel"]
-[3.8658604621887207, 4.482928276062012, "[TT] Data Distribution of the RADARSAT-2 = Commercial basis"]
-[7.125038146972656, 5.495328426361084, "[TT] Quantity of the IMUs = 3"]
-[4.473206043243408, 3.27266788482666, "[TT] Location of the Ground Station = ITU"]
-[5.973819255828857, 5.760010719299316, "[TT] FPGA of the NanoCom SDR = Xilinx Zynq Z7030"]
-[8.717084884643555, 0.17255987226963043, "[TT] Distance from the Sun at Expected Perihelion of the Comet ATLAS = Around 37 million kilometers"]
-[8.843544960021973, 2.6966161727905273, "[TT] Reconnection Duration of the Auroral imaging = Hours"]
-[9.392765045166016, 7.377896308898926, "[TT] Spatial Resolution of the HRV = 10 m for PAN, 20 m for MS"]
-[4.5266618728637695, -0.8457896113395691, "[FF] Test Type of the SpaceX Crew Dragon = NASA Commercial Crew Flight Test"]
-[6.77041482925415, 7.425865650177002, "[TT] Output Range of the DAC = 0-5 V"]
-[5.265553951263428, 0.2575480341911316, "[TT] Operation Start Year of the CFESat = 2009"]
-[7.761624336242676, 6.227035999298096, "[FF] Function of the CCD Camera = Captures images"]
-[9.454804420471191, 4.03069543838501, "[FF] Function of the CubeControl = Controls both magnetometers and samples connected sensors"]
-[10.310751914978027, 2.3298277854919434, "[TT] Presentation Date of the An Efficient Photoelectric X-ray Polarimeter = 2001"]
-[10.340523719787598, 3.235253095626831, "[TT] Payload Complement of the ALBus CubeSat = 13 CubeSats"]
-[10.312847137451172, 5.780604839324951, "[TT] Dark Current of the Instrument = Can be kept insignificant for normal instrument operating temperatures"]
-[5.292230606079102, 3.8817007541656494, "[TT] Number of Satellites in Operation of the Sentinel-2 = 2"]
-[6.63077974319458, 5.4325056076049805, "[FF] Analog to Digital Conversion (ADC) of the dsPIC33F microcontroller = Unknown"]
-[4.728279113769531, 5.920299530029297, "[TT] Radio Transmission Mode of the HORYU-2 = CW (beacon) transmission and FM transmission"]
-[9.69664478302002, 8.381935119628906, "[TT] FOV of the Optics and detector assembly = \u00b10.25\u00ba"]
-[10.23097038269043, 5.5938544273376465, "[FF] Temperature Control of the CVX = To a few millionths of a degree"]
-[9.675325393676758, 4.75291633605957, "[FF] Precession of the SS 433 = Wobbles on its axis"]
-[5.445712089538574, 7.136178016662598, "[TT] Data Transfer Rate of the LCRD = Approximately 1.2 Gbit/s"]
-[5.1333441734313965, 0.4365505278110504, "[TT] Date of the Impact Event = 5 April 5 at 2:37 UT"]
-[7.563093185424805, 6.952219009399414, "[TT] Scan Time of the ScaRaB = 6 seconds"]
-[7.987603187561035, 8.320649147033691, "[TT] Infrared Channels of the ILAS = 44"]
-[9.267731666564941, 5.006962776184082, "[FF] Attitude Angle Error of the Satellite = Occurs after 15-20 minutes"]
-[10.983053207397461, 7.309552192687988, "[TT] Swath Width of the GHGSat = 12 km"]
-[4.48357629776001, 6.122353553771973, "[FF] Goal of the NCLE = Determine the low frequency radio environment at the Earth Moon L2 point"]
-[9.683757781982422, 7.443209648132324, "[TT] Ground Sampling Distance of the TrueColour Imager = 5 m"]
-[8.664481163024902, 7.628925800323486, "[TT] CCD array size of the 16 mm camera = 750 x 580 pixels"]
-[5.473353862762451, 7.019931316375732, "[TT] Telemetry Rate of the FREND = 50 Mbit/day"]
-[9.513232231140137, 8.274186134338379, "[TT] Beam Focal Length of the Spectrometer = 400 mm"]
-[5.684939384460449, 5.056689262390137, "[TT] On-board Computer (OBC) of the Satellite = Single"]
-[5.9558539390563965, 0.853277325630188, "[FF] Image Capture Date of the Kanopus-V1 = 21.01.2013 - 27.01.2013"]
-[8.538522720336914, 6.119655609130859, "[TT] Measurement Accuracy of the ATOMMS = 1% or better"]
-[9.38573169708252, -0.20708586275577545, "[TT] Loch-in Zone of the Satellite = 800 km"]
-[7.601315975189209, 6.889979839324951, "[TT] Operational Cadence of the Instrument = Rotate 120\u00ba in < 2 minutes to space view"]
-[3.4287233352661133, -0.8998957872390747, "[TT] Orbit Type of the IRIS = Sun-synchronous orbit"]
-[9.149216651916504, 7.638144493103027, "[TT] Spatial Resolution of the Multispectral Instrument (MSI) = 20 m"]
-[7.879809856414795, 0.4656078517436981, "[TT] Moon Elevation of the CUMULOS = 67.9\u00b0"]
-[3.523552179336548, 5.338379383087158, "[TT] Wavelength of the Radar = 23.5 cm"]
-[6.1943039894104, 8.602527618408203, "[TT] Polarization of the CoSMIR = Horizontally polarized (except for the two 91.665 GHz channels)"]
-[10.07703685760498, 1.3696973323822021, "[TT] Gaia-Sausage-Enceladus Merger of the Milky Way = About two billion years later"]
-[5.638092041015625, 2.925311803817749, "[TT] Funding of the Hiber BV = \u20ac26 million"]
-[14.226181030273438, 3.2493093013763428, "[TT] Mass of the LTP = about 125 kg"]
-[3.508800745010376, 1.3820021152496338, "[TT] Mission End Date of the Sentinel-1B = 3 August 2022"]
-[4.513252258300781, 1.4903943538665771, "[TT] Launch Date of the MTSAT = 15 Nov 1999"]
-[4.278498649597168, 2.653140068054199, "[TT] Launch Site of the COPPER CubeSat = MARS (Mid-Atlantic Regional Spaceport), located at NASA's Wallops Flight Facility,Wallops Island, VA"]
-[3.7110962867736816, -0.7306710481643677, "[TT] Relative Orbit of the TSX and TDX = TDX has a relative orbit to TSX"]
-[14.632329940795898, 6.703505992889404, "[TT] Stored Power of the NiMH battery = 4200 mAh"]
-[11.270208358764648, 5.8670334815979, "[TT] Enclosure Material of the VLF Antenna = Plastic"]
-[5.910499572753906, 0.9028068780899048, "[TT] Image Acquisition Date of the Jomo Kenyatta = 20 Jan. 2013"]
-[4.920042991638184, 0.40416014194488525, "[TT] Decommissioned Date of the SASAR INSAT-2 = 2001"]
-[9.476788520812988, 7.176494121551514, "[TT] Spatial Resolution of the PMI = 53 x 31 km"]
-[9.068374633789062, 7.259570598602295, "[TT] Image Resolution of the ExoMars TGO = 460 km/pixel"]
-[14.348320007324219, 2.9967525005340576, "[TT] Mass of the Hodoyoshi-1 = 60 kg"]
-[13.385421752929688, 7.350940227508545, "[TT] Power of the NTSIC = ~ 140 W"]
-[5.63550329208374, 3.1923274993896484, "[TT] Contract Value of the Northrop Grumman = $692 million"]
-[8.084959983825684, 4.238856315612793, "[TT] Type of the TSIS-1/TIM = Earth radiation budget radiometers"]
-[9.590755462646484, -0.509467363357544, "[TT] Final Orbit Altitude of the FormoSat-7/COSMIC-2 satellites = ~520-550 km"]
-[11.252272605895996, 5.750631332397461, "[TT] Material of the Bulkhead = Two shells brazed together"]
-[8.706083297729492, 8.799670219421387, "[TT] Grating Lines of the Offner-type spectrometer = 500 lines/mm"]
-[4.553854465484619, 0.5104010105133057, "[TT] Launch Date of the M3MSat = 2016"]
-[5.442892074584961, -0.03478551656007767, "[FF] NGA Contract Date of the RapidEye = Sept. 6, 2011"]
-[13.469293594360352, 5.540923118591309, "[FF] Objective of the SMS = Measure the current and voltage characteristics of the solar cells under varies aspect angles to the sun to generate voltage-current (IV) curve traces twice per orbit"]
-[7.701718330383301, 0.28389111161231995, "[TT] Trojan Cloud Cycle of the Lucy = Every six years"]
-[13.757354736328125, 2.8278439044952393, "[TT] Spacecraft Mass at Launch of the QuickBird-2 = 931 kg"]
-[4.640965938568115, 7.928483486175537, "[TT] Frequency Ranges of the TEC Antennas = 1250 MHz and 1600 MHz"]
-[6.367493629455566, 3.9295966625213623, "[FF] Development Schedule of the SWOT = Optimised"]
-[14.05056095123291, 3.150550365447998, "[TT] Mass of the CICERO-7 = ~10 kg"]
-[4.368112564086914, 7.80932092666626, "[TT] Uplink Frequency of the CUTE-1.7+APD = L-band (1268.500 MHz)"]
-[6.211285591125488, 4.890052318572998, "[FF] Function of the Telemetry/Telecommand board = Manages the LVPS that provides bias to the electronics subsystems, the local telemetry and telecommand signals"]
-[4.711572647094727, 0.02638220228254795, "[TT] End of Life Date of the ARMADILLO = 25 June 2024"]
-[10.555893898010254, 2.7886147499084473, "[TT] Function of the Nanosatellites = Act as mobile towers in space"]
-[7.879575729370117, 2.464414119720459, "[FF] Purpose of the High-resolution camera = Collect color images of the ice surface"]
-[4.814469337463379, 7.984086036682129, "[TT] Carrier frequency (MHz) of the E6-B = 1278.750"]
-[5.2180280685424805, 5.343904972076416, "[FF] Ground-Station Uplink Passes of the SpinSat = Several"]
-[4.729172706604004, 5.610860347747803, "[FF] Measurement Technique of the RISE = Doppler shift of radio signals"]
-[9.263888359069824, 6.350976467132568, "[TT] 20 dB of the S/A: azimuth = -"]
-[4.832098960876465, 0.1331222653388977, "[TT] Return Date of the Crew-1 = April 2021"]
-[9.569398880004883, 0.7460389733314514, "[TT] Distance from Earth of the Magnetospheric Multiscale Mission = 187,166 km"]
-[3.4251224994659424, -0.017127130180597305, "[TT] Vehicle of the Orbital ATK = Antares"]
-[10.913432121276855, 10.100625991821289, "[FF] Publication Date of the Alpha Magnetic Spectrometer = 11 January 2018"]
-[8.253232955932617, 1.0968480110168457, "[TT] Soil Moisture Measurement Error of the RISAT-1 = 6.2 to 8.5 volume percent"]
-[4.747239589691162, 0.598005473613739, "[TT] Launch Status of the DirecTV 15 = To be launched in a few weeks"]
-[11.856178283691406, 0.011327460408210754, "[TT] Number of Stars of the TESS = Nearly 24 million"]
-[7.095069885253906, 3.8987951278686523, "[FF] Conference Date of the PROBA-3 High Precision Formation Flying Control System = June 5-10, 2011"]
-[11.908696174621582, 4.720206260681152, "[TT] Size of the Dove-1 = 10 cm x 10 cm x 30 cm"]
-[5.246741771697998, 1.2786667346954346, "[FF] Conference Location of the SEXTANT = Kissimmee, FL, USA"]
-[8.119064331054688, 2.4220502376556396, "[FF] Purpose of the GIIRS = Monitor and measure internal constitution and precipitation parameters of the atmosphere cloud cluster"]
-[10.380073547363281, 5.304651260375977, "[FF] Insulation Purpose of the BepiColombo = Protect the spacecraft from extreme thermal conditions"]
-[9.717354774475098, 4.57512092590332, "[TT] Type of the ACS = Passive magnetic attitude control system"]
-[5.029581546783447, 0.7597035765647888, "[TT] Mission Start Date of the MANTIS = September 11, 2019"]
-[10.938700675964355, -0.3523949682712555, "[FF] Performance Prediction of the TanDEM-X = Not provided"]
-[7.375399589538574, -0.037963081151247025, "[FF] Launch Date of the Philae = Unknown"]
-[4.654703140258789, 5.42584228515625, "[FF] Operation of the Automated Beacon Network = Notifies on-call operators and initiates response actions"]
-[5.152632713317871, -0.5918349623680115, "[FF] Project Date of the TARANIS = Dec. 5-9, 2005"]
-[4.033400535583496, 6.393725395202637, "[FF] Design of the Antenna array = Adaptive nulling design, 4 elements, f c =5 GHz"]
-[7.252634525299072, 0.06617993116378784, "[TT] Age of the Comets = 4.6 billion years"]
-[5.458914756774902, 6.076905727386475, "[FF] Control Handover of the Stamp9G20 microcontroller = Acquires control of the shared flash memory"]
-[8.275575637817383, 7.98552942276001, "[TT] Dwell Time of the SWIR/MWIR detectors = 40 \u00b5s"]
-[13.993067741394043, 7.176321983337402, "[TT] Output Voltage of the SAP = Varies"]
-[11.803854942321777, 4.939530372619629, "[TT] Dimensions of the FPGA = 42.5 mm x 42.5 mm"]
-[10.111444473266602, -1.5985852479934692, "[TT] Inclination of the STRV-1c and -1d = 7.5\u00ba"]
-[5.242747783660889, -1.2040095329284668, "[TT] Revisit Time Capability of the Kondor-E1 = 2-3 days"]
-[7.500893592834473, 2.4152464866638184, "[TT] Sky Coverage of the SPARCS = 60% over a year"]
-[5.354284286499023, 2.4065144062042236, "[TT] Mission Lead of the NuSTAR = Caltech"]
-[7.119936466217041, 6.909212112426758, "[TT] Frequency Stabilization of the Laser = One wavelength and a perfect beam out to 15 decimal places of accuracy"]
-[6.531398296356201, 4.739388465881348, "[FF] Oversight of the Characterization Process = Human oversight to ensure the integrity of the data"]
-[9.831884384155273, 4.190735340118408, "[TT] Magnet Quantity of the AMS-01 = 10"]
-[6.3541412353515625, 1.5218840837478638, "[TT] Launch Date of the MICROSCOPE = April 2016"]
-[7.628146171569824, -2.467827320098877, "[FF] Arrival Date of the GOLD instrument = January 4, 2017"]
-[4.495794773101807, 7.781515121459961, "[TT] Uplink Data Rate of the L-3 Communications Cadet UHF nanosatellite radio = 9.6 kbit/s"]
-[4.464231967926025, 6.901583194732666, "[FF] Data Flows of the PROBA-V = S-band and X-band"]
-[5.5266571044921875, 2.732614040374756, "[TT] Mission Partner of the WSF-M = Space Force"]
-[3.7968029975891113, 7.961905479431152, "[TT] Modulation of the Demodulator = QPSK"]
-[5.553946495056152, 6.72735071182251, "[TT] Data Downlink Time from Larger Platforms of the HyperScout 1 = Several hours"]
-[11.238692283630371, 5.351312637329102, "[TT] Detector Material of the TOF = Scintillator"]
-[7.066060543060303, 7.732274055480957, "[TT] Number of Reflectors of the Laser corner-cube reflectors = 96"]
-[8.55997371673584, 8.050124168395996, "[TT] Number of Pixels of the Band 1 = 1600"]
-[7.620970249176025, 2.9461870193481445, "[FF] Planned Observational Capabilities of the FengYun LEO satellites = WindRAD for sea winds, GAS for greenhouse gases absorption measurement"]
-[8.351183891296387, 4.601934432983398, "[TT] Position Improvement of the LARES = 20%"]
-[6.834898948669434, 4.366547107696533, "[FF] Unknown of the DSX Program = Unknown"]
-[10.069989204406738, 4.511778831481934, "[TT] Thrust Orientation of the NanoPS = Major-axis spin inducing"]
-[10.171891212463379, 5.41354513168335, "[FF] Thermal Modeling Supporter of the Edison Demonstration of Smallsat Networks Project = Robert F. Coker"]
-[4.510039329528809, 0.6114882826805115, "[TT] Entry Date of the DFM-FINE = 5th May"]
-[11.811229705810547, 0.05467984452843666, "[TT] Purpose of the TESS = Find exoplanets"]
-[3.3569319248199463, 5.756379127502441, "[TT] Panels of the SAR Antenna = One fixed and four deployable panels"]
-[8.277420997619629, 7.083827972412109, "[TT] Number of Images Captured of the PolyCam = 7000 images"]
-[6.87612771987915, 6.997495174407959, "[FF] Quantity of the Dichroic Beam Splitters = 3"]
-[9.199761390686035, -0.2814781665802002, "[TT] Perigee of the SeaSat = 775 km"]
-[10.410543441772461, 2.2972419261932373, "[FF] Imaging of the European Photon Imaging Camera (EPIC) = X-rays"]
-[6.827296257019043, 6.294065952301025, "[TT] Number of Targets of the IXPE = 6"]
-[4.8049187660217285, 2.492558240890503, "[TT] 3TECS Test Passes of the NorSat-2 = Six"]
-[7.8078179359436035, 7.234818935394287, "[TT] Compression Algorithm Ratio of the Camera = 3.2 : 1"]
-[5.100831508636475, 3.244148015975952, "[FF] Investment of the EDRS = German Space Administration DLR"]
-[6.17526912689209, 6.937358379364014, "[TT] Optical Downlink Rate of the NASA OCSD = Up to 200 Mbit/s"]
-[11.234301567077637, 5.899011135101318, "[TT] Telescope Structure of the MWIR = Carbon fiber composite"]
-[7.9821038246154785, 6.491413116455078, "[TT] Operating Mode of the Sich-2 = Program tilt mode during imaging"]
-[8.987482070922852, 8.24945068359375, "[FF] Publication Date of the Spaceborne Frequency Comb Metrology = Dec. 2016"]
-[4.423688888549805, 1.6151280403137207, "[TT] Launcher of the MEPSI = MightySat II.1"]
-[10.396957397460938, 2.1102476119995117, "[FF] Purpose of the X-ray Source Population Study Instrument = Study the physics of galactic X-ray source populations, like pre-main sequence stars, supernova remnants and X-ray binaries"]
-[3.142896890640259, 2.273629665374756, "[FF] Function of the U-GEO = Combines Copernicus Sentinel data with urban planning, resource management, and green infrastructure"]
-[5.649576187133789, -0.8117321133613586, "[TT] Design Life of the GOSAT-2 = 5 years"]
-[11.132946968078613, 5.854368209838867, "[TT] Coating of the MCP = KBr"]
-[9.017309188842773, 9.297586441040039, "[TT] Coverage of the FTS = Cross-track: \u00b135\u00ba, Along-track: \u00b140\u00ba"]
-[13.565176010131836, 5.7875847816467285, "[TT] Solar Panels Power of the ICESat-2 = 1320 Watts"]
-[7.969222068786621, 0.3616272509098053, "[FF] Water Loss Data Provider of the GRACE-FO = NASA\u2019s Gravity Recovery and Climate Experiment (GRACE) and GRACE-FO satellites"]
-[7.011786460876465, 7.263051986694336, "[TT] Divergence of the ATLAS lasers systems = <130 \u00b5rad"]
-[6.845449924468994, 3.7222492694854736, "[FF] Final Orbital Positions of the Satellites = Unknown"]
-[12.974562644958496, 2.1495778560638428, "[FF] Mass of the SAGE-III = Unknown"]
-[11.6371488571167, 6.653082370758057, "[TT] Energy Measurement Range of the Telescope = 1-40 MeV/n"]
-[4.991053581237793, 3.2136356830596924, "[TT] Manufacturer of the GHGSat-C2 = ABB"]
-[5.738955020904541, 0.6030908226966858, "[FF] Publication Date of the Cluster and Phoenix Missions = 1997"]
-[6.242334365844727, 4.307440757751465, "[FF] Experiment of the Airbus = Testing a completely new onboard software system in the space environment"]
-[3.7742972373962402, 4.5785698890686035, "[TT] Imaging Mechanism of the RADARSAT-2 = Active"]
-[9.582052230834961, 3.7319865226745605, "[TT] Magnetic Field Strength of the Sunspot = 6,250 gauss"]
-[7.841152191162109, 1.8235019445419312, "[FF] Monitoring Method of the Ocean Acidification = Measurements of seawater pH"]
-[7.609107494354248, 3.890310049057007, "[FF] Sensor Complement of the Trisat-R = Radiation-detection payloads from CERN, the European Council for Nuclear Research, Slovenian firm SkyLabs and ESA"]
-[13.375892639160156, 7.724970817565918, "[TT] Output Power of the RF communications = ~ 1W"]
-[8.228557586669922, 4.319697856903076, "[FF] Purpose of the Filter Assembly = Prevent stray light effects"]
-[12.725841522216797, 3.9043238162994385, "[FF] Spatial Extent of the Reconnection Lines = Large or small"]
-[7.007199287414551, 7.1048197746276855, "[TT] Pulse Peak Output Power of the Laser = 500~1000 W"]
-[9.689661026000977, 4.863677501678467, "[TT] Stabilization of the S/C = Three-axis"]
-[9.27661418914795, -0.2842172682285309, "[TT] Updated Perigee of the \u00d8rsted satellite = 640 km"]
-[9.676680564880371, -0.3721913993358612, "[TT] Altitude of the JL-1-GF03D = 535 km"]
-[6.542376518249512, 5.416692733764648, "[TT] Components of the DEM (Digital Electronics Module) = ICU (Instrumental Control Unit) and a DPU"]
-[8.237824440002441, -0.9701219201087952, "[FF] Application of the Lidar Instrument = Estimate sea ice thickness"]
-[3.2165637016296387, 3.812135934829712, "[TT] Launch Year of the TerraSAR-X = 2007"]
-[7.751707077026367, 5.7235589027404785, "[FF] Experiment of the Toshiba Co. = Vision data processing experiment"]
-[3.0555131435394287, 1.9860836267471313, "[FF] Anomaly Update of the Copernicus Sentinel-1B = 25 February 2022"]
-[6.461317539215088, 4.642759799957275, "[FF] Function of the RIU = Acquiring the housekeeping information of the spacecraft, managing the propulsion module items, managing the AOCS components, controlling the configuration of the satellite units"]
-[4.860241889953613, 2.488844394683838, "[TT] Manufacturer of the G\u00f6kt\u00fcrk-1 = Telescpazio"]
-[10.880102157592773, 3.6989638805389404, "[TT] Development Location of the NEA Scout = NASA Marshall in Huntsville, Alabama, and JPL in Southern California"]
-[12.00867748260498, -0.1670246422290802, "[FF] Sky Survey of the TESS = 20000 light-years from the Sun"]
-[7.401707649230957, 0.2642306387424469, "[FF] Purpose of the OSIRIS-REx = Detailed survey of Bennu"]
-[6.440003395080566, 3.086092948913574, "[FF] Data Location of the JERS-1 = ESA Earth Online website and the OpenSearch Datasets on NASA Earthdata website"]
-[7.420114994049072, 4.246304035186768, "[FF] Purpose of the LIRIS = Technology demonstration for future non-cooperative rendezvous applications"]
-[10.675325393676758, 6.094936847686768, "[TT] Measurement Range - Satellite Potential of the ISL Instrument = \u00b1 5 V"]
-[11.150178909301758, 6.06339693069458, "[TT] Material of the Glass Layers = Titanium-glass-epoxy-graphite"]
-[14.216853141784668, 3.2011053562164307, "[TT] Mass of the Prox-1 = 71 kg"]
-[14.182356834411621, 2.884766101837158, "[TT] Mass of the KazEOSat-2 = 185 kg"]
-[6.237094879150391, 8.576464653015137, "[TT] Polarization of the Sentinel-1 = Selectable dual polarization"]
-[3.156813859939575, 4.306244850158691, "[TT] Bistatic X-band Experiment Result of the TerraSAR-X = Success"]
-[12.079682350158691, 6.404872894287109, "[TT] Positron Fraction Energy Range of the AMS = 0.5 to 500 GeV"]
-[10.850106239318848, -0.280138224363327, "[FF] Mission Plan of the TanDEM-X = Not provided"]
-[5.728384494781494, 6.120087146759033, "[TT] Number of Bidirectional Serial Ports of the NIC = 9"]
-[7.983585834503174, 5.336805820465088, "[TT] Error Requirement of the FLLS = 300 \u00b5m or less"]
-[9.532529830932617, 1.0594977140426636, "[TT] Speed of the ICEYE-X1 = More than 7.5 km/s"]
-[8.452715873718262, 6.941879749298096, "[TT] Type of the MSI = High resolution optical imagers"]
-[12.07726001739502, 3.464322328567505, "[TT] Mass Flow Rate of the PPCU ion thruster = 10.5 cm3/s"]
-[3.2307260036468506, 5.744459629058838, "[TT] Dimensions of the SAR Antenna = 1.5 m x 15 m"]
-[11.226885795593262, 5.93872594833374, "[TT] Material of the OBA (Optical Bench Assemblies) = CFRP and aluminum core"]
-[6.5100626945495605, 3.301422357559204, "[FF] Working Life of the AMS-02 = Extended"]
-[6.833424091339111, 3.691992998123169, "[FF] Development Status of the PROBA-V = Unknown"]
-[14.658622741699219, 6.698927402496338, "[TT] Configuration of the FS-5 battery = 8 series 16 parallel"]
-[7.695010662078857, 0.8574678897857666, "[FF] Function of the LAM (Laser Altimeter, Moon) = Probe the features of the lunar soil and the space environment near the moon"]
-[4.859409809112549, 0.6023286581039429, "[TT] Project Start Date of the MinXSS = Spring 2014"]
-[13.831738471984863, 7.111701488494873, "[TT] Voltage range (V) of the PS-1 = 800~1,100"]
-[3.0820083618164062, 2.2130463123321533, "[TT] Crop Type Representation of the Copernicus Sentinel-2 = Colourful squares"]
-[6.619812488555908, 5.718142032623291, "[TT] Number of Payloads of the KPLO = 6"]
-[11.066720962524414, 0.9213588237762451, "[TT] Satellite Quantity of the LISA = 3"]
-[4.556108474731445, 1.5004494190216064, "[TT] Launch Date of the PhiSat-1 = September 2020"]
-[10.996268272399902, 7.574595928192139, "[TT] Swath Width of the MSU-100 = 960 km"]
-[8.727625846862793, 4.922474384307861, "[TT] Field of View of the Star Tracker = 8\u00ba x 8\u00ba"]
-[9.343173027038574, 2.781151294708252, "[FF] Solar Wind Speed of the Solar Wind Satellite = Speeding up"]
-[7.32280969619751, 6.455850124359131, "[FF] Integration Time of the Instrument = 2.5 ms, 1.2 ms"]
-[5.535515308380127, 5.512612819671631, "[TT] Communication Interface of the OBC = SPI (Serial Peripheral Interface)"]
-[5.170241355895996, 3.533379316329956, "[FF] Manufacturer of the 2D Camera = Not specified"]
-[11.652721405029297, 6.658192157745361, "[TT] High Energy Telescope Energy of the CRS = 70MeV"]
-[6.854575157165527, 6.698364734649658, "[TT] Sub-contractor of the Laser Transmitter = Quantel"]
-[9.480965614318848, 6.951330661773682, "[TT] Depth Resolution of the FREND = ~1 m"]
-[13.12110710144043, 7.208621501922607, "[TT] Collection Power of the IMAP-Lo = ~15 x"]
-[8.352230072021484, 7.295274257659912, "[TT] Imaging Channels of the FPA = One panchromatic and three multi-spectral channels"]
-[5.245270252227783, 3.4238121509552, "[FF] Manufacturer of the S/C-GNC = NGC (NGC Aerospace Ltd.)"]
-[8.65404987335205, 5.927817344665527, "[TT] Measurement Accuracy of the CLS (Coarse Lateral Sensor) = 1 mm @150 m (lateral)"]
-[10.231108665466309, 7.953850269317627, "[TT] Telescope Size of the MOST = 5.9-inch (15-centimeter)"]
-[10.69934368133545, 3.106893301010132, "[TT] Attitude Control of the O/OREOS nanosatellite = Permanent magnets and hysteresis rods"]
-[5.587260723114014, 3.966179370880127, "[TT] Number of Payloads of the Spaceflight SSO-A: SmallSat Express = 64"]
-[10.171815872192383, 5.528419494628906, "[TT] Temperature Stability of the COB (Coronagraph Optical Box) = \u00b12\u00b0C"]
-[4.935183048248291, 3.0785677433013916, "[TT] Manufacturer of the Harpoon = Airbus (UK)"]
-[13.53386116027832, 5.803173542022705, "[TT] Power Output of the Solar Array = Meets the satellite operation requirements"]
-[5.827920913696289, -0.7955625057220459, "[TT] Design Life of the FY-3 series spacecraft = 3 years"]
-[5.229885578155518, 7.014560699462891, "[TT] Uplink Data Rate of the Telemetry, Tracking, and Command (TT&C) = 4 kbits/s"]
-[6.063877582550049, -1.9575703144073486, "[TT] Member of the Hans-Peter Marshall = True"]
-[6.961935043334961, -0.10075276345014572, "[TT] Earth Mapping Cycle of the OCO = 32 days"]
-[8.955657958984375, 6.757813930511475, "[TT] Pointing Direction of the On-board camera (CAM) = TANSO-FTS-2 viewing"]
-[10.037985801696777, 1.9144600629806519, "[FF] Expected Cost of the Chandrayaan-3 = $35 million"]
-[5.151604652404785, 3.2643239498138428, "[TT] Manufacturer of the Pearl White-1 = United States Air Force Space Command"]
-[10.61089038848877, 1.8664767742156982, "[FF] Observed Phenomenon of the XMM-Newton = Black hole winds blowing toward us"]
-[11.441581726074219, 0.7552654147148132, "[TT] Size of the AU Mic b = Neptune-size"]
-[3.3663275241851807, 1.4670212268829346, "[TT] Launch Date of the Sentinel-2A = June 2015"]
-[5.1854658126831055, 0.44861215353012085, "[TT] Operation Start Date of the CoReCi = Since September 2012"]
-[8.937052726745605, 5.275533199310303, "[TT] Pointing Adjustment of the Kepler = Slight"]
-[3.319850444793701, 4.998281002044678, "[FF] Application of the SAR Mode = Fully polarimetric 3-D structure mode and the ultra-wide swath deformation mode"]
-[11.036112785339355, 5.639811038970947, "[TT] Vacuum Level Maintenance of the SU = Getter material"]
-[7.62139368057251, 8.96022891998291, "[TT] Spectral Range (\u00b5m) of the Band 6 = 1.58 - 1.64"]
-[7.947780609130859, 7.873647689819336, "[TT] Phototransistor Sensitive Area Diameter of the DIAL Instrument = 200 \u00b5m"]
-[5.965713024139404, 5.174984931945801, "[FF] Interface of the Spacecraft Emulator = MCS to OBC and back again"]
-[9.826132774353027, 7.029558181762695, "[TT] Capacity of the MUSES = Up to four Earth observation instruments"]
-[5.478147029876709, 7.032308101654053, "[TT] Speed of the Telemetry Data = 640 Mbps"]
-[7.39856481552124, 2.358290672302246, "[TT] Global Mapping Achievement of the Satellite = 99.7%"]
-[5.375126361846924, 4.1597113609313965, "[TT] Satellite Bus of the Tomorrow-R1 and -R2 = Corvus-XL satellite platform"]
-[4.581129550933838, 7.049539089202881, "[TT] Transmission Band of the Data Downlink = X-band"]
-[6.069121360778809, 0.2415115088224411, "[FF] BAA Framework Issuance Frequency of the NRO = Multiple times per year"]
-[2.8872835636138916, 4.58890438079834, "[TT] Data Rate of the PALSAR-2 = 278 Mbit/s for Ka-band and at 800/400/200 Mbit/s via X-band"]
-[9.232723236083984, 3.1614162921905518, "[FF] Authors of the Magnetospheric Multiscale (MMS) = J. L. Burch1, R. B. Torbert, T. D. Phan, L.-J. Chen, T. E. Moore, R. E. Ergun, J. P. Eastwood, D. J. Gershman, P. A. Cassak, M. R. Argall, S. Wang4, M. Hesse, C. J. Pollock, B. L. Giles, R. Nakamura, B. H. Mauk, S. A. Fuselier, C. T. Russell, R. J. Strangeway, J. F. Drake, M. A. Shay, Yu. V. Khotyaintsev, P.-A. Lindqvist, G. Marklund, F. D. Wilder, D. T. Young, K. Torkar, J. Goldstein, J. C. Dorelli, L. A. Avanov, M. Oka, D. N. Baker, A. N. Jaynes, K. A. Goodrich, I. J. Cohen, D. L. Turner, J. F. Fennell, J. B. Blake, J. Clemmons, M. Goldman, D. Newman, S. M. Petrinec, K. J. Trattner, B. Lavraud, P. H. Reiff, W. Baumjohann, W. Magnes, M. Steller, W. Lewis, Y. Saito, V. Coffey, M. Chandler"]
-[10.296041488647461, 2.241028308868408, "[FF] Purpose of the AST = Precise reconstruction of the direction of arrival of high energy gamma rays"]
-[9.982420921325684, 7.79538106918335, "[TT] Celestial Sphere Coverage of the Telescope = 100% annually"]
-[14.245201110839844, 3.197472095489502, "[TT] Mass of the SESAME = 1.8 kg"]
-[8.429837226867676, 3.6590213775634766, "[FF] Deviation from MSIS of the Atomic Oxygen = Up to a factor of four"]
-[9.801005363464355, 0.7669696807861328, "[TT] Observational Period of the GOSAT = 3 month - 1,000 km mesh (terrestrial region), 1 month - 500 km mesh (terrestrial region), 2,000 km mesh (ocean)"]
-[8.24288558959961, 0.7948643565177917, "[TT] Composition of the Psyche = Mostly iron and nickel"]
-[10.051025390625, 1.9018404483795166, "[FF] Launch Date of the Chandrayaan-1 = 2008"]
-[4.813694953918457, 2.803287982940674, "[TT] Location of the SPIE = NASA/MSFC (Marshall Space Flight Center) in Huntsville, Alabama"]
-[8.507072448730469, 7.676015853881836, "[TT] PAN Detector Array of the WV-3 Imager = 35,000 pixel"]
-[8.788538932800293, 4.483863353729248, "[FF] Stated Capabilities of the Honeywell Sensor = Unknown"]
-[6.442712783813477, 1.908619999885559, "[FF] URL of the D-Sat = https://www.dsat.space/"]
-[8.387333869934082, 2.5196831226348877, "[FF] Extended Mission Phases Focus of the THEMIS = Energy release mechanisms that occur beyond 10 RE and after substorm onset"]
-[4.469159126281738, 5.425570964813232, "[FF] Mission of the GOMX-3 = Unknown"]
-[8.310053825378418, 3.6442999839782715, "[FF] Cal_limb data Collection of the OCO-2 = Solar and Atmospheric Absorption Lines"]
-[7.895842552185059, 4.975915908813477, "[FF] Simultaneous Check Method of the Data Processing System = Comparison of the known power of the reference electrical source with the precision measurement of the servo-system"]
-[9.693490028381348, -0.436202734708786, "[TT] Altitude of the IRS-1B = 904 km"]
-[6.257293224334717, 5.105459213256836, "[FF] Function of the PIC (Peripheral Interface Controller) = Monitors periodically the status of the OBC"]
-[9.815927505493164, -0.19736480712890625, "[TT] Altitude of the GRACE-FO = About 490 km"]
-[13.540546417236328, 5.490014553070068, "[FF] Manufacturing of the SFINKS = Made by depositing layers of thin-film of photovoltaic material on a flexible plastic"]
-[8.021197319030762, -0.9746860265731812, "[FF] Ground Segment of the ICESat-2 = Overview"]
-[12.733235359191895, 3.9030022621154785, "[FF] Science Questions of the CuPID = (1) Under what conditions is magnetopause reconnection spatially continuous versus discontinuous? (2) under what conditions is magnetopause reconnection temporally steady versus bursty?"]
-[9.290797233581543, 5.281405925750732, "[TT] Range of the Angular Rate = \u00b1200\u00ba/s(3-axis)"]
-[5.576570510864258, 5.717392921447754, "[TT] Processor of the DHS = 32 bit RISC processor (Renesas Technology, SH-4, 300 MIPS)"]
-[6.25649881362915, 5.403759002685547, "[FF] Logic of the CPU Board = Realized with flash FPGA"]
-[13.390710830688477, 7.504950046539307, "[TT] Power of the NRA = 237 W"]
-[9.25088119506836, 8.612162590026855, "[TT] Slit Height of the Short Wavelength Band = 2.75 cm; 1/33 for bright target"]
-[5.887553691864014, -0.3777869641780853, "[TT] Mission Duration of the STEREO = 5 years"]
-[9.678173065185547, 4.0936689376831055, "[TT] Absolute Measurement Error of the Vector Magnetometer = < 1 nT"]
-[9.678238868713379, 1.4062354564666748, "[FF] Observation Content of the MIRIS = Images of M42 (Orion Nebula) and the Rosette Nebula"]
-[6.0088324546813965, 2.0086917877197266, "[FF] Deployment of the KickSat = about 250 femtosatellites into LEO (Low Earth Orbit)"]
-[14.163054466247559, 6.7675933837890625, "[FF] Battery Charging System Design of the SpriteSat = Mistake"]
-[5.676070690155029, -0.40303993225097656, "[TT] Mission Duration of the Falcon Heavy = Over six hours"]
-[8.595011711120605, 2.1290366649627686, "[TT] Pointing Knowledge of the SeaWinds = 500 arcseconds"]
-[13.376070976257324, 7.17056131362915, "[TT] Power Available to Payload of the S/C = 19 W (average), 120 W (peak)"]
-[6.4801130294799805, 4.002012252807617, "[FF] Ground Segment Responsibility of the MANTIS = Receiving and processing the satellite imagery up to Level 1C"]
-[6.286743640899658, 2.578793525695801, "[FF] Design of the Orion spacecraft = Uniquely designed for long-duration deep space flight"]
-[4.542984485626221, 6.452371120452881, "[TT] RF Communications of the Spacecraft = VHF beacon"]
-[7.34070348739624, -0.7236489653587341, "[TT] Repeat Cycle of the ICESat-2 = 91 days with subcycles of 29, 29, and 33 days"]
-[6.98661470413208, 5.456364631652832, "[TT] Quantity of the IMU = Single unit"]
-[5.28200626373291, 1.1551510095596313, "[FF] Presentation Date of the Texas 2 STEP = Aug. 11-14, 2008"]
-[5.101236820220947, 4.085424900054932, "[TT] Bus Name of the NorSat-1 = NEMO platform"]
-[9.493622779846191, 4.689744472503662, "[FF] ADCS of the NEMO-HD = Attitude Determination and Control System"]
-[6.884232521057129, -0.015159931033849716, "[TT] Repeat Cycle of the SeaSat = 17 days"]
-[13.792134284973145, 2.887622833251953, "[TT] Mass of the Flight Unit = 8.5 kg"]
-[11.183204650878906, 2.8383452892303467, "[TT] Maximum Microsatellite Mass of the NanoRacks Microsat Deployer = 100 kg"]
-[10.011305809020996, 2.9133248329162598, "[TT] Solar Panel Deployment Date of the ALBus CubeSat = December 16, 2018"]
-[7.526033878326416, 6.670610427856445, "[TT] Time Resolution of the PIXIE = 60 seconds or better"]
-[6.107776641845703, 3.4395341873168945, "[FF] Design Approach of the Constellation = Low cost and low risk, doesn't sacrifice performance"]
-[6.87300443649292, -0.41012123227119446, "[TT] Time of the Solar Maximum = End of 2000"]
-[6.505464553833008, 4.1313886642456055, "[FF] Block Diagram of the Ground System = Figure 16"]
-[7.516033172607422, 2.1961557865142822, "[FF] Purpose of the Marine Plastic Detection System = Detect marine plastic litter using satellites"]
-[6.513760089874268, 4.510112762451172, "[FF] Function of the Spacecraft Operation Planning System = Perform the planning of the satellite orbit control"]
-[5.226138114929199, 8.129839897155762, "[TT] Frequency Range of the Electric antennas (IME) = 10 Hz-20 kHz"]
-[7.745941162109375, 0.4548315703868866, "[TT] Orbit of the Lunar IceCube = Low orbit of only 62 miles above the surface of the moon"]
-[4.722818374633789, 1.5499509572982788, "[FF] Conference Date of the GCOM-W1 = 5-9 September 2011"]
-[4.540574550628662, -0.8687085509300232, "[TT] Arrival Date at Space Station of the Cargo Dragon = December 7"]
-[9.00774097442627, 5.531204700469971, "[TT] Pointing Accuracy of the Spacecraft = 2.1 arcsec absolute pointing accuracy"]
-[3.887193202972412, 4.422091484069824, "[TT] Average Monthly Acquisition Segments of the RADARSAT-2 = Over 4,200"]
-[4.952282905578613, 0.846860945224762, "[TT] Open Call Year of the OPS-SAT = 2013"]
-[6.238620281219482, 6.27574348449707, "[TT] Number of Digitiser modules of the Digital Back-End (DBE) = 6"]
-[4.8419013023376465, -1.5285651683807373, "[TT] Lander/Rover Soft Landing Time of the Tianwen-1 = 2\u20133 months after arrival of the spacecraft"]
-[7.527907848358154, 4.7333173751831055, "[TT] Mounting Location of the ShadowCam = Korean Aerospace Research Institute (KARI)"]
-[6.999128818511963, 3.740912437438965, "[FF] Unknown of the PROBA-2 = Unknown"]
-[13.052828788757324, 3.115217447280884, "[TT] Remaining Fuel of the Spacecraft = More than 120 kg"]
-[3.438218355178833, 5.492819309234619, "[TT] Mounting Location of the SAR Downlink Transmitter = On the mast"]
-[3.440603733062744, -0.87857586145401, "[TT] Orbit Type of the Meteor-M2-2 = Sun-synchronous orbit"]
-[9.304544448852539, 5.008105278015137, "[TT] Attitude Rate Measurements of the ABI = < 20 \u00b5rad drift over 15 minutes"]
-[6.305781841278076, 1.7730306386947632, "[FF] URL of the ISEE-1 and ISEE-2 = http://www-ssc.igpp.ucla.edu/personnel/russell/papers/ISEE_fluxgate/"]
-[6.588202953338623, 4.915829181671143, "[FF]  of the No devices were mentioned in the provided excerpt = "]
-[11.89747428894043, 5.47117280960083, "[FF] Instrument Dimensions of the SEVIRI = Diameter of about 1 m and a height of 2.1 m"]
-[14.182577133178711, 3.10615873336792, "[TT] Mass of the Biopan = 27 kg"]
-[12.103415489196777, 4.393606662750244, "[TT] Dimensions of the GRACE-FO satellites = Approximately 3 m x 2 m x 0.8 m"]
-[4.385517120361328, 3.080836057662964, "[TT] Location of the CSSS = 22 Wing in North Bay, Ontario"]
-[9.145319938659668, 2.8773250579833984, "[FF] Mission of the Voyager = Investigate the magnetospheres of planets and their moons, determine the physical mechanics and processes of the interactions of those magnetic fields and the solar wind"]
-[5.518786430358887, 5.764185905456543, "[TT] CPU of the STRV-2 DHS = 8086 rad-hard"]
-[10.163073539733887, 3.081394910812378, "[TT] Deployment Mechanism of the STRaND-1 = ISIPOD CubeSat dispenser of ISIS"]
-[5.077500343322754, 1.7258223295211792, "[FF] Damage of the Genesis capsule = The damage to SRC wasn't as severe as initially expected"]
-[7.880724906921387, -2.528756856918335, "[FF] Observation Capability of the GOLD = Simultaneous imaging of composition and temperature"]
-[7.894635200500488, 6.366821765899658, "[FF] Payload of the Sich-2 = Multispectral scanner, middle IR scanner, platform command & data handling subsystem, X-band communication subsystem"]
-[5.217519760131836, 2.1612701416015625, "[FF] Mission Objectives of the ZACUBE-2 = Aligned with those of MDASat-1"]
-[3.548527240753174, 3.57338809967041, "[TT] Owner of the PAZ = Hisdesat"]
-[6.856247901916504, 3.9399936199188232, "[FF] Design and Development of the ASPIICS = J.-Y. Plesseria, P. Levacher, W. Curdt, S. Vives, C. Guillon, A. Mazzoli, F. Rouesnel, A. Paschalis, N. Kranitis, A. Poulakidas, B. Fiethe, S. Shestov, S. Gunar, G. Capobianco, P. Lamy, P. Rochus, K. Tsinganos, S. Kuzin, P. Heinzel, S. Fineschi"]
-[9.462078094482422, 4.0119099617004395, "[TT] Frequency Range of the Magnetic Field Measurement System = 20 Hz - 1 kHz"]
-[8.766474723815918, 4.872562885284424, "[TT] Instrument Integration of the TanSat = Common structure and electronics device"]
-[6.6715874671936035, 4.75921630859375, "[FF] Factors Considered of the Subsystem Layout = Electrical requirements, interfaces, physical size, location feasibility, look angle, FOV requirements, thermal requirements, mechanical loads, transmissibility factors, physical parameters, balancing, ease of assembly/dis-assembly, accessibility"]
-[8.213263511657715, 4.743275165557861, "[FF] Onboard Innovations of the PROBA-1 = Gallium-arsenide solar cells, star trackers for gyroless attitude control, lithium-ion batteries, ESA\u2019s first ERC32 microprocessors"]
-[12.01091194152832, 4.5818986892700195, "[TT] Dimensions of the Spacecraft = 2.4 m (cylinder height), 3.7 m total height, 3.2 m diameter"]
-[6.870301246643066, -0.6397206783294678, "[TT] Orbital Period of the Satellites = 1 to 4 days"]
-[7.705013275146484, 4.303237438201904, "[FF] Purpose of the LPT = Improve the radiation environment knowledge and characterize the local radiation environment"]
-[9.335912704467773, 3.780127763748169, "[FF] Internal Magnetometer Calibration Method of the RAX-1 = Scalar based method that involved simple rotations of the satellite in a known magnetic field during ground calibration"]
-[9.696240425109863, 6.898437023162842, "[TT] Ground Sample Distance of the GHOSt Constellation = 8 metres"]
-[9.62304401397705, 7.663018703460693, "[TT] Pixel Scale of the Telescope = 15 \u00b5m"]
-[3.2374496459960938, 5.729652404785156, "[TT] Dimensions of the SAR antenna = 6.29 m x 2.09 m x 0.220 m"]
-[4.8440470695495605, 8.043686866760254, "[TT] Carrier frequency (MHz) of the E6-C = 1278.750"]
-[8.65357780456543, 1.1089496612548828, "[FF] Commissioning Update Date of the Aquarius = January 4, 2012"]
-[8.224974632263184, -0.46794313192367554, "[FF] Definition of the Arctic sea ice extent = Total area in which the ice concentration is at least 15 percent"]
-[7.6122846603393555, 3.382052421569824, "[FF] Contents of the Level-1B = Granule scene radiance data after radiometric correction and geometric correction processing"]
-[9.180169105529785, 2.9020705223083496, "[FF] Launch of the Coronal Mass Ejections = Launched in sequence one after another from the same active region"]
-[10.58086109161377, 3.3481574058532715, "[TT] Form Factor of the NEA Scout = Six-unit CubeSat"]
-[6.4044928550720215, 3.3842265605926514, "[FF] Importance of the Internet Connectivity = Extremely important due to the difficulty in obtaining information on the disaster in stricken areas"]
-[9.36471939086914, 4.990049362182617, "[TT] Attitude Prediction Accuracy of the ISS = Approx 0.2\u00ba for up to 4 days"]
-[9.758098602294922, 6.2768025398254395, "[FF] Rotation of the Calibration Mirror = Rotatable"]
-[10.614115715026855, 2.7611494064331055, "[TT] Distance Between Satellites of the DICE nanosatellites = ~300 km"]
-[13.769217491149902, 3.052032470703125, "[TT] Mass of the Corvus-BC satellites = 11 kg"]
-[13.21812915802002, 7.159939765930176, "[TT] Power Consumption of the BOKZ-M star tracker = 11.2 W"]
-[9.619311332702637, 0.7914619445800781, "[FF] Distance from Sun of the Solar Orbiter = About twenty percent of the way from the Earth to the Sun"]
-[10.727884292602539, 7.535882472991943, "[TT] Swath Width of the Spotlight-2B = 10km"]
-[5.135372161865234, 3.3339478969573975, "[TT] Development Funding of the TESAT payload = DLR German Aerospace Center"]
-[5.429880619049072, 0.3715698719024658, "[TT] Data Release Date of the Cheollian 2B = May 25, 2020"]
-[4.318994522094727, 2.2077434062957764, "[TT] Launch Site of the TanSat = Jiuquan Satellite Launch Centre in China"]
-[7.581076622009277, 4.185812950134277, "[TT] Carried Device of the Occulter Spacecraft (OSC) = Occulting Disk"]
-[8.35073471069336, 3.835731029510498, "[FF] Stray Light Source of the External Occulter = Diffraction by the EO (External Occulter) edge of the direct Sun light"]
-[7.022916793823242, 7.739474296569824, "[FF] Design of the RRA (RetroReflector Array) = Fizeau style reflectors similar in design to those used on Meteor-2-21"]
-[11.256709098815918, 4.132181167602539, "[TT] Size of the JY1-Sat = 1U"]
-[5.741913318634033, 7.132856369018555, "[TT] Source Data Rate per Band of the MSU-50 = 9.8 Mbit/s"]
-[6.1204633712768555, 4.004408359527588, "[FF] Development Partner of the ADRS = GOES-R GS"]
-[6.062593460083008, 5.480462074279785, "[FF] Design Philosophy of the EPS = Provide functional redundancy"]
-[5.241044521331787, 3.2896058559417725, "[TT] Responsible Organization of the PROBA-V = ESA"]
-[5.345468521118164, 8.071755409240723, "[TT] Frequency Range of the VMAG = 0 \u2013 8 Hz"]
-[8.756197929382324, 3.6633784770965576, "[FF] Leading Noise Terms of the Satellite = TM-to-satellite stiffness coupling to satellite motion"]
-[11.595160484313965, 4.426179885864258, "[TT] Size of the LICIACube = Hand-sized"]
-[9.733355522155762, -0.5754185318946838, "[TT] Orbit Altitude of the PRISMA = 614 km"]
-[12.441908836364746, 0.5889253616333008, "[FF] Observation Phases of the PLATO = Long continuous pointing phases and short duration pointing phases"]
-[9.71117877960205, 7.17526388168335, "[TT] Ground Resolution of the SUCHI = ~220 m"]
-[11.380900382995605, 4.352829456329346, "[TT] Size of the Irvine 02 = 1U"]
-[3.870983839035034, -2.1788814067840576, "[FF] Use Case of the Specialized Asset Trackers = Big productivity gains with a specific asset type"]
-[8.07536792755127, 3.58361554145813, "[FF] Observation of the OCO-3 = First dawn-to-dusk observations of how SIF varies over the course of a day"]
-[13.814217567443848, 3.0869836807250977, "[TT] Mass of Payloads of the FAST Program = Starting at just 1 kg"]
-[9.135148048400879, 1.3328806161880493, "[FF] Planned Mission Duration of the New Horizons = 2023 through 2025"]
-[8.348934173583984, 7.142290115356445, "[TT] Quantity of the Cameras = 2"]
-[5.0130462646484375, 3.3303911685943604, "[TT] Manufacturer of the PACE = NCKU (National Cheng Kung University)"]
-[13.7743501663208, 3.079108238220215, "[TT] Mass of the Payload = 25 kg"]
-[8.625131607055664, 3.0387589931488037, "[TT] Ion Region of Atmosphere of the TRACE = Photosphere"]
-[3.457407236099243, 1.914624810218811, "[FF] Launch Vehicle of the Sentinel 2 = Sentinel 2 satellite"]
-[9.26411247253418, 7.146162509918213, "[TT] Vertical Resolution of the VISION = 2 km"]
-[9.297385215759277, 3.22060489654541, "[FF] Components of the Coronagraph Instrument = Optical Bench Assembly (CGI-OBA) and the Tertiary Collimator Assembly (TCA)"]
-[5.7057294845581055, -0.8950051069259644, "[TT] Design Life of the S/C = 2 years"]
-[7.497376441955566, 1.324374794960022, "[FF] Image Catalogue Availability of the SeaSat-1 = Freely available"]
-[6.029428958892822, 6.399392127990723, "[TT] Data Transfer Time of the Data Transfer Interface = Approximately twenty-four hours"]
-[9.158679962158203, 3.106717348098755, "[FF] Objective of the Electron Spectrometer = Provide high time resolution (<1 s) solar wind electron, full 3D distribution function observations"]
-[9.722610473632812, 7.429839611053467, "[TT] Cross-Track Swath of the OMPS Nadir Profile Spectrometer = 250 km"]
-[6.282938480377197, 3.8784730434417725, "[FF] Mission Operation Concept of the VEN\u00b5S = Unknown"]
-[5.343409061431885, 7.6259002685546875, "[TT] G/T of the LET = > 28.5 dB/K"]
-[9.687512397766113, 8.320562362670898, "[TT] FOV (Field of View) of the Instrument = \u00b1 43\u00ba along track; \u00b1 51\u00ba cross track"]
-[7.62883996963501, 5.718034744262695, "[FF] Structure of the EO module = Similar to that of the Imager"]
-[12.620323181152344, 9.097417831420898, "[TT] Equator Crossing Time of the ResourceSat-2A = 10:30 AM"]
-[5.428915023803711, 2.8275043964385986, "[TT] Led by of the In-situ component = EEA (European Environmental Agency)"]
-[4.947552680969238, 7.11622953414917, "[TT] Uplink Rate of the SGLS Link = 2 kbit/s"]
-[8.861644744873047, 7.371077060699463, "[TT] Sensor of the WorldView-3 = SWIR"]
-[6.776106357574463, 6.0093464851379395, "[TT] Number of Nodes of the FODB = 2 to 128"]
-[9.40208911895752, 6.992859840393066, "[TT] Resolution of the ScanSAR-2 = 6 x 20m"]
-[8.29671859741211, 7.5705976486206055, "[TT] Detector Quantity of the TIR Subsystem = 10"]
-[8.644869804382324, 5.937419414520264, "[TT] Measurement Accuracy of the CLS (Coarse Lateral Sensor) = \u00b113 m @ 150 m (lateral)"]
-[4.146200656890869, 0.21661600470542908, "[TT] Landing Date of the Falcon 9 first stage = Jan. 11, 2015"]
-[7.8213210105896, 1.5420926809310913, "[FF] Purpose of the GPM (Global Precipitation Measurement) Mission = Study global precipitation, evaporation and the water cycle"]
-[10.726347923278809, 2.201044797897339, "[FF] Field of View of the XMM-Newton observatory = Large"]
-[9.545858383178711, -1.061989188194275, "[TT] Location of the GOMS-1 = 76.5\u00ba East"]
-[3.7187159061431885, 6.668801784515381, "[TT] Beamwidth of the Yagi Antenna = 45\u00ba"]
-[7.474149227142334, 7.6052021980285645, "[TT] Dynamic Range of the Radiometry = 0-380 Wm -2  sr -1"]
-[6.318879127502441, -0.4551527798175812, "[TT] Duration of the EM-1 = 25 days (6 at destination)"]
-[7.273824214935303, 3.7863523960113525, "[FF] Ranging Signals of the GIOVE-A = Can be used to generate a complete set of GNSS measurements: ranges, carrier phases, Doppler measurements and carrier-to-noise ratios"]
-[5.712862014770508, 6.3599019050598145, "[TT] Capacity of the Solid State Recorders = 24 GB"]
-[9.809798240661621, 8.133694648742676, "[TT] Aperture of the LWIR Camera = 131 mm"]
-[8.075499534606934, 2.132718801498413, "[FF] In-Flight Calibrations of the OCI = Cross-platform in-flight calibrations with SeaWiFS on the SeaStar spacecraft of OrbImage"]
-[13.140902519226074, 5.668900012969971, "[FF] Arcing Detection Monitoring of the High-voltage solar array and the TJ arrays = Required"]
-[9.828472137451172, -0.5170642137527466, "[TT] Altitude of the Satellite Orbit = ~666 km"]
-[9.426267623901367, 6.691837310791016, "[TT] Resolution of the MRS = 21-23 m (Azimuth) x 8 m (Range)"]
-[6.640536308288574, 1.0300090312957764, "[TT] Discovery Date of the Solar Dynamics Observatory = 24 years ago"]
-[8.13109016418457, -0.6070441603660583, "[FF] Image Content of the OPS-SAT = Arctic Laptev Sea with large amounts of drift ice"]
-[4.8640313148498535, 1.50033700466156, "[FF] Second Anniversary of the Gokturk-2 = Gokturk-2 Celebrates Second Anniversary"]
-[9.620072364807129, -0.29655206203460693, "[TT] Altitude Above Ground of the Lunar Landing Vehicle = 100 m"]
-[6.37360954284668, -0.6612358689308167, "[TT] Observation Duration of the TanSat = 8-10 minutes"]
-[4.147136688232422, 7.228996276855469, "[TT] Band of the Severyanin-M = X-band"]
-[10.908660888671875, 10.097919464111328, "[FF] Data Cable of the Alpha Magnetic Spectrometer (AMS) = Connected"]
-[6.099086284637451, 2.4225049018859863, "[FF] Affiliations of the Keith Masback = Mapping Sciences Committee of The National Academies of Sciences, Engineering, and Medicine"]
-[8.406586647033691, -0.1644354909658432, "[TT] Area of the Colorado River basin = 246,000 square miles (637,000 km2)"]
-[10.860147476196289, -0.29459136724472046, "[TT] Bistatic Phase of the TanDEM-X = March 2015 to September 2015"]
-[10.537336349487305, 4.747101306915283, "[FF] Electrical Isolation Method of the Hinge Pin = Shrink tube"]
-[10.524580001831055, 3.2389745712280273, "[TT] Spacecraft Type of the ARMADILLO = Nanosatellite (3U CubeSat)"]
-[6.141125202178955, 6.99804162979126, "[TT] Optical Downlink Rate of the Follow-on Optical Downlink Demonstrators = Approaching 1 Gbit/s"]
-[4.541378021240234, 1.291300892829895, "[TT] Launch Date of the AlSat-2A = July 2010"]
-[5.200084686279297, 5.456855297088623, "[TT] Topology of the IXV Communications Network = Star"]
-[11.756834030151367, 6.753862380981445, "[TT] Energy Range of the CXBN-2 = 30-50 keV"]
-[9.448065757751465, 5.4787187576293945, "[TT] Earth Exclusion Angle of the STARE satellites = 85\u00ba"]
-[8.403587341308594, 6.630522727966309, "[TT] Spectral Sampling of the TEMPO instrument = 0.2 nm"]
-[8.14845085144043, -0.9228481650352478, "[FF] Application of the Lidar Instrument = Quantify the polar ice sheet mass balance"]
-[11.02278995513916, 6.297518253326416, "[TT] Mirror Material of the SMA = Silicon carbide"]
-[8.073657035827637, 5.22086763381958, "[FF] Radiometric Accuracy of the Calibration Techniques = Specified"]
-[10.335747718811035, 2.1732873916625977, "[FF] X-ray Light Production of the Planet's Auroras = Low-energy X-ray light"]
-[7.058965682983398, 3.4219303131103516, "[FF] Number of Passes Over a Storm of the Weather Satellites = One or two in an entire day"]
-[7.091182231903076, 1.7251789569854736, "[TT] Status of the ACS = Reentered the Earth's atmosphere on Nov. 16, 1999"]
-[6.537514686584473, 5.497067451477051, "[FF] Functional Blocks of the CAMEX chip = Current source to bias the pnCCD JFET, JFET preamplifier for pnCCD signal amplification, Programmable RC low pass for bandwidth limitation, Eight-fold correlated double sampling filter, Sample and hold stage, 128 to 1 multiplexer, Output buffer, On-chip digital sequencer (16 x 64 bit), Serial programming interface with LVDS, Option of integrated bias current DACs (digital analog converters)"]
-[5.6738176345825195, -0.011642323806881905, "[FF] Mission Duration of the Ulysses = 16 years"]
-[3.642385482788086, 5.705165863037109, "[TT] PRF of the Radar = 1500 to 3000 Hz"]
-[11.045703887939453, 3.8572819232940674, "[TT] Size of the NEA Scout = 6U"]
-[9.22107219696045, 1.3182408809661865, "[TT] Remaining Data Transmission Completion of the New Horizons = By October"]
-[8.340353012084961, 0.5703909397125244, "[FF] Comparison of the Kuiper Belt = Big brother of the asteroid belt"]
-[4.821686267852783, 0.6103206276893616, "[TT] Launch Date of the OPAL = Jan. 27, 2000"]
-[6.820601940155029, 7.033209800720215, "[TT] Number of Beams aiming toward Asia/Pacific of the MBA System = 7"]
-[6.30825662612915, 3.0566012859344482, "[FF] Image Credit of the SSM/I radiometer = DMSP Program Office USAF, NOAA"]
-[4.440009117126465, 7.493552207946777, "[TT] Gain on transmit of the Downlink (Ku-band) = 19.6 dBi"]
-[13.348474502563477, 7.801262378692627, "[TT] Power of the L-band Transmitter = 10 W"]
-[11.636536598205566, 4.865413188934326, "[TT] Functionality of the PCU = High"]
-[9.589993476867676, 5.3263654708862305, "[TT] Accuracy of the Lateral Shearing Angular Period = 206 mas"]
-[4.434788703918457, 4.577248573303223, "[FF] Purpose of the SARSAT = Support search and rescue operations"]
-[4.808310508728027, 5.616497039794922, "[FF] Function of the Onboard Receiver = Measure Doppler shift"]
-[10.766755104064941, 2.1203458309173584, "[FF] Telescope of the XMM-Newton = Large Binocular Telescope (LBT) in Arizona"]
-[8.450346946716309, 0.772170901298523, "[TT] Utilization of the ICI-8 = Cloud ice water path and cirrus"]
-[3.6119441986083984, 6.001969814300537, "[FF] Configuration of the Reflectarray Antenna = Three panels, electrically tied together through hinges, with an array of printed circuit board patches on them"]
-[6.6123199462890625, 2.3916356563568115, "[FF] Thermal Stability of the Euclid = Maintained during slew maneuvers"]
-[9.773058891296387, -0.5297918915748596, "[TT] Orbit Altitude of the Hubble = 350 miles"]
-[5.516462326049805, -0.5035447478294373, "[TT] 3rd Lunar Night Time Hibernation Period Start Date of the Yutu = Feb. 22, 2014"]
-[10.561553955078125, 7.518396854400635, "[TT] Swath Width at Nadir of the Telescope = 30 km"]
-[5.228567123413086, 7.186968803405762, "[TT] Image Telemetry Link of the SPOT-1 = 50 Mbit/s at 8 GHz"]
-[3.9836227893829346, 6.142420291900635, "[FF] Design of the Antenna Dish = Rib consists of an inner and outer portion, connected by a spring-loaded hinge joint"]
-[6.230681419372559, 2.5553150177001953, "[FF] Function of the Orion's service module = Fuel and propel the Orion spacecraft in space"]
-[4.964778423309326, 1.1848387718200684, "[TT] Signal Broadcast Start Date of the GIOVE-A = January 12, 2006"]
-[7.63655424118042, 6.3648786544799805, "[TT] Count Rate of the XGRE = 104 \u2013 105 cm-2 s-1"]
-[4.430655002593994, 7.744194030761719, "[TT] Downlink Frequency of the Myriad RF board = 300 MHz up to 3.8 GHz"]
-[11.608152389526367, 5.566040515899658, "[TT] Bus Structure of the Tsubame = Lattice structure (CFRP material)"]
-[10.305867195129395, 5.777993202209473, "[TT] Temperature of the OBCT = Approx. 273 K"]
-[6.227676868438721, 0.6897858381271362, "[TT] Scheduled Launch Date of the Gaia = 20 December"]
-[11.784467697143555, 6.758255481719971, "[TT] Electron Isotropy Boundaries Energy Range of the ELFIN = 0.5-5 MeV"]
-[6.0736894607543945, 2.4183480739593506, "[TT] Collaboration Director of the Astrocast = Renaud de Watteville"]
-[10.028996467590332, -1.6279749870300293, "[TT] Inclination of the AlSat-2B = 98.1\u00ba"]
-[5.268031120300293, 4.821279048919678, "[TT] Function of the SGR-ReSI = Platform GNSS receiver"]
-[14.07121467590332, 4.046382904052734, "[TT] Mass of the CLARA Instrument = 2.63 kg"]
-[3.1712732315063477, 2.2153759002685547, "[TT] Operator of the Copernicus Programme = European Commission"]
-[7.216348171234131, 1.2462456226348877, "[FF] Function of the Earth Return Orbiter = Capture the sample container orbiting Mars"]
-[5.002721309661865, 7.35567569732666, "[TT] Transmission Rate of the RF communications = 640 Mbit/s"]
-[10.354880332946777, 6.873315811157227, "[FF] Unknown of the Metal mirror TMA = Unknown"]
-[9.420119285583496, 3.8688437938690186, "[FF] Components of the MIAS = Overhauser scalar magnetometer (OVM), two fluxgate vector magnetometers (FGM), and two-star imagers"]
-[6.056266784667969, 2.44431209564209, "[FF] Disciplines of the Spacelab-1 = Atmospheric science, solar science, materials science, space plasma physics, the life sciences, astrophysics"]
-[8.104612350463867, 8.403282165527344, "[TT] Spectral Range of the IRFS-2 Infrared FTS = 5-15 \u00b5m"]
-[14.169089317321777, 3.05196475982666, "[TT] Mass of the SPROUT = ~7.1 kg"]
-[4.39232873916626, 7.851035118103027, "[TT] Downlink Frequency of the L-3 Communications Cadet UHF nanosatellite radio = 468 MHz"]
-[9.784553527832031, 8.14371395111084, "[TT] FOV Resolution of the HORUS = 5.35 arcsec"]
-[3.2815651893615723, 5.040064811706543, "[TT] Abbreviation of the HRWS = High-Resolution Wide-Swath SAR"]
-[3.205129623413086, 2.2474794387817383, "[FF] Measurement Technique of the Sentinel-6 Michael Freilich = Synthetic aperture radar"]
-[7.536757946014404, 2.644857168197632, "[FF] Data Matching of the CYGNSS = SFMR data, dropsonde data from the P3 Orion for every named storm"]
-[5.773871898651123, -0.8298074007034302, "[TT] Design Life of the TanSat = 3 years"]
-[6.100790023803711, -0.41636812686920166, "[TT] Duration of the Request for Proposal = 12\u2013 to 18\u2013month period"]
-[10.168370246887207, 4.038711071014404, "[TT] Boom Length of the Overhauser magnetometer = 8 m"]
-[13.977636337280273, 7.050708770751953, "[TT] Operating Voltage of the RPI = 3 kV"]
-[14.036979675292969, 4.133621692657471, "[TT] Parameters of the Instrument mass, power = 450 kg, 400 W"]
-[8.939643859863281, 5.718022346496582, "[TT] Pointing Accuracy of the Fine Guidance Sensor = Few tenths of an arcsecond"]
-[10.39582633972168, 4.408764362335205, "[FF] Reaction Wheel of the CanX-2 = 30 mNms nanosatellite reaction wheel"]
-[8.340670585632324, 7.948034763336182, "[TT] PDA Chip Pitch of the SWIR Detector = 25 \u00b5m"]
-[10.273016929626465, 4.5409064292907715, "[TT] Performance of the SFL/Sinclair Interplanetary Miniature Wheel = Solid performance"]
-[8.522810935974121, 1.786501407623291, "[TT] Range of values of the Cloud water = 0-1"]
-[8.143915176391602, 6.7098469734191895, "[TT] Temporal Resolution of the GLI = 2 seconds"]
-[11.313203811645508, 0.9347456097602844, "[TT] LTP Operations Duration of the LISA Pathfinder = 90 days"]
-[7.656278133392334, 7.998454570770264, "[TT] SNR of the HSC-III = > 100"]
-[3.411383867263794, 3.628074884414673, "[FF] Operation al Concept Presentation Date of the PAZ Ground Segment = June 3-5, 2014"]
-[14.243613243103027, 3.1761863231658936, "[TT] Mass of the Belka = 250 kg"]
-[5.21367883682251, 2.8252720832824707, "[TT] Designing University of the VisionCube-1 = Korea Aerospace University (KAU)"]
-[6.112913131713867, 1.7680870294570923, "[FF] URL of the GPM Core = http://www.spaceflight101.com/gpm-core-mission-updates.html"]
-[6.1862335205078125, 5.563732624053955, "[TT] Principle of the EMOC = Transparency"]
-[8.652627944946289, 4.71359395980835, "[FF] Sun-Glint Observation Mode of the TanSat = Observation Mode"]
-[11.740344047546387, 3.322275161743164, "[TT] Quantity of the Propulsion System = 8"]
-[6.229490756988525, 3.395451784133911, "[TT] Constellation Size of the BlackSky = 14 Earth observation satellites"]
-[4.9679951667785645, 0.48714855313301086, "[TT] Scheduled Date of the Launch = 14 March"]
-[8.142237663269043, 1.4130209684371948, "[TT] Composition of Enhanced Aerosol of the Calbuco Volcano Eruption = Sulfate"]
-[5.113772869110107, 0.619387149810791, "[TT] Deployment Date of the BX-1 = Sept. 27, 2008"]
-[6.196633338928223, 3.3459291458129883, "[FF] Constellation Partners of the GPM Constellation = DMSPs from the U.S. Department of Defense, GCOM-W from JAXA, Megha-Tropiques from CNES and ISRO (Indian Space Research Organization), the NOAA series Suomi-NPP from NOAA-NASA, and MetOps from EUMETSAT"]
-[4.534687042236328, -0.9048720598220825, "[TT] Capture Date of the Dragon spacecraft = 17 Dec. 2017"]
-[11.32441520690918, 5.1855058670043945, "[TT] Length of the LED-bearing target = 33-m long"]
-[9.71142578125, 4.635437965393066, "[TT] Usage of the ASC (Advanced Stellar Compass) = Only at a low (<4.5 rpm) spin rate"]
-[10.218387603759766, 8.05607795715332, "[TT] Aperture of the Telescope = 30 cm"]
-[5.808814525604248, -2.1099414825439453, "[TT] Orbital period of the KOMPSAT-3 = 98.5 minutes"]
-[6.13700008392334, 6.392580509185791, "[TT] Latency of the TAO/Triton = 1 day"]
-[10.508899688720703, 7.50328254699707, "[TT] Swath Width of the IRIS Instrument = 50 km"]
-[8.423089981079102, 7.384470462799072, "[TT] Sensor Type of the CMOS Camera = CMOS"]
-[5.209989547729492, 6.84409761428833, "[TT] Data Downlink Rate of the ICESat-2 = 220 Mbit/s"]
-[9.01960563659668, 3.2431700229644775, "[FF] Intensity Variations of the Solar Disk = Neglected"]
-[13.845324516296387, 3.0719354152679443, "[TT] Mass of the SpaceCube 2 = 1.9 kg"]
-[13.864891052246094, 6.951534271240234, "[TT] Voltage of the SCM = 300 V"]
-[9.543400764465332, 1.2924786806106567, "[TT] Ejection Velocity of the ICU = At least 0.5 m/s"]
-[5.97475004196167, -0.24917156994342804, "[FF] Impact on Mission Planning of the GOCE = Weekly replanning activity required"]
-[9.566455841064453, 4.7519989013671875, "[FF] Stabilization of the ADEOS = 3-axis stabilized with zero momentum attitude control"]
-[4.888047695159912, 1.7989469766616821, "[TT] Operation Status of the Gokturk-2 = Nominal"]
-[9.132499694824219, 2.843663454055786, "[FF] Justification of the ACE = Providing context and supporting data to nearly all other solar, heliosphere, magnetosphere, and ionosphere/thermosphere missions both current and planned"]
-[10.925738334655762, 7.364024639129639, "[TT] Swath of the Satellite = 55 km"]
-[6.51411247253418, 6.568412780761719, "[FF] Communication Method of the EDRS-C = Laser and radio-frequency transmissions"]
-[5.435731887817383, 0.6555280089378357, "[FF] Time Extension Date of the BEAM = 4 Dec. 2017"]
-[10.425981521606445, 4.081044673919678, "[TT] Boom Length of the CHAMP = 4 m"]
-[6.958446025848389, 9.034510612487793, "[TT] Band Center of the POLDER-1/2 = 765 nm"]
-[6.694807052612305, 6.6692891120910645, "[TT] Repetition Rate of the Drifting (Mobile) Platforms = 90 - 150 seconds"]
-[8.088311195373535, -0.9766845703125, "[TT] Precision of the ICESat-2 = High"]
-[7.271459579467773, 4.815179347991943, "[FF] OpNav Process of the Spacecraft = Optical Navigation"]
-[5.671728610992432, 3.1905343532562256, "[TT] Contract Value of the Planet = $20 million"]
-[14.053391456604004, 3.1781086921691895, "[TT] Mass of the NSCAT = 280 kg"]
-[5.77164888381958, 0.6904435753822327, "[FF] Publication Date of the Cluster = 19 December 2014"]
-[9.113439559936523, 5.489030361175537, "[TT] Pointing Requirements of the AOCS = 2\u00ba about all axes"]
-[4.76772403717041, 7.2298197746276855, "[TT] Downlink Data Rate of the S-band RF Communications = 400 kbit/s"]
-[8.674046516418457, 4.725212097167969, "[TT] Quantity of the Star Tracker Heads = 3"]
-[10.611611366271973, 5.534385681152344, "[TT] Improved by of the Electron Temperature Probe = K. Oyama"]
-[6.3254594802856445, 2.8050150871276855, "[FF] Monitoring of the CBPSS = Monitor the progress in implementation of the recommendations of the RFSE (Recapturing a Future for Space Exploration): Life and Physical Sciences Research For a New Era decadal survey"]
-[5.413416385650635, 6.418959140777588, "[TT] Storage memory Capacity of the Payload data management = 64 to 79 Gbit BOL"]
-[10.19994831085205, 1.516491174697876, "[TT] Number of Observed Clusters of Galaxies of the eROSITA = Ten thousands"]
-[4.934592247009277, 0.7891417145729065, "[TT] Launch Date of the Aalto-1 = Feb, 5, 2012"]
-[11.58260440826416, 5.03977632522583, "[TT] Width of the Graphite Spacers = 1.2 mm"]
-[10.375754356384277, 5.603694915771484, "[TT] Temperature of the Thermosphere = Up to 2,700 \u00b0F (1,500 \u00b0C)"]
-[11.604723930358887, 3.2531094551086426, "[TT] Cycle Life of the Ion Thruster = GOCE requirement: > 1000 On/Off cycles"]
-[6.437318801879883, 0.04926447942852974, "[TT] Planning Cycle of the TDP Operations = Weekly incremental cycle"]
-[4.907346725463867, 0.9155725836753845, "[TT] Second Flight Date of the MEPSI = July 2001"]
-[9.233466148376465, 1.7805616855621338, "[TT] Signal Repeating Interval of the HARPS = 36 days"]
-[11.436223983764648, 5.714903831481934, "[TT] Material of the Inconel 718 = Nickel alloy"]
-[6.355246543884277, 3.6031556129455566, "[FF] Plans of the ESA = Develop a range of \u2018in-orbit servicing\u2019 technologies that will refuel, refurbish and de-orbit spacecraft"]
-[10.137714385986328, 5.315650463104248, "[TT] Cryocooler of the MWIR = Stirling cycle cryocooler"]
-[6.493082523345947, 4.409257411956787, "[FF] Function of the GS = Maneuver planning and scheduling for routine operations as well as special operations such as station keeping, annual yaw flips, and engineering or science investigations outside of normal operations"]
-[4.827754020690918, 7.217987537384033, "[FF] TC (TeleCommanding) capacity of the EESS S-band = Increase"]
-[8.127297401428223, 1.6380338668823242, "[FF] Effect of the Water Cycle = Moves heat"]
-[4.852481842041016, 3.3772149085998535, "[TT] Location of the JPSS Ground System = Global"]
-[9.651820182800293, 8.395994186401367, "[TT] FOV (Field of View) of the Antenna = 8\u00ba in azimuth 7\u00ba in elevation"]
-[11.517377853393555, 6.662972450256348, "[TT] Energy Band of the eROSITA = 0.6-1.0 keV"]
-[10.270731925964355, 5.705848693847656, "[TT] Deep Space Radiant Temperature of the AMSR = About 3 K"]
-[11.668112754821777, 4.861393928527832, "[TT] Size of the S/C = 50 cm in diameter and 93 cm in height"]
-[6.042386054992676, 2.4152798652648926, "[TT] Plaque Designer of the LAGEOS = Carl Sagan"]
-[9.756919860839844, -0.3951164186000824, "[TT] Groundtrack Mission Requirement of the EO-1 = Fly over the current groundtrack of Landsat-7 within \u00b13 km"]
-[11.998034477233887, 5.013501167297363, "[TT] Volume of the DeMi = ~4.5U"]
-[4.075843811035156, 6.282299995422363, "[TT] Placement of the Patch Antennas = On opposite side of the spacecraft"]
-[8.807537078857422, 5.349878311157227, "[TT] Pointing System of the Harris TANSO-FTS-2 = Agile and intelligent"]
-[5.570910930633545, -2.0275509357452393, "[TT] Image Resolution of the KOMPSAT-3 AEISS = 0.7 m"]
-[5.178557872772217, 2.5238592624664307, "[FF] Objective of the PhoneSat-1 and -2 = Use a commercial mobile telephone (smartphone) as an avionics system in a nanosatellite"]
-[8.47760009765625, 5.024410247802734, "[FF] Movement of the Telescope System = Along-track, across-track, or both"]
-[7.672867774963379, 8.980928421020508, "[TT] Spectral Range (Band 2) of the MUX = 0.52-0.59 \u00b5m"]
-[14.619771003723145, 6.643553256988525, "[TT] Battery Type of the Canopus Pipper = Molicel 18650 Li-ion batteries"]
-[13.673262596130371, 2.9933972358703613, "[TT] Payload Lift Performance to Geostationary Transfer Orbit of the Ariane 5 = Approximately 10,660 kg"]
-[6.138885974884033, 2.5453386306762695, "[TT] Developer of the Carruthers Geocorona Observatory = Ball Aerospace"]
-[7.040623664855957, 4.181685924530029, "[FF] Unknown of the Figure 29 = Unknown"]
-[5.086627960205078, 7.10693883895874, "[TT] Uplink Data Rate of the TT&C Subsystem = 2 k bit/s"]
-[5.91730260848999, 8.638540267944336, "[TT] MTF (Modulation Transfer Function) of the Channel = > 0.23"]
-[3.816939353942871, 7.922712802886963, "[TT] Modulation Scheme of the High-speed link = GFSK (Gaussian Frequency Shift Keying)"]
-[7.937571048736572, 9.13207721710205, "[TT] Wavelength of the LORE = 760 nm"]
-[8.409208297729492, 1.3223108053207397, "[TT] Soil Moisture Products Availability of the Aquarius = December 2013"]
-[10.559711456298828, 4.957056045532227, "[TT] Manufacturer of the Langmuir Probe = Center for Space Science and Applied Research of the Chinese Academy of Science"]
-[5.019954204559326, 1.538888692855835, "[FF] User Information Presentation of the Himawari-8/9 = May 13, 2013"]
-[14.184410095214844, 3.2306840419769287, "[TT] Mass of the HawkEye = 13.4 kg each"]
-[7.22269344329834, 4.316752910614014, "[FF] Function of the CIRC GTM = Perform ground calibration and carry out field observations"]
-[10.381153106689453, 7.2048726081848145, "[TT] Full Disk Circle Width of the ABI = 5000 km"]
-[7.915874481201172, 8.630528450012207, "[TT] Spectral Bands of the WPM = B13: 450 \u2013 520 nm, B14: 520 \u2013 590 nm, B15: 630 \u2013 690 nm, B16: 770 \u2013 890 nm"]
-[6.150978088378906, 5.9629034996032715, "[FF] Functions of the CIB = 1. Run a reliable link between the SSRU and the OBC ( Onboard Computer) 2. Operate the functionality of SSRU"]
-[9.618365287780762, 4.478206634521484, "[FF] Radial Trends of the SWAP = Unknown"]
-[5.503883361816406, 5.564040660858154, "[FF] Built-in Components of the THD-7 radios = AX.25 Terminal Node Controllers (TNCs) and RS-232 ports"]
-[4.704446315765381, 1.9990168809890747, "[TT] Provider of the GCOM-W1 = JAXA"]
-[14.236628532409668, 3.2338175773620605, "[TT] Mass of the M2 = 0.3 kg"]
-[10.445205688476562, 3.3179008960723877, "[FF] Structure of the XI-IV = Conforms to the requirements of the CubeSat program in size and mass"]
-[2.9233975410461426, 4.454682350158691, "[TT] Minimum Spatial Resolution of the PALSAR-2 = 3 m"]
-[8.029281616210938, -0.9941532611846924, "[FF] Data Usage of the ICESat-2 = Near-shore mapping, monitoring coral reefs, coastal mangroves, sediment transport, carbon storage capacity, water clarity, invasive species, and coastal dynamics"]
-[7.307454586029053, 8.962553977966309, "[TT] Transmission Profile FWHM of the Lyot-Michelson Filter System = 76 m\u00c5"]
-[5.287412166595459, 1.1578923463821411, "[FF] Project Date of the SOMP = September 8-10, 2009"]
-[13.533936500549316, 6.550907135009766, "[TT] Orbit Average Power of the COMMx = 200 W"]
-[5.249857425689697, 0.6571969985961914, "[TT] Safe Mode Entry Date of the Chandra = 12 October 2018"]
-[7.660599231719971, 3.2335143089294434, "[FF] Purpose of the HISUI = Earth imaging system that can benefit agriculture, forestry and other environmental areas"]
-[6.407915115356445, 2.356466293334961, "[FF] Ground Sites of the ARTEMIS = MOD (Ministry of Defense) ground sites"]
-[10.166302680969238, 1.3593212366104126, "[TT] Number of Objects of the Gaia Catalogue of Nearby Stars = 331,312"]
-[6.026454925537109, 5.988419055938721, "[TT] Quantity of the Memory Modules = 3"]
-[7.998961925506592, 8.45840835571289, "[TT] Spectral Range of the FTHSI = Visible to far-infrared"]
-[6.074466228485107, -0.2655758261680603, "[TT] Duration of the Crew-1 = Six-month"]
-[11.884291648864746, 4.917578220367432, "[TT] Size of the Digital Processing Unit = 46 cm x 19 cm x 31 cm"]
-[7.877697944641113, 9.16976261138916, "[TT] Wavelength of the Radio Waves = Decameter"]
-[11.346489906311035, 5.8477606773376465, "[TT] Primary Structure Material of the Sensor Module = Aluminum alloy"]
-[6.499896049499512, 5.817338466644287, "[FF] Attachment Location of the Optical Intersatellite Link units (OISLs) = +Z face of the spacecraft and one on the -Z face"]
-[7.5645036697387695, 2.0044028759002686, "[FF] ScanSAR ortho-slope corrected path of the Biosphere = For quasi-deforestation monitoring of pantropical regions, i.e., Brazil, Indonesia"]
-[7.827596187591553, 1.2944475412368774, "[FF] Cyclone Yasi Rainfall Date of the TRMM = Feb. 7, 2011"]
-[11.008976936340332, 3.4967756271362305, "[FF] Impact on Thrust of the Solar Activity = Isolated peaks of IPA thrust"]
-[8.384275436401367, 7.674516201019287, "[TT] Detector of the Spectral Band A = Si-PIN"]
-[6.410984039306641, 0.6589913368225098, "[TT] Anniversary Date of the Landsat = July 23, 2012"]
-[8.602094650268555, 7.692431926727295, "[FF] QE Variation of the Detector Arrays = Sub-pixel level"]
-[12.189001083374023, -0.06119981408119202, "[TT] Long-pass Filter Coating of the TESS Lens = Cutoff at 600 nm"]
-[3.191746234893799, 3.8718361854553223, "[TT] SAR Products Release Time of the TerraSAR-X = 5.5 months after launch"]
-[7.8317179679870605, 8.95590591430664, "[TT] Wavelength of the Instrument = 2.3-3.8 \u00b5m"]
-[7.255621433258057, 8.091761589050293, "[TT] Background Noise Reduction Method of the IXAE = Mutual anti-coincidence fashion"]
-[5.799010753631592, 6.580781936645508, "[TT] Data Collection of the Aleph Satellite = Up to 1,000 scenes per day"]
-[6.672842979431152, 5.843025207519531, "[TT] Total Racks of the PM = 23"]
-[11.90811824798584, 5.415114402770996, "[TT] Dimensions of the Field Measurement Device = 150 mm x 85 mm x 40 mm"]
-[10.368099212646484, -1.389166235923767, "[TT] Deployment Orbit Inclination of the SLATS = 97.9\u00ba"]
-[6.4567179679870605, 5.797279357910156, "[TT] Equipment Quantity of the MC3 CGA = 1 computer rack"]
-[3.7585361003875732, 7.147474765777588, "[TT] Antenna Gain of the GPSRO Sensor = Over 10 dBi"]
-[11.382938385009766, 4.3859357833862305, "[TT] Size of the CP-7 = 1U"]
-[4.309605598449707, 7.209039211273193, "[TT] Communication Link of the FFRF = Dual-frequency S-band"]
-[9.602959632873535, 8.074478149414062, "[TT] Optics of the CASPR = iSIM-90 optics"]
-[5.123074531555176, 8.477333068847656, "[TT] Bandwidth (MHz) of the PMI = 350"]
-[9.322057723999023, 5.170176982879639, "[TT] Placement of the Test Masses = Float freely within the spacecraft"]
-[4.906316757202148, 3.2064318656921387, "[TT] Manufacturer of the HumSat-D = University of Vigo, Spain"]
-[8.318010330200195, 1.4887677431106567, "[FF] Objective of the ALRad = Measure SSS (Sea Surface Salinity)"]
-[9.866537094116211, 7.886290073394775, "[TT] On-axis Resolution of the Mirror System = \u2264 1 arcmin"]
-[4.0143141746521, 6.392004489898682, "[FF] Downlink Antenna of the Satellite = Narrow beam"]
-[9.446881294250488, 7.870176315307617, "[TT] Max Frame Rate of the Telescope = 232 Hz"]
-[10.010357856750488, 6.6028008460998535, "[FF] Operation Characterization of the Deformable Mirror = Requires stable wavefront"]
-[13.376480102539062, 7.339014530181885, "[TT] Power Requirement of the DORIS = 20 W"]
-[7.616553783416748, 4.9502787590026855, "[FF] Navigation Algorithm Optimization of the Lander = Required"]
-[14.243247032165527, 3.204599142074585, "[TT] Mass of the Norton = 10.8 kg"]
-[8.845988273620605, 9.41089153289795, "[TT] Instrument Type of the TANSO-FTS-2 = Atmospheric chemistry"]
-[5.3066864013671875, 1.9673292636871338, "[TT] Mission Status of the FormoSat-1 = Mission complete"]
-[3.874460220336914, 6.362095832824707, "[TT] Antenna Quantity of the PROBA-V plus one = 2"]
-[14.21485424041748, 3.199984550476074, "[TT] Mass of the Severyanin-M = 150 kg"]
-[8.958931922912598, 4.46532678604126, "[TT] Quantity of the Sun Sensor Suites = 4"]
-[12.831461906433105, 7.604448318481445, "[TT] Instrument Power of the AATSR = 100 W"]
-[9.187352180480957, 7.16485071182251, "[TT] Image Resolution of the Earth Observation System = 0.8 m"]
-[6.174300670623779, 2.388700485229492, "[FF] Partnership of the GRACE-FO = NASA and the German Research Center for Geosciences (GFZ)"]
-[14.415692329406738, 6.887603759765625, "[TT] Battery Nominal Voltage of the EPS = 7.4 V"]
-[6.871022701263428, 6.99755859375, "[TT] Number of Beams of the DOE = 6"]
-[5.318544864654541, 4.227556228637695, "[TT] Rotor Type of the Knudsen Station = AlphaSpid's RAS rotor"]
-[6.4903435707092285, 3.0426478385925293, "[FF] Service of the Spire Global UK = Predict vessel locations and the ship\u2019s estimated time of arrival at port"]
-[6.317975044250488, 0.15808899700641632, "[TT] Number of Crews of the Skylab-1 = Three"]
-[4.891055583953857, 2.594231605529785, "[TT] Quantity of the MSG-1 (Meteosat-8) of EUMETSAT = 1"]
-[6.700122833251953, 4.2353434562683105, "[FF] Integration of the Science Instrument = With the avionics in the flight bus chassis"]
-[7.687615394592285, 0.6404131650924683, "[FF] Mission Date of the NASA's First Mission to the Trojan Asteroids = Unknown"]
-[10.515008926391602, 7.328279495239258, "[FF] Purpose of the Strip map mode = Acquire zonal imagery - a continuous image with a maximum length of 850 km and a width of 10 km"]
-[8.14591121673584, -1.0773508548736572, "[FF] Measurement Capability of the ICESat-2 = Height of Earth\u2019s surfaces in remarkable detail"]
-[6.395436763763428, 1.8969221115112305, "[FF] URL of the SOLSPEC = http://www.ioccg.org/groups/Thuillier.pdf"]
-[7.00043249130249, 6.874367713928223, "[TT] Lasers of the CATS = Two high repetition rate lasers"]
-[4.966289520263672, 3.425189971923828, "[TT] Manufacturer of the T6 thrusters = QinetiQ"]
-[7.620724678039551, 8.459883689880371, "[TT] Operating Bands of the GAS = Four NIR/SWIR bands"]
-[7.545171737670898, 3.696504592895508, "[FF] Calibration Process of the NightPod = Inserting the ISS orbit attitude information in terms of yaw pitch and roll in the NightPod computer"]
-[6.779489994049072, 2.159569025039673, "[FF] Mission of the Roman = Provide 3D images of the universe"]
-[5.0915985107421875, 1.974602222442627, "[TT] Status of the KMSS = Fully functional"]
-[6.156687259674072, 5.019965648651123, "[FF] Command Type of the TDP Commanding = Time tagged commands (TTC)"]
-[5.946202754974365, 5.6040849685668945, "[TT] Signal Processing and Control Module Architecture of the IRIS = PowerPC"]
-[7.041482925415039, -0.19521547853946686, "[TT] Number of Orbits of the EFT-1 = 2"]
-[4.848503112792969, 0.5452311038970947, "[TT] Operation End Date of the Metcomp experiment = 17 December"]
-[9.34900188446045, -1.6897321939468384, "[FF] Swarm Size of the Desert Locusts = 1 km2"]
-[9.025533676147461, 6.487867832183838, "[TT] Image Segment Size of the CaSSIS = 7 x 38 km"]
-[7.850091934204102, 7.075680255889893, "[FF] Frame Read-out Frequency of the EPIC CCDs = Fixed, mode dependent"]
-[8.488241195678711, 0.17283914983272552, "[TT] Asteroid Flyby Resolution of the Chang'e-2 = 3 m"]
-[11.99123764038086, 4.93857479095459, "[TT] Size of the VPU = 195 x 120 x 253 mm"]
-[1.7477726936340332, 4.560134410858154, "[FF] N/A of the thrusters group = N/A"]
-[5.860137462615967, 7.232722282409668, "[TT] Minimum Impulse Bit of the T3\u00b5PS = 30\u00b5Ns"]
-[8.44205093383789, 7.694032669067383, "[TT] Pixel Pitch of the MS CCD detector module = 2 x 17.5 \u00b5m"]
-[6.273816108703613, 7.038626194000244, "[TT] Compression Type of the Data Compression = Lossy compression based on wavelet transform"]
-[8.566454887390137, 4.526658535003662, "[FF] Repeatability of the ASTERIA = Stars positioned on the same pixels on each orbit"]
-[4.617797374725342, 6.994494915008545, "[TT] Bandwidth of the Spacecraft Repeater = 100 kHz"]
-[8.619283676147461, 3.874434471130371, "[FF] Purpose of the IDEE = Measure electrons"]
-[8.342453002929688, -0.49149420857429504, "[TT] Area of the Vatnaj\u00f6kull Glacier = 8400 km2"]
-[9.10751724243164, 4.360954761505127, "[TT] Solar Elongation Range of the NEOSSat = 45\u00ba to 55\u00ba"]
-[1.9369462728500366, -0.4024158716201782, "[TT] Apogee Drift Period of the Van Allen Probes = About 2 years"]
-[5.400537967681885, 4.063284397125244, "[TT] Version of the GSOC's core MCS = Enhanced derivative of ESA's SCOS-2000 v3.1"]
-[10.137495994567871, 3.076815128326416, "[TT] Location of the CubeSat Yonsei team = Korea"]
-[5.293195724487305, 1.3928332328796387, "[TT] Project Selection Year of the CHIPS = 1998"]
-[10.97478199005127, 7.61821985244751, "[TT] Swath Width of the Wide Fine Quad-Polarisation Mode = About 50 km"]
-[7.9645819664001465, 4.571077823638916, "[FF] Function of the On-orbit Calibration = Can reduce tedious ADCS ground testing"]
-[5.633066654205322, 1.3312857151031494, "[FF] Mission Date of the LARES 2 = 17-19 November 2015"]
-[13.230755805969238, 7.330967426300049, "[TT] Measurement Discrepancy of the TSI = 4.6 watts per square meter"]
-[11.702157020568848, 4.356291770935059, "[FF] Height and Footprint of the X50M platform = Reduced to fit within JEM fairing"]
-[3.7700135707855225, -1.085569977760315, "[TT] Orbit Shape of the LRO = Elliptical"]
-[4.901378154754639, 3.194389820098877, "[TT] Manufacturer of the SOLSPC = CNRS, France"]
-[9.720532417297363, 0.08232709765434265, "[TT] Distance from Space Station of the Dragon spacecraft = 10 meters"]
-[6.395790100097656, 1.785885214805603, "[FF] URL of Paper of the RISESAT = http://tinyurl.com/q5hq42e"]
-[3.659742832183838, 4.787158012390137, "[FF] Polarimetric Sensor of the RISAT-1 = Hybrid"]
-[4.819353103637695, 7.136716365814209, "[TT] Downlink Transmission Data Rates of the CBERS-1 = 2 x 53 Mbit/s"]
-[7.932432651519775, 5.603115558624268, "[TT] Position Calculation Method of the DIOGENE = Least squares method"]
-[8.272260665893555, 8.709875106811523, "[TT] Mission Status of the Multi-band UV/VIS Spectrometer (ACE) = Operational (extended)"]
-[9.77810001373291, 7.402413368225098, "[TT] On-Ground Separation of the Slits = 15.9 km"]
-[7.851410865783691, 1.464808464050293, "[FF] Data Collection of the Earth-observing satellites = During and after the eruption"]
-[8.84717082977295, 4.630494594573975, "[TT] Correction Level of the Sun and Galactic Glint = Level-2"]
-[10.269572257995605, 5.725727081298828, "[TT] Hot-Load Target Temperature of the Instrument = About 300 K"]
-[6.33486795425415, 2.3098719120025635, "[FF] Principal Investigators of the SMILE = Graziella Branduardi-Raymont from MSSL/UCL (Mullard Space Science Laboratory/University College London), UK, and Chi Wang from the State Key Laboratory of Space Weather, NSSC/CAS (National Space Science Center/Chinese Academy of Sciences)"]
-[6.704295635223389, 4.803416728973389, "[FF] Components of the GCS = GMCF, GADS, GTF"]
-[6.49271297454834, 7.541506767272949, "[TT] Data Quantization of the HSC-1700 = 8 bits"]
-[5.701618194580078, 2.839900255203247, "[TT] Sponsor of the Refabricator = NASA's Space Technology Mission Directorate"]
-[8.087661743164062, -0.9710474610328674, "[FF] Spatial Coverage of the ICESat-2 = Improved"]
-[5.609005928039551, 2.4980897903442383, "[FF] Structure of the Euro-Argo ERIC = Light, 1 program assistant, 1 program manager, Ifremer personnel seconded to the ERIC; Structure: 1 program assistant, 1 program manager, 1 technician, 1 engineer/scientist"]
-[2.9734339714050293, 2.3849093914031982, "[FF] Mission Objective of the Sentinel-5 = Operational monitoring of trace gas concentrations for atmospheric chemistry and climate applications"]
-[7.161372184753418, 6.696959018707275, "[FF] Frame Rate of the GLM = Unknown"]
-[9.03170108795166, 2.0775914192199707, "[FF] Origin of the Stardust Grain = Nova explosion more than 4.5 billion years ago"]
-[8.973530769348145, 4.675347328186035, "[TT] Attitude Control of the Payload = Star Tracker, Gyroscopes & Control Moment Gyros"]
-[4.900337219238281, 3.5001895427703857, "[TT] Manufacturer of the Electrical Power Subsystem (EPS) = Clyde Space"]
-[5.905195236206055, -0.5733004212379456, "[TT] Service Life of the FY-3E = At least eight years"]
-[5.589283466339111, -0.37421268224716187, "[TT] Orbit Life Without Balloon of the AeroCube-3 = 1-3 years"]
-[6.976247787475586, 2.2087929248809814, "[FF] Collaboration of the Hinode, IRIS and SOHO = Provide a suite of complementary instruments to study our Sun"]
-[10.385069847106934, 3.2959811687469482, "[TT] Bus Connection of the CubeSat = I2C or CAN"]
-[4.173926830291748, 5.694705486297607, "[FF] URL of the Automatic Dependent Surveillance-Broadcast (ADS-B) = http://www.faa.gov/nextgen/implementation/programs/adsb/"]
-[8.85869026184082, 7.589589595794678, "[TT] MS of the Pushbroom imager = 5.8 m"]
-[7.762993335723877, 1.5171043872833252, "[FF] Ocean Surface Resolution of the SWOT = 10 times current technologies"]
-[13.865652084350586, 2.7235445976257324, "[TT] Launch Mass of the IAE Experiment = 60 kg"]
-[3.7396039962768555, 6.53354024887085, "[TT] Type of the Altimeter Antenna = Parabolic"]
-[3.7500932216644287, 4.795102119445801, "[TT] Ground Swath of the RADARSAT-2 = 20km-500km"]
-[11.725823402404785, 6.651772499084473, "[TT] Energy Steps of the Genesis Electron Monitor = 24"]
-[5.040221691131592, -0.2805541157722473, "[TT] Launch Time of the OCO-2 = 09:56:23 UTC"]
-[5.525084495544434, 2.2815446853637695, "[FF] Affiliation of the Giacomo Peretto = Unknown"]
-[7.922564506530762, -2.528583288192749, "[TT] \u03a3O/N2 Column Density Ratio Enhancement of the GOLD = ~80% within the eclipse's totality"]
-[7.035074710845947, 6.722313404083252, "[TT] Dwell Time of the IRS Sounder = About 9 seconds"]
-[8.590740203857422, 5.834761619567871, "[TT] Beam Pointing Accuracy of the MWHS-II = \u22640.1\u00ba"]
-[9.496439933776855, -0.8515877723693848, "[TT] Total Orbits of the STS-85 = 185"]
-[9.269916534423828, 0.8942152261734009, "[FF] Brightness of the Venus' Orbital Dust Ring = At least a hundred times brighter than the solar wind"]
-[7.459765911102295, 2.483971357345581, "[TT] Measurement Category of the HORYU-2 = Multi-purpose imagery (ocean), Multi-purpose imagery (land)"]
-[12.031147956848145, 4.721900939941406, "[TT] Gouge Dimensions of the SMART-1 = 4 m-wide and 20 m-long"]
-[5.214273929595947, 0.8018180131912231, "[TT] Data Distribution Start Date of the GOCI = April 20, 2011"]
-[7.236600875854492, 0.8928042054176331, "[FF] Testing Focus of the RAMIS = Reduced gravitational force"]
-[5.229372501373291, 3.368104934692383, "[FF] Manufacturer of the EPIC = Not provided"]
-[13.139564514160156, 7.129698276519775, "[FF] Power Consumption of the Observation Mode = Unknown"]
-[5.101379871368408, 6.996382236480713, "[TT] Uplink Data Rate of the TanSat = 2 kbit/s"]
-[3.455963134765625, 6.465656280517578, "[TT] Access Width of the Antenna = 125 km"]
-[6.670586109161377, 3.6200051307678223, "[FF] Experiment of the Kyoto University = Robot teleoperation experiment"]
-[5.722643852233887, 2.7322897911071777, "[TT] Agency of the IMAGE = NASA"]
-[8.063336372375488, 0.8711686730384827, "[TT] 2021 Fires of the U.S. Drought Monitor = 672"]
-[4.894049167633057, 7.455479145050049, "[TT] Uplink Data Rate of the RF Communications = 4.8 kbit/s"]
-[7.195779323577881, 7.1911725997924805, "[TT] Passbands of the Radiometer = 6"]
-[6.449125289916992, -1.3121414184570312, "[FF] Performance of the GRACE = Reference"]
-[9.256034851074219, -0.2713060677051544, "[TT] Perigee of the \u00d8rsted satellite = 655 km"]
-[2.8855180740356445, 4.212681293487549, "[FF] Observation of the ALOS/PALSAR = Magnitude-9.0 Earthquake off the Pacific coast of Tohoku-Kanto District in Japan in 2011"]
-[9.914530754089355, 5.337517261505127, "[FF] Thermal Gradients of the LARES-2 = Reduced onset"]
-[5.8641228675842285, 6.151899814605713, "[FF] Fault Isolation of the SSR = The division of the storage space into independent banks"]
-[4.808259010314941, -1.8613355159759521, "[FF] Mission Objective of the Chang'e-3 = One year operation on the lunar surface"]
-[4.893764495849609, -0.8664475679397583, "[TT] Attachment Duration of the Cargo Dragon = About one month"]
-[6.146688461303711, 1.2240581512451172, "[FF] Quote of the Ericson = \u201cThis mission will be looked at as the first mission of the opening of the second space age, where space travel became much more accessible to average men and women across the world,\u201d"]
-[5.115159511566162, 0.29362374544143677, "[TT] Re-Entry Date of the Aeolus = Before the end of August"]
-[5.521008491516113, 3.2012438774108887, "[TT] Communication System of the Bartolomeo = OSIRISv3"]
-[6.635287284851074, 7.496708393096924, "[TT] Digital Conversion of the MEV = 12 bit"]
-[10.977449417114258, 7.638735294342041, "[TT] Nominal Swath Width of the Wide ultra fine = 50 km"]
-[7.690601825714111, 9.394329071044922, "[TT] Center Wavelength of the Band 2 = 14.37 \u00b5m (696 cm -1)"]
-[10.386259078979492, 2.27736496925354, "[FF] Energy Band of the Galactic Soft X-ray Background = 1/4 keV (R12)"]
-[5.855197906494141, -0.7086246013641357, "[TT] Instrument Lifetime of the Telescope = 5 years"]
-[9.940616607666016, 1.2220913171768188, "[FF] Distance from Solar System of the Pleiades = About 400 light years"]
-[14.197999000549316, 3.151838779449463, "[TT] Weight of the OSDP = 18 kg"]
-[6.493462085723877, 3.792694091796875, "[FF] Operation of the HTV = Berthing to the ISS"]
-[13.750544548034668, 3.6598193645477295, "[TT] Mass of the Antenna = < 120 kg"]
-[3.58274507522583, 4.8278422355651855, "[FF] Radar of the Sentinel-1A = C-band"]
-[7.68552827835083, 0.7264828085899353, "[FF] Pages of the Lunar Flashlight = 58\u201369"]
-[7.66212272644043, 5.229602336883545, "[FF] Tracking Capability of the ODP = Tracks on objects in the sensor's field of view"]
-[9.254804611206055, 3.1463115215301514, "[FF] Purpose of the Genesis = Measure the primordial form of oxygen in the solar wind"]
-[3.213714838027954, 1.6485605239868164, "[TT] Repeat Orbit Cycle of the Sentinel-1A and Sentinel-1B = 12 days"]
-[6.5822367668151855, 5.79801082611084, "[TT] Quantity of the GPIO board = 1"]
-[9.810844421386719, 2.382253885269165, "[FF] Optics Overview and Current Status of the NuSTAR = Unknown"]
-[10.686166763305664, 7.42605447769165, "[TT] Coverage of the Wide Multi-Look Fine Mode = 90 km"]
-[4.394351005554199, 2.048121929168701, "[TT] Launch Date of the DubaiSat-2 = November 2013"]
-[5.674877166748047, 11.344666481018066, "[FF] Approx. peak sensitivity altitude of the Channel 1 = Unknown"]
-[7.856424331665039, 0.18008504807949066, "[TT] Date of the Asteroid Day = 30 June"]
-[4.991156578063965, 1.1155234575271606, "[TT] Launch Date of the GIOVE-B = April 27, 2008"]
-[7.652910232543945, 8.661166191101074, "[TT] Bands of the Spectral Bands = 2"]
-[10.03166675567627, -1.5516295433044434, "[TT] Inclination of the ExoMars Orbiter = 74\u00ba"]
-[4.676438808441162, 6.991914749145508, "[TT] Navigation Signal Bandwidth of the Spacecraft = 3 bands (E5, E6, L1)"]
-[14.618250846862793, 6.700640678405762, "[TT] Battery Type of the EPS = NiH 2  battery"]
-[6.515453815460205, 5.829072952270508, "[TT] PRN of the GSAT-0208 = 8"]
-[10.97823715209961, 7.547388553619385, "[TT] Swath of the MERSI-RM = 2900 km"]
-[5.535339832305908, 2.2939136028289795, "[FF] Affiliation of the Nuria P\u00e9rez = Unknown"]
-[9.071066856384277, 9.965431213378906, "[TT] Swath per channel of the Eastman Kodak KLI14403 linear CCD sensor = > 300 km"]
-[12.026782989501953, -0.35257336497306824, "[TT] Science Operations Start Date of the TESS = Mid-June"]
-[6.206357479095459, 4.174510478973389, "[FF] Ground Segments of the TanDEM-X = Mission Operations Segment (MOS), Payload Ground Segment (PGS), Instrument Operations and Calibration Segment (IOCS)"]
-[7.761491775512695, 6.822067737579346, "[TT] Synchronization Accuracy of the Camera = 10 millionths of a second"]
-[6.992141246795654, 4.226178169250488, "[FF] Unknown of the MIPAS = Unknown"]
-[6.846622467041016, 1.8602067232131958, "[FF] URL of the Voyager 2 = https://www.jpl.nasa.gov/news/news.php?feature=7301"]
-[9.760969161987305, -0.5906159281730652, "[TT] Orbital Altitude of the LDEF = 335 km"]
-[9.937309265136719, -0.0744904950261116, "[TT] Altitude of the GRACE-FO satellites = ~490 km"]
-[5.649198532104492, 7.015040397644043, "[TT] Internal Data Speed of the DHU = Up to 10 Mbit/s"]
-[4.980617523193359, 3.3050432205200195, "[TT] Manufacturer of the NigeriaSat-2 = SSTL (Surrey Satellite Technology Ltd.)"]
-[6.160019397735596, 8.572795867919922, "[TT] Polarization of the C-RADAR = V and H"]
-[5.69295597076416, 0.6542019844055176, "[FF] Data Release of the NISTAR = Expected shortly after EPIC data"]
-[6.87900447845459, 4.565385818481445, "[FF] Responsibility of the NGC Aerospace Ltd = Design, implementation and validation of the autonomous GNC algorithms"]
-[13.344346046447754, 2.911931037902832, "[TT] Mass of the NPSat-1 = 86 kg"]
-[7.633385181427002, 0.8555622696876526, "[FF] Objective of the LPR = Mapping of lunar regolith and detection of subsurface geologic structures"]
-[5.6779704093933105, 11.362447738647461, "[FF] Approx. Peak Sensitivity Altitude of the Channel 6 = Unknown"]
-[8.144184112548828, 3.304872989654541, "[TT] Function of the Narrow Band Filter = Detect lightning and act as a possible TLE event trigger"]
-[7.272939682006836, 4.2778520584106445, "[FF] Objective of the Loose Maneuver = Demonstrate service operation and move from point A to point B"]
-[3.4764204025268555, 4.955560207366943, "[FF] Type of the L-band SAR = Imaging microwave radars"]
-[12.016223907470703, -0.34325599670410156, "[TT] First Year of Science Operations Completion Date of the TESS = July 18"]
-[6.368467807769775, 1.537943959236145, "[TT] Survey Date of the eROSITA = December 9, 2020"]
-[4.390059471130371, 1.8665329217910767, "[FF] Observation Date of the SGLI Polarimetric Radar = 23 March 2018"]
-[5.27999210357666, 5.663647174835205, "[TT] Communication Interface of the CEU = MIL-STD-1553B"]
-[8.113936424255371, 5.039844036102295, "[FF] Parameter Estimation of the User Segment Geometrical Calibration Tool = Exterior Orientation parameters and Interior Orientation deformations"]
-[8.747299194335938, 3.84080171585083, "[FF] Measurement of the SSI/ES-2 = Ambient electron density and temperatures, ambient ion density, average ion temperature and molecular weight"]
-[3.4294912815093994, -0.8968300223350525, "[TT] Orbit Type of the Meteor-M2 = Sun-synchronous circular orbit"]
-[4.903740406036377, 0.811235785484314, "[FF] Launch Date of the Ariane 5 ECA = August 2, 2012"]
-[9.35190486907959, 4.800421237945557, "[FF] Attitude Control Strategy Presentation Date of the LAPAN-A2 = April 8-12, 2013"]
-[6.4927659034729, 2.482870578765869, "[TT] Number of Student Images of the MoonKAM = Over 70,000"]
-[10.355528831481934, 2.1638331413269043, "[TT] X-ray Emission Brightness of the Swift = At least 10 times brighter than normal"]
-[8.972661018371582, 7.650024890899658, "[TT] Image Area Dimensions of the pnCCD camera = 3 cm x 3 cm"]
-[4.817553520202637, 2.9399378299713135, "[TT] Location of the MC3 CGA = USU (Utah State University), Logan, UT"]
-[8.776593208312988, 4.65948486328125, "[TT] Earth Sensor of the AOCS = Earth sensor"]
-[4.052186489105225, 6.201542377471924, "[FF] Access of the Antenna Dish = Cannot be readily accessed from the front due to the mesh"]
-[6.921159744262695, 4.157281875610352, "[FF] Unknown of the Spacecraft = Unknown"]
-[8.481719017028809, 1.8983577489852905, "[FF] Uncertainty in Convective Cloud Representation of the Numerical Models = More than 200%"]
-[10.058821678161621, 3.320310592651367, "[FF] Spectrum Comparison of the Vibration Testing = GSFC-7000 standard random vibration spectrum that is commonly used for CubeSats and the in-house SSTL Spectrum C random vibration spectrum"]
-[3.4606268405914307, -0.9063979983329773, "[TT] Orbit Type of the Tandem-L satellites = Sun-synchronous dawn/dusk orbit"]
-[6.634934425354004, 4.5091142654418945, "[TT] Affixing Method of the Launch Box = Straps"]
-[10.364444732666016, 0.95831698179245, "[TT] Distance from Earth of the GJ 367 b = Just under 31 light years"]
-[2.2827725410461426, 2.77215576171875, "[TT] Co-PI of the EPI-Lo = Alan Cummings"]
-[11.719359397888184, 4.584160327911377, "[TT] Primary Body Diameter of the Didymos = Approximately 800 meters"]
-[7.081202030181885, 4.667477130889893, "[FF] Responsible for of the Navigation Function = Generating estimates of the relative states \u2013 namely relative position, (linear) velocity, attitude, and angular velocity \u2013 of the S/C, in addition to (probabilistic or deterministic) bounds on the error of each estimate"]
-[9.36085319519043, 7.081059455871582, "[TT] Spatial Resolution of the TIRS-2 = 100 m"]
-[7.740522384643555, 1.9296042919158936, "[FF] References of the CIMR = Climate change resulting in ocean warming, sea level rise, and sea ice melting has consequences for the global economy, navigation, and security"]
-[10.387104034423828, 5.734907627105713, "[TT] Gas Temperature of the Cassiopeia A (Cas A) = 50 million degrees"]
-[10.469454765319824, 4.849122047424316, "[FF] Boundary Characteristics of the Warm-Core Ring = Concentric curvilinear lines"]
-[2.341553211212158, 2.7915968894958496, "[TT] PI of the MAHRSI = R. Conway"]
-[6.484068870544434, 3.192601442337036, "[TT] Image Credit of the AMS-02 = NASA, ESA, Ref. 68"]
-[8.46278190612793, 0.9787427186965942, "[TT] Annual Salt Extraction of the Saltworks = 9 million metric tons"]
-[7.327104091644287, 2.4153542518615723, "[TT] Operational Area of the SES-14 = Latin America, the Caribbean, North America, North Atlantic and West Africa"]
-[10.227215766906738, -1.3319953680038452, "[TT] Orbit Inclination of the R3 CubeSat = 85\u00b0"]
-[10.393561363220215, 5.768433570861816, "[TT] Temperature of the PICAM = ~ 70 \u00b0C"]
-[7.9362616539001465, 3.1658051013946533, "[FF] Lighting of the Highways and ring roads = Bright, regular"]
-[8.116442680358887, 2.620152235031128, "[TT] Measurement Domain of the Megha-Tropiques = Atmosphere, Ocean"]
-[8.954560279846191, -0.9380657076835632, "[FF] Orbit of the Beidou-3M/G/I satellites = MEO (Medium Earth Orbit) and GEO (Geosynchronous Orbit)"]
-[6.009979248046875, 6.429904937744141, "[TT] Occurrence Decrease of the PDHT timeouts = About 40%"]
-[14.241869926452637, 3.2595419883728027, "[TT] Mass of the TMR = 50 kg"]
-[5.951250076293945, -0.49933314323425293, "[FF] Mission Duration of the ERO = 5 years"]
-[8.0955171585083, 4.266809940338135, "[FF] Monitored Parameters of the TEDA = Radiation absorption, memory malfunction, static charge voltage, contamination, heavy ions"]
-[10.179605484008789, 3.076641798019409, "[FF] Deployment Mission Count of the CubeSat = 14"]
-[10.880120277404785, -0.349582314491272, "[TT] Complete Global DEM Availability Date of the TanDEM-X = September 2016"]
-[14.24743366241455, 3.2943387031555176, "[TT] Mass of the UVS = 3.98 kg"]
-[4.979885578155518, 0.42709437012672424, "[TT] Launch Date of the TSIS-2 = 2023"]
-[3.8947813510894775, 7.890776634216309, "[FF] Optical Technology of the LCT = Homodyne BPSK (Binary Phase Shift Keying)"]
-[11.706696510314941, 4.334018230438232, "[TT] Size of the StudSat = 10 cm x 10 cm x 13.5 cm"]
-[6.391446590423584, 5.4825568199157715, "[TT] Status of the DCS = Functional"]
-[14.269350051879883, 3.307546854019165, "[TT] Mass of the MuREM = ~400 g"]
-[14.275224685668945, 3.1499505043029785, "[TT] Mass of the S/C Structure = 191.4 kg"]
-[5.340957164764404, 5.622072219848633, "[TT] Interfaces of the PLC = MIL-STD-1553B @ 1 Mbit/s with bus BMU"]
-[7.6241655349731445, 2.4173552989959717, "[FF] Radar Altimeter of the TOPEX/Poseidon Project = Information Not Provided"]
-[9.145578384399414, 7.365691184997559, "[TT] Resolution of the IR Sensor = 0.550 km"]
-[4.819633483886719, 8.358563423156738, "[TT] Operating Frequency of the Herley MD2000C-1 = 5.4\u20135.9 GHz"]
-[5.597806453704834, 0.741766631603241, "[FF] Publication Date of the DESIS = October 2019"]
-[9.133323669433594, 3.171738862991333, "[FF] Student Collaboration Goal of the IMAP = Provides scientific involvement in studying the origin of EPs in the innermost magnetosphere"]
-[8.464263916015625, 1.7583414316177368, "[FF] Temperature of the Nearside Hemisphere = Hotter than that of the farside"]
-[4.05687141418457, 2.2194247245788574, "[FF] Presentation of the Atlas V Aft Bulkhead Carrier & Operationally Unique Technologies Satellite = Workshop"]
-[9.579350471496582, 0.792090117931366, "[TT] Distance from the Sun within the orbit of Mercury of the Solar Orbiter = Around 42 million kilometers"]
-[11.981587409973145, 6.534305572509766, "[TT] Energy Range of the Natalya-2M = 0.3 to 2 GeV"]
-[14.137696266174316, 3.3074209690093994, "[TT] Total Mass of the SASS = 103 kg"]
-[4.095489978790283, 0.18634356558322906, "[TT] Booster's Failure Date of the Falcon 9 = Feb. 15"]
-[8.296069145202637, 1.2734036445617676, "[TT] Moisture Sensors per Site of the Sensor Node = 3"]
-[4.89646053314209, 0.5760824084281921, "[TT] Launch of the CLARREO Pathfinder = 11/2022"]
-[5.488829612731934, 5.415341854095459, "[TT] Internal Harness Connectors of the ASM = Removed"]
-[9.363912582397461, 4.960121154785156, "[TT] Attitude-Rate of the NSTT = 2\u00ba/s"]
-[10.123611450195312, 2.087601661682129, "[TT] Control Center of the Chandra = Smithsonian Astrophysical Observatory's Chandra X-ray Center"]
-[8.82619571685791, 0.29786160588264465, "[TT] Diameter of the Von K\u00e1rm\u00e1n crater = 180 km"]
-[10.82583236694336, -0.29279467463493347, "[TT] Operation Status of the TanDEM-X = Nominal"]
-[5.735013484954834, 1.7237564325332642, "[FF] URL of the OGO 3 = http://aten.igpp.ucla.edu/personnel/russell/papers/OGO3_2Nature.pdf"]
-[8.028739929199219, 1.5707565546035767, "[TT] Number of Ocean Regions of the RECCAP-2 = 5"]
-[6.123593330383301, 1.1182763576507568, "[FF] Article Date of the Earth-observing satellite = 25 May 2022"]
-[6.39739465713501, 5.387991428375244, "[FF] Data Input of the Coprocessor = PRN, estimated delay, and estimated Doppler of the reflection"]
-[12.181303024291992, 3.667501926422119, "[TT] Volume of the Xenon Gas Tank = 49 liter"]
-[7.135704040527344, 4.582455158233643, "[TT] Mounting Location of the RCS Pods = Externally"]
-[9.394136428833008, 6.993485927581787, "[TT] Spatial Resolution of the MSU-S = 140 - 240 m"]
-[10.980379104614258, 7.62509298324585, "[FF] Swath width of the SBUS = "]
-[7.968100070953369, 1.9610974788665771, "[TT] Science Data Collection Start Date of the CloudSat = June 2, 2006"]
-[8.37817096710205, 6.9826812744140625, "[TT] Type of the TV Camera = Shutter-style"]
-[3.926213026046753, 6.365667343139648, "[TT] Antenna Type of the PROBA-V plus one = Directional high-data rate antenna"]
-[3.845172882080078, 3.3550612926483154, "[TT] Launch Time of the Galileo FOC-3 and FOC-4 satellites = 21:46 UTC"]
-[13.406699180603027, 7.649978160858154, "[TT] Output Power of the Iris radio = 4 W"]
-[5.635653018951416, 4.6641387939453125, "[TT] Use of the Net = In space"]
-[7.111982345581055, 7.20430326461792, "[TT] Laser Wavelength of the Triple Mirror = 1064 nm"]
-[4.074801445007324, 3.3739869594573975, "[TT] Procurements Cost of the Galileo Second Generation (G2) = Up to approximately 950 million euros"]
-[6.345516681671143, 4.2864251136779785, "[TT] Status of the ResourceSat-2 = Production"]
-[8.085183143615723, 7.359440803527832, "[FF] Imaging Modes of the SPOT satellite constellation = Multispectral and panchromatic"]
-[13.278589248657227, 2.934741258621216, "[TT] Mass of the SaudiSat-4 = 112 kg"]
-[6.4092183113098145, 0.7337724566459656, "[FF] Development Start Date of the Landsat-9 = Oct. 25, 2016"]
-[7.471058368682861, 6.568149566650391, "[TT] Operation Mode of the Radiometer = Integrate-while-scanning"]
-[7.469849586486816, 1.8546992540359497, "[FF] Deployment Priority of the Argo Floats = World ocean as their highest priority"]
-[14.682671546936035, 6.677005767822266, "[TT] NiCd Batteries Capacity of the EURECA = 40 Ah"]
-[4.473721504211426, 1.5167733430862427, "[TT] Launch Date of the FASat-Alfa = August 31, 1995"]
-[4.685436725616455, 8.120834350585938, "[TT] Center Frequency of the L5 = 1176.45 MHz"]
-[11.378046035766602, 4.395354747772217, "[TT] Size of the PhoneSat-2.5 = 1U"]
-[6.297492027282715, 8.001148223876953, "[TT] Total Number of Channels of the Communication Payload = 17"]
-[6.92958402633667, 5.126415252685547, "[FF] Housed Components of the CVX-2 = AP (Avionics Package) which includes the data acquisition and control electronics, and the power conditioning systems"]
-[5.649333477020264, 3.2265875339508057, "[TT] Contract Value of the HDEV = US$65 million"]
-[7.811935901641846, 9.071267127990723, "[TT] Central Output Angle of the Short Wavelength Band = -5.28\u00ba"]
-[5.644303321838379, 3.200465202331543, "[TT] Contract Value of the TSIS-2 = $32.9 million"]
-[4.948599338531494, 1.2157360315322876, "[FF] Announcement Date of the 2Operate and GomSpace = 5 March 2019"]
-[8.030155181884766, 3.643557071685791, "[TT] Observation Mode Switching of the OCO-2 = Alternate 16-day global ground-track repeat cycles"]
-[10.155820846557617, 8.097298622131348, "[TT] Focal Length of the Telescope = 3,650 mm 535 mm"]
-[4.829137325286865, 8.566723823547363, "[TT] Center Frequency of the Channel 2 = 18.7 GHz"]
-[7.5815558433532715, 6.2414960861206055, "[FF] Synchronization Requirement of the PH1, PH2, PH3, PH4 = Must be synchronized to be able to compare the recorded waveforms"]
-[11.943717956542969, 4.955440521240234, "[TT] Grid Size of the CVX = 7 mm x 19 mm"]
-[7.006959438323975, 4.206165790557861, "[FF] Unknown of the TASC = Unknown"]
-[10.679492950439453, 2.838219165802002, "[FF] Health Status of the OPTOS nanosatellite = Optimal"]
-[9.681192398071289, -0.6132368445396423, "[TT] Orbit Average Altitude of the STS-85 = 320 km"]
-[5.110409259796143, -0.23709125816822052, "[TT] Launch Time of the Iridium-5 = 7:17 am PDT (14:17 UTC)"]
-[5.568368434906006, 4.603057861328125, "[FF] Communication Issue of the MarCO = Unable to contact"]
-[3.592784881591797, 1.6212795972824097, "[FF] Symposium Date of the GMES Sentinel-3 = July 25-30, 2010"]
-[4.277507305145264, 3.11145281791687, "[FF] Ground Station Locations of the KazSTSAT = Svalbard, Astana and Guildford"]
-[5.337777614593506, 5.809359073638916, "[TT] Power to sub-experiments of the STRV-1d DHS = +5 V, \u00b112 V"]
-[13.860355377197266, 3.73923921585083, "[TT] Antenna Mass of the OBRC instrument = Not more 40 kg"]
-[10.637529373168945, 4.282834053039551, "[TT] Quantity of the Actuators = 2"]
-[4.750149250030518, 8.150980949401855, "[TT] Radio frequency (GHz) of the SASS = 14.6"]
-[7.42549991607666, 4.247040748596191, "[FF] Orbit Determination Goals of the GEOSAT Follow-On = High Accuracy and Near-Real-Time Processing"]
-[6.788236618041992, 4.613646507263184, "[FF] In-flight Disconnect of the CSD = Unknown"]
-[9.964576721191406, 7.8665924072265625, "[FF] Limitation of the Optical Telescopes = Orbiting objects become unresolvable at high orbits or small telescope apertures"]
-[5.5843505859375, -2.022172212600708, "[TT] Multispectral Imagery Resolution of the KOMPSAT-3 = 2.8m"]
-[9.256181716918945, 5.481679916381836, "[TT] Body Pointing Function of the ALOS-2 = \u00b130\u00ba in the roll axis"]
-[8.962251663208008, 2.965078353881836, "[FF] Contributions of the Cluster = Measurements of electric currents in space, revealed the nature of black aurorae, discovered plasma waves"]
-[11.92459487915039, 6.229508399963379, "[FF] Observed Particles of the AMS Experiment = Electrons, protons, positrons and antiprotons"]
-[9.658943176269531, 8.381431579589844, "[TT] 4\u00ba x 300\u00ba of the FOV = FOV (Field of View) 4\u00ba x 300\u00ba"]
-[9.8312349319458, 5.238470554351807, "[FF] Thermal Forces Minimization of the LARES satellite = Unknown"]
-[5.092219352722168, 2.7243382930755615, "[TT] Responsible Parties of the ESEO = ALMASpace and UniBO"]
-[4.635009288787842, 4.849897384643555, "[FF] Payload of the Perseus-M1 and M2 = AIS for ship tracking"]
-[8.698760986328125, 2.0756750106811523, "[TT] Wind Vector Direction Accuracy of the SeaWinds = 20\u00ba"]
-[5.275861740112305, 4.013450622558594, "[TT] Bus Type of the OrbView-4 = LEOStar"]
-[4.445837020874023, 6.769382953643799, "[TT] RF Communications of the Meteosat = S-band"]
-[5.673372745513916, 0.2565269470214844, "[TT] Mission Operation Start Date of the WINDS/Kizuna = 2010"]
-[7.853326320648193, 3.0311498641967773, "[FF] SIF Data Usage of the TanSat = GPP modeling and global carbon flux estimations"]
-[9.675253868103027, 5.380190849304199, "[FF] Components of the Instrument = Two sets of electronics, two cryogenic coolers for the detectors"]
-[7.436540126800537, 3.263482093811035, "[FF] Purpose of the MiDES = Gather operational data of the Earth horizon positions"]
-[6.135621070861816, 4.013617515563965, "[FF] Compatibility of the Open Cosmos satellite = Compatible with a wide variety of commercial launch vehicles"]
-[8.090058326721191, 4.240106582641602, "[FF] Thermal Vacuum Test Duration of the MMO = Three weeks"]
-[4.75410270690918, 6.176337718963623, "[TT] Type of the APL\u2019s Frontier radio = Software-defined"]
-[5.145052909851074, 0.5963113903999329, "[TT] Launch Year of the MTG-S satellite = 2024"]
-[7.992528438568115, 5.089010715484619, "[FF] In-Flight Calibration Strategy of the TRUTHS = Radiometric gain/bias, linearity, spectral performance"]
-[5.6554718017578125, 7.241311550140381, "[TT] Data Download Capacity of the GimmeRF = About 10 Mbit per orbit"]
-[4.854139804840088, 2.5194852352142334, "[FF] Prime Developers of the Gokturk-1 = Telespazio (Rome, Italy) and TAS (Thales Alenia Space)"]
-[13.74354362487793, 2.8954319953918457, "[TT] Mass of the Spacecraft = 10.165 kg"]
-[8.383999824523926, 6.1164960861206055, "[TT] Range Measurement Accuracy of the RA-1 = Better than 10 cm"]
-[10.370094299316406, 2.152202606201172, "[FF] X-ray Sources of the Fireworks galaxy (NGC 6946) = Extremely bright"]
-[4.765387535095215, 6.431313514709473, "[TT] Communication System of the Ground Station = MHX modem (Microhard Systems)"]
-[12.199125289916992, 6.917472839355469, "[TT] Charge Range for Elements of the LEICA = 1 - 26"]
-[4.383175373077393, 1.8595198392868042, "[TT] First Conjunction Alert of the RADARSAT-2 = March 2009"]
-[7.091320991516113, 3.2052197456359863, "[FF] Data Source of the GEOS DAS = Satellite data and mathematical representations of physical processes"]
-[3.500720262527466, 4.729982852935791, "[FF] Intended Replacement of the TOPSAR = Conventional ScanSAR mode"]
-[8.8296480178833, 8.352401733398438, "[TT] Refractive Index of the RICH = 1.050"]
-[11.099761962890625, 5.231296062469482, "[FF] Scintillation Data Frequencies of the CITRIS = VHF, UHF, and at L-band frequencies"]
-[6.907738208770752, 5.92565393447876, "[TT] Drag Levels of the S/C = Several N"]
-[5.79656982421875, 2.3589699268341064, "[FF] Documentary Team Member of the AzTechSat = Ana Belen Urrutia Bartsch"]
-[9.418872833251953, 8.592801094055176, "[FF] Exit Slit of the SDEA = Circular cylinder section with vertical axis passing through the entrance slit"]
-[14.24438190460205, 3.292598009109497, "[TT] Moving Part Mass of the SILEX = 70 kg"]
-[13.535881996154785, 5.885563373565674, "[FF] Solar Power Generation of the SLATS = Proportional to sin|\u03b2|"]
-[3.1257543563842773, -0.09120114147663116, "[TT] Version of the Alexander, Graham, Bell = 1.0, 1.0, 2.0 \u03b2"]
-[7.02477502822876, 4.647500991821289, "[TT] Mounting Method of the Propulsion Equipment = Mounted on a panel inside the launch adapter ring"]
-[4.171117305755615, 5.754653453826904, "[TT] Payload of the CanX-7 = ADS-B"]
-[7.684173583984375, 0.8479764461517334, "[FF] Background Noise of the Lunar Meteoroid Impact Flash Detection = Earthshine (Earth reflected light on the Moon surface) in the visible spectrum, and by thermal emissions of the Moon surface in the infrared spectrum"]
-[6.710038185119629, -0.3968653976917267, "[TT] Period of the Satellite = 98 min"]
-[8.448614120483398, 7.01434850692749, "[TT] Imaging Filters of the MRO = Three"]
-[9.406960487365723, 3.5495951175689697, "[FF] Prediction of the Magnetic Field Models = Pole will continue to drift towards Siberia"]
-[9.5093994140625, 0.5142235159873962, "[TT] Altitude of Front Heat Shield Release of the Schiaparelli = About 7 km"]
-[9.613834381103516, 7.2266130447387695, "[TT] Spatial Resolution of the CarbonSpec = 2 km x 2 km"]
-[4.377397060394287, 4.007541656494141, "[TT] Quantity of the SAR/Galileo = 6"]
-[9.712550163269043, 4.40555477142334, "[FF] Function of the Magnetorquer = Allows full 3-axis attitude control experimentation to be performed"]
-[3.1802175045013428, 4.9848761558532715, "[TT] Resolutions of the RISAT-SAR = 3 to 50 m"]
-[7.8515801429748535, 2.9991514682769775, "[FF] Scientific Goal of the TanSat = Improve the understanding on the global CO2 distribution and its contribution to the climate change, and also to monitor the CO2 variation on seasonal time scales"]
-[9.917743682861328, -0.5933300256729126, "[TT] Mission Altitude of the MicroSat-2b = 1125 km"]
-[9.16501522064209, 4.937661647796631, "[FF] Accuracy Requirement of the Attitude and Position Navigation Instruments = Good positional accuracy"]
-[13.435441970825195, 6.005650043487549, "[FF] Mission Objectives of the HORYU-2 = Educational program, On orbit demonstration of the nanosatellite bus technologies, Generate a 300 V photovoltaic power in LEO"]
-[9.475292205810547, 7.053462028503418, "[TT] Spatial Resolution of the TopSAR narrow = < 30 m"]
-[3.5275564193725586, 4.64940071105957, "[FF] Sensitivity research for disasters of the Disaster = Time-series SAR data (amplitude), PolSAR and InSAR (coherence) will be combined to detect the best combination for each disaster"]
-[6.016393184661865, -0.5549022555351257, "[TT] Project Duration of the ESEO = 1.5 years"]
-[5.995296478271484, 3.488126277923584, "[FF] Development Cost Reduction of the Software = Large"]
-[3.349733591079712, 4.659530162811279, "[TT] Coordination Partner of the PAZ SAR Processor = IGS (Ingenio Ground Segment)"]
-[7.596376419067383, 4.288023948669434, "[FF] Sensor Complement of the MMO = MERMAG, MPPE, PWI, MSASI, MDM"]
-[8.010799407958984, 0.864827036857605, "[TT] Data Distribution Center of the GRACE = National Drought Mitigation Center at the University of Nebraska-Lincoln (UNL)"]
-[7.64104700088501, 0.7936425805091858, "[FF] Neutron Moderation of the Lunar Regolith = More enriched in hydrogen"]
-[7.4350128173828125, 3.0335745811462402, "[FF] Purpose of the CICERO-4 = Weather satellite"]
-[5.82925271987915, -2.247249126434326, "[TT] Altitude of the KOMPSAT-3A = 528 km"]
-[10.730000495910645, 2.1390929222106934, "[TT] Discovery Date of the XMM-Newton X-ray observatory = January 13, 2020"]
-[5.930734157562256, 7.871643543243408, "[TT] Sampling Frequency of the PH4 = At least 20 kHz"]
-[7.28390645980835, 7.482573509216309, "[FF] Flatness Requirement of the Photon Sieve = Approximately 3\u03bb"]
-[11.049580574035645, 6.132956027984619, "[TT] Material of the Input window = Glass"]
-[4.082685470581055, 6.380174160003662, "[TT] Antenna FOV of the ROSA = \u00b145\u00b0"]
-[3.7890005111694336, 6.545219421386719, "[TT] Cross elevation of the Antenna = \u00b115\u00ba"]
-[8.722777366638184, 5.651782035827637, "[FF] Contact Attempt Options of the UFF TLE = Inertial Pointing or Scanning"]
-[9.496725082397461, 6.947366237640381, "[TT] Resolution of the MRS = 25 m"]
-[5.911187171936035, 1.5130574703216553, "[FF] Operation Date of the PRISMA = Sept. 27-Oct. 1, 2010"]
-[8.355813026428223, 8.13931655883789, "[TT] Spectral Range of the Imaging Payload = Complete visible range from 400 to 900 nanometers"]
-[7.568727493286133, -0.3308784067630768, "[TT] Capture Date of the Canadarm2 = Jan 12, 2015"]
-[7.959654331207275, 5.395313739776611, "[TT] Calibration Setup of the FLLS = Optical bench within one of the laser-safe laboratories"]
-[7.348588466644287, 8.891891479492188, "[TT] Filter Type of the NUV channel = Block with Aluminum"]
-[6.2221999168396, 4.728466987609863, "[FF] Data Service of the SGR-ReSI = Rapidly collect and invert the data into sea state"]
-[5.691261291503906, 0.009350372478365898, "[TT] Station Operations Period of the Russia = Until 2028"]
-[6.4576191902160645, 2.050601005554199, "[FF] URL of the IPv6 and IPsec on a satellite in space = http://www.cisco.com/web/strategy/docs/gov/wood-iac-07-B-2-6-06-paper.pdf"]
-[13.97663688659668, 7.118910312652588, "[TT] Voltage Range of the Suppressor Grid = 0 to -12 V"]
-[18.79882049560547, 3.4776787757873535, "[TT] Mean \u0394E (m) of the Karshi Khanabad = 14.6"]
-[5.383482456207275, 0.3227068781852722, "[TT] Launch Date of the Explorer 36 = Jan. 11, 1968"]
-[5.531708240509033, 5.118662357330322, "[FF] Interfaces of the CIU = CAN interface to the bus, PPS interface to the GPS"]
-[5.0088701248168945, 3.339306592941284, "[TT] Manufacturer of the HRC = ESA"]
-[4.523677349090576, 1.7383698225021362, "[FF] Presentation Date of the JC2Sat-FF = April 23-25, 2008"]
-[8.48346996307373, 7.650308132171631, "[TT] CCD Detector Array of the PAN Camera = 12,288 pixels"]
-[6.246598243713379, 5.202751636505127, "[FF] Type of the Standard middleware = Standard middleware"]
-[4.922684192657471, 1.1778327226638794, "[FF] Product Availability of the AMSU-A = Since 1973"]
-[4.799437522888184, 0.793039858341217, "[TT] Program Initiation Year of the Resurs-O1 = 1977"]
-[6.906434535980225, 1.0627118349075317, "[FF] Function of the CASPER = Replan activities, including downlink, based on science observations in the previous orbit cycles"]
-[8.115852355957031, 8.444814682006836, "[FF] Purpose of the Filter Assembly = Separate VNIR spectral domain into the ten bands B1 to B9"]
-[8.485509872436523, 3.1048455238342285, "[TT] Observed Gases of the Altius = Ozone, Nitrogen Dioxide, Water Vapor, Aerosol"]
-[9.324752807617188, 4.18790340423584, "[FF] Function of the Sun-seeking precession controller = Precess the solar panel normal vector to the sun vector"]
-[8.172605514526367, 6.059072494506836, "[TT] Cameras Status of the Lucy = Operational"]
-[7.995400905609131, 4.330593109130859, "[FF] Type of the Trajectory = Possible trajectory combining different maneuvers"]
-[4.340008735656738, 7.114527702331543, "[TT] Ku-band beams of the Repeater subsystem = 4 Ku-band beams using a receive-only direct radiating phased array antenna (DRA)"]
-[8.043204307556152, 3.3148460388183594, "[FF] Monitoring Capabilities of the IRFS-2 = Atmospheric temperature and humidity profiles"]
-[10.932221412658691, 7.557277679443359, "[TT] Swath Width of the TAC = 51 km"]
-[3.8439605236053467, 1.338637351989746, "[TT] Satellite Deployment Location of the Falcon 9 = 172 miles (278 km) above Earth just south of New Zealand"]
-[5.560696601867676, 6.599364280700684, "[TT] Data Distribution of the SMOS = 18 TB per year"]
-[10.007220268249512, 8.161981582641602, "[TT] Diameter of the Optic diameter = 1.27 cm"]
-[8.426411628723145, 8.494723320007324, "[FF] Speed of the Spectrometer Channel = Relatively slow (f/14)"]
-[10.0228271484375, 2.894449234008789, "[TT] Launch Date of the COPPER CubeSat = Nov. 20, 2013"]
-[3.198448657989502, 1.6045607328414917, "[TT] Tandem Flight Duration of the Sentinel-3B = 4-5 months"]
-[10.235040664672852, 8.060912132263184, "[TT] Aperture of the UVIT Telescope = ~375mm"]
-[7.664849281311035, 6.651944160461426, "[TT] Exposure Time of the SPARCS = \u224810 min"]
-[8.529274940490723, 7.646818161010742, "[FF] Image Credit of the Area Array Detector = EADS Astrium"]
-[7.7487945556640625, 9.444622039794922, "[TT] Band Center Wave of the M2 = 0.445 \u00b5m"]
-[6.926780700683594, 1.4571131467819214, "[FF] News Release Date of the Webb Telescope = 12 July 2022"]
-[5.259466171264648, 0.6254901885986328, "[TT] NASA Responsibility Start Date of the TSIS-1 = October 1, 2015"]
-[8.657339096069336, 0.08795489370822906, "[TT] Integration of the Comet = Easy"]
-[10.3486328125, 4.041812896728516, "[FF] Role of the Solenoid Valve = Allow trapped air escape during the launch phase"]
-[7.71263313293457, 6.553098678588867, "[TT] Image Scanning Time of the ABI = 5 minutes"]
-[9.796733856201172, -0.5534351468086243, "[TT] Orbit Altitude of the Spacecraft = 1 km"]
-[3.3633153438568115, 1.4873316287994385, "[FF] Launch Date of the Sentinel-1B = April 25, 2016"]
-[9.420097351074219, 4.745604991912842, "[FF] Attitude Control System Status of the ALOS-2/Daichi-2 = Shifted to the regular operation mode"]
-[4.573902130126953, 0.733121395111084, "[TT] STM Tests Dates of the PROCYON = March 2014 and April 2014"]
-[9.992120742797852, 0.6983633637428284, "[TT] Radial Distance of the Cluster 3 = 5.9 RE"]
-[8.901376724243164, 8.337337493896484, "[TT] Iron Particle Distributions of the WISPR Optics = 0.5 \u2013 3 \u00b5m"]
-[11.134790420532227, 0.4911669194698334, "[FF] Number of Planets Discovered of the UBC student = 17"]
-[7.656401634216309, 8.828461647033691, "[TT] Spectral Bands of the SLSTR = 11"]
-[8.738785743713379, 7.608276844024658, "[TT] Any two pixels in a Frame of the Within Frame Registration = \u00b121 \u00b5rad"]
-[6.8154754638671875, 0.6468055844306946, "[FF] Image Release Date of the Crab Nebula = May 10, 2017"]
-[4.840077877044678, -0.33816468715667725, "[TT] Mission Duration of the CATS = 33 months"]
-[12.01974105834961, -0.42335161566734314, "[TT] Mission Start Date of the TESS = October 30, 2019"]
-[7.426580905914307, 4.288082122802734, "[FF] Function of the Light Sensor = Confirm when the optical beacon is impinging on the satellite"]
-[8.746075630187988, 1.8691486120224, "[TT] Wind Speed Increase of the Rapid Intensification = At least 35 miles (56 km) per hour within 24 hours"]
-[7.978229522705078, 13.684744834899902, "[TT] SSD of the B8 = 10 m"]
-[6.229557514190674, 6.116783142089844, "[TT] Additional Downlink Subsystem of the Sentinel-1, -2 = Optical Communications Payload (OCP)"]
-[8.36199951171875, -0.49895933270454407, "[TT] Area covered of the Ice = 25 km"]
-[7.990542411804199, 4.8231587409973145, "[TT] Sensor Type of the MuREM = RADFET (Radiation-sensitive Field Effect Transistor) solid-state dosimeters"]
-[6.228048324584961, 5.404123783111572, "[FF] Additional Protection of the Avionics Components = Error correcting code on all memories and triple modular redundancy on logic gates in the used FPGAs"]
-[2.904914140701294, 1.9796234369277954, "[TT] Image Capture Date of the Copernicus Sentinel-2 = 20 January"]
-[7.875599384307861, 5.444728851318359, "[FF] Tests of the FG = Optical, electrical and mechanical"]
-[9.50112247467041, 6.14556884765625, "[TT] Incidence Angle Range of the TopSAR wide = 25\u00ba - 45\u00ba"]
-[5.914357662200928, 1.4856553077697754, "[TT] Boom Status of the IXPE observatory = Delivered"]
-[9.258288383483887, 2.9494755268096924, "[FF] Types of Eruptions of the Sun = Coronal mass ejection, jet, partial eruption"]
-[5.644489288330078, 3.479585886001587, "[FF] Platform Type of the SSTL-300 = EO Small Satellite"]
-[4.436974048614502, 0.6240297555923462, "[TT] Decommissioned Date of the COSPAS-1 = March 1988"]
-[5.2479352951049805, 4.5523152351379395, "[TT] Software of the MC3 = CGA (Common Ground Architecture)"]
-[11.006352424621582, 2.9575307369232178, "[TT] Maximum Mass of the O/OREOS nanosatellite = 5.5 kg"]
-[10.230598449707031, 8.123335838317871, "[TT] Aperture Diameter of the ALI = 12.5 cm"]
-[8.105169296264648, -0.5325443148612976, "[TT] Rank of the Ice Maximum = Seventh-lowest in the 43-year satellite record"]
-[5.533783912658691, 7.109755039215088, "[TT] Data Rate of the RHCP transmission = 320 Mbit/s"]
-[10.396478652954102, 6.639389991760254, "[TT] Laser Retro-reflectors Quantity of the Starshine-3 = 31"]
-[11.337316513061523, 5.027571678161621, "[TT] Free Length of the Flexi-cables = ~ 80 mm"]
-[4.26382303237915, 7.251496315002441, "[FF] Communication Bands of the Kepler 6/7 = Ku-band, S-band"]
-[7.590002059936523, 1.139893889427185, "[FF] Purpose of the RISE = Deduce the size and density of the martian core"]
-[5.811899185180664, 4.571835517883301, "[TT] Location of the TAFF = OBC of the TDX spacecraft"]
-[8.162555694580078, 7.788902282714844, "[TT] Spectral Bands of the CCD Camera = Three"]
-[3.74672794342041, 5.45799446105957, "[TT] Azimuth Resolution of the Spotlight = 3.4 m (dual pol.)"]
-[6.38340950012207, 3.6360931396484375, "[FF] Purpose of the DMSP = Monitor the meteorological, oceanographic and solar-geophysical environment of the Earth in support of DoD operations"]
-[7.96375036239624, 8.21677303314209, "[TT] Spectral Bands of the Imaging Payload = Green (520-600 nm), red (630-690 nm), near infrared (770-900 nm)"]
-[9.574216842651367, 5.007286548614502, "[TT] Wing Status of the AC4-B = Open"]
-[6.0117292404174805, 2.321775197982788, "[FF] Roles of the Hayley Arceneaux, Sian Proctor and Chris Sembroski = Not specified"]
-[8.746102333068848, -0.21531027555465698, "[TT] Perigee (km) of the Meteor-2-1 = 872"]
-[8.545770645141602, 6.2012810707092285, "[TT] Accuracy of the SCA = < 0.3 mrad"]
-[7.9276838302612305, 4.540028095245361, "[FF] On-Board Calibrators Performance Duration of the Terra MODIS = Not Provided"]
-[8.40730094909668, 5.948917388916016, "[TT] Measurement Precision of the ERS-1 and -2 = Within less than a quarter of an inch"]
-[8.73298454284668, 6.474602699279785, "[FF] Incident Angle Dependence of the Scanning Systems = Problematic"]
-[8.543194770812988, 1.3511290550231934, "[FF] Purpose of the Aquarius = Study the salt content of ocean surface waters"]
-[6.710875034332275, 4.631851673126221, "[FF] Navigation Capability of the SEXTANT = GPS-like navigation"]
-[7.672170162200928, 0.9265736937522888, "[FF] Function of the LFS (Low Frequency Spectrometer) = Low-frequency radio frequency spectrum analyzer for detection of low-frequency radio frequency characteristics of the sun and the moon's low-frequency radio environment to perform low-frequency radio astronomy observations"]
-[6.0183234214782715, -0.3757946789264679, "[TT] Recovery Operation Duration of the STEREO-B = 22 months"]
-[10.019420623779297, -1.525604248046875, "[TT] Orbit Inclination of the T/P = 66.039\u00ba"]
-[4.558539390563965, 7.276730060577393, "[TT] L-band Receivers of the UoSAT-12 = 2"]
-[13.298924446105957, 7.851802825927734, "[FF] Radio Frequency Output Power of the X-band transmitter = Programmable"]
-[11.35697078704834, 5.863908290863037, "[TT] Material of the Rails = Aluminum"]
-[11.3353271484375, 5.805170059204102, "[TT] Material of the Antenna Mast = Kevlar fabric impregnated with a temperature sensitive, rigidizable resin"]
-[4.486217498779297, 1.841147541999817, "[FF] Conference Date of the RADARSAT-2 = June 24-28, 2002"]
-[10.189471244812012, -1.4199082851409912, "[TT] Inclination of the BlackSky Satellites = 53 degrees"]
-[13.497963905334473, 5.7698655128479, "[TT] Solar Array Power of the EPS = 180 W (EOL)"]
-[6.758219242095947, 6.091628551483154, "[TT] System Mode of the KaRIn = Non Ping Pong mode"]
-[6.568284034729004, 6.60097074508667, "[FF] Communication Technology of the EDRS = Laser technology"]
-[6.934817790985107, 8.668550491333008, "[TT] Quantity of the Filter Wheel = 4 polarizes and 2 filters"]
-[13.857014656066895, 5.678421974182129, "[TT] Conversion Efficiency of the Solar Cells = 26.8%, 28.3%"]
-[3.3386404514312744, 6.452988147735596, "[TT] Antenna Diameter of the PRARE ground transponder = 60 cm"]
-[5.936671733856201, 1.5084558725357056, "[FF] Conference Date of the Small Satellites = Aug. 14-17, 2006"]
-[6.192173957824707, 5.995163917541504, "[TT] Function of the TCU = Provides requisite amplitude and phase correction required on each TR module"]
-[6.250027179718018, 6.126153945922852, "[TT] Operation Modes of the TRSR = C/A and P code, P-codeless (cross-correlation)"]
-[9.471436500549316, 3.923288106918335, "[FF] Function of the Fluxgate and search coil magnetometers = Measure low frequency and wave magnetic fields"]
-[7.830944061279297, 3.768305540084839, "[FF] Instrument Family of the ACC = GRADIO accelerometer models composing the three axis gravity gradiometer of the GOCE mission of ESA"]
-[4.880976676940918, 3.2586822509765625, "[TT] Manufacturer of the OMI = Dutch-Finnish"]
-[5.384110927581787, 3.9658007621765137, "[TT] Constellation Number of the PlanetiQ satellites = 20"]
-[8.440645217895508, 8.627208709716797, "[TT] Altitude range of the UV/VIS Spectrometer = 20 - 100 km"]
-[5.106084823608398, 1.847753882408142, "[TT] Mission Status of the HY-1C = Operating nominally"]
-[8.02505111694336, -0.5973025560379028, "[FF] Data Analysis of the GOCE = High-resolution measurements over Antarctica between November 2009 and June 2012"]
-[5.3649115562438965, 3.9179112911224365, "[FF] Number of Satellites of the Terran R = Not Disclosed"]
-[13.770901679992676, 2.861795663833618, "[TT] Mass of the Spacecraft = ~980 kg"]
-[8.956633567810059, 4.8211140632629395, "[TT] Manufacturer of the Honeywell QA-2000 Accelerometer = Honeywell"]
-[4.8127031326293945, -1.9186092615127563, "[TT] Number of Scientific Payloads of the Chang\u2019e-4 = 6"]
-[4.868814945220947, 0.8993329405784607, "[TT] Launch Date of the Alphabus = Jan. 29, 2010"]
-[7.32620906829834, 3.1769745349884033, "[TT] Spatial Resolution of the GHGSat-D = 100 x better than the current state-of-the-art"]
-[4.354096412658691, 7.460269451141357, "[TT] Uplink Frequency of the RF Communications = S-band"]
-[6.449075698852539, -0.7680501937866211, "[TT] LTAN of the Spacecraft = 10:30 hours"]
-[7.232700824737549, 7.2641215324401855, "[FF] Photon Counting Rate of the PSR B0531+21 = Poisson Distribution"]
-[3.439033269882202, 6.4447760581970215, "[TT] Antenna Size of the MSU 21 m dish antenna = 21 m"]
-[5.634469509124756, 0.9892963767051697, "[TT] Launch Date of the IBEX = Oct. 19, 2008"]
-[11.893121719360352, 5.4293365478515625, "[TT] Size of the Instrument = 415 mm x 240 mm x 160 mm"]
-[6.9502949714660645, 1.601379156112671, "[FF] Vision of the James Webb Space Telescope = Improved"]
-[9.686164855957031, 8.441071510314941, "[TT] FOV of the Instrument = 12\u00ba x 9\u00ba"]
-[7.412962436676025, 5.388500213623047, "[TT] Instrument of the ATLAS-1 = SOLCON-2, ACRIM-II"]
-[5.352297306060791, 0.4539889395236969, "[FF] Publication Date of the RadCalNet = 16 October 2019"]
-[5.572291374206543, 0.48000386357307434, "[TT] Launch Date of the GEOS-3 = April 9, 1975"]
-[9.699399948120117, 2.3538947105407715, "[FF] Image Color of the NuSTAR = Magenta"]
-[4.763915061950684, 7.269951343536377, "[TT] Data Rate of the X-band = 18.4 Mbit/s"]
-[12.062605857849121, -0.2569509446620941, "[TT] Extended Mission Observation Area of the TESS = Northern Hemisphere and ecliptic plane"]
-[10.248912811279297, 8.174012184143066, "[TT] Aperture Shape of the IDM = Square"]
-[7.036523818969727, 3.9131829738616943, "[FF] Primary Orbit Selection Constraint of the MANTIS = Maximising the potential image quality that can be provided by the payload"]
-[3.904095411300659, 6.560478687286377, "[TT] Antenna Type of the UHF Transceiver = Quadcanted monopole antenna array"]
-[5.445113658905029, 3.8357861042022705, "[TT] Bus Manufacturer of the Restore-L = Maxar"]
-[4.507917881011963, 5.895653247833252, "[TT] Payload of the GOMX-3 = L-band reconfigurable software-defined radio"]
-[9.074811935424805, 9.974193572998047, "[TT] Total FOV of the Eastman Kodak KLI14403 linear CCD sensor = 52\u00ba"]
-[9.27653694152832, -0.439658522605896, "[TT] Perigee of the Orbit = 789.0 km"]
-[4.809568405151367, 7.279794216156006, "[TT] Downlink Data Rate of the RF communications = Configurable between 3.5 \u2013 10 kbit/s"]
-[5.629385948181152, 3.777052164077759, "[TT] Number of Satellites Sold of the Neosat programme = 16"]
-[3.4630963802337646, 1.6803871393203735, "[FF] Conference Date of the Sentinel-1 = June 7-10, 2010"]
-[10.103241920471191, 7.3348822593688965, "[TT] Largest Feature Size of the Eureca = 2 mm hole in the ESA/ERNO logo plate"]
-[13.642145156860352, 5.799673080444336, "[TT] Max. Power of the Solar Panels = 14 W"]
-[6.235871315002441, 1.4293274879455566, "[TT] Commissioning Phase Completion Date of the eROSITA = October 13"]
-[6.935401439666748, 4.337356090545654, "[FF] Unknown of the BBR = Unknown"]
-[9.044450759887695, 3.489716053009033, "[FF] Science Objective of the ELFIN = Identify the magnetospheric source location of ionospheric field aligned currents (FACs), in relation to tail boundaries"]
-[6.767128944396973, 3.0074150562286377, "[TT] Agency of the Global GHG Monitoring Constellation = NASA, NOAA"]
-[10.318137168884277, 8.010831832885742, "[TT] Solar Image Diameter of the Telescope = 25 mm"]
-[7.812899112701416, 4.513091564178467, "[FF] Function of the LRR = Precision orbit determination"]
-[7.388420581817627, 1.1741392612457275, "[FF] Goal of the Ma_MISS = Study the martian subsurface environment"]
-[4.398460865020752, 3.132824659347534, "[TT] Location of the Ground Station = Kaluga (Russia)"]
-[7.073634624481201, 8.363847732543945, "[TT] SNR of the Band 2 = 160"]
-[4.360942363739014, 6.946965217590332, "[TT] Coverage of the Ka-band Channels = Two contiguous sectors in north-eastern US plus sixteen isolated spot beams"]
-[4.826627731323242, 0.5143054127693176, "[TT] Mission Launch Date of the Altius = 2025"]
-[7.972684860229492, 6.65293025970459, "[TT] Repeatability of the Imaging Mode = 23 (3 times)"]
-[3.985272169113159, 7.775610446929932, "[TT] Link Budget Improvement of the VCM Mode = About 2 dB in QPSK for the same transmitted power"]
-[7.683900356292725, -0.8526694178581238, "[FF] Mission Objectives of the ICESat-2 = Unknown"]
-[10.14939022064209, 1.4521828889846802, "[TT] Galaxy Catalog Size of the Euclid = More than 2 thousand million galaxies"]
-[5.474837303161621, 1.6320710182189941, "[FF] Symposium Date of the ALOS PRISM = 14 \u2013 16 May 2014"]
-[5.24001407623291, 1.1583101749420166, "[FF] Formation-flying Date of the PROBA-3 = 6 May, 2013"]
-[9.39116382598877, 5.9460344314575195, "[TT] Cross-Track Orientation of the ISA = Up to 30\u00ba"]
-[5.764134407043457, 6.044309616088867, "[TT] Data Storage of the Corvus-BC = 1TB"]
-[8.29165267944336, 0.053798459470272064, "[TT] Platform Size of the TOPEX/Poseidon = 5.5 m in length, 6.6 m in height, and 2.8 m in width"]
-[8.434345245361328, 4.586309432983398, "[FF] Frame-Dragging Accuracy of the LAGEOS-2 = 2%"]
-[8.333345413208008, 7.256553649902344, "[TT] Sensitivity (counts/s/Rayleigh) of the Full-scan Imaging = 0.016, 0.120, 0.160, 0.160, 0.020"]
-[5.022607326507568, -0.3202476501464844, "[TT] Launch Time of the BRO-6 = 6:49 p.m. Eastern"]
-[7.951910972595215, -0.9707611799240112, "[TT] ATLAS Instrument Data of the ICESat-2 = Exceeding scientists expectations"]
-[8.011429786682129, -1.0398304462432861, "[FF] Data Content of the ICESat-2 = Mexico coastline, mountains, trees, ocean waves, seafloor"]
-[5.966092109680176, 0.9439318180084229, "[TT] First Image Acquisition Date of the SEVIRI = August 4, 2015"]
-[3.7964627742767334, 4.712091445922852, "[TT] Ground-Track Repeatability of the RADARSAT-2 = \u00b1 5 km (with a goal of \u00b11 km)"]
-[11.625846862792969, 6.5841546058654785, "[TT] Proton Energy Detection Range of the LDT = Above 75 MeV"]
-[3.8741555213928223, 5.4700026512146, "[TT] Sensitivity of the Radar = 1.7 dB"]
-[8.18813419342041, 7.535646438598633, "[TT] Technology of the Detection subassembly = CCD 4720 from E2V"]
-[7.891108512878418, 2.665271282196045, "[FF] Purpose of the TIRS = Identify clouds and focus on the real land surface"]
-[6.640440940856934, 4.479039192199707, "[FF] Payload of the ResourceSat-2 = LISS-3, LISS-4 and AWiFS"]
-[6.019684791564941, 2.33815336227417, "[TT] Affiliation of the eROSITA = MPE (Max-Planck-Institute for extraterrestrial Physics), Garching, Germany"]
-[5.850882053375244, 1.058762550354004, "[FF] Eclipse Observation Date of the PROBA-2 = March 20, 2015"]
-[9.104340553283691, 5.512653827667236, "[TT] ACS Pointing Accuracy of the Spacecraft = \u00b12 arcsec"]
-[6.840154647827148, 1.7496434450149536, "[FF] Ground System Review Date of the Roman Space Telescope = 24 July 2020"]
-[10.261595726013184, 1.9771792888641357, "[FF] Sky Image Depth of the eROSITA = 4 times deeper than the previous all-sky survey by the ROSAT telescope 30 years ago"]
-[9.347311019897461, 5.00327205657959, "[TT] Attitude Variation During Maneuvers of the ISS = ~2-3\u00ba"]
-[9.949294090270996, -0.1915641576051712, "[TT] Initial Orbit Altitude of the Starshine = 387 km"]
-[10.081497192382812, -2.665107250213623, "[FF] Data Rate Performance of the SDR-SDRAM = Better than NAND-Flash"]
-[8.302887916564941, 7.396724700927734, "[TT] Response of the Photodiode = Linear"]
-[5.370815753936768, 6.512955665588379, "[TT] Accessible unit (read/write) of the SDR-SMM = 0.5 kbyte"]
-[6.315125942230225, 5.231176376342773, "[FF] Function of the Coprocessor = Real-time processing of the raw reflected GNSS data into DDMs"]
-[4.5354485511779785, 5.903258800506592, "[TT] Quantity in Use of the 406-MHz beacons = 1600000"]
-[11.901908874511719, 6.715135097503662, "[FF] Energy Range of the ECT Suite = 1 eV to 10's of MeV"]
-[4.862583637237549, 0.7437623143196106, "[TT] Launch Date of the MEPSI = July 19, 2000"]
-[4.4991044998168945, 6.8542375564575195, "[TT] Communication of the TT&C System = Effective and reliable UHF communication with BRMM"]
-[5.269408702850342, 3.9079842567443848, "[TT] Number of Satellites of the Falcon 9 = 60"]
-[7.975366115570068, -1.002581000328064, "[TT] Data Collection of the ICESat-2 = Arctic and Antarctic sea ice"]
-[5.71408748626709, 0.8058223128318787, "[TT] Launch Date of the Probe = July 15"]
-[8.146283149719238, -1.0287816524505615, "[FF] Ability of the ICESat-2 = Detect the top of the canopy and the forest floor below"]
-[5.95064115524292, 2.8598904609680176, "[FF] Budget of the UNITEC-1 = Very stringent"]
-[13.913897514343262, 7.187945365905762, "[TT] Power of the Voltage 6 = 0.93"]
-[13.798653602600098, 5.667269229888916, "[FF] Cost of the Low Cost Solar Panel = Low"]
-[9.406439781188965, 3.368382453918457, "[FF] Function of the Magnetic Field = Protecting Earth from cosmic radiation and charged particles"]
-[4.1393866539001465, 2.218909740447998, "[TT] Deployment System of the GeneSat-1 = P-POD (Poly\u00bfPicosatellite Orbital Deployer)"]
-[10.21872615814209, 8.386322021484375, "[TT] Entrance Pupil Diameter of the Lens = 10.5 cm"]
-[6.113636016845703, 3.31526255607605, "[FF] Experiment Types of the OPS-SAT = Artificial Intelligence (AI), data compression, and even financial transactions"]
-[5.106470108032227, 6.833642482757568, "[TT] Downlink Data Rate of the Astro Digital Satellites = 10 and 40Mbps"]
-[6.518872261047363, -0.5347698330879211, "[TT] Repeat Cycle of the CBERS-4 = 26 days"]
-[9.007818222045898, 5.536452293395996, "[TT] Spacecraft pointing capability of the ALOS/PRISM = \u00b11.5\u00ba (in cross-track)"]
-[8.412403106689453, 6.893421649932861, "[TT] Type of the Imager = Pushbroom imager (or a line scan imaging system)"]
-[5.4580488204956055, 6.071695327758789, "[TT] External RAM of the OBC = 524 kB"]
-[7.129093170166016, 3.0158863067626953, "[FF] Mission Status of the GeoSTAR = Expected to be used during the NOAA and Aqua missions"]
-[7.5707292556762695, 3.0770392417907715, "[FF] Capabilities of the VIIRS = Day-night imagery"]
-[5.687196254730225, 5.96664571762085, "[TT] Max No of Sequences of the C&DH module = 300"]
-[4.872739315032959, 3.293243169784546, "[TT] Manufacturer of the SEVIRI = EADS Astrium SAS, France"]
-[8.343366622924805, 7.035197734832764, "[TT] Detector Technology of the Optical Sensor Assembly (OSA) = Pushbroom detector technology"]
-[7.923502445220947, 3.050408124923706, "[FF] Purpose of the CO2 Dry Air Mole Fraction = Integral constraint on the sum of these in the form of a net flux of CO2 to and from the atmosphere at the surface"]
-[10.304025650024414, 2.3253400325775146, "[FF] Types of the Backgrounds = Cosmic X-ray, near-Earth extreme ultraviolet, instrument background"]
-[5.890548229217529, 0.7869729995727539, "[TT] Capture Date of the Image = 26 October 2019"]
-[5.002469539642334, 0.06736527383327484, "[TT] Shutdown Date of the STRV-1a = March 1998"]
-[8.270973205566406, 4.8033061027526855, "[FF] Components of the Recovery Subsystem = Inflation devices, floatation devices, localization devices"]
-[7.680440902709961, 9.104823112487793, "[TT] Wavelength Range of the Band 3 = 862-877 nm"]
-[5.167078495025635, 8.127523422241211, "[TT] Frequency Range of the ISEE-3 = 0.3 Hz to 100 kHz"]
-[13.409427642822266, 6.818829536437988, "[TT] Payload Electrical Power of the Al Yah-3 = Approximately 8.0 kW"]
-[5.906217575073242, 0.9723232388496399, "[TT] Start of Imagery Download of the TDRSS = April 2010"]
-[6.912712097167969, 7.045926094055176, "[TT] Number of Beams of the ATLAS = 6"]
-[11.549525260925293, 5.163859844207764, "[TT] Printed Circuit Board Thickness of the Sprite = A few millimeters"]
-[8.951753616333008, 9.402202606201172, "[TT] Spatial resolution of the TANSO-CAI = 1500 m"]
-[11.619461059570312, 3.727555274963379, "[TT] Firing Duration of the Y-axis Bang-Bang Maneuver = 10 s"]
-[13.38347053527832, 6.809604167938232, "[TT] Power of the Spacecraft = 1250 W max"]
-[10.363265991210938, 3.2330057621002197, "[TT] Quantity of the CubeSats = 4"]
-[10.89226245880127, 5.359116077423096, "[TT] Depth Requirement of the Heat Probe = At least 10 feet (3 meters)"]
-[6.804488658905029, 4.882594585418701, "[FF] Controller Modes of the GOCE = FPM and higher DFACS modes"]
-[7.273135662078857, 3.822944164276123, "[FF] Purpose of the CRISTAL = Monitor remote regions from space over long periods of time"]
-[4.545106887817383, 1.336776614189148, "[TT] Operational Status of the AlSat-1 = Nominally as of 2009"]
-[5.498668670654297, 6.364556789398193, "[TT] Capacity of the Mass Memory = > 2 TB"]
-[3.8516106605529785, -1.2100467681884766, "[TT] Orbit Location of the ACE Mission = First Lagrangian orbit point (L1)"]
-[11.290620803833008, 4.710743427276611, "[TT] Min. Depth of the PIRATA = 1 m"]
-[5.301198482513428, 1.576082468032837, "[FF] Environmental Testing of the Deimos-2 = Verified"]
-[10.624491691589355, 8.865497589111328, "[TT] Pixel Size of the Channel 7 = 32 x 32 km"]
-[6.679845333099365, 6.468620777130127, "[TT] Locking Time of the Comb Oscillator = Reached within seconds"]
-[6.132349491119385, 7.936816692352295, "[TT] Receive Channels of the T/R Module = 2"]
-[4.82118034362793, 0.08419659733772278, "[TT] End of Life Date of the CASSIOPE = 01 Apr 2024"]
-[13.37170124053955, 7.361489295959473, "[FF] Size, Weight, Power Reduction of the SPIDER = 10 to 100 times"]
-[5.733665466308594, 6.8759942054748535, "[TT] Checksum Size of the Processed Science Data Packet = 1 byte"]
-[6.5988287925720215, 4.154373645782471, "[FF] Operation of the HTV = Reentry"]
-[4.895071506500244, -0.8701286911964417, "[TT] Attachment Duration of the SpaceX Dragon = 18 days"]
-[7.326650619506836, 3.986170768737793, "[FF] No Arcing Condition Monitoring of the Satellite = Required"]
-[8.337996482849121, 1.5063139200210571, "[TT] Spatial Resolution of the Sea Surface Salinity (SSS) = 5 km"]
-[9.61836051940918, -0.4545024335384369, "[TT] Altitude of the ZY 1-02C = 781 km"]
-[3.9937806129455566, 2.144782066345215, "[TT] Launch Vehicle of the BepiColombo = Ariane 5"]
-[7.947752952575684, 8.73511791229248, "[TT] Spectral Coverage of the Red = 630-685 nm"]
-[8.152206420898438, -0.4491686224937439, "[FF] Average Concentration of Antarctic Sea Ice of the SSM/I of DMSP = November 2016"]
-[5.147080898284912, 0.4271540641784668, "[FF] Launch Date of the SpaceX = Jan. 10"]
-[8.121109008789062, -1.0761747360229492, "[FF] Purpose of the ICESat-2 = Space-borne determination of surface elevation"]
-[7.774064064025879, -0.7115048766136169, "[FF] Release Date of the Imja glacier, Himalayas = March 14, 2014"]
-[6.912137508392334, 5.874552249908447, "[TT] Quantity of the MEOLUTs = 4"]
-[7.264249801635742, 2.8865647315979004, "[TT] Design Stage of the MethaneSAT = Production"]
-[12.10395622253418, 6.211930751800537, "[TT] Antiproton Events of the AMS-02 = 3.49 x 105"]
-[7.973275661468506, 6.522741794586182, "[TT] Low Temporal Resolution of the SEM-2 = 30 minute averages"]
-[4.88588285446167, 2.936110258102417, "[TT] Manufacturer of the Himawari-8 = Mitsubishi Electric Corporation"]
-[4.181569576263428, 7.45432186126709, "[TT] X-band Frequency of the RF Communications = 8127 MHz"]
-[4.858524799346924, 0.25215259194374084, "[TT] Launch Date of the SPOT-2 = January 1990"]
-[6.268428325653076, 1.3979437351226807, "[FF] Decommissioning Date of the Midcourse Space Experiment = 2010"]
-[5.662700176239014, 6.423291206359863, "[TT] Recording Capacity of the Recording Subsystem = Up to 160 Mbit/s"]
-[13.263005256652832, 7.253301620483398, "[TT] Power Consumption of the CU = 10W"]
-[4.156805038452148, 4.628694534301758, "[FF] Capabilities of the Polar Epsilon = Near real-time ship detection, arctic land surveillance, environmental sensing, maritime surveillance radar beam optimization"]
-[5.250958442687988, 6.683202743530273, "[TT] Downlink Speed of the COSMO-SkyMed-1 = 300 Mbit/s"]
-[9.56861400604248, 8.250436782836914, "[TT] Field of View of the CPD = 15-45\u00ba"]
-[6.499834060668945, 0.6754322052001953, "[FF] Historical Record Publication Date of the Landsat-7 = Oct. 2006"]
-[4.286109447479248, 7.148038387298584, "[TT] Communication Signal of the FLP = S-band RF"]
-[6.0513787269592285, 5.474975109100342, "[TT] Redundancy Management Software of the S-193 = Yes"]
-[3.4037063121795654, 4.902430534362793, "[FF] Function of the SAR space segment = Provide first responders with highly accurate locations"]
-[9.876280784606934, 8.655293464660645, "[TT] IFOV of the PAN = 0.45 - 0.52 \u00b5rad"]
-[7.054299831390381, 3.4929773807525635, "[FF] Imaging Frequency of the Pelican Satellites = More than 10 photographs a day"]
-[7.390596389770508, 3.6165406703948975, "[FF] Mission of the GNSS-RO instrument = Provide radio occultation observation services to meteorological users"]
-[4.8958916664123535, 0.49317631125450134, "[FF] Launch Date of the Hugo = Later this year"]
-[6.377398490905762, -0.18746116757392883, "[FF] Shift Length of the On-call Operations = 16 hours"]
-[7.463047504425049, 2.3230671882629395, "[TT] Coverage of the Satellite = Not global: observes only one region of globe"]
-[4.449407577514648, 6.9706034660339355, "[TT] Modulation and Coding Scheme of the Sentinel-1, -2, and -3 = Accommodated within the 300 MHz X-band bandwidth"]
-[10.113314628601074, 6.940261363983154, "[TT] Spatial Resolution of the Sounder = 10 km"]
-[5.347132682800293, 3.946566581726074, "[TT] Quantity of the Dove Satellites = 88"]
-[9.704052925109863, 4.034175395965576, "[TT] Wave Height of the STEREO spacecraft = 100,000 km"]
-[8.58057689666748, 0.3278096914291382, "[TT] Size of the Asteroid Toutatis = ~ 5 km in length"]
-[8.294906616210938, 8.063724517822266, "[TT] Spectral Range of the INSAT-3D imager = 0.55 \u00b5m - 12.5 \u00b5m"]
-[6.728867530822754, 6.067512035369873, "[TT] Number of Subapertures of the PAIS = 8"]
-[3.5406556129455566, 4.75984001159668, "[FF] Components of the Second-Generation Platform = High-resolution dual-mode optical camera, Video optical camera, Dual-band Synthetic Aperture Radar (SAR) instrument"]
-[7.943488121032715, 8.957327842712402, "[TT] Wavelength Range of the NIR = 0.83 - 1.74 \u03bcm"]
-[5.687716960906982, 5.120759963989258, "[FF] Software Components of the X-band telemetry data process = Real-time data reception software, real-time data process software"]
-[3.864049196243286, 6.278505325317383, "[TT] Design Location of the Near Field Antenna Facility = In-house"]
-[1.7447010278701782, 4.564672946929932, "[FF] N/A of the UniSat-2 = N/A"]
-[13.651525497436523, 2.9554953575134277, "[TT] Storage Density of the Astrium Sentinel 2 MMFU = Factor of 8"]
-[9.142573356628418, -1.1827260255813599, "[FF] Orbit of the INSAT-3D = Geostationary"]
-[11.8986234664917, 3.2999117374420166, "[FF] Propulsion of the Hisea-1 = ThrustMe iodine electric propulsion"]
-[7.489911079406738, 1.0328980684280396, "[FF] Phosphine Upper Limit of the Mars = Unknown"]
-[4.391545295715332, 5.869242191314697, "[TT] Receiver Types of the GomX-3 = ADS-B tracking signals, telecom satellite signals, X-band signals"]
-[10.024827003479004, 5.502339839935303, "[FF] Housed Components of the CVX-2 = EP (Experiment Package) including the viscometer/sample cell, and precision temperature control elements"]
-[13.089278221130371, 6.273776531219482, "[FF] Thermal Capacity of the HORYU-2 = Very small"]
-[6.904572010040283, 4.76140022277832, "[FF] Avionics Unit of the ICPS = Unknown"]
-[5.621647357940674, -0.5064976811408997, "[TT] Operation Duration of the Block 5D-2 Satellite = Until mid-August 1991"]
-[5.100802898406982, 0.19085358083248138, "[TT] Launch Year of the NEMO-AM = 2023"]
-[5.39574670791626, 3.206862211227417, "[TT] Mission Name of the XI-V = X-factor Investigator-V"]
-[4.620975494384766, 7.756387233734131, "[TT] Protocol of the AstroDev Lithium 2 = AX.25"]
-[4.086688995361328, 1.132622480392456, "[FF] Launch Date of the H-II Transfer Vehicle \"KOUNOTORI6\" = Oct. 7, 2016"]
-[3.6358189582824707, 4.451910018920898, "[TT] Launch Year of the Capella X-SAR Constellation = 2018"]
-[5.924633502960205, 0.95503169298172, "[TT] Image Acquisition Date of the Masirah Island = 13 Jul. 2014"]
-[6.767225742340088, 5.914632320404053, "[TT] Quantity of the LAXPCs = 3"]
-[3.410325288772583, 1.9085332155227661, "[TT] Orbital Deviation of the Sentinel-1A and Sentinel-1B = \u00b150 m radius"]
-[12.901634216308594, 7.103464126586914, "[TT] Efficiency of the SFINKS = 32%"]
-[10.486939430236816, 3.320619583129883, "[TT] Classification System of the Cubesat = 1U, 2U, 3U, etc."]
-[14.051511764526367, 7.176084041595459, "[TT] Operational Input Voltage Range of the DC-DC converter = 22 to 34 V"]
-[10.055834770202637, 5.600970268249512, "[FF] Heater Rings of the FPA = Lower and upper sides of the telescope attachment"]
-[12.046618461608887, 4.51116943359375, "[TT] Size of the Spacecraft = 3.5 m height, 2.0 m diameter"]
-[4.8382954597473145, 1.8805123567581177, "[FF] Altimeter Observations of the Geosat = L. Miller, R. E. Cheney, B. C. Douglas"]
-[8.662195205688477, 0.10418497771024704, "[TT] Bipropellant System Lunar Insertion \u0394V of the Clementine = About 550 m/s"]
-[7.880518913269043, 2.5629987716674805, "[FF] Data Usage of the Aeolus = Climate Research, Weather Forecasting"]
-[4.755022048950195, 6.890774250030518, "[TT] TT&C of the Spacecraft = S-band (32 kbit/s in up- and downlink)"]
-[6.896204948425293, 5.177708148956299, "[FF] AC Current of the FSU = Produced on the collector plates"]
-[1.9312644004821777, -0.40338435769081116, "[FF] Whistler Waves Energy Transfer of the Van Allen Probes = From copious low-energy particles to sparse high-energy particles"]
-[7.420503616333008, 5.0828447341918945, "[FF] Components of the USS-02 = Upper USS-02 Assembly, Vacuum Case Assembly, Lower USS-02 Assembly, Keel Assembly, passive Payload Attach System (PAS) Assembly/Umbilical Mechanism Assembly (UMA)"]
-[7.16838264465332, 1.8921226263046265, "[TT] Launch Date of the Carbonite-2 = January 2018"]
-[4.852304458618164, 7.017903804779053, "[TT] Modes of the Myriad RF board = Full duplex"]
-[7.020810127258301, 3.4743340015411377, "[FF] URL of the PROBA-3 = http://m.esa.int/Our_Activities/Space_Engineering_Technology/"]
-[10.423088073730469, 5.911265850067139, "[TT] Brigthness Temperature (BT) of the Antenna = 100~300 K"]
-[5.482835292816162, 6.2098588943481445, "[TT] Capacity of the Data Storage = Flash memory 8 Mbit x 2 (redundancy)"]
-[8.684996604919434, 3.3630857467651367, "[FF] Mission of the Solar Orbiter = Perform unprecedented close-up observations of the Sun"]
-[11.814047813415527, 3.2292771339416504, "[TT] Thrusters of the RCS = 9 of 11 N"]
-[10.188285827636719, 5.688477993011475, "[TT] Detector Cooling of the AVHRR/3 = <105 K"]
-[7.921288967132568, 4.422052383422852, "[FF] Function of the \u00b5CPT = Measure radiation flux"]
-[6.915302753448486, 5.190850257873535, "[FF] Components of the ATMS = Antenna, motor, radio frequency system, electronic system"]
-[8.388689994812012, 0.2611924111843109, "[FF] Geological Process of the 67P/Churyumov-Gerasimenko = Mechanical shear stress"]
-[6.144153118133545, -0.06763935834169388, "[TT] Reliability of the Aeolus = 95%"]
-[8.213876724243164, -0.4748169183731079, "[FF] Minimum Extent of the Antarctic Sea Ice = Unknown"]
-[7.619645595550537, 5.290892124176025, "[FF] Structural Assembly of the Sensor Assembly = Two separate structural assemblies: the sensor assembly and the enclosure structure"]
-[4.630054950714111, 7.994129180908203, "[TT] Frequency Band of the Antenna = 8.025-8.400 GHz"]
-[4.588713645935059, 0.20795056223869324, "[FF] Launch Date of the ASTROSAT = Sept. 28, 2015"]
-[5.779058933258057, 1.3802170753479004, "[FF] Date of the JAXA Earth Observation Missions = March 8, 2013"]
-[8.356159210205078, 6.968508243560791, "[FF] Scanner Type of the MOMS-02 = Multispectral stereo scanner"]
-[6.841540336608887, 1.796783685684204, "[FF] URL of the NASA = https://www.nasa.gov/feature/jpl/nasa-maps-surface-changes-from-california-quakes"]
-[3.265190362930298, 2.255319356918335, "[FF] Users of the EDRS = Copernicus Sentinel Satellites"]
-[11.903351783752441, 6.618278980255127, "[TT] Energy Range of the NINA = 10-200 MeV/n"]
-[6.593992710113525, 4.433586597442627, "[FF] Design of the GNC = Coping with nominal and failure scenarios"]
-[9.080276489257812, 9.879297256469727, "[FF] Date of the Geometric Calibration of the MICAS CCD Sensor = July 16-23, 2000"]
-[5.472402572631836, 7.057734489440918, "[TT] Rate of the Data Transmission = 1.5 Mbit/s"]
-[9.120216369628906, -0.6926624774932861, "[TT] Orbital period of the MEOSAR Constellation = 11 h 58 m"]
-[9.871100425720215, 5.053435325622559, "[TT] Antenna Reflector Rotation of the SSM/T-1 = Once every 32 seconds"]
-[10.428640365600586, 5.657671928405762, "[TT] Suburban Neighborhood Temperature of the ECOSTRESS = Averaged about 14 F (8 C) cooler than pavement"]
-[12.520743370056152, 3.2195701599121094, "[TT] Propellant Mass of the RCS = 320 kg"]
-[14.276131629943848, 3.3046395778656006, "[TT] Mass of the STAFF/DWP = 5.6 kg"]
-[7.757894992828369, 9.198797225952148, "[TT] Wavelength of the UHF = 69 cm"]
-[8.503913879394531, 7.493508338928223, "[TT] Numerical Simulation Factor of the Photodetector = about 20000 rad/rad"]
-[4.700754165649414, 7.222641468048096, "[TT] Data Rate of the Ka-band telecom system = 3.5 Gbit/s"]
-[6.124039649963379, 5.782955646514893, "[TT] Data/Pilot of the L1-C = Pilot"]
-[9.673776626586914, -0.5838544368743896, "[TT] Closest Distance to ISS of the SZ-7 = Within 47 km"]
-[9.657159805297852, 7.005781650543213, "[TT] Altitude Resolution of the TMR = Less than 5 cm at 7 km spatial resolution"]
-[5.567563056945801, 6.26484489440918, "[TT] Installation Location of the Data Storage System = Coud\u00e9 laboratory of the OGS"]
-[9.91267204284668, 8.959956169128418, "[TT] IFOV of the Band 1 & band 2 = 1 km (vertical) x 21.7 km (horizontal)"]
-[11.166542053222656, 5.534024238586426, "[TT] Thickness of the IS = 0.5 mm"]
-[8.560569763183594, 5.7624945640563965, "[TT] Beam Pointing Error of the Antenna = Less than 0.83\u00ba (static)/0.0045\u00ba (dynamic)"]
-[9.490626335144043, 8.169129371643066, "[TT] Field-of-View of the Imagers = 30\u00b0"]
-[5.1766815185546875, 6.268031597137451, "[TT] SpaceWire Sources Handling of the PDHU = Up to 100 Mbit/s"]
-[3.866811752319336, 6.3286967277526855, "[TT] Number of RF Signals of the Antenna Subsystem = 6"]
-[4.245206832885742, 2.5656354427337646, "[TT] Launch Site of the BioSentinel = Kennedy Space Center, Cape Canaveral, FL"]
-[9.159504890441895, 3.3915672302246094, "[TT] Main Scientific Instruments of the Telescope = Wide Field Instrument and the Coronagraph"]
-[6.759868144989014, 5.900498867034912, "[TT] Quantity of the TEMD5110 = Two"]
-[5.937695503234863, 2.405709981918335, "[TT] Launch Date of the WorldView Legion = September 2022"]
-[7.64534854888916, -0.47938767075538635, "[FF] Publication Date of the IceCube-Gen2 = August 2020"]
-[8.256157875061035, 0.7921034097671509, "[TT] Containment of the Cooks Peak fire = 72 percent"]
-[2.921112298965454, 4.461226463317871, "[FF] Observation Band of the PALSAR-2 = Wide"]
-[9.62343692779541, 2.3297157287597656, "[FF] Data of the FREESTAR = Exceeded minimum requirements"]
-[5.814342021942139, -0.8021048903465271, "[TT] Design Lifetime of the RTAFSAT-1 = 3 years"]
-[7.640045166015625, 6.674405097961426, "[TT] Resolution of the HIT = 1 min"]
-[7.972081661224365, 1.889608383178711, "[FF] Level 2 Surface temperature and emissivity of the ECOSTRESS = 6 months after Level 1 data products are available"]
-[4.398523330688477, 7.568423271179199, "[TT] Frequency of the S-band transmitter = 2.4 GHz"]
-[5.274190902709961, 1.128053069114685, "[FF] Meeting Date of the COMS = Oct. 2-6, 2006"]
-[8.398659706115723, 3.24053955078125, "[TT] Type of the OSIRIS = Atmospheric chemistry"]
-[5.122699737548828, 1.9548232555389404, "[TT] Status of the CEASE = Still active"]
-[7.729803085327148, 2.4561126232147217, "[FF] Environmental Hazards Detection of the ABI = Wildfires, dust storms, volcanic eruptions, turbulence, and fog"]
-[9.55303955078125, 2.7344236373901367, "[FF] Affiliation of the Hard X-Ray Burst Spectrometer = Solar Maximum Mission"]
-[10.151744842529297, 10.012249946594238, "[FF] Announcement Date of the Vega Flight VV17 = 18 December 2020"]
-[7.113648891448975, 3.6936850547790527, "[FF] Purpose of the He-repressurization system = Raise the pressure in the main tank to an adequate pressure to complete the GRAIL mission"]
-[10.81135368347168, 5.560768127441406, "[TT] Heat Shield Diameter of the Orion = 5 m"]
-[7.420473575592041, 4.762141704559326, "[FF] Instruments of the CASSIOPE = CER, IRM, NMS, SEI, GAP, RRI, MGF, FAI"]
-[5.198575973510742, 6.998724460601807, "[TT] Data Rate of the Downlink = 100 Mbit/s"]
-[5.946659088134766, 1.4884977340698242, "[FF] Rocket Engine Test Date of the PRISMA Satellites = June 24, 2010"]
-[3.1495187282562256, 2.179248571395874, "[FF] Expansion of the Copernicus = With a suite of new, high-priority satellite missions"]
-[5.550685882568359, 5.766909122467041, "[TT] Model of the RAD6000 CPU = RAD6000"]
-[6.08567476272583, 6.0419697761535645, "[FF] Data Reliability of the TT&C = Lower criticality compared to ISL"]
-[5.729337692260742, -0.8619088530540466, "[TT] Design Life of the FS2 = 5 years"]
-[8.137292861938477, 8.523055076599121, "[TT] Sampling of the VNIR Spectral Bands = 10 m bands"]
-[11.802349090576172, 3.246657371520996, "[TT] Launcher Thrust of the EDRS-C = 1340 t"]
-[11.70154857635498, 3.4012181758880615, "[TT] Quantity of the Propulsion controller = 2"]
-[5.102889537811279, 3.5661239624023438, "[FF] Recipient of the Payload = Clyde Space"]
-[16.55372428894043, 3.650904655456543, "[TT] Total Fleet Size of the OneWeb = 648"]
-[4.4544219970703125, 0.7029255628585815, "[TT] Operational Date of the DMSP F-18 = March 2010"]
-[8.0709228515625, 0.8370698094367981, "[FF] Focus of the WatER = Hydrologic processes related to the spatial and temporal variability in global terrestrial surface fresh water storage"]
-[9.414765357971191, 8.12784194946289, "[TT] Aperture Diameter of the LLNL imaging system = 85 mm"]
-[9.209376335144043, 7.72634220123291, "[TT] Attachment Method of the LWIR Camera = Room temperature vulcanizing silicone-566 (RTV)"]
-[7.106828212738037, 4.993255138397217, "[FF] Tracking Location of the High Altitude Multiple Object Tracking System (HAMOTS) = Utah Test and Training Range (UTTR)"]
-[6.52738094329834, 7.6087117195129395, "[FF] Data Quantization of the Pushbroom imager = 8 bit (dynamic), 11 bit (total)"]
-[5.403428077697754, 0.9117468595504761, "[FF] Demonstration Date of the LIRIS = March 19, 2014"]
-[7.341940879821777, 1.1115033626556396, "[TT] Brochure Release Year of the OceanSat-2 = 2007"]
-[8.629514694213867, 5.538233757019043, "[TT] Position Error of the GPSR = 20 m in 3-D (1\u03c3)"]
-[5.983085632324219, 4.916749000549316, "[FF] Conference Date of the Telemetry Monitoring and Analysis System = April 25-30, 2010"]
-[9.878950119018555, 7.914872646331787, "[TT] Imaging Resolution of the NuSTAR = Sub-arcminute"]
-[4.937779903411865, 7.962085723876953, "[TT] Bandwidth of the RF communication subsystem = 20 kHz"]
-[7.852059841156006, 2.5484445095062256, "[FF] Data Uses of the Aeolus = Predicting the weather, improving climate models, tracking events in near-realtime"]
-[9.465951919555664, 6.220526695251465, "[TT] Plane Scanning Angle of the Scanning geometry = 108\u00ba, 54\u00ba"]
-[3.3540918827056885, 5.375720500946045, "[TT] Center Radar Frequency of the SAR-RCM = 5.405 GHz"]
-[8.074599266052246, -0.9984022378921509, "[FF] Objective 1 of the ICESat-2 = Quantify the polar ice sheet mass balance"]
-[8.638714790344238, 2.411329984664917, "[TT] Vertical Resolution (Troposphere) of the Aeolus = 1.0 km"]
-[7.92615270614624, -0.3865675628185272, "[TT] Location of the Cryo-cooler = Space"]
-[9.981472969055176, 3.2053885459899902, "[FF] Purpose of the CubeSats = Test new technologies, fly single science instruments, provide real-world space experience for students, provide daily imagery of the Earth, deploy a global broadband Internet constellation"]
-[6.209957599639893, 1.937930703163147, "[FF] URL of the eROSITA = http://www.russianspaceweb.com/spektr-rg-launch-attempt2.html"]
-[5.122842788696289, 6.7911577224731445, "[TT] Downlink Data Rate of the TRACE spacecraft = 2.25 Mbit/s"]
-[5.1628289222717285, 4.930493354797363, "[TT] Type of the GPS-Ex ATT = GPS-Ex"]
-[8.214935302734375, -0.012395458295941353, "[FF] User Count of the TOPEX/Poseidon = More than 600 scientists in 54 countries"]
-[11.804676055908203, 6.748470306396484, "[TT] Energy Resolution of the GRS = \u2264 9% at 662 keV"]
-[2.287447214126587, 2.773641347885132, "[TT] Co-PI of the EPI-Lo = Dick Mewaldt"]
-[3.1908671855926514, 1.6634430885314941, "[TT] Revisit Time of the Sentinel-2 = 10 days"]
-[9.674311637878418, 8.342885971069336, "[TT] Field of View (FOV) of the PH4 = Disk of 700 km radius"]
-[3.2244837284088135, 5.359405040740967, "[TT] Spotlight Scene Size of the SAR Antenna = 5.5 km side"]
-[13.617178916931152, 1.8902000188827515, "[FF] Cargo Delivery of the SpaceX = More than 2,910 kg"]
-[7.535312175750732, -2.448516845703125, "[FF] Installation Date of the GOLD = May 17, 2017"]
-[12.151174545288086, 3.5472779273986816, "[TT] High Pressure Tank Size of the I-COUPS = 2.0 L"]
-[12.1547269821167, 4.681082725524902, "[TT] Bus Structure Dimensions of the EURECA = 4.6 m x 2.6 m"]
-[6.183621406555176, 5.558523654937744, "[TT] Redundancy of the CDSU = Not redundant"]
-[8.385226249694824, 0.16665592789649963, "[TT] Anomalous Jet Firing ?V of the ICE (International Cometary Explorer) = 32 m/s"]
-[4.751944065093994, -0.20294088125228882, "[FF] Status Update Date of the CATS = March 12, 2015"]
-[5.247437477111816, 5.62831449508667, "[TT] Standard of the Communication Protocol = CCSDS"]
-[9.849006652832031, 2.7396397590637207, "[FF] Partner of the Weather Observation Satellite = NanoAvionics"]
-[8.554106712341309, 4.444634914398193, "[TT] Trajectory Correction Maneuver of the MarCO-A = Completed"]
-[7.164826393127441, 1.8981118202209473, "[TT] Launch Date of the Carbonite-1 = July 2015"]
-[7.866488456726074, 6.984592914581299, "[TT] Integration Time of the WiFS camera = 28.42 ms"]
-[7.105975151062012, 5.998876094818115, "[FF] Interval of Writing Timer Information to ROM of the MOBC = Unknown"]
-[8.293875694274902, 5.744674205780029, "[TT] Absolute Accuracy of the FFRF sensor = 1 cm on distance"]
-[5.106853485107422, 2.358377456665039, "[TT] Mission Type of the PhoneSat-1 and -2 = Non-EO"]
-[5.074112892150879, 3.4097275733947754, "[TT] Manufacturer of the LCT = Tesat-Spacecom"]
-[9.428315162658691, 3.6949503421783447, "[FF] Measurement Location of the MMS and THEMIS = Dayside magnetopause"]
-[5.969676494598389, 1.6530380249023438, "[FF] Conference Date of the Micro Satellite = Aug. 10-13, 2009"]
-[11.28370475769043, 4.760908603668213, "[TT] Number of Launch Tubes of the Picosa Launcher = 4"]
-[8.585467338562012, 0.28642982244491577, "[FF] Comet Discoveries of the SOHO = 2000"]
-[5.141660213470459, 3.011058807373047, "[TT] Prime Contractor of the FGS = COM DEV Space Systems of Ottawa Canada"]
-[9.066513061523438, 8.106809616088867, "[FF] Unknown of the Ring Imaging Cherenkov detector = Unknown"]
-[7.1840338706970215, 6.620565891265869, "[TT] Integration Time of the MWR = 0.24 s"]
-[5.969367027282715, 2.5262298583984375, "[FF] Tester of the ISIM = Randy Kimble"]
-[8.895316123962402, 6.451608180999756, "[FF] Image Type of the CaSSIS instrument = Stereo pairs"]
-[7.1974711418151855, 7.149735927581787, "[FF] Photon Detection of the ATLAS = Few to ~10 photons per footprint per laser fire"]
-[9.570296287536621, 7.685695171356201, "[TT] Number of Pixels/Image of the Telescope = 25 Mpixel"]
-[6.880938529968262, 2.990001678466797, "[TT] Mission Status of the Global GHG Monitoring Constellation = Operational (nominal)"]
-[5.387759208679199, 2.512606382369995, "[FF] Partners of the TacSat-3 = NRL (Naval Research Laboratory), AFRL (Air Force Research Laboratory), DARPA (Defense Advanced Research Projects Agency), the Army Space and Missile Defense Center, and the USAF Space and Missile Systems Center"]
-[13.359984397888184, 6.7468791007995605, "[FF] EP Technologies of the Busek = Iodine-fueled HETs up to 10 kW power"]
-[8.075119018554688, 0.8525478839874268, "[TT] Drought Percentage of the U.S. Drought Monitor = 99 percent"]
-[10.970279693603516, 2.0686001777648926, "[TT] Planned Lifetime of the XMM-Newton = 10 years"]
-[4.916323184967041, 3.495842933654785, "[TT] Manufacturer of the HYLAS-3 = MDA Corporation (Canada)"]
-[4.877818584442139, 7.3000969886779785, "[TT] Data Rate (Downlink) of the S-band transmitter = 32 kbit/s to 1 Mbit/s"]
-[14.493999481201172, 6.699406147003174, "[TT] Charge / Discharge Cycles of the Supercapacitor = Millions"]
-[6.3194804191589355, 6.356258869171143, "[TT] Data Request Time of the CEASE = 72 hours"]
-[9.137405395507812, 8.267013549804688, "[TT] First Natural Frequency of the AEISS telescope = > 70 Hz"]
-[5.606561183929443, 2.80843186378479, "[FF] Development Authors of the Tactical Satellite 3 = T. M. Davis, S. D. Straight"]
-[2.983569383621216, 2.428586959838867, "[FF] Detection Capability of the Copernicus Sentinel-5P = Methane cloud, nitrogen dioxide plumes from individual ships"]
-[9.322589874267578, 6.034820556640625, "[TT] Optical Axis Displacement of the Satellite = \u00b130\u00ba in steps of 2\u00ba"]
-[8.273573875427246, 0.2773231565952301, "[TT] Subsidence Rate of the Tulare Basin = 0.3 meters per year"]
-[10.954465866088867, 7.56606388092041, "[TT] Swath Width of the SMMR = Approximately 600 km"]
-[12.437646865844727, 0.6324113011360168, "[TT] Number of Fast Cameras of the PLATO = 2"]
-[4.827167510986328, 6.053376197814941, "[TT] Source of the ASICs = Indigenous"]
-[13.482550621032715, 5.578869819641113, "[FF] Advantages of the Semi-conductive coating = Cost savings, does not require change in solar array design"]
-[4.918453693389893, 8.351520538330078, "[TT] Frequency Bands of the MWI = 10, 18, and 37 GHz"]
-[6.843860626220703, 5.111937522888184, "[FF] Components of the Electrical System = C&DH (Command & Data Handling), PSS (Power Supply Subsystem), ADCS (Attitude Determination and Control Subsystem), Structures and Mechanisms, TCS (Thermal Control System), Communication subsystem including the TT&C (Telemetry, Tracking & Command) and the high-speed communication systems"]
-[12.079201698303223, 3.325681686401367, "[TT] Propellant Expulsion of the Advanced Composition Explorer = The pair of the tanks with less fuel expelled all of its propellant by 2014"]
-[6.414799690246582, 1.2541732788085938, "[FF] Study Purpose of the SJ-10 satellite = Enhance the comprehension of fire mechanism under microgravity"]
-[9.405229568481445, 4.978231430053711, "[TT] Attitude Control Error of the ADCS = \u2264 30 \u00b5rad"]
-[5.553511619567871, 3.7328827381134033, "[TT] Total Satellite Passes of the KSAT = 50,000 a month"]
-[9.835076332092285, -0.4646700322628021, "[TT] Orbit Altitude of the Satellite = ~670 km"]
-[5.364911079406738, 8.761149406433105, "[TT] Bandwidth of the Band 8 = 0.608 \u00b5m (50 cm -1)"]
-[12.146653175354004, -0.12058255821466446, "[TT] Camera Quantity of the TESS = 4"]
-[5.017416954040527, 3.4060745239257812, "[TT] Manufacturer of the EDRS = Tesat Spacecom"]
-[10.512213706970215, 2.226769208908081, "[TT] Time Accuracy of the NICER X-ray telescope = Better than 100 ns"]
-[4.90239143371582, -0.5998397469520569, "[TT] Initial Operations Completion Date of the SLATS = March 2018"]
-[5.795688152313232, 7.173891067504883, "[TT] Data Rates of the PID 238 = 50kb to 66MHz"]
-[4.743537425994873, 0.8483237028121948, "[TT] Birthday of the PROBA-V = May 7, 2014"]
-[9.260324478149414, 5.106415748596191, "[TT] Attitude Pointing Accuracy of the GF-2 spacecraft = 0.0025\u00ba"]
-[5.868788719177246, 0.23359520733356476, "[TT] Launch Date of the PARASOL = Dec. 18, 2004"]
-[6.621739864349365, 7.426028728485107, "[TT] Analog to Digital Conversion of the Front End Electronics = 12 bit"]
-[8.026496887207031, 5.788455963134766, "[TT] Micro Vibration Correction of the Instrument = Confirmed"]
-[10.455370903015137, 2.265376329421997, "[TT] Temporal Resolution of the X-ray telescopes = 2 \u00b5s"]
-[10.870007514953613, 2.092862367630005, "[FF] Targeted Regions of the XMM-Newton = LMC, Hickson Cluster Group 16 (HCG-16), HR 1099"]
-[14.104206085205078, 3.161151647567749, "[TT] Weight of the Yutu 2 = 140 kg"]
-[5.297630786895752, 1.2359466552734375, "[FF] Mission End Date of the SMOS = Unknown"]
-[4.221041202545166, 2.5720646381378174, "[TT] Launch Site of the ALL-STAR-1 = Cape Canaveral, FL"]
-[9.175106048583984, 1.2862842082977295, "[FF] Time to Reach Oort Cloud of the Voyager 2 = About 300 years"]
-[9.65842056274414, 4.50080680847168, "[FF] Attitude Control of the QSat = 3-axis stabilization by using RWs (nominal), magnetorquers (detumbling)"]
-[10.187034606933594, 5.288011074066162, "[FF] Performance of the Cold Gas Pressurization System = Satisfactory"]
-[5.2483601570129395, 2.3724446296691895, "[FF] In-Orbit Validation Element of the GIOVE = Unknown"]
-[11.390584945678711, 4.205082416534424, "[TT] Size of the Sunstorm = 3U"]
-[5.365389823913574, 0.9579464793205261, "[FF] Publication Date of the TRUTHS = December 2003"]
-[3.718989133834839, 5.114128112792969, "[TT] Imaging Frequency Band of the ERS-2 = C"]
-[10.14254093170166, 8.0631742477417, "[TT] Telescope Focal Length of the TRACE instrument = 8.66 m"]
-[7.075437545776367, 7.003570556640625, "[TT] Spatial Mode of the Laser = M 2 < 1.6"]
-[8.236658096313477, 0.7439298033714294, "[FF] Composition of the Earth's Core = Molten, iron-rich and in vigorous motion"]
-[4.404310703277588, 7.817692279815674, "[TT] Uplink Frequency of the CMC Transceiver = 140-150 MHz"]
-[9.179009437561035, 3.74971342086792, "[FF] Dynamic Testing Measurement of the Solar Array = Accelerometers on the mandrel"]
-[8.017531394958496, 6.331003189086914, "[FF] Design and Development Status of the METimage = Unknown"]
-[10.71926498413086, 0.9298430681228638, "[FF] Presence of the Hot Jupiters = Hints at the presence of even younger hot Jupiters"]
-[9.407394409179688, 4.792853832244873, "[FF] Attitude Control Issue of the MarCO = Wobbling and losing the ability to send and receive commands"]
-[7.012052059173584, 3.707228183746338, "[FF] Unknown of the PROBA-3 = Unknown"]
-[7.138462543487549, 4.636503219604492, "[FF] Function of the Ground Software = Search the optical counterparts of the GRB"]
-[3.8489153385162354, 0.9169796705245972, "[FF] Launch Date of the PSLV-C37 = Unknown"]
-[5.149057388305664, 6.958601951599121, "[TT] Max Data Rate (Mbit/s) of the LET = Uplink: 1244 Downlink: 1244"]
-[12.004326820373535, 4.854647159576416, "[TT] Size of the GPS Receiver = 120 mm x 70 mm x 21 mm"]
-[6.270573139190674, -0.5123399496078491, "[TT] Nominal Mission Start of the Observatories = About 90 days after launch"]
-[4.561142444610596, 7.076350688934326, "[TT] S-band Usage of the CBERS-2B = TT&C services"]
-[6.684927463531494, 1.1635276079177856, "[FF] Daily Revisit Capability of the FormoSat-2 = Significant and very useful for post disaster assessment and environmental monitoring"]
-[7.776937484741211, 2.9362452030181885, "[FF] Emission Sources of the Nitrogen Dioxide (NO2) = Burning of gasoline, coal, and diesel fuel by motor vehicles, power plants, and industrial facilities"]
-[9.901049613952637, 8.099570274353027, "[TT] Single Shot Accuracies of the TOR = 3-4 cm"]
-[6.381761074066162, -0.07819809019565582, "[TT] Coverage Repeat Period of the S/C = 5.5 days"]
-[4.4571356773376465, 1.6804434061050415, "[TT] LTDN of the RADARSAT-2 = 6am"]
-[5.031497001647949, 3.329225778579712, "[TT] Manufacturer of the Wren = StaDoKo UG, Aachen, Germany"]
-[11.405814170837402, 5.725535869598389, "[TT] Composition of the Nickel Alloy = 5% Mo and 11 W"]
-[5.9922194480896, 1.5298629999160767, "[FF] Presentation Date of the Small Satellites = April 3-6, 2017"]
-[3.11568546295166, 2.2105250358581543, "[TT] Cross-Calibration Precision of the Copernicus Sentinel-6 = Within 1 mm"]
-[4.871337890625, 0.9848936796188354, "[FF] Development to Commercialization Date of the AIS = Nov. 19, 2010"]
-[10.087874412536621, -1.5699896812438965, "[TT] Orbit Inclination of the ALOS-3 = 97.9\u00b0"]
-[10.688445091247559, 3.3247506618499756, "[FF] Subject of the Micro-gravity experiment = Multi-layer heat capillary convection"]
-[5.711054801940918, 6.222146034240723, "[TT] Access Method of the OBP (Onboard Processor) = MC-TDMA (5 channels/carrier)"]
-[9.396872520446777, 3.566202402114868, "[FF] Position of the Magnetic Pole = Shifting towards Siberia"]
-[7.042542457580566, 8.236705780029297, "[TT] SNR Variations of the OISL = Limited to about 1 dB"]
-[6.733327865600586, 5.144174575805664, "[FF] Function of the PIU = Performs the final signal processing for energy determination and time stamping"]
-[4.853653430938721, 7.872990131378174, "[TT] Frequency (MHz) of the Galileo E1-B/C = 1575.42"]
-[10.612530708312988, 5.263905048370361, "[TT] Distance to M3 of the M2 = 10 \u00b5m"]
-[11.799997329711914, 0.05900639295578003, "[TT] Data Source of the TESS = Exoplanet discovery"]
-[10.17444896697998, 0.9798994064331055, "[TT] Distance from Earth of the TOI 270 = About 73 light-years"]
-[4.824352264404297, 1.816768765449524, "[TT] Anomaly Duration of the HORYU-2 = One month"]
-[4.194277763366699, 7.305267810821533, "[FF] Frequency Band of the COPS = Ka-band"]
-[3.8104918003082275, -1.1993684768676758, "[TT] Destination of the ART-XC = Second Lagrange point (L2) of the Sun-Earth system"]
-[5.220013618469238, 1.0067144632339478, "[FF] Presentation Date of the 3MI = October 16, 2013"]
-[8.580109596252441, 1.9407198429107666, "[TT] Range of values of the Ocean surface wind speed = 3-25"]
-[8.637609481811523, 1.072187066078186, "[FF] URL of the Aquarius = http://aquarius.nasa.gov/pdfs/11-181_Aquarius_Launch_SC.pdf"]
-[12.022688865661621, -0.36211246252059937, "[FF] Arrival Date of the TESS = Feb. 15, 2018"]
-[4.608563423156738, 6.677640438079834, "[FF] Components of the Command Communications System = VHF command receiver, pair of redundant UHF command and telemetry transceivers"]
-[10.235910415649414, 5.146325588226318, "[TT] Thermal Control of the ITASat CubeSat = Passive"]
-[5.565913200378418, 5.597042560577393, "[TT] Processor of the BMU = MAR 31750"]
-[6.015378475189209, 2.355165719985962, "[FF] Disciplines of the EuTEF = Material science, physics, astrobiology and astronomy"]
-[4.890326023101807, 1.3491638898849487, "[FF] Development Announcement Date of the MIRAS = Nov. 1997"]
-[6.915133476257324, 1.8299814462661743, "[FF] URL of the Arrokoth = https://www.aaas.org/news/close-arrokoth-reveals-how-planetary-building-blocks-were-constructed"]
-[10.435765266418457, 4.1059675216674805, "[TT] Function of the Hypersonic Grid Fins = Control the stage's lift vector"]
-[9.576725006103516, 7.148054599761963, "[TT] Spatial Resolution at Nadir of the Scanning geometry = 1 km"]
-[7.965867042541504, 0.5344014763832092, "[FF] Conference Presentation Date of the Near Earth Asteroid Scout = 1 Aug 2014"]
-[7.2223711013793945, 6.467772483825684, "[TT] F-number of the Instrument = F73.7"]
-[13.481734275817871, 2.7971298694610596, "[TT] Dry Mass of the Spacecraft = 2169 kg"]
-[10.988685607910156, 5.6671977043151855, "[FF] Function of the Avcoat = Burns away (i.e., it ablates) in order to prevent heat being transferred into the crew module"]
-[5.907561779022217, 7.175110816955566, "[TT] Data Capture Rate of the MinXSS-2 = At least 6%"]
-[13.616471290588379, 7.481649875640869, "[TT] Supply Voltage of the Myriad RF board = 5 V"]
-[6.545781135559082, -0.5494731068611145, "[FF] Transfer Time of the Spacecraft = 7 days"]
-[3.730574369430542, 3.875311851501465, "[TT] Eclipse Phase of the RISAT-1 = May 2 \u2013 August 12, 2012"]
-[6.919154167175293, 6.032833099365234, "[TT] Quantity of the CSS = 6"]
-[9.506855964660645, 1.0096185207366943, "[TT] Speed of the Sally = 2 miles per hour"]
-[5.756030559539795, -0.3138880431652069, "[TT] Deployment Time of the iROSA = 6.5 hours"]
-[5.5976243019104, 6.023390293121338, "[TT] Tape Recorder of the CBERS-1 = High Density Tape Recorder (HDTR)"]
-[9.40734577178955, 6.9419965744018555, "[TT] Resolution of the ALOS-2 = Down to 6 m"]
-[6.546032428741455, 6.951015949249268, "[TT] Duty Cycle of the HPA = 12%"]
-[10.168936729431152, 3.2158405780792236, "[FF] Type of the CubeSats = DIY"]
-[6.948318958282471, 6.12966775894165, "[TT] Number of Systems of the Instrument = 5"]
-[6.522367000579834, 3.158566474914551, "[FF] Conference Presentation Date of the UK Disaster Monitoring Constellation Satellite = September 2002"]
-[3.819380283355713, 4.560328006744385, "[FF] Radar Parameters of the RADARSAT-2 = Resolution and sensitivity"]
-[6.167884349822998, 4.987949848175049, "[FF] Operation of the ISL = Usually operate without any ground intervention"]
-[14.281135559082031, 3.1529653072357178, "[TT] Mass of the PTOLEMY = 4.5 kg"]
-[3.179246187210083, 5.052201747894287, "[TT] SAR Image Parameters of the QLP/NRTP = Resolution: 1-12 m (ground range) x 1-48 m (azimuth)"]
-[9.034339904785156, 6.829902172088623, "[TT] Additional Camera Resolution of the PROBA-1 = 5 m"]
-[9.338793754577637, 3.228802442550659, "[FF] Function of the SPS = Verify the safe centering of the entrance pupil of the coronagraph into the shadow cone of the occulting disc"]
-[8.654687881469727, 2.059152841567993, "[TT] Measurement Methods of the Wind speed = 4 ways"]
-[6.7569146156311035, 6.192579746246338, "[TT] Generation of the ABI = 3rd"]
-[7.389524459838867, 6.231884479522705, "[TT] Measurement Technique of the SLR = Satellite Laser Ranging"]
-[6.947615146636963, 7.086236476898193, "[TT] Laser Diode of the HSC-III = 5mW laser diode (630 nm)"]
-[6.186002254486084, 6.3662848472595215, "[TT] Fastest Delivery Time of the Ground Network = As fast as 11 minutes"]
-[5.867643356323242, 4.309094429016113, "[FF] Operational Capability of the SSPIDR = Power 'on demand' anywhere on the globe regardless of weather or latitude, day or night and without vulnerable logistics lines"]
-[7.834605693817139, 8.966303825378418, "[TT] Wavelength Range of the S-020 = 1-20 nm (or 10 - 200 \u00c5)"]
-[7.874249458312988, 2.0334205627441406, "[FF] Impact on ILRS of the GOCE = Negative"]
-[5.768411159515381, -0.38295066356658936, "[TT] Expected Lifetime of the TSX = Several more years"]
-[7.306355953216553, 9.135564804077148, "[TT] Filter Wavelength of the ISUAL instrument = 762 nm"]
-[3.466373920440674, 4.7099995613098145, "[FF] Program Start of the SIR-C/X-SAR = SIR-A in l98l"]
-[4.49729061126709, 1.5476369857788086, "[TT] Launch Date of the FedSat = 14 Dec 2002"]
-[7.7875871658325195, 5.68006706237793, "[FF] Type of the SMM/I = DoD multifrequency microwave radiometer"]
-[9.7918062210083, -0.2276707887649536, "[TT] Altitude at Entry Interface Point of the Experiment Data = 120 km"]
-[7.638919830322266, -2.4588828086853027, "[FF] Parameter of the GOLD = Value"]
-[4.527212619781494, 6.338256359100342, "[TT] Communication Access Scheme of the COMPASS/BeiDou = CDMA"]
-[6.933652877807617, 1.4916149377822876, "[TT] Launch Date of the James Webb Space Telescope = 25 December 2021"]
-[7.458231449127197, 8.74709415435791, "[TT] Filter Thickness of the VIS channel = 3.00 mm"]
-[8.135345458984375, 4.265644073486328, "[TT] Track Spacing of the ERS-1 = ~8 km at the equator"]
-[7.633539199829102, 4.731324672698975, "[FF] Performance of the DFACS = Excellent"]
-[5.905229568481445, 5.182114601135254, "[TT] Operation of the ROSA = Performs position, time and velocity calculation based on a least square algorithm"]
-[10.131755828857422, 1.226325511932373, "[TT] Distance to Vela supernova of the eROSITA = 800 light-years"]
-[9.85860824584961, 8.067117691040039, "[TT] Field of View of the ART-XC = 0.3\u00ba x 0.3\u00ba, 36' diameter"]
-[5.468899250030518, 4.202096462249756, "[TT] Developer of the ADAM = ITR (Institute for Telecommunications Research) at the University of South Australia"]
-[14.657382011413574, 6.642716407775879, "[TT] Li-ion Battery of the EPS = ABSL (UK), 35 kg, 126 Ah"]
-[11.698634147644043, 0.17195457220077515, "[FF] Planet Size Range of the TESS = Earth-sized to gas giants"]
-[8.65854549407959, 2.474619150161743, "[FF] Location of the Polar Vortex = High above the North Pole in the polar stratosphere"]
-[12.801079750061035, 7.641051292419434, "[TT] Power of the Instrument = 30 W"]
-[7.691841125488281, 9.395407676696777, "[TT] Center Wavelength of the Band 12 = 6.51 \u00b5m (1535 cm -1)"]
-[2.962059259414673, 4.427768707275391, "[TT] Beam Steering of the XSAR = Electronic scanning capabilities in the azimuth and the elevation planes"]
-[7.240252494812012, 8.66813850402832, "[TT] Reflected Radiation Channel Spectral Band of the ISP-2 = 0.3 - 3.0 \u00b5m"]
-[4.770321369171143, 0.5455575585365295, "[FF] Launches Per Year of the SES-GS = 3 to 4 missions"]
-[6.109562873840332, -0.21775434911251068, "[TT] Period of the ISS = ~ 93 minutes"]
-[9.295351028442383, 5.653230667114258, "[TT] Pointing Error of the ASTERIA = Arcsec-level"]
-[12.183886528015137, 3.2260921001434326, "[TT] Propellant of the Propellant Tank = AF-M315E"]
-[3.362215042114258, 6.377720355987549, "[TT] Dimensions of the Dipole Antenna = 10 x 30 cm"]
-[11.271539688110352, 5.854922294616699, "[TT] Structure Material of the TUBSAT-N = Carbon fiber"]
-[4.850724697113037, 3.1880974769592285, "[TT] Manufacturer of the ERO = Airbus"]
-[9.401538848876953, 5.434499740600586, "[TT] Solar Separation Angle of the STARE satellites = > 30\u00ba"]
-[5.578424453735352, 4.913361549377441, "[TT] Platform of the Ground Software Architecture = Windows or Linux PCs"]
-[3.2303249835968018, 5.716763019561768, "[TT] Size of the SAR antenna = 6 m (along-track) x 2 m (cross-track)"]
-[10.03183650970459, 8.162461280822754, "[TT] Aperture of the Optical Payload = 85 mm"]
-[14.014486312866211, 4.030264377593994, "[TT] Mass of the Field Measurement Device = < 0.1 kg"]
-[7.726876735687256, 3.99733567237854, "[TT] Formation Control of the PROBA-3 = 6DOF with thrusters"]
-[9.87392807006836, 7.52646017074585, "[TT] Sampling Distance of the HIRS/4 = 18 km"]
-[12.170814514160156, 3.1194584369659424, "[TT] Propellant Duration of the Butane Propulsion System = 3-4 years"]
-[7.189778804779053, 4.640210151672363, "[FF] Purpose of the GNC = Improvement of the guidance algorithms, coupling of inertial measurement units with GPS for navigation, exploration of the combination of flaps and thrusters for flight control"]
-[5.231204032897949, 0.42597493529319763, "[TT] Extended Mission Start Date of the TRACE = April 1999"]
-[7.95261812210083, 9.13614559173584, "[TT] Wavelength of the LORE = 322 nm"]
-[10.642163276672363, 4.416873931884766, "[TT] LEDs of the DSAT-2 = Light up the impact space"]
-[6.715222358703613, 5.0769453048706055, "[FF] Function of the Onboard Neural Network = Detecting whistlers"]
-[7.772453784942627, 3.5098297595977783, "[TT] Data Cadence of the IMPACT and PLASTIC = Approximately 1 minute"]
-[4.271359443664551, 3.8980050086975098, "[FF] Signal Usability of the Galileo = Usable in all new mobile phones"]
-[12.087498664855957, 4.504161834716797, "[TT] Dimensions of the Landmapper-Demo6 = 0.524 m x 0.524 m x 0.62 m"]
-[8.67921257019043, 2.0630624294281006, "[TT] Wind Speed Accuracy of the Scatterometer = 2 m/s or 10%"]
-[4.839095592498779, 0.691768229007721, "[TT] Launch Date of the GOES-R satellite = 2016"]
-[12.057705879211426, -0.23802503943443298, "[FF] Data Downlinking of the TESS = Busy downlinking all of the stored data"]
-[5.501093864440918, -0.12410421669483185, "[TT] Deactivation Date of the RapidEye = March 2020"]
-[10.237627029418945, 5.35673189163208, "[FF] Application of the Loop Heat Pipe Radiator (LHPR) = Future spacecraft"]
-[5.282922267913818, 1.2816462516784668, "[FF] Conference Date of the NICT's New OGS = May 16-20, 2016"]
-[11.185712814331055, 5.152530670166016, "[TT] Distance of the Test Masses = 376 mm"]
-[5.473425388336182, 6.388496398925781, "[TT] Telemetry Data Storage of the RF Communications = Onboard memory"]
-[5.180367946624756, 4.852055072784424, "[TT] GPS Receiver of the CanX-2 = Commercially available"]
-[6.628756523132324, 6.182102680206299, "[TT] Safe-hold Mode Activation Time of the GOES-17 = 1:37 a.m. EDT"]
-[5.209009170532227, 0.03618946298956871, "[TT] End of Life Date of the GeoEye-1 = September 2023"]
-[5.280571460723877, 6.222130298614502, "[TT] Purpose of the Service Link = Communication between the user terminal and the payload (or vice versa)"]
-[3.619588613510132, -0.9656549096107483, "[FF] Orbit Type of the EQUULEUS = 1:4 synodic resonant periodic orbit"]
-[9.178133010864258, 7.025951385498047, "[TT] Resolution of the MGF = ~0.1 nT"]
-[7.831438064575195, 8.476346015930176, "[TT] Band Count of the COCTS = 8 visible, near-infrared bands"]
-[5.54201078414917, 2.2367279529571533, "[FF] Affiliation of the Yukihoro Takahashi = Unknown"]
-[7.452186584472656, 5.684169769287109, "[FF] Components of the LAC = Laser transmitter, concave mirror/detector"]
-[5.0829267501831055, 0.8938581943511963, "[FF] Mission Analysis Date of the PROBA-3 = Nov. 19, 2012"]
-[6.959056377410889, 5.164083480834961, "[FF] Components of the ASC = Control, telemetry, telecommand and power conditioning electronics"]
-[8.634700775146484, 1.3559943437576294, "[TT] Accuracy of the Aquarius = < 0.2 psu"]
-[7.695202350616455, 0.7186412215232849, "[FF] Previous Observations of the Lunar Flashlight = Surface reflectance variations measured by the LOLA 1064 nm laser altimeter and the ice-like reflectance spectra measured by M3"]
-[9.485944747924805, 4.695018768310547, "[FF] Design of the LAS = Active jettison motor, inert abort motor, inert attitude control system"]
-[5.578236103057861, 2.923544406890869, "[TT] Primary Funding of the DSX = AFRL"]
-[6.182156085968018, 1.062511920928955, "[TT] Image Credit of the CaSSIS = ESA/Roscosmos/CaSSIS"]
-[9.433327674865723, 0.8823922276496887, "[TT] Closest Approach to the Sun of the SOHO = 1,165,000 km"]
-[6.211777210235596, 1.565554141998291, "[FF] URL of the GeoEye-1 = http://www.eurimage.com/products/pdf/e-GEOS%20GeoEye.pdf"]
-[11.466608047485352, 4.638753414154053, "[TT] Deployed Length of the HY-1 = About 7.5 m"]
-[8.991257667541504, 3.570580244064331, "[FF] Purpose of the GOLF = Study of the internal structure of the sun by measuring the spectrum of free global oscillations"]
-[6.560070037841797, 7.65264368057251, "[TT] Data Quantization of the Visible Spectral Band = 6 bit"]
-[11.31517219543457, 0.942878007888794, "[TT] DRS Duration of the LISA Pathfinder = 90 days"]
-[5.157872676849365, 0.7754266262054443, "[FF] Publication Year of the WMO = 2016"]
-[7.803905963897705, 8.08613395690918, "[FF] Function of the Instrument = Broadband spectral determination of composition and distribution of volatiles"]
-[5.166599750518799, 6.823912620544434, "[TT] Uplink Data Rate of the Spacecraft = 9.6 or 19.2 kbit/s"]
-[13.999165534973145, 7.097123146057129, "[TT] Supply Voltage of the G-EPS = 12 Volt"]
-[7.997702121734619, 7.083224296569824, "[FF] Multispectral Imagery Collection of the R3 System = Successful"]
-[5.324492454528809, 3.9646987915039062, "[TT] Maximum Number of Satellites of the Telescope = Feasible if there are 1,000 satellites"]
-[8.396358489990234, 8.270797729492188, "[TT] Spectral Resolution of the Instrument = 1200 (lambda/delta lambda)"]
-[7.451329708099365, 8.377632141113281, "[FF] Number of Eligible Rows of the QWIP Array = Not specified"]
-[10.931014060974121, 5.455374240875244, "[TT] Length of the Heat Probe = 16 inches (40 centimeters)"]
-[9.985990524291992, 4.374703407287598, "[FF] Effect of Earth's magnetic field of the Reaction Wheels = Causes a weak drag"]
-[3.56943941116333, 4.62562894821167, "[FF] Function of the SAR (Synthetic Aperture Radar) = Capture the reflections of signals sent by Sentinel-1 to Earth"]
-[7.074796199798584, 6.853382587432861, "[TT] Laser Type of the Laser Altimeter (LALT) = Nd:YAG"]
-[8.509671211242676, 5.394519329071045, "[TT] Orbit Reconstruction Accuracy of the GBOT = 150 m in position and 2.5 mm/s in motion"]
-[6.647828578948975, 4.637327671051025, "[FF] Function of the SPS = Signal to the satellite (CSC) that the umbra moves out of the nominal position range of the SPS"]
-[10.08829402923584, 2.9650187492370605, "[TT] Temperature Monitoring Duration of the CubeSat = 154 days"]
-[6.680179119110107, 2.8435466289520264, "[FF] Components of the Look-Up Table = Radiative transfer simulations by MODTRAN"]
-[5.801996231079102, 7.161636829376221, "[TT] Vector Sample Rates of the NewMag = Internal = 1000/s, Standard = 10/s, Burst mode = 100/s"]
-[4.809615135192871, 5.711516380310059, "[TT] Frequency (MHz) of the GPS L5 = 1176.45"]
-[8.188502311706543, 2.8076248168945312, "[TT] Measurement Domain of the IMAGE = Atmosphere"]
-[5.025410175323486, 2.7012927532196045, "[TT] Developer of the Kappa Scheme = Professor Kanya Kusano"]
-[5.520555019378662, -1.8624848127365112, "[FF] Distribution Agreement Date of the KOMPSAT-2, -3, -3A and -5 = November 2012"]
-[7.592671871185303, 3.8735599517822266, "[FF] Implementation Complexity of the Occultation Techniques = Easy to implement in principle"]
-[3.8643665313720703, 1.346490502357483, "[TT] First Stage Flights of the Rocket = 15"]
-[8.858553886413574, 6.469387054443359, "[FF] Tree Height Measurement of the SLA altimeter = Possible"]
-[3.7170889377593994, 6.421627044677734, "[TT] Antenna Quantity of the NCLE = 3"]
-[5.956754207611084, -0.5746573805809021, "[TT] Expected Orbit Lifetime of the NuSTAR = 10 years"]
-[4.955686092376709, 0.5287608504295349, "[TT] Launch Date of the EM-1 = 2019"]
-[8.657572746276855, 5.836849212646484, "[TT] Position Accuracy of the CTECS-A = Improved"]
-[11.959455490112305, 4.376078128814697, "[FF] Size of the Nightingale site = The size of a small parking lot"]
-[3.065793991088867, 2.296762228012085, "[TT] Spatial Resolutions of the Sentinel-2 = 10 to 60 m"]
-[7.722620964050293, 5.546177864074707, "[FF] Instrument Function of the SMMR = Accurate corrections were provided for both instruments"]
-[5.249969482421875, 2.8297762870788574, "[TT] Operator of the UWE-1 = Student team at the University of W\u00fcrzburg"]
-[13.740482330322266, 3.1010830402374268, "[TT] Mass of the Sentinel-1C = 2.3 tons"]
-[5.685007572174072, 7.094704627990723, "[TT] Data Rate of the MBEI = ~184 Mbit/s"]
-[7.562804222106934, 3.5377554893493652, "[FF] Debris Containment Bags of the DSAT-2 = Unknown"]
-[8.306631088256836, 0.01614723727107048, "[TT] Global Sea Level Rise of the GRACE = 11.2 mm (0.4 inches)"]
-[12.1333589553833, 3.1692895889282227, "[TT] Propellant Manufacturer of the GPIM = U.S. AFRL (Air Force Research Laboratory)"]
-[4.7247209548950195, 0.0671122670173645, "[TT] End of Life Date of the ALL-STAR = 26 May 2014"]
-[5.094402313232422, 3.3111960887908936, "[TT] Manufacturer of the MSU-GS = FSUE/RISDE (Federal State Unitary Enterprise) / Russian Scientific Institute of Space Device Engineering"]
-[7.912343502044678, 6.5114030838012695, "[FF] Time Resolution of the Cameras = Lower than photometers"]
-[7.970453262329102, 3.8191909790039062, "[FF] Instrument Type of the AMSR = Atmospheric chemistry"]
-[7.879578590393066, 5.77955436706543, "[TT] Image Navigation and Registration Process of the ABI = Ground processing"]
-[8.542415618896484, 6.1175336837768555, "[TT] Calibration of the CERES = Highly calibrated"]
-[7.777119159698486, 9.152254104614258, "[TT] Radio Wave Wavelength of the ALOS-2 = 15 - 30 cm"]
-[4.773472785949707, 1.8852193355560303, "[TT] Observation Operation Completion of the MTSAT-2 = Around 2015"]
-[13.662581443786621, 5.7999958992004395, "[TT] Electric Power of the Double junction thin film solar cells = 3.6-4 W"]
-[5.188357830047607, 0.6051913499832153, "[FF] Newsletter Date of the NEXTAR = Q1 2011"]
-[10.807835578918457, 3.945537567138672, "[FF] Expected Stabilization Effect of the CanX-7 = Aerodynamically stabilize due to the so-called \"shuttlecock\" effect"]
-[13.72043228149414, 2.918950319290161, "[TT] Payload Mass of the Resurs-DK1 = 1200 kg"]
-[8.306117057800293, 0.757216215133667, "[TT] Burned Area of the Calf Canyon-Hermits Peak Fire = Exceeded 300,000 acres"]
-[6.248992443084717, 5.333909511566162, "[FF] About Author of the Optical Inter-orbit Communications Engineering Test Satellite (OICETS) = Yasuhiro Morita"]
-[7.287176132202148, 5.121689319610596, "[TT] TLE Events Recorded of the ISUAL = 35,000"]
-[8.008325576782227, 8.335923194885254, "[TT] Vibration Suppression of the VISS = >20 dB"]
-[10.17568302154541, 4.097536087036133, "[TT] Position of the ULF Sensor = Tip of the gravity gradient boom"]
-[7.1388444900512695, 3.898963451385498, "[TT] Small Fragments Quantity of the DMSP-F13 = More than 50,000"]
-[14.672927856445312, 6.698763847351074, "[TT] Quantity of the NiH2 batteries = 4"]
-[8.140548706054688, -1.0887609720230103, "[FF] Ability of the ICESat-2 = Detect the seafloor up to 30 m below the surface"]
-[14.053494453430176, 3.175441265106201, "[TT] Client Mass of the ELSA-d = ~20 kg"]
-[13.385953903198242, 2.918496608734131, "[TT] Mass (kg) of the RADARSAT-2 = 2200"]
-[10.872179985046387, 3.905226707458496, "[TT] Formation Ranges of the CanX-4 = 50 m"]
-[7.379906177520752, 2.8870835304260254, "[TT] Mission Focus of the MethaneSAT = Collecting data about methane emissions from the oil and gas industry"]
-[8.889528274536133, 4.857986927032471, "[TT] Saturation of the Honeywell QA2000-030 accelerometers = Around 27.5 rpm"]
-[10.34904956817627, 3.363689422607422, "[TT] Design of the QuakeSat = CubeSat"]
-[5.269168853759766, 7.40235710144043, "[TT] Margin of the EV-9 = 3 dB"]
-[6.297738075256348, 2.939042329788208, "[TT] Altitude of the WorldView Legion = 450 km"]
-[13.873329162597656, 3.5204579830169678, "[FF] Weight of the Wireless Compose-2 = One kilogram"]
-[11.724212646484375, 3.3115954399108887, "[FF] Maximum Number of Admissible Thruster Firings of the RVX = Unknown"]
-[9.127885818481445, 4.650604724884033, "[FF] Subsystem Type of the AOCS = Attitude and Orbit Control"]
-[5.209193229675293, 2.3962645530700684, "[TT] Mission Type of the OPS-SAT = EO"]
-[5.417094707489014, 2.991603374481201, "[FF] Development Organizations of the SPIDER = Lockheed Martin Advanced Technology Center (LM ATC) and University of California at Davis (UC Davis)"]
-[5.2270050048828125, 6.864292144775391, "[TT] Internet Access Speed of the EUTELSAT KONNECT = Up to 100 Mbit/s"]
-[5.027434825897217, 5.861599922180176, "[FF] Function of the NanoCom SDR = Provides the CCSDS data stream to the transmitter"]
-[5.1161956787109375, 8.375200271606445, "[TT] Bandwidth of the Total RF bandwidth = 900 MHz"]
-[14.22874927520752, 3.102069854736328, "[TT] Mass of the Rising-2 = 43 kg"]
-[9.779696464538574, 8.77975082397461, "[TT] FOV of the Infrared Bands = 3 mradians"]
-[13.971634864807129, 7.043563365936279, "[TT] Operating Voltage of the AMI-302 = 3 V"]
-[4.961141586303711, 3.361410140991211, "[TT] Manufacturer of the LALT = NEC Corporation"]
-[4.778367042541504, 0.5811923146247864, "[TT] Launch Date of the STARE-B = November 20, 2013"]
-[9.019129753112793, 3.7486624717712402, "[TT] Monitoring Frequency of the High-voltage solar array = Every minute"]
-[7.536319255828857, 2.884922742843628, "[FF] Focus of the Commercial small satellites = Detecting methane rather than carbon dioxide"]
-[3.9404399394989014, 1.9656702280044556, "[TT] Serial Number of the Rocket 3.3 = LV0007"]
-[4.726679801940918, 7.140361785888672, "[TT] S-band Downlink Data Link of the RF communications = 2 Mbit/s"]
-[7.588172435760498, 3.6105284690856934, "[FF] Objective of the CDMS = Characterize the debris and micrometeoroid environment of GTO"]
-[6.965015888214111, 1.5766910314559937, "[TT] Detection Capability of the James Webb Space Telescope = Water and carbon dioxide"]
-[4.697605609893799, 1.5362937450408936, "[TT] CDR Date of the GCOM-W1 = December 2009"]
-[6.380615234375, -0.7970972061157227, "[TT] LTAN of the GCOM-W1 = 13:30 hours"]
-[4.647799491882324, 6.6586761474609375, "[FF] Components of the TT&C subsystem = Low power S-band transceiver, microstrip antenna, two full duplex VHF/UHF transceivers, deployable turnstile antennas"]
-[7.585005760192871, -0.8994362354278564, "[FF] Continuous Attitude Mode Duration of the ICESat = Approximately six months"]
-[6.654159069061279, 3.382915735244751, "[FF] Purpose of the CIRAS = Demonstrate a critical science and meteorological measurement in a significantly smaller package enabling use in constellations for improved latency"]
-[11.480072021484375, 5.6883721351623535, "[FF] Young Modulus of the Inconel alloy = ~130 GPa"]
-[6.768829822540283, 5.827904224395752, "[TT] Quantity of the ISIPODs = 9"]
-[10.180476188659668, 1.4255200624465942, "[TT] Image Object Density of the Gaia = 750,000 objects/deg2"]
-[10.199317932128906, 8.405736923217773, "[TT] Pupil Diameter for HR of the Instrument = 75.6 mm"]
-[12.232361793518066, 6.920965671539307, "[TT] Energy Range for Electrons of the LEICA = 0.4-30 MeV"]
-[13.626287460327148, 2.9652950763702393, "[TT] Mass (kg) of the COSMO-SkyMed = 1700"]
-[10.145639419555664, -2.7659308910369873, "[TT] Erase Time of the NAND-Flash = 2 ms per block (64 pages)"]
-[10.148950576782227, -0.5036196708679199, "[TT] Orbit Altitude of the CANYVAL-X CubeSats = 505 km"]
-[11.359214782714844, 3.45886492729187, "[FF] Use of the Electric Propulsion = Reduce the mass of satellites"]
-[6.7032012939453125, 4.102710247039795, "[TT] Autonomy of the RapidScat = Autonomous"]
-[8.07243824005127, 7.063212871551514, "[FF] Number of Channels of the Interferometer Arrays = Same as a digital camera"]
-[3.230363130569458, 3.863123893737793, "[TT] Science Mission Start of the TanDEM-X and TerraSAR-X = September/October 2014"]
-[9.841883659362793, 5.605144023895264, "[TT] Decenter of the M4 = 50 \u00b5m"]
-[12.46381950378418, 0.5934814810752869, "[TT] Short Observation Phase Duration of the PLATO = Between 2 and 5 months"]
-[7.246917724609375, 4.602652072906494, "[TT] Mounting Location of the CDE = Top of the spacecraft"]
-[5.702110290527344, 2.3378193378448486, "[FF] Status of the MADRAS = Unknown"]
-[13.523372650146484, 2.8921103477478027, "[TT] Satellite Mass of the TROPOMI = 900 kg"]
-[6.343669891357422, 1.6848570108413696, "[FF] URL of the MMO = http://www.stp.isas.jaxa.jp/mercury/p_mmo.html"]
-[10.28660774230957, 5.403309345245361, "[FF] Thermal Control Methods of the Neutron-1 = Passive, Conducting heat through copper strapping, Using external spacecraft surfaces as thermal radiators, Turning off subsystem hardware"]
-[5.216142177581787, 3.5505454540252686, "[TT] Imager Manufacturer of the HySIS = ISRO\u2019s Space Application Centre (SAC)"]
-[7.242550849914551, 5.226318359375, "[FF] Components of the ALRad system = OMT (Orthomode Transducer), OMT couplers, CND (Correlated Noise Diode), two diplexers, RFE (Radiometer Front End), RBE (Radiometer Back End), DPU (Digital Processing Unit)"]
-[10.436795234680176, 6.872304916381836, "[TT] Observation Limit of the 1.2 meter mirror = Magnitude 24.5"]
-[7.0274481773376465, 8.35037899017334, "[TT] Estimated SNR of the Band 7 = 388.29 \u00b1 153.69"]
-[7.3905839920043945, 3.439549684524536, "[FF] Purpose of the EPS GRAS = Operational GPS Meteorology"]
-[10.876800537109375, 10.034993171691895, "[FF] Publication Date of the Iridium engineering magnetometer = December 15, 2000"]
-[6.332250118255615, -1.3476048707962036, "[TT] Launch Date of the GRACE-FO = May 19, 2018"]
-[11.253267288208008, 5.373213768005371, "[TT] Scintillator Thickness of the Gamma-ray Counter = 5 mm"]
-[3.1989939212799072, 1.6855403184890747, "[TT] Data Stream Availability of the Sentinel-6 = Within hours of collection"]
-[9.788084030151367, 6.933424949645996, "[TT] Background in HPD (10 - 30 keV) of the Instrument = 6:8 x 10 -4  cts/s"]
-[5.225623607635498, 4.804259300231934, "[TT] Duration of the Ground Station Passes = 8 hours"]
-[3.49398136138916, 4.848512649536133, "[FF] Program of the JERS-l = SAR (Synthetic Aperture Radar)"]
-[13.379778861999512, 7.341804504394531, "[TT] Device Power of the TCU/TRC = 3 W, 1.5 W"]
-[9.623023986816406, 6.953799247741699, "[TT] Spatial Resolution of the Nighttime SST Product = 2 km"]
-[7.536090850830078, 8.561810493469238, "[TT] Number of Turrets of the Mechanical Turrets = 3 for each spectral range"]
-[7.998720169067383, 1.9475703239440918, "[TT] Swath of the Coastal Zone Scanner = 800 km"]
-[9.329597473144531, 6.66823148727417, "[TT] Storage Capacity of the KazEOSat-2 = Up to 4000 km"]
-[10.102230072021484, 5.505136966705322, "[FF] Application of the PIRPL = Develop thermal sensors that can detect hypersonic missiles and other advanced weapons while in flight"]
-[4.807466506958008, 1.3920973539352417, "[TT] Launch Date of the G\u00f6kt\u00fcrk-1 = December 5, 2016"]
-[14.21550178527832, 3.3049426078796387, "[TT] Mass of the Herley MD2000C-1 = 425 gram"]
-[3.817164421081543, -0.9887852072715759, "[FF] Orbit of the IRNSS-1C = GTO and then raised into GEO"]
-[14.072744369506836, 4.04722785949707, "[TT] Mass of the Instrument = ~50 kg"]
-[5.420053958892822, 3.9353694915771484, "[TT] Planned Number of the Future Satellites = 2200"]
-[4.3244147300720215, 7.208274841308594, "[FF] Frequency of the X-band = Unknown"]
-[13.736223220825195, 3.6874544620513916, "[TT] Mass of the SAR Antenna = Exceeding 700 kg"]
-[14.327638626098633, 3.2005112171173096, "[TT] Mass of the ILAS = 130 kg"]
-[11.789981842041016, 4.929680347442627, "[TT] Dimensions of the ChipSats = 3.5 by 3.5 centimeters, with a thickness of just a few millimeters"]
-[6.2157721519470215, 6.972057342529297, "[TT] Data Rate of the SIOS Optical Link Demonstration Board = 1 Mbit/s"]
-[4.325540065765381, 2.76902174949646, "[TT] CoReCi Unit of the Sentinel-2A = Carried"]
-[10.138057708740234, 1.4824094772338867, "[TT] Companion Galaxy of the M51b = M51b"]
-[7.878485679626465, -0.02383498288691044, "[TT] Rotation Period of the Asteroid 1999JU3 = Around 7.6 hours"]
-[9.173944473266602, 3.901970386505127, "[FF] Components of the Plasma Wave Instrument = Triaxial magnetic search coils, pair of electric dipole antennas, two sweep-frequency receivers, multichannel analyzer, low frequency waveform receiver, wideband waveform receiver"]
-[10.449045181274414, 5.7075653076171875, "[TT] Operational Temperature Range of the ECS = -43\u00baC to 41\u00baC"]
-[5.8848795890808105, 0.2031450718641281, "[TT] First Flight Date of the TOMS = Oct. 24, 1978"]
-[8.478110313415527, 6.356686115264893, "[TT] Measurement Interval of the GLAS = 170 m"]
-[9.899421691894531, 2.656311511993408, "[FF] Largest Satellite Deployment of the NanoRacks = 20 June 2018"]
-[6.317438125610352, 1.1060196161270142, "[FF] Observation Date of the Space Sparkle = 7 January 2019"]
-[12.018244743347168, 3.016223669052124, "[TT] Orbit Transfer Thrusters of the EURECA = Redundant 4 x 21 N hydrazine thrusters"]
-[5.437802791595459, 0.40713661909103394, "[FF] Date of the OA-7 Space Station Cargo Resupply = April 18, 2017"]
-[4.368982791900635, 5.306246280670166, "[TT] Frequency of the Cospas-Sarsat Beacons = 406 MHz"]
-[4.7349090576171875, -1.8162755966186523, "[FF] Unknown of the Chang'E-1 = Unknown"]
-[9.076751708984375, 4.53732442855835, "[TT] Signal-to-Noise Ratio of the System = >120 at a 15-degree sun elevation angle for a 15% reflective object"]
-[13.261028289794922, 7.35883903503418, "[TT] Power Status of the EXIS = On"]
-[5.76252555847168, 3.790802478790283, "[FF] Number of Satellites in 2025 of the Sateliot IoT nanosatellite constellation = 250"]
-[10.651519775390625, 1.5102125406265259, "[TT] Extension of the Gaseous Atmosphere = Several hundred miles from the neutron star"]
-[9.89889907836914, -0.645298421382904, "[TT] Orbit Altitude of the MightySat II.1 (Sindri) = 556 km"]
-[12.080964088439941, 6.38698673248291, "[TT] Isotropy of the Positron Fraction = Within 3%"]
-[9.727714538574219, -0.4534631073474884, "[TT] Altitude of the Corvus-BC 5 = 481 km"]
-[5.520583629608154, 6.39656400680542, "[TT] Data Storage Capacity of the C&DH module = 2GB"]
-[6.040670394897461, 0.42419567704200745, "[TT] Primary Mission Duration of the ASTERIA = Three months"]
-[7.962453365325928, -2.57877516746521, "[TT] Wavelength Range of the GOLD = 132 to 162 nm"]
-[5.54817533493042, 5.653143405914307, "[TT] CPU of the XSAR Payload = 80486DX2 CPU"]
-[9.0654296875, -0.4040760397911072, "[TT] Apogee (km) of the Intercosmos- Bulgaria 1300 (Intercosmos-22) = 906"]
-[9.468780517578125, 4.967952728271484, "[TT] Attitude Stability of the AOCS = <0.003\u00ba/s"]
-[3.852429151535034, 6.561126232147217, "[TT] Type of the Sprite\u2019s antenna = Half-wave V-dipole"]
-[7.553032398223877, 6.697789192199707, "[TT] Tracking Capability of the MEOSAR = Almost instantaneous"]
-[2.286640167236328, 2.773655891418457, "[TT] Co-PI of the EPI-Lo = Stefano Livi"]
-[9.588470458984375, 7.429919719696045, "[TT] Angular resolution (2 px) of the FSI dual EUV 174 \u00c5 and 304 \u00c5 alternatively = 9 arcsec"]
-[8.270589828491211, 3.2926278114318848, "[FF] Measurable Gases of the OMI = Formaldehyde (a VOC) and nitrogen dioxide (NO2)"]
-[6.354979515075684, 5.46267032623291, "[TT] Status of the DCS = Operating nominally"]
-[5.329224109649658, 5.780074596405029, "[TT] Protocol of the N-FEE and N-DPU = RMAP"]
-[7.671371936798096, 6.774420261383057, "[TT] Rotation Time of the M-CAM 1 = Less than two minutes"]
-[8.521056175231934, 1.8231879472732544, "[TT] Absolute Accuracy of the Cloud amount = \u00b1 20%"]
-[12.067984580993652, 3.36346435546875, "[TT] Water Capacity of the Steam Propulsion Unit = Up to 30 grams"]
-[7.385093688964844, 9.16818618774414, "[TT] Filter Wavelength Range of the ISUAL instrument = 250-390 nm"]
-[10.502216339111328, 3.0239179134368896, "[TT] Components of the EDSN = CubeSat nanosatellites"]
-[5.675154209136963, 8.741646766662598, "[TT] Filter Bandwidth of the MCS = 10 nm FWHM"]
-[7.969821453094482, 6.544220447540283, "[TT] Time Resolution of the SEDA = 10 s"]
-[13.36946964263916, 7.352723598480225, "[TT] Power of the TCS = 2 W"]
-[6.367825508117676, 5.495156288146973, "[FF] Objective of the SOTA/SOCRATES mission = Fundamental experiment for laser communication between LEO and the ground"]
-[10.415010452270508, 2.850389242172241, "[TT] Ground Station of the Nanosatellite = Kagawa University"]
-[10.27108097076416, 3.1731820106506348, "[TT] Failure Rate of the CubeSats = 40%"]
-[3.42992901802063, 6.407230854034424, "[TT] Antenna Aperture Size of the GMI = 1.2 m"]
-[9.604044914245605, -0.3990408778190613, "[TT] Altitude Range of the SOLSE-2 = 10 km to 50 km"]
-[5.497468948364258, 5.841251373291016, "[TT] Protocol Version of the DCPS = SSP protocol version 2.1"]
-[2.9967844486236572, 2.1921942234039307, "[FF] Image Resolution of the Copernicus Sentinel-2 = Not provided"]
-[5.639616012573242, 0.537477433681488, "[FF] Observation Date of the OGO 3 = February 1, 1970"]
-[13.531478881835938, 2.7768044471740723, "[TT] Wet Mass of the OSC = About 250 kg"]
-[13.443511009216309, 6.830471515655518, "[TT] Power of the Spacecraft = 1.75 kW (EOL)"]
-[11.717623710632324, 3.3344435691833496, "[TT] Quantity of the Cold Gas Thrusters (CGT) = 12 on the OSC"]
-[3.977989435195923, 2.089794397354126, "[TT] Wrapping of the Launch Box = Foam"]
-[5.639161109924316, 4.359790325164795, "[FF] Development Lessons Learned of the EDSN = Unknown"]
-[13.279994010925293, 7.420161247253418, "[TT] Energy Distribution Steps of the WTS1 and WTS2 = 20"]
-[5.218908309936523, 8.029145240783691, "[TT] First Natural Frequency of the EOU = > 300 Hz"]
-[6.778282642364502, 5.946112632751465, "[TT] Operation of the MAP-PACE = Continuous"]
-[8.147918701171875, -0.33392253518104553, "[FF] Impact of the Arctic Sea Ice = Affects local ecosystems, regional and global weather patterns, and the circulation of the oceans"]
-[9.750438690185547, 4.140118598937988, "[TT] Resolution of the Vector Magnetometer = < 0.25 nT"]
-[6.199257850646973, 0.8706784844398499, "[TT] Launch Status of the FormoSat-7/COSMIC-2 Satellite = Cancelled"]
-[4.416818618774414, 3.1395938396453857, "[TT] Location of the Ground Station = Panska Ves (Czech Republic)"]
-[9.711858749389648, 7.18510627746582, "[TT] Cross-track resolution of the S-band = 20-45 km"]
-[6.990079402923584, 6.264885902404785, "[TT] Operating Mode of the CATS = Mode 2 (532 & 1064 nm backscatter)"]
-[4.172121047973633, 6.264034271240234, "[FF] Engineer of the ESA antenna = Peter de Maagt"]
-[6.2750091552734375, 8.069510459899902, "[TT] Rx Channels of the Reduced Solution = 2"]
-[8.32094669342041, 1.5444059371948242, "[TT] Accuracy Range of the Rain rate = 0-5 mm/hr"]
-[7.443314552307129, 2.216247797012329, "[FF] Purpose of the Vizca\u00edno Biosphere Reserve = Important whale sanctuary for the North Pacific grey whale"]
-[5.219005107879639, 1.3454138040542603, "[TT] Expected Completion Date of the ELSA-d = April 2020"]
-[7.398354530334473, 3.5623059272766113, "[FF] Observation of the STSat-1 = Airglow"]
-[9.943060874938965, 8.214517593383789, "[TT] Relative Aperture of the WPM = 5.9"]
-[5.409204959869385, 2.7368388175964355, "[FF] Owner of the INSAT-3D = Indian Space Research Organisation (ISRO)"]
-[10.024304389953613, -1.612938404083252, "[TT] Orbit Inclination of the Secondary Payloads = 98.8\u00ba"]
-[3.1882550716400146, 1.6633752584457397, "[TT] Revisit Time of the Sentinel-2C = Every five days"]
-[13.37848949432373, 7.416865825653076, "[TT] Peak Power of the TR modules = 10 W"]
-[7.560187339782715, 2.9044036865234375, "[TT] Components of the Compact Environmental Anomaly Sensor 3 = Two particle telescopes"]
-[7.108991622924805, 0.03353705629706383, "[FF] Age Difference of the IC 4665 and Collinder 350 = More than 500 million years"]
-[7.543928623199463, 6.289700984954834, "[FF] Data Acquisition of the Advanced Topographic Laser Altimeter System (ATLAS) = Elevation data"]
-[4.516698837280273, 0.2897263765335083, "[FF] Article Date of the AstroSat = February 25, 2013"]
-[3.4145238399505615, 6.288679599761963, "[TT] Ground Antenna Size of the RADARSAT-1 = About 10 m diameter"]
-[10.013900756835938, 8.010749816894531, "[TT] Separation Distance of the Optics Assembly = 285 mm"]
-[3.4846553802490234, 6.461991786956787, "[TT] Antenna Footprint of the SIRAL = 15 km"]
-[12.10791301727295, 4.490549087524414, "[TT] Dimensions of the Satellite = 6m high with a width of 2 m x 2.4 m"]
-[6.4815568923950195, 3.1230456829071045, "[TT] Manager of the Space Weather Network = ESOC"]
-[5.737540245056152, 6.226335525512695, "[FF] Data Transfer Capability of the CASCADE = Large digital data files (10s to 100s of GBytes) within hours"]
-[6.376800060272217, 4.303868770599365, "[FF] Status of the RESOURCESAT-2 = Functioning Satisfactorily"]
-[8.602301597595215, 3.919956922531128, "[FF] Function of the AMBRE = Detect low level ions and electrons"]
-[7.2314300537109375, 1.3663562536239624, "[TT] Instrument of the ExoMars Trace Gas Orbiter = Atmospheric Chemistry Suite (ACS)"]
-[5.278410911560059, 0.093988798558712, "[FF] Berthing Date of the Cygnus = July 16, 1014"]
-[11.804600715637207, 6.737206935882568, "[FF] Photon Energy Spectrum of the PSR B0531+21 = 0.5-5 keV"]
-[13.609557151794434, 5.893080234527588, "[FF] Functions of the PCU = Battery charge / discharge control, peak power tracking (PPT) control for power generation of the solar cells"]
-[11.649158477783203, 4.213828086853027, "[TT] Dimensions of the NorSat-3 = 0.62 m x 0.56 m x 0.33 m"]
-[6.180107593536377, 2.983043909072876, "[TT] Image Revisit Rate of the WorldView Legion = Up to 15 times per day"]
-[6.716520309448242, 5.971426486968994, "[TT] Quantity of the Tabs = 2"]
-[8.446488380432129, 4.65806245803833, "[FF] Type of the CSC FVM, SI = Magnetic field, Precision orbit, Atmospheric temperature and humidity sounders"]
-[8.436806678771973, 6.665103435516357, "[TT] Instrument Type of the Hyperion = Pushbroom"]
-[9.446710586547852, 6.032978534698486, "[TT] Cant Angle of the Vidicons = 26\u00ba from the vertical"]
-[4.866876125335693, 7.020440578460693, "[TT] Duplex of the RF Communications = Half"]
-[6.034004211425781, 1.1014933586120605, "[FF] Launch Date of the SJ-9 Technology Demonstration Satellite = Oct. 13, 2012"]
-[7.128056526184082, 7.318295955657959, "[TT] Laser Wavelengths of the WNISAT-1 = 1570 nm and 1556 nm"]
-[5.794971466064453, -2.202204704284668, "[TT] Horizontal Error 90% (HE90) of the KOMPSAT-3 = 13.3 meters"]
-[8.073948860168457, 1.9838004112243652, "[FF] Measurement of the ALACE Floats = Global subsurface circulation"]
-[4.173437118530273, 4.3685197830200195, "[TT] Operation Hours of the COSPAS-SARSAT system = 24 hours a day, 365 days a year"]
-[10.47725772857666, 5.463744640350342, "[FF] Active Thermal Control of the TCS = Polyimide heating film"]
-[3.1774790287017822, 2.3390963077545166, "[FF] Mission Objectives of the Sentinel-2 MSI = Habitat mapping of coral reefs, Coral reef change detection, Bathymetry over coral reefs"]
-[9.821979522705078, 4.178712368011475, "[FF] Magnetic Field of the AMS-02 = Intense and quite uniform field perpendicular to the vertical axis"]
-[13.290142059326172, 6.967397689819336, "[TT] Power Consumption of the PPCU ion thruster = <403 W @ 11.5 mN, <580W @ 17 mN"]
-[8.514695167541504, 2.7512686252593994, "[FF] Observation Area of the TARANIS = Altitudes of 20 to 100 km over thunderstorms"]
-[7.6819963455200195, 3.9351770877838135, "[FF] Angular Rate Detection of the Satellite = Too small to detect it when using the FOG measurements"]
-[9.639891624450684, 8.36248779296875, "[TT] Field of View of the FOV = 20\u00ba x 20\u00ba"]
-[5.921817302703857, 0.6360213160514832, "[TT] Launch Date of the ASTERIA = Nov. 20, 2017"]
-[8.418119430541992, 3.259500026702881, "[TT] Observation Accuracy of the Instrument = 5% (1% for ozone)"]
-[5.385270595550537, 5.8659563064575195, "[TT] Unidirectional Port Protocol of the NIC = Clock, data, and enable"]
-[9.37257194519043, -0.28587180376052856, "[TT] Perigee of the Satellite = 240 km"]
-[8.448583602905273, 0.49491292238235474, "[TT] Water Depth of the Navigable Area Limit Lines (NALL) = 3.5 meters (11 feet)"]
-[6.616072654724121, -1.1596336364746094, "[FF] Data Integration of the GRACE-FO = With data from the original GRACE mission (2002-2017) and with current and historical ground-based observations"]
-[9.43545150756836, 7.586895942687988, "[TT] Resolution of the Telescope camera = Up to several meters per a pixel"]
-[4.414742469787598, 7.84577751159668, "[TT] Uplink Frequency (Normal C-band channel) of the Communication Payload = 5850-6410 MHz"]
-[10.457947731018066, 5.5300984382629395, "[FF] Purpose of the Thermal Protection and Hot Structures = Validation of the flight performance of thermal protection materials and complex design solutions"]
-[10.071069717407227, -1.5659185647964478, "[TT] Inclination of the JPSS-1 = 98.7\u00ba"]
-[10.803550720214844, 7.448821067810059, "[TT] Swath Width of the GF-2 = 45 km"]
-[4.508115291595459, 1.2858256101608276, "[TT] Collaboration Start Date of the AlSat-2A = 2003"]
-[6.1937103271484375, 4.5342020988464355, "[FF] Command and Control Capability of the MEIDEX = Remote Payload Operations Control Center (POCC)"]
-[9.299759864807129, 4.835840225219727, "[FF] Responsibility of the AMICA = Providing real-time information for compensating the large uncertainties in the ISS flight attitude and the structural degrees of freedom"]
-[7.220578193664551, 1.1936815977096558, "[TT] Sampling System of the Mars 2020 Perseverance rover = Coring drill and sample tubes"]
-[8.829729080200195, 0.840830385684967, "[TT] Topographic Elevation Difference of the Lander = 3 km to 7 km"]
-[3.8653922080993652, 0.8999167680740356, "[FF] Launch Date of the PSLV-C33/IRNSS-1G = April 28, 2016"]
-[5.344432353973389, 6.7330121994018555, "[TT] Data Transport of the SPA-U = USB 1.1 limited to 12 Mbit/s"]
-[6.937447547912598, 7.335031509399414, "[TT] Beam Walk on QPR of the LRI = < 10 \u00b5m"]
-[13.609220504760742, 7.017551422119141, "[TT] Topology of the Power Subsystem = DET (Direct Energy Transfer)"]
-[9.264348030090332, 1.8831135034561157, "[FF] Configuration of the HTA Structure = Harpoon mounted at the top and the deployable boom at the bottom"]
-[8.784377098083496, 3.498661756515503, "[FF] Purpose of the GRIDS = Measure the distribution, motion, and velocity of ions"]
-[5.405767917633057, 1.6052976846694946, "[FF] Ground Segment Design Presentation Date of the EnMAP = 7 March 2013"]
-[8.527690887451172, 1.3474019765853882, "[TT] Measurement of the Aquarius = Changes in salinity"]
-[4.709007740020752, 0.536004364490509, "[TT] Launch Date of the SARAL = 25 Feb 2013"]
-[6.810210227966309, 5.107472896575928, "[FF] Components of the AM = Communications, power, thermal, ADCS (Attitude Determination and Control Subsystem), C&DH (Command and Data Handling)"]
-[8.65327262878418, 3.2033772468566895, "[FF] Objective of the LAICE = Investigate the gravity wave-driven coupling between the terrestrial atmosphere and the lower thermosphere/ ionosphere"]
-[8.176637649536133, 1.1839182376861572, "[TT] Soil Moisture Accuracy of the SMAP = 0.04 cm3/cm3"]
-[7.710571765899658, 5.179508209228516, "[FF] Unknown of the Millimeter Wave Atmospheric Sounder (MAS) = Unknown"]
-[11.986498832702637, -0.3388407528400421, "[TT] Management of the TESS = NASA's Goddard Space Flight Center"]
-[10.11654281616211, 6.453611850738525, "[FF] Bathymetry Analysis of the MABEL = Analysis of MABEL Bathymetry in Keweenaw Bay"]
-[6.502797603607178, 5.2422661781311035, "[FF] Components of the C&DH Subsystem = Motherboard, Processor, RTOS software"]
-[4.785245895385742, -1.8458688259124756, "[TT] Orbit Entry Time of the Chang'e-5 = Around 21:45 UTC"]
-[7.344827175140381, 1.0849307775497437, "[TT] Design Life of the OceanSat-2 = 5 years"]
-[11.744497299194336, 4.775092124938965, "[TT] Diameter of the Science Canister = 0.97 m"]
-[6.457504749298096, 5.289046287536621, "[FF] Function of the FPGA/ADC Card = Samples the analog IF signals and performs the IF signal processing"]
-[5.917501926422119, 1.1842647790908813, "[TT] Refit Date of the ERNO-Box = July 2009"]
-[9.17248821258545, 7.292929649353027, "[TT] Image Resolution of the WMC = 16 m"]
-[11.458251953125, 4.461101055145264, "[TT] Size of the MEOLUT Next = Less than six square meters"]
-[7.866119384765625, 5.080863952636719, "[FF] Vibration Testing of the Calibration Unit = Passed"]
-[5.84319543838501, 0.1832660287618637, "[TT] Operation Period of the Nimbus-7 = 1978 until 1994"]
-[10.209600448608398, 5.392543792724609, "[TT] Issue of the ABI = Cooling system malfunction"]
-[10.306474685668945, 5.190761566162109, "[FF] Function of the Resistojets = The gas is forced to spiral down the resistojet to increase the travel path and thus the heat transfer"]
-[5.563775062561035, -1.9218205213546753, "[TT] Operation Status of the KOMPSAT-3 = Nominal"]
-[5.664050579071045, 0.31137803196907043, "[TT] Possible Mission Extension of the SELENE/Kaguya = Half a year"]
-[5.4629130363464355, 7.698513984680176, "[TT] EIRP of the LET = > 78 dBW"]
-[9.734109878540039, 8.17679500579834, "[TT] Field of View of the ART-XC = ~30 arcmin"]
-[5.55033016204834, 0.37756696343421936, "[TT] Operation Start Date of the Cluster = 2009"]
-[8.030733108520508, 6.150693416595459, "[TT] Sensor Type of the ECOSTRESS = Radiometer"]
-[11.275857925415039, 5.871891498565674, "[TT] Material of the Pin-Puller = 17-4 PH H900 stainless steel"]
-[4.715516567230225, 0.7442725896835327, "[TT] Launch Date of the Hinode = Sept. 23, 2006"]
-[6.3498711585998535, -0.06039903312921524, "[TT] Processing Frequency of the International Bureau of Weights and Measures = Monthly"]
-[6.271045207977295, 4.423397541046143, "[FF] Data Interface and Control Design of the SWEM = Derived from the MAVEN DCB"]
-[7.506949424743652, 3.444842576980591, "[FF] Description of the Level-0 (L0) = Raw image (image with compression and cryptographic analysis)"]
-[5.574391841888428, 2.8507301807403564, "[TT] Sponsor of the AeroCube-7 = NASA"]
-[10.307401657104492, 5.616790294647217, "[TT] Thermal Operational Range of the Instrument = 0 / +20\u00baC"]
-[5.001808166503906, 8.168551445007324, "[TT] Frequency Range of the AMSR3 = 6.925 GHz to 183.3 GHz"]
-[7.468978404998779, 7.886140823364258, "[TT] LO Leakage and Image Suppression of the IQ Mixers = Approximately -20 dB"]
-[9.764612197875977, -0.639392614364624, "[TT] Orbit Altitude of the GEOSAR = 36,786 km"]
-[14.30614185333252, 3.1291027069091797, "[TT] Mass of the KGI-4C = 12 kg"]
-[14.275915145874023, 3.214489698410034, "[TT] Mass of the S/C = 86 kg"]
-[10.275646209716797, 4.047455787658691, "[FF] Placement of the Visual Markers = On the booms, blanket, and tip mandrel"]
-[10.43777084350586, 7.2404584884643555, "[TT] Mesoscale Sector Area of the Instrument = 1000 km x 1000 km"]
-[3.694101333618164, 3.8461203575134277, "[FF] User Interaction Meeting Date of the RISAT-1 = Feb. 16-17, 2012"]
-[9.27772331237793, 7.199065208435059, "[FF] Spatial Resolution of the SWIR FPA = Unknown"]
-[6.1524810791015625, 6.425195217132568, "[TT] Latency of the PIRATA = 1 day"]
-[5.475357532501221, 0.5742087364196777, "[TT] Observation Location of the ENVISAT satellite = Luzon Strait"]
-[13.836566925048828, 7.255329608917236, "[TT] Frequency of the Pulsed Diode Driver = 10 kHz"]
-[4.352487087249756, 7.113787651062012, "[TT] Radio Transmitter Type of the EDRS-A = Ka-band"]
-[8.853263854980469, 4.428673267364502, "[TT] Field of View of the ISIS = Within 10\u00ba of the Sun-Probe line"]
-[10.1309814453125, 7.276001930236816, "[TT] Field of Regard of the Resurs-P1 = 950 km"]
-[4.1767659187316895, 5.737456321716309, "[TT] Plane Positions Collected of the ADS-B receiver = Thousands per day"]
-[6.860548973083496, 1.037731409072876, "[FF] Installation Date of the Solar Array = 16 June 2021"]
-[4.7547502517700195, 1.2881900072097778, "[TT] Development Date of the Embedded Systems = 2010"]
-[6.6070556640625, 4.625678062438965, "[FF] Phase of the ELSA-d = AIT (Assembly, Integration and Test)"]
-[7.095587253570557, 2.812171459197998, "[FF] Focus of the RECCAP-2 = Global stocktake and tracking towards net zero emissions"]
-[6.725064277648926, 1.7090085744857788, "[FF] URL of the MAHRSI Experiment = http://www.crista.uni-wuppertal.de/campaigns/handbook/hb-iii.html"]
-[9.417182922363281, 6.048828601837158, "[TT] Canting Angle of the SAWs = -60\u00ba / 0\u00ba"]
-[3.9969735145568848, 4.421965599060059, "[FF] Product Description of the RADARSAT-2 = Unknown"]
-[13.75570011138916, 3.7345943450927734, "[TT] Instrument Mass of the Altimeter Antenna = 230 kg"]
-[8.152778625488281, 8.234210014343262, "[TT] Spectral Range of the PIC = 0.5 - 0.9 \u00b5m"]
-[6.15781307220459, 2.0090692043304443, "[FF] N/A of the http://www.russianspaceweb.com/spektr_rg.html = N/A"]
-[6.359846115112305, 1.3999457359313965, "[FF] Presentation Date of the Canadian Astro-H Metrology System = July 24, 2014"]
-[9.674566268920898, -0.25836923718452454, "[TT] Altitude at Autonomous Landing of the Hayabusa-2 = About 500 m"]
-[9.324012756347656, 5.8638811111450195, "[TT] Spring Function of the Shutter = Closes the shutter when unpowered"]
-[13.430150985717773, 6.818187236785889, "[TT] Spacecraft power of the GOSAT-2 = 5.0 kW"]
-[6.426832675933838, 3.6861512660980225, "[FF] Data Usage of the Satellite = Critical role in the resiliency mindset"]
-[6.135237216949463, -0.08772674202919006, "[TT] Calibration/Validation Period of the SSMIS = 18 months"]
-[9.654430389404297, 2.4088430404663086, "[FF] Parameter of the NuSTAR = Value"]
-[5.588266372680664, 4.723092555999756, "[FF] Avionics Architecture of the CHEOPS = OBC, RIU, two redundant 1553 buses"]
-[6.449206352233887, 1.712766408920288, "[FF] On-ground and In-orbit Calibration Presentation of the Microscope = 2010"]
-[11.71461009979248, 3.2904813289642334, "[TT] Thrust Level of the NanoPS = 50-100 mN"]
-[14.175667762756348, 3.1829023361206055, "[TT] Total Mass of the HREP = 381 kg"]
-[8.167413711547852, -0.19473107159137726, "[TT] Period (min) of the Meteor-1-2 = 97.7"]
-[8.68783187866211, 7.655869960784912, "[TT] Detector Size of the Imagers = 1280 x 1024 pixels"]
-[4.920025825500488, 1.9559533596038818, "[FF] URL of the TanSat = http://www.sasmac.cn/AP-GEOSS8/PDFversion/DAY2/WG6/2.1-TanSat-GEOSS.YiLiu1.pdf"]
-[5.3517866134643555, 6.6509222984313965, "[TT] On-board Data Recording Capacity of the RF Communications = 64 Gbit"]
-[9.932266235351562, 9.002862930297852, "[TT] Effective FOV of the Channel 2 = 52 km x 16 km"]
-[4.582642078399658, 0.9663541913032532, "[TT] Planned Launch Date of the SAOCOM-2B = 2026"]
-[5.2109503746032715, 4.912548542022705, "[TT] Instruments of the MOMS = GPS receiver"]
-[6.548756122589111, 1.0500290393829346, "[TT] Arrival in Mercury orbit of the BepiColombo = 2025"]
-[9.834197998046875, 4.800522804260254, "[TT] Stabilized Spin Rate of the SMAP spacecraft = 5 rpm"]
-[11.432083129882812, 4.45996618270874, "[FF] Cargo of the NG-10 Cygnus = Tissue on a chip and protein crystal growth"]
-[9.687017440795898, 3.9862465858459473, "[TT] Sampling Rate of the Vector Magnetometer = 100 vector samples/s in burst mode over polar latitudes"]
-[7.000091075897217, 2.9746346473693848, "[FF] Cost of the MethaneSAT = $26 million"]
-[4.48919153213501, 6.673046112060547, "[TT] Communication of the Schiaparelli = UHF link with the ExoMars Orbiter (with 2 antennas)"]
-[9.698259353637695, 8.393777847290039, "[TT] FOV of the CIRiS = 12.2\u00ba x 9.2\u00ba"]
-[8.02763843536377, 1.103352665901184, "[TT] Volumetric Soil Moisture Products Spatial Resolution (Global Scale) of the ROSE-L SAR = 50 m2"]
-[9.14694881439209, 3.5279712677001953, "[FF] Composition of the Sun = Unknown"]
-[6.426551818847656, 5.450379371643066, "[FF] Communication Test of the ArgoMoon = Optical communication capabilities between the CubeSat and Earth"]
-[5.681522369384766, 4.824792385101318, "[TT] Data Relay of the EDRS GEO satellite = Ka-band link"]
-[5.885330677032471, 2.806777238845825, "[TT] First Meeting Date of the Enhanced Marine Order Coordination (EMOC) = December 8, 2010"]
-[5.466095447540283, 5.577073097229004, "[FF] Data Format of the Modem Processor = CCSDS AOS (Advanced Orbiting Systems) Transfer Frames"]
-[6.08134126663208, 2.826098918914795, "[TT] Rendezvous Target of the OSMA-1 = Landsat-7 spacecraft"]
-[8.409626960754395, 4.653165340423584, "[FF] Integrated Components of the ADCS = Star trackers, IMU, and RWAs"]
-[4.513829231262207, -0.8751210570335388, "[TT] Launch Vehicle of the RemoveDebris spacecraft = Dragon capsule on board the SpaceX CRS-14 resupply mission"]
-[5.348205089569092, 7.199269771575928, "[TT] Ranging Margin of the CXS-810C = 8.1 dB"]
-[5.864916801452637, 5.580819606781006, "[FF] Technology of the GEC Plessey MIL-STD-1750 compatible processor = Radiation tolerant SOS technology"]
-[10.220746994018555, 7.988816738128662, "[TT] Optics of the Imager = TMA telescope with an aperture diameter of 1.1 m, focal length = 13.3 m, f/12"]
-[8.372710227966309, 1.5259850025177002, "[TT] Temporal Sampling of the Sea Surface Salinity (SSS) = Monthly"]
-[7.181746959686279, 0.12689726054668427, "[TT] Age of the Magma Ocean Planets = Less than 100 million years old"]
-[10.325547218322754, 7.435877323150635, "[TT] Mirrors of the Telescope = Conics with a fourth-order aspherical term"]
-[12.128754615783691, 2.997783899307251, "[TT] Type of the Propulsion system = Blowdown monopropellant (hydrazine) with helium pressurant"]
-[9.695956230163574, 4.132149696350098, "[TT] Number of Instruments of the Magnetometer (MAG) = 1"]
-[9.39193344116211, 6.796334266662598, "[TT] Imaging Satellite of the KazEOSat-2 = Medium resolution"]
-[3.44958758354187, -0.9072635173797607, "[TT] Orbit Type of the GEISAT Precursor = Sun-synchronous"]
-[10.23269271850586, -1.3323832750320435, "[TT] Orbit Inclination of the ALBus CubeSat = 85\u00ba"]
-[5.744482040405273, 1.1134874820709229, "[FF] Presentation Date of the ROSA = Dec. 5-7, 2012"]
-[7.381728172302246, 3.73459792137146, "[FF] Coverage Improvement of the MetOp-SG Radio Occultation = Up to three times"]
-[8.941625595092773, 6.080587387084961, "[TT] Scan Mechanism Rate of the Antenna Subsystem = 20.5 rpm"]
-[7.68795919418335, -2.5420033931732178, "[TT] Cadence of the GOLD = ~30 min"]
-[9.997246742248535, -1.4974342584609985, "[TT] Orbit Inclination of the CHORUS = 53.5\u00b0"]
-[5.404379844665527, 6.4656243324279785, "[TT] Data Generation of the MicroCarb = 500 Gbit/day"]
-[4.397116661071777, 7.918254375457764, "[TT] Downlink Center Frequency of the DRT = 4506.05 MHz"]
-[5.417999267578125, 6.589163303375244, "[TT] Daily Capacity of the CLASS data storage per satellite = 1.9 TB"]
-[4.892234802246094, 0.3472806513309479, "[TT] Launch Date of the CXBN = 13 September 2012"]
-[6.0674004554748535, 2.6194372177124023, "[FF] Team of the NuSTAR = Caltech, Columbia University, DTU (Danish Technical University), LLNL (Lawrence Livermore National Laboratory),NASA/GSFC (Goddard Space Flight Center), and UCB (University of California, Berkeley)"]
-[6.752190589904785, -0.5654531717300415, "[TT] Orbit Repeat Cycle of the MSU-SK = 21 days"]
-[6.80893087387085, -0.6500752568244934, "[TT] Orbit Duration of the QARMAN = Around four months"]
-[9.958701133728027, 9.021913528442383, "[TT] Effective FOV of the Channel 4 = 35 km x 76 km"]
-[8.207877159118652, 7.22028923034668, "[TT] Sensor Type of the LPT = Light Particle"]
-[8.346678733825684, 3.2192981243133545, "[TT] Application of the FTS = Ozone sounding"]
-[4.819027900695801, 4.432416915893555, "[FF] Channel Coding of the Argos-3 = Unknown"]
-[6.8516316413879395, 7.7380146980285645, "[TT] Reflector Dimension of the Antenna System = 65 cm"]
-[10.755826950073242, 7.367018222808838, "[TT] Beam Dimensions of the POLDER = 1440 km x 2200 km"]
-[7.885651588439941, 3.3250892162323, "[FF] Function of the GOE = Performs refractive radio occultation measurements of the Earth's atmosphere and monitors the auroral activity"]
-[8.645577430725098, 5.647681713104248, "[TT] Fast-delivery position knowledge of the POD software = \u00b1 60 m (3\u03c3 in each axis)"]
-[5.7279462814331055, 3.69673228263855, "[TT] Support of the Test Station = Ops testing and training support"]
-[13.388907432556152, 5.5620222091674805, "[FF] Solar Panels of the LF spacecraft = Four"]
-[8.307031631469727, -0.8237643837928772, "[TT] Resolution of Winter and Summer Ice-Sheet Elevation Change of the ATLAS = 0.1 m"]
-[7.088190078735352, 7.732083797454834, "[TT] Corner Cube Reflectors of the EGS = 1436"]
-[5.705482006072998, 7.169319152832031, "[TT] Data Rate of the TOMS = 700 bit/s"]
-[4.998969554901123, 2.0172641277313232, "[TT] Mission Status of the GOSAT = Operational (extended)"]
-[7.7267632484436035, 9.496342658996582, "[TT] Center Wavelength of the B8 = 842 nm"]
-[10.733884811401367, -0.18131397664546967, "[TT] Helix-Formation Distance of the TanDEM-X = Less than 1 km"]
-[7.249448776245117, 7.798916339874268, "[TT] High/Low gain ratio of the PHA = 68 or 40"]
-[9.397668838500977, -1.7084249258041382, "[TT] Orbital Altitude of the Swarm-C (Charlie) = \u2264 530 km"]
-[4.650956153869629, -0.7072727680206299, "[TT] Docking Time of the Crew Dragon = Around a day later"]
-[13.383893013000488, 5.516611099243164, "[TT] Number of Panels of the Solar Array = 6"]
-[10.334660530090332, 5.3230719566345215, "[FF] Component of the Electrical cables and components of the Thermal Control System (TCS) = Unknown"]
-[8.389982223510742, 7.215501308441162, "[TT] Power Source of the Cameras = Ancillary Electronics Units (AEUs)"]
-[14.051980018615723, 3.035809278488159, "[TT] Weight of the SPOT-2 = 1800 kg"]
-[4.989861965179443, 1.0632197856903076, "[TT] Deployment Date of the Gravity Boom and VLF Antenna = Feb. 4, 2009"]
-[7.342784404754639, 5.5456366539001465, "[FF] Components of the LCS = Laser transmitter, optical unit, pointing control mechanism, laser receiver"]
-[8.721193313598633, 4.919731140136719, "[TT] Field of View of the Star Tracker = 2\u00ba x 2\u00ba"]
-[10.933928489685059, 2.0789215564727783, "[TT] Observation Date of the XMM-Newton = 2016"]
-[3.649965286254883, 5.4275994300842285, "[TT] Resolution of the Spotlight-2A = 0.8m"]
-[13.879150390625, 3.0896377563476562, "[TT] Mass of the CubeL = 3.4 kg"]
-[7.7552618980407715, 4.9558281898498535, "[FF] Data Accuracy of the AMS = Unprecedented"]
-[5.655691146850586, 5.692301273345947, "[TT] Type of the ARM M0+ processing unit = ARM M0+"]
-[6.715154647827148, 2.1907646656036377, "[FF] URL of the Super Dual Auroral Radar Network = http://www.superdarn.ac.uk/archive/Chisham_et_al_2007.pdf"]
-[8.04088306427002, 7.99882698059082, "[FF] Camera Types of the Optical Payload = One in the VNIR (Visible Near Infrared) range and two imagers in the infrared region"]
-[9.763118743896484, 8.122607231140137, "[TT] Lens Focal Length of the Camera System = 16 mm"]
-[5.637929916381836, 4.376535415649414, "[FF] URL of the EDRS = http://www.esa.int/Applications/Telecommunications_Integrated_Applications"]
-[3.8668620586395264, 6.398496627807617, "[TT] Antenna Configuration of the ISL = Omnidirectional"]
-[6.811050891876221, 5.817079544067383, "[TT] Quantity of the MIRES = 2"]
-[8.120631217956543, 6.706908702850342, "[FF] Usage of the Ultrasound-2 = Vein scans"]
-[5.121834754943848, 7.371610164642334, "[TT] Data Rate Control of the Radio Subsystem = Manual and Automatic"]
-[4.771210670471191, 2.994349956512451, "[FF] Data Processing Center of the Satellite = POC (Payload Operations Center) located at NavOceano (Naval Oceanographic Office)"]
-[6.595666885375977, 2.324404001235962, "[TT] Exposures per Field of the Euclid Reference Survey = 4"]
-[13.61240291595459, 6.973708629608154, "[TT] Nominal power generation of the EPS = 2 W"]
-[7.056668281555176, 1.5376347303390503, "[FF] End of Life Date of the SporeSat = 4 Jun 2014"]
-[9.652094841003418, 7.172268867492676, "[TT] Spatial Resolution in Medium Resolution Mode of the OBRC instrument = 400-500 m"]
-[7.99984884262085, 5.199725151062012, "[FF] Purpose of the Longitudinal Calibration Model = Provide a correction to the FLLS data"]
-[5.1711812019348145, 1.2492797374725342, "[FF] Conference Date of the PROBA-3 = May 29-31, 2013"]
-[8.521063804626465, 7.702788829803467, "[FF] Sensor of the POLDER = Matrix CCD sensor (242 x 548 photoelements, the pixels are binned one by two, resulting in 242 x 274 sensitive areas)"]
-[4.169390678405762, 7.217693328857422, "[TT] Frequency Band of the MTB = X-band"]
-[9.293872833251953, 1.1607986688613892, "[TT] Estimated Start of the Oort Cloud = About 1,000 astronomical units (AU) from the Sun"]
-[6.006663799285889, 6.455549716949463, "[TT] Latency of the ATL04 Calibrated Backscatter Profiles = 21 days"]
-[8.930977821350098, 6.883247375488281, "[TT] Measurement Range of the FGM = \u00b164,000 nT"]
-[4.443418502807617, 4.21592378616333, "[TT] Number of Operating Satellites of the GEOSAR = 7"]
-[8.14602279663086, -1.0470986366271973, "[FF] Primary Design of the ICESat-2 = Polar ice elevation and tree canopy measurements"]
-[10.812738418579102, 2.7800557613372803, "[FF] ACS Development of the Chibis-M Microsatellite = Unknown"]
-[9.893445014953613, 6.392629623413086, "[TT] Slewing Angle of the Mirror = 9\u00ba"]
-[14.07629680633545, 2.9401557445526123, "[TT] Mass of the Genesis-2 = 1360 kg"]
-[6.375205039978027, 5.150447845458984, "[FF] Function of the FPGA = Integrated interfaces and instrument control/monitoring functions"]
-[4.680356979370117, 6.242667198181152, "[FF] Data Uplink Bands of the SDR (Software Defined Radio) = USB (Universal S-Band) and SGLS (Space Ground Link System, L-band)"]
-[5.008423328399658, 4.344264984130859, "[TT] License Status of the Starlink = Not Obtained"]
-[8.575377464294434, 7.725049018859863, "[TT] Detector Array Pixel Count of the Radiometer = 8 x 192 pixels"]
-[5.6052327156066895, 3.7106523513793945, "[FF] Members of the Providers Forum = China (CNSS), EU (Galileo, EGNOS), India (IRNSS, GAGAN), Japan (QZSS, MSAS), Russia (GLONASS), and USA (GPS, WAAS)"]
-[4.795498371124268, -1.8637698888778687, "[TT] Number of Lunar Days of the Chang'e-3 = 28"]
-[8.74216365814209, 8.81163501739502, "[TT] Volatiles of the Grating Spectrometer = Less than 0.1% volatile internals by mass"]
-[4.66988468170166, 0.1773052215576172, "[TT] Launch Date of the IDEA-OSG 1 = 28 Nov. 2017"]
-[1.3651645183563232, 2.783648729324341, "[TT] Principal Absorbing Constituents of the Band 1 = CO2"]
-[6.51895809173584, 6.285579681396484, "[FF] Performance Check Modes of the ARC = Receiver mode, Transmitter mode, Transponder mode with delay"]
-[11.567869186401367, 4.785057067871094, "[TT] Imprint Size of the Philae = 25 cm"]
-[13.408182144165039, 5.494093894958496, "[TT] Quantity of the Solar Panels = 2"]
-[10.840789794921875, 7.372312068939209, "[TT] Swath Coverage of the Corvus-HD satellites = 25 km"]
-[8.866764068603516, 5.855750560760498, "[TT] Nadir-pointing face of the PSSCT-2 = +Z face"]
-[6.798801898956299, 1.7697871923446655, "[FF] URL of the Solar Orbiter/METIS = http://congrex.nl/icso/2012/papers/FP_ICSO-089.pdf"]
-[4.873842239379883, 0.07038122415542603, "[FF] Launch Date of the SpaceX CRS-6 = April 7, 2015"]
-[3.196658134460449, 1.7146459817886353, "[TT] Data Production of the Sentinel-1, -2, and -3 = Approximately 4 TByte per day"]
-[9.664617538452148, 4.144740104675293, "[TT] Magnetic Cleanliness Requirement of the Magnetometers = Sub nT-range for VFM and ASM"]
-[9.864714622497559, -0.355623722076416, "[TT] Altitude of the Satellite = 514 km"]
-[5.377631664276123, 3.8468334674835205, "[TT] Number of Satellites of the Meteosat First Generation = 7"]
-[7.116764545440674, 4.55537748336792, "[FF] Functions of the FF-N = Collision risk detection, metrology data validity assessment, self-assessment of estimated position and velocity covariance, state estimation validity, navigation using alternative metrology, relative attitude computation, ancillary absolute orbit processing"]
-[8.28841781616211, 5.361254692077637, "[TT] Calibration of the PMI = On-board two-point"]
-[5.794245719909668, 4.866670608520508, "[TT] Function of the Development Flight Instrumentation (DFI) = Capture test results"]
-[5.325237274169922, 4.176523208618164, "[TT] Bus of the Suomi-NPP = Ball Commercial Platform 2000 (BCP 2000)"]
-[5.1172194480896, 1.469105839729309, "[TT] Mission Status of the UniSat-3 = Operational in 2010"]
-[6.338695526123047, 3.1448543071746826, "[FF] Data Collection Purpose of the ATOVS = Support regional NWP over Europe"]
-[7.070225715637207, 7.752092361450195, "[TT] Reflector Illumination of the Biomass = 3 x 2 array of cavity-backed circular microstrip radiators"]
-[8.658587455749512, 3.837402820587158, "[TT] Number of Instruments of the Solar Orbiter = 10"]
-[9.274299621582031, 0.9993005990982056, "[TT] Jupiter's Day of the Juno = About 10 hours"]
-[5.928374290466309, 4.791982650756836, "[FF] Type of the SNAPPING service = On-demand processing"]
-[7.531484127044678, 8.98717975616455, "[TT] Pass Band Wavelengths of the OTA = 500 nm to 900 nm"]
-[7.589721202850342, 8.509939193725586, "[TT] Number of Bands of the NIR = 80"]
-[9.898941993713379, 8.190225601196289, "[TT] Focal Length of the POLDER = 3.57 mm"]
-[10.436932563781738, 0.5700270533561707, "[TT] Orbital Separation of the Sapphire and NEOSSat = Approximately 4700 km"]
-[6.364586353302002, 0.14073319733142853, "[FF] EREP Investigations of the Skylab = Unknown"]
-[5.214922904968262, 0.5620891451835632, "[TT] Contract Date of the AERO-VISTA mission = May 7, 2020"]
-[8.988842010498047, 8.235461235046387, "[FF] URL of the Spaceborne Frequency Comb Metrology = https://www.osapublishing.org/DirectPDFAccess/DBE99771-B99B-C7D3-BC1981AC3BB40F6B-354726/optica-3-12-1381.pdf?da=1&id=354726-&seq=0&mobile=no"]
-[8.486422538757324, 8.219803810119629, "[TT] Spectral Resolution of the Instrument = 1.25 cm -1"]
-[8.11459732055664, 3.7762279510498047, "[FF] Modification of the OCO-2 Instrument = Implemented"]
-[3.1957974433898926, 2.2121620178222656, "[FF] Role of the Copernicus Sentinel-6 Michael Freilich = Radar altimetry reference mission"]
-[5.306008338928223, 0.8374967575073242, "[FF] Date of the MDR = July 2012"]
-[7.66839599609375, 7.182013034820557, "[TT] Cadence of the LET-Spectra = In the range 0.1-430 keV/\u00b5m"]
-[4.60413932800293, 4.823312759399414, "[FF] Signal Collection of the AIS (Automated Identification System) = Successful from space over extensive areas of open water"]
-[10.338125228881836, 5.688477993011475, "[FF] Temperature of the Japan Current = High"]
-[9.767504692077637, 8.4190092086792, "[FF] Length of the DSX = Nearly the length of a football field"]
-[8.917646408081055, 6.068398952484131, "[TT] Performance of the CSS = \u00b10.115\u00ba"]
-[13.880935668945312, 3.8369572162628174, "[TT] Mass of the Sensor Complement = ~35 kg"]
-[10.929545402526855, 7.52451229095459, "[TT] Swath Width of the OLI-2 = 185 km"]
-[5.574158668518066, -0.35230129957199097, "[TT] Design Lifetime of the RapidEye = 7.25 years"]
-[6.1040568351745605, 8.591202735900879, "[TT] Polarization of the Antenna = H and V"]
-[5.314098358154297, 4.113888740539551, "[TT] Bus Type of the NorSat-1 = Next-generation satellite bus"]
-[9.687772750854492, 6.9951171875, "[TT] Spatial Resolution of the LEND = 5 km"]
-[5.247892379760742, 0.250803679227829, "[TT] Announcement Date of the TSX-5 = July 11, 2000"]
-[11.205183029174805, 5.830591201782227, "[TT] Materials of the FSU = Molybdenum TZM"]
-[8.168285369873047, 5.838250160217285, "[TT] Precision of the S-193 = Better than 5%"]
-[5.285743713378906, 0.12413980811834335, "[TT] Radiometric Stability of the Ikonos-2 = < 1% degradation per year"]
-[8.787703514099121, 3.8129818439483643, "[TT] Type of the EDI = Electron Drift Instrument"]
-[5.509322166442871, 5.252127647399902, "[TT] Control Interface of the Yaesu G-5500 rotators = Yaesu GS-232"]
-[5.956629753112793, -0.6722043752670288, "[TT] Operation Duration of the \u00d8rsted spacecraft = 15 years"]
-[4.622254848480225, 4.272177696228027, "[FF] Ground Segment Software of the GeoSat-2 = gs4EO"]
-[8.250537872314453, 4.474922180175781, "[FF] Purpose of the LARES-2 = Test alternative theories of gravitation versus General Relativity"]
-[6.917665481567383, 6.1172099113464355, "[TT] 2nd LO of the HRIT HiRID = 1558"]
-[13.416349411010742, 7.451842308044434, "[TT] Peak Power of the TR Module = 10 W"]
-[5.1724677085876465, 2.721613883972168, "[FF] Affiliation of the UiTMSAT-1 = Malaysia"]
-[8.628364562988281, 5.560593605041504, "[TT] Achieved Accuracy of the Satellite Position = 2.8 cm"]
-[3.7780678272247314, -0.5828285217285156, "[FF] Orbit of the EO Satellite = LEO"]
-[3.3527207374572754, 4.697131156921387, "[FF] SAR of the SeaSat = SeaSat Sees the Winds with SAR"]
-[8.868958473205566, 5.883146286010742, "[TT] MNO Pointing Performance of the AlSat-2A = 500 \u00b5rad"]
-[6.361475467681885, 4.818877220153809, "[FF] Software Architecture of the AOCS = Object-oriented and modular with a static architecture"]
-[8.495767593383789, 9.385003089904785, "[TT] Uncertainty of the Responsivity Measurement = <0.1%"]
-[7.858198642730713, 5.862675666809082, "[FF] Dispersed Images of the HETG = Form a shallow X centered at the undispersed (zeroth order) position"]
-[8.145708084106445, 6.493704319000244, "[TT] Image Capture Location of the Advanced Baseline Imager (ABI) = Chile and Argentina"]
-[4.358310222625732, 5.324113368988037, "[TT] Frequency of the COSPAS-SARSAT beacons = 406.025 mHz"]
-[8.04936695098877, 1.6945993900299072, "[FF] Measurement of the SKIM = Ocean-surface currents"]
-[3.8138961791992188, 1.1883748769760132, "[TT] Fairing Reuse of the Falcon 9 = Half of which flew on two previous missions"]
-[8.53062629699707, 1.420135498046875, "[TT] Measurement of the Aquarius = Temperature and humidity profile of the troposphere and the stratosphere"]
-[10.290289878845215, 4.548554420471191, "[TT] Torque of the Reaction wheels = 10 Nms/0.1 Nm"]
-[8.753279685974121, 5.330201148986816, "[TT] Proof-mass Positioning Error of the Three-axis diagonal gradiometer = 6 x 10 -8  m Hz -1/2"]
-[9.075398445129395, 0.48128366470336914, "[FF] Earth-Orbit Phase Goals of the ARTEMIS = Raise apogee of both spacecraft through a series of ORMs to near lunar altitudes and to target the lunar gravity assists needed to transition into the Trans-Lunar trajectories"]
-[6.381128311157227, 5.99069881439209, "[TT] Quantity of the Two power control units = 2"]
-[3.1761014461517334, 2.216282606124878, "[FF] Provider of Earth observation data of the Copernicus = Yes"]
-[11.22533893585205, 4.715285301208496, "[TT] Debye Length of the TPS = 0.2 to 1 cm"]
-[14.032172203063965, 3.1252081394195557, "[TT] Total IPS Mass of the STP-2 = 3700 kg"]
-[7.60707950592041, 2.0635650157928467, "[FF] Impact of the Argo = Provided data for climate projections"]
-[3.473215341567993, 6.394623756408691, "[TT] Size of the Antennas = 0.9 m and 1.0 m"]
-[5.29085636138916, 7.1785688400268555, "[TT] Data Download of the CanX-2 = Over 370 MB of science data and engineering telemetry"]
-[5.324380874633789, 0.4348594844341278, "[TT] Operational Date of the SSM/I = July 1987"]
-[7.640844821929932, 5.4111528396606445, "[TT] Purpose of the Vision-based Sensor System = Allow one satellite to lock onto the other"]
-[10.024445533752441, -1.5209980010986328, "[TT] Inclination of the Solar Orbiter = Increasing to a minimum of 30\u00ba"]
-[3.8533895015716553, 0.9289610981941223, "[FF] Flight of the PSLV-C16 = Successful"]
-[7.880679607391357, 3.0354127883911133, "[TT] Instruments of the TanSat = Carbon Dioxide Spectrometer and CAPI"]
-[7.742404460906982, -0.5694458484649658, "[FF] Assessment Presentation of the BepiColombo MMO spacecraft = 44th ICES ( International Conference on Environmental Systems), Tucson, Arizona, 13-17 July 2014"]
-[4.903679847717285, 1.8983265161514282, "[TT] Mission Status of the SkySat Constellation = Operational (nominal)"]
-[8.06891918182373, -0.1995285302400589, "[FF] Behavior of the Polar Bear = Struggling to complete essential tasks because of declining concentrations of Arctic sea ice"]
-[7.01022481918335, 5.438879013061523, "[FF] Components of the Receiver = Low noise preamplifier with BFS17, LNA (Low Noise Amplifier), first mixer NE602, crystal filter, intermediate frequency amplifier A281D, last mixer NE602"]
-[14.657676696777344, 6.6689252853393555, "[TT] NiCd Batteries of the EURECA = 4 NiCd batteries"]
-[8.720901489257812, 2.126049280166626, "[TT] Wind Direction Blur of the LG-mod = 180\u00b0"]
-[6.061334133148193, -0.24150851368904114, "[TT] Extended Science Mission Duration of the LRO = 9/17/2012 - 9/16/2014"]
-[7.946783065795898, -0.5745142698287964, "[FF] Orbit Determination of the CryoSat-2 = Real-time orbit determination for spacecraft attitude and orbit control (on-board)"]
-[10.712437629699707, 3.7542335987091064, "[FF] Applications of the Drag-Free Technology = Navigation, Earth science, fundamental physics, and astrophysics"]
-[5.121104717254639, 0.45546531677246094, "[TT] Launch Date of the Light-1 = December 21, 2021"]
-[9.52341365814209, 0.3304673433303833, "[FF] Route of the A-68A = Across the Drake Passage"]
-[5.597414493560791, 4.330397129058838, "[TT] Number of Ranging Stations of the LAGEOS = 183"]
-[8.223432540893555, 2.437987804412842, "[FF] Function of the Radiometer = Furnished cloud-height profiles"]
-[3.569516897201538, 5.401736736297607, "[TT] Spotlight High resolution of the Resolution = 3 m"]
-[7.823528289794922, 8.712183952331543, "[TT] Model of the Piezo Stage = Modified version of the off-the-shelf P-733.2CD"]
-[7.460235118865967, 4.574650764465332, "[FF] Unknown of the Silicon Tracker = Unknown"]
-[11.62069034576416, 4.0565924644470215, "[TT] Size of the AeroCube-8B = 1.5U"]
-[7.537816524505615, 6.3757429122924805, "[TT] TGF Events of the XGRE = 1 \u00b5s relative time accuracy"]
-[8.301528930664062, 3.7818164825439453, "[FF] Operation of the MERIS = Only out of eclipse"]
-[4.823136806488037, 0.8619912266731262, "[TT] CDR Date of the TROPOMI = End of 2012, early 2013"]
-[5.797152519226074, -0.8182100057601929, "[TT] Design Life of the Spacecraft bus = 5 years"]
-[7.9264373779296875, -0.986778199672699, "[TT] Instrument of the ICESat-2 = Operation IceBridge"]
-[8.82858943939209, 5.715508460998535, "[TT] Capability of the 0.04\u00ba (3\u03c3) = 0.04\u00ba (3\u03c3)"]
-[3.3396427631378174, 1.7790859937667847, "[FF] Announcement Year of the European Sentinel Satellites = 2020"]
-[5.714105129241943, 6.205513954162598, "[FF] Realtime Storage of the Telemetry = Managed during the descent phase"]
-[9.298375129699707, 3.508762836456299, "[FF] Data Collection of the Magnetometer = Solar wind and magnetic field around Mercury"]
-[6.258895397186279, 6.366105556488037, "[TT] Max #/s in LOLA window of the NGSLR = 28"]
-[10.59033203125, 1.0514216423034668, "[FF] Confirmation of the Hot Jupiters = Across the galaxy and even in our stellar neighborhood"]
-[4.816958904266357, -0.11679135262966156, "[TT] Launch Time of the IDEA-OSG 1 = 05:41 UTC"]
-[5.42437744140625, 6.076914310455322, "[TT] Memory Type of the Second FPGA = SRAM"]
-[4.395650863647461, 3.127141237258911, "[FF] PIs of the SOVA = D. Crommelynck, IRMB, Brussels, Belgium; C. Fr\u00f6hlich, PMOD/WRC Davos, Switzerland"]
-[9.104522705078125, -1.2438366413116455, "[TT] Orbit Type of the EDRS-C = Geostationary orbit"]
-[9.57518196105957, 9.209196090698242, "[TT] Launch Date of the Iris = 2nd September 2020"]
-[5.121011257171631, -0.899683952331543, "[TT] Reentry Date of the Kounotori-6 = February 5, 2017"]
-[6.656270980834961, 0.03473128005862236, "[TT] Years on Orbit of the Landsat-7 = 19 years"]
-[4.833547592163086, 0.2355431467294693, "[FF] Deployment Date of the RemoveDebris = 20 June 2018"]
-[6.501391410827637, 5.80875301361084, "[TT] PRN of the GSAT-0203 = 26"]
-[4.751095294952393, 6.843966007232666, "[FF] Downlink Transmission of the L-band telemetry subassembly = Image data"]
-[4.424588203430176, 5.4546308517456055, "[TT] Operational Within of the GomX-3 = 96 hours"]
-[9.812125205993652, -0.5294963121414185, "[TT] Altitude of the Low-Earth Orbiting Spacecraft = Below 1000 km"]
-[9.40758991241455, 4.361754417419434, "[TT] Separation Angle of the STEREO spacecraft = 90\u00ba"]
-[4.528390884399414, 7.961761951446533, "[TT] Frequency of the NRA = 13.6 GHz (Ku-band) and 5.3 GHz (C-band)"]
-[5.74069356918335, -0.2656918466091156, "[TT] Deployment Time of the Antenna System = Few seconds"]
-[5.650561809539795, 6.203883647918701, "[TT] Storage Media of the Data Storage = CompactFlash\u00ae card"]
-[10.157610893249512, -2.771568536758423, "[TT] Accessible unit (read/write) of the SLC NAND-FMM = 256 kbyte"]
-[7.447157859802246, 2.320847988128662, "[TT] Horizontal Domain of the Aeolus = Global coverage"]
-[7.874802112579346, 7.792862892150879, "[FF] Operation Mode of the NAOMI = TDI (Time Delay Integration) mode in the Pan band"]
-[11.247832298278809, 5.359559535980225, "[TT] Scintillator Dimensions of the Scatterer = 6.5 mm x 6.5 mm x 49 mm"]
-[9.535501480102539, 7.165037155151367, "[TT] Resolution of the ABI = 500m at nadir"]
-[10.906707763671875, 7.53688383102417, "[TT] Swath Width of the WPM = 60 km"]
-[4.721673488616943, 0.4488449692726135, "[TT] Launch Date of the CHAMP = July 15, 2000"]
-[4.486672878265381, 6.954376220703125, "[TT] Bandwidth of the Spacecraft Repeater = 25 kHz"]
-[4.94111442565918, 3.4479711055755615, "[TT] Manufacturer of the CHORUS = MDA Ltd. (MacDonald, Dettwiler and Associates Ltd.)"]
-[8.458683967590332, 7.699112415313721, "[TT] Line Array of the Pan CCD detector module = 24,000 pixels"]
-[9.617728233337402, 8.33022403717041, "[TT] Focal Length of the Short Wavelength Band = 12.5 cm (f/2.2)"]
-[5.416626930236816, 6.343035697937012, "[TT] Type of the Space Micro \u00b5STDN = Digitally intensive"]
-[4.777188301086426, -1.8513141870498657, "[TT] Resumed Work Days of the Chang'e-4 = 23 days"]
-[13.288211822509766, 7.220144748687744, "[TT] Modulator Grid of the FSU = High-voltage"]
-[7.707805156707764, 8.536173820495605, "[TT] Spectral Bands of the VIIRS = 22"]
-[4.95189094543457, 1.7482082843780518, "[TT] Operation Status of the AprizeSat-3 and AprizeSat-4 = Nominal"]
-[6.339685916900635, 2.0599851608276367, "[FF] Presentation of the IXV = Mission and Flight Mechanics of IXV from design to postflight"]
-[7.375626087188721, 8.627296447753906, "[TT] Bands of the SEM = 2 XRS bands, 5 EUV bands, 7 proton bands, 6 alpha particle bands, 3 electron bands"]
-[3.444283962249756, -0.9102796912193298, "[TT] Orbit Type of the TRACE spacecraft = Sun-synchronous polar orbit"]
-[5.380072593688965, 0.4529821276664734, "[FF] Launch Date of the NASA Space Station Cargo = April 18, 2017"]
-[5.7936482429504395, 4.769684791564941, "[FF] Navigation Message performance analysis and Signal In Space User Ranging Error (SISRE) characterization of the GIOVE-B = Unknown"]
-[7.771498203277588, 1.45681893825531, "[TT] Location of the Precipitation Processing System = GSFC"]
-[8.91849422454834, 2.9419047832489014, "[FF] Publication Date of the High Altitude Observatory white-light coronagraph = April 1977"]
-[14.05228328704834, 2.772862672805786, "[TT] Launch Mass of the AprizeSat-6 = 14 kg"]
-[9.106311798095703, 6.425622463226318, "[FF] Observation Geometry of the MIPAS = Limb"]
-[9.577044486999512, 2.3199660778045654, "[FF] Mission of the NuSTAR = Data Collection"]
-[9.172600746154785, 2.8657915592193604, "[FF] Interaction of the Coronal Mass Ejections = Interacting in the interplanetary space with another Coronal Mass Ejection"]
-[6.89035177230835, 7.774147033691406, "[TT] Reflector Dimension of the MTVZA-GY Antenna System = 65 cm"]
-[9.085359573364258, 5.230707168579102, "[TT] Maneuvers of the AlSat-2A = Reach \u00b130\u00ba either being in along-track or in cross-track"]
-[9.175747871398926, 4.008408069610596, "[FF] Function of the TRIAD navigation method = Compares the magnetometer and sun vectors using a model of Earth's magnetic field and an astronomical almanac for sun position comparisons"]
-[6.536291599273682, -0.8501471281051636, "[TT] LTAN of the Satellite Orbit = 6:00/18 hours"]
-[4.878201961517334, 0.5574310421943665, "[FF] Publication Year of the CRISTA-2 = 2002"]
-[13.760760307312012, 7.345276355743408, "[TT] Transmitter Voltage of the DSX = < 10 kV"]
-[7.682855129241943, 9.435989379882812, "[TT] Center Wavelength of the Band 10 = 7.34 \u00b5m"]
-[10.928281784057617, 3.4737772941589355, "[TT] Size of the 6U nanosatellite = 6U"]
-[3.413247585296631, -0.8965638875961304, "[TT] Orbit Type of the WorldView Legion = Mid-inclination and sun-synchronous"]
-[7.822624683380127, 2.7439169883728027, "[FF] Objectives of the HSC = Urban lights, electric storms, polar regions, snow cover"]
-[10.36631965637207, 2.7951300144195557, "[FF] Launch Date of the PISAT nanosatellite = July 2016"]
-[11.728833198547363, 0.12984713912010193, "[FF] Exoplanet Candidates of the TESS = 5000"]
-[7.1567230224609375, 1.9354089498519897, "[TT] Operational Status of the Carbonite-2 = Operational"]
-[10.691259384155273, 1.1624336242675781, "[TT] Size Comparison to Sun of the HD 93396 = Three times larger"]
-[8.01374626159668, 3.169567584991455, "[FF] Gases Measured of the FTS = CO2, CH4, carbon monoxide (CO), and other gases"]
-[7.884084224700928, 5.70528507232666, "[FF] Purpose of the Optical Bench = Achieve low thermal noise and high beam pointing stability"]
-[7.100079536437988, 2.4811947345733643, "[FF] Coverage of the ETC = Argentina, Chile, Bolivia, Paraguay, Uruguay, a large part of Peru and the south of Brazil"]
-[9.8344087600708, -0.36253756284713745, "[TT] Altitude of the Computer System = 90,000 feet"]
-[6.869139194488525, 7.010084629058838, "[TT] Number of Beams of the MBA System = 19"]
-[5.113261699676514, 0.6287539601325989, "[TT] Launch Date of the LADEE = September 7, 2013"]
-[11.77683162689209, 0.09560393542051315, "[TT] Mass of the TESS = Weighs between four and 19 Earth masses"]
-[7.662846565246582, -0.9111229777336121, "[TT] Instrument CDR Date of the ICESat-2 = January 17, 2014"]
-[8.069192886352539, 1.2842345237731934, "[FF] Function of the NAC = Highlights variations in soil moisture content and vegetation density"]
-[8.303818702697754, 8.073678970336914, "[TT] Translation Range of the Imager = \u00b150 \u00b5m in the two axes orthogonal to the optical axis"]
-[7.339147090911865, 6.539690017700195, "[TT] Integration Time of the Instrument = 12 s"]
-[6.348739147186279, -0.5445641279220581, "[TT] Nominal Mission Duration of the Vega Rideshare Mission = 1 hour, 44 minutes and 56 seconds"]
-[9.015827178955078, 8.108181953430176, "[TT] Number of MWIR/TIR Focal Planes of the GLI = 1"]
-[4.533189296722412, -0.14046834409236908, "[TT] Docking Date of the MEV-1 = 2019"]
-[9.050671577453613, 8.186760902404785, "[TT] IFOV/line (pixels/scan line) of the MWHS = 98"]
-[8.732864379882812, 1.9912846088409424, "[TT] Range of the Wind Speed Measurements = 3 up to 30 m/s"]
-[7.918445110321045, 3.1542961597442627, "[TT] Absorption at 1.63 \u00b5m of the Carbon Monoxide (CO) = 10 -22 mol cm -2"]
-[6.916228294372559, -0.7474590539932251, "[TT] Orbit Period of the WD 1856 b = Every day and a half"]
-[8.519476890563965, 7.500517845153809, "[TT] Detector Telescope Head of the DOSTEL = Two PIPS detectors and one PIN diode"]
-[7.015008926391602, 2.317120313644409, "[FF] Science and Mission Overview of the STEREO =  URL: http://www.jhuapl.edu/techdigest/TD/td2802/Kaiser.pdf"]
-[3.8998947143554688, 2.0613319873809814, "[TT] Launch Vehicle of the CANYVAL-X CubeSats = PSLV-40 flight vehicle (XL configuration) of ISRO"]
-[8.813343048095703, 3.676039695739746, "[FF] Electric Field Measurement of the GEOTAIL Satellite = Unknown"]
-[11.651205062866211, 3.7647318840026855, "[TT] Firing Pressure of the X-axis Bang-Bang Maneuver = 1.56 bar"]
-[4.5195631980896, 7.596182823181152, "[TT] Band of the Transceivers = DSSS 2.4 GHz"]
-[5.886379718780518, 3.7382614612579346, "[FF] Hosted Payload Mission Objectives of the Alphasat = Fulfillment of each TDP experimentation plan"]
-[8.623664855957031, 7.502102851867676, "[TT] Size of the eROSITA pnCCD detector module = 2 cm x 2 cm"]
-[6.063004016876221, 2.3374953269958496, "[FF] Management of the LRI = JPL and the Max Planck Institute for Gravitational Physics (Albert Einstein Institute)"]
-[8.243585586547852, 7.8060994148254395, "[TT] Detector Arrays of the GIIRS = 538 TIR channels and 375 MWIR channels"]
-[8.088705062866211, 5.870933532714844, "[FF] Pixel Classification of the JWST Fine Guidance Sensor = Not Provided"]
-[5.283296585083008, 7.178312301635742, "[TT] Uplink Speed of the CXS-810C = 2 kbit/s"]
-[4.392202377319336, 3.8252720832824707, "[FF] Services of the Galileo Constellation = Positioning, navigation and timing services to our planet"]
-[8.99255657196045, 5.144952297210693, "[FF] Gyroscope of the Pico Dragon = 3-axis"]
-[5.115394115447998, -0.35528355836868286, "[TT] Image Reception Date of the CBERS-4A = December 27, 2019"]
-[9.120882034301758, 1.347794771194458, "[FF] Media Briefings Date of the New Horizons = Unknown"]
-[8.051812171936035, -0.8994427919387817, "[TT] Study Area of the ICESat-2 = Antarctica"]
-[13.821367263793945, 6.260599136352539, "[FF] Controls the state of charge of a 40 Wh battery pack and distributes power to all satellite subsystems of the PCDU = True"]
-[5.52225399017334, 1.114075779914856, "[TT] End Time of the High-voltage experiment = 17:52 Nov. 28, 2012 (UT)"]
-[8.010004043579102, 6.375308513641357, "[FF] Information of the Unresolved Imagery = Contains spectral and photometric information"]
-[7.508434772491455, 5.615902900695801, "[TT] L-band Radiometer Frequency of the SMAP = 1.4 GHz"]
-[7.0352983474731445, 0.9375937581062317, "[FF] Data Collection Period of the Liulin-MO dosimeter = Since the spacecraft reached orbit around the planet"]
-[5.067763328552246, 1.3208703994750977, "[FF] Instrument Installation Date of the GOES-U = 1 July 2019"]
-[7.606828689575195, 8.880208969116211, "[TT] Spectral Band of the MR-2000M1 = 0.5 - 0.8 \u00b5m"]
-[7.987934112548828, 1.5306199789047241, "[FF] Effect of the Sea Surface = Mimics the ocean floor"]
-[6.147125720977783, 2.601144790649414, "[FF] Space Test Program of the STP-H2-ANDE = URL: http://exploration.nasa.gov/programs/station/STP-H2-ANDE.html#overview"]
-[10.971460342407227, 6.0567307472229, "[TT] Light Intensity of the Faraday Cup = Roughly 10 kilowatts"]
-[4.035003185272217, 6.211854457855225, "[FF] Types of the Satellite Antennas = MBAs (Multi-Beam Antennas) and APAAs (Active Phased Array Antennas)"]
-[8.095281600952148, 2.204228639602661, "[FF] Derived Parameters of the MiniRad = Surface skin temperature/emissivity, sea ice edge/concentration, total precipitable water, the hydrometeor products of non-precipitating cloud liquid, rain and cloud ice, and indirect detection of the rate and phase distribution of precipitation"]
-[8.378003120422363, 1.5635241270065308, "[TT] Temperature of the Arctic Ocean = Cool"]
-[9.364352226257324, 6.774090766906738, "[TT] Spatial Resolution of the Satellite = 50 km"]
-[10.404548645019531, 2.284592866897583, "[FF] Typical X-ray Flare Duration of the X-ray Source = Up to a few hours or even days"]
-[5.208737850189209, 8.426576614379883, "[TT] Bandwidth of the Channel 6 = 1000 MHz"]
-[5.569187641143799, 6.814062595367432, "[TT] Data Rate of the Satellite = 100 kbit/s"]
-[9.002307891845703, 4.345473289489746, "[FF] Spin Phase Derivation of the CDMS = Using an analogue sun sensor (solar cell) mounted on the +Y face sensor"]
-[6.4439005851745605, 5.808315277099609, "[TT] Paths of the ABS = Three paths"]
-[7.055511474609375, 8.34710693359375, "[TT] Nominal SNR of the Band 2 = 1090"]
-[14.680742263793945, 6.680886268615723, "[TT] Capacity of the Batteries = 5.2 Ah"]
-[10.423626899719238, 5.775326728820801, "[TT] Non-operating Temperature Range of the Metrology System = -45\u00baC to 60\u00baC"]
-[13.833294868469238, 7.181242942810059, "[TT] Ripple (%) of the PS-1 = 5"]
-[9.026497840881348, 5.498335361480713, "[TT] Pointing Accuracy of the Spacecraft = \u2264 3\u00ba"]
-[7.607430458068848, -0.8284573554992676, "[TT] Launch Date of the ICESat-2 = Late August"]
-[8.868605613708496, 6.21177339553833, "[FF] Limb-Viewing Geometry of the SOLSE-2 = Illustrated in Figure 6"]
-[7.637650012969971, 3.6558055877685547, "[FF] Purpose of the Bipods = Minimize the mechanical constraints resulting from temperature gradients"]
-[8.511333465576172, 8.595292091369629, "[TT] Vertical resolution of the UV/VIS Spectrometer = 1.7 km"]
-[7.915282726287842, -0.3454864025115967, "[TT] Date of the Sea Ice Extent = October 2020"]
-[5.984915733337402, 3.4846160411834717, "[TT] Total Stationkeeping Cost of the ISEE-3 = ~30 m/s"]
-[11.929475784301758, 5.024240493774414, "[TT] Size of the ILAS = 950 mm x 1670 mm x 600 mm"]
-[5.213937282562256, 8.432379722595215, "[TT] Bandwidth of the Channel bandwidth per polarization = 450 MHz"]
-[9.878795623779297, 1.6523312330245972, "[FF] Observation Results of the Herschel = Filaments in nearby star-forming clouds seem to be roughly all the same width \u2013 about a third of a light-year"]
-[1.7435930967330933, -2.077512264251709, "[TT] Sampler Room A Close Command Date of the Hayabusa-2 = February 22, 2:20 UT"]
-[6.693621635437012, 8.432266235351562, "[TT] S/N or NEDT of the Spectral Channels = 150:1"]
-[7.7203049659729, 9.289690017700195, "[TT] Minimum Lower Band Edge of the MS1 (NIR1) = 765 nm"]
-[6.455308437347412, 1.862771987915039, "[FF] Sensitivity of the eROSITA = Higher than previous survey missions"]
-[4.833732604980469, 0.46833565831184387, "[TT] Date of the Pre-CHUVA = 3-24 March 2010"]
-[3.373818874359131, 5.685633182525635, "[TT] Number of Beams of the Integrated SAR Antenna = 126"]
-[11.155590057373047, 5.985962867736816, "[TT] Material of the SPEQS = Titanium"]
-[4.694643497467041, 0.897602915763855, "[TT] Observation Date of the ADONIS = 1996"]
-[8.988676071166992, 3.113537311553955, "[FF] Light Profile of the Bremsstrahlung Emission = Varies"]
-[11.977190971374512, -0.12837845087051392, "[FF] Follow-up Observations of the TESS = Study of the absorption and emission of light"]
-[3.7953662872314453, -1.1396052837371826, "[TT] Orbit of the Spektr-RG = Halo orbit around L2 Lagrange point"]
-[6.08706521987915, 0.623150646686554, "[TT] Orbit Control Maneuvers Start Date of the WINDS = March 2, 2008"]
-[9.72785472869873, 7.520966053009033, "[TT] Optical System of the PS0 = 2 element Maksutov Cassegrain"]
-[9.744172096252441, 8.394370079040527, "[TT] FOV of the LEICA = 24 x 20 \u00ba"]
-[5.986692428588867, -0.49729296565055847, "[TT] Mission Duration of the NuSTAR = More than eight months"]
-[13.221442222595215, 7.3286309242248535, "[TT] Maximum Power Consumption of the IES = < 20 W"]
-[5.534548282623291, 2.0707993507385254, "[FF] Mission Phases of the ABEX = Launch & Early Operations (LEOP), Science Commissioning, Science Operations, Spacecraft Decommissioning"]
-[4.83343505859375, -1.8085790872573853, "[TT] Orbit Transfer Time of the Chang'e-1 = 8-9 days"]
-[7.7085700035095215, 7.90671968460083, "[FF] Surface Quality Tolerances of the CCRs = 1/10 wavelength for the three back faces, 1/8 wavelength for the front face, 1/4 exiting wavefront"]
-[9.484612464904785, 8.966522216796875, "[TT] Revolutions/Day of the Iris Video Camera = 16"]
-[11.763410568237305, 0.08411923795938492, "[TT] New Exoplanets Found of the TESS = 66"]
-[11.331568717956543, 5.846398830413818, "[TT] Material of the Satellite Structure = Aluminum 6061"]
-[7.816890239715576, 2.3241519927978516, "[FF] Purpose of the Sensor Web Project = Global surveillance program to study volcanos"]
-[12.616991996765137, 9.095330238342285, "[TT] Initial Local Equator Crossing Time of the \u00d8rsted satellite = 14:39 hours"]
-[7.341763973236084, 4.261300086975098, "[FF] Instrument Overview and Recent Progress of the GIMS = Unknown"]
-[13.66849136352539, 5.721502304077148, "[FF] Application of the XTJ Prime solar cells = Powering Boeing's CST-100 Starliner spacecraft"]
-[9.421808242797852, 7.029257297515869, "[TT] Resolution of the CAVIS = 30 m"]
-[6.258999824523926, 1.1220195293426514, "[FF] Laser Production Date of the GEDI = April 19-20, 2016"]
-[6.19273567199707, 0.1561918556690216, "[FF] Handover to Crew-4 of the Crew-3 = Timed to maintain a U.S. presence on board"]
-[13.346312522888184, 7.383756160736084, "[TT] Tx Power of the LET = 200 W"]
-[4.742343425750732, -1.7870811223983765, "[FF] Midway Correction Control of the Chang'e-2 = 490 N"]
-[6.5805583000183105, -2.0491273403167725, "[FF] Launch Date of the Jason-3 = January 17, 2016"]
-[9.447245597839355, 7.271927833557129, "[TT] Resolution - Ground (Nadir) Visible Channel of the VIRR = 2.3 km"]
-[10.248004913330078, 5.531134605407715, "[FF] Survival Goal of the System = Launch vibration and on-orbit thermal extremes"]
-[12.448087692260742, 0.5637962222099304, "[TT] End of Life Date of the PLATO = 4 years (plus 4 years of possible mission extensions)"]
-[5.48481559753418, 1.2172404527664185, "[FF] Presentation Date of the ESTCube-1 = May 30, 2012"]
-[3.4670112133026123, 4.881814479827881, "[FF] Data Importance of the SASS = Far more interesting scientifically than the data from SAR"]
-[5.851136207580566, 5.893867015838623, "[FF] Low Overhead of the Network = Required"]
-[9.466687202453613, 5.161585807800293, "[TT] Performance of the Spacecraft AOCS = \u00b1300 \u00b5rad"]
-[9.805498123168945, 0.5524230003356934, "[FF] Range of the GLO-5 and GLO-6 = 115 - 1,150 nautical miles"]
-[7.187383651733398, 3.582151174545288, "[FF] Goal of the ADR Mission = Protect space assets from space debris and minimize collision risk"]
-[10.265551567077637, 2.078827381134033, "[FF] Principal Investigator of the eROSITA telescope = Peter Predehl"]
-[8.62729263305664, 2.2995541095733643, "[TT] Wind Random Errors of the Aeolus = Compliant to the mission requirements in the free troposphere for the Mie channel for laser output energies above about 65 mJ"]
-[11.31979751586914, 0.9430685043334961, "[TT] DRS Operations Duration of the LISA Pathfinder = 60 days"]
-[8.643047332763672, 2.2866530418395996, "[FF] Antenna Mechanism Lifespan of the SeaWinds instrument = More than a decade"]
-[7.218374729156494, 1.2420777082443237, "[FF] Image Content of the ExoMars Trace Gas Orbiter = The region where the ancient Uzboi Vallis enters the Holden crater"]
-[13.427450180053711, 5.699794292449951, "[TT] Solar Array Current of the IMPS = Up to 3 mA"]
-[6.75127649307251, -0.38765013217926025, "[TT] Observation Time of the Satellite = Approximately 10 minutes per orbit"]
-[7.599562168121338, 5.060107231140137, "[FF] Proceedings Date of the GPM microwave imager = 2014"]
-[5.948981285095215, 5.35638427734375, "[TT] Interface Module of the Non-SPA COTS components = ASIM (Appliqu\u00e9 Specific Interface Module)"]
-[7.707449913024902, 1.7321441173553467, "[FF] Indicator of Anthropogenic Stressors and Climate Change Impacts of the Coral Bleaching Events = Provides indications of anthropogenic stressors and climate change impacts"]
-[5.901635646820068, 0.5955236554145813, "[FF] Launch Date of the SuperView-1 = 9 Jan. 2018"]
-[6.582162857055664, 3.4494290351867676, "[FF] Data Volume of the Small Satellites = Increased"]
-[4.199177265167236, 1.4982507228851318, "[FF] Initiated of the Meteosat = 1972"]
-[7.008221626281738, -0.6258189082145691, "[TT] Rotation Period of the KELT-9 b = 36 hours"]
-[10.99638557434082, 7.345029354095459, "[TT] Swath Width (Full Performance) of the Satellite = 500 km"]
-[8.662370681762695, 7.559298992156982, "[TT] Photodetector Technology of the Optical Head = CMOS Active Pixel Sensor (APS)"]
-[4.388689994812012, -1.5885950326919556, "[FF] Lagrangian Point Feature of the Chang'e-2 = Utilized"]
-[10.056343078613281, -1.5479952096939087, "[TT] Orbit Inclination of the STARS spacecraft = 98.06\u00ba"]
-[5.379364967346191, 5.5900492668151855, "[FF] Function of the HSM = Collects ISP (Instrument Source Packets) in CCSDS format"]
-[6.540651798248291, -0.5215872526168823, "[FF] Orbit Duration of the LRO = Four Years"]
-[10.038887023925781, 2.9395008087158203, "[TT] Observation Date of the DICE CubeSats = March 16-17, 2013"]
-[9.108366012573242, 4.29603385925293, "[FF] Full Sun FOV of the EUVI = \u00b11.7 Rsun"]
-[9.496698379516602, 1.3104310035705566, "[FF] Internal Structure of the Celestial Bodies = Unknown"]
-[10.420648574829102, 7.083073616027832, "[TT] Full Disk Diameter of the ABI instrument = 17.76\u00ba"]
-[9.348447799682617, 5.081878662109375, "[TT] Pitch Axis Attitude Change of the TanSat = -60\u00ba~+60\u00ba"]
-[5.101797103881836, 3.2227084636688232, "[TT] Provider of the MORE = IDA TU Braunschweig"]
-[12.4542236328125, 0.5621848106384277, "[TT] Launch Date of the PLATO = 2026"]
-[5.221804141998291, 2.024313449859619, "[TT] Mission Status of the CADRE = Mission complete"]
-[9.803184509277344, 4.499908447265625, "[TT] Attitude Control of the Bus = Control using magnetorquers only, except short term"]
-[13.741355895996094, 6.877505302429199, "[TT] Electrical Power System of the IOD-1 GEMS = CSL FlexU Electrical Power System (EPS)"]
-[4.150436878204346, 7.319238185882568, "[TT] Operating Bands of the MWR = K-band and Ka-band"]
-[10.458827018737793, 4.071406364440918, "[TT] Boom Length of the MAGIC = 1 m"]
-[6.475032806396484, 0.6175779700279236, "[FF] Mission Operations Review Date of the Landsat 9 = Unknown"]
-[4.202946662902832, 0.23198145627975464, "[TT] Original Falcon 9 Launch Date of the OCSD = October 2016"]
-[4.36625862121582, 4.070791721343994, "[FF] Coding Scheme of the Galileo Signal = FEC-encoding, interleaving and improved CRC"]
-[4.134137153625488, 5.814877510070801, "[FF] Update Intervals of the ADS-B Receiver = Unknown"]
-[3.528817653656006, 4.950122356414795, "[FF] Operation during Eclipse of the SAR payload = Avoided"]
-[9.366206169128418, -1.203527569770813, "[TT] Direction of the RTN = From LEO user to GEO"]
-[12.834206581115723, 7.536685943603516, "[TT] Instrument Power of the ScaRaB = 42 W (average)"]
-[6.586931228637695, 0.7531677484512329, "[TT] TDRSS Support of the Landsat-5 = No"]
-[6.416751861572266, 2.006079912185669, "[FF] DOI of the Onboard Processing = https://doi.org/10.1109/JPROC.2018.2802438"]
-[10.622575759887695, 2.763550043106079, "[TT] Duration of Proximity of the DICE nanosatellites = Up to six months"]
-[5.050826549530029, 0.6228633522987366, "[TT] Launch Year of the Aeolus = 2018"]
-[11.510688781738281, 4.952690124511719, "[TT] Size of the Gaia = 3.5 m across"]
-[8.384023666381836, 5.421290874481201, "[FF] Trajectory Determination Accuracy of the ADEOS = Unknown"]
-[10.191121101379395, 5.8625993728637695, "[TT] Focal Plane Temperature of the TIR Instrument = 60 K"]
-[7.274625301361084, 6.9116363525390625, "[TT] Frame Rate of the GLM = 500 frames/s"]
-[6.863388538360596, 0.0406239852309227, "[FF] Development Time of the Spin-stabilized weather satellite = Not soon"]
-[12.362598419189453, 0.6267666816711426, "[TT] Accuracy of Stellar Radius Measurement of the PLATO = Up to 1-2%"]
-[2.886251211166382, 4.517624378204346, "[TT] Frequency Adjustment of the PALSAR-2 = \u00b1 21 MHz"]
-[8.574492454528809, 4.665787220001221, "[TT] Number of Recommendations of the Starliner = 60"]
-[10.065258979797363, 7.535322666168213, "[TT] Swath Width of the Pan Imager = 96 km"]
-[9.235353469848633, 0.2629259526729584, "[FF] Type of the Kurushima Kaikyo Bridge = Continuous suspension"]
-[13.257184028625488, 7.197524547576904, "[TT] Power of the ST (Star Tracker) = 6.5 W"]
-[5.375638484954834, 0.6304395198822021, "[FF] Review Date of the RHESSI = August 3, 2003"]
-[5.6312432289123535, 7.58023738861084, "[TT] Receiver Type of the Envisat = 2nd generation receiver (11 kg), a bi-frequency system in 2 channels"]
-[9.072386741638184, 5.098710060119629, "[TT] Power of the Rate gyro = 1.4 W"]
-[5.713870525360107, 4.598798751831055, "[FF] User Data Volume of the EDRS = Improved"]
-[8.932557106018066, 7.417323589324951, "[TT] Detector Thickness of the NINA = 150\u00b115 \u00b5m for the first plane, and 380\u00b115 \u00b5m for the remaining 15 planes"]
-[5.276245594024658, 0.5932608842849731, "[FF] Update Date of the Juno = 18 February 2020"]
-[5.430484294891357, 2.9660911560058594, "[FF] Transfer of the EMEA FleetBroadband = To Alphasat"]
-[9.109705924987793, 6.102844715118408, "[FF] Scan Mirror of the TEMPO = Included"]
-[4.834656238555908, 0.5396426916122437, "[TT] Launch Date of the PACE = January 2024"]
-[7.619399547576904, 7.080934524536133, "[TT] Cadence of the 3 He Spectrum = Up to roughly 20 MeV/nuc"]
-[9.79380989074707, -0.618054211139679, "[TT] Orbit Altitude of the Monitor-E = 540 km"]
-[9.251130104064941, 6.064146518707275, "[TT] Tracking acquisition of the Antenna = <12 minute cold start <5 minute warm start <1 s for 60 s lost"]
-[10.993420600891113, 3.7549431324005127, "[TT] Size of the NanoAvionics M6P 6U satellite bus = 6U"]
-[10.122058868408203, 7.551089763641357, "[TT] Image Size of the SIR-C = 100 km (azimuth, flight direction) x 50 km (swath)"]
-[8.64997673034668, 5.897189617156982, "[TT] Requirement Value of the Location accuracy = 70 m CE90"]
-[4.323374271392822, 3.3326330184936523, "[TT] Team Members of the Galileo 2nd Generation Satellites = Thales, Spaceopal, Leonardo and other partners"]
-[7.885012149810791, -2.515904426574707, "[FF] Purpose of the GOLD = Measure the density of molecular oxygen in the thermosphere"]
-[8.139177322387695, 6.583662986755371, "[FF] Problem of the Advanced Baseline Imager (ABI) = Unknown"]
-[7.196952819824219, 1.227799892425537, "[FF] Operation of the CAPSTONE = Return humans to the Moon"]
-[8.00637149810791, 5.234214782714844, "[FF] Components of the Radiometric Calibration = Radiance Calibration Coefficients, Response Linearity, Noise, Detector PRNU, Detector DSNU"]
-[10.426705360412598, 5.777904510498047, "[TT] Set Point Temperature of the OPAL = ~10\u00baC"]
-[5.356655120849609, 5.4946064949035645, "[TT] Ground Station Contacts of the LDCM = 14 per day"]
-[6.354169845581055, 4.036118984222412, "[FF] Responsibilities of the CAS = Propulsion Module, Service Module, Spacecraft Prime, Mission Operations (with ESA contribution), Chinese instruments"]
-[7.2007036209106445, 1.2727514505386353, "[FF] Sampling System of the Perseverance = Coring drill and sample tubes"]
-[13.600983619689941, 6.040843963623047, "[TT] Orbit Average Power of the Solar Generators = 280 W"]
-[13.228549003601074, 7.271838665008545, "[TT] Power Consumption of the LTP = about 150 W"]
-[12.085911750793457, 6.021202564239502, "[FF] Spatial Distribution of the EPISEM = 54% in the SAA, 26% in the Polar Regions, 20% Galactic Cosmic Rays"]
-[7.55989933013916, 8.723827362060547, "[TT] Radiances Measurement of the OLS = Down to 10-9 W/cm2/sr"]
-[9.423312187194824, 8.165637969970703, "[TT] Field of View of the Collecting Optics = \u00b1 7\u00ba"]
-[11.016075134277344, 7.295485019683838, "[TT] Swath Width of the DubaiSat-1 = 20 km"]
-[10.356046676635742, 6.710396766662598, "[TT] Mirror Planes Orientation of the Three Mirrors = Perpendicular to each other"]
-[7.9418182373046875, 2.4703805446624756, "[FF] Data Distribution of the MWI = ACC 557th Weather Wing (WW), Fleet Numerical Meteorology and Oceanography Center (FNMOC)"]
-[7.0841169357299805, 8.221930503845215, "[TT] Microphone Quantity of the Megastar = Trio"]
-[8.682987213134766, -0.2062803953886032, "[TT] Inclina. (\u00ba) of the Meteor-2-1 = 81.3"]
-[5.0778961181640625, 0.8210179209709167, "[TT] Meeting Location of the ICON = San Francisco, CA, USA"]
-[9.6199951171875, 4.891011714935303, "[TT] Stabilization of the AODCS = 3-axis"]
-[9.348122596740723, 6.2140021324157715, "[TT] Incidence Angles of the Multi-purpose beam mode = 20\u00ba to 50\u00ba"]
-[6.323544025421143, -0.194187194108963, "[TT] Characterization Duration of the SpinSat = Within the first four months"]
-[8.528098106384277, 7.873235702514648, "[TT] Number of Pixels of the Instrument = 640 x 480"]
-[6.551281452178955, 6.940512180328369, "[TT] Duty Cycle of the ScaRaB = 100%"]
-[12.498444557189941, 3.231942653656006, "[TT] Solid Propellant Quantity of the PSLV-C19 = 12 tons"]
-[13.403035163879395, 6.736389636993408, "[TT] Power of the Satellite = 250 - 1000 W"]
-[7.84590482711792, 7.157772064208984, "[TT] High-speed raw image data processing of the Frame Grabber = Sufficient computational capacity to receive and store the high-speed raw image data"]
-[6.342923164367676, 5.112588405609131, "[FF] Functions of the OBC = Processing, reconfiguration and timing"]
-[5.3655476570129395, 4.811241149902344, "[FF] GPS Antennas of the NOX Payload = Switchable pair, one pointing to the zenith and used for POD, and a second one oriented in an anti-flight direction (pointing at the Earth horizon) devoted to occultation measurements"]
-[7.140591621398926, 3.2433104515075684, "[FF] System Type of the GeoSTAR = 2-D spatial interferometric system"]
-[4.31656551361084, 0.7910992503166199, "[TT] User Commissioning Review Date of the EDRS-C = July 16, 2020"]
-[9.9249267578125, 7.442526817321777, "[TT] Ground Swath of the Imager = 15 km"]
-[7.474008560180664, 2.9407925605773926, "[TT] Swath Width of the MethaneSAT = 260 km"]
-[9.483419418334961, 0.6010869741439819, "[TT] Velocity After Engine Shutdown of the Schiaparelli = Less than 2 km/h"]
-[8.201130867004395, 6.450399875640869, "[FF] Components of the LDT = Photodiodes and LEDs"]
-[7.801877975463867, 6.155426979064941, "[FF] Function of the PIC = Create images of extended scenes"]
-[5.02067756652832, 4.8516035079956055, "[FF] Quantum Communication of the Micius = Enabled"]
-[6.54299783706665, 7.653809070587158, "[TT] Quantization of the Spectral Bands = 10-bit/pixel"]
-[8.080191612243652, 5.195530414581299, "[FF] Precision of the Data Product = Required"]
-[5.288461208343506, 2.978449821472168, "[TT] Platform of the AltiKa = Myriade"]
-[14.021129608154297, 3.2320544719696045, "[TT] Total Mass of the BeaverCube = 4.0 kg"]
-[8.48115062713623, 5.612579345703125, "[TT] Open Service Positioning Accuracy of the COMPASS/BeiDou = 10 m"]
-[8.371744155883789, 1.2715243101119995, "[FF] Modulation Technique Robustness of the RainCube = Very robust"]
-[9.310280799865723, 10.738268852233887, "[TT] Polarization of the ICI-5 = V"]
-[5.193393707275391, 2.4394683837890625, "[TT] Type of the ESPASats = Small and medium free-flying"]
-[13.771780967712402, 3.091705083847046, "[TT] Payload Capability of the EDRS-C = About 360 kg"]
-[7.66584587097168, 2.436038017272949, "[FF] Radar Altimeter of the SeaSat-1 = Device"]
-[8.856169700622559, 9.345128059387207, "[TT] Spectral Band 1 Spatial Resolution of the TANSO-CAI = 0.5 km"]
-[8.052197456359863, 7.410729885101318, "[TT] SNR of the Imager = >300"]
-[10.196427345275879, 7.987154483795166, "[TT] Telescope Aperture Diameter of the Pushbroom imager = 492 mm"]
-[10.041285514831543, 1.937962293624878, "[FF] Observation Date of the Chandra = Unknown"]
-[4.910482406616211, 3.3461945056915283, "[TT] Manufacturer of the Payload = EADS Astrium Ltd. and partners"]
-[7.86135196685791, 8.843304634094238, "[TT] Wavelength Range of the PAN = 0.50 - 0.90 \u00b5m"]
-[4.387301445007324, 2.1573050022125244, "[TT] Conceptualized Name of the KhalifaSat = DubaiSat-3"]
-[5.554139614105225, 3.8685741424560547, "[TT] Number of Operational Satellites of the DMSP (Defense Meteorological Satellite Program) = 3"]
-[5.427424430847168, 1.6172947883605957, "[TT] Service Commissioning Status of the Lacuna Space = Underway"]
-[9.284039497375488, 3.84100604057312, "[FF] Function of the V5 Sensor = Makes a simple voltage measurement near the magnetometer boom and may be used to infer the sunward electric field for plasma waves"]
-[7.558692932128906, 8.731772422790527, "[TT] Total Number of Spectral Bands of the MSU-50 = 6"]
-[7.186005592346191, 6.387688636779785, "[FF] Role of the Electrical GSE = Simulating the LEU and taking all of the required data needed to record laser performance"]
-[5.26076078414917, 4.054627895355225, "[TT] Number of orbital planes of the MEOSAR Constellation = 6"]
-[8.625307083129883, 5.799076080322266, "[TT] Alignment of the OSIRIS = Tracking sensor aligned to the collimator"]
-[10.098906517028809, 6.017001628875732, "[TT] Temperature Resolution at 100% albedo of the VNIR = \u2265 84"]
-[7.926405906677246, 7.389307975769043, "[TT] Video Data Output Frequency of the MS Detectors = 58 Mpixel/s"]
-[9.928958892822266, -1.4880249500274658, "[TT] Spin Axis Inclination of the Zeta Puppis = (24 \u00b1 9)\u00ba"]
-[5.219815731048584, 5.036280155181885, "[TT] Simultaneous Tracking of the SSTI = Up to 12 GPS satellite signals"]
-[4.976252555847168, 3.4572668075561523, "[TT] Provider of the Keramis-2 = IMST GmbH"]
-[6.210958003997803, 1.4335603713989258, "[FF] URL of the Swarm = http://www.dsri.dk/~nio/papers/EPS_58040359.pdf"]
-[8.319256782531738, -0.5078122019767761, "[TT] Measurement of the Sea Ice = 2.69 million km2 (1.04 million square miles)"]
-[6.467207431793213, 2.1211540699005127, "[FF] URL of the ACTS Satellite = http://acts.grc.nasa.gov/docs/SCAN_20010911161614.PDF"]
-[10.98566722869873, 7.576581954956055, "[TT] Swath Width of the MSU-E = 28 km"]
-[6.468690872192383, 1.0848045349121094, "[FF] Ground Segment of the FormoSat-7 / COSMIC-2 = Unknown"]
-[4.770630359649658, 0.5807122588157654, "[TT] Launch Date of the SEEDS-2 = April 28, 2008"]
-[8.226248741149902, 2.469926118850708, "[TT] Application of the VIS band (0.47 \u00b5m) = Aerosol detection and visibility estimation"]
-[4.336836814880371, 6.396745204925537, "[FF] Components of the SPIDER = Communications antenna and MakerSat"]
-[4.630579948425293, 6.617149353027344, "[TT] Transmission Protocol of the UHRIT = DVB-S2 (Digital Video Broadcasting-Satellite-Second Generation)"]
-[6.242764949798584, 3.994312047958374, "[FF] Purpose of the Muninn = Expand the geographical regions that we are testing in, and also test more advanced user scenarios on the ground with multiple satellites in view"]
-[13.819439888000488, 6.805107593536377, "[TT] Voltage of the High-Voltage Array = 300 V"]
-[6.405672073364258, -0.42493322491645813, "[TT] LTDN of the ALOS-3 = 1030 hours"]
-[7.82715368270874, 5.69532585144043, "[FF] Function of the DPU = Controls the optical sensor and processes the images. Determines the inertial pointing of the STR CHUs and the relative state of CSC using the VBS cameras"]
-[5.723429203033447, 5.311089515686035, "[FF] Flexibility of the UDP = Different telemetry packets delivered to various destinations based on onboard addressing decisions"]
-[10.312429428100586, 4.494219779968262, "[TT] Quantity of the Reaction wheels = 4"]
-[7.248969554901123, 8.031427383422852, "[TT] SNR at Maximum Radiance of the Satellite = 100"]
-[8.49466323852539, 1.7916678190231323, "[TT] 23.8 GHz Channel Function of the JMR = Primary water vapor sensor"]
-[7.487669944763184, -0.3903766870498657, "[TT] Launch Date of the Lunar IceCube = 16 November 2022"]
-[10.036626815795898, -1.4721637964248657, "[TT] Orbit Inclination of the Starshine-2 = 51.6\u00ba"]
-[9.38161849975586, 5.9168500900268555, "[TT] Motor Type of the Shutter = Limited angle DC brushless torque motor"]
-[8.002446174621582, 3.1452808380126953, "[FF] Measurement Targets of the GeoCARB = Carbon dioxide, carbon monoxide, methane and Solar-Induced Fluorescence quantities"]
-[8.582369804382324, 3.5983622074127197, "[FF] Effective Absorption Path of the Extinctive Stellar Occultations = Varies"]
-[12.123544692993164, 2.0067765712738037, "[TT] Series of the CartoSat-2E = Cartosat-2"]
-[8.587739944458008, 6.505659103393555, "[FF] Image Type of the TWINS = Stereo ENA"]
-[11.26305103302002, 5.3575615882873535, "[TT] Scintillator Dimensions of the Absorber = 6.5 mm x 10 mm x 49 mm"]
-[13.797657012939453, 6.908547878265381, "[FF] Voltage Stability of the Programmable Voltage Divider = Within one part per million"]
-[6.9727301597595215, 6.917876243591309, "[TT] Laser and Receiver Configurations of the CATS = Configuration 2a: 532 and 1064 nm narrow line width laser pulses, Configuration 2b: 355 nm laser pulses, Configuration 2c: Backup for laser 1"]
-[7.846721172332764, -0.934671938419342, "[TT] Data Presentation of the ICESat-2 = AGU meeting"]
-[1.7568384408950806, 6.158649444580078, "[TT] Mass of Dark Matter of the AMS = ~1 TeV"]
-[8.765300750732422, 3.4656379222869873, "[FF] Purpose of the APSS-1 = Monitor electrical activity in Earth\u2019s upper atmosphere to test whether ionospheric disturbances can predict earthquakes"]
-[4.320732593536377, -0.10498892515897751, "[TT] Launch Date of the P35-2 = 23.8. 1962"]
-[9.652973175048828, 8.237988471984863, "[TT] Field of View of the Optical Head = 52\u00ba x 28\u00ba / 90\u00ba x 74\u00ba (multi-hole mask: 10 x 10 spots / 3 x 3 spots)"]
-[6.283021450042725, 1.8951143026351929, "[FF] Documentation Provider of the Aalto-1 = Herbert J. Kramer"]
-[9.25101089477539, 4.906770706176758, "[FF] Function of the IMU = Attitude determination"]
-[5.566990375518799, 1.048302173614502, "[FF] Camera Installation Date of the OPTSAT 3000 = Dec. 6, 2012"]
-[6.682424068450928, -0.4714694619178772, "[TT] Halo Orbit Duration of the ISEE-3 = Nov. 1978 to June 1982"]
-[11.086193084716797, 1.5070152282714844, "[TT] Mass of the Star Tracker = < 0.5 kg"]
-[5.933611869812012, 5.999660015106201, "[TT] Number of In/Out Ports of the FPGA = About 130"]
-[5.272405624389648, 8.15195369720459, "[TT] Frequency Range of the IME-HF = Few kHz up to 37 MHz"]
-[7.4405837059021, 0.17685069143772125, "[TT] Stowage Process Duration of the OSIRIS-REx = Multiple days"]
-[5.820188045501709, -0.7649362683296204, "[TT] Goal Life of the Resurs-DK1 = 5 years"]
-[9.815629959106445, 4.360559940338135, "[FF] Particle Bending of the AMS-02 PM = Opposite directions"]
-[9.823884963989258, 6.432713508605957, "[TT] Data Rate of the Earth Radiation Budget Experiment (ERBE) = 10.5 kbit/scanner (average)"]
-[10.713890075683594, 7.39727783203125, "[TT] Swath Width of the AlSat-1 = 600 km"]
-[8.275674819946289, 0.7923728823661804, "[TT] Burned Area of the Black Fire = More than 130,000 acres"]
-[8.332250595092773, 8.598419189453125, "[TT] Band-to-band co-registration of the Spectrometer = < 1.4%"]
-[6.595809459686279, 6.857726097106934, "[TT] Laser Beam Link Speed of the EDRS-A = 600 Mbit/s"]
-[3.8732919692993164, -0.6104968190193176, "[TT] Deployment Orbit of the ABEX = Super-synchronous"]
-[5.729442596435547, 4.496048450469971, "[FF] Responsibilities of the SatsimIF = Establishing a TCP/IP connection with the Satsim computer, Uploading the simulated model on to the xpcTarget machine, Listening on the RAMSES multicast UDP network and redirecting all commands required to control the simulation"]
-[5.731417179107666, 0.6255567669868469, "[FF] Publication Date of the Cluster Mission = Oct. 1988"]
-[5.602809429168701, 6.6854143142700195, "[TT] Total Data Volume of the ISUAL instrument = About 1 Gbit/day"]
-[9.105278968811035, 0.4404982030391693, "[FF] ORM Goal of the ARTEMIS = Increase the altitude of apogee and the orbital period"]
-[5.539285659790039, 7.00009822845459, "[TT] Data Rate of the Payload = 1 GB/s"]
-[6.032266139984131, 2.898043632507324, "[TT] Mounting Location of the GEDI = Japanese Experiment Module's Exposed Facility"]
-[4.717099666595459, -0.2757364511489868, "[FF] Observation Date of the CATS = February 18, 2016"]
-[5.872074604034424, -0.7841653227806091, "[TT] Assembly and Testing Time of the Spektr-RG / SRG spacecraft = Around nine months"]
-[9.343097686767578, 3.1962826251983643, "[TT] Design Review Status of the Compact Coronagraph (CCOR) = Completed"]
-[8.031912803649902, 6.99000358581543, "[FF] Image Type of the Multispectral Visible Imaging Camera (MVIC) = Color"]
-[5.938413619995117, -0.5275792479515076, "[TT] Mission Duration of the NuSTAR = 3 years"]
-[3.365868091583252, 5.16934061050415, "[TT] Polarisation of the CSG-SAR = Dual"]
-[8.209433555603027, 0.5971987247467041, "[FF] Water Source for of the Colorado River Basin Reservoirs = 40 million people and 5.5 million acres of farmland"]
-[6.984130382537842, 7.890048027038574, "[FF] Characteristics of the MMIC = Low noise and high gain"]
-[8.958210945129395, 0.4021551012992859, "[TT] Location of the Crater = 55\u00ba16'51.6\"N/106\u00ba25'3.4\"W"]
-[14.084272384643555, 3.936873197555542, "[TT] Instrument Mass of the MSU-E = 60 kg"]
-[5.533818244934082, 7.517457008361816, "[TT] EIRP of the SDR-VSAT = > 76 dBW"]
-[6.274092674255371, 8.203895568847656, "[TT] No of bands/channels of the IRAS = 26"]
-[8.70708179473877, 5.3272705078125, "[TT] Absolute / Relative Scale Factors of the Three-axis diagonal gradiometer = 10 -3  / 10 -5"]
-[10.293227195739746, 5.895003318786621, "[TT] Operating Temperature of the VNIR, MWIR1, MWIR2, TIR1, TIR2 = 300 K"]
-[10.459832191467285, 6.7818498611450195, "[TT] Shell Radii of the Mirror = 51 - 191 mm"]
-[13.337871551513672, 2.891417980194092, "[TT] Satellite Mass of the MethaneSAT LLC = 350 kg"]
-[5.144105911254883, 2.354168653488159, "[TT] Mission Type of the GPIM = EO"]
-[9.231785774230957, 7.483008861541748, "[TT] Panchromatic of the Medium resolution = 59 m"]
-[5.07259464263916, 3.1920225620269775, "[TT] Manufacturer of the NEE-02 Krysaor = EXA (Ecuadorian Civilian Space Agency)"]
-[6.268927097320557, 2.581852674484253, "[TT] Function of the LAS = Propels the Orion Crew Module to safety in an emergency during launch or ascent"]
-[10.516694068908691, 6.590769290924072, "[TT] Quantity of the Mirror Modules = 7"]
-[5.017353534698486, 7.36561393737793, "[TT] Data Rate of the RF communications = 100 kbit/s"]
-[6.139840602874756, 4.557183742523193, "[TT] Operation of the SOLCON-3 = Remote POCC (Payload Operations and Control Center)"]
-[12.10487174987793, -0.12918396294116974, "[TT] Detection Ability of the TESS telescope = 7000 seconds"]
-[8.192915916442871, 2.9433295726776123, "[FF] Conference Presentation Date of the Geostationary Lightning Mapper = Sept. 29-Oct. 3, 2014"]
-[6.423120498657227, 4.7477126121521, "[FF] Data Processing Methods of the GOE = Differential GPS processing"]
-[4.388887882232666, 6.284266948699951, "[FF] Verification Process of the Antenna Performance = Post-launch commissioning and during the science calibration and validation campaign"]
-[7.425803184509277, 2.7311055660247803, "[FF] Symposium Date of the Astrium Earth Observation Optical Systems = May 31-June 4, 2010"]
-[7.9824042320251465, 8.66174030303955, "[TT] Measurement Range of the SIM = 200 \u2013 2400 nm"]
-[10.634110450744629, 1.4756050109863281, "[TT] Distance from Neutron Star of the Gaseous Atmosphere = 1,500 miles"]
-[7.098668575286865, -0.24710100889205933, "[FF] Orbits of the RASAT = 58,726 orbits"]
-[4.765798568725586, -1.1489309072494507, "[FF] Launch Schedule of the Shenzhou XIV = This year"]
-[7.520526885986328, 7.8133344650268555, "[TT] Dynamic Range (total) of the ScaRaB = up to 500 W m -2  sr -1"]
-[3.8210134506225586, 1.2359035015106201, "[FF] Landing Experiment of the Falcon 9 first stage = Pinpoint soft landing of a rocket onto a miniscule platform at sea"]
-[9.367103576660156, -0.9023288488388062, "[TT] Longitude of the Himawari-8 = ~140.7\u00ba east"]
-[9.71989917755127, 1.406410813331604, "[TT] Ground Resolution of the Pl\u00e9iades Neo = Larger"]
-[7.965217590332031, 5.337934970855713, "[TT] Measurement Accuracy of the FLLS (Fine Lateral and Longitudinal Sensor) = 30 \u00b5m (longitudinal)"]
-[7.373233795166016, 6.263125419616699, "[FF] Function of the LRA = Acts as a reference target for laser tracking measurements"]
-[8.984378814697266, 4.460635662078857, "[TT] Field of View (FOV) of the Sun Sensor = 4\u00ba"]
-[10.454297065734863, 5.714515209197998, "[TT] Measured Upper Atmosphere Temperature of the Jupiter = Around 800\u00ba Fahrenheit (426\u00ba Celsius)"]
-[1.7474946975708008, 4.561089038848877, "[FF] N/A of the MCP Lightning micro-camera = N/A"]
-[8.172013282775879, -1.009477138519287, "[TT] Parameter Measured of the ICESat-2 = Elevation changes"]
-[5.551681995391846, 4.479464530944824, "[FF] Ground System of the GOES-R = Global network of receiving stations linked to NOAA"]
-[10.505766868591309, 2.3716511726379395, "[TT] Optic Type of the CuPID X-ray telescope = Lobster-eye micropore optic"]
-[6.2962727546691895, 8.692704200744629, "[TT] Polarization, Right Swath of the KaRIn = VV"]
-[6.979313373565674, 6.86487340927124, "[TT] Operational Configurations of the CATS Laser 2 = Configuration 2a, Configuration 2b, Configuration 2c"]
-[12.162927627563477, -0.3013850152492523, "[TT] Monitoring Duration of the TESS = Two years"]
-[11.550619125366211, 4.6456475257873535, "[FF] Shape of the Doughnut = Clumpy"]
-[7.737670421600342, 6.797122478485107, "[TT] Interval of the Exposures = 2.7 s"]
-[9.126792907714844, 5.337517738342285, "[TT] Location of the MEMS 3-axis Gyro = Zenith end assembly"]
-[9.796292304992676, 7.605303764343262, "[TT] Cross-Track Swath of the OMPS Limb Profiler = 500 km"]
-[10.265950202941895, 5.591660976409912, "[TT] Accuracy Range of the Latent heat flux = 35 Wm- 2 0-200 Wm -2"]
-[7.475317478179932, 8.362129211425781, "[TT] Band (\u00c5) of the TRACE = 2500"]
-[3.2285425662994385, 2.2172234058380127, "[TT] Next Deployment Test Location of the Copernicus Sentinel-1C = France"]
-[9.431476593017578, 7.067285060882568, "[TT] Spatial Resolution of the SRAL = 300 m"]
-[6.743723392486572, 2.155834913253784, "[FF] URL of the PROCYON = https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=3348&context=smallsat"]
-[11.11666488647461, 5.867763042449951, "[TT] Spacer Material of the Cavity = ULE"]
-[5.962578773498535, 8.74194049835205, "[TT] MTF of the Instrument = Pan: \u2265 8.0% @ Nyquist frequency"]
-[5.9726738929748535, -2.327352285385132, "[TT] Orbit Altitude of the Kondor-E1 = 500 km"]
-[5.171387672424316, 2.7719767093658447, "[TT] Affiliation of the UWE-3 = University of W\u00fcrzburg, Germany"]
-[7.226467609405518, 7.310745716094971, "[TT] Digital I/O Pins of the CSI = 32"]
-[8.35227108001709, 7.177395343780518, "[FF] Observation Modes of the ALOS-3 = Nadir-looking and backward-looking panchromatic imager"]
-[6.173221588134766, 5.245263576507568, "[FF] Scheduling Trigger of the LMS = Reception of a payload link configuration request or when the Automator delivers the current state of the TTC buffer to the LMS"]
-[5.455038547515869, 4.655801296234131, "[TT] Size of the Corvus-BC satellites = 0.10 x 0.20 x 0.30 m"]
-[4.497231483459473, 3.2283220291137695, "[TT] Main Base of the PAZ = National Institute of Aerospace Technology in Torrejon de Ardoz, Madrid"]
-[13.450002670288086, 5.456591606140137, "[TT] Connection of the BCR = One half of the solar cell strings on two opposite sides of the spacecraft"]
-[8.663370132446289, 1.116724967956543, "[FF] Payload Contributions of the SAC-D/Aquarius = Italy, France, and Canada"]
-[6.1285200119018555, -0.5449994206428528, "[TT] Flight Operations of the RADARSAT-2 = 7 years"]
-[14.286869049072266, 2.8578290939331055, "[TT] Mass of the AprizeSat-9 = 12 kg"]
-[5.531859397888184, 2.5074410438537598, "[FF] Role of the Jared Isaacman = Mission Commander"]
-[4.781132698059082, -1.8639519214630127, "[FF] Sample Collection of the Chang'e-5 = Younger than those brought back last century by the Apollo missions"]
-[9.919370651245117, 8.218764305114746, "[TT] Telescope FOV of the BRITE = 24\u00ba diameter"]
-[10.079099655151367, -1.5379096269607544, "[TT] Orbit Inclination of the HY-2A = 99.3\u00ba"]
-[5.170043468475342, 8.206318855285645, "[TT] Frequency of the VNIR = 283 THz"]
-[5.68733549118042, 6.353086471557617, "[TT] Storage Capacity of the On-board Recorder = 1 Gbit"]
-[8.018752098083496, 8.491698265075684, "[TT] VNIR Bands of the GLI = 23"]
-[8.047371864318848, -0.9885233640670776, "[FF] Calibration and Validation Lead of the ICESat-2 = Kelly Brunt"]
-[5.417699337005615, 2.5991220474243164, "[TT] Affiliation of the LARES-2 = Italian space agency ASI"]
-[7.936263561248779, -0.9386571645736694, "[FF] Data Analysis of the ATLAS = Analyzing the preliminary ICESat-2 data"]
-[13.742770195007324, 7.323269844055176, "[TT] Voltage of the Antenna Power Supply = 100 V"]
-[3.4119205474853516, -0.8863052725791931, "[TT] Orbit Types of the WorldView Legion = Sun-synchronous orbit and mid inclination orbit"]
-[3.510798692703247, 5.401264667510986, "[TT] PRF of the SAR = About 18 kHz"]
-[6.520783424377441, 2.16125226020813, "[FF] URL of the Core Radar Electronics = http://www.nrsc.gov.in/assets/pdf/kr.pdf"]
-[9.554075241088867, -0.5182247161865234, "[TT] Initial Altitude of the FormoSat-2 = 728 km"]
-[6.9307541847229, -1.7574349641799927, "[TT] Total RSS sea Surface height LRM of the Jason-2 = 11.2/3.9/3.4 cm"]
-[6.052650451660156, -0.3715977072715759, "[FF] Mission Extension of the TIMED = Fourth Time"]
-[5.873987674713135, -0.7141838073730469, "[TT] Mission Life of the Telescope = Commissioning in < 6 months"]
-[7.344069480895996, 4.553839683532715, "[FF] Unknown of the Instrument of Grace = Unknown"]
-[3.139639377593994, 2.333698034286499, "[TT] Bands in the \u2018red edge\u2019 of the Sentinel-2 = 3"]
-[6.412557601928711, -0.6748964786529541, "[TT] Sunlit Phase Duration of the TanSat = ~46 minutes"]
-[4.935174942016602, 0.030684294179081917, "[TT] End of Life Date of the PARASOL = 11 Oct 2013"]
-[9.297595977783203, 3.2196197509765625, "[TT] Length of the Solar Coronagraph Instrument = About 150 m"]
-[6.7667765617370605, 4.834865093231201, "[FF] Configuration Capability of the AOCE = Variable"]
-[9.433499336242676, 8.432703018188477, "[TT] Input Port Field of View of the FTS = 2.6 arcmin diameter"]
-[7.298944473266602, 4.951047420501709, "[FF] Oscillation Types of the GOLF = P and g mode oscillations"]
-[7.841902732849121, 7.455690383911133, "[FF] Launch Plan of the Pixxel = Commercial hyperspectral imaging constellation of 24 satellites in 2024 - 2025"]
-[8.747807502746582, 7.163955211639404, "[FF] Field of View of the Image Quality = 0.8\u00ba (i.e. 3 Rsun)"]
-[10.222335815429688, 3.2563419342041016, "[TT] Spectrometer Frequency of the MicroMAS-2 CubeSat = Near 118 GHz"]
-[9.383245468139648, 7.130191326141357, "[TT] Resolution (Pan/MS) of the DST 35 = 1.5 m / 6 m"]
-[6.373509407043457, -0.3483441174030304, "[TT] Batch Injection Interval of the QB50 = 90 days"]
-[4.416065692901611, -1.649936318397522, "[TT] Discovery Year of the Blue Ring Nebula = 2004"]
-[3.4830615520477295, 4.643370628356934, "[TT] Imaging Modes of the Capella X-SAR Constellation = Stripmap, spotlight, and sliding spotlight"]
-[10.156014442443848, -2.763073444366455, "[TT] Die capacity of the SLC NAND-FMM = 8 Gbit"]
-[3.816179037094116, 4.550248622894287, "[TT] Area Coverage of the RADARSAT-2 = 23% over the identified area"]
-[6.010649681091309, 2.8656253814697266, "[FF] Deployment Location of the J-SSOD = ISS/JEM ( Japanese Experiment Module)/ Kibo"]
-[11.948143005371094, 6.289170742034912, "[TT] Particle Types of the TRD = Electrons, positrons, protons, antiprotons"]
-[3.4471352100372314, -0.92711341381073, "[TT] Orbit Type of the Landsat 9 = Sun-synchronous near-circular orbit"]
-[10.789377212524414, 7.573167324066162, "[FF] Accretion Disc Width of the V404 Cygni = 10 million kilometers"]
-[5.434454441070557, 0.17731153964996338, "[TT] Last Launch Year of the Space Shuttle = 2011"]
-[4.835714817047119, 0.5062358379364014, "[TT] Launch Date of the BRO-4 = 17 August 2021"]
-[6.711627006530762, 1.256205439567566, "[FF] Science Mode Start Date of the Colorado Student Space Weather Experiment (CSSWE) = Oct. 4, 2012"]
-[8.691707611083984, -0.20950660109519958, "[TT] Perigee (km) of the Meteor-3-1 = 1235"]
-[5.816112041473389, -2.213801383972168, "[TT] Longitude of the GEO-KOMPSAT-2B = 128.0\u00baE"]
-[5.075253486633301, 2.396115303039551, "[FF] URL of the EUMETSAT = http://www.eumetsat.int/website/home/Data/RegionalDataServiceEARS/index.html"]
-[6.5200605392456055, 2.7822718620300293, "[FF] Location of the Imagery Receiving Stations = Brazil and China"]
-[8.743708610534668, 7.2666239738464355, "[FF] Payloads of the ZACube-2 = Medium resolution matrix imager and a number of communication subsystems"]
-[6.355530261993408, -1.1865651607513428, "[TT] LTAN of the KOMPSAT-2 = 10:50 hours"]
-[4.778106212615967, 7.128499984741211, "[TT] Downlink of the Communications = S-band at 10 kbit/s"]
-[10.1193265914917, 5.557168006896973, "[FF] CTE of the CFRP = Coefficient of Thermal Expansion"]
-[6.394166946411133, 4.708073139190674, "[FF] Function of the Node-3 = Accommodates the items necessary for the distribution of commands and data, audio, video, electrical power, atmosphere, water and thermal energy to adjacent elements"]
-[5.549741268157959, 6.674344062805176, "[TT] Data Volume of the Mini-RF = 60 TB"]
-[10.505415916442871, 2.8595409393310547, "[FF] Image Credit of the CanX-7 nanosatellite = UTIAS/SFL"]
-[5.447519302368164, 2.314116954803467, "[FF] Development Partners of the SOHLA-1 = JAXA, Tokyo University, Osaka University, Osaka Prefecture University"]
-[4.8935699462890625, 7.189173221588135, "[TT] Uplink Data Rate of the TT&C S-band Communications = 4 kbit/s"]
-[7.0866498947143555, -0.4664943218231201, "[TT] Tumbling Motion of the Mayak = At least 1 revolution per second"]
-[5.582240104675293, 2.977649450302124, "[FF] Partners of the Hiber = Amazon Web Services, IBM Watson and Actility"]
-[9.401859283447266, 7.0126261711120605, "[TT] Spatial Resolution (VIS) of the MSU-SK1 = 210 m"]
-[9.093777656555176, 7.3415398597717285, "[FF] Quality Requirement of the Beam Splitter and Field Widening Prisms = Good quality over the area sampled by one spatial resolution element on the detector"]
-[7.690223693847656, 9.44741153717041, "[TT] Center Wavelength of the Band 10 = 7.43 \u00b5m (1425 cm -1)"]
-[6.2590508460998535, 4.647800922393799, "[FF] Function of the Onboard Computer = Controls and monitors the payload of the satellite and many other subsystems"]
-[7.309581279754639, 8.40556526184082, "[FF] Dynamic Range of the UVI instrument = Two switches"]
-[8.026619911193848, 7.514859676361084, "[TT] Feedback Sensor of the HSC-III = 2D- PSD"]
-[6.343870639801025, 3.3057892322540283, "[FF] Fly on of the HIRS/4 = NOAA-N, NOAA-N', and MetOp 1 and 2"]
-[5.170957088470459, 2.138439655303955, "[TT] Mission Type of the Buccaneer = Non-EO"]
-[13.12889289855957, 5.390419960021973, "[TT] Roll Bias Compensation of the Solar Array Drive Assembly = \u00b1 36\u00b0"]
-[10.239982604980469, 3.2159996032714844, "[TT] Beacon Signal Frequency of the ALBus CubeSat = 400.4 MHz"]
-[8.734063148498535, 0.9240015149116516, "[TT] Arrival Date of the Parker Solar Probe = April 28, 2021"]
-[4.059420108795166, 1.8702973127365112, "[TT] Launch Service Provider of the Global-9 = Spaceflight Inc."]
-[9.101726531982422, 6.442689418792725, "[TT] FSH Measurement Interval of the LCI = 167 ms"]
-[6.4446940422058105, 8.583931922912598, "[FF] Polarization of the Satellite Device = V"]
-[9.161147117614746, 7.3708696365356445, "[TT] Image Resolution of the SCAMP = 1.6 km"]
-[13.436727523803711, 2.8257734775543213, "[TT] ALMASat-1 Mass of the ALMASat-1 = 13.56 kg"]
-[6.842574596405029, 4.337701320648193, "[FF] Design Model of the OMPS = SOLSE"]
-[9.24026107788086, -0.739593505859375, "[TT] Orbit of the GreenCube = LEO (~ 500 km)"]
-[10.528619766235352, 6.500272274017334, "[FF] Developer of the Mirror Modules = M. Gubarev, B. Ramsey, S. L. O\u2019Dell, R. Elsner, K. Kilaru, J. McCracken, M. Pavlinsky, A. Tkachenko, I. Lapshov"]
-[4.763668537139893, 7.111496925354004, "[TT] Dual X-band Links Speed of the NigeriaSat-2 = 105 Mbit/s"]
-[9.905691146850586, 8.205286979675293, "[TT] Effective Focal Length of the OLS = 122 cm"]
-[13.443268775939941, 7.280678749084473, "[TT] Output Power of the STX = 2 W"]
-[6.033564567565918, 0.8423239588737488, "[TT] First Light Image Date of the SXT = October 26, 2015"]
-[5.7032389640808105, 5.381231307983398, "[FF] Digital Transparent Processor (DTP) of the SES-14 = Increases payload flexibility and will provide customized bandwidth solutions to SES\u2019s customers"]
-[6.992769718170166, 6.267697334289551, "[TT] Sub-Experiment Allotment Time of the DHS = 5 seconds"]
-[6.805728912353516, 7.410385608673096, "[TT] Digital Registers of the CAMEX chip = 16 x 64 bit"]
-[4.312918186187744, 2.4034929275512695, "[TT] Operating Environment of the ATLAS = Vacuum of space"]
-[3.7536919116973877, 6.634464263916016, "[TT] Type of the VDES Antenna = Folded dipole Yagi-Uda antenna with three elements in crossed configuration"]
-[8.36974811553955, 5.331448078155518, "[FF] Pointing Accuracy of the DMSP-19 = Degrades"]
-[2.9725465774536133, 2.0158164501190186, "[TT] SAR Data Acquisition Date of the Copernicus Sentinel-1 = 2 September 2019"]
-[5.513052463531494, -0.7989902496337891, "[TT] Design Life of the Jade Rabbit = 3 months"]
-[8.053997993469238, 5.219042778015137, "[FF] Calibration Process of the FLLS = Correcting systematic errors in the measurements"]
-[6.174157619476318, -0.20813249051570892, "[FF] Duration of the Radiation Effects Tests = Months to execute"]
-[9.43565559387207, 8.031143188476562, "[TT] Field of View of the Imaging Payload = 21.0 by 14.9 degrees"]
-[7.751119613647461, 6.478477954864502, "[TT] Mode 4 Imaging Frequency of the ABI = 30 Mesoscale images every 15 minutes as well as a Full Disk every 5 minutes"]
-[4.739263534545898, -1.211765170097351, "[TT] Launch Date of the Tianzhou-2 = 29 May 2021"]
-[6.615063667297363, 5.059566020965576, "[FF] Function of the ICM = Housekeeping"]
-[4.757508277893066, -1.8609853982925415, "[TT] Planned Launch of the Chang'e-5 = 2020"]
-[10.072307586669922, -1.5728211402893066, "[TT] Inclination of the OUTSat = 66\u00ba"]
-[7.928282737731934, 2.209552049636841, "[FF] Sensor Complement of the SeaSat = Sea surface winds, sea surface temperatures, wave heights, internal waves, atmospheric water, sea ice features, ice sheet topography and ocean topography"]
-[10.054976463317871, -0.509544849395752, "[TT] Nominal Altitude of the DubaiSat-1 = 680 km"]
-[7.597336292266846, 8.980596542358398, "[TT] NER of the Spectral Band B = 6.0 x 10^-6 W/(cm^2 sr \u00b5m)"]
-[11.00477409362793, 2.8888051509857178, "[TT] Boom Length of the Microsatellite = 2 m"]
-[3.693314552307129, 4.636828422546387, "[TT] SAR Technology of the ICEYE = Synthetic Aperture Radar"]
-[8.716261863708496, 0.18295395374298096, "[TT] Distance from Bennu of the OSIRIS-REx = 1,635 miles (2,200 km)"]
-[5.855932712554932, -0.8198001384735107, "[TT] Design Life of the Spacecraft = \u226512 years in space"]
-[13.378522872924805, 7.560822486877441, "[TT] Peak Pulse Power of the T/R module = +6 dBm"]
-[4.888360500335693, 1.6866662502288818, "[TT] Radar Instrument Data Transmission Stop Date of the SMAP = July 2015"]
-[8.91645336151123, 6.1709089279174805, "[TT] Scan Rate of the Reflector = 20.5 rpm"]
-[6.526708602905273, 5.084480285644531, "[FF] Purpose of the ETB = Evaluate and demonstrate a number of new electronic components, processors, and memory devices"]
-[9.955676078796387, 9.04084300994873, "[TT] Effective FOV of the Channel 6 = 26 km x 60 km"]
-[6.817727565765381, 7.057243824005127, "[TT] No of Elevation Beams of the TCU/TRC = 126"]
-[5.245207786560059, 3.2253987789154053, "[TT] Manufacturer of the OSIRIS-REx = Lockheed Martin Space"]
-[7.842898845672607, 8.462068557739258, "[FF] Bands of the Spectral bands = Pan: (0.42 - 0.73 \u00b5m), MS: (0.42 - 0.55, 0.55 - 0.63, 0.58 - 0.73 \u00b5m)"]
-[5.6802778244018555, 1.025187611579895, "[FF] International Astronautical Congress Date of the ETS-VII = Sept.28-0ct.2, 1998"]
-[9.211007118225098, 3.19584321975708, "[FF] Description of the Coronal Moss = The bright, reticulated pattern observed in many EUV images of solar active regions"]
-[8.950984954833984, 0.9376872181892395, "[FF] Flyby Imaging of the Parker Solar Probe = Bonus data"]
-[5.369582176208496, 0.8515149354934692, "[FF] Date of the Senior Review 2013 = June 13, 2013"]
-[10.167196273803711, 0.523780882358551, "[TT] Along-Track Separation of the TDX and TSX Satellites = 76 km"]
-[4.710067272186279, 8.248814582824707, "[TT] Center Frequency of the Satellite = 5.255 GHz"]
-[7.586324691772461, 4.08974552154541, "[FF] Calibration of the HY-2A Satellite = Unknown"]
-[13.886723518371582, 7.043776988983154, "[TT] Voltage Output of the HV Modules = Several hundred volt"]
-[5.125528335571289, 0.3948686122894287, "[TT] Forecast Period of the Hazards Outlook = Next week"]
-[8.35271167755127, 7.261113166809082, "[TT] Interface of the Supervision Cameras = CameraLink"]
-[4.201138496398926, 1.970490574836731, "[TT] Launch Date of the NigeriaSat-1 = Sept. 27, 2003"]
-[9.627476692199707, -1.0401967763900757, "[TT] Local Time Drift of the PARASOL = Drifting"]
-[8.37229061126709, 1.9340771436691284, "[TT] Instrument Type of the NSCAT = Scatterometers"]
-[8.052933692932129, -1.02559494972229, "[TT] Open Water Detection of the ICESat-2 = Open water within a lead shows up in the satellite data as a very flat surface"]
-[9.305438995361328, 7.082115173339844, "[FF] Spatial Resolution of the HPT = High"]
-[9.428666114807129, -0.2059987485408783, "[TT] Altitude of the OSIRIS = About 20 m"]
-[7.957381725311279, 8.17306137084961, "[TT] Unfolding Issue of the iROSA = Interference"]
-[5.901179313659668, -0.7420095205307007, "[FF] Operational Life of the TanSat = Three years"]
-[3.3983359336853027, 6.311124801635742, "[TT] Size of the 5-panel deployable antenna = 11m x 3,6m"]
-[9.132462501525879, 5.230030536651611, "[FF] Spacecraft Attitudes Range of the GMOD = From zenith (0\u00ba) to nadir (180\u00ba)"]
-[8.16223430633545, 1.229903221130371, "[FF] Radar of the Soil Moisture Active Passive (SMAP) = L-band"]
-[4.701634407043457, 6.870614528656006, "[FF] Data Downlink of the GHOSt satellites = Ka-band, S-band for high speed data (HSD) transmissions"]
-[5.739326477050781, -0.7077445387840271, "[TT] De-Orbit Lifetime of the Secondary Payloads = 25 years"]
-[13.997913360595703, 3.7672486305236816, "[TT] Mass of the MI Radiometer = 139 kg"]
-[8.866617202758789, 3.2071115970611572, "[FF] Imaging Capability of the ICON = Provides the ability to separate the drivers and pinpoint the real cause of ionospheric variability"]
-[7.60009765625, 6.420450210571289, "[TT] Space Look Observation Frequency of the ABI = At least every 30 seconds"]
-[5.423867702484131, 7.0565266609191895, "[TT] Instantaneous Data Rate of the WCOM = Approximately 27 Mbps"]
-[4.782764434814453, 1.6816143989562988, "[FF] Alternate Name of the GCOM-C = SHIKISAI"]
-[7.05918550491333, 7.029914379119873, "[TT] Contributing Organization of the Laser-Induced Breakdown Spectroscopy instrument = IRAP (Institut de Recherche en Astrophysique et Plan\u00e9tologie), in France"]
-[7.025899887084961, 6.504430294036865, "[FF] Data Redistribution of the GLM = Within 1 minute of reception"]
-[5.019894123077393, 2.5498456954956055, "[TT] Managing Office Location of the Lucy = NASA's Marshall Space Flight Center in Huntsville, Alabama"]
-[7.879281044006348, 4.7895684242248535, "[FF] Function of the radFET dosimeters = Trap positive charges and shift the threshold voltage"]
-[8.63664722442627, 3.6913206577301025, "[FF] Objective of the SOLCON-2 = Measurement of the absolute value of the total solar irradiance (and long-term variations)"]
-[9.085341453552246, -1.2093476057052612, "[TT] Position of the EDRS-C = Geostationary orbit with visibility over central Europe"]
-[10.187018394470215, 8.226813316345215, "[TT] Thickness of the Aperture Function = a"]
-[6.662094593048096, 6.272829532623291, "[TT] ToO Nominal Programming Delay of the SVOM = 48 hr"]
-[6.492347717285156, 7.036106109619141, "[TT] Wavelength of the SILEX Optical Terminal = 810 - 850 nm"]
-[8.441834449768066, 7.390139102935791, "[TT] Image Sensor Type of the Corvus = CMOSIS CHR70M"]
-[5.117465496063232, 2.354219913482666, "[TT] Mission Type of the CAPSTONE = Non-EO"]
-[5.958217144012451, 4.176234245300293, "[FF] API of the GOES-R Access System = Application Programming Interface"]
-[8.658244132995605, 3.4547457695007324, "[TT] Observation Spectrum of the SUVI = Extreme ultraviolet"]
-[8.866076469421387, 3.3187594413757324, "[FF] Measurement of the ROSA = Electron density profiles in the ionosphere"]
-[5.092316627502441, 0.6872784495353699, "[TT] Assembly Date of the AMS = 2011"]
-[6.971584320068359, 4.524871349334717, "[FF] Mission Objective of the FASTRAC = Investigate enabling technologies crucial for satellite formations, including on-orbit micro-thrust capability, relative navigation, attitude determination, and satellite crosslink communications"]
-[7.231788158416748, 8.317659378051758, "[FF] Sampling of the VIS Channel = Independent of the filter-wheel position"]
-[5.518423080444336, 2.244800090789795, "[FF] Affiliation of the Jonathan Gebbie = Unknown"]
-[9.720650672912598, -0.3018454313278198, "[TT] Altitude of the Elves = ~90 km altitude"]
-[8.826757431030273, 3.372365951538086, "[FF] Path Dependency of the Radio Waves = Ionosphere Location"]
-[6.4534454345703125, 0.444751113653183, "[TT] Proposal Year of the Geospace Dynamics Constellation = 2013"]
-[8.085068702697754, 0.7177380919456482, "[FF] Parameter Measurement of the GRACE-FO = State of soil moisture and groundwater"]
-[7.805640697479248, 2.040985345840454, "[TT] Primary Use of the Band 9 = Ocean color"]
-[9.570734977722168, 4.640781402587891, "[FF] URL of the Drag-Free and Attitude Control System = http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=39981"]
-[6.849912166595459, 2.2319586277008057, "[FF] Mission Status of the Solar-B / Hinode = Unknown"]
-[9.298770904541016, 0.0856187716126442, "[TT] Diameter of the Tianhe = 4.2 meters"]
-[7.581827163696289, 0.9663635492324829, "[TT] Publication Date of the Gravity Recovery and Interior Laboratory (GRAIL) = 2013 Feb 8"]
-[3.6405069828033447, -0.8350116014480591, "[FF] Applicable Orbits of the AutoConTM = Variety of orbits ranging from LEO to non-Keplerian trajectories such as libration orbits"]
-[5.677754878997803, 11.362105369567871, "[FF] Approx. peak sensitivity altitude of the Channel 7 = Unknown"]
-[6.010434627532959, 5.430845737457275, "[TT] Ability to Command Gain Adjustments of the OLS = Yes"]
-[7.401787757873535, 4.836592197418213, "[TT] Position of the ADACS = Front of the satellite"]
-[5.630211353302002, 5.648160457611084, "[FF] OBC Processor of the X-Sat = StrongARM processor"]
-[5.295133590698242, 8.107661247253418, "[TT] Frequency Range of the IME-BF = DC\u20131 MHz"]
-[10.488362312316895, 3.9604625701904297, "[TT] Tip Mass of the Gravity Gradient Boom = 40 g"]
-[9.638640403747559, 0.7651910781860352, "[TT] Closest Approach Distance of the Eta Carinae = 140 million miles (225 million kilometers)"]
-[5.372401237487793, 2.6321041584014893, "[TT] Type of the 55 Cancri e = Rocky"]
-[2.9379258155822754, 2.3808839321136475, "[FF] Nitrogen Dioxide Emission Reduction of the Copernicus Sentinel-5P = Around 40% over Chinese cities"]
-[8.971184730529785, 4.384581565856934, "[TT] Accuracy of the Fine Solar Sensors = 0.2\u00ba"]
-[12.084047317504883, -0.20963028073310852, "[TT] Monitoring Area of the TESS = 24 x 96\u00ba strips of the sky"]
-[8.057246208190918, 9.062302589416504, "[TT] Wavelength of the Iron oxides = 1 \u00b5m"]
-[4.446890830993652, 0.695559024810791, "[TT] Launch Date of the DMSP F-19 = April 2014"]
-[5.632604122161865, 7.693731784820557, "[TT] EIRP of the VSAT (Very Small Aperture Terminal) = >61.7 dBW"]
-[8.377867698669434, 7.228640079498291, "[TT] Quantity of the Payload Cameras = 24 normal and 2 fast cameras"]
-[5.063379764556885, 1.8217655420303345, "[TT] Operational Since of the PVA = Late 2013"]
-[11.563267707824707, 6.485605239868164, "[TT] Energy Range of the NuSTAR = 20 to 40 keV"]
-[5.500528812408447, 6.291912078857422, "[TT] Storage of the On-board computers = 16 MByte"]
-[7.856509208679199, 2.270831823348999, "[FF] Location of the Warm-Core Ring = About 100 km southeast of Delaware Bay"]
-[4.3096489906311035, 0.36502930521965027, "[FF] Launch Readiness Capability of the JPSS = FY 2015 and FY 2018"]
-[6.731285572052002, 4.660403728485107, "[FF] Function of the ISM = Define the spacecraft structure, model functionality, and requirements"]
-[7.912106037139893, 8.978300094604492, "[TT] Center Wavelength of the NIR (Near Infrared) = 805.0 \u00b5m"]
-[3.451904296875, 4.897281646728516, "[FF] Functionalities of the DIS = Scheduling X-band RF signal reception, X-band RF signal receiving and status monitoring, analog to digital conversion to extract CADU frames for retrieving SAR source packet data"]
-[6.31784725189209, 8.53317642211914, "[TT] Polarization Channels of the SGLI = 3 directions"]
-[11.740915298461914, 7.523954391479492, "[TT] End of Life Date of the Megha-Tropiques = 15 Dec 2021"]
-[7.396148204803467, 3.626904249191284, "[TT] Daily Soundings of the GeoCarb = ~10,000,000 soundings per day"]
-[9.099599838256836, 1.0788371562957764, "[TT] Destination of the Juice mission = Jupiter"]
-[10.74360179901123, 4.367185115814209, "[FF] Testing of the Valves = Ongoing"]
-[5.686533451080322, 1.5715668201446533, "[FF] Status of the WorldView-1 = Operational"]
-[9.306204795837402, 7.351231098175049, "[TT] Spatial resolution of the Optical System = 1.1 km"]
-[11.71223258972168, 4.81427001953125, "[TT] Structure Size of the S/C = 4 m x 3 m x 2 m"]
-[8.01480484008789, 0.8361991047859192, "[FF] Drought Information of the GRACE-FO = Soil moisture, crop health, groundwater, streamflow"]
-[7.853702068328857, 4.949047565460205, "[FF] Pre-Flight Characterization of the TRUTHS = Good level of pre-flight characterization of the sensor under test"]
-[8.591845512390137, 7.84831428527832, "[TT] Number of Detector Pixels of the Short Wavelength Band = 512 x 512"]
-[5.635801792144775, 4.738197326660156, "[TT] Communication Network of the EDRS = Geostationary orbit"]
-[5.459023475646973, 0.9309350252151489, "[FF] Launch Date of the Satellite = Unknown"]
-[6.687155246734619, 1.0751163959503174, "[FF] Publication Date of the Orbital Formation-Keeping System = Jan.\u2013 Feb. 1989"]
-[6.533132076263428, 1.8629635572433472, "[FF] DOI of the NuSTAR = 10.1088/0004-637X/770/2/103"]
-[6.53981351852417, -0.46080896258354187, "[TT] Period of the SPOT-1, -2 and -3 = 101 minutes"]
-[6.462771892547607, 3.2934348583221436, "[TT] Science Payload Sensor Type of the Neutron-1 = Elpasolite sensor"]
-[10.779024124145508, -1.1087599992752075, "[FF] Duration of Attitude Modes of the SLATS = About 40% of the orbital period"]
-[9.91183090209961, 6.294543743133545, "[TT] Detector Radiation Tolerance of the D-CIXS = Higher than conventional CCDs"]
-[7.4457197189331055, 0.9288788437843323, "[TT] Launch Initiative of the MoonLIGHT = NASA's Commercial Lunar Payload Services"]
-[9.430008888244629, 3.9329936504364014, "[FF] Development Date of the Vector Fluxgate Magnetometer (VMAG) = June 3, 2010"]
-[4.168501853942871, 1.9954533576965332, "[TT] Primary Payload of the H-IIA launch vehicle No. 37 = GCOM-C1 spacecraft of JAXA"]
-[6.905715465545654, 6.37544059753418, "[TT] Time of the Shape-Setting Process = 2 minutes"]
-[11.11709976196289, 4.149209022521973, "[TT] Bonding Technique of the GP-B = Hydroxy-catalysis bonding"]
-[9.482555389404297, 8.210672378540039, "[FF] Direction of the Photons = Out the sides of the column"]
-[5.006988525390625, 4.270937919616699, "[TT] Number of Stations of the Ground Receiving Stations = 5"]
-[14.133885383605957, 3.1400344371795654, "[TT] Cargo Weight of the CREAM = 1,258 kg"]
-[5.211372375488281, 7.025258541107178, "[TT] Data Rate of the Data downlink = 2 x 50 Mbit/s"]
-[5.636407852172852, 6.194311618804932, "[TT] Data Storage of the Sentinel-1 = Large on-board science data storage"]
-[8.442681312561035, 3.2134785652160645, "[TT] Application of the Alice = Measure ultraviolet emissions from atmospheric constituents, detect atmospheric constituents by the amount of sunlight they absorb"]
-[5.545773983001709, 5.662452697753906, "[TT] CPU of the Avionics bus = PIC32"]
-[7.9241533279418945, -2.5359110832214355, "[TT] \u03a3O/N2 Column Density Ratio Enhancement of the GOLD = ~7% after the eclipse passed"]
-[5.626150608062744, 2.9277868270874023, "[TT] Affiliation of the Dove-3 = Planet Labs Inc. (formerly Cosmogia Inc.), San Francisco, CA, USA"]
-[6.314846515655518, 8.632247924804688, "[TT] Polarization of the 4 = Horizontal"]
-[6.206536293029785, 5.2988128662109375, "[FF] Function of the RFGeo = Identifies and geolocates RF signals"]
-[8.848062515258789, 0.075703464448452, "[TT] Lighting Requirement of the OSIRIS-REx = At least a 5\u00ba elevation"]
-[8.30942440032959, 1.574580430984497, "[FF] Application of the L/S/C Tri-frequency Radiometer = Ocean salinity observation"]
-[3.859999656677246, 6.37019157409668, "[TT] No of Radiation Elements of the Antenna = 128"]
-[9.57951831817627, -1.274758219718933, "[TT] Orbit of the OCO-3 = Mounted on the exterior of the space station, which circles between 52\u00ba north and 52\u00ba south latitude"]
-[6.3527750968933105, 3.492870807647705, "[FF] Integration of the LAS = Crew and Service Module assembly"]
-[4.504635334014893, 8.01184368133545, "[TT] RF Frequency of the Antenna = Rx (uplink): 17.7-18.8 GHz Tx (downlink): 27.5-28.6 GHz"]
-[5.459115505218506, 1.6845371723175049, "[FF] Purpose of the ALOS-2 = Forest Monitoring"]
-[6.1847686767578125, 5.56016206741333, "[FF] Data Quality of the TriG receiver = Increased"]
-[7.043446063995361, 1.8946633338928223, "[FF] URL of the Picard = http://solarnet.projet.latmos.ipsl.fr/fichiers_pdf/pro_picard_SOLSPA.pdf"]
-[10.143974304199219, -2.760078191757202, "[TT] Interface of the NAND-Flash = Eight bit interface"]
-[9.608177185058594, 8.300108909606934, "[TT] Field of View of the LISS-IIM = \u00b15\u00ba"]
-[8.06528377532959, 8.099200248718262, "[FF] Bandpass Filters of the MWIR and TIR cameras = Mounted in front of one line of the MWIR array and on both lines of the TIR array"]
-[6.528456211090088, -1.9496465921401978, "[TT] Bus Provider of the Jason-2 = CNES"]
-[2.299428939819336, 2.769256353378296, "[TT] PI of the EPI-Lo = Dave McComas"]
-[6.415575981140137, -1.3041270971298218, "[TT] Data Release Date of the GRACE-FO = 12 June 2019"]
-[7.517513275146484, 1.7677687406539917, "[TT] Distribution of the Argo buoys = Ocean-wide"]
-[5.415206432342529, 1.6976921558380127, "[FF] Sensor Characterization of the Deimos-2 = DSNU, PRNU, MTF"]
-[8.839057922363281, 6.3026933670043945, "[TT] Imager Pointing Accuracy of the STARE = 0.31\u00ba"]
-[8.722665786743164, 6.747559070587158, "[TT] Imager of the STARE-B = More sensitive"]
-[11.282970428466797, 3.5625672340393066, "[FF] Ignition of the CGG = By a glow plug, avoiding the use of pyrotechnics"]
-[9.129652976989746, 7.217936038970947, "[TT] Image Resolution of the DEIMOS-2 = 0.75 m per pixel"]
-[8.955096244812012, 9.393780708312988, "[TT] Spatial Resolution of the TANSO-CAI-2 = 460 - 920 m at nadir"]
-[13.473350524902344, 6.849048137664795, "[TT] Electrical Power of the Spacecraft = 200 W"]
-[6.323816776275635, -0.06651657819747925, "[TT] SST Temporal Sampling Period of the CIMR = Sub-daily"]
-[6.862875461578369, 7.1413679122924805, "[FF] ECCM Configurations of the Complete Solution = SPAN 5, SPAN 4 through digital beamforming, SPAN 2b, SPAN 3b+3, STRX"]
-[7.520667552947998, 1.2531532049179077, "[TT] Publication Count of the SeaSat = 6 special issues of journals plus dozens of papers"]
-[12.201506614685059, 3.670151472091675, "[TT] Performance of the I2 = Similar to xenon (Xe)"]
-[8.950865745544434, 1.4235082864761353, "[TT] Program of the New Horizons = New Frontiers Program"]
-[8.01341724395752, 4.290046691894531, "[TT] Instrument Type of the POLDER = Earth radiation budget radiometers"]
-[3.171424388885498, 1.638780951499939, "[TT] Downlink Time of the Sentinel-3 = Approximately 6 minutes per orbit"]
-[5.211657524108887, 1.1384562253952026, "[FF] Project Announcement Date of the C/NOFS = Dec. 16, 2008"]
-[8.739532470703125, 0.21471737325191498, "[TT] Descent Distance of the OSIRIS-REx = About a half-mile (805 meters)"]
-[8.541593551635742, 0.1592426300048828, "[TT] Expected Perihelion of the Comet ATLAS = 31 May"]
-[14.247053146362305, 3.223845958709717, "[TT] Mass of the Venta-1 = ~5 kg"]
-[9.712689399719238, 7.653249263763428, "[TT] Scan Rate of the Telescope = 200\u00ba/s"]
-[8.56954574584961, 5.632330894470215, "[TT] SIS/URE of the QZS-1 = 40 cm (rms)"]
-[5.887721538543701, 5.8124542236328125, "[FF] Digital Data Recorder of the MUX = DDR"]
-[11.344833374023438, 5.858064651489258, "[TT] Material of the ESPA ring = Aluminum"]
-[4.434869766235352, 7.875924110412598, "[TT] Downlink Frequency (Normal C-band channel) of the Communication Payload = 3625-4185 MHz"]
-[10.153875350952148, -0.4720395505428314, "[TT] Orbit Altitude of the CuPID 6U CubeSat = 550 km"]
-[9.336426734924316, 3.704822540283203, "[FF] Mission Objective of the \u00d8rsted = Collection of high precision scalar magnetic data"]
-[9.877963066101074, 8.9429931640625, "[TT] IFOV of the VIS channels = 1 km (vertical) x 2 km (horizontal)"]
-[9.867727279663086, 8.189425468444824, "[TT] Focal Length of the Optics = 8.6 m"]
-[12.031485557556152, 4.4996418952941895, "[TT] Size of the Spacecraft = 44 cm between sides and 47 cm body height"]
-[8.504035949707031, 1.912950038909912, "[TT] Required PRI for Seawinds Interleaved Operational Design of the RapidScat = Less than 3 ms"]
-[5.026088714599609, 0.9187635183334351, "[FF] Development Status of the DRACO = Ongoing"]
-[5.109240531921387, 1.918957233428955, "[TT] Recovery Location of the Genesis Sample Return Capsule = Utah desert"]
-[4.216720104217529, 1.985520362854004, "[FF] Launch Date of the NigeriaSat-2 = Unknown"]
-[7.13100004196167, 6.620987892150879, "[TT] Signal Acquisition Range of the Satellite Laser Terminal = Up to 50,000 km"]
-[5.96768045425415, 2.4372098445892334, "[FF] Designers of the ISIM = Matthew Garrison, Keith Parrish, Charles Perrygo"]
-[4.8584418296813965, 3.765556812286377, "[TT] Manufacturer of the GATR-TRAC ground station antenna = GATR Technologies"]
-[7.384092330932617, 8.735410690307617, "[TT] ROIC Technology of the VIS channel = Thick-film technology"]
-[13.494317054748535, 6.797658920288086, "[TT] Power Generation of the Spacecraft = 4 kW"]
-[8.707171440124512, 9.050945281982422, "[TT] Sensitivity of the NIRSpec MIRI = 5000 nJy (21 \u03bcm, \u03c4 i =10,000 s, and \u03bb/\u0394\u03bb = 4.2)"]
-[5.3050103187561035, 0.941526472568512, "[FF] Launch Date of the SAC-D = Unknown"]
-[6.1603617668151855, 2.6002585887908936, "[TT] Mission Budget of the Carruthers Geocorona Observatory = $75 million"]
-[11.544541358947754, 6.518702983856201, "[TT] Energy Band of the JEM-X = 3 - 35 keV"]
-[5.1194748878479, 3.123878240585327, "[TT] Manufacturer of the CUTE-1.7+APD-2 = Tokyo Institute of Technology (TITech), Japan"]
-[5.3340888023376465, 3.9515531063079834, "[TT] Number of Satellites of the Flight Satellites = 8"]
-[7.989840030670166, 2.0288546085357666, "[FF] Cross-Calibration Time Difference of the CloudSat = 30 minutes"]
-[7.276666641235352, 4.778329849243164, "[TT] Other Components of the DOSTEL = Two PIN diodes fixed to the one print board and mounted towards the other two directions"]
-[5.2029595375061035, 2.4945061206817627, "[TT] Developer of the FSSCat = Universitat Polit\u00e8ctica de Catalunya (UPC)"]
-[5.292140960693359, 3.9748263359069824, "[TT] Maximum Satellites Launched of the Falcon 9 = 15-16 to an inclined orbit, \"something like 13\u201d to a polar orbit"]
-[7.4466423988342285, 0.9612511396408081, "[FF] Goal of the MoonKAM = Engage middle schools in the GRAIL mission and lunar exploration"]
-[3.403864860534668, 5.192193508148193, "[TT] Average Sigma Naught of the SAR instrument = -7.5 dB"]
-[14.255658149719238, 3.147536277770996, "[TT] Mass of the CAS500-1 = 500 kg"]
-[13.843724250793457, 3.3320930004119873, "[TT] Quantity of the KickSat = 1"]
-[6.513899326324463, 3.3673863410949707, "[TT] Video Frame Rate of the BlackSky Global Satellite = 1 frame per second"]
-[3.8743584156036377, 0.8603050112724304, "[FF] Launch Date of the PSLV-C38 / Cartosat-2 Series Satellite Mission = June 23, 2017"]
-[3.6788830757141113, 6.427618503570557, "[TT] Antenna Type of the Radar Altimeter (ALT) = Parabolic 1 m antenna"]
-[9.702445983886719, 2.801893472671509, "[TT] Purpose of the CREDANCE = Survey cosmic rays and particles in the radiation belts"]
-[3.0921993255615234, 3.9176583290100098, "[TT] Dataset Combination of the NISAR = GRACE Follow-On data"]
-[7.088397979736328, 6.764711380004883, "[TT] Ground Horizontal Sampling of the Laser Transmitter = 140 m"]
-[3.2092247009277344, 2.308570623397827, "[TT] Measurement Category of the Sentinel-2 = Radiation budget, Multi-purpose imagery (land), Vegetation, Albedo and reflectance"]
-[5.650518417358398, 4.983029365539551, "[FF] Data Transmission of the McMurdo Ground Station = Darmstadt"]
-[5.749176502227783, -0.6936137080192566, "[TT] Expected Lifetime of the Moving Mirror = 3 years"]
-[6.928009033203125, -0.6994265913963318, "[FF] Outer Binary Orbit Period of the TYC 7037-89-1 = Roughly every 2,000 years"]
-[10.22216510772705, 5.596550464630127, "[TT] Temperature Fluctuation of the Control System = Less than 0.02 Fahrenheit"]
-[6.226314067840576, 3.311361312866211, "[TT] Cargo Transportation Services Provider of the ISS = NASA"]
-[10.070005416870117, -1.4994720220565796, "[TT] Orbit Inclination of the ResourceSat-2A = 98.78\u00ba"]
-[6.789706230163574, 0.895521342754364, "[TT] Launch Date of the Solar Probe Plus = 2018"]
-[3.3984274864196777, 4.9141845703125, "[FF] SAR Data Acquisition of the X-UGS = Lack of capability to acquire directly SAR data"]
-[4.434269428253174, 5.429687023162842, "[FF] Bstar Drag Term of the GOMX-3 = Historical"]
-[11.336939811706543, 6.038337230682373, "[TT] Capability of the Vega = 1.5 t"]
-[4.240683555603027, 7.239175796508789, "[TT] Frequency Band of the X-band downlink transmitters = X-band"]
-[9.866798400878906, 8.819637298583984, "[TT] FOV of the C-band = 1000 km"]
-[8.16061782836914, 6.616797924041748, "[TT] Number of Instruments of the Advanced Baseline Imager (ABI) = 1"]
-[7.966282844543457, 7.669182777404785, "[FF] Type of the THI (Thermal Hyperspectral Imager) = Relatively large"]
-[6.276423931121826, 5.724615573883057, "[FF] Function of the Hertz Chamber = Assess radio signals from antennas"]
-[6.588623523712158, -2.0469415187835693, "[TT] Launch Date of the Jason-1 = Dec. 07, 2001"]
-[9.382726669311523, 5.336946964263916, "[TT] Inertial Mode Test Period of the MicroSCOPE = Ti = 120 orbits"]
-[4.92021369934082, 2.197751998901367, "[TT] LR status of the NGSLR = Operational"]
-[13.778993606567383, 2.9113361835479736, "[TT] Mass of the Spacecraft = 2.66 kg"]
-[12.04171085357666, -0.4033776819705963, "[TT] Third Year of Mission of the TESS = July 2020 to June 2021"]
-[5.91849422454834, 7.058287620544434, "[TT] Average Data Rate of the SeaWinds = 40 kbit/s"]
-[1.7482999563217163, -2.069249153137207, "[TT] Capsule Drop Location of the Hayabusa-2 = Australian Outback"]
-[3.3841731548309326, 5.011739253997803, "[FF] Design of the L-band SAR = Wide swath, high resolution, full polarimetric"]
-[9.232051849365234, 4.279822826385498, "[TT] Orientation of the Solar Panels = Roll direction of the satellite"]
-[11.192914962768555, 5.92582893371582, "[TT] Foil Material of the Dosimeter B = Nickel"]
-[6.095424652099609, 4.485560417175293, "[FF] Critical Activities of the Spacecraft = Performed in contact with the ground"]
-[8.414616584777832, 2.5688066482543945, "[FF] Function of the Hyper-Angular Rainbow Polarimeter-2 = High-resolution spatial and angular characterization of aerosol and cloud microphysics"]
-[9.38968276977539, 1.482829213142395, "[FF] Observation of the New Horizons = Variations in particle fluxes over a wide range of energies and scales"]
-[4.864417552947998, 1.8303450345993042, "[TT] Operation Status of the CYGNSS = Nominal"]
-[8.382728576660156, 8.276874542236328, "[TT] Multispectral Band: Near-Infrared of the NAOMI = 0.76 \u00b5m - 0.89 \u00b5m"]
-[5.715151786804199, 5.091782093048096, "[TT] Operation of the ROSA = Receives L1 C/A, L1 P(Y) and L2 P(Y) signals from GPS satellites"]
-[6.957036972045898, 6.682339191436768, "[FF] Operational Modes of the MOMA = 1) Heating of the sample to induce evaporation and/or thermochemical decomposition (pyrolysis) and liberate species into the gas phase, possibly also being preceded by a chemical derivatization step to aid in this gas-phase transition, and 2) Direct interrogation of the sample by intense ultraviolet (UV) laser pulses inducing prompt desorption into the gas phase"]
-[6.620276927947998, 5.658438205718994, "[FF] Data Rate of the LCT = Very high"]
-[4.858598709106445, 2.0340640544891357, "[TT] Data Transmission of the Himawari-8/9 Ground Segment = HOPE to JMA"]
-[7.716635704040527, 2.256126880645752, "[FF] Application of the Lidar Instrument = Measuring vegetation canopy height"]
-[9.974974632263184, 4.313767910003662, "[TT] Quantity of the MTQ (Magnetic Torquers) = 3"]
-[5.934572219848633, 2.419316530227661, "[FF] Designers of the CHRIS = M. A. Cutter, D. R. Lobb"]
-[5.786976337432861, 0.5693352818489075, "[TT] Days of data collection of the SASS = 91.0"]
-[7.022833347320557, -0.49637752771377563, "[TT] Local Time on Descending Node of the ASNARO-1 = 11:00 hours"]
-[6.225694179534912, 4.793419361114502, "[FF] Function of the SONATE\u2019s telecommand management = Has a complete second path of command processing for commands originating from ASAP-L"]
-[6.161507606506348, 4.459155082702637, "[FF] Implementation of the PGS = Heterogeneous Mission Access (HMA)"]
-[5.1249589920043945, -0.9591931700706482, "[TT] Launch Date of the Kounotori = August 19, 2015"]
-[9.847250938415527, 4.783615589141846, "[TT] Spin Stabilization of the IMP-8 = 22.3 rpm"]
-[9.40638542175293, 7.286901473999023, "[TT] Spatial Resolution (PAN) of the PP = 2.5 m"]
-[6.9003071784973145, 8.060938835144043, "[TT] Ground Noise Power of the RAX-1 = -110 dBm"]
-[10.38707160949707, 2.242887258529663, "[FF] Spectrum of the Sco X-1 = Soft X-ray"]
-[8.061159133911133, 9.159639358520508, "[FF] Parameter Species Wavelength of the SSUSI = N 2 1085 \u00c5 (N+), N 2 LBH bands"]
-[6.178184986114502, 2.9780526161193848, "[TT] Imaging Frequency of the WorldView Legion satellites = Every 20 to 30 minutes"]
-[5.730727672576904, 6.0077738761901855, "[TT] Device Type of the SIM = Constant-deviation monochromator"]
-[11.77674388885498, 6.706454753875732, "[TT] Ion Energy Range of the EPAM = Ei \u227350 keV"]
-[4.25410795211792, 0.7417079210281372, "[TT] Service Level Agreement Date of the EDRS Space Data Highway = 20 February 2015"]
-[5.673460483551025, 2.7347497940063477, "[TT] Development Partners of the NuSTAR = Danish Technical University and the Italian Space Agency (ASI)"]
-[8.420629501342773, 6.726254463195801, "[FF] Detector Focus of the SHS System = Nearly focused"]
-[4.225697994232178, 7.259411334991455, "[TT] Frequency of the RF communications = X-band"]
-[4.560708045959473, -2.80175518989563, "[TT] Full-polarimetric Capability Frequencies of the PMI = 10.7, 18.7, 37 GHz"]
-[14.293990135192871, 3.1525468826293945, "[TT] S/C Mass (kg) of the F-1 = 450"]
-[9.442315101623535, 5.952828407287598, "[TT] Viewing Angle Range of the POLO data set = -115\u00ba to +115\u00ba"]
-[9.600170135498047, 4.216771125793457, "[TT] Data Transmission of the Magnetometer = Real-time"]
-[5.633565902709961, 7.02347993850708, "[TT] Data Rate of the RAMIS = 10 MB / day"]
-[9.099544525146484, 6.724169731140137, "[FF] Resolution of the GeoEye-1 = Highest in the world"]
-[6.22714376449585, 6.8996782302856445, "[FF] Data Rate of the Instrument = 130 kbit/s"]
-[9.840023040771484, -0.4757806956768036, "[TT] Orbit Altitude of the FREESTAR = 275 km"]
-[7.736660480499268, 9.097570419311523, "[TT] Wavelength of the Nd:YAG master oscillator power amplifier (MOPA) = 1064 nm"]
-[5.924779891967773, -0.39510852098464966, "[TT] Flight Time Before Reentry of the RainCube = No more than twelve months"]
-[10.619451522827148, 5.136938095092773, "[TT] Electron Density Range of the Langmuir Probe = 5 x 10^2 - 10^7 cm^-3"]
-[10.15018367767334, 4.457380294799805, "[TT] Actuation Type of the Canopus Pipper = Magnetic torque coils"]
-[9.702771186828613, 7.283537864685059, "[TT] Ground Resolution of the IIM instrument = 200 m/pixel"]
-[10.38598918914795, 5.8542866706848145, "[TT] Operating Conditions of the Antenna = Ice and snow"]
-[7.672999858856201, 9.121136665344238, "[TT] Wavelength Range of the Band No 2 = 0.70 \u00b1 0.2 - 1.10 \u00b1 0.2 \u00b5m"]
-[6.649742126464844, -0.5608974099159241, "[TT] TLE Generation of the Orbit Dynamic System = By mean processing of a 6 lap orbit"]
-[7.937428951263428, 4.948323726654053, "[FF] Changes in Field Strength of the Oersted = Mostly negative and ranges up to almost 10% of the total field"]
-[8.13405704498291, 8.220173835754395, "[TT] Spectral Ranges of the Imager Filter Wheel = 4.3 to 5.15 \u00b5m and 5.4 to 6.0 \u00b5m"]
-[5.746824264526367, 0.9998412728309631, "[FF] International Astronautical Congress Date of the BepiColombo = Sept. 29-Oct. 3, 2014"]
-[8.116657257080078, 1.3257677555084229, "[FF] Measurement Coverage of the SMAP = Global land area, excluding regions of snow and ice, mountainous topography, open water, and areas of extremely dense vegetation such as tropical forests"]
-[8.701866149902344, 6.796765327453613, "[TT] Imaging Capacity of the RapidEye = 5 million km2 per day"]
-[6.3802642822265625, 0.8420631885528564, "[FF] Monitoring Duration of the NASA = Several decades"]
-[5.672488212585449, 5.599964141845703, "[TT] Processor Type of the SES-17 = Digital transparent processor (DTP)"]
-[7.979776859283447, 2.4622130393981934, "[FF] Data Usage of the GIIRS = Atmospheric temperature profiles, cloud top height and temperature, sea surface temperature, specific humidity profiles, integrated water vapor measurements, cloud cover maps, land surface temperature, horizontal winds, total column ozone, and cloud type discrimination"]
-[9.889080047607422, 0.7181481122970581, "[TT] Autonomous Abort Response Distance of the ASTRO = 120 m"]
-[13.211933135986328, 5.223454475402832, "[TT] Size of the Solar Panels = 320 mm x 320 mm"]
-[6.167330265045166, 4.614466667175293, "[FF] Ground Contacts Interval of the Intelligent Failure Detection, Isolation and Recovery System = Up to 14th interval"]
-[10.376812934875488, 4.02667236328125, "[TT] Boom Length of the Spacecraft = 10.6 m"]
-[7.558627128601074, 1.9988620281219482, "[FF] Product of the Sustainability Tech = Satellite-connected sensors that monitor wetland hydrology"]
-[6.214634895324707, 1.7667609453201294, "[FF] URL of the SWOT = http://smsc.cnes.fr/SWOT/"]
-[5.163850784301758, 7.04205322265625, "[TT] Downlink Speed of the Communication links = 9.6 - 38.4 kbit/s"]
-[7.910501003265381, 9.160262107849121, "[TT] Wavelength of the LORE = 350 nm"]
-[7.243197441101074, 6.724960803985596, "[TT] Transfer Time from CSAR to TR of the LD Output = About 1 min"]
-[5.396461009979248, 2.622037649154663, "[FF] Structure of the CXBN-2 = Robust 2-wall structure matched to a central mounting block"]
-[11.411620140075684, 4.333829402923584, "[TT] Size of the ELFIN = 3U"]
-[10.300474166870117, -1.1934125423431396, "[TT] Orbit Inclination of the BlackSky microsatellite = 42\u00b0"]
-[2.337174892425537, 1.320191502571106, "[FF] Beacon Transmissions of the NanoSail-D2 = Ongoing"]
-[10.56882381439209, 3.9426283836364746, "[FF] Steps of the Deployment Sequence = 1) Prior to launch, the inflatable tubes and the membrane are placed into the hold structure"]
-[3.9343600273132324, 6.386097431182861, "[TT] No of Beams of the Antenna = 2"]
-[13.876575469970703, 5.705337047576904, "[TT] Solar Cells Power Conversion Efficiency of the EPS = 27%"]
-[6.289436340332031, 1.7145404815673828, "[FF] URL of the ISEE-1 and ISEE-2 = http://www.ann-geophys.net/25/2633/2007/angeo-25-2633-2007.pdf"]
-[3.4081811904907227, 2.0189497470855713, "[FF] Calibration Approach of the Sentinel-1 = In-orbit"]
-[11.644237518310547, 3.404862403869629, "[TT] Ion Thrusters of the Resurs-O1 spacecraft = Propulsion"]
-[7.582658767700195, 5.355216026306152, "[FF] Interface of the Tertiary Collimator Assembly = Optically and mechanically interfaces with the FOA"]
-[13.345392227172852, 7.3766913414001465, "[TT] Power of the TWTA = 20 W"]
-[14.062477111816406, 3.3667726516723633, "[TT] Mass of the Myriad RF board = 50 g"]
-[4.393951892852783, 5.165279865264893, "[TT] Types of the Cospas-Sarsat Beacons = Personal Locator Beacons (PLBs), Emergency Position Indicating Radio Beacons (EPIRBs), Emergency Locator Transmitters (ELTs)"]
-[10.523754119873047, 1.4573299884796143, "[TT] Number of Stars of the Lower Centaurus Crux = 97"]
-[14.63209056854248, 6.736417770385742, "[TT] Battery unit of the EPS = 8 series NiMH (750 mAh, 9.6V)"]
-[7.861082553863525, 7.233476638793945, "[TT] Maximum Frame Rate of the PamCam = Up to 27 images per second"]
-[9.386215209960938, 6.660826206207275, "[TT] Compression Ratio of the KazEOSat-2 = 2.5:1"]
-[5.023408889770508, 2.9944140911102295, "[TT] Agency of the SVOM = CNES, CNSA"]
-[4.515687942504883, 4.656407833099365, "[FF] Capability of the Unseenlabs\u2019 maritime monitoring system = Monitor three different areas of interest simultaneously"]
-[5.6410369873046875, 3.7266764640808105, "[TT] Total Impulse of the SkySat-5 = 150 Ns"]
-[5.074974536895752, 0.7245339751243591, "[FF] Launch Date of the ISILaunch19 = June 23, 2017"]
-[4.9386515617370605, -2.1465492248535156, "[TT] Combined Weight of the Tiangong = Nearly 70 metric tons"]
-[7.8096604347229, 4.657353401184082, "[FF] Function of the \u00b5ASC = Output the relative state of the target spacecraft to be referenced in inertial coordinates"]
-[10.654973983764648, 2.9100513458251953, "[TT] Photometer Resolution of the Nanosatellite = 26.52 arcsec/pixel"]
-[4.32135534286499, 0.8071426153182983, "[FF] Operational Date of the EDRS = July 12, 2012"]
-[7.491424560546875, 6.412685871124268, "[TT] Refractivity Profile Comparison Time of the GNOS Instrument = Within 1 hour"]
-[10.23189640045166, 1.9561198949813843, "[TT] Imaging Survey of the eROSITA = First ever true imaging survey of the sky in the hard band (2-8 keV)"]
-[9.883054733276367, 8.963796615600586, "[TT] IFOV of the IR channels = 2 km (vertical) x 13 km (horizontal)"]
-[7.362596035003662, 4.812923908233643, "[FF] Secondary Instrument of the PACE = Possibly included"]
-[10.188286781311035, 5.424172878265381, "[TT] Problem of the ABI = Foreign object debris blocking the flow of the coolant"]
-[12.621955871582031, 9.100326538085938, "[TT] ECT (Equatorial Crossing Time) of the WV-1 = 1330 hours"]
-[6.46636962890625, 4.581186771392822, "[FF] Operation of the Cluster 3 = RF data analytics"]
-[5.770188808441162, 7.171750068664551, "[TT] Data Rate Threshold of the PDHS = 640 Mbit/s"]
-[14.640613555908203, 6.631899833679199, "[TT] Battery Capacity of the MTM = 12 Ah"]
-[5.836192607879639, 3.7349774837493896, "[FF] Partnership with Spire Global of the Myriota = Myriota will use Spire's constellation of smallsats to expand its network"]
-[5.056833267211914, 8.300896644592285, "[TT] Surface Acoustic Wave Generator Bandwidth of the Poseidon-1 = 300 MHz"]
-[6.171801567077637, 7.806497573852539, "[TT] Number of Channels of the OBP (Onboard Processor) = 500"]
-[6.541469097137451, 3.2701544761657715, "[FF] Link of the WINDS Satellite = Disaster Countermeasure Activities"]
-[5.521385669708252, 6.452324867248535, "[TT] Storage Capacity of the PLCDHS = 2 GByte"]
-[4.561673641204834, 7.873764991760254, "[TT] UHF Band Frequency of the RF Communications = 430 MHz"]
-[5.626884937286377, 1.1540539264678955, "[FF] Presentation Date of the Jaan Praks = Sept. 22-24, 2014"]
-[5.789831161499023, 2.286808729171753, "[FF] Operational of the USAF Environmental Satellite = Yes"]
-[8.255054473876953, 4.484682559967041, "[FF] Detection Type of the ASTERIA = Marginal"]
-[6.096909999847412, 2.3812167644500732, "[TT] Emergency Abort Capability of the Orion = Yes"]
-[6.712208271026611, 4.525096416473389, "[FF] Recovery Levels of the FDIR System = L0: Action None (Unit Level Local recovery), L1:Unit/Function Recovery (Recovery by FDIR), L2: Unit/Function Reconfiguration (Unit substitution by FDIR), L3: OBC / System Recovery (Safe orbit entered & System Mode to MANUAL), L4: CAM (Drifting orbit entered & System Mode to MANUAL)"]
-[5.327971458435059, 0.9094288945198059, "[FF] Mission Accomplished Date of the CanX-4 & CanX-5 = Nov. 5, 2014"]
-[6.844500541687012, 4.598723888397217, "[FF] Function of the MVP module = Holds the foam insert and slots for two MICS cement packets"]
-[4.841025352478027, 1.4198753833770752, "[FF] First Signal Reception Date of the Gokturk-2 = Dec. 18, 2012"]
-[4.949963092803955, 8.129342079162598, "[TT] Frequency Range of the WBSAAMD = Higher"]
-[9.858013153076172, 8.711444854736328, "[TT] IFOV of the InSb = 42.5 \u00b5rad"]
-[13.399837493896484, 7.23276948928833, "[TT] Peak Power Collection of the ABEX = 122 W"]
-[7.545459270477295, -0.6744314432144165, "[TT] Launch Date of the ICEYE-X1 = January, 2018"]
-[9.295045852661133, 2.7844135761260986, "[TT] Solar Wind Speed and Beta of the ACE = ~11% lower on average from 2009 through the day 79 of 2013"]
-[6.482457160949707, 3.3073601722717285, "[FF] Attachment of the USS-02 = Space Shuttle Orbiter"]
-[14.073277473449707, 4.003530979156494, "[TT] Instrument Mass of the MWHS-II = 60 kg"]
-[9.34860897064209, 6.582396984100342, "[FF] Angular Resolution of the IMAP-Ultra = Comparable or better angular resolution than IMAP-Hi"]
-[14.27121353149414, 3.2617621421813965, "[TT] Mass of the PISAT = 5.3 kg"]
-[8.846124649047852, 5.637575626373291, "[TT] Position Accuracy of the PROBA-2 = 200 m (2\u03c3) on each axis"]
-[5.281853199005127, 1.3759839534759521, "[TT] Mission Operations Extension of the SMOS = Until 2017"]
-[4.319196701049805, 2.4085183143615723, "[TT] Mounting of the ATLAS Sensor = Spacelab pallet(s)"]
-[10.798717498779297, 2.122819185256958, "[FF] Detection Band of the XMM-Newton = Low energy part of the X-ray band"]
-[5.629585266113281, 4.79777717590332, "[TT] Constellation of the EDRS = Two geostationary data relay satellites"]
-[5.451263427734375, 1.9116463661193848, "[TT] Health Diagnostics Data Transmission of the ABEX = Before the inbound VAB crossing"]
-[11.138748168945312, 5.4008331298828125, "[TT] Number of Scintillating Fibers of the Imaging Calorimeter = 448"]
-[7.851983070373535, 1.200742483139038, "[FF] Anticipate Poor Yields of the Farmers = Yes"]
-[8.767841339111328, 4.076928615570068, "[FF] Detects of the STD = The trajectory of the incoming particles and identifies the magnitude and polarity of the particles\u2019 electrical charge"]
-[8.963728904724121, 4.5290985107421875, "[TT] Quantity of the Fine Solar Sensors = 3"]
-[8.493834495544434, 5.600052833557129, "[TT] Altitude Accuracy of the GPSDR = < 10 cm"]
-[8.293760299682617, 5.2848896980285645, "[FF] Orbit Accuracy of the DORIS-DIODE = Ten Centimeters"]
-[4.033650875091553, 6.953663349151611, "[TT] X-band antenna of the TT&C = 1"]
-[5.87321662902832, 3.345341205596924, "[FF] Number of Flights of the SEDS = Two"]
-[5.3962273597717285, 8.711783409118652, "[TT] Bandwidth of the M1 = 0.02 \u00b5m"]
-[9.816152572631836, 8.59849739074707, "[TT] IFOV of the CATS = Four"]
-[9.08332633972168, 1.365708351135254, "[TT] Launch Year of the Voyager 2 = 1977"]
-[7.440442085266113, 2.2929224967956543, "[FF] Data Integration of the MODIS instruments = Vegetation indices"]
-[6.717504978179932, -1.7133485078811646, "[TT] Operational Orbit of the Jason-1 = Exact repeat ground track every 127 revolutions in ten days"]
-[3.9933712482452393, 2.1804473400115967, "[TT] Launch Vehicle of the Lucy = Atlas V 401 rocket"]
-[6.832351207733154, 4.08909797668457, "[FF] Baseline of the KaRIn = Unknown"]
-[11.494622230529785, 4.703187465667725, "[TT] Primary Cube Structure Side Length of the COMMx = 0.93 m"]
-[6.770442485809326, -0.3000788986682892, "[TT] Updated Period of the \u00d8rsted satellite = 99.7 minutes"]
-[7.006765365600586, 7.1356401443481445, "[TT] Pulse Width of the Laser = 1~999 \u00b5s"]
-[5.231252670288086, 7.266055107116699, "[TT] Data Rate of the Transmitter = 100 Mbit/s"]
-[8.593287467956543, 1.416251540184021, "[TT] Measurement Error of the Aquarius = Less than 0.2 PSU"]
-[7.229400634765625, 6.463645935058594, "[TT] Distance Metrology of the Satellite Pairs = Laser-based"]
-[5.5825371742248535, 7.9949951171875, "[TT] Oscillation Amplitude of the CVX-1 = < 0.01 mm"]
-[9.360156059265137, 6.064371109008789, "[TT] Elevation Threshold of the CBR = 20\u00b0"]
-[4.263772964477539, 7.255276203155518, "[TT] Signal Frequency of the Ground Station Antenna System = 1.2 GHz or 720 MHz"]
-[6.768925666809082, 4.010970115661621, "[TT] Location of the ISS-EMIT = Onboard the International Space Station\u2019s (ISS) primary forward-facing hub for externally mounted instruments"]
-[4.931539058685303, 7.989633083343506, "[TT] Frequency of the OCXO = 222 Hz"]
-[8.448704719543457, 8.015307426452637, "[TT] Spectral Band (MS B3) of the Pushbroom imager = 0.62-0.69 \u00b5m"]
-[8.847455978393555, 9.521492004394531, "[FF] Band 5 Spectral Range of the TANSO-FTS-2 = 8.45 - 14.29 \u00b5m"]
-[7.4086995124816895, 5.117961883544922, "[FF] Design and Performance of the ILAS-II = Unknown"]
-[8.90160846710205, -0.34544339776039124, "[TT] Orbit Inclination of the Meteor-M2 = 98.8\u00ba"]
-[10.283062934875488, 7.332335472106934, "[FF] Telescope Mirrors of the Sentinel-2 MSI = Manufacturing, testing and alignment"]
-[7.970346450805664, 5.269102573394775, "[FF] Calibration Parameter of the LUIS = Signal to noise ratio, linearity, saturation and uniformity of radiometric response"]
-[6.479312419891357, 3.756622314453125, "[FF] Standards of the Data Processing Chain = OGC (Open Geospatial Consortium) standards, EO GML meta data, OGC WPS, ESA's Generic Interface for Instrument Data Processing"]
-[6.343108177185059, -1.3121899366378784, "[FF] Mission Date of the GRACE = 21 Dec. 2017"]
-[7.838968276977539, 2.831226110458374, "[FF] Air Pollution Observation of the GOSAT = December 2016"]
-[5.828275680541992, -0.8519287705421448, "[TT] Spacecraft Design Life of the QuickBird-2 = 5 years"]
-[3.759528160095215, 4.663458824157715, "[TT] Number of Phase Centers of the RADARSAT-2 = 3"]
-[9.806377410888672, 3.731311798095703, "[TT] Attitude Determination Accuracy of the X-ray Telescope = 0.5\u00ba"]
-[6.747420787811279, 8.377694129943848, "[FF] New spectral channels of the OLCI = Implemented in OLCI"]
-[11.574155807495117, 3.3881995677948, "[TT] Propulsion System of the MASCOT = None"]
-[10.222860336303711, 5.297443389892578, "[FF] Function of the Fridge = Provide cold stowage facility capability on-orbit"]
-[13.654497146606445, 7.149456024169922, "[TT] Peak Power of the ECS = 66W (allocated), 34W (measured @ 30\u00baC) at 28V"]
-[10.127315521240234, 7.849954128265381, "[TT] Telescope of the Tyvak-0130 = One with a narrow field of view"]
-[13.317269325256348, 7.736640930175781, "[TT] Power Output of the Tracking Receiver and Low Noise Amplifiers = 10.6 W"]
-[5.456282615661621, 6.4340057373046875, "[TT] Onboard Data Storage Capacity of the DTS = 128 Gbit"]
-[12.022610664367676, 4.608110427856445, "[TT] Dimensions of the Large Space Simulator = 15m high by 10m wide"]
-[9.678032875061035, 6.914552688598633, "[TT] Spatial Resolution of the SSM/T-2 = About 48 km"]
-[8.607593536376953, 8.635878562927246, "[FF] Proto-Flight Model Components of the Prism Spectrometer = Entrance slit assembly, front-side optical system, dispersing assembly and back-side optical system"]
-[4.81266450881958, 0.7608500719070435, "[FF] Date of the GOES-R Series Program SIR = July 22\u201324, 2014"]
-[4.764043807983398, -1.2409040927886963, "[TT] De-orbit Date of the Tiangong-2 = July 2019"]
-[7.027044773101807, 5.262703895568848, "[FF] Components of the TESIS = TESIS-BD, TESIS-BE, TESIS-OD"]
-[4.258660316467285, 1.0119645595550537, "[FF] Release Date of the Argos-3 = May 24, 2005"]
-[11.008647918701172, 6.161417007446289, "[FF] External Surface Coating of the Receiver Housing = Gold"]
-[9.816041946411133, 7.806164741516113, "[TT] Turnaround Time of the Telescope = +0.2 s"]
-[4.075538158416748, 2.1361589431762695, "[TT] Launch Cost Savings of the ORS-6 = 25-50%"]
-[4.012146949768066, 1.6064447164535522, "[TT] Launch Failure Cause of the Global-9 = Anomaly in the second stage of the launch vehicle"]
-[4.741633415222168, -1.2556289434432983, "[TT] Launch Year of the Beijing-1 = 2005"]
-[6.767544746398926, 3.844594955444336, "[FF] Purpose of the SEXTANT = Realizable in a single package with NICER"]
-[4.875550270080566, 7.330117225646973, "[TT] Downlink Rate of the RF communications system = 1 kbit/s"]
-[8.684895515441895, 0.1401555836200714, "[TT] Large Lobe Dimensions of the Comet = 4.1 x 3.3 x 1.8 km"]
-[6.28659725189209, -1.2303903102874756, "[TT] Operation Period of the GRACE = 2002 to 2017"]
-[11.927803039550781, 4.981253147125244, "[TT] Size of the TRM (T/R Module) = 170 mm x 70 mm x 20 mm"]
-[10.313949584960938, 5.744382858276367, "[TT] NE\u0394T @ specified scene temperature of the Instrument = 0.15-0.4 K @ 250 K"]
-[6.513949871063232, 5.602035045623779, "[TT] Type of the Linear Encoder = Non-contacting"]
-[10.169357299804688, 1.3629339933395386, "[TT] Previous Catalogue Distance Limit of the Gaia Catalogue of Nearby Stars = 82 light years"]
-[8.858808517456055, 8.109989166259766, "[TT] Mass Reduction of the Overall Optical Train = About 30%"]
-[11.648603439331055, 4.595581531524658, "[FF] Shape of the Van Allen Belts = Doughnut-shaped"]
-[9.862629890441895, -0.7168719172477722, "[TT] Orbital altitude of the GALILEO = 23,222 km"]
-[12.419439315795898, 0.6178011894226074, "[TT] Field of View of the PLATO = 2232\u00ba x 2232\u00ba"]
-[4.568298816680908, 2.854252338409424, "[TT] Subsidiary Location of the Spacety = Luxembourg"]
-[5.752516269683838, 2.7182252407073975, "[FF] Partnership of the Webb = European Space Agency ESA, US space agency NASA, and the Canadian Space Agency CSA"]
-[5.721332550048828, -0.8627007007598877, "[TT] Design Life of the ACRIMSat = 5 years"]
-[14.217638969421387, 3.151611566543579, "[TT] Mass of the CATS = 494 kg"]
-[8.334177017211914, 3.531979560852051, "[FF] Objective of the GFSE = To demonstrate in space a gas flow control and sensing principle"]
-[9.871746063232422, 6.964346408843994, "[TT] Resolution of the Limited coverage = 0.6 km"]
-[13.361879348754883, 7.341371059417725, "[TT] Power of the Power = 275 W"]
-[5.9601240158081055, 4.165500164031982, "[FF] Service Infrastructure of the Airbus Defence and Space = Commercial data exploitation and customer interfaces"]
-[7.218404769897461, 5.0216875076293945, "[TT] Safety Criterion of the EO-1 = The six-second tolerance"]
-[6.852273464202881, 8.963340759277344, "[TT] Bandwidth of the POLDER = 20 nm"]
-[6.508957862854004, 1.7961798906326294, "[TT] Survey Sensitivity of the eROSITA = Unprecedented"]
-[11.881596565246582, 3.0158438682556152, "[TT] Total \u0394V of the Deorbit = 55 m/s"]
-[10.150205612182617, 10.010662078857422, "[FF] Maiden Flight Date of the Vega = Feb. 13, 2012"]
-[8.421731948852539, 5.620509147644043, "[TT] Positioning Accuracy of the GPS Receiver = < 1m"]
-[4.636358737945557, 7.35132360458374, "[TT] S-band 1Mbit/s Downlink Data Rate Range of the UoSAT-12 = 1 Mbit/s - 64 kbit/s"]
-[12.075955390930176, 6.318521022796631, "[FF] Positron Flux of the AMS = Higher than the rate for electrons"]
-[5.274990558624268, 1.596566081047058, "[FF] Mission Status of the TET-1 = On-Orbit Verification"]
-[11.826665878295898, 3.1222171783447266, "[TT] Total \u0394V of the CanX-4&5 = 14 m/s"]
-[4.536148548126221, -0.807990550994873, "[FF] Purpose of the SpaceX Crew Dragon = Transporting astronauts to and from the International Space Station"]
-[10.772195816040039, 1.0627880096435547, "[TT] Star Type of the TOI 700 d = M dwarf"]
-[5.180026054382324, 0.6992442011833191, "[TT] Delivery Date of the EXIS = September"]
-[5.081653594970703, 8.330337524414062, "[TT] Bandwidth of the Total RF bandwidth = 1800 MHz"]
-[5.898473262786865, 1.4313604831695557, "[FF] Conference Date of the MTG Satellites = June 10 - 14, 2013"]
-[5.470945835113525, 8.501951217651367, "[TT] Channel Spacing of the MDD = 31.2 kHz"]
-[7.925161361694336, 8.958578109741211, "[TT] Wavelength of the SWIR = 0.1 \u00b5m"]
-[12.706745147705078, 3.898442268371582, "[TT] Observation of the Cluster = Magnetic Reconnection Events"]
-[5.672002792358398, -0.9328697323799133, "[TT] Design Cycle Count of the HISat and PACs = Over 80 times during the last three years"]
-[5.343346118927002, 7.6046624183654785, "[FF] Transmit Signal Distribution of the EPDN (Elevation Power Dividing Networks) = Distributes low power transmit signal pulses to T/R modules"]
-[7.612740993499756, -2.330352306365967, "[FF] URL of the GOLD = https://gold.cs.ucf.edu"]
-[5.127446174621582, 1.065407633781433, "[TT] Launch Date of the NPOESS = 2009"]
-[7.437036514282227, 0.9384143948554993, "[FF] Mission of the Lunar Reconnaissance Orbiter = LRO mission"]
-[2.9007163047790527, 4.471429347991943, "[TT] Beams of the PALSAR-2 = 116"]
-[6.560318470001221, 7.664208889007568, "[TT] Data Quantization of the Imager = 10 bit"]
-[12.234591484069824, 4.81369161605835, "[TT] Size of the TREX-823 X-band transmitter = 9 cm x 31 cm x 8 cm"]
-[6.509509563446045, 2.045109748840332, "[FF] URL of the ACTS 118x = http://acts.grc.nasa.gov/docs/5thKa_Ivancic_etal.pdf"]
-[6.3338704109191895, -1.2848149538040161, "[FF] Operation Review Date of the Grace Mission = June 30, 2011"]
-[7.668155670166016, 1.2365005016326904, "[FF] Symposium Date of the WatER = March 13-16, 2006"]
-[7.462978363037109, 8.510869979858398, "[FF] Amplitude Spectral Density of the DOSS system = Measured"]
-[7.857889175415039, 0.8170294165611267, "[FF] Lunar gravity field detection of the Kaguya (SELENE) = Unknown"]
-[8.27733325958252, 7.466085433959961, "[TT] Detector Type of the SSULI = Imaging microplate detector with a wedge and strip anode"]
-[8.965373992919922, 4.407065391540527, "[TT] Sun Aspect Sensors of the ERG = 2"]
-[3.9953958988189697, 5.028240203857422, "[TT] Power Consumption of the Cospas-Sarsat search and rescue package = 3% of onboard power"]
-[6.010437488555908, 5.105506896972656, "[FF] Components of the ROSA = GPS receiver for RO (Radio Occultation), Velocity & anti-velocity antenna assembly, POD (Precise Orbit Determination) antenna, RF cables"]
-[6.854762554168701, 2.2676684856414795, "[FF] URL of the China High-resolution Earth Observation System (CHEOS) = http://www.nasaspaceflight.com/2013/04/china-back-in-action-long-march-2d-gaofen-1/"]
-[7.974350452423096, 7.9201226234436035, "[TT] Radiometric Resolution of the HSC-III optics subsystem = 10 bits"]
-[12.091911315917969, 6.3447184562683105, "[TT] Positron Flux Measurement of the AMS-02 = Up to 500 GeV"]
-[5.072915077209473, 1.8305937051773071, "[TT] Mission Status of the Odin = Operational (extended)"]
-[13.752148628234863, 5.389086723327637, "[TT] Type of the Solar Cells = Improved triple junction cell, ultra triple junction cell"]
-[3.7174582481384277, 6.443256378173828, "[TT] Antenna Polarization of the NSCAT = 6 V, 2 H"]
-[4.006750583648682, 2.1865358352661133, "[TT] Launch Vehicle of the STARE-A = Atlas-5-411"]
-[4.654237747192383, 7.460153579711914, "[FF] Operating Frequencies of the NorAIS-2 Receiver = Set to any frequency within the maritime VHF band"]
-[6.931169033050537, 7.146506309509277, "[TT] Repetition Rate of the Micropulse Laser Transmitter = 10 kHz"]
-[8.307019233703613, 3.192692279815674, "[FF] Measurement of the Improved Limb Atmospheric Spectrometer (ILAS) = Upper atmosphere\u2019s gaseous composition"]
-[7.30595064163208, 4.88775110244751, "[FF] O2 A-band of the IAPCAS/SIF = Within the O2 A-band"]
-[7.123047828674316, 6.635434627532959, "[FF] Event Detection Thresholds of the GLM = Unknown"]
-[8.900511741638184, 4.868670463562012, "[TT] Type of the Honeywell QA-2000 Accelerometer = Commercial-grade"]
-[5.5699920654296875, 0.2670407295227051, "[TT] Mission Status of the ISS-RapidScat = Mission complete"]
-[5.176486015319824, 8.399067878723145, "[TT] Tx Bandwidth of the KaRIn = 200 MHz"]
-[5.607672691345215, 0.41344597935676575, "[TT] Operation Start Date of the Cluster = 1 September 2000"]
-[11.75165843963623, 3.263585329055786, "[TT] Specific Impulse of the NanoPS = 500-1000 m/s"]
-[3.6530189514160156, 6.351691246032715, "[TT] Diameter of the Ground Station = 5 m"]
-[7.810812950134277, 1.9821386337280273, "[FF] Mission Objectives of the SeaSat-A = Global monitoring of oceanographic phenomena and features, provision of oceanographic data, demonstration of key features of an operational ocean dynamics monitoring system"]
-[10.41644287109375, 1.8349560499191284, "[FF] Imaging of the NuSTAR = Cosmic clumpy doughnut around a black hole"]
-[6.13288688659668, 1.3160977363586426, "[FF] Mission Presentation Date of the Deep Space Atomic Clock = Oct. 29- Nov. 2, 2012"]
-[5.794206619262695, 3.831010580062866, "[FF] Volume Number of the Satellite = 15"]
-[12.069066047668457, 4.626084327697754, "[TT] Wide Area Image Dimensions of the Satellite = 100 km x 34 km"]
-[13.74274730682373, 7.007987022399902, "[TT] Power Supply Backup of the G-EPS = 75%"]
-[7.675217628479004, 0.4635845422744751, "[TT] Mission Lead of the Lunar IceCube = Morehead State University in Morehead, Kentucky"]
-[14.048029899597168, 3.054899215698242, "[TT] Mass of the Eaglet-1 = 5 kg"]
-[3.3209705352783203, 5.6667160987854, "[TT] Number of Radiation Elements of the L-band SAR antenna = 1,080"]
-[6.135796546936035, -0.6199131608009338, "[TT] Initial Mission Checkout Duration of the ADEOS = 90 days"]
-[7.063720226287842, 4.566364288330078, "[FF] Operational Modes of the Spacecraft = Initial, Nominal, Scientific, Observation, Safe"]
-[9.804715156555176, 7.12406587600708, "[TT] Ground Resolution of the GeoCARB = 5 to 10 km"]
-[9.131253242492676, 0.18619906902313232, "[TT] Embankment Length of the Ataturk Dam = 1,820 m"]
-[11.228838920593262, 5.792531490325928, "[FF] Material of the MFCBS = New materials"]
-[8.034496307373047, 1.8373838663101196, "[FF] Uncertainty of the Evapotranspiration = 0.5 mm per year"]
-[3.1555395126342773, 2.2367141246795654, "[FF] Mission Objective of the Copernicus Sentinel-6 = Monitor sea-level change"]
-[7.0447516441345215, 0.138935849070549, "[TT] Existence Period of the Ichthyosaurs = 250 and 90 million years ago"]
-[6.237504959106445, 4.809369087219238, "[FF] Data Utilization and Applications Program of the RCM = Provides technical assistance to federal departments to upgrade their applications and develop new ones exploiting data generated by the RCM"]
-[9.545796394348145, 7.220032215118408, "[TT] Spatial Resolution of the VIS = 400 m (at nadir)"]
-[4.7776360511779785, 7.931347846984863, "[TT] Frequency (MHz) of the GLONASS L1 OC = 1575.42"]
-[9.254703521728516, 3.1913414001464844, "[FF] Observation Purpose of the SWFO-L1 = Continuous unobstructed observation of the corona"]
-[4.765362739562988, 0.41986316442489624, "[TT] Testing Start Date of the Prichal = Early October 2021"]
-[11.776176452636719, 6.536422252655029, "[TT] Gamma-ray Energy Range of the MGNS = 300 keV to 10 MeV"]
-[5.66220235824585, 2.823375701904297, "[TT] Agency of the GPIM = NASA, USAF"]
-[6.521139621734619, 3.8824312686920166, "[FF] Affiliation of the MetOp-3 = Not formally part of IJPS"]
-[10.198187828063965, 5.3689985275268555, "[TT] Thermal Control of the LARES = None"]
-[6.9256720542907715, -0.6843246221542358, "[TT] Primary Orbit Period of the Didymos = 11.9 hours"]
-[11.848786354064941, 6.697636604309082, "[TT] Final Energy Ef of the GEMS = 900 eV"]
-[7.1401686668396, 6.881880283355713, "[TT] Alignment of the Laser frequency stabilization subsystem = 100 \u00b5rad"]
-[7.720487594604492, -0.04727998375892639, "[TT] New Landing Site of the Philae lander = Abydos"]
-[11.918840408325195, 5.420377731323242, "[TT] Dimensions of the Instrument = 120 mm x 300 mm x 250 mm"]
-[4.436515808105469, 7.593925476074219, "[FF] Frequency Bands of the IMI = L/S/C"]
-[7.168262481689453, 2.4594757556915283, "[FF] Potential Evaluation of the Indian Remote Sensing Satellite = \"Potential of High-resolution Indian Remote Sensing Satellite Imagery for Large Scale Mapping\""]
-[7.104794025421143, 4.844074726104736, "[FF] Unknown of the FEE Power Convertors = Unknown"]
-[8.631845474243164, 8.595664978027344, "[TT] Microshutter Arrays of the NIRSpec = More than 200 spectra"]
-[7.4256591796875, 8.783096313476562, "[TT] Passband of the Instrument = 4 nm"]
-[11.14047908782959, 6.234431266784668, "[TT] Temperature of the Proton Component Measurement Range of the DSCOVR = 40,000 \u2013 2,000,000 Kelvin"]
-[8.086549758911133, 6.45192289352417, "[FF] Unknown of the JSS Multispectral Imagers = Unknown"]
-[11.640430450439453, 4.712586879730225, "[TT] Structure Dimensions of the FormoSat-2 = 1.6 m side length, 2.4 m in height"]
-[6.5418701171875, 4.130218505859375, "[FF] Payload of the MetOp Second Generation = Unknown"]
-[3.1766889095306396, 1.649659276008606, "[TT] NRT Data Freshness of the Sentinel-6 = Not older than 3 hours"]
-[6.895964622497559, 4.853305816650391, "[FF] Function of the PIU = Provides the connection to the JEM-EF"]
-[10.802099227905273, 7.480857849121094, "[TT] Swath of the TANSO-CAI-2 = 1000 km"]
-[8.819021224975586, 5.885904788970947, "[TT] Pointing Accuracy of the Primary Imaging Sensor = Within 0.01 degree"]
-[11.557994842529297, 4.79626989364624, "[TT] Width of the Conical Octagon Structure = 1.5 m at the bottom to 2.2 m at the top"]
-[8.89877986907959, 8.532733917236328, "[TT] Instrument size of the Spectrometer = 71 cm x 88 cm x 94 cm"]
-[5.198758125305176, 7.97587776184082, "[TT] Primary Structure Stiffness of the COMMx = 50 Hz"]
-[5.187267780303955, 2.1595993041992188, "[TT] Mission Status of the PhoneSat-1 and -2 = Mission complete"]
-[9.580544471740723, 1.2172907590866089, "[TT] Velocity Change of the Solar System = 0.23 nm/s2"]
-[6.926646709442139, 1.0379890203475952, "[TT] Launch Date of the Mars 2020 rover = July 2020"]
-[9.279714584350586, 4.850049018859863, "[FF] Role of the IMU = Determine initial attitude at de-boost"]
-[8.03937816619873, 5.155392646789551, "[FF] Required Precision of the AAOD = 0.03"]
-[9.644532203674316, 0.4277215301990509, "[TT] Orbit Extent of the Observatories = Close to Earth to just beyond the moon's orbit"]
-[6.131227493286133, -0.38381633162498474, "[TT] Fuel Endurance of the Wind = Until 2074"]
-[9.893744468688965, -0.37207651138305664, "[TT] Altitude Range of the RAIDS = 75-220 km"]
-[18.665813446044922, 3.935445547103882, "[TT] NE\u0394T (K) of the ICI-2 = 0.7"]
-[9.379319190979004, -0.45046645402908325, "[TT] Orbit Altitude of the Tianhe = 370 kilometers"]
-[6.291497707366943, 0.35415196418762207, "[TT] Revisit Time of the ROSE-L = Three or six days"]
-[5.29935884475708, 6.887556076049805, "[FF] Bandwidth Impact of the Telemetry = Limited"]
-[8.57707691192627, 1.4563040733337402, "[TT] Scatterometer Objective of the Aquarius = Measure the surface roughness"]
-[4.919044494628906, 2.8993093967437744, "[TT] Heritage of the LET = SOHO/ERNE"]
-[3.066981792449951, 2.3353161811828613, "[TT] Radar Antenna Length of the Copernicus Sentinel-1C = 12 m"]
-[8.337646484375, 7.64834451675415, "[TT] Sensor System of the EPI-Hi = Ion-implanted silicon SSDs"]
-[6.64545202255249, 5.262072563171387, "[TT] Delivery System Type of the PONDS = Passive"]
-[9.460885047912598, 4.035348892211914, "[TT] Mission Status of the Fluxgate magnetometer = Complete"]
-[13.473690032958984, 2.847727060317993, "[TT] Mass of the Satellite = 2500 kg"]
-[12.0208740234375, 6.303461074829102, "[FF] Purpose of the PAMELA = Measurement of positron-to-electron ratio"]
-[9.073125839233398, 7.3215813636779785, "[TT] Panchromatic Imagery Resolution of the Raytheon imagers = 30 cm"]
-[5.611746311187744, 4.8313069343566895, "[FF] Design of the Mobile Station = Move to an adequate atmospheric condition area"]
-[11.562566757202148, 4.562097072601318, "[TT] Overall Length of the GSLV-F05 = 49.1 m"]
-[11.589717864990234, 4.752081871032715, "[TT] Crevice Length of the Philae = 2.5 m"]
-[5.008735656738281, 4.337651252746582, "[TT] Hardware Cost of the Starlink Premium = $2,500"]
-[5.058303356170654, 2.8647258281707764, "[TT] Provider of the POLDER-2 = French National Centre for Space Studies (CNES)"]
-[10.450654983520508, 1.6947458982467651, "[FF] Nature of the Accretion Disk = Superheated disk of material feeding the black hole"]
-[5.939379692077637, 2.4502735137939453, "[TT] Affiliation of the STScI = Association of Universities for Research in Astronomy (AURA)"]
-[5.106706142425537, 1.35702383518219, "[FF] Conference Presentation Date of the X-Sat = Nov. 22-26, 2004"]
-[7.9966721534729, 7.279338359832764, "[TT] TDI Stages of the Kruiz CCD = 128, 64, 32, 16, 8"]
-[6.156497478485107, 4.627167701721191, "[FF] Update Frequency of the AI Apps = Can be updated in orbit after fine tuning is done with real images on the ground"]
-[11.391005516052246, 4.341218948364258, "[FF] Size of the TacSat-6 = 3U"]
-[4.982086181640625, 0.7070064544677734, "[TT] Mission Start Date of the PROBA-V = July 2010"]
-[10.492518424987793, 3.342395782470703, "[TT] Power Requirement of the CubeSats = None from the rocket"]
-[4.579263687133789, 4.783930778503418, "[FF] Mission Objectives of the M3MSat = 1) augment existing maritime surveillance capabilities through the space-based monitoring of ship Automatic Identification System (AIS) 2) foster Canadian capabilities by providing an opportunity for the contractor to propose and demonstrate a new technology for a secondary payload 3) provide a flight opportunity for Canadian industry to space qualify new technology and to establish flight heritage 4) the primary mission objective is to provide maritime surveillance for both commercial customers, and for the Canadian government, by detecting AIS messages from space"]
-[10.470703125, 6.847270965576172, "[TT] Size of the Secondary Mirror = 2.4-foot (0.74 m)"]
-[3.252487897872925, 5.065297603607178, "[TT] Ground Resolution of the SAR = 25 x 6 m"]
-[7.677181720733643, 6.516509056091309, "[TT] Full Disk Swath Collection Interval of the ABI = 30 seconds"]
-[4.392763614654541, 7.0553483963012695, "[TT] Data Transmission Bands of the ICEYE-X1 = S- and X-band"]
-[9.463032722473145, 7.138354778289795, "[TT] Spatial Resolution of the PMI = 19 x 11 km"]
-[1.9469821453094482, -0.39948326349258423, "[TT] Launch Date of the Van Allen Probes = Aug. 30, 2012"]
-[14.230710983276367, 3.205583095550537, "[TT] Mass of the CIRC = ~ 3 kg"]
-[9.541504859924316, 6.3239264488220215, "[TT] View Angles of the LRR = 360\u00ba in azimuth and 60\u00ba elevation"]
-[13.804168701171875, 3.716355800628662, "[TT] Full-Scale Unit of the MEMS Cantilever Beam Accelerometers = 2 gram"]
-[8.290046691894531, 7.805904388427734, "[TT] Signal Range of the PMT = From a few photo-electrons for MIP to ~ 105 photo-electrons for electromagnetic showers"]
-[9.581607818603516, 6.995137691497803, "[TT] Vertical Resolution of the OMPS = 1 km"]
-[5.104857444763184, 3.47910737991333, "[TT] Manufacturer of the FASat-Alfa = SSTL"]
-[5.4918670654296875, 0.38555842638015747, "[TT] Launch Date of the GEOS-2 = Jan. 11, 1968"]
-[7.563836574554443, 6.943253040313721, "[TT] Cadence of the Thermal Neutron Counts = 5 minutes"]
-[6.018875598907471, 4.376305103302002, "[FF] Objective of the MUSIS = Provide continuity of service of the current generation of optical and radar satellites and ensure adequate access of the partners to space systems which will enter into service in the coming years"]
-[6.781561374664307, 4.130778789520264, "[FF] Design and Ground Testing of the HSC = Unknown"]
-[9.556941986083984, 7.024721622467041, "[TT] Spatial Resolution of the Maps = 0.5\u00b0 to 2\u00b0"]
-[9.456002235412598, 5.506393909454346, "[TT] Rotating Mode Test Period of the MicroSCOPE = Ti = 20 orbits"]
-[11.911781311035156, 3.064981460571289, "[TT] \u0394V of the Propulsion Module = 80 m/s"]
-[9.798637390136719, 5.413341045379639, "[FF] Thermo-elastic Stability of the FG = Unknown"]
-[11.839032173156738, 6.694879055023193, "[TT] Electron Energy Range of the EPAM = Ee >30 keV"]
-[5.693342685699463, 2.7067315578460693, "[TT] Program of the SMAP = ESSP (Earth System Science Pathfinder)"]
-[3.5384361743927, 5.419300556182861, "[TT] Data Rate of the AMI SAR = 105 MBit/s"]
-[8.328612327575684, -0.5585159063339233, "[TT] Spatial Resolution (km) of the Ice: area covered = 25"]
-[8.095715522766113, 8.445989608764648, "[TT] Infrared Wavelength Detection Range of the Mapping Channel = 0.95 \u00b5m to 5 \u00b5m"]
-[8.298515319824219, 8.658289909362793, "[TT] Spectral Resolution of the VIS = 0.63 nm"]
-[8.403486251831055, 8.656307220458984, "[TT] Depolarization Measurements of the Science mode 2 = Not provided at 532 nm"]
-[6.5398688316345215, -0.45964810252189636, "[TT] Revisit Cycle of the LISS-4 = 5 days"]
-[5.4861626625061035, 6.919357776641846, "[TT] Data Download Capacity of the TM (telemetry) subsystems = Few hundred Mbit per day"]
-[8.563297271728516, 3.613046646118164, "[FF] Parameter of the NASA BIRD = Active radiation monitor capable of time-resolved particle flux measurements"]
-[4.7620744705200195, 8.083212852478027, "[TT] Frequency Range of the GAMALINK = 300 MHz to 3 GHz"]
-[6.959499359130859, 6.148015975952148, "[TT] Number of Instruments of the EuTEF = 9"]
-[9.371243476867676, -0.6033896207809448, "[TT] Orbit Altitude of the Beijing-3A = 500 km"]
-[8.678160667419434, 4.530599117279053, "[FF] Purpose of the Star Simulator = Improvement of the HILS environment"]
-[8.617980003356934, 5.178949356079102, "[FF] Quantity of the SCA = Three temperature controlled CCD star cameras"]
-[5.934630870819092, -0.45761358737945557, "[TT] Operational Duration of the F-14 = More than 22 years"]
-[4.499478340148926, -0.8814128637313843, "[FF] Mission Completion Date of the CRS-18 Dragon = 27 August 2019"]
-[10.094411849975586, 5.480554580688477, "[TT] Cooling System of the Focal Plane Assembly = Active cooling subsystem"]
-[5.275914669036865, 3.2214715480804443, "[TT] Manufacturer of the Lucy = Lockheed Martin"]
-[7.598042011260986, 1.95856511592865, "[TT] Detection Capability of the JJ-FAST = Areas of deforestation in the order of a few hectares"]
-[3.4140784740448, 6.415238380432129, "[TT] Size of the Cross dipole antenna = 1050 mm x 800 mm x 800 mm"]
-[8.145209312438965, 3.3269314765930176, "[FF] Objective of the Argus = Detect the greenhouse gas constituents in the near-infrared spectrum using earthshine spectra"]
-[11.786272048950195, 0.08323530107736588, "[FF] Follow-up Observations of the TESS = Refine Measurements of Planet Masses, Sizes, Densities, and Atmospheric Properties"]
-[11.011157035827637, 3.586372137069702, "[FF] Size of the PhiSat-1 = About the size of a cereal box"]
-[5.7555832862854, 4.789798736572266, "[FF] Supporting GPS/GLONASS Multi-Constellation Augmentation of the QZSS L1-SAIF = ITM 2013 (International Technical Meeting) of The Institute of Navigation, San Diego, Ca, USA, January 28-30, 2013"]
-[7.080735206604004, 1.3038276433944702, "[FF] Retired of the Spitzer Space Telescope = Recently retired"]
-[5.389951705932617, 0.7321860790252686, "[TT] Arrival Date of the ExoMars = June 2023"]
-[9.632762908935547, -1.0147048234939575, "[TT] Orbit Longitude of the COSPAS GOMS-1 = 76.5\u00ba E"]
-[10.4497709274292, 4.099227428436279, "[TT] Independence of the Hypersonic Grid Fins = Each fin moves independently for roll, pitch and yaw"]
-[7.053464412689209, 7.7263503074646, "[TT] Quantity of the Reflector Cubes = 9"]
-[4.696376323699951, 2.8583412170410156, "[FF] Location of the Ground Segment = Roof of the research lab IES (Institut d'Electronique du Sud) building located on the campus of UM2 (University Montpellier 2)"]
-[11.977198600769043, 4.948030471801758, "[TT] Volume of the SDR = ~175.1 cm 3"]
-[7.542537212371826, 5.670923233032227, "[FF] Ta Bias Model of the MWR = Linear function of MWR Ta"]
-[9.976005554199219, 7.757359981536865, "[TT] Celestial Sphere Coverage of the Telescope = Observatory ~80.7%"]
-[12.115458488464355, -0.3104453980922699, "[TT] Sector Observation Duration of the TESS = At least 27 days"]
-[5.488076686859131, 2.7166948318481445, "[FF] Management of the Swift = NASA's Goddard Space Flight Center"]
-[3.2208733558654785, 5.013580322265625, "[TT] Swath Width of the SAR = Larger than 40 km"]
-[10.324664115905762, 5.7451863288879395, "[TT] Measurement Error of the Temperature = \u00b13\u00baC (-50 to +400\u00baC), \u00b18\u00baC (+400 to +600\u00baC)"]
-[5.270967483520508, 1.139912486076355, "[FF] Overview Meeting Date of the CLARREO = October 20-22, 2009"]
-[8.429061889648438, 6.899506092071533, "[FF] Imaging Resolution of the Direct Imaging System = Lower than PAIS with eight subapertures"]
-[8.136794090270996, 3.1420788764953613, "[FF] Detection Capability of the OMI = Sulfur Dioxide"]
-[8.942543983459473, 3.098945140838623, "[FF] Impact Area of the Solar Storm = Earth's ionosphere"]
-[7.423296928405762, 6.581123352050781, "[FF] Purpose of the Scale Factor Measurements System (SFMS) = Measurement of the absolute laser frequency"]
-[9.744327545166016, 8.186177253723145, "[TT] Number of Holes of the Optical Head = 1 / 100 (enhanced configuration)"]
-[7.437002658843994, 8.357688903808594, "[TT] Number of Rows to Make Two Perfect Rows of the QWIP Array = 3"]
-[9.888078689575195, 1.6769521236419678, "[FF] Data Analysis of the eROSITA = Study the abundance of chemical elements, the degree of their ionization, the density and temperature of the emitting gas in the bubbles, and to identify the locations of shock waves and estimate characteristic timescales"]
-[5.2461628913879395, 2.2678496837615967, "[FF] Comparison of the Variant = DEMETER mission"]
-[7.8154144287109375, 7.196846008300781, "[TT] Frame Rate of the Camera = 500 frames/s"]
-[5.136023998260498, 4.349066734313965, "[TT] Average Number of Jointly Tracked Satellites of the T3000G2 receiver = 2-3"]
-[5.296618461608887, 0.6298993229866028, "[TT] Launch Date of the Satellite = Announced on 7 October 2021"]
-[8.55251407623291, 6.212252616882324, "[TT] Planned Position of the TEMPO = 91\u00b0 West, above the equator"]
-[11.088942527770996, 1.1664601564407349, "[TT] Development of the Gravitational Reference Sensor = Pre-developed by ESA, NASA and the LISA consortium of ESA member states"]
-[7.9353437423706055, 3.055997371673584, "[FF] Retrieval Technique of the SIF, XCO2, XCH4, XCO = Optimal estimation technique"]
-[9.010894775390625, 5.639008522033691, "[TT] Pointing Performance of the ACS = \u2264 150 arcsec"]
-[6.32157039642334, 5.3686957359313965, "[TT] Type of the CIRC = Other"]
-[10.862442970275879, -0.29507485032081604, "[FF] Presentation Location of the TanDEM-X = Fort Worth, Texas, USA"]
-[6.790914058685303, 5.956165313720703, "[TT] Operational Mode of the REPT = Continuous"]
-[5.750345706939697, -0.8413159251213074, "[TT] Design Life of the Optsat-3000 = 7 years"]
-[5.3775482177734375, 7.806487560272217, "[FF] Function of the SSPA (Solid-State Power Amplifier) = Generate the high-power radar transmit signal"]
-[6.581603050231934, 7.627225399017334, "[TT] Data Quantization of the Pushbroom imager = 12 bit"]
-[9.56164264678955, 7.956590175628662, "[TT] Aberrations of the SHS = Introduce field of view limitations"]
-[7.0280256271362305, 0.5130330324172974, "[TT] Partners of the Kepler = 6"]
-[3.7519450187683105, 5.113031387329102, "[TT] Imaging Frequency Band of the HJ-1C = S"]
-[3.923520803451538, 6.602988243103027, "[TT] Frequency of the Patch Array Antenna = 5182 MHz"]
-[8.89791488647461, 0.028106046840548515, "[TT] Latitude Limit of the High power VLF transmission = \u00b120\u00ba about the equatorial plane"]
-[8.129974365234375, 2.897092342376709, "[FF] Mission Objective of the GLM = Measure from GEO the total lightning activity on a continuous basis over the Americas and portions of the adjoining oceans"]
-[9.549468994140625, 3.0113677978515625, "[TT] Interaction with Magnetic Fields of the Cosmic Rays = Their path is bent by magnetic fields"]
-[7.515401363372803, 0.719176173210144, "[FF] Orbit of the LunaH-Map = Elliptical science orbit"]
-[11.66160774230957, 4.084524154663086, "[FF] Body Size of the NorSat-2 = Smaller than 62 x 62 x 73 cm"]
-[10.023639678955078, 5.186481952667236, "[TT] Electrode Shape of the TPS = Spherical"]
-[9.275026321411133, 3.146000862121582, "[FF] Oxygen Isotopic Composition of the Solar Wind = Unknown"]
-[9.58515739440918, 4.1378960609436035, "[FF] Instruments of the Variant = Split Langmuir probe, Rogovsky coil, Faraday cup"]
-[4.560149669647217, 2.948068618774414, "[TT] Location of the TETX = Toulouse"]
-[9.18989372253418, 2.440595865249634, "[FF] Journey Time to Earth of the Solar Energetic Particles = Under an hour"]
-[7.584650993347168, 3.672750234603882, "[TT] Mounting of the M3 = Glued bipods on outer edges"]
-[3.614392042160034, 5.281067848205566, "[TT] Minimum Looks in Range of the Radar = 40 looks for 10 km cells"]
-[14.065590858459473, 4.0532684326171875, "[TT] Mass of the SEIS Instrument = 3 kg"]
-[13.970541000366211, 7.139171600341797, "[TT] Bus Voltage of the Spacecraft = 4.0 V"]
-[8.994901657104492, 0.4615151286125183, "[TT] Displacement of the Boulders = More than 3cm"]
-[7.016139507293701, 7.716457843780518, "[TT] Number of Reflectors of the RRA = 264"]
-[4.858245372772217, 3.193265199661255, "[TT] Provider of the SARP = CNES/France"]
-[4.484856605529785, 3.0407378673553467, "[TT] Location of the SCC = S\u00e3o Jos\u00e9 dos Campos, Brazil"]
-[12.77377986907959, 7.224851131439209, "[TT] Main Beam Efficiency (%) of the Antenna = 88"]
-[5.448054790496826, 0.9533854722976685, "[FF] Testing Date of the EO-1 = Oct. 18, 2004"]
-[5.050423622131348, 0.6301031112670898, "[TT] Year of the RSATS = 2004"]
-[5.815396785736084, -0.5488892197608948, "[TT] Design Life of the PROBA-1/-2 = Nominal mission life of 2.5 years (with a possible extension of up to 5 years)"]
-[3.5241100788116455, 5.287159442901611, "[FF] Function of the Mechanisms = Deploy the SAR antenna after launch"]
-[8.146295547485352, 8.82325267791748, "[TT] Spectral Range of the UV-2 = 306 - 380 nm"]
-[8.975868225097656, 5.017378330230713, "[FF] Components of the Microstrain 3DM-GX2 = 3-axis magnetometer, three accelerometers, and a rate gyroscope"]
-[6.548002243041992, 0.0933816060423851, "[TT] Mission Duration of the CryoSat = 8 years"]
-[10.279417037963867, 5.734502792358398, "[TT] Temperature of the CCD = As low as -110\u00baC"]
-[3.1957650184631348, 4.945253849029541, "[TT] Field of Regard of the RISAT-SAR = 659 km"]
-[9.566672325134277, 9.11197566986084, "[TT] Field of View of the IRIS = 120 arcseconds"]
-[5.903027534484863, 2.17621111869812, "[FF] Number of the Columbus ESA ISS Science & System = 78"]
-[8.222088813781738, 5.132419109344482, "[TT] Type of the Accelerometer (ACC) = Accelerometer"]
-[10.1420259475708, -2.752727746963501, "[TT] Die Capacity of the SLC NAND-Flash = 8 Gbit"]
-[12.06283187866211, -0.22982202470302582, "[TT] Sky Survey Time of the TESS = 2 years"]
-[8.096969604492188, -0.5396193265914917, "[TT] Ice Mass Loss of the GRACE = 280 Gt per year"]
-[5.249266147613525, 7.646598815917969, "[TT] G/T of the Ground terminal = -24 dB/K"]
-[7.372612953186035, 2.4186482429504395, "[FF] Coverage Regions of the MOMS-02 = General"]
-[4.514235973358154, -0.8880378007888794, "[TT] Certification Date of the SpaceX Crew Dragon = November 11, 2020"]
-[9.720523834228516, 7.837466239929199, "[TT] Number of Telescopes of the ASAS-SN = 20"]
-[6.623411178588867, 8.420975685119629, "[TT] Cross-polarization Ratio of the Instrument = \u2264-25 dB"]
-[8.2793607711792, 0.7893161773681641, "[TT] Current Size of the Cerro Pelado fire = More than 25,000 acres"]
-[7.545094966888428, 7.226988792419434, "[TT] Value of the Frame Rate = 500 Hz"]
-[10.136297225952148, 6.94389009475708, "[TT] North-South Block of the Sounder = 640 km"]
-[13.751721382141113, 5.35654878616333, "[TT] Transistor Type of the HPA = GaN HEMT (Gallium Nitride High Electron Mobility Transistor)"]
-[4.947345733642578, 0.977774977684021, "[FF] Annual Production of the APL\u2019s Research and Exploratory Development Department (REDD) = Thousands of boards, cables and assemblies"]
-[18.797054290771484, 3.479288101196289, "[TT] Mean \u0394N (m) of the Bandari = -2.8"]
-[9.620157241821289, 6.944255352020264, "[TT] Global Maps Resolution of the LEND = 5-20 km"]
-[6.554521560668945, -0.5967807173728943, "[TT] Orbital Residence Times of the RemoveDebris = <3 years"]
-[5.296517848968506, 6.332882881164551, "[TT] Maximum Read Performance of the SDR-SDRAM = < 800 Mbit/s @ 100 MHz burst operation"]
-[4.981387138366699, 3.3907268047332764, "[TT] Manufacturer of the OHRIS = Northrop Grumman"]
-[9.553586959838867, 4.762017726898193, "[FF] Power Consumption of the Passive Attitude Control System = None"]
-[7.2703166007995605, 6.610598564147949, "[TT] Microvalve Opening Time of the CGMS = 1ms"]
-[6.477563381195068, 3.4779343605041504, "[TT] Function of the Devices to Capture the Fasteners = Capture the fasteners the astronauts remove from AMS"]
-[10.626075744628906, 8.870721817016602, "[TT] Pixel Size of the Channel 6 = 32 x32 km"]
-[4.506567001342773, 2.8695907592773438, "[FF] Location of the PDMC = ESA/ESRIN, Frascati, Italy"]
-[8.699261665344238, 3.286534309387207, "[FF] Impact of the Solar Energetic Particles = Can fry sensitive spacecraft electronics and pose serious risks to human astronauts"]
-[14.072810173034668, 7.191315650939941, "[TT] Voltage Levels of the Power Regulation = 5V and 8V"]
-[9.036273956298828, 8.554426193237305, "[TT] Band 6 Wavelength Range of the Telescope = 11.5 - 12.5 \u00b5m"]
-[7.133566379547119, 0.05078017711639404, "[TT] Age of the Swift J1818.0-1607 = About 240 years old"]
-[4.402158737182617, 7.769218444824219, "[TT] Downlink Frequency of the SafetyNetTM = Ka-band (26.7 GHz)"]
-[8.074427604675293, 3.7095885276794434, "[FF] Model Intercomparison Project (MIP) of the OCO-2 = Organized by the OCO-2 Science Team"]
-[5.428523063659668, 1.691841721534729, "[FF] Mission of the ALOS-2/Daichi-2 = Forest Monitoring"]
-[3.7071259021759033, 4.908491134643555, "[TT] Imaging Frequency Band of the RISAT-1 = X"]
-[9.678466796875, 4.562300205230713, "[FF] Functions of the Spin Mechanism Assembly = Conical scanning, signal transfer and power distribution through internal slip rings"]
-[3.659942388534546, 6.522035598754883, "[TT] Reflector Type of the SMMR = Fixed offset parabolic"]
-[8.539081573486328, 2.193603277206421, "[FF] Seasonal Occurrence of the Dust Storm = Spring"]
-[9.595333099365234, 3.7592053413391113, "[FF] Resistance of the GMR = Very high without an external magnetic field and a current applied perpendicular to the magnetization of the layers"]
-[7.27827787399292, 2.8050336837768555, "[FF] Payload of the PROBA-II = PROBA-II Payload: A Belgian Mini Space Weather Observatory"]
-[14.01443099975586, 3.9149584770202637, "[TT] Instrument mass of the Optical System = 120 kg"]
-[7.970472812652588, 7.651838779449463, "[FF] Model of the MightySat II.1 hyperspectral imager = Engineering model"]
-[10.061125755310059, -1.5512001514434814, "[TT] Inclination of the SZ-7 = 42.4\u00ba"]
-[5.652534484863281, -0.6180253028869629, "[TT] Expected Service Period of the GOES-R = At least 22 years"]
-[5.70143461227417, 1.1171327829360962, "[FF] Test Date of the HEPS = Beginning of the second calibration and validation phase"]
-[8.744234085083008, 6.748465061187744, "[FF] Image of the CIRC PFM = Figure 80"]
-[4.35658073425293, 0.6487556099891663, "[TT] Launch Date of the DMSP-F14 = 1997"]
-[4.459895610809326, -0.028938036412000656, "[TT] Landing Date of the Starliner = December 22, 2019"]
-[11.32599925994873, 0.7456411719322205, "[TT] Debris Disk of the AU Microscopii = Yes"]
-[9.025471687316895, 5.253865718841553, "[FF] Pointing Control of the ExoplanetSat = One-arcsecond Line-of-Sight"]
-[11.479778289794922, 6.6808600425720215, "[FF] Energy Bands of the eROSITA = Red, green and blue"]
-[7.268232345581055, 5.282034873962402, "[FF] Subsystems of the Instrument Electronics Assembly = Instrument controller, Detector readout electronics, HVPS, LVPS"]
-[7.483660697937012, 8.516335487365723, "[TT] Spectral Sensitivity (Source) of the SXI = Al (8.3 \u00c5)"]
-[8.257935523986816, 4.588642120361328, "[FF] Measurement Accuracy of the LARES satellite = Accurately reflects Earth's tidal perturbations"]
-[9.656503677368164, 1.4535728693008423, "[TT] Number of Satellites of the Pl\u00e9iades Neo constellation = 4"]
-[13.802199363708496, 6.773291110992432, "[TT] Power Source of the EAGLE ESPAStar = 96 Ahr battery"]
-[4.937767505645752, 4.218029499053955, "[TT] Products Distributed in 2012 of the IC Stations = More than 215,000"]
-[4.2861409187316895, 4.815634250640869, "[FF] Output of the MDA Tool = Statistically probable Minimum Detectable Ship Length (MDSL) metric at a 90% confidence level"]
-[6.564271450042725, 4.800518989562988, "[FF] Objective of the Electrical & Functional Model (EFM) = Validate the electrical architecture and the on board software"]
-[7.71577262878418, 8.846158027648926, "[TT] Range of the Spectral Bands = 0.32 - 4.0 \u00b5m"]
-[4.770608901977539, -1.8297133445739746, "[TT] Extended Mission of the Chang'e-2 = Earth-Sun L2 mission followed by a deep-space mission"]
-[9.797622680664062, 8.598386764526367, "[TT] IFOV of the ScaRaB = 48 mrad x 48 mrad"]
-[9.088888168334961, 2.8495805263519287, "[FF] Source of the Solar Energetic Particle Events = Super active region 11944"]
-[7.374454975128174, 6.28806734085083, "[TT] Real-time Navigation Data Frequency of the DIOGENE = Every 30 s"]
-[6.278292179107666, 6.326625823974609, "[TT] Payload Interaction Window of the SOC = Up to 20 minutes before each contact"]
-[5.532654285430908, 2.870006799697876, "[TT] Funding from ESA of the Copernicus = 2.55 billion euros"]
-[4.066552639007568, 6.272396087646484, "[TT] Configuration of the NanoCom Ant430 = Canted turnstile"]
-[8.402567863464355, 1.1673085689544678, "[TT] Quantization levels of the Soil moisture = 1"]
-[5.784660339355469, 3.3730366230010986, "[TT] Business Opportunities of the Satellogic = $2.1 billion in the near and longer term"]
-[3.4069035053253174, 5.978668212890625, "[TT] Antenna Type of the Biomass = SAR antenna with a large deployable reflector"]
-[14.060595512390137, 3.2915756702423096, "[TT] Mass of the IOD-1 GEMS = Approximately 4 kg"]
-[5.12759256362915, 7.065646648406982, "[TT] Uplink Speed of the Communication system = 2 kbit/s"]
-[3.4978737831115723, 3.7267041206359863, "[TT] Operation Status of the TSX (TerraSAR-X) = Nominal"]
-[4.314201831817627, 7.225668430328369, "[TT] Downlink Frequency of the Communication = X-band"]
-[5.748394012451172, 4.11569881439209, "[FF] Objective of the XI-IV = Demonstrate and validate a picosatellite bus system and the space use of commercial-of-the-shelf (COTS) parts"]
-[7.671630382537842, 5.446114540100098, "[FF] Parameter of the Detector Assembly = Value"]
-[8.794621467590332, 4.062965393066406, "[TT] Mission of the Hot Ion Analyzer = Cluster"]
-[5.240981101989746, 2.7997257709503174, "[FF] Winning Team of the EDC = Governor's School for Science and Technology in Hampton, Va"]
-[11.067922592163086, 2.9441444873809814, "[TT] Solar Array Efficiency of the PARASOL microsatellite = 26%"]
-[9.062372207641602, 4.532998085021973, "[FF] Attitude Sensing of the ADCS = Magnetometers, gyros and photodiodes"]
-[7.471103668212891, 2.0581893920898438, "[TT] Surface Mapping Coverage of the Bennu = At least 80%"]
-[7.655860424041748, 3.2893378734588623, "[FF] Applications of the Satellite = Weather model assimilation of RO, space weather monitoring, ionosphere corrections for navigation, thermospheric density (POD)"]
-[3.9862122535705566, 2.1518731117248535, "[TT] Launch Vehicle of the COPPER CubeSat = Minotaur-1 of OSC (Orbital Sciences Corporation)"]
-[5.066858768463135, 0.6151607036590576, "[TT] Next Release of the Request for Information = Q2 of CY 2022"]
-[6.749299049377441, 5.769138813018799, "[TT] Quantity of the LIN bus = 2"]
-[4.847629070281982, 7.3172101974487305, "[TT] Data Rate of the S-band Transmitter = 32 kbit/s to 256 kbit/s"]
-[9.091004371643066, 7.597032070159912, "[TT] Multispectral of the Medium resolution = 118 m"]
-[11.793835639953613, 3.286686897277832, "[TT] Thruster Burn Arcs of the BepiColombo = 22"]
-[10.019182205200195, 1.3828397989273071, "[TT] Outflow Channels of the Milky Way = Above and below the plane of the Milky Way"]
-[11.25695514678955, 5.137168884277344, "[TT] Sense Wires Material of the Straw Tubes = 30 \u00b5m gold plated tungsten"]
-[9.148842811584473, 4.9213786125183105, "[TT] Purpose of the CADET = Examining attitude estimation and non-cooperative approach using a visual and infrared system"]
-[8.083158493041992, -0.4688846170902252, "[FF] Data Source of the DMSP instruments SSM/I and SSMIS = Arctic sea ice growth in 2018"]
-[4.690732955932617, 1.5504107475280762, "[FF] Renaming Date of the GCOM-C = July 14, 2017"]
-[6.191896438598633, 1.4502679109573364, "[TT] Launch Date of the eROSITA = July 13, 2019"]
-[4.723156929016113, 0.5005894303321838, "[TT] Launch Date of the GOES-T = April 2024"]
-[6.240063667297363, 2.9899544715881348, "[TT] Company Type of the Spire = Provider of space-based data, analytics, and space services"]
-[5.612949848175049, 3.707796096801758, "[TT] Number of Maneuvers of the SkySat-4 = 3"]
-[11.430299758911133, 2.160759210586548, "[TT] \u0394V (cm/s) of the Thorad Agena D Debris = 0.39"]
-[9.760190963745117, 0.8209271430969238, "[TT] Distance from Star of the TOI 270 b = About 13 times closer than Mercury orbits the Sun"]
-[8.709980964660645, 8.517036437988281, "[FF] Dithering Maneuver Requirement of the Spectrometer (SPI) = Required"]
-[4.043946743011475, 6.354629039764404, "[FF] Designs of the Antenna = Omnidirectional, high gain and arrays"]
-[5.036770820617676, 3.5302278995513916, "[TT] Manufacturer of the Imager Driver Board = Ecliptic Enterprises"]
-[7.649746417999268, -2.5326101779937744, "[TT] Imaging Time of the GOLD = 20:10 UT on 2 July 2019"]
-[13.131633758544922, 7.27537727355957, "[TT] Power Consumption of the SIR-2 = 2.2 W"]
-[13.88687515258789, 2.937937021255493, "[FF] Mass of the STRV-1c and -1d Spacecraft = Larger than STRV-1a/-1b"]
-[5.57073450088501, 5.7235517501831055, "[TT] Processor of the C&DH subsystem = RAD 6000"]
-[8.693074226379395, 7.672089576721191, "[TT] Pixel Size of the CCD = 21 x 21 \u00b5m (0.5 x 0.5 arcsec)"]
-[10.271806716918945, 7.999822616577148, "[TT] Path Length of the Telescope = 200 \u03bcm"]
-[5.2678914070129395, 8.15308666229248, "[TT] Frequency Range of the IME-HF instrument = 100 kHz to 30 MHz"]
-[7.7430033683776855, 7.148229122161865, "[TT] Data Readout of the CCD = Serial"]
-[9.879481315612793, 6.243967533111572, "[TT] Heritage of the CIXS = D-CIXS (Demonstration of a Compact Imaging X-ray Spectrometer)"]
-[8.709030151367188, 1.8515417575836182, "[FF] Wind Speed of the Tropical Storm Victor = 75 kilometers (45 miles) per hour"]
-[14.60291862487793, 6.638486385345459, "[TT] Battery Type of the EPS = Li-ion"]
-[9.972660064697266, 2.859774351119995, "[FF] First Light Date of the Sunstorm CubeSat = 27 August 2021"]
-[7.366116046905518, 6.1767578125, "[FF] Operation of the Laser Retro Reflector (LRR) = Enabled tracking by ground-based satellite laser ranging stations"]
-[7.700592041015625, 0.9347196221351624, "[FF] Purpose of the Matroshka AstroRad Radiation Experiment (MARE) = Provide valuable data on radiation levels during missions to the Moon and test the effectiveness of the new vest"]
-[7.984565734863281, 2.028494119644165, "[FF] Controller Gains of the GOCE = Unknown"]
-[12.718164443969727, 3.901151180267334, "[FF] Objective of the CuPID = Study macroscale properties of dayside magnetopause reconnection"]
-[10.33320140838623, 2.1379199028015137, "[FF] Mission of the Chandra and Swift = X-ray Emission Characterization"]
-[5.507375717163086, 7.267555236816406, "[TT] Power Consumption of the ODTML = < 0.1 Joule per bit transmitted"]
-[6.977780342102051, 0.06193578243255615, "[FF] Ground Track Repeat of the SeaSat-1 = 3 days"]
-[7.94136381149292, 6.445209503173828, "[FF] Type of the MTG-I = Imager"]
-[9.996134757995605, -1.5169110298156738, "[TT] Inclination of the Orbit = 89.0\u00b10.06\u00ba"]
-[13.278589248657227, 5.280960559844971, "[TT] Power Area of the Solar Panels = 80 square meters"]
-[3.648280620574951, 4.8450822830200195, "[FF] Polarimetric Observations of the RISAT-1 = At multiple incidence angles"]
-[7.192402362823486, 7.359799385070801, "[TT] Signal Photon Density of the MABEL = Greater than 4 photons/m"]
-[6.448132038116455, 5.745365619659424, "[TT] Capacity of the Node-3 = Up to eight ISS equipment racks"]
-[10.153902053833008, 2.0802805423736572, "[FF] Image Credit of the Chandra X-ray Observatory = X-ray: NASA/CXC/NCSU/K. Borkowski et al; Optical: DSS"]
-[9.71425724029541, 6.451450347900391, "[FF] Operation Schedule of the Moving Mirror = 4 days of operation and 10 days of standby"]
-[7.2471723556518555, 5.753319263458252, "[FF] Download Method of the Image Data = During ground contact windows"]
-[4.52457857131958, -0.7839655876159668, "[TT] Training Location of the Crew Dragon = NASA\u2019s Neutral Buoyancy Laboratory near the Johnson Space Center in Houston"]
-[6.190856456756592, 1.616428256034851, "[FF] Impact of the Aeolus = Amongst the most important satellite missions"]
-[10.048145294189453, 7.5605926513671875, "[TT] Swath Width of the Pushbroom imager = 17.5 km at nadir"]
-[5.571841716766357, 7.141696929931641, "[TT] Data Rate of the LISS-3 = 52.5 Mbit/s"]
-[7.282712936401367, 6.6313676834106445, "[TT] Integration Time (ms) of the Antenna = 100"]
-[6.260714054107666, 1.1385867595672607, "[FF] Image Capture Date of the Earth Observation Satellite = 25 June 2021"]
-[5.794133186340332, 5.412202835083008, "[TT] Redundancy of the TT&C Receiver = Half Satellite"]
-[12.065526962280273, 4.998173713684082, "[TT] Volume of the Superfluid Helium = 2500 l"]
-[3.335277795791626, 5.333256244659424, "[FF] Reference Position of the ODMP = Tends towards RADARSAT-2's center of mass, which is approximately 1 m above the center of the SAR antenna"]
-[3.7361252307891846, 7.1717095375061035, "[TT] Gain of the Telemetry Antenna = 0 dBi at \u00b1 60\u00b0"]
-[4.223462104797363, 6.327308654785156, "[FF] Unknown of the Y antenna = Unknown"]
-[7.360145092010498, 6.77773380279541, "[FF] Measurement Method of the ATLAS = Sending pulses of light to Earth\u2019s surface and measuring how long it takes individual photons to return to the satellite"]
-[6.270452499389648, 0.3198862373828888, "[TT] Lifetime of the ROSE-L = 7\u00bd years"]
-[7.640059471130371, 1.3693010807037354, "[FF] Function of the ShadowCam = Acquire images of shadowed regions of the moon"]
-[9.657235145568848, 3.8356096744537354, "[FF] Magnetic Field Strength of the CME (Coronal Mass Ejection) = Double that of a normal CME"]
-[8.307245254516602, 5.3148603439331055, "[TT] Orbit Determination Accuracy of the DORIS = 0.2 m - 0.6 m"]
-[3.544525623321533, 1.82719886302948, "[FF] URL of the Sentinel-5 = http://www.space-airbusds.com/media/document/10607tl-sentinel-5-lr.pdf"]
-[5.669516563415527, -0.21602308750152588, "[TT] Development Time of the Instrument = 2 years"]
-[5.7168169021606445, 2.3896937370300293, "[FF] Project Team Members of the AzTechSat = Maria de la Luz Garcia Cruz, Rosa Reyna Gonzalez Cancino, Ana Belen Urrutia Bartsch"]
-[14.122231483459473, 2.8418655395507812, "[TT] Mass of the CartoSat-2E = ~712 kg"]
-[13.221497535705566, 5.482215881347656, "[FF] Power Distribution of the MERLIN = Unknown"]
-[9.069604873657227, 1.3504096269607544, "[FF] URL of the New Horizons = https://www.nasa.gov/feature/nasa-s-new-horizons-reaches-a-rare-space-milestone"]
-[7.714347839355469, 6.364044189453125, "[TT] Visible Stars Observation Frequency of the ABI = On average at least every 100 s"]
-[6.32446813583374, 3.1177961826324463, "[FF] Planned Satellite Name of the Capella Space = Sequoia"]
-[9.940616607666016, 4.369236946105957, "[TT] Magnet Type of the AMS-02 = Superconducting"]
-[8.158795356750488, 1.1844197511672974, "[FF] Level-3 Data Availability of the SMAP (Soil Moisture Active Passive) = Beta version available as of Sept. 9, 2015"]
-[5.838046550750732, 3.4084291458129883, "[TT] Cost Savings of the Satellogic = 100 times cheaper than competitors"]
-[5.102604389190674, 2.6472361087799072, "[TT] Data Distributor of the Resurs-P1 = Sovzond JSC of Moscow"]
-[2.2816543579101562, 2.7718162536621094, "[TT] Co-PI of the EPI-Lo = Matthew Hill"]
-[5.963049411773682, -0.5822063684463501, "[TT] Duration of the Mission Life = 1 year science operation with an additional several months for maneuvering and decommissioning"]
-[6.484952926635742, 5.283987522125244, "[FF] Data Transfer of the OISL = LCT to modulators through the DPU (Data Processing Unit)"]
-[5.492735862731934, 1.4619146585464478, "[FF] Commissioning Status of the IPA = Successful"]
-[8.431680679321289, 4.013914108276367, "[TT] Frequency of the Solar Calibration = Daily"]
-[10.464618682861328, 2.1329402923583984, "[FF] X-ray Emission of the SS 433 = Confined within two cones of gas extending outward from opposite sides of the central object"]
-[5.486947059631348, 6.797818183898926, "[TT] Total Data Downlink Time of the WCOM = About 52 minutes per day"]
-[5.904393196105957, 3.5283312797546387, "[TT] Cost of the HTA = Low"]
-[7.8465800285339355, 2.131000518798828, "[FF] Resolution of the ZY-3 = High"]
-[5.339550018310547, 2.482374429702759, "[TT] Contractor of the ALOS-2 = JAXA (Japan Aerospace and Exploration Agency)"]
-[4.178468227386475, 3.7523462772369385, "[TT] Atmospheric Pressure of the Galileo probe = About 320 pounds per square inch (22 bar)"]
-[10.923453330993652, 3.5256972312927246, "[TT] Size of the SkySats = About the size of a mini-fridge"]
-[11.14138126373291, 1.1306697130203247, "[FF] Sensitivity of the LISA = Milky Way systems"]
-[10.261738777160645, 5.3709001541137695, "[FF] Thermal Control of the Satellite = Milli-Kelvin (mK) passive thermal control of the payload"]
-[10.830101013183594, 2.8109188079833984, "[TT] Goal Mission Life of the PARASOL microsatellite = Two years"]
-[7.621851444244385, -2.521380662918091, "[TT] Observation Date of the GOLD = November 4-5, 2018"]
-[5.642553806304932, 5.273187637329102, "[FF] Requirements of the GRDDP = Utilize the SpaceWire capabilities to provide a packet delivery protocol that is able to detect and recover lost packets"]
-[7.048888683319092, 3.2523255348205566, "[FF] Function of the CCRS = Handle and bio-seal the OS, provide the Earth Entry Vehicle (EEV)"]
-[8.402556419372559, 8.112614631652832, "[TT] Band of the SWIR Camera = 0.9 to 1.7 \u00b5m"]
-[3.4462833404541016, 2.10597562789917, "[FF] Host for Sentinel-4 of the MTG-S = True"]
-[9.840487480163574, 8.18404483795166, "[TT] Lens Optical Diameter of the ISIR = 70 mm"]
-[8.917558670043945, 5.601006984710693, "[TT] Antenna pointing accuracy of the AOCS = < 0.1\u00ba (3\u03c3) half cone"]
-[8.51369571685791, 4.771660804748535, "[FF] Function of the Starfire Optical Range = Develop optical sensing, imaging, and propagation technologies"]
-[4.485649108886719, 1.845599889755249, "[FF] Space Radiation Environment Analysis Date of the EgyptSat-1 = October 5-9, 2008"]
-[6.43332052230835, 4.705307483673096, "[FF] Control Mode of the CVX = Autonomous, but in the most desirable scenario it is being controlled interactively via ground commands"]
-[6.292793273925781, -0.257488489151001, "[TT] Autonomous Operations of the CDMU = Up to 48 hours"]
-[9.023711204528809, 5.525156021118164, "[TT] Pointing Accuracy of the Spacecraft = 360 arcsec"]
-[8.282819747924805, 7.691845417022705, "[TT] Counting Ability of the Particle Detector = 5\u00d710 4  event/s"]
-[2.9429516792297363, 2.381770372390747, "[FF] Nitrogen Dioxide Emission Reduction of the Copernicus Sentinel-5P = Decline of air pollution, specifically nitrogen dioxide emissions, over Italy"]
-[5.7736101150512695, 3.0902974605560303, "[FF] Funding Round Amount of the Aleph-1 Constellation = $27 million"]
-[11.648810386657715, 6.8517842292785645, "[TT] Energy of the ART-XC = Up to30 keV"]
-[8.264699935913086, 0.021016838029026985, "[TT] Sea-Level Anomaly of the TOPEX/Poseidon = Over 10 cm"]
-[8.597150802612305, 0.12568210065364838, "[TT] Scalability of the Comet = Available"]
-[5.495622634887695, 6.065591335296631, "[TT] EEPROM of the Model calculator = 256 kB"]
-[10.38704776763916, 5.619725227355957, "[TT] Maximum Heat Flux of the Hayabusa-2 SRC = 13 MW/m2"]
-[6.373419761657715, 4.7337117195129395, "[FF] Function of the MOC = Transfer science data"]
-[4.710368633270264, 7.037154197692871, "[TT] Data Downlink of the LEOStar-3 = X-band, data rate of 220 Mbit/s"]
-[8.42541217803955, 0.9427542090415955, "[TT] Observation Purpose of the DPS = Snow water equivalence and freeze/thaw"]
-[6.772988796234131, 4.813571453094482, "[FF] Function of the ISL = Provide time correlation and synchronization between the two satellites, enable the exchange of formation control data among the platforms and determine their relative distance during the complete orbit including the precise formation flying maneuvers"]
-[10.96993350982666, 5.839396953582764, "[TT] Gate-Oxide Thickness of the RadFETs = 400 nm"]
-[13.584003448486328, 5.539947986602783, "[TT] Solar-Battery Cells of the PDL = 55,680"]
-[8.341382026672363, 6.048565864562988, "[TT] Accuracy at 511 keV of the XGRE = 9%"]
-[11.199796676635742, 1.0240859985351562, "[FF] Detectable Binaries of the LISA = Dozens"]
-[10.362412452697754, 3.230954885482788, "[TT] Platform Standard of the OPTOS = CubeSat"]
-[10.599870681762695, 3.8908681869506836, "[FF] Formation Flying Mission of the CanX-4/CanX-5 = One Month"]
-[4.953735828399658, 8.437639236450195, "[TT] Spectral Band of the MIVZA = 20.0-94.0 GHz"]
-[7.701534271240234, 6.814825057983398, "[TT] Cadence of the Normal Cameras = 25 seconds"]
-[12.4319486618042, 0.6242935061454773, "[TT] Number of Normal Cameras of the PLATO = 24"]
-[6.062287330627441, 6.4965434074401855, "[TT] Latency of the ATL02 Science Unit = 2 days"]
-[6.239879608154297, 2.012373685836792, "[FF] URL of the OPS-SAT = http://esamultimedia.esa.int/docs/gsp/C4000108683ExS.pdf"]
-[8.011307716369629, 3.341953754425049, "[TT] Measurement Category of the TARANIS = Lightning Detection"]
-[9.63453483581543, 4.056113243103027, "[TT] Interplanetary Vector Magnetic Field Measurement Range of the DSCOVR = 0 \u2013 100 nT"]
-[11.762640953063965, 6.795341968536377, "[TT] Energy Range of the TED = 0.05 to 20 keV"]
-[7.491727352142334, 5.85214900970459, "[FF] Transmission Method of the Full Frame Images = Transmitted to ground"]
-[11.783303260803223, 3.2686173915863037, "[TT] Quantity of the Propulsion thrusters = 2 x 8 x 1N Monopropellant, 2 x 12 x 10 mN Cold Gas"]
-[5.378255844116211, 3.1047310829162598, "[TT] Sponsor of the BEPT = NIVR"]
-[5.115818500518799, 3.2870895862579346, "[TT] Manufacturer of the Dragsail = Surrey Space Centre (UK)"]
-[4.887621879577637, 3.1171157360076904, "[TT] Manufacturer of the SARah-1 = Airbus"]
-[4.421151638031006, 7.105062961578369, "[TT] Ka-band Repeater of the Repeater subsystem = 5/3 simultaneously operating transponders at saturation"]
-[10.986298561096191, 7.629383563995361, "[TT] Swath Width of the Wide Standard Quad-Polarisation Mode = Approximately 50 km"]
-[7.236208438873291, 8.192889213562012, "[TT] Sensitivity of the Channel 6 = 0.4 K/pixel"]
-[9.58215045928955, 4.495768070220947, "[FF] Spin Rate of the Stars = Varies"]
-[2.9056589603424072, 1.9555163383483887, "[FF] Image Capture Date of the Copernicus Sentinel-2 = June 2020"]
-[14.331469535827637, 3.1089682579040527, "[TT] Mass of the S/C mass = 60.7 kg"]
-[9.416265487670898, 8.121183395385742, "[TT] Field of View of the Supervision Cameras = 17\u00ba x 14\u00ba"]
-[5.174666404724121, 4.771708011627197, "[TT] Chip Set of the GPS receiver = MITEL chip set"]
-[7.632077217102051, 5.66213846206665, "[FF] Information Delivery of the LiDAR = Target distance"]
-[10.615832328796387, 1.717004656791687, "[FF] Measurement Capability of the NICER = Neutron star's rotation rate"]
-[5.220525741577148, 3.0805444717407227, "[TT] Developer of the NewMag = University of Newcastle"]
-[3.036303758621216, 2.0541977882385254, "[FF] Announcement Date of the Copernicus = December 11, 2012"]
-[3.4516589641571045, 6.3704657554626465, "[TT] Electric Antennas Length of the ISEE-3 = 0.6 and 45 m"]
-[8.114684104919434, 2.5921216011047363, "[FF] Measurement Domain of the GIIRS = Ocean, Land"]
-[7.999271869659424, 4.281158447265625, "[FF] Parameter of the Multiple direction/polarisation radiometers = Atmosphere"]
-[5.483683109283447, -1.796238660812378, "[TT] Launch Date of the KOMPSAT-2 = 27 Jul 2006"]
-[11.681522369384766, 6.600205898284912, "[TT] FSH Measurement of the LCI = 50 \u2013 700 keV electrons"]
-[8.93332290649414, -0.08936119824647903, "[TT] Distance to EML-2 of the Queqiao = 60-80,000 km"]
-[8.48958969116211, 2.310760021209717, "[FF] Communication Modes of the WINDS = Regenerative mode, bent pipe mode relay"]
-[6.0145440101623535, 6.805075168609619, "[TT] Number of DCPs in Visibility Zone of the Onboard data collection and transmission system = 150, < 500"]
-[3.7711591720581055, -1.1668956279754639, "[TT] Orbit Position of the Vigil = L5 (Langrage Point 5)"]
-[6.043993949890137, 1.721435308456421, "[FF] URL of the PRISMA = http://elib.dlr.de/46839/1/ESA4S_06_10a.pdf"]
-[6.056036472320557, 4.147585868835449, "[FF] Integration Levels of the Cooperation by Expansion = Within CSK boundaries and with other EO systems"]
-[6.656416416168213, 4.617084503173828, "[FF] Data Provider of the RADMON = Aalto-1"]
-[12.957369804382324, 7.3714375495910645, "[TT] Power Consumption of the POLDER-P = 50 W in imaging mode (mean power of 29 W)"]
-[9.030437469482422, 5.112037181854248, "[TT] Quantity of the Attitude Gyro = 4 in cold redundancy"]
-[7.515167236328125, 5.4165239334106445, "[FF] Components of the INMS = Front-end optics, post acceleration, gated time of flight, ESA (Electrostatic Analyzer) and CEM (Channel Electron Multiplier) or MCP (Micro Channel Plate) detectors"]
-[10.313126564025879, 5.555362224578857, "[TT] Thermal Operating Range of the SeaWinds = 5-40\u00baC"]
-[8.231456756591797, 2.8105130195617676, "[TT] Measurement Domain of the Odin = Atmosphere"]
-[9.828767776489258, 8.714597702026367, "[TT] Parameter of the FOV = \u00b143\u00ba (swath = 1600 km)"]
-[10.529562950134277, 1.807288408279419, "[FF] Purpose of the NICER = Provide both unique insights into neutron star physics and validation of a technology that may one day lead humanity into deep space"]
-[8.25712776184082, 6.743183612823486, "[FF] Detectors of the SBUV = Photomultiplier tube (PMT) and a photodiode for the monochromator, and one photodiode for the photometer"]
-[5.4364542961120605, 6.401413917541504, "[TT] Capacity of the Onboard Data Storage = ~ 350 Mbit"]
-[13.512446403503418, 5.589042663574219, "[TT] Number of Solar Panels of the EPS = 7"]
-[8.300640106201172, -0.5988178849220276, "[TT] Absolute Accuracy of the Ice: area covered = \u00b1 12%"]
-[6.632148742675781, 0.14813663065433502, "[TT] Repeat Coverage of the Landsat-9 = 16 days"]
-[9.45766830444336, 4.001643180847168, "[TT] End of Life Date of the Fluxgate magnetometer = 31 May 2021"]
-[8.187774658203125, -0.922129213809967, "[TT] Spatial Resolution of the ICESat\u20102 = 1 km"]
-[10.115792274475098, 2.3856818675994873, "[FF] Localization of the Fermi-GBM = Larger"]
-[3.4811840057373047, -0.9666860103607178, "[TT] Orbit Type of the SPROUT = Sun-synchronous near-circular orbit"]
-[4.913339614868164, 2.2377960681915283, "[TT] Service Entry of the Eutelsat 172B = Fourth quarter of 2017"]
-[13.318702697753906, 5.359072685241699, "[TT] Solar Panel Deployment of the Sentinel-2B = Complete"]
-[8.52060317993164, 5.398947238922119, "[TT] Orbit Determination Accuracy of the AutoNav = <1000 km in position and <0.4 m/s in the velocity vector"]
-[8.39709186553955, 6.053700923919678, "[TT] Accuracy Improvement of the SORCE / TIM = Tenfold"]
-[9.225151062011719, 7.1040940284729, "[TT] Spatial Resolution of the HSC = 300 m"]
-[9.32689380645752, -0.680439293384552, "[TT] Orbit of the CXS-810C = 6,000 km x 12,000 km"]
-[10.69644546508789, 2.860041379928589, "[FF] Architecture of the Microsatellite = Single string hardware architecture"]
-[4.528724670410156, 6.828813076019287, "[FF] Communication Link of the Bus = S-band radio frequency (RF) link"]
-[6.792827606201172, 6.588006973266602, "[TT] Spectrum Acquisition Time of the SOLSPC = 11 minutes"]
-[10.014683723449707, 2.8635544776916504, "[FF] Interface Control Document Date of the NanoRacks CubeSat Deployer = Dec. 10, 2013"]
-[11.689264297485352, 4.561185359954834, "[TT] Dimensions of the ALOS-3 = 9.9 m x 16.6 m x 3.7 m"]
-[6.090336799621582, 8.014938354492188, "[TT] Type of the E-cal Signal = Sixteen step staircase"]
-[3.849641799926758, 6.293470859527588, "[TT] Beam Steering Range of the Antenna = 8\u00ba (half cone angle)"]
-[6.773379802703857, 5.929574966430664, "[TT] Mode of the Operational mode = Continuous"]
-[6.081277370452881, 1.5649709701538086, "[FF] Date of the 32nd Space Symposium = April 11-14, 2016"]
-[9.796440124511719, -0.27062925696372986, "[TT] Burn Altitude Change of the EURECA = From 420 km to 508 km"]
-[10.262986183166504, 5.297051429748535, "[FF] Function of the Cooling System = Move heat away and dissipate it into cold space"]
-[5.131261825561523, 3.2259507179260254, "[TT] Manufacturer of the Eagle-1 (BeakerSat) = MSU (Morehead State University)"]
-[10.168825149536133, 6.940009593963623, "[TT] Ground Track Velocity of the ICIR = Approximately 7 km/s"]
-[13.397698402404785, 7.114434242248535, "[TT] Transmitter Power of the Spacecraft Repeater = 8 W"]
-[12.852049827575684, 5.496609687805176, "[TT] Panel Type of the Collector Arrays = Individual hexagon collectors"]
-[11.469809532165527, 4.641781330108643, "[TT] Diameter of the Corner cube = 50 mm"]
-[8.30203628540039, 4.735433101654053, "[FF] Bias Estimation of the Overall System = Use of surface return"]
-[6.506458759307861, 3.1303536891937256, "[FF] Objective of the Kent Ridge 1 = Integrate a VNIR/SWIR FTR (Fourier Transform Recovery) instrument into a microsatellite in support of disaster monitoring in Asia"]
-[9.686922073364258, 6.170562267303467, "[TT] Motors of the Steering Mirror Mechanism = Two coreless DC motors"]
-[7.353997230529785, 6.618547439575195, "[TT] Minimum Detectable Pulse of the Rangefinder Module = 6 photons"]
-[5.665060997009277, 0.5713694095611572, "[FF] Report Date of the GEOS-1 = Jan. 1977"]
-[7.983084678649902, 0.14554919302463531, "[FF] Application Area of the GRACE-FO = Monitoring water storage, ice sheets and glaciers, sea level, and solid earth"]
-[8.306221961975098, 3.792912244796753, "[TT] Components of the AMO = Atomic Oxygen Fluence Sensor (AOFS) and the Material Degradation Monitor (MDM)"]
-[6.592159271240234, 5.369281768798828, "[FF] Components of the FEU = Preamplifiers, FPGA, ADC, HMB"]
-[7.140846252441406, 5.305749416351318, "[FF] Components of the VBS = WAC, NAC, ISM, MOH, AMU, STR CHU, MIRU, DPU"]
-[9.369071960449219, 3.339203357696533, "[FF] Magnetic Field of the Earth = Protective shield, repelling and trapping charged particles from the Sun"]
-[5.516262054443359, 2.058018684387207, "[FF] Mission Status of the BeiDou-1 = Unknown"]
-[6.128052711486816, 2.26042103767395, "[FF] Members of the Euclid Consortium = Teams of researchers in theoretical physics, particle physics, astrophysics and space astronomy, engineers, technicians, and management and administrative staffs"]
-[6.727381229400635, 3.6660094261169434, "[FF] Components of the AMS Payload = AMS Experiment, AMS Payload Integration Hardware (PIH)"]
-[5.301649570465088, 6.806733131408691, "[TT] Downlinked Data of the Mission Operation System = 100 GB/day"]
-[5.948464870452881, 2.04106068611145, "[FF] Service Module Assembly Start Date of the Orion = May 19, 2016"]
-[7.342297554016113, 3.9641568660736084, "[FF] Monitoring of the Visual Inspection Poseable Invertebrate Robot 2 (VIPIR2) = Make sure tools are properly positioned"]
-[6.926427364349365, 5.0137457847595215, "[FF] Data Latency of the SENSE = Operational SEM data latency requirements are satisfied"]
-[11.200177192687988, 0.6230431795120239, "[FF] Function of the Cheops = Measure minuscule brightness changes due to the planet\u2019s transit across the star\u2019s disc"]
-[4.694430351257324, 6.283410549163818, "[FF] Communication Capability of the IME-HF = Communicate with the spacecraft, even when it is out of visibility from ground antenna"]
-[6.713739395141602, 2.039689302444458, "[TT] Expected Data Collection of the Nancy Grace Roman Space Telescope = More than any of NASA\u2019s other astrophysics missions"]
-[5.310115814208984, 6.8436713218688965, "[TT] Payload Data Rate of the LDCM spacecraft = 440 Mbit/s"]
-[8.04162311553955, 8.49356746673584, "[TT] Wavelength Range of the IR Channel = 1.3 \u2013 4.5 \u00b5m"]
-[9.798629760742188, 2.714398145675659, "[TT] Integration Location of the HaloSat = BCT"]
-[7.719667434692383, 2.045863628387451, "[FF] Purpose of the BeaverCube = Gather important ocean and atmospheric measurements"]
-[5.004205703735352, 7.393771648406982, "[TT] Data Transmission Rate of the RF Communications = 2 Mbit/s"]
-[4.719961643218994, -1.808251976966858, "[FF] URL of the Chang'E-1 = http://www.cjss.ac.cn/qikan/manage/wenzhang/2008-05-03.pdf"]
-[8.88210391998291, 5.669647216796875, "[TT] Pointing Accuracy of the Telescope = 10\u00ba"]
-[6.879678249359131, -0.6386483311653137, "[TT] Osculating Orbital Period of the SMART-1 = 4.978457 hours"]
-[4.777885913848877, 0.9552828073501587, "[TT] System CDR Date of the PROBA-V = Spring of 2011"]
-[3.3875510692596436, 2.2708325386047363, "[FF] Data Access Level of the SAPHIR and SCARAB = 1A and 1A2"]
-[9.259955406188965, 1.8147120475769043, "[TT] Hit Position of the Harpoon = Center"]
-[11.626456260681152, 4.742687702178955, "[TT] Structure of the S/C = Cube (60 cm x 60 cm x 60 cm)"]
-[5.632347583770752, 1.0821995735168457, "[TT] First Image Date of the MSU-MR = July 25, 2014"]
-[5.151397228240967, 0.20432505011558533, "[FF] Program Launch Date of the Polar Scout = 11 December 2018"]
-[4.782653331756592, -1.839166522026062, "[FF] Power Descent Phases of the Chang'e-4 = Oblique forward motion trajectory to vertical down trajectory, Pointing of ranging consistent with the location of the landing point"]
-[5.317141056060791, 6.428702354431152, "[TT] Module power (max data rate) of the SDR-SMM = 14 W"]
-[9.371017456054688, 5.059908390045166, "[TT] Attitude Control Stability of the Spacecraft = 1 arcmin rms (or FWHM of ~2.2 arcmin)"]
-[8.98023796081543, 0.5314886569976807, "[FF] Conference Presentation Date of the ARTEMIS = July 31- Aug. 4, 2011"]
-[7.725272178649902, 6.870477199554443, "[FF] CCDs Read-Out Chain of the MATS = Characterized"]
-[11.654230117797852, 3.3437137603759766, "[FF] Thruster Type of the Cold Gas System = 16 attitude control thrusters, 4 orbit control thrusters"]
-[5.9485554695129395, 0.2229190617799759, "[TT] Arrival Date of the JUICE = 2029"]
-[4.280930519104004, 7.373039245605469, "[TT] Downlink Frequency of the RF Communications = X-band (8345.968-8346.032 MHz)"]
-[14.371212005615234, 6.8909101486206055, "[TT] Battery Nominal Voltage of the S/C = 3.7 V"]
-[9.260598182678223, 6.638603210449219, "[TT] Resolution of the ASC = 6 arcsec or less"]
-[7.794320583343506, 2.9760167598724365, "[TT] Developer of the CO2M Monitoring and Verification Support Capacity = ECMWF (European Centre for Medium-Range Weather Forecasts)"]
-[14.239832878112793, 3.2833211421966553, "[TT] Grid Weight of the CVX\u20132 Device = Less than 1 mg"]
-[6.068550109863281, -1.9458173513412476, "[TT] Member of the Mark Bourassa = True"]
-[8.229911804199219, 6.607814311981201, "[FF] Support Mode of the SLIM6 = Strip Real-Time Imaging"]
-[9.364853858947754, 3.8487164974212646, "[FF] Function of the VMAG = Measures the local magnetic field"]
-[5.064897537231445, 1.017196774482727, "[TT] Launch Date of the Ax-1 mission = No earlier than January 2022"]
-[9.72957992553711, 8.390497207641602, "[TT] FOV of the MSU-E = 2.5\u00ba"]
-[8.204123497009277, 2.6126084327697754, "[FF] Orbit of the ISS = Passes over and along many of the primary aerosol transport paths within the atmosphere"]
-[13.478385925292969, 5.749955177307129, "[TT] Solar Array Output of the EPS = 1418 W (EOL)"]
-[5.001786708831787, 0.4570217430591583, "[TT] Critical Design Review Completion Date of the WSF-M = April"]
-[6.572811603546143, 6.908843040466309, "[TT] Duty Cycle of the VRSS-1 = 10%"]
-[5.013433456420898, 3.4568796157836914, "[TT] Developer of the PIRPL = Northrop Grumman"]
-[6.288873195648193, 3.8781890869140625, "[FF] Mission Analysis of the COSMOS = Analysis and trending of spacecraft and ground network SOH data, orbital and trajectory data, and mission accomplishment data"]
-[5.469592571258545, 7.02442741394043, "[TT] Data Transmission Rate of the Onboard data collection and transmission system = 1200 or 400 bit/s"]
-[8.106959342956543, 8.753765106201172, "[TT] Phase of the UV2VIS SO = PDR (Preliminary Design Review)"]
-[8.05379581451416, 8.81312370300293, "[TT] Spectral Ranges of the CarbonSpec = Oxygen A-band at 758nm - 778 nm, Carbon dioxide bands: 1594-1624 nm, 2042 nm-2082 nm"]
-[9.372941970825195, 8.457493782043457, "[TT] Ensquared Energy of the Lens = 50% within 15 x 15 \u00b5m"]
-[10.74170970916748, 0.9541798233985901, "[TT] Mass of the TOI-148, TOI-587, TOI-681, TOI-746, TOI-1213 = Between 77 and 98 times more massive than Jupiter"]
-[3.458850860595703, -0.9063206911087036, "[TT] Orbit of the AERO-VISTA mission = Sun-synchronous, near-polar orbit"]
-[6.5764641761779785, 7.692895412445068, "[TT] Pixel Quantization of the Telescope = 12 bit plus 1 bit for low and high gain setting"]
-[5.292726516723633, 2.1724374294281006, "[FF] Complexity of the EIRSAT-1 = Equivalent to a standard space mission"]
-[10.79316520690918, 6.125019550323486, "[TT] Best Energy Resolution Temperature of the pnCCD = Below -60\u00ba C"]
-[8.677937507629395, 3.7243876457214355, "[FF] Measurement Record of the TIM = Extends a 40-year measurement of the Sun's total energy to Earth"]
-[13.71427059173584, 2.9144442081451416, "[TT] Aquarius Assembly Mass of the SAC-D spacecraft = 375 kg"]
-[4.336782455444336, 7.389734268188477, "[TT] Downlink Frequency of the Transponders = S-band"]
-[1.7130779027938843, 6.145979404449463, "[FF] Composition of the Normal Matter = ~5%"]
-[9.092511177062988, 1.358052372932434, "[TT] Communication Status of the Voyager 2 = Without receiving commands from Earth"]
-[7.330075263977051, 3.506068706512451, "[FF] Pass Frequency of the Satellite = Once per orbit"]
-[7.975111961364746, 8.470974922180176, "[TT] Spectral Coverage of the ILAS-II = 3-12.85 \u00b5m and 753-784 nm"]
-[5.816900253295898, 7.545560359954834, "[TT] Pulse Repetition Frequency (PRF) of the PR = 2776 Hz"]
-[4.41532039642334, 3.1089484691619873, "[TT] Location of the TANSO-FTS = Melbourne FL USA"]
-[6.062225818634033, -0.26472076773643494, "[TT] Operation Duration of the RadSat = ~12 months"]
-[9.457988739013672, 3.9312634468078613, "[FF] Technology of the MI/RadFET = Magnetic sensors"]
-[9.865499496459961, 8.723715782165527, "[TT] IFOV of the Pan = 3.68 \u00b5rad"]
-[9.32906436920166, 7.340631484985352, "[TT] Imagery Resolution of the FormoSat-2 = 2m in Pan, 4 m MS"]
-[7.474475383758545, 5.0853071212768555, "[TT] Moving Parts of the BRITE = None"]
-[8.31839370727539, 6.892472267150879, "[FF] Instrument of the Cheops = Detector"]
-[10.384937286376953, 4.5104169845581055, "[TT] Quantity of the Reaction wheels = Three"]
-[11.307580947875977, 2.7500743865966797, "[TT] Mass of the Microsatellites = < 100 kg"]
-[8.164631843566895, 5.4554829597473145, "[FF] Manufacturer of the DORIS = Unknown"]
-[9.5767822265625, 9.177352905273438, "[FF] Designer and Builder of the IRIS Imager = SI (Satrec Initiative Co. Ltd.) of Daejeon, Korea"]
-[4.939992427825928, 4.001530647277832, "[TT] Number of Galileo FOC satellites of the MEOSAR satellite constellation = 2"]
-[9.964269638061523, 5.666733264923096, "[TT] Operation Temperature of the ASTERIA = Room temperature"]
-[5.289682865142822, 0.45541366934776306, "[FF] Publication Date of the Rise of the Titans = 13 Nov. 2017"]
-[13.660089492797852, 3.253451108932495, "[FF] Mass of the AeroCube-1 = Unknown"]
-[4.222470760345459, 4.301438808441162, "[FF] Participants Associated with the Management of the COSPAS-SARSAT = 9"]
-[11.787092208862305, 6.749955177307129, "[TT] Energy Range of the HEAO-1 A2 = 3 to about 45 keV"]
-[6.483017444610596, 4.27669620513916, "[FF] Collection Mode of the QuakeSat = Unknown"]
-[7.98957633972168, 6.035640716552734, "[FF] Photon Number Calculation of the Cameras = Source radiance and its duration, the characteristics of the optics and the filter and the distance from the source to the satellite"]
-[11.834577560424805, -0.006582140922546387, "[FF] Far-flung Supernovae of the TESS = Unknown"]
-[10.927478790283203, 7.529409885406494, "[TT] Swath Width of the HSC = 700 km"]
-[5.804378032684326, 3.09033465385437, "[FF] Funds Raised of the Inspiration4 = $29.2 million"]
-[10.29679012298584, 5.795622825622559, "[TT] NE\u0394T @ specified scene temperature of the Instrument = 0.3-1.2 K @ 250 K"]
-[7.838373184204102, 5.69956636428833, "[TT] Measurement Type of the Microwave Imager (MWI) = Calibrated passive radiometric measurements at multiple microwave frequencies"]
-[6.082487106323242, 5.908730983734131, "[TT] Antenna Array of the TR Module = 12 modules"]
-[9.90320110321045, -0.28342369198799133, "[TT] Deployment Altitude of the Stingray = Approximately 500 km"]
-[8.393813133239746, 7.567563056945801, "[TT] Dimensions of the CCD detector array = 1024 x 1024"]
-[6.897071361541748, 2.303514003753662, "[FF] Plaque Content of the LAGEOS = Binary numbers, Earth orbiting the sun, Maps of Earth at different epochs"]
-[5.263871192932129, 1.2016818523406982, "[FF] Copyright of the eoPortal = \u00a9 2024"]
-[10.74854850769043, 1.120516300201416, "[FF] Description of the White Dwarf = White dwarfs are the collapsed, burned-out remains of stars not massive enough to explode in supernovae"]
-[8.176176071166992, 5.691857814788818, "[FF] Calibration of the Advanced Land Imager = Spectral and Radiometric"]
-[11.42197036743164, 4.397934913635254, "[TT] Size of the GRIFEX = 3U"]
-[9.128949165344238, 4.642287731170654, "[TT] Perigee Pass Sun Pointing of the Activity Attitude = 161\u00ba"]
-[8.326813697814941, 1.6742520332336426, "[TT] Temporal Sampling of the Sea Surface Temperature (SST) = Sub-daily"]
-[7.378082275390625, 3.233638286590576, "[TT] Data Sharing Resolution of the GHGSat = 50 m2"]
-[4.131494045257568, 4.246343612670898, "[FF] Ground Segment Development Completion of the RADARSAT-2 = Almost a decade after launch"]
-[9.058210372924805, 8.305665969848633, "[TT] Swath Width of the Imaging Spectrometer = 260 km"]
-[5.5668511390686035, 5.44717264175415, "[TT] Interface of the Personal Computer = USB"]
-[4.719479560852051, 7.327356338500977, "[TT] X-band Data Rate of the RF Communications = 10 Mbit/s"]
-[5.0437188148498535, 4.276605606079102, "[TT] Service Availability of the Ground Station = >97%"]
-[13.755273818969727, 2.9051501750946045, "[TT] Mass of the Spacecraft = 12 kg"]
-[6.771638870239258, 1.8258041143417358, "[FF] URL of the LAGEOS-1 = http://www.nasa.gov/feature/goddard/2016/now-40-nasas-lageos-set-the-bar-for-studies-of-earth"]
-[4.253207206726074, 7.219020366668701, "[TT] Frequency Band of the RF Communications = S-band"]
-[9.787515640258789, 8.627017974853516, "[TT] FOV of the Long Wavelength Band = 8\u00ba x 5'"]
-[4.443638801574707, 7.322341442108154, "[TT] Uplink Band of the SAS&R = Extended C-band"]
-[8.194513320922852, 8.249436378479004, "[FF] Slit Masks of the IR Instrument = Present"]
-[6.241494655609131, 6.993907451629639, "[TT] Data Rate of the SIOS Optical Link Demonstration Board = 100 Mbit/s"]
-[7.681915283203125, -0.9171677827835083, "[TT] Operational Status of the ICESat-2 = On all the time"]
-[10.645615577697754, 2.836540460586548, "[FF] On-board Computer of the Microsatellite = Not implemented"]
-[3.3597781658172607, -0.8308109641075134, "[TT] Orbit Compatibility of the Carbonite-1 = Sun-synchronous and low inclination orbits"]
-[6.350227355957031, 1.3292187452316284, "[FF] URL of the BepiColombo = http://sait.oat.ts.astro.it/MSAIS/20/PDF/127.pdf"]
-[10.083404541015625, -1.5014894008636475, "[TT] Inclination of the Satellite Constellation = 105.6\u00ba"]
-[7.2270026206970215, 0.9254978895187378, "[TT] Power Failure Date of the SeaSat = October 8, 1978"]
-[5.600194931030273, 6.8942131996154785, "[TT] Data Stream Treatment Capacity of the PLCDHS = 48 Mbit/s"]
-[5.215241432189941, 7.014951229095459, "[TT] Data Downlink Speed of the Payload = 4 Gbit/s"]
-[5.326502799987793, 7.590477466583252, "[TT] PRF of the HPA = 3050 Hz"]
-[3.890184164047241, -1.2674998044967651, "[TT] Mission Position of the IMAP = First L1 (Lagrange point)"]
-[7.939035415649414, 8.98086166381836, "[TT] Wavelengths of the EPIC = 10"]
-[8.475618362426758, 6.906060695648193, "[FF] Image Quality of the SMART = Better than direct imaging and PAIS"]
-[7.918673992156982, 3.1735680103302, "[TT] Absorption at 1.4 \u00b5m of the Water (H2O) = 10 -19 mol cm -2"]
-[10.467419624328613, 3.213878870010376, "[TT] VPU of the Ubotica CogniSAT-XE1TM CubeSat Board = Intel\u00ae Movidius\u2122 Myriad\u2122 2"]
-[13.417890548706055, 5.404694557189941, "[TT] Solar Array Paddles of the ALOS-2 = Two"]
-[2.9060161113739014, 4.560471534729004, "[TT] Wave Length of the PALSAR-2 = about 24 cm"]
-[6.447202205657959, -0.6886879205703735, "[TT] Contact Time with Spacecraft of the MOC = Eight hours per day"]
-[13.44076919555664, 6.790102958679199, "[TT] Power Generation of the Spacecraft = 48 W"]
-[6.9337968826293945, 6.5831475257873535, "[TT] Registration Time of the RGD = 20 ms"]
-[7.462401390075684, -0.04863154515624046, "[FF] Mission Status of the Philae = Unknown"]
-[6.707311153411865, -0.5498154163360596, "[TT] Period of the LAGEOS = 225 min"]
-[6.556689739227295, 5.263221740722656, "[TT] Function of the Instrument Control Unit (NI-ICU) = Housekeeping management"]
-[9.206583976745605, 8.071080207824707, "[TT] Pixel Resolution of the Focal Plane Assemblies = 2048 x 2048 pixels"]
-[6.20391845703125, 4.896610260009766, "[FF] Function of the Bus = Provides the structural, power, and communications interfaces to the payload"]
-[6.3035383224487305, 4.827239036560059, "[FF] Onboard System of the CAPSTONE = Communications system"]
-[8.490058898925781, 7.986215114593506, "[TT] Spectral Band (MS B2) of the Pushbroom imager = 0.53-060 \u00b5m"]
-[9.070884704589844, 5.153441429138184, "[FF] Objectives of the TDP = Technology demonstration Position, velocity and time inertial angular velocity determination"]
-[9.644095420837402, -0.4184504747390747, "[TT] Altitude of the GCOM-W1 = 699.6 km"]
-[9.255914688110352, 3.1989738941192627, "[FF] Image Capture of the Pumbaa and Timon smallsats = Solar corona\u2014including the region that is 10 times the Sun\u2019s angular diameter"]
-[7.182746887207031, 5.040019512176514, "[FF] Components of the HSB = AM (Avionics Module), PM (Payload Module) structure, harness, ESPA (EELV Secondary Payload Adapter) ring"]
-[6.918497562408447, 5.74569845199585, "[TT] Information Provided of the \u00b5SCIA = Total column amount"]
-[7.937533855438232, 5.068199634552002, "[FF] Design Considerations of the SAS = Mechanical loads, stiffness, mass and frequency response"]
-[14.531914710998535, 6.577085494995117, "[TT] Battery Type of the Sail = Lithium-ion"]
-[7.880108833312988, 8.027835845947266, "[TT] Bandwidth of the Band Photometers = 90 nm"]
-[3.6799509525299072, 4.805003643035889, "[TT] XF Mode of the RADARSAT-2 = 5 m resolution, 125 km swath width"]
-[5.508001327514648, 3.3721554279327393, "[TT] Host Satellite of the GOLD = SES-14"]
-[5.687942028045654, 0.6664812564849854, "[FF] Spacewalk Installation Date of the UrtheCast = Jan. 2014"]
-[5.341782093048096, 3.870805263519287, "[TT] Number of Images of the Sentinel 2 = Over 400"]
-[8.716630935668945, 8.453363418579102, "[TT] Spatial Resolution of the Spectrometer = 4.5 km x 9 km"]
-[5.609163284301758, -2.050745725631714, "[TT] Observation Capability of the KOMPSAT-5 = Left or right-looking"]
-[7.479081630706787, 5.484646320343018, "[FF] Components of the LRI = Laser, cavity assembly, ranging processor, measurement optics, steering mirror assembly"]
-[9.867862701416016, 8.151440620422363, "[TT] Diameter of the Focal Plane = 11.23 mm"]
-[14.393776893615723, 3.1331729888916016, "[TT] Mass of the MKA-N 1 = 10 kg"]
-[6.534086227416992, 3.5854249000549316, "[FF] Function of the Refabricator = Closed-loop recycler and 3D printer"]
-[3.9101150035858154, 2.177359104156494, "[TT] Launch Vehicle of the TerraSAR-X = Russian/Ukrainian Dnepr-1"]
-[9.04463005065918, 3.347007989883423, "[FF] Electric Fields Forecast of the C/NOFS = Pre-reversal enhancement strength"]
-[10.82974624633789, 2.139777183532715, "[TT] Brightness Change Time Scales of the XMM-Newton = Up to 14.5 years"]
-[9.624689102172852, 4.666919231414795, "[FF] Effect of the Hysteresis (Memory) Material = Provides the needed damping effect to stabilize KySat-2 on the two control axes, and resist changes on the uncontrolled axis as well"]
-[10.125337600708008, 7.540921211242676, "[TT] Field of View of the NIRST = \u00b137.8\u00ba"]
-[5.883137226104736, 0.882809042930603, "[FF] Observation Date of the RHESSI = SOL2017-09-10"]
-[3.2201693058013916, 5.7157511711120605, "[TT] Short Dimension of the SAR Antenna = 1.4 m"]
-[7.958514213562012, 8.996774673461914, "[TT] Frequency Range of the TOMS = 308.6 nm to 360 nm"]
-[9.078141212463379, 2.797492027282715, "[FF] Authors of the Ultra-impulsive Solar Flare Seismology = Angel D. Mart\u00ednez, Valeria Quintero Ortega, J. C. Buitrago-Casas, Juan Carlos Mart\u00ednez Oliveros, Benjam\u00edn Calvo-Mozo, and Charles Lindsey"]
-[4.506227970123291, -0.9063235521316528, "[TT] Departure Date of the Dragon spacecraft = Feb. 10, 2015"]
-[14.41351318359375, 3.3321478366851807, "[TT] Mass of the LISS-IIM = 80.8 kg"]
-[11.828222274780273, 3.2590813636779785, "[TT] Nominal Thrust of the Chemical Propulsion Thrusters = 10 N"]
-[10.02968978881836, 0.8168387413024902, "[TT] Capture Box Separation of the ASTRO = < 1 m"]
-[9.455604553222656, 5.084103107452393, "[TT] Roll Tilt Capability of the Satellite = \u00b135\u00ba"]
-[9.185951232910156, 5.353332042694092, "[TT] Attitude Jitter of the ADCS = 15.7 arcsec/sec"]
-[4.681865692138672, 0.9969807863235474, "[TT] Malfunction Date of the DORIS receiver = Nov. 1, 2004"]
-[4.646149158477783, 1.710602879524231, "[FF] Symposium Presentation Date of the TanSat = June 22-26, 2015"]
-[10.424556732177734, 2.1304831504821777, "[FF] X-ray Light Source of the SS 433 = Bright"]
-[8.597640991210938, 8.723240852355957, "[FF] Purpose of the Grating Reflection Unit = Manipulation and compression of high-power ultra-short laser pulses"]
-[4.145406246185303, 1.362216830253601, "[TT] Replacement Date for Meteosat-7 of the Meteosat-8 = First quarter of 2017"]
-[9.011225700378418, 0.9237539768218994, "[FF] View of Venus of the Parker Solar Probe = Stunning"]
-[13.545429229736328, 5.422455310821533, "[TT] Number of Cells per Array of the Solar Panel = 26"]
-[9.372194290161133, 7.446442127227783, "[FF] Ground Sample Distance of the AEISS = 0.7 m for the panchromatic band at nadir, and 2.8 m for multispectral bands at nadir"]
-[5.194894790649414, 2.0155227184295654, "[TT] Operation Status of the CHAMP = Mission complete"]
-[10.708589553833008, 6.535242557525635, "[FF] Optics of the NuSTAR instrument = Depth-graded multilayer coated grazing incidence optics"]
-[7.993104457855225, -0.6382625699043274, "[TT] Instrument of the CryoSat-2 = Radar altimeter"]
-[10.933171272277832, 7.505475997924805, "[TT] Swath of the HSC = \u00b1 700 km"]
-[4.034559726715088, 2.111448287963867, "[TT] Launch Program of the MakerSat = ELaNa XX program"]
-[6.127001762390137, 4.058431148529053, "[FF] Adaptability of the COSMOS = Easily adaptable for adding spacecraft, interfacing with external software, and porting to MOCs"]
-[3.9162306785583496, 7.879974842071533, "[FF] Signal Processing Capability of the LPT Demodulator = Phase shift keyed (PSK) and more general linear phase modulated (PM) signals, either spread or non-spread"]
-[5.325232028961182, 2.1089210510253906, "[FF] Mission Status of the MOMS = Mission complete"]
-[9.735215187072754, -0.46734321117401123, "[TT] Mean Altitude of the UniSat-3 = 750 km"]
-[8.773075103759766, 1.0045077800750732, "[TT] Range of measurements of the Land = Up to 16 km"]
-[4.874892711639404, 0.5101040601730347, "[TT] Scheduled Launch of the Hugo = By the end of the year"]
-[6.718219757080078, 6.044801712036133, "[TT] Modes of the ABI = Mode 3 and Mode 4"]
-[9.485947608947754, 8.95807933807373, "[TT] Video Format of the Iris Video Camera = Ultra High Definition and High Definition (H.264 encoding)"]
-[7.987851619720459, 6.388875961303711, "[TT] Observation Frequency of the TEMPO = Every 10 minutes"]
-[5.983458042144775, 6.044702053070068, "[FF] Isolation Among Output Ports of the MPA = High performance"]
-[12.732600212097168, 3.900162935256958, "[FF] Continuity of the Reconnection Process = Continuous along the dayside boundary"]
-[6.5831170082092285, 2.3196353912353516, "[FF] Image Credit of the NuSTAR = NASA/JPL, Caltech"]
-[4.925988674163818, 3.457219123840332, "[TT] Manufacturer of the ECS (Experimental Computer System) = Planning Systems Inc. (PSI)"]
-[14.25987720489502, 3.271191120147705, "[TT] Mass of the ANGELS = 30 kg"]
-[12.67004680633545, 3.8748300075531006, "[FF] Charged Particle Flow of the Magnetospheric Cusps = From the magnetosheath flow along the newly opened magnetic field lines into the cusps"]
-[13.93917465209961, 7.08752965927124, "[FF] Voltage of the TriTel Electrical System = 60 V"]
-[3.455820083618164, 6.1204729080200195, "[TT] Elevation Dimension of the Active Phased Array Antenna = 1.232 m"]
-[10.247206687927246, 5.377492427825928, "[FF] Thermal Control of the G\u00f6kt\u00fcrk-1A = Passive radiators along with a heater system"]
-[4.377474308013916, 1.8410691022872925, "[TT] Establishment Year of the RADARSAT International Ltd. = 1989"]
-[4.738250255584717, 0.7795950174331665, "[TT] Launch Date of the PROBA-3 = 2024"]
-[12.844858169555664, 7.577465534210205, "[TT] Power of the Instrument = 400 W"]
-[10.156816482543945, 3.188711166381836, "[FF] Parts of the CubeSat = Overall management, mechanical structure, power supply and power management subsystem, radio communication subsystem, controller subsystem, payload, ground station, public communication and value of the project"]
-[13.74092960357666, 2.9034664630889893, "[TT] Mass of the WINGS suite = ~ 0.850 kg"]
-[4.278320789337158, 7.310320854187012, "[TT] Ku-band Link Availability of the Bartolomeo = 70 - 90%"]
-[11.135823249816895, 1.0943655967712402, "[TT] Development of the Phasemeters = Pre-developed by ESA, NASA and the LISA consortium of ESA member states"]
-[7.493668556213379, -0.7207350134849548, "[FF] Constellation Proposal Date of the ICEYE = September 14, 2022"]
-[10.339920997619629, 5.791802406311035, "[TT] Blackbody Temperature of the SOLSPEC = 3300 K"]
-[5.575271129608154, 4.4481520652771, "[FF] Mission Success of the MarCO = Yes"]
-[5.307900905609131, 3.1357200145721436, "[TT] Developer of the Beijing-3 = Aerospace Dongfanghong (DFH) Satellite Co., Ltd"]
-[4.117811679840088, 1.447049617767334, "[FF] Proposal Acceptance of the Meteosat = 1972"]
-[7.499846935272217, 5.305279731750488, "[FF] Advantages of Digital Polarimetry of the MWI = Reduced complexity and better calibration performance than analog designs"]
-[6.789449691772461, 2.8825430870056152, "[FF] 3D Map Compilation Capacity of the DAICHI project = 150,000 maps per month"]
-[5.924285411834717, 1.6380635499954224, "[FF] Conference Presentation Date of the Starshine 3 Satellite = Aug. 13-16, 2001"]
-[5.861590385437012, -0.7728782296180725, "[TT] Service Life of the Aleph Satellite = Three years"]
-[7.818915367126465, 4.625676155090332, "[TT] Type of the MTVZA-GY = Atmospheric temperature and humidity sounders"]
-[7.106950283050537, -0.14757178723812103, "[TT] Number of Orbits of the DMSP-F13 = More than 100,000"]
-[9.243430137634277, 3.2128496170043945, "[FF] Observation Target of the EUVI = Chromosphere and innermost corona"]
-[7.217417240142822, 6.877686977386475, "[FF] Power Consumption of the APD = Low"]
-[3.928821563720703, 4.275876045227051, "[FF] Marine Pollution Monitoring Capability of the RADARSAT-1 = ISTOP (Integrated Satellite Tracking of Pollution)"]
-[5.153963088989258, 2.408163070678711, "[FF] Unknown of the Universat-Tatyana-2 = Unknown"]
-[8.695927619934082, 3.5908143520355225, "[FF] Solar Irradiance Measurements of the TRUTHS = Direct measurements of Earth incident solar irradiance, total and spectrally resolved"]
-[7.6905436515808105, 9.392337799072266, "[TT] Center Wavelength of the Band 6 = 12.66 \u00b5m (790 cm -1)"]
-[6.020084857940674, -0.5830280780792236, "[TT] Duration of the CRISTA/MAHRSI Campaign 2 = Three weeks"]
-[8.734436988830566, 5.335397243499756, "[FF] Probe Tips Contamination of the m-NLP = Design Challenge"]
-[9.666723251342773, -0.3961317241191864, "[TT] Altitude Range of the LEMUR-2 constellation = 400-600 km"]
-[11.54013729095459, 4.88967227935791, "[TT] Diameter of the EGS = 2.15 m"]
-[13.383665084838867, 5.49812650680542, "[TT] Quantity of the Solar Panels = 4"]
-[11.073025703430176, 6.0596513748168945, "[TT] Light Guide Material of the RICH = Polymethyl Methacrylate (PMMA)"]
-[8.96534252166748, 5.415014743804932, "[TT] Positioning Accuracy of the GOMX-3 = 7 km"]
-[4.59010124206543, 5.80820894241333, "[TT] False Alarm Rate of the Analog Distress Beacon Signals = 97 percent"]
-[6.485086441040039, 5.8094635009765625, "[TT] PRN of the GSAT-0206 = 30"]
-[4.445039749145508, 3.113356828689575, "[TT] Location of the Ground Station = Montpellier University campus"]
-[12.708276748657227, 1.927089810371399, "[FF] Data Usage of the SAGE-III on ISS = Assess the performance of OMPS flying on the Suomi-NPP satellite"]
-[10.79407024383545, 1.6981836557388306, "[FF] Mission Type of the INTEGRAL = Follow-up of Gravitational Wave Detections"]
-[6.319851875305176, 4.611690998077393, "[FF] Objective of the Intelligent Failure Detection, Isolation and Recovery System = Autonomous execution of the operational scenario"]
-[7.876874923706055, -0.9631076455116272, "[TT] ATLAS Instrument Status of the ICESat-2 = Nearly perfect working order"]
-[5.286358833312988, 2.900390863418579, "[TT] Developer of the Unicorn-2A = Alba Orbital UG (Germany)"]
-[10.18472957611084, 4.900321006774902, "[FF] Boiling of the Superfluid Helium = Throughout the lifetime of the experiment"]
-[5.139591217041016, 1.2724424600601196, "[FF] Conference Presentation of the ADM Aeolus = Functional Verification Of the ADM-AEOLUS Autonomy Requirements"]
-[11.467903137207031, 3.4926633834838867, "[TT] Minimum Impulse Bit of the CanX-4&5 = 0.1 mNs"]
-[5.2745866775512695, 6.358124732971191, "[TT] Microprocessor Clock Speed of the C&DH subsystem = 29.4 MHz"]
-[9.458403587341309, -1.3964492082595825, "[TT] Eccentricity of the Satellite = 0.8"]
-[5.40346622467041, 2.819108486175537, "[FF] CEO of the Maxar Space Solutions = Dan Jablonsky"]
-[8.998650550842285, 0.8520849943161011, "[TT] Flybys of the BepiColombo = 9 (at Earth, Venus and Mercury)"]
-[6.4056901931762695, 4.245140075683594, "[FF] Autonomy of the ESEX = Somewhat autonomous"]
-[7.824991703033447, 0.9398342370986938, "[FF] Date of the Severe Rainfall and Flooding in Japan = 10 July 2018"]
-[13.373931884765625, 6.810784816741943, "[TT] Power of the LADEE spacecraft = ~295 W"]
-[7.6883320808410645, 6.359994411468506, "[TT] Mesoscale #1 of the ABI = 0.5 minutes"]
-[10.299525260925293, 2.248110294342041, "[FF] Brightness Fluctuations of the SMC X-1 = Observed"]
-[9.630663871765137, 6.351539611816406, "[FF] Purpose of the Steering Mirror = To serve the feedback signal in the LRI"]
-[13.868118286132812, 3.0591483116149902, "[FF] Mass of the Pegasus = Unknown"]
-[4.431413650512695, 3.047224760055542, "[TT] Ground Stations of the Genesis-2 = Las Vegas, Virginia, Alaska, Hawaii"]
-[5.086505889892578, 0.7224422693252563, "[FF] Date of the SLAP = 2015"]
-[7.074063301086426, 6.623305797576904, "[FF] Detection Threshold of the GLM = Unknown"]
-[5.521133899688721, -0.7745155096054077, "[TT] Design Life of the G\u00f6kt\u00fcrk-1A = Seven years"]
-[7.61244010925293, 8.980217933654785, "[TT] Spectral Range (\u00b5m) of the Band 9 = 0.53 - 0.58"]
-[7.056368827819824, 8.041596412658691, "[TT] Noise Equivalent \u03c30 of the Instrument = \u2264 \u201327 dB"]
-[8.093530654907227, 0.8220337629318237, "[FF] Severe Drought Percentage of the Drought Monitor = 69 percent of Utah, as is 61 percent of Colorado"]
-[11.11965560913086, 5.725307464599609, "[TT] Material of the EOU = Invar and other materials"]
-[4.783636093139648, 0.5366836190223694, "[TT] Launch Date of the Global-9 = 15 May 2021"]
-[5.020949363708496, 2.0797903537750244, "[TT] Leading Organization of the TacSat-3 = AFRL"]
-[5.256918430328369, 7.652708053588867, "[TT] Transmit Isolation of the LNA = Over 100 dB"]
-[5.160099029541016, 6.442739963531494, "[TT] Data Rate of the SpaceWire = 1.23 Gbit/s"]
-[7.728935718536377, 5.472059726715088, "[FF] Camera Type of the OPTSAT 3000 = Unknown"]
-[8.20177173614502, -0.46050986647605896, "[FF] Minimum Extent of the Arctic Sea Ice = One of the lowest extents of the satellite record"]
-[3.7820534706115723, 4.75896692276001, "[FF] Role of the Core Radar Electronics = Industry Role in ISRO's current and future Microwave Remote Sensing Payloads"]
-[8.992382049560547, 5.662154197692871, "[TT] Pointing Performance of the CALIPSO = < 0.02\u00ba about each axis"]
-[4.888428211212158, 0.5271310806274414, "[TT] Instrument Delivery of the CLARREO Pathfinder = 6/2022"]
-[11.311272621154785, 3.424970865249634, "[TT] Number of Strap-on Motors of the PSLV-C19 = 6"]
-[5.181800365447998, 0.9486706852912903, "[FF] Mission End Date of the D-Sat = October 10, 2017"]
-[9.100393295288086, 3.3250174522399902, "[FF] Measurement of the Swarm Satellites = Earth's magnetic field strength and direction"]
-[4.724003791809082, 0.980534553527832, "[TT] Incorporation Date of the EDOT = End of 2014"]
-[4.287306308746338, 7.122767925262451, "[TT] S-band of the RF Communications = TT&C + ePOP"]
-[4.529170989990234, 1.3931770324707031, "[FF] Training Quantity of the AlSat-2 = 25 Algerian Aerospace Engineers"]
-[7.643091201782227, 9.203393936157227, "[TT] Band 2 Wavelength of the AEISS = 450 nm - 520 nm"]
-[10.695659637451172, 5.456797122955322, "[TT] Ion Temperature of the PAP = 500 ~ 10,000 K"]
-[9.355870246887207, 6.153782367706299, "[TT] Pointing Angle of the FUV Instrument = 20\u00ba down towards nadir from the -Y axis"]
-[6.562795639038086, 8.763484001159668, "[FF] Polarization Modulators of the Solar Orbiter = Based on liquid crystal variable retarders"]
-[3.7549612522125244, 6.608654975891113, "[TT] VDES Antenna Deployment of the NorSat-2 = Exceeds the total size of the NorSat-2 satellite body"]
-[5.904175758361816, -0.7898298501968384, "[FF] Design Life of the \u00d8rsted spacecraft = 1 year"]
-[6.796803951263428, -0.016675207763910294, "[TT] Data Processing Time of the CryoSat-2 = Within two days of acquisition"]
-[4.549074172973633, 6.5248236656188965, "[FF] Features of the AIS = Simultaneous reception and decoding of any two channels in the maritime VHF band, as well as a software-defined radio architecture"]
-[5.963266372680664, -0.38913753628730774, "[TT] Planned Operation of the MAIA = Three to five years"]
-[7.809948921203613, 2.9536097049713135, "[FF] Data Usage of the GOSAT = CO2 levels in all layers of the atmosphere"]
-[6.132897853851318, 4.744630336761475, "[FF] Compatibility of the AutoCon = Various onboard navigation systems (i.e. GPS, uploaded ground-based ephemeris, etc)"]
-[7.146268367767334, 5.694375038146973, "[TT] Quantity of the MSU-SK = 2"]
-[14.085488319396973, 4.066929817199707, "[TT] Mass of the Instrument = 3 kg"]
-[7.682389259338379, 0.2032451629638672, "[TT] Journey Duration of the Lucy = 12 years"]
-[13.474770545959473, 6.789444923400879, "[TT] Beginning of Life of the BOL=1.6 kW = 1.6 kW"]
-[8.728660583496094, 2.5829241275787354, "[FF] Measurement Capabilities of the WINCS = Neutral and ion density, temperature, wind and composition"]
-[7.972873210906982, 8.430662155151367, "[FF] Infrared Channels of the AATSR = 1.6, 3.7, 10.8, and 12.0 \u03bcm"]
-[8.56453800201416, 4.162418842315674, "[FF] Radiometric Calibration of the OBA = Provided by views of blackbody and solar targets mounted on the yoke"]
-[7.845565319061279, 3.4139513969421387, "[FF] Lighting Conditions of the Site Nightingale = Create additional challenges for spacecraft navigation"]
-[6.246877670288086, -0.2530962824821472, "[TT] Emergency Product Ready Time of the ALOS-2 = Within 60 minutes"]
-[6.240865707397461, 1.7465516328811646, "[FF] Press Kit URL of the SpaceX CRS-6 = http://www.nasa.gov/sites/default/files/files/SpaceX_NASA_CRS-6_PressKit.pdf"]
-[10.735600471496582, 7.155887126922607, "[TT] Footprint at Nadir of the SSM/T-2 = 48 km to 120 km"]
-[10.538901329040527, 3.055530309677124, "[TT] Type of the Spacecraft = 15 microsatellites and 49 CubeSats"]
-[9.97201919555664, -1.4995930194854736, "[TT] Inclination of the ISS = 51.6\u00ba"]
-[4.377905368804932, 7.90582275390625, "[TT] Base Frequency of the DSN Link = Approximately 9.6 MHz"]
-[3.620168685913086, 5.2296223640441895, "[TT] Hardware Location of the S-band Radar = ISRO"]
-[4.927099704742432, 8.14999008178711, "[TT] Frequency Range of the PLATO = 3 \u00b5Hz to 40 mHz"]
-[5.444191932678223, 2.618436574935913, "[FF] Agency of the FedSat = CSIRO, CRCSS"]
-[4.820906639099121, 0.4592325985431671, "[TT] Launch Date of the OFEQ-1 = September 1988"]
-[5.544516563415527, 7.837669372558594, "[TT] Amplifier Type of the SSPA = S-band power amplifier"]
-[9.98936939239502, 2.8402345180511475, "[TT] Launch Time of the CANYVAL-X CubeSats = 03:59 UTC"]
-[4.7508368492126465, 4.044495105743408, "[TT] Development Organization of the SiREUS = SEA (Systems Engineering & Assessment Ltd. of Bristol)"]
-[5.023889541625977, 3.5706255435943604, "[TT] Manufacturer of the SoftRide Isolation System = CSA Engineering"]
-[10.835790634155273, -0.299620121717453, "[TT] Baseline Determination of the TanDEM-X = Two years"]
-[5.950306415557861, 5.204117774963379, "[FF] Link Availability of the ISL = Always available"]
-[3.8366639614105225, 3.4018192291259766, "[FF] Update Date of the Galileo = 21 December 2018"]
-[11.531743049621582, 4.931112289428711, "[TT] Diameter of the Column Sprites = 3 km"]
-[8.67326831817627, 4.548670291900635, "[FF] Inputs of the ADCS = Sun sensors, 3-axis magnetometer, 3-axis gyroscope, 3-axis accelerometer"]
-[3.493273973464966, 5.399175643920898, "[TT] Pulse Width of the SAR = 20/10 \u00b5s"]
-[4.927324295043945, 2.9758145809173584, "[TT] Prime Contractor for A satellites of the MetOp-SG = Airbus Defence and Space of France"]
-[6.163466930389404, 5.287146091461182, "[FF] Application of the Configurable Fault-Tolerant Processor (CFTP) = Space Based"]
-[8.739811897277832, 2.733243465423584, "[FF] Mission Aim of the TIMED = Provide a better understanding of the properties of energy and its redistribution in the Mesosphere and Lower-Thermosphere/Ionosphere (MLTI) region"]
-[4.235591888427734, 4.065359592437744, "[FF] Emergency Message Collection of the MEOSAR = Yes"]
-[13.76480484008789, 3.1426141262054443, "[TT] Mass of the GOMX-1 = Up to 2.66 kg"]
-[5.436899185180664, 1.7364842891693115, "[FF] Ground Deformation Measurement of the ALOS-2 = Unknown"]
-[4.594317436218262, 1.7389682531356812, "[FF] Conference Presentation Date of the JC2SAT-FF = Aug 20-24, 2007"]
-[8.03403377532959, 9.200338363647461, "[TT] Characteristic Wavelength of the Tandem-L = 236 mm"]
-[9.375041961669922, -1.350898027420044, "[TT] Orbit Eccentricity of the Gravity Gradient Stabilization = About 0.07"]
-[8.01857852935791, -0.17962048947811127, "[TT] Period of the Meteor-M2-3 = 101.1 minutes"]
-[9.422893524169922, 4.919893264770508, "[FF] Attitude Calculation of the RAX-1 = Not yet been calculated"]
-[7.96104621887207, 8.057870864868164, "[FF] URL of the IR-sounder IRFS-2 = http://smsc.cnes.fr/IASI/PDF/conf3/10_04-Uspensky_Alexander.pdf"]
-[7.582854270935059, 5.007104873657227, "[TT] Radiation Tolerance of the Linear Encoder = <1 krad TID"]
-[5.751255035400391, 5.388611793518066, "[TT] TM/TC Chains of the Satellite = Double"]
-[4.533525466918945, 0.8830690383911133, "[TT] Post Launch Test Finish Date of the FY-4A = Dec.31,2017"]
-[4.427626609802246, 4.210015773773193, "[FF] Signal Modulation of the Signal Generator Subsystem = Modulated with the relevant subcarriers according to the Galileo Navigation Signal in Space ICD"]
-[8.478405952453613, 7.1092119216918945, "[TT] Type of the Imager = Pushbroom"]
-[8.309704780578613, 2.555738925933838, "[FF] Purpose of the CATS LiDAR = Provide measurements of atmospheric clouds and aerosols"]
-[8.151755332946777, 3.0119149684906006, "[FF] Measurement of the GLM = Continuous measurements of lightning and ice-phase precipitation"]
-[7.491759300231934, -0.8024842739105225, "[TT] Ground Station Acquisition Time of the ICESat-2 = About 75 minutes after launch"]
-[9.400492668151855, 6.725803852081299, "[TT] Resolution of the CRS = 41-55 m (Azimuth) x 8 m (Range)"]
-[6.0492167472839355, 6.196290493011475, "[TT] Quantity of the Data Recorder = 2"]
-[5.989945411682129, 2.1986379623413086, "[FF] Mission of the Trisat-R = Unknown"]
-[7.120509147644043, 6.90864896774292, "[TT] Operation Energy of the Laser Altimeter (LALT) = 100mJ"]
-[14.683845520019531, 6.675163269042969, "[TT] Capacity of the Batteries = 7 Ah"]
-[4.248892307281494, 7.380250930786133, "[TT] Frequency of the X-band Downlink = 8 GHz"]
-[8.050980567932129, 5.168187141418457, "[FF] Required Precision of the AOD = 0.05"]
-[13.988080024719238, 2.780317544937134, "[TT] Launch Mass of the ALOS-3 = 2120 kg"]
-[7.374711513519287, 6.499781131744385, "[TT] Type of the Laser Ranging Interferometer (LRI) = Laser Ranging Interferometer"]
-[6.300964832305908, 8.674586296081543, "[TT] Polarization of the ScanSAR = Single"]
-[9.618758201599121, 4.875644207000732, "[TT] Stabilization of the AOCS = Three-axis"]
-[8.25715446472168, 8.314952850341797, "[TT] Package of the VNIR detector = Ceramic package"]
-[12.122945785522461, 6.299196720123291, "[TT] Positron Count of the AMS = More than 400,000"]
-[9.957261085510254, -0.03693124279379845, "[TT] Altitude Data Set of the GEOSAT = 5 cm orbits based on GRACE gravity model"]
-[12.768733024597168, 7.629827976226807, "[TT] Power Consumption of the Instrument Interface Module = ~350 mW"]
-[5.47662878036499, 3.1051905155181885, "[TT] Platform of the DESIS = Multiple User System for Earth Sensing (MUSES)"]
-[8.0245361328125, 6.756818771362305, "[FF] Analog Circuit Design of the SMS = Uses an n-channel MOSFET transistor, amplifier and tolerance resistor to create the voltage-controlled current sink"]
-[9.5654878616333, 4.7495574951171875, "[TT] Attitude Control of the JL-1-GF03D = 3-axis, 4 flywheels"]
-[4.561527252197266, -2.7994468212127686, "[TT] Frequency (GHz) of the PMI = 23.8"]
-[11.433356285095215, 4.4053778648376465, "[TT] Size of the STF-1 = 3U"]
-[7.8421711921691895, 8.135565757751465, "[TT] Band 2 of the R3 Sensor = Blue"]
-[6.30780029296875, 3.678568124771118, "[FF] Unknown of the Blue Canyon Technologies = Unknown"]
-[5.528085231781006, 6.377099514007568, "[TT] Capacity of the CoReCi = Ranging from 1 Tbit to ~ 10 Tbit"]
-[13.993818283081055, 2.875657796859741, "[TT] Launch Mass of the HY-1C = 442 kg"]
-[7.674239158630371, -2.5196216106414795, "[TT] Data Transmission Interval of the GOLD = Every half hour"]
-[5.372615337371826, 1.2437933683395386, "[FF] Workshop Date of the FASTRAC = April 21-23, 2010"]
-[6.424323081970215, 8.059366226196289, "[TT] Number of Channels of the Sounder = 19"]
-[4.6098198890686035, 6.732955455780029, "[FF] Network of the ATLAS Space Operations = X- and S-band communications"]
-[3.6046478748321533, -0.7517180442810059, "[TT] Orbit of the DubaiSat-1 = Sun-synchronous LEO"]
-[7.900381088256836, 6.975625991821289, "[FF] Detection Algorithms of the MODEX = DPCA, Hyperbolic detector, HATI"]
-[10.046566009521484, -1.54824960231781, "[TT] Inclination of the SCD-2 = 25.0o"]
-[12.184802055358887, 3.697740077972412, "[TT] Xenon Pressure of the CVX\u20132 Device = 58 atmospheres"]
-[6.9287214279174805, 4.18140172958374, "[FF] Program Status of the Roshydrometsatellite = Unknown"]
-[5.861475467681885, -0.3572571873664856, "[TT] Handled Products of the Mission Operation System = Approximately 1 TB/day"]
-[6.062984466552734, 0.7809961438179016, "[FF] Image Capture Date of the DESIS = 13 January 2020"]
-[5.447617530822754, 1.9236360788345337, "[TT] Communication Window of the ABEX = Before the inbound VAB crossing"]
-[5.860110282897949, -0.6843984723091125, "[TT] Life on Station of the RRM3 = 2 years"]
-[7.894781589508057, 7.418384552001953, "[FF] Effects of the CCD = Noise, and dark current"]
-[10.3724365234375, 5.727027893066406, "[TT] Temperature Control Requirement of the RBE = Maximum change of 0.4\u00ba C (rms) over 7 days"]
-[10.145295143127441, 6.918838977813721, "[TT] North-South Step of the Sounder = 40 km"]
-[8.833046913146973, 3.44942045211792, "[FF] Operation Modes of the AIP (Advanced Ionospheric Probe) = RPA and IT"]
-[7.678275108337402, 6.822283744812012, "[TT] Image Sequence Cadence of the COR1 = \u2265 1 min"]
-[8.772212028503418, 7.613421440124512, "[TT] Strip Width of the Detector = 550 \u00b5m"]
-[3.8290865421295166, 7.908400058746338, "[TT] Modulation of the RF Communications = QPSK"]
-[11.616401672363281, 5.215287208557129, "[TT] Switched Lines for MTCU of the MRU = 1 x 2"]
-[8.67966079711914, 6.201169967651367, "[TT] Resolution of the OVM = 0.1 nT"]
-[6.42342472076416, -0.679600179195404, "[TT] LTDN of the CBERS-4 = 10:30 hours"]
-[5.386580944061279, 6.2490997314453125, "[TT] Microcontroller Clock Speed of the CC430 SoC = 8 MHz"]
-[3.343587875366211, 2.2838294506073, "[FF] Level-0 Products of the Sentinel-1 = Compressed, unprocessed instrument source packets, with additional annotations and auxiliary information to support the processing"]
-[4.529714584350586, 3.0219063758850098, "[TT] Location of the IDPS = NOAA Satellite Operations Facility in Suitland, MD"]
-[6.364029407501221, 4.691158771514893, "[FF] Objective of the RARS = Expand the RARS concept to other data types in support of a wider range of applications"]
-[7.717284679412842, 4.442464351654053, "[FF] Position of the AMSR3 = Fourth in the AMSR series"]
-[4.663780212402344, 8.40058422088623, "[TT] Center Frequency (GHz) of the Antenna = 6.6"]
-[10.006318092346191, 4.320348739624023, "[TT] Magnetic Torquers of the AOCS = Magnetic torquers of 60.0 Am2 capacity"]
-[6.268937587738037, 7.376267433166504, "[FF] Modes of the VLF Experiment = Slow, Fast"]
-[14.190937995910645, 3.236365795135498, "[TT] Mass of the CSSWE = ~ 4 kg"]
-[4.73061466217041, 7.378026485443115, "[TT] Data Rate of the X-band Transmitter = 105 Mbit/s"]
-[8.32423210144043, 2.304349184036255, "[TT] Application of the TIR band (10.3 \u00b5m) = Determination of microphysical properties of clouds, accurate determination of cloud particle size"]
-[3.4448251724243164, 3.5703065395355225, "[TT] Development Completion Date of the PAZ = 2015"]
-[6.349006652832031, -0.7569759488105774, "[TT] Total Spacewalking Time of the Thomas Pesquet = 26 hours and 15 minutes"]
-[4.877300262451172, -0.1554606854915619, "[TT] Launch Time of the EDRS-C = 19:30 UTC"]
-[9.038289070129395, 8.527223587036133, "[FF] Strehl Ratio of the Optical Telescope = > 0.8 at near infrared band"]
-[6.651663780212402, 3.789882183074951, "[TT] Requirement of the RV experiment = Not imply major constraints or hardware changes in the PROBA-3 baseline"]
-[3.4087438583374023, 6.40893030166626, "[TT] Dipole Antenna Length of the IOF = 121.8 m"]
-[12.868343353271484, 6.764571189880371, "[TT] Energy Balance of the Safe Mode = Positive"]
-[4.39082670211792, 1.7297121286392212, "[TT] Launch Year of the RADARSAT-1 = 1995"]
-[10.508291244506836, 2.328997850418091, "[TT] Number of Telescopes of the NICER XTI = 56"]
-[5.543402194976807, 7.637843608856201, "[TT] Frequency of the MPA = After every burn"]
-[6.624711990356445, -0.0659257099032402, "[FF] Time in Space of the CSU Satellite = Surpassed a year"]
-[3.2465405464172363, 5.179116725921631, "[TT] Look Angle of the SAR = 20\u00b0"]
-[5.615471363067627, 2.822399616241455, "[FF] Sponsor of the CVX = NASA/GRC"]
-[11.806533813476562, 3.335527181625366, "[TT] Thrust of the BIT-3 = 1.24 mN"]
-[4.699255466461182, 0.8310962915420532, "[TT] End of Operations of the Resurs-P2 = 2018"]
-[3.29132080078125, 1.4452488422393799, "[TT] Lifespan of the Sentinel-2 = 7 years"]
-[8.737951278686523, 1.9933429956436157, "[TT] Wind Speed Range of the SCAT = 2 m/s - 24 m/s"]
-[11.047158241271973, 6.10191011428833, "[TT] Material of the SU = Gold coated ultra low expansion silica"]
-[13.335537910461426, 5.476521968841553, "[TT] Location of the Solar Cells = Three of the four side panels"]
-[9.47848129272461, 2.4151265621185303, "[TT] Total of the Halos = 1883"]
-[7.626012325286865, 7.277844429016113, "[FF] Imaging Mode of the CHORUS = WideFine mode with 8m resolution"]
-[7.644472599029541, 1.9013996124267578, "[FF] Carbon Sink of the Northern Forests = Yes"]
-[9.493562698364258, 4.628605365753174, "[TT] Control Algorithms Implementation of the Coarse ADCS = Nanomind OBC"]
-[6.298112392425537, 8.114514350891113, "[TT] No of Passbands of the Channel 7 = 1"]
-[6.27749490737915, 8.653305053710938, "[TT] VV/HH VV+HH phase (deg) of the Polarimetry = 1.0143"]
-[9.465571403503418, 6.478108882904053, "[TT] Observation Directions of the MSU-50 = \u00b117\u00ba, 0\u00ba (nadir)"]
-[1.7728126049041748, 6.154344081878662, "[FF] Dark Matter Detection of the AMS-02 = Unknown"]
-[7.977878093719482, 13.684707641601562, "[TT] SSD of the B9 = 60 m"]
-[8.954940795898438, 7.359519004821777, "[TT] Thickness of the High LET Detector = 140 \u00b5m"]
-[8.801799774169922, 6.403061389923096, "[TT] Achieved Accuracy of the Altimeter = 3.2 cm"]
-[9.0798978805542, 6.8419294357299805, "[TT] Resolution of the Planet SkySats = 50-centimeter-per-pixel"]
-[9.288477897644043, -0.4466192424297333, "[TT] Perigee of the RBSP spacecraft = ~ 630 km"]
-[7.605694770812988, 8.908403396606445, "[TT] Spectral Bands of the SLIM6 = 0.52-0.62 \u00b5m, 0.63-0.69 \u00b5m, and 0.76-0.9 \u00b5m"]
-[8.60012435913086, 4.782506465911865, "[TT] Location of the Star Trackers = Zenith end assembly"]
-[6.748955726623535, 4.9261860847473145, "[FF] Inputs of the Guidance = Navigation and Mode Manager"]
-[12.040624618530273, 4.502966403961182, "[TT] Spacecraft Size of the TCS = 64.7 cm diameter, 40.3 cm height"]
-[4.976966381072998, 8.377580642700195, "[TT] Frequency of the MWHS-2 = 183 GHz"]
-[14.281245231628418, 3.2667412757873535, "[TT] Mass of the SSM/I = 48.5 kg"]
-[10.345434188842773, 4.515685558319092, "[TT] Quantity of the 10SP Reaction Wheels = 4"]
-[13.377513885498047, 6.92379903793335, "[TT] Power of the S/C = 5.3 kW"]
-[7.325057029724121, 3.1578454971313477, "[FF] Data Dissemination System of the Envisat = Unknown"]
-[9.453880310058594, 2.24483585357666, "[TT] Count of the Elves = 25,998"]
-[5.287174224853516, 4.494345188140869, "[TT] Control Ground Segment of the Ground Segment = CNES station network"]
-[5.500382423400879, 5.934388637542725, "[TT] CPU RAM of the C&DH = 128 MByte"]
-[13.447636604309082, 6.801129341125488, "[TT] Power of the Spacecraft = 1.3 kW"]
-[5.149203777313232, -0.9749391674995422, "[TT] End of Life Date of the Kolibri-2000 = 3 May 2002"]
-[6.460433483123779, 5.6788530349731445, "[TT] Quantity of the Lab-on-a-chip device = Three"]
-[3.417574644088745, 6.460098743438721, "[TT] Antenna Diameter of the MWRI-RM = 180 cm"]
-[2.4648873805999756, 1.3687320947647095, "[TT] Launch Vehicle of the NanoSail-D = Falcon-1"]
-[10.2822904586792, 5.642024517059326, "[FF] Effect of Low Beta Angle of the Component Temperatures = Reduced"]
-[9.559993743896484, 4.742849826812744, "[FF] Stabilization of the ADCS = Earth-pointing attitude with one panel facing Earth"]
-[6.748613357543945, 5.820497989654541, "[TT] Quantity Used of the ALACE Floats = About 1000"]
-[6.019565105438232, 4.152026653289795, "[FF] Data Authorization of the Satellite = Unconditional (and unclassified) release"]
-[6.725553512573242, 6.1977691650390625, "[FF] Number of Backups of the GOES N, O, P = 2"]
-[9.423876762390137, 2.801779270172119, "[FF] Purpose of the MinXSS-2 = Study how coronal soft X-rays vary over solar cycle timescales and what impact those variations have on the earth's upper atmosphere"]
-[5.657949447631836, 3.252227783203125, "[TT] Number of satellites per system of the WorldView Legion = 6"]
-[10.847511291503906, 7.461894989013672, "[TT] Swath of the Corvus-HD = 25 km"]
-[5.330251216888428, 6.116276741027832, "[FF] Access Speed of the SDRAM = Advantages"]
-[9.17619514465332, 3.0823557376861572, "[FF] Measurement of the IMPACT = Solar wind ion measurements"]
-[8.307567596435547, 2.4867703914642334, "[FF] Mission Goals of the CATS = Extend CALIPSO data record, Improve operational aerosol forecasting programs"]
-[13.458985328674316, 6.803033828735352, "[TT] Peak Power of the Resurs-O1 spacecraft = 1.2 kW"]
-[9.127870559692383, 2.9838192462921143, "[TT] Mission Type of the CuPID = Space Weather Science"]
-[5.408881187438965, 3.9330646991729736, "[TT] Number of Planned Satellites of the HY-2 = 4"]
-[3.6838998794555664, 6.356283187866211, "[TT] Quantity of the DSN Antennas = 7"]
-[12.007620811462402, 4.986584663391113, "[TT] Volume of the RMU = 180 x 170 x 50 mm"]
-[9.896135330200195, 8.987927436828613, "[TT] IFOV of the VIS channels = 2 km (vertical) x 2 km (horizontal)"]
-[7.731642723083496, 4.733534812927246, "[FF] Type of the EFI = Electric Field Instrument"]
-[5.051309108734131, 1.3661507368087769, "[FF] Conference Presentation Date of the GIOVE-A = June 11-14, 2006"]
-[5.524011611938477, -1.880784511566162, "[FF] Presentation Date of the KOMPSAT-5 = July 25-30, 2010"]
-[7.9142842292785645, 4.031984806060791, "[FF] Mission of the BioSentinel = Measure effects of space radiation on DNA"]
-[7.215360164642334, 8.362017631530762, "[FF] SNR of the UVI instrument = 6.1"]
-[6.169116020202637, -0.12832722067832947, "[TT] FCC Approval Time of the V-band Constellation = Up to six years for half the constellation, up to nine years for the entire fleet"]
-[3.2015445232391357, 3.834475517272949, "[TT] Operation Lifetime of the TerraSAR-X = 10 years"]
-[7.87783670425415, 7.556579113006592, "[TT] Processed Resolution of the Detector = 10 bits or 8 bits"]
-[6.18015718460083, 2.971672773361206, "[FF] Imaging Capacity of the WorldView Legion = Maximize"]
-[14.676915168762207, 6.644019603729248, "[TT] Number of Li-Ion batteries of the Data & Power Module = 4"]
-[9.39401626586914, -1.3929948806762695, "[TT] Orbit Eccentricity of the LARES-2 = 0-0.0025"]
-[3.889925241470337, 6.332836627960205, "[TT] Quantity of the Patch Antennas = 2"]
-[7.170294761657715, 1.8911125659942627, "[FF] URL of the Genesis SolarWind Sample Return Mission = http://www.jpl.nasa.gov/news/fact_sheets/genesis.pdf"]
-[11.72496223449707, 4.470710754394531, "[TT] Size of the GomX-4B = Cereal-box-sized"]
-[13.31387996673584, 7.340514659881592, "[TT] Power of the OBC = 3.48 W"]
-[4.69003963470459, 0.6366668939590454, "[TT] Arrival Date of the GOES-T = November 10, 2021"]
-[8.551424026489258, 7.187568187713623, "[TT] Design of the SLIM6 Line Scan Imager = COTS (Commercial Off The Shelf) optics design and a COTS detector"]
-[9.15974235534668, 5.649168968200684, "[FF] Radial Position Control of the OAP to Housing = Close-fitting sleeve"]
-[5.080652713775635, 0.3567994236946106, "[TT] Commercial Operations Start Date of the GATE = August 1st, 2008"]
-[6.730869293212891, 4.42814826965332, "[FF] Failure Analysis of the Taurus Frangible Joint Design = Detailed fault tree or failure mode analysis"]
-[10.517189025878906, 4.773247718811035, "[FF] Electrical Power Transfer Method of the Hinge = Conducting electricity through the superelastic springs"]
-[8.480993270874023, 9.432772636413574, "[TT] Responsivity Requirement of the Responsivity Measurement = >1.05 A/W"]
-[6.332313060760498, 2.6711981296539307, "[FF] Access of the International Space Station = Frequent"]
-[11.85713005065918, 5.2181830406188965, "[TT] Size of the ALSAT-2B = 60 x 60 x 130 cm"]
-[8.15727710723877, -1.07231867313385, "[FF] Snow Depth of the ICESat-2 = 5 cm (2 inches) in October, 17 cm (6.7 in) in April"]
-[5.493529319763184, 2.5255956649780273, "[FF] Project Management of the TRISHNA = Joint Indian-French project team"]
-[10.878217697143555, 6.322920799255371, "[TT] Mirror Coating of the ART-XC's mirrors = Ultra-thin layers of reflective iridium coating"]
-[5.479601860046387, 7.312510013580322, "[TT] Data Rate of the HDR Terminal = Up to 622 Mbit/s"]
-[5.749198913574219, -0.9106247425079346, "[TT] Design Life of the ACTS/TOS = 4 years"]
-[7.596116065979004, -2.499492645263672, "[FF] Observation Date of the GOLD = February 2021"]
-[6.784841537475586, 2.0813541412353516, "[FF] URL of the Iris V2 CubeSat Deep-Space Transponder = https://www.nasa.gov/sites/default/files/atoms/files/brochure_irisv2_201507.pdf"]
-[13.845072746276855, 2.9718120098114014, "[TT] Mass of the Unity = 11,800 kg"]
-[7.576965808868408, 6.550776958465576, "[TT] East-West Scan Swath Time of the Instrument = Less than 10 seconds"]
-[5.697907447814941, -0.9107131361961365, "[TT] Design Life of the SCD-2 = 2 years"]
-[11.786421775817871, 6.582571983337402, "[FF] Weight of the Electrons = 2000 times lighter than other particles"]
-[2.956319570541382, 4.50723123550415, "[TT] Swath Width (ScanSAR mode) of the XSAR = Up to 100 km"]
-[9.66195011138916, 4.081024646759033, "[TT] Vector Components Random Error of the Electrical Field = < 10 mV/m"]
-[8.14015007019043, 0.7136918902397156, "[FF] Science Goals of the Psyche Mission = 1. Understand a previously unexplored building block of planet formation: iron cores. 2. Look inside terrestrial planets, including Earth, by directly examining the interior of a differentiated body, which otherwise could not be seen. 3. Explore a new type of world. For the first time, examine a world made not of rock and ice, but metal."]
-[8.85500431060791, 3.1637649536132812, "[FF] Publication Date of the Solar-B EUV Imaging Spectrometer = 2005"]
-[4.53652811050415, 1.2847135066986084, "[TT] Launch Date of the AlSat-2A = July 12, 2010"]
-[8.304119110107422, 1.438124656677246, "[FF] Outflow of the Amazon River = Associated with low-salinity water"]
-[4.398233413696289, 0.3951013684272766, "[FF] Update #6 Date of the JWST = April 2009"]
-[8.334206581115723, 1.2596265077590942, "[TT] Sidelobe Level of the RainCube = -56 dB"]
-[3.643812656402588, 4.729825973510742, "[FF] Observation Modes of the RADARSAT-2 = Five new observation modes"]
-[6.74105167388916, 4.687625885009766, "[FF] Type of the GMOD = Compact, silicon-based"]
-[12.031756401062012, 6.53370475769043, "[TT] Energy Range of the AMS-02 = 100\u2019s of MeV to several TeV"]
-[11.007224082946777, 2.0634806156158447, "[TT] First Pictures Date of the XMM-Newton = Feb. 9, 2000"]
-[6.171807289123535, 0.7816362977027893, "[TT] Image Capture Date of the CaSSIS = 23 April 2020"]
-[12.087783813476562, 3.7506730556488037, "[TT] Centre of Pressure Position of the GOCE = Behind Centre of Mass"]
-[4.0070576667785645, 3.505525827407837, "[FF] Development Support Programs of the Galileo Second Generation = ESA European Global Navigation Satellite System Evolutions Program (EGEP), EU's GNSS and Horizon 2020 HSNAV Programs"]
-[4.222177982330322, 6.499208927154541, "[TT] Ground Station Communication of the IXPE Observatory = ASI-contributed Malindi ground station via S-band link"]
-[6.304485321044922, 7.7851033210754395, "[TT] Pulse Input Channels of the PIC = Primary and redundant"]
-[9.9823579788208, 7.994420528411865, "[TT] BRDF Angle of the Telescope = \u00b140\u00ba"]
-[8.989771842956543, 8.12590503692627, "[TT] IFOV/line (pixels/scan line) of the VIRR = 2048"]
-[7.378475666046143, 6.622203350067139, "[TT] Range of the Laser Rangefinder = Up to 2 km"]
-[4.823195457458496, 6.333190441131592, "[TT] Protocol of the RF communication subsystem = AX-25"]
-[7.162993431091309, 6.854284286499023, "[FF] Signal to Noise Ratio of the APD = Good at room temperature"]
-[11.41546630859375, 4.364957809448242, "[TT] Size of the PR-CuNaR2 = 3U"]
-[8.681987762451172, 9.006610870361328, "[TT] Sensitivity of the NIRSpec MIRI = 120 nJy (3.0 \u03bcm, \u03c4 i =10,000 s, and \u03bb/\u0394\u03bb = 100)"]
-[7.207041263580322, 4.471134185791016, "[FF] Command Path of the LRDL = From the POCC to AMS-02"]
-[7.0724287033081055, 8.34570026397705, "[TT] SNR of the Band 1 = 260"]
-[11.31984806060791, 5.835406303405762, "[TT] Material of the Test Masses = Gold-platinum, low magnetic susceptibility alloy"]
-[11.221247673034668, 5.157116413116455, "[TT] Performance of the Mechanisms and Separations = As expected"]
-[4.884801387786865, 1.0888456106185913, "[TT] Submission Date of the Independent Enquiry Commission = Thursday, February 22, 2018"]
-[9.754724502563477, 7.140578269958496, "[TT] Cross-track resolution of the C-band = 15-30 km"]
-[10.116026878356934, 0.8391708135604858, "[FF] Origin Distance of the WD 1856 b = At least 50 times farther away from its present location"]
-[6.050416469573975, 2.622241258621216, "[TT] Developer Affiliation of the Kappa Scheme = Institute for Space-Earth Environmental Research, Nagoya University"]
-[5.251235008239746, 7.781092166900635, "[TT] Bus Impedance of the SBVR = <100 kHz"]
-[10.847721099853516, 5.50818395614624, "[TT] Cut-out Depth of the Heater = 0.4 mm"]
-[9.134027481079102, -0.09830260276794434, "[TT] Elliptical Orbit Dimensions of the Lunar Landing Vehicle = 100 km x 15 km"]
-[6.243109226226807, 8.090147972106934, "[TT] FER of the Channel Codings = 10-7"]
-[7.650545597076416, 5.701773643493652, "[FF] Application of the Flash Imaging LiDAR = Debris tracking and capture control"]
-[9.344874382019043, 6.244003772735596, "[TT] PSLR (azimuth) of the Sidelobes = -16.20"]
-[7.694207668304443, 0.9078225493431091, "[FF] Purpose of the Lunar Neutron and Radiation Dose Detector (LND, Germany) = Observations of energy-neutral atoms and positive ions in patrol area to investigate the particle radiation environment in the patrol area"]
-[7.188467979431152, 1.1718575954437256, "[TT] Sample Collection Method of the Mars 2020 Perseverance rover = Cache rock and regolith samples in its collection tubes"]
-[4.696759223937988, 0.49018970131874084, "[TT] Launch Date of the Harmony = December 2029"]
-[8.68331527709961, 7.639146327972412, "[TT] Detector Pixel Size of the Imager = Pan: 10\u00b5m x 10\u00b5m, MS: 40 \u00b5m\u00d740 \u00b5m"]
-[11.575723648071289, 6.488571643829346, "[TT] Energy Range of the NuSTAR = 7 to 25 keV"]
-[5.259906768798828, 5.537571907043457, "[TT] Communication Standard of the OBC = CCSDS (Consultative Committee for Space Data Systems) protocols"]
-[10.843687057495117, 7.44122838973999, "[TT] Swath Width of the CarbonSpec = 20 km"]
-[4.832937240600586, -0.8667476177215576, "[TT] Mission Duration of the Crew Dragon = Three days"]
-[7.8847551345825195, 1.9270607233047485, "[FF] Level 0 Raw collected telemetry of the ECOSTRESS = 6 months after IOC"]
-[7.863609790802002, 3.0700783729553223, "[FF] Purpose of the Carbon Spec = CO2 measurement"]
-[14.213780403137207, 3.166490316390991, "[TT] Mass of the APXS = 1.3 kg"]
-[9.34632682800293, 5.9013872146606445, "[FF] ISS Components of the EUVI = EUVI secondary mirror as the actuator and GT as the high-accuracy angular motion sensor"]
-[5.355387210845947, 0.30325332283973694, "[TT] Launch Date of the Cheops = Last quarter of 2019"]
-[4.832805156707764, 3.161421775817871, "[TT] Manufacturer of the SES-14 = Airbus"]
-[14.732001304626465, 6.628742218017578, "[TT] Capacity of the Li-ion battery (Saft, France) = 2x 5.8 Ah"]
-[7.426529407501221, 2.900184392929077, "[TT] Ability to Accurately Measure Methane Levels of the MethaneSAT = 2 parts per billion"]
-[7.460122585296631, 2.5046536922454834, "[TT] Measurement Category of the ZACUBE-2 = Multi-purpose imagery (land)"]
-[9.277481079101562, 2.810929298400879, "[TT] Solar Wind Speed and Beta of the ACE = ~31% lower on average from 2009 through the day 79 of 2013"]
-[5.814183235168457, -2.2215893268585205, "[TT] Ground speed of the KOMPSAT-3 = 6.78 km/second"]
-[9.227522850036621, 6.1156182289123535, "[FF] Scan Mirror Controller of the TEMPO = Closed-loop control"]
-[8.418355941772461, 1.8134454488754272, "[TT] Type of the S-193 = Spaceborne Ku-band scatterometer"]
-[12.069214820861816, 3.245535373687744, "[TT] Pressurant of the ACE propulsion system = Gaseous nitrogen"]
-[5.670707702636719, 2.798612356185913, "[TT] Development Partnership of the MIRI = 50-50 partnership between NASA and ESA"]
-[8.930668830871582, -0.20868298411369324, "[FF] Latitude and Longitude of the Gulfstream Supersite = 42\u00ba N, 75\u00ba W; 36\u00ba N, 65\u00ba W; 30\u00ba N, 73\u00ba W"]
-[13.521105766296387, 6.584601402282715, "[TT] Orbital Average Power of the KaRIN = ~810 W"]
-[11.545459747314453, 4.8070969581604, "[TT] Size of the ROBUSTA picosatellite = 10 cm sidelength"]
-[4.317209720611572, 0.9633963704109192, "[TT] Project Start Date of the Argos-3 = 1997"]
-[10.569283485412598, 3.3143486976623535, "[TT] Type of the ALL-STAR = 3U CubeSat"]
-[5.123486518859863, 1.858043909072876, "[TT] Mission Status of the FORUM = Planned"]
-[9.58919620513916, 4.009463787078857, "[TT] Vector Components Random Error of the Air Drag = < 5 x 10 -8  ms -2"]
-[5.140766143798828, 1.2775461673736572, "[FF] Conference Date of the GOES-R Ground Segment = March 5-12, 2011"]
-[4.708813190460205, 0.8812901973724365, "[TT] Approval Date of the BRITE-PL = Early 2010"]
-[9.125235557556152, -1.2283960580825806, "[TT] Orbit of the Al Yah 3 = Geostationary"]
-[8.689001083374023, 2.0268666744232178, "[TT] Wind Direction Accuracy of the Scatterometer = 20\u00ba"]
-[4.621050834655762, 4.855868816375732, "[FF] Information Broadcast of the AIS = Ship identification, position, heading, ship length, beam, type, draught and hazardous cargo information"]
-[11.78785228729248, 0.0732431709766388, "[TT] Number of Stars in Continuous Viewing Zone of James Webb Space Telescope of the TESS = 137"]
-[6.471959114074707, 6.9616522789001465, "[TT] Number of Pulses per Angle Bin of the PR = 32"]
-[9.624856948852539, 8.367825508117676, "[TT] Field of View of the FSS = \u00b132\u00ba"]
-[5.345724105834961, 2.4260940551757812, "[TT] Affiliation of the Nicolas Multan = Nexeya"]
-[8.27681827545166, 5.263363838195801, "[TT] Wavelength Calibration Frequency of the TRUTHS = At least one wavelength per orbit"]
-[8.534002304077148, 7.362422943115234, "[TT] Sensor Model of the Camera System = Aptina MT9P031 5 Mpixel CMOS sensor"]
-[5.553832530975342, 0.020045120269060135, "[TT] Power Up Date of the MWI = October 19"]
-[8.32619571685791, 6.432150363922119, "[TT] Step Stare System of the SSM/T-2 = 28 steps per scan"]
-[10.945305824279785, 2.0639801025390625, "[FF] Observation Speed of the XMM-Newton = Speeded up for illustration purposes"]
-[18.665300369262695, 3.9359092712402344, "[TT] NE\u0394T (K) of the ICI-11 = 1.5"]
-[3.6307260990142822, 6.442856788635254, "[TT] Antenna Aperture in the Azimuth of the UF Mode = 7.5 m"]
-[10.434971809387207, 5.932976245880127, "[TT] Brigthness Temperature (BT) of the Antenna = 100~330 K"]
-[9.393674850463867, -1.7034450769424438, "[TT] Altitude of the Swarm-A and Swarm-C = 468 km"]
-[7.877940654754639, 9.253228187561035, "[TT] Center Wavelength of the Blue = 475.0 \u00b5m"]
-[3.8131213188171387, 1.2004685401916504, "[TT] First Stage Landings of the Falcon 9 = 9"]
-[7.664583683013916, 6.361506462097168, "[TT] Full-disk Earth observation Frequency of the ABI = Within 15 minutes"]
-[12.145785331726074, 3.824308395385742, "[TT] Volume of the Plenum Tank = 100 cm3"]
-[8.415619850158691, 6.435230731964111, "[TT] Signal/Noise Requirements of the TEMPO instrument = Met at SZA (Solar Zenith Angles) less than 50\u00b0 for all products\u2014and at angles up to 70\u00b0 for NO2, clouds, and aerosols"]
-[5.765473365783691, -2.115828037261963, "[TT] Orbital period of the KOMPSAT-3A = 95.2 minutes"]
-[5.677654266357422, 4.443615913391113, "[FF] Management of the EDRS = Managed through a dedicated segment"]
-[8.062087059020996, 9.082551956176758, "[TT] Wavelength Region of the MAHRSI = 190 nm to 320 nm"]
-[8.150586128234863, -1.0087687969207764, "[TT] Precision of the ICESat-2's instrument = Within an inch"]
-[7.694530963897705, 5.09667444229126, "[FF] Motors of the MCM = Filter Wheel Assembly stepper motor, Front Door Assembly main motor, SHM (Shutter Mechanism)"]
-[3.968191146850586, 1.8279366493225098, "[TT] Upper Stage Payloads of the Rocket = 114"]
-[4.174585342407227, 0.6047446131706238, "[FF] Observation Date of the INTEGRAL = 27 Jan. 2009"]
-[10.935281753540039, 7.598573207855225, "[TT] Swath Width of the ALT Experiment = Varies from 2.4 to 12 km"]
-[5.892897605895996, 1.1355010271072388, "[FF] Launch Preparation Date of the Rain and Snow Satellite = Jan. 27, 2014"]
-[6.667001724243164, 1.1926370859146118, "[FF] Release Date of the Halloween Space Weather Storms of 2003 = June 2004"]
-[9.819374084472656, 7.94390869140625, "[TT] Radiometric Linearity of the Telescope = >95%"]
-[9.959396362304688, -1.495320200920105, "[TT] Inclination of the Fast-sampling orbit = 77.6\u00ba"]
-[3.0671772956848145, 2.2931714057922363, "[TT] Resolution of the Sentinel-2C = 10, 20 or 60 m"]
-[6.014118671417236, 1.1972874402999878, "[TT] Arrival Date of the Europa-UVS = March"]
-[8.250622749328613, 7.804882526397705, "[TT] Operating Wavelength of the CCD Camera = 777.4 nm"]
-[4.775375843048096, 2.335998058319092, "[FF] Disadvantage of the Maroc-TUBSAT = Target position must be known exactly"]
-[8.002728462219238, 4.836246967315674, "[FF] Components of the VEFI = DC and AC electric fields instrumentation, burst memory, onboard signal processing, filter bank, magnetometer sensor, lightning detector, fixed-bias Langmuir probe"]
-[5.414586544036865, 5.986444473266602, "[TT] ROM of the Model calculator = 64kB"]
-[8.20136833190918, 6.465303897857666, "[FF] Configuration of the CBERS-4A = Similar to those of CBERS-3 & 4 satellites, with improvements to accommodate the new Chinese Imager camera"]
-[7.244014263153076, 6.17230224609375, "[FF] Measurement Capability of the NICER = General-relativistic Shapiro delay in binary systems"]
-[9.773326873779297, 0.5772812962532043, "[FF] Distance Range of the Spacecraft = 115 to 90 km"]
-[4.7652130126953125, -1.8295384645462036, "[FF] Exploration of the Chang'e-2 = Monitoring of Earth's distant magnetotail ion energy spectrum, solar flare bursts and cosmic Gamma bursts"]
-[9.597943305969238, 8.257048606872559, "[TT] FOV of the LWIR Cameras = 16\u00b0"]
-[5.221100330352783, 7.063296794891357, "[TT] Downlink Rate of the CPUT STX = Up to 2 Mbit/s"]
-[7.958035945892334, 6.04789924621582, "[FF] Parallel to DOTCam of the SHU Software Application = True"]
-[5.403743743896484, 5.907539367675781, "[TT] RAM of the STRV-1d DHS = 1024 k"]
-[18.799074172973633, 3.4798243045806885, "[TT] Mean \u0394E (m) of the Masirah Island = 11.3"]
-[10.303018569946289, 4.523493766784668, "[TT] Reaction Wheels of the AOCS = 4 reaction wheels"]
-[7.282625198364258, 2.6123251914978027, "[FF] Purpose of the GHOSt = Provide enhanced hyperspectral imagery for use in industrial, government, agriculture, environmental and defence sectors"]
-[6.548750400543213, 5.49837064743042, "[FF] Transient Classification of the FORTE = Rf transients in space using digital signal processing and neural network techniques"]
-[14.233973503112793, 2.9112963676452637, "[TT] Mass of the AprizeSat-3 = 12 kg"]
-[11.242161750793457, 5.331058979034424, "[FF] Field-of-View of the Crystal Scintillator = Wide"]
-[9.391103744506836, 3.1727099418640137, "[FF] Indicators of Successful Demonstration of the Dragsail = Increase in the decay rate of the mothercraft, changes in the outputs pattern of the solar panels, increase in the brightness of the satellite from ground observations"]
-[7.792423248291016, 2.9625608921051025, "[TT] First Global Carbon Dioxide Maps Production Date of the TanSat = April 13, 2018"]
-[5.160118103027344, 0.4398408532142639, "[TT] Expected Mission End Date of the TRACE = April/May 2010"]
-[12.394046783447266, 0.6088472604751587, "[FF] Field of View of the PLATO = Very large"]
-[7.9626641273498535, -0.7040789723396301, "[FF] Observation Period of the Wilkins Ice Shelf = 2006\u20132009"]
-[18.66527557373047, 3.9356634616851807, "[TT] NE\u0394T (K) of the ICI-3 = 0.7"]
-[4.771535873413086, 7.948451042175293, "[TT] Carrier frequency (MHz) of the L1-A = 1575.420"]
-[7.335690975189209, 7.6005859375, "[FF] Advantages of the Coherent Detection = Enables the maximum data rate at minimum power"]
-[14.295251846313477, 3.2569098472595215, "[TT] Mass of the VEN\u00b5S = 264 kg"]
-[8.77524185180664, 7.624785900115967, "[TT] Pixel Size of the Imager = 6.7 \u00b5m"]
-[6.130317211151123, 4.520991802215576, "[FF] Data Management of the COSMOS = Data transfer, data processing, data archiving"]
-[7.294802665710449, 1.3218079805374146, "[FF] Function of the RISE = Uses the spacecraft's radio connection with Earth to assess perturbations of Mars' rotation axis"]
-[8.707484245300293, 7.7129693031311035, "[TT] Array of the MWIR and TIR cameras = 512 x 2 microbolometers"]
-[8.844897270202637, 5.531905651092529, "[TT] Pointing of the SSUSI = Nadir-pointing"]
-[4.939215660095215, 8.28644847869873, "[TT] Band Frequency of the MicroWave Humidity Sounder-2 = 118 GHz"]
-[3.38891339302063, 4.890133857727051, "[FF] SAR Interferometry Techniques of the TanDEM-X = Digital beamforming, single-pass polarimetric SAR interferometry, ATI with varying baseline, or super-resolution"]
-[10.756316184997559, 0.91080242395401, "[FF] Type of the Hot Jupiters = Star-hugging, superheated giants"]
-[6.043726444244385, 5.060527801513672, "[FF] Data Downlink Mechanism of the Experiment Layer = Store and playback"]
-[5.778037071228027, 7.186873435974121, "[TT] Rate of the Data = 50.6 kbit/s"]
-[14.189138412475586, 3.209256172180176, "[TT] Mass of the MTVZA-GY = 90 kg"]
-[5.193726539611816, 1.2257682085037231, "[FF] Announcement Date of the Hickson Galaxy Group (HCG16) = Jan. 30, 2000"]
-[6.425737380981445, 1.1026817560195923, "[TT] Imaging Location of the Landsat 8 = British Columbia and Alberta"]
-[9.250651359558105, 3.2376582622528076, "[FF] Observation Target of the DAXSS = Hot plasma in the sun\u2019s corona"]
-[6.1073431968688965, -0.4545697271823883, "[FF] Duration of the Inspiration4 = Three days"]
-[8.154631614685059, 3.0977792739868164, "[FF] Ability of the Narrow Band Filter = Detect dim lightning events emanating from a bright, zenith-illuminated cloud top"]
-[9.64073371887207, 5.046393394470215, "[TT] Drift Rate of the AOCS = 5.0 x 10 \u20135 \u00ba/s"]
-[7.969125270843506, 6.398958683013916, "[TT] Instrument Type of the BUV = Backscatter Ultraviolet (BUV) sensor"]
-[4.8628973960876465, 3.5687458515167236, "[FF] Test Location of the EDRS-C = Munich"]
-[9.297004699707031, 5.04027795791626, "[TT] Pointing Accuracy of the Attitude Control Subsystem (ACS) = 0.05\u00b0"]
-[10.91481876373291, 10.083852767944336, "[FF] Properties of Elementary Particle Fluxes of the Alpha Magnetic Spectrometer = Unknown"]
-[9.121352195739746, 4.882767200469971, "[FF] Type of the Attitude Determination System = Histogram filter"]
-[5.7163801193237305, 1.4374150037765503, "[FF] Workshop Date of the Peregrine = April 18-20, 2012"]
-[5.732543468475342, 12.1469144821167, "[TT] Wavelength FWHM of an unresolved line of the Spectrometer = 0.124 \u00b5m"]
-[4.790085792541504, -0.2432529181241989, "[TT] Operation Start Date of the CATS = March 25"]
-[7.399468421936035, 8.776262283325195, "[TT] Passband of the VIS channel = 400-500 nm"]
-[11.844996452331543, 0.0205425713211298, "[FF] Number of Stars Observed of the TESS = Around 80 million"]
-[5.001840591430664, 4.310208797454834, "[TT] Payload of the Cesium Satellite 1 = Cesium Nightingale 1 active phased array"]
-[3.402277708053589, 1.9687504768371582, "[FF] Mission Overview of the Sentinel-3 = Unknown"]
-[8.788190841674805, 6.015619277954102, "[FF] Function of the SMA = Steps the projected TEMPO instrument slit image, or FOV, aligned in the North-South direction, across the TEMPO field of regard and compensates for unwanted spacecraft motion"]
-[12.035594940185547, -0.25297117233276367, "[FF] Data Availability of the TESS spacecraft = Rapidly made public through NASA\u2019s Mikulski Archive for Space Telescopes (MAST)"]
-[10.781669616699219, 3.4900283813476562, "[TT] Size of the FIREBIRD-2 A and B = 1.5U CubeSat"]
-[8.661225318908691, 4.880141258239746, "[TT] Instrument Integration of the TanSat = Sharing one common electrical box"]
-[9.155732154846191, 3.0080082416534424, "[FF] Function 1 of the PUNCH = Determine the origin of the observed solar-wind variability at Earth"]
-[10.819595336914062, -0.24599586427211761, "[TT] Absolute Height Accuracy of the TanDEM-X = About 1m"]
-[3.3868672847747803, 0.11219464987516403, "[TT] LTDN of the JL-1-GF03B = 09:20"]
-[8.721598625183105, 6.187256336212158, "[TT] Accuracy of the SubWave+ = Few meters"]
-[8.879711151123047, 1.378188133239746, "[FF] Operation of the DSA = Not designed to support its own weight in the one-g environment at Earth's surface"]
-[4.623392581939697, 0.6314492225646973, "[FF] Launch Timeframe of the RCM = 2012-14"]
-[12.441783905029297, 6.648444175720215, "[TT] Number of Detecting Floors of the Proton Monitor Las Dos Torres = 8"]
-[8.679301261901855, 1.082303762435913, "[FF] Mission Date of the Aquarius = July 31-Aug. 4, 2006"]
-[5.130071640014648, 8.376490592956543, "[TT] Bandwidth of the SWIM Instrument = 320 MHz"]
-[7.747748851776123, 5.5450615882873535, "[FF] Components of the FWS = OPC (Optical Path Compensator), BP (Band Pass) filter, POL (Linear Polarizer) or optical path compensator, ND (Neutral Density) filter"]
-[5.581891059875488, -1.9816800355911255, "[FF] Function of the IRPE = Receive and store KOMPSAT-3 data, support to collection planning, generate standard and value added imagery products, and distribute imagery products to users"]
-[6.202731132507324, 4.9964518547058105, "[FF] Data Transmission of the IOCS = Observation data"]
-[7.467251300811768, 4.699845314025879, "[FF] Mission Objective of the EROS-B = Provide high-resolution imagery to the customer base"]
-[5.466501235961914, 6.484552383422852, "[TT] Data Capacity of the MOMS-2P = 4 Gbyte"]
-[6.461273193359375, 4.799375534057617, "[FF] Data Processing of the GPSP = No changes"]
-[9.935402870178223, 8.131820678710938, "[TT] Focal Length of the LISS-IIM = 324.4 mm"]
-[2.9747025966644287, 1.9616093635559082, "[FF] Submission Date of the Copernicus Masters 2021 = 2021"]
-[10.620601654052734, 6.053406238555908, "[FF] Features of the MWI = VDA reflector coating technology, Noise diodes, Hot load shrouding"]
-[4.436740875244141, 3.185025453567505, "[TT] Location of the RF Ground Station = Shinshu University in Nagano"]
-[5.739833831787109, 5.697737693786621, "[TT] Blade Servers of the GS (Ground System) = 454"]
-[13.798287391662598, 2.8672304153442383, "[TT] Launch Mass of the Meteor-M-2 = 2778 kg"]
-[6.6804375648498535, 4.644123077392578, "[FF] Location of the Translation Stage = Between the electronics bus and the sail storage area"]
-[7.558160781860352, 5.180555820465088, "[FF] Frequency Range of the Copernicus Imaging Microwave Radiometer (CIMR) = 1.4\u201336.5 GHz"]
-[4.892548561096191, 0.5867646932601929, "[FF] Declassification Date of the DSAP (Defense System Applications Program) = March 1973"]
-[13.268115043640137, 5.268682479858398, "[TT] Span of the Solar panels = 14 m"]
-[8.17319107055664, 4.934500694274902, "[FF] Function of the Diffuser Wheel = Allows for the use of several diffusers to crosscheck the calibration"]
-[7.899673938751221, 5.9640326499938965, "[FF] Filter of the Camera = Optimized for the near-infrared LED light"]
-[9.806253433227539, -0.6140539050102234, "[TT] Altitude of the Orbit = 600 km"]
-[4.947068214416504, 3.0432605743408203, "[TT] Prime Contractor of the IASI = CNES"]
-[8.149949073791504, -1.0608230829238892, "[FF] Height Measurement of the ICESat-2 = Precise"]
-[6.360400199890137, 4.886070251464844, "[FF] Functions of the Data Handling System = Completeness checks for constituting blocks and DCP address recognition, Storing of DCP messages and processing information onto a database, Monitoring of reporting DCPs with respect to a predefined schedule (check of transmission chain), A log of received and processed messages, including anomalies, Processing of DCP data and bulletin preparation for distribution, Archiving of DCP data, Retrieval for DCP users, Generation/storage of performance analysis"]
-[7.281457901000977, 0.36396023631095886, "[TT] Mission Management of the OSIRIS-REx = Goddard"]
-[7.754708766937256, 8.228485107421875, "[TT] Dynamic Response Amplitude of the IPEX-II = Micrometers or less"]
-[3.585738182067871, 4.846002101898193, "[TT] Radar Type of the Biomass satellite = Fully polarimetric P-band synthetic aperture radar"]
-[9.557577133178711, 3.7183620929718018, "[FF] Resistance of the GMR = Decreases in the presence of an external magnetic field perpendicular to the magnetization of the layers"]
-[8.226502418518066, 1.9334099292755127, "[FF] Data Source of the Multiscale Ultrahigh Resolution Sea Surface Temperature (MUR SST) project = Measurements of sea surface temperatures from multiple NASA, NOAA, and international satellites, as well as ship and buoy observations"]
-[6.160828113555908, 0.9274778366088867, "[TT] Observation Date of the NGC 1068 = Between 2014 to 2015"]
-[6.981020450592041, 6.675166130065918, "[TT] Operational Mode of the CATS Laser 1 = Science Mode 1"]
-[8.382375717163086, 4.286446571350098, "[TT] Maneuver Type of the Spacecraft = Acquisition maneuvers"]
-[12.195751190185547, 2.9860782623291016, "[TT] Fuel of the RADARSAT-2 = Monopropellant hydrazine"]
-[12.152909278869629, 3.0399482250213623, "[TT] Propellant of the MTM CPS = MMH (Mono-Methyl Hydrazine) and MON (Mixed Oxides of Nitrogen)"]
-[12.162858963012695, 4.6005167961120605, "[TT] Bus Dimensions of the DubaiSat-1 = 1.2 m in diameter and 1.35 m in height"]
-[7.660897731781006, 6.802473545074463, "[TT] Exposure Time of the Active Regions = < 100 ms"]
-[5.850687503814697, 5.291975975036621, "[FF] Recommendation of the Connector Savers = Future projects should consider their implementation for external access ports"]
-[13.875692367553711, 2.745370626449585, "[TT] Launch Mass of the SES-17 = 6,411 kg"]
-[6.2122344970703125, 5.312213897705078, "[TT] Structure of the X50 avionics system = Card-frame with backplane interconnections"]
-[12.11281967163086, 4.576739311218262, "[TT] Size of the BRITE spacecraft = 200 mm x 200 mm x 200 mm"]
-[8.803078651428223, 5.386991500854492, "[TT] Absolute / Relative Misalignment of the Three-axis diagonal gradiometer = 10 -3  rad / 10 -5  rad"]
-[9.909205436706543, 7.3690104484558105, "[TT] Ground Sample Distance of the HPT = 3 m"]
-[6.347248554229736, 1.5320554971694946, "[TT] Survey Completion Date of the eROSITA = 11 June 2020"]
-[13.828082084655762, 7.231446266174316, "[TT] Output Short Circuit Protection of the DC-DC converter = Yes"]
-[7.734364032745361, 5.02691650390625, "[FF] Applications of the Special Sensor Microwave Imager Sounder (SSM/IS) = Global measurements of air temperature profiles, humidity profiles and other atmospheric measurements"]
-[6.288022041320801, 8.016575813293457, "[TT] Number of User-Platform Channels of the DCS = 433"]
-[4.3282928466796875, 3.1125829219818115, "[FF] Ground Stations of the GIOVE-B = Dongara (Australia), Kiruna (Sweden), Santiago de Chile (Chile), South Point Hawaii (USA), and Fucino (Italy)"]
-[2.9531185626983643, 4.422049522399902, "[TT] Surface Movement Detection of the NISAR = As small as 0.4 inches (1 cm)"]
-[8.590938568115234, 5.711236000061035, "[TT] Geodesy of the GPS and Galileo = Nearly identical at ~ 2 cm"]
-[3.702268600463867, 5.336112022399902, "[TT] Beam Steering Range of the Radar = Elevation: \u00b130\u00ba; Azimuth: \u00b13.5\u00ba"]
-[8.750248908996582, 0.133588969707489, "[TT] Checkpoint Maneuver Altitude of the OSIRIS-REx = 410 feet (125 meters)"]
-[5.694331169128418, 3.722025156021118, "[FF] Constellation Type of the OptiSAR\u2122 Constellation = Paired, tandem configuration"]
-[6.059776782989502, 6.291691303253174, "[TT] Technology Readiness Level of the OEM628 Receiver = TRL5"]
-[5.188736438751221, 1.7427070140838623, "[FF] Conference Presentation Date of the TacSat-4 = Aug. 10-15, 2013"]
-[6.758692741394043, 7.14492654800415, "[TT] Transmit Pulse Length of the SCA = 600 \u00b5s"]
-[6.030137538909912, 3.4165210723876953, "[TT] Number of Experiments of the ORS-3 Mission = 2"]
-[11.672560691833496, 3.3709208965301514, "[TT] Image Credit of the X50 series propulsion system = SSTL"]
-[6.5890793800354, 4.081353664398193, "[FF] Equipment Modules of the Terra = Sized and partitioned to facilitate pre-launch integration and test of the spacecraft"]
-[6.503530979156494, -0.4717554748058319, "[TT] Period of the RESURS-O1-4 = 101.2 minutes"]
-[11.762815475463867, 6.546830177307129, "[TT] Gamma Efficiency of the ECAL = > 90% above 2 GeV"]
-[9.648839950561523, 1.4179983139038086, "[TT] Image Resolution of the Pl\u00e9iades Neo constellation = 30 cm"]
-[7.968972682952881, 1.835472583770752, "[FF] Importance of the Near-shore Measurements = Provide a window into the coastal dynamics and processes"]
-[9.57027816772461, 4.261336803436279, "[TT] Orientation of the Magnetic Field Sensor = Four different orientations"]
-[5.064594745635986, 0.08334848284721375, "[TT] Founding Year of the Kleos Space = 2017"]
-[5.667549133300781, 0.6110416054725647, "[FF] First Quasi-Real-Time Demonstration Date of the SpaceDataHighway = Feb. 29, 2016"]
-[7.705730438232422, 0.518665075302124, "[FF] Purpose of the Lunar IceCube = Provide useful scientific data"]
-[13.1676025390625, 7.227199554443359, "[TT] Power Usage of the Microelectronic device = 20 times less than proven technology"]
-[5.261623382568359, 8.115434646606445, "[TT] ULF Frequency Range of the IME = 0 \u2013 64 Hz"]
-[6.133754253387451, 1.8048043251037598, "[FF] URL of the SCD-2 = http://www.las.inpe.br/~veissid/eng18.html"]
-[10.537144660949707, 5.737770080566406, "[TT] Dayside Temperature of the KELT-9 b = 7,800\u00ba Fahrenheit (4,300\u00ba C)"]
-[11.134039878845215, 3.7590835094451904, "[TT] Dimensions of the CubeSat = 10 cm x 10 cm x 10 cm"]
-[8.548019409179688, 8.468218803405762, "[TT] Spectral Resolution of the Spectrometer = <1.25 cm -1"]
-[4.59160041809082, 3.6075894832611084, "[TT] Ground Station of the CanX-7 = SFL ground station in Toronto"]
-[9.504587173461914, 7.011438846588135, "[TT] Spatial Resolution of the OCTS = Approx. 700 m"]
-[9.629091262817383, 4.5256547927856445, "[FF] Spin Rate of the P2 = Unknown"]
-[10.279293060302734, 1.9804365634918213, "[TT] Brightness Comparison of the Newly Detected Source = More than 1000 times fainter than Beta Pictoris"]
-[4.074803352355957, 2.116783618927002, "[TT] Stages of the Vega Launcher = Three SRM stages, a liquid propulsion upper module"]
-[11.20706558227539, 0.5798819661140442, "[FF] Mission Purpose of the SPARCS = Understand the Impact of Stars in Exoplanets"]
-[7.113165855407715, 3.8090457916259766, "[FF] Mission Objectives of the PROBA-3 = Formation flying demonstration, Equipment qualification, Development, design and validation principles for formation flight, Relative dynamics experiments, Guest payload"]
-[8.498723983764648, 4.170195579528809, "[FF] Function of the Sun Baffle = Ensures the straylight rejection for the sun calibration"]
-[5.755080223083496, 8.163688659667969, "[TT] Footprint Sampling of the SSM/I sensor = Every 25 km for the 19, 22, and 37 GHz channels, and every 12.5 km for the 85 GHz channel"]
-[12.075129508972168, 4.483489513397217, "[TT] Platform Size of the Satellite = 2.26 m x 1.9 m x 2.53 m"]
-[8.260157585144043, 2.5342931747436523, "[TT] Purpose of the CATS = Measure clouds and aerosols"]
-[11.798086166381836, 4.7163801193237305, "[TT] Length of Central Cylinder of the Vacuum Tank = 0.9 m"]
-[4.85603141784668, 7.05411958694458, "[TT] TRL of the Myriad RF board = 3"]
-[7.252552032470703, 8.332648277282715, "[TT] Artists of the Sojourner 2020 = Nine"]
-[13.622661590576172, 5.770691394805908, "[TT] Solar Cell Average Power of the S/C = 1.4 W"]
-[5.58965539932251, 2.27951979637146, "[TT] Secretariat Location of the Joint Project Team (JPT) = JAXA"]
-[6.510728359222412, 8.467352867126465, "[TT] Cross Polarization of the Satellite = >20 dB"]
-[6.323929309844971, -0.3281732201576233, "[TT] Payload Calibrations and Experiments Duration of the TeLEOS-1 = Five months"]
-[6.551190376281738, 5.456004619598389, "[TT] Environment of the Linear Encoder = Vacuum-rated"]
-[6.826980113983154, 0.6581359505653381, "[FF] Sky Survey Period of the Kepler and K2 missions = 2009 to 2018"]
-[8.275568008422852, 8.713674545288086, "[TT] Spectral stability of the UV/VIS Spectrometer = 0.04 nm"]
-[9.39993667602539, 6.2349467277526855, "[TT] Scan Angle of the VIRR = \u00b151.2\u00ba"]
-[10.348668098449707, 7.133180618286133, "[TT] CONUS Rectangle Height of the ABI = 3000 km"]
-[11.718214988708496, 6.606435775756836, "[TT] Energy Measurement Range of the ECAL = Up to 1 TeV"]
-[6.126941680908203, 5.404085159301758, "[FF] Type of the OBC = Proof-of-concept test"]
-[10.126282691955566, 4.53548526763916, "[TT] Torque Margin of the SADM = High"]
-[13.73056411743164, 5.401003837585449, "[TT] Solar Cells of the GNB = Up to six triple-junction solar cells on each face"]
-[14.066032409667969, 3.0171430110931396, "[TT] Mass of the ADEOS-II = 3700 kg"]
-[7.104408264160156, 1.8562930822372437, "[TT] Launch Date of the Carbon Mapper constellation = 2023"]
-[8.904524803161621, 4.734480857849121, "[TT] Attitude Data Update Frequency of the BOKZ-M star tracker = 0.3 Hz"]
-[8.169766426086426, 0.0950741171836853, "[TT] Launch Date of the Meteor-1-2 = 06.10.1969"]
-[8.768765449523926, -0.08675485849380493, "[TT] Deep Space Flight Distance of the Chang'e-2 = 40,000,000 km"]
-[5.001082420349121, 3.193852663040161, "[TT] Manufacturer of the CHRIS = Space Group of Sira Electro-Optics"]
-[5.751519680023193, 0.7851089239120483, "[TT] Release Date of First 13 Photos of the Gaofen-1 = June 6, 2013"]
-[10.877657890319824, -0.32981663942337036, "[FF] First Image Transmission Date of the TanDEM-X = June 25, 2010"]
-[9.776789665222168, 1.948607325553894, "[FF] Function of the WFIRST = Provide the largest picture of the universe ever seen with the same depth and precision as the Hubble Space Telescope"]
-[8.498614311218262, 1.9795621633529663, "[FF] Characteristics of the Streamer belt = Longitudinal density fluctuations"]
-[9.73194694519043, 4.841706275939941, "[FF] Rotation Modes of the AMSR2 = Lower (11 rpm), Regular observation mode (40 rpm)"]
-[5.558485984802246, 6.579933166503906, "[TT] Data Volume of the Hubble = 172 terabytes of data since its launch in 1990"]
-[6.098351955413818, 2.629441976547241, "[TT] Number of Countries with Researchers of the International Space Station = 106 countries"]
-[9.160809516906738, 8.686827659606934, "[TT] Slit Width of the Spectrometer = 84 \u00b5m"]
-[9.541478157043457, -1.1335099935531616, "[TT] Longitude of the Launch/Check-out Position = 90\u00ba W"]
-[4.704765319824219, 0.36354032158851624, "[TT] Telemetry Monitor of the SpaceX CRS-17 = Christina Koch"]
-[6.709295272827148, 3.8409247398376465, "[FF] Data Collection of the Ground Penetrating Radar = Ongoing"]
-[4.4503173828125, 7.923681259155273, "[TT] UHF RDS Transmission Frequencies of the DMSP = 400.328 MHz, 400.822 MHz"]
-[8.155557632446289, 4.094092845916748, "[TT] Ground Track of the JPSS-1 = 20 km repeat accuracy at the equator with 20 day repeat cycle"]
-[3.4155287742614746, 4.879782199859619, "[FF] Application of the SAR Sensor = Counting parked vehicles"]
-[5.265080451965332, 4.741190433502197, "[TT] Availability of the GPS Simulator = Not available"]
-[8.039661407470703, 8.649968147277832, "[TT] Spectral range of the TOU = 308-361 nm"]
-[7.201549053192139, 7.904497146606445, "[TT] Dynamic Range (Near) of the Satellite = -8.6 - 4.3 dB"]
-[14.087568283081055, 4.0489115715026855, "[TT] Mass of the Instrument = 13 kg"]
-[9.698046684265137, -0.3781513273715973, "[TT] Scan Altitude of the MAHRSI = 160 to 48 km"]
-[8.732583045959473, 7.596541404724121, "[TT] Detector Format of the CIRC = 640 x 480 pixels"]
-[8.058616638183594, 3.3340675830841064, "[FF] Concentration of the TANSO-FTS-2 = Higher CH4 concentration in Southeast and South Asia, Central Africa and in the northern part of South America"]
-[6.572396755218506, 8.690290451049805, "[TT] Value of the Polarization Sensitivity = Less than 2%"]
-[10.545133590698242, 5.334748268127441, "[TT] Heater Lines of the STC = 8"]
-[8.531595230102539, 5.489701747894287, "[TT] Ambiguity Under Worst Case Scenario of the Satellite = 0.34 - 3.3%"]
-[6.060109615325928, 3.8840243816375732, "[FF] Design of the DMSP Block 5D-1 = Resembled in appearance conventional Earth-oriented satellites of this period"]
-[9.508942604064941, 6.192702293395996, "[TT] Incidence Angle Range of the Wide Fine Quad-Polarisation Mode = 18-42\u00ba"]
-[8.162732124328613, 1.4367810487747192, "[FF] Objective of the IMI = Provide an advanced measurement capability on soil moisture and ocean salinity parameters from space"]
-[8.020467758178711, 5.835715293884277, "[FF] Purpose of the BPP = Enable the High-Resolution Camera to point in the direction of its targets and keep its field of view stable"]
-[4.874906063079834, 8.354046821594238, "[TT] Frequency of the 37 GHz MWI = 37 GHz"]
-[3.1974713802337646, 3.850332736968994, "[TT] Data Collection Time of the TerraSAR-X = 60 years"]
-[5.629095077514648, 2.779726505279541, "[FF] Consortia of the Moonlight = The consortium includes: satellite operators Inmarsat and Hispasat; manufacturing companies such as Thales Alenia Space Italy, OHB System in Germany and Canadian space technology company MDA; Italian Aerospace Logistics Technology Engineering Company (ALTEC); small and medium-sized enterprises such as Nanoracks Europe and Argotec; and universities and research centres such as SEE Lab, SDA Bocconi and Politecnico di Milano"]
-[7.802517890930176, 2.936394691467285, "[TT] Team Leader of the Carbon Dioxide Spectrometer = Changxiang Yan"]
-[9.694476127624512, -0.1648523062467575, "[TT] Orbital Altitude Range of the TSUBAME = 200 km - 300 km"]
-[5.045091152191162, 2.4289371967315674, "[FF] Sponsor of the STPSat-3 = ORS (Operationally Responsive Space) Office"]
-[4.851125717163086, 3.2008931636810303, "[TT] Manufacturer of the ACLS = Airbus"]
-[6.308697700500488, 5.370543956756592, "[FF] Data Storage of the SSMM = Unknown"]
-[7.98781681060791, 6.3416571617126465, "[TT] Type of the SUVI = Imaging multi-spectral radiometers (vis/IR)"]
-[5.175130367279053, 0.699347734451294, "[TT] First Data Transmission Date of the FTHSI = Aug. 1, 2000"]
-[8.068265914916992, -0.9070863723754883, "[TT] GPS Data Collection Location of the ICESat-2 = 88 degrees south"]
-[5.4238200187683105, 2.747810125350952, "[FF] Operator of the Canadarm2 = Astronauts"]
-[10.530096054077148, 2.84135103225708, "[TT] Onboard Computers of the Nanosatellite = 2"]
-[8.532977104187012, 5.7434563636779785, "[TT] Accuracy of the NIDEM = Less accurate for rocky shores"]
-[10.076181411743164, 2.9572412967681885, "[TT] Manifested Date of the ELaNa-4 CubeSats = March 1, 2013"]
-[6.713024139404297, 0.9091625809669495, "[TT] Data Availability of the Landsat 5 TM = All TM data December 2008"]
-[7.993707180023193, 2.1308376789093018, "[FF] Sensor Capabilities of the SeaSat-A = Wave heights, Wavelength and direction, Surface wind speed and direction, Ocean surface temperature, Atmospheric water content (liquid and vapour), Sea ice morphology and dynamics, Icebergs"]
-[10.648550033569336, 1.5829684734344482, "[FF] Luminosity of the Neutron Star = 1000 times more than the maximum thought possible for an accreting neutron star"]
-[7.560641765594482, 2.852724075317383, "[TT] Payloads of the FormoSat-2 = ISUAL (Imager of Sprites and Upper Atmospheric Lightning), RSI (Remote Sensing Instrument)"]
-[11.616244316101074, 3.212963581085205, "[TT] Attitude Control Thrusters of the INSAT-2A/2B = 16"]
-[8.002245903015137, 7.28368616104126, "[TT] Exposure Levels of the CCD Detector = Six non-zero levels"]
-[8.4020414352417, 3.1736953258514404, "[FF] Publication Date of the Solar Backscatter Ultraviolet/Total Ozone Mapping Spectrometer (SBUV/TOMS) = 1975"]
-[5.636249542236328, 5.054680824279785, "[TT] Operation of the ROSA = Provides observable data for each GPS satellite in lock"]
-[7.296020030975342, 8.888261795043945, "[TT] Passbands of the HIRES = 395 - 435 nm, 535 - 585 nm, 625 - 675 nm, 725 - 775 nm, and 450 - 800 nm"]
-[6.804305076599121, 4.255943298339844, "[FF] Projected Quantity of the Artificial Objects = Double"]
-[6.2563910484313965, 4.8521647453308105, "[FF] Function of the Control and Timing Unit (CTU) = Receives commands from the satellite platform and sends state monitoring data to it"]
-[11.449761390686035, 3.3048171997070312, "[TT] Type of the ENPULSION MICRO R3 = Microthruster"]
-[3.168097496032715, 2.3606560230255127, "[FF] Data Contribution of the Sentinel-6 = Sea state and wind speed measurements"]
-[10.230746269226074, 5.3613152503967285, "[FF] Reason for Concept Change of the ALBus = Critical thermal issue and mass budget constraints"]
-[12.239872932434082, 3.6674482822418213, "[FF] URL of the Critical Viscosity of Xenon\u20132 (CVX\u20132) = http://spaceresearch.nasa.gov/sts-107/107_cvx.pdf"]
-[8.057605743408203, 3.653416872024536, "[TT] Observation Mode Switching of the OCO = Alternate 16-day global ground-track repeat cycles"]
-[7.316059112548828, 5.934440612792969, "[FF] Flatness of the FPA = Guaranteed"]
-[12.17116928100586, 0.5654935836791992, "[FF] Mission Goal of the PLATO = Detect and study exoplanets"]
-[3.8057239055633545, 0.8782907128334045, "[FF] Launch Date of the PSLV-C38 = June 23, 2017"]
-[9.941965103149414, -0.3581986725330353, "[TT] Altitude of the Meteosat-7 = 35,786 km"]
-[5.747155666351318, 1.9472777843475342, "[FF] Deployment of the LARES-2 = Italian Space Agency's LARES-2 scientific payload"]
-[7.263027191162109, 5.622691631317139, "[FF] Instruments of the Resurs-DK1 = Arina, Pamela, Geoton-L1"]
-[4.527604103088379, 1.2578014135360718, "[TT] Launch Time of the AlSat-2B = 03:42:00 UTC"]
-[9.109550476074219, 3.0619332790374756, "[FF] Purpose of the PLS = Measure plasma and ionized particles around the outer planets and to measure the solar wind\u2019s influence on those planets"]
-[6.027456283569336, 2.0252740383148193, "[FF] NEdT Performance of the VIIRS = Excellent"]
-[7.868511199951172, -0.9563814401626587, "[FF] Issue of the ICESat-2 = Issue3"]
-[5.763313293457031, 6.825860500335693, "[TT] Data Packet Length of the Science Data Interface = 1024 bytes"]
-[7.879580974578857, 3.2547755241394043, "[FF] Camera Function of the InSight = Guiding the placement of the SEIS and HP3 instruments, taking pictures of the surrounding landscape"]
-[6.082983016967773, 5.473057270050049, "[FF] Redundancy of the EPS = MPPT system and regulators had been duplicated"]
-[5.010931968688965, 3.38950777053833, "[TT] Manufacturer of the SCM = CNRS/CETP"]
-[6.028719425201416, 5.722976207733154, "[TT] FPGA of the AIM = Xilinx XQR4062XL"]
-[10.360645294189453, 3.2364420890808105, "[TT] Number of Non-separating Components of the CubeSat = 2"]
-[4.789935111999512, 7.26664400100708, "[FF] RF Communications of the ASNARO-2 = X-band downlink, 16QAM(Quadrature Amplitude Modulation) scheme, data rate ~800 Mbit/s"]
-[11.170015335083008, 3.312199354171753, "[FF] Purpose of the Micropropulsion = Provide propulsion for small satellites, nanosatellites, and CubeSats"]
-[5.206916332244873, 0.18790118396282196, "[FF] Resupply Mission Finish Date of the Cygnus Commercial Cargo Ship = August 15, 2014"]
-[13.233033180236816, 7.267641067504883, "[TT] Power Consumption of the DPU = < 29 W"]
-[6.323293209075928, 6.995739459991455, "[TT] Operating Ranges of the Cluster S/C = 64 to + 63.992 nT, 256 to + 255.97 nT, 1024 to + 1023.9 nT, 4096 to + 4095.5 nT, 65536 to + 65528 nT"]
-[7.555904865264893, 3.0513100624084473, "[TT] Cryogenic System of the MethaneSAT = Focal Plane Cooling"]
-[4.7989501953125, 0.8191361427307129, "[TT] Start of Operations of the Resurs-O1 = 1985"]
-[6.952680587768555, 8.839812278747559, "[TT] Lidar of the POLDER-1/2 = 532 nm"]
-[4.262512683868408, 0.69364994764328, "[TT] Launch Date of the EDRS-C = 2018"]
-[13.985688209533691, 2.837928533554077, "[TT] Mass of the Tianquin-1/CAS-6 = 35 kg"]
-[9.634970664978027, 8.17123794555664, "[TT] Field of View of the LRR = \u00b157.6\u00b0"]
-[11.135339736938477, 5.275547504425049, "[FF] Affiliation of the Gamma-ray Spectrometer Experiment = University of New Hampshire"]
-[4.406463623046875, 3.0600690841674805, "[TT] Location of the RBU (Remote Backup) Facility = Fairmont, W.VA"]
-[5.899941921234131, 1.620740294456482, "[TT] Launch Date of the VIIRS = Oct. 28, 2011"]
-[9.265242576599121, -0.3848095238208771, "[TT] Second Orbit Apogee Altitude of the EFT-1 Orion = 5,808 km"]
-[6.603898048400879, 5.155220985412598, "[FF] Function of the IPU = Sampling and digital signal processing"]
-[8.128815650939941, 4.582214832305908, "[FF] Components of the Unpressurized Cargo = CALET (Calorimetric Electron Telescope)"]
-[3.341419219970703, 1.4793996810913086, "[FF] Launch Date of the Sentinel-3B = Spring 2018"]
-[6.94476842880249, 0.9062574505805969, "[FF] Landing Date of the Zhurong Mars Rover = Last week"]
-[9.824382781982422, 0.6248547434806824, "[TT] Distance from Surface of the Spacecraft = Several hundred meters"]
-[5.927194595336914, 3.643584966659546, "[FF] Service Emphasis of the Lacuna Space = Lowest price"]
-[3.4699923992156982, -0.8880394697189331, "[TT] Constellation of the DMSP = Two near-polar, sun-synchronous satellites"]
-[5.585636138916016, 6.962848663330078, "[TT] Upload Data Rate of the IXPE = 2 kbit/s"]
-[8.743514060974121, 2.986693859100342, "[FF] Goal of the CADRE = Enable more accurate specification and prediction of the state of the thermosphere"]
-[6.29537296295166, 4.61378288269043, "[FF] Affiliation of the Global Navigation System GPS = Various"]
-[5.493955612182617, 6.294131755828857, "[TT] Capacity of the Mass Memory System = 256 Gbit"]
-[8.548017501831055, 7.881667137145996, "[TT] Spectral Data Pixels of the Detector = 75 pixels"]
-[6.81553840637207, 1.7447353601455688, "[FF] URL of the InSight Mars Lander = https://www-robotics.jpl.nasa.gov/projects/InSight.cfm?Project=7"]
-[4.935073375701904, -0.34425121545791626, "[TT] Launch Time of the FY-3E = 23:28 UTC"]
-[12.056365966796875, 6.25767707824707, "[TT] Studied Nuclei of the AMS = Helium, lithium, carbon, oxygen and heavier nuclei up to iron"]
-[5.883872985839844, 0.9179050326347351, "[TT] Image Acquisition Date of the Kirkuk = 21 Jun. 2014"]
-[5.544559001922607, 4.972651958465576, "[FF] GPS Receiver of the AOCS = Dual frequency GPS receiver (GPSR)"]
-[8.29189682006836, 2.0596392154693604, "[FF] Instruments of the CFOSAT = SWIM (Surface Waves Investigation and Monitoring), SCAT"]
-[10.655282974243164, -0.41444501280784607, "[TT] Mission Duration of the Tandem-L = 10 years"]
-[8.470507621765137, 6.951421737670898, "[FF] Assumption of the Background Level = Use of depth-of-interaction measurement to reject interactions in the back of the detector"]
-[6.165246486663818, 6.885290622711182, "[TT] Number of Optical Links per Day of the System = Up to 22"]
-[9.220372200012207, 7.128726482391357, "[TT] Resolution of the Overall Moon Image = 7 m"]
-[8.918732643127441, 4.758023262023926, "[FF] Purpose of the OSIRIS = Attitude control system and satellite performance testing"]
-[11.75666332244873, 4.725478172302246, "[TT] Dimensions of the IMP-8 = 135.6 cm diameter and 157.4 cm high"]
-[5.040414810180664, 3.4100661277770996, "[TT] Manufacturer of the POPSat-HIP-1 = Microspace Rapid Pte Ltd."]
-[3.4385998249053955, 3.632073402404785, "[FF] Mission Type of the PAZ = Dual use (civil/defense)"]
-[12.155936241149902, 3.2590816020965576, "[TT] Capacity of the Iodine Storage Tank = 1.5 kg"]
-[3.357168436050415, 4.319876194000244, "[FF] Measurement Domain of the PALSAR-2 = Ocean imagery and water leaving spectral radiance, Land surface imagery, Vegetation type, Fire fractional cover, Earth surface albedo, Land surface temperature, Land surface topography, Wind vector over sea surface (horizontal), Sea-ice cover, Snow cover, Soil moisture at the surface, Iceberg fractional cover, Sea-ice type, Glacier motion, Sea-ice sheet topography, Oil spill cover, Crustal Motion, Above Ground Biomass (AGB), Active Fire Detection, Snow melting status (wet/dry)"]
-[3.342417001724243, 4.950761318206787, "[FF] Imaging Modes of the SAR Instrument = Strip imaging, spot imaging"]
-[4.745448589324951, -0.003046994097530842, "[TT] End of Life Date of the MTSAT = 31 Dec 2018"]
-[6.782777309417725, -0.5881240367889404, "[TT] Period of the ExoMars Orbiter = ~2 hours"]
-[4.397724151611328, 1.5603476762771606, "[FF] URL of the ROCSAT 2 = https://web.archive.org/web/20170812134946/http://sprite.phys.ncku.edu.tw/En/Eindex.html"]
-[7.183760643005371, 5.095368385314941, "[TT] Safety Factor of the ESPA ring = 2.0"]
-[10.212881088256836, 1.3625853061676025, "[TT] Number of Stars with Parallax and Proper Motion of the Gaia EDR3 = Almost 1.5 billion"]
-[9.820199012756348, -0.4730176031589508, "[TT] Longitude Range of the PRISMA Payload = 180\u00b0W - 180\u00b0E"]
-[6.11472225189209, 5.522404670715332, "[FF] Redundancy of the PCDM = Cold redundant"]
-[10.636404037475586, 8.881159782409668, "[TT] Pixel size of the Channel 2 = 32 km x 32 km"]
-[3.2609825134277344, 5.224363327026367, "[TT] Inclination Angle of the SAR Antenna = 29.8\u00ba"]
-[5.759963512420654, -0.7321352362632751, "[TT] Operational Lifetime of the Observatory = 5 years"]
-[7.9945478439331055, 6.255345344543457, "[TT] Instrument Type of the QBITO = Imaging multi-spectral radiometers (vis/IR)"]
-[8.106945991516113, 4.228997707366943, "[FF] Orbit Offset of the ERS-2 = 2 km versus nominal ground track"]
-[9.319746971130371, 3.3833324909210205, "[FF] Research Focus of the MMS = How electrons move through the magnetosphere"]
-[9.813013076782227, 8.371210098266602, "[TT] FOV of the Optical telescope = 1.38\u00ba"]
-[3.741229295730591, -0.7370008230209351, "[TT] Orbit of the CSSWE = Low Earth Orbit"]
-[6.478489398956299, 0.21845978498458862, "[TT] Operation Pause Duration of the InSight = Several weeks"]
-[6.952686309814453, 1.9653903245925903, "[FF] URL of the CubeSat = http://m.esa.int/Our_Activities/Space_Engineering_Technology/ESA_CubeSat_found_answers_blowing_in_the_wind"]
-[6.263747215270996, -0.40779909491539, "[TT] Underflight Duration of the SSMIS = 5 hours"]
-[11.90895938873291, 5.478625774383545, "[TT] Instrument Size of the HySI = 275 mm x 275 mm x 205 mm"]
-[13.404708862304688, 5.4669718742370605, "[FF] Solar Array of the ESPA Ring = Single-panel body mounted"]
-[13.165940284729004, 7.290289402008057, "[TT] Power Consumption of the Nexus = 1 watt"]
-[5.441703796386719, 3.018120527267456, "[TT] Coverage of the EUTELSAT KONNECT = Up to 40 countries across Africa and 15 over Europe"]
-[8.360528945922852, 3.969654083251953, "[FF] On-orbit Calibration Target of the ARTEMIS = Panel with relatively flat spectral reflectance and measured reflectance characteristics"]
-[6.370800971984863, 5.5988922119140625, "[TT] L0 Product Destination of the EnMAP = DIMS Product Library"]
-[9.283185958862305, 2.755662202835083, "[TT] Solar Wind Speed and Beta of the ACE = ~34% lower on average from 2009 through the day 79 of 2013"]
-[10.504365921020508, 2.272296905517578, "[FF] Localization Area of the Optical or X-ray observation = Large"]
-[3.9136083126068115, 6.5863471031188965, "[TT] Antenna Type of the DCS platform = UHF receive antenna"]
-[6.575930595397949, 5.679003715515137, "[FF] Signal Assessment Modes of the Hertz = Local \u2018near-field' or as if the signal has crossed thousands of kilometers of space"]
-[9.959382057189941, 0.8298025727272034, "[TT] Separation Method of the ASTRO and NextSat = ASTRO's robotic arm"]
-[9.861178398132324, 8.759185791015625, "[TT] IFOV of the MS = 7.35 \u00b5rad"]
-[5.559942245483398, -1.9192333221435547, "[FF] Mission Status of the KOMPSAT-3A = Unknown"]
-[5.23089075088501, 0.9555892944335938, "[FF] Date of the E-OSPF = May 3-6, 2009"]
-[8.740967750549316, 6.670073986053467, "[TT] Commanded Rate of the MicroSCOPE = 5 x 10-3 rad/s around the X-axis"]
-[5.331316947937012, 6.6369781494140625, "[TT] On-board Storage Capacity of the RF Communications = 32 Gbit"]
-[3.409975051879883, -0.8758770823478699, "[TT] Orbit Type of the STARS spacecraft = Sun-synchronous near-circular orbit"]
-[9.445281982421875, 8.926796913146973, "[TT] Frame Rate of the Iris Video Camera = 30 frames/s"]
-[2.080622911453247, -0.29563379287719727, "[FF] URL of the Radiation Belt Storm Probes = http://vanallenprobes.jhuapl.edu/common/content/pdfs/VanAllenProbes_FS_Press.pdf"]
-[1.7694926261901855, -2.0610618591308594, "[FF] Mission of the Hayabusa-2 = Asteroid surface exploration"]
-[10.981182098388672, 6.358760356903076, "[FF] Polishing, Coating, Integration of the SiC mirrors = Unknown"]
-[4.407963752746582, 7.782040596008301, "[TT] Frequency of the VHF Downlink = 143.625 MHz"]
-[5.691814422607422, 4.736517906188965, "[TT] Communication Link of the EDRS-D = Geostationary relay satellite of the SpaceDataHighway"]
-[4.940227508544922, 0.3766736388206482, "[TT] Actual Launch Date of the Spacelab-1 = End of November 1983"]
-[6.400120735168457, 0.9416404366493225, "[FF] Observation Date of the Perseus = 29 October 2018"]
-[11.468457221984863, 5.7581706047058105, "[FF] Components of the Bus Structure = Metallic cube (aluminum panels), four motherboards"]
-[6.997496604919434, 8.250345230102539, "[TT] SNR of the ALOS-3/PRISM-2 = >200"]
-[7.890657424926758, 6.236494541168213, "[TT] Instrument Type of the CZI = Imaging multi-spectral radiometers (vis/IR)"]
-[4.819925785064697, 7.383677005767822, "[TT] TC Rate of the S-band transceivers = 20 kbit/s"]
-[10.379905700683594, 3.2138421535491943, "[TT] Platform of the SpooQySat = 3U GomX CubeSat"]
-[4.894442558288574, 0.43452540040016174, "[TT] Launch Date of the RHESSI = Jun 13, 2012"]
-[9.830764770507812, 4.765867710113525, "[TT] Spin Rate of the CINEMA satellites = 2 rpm"]
-[11.317620277404785, 5.825564861297607, "[TT] Material of the Canister = Aluminum alloy"]
-[6.924949645996094, 4.401050090789795, "[TT] Mounting Location of the TSIS-1 = ELC-3 platform, which is attached to the station\u2019s P3 port truss segment"]
-[8.072199821472168, 7.358443260192871, "[TT] Photometric Sensitivity of the Instrument = 0.75 counts /s /Rayleigh /1\u00ba pixel"]
-[18.66605567932129, 3.9355928897857666, "[TT] NE\u0394T (K) of the ICI-10 = 1.9"]
-[4.804837226867676, 8.197815895080566, "[TT] Band Frequency of the OneWeb = 12 GHz"]
-[3.0660524368286133, 2.4607627391815186, "[TT] Wavefront Error of the Sentinel-4 GRU = 19.8 nm (rms)"]
-[10.154393196105957, 5.392792224884033, "[TT] Handling Safety of the Soft Stack = Can be handled safely for thermal cycling"]
-[9.160752296447754, -1.2650808095932007, "[TT] Orbit of the GOMS-1 = Geostationary orbit"]
-[10.350408554077148, 5.358834266662598, "[FF] Active Temperature Control of the SVM = Heaters controlled by thermostats"]
-[4.892673969268799, 0.8341925740242004, "[TT] Anomaly Date of the Ariane 5 = January 25, 2018"]
-[7.3550496101379395, 0.22876262664794922, "[TT] Launch Date of the OSIRIS-REx = September 2017"]
-[8.443794250488281, 1.676647424697876, "[TT] Sea Surface Temperature of the Tauktae = 31\u00b0 Celsius (88\u00b0 Fahrenheit)"]
-[9.849700927734375, 5.7199835777282715, "[FF] Purpose of the PLM Demonstrator Breadboard (DMBB) = To get early information on suitability of Optical Bench design w.r.t. thermoelastic stability requirements"]
-[9.444559097290039, 4.080873966217041, "[TT] Type of the Fluxgate Sensors = Ring core-types"]
-[4.142367362976074, 5.7351765632629395, "[FF] Current Fleet Installation of the ADS-B Receiver = 70%"]
-[6.39391565322876, 7.56531286239624, "[TT] Data Quantization of the DubaiSat-2 = 10 bit"]
-[6.089061260223389, 6.514063358306885, "[TT] Bit Size of the Event = 64-bit"]
-[7.769378185272217, 9.414680480957031, "[TT] Band Center Wave of the DNB = 0.70 \u00b5m"]
-[5.863255500793457, 3.7806365489959717, "[TT] Environment of the Functional Tests = Ambient (and gravity)"]
-[8.759313583374023, 2.105851411819458, "[TT] Wind Speed Accuracy of the NSCAT = 2 m/s (rms)"]
-[3.50504207611084, 4.8904008865356445, "[FF] Real Time of the SAR Processors = Unknown"]
-[3.9670357704162598, 2.126288414001465, "[TT] Compatible Launch Vehicles of the CubeStack = Athena, Minotaur I, Taurus, Pegasus and Falcon 1"]
-[13.371843338012695, 7.18067741394043, "[TT] Power of the Payload = 3.5 W"]
-[7.690800189971924, 0.33092209696769714, "[FF] Expected Discoveries of the Lucy = Open new insights into the origins of our Earth and ourselves"]
-[5.833115100860596, -0.833443284034729, "[TT] Design Life of the Spacecraft = 1 year with expendables"]
-[3.0317726135253906, 0.010066349059343338, "[TT] NORAD ID of the BX-1 = 33392"]
-[10.066543579101562, -1.5419394969940186, "[TT] Orbit Inclination of the CanX-6/NTS = 97.83\u00ba"]
-[9.370450019836426, 6.24722146987915, "[TT] Maximum Beam Scanning Angle of the P Mode = \u00b1 1.9\u00ba"]
-[7.791875839233398, 5.021725654602051, "[FF] Ground Resolutions of the DMSP SSM/I sensor = Different for each frequency"]
-[6.128781318664551, 4.3342766761779785, "[FF] (International) Harmonization of the CSK GS = Verify and harmonize the Service Request lists coming from the different Partners"]
-[6.995219707489014, 8.054228782653809, "[TT] Intrinsic Noise Level of the ISA = About 10-10g/\u221aHz"]
-[13.396357536315918, 6.915735244750977, "[TT] Average Power of the Payload = 1 kW"]
-[7.508660316467285, 8.681808471679688, "[FF] Max Radiance of the UVI instrument = 1000"]
-[9.745954513549805, 0.44949665665626526, "[TT] Relative Maneuver Precision of the PROBA-3 = Millimeter and fraction-of-a-degree"]
-[7.808448791503906, 2.458040475845337, "[FF] Test Types of the Sensor Web Project = Volcanos, flooding, cryosphere events, and atmospheric phenomena"]
-[7.7974114418029785, 2.3296732902526855, "[FF] Impact of the PACE = Affect and are affected by rising atmospheric CO2 levels and Earth\u2019s changing climate"]
-[7.843588829040527, 6.6220550537109375, "[TT] Sector Observation Time of the Cameras = 27 days"]
-[8.439920425415039, 6.595129013061523, "[TT] Spectral Resolution of the TEMPO instrument = 0.6 nm"]
-[4.3916015625, 3.175285816192627, "[TT] Ground Station of the RF Communications = SPIV (San Pietro in Vincoli)"]
-[6.356748104095459, 0.3863489329814911, "[TT] General Program Max Targets per Day of the SVOM = 14"]
-[5.586305141448975, 0.4128943979740143, "[TT] End of Operations Date of the GEOS-1 = January 1968"]
-[7.169658660888672, 1.799815058708191, "[FF] URL of the Jupiter's Auroras = https://www.nasa.gov/feature/jpl/jupiter-s-aurora-presents-a-powerful-mystery"]
-[9.8603515625, 2.9146599769592285, "[FF] Flight Selection of the KickSat-2 = NASA's CubeSat Launch Initiative (CSLI)"]
-[7.589121341705322, 3.0804085731506348, "[TT] Mission Priority of the GOSAT = Short wave infrared observation"]
-[5.320939540863037, 6.603890419006348, "[TT] Mass Memory Capacity of the RF Communications = 16 Gbit"]
-[9.654104232788086, 8.345077514648438, "[TT] Field of View (FOV) of the PH1, PH2, PH3 = Same as that of the camera"]
-[9.348902702331543, 5.195019721984863, "[TT] Pointing Stability of the ADCS = \u00b11\u00ba"]
-[3.8236851692199707, 4.532180309295654, "[TT] Average AOI Coverage of the RADARSAT-2 = 48.8%"]
-[8.926549911499023, -0.5123521685600281, "[TT] Super-Synchronous Deployment Perigee of the ABEX = 185 km"]
-[8.699175834655762, -0.21272912621498108, "[FF] Preliminary Circular Lunar Orbit of the Chang'e-2 = 100 km x 100 km"]
-[7.79056978225708, 2.000655174255371, "[FF] Purpose of the GOCI = Monitor marine ecosystems and measure ocean chlorophyll concentration"]
-[5.818720817565918, 2.84535813331604, "[FF] Approach of the New Space Companies = Make access to space affordable through innovation, flexibility, and miniaturization"]
-[9.724417686462402, 4.5402140617370605, "[FF] Components of the Momentum-Bias Attitude-Control System = Momentum wheel, horizon scanner, magnetic coils"]
-[9.375510215759277, 5.019163608551025, "[TT] Roll/Pitch Pointing Accuracy of the Attitude Control = \u00b10.3\u00ba"]
-[13.472384452819824, 7.415657997131348, "[TT] Power of the PEACE = 5.0 W"]
-[8.350653648376465, 5.3632354736328125, "[TT] Radiometric Calibration Accuracy (Absolute) of the TanSat = 5%"]
-[7.704301834106445, 0.4407844841480255, "[TT] Shrunk Period of the Po River = June 2020 and June 2022"]
-[7.290258884429932, 1.0463809967041016, "[FF] Legacy of the Seasat = 25 years"]
-[10.77499008178711, 1.7552183866500854, "[FF] Gravitational wave detections of the LIGO = Captured four dozen mergers"]
-[7.061502456665039, 8.061336517333984, "[TT] Total Ambiguity Ratio of the Instrument = \u2264 -18 dB"]
-[5.371566295623779, 2.218405246734619, "[TT] Mission Type of the FalconSat-7 = Proof-of-concept"]
-[3.782391309738159, 6.222057342529297, "[TT] Number of Antennas of the KSAT = Over 200"]
-[6.513266563415527, 4.404562473297119, "[FF] Parameters of the Optional Payloads = Mass, Power, Data Requirements"]
-[7.90924596786499, 3.165210247039795, "[TT] Absorption at 0.90 \u00b5m of the Water (H2O) = 10 -21 mol cm -2"]
-[6.582215309143066, -2.0411500930786133, "[FF] Launch Services Contract Date of the Jason-3 = July 16, 2012"]
-[10.153360366821289, -2.765925645828247, "[TT] Partition net capacity of the SLC NAND-FMM = 512 Gbit"]
-[9.295180320739746, 5.006434440612793, "[TT] Attitude Error of the AOCS = <0.3\u00ba"]
-[6.615133762359619, 0.9756475687026978, "[FF] Orbital Energy of the BepiColombo = Same as Earth's"]
-[3.359344005584717, 6.307635307312012, "[TT] Payload Dimensions of the Antenna Mast = Approximately 38 cm x 36 cm x 32 cm"]
-[4.203607559204102, 3.8629322052001953, "[TT] Signal Health of the Galileo = 97.33%"]
-[4.271414279937744, 0.813441276550293, "[FF] Launch Year of the EDRS-C = 2019"]
-[7.704156398773193, 9.392515182495117, "[TT] Center Wavelength of the Band 5 = 1.61 \u00b5m"]
-[6.278947353363037, 3.9420716762542725, "[FF] Objective of the CIL = Reduce life cycle costs"]
-[8.115623474121094, -0.6689412593841553, "[FF] Observation Data of the CryoSat-2 = Changes in ice thickness for October/November 2011, 2012 and 2013"]
-[5.437848091125488, 0.5525213479995728, "[FF] Release Date of the LRO = Nov. 16, 2011"]
-[11.12003231048584, 3.6733970642089844, "[FF] Purpose of the ELF = Mitigation of spacecraft charging"]
-[9.273209571838379, 4.887093544006348, "[TT] True Anomaly of the Activity Attitude = 0\u00ba"]
-[10.089984893798828, -1.588179111480713, "[TT] Inclination of the H-IIA Launch Vehicle = 98.6\u00ba"]
-[9.25724983215332, 1.8361153602600098, "[TT] Locking Mechanism of the Harpoon = Flip-out"]
-[8.425227165222168, 7.424236297607422, "[TT] Analog Outputs of the CMOSIS CHR70M Image Sensor = 8"]
-[7.687470436096191, 4.845294952392578, "[TT] Launch Year of the MicroWave Humidity Sounder-2 = 2013"]
-[7.852678298950195, 6.224931716918945, "[FF] Image Capture Method of the NAC = One line at a time"]
-[11.864147186279297, 6.634815216064453, "[TT] Kinetic Energy of Atomic Hydrogen of the Mass Spectrometer = 0.3 eV"]
-[7.087121486663818, 2.376404047012329, "[FF] URL of the Observation of the Earth and Its Environment: Survey of Missions and Sensors = http://link.springer.com/article/10.1007/s12273-015-0241-8"]
-[8.658218383789062, 4.725501537322998, "[FF] Type of the Star Tracker = Unknown"]
-[5.703500270843506, 2.0528690814971924, "[FF] Mission Phases of the Satellite = Commissioning phase, Science phase"]
-[6.671853542327881, -0.5053422451019287, "[TT] Table Switch Time of the Inter-satellite Antenna = 8 hours"]
-[8.068811416625977, -1.2724392414093018, "[TT] Laser Pulses of the ICESat-2 = 10,000 per second"]
-[12.642772674560547, 4.9120097160339355, "[TT] Dimensions of the Solar Paddle = 3 x 13 m"]
-[9.868415832519531, 2.903557538986206, "[TT] Flight Selection of the TechEdSat-8 = NASA's CubeSat Launch Initiative (CSLI)"]
-[6.1990132331848145, 2.981550931930542, "[TT] Signal-to-Noise Ratio of the WorldView Legion sensor = High"]
-[4.70198392868042, 8.089414596557617, "[TT] Frequency of the SASS = 14.599 GHz"]
-[9.727964401245117, -0.5164387822151184, "[TT] Orbit Altitude of the ADEOS-II = 802.9 km"]
-[8.150089263916016, -0.6650999188423157, "[TT] Arctic Sea-Ice Measurement Accuracy of the CryoSat = 1.6 cm/year"]
-[10.17002010345459, 1.508937120437622, "[FF] Quantity of the Intergalactic Medium Detector = 50-100 thousand galaxy clusters and groups"]
-[5.027698993682861, 2.709371566772461, "[FF] Program Location of the GOES-R = Goddard Space Flight Center (GSFC), Greenbelt, MD"]
-[4.6273512840271, 6.303083419799805, "[FF] Communication Direction of the APAA = Flexible and rapid"]
-[4.9553351402282715, 0.7005879282951355, "[TT] Update Date of the CSDA = January 28, 2022"]
-[10.620140075683594, 5.6671857833862305, "[TT] Heat Shield Maximum Temperature of the Orion = 2750\u00baC"]
-[6.909317970275879, 5.302546501159668, "[FF] Components of the Group Delay = Data generator, modulator, up converter, travelling-wave tube amplifier (TWTA), cable, and integration components"]
-[8.201519012451172, 7.149383544921875, "[TT] Onset of Latchup of the CMOS Sensors = Occurs at LET values typically 16 MeV cm-2/mg and higher"]
-[4.8384246826171875, 0.8918245434761047, "[FF] Launch Date of the PROBA-V = Before July 2013"]
-[5.7384161949157715, 4.6784796714782715, "[FF] Technology Objectives of the ExoMars = Qualification of Russian ground-based means for deep-space communications in cooperation with ESA\u2019s ESTRACK, Adaptation of Russian on-board computer for deep space missions and ExoMars landed operations, Development and qualification of throttleable braking engines for prospective planetary landing missions"]
-[5.104470252990723, 4.371986389160156, "[TT] Number of Satellites Launched of the Starlink = 60"]
-[5.601261138916016, -0.3008488416671753, "[TT] Loss of Communication of the AeroCube-3 = After 205 days on orbit"]
-[7.602413177490234, 2.2749314308166504, "[TT] Radiance Range Coverage of the DNB = More than 500:1"]
-[5.734468460083008, 0.5928013920783997, "[FF] Bulletin Date of the GEOS-1 = May 1977"]
-[3.563819169998169, 4.674162864685059, "[FF] Instrument of the Sentinel-1 = Imaging microwave radar"]
-[7.896428108215332, 7.935528755187988, "[FF] Color Composition of the False-color image = Shortwave infrared, near-infrared, and green light in the red, green, and blue channels of an RGB picture"]
-[5.829190731048584, 3.2032859325408936, "[TT] Development Cost of the FORUM = \u20ac160 million"]
-[8.384868621826172, 3.559427261352539, "[FF] Density Variation of the Atomic Oxygen = Over an order of magnitude"]
-[7.830001354217529, 1.2327595949172974, "[TT] Peak Timing of the Australian Wildfires = January"]
-[10.548482894897461, 1.9852875471115112, "[FF] Emission Types of the Pulsars = Radio, other types of radiation, thermal radiation, non-thermal radiation"]
-[9.528675079345703, 8.198884010314941, "[TT] IFOV of the Sensor Unit = 25 pixels of 1\u00ba x 1\u00ba = 5\u00ba x 5\u00ba"]
-[4.56498908996582, 7.97528600692749, "[TT] Frequency Band of the SWOT = 8.025-8.400 GHz"]
-[11.249303817749023, 1.0057384967803955, "[TT] Maneuver of the LISA Pathfinder = Keep test masses away from the housing walls"]
-[5.7304463386535645, 0.9417988061904907, "[FF] Observation Date of the HSRL-2 = TCAP 2012"]
-[9.679978370666504, -0.36958634853363037, "[TT] Altitude of the AMO = 380 km"]
-[8.33767032623291, 7.688594818115234, "[TT] Detector Type of the SPIRIT-III = Arsenic-doped silicon, blocked impurity-band conductor detectors"]
-[8.29928207397461, 1.4733009338378906, "[TT] Sea Surface Salinity Accuracy Goal of the SMOS = 0.1 psu"]
-[8.25497055053711, -0.701691746711731, "[TT] Ice Edge and Snow Edge Accuracy of the Lower atmosphere = \u00b1 3 cm, \u00b1 2.5 K"]
-[7.013702392578125, 0.9061240553855896, "[FF] Conference Presentation Date of the Triple Probe System = Sept. 19-22, 2005"]
-[3.125211477279663, 2.235372543334961, "[FF] Purpose of the Copernicus Sentinel-6 Michael Freilich = Provide accurate measurements of sea-level change"]
-[10.09650993347168, 4.419379234313965, "[FF] Actuation of the FDV = Opened using its torquing mechanism"]
-[5.612817764282227, 5.614521026611328, "[TT] Processor of the NANOhpm of SkyLabs = PicoSkyFT"]
-[9.979484558105469, 7.153686046600342, "[TT] Angular Resolution of the ART-XC = HPD~ 30\u201d on-axis at 8 keV"]
-[4.326377868652344, 0.9528335332870483, "[FF] Launch Date of the HYLAS-2 = August 2, 2012"]
-[5.851259708404541, -1.0651427507400513, "[TT] Exceeded Design Life of the EO-1 = Yes"]
-[5.92272424697876, 3.1877927780151367, "[FF] Coordination of the Commercial Partners = Required"]
-[3.107408046722412, 1.7834187746047974, "[TT] Tandem Flight Duration of the Copernicus Sentinel-6 Poseidon-4 = 12 months"]
-[4.856112003326416, 2.9138684272766113, "[TT] Location of the Mission Operations = POCC (Project Operations Control Center) at JPL, Pasadena, CA"]
-[9.38838005065918, 7.014614105224609, "[TT] Spatial Resolution of the MSU-E = 28 x 28 m"]
-[4.395162582397461, 3.070643186569214, "[TT] Ground Stations of the GimmeRF = Puerto Rico, Florida, Texas, California, Hawaii, and Guam"]
-[5.288613319396973, 2.4692702293395996, "[TT] Operations of the SwissCube = Shared with the Swiss Radio Amateurs association"]
-[4.986616611480713, 8.269876480102539, "[TT] Spectrum Observation of the CubeRRT = 1 GHz wide portion of the electromagnetic spectrum"]
-[8.497732162475586, 8.215681076049805, "[TT] Spectral Resolution of the Instrument = 2.5 cm -1"]
-[6.8952717781066895, 6.889063358306885, "[FF] Beam Splitting of the DOE (Diffractive Optic Element) = Split the single transmit beam into 6 beams"]
-[6.6689252853393555, 1.8093578815460205, "[FF] URL of the Glory = http://glory.gsfc.nasa.gov/launch.html"]
-[7.771163463592529, 3.992255210876465, "[TT] Phase of the SPARCS = Phase B"]
-[8.17273998260498, 4.579039096832275, "[TT] Total Ionized Dose Radiation of the TacSat-4 = 100 MRad"]
-[4.343874454498291, 2.94648814201355, "[FF] Locations of the CGS = Matera (Italy), Maspalomas (Spain), Svalbard (Norway), Alaska (USA)"]
-[4.718295097351074, 3.2120306491851807, "[TT] Manufacturer of the Remote Interface Unit (RIU) = Thales Alenia Space in Spain"]
-[12.00899887084961, 4.748322486877441, "[TT] Dimensions of the ADEOS-II = 6 x 4 x 4 m"]
-[5.895452499389648, 7.603020668029785, "[TT] Pulse Repetition Frequency of the RA-1 = 1020 Hz"]
-[6.044706344604492, 0.8733147382736206, "[FF] Image Capture Date of the ABI (Advanced Baseline Imager) = January 15"]
-[6.151636600494385, -0.26222842931747437, "[TT] Testing Duration of the AMCS = Several weeks"]
-[9.474430084228516, 4.080482482910156, "[TT] Dynamic Range of the Electric Field Measurement System = 80 dB"]
-[4.974453926086426, 1.6729295253753662, "[FF] URL of the Gokturk-2 = http://blog.gezgin.gov.tr/?p=1898"]
-[7.372467517852783, 4.499250888824463, "[FF] Unknown of the OPTOS = Unknown"]
-[4.068853378295898, 2.190166473388672, "[TT] Launch Site of the SES-17 = Launch Complex ELA-3 in Kourou"]
-[7.081998825073242, 7.243595600128174, "[FF] Wavelength of the Lasers = Shorter wavelengths"]
-[13.56276798248291, 5.885359764099121, "[TT] Solar Array Power of the MTM = 13 kW"]
-[5.886468887329102, 1.8312815427780151, "[FF] URL of the COMS = http://cimss.ssec.wisc.edu/cimss25th/presentations/chung.pdf"]
-[3.8870832920074463, 2.0190489292144775, "[FF] Launch Vehicle of the KANOPUS-V-IK = Soyuz-2.1a"]
-[7.909377574920654, 6.136166095733643, "[TT] Instrument type of the SMMR = Imaging multi-spectral radiometers (vis/IR)"]
-[5.107776165008545, 0.09103146940469742, "[TT] Launch Date of the AeroCube-11/TOMSat = 16 December 2018"]
-[8.011809349060059, 0.467794805765152, "[FF] Weight Measurement of the GRACE-FO = Midwestern Floods"]
-[8.731588363647461, 0.15925265848636627, "[TT] Distance from Comet Center of the NAVCAM = 9.9 km"]
-[7.645267486572266, 8.719265937805176, "[TT] Measurement Bands of the Instrument Package = 4 bands in the UV and visible range"]
-[5.336880207061768, 4.606423854827881, "[TT] OBR of the Payload = Special Operations, one unit only (emergency use)"]
-[4.437961578369141, 7.744706630706787, "[FF] Frequency Bands of the DCS = UHF (401.9 MHz), S-band (1694.5 MHz), S-band (2034.9 MHz), UHF (468.8 MHz)"]
-[9.904014587402344, 8.145367622375488, "[TT] Focal Length of the MSU-50 = 50 mm"]
-[6.025655269622803, 0.9952576160430908, "[TT] Image Capture Date of the WorldView-3 = 18 December 2021"]
-[5.039405822753906, 0.5408919453620911, "[TT] Integration Date of the Capella Space = 2022"]
-[4.767973899841309, 7.84563684463501, "[TT] Frequency 2 of the Onboard Receiver = 401.25 MHz"]
-[8.72148609161377, 3.88801646232605, "[TT] Measurement of the ICARE = Electron, proton and ion fluxes"]
-[13.287100791931152, 5.504489421844482, "[FF] Features of the SAP (Solar Array Paddle subsystem) = Reduced number of units, compact size, light weight and low cost"]
-[7.648007392883301, 8.667096138000488, "[TT] Spectral Bands of the ECOSTRESS = Five"]
-[8.00646686553955, -2.420623302459717, "[TT] Observation Range of the GOLD = About 50 to 400 miles in altitude"]
-[6.849925994873047, 7.432088375091553, "[TT] Beam width of the Sub-mm = 4.5 mrad"]
-[10.027738571166992, 4.198273181915283, "[FF] Function of the Magnetorquer = Liberation damping in the event that the gravity gradient boom deployment erroneously causes the patch antennas to settle in zenith pointing attitude"]
-[8.355701446533203, -0.6328690648078918, "[TT] Dimensions of the Iceberg B-22A = 71 km by 45 km"]
-[4.48451042175293, 3.206153392791748, "[TT] Location of the DRS = Shadnagar, Hyderabad"]
-[11.570594787597656, 4.868316173553467, "[TT] Side Length of the ESTCube-1 & -2 = 10 cm"]
-[6.457333564758301, 1.762758731842041, "[FF] In-Orbit Calibration Plan Presentation of the Microscope = Sept. 23-27, 2013"]
-[9.578381538391113, 7.686886310577393, "[TT] Swath Width of the Multispectral Camera = 95 km"]
-[11.712912559509277, 3.37042236328125, "[TT] Engine Type of the IES = Xe microwave discharge ion engine system"]
-[6.388242244720459, 3.550036668777466, "[FF] Evaluation of the GPM/DPR = Can be evaluated using ground validation observation network in Okinawa"]
-[9.648122787475586, 4.263978481292725, "[FF] Components of the CDRA = Two beds known as a Desiccant/Adsorbent Bed Orbital Replacement Unit"]
-[14.309781074523926, 3.051116943359375, "[TT] S/C Mass of the JL-1-GF03B = <45 kg"]
-[3.7934317588806152, 2.4564528465270996, "[TT] Alternate Launch Service Provider of the Iridium Next = SpaceX"]
-[9.569817543029785, 9.137073516845703, "[TT] Iris of the BIRCHES = Adjustable 4-sided"]
-[3.89349102973938, -2.1553759574890137, "[FF] Pros of the Specialized Asset Tracking = Gather lots of data for a specific asset"]
-[12.106669425964355, 6.345889568328857, "[TT] Positron Fraction Measurement of the AMS-02 = Up to 500 GeV"]
-[8.220881462097168, 7.981420993804932, "[TT] Number of Pins of the SWIR Detector = 72"]
-[13.364116668701172, 7.792984485626221, "[TT] Technology of the LRO Mini-RF Transmitter = MPM (Microwave Power Module)"]
-[5.004366874694824, 4.663743019104004, "[FF] Scientific Objective of the QUESS satellite = Provide insight into the strangest phenomenon in quantum physics \u2014 quantum entanglement"]
-[7.791116237640381, 4.735393047332764, "[FF] Absolute Calibration of the NOAA/AVHRR-2 = IR yes (10 bit), VIS no (pre-launch, drifts)"]
-[6.386725902557373, 4.034578323364258, "[FF] Responsibilities of the ITF = Instrument builds and tests, building a repository of engineering information"]
-[10.607091903686523, 7.325074672698975, "[TT] Swath Width of the Instrument = 2250 km"]
-[13.339973449707031, 6.922112941741943, "[TT] Payload Power Consumption of the Kondor-E = 240-1500 W"]
-[8.089112281799316, -1.1411939859390259, "[FF] Purpose of the Laser Altimeters = Measure ice height"]
-[14.115436553955078, 3.3549818992614746, "[TT] Mass of the CSS = 48 gram"]
-[7.805334091186523, 2.9769606590270996, "[FF] URL of the TanSat = http://earth.esa.int/dragon-2015-programme/liu-monitoring_carbon_dioxide_from_space-220_ppt_present.pdf"]
-[4.680622577667236, 6.947910308837891, "[TT] Downlink Band of the Spacecraft = S-band (variable to 2 Mbit/s)"]
-[6.552696228027344, 0.7555637955665588, "[TT] Service Module Commissioning Start Date of the Herschel = May 15, 2009"]
-[8.39694881439209, 7.220232009887695, "[TT] Photomultiplier Tubes of the RICH = 680 R7600-M16 multianode Hamamatsu PMTs"]
-[4.235513210296631, 7.17481803894043, "[TT] Ground Monitoring Frequency of the EROS-A = S-band"]
-[7.826005458831787, 2.131645441055298, "[FF] Purpose of the COCTS = Ocean color and temperature scanning"]
-[3.5711658000946045, 6.453365325927734, "[TT] Antenna Diameter of the X-band ground station = 3.4 m"]
-[6.635861396789551, 5.304831027984619, "[FF] Components of the MEX = Memories, linear and optoelectronic devices, power MOSFETs"]
-[6.37366247177124, 2.182856559753418, "[FF] URL of the Advanced Communication Technology Satellite (ACTS) = http://www.lr.tudelft.nl/live/pagina.jsp?id=d9741070-a2e1-4499-a9f8-d4fdca22d2e3&lang=en"]
-[6.497827529907227, 4.818213939666748, "[FF] Function of the RBU = Provide backup facility"]
-[4.985384941101074, 2.4441232681274414, "[TT] Executive Chairman of the Viasat = Mark Dankberg"]
-[4.618990898132324, 7.1842427253723145, "[FF] Operational Scenario of the QWIP Experiment = Turned on every few days to collect and transfer data to the S/C for downlink transmission"]
-[3.7961585521698, 1.157092809677124, "[TT] Height of the Falcon 9 first stage = 42 m"]
-[3.1049282550811768, 2.1251437664031982, "[FF] Vice-President of the Copernicus = Antonio Tajani"]
-[4.462333679199219, 3.7036499977111816, "[TT] Ground Segment Control Centers of the Galileo = Italy and Germany"]
-[5.198034763336182, 1.7298097610473633, "[TT] Operation Status of the ALOS-2 = Nominal"]
-[14.209417343139648, 3.226966381072998, "[TT] Mass of the COPPER = 1.3 kg"]
-[6.200891971588135, 1.4618600606918335, "[FF] Mission Date of the eROSITA = June 24, 2020"]
-[8.461176872253418, 5.771488666534424, "[TT] Test Cycles of the RTV Adhesive = 15 cycles"]
-[6.174593925476074, 2.2205042839050293, "[TT] Lead Scientist of the GPM = George Huffman"]
-[9.13547134399414, 7.228762626647949, "[TT] Resolution of the Deimos-2 = 75 cm per pixel"]
-[5.488432884216309, 0.06842459738254547, "[TT] Reporting Frequency of the Paris Agreement = Every five years beginning in 2023"]
-[3.9165754318237305, 9.743184089660645, "[TT] Bandwidth (GHz) of the ICI-4 = 6"]
-[5.781219482421875, 4.972019672393799, "[FF] Data Relay System of the Alphasat and Sentinel-1A = LCTs"]
-[3.1892364025115967, 2.450103998184204, "[FF] Radiometric Image Quality of the Sentinel-2 = Very good"]
-[5.961045265197754, 8.721879959106445, "[TT] MTF of the Instrument = About 20% at Nyquist frequency"]
-[6.442836284637451, -0.25704866647720337, "[TT] Average Period Between In-Plane Orbit Manoeuvres of the ALOS-2 = 4.9 days"]
-[8.729153633117676, 4.747784614562988, "[FF] Robustness of the Star Tracker = Better robustness to Moon-blinding and to temperature constraints"]
-[10.994449615478516, 6.221445560455322, "[TT] Mirror Material of the PAN Camera = Zerodur glass"]
-[8.13152027130127, 0.766827404499054, "[TT] Storage Rate of the Istanbul Reservoirs = Just below 25 percent"]
-[6.1251702308654785, 7.056666851043701, "[TT] Data Compression of the Instrument = DPCM (Differential Pulse Code Modulation) method"]
-[4.501865386962891, 7.633662223815918, "[TT] Gain on transmit of the Uplink (VHF) = 16.15 dB"]
-[4.916162490844727, -2.127124071121216, "[TT] Orbiter Weight of the Chang\u2019e-5 = Nearly 2,000 kg"]
-[13.77380657196045, 5.374309062957764, "[TT] Composition of the Solar Array = GaAs/InGaP/Ge multi-junction solar cells"]
-[12.458024978637695, 0.6510772705078125, "[TT] Aperture of the Plato Camera = 12 cm"]
-[9.587027549743652, 1.4592491388320923, "[TT] Data Access of the Pl\u00e9iades Neo constellation = Immediate"]
-[8.766297340393066, 5.760098934173584, "[TT] Location Accuracy of the SPOT-6 = 19.3 m CE90 @30\u00ba"]
-[5.076170444488525, 0.7586351633071899, "[TT] Launch Date of the DMC-3 Constellation = July 10, 2015"]
-[7.018290042877197, 4.276666164398193, "[FF] Habitable Zone of the L 98-59b = None"]
-[9.300692558288574, 3.1634628772735596, "[FF] Function of the Solar Wind Concentrator = Make possible oxygen and nitrogen measurements"]
-[8.176340103149414, 7.100828647613525, "[FF] Sensor Complement of the HJ-1B = Wide View CCD Cameras (WVC), Infrared Multispectral Scanner (IRMSS)"]
-[7.088871955871582, 7.085976600646973, "[TT] Heat Dissipation of the Power Laser Head = ~150 W"]
-[4.451934814453125, 3.15310001373291, "[TT] Location of the IMGEOS = NRSC (National Remote Sensing Center), Shadnagar, Hyderabad Complex"]
-[9.406394958496094, 2.314854383468628, "[FF] Gigantic Jets of the ISUAL = 0.30%"]
-[5.826886177062988, 4.425321578979492, "[TT] Platform of the SDDS/E = Eclipse-based embedded software integrated development environment"]
-[6.75481653213501, 2.0123164653778076, "[TT] Number of Images Collected of the Landsat-9 = More than 57,000"]
-[14.074661254882812, 3.461977958679199, "[TT] Mass of the Kestrel Eye-2M = ~50 kg"]
-[8.071907997131348, 5.464468955993652, "[FF] Objective of the Photometers and Radiometers = Measure changes in optical transmission, thermal absorption and emission"]
-[8.021570205688477, 8.856021881103516, "[TT] Wavelength Range of the SORCE = 1 to 2400 nanometers"]
-[6.86794376373291, 2.845288038253784, "[FF] Focus of the RECCAP-2 = Regional GHG budgets"]
-[9.123003959655762, -1.1800282001495361, "[TT] Orbit of the INSAT-3D = Geostationary"]
-[7.02090311050415, 0.1294582039117813, "[TT] Deposition Time of the Fortescue, Hamersley, and Turee groups = Between 2.7 billion and 2.3 billion years ago"]
-[8.185564041137695, -0.623963475227356, "[TT] Sector Ice Discharge Increase of the Austfonna = 45-fold"]
-[8.433951377868652, 7.740675926208496, "[TT] Detector Arrays Bands of the FTS = 200-325 \u00b5m and 315-670 \u00b5m"]
-[8.340709686279297, 7.237063407897949, "[TT] Imaging Modes of the Imager = Panchromatic (Pan), Multispectral (MS)"]
-[4.3835129737854, 5.426774978637695, "[TT] Launch Date of the GOMX-3 = August 19, 2015"]
-[14.185497283935547, 3.1547505855560303, "[TT] Mass of the LEICA = 7.4 kg"]
-[9.156061172485352, 2.805079221725464, "[FF] Flare Class of the Solar Dynamics Observatory = X1-class"]
-[9.515945434570312, 9.068354606628418, "[FF] Capability of the Iris 2.1 = High data throughput and Doppler ranging capabilities"]
-[6.298020362854004, 3.7300970554351807, "[TT] Management of the DMSP Block-5D = Air Force"]
-[8.84952163696289, 9.412009239196777, "[TT] Spectral Band 4 Spatial Resolution of the TANSO-CAI = 1.5 km"]
-[10.125855445861816, 3.216671943664551, "[FF] Platform of the CubeSats = Ion/neutral mass spectrometer"]
-[8.934266090393066, 7.399875640869141, "[TT] Margin for Smear of the BAE Detector = 473%"]
-[7.231601238250732, 1.7096025943756104, "[FF] Objective of the Sensor Complement = Investigate how variations in gravity affect calcium signaling in germinating spores of the fern Ceratopteris richardii"]
-[4.899663925170898, 0.8457988500595093, "[TT] Fourth Flight Date of the MEPSI = July 4-17, 2006"]
-[1.7629802227020264, -2.0604751110076904, "[FF] URL of the Hayabusa-2 = https://iafastro.directory/iac/proceedings/IAC-19/IAC-19/A3/4A/manuscripts/IAC-19,A3,4A,2,x52566.pdf"]
-[6.193823337554932, 2.8516056537628174, "[FF] Developer of the SEDS = NASA/MSFC and Tether Applications Co. of San Diego"]
-[6.451046943664551, 0.6318460702896118, "[FF] Launch Delay of the Landsat-9 = Liquid nitrogen shortage"]
-[7.222949981689453, 1.0209875106811523, "[FF] Mission of the Beresheet = Journey to the moon"]
-[10.211992263793945, 5.485438823699951, "[FF] Attenuator Control of the BSC = Compensate for gain variations due to temperature inputs"]
-[4.825337886810303, 0.14862710237503052, "[TT] End of Life Date of the SpaceX CRS-16 = 14 January 2019"]
-[5.778132915496826, 0.7998372912406921, "[FF] Detector Annealing Date of the RHESSI = Jan. 16, 2008"]
-[4.49270486831665, 4.223529815673828, "[FF] Radio Frequency of the GPS and Galileo = Compatible"]
-[3.8856329917907715, 4.242159843444824, "[FF] Emergency Observation Request of the RISAT-1 = EOR (Emergency Observation Request)"]
-[11.135868072509766, 5.255624294281006, "[FF] Objective 1 of the CITRIS = Reconstruct real-time phase screens for multiple frequency scintillation estimation"]
-[6.903810024261475, 2.2763864994049072, "[FF] Workshop Date of the China Earth Observation Satellite Program = Feb. 11-13, 2009"]
-[4.5678558349609375, 0.20373426377773285, "[TT] Launch Date of the AstroSat = 28 September 2015"]
-[11.662200927734375, 4.184407711029053, "[TT] Length of the Meteosat = 3.195 m"]
-[7.311773777008057, 3.0131590366363525, "[FF] Satellite Type of the MethaneSAT = Sensorcraft"]
-[7.1795973777771, 0.0007015718147158623, "[TT] Host Star Age of the WD 1856 b = Up to 10 billion years old"]
-[7.150412082672119, 0.7931811809539795, "[TT] Field of View of the Herschel = Little more than two times the width of the full Moon"]
-[9.065792083740234, 2.671058416366577, "[FF] Date of Event of the Solar Flare = September 6, 2017"]
-[4.794945240020752, 8.221200942993164, "[TT] Frequency Band of the SSM/T-1 = 50 to 60 GHz"]
-[11.374903678894043, 0.7600211501121521, "[FF] Nature Volume of the AU Microscopii = 582"]
-[13.447504997253418, 6.822717666625977, "[TT] Power of the Spacecraft = 2.5 kW (EOL)"]
-[6.164144039154053, 2.9561409950256348, "[TT] Imaging Frequency of the WorldView Legion = Up to 15 times per day"]
-[7.5734357833862305, -2.4960427284240723, "[TT] Data Release Date of the GOLD = December 7, 2019"]
-[3.7175216674804688, 2.4681291580200195, "[FF] URL of the Iridium NEXT = http://multivu.prnewswire.com"]
-[5.516716003417969, 7.014796257019043, "[TT] Data Rate of the SPACE HAUC = Up to 100 Mbit/s"]
-[10.404230117797852, 7.670490741729736, "[TT] Telescope Diameter of the S-192 optomechanical scanner = 30 cm"]
-[13.397496223449707, 7.2621026039123535, "[TT] Power of the ADCS = 0.66 W"]
-[8.94757080078125, 7.097790241241455, "[FF] Camera Resolution of the Chang'e-2 = Higher resolution camera compared to Chang'e-1"]
-[11.755375862121582, 6.627200126647949, "[TT] Proton Energy Range of the LDT = Above ~75 MeV"]
-[3.4309372901916504, -0.9287568926811218, "[TT] Orbit Type of the BUV = Sun-synchronous near-circular polar orbit"]
-[5.692973613739014, 4.447620868682861, "[FF] Service Provider of the EDRS = Satellite Operator"]
-[4.639039039611816, 0.5707118511199951, "[TT] Launch Date of the QBITO = 18 April 2017"]
-[6.798910140991211, 6.361483097076416, "[TT] Number of Positions of the FWA = 6"]
-[10.123122215270996, -1.5406975746154785, "[TT] Inclination of the MetOp-B satellite = 98.7\u00b0"]
-[8.261984825134277, 4.669321537017822, "[FF] Components of the Instrument Carrier = IOA, WFI, CGI, and the Spacecraft\u2019s Star Tracker/Inertial Reference Unit"]
-[10.588031768798828, 6.477298259735107, "[TT] Mirror Assemblies of the eROSITA = 8"]
-[7.800577640533447, 8.860587120056152, "[TT] Spectral Range of the O2 A-band channel = 0.758 to 0.772 \u00b5m"]
-[13.365400314331055, 7.768431663513184, "[TT] Transmitter Power of the UHF Radio System = 30 dBm (1 W)"]
-[9.25560188293457, 5.628063201904297, "[FF] Unit of Measure of the ASTERIA = Arcseconds"]
-[4.812038898468018, 7.398248672485352, "[TT] Downlink Data Rate of the UHF Radio System = 4 kbit/s"]
-[6.612903118133545, 4.603710651397705, "[FF] Status of the IPU = Unsuccessful"]
-[10.785921096801758, 1.4489169120788574, "[TT] Black Hole Mass of the PG211+143 = 40 million solar masses"]
-[5.965519905090332, 1.5225507020950317, "[FF] Conference Date of the Joint Polar Satellite System = June 11-15, 2012"]
-[5.472171783447266, 5.258881568908691, "[TT] Operating System of the UWE-1 = \u00b5CLinux"]
-[5.739725589752197, 5.397244453430176, "[FF] Components of the XSAR = RSC (Radar Signaling and Control) system, MTT (Multi-Tube Transmitter), Deployable paraboloid mesh antenna with electronic beam steering, OBR (Onboard Recorder) of 256 Gbit capacity, DLTU (Data-Link Transmission Unit)"]
-[9.144338607788086, 3.421497344970703, "[FF] Relationship with Plasma Density of the Plasma Drifts = Requires components of drift parallel and perpendicular to the magnetic field to be considered, as well as season, and location with respect to the magnetic equator"]
-[10.39157772064209, 7.941530704498291, "[TT] Structure Dimensions of the OrbView-4 = 102 cm in diameter and 152 cm in length"]
-[5.458805561065674, 3.005708694458008, "[TT] Developer of the SRC = Lockheed Martin Astronautics"]
-[9.630367279052734, 8.113003730773926, "[FF] Application of the Scanning Shack Hartmann Sensor = Measurement of the human eye"]
-[4.635502815246582, 2.9911258220672607, "[TT] Operation Center Location of the Cheops = Torrej\u00f3n, near Madrid, Spain"]
-[9.95466136932373, 6.338936805725098, "[TT] Detector Energy Resolution of the D-CIXS = > 200 eV"]
-[4.384920597076416, 2.0609517097473145, "[TT] Commissioning Completion Date of the DubaiSat-2 = April 14, 2014"]
-[13.738846778869629, 2.7235865592956543, "[TT] Mass of the SA-200HP = Launch mass of 2780 kg; dry mass of 1512 kg"]
-[3.8806002140045166, 3.4422242641448975, "[FF] Announcement Date of the Galileo Second Generation = 27 May 2021"]
-[4.780426979064941, 2.870325803756714, "[FF] Control Node Locations of the GeneSat-1 = Multi-Mission Operations Center (MMOC) at NASA/ARC, SCU Robotic Control Center located in the NASA Research Park in Moffett Field, GeneSat-1 operations development and training laboratory on the SCU campus, SRI communication station"]
-[8.2064790725708, 6.996664524078369, "[TT] Number of Subapertures of the Direct Imaging System = 8"]
-[3.2579100131988525, 5.069721221923828, "[TT] SAR Payload Spatial Resolution of the RCM = 5 - 50 m"]
-[5.379253387451172, 2.661754846572876, "[FF] Collaborating Institution of the MAST = Stanford University's SSDL"]
-[8.79482650756836, 2.3644793033599854, "[FF] Function of the GIADA = Grain Impact Analyser and Dust Accumulator"]
-[11.347161293029785, 2.786604404449463, "[TT] Mass of the Microsatellite = ~ 10 kg"]
-[6.499335289001465, 3.1820077896118164, "[FF] Conference Presentation of the UK Disaster Monitoring Constellation Satellite = ION 2003"]
-[4.226633071899414, 2.584477424621582, "[TT] Launch Site of the TESS = Cape Canaveral Air Force Station in Florida, SLC-40"]
-[9.083070755004883, 3.31833553314209, "[TT] Glare Impact of the ISS-LIS = Will not impact ISS-LIS"]
-[8.488785743713379, 7.66275691986084, "[TT] Array Size of the CCID-80 = 2048 (H) x 2048 (V)"]
-[5.959839344024658, 1.5412354469299316, "[TT] Solar Array Status of the IXPE observatory = Not delivered"]
-[6.226586818695068, 3.8663814067840576, "[FF] Operation of the DMC Constellation = Can act as a single coordinated instrument if required"]
-[8.057965278625488, 8.185896873474121, "[TT] Type of the MWIR Sensor = Miniature high temperature Mid-Wave Infra-Red (MWIR)"]
-[10.960638046264648, 2.0729966163635254, "[FF] Collaboration Date of the NuSTAR and XMM-Newton = Feb. 27, 2013"]
-[7.870623588562012, 6.995248794555664, "[FF] Unapodized Spectral Resolution Requirement of the Michelson Interferometer = I/(2L)"]
-[6.254809379577637, 8.50590705871582, "[TT] Mode of the Polarization diversity mode = Auto track and ranging functions"]
-[3.2298378944396973, 5.114704132080078, "[TT] Spotlight (SL) Image Size of the TSX-SAR = 10km x 10km"]
-[11.54118824005127, 6.465449810028076, "[TT] Energy Range of the NuSTAR = 68 to 78 keV"]
-[13.369229316711426, 7.38378381729126, "[TT] Power of the TxU = 26 W"]
-[13.347579956054688, 7.118321418762207, "[TT] Power Dissipation of the IEC = 200 W"]
-[7.0487494468688965, 1.8901973962783813, "[FF] Data Improvement of the Las Cumbres Observatory = Improve scientists\u2019 confidence in the orbital period and size of TOI 700 c by 30% and 36%"]
-[7.045045375823975, 7.099431991577148, "[TT] Output Energy of the Laser Transmitter = More than 35 mJ at 355 nm"]
-[9.840152740478516, 4.759261131286621, "[TT] Rotation Speed of the Spin-Stabilized Spacecraft = 20 rpm"]
-[12.052412033081055, 4.722630500793457, "[TT] Envelope Dimensions of the BIT-3 flight system = 180 x 88 x 102 mm"]
-[8.429823875427246, 6.333355903625488, "[TT] Relative Brightness Evaluation of the ASTER = 5% uncertainty"]
-[9.544694900512695, 0.6312428712844849, "[TT] Thruster Firing Duration of the Schiaparelli module = 3 sec"]
-[9.441141128540039, 6.250833988189697, "[TT] Observation Direction Angles of the TANSO-CAI-2 = Forward- (+20\u00ba) and backward-looking (-20\u00ba)"]
-[11.206117630004883, 5.683032035827637, "[TT] Thickness of the pnCCD Chip = 450 \u00b5m"]
-[4.574170112609863, 7.849577903747559, "[TT] Radio Frequency of the Reception Station = 7.8 GHz"]
-[7.944253444671631, 7.25872278213501, "[TT] Time Resolution of the Detector = 1 ms"]
-[9.62272834777832, 4.830135822296143, "[TT] Stabilization of the ROSE-L = 3 axis"]
-[6.436737060546875, -0.4736926555633545, "[TT] Nadir Orientation Duration of the PSSCT-2 = 4 hours"]
-[11.130589485168457, 3.3566226959228516, "[FF] Type of the Micro Systems Technology = In-Orbit"]
-[9.164895057678223, 3.0699920654296875, "[FF] Primary Science Objectives of the Solar-A / Yohkoh = 1) to further the understanding of the magnetofluid dynamics of the repeated expansion of the solar corona, 2) clarification of the changes in the shape of the solar corona, and 3) the study of the mechanism underlying the occurrence of plasma disturbance phenomena in interplanetary space"]
-[11.851720809936523, 2.906773090362549, "[TT] Hydrazine Thrusters Isp of the PARASOL microsatellite = 210 s"]
-[6.701821804046631, 7.373236656188965, "[TT] ADC of the DACS = 8 I+8Q @ 20.8 - 250 MHz sampling rate"]
-[10.6466064453125, 3.3946213722229004, "[TT] Platform Space of the ITASat CubeSat = 4U"]
-[8.914422988891602, 5.270397186279297, "[FF] Fine-Pointing Capability of the ATLAS-1 = Limited"]
-[6.193058967590332, 2.7491865158081055, "[FF] Stack Components of the Orion CSM = Conical CM (Crew Module), and a cylindrical SM (Service Module)"]
-[8.417012214660645, 1.734169363975525, "[TT] Spatial Resolution (km) of the Cloud water = 25"]
-[13.88886547088623, 3.7409987449645996, "[TT] Instrument Mass of the Telescope = 88 kg"]
-[8.419012069702148, 3.9868476390838623, "[TT] Operation of the MERIS = Only out of eclipse and when the sun's zenith angle at the subsatellite point is less than 80\u00ba"]
-[5.611579418182373, 5.8633270263671875, "[TT] Microcontroller Unit of the On-board data handling = 100 MHz 8051 MCU"]
-[4.567645072937012, 7.023260593414307, "[TT] Data Path of the Antenna System = Primary path for L1b data from WCDAS to NSOF"]
-[5.100593090057373, 2.2285261154174805, "[TT] Operational Status of the PhoneSat 2.5 = Operational"]
-[8.266069412231445, 7.494886875152588, "[TT] Detector Type of the Instrument = Uncooled infrared detector"]
-[6.460306167602539, -0.8576683402061462, "[TT] LTAN of the RISAT-1 = 0600 and 1800 hours"]
-[5.682590007781982, 5.634830951690674, "[FF] Type of the BOC 1.1 = Binary Offset Carrier 1.1"]
-[10.161149978637695, 1.9331727027893066, "[TT] Sky Scanning Interval of the eROSITA = 6 months"]
-[13.509315490722656, 6.1729278564453125, "[TT] Solar Panel Power of the DubaiSat-2 = More than 450 W"]
-[7.898769378662109, 8.320159912109375, "[FF] Minimum Value of the Spectral Angle = Achieved when the yellow-gold reflection of the satellite bus is prominent"]
-[1.7280410528182983, 6.149626731872559, "[FF] Composition of the Dark Matter = Unknown"]
-[4.592949390411377, 7.876794338226318, "[TT] Frequency of the UHF Band = 436.675 MHz"]
-[4.548426628112793, 5.884164810180664, "[FF] Operational Characteristics of the 406 MHz units = High peak power output and a low duty cycle, Improved radio frequency stability, A unique identification code in each beacon, Digital transmissions that could be stored in a satellite's memory"]
-[5.746967792510986, 3.3456685543060303, "[TT] Number of Satellites of the WorldView-Legion = 6"]
-[7.840695381164551, 4.914531707763672, "[TT] Number of Locations of the radFET dosimeters = 3"]
-[12.14599609375, -0.09907515347003937, "[TT] Number of Cameras of the TESS = 4"]
-[6.602325916290283, 4.132632732391357, "[FF] Status of the Ground Segment = Unknown"]
-[8.724098205566406, 6.3483476638793945, "[TT] DEM/DSM Accuracy of the HRS = 5 m (relative) and 10/15 m (absolute)"]
-[8.626537322998047, 1.7986500263214111, "[TT] Intensification of the Hurricane Eta = Stalled and rapidly intensified"]
-[7.452747821807861, 5.994572639465332, "[FF] Inter-beam Biases of the MWR = Negligible"]
-[14.608381271362305, 6.609273433685303, "[TT] Battery of the Spacecraft = 78 AH Li-ion battery"]
-[11.592903137207031, 3.450732469558716, "[FF] Electric Propulsion Systems of the SJ-9A = Ion Electric Propulsion, Hall Effect Propulsion"]
-[5.690549373626709, 5.21703577041626, "[TT] Basis of the OBC Software = RTOS (Real Time Operating System)"]
-[11.074274063110352, 5.864684104919434, "[TT] Shielding Efficiency of the MLI Design = 30 dB"]
-[5.734838962554932, 1.139448642730713, "[FF] Launch Date of the Commercial small satellites = Late 2022 or early 2023"]
-[6.607707500457764, 1.2148209810256958, "[FF] Symposium Date of the European Student Earth Orbiter = May 26-30, 2014"]
-[8.135601043701172, 5.169599533081055, "[FF] Observation Method of the Student Observers = Record the precise time of their observations by the use of stopwatches synchronized with international time signals"]
-[8.518976211547852, 5.966272354125977, "[TT] Range Accuracy of the Retroreflector Cube = Few centimetres"]
-[3.8292770385742188, 1.2831000089645386, "[TT] First Stage Landing Site of the Falcon-9 V1.1 = \u201cOf Course I Still Love You\u201d droneship in the Atlantic Ocean"]
-[2.9713590145111084, 2.362199544906616, "[FF] Data Collection of the Copernicus Sentinel-5P = Nitrogen dioxide concentrations"]
-[3.7907426357269287, 3.3520050048828125, "[TT] Launch Date of the Galileo satellites = 12 October 2012"]
-[10.137767791748047, 8.17617416381836, "[TT] Aperture Diameter of the Lenses = 26 cm"]
-[14.250003814697266, 3.1583545207977295, "[TT] Mass of the DeMi = 2.5 kg"]
-[7.576010227203369, 2.347686529159546, "[FF] Purpose of the Microwave and Optical Instruments = Assess if orbital monitoring of plastic might be practical"]
-[3.3624417781829834, 6.443028450012207, "[TT] Antenna Diameter of the RA-1 = 1.2 m"]
-[5.58875846862793, 6.445525646209717, "[TT] Volume of the HSC = ~150-600 MByte"]
-[7.965176582336426, 4.297690391540527, "[TT] Frequency of the LED Light Source Linearity Checks = Weekly"]
-[14.087699890136719, 3.055237293243408, "[TT] Mass of the SporeSat = 5.5 kg"]
-[11.13135051727295, 0.6219003796577454, "[TT] Usage of the W. M. Keck Observatory\u2019s High-Resolution Echelle Spectrometer (HIRES) = Confirm the existence of the three planets"]
-[7.029422283172607, 5.7614264488220215, "[TT] Quantity of the MSU-E = 2"]
-[5.236909866333008, 2.7206597328186035, "[FF] University of the EXCISS = Goethe University in Frankfurt"]
-[11.716592788696289, 4.881236553192139, "[TT] Body Size of the M1S/M2S = 2.0 m x 2.5 m x 3.6 m"]
-[5.370599269866943, 8.783586502075195, "[TT] Bandwidth of the Band 11 = 0.394 \u00b5m (80 cm -1)"]
-[10.079425811767578, 0.9514641165733337, "[TT] Distance from Earth of the Crab Nebula = 6,500 light-years"]
-[8.51591968536377, 7.28043794631958, "[TT] Groups of the Camera = 4 groups of 6 cameras"]
-[9.197686195373535, -0.3975588381290436, "[TT] Phase 1 Apogee Altitudes of the MMS = 12 Re"]
-[7.349684238433838, 0.24472783505916595, "[TT] Sample Delivery Date to Earth of the OSIRIS-REx = September 24, 2023"]
-[8.37946891784668, 7.404163837432861, "[TT] CMOS Image Sensor Type of the Imager = Radiation-hardened"]
-[7.2283806800842285, 0.9433754086494446, "[TT] Imaging Period of the SeaSat = August 16 to October 6, 1978"]
-[8.62605094909668, 6.63875150680542, "[TT] Imagery Geolocation Accuracy with GPCs of the WV60 imager = 2 m"]
-[13.404930114746094, 7.3351359367370605, "[TT] Power of the HEPD = 2.0 W"]
-[8.796148300170898, 6.363644123077393, "[TT] Backscatter Coefficient Measurement Accuracy of the ALT = \u00b1 1.0 dB"]
-[8.269283294677734, 5.183923721313477, "[FF] Function of the Radiometers = Detect changes in thermal control paint coefficients of heat gain / loss based on exposure"]
-[5.187768459320068, 3.2110917568206787, "[TT] Provider of the HW-BOSS = Fraunhofer-Gesellschaft FIRST"]
-[11.276037216186523, 5.585456848144531, "[TT] MLI Thickness of the MPO TCS = 65 mm"]
-[5.399985313415527, 7.061983585357666, "[TT] Data Stream of the 1st generation Tesat LCT = 5.625 Gbit/s"]
-[9.350607872009277, 3.6269237995147705, "[FF] Purpose of the MAG = Measures the magnetic field in the outer magnetosphere of the Earth"]
-[10.285258293151855, 5.39788818359375, "[TT] Distance to M4 of the M3 = 10 \u00b5m"]
-[9.511327743530273, 7.263671875, "[TT] Resolution (Infrared channel) of the OLS = ~3.6 km at nadir"]
-[8.824049949645996, 3.3126778602600098, "[FF] Authors of the Proposed visible emission line space solar coronagraph = Jagdev Singh, B. Raghavendra Prasad, P. Venkatakrishnan, K. Sankarasubramanian, Dipankar Banerjee, Raja Bayanna, Shibu Mathew, Jayant Murthy, Prasad Subramaniam, R. Ramesh, S. Kathiravan, S. Nagabhushana, P. K. Mahesh, P. K. Manoharan, Wahab Uddin, S. Sriram, Amit Kumar, N. Srivastava, Koteswara Rao, C. L. Nagendra, P. Chakraborthy, K. V. Sriram, R. Venkateswaran, T. Krishnamurthy, P. Sreekumar, K. S. Sarma, Raghava Murthy, K. H. Navalgund, D. R. M. Samudraiah, P. Narayan Babu, Asit Patra"]
-[2.328047275543213, 1.3129806518554688, "[FF] Conference Presentation of the NanoSail-D = Aug. 11-14, 2008"]
-[4.309595584869385, 3.1011955738067627, "[TT] Data Reception Station of the Ground Segment = Svalbard (Spitzbergen)"]
-[6.995672225952148, 1.8274810314178467, "[FF] Launch Date of the Orbiting Carbon Observatory-2 = Unknown"]
-[8.426888465881348, 6.898711204528809, "[TT] Imaging Mode of the Pushbroom System = Continuous"]
-[9.237587928771973, 1.8810029029846191, "[FF] Testing Location of the Harpoon = Airbus DS test range"]
-[5.702097415924072, -0.2429898977279663, "[TT] Deployment Timeline of the NRCSD = 1 month after berthing"]
-[5.490200996398926, 6.661252498626709, "[TT] Data Archive Size of the Gaia = 1 PB"]
-[5.73365592956543, 1.1730257272720337, "[FF] Deployment Date of the Pulsar satellites = Early 2025"]
-[4.5303802490234375, 3.25447416305542, "[TT] Ground Station Location of the QBITO = E-USOC"]
-[10.347467422485352, 5.382069110870361, "[TT] Active Control of the TCS = Heaters"]
-[3.5369162559509277, 4.929784297943115, "[FF] Performance of the SAR Mode = Excellent"]
-[8.291354179382324, 2.529757499694824, "[FF] Purpose of the CATS = Aerosol and cloud profiling"]
-[6.3260178565979, -0.43952181935310364, "[TT] Initial Staffing of the LMOC and OGSs = 8 hours per day, 5 days per week"]
-[4.328858375549316, 5.332076549530029, "[TT] Frequency Bands of the COSPAS satellites = 121.5 MHz and 406 MHz"]
-[9.718379020690918, -0.090426966547966, "[TT] Position of the GIOVE-A = More than 1000 km above the GPS constellation"]
-[3.2089695930480957, 4.4031171798706055, "[TT] Latitude Band of the TerraSAR-X and TanDEM-X = \u00b160\u00ba"]
-[7.108067512512207, 6.435257911682129, "[FF] Development and Evaluation of detection algorithm of the GLI = Unknown"]
-[10.268109321594238, 8.00055980682373, "[TT] Diameter of the Telescope = 620 mm"]
-[9.801342964172363, 5.677390098571777, "[TT] Tilt of the M5 = 100 \u00b5rad"]
-[3.0680315494537354, -0.04134317860007286, "[TT] Orbital Slot of the GSAT-0101 = B05"]
-[10.937971115112305, 7.5562262535095215, "[TT] Swath Width of the HORUS = 15 km"]
-[5.166341304779053, 1.91423761844635, "[TT] Status of the HSC = Fully operative"]
-[7.375979900360107, 4.046980381011963, "[TT] Type of the Radio Occultation receiver (TriG-RO) = Radio Occultation receiver"]
-[6.587382793426514, 4.648001194000244, "[FF] Function of the CAPSTONE = Demonstration of spacecraft-to-spacecraft navigation services"]
-[6.0092010498046875, 5.522425651550293, "[FF] Command Types of the DCU = Plain TCs, authenticated and encrypted messages"]
-[7.148248672485352, 5.678329944610596, "[FF] Operation of the HATI = Uses an adaptive nonparametric CFAR detection scheme that does not involve the theoretical modeling of clutter statistics"]
-[5.096076011657715, 6.120048999786377, "[FF] D-STAR Capability of the OUFTI-1 = Provides a repeater functionality to any D-STAR equipped ham-radio operator"]
-[7.955626010894775, 0.8613908886909485, "[FF] Date of the The Drying U.S. West = 14 December 2020"]
-[8.312393188476562, 7.588657379150391, "[TT] Detector Elements of the Instrument = 8000 elements"]
-[8.690536499023438, 5.764523506164551, "[TT] Location Accuracy of the SPOT-6 = 11.9 m CE90 @30\u00ba"]
-[13.991477012634277, 3.0365309715270996, "[FF] Mass of the KUTESat = Unknown"]
-[7.663390636444092, 4.350203037261963, "[FF] Operation Sequence of the Part B2 = Handover from FF to RVX at WP0, Reaching WP1 through a forced motion retreat maneuver, Reaching pre-perigee WP2 by non-drifting hop, Demonstration of perigee passage under Sun illumination until WP3"]
-[11.54533863067627, 3.6819212436676025, "[TT] Number of Firings of the IEPS = 22"]
-[7.931015968322754, 4.194368839263916, "[FF] Purpose of the CHIMERA board = Test susceptibility of commercial computer memories to space radiation"]
-[4.9325432777404785, 1.30785071849823, "[TT] Development and Testing Period of the EDOT = Throughout 2014"]
-[13.966073036193848, 7.203998565673828, "[TT] Current of the Voltage 2 = 10"]
-[4.388023376464844, 3.187889337539673, "[TT] Location of the Redu in Belgium = Redu in Belgium"]
-[7.001595973968506, 7.099201202392578, "[TT] Q-Switched Master Oscillator Output of the Power Laser Head (PLH) = About 8 mJ"]
-[4.3284831047058105, 2.9067416191101074, "[TT] Ground Segment Location of the KazEOSat-2 = Astana, Kazakhstan"]
-[7.563119411468506, 2.0229358673095703, "[FF] Band 1 of the Landsat TM = Coastal water mapping, soil/vegetation differentiation, deciduous/coniferous differentiation, chlorophyll absorption"]
-[4.196713447570801, 7.182426452636719, "[TT] Bands of the High Gain Antenna = Ka-band and S-band"]
-[4.6977996826171875, 0.19452306628227234, "[TT] Launch Date of the IDEA OSG 1 = 2018"]
-[7.964868068695068, 6.343271255493164, "[TT] Type of the VHRR = Imaging multi-spectral radiometers (vis/IR)"]
-[8.972813606262207, 5.770402908325195, "[TT] Electrode Position of the CVX\u20132 Device = 4 mm to each side of the screen"]
-[10.791424751281738, 7.475126266479492, "[TT] Swath of the LISS-4 = 70 km"]
-[8.120906829833984, 8.842707633972168, "[TT] Absorption Wavelength of the Solar Cells = 300 nm to 650 nm"]
-[4.8100481033325195, 5.687751293182373, "[FF] GPS Data Flagging of the Stensat Beacon = Observed"]
-[4.750977993011475, 1.826372742652893, "[TT] Launch Date of the HORYU-2 = 17 May 2012"]
-[6.458123207092285, 8.66881275177002, "[FF] Polarization Directions of the POL = -60\u00b0, 0\u00b0 and +60\u00b0"]
-[12.819473266601562, 7.614752769470215, "[TT] Power of the Instrument = 13 W"]
-[7.045227527618408, 2.3691916465759277, "[FF] Mission of the Greencube = Growing plants in microgravity"]
-[14.296290397644043, 3.140026092529297, "[TT] Mass of the SOCRATES = ~ 50 kg"]
-[12.838455200195312, 7.568216800689697, "[TT] Power Transfer of the MWI Instrument = 200 W"]
-[5.972300052642822, 2.9389939308166504, "[TT] Deployment of the DIAL Instrument = NACP (North American Carbon Program) regional intensive field campaigns"]
-[8.22562026977539, 7.411920070648193, "[FF] Detector Technology of the SSULI = Wedge and strip microchannel plate detector technology"]
-[9.283614158630371, 2.813286542892456, "[TT] Solar Wind Speed and Beta of the ACE = ~48% lower on average from 2009 through the day 79 of 2013"]
-[7.793285846710205, 4.881941318511963, "[FF] Objective of the Sounder = Measure the temperature and humidity profiles"]
-[7.975900650024414, 4.745227813720703, "[FF] Components of the SVM = High-gain antenna, three low-gain antennas, hydrazine and cold-gas thrusters, sun sensors"]
-[5.557529449462891, 1.226421594619751, "[TT] Funding Period of the AIM spacecraft = Through September 2018"]
-[4.850592136383057, 6.2884931564331055, "[TT] Protocol of the RF Communications = AX.25 or SRLL"]
-[5.735227584838867, -0.49934452772140503, "[TT] Operation Duration of the Yutu 2 = 321 Earth days"]
-[8.661197662353516, 4.725919723510742, "[TT] Quantity of the STR (Star Tracker) = 3"]
-[7.43965482711792, 4.636086463928223, "[FF] Function of the SADA = Reduce the spacecraft disturbances"]
-[8.577472686767578, 6.703339576721191, "[TT] Daily Imaging Capacity of the PRISMA System = Up to 200,000 km2"]
-[9.346574783325195, 4.73944616317749, "[FF] Observation of the Transient Attitude Instabilities = Small changes were needed to the on-board attitude control logic"]
-[6.810473442077637, 0.03134872764348984, "[TT] Observation Duration of the Kepler space telescope = Nine years"]
-[9.86250114440918, -0.4080796241760254, "[TT] Apoapsis Altitude of the Satellite = 21813.2 km"]
-[2.3241615295410156, 1.3132622241973877, "[FF] Deorbiting of the NanoSail-D2 = Ongoing"]
-[9.684982299804688, 0.3781631886959076, "[TT] Formation Flying Distance of the PROBA-3 = 144 m"]
-[3.535607099533081, 5.333621501922607, "[TT] Data Rate of the SAR payload = 640 Mbit/s"]
-[6.862607479095459, 2.1597237586975098, "[TT] Launch Year of the FormoSat-5 Remote Sensing Instrument (RSI) = 2013"]
-[13.52893352508545, 2.8990414142608643, "[TT] Spacecraft Mass of the QSat = < 50 kg"]
-[9.37602710723877, 4.770063400268555, "[FF] Component of the Cryomagnet Avionics Box (CAB) = Unknown"]
-[14.079291343688965, 3.1528749465942383, "[TT] Mass of the IPS = 1,180 kg"]
-[4.90474271774292, 0.06494618207216263, "[TT] Launch Date of the REXJ = July 21, 2012"]
-[9.157933235168457, 7.638877868652344, "[TT] Spatial Resolution of the spaceCam c4000 = 6 m"]
-[5.251006126403809, 7.972326755523682, "[TT] Stiffness Requirement of the COMMx = 50 Hz or greater"]
-[5.017729759216309, 1.0815380811691284, "[TT] Launch Date of the ALOS-3 = February 16, 2023"]
-[6.843207359313965, -0.5714073777198792, "[TT] ToO Exceptional Duration of Observation of the SVOM = 14 orbits (tunable)"]
-[8.434062004089355, 8.309554100036621, "[TT] FPA Type of the HyperCube Instrument = 6 x 6 MWIR FPA"]
-[4.556242942810059, 6.956121444702148, "[TT] Bandwidth of the Spacecraft Repeater = 46 kHz"]
-[9.540817260742188, 4.064269542694092, "[TT] Failure of the Magnetometer = Z-axis failure during the first year in orbit"]
-[5.029450416564941, 3.102245569229126, "[TT] Manufacturer of the Resurs-DK1 = TsSKB Progress"]
-[8.368476867675781, 1.2478201389312744, "[TT] Data Collection Altitude of the RainCube = About 310 km"]
-[10.253256797790527, 2.11185884475708, "[FF] Image Credit of the eROSITA telescope = Jeremy Sanders, Hermann Brunner, Andrea Merloni and the eSASS team (MPE); Eugene Churazov, Marat Gilfanov (on behalf of IKI)"]
-[10.261468887329102, 4.833211898803711, "[TT] Ion Drift Velocity of the PAP = -3 ~ +3 km/s"]
-[9.43581485748291, 4.068068504333496, "[TT] Frequency Range of the Electric Field Measurement System = 20 Hz - 100 kHz"]
-[8.695205688476562, 6.853549480438232, "[FF] Image Quality of the SPOT 6 = Unknown"]
-[4.733567714691162, 0.8154111504554749, "[TT] Launch Date of the Foton = May 31, 2005"]
-[13.346092224121094, 5.564342498779297, "[TT] Quantity of the ISS Roll-Out Solar Array (iROSA) = 2"]
-[3.7985141277313232, 1.1482125520706177, "[TT] First Stage Diameter of the Falcon 9 = 3.66 m"]
-[8.466699600219727, 3.1984050273895264, "[TT] Minimum Concentration in 2016 of the Ozone Layer = 114 Dobson Units"]
-[6.021452903747559, 6.47382116317749, "[TT] Data Product Delivery Time of the CATS = Within 12 hours"]
-[11.858619689941406, 0.01649506948888302, "[TT] Number of Stars in Catalog of the TESS = 227"]
-[8.837326049804688, 6.9319658279418945, "[FF] Position of the Earth Imaging Camera = Bottom Middle"]
-[5.995818138122559, 0.8078365921974182, "[TT] Capture Time of the Images = Around 10:30 JST on 6 January 2018"]
-[7.969237804412842, 8.728677749633789, "[TT] Spectral Range of the XRS = 0.05 - 0.8 nm"]
-[4.7180304527282715, 0.41792920231819153, "[TT] Launch Date of the WCOM = Unknown"]
-[7.729931831359863, 1.7163894176483154, "[FF] Coverage of the WatER = Tropical wetlands, particularly in the Amazon Basin, cover nearly 20% of their watershed"]
-[10.97672176361084, 4.749213695526123, "[FF] Principle of the Momentum-exchange Tethers = Based on the gravity gradient force"]
-[7.177850246429443, -0.16381889581680298, "[TT] Number of Parameters of the PEM (Parameterized Exospheric Model) = 30 parameters"]
-[7.609149932861328, 8.983766555786133, "[TT] NER of the Spectral Band A = 3.0 x 10^-5 W/(cm^2 sr \u00b5m)"]
-[13.361682891845703, 7.341294288635254, "[TT] Power of the DCG = 4.5 W"]
-[9.127363204956055, 2.823227882385254, "[FF] Purpose of the X-ray flux monitor = Better space weather forecasts"]
-[11.862156867980957, 4.51261043548584, "[TT] Legspan of the Autonomous spaceport drone ship = About 18 m"]
-[14.27405834197998, 3.0197079181671143, "[TT] Mass of the UniSat-2 = 12 kg"]
-[9.992860794067383, -0.6975617408752441, "[TT] Orbit Altitude of the Optsat-3000 = 720 km"]
-[7.054582118988037, 3.7031404972076416, "[FF] Presentation Date of the Proba-3 Formation Flying System = 17 July 2017"]
-[8.476645469665527, 6.859455108642578, "[TT] Time Resolution of the FY-4 GLI = About 2 ms"]
-[10.819677352905273, -0.2698034942150116, "[TT] Data Resolution of the TanDEM-X = 50 m x 50 m"]
-[5.782496452331543, 3.248802661895752, "[TT] Number of Satellites of the WorldView Legion = 6"]
-[7.685405254364014, 9.407328605651855, "[TT] Center Wavelength of the Band 4 = 13.96 \u00b5m (733 cm -1)"]
-[7.347552299499512, 6.358304977416992, "[FF] Operating Principle of the LRR = Measure the round-trip run time of laser pulses reflected from an array of corner cubes at the satellite"]
-[14.035341262817383, 3.1383450031280518, "[TT] Mass of the Corvus-BC-3 = 11 kg"]
-[7.983747482299805, 7.916193962097168, "[FF] Camera Type of the BIROS = One pushbroom camera operated in the near-infrared (VNIR) spectral range, while the other two were infrared pureplays"]
-[9.943577766418457, 8.170510292053223, "[TT] Individual Focal Length of the MAs and MCs = 1600 mm"]
-[7.6558685302734375, 7.179741859436035, "[TT] Read Noise of the CCD = 10 e-"]
-[9.949976921081543, -1.3707319498062134, "[TT] Orbit Inclination of the BeaverCube = 51.6\u00b0"]
-[14.127950668334961, 3.3258402347564697, "[TT] Total PCB Mass of the GAMALINK = < 100 g"]
-[8.741454124450684, 4.93729829788208, "[TT] Accuracy of the Star Trackers = >99.45% per orbit"]
-[6.898842811584473, -0.7057914137840271, "[TT] Orbital Period of the AlSat-2B = 99.19 minutes"]
-[10.91956901550293, 7.533524036407471, "[TT] Swath Width of the HSRS = 190 km"]
-[4.413603782653809, 2.72802996635437, "[TT] Location of the GWUH = Wuhan China"]
-[5.467162609100342, 0.47627517580986023, "[TT] Anniversary Date of the LRO = June 18, 2014"]
-[13.324407577514648, 5.43364953994751, "[FF] Solar Array Deployment of the MicroSCOPE = 3 pyrolock mechanisms for release and 2 Carpenter blades for deployment"]
-[8.296524047851562, 6.9665846824646, "[TT] Number of Public Images of the Ikonos = 597,802"]
-[9.377859115600586, 3.539581298828125, "[FF] Amplitude of the daily variation of the horizontal magnetic intensity (\u0394H) of the EEJ (Equatorial Electrojet) = 3\u20135 fold higher than the variation of data from other regions of Earth"]
-[8.073822021484375, 5.878101348876953, "[FF] Measurement of the Imaging Spectrometer = Visible and infrared light reflecting from surfaces below"]
-[9.40961742401123, 7.062572479248047, "[TT] Spatial Resolution of the Ma_MISS = 120\u2009\u00b5m"]
-[3.847902774810791, 3.4155285358428955, "[TT] First launch date of the GALILEO = October 2012"]
-[13.373598098754883, 7.632629871368408, "[TT] Output Power of the Prototype Chip = Three times more than the current amplifier"]
-[10.330390930175781, 4.032206058502197, "[TT] Retention Mechanism of the Deployment Systems = Pyro cutters"]
-[9.834047317504883, 8.162014961242676, "[TT] Size of the Focal Plane Unit = 25 cm x 23 cm x 23 cm"]
-[10.174948692321777, 9.37431812286377, "[TT] Nominal IGFOV of the Band 10 = 2 km"]
-[4.430697917938232, -0.25116416811943054, "[FF] Technical Problems of the Nauka = Several"]
-[10.137735366821289, 9.995528221130371, "[TT] Next Launch Schedule of the Vega = Q1 2021"]
-[5.9077839851379395, 5.736044406890869, "[TT] Subsystem Type of the OBCom = Internal wireless optical communications subsystem"]
-[10.330484390258789, 4.514467716217041, "[TT] Reaction Wheels of the S/C = Four"]
-[5.843171119689941, -0.7937359809875488, "[TT] Useful Lifespan of the Satellites = Shortened by moving more often than needed"]
-[6.639437675476074, 8.83323860168457, "[FF] Purpose of the Polarisation and Directionality of the Earth\u2019s Reflection-2 (POLDER-2) = Earth observation"]
-[13.384310722351074, 7.263027667999268, "[TT] Specific Power of the SBVR = 373 W/kg"]
-[2.958181381225586, 4.462906837463379, "[TT] Stripmap Mode Spatial Resolution of the PALSAR-2 = 10 m, 6 m, and 3 m"]
-[3.5205845832824707, 1.2614402770996094, "[TT] Launch Date of the Dove 3 and Dove 4 = Nov. 21, 2013"]
-[5.221845626831055, 1.0926085710525513, "[FF] Conference Presentation Date of the SEXTANT = March 7-14, 2015"]
-[8.08116340637207, 1.88523530960083, "[TT] High Surf Warnings of the California Coast = Swells of 16 to 24 feet"]
-[11.413474082946777, 4.410463809967041, "[TT] Size of the OptiCube-3 = 3U"]
-[5.315458297729492, 1.3316420316696167, "[FF] Conference Date of the Roshydromet Program = Sept. 19-23, 2005"]
-[4.1368727684021, 0.17263945937156677, "[FF] Last-Second Abort Date of the Falcon 9 = Oct. 2"]
-[9.96986198425293, 7.829880237579346, "[TT] Design Load of the AEISS telescope = 15 g per axis"]
-[11.424246788024902, 3.9647555351257324, "[TT] Size of the TechEdSat = 10 cm x 10 cm x 11.3 cm"]
-[5.269801616668701, 7.2568182945251465, "[TT] Data Rate of the Transmitter = 500 Mbit/s"]
-[6.928741931915283, -0.31536921858787537, "[TT] Number of Orbits of the Quasi-Halo Orbits = 14"]
-[10.706790924072266, 0.9905068874359131, "[TT] Radius of the GJ 367 b = 72 percent that of Earth's"]
-[9.388671875, -0.02725394256412983, "[TT] North to South of the Aso Caldera = 25 km"]
-[5.812404155731201, 3.17014217376709, "[FF] Major Challenge of the NPOESS = Jointly executing the program between three agencies of different size with divergent objectives and different acquisition procedures"]
-[7.729970455169678, 0.5355833172798157, "[FF] Coverage of the Lunar IceCube = Lunar nearside, function of latitude, several times of day"]
-[5.210721969604492, 6.807198524475098, "[TT] Telemetry, Tracking, and Command (TT&C) Data Link Uplink of the AstroBus-L = 64 kbit/s"]
-[5.65939998626709, 7.105509281158447, "[TT] Data Rate of the ABI = 2.6 Mbit/s - 75 Mbit/s"]
-[11.283394813537598, 5.457986354827881, "[TT] Device Mass of the Gamma-ray Counter = 260 g / unit"]
-[3.1055212020874023, 2.333984851837158, "[FF] Spectral Sampling of the Sentinel-2 = Unique set of measurement/calibration bands"]
-[6.909633159637451, 1.6234863996505737, "[FF] Purpose of the Webb = To see farther into our origins: from the formation of stars and planets to the birth of the first galaxies in the early Universe"]
-[7.838333606719971, 4.473533630371094, "[FF] Characteristics and Calibration of the AMSR and AMSR-E = Unknown"]
-[6.058224678039551, 2.4414591789245605, "[TT] Operator of the New Horizons = Johns Hopkins University Applied Physics Laboratory"]
-[6.467066764831543, -0.45353400707244873, "[TT] Period of the BUV = 107.2 minutes"]
-[4.556585788726807, 5.944119453430176, "[TT] Frequency of the Distress Beacons = 406.025 MHz"]
-[8.421875, 7.679993152618408, "[TT] Sensor Complement of the QSat = 2-band CMOS camera (VNIR) 3000 x 2000 pixels"]
-[13.176244735717773, 7.290621757507324, "[TT] Power Consumption of the SSM/I = 45 W"]
-[10.706415176391602, -0.20204922556877136, "[TT] Geophysical Products of the Tandem-L = 26"]
-[8.151668548583984, -1.0839933156967163, "[TT] Function of the ICESat-2 = Measure the shape and depths of lake beds and shallow seafloors"]
-[3.469233512878418, -0.9193795919418335, "[TT] Type of the Orbit = Sun-synchronous near-circular"]
-[5.339438438415527, 2.1516969203948975, "[TT] Data Analysis Lead of the ROMAP = Philip Heinisch"]
-[4.9742207527160645, 3.241762399673462, "[TT] Manufacturer of the MVIRI = Matra Marconi Space"]
-[13.499314308166504, 2.8422653675079346, "[TT] Maximum Satellite Mass of the AD-SS 200 = 200 kg"]
-[7.376690864562988, 8.84825611114502, "[TT] Filter Type of the FUV channel = Calcium Fluoride"]
-[7.692726135253906, 9.045768737792969, "[TT] Measurement Bands of the OCTS = 12 bands from 0.402 - 12.5 \u00b5m"]
-[6.365108013153076, 4.5800957679748535, "[FF] Function of the UIS = Manage orders from the end-users"]
-[9.913812637329102, 6.188547134399414, "[TT] Detector Operating Temperature of the D-CIXS = Near room temperature"]
-[7.136122703552246, 2.7657694816589355, "[TT] Launch Date of the MethaneSAT = Mid-2022"]
-[6.462863922119141, -0.39917364716529846, "[TT] Operation Duration of the SloshSat = 57.5 hours"]
-[9.923169136047363, 5.46944522857666, "[FF] Function of the SES = Demonstrate that the instrument can survive the extreme thermal gradients and mechanical strains"]
-[4.645503044128418, 0.10608546435832977, "[TT] End of Life Date of the FREESTAR = 1 February 2003"]
-[13.205445289611816, 7.22702169418335, "[TT] Power Consumption of the ICARE = 2.5 W"]
-[9.814367294311523, 8.660118103027344, "[TT] IFOV (Instantaneous FOV) VIS of the MVIRI = 0.065 mrad"]
-[8.153252601623535, -0.4360577166080475, "[TT] Rank of the Arctic Sea Ice = 12th-Lowest on Record"]
-[13.239856719970703, 5.239593029022217, "[TT] Size of the Solar Cells = 40 x 80 cm"]
-[10.718408584594727, 5.535520076751709, "[FF] Heat Shield Material of the Orion spacecraft = 3-D woven thermal protect system fabric"]
-[7.698732852935791, 0.25494885444641113, "[TT] Launch Date of the Lucy = 16 October 2021"]
-[10.098136901855469, 0.14354924857616425, "[TT] Flight Formation of the Harmony = At a distance of 350 km from the Sentinel-1 satellite"]
-[9.498003005981445, 6.103936672210693, "[TT] Incidence Angle of the AMSR = 55\u00b0"]
-[6.0569305419921875, 6.357907772064209, "[TT] Data Transmission of the DSP event processor = Energy, position and time information"]
-[4.280681133270264, 6.342128753662109, "[FF] Nominal Input Level of the Antenna = Unknown"]
-[8.600642204284668, 2.9242422580718994, "[FF] Mission Purpose of the TARANIS = Study of transient event energetic mechanisms that generate transient luminous emissions and gamma ray flashes in the terrestrial atmosphere above the thunderstorm areas"]
-[7.035708904266357, 1.986116647720337, "[FF] URL of the Micro-Particle Impact Detector = http://setas-www.larc.nasa.gov/mpid/mpid.html"]
-[9.729684829711914, -0.3786196708679199, "[TT] Retrieval Altitude of the EURECA = 476 km"]
-[6.525262832641602, 6.295807361602783, "[FF] RFI Source Levels of the SMOS Satellite = Moderate, Strong, Very Strong"]
-[8.456938743591309, 5.579802989959717, "[TT] Open Service Timing Accuracy of the COMPASS/BeiDou = 20 ns"]
-[8.677359580993652, 7.653892517089844, "[TT] Pixel Arrangement of the CCD = 516 x 512 pixels"]
-[10.948822021484375, 7.502796173095703, "[TT] Swath Width of the COSI = 16.8 km"]
-[4.375115871429443, 7.081754684448242, "[TT] TT&C Data Transmission of the RF Communications = S-band"]
-[7.457113265991211, 3.736449718475342, "[FF] Material of the Phantoms = Mimic human bones, soft tissues, and organs of an adult female"]
-[4.7234578132629395, 6.815682411193848, "[FF] Protocol of the UoSAT-12 = AX.25 (Amateur radio X.25)"]
-[7.463339805603027, 6.247706890106201, "[TT] Measures of the Dual-color laser altimeter = Surface elevation"]
-[13.316492080688477, 7.642003059387207, "[TT] Peak RF Power of the HPA = 120 W"]
-[4.328617572784424, 7.590538024902344, "[TT] X-band frequency of the Transmitter/Receiver EMC = 7167 MHz"]
-[5.1490044593811035, 1.028661847114563, "[FF] Conference Presentation Date of the CANYVAL-X = 28 May - 1 June 2018"]
-[4.477022171020508, 2.4358108043670654, "[TT] Location of Inspection of the EFT-1 Orion = Naval Base San Diego Mole Pier"]
-[9.689339637756348, 8.369911193847656, "[TT] Nominal FOV of the SPARCS = 2\u00b0"]
-[11.185999870300293, 1.0737223625183105, "[TT] Sensitivity of the LISA Laser Receiver = Few hundreds of picowatts"]
-[7.264055252075195, 4.688427448272705, "[FF] GNC Functions of the P3RVX = Guidance, Navigation, and Control"]
-[10.328468322753906, 2.3176300525665283, "[TT] Presenters of the An Efficient Photoelectric X-ray Polarimeter = Enrico Costa, Paolo Soffitta, Ronaldo Bellazzini, Alessandro Brez, Nicholas Lumb & Gloria Spandre"]
-[5.818615436553955, -0.7078254222869873, "[TT] Nominal Lifetime of the HY-2A = 3 years"]
-[11.795318603515625, 6.738171577453613, "[FF] Ion Energy Threshold of the DIDM = Certain threshold potential"]
-[4.142367362976074, 3.723501682281494, "[FF] Nitrogen Variation of the Galileo probe = Up to 38 percent"]
-[11.9137544631958, 6.78921365737915, "[TT] Energy Resolution of the IMAP = 100 eV"]
-[5.080547332763672, 2.0971603393554688, "[FF] Mission Type of the TacSat-3 = Technology demonstration"]
-[5.557742118835449, 4.8603386878967285, "[FF] On-board and Ground Time Management System Presentation of the QZSS = ION NTM (National Technical Meeting) 2007, San Diego, CA, USA, January 22-24, 2007"]
-[9.234862327575684, 0.21766161918640137, "[TT] Number of Railway Lanes of the Yavuz Sultan Selim Bridge = 2"]
-[8.974382400512695, 4.392323970794678, "[FF] Purpose of the MAS = Orientation of the satellite in the direction of the Sun, with a slow rotation around the X-axis for thermal reasons"]
-[13.100098609924316, 7.218379020690918, "[TT] Power Consumption of the FTS-2 = 270 W"]
-[8.684189796447754, 2.0423717498779297, "[TT] Wind Speed Accuracy of the SCAT = 10%"]
-[8.273599624633789, 3.1729791164398193, "[FF] Award Date of the Ozone Monitoring Instrument = 3 May 2019"]
-[6.311945915222168, 2.4195406436920166, "[TT] Principal Investigators of the SCIAMACHY = J. P. Burrows, H. van Dop"]
-[5.778704643249512, 5.990920543670654, "[TT] Ground of the Data Transmission = Real time"]
-[6.920699119567871, 8.870522499084473, "[TT] Spectral Region of the POLDER = 443 to 910 nm"]
-[8.600922584533691, 4.7582831382751465, "[FF] Observation Method of the Student Observers = Measure right ascension and declination at precise times by reference to known stars"]
-[8.001388549804688, 6.387323379516602, "[TT] Instrument Type of the HJ-1 = Imaging multi-spectral radiometers (vis/IR)"]
-[9.375116348266602, 4.964695453643799, "[TT] Stability of the Attitude Control System = Low jitter"]
-[5.3452372550964355, 7.8384857177734375, "[TT] Power Consumption of the Ka-Band unit = 13 Watts"]
-[6.439226150512695, 4.975905418395996, "[FF] Auto-generated Components of the FSW = Partial C++ implementation, C++ code for instantiating the components and connecting the ports, interface dictionaries for use by the ground data system"]
-[7.1720967292785645, 1.233168363571167, "[TT] Type of the Mars Ascent Vehicle (MAV) = Two-stage"]
-[9.504443168640137, 7.138113975524902, "[TT] Spatial Resolution of the Severyanin-M OBRC = 400 - 1000 m"]
-[11.844799041748047, 6.6554856300354, "[TT] Particle Energies of the Inward Moving Shocks = About 30 times the energies of the LHC"]
-[9.54194164276123, 4.428524017333984, "[FF] Design of the SpinSat = Spherical"]
-[3.4801549911499023, 1.8343021869659424, "[FF] URL of the Sentinel-1 = http://earth.eo.esa.int/workshops/fringe09/participants/1197/pres_1197_Rosich.pdf"]
-[8.0020112991333, 8.81417179107666, "[TT] Lamps of the SOLSPEC = Two with deuterium"]
-[3.2135133743286133, 5.136914253234863, "[TT] Height of the Kanjut Sar = 7,760 m"]
-[10.812567710876465, 3.8953566551208496, "[FF] Function of the Drag-sail = Speed de-orbit into the Earth\u2019s atmosphere"]
-[9.559834480285645, 9.107924461364746, "[FF] Usage of the Iris = Raw measurements transfer and remote control of the spacecraft"]
-[6.855414867401123, 5.1312150955200195, "[FF] Function of the Remote Power Control Module (RPCM) Type V Internal = Distributing power capabilities across the ISS"]
-[10.38613224029541, 2.7869012355804443, "[FF] Presentation Date of the Nanosatellite Tracking Ships = April 27\u201330, 2009"]
-[7.669293403625488, 2.9604830741882324, "[FF] Mission of the GOSAT-2 = Greenhouse gas monitoring"]
-[10.528360366821289, 2.8012049198150635, "[FF] Agreement Date of the Nanosatellite And Plug-and-play Architecture (NAPA) Project = Sept. 17, 2010"]
-[5.366251468658447, 7.218444347381592, "[TT] Transmission Rate of the Modulator = 155 Mbit/s"]
-[7.964387893676758, 2.531540632247925, "[TT] Measurement Domain of the TAIKI = Land"]
-[3.108541488647461, 2.24348783493042, "[FF] Land Measurements of the Copernicus Sentinel-3 = Maps land, provides indices of vegetation state and measures the height of rivers and lakes"]
-[5.273585319519043, 4.118083953857422, "[TT] Bus Type of the MEV-1 = GEOStar 3"]
-[7.836401462554932, -0.12602537870407104, "[TT] Location of the Eureka Station = Canadian Arctic at 80 degrees north latitude"]
-[8.122076988220215, 7.801435470581055, "[FF] Mean Dark of the NISP IR Detector = Around 0,005 e\u2013/pix/s at 100 K"]
-[13.954211235046387, 3.7112138271331787, "[TT] Mass of the Optics Module = 37.5 kg"]
-[8.232966423034668, 8.224655151367188, "[TT] Spectral Range of the Imager = 0.4-2.4 \u00b5m (VNIR + SWIR)"]
-[11.794466018676758, 6.747845649719238, "[TT] Electron Energy Range of the MSGI-MKA = 0.1 to 15 keV"]
-[6.708999156951904, -0.4610636830329895, "[TT] Period of the COMPASS-1 = 102 minutes"]
-[5.237091064453125, 1.3037694692611694, "[FF] Conference Presentation Date of the THEMIS = Aug. 8-11, 2005"]
-[14.086423873901367, 4.012801170349121, "[TT] Mass of the Instrument = 32 kg"]
-[11.395901679992676, 4.336402893066406, "[TT] Size of the QBus-4 = 2U"]
-[6.522926330566406, 4.685471057891846, "[FF] Observation Method of the Some observers = Use GPS receivers to measure the latitude, longitude and altitude of their observing sites"]
-[7.570573806762695, 0.9291204214096069, "[FF] Purpose of the Moon Radar = Surveying the lunar sub-surface structure"]
-[7.366907119750977, 5.3505353927612305, "[FF] Components of the LF Receiver = Laser diodes, collimation lenses, electrical and mechanical hardware, copper heatsink, aluminum-alloy chassis, PCM module"]
-[3.9499292373657227, 6.319591999053955, "[TT] Antennas of the R3 Spacecraft = Two patch antennas"]
-[5.363649368286133, 3.0606160163879395, "[TT] Builders of the SCIAMACHY = DASA/DSS, Fokker Space, TNO, SRON"]
-[7.465803146362305, 2.2703206539154053, "[FF] Data of the ICEYE = Used to monitor oil wells and measure global oil storage"]
-[5.976888179779053, -0.6733105778694153, "[TT] Design Life of the RADARSAT-2 = Seven years"]
-[8.046270370483398, 3.3813960552215576, "[FF] Rayleigh Impact of the Aeolus = Gradually declining as the instrument noise increases"]
-[14.31983470916748, 3.0051255226135254, "[TT] Mass of the Global-3 = 60 kg"]
-[2.941046953201294, 4.476670742034912, "[TT] Pixel Size of the ALOS-2 PALSAR-2 = About 50 m2"]
-[4.649273872375488, 6.603126525878906, "[FF] Receiver Type of the DVB-S2 = Commercial mass-market"]
-[10.86870002746582, 3.299762487411499, "[TT] Crystal Growth Environment of the CASIS PCG-16 = Microgravity"]
-[5.949232578277588, 2.55682373046875, "[FF] Project Philosophy of the ESEO = Maximize student participation in AIV activities and spacecraft operations"]
-[10.063695907592773, 3.0310568809509277, "[FF] CubeSat Observatory of the CuPID = Unknown"]
-[14.400487899780273, 3.1146254539489746, "[TT] Mass of the BIRCHES = 2.5 kg"]
-[13.228400230407715, 7.3330607414245605, "[TT] Electric Power of the FLP = 270 W"]
-[8.543534278869629, 5.475600719451904, "[TT] Aliasing Error of the Satellite = 0.08%"]
-[7.688573837280273, 3.2412564754486084, "[TT] Sensing Capability of the OLS = View clouds by moonlight"]
-[7.97627067565918, 7.269339084625244, "[TT] Interferometer Ports of the FTS = Four"]
-[9.282586097717285, 9.146666526794434, "[TT] Far-UV Channel Range of the IRIS = 133.0\u2013141.0 nm"]
-[10.794775009155273, 3.796384811401367, "[TT] Sail Deployment Time of the InflateSail = Approximately one hour after ejection"]
-[5.955758571624756, 6.808133125305176, "[FF] Function of the PIU = Access TTE data from each DP5G unit and store in a rolling buffer"]
-[7.001112461090088, 4.234877109527588, "[FF] Definition of the PUG = Unknown"]
-[13.443750381469727, 5.4620232582092285, "[TT] Number of Strings per Panel of the Solar Array = 11"]
-[11.08792781829834, 4.844046592712402, "[TT] Electric Charge of the Tether = 500 V"]
-[6.856750965118408, 0.5363635420799255, "[TT] Observation Campaign of the Kepler spacecraft = 18th"]
-[5.414862155914307, 3.891130208969116, "[FF] Number of Satellites of the Satellite Cluster = Up to 20"]
-[6.268283843994141, 3.338456630706787, "[TT] Number of Satellites of the BlackSky Constellation = 60"]
-[10.061811447143555, -1.5128079652786255, "[TT] Rotation Angle of the GR700XD grism = ~2\u00ba"]
-[7.55305814743042, 8.467272758483887, "[TT] Usable Bands of the FTHSI instrument = 137"]
-[7.652828216552734, 8.58686351776123, "[FF] MWIR Band of the OHIS = Cancelled in 2000"]
-[8.09015941619873, 8.03281307220459, "[TT] Spectral Band of the Band Cameras = 650-740 nm"]
-[13.486984252929688, 2.8525168895721436, "[TT] Maximum Satellite Mass of the AD-SS 150 = 150 kg"]
-[12.140009880065918, 3.1900267601013184, "[TT] Propellant Type of the GPIM = AF-M315E"]
-[10.428526878356934, 4.022423267364502, "[TT] Tip Mass of the Gravity-Gradient Boom = 3 kg"]
-[5.029216766357422, 5.632164478302002, "[FF] Gyro-holding Mode of the Antenna Subsystem = Keeps the antenna pointed into the same location in the sky during periods when the beacon is suddenly lost"]
-[9.95943546295166, 4.17387580871582, "[FF] Attitude Stabilization of the UniSat-4 Microsatellite = Passive Magnetic"]
-[4.325138092041016, -0.10837479680776596, "[FF] Comments of the P35-6 = Also known as Ops-3367"]
-[4.869684219360352, 0.5978870987892151, "[FF] Launch Contract Date of the Muninn = Early 2023"]
-[5.703198432922363, 5.029648303985596, "[FF] Messaging Capability of the ODTML = Two-way delay-tolerant"]
-[4.3943071365356445, 3.8248708248138428, "[FF] Function of the Galileo App = Overlaid Satellites in Real Time"]
-[8.355164527893066, 3.084212303161621, "[FF] Function of the MiniRad = Measure temperature at different levels of the atmosphere"]
-[8.439936637878418, 1.8098435401916504, "[FF] Definition of the Total Precipitable Water Vapor = Amount of water in a column of the atmosphere if all the water vapor in that column were condensed into liquid"]
-[7.798844814300537, 6.953239917755127, "[FF] Deformation Mode of the Tandem-L = Repeat-pass interferometry"]
-[5.590859413146973, 0.10843916237354279, "[TT] Launch Date of the Ulysses = 1990"]
-[6.708075046539307, -0.6437032222747803, "[TT] Flight Time to Separation Orbit of a group of smallsats of the Fregat upper stage = 1 minute 6 seconds"]
-[5.985336780548096, -0.4248218834400177, "[TT] Planned Mission Duration of the Wind = 5 years"]
-[13.773602485656738, 5.353271007537842, "[TT] Solar Cells of the EPS = Triple junction GaAs"]
-[5.767079830169678, 5.663437843322754, "[TT] Operating Models of the DHS = 1) processor-based; 2) state-machine based; and 3) analog only"]
-[5.993588447570801, -0.45177674293518066, "[TT] System and Software Integration and Testing Duration of the PhiSat-1 = Four months"]
-[2.4037649631500244, 1.3339288234710693, "[FF] Patch Content of the NanoRacks Module 74 = Antimicrobial hydrogel"]
-[4.632494926452637, 1.5707824230194092, "[FF] Meeting Date of the GOSAT TANSO-FTS = June 18-20, 2012"]
-[7.682226657867432, 5.729803085327148, "[FF] Components of the SIM = Focal-plane cameras, ACIS, HRC"]
-[11.001286506652832, 3.7661638259887695, "[TT] \u0394V of the NEA Scout = Up to 2km/s"]
-[9.6991605758667, -1.0874860286712646, "[TT] Orbit Longitude of the FY-4A = 104.7\u00ba E"]
-[8.320049285888672, -0.8353767991065979, "[TT] Accuracy of Land Ice Surface Elevation Changes Measurement of the ATLAS = 0.25 m per year"]
-[3.2965052127838135, 1.481597900390625, "[TT] Launch Date of the Sentinel-6A = November 2020"]
-[4.4402174949646, -0.061487022787332535, "[FF] Close Call Classification of the Starliner = High-visibility close call"]
-[1.71797776222229, 6.144655227661133, "[FF] Composition of the Dark Energy = ~68%"]
-[12.042780876159668, 3.6886050701141357, "[TT] Pressurized Module Interior Pressure of the JEM/Kibo = 1 atmosphere (1atm)"]
-[5.515558242797852, 6.167694091796875, "[TT] Capacity of the Flash Memory Card = 8GB"]
-[9.604989051818848, 7.652372360229492, "[TT] Ground Pixel Size of the Telescope = 2.5 km x 2.5 km"]
-[11.152191162109375, 1.1276952028274536, "[FF] Wavelength of the LISA = Much longer"]
-[5.589221477508545, 5.715316295623779, "[TT] Microprocessor of the C&DH = Single"]
-[10.359285354614258, 3.2275824546813965, "[TT] OBCs of the CubeSat = 2"]
-[8.273547172546387, 2.835183620452881, "[FF] Purpose of the Delfi-n3Xt = Space Weather Research and Qualification of Microtechnology"]
-[2.8974881172180176, 1.9753544330596924, "[FF] Image Capture Date of the Copernicus Sentinel-2 = March 2018 and March 2022"]
-[3.5934560298919678, -0.7431134581565857, "[TT] Type of the Orbit = SSO"]
-[6.972092628479004, -0.7041159272193909, "[TT] Orbital period of the GALILEO = 14 h 22 m"]
-[5.895772933959961, 1.115927815437317, "[FF] Launch Date of the Rain and Snow Satellite = Unknown"]
-[7.845057964324951, 5.111385822296143, "[FF] Instrument of the GRACE-FO = Accelerometers, microwave ranging instruments"]
-[13.951729774475098, 2.7681469917297363, "[TT] Launch Mass of the ResourceSat-2A = 1235 kg"]
-[9.394970893859863, 4.485818386077881, "[FF] Components of the Reaction Dynamics Study = 1) Manipulator operation that yields minimum reaction on the base satellite 2) Manipulator endpoint control for inertial target under the free-floating environment 3) Terminal state control for free-floating space robot 4) Base attitude control for quick recovery from the manipulator motion disturbance"]
-[8.1819429397583, 2.0755677223205566, "[FF] Cross-Calibration Latitude of the CloudSat = 12 degrees"]
-[3.3710238933563232, 5.656862258911133, "[TT] Number of T/R Modules of the SAR Antenna = 512"]
-[11.017759323120117, 5.404638767242432, "[FF] Target for Researchers of the Silkworm = Development of new silkworm strains for multiple purposes"]
-[3.2178173065185547, 2.3340814113616943, "[FF] Instrument of the Copernicus Sentinel-6 = Radar Altimeter"]
-[6.147812366485596, 4.289602756500244, "[FF] Purpose of the USAT = Establish telecommunications in disaster areas"]
-[7.539009094238281, 2.0157485008239746, "[FF] Band 2 of the Landsat TM = Green reflectance, peak of healthy vegetation, plant vigor"]
-[3.592175245285034, 4.956175327301025, "[TT] Subswaths of the C-RADAR = 4 C-band subswaths"]
-[10.009281158447266, -1.5163774490356445, "[TT] Orbit Inclination of the G\u00f6kt\u00fcrk-2 = 98.1\u00ba"]
-[9.650595664978027, 1.6419810056686401, "[FF] Primary Science Missions of the MIRIS = (1) mapping of the Galactic plane with Paschen-\u03b1 line (1:88 \u00b5m) for the study of warm interstellar medium and (2) measuring large angular fluctuations of cosmic near infrared background radiation with I (1:05 \u00b5m) and H (1:6 \u00b5m) bands to identify the origin of these fluctuations"]
-[3.1514289379119873, 2.3293535709381104, "[FF] Objective of the Sentinel-2 = Continuously providing optical observations of land and coastlines"]
-[9.038063049316406, 5.109966278076172, "[TT] Quantity of the Gyro Control Unit = 1"]
-[7.736424922943115, 2.138981580734253, "[FF] Application of the Altimeter = Detailed maps of the marine geoid"]
-[10.912675857543945, 10.09216022491455, "[FF] Antiproton Flux of the Alpha Magnetic Spectrometer = Unknown"]
-[9.274709701538086, 1.9915814399719238, "[FF] Purpose of the LRF-S2 = Measure the distance to the tip of the sampler horn"]
-[10.217238426208496, 0.9605823755264282, "[TT] Distance from Earth of the SS 433 = About 20,000 light-years"]
-[9.904703140258789, 8.924883842468262, "[TT] NS FOV: max channel of the AHI = 16,311 \u00b5rad"]
-[4.605315208435059, 6.864826679229736, "[TT] Telemetry Downlink of the TT&C radio = UHF"]
-[3.4505817890167236, 1.4798250198364258, "[TT] Arrival Date at Kourou spaceport of the Sentinel-2B = January 12, 2017"]
-[8.325716018676758, 5.328470230102539, "[TT] Spectral Calibration Accuracy of the TanSat = Superior to 1/10 FWHM"]
-[10.22927188873291, 3.2828152179718018, "[FF] Proximity to Payload of the VBN dedicated CubeSat = VBN sensor and ISL"]
-[7.205096244812012, 7.064648628234863, "[TT] Thermal Expansion Coefficient of the HeNe laser = Less than \u00b1 5 x 10-8/K"]
-[6.472304821014404, 4.226219177246094, "[FF] Mission Type of the CHIPS = Secondary payload"]
-[5.298448085784912, 4.076632499694824, "[TT] Bus Structure of the DubaiSat-1 = Deck-and-longeron type"]
-[9.275537490844727, 6.96281099319458, "[TT] Mass Resolution of the INMS = Approximately 12"]
-[9.693198204040527, 4.010942459106445, "[TT] Positioning of the GNB = \u00b120\u00ba about the magnetic field vector"]
-[11.411768913269043, 4.478011608123779, "[TT] Size of the SPATIUM-I = 2U"]
-[9.99299144744873, 6.087063312530518, "[TT] Albedo cal constant of the ADEOS/TOMS = 0.093 steradian -1"]
-[7.610688209533691, 8.229398727416992, "[TT] Point Response (2 x 2 pixel) of the SXI = 40%"]
-[6.091152667999268, 4.419589042663574, "[TT] Variants of the FY-4 = Two"]
-[8.317646026611328, 6.024438381195068, "[TT] Motion Measurement Accuracy of the Applique Ceramic Piezoelectric Actuators = 10 nm"]
-[5.738157749176025, 7.148390769958496, "[TT] Data Rate of the LRDL = ~ 10 kbit/s"]
-[8.766146659851074, 2.160970449447632, "[FF] Altitude Range of the Temperature Ch. 4 difference & ch. 7 difference = 50 - 100 km"]
-[7.958023548126221, 9.178070068359375, "[TT] Wavelength for Pointing Information of the LORE = 350 nm"]
-[7.163583755493164, 8.274009704589844, "[FF] SNR of the EUVS = 1:1 over 10 minute average, > 20:1 over 10 minute average"]
-[5.879240036010742, -0.7285565137863159, "[TT] Mission Design Life of the WINDS satellite = 5 years"]
-[11.63081169128418, 4.459718227386475, "[TT] Antennae Length of the Spin-Stabilized Spacecraft = 100 meter"]
-[5.021502494812012, 0.46245571970939636, "[TT] Launch Date of the RadSat = 2018"]
-[13.480903625488281, 2.860907554626465, "[TT] Total Mass of the Satellite = 110 kg"]
-[6.463169097900391, 3.903670310974121, "[FF] Objective of the SSBB = Remote maintenance of geostationary telecommunications satellites using a robotic arm"]
-[6.1488142013549805, 6.055415153503418, "[TT] Source Transit Time of the LWFT instrument = 300-1800 s"]
-[10.018035888671875, -1.5372520685195923, "[TT] Orbit Inclination of the IRIS = 97.9\u00ba"]
-[6.48378849029541, 4.149322986602783, "[FF] Sovereignty of the Ground Segments = Independent"]
-[11.875654220581055, 3.3001708984375, "[TT] Deceleration of the OMS-E engine = 0.3 g"]
-[10.680319786071777, 1.056214690208435, "[TT] Size of the L 98-59d = Around 1.6 times Earth\u2019s size"]
-[9.272331237792969, 2.7751305103302, "[FF] Change Date of the ACE Realtime Solar Wind Lists = Feb. 21, 2015"]
-[10.215120315551758, 7.3015594482421875, "[TT] Field of Regard of the WPM = \u00b1 500 km"]
-[11.190326690673828, 0.6192461252212524, "[FF] Purpose of the CHEOPS = Search for transits of exoplanets by means of ultrahigh precision photometry on bright stars already known to host planets"]
-[7.841573238372803, 5.80461311340332, "[FF] Function of the ROLIS = Down-looking imager that acquires images during the descent and doubles as a multispectral close-up camera after the landing"]
-[10.911212921142578, 1.5434272289276123, "[TT] Size of the STARS-Me = 1U"]
-[9.377386093139648, 9.097936630249023, "[FF] Objective of the IRIS Imager = Provide multispectral imagery in the visible and near-infrared wavelength range"]
-[3.488438606262207, -0.8775452375411987, "[TT] Orbit of the WSF-M = Sunsynchronous orbit, LEO"]
-[9.631361961364746, 7.109951496124268, "[TT] Spatial Resolution (Playback Mode) of the OCM = 2.16 km"]
-[5.917438983917236, 2.4703972339630127, "[FF] Performing Teams of the Fundamental Physic Analyses = University of Alberta in Canada and the Technical University Delft in the Netherlands"]
-[7.506936073303223, 5.502883434295654, "[FF] Function of the OBA = Contains all of the instrument optical subassemblies"]
-[10.392045974731445, 2.153583526611328, "[TT] Sensitivity of the NuSTAR = High-energy X-rays"]
-[3.3942840099334717, 6.449124813079834, "[TT] Installation of the Antenna = In a cavity equal to half of a 4U standard volume (211 x 211 x 43 mm)"]
-[10.68649959564209, 3.335916042327881, "[FF] Objective of the RUBI = Investigate the fundamentals of boiling fluids in microgravity"]
-[7.695314407348633, 9.334977149963379, "[TT] Band Center Wavelength of the COCTS = 0.355 \u00b5m"]
-[5.358320236206055, 7.963006019592285, "[TT] Frequency/Phase of the DCG = 12 bit"]
-[8.006400108337402, 9.115496635437012, "[FF] Wavefront Planarity of the M2 = Not specified"]
-[4.469705104827881, 2.966557264328003, "[TT] Locations of the MSOCs = Halifax and Esquimalt"]
-[6.6321940422058105, 4.944084644317627, "[FF] Subsystems of the SVM = Thermal environment control, power generation and storage, orbit path control, payload data handling and transmission (PDHT)"]
-[5.90512228012085, 3.3837265968322754, "[TT] Number of Spacecraft of the GRACE-FO = 2"]
-[14.379448890686035, 3.1796984672546387, "[TT] Mass of the Rubin-2 = 10 kg"]
-[9.049150466918945, 5.369523048400879, "[TT] Axis of the MEMS device = 2-axis"]
-[8.703248023986816, 4.5823283195495605, "[FF] Sensors of the ADCS = Fine and coarse sun sensors, magnetometers, rate gyro"]
-[11.161259651184082, 5.176761627197266, "[TT] Sensor Size of the Sensor = 400 x 300 x 2"]
-[9.105405807495117, 3.4586410522460938, "[FF] Purpose of the GEOTAIL = Determine the overall plasma, electric and magnetic field characteristics of the distant and geomagnetic tail"]
-[4.4151716232299805, -1.6500145196914673, "[TT] Study Duration of the Blue Ring Nebula = 16 years"]
-[5.422699451446533, 6.003451347351074, "[TT] Onboard Computers RAM of the STRV-1b spacecraft = 128 kByte"]
-[5.411962985992432, 6.989003658294678, "[TT] Maximum Operating Speed of the DCU-S(TC) module = 128 kbit/s"]
-[7.242680549621582, 7.7793684005737305, "[TT] Threshold programmability of the PHA = Up to 6% of full scale"]
-[8.897967338562012, 4.3870086669921875, "[FF] Purpose of the Sun Sensors = Used for initial attitude acquisitions and other maneuvers"]
-[13.78168773651123, 5.340652942657471, "[TT] Solar cells type of the EPS = GaAs multijunction cell"]
-[5.353532791137695, 0.3505798578262329, "[TT] Launch Date of the Cheollian 2B = February 19"]
-[11.802519798278809, 5.511890888214111, "[TT] Nadir Footprint of the Instrument = 60 x 0.3 arcmin2"]
-[7.604648590087891, 8.615729331970215, "[TT] VIS (Reflective Bands) Calibration of the ABI = Yes"]
-[7.898126125335693, 2.1850032806396484, "[TT] IADP of the LI = 90% for latitude 45\u00ba, 70% as average over the FOV, 40% over EUMETSAT member states"]
-[4.906862258911133, 7.16184139251709, "[TT] Uplink Data Rate of the TT&C S-band Link = 64 kbit/s"]
-[14.330758094787598, 2.922942638397217, "[TT] Mass of the Global-6 = 55 kg"]
-[7.129819393157959, 6.775125026702881, "[FF] Beam Diameter of the Laser Beam = Not specified"]
-[9.553879737854004, 7.69084358215332, "[TT] Field of View of the HPT = 1.9 km x 1.4 km"]
-[5.104772567749023, 8.303547859191895, "[TT] Measurement Range of the MIS Instrument = 6 GHz to 183 GHz"]
-[4.364834785461426, 3.119429111480713, "[FF] Ground Stations of the XMM-Newton = Perth, Kourou, Villafranca, Santiago"]
-[5.37841796875, 3.151733875274658, "[TT] Manufacturer of the MethaneSAT = Ball Aerospace"]
-[5.878267288208008, 3.441798210144043, "[TT] Constellation Cost of the Lightspeed Satellites = $5 billion"]
-[5.853707313537598, 1.8113658428192139, "[TT] Launch Date of the Orion = 2017"]
-[6.899867534637451, 6.87100887298584, "[FF] Beam Directions of the BSC = Eight spot beam directions for each beam"]
-[4.153465270996094, 7.097209930419922, "[TT] Frequency Band of the Antenna System = X-band, S-band, L-band"]
-[8.500897407531738, 7.017864227294922, "[TT] Instrument type of the DMAC = High resolution optical imagers"]
-[5.883709907531738, 1.1273084878921509, "[TT] First-Light Measurement Date of the ICIR = June 6, 2017"]
-[11.113839149475098, 0.6384315490722656, "[FF] Heat Emission of the Magma Ocean Planets = Enough to be observed with the next generation of infrared telescopes"]
-[8.902464866638184, 6.247214317321777, "[TT] Viewing Technique of the SOLSE-2 = Limb-viewing"]
-[6.878354549407959, 7.524219989776611, "[TT] Resolution of the A/D Converter = 14 bit"]
-[4.969944000244141, 0.4644329845905304, "[FF] Launch Date of the Bartolomeo = June 2, 2016"]
-[6.717895030975342, 7.602031707763672, "[TT] Half-Power Beamwidth of the ECA = 120\u00ba"]
-[5.084506988525391, 8.210712432861328, "[TT] Radio frequency (GHz) of the VIRR = 0.49-0.94"]
-[7.698634624481201, 8.552850723266602, "[TT] Spectral Bands of the CZI = 4 bands in the VIS/NIR region"]
-[8.006792068481445, 2.4507455825805664, "[FF] Products of the AMSR3 = Brightness Temperature, Total Precipitable Water, Sea Surface Temperature, Sea Ice Motion Vector, Precipitation, Land Surface Temperature, Sea Surface Wind Speed, Soil Moisture Content, Vegetation Water Content, Sea Ice Concentration, Snow Depth"]
-[10.518379211425781, 2.2610414028167725, "[FF] Demonstration Date of the X-ray Navigation System = 11 Jan. 2018"]
-[4.655007839202881, 0.8078317642211914, "[TT] Launch Date of the Queqiao = May 21, 2018"]
-[6.692065238952637, 6.593024730682373, "[TT] Sub-contractor of the Laser Transmitter = TESAT"]
-[6.54376745223999, -0.4056163728237152, "[TT] Observation Time of the MOMS-2P = 3 minutes/day"]
-[5.354063510894775, 8.77434253692627, "[TT] Bandwidth of the AGRI = 0.45 \u00b5m - 13.8 \u00b5m"]
-[13.668012619018555, 2.923096179962158, "[TT] Mass of the Spacecraft = 1050 kg"]
-[10.696920394897461, 7.45639181137085, "[TT] Dynamic Range of Earth Background of the LI = 0 - 296.5 W/m 2 /\u00b5m/sr"]
-[6.408992767333984, 0.8570910096168518, "[TT] Monitoring Frequency of the Gaia = About 70 times"]
-[14.019048690795898, 7.159192085266113, "[TT] Voltage of the Operating voltage = 30 to 53 VDC"]
-[7.401774883270264, 3.8816733360290527, "[FF] Measurement of the GOE = Delays in GPS signals through the atmosphere"]
-[5.78527307510376, 3.2259135246276855, "[FF] Customer Industries of the Climavision = Delivery companies and airlines"]
-[6.724997043609619, 1.8458504676818848, "[FF] URL of the RHESSI = http://hesperia.gsfc.nasa.gov/hessi/news/aug_11_03.htm"]
-[7.070422649383545, 7.089993953704834, "[TT] Footprint Diameter of the Micropulse Laser Transmitter = 10 m"]
-[7.815329551696777, 2.009568452835083, "[FF] Data Distribution of the SeaSat = Geophysical data"]
-[5.427873134613037, 1.9344370365142822, "[TT] Development Status of the ABEX = In development"]
-[8.449398040771484, 8.018406867980957, "[TT] Spectral Band (MS B1) of the Pushbroom imager = 0.45-0.52 \u00b5m"]
-[5.675180912017822, 4.587473392486572, "[FF] Network Support and Space Operations Services of the GISTDA and NSPO = Provided to each other"]
-[7.52548360824585, 6.664228916168213, "[TT] Scanning Period of the Microbolometer Array = Up to 140 ms"]
-[7.167673587799072, 3.4157636165618896, "[FF] Number of Alerts Per Day of the LSST = Thousands"]
-[7.443065166473389, 2.989470958709717, "[TT] Instrument of the MethaneSAT = Spectrometers"]
-[10.735891342163086, 2.826343059539795, "[TT] Mission Design Life of the Microsatellite = \u2265 2 years"]
-[7.763697624206543, 6.598681926727295, "[TT] Full Disk Imaging Time of the AGRI = 15 minutes"]
-[6.276859283447266, 5.018623352050781, "[FF] Role Assignment of the OBDH = Assigned to a specific OBDH-board"]
-[7.417261600494385, 2.7259905338287354, "[FF] URL of the Terrestrial Imaging Spectroscopy Missions = doi:10.1109/IGARSS.2013.6723584"]
-[6.0451178550720215, 5.481701374053955, "[TT] Redundancy of the Avionics = Fully redundant"]
-[9.714643478393555, 7.820091724395752, "[TT] IFOV Resolution of the MWR = 50 km"]
-[13.836326599121094, 5.678998947143555, "[TT] Illumination Time of the Solar Panels = 65% of the time"]
-[14.070269584655762, 7.173975467681885, "[TT] Power Line Voltage of the eROSITA camera module = +27 V"]
-[10.938268661499023, 7.423349380493164, "[TT] Swath Widths of the RISAT = 10-225 km"]
-[6.957857608795166, -0.25550881028175354, "[TT] Orbits of the Odin = > 60,000"]
-[5.367066860198975, 0.31635767221450806, "[FF] Accident Date of the STS-107 = Feb. 1, 2003"]
-[2.994523763656616, 2.4476966857910156, "[FF] Data Usage of the Copernicus Sentinel-5P = Track and attribute methane emissions"]
-[8.89978313446045, 4.873064041137695, "[TT] Number of Sensors per Instrument of the PIMS = 2"]
-[3.588275909423828, 4.728107452392578, "[FF] Instrument type of the SAR (RISAT) = Imaging microwave radars"]
-[7.841690540313721, 3.0580344200134277, "[TT] December 2015 Value of the CO2 Concentration = 400.2 ppm"]
-[10.060006141662598, 3.0813021659851074, "[FF] Conference Presentation Date of the CubeSat TestBed 1 = Aug. 10-13, 2009"]
-[6.341677188873291, 5.665823459625244, "[TT] Operation of the BCR = Independent"]
-[6.204989910125732, 2.9648549556732178, "[TT] Resolution of the WorldView Legion = Sub 30 cm"]
-[7.505606174468994, 5.919971942901611, "[FF] Effect on Displacement Measurement of the Clock = Scales with distance"]
-[5.032655239105225, 0.7328237891197205, "[TT] Launch Date of the Hitomi = February 17, 2016"]
-[6.525475978851318, 6.84645938873291, "[FF] Performance Characteristics of the Small Optical Transponder (SOTA) = Unknown"]
-[3.3677444458007812, 4.849314212799072, "[FF] Civil SAR System of the SAR spacecraft = First of China"]
-[8.390419960021973, 7.410214424133301, "[TT] Frame Rate of the CMOSIS CHR70M Image Sensor = 0.5 frames per second"]
-[7.938327312469482, 8.735370635986328, "[TT] Spectral Range of the TROPOMI = Short Wave Infrared around 2.3 \u00b5m"]
-[10.567560195922852, -0.273131400346756, "[TT] Orbit Altitude of the TanDEM-X = 514 km"]
-[10.129461288452148, 6.457408428192139, "[TT] Aircraft Speed of the MABEL = ~200 m/s"]
-[6.440224647521973, 7.571482181549072, "[TT] Data Quantization of the MSU-100 = 8 bit"]
-[9.322312355041504, 3.229170322418213, "[FF] Occulter Mounting Requirement of the NIRCam coronagraph = The occulters must be rigidly mounted and must not interfere with imaging during non-coronagraphic observations, requiring placement outside the normal field of view"]
-[8.935730934143066, 2.868117094039917, "[FF] Relevance of the MinXSS mission = NSF Division of Atmospheric and Geospace Sciences (AGS)"]
-[13.482978820800781, 5.953165531158447, "[TT] Maximum Generation Voltage of the High-voltage solar array = Approximately 900 V"]
-[10.218217849731445, 5.636765956878662, "[FF] Temperature Control Zones of the AEM = Front tube of the COB, Equipment Box of the COB"]
-[9.788741111755371, 7.102576732635498, "[TT] Ground Coverage of the HRG Sensors = Minimum of 60 m"]
-[5.099442958831787, 1.8300480842590332, "[TT] Status of the DWSS = Canceled"]
-[5.476757049560547, 6.112593650817871, "[TT] Memory of the OBC = 16 MByte"]
-[6.907312393188477, -0.6743126511573792, "[TT] Orbital Period of the SZ-7 = 91 minutes"]
-[10.92296028137207, 5.657771110534668, "[TT] Heat Shield Layers of the MPO TCS = 2 layers of Nextel ceramic cloth, 11 aluminum layers"]
-[7.581578731536865, 8.851540565490723, "[TT] Max Radiance of the CZI = 12-40 mW cm-2 \u00b5m-1 sr-1"]
-[10.592073440551758, 5.026115894317627, "[TT] Probe Diameters of the Langmuir Probe = 5 cm and 1 cm"]
-[9.531120300292969, 6.18015193939209, "[TT] Angle of Incidence of the TopSAR wide = 20\u00b0 - 45\u00b0"]
-[7.6065592765808105, -2.5151236057281494, "[TT] Observation Date of the GOLD = Dec. 29, 2020"]
-[5.508052825927734, 1.6579947471618652, "[FF] Validation Scope of the KONNECT satellite = Complete end-to-end system of the new Spacebus Neo product line, including the fully electric orbit-raising phase"]
-[8.283086776733398, 0.960944414138794, "[FF] Size of the Vizca\u00edno Biosphere Reserve = Largest protected area in Mexico"]
-[13.738253593444824, 2.9707019329071045, "[TT] Total Weight of the GRACE-FO = Around 45 tons"]
-[7.949776649475098, 7.406456470489502, "[TT] Data Output of the TDI Detector = 58 Mpixel/s"]
-[7.453089714050293, 5.261057376861572, "[FF] Purpose of the Antenna Calibration Modes = Acquire information about the relative amplitude and phase of the secondary far-field patterns associated with pairs of feed elements/channels"]
-[11.121831893920898, 4.684807300567627, "[TT] Hold Distance of the Canadarm2 = 10 m"]
-[4.243689060211182, 7.181360244750977, "[TT] Frequency Band of the TT&C communications = S-band"]
-[5.654522895812988, 3.190480947494507, "[FF] Website of the GOCE = http://www.amptek.com/didm.html"]
-[7.354936599731445, 2.849994659423828, "[FF] Data Usage of the JAXA = Precipitation Monitoring"]
-[4.336026668548584, 6.244436264038086, "[FF] Unknown of the Z antenna = Unknown"]
-[6.47084903717041, 6.283115863800049, "[FF] Receiver Type of the Uplink Receiver = Optically pre-amplified direct detection receiver"]
-[5.5418171882629395, 7.108903408050537, "[TT] Data Rate of the Data Transmission Test = 18 Mbit/s"]
-[6.814273357391357, -0.3384256660938263, "[TT] Lunar Disk Presence in FOV of the PACE spacecraft = Nine minute period"]
-[7.763607025146484, 0.44718918204307556, "[FF] Orbit of the Lunar Icecube = Low-perigee, highly inclined lunar orbit"]
-[7.080958843231201, 4.691813945770264, "[TT] Mounting Location of the TRSR antenna = Upper right edge of the panel"]
-[8.490421295166016, 0.6222967505455017, "[FF] Mounting Orientation of the OPS systems = Not flat to the surface but shifted inside the body of MASCOT"]
-[6.319328784942627, 3.3101184368133545, "[TT] Number of 1-meter satellites in orbit of the BlackSky = Four"]
-[14.150851249694824, 3.274224042892456, "[TT] Ion Masses of the COSIMA = Above 28 Daltons"]
-[8.949706077575684, 7.179449558258057, "[TT] Imaging Resolution of the AlSat-1 = 32 m"]
-[9.670784950256348, 8.294074058532715, "[TT] Field of View (FOV) of the POLDER-P = \u00b1 43\u00b0 along track; \u00b1 51\u00b0 cross track"]
-[9.674694061279297, 1.3921875953674316, "[FF] Heliacal Rising Significance of the Pleiades = Marked the opening of seafaring and farming seasons"]
-[6.938912868499756, 9.048389434814453, "[TT] Band Center of the POLDER-1/2 = 865P nm"]
-[2.850872278213501, 0.0841195210814476, "[TT] J2000 declination (deg) of the GROJ1744-28 = -28.741"]
-[9.056812286376953, 7.020417213439941, "[TT] Limb-Viewing Section Cross-Track Resolution of the SIS = 0.4\u00ba per pixel"]
-[6.186862468719482, 2.5638651847839355, "[FF] Development Status of the Orion Vehicle = Unknown"]
-[8.518030166625977, 7.469202995300293, "[TT] CCD Cameras of the HJ-1B = 2"]
-[10.554645538330078, 6.488966464996338, "[TT] Mirror Module Assemblies Presenter of the IXPE = Brian Ramsey"]
-[13.611662864685059, 7.177015781402588, "[TT] Maximum Power (W) of the PS-2 = 5.5"]
-[4.845895767211914, 7.304854869842529, "[TT] Data Downlink Rate of the RF Communications = 20.8 Mbit/s"]
-[8.35552978515625, 7.911961078643799, "[TT] Array Size of the B1 Band = 4 x 4"]
-[7.970283508300781, -2.580322742462158, "[TT] Spectral Dispersion of the GOLD = 0.04 nm/pixel"]
-[3.320924758911133, 4.993103504180908, "[TT] Sensor of the TSX = X-band SAR sensor"]
-[6.235025882720947, 4.709300994873047, "[FF] Function of the Flight harness = Connecting satellite components and payload and for transmitting power, commands, and signals"]
-[6.211432933807373, 2.3911936283111572, "[FF] Target Audience of the MoonKAM = Fifth- to eighth-grade students"]
-[9.240030288696289, 3.3947415351867676, "[FF] Objective of the SGPS = Measure the solar and galactic protons found in the Earth's magnetosphere"]
-[12.205536842346191, -0.22534090280532837, "[TT] Imaging Frequency of the TESS = Every 30 minutes"]
-[6.381404399871826, -0.621886670589447, "[TT] Period of the NEMO-AM = 97.4 minutes"]
-[8.407137870788574, 7.32603120803833, "[TT] Cumulative Imaging Capability of the MBA detector = x 40"]
-[3.459956407546997, 2.3767385482788086, "[FF] Responsibilities of the Payload Data Ground Segment (PDGS) = Payload and downlink planning, data acquisition, processing, archiving and downstream distribution of the Sentinel-2 satellite data"]
-[6.688289165496826, 4.570206165313721, "[FF] Purpose of the MFD = Evaluate the operation of the SFA (Small Fine Arm)"]
-[7.8042426109313965, 8.474905014038086, "[FF] Bands of the Spectral Bands = SWIR, MWIR, TIR"]
-[8.717784881591797, 7.627621650695801, "[TT] 1.378, 2.25, 3.9, 6.185, 6.95, 7.34, 8.5, 9.61, 10.35, 11.2, 12.3, and 13.3 \u00b5m channels of the Frame-to-Frame Registration = \u00b121 \u00b5rad"]
-[10.622270584106445, 5.03897762298584, "[FF] Electron Suppression of the CuPID Sweeping Magnets and Filter System = More than protons"]
-[4.268826484680176, 0.8450693488121033, "[FF] Announcement Date of the EDRS-C Satellite = Sept. 22, 2011"]
-[9.640673637390137, -1.4254701137542725, "[TT] Impact Location of the SMART-1 = 34.262\u00b0 south, 46.193\u00b0 west"]
-[5.024624347686768, 0.9352678656578064, "[TT] Launch Date of the GIOVE = December 28, 2005"]
-[6.504566192626953, 3.7348382472991943, "[FF] Design Principle of the RemoveDebris platform = Accommodates the majority of the platform avionics and equipments in the lower half of the spacecraft, with the upper half of the spacecraft primarily dedicated to accommodating the RemoveDebris payloads"]
-[5.118228912353516, 7.0142436027526855, "[TT] Regenerative Mode Uplink of the Communication Modes = 1.5, 6, 24, 51, or 155 Mbit/s"]
-[13.9544038772583, 2.7421178817749023, "[TT] Launch Mass of the INSAT-3D = ~2060 kg"]
-[8.226068496704102, 6.480356693267822, "[TT] Ground Footprint of the ATLAS instrument = 10 m"]
-[6.710844039916992, -0.5478318929672241, "[TT] Recurrent Period of the ADEOS-II = 4 days"]
-[6.013303279876709, 0.8397969007492065, "[TT] Image Capture Date of the MERIS = April 2, 2012"]
-[9.624604225158691, 8.12820053100586, "[TT] Number of Lenses of the TOU = 6"]
-[9.406073570251465, 5.036900520324707, "[TT] Roll Motion Range of the GF-2 spacecraft = \u00b135\u00ba"]
-[4.353686809539795, 1.62983238697052, "[FF] Launch Date of the ROCSat-1 = Unknown"]
-[8.747307777404785, 4.979254245758057, "[TT] Field of View of the Star Tracker = ~15\u00ba"]
-[3.618356704711914, 4.133205890655518, "[FF] Data Applications of the NISAR = Monitoring of agricultural biomass, assessing disasters, studying snow and glaciers, studying Indian coastal and near-shore oceans"]
-[4.34981107711792, 6.438975811004639, "[FF] Drum Rotation of the MTVZA-GY Antenna System = Continuous"]
-[14.25274658203125, 3.2760024070739746, "[TT] Mass of the MSI = 44 kg"]
-[14.647379875183105, 6.680071830749512, "[TT] Li-ion Battery Capacity of the EPS = 15 Ah BOL"]
-[13.820773124694824, 3.722381114959717, "[TT] Mass of the Orbital Reflector = 4 kg"]
-[6.218993186950684, 1.2200905084609985, "[FF] Announcement Date of the Photon Sieve = June 4, 2012"]
-[5.718757629394531, 4.364317417144775, "[FF] Hosted Payload of the EDRS-C Satellite = Unknown"]
-[11.31543254852295, 5.766310214996338, "[TT] Components of the COPV = Aluminum inner liner with a carbon over-wrap"]
-[7.620590686798096, 7.1820783615112305, "[TT] Frame Rate of the ROIC/FPA = 16 kHz"]
-[5.310435771942139, 2.163533926010132, "[TT] Agency of the CryoSat = ESA"]
-[8.432973861694336, 1.19548499584198, "[TT] Quantization Levels of the Land surface temperature = 1"]
-[9.12967586517334, 2.7944719791412354, "[FF] URL of the Submerged Sources of Transient Acoustic Emission from Solar Flares = https://iopscience.iop.org/article/10.3847/2041-8213/abad2a/pdf"]
-[8.822096824645996, 8.444292068481445, "[TT] Pixel Sampling FWHM of the Instrument = \u22652"]
-[7.654931545257568, -0.5163057446479797, "[TT] Operation Start Date of the ICE-Cubes facility = December"]
-[6.341958522796631, 1.4510630369186401, "[TT] Integration Time of the eROSITA = About one day"]
-[8.026752471923828, 2.9185400009155273, "[FF] Measurement Capability of the DIAL Instrument = Range-resolved and column amounts of atmospheric CO2, high-resolution aerosol profiles, cloud distributions"]
-[9.004143714904785, 2.734675168991089, "[FF] URL of the Can ripples on the sun help predict solar flares? = https://news.berkeley.edu/2020/09/21/can-ripples-on-the-sun-help-predict-solar-flares/"]
-[14.203399658203125, 3.269864797592163, "[TT] Mass of the FLP = 120 kg"]
-[9.590853691101074, 6.755458831787109, "[TT] Diameter of the Ceres = 950 km"]
-[9.482213973999023, 6.669581890106201, "[TT] Azimuth Resolution of the Wide standard Quad-Pol = 7.6 m"]
-[7.653905868530273, 2.108100414276123, "[TT] Total Coverage Area of the RASAT = 4,650,000 km2"]
-[9.75879192352295, 7.49005651473999, "[TT] Ground Sample Distance (GSD) - Dual Image Mode of the PAN Band = 3.5 m x 3.5 m"]
-[7.295921802520752, 4.8379011154174805, "[FF] Operation Mode of the ASAR = High-rate mode"]
-[8.28171443939209, 5.705446720123291, "[FF] Pointing Information of the MWI = TLE-based"]
-[4.866772174835205, 5.56370210647583, "[TT] Frequency Band of the Receiver = GPS L1: 1575.42 MHz, GPS L2: 1227.6 MHz"]
-[10.558168411254883, 1.9539953470230103, "[FF] Energy Source of the Pulsar = Emission seen by all three telescopes"]
-[8.903475761413574, 0.11548598110675812, "[TT] Location of the Cendrillon = Eastern Hemisphere near the meridian"]
-[8.536745071411133, 5.064303874969482, "[TT] Number of Accelerometers of the SloshSat = 6"]
-[8.569454193115234, 8.609169960021973, "[TT] Instantaneous spectral coverage of the Spectrometer = 1.06 km/s"]
-[7.45405912399292, 7.925204753875732, "[TT] Dynamic Range of the Instrument = 180 K - 400 K"]
-[10.218722343444824, 7.552661418914795, "[TT] Telescope Type of the TIR Subsystem = Newtonian catadioptric system with aspheric primary mirror and lenses for aberration correction"]
-[6.82503604888916, 5.809087753295898, "[TT] Number Assembled of the HISats = Over 100"]
-[7.139363765716553, 3.7679450511932373, "[FF] Formation Flying of the PROBA-3/ASPIICS = Complete Metrology"]
-[3.6516528129577637, 6.527613162994385, "[TT] Antenna Type of the L-band spaceborne radiometer = Parabolic cylinder reflector antenna"]
-[5.975819110870361, -0.38267242908477783, "[TT] Duration of the Station Keeping = 15+ years"]
-[9.513571739196777, 4.501018047332764, "[FF] Measurement of the SSAS = Spin rate"]
-[8.22026252746582, 1.1507964134216309, "[TT] Range of values of the Soil moisture = 0-60%"]
-[6.099459648132324, 5.974880695343018, "[TT] Number of Modules of the CCB = 5"]
-[6.8846869468688965, 1.739989161491394, "[FF] URL of the James Webb Space Telescope = http://ircamera.as.arizona.edu/MIRI/miricooler.pdf"]
-[10.354832649230957, 1.7569252252578735, "[FF] Science Goals of the NuSTAR = Locate massive black holes, Study the population of compact objects in the Galaxy, Understand explosion dynamics and nucleosynthesis in core collapse and Type Ia SNe, Constrain particle acceleration in relativistic jets in supermassive black holes"]
-[12.726594924926758, 3.894252300262451, "[FF] Magnetic Reconnection of the Magnetospheric Cusps = Occurs at one or more places along the dayside magnetopause"]
-[8.245756149291992, 6.9253621101379395, "[FF] Type of the WPM = Multispectral and Panchromatic Wide-Scan Camera"]
-[6.820377826690674, 0.5252763628959656, "[TT] Onboard Software Reset of the Kepler = Five-day break in science data collection"]
-[4.611001968383789, 2.7168080806732178, "[FF] Direction of the Japan Current = South"]
-[13.81070327758789, 2.636099338531494, "[TT] Launch Mass of the IMP-8 = 410 kg"]
-[10.248098373413086, 8.39145278930664, "[FF] Pupil Diameter of the NAOMI = No longer sized to comply with SNR requirements"]
-[4.640101909637451, 2.5399160385131836, "[TT] Location of the Wetlands = Iran's border with Afghanistan"]
-[10.154178619384766, -2.764759063720703, "[TT] Device capacity of the SLC NAND-FMM = 32 Gbit"]
-[13.618523597717285, 1.7719340324401855, "[TT] Payload Mass of the SpaceX CRS-13 Dragon = 2205 kg"]
-[5.101768493652344, 7.593396186828613, "[TT] G/T of the Antenna = >13.5dB/K"]
-[9.01722240447998, 6.470657825469971, "[FF] Image Center Coordinates of the CaSSIS = 28.36\u00baS/79.75\u00baE"]
-[4.270905017852783, 7.281195163726807, "[TT] Frequency of the RF communications = S-band"]
-[3.2895450592041016, 1.8780571222305298, "[FF] Image Content of the Sentinel-2C = A portion of the northwest coast of Poland"]
-[9.808917045593262, 7.369750499725342, "[TT] Ground Sample Distance of the PamCam = Around 200 m"]
-[10.692716598510742, 3.4180712699890137, "[TT] Configuration of the 6U CubeSat = 6U"]
-[11.978252410888672, 2.9815785884857178, "[TT] Hydrazine Thrusters of the PARASOL microsatellite = Four 1 N thrusters"]
-[8.851201057434082, 4.643575668334961, "[TT] Attitude Determination Device of the ACS = Commercial star tracker, AST (Autonomous Star Tracker)"]
-[5.6024699211120605, 0.8388650417327881, "[TT] Operation End Date of the ERBS satellite = Summer of 2005"]
-[7.95993709564209, -0.9920430779457092, "[FF] Next Step of the ICESat-2 = Building a statistical model"]
-[5.967501163482666, 0.24458374083042145, "[TT] Operation Period of the Rosetta = August 2014 to September 2016"]
-[5.342230796813965, 3.9707725048065186, "[TT] Number of Satellites of the Transport Layer Tranche 1 = 42"]
-[9.710930824279785, 8.328936576843262, "[TT] FOV in Cross-Track Direction of the MSU-50 = 31\u00ba, 62\u00ba"]
-[10.870530128479004, -0.3165789842605591, "[TT] Mission Observation Period of the TanDEM-X = 21 September 2017 until June 2020"]
-[7.242015361785889, 2.4377405643463135, "[FF] Uninterrupted Earth Coverage of the MEO Orbit = Attractive for a number of observation services"]
-[5.090383529663086, 3.2747621536254883, "[TT] Manufacturer of the Beijing-1 = SSTL"]
-[9.81537914276123, 2.5916481018066406, "[TT] Detection Area of the Solar X-ray monitor = 0.75 mm2"]
-[6.526230812072754, -1.2519525289535522, "[FF] Data Gap of the GRACE-FO = Minimizing any data gap after GRACE"]
-[5.183464050292969, 3.295219898223877, "[TT] Project Name of the XI-IV = XI-IV"]
-[10.94347858428955, 4.026321887969971, "[TT] Shape of the Drag Sail Modules = Wedge-shaped"]
-[12.259565353393555, 2.965543746948242, "[TT] Hydrazine Usage of the SPOT-4 = 2.8 kg"]
-[10.19502067565918, 5.695127964019775, "[TT] Required Detector Temperature of the TCS (Thermal Control Subsystem) = Less than 95 K"]
-[9.779485702514648, 0.9706147313117981, "[TT] Contamination Distance of the Sun and Galactic Glint = Up to 1000 km from the coastlines"]
-[7.18269157409668, 1.8937063217163086, "[TT] Operational Status of the Carbonite-1 = Still operational after two years"]
-[4.774847507476807, -1.4692292213439941, "[TT] Landing Date of the Tianwen-1 = May 15, 2021"]
-[4.558496475219727, 5.8514275550842285, "[TT] Population of the 406 MHz Beacons = Projected to reach one million by the end of 2010"]
-[7.86836576461792, 7.395568370819092, "[TT] Data Rate of the TDI Detector = 3.5 Gbit/s total"]
-[9.548699378967285, 0.8487637042999268, "[TT] Closest Approach Distance of the Solar Orbiter = 460 km"]
-[10.037976264953613, -1.601521611213684, "[TT] Inclination of the Tsubame = 97.4\u00ba"]
-[7.845041275024414, 3.8138065338134766, "[FF] Range Measurement of the GFO-RA = Between satellite and subsatellite point (at nadir) of the orbit"]
-[14.7103271484375, 6.615180969238281, "[TT] Capacity of the Lithium-ion Polymer Batteries = 1.2 Ahr"]
-[6.795502662658691, 4.061887741088867, "[FF] Anomaly Resolution of the DMSP-19 = Closed"]
-[6.9562883377075195, 6.137895107269287, "[TT] Number of Instruments of the AMSU-B = 3"]
-[8.479985237121582, 0.962672233581543, "[TT] Quantization levels of the Snow water content = 1"]
-[8.615330696105957, 3.0297694206237793, "[FF] Observation of the MAHRSI = Nitric Oxide in the Mesosphere and Lower Thermosphere"]
-[5.721011161804199, 0.5791099071502686, "[TT] Data Collection Time of the AMS-02 = 18 years"]
-[8.074750900268555, 3.6547882556915283, "[TT] Target Observation Frequency of the OCO-2 = Roughly once each day"]
-[11.060005187988281, 5.226395130157471, "[FF] Size of the Micro Cold Traps = Smaller than 1 meter"]
-[9.649317741394043, 8.149433135986328, "[TT] Degrees-of-freedom of the Active Optics = 6"]
-[9.528830528259277, 0.5937998294830322, "[TT] Distance from Earth of the Vigil = 1.5 million km"]
-[13.896602630615234, 3.0957412719726562, "[FF] Mass of the nCube-1 = Unknown"]
-[12.076024055480957, 6.339911460876465, "[FF] Positron Fraction of the AMS = Precision measurements"]
-[8.994884490966797, 10.24733829498291, "[TT] Pixel Resolution of the SPIM1 = 14 bit"]
-[3.0679497718811035, 4.390108585357666, "[TT] Geometric Resolution of the TerraSAR-X = Up to 0.25 m"]
-[14.070792198181152, 4.013483047485352, "[TT] Mass of the Total Instrument = 171 kg"]
-[7.653328895568848, 2.9704113006591797, "[FF] Mission of the GOSAT-2 = Provide observation data to environmental administrations and drive international anti-global warming efforts"]
-[5.347159385681152, 2.1848604679107666, "[FF] Mission Goal of the HORYU-2 = Contributing to the local educational program for elementary and junior high school students"]
-[4.922893047332764, 3.1370737552642822, "[TT] Prime Contractor of the S/C = EADS Astrium Ltd."]
-[8.398781776428223, 0.677625298500061, "[TT] Water Level of the Desna River = 5 meters below normal"]
-[10.131815910339355, -1.552066445350647, "[TT] Inclination of the Landsat 9 = 98.2\u00ba"]
-[10.736505508422852, 2.862550735473633, "[FF] Intersatellite Link of the CM1 and CM2 = In LEO"]
-[5.164639472961426, 2.7213094234466553, "[TT] Affiliation of the Harrison Agrusa = University of Maryland"]
-[10.399773597717285, 4.066800594329834, "[TT] Boom Length of the SOSMAG = 1m"]
-[8.564596176147461, 6.165637493133545, "[TT] Accuracy of the PREMOS = \u00b10.4 W/m2 or \u00b1290 ppm"]
-[14.201488494873047, 3.1600911617279053, "[TT] Mass of the FTS-2 = 225 kg"]
-[6.493463516235352, -0.4995144009590149, "[TT] Period of the Anand = 94.6 minutes"]
-[9.935406684875488, 4.156860828399658, "[TT] Search Coil Mass of the ULF Sensor = 2 kg"]
-[10.333670616149902, 2.135467767715454, "[TT] Detection of the \"NuSTAR\" = Unexpected periodic pulsed emissions"]
-[4.412265777587891, 3.0687966346740723, "[TT] Location of the RBU = Fairmont, WV"]
-[7.454807758331299, 4.758480072021484, "[FF] Data Output Modes of the OLS sensor system = L data, T data, TF data, LF data, TS, LS"]
-[9.232551574707031, 3.238208770751953, "[FF] Camera of the Occulter satellite = Looking out for pulsing LEDs on the Coronagraph"]
-[3.9136803150177, 6.327171802520752, "[TT] Number of Antennas of the ADM = 2"]
-[7.229340553283691, 7.838390350341797, "[TT] Differential non-linearity of the PHA = <1%"]
-[10.019011497497559, 4.068887710571289, "[TT] Location of the USU magnetoresistive magnetometer = At the base of the boom"]
-[4.431553363800049, 3.3353660106658936, "[TT] Ground Segment Location of the RISAT-1 = MOX (Mission Operations Complex) of ISTRAC (ISRO Telemetry, Tracking and Command Network), Bangalore"]
-[5.306602478027344, 8.121502876281738, "[TT] VLF Frequency Range of the IME = Few Hz to 20 kHz"]
-[9.177629470825195, 8.346938133239746, "[TT] Stages of the Optics = Front and back to the spectral filter"]
-[11.421229362487793, 3.4984939098358154, "[TT] Relative Position Determination of the CNAPS = 10 cm"]
-[8.019233703613281, 8.03343391418457, "[TT] Sensor Payloads of the Gen-3 Satellite = Dual optical-infrared sensor payloads"]
-[8.582918167114258, 2.7898216247558594, "[TT] Altitude Range of the Air Density Measurement Device = ~200 km"]
-[4.7208170890808105, 5.43952751159668, "[FF] Beacon Detection of the Ground System = At least one beacon per pass"]
-[5.287110328674316, 0.8546167016029358, "[FF] Online Availability Date of the TRUTHS = 13 February 2004"]
-[6.870601654052734, 5.981799125671387, "[TT] Quantity of the SMEs = 13"]
-[8.044384002685547, -0.981612503528595, "[TT] Data Collection of the ICESat-2 = Open water in the cracks between the ice floes, called leads"]
-[4.61794900894165, 6.431191444396973, "[FF] Purpose of the JY1-Sat = Carry a UHF/VHF amateur radio"]
-[8.16077709197998, -0.8422420620918274, "[FF] Mission of the CRISTAL = Measure and monitor sea-ice thickness, overlying snow depth and ice-sheet elevations"]
-[13.202573776245117, 7.3356757164001465, "[TT] Power Consumption (Receive Mode) of the NSX = 6 W"]
-[6.33701229095459, -0.0707995668053627, "[TT] SSS Temporal Sampling Period of the CIMR = Once per month"]
-[13.867718696594238, 7.274429798126221, "[TT] Power Input of the CU = 6-36 VDC"]
-[6.3427252769470215, 4.541159629821777, "[FF] Features of the AutoCon = Fuzzy logic decision making capabilities, natural language resolution of conflicting constraints, scripting environment, flight wrapper interfaces, multiple operating modes, generic closed-loop formation flying control algorithms, modular architecture design"]
-[8.406927108764648, 1.9656518697738647, "[TT] Spatial Resolution (km) of the Cloud amount = 25"]
-[7.758260726928711, 8.758323669433594, "[TT] Spectral Range of the DNB = 0.5-0.9 \u00b5m"]
-[6.704957485198975, 4.694627285003662, "[FF] Function of the FC = Spacecraft controller"]
-[5.286102294921875, 5.6131391525268555, "[TT] Communication Interface of the ROSA = MIL-STD-1553"]
-[5.833109378814697, 1.202781081199646, "[TT] Jettison Date of the ROSA = June 26, 2017"]
-[11.006990432739258, 2.9391980171203613, "[TT] Solar Array of the PSSCT Nanosatellite = 4-cell"]
-[9.859304428100586, 4.484216690063477, "[TT] Attitude Control of the SporeSat = Permanent magnets and hysteresis rods"]
-[5.128012180328369, 0.5737935900688171, "[TT] Operational Start Date of the RASAT = Start of 2012"]
-[4.709548473358154, 7.0700225830078125, "[TT] Downlink Data Rate of the X-band = 30 Mbit/s"]
-[8.569990158081055, 0.25857990980148315, "[TT] Non-Group Comet Sightings Frequency of the SOHO = A few times a year"]
-[6.739442825317383, 5.417471885681152, "[FF] Components of the Prototype Channelizer = A/D converters, de-multiplexers, switches, multiplexers, D/A converters, and control unit"]
-[7.545978546142578, 2.291520357131958, "[FF] Monitoring Capability of the Offshore Platform in the Gulf of Mexico = Systematic monitoring of emissions"]
-[11.315145492553711, 0.9429329037666321, "[TT] Joint Operations Duration of the LISA Pathfinder = 30 days"]
-[11.384588241577148, 4.420284271240234, "[TT] Size of the CXBN = 2U"]
-[5.784389019012451, 2.6028599739074707, "[FF] Developers of the SoloHI = Russell A. Howard, Angelos Vourlidas, Clarence M. Korendyke, Simon P. Plunkett, Michael T. Carter, Dennis Wang, Nathan Rich, Donald R. McMullin, Sean Lynch, Adam Thurn,; Greg Clifford, Dennis G. Socker, Arnaud F. Thernisien, Damien Chua, Mark G. Linton, David Keller, James R. Janesick, John Tower, Mark Grygon, Robert Hagood , William Bast, Paulett C. Liewer, Eric M. DeJong, Marco M. C. Velli, Zoran Mikic, Volker Bothmer, Pierre Rochus, Jean-Philippe Halain, Philippe L. Lamy"]
-[5.717662811279297, -0.487912118434906, "[TT] Mission Lifetime of the EDRS-A hosted payload = 15 years"]
-[5.246845722198486, 2.078707695007324, "[TT] Mission Status of the Satellite = Planned"]
-[8.960908889770508, 9.395987510681152, "[TT] Spatial resolution of the TANSO-CAI = 1 km"]
-[3.30778169631958, 2.301513195037842, "[FF] Level 0 Products of the Sentinel-6 = Raw data after restoration of the chronological sequence for each instrument and removal of data overlaps at dump boundaries and relevant quality flags related to the reception and decoding"]
-[5.014752388000488, 6.931163787841797, "[TT] Data Rate of the DVB-S2 CCSDS telemetry standard = Lower and also higher than 100 Mbit/s"]
-[9.408095359802246, 5.575284957885742, "[TT] Longitude Range for Surface Target Detection of the TanSat = -86\u00b0 to 79\u00b0"]
-[6.941954135894775, 3.3920845985412598, "[FF] Purpose of the BEAT experiment = Measure an astronaut\u2019s ballistocardiographic data, including pulse and blood pressure"]
-[10.146212577819824, 1.1250627040863037, "[TT] Distance from Earth of the M33 galaxy = Three million light years"]
-[6.864763259887695, 6.496882438659668, "[FF] Type of the Laser Communication Terminal = Unknown"]
-[10.820908546447754, -0.29175305366516113, "[FF] Observation Date of the TWINS-LAD = Feb. 27-31, 2006"]
-[8.286847114562988, 5.110971450805664, "[FF] Function of the SES = Confirm the energy resolution and measurement noise are unaffected by changes in light level and temperature"]
-[9.533225059509277, 7.132802963256836, "[TT] Resolution (IR) of the VHRR = 11 km"]
-[10.777729034423828, -1.1389104127883911, "[FF] Atmospheric Drag of the SLATS = Estimated to be greater than the actual one"]
-[9.300870895385742, 2.2246010303497314, "[TT] Most Powerful Auroras of the Jupiter = Yes"]
-[3.8944976329803467, 6.3329596519470215, "[TT] Antenna Quantity of the RF communications = 4"]
-[6.608829975128174, 4.101204872131348, "[FF] Overview of the Ground Segment = Unknown"]
-[8.20395278930664, 5.508984565734863, "[TT] Inversion Rate Validity Criterion of the RISAT-1 = 5%"]
-[5.9758687019348145, 1.2678921222686768, "[FF] Date of the NASA Earth Science Senior Review 2011 = June 30, 2011"]
-[4.849743366241455, 0.45245492458343506, "[TT] Launch Date of the EMIT = 2022"]
-[6.7767014503479, 4.071195602416992, "[FF] Power Failure of the DMSP-19 = Within the command and control system"]
-[4.728577613830566, 0.7760891318321228, "[TT] Launch Date of the PROBA-1 = 22 October 2001"]
-[8.062409400939941, 6.247833728790283, "[FF] Type of the SBUV = Double Ebert-Fastie spectrometer and filter photometer"]
-[8.75588321685791, 4.0885329246521, "[FF] Components of the KSEM = Particle Detector (PD), Magnetometer (MAG), and a Satellite Charging Monitor (SCM)"]
-[13.504461288452148, 5.474236011505127, "[TT] Number of Cells per String of the Solar Array = 7"]
-[7.322278022766113, 6.368631362915039, "[TT] Data Update Frequency of the IMERG = Every half-hour"]
-[6.833799839019775, 5.103968620300293, "[FF] Components of the SMS = Versatile onboard computer(SpaceCube2), Telemetry/Command interface module, SpaceWire router, Network data recorder, Standard middleware, Software development kit"]
-[3.1291728019714355, 1.7436940670013428, "[TT] Mode of the Sentinel-1 = Complete coverage of Earth in six days"]
-[6.969863414764404, 4.1780877113342285, "[FF] Design of the CST-100 spacecraft = Baseline design"]
-[2.944204807281494, 2.381990432739258, "[FF] Purpose of the Sentinel-5P = Deliver a key set of atmospheric composition, cloud and aerosol data products for air quality and climate applications"]
-[4.861637115478516, 0.5313025712966919, "[TT] Launch Date of the ProSEDS = 2003"]
-[6.9813642501831055, -0.7933282256126404, "[TT] Orbital Period of the TOI-148, TOI-587, TOI-681, TOI-746, TOI-1213 = 5 to 27 days"]
-[10.21346378326416, 5.757743835449219, "[TT] Operating Temperature of the Detector = < 60\u00baC"]
-[4.625511169433594, 0.9708775281906128, "[TT] Establishment Year of the GSA = 2004"]
-[9.648880958557129, 8.35557746887207, "[TT] Field of View of the MiniCOR = 60% of the C3 FOV"]
-[6.621440887451172, 5.663047790527344, "[TT] Quantity of the Secondary Payloads = 30"]
-[10.038610458374023, 2.9038751125335693, "[FF] Pilot Program Start Date of the CubeSat = Nov. 10, 2010"]
-[9.985013008117676, -1.4630800485610962, "[FF] Transition Orbit Inclination of the LUMIO = Lies within the parking orbit bounds"]
-[9.99503231048584, 2.9176597595214844, "[FF] Update Date of the CubeSats = 07 February 2018"]
-[8.889724731445312, 7.994805335998535, "[TT] Focal Plane Array of the NIRST = 512 x 3 pixel microbolometer focal plane array (FPA)"]
-[5.443765163421631, 5.249614715576172, "[TT] Data Handling System of the EDSN = Nexus S smartphone"]
-[11.435259819030762, 5.810115814208984, "[FF] Wafer Material of the Collector Array = Silicon, aluminum, gold foils"]
-[4.981295585632324, 0.356729120016098, "[TT] Commercial Operation Start Date of the Hiber = Q1 2019"]
-[11.960861206054688, 4.999919891357422, "[TT] Size of the OCM = 701 mm x 527 mm x 470 mm"]
-[6.791931629180908, 1.981828212738037, "[FF] Global browse of the Biosphere = 500 m global browse mosaic"]
-[9.367015838623047, 3.980053186416626, "[TT] Frequency Range of the Plasma Wave Instrument = 5 Hz - 800 kHz"]
-[7.53670072555542, 4.56621789932251, "[FF] Calibration Performance of the VIIRS = Continuously Assessed"]
-[9.954998016357422, 7.011384963989258, "[TT] Height Coverage of the Sensor = Up to about 32 km"]
-[5.765797138214111, 2.0497210025787354, "[FF] TRL of the P3RVX = Technology Readiness Level"]
-[13.00279712677002, 7.021657943725586, "[TT] Thermal Control Power Requirement of the WCOM = 50 W"]
-[7.027358531951904, 7.075581073760986, "[TT] Pulse Width of the Lasers = 1 to 6 ms"]
-[5.746547698974609, 4.180449485778809, "[FF] Business Focus of the Lacuna Space = IoT (Internet of Things)"]
-[14.099811553955078, 3.9422905445098877, "[TT] Instrument Mass of the MSU-E = 17 kg"]
-[7.0408759117126465, 3.3051092624664307, "[FF] Product Sectorization Parameters of the GS PD element = Geographic coordinate corner points, Map projection, Spatial resolution, Bit depth, ABI channel, Periodicity"]
-[8.35530948638916, -0.898967981338501, "[FF] Off-nadir Angle of the ICESat = 0.3\u00ba"]
-[11.147757530212402, 2.257617950439453, "[FF] Main Tank Replenishing Procedure of the XMM-Newton = Under development"]
-[6.703284740447998, -0.36205899715423584, "[TT] Measurement Datation of the Satellite = \u00b1100 \u03bcs with respect to UTC"]
-[9.278421401977539, 3.240609884262085, "[FF] Function of the Solar-Wind Monitors = Monitor solar wind"]
-[5.851089954376221, 3.1421921253204346, "[FF] Number of Spaceships of the Soyuz MS-18 = 1"]
-[9.512991905212402, 1.127807378768921, "[FF] Shock Wave Speed of the Tycho = Millions of miles per hour"]
-[13.843701362609863, 2.6781463623046875, "[TT] Weight of the Launch Abort System = 410 kg"]
-[9.40097713470459, 7.9458537101745605, "[TT] Optics Lens of the NEA Scout Camera = Ruggedized commercial lens"]
-[8.719895362854004, 7.651700019836426, "[TT] Pixel Size of the Detector = 15 \u00b5m"]
-[11.428115844726562, 5.239526271820068, "[TT] Effective Collecting Area of the OLS = 185 cm2"]
-[5.740316867828369, 2.598208427429199, "[FF] Developers of the FLEX = J. Vicent, N. Sabater, C. Tenjo, J. Acarreta, M. Manzano, J. Rivera, P. Jurado, R. Franco, L. Alonso, J. Verrelst, J. Moreno"]
-[6.81953763961792, -0.5016431212425232, "[TT] Repeat Cycle of the Satellite Orbit = 17 days"]
-[9.703943252563477, 7.921388149261475, "[TT] FOV of the HRI Lyman-\u03b1 1216 \u00c5 = 1000 arcsec x 1000 arcsec"]
-[8.240252494812012, 0.4935719072818756, "[FF] Location of the Ceres = Asteroid belt, between the orbits of Mars and Jupiter"]
-[9.358397483825684, 6.255959510803223, "[TT] Azimuth Extent of the HRS = Up to 100 km"]
-[14.003067970275879, 7.1683197021484375, "[TT] Voltage of the Power Storage = 1.2 V"]
-[12.121506690979004, 6.176078796386719, "[TT] Particles Collected of the AMS-02 = 100 billion"]
-[7.9072370529174805, 5.503287315368652, "[FF] Components of the PowerCell = 48-segment 3-color optical density or absorbance measurement system, grow light system, microfluidic system for nutrient delivery and waste flushing, thermal control and internal environmental sensing including temperature, pressure, humidity, and acceleration"]
-[5.679563045501709, 2.2563304901123047, "[FF] Team Size of the ATMS = 100 people"]
-[10.960991859436035, 5.179789066314697, "[TT] Apoherm of the MMO = 12,000 km"]
-[7.930726528167725, 6.38745641708374, "[TT] Operation Mode of the RDSA = Along-track imaging (default mode)"]
-[5.8018364906311035, -0.37099525332450867, "[TT] Heritage Deployment Duration of the RBA = Over long periods (hours)"]
-[11.52796745300293, 5.1464738845825195, "[TT] Surface Area of the SDS = 1 m2"]
-[8.081543922424316, 2.6902670860290527, "[TT] Measurement Domain of the JERS-1 = Land, Snow & Ice"]
-[6.745403289794922, -0.3756016194820404, "[TT] Observation Timescales of the Harmony = Tens of milliseconds to years"]
-[13.794548988342285, 2.891774892807007, "[TT] Lift-off Mass of the GSLV-F05 = 415.2 tons"]
-[10.663500785827637, -0.12109788507223129, "[TT] Formation Distance of the TanDEM-X and TerraSAR-X = 20 km"]
-[10.099648475646973, 5.95483922958374, "[TT] CCD Detector Temperature of the CHEOPS = 233 K"]
-[3.441894054412842, -0.9193903803825378, "[TT] Orbit Type of the Satellite = Sun-synchronous near-polar circular orbit"]
-[4.904576301574707, 8.238903999328613, "[TT] Frequency Range of the AMSR = 6.9-89 GHz"]
-[10.036043167114258, -1.5105634927749634, "[TT] Orbit Inclination of the Light-1 = 51.6\u00b0"]
-[3.93537974357605, 9.717560768127441, "[TT] Frequency (GHz) of the ICI-8 = 448\u00b17.2"]
-[13.664058685302734, 7.006997585296631, "[TT] Maximum Power of the EPS = 65 W"]
-[9.470998764038086, 8.93958568572998, "[TT] Frame Format of the Iris Video Camera = 4096 x 20 pixels (UHD); 1920 x 1080 pixels (HD)"]
-[7.696989059448242, 2.2158443927764893, "[TT] Regions of the AAI = Mumbai, Chennai and Kolkata's oceanic airspaces"]
-[13.414200782775879, 6.724453926086426, "[TT] Power of the KOMPSAT-2 = 1.0 kW"]
-[8.499916076660156, 0.1534150242805481, "[FF] Magnetic Field Behavior of the Comet 67P = Became stronger and more turbulent when the forming bow shock washed over Rosetta"]
-[4.523179054260254, -0.888188898563385, "[FF] Purpose of the Dragon = Taking home a variety of critical space research"]
-[4.2262773513793945, 2.573051929473877, "[TT] Transport Destination of the Beresheet = Cape Canaveral Air Force Station"]
-[11.722171783447266, 4.410006999969482, "[TT] Mast Length of the Spin-Stabilized Spacecraft = 6 m"]
-[7.867864608764648, -0.4269370138645172, "[FF] Date of the Cracking Icy Secrets of New Penguin Colonies = 24 September 2020"]
-[7.305795669555664, 6.570270538330078, "[FF] Algorithms of the Instrument Computer = Lossless (2:1 Rice compression) and lossy (JPEG)"]
-[4.931546211242676, 5.12267541885376, "[TT] CCSDS ID of the GSAT-0205 = 265"]
-[9.56214714050293, 0.32853320240974426, "[TT] Travel Distance of the Yutu 2 = 590 meters"]
-[9.764104843139648, -0.5872636437416077, "[TT] Orbital Altitude Decay of the ProSEDS = At least 5-15 km in altitude per day"]
-[3.907457113265991, 6.306283950805664, "[TT] Quantity of the S&F antennas = 4"]
-[3.9626312255859375, 2.111285448074341, "[TT] Launch Vehicle of the Landsat-6 = Titan 2 booster"]
-[12.412168502807617, 0.5651332139968872, "[TT] Lead Activities of the PLATO = Transferred from France to Germany"]
-[4.714270114898682, 7.2223381996154785, "[TT] Maximum Data Rate of the X-band transmission = 170 Mbit/s"]
-[10.577568054199219, 1.6146516799926758, "[FF] Gravity of the Black Hole = Enormous"]
-[3.469897508621216, -0.91645747423172, "[TT] Orbit Type of the HY-1C = Sun-synchronous"]
-[7.677967548370361, 5.222240447998047, "[FF] Onboard Means of the Internal Calibration = Matched loads in each of the receivers, Centralized noise source/network on the hub, Distributed noise sources/networks in the arms, Fringe wash function in the CCU"]
-[8.755773544311523, 7.755209445953369, "[TT] Element Size of the S4-S6 detectors = 100 x 100 \u00b5m"]
-[9.429718971252441, 5.992380619049072, "[TT] Off-nadir Angle of the CIRC = 30\u00ba"]
-[6.639348030090332, -0.46952179074287415, "[TT] Period of the COMPASS-2 = 93.5 minutes"]
-[9.129508018493652, -1.2762740850448608, "[TT] Orbit of the Meteosat-1 to -7 = GEO (geostationary)"]
-[3.3588767051696777, 6.199808597564697, "[TT] Length of the LRS (Lunar Radar Sounder) antennas = 15 m"]
-[1.6113238334655762, 3.758115530014038, "[TT] Multi-function component assembly of the BEESAT-2 = Yes"]
-[3.4044246673583984, 4.990816593170166, "[FF] Receive Chain Selection of the SAR Instrument = Chain 1 or 2"]
-[5.720108509063721, 3.149895429611206, "[TT] Participants of the TTP = ~10 young engineers and scientists from UAE"]
-[10.034858703613281, 2.6884703636169434, "[TT] Orbit of the NanoRacks CubeSat = Near-circular orbit of the ISS, altitude of ~400 km, inclination of 51.6o"]
-[4.330738067626953, 1.2469384670257568, "[TT] Loss Date of the SEOSAT-Ingenio = 17 November 2020"]
-[7.7627387046813965, 6.5275444984436035, "[TT] Repeatability of the Imaging Mode = 23 min"]
-[7.940615653991699, 6.511033535003662, "[TT] High Temporal Resolution of the SEM-2 = 500 - 600 second averages"]
-[7.798649787902832, 5.76382303237915, "[TT] Polarization of the Advanced Microwave Scanning Radiometer (AMSR) = Dual"]
-[8.307394027709961, 4.6329169273376465, "[FF] Improvement of EOP of the LARES 2 = 17%"]
-[5.4486799240112305, 4.171197891235352, "[TT] Bus Design of the Restore-L = Maxar's decades-proven 1300-class platform"]
-[6.877347469329834, 8.972640991210938, "[TT] Bandwidths of the POLDER-2 = 10 - 40 nm"]
-[13.411961555480957, 7.331381797790527, "[TT] Power of the HIRES = 10 W"]
-[7.227199077606201, 2.239964723587036, "[FF] Application of the Spacecraft = Ice and ocean monitoring, land use, geology, forestry, and mapping"]
-[7.130885124206543, 8.570030212402344, "[TT] Solar Constant Channel Accuracy of One Measurement of the ISP-2 = 0.05%"]
-[7.5971598625183105, 6.7629313468933105, "[TT] Sample Exposure Time of the METIS = More than 200 days"]
-[10.243966102600098, 3.3363659381866455, "[TT] Quantity of the Prometheus-2.1 to -2.8 = Seven"]
-[12.351415634155273, 0.5985032916069031, "[TT] Observation Target of the Plato = More than 200,000 stars"]
-[10.126124382019043, 6.4816789627075195, "[TT] Survey Date of the MABEL = April 20, 2012"]
-[11.416748046875, 3.030414581298828, "[TT] Altitude Maintenance Duration of the Electric Thruster = One year"]
-[4.94358491897583, -0.8567111492156982, "[TT] Deorbit Burn Duration of the Crew Dragon spacecraft Resilience = 50 minutes"]
-[13.901463508605957, 7.181303024291992, "[TT] Power Bus Voltage of the CanX-2 = 4.0 V"]
-[9.535244941711426, 0.9862217307090759, "[TT] Reentry Speed of the EFT-1 = Over 32,000 km/hr"]
-[11.973233222961426, 6.586928844451904, "[TT] Energy Range of the AMS = Above 8 GeV"]
-[7.863685131072998, 3.0086498260498047, "[TT] Purpose of the TanSat = Monitors global atmospheric CO2 concentrations and is capable of measuring SIF"]
-[8.396041870117188, 4.396415710449219, "[FF] Orbit Control of the MEV-2 = Does not control the orbit"]
-[13.302788734436035, 2.9549996852874756, "[TT] Mass of the GHGSat-C2 = 16 kg"]
-[9.648250579833984, 8.338254928588867, "[FF] FFOV (Forward FOV), AFOV (Aft FOV), LSFOV (Left Side FOV), RSFOV (Right Side FOV) of the CATS = Legend"]
-[7.696048736572266, 9.259472846984863, "[TT] Band of the Nighttime SST Product = Band 7 (3.9 \u00b5m wavelength)"]
-[7.197070598602295, 1.252065658569336, "[TT] Function of the Mars Ascent Vehicle = Launch the samples into orbit around Mars"]
-[11.99000072479248, 4.152042865753174, "[TT] Size of the GOLD payload = Microwave-sized"]
-[9.67428970336914, 6.309749603271484, "[FF] Drive Signal of the Fast-Steering Mirror = Sinusoidal voltage signal"]
-[8.372429847717285, 1.2905712127685547, "[FF] Pulse Width of the RainCube = Variable"]
-[6.847164630889893, -0.6589644551277161, "[TT] Orbit Period of the RISAT-1 = 95.49 minutes"]
-[11.552111625671387, 3.3985509872436523, "[TT] Propulsion System of the Spacecraft = Hybrid"]
-[9.038792610168457, 5.596456527709961, "[TT] Pointing Accuracy of the AOCS = < 36 arcsec for the Z-axis"]
-[5.192317485809326, 7.224804878234863, "[TT] Uplink Margin of the CXS-810C = 23.2 dB worst case"]
-[4.450924873352051, 4.188323020935059, "[TT] Number of LEOLUTs of the LEOSAR = 53"]
-[8.894651412963867, 1.6437784433364868, "[TT] Mid-course correction burn speed addition of the Webb = Approximately 45 mph (20 m/s)"]
-[6.670982837677002, 8.54488754272461, "[TT] Spectral Channels of the POLDER-P = 9"]
-[7.833113193511963, 1.9449095726013184, "[FF] Objective of the Gulfstream Supersite = Investigate oceanographic phenomena"]
-[5.128013610839844, 5.919251441955566, "[TT] Expected Number of Users of the GSM = One billion"]
-[9.531514167785645, 7.050044536590576, "[TT] Ku-band of the Scatterometer = 25 x 25 km spatial resolution"]
-[5.338277816772461, 4.042057991027832, "[TT] Satellite Tracking Capacity of the MEOLUT Next = Up to 30 satellites"]
-[10.204596519470215, 2.8163769245147705, "[TT] Agency of the NanoSat-1B = INTA"]
-[4.141964912414551, 6.332626819610596, "[TT] Antenna Type of the ROSA = Hemispherical-coverage"]
-[11.5410737991333, 4.862828731536865, "[TT] Outer Diameter of the PM = 4.4 m"]
-[4.491039276123047, -0.8821381330490112, "[FF] Installation Date of the Dragon = 27 July 2019"]
-[10.646346092224121, 3.824599027633667, "[FF] Deployment Status of the InflateSail = Not Deployed"]
-[4.940822124481201, 3.389066696166992, "[TT] Manufacturer of the Rubin-8-AIS = OHB-System, Bremen, Germany"]
-[5.686287879943848, 2.7475433349609375, "[FF] Funding of the GIDAS = Co-funded basis"]
-[5.982102394104004, 6.112426280975342, "[FF] Status of the SSR (Solid State Recorder) = Limited onboard resources"]
-[7.951107025146484, 3.0883450508117676, "[FF] Measurement Domain of the CarbonSpec = Carbon Dioxide detection"]
-[3.3194124698638916, 5.319547653198242, "[TT] Centre Wavelength of the SAR = 0.235 m"]
-[5.370599746704102, 8.765629768371582, "[TT] Bandwidth of the Band 7 = 0.723 \u00b5m (50 cm -1)"]
-[7.417359828948975, 3.7504594326019287, "[FF] Observation Method of the Global Positioning System = Radio occultation"]
-[6.510097503662109, 3.679180383682251, "[FF] Types of Environmental Data Records (EDRs) of the IDPS = Cloud coverage, temperature, humidity, ozone distribution, snow cover, vegetation, sea surface temperatures, aerosols, space environment, earth radiation budget information"]
-[11.852462768554688, 3.168633460998535, "[TT] Reaction Control Assembly of the EURECA = 6 x 21 mN nitrogen thrusters"]
-[14.648163795471191, 6.648151397705078, "[TT] NiH2 Batteries Capacity of the DSP satellites = 36 Ah"]
-[7.9186882972717285, -0.32915619015693665, "[FF] Below Normal Date of the Arctic Sea Ice = 25 March 2020"]
-[7.671450614929199, 5.206016540527344, "[TT] Vibration Test of the GOES-S = Completed"]
-[6.008736610412598, 5.517773628234863, "[TT] Avionics Redundancy of the TDS-1 = Fully redundant"]
-[9.586108207702637, 0.7166013121604919, "[TT] Distance of the Closest Approach = 0.71 km"]
-[8.725624084472656, 2.752992868423462, "[FF] Areas of Application of the TIMED = The MLTI (Mesosphere and Lower-Thermosphere/Ionosphere)"]
-[13.1713228225708, 5.190044403076172, "[TT] Solar Cell Dimensions of the TUBSAT-N = 6 cm x 4 cm"]
-[10.173612594604492, 7.965604782104492, "[TT] Clear Aperture of the Ritchey-Chretien telescope = 165 mm"]
-[5.8095622062683105, -0.05843318626284599, "[TT] ISS Onboard Waiting Period of the MicroMAS-1 = 8 months"]
-[5.242745876312256, 2.2998178005218506, "[FF] Mission Type of the Badr-B = EO"]
-[8.452531814575195, 1.315455675125122, "[FF] Objectives of the Aquarius = Understanding ocean circulation, global water cycle and climate interaction. Soil moisture over Argentina Global sea salinity measurements & Retrieval of soil moisture from Aquarius over Argentina"]
-[6.2128400802612305, 0.73939448595047, "[FF] Online Publication Date of the Gaia16aye = 21 January 2020"]
-[8.638392448425293, 0.11555203050374985, "[TT] Propellant of the Comet = Water"]
-[7.805849552154541, 8.465336799621582, "[TT] Bands of the Multispectral Instrument (MSI) = 13"]
-[8.530817031860352, 2.048771858215332, "[FF] Measurement Objective of the ASCAT = Measure wind speed and direction over the oceans"]
-[9.608748435974121, -0.5618548393249512, "[TT] Closest Point of Orbit of the ExoMars TGO = About 113 km"]
-[10.287301063537598, 5.386324405670166, "[FF] Purpose of the Thermal Desktop = Evaluate surface treatments and other design decisions"]
-[11.877290725708008, 4.981457233428955, "[TT] Size of the VectorSol = 30 mm x 50 mm"]
-[6.559160232543945, 4.696405410766602, "[FF] Function of the BCR = Provides power for all spacecraft loads and performs ancillary functions including heater control, SRM fire, and separation system actuation"]
-[9.115219116210938, 4.606629848480225, "[TT] Sensors of the ADCS = Magnetometers and gyroscopes"]
-[10.739733695983887, 7.505810260772705, "[TT] Scanning Swath Width of the ATM = ~250 m"]
-[5.678049087524414, 5.232451915740967, "[FF] Broadband Connectivity of the SES-17 = Commercial shipping, aviation, governments, enterprises, and underserved areas"]
-[6.111392498016357, 0.8774957656860352, "[FF] Image Capture Date of the TopSat = Unknown"]
-[5.8452229499816895, 1.5782209634780884, "[FF] Presentation Date of the Hokkaido Satellite Project = June 4-11, 2006"]
-[6.5676984786987305, 6.616243839263916, "[TT] Laser Terminals Developer of the EDRS-C = Tesat-Spacecom and the DLR German Space Administration"]
-[12.470418930053711, 3.147840738296509, "[TT] Propellant Mass of the XMM-Newton = 140 kg"]
-[5.938740253448486, 2.903790235519409, "[TT] Number of Launches of the Worldview Legion = Two"]
-[5.516569137573242, 5.926436424255371, "[FF] Design of the DCAM3 = Similar to IKAROS DCAM1,2"]
-[6.456003665924072, -0.27658408880233765, "[TT] Repeat Cycle of the ALOS-3 = 35 days"]
-[7.7205729484558105, 6.475012302398682, "[FF] Image Collection of the ABI = Full Disk, CONUS, Mesoscale"]
-[10.441630363464355, 6.897740840911865, "[TT] Size of the 1.2 meter mirror = 1.2 meter"]
-[13.207521438598633, 7.338292121887207, "[TT] Power Consumption of the DCS = 60 W"]
-[7.8246893882751465, 3.6702892780303955, "[FF] Function of the SODAD = Orbital debris/micrometeorite/\u00b5particle detection"]
-[5.64758825302124, 0.46300840377807617, "[TT] Mission Extension of the Cluster = December 2005 to December 2009"]
-[6.885519981384277, 5.844219207763672, "[TT] Quantity of the MRFOD = 1"]
-[10.060751914978027, 2.835261106491089, "[TT] CubeSat Deployment Count of the NanoRacks = 190"]
-[10.334110260009766, 2.2807395458221436, "[FF] Resolution of the ASTRO-H = 30-50% of the hard X-ray Cosmic Background"]
-[9.024978637695312, 2.607191801071167, "[FF] Function 3 of the PUNCH = Provide the first continuous, detailed 3D images of CME substructure propagating through the heliosphere"]
-[10.585433959960938, 5.749246597290039, "[TT] Thermionic Emission Peak Temperature of the SPC = About 1200 \u00b0C"]
-[13.007722854614258, 7.057921409606934, "[TT] Power Requirement of the WCOM = 1550 W"]
-[7.479310512542725, 2.5936338901519775, "[FF] Measurement Category of the Satellite = Multi-purpose imagery (ocean), Radiation budget, Multi-purpose imagery (land), Surface temperature (land), Vegetation, Gravity, Magnetic and Geodynamic measurements, Surface temperature (ocean), Landscape topography, Ocean topography/currents, Atmospheric Winds, Ice sheet topography, Lightning Detection"]
-[3.070167064666748, 2.305161237716675, "[TT] Spatial Resolution of the Sentinel-2 = 10 m, 20 m, and 60 m"]
-[9.08634090423584, 6.9985032081604, "[TT] Imagery Collection of the Monitor-E = 80 million km2"]
-[10.275132179260254, 4.546016693115234, "[TT] Maximum Power of the Reaction Wheels = 0.7 W"]
-[8.56011962890625, 7.801060676574707, "[TT] Number of Robotic Profiling Floats of the Argo Array = 3000"]
-[5.293514728546143, 7.00116491317749, "[TT] Data Downlink Speed of the CDSU = 4 Mbit/s"]
-[7.764543056488037, 6.554375171661377, "[TT] Image Interval of the IBIS = Roughly eight minutes"]
-[8.32645034790039, 3.387110471725464, "[FF] Utilized Atmospheric Emissions of the MATS = O2 Atmospheric Band airglow and scattering of sunlight by NLC"]
-[4.818138122558594, 7.922461032867432, "[TT] Frequency of the EPIRB = 121.5/243 MHz"]
-[5.019145965576172, 0.4661567211151123, "[TT] Signal Upgrade Completion Date of the GATE = Early 2010"]
-[5.538180828094482, 2.4954850673675537, "[TT] Developer of the TEMPO = Ball Aerospace"]
-[4.793426990509033, 0.49415889382362366, "[TT] Launch Date of the Monitor-E = 26 Aug 2005"]
-[10.368863105773926, 8.01232624053955, "[TT] Telescope Diameter of the SILEX = 25 cm"]
-[5.657569885253906, 0.7556864023208618, "[FF] Publication Date of the Tolulope E. O\u2019Brien = December 2011"]
-[10.861749649047852, 6.329930782318115, "[TT] Lens Surfaces Coatings of the Instrument = Narrow-band AR coatings with R<0.2%"]
-[6.170332431793213, 4.3466339111328125, "[FF] Ordering of the CSK GS = Allow S-IM to submit production requests towards the FM when receiving confirmation that the acquisition is planned"]
-[3.794304132461548, 6.459006309509277, "[TT] Pulse Duration of the Antenna = 33.4 \u00b5s"]
-[6.939019680023193, 0.898086428642273, "[FF] Data Analysis of the ICON = First year of observations coincided with solar minimum"]
-[3.46213698387146, 5.198179721832275, "[TT] Pixel Size of the Radar = 25 m x 25 m"]
-[5.073973178863525, 7.391636371612549, "[TT] IMG Data Rate of the RF communications = 0.9 Mbit/s"]
-[11.49533748626709, 4.66148567199707, "[TT] Size of the LightSail-2 = Small washing machine"]
-[10.48145866394043, 6.666210651397705, "[TT] Total Mirror Segments of the Mirror = 4680"]
-[6.946227550506592, -0.6524806618690491, "[TT] Orbital Periods of the TRAPPIST-1 = 1.5 to 20 Earth days"]
-[11.346345901489258, 5.870845794677734, "[TT] Housing Material of the NIRST instrument = Aluminum"]
-[7.6234211921691895, 0.7055941224098206, "[FF] Mission of the Lunar Flashlight = Look for ice deposits and identify locations where resources may be extracted from the lunar surface"]
-[10.816690444946289, 6.409702301025391, "[TT] Material of the Focal Plane Assemblies = Teledyne HgCdTe"]
-[8.897915840148926, 7.579038619995117, "[TT] Pixel Pitch of the PamCam = 6.7 \u00b5m"]
-[6.404346466064453, 4.268322467803955, "[FF] Leveraging of the COTS technology = Reuse of commercial design tools, foundry, processes, masks"]
-[6.821970462799072, 4.121064186096191, "[FF] Unknown of the Space Environment Data Acquisition Equipment = Unknown"]
-[7.4432148933410645, 3.6240296363830566, "[FF] Signal Quality of the MetOp-SG Radio Occultation = Higher quality observations on the lower troposphere regions"]
-[9.63924503326416, 8.333210945129395, "[TT] Field of View of the Field of View (FOV) = 19.25\u00ba"]
-[4.515879154205322, 7.137816429138184, "[TT] Data Download System of the FY-4B = Ka-band communications"]
-[5.804974555969238, 0.7657991647720337, "[TT] Departure Date from MSSS of the ShadowCam = 13 August 2021"]
-[6.024444580078125, -1.1662113666534424, "[TT] Exceeded Design Life of the GRACE = Yes"]
-[6.237853050231934, 5.347069263458252, "[FF] Data Format of the HSM = Virtual Channel Data Units"]
-[13.322248458862305, 7.3403520584106445, "[TT] Power of the OSIRIS = Maximum power of 50 W"]
-[5.544785976409912, 0.6107308268547058, "[FF] Monitoring Period of the Envisat = 2008-2009"]
-[4.793932914733887, 0.6451398134231567, "[FF] Launch Date of the ANDE-2 = July 17, 2009"]
-[5.20731258392334, 4.690483093261719, "[TT] Staffing of the Ground Segment = 24 hour period during the mission"]
-[12.089526176452637, 7.634762287139893, "[TT] Total Mass of the Model 1000 Camera System = <100 kg"]
-[5.808123588562012, 3.1168744564056396, "[TT] Development Cost of the EPS-MACCS = Maximum of \u20ac30 million"]
-[9.641988754272461, 7.047281742095947, "[TT] Spatial Resolution of the VISSR = 1.25-5 km"]
-[8.525177001953125, 1.3523521423339844, "[FF] Purpose of the Aquarius = Monitor Sea Surface Salinity"]
-[3.6883816719055176, 3.855353355407715, "[TT] Launch Date of the RISAT-1 = April 2012"]
-[7.272066593170166, 6.409453868865967, "[TT] Method of the GLI = Piecewise linear method with cascade amplification"]
-[10.143474578857422, 10.002748489379883, "[FF] Launch Date of the Vega = Aug. 2, 2017"]
-[7.537675380706787, 2.1897456645965576, "[FF] Application of the Space Technology = Water management, orbital tracking of water quality and pollution, spacecraft-grade recycling systems, identify marine plastic litter using satellites"]
-[5.484688758850098, 5.055470943450928, "[TT] Location Knowledge of the GFO = Redundant GPS receivers"]
-[9.047506332397461, 5.681351184844971, "[TT] Pointing Accuracy of the Resurs-P1 = 0.2 arcmin"]
-[5.190230369567871, 6.941560745239258, "[FF] Presentation Date of the Scalable Payload Downlink Chain = June 11-13, 2009"]
-[5.76283597946167, 7.160425186157227, "[TT] Parameter of the Data Rate = 150 kbit/s max"]
-[7.500375270843506, 3.4592366218566895, "[FF] Task of the Lost at Night = Identify Cities in Images Encompassing a Circle 310 Miles Around"]
-[14.181727409362793, 3.1328673362731934, "[TT] Mass of the Carbonite-1 = Approximately 100 kg"]
-[11.474611282348633, 3.466547966003418, "[TT] Minimum Relative Distance of the CNAPS = 50 m"]
-[7.549505233764648, 6.45302677154541, "[TT] Image Production of the GOCI = 3 times per day"]
-[11.946961402893066, 4.820455074310303, "[FF] Physical Size of the GPS Receiver = Small"]
-[5.601412296295166, 1.4225932359695435, "[FF] Workshop Date of the MTG Mission Team (MMT) = Dec.3-5, 2007"]
-[7.081457138061523, 5.203169822692871, "[FF] Function of the Test Source = Test measurements over long distances"]
-[4.89155912399292, 5.235484600067139, "[FF] Signal Strength of the NPSat-1 = Too weak for data to be decoded"]
-[4.864302158355713, 0.359512060880661, "[FF] Operational Role Start Date of the GOES-T = Unknown"]
-[8.09865951538086, -1.2372950315475464, "[TT] Laser Altimeter of the ICESat-2 = 10,000 pulses of light each second"]
-[11.59335708618164, 4.813837051391602, "[TT] Cone Structure Length of the COMMx = ~1.85 m"]
-[13.831546783447266, 7.295611381530762, "[TT] Power Supply Voltage of the Big Apple board = 5 V"]
-[8.051583290100098, 1.116241455078125, "[FF] Importance of the Soil Moisture = Essential for managing agricultural crops and predicting their yields"]
-[7.497936725616455, 2.292781114578247, "[FF] Coverage of the FlytLIVE = Entire Americas and North Atlantic Corridor"]
-[7.988184452056885, 8.632044792175293, "[TT] Application of the SWIR band (1.378 \u00b5m) = Daytime sensitivity to very thin cirrus"]
-[4.97395658493042, 0.4132021367549896, "[FF] Article Date of the CXO = 29 January 2019"]
-[6.658879280090332, 3.3729169368743896, "[FF] Purpose of the BioNutrients = Enables on-demand production of nutrients needed during long-duration space missions"]
-[3.406978130340576, 5.039042949676514, "[TT] Instrument type of the L-band SAR = Scatterometers"]
-[9.98052978515625, -1.583502173423767, "[TT] Orbit Inclination of the HTV-8 = 51.6\u00ba"]
-[8.967032432556152, 5.593505859375, "[TT] Position Knowledge of the Pointing Mechanism = Better than 10 \u00b5rad"]
-[5.990362644195557, -0.2010061889886856, "[TT] Mission Duration of the Rosetta spacecraft = 2014 to 2016"]
-[4.3958940505981445, -1.6495287418365479, "[FF] Formation Event of the Blue Ring Nebula = Stellar merger between a star similar to our Sun and another star only about one-tenth that size"]
-[5.520118236541748, 1.899186611175537, "[FF] Symposium Date of the Flying Laptop = April 4-8, 2005"]
-[6.093341827392578, 6.314815521240234, "[TT] Data Processing of the MODEX-1 = GMTI processing"]
-[6.888554573059082, 6.414113521575928, "[TT] Data Processing Level of the GLM = L0, L1b, L2+"]
-[8.798806190490723, 7.451768398284912, "[FF] ICRA Requirement of the MTG-I = Inter-Channel Co-registration Accuracy"]
-[5.545495510101318, 6.736110687255859, "[TT] Data Delivery of the Mini-RF = More than 40 TB"]
-[7.857370853424072, 8.74100112915039, "[FF] Continuum Spectrum of the GRS 1915+105 = Figure 6"]
-[5.158566951751709, 2.334137439727783, "[TT] Agency of the ZACUBE-2 = SANSA, CPUT"]
-[8.135808944702148, -0.6120957136154175, "[FF] Five-Year Average Arctic Sea Ice Volume of the CryoSat-2 = Relatively stable"]
-[7.794722080230713, 5.588440895080566, "[FF] Backup Function of the BEI Systron Donner QRS100 = Nutation measurement"]
-[8.511192321777344, 5.363220691680908, "[TT] Position Accuracy (RMS orbit) of the S-2 NRT = < 3 m (3D) 3-sigma"]
-[14.206589698791504, 3.2292592525482178, "[TT] Mass of the CXBN = 2.6 kg"]
-[7.5864667892456055, 6.305027008056641, "[TT] Time Tagging Precision of the ATLAS = 0.15 ns"]
-[6.7311601638793945, -0.369567334651947, "[TT] Period of the Satellite = 105.33 min"]
-[11.134710311889648, 5.82534646987915, "[TT] Baffles Material of the Collimator = Tantalum (Z=73)"]
-[8.631928443908691, 8.26926326751709, "[TT] Microshutter Arrays of the NIRSpec = Four"]
-[4.824615955352783, 0.4172888696193695, "[TT] Launch Date of the CHOMPTT = 16 Dec 2018"]
-[7.653488636016846, 8.784214973449707, "[TT] Band Wavelengths of the Spectral bands = 0.64\u00b10.05, 1.61\u00b10.03; 3.9\u00b10.1; 6.15\u00b10.45; 7.0\u00b10.2; 10.7\u00b10.5; 12.0\u00b10.5; 13.3\u00b10.3"]
-[4.880800247192383, 8.301077842712402, "[TT] Frequency of the MWR = 23.8 and 37 GHz"]
-[10.362773895263672, 2.3303582668304443, "[FF] Technology of the Hard X-ray optics = Hard X-ray optics"]
-[5.012288570404053, 1.8517179489135742, "[FF] Imaging Capabilities of the G\u00f6kt\u00fcrk-2 = Urban land use and land-cover maps, forest areas monitoring, agricultural areas discrimination and classification, vegetation cover maps and crop identification, fire risk areas mapping, flood monitoring, land-cover change and snow cover maps"]
-[8.334269523620605, 0.7498984336853027, "[TT] Perimeter Length of the Calf Canyon-Hermits Peak fire = 50 miles (80 km)"]
-[5.46260929107666, 2.4829986095428467, "[TT] Mission Name of the NuSTAR = NuSTAR"]
-[3.460214376449585, -0.8860579133033752, "[TT] Deployment Orbit of the NPSat-1 = Sun-synchronous circular orbit of 720 km with an inclination of 24\u00ba"]
-[9.477465629577637, 1.2986726760864258, "[TT] Deployment Velocity of the BEESAT-4 = 1.5 m/s"]
-[3.863126039505005, 1.3141602277755737, "[TT] Landing Location of the Falcon 9 = Atlantic Ocean"]
-[9.12285041809082, 8.053343772888184, "[TT] Number of Pixels of the LLNL imaging system = 1280 x 1024"]
-[3.8204352855682373, 1.502548098564148, "[TT] Booster of the Falcon 9 = B1060"]
-[9.272994995117188, 1.0052785873413086, "[TT] Travel Time from Ganymede to Jupiter of the Juno = 14 hours, 50 minutes"]
-[6.4690446853637695, -0.8387126326560974, "[TT] LTAN of the GOSAT-2 = 1300 \u00b1 0015 hours"]
-[5.647970199584961, 2.8354127407073975, "[FF] Sponsors of the CanX-7 = Defence R&D Canada \u2013 Ottawa, the Natural Sciences and Engineering Council of Canada, COM DEV, Royal Military College of Canada, and the Canadian Space Agency"]
-[9.581649780273438, 8.307258605957031, "[TT] Field of View of the Primary Objective = ~1.02 Rsun"]
-[7.903658390045166, 5.26541805267334, "[FF] Components of the Calibration Network = Central redundant noise diode, distributed noise diodes on each arm segment"]
-[10.899842262268066, 7.537623882293701, "[TT] Overlapping Swath of the WFI = 830 km"]
-[11.715682029724121, 3.330561399459839, "[TT] Total Firings of the LM thruster = More than 85"]
-[9.311532974243164, 3.191016435623169, "[TT] Design of the 20 cm off-axis internally occulted coronagraph = Off-axis"]
-[10.10879898071289, 3.2103829383850098, "[FF] Purpose of the ASTERIA 6U CubeSat = Test the use of CubeSats for astronomy research"]
-[5.184717178344727, 1.2580621242523193, "[FF] Operational of the BDS-3 = Yes"]
-[5.460043430328369, 0.26827818155288696, "[TT] Meeting Date of the International Space Station (ISS) = March 11, 2010"]
-[8.385808944702148, 7.633848190307617, "[TT] Detector Type of the WUPPE = Intensified diode-array"]
-[6.576541423797607, 5.766238689422607, "[TT] Quantity of the Total Board Count = 10"]
-[13.960041999816895, 3.982123851776123, "[TT] Instrument Mass of the DUST sensor = 3.8 kg"]
-[14.678816795349121, 6.669116020202637, "[TT] Number of Batteries of the ABEX = 16"]
-[5.399051666259766, 7.170585632324219, "[TT] Data Rate of the Communications Signal = 600 Mbit/s"]
-[6.472519397735596, 1.5393266677856445, "[TT] Number of Passes of the Europa Clipper = 45"]
-[9.074339866638184, 5.700580596923828, "[TT] Boresight Pointing Accuracy (Azimuth) of the SXI = Within 3.5 arcmin"]
-[6.628737926483154, 6.21462869644165, "[FF] Issue of the File Transfer Test = Long strings of zeros in various places in each file"]
-[9.544304847717285, 7.139631748199463, "[TT] Resolution at Edge of Swath of the Vidicons = 5.5 km"]
-[8.389528274536133, 7.0206451416015625, "[TT] Imager Type of the ResourceSat-2 = Multispectral pushbroom scanners"]
-[8.652739524841309, 1.1076072454452515, "[FF] IGARSS Proceedings of the Aquarius = July 13-18, 2014"]
-[14.085585594177246, 4.0319390296936035, "[TT] Instrument Mass of the IES = < 6.2 kg"]
-[10.320466041564941, 2.1942214965820312, "[FF] Characteristics of the NAOJ team's model = High luminosity and directed beams of photons"]
-[11.986281394958496, -0.37388163805007935, "[TT] Mission Operations Center of the TESS = OA Mission Operations Center"]
-[5.303121566772461, 3.320394992828369, "[TT] Operator of the CSSS = DND"]
-[11.083874702453613, 5.5411882400512695, "[TT] Accuracy of Position Determination of the Gamma-ray Counter = < 5\u00ba"]
-[10.139786720275879, 6.958827018737793, "[TT] Footprint Area of the Sounder = 10 km x 40 km"]
-[6.473392963409424, 1.949552059173584, "[FF] URL of the AstroSat = http://www.isro.gov.in/Spacecraft/astrosat"]
-[8.319191932678223, 8.103775978088379, "[TT] Spectral Resolution of the EPIC Cameras = E/\u0394E ~ 20-50"]
-[4.692422866821289, 7.285648822784424, "[TT] Data Rate of the Ka-Band unit = 200Mbps"]
-[6.611830711364746, 5.340519905090332, "[FF] RFU of the ASCAT = Radio Frequency Unit"]
-[4.496955394744873, 4.035637855529785, "[FF] Signal in Space Representation of the GIOVE-A = Fully representative of the operational GALILEO system"]
-[4.349791049957275, 7.613579750061035, "[TT] Uplink Frequency of the RF Communications = S-band (2025-2110 MHz)"]
-[5.0793232917785645, 1.1876245737075806, "[FF] Conference Presentation Date of the PROBA-2 = Oct. 17-20, 2005"]
-[13.388501167297363, 6.829822063446045, "[TT] Payload Power of the Spacecraft = 350 W, 1.1 kW"]
-[8.328414916992188, 7.705908298492432, "[TT] Number of Detectors of the OLI = 6500 per multispectral band, 13000 for the panchromatic band"]
-[5.72083044052124, 6.760776996612549, "[TT] Data Collected of the Juno = About three terabits"]
-[10.934273719787598, 10.07052230834961, "[FF] Longevity of the Alpha Magnetic Spectrometer (AMS-02) = Unknown"]
-[9.190441131591797, 3.3280179500579834, "[FF] Objective of the COR2 = Explore the outer corona (2-15 Rsun) in white light and pB with high spatial and temporal resolutions"]
-[4.935533046722412, 8.420604705810547, "[TT] Spectral Range of the MTVZA-GY Imaging/Sounding Microwave Radiometer = 10.6-183 GHz"]
-[5.4252543449401855, 1.01039719581604, "[FF] Date of the Maxar\u2019s path to growth = 10 April 2019"]
-[9.541202545166016, 7.404138565063477, "[TT] Pixel Angular View of the EXI instrument = 23 arcsec per pixel"]
-[5.454634189605713, 5.464211463928223, "[TT] Connection of the USRP = Interfaced with a PC"]
-[9.989792823791504, -0.22625111043453217, "[TT] Orbit Altitude of the Starlink Group 4-14 = 550 km"]
-[10.255209922790527, 5.174615859985352, "[FF] Loading Temperature Change of the Helium = To allow warmer temperature helium to be loaded"]
-[8.285825729370117, -0.7819882035255432, "[FF] Function of the ATLAS = Measure melting ice sheets and investigate how this effects sea level rise, investigate changes in the mass of ice sheets and glaciers, estimate and study sea ice thickness, and measure the height of vegetation in forests and other ecosystems worldwide"]
-[12.420581817626953, 0.6425616145133972, "[TT] Number of Cameras of the Plato = 26"]
-[5.29816198348999, -0.3517906963825226, "[TT] Life Expectancy of the SPOT-4 = End of 2012"]
-[4.571580410003662, 5.49228048324585, "[TT] Passes per Day of the GOMX-3 = 5"]
-[11.74323844909668, 3.3131489753723145, "[TT] Number of Thrusters of the PROP unit = 4"]
-[5.844966411590576, 3.2708377838134766, "[TT] Annualized cost to collect 10 6  km 2 /day of the SkySat = > $75 million"]
-[10.309050559997559, 5.764293670654297, "[TT] Temperature of the MIRIS = Around 200 K"]
-[4.52294397354126, -0.853190541267395, "[TT] Splashdown Location of the Crew Dragon = Atlantic Ocean or Gulf of Mexico"]
-[3.455911159515381, 6.41665506362915, "[TT] Antenna Diameter of the Integrated Mobile Station = 4.6m"]
-[6.826235771179199, -0.3264465928077698, "[FF] Observation Duration of the Cal_doppler = One entire day side of the orbit"]
-[8.077054023742676, 7.9672112464904785, "[FF] Type of the PHI = Diffraction limited, wavelength tunable, quasi-monochromatic, polarization sensitive imager"]
-[7.127516269683838, 1.541543960571289, "[TT] Orbital Life of the SporeSat = 30-60 days"]
-[7.763472557067871, 2.9487078189849854, "[FF] Mission of the NIRS = RAIDS (Remote Atmospheric and Ionospheric Detection System)"]
-[6.298935890197754, 8.657541275024414, "[TT] SP of the Polarization = -"]
-[13.296221733093262, 5.3323869705200195, "[TT] Solar Array Size of the IMPS = 1cm2"]
-[9.897136688232422, 6.466429233551025, "[FF] URL of the Nimbus Earth Radiation Budget (ERB) Experiment = http://badc.nerc.ac.uk/data/gedex/detail/erb_soli.det"]
-[6.448575019836426, -0.754609227180481, "[TT] LTAN of the RADARSAT-2 = 18:00 hrs \u00b115 min"]
-[6.331603050231934, 5.040703773498535, "[FF] Functions of the CMN = Switching of receivers and calibration network, Acquiring some housekeeping information, Providing some power conversion and distribution to the receivers, Providing the receivers with a local oscillator signal derived from DICOS"]
-[13.826059341430664, 5.673314094543457, "[TT] Efficiency of the Silicon Solar Arrays = 16%"]
-[5.393100261688232, 1.044887661933899, "[FF] Presentation Date of the ABI = Jan. 17-21, 2010"]
-[5.426370143890381, 6.784016132354736, "[TT] Data Transport of the SPA-S = 400~600 Mbit/s"]
-[8.006217956542969, 3.1795263290405273, "[TT] Measured Gases of the TANSO-FTS-2 = CO2, CH4, CO"]
-[4.010099411010742, 1.9338237047195435, "[TT] Launch Vehicle of the GCOM-W1 = H-IIA F21"]
-[6.736467361450195, 5.270133018493652, "[FF] Lower Module Components of the Merlin = `generic processor board', power conditioning, microprocessor, analog-to-digital converter, memory, I/O ports, data interfaces"]
-[6.778819561004639, 6.654563903808594, "[TT] Laser Connection of the SpaceDataHighway = More than 50,000 within the first five years"]
-[10.305148124694824, 3.945223093032837, "[FF] Attitude Control Duration of the Active solar or drag sails = Months or even years"]
-[8.06322956085205, 4.601247787475586, "[FF] Orbital Parameter Refinement of the STARE satellite = Reduce uncertainty in position estimation and improve accuracy of conjunction analysis"]
-[7.642467498779297, 8.794816970825195, "[TT] Spectral Band (\u00b5m) of the Spectral Bands = 0.402 - 0.422, 0.433 - 0.453, 0.480 - 0.500, 0.511 - 0.529, 0.555 - 0.575, 0.660 - 0.680, 0.745 - 0.785, 0.845 - 0.885"]
-[6.2303080558776855, 6.350203037261963, "[FF] Data Throughput of the BIROS = Unknown"]
-[8.244537353515625, -0.12998420000076294, "[TT] Bedrock Rise Rate of the Earth = About 10 mm a year"]
-[7.538336753845215, 0.9493371248245239, "[FF] URL of the Lunar Polar Hydrogen Mapper = https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20170009830.pdf"]
-[10.250846862792969, 8.123139381408691, "[TT] Telescope Aperture of the SIS (Scanning Imaging Spectrograph) = 25 x 50 mm"]
-[8.96968936920166, 5.665759563446045, "[TT] Pointing Accuracy of the ADCS = \u00b15\u00ba"]
-[14.166237831115723, 3.0951573848724365, "[TT] Mass of the BlackSky Pathfinder-1 = ~44 kg"]
-[4.439693450927734, 1.8164615631103516, "[FF] Presentation Date of the Core Radar Electronics = Sept. 29 to Oct. 3, 2008"]
-[8.39698314666748, 5.244612693786621, "[TT] Payload of the CRISTA-SPAS-2 = Three telescopes and four spectrometers"]
-[4.510910511016846, -0.9073271155357361, "[TT] Installation Date of the Dragon = 8 December 2019"]
-[5.136620998382568, 7.021896839141846, "[TT] Downlink Rate of the ASNARO = ~800 Mbit/s"]
-[1.7653508186340332, -2.059998035430908, "[FF] URL of the Hayabusa2 = http://global.jaxa.jp/activity/pr/brochure/files/sat33.pdf"]
-[8.522252082824707, 4.670279502868652, "[FF] Pointing Capability of the Satellite = Allows calibration using the sun, moon and stars"]
-[9.024497032165527, 4.442321300506592, "[FF] Sun Constraint of the STARE = The sun constraint shown in Figure 10"]
-[4.937239646911621, 0.2833365797996521, "[TT] Impact Date of the DART = October, 2022"]
-[10.226426124572754, 8.102556228637695, "[TT] Clear Aperture of the Etalon = 50 mm"]
-[11.839604377746582, 4.792953014373779, "[TT] Size of the NSX = 14.5 cm x 14.5 cm x 7 cm"]
-[14.275506973266602, 3.0582275390625, "[TT] Mass of the OTB-1 = 138 kg"]
-[8.691125869750977, 6.961648941040039, "[FF] Nodal Position of the PICO22 = Unknown"]
-[7.900575160980225, 0.8531877398490906, "[FF] Date of the Alaska Ablaze = 15 June 2022"]
-[13.446758270263672, 6.833409309387207, "[TT] Power of the LEOStar-3 = 1.2 kW"]
-[5.780818462371826, 0.43004852533340454, "[FF] Data Gap of the \u00d8rsted = Mid July 2006 through June 2007"]
-[11.200304985046387, 5.949631214141846, "[TT] Material of the Gnome Chompski = Titanium"]
-[6.9171061515808105, 7.775838375091553, "[TT] Reflector Diameter of the Instrument = 6.6 cm"]
-[4.065921783447266, 3.4616570472717285, "[FF] URL of the Galileo = https://www.esa.int/Applications/Navigation/406_Day_celebrating_Galileo_saving_lives"]
-[6.148761749267578, 3.4365792274475098, "[FF] Design Verification of the ESA Young Engineers Satellite 2 = FEM Analysis"]
-[9.085455894470215, 7.582739353179932, "[TT] Multispectral RGB Imagery Resolution of the WPM = 8 m"]
-[4.659352779388428, 1.1728910207748413, "[TT] Initial Deployment of the GSM = 1991"]
-[3.172203302383423, 3.956624746322632, "[TT] Development Status of the TerraSAR-NG System = Preliminary Design Phase"]
-[5.000189304351807, 3.2303550243377686, "[TT] Manufacturer of the CubeStack = LoadPath LLC of Albuquerque, NM"]
-[6.994121551513672, 6.520506381988525, "[FF] Unknown of the U.S. laser system = Unknown"]
-[5.126409530639648, 1.6738425493240356, "[TT] Development Status of the DST = Under development"]
-[8.034679412841797, 0.6146805882453918, "[FF] Data Usage of the NASA/GFZ GRACE-FO satellites = Groundwater data for the initial conditions"]
-[6.224297523498535, 4.030008316040039, "[FF] Avionics System of the DLR Compact-Satellite Series = Core"]
-[10.250951766967773, 3.1365301609039307, "[TT] Mission Quantity of the CubeStack = 2"]
-[16.544145584106445, 3.6366705894470215, "[TT] Number of Satellites Launched of the OneWeb = 36"]
-[5.2119340896606445, 3.0250461101531982, "[TT] Platform of the SOVA = Eureca"]
-[7.995781898498535, -0.3845731019973755, "[TT] Annual Maximum Extent Date of the Arctic Sea Ice = March 5"]
-[9.228556632995605, 5.108736991882324, "[TT] Y Axis Alignment of the SSM = Parallel to the velocity vector for spacecraft with ascending node in the afternoon/evening sector"]
-[7.929176330566406, 7.5470662117004395, "[FF] Conference Presentation Date of the EnMAP Hyperspectral Imager = July 31-Aug. 4, 2006"]
-[7.5624098777771, 3.538538694381714, "[FF] Type of the DebrisSats = DSAT-1"]
-[9.698607444763184, 0.3634691536426544, "[TT] Formation Distance of the PROBA-3 = 144 m"]
-[5.593729019165039, 4.313484191894531, "[FF] Satellite Network Provider of the Kongsberg Satellite Services = True"]
-[8.009112358093262, 8.82383918762207, "[TT] Lamps of the SOLSPEC = Two with tungsten"]
-[4.5222930908203125, 1.2689952850341797, "[TT] Launch Date of the AlSat-2 = 12 Jul 2010"]
-[12.686705589294434, 7.626068115234375, "[FF] Working Principle of the Instrument = Balance between the total amount of power received in the first and second half of the Dicke cycle"]
-[5.5422210693359375, 2.6134488582611084, "[FF] Development Team of the BeaverCube = Undergraduate and graduate students at the Massachusetts Institute of Technology"]
-[18.80048370361328, 3.4779648780822754, "[TT] Mean \u0394E (m) of the Dobbins = 3.9"]
-[8.260674476623535, 7.194751262664795, "[FF] Monoscopic Collection Capacity of the GIS Instrument = Up to 700,000 km2 of panchromatic imagery, Up to 350,000 km2 of pan-sharpened multispectral imagery"]
-[5.2940192222595215, 1.4755260944366455, "[TT] Report Recommendation of the SMAP = Highest priority among all proposed missions"]
-[7.345413684844971, 8.89494800567627, "[TT] Composition of the Filter = 30.7 nm aluminum and a 217.9 nm polyimide layer"]
-[3.626842975616455, 6.400136947631836, "[TT] Antenna Aperture in the Azimuth of the P Mode = 7.5 m"]
-[8.810589790344238, 3.7171213626861572, "[FF] Measured Parameters of the Special Sensor Ionospheric Plasma Drift / Scintillation Meter (SSI/ES-3) = Ambient electron density and temperature"]
-[5.9505462646484375, 0.9702069163322449, "[TT] Image Content of the DMAC = Snapshot of the Palm Jebel Ali"]
-[6.270503997802734, 6.6991400718688965, "[FF] Data Rate of the MWR = Unknown"]
-[6.874783992767334, 4.460028648376465, "[FF] Location of the Avionics = Fit in the other half of the chassis"]
-[7.089641571044922, 7.900463581085205, "[TT] Signal Strength Level of the RRA = Between LAGEOS and ETALON"]
-[13.200735092163086, 7.252209663391113, "[TT] Power Consumption of the RAMIS = 3 W \u2013 4 W"]
-[9.819405555725098, -0.10271281003952026, "[TT] Orbit Distance from Earth of the SWFO-L1 = Approximately 1.5 million kilometers"]
-[5.310844898223877, 3.9965007305145264, "[TT] Number of Satellites of the RapidEye = 5"]
-[9.58633804321289, 9.064491271972656, "[TT] Spatial Resolution of the IRIS Instrument = 10 m GSD"]
-[7.495971202850342, 6.283946990966797, "[FF] Displacement Observation of the Retroreflector = Twice the actual beam displacement"]
-[7.878269672393799, 1.520856261253357, "[FF] Purpose of the MSW = To understand the state of a volcanic eruption"]
-[5.97705602645874, 3.27616548538208, "[TT] Number of Institutions of the ASTRO-H = 58"]
-[6.475179195404053, 4.814880847930908, "[FF] Unknown of the Receiver Front-End = Unknown"]
-[9.136723518371582, 0.6831455230712891, "[TT] Distance to Ingenuity Mars Helicopter of the InSight = Roughly 2,145 miles (3,452 km)"]
-[3.8175079822540283, 7.921812534332275, "[TT] Modulation Scheme of the XMOD = QPSK"]
-[8.316442489624023, 0.7484532594680786, "[TT] Containment of the Calf Canyon-Hermits Peak fire = 29 percent"]
-[13.816615104675293, 2.677288770675659, "[TT] Launch Mass of the LADEE spacecraft = ~383 kg"]
-[3.570211410522461, -0.9720664620399475, "[TT] Orbit Type of the Vstar = Near-circular"]
-[7.934652805328369, 5.137221336364746, "[FF] Calibration Parameters of the SOFIE = Measurement background and noise, FOV, response linearity, relative spectral response, time response, absolute gain, difference signal gain"]
-[10.611531257629395, 3.386060953140259, "[TT] Form Factor of the Syrlinks EWC31 TT&C transceiver = CubeSat with a height of about 4 cm"]
-[9.561736106872559, -0.01974647119641304, "[TT] Expected Altitude Range of the RapidScat = Near 410 km mean altitude, plan for 375 km to 435 km"]
-[5.36014461517334, 5.829183101654053, "[TT] Protocol of the FODB = Asynchronous Transfer Mode (ATM) based"]
-[13.224786758422852, 7.1845269203186035, "[TT] Power Consumption of the HSC-III = 1.5 W"]
-[5.008432388305664, 3.196934938430786, "[TT] Manufacturer of the CubeSat power module = Clyde Space Ltd"]
-[4.907793998718262, 3.4274983406066895, "[TT] Manufacturer of the Pressurized Modules = MBB/ERNO-VFW Fokker (now EADS Space Transportation)"]
-[7.67349100112915, 1.6213051080703735, "[FF] Data Usage of the SeaSat = Better routing of ships with substantial savings in operating costs"]
-[7.261815071105957, 8.213055610656738, "[FF] Support Vectors of the GOSAT-2 CAI-2 = Unknown"]
-[5.840146541595459, -2.2584691047668457, "[TT] Orbital Altitude of the KOMPSAT-1 = 685 km"]
-[5.596370220184326, 5.696878910064697, "[TT] Processor of the Controller card = PowerPC processor"]
-[10.27784538269043, 2.043030261993408, "[FF] Discovery of the ASIM = Recently detected a unique gamma-ray burst from outer space"]
-[5.040615081787109, 7.348296165466309, "[TT] Symbol Rate of the Transmitter = 200 Msample/s"]
-[7.415315628051758, 5.421483516693115, "[FF] Detection Capability of the PROBA-V = Aircraft"]
-[14.364367485046387, 3.139591932296753, "[TT] Mass of the PTD-1 = 11 kg"]
-[8.704919815063477, -0.6663748621940613, "[TT] Resolution of the ICEYE-X1 = 3 m"]
-[5.749136924743652, -0.3777867257595062, "[TT] Mission Lifetime of the PROBA-3 = Over 2 years"]
-[10.96251106262207, 2.9364547729492188, "[TT] Dimensions of the PACE nanosatellite = 100 mm x 100 mm x 243 mm"]
-[9.653838157653809, -0.3023884892463684, "[FF] Altitude of the SARAL/AltiKa = Unknown"]
-[5.767185688018799, 1.1938836574554443, "[TT] Data Return of the IXPE = March 22, 2022"]
-[13.65080738067627, 5.8191680908203125, "[TT] Solar Panel Power Output of the AprizeSat = 15 W"]
-[9.858793258666992, 4.508177280426025, "[FF] Control Devices of the Attitude Control Subsystem = Reaction wheels and magnetic torquers"]
-[5.5060038566589355, 7.565301895141602, "[TT] -24 dB of the NESZ = -"]
-[8.371400833129883, 2.773474931716919, "[FF] Measurement Domain of the ROSE-L = Gravity and Magnetic Fields"]
-[7.744621753692627, 9.053744316101074, "[TT] Wavelength Range of the Spectral band 1 = 0.5 - 0.7 \u00b5m"]
-[4.451120376586914, 3.034841299057007, "[TT] Ground Stations of the TRACE spacecraft = Wallops, VA, and Fairbanks, Alaska"]
-[6.468364238739014, 4.170994281768799, "[FF] Simulation Levels of the SEXTANT ground testbed architecture = Level 0, Level 1, Level 2"]
-[8.389610290527344, 1.2716312408447266, "[FF] Modulation Technique of the RainCube = Offset IQ technique"]
-[8.94472599029541, 6.936315536499023, "[TT] Observation Range of the NAC = 50 - 550 m"]
-[8.241192817687988, 2.5296223163604736, "[FF] Purpose of the CATS = Study the impact of clouds and aerosols on global energy balance and climate feedback mechanisms"]
-[10.299090385437012, 3.1727607250213623, "[TT] Number of CubeSats of the CubeSat - Launch 4 = 7"]
-[7.071334362030029, 7.243925094604492, "[FF] Antenna Beams of the Optical layout = 3 antenna beams at \u03b8 = 25.8\u00ba, 33.8\u00ba, 40.3\u00ba incidence angles with respect to nadir (to shadow side of orbit)"]
-[8.040299415588379, 0.4234229028224945, "[FF] Confirmation of the MASCOT = Small fragments of carbon-rich asteroids are too fragile to survive entry into Earth\u2019s atmosphere"]
-[6.2788777351379395, 4.252036094665527, "[FF] Control Application Software of the ROSE-L = Developed and delivered by SPACEBEL"]
-[4.759264945983887, 5.705098628997803, "[TT] Type of the Tranet = Two-frequency Doppler"]
-[10.400506973266602, 7.319658279418945, "[TT] Ground Range x Product Length of the Stripmap = 30 x 50 km (single pol.); 15 x 50 km (dual pol.)"]
-[4.442867755889893, 3.806185722351074, "[FF] Satellite Usage of the Surveying System = EGNOS and Galileo satellites"]
-[12.161888122558594, 3.6258339881896973, "[TT] Maximum Capacity of the Xenon Gas Tank = 82 kg"]
-[10.512608528137207, 1.4399027824401855, "[TT] Number of Stars of the Upper Centaurus Lupus = 134"]
-[8.18450927734375, 7.43723201751709, "[TT] CCD Detector of the PS2 = 29MP"]
-[10.407288551330566, 2.126154899597168, "[FF] Wavelengths of the NuSTAR = Almost the whole range of X-ray wavelengths"]
-[7.3152337074279785, 2.42398738861084, "[FF] Cross Correlation Validation of the Image Processing Facility = Global Landsat Survey GLS 2000 cloud free dataset"]
-[6.248507976531982, 1.034591555595398, "[TT] Image Acquisition Date of the Landsat-8 = October 18, 2021"]
-[9.982391357421875, 2.7926762104034424, "[TT] Total Small Satellite Deployments by NanoRacks of the CubeSats = 217"]
-[6.839437961578369, 4.408538341522217, "[FF] Unknown of the RCC = Unknown"]
-[6.668432235717773, 7.55873441696167, "[TT] A/D Conversion of the VEU = 12-bit"]
-[7.971858501434326, 1.5298120975494385, "[FF] Data Contribution of the DPR = Global database of precipitation characteristics"]
-[8.928922653198242, 7.494884490966797, "[TT] GSD of the Detector assembly = 15 m"]
-[7.14231538772583, 7.30165958404541, "[TT] Data Set of the MABEL and ATLAS = Just a few dozen photons at most"]
-[7.917514801025391, 1.1889604330062866, "[FF] Fine Spatial and Temporal Resolutions and Accuracies of the Satellites = Essential for water cycle and global change research"]
-[14.326337814331055, 3.1046907901763916, "[TT] Mass of the Pratham = ~10 kg"]
-[13.93590259552002, 7.108269214630127, "[TT] Voltage of the Satellite power bus = 4.0 V"]
-[6.761267185211182, 5.564457416534424, "[FF] Performance Assessment of the GSTB-V2 = Unknown"]
-[5.598021507263184, 1.0351111888885498, "[FF] Test Completion Date of the Integrated Circuit Boards = June 2019"]
-[7.965235710144043, 6.941812992095947, "[FF] Triggering Strategy of the PH1 = Search the occurrence of a sharp peak inside each photometer waveform"]
-[11.366732597351074, 4.490856647491455, "[TT] Size of the PolyITAN-2-SAU = 2U"]
-[13.257989883422852, 7.359165191650391, "[TT] Power Supply Voltage of the GPS OEM Sensor = 3.3 VDC"]
-[8.980749130249023, 5.234010696411133, "[TT] Type of the Interferometric fiber optic gyro = Interferometric fiber optic gyro"]
-[5.629350185394287, 7.002238750457764, "[TT] Data Transfer Rate of the SSRNI = 7.68 Mbit/s"]
-[3.2599027156829834, 5.647785663604736, "[TT] Size of the L-band SAR antenna = 9.9 m (azimuth) x 2.9 m (elevation)"]
-[6.957876205444336, -0.4942680597305298, "[TT] Orbit Frequency of the GRACE = About 15 times a day"]
-[2.0246827602386475, -0.3305467665195465, "[FF] Trajectory of the Orion = Lingering for many hours in the Van Allen radiation belts"]
-[11.606939315795898, 4.392862796783447, "[TT] Size of the Sun Diffuser = 700 x 250 mm2"]
-[5.688327789306641, 4.980838298797607, "[FF] Purpose of the SpaceLink = Provide real-time connectivity between space and the ground"]
-[8.73250675201416, 8.831451416015625, "[TT] Flatness of the Grating = 10 \u03bb (6348 nm)"]
-[8.408289909362793, 1.332155704498291, "[FF] Soil Moisture Maps of the Aquarius = July 7, 2014"]
-[9.011152267456055, 5.7183685302734375, "[TT] Configuration of the Inertial Sensors = Concentric coaxial cylinders"]
-[4.781075954437256, 0.6359496712684631, "[TT] Transmitter Fault Date of the MicroMAS-1 = August 2015"]
-[13.849061012268066, 2.816244602203369, "[TT] Launch Mass of the GOES-S = ~4,990 kg"]
-[10.252628326416016, 7.115696430206299, "[TT] Ground Spot Size of the HRS = 10 km x 100 km"]
-[4.788537979125977, 0.6966326832771301, "[TT] Launch Year of the OCO-2 and OCO-3 = 2014 and 2019"]
-[4.7512078285217285, 8.0400390625, "[TT] Frequencies of the CERTO = 150, 400 and 1067 MHz"]
-[7.655177593231201, 4.844351291656494, "[FF] Function of the Onboard Attitude Estimation Software = Provide \u2018ground truth\u2019 data against which the navigation algorithms will be compared for validation and performance assessment"]
-[13.070690155029297, 7.257094383239746, "[TT] Power Consumption of the TOTEM SDR = Low"]
-[2.3330087661743164, 1.3155628442764282, "[FF] Subsystem of the NanoSail-D2 = Sail"]
-[4.017430305480957, 2.1717495918273926, "[FF] Upper Stage Functions of the Atlas-Agena launch vehicle = Power, telemetry, attitude control, command and control"]
-[2.943167209625244, 4.460097789764404, "[TT] Spotlight Mode Resolution of the PALSAR-2 = 1 m x 3 m"]
-[14.592238426208496, 6.62868595123291, "[TT] Battery Type of the PCU = Li-ion"]
-[4.996448516845703, 0.6167923808097839, "[TT] Launch Date of the GFO = Feb. 10, 1998"]
-[6.156022548675537, 5.111664772033691, "[FF] Main Task of the OBSW = Keep an autonomous and safe operation environment, ensure housekeeping data generation and collection, manage communications windows, manage on board time, manage and execute TC"]
-[7.806867599487305, 8.433995246887207, "[TT] Wavelength Range of the HSC-III = 450-1000 nm"]
-[5.273246765136719, 5.003166675567627, "[TT] Network of the Data Downlink Stations = Global"]
-[9.392082214355469, 4.528611660003662, "[FF] Performance of the SpinKF = Very well"]
-[11.51207160949707, 4.841462135314941, "[TT] Diameter of the OPS = 2 cm"]
-[10.73246955871582, 2.765892505645752, "[TT] Number of Microsatellites of the BlackSky Constellation = 60"]
-[8.444716453552246, 6.157064437866211, "[TT] Single Shot Precision of the TDC-GPX = 10 ps"]
-[7.527716636657715, 3.2285473346710205, "[FF] Data Type of the Tropospheric Monitoring Instrument (TROPOMI) = High-resolution fluorescence data"]
-[8.206025123596191, 8.422779083251953, "[TT] Main Imager Spectral Wavelengths of the PROBA-1 = 18 programmable visible and near-infrared wavelengths"]
-[10.464813232421875, 1.9924763441085815, "[FF] X-ray emission source of the NuSTAR = Realized it was the same object as this likely pulsar"]
-[7.189485549926758, 5.470468997955322, "[FF]  of the MW = "]
-[5.2236738204956055, 4.049958229064941, "[TT] Bus Type of the NorSat-1 = Nanosatellite and a small microsatellite"]
-[5.634578227996826, 2.9333930015563965, "[TT] Post-Project Careers of the SAPPHIRE = Three are involved in strong system-based research and management in industrial or government laboratories"]
-[9.056906700134277, 9.968618392944336, "[TT] Spectral Bands of the Eastman Kodak KLI14403 linear CCD sensor = 0.52-0.62 \u00b5m (green), 0.63-0.69 \u00b5m (red), and 0.76-0.9 \u00b5m (NIR)"]
-[5.82424259185791, 3.403064012527466, "[FF] Mission of the ArgoMoon = Perform proximity operations with the ICPS post-disposal and record imagery of engineering and historical significance \u2014 as well as of the Earth and moon"]
-[4.665560245513916, 7.652477741241455, "[TT] G/T of the Uplink (VHF) = 30 dBK"]
-[6.98555326461792, -0.3424503803253174, "[TT] Signal Reception Time of the MarCO-B = 11:16 am"]
-[10.311962127685547, 3.2013514041900635, "[TT] Compatibility of the GAMALINK = CubeSat standard compatible version"]
-[8.729366302490234, 0.19686894118785858, "[TT] Distance from the Sun of the Comet 67P/C-G = About 1.7 au"]
-[11.798341751098633, 6.743739128112793, "[TT] Electron Pass Energy of the Dosimeter A = Greater than 50 keV"]
-[8.37975025177002, 7.755878448486328, "[TT] Detector Array of the ISIR = Approximately 80,000 detectors"]
-[9.565760612487793, 9.214125633239746, "[TT] Development Time of the IRIS = One year"]
-[11.618439674377441, 5.422325134277344, "[TT] Effective Area of the XRD = 17 cm2"]
-[8.55809211730957, 6.219603061676025, "[TT] Relative Accuracy of the 215 nm Band = 1000 ppm"]
-[10.45566177368164, 2.1776154041290283, "[TT] Exposure Time of the eROSITA X-ray telescope = More than 500 seconds"]
-[8.939810752868652, 4.456316947937012, "[TT] Quantity of the Fine and Coarse Sun Acquisition Sensors (FSAS and CSAS) = 1 of each on each S/C"]
-[7.553437232971191, 3.7541632652282715, "[TT] Focal Length Limit of the NightPOD = 180 mm"]
-[3.2974424362182617, 2.2659647464752197, "[FF] Level-1 SLC Products of the Sentinel-1 = Focused data in slant-range geometry, single look, containing phase and amplitude information"]
-[4.898066520690918, -2.1730010509490967, "[TT] Propellant Left of the Chang'e-2 = 520 kg"]
-[9.315832138061523, 7.4087677001953125, "[TT] Resolution - Ground (Nadir) Infrared Channel of the VIRR = 4.4 km"]
-[6.879899024963379, -0.6745790243148804, "[TT] Orbital Period of the Binary = 6.91 minutes"]
-[10.836397171020508, 0.9338870644569397, "[TT] Radius Precision of the Exoplanet GJ 367 b = 7 percent"]
-[8.31076431274414, 4.616081714630127, "[TT] Polar Motion Improvement (y-component) of the LARES = 18.7%"]
-[3.687992811203003, 4.731329917907715, "[FF] Mode of the RADARSAT-2 = ScanSAR Wide mode"]
-[8.430703163146973, 5.75426721572876, "[TT] Data Accuracy of the AMS Experiment = ~1%"]
-[9.649131774902344, -0.3405095040798187, "[FF] Altitude of the NASA ER-2 = High"]
-[6.729439735412598, 5.782925605773926, "[TT] Quantity of the ORS-7 = Two"]
-[4.900504112243652, -0.1588122397661209, "[FF] Development Date of the TAIKI = Unspecified"]
-[10.731348991394043, 2.951479434967041, "[FF] Components of the PACE nanosatellite = COTS (Commercial off-the-Shelf) components as well as in-house developed parts"]
-[13.364748001098633, 5.678846836090088, "[FF] Purpose 1 of the PW-Sat = System test of a flexible solar generation system"]
-[4.3800811767578125, -0.0039775618351995945, "[FF] Software Glitches of the Starliner = Major software error, communications dropouts, another software mistake"]
-[4.432914733886719, 2.7382428646087646, "[FF] Location of the WINDS transportable station = Kesennuma and Higashimatsushima"]
-[11.830402374267578, 3.247932195663452, "[TT] Thrust of the Bipropellant Thrusters = 9.25 N"]
-[8.750469207763672, 2.3681163787841797, "[TT] Dust Composition of the EXCISS = Forsterite (Mg2SiO4)"]
-[7.487128257751465, 3.6004984378814697, "[FF] Data of the NightPod = Atmospheric phenomena"]
-[6.079994201660156, 7.304588794708252, "[TT] Wordlength of the BAC = Normally 4 bits I + 4 bits Q"]
-[6.191899299621582, 1.815211534500122, "[FF] URL of the SCD-2 = http://www.inpe.br/programas/mecb/ingl/satellite/scd2/scd2.htm"]
-[4.702682971954346, 8.108859062194824, "[TT] Frequency of the W-band = 77 GHz"]
-[3.1931095123291016, 1.8099291324615479, "[TT] Image Acquisition Date of the Sentinel-1A = 2014"]
-[10.490386009216309, 6.465145111083984, "[FF] Development Date of the Mirror Modules = Sept. 2013"]
-[13.845803260803223, 5.675014495849609, "[TT] Reduced Efficiency of the Solar Panels = 26.5%"]
-[8.540969848632812, 4.8832197189331055, "[FF] Pointing Stability of the Hosting satellite = Required"]
-[6.470647811889648, 0.06551190465688705, "[FF] Mission Duration of the Solar Maximum Mission = 14 Oct.. 1984 - 15 April 1986"]
-[4.844509124755859, 3.2068445682525635, "[TT] Manufacturer of the Sentinel-2B = EADS-Astrium GmbH"]
-[5.116724491119385, 3.353835105895996, "[TT] Manufacturer of the SBSS-1 Pathfinder = Boeing"]
-[5.6035261154174805, -0.3804973363876343, "[TT] Deployment Time of the Kibo module = 10:05 UTC"]
-[10.175337791442871, 0.9956448078155518, "[TT] Distance from Earth of the Swift J1818.0-1607 = 16,000 light-years"]
-[6.716446876525879, 3.283538579940796, "[TT] Increase in Observations of the SBSS-1 = Fivefold"]
-[3.7242231369018555, 2.4674065113067627, "[TT] User Types of the Iridium NEXT = Commercial and government users"]
-[4.585813522338867, 4.816492080688477, "[FF] Purpose of the AIS = Broadcasts a ship's identification, position and other maritime navigational data"]
-[6.14918327331543, 7.349236488342285, "[FF] Log Amp Bias of the Signal Processing = Log Amp termination mode"]
-[8.742222785949707, 4.7504682540893555, "[FF] Star Tracker Noises Consideration of the Sentinel-2 = By covariance tuning"]
-[9.830979347229004, -0.6286242008209229, "[TT] Orbit Altitude of the SpaceEye-T = 600 km"]
-[8.92228889465332, 7.585338115692139, "[TT] GSD of the Pushbroom imager = 1.5-2.5 m"]
-[9.073291778564453, 5.069182395935059, "[TT] Gyro Tilt Detection of the SQUID = 0.1 milliarcseconds"]
-[5.4561991691589355, 7.911332607269287, "[TT] Frequency Stability Limit of the Spacer = One order of magnitude lower than the adopted goal"]
-[8.643808364868164, 8.505073547363281, "[TT] Field of View of the Electron Spectrometer = Nearly 4\u03c0"]
-[5.666320323944092, 0.919106125831604, "[TT] Imaging Date of the STEREO-A = June 5, 2020"]
-[7.671223163604736, 9.086671829223633, "[TT] Spectral Range (\u00b5m) of the Band 5 = 11.5 - 12.5"]
-[13.206830024719238, 7.259354591369629, "[TT] Power Consumption of the ACC = 800 mW"]
-[4.621297359466553, 2.5933210849761963, "[FF] Collection Areas of the HawkEye 360 = Mediterranean, South China Sea, Korean Peninsula"]
-[5.964839935302734, 1.8064708709716797, "[FF] Presentation Date of the VIIRS = June 20-24, 2005"]
-[11.82281494140625, 4.7891764640808105, "[TT] Size of the Sundancer = ~180 m3"]
-[4.155169486999512, 7.002573013305664, "[FF] Frequency Band of the X-band antennas = X-band"]
-[4.395509243011475, 7.856143951416016, "[TT] Downlink Frequency of the RF communications = 436.450 MHz"]
-[5.7917985916137695, 0.9318225979804993, "[FF] Approval Date of the BepiColombo = November 2009"]
-[10.765070915222168, -1.1267513036727905, "[FF] Orbit Transfer Status of the Super Low Altitude Test Satellite (SLATS) = Ongoing"]
-[6.26944637298584, 3.570378065109253, "[TT] Quantity of the Primary demonstration experiments = 2"]
-[6.152463912963867, 2.297269105911255, "[FF] Principal Investigator of the TEMPEST-D = Steven Reising"]
-[4.03711462020874, 3.4997384548187256, "[TT] Mission Type of the Galileo = Non-EO"]
-[3.737455129623413, -1.0859748125076294, "[TT] Orbit Type of the IBEX = Highly Elliptical Orbit"]
-[5.182723045349121, 5.910356044769287, "[TT] Router External Links of the SpaceWire ASIC = 4"]
-[10.237868309020996, 7.504968643188477, "[TT] Telescope Type of the OPS = TMA (Three Mirror Anastigmat)"]
-[5.169247150421143, 2.65128755569458, "[TT] Outreach Program Location of the NuSTAR = Sonoma State University, Rohnert Park, Calif"]
-[8.54350471496582, 8.11426830291748, "[TT] Spectral Resolution of the MicrOmega/MASCOT = 20 cm-1"]
-[7.311983585357666, 1.7147175073623657, "[FF] Coverage of the ERS Tandem Mission = Nearly the whole global land surface"]
-[5.413319110870361, 5.48314094543457, "[TT] Interface Types of the SGR-ReSI = CAN, RS422, SpaceWire"]
-[9.354742050170898, 5.1060967445373535, "[TT] Yaw Axis Flip Angle of the Trail Spacecraft = 180\u00ba"]
-[9.700932502746582, 7.4428277015686035, "[TT] Image Span of the BlackSky Pathfinder-1 = 10 km x 3 km"]
-[6.539194107055664, 3.8594510555267334, "[FF] Launch Mass of the PARASOL = Unknown"]
-[5.697916507720947, 3.2445294857025146, "[TT] Prize Amount of the Google Lunar X-Prize = $20 million"]
-[8.507966995239258, 6.106689929962158, "[TT] Accuracy of the CERES = 0.6 Wm -2  sr -1"]
-[8.596660614013672, 3.1659555435180664, "[FF] Formation Mechanism of the Ozone Layer = Photodissociation of stratospheric molecular oxygen by solar middle and far ultraviolet radiation"]
-[7.452641487121582, 4.703265190124512, "[FF] Microcontroller of the Sensor Suite = Shared"]
-[3.807508945465088, -1.138653039932251, "[FF] Function of the Propulsion Subsystem = Support trajectory maneuvers to L2 and maintain the halo orbit at L2"]
-[7.635217666625977, 5.308841705322266, "[TT] Scanning of the Satellite = Always \"looked down\""]
-[5.9996113777160645, 5.426553249359131, "[TT] Operations Support of the TGO = Yes"]
-[9.50964641571045, 8.113277435302734, "[TT] Focal Plane Format of the EXI instrument = 12.6 MP 4:3 format"]
-[6.17514181137085, 5.547603607177734, "[FF] Data Compression of the Ground Segment = Prior to transmission to the ground"]
-[8.322576522827148, 6.883198261260986, "[TT] Pixel Type of the MWIR Imager = MWIR"]
-[9.04819393157959, 0.5014857649803162, "[TT] Parking Orbit Achievement Date of the ARTEMIS = Aug. 24, 2001"]
-[7.276947498321533, 6.666982650756836, "[TT] Model of the Laser Rangefinder = Jenoptik DLEM-SR"]
-[4.616744518280029, 5.965835094451904, "[TT] CW Beacon Frequency of the HORYU-2 = 437.375 MHz"]
-[7.636381149291992, 2.9270858764648438, "[FF] Purpose of the LIDAR and wide-field camera instruments = Measure air quality and detect global methane emissions"]
-[11.800077438354492, 6.738727569580078, "[TT] Energy Range of the XGRE = 20 keV - 10 MeV"]
-[10.971348762512207, 2.065337657928467, "[FF] Article Date of the XMM-Newton = July 12, 2016"]
-[8.719278335571289, 3.696124792098999, "[FF] Inclusion Plan of the Energetic Charged Particle sensors = On all future satellites"]
-[4.9500508308410645, 0.9321064949035645, "[TT] Business Support Start Date of the OPS-SAT = 01 October 2021"]
-[3.516491413116455, -0.8457764983177185, "[TT] Orbit Type of the Alba Cluster 3 = SSO (Polar)"]
-[7.617844581604004, -0.4144652783870697, "[FF] Publication Date of the Spain's Chilly Blanket Image = 13 January 2021"]
-[10.299118995666504, 5.649220943450928, "[TT] Cooling Temperature of the Radiative Cooler = 83 K"]
-[6.185598850250244, 4.348881721496582, "[FF] Design Goal of the EGS = Disassociate space missions from pipeline ground system approaches and standardize ground system software, hardware, and interfaces"]
-[9.561407089233398, 9.075228691101074, "[TT] Emission Detection Capability of the Iris = 100 times smaller than any other satellite"]
-[3.7748208045959473, 4.665807247161865, "[TT] Swath Positions of the RADARSAT-2 = 31"]
-[4.992068290710449, 4.310766696929932, "[FF] ITU Approval of the Starlink = Required"]
-[4.839820384979248, 8.263436317443848, "[TT] Frequency Band of the AMSU = 50 to 60 GHz"]
-[5.658000469207764, 6.43519926071167, "[TT] Quantity of the Frequency generation and up-conversion units = 2"]
-[14.360806465148926, 6.405826091766357, "[TT] Components of the IMPS = Thin-film photovoltaic array, thin-film lithium-ion battery"]
-[8.954305648803711, 5.412728309631348, "[TT] Pointing Accuracy of the GOMX-3 = 3\u00b0"]
-[7.1695966720581055, 6.625838279724121, "[TT] Integration Time of the Radiometer = 65 ms"]
-[5.5196051597595215, 0.814129114151001, "[FF] Arrival Date of the E-THEMIS = Unknown"]
-[4.436797618865967, 2.3589260578155518, "[TT] Manufacturer of the KhalifaSat = MBRSC (Mohammed Bin Rashid Space Center)"]
-[5.258026599884033, 6.914831638336182, "[TT] Max Data Rate (Mbit/s) of the SDR-VSAT = Uplink: 622 Downlink: 622"]
-[8.988218307495117, 0.5067098736763, "[FF] Size Discrepancy of the Impact Basins = Up to twice the diameter"]
-[9.8765287399292, -0.35341963171958923, "[TT] Altitude Range of the RAIDS = 100 to 200 km"]
-[9.135445594787598, 2.774229049682617, "[FF] Occurrence of the Solar Flare = Second largest to have occurred from the past 11-year solar cycle"]
-[4.792010307312012, 7.105352401733398, "[TT] Downlink Data Rate of the S-band system = 102 MB/day"]
-[13.606918334960938, 2.0316662788391113, "[TT] Total Cargo of the QBITO = 3380 kg"]
-[8.624448776245117, 5.134480953216553, "[TT] Accommodation Requirement of the ACC (Accelerometer) = Precise and stable in CoG (Center of Gravity)"]
-[12.042272567749023, -0.1523546278476715, "[TT] Sky Section Size of the TESS = 24 x 96 degree"]
-[11.986948013305664, 4.463447093963623, "[TT] Spacecraft Size of the ArgoMoon = 6U"]
-[4.765884876251221, -1.7611302137374878, "[FF] Landing Camera Type of the Chang'e-2 = Brand-new"]
-[9.95221996307373, -1.5621317625045776, "[TT] Inclination of the Explorer 36 = 105.8\u00ba"]
-[7.857605934143066, 8.305455207824707, "[FF] Minimum Value of the Spectral Angle = Achieved when the red panel is prominent on the satellite"]
-[10.354065895080566, 3.227898597717285, "[TT] URL of the SUM = http://www.cubesat.org/images/stories/workshop_media/DevelopersWorkshop2013/Maly_MoogCSA_ESPA-SUM.pdf"]
-[3.328636407852173, 1.4463037252426147, "[TT] Replacement Year of the Sentinel-2C = 2024"]
-[6.320209503173828, 2.679422616958618, "[TT] Operator of the SORCE = LASP (Laboratory for Atmospheric & Space Physics) of the University of Colorado"]
-[5.676295757293701, 7.194597244262695, "[TT] Bit Rate of the SBUV/TOMS = 4 kbit/s"]
-[8.211544036865234, 5.178025245666504, "[FF] Accuracy of the EO System = 0.3%, k = 2"]
-[10.369471549987793, 3.2093257904052734, "[TT] Quantity of the CubeSats = 6"]
-[13.62121868133545, 5.874485492706299, "[TT] Backup Power Output of the Solar Array = 55Ah NiCd (Nickel-Cadmium) battery charge power requirement"]
-[5.583293437957764, -2.017899513244629, "[FF] Image Resolution of the KOMPSAT-3 = Unspecified"]
-[6.540077209472656, 4.851018905639648, "[FF] Malfunction of the BCRs = Detected"]
-[14.614113807678223, 6.771883010864258, "[TT] Battery Configuration of the EPS = 8 in series"]
-[11.723489761352539, 4.652946949005127, "[TT] Height of the Nimbus-7 S/C = 3.04 m"]
-[13.952463150024414, 3.754469633102417, "[TT] Form Factor Weight of the Compact Laser Comms Terminals (CLCT) = Less than 2 kg"]
-[7.071106910705566, -0.1764308512210846, "[TT] Duration of the Solar Eclipse = About two hours"]
-[8.731070518493652, 2.0967655181884766, "[TT] Wind Direction Accuracy of the NSCAT = 20\u00ba (rms)"]
-[7.109842777252197, 5.559379577636719, "[FF] Quantity of the MSU-MR = 2"]
-[8.722633361816406, 7.438314914703369, "[TT] Silicon Thickness of the L0 Detector = 12 \u00b5m"]
-[9.251442909240723, 1.9034007787704468, "[FF] Operation of the LRF-S2 = During touchdown, the sampler horn will compress as it touches the surface of Ryugu"]
-[8.726879119873047, 6.8269171714782715, "[TT] Generation of the DMC-1 = First"]
-[11.045735359191895, 5.2653961181640625, "[TT] Separation of the MMS = Tens of km to a few hundreds of kilometers"]
-[7.426550388336182, 2.3408362865448, "[FF] Coverage of the TT&C System = Full spherical coverage in uplink and downlink"]
-[6.786386966705322, 7.480690956115723, "[TT] Beam Width of the RA-1 = 1.3\u00ba"]
-[9.304644584655762, 8.652961730957031, "[TT] Exit Slit of the UVS Instrument = 2 x 4 mm"]
-[10.438715934753418, 7.0679802894592285, "[FF] Design Basis of the OAP (Off-Axis Parabola) mirrors = COTS (Commercial Off-The-Shelf ) diamond-turned"]
-[3.2354698181152344, 5.013861656188965, "[TT] Footprint of the Seasat SAR sensor = 100 km x 15 km (3 dB contour)"]
-[10.188636779785156, 1.5879082679748535, "[FF] Energy Release of the Ophiuchus Galaxy Cluster = Hundreds of thousands of times more than typical clusters"]
-[7.963886260986328, 1.6109410524368286, "[FF] Effect of the Deep Ocean Trenches = Producing a dip on the sea surface"]
-[9.496733665466309, 6.809972763061523, "[TT] Range Resolution of the Wide standard Quad-Pol = 9-30.0 m"]
-[5.33872652053833, 1.090031623840332, "[FF] Presentation Date of the SEDA-AP = August 3-6, 2010"]
-[9.066129684448242, 5.929460525512695, "[TT] Off-Track Look Capability of the NEMO-AM = 30\u00ba"]
-[9.887287139892578, 7.936751842498779, "[TT] F-Number of the Telescope = 3.1"]
-[7.631505966186523, -2.406219959259033, "[FF] Data Center of the GOLD = Collect, process, and distribute the science data for the mission"]
-[8.314549446105957, 7.974244594573975, "[TT] Band of the SWIR Camera = 0.9-1.7 \u00b5m"]
-[7.408252716064453, 3.711644172668457, "[TT] Data Interface of the NightPod = USB"]
-[8.054941177368164, 5.038190841674805, "[FF] Typical Value of the O3 Profile = 40, 50, 8 x 10 3"]
-[8.999165534973145, 7.480663776397705, "[TT] Multispectral GSD of the CCD Pushbroom Camera = 10m"]
-[7.87598180770874, 2.220628499984741, "[FF] Purpose of the SGLI = Measure ocean color, SST (Sea Surface Temperature), land use and vegetation, snow and ice, clouds, aerosols and water vapor"]
-[3.740885019302368, 4.934581756591797, "[FF] Mode Name of the Poseidon 4 = InterLeaved Mode"]
-[5.333486080169678, 7.152530670166016, "[TT] Communication Link Speed of the GEO LCT = 2.8 Gbit/s"]
-[11.980623245239258, -0.4133244454860687, "[TT] Mission Classification of the TESS = SMEX (Small Explorer) Class Mission"]
-[4.6672682762146, 8.100536346435547, "[TT] Chirp Generation Method of the Ty module = Direct digital synthesis at an IF of 150 MHz"]
-[11.062596321105957, 5.409316062927246, "[TT] Superelastic Plateau Stress of the Superelastic SMA = Between 200 and 300 MPa"]
-[6.555027008056641, -0.42919063568115234, "[TT] Repeat Cycle of the MSU-E = 18 days"]
-[12.401789665222168, 3.2332398891448975, "[TT] Total propellant used of the Deorbit = 23 g"]
-[5.660212993621826, 5.714991569519043, "[TT] Software of the TPMU = 8051 Pascal mode"]
-[10.363395690917969, 2.7121574878692627, "[TT] Data Downlink Time from Nanosatellite of the HyperScout 1 = Several weeks"]
-[5.589825630187988, -2.0053069591522217, "[FF] Advanced Meteorological Imager (AMI) Development of the GEO-KOMPSAT-2A = Unknown"]
-[14.625380516052246, 6.662317276000977, "[TT] Cell Type of the Two 6-cell NiCd battery packs = NiCd"]
-[8.34426212310791, 5.434658050537109, "[TT] Tracking System Accuracy of the AMS-02 = Microns level"]
-[9.462404251098633, 4.7544355392456055, "[TT] Secondary Attitude Sensor of the ADCS = SCDM"]
-[11.724907875061035, 3.4122774600982666, "[TT] Electric Power of the Ion engine = 370 W @ 10 mN"]
-[6.592579364776611, 6.187320232391357, "[TT] Expected Level of the TRL = 6"]
-[5.847710609436035, 1.6618324518203735, "[FF] Operational Acceptance Date of the Lockheed Martin Defense Weather Satellite = Sept. 16, 2014"]
-[7.6894612312316895, 6.401237964630127, "[TT] Range of the Rangefinder Module = 500 km"]
-[5.988725662231445, 4.760063171386719, "[FF] Purpose of Point-to-Point Communication of the MCS = Commanding"]
-[5.755067348480225, -2.157322406768799, "[TT] Body Pointing Capability of the KOMPSAT-3 = \u00b145\u00ba"]
-[10.912008285522461, 0.8950403332710266, "[FF] Eclipsing Behavior of the ZTF J1539+5027 = The white dwarfs eclipse each other as viewed from Earth"]
-[3.1400558948516846, 2.2125656604766846, "[TT] Former Name of the Copernicus = GMES (Global Monitoring for Environment and Security) program"]
-[8.317453384399414, -0.8473146557807922, "[TT] Ice\u2010sheet elevation changes accuracy of the ATLAS = 0.4 cm/yr"]
-[8.746610641479492, 3.0857622623443604, "[FF] Authors of the Wide-Field Imager for Solar Probe+ = Angelos Vourlidas, Russell A. Howard, Simon P. Plunkett, Clarence M. Korendyke, Michael T. Carter, Arnaud F. R. Thernisien, Damien H. Chua, Peter Van Duyne, Dennis G. Socker, Mark G. Linton, Paulett C. Liewer, Jeffrey R. Hall, Jeff S. Morrill, Eric M. DeJong, Zoran Mikic, Pierre L. P. M. Rochus, Volker Bothmer, Jens Rodman, Philippe Lamy"]
-[5.314560890197754, 8.474557876586914, "[TT] Operating Frequency of the Passive Microwave Spectrometer = Near the 118.75 GHz oxygen absorption line"]
-[6.585144996643066, -0.463839054107666, "[TT] Revisit Frequency of the Spacecraft = Maximum of 4 days"]
-[5.786587238311768, 2.467487096786499, "[FF] Phase of the OPS-SAT = A-B1"]
-[8.584670066833496, 5.993963241577148, "[TT] Accuracy of the NIDEM = High"]
-[7.160351276397705, 2.015779495239258, "[FF] Surface Features of the WISPR = Aphrodite Terra, Tellus Regio plateau, Aino Planitia plains"]
-[7.601088523864746, -0.8257795572280884, "[TT] Launch Date of the ICESat-2 = September 2018"]
-[11.953356742858887, 4.993425369262695, "[TT] Dimensions of the RPU = 195 mm x 280 mm x 365 mm"]
-[11.535823822021484, 5.180057525634766, "[TT] Module Depth of the ECAL = 18 mm"]
-[5.7517008781433105, -0.33954304456710815, "[TT] Deployment Duration of the ATEx = 18 minutes"]
-[10.282940864562988, 5.390946865081787, "[FF] Heat Load Minimization of the TCS (Thermal Control Subsystem) = By not allowing any object to come into the FOV of the coolers and incorporating a bi-annual yaw rotation of the spacecraft"]
-[8.413607597351074, 8.100025177001953, "[TT] Multi-channel Observation Capability of the AMI = 16 channels (4 VIS and 12 infrared)"]
-[6.534802436828613, 6.7944560050964355, "[TT] Data Collection Interval of the High-voltage experiment = 1 minute"]
-[7.5592145919799805, 8.014891624450684, "[TT] Type of the HD 93396 = Subgiant yellow"]
-[3.765275478363037, -1.0200772285461426, "[FF] Purpose of Orbit Parameters of the LAGEOS = Minimizing the effects of disturbing forces"]
-[5.091434955596924, 6.3301167488098145, "[TT] Data Transfer Interfaces of the UVN-DEMs and SWIR modules = 140 Mbit/s Channel Link interfaces, 80 Mbit/s SpaceWire interface"]
-[7.094918727874756, 3.0376644134521484, "[FF] Data Application of the DAICHI = Compilation of Global Digital 3D Map with World's Best Precision"]
-[10.829078674316406, 0.7314797043800354, "[TT] Planet Sizes of the TRAPPIST-1 = Very close to the size of Earth"]
-[9.775334358215332, -0.5797407031059265, "[TT] Orbit Altitude of the Aalto-1 = 505 km"]
-[8.09893798828125, 2.4970972537994385, "[FF] Purpose of the UVI = Improve the atmospheric correction accuracy of high turbid water in the near shore"]
-[9.561004638671875, 0.9858891367912292, "[TT] Speed of the Rosetta = 8.6 km/s"]
-[3.8414580821990967, 1.5876221656799316, "[TT] First Stage Engine of the Falcon 9 = Retro Rocket"]
-[9.41709041595459, 6.296128273010254, "[FF] Device of the GLI scan mirror = GLI scan mirror"]
-[10.041971206665039, 7.678718090057373, "[TT] Co-aligned Telescopes of the ASTRO-1 = 3"]
-[12.78364372253418, 2.0597856044769287, "[TT] FOV Elevation of the SAGE-III = -24.81 to -31.02\u00ba"]
-[6.587538719177246, 4.594893932342529, "[FF] Purpose of the GIPSY-OASIS = Earth orbit determination using GPS data"]
-[3.456275224685669, -0.9183766841888428, "[TT] Orbit Type of the WV-1 = Sun-synchronous circular"]
-[9.690579414367676, 0.32300999760627747, "[TT] Distance Between Disc and Satellite of the PROBA-3 = 150 m"]
-[5.208589553833008, 8.390979766845703, "[TT] Channel Bandwidth of the Channel = 100 MHz"]
-[9.45674991607666, 5.609034538269043, "[TT] Location of the Scanwheel assemblies = Near the forward end on the tubular supports"]
-[6.989995002746582, 6.998850345611572, "[TT] PER of the Laser = > 100:1"]
-[10.474177360534668, 1.824600338935852, "[FF] Parameter Measurement of the NuSTAR = Black hole's spin"]
-[4.3370795249938965, 4.834261417388916, "[TT] Sub-beams of the Vessel detection optimized beam mode = 7 (in the HH polarization channel only)"]
-[7.501092433929443, 3.507871627807617, "[FF] Usage of the AOPOD = Weather forecasting"]
-[8.402621269226074, 1.2413088083267212, "[TT] Spatial Resolution of the Solid Earth Sedimentary basins = 20-100 km"]
-[10.724370956420898, 1.4276933670043945, "[FF] Mass of the The Horse and the Dragon = Roughly as massive as our Milky Way"]
-[4.956264019012451, 0.8319664597511292, "[TT] Development Timeline of the Dellingr = February 2014 to February 2015"]
-[8.694685935974121, 8.77227783203125, "[TT] FOV of the Grating Spectrometer = 0.1\u00ba"]
-[8.24803638458252, 8.418688774108887, "[TT] Spectral Resolution of the Satellite = < 0.6 nm"]
-[10.152214050292969, 10.014041900634766, "[FF] Failure Date of the Vega Flight VV17 = 17 November 2020"]
-[8.197189331054688, 1.3411369323730469, "[TT] Rainfall Totals of the IMERG = Over 8 inches (203 mm)"]
-[4.421663761138916, 4.527413845062256, "[FF] Payload Types of the COSPAS-SARSAT = SARR (Search and Rescue Relay) payloads, SARP (Search and Rescue Processing) payloads"]
-[9.546823501586914, 5.355796813964844, "[TT] Slew Capability of the CMG = Up to \u00b130\u00ba"]
-[5.811577320098877, -0.7448069453239441, "[TT] Satellite Build Time of the \u00c5AC Microtec group = 4 months"]
-[3.528038740158081, 6.442166805267334, "[TT] Inter-element Spacing of the Antenna Array = 90 mm"]
-[5.701046466827393, 2.7682652473449707, "[FF] Partnership of the LOFTID = NASA's Space Technology Mission Directorate and United Launch Alliance (ULA)"]
-[8.942619323730469, 6.0240960121154785, "[FF] Optical Path of the TEMPO = Yellow arrows through the block diagram"]
-[4.984582424163818, 0.35220611095428467, "[TT] Launch Date of the Odin = February 2001"]
-[8.844635009765625, 5.7967729568481445, "[TT] Accuracy of the GISTEMP = Within 0.1 degrees Fahrenheit"]
-[6.348756313323975, 8.665945053100586, "[TT] Polarization of the 2 = Horizontal"]
-[5.163035869598389, 1.5426411628723145, "[TT] Recovery Date of the Genesis Sample Return Capsule = Oct. 4, 2004"]
-[7.5070390701293945, 6.055416107177734, "[FF] Distance Measurement Accuracy of the Laser Altimeter (LIDAR) = Several hundred meters"]
-[9.609023094177246, 7.112021446228027, "[TT] Spatial Resolution of the O2-A = 1 km x2 km, 2 km x 2 km"]
-[10.116438865661621, 8.149869918823242, "[TT] Size of the USAT (Ultra Small Aperture Terminal) = 0.65 m"]
-[9.76298713684082, 6.96268367767334, "[TT] Scan Area of the Scanner = 8 m x 4 m"]
-[5.448402404785156, -0.17636679112911224, "[TT] Re-entry Date of the AeroCube-3 = January 6, 2011"]
-[8.293993949890137, 7.169167518615723, "[FF] Image Type of the ALOS-3 = Pan-sharpened images with simultaneous acquisition of panchromatic images and four-band multi-spectral images"]
-[10.03514289855957, -1.5516176223754883, "[TT] Orbit Inclination of the CBERS-4A = 97.9\u00b0"]
-[10.217660903930664, 3.2368929386138916, "[FF] Technology of the XFM-CubeSat instrument = Silicon drift diode"]
-[8.266824722290039, 9.020602226257324, "[TT] Spectral Range of the Argus = 900 - 1700 nm"]
-[7.509698867797852, 5.353415012359619, "[FF] Components of the EO module = Scan mechanism assembly, telescope, aft optics, filter-wheel assembly with its cooler, cooler assembly with the cooled detectors, detectors for the uncooled channels, preamplifiers, viewport sunshade"]
-[7.476632595062256, 6.716121196746826, "[TT] Integration Time of the EyeSat = 15 seconds"]
-[9.1409330368042, 7.34226655960083, "[TT] Orbital Altitude of the Cameras = ~ 700 km"]
-[7.985562324523926, 2.5775983333587646, "[TT] Measurement Domain of the THEOS-2 = Land"]
-[7.9484028816223145, 1.7686400413513184, "[TT] Distribution of the PIRATA = Tropical Atlantic"]
-[5.405817985534668, 5.775111198425293, "[TT] Supported Links of the MDP file transfer protocol = One-way and two-way"]
-[3.7666280269622803, -1.0611660480499268, "[TT] Orbit Stability of the LAGEOS = Very stable"]
-[6.784683704376221, 6.175312519073486, "[TT] Spotlight of the Mode = -"]
-[8.978324890136719, 5.682016372680664, "[TT] Pointing Accuracy of the PARASOL = 0.1\u00b0"]
-[7.0381646156311035, 6.806095123291016, "[FF] Pump Module of the GEDI Laser = Below the layout"]
-[9.385096549987793, 6.011167049407959, "[TT] Type of the SHM = Mechanical shutter, under form of a blade"]
-[6.31288480758667, 3.652269124984741, "[TT] Operational Location of the GOES-S = GOES-West"]
-[8.225456237792969, 7.552459716796875, "[FF] Gamma Ray Detector System of the CXBN = CZT (Cadmium Zinc Telluride) array"]
-[5.256186008453369, 2.647543430328369, "[FF] Managing Center of the GPM = NASA's Goddard Space Flight Center in Greenbelt, Maryland"]
-[8.568700790405273, 8.488043785095215, "[TT] Mapping accuracy of the Spectrometer = < 1.5 km"]
-[11.755146980285645, 4.801299571990967, "[TT] Size of the LTP = 64 cm x 38 cm x 38 cm"]
-[7.245411396026611, 5.250253677368164, "[FF] Components of the Instrument Control Unit (ICU) = Phasemeter, Laser Ranging Processor (LRP), narrow linewidth NPRO laser, Laser Stabilization Unit (LSU), interferometer Optical Bench Assembly (OBA), Retro-Reflector Unit (RRU), scale factor measurements system (SFMS), Ultra Stable Oscillator (USO)"]
-[5.76539945602417, 7.032827377319336, "[TT] Scale of the Data Products = 1:50,000"]
-[8.565378189086914, 4.5582404136657715, "[FF] Purpose of the STR = Matched centroid and star list error distribution validation"]
-[7.348442554473877, 0.24855391681194305, "[FF] Deep Space Maneuver Date of the OSIRIS-REx = 3 July 2018"]
-[6.657869338989258, 6.9286699295043945, "[TT] Data Rate of the LaserCom = 50 - 100 Mbit/s"]
-[10.11855411529541, -1.6240042448043823, "[TT] Inclination of the WorldView-3 = 98\u00ba"]
-[13.955527305603027, 3.388845443725586, "[TT] Mass of the Max Valier = 16 kg"]
-[13.536576271057129, 5.472531318664551, "[TT] Number of Spherical Cell Modules of the High-voltage solar array = 66"]
-[6.753165245056152, 5.146625995635986, "[FF] Components of the Core-DHS = S-band Transmitter and Receiver, Global Positioning System, Attitude & Orbit Control System, Interface Module and Bridge and On Board Computer"]
-[3.7229936122894287, 6.682485580444336, "[TT] Beamwidth of the Onboard Antenna = 20\u00ba"]
-[6.636664867401123, 2.0197997093200684, "[FF] URL of the SOLSE\u20132 = http://library01.gsfc.nasa.gov/host/hitchhiker/solse_2.html"]
-[10.365606307983398, 5.790133476257324, "[TT] Temperature Sensitivity of the Etalon = 2.9 pm/K"]
-[8.580374717712402, 3.5921218395233154, "[FF] Purpose of the TSIS-1 = Measures the total amount of solar energy input to Earth as well as the distribution of the Sun's energy input across a wide range of wavelengths"]
-[7.841029644012451, 6.983636856079102, "[FF] Self-apodisation effect of the Michelson Interferometer = Reduces the signal level when increasing the FOV and the OPD range"]
-[5.973512172698975, 7.1482720375061035, "[TT] Data Rate of the MWHS-II = 15 kbit/s"]
-[8.670247077941895, 0.13793246448040009, "[TT] Sampling Arm Length of the OSIRIS-REx = 11-foot (3.35-meter)"]
-[7.366677761077881, 2.3042378425598145, "[TT] Near-Global Coverage of the Satellite = Every three days"]
-[9.165719032287598, 4.964321136474609, "[FF] Algorithm Selection Criteria of the Attitude Determination Quaternion Filter = Maximum trace of the associated information rate matrix"]
-[9.06602668762207, 9.98941707611084, "[TT] Total Imaging Swath of the Eastman Kodak KLI14403 linear CCD sensor = > 600 km"]
-[8.407618522644043, 0.684831440448761, "[FF] Lunar Eclipse Survival Plan of the Spacecraft = Developed baseline spacecraft configuration to use prior to and during the lunar eclipse"]
-[10.353959083557129, 5.764378547668457, "[TT] Temperature Range of the XRT = 0.5 to 20 MK"]
-[8.353529930114746, 7.152647972106934, "[TT] Number of Fast Cameras of the Payload = 2"]
-[4.632200241088867, 3.009350299835205, "[TT] Operations Center of the RemoveDebris = SSTL\u2019s MOC (Mission Operations Centre) in Guildford"]
-[7.613126754760742, 3.3175084590911865, "[FF] Purpose of the PRIma (PR-Imager) = Earth observation and to test the camera in space"]
-[5.142248630523682, 0.06256120651960373, "[FF] End of Life of the THEIA = Shutdown Procedure"]
-[7.984508514404297, 3.2561469078063965, "[TT] Instrument Type of the ISS:LIS = Lightning sensors"]
-[4.263911247253418, 0.6498656868934631, "[TT] Launch Date of the EDRS-C = May"]
-[3.7061243057250977, 4.777855396270752, "[FF] Polarimetric Data of the RISAT-1 = Unknown"]
-[10.453994750976562, 6.657270431518555, "[TT] Number of Mirrors of the Starshine-1 = 878"]
-[5.147693157196045, 6.804154872894287, "[TT] Downlink Chains of the ResourceSat-2 = 2"]
-[4.747265815734863, 7.295538902282715, "[TT] Data Transmission Rate of the RF Communications = 9.6 to 100 kbit/s in S-band"]
-[8.307254791259766, 1.265170931816101, "[TT] Above-Normal Precipitation of the Northwest Washington = 3 to 5 inches"]
-[10.264463424682617, 5.324233055114746, "[FF] Function of the TET Radiator = It is small enough to prevent an out cooling of the system during \"cold\" phases"]
-[5.752639293670654, 2.917370319366455, "[TT] Organization of the NOSS-36A and NOSS-36B = NRO/MSD (Mission Support Directorate)"]
-[3.4093215465545654, -0.8893173933029175, "[TT] Orbit Types of the WorldView Legion = Mid-inclination and sun-synchronous"]
-[7.4809346199035645, 0.4770909249782562, "[FF] Full Name of the REXIS = Regolith X-ray Imaging Spectrometer"]
-[5.129713535308838, 4.424190998077393, "[TT] Number of Satellites of the SpaceLink = 4"]
-[12.024526596069336, 3.7759029865264893, "[TT] Max Recorded Pressure of the T3\u00b5PS = 3000 mbar"]
-[3.6554348468780518, 1.5784869194030762, "[FF] Conference Date of the GMES-Sentinels = April 25-30, 2010"]
-[7.203752517700195, 4.360442638397217, "[FF] Effective Area of the GMOD = Function of off-axis angle and azimuth of the source GRB"]
-[4.148027420043945, 7.643843650817871, "[FF] Function of the RF modules = Perform quadrature modulation"]
-[7.195157527923584, 5.11233377456665, "[FF] Components of the T3\u00b5PS = MEMS based valve and nozzle, MEMS-based pressure transducer and filter, CGG (Cool Gas Generator)"]
-[5.912692070007324, 6.859383583068848, "[TT] SCI of the OBC = 38.4 kbit/s"]
-[9.085040092468262, -0.5135780572891235, "[TT] Thruster Operation of the ABEX = Within 20% of the apogee location, up to 10% on each side of apogee while above 52,000 km"]
-[14.340604782104492, 6.517569065093994, "[TT] Maximum Battery Power Before 100% Depletion in Orbits of the Satellite = 6 orbits"]
-[4.376580238342285, 4.123239517211914, "[TT] Modulation of the Galileo L1F signal = MBOC waveform"]
-[5.037256240844727, 0.014021561481058598, "[TT] Launch Date of the Yubileyniy-2/MiR = July 28, 2012"]
-[9.723247528076172, 7.041897773742676, "[TT] Spatial Resolution of the LISS III = 23.5 m"]
-[5.599655628204346, 6.91057014465332, "[TT] Data Delivery of the Command and Telemetry Interface = 19-byte status of health information of the AIP"]
-[5.440190315246582, 2.5250625610351562, "[TT] Agency of the TechEdSat = JAXA, NASA, ARC"]
-[11.88495922088623, 4.690333366394043, "[TT] Dimensions of the WINGS suite = 7.6 cm x 7.6 cm x 7.1 cm"]
-[8.758880615234375, 4.100625514984131, "[TT] Measurement Type of the Hot Ion Analyzer = Ion Dispersion"]
-[4.409970760345459, 3.147592544555664, "[TT] Locations of the IOT Stations = Redu, Belgium and Chilbolton, UK"]
-[8.098679542541504, -0.668755292892456, "[FF] Measurement Coverage of the CryoSat-2 = Polar oceans, Greenland, Antarctica"]
-[4.894927501678467, 0.037530940026044846, "[TT] End of Life Date of the Badr-B = 2 years"]
-[10.057485580444336, 4.191266059875488, "[TT] Location of the Coarse Sensor Boom = S/C top deck"]
-[5.972225189208984, 2.166928768157959, "[FF] URL of the FalconSAT-3 = http://www.globalsecurity.org/space/library/news/2009/space-091216-afns01.htm"]
-[7.914410591125488, 8.012360572814941, "[TT] Bands of the HSC-III = 138"]
-[5.828524112701416, -0.6468757390975952, "[TT] Lifetime of the OFEQ-2 = 6 months"]
-[13.444278717041016, 5.52419900894165, "[TT] Solar Panels of the Meteosat = Six"]
-[4.815891742706299, 2.9624202251434326, "[TT] Managing Center of the Eu:CROPIS = DLR (German Aerospace Center)"]
-[10.763599395751953, -1.1328129768371582, "[FF] Altitude of the SLATS = Lowest altitude by an Earth observation satellite in orbit"]
-[10.2965087890625, 2.6762516498565674, "[TT] Altitude Range for Data Collection of the NanoSat-1B = ~588 km to ~706 km"]
-[10.750356674194336, -1.1468883752822876, "[TT] Altitude of the SLATS = 270 km"]
-[3.4894018173217773, 3.578376531600952, "[TT] Manager of the PAZ = HISDESAT"]
-[7.672626972198486, 2.940948247909546, "[FF] Presenter of the CO2Image Demonstrator = Andre Butz"]
-[6.467275619506836, 4.953512668609619, "[FF] Operation of the THEIA = Data Processing"]
-[9.812541961669922, -0.5135284066200256, "[TT] Altitude of the Rideshare mission = 560 km"]
-[9.185288429260254, 8.511434555053711, "[TT] Wavelength of the Lens 1 = 0.38 \u00b5m"]
-[5.272756576538086, 3.977806568145752, "[TT] Number of Satellites of the Transport Layer = Up to 150"]
-[8.724996566772461, 0.42431846261024475, "[TT] Descent Altitude of the MASCOT = 51 meters"]
-[9.670085906982422, 5.003708362579346, "[TT] Drift Rate of the IRS-1C and IRS-1D = 3.6 x 10-4 \u00ba/s"]
-[7.736668109893799, 3.214306354522705, "[TT] Operation Requirements of the OCTS = Global observation of the Earth during daytime"]
-[9.954129219055176, -0.5174790620803833, "[TT] Mean Altitude of the RADARSAT-2 = 798 km"]
-[10.281526565551758, 1.4568774700164795, "[FF] Brightness of the Quasars = Up to 10 000 times brighter than the Milky Way"]
-[11.824917793273926, 6.598034381866455, "[TT] Proton Dynamic Pressure of the ACE = ~2.4 nPa"]
-[6.992863178253174, 6.032835483551025, "[FF] Instrument Count of the GOES-17 = 6"]
-[3.4601824283599854, -0.8979240655899048, "[TT] Diffusion Sun Observation of the Satellite = +Zs axis toward the sun with 15\u00b0 bias on the pitch axis"]
-[14.49189281463623, 6.6100382804870605, "[TT] Power Source of the EPS = Rechargeable Li-ion battery"]
-[10.324150085449219, 4.483389377593994, "[FF] Function of the Reaction Wheels = Desaturate"]
-[8.880870819091797, 9.474024772644043, "[FF] Update Authors of the TANSO-FTS-2 = Ronald Glumb, Peter Mantica, Alan Bell, Christopher Ellsworth, Lawrence Suwinski, and Jeremy Dobler"]
-[5.922220706939697, 4.225817680358887, "[FF] Mission of the IOV (In-Orbit Verification) Payload = Developing system capability for communications payloads on small geostationary satellites"]
-[6.690647125244141, 0.3674875795841217, "[TT] Establishment Date of the Yaguas National Park = January 2018"]
-[11.833440780639648, 6.766890048980713, "[TT] Electron energy of the Microdosimeter B = > 50 keV"]
-[6.040616989135742, 6.008139610290527, "[FF] On-board SSRs Compact Flash Cards of the Telemetry = Successful"]
-[5.502913475036621, 3.615375518798828, "[FF] TDP Command Release of the Inmarsat Automated Procedure Execution System = Automatic"]
-[5.761935234069824, 5.1583991050720215, "[TT] Type of the On Board Computer (OBC) = Single powerful"]
-[7.543185234069824, 3.010946273803711, "[FF] Synergy products of the OLCI = Based on combination of OLCI and SLSTR data"]
-[7.372847080230713, 0.2909502387046814, "[TT] Sample Collection Opportunities of the OSIRIS-REx = 3"]
-[9.126958847045898, 1.4879823923110962, "[TT] Plasma Instrument Status of the Voyager 1 = Damaged during a fly-by of Saturn"]
-[14.347607612609863, 2.954385757446289, "[TT] Mass of the Hodoyoshi-4 = 65 kg"]
-[1.4208166599273682, 1.9044679403305054, "[TT] Cargo Delivery of the Starliner = 500 pounds"]
-[8.754081726074219, 7.617149829864502, "[TT] Detector Format of the Camera = 512 x 512 pixels"]
-[6.7978596687316895, 6.596258163452148, "[FF] Performance of the APAA = Working well"]
-[5.4640703201293945, 6.889796733856201, "[TT] Data Transfer Rate of the Ground Station = 9600 baud"]
-[6.345588684082031, -1.3538790941238403, "[TT] Launch Date of the GRACE-FO = 22 May 2017"]
-[7.369034290313721, 2.3137929439544678, "[TT] Global Mapping Achievement of the Satellite = 86.7%"]
-[5.47411584854126, 6.346313953399658, "[TT] Fiber Core Diameter of the Data Storage System = 200 \u00b5m"]
-[5.595109462738037, 0.9011043310165405, "[FF] Mission Start Date of the THEMIS = Unknown"]
-[4.391112804412842, 0.10796719044446945, "[TT] Launch Date of the Starlink = March 18, 2020"]
-[10.414931297302246, 7.471170425415039, "[TT] Telescope Mirror Diameter of the Euclid = 1.2 m"]
-[12.389725685119629, 0.5989189743995667, "[TT] Telescope Quantity of the PLATO = 26"]
-[3.8757781982421875, 4.465511798858643, "[TT] Technology of the RADARSAT-2 = State-of-the-art"]
-[11.601348876953125, 4.756126403808594, "[TT] Crevice Width of the Philae = 1\u20131.5 m"]
-[7.435035228729248, 6.187588691711426, "[TT] Chip-Based Timing Resolution of the LLMS/IRIS = 0.2 \u00b5s"]
-[13.91788387298584, 7.050174236297607, "[TT] Power Supply Voltage Range of the Resurs-O1 spacecraft = 23-34 V"]
-[4.863105297088623, 3.288933515548706, "[TT] Manufacturer of the SPOT 6 = Astrium"]
-[6.2500786781311035, 3.348165273666382, "[FF] Number of Satellites of the BlackSky Global = 60"]
-[9.740761756896973, 7.18130350112915, "[TT] Resolution of the MIVZA = 80 km to 40 km"]
-[11.701143264770508, 3.4379260540008545, "[FF] Class of the Ion Thruster = 20 mN"]
-[6.670467853546143, 5.54755163192749, "[TT] Number of Experiments of the TPMU = 3"]
-[7.858307361602783, -2.4728426933288574, "[FF] Purpose of the GOLD = Study the ionosphere"]
-[8.056918144226074, 8.640242576599121, "[FF] Spectral Resolution of the HR Bands (677\u2013686 nm, 740\u2013759 nm and 769\u2013780 nm) = Principally driven by the slit width (Figure 23a)"]
-[8.915617942810059, 7.414310932159424, "[TT] Optical System of the AVNIR = Catadioptric Schmidt optical system (telescope)"]
-[6.860450744628906, 6.686524868011475, "[TT] Data Format Repeat of the Sounder = 100 ms"]
-[7.977717876434326, 13.685138702392578, "[TT] SSD of the B12 = 20 m"]
-[10.363160133361816, 7.33665657043457, "[TT] Primary Mirror Aperture Diameter of the Optical Telescope Assembly = 0.70 m"]
-[9.518872261047363, 4.123905658721924, "[TT] Transformation Factor of the Field Measurement Device = 64 \u00b1 0.6 (\u00b5V/nT)"]
-[9.367057800292969, 5.054694652557373, "[TT] Attitude Subsystem Stability of the Spacecraft = 0.009\u00ba/s (3\u03c3)"]
-[9.492825508117676, 1.020678997039795, "[FF] Speed of the Reconnecting Jets = Up to 100 kilometers per second"]
-[9.298815727233887, 7.1658220291137695, "[TT] Mapping Resolution of the EIS = 330 feet (100 m) per pixel"]
-[4.943081855773926, 1.3668333292007446, "[TT] Test Results of the IEPS = All 21 tests were completed faultlessly, except for the break-down protection test"]
-[7.729742050170898, 9.518620491027832, "[TT] Center Wavelength of the B8a = 865 nm"]
-[3.1963136196136475, 3.82932186126709, "[TT] Launch Date of the TerraSAR-X = June 15, 2007"]
-[5.677453994750977, 4.197646141052246, "[FF] Purpose of the Hiber-3 smallsat = Provision of satellite connectivity to \u201cinternet-of-things\u201d (IOT) devices"]
-[5.225343704223633, 5.636787414550781, "[TT] Communication Bus of the SMEX = MIL-STD-1553 data bus"]
-[4.820186614990234, 0.4513553977012634, "[TT] Launch Date of the CRISTAL = 2028"]
-[5.208322525024414, 2.4117941856384277, "[TT] Mission Type of the CXBN = Non-EO"]
-[6.874987602233887, 1.8547810316085815, "[FF] URL of the Solar Dynamics Observatory = http://sdo.gsfc.nasa.gov/"]
-[8.845685958862305, 0.09667128324508667, "[TT] Latitude Coverage of the Sentinel-2 = -56\u00b0 to 84\u00b0"]
-[4.934219837188721, -2.090287685394287, "[TT] Rover Mass of the Tianwen-1 = ~240 kg"]
-[6.2884039878845215, 2.8367557525634766, "[TT] Operation of the AMS-02 = June 1998"]
-[4.915087699890137, 0.6099374890327454, "[TT] Release Date of the DCAM3 = 5 April 5 at 2:14 UT"]
-[5.412890911102295, 6.435436725616455, "[TT] Onboard Storage Capacity of the NigeriaSat-2 = 16 gigabytes"]
-[12.06873607635498, 2.9887049198150635, "[FF] Propulsion System of the TanDEM-X = Combined hydrazine/cold-gas"]
-[5.521083354949951, -1.8735243082046509, "[FF] Workshop Date of the KOMPSAT-3 = March 26-28, 2014"]
-[9.29500675201416, 6.040676593780518, "[TT] Boresight Look Angle of the KaRIn = \u00b12.7\u00ba"]
-[5.096268177032471, 4.155453205108643, "[FF] Communication Support of the Tianwen 1 = Argentina's deep space tracking antenna, ESA's global network of ground stations"]
-[8.330781936645508, -0.4549082815647125, "[TT] Extent of the Sea Ice = 1.82 million square miles"]
-[4.432438373565674, 5.40895938873291, "[FF] Image Subject of the GomX-4B = Southern coast of Cuba"]
-[6.489295959472656, 1.5479158163070679, "[TT] System Integration Review Date of the Europa Clipper = Late 2021"]
-[4.5914483070373535, 2.7157297134399414, "[TT] Platform Reference of the BRITE Satellites = CanX-3"]
-[6.766071796417236, -0.21316856145858765, "[TT] Observation Duration of the Kepler = 72 days"]
-[14.64472770690918, 6.723408222198486, "[TT] Battery Packs of the EPS = 2 Li-ion battery packs"]
-[5.691418170928955, 11.299531936645508, "[FF] LOS Wind Error Requirement of the Rayleigh Channel = Below a certain value"]
-[5.357683181762695, 6.919233798980713, "[TT] Data Generation Rate of the Artemis I mission = About 100 MB/s"]
-[6.327881336212158, 4.629140377044678, "[FF] Layer 1 Components of the MCS = Commanding front-end and automation engine"]
-[13.757129669189453, 7.147939205169678, "[TT] Load Regulation of the DC-DC converter = \u00b11% from 40% load to 100% load"]
-[4.800212383270264, 0.5745683908462524, "[TT] Planned Launch of the Resurs-P4 = 2023"]
-[7.802823543548584, 5.829320430755615, "[FF] Function of the Motorized Filter Wheel = Enables the successive study of different wavebands of visible light"]
-[12.115031242370605, 1.9879413843154907, "[TT] Launch of the SEEDS-2 = Secondary payload to the CartoSat-2A primary spacecraft of ISRO"]
-[4.129627704620361, 1.4038770198822021, "[TT] Launch Date of the Meteosat-1 = November 23, 1977"]
-[5.7452616691589355, -0.8853716850280762, "[TT] Design Life of the Mission design life = 2 years"]
-[12.079998970031738, -0.3039935827255249, "[TT] Orbit Period of the TESS = N/A"]
-[9.835018157958984, 8.458183288574219, "[TT] IFOV of the AVHRR/3 = 1.1 km at nadir"]
-[12.479684829711914, 7.341061115264893, "[TT] Power Dissipation of the Detector Readout Chip = 50 \u00b5W/pixel"]
-[10.288665771484375, 1.9128029346466064, "[TT] X-ray Sources Discovered of the eROSITA = More than 1 million"]
-[10.052892684936523, -1.5118978023529053, "[TT] Inclination of the PROBA-3 = 59\u00ba"]
-[10.166441917419434, 2.0140397548675537, "[TT] Brightness Outburst of the V404 Cygni = June 2015"]
-[10.31640625, 1.760770559310913, "[FF] Topics Addressed of the INTEGRAL = Compact Objects: White Dwarfs, Neutron Stars, Black Hole Candidates, High Energy Transients; Extragalactic Astronomy: Galaxies, Clusters, AGN (Active Galactic Nuclei), Seyferts, Blazars (very compact quasars associated with a presumed supermassive black hole at the center of an active, giant elliptical galaxy), CDB (Cosmic Diffuse Background); Nucleosynthesis Studies: Hydrostatic Nucleosynthesis (AGB, WR Stars), Explosive Nucleosynthesis (Supernovae, Novae); The Galactic Center: Sgr A*, diffuse emission, monitoring the Galactic Center and Bulge; GRBs (Gamma-Ray Bursts): Alerts, GRB properties; Classification and Identification of High Energy Sources: Source Catalogues, Identifying Gamma-Ray Objects; Unexpected Discoveries (Obscured sources, Supergiant Fast X-ray Transients, hard tails from magnetars)"]
-[10.885139465332031, 7.479454040527344, "[TT] Swath of the TES = 5.3 km x 8.5 km"]
-[12.031587600708008, 6.468398571014404, "[TT] Observation of the AMS = Fraction increases steadily between 10 GeV to ~250 GeV"]
-[10.651927947998047, 1.3957881927490234, "[TT] Energy Received from Star of the L 98-59c = 11 times as much radiation as Earth"]
-[4.192298889160156, 7.183569431304932, "[TT] Frequency of the PALS = L- and S-band"]
-[9.860913276672363, 7.726360321044922, "[TT] Spatial Resolution & Stability of the Telescope = Strehl ratio of ~ 0.86 at 2 \u00b5m"]
-[1.9493473768234253, -0.39501136541366577, "[FF] De-orbit Maneuvers Date of the Van Allen Probes = February of this year"]
-[6.031832218170166, 1.960652232170105, "[FF] Pre-launch Performance of the VIIRS = Unknown"]
-[7.6129302978515625, -2.515416145324707, "[TT] Observation Date of the GOLD = Oct. 7-25, 2019"]
-[8.986538887023926, 0.5806424617767334, "[FF] Planned Operation of the ARTEMIS Probes = Routinely operate in the most eccentric lunar science orbits of any mission to date"]
-[7.492249965667725, 3.4827723503112793, "[FF] Description of the Level-4 (L4) = Digital Elevation Model ( DEM)"]
-[8.550251960754395, 4.622704982757568, "[FF] ACNS Units of the PROBA-2 = 4 reaction wheels, 2 magnetometers, a miniaturised \u00b5ASC star tracker with two hot-redundant camera heads and cold-redundant DPUs, a cold redundant GPS receiver, and internally redundant magnetotorquers"]
-[7.936197757720947, 3.1511220932006836, "[TT] Observation Mode of the CO2 Spectrometer = Direct sun observation, Diffusion sun observation"]
-[4.29161262512207, 7.461740493774414, "[TT] Operating Frequency of the Nanolink = S-band"]
-[5.2055134773254395, 1.2653666734695435, "[FF] Conference Date of the TBIRD Program = August 3-8, 2019"]
-[9.891521453857422, 4.407507419586182, "[TT] Actuators of the ADCS = Magnetorquers"]
-[6.05719518661499, 6.439006805419922, "[TT] Latency of the Shipboard Thermosalinograph = 2 days"]
-[9.202942848205566, 3.057621955871582, "[FF] Mission Objectives of the MiniCOR = Improved measurements of CME kinematics and CME-shock standoff distance, Analysis of small-scale structures in the corona and solar wind"]
-[8.448443412780762, 1.998261570930481, "[FF] Measurement Goals of the SMMR = Obtain integrated liquid water and water vapour content in the atmosphere"]
-[9.39513111114502, -0.483079195022583, "[TT] Altitude Range of the MEOSAR = 19 000 to 24 000 km"]
-[7.892734527587891, 7.556838512420654, "[FF] Development Date of the Hyperspectral sensor = Sept. 29 to Oct. 3, 2008"]
-[7.5453314781188965, 3.7855288982391357, "[TT] Lens of the NightPod = Nikkor 400mm"]
-[6.245334625244141, 8.579949378967285, "[FF] Polarization Modes of the PALSAR-2 = SP: Single Polarization, DP: Dual Polarization, FP: Full Polarization (quad), CP: Compact Polarization"]
-[9.725568771362305, 0.17993338406085968, "[TT] Average Distance of the Thuban = about 61 million km"]
-[6.994519233703613, 5.098984241485596, "[TT] Segments of the ICU = Bottom, Middle, Top"]
-[9.957342147827148, -0.5156480073928833, "[TT] Orbit Altitude of the KySat-1 = 705 km"]
-[9.399653434753418, 7.316432476043701, "[TT] PAN Spatial Resolution of the PMC = 2 m"]
-[4.856827259063721, 2.750641107559204, "[TT] Operator of the Eutelsat Quantum = Eutelsat Communications"]
-[6.74971342086792, -0.5310163497924805, "[TT] Core Program Duration of the SVOM = 14 orbits (tunable)"]
-[6.984713554382324, 6.658871650695801, "[FF] Type of the LaserCom = Laser"]
-[8.588462829589844, 2.7913053035736084, "[FF] Data Gathered of the MAHRSI = New vertical profile data on the distribution of OH in the mesosphere and upper stratosphere"]
-[3.797253131866455, 1.2519100904464722, "[TT] First Stage Booster Flights of the Falcon-9 Rocket = 3"]
-[6.752949237823486, -0.5036888718605042, "[TT] Orbit Lagging Time of the Observatories = About 1 month later"]
-[5.876530170440674, 6.9208269119262695, "[TT] Data Stream Width of the DPU = 16-bit"]
-[6.465315341949463, 0.5888301730155945, "[TT] Year of Launch of the Landsat-7 = 1999"]
-[7.992090702056885, 5.360745906829834, "[TT] Range-dependent Noises of the FLLS = Dimensionless"]
-[8.00369930267334, 2.668253183364868, "[TT] Measurement Domain of the SkySat Constellation = Ocean, Land"]
-[13.732757568359375, 2.905083417892456, "[TT] Per spacecraft mass of the WorldView-4 = 2500 kg"]
-[8.755776405334473, 7.055600643157959, "[TT] Payload Structure of the CartoSat-2 = CFRP (Carbon Fabric Reinforced Plastic) based electro-optic payload structure with a two mirror on-axis single camera"]
-[6.178915023803711, 7.868117809295654, "[TT] Signal Transmission of the GIOVE-B = Three separate channels"]
-[5.330004692077637, 7.403237819671631, "[FF] Transmitted Information of the NorAIS-2 Receiver = Identity, position, speed and heading"]
-[10.428997993469238, 4.5950541496276855, "[TT] Radio and Reaction Wheels Voltage of the MarCO-B = Greater than 8V"]
-[11.218924522399902, 5.891867637634277, "[FF] Components of the SMATTE = Layer of polymer matrix composite with a thin strip of shape memory alloy on each side"]
-[7.705058574676514, -2.5312047004699707, "[TT] Typical Observation Duration of the GOLD = Six to eight hours"]
-[3.740262031555176, 2.647007703781128, "[FF] Data Handling of the Iridium NEXT = Near real-time transport of mission data and sensor telemetry"]
-[7.903473377227783, 2.4419057369232178, "[TT] Inclusion of Aeolus data of the ECMWF = Since January"]
-[9.96628475189209, -0.16524255275726318, "[TT] Location of the CDN2 Site = 35\u00b0 20.729' N, 23\u00b0 46.577'E"]
-[5.98602819442749, 2.6377928256988525, "[FF] Type of the NIU VShE \u2014 DZZ = Earth Observation spacecraft"]
-[4.608969211578369, 0.6712043285369873, "[TT] ADCS Malfunction Date of the Monitor-E = Feb. 2007"]
-[11.240812301635742, 5.8625102043151855, "[TT] Material of the Instrument Structure = CFRP (Carbon Fiber Reinforced Plastic)"]
-[5.777948379516602, 7.150018215179443, "[TT] Data Rate of the MTVZA-GY = 35 kbit/s"]
-[8.68360710144043, 3.2019994258880615, "[FF] Measures of the EMUS = Oxygen and carbon monoxide in the thermosphere and the variability of hydrogen and oxygen in the exosphere"]
-[5.12673807144165, 3.278449773788452, "[TT] Sponsor of the ETB = BMDO"]
-[13.125178337097168, 6.870789527893066, "[FF] Power Consumption of the Safe-mode System = Very low"]
-[8.675237655639648, 7.661969184875488, "[TT] Detector Pixel Size of the Instrument = 7 \u00b5m x 7 \u00b5m"]
-[7.063455581665039, 3.2628226280212402, "[FF] Derivative Datasets of the Vricon 3D Surface Model = Digital Surface Model (DSM), Digital Terrain Model (DTM), and 3D Vectors"]
-[5.8279266357421875, 2.6925761699676514, "[FF] Funding Agency of the OPAL = National Science Foundation (NSF)"]
-[7.857728958129883, 8.29757308959961, "[FF] Transmission Spectra of the Optical Depth Range = 0.01\u20134.5"]
-[8.022298812866211, 6.402663230895996, "[FF] Imaging Modes of the TeLEOS-1 = Various"]
-[5.919437408447266, 0.9410156011581421, "[TT] Image Transmission Date of the DMAC = Aug. 9, 2009"]
-[3.4459919929504395, -0.9117938280105591, "[TT] Orbit of the HAUSat-2 = Sun-synchronous Orbit"]
-[5.9723968505859375, 5.700472831726074, "[TT] FPGA Co-processor of the SGR-ReSI = Virtex 4"]
-[6.443052768707275, 5.412779808044434, "[FF] Architecture of the SPAISE2 = Digital sampling and ground signal processing"]
-[9.808966636657715, 8.702680587768555, "[TT] FOV (swath) of the ScaRaB = 97.82\u00ba (3300 km)"]
-[4.33664608001709, -0.097650907933712, "[TT] Reentry Date of the P35-10 = 13.7.1979"]
-[7.943486213684082, 0.9737583994865417, "[FF] Distribution Changes of the Water Mass = Sub-daily to inter-annual, and decadal"]
-[9.983147621154785, -0.3727981448173523, "[TT] Altitude of the SEOSAT-Ingenio = 670 km"]
-[8.443475723266602, 2.482429265975952, "[FF] Data of the Aeolus = Altitude and vertical extent of the aerosol layer"]
-[3.9051806926727295, 4.475626468658447, "[TT] Orbit Maintenance Maneuvers of the RADARSAT-2 = 42"]
-[7.01182746887207, 0.14670054614543915, "[FF] Formation Start of the Azores archipelago = About 10 million years ago"]
-[8.730741500854492, 5.322336196899414, "[TT] Sensitivity of the Three-axis diagonal gradiometer = < 10 -12  m s -2  Hz -1/2"]
-[9.57327938079834, 5.057091236114502, "[TT] Relative Position of the AC4-B = Below AC4-A"]
-[13.601943969726562, 1.7412889003753662, "[TT] Cargo Capacity of the Dragon spacecraft = ~2360 kg"]
-[9.442489624023438, 7.614686489105225, "[TT] Swath Width of the WiFS camera = 810 km"]
-[13.497357368469238, 2.8723034858703613, "[TT] Satellite Mass of the Kleos S.A. = 8 kg"]
-[5.1523895263671875, 0.9758836030960083, "[FF] Flight Results Presentation Date of the BIRD Onboard Navigation System = Oct. 22-25, 2002"]
-[8.517865180969238, 1.5271433591842651, "[TT] Radiometer Objective of the Aquarius = Measure the microwave brightness temperatures of the ocean surface"]
-[11.947823524475098, 3.290226697921753, "[FF] Control Scheme of the Iodine BIT-3 propulsion unit = Works best for long-duration, steady-state maneuvers"]
-[6.547426223754883, 5.137816905975342, "[TT] Function of the AIU = Command & control and power distribution"]
-[11.785850524902344, 0.08055280894041061, "[FF] Data Collection of the Transiting Exoplanet Survey Satellite (TESS) = Sensitive to different wavelengths of light"]
-[6.950132369995117, -0.4193006157875061, "[TT] Local Time of Ascending Node of the Satellite = 9:15 AM"]
-[11.264067649841309, 4.950551986694336, "[TT] Mast Length of the NuSTAR = 10-m"]
-[8.301156044006348, 8.254182815551758, "[TT] Manufacturer of the VNIR Detectors = Airbus DS-ISAE-e2v"]
-[5.302816867828369, 6.437068939208984, "[TT] Data Transmission Mode of the Satellite = Direct transmission (DD)"]
-[10.322660446166992, 5.748227596282959, "[TT] Operating Temperature of the Telescope = -50\u00baC to ~ 100\u00baC"]
-[5.471969127655029, 0.5893782377243042, "[TT] Launch Date of the FormoSat-1 = January 26, 1999"]
-[6.898728370666504, 7.747669696807861, "[TT] Sigma 0 (\u03c30) Range of the DPS = HH, VV: +15~-25 dB HV,VH: +5~-35 dB"]
-[7.906987190246582, 9.074652671813965, "[TT] Wavelength of the TIR = 0.5, 1.0, 1.0 \u00b5m"]
-[7.717831611633301, 9.379853248596191, "[TT] Center Wavelength of the Band No. 30 = 891.11 nm"]
-[7.464452266693115, 8.02348518371582, "[TT] -1 Order Diffraction Angle (780 nm) of the Diffracted Beam = 30.9 \u00ba"]
-[3.084850549697876, 3.902277708053589, "[TT] Launch Date of the NISAR = Late 2021"]
-[6.787591457366943, 8.42241096496582, "[FF] SNR @Lref [EOL] of the Spectral Channel = 202-408"]
-[10.844345092773438, 7.394318103790283, "[TT] Width of the Deir el-Medina = 130 m"]
-[10.598373413085938, 2.764124631881714, "[TT] Orbit Altitude of the Nanosatellites = Approximately 500 km"]
-[8.600455284118652, 1.8636869192123413, "[TT] Water Vapor Detection Channels of the FY-4B = New"]
-[8.989347457885742, 0.9634453058242798, "[FF] Objective of the DART = Demonstrate a kinetic impact on a small asteroid"]
-[7.785367965698242, 6.723645210266113, "[TT] Number of Ground Receptors of the SafetyNetTM = 15"]
-[7.5644097328186035, 8.805456161499023, "[TT] Spectral Bands of the MSU-SK = 0.5-0.6, 0.6-0.7, 0.7-0.8, 0.8-1.1, and 10.4 - 12.6 \u00b5m"]
-[6.794594764709473, -0.6501290202140808, "[TT] Orbital Period of the CBERS-4 = 100.26 minutes"]
-[11.519278526306152, 4.681020736694336, "[TT] Mounting Locations of the OPS systems = 5 different sides of the cuboid"]
-[4.623758316040039, 0.608481228351593, "[TT] AI Deployment Date of the CIMON-1 = 15 November 2018"]
-[4.8859076499938965, 0.2527903616428375, "[TT] Launch Date of the SPOT-4 = March 24, 1998"]
-[6.444063663482666, 7.580512523651123, "[TT] Data Quantization of the MSU-50 = 8 bit"]
-[8.352880477905273, 1.5210680961608887, "[FF] Parameter of the PMI = Sea Surface Salinity - L-band BT sensitive to SSS"]
-[9.603901863098145, 8.248072624206543, "[TT] Optics Field of View of the Wide-angle camera = 65.8\u00b0"]
-[10.143375396728516, 3.0275964736938477, "[FF] Original Manifest of the Falcon-9 CRS-2 = ELaNa-4 CubeSats"]
-[9.395277976989746, 5.495085716247559, "[TT] Maximum Slew Rate of the ADCS = 3\u00ba/s"]
-[10.494011878967285, 2.8597049713134766, "[FF] Mission Goal of the FASTRAC = Demonstrate enabling technologies for nanosatellites that work together in space"]
-[10.852958679199219, 1.076308250427246, "[FF] Predicted Mass of the White Dwarf = Two tenths the mass of the Sun"]
-[9.677781105041504, -0.5567179322242737, "[TT] Altitude of the GOES-R = ~35,786 km"]
-[10.207107543945312, 5.581236839294434, "[FF] Activation Sequence of the CCD Heater Controller = Enabled and allowed to settle to the desired temperature"]
-[10.383591651916504, 4.50034761428833, "[TT] Quantity of Reaction Wheels of the Earth Observation Compartment = 3"]
-[9.868521690368652, -0.34257832169532776, "[TT] Operating Altitude of the Sentinel-6 and Jason-3 = 1330 km"]
-[13.233671188354492, 7.278667449951172, "[TT] Peak Power Consumption of the ETB sub-experiment = < 5 W"]
-[6.15597677230835, 6.451528549194336, "[TT] Maximum Report Duration of the DCPs = About one minute"]
-[3.185974359512329, 1.8460793495178223, "[TT] Image Acquisition Date of the Sentinel-2A = Feb. 10, 2016"]
-[10.345224380493164, 3.2797884941101074, "[TT] Downlink Channels of the CubeSat = 2"]
-[9.08554744720459, 8.294528007507324, "[FF] DOI of the Spaceborne Frequency Comb Metrology = 10.1364/optica.3.001380"]
-[11.673958778381348, 3.4093074798583984, "[TT] Number of Upper-Stage Engine Burns of the STP-2 = Four"]
-[8.071879386901855, -1.0108270645141602, "[FF] Purpose of the ICESat-2 = Investigate why and how much of the frozen parts of our world are changing as a result of climate change"]
-[5.978750705718994, -0.6858412623405457, "[TT] Mission Design Life of the DSP satellites = >18 months for the near-equatorial S/C, and >12 months for the polar S/C"]
-[3.2966129779815674, 2.2649359703063965, "[FF] Data of the Sentinel-1A = Raw"]
-[6.316740036010742, 1.8343772888183594, "[FF] URL of the FY4A = https://fy4.nsmc.org.cn/nsmc/en/theme/FY4A.html"]
-[14.119601249694824, 3.0106029510498047, "[TT] Mass of the HAUSat-2 = 25 kg"]
-[6.289853572845459, 0.7518044710159302, "[TT] Data Release 2 of the Gaia = April 25, 2018"]
-[9.05621337890625, 4.24832820892334, "[FF] Absolute Attitude Sensors of the PSSCT-2 = Aerospace-developed sun and Earth nadir sensors, plus COTS (Commercial-of-the-Shelf) magnetic field sensors from Honeywell"]
-[4.463888168334961, 5.5406928062438965, "[TT] Functionality Status of the GomX-3 = Operational"]
-[6.920774459838867, 1.482783317565918, "[TT] Expected Completion of Optical Telescope Element alignment of the Webb = Early May"]
-[10.31970500946045, 6.872131824493408, "[TT] Integration Process of the Mirror = VOB (Vertical Optical Bench)"]
-[4.920506954193115, 7.390745162963867, "[TT] Uplink Data Rate of the RF communications = 9.6 kbit/s"]
-[9.436853408813477, 6.102358818054199, "[TT] Canting Angle of the SAWs = +55\u00ba / 0\u00ba"]
-[6.89012336730957, 6.0109686851501465, "[TT] Background of the NICER = < 0.2 counts/s"]
-[4.923291206359863, 2.0885348320007324, "[TT] Operational Status of the MTSAT-1R = Standby"]
-[5.937553405761719, 0.8316261768341064, "[FF] Image Capture Date of the LRO = Jan. 29, 2014"]
-[7.476724147796631, 7.248392105102539, "[TT] Imaging Time of the CHORUS = About 20 minutes earlier each day"]
-[14.24555492401123, 3.2433042526245117, "[TT] Mass of the MDIM = 0.7 kg"]
-[3.250807046890259, 4.918288707733154, "[FF] Incidence Angle Issue of the SeaSat SAR = Produced severe geometric layover distortions on terrain images of high-relief regions"]
-[8.24621868133545, 5.054124355316162, "[FF] Change Monitoring of the IEM = Secular change of the shape and the stiffness"]
-[8.857267379760742, 2.747523546218872, "[TT] Standard Deviation of the Altitude error = 66.0 m"]
-[7.757469654083252, 8.978595733642578, "[TT] Band Spacing of the SWIR = 11.4 nm"]
-[8.51722240447998, 4.20164680480957, "[FF] Cross-Calibration Purpose of the TRACE = With NASA's SDO (Solar Dynamics Observatory) mission"]
-[5.220617771148682, 2.2871317863464355, "[TT] Mission Type of the FalconSat-3 = Non-EO"]
-[13.384529113769531, 6.929545879364014, "[TT] Power of the CATS = < 1 kW"]
-[4.472961902618408, 0.6540352702140808, "[FF] Redesign Date of the FPM = Unknown"]
-[5.528304100036621, 0.6370885968208313, "[FF] Launch Date of the FormoSat-5 = July 17, 2017"]
-[3.901334762573242, 4.339876651763916, "[FF] Presenters of the RADARSAT-2 Moving Object Detection Experiment (MODEX) = Shen Chiu, Chuck Livingstone, Ishuwa Sikaneta, Christoph Gierull, Pete Beaulne"]
-[6.8945722579956055, 7.302404403686523, "[TT] Diameter Increase of the BEAM = 40%"]
-[8.955613136291504, 6.002939224243164, "[TT] Orientation Adjustment of the PSSCT-2 = Continuous"]
-[13.263249397277832, 5.479301452636719, "[FF] Manufacturer of the Roll Out Solar Arrays (ROSA) = Deployable Space Systems"]
-[9.78172779083252, -0.5506514310836792, "[TT] Altitude of the CBERS-3 = 778 km"]
-[4.764310836791992, 0.8155229687690735, "[TT] Operation Start Date of the PROBA-2 = July 1, 2013"]
-[3.813281297683716, 6.215559005737305, "[TT] Number of Antennas of the Heinrich Hertz = 8"]
-[5.148033142089844, 8.382460594177246, "[TT] Bandwidth of the FIELDS suite = 20 MHz"]
-[8.755621910095215, 3.563096523284912, "[FF] Leading Noise Terms of the Satellite = Optical sensing"]
-[7.430752754211426, 6.39397668838501, "[TT] Time Tagging Accuracy of the XGRE = About one microsecond"]
-[11.342580795288086, 4.400839328765869, "[TT] Size of the DSAT-2 = 2U"]
-[8.76475715637207, 3.7596335411071777, "[FF] Instrument Unit Volume of the Solar Orbiter = Tightly controlled"]
-[13.827406883239746, 3.853524923324585, "[TT] Weight of the Kowa LM16JC lens = 55 g"]
-[6.37750768661499, 2.318265438079834, "[FF] Affiliated Institutions of the TESS Science Center = MIT's Physics Department, Kavli Institute for Astrophysics and Space Research, the SAO (Smithsonian Astrophysical Observatory), and the NASA Ames Research Center"]
-[4.850171089172363, -0.9313875436782837, "[FF] Measurement Sensitivity of the Fengyun-4B = Doubled compared with the Fengyun-4A satellite"]
-[5.778908729553223, 0.9178263545036316, "[FF] Observation Date of the HSRL-2 = 10 October 2014"]
-[6.9041242599487305, 4.931550979614258, "[FF] Additional Board of the DSAT-1 = Control of the air valve and the CGG system"]
-[5.883966445922852, -0.8596261143684387, "[TT] Design Life of the Aqua = 6 years"]
-[3.977886915206909, 2.112400770187378, "[TT] Launch Type of the ORS-6 = Commercial rideshare"]
-[7.962898254394531, 9.172690391540527, "[TT] Wavelength of the LORE = 603 nm"]
-[8.055774688720703, 3.478896379470825, "[FF] Collection of the Infrared Background Data = Selected wavelength bands at low and high altitudes"]
-[10.271851539611816, 7.254966735839844, "[TT] Number of Mirrors of the Korsch telescope = 5"]
-[14.107577323913574, 2.993267059326172, "[TT] Mass of the Prometheus-2.1 to -2.8 = 2 kg"]
-[7.448493957519531, 2.3465590476989746, "[FF] Dataset of the SMOS = Vegetation optical depth dataset"]
-[12.095050811767578, -0.36189013719558716, "[TT] Operation Duration of the TESS = 2 years"]
-[7.277970314025879, 4.755314826965332, "[FF] Data Collection Duration of the ASAS-SN = Provides a longer baseline"]
-[6.82503080368042, 1.1342319250106812, "[FF] Conference Date of the Solar Orbiter = Oct. 7-10, 2014"]
-[11.625675201416016, 3.3849778175354004, "[TT] Purpose of the HEMPT Thruster Assembly = Satellite position maintenance"]
-[6.005282878875732, 1.5833946466445923, "[FF] Presentation Date of the Quasi-Zenith Satellite System = July 5-12, 2009"]
-[5.313346862792969, 2.9757537841796875, "[TT] Funding of the NorSat-3 = Norwegian Ministry of Defence"]
-[8.015240669250488, 5.333686351776123, "[FF] Calibration Capabilities of the Instrument = Spectral behavior, relative and absolute radiometric properties"]
-[3.375828504562378, 4.938294410705566, "[FF] Calibration Measurement Recommendation of the SAR System = Measure at least one beam of each mode against the SENTINEL-1 transponders deployed at different locations"]
-[7.1521077156066895, 5.984862804412842, "[FF] Function of the Ti = Record a radio signal over a time period"]
-[5.799714088439941, 3.4211654663085938, "[FF] Business Model of the Astrocast = Monthly subscription fee for every device connected"]
-[8.400093078613281, 2.022773265838623, "[FF] Purpose of the CFOSAT = Study ocean surface wind and wave conditions"]
-[9.884296417236328, 8.129777908325195, "[TT] Effective Focal Length of the Primary Objective = 300 mm"]
-[6.245952606201172, 4.630270957946777, "[FF] Function of the Satellite Control Center (SCC) = Receive a variety of satellite information"]
-[10.48891544342041, 4.867493152618408, "[FF] Redesign Purpose of the SMA Hinge Spring = Increase area to reduce stress on the part by more than 20%"]
-[4.642478942871094, 7.934354305267334, "[FF] Function of the Transmit and Synthesizer Module (TSM) = Conditioning and amplifying the transmit chirp, hosting and distributing the instrument Ultra Stable Oscillator"]
-[10.305761337280273, 3.178896427154541, "[TT] Quantity of the CubeSat Yonsei team = 1"]
-[6.634515285491943, 5.120913505554199, "[FF] Components of the Instrument Front-End = Active Antenna Panels, Transmit Receive Modules (TRMs), Radio Frequency Distribution Network (RFDN), Mechanisms"]
-[12.015138626098633, -0.23146246373653412, "[TT] Atmospheric Interference of the TESS = None"]
-[8.04079532623291, 8.551653861999512, "[TT] Channel Band (\u00b5m) of the VNIR = 0.45-0.49"]
-[10.113112449645996, 1.96352219581604, "[TT] Launch Date of the Chandra X-Ray Observatory = 22 November 2021"]
-[6.582211017608643, 6.246025085449219, "[TT] Number of ISLs of the LCT = More than 100"]
-[5.802351951599121, 5.097012519836426, "[FF] Application of the SCPS Workstation = SCPS software"]
-[6.061405181884766, 1.6050001382827759, "[FF] Presentation Date of the Kaber Small Satellite Deployment System = February 17, 2015"]
-[8.604689598083496, 1.4457684755325317, "[TT] Quantization levels of the Cloud amount = 1"]
-[5.875392436981201, 2.7801883220672607, "[FF] Operations Concept of the OPS-SAT = Transition from supporting educational missions to supporting operational ones"]
-[8.695451736450195, 8.451769828796387, "[TT] Ground Projection of the Spectrometer = 0.4 km x 12 km"]
-[5.802641868591309, 3.4866607189178467, "[TT] Average Stationkeeping Cost of the ISEE-3 = 8.5 m/s per year"]
-[5.06558895111084, 1.0928215980529785, "[TT] Launch Date of the NPP = October 28, 2011"]
-[9.94251537322998, 9.023163795471191, "[TT] Effective FOV of the Channel 4 = 35 x 76 km"]
-[8.149781227111816, 0.9122838973999023, "[FF] Mission Objective of the EQUULEUS = Demonstrate trajectory control techniques within the sun-Earth-moon region for the first time by a smallsat"]
-[9.450901985168457, 6.029855728149414, "[TT] Polar Angles of the Instrument = 30o, 60o, 90o, 120o, and 150o"]
-[6.362185478210449, 1.9258909225463867, "[FF] URL of the AstroSat = http://www.tifr.res.in/~laxpcworkshop14/presentations/LAXPC_WORKSHOP%20%20_3-k%20s%20sharma.pdf"]
-[8.933818817138672, 6.575408935546875, "[TT] Foot Print of the RA-1 = 16 - 20 m"]
-[6.933784484863281, 4.514452934265137, "[FF] Unknown of the RadMon = Unknown"]
-[12.722369194030762, 3.3439269065856934, "[TT] Average Consumption of the Fuel Consumption = 0.009 kg per burn"]
-[10.469439506530762, 2.15275239944458, "[FF] X-ray Nova Detection Date of the ISS, Swift = Oct. 25, 2010"]
-[5.127217769622803, -0.7112600207328796, "[TT] Departure Date from ISS of the Kounotori-6 = Jan. 27"]
-[13.659296989440918, 6.013000965118408, "[FF] Function of the EPS = Regulates battery charge levels, controls power generation through a peak power tracker on the solar panels, and provides regulated 5 and 12 V DC power outputs to the spacecraft"]
-[5.921941757202148, 0.8832976222038269, "[TT] Image Acquisition Date of the Marctan = 04 Feb. 2014"]
-[5.563558101654053, 6.341246604919434, "[TT] SSDR Capacity of the SLIM6 = 1.5 GB"]
-[8.760451316833496, 7.547201156616211, "[TT] Pixels of the Multispectral Imager = 450,000 pixels"]
-[8.968094825744629, 0.42035382986068726, "[TT] Distribution Range of the New Boulders = Up to ~40 m from the crater center"]
-[3.6415746212005615, 1.5548175573349, "[FF] Meeting Date of the GMES Sentinel-3 = 18-20 January 2010"]
-[10.131484031677246, 6.979207992553711, "[TT] Detector Element Size of the Sounder = 10 km x 10 km"]
-[8.57019329071045, 8.042794227600098, "[TT] Spectral Resolution (86 keV) of the Detector = 1.2 keV"]
-[10.694478988647461, 1.0970364809036255, "[TT] Size of the L 98-59c = Around 1.4 times Earth\u2019s size"]
-[9.89496898651123, -0.5362485647201538, "[TT] Initial Orbit Altitude of the Satellite = 570 km"]
-[8.064020156860352, -1.2708137035369873, "[TT] Number of Laser Beams of the ICESat-2 = 6"]
-[3.3499748706817627, 2.3068695068359375, "[FF] Data Access of the Sentinel-1 = Full and open access"]
-[13.157261848449707, 7.188741207122803, "[TT] Power Consumption of the MUX = 66 W"]
-[10.339622497558594, 5.725554943084717, "[TT] On-Orbit Temperatures of the TacSat-4 = \u00b1150o C"]
-[5.830169677734375, 0.9909562468528748, "[TT] Launch Date of the WorldView-4 = November 11, 2016"]
-[9.409801483154297, 7.032602310180664, "[TT] Surface Resolution of the FREND = ~40 m"]
-[9.097447395324707, -0.4987969696521759, "[TT] Orbit Apogee of the P35 series = 810 km"]
-[8.037315368652344, 8.440441131591797, "[TT] Dynamic Range Visible Channel of the VIRR = 65 - 10,000 fL (scene brightness)"]
-[5.64667272567749, -0.3645767569541931, "[TT] Deployment Confirmation Time of the STSAT-3 = About 6 hours after lift-off"]
-[7.498852729797363, 2.3518729209899902, "[FF] Applications of the ASAR = Measuring sea-state conditions, Mapping ice-sheet characteristics and dynamics, Mapping sea-ice distribution and dynamics, Detecting large-scale vegetation changes, Monitoring natural and man-made pollution over the oceans, Offshore operations in sea ice, Snow and ice mapping, Coastal protection and pollution monitoring, Ship traffic monitoring, Agriculture and forest monitoring, Soil moisture monitoring, Geological exploration, topographic mapping, Predicting, tracking, and responding to natural hazards"]
-[5.652952194213867, 2.7493772506713867, "[TT] Developing Entity of the MoonLIGHT = Italian National Institute of Nuclear Physics (INFN) in Frascati"]
-[3.8354625701904297, 1.1303980350494385, "[TT] Speed of the Falcon-9 first stage = 1300 m/s to about 250 m/s"]
-[6.771639823913574, 7.587015151977539, "[TT] Beam Width of the Channel = 1.06 \u00ba"]
-[10.47709846496582, 5.745110988616943, "[TT] Temperature of the TPS pads = 2200\u00ba C"]
-[11.881731986999512, 5.600831508636475, "[TT] Model of the ICON FUV Instrument = Dalsa FTT1010M"]
-[5.17184591293335, 7.017824649810791, "[TT] Downlink Speed of the Communication links = 1 Mbit/s"]
-[5.738377094268799, -0.26421302556991577, "[TT] Operation Goal of the TSX-5 = 1 year"]
-[8.484387397766113, 6.043057918548584, "[TT] Onboard Calibration Accuracy of the AVNIR = \u00b15%"]
-[9.01909065246582, 3.947279691696167, "[FF] Objectives of the S 329 = Measurement of DC electric field grad |B|"]
-[13.885100364685059, 4.059566974639893, "[TT] Mass of the Alpha Magnetic Spectrometer = 8.5 ton"]
-[13.324827194213867, 7.740097522735596, "[TT] High Power Output of the VLF transmitter = Up to 500 W"]
-[5.193141460418701, 1.3077565431594849, "[FF] Publication Date of the Dual Gimbal Antenna = January 2009"]
-[14.339802742004395, 3.314728260040283, "[TT] Mass of the MUPUS = 2.2 kg"]
-[7.624740123748779, 1.6369389295578003, "[FF] Mission of the Far Ultraviolet Camera/Spectrograph = Apollo 16"]
-[3.6897222995758057, 6.099676132202148, "[TT] Size of the Canberra DSN station = 70-meter"]
-[8.111735343933105, 0.6613276600837708, "[TT] Average Seasonal Fluctuation of the Reservoirs = 34 inches (0.86 m)"]
-[5.7065019607543945, 1.8907239437103271, "[FF] Rideshare Mission of the SpaceX = Transporter-8"]
-[3.503974676132202, -0.9871688485145569, "[TT] Moon Orbit of the Chandrayaan-2 = 100 km circular polar orbit"]
-[7.866117477416992, 6.731868267059326, "[TT] Interferometer Type of the SPIDER sensor = MMI (Multi-Mode Interferometer)"]
-[7.973859786987305, 2.215134859085083, "[FF] Data Collection of the TOPEX/Poseidon = Oceanic circulation, tides, El Ni\u00f1o, La Ni\u00f1a, Pacific Decadal Oscillation, ocean floor topography"]
-[5.984954833984375, 1.5676846504211426, "[TT] Retrieval Date of the EURECA = June 21 - July 1, 1993"]
-[7.602550029754639, 5.80357551574707, "[TT] Type of the MMIC Amplifiers = Monolithic Microwave Integrated Circuit"]
-[6.803531169891357, 1.0845574140548706, "[FF] Study Date of the Small Sun Structures = 19 January 2021"]
-[9.407645225524902, 0.7300785183906555, "[TT] Closest Approach Time of the BepiColombo = 23:34:41 UTC"]
-[6.011308193206787, 2.8645503520965576, "[TT] Number of Research Facilities of the JEM = 2"]
-[10.369693756103516, 5.939624309539795, "[FF] Temperature Jump of the NIR_AB Antenna = Self-recovered in a few weeks"]
-[3.9336931705474854, 9.722393035888672, "[TT] Bandwidth (GHz) of the ICI-10 = 2.4"]
-[9.5218505859375, 6.038737773895264, "[TT] Orientation Deviation of the Collimator = -0.27\u00b0 to -0.25\u00b0 in horizontal and 0.40\u00b0 to 0.48\u00b0 in vertical direction"]
-[9.572527885437012, 8.2279691696167, "[TT] Field of View of the PIC = 1.5\u00ba"]
-[7.33384370803833, 3.6838767528533936, "[FF] Presentation Date of the GPS Radio Occultation Instrument = April 3-6, 2017"]
-[4.752708435058594, 1.565194010734558, "[FF] Mission Status Presentation of the GCOM-W = August 13, 2005"]
-[7.25945520401001, 5.217120170593262, "[FF] Function of the DDA = Measure the along-track position of the range measurement"]
-[5.6317973136901855, 5.6120429039001465, "[TT] Processor of the OBC = ERC-32 processor of ATMEL"]
-[9.534565925598145, 8.265828132629395, "[TT] Field of View of the RRA = More than 30\u00ba"]
-[6.657577037811279, 5.653100967407227, "[TT] Action of the Critical Mode = All subsystems besides the EPS power off"]
-[1.365261197090149, 2.782893419265747, "[TT] Principal Absorbing Constituents of the Band 8 = Window"]
-[11.806624412536621, 6.701081275939941, "[TT] Proton Energy Range of the MSGI-MKA = 0.1 to 15 keV"]
-[6.032155513763428, 0.9128044843673706, "[FF] Date of the Arabian Night Lights = 17 May 2021"]
-[1.3163872957229614, 1.8993829488754272, "[TT] Cargo Storage of the HTV-8 = 3.5 metric tons in the PLC, 1.9 metric tons in the ULC"]
-[11.804265975952148, 0.08803284913301468, "[FF] Principal Goal of the TESS = Detect small planets with bright host stars in the solar neighborhood"]
-[7.465522766113281, 6.417479038238525, "[TT] Dead Time of the XGRE = < 300 ns"]
-[10.105657577514648, 3.193063735961914, "[FF] Use Case of the CubeSats = Atmospheric calibration objects"]
-[4.9314398765563965, -0.09542357176542282, "[TT] Launch Time of the STPSat-3 = 01:15:00 UTC"]
-[6.709116458892822, 3.542083263397217, "[FF] Purpose of the Commercial Crew Vehicle Emergency Breathing Air Assembly (CEBAA) Flight Support Equipment (FSE) and Air Recharge Tank Assembly (RTA) = Critical hardware to support the build of the second set of emergency air supply for commercial crew vehicles, supporting as many as five crew members for up to 1 hour during an International Space Station emergency ammonia leak"]
-[10.587425231933594, 3.3501667976379395, "[FF] Form Factor of the SpaceBEE x 4 = 0.25 CubeSat"]
-[10.28945541381836, 5.774675369262695, "[TT] Operating Temperature of the Sensor = Approximately 660\u00b0C"]
-[10.105557441711426, 6.5571160316467285, "[TT] Maximum Ground Spacing of the MABEL = ~2 km at 20 km"]
-[13.701730728149414, 2.925313711166382, "[TT] Satellite Mass of the ADEOS spacecraft = 3560 kg"]
-[9.570454597473145, 0.8269848823547363, "[TT] Image Distances of the Rosetta = 80-100 km"]
-[8.600576400756836, 5.086042404174805, "[FF] Design of the Hyperion = Telescope, two grating spectrometers with supporting focal plane electronics, and a cooling system"]
-[9.272659301757812, 5.112174987792969, "[TT] Surface Solar Zenith Angle Constraint of the TanSat = < 70\u00b0"]
-[7.9079132080078125, 2.494234323501587, "[FF] Data Impact of the Aeolus = Positive impact of the data obtained in 2019 was roughly twice as big as it is now"]
-[4.731998920440674, -1.814682126045227, "[FF] Photo Transmission Date of the Chang'e-3 = Dec. 15, 2913"]
-[7.504781723022461, 8.692688941955566, "[TT] GSD of the Spectral Band B = 5"]
-[6.531126499176025, 2.0141470432281494, "[FF] URL of the NuSTAR = http://www.orbital.com/newsinfo/publications/NuStar_Fact.pdf"]
-[7.518831729888916, 6.380719184875488, "[TT] Fast Plasma Investigation Event Duration of the MMS = 45 milliseconds"]
-[4.7143988609313965, 7.0143818855285645, "[FF] Data Downlink of the ATLAS = X-band, data rate of 220 Mbit/s"]
-[3.524778366088867, 6.3310933113098145, "[TT] Antenna Dish Size of the KSAT = 3.7 meter"]
-[4.247067928314209, 0.33726656436920166, "[FF] Launch Date of the JPSS-2 = 2019"]
-[9.676153182983398, 8.41650676727295, "[TT] FOV of the Microdosimeter A = 38\u00ba"]
-[5.0037150382995605, 3.5715248584747314, "[TT] Manufacturer of the Safe-mode Computer = \u00c5AC Microtec"]
-[5.964445114135742, 0.693821132183075, "[TT] Discovery Year of the Lutetia = 1852"]
-[10.520256996154785, 3.30452561378479, "[TT] Type of the TROPICS = 3U CubeSats"]
-[11.34805679321289, 4.283173561096191, "[TT] Size of the ZACUBE-1 = 1U"]
-[8.991762161254883, 6.16971492767334, "[TT] Scanning of the MIS Instrument = Conical scanning at 31.6 rpm"]
-[11.75450611114502, 3.2968223094940186, "[TT] Number of the Thrusters = 4"]
-[5.896007537841797, 0.799153208732605, "[TT] Image Capture Date of the Payload Camera = July 29, 2018"]
-[11.613405227661133, 3.5830078125, "[TT] Motor Type of the FWA = Stepper motor / gear box with reduced backlash"]
-[10.082791328430176, 1.3176140785217285, "[TT] Formation Start of the Milky Way = 0.8 billion years after the Big Bang"]
-[4.495406627655029, 0.9758433699607849, "[TT] Malfunction of the IRU = September 2006"]
-[7.124533176422119, 7.178822040557861, "[TT] Doubled Pulse Energy of the LOM = 250 \u00b5J to 1.2 mJ"]
-[8.08240795135498, 8.510013580322266, "[TT] Spectral Range of the Radiometer = Advanced Visible and Near-Infrared (AVNIR)"]
-[7.3821868896484375, 3.846855640411377, "[TT] Model of the Nikon D3S = Nikon D3S"]
-[9.037398338317871, 0.2925199568271637, "[TT] Orientation of the Burroughs Crater = North is up"]
-[5.448145389556885, 0.6129593849182129, "[FF] Launch Date of the ENVISAT-1 = 2002"]
-[8.903627395629883, 4.873486518859863, "[TT] Group Organization of the SPS = 2 groups of 4 sensors"]
-[8.252168655395508, 0.8177782893180847, "[TT] Containment of the Cerro Pelado fire = 10 percent"]
-[6.099756240844727, 6.354247093200684, "[TT] Number of Services of the DCPs = 1000"]
-[10.272713661193848, 7.369926929473877, "[TT] Primary Mirror Manufacturer of the Telescope = L3Harris"]
-[4.692316055297852, 0.48737168312072754, "[TT] Launch Year of the S3D = 2028"]
-[6.176346778869629, 1.357179045677185, "[TT] Launch Date of the eROSITA = 2018"]
-[8.723637580871582, 4.722232341766357, "[TT] Star Sensor of the AOCS = Star sensor"]
-[7.096948146820068, 4.743870735168457, "[FF] MLI Area Ratio of the MLI = Unknown"]
-[6.42175817489624, 3.505384922027588, "[FF] Realignment of the DMSP F-19 = A 1994 presidential directive realigned primary command and control of DMSP under the Department of Commerce\u2019s National Oceanic and Atmospheric Administration"]
-[5.593236923217773, -0.4399208426475525, "[TT] Deployment Timing of the KE-2M satellite = After ISS reboost"]
-[6.4591851234436035, 4.743790626525879, "[FF] Operation Phases of the GPSPAC = Experimental (approximately 90 days) and Operational"]
-[11.504151344299316, 4.835171222686768, "[TT] Particle Size of the EXCISS = About the diameter of a human hair"]
-[5.574573993682861, 0.5605380535125732, "[TT] Launch Year of the ERS-1 = 1991"]
-[10.130317687988281, 7.756653308868408, "[FF] Telescope Type of the EUVI = Small Ritchey-Chretien telescope"]
-[8.518654823303223, 1.723375916481018, "[TT] Integrated water vapor of the Integrated water vapor = 2.0 kg/m 2"]
-[8.205789566040039, 7.267390727996826, "[FF] Modes of the HRV = Panchromatic (PAN) mode and Multispectral (MS) mode"]
-[5.009912967681885, 4.531791687011719, "[TT] Entanglement Test Performer of the QUESS = Chinese team"]
-[4.925512313842773, -0.056489571928977966, "[TT] Launch Date of the TAIKI = 31 December 2023"]
-[7.046403408050537, 3.314495086669922, "[FF] Unknown of the Vricon\u2019s 3D Technology = Unknown"]
-[8.320895195007324, 5.350600242614746, "[TT] Radiometric Calibration Accuracy of the Satellite = < 4%"]
-[5.451196670532227, 0.6867760419845581, "[FF] Utilization Presentation Date of the ISERV Pathfinder = Oct. 1-5, 2012"]
-[8.892740249633789, 5.759984970092773, "[TT] Fine-Pointing Range of the GT = Approximately 70 arcsec"]
-[10.213345527648926, 8.163113594055176, "[TT] Aperture Diameter of the GMI = 1.22 m"]
-[8.419376373291016, 7.225094318389893, "[TT] Number of CMOS Cameras of the CubeSense = 2"]
-[10.273178100585938, 8.05788803100586, "[TT] Telescope Aperture of the LCT = 135 mm"]
-[4.516398906707764, 3.0690367221832275, "[FF] Location of the CONAE MOC = Te\u00f3filo Tabanera Space Center in the Province of C\u00f3rdoba (Argentina)"]
-[9.920616149902344, 1.7061851024627686, "[FF] Theme of the L3 = Gravitational Universe"]
-[12.118003845214844, 4.652490615844727, "[TT] Size of the ATLAS = About the size of a Smart Car"]
-[5.98030948638916, 8.741751670837402, "[TT] MTF of the Instrument = MS: \u2265 12.0% @ Nyquist frequency"]
-[11.898354530334473, 5.58521032333374, "[TT] Active Area of the ICON FUV Instrument = 25 mm (circular)"]
-[5.660943508148193, 7.108029842376709, "[TT] Data Rate of the Source data rate = 25 Mbit/s"]
-[7.6054582595825195, 3.810377359390259, "[TT] Tracking Accuracy of the NightPod = 7 arcsec"]
-[6.752989292144775, 5.967341899871826, "[TT] AOCS Mode of the TTTC = Precise mode"]
-[5.465348243713379, 6.170241832733154, "[TT] Code Memory Storage of the CPU Board = 3 MB of EEPROM"]
-[4.9650187492370605, 0.5671393275260925, "[FF] Launch Date of the Inspiration4 = Mid-September"]
-[10.759538650512695, 1.4752277135849, "[FF] Size of the Neutron Stars = Typically only the size of a large city"]
-[10.334246635437012, 2.1258320808410645, "[FF] High-energy source of the Swift = Unknown"]
-[11.790124893188477, 5.380427837371826, "[FF] Size of the REXJ = Small as a microwave oven"]
-[6.323105335235596, 2.592489719390869, "[FF] Purpose of the Orion Spacecraft = Launch astronauts into space, perform multiple long distance/long duration space missions, and then return the astronauts safely back to Earth"]
-[4.56904935836792, 7.866024971008301, "[TT] Transmit Frequency (MHz) of the HRIT HiRID = 1558"]
-[7.7542290687561035, 3.062573194503784, "[FF] CO of the GOSAT-2 = Measuring Item"]
-[4.486708641052246, 3.0117177963256836, "[TT] Location of the GSOC = Oberpfaffenhofen"]
-[5.93853235244751, 5.24064302444458, "[TT] Command Uplinks of the ISL = Can be uploaded in advance"]
-[10.750312805175781, 1.0682555437088013, "[TT] Diameter Uncertainty of the KELT-11b = Just under 4300 km"]
-[4.659546852111816, 3.227609157562256, "[TT] Responsible Organization of the MOC = CONAE"]
-[4.700207233428955, 1.7123584747314453, "[TT] Launch Date of the EUTELSAT KONNECT = 17 January 2020"]
-[3.8468220233917236, 3.4377965927124023, "[TT] Launch Date of the Galileo = May 24, 2016"]
-[4.797278881072998, 0.5284311771392822, "[TT] Launch Date of the STARE-C = Q3 of 2014"]
-[7.448032855987549, 0.8209540247917175, "[FF] Mission Name of the LunaH-Map = LunaH-Map"]
-[14.23910140991211, 3.2370188236236572, "[TT] Mass of the DPS = Approximately 100 kg"]
-[11.67829704284668, 6.582820415496826, "[TT] Energy Range of the Chandra = 0.5 to 7 keV"]
-[3.8249905109405518, 3.4503493309020996, "[TT] Launch Date of the Galileo = 22 August 2014"]
-[3.835963487625122, 3.3924899101257324, "[TT] Launch Date of the SAR/Galileo VOV-3, IOV-4 = Oct. 12, 2012"]
-[10.0673828125, -1.5289537906646729, "[TT] Orbit Inclination of the ResourceSat-2 = 98\u00ba"]
-[5.585662841796875, -2.0223348140716553, "[FF] Conference Date of the Cross-calibration for KOMPSAT-2 MSC images using EO-1 Hyperion = April 16-18, 2014"]
-[8.446695327758789, 7.37113618850708, "[FF] Signal-to-Noise Ratio of the GOCI-II CMOS Imaging Sensor = Not provided"]
-[6.301983833312988, 8.129386901855469, "[TT] No of Passbands of the Channel 9 = 1"]
-[8.020302772521973, 9.10029125213623, "[TT] Wavelengths of the OSIRIS = 1263 nm, 1273 nm, 1530 nm"]
-[5.536671161651611, 5.782277584075928, "[TT] CPU of the C&DH = RAD750"]
-[13.55212116241455, 5.464515209197998, "[TT] Solar Cells Quantity of the H3 and H4 = 140 cells"]
-[6.738021373748779, 6.068060398101807, "[FF] Development Date of the Space Laser Transmitter = Feb. 15-18, 2010"]
-[5.59623384475708, 3.6512486934661865, "[TT] Number of Secondary Payloads of the PSLV-C37 = 103"]
-[9.046055793762207, 6.50266170501709, "[TT] Image Segment Size of the CaSSIS = 22.7 x 6.6 km"]
-[3.422893524169922, 5.270269870758057, "[TT] Data Downlink Frequency of the SAR = 2.265 GHz"]
-[4.886685848236084, 0.4802980422973633, "[TT] Launch Date of the ExoMars 2020 = 2022"]
-[6.235929012298584, 4.132482528686523, "[FF] Data Distribution of the ADEOS-II = Online or through a medium"]
-[8.761573791503906, 4.9135332107543945, "[TT] Number of Sensors of the SloshSat = 270"]
-[6.1743316650390625, 1.3136374950408936, "[FF] Status Update Date of the Europe\u2019s laser satellite = 23 January 2019"]
-[10.698347091674805, 4.0694169998168945, "[TT] Attitude Control of the CanX-4&5 = 0.5\u00ba"]
-[6.763838768005371, -0.6209681034088135, "[TT] Repeat Cycle of the GOSAT-2 = 6 days"]
-[6.939294338226318, 1.5782893896102905, "[TT] Image Resolution of the Landmapper BC = 2.5-meter"]
-[8.978418350219727, 3.3374645709991455, "[FF] Purpose of the PME = Studying characteristic macroscopic properties of ionospheric plasmas"]
-[11.88039779663086, 5.446712017059326, "[TT] Physical Size of the Instrument = Optics: \u00d8 420 mm x 755 mm, Electronics : 320 mm x 215 mm x165 (mm)"]
-[7.152092456817627, 4.786267280578613, "[FF] Data Transport of the SPA-1 = Unknown"]
-[9.046333312988281, 7.301637649536133, "[TT] Resolution of the Image = 4.5 m/pixel"]
-[7.5970778465271, 4.592358112335205, "[FF] Purpose of the Lateral Sensor = Alignment of two formation-flying satellites"]
-[7.195512294769287, 2.53841495513916, "[FF] Documentation of the Herbert J. Kramer = Observation of the Earth and Its Environment: Survey of Missions and Sensors"]
-[8.727518081665039, -0.6808024048805237, "[TT] Spatial Resolution of the ICEYE-X1 = 10 m x 10 m"]
-[13.412837982177734, 2.9028520584106445, "[TT] Propellant for Initial Orbit Raising of the Geo Satellite = 2 tons"]
-[3.290020227432251, 5.03732967376709, "[TT] Quad Pol Swath Width of the SAR Processor = 175 km"]
-[8.417913436889648, 3.8678090572357178, "[FF] Total Irradiance Monitor (TIM) and the Spectral Irradiance Monitor (SIM) of the TSIS = Upgraded versions of those flying on the SORCE mission"]
-[7.097800254821777, 6.752600193023682, "[FF] Function of the Signal Processor = Works only when the MAPMTs and the APDs detect a signal simultaneously"]
-[4.733951568603516, -1.8082036972045898, "[FF] Measurement Date of the Chang'e-4 = 15 August 2020"]
-[14.283036231994629, 3.152897357940674, "[TT] Total Mass of the FOTINO = 6 kg"]
-[11.743698120117188, 6.752079963684082, "[TT] Ion Isotropy Boundaries Energy Range of the ELFIN = 100-500 keV"]
-[7.981729030609131, 5.323660850524902, "[TT] Short-range of the FLLS system = < 7 m"]
-[5.1457085609436035, -0.5866966247558594, "[FF] CNES Board Approval Date of the TARANIS = Dec. 9, 2010"]
-[5.316967964172363, 0.3481285274028778, "[TT] Payload Status of the RAVAN = Powered off"]
-[5.237231731414795, 4.884775161743164, "[TT] Sensor Type of the Satellite = GNSS receiver"]
-[8.172924995422363, 6.211480140686035, "[TT] Type of the ECP-Lite = Low size, weight and power sensor"]
-[8.713953018188477, 4.826608180999756, "[FF] Measurement Performances of the Star Tracker = Better measurement performances than the current baseline Myriade's Star Tracker"]
-[13.24802017211914, 7.315832138061523, "[TT] Power Consumption of the TWTA = < 1385 W"]
-[7.643532752990723, 9.228717803955078, "[TT] Band 4 Wavelength of the AEISS = 630 nm - 690 nm"]
-[5.699810028076172, -0.5919510126113892, "[TT] Operating Lifetime of the SPOT-6 = 10 years"]
-[7.393998146057129, 0.2899317741394043, "[FF] Launch of the OSIRIS-REx = Required considerable power"]
-[12.04369831085205, -0.1983644813299179, "[TT] Sky Coverage of the TESS = About 75%"]
-[11.29738712310791, 2.8282716274261475, "[TT] Mass of the Nanosatellite = 5.5 kg"]
-[7.846871852874756, 1.029141902923584, "[FF] Date of the The Black Fire Blows Up in New Mexico = 24 May 2022"]
-[5.446107864379883, 3.5390546321868896, "[TT] Location of the Procedures = Inmarsat Operations Center"]
-[5.568087577819824, 6.740784645080566, "[TT] Data Downlink Time of the ABEX = Within eight hours"]
-[8.3745756149292, 1.7893400192260742, "[TT] Range of measurements of the Ocean SST = 16 km"]
-[4.140094757080078, 7.209743976593018, "[TT] Frequency Band of the X-band subsystem = X-band"]
-[5.715395450592041, 6.797793388366699, "[TT] Packet Size of the UDP = ~ 425-475 bytes"]
-[10.37508487701416, 4.590401649475098, "[FF] Radio and Reaction Wheels Current of the MarCO-B = Significantly more"]
-[13.528899192810059, 6.591808795928955, "[FF] Battery Recharge of the Safe-mode System = Possible while it is in operation"]
-[14.225584983825684, 3.1000173091888428, "[TT] Mass of the ASTERIA = 12 kg"]
-[6.662859916687012, 5.271045684814453, "[FF] Functions of the DAQLB = Quicklook display, browse generation, calibration analysis and ADIF generation"]
-[7.419187068939209, 6.196103096008301, "[FF] Observation Type of the Shuttle Laser Altimeter (SLA) = Laser-pulse echo-recovery measurements of terrestrial surfaces"]
-[11.467034339904785, 4.816928863525391, "[TT] Length of the Agena = ~ 21 m"]
-[8.251422882080078, 2.155888557434082, "[TT] Provider of the SeaWinds scatterometer = National Aeronautics and Space Administration/Jet Propulsion Laboratory (NASA/JPL)"]
-[5.446462631225586, 6.4096527099609375, "[TT] Data Storage Capacity of the LEOStar-3 = 704 Gbit at EOL"]
-[13.729620933532715, 2.9094040393829346, "[TT] Mission of the TeleSat LEO Phase 1 = 168 kg"]
-[8.661779403686523, 4.499882221221924, "[FF] Purpose of the Camera System = Demonstrate a star- and horizon tracker for attitude determination, as well as observe meteors to improve the understanding of the beginning of the solar system and test the system for future missions"]
-[3.623528242111206, -0.8405502438545227, "[TT] Orbit Type of the Unicorn-2L, -2M and -2N = Low-Earth"]
-[3.915031671524048, 2.015679121017456, "[TT] Launch Vehicle of the AlSat-2A and -2B = PSLV (Polar Satellite Launch Vehicle)"]
-[8.001886367797852, 4.406857490539551, "[FF] Orbit Transfer Method of the LUMIO = Stable Manifold Injection Maneuver"]
-[4.198450088500977, 3.935441493988037, "[FF] Development of the COSPAS = Russia (former Soviet Union) in the mid-1970s"]
-[7.120975494384766, -0.5578033328056335, "[TT] Spin of the Bennu = Opposite direction of its orbit"]
-[6.830148696899414, 1.827972650527954, "[FF] URL of the ACE - Advanced Composition Explorer = http://www.nasa.gov/press-release/goddard/2016/ace-cosmic-ray"]
-[6.0373005867004395, 3.4067800045013428, "[FF] Deployment Methods of the Argo Floats = Volunteer Observing Ships (VOS), aircraft, naval ships and research vessels"]
-[6.7310895919799805, 6.107900142669678, "[TT] Number of Configurations of the TIM = 7"]
-[7.784346580505371, 8.630928039550781, "[FF] Spectral Bands of the Maps = 400-500 nm, 500-600 nm, 600-700 nm, 750-925 nm"]
-[3.4298489093780518, 6.371443748474121, "[TT] Size of the Antenna = 3.3 m x 2.7 m"]
-[6.282101154327393, 2.502817153930664, "[TT] Principal Investigator of the Carruthers Geocorona Observatory = Lara Waldrop"]
-[7.9881792068481445, 7.658204078674316, "[TT] Spectral Range of the High-Resolution Hyperspectral Imager = 0.4 to 2.5 \u00b5m"]
-[5.8239898681640625, -0.8034570217132568, "[FF] Function of the Restore-L servicer = Extend a satellite's lifespan"]
-[10.1841402053833, 4.622864723205566, "[TT] Maximum Attitude Rate of the Reaction Wheel (RW) = 0.7\u00ba/s in roll axis"]
-[13.363036155700684, 5.410717010498047, "[TT] Configuration of the NPSat-1 = 12-sided cylinder with body-mounted solar cells on all cylinder sides"]
-[7.132690906524658, -0.40807223320007324, "[TT] Nodal Crossing Time of the SAC-D/Aquarius = 18:00 hours on the ascending node"]
-[5.460170745849609, 0.8026865720748901, "[TT] Operational Date of the QUESS satellite = January 19, 2017"]
-[10.430871963500977, 3.316622257232666, "[TT] Antennas of the SOURCE 3U CubeSat = 2"]
-[5.758570671081543, 5.132527828216553, "[FF] Connection of the ROSA Radio Occultation Antenna = Connected to the ROSA receiver unit by two different RF cables for L1 and L2 frequency signals directly to the LNA's, without passing through the diplexer used for the navigation one"]
-[14.610913276672363, 6.566349029541016, "[TT] Battery Capacity of the DMSP-19 = Better"]
-[5.5669264793396, 6.663333415985107, "[TT] Data Transmission of the EDRS-A = 1.7 petabytes"]
-[10.97317886352539, 2.8764684200286865, "[TT] Dimensions of the BlackSky microsatellite = 0.4 x 0.46 x 0.84 m"]
-[8.27100658416748, -0.4754217565059662, "[TT] Annual Maximum Extent of the Arctic Sea Ice = 15.05 million km2 (5.81 million square miles)"]
-[5.22458028793335, 0.6924655437469482, "[FF] Launch Date of the CanX-4 and -5 = 2014"]
-[5.328060150146484, 4.0432047843933105, "[TT] Number of Satellites of the MEO Constellation = 30"]
-[8.180034637451172, 6.424142360687256, "[FF] Observation Capabilities of the BILSAT-1 = Wide Field of Regard"]
-[11.512175559997559, 0.8286833763122559, "[TT] Mass of the Beta Pictoris b = At least 50 times more massive than AU Mic b"]
-[7.421456813812256, -0.11027029156684875, "[TT] Primary Science Mission Duration of the Philae = Nearly 57 hours"]
-[9.810136795043945, 7.491659641265869, "[TT] GSD of the CIRiS = 0.166 km"]
-[7.180506229400635, 3.066401243209839, "[FF] Data Usage of the SMOS = All-weather microwave data"]
-[8.597923278808594, 0.11447189748287201, "[TT] Porosity of the Comet = 70-80%"]
-[4.84208345413208, 2.5276072025299072, "[TT] Launch Provider of the Eutelsat Quantum = Arianespace"]
-[11.372329711914062, 4.322916030883789, "[FF] Size of the MCubed/COVE-2 = 1U"]
-[6.467861652374268, 6.395340442657471, "[FF] Communication Method of the OUFTI-1 = Direct communication"]
-[4.877388000488281, 0.6439223885536194, "[FF] Validation Mission Date of the MOMS-02 = 1995"]
-[5.73527193069458, 7.149455547332764, "[TT] Data Rate of the Level 2/3 products = < 4.7 Mbit/s"]
-[11.53720474243164, 0.5122901201248169, "[FF] Observation Targets of the Twinkle = Astrophysical objects (e.g. exoplanets, solar system bodies, stars, disks)"]
-[10.15962028503418, 8.060770034790039, "[TT] Focal Length of the Telescope = 320 mm"]
-[7.052627086639404, 7.23975944519043, "[TT] Laser Energy of the ATLAS instrument = ~1 mJ"]
-[10.982812881469727, 2.057784080505371, "[FF] Extension Approval Date of the XMM-Newton = Nov. 14, 2007"]
-[8.358540534973145, 2.946429491043091, "[FF] Function of the TEMPO = Provide near-real-time North American air quality information"]
-[5.798222541809082, 1.3908387422561646, "[FF] Mission Start Date of the MMS (Magnetospheric Multiscale) Mission = 2014"]
-[6.184660911560059, -0.5775588750839233, "[TT] Commissioning Phase Duration of the CBERS-4A = About three months"]
-[4.372136116027832, 7.420825004577637, "[TT] Uplink and Downlink Frequency of the \u00d8rsted satellite = S-band (2.114 GHz and 2.296 GHz)"]
-[4.356775760650635, 0.7200143337249756, "[FF] Integration Test Date of the PROBA-V = April 15, 2013"]
-[14.232354164123535, 3.177173376083374, "[FF] Mass of the Lemur-1 = 3U"]
-[9.011530876159668, 2.5438108444213867, "[FF] Mission of the Voyager = Outer heliosphere research"]
-[8.862408638000488, 2.5520973205566406, "[FF] Original Purpose of the CRS = Measure planetary systems"]
-[7.629421234130859, 2.2834668159484863, "[FF] Emission Sources of the CH4 = Intense emission plumes from pipelines to large scale, weakly emitting wetlands and agricultural sources"]
-[11.317185401916504, 6.062741279602051, "[TT] Deployment System Material of the LFSA = Shape Memory Alloys (SMA)"]
-[4.260300159454346, 1.9897559881210327, "[TT] Mission Status of the NigeriaSat-X = Operational (extended)"]
-[5.671650409698486, 4.010249137878418, "[TT] Instrument Type of the TDP = Space environment"]
-[11.685916900634766, 4.58440637588501, "[TT] Secondary Body Diameter of the Didymos = About 150 m"]
-[8.575424194335938, 2.226788282394409, "[FF] Description of the Sudden Stratospheric Warming = Causes the strong wind around the edge of the polar vortex to weaken or reverse, leading the temperature of the polar stratosphere to rise rapidly by tens of degrees Celsius"]
-[8.385591506958008, 0.804432213306427, "[TT] Area of the Yaguas National Park = 2 million acres (809,370 ha)"]
-[12.415098190307617, 0.6118569374084473, "[FF] Disturbance Sources of the PLATO = Thermoelastic effects, attitude control and determination, image acquisition"]
-[6.944728851318359, 7.77003288269043, "[TT] Size of the Main Reflector = 1.8-m"]
-[7.551750183105469, 3.7266945838928223, "[FF] Technology Demonstrations of the RemoveDebris = Use of a net, a harpoon, VBN (Vision-Based Navigation) and a dragsail"]
-[7.716560363769531, 5.6057448387146, "[FF] Test Campaign Date of the SAC-D/NIRST Radiometer = Oct. 14-17, 2008"]
-[6.656601905822754, 3.7628333568573, "[FF] Ground Truth of the LPR = Stratigraphic architecture of an ejecta deposit"]
-[7.940141677856445, 2.0719120502471924, "[FF] Objective of the SeaWiFS = Measurement of reflected visible sunlight from the ocean surface for the derivation of ocean-color data"]
-[6.287166595458984, -0.4134094715118408, "[TT] Operating Hours of the LMOC = 24 hours per day, seven days per week"]
-[5.810192108154297, -0.5992749333381653, "[TT] Lifetime of the PM = More than 10 years"]
-[9.784276008605957, 0.45630544424057007, "[TT] Formation Control Accuracy of the PROBA-3 = Millimeter level"]
-[14.223662376403809, 3.1731655597686768, "[TT] Mass of the OWLS = 0.5 kg"]
-[6.712121963500977, 4.708531856536865, "[FF] Type of the Atmospheric Skip Entry = Navigation System"]
-[5.085918426513672, 3.3251545429229736, "[TT] Manufacturer of the BEAM = Bigelow Aerospace"]
-[8.152915954589844, 8.034392356872559, "[FF] Calibration Methods of the OCTS sensor = Solar and internal lamp for VNIR, deep space and black body for IR"]
-[5.319061756134033, 0.9377832412719727, "[FF] Launch Date of the Kaber = Unknown"]
-[10.215340614318848, 6.564027309417725, "[TT] Laser Retroreflector Assemblies of the EGS = 120"]
-[5.731959342956543, 3.776226758956909, "[TT] Support of the Test Station = Rapid AI&T (Assembly, Integration, and Test)"]
-[4.553518772125244, 1.0656415224075317, "[TT] Launch Date of the SAOCOM-1B = August 2020"]
-[8.32877254486084, 3.995060920715332, "[FF] Solar Calibration Frequency of the Satellite = Roughly weekly"]
-[3.4524261951446533, -0.89936763048172, "[TT] Orbit Type of the ROSE-L = Sun-synchronous"]
-[7.820976734161377, 3.0513622760772705, "[TT] Measurement Goal for Carbon Dioxide of the GOSAT-2 = 0.5 ppm"]
-[10.8627347946167, 7.470032691955566, "[TT] Swath Width of the ALOS-4 = 50 km"]
-[11.723377227783203, 6.684914588928223, "[TT] Energy: 0.53 keV (2.3 nm) of the O K-edge = O at 0.53 keV (2.3 nm)"]
-[16.486539840698242, 3.571916341781616, "[FF] Date of the OneWeb = 2 November 2021"]
-[5.238428592681885, 5.605494022369385, "[TT] Data Bus of the C&DH = MIL-STD-1553B"]
-[9.220354080200195, 6.751953125, "[TT] Polarization of the Atmospheric-sounding instrument = Lower than 0.1% in both nadir and glint modes"]
-[9.46749496459961, 6.199919700622559, "[TT] Scanning Technique of the MWRI-RM = Conical scanning technique of 53.1\u00b0 zenith angle"]
-[10.77672290802002, -0.26953092217445374, "[TT] Radial Baselines of the Tandem-L = 0 m to 600 m"]
-[5.549811840057373, 5.0239949226379395, "[TT] GPS/QZSS Differential Code Biases Stability of the QZS-1 = Better than 1 ns"]
-[10.017391204833984, 7.891831874847412, "[TT] Telescopes of the ROLO = 2"]
-[6.675522327423096, 4.98868989944458, "[FF] Precise Tracking of the GPS = Unknown"]
-[4.907650470733643, 3.460174322128296, "[TT] Manufacturer of the EROS-B = ImageSat International N.V."]
-[7.583995342254639, 5.224909782409668, "[FF] Payload Module Components of the Euclid = Telescope, Visual Imager, Near-Infrared Spectrometer and Photometer"]
-[12.071145057678223, 6.330880165100098, "[TT] First Event of the AMS-02 = 20 GeV electron"]
-[5.663895606994629, 3.6960043907165527, "[TT] Total Impulse of the SkySat-3 = 1,732 Ns"]
-[11.238811492919922, 5.732265472412109, "[TT] Thickness of the Aluminum Film = 70 nm"]
-[9.617856979370117, 8.314046859741211, "[FF] Field of View Map of the EPI-Hi = Unknown"]
-[8.453794479370117, 0.7993115186691284, "[TT] Utilization of the ICI-4 = Quasi-window, cloud ice retrieval, cirrus clouds"]
-[10.294197082519531, 5.500269889831543, "[TT] Cooling Power of the ABI cooler system = 53 K and 183 K"]
-[3.940483808517456, 6.273301601409912, "[TT] Deployable Antennas of the Satellite = Four"]
-[10.606650352478027, 0.9450677037239075, "[TT] Total Mass of Jet Streams of the Juno = About 1% of Jupiter's mass"]
-[10.279348373413086, 1.8021507263183594, "[FF] Observation Result of the NuSTAR = Inner regions of a star are extremely turbulent at the time of detonation"]
-[5.597055435180664, 1.2624871730804443, "[FF] Conference Presentation Date of the EO-1 = Mar. 6-13, 2004"]
-[8.20010757446289, 4.964132308959961, "[FF] Additional Test of the Biomass = Thermal elastic distortion test"]
-[8.119415283203125, 5.482861042022705, "[FF] Purpose of the Refocus Mechanism Assembly = Fine-tune the instrument focus"]
-[5.955234527587891, -0.22911325097084045, "[FF] Operations Budget of the Small space mission = May have long since been exhausted at end of mission"]
-[10.538993835449219, 2.2003567218780518, "[TT] Target of Opportunity (ToO) Response Time of the X-ray telescopes = Less than 24 hours"]
-[10.94378662109375, 3.7258832454681396, "[TT] Propulsion of the NEA Scout = Solar sail"]
-[4.4031548500061035, 2.8181114196777344, "[TT] Location of the STMSat-1 = Arlington, VA"]
-[10.850595474243164, 7.548044204711914, "[TT] Swath Width of the PanMUX = 60 km"]
-[2.3377745151519775, 1.31678307056427, "[FF] Deployment of the NanoSail-D2 = Shortly after deployment of the NanoSail-D2, the solar sail will deploy"]
-[5.998114585876465, 0.27971506118774414, "[TT] Deployment Gap of the ASTERIA = 3 hours plus"]
-[13.310054779052734, 7.699997425079346, "[TT] Peak Transmit Power of the KaRIn = 1500 W"]
-[4.789358615875244, 0.06575224548578262, "[TT] End of Life Date of the CAPSTONE = June 28, 2023"]
-[10.010771751403809, 2.9282333850860596, "[FF] Launch Date of the CubeSat = October 2011"]
-[4.951581001281738, 2.712966203689575, "[FF] Product of the Kleos Space = GEOINT DaaS"]
-[8.926233291625977, 4.8366899490356445, "[TT] Manufacturer of the Control Moment Gyros = Honeywell"]
-[6.576668739318848, 2.3452916145324707, "[FF] URL of the PROBA-V-CC = https://space.oscar.wmo.int/satellites/view/proba_v_cc"]
-[3.2143454551696777, 5.760202407836914, "[TT] Dimensions of the SAR Antenna = 3.3 m x 2.7 m"]
-[6.722757339477539, 5.261704921722412, "[FF] Components of the HPS = OBC (On-Board Computer), TCTM (Telecommand & Telemetry) module, PDU (Power Distribution Unit)"]
-[11.955934524536133, 5.0079193115234375, "[TT] Size of the SIR-2 = 260 mm x 171 mm x 143 mm (EO module), 146 mm x 125 mm x 33.5 mm (electronics box)"]
-[7.811628341674805, 5.25816011428833, "[FF] Navigation Purposes of the Vision Based Sensors = Long distance detection and tracking of a moving target (VBS FR), relative position/attitude estimation of a cooperative target (VBS CR)"]
-[3.0190703868865967, 2.319986581802368, "[FF] Information Provided of the Copernicus Sentinel-4 and Sentinel-5 = Air quality, solar radiation and climate monitoring"]
-[8.999443054199219, 5.318063735961914, "[TT] Accuracy for 2000 kg payload of the IPS = 0.5 arcseconds lateral and 41 arcseconds roll in sun mode"]
-[4.428003311157227, 7.836297988891602, "[TT] Frequency of the UHF Uplink = 449.850 MHz"]
-[3.320470094680786, 5.025432586669922, "[FF] Measurement Accuracy of the SAR Instrument = 3.5 cm/year, 1.6 cm/year"]
-[9.678483963012695, -0.5909449458122253, "[TT] Orbital Altitude of the MVIRI = About 35,786 km"]
-[4.096979141235352, 6.856451988220215, "[TT] PRF of the Antenna = 2800-3700 Hz"]
-[13.644240379333496, 2.8237695693969727, "[TT] In-Orbit Mass of the WINDS satellite = 2750 kg"]
-[7.283685207366943, 3.805605888366699, "[FF] Potential Debris Release Prevention of the DMSP-F13 = Within hours"]
-[7.026456832885742, 4.505663871765137, "[TT] Accommodation Location of the Hosted Military Payload = South Panel"]
-[7.6683783531188965, 6.376455307006836, "[FF] Monitoring Device of the Telescope System = Laser displacement meter"]
-[5.604290962219238, 3.242037534713745, "[TT] Payload Sites of the Bartolomeo research platform = 13 (12 active, 1 passive)"]
-[5.6277642250061035, 5.711372375488281, "[TT] Processor of the SCP = Honeywell 1750A processor"]
-[9.557619094848633, 7.333127975463867, "[TT] Ground Resolution of the Visible Band = 900 m"]
-[5.982905387878418, -0.4930303692817688, "[TT] Mission Duration of the RAX-2 = One year"]
-[10.223264694213867, 5.30840539932251, "[FF] Cooling Method of the Chamber with a heat exchanger = Direct contact to the base plate of the payload compartment"]
-[8.03925895690918, 5.268218994140625, "[FF] Absolute Radiometric Calibration Accuracy of the PROBA-V = Unknown"]
-[3.89404559135437, 0.18728438019752502, "[FF] Image Release Date of the SMART-1 = Oct. 5, 2015"]
-[4.872868061065674, 8.233884811401367, "[TT] Frequency of the DPS = 9.6 GHz, 17 GHz"]
-[5.106198310852051, 2.6623361110687256, "[TT] Designing Institution of the ZACube-2 = F'SATI (French South African Institute of Technology) at CPUT (Cape Peninsula University of Technology)"]
-[12.093770980834961, 3.719902753829956, "[TT] Regulated Pressure of the EPTA = 2.2 bar"]
-[9.470528602600098, -1.3217194080352783, "[FF] Orbit of the Galileo Navigation = Geostationary orbit"]
-[7.452480792999268, 6.753643989562988, "[TT] Integration Time of the Optics = 15 ms"]
-[7.107152462005615, 3.704035997390747, "[FF] Design and Prototyping of the PROBA-3 = Unknown"]
-[6.492608547210693, 2.9420762062072754, "[FF] Operation of the NICER = Space Station Twist"]
-[9.867181777954102, 7.364716529846191, "[TT] Ground Sample Distance of the Dove-1 = 4.4 m"]
-[8.90976333618164, 5.744617938995361, "[TT] Accuracy Requirement of the Metrology System = ~10 arcseconds"]
-[5.479144096374512, 1.2436264753341675, "[TT] Mission Extension of the SOHO = End of 2016"]
-[8.041914939880371, 5.822139739990234, "[FF] Technology of the EMIT = Image spectrometer"]
-[8.801809310913086, 7.5517120361328125, "[TT] Cross-channel Image Co-registration of the ABI = 50 \u00b5rad (VIS to IR), 28 \u00b5rad (IR to IR), 6.3 \u00b5rad (0.5, 1.0 to2 km), 5.2 \u00b5rad (0.5, 1.0 to1 km)"]
-[11.417623519897461, 4.369140625, "[TT] Size of the PR_CuNaR2 = 3U"]
-[7.95967960357666, 4.987719535827637, "[FF] Calibration of the DESIS = Pre-launch and post-launch"]
-[5.950137138366699, 6.013266563415527, "[TT] Number of Active Modules (SDRAM) of the Memory Modules = 10"]
-[5.410148620605469, 5.930180549621582, "[TT] PROM of the STRV-2 DHS = 32 k PROM"]
-[5.807053089141846, 2.6604597568511963, "[FF] Development and Launch Funding of the HyperScout 1 = Through the ESA GSTP program with contributions from the Dutch, Belgian and Norwegian national space organizations"]
-[5.502105236053467, 2.8644328117370605, "[TT] Funding Source of the SPIDER = DARPA (Defense Advanced Research Projects Agency)"]
-[4.865005970001221, -0.29980188608169556, "[TT] Launch Time (EST) of the Falcon 9 = 3:24:54 a.m."]
-[4.995889186859131, 3.132969617843628, "[FF] Satellite Manufacturer of the Airbus = True"]
-[10.349417686462402, 4.481974124908447, "[FF] Interface of the Central Cylinder = Interface for the propellant tank and reaction wheel deck"]
-[4.4923224449157715, 7.075284004211426, "[FF] Type of the Q/V-band transponder = Unknown"]
-[6.146728038787842, -0.47702911496162415, "[TT] Mission Duration of the STS-85 = 11 days and 19 hours"]
-[8.02084732055664, 6.5079851150512695, "[TT] Scan Duration of the SSMIS = 1.88 seconds"]
-[8.281123161315918, 1.303743600845337, "[TT] Precipitation on October 24 of the Downtown San Francisco = 4.02 inches"]
-[3.224994421005249, 5.048449993133545, "[TT] Spatial Resolution of the SAR = 25 m"]
-[5.524398326873779, -0.5469744205474854, "[TT] 14-Day Lunar Night of the Yutu = Feb. 13, 2014"]
-[9.018502235412598, 4.648692607879639, "[TT] Quantity of the HAM sensor = 3"]
-[6.79449987411499, 5.377705097198486, "[FF] Components of the TXA = Differential-QPSK modulators, Coaxial switches matrix, HPAs, Output ports filtering and diplexing, Waveguide switch matrix"]
-[11.173924446105957, 5.19962215423584, "[FF] Scintillation Climatology Model of the C/NOFS = Improve scintillation climatology model"]
-[10.977320671081543, 2.045849084854126, "[FF] Article Date of the XMM-Newton = 18 May 2018"]
-[10.115918159484863, 3.036203622817993, "[FF] Door Opening of the PEPPOD#2 = Initiating the release of the Dove-4 nanosatellite"]
-[3.4343087673187256, -0.871987521648407, "[TT] Orbit of the Vigilance Mission (KSF1) = 525 km Sun Synchronous orbit"]
-[7.943750858306885, 8.410021781921387, "[TT] Spectral Bands of the Pan Imager = 0.536-0.843 \u00b5m, 0.783-0.883 \u00b5m"]
-[5.611227512359619, -0.7802152037620544, "[TT] Design Life Span of the Yutu = Three months"]
-[11.398324012756348, 8.927016258239746, "[FF] Image Acquisition Dates of the MODIS = April 16, 2021 and October 16, 2021"]
-[5.980216026306152, 7.528540134429932, "[TT] Sampling Rate of the IMU = 400 Hz"]
-[5.016495227813721, 3.3321471214294434, "[TT] Manufacturer of the LAICE = Virginia Tech"]
-[7.119570732116699, 2.074024200439453, "[FF] Image Source of the MTVZA-GY = Roskosmos, Roshydromet/Planeta"]
-[7.079128265380859, 8.268268585205078, "[TT] Radiometric SNR of the Instrument = 400 at the bottom of the limb to 40 at the top"]
-[7.4347639083862305, 2.3700711727142334, "[TT] Coverage of the Satellite = Global"]
-[8.236141204833984, 7.57966947555542, "[TT] Spectral Range of the CCD Detector System = 450 nm to 900 nm"]
-[13.639922142028809, 5.810471534729004, "[TT] Solar Panels Power of the EROS-A = 450 W"]
-[6.253104209899902, -1.1293905973434448, "[TT] Mission Length of the GRACE = 5 years"]
-[11.527356147766113, 6.196852684020996, "[TT] Detectable Minimum Energy of the Gamma-ray Counter = < 30 keV"]
-[9.45519733428955, -0.42081671953201294, "[TT] Perigee Altitude of the STRV-1a = 280 km"]
-[5.387267112731934, 4.3069329261779785, "[TT] Provider of the Ground Station = KSAT (Kongsberg Satellite Services AS) and the Near-Earth Network (NEN)"]
-[10.346919059753418, 2.060821771621704, "[TT] Scientific Goal of the ABEX = Study Gamma-Ray Bursts (GRBs)"]
-[10.911330223083496, 10.080224990844727, "[FF] Cooling Pump Failure of the Alpha Magnetic Spectrometer (AMS-02) = Unknown"]
-[3.9585959911346436, 6.487520217895508, "[FF] Number of Consecutive Deployments of the VDES Antenna = Over 100"]
-[8.556014060974121, 5.516550540924072, "[TT] Required Accuracy of the Satellite Position = 12.8 cm"]
-[11.828252792358398, 6.638330936431885, "[TT] Energy of the VIS (red) = 1.9 eV"]
-[4.630467414855957, 2.763810157775879, "[TT] Mission Control Location of the Odin = Stockholm"]
-[6.73832368850708, 0.8721956610679626, "[TT] Encounter Date of the Solar Orbiter = 4 June"]
-[4.786406993865967, 4.5477986335754395, "[FF] Number of Simultaneous Message Processing of the Argos = Up to four (eight in next series) messages"]
-[5.959594249725342, 5.78624963760376, "[TT] Modulator Module of the Transmitter = Xilinx Virtex-5 SX FPGA"]
-[12.297307014465332, 4.7746052742004395, "[FF] Size of the X-band transmitter = m3-sized"]
-[7.670899391174316, -0.7761119604110718, "[FF] Date of the ICESat-2 Antarctic Traverse = 12 Dec. 2017"]
-[6.472257137298584, 5.965925693511963, "[FF] Architecture of the LCRD = Optical-to-optical relay"]
-[9.148871421813965, 2.8719961643218994, "[FF] Technique Developer of the Solar Flare = Francoise Roddier"]
-[8.639552116394043, 8.976726531982422, "[TT] Sensitivity of the NIRSpec MIRI = 3.4 x 10 -21  Wm -2  (9.2 \u00b5m, \u03c4 i =10,000 s, R=2400)"]
-[7.815850734710693, 8.727118492126465, "[TT] Spectral Responsivity of the SPIRIT-III = 2.5 to 28.0 \u00b5m"]
-[5.248448371887207, 1.419776201248169, "[TT] Orbit Maintenance of the JERS-1 = TACC"]
-[7.438279151916504, 2.896583318710327, "[FF] Purpose of the MethaneSAT = Locate and measure methane from human sources worldwide"]
-[10.457259178161621, 1.6359877586364746, "[FF] Accretion Disk Formation of the Supermassive Black Hole = Formed as their gravity pulls matter inward"]
-[6.400904655456543, 5.5503458976745605, "[TT] Operation of the LRI = Successful"]
-[4.51835298538208, -0.8618489503860474, "[TT] Splashdown Location of the Dragon cargo spacecraft = Pacific Ocean, approximately 300 miles southwest of Long Beach, California"]
-[8.228912353515625, 7.3799872398376465, "[TT] Function of the Photo MOSFET Switch = DLP mission"]
-[7.080509185791016, 7.86704158782959, "[TT] Optical Retro Reflector Locations of the ANDE-2 = \u00b1 90\u00ba, \u00b1 52.5\u00ba, and \u00b1 15\u00ba"]
-[6.048450946807861, -0.49831461906433105, "[TT] Experiment Duration of the DSX and VPM spacecraft = About another six months"]
-[6.84197473526001, 8.446141242980957, "[TT] Spectral Channels of the CAPI = Five spectral channels between 365 nm and 1654 nm"]
-[4.834218502044678, 7.240966796875, "[TT] RF Wideband Downlink of the QuickBird-2 = 320 Mbit/s"]
-[10.355266571044922, 2.1045093536376953, "[TT] Energy Spectrum of the eROSITA X-ray telescope = 0.3\u20130.6 keV, 0.6\u20131 keV, 1\u20132.3 keV"]
-[3.641202211380005, -0.8479131460189819, "[FF] Orbital Angles of the PolyCam = Northern hemisphere, equator, southern hemisphere"]
-[10.462479591369629, 3.257521629333496, "[TT] NN Frameworks of the Ubotica CogniSAT-XE1TM CubeSat Board = TensorFlow, PyTorch, Caffe"]
-[14.661352157592773, 6.630316734313965, "[TT] Cell Configuration of the Battery = 2P24S"]
-[7.849012851715088, 1.479905366897583, "[FF] Eruption Observation of the GOSAT = October 2017"]
-[11.959583282470703, 5.008193016052246, "[TT] Size of the IMG = 1150 mm x 930 mm x 650 mm"]
-[5.8415207862854, -0.7889609932899475, "[TT] Design Life of the STRV spacecraft = One year"]
-[4.538583278656006, 6.362393856048584, "[TT] Radio Type of the ELFIN-A = AstroDev Helium radio"]
-[5.7795209884643555, 5.8377766609191895, "[FF] Download Marking Behavior of the Data Download System = All downloaded files are marked as downloaded after the completion of the download"]
-[3.931302070617676, 6.928943157196045, "[TT] Polarization of the S-band Rx/Tx patch antennas = Circular"]
-[13.410757064819336, 5.450284004211426, "[TT] Solar Array of the Orion = Weight 260 kg"]
-[5.916928768157959, 5.600532531738281, "[FF] Redundancy of the Telemetry = High"]
-[7.979171276092529, 1.4106379747390747, "[FF] Effect of the Undersea Mountain = Attract a mound of water several meters high over the seamount"]
-[4.892337799072266, 0.38950446248054504, "[TT] Deployment Date of the SOAR = 14 June 2021"]
-[3.572841167449951, -0.9462531805038452, "[TT] Orbit of the TOMS = Polar orbit"]
-[8.504618644714355, 7.3989715576171875, "[TT] Type of the Earth sensor = CMOS camera with a fisheye lens and an image sensor of 1.3 Mpixel"]
-[7.182091236114502, 6.986243724822998, "[FF] Capability of the PTT-A3, PTT-ZE, PMT-A3 = Very low-power consumption"]
-[5.712466239929199, 0.7978034019470215, "[TT] Arrival Date of the BepiColombo = 2024"]
-[5.670416355133057, 0.2864753305912018, "[TT] Mission Lifetime of the ATLAS = 2018 to 2022"]
-[5.450098037719727, 6.995580673217773, "[TT] Nominal Operating Speed of the DCU-S(TC) module = 64 kbit/s"]
-[5.786049842834473, 1.0386528968811035, "[FF] Calibration Date of the NOAA-11 = 1989 to 1993"]
-[3.7645509243011475, 4.690679550170898, "[TT] Field of Regard of the RADARSAT-2 = 150-500km"]
-[5.071229934692383, 5.07992696762085, "[TT] Quantity of the GPS receiver = 2"]
-[4.093402862548828, 0.3319312334060669, "[TT] Revisit Time of the Corvus-HD = One to four days"]
-[9.87708854675293, 7.345161437988281, "[TT] Value of the Ground Sampling Distance = 15 m"]
-[7.009374618530273, 4.3011322021484375, "[FF] Unknown of the SUSIM = Unknown"]
-[10.280862808227539, 4.578359603881836, "[TT] Momentum Capacity of the Reaction Wheels = 80 mNms"]
-[14.231668472290039, 3.1505470275878906, "[TT] Mass of the PROCYON = 50 kg"]
-[8.36748218536377, 2.3270487785339355, "[FF] NWP Impact of the Aeolus = Positive"]
-[8.240148544311523, 3.487823963165283, "[FF] Purpose of the CRISTA = Measure infrared radiation emitted by the Earth's middle atmosphere"]
-[5.061938762664795, 2.75657320022583, "[TT] Developer of the SATTLA-2 = Ariel University (Israel)"]
-[4.624754428863525, 4.895042419433594, "[FF] Device Type of the AIS = Mixed ship and shore-based broadcast transponder system"]
-[10.143693923950195, 10.003839492797852, "[FF] Quality and Competitiveness of the Vega = On the market"]
-[8.205689430236816, -0.8653659820556641, "[FF] Measurement Type of the Skidoos = GPS to map the height of the ice"]
-[6.799170017242432, 0.7156853675842285, "[FF] First Selfie Date of the InSight = 11 December 2018"]
-[9.207271575927734, 8.126334190368652, "[TT] Target Speed of the LLNL imaging system = \u2264 3 km/s"]
-[6.402695655822754, 2.6816108226776123, "[TT] Daily Access of the RCM (RADARSAT Constellation Mission) = Daily access to 95% of the world"]
-[6.95205545425415, -0.47469502687454224, "[TT] Local Time at Descending Node of the Satellite = 10:30 hours"]
-[8.49144172668457, 6.487143516540527, "[TT] Sensor Type of the OCTS = Mechanical scanning (whiskbroom)"]
-[9.383349418640137, 4.993192672729492, "[TT] Attitude Knowledge Error of the ADCS = \u2264 29 \u00b5rad"]
-[10.774669647216797, 2.931612491607666, "[TT] Quantity of the Intersatellite Link = 1"]
-[11.484893798828125, 4.959214687347412, "[TT] Diameter of the Sample Return Capsule (SRC) = 1.5 m"]
-[5.619996547698975, 4.893733024597168, "[TT] Communication Network of the Pl\u00e9iades-Neo satellites = EDRS (European Data Relay System)"]
-[6.000800132751465, -0.3641373813152313, "[TT] Mission Lifetime of the EarthDaily Constellation = 10 years"]
-[5.562531471252441, -1.9338898658752441, "[FF] Mission Planning Verification System of the KOMPSAT-2 = Unknown"]
-[10.375609397888184, 6.793768882751465, "[TT] Length of the Secondary Mirror Support Structure = Almost 25 feet"]
-[8.784408569335938, 3.0282602310180664, "[FF] Study Area of the CADRE = Earth's ionosphere and thermosphere"]
-[3.6057140827178955, 6.996737957000732, "[FF] Polarizations of the Communication System = RHCP (Right-Hand Circular Polarization) and LHCP (Left-Hand Circular Polarization)"]
-[5.950334072113037, 0.855846107006073, "[FF] First Earth Imagery Sent Date of the Kanopus-V = Sept. 3, 2012"]
-[6.08936071395874, 3.101088047027588, "[FF] Objectives of the COTS 2/3 = Complete Licenses and Certifications, Rocket Launch and Spacecraft Inserted into Orbit, On-Orbit Operations, De-orbit Burn & Separation, Controlled Entry, Descent, and Landing, Recovery"]
-[3.417898178100586, 5.23344087600708, "[TT] SAR Payload Orbit Average Power Consumption of the RCM = Approximately 200 W"]
-[8.443581581115723, 4.16108512878418, "[FF] Input Spectral Radiance Sources of the ICU = The Sun (ICU_S mode) or by Internal Sources (ICU_IS mode)"]
-[4.264979839324951, 0.3291882574558258, "[TT] Launch Year of the JPSS-1 = 2017"]
-[10.156458854675293, 5.819531440734863, "[TT] Operative Detector Temperature of the Detector = 238 K \u00b10.10 K"]
-[9.57619571685791, 9.206212997436523, "[FF] Development Initiation Date of the IRIS Imager = April 2002"]
-[7.685434341430664, 8.000843048095703, "[TT] Sensitivity of the MWHS-II = 1.1 K"]
-[9.71545696258545, -0.34960004687309265, "[TT] Altitude of the Resurs-P1 = 475 km"]
-[4.538854598999023, 7.67572546005249, "[TT] C/N of the Uplink (VHF) = 60.515 dB"]
-[6.491464138031006, 7.613879203796387, "[TT] Data Quantization of the Instrument = 10 bit (VIS); 12 bit (NIR)"]
-[5.690617084503174, 3.338954448699951, "[TT] Delivery of Operational Requests of the TDP Operations = Weekly"]
-[5.447507858276367, 3.127443313598633, "[TT] Replacement of the MHS = AMSU-B"]
-[13.719146728515625, 2.8731119632720947, "[TT] Other SAC-D Instruments Mass of the SAC-D spacecraft = 275 kg"]
-[11.268498420715332, 0.9770285487174988, "[TT] Arrival Date at IABG of the LISA Pathfinder = March 2015"]
-[4.950057029724121, 5.857126712799072, "[FF] Prime Objective of the ZACube-2 = Demonstrate AIS (Automatic Identification System) message reception using its SDR-based payload"]
-[10.96889591217041, 7.612465858459473, "[FF] Swath width of the TOU = "]
-[5.977598667144775, 2.456780195236206, "[TT] Number of Holes of the Deployment Specialists = 86"]
-[5.334022521972656, 3.887730598449707, "[TT] Number of Satellites of the Cluster Satellites = 4"]
-[9.363598823547363, 7.074615955352783, "[TT] Spatial Resolution of the HySI = 80 m"]
-[4.861732482910156, -0.3142683506011963, "[TT] Launch Time of the SpaceX Falcon-9 Block 5 = 18:34 GMT"]
-[4.690275192260742, 8.287841796875, "[TT] Center Frequency (GHz) of the Antenna = 37"]
-[7.830718040466309, 6.967466354370117, "[FF] Design of the Interferometer = V-shaped scan arm oscillating about a beamplitter"]
-[8.709687232971191, 9.037598609924316, "[FF] Data Collection of the SMMR of Nimbus-7 = In situ measurements"]
-[8.509835243225098, 5.851588726043701, "[TT] Location Accuracy of the LIS = Within one pixel"]
-[4.595880031585693, 4.772815704345703, "[FF] Mission Objectives of the M3MSat = The primary mission objective is to provide maritime surveillance for both commercial customers, and for the Canadian government, by detecting AIS messages from space"]
-[6.153550148010254, 6.620237350463867, "[TT] Transmission Slots per Hour of the DCP = 15"]
-[9.304633140563965, 3.176975727081299, "[FF] Value of the Solar Wind Thermal Pressure = Unknown"]
-[3.7232460975646973, 6.665092945098877, "[TT] Beamwidth of the Antenna = 2.2\u00ba (Nyquist-sampling in both along-scan & down-track directions)"]
-[8.097063064575195, -1.0282683372497559, "[FF] Purpose of the ICESat-2 = Precisely measure the height of ice and track how it changes over time"]
-[6.848787307739258, 5.196586608886719, "[FF] Components of the Communications PCPMU = PU (Processing Unit), DSU (Data Storage Unit), MDMs (Modulator/Demodulator) assemblies, FGMs (Frequency Generator Modules), EPCs (Electric Power Control) cards"]
-[6.72257661819458, 5.002172470092773, "[FF] Components of the MIGS = CCC (Command and Control Center), Network of S-band satellite tracking stations, TETX (Telemetry Earth Terminal X-band), Communication network, Mission Center, ICARE Data Processing and Management Center"]
-[5.533798694610596, 6.320837497711182, "[TT] Storage and Reuse Capability of the OWS = Yes"]
-[7.586608409881592, 0.8636646866798401, "[FF] Science Objectives of the LRO = Bombardment history of the Moon, Lunar geologic processes, The processes that have shaped the global lunar regolith"]
-[5.02329158782959, 0.8999561667442322, "[TT] Shipping Date of the ALD Flight Model = 8 May"]
-[12.075064659118652, 4.835875511169434, "[TT] Interior Volume of the BA 330 module = 330 m3"]
-[8.080597877502441, 2.7971291542053223, "[FF] Objectives of the GLM = Thunderstorm & tornado warning lead time, Aviation flight route planning"]
-[13.818977355957031, 6.947056770324707, "[TT] Potential of the SCM = 300 V"]
-[9.548501014709473, 4.709601402282715, "[TT] Attitude Control of the ADCS unit = Nutation damping"]
-[11.327664375305176, 5.859130859375, "[FF] Structure of the VELOX-PII = Hard anodized Al. 7075 chassis, with stainless steel load bearing parts"]
-[8.081131935119629, 3.3921101093292236, "[TT] Operation of the RSI = Daytime (sunlit period)"]
-[8.25551986694336, -0.49794137477874756, "[FF] Annual Maximum Extent of the Antarctic Sea Ice = 18.95 million km2 (7.32 million square miles)"]
-[8.052580833435059, 6.234055042266846, "[FF] Mission Type of the NEMO-HD = High Definition Video and Multispectral Earth Imaging"]
-[8.523759841918945, 1.4801640510559082, "[FF] Microwave Spectrum of the Aquarius = Measures the wetness of the land"]
-[9.496084213256836, 7.234502792358398, "[TT] Minimum Imagery Size of the ABI = 1000 km x 1000 km (nadir)"]
-[8.572921752929688, 6.168479919433594, "[TT] Relative Accuracy of the 782 nm Band = 100 ppm"]
-[5.940735816955566, 2.8046469688415527, "[FF] Support Program of the WCOM = Strategic Priority Research Program for Space Sciences"]
-[7.137909412384033, -0.6854869723320007, "[TT] Drift of RAAN of the Fast-sampling orbit = -9.44 minutes/day"]
-[11.170602798461914, 4.8069891929626465, "[TT] Depth Range of the Ma_MISS = Between 0 and 2\u2009m"]
-[4.065539360046387, 6.390224933624268, "[FF] Pointing Type of the Antennas = Body-pointed"]
-[10.380824089050293, 5.3154191970825195, "[FF] Electrical Connection of the SMA Heaters = In series"]
-[9.696538925170898, 0.061817605048418045, "[FF] Function of the G-switch sensors = Unable to sense sample return capsule deceleration during atmospheric entry and initiate parachute deployments"]
-[8.552186965942383, 6.093716144561768, "[FF] Relative Accuracy of the 607 nm Band = Not provided"]
-[9.696170806884766, -0.814910352230072, "[FF] Orbital Altitude of the SPOT-4 = Increased slightly"]
-[3.8595337867736816, 3.4024856090545654, "[FF] Contract Signing Date of the Galileo = 20 December 2018"]
-[2.9096152782440186, 4.45152473449707, "[TT] Spotlight Mode Swath of the PALSAR-2 = 25 km x 25 km"]
-[10.244976997375488, -1.291337251663208, "[TT] Inclination of the 7 microsatellites = 97.45\u00ba"]
-[10.372066497802734, 4.501791000366211, "[TT] Location of the Reaction Wheels = On a circular deck in a tetrahedral configuration"]
-[9.633220672607422, 8.388181686401367, "[TT] IFOV of the LWIR Camera = 143 \u00b5rad"]
-[11.994672775268555, 6.577589988708496, "[TT] Energy Range of the AMS = 0.5 to 350 GeV"]
-[6.950049877166748, 5.944977760314941, "[FF] Task of the ACC = Reduce the trigger rate during periods of very large flux activity"]
-[8.47020435333252, 4.1320600509643555, "[FF] Target of the External Calibration = Deep space, the moon, the sun, or known ground targets"]
-[8.259666442871094, 4.283342361450195, "[FF] Irradiance Range Requirement of the PH1, PH2 and PH3 = Derived from the ISUAL observations"]
-[6.123855113983154, 4.504937648773193, "[FF] Conference Presentation of the Sensor Web = 7th International Symposium Reducing the Costs of Spacecraft Ground Systems and Operations (RCSGSO 2007)"]
-[3.375666856765747, 5.0873847007751465, "[TT] Frequency of the Copernicus L-band SAR = L-band"]
-[5.532083034515381, 6.7372355461120605, "[TT] Data Volume of the SSJ/4 = Approximately 1 Mbyte per satellite"]
-[10.124396324157715, 5.712957859039307, "[TT] Detector Module Temperature Change Limit of the Neutron-1 = 0.5\u00b0C/min"]
-[6.733631134033203, 5.02814245223999, "[FF] Utilized Services of the CVX-2 = Power control, command, and telemetry provided through the HHC avionics equipment"]
-[6.975759506225586, 5.787154197692871, "[FF] Unknown of the Atomic Clock = Unknown"]
-[4.755298137664795, 0.2619308531284332, "[FF] In-Orbit Commissioning Completion Date of the RemoveDEBRIS = 23 August 2018"]
-[7.151470184326172, 6.8046746253967285, "[TT] High-Energy Laser Transmitter Range of the OLA = 1\u20137.5 km"]
-[10.223128318786621, 1.7466068267822266, "[FF] Handling of the North Polar Spur, the Monogem supernova remnant, the Cygnus superbubble = Must be handled differently"]
-[6.119184494018555, 0.8281281590461731, "[TT] Image Capture Date of the CaSSIS = 31 May 2018"]
-[10.026106834411621, 4.38369607925415, "[TT] Capability of the Torque Rods = 15 Am2"]
-[4.440721035003662, 7.139054298400879, "[TT] X-band Downlink Frequencies of the Landsat-6 = 8082.5, 8212.5, and 8342.5 MHz"]
-[9.381766319274902, 7.053448677062988, "[TT] Spatial Resolution of the TAC = 3.5 m"]
-[9.080923080444336, 4.607819080352783, "[FF] Attitude Hardware of the BRITE satellites = Reaction wheels and star trackers"]
-[5.12484073638916, 1.8079349994659424, "[FF] Utility Assess Date of the TacSat-4 = Trident Warrior 2012"]
-[11.809986114501953, 3.288120985031128, "[TT] Thruster Type of the LAM = 22 N bipropellant"]
-[5.861247539520264, 1.2348177433013916, "[TT] Date of the NASA\u2019s Exploration Enterprise Workshop = May 2010"]
-[6.9637956619262695, 1.8243024349212646, "[TT] Observation Date of the Orbiting Carbon Observatory-2 (OCO-2) = 8 February 2018"]
-[9.82471752166748, -1.0262746810913086, "[TT] Position Knowledge of the FormoSat-2 = < 70 m (0.02\u00ba)"]
-[11.703639030456543, 5.005128860473633, "[TT] Size of the SI-300 = 1.5 m in diameter and 1.95 m in height"]
-[7.522314071655273, 4.780939102172852, "[FF] Objective of the VBS = Measure the relative state of the target spacecraft"]
-[8.40252685546875, 6.523670196533203, "[TT] Type of the Line Scanning Sensors = Line scanning"]
-[8.9329195022583, 5.635420322418213, "[TT] Pointing Accuracy of the AOCS = 0.05\u00ba"]
-[8.20621395111084, 8.793581008911133, "[TT] Spectral Resolution of the SOSP = 1 nm in UV/VIS, 20 nm in IR"]
-[13.143593788146973, 7.0881476402282715, "[TT] Sunlit Average Power of the UKube-1 = < 1200 mW"]
-[5.598641872406006, 7.905755996704102, "[TT] Amplitude of the DCG = 10 bit"]
-[7.7608819007873535, 0.02057533897459507, "[TT] Landing Accuracy of the Philae Lander = Less than 100 m from the planned Agilkia site"]
-[11.839137077331543, 0.042452335357666016, "[TT] Number of Stars in Habitable Zone of the TESS = 1,822"]
-[5.414438724517822, 4.78078031539917, "[TT] Operation of the Monitoring and Control Segment = 24/7 monitoring"]
-[3.8035199642181396, 2.5037167072296143, "[TT] Launch Service Provider of the Iridium Next = ISC Kosmotras"]
-[4.738983631134033, 2.8576419353485107, "[TT] Ground Station of the ASTERIA = Morehead State University"]
-[11.70699691772461, 4.523492336273193, "[TT] Size of the Atlantic Basin Facility = Half the size of an Olympic swimming pool"]
-[11.778096199035645, 3.36429500579834, "[TT] Thrust of the T3\u00b5PS = Up to 6 mN"]
-[8.383103370666504, 7.3435516357421875, "[TT] Design of the Cameras = Monochromatic with optical filters"]
-[9.714120864868164, 8.405491828918457, "[TT] Cross-track FOV of the TIR Subsystem = \u00b111.5\u00ba"]
-[5.129636764526367, 1.768642544746399, "[TT] Status of the Teledesic = Cancelled"]
-[13.75449275970459, 5.362823009490967, "[TT] Type of the Solar Cells = UTJ (Ultra Triple Junction)"]
-[11.857124328613281, 5.427395343780518, "[FF] Size of the Instrument = 10 cm x 10 cm x 8.2 cm"]
-[8.80762767791748, 3.207338333129883, "[FF] Mission Objective of the TWINS = Investigate the distribution of the extended neutral hydrogen (H) exosphere and the relative contributions of hydrogen and oxygen to the terrestrial ring current (RC) and plasma sheet"]
-[6.567595481872559, 7.070516586303711, "[TT] Instrument Envelope of the SILEX Optical Terminal = 0.5 m x 0.5 m x 0.6 m"]
-[4.247072696685791, 2.424455165863037, "[TT] Launch Site of the Crew Dragon = Kennedy Space Center"]
-[4.935253620147705, 1.3598480224609375, "[TT] Operation Start Date of the OptiSAR\u2122 Constellation = 2022"]
-[9.334294319152832, 6.651884078979492, "[TT] Linear Resolution of the Satellite = 34 m x 24 m"]
-[11.647042274475098, 4.979031085968018, "[TT] Width of the New Depression = 70 m"]
-[9.764079093933105, 4.032498836517334, "[TT] Magnetic Field Strength of the AMS-02 = 4,000 times stronger than the Earth\u2019s own magnetic field"]
-[6.013773441314697, 5.097198963165283, "[FF] Function of the Control Center = Captured LPT housekeeping telemetry, displayed it, and forwarded UDP status packets to multiple systems with LabView graphical status displays"]
-[5.983392238616943, -0.49207907915115356, "[TT] Mission Duration of the GPM = Expected to last to the mid-2030\u2019s or beyond"]
-[7.7875142097473145, 7.858983039855957, "[TT] Sensitivity of the SCM = 3000 nT"]
-[13.187969207763672, 7.295528888702393, "[TT] Power Consumption of the MWIR = < 60 W"]
-[8.196144104003906, 7.041627407073975, "[TT] f/number of the Imaging Subsystem = 4"]
-[7.9784979820251465, 1.4564101696014404, "[FF] Core Objective of the SMOS = Improving our understanding of Earth\u2019s water cycle"]
-[3.7017476558685303, -0.8554843068122864, "[TT] Orbit Type of the EURECA = Low Earth Orbit (LEO) circular"]
-[13.7883939743042, 2.7012205123901367, "[TT] Weight of the Rocket = 881-pound (400 kg)"]
-[6.423271656036377, 4.324735641479492, "[FF] Application of the AutoConTM = Orbit maintenance of single spacecraft or constellations and formations"]
-[5.820130825042725, 6.0644145011901855, "[TT] Devices per Partition of the FMM (Flash Memory Module) = 16 for user data, 3 for parity information"]
-[18.665552139282227, 3.93525767326355, "[TT] NE\u0394T (K) of the ICI-9 = 1.5"]
-[5.0583319664001465, 7.335571765899658, "[TT] UHF Communication Data Rate of the CanX-2 = 256 kbit/s"]
-[7.973583221435547, 4.1953511238098145, "[FF] Function of the ICARE-NG = Study the influence of space radiation and their effects on electronic components"]
-[5.191766738891602, 0.3095633089542389, "[TT] Operation Start Date of the TRACE = March 2010"]
-[9.004105567932129, 8.56075382232666, "[TT] OPD for Shortest Wavelength of the Telescope = Stays below a quarter of a wave"]
-[7.125800609588623, 8.117321968078613, "[TT] Readout Channels of the STD = 196 k"]
-[5.296354293823242, 6.191684246063232, "[TT] Number of Users of the EAN = 16.5 million IAG passengers"]
-[11.838227272033691, 0.036978449672460556, "[FF] Discovery of the TESS = Revolutionize scientists\u2019 ability to study details like the ages, sizes and compositions of stars"]
-[11.28298282623291, 2.8089804649353027, "[TT] Mass of the NanoSatellite-1B = 23.9 kg"]
-[6.786631107330322, -0.6810487508773804, "[TT] Orbital Period of the TanSat = 90 minutes"]
-[8.335567474365234, 7.156914710998535, "[TT] Number of Cameras of the spaceCam c4000 = 2"]
-[4.691716194152832, 7.252597808837891, "[TT] Data Transmission Rate of the X-band = 25 Mbit/s"]
-[9.725790977478027, -0.5667256712913513, "[TT] Altitude of the Orbit = 467 km x 883 km"]
-[8.702963829040527, 2.3962135314941406, "[FF] Mission Goal of the EMIT = Map where the dust originates and estimate its composition"]
-[5.224932670593262, 1.055181622505188, "[TT] Launch Date of the ABEX = 2024"]
-[13.421063423156738, 6.430952548980713, "[TT] Power Generation of the HORYU-2 = 300 V"]
-[5.505639553070068, -0.05366970971226692, "[FF] Presentation Date of the RapidEye = Oct. 4-8, 2004"]
-[10.022314071655273, -1.3847811222076416, "[TT] Orbital Inclination of the IceCube = 51.6\u00b0"]
-[6.9232330322265625, 0.8150820136070251, "[TT] Next Dust Clearing Date of the InSight Mars lander = June 5, 2021"]
-[8.42167854309082, 5.490246295928955, "[TT] Geo-location Accuracy of the SEOSat = 20 m"]
-[7.899898529052734, 8.091485023498535, "[TT] Signal-to-Noise Ratio of the NISP Photometer = Magnitude 24.0"]
-[6.038911819458008, 5.8022308349609375, "[TT] Quantity of the Virtex-7 FPGAs = 2"]
-[7.0598835945129395, 3.047093152999878, "[FF] Service Spectrum of the NPOESS = NPOESS ground segment will acquire and store global and regional environmental imagery, specialized meteorological, climatic, terrestrial, oceanographic, solar-geophysical, and other data"]
-[7.612605094909668, 0.808660626411438, "[FF] Mission of the LunaH-Map = Help scientists understand the quantity of hydrogen-bearing materials in cold traps in permanently shaded lunar craters"]
-[10.864811897277832, 5.923004627227783, "[TT] Measurement Range - Plasma Density of the ISL Instrument = 100 to 5 x 10^6 particles/cm3"]
-[4.58826208114624, 7.887030124664307, "[TT] Downlink Frequency of the Payload Imagery = 8246.56 MHz"]
-[7.828360080718994, 5.164132118225098, "[FF] Purpose of the Machine Vision Tasks = In-space assessment of fiducials (decals) with unique patterns that enhance machine vision algorithms and aid in autonomous rendezvous and tool positioning"]
-[3.3854613304138184, 6.446238040924072, "[TT] Antenna Diameter of the DORIS = 160 mm"]
-[9.781654357910156, -0.6073839664459229, "[TT] Orbit Altitude of the Hinode = 680 km"]
-[10.210407257080078, 6.535758018493652, "[TT] Spacing of the LED-bearing target = 30 m intervals"]
-[9.953486442565918, 4.387575149536133, "[FF] Function of the Torque Rods = Apply constant open-loop dipole to counteract the body-fixed residual dipole disturbance torque"]
-[6.927274227142334, 1.7176392078399658, "[FF] URL of the James Webb Space Telescope = http://www.sciencecodex.com/james_webb_space_telescope_begins_to_take_shape_at_goddard"]
-[4.153528213500977, 2.2182199954986572, "[TT] Launcher Compatibility of the INTEGRAL = Ariane 5 and Proton"]
-[4.847976207733154, 0.3606337606906891, "[TT] Launch Date of the DeMi = 15 February 2020"]
-[5.844846725463867, 4.483203887939453, "[TT] Validation Data Source of the CYGNSS = IWARP"]
-[9.827361106872559, -0.8209267258644104, "[TT] Orbit Altitude of the COSPAS-1 = 989 x1082 km"]
-[10.140525817871094, 6.531957626342773, "[TT] Ground Spacing of the MABEL = ~85 m"]
-[5.46968936920166, 6.099015712738037, "[TT] Internal RAM of the OBC = 4 kB"]
-[4.166843891143799, 2.572561740875244, "[TT] Launch Site of the Aeolus = Kourou, French Guiana"]
-[3.9237940311431885, 9.735414505004883, "[TT] Bandwidth (GHz) of the ICI-9 = 4"]
-[7.653965473175049, 6.5021867752075195, "[TT] India Scan Time of the INSAT-3D = ~40 minutes"]
-[5.549410343170166, 5.5114521980285645, "[TT] Microprocessor of the IBIS5-B-1300 = PXA 270"]
-[3.5867161750793457, 4.842475414276123, "[TT] Type of the MSU-MR = Imaging microwave radars"]
-[9.856038093566895, 8.204447746276855, "[TT] Focal Length of the Instrument = 65 mm"]
-[9.817351341247559, -0.5311251282691956, "[TT] Second Deployment Batch Altitude of the STP-2 = 720 km"]
-[9.698368072509766, 8.43441390991211, "[TT] Value of the FOV = 1.38\u00ba"]
-[7.118447303771973, 1.3540903329849243, "[FF] Data Archive Location of the Spitzer Space Telescope = Infrared Science Archive at IPAC at Caltech in Pasadena, California"]
-[7.335519790649414, 3.700277090072632, "[FF] Microwave Scatterometer of the HY-2A Satellite = Unknown"]
-[8.867915153503418, -0.2668326795101166, "[TT] Apogee of the Chang'e-1 = 51000 km"]
-[7.157366752624512, 3.598553419113159, "[TT] Mission Type of the NightPod = EO"]
-[8.730646133422852, 8.452656745910645, "[FF] Swath of the Imaging Spectrometer = Large"]
-[16.486534118652344, 3.570096492767334, "[FF] Greg Wyler Testimony Date of the OneWeb = October 25, 2017"]
-[7.85072135925293, 8.029923439025879, "[TT] Bandwidth of the Band Photometers = 5.0 nm"]
-[6.300290584564209, 0.6943732500076294, "[FF] Publication Date of the CONGO = Sept. 1, 2009"]
-[10.042840003967285, -1.4793992042541504, "[TT] Orbit Inclination of the ALMASat-1 = 69.5\u00ba"]
-[11.225502967834473, 6.345633506774902, "[TT] Density of the Proton Component Measurement Accuracy of the DSCOVR = 20%"]
-[4.153439521789551, 0.16037817299365997, "[TT] Launch Date of the FalconSat-3 = 9 March 2007"]
-[13.812137603759766, 2.6723334789276123, "[TT] Launch Mass of the Spacecraft = ~310 kg"]
-[7.957018852233887, 7.214928150177002, "[TT] Event Rate of the Imager = 1 x 10  -5  s -1"]
-[8.24935245513916, 7.691514015197754, "[TT] Dynamic Range of the CCD Camera = 0-100% albedo"]
-[10.21802806854248, 3.202096700668335, "[FF] Data Collection of the MicroMAS-2 CubeSat = Autonomously collecting radiometry data"]
-[7.675878047943115, 3.972470998764038, "[FF] Objective of the CEASE = To demonstrate on-orbit autonomous monitoring of the S/C environment and to provide \u201calerts\u201d when satellite charging, SEUs or other radiation events are likely"]
-[11.081254959106445, 1.340644359588623, "[FF] Gravitational Wave Sources of the LISA = Ultra-compact binaries, supermassive black hole mergers, extreme mass ratio inspirals"]
-[8.458468437194824, 7.696868419647217, "[TT] CCD Array Size of the Instrument = 128 x 128 pixels"]
-[9.376808166503906, 5.018681049346924, "[TT] Attitude of the ISS = Torque Equilibrium Attitude (TEA)"]
-[5.679087162017822, 1.9729830026626587, "[FF] URL of the CICERO = http://www.prweb.com/releases/2009/12/prweb3295414.htm"]
-[14.1635160446167, 3.194399356842041, "[TT] Mass of the TDS-1 = 150 kg"]
-[13.374815940856934, 7.681306838989258, "[TT] Transmitting Power of the Iris Radio = 2 W"]
-[9.820645332336426, 4.219852924346924, "[FF] Dipole Moment of the AMS-02 = Negligible"]
-[6.785322666168213, 0.914651095867157, "[TT] First Measurements Date of the Solar Orbiter = February 17, 2020"]
-[8.284173965454102, 1.4788132905960083, "[TT] Range of values of the Land surface temperature = 180-340 K"]
-[7.430770397186279, 3.9705190658569336, "[FF] Producing Instruments of the AVTP and AVMP retrievals = Cross-track Infrared Sounder and the Advanced Technology Microwave Sounder suite (CrIMSS)"]
-[9.667174339294434, 7.073446273803711, "[TT] Observation Area of the T1 = 160 km x 160 km"]
-[9.261831283569336, 5.060475826263428, "[TT] Attitude Rate Control Accuracy of the Spacecraft = 0.001\u00ba/s"]
-[9.86548900604248, 1.6751492023468018, "[FF] Expansion of the Universe = Speeding up"]
-[9.307052612304688, 5.600250720977783, "[TT] Pointing Repeatability of the ASTERIA = 1 arcsecond RMS"]
-[3.4138381481170654, 4.862364768981934, "[FF] SAR Interferometry Capability of the ROSE-L = Yes"]
-[4.899613380432129, 3.496603488922119, "[TT] Manufacturer of the Ka-band equipment = MDA Corp. of Canada"]
-[11.747393608093262, 3.5606424808502197, "[TT] Diameter of the T6 thrusters = 22 cm"]
-[11.683337211608887, 4.571033000946045, "[TT] Height of the Resurs-DK1 = 7.4 m"]
-[6.364792346954346, 1.4867562055587769, "[TT] Expected Data Processing End Date of the MICROSCOPE = 2019"]
-[7.043844223022461, 3.791614294052124, "[FF] Formation Flying Applied of the ASPIICS = Unknown"]
-[10.44513988494873, 2.251469612121582, "[FF] Angular Resolution Metric of the X-ray telescopes = HPD (Half-Power Diameter), HEW (Half-Energy Width)"]
-[7.0546956062316895, 1.4491543769836426, "[FF] Mission Operations Location of the Spitzer Space Telescope = NASA\u2019s Jet Propulsion Laboratory, a division of Caltech"]
-[7.225506782531738, 1.7383036613464355, "[FF] Function of the Lab-on-a-chip device = Supports and measures the fern spore ion channel activity"]
-[4.988598346710205, 3.415013551712036, "[TT] Manufacturer of the MWI Instrument = CGS (Carlo Gavazzi Space) S.p.A"]
-[5.498709678649902, 6.4113640785217285, "[TT] Capacity of the HSDR = 16 GByte"]
-[5.610201358795166, 5.91295051574707, "[TT] Bit of the BILGE processor = 32-bit"]
-[8.080979347229004, 2.6559174060821533, "[TT] Measurement Domain of the KySat-2 = Ocean, Land, Snow & Ice"]
-[6.3466410636901855, 2.4489898681640625, "[FF] Ability to Support HDLC Framing of the UoSAT-12 = True"]
-[16.54764747619629, 3.6433496475219727, "[TT] Number of Satellites of the OneWeb = 34"]
-[5.330132961273193, 1.1177036762237549, "[FF] Date of the 69th IAC = 1-5 October 2018"]
-[11.778254508972168, 0.10645338892936707, "[FF] Transit Recognition of the TESS = Usually, it takes at least two observed transits to recognize a planet's presence"]
-[9.534565925598145, 1.4852124452590942, "[FF] Tasking Priority of the SPOT or Pleiades constellations = Highest"]
-[10.669283866882324, 5.472114562988281, "[TT] Radiation Protection of the Orion = None beyond Earth's atmosphere and magnetic field"]
-[9.397330284118652, 3.2127134799957275, "[TT] Cleanroom Class of the Solar Wind Collectors = Class 10"]
-[8.240885734558105, 1.4146335124969482, "[FF] Characteristic of the La Ni\u00f1a = Cooler than normal sea-surface temperatures in the central and eastern tropical Pacific Ocean"]
-[8.093463897705078, 0.6677855849266052, "[FF] Measurement Unit of the GRACE-FO = Groundwater Rebound Time"]
-[6.287922382354736, 4.0713419914245605, "[FF] Architecture of the ASNARO = New system Architecture for Observation"]
-[11.390917778015137, 3.9441781044006348, "[TT] Size of the QuakeSat = 10 cm x 10 cm x 30 cm"]
-[6.946661472320557, 0.9743787050247192, "[FF] Orbital Drift of the SPOT-4 = Tolerated"]
-[8.428228378295898, 4.5587849617004395, "[TT] Frame-Dragging Accuracy of the LARES-2 = Approximately 2 x 10-3"]
-[8.227032661437988, 3.855034828186035, "[TT] Entrance Slits Alignment of the OCO Instrument = Co-aligned"]
-[8.537897109985352, 8.156757354736328, "[TT] Spectral Resolution of the HIRES = Very high"]
-[13.3743896484375, 2.9135701656341553, "[TT] Mass of the PicSat = 3.5 kg"]
-[10.068612098693848, 8.1961030960083, "[TT] Aperture of the Optics System = 50 cm"]
-[13.76546573638916, 2.8727400302886963, "[TT] Spacecraft Mass of the ASNARO-2 = 570 kg"]
-[5.812170028686523, 1.5781773328781128, "[FF] Conference Presentation Date of the Eu:CROPIS = May 16-20, 2016"]
-[8.1275053024292, 4.323812484741211, "[FF] Objective of the DDM = To record the space radiation environment absorbed dose behind various thin shields and to estimate the dose due to low energy electrons"]
-[3.6733124256134033, 3.8497636318206787, "[TT] Launch Timeframe of the RISAT-1A = 2018-19"]
-[1.765942096710205, -2.0570871829986572, "[FF] Design Concept of the Hayabusa-2 SRC = Not to change the design from the former SRC except for the following items"]
-[8.158576965332031, 7.709982395172119, "[TT] Maximum Quantum Efficiency of the Kruiz CCD = 0.33"]
-[7.1575469970703125, 2.540914297103882, "[FF] Publisher of the Observation of the Earth and Its Environment: Survey of Missions and Sensors = Springer Verlag"]
-[13.645575523376465, 5.441263675689697, "[TT] Solar Panels of the SporeSat = Fixed body mounted triple junction"]
-[7.472037315368652, 2.9827563762664795, "[TT] Emissions Measurement of the GHGSat-D = Carbon dioxide and methane"]
-[7.659079551696777, 8.0791597366333, "[FF] Diffraction Pattern of the CCRs = Airy pattern"]
-[4.645260810852051, 0.15451256930828094, "[TT] Observation Start Time of the INTEGRAL = 15:30:59 on 24 January"]
-[9.826269149780273, 8.02403736114502, "[TT] Replaced by of the TMA = Lens objective (doublet)"]
-[8.261735916137695, 4.779369354248047, "[FF] IMU and Star Trackers Mounting of the Sentinel-2 = On the thermally controlled sensor plate on the MSI"]
-[10.465019226074219, 5.700942039489746, "[TT] Operating Temperature of the Ion Thruster = -80\u00baC to +270\u00baC"]
-[12.011180877685547, 6.880356311798096, "[TT] Normalization at 1 keV of the First Broken Powerlaw = 5.7 photon cm-2 s-1 keV-1 ster-1"]
-[14.113561630249023, 7.070639610290527, "[TT] Voltage levels of the EPS = 3.3 V, 5 V, battery output (nominal 3.7 V)"]
-[5.219203948974609, 1.014760136604309, "[TT] Data Flow Start Date of the SMAP = November 19"]
-[10.281167030334473, 7.25781774520874, "[TT] Field of Regard of the NIRST = 1064 km"]
-[10.153241157531738, 0.015382450073957443, "[TT] Diameter of the Block 5 Satellite = 76 cm"]
-[14.380383491516113, 3.140427589416504, "[TT] Mass of the ITUpSat-1 = \u2264 1 kg"]
-[8.11094856262207, -0.6286789774894714, "[FF] Contribution of the GOCE = New view of the remnants of lost continents hidden deep under the ice sheet of Antarctica"]
-[11.313155174255371, 4.387845516204834, "[TT] Size of the CubeBug-2 = 2U"]
-[5.550680160522461, 7.085111618041992, "[TT] Maximum Data Rate of the LPT Demodulator = 1 Mbit/s"]
-[7.001785755157471, 3.2885231971740723, "[FF] Data Standard of the LUTI = PDS4 standard established by NASA"]
-[12.66695785522461, 1.9057955741882324, "[FF] Data Collection of the SAGE III = Several high stratospheric aerosol events"]
-[6.167393207550049, 2.3769302368164062, "[FF] Primary Objective of the EFT-1 = Testing of the spacecraft launch, orbital, reentry, and recovery systems"]
-[10.555292129516602, 3.3554165363311768, "[TT] CubeSat of the Satellite = 3U"]
-[6.009900093078613, -0.4781222641468048, "[TT] Mission Duration of the PSAT = 18 months"]
-[9.691189765930176, 2.7215774059295654, "[TT] Airlock Compatibility of the ArgUS = JEM-A/L (Airlock), NRAL (NanoRacks Airlock)"]
-[6.291754722595215, 5.393519878387451, "[FF] Contents of the FEEU = FPGA"]
-[12.139697074890137, 1.970770001411438, "[TT] Launch Date of the CartoSat-2D = February 15, 2017"]
-[8.600903511047363, 6.964865684509277, "[TT] Image of the Wide Ultra-Fine Mode = Single-pol (HH, VV, HV or VH)"]
-[11.705150604248047, 6.496297359466553, "[TT] Detects of the JEDI = Energetic electrons"]
-[6.497708320617676, 3.6000943183898926, "[FF] Reliance of the 3D Printing Capability = On delivery of filament feedstock from cargo resupply missions"]
-[5.05366849899292, 0.6069871187210083, "[TT] Testing Start Date of the OCK (Orbit Control Kit) = Summer of 2007"]
-[8.23261833190918, 4.5220794677734375, "[FF] Goal of the STARE mission = Demonstrate usefulness of space based sensing for refining orbital parameters of an orbiting object"]
-[9.725504875183105, -0.5555484890937805, "[TT] Orbit Altitude of the ERBS = 610 km"]
-[10.316939353942871, 2.1772592067718506, "[FF] Spectral Band of the AstroSat = Hard X-ray to visible bands"]
-[7.737482070922852, 5.351792812347412, "[FF] Instrument Elements of the SHIMMER FTS = Telescope, relay optics, interferometer, CCD camera"]
-[11.470351219177246, 3.3949778079986572, "[TT] Maneuverable of the T6 thrusters = True"]
-[8.1437406539917, 3.1785247325897217, "[FF] Usage of the Ti = Record likely lightning discharge at the same moment as the RFA in the ultraviolet, infrared, gamma radiation and ELF frequency ranges"]
-[7.747970104217529, 5.707729339599609, "[FF] Quantity of the Multiple direction/polarisation radiometers = +49"]
-[8.258307456970215, 6.942558765411377, "[TT] Data Capacity of the Imaging Payload = 6 TB"]
-[8.459816932678223, 6.344964504241943, "[TT] Shortwave Range of the CERES = 0.3 - 5.0 \u00b5m"]
-[6.615371227264404, 4.730179786682129, "[FF] Deliverable of the Product Level 1C (L1C) = Level 1b data orthorectified, re-sampled to a specified grid"]
-[4.6881537437438965, 7.210892677307129, "[TT] Transmission Rates of the XBT = 12.5, 25, or 50 Mbit/s"]
-[9.200740814208984, -0.7182668447494507, "[TT] Orbit of the CELESTA (ROBUSTA 1D) = LEO (~ 500 km)"]
-[6.913003444671631, 7.469170570373535, "[TT] Resolution of the ADCs = 8 bit"]
-[11.969356536865234, 4.941150188446045, "[TT] Volume of the OSDP = 0.024 m3"]
-[5.528757095336914, 0.5689604878425598, "[TT] Mission Approval Year of the Aditya-L1 = 2015"]
-[7.035153865814209, 8.32563591003418, "[TT] Band 1 SNR of the COCTS = 9.103"]
-[4.234251976013184, 5.877767086029053, "[TT] Latency of the ADS-B Receiver = Fewer than 5 minutes"]
-[7.835174560546875, 5.928133964538574, "[TT] Measurement Rate of the FFRF Sensor = 1 Hz"]
-[10.680434226989746, 0.9237332940101624, "[TT] Size of the Kepler-1658 = Three times larger than the Sun"]
-[4.498334884643555, 7.666177272796631, "[TT] Number of Stations of the SVOM VHF Network = 45"]
-[4.999112606048584, 3.306216239929199, "[TT] Provider of the Picosatellite propulsion system = Aerospace Innovation GmbH"]
-[7.297287464141846, 5.265106678009033, "[FF] Components of the RSI = Camera, IPU (Instrument Processing Unit), optical subassembly, secondary structure, FPA (Focal Plane Assembly), Korsch telescope, video electronics, sequencer, DC/DC converter, compression cards"]
-[6.775527477264404, 5.526596546173096, "[FF] Function of the Readout Architecture = Measure deposited energy and arrival time for each event, enable depth of interaction measurement"]
-[3.0250768661499023, 1.9968376159667969, "[FF] Announcement Date of the Copernicus Sentinel-5P = May 04, 2020"]
-[5.549419403076172, 5.299588203430176, "[TT] Operating System of the SpaceCube 2 = RTOS based on TRON"]
-[4.944876194000244, 3.2944021224975586, "[TT] Manufacturer of the ACC = ONERA, France"]
-[8.178631782531738, 0.114081010222435, "[TT] Launch Date of the Meteor M2-3 = June 27, 2023"]
-[14.354881286621094, 2.99234676361084, "[TT] Mass of the Hodoyoshi-3 = 60 kg"]
-[11.89540958404541, 3.2650136947631836, "[TT] Type of the Propulsion System = Chemical bi-propellant"]
-[5.670141696929932, -0.9471642971038818, "[TT] Design Life of the SES-17 = 15 years"]
-[6.755545616149902, 5.696481227874756, "[TT] Satellite Quantity of the CM1 = 2"]
-[5.9574971199035645, 1.825921893119812, "[FF] Testing Date of the Orion Spacecraft = April 11, 2014"]
-[3.2233963012695312, 5.773237228393555, "[TT] Panel Size of the SAR antenna subsystem = 2 m x 2 m"]
-[5.946201801300049, 1.6464214324951172, "[FF] Conference Presentation of the MEIDEX = AGU Fall Meeting 2003, San Francisco, CA, Dec. 8-12, 2003"]
-[9.492777824401855, 7.278815269470215, "[TT] Resolution of the BlackSky Pathfinder-1 = 1 m"]
-[13.100567817687988, 2.217116355895996, "[TT] Mass of the SAGE-III = 76 kg"]
-[5.0446648597717285, 0.9923913478851318, "[FF] Congress Date of the ADM-Aeolus = Oct. 2-6, 2006"]
-[4.66581392288208, 1.7078124284744263, "[TT] Platform Series of the GovSat-1 = Advanced GEOStar-3"]
-[8.747200012207031, 4.753691673278809, "[TT] Control of the Piezoelectric Stage = Small, rapid adjustments to the detector position to keep the target star stationary"]
-[9.815669059753418, 5.659818649291992, "[TT] Tilt of the M3 = 50 \u00b5rad"]
-[6.5263848304748535, 1.8409122228622437, "[FF] URL of the OSCAR-QUBE = https://www.esa.int/Education/Orbit_Your_Thesis/"]
-[6.6343464851379395, 5.129376411437988, "[FF] Function of the ICU = FCI and IRS management and data-processing"]
-[11.357285499572754, 0.6800619959831238, "[TT] Planet of the AU Microscopii = Yes"]
-[10.421424865722656, 5.7939066886901855, "[TT] Operating Temperature of the FEU = Approximately 70\u00baC"]
-[4.708508014678955, -1.8075352907180786, "[FF] URL of the Chang'e-1 = http://www.esa.int/esaSC/SEMPM53Z28F_index_0.html"]
-[5.428732872009277, 2.5272958278656006, "[TT] Mission Type of the CM1 = Technology Demonstration"]
-[12.405290603637695, 3.198585271835327, "[TT] Propellant of the S/C = 81 kg, N 2 H 4"]
-[4.922826290130615, 0.28833457827568054, "[TT] Launch Date of the SPOT-2 = Jan. 22, 1990"]
-[8.548359870910645, 2.306065082550049, "[FF] Purpose of the Aeolus = Measure Earth's wind on a global scale"]
-[9.017182350158691, 8.531402587890625, "[TT] Bandpass of the Telescope = 540\u2013590 nm"]
-[11.245462417602539, 5.441596984863281, "[TT] Quantity of the Microcalorimeter = 14"]
-[3.810647487640381, 2.4607646465301514, "[TT] Number of Failed Orbital Launch Attempts of the Astra = Three"]
-[10.140320777893066, 5.996737003326416, "[TT] Detector Array Temperature of the LWIR Camera = 65 K"]
-[5.680327892303467, 0.716681182384491, "[FF] Bulletin Date of the GEOS-1 = Feb. 2004"]
-[6.870731830596924, -0.21095822751522064, "[TT] Observation Time of the Band-1 and Band-64 = 37.68 seconds"]
-[4.832861423492432, 0.537738561630249, "[TT] Start Year of the SOHLA = 2002"]
-[7.350559234619141, 4.612943172454834, "[FF] Location of the Dosimeter = Fit in the other half of the chassis"]
-[8.8838472366333, 9.574947357177734, "[FF] Band 2 Wave Numbers of the TANSO-FTS-2 = 5900 - 6400"]
-[9.249361038208008, 5.045815467834473, "[TT] Control Accuracy of the Mango = Within 0.3 m from the commanded approach"]
-[3.077214479446411, 2.3122284412384033, "[TT] Spatial Resolution of the Sentinel-2 = < 1 ha MMU"]
-[6.509803771972656, 3.4810519218444824, "[FF] Provider of the AMS Payload Integration Hardware (PIH) = NASA/JSC (Johnson Space Center), Houston, TX, with the support of Lockheed Martin Space Operations (LMSO)"]
-[11.429616928100586, 4.420483589172363, "[TT] Dimensions of the Kubik = 40 cm cube"]
-[10.292191505432129, 7.834461212158203, "[TT] Uplink Telescope Size of the GS-2 = 15 cm"]
-[3.2256662845611572, 5.022482872009277, "[TT] SAR Measurements Spatial Resolution of the L2SMA = About 3 km"]
-[8.613165855407715, 1.9965335130691528, "[TT] Resolution of the Wind Vector Resolution = 25 km"]
-[8.243067741394043, 1.9798057079315186, "[TT] Percentage of World's Tropical Cyclones of the North Indian Ocean = About 7 percent"]
-[11.25137710571289, 0.9435603618621826, "[TT] Mission Duration of the LISA = 8 March to 5 May 2017"]
-[9.224392890930176, 7.156435012817383, "[TT] Image Resolution Comparison of the Solar Orbiter = Ten times better than what a 4k TV screen can display"]
-[10.548809051513672, 1.8551629781723022, "[FF] Spin Rate of the Supermassive Black Hole = Can be determined conclusively"]
-[6.547555446624756, 0.6336839199066162, "[TT] Operation Period of the Herschel = 2009 until 2013"]
-[11.434319496154785, 5.711203098297119, "[TT] Density of the Copper, Cobalt, Nickel Alloys = 9,870 kg/m3, 9,900 kg/m3, 9,860 kg/m3"]
-[6.392416477203369, 5.37837028503418, "[FF] Components of the PCU = Antifuse FPGA"]
-[9.191396713256836, 7.204671859741211, "[TT] Vertical Resolution of the IMG = About 2-6 km"]
-[10.877538681030273, -0.32413047552108765, "[TT] Change DEM Availability of the TanDEM-X = Mid-2021"]
-[12.038146018981934, 3.280238628387451, "[TT] Volume of the iodine BIT-3 flight system = 1.6U"]
-[13.776898384094238, 7.039273262023926, "[TT] Redundancy of the Buck-Boost Converter = 2 of 3 Red."]
-[11.241083145141602, 5.3282599449157715, "[TT] NaI Scintillators of the XGRE = 900 cm2 detector area"]
-[3.871522903442383, 7.86201810836792, "[TT] Modulation of the RF Communications = FSK"]
-[11.86597728729248, 0.020996922627091408, "[TT] Monitoring Target of the NASA TESS telescope = Planetary Systems"]
-[6.9006733894348145, 7.761538505554199, "[TT] Reflector Size of the IMI = 9 m x 6 m"]
-[5.5089263916015625, 3.8747060298919678, "[TT] Satellite Cluster Quantity of the Kleos S.A. = 4"]
-[9.627811431884766, 0.8745651841163635, "[FF] Observation Distance of the Herschel = Within 1500 light years from the Sun"]
-[4.937089920043945, 0.8444867730140686, "[TT] Engineering Model Flight Date of the OCSD = 2015"]
-[7.19719123840332, 3.8454208374023438, "[FF] Function of the TriG = Provides Precise Orbit Determination (POD), Global Navigation Satellite System (GNSS) Radio Occultation, neutral atmosphere, ionosphere and scintillation and GNSS reflections"]
-[9.080144882202148, 1.363662600517273, "[TT] Launch Year of the Voyager 1 = 1977"]
-[5.051968097686768, 5.941262722015381, "[TT] Data Handling of the Stensat = Keeps the most recent science packet as part of a beacon packet"]
-[6.462932586669922, 6.277310848236084, "[FF] Types of the RFI Sources = In-band emissions, Excessive out-of-band emissions, Spurious emissions"]
-[9.880975723266602, 6.466314792633057, "[TT] Mass of the Earth Radiation Budget Experiment (ERBE) = 57 kg/scanner"]
-[6.932898998260498, -0.5630112290382385, "[TT] Repeat Cycle of the RADARSAT-2 = 24 days (343 orbits)"]
-[5.05649471282959, 7.157660007476807, "[TT] Uplink Data Rate of the TT&C Communications = 2 kbit/s"]
-[11.796825408935547, 3.261796474456787, "[TT] Maximum Thrust of the Mono-propulsion Chemical System = 1 Newton"]
-[10.260425567626953, 5.918872833251953, "[TT] Temperature Resolution at 300 K of the VNIR, MWIR1, MWIR2, TIR1, TIR2 = \u2264 0.18 K"]
-[6.484902858734131, 1.977319598197937, "[FF] URL of the Earth Observation Constellation Satellites = http://www.nspo.narl.org.tw/ICGPSRO2013/"]
-[8.21086597442627, 7.846555709838867, "[TT] Number of Infrared Detectors of the CrIS = 27"]
-[7.249387741088867, 6.683553695678711, "[TT] Position Accuracy of the Laser Alignment System = Better than 4 \u00b5m"]
-[7.267105579376221, -0.7041969895362854, "[TT] Repeat Cycle of the ICESat-2 = 91 days"]
-[4.871804714202881, 1.9750112295150757, "[FF] Built by of the Gokturk-2 = TUBITAK-UZAY and TAI (Turkish Aerospace Industries Inc.) consortium"]
-[11.93295669555664, -0.08583009988069534, "[TT] Angular Momentum Build-up of the TESS = ~1.5 N m"]
-[3.670267105102539, 4.749800682067871, "[FF] Purpose of the Tool = Make useful relative comparisons between the existing RADARSAT-2 beam modes and these new beam modes"]
-[10.821219444274902, -0.2579309940338135, "[TT] Cumulative Absolute Height Error of the TanDEM-X = 0.9 m"]
-[9.033679008483887, 5.64922571182251, "[TT] Pointing Accuracy of the ACS = 0.14\u00ba (8.4 arcmin)"]
-[7.052031517028809, 5.132242679595947, "[FF] Design of the BBR Instrument = Physically separated into two units: OU (Optics Unit) and the ICU (Instrument Control Unit)"]
-[6.234505653381348, 3.3275721073150635, "[FF] Utilization Plan of the KIBO = Unknown"]
-[6.928534030914307, 2.456695318222046, "[FF] Components of the ROE = UKTAC, Institute of Astronomy, ROE Visitor Center"]
-[9.742164611816406, 8.424702644348145, "[TT] FOV of the WTS1 and WTS2 = 30\u00ba x 2\u00ba"]
-[9.824018478393555, 4.34619665145874, "[FF] ADCS System of the DeorbitSail = Orientation Suitable for Sail Deployment"]
-[8.355012893676758, 0.2160293012857437, "[TT] Number of Propulsive Maneuvers of the ICE (International Cometary Explorer) = 15"]
-[4.7040252685546875, 7.5941972732543945, "[FF] Modulation of the Ranging Tones = Onto the downlink"]
-[5.93508243560791, 3.51316499710083, "[FF] Cost of the Block 5D satellites = Increased"]
-[13.716890335083008, 6.959372043609619, "[TT] Bus Total Power of the EPS = ~286 W"]
-[6.9500322341918945, -0.7184579968452454, "[FF] Orbital Period of the Planet Candidate = Roughly every 70 years"]
-[8.86362361907959, 1.4790765047073364, "[FF] Gravity Conditions of the MSL SCA-GEDS-German = Earth-gravity (1g) and microgravity (\u00b5g)"]
-[10.183969497680664, 9.390783309936523, "[TT] Nominal IGFOV of the Band 14 = 2 km"]
-[8.558277130126953, 5.022907257080078, "[FF] Tracking and Pointing Performance of the Telescope System = Enough for LEO satellite support"]
-[5.397839069366455, 2.393503427505493, "[TT] Mission Type of the NuSTAR = Small Explorer"]
-[9.577818870544434, 8.141810417175293, "[TT] Lens System of the Spectrometer = Spherical lenses"]
-[7.3727827072143555, 5.482315540313721, "[FF] Function of the LRI = Measures the same range fluctuations as KBR but with reduced noise and provides accurate measurements of the relative pointing of the two satellites"]
-[8.237021446228027, 2.1786277294158936, "[FF] Ephemeris Accuracy Improvement of the SeaSat = Expected"]
-[9.875883102416992, 4.337447643280029, "[TT] Configuration of the AMS-02 = Permanent Magnet (PM)"]
-[6.42381477355957, -0.841874897480011, "[TT] LTAN of the TanSat = 13:30 hours"]
-[3.431406021118164, -0.9160764813423157, "[FF] Synopticity and a mix of sun-synchronous and mid-inclination orbits of the Satellite = Requirement"]
-[7.087928295135498, 4.232872009277344, "[FF] Purpose of the Payload = Capturing satellite streaks"]
-[8.398740768432617, 6.2542877197265625, "[TT] Cross Section Per Unit Area of the CCR = Smallest change in range correction versus velocity aberration occurs at 1.0 inches"]
-[6.726925849914551, 6.397507190704346, "[TT] Wait Time of the LT = 120 seconds"]
-[6.312299728393555, 3.570650577545166, "[TT] Number of Deployable Subsatellites of the EAGLE = 1"]
-[13.40967845916748, 2.900336503982544, "[TT] Mass of the LatinSat-1/2 = 12 kg"]
-[11.539764404296875, 3.326401948928833, "[FF] Cause of Failure of the AVUM Thrust Vector Control (TVC) system = Wrong routing and connection of the control lanes"]
-[5.170082092285156, -0.02535044588148594, "[TT] Launch Date of the Cygnus NG-10 = 17 November 2018"]
-[6.73475456237793, 5.919636249542236, "[TT] Operational Mode of the ASTERIA = Safe Mode"]
-[7.407337188720703, 0.9582061767578125, "[FF] Spacedaily Article Date of the GRAIL = Dec. 12, 2007"]
-[11.794673919677734, 6.743931770324707, "[TT] Energy Range of the HOPE = From less than or equal to 20 eV or spacecraft potential (whichever is greater) to greater than or equal to 45 keV"]
-[9.680691719055176, 6.967231750488281, "[TT] Spatial Resolution of the DPS = 2-5 km"]
-[6.077436923980713, 3.387348175048828, "[FF] Operation Phase of the DSX = Launch and Early Operations"]
-[10.25704288482666, 3.120713472366333, "[TT] Number of Missions of the ELaNa-4 CubeSats = 8"]
-[11.674439430236816, 4.596151351928711, "[TT] Diameter of the [65803] Didymos = ~160 m"]
-[8.11866283416748, 8.552070617675781, "[TT] Spectral Range of the NTSIC = VNIR (Visible Near Infrared)"]
-[8.497391700744629, 7.609238147735596, "[TT] NEP of the Detector = < 3.7 nW at 17 Hz"]
-[6.731163024902344, 8.038228034973145, "[TT] NEDT (K) of the SSM/T-2 = 0.6, 0.4, 0.4, 0.4, 0.5, 0.4, 0.4"]
-[5.412256717681885, 3.954437732696533, "[TT] Number on Order for the Air Force of the Block 5D-2 satellite = 13"]
-[11.824797630310059, 4.798955917358398, "[TT] Size of the HIRES = 17 cm x 18 cm x 36.5 cm"]
-[9.334863662719727, 6.702336311340332, "[TT] Resolution of the FRS-1 = 3 m (Azimuth) x 2 m (Range)"]
-[5.892944812774658, 2.739859104156494, "[FF] Rumors about Funding of the Worldview Legion = I\u2019ve heard rumours that you don\u2019t have enough money for Worldview Legion"]
-[5.25280237197876, 1.1994394063949585, "[FF] Press Conference Date of the C/NOFS = Dec. 15-19, 2008"]
-[9.247901916503906, 3.1812050342559814, "[FF] Presentation Date of the Magnetospheric Multiscale (MMS) = 2008"]
-[9.384499549865723, 4.991866588592529, "[FF] Attitude Orientation of the ICESat = -ZG axis is 0.3\u00ba from geodetic nadir"]
-[9.992218017578125, 4.291629314422607, "[TT] Type of the Magnetorquers = Two cylindrical coils with ferrite cores, one flat square with no core"]
-[14.193370819091797, 3.143907308578491, "[TT] Total Mass of the Landmapper-Demo6 = Approximately 80 kg"]
-[9.2318696975708, 0.3054313063621521, "[TT] Total Length of the Gathering Pipelines = 435,000 miles"]
-[6.353854656219482, 0.7047772407531738, "[TT] Last Eclipse Avoidance Maneuver Date of the Gaia = 16 July 2019"]
-[5.989324569702148, 4.105963706970215, "[FF] CONOPS and FDIR Features of the Twinkle = Robustness and redundancy; on-board autonomy and simple satellite safe-modes; extensive use of proven, off-the-shelf components; modularity"]
-[6.254895210266113, 5.6207733154296875, "[TT] Alternate Name of the Prichal Module = Prichal Node Module (UM) or Progress M-UM"]
-[9.060288429260254, 3.1236414909362793, "[FF] Function of the SWID (Solar Wind Ion Detector) = Probe the near-moon space environment"]
-[10.152031898498535, 1.343967318534851, "[TT] Previous Catalogue Object Count (1991) of the Gaia Catalogue of Nearby Stars = 3803 celestial objects"]
-[3.3571202754974365, 5.380875587463379, "[TT] Frequency of the SAR antenna = 5.350 GHz"]
-[9.724987030029297, 8.365257263183594, "[TT] FOVs of the CrIS = 9"]
-[7.631868839263916, 8.33011245727539, "[FF] Spectral Ranges of the GOSAT-2 = Nadir viewing b1: 370-390 nm, b2: 664-684 nm, b3: 860-880 nm, b4: 1555-1645 nm"]
-[7.902924060821533, 7.165370464324951, "[TT] Interferometer Configuration of the FTS = Mach-Zehnder"]
-[6.240232944488525, 2.177344799041748, "[FF] URL of the WorldView Legion = https://blog.maxar.com/earth-intelligence/2020/enhancing-national-security-missions-with-worldview-legion"]
-[10.402552604675293, 2.3952438831329346, "[FF] Operation Modes of the NICER X-ray telescope = 2-axis gimbal, tracking celestial X-ray sources, pointing towards ELC 3"]
-[4.689081192016602, -0.03916218504309654, "[TT] End of Life of the S3B = 2028"]
-[2.96159291267395, 2.382589340209961, "[FF] Atmospheric Constituents of the Sentinel-5 = Ozone, nitrogen dioxide, sulphur dioxide, carbon monoxide, methane, formaldehyde, and aerosol properties"]
-[14.621607780456543, 6.647489070892334, "[TT] Li-ion-polymer Battery Capacity of the EPS = 910 mAh"]
-[8.565961837768555, 4.64923620223999, "[TT] Sensors of the iADCS-100 = ST-200 star tracker"]
-[3.403393507003784, 3.635232925415039, "[FF] Mission Date of the PAZ = Sept. 6-11, 2010"]
-[8.695168495178223, 6.74582576751709, "[TT] Instrument of the DMC-3 = PAN (BJ-2)"]
-[9.521836280822754, 4.787043571472168, "[TT] Attitude Control of the AlSat-2 = 3-axis stabilized"]
-[5.707540512084961, 4.753354072570801, "[TT] Downlink Encryption of the EDRS GEO satellite = Planned"]
-[5.908561706542969, 0.22616147994995117, "[TT] Launch Date of the JUICE = 2022"]
-[8.984762191772461, 8.138465881347656, "[TT] Number of SWIR Focal Planes of the GLI = 2"]
-[9.55314826965332, 4.217219829559326, "[TT] Sensor Type of the MPS = Three-axis vector magnetometer"]
-[13.33431625366211, 7.348547458648682, "[TT] Power Increase of the Arrays = 20 to 30 percent"]
-[9.751015663146973, -0.530610203742981, "[TT] Orbit Altitude of the Light-1 = Approximately 400 km"]
-[6.4864277839660645, 7.647696495056152, "[TT] Data quantization of the ALOS-3/PRISM-2 = 11 bit"]
-[9.51003360748291, -0.6480185389518738, "[TT] Current Orbit of the ExoMars TGO = One-day, 200 x 33 000 km"]
-[8.203461647033691, 6.799339294433594, "[FF] Design Requirements of the WSF-M = OSVW, TCI, Imagery SDR"]
-[6.2055134773254395, 1.5291075706481934, "[TT] Status of the eROSITA = Operational"]
-[6.221524715423584, 6.013363838195801, "[TT] Performance of the VBN = Proven"]
-[10.096003532409668, 1.9808427095413208, "[FF] Return to Science Operations Date of the Chandra X-ray Observatory = 24 October 2018"]
-[8.352166175842285, 0.6292523145675659, "[FF] Scientific Objectives of the DCAM3-D = (1) clarifying the subsurface structure, and (2) constructing the impact scaling rule applicable to the surface of asteroid 1999JU3"]
-[4.4133806228637695, 1.116192102432251, "[TT] Delegated Regulation Date of the GMES-S = December 2013"]
-[9.298025131225586, 2.623711347579956, "[TT] Number of X-class flares of the SOHO = 11"]
-[6.594083309173584, 5.904791355133057, "[TT] Quantity of the BCR = 6"]
-[4.592405319213867, 7.236988067626953, "[TT] Ka-band System of the STPSat-6 = Receive up to 64 Mbit/s"]
-[5.325839996337891, 7.0205559730529785, "[TT] Data Downlink Speed of the Payload = 800 Mbit/s"]
-[14.251714706420898, 3.2168829441070557, "[TT] Mass of the CanX-2 = About 3.5 kg"]
-[6.907556056976318, 3.519730806350708, "[FF] Purpose of the Vascular Echo study = Investigates cardiovascular health in space"]
-[4.163032054901123, 0.6382158398628235, "[FF] News Archive Date of the INTEGRAL = 5 Aug. 2011"]
-[5.571331977844238, 2.2541236877441406, "[FF] Affiliation of the Yoshihiro Tomioka = Unknown"]
-[6.989585876464844, 0.1273079514503479, "[TT] Mission Duration of the SeaSat = 70 days (data generation) of 105 operational days (1503 orbits)"]
-[10.993184089660645, 7.353431224822998, "[TT] Swath Width of the Satellite = 63 km"]
-[9.335206031799316, 5.001026630401611, "[TT] Attitude Knowledge of the AOCS = 0.02\u00b0"]
-[5.314145565032959, 5.642083168029785, "[TT] Data Interface Protocol of the CDMU = dedicated packet structure"]
-[4.70243501663208, 0.3913804888725281, "[TT] End of Life Date of the Monitor-E = 21 Jan 2008"]
-[5.392470836639404, 5.667954921722412, "[TT] Data Transfer Protocol of the Ground Support System = TFTP (Trivial File Transfer Protocol)"]
-[5.254911422729492, 3.9058966636657715, "[TT] Number of Satellites per Mission of the Copernicus = 2"]
-[5.95220422744751, -0.4348929524421692, "[TT] Primary Mission Duration of the NEA Scout = 2.5 years"]
-[4.513840198516846, -0.9111248850822449, "[TT] Launch Date of the Dragon spacecraft = 3 June 2021"]
-[4.68187952041626, 0.18370188772678375, "[TT] Launch Date of the IDEA OSG 1 = 28 November 2017"]
-[8.468945503234863, 7.567966938018799, "[TT] Detector Type of the RAMIS = Two silicon detectors"]
-[5.5748162269592285, 4.876731872558594, "[FF] Commissioning Sequence of the GPS receivers = Relative GPS sensors, CLS, FLLS"]
-[8.03901481628418, 5.78131628036499, "[TT] Calibration Period of the LISS-3 camera = Eclipse period of the satellite pass"]
-[9.130440711975098, 3.4632699489593506, "[FF] Purpose of the GEOTAIL = Study the processes that initiate magnetic field reconnection in the near-Earth tail and observe the microscopic nature of the energy conversion mechanism in the reconnection region"]
-[14.676756858825684, 6.6512227058410645, "[TT] Battery Capacity of the UK-DMC-2 = 15 Ah"]
-[7.527540683746338, 2.025071144104004, "[FF] Mission Goals of the Tandem-L = Global measurement of forest biomass, recording of earth\u2019s surface deformations for earthquake research and risk analysis, large scale observation of ocean currents and sea ice drift, and quantification of glacier movements and melting processes"]
-[2.36264705657959, 2.792290210723877, "[TT] PI of the SORCE = G. J. Rottman"]
-[16.501035690307617, 3.585653781890869, "[TT] Global Service Availability of the OneWeb = 2022"]
-[3.833221912384033, 6.373267650604248, "[TT] Ground Segment Antennas of the IXPE = 10 m antennas at Malindi (primary) and Singapore (backup)"]
-[5.707089900970459, 2.4423959255218506, "[FF] Educational Mission of the ABEX = Provide educational opportunities with academic engagement for students on an actual aerospace system"]
-[5.292172431945801, 0.6200381517410278, "[TT] Launch Date of the Small Satellite = 2021 or 2022"]
-[4.816863059997559, 0.8293817043304443, "[TT] Completion Date of the CST-100 = October 17, 2014"]
-[4.989239692687988, 0.16844841837882996, "[TT] Launch Date of the Vigilance Mission (KSF1) = End of June"]
-[4.74915075302124, 6.59082555770874, "[FF] Communication Protocol of the UHF/VHF data frame = AX.25"]
-[6.646381855010986, 1.818164348602295, "[FF] URL of the ELSA-d = https://astroscale.com/missions/elsa-d/"]
-[8.330846786499023, 7.385461330413818, "[TT] Linearity of the PMC-2 Imagers = Better than 3%"]
-[7.681796550750732, 8.515027046203613, "[TT] NIR Bands of the MTI = E, F, and G"]
-[4.069194316864014, 3.571063756942749, "[FF] Purpose of the GPLTBs = Development models of the navigation payloads intended for the Galileo Second Generation (G2) satellites"]
-[9.90778923034668, 5.61851167678833, "[FF] Function of the Thermal Straps = Transfer heat and decouple any external CTE and/or structural loads into the optical systems"]
-[5.631716728210449, 0.547679603099823, "[FF] International Space Station Operations Update Date of the UrtheCast = April 3, 2014"]
-[5.689986705780029, -0.36268290877342224, "[TT] Connection Time of the Deployment Specialists = 11 hours"]
-[5.813109397888184, 4.2052788734436035, "[FF] System Module Electronics Boxes of the GOES-R Series Weather Satellite = More than 70"]
-[5.363574981689453, 4.542747974395752, "[TT] Services of the Ground Station = Monitoring and control"]
-[10.344012260437012, 5.631949424743652, "[TT] Number of Temperature-Controlled Zones of the HTSSE-II payload = 5"]
-[5.922430038452148, 6.044336795806885, "[TT] Daily Imaging Capacity of the Corvus-BC = 1.2 TB"]
-[4.1463823318481445, 7.3014326095581055, "[TT] Band of the ScatSat-1 = Ku-band"]
-[10.901966094970703, 0.67547208070755, "[TT] Cosmic Ray Susceptibility Occurrences of the Kepler = Four"]
-[10.193999290466309, 5.5054240226745605, "[TT] Thermal Control of the Telescope Tube Assembly = On-board heaters"]
-[1.7606364488601685, -2.0627787113189697, "[FF] URL of the Hayabusa2 = http://www.jspec.jaxa.jp/e/activity/hayabusa2.html"]
-[9.137904167175293, 5.938597202301025, "[TT] Directions of the Instrument = Nadir, Forward, Backward"]
-[10.237603187561035, 2.4274117946624756, "[TT] Energy Range of the SXD and solar X-ray monitor = 1-10 keV"]
-[5.091132164001465, 0.4283057749271393, "[TT] Launch Date of the Aeolus = 22 August 2018"]
-[5.802774906158447, 4.826989650726318, "[FF] Function of the Feeder-link station = Transmit commands through a relay satellite and obtain telemetry data"]
-[7.053873062133789, -0.4062983989715576, "[TT] Orbit Completion of the DMSP-14 = 100,000th"]
-[4.281183242797852, 0.3440890908241272, "[TT] Launch Date of the JPSS = 2017"]
-[5.524111270904541, -0.5847703814506531, "[TT] Design Life of the Odin = 2 years"]
-[3.410395622253418, 6.416430950164795, "[TT] Diameter of the Ka-band parabolic dish antenna = 70 cm"]
-[7.278310298919678, 2.7976925373077393, "[FF] Documentation Source of the Sensor Complement = Observation of the Earth and Its Environment: Survey of Missions and Sensors"]
-[6.1915483474731445, 3.51007080078125, "[TT] Required Thesis Level of the Experiment = Master or PhD"]
-[4.882089138031006, 3.231184244155884, "[TT] Manufacturer of the Kanopus-V-IK = NPO VNIIEM"]
-[6.134993553161621, -0.25687211751937866, "[TT] Sampling Duration of the CREAM = At least three years"]
-[14.25385570526123, 3.2355105876922607, "[TT] Mass of the MWR = 99 kg"]
-[8.074722290039062, 3.8801305294036865, "[FF] Design Requirement 2 of the OCO-3 PMA = Movement not affect the measurements through angular dependent polarization or radiance changes"]
-[6.6527886390686035, 0.7319232225418091, "[TT] Number of Observations of the Claire = Over 4000"]
-[6.241690158843994, 1.5836259126663208, "[FF] URL of the GeoEye-1 = http://launch.geoeye.com/LaunchSite/assets/documents/geoeye1_factsheet.pdf"]
-[6.41339635848999, 7.30730676651001, "[TT] Output of the SPM = Digital Signals"]
-[4.961671829223633, 3.309427499771118, "[TT] Data Management Center of the SASS = LaRC (Langley Research Center)"]
-[5.360258102416992, 3.0188419818878174, "[TT] Developer of the TransHab = William Schneider"]
-[12.111753463745117, 3.4584498405456543, "[TT] Propellant Mass of the PPCU ion thruster = 12 kg"]
-[8.5140380859375, 5.52923059463501, "[TT] Accuracy of the GPS-fed high-accuracy ephemerides = ~5 m"]
-[4.239231586456299, 2.5682132244110107, "[TT] Launch Location of the GOES-T = Cape Canaveral Air Force Station in Florida"]
-[7.243884563446045, 3.4178569316864014, "[FF] Pass Frequency of the Satellite = 16 passes per day"]
-[5.348597049713135, 0.29421818256378174, "[TT] Operation Start Date of the Cheops = Beginning of April"]
-[5.049134731292725, 6.792921543121338, "[TT] TT&C Communications of the Spacecraft = 4 kbit/s (uplink), 32 kbit/s to 6.25 Mbit/s (downlink)"]
-[5.016522407531738, 5.667382717132568, "[TT] Instrument Type of the HORYU-2 = Other, Communications, Data collection, Lightning sensors"]
-[9.662576675415039, 4.631878852844238, "[TT] Control Method of the ACS = Magnetic control"]
-[6.450907230377197, 3.820315361022949, "[FF] Servicing Concept of the Bartolomeo Platform = Fully robotically serviceable"]
-[5.960202693939209, -0.3896300792694092, "[TT] Duration of the Mission of the BRITE = Longer than 2 years"]
-[6.985767841339111, 1.0676193237304688, "[TT] Launch Date of the Mars Ascent Vehicle (MAV) = 2026"]
-[6.708414554595947, 4.899333953857422, "[FF]  of the CubeControl = "]
-[10.013035774230957, -1.6158310174942017, "[TT] Orbit Inclination of the Secondary Payloads = 102\u00ba"]
-[7.354644298553467, 0.24392585456371307, "[TT] Sample Collection Date of the OSIRIS-REx = Oct. 20, 2020"]
-[4.821798324584961, -1.0004814863204956, "[TT] Launch Date of the FengYun-4A = December 2016"]
-[6.061469554901123, -0.27076321840286255, "[FF] Planning Duration of the MOPITT = 12 Years"]
-[7.830418109893799, 6.36772346496582, "[TT] Name of the VNIIFTRI = VNIIFTRI (All-Russian Scientific Research Institute of Physical and Radio-Engineering Measurements)"]
-[10.992060661315918, 6.312596797943115, "[TT] Material of the Secondary Mirror = SiC"]
-[5.732837200164795, 4.563398838043213, "[FF] User Ground Stations of the EDRS = The users can also operate their own user ground stations to receive directly the user data"]
-[5.608119964599609, -0.35536694526672363, "[TT] Deployment Duration of the STP-2 mission = Approximately 3 hours and 32 minutes"]
-[3.9462742805480957, 6.287386894226074, "[TT] Antennas of the SGR-10 = Two antennas"]
-[8.770556449890137, 4.714881896972656, "[FF] Approach of the Precise Position Determination System = Star tracker calibration, estimate of optical sensor directional alignment and precise attitude determined value processing"]
-[6.776973724365234, 5.26926326751709, "[FF] Components of the DHU = IPC (Image Processing Computer), Proton 400 k single board computer, 192 GB SSB (Solid-State Buffer) cards, analog I/O power switch board, power supply board"]
-[8.901375770568848, 5.944826126098633, "[TT] Tracking Test Speed of the Antenna Subsystem = Approximately 10 km/h"]
-[6.07746696472168, 5.944775581359863, "[TT] Test Modules (TM) of the SAMMES = 5 units"]
-[7.860110759735107, 8.546541213989258, "[TT] Spectral Bands of the TIR Instrument = 8-12 \u00b5m range"]
-[1.715840458869934, 6.139400482177734, "[TT] Normal Matter Percentage of the Universe = Under 5%"]
-[5.293718338012695, 8.371471405029297, "[FF] Brightness Temperature Channels of the GCOM-W1 = 89.0 GHz, 23.8 GHz"]
-[9.023977279663086, 5.618237495422363, "[TT] Pointing Capability of the ADCS = \u00b130\u00ba"]
-[12.002034187316895, 4.694995880126953, "[TT] Housing Dimensions of the MuREM = 10 cm x 10 cm x 4.5 cm"]
-[6.850753307342529, 1.6085337400436401, "[FF] URL of the ExoMars = http://exploration.esa.int/mars/48088-mission-overview/"]
-[8.961305618286133, -0.7909654378890991, "[TT] Longer Spacecraft Contact Periods of the MEO Orbit = Than in LEO"]
-[11.206904411315918, 5.351635932922363, "[TT] Components of the GARI-1 = Two cerium-doped gadolinium aluminum gallium garnet (GAGG (Gd3(Al,Ga)5O12 :Ce)) scintillation detectors"]
-[8.201306343078613, 3.272739887237549, "[TT] Instrument Type of the ST5 = Magnetic field, Atmospheric chemistry, Data collection"]
-[5.193432807922363, 6.981195449829102, "[TT] Uplink Lock Time of the LLCD PAT Systems = Within seconds"]
-[9.806406021118164, 4.543435096740723, "[TT] Control Type of the AOCS = Bias-wheel and magnetic torquer control"]
-[4.940519332885742, 7.384444236755371, "[TT] Data Rate of the RF communication = 4 kbit/s uplink, 1.6 Mbit/s downlink"]
-[7.457949161529541, 8.357625007629395, "[TT] Preferred Number of Perfect Rows of the QWIP Array = 2"]
-[6.380560874938965, -0.09163829684257507, "[TT] Operation Time of the SCOPE = Day and night"]
-[10.147305488586426, 1.3943743705749512, "[TT] Star Detection Rate of the Gaia = Up to 10,000 stars/s"]
-[7.538559436798096, 1.2278633117675781, "[FF] Image of the Remote Lakes = URL: https://earthobservatory.nasa.gov/images/148230/sizing-up-remote-lakes"]
-[5.795239448547363, 2.984266757965088, "[FF] Technology Development Funding of the MAST = NASA Small Business Technology Transfer (STTR) contract"]
-[9.867807388305664, 2.667649984359741, "[FF] Deployment Rounds of the NanoRacks = 3"]
-[9.752518653869629, -0.5540733933448792, "[TT] Altitude of the CBERS-2B = 778 km"]
-[9.109319686889648, -1.2521536350250244, "[TT] Orbit of the Konnect = GEO"]
-[7.985398292541504, 0.24325327575206757, "[FF] Data Usage of the GRACE-FO = Detect the movement of water on Earth based on variations of Earth\u2019s gravity field"]
-[8.452061653137207, 0.15352286398410797, "[FF] Structure of the Comet 67P/Churyumov-Gerasimenko = Double-lobed body with extensive layering"]
-[6.083674430847168, 3.4747045040130615, "[TT] Development Risk of the HTA = Low"]
-[13.607754707336426, 5.555357456207275, "[TT] Solar Cells of the EPS = 24"]
-[9.106760025024414, 7.462158679962158, "[TT] Pixel Size of the SXI = 5 arcsec x 5 arcsec"]
-[9.704255104064941, 7.902209281921387, "[FF] Image Span of the NGC 7538 = About 50 x 50 arc minutes"]
-[9.743663787841797, 0.5502920150756836, "[FF] Distance Range of the Spacecraft = 70 to 50 km"]
-[7.170694828033447, 4.976529121398926, "[FF] Function of the Motor Control Module = Control the position or speed loops"]
-[13.521047592163086, 2.931774616241455, "[TT] Mass of the LituanicaSAT-2 = 3 kg"]
-[10.024615287780762, 0.703986406326294, "[TT] Closest Separation Distance of the Cluster spacecraft = 4 km"]
-[11.007770538330078, 0.576261043548584, "[TT] Number of Planet Candidates Identified of the Kepler = 1,235"]
-[4.2811174392700195, 4.130792140960693, "[FF] Operation of the GEOLUTs = With the GEOSAR payloads flown on various GEO missions"]
-[6.44651460647583, 7.608882427215576, "[TT] Data Quantization of the Spacecraft = 10 bit"]
-[5.205110549926758, 2.304516077041626, "[TT] Mission Type of the HAUSat-2 = Non-EO"]
-[5.5913825035095215, -0.0413297675549984, "[TT] Retrieval Planned Time of the LDEF = 10 months"]
-[10.537471771240234, 5.799984931945801, "[FF] Battery Temperature of the SpriteSat = Can go up to a critical level"]
-[4.807783126831055, 7.963307857513428, "[TT] Frequency of the PLB = 121.5 and 406 MHz"]
-[4.776706695556641, 5.815736770629883, "[TT] Frequency (MHz) of the Compass-BeiDou B1 = 1575.42"]
-[8.172957420349121, -0.18055295944213867, "[TT] Period (min) of the Meteor-2-1 = 102.5"]
-[11.245162963867188, 5.336279392242432, "[FF] Scintillator Size of the Gamma-ray Counter = 12 cm x cm"]
-[6.3544793128967285, 4.788619518280029, "[FF] Functional Architecture of the EO-ALERT = Modular, scalable and reconfigurable"]
-[6.922636032104492, 4.643337249755859, "[FF] Unknown of the Spectrum-RG = Unknown"]
-[14.06914234161377, 7.153986930847168, "[TT] Power Bus of the Payload Instruments = 28 V unregulated, switched"]
-[12.136590003967285, 4.6306304931640625, "[TT] Dimensions of the Spacecraft = 765 x 730 x 830 mm"]
-[9.734339714050293, 8.572026252746582, "[TT] IFOV (Instantaneous FOV) WV and TIR of the MVIRI = 0.14 mrad"]
-[3.524984121322632, 4.50091028213501, "[TT] Ground Station of the SAR-Lupe = 1"]
-[11.761536598205566, 3.291682720184326, "[TT] Thrusters of the LISA Pathfinder = \u00b5N"]
-[14.096635818481445, 3.4674060344696045, "[TT] Mass of the Kestrel Eye II = ~50 kg"]
-[9.588823318481445, 8.265947341918945, "[TT] Field of View of the SSJ/5 = 90\u00ba"]
-[11.381221771240234, 4.400341510772705, "[TT] Size of the CSSWE = 3U"]
-[9.655203819274902, 7.18902587890625, "[TT] Pixel Size of the OCO-3 = About 1.3 miles (2.2 km)"]
-[5.781005382537842, 2.302543878555298, "[FF] Partners of the ExoMars = ESA and Roscosmos"]
-[9.14677619934082, 6.003175258636475, "[TT] Ground Pointing Accuracy of the NEMO-HD = Approximately 260 m"]
-[13.340998649597168, 7.844446659088135, "[TT] Output Power of the TREX-823 X-band transmitter = 7 W (min)"]
-[9.536260604858398, 6.211154460906982, "[TT] Incidence Angle of the Wide fine = 20 - 45\u00ba"]
-[11.281228065490723, 3.4194436073303223, "[FF] Propulsion System of the Spacecraft = Electric propulsion for the cruise and spiral down phases and chemical propulsion for Mars orbit insertion"]
-[5.146684646606445, 8.432522773742676, "[TT] Bandwidth (MHz) of the PMI = 750"]
-[5.818704605102539, -0.7570726871490479, "[TT] Design Life of the Satellite = Ten years"]
-[13.329702377319336, 7.121776580810547, "[FF] Power Efficiency of the VGT-P = Required to be very efficient in its power use"]
-[3.894725799560547, 4.249345779418945, "[TT] Operational Status of the RADARSAT-2 = Fully operational"]
-[8.937987327575684, 4.416398525238037, "[TT] Quantity of the FM coarse sun sensors = 6"]
-[11.924178123474121, 5.0421881675720215, "[TT] Size of the MSI = 1.47 m long x 0.93 m wide x 0.62 m high"]
-[9.506400108337402, 6.0992231369018555, "[TT] Earth Incidence Angle of the AMSR-E = 55.0\u00ba"]
-[5.071251392364502, 0.4665983319282532, "[TT] Critical Design Review Status of the MSASI = Finished"]
-[5.9761881828308105, -0.33748069405555725, "[TT] Operation Duration of the DMSP = Over 50 years"]
-[8.478131294250488, 6.218345642089844, "[TT] Acceptable Location of the TEMPO = 80-120\u00ba W"]
-[4.448936462402344, 3.180366039276123, "[TT] Ground Segment Location of the PROBA-3 = Redu (in Belgium)"]
-[5.946944713592529, 8.729720115661621, "[TT] MTF at Nyquist Frequency of the Spacecraft = > 20% for MS"]
-[9.616681098937988, 4.798283100128174, "[FF] Stabilization of the Block 5D-1 = The attitude-control system thereafter slowed the rate of tumbling until the satellite stabilized on three axes and began operating properly"]
-[9.181111335754395, -0.369289755821228, "[TT] Apogee of the SeaSat = 799 km"]
-[13.835845947265625, 6.682465076446533, "[TT] Power Source of the SPAS carrier = Battery"]
-[6.847021102905273, 4.817722320556641, "[TT] Panel 5 Function of the CSTB1 = Payload panel"]
-[7.249212741851807, 6.892877578735352, "[FF] Size of the APD detector = Very small"]
-[7.986685752868652, 0.1646977663040161, "[FF] Purpose of the GRACE-FO = Measure the change in the mass of water across the planet"]
-[9.59047794342041, 6.978265762329102, "[TT] Spatial Resolution of the AltiKa = 40-50 km"]
-[2.3286120891571045, 1.3109983205795288, "[FF] Sponsors of the NanoSail-D2 = Army Space and Missile Defense Command, the Von Braun Center for Science and Innovation, Dynetics Inc"]
-[6.013352870941162, 4.862280368804932, "[FF] Function of the LCT link service = Forward data from the EDRS GEO satellite to the target LEO satellite"]
-[11.1345853805542, 0.9431924819946289, "[TT] Triangular of the LISA = Yes"]
-[10.796496391296387, 3.4898598194122314, "[TT] CubeSat Size of the MiRaTA = 3U"]
-[5.550597667694092, 0.12108727544546127, "[TT] Start of Operation of the LS-7 = 2010"]
-[5.297250747680664, 0.7681430578231812, "[FF] Contract Date of the Capella = 17 June 2021"]
-[8.756183624267578, 2.381892442703247, "[FF] Dust Production of the McNaught = High"]
-[4.411036968231201, 3.151080846786499, "[FF] Ground Stations of the MOC = Harwell, Weilheim, and Redu"]
-[11.271817207336426, 3.3175907135009766, "[FF] Conference Date of the Micropropulsion Experiment = March 9-16, 2002"]
-[5.47592830657959, 6.067783355712891, "[TT] Memory of the OHDH = 512 kB EEPROM & 2 MB RAM"]
-[4.857257843017578, 0.5999686121940613, "[TT] Failure Date of the MWTS-2 = Feb. 2, 2015"]
-[6.581767559051514, 2.163759708404541, "[FF] Debut Location of the Visualization = American Astronomical Society meeting in Honolulu, Hawaii"]
-[11.061643600463867, 6.04998779296875, "[TT] Material of the Optical Bench = Zerodur"]
-[10.531046867370605, 6.592804908752441, "[TT] Total Shells per Module of the Mirror = 130"]
-[9.536710739135742, 0.9619583487510681, "[TT] Material Collision Speed of the Cassiopeia A (Cas A) = 10 million miles per hour"]
-[3.085696220397949, 4.45292854309082, "[FF] Modes of the TerraSAR-X NG = Very high-resolution modes, heritage modes, wide swath modes"]
-[3.8826801776885986, 1.9746251106262207, "[TT] Launch Vehicle of the OCO-3 = Falcon 9 rocket"]
-[9.382062911987305, 3.578862190246582, "[FF] Data Collection of the Magnetometer = Planet's southern hemisphere"]
-[3.2367005348205566, 2.2019402980804443, "[FF] Mission Location of the Copernicus Sentinel-2 = Tarawa Atoll in the Republic of Kiribati"]
-[7.216245174407959, 0.9307397603988647, "[TT] Launch Date of the SeaSat = June 26, 1978"]
-[10.973366737365723, 2.0743963718414307, "[FF] First Observation of the XMM-Newton = June 1962"]
-[7.8986334800720215, 2.5912883281707764, "[FF] Partial Pressure of Carbon Dioxide in the Water of the Marine Chemistry = Unknown"]
-[9.658438682556152, 3.980527639389038, "[TT] Client Docking Plate of the ELSA-d = Ferromagnetic"]
-[8.573655128479004, 1.9408246278762817, "[TT] Quantization Levels of the Ocean surface wind speed = 1"]
-[4.433478832244873, 7.649202823638916, "[TT] Frequencies of the IMI = L-, S-, C-band 6.8, 10.65, 18.7, 23.8, 37, 89, 150 GHz X-band, Ku-band"]
-[9.22864818572998, 8.703587532043457, "[TT] Entrance Slit Widths of the Ultraviolet Spectrograph = 0.2 mm and 0.4 mm"]
-[5.238349437713623, 1.2911146879196167, "[FF] Conference Date of the ALOS-2 = Sept. 20-23, 2010"]
-[3.401067018508911, 4.809184551239014, "[FF] Conference Presentation of the CSG SAR instrument = EUSAR 2016, 11th European Conference on Synthetic Aperture Radar, Hamburg, Germany, June 6-9, 2016"]
-[8.27740478515625, 5.669041156768799, "[FF] Pointing Accuracy of the MWI Instrument = Unknown"]
-[8.02832317352295, -0.9471908211708069, "[TT] Data Collection of the ICESat-2 = Every 70 cm"]
-[5.901400566101074, -0.4884956181049347, "[TT] Mission Goal of the MinXSS-2 = 5 years"]
-[4.526773452758789, 7.603139877319336, "[TT] Bandwidth of the Downlink (Ku-band) = 12 MHz"]
-[8.514065742492676, 4.932798385620117, "[FF] Function of the Shutterless system = Achieve temperature calibration and straylight correction"]
-[9.168756484985352, 7.0503153800964355, "[TT] Resolution of the Sun Tracker = 8 arcsec per pixel"]
-[8.303871154785156, 6.8200201988220215, "[TT] Operating Mode of the CIRiS = Pushbroom"]
-[9.298266410827637, 7.125514030456543, "[TT] Resolution of the AEISS = 4 m (4 x MS)"]
-[7.454192638397217, 3.401481866836548, "[FF] Measurement Frequency of the GeoCARB = Daily"]
-[9.115476608276367, -1.2706016302108765, "[TT] Satellite Type of the EUMETCast = Geostationary"]
-[10.632328987121582, 1.6696772575378418, "[FF] Volume of the The Astronomical Journal = 155"]
-[3.7072784900665283, 2.441204309463501, "[TT] In-Service Date of the Iridium Next = October 2015"]
-[8.03121280670166, -0.14259019494056702, "[FF] Cub Litter Size of the Polar Bears = Larger when spring breakup occurred later in the year"]
-[8.3990478515625, 6.079689025878906, "[TT] Overall Absolute Measurement Error at 333 K in Bands 4-6 of the Scanning geometry = 0.5 K"]
-[9.13672161102295, -1.1785244941711426, "[TT] Orbit Type of the INSAT-3D = Geostationary"]
-[7.160948753356934, 2.8240208625793457, "[TT] Mission Date of the MethaneSAT = August 7-12, 2021"]
-[6.060777187347412, 5.505399703979492, "[TT] Redundancy Type of the Computer System = Cold redundant"]
-[6.986444473266602, 4.238914966583252, "[FF] Unknown of the AMICA = Unknown"]
-[12.13165283203125, 6.215281009674072, "[TT] Number of Particles Recorded of the Alpha Magnetic Spectrometer - 02 (AMS-02) = Over 140 billion particles"]
-[6.459836006164551, 1.923825740814209, "[FF] URL of the Shuttle Radar Topography Mission = http://www.shuttlepresskit.com/STS-99/payload56.htm"]
-[10.928579330444336, 7.534319877624512, "[TT] Swath Width of the NAOMI = 10 km to 60 km"]
-[4.911380767822266, 0.39466017484664917, "[TT] Launch Date of the Electron rocket = November 11, 2018"]
-[11.248431205749512, 3.333573341369629, "[FF] Design and Prototyping Date of the Micropropulsion System = Nov./Dec. 2002"]
-[4.690151691436768, 3.1844987869262695, "[TT] Manufacturer of the Copernicus CIMR satellites = Thales Alenia Space"]
-[9.469694137573242, 2.779802083969116, "[FF] Purpose of the Solar X-ray Spectrometer = Detect X-ray pulses produced by coronal mass ejections"]
-[1.9310846328735352, -0.40254488587379456, "[FF] Nonlinear Wave Structures Effect of the Van Allen Probes = Rapidly energize very low energy (~10 electron volts) electrons up to intermediate energies (~100 keV)"]
-[7.557416915893555, 6.895668029785156, "[TT] Operational Cadence of the Instrument = Stare nadir for 30-40 minutes"]
-[9.387520790100098, 8.403185844421387, "[TT] 50% Ensquared-Energy Half-Width of the Lens = 15 \u00b5m (one pixel or 0.35 arcmin)"]
-[9.341276168823242, 6.684067726135254, "[TT] Resolution of the FRS-2 = 3 m (Azimuth) x 4 m (Range)"]
-[6.547991752624512, 3.0054361820220947, "[FF] Data Archive and Distribution of the TSIS-1 = ESDIS (Earth Science Data and Information System) Project/GES DISC (Goddard Earth Sciences Data and Information Services Center)"]
-[9.270182609558105, 0.8704432845115662, "[FF] Article Title of the E. Christiansen, A. Davis, J. Miller, D. Lear = Hypervelocity Impact Test with Large Mass Projectile"]
-[5.081639289855957, 0.7676381468772888, "[FF] Mission Date of the STARE = Aug. 10-15, 2013"]
-[7.652372360229492, 5.603222370147705, "[TT] Manufacturer of the Scanning Shack Hartmann Sensor = AMO WaveFront Sciences, LLC"]
-[10.685663223266602, -0.13817305862903595, "[FF] Vertical Distance of the TerraSAR-X and TanDEM-X = Constant for most of the time"]
-[14.596979141235352, 6.623032569885254, "[TT] Type of the Li-Ion batteries = Li-Ion"]
-[10.912596702575684, 10.096659660339355, "[FF] Collaboration of the Alpha Magnetic Spectrometer (AMS-02) = North America (USA, Mexico), Asia (China, Korea, Taiwan), Europe, including nine ESA Member States (Denmark, Finland, France, Germany, Italy, The Netherlands, Portugal, Spain, Switzerland) and Russia"]
-[6.188093185424805, 2.1539011001586914, "[TT] Selection Date of the Euclid Consortium = June 2012"]
-[7.6324543952941895, 1.6486960649490356, "[FF] Indicator of Future Reef State of the Coral Mortality = May be a key determinant of future reef state"]
-[5.04670524597168, 2.9000680446624756, "[TT] Developer of the Proteus Platform = French space agency CNES and Thales Alenia Space"]
-[10.333821296691895, 3.1167945861816406, "[FF] Quantity of the GEMSat/ELaNa-2 = 12 CubeSats/nanosatellites"]
-[4.17668342590332, 2.023019552230835, "[TT] Global Revisit Opportunities of the NigeriaSat-2 = At least every 2 days"]
-[10.913802146911621, 3.774195671081543, "[FF] Maneuvering Principle of the NEA Scout = Tipping and tilting its sail to change the angle of sunlight"]
-[5.136101722717285, 0.9618539810180664, "[FF] Launch Date of the HISUI = Unknown"]
-[4.507964134216309, 1.2860345840454102, "[FF] Launch Date of the AlSAT-1 = Unknown"]
-[6.7057647705078125, 0.7288818359375, "[FF] Article URL of the Herschel = http://sci.esa.int/herschel/54252-young-suns-violent-history-solves-meteorite-mystery/"]
-[7.567421913146973, 8.834716796875, "[TT] Band 1 Max Radiance of the COCTS = 13.94"]
-[5.4631028175354, 0.7357985377311707, "[FF] Contract Win Date of the Spire, GeoOptics = Sept. 16, 2016"]
-[7.599948406219482, 2.9730491638183594, "[FF] Contribution of the PROBA-3 = Space Weather Studies"]
-[3.382884979248047, 6.446818828582764, "[TT] Antenna Diameter of the USAT = 0.65 m"]
-[3.4454824924468994, 5.9661478996276855, "[TT] Azimuth Dimension of the Active Phased Array Antenna = 15 m"]
-[8.218276977539062, 3.158752202987671, "[FF] Mission of the TGO = Measure the abundance and distribution of rare gases in the atmosphere"]
-[8.86711597442627, 5.754336357116699, "[TT] Strong source (> 10\u03c3) positioning of the Instrument = 1.5 arcsec (1\u03c3)"]
-[10.525811195373535, 6.682224750518799, "[TT] Reflectance of the Primary Mirror = >0.27 between 40 nm and 200 nm"]
-[4.3304948806762695, 2.9542789459228516, "[TT] Location of the GVES = Vesleskarvet Antarctica"]
-[9.488694190979004, 6.92581033706665, "[TT] Resolution of the Scatterometer Antenna = 25 km"]
-[13.970527648925781, 7.029704570770264, "[TT] Output Voltage of the NanoPower P31us = 3.3 V and 5.0 V"]
-[5.3795366287231445, 8.770040512084961, "[TT] Bandwidth of the Band 2 = 433-453 nm"]
-[10.082136154174805, 8.010665893554688, "[TT] Focal Length of the NuSTAR instrument = 10.15 m"]
-[8.187206268310547, 8.202483177185059, "[TT] Spectral Range of the IMG = 303 - 714 cm -1 (3.3 - 14.7 \u00b5m)"]
-[9.937500953674316, 4.84017276763916, "[TT] Rotation Rate of the MWI = 45 rpm"]
-[11.213521003723145, 0.5948509573936462, "[FF] Mission Objective of the CHEOPS = Study the structure of exoplanets smaller than Saturn and measure the bulk density of super-Earths and Neptunes"]
-[3.450317859649658, -0.5130206942558289, "[TT] Orbital Plane of the Orbital Phase 2 = Moved to the terminator plane"]
-[6.243375301361084, 1.0705201625823975, "[TT] Expected GRB Detections per Year of the GMOD = Approximately 20"]
-[7.920883655548096, 8.488958358764648, "[TT] Spectral Range of the Instrument = 450-700 nm"]
-[9.430991172790527, 2.3229594230651855, "[TT] Blue Jets Percentage of the ISUAL = 13.42%"]
-[7.869388103485107, -2.4606895446777344, "[TT] Observation Target of the GOLD = Earth"]
-[10.136693954467773, 9.995617866516113, "[TT] Launch Date of the Vega = 28 April 2021"]
-[10.528546333312988, 1.0198780298233032, "[TT] Brightness of Star at High Noon of the Kepler-186f = As bright as our sun appears to us about an hour before sunset"]
-[3.7211194038391113, -0.7272105813026428, "[TT] Satellite Type of the WSF-M = Low Earth Orbit (LEO)"]
-[6.550169467926025, 0.31288841366767883, "[TT] Design Life of the Landsat-7 = 5 years"]
-[3.403717279434204, 3.652693748474121, "[FF] Sovereignty of the PAZ and TerraSAR = Independent"]
-[12.802905082702637, 7.588099002838135, "[TT] Power Consumption of the ATLAS instrument = 300 W"]
-[5.581087112426758, 6.8079609870910645, "[TT] Data Processing Capacity of the IDPS = 100 times the volume of legacy data"]
-[8.70969009399414, 7.352502822875977, "[TT] Object Detection Limit of the NEOSSat = 20th V magnitude"]
-[6.426529884338379, 4.883927822113037, "[FF] Function of the ISSAC SOC = Downlink resultant imagery data and transfer to UND for processing and quick delivery to image requestors"]
-[5.117445945739746, 4.0823187828063965, "[FF] Application of the Argos DCS = Sustainable management of marine resources"]
-[5.283377647399902, 0.9280397891998291, "[FF] Flight Status Presentation Date of the IKAROS = Sept. 27-Oct. 1, 2010"]
-[6.860268592834473, -0.45714443922042847, "[TT] Observation Cycle Time of the Solar Orbiter = 3 days"]
-[6.842180252075195, 8.019111633300781, "[TT] Noise Levels (NEDT) of the SSM/T-2 = 0.6 K to 0.8 K"]
-[7.429403305053711, 2.4205832481384277, "[FF] Coverage Area of the Satellite = Varies"]
-[5.509225845336914, -1.8236379623413086, "[TT] Design Life of the KOMPSAT-2 = 3 years"]
-[7.745044708251953, 0.5464773178100586, "[FF] Measurement of the Lunar IceCube = Diurnal variation in OH absorption"]
-[12.026796340942383, 4.732797622680664, "[TT] Envelope of the EXIS = 76 cm x 30 cm x 37 cm"]
-[3.1584312915802, 3.873629331588745, "[FF] Mission Date of the NovaSAR-1 = Sept. 13-14, 2012"]
-[6.903578758239746, 4.4761552810668945, "[FF] Purpose of the RVX FDIR = Ensure continuous monitoring of the RVX GNC and the satellites\u2019 relative state, and prompt response to failures"]
-[5.93686580657959, 0.8366952538490295, "[TT] Image Release Date of the MERIS = Nov. 15, 2013"]
-[3.8780767917633057, 7.8596673011779785, "[TT] Modulation of the X-band transmitter = 16-QAM (Quadrature Amplitude Modulation)"]
-[9.227313041687012, 0.2407645583152771, "[TT] Number of Highway Lanes of the Yavuz Sultan Selim Bridge = 8"]
-[5.625926494598389, 0.4238482713699341, "[TT] Finding Date of the Cluster = 2017"]
-[14.369760513305664, 3.301269054412842, "[TT] Mass of the SDST = 3 kg"]
-[7.777952671051025, 4.969947814941406, "[TT] Use Case of the FLLS = Position-monitoring in PROBA-3"]
-[9.775010108947754, 7.167382717132568, "[TT] Ground Resolutions of the MSR = 32 km and 23 km"]
-[5.024547100067139, 4.166072845458984, "[TT] Signal Processing System of the NorSat-3 = Zynq Ultrascale+ system-on-chip"]
-[10.270127296447754, 8.305625915527344, "[TT] Entrance Pupil Diameter of the Telescope = 104 mm"]
-[8.260467529296875, 7.648010730743408, "[TT] CCDs of the AVNIR = 5,000 and 10,000 detector elements"]
-[4.886586666107178, 7.357953071594238, "[TT] Downlink Data Transmission Rate of the RF = 9600 bit/s"]
-[11.125494956970215, 0.5934329032897949, "[TT] Dynamics Observed of the Transiting Exoplanets = Planet-planet interactions, mutual inclinations, moons, tides"]
-[5.4871087074279785, 7.103024482727051, "[TT] Data Rate of the 1st generation Tesat LCT = 5.6 Gbit/s"]
-[13.055583953857422, 7.275940895080566, "[TT] Power of the Sensor = 2.24 W"]
-[7.796668529510498, -2.5110321044921875, "[FF] Heat Dependence on Time of Day of the GOLD = Stronger effect in the morning hours compared to that in the afternoon"]
-[7.859270095825195, 7.797253131866455, "[TT] No of detectors of the Channel = 4 +4 redundant"]
-[9.878743171691895, 0.8998916745185852, "[TT] Spatial Resolution of the GOSAT-2 = Band 1-3, 500 m(750 \u00b5rad)"]
-[10.507180213928223, 3.3467588424682617, "[FF] Application of the Frontier Radio LT = 3U and larger CubeSat as well as microsatellites"]
-[9.16529369354248, 1.3458679914474487, "[FF] Imaging Date of the New Horizons = July 14, 2015"]
-[8.40594482421875, 1.2125773429870605, "[TT] Quantization levels of the Land surface temperature = 1"]
-[7.311931133270264, 2.186397075653076, "[FF] URL of the Whale Ecology Observation Satellite = http://www2.nict.go.jp/mt/b150/SJR/English/eng12-1/smallsatelliteweose.pdf"]
-[6.434927940368652, 2.8381524085998535, "[TT] Striping of the Constellations = Almost Entirely Removed"]
-[3.458131790161133, 1.9379366636276245, "[FF] Purpose of the Sentinel-6 = Ensure the \u2018continuity of service' of the Jason missions"]
-[12.142694473266602, 1.973480224609375, "[FF] Operational Date of the CartoSat-2B = July 2010"]
-[10.424569129943848, 2.352193832397461, "[FF] Calibration Focus of the Telescope = Bright X-ray sources"]
-[7.149336338043213, 6.457870960235596, "[TT] Response Time of the CuPID = Minutes"]
-[6.165082931518555, 5.763813018798828, "[TT] Information Type of the Analog only sub-experiments = Analog"]
-[3.8494341373443604, 0.913567304611206, "[FF] Launch Date of the PSLV-C45/EMISAT Mission = 1 April 2019"]
-[8.190052032470703, 1.2604371309280396, "[FF] Soil Moisture Data of the SMOS = Unknown"]
-[10.261988639831543, 3.0463948249816895, "[TT] Usable Passes per Day of the ISARA CubeSat = One"]
-[11.004937171936035, 5.633717060089111, "[TT] Thickness of the Dobson Unit = 0.01 mm"]
-[8.681102752685547, 2.011237621307373, "[TT] Wind Speeds of the SeaWinds scatterometer = 3 - 20 m/s"]
-[5.182526111602783, 5.707668304443359, "[TT] Protocol of the Downlink Framer = CCSDS compatible protocol"]
-[8.727700233459473, 0.24706502258777618, "[FF] Size of Mount Doom of the OSIRIS-REx = The size of a small parking lot"]
-[13.403124809265137, 7.371858596801758, "[TT] Power of the TRMM = 1100 W"]
-[5.679365634918213, 1.268095850944519, "[FF] Presentation Date of the MIPAS Instrument = Jan 1999"]
-[7.99209451675415, 3.162692070007324, "[TT] Gases Column Density Retrieval Accuracy of the TANSO-CAI = 1%"]
-[7.06272029876709, 2.0595717430114746, "[FF] Sensor Performance of the Landsat-7 = Not provided"]
-[6.64720344543457, -1.9415204524993896, "[TT] Managing Organization of the Jason-3 = NASA's Jet Propulsion Laboratory in Pasadena, California"]
-[6.2489447593688965, 4.677862167358398, "[FF] Function of the Payload Control = Receive and monitor on-board parameters of the satellite payload and platform"]
-[5.663228988647461, 2.5893795490264893, "[FF] Image Credit of the RADARSAT-2 = NASA/JPL, UCI, ESA, CSA, JAXA"]
-[7.875591278076172, 0.48239508271217346, "[FF] Measurement Unit of the GRACE-FO = Dry Conditions Occur Once Every 50 Years"]
-[6.238335132598877, 1.3543767929077148, "[TT] News Release Date of the NASA Space Laser Missions = 30 April 2020"]
-[9.050189971923828, 5.923583030700684, "[TT] STARE Smear Rate of the ADCS = 0.02\u00ba/s"]
-[14.260003089904785, 3.2781765460968018, "[TT] Mass (kg) of the TecSAR = 300"]
-[8.145485877990723, 1.3610877990722656, "[FF] Purpose of the SMAP = Soil moisture and ocean salinity"]
-[13.600040435791016, 5.491710186004639, "[TT] Solar Cells Manufacturer of the EPS = Emcore"]
-[6.953375816345215, -0.55173659324646, "[TT] LSDN of the SPROUT = Local Sun time on Descending Node"]
-[7.902187824249268, 6.221571445465088, "[TT] Type of the NigeriaSat X Remote Sensing = Imaging multi-spectral radiometers (vis/IR)"]
-[5.229646682739258, 2.851423740386963, "[TT] Funding of the IASI = EUMETSAT"]
-[7.898276329040527, 3.138603687286377, "[TT] Absorption at 1.24 \u00b5m of the Carbon Dioxide (CO2) = 10 -21 mol cm -2"]
-[5.968123435974121, 6.447912216186523, "[TT] Latency of the ATL03 Global Geolocated Photon Data = 21 days"]
-[13.17308235168457, 7.352426052093506, "[TT] Power Consumption of the OBCom module = 50 mW"]
-[4.282131195068359, 2.537914991378784, "[TT] Launch Site of the Starshine-3 = Kodiak Launch Complex on Kodiak Island, Alaska"]
-[3.4231085777282715, 3.9375414848327637, "[FF] NESZ of the TerraSAR-X = Unknown"]
-[10.572724342346191, 6.520862579345703, "[TT] Mirror Modules of the eROSITA = 7"]
-[6.441391944885254, 4.633044719696045, "[FF] Function of the MCE = Mission planning and satellite command, control"]
-[10.1669921875, 5.746720314025879, "[FF] Thermal Model Identification of the Multi-Beam Antenna System = Unknown"]
-[6.877093315124512, 7.806407451629639, "[TT] Diameter of the IOL Antenna Reflectors = 2.85 m"]
-[13.405341148376465, 6.794257640838623, "[TT] Power of the BRITE spacecraft = 5.4 W to 10 W"]
-[6.555915832519531, 4.275349140167236, "[FF] Types of the Data Products = 3-hourly, 6-hourly and daily products"]
-[6.78494930267334, 5.860077381134033, "[TT] Quantity of the AIM = 2"]
-[8.59255599975586, 8.78976058959961, "[TT] Slit 1 Material of the MEGS-A = Mo/C"]
-[9.639159202575684, 7.712520599365234, "[TT] Pixel Size of the Telescope = 24 x 24 \u00b5m"]
-[9.896408081054688, -0.646555483341217, "[TT] Orbit Altitude of the AERO-VISTA mission = Approximately 450 - 600 km"]
-[8.157739639282227, 2.1695544719696045, "[FF] Application of the TEMPEST = Numerical models and characterizing the moisture surrounding tropical cyclones"]
-[1.8006689548492432, -2.0277323722839355, "[TT] Attitude Maneuver of the Hayabusa-2 = Around the Z-axis"]
-[5.008169651031494, 1.0885212421417236, "[TT] Launch Date of the ALOS-2 = May 24, 2014"]
-[4.861009120941162, 2.4622459411621094, "[FF] Delivery Location of the LunaH-Map = NASA's Kennedy Space Center"]
-[4.5095133781433105, 4.196396827697754, "[FF] Operation of the LEOLUTs = With the LEOSAR payloads on the various spacecraft in orbit"]
-[3.873016834259033, 2.1114306449890137, "[TT] Launch Vehicle of the Galileo FOC-3 and FOC-4 satellites = Soyuz-STB/Fregat-MT"]
-[9.69534969329834, 2.3519864082336426, "[FF] Parameter of the NuSTAR = Unknown"]
-[7.951162338256836, 3.349360704421997, "[TT] Instrument Type of the IMAGE = Atmospheric chemistry, Communications, Data collection"]
-[3.0865795612335205, 4.397188663482666, "[TT] Spatial Resolution of the TerraSAR-X NG = Down to 0.25 meters"]
-[9.591227531433105, 1.422519326210022, "[TT] Tasking Rate of the Pl\u00e9iades Neo constellation = Five times higher than previous constellations"]
-[6.828042030334473, 5.1385111808776855, "[FF] House-keeping (HK) Data of the Control Units = Voltage, current, and temperature"]
-[4.99337100982666, 2.9096436500549316, "[TT] Mission Operator of the SPOT 6-7 = Airbus Defence and Space"]
-[6.665948390960693, -0.36480340361595154, "[TT] Repeat Cycle of the HY-2B = 14 days"]
-[7.172677040100098, 5.102232933044434, "[FF] Alignment Performance of the AIT Approach = Achieved through adequate alignment strategies and accuracies"]
-[6.94777774810791, 1.6465797424316406, "[FF] URL of the Webb Telescope = http://www.stsci.edu/jwst/overview/design/deployment.html"]
-[8.074919700622559, 7.614077568054199, "[TT] Cameras of the Hypatia = Sub-meter multispectral and 30 m hyperspectral"]
-[8.594449043273926, 7.44735050201416, "[TT] Threshold of the Imager = < 4.0 J m -2  sr -1"]
-[5.184813976287842, 4.77541971206665, "[TT] Crew Return Time to Earth of the Proving Ground = Matter of days"]
-[6.872256755828857, 5.857795715332031, "[TT] Quantity of the MTM = 2"]
-[10.513813972473145, 2.3673465251922607, "[TT] Intrinsic Temporal Resolution of the X-ray telescopes = Better than 1 \u00b5s"]
-[5.003086090087891, 7.441483497619629, "[TT] NSCAT Data Rate of the RF communications = 2.9 kbit/s"]
-[4.560124397277832, 7.742196559906006, "[TT] Frequency Range of the L-band data transmission = 1.69 - 1.71 GHz"]
-[3.357933759689331, 4.7036519050598145, "[FF] Operational Modes of the SIR-C = ScanSAR and Spotlight"]
-[5.0543413162231445, 0.40659770369529724, "[TT] Deployment Date of the Net = October"]
-[9.978594779968262, -0.5321897268295288, "[TT] Orbit Altitude of the TanSat = ~ 700 km"]
-[8.57394027709961, 2.2692811489105225, "[FF] Purpose of the Plane = Drop lower again to measure wind speed"]
-[9.67959976196289, 4.756716251373291, "[TT] Stabilization of the ROSE-L satellite bus = Three-axis"]
-[11.87952709197998, 3.072261333465576, "[TT] Total Velocity Change of the Propulsion Subsystem = \u0394V = 334 m/s"]
-[8.086446762084961, 8.791621208190918, "[TT] Spectral Range of the SOSP = 170 - 3200 nm"]
-[5.754186630249023, 8.163843154907227, "[TT] Footprint of the Submillimeterwave receiver = 5 m"]
-[3.8429994583129883, 3.427365779876709, "[FF] SAR Service Date of the Galileo = 21 January 2020"]
-[7.787552833557129, 8.981945037841797, "[TT] Wavelength Range of the Visible Spectral Band = 0.55 - 1.05 \u00b5m"]
-[6.400190353393555, 5.76260232925415, "[FF] Execution Time of the Payload basic configuration request = Unknown"]
-[6.203272342681885, 4.651306629180908, "[FF] Functions of the IPACS = Telemetry processing, spacecraft commanding, ground system configuration and management"]
-[5.531962871551514, 2.2073183059692383, "[FF] Affiliation of the K. Kondo, A. Kuze, T. Hamazaki = Unknown"]
-[7.753349304199219, 2.7449862957000732, "[FF] Location of the Observed and simulated features of the CO2 diurnal cycle = Beijing and Hefei, China"]
-[3.545470714569092, 1.644246220588684, "[FF] Conference Date of the Sentinel-3 = 5-9 September 2011"]
-[9.96706771850586, 7.105820655822754, "[FF] Scene Spacing of the SSMIS = 480 km for the earlier instruments, 50 km for the lower atmosphere and 75 km altitude for the upper atmosphere measurements"]
-[8.498773574829102, 1.57248854637146, "[FF] Brightness Temperature Calibration of the Aquarius/SAC-D Microwave Radiometer (MWR) = Unknown"]
-[8.271835327148438, 8.455275535583496, "[TT] Channels of the Spectrometer = 385, 454, 600, 1020, 940, 448, 525 nm"]
-[6.461421966552734, 1.8193970918655396, "[FF] URL of the RASAT = https://en.wikipedia.org/wiki/RASAT"]
-[3.410351037979126, 6.426723480224609, "[TT] Antenna aperture of the Feeder Link = 0.8 m diameter"]
-[7.882920265197754, 8.79175090789795, "[TT] Displacement Range of the Piezo = \u00b16 \u00b5m (\u00b11 arcmin)"]
-[14.312073707580566, 2.9936327934265137, "[TT] Mass of the Philae Lander = 100 kg"]
-[14.302741050720215, 3.2126598358154297, "[TT] Mass of the RMU = 1.6 kg"]
-[5.784258842468262, 7.168391704559326, "[TT] Data Rate of the PEACE = 3.54 kbit/s"]
-[10.392494201660156, 7.630940914154053, "[TT] Instrument Mass of the S-192 optomechanical scanner = 57 kg"]
-[10.191704750061035, 3.1057116985321045, "[FF] Release of the UNISAT-7 = Six smallsats"]
-[9.283784866333008, 6.404151916503906, "[TT] Steps to the next location of the Scan Mirror = Around 20 ms"]
-[9.669955253601074, 1.4028126001358032, "[TT] Availability of the Pleiades System = Close to 100%"]
-[11.040811538696289, 6.07988977432251, "[FF] Sensitivity of the LDEX = Especially sensitive to the metallic compounds of minerals and any species which easily form ions (e.g. water)"]
-[11.829843521118164, 3.276275396347046, "[TT] Thruster Quantity of the GPIM = 5"]
-[9.180672645568848, 8.065583229064941, "[TT] Pixel Format of the Focal Plane Module = 32 x 32"]
-[7.8214497566223145, 9.276666641235352, "[TT] Center Wavelength of the Red edge = 710.0 \u00b5m"]
-[8.405252456665039, 2.8920938968658447, "[FF] Inference of the MSX/UVISI = Atmospheric Refractivity, Bulk Atmospheric Density, Pressure, and Temperature"]
-[6.952048301696777, 7.068643093109131, "[TT] Beam Pair Separation of the ATLAS = 3 km"]
-[6.226343154907227, 0.6750280261039734, "[TT] Launch Date of the Gaia = 2013"]
-[11.000953674316406, 5.774308681488037, "[TT] Al Shielding Thickness of the RADFET Dosimeters = 165 \u00b5m"]
-[6.26539421081543, 4.531818389892578, "[FF] Task of the Automator = Executing the automatized flight operations procedures"]
-[13.192453384399414, 7.622473239898682, "[FF] TWTA of the MPA = Traveling Wave Tube Amplifier"]
-[5.666817665100098, 0.9947781562805176, "[TT] Launch Date of the IBEX = 2008"]
-[11.347078323364258, 4.326612949371338, "[TT] Size of the RSP-00 = 1U"]
-[6.549936771392822, -0.5871782898902893, "[TT] Target Availability of the SPARCS = ~3 months for targets in the ecliptic plane"]
-[12.10682201385498, 6.227005481719971, "[FF] Helium Flux of the AMS = Second most abundant cosmic ray"]
-[7.28402042388916, 5.7917962074279785, "[FF] Detection Thresholds of the RTEP = Adjustable"]
-[8.969147682189941, 7.256114959716797, "[TT] Effective Area of the Observation Instrument = 0.6 cm 2 @ 125 nm"]
-[5.380520343780518, 4.598172187805176, "[TT] Selective Availability (SA) of the GPS = Removed on May 2, 2000"]
-[7.8416571617126465, 6.188414573669434, "[FF] Function of the Colour Imager = Taking snapshots of targets of interest"]
-[7.1842193603515625, 5.1983466148376465, "[TT] Mounting Interface Requirement of the SOSMAG = None"]
-[10.075424194335938, -1.5444411039352417, "[TT] Orbit Inclination of the CanX-2 = 97.4\u00b0"]
-[7.878057956695557, 8.220812797546387, "[TT] Spectral Bands of the EarthDaily Optical Imager = 22"]
-[4.1277055740356445, 0.6102825999259949, "[FF] Clues Date of the INTEGRAL = 14 Nov. 2008"]
-[4.107565879821777, 1.407885193824768, "[FF] Operation Start Date of the Meteosat = June 1986"]
-[5.827652454376221, 7.1630988121032715, "[TT] Parameter of the Data Rate = 1.2 kbit/s"]
-[4.793749809265137, 0.10487289726734161, "[TT] End of Life Date of the RASAT = 28 August 2022"]
-[5.6296892166137695, 2.2825767993927, "[TT] Test Emphasis of the MPO spacecraft = Transient operation"]
-[13.375185012817383, 2.902878522872925, "[TT] Mass of the SkySat-1 = ~100 kg"]
-[5.459074974060059, 0.38857147097587585, "[FF] Extension Date of the International Space Station = April 27, 2023"]
-[5.307229995727539, 1.5741928815841675, "[FF] Calibration Phase of the DEIMOS-2 = Coming days"]
-[11.63448715209961, 3.37945556640625, "[FF] Thruster System of the BeaverCube = Tiled Ionic Liquid Electrospray (TILE 2) thruster system technology, developed and manufactured by Accion Systems, Inc"]
-[7.374878883361816, 0.2783011794090271, "[FF] Sample Stowage of the OSIRIS-REx = Expedited"]
-[8.476037979125977, 3.1201860904693604, "[FF] URL of the Solar Ultraviolet Imager (SUVI) = http://www.goes-r.gov/spacesegment/suvi.html"]
-[7.993078231811523, 2.738121271133423, "[TT] Measurement Category of the GOSAT-2 = Cloud type, amount and cloud top temperature, Atmospheric Temperature Fields, Aerosols, Vegetation, Ozone, Trace gases (excluding ozone)"]
-[8.220484733581543, 4.354863166809082, "[FF] General Relativity Test of the LARES and LAGEOS satellites = Conducted"]
-[5.590586185455322, 1.5501679182052612, "[TT] Initial Electromagnetic Interference Tests Completion Date of the LADEE = November 2012"]
-[4.397166728973389, 0.18720608949661255, "[FF] Error of the Soyuz-2-1b Fregat = Programming error in the upper stage"]
-[7.7150726318359375, 2.6483092308044434, "[FF] Percentage of Global Warming of the CO2 and CH4 = ~90%"]
-[14.084532737731934, 4.044683933258057, "[TT] Instrument Mass of the Instrument = 25 kg"]
-[11.688387870788574, 3.3984591960906982, "[TT] Main Rocket Motor Usage of the Juno spacecraft = Twice"]
-[6.802702903747559, 4.146214485168457, "[FF] Additional Capability of the TRUTHS = Allow multiple angle observations"]
-[8.276646614074707, 2.47589373588562, "[FF] Specific Interest of the PARASOL = Role of clouds and aerosols in climate mechanisms"]
-[8.897961616516113, 4.491774082183838, "[FF] Navigation System of the Resurs-P = Star and sun sensors for attitude data, GLONASS/GPS system for orbital position determination"]
-[14.235350608825684, 3.072688579559326, "[TT] Mass of the SCD-2 = 117 kg"]
-[5.048708438873291, 0.5969802141189575, "[TT] Launch Contract Date of the SpaceIL = October 2015"]
-[5.247812271118164, 5.289837837219238, "[TT] External SRAM of the Namuru V3.2 GPS Receiver = 1 MB"]
-[3.4492347240448, 1.874939203262329, "[FF] Re-use of Electronic Equipment of the Sentinel-5P = From several suppliers"]
-[6.686305522918701, 0.855377733707428, "[FF] DOI of the Herschel = 10.1088/0004-637X/773/2/102"]
-[4.482664585113525, 7.007664680480957, "[FF] Repeater Modes of the Satellite Communications Subsystems = Regenerative repeater mode and bent-pipe repeater mode"]
-[5.988085746765137, 4.620905876159668, "[FF] Communication Systems of the Shelter Room = Mobile data communication system and satellite communication system"]
-[7.890519618988037, 8.28665828704834, "[TT] Infrared Bands of the IMG = 3"]
-[7.811101913452148, 5.485166072845459, "[FF] Purpose of the PLM Proto-Flight Model (PLM-PFM) = Integrates the P/L Flight units on the flight Optical Bench"]
-[5.802860736846924, 2.600799083709717, "[FF] Designers of the CSG End-to-End System Deployment and Calibration = Andrea Gallon, Andrea Francioni, Andrea Gallonalerio Grimani, Fabio Covello, Stefano Serva"]
-[10.486974716186523, 6.643930912017822, "[TT] Number of Mirrors of the Top Dome = 499"]
-[10.28802490234375, 4.687536239624023, "[TT] Ion Velocity Components of the DIDM = Normal and perpendicular"]
-[6.936212062835693, 3.852649450302124, "[FF] Proximity of the POPACS = DANDE"]
-[6.17628812789917, 5.052886486053467, "[FF]  of the ISL = "]
-[5.024314880371094, 2.128573417663574, "[FF] Mission Requirements and Specifications of the GOSAT-2 = Unknown"]
-[10.59707260131836, 3.409160852432251, "[TT] Design Standard of the Neutron-1 = 3U CubeSat standard"]
-[4.677860260009766, 7.103734016418457, "[TT] Downlink Rate of the X-band = 60 Mbit/s"]
-[4.522697448730469, 1.3743008375167847, "[FF] Applications of the AlSat-2 = Cartography, agricultural management, crop monitoring, disaster management"]
-[5.8596343994140625, -0.6989820003509521, "[TT] Design Lifetime of the SPOT satellite constellation = 3 years"]
-[3.68717098236084, 5.183279991149902, "[TT] Azimuth Resolution of the Radar = 1500 m"]
-[5.662882328033447, 1.3956592082977295, "[TT] Magnetometer Installation Date of the Iridium Constellation Satellites = February 1999"]
-[14.662043571472168, 6.66006326675415, "[TT] Capacity of the Battery = 9 Ah"]
-[9.12397289276123, -0.3523353040218353, "[FF] Trajectory of the Periselene-1 = One loop around the Earth with perigee > 100,000 km altitude"]
-[5.939736843109131, -0.28863707184791565, "[TT] Structural Qualification Time of the SSTL-300 S1 = 24 months"]
-[9.619779586791992, 5.052106857299805, "[TT] Drag Profile of the AC4-B = Larger"]
-[3.8143911361694336, -1.1353580951690674, "[TT] Orbit of the LPF Spacecraft = L1"]
-[9.53138256072998, 4.756981372833252, "[TT] Attitude Control of the ADCS = 3-axis stabilization"]
-[5.97847843170166, 5.006258964538574, "[FF] Protocol of the OBC = CSP (CubeSat Space Protocol)"]
-[8.75500774383545, 7.871318817138672, "[TT] Earth Rotation Effect of the Band-64 = Limit to about 0.1 pixels"]
-[6.094357490539551, 8.567276954650879, "[TT] Antenna Polarization of the DRS = Dual"]
-[3.4139773845672607, 6.411118984222412, "[TT] Length of the DSX Y antenna = 80 m"]
-[5.605883598327637, 4.614208698272705, "[TT] Program of the EDRS = ARTES-7 (Advanced Research in Telecommunications Systems)"]
-[8.283079147338867, 7.934485912322998, "[TT] Material of the SWIR Detector = HgCdTe"]
-[10.210780143737793, 2.432976722717285, "[FF] Mission of the ART-XC Instrument = Spectrum-Roentgen-Gamma"]
-[3.6127676963806152, 5.126924514770508, "[TT] Ground Range Resolution of the Radar = Approximately 250 m"]
-[9.077067375183105, 4.791478633880615, "[FF] Attitude Determination and Control Subsystem Calibration of the Spacecraft = Ongoing"]
-[8.22747802734375, 1.4526383876800537, "[FF] Climate of the Tenerife = Heavily influenced by the trade winds blowing from the northeast for most of the year"]
-[9.201910018920898, 7.055006980895996, "[TT] Resolution Improvement of the EIS = 100 times better"]
-[6.76198148727417, -0.4227762222290039, "[TT] S-band Transmitter Activation Time of the Satellite = 30 minutes after separation"]
-[4.626996994018555, 6.920670986175537, "[TT] Command Uplink of the Aleph-1 satellites = S-band"]
-[6.813934326171875, 5.0364580154418945, "[FF] Operation of the DPCA = Detects moving targets in the differential data"]
-[6.621744632720947, 4.969404220581055, "[FF] Function of the PGSC = Control and command"]
-[7.867224216461182, 6.747470378875732, "[FF] Operation of the CCD Readout = Vertical shift of the image rows"]
-[9.844902038574219, 7.942560195922852, "[TT] FMC Mode Rotation Speed of the Telescope = 1.5\u00ba/s"]
-[10.216428756713867, -0.4518451690673828, "[FF] Altitude of the LLITED CubeSat = Lower altitudes"]
-[10.474624633789062, 1.7438857555389404, "[FF] Expected Frequency of Outbursts of the Black Hole = Rarely"]
-[5.041165351867676, -0.4573323726654053, "[TT] Separation Time from Launch Vehicle of the Mey-Lin (C6), Gaspard (C7), and Oc\u00e9ane (C8) = Around 63 minutes"]
-[6.747422218322754, -0.3305542469024658, "[TT] Period of the Capella's Satellites = 90 minutes"]
-[9.758801460266113, 7.460160255432129, "[TT] Ground Sample Distance (GSD) of the Optical Sensor (OPS) = 0.5 m"]
-[14.262381553649902, 3.2547271251678467, "[TT] Mass of the HEPD = 2.2 kg"]
-[8.027291297912598, 8.265863418579102, "[FF] Emission Lines of the EUVI = Four EUV emission lines between 17.1 and 30.4 nm"]
-[6.456629276275635, -0.028779814019799232, "[TT] Observation Period of the ASTERIA = 20 minutes"]
-[5.001466274261475, 3.420827627182007, "[TT] Manufacturer of the DECA = OIP (Optique et Instruments de Pr\u00e9cision)"]
-[13.579057693481445, 2.797888994216919, "[FF] Launch Vehicle Utilization of the PODSat = Excessive capacity on launch vehicles delivering a primary payload to geostationary orbit"]
-[5.781863689422607, 1.3731470108032227, "[FF] Conference Date of the GPS Receivers = August 13-16 2007"]
-[6.593778610229492, 0.8757458925247192, "[FF] High Agility of the FormoSat-2 = Unknown"]
-[7.878181457519531, -0.3543446660041809, "[FF] Article Date of the Small Water Ice Reservoirs = 26 October 2020"]
-[9.230478286743164, -0.6515739560127258, "[TT] Orbit of the MKS-PN2 (Relek) = Elliptical orbit of 632 km x 824 km"]
-[4.402648448944092, 4.216212272644043, "[TT] Number of MCCs of the LEOSAR = 31"]
-[8.056413650512695, 9.277061462402344, "[TT] Wavelength of the Hydrated silicates = 3-3.5 \u00b5m"]
-[5.491635799407959, 3.857241153717041, "[TT] Number of Satellite Operators of the Neosat = 6"]
-[5.3129119873046875, 1.2597715854644775, "[FF] Launch Date of the ABEX = Unknown"]
-[3.426988363265991, -0.8844082951545715, "[TT] Orbit of the NorSat-3 = 550-650 km sun synchronous"]
-[5.445426940917969, 6.5103912353515625, "[TT] On-board Storage Capacity of the ALOS-3 = Greater than 200 Gbit"]
-[8.113301277160645, 8.549463272094727, "[TT] Spectral Range of the HySI = 400-950 nm (VNIR)"]
-[7.2396087646484375, 2.9048216342926025, "[FF] References of the GeoSTAR-III = Observation of the Earth and Its Environment: Survey of Missions and Sensors"]
-[7.825892448425293, 5.6687541007995605, "[FF] Imaging Sensor of the ResourceSat-2 = LISS-3"]
-[5.077937602996826, 4.090904235839844, "[TT] Bus of the NorSat-3 = NEMO bus from UTIAS/SFL"]
-[9.225186347961426, 6.9148736000061035, "[TT] Spatial Resolution of the PROBA-V = 100 m"]
-[7.150225639343262, 6.541840076446533, "[TT] Maneuver Execution Time (60 minute window) of the RASP = 176.7 minutes"]
-[14.242904663085938, 3.118337392807007, "[TT] Mass of the PSat-2 = 2 kg"]
-[9.405692100524902, -0.30385124683380127, "[TT] Earth Parking Orbit of the Chandrayaan-2 = 170 km x 45,475 km"]
-[4.175839900970459, 4.289780139923096, "[FF] Issue 21 Date of the Cospas-Sarsat Information Bulletin = Feb. 2009"]
-[13.881757736206055, 2.7497594356536865, "[TT] Launch Mass of the ACTS/TOS = 2800 kg"]
-[7.5427703857421875, 4.570474624633789, "[FF] Sensor Units of the SEM-2 = TED, MEPED, HEPAD"]
-[3.4073305130004883, 1.905897855758667, "[TT] Orbital Plane of the Sentinel-1A and Sentinel-1B = Same"]
-[9.015771865844727, 6.4735941886901855, "[TT] Crater Location of the CaSSIS camera = 134\u00b012'13.0\"W/43\u00b014'59.7\"N"]
-[4.939208984375, 1.5054129362106323, "[TT] Data Production Start Date of the Tatiana-2 = Early January 2010"]
-[5.765834808349609, 4.965720176696777, "[FF] Connector Type of the Satellite = Second connector provides access to the battery and charging circuitry"]
-[8.511631965637207, 1.7919787168502808, "[TT] Ocean Current Speed Accuracy of the Satellite System = 0.2 m/s"]
-[10.871988296508789, 7.578238010406494, "[TT] Swath Width of the ATM = 200 m"]
-[3.4309654235839844, -0.8919491767883301, "[TT] Orbit of the MOST = Sun-synchronous orbit of 820 km near-circular altitude"]
-[8.329951286315918, 3.29144287109375, "[FF] Purpose of the Improved Limb Atmospheric Spectrometer-II (ILAS-II) = Earth observation"]
-[6.718808174133301, 4.625888824462891, "[FF] Purpose of the Product Monitoring = Identify anomalies in the instrument data"]
-[10.143954277038574, 4.518462181091309, "[TT] Actuators of the AODCS = Four reaction wheels and three magnetorquers"]
-[12.09899616241455, 4.521421909332275, "[TT] Size of the Satellite = 35.7 x 36.2 x 15.8 cm"]
-[9.579516410827637, 7.662781715393066, "[TT] Image Scale of the Galileo = 1.6 km/pixel"]
-[4.02072286605835, 4.250491619110107, "[FF] Data Uses of the RADARSAT-1 = Disaster management, interferometry, agriculture, cartography, hydrology, forestry, oceanography, ice studies and coastal monitoring"]
-[8.350749015808105, 2.798372983932495, "[TT] Measurement Domain of the Myriade/AstroSat-100 = Atmosphere, Gravity and Magnetic Fields"]
-[4.538076877593994, 1.5885530710220337, "[TT] Data Set Release Date of the GEOSAT = June 1997"]
-[4.568912506103516, 5.931647300720215, "[TT] Transmission Power of the 406 MHz beacons = 5 W"]
-[9.33602523803711, 6.712985038757324, "[TT] Resolution of the EarthDaily Constellation = 5-metre"]
-[8.70666790008545, 2.6702773571014404, "[TT] Accuracy of Atmospheric Temperature Profiles of the CrIMSS = 1 K"]
-[6.43851375579834, 5.00793981552124, "[FF] Data Rate Control of the MIU = Based on commands from the FC"]
-[14.174607276916504, 3.292527437210083, "[TT] Mass of the CSSWE = 3.5 kg"]
-[5.898052215576172, 8.112932205200195, "[TT] Beam size of the Millimeterwave receiver = 22 arcmin"]
-[6.524815082550049, 5.040763854980469, "[FF] Function of the DPCC = Process forward tasking data request"]
-[4.75712251663208, 0.3242946267127991, "[TT] Launch Date of the HyperScout = 2 February 2018"]
-[5.467957973480225, 6.976658821105957, "[TT] Speed of the SDR-VSAT = 622 Mbit/s"]
-[13.82505989074707, 6.532150745391846, "[FF] Fuse of the Power line = To protect the circuit from the overcurrent"]
-[10.805383682250977, -0.25298550724983215, "[TT] Horizontal Baseline of the TanDEM-X = 200 m to 3000 m"]
-[14.63888168334961, 6.757314682006836, "[TT] Battery pack capacity of the EPS = 3.6 Ah"]
-[9.423811912536621, 7.110962390899658, "[TT] Spatial Resolution (km) of the VIRR = 2280"]
-[13.079399108886719, 7.647924900054932, "[TT] Power Capacity of the AlSat-2 = Up to 50 W"]
-[4.6482768058776855, 0.6273084282875061, "[TT] Development Timeline of the EPS-MACCS = From kick-off to launch within three years"]
-[3.2801570892333984, 3.9132747650146484, "[FF] Formation Control of the TerraSAR-X = Yes"]
-[9.0213041305542, 5.566230297088623, "[TT] Pointing Adjustment Time of the ACS = About 30 s"]
-[3.8541483879089355, 4.4908270835876465, "[TT] Percentage of Availability of the RADARSAT-2 = 99.95%"]
-[10.949586868286133, 4.72550106048584, "[TT] Type of the Tethered System = Momentum-exchange"]
-[14.339744567871094, 2.9754467010498047, "[TT] Mass of the Global-5 = 55 kg"]
-[4.927574157714844, -2.136431932449341, "[TT] Launch Mass of the Chang'e-2 = About 2480 kg"]
-[10.173099517822266, 5.565277099609375, "[FF] Thermal Isolation of the Telescope, Batteries, Interface Board = Thermally isolated from the bottom plate"]
-[3.9441616535186768, 6.514645099639893, "[FF] Antenna Type of the Tandem-L = Digital radar antenna"]
-[9.687800407409668, 0.12040121108293533, "[TT] Number of Drogue Parachutes of the Parachute System = 2"]
-[8.464516639709473, 2.3309407234191895, "[FF] Data of the Aeolus = Profiles of Earth's wind on a global scale"]
-[6.07362174987793, 0.8677008748054504, "[TT] Detection Date of the GRB 031203 = 3 December 2003"]
-[5.075884819030762, 8.618410110473633, "[FF] Center Frequency of the Channel = 37.3 \u03bd, h"]
-[8.02049732208252, 8.653127670288086, "[TT] Spectral range of the SBUS = 250-340 nm"]
-[11.8443603515625, 0.03488381952047348, "[FF] Purpose of the TESS Extended Missions = Provide much tighter constraints on planet in-spiral"]
-[7.608851909637451, -0.3465729057788849, "[TT] Event Name of the IceCube Neutrino Observatory = IceCube-170922A"]
-[6.8986897468566895, 3.2972590923309326, "[FF] Purpose of the Rodent Research Habitats (AEM-X) = Used during Rodent Research missions"]
-[4.784814357757568, 5.597434997558594, "[FF] Usage of the Doppler Velocity Sensor = Terminal landing phase"]
-[8.663578987121582, 4.7377753257751465, "[FF] Flash Rate of the Starshine = Once per 15 seconds to once or twice per pass"]
-[7.19384765625, 5.108036041259766, "[FF] Modes of Operation of the ISUAL instrument = Sprite continuous mode, sprite burst mode, auroral mode"]
-[9.487604141235352, 7.066933631896973, "[TT] Spatial Resolution of the TopSAR narrow = 30 - 50 m"]
-[9.275588035583496, 6.939552307128906, "[TT] Resolution of the HRMX = 2 m"]
-[8.057650566101074, 9.09582805633545, "[TT] Observation Wavelength of the NACO = 3.6 \u00b5m"]
-[8.620264053344727, 5.655062675476074, "[TT] Location Accuracy of the NSCAT = 25 km (rms), absolute 10 km (rms)"]
-[9.734332084655762, -0.6332935690879822, "[TT] Orbit Altitude of the HORYU-4 = ~575 km"]
-[10.145166397094727, 6.953741550445557, "[TT] Footprint of the Sounder = 10 km x 40 km"]
-[8.980371475219727, -0.5385070443153381, "[TT] Orbit Perigee of the P35 series = 488 km"]
-[10.85322380065918, 2.114128351211548, "[FF] Catalog Use of the XMM-Newton = Get new information about their research objects and to search for rare and as yet unknown sources of X-rays"]
-[7.161144256591797, 5.178962230682373, "[TT] Mounting of the HETG = Concurrent"]
-[9.305818557739258, -0.768902063369751, "[TT] Orbit of the Trisat-R = LEO (~ 5900 km)"]
-[11.709468841552734, 3.4614980220794678, "[TT] Quantity of the Resistojet \u00b5QCT valve = 1"]
-[14.279834747314453, 3.1673054695129395, "[TT] Mass of the S/C = 195 kg"]
-[7.2202043533325195, 2.9212286472320557, "[FF] Application of the GeoSTAR = Detect and track hurricanes and other severe storms"]
-[5.042609691619873, 1.0404094457626343, "[FF] Communication Recovery Efforts of the Hitomi = Ongoing"]
-[7.8656840324401855, 8.937911987304688, "[TT] Wavelength Range of the Instrument = 115-180 nm"]
-[8.828468322753906, 3.553745985031128, "[FF] Design and Operation of the Tiny Ionospheric Photometer (TIP) = Not provided"]
-[5.174121379852295, 6.9613776206970215, "[TT] Download Transmission Rate of the DubaiSat-1 = 30 Mbit/s"]
-[10.480535507202148, 3.274528980255127, "[TT] VPU Cores of the Ubotica CogniSAT-XE1TM CubeSat Board = 12 vector cores"]
-[9.547478675842285, 7.305582046508789, "[TT] Radiometric resolution of the S-band = 1.5 K"]
-[8.533636093139648, 7.302217483520508, "[TT] Time Resolution of the Particle Detector = 1 s"]
-[5.547740459442139, 4.571012020111084, "[FF] Communication Status of the MarCO = Silent"]
-[7.072975158691406, 1.240977168083191, "[FF] Mission of the ERO = Bring samples back to Earth from Mars"]
-[13.746419906616211, 2.910660743713379, "[TT] Mass of the Spacecraft = 2120 kg"]
-[7.220207691192627, 2.8047802448272705, "[FF] Critical Design Review Completion Date of the MethaneSAT = 21 September 2020"]
-[9.029635429382324, 7.665536403656006, "[FF] Payload of the Planet Satellite = Telescope and a frame CCD camera equipped with Bayer-mask filter"]
-[8.159899711608887, -1.1361640691757202, "[FF] Melt Pond Size of the ICESat-2 = As big as Olympic-sized swimming pools, or bigger"]
-[5.354086875915527, 5.014383316040039, "[FF] GPS Receiver of the BEESAT-4 = Phoenix"]
-[6.262362003326416, 3.2773756980895996, "[TT] Planned Number of Satellites of the BlackSky = 8 by year\u2019s end"]
-[8.631200790405273, 5.6690521240234375, "[TT] Positioning Precision of the Galileo = Meter-scale"]
-[7.467601776123047, 3.322138786315918, "[FF] Experiment of the IRT Saint Exup\u00e9ry = Using a form of artificial intelligence called \u2018deep learning\u2019 to recognize patterns such as cloud formations or fires on Earth"]
-[9.643235206604004, 4.004177093505859, "[TT] Magnitude Stability of the Magnetic Field = < 0.12 nT over 3 months"]
-[8.511988639831543, 5.338449001312256, "[TT] Position Accuracy (RMS orbit) of the S-3 NTC = 3 cm threshold with a target of 2 cm (radial)"]
-[6.114639759063721, 5.145929336547852, "[FF] Reset Function of the PIC (Peripheral Interface Controller) = Can be performed automatically or manually"]
-[10.376261711120605, 8.071256637573242, "[TT] Telescope Diameter of the Millimeterwave receiver = 30 cm"]
-[4.495394706726074, 6.166689872741699, "[TT] Radio Frequency Interference of the MIRAS = Present"]
-[10.978182792663574, 7.562854766845703, "[FF] Swath of the HISUI = Narrow"]
-[8.561502456665039, 7.714155197143555, "[TT] Detector Array of the LWIR Camera = HgCdTe detector array of 128 x 128 pixels"]
-[10.36925983428955, 3.9658360481262207, "[TT] Coarse Stabilization of the S/C = Gravity gradient boom (actuator, 6 m long)"]
-[7.117447376251221, 4.884142875671387, "[FF] Hardware of the Sentinel-2 MSI = SiC"]
-[4.639274597167969, 7.082494258880615, "[TT] Downlink Transmission of the CBERS-1 = X-band"]
-[12.092325210571289, 6.353033065795898, "[TT] Electron Flux Measurement of the AMS-02 = Up to 750 GeV"]
-[7.447414875030518, -0.17269854247570038, "[TT] Operation Time on Primary Batteries of the Philae = Approximately 5 days"]
-[7.071349143981934, 3.756394624710083, "[FF] Formation Flying of the PROBA-3 = Yes"]
-[10.077946662902832, -1.524381160736084, "[TT] Orbit Inclination of the Landsat-9 = 98.2\u00b0"]
-[9.507506370544434, 0.6867259740829468, "[TT] Maximum Range of the ARTEMIS = 1.5 million km"]
-[5.899716377258301, 0.5634064078330994, "[FF] Data Collection Performance Assessment Date of the Hyperion = March 9-16, 2002"]
-[6.5738091468811035, 0.15111970901489258, "[TT] Mission Duration of the CryoSat-2 = October 2010 to April 2013"]
-[5.48884916305542, 7.102263450622559, "[TT] Ground Monitoring Data Rate of the EROS-A = 2.5 or 15 kbit/s"]
-[7.802720546722412, 5.187881946563721, "[FF] Training Data of the Machine Learning Algorithm = Images from sounding rocket calibration flights"]
-[6.270622730255127, 8.05440616607666, "[TT] UART Channels of the CSI = 4"]
-[6.030006408691406, 5.921780586242676, "[TT] Configuration Bitstream Source of the V5QV FPGA = PROMs"]
-[13.482691764831543, 5.688589096069336, "[FF] Power Source of the Spacecraft Bus = Six solar panels in two wings, with two Lithium-ion batteries"]
-[5.226203918457031, -0.04601489007472992, "[TT] Launch Date of the Tsubame = November 6, 2014"]
-[8.17595386505127, 1.2016067504882812, "[FF] Potential Impact of the SMAP = Improve the accuracy of the soil moisture characterization in the Air Force systems"]
-[4.260593414306641, 4.340315818786621, "[TT] Persons Rescued of the COSPAS-SARSAT system = Over 27,000"]
-[5.943222999572754, 2.4375312328338623, "[TT] Launch Year of the WorldView Legion = 2021"]
-[6.707903861999512, 4.8236541748046875, "[FF] Interface Handling of the CCB = Towards the spacecraft, housekeeping data acquisition, automatic image data acquisition & processing, execution of autonomous measurement sequences"]
-[8.999330520629883, 8.51306438446045, "[TT] Spectral Range of the Telescope = 0.5 - 0.9 \u00b5m"]
-[10.577239990234375, 6.595971584320068, "[TT] Mirror Shells per Module of the ART-XC = 28"]
-[4.317970275878906, 1.2583037614822388, "[FF] Launch Date of the SEOSAT-Ingenio = November"]
-[8.613710403442383, 3.670478343963623, "[FF] Measurement of the ILAS-II = Resolves solar light into spectra"]
-[3.1641650199890137, 3.8910205364227295, "[TT] Launch Date of the GEOSAR GOES-7 = Feb. 26, 1987"]
-[10.978397369384766, 7.632565021514893, "[TT] Swath Width for Regular Corresponding Mode of the Wide ultra fine = 20 km"]
-[10.232553482055664, 5.798182487487793, "[TT] NEDT (Noise Equivalent Differential Temperature) at 300 K of the Scanning geometry = Band 4 - Band 5 - Band 6 \u2264 1 K \u2264 0.2 K \u2264 0.2 K"]
-[3.8704264163970947, 3.3905727863311768, "[FF] Return Link Delivery Time of the Galileo = A couple of minutes in the majority of cases, up to 30 minutes maximum"]
-[7.963863372802734, 8.154300689697266, "[TT] Spectral Scans of the ISEE-3 = Two per second"]
-[7.433067798614502, 3.7875313758850098, "[FF] On-orbit reference standard for calibrating precipitation measurements of the GMI = Unknown"]
-[6.982149600982666, 4.052804470062256, "[FF] Formation Flying Algorithms of the Formation Flying Computer = Runs"]
-[9.335665702819824, 0.8813129663467407, "[TT] Closest Approach to the Sun of the Parker Solar Probe = Within 4 million miles"]
-[9.078598022460938, 7.092350482940674, "[TT] Image Resolution of the Chang'e-2 = 10 m per pixel"]
-[8.550365447998047, 7.313958168029785, "[TT] Quantity of the VBS (Vision Based Sensor) = 8+8"]
-[7.585987567901611, 3.464838981628418, "[TT] Debris-Capture Materials of the DSAT-2 = Bag or net"]
-[6.911484718322754, 7.4982757568359375, "[TT] Electronic Outputs Resolution of the SEVIRI = 10 bit"]
-[8.58061408996582, 1.920615792274475, "[TT] Quantization levels of the Ocean surface wind speed = 1"]
-[6.986589431762695, 6.179118633270264, "[TT] Number of Instruments of the ISIM = 4"]
-[12.19041633605957, -0.24075067043304443, "[TT] Imaging Duration of the TESS = Nearly a month"]
-[5.419554710388184, 6.723652362823486, "[TT] Transfer Method of the KPLO = WSB/BLT (Weak Stability Boundary/Ballistic Lunar Transfer)"]
-[6.332623481750488, 5.878726005554199, "[FF] Detector of the skCUBE = Very-low-frequency radio waves"]
-[4.950094223022461, 0.8296449184417725, "[FF] Manifestation Date of the HICO and RAIDS = Spring of 2007"]
-[5.382653713226318, -0.22553302347660065, "[TT] Recovery Date of the Block 5D-1 = A few months later"]
-[5.773568630218506, 7.150280952453613, "[TT] Data Rate of the COCTS = 670 kbit/s"]
-[5.678036212921143, 0.6398972272872925, "[FF] Observation Date of the Space Shuttle = January 2005"]
-[13.216567993164062, 7.279128074645996, "[TT] Power Consumption of the CMG = 3 W (peak)"]
-[4.702864170074463, -1.7501909732818604, "[FF] Photogrammetric Processing of the Chang'e-2 = Rigorous"]
-[3.336752414703369, 2.3592193126678467, "[TT] Budget Allocation of the Copernicus = 4.81 billion euros"]
-[7.406985282897949, 8.829042434692383, "[TT] Filter Thickness of the FUV channel = 2.50 mm"]
-[5.531125545501709, -1.8561006784439087, "[TT] Operation Start Date of the KOMPSAT-3 = September"]
-[13.358098030090332, 7.325892925262451, "[TT] Power of the POLDER = 42 W"]
-[5.822147369384766, 2.9992642402648926, "[FF] Strategy of the NASA = Partner with private industry to assist in the development of private industry transportation services, and then to directly contract for resupply and return transportation services after these designs have proven reliable"]
-[10.255105972290039, 1.6299877166748047, "[FF] Observation Results of the eROSITA = Catalogues of millions of exotic celestial objects such as black holes, galaxy clusters, neutron stars, supernovae and active stars"]
-[7.658792018890381, 0.6590114235877991, "[FF] Objective of the Lunar Flashlight = Look for ice deposits and identify locations where resources may be extracted from the lunar surface"]
-[6.832918643951416, 1.1972960233688354, "[FF] Meeting Date of the Solar Radiation and Climate Experiment (SORCE) = Nov./Dec. 2000"]
-[4.769403457641602, 7.971036434173584, "[TT] 1236.5 / 1278.5 MHz of the Frequency = -"]
-[8.151725769042969, 0.09927556663751602, "[TT] Launch Date of the Meteor-M-1 = Sept. 17, 2009"]
-[9.669179916381836, -0.43310195207595825, "[TT] Altitude of the HY-1D = 780 km"]
-[6.017705917358398, 2.4950456619262695, "[FF] Developers of the Tool = Spatial data scientists from the University of St Andrews in Scotland in collaboration with researchers from the British Geological Survey and Canada\u2019s University of Western Ontario"]
-[5.719906330108643, 2.076658010482788, "[TT] Technology Readiness Level of the DSAC = 5 to 7"]
-[6.907893180847168, -1.7654463052749634, "[TT] Significant wave Height of the Jason-2 = 50 cm or 10%"]
-[14.642033576965332, 6.769694805145264, "[TT] Battery Capacity of the EPS = 14.4 Ah"]
-[7.731044769287109, 5.208457946777344, "[FF] Integration of the OB = Instruments are calibrated as stand alone, and once integrated in the OB, an intercalibration and system verification is carried out"]
-[4.954176902770996, 2.397284984588623, "[FF] URL of the Eutelsat Quantum = https://news.eutelsat.com/pressreleases/universal-eutelsat-quantum-satellite-to-revolutionise-telecoms-markets-1190652"]
-[5.730905532836914, 2.02364444732666, "[TT] Recovery Location of the Orion = Pacific Ocean"]
-[4.551714897155762, 5.881464004516602, "[FF] Function of the Transparent Repeater Instruments = Relay 406 MHz beacon signals"]
-[8.289693832397461, 4.185721397399902, "[FF] Purpose of the Gasket = Create a light-tight seal"]
-[10.435457229614258, 2.1625330448150635, "[FF] X-ray Study of the XMM-Newton observatory = Low-energy X-rays from Jupiter's auroras"]
-[5.37123441696167, 1.65516996383667, "[FF] Planned Mission Advantages of the ALOS-2 = Unknown"]
-[5.913125514984131, 0.5308982133865356, "[TT] Observation Period of the MOMS-2P = May 5, 1996 to August 1999"]
-[5.085197925567627, 1.9753340482711792, "[TT] Mission Status of the OCO-3 = Operational (nominal)"]
-[11.817560195922852, 3.265038013458252, "[TT] Main Engine Thrust of the ExoMars TGO = 424 N"]
-[7.346889972686768, 1.9012929201126099, "[FF] Microbe Types of the Experiment = Halorubrum chaoviatoris and Bacillus subtilis"]
-[7.884218215942383, 5.24081563949585, "[FF] Reference Frames of the FLLS = OHU boresight frame, alignment frame of FLLS"]
-[14.219991683959961, 3.3738646507263184, "[TT] Weight of the PowerCell = 4.3 kg"]
-[9.943169593811035, -0.19965310394763947, "[TT] Re-entry Altitude of the Starshine = 80 km"]
-[7.49759578704834, 1.333279013633728, "[FF] URL of the SWIM = http://smsc.cnes.fr/CFOSAT/GP_swim.htm"]
-[10.201117515563965, 1.5393925905227661, "[FF] Energy Release of the Ophiuchus Galaxy Cluster = Factor of five more than the previous record holder"]
-[6.096271514892578, 2.0160396099090576, "[TT] Mission Proposal Year of the Euclid = 2007"]
-[13.599976539611816, 1.851732611656189, "[TT] Cargo Capacity of the Cygnus cargo ship = 3,356 kg"]
-[3.8440613746643066, 7.907314777374268, "[TT] Modulation of the OBP (Onboard Processor) = 35 k symbol/s, \u03c0/4 QPSK"]
-[8.854357719421387, 4.516366958618164, "[FF] Modes of the SC-GNC = High accuracy inertial pointing, target pointing and safe sun pointing"]
-[5.198408126831055, 0.43490472435951233, "[FF] Launch Date of the EyeSat = 2019"]
-[4.97076940536499, 3.632173776626587, "[TT] Manufacturer of the AMERGINT softFEP-9000 modem = AMERGINT"]
-[9.700940132141113, 6.925821781158447, "[TT] Spatial Resolution of the AGRI = 0.5-4 km"]
-[11.822494506835938, 3.657195568084717, "[TT] Dimensions of the Ion Thruster = Diameter of 180 mm x 200 mm long"]
-[7.444034576416016, 4.400540351867676, "[FF] Monitoring Method of the Bioburden Monitoring System = Essays taken at regular intervals"]
-[11.410931587219238, 4.419083118438721, "[TT] Size of the OSIRIS = 3U"]
-[14.087986946105957, 4.039694309234619, "[TT] Mass of the Instrument = 27.7 kg"]
-[8.39916706085205, 7.73386287689209, "[TT] Detector of the Spectral Band B = Si-PIN"]
-[6.290877819061279, 4.018546104431152, "[FF] Mission Programming of the VEN\u00b5S = Unknown"]
-[9.064404487609863, 4.8985490798950195, "[TT] Absolute Solar Shape Precision of the Instrument = Better than 10 marcsec (milli-arcseconds)"]
-[8.534445762634277, 7.866316318511963, "[TT] Number of Detector Pixels of the Long Wavelength Band = 512 x 512"]
-[8.825702667236328, 3.362591028213501, "[FF] Path Dependency of the Radio Waves = Ionosphere Density"]
-[6.38798713684082, 2.028684616088867, "[FF] URL of the Space Data Highway = https://www.airbus.com/en/products-services/defence/connectivity/space-data-highway"]
-[5.849590301513672, -0.8126110434532166, "[TT] Mission Design Life of the LEOStar-3 = 3 years with a 5 year goal; 7 years of propellant available"]
-[9.612031936645508, 4.6693949699401855, "[TT] Control Systems of the AVUM = RACS (Roll and Attitude Control System) and the LPS (Liquid Propulsion System)"]
-[9.541041374206543, 0.6912082433700562, "[TT] Maximum Range of the ARTEMIS = 1.2 million km"]
-[5.304704666137695, 2.195131301879883, "[TT] Mission Status of the NuSTAR = Operational"]
-[4.565246105194092, 6.545422554016113, "[TT] RF Communications of the Spacecraft = 437.365 MHz"]
-[10.459278106689453, 1.6796902418136597, "[FF] Cause of the ASASSN-14ko = Supermassive black hole at the galaxy\u2019s center creates the bursts as it partially consumes an orbiting giant star"]
-[9.831165313720703, -0.4100019335746765, "[TT] Location of the S-6 LRA = Nadir plate of the satellite close to the center of gravity"]
-[7.425370693206787, 2.609590768814087, "[FF] Platform of the InnoSat = Mesospheric Tomography and Spectroscopy"]
-[14.172218322753906, 3.2135534286499023, "[TT] Mass of the LEID = 3.1 kg"]
-[4.643405914306641, 6.389699935913086, "[TT] Source of the RF MMICs = Indigenous"]
-[3.5527052879333496, 5.536550521850586, "[TT] PRF of the SAR = 3500 Hz \u00b1 200 Hz 3000 Hz \u00b1 200 Hz 3000 Hz \u00b1 200 Hz 3000 Hz \u00b1 200 Hz"]
-[5.125884532928467, -0.5911062359809875, "[FF] Mission Date of the TARANIS = Aug. 13-21, 2011"]
-[8.529031753540039, 8.176572799682617, "[TT] TDI Stage of the VNIR FPA = 1 for 2 lines, 2 additional lines for pixel deselection"]
-[18.797670364379883, 3.4797985553741455, "[TT] Mean \u0394E (m) of the Dyess = 2.4"]
-[14.021459579467773, 4.157745838165283, "[TT] Instrument Mass of the Spectral bands = 114 kg"]
-[10.634953498840332, 3.923339605331421, "[TT] Deployment Date of the Dragsail = 4 March 2019"]
-[8.533302307128906, 8.61458969116211, "[TT] F Number of the Prism Spectrometer = 3.0"]
-[5.6699538230896, 5.643533229827881, "[TT] Microprocessor of the ADCS Mainboard = STM32 L4"]
-[5.935141086578369, 5.1835222244262695, "[TT] Onboard Network of the JWST Avionics = FPE (Focal Plane Electronics)"]
-[8.104585647583008, 5.147778034210205, "[FF] Calibration Procedure of the Radiometer System = Shutter of both channels closed, reference power source applied to one heater, and servo-system used to adjust the power applied to the other until heat flux balance is achieved"]
-[3.4331533908843994, 4.968818187713623, "[FF] Polarimetric Observation Technique of the ALOS-2 = Compact (or hybrid) polarimetry"]
-[5.415921688079834, 7.5978193283081055, "[TT] Fire rate (Hz) of the NGSLR = 28"]
-[10.132577896118164, -1.467218041419983, "[TT] Launch Inclination of the TESS = 28.5\u00ba"]
-[7.703120708465576, -2.5525455474853516, "[TT] Observation Frequency of the GOLD = About every 30 minutes"]
-[5.178689956665039, 8.400931358337402, "[TT] Bandwidth of the DCG = 0-75 MHz"]
-[9.100810050964355, 2.594054937362671, "[FF] Shape of the Heliosphere = Deflated croissant"]
-[12.10154914855957, 4.549230575561523, "[TT] Size of the Spacecraft = 320 mm x 340 mm x 362 mm"]
-[5.4949846267700195, 7.0319929122924805, "[TT] Transfer Rate of the C&DH = 21.6 MByte/s"]
-[3.0998287200927734, 1.778846025466919, "[TT] Revisit Time of the Copernicus Sentinel-2 = 5 days"]
-[6.403152942657471, 5.4879021644592285, "[FF] Function of the Encoder = Stall warning system"]
-[3.732590675354004, 6.682440757751465, "[TT] IFOV (beam width) of the Antenna = 1.57\u00ba"]
-[8.189217567443848, -1.007278561592102, "[TT] Measurement Accuracy of the ICESat-2 = Within a fraction of an inch"]
-[3.697331190109253, 5.147727966308594, "[TT] Polarization of the RADARSAT-1 = HH"]
-[7.299646377563477, 3.5503790378570557, "[FF] Frequency of the Internal Satellite Diffuser = Potentially every orbit"]
-[4.844791889190674, 7.337887763977051, "[TT] Data Rates of the EXIS = 7.2 kbit/s (X-band), 0.9 kbit/s (L-band)"]
-[10.396333694458008, 3.2351794242858887, "[TT] Number of CubeSat Units of the TetherSat = 3"]
-[4.280168533325195, 7.358029365539551, "[TT] Gain of the X-band Transmitter = >0 dBi"]
-[9.184200286865234, 2.760002374649048, "[FF] Mission Objective of the X-Ray Flux Monitor (XFM) = Space Weather monitoring and forecasting"]
-[14.119247436523438, 6.810020446777344, "[TT] Capacity of the Power Storage = 5 Ah"]
-[8.942280769348145, 5.615147113800049, "[TT] Earth Observation Precision of the ADCS = Sub-degree"]
-[12.618234634399414, 9.094115257263184, "[TT] Equator Crossing Time of the OrbView-2 = 12:00 hours on descending node"]
-[8.521702766418457, 8.054084777832031, "[TT] Number of Pixels of the Band 3 = 1600"]
-[8.66152286529541, 3.822185754776001, "[TT] Number of Scientific Instruments of the SOLAR = 3"]
-[10.154163360595703, -2.7662949562072754, "[TT] Max. Output data rate of the SLC NAND-FMM = 800 Mbit/s"]
-[7.329519271850586, 5.321821212768555, "[FF] Components of the nSight-1 = Gecko Imager, VHF/UHF transceiver, OBC and ADCS module, Break-out Board"]
-[8.515616416931152, 5.406747817993164, "[TT] Position Calculation Time of the Transit Navigation = 10 to 15 minutes"]
-[4.464870452880859, 2.9753735065460205, "[FF] Test Location of the AMS-02 = ESA/ESTEC in Noordwijk, The Netherlands"]
-[8.60700511932373, 1.437984585762024, "[TT] Quantization Levels of the Cloud amount = 1"]
-[10.143305778503418, 10.001667022705078, "[TT] Launch Date of the Vega = 17 August 2021"]
-[9.613807678222656, -0.6648522019386292, "[TT] Orbit Reach of the Akatsuki = 2016"]
-[9.574459075927734, 5.921752452850342, "[TT] Tilt Angle of the Cube corners = 25\u00ba and 50\u00ba"]
-[13.287272453308105, 5.308481693267822, "[TT] Solar Array Size of the EPS = 5.661 m 2"]
-[6.3045759201049805, 8.033674240112305, "[TT] Number of International Channels of the DCP = Up to 33"]
-[10.373642921447754, 5.775817394256592, "[TT] Operational Temperatures of the FPM = -40 \u00b0C and -10 \u00b0C"]
-[6.522793292999268, -1.9902681112289429, "[TT] Recommended Mission Extension of the Jason-2/OSTM = 2015"]
-[7.603245735168457, 5.7602219581604, "[FF] Scanning Frequency of the Scanning LIDAR = Varied according to a predefined scanning scheme"]
-[13.182120323181152, 7.249928951263428, "[TT] Average Power Consumption (Standby Mode) of the COMIS = 8 W"]
-[5.4187235832214355, 5.081920146942139, "[TT] Main Communication Bus of the CSI = CAN (Controller Area Network)"]
-[8.950496673583984, 3.7515616416931152, "[TT] Solar Panels of the Occulter satellite = On its Sun-facing side"]
-[10.810665130615234, 7.572478771209717, "[TT] Swath Width of the DMC-1 = 600 km"]
-[9.251928329467773, 1.8728188276290894, "[FF] Sensor Type of the HARP = Polarimeter"]
-[10.32151985168457, 4.552034378051758, "[TT] Failed Components of the FormoSat-2 = One gyro (out of four) and one reaction wheel (out of four)"]
-[3.393505096435547, 6.400720596313477, "[TT] Dish Size of the Chilbolton Site = 25 m"]
-[7.518296241760254, 2.9715678691864014, "[TT] Detection Threshold of the MethaneSAT = 2 ppb"]
-[7.588421821594238, 9.253253936767578, "[TT] Band 2 of the CIRiS = 9.85 \u00b5m to 11.35 \u00b5m"]
-[13.925938606262207, 3.1747219562530518, "[TT] Mass of the User Terminal = < 1 kg"]
-[13.213059425354004, 5.5103864669799805, "[FF] Analysis of the SOLID Panels = The four panels will be analyzed continuously one after another"]
-[10.946907997131348, 2.0616393089294434, "[TT] Science Mission Duration of the XMM = Well into its third decade"]
-[7.005120754241943, 4.801301956176758, "[FF] Configuration of the RAFS Flight Model 4 (RAFS FM4) = Driven by the RAFS Flight Model 4 (RAFS FM4)"]
-[5.474380016326904, 3.916274070739746, "[TT] Number of Satellites of the JL-1-GF03B = 6"]
-[10.776264190673828, 5.904829978942871, "[TT] Testing Temperature of the Faraday Cup = Exceeding 1650 \u00baC"]
-[6.77763032913208, 6.417191028594971, "[TT] Processing Time of the F2 AIPS = 2 hours"]
-[2.3375089168548584, 1.3113141059875488, "[TT] Mission Status of the NanoSail-D2 = Active"]
-[6.413082122802734, 7.044007778167725, "[TT] False Event Rate of the Instrument = <5%"]
-[11.770564079284668, 6.736473083496094, "[TT] Energy Resolution of the RHESSI = One- to a few- keV"]
-[5.437570095062256, 8.684793472290039, "[TT] Bandwidth of the Spectral bandwidth = 5.0 nm"]
-[5.4634108543396, 6.055391311645508, "[TT] ROM/RAM of the SCU = EEPROM(128KB x 2), SRAM(512KB x 4, 8MB x 1)"]
-[8.666421890258789, 7.691633224487305, "[TT] Pixel Size of the Detector Array (MS) = 48 x 48 \u00b5m"]
-[9.768013000488281, 7.415781021118164, "[TT] Ground Sample Distance (GSD) of the Optical Sensor (OPS) = 2 m"]
-[9.654715538024902, 4.3043413162231445, "[FF] ADCS System of the DeorbitSail = First in-orbit demonstration of the CubeComputer"]
-[5.429290294647217, 1.8207780122756958, "[FF] Design Factors of the ELSA-d = Mission safety, market leadership, engagement in discussions for doctrine, standards, and regulation, interface with legal structures"]
-[10.204501152038574, 8.299996376037598, "[TT] Entrance Pupil Size of the Telescope = 30 mm x 30 mm"]
-[3.9708640575408936, 6.334716320037842, "[TT] Feed Horn Type of the SSM/I = Corrugated broadband seven-port horn"]
-[8.456422805786133, 2.9616456031799316, "[FF] Objectives of the ATLAS-1 = Study of the chemical makeup of the atmosphere, measurement of the total energy contained in sunlight, investigation of how the Earth's electric and magnetic fields and atmosphere influence one another, examination of sources of ultraviolet light in the universe"]
-[8.638556480407715, 0.8731528520584106, "[TT] Distance to Seismically Active Region of the InSight lander = More than 1,000 kilometers"]
-[6.867607593536377, 1.1846983432769775, "[FF] Observation Time of the Solar Dynamics Observatory (SDO) = Sep. 6, 2017"]
-[7.556603908538818, 7.027340412139893, "[TT] Readout Time of the CCD = Less than 10 ms"]
-[11.697264671325684, 3.351430892944336, "[TT] Total Impulse of the Field Emission Electric Propulsion System = 6000 Newton-seconds"]
-[9.763643264770508, -0.37609344720840454, "[TT] Altitude of the Satellite Constellation = About 500 km"]
-[5.383360862731934, 7.280545711517334, "[TT] Data Rate of the CanX-2 = 1 Mbit/s"]
-[7.0047407150268555, 3.9479920864105225, "[FF] Objective of the DCS = Collect and relay environmental data from unattended land- and ocean-based automatic data collection platforms"]
-[13.378173828125, 7.340926647186279, "[TT] Electrical Power of the HiSPiCO = 5 W"]
-[12.154932975769043, -0.08525867760181427, "[FF] Instrument of the TESS = Cameras"]
-[10.160557746887207, 0.9138035178184509, "[TT] Distance to Signal Source of the LIGO = 1.3 billion light-years"]
-[5.3947672843933105, 4.165390968322754, "[TT] Type of the PCSat = Prototype Communications Satellite"]
-[5.916930675506592, 1.0836694240570068, "[FF] Launch Date of the Earth Science Sensor = 2021"]
-[5.233002185821533, 3.3186984062194824, "[TT] Hosting Spacecraft Provider of the DSAC = Surrey Satellite Technologies US LLC"]
-[4.5701069831848145, 2.754007339477539, "[TT] Construction Location of the BRITE Satellites = UTIAS/SFL"]
-[14.756976127624512, 6.591955661773682, "[TT] Capacity of the Li-ion Battery = 15 Ah"]
-[8.80070972442627, 2.627432346343994, "[TT] Error of the Land = \u00b10.2 m"]
-[12.616142272949219, 9.094035148620605, "[TT] Equator Crossing Time of the SMAP = 6:00 a.m. and 6:00 p.m. local time"]
-[6.003418922424316, 2.119630813598633, "[FF] Area of the RESTEC = Asia and Russian area"]
-[3.882554292678833, 2.0396761894226074, "[TT] Launch Vehicle of the PLATO = Soyuz 2-1b rocket"]
-[4.959021091461182, 0.41562211513519287, "[TT] Operation Declaration Date of the QZS-1/Michibiki = July 2011"]
-[5.8737711906433105, 3.760953903198242, "[FF] Constellation Operator of the Nanosatellite = Open Cosmos"]
-[6.271953105926514, 2.49351167678833, "[FF] Previous Projects of the International Space Station, Orion, Gateway = International Space Station, Orion and the future Gateway around the Moon"]
-[4.349074840545654, 0.16083258390426636, "[FF] Launch Rate Goal of the Starlink = Roughly two Starlink launches a month"]
-[3.248206377029419, 2.238222360610962, "[FF] Data Policy of the Copernicus Space Component = Open access to Sentinel data by anybody and for any use"]
-[6.528591156005859, 0.8749796152114868, "[FF] Oscillation Modes Frequency Shift of the Gaia = 8.6 million times"]
-[8.247359275817871, 6.814091682434082, "[TT] Type of the Advanced Baseline Imager = Imager"]
-[7.926116466522217, 6.309704303741455, "[TT] Instrument Type of the AIS = Imaging multi-spectral radiometers (vis/IR)"]
-[14.654070854187012, 6.61661434173584, "[TT] DOD (Depth of Discharge) of the Li-ion battery = 17.9%"]
-[12.091198921203613, 4.994871139526367, "[TT] Size of the Transmitter = 230 mm x 136 mm x 30 mm"]
-[8.608272552490234, 3.047551155090332, "[TT] Horizontal Resolution of the ROSA = 300 km"]
-[6.5819196701049805, 5.019990921020508, "[FF] Subsystems of the IRPE = Antenna and RF equipment, DIS (Data Ingestion Subsystem), DAS (Data Acquisition Subsystem), ICPS (Image Collection Planning Subsystem), WMS (Workflow Management Subsystem), DPS (Data Processing Subsystem), UIS (User Interface Subsystem)"]
-[4.609437465667725, 0.7677645087242126, "[FF] Planned System of the SARah = SARah"]
-[4.9437079429626465, 7.399059295654297, "[TT] Uplink Data Rate of the RF Communications = 2 kbit/s"]
-[3.9128870964050293, 2.0650622844696045, "[FF] Previous Launch Arrangement of the RADARSAT-2 = Delta-2 vehicle from VAFB"]
-[11.726889610290527, 3.3269996643066406, "[TT] Number of Tests of the SuperDraco Engines = Hundreds"]
-[5.862292766571045, -0.006361505948007107, "[TT] Operation Period of the S-193 = May 1973 to Feb. 1974"]
-[14.046061515808105, 3.0128607749938965, "[TT] Mass of the SporeSat = ~5.5 kg"]
-[11.830820083618164, 4.7075653076171875, "[TT] Size of the CanX-7 = 10 x 10 x 34 cm"]
-[6.7665324211120605, -0.538564145565033, "[TT] Orbital Period of the DMSP Satellites = 101 minutes"]
-[7.693775177001953, 0.26492902636528015, "[TT] L4 Cloud Flyby Dates of the Lucy = 2027-2028"]
-[9.179281234741211, 4.879322528839111, "[TT] Quantity of the Temperature Sensors = 4 (2 in the head and 2 close to the ADC)"]
-[10.587530136108398, 6.424177169799805, "[FF] Retroreflector Coating of the Norton = Reflects both transmitted wavelengths"]
-[9.145699501037598, -0.4574151635169983, "[TT] Orbit Apogee of the ABEX = 60,000 km"]
-[5.366572380065918, 1.673760175704956, "[FF] Purpose of Agreement of the ALOS-2/Daichi-2 = Survey secular changes in landscape and ash fall, isolated islands for their upkeep"]
-[5.475968837738037, 5.935287952423096, "[FF] Technology of the Hitachi 128 k x 8 SRAM = Unknown"]
-[6.6259565353393555, 6.162148475646973, "[TT] TRL of the ROIC = 7"]
-[6.475141525268555, -0.5420482754707336, "[TT] Revisit Period of the ZY-3A = 59 days"]
-[3.5354983806610107, -0.9756868481636047, "[TT] Exploration Mission Orbit of the LRO = Quasi-circular polar orbit (50 \u00b1 15km)"]
-[4.8913092613220215, 7.3268609046936035, "[TT] Nominal Mode Uplink Data Rate of the ASTERIA Transceiver = 32 kbit/s"]
-[6.521119117736816, 4.764053821563721, "[FF] Team Leader of the Data receiver, Calibration and Operational Process = Liu Yi"]
-[12.454341888427734, 0.5708009004592896, "[FF] Announcement Date of the PLATO = 11 April, 2018"]
-[6.704864978790283, 0.8824701905250549, "[TT] Mission Start Date of the Solar Orbiter = February 14, 2020"]
-[7.223499298095703, 2.9718501567840576, "[FF] Data Usage of the Iridium Constellation Satellites = Characterize the variation of the Birkeland currents with interplanetary conditions, particularly during magnetic storms"]
-[10.408270835876465, 3.25302791595459, "[TT] Number of CubeSat Units of the ORS-3 = 3"]
-[5.368902206420898, 0.18934465944766998, "[TT] Launch Date of the STS-45 = March 24 - April 2, 1992"]
-[11.936433792114258, 4.922140121459961, "[TT] Volume of the XRD = ~34 x 109 x 109 cm3"]
-[5.42861270904541, 8.768733024597168, "[TT] Band 1 Bandwidth of the COCTS = 0.402-0.422 \u00b5m"]
-[5.433494567871094, 2.695361852645874, "[TT] User of the Canadarm2 = NASA astronaut Megan McArthur"]
-[4.5997209548950195, 6.3777174949646, "[FF] Purpose of the Alinco UHF Transceiver = Monitor the spacecraft beacon messages"]
-[7.703736305236816, 8.634359359741211, "[TT] Spectral Bands of the FTHSI = Hundreds"]
-[6.011949062347412, -0.2976076006889343, "[TT] Operation Duration of the LRO = 9 years"]
-[7.680219650268555, 2.1846728324890137, "[TT] Daily Coverage of the ZY-3A = 150,000 km2"]
-[8.174043655395508, 5.659504413604736, "[FF] Placement of the Calibration Module = In front of the aperture of the spectrometer"]
-[14.164521217346191, 2.872467279434204, "[TT] Mass of the KazEOSat-2 = ~185 kg"]
-[7.292268753051758, 2.6343436241149902, "[FF] Aim of the INSAT-3D = Provide enhanced meteorological observations and monitoring of land and ocean for weather forecasting and disaster warning"]
-[14.09347152709961, 7.123359680175781, "[TT] Voltage of the Battery = 28 V"]
-[6.280181884765625, 1.4510161876678467, "[FF] First Light Date of the eROSITA = 22 October 2019"]
-[5.32945442199707, 5.020160675048828, "[TT] Compatibility of the NovAtel OEM-615 = GOMSpace Nanodock DMC-3 Motherboard"]
-[6.352025985717773, 0.7741143107414246, "[TT] Third Full Data Release (DR3) Date of the Gaia = 13 June"]
-[8.785905838012695, 6.366106986999512, "[TT] Required Accuracy of the Altimeter = 4.0 cm"]
-[4.757498741149902, 0.20158807933330536, "[TT] Launch Date of the RemoveDebris = 2nd of April 2018"]
-[11.401750564575195, 4.763310432434082, "[FF] Lever Arm Length of the STD = ~ 1 m to ~ 4 m"]
-[5.507791996002197, 1.0200327634811401, "[FF] Regional Service Start Date of the BeiDou-2 Navigation Satellite System = Unknown"]
-[9.368332862854004, 0.4768296182155609, "[TT] Pericenter Distance of the SMART-1 = 2189.702 km"]
-[6.957116603851318, 4.410752773284912, "[FF] Complement of the TDP = Unknown"]
-[10.056487083435059, 7.020784378051758, "[TT] Horizontal Integration of the Aeolus = 50 km"]
-[7.393628120422363, 8.238564491271973, "[TT] Log (T) of the TRACE = 3.6 - 3.8"]
-[4.270298480987549, 7.306728363037109, "[TT] Downlink Frequency of the TT&C = X-band"]
-[13.744526863098145, 2.8853132724761963, "[TT] Total Mass of the Spacecraft = 236 kg"]
-[7.721838474273682, 9.102949142456055, "[TT] Band Wavelength of the MISR = 0.67 and 0.87 \u00b5m"]
-[6.166950702667236, 1.8095743656158447, "[FF] URL of the SpaceX CRS-2 Mission = http://www.spacex.com/downloads/crs2-press-kit.pdf"]
-[5.024894714355469, -0.38969534635543823, "[TT] Launch Time of the CuPID = 18:12 UTC"]
-[4.603479385375977, 4.803500652313232, "[FF] Purpose of the AIS = Navigation aid and anti-collision system for vessels at sea"]
-[4.424035549163818, 5.402900218963623, "[TT] Beacon Signal Period of the Trisat = Approximately 400 seconds"]
-[6.379969120025635, -0.25853294134140015, "[TT] Revisit Time of the ALOS = 46 days"]
-[13.949973106384277, 3.7899599075317383, "[TT] Mass of the Metrology Laser = ~ 1.5 kg"]
-[5.315636157989502, 7.722323417663574, "[TT] EIRP of the Antenna = More than 67.9 dBW"]
-[7.512490272521973, 3.5311548709869385, "[FF] Objective of the e.Deorbit = Removing a large ESA-owned object from space"]
-[9.087750434875488, 4.556201934814453, "[FF] Attitude Control System of the Corvus = ST-16 star tracker, three reaction wheels, Smart Solar Panels"]
-[7.924393177032471, 2.142354726791382, "[FF] Sea Surface Temperature Product Algorithm of the Ocean Color and Temperature Scanner (OCTS) = Unknown"]
-[13.781259536743164, 5.582981109619141, "[TT] Directional Impact Proportion of the Solar-cell cover glasses = About 30%"]
-[11.519848823547363, 6.748990535736084, "[TT] Electronic Noise Contribution to Energy Resolution of the Detector = 400 eV"]
-[8.959000587463379, 4.476207256317139, "[TT] Control Mode of the NEOSSat = Sun-Point"]
-[9.42594051361084, 7.958134174346924, "[TT] Field of View of the Limb Imager = 75 to 110 km tangent altitudes, 300 km across the track"]
-[6.151247978210449, 4.468844890594482, "[FF] Content of the High-level Activity Schedule = Times the LCRD payload will operate and any operational events that may impact host spacecraft flight or ground operations"]
-[5.106342792510986, 3.462416648864746, "[TT] Satellite Navigation Company of the GMV-NSL = British"]
-[4.669514179229736, 0.7559157609939575, "[TT] Phase D Start Date of the PROBA-V = Summer 2012"]
-[5.76108455657959, 1.6532173156738281, "[TT] Measurement Date of the MPO PFM Spacecraft = January 2016"]
-[7.108819961547852, 8.291521072387695, "[TT] SNR of the Instrument = Between 350 and 450"]
-[5.348573684692383, 1.6517691612243652, "[FF] Geolocation and Ortho-rectification Methods of the Deimos-2 = Physical sensor model, RFM (Rational Function Model)"]
-[4.841257572174072, -1.837746262550354, "[FF] Circumlunar Flight Duration of the Chang'e-2 = 150 days"]
-[10.186854362487793, 5.2433905601501465, "[FF] Principle of the RTG = Based on the Seebeck principle to transform the heat energy into the electric energy"]
-[10.781835556030273, 3.0121548175811768, "[TT] Configuration of the O/OREOS nanosatellite = 3U CubeSat"]
-[4.0679612159729, 2.210731267929077, "[TT] Launch Vehicle of the Atlas V = Atlas V"]
-[13.45589828491211, 5.937880039215088, "[FF] Power Experiment Conditions of the Scientific Payload = Adequate Solar Illumination"]
-[9.301300048828125, 7.822023868560791, "[TT] Target Detection Image Size of the NEA Scout Camera = 3840 x 2184 pixels"]
-[5.386953353881836, 6.174704551696777, "[TT] Processor Speed of the ECS = 1500 MIPS"]
-[7.601507663726807, 0.8197920918464661, "[FF] Mission of the LunaH-Map = Map hydrogen within craters and other permanently shadowed regions throughout the moon's south pole"]
-[9.92098331451416, 0.7981621623039246, "[FF] Orbital Distance of the Planet Candidate = Tens of times the Earth-Sun distance"]
-[10.319310188293457, 4.50897216796875, "[FF] Type of the Reaction Wheels = Ball bearing"]
-[13.207866668701172, 5.213104724884033, "[TT] Dimensions of the Solar Panels = 3.73 m x 1.8 m"]
-[1.313928246498108, 1.8986141681671143, "[TT] Cargo Capacity of the HTV-9 = Up to six tons"]
-[8.340888977050781, 8.800314903259277, "[TT] Dust Measurement Particle Size of the UVS = 100 nm"]
-[8.02605152130127, 6.123908519744873, "[FF] Zoom Capability of the Zoom-in Camera = Yes"]
-[7.448788642883301, 4.317401885986328, "[FF] Sensor Complement of the ERS-2 = Unknown"]
-[9.949535369873047, 6.688045024871826, "[FF] Focusing Method of the Camera = Adjusting the focal plane position resulting from the adjustment of the flat mirror assembly position"]
-[5.071334362030029, 1.8062734603881836, "[FF] Mission Status of the Tatiana-2 = Finished"]
-[5.552974700927734, 3.9263758659362793, "[TT] Number of Launches of the DMSP spacecraft = 44"]
-[11.209644317626953, 4.76436710357666, "[TT] Length of the Hydra = 55 km"]
-[4.575534820556641, 6.531510829925537, "[TT] RF Communications of the Spacecraft = 2234.4 MHz"]
-[9.53589153289795, 7.547871112823486, "[TT] Angular resolution (2 px) of the HRI Lyman-\u03b1 1216 \u00c5 = 1 arcsec"]
-[6.490719318389893, 7.181642055511475, "[TT] Pulse Length of the RA-1 = 20 \u03bcs"]
-[3.0458779335021973, 4.5052876472473145, "[FF] Performance of the PALSAR-2 = Extremely good with high-quality SAR imagery"]
-[8.241964340209961, -0.23082709312438965, "[TT] Period (min) of the Cosmos-1066 (Astrofizika) = 102.2"]
-[9.181558609008789, 2.2364823818206787, "[FF] URL of the \"Discrete and broadband electron acceleration in Jupiter's powerful aurora\" = https://doi.org/10.1038/nature23648"]
-[8.350831031799316, 4.533342361450195, "[FF] Quantity of the Electric and magnetic antennas, 2 cameras, 4 photometers, X-ray and Gamma-ray (\u03b3-ray) sensors = 1 set each"]
-[6.250388145446777, 1.4696736335754395, "[FF] Purpose of the Swarm = Space science studies"]
-[9.496872901916504, 8.146120071411133, "[TT] Field of View of the Cameras = Overlapping"]
-[6.78154182434082, -0.4128323495388031, "[TT] Repeat Cycle of the Harmony satellites = 12 days"]
-[9.557294845581055, 9.152847290039062, "[TT] Flare Class of the IRIS = M-class"]
-[5.759894371032715, 1.1261898279190063, "[FF] Meeting Date of the SHIZUKU and IBUKI = May 30-June 1, 2012"]
-[6.470277786254883, 4.66215181350708, "[FF] Principal Units of the Corvus-BC satellite = Data & Power Module, Attitude Control System module, Ka-Band radio, Multi-Spectral Imager"]
-[6.387602806091309, 2.181652069091797, "[FF] Overview of the Aditya I = URL: http://www.iiap.res.in/meet/sol2011/sol_ppt/RPrasad.pdf"]
-[6.142065048217773, 2.2562222480773926, "[TT] Principal Investigator Institution of the Lucy = Southwest Research Institute in Boulder, Colorado"]
-[12.211226463317871, 0.5815341472625732, "[FF] Transit Signal Study Method of the PLATO = Further information about the planet's bulk properties can be determined by studying the transit signal"]
-[6.27186918258667, 0.3274421989917755, "[TT] Operational Period of the ROSE-L = Until 2026-2028"]
-[7.591666221618652, 6.88122034072876, "[FF] Nominal L Value of the CrIS Instrument = Given in the table"]
-[9.013699531555176, 3.271878242492676, "[FF] Composition of the Plasma = Gaseous and highly conductive charged particles"]
-[13.12054443359375, 7.186126232147217, "[TT] Power Consumption of the MuREM = ~1.4 W"]
-[9.60977840423584, 4.8684492111206055, "[TT] Stabilization of the ADCS = 3-axis"]
-[7.716953754425049, 1.7679623365402222, "[FF] Emissions Contribution in 2019 of the Sudd wetlands in South Sudan = Over a quarter of the growth in global emissions"]
-[11.821093559265137, 3.384648323059082, "[FF] Function of the Resistojets = Acts as a vaporizer to ensure no liquid propellant is expelled, as well as increasing the specific impulse of the system"]
-[5.485473155975342, 4.322498321533203, "[TT] Number of Stations of the EDRS DGS = Two"]
-[7.3110127449035645, 1.0558221340179443, "[FF] Material of the Site Kingfisher = Fresher, minimally-altered"]
-[8.99596881866455, 10.268156051635742, "[TT] Pixel Resolution of the SPIM5 = 14 bit"]
-[11.447535514831543, 4.733266830444336, "[TT] Length of the ERA = Over 11 m"]
-[5.830908298492432, 5.929238319396973, "[TT] Number of Libraries of the C&DH Subsystem = 8"]
-[11.28139591217041, 5.454468250274658, "[TT] NaF Tile Thickness of the RICH = 5 mm"]
-[7.454807281494141, 4.562623023986816, "[FF] Potential Future Use of the LRI = Primary instrument in future GRACE-type missions"]
-[14.223124504089355, 3.248342514038086, "[TT] Total Mass of the CGM = 0.835 kg"]
-[8.021600723266602, -0.42994794249534607, "[TT] Daily Record Lows of the Antarctic Sea Ice = Reached by November"]
-[10.980359077453613, 6.324963092803955, "[TT] Primary Mirror Material of the OPS = NTSIC (New Technology Silicon Carbide)"]
-[5.405148506164551, 0.8218938112258911, "[TT] Test Measurement Period of the ExoMars TGO ACS = 28 February to 7 March 2017"]
-[6.398585796356201, -0.04025784134864807, "[TT] Frequency of the Command and control requirements = Once per month"]
-[8.317110061645508, -0.46863552927970886, "[TT] Measurement of the Sea Ice Extent = 5.28 million km2"]
-[7.113312721252441, 5.939088821411133, "[TT] Ovenized Crystal USO Frequency Drift of the DSAC = Below 1 x 10 -10/day"]
-[8.812601089477539, 5.912936210632324, "[FF] Objective of the SCDE = Non-contact measurement of surface potentials"]
-[6.422647953033447, 3.5474281311035156, "[FF] Constellation of the GPM = Various satellites"]
-[7.684839725494385, -2.2925729751586914, "[FF] URL of the GOLD instrument = http://gold.cs.ucf.edu/science-mission/gold-instrument/"]
-[10.484278678894043, 6.644787311553955, "[TT] Number of Mirrors of the Bottom Dome = 399"]
-[6.793091773986816, 3.3760526180267334, "[FF] Stowage of the Kaber = ISS"]
-[14.246245384216309, 3.2203776836395264, "[TT] Mass of the APAA = 183 kg"]
-[8.507050514221191, 0.7440320253372192, "[TT] Quantization Levels of the Ice: edge location = 1"]
-[8.184789657592773, 7.499257564544678, "[TT] Quantity of the LED-arrays = 3"]
-[8.937562942504883, -1.00152587890625, "[TT] Orbit Type of the SES-17 = GEO and MEO"]
-[10.196491241455078, 8.138179779052734, "[TT] Clear Aperture of the OLS = 20.3 cm"]
-[10.458148002624512, 5.726343631744385, "[TT] Average Upper Atmosphere Temperature of the Jupiter = About minus 100 \u00ba Fahrenheit or a chilly minus 73\u00ba Celsius"]
-[9.619979858398438, -0.4768102467060089, "[TT] Orbital Altitude of the FORMOSAT-7/COSMIC-2 Constellation = 550 km"]
-[12.407093048095703, 3.2128098011016846, "[TT] Total propellant used of the Perigee Raising = 9 g"]
-[3.3374948501586914, 5.0750226974487305, "[TT] SAR Payload Orbital Altitude of the RCM = 600 km"]
-[13.363971710205078, 7.368289470672607, "[TT] Power of the OVM = 3 W"]
-[8.235152244567871, 8.920272827148438, "[TT] Spectral Range of the UV-1 = 270 - 314 nm"]
-[6.765864372253418, 4.8040924072265625, "[FF] Control Loop Input of the ADACS = GPS position knowledge"]
-[5.213490962982178, 0.2786601185798645, "[TT] Launch Date of the JERS-1 = 11 Feb 1992"]
-[3.767122983932495, 5.463202476501465, "[TT] Azimuth Resolution of the Spotlight = 1.7 m (single pol.)"]
-[8.224109649658203, 2.392458438873291, "[TT] Application of the TIR band (8.5 \u00b5m) = Detection of volcanic cloud with sulfuric acid aerosols, thin cirrus, determination of cloud microphysical properties"]
-[3.6322755813598633, 4.804872035980225, "[FF] Purpose of the QSAT = Polar Plasma Observation"]
-[7.827326774597168, 8.402566909790039, "[TT] Bands of the PMC = NIR and three visible (blue, green and red)"]
-[4.792253017425537, -1.5402940511703491, "[TT] Lander/Rover Landing Site of the Tianwen-1 = Utopia Planitia"]
-[6.186808109283447, 3.0112497806549072, "[FF] Intended Use of the SFA = Future RMS (Remote Manipulator System) of JEM (Japanese Experiment Module) on ISS"]
-[12.141755104064941, 4.489433765411377, "[TT] Dimensions of the Satellite = 4 m x 3 m x 2 m"]
-[9.944559097290039, -0.18926914036273956, "[TT] Orbit Altitude of the Starshine = 500 km"]
-[12.142247200012207, 3.4900145530700684, "[TT] Quantity of the Commercial Off-the-Shelf (COTS) Air Tanks = Sixteen"]
-[12.096040725708008, -0.36912664771080017, "[TT] Primary Mission Duration of the TESS = Two years"]
-[9.796483993530273, 7.479637622833252, "[TT] Ground Sample Distance (GSD) of the GIS Instrument = 41 cm for Pan and 1.64 m for MS"]
-[8.872264862060547, 6.489007949829102, "[FF] Function of the CaSSIS = Acquiring color stereo images of surface features possibly associated with trace gas sources and sinks"]
-[4.25907039642334, 0.7228077054023743, "[TT] Positioning of the EDRS-D = Over the Asia-Pacific (APAC) region by 2020"]
-[8.9667387008667, 5.30506706237793, "[TT] Orbit Altitude of the GomX-4B = 500 km"]
-[4.448105812072754, 0.6927484273910522, "[TT] Integration and Test Start Date of the PROCYON = July 2014"]
-[4.6868367195129395, 1.6384477615356445, "[TT] Patent Award Date of the GHGSat-D = January 2016"]
-[6.313546180725098, 8.101239204406738, "[TT] Quantity of Channels of the MAPMT = 16"]
-[8.187822341918945, 7.444173336029053, "[TT] Well Depth of the GLM CCD = Approximately 2 million electrons"]
-[8.608624458312988, 3.292851448059082, "[FF] Objective of the SENSE = Provide data for ionospheric prediction models"]
-[6.47275972366333, 5.690584182739258, "[TT] Number of Electronic Boards of the C&DH = 9"]
-[5.390998363494873, 3.3469858169555664, "[FF] Manufacturer of the Lemur-2 x 4 = Spire Global Inc."]
-[4.302464008331299, 0.7762571573257446, "[FF] Evaluation Date of the CrIMSS OPS-EDR Product = 02/24/2012"]
-[4.609435081481934, 4.706536293029785, "[FF] Efficiency of the Boat-based sonar surveys = Inefficient in shallow waters"]
-[6.886702537536621, 5.878111839294434, "[TT] Quantity of the MTs = 3"]
-[5.543984889984131, 4.9877495765686035, "[TT] Operating System of the CanX-2 = CANOE"]
-[10.78418254852295, -1.1335433721542358, "[TT] Orbit Type of the SLATS = Super Low Altitude"]
-[4.378255844116211, 7.606862545013428, "[TT] S-band Downlink Frequency of the MSX = 2282.5 MHz"]
-[7.065446376800537, 7.746822357177734, "[TT] Calibration Experiment Targets of the RISAT-1 MRS = Triangular tetrahedral corner reflectors"]
-[4.712062358856201, 8.075989723205566, "[TT] Chirped Carrier Frequency of the Frequency Generator = 5.35 GHz"]
-[4.374135494232178, 3.059776782989502, "[FF] Location of the RBU = Fairmont, WV"]
-[9.234197616577148, 1.9002453088760376, "[FF] Operation of the Space Maid Robot Harpoon and Net System = In-orbit"]
-[14.25838851928711, 3.3291144371032715, "[TT] Mass of the TEPCE = 3 kg"]
-[12.087686538696289, 6.328976154327393, "[FF] Measurement Parameters of the AMS-02 = Positron fraction falls beyond its maximum, antiproton to proton ratio"]
-[10.04467487335205, -1.5365318059921265, "[TT] Inclination of the Corvus-BC 4 = 97.6\u00b0"]
-[10.30974292755127, 2.6956684589385986, "[TT] Geographical Position Visit Frequency of the NanoSat-1B = Every 4 days"]
-[4.008828639984131, 3.5935587882995605, "[FF] PRS Element of the Galileo = Unknown"]
-[4.327747344970703, 1.2548903226852417, "[FF] Launch Date of the SEOSAT-Ingenio = Later this year"]
-[9.525406837463379, 1.8518000841140747, "[FF] Chief Scientist of the Hubble Space Telescope = Ed Weiler"]
-[10.172796249389648, 1.4469058513641357, "[TT] Survey Density of the VIS = At least 30 galaxies per arcmin2"]
-[8.307877540588379, 4.567941665649414, "[FF] Accuracy Improvement of the LARES 2 = mm-level"]
-[7.101312160491943, 6.874251842498779, "[FF] Frequency Offset of the Local Laser = Chosen such that after picking up once more the Doppler shift (with the same sign) on the way back to S/C 1, the beat note between the light arriving back at S/C 1 and the local, stabilized, laser at S/C 1 is in the sensitive frequency range of the phasemeter (approximately 2 - 15 MHz)"]
-[14.589706420898438, 6.622288703918457, "[TT] Battery Type of the HTV = Lithium ion"]
-[7.394588470458984, 4.33638334274292, "[FF] Unknown of the Sensor Complement = Unknown"]
-[5.475061893463135, 2.886871576309204, "[FF] URL of the SPIDER = https://lockheedmartin.com/content/dam/lockheed-martin/eo/documents/webt/spider-infographic.pdf"]
-[10.919708251953125, 5.160799026489258, "[FF] CCRs of the LARES-2 = COTS components"]
-[5.517253875732422, -1.8463553190231323, "[FF] Conference Date of the KOMPSAT-3A = May 16-20, 2016"]
-[13.318865776062012, 7.594276428222656, "[TT] SSPA output power of the Antenna = 20 W (linear) 40 W (saturated)"]
-[8.211182594299316, 1.4577903747558594, "[FF] Rainfall Measurement of the IMERG = Greater than 160 mm"]
-[10.988763809204102, 3.527641534805298, "[TT] Dimensions of the 6U CubeSat = Roughly 10 x 20 x 30 cm"]
-[5.688312530517578, -0.7926968336105347, "[TT] Design Life of the SPOT-2 = Three years"]
-[4.821368217468262, 7.261385440826416, "[TT] Uplink Data Rate of the S-band RF Communications = 20 kbit/s"]
-[3.5999224185943604, 4.770371437072754, "[TT] Instrument type of the SAR (RADARSAT-2) = Imaging microwave radars"]
-[6.756897449493408, 1.7423378229141235, "[FF] URL of the LRO = http://www.nasa.gov/mission_pages/LRO/news/lro-topo.html"]
-[8.412243843078613, 3.1009879112243652, "[FF] Observing Opportunity of the Ground-based Telescopes = Only brief windows exist near the Sun as the Earth rotates through 15\u00ba every hour"]
-[13.707828521728516, 5.405119895935059, "[FF] Components of the SMS = 22 triple-junction cells, two commercial dual-junction control cells, analog cell measurement circuitry, data converters, microcontroller, FPGA, n-channel MOSFET transistor, amplifier, tolerance resistor"]
-[9.626655578613281, 4.759064674377441, "[TT] Control of the ACS = Zero momentum 3-axis stabilized control with nadir pointing (5\u00ba)"]
-[9.061201095581055, 5.205173969268799, "[TT] Power Supply Redundancy of the IRU (Inertial Reference Unit) = Full redundancy"]
-[5.010879039764404, 4.35831880569458, "[TT] License Requirement of the Starlink = Yes"]
-[5.677980899810791, 7.065234661102295, "[TT] Average Data Rate Over Ocean of the KaRIN = ~3 Mbit/s"]
-[5.046077728271484, 3.398183584213257, "[TT] Manufacturer of the CEPA = Boeing"]
-[7.842600345611572, 6.523326396942139, "[FF] Imaging Cycles of the ABI = Faster"]
-[12.936153411865234, 7.102867603302002, "[TT] Efficiency of the Transponders = 40%"]
-[13.398445129394531, 6.841247081756592, "[TT] Power of the Spacecraft = > 1300 W (SAP power), 400 W (payload power)"]
-[5.480710983276367, 5.170730113983154, "[TT] Tracking Method of the TDRS = Track the spacecraft"]
-[8.203102111816406, 8.644761085510254, "[FF] Spectral Resolution of the HR Bands (677\u2013686 nm, 740\u2013759 nm and 769\u2013780 nm) = Principally driven from the aggregated pixel size (140 \u00b5m)"]
-[9.5639009475708, 3.7011752128601074, "[TT] Field Strength of the Sunspot = More than 6,000 gauss"]
-[8.206038475036621, 2.2055130004882812, "[TT] Composition of Enhanced Aerosol of the Australian Wildfires = Carbonaceous"]
-[7.149123668670654, 0.08910436928272247, "[TT] Age of the Cosmos 2251 = Older"]
-[8.645593643188477, 3.9580328464508057, "[FF] Measurement Range of the IRM = 0.5-100 eV ions"]
-[6.235586643218994, 6.184019088745117, "[TT] Receiver Tank Content of the RRM3 module = Empty"]
-[9.318411827087402, 5.261887550354004, "[TT] Solar b-angles of the SPARCS = Up to 40\u00b0"]
-[5.559803009033203, 5.008532524108887, "[TT] Interface Type of the GOES-R Access System = Subscription-based and ad hoc data requests"]
-[6.450728893280029, -0.41128358244895935, "[TT] Autonomy Period of the Satellite = Up to 15 days"]
-[9.487908363342285, 7.165527820587158, "[TT] Spatial Resolution of the IMI = Better than real aperture system"]
-[6.718654632568359, 1.1261935234069824, "[TT] Observation Date of the Solar Dynamics Observatory = July 30, 2011"]
-[6.227695941925049, 3.6442177295684814, "[FF] Risk of the ASAP = Loss of Mission"]
-[8.16607666015625, 7.650218486785889, "[TT] Detector Type of the TIR Subsystem = Mercury cadmium telluride (HgCdTe)"]
-[9.676328659057617, 8.336071014404297, "[TT] FOV (Field of View) of the Medium resolution = 54\u00ba 30'"]
-[13.268067359924316, 5.244932174682617, "[TT] Effective Active Area of Solar Arrays of the CHEOPS = Just over 2.1 m2"]
-[12.791062355041504, 7.67095422744751, "[TT] Design of the LCT = One-unit"]
-[4.704190731048584, 1.5077818632125854, "[FF] Observation Operations Start Date of the GCOM-W1 = August 13, 2012"]
-[3.7950360774993896, 1.1635264158248901, "[TT] Booster Reuse Count of the Falcon 9 = Three times"]
-[10.204327583312988, 1.3805328607559204, "[TT] Number of Extragalactic Sources of the Gaia EDR3 = More than 1.6 million"]
-[3.4405646324157715, 4.836166858673096, "[FF] Purpose of the TOPSAR = Wide swath imaging"]
-[10.6959228515625, 2.8256266117095947, "[FF] Design Options of the Microsatellite = NFI + STEAM, or a WFI"]
-[11.058640480041504, 3.63484525680542, "[TT] Platform Size of the MicroMAS-2 CubeSat = 10 x 10 x 34 cm"]
-[7.095282077789307, 5.22227144241333, "[FF] Function of the VMC = Visual Monitoring"]
-[8.009247779846191, 2.686246156692505, "[TT] Measurement Domain of the IRS-P6 = Land, Snow & Ice"]
-[14.019556045532227, 3.760732650756836, "[TT] Mass of the Laser = < 10 kg"]
-[8.177966117858887, 3.0001513957977295, "[TT] Number of Instruments of the Geostationary Lightning Mapper (GLM) = 1"]
-[6.3006591796875, 4.480288982391357, "[TT] Simulation Platform of the IMI = Matlab"]
-[8.550232887268066, 3.567828416824341, "[TT] Detector of the Extinctive Stellar Occultations = Spectrometer"]
-[5.197227478027344, 2.4246883392333984, "[TT] Agency of the THEOS-2 = GISTDA"]
-[4.807217597961426, 6.627711296081543, "[FF] Module Size of the Wireless Compose-2 = Roughly the size of a small smartphone"]
-[4.672370433807373, 6.296983242034912, "[TT] Compatibility of the Frontier Radio = NASA's STRS (Space Telecommunications Radio System) architecture"]
-[8.106507301330566, -0.1538916677236557, "[FF] Warming Rate of the Arctic regions = Twice as fast as the rest of the world"]
-[3.3483779430389404, 1.497536301612854, "[FF] Launch Date of the Sentinel-3B = Unknown"]
-[9.535735130310059, 0.7403277158737183, "[TT] Distance from the Sun at First Perihelion of the Solar Orbiter = Around 77 million kilometers"]
-[7.959908485412598, 7.544088363647461, "[TT] SNR of the Imager = 100:1"]
-[9.493104934692383, 7.0417304039001465, "[TT] Radiometric Resolution (K) of the PMI = 0.3"]
-[9.693561553955078, 4.051270961761475, "[TT] Observation of the Magnetic Null = In situ"]
-[9.525116920471191, 6.163010597229004, "[TT] Angle of Incidence of the TopSAR narrow = 20\u00b0 - 45\u00b0"]
-[5.393310546875, 2.2402303218841553, "[TT] Project Manager of the HORYU-4 = Professional staff"]
-[5.856199741363525, -2.2790563106536865, "[TT] Orbital Altitude of the KOMPSAT-3 = 685 km"]
-[9.079611778259277, 1.3817105293273926, "[FF] Public Engagement of the New Horizons = Broke NASA records, touched lives, and awed the world"]
-[8.696687698364258, 2.137413740158081, "[TT] Location of the WIND = L1 halo upstream of Earth"]
-[4.9239182472229, -0.27738577127456665, "[TT] Launch Time of the SES-17 = 02:10 UTC"]
-[7.430989742279053, 8.356504440307617, "[TT] Number of Rows of the QWIP Array = 512"]
-[11.39649486541748, 4.396210670471191, "[TT] Size of the OptiCube-2 = 3U"]
-[13.77661418914795, 2.7588016986846924, "[TT] Launch Mass of the SAC-D spacecraft = 1515 kg"]
-[9.458627700805664, 9.170563697814941, "[TT] Data Rate for Spectra of the IRIS = Every 1\u20132 s"]
-[5.839169502258301, 0.14343984425067902, "[FF] Onboard Performance Duration of the EO-1 Hyperion = Eight years"]
-[4.901243686676025, 7.308046340942383, "[TT] Data Transmission Rate of the S-band = 16 kbit/s"]
-[6.299300670623779, 4.45028829574585, "[FF] Function of the NanoMind A3200 OBC = Stores mission-specific commands"]
-[10.004217147827148, 2.90278697013855, "[FF] Launch Date of the CubeSats = Dec. 9, 2013"]
-[5.076388835906982, 4.05000114440918, "[TT] Provider of the Argos DCS = CNES"]
-[14.019942283630371, 2.911738157272339, "[TT] Launch Mass of the DMSP F-18 = 1230 kg"]
-[13.890231132507324, 2.691037654876709, "[TT] Launch Mass of the GSAT-30 = 3357 kg"]
-[10.928680419921875, 7.558524131774902, "[TT] Swath Width of the Swath width = 30 km"]
-[9.586718559265137, 0.8238491415977478, "[TT] Closest Approach Distance of the Rosetta = 800 km"]
-[7.607171535491943, 6.481272220611572, "[TT] Image Capture Frequency of the Elektro-L = Every 15-30 minutes"]
-[5.7965850830078125, 4.850622653961182, "[FF] Signal Augmentation of the MTSAT = GPS wide-area signal augmentation"]
-[7.4535908699035645, 2.1067750453948975, "[FF] Technical Specification of the Vegetation-2 = Identical to Vegetation flown on SPOT-4"]
-[5.212182998657227, -0.30485162138938904, "[TT] Launch Time of the ALOS-2 = 03:05 UTC"]
-[13.346084594726562, 7.830671310424805, "[TT] Power of the X-band Transmitter = 3.4 W"]
-[7.644745826721191, 5.660284996032715, "[FF] Sensors of the VBN Demonstration = Standard high quality camera and a flash imaging LiDAR system"]
-[9.322028160095215, 5.304595947265625, "[TT] Stabilization of the Navigation and Stabilization = \u00b12.5 arcsec"]
-[11.315895080566406, 4.350210189819336, "[TT] Size of the CSIM-FD = 6U"]
-[3.8053886890411377, 6.336467742919922, "[TT] Antennas of the Yutu-2 = Three 5-meter antennas"]
-[6.004605770111084, 0.5272453427314758, "[TT] Survey Date of the ATM = April 11, 2012"]
-[6.137657642364502, 0.5218085050582886, "[FF] Data Sets of the Rosetta = Surprising"]
-[14.11623477935791, 3.2879416942596436, "[TT] Mass of the RemoveSat = ~100 kg"]
-[9.568268775939941, 7.0849480628967285, "[TT] Resolution of the OLS = 2.77 km"]
-[4.973765850067139, 0.4591290056705475, "[FF] Implementation Date of the QZSS L1-SAIF Message Generator = Jan. 28-30, 2008"]
-[5.294630527496338, 0.015239651314914227, "[FF] Expected Hatch Opening Time of the NG-10 Cygnus = Later today"]
-[6.962860584259033, 1.8913764953613281, "[FF] Mission of the Orbiting Carbon Observatory = Unknown"]
-[11.447827339172363, 5.797277450561523, "[TT] Material of the Platform Structure = Composite honeycomb aluminium panels"]
-[10.765671730041504, 1.1285966634750366, "[TT] Mass Compared to Earth of the TOI 270 c = 7 times Earth\u2019s mass"]
-[4.47749137878418, 4.321172714233398, "[TT] Number of the COSPAS-SARSAT Payloads = 2"]
-[6.245184898376465, 8.647466659545898, "[TT] Polarization Mode of the TopSAR wide = HH or HV or VH or VV"]
-[11.791781425476074, 6.753761291503906, "[TT] Energy Range of the SEM-2 = 42.9-300 keV"]
-[7.382400035858154, 3.829922676086426, "[FF] Unknown of the NighPod = Unknown"]
-[11.588826179504395, 6.644765853881836, "[TT] Power of the Particle Detectors = 20 - 50 V"]
-[5.006406307220459, 3.411306381225586, "[TT] Manufacturer of the Lee Solenoid Valve = Lee"]
-[10.122659683227539, 7.124889850616455, "[TT] Cell Resolution of the OSCAT = 25 km x 25 km"]
-[12.211971282958984, 0.5816712379455566, "[TT] Purpose of the Plato = Find and study extrasolar planetary systems"]
-[10.677154541015625, 5.943966865539551, "[TT] Opening Angle of the CsI(Na) Shield = 16\u00ba"]
-[9.695076942443848, 1.721702218055725, "[FF] Purpose of the Herschel = Map the star formation in clusters by measuring the far-infrared emission from the particles of dust"]
-[3.5271503925323486, 1.807783842086792, "[FF] URL of the Sentinel-1 = http://m.esa.int/Our_Activities/Observing_the_Earth/Copernicus/Sentinel-1/Satellites_shed_new_light_on_earthquakes"]
-[4.756204128265381, -1.8309026956558228, "[TT] Landing Date of the Chang'e-4 = 3 January 2019"]
-[9.273655891418457, -1.1922755241394043, "[TT] Orbit of the GOES-R = Geostationary orbit at a longitude of 75\u00b0 West"]
-[12.129607200622559, 1.9738565683364868, "[TT] Revisit Time of the Cartosat-2E = Four-day"]
-[8.885405540466309, 2.911877155303955, "[FF] Mass of the Neutral winds = More than ions"]
-[5.612577438354492, 7.087158679962158, "[TT] Telemetry Data Rate of the Instrument = 8 kbit/s"]
-[9.670988082885742, 7.004297733306885, "[TT] Spatial Resolution of the SSM/IS = Varies with the frequency with the highest spatial resolution of 25 km x 17 km and the lowest at 70 km x 42 km"]
-[6.307234287261963, 6.968893051147461, "[TT] Fiber Optics Link Speed of the MIRAS = 110 Mbit/s"]
-[6.7233805656433105, 3.3135082721710205, "[FF] Data Size of the Earth Observation Services = Massive and large-sized data"]
-[7.531687259674072, 7.972263813018799, "[TT] Signal to Noise Ratio (SNR) of the Climate Observatory = ~300 in the vis-NIR"]
-[10.972023010253906, 0.5861971974372864, "[TT] Number of Stars with Multiple Planetary Candidates of the Kepler = 170"]
-[10.968168258666992, 6.027996063232422, "[TT] Components of the PLS = Four Faraday cups"]
-[9.782508850097656, 7.220616817474365, "[TT] Vertical Spatial Resolution of the MTVZA-GY = 1.5 - 7 km"]
-[6.606707572937012, 8.451525688171387, "[FF] Measurement Channels of the POLDER = 15 channels (three channels for each polarized band)"]
-[4.833575248718262, 7.242607116699219, "[TT] Downlink Data Rate of the TT&C S-band Communications = 722.116 kbit/s"]
-[9.127751350402832, -1.2365719079971313, "[TT] Orbit of the Himawari-9 = Geostationary"]
-[4.831956386566162, 0.5539802312850952, "[TT] Operation Start Date of the Metcomp experiment = 3 December"]
-[4.795983791351318, 6.1914963722229, "[FF] Operation of the Frontier Radio = Hardened to continue working even in the harshest conditions"]
-[13.387277603149414, 7.4196248054504395, "[TT] Output Power of the STX-01 = 30 dBm"]
-[3.4774258136749268, -0.9237334728240967, "[TT] Orbit Type of the NEMO-AM = Sun-synchronous orbit"]
-[8.213886260986328, 7.083984851837158, "[TT] Data Type of the TanDEM-X = Quicklook images"]
-[7.466929912567139, 3.479593276977539, "[FF] Deorbiting Requirement of the IDEA OSG 1 = IDEA OSG 1 should, after termination of its mission, attempt to deorbit in order to meet the 25 year debris mitigation guideline"]
-[4.9799041748046875, 3.371072292327881, "[TT] S/C Manufacturer of the ADEOS-II = Mitsubishi Corporation"]
-[8.028099060058594, 0.7911849021911621, "[FF] Drought Intensity of the GRACE = Second most intense since 2002"]
-[11.693167686462402, 4.544968605041504, "[TT] Size of the Didymos A = About one-half mile"]
-[8.133027076721191, 8.819350242614746, "[TT] Resolving Power of the CarbonSpec = Near 21,000 in the A-band, near 12,000 in the CO2 bands"]
-[3.8933844566345215, 4.477497577667236, "[TT] Data Access of the RADARSAT-2 = Free"]
-[6.220153331756592, 2.0841174125671387, "[FF] Future Mission of the GEO-CAPE = Yes"]
-[10.555648803710938, 2.1654880046844482, "[FF] Publication Date of the S-054 X-ray Telescope = Feb. 1977"]
-[8.70915412902832, 7.69436502456665, "[TT] Photodetector Model of the Optical Head = MT 9M001 by Micron Technology, Inc."]
-[7.3007917404174805, 4.491663932800293, "[TT] ECP Sensor of the WSF-M = Hosted Government furnished"]
-[8.06234359741211, 4.930387496948242, "[TT] Calibration Frequency of the MAC = Periodic basis"]
-[6.91814661026001, 8.050837516784668, "[TT] Noise Equivalent \u03c3o of the ALScat = 0 dB to -40 dB"]
-[8.418619155883789, 7.841195106506348, "[TT] Array Design of the Argo Array = Global 3\u00ba x 3\u00ba"]
-[6.324775218963623, 0.7161375284194946, "[FF] Survey Date of the Gaia = 13 June 2022"]
-[7.657313823699951, 6.451491355895996, "[FF] Targeted Processing Time of the Image processing system = Less than one hour from image acquisition"]
-[4.9089508056640625, -0.5726802945137024, "[TT] Launch Date of the SLATS = December 23, 2017"]
-[7.957278728485107, 8.838204383850098, "[TT] Wavelength Range of the TSIS-1 SIM = 200\u20132400 nm"]
-[3.253422498703003, 5.538206100463867, "[TT] Side Lobe Level of the SAR antenna = -13 dB (azimuth), -13 dB (elevation)"]
-[11.81219482421875, 6.7339863777160645, "[TT] Energy Range of the EPI-Lo = ~25 keV to 1000 keV"]
-[13.060811042785645, 7.291811943054199, "[TT] Power of the Magnetometer = < 0.8 W"]
-[5.047905445098877, 2.6795082092285156, "[TT] Mission Operations Center of the NuSTAR = UC Berkeley"]
-[4.952316761016846, 3.4640300273895264, "[TT] Manufacturer of the EDRS-C = OHB System"]
-[8.295084953308105, 8.756170272827148, "[TT] Spectral Resolution of the O2-A = 0.044 nm"]
-[8.312237739562988, 7.559023857116699, "[TT] Detector Types of the Spectrometer = Silicon and extended InGaAs photodiodes"]
-[4.758610725402832, 0.6452943682670593, "[TT] MetOp Services Start of the EPS = 2005/6"]
-[10.16342830657959, 2.080522298812866, "[TT] Mission Name of the Chandra X-ray Observatory = Chandra X-ray Observatory"]
-[14.261242866516113, 3.2468628883361816, "[TT] Mass of the NSX = 1.5 kg"]
-[5.274872303009033, 0.6927245855331421, "[TT] Data Record Start of the CERES FM6 = 1997"]
-[7.602412700653076, 2.250822067260742, "[FF] Mission Purpose of the Tandem-L = Climate research and environmental monitoring"]
-[10.906103134155273, 2.0934321880340576, "[FF] Data Representation of the XMM-Newton = Blue squares"]
-[9.272154808044434, 3.241457939147949, "[TT] Main Instrument of the Coronagraph Spacecraft (CSC) = Coronagraph"]
-[7.146216869354248, 6.629119396209717, "[TT] Threshold Optimization of the GLM = Post-launch test"]
-[6.44503116607666, 0.6096267104148865, "[TT] Launch Date of the Landsat-6 = October 1993"]
-[8.210192680358887, 4.6329779624938965, "[TT] TID Radiation Test of the Tested Devices = Up to 50 krad (Si)"]
-[9.446691513061523, 6.367556571960449, "[TT] Scan Path of the Two-axis gimbaled mirror scan system = Predominantly N/S"]
-[4.742373466491699, 7.128031253814697, "[TT] Data Rate of the X-band Data Downlink = 560 Mbit/s"]
-[5.786482810974121, 4.253039360046387, "[FF] Primary Aim of the TESSA = Improve performance analysis of the SSN (Space Surveillance Network)"]
-[10.238897323608398, 7.987842559814453, "[TT] Area of the Telescope = 10 mm x 10 mm"]
-[11.933072090148926, 4.961662769317627, "[TT] Dimensions of the COVE Board = 90 mm x 90 mm"]
-[7.816442012786865, 1.559031367301941, "[FF] Calibration Data of the GPM = Measurements from the GPM Core Observatory and rain gauge networks around the world"]
-[4.993031024932861, 7.36092472076416, "[TT] Data Transmission Streams of the RF communications = 25 kbit/s, 800 kbit/s, 20 MHz"]
-[13.063437461853027, 7.602298736572266, "[TT] Total Power of the AlSAT-1 = 240 W"]
-[12.619853973388672, 9.099233627319336, "[TT] Equatorial Crossing Time of the CanX-2 = 9:30 hours"]
-[3.136115789413452, 2.2038543224334717, "[FF] Areas of Focus of the Copernicus Programme = Climate change and global warming"]
-[10.064986228942871, 3.9140961170196533, "[FF] Purpose of the CarboNIX = Test a new \u201cshock-free\u201d payload deployment mechanism"]
-[7.604680061340332, -2.5196409225463867, "[TT] First Image Capture Date of the GOLD = 17 September 2018"]
-[7.8729143142700195, 5.368121147155762, "[FF] Compatibility of the Metrology System = Not work with an integrating detector"]
-[7.731433868408203, 9.48906421661377, "[TT] Center Wavelength of the B10 = 1375 nm"]
-[8.239988327026367, 7.279009819030762, "[TT] Sensor Technology of the C3D Instrument = 0.18 \u00b5m CMOS technology"]
-[7.369906902313232, 3.262573003768921, "[FF] Limb Sounder of the EnviSat = MIPAS"]
-[10.79411506652832, 1.6558079719543457, "[FF] Purpose of the Laser Interferometer Space Antenna = Detect the telltale ripples in gravitational fields caused by the mergers of neutron stars, black holes, and supermassive black holes in space"]
-[4.885469913482666, 7.325171947479248, "[TT] Downlink Beacon Data Rate of the RF Communications = 20 bit/s"]
-[7.6551947593688965, 0.26015666127204895, "[TT] Launch Date of the Lucy = October 2021"]
-[14.101404190063477, 7.166839122772217, "[TT] Voltage Range of the BIT-3 system = 28-37 V"]
-[2.901561975479126, 1.9693673849105835, "[FF] Image Capture Date of the Copernicus Sentinel-2B = 27 October 2017"]
-[10.681929588317871, -1.203196406364441, "[TT] Orbit of the SLATS = Initial sun-synchronous elliptical orbit, altitude 643 x 450 km, inclination of 98.3\u00ba"]
-[8.229329109191895, 8.553580284118652, "[TT] Channel 5 Wavelength Range of the FT Spectrometer = 10.6-13 \u00b5m"]
-[10.361536979675293, 7.949019908905029, "[TT] Fabrication Finesse of the Etalon = \u2265 30"]
-[6.8449249267578125, 4.778642177581787, "[FF] Prototype of the Instrument Controller Electronics (ICE) = Built and tested by Ball"]
-[11.558024406433105, 6.502591133117676, "[TT] Energy Band of the NuSTAR instrument = 5 - 79 keV"]
-[7.117098808288574, 2.48982310295105, "[FF] Edition of the Observation of the Earth and Its Environment = 4th edition"]
-[14.061006546020508, 3.176548719406128, "[TT] Total Mass of the BA 330 module = 23,000 kg"]
-[5.333806037902832, 8.553860664367676, "[TT] Bandwidth of the SCM = 10 Hz-8 kHz"]
-[9.272249221801758, 6.941852569580078, "[TT] Resolution of the Optical Satellite = 0.5 m GSD"]
-[7.334050178527832, 2.3773953914642334, "[FF] Observation Area of the GOES-16 and -17 = United States, Mexico, Central America, South America, the Caribbean and much of the Pacific and Atlantic Oceans"]
-[7.196712493896484, 7.087398052215576, "[FF] Operation of the ATLAS = Sends pulses of light to Earth"]
-[9.447070121765137, -1.0672991275787354, "[TT] Longitude of the GOES-R = 75\u00ba West and 137\u00ba West"]
-[8.806655883789062, 0.8527795076370239, "[FF] Mission Objective of the DART = Collide with an asteroid and deflect it from its orbit"]
-[6.744322776794434, 3.2815282344818115, "[TT] Reduction in Satellite Loss of the SBSS-1 = 66%"]
-[9.555767059326172, 1.1767909526824951, "[TT] Speed of the Heliosphere = 52,000 miles per hour"]
-[4.77083158493042, 7.879664897918701, "[TT] Alert Signal Frequency of the EPIRB = 406.025 MHz"]
-[14.531351089477539, 6.6047539710998535, "[TT] Battery Capacity of the Spacecraft = 2 x 21 Ah"]
-[4.8000054359436035, 7.0531158447265625, "[TT] Operation Mode of the S-band transponder = Full duplex"]
-[14.3394193649292, 2.7575461864471436, "[TT] Mass of the Kolibri-2000 = 20.5 kg"]
-[3.849423885345459, 7.868198394775391, "[TT] Modulation of the CW transmitter = FSK"]
-[4.919073581695557, 5.914659023284912, "[FF] Crosslink Communications of the INSPIRE = Demonstrated early in the mission timeline"]
-[11.490371704101562, 4.773645401000977, "[TT] Diameter of the Pivot Irrigation Fields = Around 750 m"]
-[8.697712898254395, 3.721236228942871, "[FF] Mission of the Space-based telescopes = Actionable refinement of ephemeris pathfinder"]
-[5.036923408508301, 1.8951308727264404, "[TT] Status of the Carmen-2 = Performing well"]
-[4.973940849304199, 3.5504958629608154, "[TT] Manufacturer of the OBC = Atmel"]
-[6.032085418701172, 1.6338292360305786, "[FF] Symposium Date of the Small Satellites = May 4-7, 2009"]
-[12.009696006774902, 6.563290596008301, "[TT] Energy Range of the AMS = 20-200 GeV"]
-[14.093565940856934, 3.205369234085083, "[TT] Mass of the Carbonite-2 = ~100 kg"]
-[5.413361072540283, -0.7155200242996216, "[FF] Deployment Date of the Jade Rabbit = Dec. 14, 2013"]
-[11.134880065917969, 5.184842109680176, "[FF] Experiment Date of the X-ray Gas Scintillation Spectrometer = July 13, 1984"]
-[8.130450248718262, 2.326338529586792, "[FF] Measurement of the Multibeam Thermal-Infrared Instrument = Sea-surface temperature differences"]
-[5.384066104888916, 2.3783695697784424, "[TT] Mission Type of the CUTE = Astronomy"]
-[6.017762660980225, 6.8466105461120605, "[TT] Lossy Compression Ratio of the HSDR FPGA = 4:1 or higher"]
-[10.290407180786133, 5.82987642288208, "[TT] In-orbit Environmental Temperatures of the AEISS telescope = -10\u00baC ~ +45\u00baC"]
-[13.685574531555176, 2.7242205142974854, "[TT] Launch Mass of the TanSat = 620 kg (including 10 kg propellant)"]
-[6.335428237915039, 1.9138695001602173, "[FF] URL of the TeleSupport-2-bis = http://www.prismasatellites.se/filearchive/3/3615/2005%20tsuengelsk.pdf"]
-[5.785956859588623, 3.6983468532562256, "[FF] Status of the DMSP-F13 = Oldest continuously operational satellite in the DMSP weather constellation"]
-[5.401487350463867, 6.758572578430176, "[TT] Data Volume of the RF Communications = ~ 4 GB/day"]
-[7.907292366027832, 2.8903071880340576, "[FF] Estimation Accuracy of Flux of the GOSAT = Reduce the estimation error on the sub-continental scale to half compared with the one estimated using only ground observation data, Estimate the monthly net fluxes with the accuracy of \u00b1100%"]
-[8.18525505065918, 1.2252684831619263, "[FF] Importance of the SMAP = Timely and accurate knowledge of the root-zone soil moisture is very important for farmers, stakeholders, and agricultural agencies"]
-[6.4480180740356445, 2.0733916759490967, "[FF] Design and Performance of the eROSITA = Not provided"]
-[4.600240230560303, 2.508695125579834, "[TT] Coverage Area of the Kleos Scouting Mission (KSM1) = South China Sea and Strait of Hormuz"]
-[9.908695220947266, -1.5028165578842163, "[TT] Orbital inclination of the GALILEO = 56\u00ba"]
-[10.13672161102295, 8.109248161315918, "[TT] Focal Length of the Telescope = 522 mm"]
-[1.7221943140029907, 6.140114784240723, "[FF] Effect of the Dark Energy = Shoving galaxies away from each other"]
-[13.143966674804688, 7.280430316925049, "[TT] Power Consumption of the MIRAD = 500 mW"]
-[5.7664408683776855, 4.700827598571777, "[FF] Operation of the EDRS = RF feeder link between Alphasat and its ground segment"]
-[6.8248491287231445, 3.254774808883667, "[TT] Number of Satellites Waiting to be Launched of the GHGSat = Two"]
-[7.95670747756958, -0.6409858465194702, "[FF] Feeder Link of the EFAL = Antarctic Latitudes"]
-[6.532712459564209, 6.543511867523193, "[TT] Time Slot of the DCP = 27 seconds"]
-[10.895445823669434, 3.9000439643859863, "[TT] Formation Ranges of the CanX-5 = 1000 m, 500 m, 100 m"]
-[8.525755882263184, 4.59894323348999, "[FF] Function of the ASTERIA = Stabilizes the position of a star image on the telescope detector"]
-[5.557704925537109, 5.5798234939575195, "[TT] Microprocessor of the Beresheet lander = LEON3 cores"]
-[9.863039016723633, -0.6026768684387207, "[TT] Orbit Altitude of the Primary Mission = 824 km"]
-[8.641090393066406, 6.009200572967529, "[TT] Measurement Precision of the SOFIE = T 0.2 K, O3 11 ppbv, H2O 70 ppbv, CH4 5 ppbv, PMC extinction 5 x 10 -8 km -1"]
-[6.275234222412109, 0.08845021575689316, "[TT] Patent Number of the Helix Orbit = US 6,677,884 B2"]
-[13.887678146362305, 2.7617530822753906, "[TT] Launch Mass of the EROS-A = 260 kg"]
-[4.5328688621521, 1.5194463729858398, "[TT] Launch Date of the GOSAT-2 = 29 October 2018"]
-[7.875585079193115, 6.16434383392334, "[FF] Model of the Imager = MODTRAN"]
-[5.114708423614502, 0.17021700739860535, "[TT] Replacement Year of the TSIS-2 = 2023"]
-[9.387381553649902, 5.3451828956604, "[TT] Typical Azimuth Alignment of the Inertial Reference Systems = 90 degrees"]
-[6.663602352142334, 1.8112188577651978, "[FF] URL of the GFO = http://gfo.wff.nasa.gov/"]
-[6.388952255249023, -0.9513237476348877, "[TT] Checkout Phase Duration of the GRACE-FO = 85 days"]
-[5.763245105743408, 4.1468825340271, "[FF] Access Availability of the Inmarsat BGAN Service = 24/7"]
-[5.321163654327393, 0.839141309261322, "[TT] Arrival Date of the Electro-L = February 3, 2011"]
-[10.947667121887207, 7.523482799530029, "[TT] Swath Width of the SSM/I = 1400 km"]
-[7.6197614669799805, 0.8168814778327942, "[FF] Mission Title of the LUMIO = Characterizing lunar meteoroid impacts"]
-[3.320791482925415, 5.584366321563721, "[TT] Number of TRMs of the L-band SAR antenna = 180"]
-[8.624154090881348, 5.9275803565979, "[TT] Image Geolocation Accuracy of the SSTL-300 bus system = < 35 m (CE90 = Circular Error 90%)"]
-[11.961602210998535, 5.016294956207275, "[TT] Size of the DCG = 260 mm x 210 mm x 150 mm"]
-[8.077744483947754, -2.372039318084717, "[TT] Altitude of the GOLD = Around 160 km"]
-[12.074604988098145, -0.2273373007774353, "[TT] Southern Sky Study Duration of the TESS = First year of operations"]
-[4.900234222412109, 2.6833295822143555, "[TT] Operator of the Odin = OHB Sweden, on behalf of the Swedish National Space Agency (SNSA) and the Swedish Space Corporation (SSC)"]
-[8.222204208374023, 4.095274925231934, "[FF] Instruments of the Psyche spacecraft = Magnetometer, multispectral imager, spectrometers"]
-[8.820313453674316, 5.627983570098877, "[TT] Horizontal Velocity Error of the TAG Contact Safety Requirements = Under 2 cm/s (3\u03c3)"]
-[8.714776039123535, 3.8370301723480225, "[FF] ESA: electrons, ISA: ions of the Particle Species = ESA electrons, ISA: ions"]
-[4.9518632888793945, 7.835618495941162, "[TT] Processing Frequency of the RPU = 401.6 MHz"]
-[7.499340057373047, 4.100108623504639, "[FF] Instrument Similarity of the ACC = Very similar to the SuperSTAR instrument operating for the last 10 years on board the twin GRACE-1 satellites"]
-[8.805373191833496, 5.627685070037842, "[TT] Pointing Requirements of the VLF Antennas = 2\u00ba control and a 1\u00ba knowledge requirements"]
-[8.662312507629395, 5.235895156860352, "[FF] Accuracy of the CLARREO Pathfinder = 4 to 8 times more accurate than current best available sensors on orbit"]
-[3.4434969425201416, 1.7278759479522705, "[FF] Campaign of the Sentinel-1 = AgriSAR 2009"]
-[11.93615436553955, 6.197023391723633, "[FF] Purpose of the AMS-02 = Look for antimatter in cosmic rays above the atmosphere"]
-[10.798416137695312, 4.247876167297363, "[FF] Function of the \u00b5C = Regulates the direct current power supply of the pump"]
-[5.769414901733398, 7.202220439910889, "[TT] Output Data Rate of the IRM = 0-300 kwords/s"]
-[6.27000617980957, 8.165637969970703, "[TT] Channels of the MERSI-RM = 8"]
-[14.621094703674316, 6.644904613494873, "[TT] Batteries of the EPS = 2 Rose Li-ion batteries"]
-[8.564322471618652, 2.8156163692474365, "[TT] Range of measurements of the Atmosphere = 0-25 mm/h"]
-[5.931759834289551, 2.0881950855255127, "[TT] Location of the EuTEF = Outside of the Columbus laboratory"]
-[4.797833442687988, 2.9918503761291504, "[TT] Location of the MC3 CGA = NPS (Naval Postgraduate School), Monterey, CA"]
-[8.677401542663574, -0.19666078686714172, "[TT] Perigee (km) of the Meteor-1-2 = 630"]
-[7.242934226989746, 9.000778198242188, "[TT] Filter Center of the MCS = 762 nm"]
-[4.443476676940918, 7.7364583015441895, "[TT] VHF Band Frequency of the RF Communications = 144 MHz"]
-[10.850371360778809, 7.4458465576171875, "[TT] Swath width of the ALOS/PRISM = 35 km / 70 km"]
-[8.14964485168457, 4.56915807723999, "[FF] Research Topics of the MEMS Space Telescope = Unknown"]
-[10.712491989135742, 1.1993509531021118, "[TT] Atmosphere Mass of the Earth = Less than one millionth of the total mass of Earth"]
-[13.781760215759277, 5.33565092086792, "[TT] Amplifiers of the RainCube = GaAs solid-state"]
-[5.157703876495361, 2.325385332107544, "[TT] Mission Type of the PSat-2 = Non-EO"]
-[8.74431324005127, 7.640384674072266, "[TT] Size of the CCD Window = 636 pixels (939 pixels for the fast cameras)"]
-[11.746699333190918, 6.551804542541504, "[TT] Gd Cross Section for Thermal Neutrons of the LND = 48\u2019890 b"]
-[4.560268878936768, 3.440187931060791, "[TT] Ground Operator Location of the NPSat-1 = NPS (Naval Postgraduate School) in Monterey, California"]
-[10.451057434082031, 2.2226595878601074, "[FF] Purpose of the X-ray Space Telescopes = Study X-ray light"]
-[9.216154098510742, 3.1490166187286377, "[FF] Signal Modulation Causes of the IMAP = 1) the small inclination of the ISN gas inflow direction to ecliptic 2) due to the latitudinal structure of solar wind flux (Ly-\u03b1) and the solar wind electron density and temperature (He 58.4)"]
-[13.880011558532715, 7.197775363922119, "[TT] Output Open Circuit Protection of the DC-DC converter = Yes"]
-[9.26614761352539, 2.0321078300476074, "[FF] Calibration Method of the VBN system = Uses the previous net and harpoon experiments"]
-[7.264764308929443, 2.3581957817077637, "[TT] Measurement Type of the GEOSAT Radar Altimeter (GRAS) = High-precision range measurements between the satellite and the subsatellite point at nadir"]
-[7.172175884246826, 0.9331412315368652, "[FF] Date of the Kaik\u014dura earthquake = 23 Mar 2017"]
-[13.423233032226562, 6.912582874298096, "[FF] Power Range of the Small-GEO = 2.5 kW to 7.5 kW"]
-[8.27503776550293, 6.078323841094971, "[FF] Measurement Capability of the Piezoelectric Elements = Acoustic waves propagating through the satellite structure"]
-[6.575772762298584, 6.2569451332092285, "[TT] Flight Heritage of the LCT (Laser Communications Terminals) = Over 15 years"]
-[14.74365234375, 6.606772422790527, "[TT] Capacity of the Li-ion battery = 225 Whr"]
-[9.78052043914795, 8.22996997833252, "[TT] Field of View of the NuSTAR = 12 arcminute"]
-[3.998464345932007, 4.104941368103027, "[FF] Mission Objectives of the FSSCat = Polar Ice and Snow monitoring, soil moisture monitoring, terrain classification and terrain change detection"]
-[14.68297004699707, 6.665767669677734, "[TT] Capacity of the BAT = 50 Ah"]
-[4.527076244354248, 6.645246505737305, "[FF] Communication System of the CM1 and CM2 = Phased array communication system"]
-[5.4701337814331055, -0.6337141990661621, "[TT] Design Life of the Odin = Two years"]
-[8.429893493652344, 5.982576370239258, "[TT] Precision of Trigger Binding of the RFA = 1 \u00b5s"]
-[3.773405075073242, 6.603241443634033, "[TT] VDES Antenna Elements of the NorSat-2 = Three"]
-[6.528566360473633, -1.2388252019882202, "[FF] Data Continuity of the GRACE-FO = Maintaining data continuity from GRACE"]
-[13.343827247619629, 5.4978814125061035, "[TT] Quantity of the Solar Panels = 4 3U double sided solar panels and 1 additional 2U solar panel"]
-[4.966981410980225, 0.5146704316139221, "[TT] Launch Date of the RESURS-O1-4 = July 10, 1998"]
-[8.316593170166016, 8.321165084838867, "[TT] Multispectral Band: Blue of the NAOMI = 0.45 \u00b5m - 0.52 \u00b5m"]
-[8.760822296142578, 7.685160160064697, "[TT] Pixel Size of the VISIM = 7.4 \u00b5m"]
-[13.803936958312988, 6.952776908874512, "[TT] Output Potential of the SCM = Fluctuates between 250 and 310 V"]
-[7.061334133148193, 8.211405754089355, "[TT] Value of the SNR = > 100 (peak)"]
-[8.797133445739746, 9.41675853729248, "[TT] Spectral Band 4 Number of Pixels of the TANSO-CAI = 500"]
-[13.064875602722168, 7.393603324890137, "[TT] Power Consumption of the GPS OEM Sensor = About 0.5 W"]
-[11.159579277038574, 5.855844020843506, "[TT] Material of the Baffle = CFRP laminate"]
-[8.639389038085938, 1.0814456939697266, "[FF] Commissioning Phase End Date of the Aquarius = End of July"]
-[6.235175609588623, 5.971567153930664, "[FF] Control of the TR-modules = Off in the width direction"]
-[8.256794929504395, -0.7521019577980042, "[FF] Ice Movement Resolution of the Map = 20 cm/year in speed and 5 degrees in annual flow direction"]
-[9.66208267211914, 8.346959114074707, "[TT] Field of View (FOV) of the BEO = 0.32\u00ba"]
-[1.7444381713867188, 4.561049938201904, "[FF] N/A of the power = N/A"]
-[6.244642734527588, -0.043088190257549286, "[TT] Timeliness of Data Availability of the Aeolus = 3 hours"]
-[6.765186309814453, 2.9475228786468506, "[TT] Purpose of the Spire = Collect global weather data"]
-[5.8520188331604, 2.7652671337127686, "[FF] Phase A/B1 Study Contracts of the OPS-SAT = Awarded to TU Graz and GOMSPACE"]
-[9.686527252197266, 7.124860763549805, "[FF] Data Acquisition Sites of the VSSC = Existing or planned experimental sites with sizes ranging from 27 km x 27 km to 27 km x 54 km or more"]
-[7.63810920715332, 2.0502281188964844, "[FF] Band 5 of the Landsat TM = Vegetation moisture measurement, snow/cloud differentiation"]
-[5.027959823608398, 0.5071334838867188, "[TT] Launch Date of the Enxaneta = March 2021"]
-[5.393369674682617, 3.2003681659698486, "[FF] Business Unit of the Maxar = SSL"]
-[13.008776664733887, 6.878052234649658, "[TT] Energy Consumption of the Nominal Mode = More than Safe Mode"]
-[10.097992897033691, -1.5109837055206299, "[TT] Orbit Inclination of the Satellite = 98.5\u00ba"]
-[6.1184186935424805, 2.4139108657836914, "[TT] Safe Reentry Capability of the Orion = Yes"]
-[5.071192741394043, 7.583427906036377, "[TT] G/T of the 7.5 m Cassegrain antenna system = 32 dB/\u00b0K @ 5\u00b0 EL"]
-[8.599106788635254, 3.071288824081421, "[FF] Measurement of the ROSA = POD"]
-[4.941540241241455, -0.3526149392127991, "[TT] Launch Time of the FY-4B = 17:29 UTC"]
-[7.172094821929932, 7.345520496368408, "[TT] Signal Photon Density of the MABEL = 3.4 photons per 70 cm"]
-[8.678950309753418, 7.765429496765137, "[TT] Number of Images for Signal to Noise Ratio of the EyeSat = 10 images"]
-[10.739420890808105, 7.550211429595947, "[TT] Swathwidth of the PAN = 9.6 km"]
-[5.457461833953857, 7.15460729598999, "[TT] Max Transmission Rate of the DTS = 320 Mbit/s"]
-[8.824950218200684, 7.63535213470459, "[TT] TIR Channel Windows of the Imager = 10.2-11.2 and 11.5-12.5 \u00b5m"]
-[7.409058094024658, 4.535236358642578, "[FF] Unknown of the AMS-02 TRD = Unknown"]
-[6.9152913093566895, 6.842556953430176, "[TT] Type of the Laser diode = Fiber optic pump laser diode"]
-[3.089763641357422, 2.32940411567688, "[TT] Bands Resolution of the Sentinel-2 = 20 m"]
-[8.656107902526855, 7.689115524291992, "[TT] Pixel Size of the Detector array = 10.8 \u00b5m"]
-[7.262078285217285, 0.9578788876533508, "[FF] Launch Date of the SeaSat-1 = Sept. 19, 1977"]
-[5.360906600952148, 4.948932647705078, "[TT] Bootloader-1 (BL1) of the CanX-2 = Pre-programmed EPROM"]
-[7.175373077392578, 0.9059289693832397, "[FF] Data Collection Period of the Liulin-MO dosimeter = Six-month interplanetary cruise to Mars"]
-[10.116501808166504, -1.5007905960083008, "[TT] Inclination of the Satellite = 98.13\u00b0"]
-[11.690605163574219, 4.701138019561768, "[TT] Shape of the 67P/Churyumov-Gerasimenko = Dual-lobed"]
-[5.600119590759277, 7.059436321258545, "[TT] Source Data Rate of the Payload = 336 Mbit/s"]
-[8.632375717163086, 3.861398220062256, "[FF] First US solar research satellite of the TRACE = Since the Solar Maximum Mission"]
-[4.5772576332092285, 5.646925449371338, "[TT] Global Coverage of the Distress Beacons = Yes"]
-[9.215117454528809, -0.6086783409118652, "[TT] Orbit of the MIMOSA = Elliptical orbit of 820 km x 320 km"]
-[4.955618858337402, 2.753251314163208, "[TT] Mission Operations Center of the NuSTAR = University of California, Berkeley"]
-[5.601137638092041, 3.7238926887512207, "[TT] Production Capacity of Factory of the Satellogic = 25 satellites a quarter"]
-[4.8680009841918945, 0.17770084738731384, "[TT] Structure Assembly Time of the CXBN-2 = Months rather than years"]
-[7.525570869445801, 6.538614749908447, "[FF] Data Type of the Hardware Compression Engine = JPEG imagery of the VISIM data"]
-[9.28491497039795, 3.2438204288482666, "[FF] Aperture Size of the SWAP = Largest ever used to measure the solar wind"]
-[4.58356237411499, 7.475247859954834, "[TT] Gain Setting Ability of the Intermediate Frequency Amplifier = Yes"]
-[6.215707778930664, 6.639376640319824, "[FF] Data Compression of the TTTC = Optional"]
-[5.463840961456299, 5.539009094238281, "[TT] Interface Standard of the DSX = Electrical, power, command & communications protocol"]
-[8.935359001159668, 5.45581579208374, "[FF] Solution of the BPP (Bi-axial Pointing Platform) = Use existing gyroscopes on the HRC to improve the BPP pointing control"]
-[7.259998321533203, 0.9707423448562622, "[TT] Planning Start Year of the Seasat = 1972"]
-[3.616910934448242, 2.7181313037872314, "[TT] Positional Error of the Iridium constellation of satellites = 1000 m"]
-[13.314763069152832, 7.398692607879639, "[TT] Power of the SILEX = 130 W"]
-[10.15035629272461, 1.7597402334213257, "[FF] Number of Sources of the eROSITA = Around 10 times more sources than the previous all-sky survey"]
-[14.309229850769043, 3.105882406234741, "[TT] Mass of the CEASE-1 = 1 kg"]
-[9.612916946411133, 8.20803165435791, "[TT] Field of View of the Optical Head = 94\u00ba x 81\u00ba (1-hole mask)"]
-[6.772146701812744, 4.241154193878174, "[FF] Component of the EVA Handrails = Unknown"]
-[6.672414302825928, 8.111778259277344, "[TT] NEDT (K) of the SSMIS = 0.6-0.8"]
-[5.630801677703857, 6.926496505737305, "[TT] Telemetry of the CEASE-1 = 10 byte/min"]
-[6.272315979003906, 5.1207051277160645, "[FF] Function of the Interface Modules = Interface to the hardware components and the ONS module"]
-[18.643789291381836, 3.939685583114624, "[TT] NE\u0394T of the 3 = 0.4 K"]
-[7.004282474517822, 8.101176261901855, "[FF] Dependency of the Signal to Noise Ratio (SNR) = Dependent on the choice of GIFOV and spectral bandwidth"]
-[11.644425392150879, 4.389322757720947, "[TT] Vehicle Height with 5 m short PLF of the CBAS and EAGLE = Approximately 60 m"]
-[13.379204750061035, 6.702188491821289, "[TT] Power of the KOMPSAT-3 = 1.3 kW"]
-[5.095639705657959, 0.6251218318939209, "[FF] Date of the Dnepr-1 = April 18, 2007"]
-[9.267533302307129, 3.2022640705108643, "[FF] Purpose of the Pumbaa and Timon smallsats = Obtain images of solar corona"]
-[6.045695781707764, -0.3150734305381775, "[TT] In-Orbit Design Life of the Aeolus = 36 months"]
-[9.271663665771484, 7.394115924835205, "[TT] Panchromatic Imagery Resolution of the WPM = 2 m"]
-[12.03812026977539, 3.274172306060791, "[FF] Response Time of the Iodine BIT-3 propulsion unit = Can be slow"]
-[6.867251396179199, 1.523978590965271, "[TT] Alignment Status of the Webb = Complete"]
-[8.525169372558594, 1.9636714458465576, "[TT] Spatial Resolution (km) of the Ocean surface wind speed = 25"]
-[5.118927478790283, -0.6081284284591675, "[FF] Launch Date of the TARANIS = March 1, 2011"]
-[5.120213031768799, 4.883918285369873, "[FF] Random Number Generation of the SpooQySat = Quantum random numbers"]
-[12.475103378295898, 3.1377151012420654, "[TT] Propellant Mass of the DMC Propulsion Subsystem = 2.35 kg"]
-[10.743537902832031, 7.542978763580322, "[TT] Swath Width of the NTSIC = 10 km at nadir"]
-[6.873956203460693, -0.6907637119293213, "[TT] Period of the Orbit = 13.7 days"]
-[3.038243532180786, 2.0912961959838867, "[FF] New Name Announcement Date of the Copernicus = Dec. 12, 2012"]
-[5.074212074279785, 1.9195449352264404, "[FF] Complement of the CARMEN-1 = Unknown"]
-[10.436832427978516, 5.413997173309326, "[FF] Electrical Conduction Method of the Fasteners = Conduct the electricity to a copper lug"]
-[13.634599685668945, 6.908059120178223, "[TT] Maximum Power Point Tracking (MPPT) Mode of the NanoPower P60 = Allows to gain around 20% of the input power"]
-[9.946721076965332, -0.2977231442928314, "[TT] Altitude of the Satellites = 550 km"]
-[11.945329666137695, 6.530515193939209, "[TT] Rigidity Range of the AMS = 2.65 GV to 3.0 TV"]
-[8.227673530578613, 4.503509998321533, "[FF] Orbit Accuracy Improvement of the LARES-2 = One order of magnitude"]
-[13.280081748962402, 2.9420859813690186, "[TT] Mass of the GHGSat-C2 (Hugo) = 16 kg"]
-[8.208236694335938, 6.865871906280518, "[TT] Data frame Date rate of the Full-scan Imaging = 3816 bit/s"]
-[5.145524501800537, 8.443031311035156, "[TT] Bandwidth/Passband of the 7 = 250 MHz"]
-[6.171512126922607, -0.6277949213981628, "[TT] Potential Loss Time of the NextSat = First day of the mission"]
-[6.629235744476318, 4.793010711669922, "[FF] Control Functions of the MECA = Management of the command data interface, control of the dust door, scanning mirror, rotating polarizing filter, and scanned grating"]
-[9.495400428771973, 2.387526750564575, "[TT] Count of the Halos = 2,043"]
-[6.349156856536865, 0.15972036123275757, "[FF] URL of the EP-107 Skylab = http://history.nasa.gov/EP-107/ch5.htm"]
-[5.333090305328369, 6.863245964050293, "[TT] Global Average Detection Rate of the Complex Receiver = 6 Messages/s"]
-[11.811532974243164, 4.7471160888671875, "[TT] Diameter of the Lorentz Chamber = 2.8 m"]
-[4.982988357543945, 2.9685094356536865, "[TT] Prime Contractor of the Euclid = Thales Alenia Space"]
-[5.810163497924805, 0.679162323474884, "[FF] Data Collection Period of the Cluster, Polar, Geotail, THEMIS = 1995\u20132012"]
-[13.970780372619629, 7.060844421386719, "[TT] Operating Voltage of the C&DH Subsystem = 3.3 V"]
-[5.755555629730225, 0.8136941194534302, "[FF] Discovery Date of the Sprites = Unknown"]
-[14.285091400146484, 3.194187641143799, "[TT] Mass of the UBAKUSAT = 4 kg"]
-[4.3472723960876465, 0.7074125409126282, "[TT] Decommission Date of the DMSP Flight 14 = Feb. 11"]
-[8.79681396484375, 3.1927003860473633, "[FF] Authors of the Solar-B EUV Imaging Spectrometer = J. L. Culhane, L. K. Harra, G. A. Doschek, J. T. Mariska, T. Watanabe, H. Hara"]
-[7.016678333282471, 2.6002917289733887, "[FF] Mission Type of the Etalon = Solid Earth Studies"]
-[5.8274712562561035, -0.8471267223358154, "[TT] Design Life of the Spacecraft = 5 years"]
-[7.841217994689941, 4.762628555297852, "[FF] Components of the SWE = SensorML, Observations and Measurements"]
-[3.501206398010254, 6.419358253479004, "[TT] Antenna Length of the NSCAT = 3 m"]
-[10.327197074890137, 3.983643054962158, "[FF] Function of the TEMBOTM EMC = Both the primary deployment mechanism and the principal structural members of the boom"]
-[6.751212120056152, 4.2552409172058105, "[FF] Integration Status of the Instrument Flight Model = Near completion"]
-[8.166996002197266, 3.2843148708343506, "[FF] Function of the RTEP = Detects weak lightning flashes from the intense but slowly evolving background"]
-[4.484673023223877, 7.019070625305176, "[TT] Data Transmission Subsystem of the Sentinel-1, -2, and -3 = X-band TXA (Transmission Assembly)"]
-[6.676868915557861, 5.449833869934082, "[FF] Interrupts of the dsPIC33F microcontroller = Unknown"]
-[10.629914283752441, 7.328332424163818, "[TT] Swath Width of the Instrument = 40 km (full mode)"]
-[5.206704139709473, 1.3853307962417603, "[FF] Mission Completion Date of the ELSA-d = 4 May 2022"]
-[8.389646530151367, -0.3396458327770233, "[TT] Size of the Langj\u00f6kull = Iceland\u2019s second largest ice cap"]
-[7.982126712799072, 4.755672454833984, "[FF] Contents of the Avionics Bay = Magnetometers, magnetorquers, reaction wheels, gyros, on-board computers, GPS receiver, X50 avionics stack, and batteries"]
-[7.9622697830200195, 3.0522429943084717, "[FF] Objective of the TanSat = Retrieve the atmosphere column-averaged CO2 dry air mole fraction (XCO2) with precisions of 1% (4 ppm) on national and global scales"]
-[7.6737961769104, 0.21485786139965057, "[TT] Mission Number of the Lucy = 13th"]
-[8.307393074035645, 1.2068125009536743, "[TT] Pass Over of the RainCube = North-eastern edge"]
-[5.661191463470459, 1.2935022115707397, "[TT] Date of the ESA Space19+ ministerial conference = End of 2019"]
-[8.347487449645996, 6.311785697937012, "[TT] Absolute Accuracy of the Radiometry = < 2.4 Wm -2  sr -1"]
-[7.182971954345703, 2.5189225673675537, "[TT] Geographic Region of Interest of the ZACUBE-2 = Southern African coastal regions"]
-[13.354023933410645, 7.721339225769043, "[TT] Transmitter Power of the Radio = 5 W"]
-[7.548129081726074, 2.095069169998169, "[FF] Primary Applications of the AATSR = Chlorophyll, Vegetation index, Cloud clearing, SST"]
-[11.871428489685059, 4.844069004058838, "[TT] Dimensions of the Card Size = 15.3 cm x 23 cm"]
-[14.060928344726562, 3.16463303565979, "[TT] Mass of the Nauka module = 20 tons"]
-[5.71238374710083, 8.769289016723633, "[TT] Wavelength Bandwidth of the MC-U = 10 nm FWHM"]
-[7.420462608337402, 3.2735371589660645, "[FF] Purpose of the Space Cameras = Monitor forests"]
-[4.37009334564209, 7.548209190368652, "[TT] S-band Monitor of the MSX = AFSCN"]
-[6.259326934814453, 4.365280628204346, "[FF] Function of the Mission Planning System = Receives the acquisition requests from end-users via Order Handling and Distribution System and plans the acquisition planning"]
-[9.82767391204834, -0.44254085421562195, "[TT] Orbital altitude of the GPS-DASS = 19,140 km"]
-[3.2798330783843994, 5.054244518280029, "[TT] SAR Payload Swath Width of the RCM = 20 - 350 km"]
-[6.599704742431641, 5.762794017791748, "[FF] Number of Boards of the ELDRS = 1"]
-[6.362564563751221, -0.5636547207832336, "[TT] Duration of the Lunar Sortie mission = 26 days (7 uncrewed in LLO)"]
-[10.57669448852539, 1.1104811429977417, "[FF] Physical Properties of the HD 212771 and HD 203949 = Mass, size and age"]
-[5.83162784576416, 6.274535179138184, "[TT] Storage Capacity of the SSRNI = 4 Gbit"]
-[12.119536399841309, 6.182358264923096, "[TT] Cosmic Rays Energy of the AMS Experiment = Up to multi-TeV"]
-[10.362001419067383, 2.277595043182373, "[TT] Energy Range (Red) of the Chandra X-ray Observatory = 300 to 1,000 electron volts (eV)"]
-[9.213905334472656, -0.4541764557361603, "[TT] Apogee Height of the INTEGRAL = 153,657.2 km"]
-[8.718242645263672, 7.721372604370117, "[TT] Pixel Size of the Detector Array Assembly = 13 \u00b5m"]
-[8.811494827270508, 6.387753009796143, "[TT] Wave Height Measurement Accuracy of the ALT Experiment = 10% or 0.5 m, whichever was greater"]
-[10.886959075927734, 2.0046041011810303, "[FF] URL of the XMM-Newton = http://www.esa.int/Science_Exploration/Space_Science/XMM-Newton_maps_black_hole_surroundings"]
-[8.249404907226562, 7.735445976257324, "[TT] Number of Detectors of the SIS (Scanning Imaging Spectrograph) = 2"]
-[4.707488536834717, 5.394593238830566, "[FF] Operation of the Automated Beacon Network = Forwards the message to a central monitoring workstation"]
-[6.8528876304626465, 3.2298014163970947, "[FF] Monitoring Capability of the SBSS = Objects as small as a 1 m cube all the way out to the Geosynchronous belt at 35, 786 km from Earth"]
-[5.639778137207031, 6.5667266845703125, "[TT] Advanced Mode Daily Capacity of the EDRS-A and EDRS-C nodes = 32.4 TB/day"]
-[13.539899826049805, 7.348704814910889, "[TT] Power Generation of the CanX-2 = 4 W"]
-[7.910831451416016, -2.4855823516845703, "[TT] Mission Purpose of the GOLD = Ionosphere observations"]
-[7.485597610473633, 2.433109998703003, "[TT] Synoptic Coverage of the Satellite = 6000 km2"]
-[7.693531036376953, 6.517274379730225, "[TT] Earth Disk Scanning Time of the MVIRI = 30 min"]
-[8.417909622192383, 6.297082424163818, "[TT] Accuracy of the VISION = 5%"]
-[4.777291774749756, 1.9905130863189697, "[TT] Airlock Cycles for Orbital Deployment of the QB50 = At the least two"]
-[6.37050199508667, 1.017014503479004, "[FF] Position Date of the Storm Hunter = 13 April, 2018"]
-[12.128284454345703, 6.146306037902832, "[TT] Particles Collected of the AMS-02 = Hundreds of million"]
-[6.7325334548950195, 5.733730316162109, "[TT] Number of Additional Containers of the BepiColombo = 15"]
-[6.647171497344971, 3.833065986633301, "[FF] Hosting of the HISats = In an unused recess on the host spacecraft"]
-[5.652818202972412, 4.643771171569824, "[FF] Data Relay of the MarCO = Successful"]
-[13.16682243347168, 7.27748966217041, "[TT] Power Consumption of the AIM = 1.5 to 5 W"]
-[14.272520065307617, 3.205498695373535, "[TT] Mass of the Arkyd-3 = 4 kg"]
-[11.837666511535645, 0.039560090750455856, "[FF] Purpose of the TESS = Find young stars like DS Tuc A"]
-[13.444233894348145, 5.750924587249756, "[TT] Voltage of the Solar Arrays = 23 to 37 Volts"]
-[8.316039085388184, 0.7036393880844116, "[FF] Observation Objects of the DCAM3-D = Ejecta and a subsequent crater of the SCI impact, and a relative position of the SCI to the asteroid when it is launched"]
-[8.739240646362305, -0.21320150792598724, "[TT] Apogee (km) of the Meteor-1-1 = 713"]
-[9.05157470703125, 7.350922107696533, "[TT] Photon Data Resolution of the SIMPL = 10 m"]
-[14.11590576171875, 3.953734874725342, "[TT] Mass of the Instrument mass = 12 kg (max)"]
-[8.309910774230957, 0.1666894555091858, "[TT] Number of Planned Propulsive Maneuvers of the ICE (International Cometary Explorer) = 4"]
-[13.657747268676758, 5.858852386474609, "[TT] Power Output of the Solar Panels = 200 W"]
-[5.532756328582764, 7.079024314880371, "[TT] Telemetry Data Rate of the AltiKa = 43 kbit/s"]
-[5.028233051300049, 3.369483232498169, "[TT] Manufacturer of the NewSat = Satellogic"]
-[7.4433159828186035, 2.922927141189575, "[FF] Maintain Cryogen Fluid Mass of the RRM3 = 6 months"]
-[9.467676162719727, 8.94118595123291, "[TT] File Format of the Iris Video Camera = MPEG-4"]
-[5.620274066925049, 2.801610231399536, "[FF] Sponsor of the VECTION = Canadian Space Agency (CSA)"]
-[7.304112911224365, 5.430267333984375, "[FF] Components of the TT = Upper and lower tubes, VOD, OGB"]
-[8.565949440002441, 8.013128280639648, "[FF] Spectral Resolution of the GK-2A = Improved"]
-[7.9775614738464355, 13.684835433959961, "[TT] SSD of the B10 = 60 m"]
-[9.449273109436035, 1.39007568359375, "[TT] Required Velocity of the Deployer = 20m/s"]
-[10.872879028320312, -0.3022595942020416, "[TT] Data Processing of the TanDEM-X = More than 400,000 datasets"]
-[4.387828350067139, 7.61867094039917, "[TT] Frequency of the IMI = L-/S-/C-band"]
-[5.515984058380127, 3.0329601764678955, "[FF] Overall Project Management of the OHB System AG = Responsible"]
-[4.381155014038086, 7.160251617431641, "[TT] Communications of the Telescope = TT&C in S-band; data acquisition in Ka-band"]
-[4.712386131286621, 3.1816468238830566, "[TT] Location of the TQCMs = Inside/outside of the SLATS structure"]
-[7.731051921844482, 5.468575477600098, "[FF] Optical Elements of the AEISS Telescope = 5 mirrors, the FPA (Focal Plane Assembly) with 1 panchromatic and 4 multispectral bands, and two Star Trackers"]
-[10.623228073120117, 7.315961837768555, "[TT] Swath Width of the Instrument = 17.5 km (half mode)"]
-[5.08447265625, 0.7840282917022705, "[TT] Phase C/D Contract Signing of the Spacebus Neo = Separate Phase C/D contracts were signed with both primes at the end of 2015"]
-[6.623434066772461, 4.016650199890137, "[TT] Installation Location of the Wireless Compose module = Space Station"]
-[6.233364582061768, 3.287809371948242, "[TT] Business Model of the BlackSky Global Satellite = Pay-per-picture"]
-[8.052037239074707, 3.0436835289001465, "[TT] Type of the GLM = Lightning sensors"]
-[7.321926593780518, 3.188368558883667, "[FF] Orbit of the EnviSat = Not provided"]
-[8.10694408416748, 1.1939383745193481, "[FF] Level-2 Data Availability of the SMAP (Soil Moisture Active Passive) = Beta version available as of Sept. 9, 2015"]
-[4.690329551696777, 0.5757688879966736, "[TT] Launch Date of the Unicorn-2L, -2M and -2N = December 1, 2023"]
-[4.271605968475342, 7.195205211639404, "[TT] Frequency Band of the S-band TT&C transceiver = S-band"]
-[6.66339111328125, 2.867149591445923, "[TT] Unique Feature of the Spire = Reaching remote areas like the open oceans"]
-[11.393026351928711, 5.870963096618652, "[TT] Material of the Satellite structure = Aluminum frame"]
-[6.408429145812988, 3.004101514816284, "[TT] Constellation Redundancy of the CYGNSS = Full"]
-[6.654567718505859, 0.28527337312698364, "[TT] Revisit Rate of the Constellation = Six consistent visits per day"]
-[4.524986267089844, 2.756305456161499, "[TT] Assembly Location of the BRITE Satellites = Space Research Center in Warsaw"]
-[9.365593910217285, 3.8130710124969482, "[FF] Faraday Rotation of the AIS System = Inversely proportional to the square of the frequency"]
-[5.244567394256592, 3.7548959255218506, "[TT] Type of the Swift J0042.6+4112 = Possible pulsar"]
-[4.778453350067139, -1.157523274421692, "[TT] Corresponding Time of the FY-3E = 7:28 Beijing Time on 5 July"]
-[13.19640064239502, 7.2865400314331055, "[TT] Power Consumption of the MWR = 96 W"]
-[9.386347770690918, 6.76969051361084, "[TT] Spatial Resolution of the Pixxel\u2019s planned satellites = 5 m"]
-[5.184842586517334, 8.113611221313477, "[TT] Frequency Range of the LISA = 0.1 mHz to 1 Hz"]
-[6.463804721832275, 4.879001140594482, "[FF] Function of the BEU = Combines all subsystem and payload electronics into one electronics box"]
-[9.55533504486084, 1.189208745956421, "[FF] Speed of the CME (Coronal Mass Ejection) = Tens of kilometres per second"]
-[13.35990047454834, 7.690553665161133, "[TT] RF Transmit Power of the Transmitter = 9.6 W"]
-[6.967085838317871, 3.0281364917755127, "[FF] Application of the MDD = Broadcast of operational meteorological charts"]
-[9.428877830505371, 7.091029644012451, "[TT] Spatial Resolution of the AEISS = 0.7 m"]
-[7.739388465881348, 9.11833381652832, "[TT] Wavelength of the W-band = 3.9 mm"]
-[8.18413257598877, 7.298251152038574, "[TT] Imaging System of the NewSat = Multispectral imager"]
-[8.45766830444336, 3.1840193271636963, "[TT] Number of Ozone Altitude Profiles of the UVSP = Approximately 20,000"]
-[3.4391515254974365, -0.9110186100006104, "[TT] Orbit Type of the QuakeSat = Near-circular sun-synchronous dawn-dusk orbit"]
-[8.707297325134277, 3.435368061065674, "[FF] Measurement of the EUVS = Changes in the solar extreme ultraviolet irradiance"]
-[9.827619552612305, -0.6054828763008118, "[TT] Orbit Altitude of the Pegasus rocket = ~650 km x 610 km"]
-[4.215424537658691, 2.59771466255188, "[TT] Launch Site of the DMSP = VAFB (Vandenberg Air Force Base), Vandenberg, CA, USA"]
-[7.785971641540527, 6.3963541984558105, "[FF] Observation Time of the Atmospheric Imaging Assembly (AIA) = 11:52 UT"]
-[4.412552833557129, 4.282588005065918, "[TT] Quantity of the ICEYE SAR Satellites = 5"]
-[5.648303508758545, -0.8587505221366882, "[TT] Design Life of the GCOM-W1 = 5 years"]
-[9.114459991455078, 3.4156930446624756, "[FF] Observation Type of the TIMED spacecraft = Plasma distribution around the magnetic equator"]
-[9.70638370513916, 8.43166732788086, "[FF] Angular FOV of the CEASE = Relatively large"]
-[7.657627105712891, 7.095081806182861, "[TT] FSR of the Radiometry = 240 Wm -2  sr -1"]
-[9.02100944519043, -0.6802511811256409, "[TT] Orbit Type of the PROBA-3 = Highly-elliptical Earth Orbit"]
-[8.258061408996582, 4.818785667419434, "[FF] Components of the EPAM = LEMS (Low Energy Magnetic Spectrometers), LEFS (Low Energy Foil Spectrometers), CA (Composition Aperture)"]
-[8.73291015625, -0.6684369444847107, "[TT] Scene Size of the ICEYE-X1 = 40 x 83.3 km"]
-[6.383536338806152, 1.174977421760559, "[FF] Ground Network of the FormoSat-7 / COSMIC-2 mission = USN ground stations for the first 2 years, and then service provision by NOAA's ground stations for the following 3~5 years"]
-[6.268904685974121, 1.131020188331604, "[FF] Date of the \"NASA Data Powers New USDA Soil Moisture Portal\" = 08 March 2021"]
-[7.744619369506836, 8.801093101501465, "[TT] Spectral Bands of the NEMO-HD = 450-520 nm, 520-600 nm, 630-690 nm, and 760-900 nm"]
-[6.976231575012207, -0.5066473484039307, "[TT] Local Time of Descending Node of the ASNARO satellite = 11:00 hours \u00b1 15 min"]
-[5.829320430755615, 6.286727428436279, "[TT] Total Storage Capacity of the SSRU = 256 Gbit"]
-[6.420294284820557, -0.1766589730978012, "[TT] Observation Duration of the ULX-4 = 10 days"]
-[4.298968315124512, 2.2664151191711426, "[TT] Launch Provider of the DubaiSat-1 = ISC (International Space Company) Kosmotras of Moscow, Russia"]
-[4.324889659881592, 0.9301148653030396, "[TT] Testing Completion Date of the Argos-4 = July 27, 2022"]
-[8.7332181930542, 4.917505264282227, "[TT] Field of View of the ST (Star Tracker) = 33.5\u00ba x 23.5\u00ba"]
-[5.158803462982178, 0.7227168679237366, "[TT] EVA Date of the AMS-02 = May 20, 2011"]
-[5.044412612915039, 0.07176066935062408, "[TT] Launch Date of the STRV-1a and -1b = 17 June 1994"]
-[8.992488861083984, 8.13685417175293, "[TT] IFOV/line (pixels/scan line) of the MERSI = 2048/8192"]
-[11.802215576171875, 0.05403085798025131, "[FF] Discoveries of the TESS = Three newly-discovered planets"]
-[11.793001174926758, 3.2498691082000732, "[TT] Thrusters of the Propulsion = Twelve 22 N"]
-[8.648096084594727, 7.745946407318115, "[TT] Size of the Detector Array Assembly = 5 x 6000 (30,000 pixels or samples in cross-track)"]
-[8.175779342651367, 0.9002988338470459, "[FF] Response Time to Rain or Pumping of the Unconfined Soil = Rises or falls more quickly in response to rain or pumping"]
-[7.329970359802246, 3.969674587249756, "[FF] Technology of the MiRaTA = Radio Occultation"]
-[7.4467291831970215, 7.637269973754883, "[TT] Radiometric Stability of the Instrument = \u2264 0.5 dB"]
-[5.908091068267822, 1.6615233421325684, "[FF] URL of the LARES 2 = http://www.lares-mission.com/LARES_2.asp"]
-[16.5556640625, 3.6498076915740967, "[FF] Number of Additional Satellites of the OneWeb = 34"]
-[1.6234983205795288, 3.7624197006225586, "[TT] Sun sensors of the BEESAT-3 = Yes"]
-[9.694730758666992, 4.802146911621094, "[TT] Stabilization of the Block 5B/C satellites = Spin stabilization was abandoned"]
-[4.745615482330322, 6.678715705871582, "[TT] RF Communications of the Spacecraft = 2 kbit/s, 2 Mbit/s"]
-[13.281512260437012, 5.43509578704834, "[FF] Solar Array Capacity of the MERLIN = Unknown"]
-[10.102862358093262, 2.054602861404419, "[FF] Director of the Chandra X-ray Observatory = Harvey Tananbaum"]
-[5.286689758300781, 4.8266096115112305, "[FF] GPS Receiver of the CanX-2 = Commercially available"]
-[12.697874069213867, 1.927079677581787, "[FF] Data Usage of the SAGE-III on ISS = Help the scientific community identify the cause and assess the threat of any new threats to the ozone layer"]
-[8.626848220825195, 6.722560405731201, "[TT] Type of the Ion sensor = Planar aperture, planar collector sensor"]
-[14.096541404724121, 7.215888500213623, "[TT] Efficiency of the 28 V Regulator = 93%"]
-[7.213738441467285, 5.218064308166504, "[FF] Components of the Merlin = Two `card-frame' modules, printed circuit boards, lid, base, EMC screen"]
-[8.00562572479248, 5.644167423248291, "[FF] Data Transfer of the Webb's Fine Guidance Sensor (FGS) = Limited communications bandwidth between L2 and Earth"]
-[5.345897674560547, 0.8651183247566223, "[FF] Date of the Bristol Abloom = 4 June 2022"]
-[12.43016242980957, 0.6650528907775879, "[TT] Temperature Range of the Plato Camera = -80\u00b0C"]
-[9.582024574279785, 7.095841884613037, "[TT] Spatial Resolution of the IMI = 15-50 km"]
-[7.6456098556518555, 8.058550834655762, "[TT] Enclosure Color of the VLF Receiver = White"]
-[8.289276123046875, 6.487178325653076, "[TT] Scan Rate of the SSM/I sensor = 31.9 scans/min"]
-[6.264629364013672, 4.7095441818237305, "[FF] Function of the Spacecraft Operation Control System = Receives the telemetry data demodulated at the ground station and provides the information for monitoring the status of the satellite to the operators"]
-[5.764665603637695, 4.425299644470215, "[FF] Control Software of the SATLAB = RAMSES software"]
-[14.249467849731445, 3.169290781021118, "[TT] Mass of the PPL1 and PPL2 = 5.96 kg"]
-[10.072123527526855, 2.1181914806365967, "[FF] URL of the High-resolution x-ray telescopes = http://constellation.gsfc.nasa.gov/resources/Published_Papers/HighResolutionXrayTelescopes2010.pdf"]
-[3.594463348388672, 6.971285820007324, "[TT] Polarisation of the Transmitting antenna = RHCP or LHCP"]
-[3.7022955417633057, 4.493486404418945, "[FF] Radar Remote Sensing of the RISAT-1 = Contribution to radar remote sensing"]
-[8.148080825805664, -0.7299438714981079, "[FF] Applications of the Optical Payload = Monitoring plankton blooms to changes in the polar ice caps"]
-[11.363676071166992, 2.7854886054992676, "[TT] Power Supply System Mass of the Microsatellite = 1.9 kg"]
-[9.046029090881348, 10.026487350463867, "[TT] IFOV of the Eastman Kodak KLI14403 linear CCD sensor = 32.07 \u00b5m"]
-[8.31332015991211, 7.195897579193115, "[TT] Type of the CMOS Sensor = CMOS"]
-[10.323427200317383, 1.8820158243179321, "[FF] Purpose of the eROSITA X-ray telescope = Look for previously unknown supernova remnants"]
-[4.951813697814941, 7.396443843841553, "[TT] TOMS Data Rate of the RF communications = 0.7 kbit/s"]
-[4.4672417640686035, 1.9084969758987427, "[FF] Loss Date of the EgyptSat-2 = Unknown"]
-[6.151237964630127, -0.2191677838563919, "[TT] Operation Status of the Genesis-2 = Nominal in 2012"]
-[10.14836597442627, 8.245911598205566, "[FF] Medium-sized Aperture Camera (MAC) of the RazakSAT = Unknown"]
-[8.411130905151367, 0.41913312673568726, "[TT] Crest Height of the Yellowstone River = 13.88 feet"]
-[9.288792610168457, 3.5531563758850098, "[FF] URL of the RHESSI = http://berkeley.edu/news/media/releases/2005/02/18_magnetar.shtml"]
-[16.49947166442871, 3.5867013931274414, "[TT] Full Commercial Service Launch of the OneWeb = 2022"]
-[3.5132343769073486, 5.2967915534973145, "[TT] SAR antenna of the Payload = Nominal operations"]
-[9.71961498260498, -0.6225876808166504, "[TT] Orbit Altitude of the ASNARO-1 = 504 km"]
-[5.738701343536377, 2.511303663253784, "[FF] Autonomy of Access to Space of the Vega = Europe"]
-[13.87709903717041, 2.7057673931121826, "[TT] Launch Mass of the FY-3 series spacecraft = 2450 kg"]
-[5.364868640899658, 0.32098332047462463, "[TT] Implementation Year of the TESSA = 2008"]
-[11.171623229980469, 4.76379919052124, "[TT] Burrowing Depth of the HP3 = 3 to 5 meters"]
-[8.298601150512695, 0.7754831314086914, "[FF] Burned Area of the LNU Lightning Complex = More than 130,000 acres"]
-[11.804689407348633, 4.8076982498168945, "[TT] Side Panels Surface Area of the UniSat-5 = 50 cm x 50 cm"]
-[14.134148597717285, 3.225019931793213, "[TT] Mass of the XRD = 125 g"]
-[14.57533073425293, 6.606995582580566, "[FF] Type of the BP4 battery pack = Battery Pack"]
-[10.119084358215332, 7.585118293762207, "[FF] Modification of the OCTL Telescope = Optical flat to support links in the presence of more windy conditions"]
-[8.52140998840332, 2.3680663108825684, "[FF] Impact of the EMIT = Help climate scientists better understand the impact of airborne dust particles in heating and cooling the planet\u2019s atmosphere"]
-[2.866597890853882, 0.08663686364889145, "[TT] J2000 declination (deg) of the J1846-0258 = -2.97503"]
-[10.464314460754395, 6.165833473205566, "[TT] Surrounding Temperature of the eROSITA camera = +20\u00baC"]
-[6.5450439453125, 1.788346529006958, "[FF] URL of the Landsat-9 = https://landsat.gsfc.nasa.gov/landsat-9/"]
-[10.935408592224121, 7.552563190460205, "[TT] Swath Width of the HIRDLS = 2000 - 3000 km"]
-[7.688729763031006, 2.245591402053833, "[FF] Objective of the CZI = Provide imagery of coastal regions"]
-[9.17823600769043, 7.58457088470459, "[TT] Swath Width of the CCD Pushbroom Camera = 60 km"]
-[4.886504173278809, 7.221320152282715, "[FF] Development Test Date of the X-band Multi-mode High speed Modulator = June 5-12, 2011"]
-[9.474513053894043, 4.751827239990234, "[FF] Control Capability of the Attitude Control System = Full three-axis control"]
-[5.133519649505615, 3.3705527782440186, "[TT] Avionics Subsystems Manufacturer of the CHORUS = Magellan Aerospace Corporation"]
-[6.545599937438965, 4.602135181427002, "[FF] Activity of the COVE payload = Complete"]
-[6.1032891273498535, 3.0341291427612305, "[TT] Responsible Organizations of the Archives = NOAA National Environmental Satellite Data and Information Service and Jet Propulsion Laboratory Pilot Ocean Data System"]
-[6.355541706085205, 0.7683814764022827, "[TT] Number of Users of the FormoSat-3/COSMIC-1 = 3,000"]
-[5.095338821411133, 7.592724800109863, "[TT] G/T of the Antenna = More than 16.9 dB/K"]
-[5.853878974914551, -0.8790959119796753, "[TT] Design Life of the DMSP 5D-3 spacecraft = 5 years"]
-[7.7802734375, 2.5651466846466064, "[FF] Application of the Lidar Instrument = Estimate land carbon storage"]
-[5.3033599853515625, 1.1846665143966675, "[FF] Presentation Date of the COMS = July 12, 2005"]
-[11.457011222839355, 5.727881908416748, "[FF] Design of the Rack = Simplified design with a back plane containing the interfaces between the individual slices"]
-[6.25668478012085, -0.3710944950580597, "[TT] Years in Orbit of the RADARSAT-2 = 3"]
-[5.5079498291015625, 5.3766608238220215, "[TT] Connector of the ENT = Quick Disconnect Connector"]
-[10.855300903320312, 2.8758339881896973, "[TT] Quantity of the Nanosatellites = 100"]
-[5.951014518737793, 6.0717267990112305, "[TT] Data Product Format of the OSCAT-2 = HDF 5 (Hierarchical Data Format 5)"]
-[13.17712116241455, 5.135678768157959, "[TT] Solar Wings Span of the Satellite = 25 m"]
-[9.254226684570312, 5.917364120483398, "[FF] Calibration Method of the SSM/I = Mirror and hot reference absorber"]
-[11.745636940002441, 3.3317649364471436, "[TT] Nozzle Thrust of the CGMS = 1mN"]
-[9.834256172180176, 7.787296295166016, "[TT] Step and Dwell Time of the Telescope = 0.1, 0.2 and 0.4 s"]
-[9.162473678588867, 4.691282272338867, "[FF] Control Laws of the Attitude Control Software = Detumbling, sun tracking and camera pointing"]
-[8.256543159484863, 6.933843612670898, "[TT] Temporal Resolution of the ABI = More than five times the current GOES Imagers"]
-[10.017159461975098, 4.562551975250244, "[TT] Magnet Type of the Cryomag = Cryogenic superfluid helium superconducting magnet"]
-[5.338508129119873, 3.946117639541626, "[TT] Number of Satellites of the Satellite Constellation = 8"]
-[7.197019100189209, 2.7844743728637695, "[FF] Design Milestone Date of the MethaneSAT Instrument = 21 February 2020"]
-[14.015196800231934, 4.055715560913086, "[TT] Instrument Mass of the Hyperion = 49 kg"]
-[4.991955280303955, 2.949542760848999, "[TT] Contractor of the BRITE-PL = UTIAS/SFL"]
-[5.3608622550964355, -0.38351762294769287, "[TT] Separation Time of the OG2-1 = Approximately 9:00 pm EST"]
-[5.675052642822266, 11.347135543823242, "[FF] Approx. peak sensitivity altitude of the Channel 2 = Unknown"]
-[8.237740516662598, 7.599850654602051, "[TT] Quantity of the CPD detectors = 6"]
-[8.445137023925781, 6.829494476318359, "[FF] Quality Comparison of the Imaging Methods = SMART > PAIS > Direct"]
-[8.396299362182617, 3.669302225112915, "[FF] Objective of the AOE-2 = To characterize and to flight test a novel zinc-oxide sensitive renewable atomic oxygen flux sensor based on semiconducting thin films"]
-[7.616624355316162, -2.5181894302368164, "[TT] Data Visualization of the GOLD = March 2019"]
-[8.644558906555176, 7.090694427490234, "[TT] Imaging Capacity of the Raytheon's Payload = Doubles DigitalGlobe's capacity to capture multispectral and 30 cm imagery"]
-[4.188313007354736, 2.5953705310821533, "[TT] Launch Site of the KazSTSAT = VAFB (Vandenberg Air Force Base) in California"]
-[8.988751411437988, 0.5610184669494629, "[FF] Resupply Mission of the ARTEMIS = Successful"]
-[6.548171520233154, 3.2952187061309814, "[TT] Collaboration of the AMS-02 = 15 Countries, 44 Institutes and 600 Physicists"]
-[8.56148624420166, 0.1518305093050003, "[FF] Normal Activity of the Comet = Driven by sunlight vaporizing the ices near the surface of the nucleus"]
-[9.1631441116333, 8.512368202209473, "[TT] Wavelength of the Lens 3 = 0.67 \u00b5m @ 60\u00ba&120\u00ba"]
-[9.380913734436035, 4.974673271179199, "[TT] Attitude Stabilization Margin of the HIT-Sat = About 10\u00ba"]
-[7.581689834594727, 3.507612466812134, "[FF] Sun Off-pointing Effect of the PROBA-3 = Thermo-elastic deformations"]
-[3.8841817378997803, 1.9642571210861206, "[TT] Launch Vehicle of the TSIS-1 = SpaceX-13 Falcon 9FT"]
-[9.35888957977295, 3.6106104850769043, "[FF] Objective of the GEOS-2 = Measurement of fluctuations in the magnetic field"]
-[8.848126411437988, 6.921040058135986, "[FF] Target Size of the PROBA-3 = Smaller than 1 pixel in camera image"]
-[9.42025089263916, 3.7989604473114014, "[FF] Signal Amplification Method of the Scalar Magnetometer = Dynamic nuclear polarization process"]
-[8.943086624145508, 0.9413434863090515, "[FF] Imaging of the Parker Solar Probe = Visible Light"]
-[7.601284027099609, -2.321636438369751, "[FF] Lead of the GOLD = Richard W. Eastes of UCF (University of Central Florida)"]
-[10.224059104919434, 1.9277037382125854, "[FF] Brightness of the Sw J1644+57 = Exceptionally bright for a few weeks"]
-[8.079133987426758, -1.165176272392273, "[TT] Instrument of the ICESat-2 = Earth-observing laser instrument"]
-[5.947220802307129, 3.419267177581787, "[TT] Cost of the Prometheus Block 2 CubeSats = Less than $100,000"]
-[4.831583499908447, 2.943164110183716, "[TT] Overall Responsibility of the ERO mission = Airbus"]
-[6.606173992156982, 1.8812906742095947, "[FF] Testbed for Precise Onboard Orbit Determination of the SAC-C = Unknown"]
-[8.791943550109863, 7.457552909851074, "[FF] Image Generation of the MVIRI = Simultaneous in TIR, WV, and VIS"]
-[9.235164642333984, 4.658117294311523, "[FF] Degradation of the ASC (Advanced Stellar Compass) = Commercial-grade CCD"]
-[4.801923751831055, -0.8890208005905151, "[TT] Launch Site of the CBERS-2A = Taiyuan Satellite Launch Center in China"]
-[11.161840438842773, 0.6236534714698792, "[FF] Mission Type of the ASTERIA = Exoplanet Survey"]
-[4.414146900177002, 7.4667840003967285, "[TT] Gain on receive of the Downlink (Ku-band) = 38.74 dB"]
-[6.517025470733643, -0.49642086029052734, "[TT] Period of the JPSS-1 = 101 minutes"]
-[8.493854522705078, 9.460929870605469, "[TT] Responsivity Requirement of the Responsivity Measurement = >1.04 A/W"]
-[10.369830131530762, 2.968616008758545, "[TT] Onboard AI Processing Unit of the PhiSat-1 = Intel\u00ae Movidius\u2122 Myriad\u2122 2 Vision Processing Unit (VPU)"]
-[5.019519329071045, 8.17920970916748, "[TT] Frequency of the Aquarius = 1..413 GHz"]
-[8.135026931762695, 4.3295063972473145, "[FF] Star Calibration Frequency of the Satellite = During commissioning"]
-[12.156021118164062, -0.24655282497406006, "[TT] Observation Duration of the TESS = About a month"]
-[10.128079414367676, 5.452474117279053, "[FF] Focus Mechanism of the EOS = Active/passive thermal control mechanism"]
-[7.4658942222595215, 3.362689971923828, "[FF] Definition of the Level 2 = Comprehension of the current situation"]
-[3.9278717041015625, 3.503737449645996, "[FF] Name of the GSTB-V2 = Galileo System Test Bed-V2"]
-[13.457181930541992, 2.9286787509918213, "[TT] Weight of the Satellite = 95 grams"]
-[6.09448766708374, 6.116954326629639, "[TT] Number of Control Units of the SSR = 2"]
-[3.4233498573303223, 5.0242414474487305, "[TT] Instruments of the HJ-1 = S-Band SAR"]
-[10.719388961791992, 1.0824439525604248, "[TT] Size of the TOI 2076 b = Three times Earth\u2019s size"]
-[7.077293395996094, 8.226223945617676, "[TT] Ku-band range Noise LRM of the Jason-2 = 1.7 cm"]
-[7.407952308654785, 4.855617046356201, "[FF] Components of the IRIS spacecraft = Bus structure, harness and interconnects, MLI blanketing, ACS flight software, fault management scheme, EGSE, solar arrays, deployment mechanisms, reaction wheel assemblies, torque rods, IAU, coarse and digital sun sensors, magnetometer, star trackers"]
-[14.568940162658691, 6.623650550842285, "[TT] Battery Type of the IMPS = Manganese/lithium-ion rechargeable"]
-[12.69629192352295, 1.9087069034576416, "[FF] Science Objectives of the SAGE-III = Retrieve global profiles of atmospheric aerosols, ozone, water vapor, NO2, NO3, OClO, temperature and pressure"]
-[6.009103298187256, 4.4368696212768555, "[FF] Provider of the Mission Control System = GomSpace"]
-[10.27822494506836, 7.150599956512451, "[TT] Resolution of the NIRST = 350 m"]
-[5.475286483764648, 3.387009859085083, "[TT] Operator of the PARASOL = CNES"]
-[7.754545211791992, 6.70973014831543, "[FF] Alignment Tools of the Interferometer Alignment = Personnel from the OPC (Optical Physics Company), custom goniometer, collimated light source"]
-[5.861660003662109, 1.1187289953231812, "[TT] Operation Period of the EarthCARE = 2018 to 2022"]
-[6.708049774169922, 6.485454082489014, "[TT] Frame Size of the Event Processor = 147,456 pixels"]
-[6.23327112197876, 3.8535730838775635, "[FF] Conference Presentation Date of the Plug-and-play System = Aug. 13-16, 2007"]
-[7.809579372406006, 8.056472778320312, "[TT] Sensitivity of the CHIPS = High"]
-[11.287516593933105, 0.576504647731781, "[FF] Brightness Dip of the Star = Indicates the presence of a planet passing in front of it"]
-[7.128728866577148, 1.7238918542861938, "[FF] Purpose of the Geohazards Exploitation Platform = Terrain motion mapping"]
-[7.902424335479736, 4.787973880767822, "[FF] Purpose of the Sensor Fusion = Combine measurements from several different sensors to obtain a better result"]
-[8.65163516998291, 2.5474917888641357, "[TT] Measurement Altitude Range of the MLS = Upper troposphere to the lower thermosphere"]
-[6.111085414886475, 5.689259052276611, "[TT] Communication Ports of the CDSU = Multiple RS-485 input/output ports"]
-[8.572246551513672, 5.95644998550415, "[TT] Relative Bias Accuracy of the TOPEX/Poseidon = 1.6 mm"]
-[9.52367115020752, 7.335770606994629, "[TT] Ground Resolution of the Infrared Bands = 2700 m"]
-[9.92170238494873, 8.27127742767334, "[TT] Relative Aperture of the Lenses = 1/10"]
-[4.361391067504883, 7.373554706573486, "[TT] Frequency Range of the X-band data transmission = 8025-8400 MHz"]
-[10.829083442687988, 3.826329469680786, "[FF] Packaging and Mass Efficiency of the Drag Sail Modules = Superior or competitive to state-of-the-art solar sails"]
-[6.433282852172852, 1.4067960977554321, "[FF] Intended Missions of the TriG receiver = FormoSat-7/COSMIC-2, DESDynI, ICESat-2, Jason-CS, SWOT, DSAC, GRACE-FO, other NASA/NOAA missions"]
-[9.946404457092285, 5.438853740692139, "[FF] Purpose of the Sensors = Collect critical entry environment and thermal protection performance data"]
-[4.339847564697266, 4.791647434234619, "[TT] Ship Detection Capability of the Ship Detection mode = Ships 25 meters in length or greater"]
-[7.769233226776123, 5.632067680358887, "[FF] Purpose of the IMM = Automatically detect the occurrence of a special kind of electromagnetic wave known as 0+ whistlers"]
-[6.953999996185303, 6.968493938446045, "[TT] Number of Units of the Laser Transmitter = Three"]
-[9.29055118560791, -1.6837749481201172, "[TT] LTAN Evolution of the Swarm-A (Alpha) = 24 hours of local time coverage every 7-10 months"]
-[5.492486953735352, 6.025965213775635, "[TT] Memory of the C&DH = 16 MByte Flash"]
-[9.089556694030762, -1.2171598672866821, "[TT] Orbit of the SES-14 = Geostationary"]
-[4.159441947937012, 1.408928632736206, "[FF] Repositioned Location of the Meteosat-3 = 50o (75o W in Feb. 1993)"]
-[3.377621650695801, 1.4504019021987915, "[TT] Launch Date of the Sentinel-2A = Early March 2017"]
-[9.796159744262695, 4.759213924407959, "[TT] Stabilization of the S/C = Spin at 5 rpm"]
-[5.694314479827881, 0.9165233969688416, "[FF] Inspection Date of the Heat Shield = March 11, 2015"]
-[3.205601692199707, 1.69791579246521, "[TT] Revisit Times of the Sentinel-2 = Very fast"]
-[10.54364013671875, 1.7795710563659668, "[TT] Type of the \"ULX-pulsar\" = Pulsar, a kind of neutron star"]
-[5.902328968048096, 1.8333066701889038, "[FF] Test Flight Date of the Orion Crew Capsule = Fall 2014"]
-[6.997916221618652, 0.9960421323776245, "[FF] Planned Timeframe of the Mars Sample Return Mission = Around 2028-30"]
-[9.939599990844727, -0.20298288762569427, "[TT] Altitudes of Operation of the Starlink = Around 550 kilometers"]
-[7.6998982429504395, -0.8096468448638916, "[TT] Publication Date of the ICESat\u20102 = 15 May 2020"]
-[8.1613130569458, 7.8259806632995605, "[TT] Spectral Channels of the Multispectral Imager = 400-690, 400-510, 510-580, 580-690 for RGB and broad range imaging and a near-IR channel from 750 to 900 nm"]
-[5.7580790519714355, 2.5475504398345947, "[FF] Team Members of the CLARREO = D. F. Young, M. G. Mlynczak, K. J. Thome, S. Leroy, C. O. Ao, R. Bantges, F. Best, H. Brindley, J. Butler, R. Cageao, W. Collins, R. Cooke, J. Corliss, J. C. Currey, J. A. Dykema, D. R. Doelling, B. Dunn, D. R. Feldman, D. Goldin, H. Huang, R. Holz, Y. Huang, Z. Jin, D. Jennings, D.G. Johnson, S. Kato, R. Knuteson, G. Kopp, D. P. Kratz, X. Liu, C. Lukashin, A. Lyapustin, A. J. Mannucci, J. McCorkel, N. Phojanamongkolkij, P. Pilewskie, H. Revercomb, J. Rice, Y. Roberts, C. M. Roithmayr, F. Rose, W. L. Smith, Sr., B. Soden, P. W. Speth, T. C. Stone, W. Sun, D. Tobin, X. Xiong"]
-[8.116579055786133, 8.618528366088867, "[TT] Performance of the MTQ = 0-4 Nms"]
-[10.30604076385498, 4.523680686950684, "[FF] Purpose of the MTQs = Desaturate the reaction wheel assembly"]
-[7.057938575744629, 6.260941028594971, "[FF] Transmission Frequency of the GLB = Unknown"]
-[5.941350936889648, 4.768371105194092, "[FF] Ground Segment Component of the Delfi-C3 = Radio amateur network"]
-[10.933115005493164, 7.515871047973633, "[TT] Swath Width of the SSM/I = About 1400 km"]
-[4.372550964355469, 1.4951832294464111, "[TT] Constellation of the GCOM-W1 = A-Train"]
-[5.4268879890441895, 0.4601501226425171, "[TT] Deployment Date of the Flock 1b = August 19, 2014"]
-[6.98555850982666, 4.3604044914245605, "[FF] Unknown of the Table 1 = Unknown"]
-[5.403444766998291, 3.9968180656433105, "[TT] Number of Satellites of the 90-satellite constellation = 90"]
-[3.784749746322632, 4.446462154388428, "[FF] Mission Aim of the NeuSAR = Pathfinder mission for a potential constellation of small SAR satellites"]
-[4.940132141113281, 0.4037928581237793, "[FF] Launch Date of the Vigil = Mid-2020's"]
-[3.184683322906494, 5.090219020843506, "[TT] Elevation Beam Width of the RISAT-SAR = 2.2\u00ba -1.5\u00ba"]
-[5.524339199066162, 3.313523054122925, "[TT] Imager Manufacturer of the WorldView Legion = Raytheon Space Systems"]
-[5.821433067321777, 4.424976348876953, "[FF] Software of the HISat = Enables HISats to be aggregated together informationally so that satlet resource exposure and sharing is transparent to the operation of the system"]
-[5.54834508895874, 6.331499099731445, "[FF] Storage Capacity of the CEU = Much larger than 3 MB"]
-[6.546670913696289, -0.43988797068595886, "[TT] Total Observation Time of the MOMS-2P = 25 hours"]
-[9.218408584594727, 0.6788309812545776, "[FF] Orbital Period of the Solar Orbiter = 3:2 resonance with Venus"]
-[6.472550392150879, -0.33695799112319946, "[TT] Mean Time Between Resets of the BRMM = 8 days"]
-[6.362136363983154, 6.054518222808838, "[TT] Number of Centers of the DSDS = 4"]
-[6.794595718383789, 2.6400680541992188, "[FF] Data Source of the MODIS = NASA EOSDIS LANCE and GIBS/Worldview"]
-[5.034599304199219, 7.363145351409912, "[TT] Data Rate of the RF Communications = Collect and transmit up to 100 Mbit/s"]
-[8.879242897033691, 0.027294697239995003, "[TT] Latitude Range of the TanSat = -51\u00ba to 56\u00ba"]
-[7.18514347076416, 7.410717010498047, "[TT] Signal Photon Density of the MABEL = 3.1 photons per 70 cm"]
-[12.12521743774414, -0.32387208938598633, "[TT] Solar Array Deployment Time of the TESS = 60 days"]
-[13.02953815460205, 7.5870513916015625, "[TT] Signal Power of the Clementine = 6 W"]
-[16.49960708618164, 3.5832161903381348, "[TT] Partial Services Start Year of the OneWeb = 2021"]
-[8.015543937683105, 5.834272861480713, "[TT] Horizontal Resolution of the JPL Microwave Radiometer = 3.1 km"]
-[10.602518081665039, 3.3393006324768066, "[TT] Form Factor of the Dove-1 = 3U CubeSat"]
-[8.091771125793457, 1.325616478919983, "[FF] Moisture Source of the Atacama Desert = Blocked by the Andes to the east, as well as from the Pacific Ocean by the Chilean Coastal Range to the west"]
-[6.704589366912842, 4.935732364654541, "[FF] Operation of the TCU = Acquires parameters from sensors, monitors and commands valves, issues commands to the FCA, commands heater chains, monitors thermistors, commands valves, monitors their position, monitors pressure and temperature parameters"]
-[2.876619338989258, 4.240133285522461, "[TT] Observation Date of the ALOS-2 PALSAR-2 = July 25, 2017"]
-[3.9330923557281494, 7.795758247375488, "[TT] Modulation scheme of the Service downlink = O-QPN"]
-[8.920458793640137, 4.922881603240967, "[TT] Number of Sensors of the SPS = 8"]
-[14.228917121887207, 3.249260902404785, "[TT] Maximum Weight of the MS-2 = 200 kg"]
-[1.3636149168014526, 2.7835569381713867, "[TT] Principal Absorbing Constituents of the Band 9 = Ozone"]
-[13.632060050964355, 5.935497760772705, "[FF] Components of the EPS (Electrical Power Subsystem) = EPS card, battery, solar array"]
-[11.719782829284668, 4.177902698516846, "[TT] Diameter of the Meteosat = 2.10 m"]
-[5.804220199584961, 7.178203582763672, "[TT] Data Rate of the HIA = 3.12 kbit/s"]
-[6.367458343505859, 0.9860795736312866, "[FF] Presentation Date of the FormoSat-7 /COSMIC-2 = September 6-11, 2010"]
-[6.323384761810303, -0.18227243423461914, "[FF] Staffing of the On-call Operations = Initially 24/7, eventually reduced to 8 hours on weekdays"]
-[7.520623683929443, 2.4979407787323, "[FF] Location of the China\u2019s sizeable and uncertain carbon sink = China"]
-[10.206235885620117, 3.0784542560577393, "[TT] Number of CubeSat Missions of the ELaNa-4 = 8"]
-[6.363245964050293, 6.073072910308838, "[TT] Configuration of the NGAVGS = Two box"]
-[8.335957527160645, 1.532087802886963, "[TT] Range of Values of the Land surface temperature = 180 - 340 K"]
-[3.067108392715454, 2.247915267944336, "[TT] Burn Scars Area of the Copernicus Sentinel-2 = Around 1700 hectares"]
-[9.686532020568848, 0.32882288098335266, "[TT] Formation Distance of the PROBA-3 = 150 m"]
-[3.324422597885132, 5.075084686279297, "[TT] SAR Payload Imaging Time of the RCM = 12 minutes per orbit"]
-[10.981529235839844, 2.052621364593506, "[TT] Launch Date of the XMM-Newton = December 1999"]
-[5.186620712280273, 4.930382251739502, "[FF] Baseline Design of the SpooQySat = GomX-313 with modifications"]
-[9.226469039916992, 6.119401454925537, "[TT] Quantity of Cylindrical Electrostatic Deflection Analyzers of the VEIS = 6"]
-[9.674760818481445, 0.3615162968635559, "[TT] Distance between spacecraft of the PROBA-3 = About 150 m"]
-[8.407363891601562, 4.211625099182129, "[FF] Function of the Lens Hood = Reduces the effects of scattered light from the Earth and Moon"]
-[7.688047409057617, 0.847831130027771, "[FF] Function of the GRS (Gamma-Ray Spectrometer) = Explore the lunar soil properties"]
-[6.850906848907471, 1.199426293373108, "[FF] Measurement Date of the Solar Storm = February 2014"]
-[7.483444690704346, 3.48051381111145, "[FF] Phase 0 of the SOADR = Analysis of a mission that could remove very heavy debris from orbit"]
-[6.683378219604492, 4.859787464141846, "[FF] Components of the AAE = Appliqu\u00e9 sensor network, adaptive wiring manifold, high-performance computing on-orbit, and software definable radio"]
-[5.201843738555908, 3.0871753692626953, "[TT] Manufacturer of the Canadarm-1 = Canadian Space Agency"]
-[5.032374858856201, 8.060797691345215, "[TT] Frequency of the CPR = 94GHz"]
-[7.983891487121582, -1.0519540309906006, "[FF] Data Content of the ICESat-2 = Amery Ice Shelf, meltwater pooling on the surface of the ice shelf"]
-[9.41915512084961, 5.176192283630371, "[TT] Pointing of the Navigation and Stabilization = 2 arcmin"]
-[9.401754379272461, 6.977835655212402, "[TT] Angular Resolution of the S-020 = Modest"]
-[5.213033199310303, -0.37473902106285095, "[TT] Handover Time of the Launch and Early Operations Control Centers = Typically one week after the launch"]
-[7.91303825378418, 2.8289225101470947, "[FF] Field of View of the Lightning Imager = Atlantic Ocean, a small part of Africa and part of South America"]
-[7.924918174743652, 7.252362251281738, "[TT] Data Rate of the Camera = 336 Mbit/s"]
-[3.40643310546875, 6.393126010894775, "[TT] Panel Size of the Antenna = 1.3 m x 2.16 m"]
-[9.994094848632812, 2.8711681365966797, "[FF] Presentation Date of the NANOSATC-BR Cubesat Program = Oct. 1-5, 2012"]
-[5.432828426361084, 3.965392589569092, "[TT] Operational Phase Satellites of the FY-3 = 2"]
-[7.487493991851807, 6.604669570922852, "[TT] Material Exposure Duration of the Bartolomeo = Minimum of six months"]
-[5.884208679199219, -0.7660127282142639, "[TT] Mission Design Life of the Spacecraft = 12 months"]
-[10.109116554260254, -1.4783389568328857, "[TT] Inclination of the GRACE-FO Satellites = Approximately 89\u00b0"]
-[9.261877059936523, 1.8153948783874512, "[TT] Global Coverage of the HARP-2 = 2 days"]
-[6.042028427124023, -0.4526351988315582, "[TT] Duration of Mission of the Swarm = At least four years"]
-[6.128083229064941, 4.008849143981934, "[FF] Optics of the SSN dedicated satellites = Small aperture"]
-[6.456673622131348, 3.9129679203033447, "[TT] Technology of the Antennas = Metal 3D printing (additive manufacturing)"]
-[13.47927188873291, 6.826119899749756, "[TT] Electricity Production of the Arrays = More than 120 kW"]
-[11.711220741271973, 4.552144527435303, "[TT] Dimensions of the WISA Woodsat = 10 x 10 x 10 cm"]
-[5.992308139801025, 5.154364109039307, "[FF] Link Availability of the ISL = Immediately when they need it"]
-[6.808650970458984, 5.830835819244385, "[TT] Number of MFUU of the GIOVE-A = 2"]
-[6.20843505859375, 3.574342727661133, "[FF] Objective of the DHS = Establish a plug-and play space experiment brokering system"]
-[10.031021118164062, -1.5145710706710815, "[TT] Inclination of the ALL-STAR-1 = 51.6o"]
-[9.840347290039062, 4.847393035888672, "[TT] Final Antenna's Spin Speed of the SMAP spacecraft = Approximately 15 rpm"]
-[5.563607692718506, 5.619568347930908, "[TT] Main Processor of the DHU = MA 31750"]
-[10.617050170898438, 2.1704964637756348, "[FF] X-ray Nova Detection Date of the ISS Instrument = Oct. 4, 2010"]
-[7.499212741851807, 2.4477813243865967, "[FF] Spatial Coverage of the TANSO-CAI = Continuous"]
-[14.296313285827637, 3.211383819580078, "[TT] Packaging Weight of the MRM = 1.6 kg"]
-[6.570332050323486, 7.101954460144043, "[TT] Data Enhancement Technique of the Spire = Cutting-edge machine learning techniques"]
-[4.973921775817871, 1.8070943355560303, "[TT] Operation Status of the SPOT-4 = Nominal"]
-[9.790013313293457, 7.772579669952393, "[FF] Purpose of the SPIDER = Provide a 10 x to 100 x SWaP (Size, Weight, and Power) reduction alternative to the traditional bulky optical telescope and focal-plane detector array"]
-[8.67635726928711, 6.024171829223633, "[TT] Input Impedance of the Surface Potential Meter = Extremely large"]
-[9.274612426757812, 5.57719087600708, "[TT] Pointing Stability of the ASTERIA = 5 arcsecond RMS"]
-[7.3490166664123535, 4.620055198669434, "[FF] Function of the S/C Control (GNC-CTL) = Processes navigation estimates and guidance attitude profiles to generate the commanded torques needed to follow the reference profiles"]
-[8.043503761291504, -0.7304818034172058, "[TT] Number of Targets of the FormoSat-2 = 307 in northern polar areas, 37 in Antarctic areas"]
-[4.551450729370117, 6.220299243927002, "[TT] Beacon Transmission Frequency of the ELFIN-B = 437.475 MHz"]
-[3.8691565990448, 6.230609893798828, "[FF] Antenna Subsystem of the Severyanin-M = Consists of seven segments, six of which are deployed after launch with the central segment attached to the zenith-pointing deck of the satellite"]
-[11.749919891357422, 4.781484603881836, "[TT] Dimensions of the DSAT-1 = 100 x 100 x 227 mm"]
-[9.334735870361328, 7.058797836303711, "[TT] Spatial Resolution of the TAC = 2.1 m"]
-[4.7308831214904785, 7.023352146148682, "[TT] Image Transmission of the Spacecraft = X-band with 160 Mbit/s downlink rate"]
-[13.820582389831543, 2.654386281967163, "[TT] Launch Mass of the Spacecraft = 790\u00b130kg"]
-[10.777511596679688, 1.3367438316345215, "[TT] Size of the Primary Star = 4.3 times bigger than the Sun"]
-[10.454604148864746, 4.1035332679748535, "[TT] Quantity of the Hypersonic Grid Fins = 4"]
-[8.20537281036377, 8.376203536987305, "[TT] Readout Noise of the VNIR Detector = 130 \u00b5V rms"]
-[10.22111701965332, 3.1215639114379883, "[FF] Type of the ELaNa X = 3 P-PODs (Poly Picosatellite Orbital Deployers) containing a total of four CubeSats"]
-[5.757857322692871, 3.2201080322265625, "[TT] Goal Unit Cost of the Super Strypi = $12 million"]
-[8.216801643371582, 0.26125481724739075, "[FF] Orbit of the Asteroid 1999JU3 = From just inside the orbit of the Earth to just outside the orbit of Mars"]
-[9.387581825256348, 7.1590962409973145, "[TT] Spatial Resolution of the WFI = 55 m"]
-[3.4557225704193115, -0.9133493900299072, "[TT] Type of the Satellite Orbit = Sun-synchronous near circular dawn-dusk"]
-[5.577954292297363, 4.675472736358643, "[FF] Broadcasting Service Channels of the GK2A satellite = LRIT, HRIT, UHRIT"]
-[8.655324935913086, 6.00595235824585, "[TT] Type of the Surface Potential Meter = Contact type"]
-[13.315587997436523, 7.576162338256836, "[TT] Power Consumption of the Antenna = \u2264 750 W"]
-[6.961365222930908, -0.7239035367965698, "[TT] Orbital Period of the DS Tuc Ab = 8 days"]
-[12.162191390991211, 4.581475734710693, "[TT] Bus Diameter of the Resurs-O1 spacecraft = 1.4 m"]
-[4.199963569641113, 4.207643508911133, "[FF] New Home of the Program Office of the COSPAS-SARSAT = Montreal, Canada"]
-[9.693887710571289, 8.320680618286133, "[TT] FOV (Field of View) of the X-ray Imager = 4.6\u00ba x 4.6\u00ba"]
-[10.64759349822998, 3.402794122695923, "[TT] Size of the iADCS100 = Two standard CubeSat PCBs"]
-[5.869824409484863, -0.2867327928543091, "[TT] Maximum Daily Observations of the NEMO-AM = 2"]
-[6.679426670074463, 3.2882964611053467, "[FF] Operational Concept of the PRISMA = Servicing a variety of experimental teams for the flight demonstration of formation flying technologies"]
-[13.803536415100098, 2.675232172012329, "[TT] Maximum Launch Mass of the NightPod = 10 kg"]
-[12.07178783416748, 4.645086288452148, "[TT] Size of the Spacecraft = 100 mm x 100 mm x 227 mm"]
-[10.265859603881836, 5.359256267547607, "[TT] Heat Rejection Method of the CASSIOPE spacecraft = From strategically placed radiator surfaces along the bus hex sidewalls"]
-[6.406668186187744, 1.3172155618667603, "[TT] Arrival Date in Final Orbit Position of the COSMO-SkyMed-4 = April 2011"]
-[5.438061237335205, 0.018251676112413406, "[TT] Operation End Year of the IRS = 2019"]
-[8.269269943237305, 8.568339347839355, "[TT] Spectral Range of the Spectrometer = 5-11 \u00b5m"]
-[6.555532932281494, -0.5104354619979858, "[TT] Period of the ZY 1-02C = 100.3 minutes"]
-[5.704674243927002, -0.9286524653434753, "[TT] Outlived Design Lifetime of the ERBE = Factor of 5"]
-[14.315556526184082, 2.8200855255126953, "[TT] Mass of the Kondor = Up to 1000 kg"]
-[6.658381462097168, 0.7477405667304993, "[FF] Mission Status of the Herschel = Ongoing"]
-[3.3081886768341064, 1.4204678535461426, "[TT] Replacement Year of the Sentinel-2D = 2025"]
-[7.893660068511963, 3.941810369491577, "[FF] Purpose of the NASA Instrument = Determines Hazards of Deep-Space Radiation"]
-[2.298031806945801, 2.7628462314605713, "[TT] SSM of the EPI-Lo = Stamatios Krimigis"]
-[7.64335823059082, 3.4450302124023438, "[FF] Data Collection of the OLS sensor system = Infrared Fine resolution data (TF data) can be collected continuously, day and night. Visible fine (LF data) is collected during daytime only"]
-[7.477856159210205, 6.777851104736328, "[TT] NEDT, 12 s integration of the Radiometer = 0.05 K"]
-[9.614143371582031, 8.234331130981445, "[TT] Field of View of the ALI = 15\u00ba x 1.26\u00ba"]
-[13.783120155334473, 5.356015205383301, "[TT] Cell Types of the Solar Cells = GaInP/GaAs/Ge"]
-[5.77443265914917, 7.303736209869385, "[TT] Passes per Day of the GimmeRF = About two"]
-[10.93715763092041, 7.448008060455322, "[TT] Swath Width of the Sentinel-5P = 2600 km"]
-[8.927423477172852, 5.841266632080078, "[TT] TAG Angle Due to Absolute Time of Contact Error of the TAG Contact Safety Requirements = Less than 4.4\u00ba (3\u03c3) (~3 minutes)"]
-[9.164481163024902, 7.419126510620117, "[TT] MS of the Medium resolution = 10 \u00b5m x 10 \u00b5m"]
-[8.998583793640137, 10.266718864440918, "[TT] Pixel Resolution of the SPIM3 = 14 bit"]
-[4.457386016845703, 6.862037658691406, "[FF] Communication Type of the Wideband Internetworking Engineering Test and Demonstration Satellite \"KIZUNA\" = Broadband"]
-[10.047616958618164, -1.6074761152267456, "[TT] Inclination of the COMPASS-2 = 78.9\u00ba"]
-[5.498638153076172, 4.987690448760986, "[TT] Function of the GPS Receiver = Orbital position information"]
-[10.910663604736328, 10.10105037689209, "[FF] Service Life of the Alpha Magnetic Spectrometer (AMS-02) = Long after its original three-year mission"]
-[5.121978282928467, 3.526688575744629, "[TT] Manufacturer of the SSJ/5 = Amptek Inc."]
-[6.290444850921631, 4.087447643280029, "[FF] Responsibilities of the SC = Scientific experimental plan proposal, high-level data products generation, research and application functions organization"]
-[7.363707542419434, 2.3611104488372803, "[FF] Primary Coverage Location of the Meteosat = 0o location over the equator"]
-[5.1124267578125, 1.4471075534820557, "[FF] Expected Outcome of the MiRaTA = Great science data"]
-[6.653652191162109, -1.929814100265503, "[FF] Partner Responsibilities of the Jason-2 = Overall system integration, Earth terminals and part of the ground network, near-real-time product processing, archiving, product dissemination, user support, science algorithm development, calibration and validation activities"]
-[3.7518506050109863, 2.58073091506958, "[FF] Command and Data Path of the Iridium NEXT = MPLS cloud"]
-[6.062370300292969, 2.007540464401245, "[FF] URL of the Orion = http://www.nasa.gov/feature/orion-passes-the-pressure-test"]
-[5.694456577301025, 2.248166084289551, "[FF] Joint Endeavor of the ExoMars = ESA and Roscosmos"]
-[13.406213760375977, 7.342844009399414, "[TT] Power Requirement of the ISL = High"]
-[8.826848983764648, 7.646026134490967, "[TT] Pixel Size of the Imager = 30 x 30 \u00b5m"]
-[7.973220348358154, 8.526077270507812, "[FF] Uncertainty of the SIM = 0.42% for the range of 200-460 nm, 0.24% for the range of 460-2400nm"]
-[7.868111610412598, 6.404191017150879, "[FF] Objective of the Sich-2 = Obtain high-resolution imaging data in the visible and infrared region"]
-[13.24071979522705, 5.440503120422363, "[TT] Configuration of the Solar Arrays = Sun tracking"]
-[9.392335891723633, 7.098055362701416, "[TT] Spatial Resolution of the HY-1C = 1 km"]
-[5.5659589767456055, 2.2544238567352295, "[TT] Affiliation of the Junichi Kurihara = Hokkaido University"]
-[9.305007934570312, 0.5020794868469238, "[TT] Distance from Mars of the Tianwen-1 = 1.1 million kilometers"]
-[11.094714164733887, 4.093341827392578, "[TT] Area of the Drag Sail = Approximately 1 m2"]
-[10.068506240844727, 2.9492902755737305, "[TT] Development Cycle of the CubeSats = Six to twelve months"]
-[5.759360313415527, 0.23741956055164337, "[TT] Data Collection Duration of the RAVAN = 20 months"]
-[8.2782564163208, -0.4793677031993866, "[FF] Minimum Extent Area of the Arctic Sea Ice = 3.74 million km2 (1.44 million square miles)"]
-[5.529538631439209, 0.7056685090065002, "[TT] Release Date of the Figure 7 = Sept. 29, 2015"]
-[10.319201469421387, 7.981934070587158, "[TT] Diameter of the Telescope = 3 cm"]
-[7.940366268157959, 2.0118556022644043, "[TT] Bathymetric Map Coverage of the Hurricane Dorian = 130,000 km2"]
-[3.724963426589966, -0.755007803440094, "[FF] Orbit of the SEOSAT/Ingenio = Low Earth Orbit"]
-[9.349502563476562, 4.996654510498047, "[TT] Attitude Knowledge of the AOCS = 0.01\u00ba"]
-[8.136360168457031, -0.3969769775867462, "[TT] Extent Rank of the Arctic sea ice = Second-lowest"]
-[8.357816696166992, 7.502380847930908, "[FF] Type of the Photodetector = 3 mm FCI InGaAs quadrant photodiode with amplifier board"]
-[5.70871114730835, 5.9412946701049805, "[TT] Max No of Commands of the C&DH module = 500"]
-[10.161803245544434, 6.941868305206299, "[TT] Nominal Along-Track Separation of the EO-1 = One-minute (450 km), \u00b1 6 s (42.5 km)"]
-[8.08680248260498, 8.047284126281738, "[TT] Spectral Band of the Band Cameras = 336.2 nm"]
-[5.069642543792725, 3.4215073585510254, "[TT] Manufacturer of the EDRS-A and EDRS-C payloads = Tesat Spacecom (Backnang, Germany)"]
-[7.999473571777344, 6.378133296966553, "[TT] Operation Mode of the STEREO = Autonomous operation - beacon mode"]
-[8.812030792236328, 8.4429349899292, "[TT] Size of the Miniature High-Resolution Imaging Spectrometer = 360 x 260 x 180 mm"]
-[3.47357439994812, -0.9334878921508789, "[FF] Orbit of the KELT-9 b = Very close, nearly polar orbit around a rapidly rotating star"]
-[7.148413181304932, 2.3580551147460938, "[FF] Imagery of the Landsat-8 OLI = Data"]
-[8.390527725219727, 4.316781520843506, "[FF] Solar Calibration Components of the SeaWiFS = Solar radiation diffuser, input port"]
-[5.459264278411865, 5.010530948638916, "[TT] Communication Network of the TTCS = CAN (Controller Area Network) bus"]
-[7.873523235321045, 5.9657440185546875, "[FF] Component of the External Berthing Camera System (EBCS) = Unknown"]
-[8.327173233032227, 8.603914260864258, "[FF] Publication Date of the Extreme UV spectroheliometer = April 1977"]
-[3.8421342372894287, 0.8874025940895081, "[FF] Launch Date of the PSLV = Dec. 16, 2015"]
-[6.292613983154297, 8.020525932312012, "[TT] Number of Channels of the HSB = 4"]
-[13.09046459197998, 7.400198936462402, "[TT] Power Consumption of the GPSDR = 29 W"]
-[13.560468673706055, 6.029879093170166, "[TT] Solar Array Voltage Input of the SABR = Up to 65 V"]
-[9.885284423828125, 7.158933639526367, "[TT] Eastward Movement of the Band-64 = 17.4 km"]
-[6.205466270446777, 8.015833854675293, "[TT] Channels of the Receiver = 16 dual frequency channels (equal to 48 single channels)"]
-[5.593306064605713, 4.763742446899414, "[FF] Developer of the Deep-space Communications = UK"]
-[7.0674285888671875, 7.262070178985596, "[TT] Maximum Number of Optical Pulses in the FOV of the LI = 25 in 1 millisecond, 800 in 1 second"]
-[5.010281085968018, 6.424309730529785, "[TT] Mobility of the TUC Transponder = Mobile"]
-[7.975132465362549, 8.509889602661133, "[TT] Measurement Range of the PRI = 500\u2013600 nm"]
-[9.529855728149414, 5.02870512008667, "[TT] Agility of the Spacecraft = \u00b130\u00ba roll in 90 s"]
-[10.31390380859375, 5.888454914093018, "[TT] Operating Temperature of the VNIR = 257 K"]
-[8.972978591918945, 2.459352731704712, "[FF] Authors of the Interstellar Boundary Explorer = D. J. McComas, F. Allegrini, P. Bochsler, M. Bzowski, E. R. Christian, Gjson B. Crew, R. DeMajistre, H. Fahr, H. Fichtner, P. C. Frisch, H. O. Funsten, S. A. Fuselier, G. Gloeckler, M. Gruntman, J. Heerikhuisen, V. Izmodenov, P. Janzen, P. Knappenberger, S. Krimigis, H. Kucharek, M. Lee, G. Livadiotis, S. Livi, R. J. MacDowall, D. Mitchell, E. M\u00f6bius, T. Moore, N. V. Pogorelov, D. Reisenfeld, E. Roelof, L. Saul, N. A. Schwadron, P. W. Valek, R. Vanderspek, P. Wurz, G. P. Zank"]
-[4.853836536407471, 0.538536548614502, "[TT] Launch Timeframe of the Aditya-L1 = 2019 \u2013 2020"]
-[4.306879043579102, 7.4279093742370605, "[TT] Frequency of the Space Micro \u00b5STDN = S-band"]
-[5.329026699066162, 7.053509712219238, "[TT] Downlink Data Rate of the WCOM = 750 Mbps"]
-[8.257761001586914, 6.738483905792236, "[TT] Scene Scanning of the DNB = Sequential"]
-[4.317712306976318, 0.9697791934013367, "[FF] Launch Date of the Argos-3 = November 6th \u2013 November 7th"]
-[7.932316303253174, -0.49304819107055664, "[FF] Location of the Satellite = National Snow and Ice Data Center"]
-[12.785661697387695, 7.608639717102051, "[TT] Instrument Power of the ERIP = 3 W"]
-[4.232839107513428, 7.212493896484375, "[TT] Frequency Band of the S-band carrier reception = S-band"]
-[6.9556097984313965, 4.379745960235596, "[TT] Autonomy of the MPO-MAG instrument = Largely autonomous"]
-[8.407254219055176, 7.637576103210449, "[TT] Detector Operation of the SIS (Scanning Imaging Spectrograph) = Selected by a \u201cpop-up\u201d mirror"]
-[11.231074333190918, 1.0569967031478882, "[FF] Measurement System of the LISA Pathfinder = Optical metrology system"]
-[4.861415863037109, 0.05123509466648102, "[TT] End of Life Date of the Solar-A / Yohkoh = 23 April 2004"]
-[8.038690567016602, -0.7292873859405518, "[FF] Surface Velocities of the Wilkins Ice Shelf = 1994\u201396 and between 2006 and 2010"]
-[7.816794395446777, 9.015213012695312, "[TT] Input Angle alpha of the Long Wavelength Band = 21.9\u00ba"]
-[8.263206481933594, 3.1454100608825684, "[FF] Data Products of the Ozone Monitoring Instrument (OMI) = Available at the NASA GES DISC"]
-[8.532201766967773, 7.621651649475098, "[TT] Array Size of the MBA detector = 327 x 240"]
-[8.103543281555176, 7.565061092376709, "[TT] Sensor Type of the TET-1 = Mid-wave and longwave infrared"]
-[8.49466323852539, 3.035485029220581, "[FF] Avoided Objects of the Observation Restrictions = Earth and its atmosphere, the Moon, the bright planets, the Milky Way, the galactic band within \u00b1 30\u00b0 from the galactic plane"]
-[11.571160316467285, 3.4749631881713867, "[TT] Propulsion of the SES-17 = Electric"]
-[7.975877285003662, 3.3921539783477783, "[FF] Application of the Compact off-axis telescope = Satellite-borne instrument for atmospheric research"]
-[9.770904541015625, 2.695469856262207, "[TT] Operation Start of the EXCISS = As soon as the universal serial bus (USB) connects to the NanoRacks platform"]
-[6.249363422393799, 4.5636749267578125, "[FF] Functions of the FOS = Operation and control of the satellite, provision of telemetry"]
-[4.938570976257324, 2.050398826599121, "[TT] Operator of the Himawari-8/9 Ground Segment = Himawari Operation Enterprise Corporation (HOPE)"]
-[5.532658100128174, 2.233988046646118, "[FF] Affiliation of the Yuji Sakamoto = Unknown"]
-[5.9952073097229, 5.9205522537231445, "[TT] Data/Pilot of the E5a-Q = Pilot"]
-[6.3378729820251465, -1.3619474172592163, "[TT] Launch Date of the GRACE Follow-On = August 2017"]
-[7.742737770080566, 2.1447792053222656, "[FF] Applications of the Resurs-O1 = Observation of the state of agricultural crops, assessment of hydrological conditions, forest and tundra fires, pollution monitoring"]
-[6.135887145996094, -0.1292908936738968, "[TT] Daily Operation Time of the SAOCOM-1A = 450 minutes per day"]
-[5.866990089416504, 1.7845979928970337, "[TT] Landing Date of the Orion spacecraft = Dec. 5, 2014"]
-[6.769575595855713, 3.192732334136963, "[FF] Impact on Astronomical Observations of the Satellite Constellations = Not specified"]
-[8.592556953430176, 4.625339031219482, "[FF] Function of the \u00b5STR = Determines the orientation of the satellite by tracking it relative to the position of the stars"]
-[7.414074420928955, 5.119384765625, "[TT] User's Handbook Version of the ILAS-II = 1.1"]
-[9.360644340515137, 5.087183475494385, "[TT] Attitude Determination Accuracy of the ADCS = \u22640.03\u00ba (3\u03c3, 3-axis)"]
-[9.767488479614258, -0.5500098466873169, "[TT] Altitude of the Orbit = 686 km"]
-[4.706371784210205, 7.094676971435547, "[TT] Telemetry S-band of the RF communications = 0.1 W, 9.6 kbit/s"]
-[10.178685188293457, 9.380928039550781, "[TT] Nominal IGFOV of the Band 12 = 2 km"]
-[10.082399368286133, -1.5803654193878174, "[TT] Inclination of the GEMS = 0\u00ba"]
-[7.208600997924805, 1.2520573139190674, "[TT] Trace Gas Orbiter (TGO) of the ExoMars = Launched in 2016"]
-[9.668179512023926, 8.231468200683594, "[TT] Field of View of the POLDER = \u00b157\u00ba diagonal"]
-[6.406121253967285, 1.135424256324768, "[FF] Presentation Date of the COSMIC-2 = April 3, 2015"]
-[7.656214714050293, 8.740422248840332, "[TT] Spectral Range of the MSU-S = 0.58 - 0.7 \u00b5m, and 0.7 - 1.0 \u00b5m"]
-[3.0962843894958496, 2.1500720977783203, "[FF] New Name of the Copernicus = Copernicus"]
-[4.317930221557617, 2.445611000061035, "[TT] Launch Site of the Meteor-M2 spacecraft = Baikonur Cosmodrome, Kazakhstan"]
-[5.250593662261963, 1.4068934917449951, "[FF] Progress Update of the TET-1 = Aug. 10, 2012"]
-[6.830824851989746, 3.7304108142852783, "[FF] Unknown of the NASA/JPL = Unknown"]
-[6.488273620605469, 2.0824713706970215, "[FF] Status of the Microsat-R = Destroyed"]
-[7.605036735534668, -0.03666658326983452, "[TT] Historic Landing Date of the Philae lander = 12 November 2014"]
-[5.75435733795166, 5.3708696365356445, "[FF] Technology of the SES-17 = Fully-digital and highly-innovative"]
-[9.272883415222168, 5.254958629608154, "[TT] Pitch Steering Capability of the Spacecraft = Up to \u00b1 13\u00ba"]
-[5.036600112915039, 1.3929672241210938, "[FF] Workshop Date of the GIOVE-A and GIOVE-B = October 13, 2008"]
-[8.533857345581055, 0.8978483080863953, "[TT] Seismometer Distance from Lander of the InSight Lander = 1.636 m"]
-[4.559749603271484, -2.7980382442474365, "[TT] Frequency Capability of the PMI = 6.8/7.2-90 GHz"]
-[10.029794692993164, -1.5369676351547241, "[TT] Orbit Inclination of the ERBS = 57\u00ba"]
-[7.817206859588623, 5.6358137130737305, "[FF] Calibration Mode Components of the LIBRA = Rotating mirror, middle optics, two monochromators, avalanche photodiodes"]
-[9.721041679382324, 8.001747131347656, "[TT] FOV of the HRI dual EUV 174 \u00c5 and 335 \u00c5 alternatively = 1000 arcsec x 1000 arcsec"]
-[6.536640167236328, 1.6180219650268555, "[FF] Instruments of the Europa Clipper = EIS, E-THEMIS, Europa-UVS, MISE, ECM, PIMS, Gravity & Radio Science, REASON, MISE, MASPEx, SUDA"]
-[11.730325698852539, 3.2958383560180664, "[TT] Thruster Pairs of the Propulsion Subsystem = 3"]
-[7.691651821136475, 9.21944522857666, "[TT] Wavelength Range of the Band 14 = 10.8-11.6 \u00b5m"]
-[13.289999008178711, 7.657328128814697, "[TT] Peak Transmit Power of the NSCAT = 110 W"]
-[8.148032188415527, 2.166905164718628, "[FF] Science Objectives of the TROPICS = Assimilate microwave radiances and/or retrievals in mesoscale and global numerical weather prediction models to assess impacts on storm track and intensity"]
-[8.876208305358887, 5.736839771270752, "[TT] Pointing Accuracy of the S/C = 0.12\u00ba, 0.02\u00ba"]
-[4.262982368469238, 7.4854254722595215, "[TT] Frequency Band of the X-band Transmitter = 8.025 and 8.4 GHz"]
-[9.312840461730957, 10.74027156829834, "[TT] Polarization of the ICI-8 = V"]
-[5.438211917877197, 0.8307661414146423, "[FF] Logo Release Date of the Hera = 3 May 2019"]
-[8.475022315979004, 6.58780574798584, "[FF] Principle of the Microbolometer = Detecting infrared energy as minute changes of the IR absorber temperature when infrared radiation id detected"]
-[10.269283294677734, 7.517200469970703, "[TT] Swath Width of the SIR-C = 40 to 90 km for mapping mode (ScanSAR) images"]
-[4.739226341247559, 5.62025260925293, "[TT] Doppler Correction of the Communication System = Pre-correcting Doppler"]
-[4.91168737411499, 0.6387856006622314, "[TT] Launch Date of the TEMPO = 7 April 2023"]
-[5.131166934967041, -0.5271652340888977, "[TT] Launch Date of the TARANIS = 17 November 2020"]
-[12.778247833251953, 2.005389451980591, "[TT] Observation Range of the SAGE III = 70\u00b0S"]
-[8.026982307434082, 8.689765930175781, "[TT] Spectral Range of the SSULI = 80 to 170 nm"]
-[9.475271224975586, 0.5671841502189636, "[TT] Diameter of the Schiaparelli = 2.4 m with heatshield, 1.65 m without heatshield"]
-[9.099753379821777, 7.701344966888428, "[TT] Plate Scale of the TOU = 15 arcsec/pixel"]
-[4.880157470703125, 3.554250717163086, "[TT] Manufacturer of the Hiber-3 = Hiber"]
-[8.454890251159668, 3.793672800064087, "[FF] Calibration Task of the Machine Learning Algorithm = Recognize solar structures and determine calibration needed"]
-[7.570775032043457, 4.99683952331543, "[FF] Purpose of the IQS Workstations = Analysis of data and generation of calibration information"]
-[8.980921745300293, 5.557989597320557, "[FF] Pointing Stability Requirements of the TEMPO = High precision"]
-[8.148971557617188, -0.7197996973991394, "[TT] Objective of the Severyanin-M = Sea ice monitoring in the polar regions"]
-[4.606209754943848, 2.7402191162109375, "[TT] Location of the ERSDAC = Japan"]
-[3.8852739334106445, 4.527054309844971, "[FF] Function of the RADARSAT-2 = Ship detection with SAR imagery"]
-[8.615715980529785, 4.748926162719727, "[TT] Type of the Star tracker = Star tracker"]
-[5.306975841522217, 3.082465410232544, "[TT] Contractor of the GOES-R Series = Lockheed Martin"]
-[10.95391845703125, 7.501971244812012, "[TT] Swath of the MWRI-RM = 800 km"]
-[4.326601505279541, -0.1266513615846634, "[TT] Launch Date of the P35-1 = 23.51962"]
-[5.655775547027588, 2.439760208129883, "[FF] Teamwork Importance of the AzTechSat = Crucial"]
-[8.798497200012207, 7.116683006286621, "[TT] Imaging Mission of the SSOT = High-resolution"]
-[5.190160751342773, 2.7686092853546143, "[TT] Abbreviation of the MTSAT = Multifunction Transport Satellite"]
-[5.260868549346924, 0.7717210054397583, "[TT] Launch Contract Date of the 90-satellite constellation = January 15, 2019"]
-[7.505768299102783, 3.134603977203369, "[FF] Purpose of the GOES-R = Geostationary meteorological imager"]
-[6.158475399017334, 3.594923734664917, "[FF] Satellite Mission Types of the Spacety = Science experiments or observation, in-orbit demonstrations and/or validations of space technologies and products, or space systems"]
-[6.69075345993042, 5.193366050720215, "[FF] Data Acquisition of the DAC = Acquires temperature, current, and logic state values from sensors"]
-[10.912646293640137, 10.101696014404297, "[TT] Mission Duration of the Alpha Magnetic Spectrometer - 02 (AMS-02) = Since 2011"]
-[6.359649181365967, 1.2275620698928833, "[FF] Presentation Date of the Membrane Photon Sieve Space Telescope = May 21, 2013"]
-[8.520402908325195, 3.8529932498931885, "[FF] Technology of the RAVAN = Carbon nanotubes that absorb outbound radiation and a gallium phase change blackbody for calibration"]
-[9.492047309875488, 7.104577541351318, "[TT] Spatial Resolution (VIS) of the ABI = 0.64 \u00b5m"]
-[12.729185104370117, 1.9541445970535278, "[TT] Mission Duration of the SAGE III = Three years"]
-[6.5841145515441895, 4.188496112823486, "[FF] Function of the CoReCi = Process, store and format multi-spectral video instrument data for the satellite downlink"]
-[4.132410526275635, 1.4004749059677124, "[TT] Exploitation Period of the Meteosat-1 = November 1983 until November 1995"]
-[4.211339950561523, 7.273355484008789, "[TT] Frequency of the DRS = S-band and X-band"]
-[4.1199469566345215, 4.199751853942871, "[FF] Development of the SARSAT = France, Canada, and the USA"]
-[9.360776901245117, 3.1271543502807617, "[TT] Movement Range of the Coronagraph Spacecraft = \u00b125 mm along the Z and Y axes"]
-[6.949448108673096, -1.7423228025436401, "[TT] Objective 3 Requirement of the Jason-CS = Global sea surface height to an accuracy of < 4 cm every 10 days"]
-[10.093809127807617, 1.458524227142334, "[FF] Thick Disc Gas Mixing of the Milky Way = Well-mixed"]
-[12.999576568603516, 7.577118873596191, "[TT] Instrument Power of the NSCAT = 240 W"]
-[8.389955520629883, 1.453924536705017, "[FF] Salinity of the Arabian Sea = High"]
-[6.695844650268555, 5.9985785484313965, "[TT] Modes of the BlackJack = C/A, P, or codeless"]
-[12.324021339416504, 7.528440475463867, "[TT] Current Consumption of the LinkSprite JPEG color VGA camera = 80-100 mA"]
-[3.906447649002075, 4.455411434173584, "[FF] Follow-up System of the RCM = RADARSAT-2"]
-[4.503142356872559, 0.006315683014690876, "[TT] Re-entry Date of the Starshine = Feb. 8, 2000"]
-[4.995655536651611, 4.8310675621032715, "[FF] Communication Objective of the QUESS satellite = \"hack-proof\" quantum communications"]
-[7.0187668800354, 5.045176982879639, "[FF] Measurement of the GPS = Target distance"]
-[5.070230484008789, 5.086483955383301, "[TT] Log Size of the GPS Receiver = Approximately 200-300 bytes"]
-[11.626250267028809, 6.872060298919678, "[TT] Effective Area of the ART-XC = 455 cm^2 at 8 keV"]
-[9.663033485412598, 8.375187873840332, "[TT] FoV of the TOU = ~1037\u00ba x 1037\u00ba"]
-[12.007498741149902, -0.23629720509052277, "[TT] Sky Coverage of the TESS = 85 percent"]
-[5.38475227355957, 1.6349639892578125, "[FF] Observation Location of the ALOS satellite = Al Jawf oasis in southeastern Libya"]
-[5.6150407791137695, -0.5393255352973938, "[TT] Planned Operational Lifetime of the Heinrich Hertz = 15 years"]
-[4.833110809326172, 7.381109237670898, "[TT] Data Rate of the UHF Transceiver = 4Kbps"]
-[8.65101432800293, 8.812654495239258, "[TT] Grating Type of the OCO-3 = Reflection gratings"]
-[7.090412139892578, 7.217308521270752, "[TT] Pulse Rate of the ATLAS = 10,000 pulses/s"]
-[3.576026201248169, -1.0060356855392456, "[FF] Future Evolution of the Star and its Orbit = More circular and grow in size"]
-[9.15683364868164, 7.443904399871826, "[TT] Resolution of the Visible Camera = < 0.5 km"]
-[7.952958106994629, 8.652942657470703, "[TT] Spectral Range TIR of the MVIRI = 10.5 - 12.5 \u00b5m"]
-[6.1112284660339355, 3.0385377407073975, "[TT] Capacity to Collect Imagery of the WorldView Legion satellites = 30 cm and multi-spectral"]
-[10.244166374206543, 8.036962509155273, "[TT] Telescope Length of the TRACE instrument = 160 cm"]
-[8.46595573425293, 1.7493009567260742, "[TT] Landfall of the Hurricanes Eta and Iota = Central America, same part of Nicaragua"]
-[8.51358699798584, 5.672577381134033, "[TT] Vertical Accuracy of the Galileo Service = 8 m"]
-[5.614131927490234, -0.23336496949195862, "[TT] Minimum Success Criteria of the SMDC-One = 6 months"]
-[5.298895835876465, 3.891937732696533, "[TT] Number of Satellites of the Long March 6 = 13"]
-[3.3730480670928955, -0.34037208557128906, "[TT] AMOS Terminator Passes of the SpinSat = 3"]
-[11.755334854125977, 6.7737650871276855, "[TT] Energy Resolution of the HXD = \u2264 10% at 59.5 keV"]
-[6.432821750640869, 3.5808897018432617, "[FF] Data Access of the GPM = Free and available to the public"]
-[7.4147491455078125, 5.029630184173584, "[FF] Probability Calculation of the Coherency Filter = Based on event intensity, the electronics noise, and the photon noise of the background"]
-[8.0804443359375, 0.887363076210022, "[TT] Extreme to Exceptional Dryness Percentage of the U.S. Drought Monitor = 83 percent"]
-[9.49543571472168, 6.04197883605957, "[TT] Cross-Track of the WAOSS-B = 50\u00b0"]
-[4.11169958114624, 5.723923683166504, "[FF] Conference Date of the Space-based ADS-B = Nov. 19-30, 2012"]
-[8.868355751037598, 8.46544361114502, "[TT] Dimensions of the Micro-spectrometer = 50 mm x 60 mm x 80 mm"]
-[8.2775297164917, 8.666074752807617, "[FF] Spectral Resolution of the EO System = <8 nm"]
-[7.354150772094727, 3.367384195327759, "[FF] Objective of the SAS = To demonstrate the capabilities of a new type of infrared Earth sensor over a range of altitudes from LEO to GEO in a harsh radiation environment on a slow-spinning satellite"]
-[9.562967300415039, 4.283372402191162, "[TT] Number of Voltage Probes of the FIELDS suite = 5"]
-[7.522405624389648, 6.766512393951416, "[TT] Time Resolution of the CCD = 2.6 seconds"]
-[7.310174942016602, 8.379684448242188, "[TT] Fringe Distortions of the SHS = Degrade the instrumental profile and reduce the signal-to-noise ratio"]
-[7.850142478942871, 6.601698875427246, "[TT] Pole Observation Time of the Cameras = More than 80 days"]
-[5.256524085998535, 0.08170662075281143, "[FF] Arrival Date of the Cygnus = 14 Nov. 2017"]
-[7.335893630981445, 8.340057373046875, "[FF] Spectral Cross-Talk Minimization of the Optical Filters = Masks"]
-[6.982509136199951, 5.026885986328125, "[FF] Processes the return signal of the LCEU = Yes"]
-[4.004456996917725, 6.965631008148193, "[TT] Interface of the CPUT STX = 7 dBi S-band patch antenna"]
-[8.221013069152832, 8.81200122833252, "[TT] Spectral Resolution of the MAHRSI = 0.018 nm"]
-[7.848510265350342, 8.391152381896973, "[TT] Spectral Bands of the NTSIC = Panchromatic:1 MS (Multispectral): 6 bands"]
-[6.434643268585205, 1.9621448516845703, "[FF] URL of the OPS-SAT = http://www.esa.int/ESA_Multimedia/Videos/2019/12/OPS-SAT_the_flying_laboratory"]
-[9.301420211791992, -1.14747154712677, "[TT] Orbit of the WINDS = Geostationary orbit (GEO) over the Pacific Ocean at 143\u00ba E longitude, altitude ~ 35,786 km"]
-[9.388891220092773, 8.249601364135742, "[FF] Group FoV of the Camera = All 6 cameras of each group have exactly the same FoV"]
-[6.067233562469482, 3.309990882873535, "[TT] Experiment Proposals of the OPS-SAT = 55"]
-[5.181715965270996, 5.0009660720825195, "[TT] Fix Interval of the NovAtel OEMV-1 GPS receiver = Approximately once every 25 hours"]
-[1.745987057685852, -2.0753703117370605, "[TT] Touchdown Date of the Hayabusa-2 = February 22, 2019"]
-[8.415903091430664, 3.224480628967285, "[TT] Precision of the Ozone Measurement Instrument = 3%, 15-50 km"]
-[3.68697190284729, 6.699748992919922, "[TT] Half-Power Half-Beamwidth of the High Gain Antenna = 4.0\u00ba"]
-[4.023659706115723, 2.1835739612579346, "[TT] Launch Vehicle Configuration of the GOES-T = 541 version of the Atlas 5 with four solid-fuel boosters"]
-[12.011693954467773, -0.3758818507194519, "[TT] Lead Institution of the TESS = MIT (Massachusetts Institute of Technology)"]
-[10.039495468139648, -1.5534123182296753, "[TT] Orbit Inclination of the CBERS-4 = 98.55\u00ba"]
-[8.305461883544922, -0.49569937586784363, "[TT] Extent of the Sea Ice = 4.72 million km2"]
-[13.385353088378906, 5.493222713470459, "[TT] Solar Array of the Orion = Designed to bend up to 60\u00ba forward and backward"]
-[11.733543395996094, 3.283677339553833, "[TT] Number of Reaction Control Thrusters of the Propulsion Subsystem = 16"]
-[5.951079368591309, 4.42842435836792, "[FF] Mobility of the USAT = Can be used while being moved in off-road and all-weather conditions"]
-[6.500854015350342, 2.198286533355713, "[FF] CCDs of the eROSITA = Not provided"]
-[10.358927726745605, 5.436726093292236, "[TT] Thermal Control of the Blackbodies = Continuous"]
-[7.820688724517822, 9.009540557861328, "[TT] Wavelength Range of the S3 = 300-800 nm"]
-[6.158939838409424, 4.190154552459717, "[FF] Type of the SGR-07 = Space"]
-[7.640502452850342, 2.0844950675964355, "[FF] Biomass Estimate Comparison of the GEDI = Compared favorably to forest inventories from the Food and Agriculture Organization of the United Nations and U.S. Forest Service Forest Inventory and Analysis data"]
-[4.856001853942871, 0.09007148444652557, "[FF] Launch Date of the SpaceX CRS -5Mission = December 2014"]
-[4.794787883758545, 0.46813613176345825, "[TT] Launch Date of the Monitor-E = Aug. 26, 2005"]
-[14.496088027954102, 6.597757339477539, "[TT] Battery Capacity of the BRITE spacecraft = 5.3 Ah"]
-[7.800284385681152, 5.827751159667969, "[TT] Type of the IKFS-2 = Imaging multi-spectral radiometers (passive microwave)"]
-[6.479625701904297, 4.667625427246094, "[FF] Modularity of the AIT Approach = Parallelize activities and reduce the lead time"]
-[8.760662078857422, 0.07050252705812454, "[TT] Observation Region (Summer) of the WNISAT-1 = Northern latitude range of 70-80\u00ba"]
-[10.270892143249512, 7.398266315460205, "[FF] Design of the Rotating Telescope Scanner = Three-mirror anastigmat, rotating at constant speed about an axis parallel to the line-of-sight, followed by a HAM (Half-Angle-Mirror), a plane mirror rotating at half of the telescope speed"]
-[14.008442878723145, 3.8939566612243652, "[TT] Mass of the Monitor-E = 700 kg"]
-[9.20412540435791, 3.2417001724243164, "[TT] Observable of the COR1 = K-corona and CMEs"]
-[9.444435119628906, 3.591611385345459, "[FF] Symmetry of the Earth's main magnetic field = Not Geometrically Opposite"]
-[5.9112629890441895, 0.3534320890903473, "[TT] One Year on Orbit Date of the MaSat-1 = Feb. 13, 2013"]
-[7.830350875854492, 1.3552566766738892, "[FF] Preliminary Design of the Water Cycle Observation Mission (WCOM) = Unknown"]
-[5.356378555297852, 5.642332077026367, "[TT] Interface of the CEASE = RS-422 or 1553B"]
-[13.397726058959961, 6.744591236114502, "[TT] Power of the DubaiSat-1 = 53.2 W"]
-[14.203364372253418, 3.273702383041382, "[TT] Mass of the MTQ = 225 g"]
-[6.566303730010986, 1.7606531381607056, "[FF] URL of the COCTS = https://www.wmo-sat.info/oscar/instruments/view/88"]
-[4.987691402435303, 0.39649370312690735, "[TT] Installation Date of the SpaceChain's multisignature blockchain payload = 2020"]
-[5.221019268035889, 2.4501304626464844, "[TT] Mission of the MTG-S = Sounding"]
-[7.877800941467285, 9.007915496826172, "[TT] Wavelength Coverage of the UVS Instrument = 215 nm (cha. 1), 236.5 nm (cha. 2)"]
-[7.384272575378418, 6.55273962020874, "[FF] Function of the BSA = Deviating a pulsed high-energy UV laser beam to compensate for the pointing misalignment between the emission and reception paths of ATLID"]
-[6.340219020843506, 8.096174240112305, "[TT] Number of Channels of the CTECS-A = 16"]
-[4.523810386657715, 7.922021865844727, "[TT] RF Uplink Frequency of the DCP = Between 402.001 and 402.199 MHz"]
-[10.867244720458984, -0.313381165266037, "[FF] Presentation Date of the TanDEM-X = July 23\u201328, 2017"]
-[6.968703746795654, 3.445124626159668, "[FF] Purpose of the MANTIS = Provide low-latency and targeted imagery tailored to the data needs of the oil and gas sector"]
-[4.633749961853027, 2.88555645942688, "[FF] Control Station Location of the JERS-1 = Tracking and Control Center (TACC), located at the Tsukuba Space Center"]
-[5.5077385902404785, 6.395759582519531, "[TT] Solid-State Memory of the Command and Data Handling Subsystem = 300 MByte"]
-[9.401705741882324, 0.9932911396026611, "[TT] Speed Relative to Jupiter of the Juno = Almost 130,000 mph (210,000 km/h)"]
-[7.649463653564453, 5.984715938568115, "[FF] Task of the OBC = Marshalling of images from the smartphone, via the HPC to the transmitter"]
-[6.167285919189453, -0.26584938168525696, "[TT] Duration of the Experiment = Up to 4 months"]
-[5.553185939788818, -1.891521692276001, "[FF] URL of the KOMPSAT-3 = http://kompsat.satreci.com/ds4_2_1.html?db=gal"]
-[3.4174211025238037, 5.327450275421143, "[TT] Average DC Input Power of the SAR = 1.8-3.9 kW"]
-[5.354203701019287, 3.479017972946167, "[FF] Image of the Terminator Tape Deorbit Module = Prototype version of the Terminator Tape Deorbit Module"]
-[11.653718948364258, 4.336583614349365, "[TT] Diameter of the Payload Fairing = 4 meters"]
-[6.009631156921387, 5.762196063995361, "[TT] FPGA of the SCU = XQ2V1000-4FG456N (Virtex2)"]
-[11.698074340820312, 3.3448686599731445, "[TT] Type of the Electric thruster = Small"]
-[4.139959812164307, 5.834528923034668, "[TT] Data Collection Frequency of the ADS-B receiver = 1090 MHz"]
-[4.627255439758301, 7.324312210083008, "[TT] S-band 1Mbit/s Downlink Data Rate of the UoSAT-12 = 1Mbit/s"]
-[4.808252334594727, 3.0150978565216064, "[TT] Affiliated Countries of the PUTC = France, Belgium, Spain, Sweden and Austria"]
-[3.7480082511901855, 6.6642045974731445, "[TT] Antenna Beamwidth of the Satellite = 1.33\u00ba (Ku-band), 5.25\u00ba (S-band)"]
-[14.202648162841797, 3.231137990951538, "[TT] Mass of the MC-U = ~ 2 kg"]
-[14.032877922058105, 6.328738212585449, "[TT] Model of the OBC = GomSpace NanoMind A712D"]
-[10.964747428894043, 7.587085247039795, "[TT] Swath Width of the PP = Approximately 28 km"]
-[13.949196815490723, 2.8374574184417725, "[TT] Launch Mass of the Bion-M1 = ~6,840 kg"]
-[9.740937232971191, -0.5814558863639832, "[TT] Operating Orbits of the MS-2 = Near-Earth orbits in the altitude range from 500 to 700 km"]
-[12.926889419555664, 7.1551666259765625, "[TT] Efficiency of the HPA = 25%"]
-[10.32620906829834, 4.032558917999268, "[TT] Boom Type of the VIRR = Deployable"]
-[9.040753364562988, 2.974818229675293, "[TT] Publication Year of the The Transition Region and Coronal Explorer = 1999"]
-[11.654141426086426, -0.019289130344986916, "[TT] Closest Approach Distance to Lunar Surface of the TESS = 8,253 km"]
-[5.642644882202148, 3.2707648277282715, "[TT] Consideration of the Eutelsat Communications = $165 million"]
-[5.107929229736328, 2.3812315464019775, "[TT] Mission Type of the SLATS = Non-EO"]
-[7.730581283569336, 2.8576998710632324, "[TT] Function of the Green City Watch = Quantify the CO2 uptake of urban green spaces"]
-[4.876036643981934, 0.2434643656015396, "[TT] Launch Date of the STRV-2 = June 7, 2000"]
-[7.36325216293335, 2.447906494140625, "[FF] Global Coverage of the ILRS = Yes"]
-[4.546884536743164, 3.848628520965576, "[TT] Number of Satellites of the Galileo = Two"]
-[7.178732872009277, 3.9274473190307617, "[FF] OpNav Process of the Spacecraft = Full shape model creation"]
-[5.705379486083984, 7.292555809020996, "[TT] Receiver Recovery Time of the RAX-1 = Within 100 microseconds"]
-[8.230549812316895, 7.816418170928955, "[FF] Number of Detectors of the ULEIS = Six"]
-[5.159006595611572, 0.7365646362304688, "[FF] Launch Date of the Unknown = Dec. 17, 2015"]
-[3.4552812576293945, -0.9080120325088501, "[TT] Orbit Type of the SPOT 6-7 = Sun-synchronous"]
-[5.352728366851807, 8.692855834960938, "[TT] Bandwidth of the CZI = 0.42-0.89 \u00b5m"]
-[9.21178913116455, 8.698484420776367, "[TT] Slit Width of the Long Wavelength Band = 150 \u00b5m"]
-[6.502668380737305, 6.639892578125, "[FF] Technology of the EDRS = Optical and Ka-band"]
-[10.131567001342773, -2.73730731010437, "[TT] Capacity of the NAND-Flash device = 32 Gbit"]
-[4.385576248168945, 2.0295708179473877, "[TT] Launch Date of the DubaiSat-2 = 21 November, 2013"]
-[7.487978458404541, -0.8927088975906372, "[TT] Mission Duration of the ICESat-2 = Decade-long"]
-[13.620129585266113, 6.347414016723633, "[TT] Quantity of the EPS Panels = 13"]
-[5.4604597091674805, 6.506999969482422, "[TT] Data Handling of the LT = Deletes SOH and science data from its crosslink queue"]
-[7.0177764892578125, 1.3232258558273315, "[FF] Operation Period of the CoRoT space telescope = 2006 to 2013"]
-[4.818544387817383, 7.915162086486816, "[TT] Frequency of the Receiving Frequency = 401.65 MHz\u00b10.0405 MHz"]
-[6.294119358062744, -0.7057560682296753, "[TT] Space Walk Duration of the Skylab = Three and a half hours"]
-[12.108011245727539, 7.640188217163086, "[TT] Instrument Mass of the Pushbroom imager = 18.5 kg"]
-[9.510551452636719, 6.090424060821533, "[TT] Incidence at the ground about of the S-193 = 35\u00ba"]
-[10.83630084991455, -0.2687799632549286, "[TT] Imaging Mode of the TanDEM-X = Left-looking"]
-[13.825592041015625, 5.331030368804932, "[TT] Cell Type of the Solar Panels = Third generation Azur GaAs triple junction cells"]
-[9.54172420501709, 7.039671897888184, "[TT] Spatial Resolution of the TopSAR wide = < 50 m"]
-[7.742501735687256, 9.045913696289062, "[TT] Band Spacing of the OHIS = 25 nm"]
-[13.532510757446289, 3.632927656173706, "[TT] Mass of the Miniaturized X-band transponders = < 0.300 kg"]
-[3.2428035736083984, 2.2248542308807373, "[TT] Deployment Test Location of the Copernicus Sentinel-1C = Airbus\u2019 facilities in Germany"]
-[6.025066375732422, 1.1604197025299072, "[FF] Response Date of the NASA = July 10, 2015"]
-[13.548188209533691, 2.8438429832458496, "[TT] Dry Mass of the GOES-R = < 2800 kg"]
-[6.3982062339782715, 4.6048173904418945, "[FF] Function of the PASTEC = Study the orbital environment, studying concepts such as the measurement of satellite dynamics (MEDY) and electrostatic potentials outside the SPOT spacecraft (SILLAGE)"]
-[6.694215774536133, -0.3635563552379608, "[TT] Yaw Maneuvers Frequency of the ERBE = Approximately every 36 days"]
-[12.030369758605957, 4.748753070831299, "[TT] Body Shape of the Bus = Square-shaped"]
-[6.258652687072754, 8.035120964050293, "[TT] Channel Nr. of the SSM/I = 1, 2, 3, 4, 5, 6, 7"]
-[8.086658477783203, 3.5800247192382812, "[TT] Characterization of the OCO-2 = Before Observatory launch"]
-[7.740591526031494, 5.248308181762695, "[FF] Publication Year of the Special Sensor Microwave/Imager (SSM/I) and Special Sensor Microwave Imager Sounder (SSMIS) = 2010"]
-[8.115670204162598, 3.085179567337036, "[FF] Required Climate Record of the Infrared Spectrometer = 12 years to reach a trend uncertainty of 0.2 K/decade at 95% confidence"]
-[8.086342811584473, -1.27781081199646, "[TT] Signal Photons per Laser Shot of the ICESat-2 = 8.5 for strong beam, 2.1 for weak beam"]
-[8.01140022277832, 2.7446351051330566, "[FF] Types of the Output Products = Ground reflectance cube, maps of the aerosol optical thickness and atmospheric water vapor, masks of land, water, haze, cloud, shadow and snow"]
-[6.912669658660889, 1.57823646068573, "[FF] Development Status Presentation of the James Webb Space Telescope = Jon Arenberg, \"JWST Development Status,\" 213th AAS (American Astronomical Society) Meeting, Long Beach, CA, USA, Jan. 4-8, 2009"]
-[4.737040042877197, 8.018533706665039, "[TT] Frequency Range of the RFA = 26-48 MHz"]
-[7.38223934173584, 0.9828048348426819, "[FF] URL of the GRAIL = http://science.nasa.gov/headlines/y2008/22may_grail.htm"]
-[4.366755962371826, 7.796547889709473, "[TT] Downlink Frequency of the RF communications = 2.207 GHz"]
-[6.752103328704834, 5.8818440437316895, "[TT] Quantity of the XPOD = 6 units"]
-[7.6367573738098145, 1.300926923751831, "[FF] Objective of the PanCam = Acquire 3D imagery of the lunar surface"]
-[5.146050453186035, 3.772651195526123, "[TT] Provider of the Sensor bus system = Kayser-Threde GmbH"]
-[5.620606899261475, 5.545044422149658, "[TT] Model of the Microcontroller = PIC24"]
-[8.95652961730957, 2.53342866897583, "[TT] Mission of the IBEX = Interstellar Boundary Explorer"]
-[9.085576057434082, 6.439677715301514, "[TT] Image Location of the CaSSIS = 29.2\u00baS/66.8\u00baE"]
-[9.581311225891113, 5.847591876983643, "[TT] FOR of the SSULI = 30\u00ba x 2.4\u00ba"]
-[6.598099231719971, 8.148696899414062, "[TT] Channels of the SOLCON = 2"]
-[10.832045555114746, 5.971935272216797, "[TT] Main Detector of the GRS = 12 cm diameter x 7.6 cm long CsI (Tl) crystal"]
-[10.783082962036133, -0.209832563996315, "[FF] Formation Flying Concept Presentation Date of the TanDEM-X = Jan. 23-27, 2005"]
-[3.120464324951172, 2.146580934524536, "[FF] Coverage of the Copernicus Sentinel-5P = Global"]
-[5.011418342590332, 3.2049973011016846, "[TT] Manufacturer of the Planet SkySats = Maxar Technologies"]
-[6.208723545074463, 2.424028158187866, "[TT] Type of the eCOS = Open-source"]
-[6.896076679229736, 4.059938430786133, "[FF] Unknown of the Ecliptic Enterprises = Unknown"]
-[6.316732406616211, -0.16975881159305573, "[TT] Observation Duration of the DAICHI-2 = More than 11 years"]
-[1.9305222034454346, -0.40577253699302673, "[FF] Whistler Waves Amplitudes of the Van Allen Probes = Unusually large"]
-[10.917987823486328, 7.546420574188232, "[TT] Swath width of the VIRR = 2800 km"]
-[1.6183743476867676, 3.7623229026794434, "[TT] Sun sensors of the BEESAT-2 = Yes"]
-[11.050127029418945, 4.7579874992370605, "[FF] Energy Conversion of the Electrodynamic Tether (Power or Drag System) = Converts the orbital energy of the host S/C into electrical power"]
-[6.854321002960205, -0.3677794337272644, "[TT] Orbit Drift of the \u00d8rsted satellite = Approximately 0.91 minutes in local time each day"]
-[6.497875690460205, 8.209957122802734, "[TT] SWIR Channels of the PROBA-V = 3"]
-[9.686868667602539, 5.33775520324707, "[TT] Protection of the Flywheel Housing = Capton tape"]
-[6.705554485321045, -0.5730715990066528, "[TT] Repeat Cycle of the SARAL spacecraft = 35 days"]
-[11.124310493469238, 0.6057543754577637, "[TT] Properties Observed of the Transiting Exoplanets = Mass, radius, orbit"]
-[5.628050804138184, 4.198939323425293, "[TT] Number of Tests of the EDRS-C terminal = More than 90"]
-[5.591021537780762, 1.1596254110336304, "[FF] Joining Date of the Hisaki Satellite = 4 August 2021"]
-[14.01773452758789, 6.3755269050598145, "[FF] Manufacturer of the NanoPower Modules = GomSpace"]
-[6.375034332275391, 3.6983962059020996, "[TT] Instrument Provider of the SPARCS = NASA's Jet Propulsion Laboratory"]
-[5.165579795837402, 0.18355493247509003, "[TT] Launch Date of the Ikonos-2 = 24 Sep 1999"]
-[5.233572483062744, 2.3589260578155518, "[TT] Mission Type of the IMAGE = EO"]
-[8.202144622802734, 6.554598808288574, "[FF] Image Capture of the EPIC = Figure 81"]
-[9.093179702758789, -1.1939603090286255, "[FF] Geostationary Position of the EDRS-C = Nearly 36,000 km above Earth"]
-[11.81855297088623, 0.06979012489318848, "[FF] Purpose of the TESS = Look for planets in orbit around nearby bright stars using the transit method"]
-[8.692246437072754, 5.855860710144043, "[TT] Accuracy Specification of the ASM = 300 pT (2\u03c3)"]
-[6.14026403427124, 6.144525527954102, "[FF] Operating Modes of the DCS = Random access to collect messages transmitted at fixed times (self-timed DCP) or in emergency (alert DCP), Message acquisition only after interrogation of the DCP"]
-[6.002211570739746, 1.9976744651794434, "[FF] Program URL of the DRACO = [DRACO Program URL](https://www.darpa.mil/program/demonstration-rocket-for-agile-cislunar-operations)"]
-[5.6915388107299805, 2.029435396194458, "[FF] Mission Status of the PACE = Construction and testing phase"]
-[7.381763935089111, 3.7733266353607178, "[FF] Unknown of the GOE (GPS Occultation Experiment) = Unknown"]
-[7.184592247009277, 9.032608032226562, "[FF] Broadband Blocking Filter of the GLM instrument = Placed on the front surface of the filter substrate"]
-[6.0993876457214355, 4.102633476257324, "[FF] Components of the JUICE Science Ground Segment (SGS) = Science Operation Center (SOC) and the PI instrument teams"]
-[10.964065551757812, 7.4079132080078125, "[TT] Swath width (550 km orbital altitude) of the DST 35 = 12-18 km with 8-12 kpixel"]
-[5.805559158325195, 4.5375590324401855, "[FF] Design Purpose of the SKOUT = To connect government and commercial relay satellite constellations as well as direct-to-ground communications networks"]
-[8.967293739318848, 4.532161712646484, "[TT] Array Pointing Requirement of the IXPE Mission = Within \u00b125 degrees of sun normal"]
-[3.6996726989746094, 3.8835501670837402, "[TT] Data Acquisition Date of the RISAT-1 MRS = Dec. 31, 2014"]
-[13.62315559387207, 5.900280475616455, "[TT] Orbit Average Power of the Solar Panels = 3 W"]
-[8.009540557861328, 0.5391274690628052, "[FF] Wetness Percentile of the GRACE-FO = Varies"]
-[3.9869699478149414, 6.934159755706787, "[TT] Polarization of the S-band Rx/Tx patch antennas = Same"]
-[9.291888236999512, 3.2095935344696045, "[TT] Data Recording of the Corona Satellites = Conventional film"]
-[6.380937099456787, 1.5035229921340942, "[FF] Presentation Date of the MICROSCOPE = Oct. 2-6, 2006"]
-[11.958434104919434, 4.98204231262207, "[TT] Size of the LEID = 330 mm x 150 mm x 130 mm"]
-[8.956079483032227, 7.659226894378662, "[TT] MTF of the Imager = \u22650.18(PAN), \u22650.2(MS)"]
-[11.882326126098633, 4.768397808074951, "[TT] Dimensions of the GNB = 20 cm side length"]
-[4.858222961425781, 7.432764530181885, "[TT] Uplink Data Rate of the RF communications = 4 kbit/s"]
-[11.000835418701172, 7.581871032714844, "[TT] Swath Width of the MSI = 290 km"]
-[8.28522777557373, 7.574104309082031, "[TT] Detector Technology of the SIS (Scanning Imaging Spectrograph) = Position-sensitive anode"]
-[13.414812088012695, 6.891053199768066, "[TT] Power of the ADEOS = 4.5 kW"]
-[9.494515419006348, 3.594893455505371, "[FF] Intensity of the Earth's main magnetic field = Not the same in the north as in the south"]
-[7.402154922485352, 3.63472843170166, "[TT] GPS Occultations of the GNOS Instrument = More than 500 per day"]
-[6.127370357513428, 7.280059337615967, "[TT] Data Rate of the Spectrometer = 453.7 kbit/s"]
-[5.904565334320068, 0.7961150407791138, "[TT] Image Capture Date of the BepiColombo = 10 April"]
-[4.232338905334473, 0.7184345722198486, "[TT] Launch Date of the EDRS-C = Days away from July 26, 2019"]
-[4.3337883949279785, 1.2453234195709229, "[TT] Launch Time of the SEOSAT-Ingenio = 02:52 CET / 22:52 local time on 16 November"]
-[4.985856056213379, 0.6036384105682373, "[TT] Failure Date of the NEOSSat = Late 2016"]
-[8.112128257751465, 0.846505343914032, "[FF] Mission Unique Feature of the EQUULEUS = Measure the LIF at the far side of the moon from EML2 and control trajectory within the Sun-Earth-Moon region"]
-[8.504792213439941, 7.460931777954102, "[FF] Detectors of the Pushbroom imager = Silicon area array with 7000 pixels Pan, 1750 pixels in each MS band"]
-[4.832409858703613, 0.5684608817100525, "[TT] Launch Date of the Pathfinder 2 = 2016"]
-[13.490486145019531, 2.807967185974121, "[TT] Mass of the Spacecraft = 494 kg (dry mass), 636 kg (wet mass)"]
-[3.0944197177886963, 4.424103260040283, "[FF] Data Used of the DInSAR = TOPS (Terrain Observation with Progressive Scan)"]
-[5.391926288604736, 8.79488754272461, "[TT] Bandwidth of the Band 4 = 0.298 \u00b5m (16 cm -1)"]
-[5.049452304840088, 3.117926836013794, "[FF] Manufacturer of the NRO Taps Boeing for Next Batch of Cubesats = Boeing"]
-[4.838572025299072, 7.446752071380615, "[TT] Bandwidth of the RF Ground Network = 500 kbit/s"]
-[13.589218139648438, 7.531831741333008, "[TT] Power supply of the Antenna = AC 90 V~120 V 50/60 Hz"]
-[10.424836158752441, 2.2207846641540527, "[TT] Telescope Type of the Swift = High-resolution X-ray"]
-[4.417381286621094, 2.9915523529052734, "[FF] Location of the WCDAS = Wallops, VA"]
-[4.906247615814209, 3.404074192047119, "[TT] Provider of the SAS = CREST (Canada)"]
-[5.003729820251465, 0.4952278137207031, "[TT] Commercial Service Start Date of the SES-17 = July 22, 2022"]
-[9.284255027770996, 7.154041290283203, "[TT] Viewing Range of the TWINS = \u00b190\u00ba"]
-[6.238969802856445, 1.0124086141586304, "[FF] Image Capture Date of the Landsat-8 = May 30, 2021"]
-[10.267709732055664, 5.649438858032227, "[FF] Temperature of the Tank B1 = Daily average"]
-[4.990598201751709, 0.6669344305992126, "[TT] Launch Date of the ETS-VIII = Dec. 18, 2006"]
-[10.602266311645508, 3.3685290813446045, "[TT] Payload Space of the ITASat CubeSat = 2U"]
-[5.543521404266357, 6.261721134185791, "[TT] Number of MS Scenes of the Memory = 31"]
-[11.900930404663086, 5.273550033569336, "[TT] Volume of the Instrument = 0.8 m x 0.5 m x 0.25 m"]
-[5.919705390930176, 4.694250583648682, "[FF] Requirements of the KE Ground Station = Enable the user to easily choose a target of interest (point-and-click) and receive the satellite image during the same satellite access time (pass)"]
-[4.696102142333984, -1.1149369478225708, "[FF] Docking Date of the Tianzhou-3 = 20 September 2021"]
-[8.235749244689941, 2.3874731063842773, "[TT] Number of Probe Conjunctions of the THEMIS Constellation = 154 hours"]
-[4.883426666259766, 7.811037063598633, "[FF] Capability of the GATE = Receive the Galileo bands E6, E5a,b and L1 in full bandwidth"]
-[10.928473472595215, 5.170267105102539, "[TT] W/L Ratio of the CuPID = 1/50"]
-[8.100207328796387, 5.16055965423584, "[FF] Calibration Aim of the SODISM = Provide long term sensitivity calibration"]
-[8.521839141845703, 5.7570905685424805, "[TT] Positional Accuracy of the LRA = Within 3 cm"]
-[5.973299026489258, 8.627605438232422, "[TT] MTF (Modulation Transfer Function) of the Channel = > 0.21"]
-[6.441470623016357, -1.3148478269577026, "[FF] Management of the GRACE = JPL"]
-[5.19688081741333, 6.353330135345459, "[TT] Data Rates of the SpaceWire bus = 10-100 Mbit/s"]
-[13.130463600158691, 7.22329044342041, "[TT] Design of the MTVZA-GY = Total-power"]
-[7.0087809562683105, 6.794342041015625, "[TT] TFSC Data of the AlSat Nano = Regularly returned"]
-[6.136773109436035, 0.5488899350166321, "[TT] Lunar Orbit Entry Date of the LRO = June 23, 2009"]
-[8.701889038085938, 9.022552490234375, "[TT] Sensitivity of the NIRSpec MIRI = 10.4 nJy (2.0 \u03bcm, \u03c4 i =10,000 s, and \u03bb/\u0394\u03bb = 4)"]
-[13.524152755737305, 5.726836681365967, "[FF] Thermal Load of the Solar Panels = Non-trivial"]
-[7.716253280639648, 6.786965847015381, "[TT] Sampling duration of the Imager = 4 s"]
-[10.394795417785645, 4.027968883514404, "[TT] Type of the Deployable Boom = Coiled CPFR mono-stable boom"]
-[8.524528503417969, 8.18824291229248, "[TT] Spectral Resolution of the GIIRS = 0.8 to 1.6 cm -1"]
-[9.49539566040039, 7.356910228729248, "[TT] Spatial Resolution of the IRFS-2 = About 30 km"]
-[9.78648567199707, 7.106409549713135, "[TT] Along-Track Resolution of the OMI = 13 km x 48 km to 13 km x 12 km"]
-[10.587387084960938, 3.935868263244629, "[FF] Dragsail of the RemoveDEBRIS = Unknown"]
-[7.905889511108398, 4.283954620361328, "[FF] Description of the Part B1 = Sun-aligned stationkeeping is performed while the perigee is in eclipse and the VBS is used in cooperative mode"]
-[4.528658390045166, 2.8208351135253906, "[FF] Locations and Operators of the Sentinel-1 PDGS centers = KSAT for X-band reception (CGS) in Svalbard (Norway) and Alaska, INTA for X-band reception in Maspalomas (Spain), E-Geos for X-band reception in Matera (Italy), Astrium Services for the PAC (Processing and Archiving Center) in Farnborough (UK), DLR for the PAC in Oberpfaffenhofen (Germany), CLS for the MPC (Mission Performance Center) operations in Brest (France), PDMC (Payload Data Management Center) will be located at ESRIN and be operated by the European Space Agency, The POD (Precise Orbit Determination) service will be provided by GMV (Spain)"]
-[9.051241874694824, 5.695725440979004, "[TT] Boresight Pointing Accuracy (Elevation) of the SXI = Within 3 arcmin"]
-[5.677422523498535, 4.915660858154297, "[TT] Function of the MEXIC = Make in-flight modifications to the MEXIC software"]
-[6.26038122177124, 4.26608419418335, "[FF] Product Processing of the ADEOS-II = Processes AMSR and GLI 1km products on a semi-real-time basis"]
-[6.130369186401367, 2.2154712677001953, "[FF] Leadership of the Euclid Consortium = Euclid Consortium Lead (ECL) and a Euclid Consortium Board (ECB)"]
-[7.951589584350586, 6.2689337730407715, "[TT] Purpose of the SHIROP = Photographing"]
-[13.555998802185059, 6.840096473693848, "[TT] Power of the Satellite Bus = Approximately 1.9 kW"]
-[5.827410697937012, 0.9556292295455933, "[TT] Image Capture Time of the GOES-17 = Around noon on August 20, 2020"]
-[8.110421180725098, -0.6681756377220154, "[FF] Measurement Purpose of the CryoSat-2 = Collect measurements for scientific research"]
-[9.083401679992676, 6.917269229888916, "[TT] Horizontal Error 90% (HE90) of the WorldView-3 = 3.7 m"]
-[7.665098667144775, 0.4972260296344757, "[TT] Development Company of the Lunar IceCube = Morehead State University, Kentucky"]
-[10.400552749633789, 5.936588287353516, "[TT] Brigthness Temperature (BT) Sensitivity of the Antenna = \u00b10.26 K"]
-[10.715803146362305, 7.061804294586182, "[TT] Footprint of the TMR = 35 km"]
-[5.240141868591309, 5.236487865447998, "[TT] Power Supply of the Namuru V3.2 GPS Receiver = Latch up detection on the power supply"]
-[6.819034576416016, 8.41557502746582, "[TT] Total Channels of the Spectral Bands = 433"]
-[6.3972649574279785, 1.952515959739685, "[FF] URL of the Aalto-1 = http://blogs.aalto.fi/satellite/"]
-[13.551926612854004, 5.847777843475342, "[TT] Solar Array Power of the Power Subsystem = 35 W"]
-[10.812265396118164, 1.356797695159912, "[FF] Mass of the SS 433 = Millions to billions of times the mass of the Sun"]
-[14.142190933227539, 3.035377025604248, "[TT] Mass of the HAUSat-2 = \u2264 25 kg"]
-[5.115304946899414, 7.274500370025635, "[TT] Data Rate of the Reception Station = 16 Mbit/s"]
-[6.369528293609619, 1.0493770837783813, "[TT] Image Acquisition Year of the Landsat 8 = 2020"]
-[3.820251226425171, 4.605624675750732, "[TT] Collision Avoidance Maneuvers of the RADARSAT-2 = 1"]
-[4.399571895599365, 7.812612056732178, "[TT] Uplink Frequency of the RF Communications = 144 MHz"]
-[10.447778701782227, 5.778954982757568, "[TT] Temperature of the Operating temperature = -20 to + 50\u00baC"]
-[6.907325267791748, 6.992588043212891, "[TT] Interchangeable of the Laser Diodes = Yes"]
-[10.889654159545898, 7.477568626403809, "[TT] 25 km (rg) x 25 km (az) of the Swath = -"]
-[8.381508827209473, 1.5032960176467896, "[TT] Humidity Accuracy of the Lower atmosphere = Specific humidity 1.5 grams/kg or \u00b1 20 percent over clear sky or ocean"]
-[4.381560325622559, 7.4245686531066895, "[TT] Transmitter Modulation Bandwidth of the S-band transponder = 3 MHz"]
-[11.785229682922363, 6.665566444396973, "[FF] Energy Range of the Satellite = Above 10 keV"]
-[10.776287078857422, -1.112972378730774, "[FF] Collision Avoidance of the SLATS = ISS Orbit"]
-[6.040369510650635, 5.100688934326172, "[FF] Interface Requirements of the LCT = Electrical, mechanical, data bus"]
-[3.0751168727874756, 3.9155170917510986, "[TT] Launch Target of the NISAR = 2022"]
-[4.406680107116699, 7.8732733726501465, "[TT] Uplink Frequency of the DRT = 402.75 MHz"]
-[5.5011305809021, 2.6891188621520996, "[TT] Number of Graduate Students of the MinXSS = 11"]
-[9.516282081604004, 4.476315498352051, "[FF] Spin Axis Measurement of the LAGEOS = Unknown"]
-[8.51548957824707, 6.117696762084961, "[TT] Data Acquisition Duration of the CERES on TRMM = 9 months"]
-[9.4060697555542, 6.95516300201416, "[TT] Image Resolution of the ALOS/ Daichi = 30 m mesh (1 arcsec)"]
-[9.63577938079834, -0.45231348276138306, "[TT] Altitude of the SPOT-1, -2 and -3 = 832 km"]
-[12.424981117248535, 0.626545250415802, "[FF] Components of the PLATO Payload = Cameras made of telescopes, their focal planes, all related electronics and the on-board DPS (Data Processing System)"]
-[5.168352127075195, 0.6694467663764954, "[TT] Acquisition Completion Date of the ICON = 6 June 2018"]
-[10.943201065063477, 4.727915287017822, "[FF] Tether Angle Sensor of the ATEx = Triggered the jettison mechanism"]
-[3.6524486541748047, 6.349380970001221, "[TT] Antenna Composition of the SAOCOM-1A = 140 smaller antennas"]
-[4.314909934997559, 4.266513347625732, "[TT] Satellite Types of the COSPAS-SARSAT = LEOSAR, GEOSAR, MEOSAR"]
-[10.969583511352539, 5.690046787261963, "[TT] Material of the Heat Shield = Avcoat ablator"]
-[6.932795524597168, 6.085184097290039, "[FF] Number of Instruments of the ISEE-1 = Unknown"]
-[4.86216402053833, 7.216310501098633, "[TT] Data Rate of the Ka-band ISL = Approximately 300 Mbit/s"]
-[11.088398933410645, 5.808879852294922, "[TT] Material of the Baffles = Same material as the heatshield first layer"]
-[12.134902000427246, 6.083238124847412, "[TT] Cosmic Ray Events of the AMS-02 = More than 90 billion"]
-[5.722504615783691, -0.8975037336349487, "[TT] Design Life of the VEN\u00b5S = 4 and a half years"]
-[12.404510498046875, 0.6038098931312561, "[TT] Optical Bench Location of the PLATO Spacecraft = Second Sun-Earth Lagrange point (L2), 1.5 million km from Earth"]
-[5.500744819641113, 5.307796478271484, "[FF] Purpose of the DRSE = Provide a distribution of dosimeters in key spacecraft locations during the STRV-1d mission"]
-[3.063890218734741, 2.3117661476135254, "[TT] Spatial Resolution of the Sentinel-2 = 10, 20 or 60 m"]
-[7.315850257873535, 6.546815872192383, "[TT] Planning Window Length of the RASP = 60 minutes"]
-[8.482377052307129, 3.2075181007385254, "[TT] Range of the Ozone Measurement Instrument = 50-650 Dobson Units (DU)"]
-[10.586095809936523, 6.509780406951904, "[FF] Mirror Quantity of the eROSITA = 54 nested gold-coated mirrors each"]
-[4.437962055206299, 0.3834793269634247, "[FF] Presentation Date of the MERLIN = Oct. 3-7, 2011"]
-[1.7667293548583984, 6.1590471267700195, "[TT] Dark Matter Particle Mass of the AMS-02 = 80 GeV/c2"]
-[5.710581302642822, 4.518558979034424, "[TT] Type of the Satellite Control Software (SCSW) = Onboard software"]
-[11.661181449890137, 4.348742485046387, "[TT] Payload Fairing Diameter of the Atlas 5 = Five-meter"]
-[14.251688957214355, 3.2065958976745605, "[TT] Mass of the ETRSS-1 = 70 kg"]
-[4.546546459197998, 0.018676195293664932, "[TT] Reentry Date of the Starshine-1 = Feb. 19, 2000"]
-[10.779670715332031, 2.1124989986419678, "[FF] URL of the XMM-Newton = http://sci.esa.int/xmm-newton/60950-from-gamma-rays-to-x-rays-new-method-pinpoints-previously-unnoticed-pulsar-emission/"]
-[13.250322341918945, 2.9224789142608643, "[TT] Mass of the E1P-2 CubeSat = \u2264 1 kg"]
-[6.607276916503906, 5.338623523712158, "[FF] Quantity of the DCS = 1"]
-[8.826166152954102, 7.155446529388428, "[TT] Provides of the PMT = Visible Imagery (0.5 - 0.85 \u00b5m) at night"]
-[5.4528279304504395, 7.283421039581299, "[TT] Maximum Data Rate of the Channel = 1674 Mbit/s"]
-[10.91802978515625, 3.7307095527648926, "[TT] Target Asteroid Size of the NEA Scout = Less than 100 meters (330 feet) across"]
-[5.912583827972412, 1.5165824890136719, "[FF] Date of the Space Tethers and Small Satellites = Unknown"]
-[13.601349830627441, 7.077215194702148, "[TT] Power Supply of the XGRE = Same power supply for four LEDs"]
-[4.800171375274658, 0.5965251922607422, "[TT] Launch Date of the Resurs-P1 = June 2013"]
-[6.279355049133301, 5.200521469116211, "[FF] Layout of the DHS = Not Applicable"]
-[3.0609540939331055, 1.9186828136444092, "[TT] Data Stream of the Copernicus Sentinel-6 = Slated for distribution later this year or early next year"]
-[7.607331275939941, 8.466891288757324, "[TT] Number of Bands of the OHIS = 80"]
-[7.438739776611328, 2.9355132579803467, "[FF] Purpose of the RRM3 = Pioneer techniques for storing and replenishing cryogenic spacecraft fuel"]
-[9.739058494567871, -0.6521103382110596, "[TT] Orbit Altitude of the HY-2C = 957 km"]
-[6.807419300079346, 5.3168134689331055, "[TT] Quantity of the INSAT-3A of ISRO = 1"]
-[13.95598316192627, 7.188586711883545, "[TT] Voltage of the Voltage 2 = -5.5\u00b15%"]
-[14.254290580749512, 3.4126899242401123, "[TT] Proof Mass Mass of the GFO Accelerometer = 72 gram"]
-[5.938549041748047, 3.0271477699279785, "[TT] Mission Count of the X-37B space plane = 4"]
-[3.950448513031006, 3.460489511489868, "[FF] Program Start of the Galileo = Latter part of the 1990s"]
-[11.396614074707031, 4.320537090301514, "[TT] Size of the ZACube-2 = 3U"]
-[7.487705230712891, 2.463188886642456, "[FF] Mission Targets of the CIRC = Wildfires, volcanoes, heat island phenomena"]
-[10.578850746154785, 5.0030012130737305, "[TT] Decontamination Power of the Langmuir Probe = 6 W"]
-[5.589834690093994, 1.6525614261627197, "[TT] Orbit Direction of the ALOS-2 = Ascending"]
-[8.541885375976562, 4.728840351104736, "[FF] Purpose of the Camera = Star brightness measurements, fine guidance sensors, spectral band measurements"]
-[11.888676643371582, 0.004869455471634865, "[TT] Number of Science Images Captured of the TESS = 15,347"]
-[6.055409908294678, -0.5148330330848694, "[TT] Mission Life of the GOLD = 15 years"]
-[7.093489170074463, 7.25103759765625, "[TT] Laser Pulses of the MABEL = ~1.5 ns"]
-[8.757027626037598, 7.269643306732178, "[TT] Position of the SiPMs = Mounted to the large face of the detector"]
-[3.9890780448913574, 2.1629040241241455, "[TT] Launch Vehicle of the AeroCube-4 = Atlas-5-411"]
-[6.614754676818848, 2.963740348815918, "[FF] Application Fields of the HJ-1 minisatellite constellation = Environmental monitoring and prediction, solid waste monitoring, disaster monitoring and prediction (flood, drought, typhoon and wind damage, sand storm, earthquake, landcreep, frost and grassland fires, coal fires, crop pest monitoring, ocean disaster monitoring)"]
-[7.8771586418151855, 4.966085433959961, "[FF] Post-Launch Testing Status of the ABI = Undergoing testing, validation and calibration"]
-[5.262414455413818, 5.096776485443115, "[TT] Comments of the L1-C/A = Compatibility and interoperability with existing and future modernized GPS signals L1C"]
-[4.800169467926025, 3.526867389678955, "[TT] Ground Station Provider of the NuSTAR = ASI"]
-[12.522201538085938, 3.2022557258605957, "[TT] Mass of the Propulsion = 1.1 kg"]
-[8.012212753295898, 6.037871837615967, "[FF] Components of the VIS/UV Czerny-Turner imaging spectrometer = Photodiode array, visible light cameras, calibration lamp, optics and baffling"]
-[7.935616970062256, 9.147563934326172, "[TT] Wavelength of the LCT = 1.064 \u00b5m"]
-[3.575460195541382, -0.8301406502723694, "[TT] Orbit Type of the PhoneSat-2.5 1U CubeSat = Near-circular orbit"]
-[7.2687482833862305, 5.306698322296143, "[FF] Components of the DLP System = Probe biasing circuit, analog measurement circuit, controlling electronics"]
-[6.14074182510376, 6.951916217803955, "[TT] User Data Rates of the Optical Downlink = 39 \u2013 620 Mbit/s"]
-[7.745689392089844, 6.486601829528809, "[FF] Test Image Time of the WFC = Almost 12 hours before the boom deployment"]
-[7.411303997039795, 1.2022600173950195, "[FF] Development Prize Date of the Global Change Observation Mission 1st \u2013 Water \u201cSHIZUKU\u201d = October 17, 2013"]
-[4.173644065856934, 7.053340435028076, "[TT] Downlink Capability of the Matera station = X-band"]
-[7.331837177276611, 1.0196073055267334, "[FF] Launch Date of the Seasat = July 1978"]
-[10.654023170471191, -0.13816815614700317, "[FF] Mission Goal of the Tandem-L = Set new standards in Earth observation"]
-[9.76535415649414, 6.720038414001465, "[TT] Detection Area Size of the Debris Sensor = 8 cm x 8 cm"]
-[3.6603541374206543, 2.831597328186035, "[FF] Atomic Clocks of the Indian Regional Navigation Satellite System (IRNSS) = Failed"]
-[7.586615562438965, 4.410269737243652, "[TT] Demonstration Requirement of the RVX = Non-cooperative forced motion maneuvers in closed-loop GNC, including hold, approach, retreat, and target inspection maneuvers"]
-[8.399223327636719, 4.679366111755371, "[FF] Function of the Calibration and Shutter Mechanism = Integrates a large spectralon sunlight diffuser"]
-[6.542771816253662, 4.871639728546143, "[FF] Backup of the MWI = Redundant systems"]
-[4.590325832366943, 1.5381648540496826, "[TT] Contract Award Date of the GOSAT-2 = May 20, 2014"]
-[4.965471267700195, 3.374411106109619, "[TT] Manufacturer of the RSA = ATK Space Systems, San Diego, CA"]
-[12.08754825592041, 4.539608955383301, "[TT] Structure Dimensions (Stowed) of the FY-3 series spacecraft = 4.4 m x 2.0 m x 2.0 m"]
-[5.123348712921143, 5.1924896240234375, "[TT] Tracking of the TRSR = Dual-frequency code and cross-correlation, data output of up to eight GPS satellites simultaneously"]
-[5.810888767242432, -2.2141849994659424, "[TT] Orbit velocity of the KOMPSAT-3 = 7.51 km/second"]
-[8.732475280761719, 3.8617231845855713, "[FF] Objective of the ESA = Measure electrons and ions with high time resolution"]
-[7.10051155090332, 4.932989597320557, "[FF] Configuration of the AOCS = Presented in Table 2"]
-[7.97054386138916, 8.598310470581055, "[TT] Spectral Range of the SphinX = 1-12 \u00c5"]
-[5.101294994354248, 8.283882141113281, "[TT] Launch Year of the 118 GHz Radiometer = 2019"]
-[7.653234004974365, -0.8838099241256714, "[TT] Launch Date of the ICESat-2 = 15 September 2018"]
-[6.096724033355713, 4.222078323364258, "[FF] Objective of the CIL = Enable multi-sensor cooperation"]
-[8.646278381347656, 0.1544884890317917, "[TT] Size of the Comet Leonard = About a kilometer across"]
-[6.4705610275268555, -0.7285022735595703, "[TT] LTAN of the FY-3D = 14:00 hours"]
-[8.491817474365234, 1.9082345962524414, "[TT] Commandable PRI Range of the RapidScat = 5-6 ms"]
-[6.703586101531982, 6.108778476715088, "[FF] Laser Transmitter of the Aeolus satellite = World's first"]
-[8.399256706237793, 2.6769156455993652, "[TT] Air Quality Prediction Accuracy Improvement of the TEMPO = 50 percent"]
-[9.703804016113281, 0.1471773087978363, "[FF] Location of the Drogue Parachute = On the centerline of the backshell"]
-[12.429398536682129, 2.9469847679138184, "[TT] Hydrazine Mass of the Satellite = 80 kg"]
-[8.174448013305664, 2.703261137008667, "[TT] Measurement Domain of the Meteor-1/Meteor-2/Meteor-Priroda Series = Atmosphere, Snow & Ice"]
-[9.240768432617188, 7.130935192108154, "[TT] Image Resolution of the Solar Orbiter = 9148 x 9112 pixels"]
-[7.495306015014648, 2.8899648189544678, "[FF] Purpose of the Methane Satellite = Track methane emissions"]
-[6.388119220733643, -0.3344152569770813, "[TT] Orbit Prediction and Pass Planning of the ASTERIA = TLE (Two-Line Element) sets from the JSpOC (Joint Space Operations Command)"]
-[5.00304651260376, 0.5110951662063599, "[TT] Launch Date of the Enxaneta = March 22, 2021"]
-[6.387355804443359, -0.7386934757232666, "[TT] LTDN of the SkySat-16 to -18 = 10:30 hours"]
-[5.232229232788086, 1.1876777410507202, "[FF] Schedule of the NPOESS = Further delays"]
-[8.22195816040039, 1.287984848022461, "[FF] Mission Status of the RaInCube = Unknown"]
-[13.934188842773438, 3.0549182891845703, "[TT] Mass of the CE-SAT-1 = 50 kg"]
-[11.405757904052734, 4.327301502227783, "[TT] Size of the Dove-4 = 3U"]
-[5.905539035797119, -0.6628637909889221, "[TT] Operational Lifetime Requirement of the SST = 7.5 years"]
-[12.812255859375, 7.612774848937988, "[TT] Instrument Power of the SEVIRI = 123 W"]
-[8.96847152709961, 4.214444637298584, "[FF] Presentation Date of the Micro Digital Sun Sensor = Aug 25-27, 2004"]
-[10.282966613769531, 4.546627044677734, "[TT] Maximum Torque of the Reaction Wheels = 5 mNm"]
-[6.9675984382629395, 4.268357276916504, "[FF] Unknown of the CFOSat = Unknown"]
-[5.477086067199707, 0.7826301455497742, "[FF] Arrival Date of the ECOSTRESS = 17 April 2018"]
-[13.405607223510742, 3.1149940490722656, "[TT] Instrument Support Capacity of the Bus = Up to 206 kg"]
-[8.081487655639648, -0.37491676211357117, "[TT] Polar Ice Decline of the Sea Ice = Since the start of the satellite record in the 1970s"]
-[11.586986541748047, 3.553048849105835, "[TT] Engine Firing Duration of the ExoMars TGO = 52 minutes"]
-[9.282440185546875, 7.238162994384766, "[TT] Pixel Footprint Resolution of the GLI = 8-14 km"]
-[5.092892646789551, 0.9145830869674683, "[TT] Termination Date of the NPOESS = Feb. 2010"]
-[3.36905574798584, 6.446294784545898, "[TT] Diameter (mm) of the Antenna = 760"]
-[11.378077507019043, 5.8469624519348145, "[TT] Material of the Separation Panel = Machined aluminum"]
-[4.011761665344238, 6.363717079162598, "[FF] Antenna Type of the RF communications = Omnidirectional antenna system for both up and down links and additional global horn for downlink"]
-[5.1319050788879395, 6.990588665008545, "[TT] Symbol rate (s/s) of the Service downlink = 4207"]
-[9.536028861999512, 6.122574329376221, "[TT] Tilt Angle of the MSU-100 = \u00b114\u00ba"]
-[5.279709339141846, 5.606485366821289, "[FF] Standard of the TM Synchronization and Channel Coding = CCSDS 131.0-B-2"]
-[8.486917495727539, 7.130295276641846, "[FF] Modulation Transfer Function of the UK-DMC-2 = Improved compared to the first generation 32 m DMC imagers"]
-[10.82705307006836, 7.464356899261475, "[TT] Swath of the ALSAT-2B = 17.5 km"]
-[8.114816665649414, 8.533300399780273, "[TT] Absolute Pointing Uncertainty of the Spectral Block = \u00b10.25\u00ba"]
-[8.61160945892334, 3.6422131061553955, "[FF] Measurement of the ILAS-II = Components of solar light absorbed"]
-[7.657801151275635, 8.755120277404785, "[TT] Channel Spectral Widths of the IIR = 0.9 \u00b5m, 0.6 \u00b5m, 1.0 \u00b5m"]
-[10.080805778503418, 8.112882614135742, "[TT] Focal Length of the Geoton-L1 imager = 400 cm"]
-[4.803037643432617, -1.8047666549682617, "[FF] Relay Hazard Avoidance Method of the Chang'e-3 lander = Large-scale rough-hazard avoidance, three-dimensional imaging in hovering status, small-scale precise-hazard avoidance of the final landing site"]
-[5.5089850425720215, 0.8982356190681458, "[FF] Launch Date of the Space Technology 5 = Unknown"]
-[14.089550018310547, 3.244150400161743, "[TT] Total Mass of the Aquajet = ~0.5 kg"]
-[13.352328300476074, 7.407530307769775, "[TT] Predicted Power Levels of the IXV = 700 W"]
-[10.222833633422852, 4.482166767120361, "[FF] Actuation of the OceanSat-2 = Four reaction wheels in a tetrahedral configuration, two magnetic torquer coils and monopropellant hydrazine thrusters"]
-[4.277774333953857, 0.8555182814598083, "[FF] Timeliness of the EDRS = Improved"]
-[3.605430841445923, 4.618412494659424, "[FF] Interface of the SAR-VTB = LUT-to-MCC and nodal-MCC -to-RLSP"]
-[7.56467342376709, 8.340531349182129, "[FF] Spectral Ranges of the GOSAT-2 = Forward viewing (+20\u00ba) b1: 333-353 nm, b2: 433-453 nm, b3: 664-684 nm, b4: 859-879 nm, b5: 1585-1675 nm"]
-[6.7182393074035645, 7.565041542053223, "[TT] Beam width of the S-band = 0.64 rad"]
-[9.427236557006836, 5.165665149688721, "[FF] Thrust Level of the Satellite = Varying"]
-[4.1942596435546875, 2.3854358196258545, "[TT] Implementation of the LIRIS Demonstrator = ATV-5 George Lema\u00eetre"]
-[16.542173385620117, 3.641890287399292, "[TT] Initial Size of the OneWeb = 650"]
-[7.969580173492432, 5.752446174621582, "[FF] Method of the Lateral System = Center-of-mass"]
-[5.506611347198486, 7.1517510414123535, "[TT] Data Rate of the GEO LCT = 2.8 Gbit/s (1.8 Gbit/s user data)"]
-[7.305455207824707, 9.070189476013184, "[TT] Tuning Positions Separation of the Lyot-Michelson Filter System = 69 m\u00c5"]
-[5.69472599029541, 4.288451194763184, "[FF] Service of the Sateliot = Roaming services for sensors and devices on trucks, precision agriculture equipment, clean energy infrastructure and other sectors"]
-[5.236419200897217, 8.130110740661621, "[TT] Input Matching of the Array Radiator = Better than -18 dB in the full 300 MHz bandwidth"]
-[5.27889347076416, 1.0823392868041992, "[FF] Meeting Date of the COMS = Dec. 2-13, 2008"]
-[11.26651382446289, 0.9672691226005554, "[FF] URL of the LISA Pathfinder = http://www.esa.int/spaceinimages/Images/2015"]
-[4.832422256469727, 1.8662787675857544, "[FF] Development Status of the G\u00f6kt\u00fcrk-1 = Stuck in a production facility in France"]
-[10.091909408569336, -1.4296295642852783, "[TT] Inclination of the RADARSAT-2 = 98.6\u00ba"]
-[8.491677284240723, 7.657615661621094, "[TT] Average Power of the 4-band CCD Imager = 6 W"]
-[4.785623073577881, 3.322711944580078, "[TT] Manufacturer of the Monitoring camera = Thales Alenia Space in Switzerland"]
-[9.020332336425781, -0.6597384214401245, "[TT] Orbit of the PROBA-3 = Highly-elliptical Earth Orbit"]
-[10.110028266906738, 1.433577060699463, "[FF] Ability of the Gaia = Detect stars up to 400,000 times fainter than those visible to the naked eye"]
-[5.288280963897705, 1.153118371963501, "[FF] System of Systems Presentation Date of the UrtheCast = October 20-24, 2014"]
-[8.001367568969727, 1.5933599472045898, "[FF] Function of the DPR = Measure precipitation"]
-[4.384345054626465, 7.804412364959717, "[TT] Uplink Frequency of the SCD-2 = 401.650 MHz and 401.620 MHz"]
-[7.751698970794678, 8.980712890625, "[TT] Transmitter Wavelength of the DIAL Instrument = 2 \u00b5m"]
-[6.6685791015625, 2.3046278953552246, "[TT] Percentage of Sky Observed in Four Exposures of the Euclid Reference Survey = 50%"]
-[6.120545864105225, 2.3840177059173584, "[FF] Cooperating Institutions and Companies of the eROSITA = Institut f\u00fcr Astronomie und Astrophysik der Universit\u00e4t T\u00fcbingen (IAAT); Astrophysikalisches Institut Potsdam (AIP); Dr.-Remeis-Sternwarte, Bamberg; Hamburger Sternwarte; Space Research Institute (IKI), Moscow; Roskosmos, Moscow; Kayser-Threde GmbH, Munich; Carl Zeiss AG, Oberkochen; MLT (Media Lario Technologies), Italy"]
-[13.841117858886719, 6.960225582122803, "[FF] Induced Voltage of the 300 V system = > 5 to 6 V"]
-[5.016347408294678, -0.34463033080101013, "[TT] Capture Time of the Canadarm2 = 10:54 UTC"]
-[11.414530754089355, 4.363588809967041, "[TT] Size of the BRIO = 3U"]
-[6.498224258422852, 1.0786561965942383, "[FF] Image of the Day Date of the NASA Earth Observatory = 11 May 2022"]
-[3.8917994499206543, 3.362581491470337, "[TT] Mission Duration of the Galileo spacecraft = 1995 and 2003"]
-[9.654793739318848, -0.39129719138145447, "[TT] Altitude of the RESURS-O1-4 = 835 km"]
-[5.8624749183654785, -0.5317010879516602, "[TT] Mission Life of the ATSR = 1 year"]
-[4.516465663909912, 1.8821475505828857, "[TT] Launch Date of the NorSat-1 = July 2017"]
-[10.255693435668945, 4.5876054763793945, "[TT] Momentum Storage of the RWAs = 75 Nms"]
-[3.8784399032592773, 1.9960745573043823, "[TT] Launch Vehicle of the Beresheet = SpaceX Falcon 9 rocket"]
-[8.571746826171875, 5.905559539794922, "[TT] Overall Accuracy of the ARI = <0.1 K 2\u03c3"]
-[13.291082382202148, 7.04108190536499, "[FF] Power Source of the HRIU = HH avionics"]
-[6.269254207611084, 8.008225440979004, "[FF] Parameter of the Channels = Value"]
-[7.669164180755615, 9.449077606201172, "[TT] Center Wavelength of the Band 8 = 11.03 \u00b5m (907 cm -1)"]
-[8.128249168395996, 3.146484375, "[FF] Data Output of the GLM = Shot noise fluctuating about zero with occasional peaks due to lightning events"]
-[5.2018890380859375, 7.001989364624023, "[TT] Data Downlink Rate of the MinXSS-2 = At least a factor of 6 increase from 1 MB per day"]
-[6.022621154785156, 4.9366984367370605, "[FF] Segments of the TET-X bus = Service Segment, Electronic Segment, Payload Segment"]
-[6.465171813964844, 1.845346450805664, "[FF] URL of the ROSE-L = https://www.d-copernicus.de/daten/satelliten/satelliten-details/news/rose-l-radar-observing-system-for-europe-l-band-sar/?tx_news_pi1%5Bcontroller%5D=News&tx_news_pi1%5Baction%5D=detail&cHash=a04a6343ad86edd934b7d33e53318699"]
-[8.855086326599121, 2.9880170822143555, "[FF] Conference Presentation of the MEIDEX = ICAE (International Conference on Atmospheric Electricity) 2003, Versailles, France, June 9-13, 2003"]
-[3.121401786804199, 2.2160208225250244, "[TT] Map Area Coverage of the Copernicus Sentinel-1 = 176 km by 170 km"]
-[4.96378755569458, 0.7066017389297485, "[TT] Clearing Date of the Aalto-1 = June 21, 2018"]
-[4.129116058349609, 7.336691379547119, "[FF] Band of the KBR = K-Band"]
-[5.645629405975342, 2.4795947074890137, "[FF] Project Management Importance of the AzTechSat = Main step for successfully completing any project"]
-[13.634387016296387, 5.829288959503174, "[TT] Power Output of the Solar Cells = 220 W"]
-[8.54370403289795, 5.936680316925049, "[TT] Precision of the OCO-2 = <0.3% (1 ppm)"]
-[4.666583061218262, 1.5307111740112305, "[TT] Operation Duration of the GHGSat-D = Over three years"]
-[4.830732822418213, 3.3673641681671143, "[TT] Provider of the SARR = CRC/Canada"]
-[3.562847137451172, -0.9345376491546631, "[TT] Orbit of the JPSS-1 = Polar"]
-[8.670987129211426, 5.877481937408447, "[TT] Targeted Localization Accuracy of the Precise Position Determination System = Less than 10 m (CE90)"]
-[6.66684103012085, 4.4623823165893555, "[FF] Unknown of the Linear Feed Array = Unknown"]
-[3.832995653152466, 6.496702194213867, "[TT] Type of the Antenna = Planar with two elements"]
-[11.322517395019531, 4.873847961425781, "[TT] Recovery Method of the Sample Return Capsule = Mid-air recovery"]
-[12.11696720123291, 2.9760212898254395, "[TT] Propellant of the Hydrazine Propulsion Subsystem = N2H4"]
-[9.079724311828613, 2.913457155227661, "[FF] Conference Date of the Genesis Solar -Wind Sample Return Mission = March 13-17, 2000"]
-[13.445215225219727, 5.469348907470703, "[TT] Number of Strings of the Solar Array = 8"]
-[11.76746654510498, 0.09841232001781464, "[FF] Follow-up Targets of the CHEOPS = Targets from the planned TESS (Transiting Exoplanet Survey Satellite) mission of NASA"]
-[11.271464347839355, 0.5446851849555969, "[FF] Definition of the Transit = Occurrence when a planet passes in front of a star"]
-[8.79054069519043, 0.3726220428943634, "[TT] Location of the Sandpiper = Bennu\u2019s southern hemisphere"]
-[7.550567626953125, 3.723240613937378, "[FF] Function of the Gear Drives = Set and lock the orientation of the NightPod axes"]
-[7.930734157562256, 0.8467534184455872, "[FF] Mission of the NEOSSat = Asteroid astronomy and Space Situational Awareness experimentation"]
-[7.099135875701904, 4.332991123199463, "[FF] Field of Regard of the GF-2 spacecraft = Not specified"]
-[6.498173236846924, 5.617597579956055, "[FF] Redundancy of the MCM = All the modules have redundancy except the optical part and the FPA"]
-[9.136481285095215, -0.3635782301425934, "[FF] Apogee Alignment of the THEMIS = Opposing"]
-[13.209772109985352, 7.2313079833984375, "[TT] Power Consumption of the FREND = 14 W"]
-[14.575096130371094, 6.616785526275635, "[TT] Type of the Lithium iron phosphate (LiFePO4) battery = Secondary power source"]
-[5.1782121658325195, 6.150774955749512, "[TT] SpaceWire Interface Channels of the SpaceCube 2 = 8"]
-[5.338177680969238, 7.665667533874512, "[TT] G/T of the Satellite = 13 dB/K"]
-[10.08279037475586, 5.32553768157959, "[FF] Design of the PFM Cooler System = Linear pulse tube cold head that is integral to the compressor assembly and a coaxial remote pulse tube cold head"]
-[5.595826625823975, 2.809157133102417, "[TT] Project Funding of the SCIAMACHY = DLR/NIVR"]
-[6.151419639587402, 4.468484878540039, "[FF] Experiment Types of the LCRD = Executing timelines that include multiple orbiting users with different data rates and service requirements"]
-[14.49893856048584, 6.654246807098389, "[TT] Battery Capacity of the Power Subsystem = 7 Ah"]
-[11.19019889831543, 5.953430652618408, "[TT] Primary Structure Material of the KOMPSAT-6 = CFRP (Carbon Fiber Reinforced Polymer)"]
-[11.492324829101562, 4.904114246368408, "[TT] Diameter of the RRA = 60 mm"]
-[13.776759147644043, 7.110803604125977, "[TT] Voltage range (V) of the PS-2 = 400~500"]
-[4.077255725860596, 4.445960521697998, "[FF] Unknown of the SARP-3 = Unknown"]
-[4.353555202484131, 6.790921211242676, "[FF] Coverage Zones of the Scientific Payload = Ka-band (20/30 GHz): one steerable spotbeam over South Germany and the H2KAR antenna (IOV) over North Germany, ISL (23/26 GHz): one ISL tracking antenna, steerable over the whole Earth and the receive GeReLEO Smart antenna (IOV), Ku-band (11/14 GHz): anchor coverage over Germany"]
-[6.966833114624023, 5.651941776275635, "[TT] Quantity of F-DPUs of the Fast Electronics Unit (FEU) = 2"]
-[6.203831672668457, 3.770798921585083, "[FF] Use Case of the Mobile Satellite Network = Maintain communications during natural disasters"]
-[8.379555702209473, 1.1429117918014526, "[FF] Affiliation of the AMSR-E = Developed by NASDA, flown on NASA's Aqua mission"]
-[12.025489807128906, 3.7597758769989014, "[TT] Gas Mixture of the Detector = 80% Xe / 20% CO2"]
-[6.604450225830078, 5.1886467933654785, "[FF] Function of the AIU = Provides DC power, the standard frequency, and signal interface ports"]
-[11.916755676269531, 4.999967098236084, "[TT] Dimensions of the ALTIUS = 800 x 800 x 1200 nm"]
-[7.441035270690918, 5.065629959106445, "[FF] Components of the ROSE-L satellite bus = Three cameras (CAM), Power Control and Distribution Unit (PCDU), Solar array Photovoltaic Assembly (PVA), Ka-band transmission unit, S-band transponder and star trackers"]
-[4.773889541625977, -1.874603509902954, "[FF] Mission Expectations of the Chang'e-5 = Major Contributions"]
-[3.0821950435638428, 2.0203516483306885, "[TT] Launch Date of the Copernicus Sentinel-6 Michael Freilich = 10 November"]
-[10.032134056091309, 7.2823100090026855, "[TT] Field of Regard of the FOR = ~ 800 km"]
-[14.139095306396484, 3.2535953521728516, "[TT] Mass of the DPU = 14 kg"]
-[7.123466968536377, 4.387785911560059, "[FF] Orbit Determination Data Source of the WEOS = Onboard GPS receiver, TLE sets provided by NORAD"]
-[7.0837788581848145, 3.7336812019348145, "[TT] GPS Measurement Availability of the PROBA-3 = Not available during Formation Flying operation periods"]
-[9.007709503173828, 4.399846076965332, "[TT] Range of the Sun sensors = \u00b150\u00ba"]
-[8.896194458007812, 4.393693447113037, "[FF] Type of the Fine Sun Sensors = Unknown"]
-[5.4849443435668945, 1.205215573310852, "[FF] Launch Date of the Oculus-ASR = Unknown"]
-[5.737880229949951, 0.5533224940299988, "[FF] Publication Date of the ATLAS = 2012"]
-[3.8032846450805664, 4.721651077270508, "[TT] Ground-Track Control of the RADARSAT-2 = Within 150 m of nominal"]
-[8.073473930358887, 0.8343763947486877, "[TT] Drought Impact of the Wells = Mild to extreme"]
-[4.5639848709106445, 5.799355506896973, "[TT] Identification of the 121.5 MHz emergency beacons = Not included"]
-[3.9333810806274414, 0.8759679794311523, "[FF] Mission Date of the PSLV-21 = Sept. 4, 2012"]
-[3.418532371520996, 5.277345657348633, "[FF] Downlink Power of the SAR (Synthetic Aperture Radar) Instrument = Increased"]
-[6.959891319274902, 7.767910480499268, "[TT] Surface Accuracy Goal of the Reflector Assembly = 1.0 mm rms"]
-[5.089707374572754, 8.327317237854004, "[TT] Bandwidth of the ALScat = 4 MHz"]
-[4.435022830963135, 7.7369489669799805, "[TT] Downlink Frequency of the CUTE-1.7+APD = UHF (437.505 MHz)"]
-[8.430145263671875, 1.152071237564087, "[TT] Quantization Levels of the Precipitation over land ares = 0,5,10,15,20, \u226525"]
-[13.763839721679688, 2.8648595809936523, "[TT] Total Mass of the Spacecraft = 7.5 kg"]
-[5.331583023071289, 0.6345958709716797, "[FF] Joining Date of the Juno = 4 August 2021"]
-[7.920130729675293, 1.4530829191207886, "[FF] Purpose of the Observation Data = Evaluation of irrigated rice"]
-[10.641560554504395, 3.32755708694458, "[TT] Behavior in Microgravity of the Cryogens = Bubbles don't rise to the top"]
-[10.261651039123535, 3.421299457550049, "[TT] Stabilization of the MicroMAS-2 CubeSat = Three-axis"]
-[9.447748184204102, 1.5010790824890137, "[FF] Observation of the New Horizons = Tons of material from Io's volcanoes move down the tail in large, dense, slow-moving blobs"]
-[4.551130294799805, 7.057374000549316, "[FF] Limitations of the Q/V-bands = Increase of atmospheric impairments"]
-[13.972052574157715, 7.1314311027526855, "[TT] Internal Power Lines of the MuREM = +1.5V, +3.3V, -5V, \u00b110V, +20V"]
-[3.8744699954986572, -2.173056125640869, "[FF] Personnel Needs of the Specialized Asset Trackers = Full time employees for monitoring"]
-[8.937357902526855, 8.025691032409668, "[TT] CCD Line Read-Out Rate of the FPM (Focal Plane Module) = 6.5 MHz"]
-[10.763140678405762, -1.130640983581543, "[TT] Altitude Control Accuracy of the SLATS = \u00b11km (1\u03c3) at each altitude"]
-[5.951173782348633, 5.187033176422119, "[TT] Interface of the CEPA = FRAM (Flight Releasable Attachment Mechanism)"]
-[9.760615348815918, -1.437522292137146, "[FF] Targeted Orbit of the Galileo FOC satellites = Circular, inclined at 56\u00ba with a semi major axis of 29,900 km"]
-[7.916710376739502, -2.5506980419158936, "[TT] LBH Emission Production Mechanism of the GOLD = Photoelectron impact on N2"]
-[8.268122673034668, 7.941149711608887, "[TT] Detector Array of the SWIR Spectrometer = 160 x 250 channels"]
-[8.00351619720459, 0.8086931705474854, "[FF] Drought Duration of the GRACE = 2015-16"]
-[4.17631721496582, 3.263805627822876, "[FF] Location of the SAR-VTB = Maspalomas station, at the southern end of the largest island of the Canary Islands"]
-[10.009904861450195, 3.0445735454559326, "[FF] Mission Objective of the LLITED CubeSat = Provide ionosphere and thermosphere measurements"]
-[3.793994665145874, 2.037804126739502, "[TT] Mission Type of the Sentinel-5P = EO"]
-[2.5564091205596924, 0.16525763273239136, "[TT] Pulse period (ms) of the B0540-69 = 50.499"]
-[4.839624404907227, 8.56512451171875, "[TT] Center Frequency of the Channel 1 = 10.6 GHz"]
-[10.674517631530762, 8.765056610107422, "[TT] 3 dB Footprint Size of the Channel = 23 x 15 km"]
-[9.574047088623047, 8.311957359313965, "[TT] Field of View of the INTEGRAL = Large"]
-[8.616646766662598, 4.791303634643555, "[FF] Position of the Star Tracker = Left"]
-[5.028802871704102, 3.3175110816955566, "[TT] Partners of the STPSat-1 = Northrop Grumman TASC, and Avidyne"]
-[11.352211952209473, 3.306607246398926, "[FF] Propulsion System of the Lunar Flashlight 6U CubeSat = Novel technology developed by VACCO Industries, Inc."]
-[3.0818238258361816, 2.3241450786590576, "[TT] Bands Resolution of the Sentinel-2 = 10 m"]
-[8.864748001098633, 4.582300662994385, "[FF] Number of Sensors of the S/C Adaptors = 2 S/C-based separation sensors and one LV-based separation sensor"]
-[7.023603916168213, 2.8511557579040527, "[FF] Included Features of the Spectra On-Demand Secure Bundle = Global activity monitoring, Comprehensive commercial satellite imagery, Automated tipping and cueing, Secure online environment for analyst collaboration"]
-[8.497992515563965, 1.138360619544983, "[TT] Quantization Levels of the Precipitation over water = 0,5,10,15,20,\u226525"]
-[5.871260643005371, 8.522285461425781, "[TT] Channels of the CoSMIR = 50.3, 52.8, 53.6, 91.665 (V and H polarization), 150, 183.3 \u00b1 1, 183.3 \u00b1 3, and 183.3 \u00b1 6.6 GHz"]
-[9.966816902160645, -1.4235323667526245, "[TT] Inclination of the OceanSat-1 = 98.28\u00ba"]
-[8.400620460510254, 3.4047482013702393, "[TT] Vacuum Level of the Large Space Simulator = A billion times sparser than standard sea-level atmosphere"]
-[7.706655025482178, 2.9582605361938477, "[FF] Observation Type of the GOSAT = Similar to Copernicus Anthropogenic Carbon Dioxide Monitoring, CO2M mission"]
-[7.45038366317749, 2.279578924179077, "[TT] Coverage Area of the GOES-S = Western U.S., Alaska, Hawaii and the Pacific Ocean"]
-[4.505465507507324, 6.94644832611084, "[FF] Type of the S-band Communications System = Experimental"]
-[9.589219093322754, 4.746522903442383, "[TT] Attitude Control of the ADCS unit = Y-momentum 3-axis stabilization"]
-[6.929736614227295, 9.05298900604248, "[TT] Band Center of the POLDER-1/2 = 490 nm"]
-[9.01895523071289, 5.419727325439453, "[TT] Body-Pointing Capability of the Resurs-DK1 = \u00b1 30o into the cross-track direction"]
-[5.918699264526367, 6.177565574645996, "[FF] Communication Delay of the EDRS-C = Up to 90 minutes"]
-[9.181647300720215, 3.5480237007141113, "[FF] Surface Pressure Retrieval Algorithm of the Unknown = Unknown"]
-[10.64190673828125, 7.326241493225098, "[TT] Swath Width of the Instrument = 2400 km"]
-[6.501965045928955, 0.850565493106842, "[FF] Contract Signing Date of the Three high-priority environmental missions = 13 November 20220"]
-[10.067421913146973, 7.986117362976074, "[TT] Telescope Type of the R3 Sensor = 1-inch refractive optical telescope"]
-[6.81094217300415, 1.182384729385376, "[TT] Science Data Duration of the Colorado Student Space Weather Experiment (CSSWE) = 3 weeks"]
-[6.075096130371094, 7.832180976867676, "[TT] Gain Variable Range/Step of the D-Amps = Range: 0 to 3 dB Step: 0.5 dB"]
-[7.0549635887146, 3.490724802017212, "[FF] Design of the MMS = Four spacecraft flying in a tight tetrahedral formation"]
-[5.84653902053833, -0.7651386857032776, "[TT] Lifetime of the MetOp-A = 10 years"]
-[11.877155303955078, 5.086757659912109, "[TT] Volume of the POLDER-2 = 0.8 m x 0.5 m x 0.25 m"]
-[10.01436710357666, -1.5130990743637085, "[TT] Inclination of the Orbit = 123\u00ba"]
-[5.325139045715332, 3.6587178707122803, "[TT] Avionics of the Platform = SSTL-100, SSTL-150 and SSTL-300"]
-[8.82873821258545, 5.156377792358398, "[TT] Pointing Accuracy of the Star Tracker = 10 arcsec"]
-[10.421688079833984, 1.5863908529281616, "[TT] Number of Identified Stars of the Delta Scuti stars = 60"]
-[9.47080135345459, 0.5970508456230164, "[TT] Impact Speed of the Schiaparelli module = 540 km/h"]
-[5.8871750831604, -0.6061621904373169, "[TT] Mission Lifetime of the Platform = ~ 15 years"]
-[4.430666923522949, 3.0648624897003174, "[TT] Location of the TTS: Thule Tracking Station, Thule, Greenland = Thule, Greenland"]
-[6.387781143188477, 4.391172885894775, "[FF] Function of the Mission Control = Collect, consolidate and route system parameters of the space and ground segment"]
-[8.899173736572266, 6.496993541717529, "[TT] Resolution of the Altimeter = About 0.9 m"]
-[4.950066089630127, 3.305230140686035, "[TT] Manufacturer of the STPSat-1 = Comtech-AeroAstro Inc."]
-[5.220293998718262, 5.513173580169678, "[TT] Protocol of the IXV Communications Network = IP"]
-[5.4024529457092285, 0.5241230130195618, "[TT] Launch Date of the Envisat = March 01, 2002"]
-[3.087392807006836, 1.8257935047149658, "[TT] Image Capture Date of the Sentinel-2C = February"]
-[7.402459621429443, 1.1628139019012451, "[TT] Data Utilization Project Period of the SeaSat = 1979-1982"]
-[13.904163360595703, 7.185520172119141, "[TT] Voltage of the Pulsed Diode Driver = ~28 VDC"]
-[5.409329414367676, 8.652517318725586, "[TT] Spectral Bandwidth of the Spectral Bandwidth = 16 nm >1000 nm"]
-[4.88505744934082, 7.342385768890381, "[TT] Data Rate of the L-band Transmitter = 1 Mbit/s"]
-[7.837534427642822, 9.146954536437988, "[TT] Amplified Output Wavelength of the LOM = 1064 nm"]
-[3.1768791675567627, 5.070688724517822, "[TT] Imaging Resolution of the SAR module = 3m-100m"]
-[8.14846134185791, 2.480703353881836, "[FF] Measurement of the Multibeam Thermal-Infrared Instrument = Height-resolved cloud movements"]
-[10.435635566711426, 5.823998928070068, "[TT] Temperature Range of the LCPR = 10-30 degrees Celsius"]
-[4.795804977416992, 1.1754800081253052, "[TT] Development Cooperation Agreement Date of the Alphabus = March 2006"]
-[7.7065300941467285, 6.952341079711914, "[TT] F Number of the CIRiS = F/1.8"]
-[5.181697368621826, 0.19868133962154388, "[FF] Launch Date of the Polar Scout = 3 December 2018"]
-[6.578989505767822, 3.035003900527954, "[FF] Data Processing of the TSIS-1 = Performed at the University of Colorado Boulder"]
-[10.4072904586792, 2.158156394958496, "[TT] X-ray Detection Range of the NuSTAR = Higher end of the range"]
-[5.4667439460754395, 6.320063591003418, "[FF] Memory of the Satellite Memory = Limited"]
-[5.801578044891357, 0.9343458414077759, "[FF] Calibration Date of the Mirror Modules = Sept. 2013"]
-[7.682023525238037, 9.068952560424805, "[TT] Bandpass of the Short Wavelength Band = 900-1150 \u00c5"]
-[10.955036163330078, 5.89581823348999, "[TT] Anticoincidence CsI Crystal Thickness of the GRS = 30 mm"]
-[9.922635078430176, 7.627920150756836, "[TT] GSD at Nadir of the Telescope = 30 m"]
-[6.7162346839904785, -0.27764177322387695, "[TT] Period of the Satellite Constellation = 136 minutes"]
-[13.873608589172363, 3.693528890609741, "[TT] Mass of the AEISS telescope = < 80 kg"]
-[6.923283576965332, 3.1282472610473633, "[FF] Purpose of the Proposed Constellations = Enhance Arctic weather observations"]
-[7.4672770500183105, 4.290246486663818, "[FF] Sensor Complement of the CXBN-2 = Unknown"]
-[7.119831562042236, 8.651424407958984, "[TT] Order of the Bandpass Filters = 9th order"]
-[6.945058822631836, 1.461488962173462, "[TT] Deployment Status of the SporeSat = Ongoing"]
-[11.858827590942383, 3.144674301147461, "[TT] Delta-V of the Water Propulsion System = More than 130 m/s"]
-[6.584829330444336, -2.0487096309661865, "[TT] Meeting Date of the Jason-3 = Oct. 18-20, 2010"]
-[5.130180358886719, 0.9451605677604675, "[FF] Deployment of the MUPUS-PEN = Will be deployed"]
-[10.701803207397461, 3.264101266860962, "[FF] Testing Environments of the Bricks = Microgravity, 1 g, less than 1 g"]
-[8.449407577514648, 3.1044628620147705, "[FF] Data Products of the TOMS = Vertical distribution of ozone, global maps of total ozone and 200-mb height fields; incident solar ultraviolet irradiance and ultraviolet radiation backscattered from the Earth"]
-[7.04519510269165, 0.869910478591919, "[FF] Mission Overview URL of the Gravity Probe B = http://einstein.stanford.edu/MISSION/mission1.html"]
-[9.664905548095703, 7.176631450653076, "[TT] Ground Resolution of the WPM = 55 m"]
-[5.802107334136963, 1.0133612155914307, "[FF] Report Date of the KUKAI = April 23, 2009"]
-[5.480164527893066, 6.2702131271362305, "[TT] Onboard Mass Memory of the Solar Orbiter = Yes"]
-[11.742804527282715, 4.865370273590088, "[TT] Size of the HAUSat-2 = 32 cm x 32 cm x 40 cm"]
-[5.403134346008301, 5.59020471572876, "[FF] Data Encoding of the MIU = CCSDS"]
-[8.508140563964844, 0.13650161027908325, "[FF] Objectives of the Rosetta Mission = Global characterization of the nucleus, determination of its dynamic properties, surface morphology and composition, determination of chemical, mineralogical and isotopic compositions of volatiles and refractories in the cometary nucleus, determination of the physical properties and interrelation of volatiles and refractories in the cometary nucleus, studies of the development of cometary activity and the processes in the surface layer of the nucleus and inner coma, studies of the evolution of the interaction region of the solar wind and the outgassing comet during perihelion approach"]
-[9.64050579071045, 7.2291131019592285, "[TT] Interference Nadir Gap of the NNI = \u00b14 km"]
-[9.72673225402832, -0.5104444026947021, "[TT] Altitude of the Corvus-BC 3 = 481.2 km"]
-[5.914412975311279, 1.8342947959899902, "[FF] Date of the Orion's First Flight Test = June 19, 2014"]
-[8.036327362060547, 3.1377933025360107, "[FF] Measurement Category of the CarbonSpec = Near-infrared absorption of carbon dioxide and the molecular oxygen in reflected sunlight"]
-[7.725604057312012, 9.527438163757324, "[TT] Center Wavelength of the B2 = 490 nm"]
-[3.8039867877960205, 7.176044464111328, "[TT] Antenna Gain of the LNA = 6 dBi"]
-[1.7208378314971924, 6.137490749359131, "[TT] Hot Intergalactic Gas Percentage of the Universe = 40 percent"]
-[6.722598075866699, 7.595733165740967, "[TT] Beam Width of the Channel = 0.43 \u00ba"]
-[10.34891414642334, 1.9757636785507202, "[FF] X-ray Data Discovery of the Hoinga SNR = Expected to discover new supernova remnants in its X-ray data over the next few years"]
-[6.252752780914307, 6.230599880218506, "[TT] Monitoring Duration of the IPU = At least 30 days"]
-[4.474221706390381, -0.027438988909125328, "[TT] Launch Date of the Starliner = Dec. 20"]
-[7.430712699890137, 6.588919639587402, "[TT] Time Resolution of the FREND = From 1 second"]
-[3.6376545429229736, 3.389129877090454, "[TT] Payload of the Falcon 9 rocket = Spain\u2019s PAZ satellite"]
-[6.776996612548828, 6.04855489730835, "[TT] Control Mode of the HS = SHM (Safe Hold Mode) and controlled through Proteus platform"]
-[8.623390197753906, 4.72408390045166, "[TT] Star Spot Coverage of the DS Tuc A = Up to 40%"]
-[9.30377197265625, 3.5471508502960205, "[FF] Objective of the NanoSatC-BR = Provide monitoring of Earth's magnetosphere by measuring the magnetic field over Brazil and to study the magnetic phenomena of the SAA (South Atlantic Anomaly) and the EEJ (Equatorial Electrojet)"]
-[6.517975807189941, -0.37561893463134766, "[TT] Test Period of the Sloshsat-FLEVO = About a week"]
-[10.402250289916992, 2.123047351837158, "[TT] Number of X-ray Telescope Modules of the eROSITA = 7"]
-[6.70150089263916, 6.082587718963623, "[FF] Development Date of the Laser Communication System = Sept. 29 to Oct. 3, 2008"]
-[8.725471496582031, 2.2103097438812256, "[FF] Number of Published Papers of the SOHO = More than 2500"]
-[6.563767433166504, 3.5022149085998535, "[FF] Purpose of the Airlock Stowage Platform = This deck configuration of the upgraded platform will increase the overall stowage capability on the International Space Station, allowing the crew to further reduce the impact of on-orbit cargo kept and maintained"]
-[5.094892501831055, 7.289158344268799, "[TT] Telemetry Bit Rates of the UHF = Hundred of kbit/s"]
-[11.19360637664795, 5.951911926269531, "[TT] Material of the Hexapod Structure = SiC"]
-[5.178933620452881, 4.448628902435303, "[TT] Position and Attitude Determination of the Ground Station = Automatic"]
-[14.745096206665039, 6.641740322113037, "[TT] Capacity of the Lithium-ion batteries = 4.8 Ah"]
-[9.255034446716309, 1.8391554355621338, "[FF] Contribution of the HARP-2 = PACE mission"]
-[14.25166130065918, 3.2210748195648193, "[TT] Total Mass of the ACC = 54 kg"]
-[10.909326553344727, 3.530747175216675, "[TT] Size of the 6U CubeSat = 10 x 20 x 30 cm"]
-[9.915462493896484, -0.5024043321609497, "[TT] Altitude of the GOSAT-2 = 613 km"]
-[4.7457404136657715, -1.8217995166778564, "[FF] Discovery Date of the Chang'e-4 = 21 July 2020"]
-[10.538683891296387, 7.438660144805908, "[TT] Swath Width of the ETM+ Scanner = 185 km"]
-[4.760263442993164, -0.3121945858001709, "[TT] Proposed Doubleheader Launch Time of the Falcon 9 = Less than four and a half hours apart"]
-[8.988471984863281, 7.365280628204346, "[TT] Resolution of the Visual Imager = More than 600 mega pixels"]
-[8.66318130493164, 4.766534805297852, "[TT] Availability of the Star Tracker = >99.9%"]
-[4.938042163848877, 1.9925071001052856, "[FF] Mission Status of the TUBSAT = Mission complete"]
-[3.834393262863159, 7.2035956382751465, "[TT] EOC Gain of the NAVANT = 15 dBi"]
-[6.368555545806885, 8.611076354980469, "[TT] Polarization of the MTVZA-GY = Vertical and horizontal"]
-[10.369524002075195, 5.692399024963379, "[TT] Total Heat Input of the Hayabusa-2 SRC = 270 MJ/m2"]
-[8.146852493286133, 4.987840175628662, "[TT] Calibration of the Calibration = Total calibration of instrument artifacts <0.5% at top-of-atmosphere"]
-[5.5852813720703125, 2.206413984298706, "[FF] Mission Status of the OPS-SAT = Operational"]
-[6.941954612731934, 4.2128777503967285, "[FF] Quantity of the ScaRaB = Unknown"]
-[3.8478856086730957, 4.442469120025635, "[TT] Data Acquisition of the RADARSAT-2 = Regardless of light or weather conditions"]
-[2.891813039779663, 4.255937099456787, "[TT] Observation Date of the PALSAR-2 = Feb. 21, 2015"]
-[8.137962341308594, 6.446352005004883, "[FF] Cropping Effect of the OHU = Decreases power on the two detectors within FLLS"]
-[10.752741813659668, 1.0825749635696411, "[TT] Planet Diameter of the ExoMars TGO = 34 arcseconds"]
-[12.973196983337402, 7.062220096588135, "[TT] Data Transfer Power Requirement of the WCOM = 30 W"]
-[9.739563941955566, 7.17349910736084, "[TT] Along-track resolution of the C-band = 10 km"]
-[8.61446475982666, 3.432197332382202, "[FF] Function of the Machine Learning Algorithm = Recognize a solar flare and determine how much degradation is affecting AIA's current images and how much calibration is needed"]
-[7.922736644744873, 3.553870677947998, "[TT] Sensor complement / remarks of the Meteor-1-2 = TV, IR, AC"]
-[4.714630603790283, 2.891925096511841, "[TT] Location of the Mission Operations Center (MOC) = Boston University (BU)"]
-[10.187196731567383, 8.028818130493164, "[TT] Aperture Size of the WorldView satellites = 1.1-meter"]
-[7.181190013885498, 5.223534107208252, "[FF] Function of the LCEU = Converts the lateral and longitudinal signals into a 3D displacement"]
-[5.130392551422119, 5.017168998718262, "[FF] Payload of the Quango = Double payload with 5G connection and end-to-end encryption device"]
-[8.226770401000977, 7.789222717285156, "[TT] Number of Detectors of the Spectrometer = 3"]
-[10.37146282196045, 2.81001615524292, "[FF] URL of the Galassia Nanosatellite = http://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=3418&context=smallsat"]
-[6.995355606079102, 7.750120162963867, "[TT] Focal Length of the Primary Reflector = 28,500 mm"]
-[14.092494010925293, 3.086320400238037, "[TT] Mass of the S-Cube = 4 kg"]
-[8.967443466186523, 3.396153688430786, "[FF] Changes of the Ion flows = Rapidly"]
-[6.7652411460876465, -0.5896680951118469, "[TT] Orbit Period of the Primary Mission = 101 minutes"]
-[5.47543478012085, 6.067966938018799, "[TT] FLASH for boatload of the Memory = 2 MByte"]
-[6.0171027183532715, 2.6270248889923096, "[FF] Development Team of the Binar-1 = Team of students and engineers at Curtin University's Space Science and Technology Centre"]
-[7.791774272918701, 8.124238967895508, "[TT] Color of the Optomechanics = Blue"]
-[4.297247886657715, 2.2468857765197754, "[TT] Integration Partner of the LightSail-2 = Prox-1"]
-[7.653148174285889, 5.434259414672852, "[FF] Instrument of the SMAP satellite = Radar and radiometer"]
-[7.680868148803711, 0.8029976487159729, "[FF] Quantification Method of the Lunar Meteoroid Impact Flash Detection = Using the apparent magnitude of the light flash"]
-[10.676868438720703, 7.172025680541992, "[TT] Footprint Diameter of the Skylab S-194 = 124 km"]
-[9.77729320526123, -0.4234192669391632, "[TT] Altitude of the Suomi-NPP = 824 km"]
-[6.2445969581604, 5.932018756866455, "[TT] User Beams of the SES-17 = Nearly 200"]
-[9.993549346923828, 2.8800601959228516, "[FF] Launch Date of the CubeSat = 24 May 2022"]
-[8.179285049438477, 5.280730724334717, "[TT] Number of Lines of the Calibration Cycle = 2048"]
-[4.982436180114746, 2.6345062255859375, "[FF] Refurbishment Locations of the OMS-E = NASA\u2019s White Sands Test Facility in New Mexico, Johnson Space Center in Houston"]
-[6.10174036026001, 4.350173473358154, "[FF] Purpose of the OPS&GRND = Planned operation of the satellite and the infrastructure required to operate the ground segment"]
-[9.423063278198242, -0.6810871958732605, "[TT] Orbit of the DSX = 6000 km by 12000 km"]
-[11.22497272491455, 5.380273342132568, "[TT] Scintillation Panels Material of the ACC = Bicron BC-414"]
-[8.59758186340332, 6.748269081115723, "[TT] Camera Suite of the OSIRIS-REx = OCAMS (PolyCam, MapCam, and SamCam)"]
-[8.47999382019043, 4.9654035568237305, "[FF] Bias Requirements of the Aeolus = Can be expected to be met after further optimization of the instrument calibration and data processing"]
-[9.629748344421387, 0.764095664024353, "[TT] Expected Earth-Probe Distance of the INSPIRE = 1.5 x 10^8 km"]
-[10.229538917541504, 1.1381562948226929, "[TT] Diameter of the Cassiopeia A = 15 light years"]
-[11.05130386352539, 6.280577182769775, "[TT] Construction Material of the LORRI = Silicon carbide"]
-[6.605255603790283, -0.14661607146263123, "[TT] Period of the Landsat-9 = 99 minutes"]
-[10.818801879882812, -0.25542137026786804, "[TT] Global Absolute Height Error of the TanDEM-X = 0.9 m"]
-[5.295345306396484, 3.9155800342559814, "[TT] Number of Satellites of the Swarm = Three"]
-[9.008793830871582, 4.903492450714111, "[FF] Output Information of the AVGS = Azimuth, elevation, range, and relative attitude"]
-[6.0937371253967285, 6.03857421875, "[TT] Source of the TR modules = Indigenous"]
-[6.669067859649658, 1.9069045782089233, "[FF] URL of the Sierra Nevada Corporation = https://www.sncorp.com/press-releases/snc-hardware-on-nasa-insight-mission/"]
-[5.195472240447998, 0.33076247572898865, "[TT] Founding Date of the Spacety = 2016"]
-[5.833954334259033, 7.089742183685303, "[TT] Data Rate of the DORIS = 200 bit/s"]
-[5.716401100158691, 6.467405319213867, "[TT] Solid-State Recording Capacity of the Onboard Data Handling Subsystem (OBDH) = 90 Gbit"]
-[5.58754825592041, -2.0402960777282715, "[TT] Panchromatic Imagery Resolution of the KOMPSAT-3 = 0.7m"]
-[6.252429008483887, 3.8819382190704346, "[TT] Time Synchronization of the Spacecraft Plug-n-Play Avionics (SPA) = One pulse per second (1PPS) signal"]
-[10.096976280212402, -2.696082830429077, "[TT] Reliability of the Astrium MMFU NAND-Flash SDR-SDRAM = \u2265 0.98"]
-[3.1163389682769775, 2.3188323974609375, "[TT] High-resolution optical imager of the Sentinel-2 = Onboard"]
-[10.87443733215332, 7.397130966186523, "[TT] Swath of the HY-1C = More than 2900 km"]
-[6.68241024017334, 3.5593202114105225, "[FF] Target Industry of the MANTIS = Oil and gas sector"]
-[9.367206573486328, 3.735968828201294, "[FF] Objectives of the MAG = Not specified"]
-[11.96207332611084, 3.7050540447235107, "[FF] Function of the CDRA = Maintains the carbon dioxide partial pressure at under 5.3mm Hg for up to nine crew members"]
-[8.181136131286621, 2.975205659866333, "[FF] Observation Demonstration of the FORTE = Multisatellite observations of oceanic lightning"]
-[3.377976655960083, 5.829315662384033, "[TT] Number of Radiating Elements per Tile of the SAR antenna subsystem = 24 x 24"]
-[4.530905723571777, -0.17726445198059082, "[FF] Docking Date of the HTV-1 = Unknown"]
-[6.45389461517334, 2.824500799179077, "[FF] Research Benefits of the International Space Station (ISS) = Benefits to humanity on Earth"]
-[9.132920265197754, 5.038945198059082, "[TT] Measurement Type of the Gyrometers = Attitude"]
-[11.405506134033203, 0.7158228158950806, "[TT] Planet Orbit of the AU Mic = Just over a week"]
-[6.853855609893799, 1.7275534868240356, "[FF] URL of the Webb Telescope = https://www.nasa.gov/press-release/nasas-webb-telescope-launches-to-see-first-galaxies-distant-worlds"]
-[10.91529369354248, 2.098705768585205, "[TT] Leader of the XMM-Newton Survey Science Center = Professor Mike Watson"]
-[8.529010772705078, 5.866466999053955, "[TT] Impact of 1 mrad Error of the Beam Pointing = Radiometric error of \u00b10.5 dB or less"]
-[11.762296676635742, 6.6748576164245605, "[TT] Energy Range for Neutrons of the FREND = 0.4\u2013500 keV"]
-[5.042050361633301, 1.4663102626800537, "[TT] Development Started of the DST 8 = As of 2007"]
-[5.209060192108154, 3.72422194480896, "[TT] Mounting Satellite of the METimage = MetOp-SG-A"]
-[3.832784414291382, 7.8822922706604, "[TT] Modulation Scheme of the VHF and UHF Links = GMSK (Gaussian Minimum Shift Keying)"]
-[7.707047939300537, 9.386358261108398, "[TT] Center Wavelength of the Band 1 = 14.71 \u00b5m (680 cm -1)"]
-[8.82011604309082, 5.438175201416016, "[TT] Angle Accuracy of the MEMS device = Better than 0.15\u00ba"]
-[12.102900505065918, 7.63258171081543, "[TT] Total Mass of the LWIR Camera = 2.1 kg"]
-[5.904697895050049, 7.169025897979736, "[TT] Data Rate of the NRA = 9.8 kbit/s"]
-[10.716435432434082, 7.424544334411621, "[TT] Ground Swath of the ALI = 185 km"]
-[6.028863906860352, 5.945012092590332, "[TT] Data/Pilot of the E6-C = Pilot"]
-[8.108386993408203, 6.489050388336182, "[FF] Data Set of the EPIC = Single-pixel images taken multiple times per day, in 10 wavelengths, over an extended period"]
-[5.884988784790039, 5.861688613891602, "[TT] Data Capture of the Corvus-HD satellites = 15TB per day"]
-[9.707388877868652, 6.236639976501465, "[TT] Mirror Rotation Capability of the TIR Subsystem = 180\u00ba from the nadir position"]
-[6.412433624267578, 1.9785301685333252, "[FF] URL of the Satellite = http://badc.nerc.ac.uk/data/gedex/detail/aem2sag1.det"]
-[14.657530784606934, 6.659256935119629, "[TT] Battery Type of the ABEX = Li-ion 18650s"]
-[9.532940864562988, 4.8503642082214355, "[TT] Attitude Stabilization of the Spacecraft = 3-axis stabilized"]
-[4.535711288452148, 8.163652420043945, "[TT] Centre Frequency of the Radar = 1.275 GHz"]
-[6.445828437805176, 4.441538333892822, "[FF] Continuation of the SIM = Provided by TSIS"]
-[9.435383796691895, 8.204111099243164, "[TT] IFOV along-track of the Full-scan Imaging = 0.18\u00ba - 11.84\u00ba"]
-[10.768320083618164, 1.4232916831970215, "[TT] Mass of the Black Hole = Around fifty thousand times that of the Sun"]
-[6.9425787925720215, 4.3131279945373535, "[FF] Provides a larger target area of the Balloon = Unknown"]
-[9.991267204284668, 5.395145416259766, "[FF] Purpose of the EMB = Measure the temperature inside the Maple-1 enclosure"]
-[5.101489543914795, 0.6378272771835327, "[TT] Delivery Date to KSC of the AMS-02 = August 26, 2010"]
-[6.997629165649414, 2.3062620162963867, "[TT] Structure Manufacturer of the Biomass = APCO Technologies in Switzerland"]
-[7.298104763031006, 4.206437110900879, "[TT] Imaging Instrument of the Suomi NPP satellite = Visible Infrared Imaging Radiometer Suite (VIIRS)"]
-[10.560648918151855, 3.3810298442840576, "[TT] Structure of the TurkSat-3USat = 3U CubeSat"]
-[3.380099058151245, 3.6910860538482666, "[TT] Operational Date of the PAZ-TerraSAR Constellation = Late 2017"]
-[8.434724807739258, 5.362244606018066, "[TT] TLE Accuracy of the Orbit Dynamic System = Low distance difference of the appropriate time zone"]
-[9.970383644104004, 2.7425975799560547, "[FF] Image Credit of the HaloSat = BCT"]
-[8.276177406311035, 6.674600601196289, "[TT] Data Rate of the Scanning geometry = 660 kbit/s"]
-[8.411639213562012, 4.546762943267822, "[FF] General Relativistic Effect Test of the LAGEOS = Frame-dragging"]
-[8.274516105651855, 8.716891288757324, "[TT] Spectral Resolutions of the Ultraviolet Spectrograph = 0.2 nm and 0.4 nm"]
-[10.038459777832031, -1.5118958950042725, "[TT] Targeted Inclination of the Ariane 5 = 3 degrees"]
-[6.158289909362793, -0.5088799595832825, "[TT] Mission Duration of the Spacecraft = 2 years"]
-[10.239035606384277, 7.550712585449219, "[TT] Telescope Type of the GOES Imager = Cassegrain telescope"]
-[9.686434745788574, 1.4173710346221924, "[TT] Number of Spacecraft of the Pl\u00e9iades = 2"]
-[5.42960262298584, 3.4871139526367188, "[FF] Demonstration Launches of the MakerSat = MakerSat-0 and MakerSat-1"]
-[4.741057872772217, 3.2445762157440186, "[TT] Manufacturer of the Power Control and Distribution Unit (PCDU) = Thales Alenia Space in Belgium"]
-[6.665958881378174, 6.376442909240723, "[TT] Data Processing Time of the CPOM = Within two days of acquisition"]
-[13.889108657836914, 2.864259958267212, "[TT] Launch Loads of the SRMSat = \u00b1 11 g longitudinal and \u00b1 6 g lateral"]
-[7.722052097320557, 0.3973453938961029, "[FF] Purpose of the Lucy = Show us the diversity of the primordial bodies that built the planets"]
-[11.69240951538086, 6.713076114654541, "[TT] Energy Range of the Telescope = 3/4 keV"]
-[5.566198825836182, 2.9192633628845215, "[FF] URL of the GOES-R Series = http://www.lockheedmartin.com/us/products/geostationary-operational-environmental-satellite-r-series--goes.html"]
-[3.460258960723877, 6.419743061065674, "[TT] Size of the Transmit Antenna = 3.3 m dish"]
-[8.318174362182617, 5.225841522216797, "[TT] Calibration Mode of the TOMS = Standby mode, Solar calibration mode, Direct control mode"]
-[4.2236738204956055, 0.20418407022953033, "[FF] Launch Date of the FalconSAT-3 = Unknown"]
-[8.477044105529785, 6.240355968475342, "[TT] Total Range of the CERES = 0.3 - 100 \u00b5m"]
-[14.538841247558594, 6.575987339019775, "[TT] Battery Capacity of the GHGSat-D = 26 W hr"]
-[6.488292694091797, 4.2600836753845215, "[FF] Availability of the Avionics Components = Flight model version"]
-[5.421912670135498, -0.0029605035670101643, "[TT] Reentry Time of the Cygnus = Feb. 25 at 4:05 a.m. EST"]
-[14.099336624145508, 7.202810764312744, "[TT] Main Power Bus Voltage of the PCDU = 28 V \u00b14 V"]
-[13.251541137695312, 7.396796226501465, "[TT] Average Power of the Downlink Data Power = 0.5 W"]
-[6.371102809906006, 4.515200614929199, "[FF] Function of the SOC = Receives and stores all AMS science and housekeeping data, as well as ancillary data from NASA, ensures full science data reconstruction, calibration and alignment; archives all data and keeps data available for physics analysis"]
-[4.982429504394531, 3.312575340270996, "[TT] Manufacturer of the ESA = JPL"]
-[8.041522979736328, 4.6160078048706055, "[FF] Involvement of the HSI payload, the mass memory and coding unit (DSHA) and the AOCS (Attitude and Orbit Control Subsystem) = Image acquisition and calibration"]
-[2.904663562774658, 4.46128511428833, "[FF] System Components of the PALSAR-2 = Exciter (EX), Transmitter (TX), Receiver (RX), Digital Processor (DP), and System controller (SC)"]
-[3.2968106269836426, 5.032724857330322, "[TT] Mode of the SAR Sensor Subsystem = ST (Standard Mode)"]
-[4.530723571777344, 3.869110584259033, "[TT] Number of Satellites of the Galileo Constellation = 24"]
-[8.443133354187012, 3.202601194381714, "[TT] Minimum Concentration in 2015 of the Ozone Layer = 101 Dobson Units"]
-[8.261748313903809, -2.1665961742401123, "[FF] Orbit of the GOLD = Geostationary"]
-[7.892788410186768, 5.983850002288818, "[FF] Video Camera Assembly of the LAPAN-A2 = COTS (Commercial-of-the-Shelf) RGB medium format video camera"]
-[4.511309623718262, 2.958652973175049, "[TT] Coordination Location of the GBOT = Heidelberg"]
-[8.166711807250977, 2.9597744941711426, "[FF] Conference Date of the Geostationary Lightning Mapper (GLM) = Jan. 30- Feb. 2, 2006"]
-[14.745614051818848, 6.606269836425781, "[TT] Overall Capacity of the Li-battery = 80 Ah"]
-[8.072601318359375, -1.2429213523864746, "[TT] Laser Beams of the ICESat-2 = 6"]
-[6.297521114349365, 4.659276008605957, "[FF] Requirement of the Monitoring and shutdown system = Detect and shutdown any power line which has encountered a fault"]
-[16.544471740722656, 3.6380162239074707, "[TT] Planned Number of Satellites of the OneWeb = 648"]
-[4.572584629058838, 8.096307754516602, "[TT] Center Frequency of the Radar = 1236.5 /  1257.5  / 1278.5 MHz"]
-[6.573566913604736, 1.7038955688476562, "[FF] URL of the GIADA = http://sci.esa.int/rosetta/35061-instruments/?fbodylongid=1639"]
-[5.622945785522461, 4.761803150177002, "[FF] Design Principles of the X-Series platforms = Use of mature, well developed non space specific protocols such as CAN (Controller Area Network)and LIN (Local Interconnect Network), On board autonomy, Robustness and redundancy, The use of COTS (Commercial-off-the-Shelf) components and technologies, Modularity, Low recurrent costs at unit level"]
-[7.614038944244385, 8.830170631408691, "[TT] Spectral Band of the MSU-E = 0.8 - 0.9 \u00b5m"]
-[7.879473686218262, 0.7836477756500244, "[FF] Mass Distribution of the Earth System = Continuously Changing"]
-[6.057426929473877, -0.207991823554039, "[TT] Operational Lifetime of the KazEOSat-2 = 7 years"]
-[7.6916608810424805, 2.966704845428467, "[FF] Mission of the GOSAT-2 = Gather observations of greenhouse gases"]
-[7.429441452026367, 0.9704771041870117, "[FF] Purpose of the Lunar Pathfinder = Provide affordable communications services to lunar missions"]
-[6.950316905975342, 4.590881824493408, "[TT] Science Payload of the nSight-1 = FIPEX (Flux-\u03a6-Probe Experiment)"]
-[13.384076118469238, 6.763646602630615, "[TT] Power of the DubaiSat-2 = 100 W"]
-[7.831129550933838, 8.699610710144043, "[TT] Spectral Range (Band 1) of the PanMUX = 0.51-0.85 \u00b5m"]
-[5.491611480712891, 2.252765417098999, "[FF] Affiliation of the Bruno N. Calvo = Unknown"]
-[6.9152750968933105, 6.11568546295166, "[TT] Data Update Frequency of the GPM = Every 30 minutes"]
-[4.112717628479004, 5.69150972366333, "[TT] Deployment Goal of the ADS-B = End of 2019"]
-[8.739527702331543, 2.125776529312134, "[TT] Look Angle of the SeaWinds = 40\u00ba and 46\u00ba from nadir"]
-[13.23207950592041, 5.430382251739502, "[TT] Solar Array Deployment Status of the Lucy = Incomplete"]
-[9.353489875793457, 7.090902328491211, "[TT] Resolution of the COSI = 2.8 m (4 x MS)"]
-[9.40720272064209, 6.983271598815918, "[TT] Spatial Resolution of the MSU-E = 45 m x 33 m"]
-[4.874539852142334, 7.016076564788818, "[FF] Telemetry of the ISM S-band (2400-2483.5 MHz) = Possible for telemetry"]
-[13.460916519165039, 7.317997932434082, "[TT] Short Circuit Current of the CSS = 34 mA"]
-[11.803373336791992, 6.7395243644714355, "[TT] Proton Energy Range of the LIPS = 30 keV - 2 MeV"]
-[9.267321586608887, 6.12436580657959, "[TT] Mount Type of the Argus = Adjustable vernier kinematic mount with five degrees of freedom"]
-[4.3532304763793945, 0.780194878578186, "[TT] Launch Date of the HY-1D = 10 June 2020"]
-[11.940017700195312, 5.388716697692871, "[TT] Structure Dimensions of the eROSITA instrument = ~ 1.9 m in diameter x 3.25 m in hight"]
-[6.557336330413818, 6.448009490966797, "[TT] Burst Alert System Response Time of the INTEGRAL = Within a record 18 seconds"]
-[5.187274932861328, 7.012996196746826, "[TT] Data Downlink Rate of the TDRSS = 20 kbit/s"]
-[9.302986145019531, -0.40343189239501953, "[TT] Performance of the Vega-C = About 2.2 t in a reference 700 km polar orbit"]
-[6.2768988609313965, 8.60892391204834, "[TT] Beam Polarization of the ALOS-2 = HH+HV"]
-[5.886648178100586, 0.9132247567176819, "[TT] Image Acquisition Date of the DMS = November 3, 2017"]
-[6.923854351043701, 7.1507182121276855, "[TT] Pulse Frequency of the Laser = 500 Hz ~ 10 kHz"]
-[4.720883369445801, 3.2748193740844727, "[TT] Manufacturer of the S-band Transponder = Thales Alenia Space in Spain"]
-[5.766612529754639, 6.318032741546631, "[TT] Capacity of the SSR = 150 Gbit BOL"]
-[6.918828964233398, 1.4558464288711548, "[FF] Mirror Alignment Continues Date of the Webb = 25 February 2022"]
-[8.315747261047363, -0.8495284914970398, "[TT] Accuracy of Ice-Sheet Elevation Changes Measurement of the ATLAS = 4 mm per year"]
-[7.629454135894775, 3.033557653427124, "[FF] Measure Emissions from Individual Facilities of the GHGSat = Unknown"]
-[12.513113021850586, 3.1838371753692627, "[TT] Mass of the Propellant = 80 kg"]
-[7.41488790512085, -0.07257772237062454, "[TT] Mission Status of the Philae = Active"]
-[11.588167190551758, 6.876822471618652, "[TT] Effective Area of the ART-XC = 2500 cm^2 at 1 keV"]
-[9.396218299865723, 8.28101921081543, "[TT] Sampling Interval of the Telescope = 280 \u00b5rad"]
-[7.601444244384766, -0.1525282859802246, "[FF] Presentation Date of the Lunar Ice Cube Mission = March 21-25, 2016"]
-[7.341071128845215, 4.195099353790283, "[FF] Sensor Complement of the BRITE-Austria = Unknown"]
-[8.302145004272461, 7.8236165046691895, "[TT] Number of Detectors of the Scanner Assembly = 96"]
-[4.677476406097412, 7.588599681854248, "[TT] Data Transmission of the LT = Lithium radio"]
-[5.107819080352783, 1.2177397012710571, "[FF] Launch Date of the ALOS-2 = May 24, 2014"]
-[11.901695251464844, 5.375545024871826, "[TT] Dimensions of the Instrument = 900 mm x 600 mm x 230 mm"]
-[3.3595073223114014, 1.5435857772827148, "[FF] Application Date of the Sentinel-5P = 18 September 2020"]
-[5.527639865875244, 0.8037025332450867, "[FF] Operation Timeframe of the AaSI = June-August growing season"]
-[3.837892770767212, 1.3333686590194702, "[TT] Landing Location of the Falcon 9 = \"Just Read the Instructions\" droneship, which was stationed in the Pacific Ocean"]
-[8.715402603149414, 1.265384316444397, "[FF] Used in Test of the GRACE Earth gravity model = Yes"]
-[9.887947082519531, -0.4005931615829468, "[TT] Data Point Interval of the GEOSAT = 6.7 km"]
-[4.532557487487793, 7.699487686157227, "[TT] Receiver Type of the LICEF = Frequency-selective"]
-[9.918251037597656, 7.995101451873779, "[TT] FWHM of the Telescope's PSF = Less than 0.22\u00b0"]
-[7.972222328186035, 4.770586013793945, "[FF] Frequency of the Calibration Phases = Periodically"]
-[10.70808219909668, 2.8184075355529785, "[FF] Design Presentation Date of the Microsatellites = Oct. 10, 2002"]
-[6.293429851531982, 0.16555923223495483, "[TT] Crew Size of the Skylab-1 = Three astronauts"]
-[7.980223655700684, 6.231817245483398, "[FF] Fidelity Maintenance of the Infrared Radiometric = Timed interval views of the space for reference (approximately every 120 s)"]
-[13.418612480163574, 6.819614410400391, "[TT] Payload Power of the LEOStar-2 = Up to 2 kW"]
-[4.932153701782227, -2.1451125144958496, "[TT] Chang'e 5 Weight of the Chang'e-5 = 8.2 metric tons"]
-[10.429181098937988, 3.2615764141082764, "[TT] Number of CubeSat Units of the Ho'ponopono = 3"]
-[8.471129417419434, 7.1557536125183105, "[TT] Mode of the BIRCHES = Imager"]
-[8.784750938415527, 4.649207592010498, "[FF] Function of the Star Sensors = Measure and report the S/C orientation relative to an inertial reference frame"]
-[13.353165626525879, 7.6802544593811035, "[TT] RF Transmit Power of the RA-1 = 55 W peak"]
-[6.281551837921143, 7.708010196685791, "[TT] Close Passes of the Mariner 10 = 3"]
-[9.554010391235352, 2.5144996643066406, "[FF] Parameter Extraction of the Vricon = x, y and z coordinates"]
-[8.120976448059082, 2.5676183700561523, "[TT] Measurement Types of the AIM = Polar Mesospheric Clouds, temperature, O3, H2O, CH4, NO, limb extinction, gravity waves"]
-[7.845129013061523, -0.15845488011837006, "[TT] Latency of the ATL07 Arctic/Antarctic Sea Ice Elevation = 45 days"]
-[6.253932476043701, 4.580872058868408, "[FF] Data Management of the LUTI = SDMS (Science Data Management Subsystem)"]
-[7.666722774505615, 2.1837868690490723, "[TT] Application of the GLI = Automatic observation of objects with large radiance differences (ocean colour and land vegetation)"]
-[4.39201545715332, 1.5575882196426392, "[FF] URL of the ROCSAT 2 ISUAL = http://sprg.ssl.berkeley.edu/sprite/ago96/isual/ROCSAT.html"]
-[9.099488258361816, 3.3712821006774902, "[FF] Upward Drift of the Plasma Blobs = Invoked away from the magnetic equator"]
-[7.502415657043457, 5.351919174194336, "[TT] Amplifier Technology of the TEMPEST-D = High-frequency microwave"]
-[5.99950647354126, 6.275175094604492, "[FF] Design Improvements of the SRC = New HK telemetry, backup timer"]
-[10.535079002380371, 4.95391845703125, "[TT] Carried Payload of the BeEagleSat = m-NLP (Multi-Needle Langmuir Probe)"]
-[5.101775646209717, 3.6679039001464844, "[TT] Hardware Source of the TBIRD = Existing commercial, telecommunications hardware products"]
-[9.326858520507812, 5.068235397338867, "[TT] Attitude Pointing Accuracy of the TanSat = \u2264 0.1\u00ba"]
-[3.271193742752075, 2.1874749660491943, "[TT] Instrument of the Sentinel-6 Michael Freilich = GNSS-RO"]
-[3.677180290222168, 6.506124973297119, "[TT] Antenna Type of the Antenna = Offset Feed Paraboloidal Reflector Antenna"]
-[9.399219512939453, 6.149878978729248, "[TT] Scan Angle of the OLS = \u00b156.25\u00ba"]
-[7.048482418060303, 7.819113731384277, "[TT] Tolerance of the Cube Corner Reflectors = \u00b10.5 arcseconds"]
-[7.5074028968811035, 3.161278247833252, "[FF] Blackouts of the Satellites = Multi-day periods when it is only in view of that geography during local nighttime"]
-[10.935800552368164, 7.559266090393066, "[TT] Swath Width of the AMSR-E = 1445 km"]
-[10.703583717346191, 6.533474445343018, "[FF] Multilayer Thickness (layer 90-133) of the Mirror = W/Si"]
-[11.39798355102539, 4.317587375640869, "[TT] Size of the CAPSat = 3U"]
-[14.264785766601562, 3.2878596782684326, "[TT] Mass of the PM = 14,800 kg"]
-[4.944519996643066, 1.3377659320831299, "[TT] Launch Date of the OptiSAR\u2122 Constellation = 2020-2021"]
-[7.578464508056641, -2.5018866062164307, "[TT] Launch Date of the GOLD = 28 Jan 2018"]
-[13.382742881774902, 6.822287082672119, "[TT] Power of the Spacecraft = 800 W"]
-[10.342522621154785, 5.369290351867676, "[FF] Heat Dissipating Packages of the TCS = Number of packages"]
-[10.764435768127441, 5.436801433563232, "[TT] Ion Composition of the PAP = H+, He+, O+"]
-[10.328911781311035, 4.539259433746338, "[TT] Reaction Wheels Capacity of the AOCS = 0.12 Nms"]
-[6.283395290374756, -0.25385934114456177, "[TT] Revisit Time of the WFI = 5 days"]
-[11.644147872924805, 4.661935329437256, "[TT] Diameter of the Didymos = 780 m"]
-[6.569221019744873, 4.600651741027832, "[FF] Components of the Support Segment = GUT, GMSF, GSL"]
-[5.570559024810791, 4.336650371551514, "[TT] SCOS-2000 Version of the Ground Segment = Version 5"]
-[5.2977213859558105, 0.5315858125686646, "[FF] Mission Date of the KazSTSAT = Unknown"]
-[4.918137550354004, -2.1342217922210693, "[TT] Ascender Weight of the Chang\u2019e-5 = 300 to 400 kg"]
-[9.136536598205566, 7.565689563751221, "[TT] Multispectral Imagery Resolution of the Satellogic = 1 meter"]
-[8.298215866088867, 7.343122482299805, "[TT] CMOS Image Sensors of the C3D Instrument = 2"]
-[8.385703086853027, 4.593345642089844, "[FF] Features of the XACT = Star tracker, sun sensor, inertial measurement unit (IMU), magnetometer, reaction wheels, torque rods, and processor"]
-[7.384121894836426, 2.4153494834899902, "[FF] Geographic Coverage of the POPACS = Data"]
-[4.56967306137085, 3.1941819190979004, "[TT] Location of the EDRS SCC = DLR in Oberpfaffenhofen"]
-[7.107525825500488, 5.249386310577393, "[TT] Radiation Hardened of the MCM (Multi-Tip-Module) = True"]
-[6.714183807373047, 2.2713398933410645, "[FF] URL of the TechnoSat = http://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=2986&context=smallsat"]
-[12.452295303344727, 0.5644164085388184, "[TT] Candidate Since of the PLATO = March 2013"]
-[6.484793663024902, 3.738927125930786, "[FF] Provision of Satellite Data of the Meteosat-1 = Continuous basis"]
-[13.353360176086426, 6.703155040740967, "[TT] Power Consumption of the Satellite = < 5000 W (BOL) and 4500 W (EOL) without EPPS operation in GEO"]
-[6.363842010498047, 5.5024333000183105, "[TT] Type of the DCS = Data collection"]
-[10.881026268005371, 3.573801279067993, "[TT] CubeSat Size of the SUNSTORM = 3U"]
-[6.6066107749938965, 3.1246728897094727, "[TT] Responsible Organization of the Real-time processing = Navy Fleet Numerical Weather Central"]
-[5.350426197052002, 6.596123218536377, "[TT] Data Distribution Capacity of the GS-CLASS interface = Over 2.5 TB per day per satellite"]
-[8.223311424255371, -0.150399312376976, "[FF] Sea Level Rise of the Greenland = 1 cm between 2011 and 2020"]
-[9.617423057556152, 8.26783275604248, "[TT] Field of View of the HXCP = \u00b115\u00ba"]
-[5.37584114074707, 8.011968612670898, "[TT] Oscillation Frequency of the CVX-1 = < 13 Hz"]
-[4.257053852081299, 7.325930595397949, "[FF] Ka-band Advantages of the SARAL/AltiKa = Reduction of ionosphere effects, smaller footprint, better horizontal resolution, higher vertical resolution"]
-[4.485733985900879, 5.303685665130615, "[TT] Manufacturer of the GOMX-1 = GomSpace ApS of Aalborg, Denmark"]
-[10.16824722290039, 8.064958572387695, "[TT] Telescope VIS Focal Length of the MVIRI = 3650 mm"]
-[8.772366523742676, 7.328590393066406, "[TT] L1 Detectors Thickness of the HIT = 24 \u00b5m"]
-[10.769172668457031, 5.5867018699646, "[FF] Components of the TCS = FSSM (Flexible Second Surface Mirror coatings), MLIs (Multi-Layer Insulation Blankets), Germanium-coated black Kapton foil, black paint, aluminized tapes/low emissivity surface treatments, thermal doublers, interface fillers and thermal washers"]
-[13.512392044067383, 2.947641611099243, "[TT] GCP Density of the GCP Extraction Approach = About 450 GCP per 1000 km2"]
-[5.298314571380615, 7.603541374206543, "[FF] Transmit Signal Distribution of the APDN (Azimuth Power Dividing Networks) = Distributes low power transmit signal pulses to T/R modules"]
-[8.935089111328125, 4.357282638549805, "[FF] Processing Algorithm of the Fine Sun Sensors = Logic added to improve performance"]
-[6.337108612060547, 0.18899653851985931, "[TT] Afterglow Period Duration of the ABEX = Hours to months"]
-[6.347961902618408, 5.087337493896484, "[FF] Computes the complex correlation between the v-pol and h-pol channels of the Digital processor = Yielding the 3rd and 4th Stokes parameters essential to OSVW retrievals"]
-[11.438009262084961, 0.6912410259246826, "[TT] Planet Size of the AU Mic = About as large as Neptune"]
-[9.667108535766602, 4.870400428771973, "[TT] Stabilization of the JAWSAT = Three-axis"]
-[7.353029727935791, 5.130800724029541, "[FF] Function of the Coherency Filter = Identify flashes by reviewing the remaining events"]
-[6.587678909301758, 6.058340072631836, "[TT] Quantity of the Optical Intersatellite Link units (OISLs) = 2"]
-[4.683061599731445, 0.623916506767273, "[TT] Launch Date of the GOES-R = November 19, 2016"]
-[4.959616184234619, 3.9824094772338867, "[FF] Bi-directional sharing of the TT&C Services = Enhances effectiveness and reduces the risk for both agencies"]
-[8.780258178710938, 2.9626269340515137, "[FF] Visibility of the Transient Luminous Events = Rarely seen from the ground"]
-[6.977540969848633, 4.295689582824707, "[FF] Unknown of the ISIR = Unknown"]
-[9.26331615447998, 8.210749626159668, "[TT] Number of Bands of the Telescope = 6"]
-[9.568758964538574, 5.672000885009766, "[TT] Range of the Rotation Mechanism = 180\u00ba"]
-[4.5564188957214355, 5.964241027832031, "[FF] Alert Message Content of the 406 MHz devices = Identification code"]
-[5.471241474151611, 2.2134134769439697, "[TT] Leader of the GRNS = David Lawrence"]
-[5.209204196929932, 7.153874397277832, "[TT] Data Streams of the Baseband Processor = Two 110 Mbit/s TDMA/DAMA data streams assignable in increments of 64 kbit/s"]
-[8.973509788513184, 7.589358806610107, "[TT] High Spatial Resolution of the AMI = 0.5-1.0 km for VIS and 2 km for the infrared channels"]
-[10.993133544921875, 5.070693016052246, "[TT] Number of CCRs of the LARES-2 = 303"]
-[11.25599193572998, 2.8277649879455566, "[TT] Fluxgate Magnetometer Mass of the Microsatellite = 3.6 kg"]
-[5.81657075881958, 7.153329849243164, "[TT] Data Rate of the GVAR = 31 Mbit/s"]
-[12.034420013427734, 3.621544361114502, "[TT] MEOP of the Main Tank = 31 bar"]
-[3.974900484085083, 6.362661838531494, "[TT] Antenna Configuration of the Satellite = Two nadir antennas"]
-[8.832575798034668, 3.688685655593872, "[TT] Ways to Measure Space Radiation of the DIME = 6"]
-[8.181035041809082, -1.054076075553894, "[TT] Surface Height Measurements Interval of the ICESat-2 = Every 28 inches (70 cm)"]
-[13.792594909667969, 3.659520387649536, "[TT] Mass of the Antenna = 183 kg"]
-[3.797511577606201, 4.275951385498047, "[FF] Marine Winds Monitoring Capability of the RADARSAT-1 = SAR derived marine winds"]
-[5.5149335861206055, 2.5930097103118896, "[FF] Operator of the SSRMS = JAXA astronaut Kimiya Yui"]
-[11.277641296386719, 0.9711572527885437, "[TT] Feasibility Study Phase End Date of the LISA = January 2020"]
-[6.802492141723633, 4.0639328956604, "[FF] Purpose of the GAMANET = Maximize coverage and throughput of each space platform"]
-[6.668945789337158, 0.2874259054660797, "[TT] Expected Coolant Exhaustion of the Herschel = March 2013"]
-[8.158549308776855, 4.470232009887695, "[FF] Purpose of the S-WPIA = Measure the wave-particle interactions"]
-[9.536238670349121, 8.204764366149902, "[TT] Field of View of the Cameras = 24\u00ba x 96\u00ba"]
-[4.8938422203063965, 1.7740141153335571, "[FF] Integration and Testing of the Gokturk-2 = TAI's facilities"]
-[8.084047317504883, 7.546004772186279, "[TT] Source Data Rate of the MS CCD detector module = 4 x 240 Mbit/s"]
-[10.519360542297363, 2.89223313331604, "[FF] On-board GPS of the Nanosatellites = Capability"]
-[11.44975471496582, 3.4998605251312256, "[FF] Type of the NEXT-C = Solar electric ion propulsion system"]
-[10.742216110229492, 0.9267753958702087, "[FF] Formation Hypotheses of the Hot Jupiters = Disk interaction, Gravity of other planets"]
-[12.134968757629395, -0.22564230859279633, "[TT] Data Analysis of the TESS = Determine how bright the burst was"]
-[8.761092185974121, 1.9428383111953735, "[TT] Speed of the Easterly Winds = 2.5 to 5 m/s"]
-[5.520101547241211, 5.475752830505371, "[TT] Onboard Recorder of the Satellite = No"]
-[9.952606201171875, 2.262408494949341, "[FF] Ability of the NuSTAR = Look closer to home to study our sun"]
-[5.11863374710083, 1.1624661684036255, "[TT] Launch Date of the NPP (NPOESS Preparatory Project) = October 28, 2011"]
-[7.516602039337158, 4.9866228103637695, "[FF] Components of the MiRaTA = Batteries, a radio, a computer, instruments, wheels, folded solar panels, antennas"]
-[9.246033668518066, 1.8593560457229614, "[TT] Tethered of the Harpoon = Yes"]
-[12.25407600402832, -0.20700207352638245, "[TT] Image Collection Frequency of the TESS = Every 30 minutes"]
-[13.466205596923828, 5.973557949066162, "[FF] Power Requirement of the High-power missions = High-voltage photovoltaic generation"]
-[11.828469276428223, 3.3680572509765625, "[TT] Quantity of the Mono Propellant Thrusters (MPT) = 8 on the CSC"]
-[6.178177356719971, 6.40097713470459, "[TT] System Latency of the DSCOVR = No more than 5 minutes"]
-[4.59041690826416, 3.981987476348877, "[TT] Positioning Services of the Galileo = OS (Open Service), SoL (Safety-of-Life) service, CS (Commercial Service), PRS (Public Regulated Service)"]
-[4.569085121154785, 3.0561251640319824, "[FF] Location of the Hertz Chamber = ESA's ESTEC technical heart in the Netherlands"]
-[9.61242389678955, 0.8415346145629883, "[TT] Operating Distance from the Sun of the Rosetta = Over 800 million km"]
-[5.173659324645996, -1.193074107170105, "[TT] Launch Option of the Kondor = Low-cost"]
-[5.0338239669799805, 2.0878028869628906, "[TT] Mission Status of the TechnoSat = Operational (extended)"]
-[7.796649932861328, 2.3977272510528564, "[FF] Applications of the MiniRad = Improved weather forecasting, better crop yields, safer and more efficient route planning for aviation and shipping"]
-[10.386199951171875, 1.4736003875732422, "[FF] Star Formation of the The Horse and the Dragon = Teeming with star formation, 10 to 100 times more massive than most galaxies at the same epoch"]
-[4.45952844619751, 0.5350203514099121, "[TT] Launch Date of the HTV-9 = 20 May 2020"]
-[10.057056427001953, 3.226356029510498, "[FF] Project Role of the Dragsail = CubeSat development and de-orbit technology development"]
-[8.56833553314209, 7.072183609008789, "[FF] Detector of the Image Quality = 2 x 2 pixels"]
-[9.416970252990723, 7.335134983062744, "[TT] Resolution of the EOC = 6.6 m (Pan)"]
-[8.069814682006836, 2.0910964012145996, "[TT] Swath Width of the Ocean and Land Color Instrument = 1270 km"]
-[5.711333751678467, 6.30990743637085, "[TT] Capacity of the Solid-State Recorder = 58.9 GB"]
-[11.204819679260254, 4.736739158630371, "[TT] Depth of the Holes = 2,450 meters"]
-[3.423504114151001, 5.01311731338501, "[TT] Polarization of the ICEYE SAR (Synthetic Aperture Radar) = Circular"]
-[10.18127727508545, 3.0879600048065186, "[FF] Number of CubeSats of the QB50 Project = 50"]
-[10.303899765014648, 5.426722049713135, "[TT] Enclosure of the CVX cell = Three-layer thermostat"]
-[7.329272270202637, 4.871067523956299, "[FF] Purpose of the VBS = Eliminating false or erroneous signals"]
-[5.969305992126465, -2.3231403827667236, "[TT] Orbit Altitude of the Kondor-E1 = 499 km x 521 km"]
-[5.747715950012207, 7.640902042388916, "[TT] Duration Limit of the High power VLF transmission = Less than 30 minutes"]
-[3.8425228595733643, 6.204629898071289, "[TT] Mission of the Helical Antenna = PROBA-3"]
-[8.638285636901855, 7.113647937774658, "[FF] Pixel Size Requirement of the Optical System = Small"]
-[13.309134483337402, 5.176767349243164, "[TT] Mass of the Solar Array = < 40 kg"]
-[5.547487258911133, 3.0051443576812744, "[TT] Host of the OSIRISv2 = BiROS satellite"]
-[4.292479991912842, 1.9662407636642456, "[FF] Launch Vehicle of the G\u00f6kt\u00fcrk-1 = Europe's new Vega small-satellite launch vehicle"]
-[7.054895401000977, 8.186477661132812, "[TT] Signal-to-Noise Ratio of the SNR = \u2265 100"]
-[5.876057147979736, -0.4309254288673401, "[TT] Mission Duration of the WINDS/Kizuna satellite = 5 years"]
-[8.63473129272461, 1.103850245475769, "[TT] Data Collection Duration of the Aquarius = At least three years"]
-[13.803074836730957, 3.1518921852111816, "[TT] Payload Mass of the TCS = 7.26 kg"]
-[9.980949401855469, 1.6016342639923096, "[FF] Purpose of the Tereza's Computer Model = Simulate the various perturbations that escaping stars in the cluster might feel during their hundreds of millions of years in space"]
-[3.1856296062469482, 5.080286026000977, "[TT] Gridding Size of the SAR Image = 2000 x 2000"]
-[8.49092960357666, 4.764796257019043, "[TT] Manufacturer of the Star Tracker = Sodern"]
-[13.579937934875488, 1.7779417037963867, "[TT] Cargo Capacity of the Tianzhou-2 = 4.69 tons"]
-[5.967800140380859, 7.058437347412109, "[TT] Data Rate of the DORIS = 4 kbit/s"]
-[7.629150390625, 8.97634506225586, "[TT] Polarization Angle of the Band 5 = 0/60/120 \u00ba"]
-[10.177607536315918, 3.2568039894104004, "[FF] Proximity to Payload of the CubeSat = Net payload"]
-[10.652484893798828, 6.827547073364258, "[TT] Transmission Efficiency for Receive Path of the Triple Mirror = 97%"]
-[8.629691123962402, 4.833960056304932, "[TT] Type of the Star Camera = Multi-head"]
-[5.241390705108643, 1.8779865503311157, "[TT] Mission Status of the OrbView-4 = Cancelled"]
-[5.755030155181885, 8.058321952819824, "[TT] Rotating Mode Test Frequency of the MicroSCOPE = fep \u2248 1.0 x 10-3 Hz"]
-[5.205182075500488, 2.834165573120117, "[TT] Ownership of the Deimos-2 = Elecnor"]
-[10.438608169555664, 7.80539083480835, "[TT] Telescope Diameter of the Euclid = 1.2 m"]
-[6.138920783996582, 2.526385545730591, "[FF] Responsive Exploitation of Space of the HAUSat-2 = Low-cost"]
-[9.938544273376465, 6.374664783477783, "[TT] Spatial Resolution of the NuSTAR = Approximately 10 times greater than previous missions"]
-[12.164750099182129, -0.2431129664182663, "[TT] Data Transmission of the TESS-L5 = 6 megabits per second"]
-[11.604789733886719, 6.547698497772217, "[FF] Threshold Energy of the LDT = Unknown"]
-[10.767043113708496, 6.430503845214844, "[FF] Components of the NAOMI family of optical instruments = Silicon carbide (SiC) optics and structures, multiple-line detectors, integrated focal planes and ultra-compact optical configurations"]
-[11.807560920715332, 6.762444019317627, "[TT] Energy Range of the GIM = 200 eV/q to 25 keV/q"]
-[10.097051620483398, -2.6880760192871094, "[TT] Power (data retention) of the Astrium MMFU NAND-Flash SDR-SDRAM = < 29 W (0 W)"]
-[8.524767875671387, 8.803367614746094, "[TT] Fringe Distortions for Monochromatic Light of the SHS = Provide a measure of the grating figure errors"]
-[6.17218017578125, 3.892186164855957, "[FF] Leads of the Project System Engineer = Mission-level engineering efforts"]
-[5.71224308013916, 3.60910964012146, "[FF] Mission Result of the PSLV-C38 = All 31 satellites separated"]
-[9.322245597839355, 7.194784164428711, "[TT] Resolution of the FY-4 GLI = 7.8 km"]
-[7.730662822723389, 5.0398969650268555, "[TT] Mounting Location of the Fine Lateral and Longitudinal Sensor (FLLS) = OSC"]
-[7.691391944885254, 9.378993034362793, "[TT] Center Wavelength of the Band No. 4 = 504.96 nm"]
-[5.084397315979004, 3.2152717113494873, "[TT] Manufacturer of the Maeva Hinges = CNES"]
-[5.4802422523498535, 3.867126703262329, "[TT] Contacted Satellites of the CYGNSS = Eight"]
-[8.870288848876953, 3.367473840713501, "[FF] Location of the Equatorial ionization anomaly = Just north and south of the equator"]
-[7.963747978210449, 8.601635932922363, "[TT] Wavelength Detection Range of the Mapping Channel = 0.25 \u00b5m to 1 \u00b5m"]
-[5.449116230010986, 6.445900917053223, "[TT] Capacity of the Onboard Data Storage = 8 GByte"]
-[9.634761810302734, 8.344429016113281, "[TT] Field of View (FOV) of the Dosimeter Suite = 44\u00b0 and 42\u00b0"]
-[6.145971775054932, 6.425642490386963, "[TT] Revisit Rate of the Cluster 3 = Less than one hour"]
-[3.978419542312622, 4.118040084838867, "[FF] Mission of the PhiSat-1 = Monitor polar ice and soil moisture, test intersatellite communication systems"]
-[6.843113422393799, 1.8850852251052856, "[FF] URL of the Window Observational Research Facility (WORF) = http://www.nasa.gov/mission_pages/station/science/experiments/WORF.html#description"]
-[5.9936323165893555, 5.058228492736816, "[FF] Responsible for of the CSP = Core subsystem communication"]
-[8.136908531188965, -1.0696934461593628, "[FF] Detection Capability of the ICESat-2 = Ponds half the size of the Lincoln Memorial Reflecting Pool"]
-[7.016053199768066, 4.049363136291504, "[TT] Sensor Quantity of the DMSP Block 5D-3 = 6"]
-[4.891282558441162, -0.5865012407302856, "[FF] Development Date of the SLATS = June 2-8, 2013"]
-[12.053770065307617, 6.240098476409912, "[TT] Antihelium Candidate to Helium Rejection of the AMS-02 = One in a billion"]
-[5.787394046783447, 5.154208660125732, "[FF] Interface of the ADCS = Can interface with thrusters"]
-[4.738884925842285, 7.383613586425781, "[TT] Data Rate of the TREX-823 X-band transmitter = 25, 50 or 100 Mbit/s (selectable)"]
-[6.981335639953613, 4.093497276306152, "[FF] Purpose of the Formation Flying System (FFS) = Permit to autonomously perform, with the required strict accuracy, the maneuvers necessary for accomplishing mission scientific and technology demonstration goals, guaranteeing at the same time the mission safety"]
-[7.5780415534973145, 8.900909423828125, "[TT] Spectral Band (VIS channel) of the OLS = 0.4 - 1.1 \u00b5m"]
-[4.878767490386963, -0.2282305210828781, "[TT] Launch Time of the SpaceX CRS-13 = 15:36 GMT"]
-[7.088902950286865, 7.1791605949401855, "[TT] Wavelength of the Laser Head Unit (LHU) = 1064 nm"]
-[10.493484497070312, 5.835681915283203, "[TT] Temperature Range of the ANUSat = 10\u00ba C \u2013 30\u00ba C"]
-[11.211026191711426, 2.848003387451172, "[TT] Mass of the NanoRacks Kaber Microsat Deployer = 10 kg"]
-[8.992448806762695, 6.98172664642334, "[TT] Sensor of the WorldView-3 = CAVIS"]
-[9.437210083007812, 3.606863021850586, "[FF] Electric Field Property of the IVM = Direction parallel to the Earth's magnetic field is an electric equipotential for horizontal scales greater than 25 km"]
-[7.683630466461182, 8.732124328613281, "[TT] Number of Spectral Bands of the ERIP = 7"]
-[5.359983921051025, 6.986863136291504, "[TT] Data Transmission Rate of the GOMX-3 = 19.2 kbit/s"]
-[10.996810913085938, 6.110198020935059, "[TT] Material Used for Signal Amplification of the ATMS = Indium Phosphide"]
-[5.451136112213135, 6.109866619110107, "[TT] Microcontroller RAM of the CC430 SoC = 4 kB"]
-[11.973636627197266, 4.946396827697754, "[TT] Dimensions of the SGR-ReSI = Approx 300 x 160 x 30 mm"]
-[9.039901733398438, 4.830121994018555, "[TT] Attempted ?V Maneuver of the Satellite = 7 m/s"]
-[9.47909927368164, -1.0655639171600342, "[TT] Operational Position of the GOES-S = GOES-WEST at 137.2\u00b0 West"]
-[10.00832462310791, -0.07338842004537582, "[TT] Proximity to Sentinel-3B of the CDN2 Site = 300 m west"]
-[6.804642677307129, 4.65540885925293, "[FF] Mission Objective of the FASTRAC = Perform on-orbit real-time GPS relative navigation between satellites"]
-[8.990086555480957, 5.634035110473633, "[TT] Pointing Knowledge Accuracy of the ACS = < 10 arcsec"]
-[3.7676842212677, 7.160157203674316, "[TT] Directive Gain of the Antenna = 37.8 dBi at \u03b8=0"]
-[9.080199241638184, 5.024149417877197, "[TT] Emergency Maneuvers of the AlSat-2A = 2"]
-[9.271750450134277, 6.9091339111328125, "[TT] Processed Imagery of the Image Location Knowledge = < 100 m"]
-[3.8684403896331787, 6.4892425537109375, "[TT] Antenna Type of the CTECS-A = Custom"]
-[3.9958486557006836, 2.042280435562134, "[TT] Launch Vehicle of the ADEOS = H-II"]
-[4.474970817565918, 7.79018497467041, "[TT] Downlink Frequency of the TT&C Data = 2089 MHz"]
-[10.563298225402832, 6.509344100952148, "[TT] Mirror Modules of the eROSITA = Seven identical Wolter-1 mirror modules"]
-[4.784111022949219, 2.315352439880371, "[FF] Launch Date of the Eutelsat Quantum = 26 July 2021"]
-[4.46981143951416, 7.612565517425537, "[TT] Frequency Band of the COM = VHF/UHF"]
-[5.931930065155029, 2.5354602336883545, "[FF] Objectives of the YouthSat = Provide hands-on experience to student in space experiments and data analysis, Study solar radiation, Create a common platform for aerospace students across the world to jointly conduct experiments in space"]
-[4.446900367736816, 2.282895088195801, "[TT] Launch Provider of the NPP = ULA"]
-[11.578241348266602, 3.5723094940185547, "[TT] Firing Duration of the Micronozzle = 10 s x 3"]
-[12.49386215209961, 3.185103178024292, "[TT] Propellant Mass of the Propulsion Subsystem = 2.3 kg"]
-[6.000207424163818, 4.875228404998779, "[TT] Software of the OBC = FCS (Flight Control Software)"]
-[7.423694133758545, 2.1521518230438232, "[FF] Focus of the FLEX mission = Estimation of fluorescence emission by terrestrial vegetation on a global scale with high spatial resolution and spectral resolution"]
-[11.131485939025879, 1.3156992197036743, "[FF] Detector Type of the LISA = Gravitational Waves"]
-[7.8977742195129395, 9.21265983581543, "[TT] Wavelength of the NPS = 427.8nm and 630nm"]
-[7.635061740875244, 6.424463272094727, "[TT] Image Acquisition Frequency of the AutoNav = About once per week"]
-[4.499350070953369, -0.8911313414573669, "[TT] First Signal Reception Date of the Pico Dragon = Nov. 20, 2013"]
-[6.37518835067749, -0.3175291121006012, "[TT] Operation of the GLM = 24 hours"]
-[7.234511375427246, 9.183212280273438, "[TT] Estimated Total Conductance of Bipods of the OTA = 0.015 W/K"]
-[5.717329502105713, 6.126233100891113, "[FF] Data Storage Method of the Tape Recorders = Encrypted, digital format"]
-[10.25285816192627, 5.932430267333984, "[TT] Temperature Resolution at 220 K of the VNIR, MWIR1, MWIR2, TIR1, TIR2 = \u2264 0.50 K"]
-[3.302729845046997, 5.728868007659912, "[TT] Panel Quantity for a Panel of the SAR Antenna = 4"]
-[5.240215301513672, 0.7864063382148743, "[FF] Launch Date of the Indian rocket = April 15, 2017"]
-[11.1103515625, 0.614378035068512, "[TT] Partner Levels of the Planet Orbit = Gold and Platinum"]
-[9.881101608276367, 7.333407878875732, "[TT] Ground Sampling Distance of the TET-1 = 160 m"]
-[11.094972610473633, 5.54611873626709, "[FF] Production Method of the Bally's 3-D quartz fiber material = Woven using a newly developed version of a \"Jacquard loom\""]
-[7.118454933166504, 2.859546184539795, "[TT] Mission Operations Control Center (MOCC) of the MethaneSAT = Developed and managed by Rocket Lab"]
-[9.739142417907715, 4.153830051422119, "[FF] Safety Regulations Compliance of the AMS-02 = Fringe magnetic fields on the ISS"]
-[3.412255048751831, -0.9279360175132751, "[TT] Orbit Type of the AlSat-2 = Sun-synchronous"]
-[6.242180347442627, 3.907973289489746, "[TT] Avionics Architecture of the TechEdSat = SPA (Space Plug-and-Play Avionics)"]
-[10.942194938659668, 7.566947937011719, "[TT] Swath Width of the EOC = 17 km"]
-[7.1016011238098145, 2.89764404296875, "[TT] Operator of the MethaneSAT = MethaneSAT LLC"]
-[4.102137088775635, 6.372503757476807, "[FF] Experiment of the GeReLEO Smart Antenna = Test"]
-[7.9806976318359375, 0.15855732560157776, "[FF] Purpose of the GRACE-FO = Measuring changes in Earth's gravity field, tracking water movement and surface mass changes"]
-[10.387301445007324, 6.793548583984375, "[TT] Alignment Requirement of the Triple mirror vertex = 100 \u00b5m"]
-[8.985075950622559, 7.024171829223633, "[TT] Resolution of the FGM = \u00b10.06 @ maximum of the dynamics"]
-[14.109829902648926, 7.188501358032227, "[TT] Bus Voltage of the PCDU = 28 V"]
-[3.77248477935791, 4.477730751037598, "[FF] Image Acquisition Success Rate of the RADARSAT-2 = Maintained at a high level"]
-[4.45933723449707, 0.6073624491691589, "[TT] Release Date of the HTV-6/Kounotori-6 = January 23, 2017"]
-[10.178019523620605, 5.661989212036133, "[FF] CCD Temperature of the FPA = Within Budget"]
-[10.870172500610352, -0.300321489572525, "[TT] Bistatic Recordings of the TanDEM-X = Since June 2020"]
-[14.301377296447754, 3.130051851272583, "[TT] Mass of the TabletSat-Aurora = 25 kg"]
-[10.959417343139648, 7.536844253540039, "[TT] Swath width (km) of the SMMR = 10.7"]
-[6.508927822113037, 6.325138568878174, "[TT] Number of Tapes of the MOMS-2P = 19"]
-[8.766936302185059, 4.819700241088867, "[TT] Tilt of the Star Tracker = 87 \u00b5rad"]
-[5.374452114105225, 5.344160556793213, "[FF] Interface Types of the Satellite Bus = SpaceWire, RS422/485, CAN-Bus"]
-[8.482712745666504, 1.9318147897720337, "[FF] Required Precision of the Cloud Top Pressure = 100"]
-[9.050690650939941, 9.376164436340332, "[TT] Size of the TANSO-CAI = 0.5 m x 0.4 m x 0.5 m"]
-[10.15485668182373, -2.7486443519592285, "[TT] Device package of the SLC NAND-FMM = Quad Die Stack TSOP I"]
-[7.253396987915039, 5.2083659172058105, "[FF] RF Labs Equipment of the CesiumAstro = High performance test equipment, multiple RF chambers, antenna ranges, and environmental test stands"]
-[10.350347518920898, 5.779999732971191, "[TT] Temperature of the Shape-Setting Process = 550\u00baC"]
-[9.542755126953125, 8.342195510864258, "[TT] Total FOV of the Cameras = 2300 square degrees"]
-[10.030596733093262, -1.5562385320663452, "[TT] Inclination of the Orbit = 98.28\u00ba"]
-[2.9029016494750977, 4.459022045135498, "[TT] Local Displacement of the PALSAR-2 = Up to 30 cm in the satellite-ground direction"]
-[5.931480884552002, 6.999373912811279, "[TT] Data Samples of the Experiment Data = Roughly 1.3 million"]
-[3.266049861907959, 4.965607643127441, "[TT] Data Tapes of the SAR = 516 film reels"]
-[10.724958419799805, 5.292508125305176, "[FF] Charge-exchange emission lines and normalized effective area of the CuPID = Unknown"]
-[10.098320007324219, 3.1836447715759277, "[FF] Payload of the Cubesats = Scientific Persuasions"]
-[8.972160339355469, 4.413190841674805, "[TT] Field of View of the Sun Sensor Device = \u00b160\u00ba"]
-[5.6072540283203125, 8.244293212890625, "[FF] Bandwidth of the Dual-channel Receiver Unit (DRU) = Variable"]
-[8.371840476989746, 8.216386795043945, "[TT] Pan Pixels of the Spectral bands = 12,000 pixels"]
-[8.701739311218262, 5.221489429473877, "[FF] Pointing Control System of the Telescope = Instrument sends corrections to put the science target precisely in the correct location within the instrument's field of view"]
-[8.993022918701172, 5.312434196472168, "[TT] Extended Range Testing Distance of the GomX-4A and GomX-4B = Up to 4500 km"]
-[6.497857093811035, -0.12536220252513885, "[FF] Various Times of the Notional Pass Time = 12:00 pm, 1:30 pm, 12:00 am, 1:30 am, 8:00 am, 2:00 pm, 11:30 am"]
-[8.252165794372559, 4.519541263580322, "[FF] Transfer Function of the LARES = Not specified"]
-[6.787852764129639, 6.586501121520996, "[FF] Laser of the EDRS-A = Ready to fly"]
-[7.687734603881836, 5.30875825881958, "[FF] Precision of the Tracking Systems = Unknown"]
-[8.319731712341309, 5.528340816497803, "[TT] CH4 Relative Accuracy of the GOSAT = 2%"]
-[3.8160901069641113, 1.176823616027832, "[TT] Landing Attempt of the Falcon 9 first stage = Mostly successful"]
-[5.839449405670166, 3.3711414337158203, "[TT] Total Cost of the Satellogic = $20 million in total per year"]
-[16.487472534179688, 3.5715200901031494, "[FF] Announcement Date of the OneWeb = January 15, 2015"]
-[9.805355072021484, 7.035070419311523, "[TT] Spatial Resolution of the LIS = 4km"]
-[10.81775951385498, 7.377103805541992, "[TT] Width of the Umbra = 50-100 km"]
-[6.199037551879883, 5.489392280578613, "[FF] Control System of the CUTE-1.7 = PDA-Controlled"]
-[7.9193291664123535, 5.714943885803223, "[FF] Fragile Component of the Photomultiplier = Special care will have to be paid in the choice of the model, or in its accommodation"]
-[5.021972179412842, 3.230586290359497, "[FF] Manufacturer of the Resurs-P1 = NTs OMZ (Research Center for Earth Operative Monitoring)"]
-[11.28779411315918, 0.9863914847373962, "[TT] Mission Lifetime Cycle Phase of the LISA = Phase A"]
-[3.8577826023101807, -1.1421715021133423, "[FF] Orbit of the Queqiao = Halo orbit"]
-[6.925478935241699, 2.9140570163726807, "[FF] Conference Date of the Microwave Remote Sensing = Sept. 20\u202224, 2004"]
-[3.8293051719665527, 4.579437255859375, "[FF] Operation with MUIR radar of the Receiver = Yes"]
-[10.18614673614502, 3.0794684886932373, "[TT] Deployment Mission Count of the CubeSat = 13"]
-[5.017706394195557, 3.560206651687622, "[TT] Satellite Subsystems and Components Source of the SpaceLink = U.S. suppliers"]
-[11.906266212463379, 3.060481071472168, "[TT] Delta V of the MTM CPS = 68 m/s"]
-[13.856806755065918, 3.2187435626983643, "[TT] Mass of the NanoACE = 5.2 kg"]
-[6.677783966064453, 1.6679199934005737, "[FF] Journal of the ASASSN-19bt = The Astrophysical Journal"]
-[4.97944450378418, 0.429905503988266, "[TT] Declaration Date of the STRaND-1 = March 07, 2013"]
-[9.344985008239746, 3.2069733142852783, "[FF] Function of the Collector arrays = Allow solar wind particles to be deeply embedded within the material"]
-[7.451724052429199, 8.375685691833496, "[TT] Number of Available Rows per Filter Band of the QWIP Array = 32"]
-[8.647122383117676, 3.6263952255249023, "[FF] Mission of the Spectrometer Telescope = Solar Orbiter"]
-[10.427058219909668, 5.457201957702637, "[TT] Heat Rejection (Parasitic) of the TCS = Up to 300 W"]
-[4.462444305419922, 4.209373474121094, "[TT] Supported Signals of the GTR = Galileo (L1 and E5) and GPS"]
-[6.569760799407959, -0.464825838804245, "[TT] Period of the ANUSat = ~90 minutes"]
-[4.022924900054932, 7.222822189331055, "[TT] Gain of the Ku-band Antenna = Greater than 42.5dB"]
-[13.46427059173584, 6.751932621002197, "[TT] S/C Power of the QuikTOMS spacecraft = 228 W EOL"]
-[3.675624370574951, 6.636411190032959, "[TT] Redundancy of the Altimeter Antenna = Yes"]
-[7.977602958679199, 5.523808002471924, "[FF] Sequence Steps of the AVGS = Image 1 is taken at 808 nm, Image 2 is taken at 850 nm, A threshold is taken of the differential image, A centroid is found for each spot in the image, Tracking windows are established, Position (azimuth/elevation and range); attitude (roll, pitch, yaw)"]
-[5.200805187225342, 8.48024845123291, "[TT] Spectral range of the Microwave System = 6.9, 10.6, 18.7, 23.8, 31, 36.5, 42, 48, 52.3-57.0, 89, 183.31 (GHz)"]
-[11.346186637878418, 5.851375102996826, "[TT] Structure Material of the GNB = Al 6061-T6"]
-[11.500420570373535, 5.78090763092041, "[TT] Structure of the TARANIS = Four vertical struts and four lateral panels made of alloy honeycomb"]
-[8.724703788757324, 7.517448902130127, "[TT] Image Sensor Resolution of the CMV4000 = 2048 x 2048 pixels"]
-[10.463672637939453, 1.5867708921432495, "[FF] Luminosity of the AGN = More active than the larger galaxy's central black hole"]
-[3.4497132301330566, 5.427072048187256, "[TT] Deployment of the SAR Antenna = Automatic"]
-[9.023921966552734, 5.684562683105469, "[TT] Achievable of the Pointing Accuracies = < 1arcsec"]
-[6.460327625274658, -1.3028757572174072, "[FF] Contributor to Map of the GRACE = Unknown"]
-[7.3881988525390625, 5.687772750854492, "[FF] Sampling Method of the Science Question Methodology = In-situ instruments"]
-[5.414958477020264, 4.373599052429199, "[TT] Ground System of the ORS-6 = EGS (Enterprise Ground System)"]
-[5.0946455001831055, 0.4416959881782532, "[TT] Launch Date of the TSIS-1 = 15 December 2017"]
-[13.456710815429688, 6.8538970947265625, "[TT] Maximum Electrical Power Production of the SAWs = 11.2 kW"]
-[9.721750259399414, 4.511839389801025, "[FF] Attitude Control of the XI-IV = Passive stabilization of a permanent magnet"]
-[7.721218109130859, 6.820420265197754, "[TT] Exposure Time of the NISP Photometer = About 100 seconds per filter"]
-[11.122742652893066, 1.5497738122940063, "[TT] Structure Mass of the Starshine-3 = 91 kg"]
-[10.431370735168457, 2.8583667278289795, "[TT] Communication Protocol of the NEMO-AM = SFL's nanosatellite protocol"]
-[4.931669235229492, 1.5139378309249878, "[TT] Operation End Date of the Tatiana-1 = March 7, 2007"]
-[3.535557508468628, 5.2224884033203125, "[FF] Components of the SARR = Two dual-conversion receivers, two 4.0 W phase modulated L-band transmitters, two Power, Telemetry and Command (PTC) units"]
-[9.304975509643555, -0.5337303876876831, "[TT] Orbital altitude of the MEOSAR Constellation = 20,180 km"]
-[5.793582916259766, -0.8055147528648376, "[TT] Planned Total In-Orbit Lifetime of the GHOSt satellites = Just over 5 years"]
-[8.668012619018555, 8.743274688720703, "[TT] Grating Order of the Spectrometer = 3"]
-[3.9056389331817627, 3.4960057735443115, "[FF] Name of the GSTB-V1 = Galileo System Test Bed-V1"]
-[7.6190009117126465, 0.9698391556739807, "[FF] Development Start Date of the Airborne Lunar Spectral Irradiance (Air-LUSI) = 28 October 2020"]
-[4.989269733428955, 2.9227280616760254, "[FF] Manufacturer of the MightySat II.1 = General Dynamics"]
-[11.334991455078125, 2.7508742809295654, "[TT] Total Mass of the Microsatellite = 20.5 kg"]
-[4.076748847961426, 4.337225914001465, "[FF] Approach for Operations of the RADARSAT-2 = Multi-mission"]
-[6.75715446472168, -0.5357943773269653, "[TT] Time to Point to the Sun of the TSUBAME = 33873 seconds after the separation"]
-[8.354928970336914, 8.332706451416016, "[TT] Spectral Resolution of the CHIPS = Near 170 \u00c5"]
-[3.3959805965423584, 6.425482749938965, "[TT] Antenna Size of the HDR Terminal = 3.4 m"]
-[6.546289920806885, -0.4205327332019806, "[TT] Repeat Period of the CZI = 7 days"]
-[4.654470920562744, 1.8463131189346313, "[TT] Satellite Launches Planned of the RCM (RADARSAT Constellation Mission) = 2018"]
-[14.064593315124512, 3.9398093223571777, "[TT] Instrument Mass of the NSCAT = 280 kg"]
-[8.96576976776123, 7.6534342765808105, "[TT] Pan of the Pushbroom imager = 1.45 m"]
-[9.667140007019043, 4.70255708694458, "[TT] Attitude Control of the MicroMAS-2 = Dual-spinner local-vertical local-horizontal"]
-[3.6606178283691406, 2.8170647621154785, "[FF] Atomic Clocks of the Indian Regional Navigation Satellite System (IRNSS) = Break"]
-[8.913039207458496, 7.490589618682861, "[TT] Photon Detector Surface Area of the REM = 150 mm2"]
-[6.673929214477539, 1.889957308769226, "[FF] URL of the International Space Station Agricultural Camera (ISSAC) = http://www.nd.gov/gis/news/2011pres/olsen-kim-keynote2.pdf"]
-[14.246013641357422, 3.348613739013672, "[TT] Housing Mass of the MuREM = 0.5 kg"]
-[5.2966837882995605, 3.908308982849121, "[FF] Planned Satellite Launches of the ICEYE = At least eight more satellites in the coming year"]
-[5.747189521789551, -0.8216811418533325, "[TT] Working Life of the FS2 = 10 years"]
-[10.619140625, 1.2125146389007568, "[TT] Diameter of the Markarian 335 = 30 times the diameter of the sun"]
-[6.477599620819092, 1.0413316488265991, "[TT] Observation Start Date of the Planet Finder Spectrograph = August 2019"]
-[11.867096900939941, 5.413010120391846, "[TT] Size of the XFM instrument = Less than 10 x 10 x 8 cm"]
-[5.866007328033447, 3.2234344482421875, "[FF] Number of Spaceships of the Progress 77 = 1"]
-[6.708024024963379, 1.8304197788238525, "[FF] URL of the ICON = https://icon.ssl.berkeley.edu/science/"]
-[7.924922943115234, 8.981792449951172, "[TT] Wavelength Sensitivity of the Polarimeter = 1170 - 1800 \u00c5 in second order and up to 3600 \u00c5 in first order"]
-[4.938072204589844, 3.520984649658203, "[TT] Manufacturer of the OBC = SWE"]
-[4.995046615600586, -0.32038965821266174, "[TT] Launch Time (UTC) of the ESAIL = 01:51"]
-[7.093618869781494, 4.79866886138916, "[FF] Design Discussion of the MSX/UVISI = Three-paper series"]
-[5.31538200378418, 3.9705650806427, "[TT] Quantity of Satellites of the Planet Labs = More than 200 satellites"]
-[7.58219575881958, 0.8409978151321411, "[FF] Impact Detection of the Apollo seismometers = Large impacts"]
-[8.8774995803833, 3.09873366355896, "[FF] Purpose of the WIND = Measure the plasma and fields around the spacecraft, including energetic particles and radio waves"]
-[7.970017433166504, 2.611027240753174, "[FF] Other Names of the CALIPSO = Earth System Science Pathfinder-3 (ESSP-3), Pathfinder Instruments for Cloud and Aerosol Spaceborne Observations - Climatologie Etendue des Nuages et des A\u00e9rosols (PICASSO-CENA)"]
-[9.852982521057129, 0.8863477110862732, "[TT] Spatial Resolution of the GOSAT-2 = Band 4, 1500 m(2250 \u00b5rad)"]
-[7.496150970458984, 8.436810493469238, "[TT] Bands of the Instrument = 16"]
-[4.942333221435547, 3.3176891803741455, "[TT] Affiliation of the BPA-3 = Hartron-Arkos, Ukraine"]
-[7.662069320678711, 6.466202735900879, "[TT] Cross-Scan Time of the TOMS = Eight seconds"]
-[8.6190824508667, 4.809324741363525, "[TT] Guide Stars Monitoring Interval of the DPU = 10-20 seconds"]
-[6.199939727783203, 0.6601206064224243, "[TT] Launch Date of the Planet Orbit = October 14, 2019"]
-[3.0054397583007812, 4.582309246063232, "[TT] Observation Mode of the ALOS-2 PALSAR-2 = High-resolution 10 m mode (dual polarisation)"]
-[9.646663665771484, 8.388996124267578, "[TT] Total FOV of the Sensor Unit = > 2\u03c0 sr"]
-[8.187858581542969, 2.7575528621673584, "[FF] Purpose of the SSULI = Measure Natural Airglow in the Upper Atmosphere"]
-[6.691856861114502, 1.6411277055740356, "[FF] URL of the ISS-RapidScat = URL: http://www.nasa.gov/jpl/rapidscat/nasas-new-winds-mission-installed-gathers-first-data/"]
-[5.632745742797852, 2.727013111114502, "[FF] Agency of the ASNARO = NEC Corporation and the Institute for Unmanned Space Experiment Free Flyer (USEF)"]
-[4.180597305297852, 7.093626499176025, "[TT] Communications Beam Width of the Ka-Band unit = 10.2-degree"]
-[11.731561660766602, 4.699182510375977, "[TT] Edge Length of the BEESAT-4 = 10 cm"]
-[13.88997745513916, 3.702526569366455, "[TT] Mass of the Telescope = 90 kg"]
-[10.080780029296875, 7.063292026519775, "[TT] Along-Track Coverage of the MSI-0 and MSI-1 = 30 km"]
-[3.7554659843444824, 6.49167537689209, "[TT] Antenna of the User Terminal = 1/4 wave groundplane or drooped-dipole"]
-[11.97213077545166, 5.007286548614502, "[TT] Size of the Assembly = 310 mm x 200 mm x 480 mm"]
-[10.012904167175293, -1.6224497556686401, "[TT] Inclination of the Secondary Payloads = ~51.6\u00ba"]
-[2.323138475418091, 1.3037384748458862, "[TT] Full Deployment Time of the NanoSail-D2 = Within just five seconds"]
-[10.339385986328125, 6.594850063323975, "[TT] Detector-Mirror Separation of the NuSTAR Metrology System = 10 m"]
-[10.19292163848877, 7.371635437011719, "[TT] Image Size of the ABI = 17.4 degree diameter circle"]
-[7.352091312408447, 6.271969318389893, "[TT] Purpose of the LARES = Laser Ranging Target"]
-[5.424156188964844, 5.072266101837158, "[TT] Communication Approach of the CAN Bus = Wait-on-send"]
-[4.764878749847412, 0.40565603971481323, "[TT] Launch Date of the SET = June 2019"]
-[9.52861499786377, 8.163689613342285, "[TT] Field of View of the Optics = 10\u00ba"]
-[10.202016830444336, 7.6621623039245605, "[FF] Type of the OTA = 50 cm aperture Gregorian telescope with a collimating lens unit and an active tip-tilt mirror for image-stabilization"]
-[8.240734100341797, 7.380763053894043, "[TT] Light Sensor of the GRD = Silicon Photomultipliers (SiPMs)"]
-[11.499262809753418, 4.693925380706787, "[TT] Length of the FY-2F = 4.5 m"]
-[7.073479652404785, 3.711928367614746, "[FF] Formation Flying Operation Phase Duration of the PROBA-3 = 7 orbits"]
-[8.033219337463379, 4.833122730255127, "[TT] Calibration Concept of the Atmospheric-sounding instrument = Extensive on-ground characterization and in-flight calibration concept"]
-[5.126623153686523, 2.7185041904449463, "[TT] Coordinator of the ESEO = University of Bologna"]
-[5.374016761779785, 8.548290252685547, "[TT] Bandwidth of the MDD = \u00b110 kHz"]
-[7.692198276519775, -2.54459285736084, "[TT] Cadence of the GOLD = ~15 min"]
-[7.977924346923828, 13.68613338470459, "[TT] SSD of the B7 = 20 m"]
-[12.00210189819336, 3.4291019439697266, "[TT] Quantity of the Propulsion tank = 1"]
-[12.036962509155273, -0.4141155779361725, "[TT] Launch Date of the TESS = April 2018"]
-[7.9174113273620605, 9.13262939453125, "[TT] Wavelength of the Olivine = 1 \u00b5m"]
-[8.915497779846191, 3.877729654312134, "[TT] Data Provided of the UVSTAR = Jovian system EUV data"]
-[3.3387532234191895, 5.167507171630859, "[TT] Polarization of the CSG-SAR = Single, Dual, Quad"]
-[8.33837890625, 8.678483963012695, "[TT] Spectral Sampling of the Littrow spectrometers = 0.1 nm"]
-[3.904590606689453, 6.32870626449585, "[TT] Quantity of the Patch Antennas = Two"]
-[4.998363018035889, 2.8291516304016113, "[TT] Manufacturer of the Sich-2 = Yuzhnoye SDO"]
-[9.485115051269531, 7.013747692108154, "[TT] Resolution of the T1 = 20 km x 20 km"]
-[14.291983604431152, 3.1705758571624756, "[TT] Total Mass of the S/C = 123.7 kg"]
-[5.146067142486572, 3.165602684020996, "[TT] Provider of the ESA = ESA"]
-[8.302979469299316, 4.560631275177002, "[FF] Improvement of EOP of the LARES 2 = 21%"]
-[5.584530830383301, 6.070284843444824, "[TT] Data Storage of the SCP = Half of programming space"]
-[6.951561450958252, 1.7260346412658691, "[FF] URL of the GRACE-FO = https://www.nasa.gov/press-release/twin-spacecraft-launch-to-track-earth-s-water-movement"]
-[7.925243377685547, 7.858860492706299, "[TT] Sampling Rate of the HSC-III optics subsystem = 200 frames/s"]
-[10.37841510772705, 5.388057708740234, "[TT] Heater Systems of the TCS = HM and HS"]
-[8.337214469909668, 7.574276924133301, "[TT] Quantum Efficiency of the CMOS Image Sensor = ~85% (at 650 nm)"]
-[12.46958065032959, 6.644618511199951, "[FF] Intercomparison of the Proton monitor Las Dos Torres = In-orbit results"]
-[10.107059478759766, 5.72434139251709, "[TT] Detector Cooling of the Imager = Cooling of SWIR detector to < 210 K"]
-[14.34522533416748, 3.242976188659668, "[TT] Mass of the DCS = 76 kg"]
-[8.569266319274902, 1.2252740859985352, "[TT] Survey Coverage of the Aquarius = Worldwide with gaps in mountainous or vegetated terrain"]
-[5.810208320617676, 3.3715980052948, "[TT] Current Backlog of the Satellogic = $38 million"]
-[8.384928703308105, 1.5150691270828247, "[TT] Humidity of the PM = 25~70%"]
-[6.21312141418457, 5.973446846008301, "[TT] Number of Data Collection Platforms of the DCS = 19,000"]
-[3.969611883163452, 6.334444046020508, "[TT] Connector Type of the Antennas = SMA male"]
-[5.73298454284668, 3.0922725200653076, "[TT] Funding of the GPSP = NOAA"]
-[3.329249620437622, 5.13373327255249, "[TT] Operation Mode of the Radar = Standby"]
-[11.432992935180664, 4.827380180358887, "[TT] Shape of the M3 = Aspheric of-axis concave"]
-[7.134896278381348, 3.977587938308716, "[FF] Application of the Generic Radio-Frequency Subsystem = High-Altitude Formation-Flying Missions"]
-[9.836488723754883, 7.84285306930542, "[FF] Configuration of the UVIT = Two telescopes"]
-[3.6315391063690186, 2.703395128250122, "[TT] Number of Possible Conjunctions of the Iridium constellation of satellites = 1 in 10 days"]
-[5.23618745803833, 2.3055195808410645, "[TT] Mission Type of the SpaceX CRS-16 = Non-EO"]
-[7.335109233856201, 8.831986427307129, "[TT] FWHM of the Filters of the MEIDEX = 4, 4, 30, 30, 50 and 40 nm"]
-[4.147397041320801, 5.758753299713135, "[TT] Data Collection of the ADS-B Receiver = Global (except in polar areas due to ISS orbit)"]
-[16.490449905395508, 3.612870454788208, "[TT] Investment in OneWeb of the Hughes = $50 million"]
-[3.9908738136291504, 1.8346576690673828, "[TT] Launch Service Provider of the Global-9 = Rocket Lab"]
-[9.263327598571777, 6.092765808105469, "[TT] Telecentric Optics Array Angle of the Sensor = 90\u00ba"]
-[3.678431510925293, 2.5985400676727295, "[FF] Data Speed Options of the Iridium Certus = Multiple"]
-[6.69265604019165, 4.400760650634766, "[FF] Use of the PREMOS = Entry point for GCM simulations"]
-[4.407588005065918, 1.7847254276275635, "[TT] Launch Year of the RADARSAT-2 = 2007"]
-[9.674113273620605, 4.831649303436279, "[TT] Method of the Three-axis stabilized = Three-axis stabilized"]
-[9.875421524047852, 1.7034493684768677, "[FF] Article Date of the Black Hole = July 12, 2016"]
-[1.7854822874069214, -2.0470705032348633, "[FF] Hill Coordinate System of the Hayabusa-2 = The Sun is always to the left and outside the figure"]
-[8.03348445892334, 4.586997985839844, "[FF] Objective of the SEU (Single Event Upset)/RADMON (Radiation Monitor) = Develop a small, low-cost, low-power SEU and TD (Total Dose) RADMON using standard CMOS processes"]
-[6.377028465270996, 4.871333122253418, "[FF] Function of the ACE = Interfaces to the ACS components and hosts the ACS software"]
-[13.159289360046387, 7.140268325805664, "[TT] Power of the Star sensor = 4 W"]
-[8.152148246765137, 0.03534902259707451, "[TT] Mission Completion Date of the TOPEX/Poseidon = August 1995"]
-[8.943963050842285, 5.598400115966797, "[TT] Pointing Stability Requirement of the IRS Sounder = 300 m at SSP"]
-[8.566579818725586, 4.32535457611084, "[FF] Protection Function of the Shutter = Blocks Sun light"]
-[10.1670503616333, 5.9511542320251465, "[TT] Temperature Control of the Imager = \u00b10.01 K"]
-[7.187977313995361, 7.614141464233398, "[TT] Signal Depth of the HF-A analyzer = 12 bit"]
-[8.54077434539795, 5.382014751434326, "[TT] Position Accuracy (RMS orbit) of the S-3 NRT = 10 cm threshold with a target of 8 cm (radial)"]
-[8.026498794555664, 7.14656925201416, "[FF] Detector of the SEXTANT = Required to provide source and background count rates"]
-[6.237514972686768, 3.8293442726135254, "[FF] Operator of the PARASOL = Unknown"]
-[8.053767204284668, -0.9994547367095947, "[TT] Purpose of the ICESat-2 = Study polar ice"]
-[8.583346366882324, 3.054567813873291, "[FF] Application of the MCP = Measure the gas density in the upper atmosphere"]
-[6.681446075439453, -0.6625189185142517, "[TT] Flight Time to Transfer Orbit of the Fregat upper stage = 6 minutes 36 seconds"]
-[5.1894025802612305, 4.6865715980529785, "[TT] Service Type of the BlackSky = Global monitoring and alerting services"]
-[8.53282642364502, 6.031008243560791, "[TT] Acquisition Range of the Guider = 1.2\u00ba"]
-[6.687154769897461, 7.396385192871094, "[TT] Conversion Type of the ADC = Linear analog to digital conversion of dV in 256 channels"]
-[10.10047435760498, 1.456164002418518, "[FF] Microlensing Event of the Gaia16aye = Northern Galactic disc"]
-[4.451523780822754, 5.444815158843994, "[TT] Deployment of the GOMX-3 = ISS (International Space Station)"]
-[7.001530170440674, 4.59495735168457, "[FF] Fairing of the Dnepr = Modified"]
-[13.235240936279297, 5.228339672088623, "[TT] Solar Array Dimensions of the IRIS = 0.6 m x 1.3 m"]
-[6.001952171325684, 5.145846843719482, "[TT] Purpose of the ISL = Relay camera measurements"]
-[5.909203052520752, 1.6373122930526733, "[FF] Conference Presentation Date of the Small Satellite = Aug. 4-9, 2018"]
-[8.660720825195312, 8.804885864257812, "[TT] Spectral Range of the Grating Spectrometer = 0.9-1.7 \u00b5m"]
-[6.579411029815674, 4.749839782714844, "[FF] Components of the AFSS = GPS, IMU, algorithms"]
-[7.872339248657227, 6.1947503089904785, "[FF] Image Capture Method of the WAC = Moderate resolution images using filters"]
-[9.22603702545166, 6.190992832183838, "[TT] Line of Sight Range of the TIR Subsystem = \u00b1 8.54\u00ba in the cross-track direction of nadir"]
-[8.297056198120117, 7.619442939758301, "[TT] Detector Type of the Telescope = Si HgCdTe HgCdTe"]
-[9.519247055053711, -1.011063814163208, "[TT] Orbit Longitude of the GEOSAR GOES-7 = 155\u00ba E"]
-[13.281511306762695, 5.166350841522217, "[TT] Size of the Solar Array = 1.83 m x 4.9 m"]
-[11.625847816467285, 4.556377410888672, "[TT] Primary Diameter of the Didymos = 780 m"]
-[5.7051239013671875, 7.14391565322876, "[TT] Data Rate of the IREI = 1.92 Mbit/s"]
-[13.377381324768066, 6.735208511352539, "[FF] Power Conversion of the PPM = Converts electrical power (300 W) provided by solar panels of STSat-3 to the power required for accelerating charged particles inside the channel of the thruster head"]
-[4.641021728515625, 0.6397860050201416, "[TT] Launch Date of the SGR-ReSI receiver = Q4 2016"]
-[6.004398822784424, 5.464797019958496, "[TT] Redundancy of the OBC = Yes"]
-[7.537487030029297, 2.2887792587280273, "[TT] Coverage Area of the Ground Segment = Alps, Pannonian Plain, and Mediterranean region"]
-[7.167000770568848, 7.849236965179443, "[TT] Reflectance of the Reflection Diffuser = \u03c1=100%"]
-[11.326108932495117, 5.496705055236816, "[TT] Payload Fairing Material of the Minotaur = Carbon fibers and epoxy"]
-[6.557780742645264, 5.9088592529296875, "[FF] Incorporation of Laser Intersatellite Links of the Starlink = Undergoing Technology Improvements"]
-[9.653573989868164, 1.3826446533203125, "[FF] Launch Date of the Pleiades-1A = Unknown"]
-[4.3662919998168945, 5.499660968780518, "[TT] Frequency of the COSPAS-1 = 406 MHz"]
-[4.85566520690918, 0.8153538107872009, "[TT] Third Flight Date of the MEPSI = Nov. 24 to Dec. 7, 2002"]
-[5.444126129150391, -0.04446237161755562, "[FF] China Coverage Contract Date of the RapidEye = Dec. 7, 2011"]
-[6.147624969482422, 3.652867555618286, "[TT] Task of the Restore-L = Manipulate its fill and drain valve"]
-[4.777814865112305, 6.573845863342285, "[TT] Communication System of the TRMM = Telemetry, Tracking and Control (TT&C) transponders"]
-[14.257589340209961, 3.195073366165161, "[TT] Mass of the Ralph = 37.7 kg"]
-[5.027713775634766, 0.5643835067749023, "[TT] Launch Date of the ZACUBE-2 = 27 Dec 2018"]
-[9.014508247375488, 5.032345771789551, "[TT] Onboard Sensors of the LAGEOS = None"]
-[9.55070972442627, -0.1612236201763153, "[TT] Altitude of the MCAM-2 = 200 km"]
-[3.5582070350646973, 5.0736918449401855, "[TT] Configuration of the SARP-1 = SARP with memory"]
-[6.608120441436768, -0.5798989534378052, "[FF] Orbit Duration of the SMOS = Almost 1 Year"]
-[5.087949752807617, 3.4945271015167236, "[TT] Bus Manufacturer of the THEMIS Probes = Swales Aerospace"]
-[8.80062484741211, 3.414182424545288, "[FF] Image Credit of the AIP (Advanced Ionospheric Probe) = NCU"]
-[7.877801895141602, 2.761321783065796, "[FF] Purpose of the CASE = Help zero in on exoplanet clouds and hazes"]
-[8.77829647064209, 7.9888997077941895, "[FF] Design of the Optic with SDD = Low-cost, low-mass"]
-[4.205615520477295, -1.4671474695205688, "[TT] Mission Type of the Chang'e-2 = Lagrange L2 Point"]
-[14.112436294555664, 3.2485785484313965, "[TT] Mass of the Mass = 241 kg"]
-[6.745331764221191, -0.7162639498710632, "[TT] LSDN of the Orbit = 12:00 hours \u00b1 15 min"]
-[4.905332565307617, 2.402580738067627, "[FF] URL of the Eutelsat Quantum = https://www.esa.int/Applications/Telecommunications_Integrated_Applications/Reprogrammable_satellite_is_ready_for_launch"]
-[10.089777946472168, 1.9118489027023315, "[TT] Launch Date of the Chandrayaan-2 = 6 September"]
-[4.279513359069824, 7.214397430419922, "[TT] Band of the Wide-beam payload = C- and Ku-band"]
-[8.27663803100586, 4.189460277557373, "[TT] Data Record of the Merlin Radiation Monitor = 10 years"]
-[10.537476539611816, 2.8098676204681396, "[TT] Manufacturer of the CICERO-4 = Tyvak Nanosatellite Systems"]
-[9.32202434539795, 5.13339376449585, "[TT] Yaw Pointing Accuracy of the Attitude Control = \u00b10.3\u00ba"]
-[7.293705463409424, 7.698628902435303, "[TT] Power of the PHA = 11 mW per active PHA"]
-[6.693643569946289, 2.996520757675171, "[FF] Weather Data of the Spire Global = Improve Maritime Vessel Performance and Reduce Carbon Emissions"]
-[8.07076358795166, 1.8459670543670654, "[TT] Coastal Zones Spatial Resolution of the HY-1C = 50 m"]
-[8.348496437072754, 5.382372856140137, "[TT] Orbit Determination Accuracy of the QZS-1 = Sub-meter"]
-[7.646515846252441, 9.449251174926758, "[TT] Center Wavelength of the Band 7 = 3.90 \u00b5m"]
-[13.363868713378906, 7.652217388153076, "[TT] Power consumption of the Antenna = <1.5 KVA"]
-[12.040884971618652, -0.3813878893852234, "[TT] Mission of the TESS = Extended"]
-[8.992968559265137, 4.408677577972412, "[TT] Digital sun sensors of the ADCS = 1\u00ba (accuracy), \u00b160\u00ba (range)"]
-[6.180715084075928, 4.97447395324707, "[FF] Main Tasks of the OBDH = Processing of telecommands and telemetry, time management, navigation, management for concepts of redundancy, allocation of interfaces to all subsystems onboard SONATE, monitoring of its state with an autonomous response in case of failures or critical values"]
-[9.566926956176758, 7.038425445556641, "[TT] Resolution of the CHRIS = 17 to 34 meter"]
-[2.8975167274475098, 4.22430419921875, "[TT] Observation Date of the PALSAR-2 = May 2, 2015"]
-[9.526204109191895, 6.781757831573486, "[TT] Range Resolution of the Wide fine Quad-Pol = 5.2-17.3 m"]
-[4.839452266693115, 5.323940277099609, "[TT] Quantity of the GPS Antennas = 2"]
-[7.078609943389893, 8.766371726989746, "[TT] Dynamic Range (Normalized Radiance) of the POLDER-2 = 0.05-0.22"]
-[5.565796375274658, 5.669665813446045, "[TT] CPU of the OBC = 16-bit CPU of Siemens"]
-[11.975809097290039, 6.276551246643066, "[FF] Flux Measurement of the AMS = Smooth"]
-[9.446146965026855, 6.189673900604248, "[FF] Function of the Shutter = Oscillates in synchronization with the scan mirror and crosses the optical axis at the end of each scan"]
-[10.01494312286377, 2.900909662246704, "[TT] Launch Date of the ALBus CubeSat = 16 December 2018"]
-[4.3773956298828125, 7.453444004058838, "[TT] Frequency of the TT&R = Ku-band"]
-[7.15443229675293, 3.3540079593658447, "[FF] Illustration of the \u00d8rsted = Figure 1"]
-[9.585590362548828, 6.724972724914551, "[TT] Spatial Resolution of the Geodesy Orbits = 100-1000 km"]
-[8.30628776550293, 8.950067520141602, "[TT] Spectral Range Extension of the Argus = Up to 2500 nm"]
-[8.16635799407959, 8.81422233581543, "[FF] Advantage of the MSX/UVISI = Simultaneous Measurement of Refraction Angles and Extinction"]
-[10.550638198852539, 3.3585896492004395, "[TT] Form Factor of the TechEdSat = 1U CubeSat"]
-[5.273159980773926, 2.8819572925567627, "[TT] Operator of the Deimos-2 = Elecnor Deimos"]
-[4.799554824829102, 0.23913846909999847, "[TT] Launch Date of the RemoveDebris spacecraft = December 18, 2017"]
-[3.465696334838867, 6.400857448577881, "[TT] Size of the Antennas = 9.1 m"]
-[11.72342586517334, 0.11987243592739105, "[TT] Candidate Exoplanets of the TESS = Over 850"]
-[10.071366310119629, -1.5979869365692139, "[TT] Inclination of the Main Payload = 98\u00ba"]
-[6.311948299407959, -0.5292470455169678, "[TT] Duration of the EM-2 = 14 days (4 at destination)"]
-[7.663593769073486, 2.263951539993286, "[FF] Data Relay Type of the DRT = Globally metrological, hydrological and oceanographic data"]
-[8.073954582214355, 9.281146049499512, "[TT] Wavelength of the Liquid water = 1.4 \u00b5m"]
-[7.723723411560059, 5.698514461517334, "[FF] Ortho-rectification Methods of the Deimos' ground segment = Automatic, Human-driven"]
-[4.681301593780518, 2.8995962142944336, "[TT] Control Room of the Aeolus = Earth Explorer control room at ESOC"]
-[14.484370231628418, 6.877579689025879, "[TT] Battery Voltage of the EPS = 4.2 V"]
-[9.3623685836792, 7.363269329071045, "[TT] Mounting Height of the Panoramic Camera system = 2 m above ground level"]
-[5.931000709533691, 1.5241482257843018, "[FF] Status and Instrument Performance of the SUOMI National Polar-orbiting Partnership = Unknown"]
-[5.580556392669678, 4.867349624633789, "[FF] Inputs of the TAFF = GPS data provided by the GPS receiver onboard TDX and, through the ISL, also from the GPS receiver data onboard the TSX"]
-[7.572198390960693, 1.2937570810317993, "[FF] Image Content of the LROC = Earth and moon"]
-[8.75975513458252, 4.77485990524292, "[FF] Accuracy of the Star Tracker (SST) = Most accurate ones for three-dimensional orientation measurements"]
-[4.921298027038574, 0.6045060753822327, "[TT] Launch Date of the MANTIS = 11 November 2023"]
-[5.58851432800293, -2.042076826095581, "[TT] Image Resolution of the KOMPSAT-3 = Sub-meter"]
-[12.146913528442383, 6.138318061828613, "[TT] Measurement Events of the AMS = 41 billion cosmic ray events"]
-[5.758791446685791, 2.900261878967285, "[TT] Funding of the ISS = $17 million in fiscal year 2021"]
-[8.473556518554688, 2.4698638916015625, "[FF] Purpose of the Cold Atom Laboratory (CAL) = Produces clouds of atoms chilled to temperatures much colder than deep space"]
-[14.4550142288208, 3.146397113800049, "[TT] Total Mass of the CBERS-4A = 1980 kg"]
-[8.073795318603516, 6.888586521148682, "[TT] Strength of the PM = 5 times weaker than the SCM"]
-[8.166805267333984, -1.0092175006866455, "[TT] Measurement Precision of the ICESat-2 = Few inches"]
-[7.521121978759766, 0.9580161571502686, "[FF] Density Profile of the GRAIL = Not constant at all depths below the deepest topographic excursion"]
-[11.406049728393555, 5.924422740936279, "[TT] Material of the OAP = Rapidly solidified aluminum (RSA) alloy RSA-6061"]
-[13.618529319763184, 5.529088497161865, "[TT] Solar Arrays of the UK-DMC-2 = Three body-mounted heritage solar arrays"]
-[9.683221817016602, -0.4700624942779541, "[TT] Orbit Altitude of the ASTERIA = ~400 km"]
-[6.758432388305664, 1.506531000137329, "[TT] Imagery Acquisition Period of the FormoSat-2 = Spring of 2006 to the spring of 2008"]
-[5.473635196685791, 2.229727268218994, "[FF] Affiliation of the Frank Preud'homme = Unknown"]
-[10.010080337524414, 2.8870816230773926, "[TT] Deployment Date of the ASTERIA 6U CubeSat = November 21, 2017"]
-[10.482370376586914, 1.5852495431900024, "[FF] Study Subject of the Quasars = Gravity in the very strong field of the supermassive black holes"]
-[8.943761825561523, 0.4856356978416443, "[TT] Maximum Number of the New Boulders = Found at a distance of 17 m"]
-[4.1345744132995605, 4.2400689125061035, "[FF] Mission of the RAX-2 = UHF radar experiment to remote sense ionospheric plasma properties"]
-[9.297365188598633, 3.1781651973724365, "[FF] Measurement of the WISPR = Solar Corona Structure"]
-[11.747398376464844, 0.07468689978122711, "[TT] Number of Exoplanets Discovered of the TESS = 29"]
-[10.636580467224121, 8.883867263793945, "[TT] Pixel size of the Channel 7 = 32 km x 32 km"]
-[7.57585334777832, 0.8406646251678467, "[FF] URL of the Lunar Polar Hydrogen Mapper = https://live-lunah-map.ws.asu.edu/mission"]
-[10.019556999206543, -0.14005136489868164, "[TT] Orbit Altitude of the Starshine-2 = 387 km"]
-[12.854930877685547, 3.250237226486206, "[FF] Fuel Tank Status of the Kepler spacecraft = Running very low"]
-[6.433810710906982, 5.441891670227051, "[TT] Design of the OLS = Cassegrain"]
-[9.81727409362793, -0.5659981966018677, "[TT] Orbit Altitude of the MFG series = 35,786 km"]
-[3.294518232345581, 5.392638206481934, "[TT] Wavelength of the SAR-10 = 9.6 cm"]
-[7.8184967041015625, 8.107378959655762, "[TT] Band 4 of the R3 Sensor = NIR"]
-[7.608314037322998, 8.410999298095703, "[TT] Number of Bands of the WFI = 4"]
-[4.565824031829834, 7.296826362609863, "[TT] Data Modulation Type of the X-band data transmission = RFM, DRFM (Digital Radio Frequency Memory)"]
-[10.309181213378906, 3.1604597568511963, "[TT] Number of Experiments of the CubeSat = 26"]
-[8.129989624023438, -0.6789173483848572, "[FF] Measurement Type of the CryoSat-2 = Height of ice"]
-[13.183616638183594, 6.1184983253479, "[FF] Mission Purpose of the HORYU-4 = Estimate the photo-electron emission current influence on spacecraft charging"]
-[6.2368950843811035, 3.1594932079315186, "[FF] Key Features of the BlackSky Global Intelligence Platform = Ease of use, Rapid revisit, Affordability"]
-[9.51210880279541, 2.7717068195343018, "[FF] Purpose of the XFM = Measure X-ray emissions from the Sun"]
-[11.924193382263184, 5.402308940887451, "[TT] Instrument Size of the RAMIS = 140 x 140 x 35 mm3"]
-[6.289531230926514, 2.426726818084717, "[FF] Purpose of the EFT-1 = Demonstrate Orion structural integrity, thermal protection systems, jettison separation of the launch abort system tower, on orbit energy and guidance capability, re-entry crew module control, separation from the service module, parachute and landing separation events"]
-[8.933093070983887, 4.856039047241211, "[TT] Quantity of the CLS sensor = 1"]
-[4.930644989013672, 5.128610610961914, "[TT] CCSDS ID of the GSAT-0209 = 269"]
-[9.45897388458252, 7.0923919677734375, "[TT] Radiometric Resolution (K) of the PMI = 0.4"]
-[5.00994873046875, 2.1392712593078613, "[TT] Carries of the QBITO = INMS"]
-[7.414262771606445, 2.8862555027008057, "[TT] Number of Detections of the Methane Leak = 12"]
-[3.7474896907806396, -0.7527007460594177, "[FF] Crowdedness of the Low Earth Orbits = Increasing"]
-[6.268757343292236, 0.04434521123766899, "[TT] Planned Crew Capacity of the Tiangong Space Lab = 3"]
-[7.098114967346191, 4.377285480499268, "[FF] Challenges of the MiRaTA = Miniaturization, component integration"]
-[11.820075035095215, 4.719925880432129, "[TT] Inner Diameter of the Vacuum Tank = 1.1 m"]
-[13.665628433227539, 5.808996677398682, "[TT] Peak Power Demand of the Solar Panels = ~24 W"]
-[5.553584575653076, 2.0533089637756348, "[FF] Workshop Date of the JAXA Satellite Application Mission = Oct. 24-25, 2013"]
-[3.136924982070923, 5.202248573303223, "[TT] Stripmap Scene Size of the SAR Antenna = 60 km x 8 km"]
-[8.718793869018555, 8.642602920532227, "[TT] Pixels per FWHM of the Spectrometer = 1720"]
-[18.64043617248535, 3.96113920211792, "[TT] NE\u0394T of the 7 = 0.6 K"]
-[4.660664081573486, 0.548932671546936, "[TT] Launch Date of the GOES-S = March 1, 2018"]
-[10.074263572692871, 5.519843578338623, "[TT] Ovenized Crystal USO Stability of the DSAC = Between 1 \u2013 100 seconds"]
-[3.8752262592315674, 3.445697784423828, "[FF] Full Operational Capability Date of the Galileo Satellite = Unknown"]
-[7.076719284057617, 6.921743392944336, "[TT] Readout Interval of the N-FEE = 6.25 s"]
-[9.941475868225098, -0.5143216848373413, "[TT] Orbit Altitude of the RISAT-1 = 536 km"]
-[9.89979076385498, 7.381862163543701, "[TT] Ground Sampling Distance of the UK-DMC-2 = 22 m"]
-[8.297502517700195, 8.29012680053711, "[TT] Number of Bands of the Telescope = 18 Infrared + 1 Visible"]
-[2.8618757724761963, 4.224042892456055, "[TT] Observation Image Date of the ALOS-2 PALSAR-2 = 29th September 2017"]
-[10.107758522033691, 7.525348663330078, "[TT] Diameter of the Image Surface = 246 mm"]
-[5.3550519943237305, 6.215484142303467, "[TT] Device package of the SDR-SMM = Eight Die Stack TSOP II"]
-[6.915655612945557, 3.5451700687408447, "[FF] Purpose of the Nitrogen/Oxygen Recharge System (NORS) Recharge Tank Assembly (RTA) = Support high-pressure gas operations and activities on-orbit"]
-[6.943305969238281, 4.9590678215026855, "[FF] DPU of the SEM-2 = Data Processing Unit"]
-[3.812812328338623, 6.49681282043457, "[TT] Offset Angle of the Antenna = 42\u00ba"]
-[8.260348320007324, 1.8716275691986084, "[FF] Objectives of the AATSR = Continuation of precise measurement of Sea Surface Temperature (SST) started with ATSR-1 and ATSR-2"]
-[7.323831081390381, 4.415502071380615, "[FF] Design of the Spacecraft Structure = Stiffness, strength and pointing requirements of the payload, sensors"]
-[7.31570291519165, 3.4614462852478027, "[FF] Pass Frequency of the Satellite = Three to five times per day"]
-[10.935039520263672, 5.659642696380615, "[FF] Parameter Measured of the Instrumentation = Surface and internal temperatures during reentry, ablation rate of the shield's coating"]
-[7.053715229034424, 6.94675350189209, "[TT] Components of the Laser Metrology System = Two laser pointers, 2 PSD detectors"]
-[10.427129745483398, 5.713090419769287, "[TT] Pavement Temperature of the ECOSTRESS = Exceeded 122 F (50 C)"]
-[6.57127571105957, 1.722672939300537, "[FF] Partnership Date of the Skybox Imaging = May 14, 2013"]
-[12.075035095214844, 6.310937881469727, "[TT] Positron Fraction of Cosmic Ray Electrons of the AMS = Up to 10%"]
-[5.830753803253174, 1.4422835111618042, "[TT] Sample Dispersal Deadline of the JAXA = By the close of 2021"]
-[4.7440409660339355, -1.2301666736602783, "[TT] Number of Private Launch Companies Prepared to Make First Attempts to Reach Orbit of the China = 4"]
-[8.637889862060547, 7.70059871673584, "[TT] Detector Size of the MS Bands = 13 \u00b5m"]
-[9.857779502868652, -0.5911655426025391, "[TT] Orbit Altitude of the ICESat-2 = 496 km"]
-[5.382733345031738, 0.2379438430070877, "[TT] Launch Date of the STS-107 = Jan. 16-Feb. 1, 2003"]
-[13.792641639709473, 2.9061830043792725, "[TT] Mass of the Block-5D-2 spacecraft = 812 kg"]
-[9.861625671386719, 7.162582874298096, "[TT] Resolution of the MTVZA = 12-75 km"]
-[5.015736103057861, 7.679502010345459, "[TT] Gain Factors of the Amplifier Module = Four possible"]
-[6.000015735626221, 2.5215911865234375, "[TT] Number of People of the SSV Robert C. Seamans = 40"]
-[4.493472099304199, -0.8969230055809021, "[TT] Arrival Date of the SpaceX-CRS-4 Dragon capsule = Sept. 23, 2014"]
-[4.542695045471191, 5.832490921020508, "[TT] Production Increase of the Location Protocol Beacons = 6.3%"]
-[8.875679969787598, 2.526611328125, "[FF] Mission of the SOHO = Solar and Heliospheric Observatory"]
-[6.628382682800293, -0.3903912603855133, "[TT] Period of the TSX-5 = 106 minutes"]
-[4.845319747924805, -1.833272933959961, "[TT] Altitude of the Chang'e-3 lander = 4 m"]
-[5.378533840179443, 3.971295118331909, "[TT] Number of Satellites of the RADARSAT Constellation = 3"]
-[6.381984233856201, 3.143357038497925, "[FF] Mission Status of the AMS-02 = Unknown"]
-[5.91828727722168, 3.501152753829956, "[FF] Cost of the Brexit Satellite = BS billions"]
-[6.712070941925049, 7.618218421936035, "[TT] Beam Width of the Channel = 0.58 \u00ba"]
-[4.947922229766846, 7.2350592613220215, "[FF] Data Rate of the Communication links = 3 single channel RCV, 2 synthesized RCV 2 synthesized transmitters"]
-[9.760711669921875, -0.5980669260025024, "[TT] Orbit of the MicroMAS-2 = Polar orbit of 365 km height"]
-[9.959517478942871, -1.5563336610794067, "[TT] Orbit Inclination of the TecSAR = 41\u00b0"]
-[9.704025268554688, 1.4281816482543945, "[TT] Moon Images Acquired of the Pleiades-1A and Pleiades-1B = More than 800 images"]
-[11.650665283203125, 6.8884687423706055, "[TT] Energy Channels of the SSJ/4 = 20 fixed energy channels between 30 eV and 30 keV"]
-[7.077205181121826, 7.224245071411133, "[FF] Laser Power Levels of the ATLAS = Unknown"]
-[13.509908676147461, 6.033540725708008, "[FF] Model of the GSE Power Supplies = Solar eclipse"]
-[14.734844207763672, 6.60988712310791, "[TT] Nominal Capacity of the Li-ion Battery Block = 34.8 Ah"]
-[4.1417036056518555, 7.292812824249268, "[TT] Band of the OceanSat-3 = Ku-band"]
-[11.034750938415527, 2.8848226070404053, "[TT] Size of the Minisatellite = 2.5 m x 5.2 m x 0.9 m"]
-[9.436136245727539, 5.461963653564453, "[TT] Spin Axis Orientation of the IMP-8 = Normal to the ecliptic plane within 1\u00ba"]
-[5.609785556793213, 0.28005823493003845, "[FF] Data Collection of the ISS-RapidScat = Started on October 6, 2014"]
-[14.061590194702148, 4.008205413818359, "[TT] Mass of the Instrument = 120 kg"]
-[6.870372295379639, 2.2574455738067627, "[FF] Remote Sensing Image Record Change Date of the Tongzhou Beijing = 13 Oct. 2017"]
-[8.538593292236328, 0.5786659717559814, "[TT] Landing Mechanism of the MASCOT = Free fall"]
-[14.228425979614258, 3.2774407863616943, "[TT] Mass of the EGS = 685.2 kg"]
-[5.76483154296875, -0.8531952500343323, "[TT] Nominal of the T/P Design Life = 3 years plus 2 years for an extended mission"]
-[10.504179000854492, 6.929299831390381, "[TT] Mirror Diameter of the Magnetic Suspension System = 10 cm"]
-[4.147923469543457, 2.5349535942077637, "[TT] Launch Site of the EDRS-C = Kourou in French Guiana"]
-[10.460586547851562, 5.807293891906738, "[TT] Temperature of the Infinity-shaped loop = 15 degrees above absolute zero"]
-[7.413524150848389, 3.7328619956970215, "[FF] Sensitivity to Instrument Degradation of the Occultation Techniques = Less sensitive than other remote sensing methods"]
-[14.244290351867676, 3.2699146270751953, "[TT] Mass of the eXCITe = 155 kg"]
-[4.798732280731201, 7.748026371002197, "[FF] Delay Variation of the Ranging Channel = Varies slightly with RF uplink power and temperature"]
-[8.293389320373535, 7.682487487792969, "[TT] Detectors of the Multispectral Imager = 12 detectors"]
-[4.4568190574646, 6.765611171722412, "[TT] RF Communications of the Spacecraft = S-band"]
-[12.027770042419434, -0.15638601779937744, "[FF] Unknown of the TESS Science Instrument = Unknown"]
-[6.471863269805908, 3.293555736541748, "[FF] Imagery Access of the BlackSky platform = More than 10 high-resolution imaging spacecraft"]
-[4.726480960845947, 6.597219467163086, "[FF] Data Transfer of the X-band communications link = Ground stations"]
-[9.286459922790527, 7.471154689788818, "[TT] Spatial Resolution (Panchromatic Band) of the NAOMI = 2.5 m"]
-[2.872333288192749, 4.275683879852295, "[FF] Observation Results of the ALOS-2/PALSAR-2 = Flooding on the Mississippi River"]
-[9.327946662902832, -1.7213953733444214, "[TT] Ascending Node Crossing Time Differences of the Swarm-A and Swarm-C = Between 4 and 10 seconds"]
-[8.635669708251953, 1.0980761051177979, "[TT] 9th Science Meeting Date of the Aquarius/SAC-D = 11-14 November 2014"]
-[13.885344505310059, 6.492868423461914, "[FF] Fault Protection of the EPS = Overcurrent protection, load switching, autonomous transitions between internal modes based on battery voltage"]
-[12.617716789245605, 9.094480514526367, "[TT] Equator Crossing Time of the OceanSat-1 = 12:00 hours on the descending node"]
-[14.289241790771484, 3.1716058254241943, "[TT] Mass of the TDU = 5.5 kg"]
-[16.504961013793945, 3.5904531478881836, "[TT] Launch Success Rate of the OneWeb = 100%"]
-[9.599495887756348, 8.276456832885742, "[FF] Function of the Quasi-circular Mask = Applied to the detector image to simulate a circularly symmetric FOV"]
-[8.370473861694336, 5.603750228881836, "[TT] Positioning Accuracy of the Lunar Pathfinder's Receiver = Around 100 m"]
-[8.975786209106445, 4.420778274536133, "[TT] Sun Sensor Field of View of the ACS = \u00b145\u00ba"]
-[4.775163173675537, -1.8840399980545044, "[TT] Launch Date of the Chang'e-5 = 23 November 2020"]
-[5.218518257141113, 0.8740980625152588, "[FF] Approval Date of the EPS-SG = Nov. 16, 2012"]
-[6.062803745269775, 8.048759460449219, "[FF] Accommodated Number of Users of the Channelizer = Increased in a disaster scenario"]
-[9.101619720458984, 4.476898670196533, "[FF] Attitude Requirement of the TIMED = Nadir-pointing with the +z axis in the direction of the Earth\u2019s geocentric center, the +y axis in the direction of orbit normal, and the +x axis generally in the ram or wake direction"]
-[8.19732666015625, -1.0983412265777588, "[TT] Bathymetry Measurement Depth of the ICESat-2 = 10 meters or more"]
-[5.869107723236084, -0.6426395773887634, "[TT] Lifetime of the Battery = 5 years"]
-[11.325759887695312, 5.861408710479736, "[TT] Structure Material of the Spacecraft = Aluminum and composite materials"]
-[8.630208015441895, 1.0897157192230225, "[TT] Data Collection Start Date of the Aquarius = December 1, 2011"]
-[7.430221080780029, 2.249842405319214, "[FF] Mission of the PROBA-V = Vegetation monitoring"]
-[8.197002410888672, 0.10411623120307922, "[TT] End of Life Date of the Meteor-1/Meteor-2/Meteor-Priroda Series = 01 Jan 2001"]
-[5.164742946624756, 2.3446574211120605, "[TT] Mission Type of the HTV-9 = Non-EO"]
-[5.072920322418213, 4.3603386878967285, "[TT] Number of Operational Satellites of the Starlink = About 1,350"]
-[5.565008163452148, 0.30615055561065674, "[FF] Meeting Date of the ISS-RapidScat = May 5-8, 2013"]
-[5.324314117431641, 0.24046261608600616, "[TT] Launch Date of the ISS:LIS = 19 Feb 2017"]
-[4.7719316482543945, -1.478537678718567, "[TT] Image Color of the Tianwen-1 = Black and White"]
-[8.160922050476074, -0.5212581753730774, "[TT] Headwaters of River of the Saskatchewan Glacier = North Saskatchewan River"]
-[10.717241287231445, 3.303385019302368, "[FF] Importance of the Micro-gravity experiment = Development of fluids, space material science, space life science"]
-[8.20141887664795, 2.8783462047576904, "[TT] Measurement Domain of the ISS:LIS = Atmosphere"]
-[10.763431549072266, 1.0424935817718506, "[TT] Diameter of the GJ 367 b = Just over 9000 km"]
-[10.679097175598145, 7.640390872955322, "[FF] Directional and Omni-directional Measurements of the MEPED = Available"]
-[10.338419914245605, 5.867346286773682, "[TT] Operating Temperature of the SWIR = 257 K"]
-[5.185321807861328, 8.430276870727539, "[TT] Bandwidth of the Channel 2 = 200 MHz"]
-[4.800701141357422, -1.4608608484268188, "[TT] Manufacturer of the Tianwen-1 = China"]
-[6.320806503295898, 1.1666936874389648, "[TT] Study Publication of the GRB 191016A = The Astrophysical Journal"]
-[9.011056900024414, 6.705616474151611, "[TT] Resolution of the HRS = 1m"]
-[6.815587520599365, 1.2014743089675903, "[FF] Meeting Date of the Solar Radiation and Climate Experiment (SORCE) = July 30 - Aug. 4, 2000"]
-[9.69819450378418, 4.888981342315674, "[FF] Interaction of the CNES and ONERA centers = Illustrated in Figure 34"]
-[5.562094688415527, 7.188210964202881, "[TT] Data Rate of the LHCP transmission = 320 Mbit/s"]
-[3.1298341751098633, 2.2593791484832764, "[FF] Instruments of the Sentinel-3 = Measure oceans, land, ice and atmosphere"]
-[8.049622535705566, -0.12976157665252686, "[TT] Period of the Meteor-M2-2 = 101.1 minutes"]
-[10.116390228271484, 8.170699119567871, "[TT] Aperture of the MWIR = 200 mm"]
-[6.8827595710754395, -0.5497576594352722, "[TT] Orbit Frequency of the HyperScout\u00ae = 15 times a day"]
-[8.416296005249023, 7.523521423339844, "[TT] Data Output of the Mid-IR Imagers = PAL format (384 H x 288 V pixels)"]
-[6.0276360511779785, 6.577469825744629, "[TT] Quantity of the RF switches, couplers, and diplexers = Multiple"]
-[5.093338966369629, 5.138633728027344, "[TT] GPS Receiver Channels of the SPS = 10-channel and 8-channel"]
-[3.589357852935791, 6.435815334320068, "[TT] Antenna Size of the Ground Station = 3.7 m"]
-[9.07017707824707, 5.464573383331299, "[TT] Absolute Performance Error of the Spacecraft = < 20 arcsec (95%)"]
-[10.93205451965332, 3.764127016067505, "[TT] Solar Sail Deployment Test Environment of the NEA Scout = Large, low-friction table"]
-[8.235919952392578, 1.4760798215866089, "[FF] Ocean Salinity Measurement of the SMOS = Unknown"]
-[7.868617057800293, 7.4840803146362305, "[TT] LVDS Image Data Ports of the CSM = Operating Frequency: 25 MHz"]
-[9.447700500488281, 3.6534664630889893, "[FF] Reference Vector of the Magnetometer = Truncated IGRF-11 (International Geomagnetic Reference Field-11) model of the Earth's magnetic field with 2010 coefficients"]
-[10.734169960021973, 3.7962586879730225, "[FF] Solar Sail Deployment Date of the IKAROS = June 11, 2010"]
-[4.767817974090576, -1.8770132064819336, "[FF] Re-entry Module Verification of the Chang'e-5 = Aerodynamic design, heat-resistant materials, flight control system"]
-[13.393730163574219, 6.771456241607666, "[FF] Navigation Payload Power of the GNSS Satellites = Kilowatt"]
-[6.76971435546875, 4.372161388397217, "[TT] Mounting Method of the Avionics = Built up into stacks based on a generic SSTL module box design"]
-[9.91111946105957, 2.3134186267852783, "[TT] Issue of the NuSTAR = Stray light"]
-[4.337573051452637, 2.3010995388031006, "[TT] Launch Site of the DubaiSat-1 = Baikonur, Kazakhstan"]
-[13.218849182128906, 7.316095352172852, "[TT] Average Power of the JAWSAT = 80 W"]
-[7.211707592010498, 1.2618180513381958, "[TT] Function of the Fetch Rover = Collect and deliver samples to Mars Ascent Vehicle"]
-[7.938586711883545, -0.6368209719657898, "[FF] Action of the UK Committee for Antarctic Place-Names = Named 28 mountains, glaciers and bays after modern-day scientists"]
-[11.525561332702637, 3.400458574295044, "[TT] Minimum Impulse Bit of the CNAPS = 0.7 mNs"]
-[4.279882907867432, 2.4490106105804443, "[TT] Launch Locations of the OneWeb = Baikonur Cosmodrome in Kazakhstan, and Vostochny Cosmodrome in Russia"]
-[9.244118690490723, 1.792769432067871, "[TT] Location of the HARPS = Chile"]
-[9.35977840423584, 7.026957988739014, "[TT] Spatial Resolution of the SLSTR = 500 m"]
-[9.122724533081055, -1.2630523443222046, "[TT] Orbit of the Eutelsat 172B = Geostationary"]
-[6.593999862670898, 5.831198215484619, "[TT] System Racks of the PM = 11"]
-[11.278393745422363, 0.9485358595848083, "[TT] Mission End Date of the LISA Pathfinder = 25 June 2016"]
-[7.3020830154418945, 5.053892135620117, "[FF] Components of the Descent Subsystem = Supersonic pilot, supersonic ribbon drogue, subsonic ribbon drogue, ringsail main parachute, mortar, strap-cutters"]
-[8.34539794921875, 8.026122093200684, "[TT] Spectral Band (Pan) of the Pushbroom imager = 0.45-0.9 \u00b5m"]
-[5.851275444030762, 7.066433906555176, "[TT] Maximum Data Rate of the Instrument = 115 Mbit/s"]
-[6.088129043579102, 2.296354293823242, "[FF] Principal Investigator of the NuSTAR = Nanda Rea"]
-[10.051412582397461, -1.5636509656906128, "[TT] Orbit Inclination of the CBERS-4A = 97.9\u00ba"]
-[11.831871032714844, 6.70370626449585, "[TT] Electron Energy Ranges of the EPE = 30-90 keV, 100-200 keV"]
-[5.695109844207764, 6.382002830505371, "[TT] Data Handling of the NOAA POES series fifth generation satellites = Up to five 0.9 Gbit DTRs (Digital Tape Recorder) and up to three 2.7 Gbit SSRs (Solid State Recorder)"]
-[6.157266139984131, 2.2988882064819336, "[FF] Image Credit of the CU = GWU, USNA"]
-[8.06325912475586, 4.279841423034668, "[TT] Test Location of the Thermal Testing = Thermal vacuum chamber on USSC premises"]
-[4.565678119659424, 0.8831538558006287, "[TT] Launch Date of the ADEOS = August 17, 1996"]
-[11.932124137878418, -0.2048947513103485, "[FF] URL of the TESS = https://arxiv.org/pdf/1901.00051.pdf"]
-[5.458280086517334, 2.359090805053711, "[FF] Affiliation of the Shuaib Lwasa = Urban Action Lab, Makerere University"]
-[6.023945331573486, 2.235746145248413, "[TT] Data Center of the Euclid = CosmoHub hosted by PIC"]
-[4.4597015380859375, 7.555722236633301, "[FF] Data Transmission of the VT = Immediate downlink to the ground through the VHF network"]
-[3.954348087310791, 4.268128395080566, "[FF] Field of Regard of the RISAT-2 = Wide"]
-[5.5836992263793945, 5.611677169799805, "[TT] BMU Configuration of the CartoSat-2 = Dual microprocessor configuration, each one acting as redundant processor for all the above functions"]
-[8.128279685974121, -0.6688477396965027, "[FF] Radar Measurements of the CryoSat-2 = Ice"]
-[7.694774150848389, 9.153882026672363, "[TT] Wavelength Range of the Band 2 = 660-685 nm"]
-[5.713411331176758, 1.426332712173462, "[FF] Presentation Date of the Hiroyuki Shindou = Oct. 6-7, 2008"]
-[5.483908653259277, 1.5638165473937988, "[TT] Mission Status of the TEMPO = Commissioning"]
-[10.39401626586914, 5.797226905822754, "[TT] Operating Temperature of the Ground Penetrating Radar = -30\u00baC"]
-[13.72052001953125, 5.3645548820495605, "[TT] Solar Cells of the CartoSat-2 = Advanced triple junction solar cells"]
-[5.297910690307617, 3.9503376483917236, "[TT] Number of Satellites of the BRITE Constellation = 5"]
-[8.739675521850586, 2.869626760482788, "[FF] Mission of the Solar Dynamics Observatory = Investigating the causes of solar variability and how space weather results from that variability"]
-[3.6586625576019287, 5.426120281219482, "[TT] Spotlight Mode Resolution of the Payload = 1-2 m"]
-[5.675170421600342, 3.901911735534668, "[FF] Mission Aim of the ASNARO = Develop next-generation minisatellite bus systems which utilise open architecture techniques and manufacturing methods to reduce the overall cost and development period of a satellite, whilst providing high-resolution Earth observation imaging"]
-[5.030305862426758, 4.281069755554199, "[TT] Program Name of the DASS = DASS"]
-[9.632170677185059, 8.307262420654297, "[TT] Field of View of the SIMBA = Wild"]
-[8.580463409423828, 5.171779155731201, "[FF] Pointing Error of the Hosting Satellite = 1200-1500 \u00b5rad"]
-[6.951807022094727, 1.6306231021881104, "[FF] Primer Version of the James Webb Space Telescope = 1.0"]
-[8.905719757080078, 2.2124745845794678, "[FF] Study Date of the Stardust Grain = Last year"]
-[10.858014106750488, 7.546575546264648, "[TT] Swath width (km) of the SASS = 750+"]
-[14.194896697998047, 3.1352689266204834, "[TT] Mass of the BLITS = 7.5 kg"]
-[6.697732448577881, 4.224720001220703, "[FF] Docking Status of the ATV-5 = De-docked"]
-[10.123543739318848, 0.22790420055389404, "[TT] Formation Distance (Stereo) of the Harmony satellites = 350 km"]
-[4.951793670654297, 3.329495906829834, "[TT] Manufacturer of the ABI instrument = ITT Exelis"]
-[10.268759727478027, 3.16579008102417, "[FF] Image Credit of the 6U CubeSat = BCT, University of Iowa"]
-[9.1466646194458, 4.281933307647705, "[FF] Tracking of the SA (Solar Array) = 360\u00ba about the axis"]
-[7.340625286102295, 3.6832804679870605, "[FF] Radio Occultation Profiles of the Spire = 3,000 profiles a day for six months"]
-[7.217251300811768, 6.587586402893066, "[TT] Integration Time of the SSJ/4 = 0.09 s"]
-[6.817408561706543, 3.519199848175049, "[FF] Purpose of the Commercial off-the-shelf (COTS) Air Tanks = Support gas resupply for routine cabin repress activities on-orbit"]
-[11.02458667755127, 0.5904403924942017, "[FF] System of the Kepler-80g = Resonant chain with four neighboring planets"]
-[3.567223072052002, -0.759473979473114, "[TT] Operation of the NPS = Nightside of the orbit"]
-[12.791946411132812, 7.601606369018555, "[TT] Power Consumption of the GOLD instrument = 72 W"]
-[8.79365348815918, 3.5985779762268066, "[FF] Unknown of the Thermal Plasma Measurement Unit = Unknown"]
-[3.238650321960449, 5.7565484046936035, "[TT] Long Dimension of the SAR Antenna = 15 m"]
-[8.42711067199707, 5.6634955406188965, "[TT] GPS Receiver Resolution of the TDP = 20 m"]
-[5.188565254211426, 1.0893363952636719, "[FF] Launch Date of the AISsat-1 = June 25, 2007"]
-[12.456035614013672, 0.5774208307266235, "[TT] Rotation Interval of the PLATO = 3 months"]
-[8.355006217956543, 5.04819393157959, "[FF] Noise Equivalent Delta Temperature (NEDT) of the E2E simulation = Unknown"]
-[11.196243286132812, 4.980462551116943, "[TT] Diameter of the LARES-2 = 424 mm"]
-[6.954411029815674, 6.103682041168213, "[TT] Number of Instruments of the Envisat = Ten"]
-[10.198684692382812, 8.023431777954102, "[TT] Size of the Planetary Systems Lightband = 15-inch"]
-[9.637755393981934, -1.160843849182129, "[TT] Orbit Position of the SES-17 = 67.1\u00ba W above the equator"]
-[5.583125114440918, 8.017010688781738, "[TT] Frequency in Inertial Mode of the FEP = 1.7 x 10-4 Hz"]
-[5.8445234298706055, -0.6709932684898376, "[TT] Designed Mission Life of the DMSP-14 = Three years"]
-[5.133859157562256, 0.7342312335968018, "[TT] End of Life Date of the ASNARO = 6 November 2019"]
-[9.250527381896973, 1.8541295528411865, "[FF] Design Variables of the Harpoon Test Rig = Projectile configuration, panel type, panel offset, chaser momentum"]
-[8.30847454071045, 5.181266784667969, "[TT] Number of Accelerometers of the Truss = 22"]
-[6.104473114013672, -0.2985067069530487, "[TT] Operation Duration of the FAST Program = Up to 12 months"]
-[5.170953750610352, 1.9584543704986572, "[TT] Mission Status of the Satellite = Operational (extended)"]
-[8.980813980102539, 7.504354000091553, "[TT] Visible Channel Resolution of the Imager = 1 km"]
-[8.537551879882812, 5.561773777008057, "[FF] Position Determination Accuracy of the SEXTANT = Expected to be on the order of hundreds of meters"]
-[8.169702529907227, 0.46587374806404114, "[TT] Lowest Level Date of the Lake Powell = 1980"]
-[4.362509250640869, 3.198509931564331, "[TT] Location of the Backup Ground Station = Bordon, UK"]
-[6.722578525543213, 4.300192356109619, "[FF] Function of the Coud\u00e9 Laboratory = Allows experiments to be set up efficiently in a laboratory environment"]
-[9.122404098510742, 6.105499267578125, "[FF] Observation Range of the Limb Sensing Instrument = Tangent radius upward"]
-[6.4110331535339355, 1.9830317497253418, "[FF] URL of the Aleph-1 Constellation = https://satellogic.com/technology/constellation/"]
-[9.022233009338379, 0.5464595556259155, "[FF] ORM and FTM Event Designation of the ARTEMIS = Serially from 1 (ORM1, ORM2, etc)"]
-[5.347756385803223, 0.9886457324028015, "[FF] Presentation Date of the Timepix = June 2-8, 2013"]
-[13.962512016296387, 3.00305438041687, "[FF] Mass of the HAUSat-1 = Unknown"]
-[4.324809551239014, 2.987337827682495, "[TT] Downlink Destination of the TT&C = Svalbard"]
-[5.318904399871826, 5.948968410491943, "[TT] Ground Contacts per Day of the LDCM spacecraft = Up to 35"]
-[11.62948989868164, 4.551578998565674, "[TT] Surface Cohesion of the Didymos = 3 to 6 Pascals"]
-[5.18028450012207, 2.6078333854675293, "[TT] Mission Type of the TechEdSat = Non-EO"]
-[7.900805473327637, 4.1383843421936035, "[FF] Purpose of the 6DOF Control with Thrusters = Repeat the formation maneuvers controlling the relative spacecraft position and attitude only with the thrusters"]
-[6.5909576416015625, 4.767599582672119, "[FF] Function of the EM = Status reporting, monitoring, configuration and asset management"]
-[7.789092540740967, 5.5266947746276855, "[FF] Tracking Method of the Payload = Time-resolved optical density and absorbance measurements"]
-[14.57149600982666, 6.607059001922607, "[TT] Type of the Photocathode = Bi-alkali"]
-[7.485434532165527, 0.38131818175315857, "[TT] Visible and Infrared Spectrometer of the OSIRIS-REx = OVIRS"]
-[9.26041316986084, 1.0041767358779907, "[TT] Transit Time to Jupiter of the Juno spacecraft = About three years"]
-[10.228633880615234, 6.591519355773926, "[TT] East-West Movement of the Mirror = 280 \u00b5rad"]
-[7.959270000457764, 2.76651930809021, "[FF] Error Assimilation Purpose of the LI System = Improve very short range forecasts of severe convective events"]
-[10.430145263671875, 5.513205051422119, "[TT] Surface Temperature of the Zeta Puppis = Seven times hotter than our sun"]
-[11.007354736328125, 5.156242847442627, "[FF] Measurement Parameters of the CITRIS = Total electron content (TEC) and scintillation parameters"]
-[8.686605453491211, 2.079848527908325, "[TT] IFOV of the SeaWinds = \u00b152\u00ba from nadir"]
-[3.174624443054199, 2.316530466079712, "[FF] Objectives of the Other Sentinel missions = Radar mapping of land and sea, air quality, and sea-surface topography and temperature"]
-[11.889598846435547, 3.0847010612487793, "[TT] Delta V of the PROP unit = 10 m/s"]
-[14.11963939666748, 3.162428379058838, "[TT] Mass of the WFI = 43 kg"]
-[11.093039512634277, 6.125072956085205, "[FF] Form of the Glass Layers = ~60\u00ba sectors and ~30\u00ba sectors"]
-[14.207015991210938, 3.1923654079437256, "[TT] Mass of the CanX-2 = 3.5 kg"]
-[6.9972639083862305, -0.3354121744632721, "[TT] Signal Reception Time of the MarCO-B = 11:31 am"]
-[7.902182579040527, -0.9097493886947632, "[TT] Data Downloads of the ICESat-2 = About 500,000"]
-[6.834598064422607, 7.49074125289917, "[TT] Resolution of the A/D converter = 5 bit"]
-[4.932861804962158, 0.5639166235923767, "[TT] Launch Date of the MicroMAS-2a = 12 January 2018"]
-[16.50108528137207, 3.583893060684204, "[TT] Partial Service Launch Timeline of the OneWeb = Next 60-90 days"]
-[7.883755207061768, 7.200689315795898, "[TT] Frame Rate of the Camera = More than 10,000 frames/s"]
-[5.742702484130859, 5.236605644226074, "[TT] Operating System of the OBC = RTEMS (Real-Time Executive for Multiprocessor Systems)"]
-[10.890926361083984, 7.489494323730469, "[TT] Swath of the FRS-2 = 25 km"]
-[6.0975470542907715, 3.396709442138672, "[TT] Number of Experiments of the OPS-SAT = Over 100"]
-[5.559046745300293, 2.648800849914551, "[TT] Mirror Data Archive Provider of the NuSTAR = ASI"]
-[5.477546215057373, 4.698422908782959, "[FF] Mission Objective of the UWE-1 = Analyze and optimize different implementations of Internet protocols in space"]
-[6.440612316131592, 0.5612866878509521, "[TT] Number of Atmospheric Profiles per Day of the FORMOSAT-7/COSMIC-2 Constellation = More than 4000"]
-[8.832033157348633, 5.147681713104248, "[TT] Pointing Accuracy of the BOKZ-M star tracker = 2 / 20 arcsec (x, y / z)"]
-[5.075711250305176, 7.053889274597168, "[TT] Data Rate (Downlink) of the S-band telemetry system = 1 Mbit/s"]
-[11.799242973327637, 6.723948001861572, "[TT] Integral Electron Fluxes Energy Range of the MSGI-MKA = Up to 40 keV"]
-[8.119624137878418, 8.21324348449707, "[TT] 2 km to 2 km, 1 km, 0.5 km (wavelength/detector dependent) of the Channel-to-Channel Registration = \u00b1 6.3 \u00b5rad"]
-[10.351703643798828, 4.583111763000488, "[FF] Life-Test Status of the NIRISS Dual Wheel Cryogenic Mechanism = Not Provided"]
-[14.12460994720459, 7.2239909172058105, "[TT] Voltage of the 28V main bus = 28V"]
-[5.10890531539917, 2.6834182739257812, "[TT] Mission Operations Center of the NuSTAR = University of California Berkeley"]
-[10.922470092773438, 2.844215154647827, "[TT] Number of Microsatellites of the ANDE-2 = 2"]
-[5.996159076690674, 6.981984615325928, "[TT] LEO-to-ground Communication Link Speed of the Optical Ground Station = 5.625 Gbit/s"]
-[5.832498073577881, -2.243759870529175, "[TT] Orbit Altitude of the KOMPSAT-3 = 685.1 km"]
-[11.122369766235352, 1.016032099723816, "[TT] Spread of the LISA Laser Beam = About 20 km"]
-[4.433953285217285, 2.735738754272461, "[TT] Setting Up Date of Receiving Station in Sodankyl\u00e4, Finland of the COSMO-SkyMed = Before the end of 2012"]
-[9.22807502746582, 5.152510643005371, "[TT] Attitude Subsystem Pointing Error of the Spacecraft = 0.15\u00ba (3\u03c3)"]
-[13.604235649108887, 5.502521514892578, "[TT] Solar Cells per Panel of the TCS = 19"]
-[6.424814224243164, 4.53026008605957, "[TT] Location of the ISSAC SOC = UND"]
-[4.829155921936035, 7.122913837432861, "[TT] Data downlink of the ALOS-3/PRISM-2 = 800 Mbit/s (X- and Ka-band)"]
-[6.950924396514893, 4.2602219581604, "[FF] Unknown of the ScaRaB = Unknown"]
-[4.830015182495117, 8.073351860046387, "[TT] Frequency of the NSCAT = 13.995 GHz"]
-[7.284885406494141, 5.3235321044921875, "[TT] Monitoring Frequency of the TSIS-1 SIM = Every 12 h"]
-[9.20168399810791, 3.1847758293151855, "[FF] Mission Type of the Cluster = Magnetosphere Measurement"]
-[7.715817451477051, 5.423717021942139, "[FF] Instrument of the SMOS = Microwave instrument"]
-[6.324592113494873, -0.7813338041305542, "[TT] Total Spacewalking Time of the Shane Kimbrough = 52 hours and 43 minutes"]
-[4.718663692474365, 5.998991012573242, "[TT] Technology of the Ground Station = SDR (Software Defined Radio)"]
-[6.429059028625488, 2.111804246902466, "[FF] URL of the Advanced Communication Technology Satellite (ACTS) = http://www.nasa.gov/centers/glenn/multimedia/artgallery/art_feature_006_ACTS.html"]
-[9.492476463317871, 7.141504287719727, "[TT] Spatial Resolution of the Sensor = 6.8 km"]
-[4.173832416534424, 2.073496103286743, "[TT] Mission Status of the NigeriaSat-2 = Operating nominally"]
-[8.363005638122559, 2.7945642471313477, "[TT] Measurement Domain of the CASSIOPE = Gravity and Magnetic Fields"]
-[7.848264694213867, -2.486302375793457, "[FF] Retrieved Thermospheric Temperatures of the GOLD = Unknown"]
-[9.001423835754395, 3.259488582611084, "[FF] Atmosphere Color of the Pluto = Blue"]
-[6.904419898986816, 0.7633959650993347, "[TT] Technology Demands of the GP-B probe = Extreme"]
-[6.2685465812683105, 5.620513439178467, "[TT] Former Name of the GIOVE-B = GSTB-V2/B"]
-[3.3993043899536133, 4.924027919769287, "[FF] Modes of the MRSE = SAR, Scatterometer, Radiometer"]
-[6.256231307983398, 2.094116449356079, "[TT] Project Lead of the TEMPO = Kelly Chance from the Smithsonian Astrophysical Observatory (SAO)"]
-[1.7461167573928833, -2.0748369693756104, "[TT] Solar Conjunction Operation Period of the Hayabusa-2 = Late November 2018 until the end of December 2018"]
-[9.847905158996582, 4.777836322784424, "[TT] Spin Stabilization of the MightySAT I = 3 rpm"]
-[4.452952861785889, 7.046004295349121, "[TT] Ka-band System of the STPSat-6 = SpaceWire command, control, and telemetry to the spacecraft"]
-[7.374757289886475, 1.5752007961273193, "[TT] Development Period of the Argo Float = 1990-1997"]
-[4.404139995574951, 3.0871071815490723, "[TT] Location of the LRAC = Kiruna"]
-[4.909626007080078, -0.24317577481269836, "[TT] Launch Time of the SpaceX CRS-22 = 17:29 UTC (1:29 EDT)"]
-[5.775374412536621, 0.7537119388580322, "[FF] Discovery Date of the Elves = Unknown"]
-[2.900759220123291, 1.9564403295516968, "[FF] Image Capture Date of the Copernicus Sentinel-2 = April 8, 2022"]
-[7.873926639556885, -0.812485933303833, "[TT] Data Center of the ICESat-2 = NASA National Snow and Ice Data Center Distributed Active Archive Center (NSIDC DAAC)"]
-[13.794461250305176, 2.9437811374664307, "[TT] Dry Mass of the EAGLE ESPAStar = 430 to 470 kg"]
-[7.4279961585998535, 6.383317470550537, "[TT] Data Generation Interval of the IMERG = Half hourly"]
-[6.6639323234558105, 3.7112629413604736, "[FF] Purpose of the DSX = Develop technologies to protect low Earth orbiting (LEO) satellites from the effects of HANE (High Altitude Nuclear Explosions)"]
-[9.075446128845215, 5.044301986694336, "[FF] Function of the Gyrocompassing = Maintain yaw attitude"]
-[13.134016990661621, 7.20033597946167, "[TT] Collection Power of the IMAP-Ultra = ~ 35 x"]
-[5.769392967224121, -0.4674169421195984, "[TT] Lifetime of the EDRS-C = 15 years"]
-[3.4658493995666504, 5.210921764373779, "[TT] Frequency of the RISAT-SAR = 5.35 GHz"]
-[10.355867385864258, 4.500682830810547, "[TT] Quantity of the Reaction wheels = Three wheels"]
-[13.479360580444336, 2.8883326053619385, "[TT] Mass of the FormoSat-7/COSMIC-2 satellites = 280 kg"]
-[9.734719276428223, 6.280681133270264, "[TT] Parallelism Maintenance of the Moving Mirror Alignment and Suspension Control System = Within 1.9 x 10-4 degrees"]
-[5.112818241119385, 6.942907810211182, "[TT] Download Transmission Rate of the DubaiSat-2 = 160 Mbit/s"]
-[9.791969299316406, 4.229773044586182, "[FF] Instrumentation of the AMS-02 = Before and after magnet change"]
-[10.310263633728027, 4.540406227111816, "[FF] Reaction Wheel Configuration of the AlSat-2A = Pyramid configuration"]
-[9.167892456054688, 3.5020172595977783, "[FF] Function of the EON-IR = Earth Observation Nanosatellite -Infrared"]
-[10.107858657836914, 1.5084792375564575, "[TT] Host Galaxy of the Sw J1644+57 = Distant"]
-[3.9475603103637695, 1.6113313436508179, "[FF] Launch Campaigns of the Soyuz and Ariane 5 = Continuing"]
-[10.130730628967285, 1.4750807285308838, "[FF] Type of the M83 = Barred spiral galaxy"]
-[6.589100360870361, 1.8833081722259521, "[FF] Concept of the TransHab = URL: http://spaceflight.nasa.gov/history/station/transhab/"]
-[4.895463466644287, 6.906184196472168, "[TT] Model of the AMERGINT softFEP-9000 modem = softFEP-9000"]
-[5.3440842628479, 0.9817405939102173, "[FF] Rejoining Date of the Biden administration = Not yet clear"]
-[6.187047004699707, 2.4985783100128174, "[FF] Image Credit of the Vikram Lander = NASA/Goddard/Arizona State University"]
-[5.22053861618042, 0.6057251691818237, "[TT] Launch Date of the MidSTAR-1 = 9 March 2007"]
-[5.650200366973877, 6.724413871765137, "[TT] Data Delivery of the Command and Telemetry Interface = 3-byte commands and 64-byte ancillary data"]
-[8.478998184204102, 1.7720484733581543, "[TT] Absolute Accuracy of the Cloud water = \u00b1 0.1 kg/m 2"]
-[14.31845760345459, 3.1007864475250244, "[TT] Mass of the SHIROP = 19.4 kg"]
-[5.04538106918335, 8.309391975402832, "[TT] Platform of the 118 GHz Radiometer = Aircraft"]
-[10.004216194152832, 4.544707775115967, "[FF] Thrust Vector Control of the IFM Nano AR3 thruster = Redundancy measure for reaction wheel desaturation in two axes"]
-[3.4355435371398926, 1.5777515172958374, "[FF] Arrival Date of the Sentinel-1A = Feb. 24-28, 2014"]
-[6.543004035949707, 6.312828540802002, "[TT] Reliability Rate of the EDRS-SpaceDataHighway = 99.8 percent"]
-[6.991209506988525, 0.1458214521408081, "[TT] Formation Time of the Pilbara and Yilgarn = About 2.2 billion years ago"]
-[14.253677368164062, 3.2484841346740723, "[TT] Mass of the Overview-1A = 4.2 kg"]
-[6.209878444671631, 5.3052191734313965, "[FF] Communication Changes Article of the Optical Inter-orbit Communications Engineering Test Satellite (OICETS) = Takashi Jono"]
-[5.2563581466674805, 0.8195446729660034, "[FF] Design File Transmission Date of the Ratchet Wrench = Unknown"]
-[5.131896495819092, 2.8287665843963623, "[TT] Operator of the Resurs-DK1 = Russia's Science Center for Remote Sensing of Earth, NTs OMZ"]
-[6.562824726104736, 1.1999495029449463, "[FF] Observation Date of the Giant Meterwave Radio Telescope (GMRT) = Unknown"]
-[13.390247344970703, 7.328780174255371, "[TT] Up to 15 W of the CLAVIS = True"]
-[9.710131645202637, -1.1945236921310425, "[TT] Position of the SES-14 = 47.5 degrees West"]
-[6.101114749908447, -0.5306079983711243, "[TT] Operation Time of the FY-3D = 8 years"]
-[10.74187183380127, -0.18757911026477814, "[TT] Formation Flying Separation of the TanDEM-X = 200m"]
-[6.148219585418701, 6.175877094268799, "[TT] Data Relay Delay of the MarCO = Not more than a few minutes"]
-[9.598311424255371, -0.34308117628097534, "[TT] Altitude of the SpinSat = 242.95 km"]
-[5.320399284362793, 3.256432294845581, "[TT] Operator of the Gonets-M No.3 = Gonets Satellite Company"]
-[6.7226643562316895, -0.42216169834136963, "[FF] Visibility Time of the EDRS = Around 50% of the LEO satellite\u2019s orbital period"]
-[10.91805362701416, 7.522229194641113, "[TT] Size of the 2020 GE = About 65 feet (20 meters) in diameter"]
-[8.97269058227539, 8.218276977539062, "[FF] Radiometer Performance of the Telescope = SNR > 200 for 25% albedo NEDT < 1.0 K at 260 K NEDT < 1.0 K at 260 K"]
-[11.827313423156738, 5.048558235168457, "[TT] Dimensions of the AlSAT-1 = 0.6 m x 0.6 m x 0.6 m"]
-[9.919984817504883, 4.399003505706787, "[FF] Components of the ADCS = 3 magnetorquers: two torque rods and one air coil torquer"]
-[9.272547721862793, 3.206047773361206, "[FF] Purpose of the CCOR = Image the solar corona and help detect and characterize CMEs"]
-[10.233510971069336, 4.523024559020996, "[FF] Actuators of the Slew Mode = Reaction wheels as the primary actuators, and torque rods"]
-[5.55648946762085, 2.607736825942993, "[FF] Development Team of the MiniCOR = NRL (Naval Research Laboratory), NASA/JPL, the University of Michigan, and JHU/APL (Johns Hopkins University/Applied Physics Laboratory)"]
-[4.904970169067383, 3.552269458770752, "[TT] Operation Center of the EDR-2 = CADMOS, the French User Support Operations Centre located in Toulouse, France"]
-[7.721377849578857, 2.044680118560791, "[TT] Primary Use of the Band 8 = Ocean color"]
-[10.336465835571289, 4.522528648376465, "[TT] Quantity of the Reaction Wheels = 4 on each S/C"]
-[6.1241559982299805, 7.521585464477539, "[FF] Signal Transmission of the GIOVE-A = L1+E5 or L1+E6"]
-[6.793445110321045, 1.8140710592269897, "[FF] URL of the MEOSAR = http://searchandrescue.gsfc.nasa.gov/dass/spacesegment.html"]
-[4.91978645324707, 0.26370474696159363, "[TT] Installation Date of the Bartolomeo = 2 April 2020"]
-[1.8128358125686646, -2.0429437160491943, "[FF] Purpose of the Hayabusa-2 Deployable Camera (DCAM3) = Observation of impact simulation on asteroid"]
-[7.116634368896484, 0.17895975708961487, "[TT] Extinction of the Ichthyosaurs = The creatures are now extinct"]
-[3.4626824855804443, -0.857121467590332, "[TT] Orbit Type of the EarthDaily Constellation = Sun-synchronous"]
-[11.859230995178223, 4.4920477867126465, "[TT] OBC of the Spacecraft = LEON3 FT"]
-[6.4956231117248535, 3.3706066608428955, "[TT] Resolution of the BlackSky Global Satellite = 1 meter"]
-[5.827183246612549, 7.059183120727539, "[TT] Data Rate of the SDF (TF or LF) = 1.33 MBit/s"]
-[7.065324306488037, 1.1553388833999634, "[FF] Release Date of the Haa Alif Atoll, Maldives = June 5, 2014"]
-[10.943255424499512, 7.569507122039795, "[TT] Swath Width of the OLS = 2960 km"]
-[9.184663772583008, 3.0600695610046387, "[FF] Magnetic Field Profile of the Solar Flare = Matched the theoretical prediction"]
-[8.0368013381958, 0.8430467247962952, "[FF] Partners of the U.S. Drought Monitor program = U.S. Department of Agriculture, the National Oceanic and Atmospheric Administration, and the University of Nebraska\u2013Lincoln"]
-[11.578457832336426, 3.3295786380767822, "[FF] Ion Propulsion System of the GOCE = Commissioned"]
-[4.521941661834717, 3.1479008197784424, "[FF] Direct Data Reception Locations of the TerraSAR-X = US, Japan, and Germany"]
-[3.290902853012085, 4.851818084716797, "[TT] Imaging Radar Instrument (SAR) of the SeaSat = Flown in 1978"]
-[7.090630531311035, -0.8274190425872803, "[TT] Orbital Period of the GJ 367 b = Only one-third of an Earth day"]
-[3.7134528160095215, 4.719742774963379, "[FF] Type of the CRATEX (C-band Radar Transponder Experiment) = Eliminated"]
-[9.603238105773926, 6.318122863769531, "[TT] Mirror Mounting Angle of the Scan Mirror Mechanism = 45\u00b0"]
-[7.707055568695068, 3.252901077270508, "[FF] Independence of the PRARE = Weather and daylight conditions"]
-[9.892348289489746, 1.4410476684570312, "[FF] Publication Date of the Colliding star clusters = 3 January 2022"]
-[10.387628555297852, 3.226654052734375, "[TT] Number of CubeSat Units of the NPS-SCAT = 1"]
-[3.3212802410125732, 5.665997505187988, "[TT] Number of Elements of the ICEYE SAR Antenna = 5"]
-[3.3640177249908447, 5.15386962890625, "[FF] Polarizations of the Integrated SAR Antenna = Both"]
-[8.535468101501465, 6.257711887359619, "[TT] Target Accuracy of the MicroSCOPE = 10-15"]
-[6.14475154876709, 2.2600033283233643, "[TT] Principal Investigator of the Genesis = Donald Burnett"]
-[10.684900283813477, 7.330000877380371, "[TT] Swath Width of the CAPI instrument = 400 km"]
-[4.169193267822266, 1.3994249105453491, "[TT] Launch Date of the Meteosat-7 = 1995"]
-[8.33564281463623, 0.7542573809623718, "[TT] Wind Speed of the Calf Canyon-Hermits Peak fire = 65 miles (105 km) per hour"]
-[4.328157901763916, 7.810353755950928, "[TT] Downlink Frequency of the RF communications system = 2.2-2.3 GHz"]
-[7.589964389801025, -2.3818142414093018, "[FF] Project Manager of the GOLD = LASP"]
-[5.820996284484863, 6.293896675109863, "[TT] Total Storage Capacity of the SSRU = Approximately 17,000 km2 of imagery"]
-[6.875856876373291, -0.6104307174682617, "[TT] Orbital Period of the Shakuntala = 94.0 minutes"]
-[8.168699264526367, 5.951395511627197, "[TT] Interface of the Google Earth = Camera"]
-[8.508806228637695, 0.023844962939620018, "[TT] Depth of the South Pole-Aitken Basin = 13 km"]
-[10.41464900970459, 5.544318199157715, "[TT] Surface Temperature of the Primary Star = around 17,500 \u00baF (9,700\u00baC)"]
-[5.206398963928223, -1.2314726114273071, "[FF] Funding of the Kondor-E = Cut by the end of the decade"]
-[5.558358669281006, 7.206474781036377, "[TT] Net Bit Rate of the LCT = 1800 Mbit/s"]
-[8.134119987487793, 4.630106449127197, "[TT] Tolerant to Total Ionizing Dose of the TriG = 40 kRad"]
-[6.3614678382873535, 1.8300259113311768, "[FF] Address of the URL = http://elib.dlr.de/89312"]
-[4.862359523773193, 8.305831909179688, "[TT] Operating Frequencies of the MWR = 23.8 and 36.5 GHz"]
-[10.641432762145996, 1.7235233783721924, "[FF] Rotation Frequency of the Neutron Star = Rapidly increasing"]
-[6.5307936668396, -1.9756687879562378, "[TT] Design Lifetime of the Jason-3 = 5 years"]
-[6.836302280426025, 6.9726715087890625, "[TT] Number of gateway beams of the Al Yah-3 = 4"]
-[13.352455139160156, 7.80021333694458, "[TT] RF Output Power of the VHF COTS transmitter = 22 dBm"]
-[8.334039688110352, 2.4585275650024414, "[FF] Authors of the Case studies of aerosol retrievals = J. B. Chowdhury, B. Cairns, L. D. Travis"]
-[6.664981842041016, 2.4081637859344482, "[TT] Flatness Target of the Euclid = 0.05 mm"]
-[4.616725444793701, 1.1971099376678467, "[TT] Acquisitions per Day of the SAOCOM-1A = 225"]
-[4.42085075378418, -0.23857100307941437, "[TT] Launch Date of the Nauka = No earlier than 15 July"]
-[6.989749908447266, 7.521573543548584, "[TT] Resolution of the NewMag = 16 bit (\u00b10.2 nT)"]
-[9.858078002929688, 1.6381642818450928, "[FF] Publication Date of the A Hubble Diagram for Quasars = Dec. 3, 2015"]
-[9.400629997253418, 2.31512188911438, "[TT] Gigantic Jets Percentage of the ISUAL = 0.30%"]
-[9.460719108581543, 3.883774518966675, "[FF] Calibration Method of the AMI-302 = Current varying among several fixed values is applied to a coil that generates a constant magnetic field for the three axes"]
-[4.762362957000732, 7.446447372436523, "[TT] Data Rate of the UHF Transceiver = 9.6 kbit/s"]
-[6.466279983520508, 0.2474224865436554, "[TT] Program of the Skylab-1 = Apollo Applications Program (AAP)"]
-[8.192476272583008, 5.519076347351074, "[TT] Accuracy of the DORIS = About 1m"]
-[4.2097673416137695, 2.56711483001709, "[TT] Launch Site of the Launch Segment = Guiana Space Center"]
-[9.972073554992676, 1.945644736289978, "[FF] Image Location of the NuSTAR = Center of our Milky Way galaxy"]
-[7.678422451019287, 9.417842864990234, "[TT] Center Wavelength of the Band 4 = 1.378 \u00b5m"]
-[3.420105457305908, 3.626760244369507, "[FF] Symposium Date of the PAZ = July 26-31, 2015"]
-[10.930468559265137, 7.603029251098633, "[TT] Swath Width of the WCOM = Over 1000 km"]
-[6.751821041107178, 5.828248500823975, "[TT] Quantity of the FLGS / B-FLGS = 2"]
-[13.38283634185791, 6.88777494430542, "[TT] Power of the SES-17 = 15 kW"]
-[6.023843288421631, 6.407957553863525, "[TT] Latency of the ISL = High"]
-[8.123713493347168, 4.517210483551025, "[FF] Conference Date of the 3D Imaging Electromagnetic Calorimeter = April 2, 2004"]
-[9.22046184539795, 6.893507957458496, "[TT] Image Resolution of the Gen-3 satellites = 50-cm"]
-[4.268892288208008, 3.284815549850464, "[TT] Deputy CEO of the Galileo 2nd Generation Satellites = Massimo Claudio Comparini"]
-[5.68208122253418, 2.329993963241577, "[TT] Normal Size of the Upgrade Team = About 30 experts"]
-[6.329473495483398, -0.23574693500995636, "[TT] Attitude Manoeuvring Time of the ALOS-2 = Up to 3 minutes from right- to left-looking (or from left- to right-looking)"]
-[7.415104866027832, 4.66416597366333, "[FF] Mounting Location of the SPS head = In front of the instrument Tube"]
-[2.9965200424194336, 4.390177249908447, "[FF] Observation Data of the PALSAR-2 = Useful for disaster monitoring"]
-[3.121473789215088, 3.8974335193634033, "[FF] URL of the NovaSAR-1 = http://www.eotechcluster.org.uk/eotechcluster/documents/novasar-overview-for-rspsoc-sep12.pdf"]
-[9.926188468933105, 4.42338228225708, "[TT] Actuators of the ADCS = Three in-house designed magnetorquer coils"]
-[6.486935615539551, 3.585721015930176, "[FF] Mission of the DMSP = Provide global visible and infrared cloud data and other specialized meteorological, oceanographic and solar-geophysical data in support of world wide Department of Defense (DoD) operations"]
-[5.709723949432373, 0.19947457313537598, "[TT] End of Mission Date of the KIZUNA = March 1, 2019"]
-[8.716231346130371, 2.8012192249298096, "[FF] Mission Objectives of the TIMED = Determine the temperature, density and solar wind structure in the MLTI region, including the seasonal and latitudinal variations"]
-[4.582930088043213, 7.075287818908691, "[TT] X-band Downlink Transmission Frequency of the CBERS-2B = 8103 and 8321 MHz"]
-[6.957993984222412, 0.8424248099327087, "[FF] Presentation Date of the InSight Mars Mission = 27 April 2017"]
-[13.521245956420898, 6.595109462738037, "[FF] Total Energy of the Station Keeping = Roughly half the amount needed for initial orbit raising"]
-[11.715761184692383, 6.759537220001221, "[TT] Sensitive Range of the XRD = 2 keV \u2013 15 keV"]
-[5.7956109046936035, 7.379310131072998, "[TT] Data Reduction Factor of the GimmeRF = About 2.4 x 10^6"]
-[8.606789588928223, 7.497287750244141, "[TT] Pixels per PMT of the PMT (Photomultiplier Tube) = 4"]
-[7.7536773681640625, 6.637090682983398, "[TT] Camera Warm Up Time of the Voyager 1 = 3 hours"]
-[10.167137145996094, 3.284135580062866, "[FF] Deployment of the Reflectarray Antenna = Can be folded down against the CubeSat"]
-[10.652092933654785, 3.3781957626342773, "[TT] Quantity of the MP6 6U CubeSat = 4"]
-[7.855051040649414, 0.5734767913818359, "[FF] URL of the Near Earth Asteroid Scout = https://web.archive.org/web/20220815171855/https://ieeexplore.ieee.org/document/8742190"]
-[5.407498359680176, 4.344503402709961, "[FF] Ground Earth Stations of the MSAS = Kobe Aeronautical Satellite Center and the Hitachi-Ota Aeronautical Center"]
-[6.28376579284668, 2.5105342864990234, "[FF] Purpose of the Orion MPCV = Carry the crew to space, provide emergency abort capability, sustain the crew during the space travel, and provide safe reentry from deep space return velocities"]
-[5.334561824798584, 5.484494209289551, "[TT] Standard of the Telecommand function = ESA CCSDS packet telecommand standard tailored for G-PUS"]
-[14.020513534545898, 4.016633987426758, "[TT] 1.4 kg/sensor head (including HVPS and preamplifier) of the Instrument Mass = Instrument mass 1.4 kg/sensor head (including HVPS and preamplifier)"]
-[9.321124076843262, -1.681830644607544, "[FF] Swarm Size of the Desert Locusts = 40 million locusts"]
-[8.23057746887207, -0.7355107069015503, "[TT] Measurement Methods of the Ice type = 3 ways"]
-[5.16417121887207, 2.9000585079193115, "[TT] Provider of the MHS = EUMETSAT"]
-[6.636062145233154, 1.68759024143219, "[FF] Experiment URL of the ETS-VII = http://www.astro.mech.tohoku.ac.jp/~yoshida/ETS-VII/presentation.PDF"]
-[9.030610084533691, 5.615307807922363, "[TT] Pointing Requirement of the ADCS = 1\u00ba"]
-[5.8651251792907715, 2.9343957901000977, "[TT] Mission Cost of the ROSE-L = \u20ac190 million"]
-[6.760339260101318, 6.560153007507324, "[TT] Repetition Rate of the Fixed Platforms = 200 seconds"]
-[7.810737133026123, 8.187376022338867, "[TT] Number of Bands of the R3 Sensor = 6"]
-[10.372550964355469, 7.400888442993164, "[TT] Swath Width of the Scanner Assembly = 800 km"]
-[10.389747619628906, 2.1083390712738037, "[FF] Complements of the NuSTAR = Telescopes that observe lower-energy X-ray light, such as XMM-Newton and NASA's Chandra X-ray Observatory"]
-[5.994895935058594, 0.4329366683959961, "[FF] Operations Schedule of the Mission Plan = Weekly"]
-[6.445757865905762, 1.4052224159240723, "[FF] Mission Status Presentation of the COSMO-SkyMed = EUSAR 2018 (12th European Conference on Synthetic Aperture Radar), Aachen, Germany, June 4-7, 2018"]
-[9.076454162597656, 1.357835292816162, "[TT] Upgrade Duration of the Voyager 2 = About 11 months"]
-[8.18921184539795, 5.014199256896973, "[FF] Functionality of the VBS CHU = Attitude pointing and navigation information"]
-[6.758436679840088, 4.762123107910156, "[FF] Function of the AOCS = Navigation, guidance, and control"]
-[5.88657283782959, 5.940333843231201, "[TT] Data Collection Capacity of the Corvus-BC = Up to 150 million square kilometres per day"]
-[6.242983818054199, 6.872401237487793, "[TT] Tracking Rates of the Astro-APS = 10 Hz"]
-[4.462575435638428, 7.769871234893799, "[TT] Frequency of the Uplink (VHF) = 150 MHz"]
-[9.419039726257324, 2.322331428527832, "[FF] Blue Jets of the ISUAL = 13.51%"]
-[13.392470359802246, 2.9380829334259033, "[TT] Mass of the NorSat-1 = < 30 kg"]
-[5.109364032745361, 2.030143976211548, "[TT] Mission Status of the EXPORTS = Operational (nominal)"]
-[4.743392467498779, 1.0697810649871826, "[FF] Development Status of the 3MI = PDR completed in October 2015, moving toward a CDR scheduled in January 2018"]
-[7.7836103439331055, 5.226708889007568, "[FF] Vibration Test of the STM = Passed"]
-[8.022546768188477, 1.8512673377990723, "[FF] Trend of the Evapotranspiration = 2.30 mm per year"]
-[6.542203426361084, 1.0616910457611084, "[FF] Observation Area of the FORMOSAT-7/COSMIC-2 = Global meteorology, climate and ionosphere"]
-[10.35217571258545, 5.7852888107299805, "[TT] Operating Temperatures of the Low-temperature system = 80 K and 2.5 K"]
-[8.388240814208984, 2.4703547954559326, "[FF] Location of the Aerosol Images = Ganges river"]
-[6.3416266441345215, 2.181450366973877, "[TT] Principal Investigator of the Cluster S/C = A. Balogh"]
-[5.942759990692139, 0.5998361706733704, "[TT] Arrival Date to Lunar Orbit of the CAPSTONE = November 13, 2022"]
-[7.611441135406494, 3.1128273010253906, "[FF] Purpose of the AEISS = Advanced Earth Imaging"]
-[10.485383033752441, 2.9031147956848145, "[FF] Design of the CanX Nanosatellites = Adaptable, Multi-Mission"]
-[5.519298553466797, 6.3540449142456055, "[TT] Usage of the SD Card = Payload data storage"]
-[7.5549139976501465, 6.089382648468018, "[FF] Function of the RTEP = Averages the output from the focal plane over a number frames on a pixel-by-pixel basis to generate a background estimate"]
-[9.0372896194458, 4.485774517059326, "[TT] Platform Orientation of the Sich-2 = Sun-oriented in standby mode"]
-[6.314450263977051, 3.2370550632476807, "[TT] Satellite of the VIIRS = NOAA-NASA Suomi NPP"]
-[6.604113578796387, 5.550379753112793, "[TT] State-of-Health of the EPS = Normal"]
-[9.028423309326172, 3.72493314743042, "[FF] Performance Measurement Frequency of the Solar Array = Approximately every two minutes"]
-[5.448957443237305, 1.861086130142212, "[TT] VAB Crossings and Perigee Operations of the ABEX = No transmissions are planned"]
-[13.993425369262695, 2.9666295051574707, "[TT] Weight of the SPOT-1 = 1800 kg"]
-[14.24094295501709, 3.234779119491577, "[TT] Total Mass of the IMS-2 = 199 kg"]
-[6.274880409240723, 8.18801212310791, "[TT] No of bands/channels of the TOU = 6"]
-[8.994416236877441, 6.343746662139893, "[FF] Limb- and Nadir-viewing Observation Techniques of the OMPS = Employed on the future NPOESS (National Polar-orbiting Operational Environmental Satellite System) missions"]
-[9.25858211517334, 3.1155037879943848, "[FF] Measurement of the WISPR = Solar Wind Properties"]
-[8.616188049316406, 8.791447639465332, "[TT] Light Energy Separation Method of the OCO-3 = Diffraction grating"]
-[6.9150776863098145, 9.064428329467773, "[TT] Band Center of the POLDER-1/2 = 910 nm"]
-[8.048896789550781, 1.720052719116211, "[FF] Detection Capability of the Satellite-based Radar = Ripples and splashes caused by falling raindrops"]
-[4.717824935913086, 8.433115005493164, "[TT] Center Frequency of the T/R module = 5.405 GHz"]
-[5.291764259338379, 1.1263552904129028, "[FF] Conference Presentation Date of the STSat-2 = March 3-5, 2005"]
-[8.302070617675781, 0.06354828178882599, "[FF] Location of the Philae lander = Wedged into a dark crack on Comet 67P/Churyumov\u2013Gerasimenko"]
-[6.087525844573975, 4.821526050567627, "[FF] Function of the DHS = Records experimental results, stores them locally, and then communicates those results to the spacecraft for download to the ground station"]
-[13.305161476135254, 7.6413187980651855, "[TT] Power Consumption of the Antenna = Very low"]
-[3.838702440261841, 6.3476881980896, "[TT] Polarizer of the KhalifaSat Antennas = Septum polarizer"]
-[11.988091468811035, 5.117969989776611, "[TT] Volume of the Instrument = < 6800 cm^3"]
-[9.208163261413574, -0.4313301146030426, "[TT] Apogee of the Transfer Orbit = 1.5 x 10^6 km"]
-[10.364542007446289, 1.6288517713546753, "[TT] Number of Active Black Holes Detected of the eROSITA = Millions"]
-[4.578473091125488, 7.110275745391846, "[TT] Telemetry Ku-band of the RF communications = 0.1 W, 500 kbit/s"]
-[10.68282413482666, 4.442109107971191, "[TT] Deorbiting of the DSAT-2 = Yes"]
-[11.14535140991211, 5.581835746765137, "[TT] Detectable Count Rates of the Gamma-ray Counter = > 10 Hz"]
-[8.086505889892578, 3.046363592147827, "[TT] Mid-tropospheric CO2 Measurements per Day of the AIRS = About 15,000"]
-[12.220643997192383, -0.2128174901008606, "[TT] Camera of the TESS = 30-minute period"]
-[10.50610637664795, 2.361543893814087, "[TT] Optic Size of the CuPID X-ray telescope = 4 x 4 cm"]
-[7.511780261993408, 0.92618328332901, "[FF] URL of the Mass Change (MC) = URL:\u00a0https://science.nasa.gov/earth-science/decadal-mc"]
-[10.140661239624023, -1.3498789072036743, "[TT] Inclination of the ICESat-2 = 92\u00ba"]
-[5.395737648010254, 3.1449267864227295, "[TT] Spacecraft Builder of the Lucy = Lockheed Martin Space Systems"]
-[9.024591445922852, 5.471930980682373, "[TT] Pointing Knowledge of the QuikTOMS spacecraft = < 0.25\u00ba"]
-[3.8430426120758057, 3.4458365440368652, "[FF] Launch Date of the Galileo-FOC FM2 = Unknown"]
-[16.487173080444336, 3.573146343231201, "[FF] Announcement Date of the OneWeb = June 25, 2015"]
-[4.499789714813232, 7.653015613555908, "[TT] Band of the Electra = UHF"]
-[7.988557815551758, 3.1668169498443604, "[FF] Parameter Measured of the Microwave Limb Sounder = Carbon Monoxide in the Troposphere"]
-[6.032528877258301, 1.3590099811553955, "[FF] Conducted By of the Saffire-1 = Saffire and Orbital ATK personnel"]
-[7.102510452270508, 3.2341244220733643, "[FF] Parameter Representation of the GEOS Model = Mathematical equations that represent physical processes"]
-[8.025315284729004, 0.5596074461936951, "[TT] Name Meaning of the Watoga Lake = Cherokee word for \u201cstarry waters\u201d"]
-[5.968663215637207, -0.2570990324020386, "[FF] Mission Duration of the D-Sat = More than three months"]
-[4.740492343902588, 0.48768487572669983, "[TT] Phase-A Plan Arrangement of the Harmony = Autumn 2022"]
-[9.281144142150879, 8.69503116607666, "[TT] Slit Width of the ISRF = 84 \u00b5m"]
-[4.822983741760254, 0.37830254435539246, "[TT] Launch Date of the EnMAP = 2013"]
-[5.0578293800354, 3.601386070251465, "[TT] Manufacturer of the ADCS = Stellenbosch University"]
-[9.622505187988281, -0.4685174524784088, "[TT] Altitude of the OceanSat-1 = 720 km"]
-[8.970915794372559, 5.671705722808838, "[TT] Drift Accuracy of the DPU = ~ 0.1 arcsec"]
-[3.547510862350464, 5.345683574676514, "[TT] SNR of the SAR = > 2"]
-[7.8622145652771, 6.452943325042725, "[FF] Restoration Time of the ABI (Advanced Baseline Imager) = Earlier this morning"]
-[5.173624515533447, 0.29693400859832764, "[TT] Deployment Date of the Kestrel Eye II = 24 October 2017"]
-[5.922530651092529, 5.458746433258057, "[FF] Processing Functions of the DCU-S(TC) module = CLTU delimitation, BCH decoding, de-randomization, Security Header extraction, TC Transfer Frame (TF) authenticated decryption and anti-replay control, pseudorandomization and BCH encoding"]
-[5.148881912231445, 7.389420032501221, "[TT] Event Rates of the LET = Up to ~10 kHz"]
-[11.859421730041504, 5.417102813720703, "[FF] Size of the SHS Instrument = Small"]
-[5.286982536315918, 2.6440956592559814, "[FF] Mission Type of the FedSat = EO"]
-[4.922847270965576, 5.864461421966553, "[TT] Receiver Type of the Satellite = Dual-frequency"]
-[5.039904594421387, 1.11348295211792, "[TT] Anomaly Start Date of the GOMOS instrument = August 2011"]
-[14.216586112976074, 3.2095720767974854, "[TT] Mass of the Total with contingency = 8.83 kg"]
-[8.150288581848145, 8.321391105651855, "[FF] Spectral Bands of the Focal Plane Array = VNIR and SWIR"]
-[5.251955986022949, 3.9364938735961914, "[TT] Number of Satellites of the Flock 1 = 28"]
-[8.351239204406738, 7.408544540405273, "[TT] Spectrometers of the DebriSat = 2"]
-[3.6136670112609863, 2.7072739601135254, "[TT] Quantity of the Iridium NEXT satellites = 10"]
-[13.862369537353516, 2.8615708351135254, "[TT] Mass of the Genesis spacecraft = 494 kg"]
-[6.083299160003662, 6.833191394805908, "[TT] GPS Update Rate of the GAMALINK = 5 Hz"]
-[6.546462535858154, 3.0522842407226562, "[FF] Service of the Spire Global UK = Predictive analysis for global shipping, aviation and weather forecasting"]
-[7.877807140350342, 8.581650733947754, "[TT] Spectral Range of the GIIRS = 0.55 - 14.3 \u00b5m"]
-[5.885501384735107, 7.655202865600586, "[TT] Sample Rate of the MPO-MAG instrument = 128 Hz"]
-[4.808452606201172, -1.8775192499160767, "[FF] Goal of the Chang'e-5 = Establish an international lunar research station"]
-[5.028731822967529, 3.3814985752105713, "[TT] Manufacturer of the DSP satellites = DFHSat (DFH Satellite Co. Ltd.)"]
-[9.01634693145752, 5.117776393890381, "[TT] Accuracy of the Gyroscopes = About 10-9"]
-[12.230259895324707, 3.972315549850464, "[FF] Payload Sizes of the Bartolomeo Platform = Airlock-compatible size, FRAM-based standard size"]
-[9.831149101257324, -0.6723237037658691, "[TT] Orbit Altitude of the Rocket 3.3 = 500 km"]
-[5.93428897857666, -0.5668885707855225, "[TT] Phase E Duration of the NuSTAR = Three months"]
-[8.949823379516602, 2.639035701751709, "[FF] URL of the INTEGRAL = http://sci.esa.int/integral/57257-integral-x-rays-earths-aurora/"]
-[6.256978988647461, 4.640302658081055, "[FF] Automation Flexibility of the VMOC = Full automation to complete manual scheduling"]
-[10.59577465057373, 5.43749475479126, "[TT] Sensitivity of Ion Density Fluctuation of the PAP = 1 x 10^27"]
-[9.056974411010742, 9.978657722473145, "[TT] SNR of the Eastman Kodak KLI14403 linear CCD sensor = > 100"]
-[11.69077205657959, 3.2811970710754395, "[FF] Propulsion System of the Cislunar Explorers = Inert water"]
-[6.905088424682617, 5.237954139709473, "[FF] Functionality of the XB1 = GN&C, EPS, Thermal, C&DH, RF Comm, and SSR"]
-[4.0057573318481445, 5.974384784698486, "[TT] Development Partners of the 3D-printed metal antenna = SENER Aeroespacial and CATEC"]
-[6.39182710647583, 4.914446830749512, "[FF] Unknown of the Multi Band Receiver = Unknown"]
-[7.294902324676514, 9.16641616821289, "[TT] Filter Wavelength Range of the ISUAL instrument = 623-750 nm"]
-[10.172043800354004, 5.269463539123535, "[FF] Performance of the ABI Cryocooler = Unknown"]
-[7.793115139007568, 6.927000999450684, "[FF] Functions of the TDP = Gamma (spike) event circumvention, detector responsivity correction, background subtraction, time delay and integration (TDI), matched filtering, and thresholding"]
-[8.532768249511719, 8.675498008728027, "[TT] Dispersing Element of the Spectrometer = Direct vision prism, S-FPL53 and L-NBH54"]
-[5.156134128570557, 0.5435726642608643, "[TT] Launch Date of the Stingray satellite = January 2024"]
-[13.596044540405273, 5.501659393310547, "[FF] Solar Panels of the EURECA = Twin deployable/retractable panels of silicon solar cells"]
-[14.113883972167969, 7.189579963684082, "[TT] Operating Voltage of the Herley MD2000C-1 = 22\u201332 VDC"]
-[7.803504467010498, 5.836179256439209, "[TT] Observation Wavelengths of the Scanning Multichannel Microwave Radiometer (SMMR) = Five different wavelengths"]
-[6.531783103942871, 3.593693256378174, "[TT] Location of the LIS = ISS"]
-[7.478219985961914, 2.348592758178711, "[TT] Real-time Coverage of the Ground Network = 40\u201345% of the landmass"]
-[10.751399993896484, 3.657229423522949, "[FF] Propulsion of the TEPCE = Earth's magnetic field"]
-[10.79935073852539, -0.2832720875740051, "[FF] Global Forest/Non-Forest Map Publication Date of the TanDEM-X = Feb. 2018"]
-[4.256663799285889, 6.3416829109191895, "[FF] High-Gain Antenna Dish of the New Horizons = Linked to advanced electronics and shaped to receive even the faintest radio signals from home"]
-[5.141907215118408, 2.3356270790100098, "[TT] Mission Type of the CAS500 = EO"]
-[8.787616729736328, 7.554744720458984, "[TT] MS B3 of the Pushbroom imager = 0.62-0.69 \u00b5m"]
-[9.155835151672363, 7.23004674911499, "[FF] Vertical Resolution of the Detector = 250 m to 2 km or more"]
-[12.204219818115234, -0.051253970712423325, "[FF] Camera of the TESS-L5 = Unknown"]
-[5.0631561279296875, 7.800236225128174, "[TT] Timer Interrupt Frequency of the AT91SAM9G20 = 1 millisecond"]
-[6.821175575256348, 4.31442403793335, "[FF] Location of the INMCC = Unknown"]
-[8.679808616638184, 1.1437584161758423, "[TT] Data Product Grid of the Aquarius = 150 km"]
-[4.803971767425537, 2.9751436710357666, "[TT] Location of the MC3E = DOE-ASR Central Facility in Oklahoma"]
-[7.768017292022705, 8.651674270629883, "[TT] Spectral Bands of the SMI = Visible (420\u2013700 nm) and near infrared (650\u20131050 nm)"]
-[4.4026970863342285, -1.6513524055480957, "[FF] Study Importance of the Blue Ring Nebula = Show us what they look like so we can identify more of them"]
-[8.130433082580566, 7.306524276733398, "[TT] Frame Rate of the CMOS Image Sensor = 230 frames/s"]
-[10.31087589263916, 4.496947288513184, "[TT] Type of the Reaction wheels with magnetorquers = Standard"]
-[8.182455062866211, 6.504162788391113, "[FF] Instruments of the Almaz-1B = 2 Ekor-A, a 4-band optical imager, etc."]
-[11.371796607971191, 4.34480094909668, "[TT] Size of the RamSat = 2U"]
-[7.89637565612793, 2.0989034175872803, "[FF] Ocean Color Information of the MODIS = Assists with operational use of maritime patrol aircraft, ships, submarines and sonar performance prediction"]
-[5.372613906860352, 0.3409203290939331, "[TT] Operation Start Date of the LRO = 2009"]
-[8.765314102172852, 1.983062505722046, "[TT] Wind Velocity of the NSCAT = 2 m/s, 3 - 20 m/s, 20 - 30 m/s"]
-[9.483689308166504, 6.839322566986084, "[TT] Angular Resolution of the Scanning geometry = 1.2 +0.2 mrad"]
-[10.271831512451172, 7.23332405090332, "[TT] Pitch of the Instrument = 100-110 km"]
-[7.009643077850342, 6.915517330169678, "[TT] Readout Time of the N-FEE = ~2.5 s"]
-[4.796990871429443, 2.292304754257202, "[FF] Hibernation Mode of the Maroc-TUBSAT = Easier to control than that of its predecessor (DLR-TUBSAT)"]
-[9.718826293945312, 8.325335502624512, "[TT] Focal Length of the UVS Instrument = 250 mm"]
-[7.090824604034424, 7.759675979614258, "[TT] Dihedral Angle Offset (DAO) of the Cube Corner Reflectors = 1.25 arcseconds for LAGEOS-1, 1.5 arcseconds for LARES-1"]
-[6.075427532196045, -0.2062537521123886, "[TT] Science Co-Investigators of the Genesis = Approximately 18"]
-[4.089405536651611, 7.828981399536133, "[TT] Modulation Factor of the HXCP = 47.8%"]
-[9.46061897277832, 7.042820453643799, "[TT] Spatial Resolution of the TopSAR wide = 50 - 100 m"]
-[8.501130104064941, 4.763778209686279, "[FF] Function of the MARIN = Monitor the position, orientation, and movement of the satellite"]
-[5.404516220092773, 6.783145904541016, "[TT] Data Handling System of the RISAT = 160 x 4 Mbit/s"]
-[5.5901031494140625, 0.8300004005432129, "[TT] Activation Date of the Imaging System = August 7 - 8, 2013"]
-[6.352033615112305, 2.657813787460327, "[TT] Number of Research Investigations of the International Space Station = More than 2,500"]
-[8.326177597045898, 7.839716911315918, "[TT] Detector Assembly of the BIRCHES instrument = JDSU LVF (Linear Variable Filter)"]
-[7.704163551330566, 4.341346740722656, "[FF] Maneuvers of the RVX = Transition to non-cooperative mode, Non-cooperative hop, Sun-aligned station-keeping maneuver"]
-[8.12346076965332, -0.49286407232284546, "[TT] Average Annual Ice Loss of the Antarctica's ice sheet = 118 gigatons"]
-[7.516360759735107, 6.6540727615356445, "[TT] Timing Time Resolution of the CCD = ~10 -3 seconds"]
-[3.77144718170166, -0.7282136678695679, "[FF] Orbit of the OTB-1 minisatellite = Earth's orbit"]
-[5.279573917388916, 5.589974403381348, "[TT] Communication Protocol of the Ground Software Architecture = TCP/IP"]
-[11.472694396972656, 5.521153450012207, "[TT] Radiation Depth of the ECAL = 17 Xo"]
-[13.396637916564941, 7.3524627685546875, "[TT] Nominal Power of the IMP-8 = 150 W"]
-[9.421686172485352, 3.6086034774780273, "[FF] Magnetic Field Profile of the Current Sheet = Matched the theoretical prediction"]
-[6.624871730804443, 4.358591556549072, "[FF] Function of the AFSS (Autonomous Flight Safety System) = Uses launch vehicle orbital targeting and range safety planning processes to protect public safety from an errant launch vehicle during flight"]
-[9.705740928649902, 4.845301151275635, "[TT] Stabilization of the G\u00f6kt\u00fcrk-1A = 3-axis"]
-[10.08973503112793, 7.608468055725098, "[TT] Swath Width of the Imager = 16.4 km"]
-[8.519647598266602, 1.4740278720855713, "[TT] Measurement of the Aquarius = Sea Surface Temperature (SST)"]
-[5.428894996643066, 7.278210163116455, "[TT] Transmission Rate of the MDD = 2400 bit/s"]
-[8.127138137817383, 7.834555625915527, "[FF] Spectral Ranges of the 4-band CCD Imager = 0.42 - 0.50, 0.52 - 0.60, 0.61 - 0.69, 0.76 - 0.89 \u00b5m"]
-[6.413315773010254, 3.8669936656951904, "[TT] Hosted Instrument of the PLATiNO 2 = MAIA instrument"]
-[7.521846294403076, 0.8750441074371338, "[FF] Purpose of the Moonlight = To create a lasting lunar link to enable sustainable space exploration"]
-[8.493854522705078, 5.792778015136719, "[TT] Coarse Localization Accuracy of the LLMS/IRIS = <3 km"]
-[13.302616119384766, 7.328448295593262, "[TT] Power of the MSU-50 = 6.8 W"]
-[5.295759677886963, 7.692729473114014, "[TT] G/T of the USAT = > 11.5 dB/K"]
-[5.357821941375732, 8.092986106872559, "[TT] Sampling Frequency of the HF-A analyzer = 80 MHz"]
-[5.5967206954956055, 8.003981590270996, "[TT] Measurement Frequency of the MAG = Up to 5 Hz"]
-[13.057567596435547, 7.298528671264648, "[TT] Power of the DUST sensor = 2.2 W"]
-[8.304258346557617, 7.3750410079956055, "[TT] Detector Type of the DIDM = MCP (Microchannel Plate)"]
-[5.216792106628418, 3.273449182510376, "[TT] Responsible Organization of the PROBA-V = CNES"]
-[5.676789283752441, 2.3860769271850586, "[FF] Educational Mission of the ABEX = Facilitate continuous engagement with ASGC universities in the engineering and management of the project"]
-[3.4001035690307617, 6.381061553955078, "[TT] Antenna Dish Size of the ATLAS Space Operations = 3.4 m to 9.1 m"]
-[6.792441368103027, 6.0206146240234375, "[TT] Activation of the Safe Mode = Immediate pass-through from Initial Mode"]
-[7.852814197540283, 8.403219223022461, "[TT] Spectral Range of the Instrument = 5.71-8.26 \u00b5m"]
-[10.416934967041016, 5.9425506591796875, "[TT] Antenna and Camera Temperature of the Yutu = Below -180\u00baC"]
-[13.400221824645996, 2.9275271892547607, "[TT] Total Mass of the StudSat = 1.3 kg"]
-[3.077075481414795, 3.9164223670959473, "[TT] Collaboration Start Date of the NISAR = September 30, 2014"]
-[6.443094253540039, 5.03879976272583, "[FF] Function of the OBC (On Board Computer) = Manages all peripheral instruments including the sensors and the actuators"]
-[10.763802528381348, 1.5006239414215088, "[FF] Diameter of the Neutron Star = Hundreds of thousands of times smaller than the Sun"]
-[8.525125503540039, 5.173798561096191, "[FF] Dark Calibration of the ICU = Implemented by means of a lightweight shutter placed in front of the optical slit"]
-[9.874099731445312, 1.6909220218658447, "[FF] Expansion of the Universe = Not Uniform"]
-[11.300522804260254, 4.264820575714111, "[TT] Satellite Size of the OMS Radiometer = 3U"]
-[9.677841186523438, 1.380401611328125, "[TT] Expected Lifetime of the Pleiades Neo = 10-12 years"]
-[3.556659698486328, 5.488070011138916, "[TT] Antenna Type of the Synthetic Aperture Radar (SAR) = Phased array antenna"]
-[8.660929679870605, 2.0256764888763428, "[TT] Service Area of the WINDS/Kizuna = Almost one third of Earth's surface"]
-[7.937614917755127, 0.5321495532989502, "[FF] Conference Presentation of the Near Earth Asteroid Scout = AIAA Space 2014 Conference and Exposition"]
-[10.66239070892334, 3.3866381645202637, "[TT] Stabilization of the Microsatellite = 3-axis stabilized + passive stabilization of the gravity gradient boom"]
-[7.503404140472412, 9.092283248901367, "[TT] Wavelength of the Pyroxene = 0.95-1 \u00b5m"]
-[10.944705963134766, 6.2480878829956055, "[TT] Thermal Conductivity of the SiC = Very high"]
-[8.882635116577148, 9.538108825683594, "[FF] Band 2 Resolution of the TANSO-FTS-2 = 0.2 cm -1"]
-[10.801294326782227, 0.8548800349235535, "[FF] Flight Path of the BioSentinel = Past the moon and then subsequently into an Earth trailing, Heliocentric orbit"]
-[11.732844352722168, 5.499248504638672, "[TT] Bus Type of the SOLID Panels = I2C"]
-[5.857532501220703, 2.472059726715088, "[TT] Flight Heritage of the ESA = AMPTE/IRM, Giotto, FAST, WIND, and Cluster"]
-[14.326258659362793, 6.58108377456665, "[TT] Cell Type of the GomSpace NanoPower BPX = Lithium-ion 18650"]
-[8.95254135131836, 2.982182264328003, "[FF] Purpose of the EXCISS = Simulating the high-energy, low gravity conditions that were present during formation of the early solar system"]
-[4.680059909820557, -0.45402300357818604, "[FF] Activation Time of the LIRIS = Two and a half hours before docking"]
-[8.046881675720215, 1.663296103477478, "[FF] Parameter of the DPS = Vapour and precipitation - Help for determination of land surface emissivity"]
-[8.355151176452637, 2.755072832107544, "[FF] Measurement Domain of the SEP = Gravity and Magnetic Fields"]
-[6.508480548858643, 3.743821382522583, "[FF] Operation of the Bartolomeo = Robotic installation via remote control from Earth"]
-[5.594343185424805, -0.35222163796424866, "[TT] Orbit Life With Balloon of the AeroCube-3 = 2-3 months"]
-[7.7013163566589355, 8.012625694274902, "[TT] Sensitivity of the PMT = 0.47 - 0.95 \u00b5m"]
-[6.070043563842773, 5.519824028015137, "[TT] Redundancy of the OSDP = Fully redundant"]
-[7.094212055206299, 1.2376149892807007, "[FF] Mission End Date of the Spitzer Space Telescope = 30 January 2020"]
-[5.7170023918151855, 5.350936412811279, "[TT] Payload Receiver of the Satellite = Double"]
-[8.219204902648926, 3.3666954040527344, "[FF] Observables of the LIMS = O3, H2O, NO2, HNO3 and temperature"]
-[5.834829807281494, 2.030738353729248, "[FF] Project Management of the TEMPO = NASA/LaRC"]
-[4.825027942657471, 3.803990364074707, "[TT] Manufacturer of the Telemetry and telecommand antennas = SENER Aeroespacial and CATEC"]
-[11.602932929992676, 3.279186487197876, "[TT] Operating Hours of the Electric Thruster = More than 1000"]
-[10.037819862365723, 3.4303066730499268, "[FF] Type of the VISION = CubeSat optical payload"]
-[6.1317243576049805, 2.4448277950286865, "[TT] Crew Sustainment of the Orion = Yes"]
-[4.38812780380249, 3.083695650100708, "[TT] Location of the TT&C Station = Kiruna, Sweden"]
-[13.443045616149902, 2.8761916160583496, "[TT] Mango Satellite Mass of the PRISMA = 95 kg"]
-[3.6668708324432373, 3.882972478866577, "[TT] Image Product Release Date of the RISAT-1 = October 19, 2012"]
-[3.9809529781341553, 2.13132905960083, "[TT] Launch Vehicle of the CubeStack = Minotaur I"]
-[10.660772323608398, 5.573285102844238, "[TT] Ionized H Temperature of the RHESSI = <104 K"]
-[10.93017292022705, 3.7441506385803223, "[TT] Solar Sail Deployment Test Location of the NEA Scout = NeXolve, a space materials company near Marshall Space Flight Center in Huntsville, Alabama"]
-[8.256438255310059, 6.86664342880249, "[TT] Data frame period of the Full-scan Imaging = 22 s"]
-[12.140000343322754, 4.534124851226807, "[FF] Size of the Sample Retrieval Lander = Roughly one-third the size of what the actual spacecraft would be"]
-[11.56119441986084, 3.3881397247314453, "[FF] Propulsion Systems of the MTM = Chemical Propulsion System and Electrical Propulsion System"]
-[6.636224269866943, 6.959795951843262, "[TT] Duty Cycle of the Closed-loop heaters = No greater than 72%"]
-[6.893166542053223, 1.57989501953125, "[FF] URL of the Mars Terrain Simulator = https://iafastro.directory/iac/proceedings/IAC-18/IAC-18/B6/3/manuscripts/IAC-18,B6,3,5,x42837.pdf"]
-[6.2189812660217285, 2.924506425857544, "[TT] Visits/Day of the Legion constellation = \u226516 at 1.3m"]
-[3.1310312747955322, 2.347381114959717, "[FF] Spectral Bands of the Sentinel-2 = Range of spectral bands"]
-[6.586277484893799, -0.525501012802124, "[TT] Period of the FormoSat-2 = 102.9 minutes"]
-[4.7659478187561035, 6.022308349609375, "[FF] Encoding Scheme of the Software-Defined Radio (SDR) = Concatenated external Reed Solomon (255,223) encoder and an internal convolutional (7,1/2) encoder with an interleaving depth of 5"]
-[8.071301460266113, 1.9083291292190552, "[TT] Image Coverage of the CATS = From 30 \u00ba North to 30 \u00ba South"]
-[9.253423690795898, 6.033267021179199, "[TT] Sensor Angle of the XGRE = About 40\u00b0"]
-[8.764456748962402, 7.446680545806885, "[TT] Leakage Current of the Detector = Negligible"]
-[10.405060768127441, 5.774285316467285, "[TT] Temperature Range of the PICAM = Up to 225 \u00b0C"]
-[10.439716339111328, 5.7644267082214355, "[TT] Operation Temperature of the IES = -25\u00ba to 55\u00baC"]
-[13.464604377746582, 2.954467535018921, "[TT] Spacecraft mass of the GOSAT-2 = < 2,000 kg"]
-[6.462100982666016, -0.5465046763420105, "[TT] Approximate Time to Deorbit of the Spacecraft = 5-20 days"]
-[6.177820205688477, 4.885390758514404, "[FF] Interface of the Service Module = Power and data handling bus"]
-[3.8726344108581543, 7.886040687561035, "[TT] Modulation Type of the High-rate Modulation = 4 Mbit/s with DQPSK modulation"]
-[9.911383628845215, 2.684299945831299, "[TT] Deployment Position of the NanoRacks Kaber Deployment System = Pointed retrograde to the ISS"]
-[4.13462495803833, 5.845137596130371, "[TT] Frequency of the ADS-B receiving payload = 1090 MHz"]
-[10.850836753845215, 3.9080965518951416, "[TT] Configuration of the CanX-2 = Triple-cube"]
-[9.067984580993652, 4.681337356567383, "[TT] Components of the AOE = Twelve silver resistance sensors"]
-[9.79077434539795, 2.6930179595947266, "[TT] Provider of the SIMPL = NanoRacks"]
-[10.980083465576172, 2.0605838298797607, "[FF] Announcement Date of the XMM-Newton = Dec. 21 2007"]
-[11.759855270385742, 3.3847782611846924, "[TT] Type of the Abort Motor = Solid Rocket Motor"]
-[8.018403053283691, 5.049181938171387, "[FF] Calibration Method of the Viscometer = Exploiting a hydrodynamic similarity which relates viscosity to frequency"]
-[5.881474494934082, -0.7287989258766174, "[TT] Expected Lifetime of the RISAT-1 = Five years"]
-[11.65881061553955, 6.820858478546143, "[TT] Energy Resolution of the ART-XC = 130 eV at 6 keV"]
-[5.972111701965332, 0.48703229427337646, "[TT] Development Time of the ASTERIA FSW = 2.4 years"]
-[7.948723316192627, 0.8374269604682922, "[FF] Date of the Drought Conditions = Spring 2021"]
-[4.8993330001831055, -0.5587067008018494, "[TT] Launch Date of the SLATS = 23-12-2017"]
-[4.6972222328186035, 5.771401882171631, "[TT] GPS Capability of the 406 MHz EPIRB = Internal or external"]
-[8.53317642211914, 7.74652624130249, "[TT] Coverage of the ETFE Film = Entire TJ array"]
-[9.175603866577148, 3.3210792541503906, "[FF] Observation of the ERG (Arase) spacecraft = Chorus waves and scattered electrons in the magnetosphere"]
-[6.195202827453613, 4.833408355712891, "[FF] Function of the SCL = Enable event-driven processing and low-level autonomy"]
-[10.414693832397461, 3.222440004348755, "[TT] CubeSat Capacity of the SlingShot = 18"]
-[6.500606060028076, 6.088916301727295, "[FF] Technology of the SpaceLink = Optical communications"]
-[3.7245194911956787, 4.667972087860107, "[FF] Data Types of the EO-ALERT = Optical and SAR data"]
-[13.692996978759766, 3.082303047180176, "[TT] Payload Weight Capacity of the IPS = Up to 7,000 kg"]
-[8.979413986206055, 6.414498805999756, "[TT] Image Location of the CaSSIS = Melas Chasma"]
-[5.444906234741211, 0.5985863208770752, "[FF] Last Operation Date of the Envisat = Nov. 2, 2010"]
-[4.6596784591674805, 2.8942368030548096, "[TT] Observations Management Center of the XMM-Newton = ESAC (European Space Astronomy Center), formerly known as VILSPA) at Villafranca, Spain"]
-[8.200658798217773, 5.8609442710876465, "[FF] Measurement Range of the FLEX = 500\u2013600 nm"]
-[10.992477416992188, 7.573949337005615, "[TT] Swath Width of the MSU-S = 1380 km"]
-[9.350750923156738, 4.995258331298828, "[TT] Attitude Determination Accuracy of the ADCS = \u00b110\u00ba"]
-[7.5951619148254395, 6.07778787612915, "[FF] Function of the RTEP = Subtracts the average background estimate of each pixel from the current signal of the corresponding pixel"]
-[7.863278865814209, 5.7261176109313965, "[FF] Disintegration Recording of the ATV-5 = Camera"]
-[8.982449531555176, 0.49115779995918274, "[TT] Launch Year of the Artemis = 2001"]
-[5.859675407409668, 0.04472269490361214, "[TT] Object Match of the CSpOC Catalog = Correct"]
-[13.27312183380127, 5.2097249031066895, "[TT] Solar Array Surface Area of the IRIS = 1.7 m2"]
-[3.505131244659424, 6.386823654174805, "[TT] Inflated Length of the Antenna Mast = 2.4m"]
-[4.680034637451172, 7.210265636444092, "[FF] RF Communications of the Kanopus-V = X-band (8.2 GHz) downlink of payload data, data rate of 300 Mbit/s, onboard data storage of 24 GB"]
-[8.135204315185547, 3.8540918827056885, "[FF] Modification of the OCO-2 Instrument = Seating Vibration followed by an alignment test"]
-[8.581357955932617, 3.250739097595215, "[FF] Purpose of the EUV Camera = Observe Earth's plasmasphere"]
-[13.31599235534668, 2.912686824798584, "[TT] Mass of the MicroSat-2a = 400 kg"]
-[9.188626289367676, 7.489489555358887, "[TT] Size of the Optical Payload = 1.5U"]
-[10.032453536987305, 4.305984020233154, "[TT] Quantity of the 400 Am2 magnetic torque rods = 3"]
-[7.575807571411133, 7.658987998962402, "[TT] Value of the Dynamic Range = 10 bit"]
-[3.126877784729004, 2.1999478340148926, "[FF] Mission of the ROSE-L = Copernicus expansion"]
-[13.905706405639648, 2.644029378890991, "[TT] Launch Mass of the Konnect = 3619 kg"]
-[12.063240051269531, 7.635662078857422, "[TT] Mass of the PAN Camera = 200 kg"]
-[9.520888328552246, 7.946672439575195, "[TT] Optics Lens Speed of the NEA Scout Camera = f/2.8"]
-[6.134860038757324, 3.1255404949188232, "[TT] Cash on Balance Sheet of the BlackSky = $198 million"]
-[6.326333999633789, 8.213702201843262, "[TT] Channels of the SGLI = 11"]
-[8.819128036499023, 3.8322079181671143, "[FF] Components of the SSI/ES = Langmuir probe, planar collector, plasma drift meter, scintillation meter"]
-[3.5875868797302246, 4.820708751678467, "[TT] Instrument Type of the CHORUS = Imaging microwave radars"]
-[9.890296936035156, -0.6307241320610046, "[TT] Orbit Altitude of the MicroSat-2b = 514 km"]
-[4.378701210021973, 3.026279926300049, "[FF] Locations of the PAC = Farnborough (UK), Madrid (Spain)"]
-[8.87341022491455, 2.7269439697265625, "[TT] Average Value of the Altitude error = 9.75 m"]
-[6.524744987487793, 1.657732605934143, "[FF] URL of the Spacecraft Fire Experiment (Saffire) = http://orbit.dtu.dk/ws/files/97737980/2014_ICES_SFS_Demo_Paper_265_5_16_2014.pdf"]
-[10.231225967407227, 2.538455009460449, "[FF] Calibration Measurement of the Telescope = Dark Earth, X-ray point sources"]
-[6.3369245529174805, 5.531383514404297, "[FF] Data Format of the Processor-based sub-experiments = Analog voltages on the two analog channels"]
-[7.9867939949035645, 4.37221622467041, "[FF] Frequency of the Full Calibration of HIS = Bimonthly"]
-[10.969765663146973, 7.588968753814697, "[TT] Swath Width of the KLIMAT = 3100 km"]
-[7.9505085945129395, 3.770894765853882, "[TT] Instrument Type of the STARSHINE = Other, Atmospheric chemistry, Data collection, Atmospheric temperature and humidity sounders"]
-[5.146115303039551, 3.2884182929992676, "[TT] Manufacturer of the MAG = Lockheed Martin"]
-[3.54968523979187, 4.4390387535095215, "[TT] Full Operational Service Date of the SAR-Lupe Constellation = 2008"]
-[7.10354471206665, 4.527160167694092, "[FF] Unknown of the WTS = Unknown"]
-[8.30183219909668, 0.734679639339447, "[TT] Burned Area of the Calf Canyon-Hermits Peak fire = 270,000 acres"]
-[6.05510139465332, 3.857459306716919, "[FF] Variant of the DMSP Block-5D = DMSP Block-5D military satellite bus"]
-[11.898944854736328, 5.550168037414551, "[TT] Binning of the ICON FUV Instrument = 4 x 4"]
-[13.408671379089355, 5.457435131072998, "[TT] Solar Array of the Orion = Four wings of three panels"]
-[8.031956672668457, 8.787335395812988, "[TT] Resolving Power of the 1.61 and 2.06 \u00b5m CO2 channel = > 20,000"]
-[3.821810007095337, 0.888759434223175, "[FF] Launch Date of the PSLV-C35 / SCATSAT-1 = Sept. 26, 2016"]
-[2.331061840057373, 1.3135885000228882, "[FF] Purpose of the NanoSail-D2 = Demonstrate and test the deorbiting capabilities of a large low mass high surface area sail"]
-[8.203007698059082, 7.164909362792969, "[TT] Mechanical Coupling of the Readout Electronics = No"]
-[7.392775535583496, 3.888097047805786, "[FF] Technology Experiments of the PROBA-3 = 6DOF formation control with thrusters, realistic collision avoidance demonstration and technology payloads"]
-[8.719050407409668, 6.455463886260986, "[TT] Altimeter range RSS error LRM of the Jason-2 = 5/3/3 cm"]
-[4.541098117828369, 8.107083320617676, "[TT] Frequency of the Radar = 13.4 GHz (Ku-band)"]
-[5.055063724517822, 1.9238640069961548, "[FF] Landing of the SRC (Sample Return Capsule) = Hard landing in the Utah desert"]
-[8.161968231201172, 0.10522545874118805, "[TT] Launch Date of the Meteor-M2-1 = November 28, 2017"]
-[6.309621810913086, 4.618216514587402, "[FF] Bus Functions of the Restore-L = Structural support, propulsion, attitude control, data and communications interface and power"]
-[4.7932000160217285, 2.364879608154297, "[FF] Autonomous Operations of the Maroc-TUBSAT = Worldwide scale"]
-[7.14111328125, 6.642693996429443, "[FF] Ability of the GLM sensor = Detect not only flash location but average flash area and total optical energy"]
-[13.306672096252441, 5.435172080993652, "[FF] Components of the Trisat-R = Solar panels from DHV, antennas and CubeSat deployer from ISISpace, satellite structure from RIEDL AeroSpace, main NANOsky platform from SkyLabs"]
-[9.473994255065918, 5.563343048095703, "[TT] Elevation Rotation Axis of the CPA = Perpendicular to the azimuth rotation axis"]
-[9.58023452758789, 4.9463210105896, "[TT] Rotation Speed of the Satellite = Less than 1\u00ba/s"]
-[5.545537948608398, 5.733459949493408, "[TT] Microprocessor of the TPMU = ADuC845"]
-[10.018953323364258, -1.5337193012237549, "[TT] Inclination of the Orbit = 51.6\u00ba"]
-[6.302236557006836, 1.000769853591919, "[FF] Presentation Date of the FORMOSAT-3/COSMIC Follow-On Mission = Aug. 11-14, 2008"]
-[8.418662071228027, 4.5765061378479, "[TT] Frame-Dragging Measurement Accuracy of the LARES-2 = About 2 x 10-3"]
-[9.197747230529785, 2.917590379714966, "[FF] Measurement Range of the ACE Mission = Low energies of the solar wind up to the high energies of the galactic cosmic rays"]
-[4.82055139541626, 7.700689792633057, "[FF] Calibration Method of the Ranging Channel = Calibration model can be derived from the data of transponder's RF front end, digital processing and the RF back end as well as the delay in the various passive elements in the RF chain such as the diplexer"]
-[6.247743129730225, 4.023252487182617, "[FF] Architecture of the MicroStar avionics = Largely unchanged"]
-[5.7845563888549805, 1.081557035446167, "[FF] Development Date of the Back-Illuminated CCD = June 8-11, 2015"]
-[7.5379204750061035, -0.6740623712539673, "[FF] Launch Date of the ICEYE X1 = 17 Jan. 2018"]
-[5.941610813140869, 1.849994421005249, "[FF] Launch Date of the Orion EFT-1 Spacecraft = Dec. 2014"]
-[8.959683418273926, 0.9339236617088318, "[TT] Solar Encounters of the Parker Solar Probe = 7"]
-[4.516462326049805, 3.0799360275268555, "[TT] Ground Stations of the LAPAN-TUBSAT = Biak (Papua, east of Indonesia) and Rumpin (near Jakarta, Indonesia)"]
-[9.231541633605957, 6.739726543426514, "[TT] Vertical Resolution of the SLA-2 = Sub-meter"]
-[9.235930442810059, 4.420078754425049, "[TT] Z Axis Alignment of the SSM = Away from the solar panel and anti-parallel to the orbit normal vector"]
-[8.617745399475098, 2.401041030883789, "[FF] Purpose of the EMIT = Map the surface composition of minerals in Earth\u2019s dust-producing regions"]
-[5.755711555480957, 1.9061205387115479, "[TT] Test Location of the Orion Spacecraft = Plum Brook Station in Sandusky, Ohio"]
-[8.098843574523926, 8.571477890014648, "[TT] Spectral Range of the AVNIR = 0.42 - 0.89 \u00b5m"]
-[8.383740425109863, 5.412638187408447, "[TT] Orbit Determination Accuracy of the LEO Satellites = Sub-decimeter"]
-[4.857781887054443, -1.9216986894607544, "[TT] Sample Collection Goal of the Chang'e-5 = Around two kilograms of lunar samples"]
-[11.164989471435547, 6.018093109130859, "[TT] Material of the Gimbal = Silicon nitride"]
-[10.359024047851562, 5.834324359893799, "[TT] Offset temperature coefficient of the PHA = <0.1 channel/\u00baC"]
-[7.501650810241699, 2.1202900409698486, "[FF] Purpose of the Remote Sensing Satellite = Remote sensing of terrestrial vegetation fluorescence"]
-[5.324162006378174, 0.7247409820556641, "[FF] Contract Date of the Ball Aerospace = Feb. 12, 2014"]
-[9.821700096130371, 4.260408401489258, "[TT] Thermomagnetic Perturbations of the ASM = 20-30 pT +/- 5 pT peak-to-peak range"]
-[8.457660675048828, 1.1444350481033325, "[TT] Quantization levels of the Precipitation over land areas = 0.5,10,15,20, \u226525"]
-[4.74283504486084, 0.3545437157154083, "[TT] Launch Date of the ITUpSat-1 = 23 September 2009"]
-[8.461967468261719, 5.108529567718506, "[FF] Delivery Date of the GFO accelerometer = September 2015"]
-[5.344671726226807, 3.9417190551757812, "[TT] Number of Satellites of the BeiDou-2 = 35"]
-[4.773469924926758, 7.160417079925537, "[TT] Downlink Rate of the S-band = 384 kbit/s"]
-[9.618246078491211, 6.967556476593018, "[TT] SSP Resolution of the LMI = 7.8 km"]
-[11.049830436706543, 2.9480183124542236, "[TT] Solar Array Length of the PARASOL microsatellite = 1.7 m"]
-[10.593544006347656, 5.484829902648926, "[FF] Thermal Control Elements of the TCS = OSR (Optical Solar Reflector), MLI (Multilayer Insulation), paints, thermal control tapes, quartz wool blanket, sink plates and heat pipes"]
-[5.838325023651123, 5.6662774085998535, "[TT] Data Recorders Redundancy of the Vital Layer = Two redundant recorders"]
-[10.932724952697754, 7.524717330932617, "[TT] Swath of the HRS = 10 km x 10 km"]
-[8.288872718811035, 8.173616409301758, "[TT] Spectral Range of the IMG = 3.3 - 14.0 \u00b5m"]
-[5.632852077484131, 0.41636306047439575, "[TT] Operation Extension Date of the Cluster = June 2009"]
-[7.671353340148926, 7.680599689483643, "[TT] Dynamic Range of the Sensor = > 100"]
-[7.515084266662598, 5.366252899169922, "[FF] Components of the EO module = Scan mechanism assembly, telescope, aft optics, cooler assembly with cooled detectors, detector heads for un-cooled channels, preamplifiers, and view-port sunshade"]
-[7.680953025817871, 9.469200134277344, "[TT] Center Wavelength of the Band 11 = 7.02 \u00b5m (1425 cm -1)"]
-[7.78617525100708, 6.464611530303955, "[TT] Imaging Frequency of the Meteosat-11 = Every 15 minutes"]
-[5.33346700668335, 3.9042625427246094, "[TT] Number of Satellites of the FormoSat-3/COSMIC-1 = 6"]
-[10.24526309967041, 4.059008598327637, "[TT] Measurement Objective of the SSM-Boom = Source 2"]
-[5.01915168762207, 3.857269048690796, "[TT] Bus Type of the NigeriaSat-2 = SSTL-300"]
-[14.189058303833008, 3.3295185565948486, "[TT] Total Mass of the LALT = 19.1 kg"]
-[5.747460842132568, 7.221770286560059, "[TT] Data Rate (max) of the STX-01 = 2000 kbit/s"]
-[7.742682456970215, 3.132225751876831, "[FF] Measurement Type of the Imaging Spectrometer = Methane in the atmosphere"]
-[5.986422538757324, 6.457123279571533, "[FF] Message Length of the DCP Retransmission System = Unknown"]
-[13.289990425109863, 7.188619136810303, "[TT] Operational Power Consumption of the PPU = Approximately 15 W"]
-[10.545900344848633, 3.3700923919677734, "[TT] CubeSat Standard of the nSight-1 = 2U"]
-[8.918631553649902, 4.910027503967285, "[TT] Number of Sensors of the STD = 2300"]
-[5.242462158203125, 1.5226516723632812, "[FF] Workshop Date of the ALOS-2 = Jan. 26-30, 2009"]
-[13.223990440368652, 5.336679458618164, "[FF] Solar Panels and Battery Deployment of the OPTOS nanosatellite = Confirmed"]
-[7.046438217163086, 4.207632541656494, "[FF] Unknown of the Myriade = Unknown"]
-[10.717020988464355, 5.570141315460205, "[FF] Thermal Isolation of the VGT-P = Multi-layer insulation (MLI) and titanium quasi isostatic mounting feet"]
-[14.12267017364502, 7.183829307556152, "[TT] Operating Voltage of the LVPS Board = 28 V"]
-[5.6764235496521, -0.7749457955360413, "[TT] Design Life of the DubaiSat-1 = Five years"]
-[7.0840067863464355, 7.8566060066223145, "[FF] Performance Independence of the Instrument = Independent of variations of the receiver gain"]
-[5.2377119064331055, 4.101241588592529, "[TT] Number of L-band Satellites of the MEOSAR satellite constellation = 3"]
-[11.484143257141113, 5.770598888397217, "[TT] Structure of the S/C = Carbon/PEEK thermoplastic skinned Al honeycomb"]
-[6.073927402496338, 5.0555267333984375, "[TT] Language of the OCL = C-like"]
-[4.404292583465576, -1.6530424356460571, "[FF] Hypothesis of the Blue Ring Nebula = Composed of debris from two stars that collided and merged into a single star"]
-[7.522034168243408, 3.551971197128296, "[FF] Function of the RemoveSat = Release and capture several space debris targets"]
-[14.081923484802246, 3.1336629390716553, "[TT] Mass (kg) of the TerraSAR-X = 1230"]
-[5.484949588775635, 5.4191436767578125, "[FF] Communication of the HORYU-2 = Ground communications and the distribution of Earth surface imagery"]
-[10.027482032775879, -1.4883280992507935, "[TT] Orbit Inclination of the HORYU-4 = 31\u00ba"]
-[10.749249458312988, 7.390151500701904, "[TT] Swath Width of the Sensor = 1,700 km"]
-[7.727305889129639, 9.53746223449707, "[TT] Center Wavelength of the B9 = 940 nm"]
-[7.702127456665039, 7.09200382232666, "[TT] Typical high cadence of the HRI Lyman-\u03b1 1216 \u00c5 = Sub-second"]
-[10.444049835205078, 2.095811605453491, "[TT] X-ray Luminosity of the SS 433 = About a million times brighter than the total light output of the Sun"]
-[4.841465950012207, 0.10034079104661942, "[TT] Launch Date of the SpaceX CRS-17 = 04 May 2019"]
-[6.248398303985596, 2.906912088394165, "[TT] Revisits per Day of the Legion Constellation = Up to 14"]
-[7.6462321281433105, 8.444546699523926, "[TT] Simultaneous Soundings of the INSAT sounder = Four per band"]
-[7.541476249694824, 5.3940582275390625, "[FF] Subsystems of the CrIS = Step and settle two-axis scene selection module with image motion compensation capability, full-aperture internal calibration source, large-aperture Michelson interferometer, three-element all reflective telescope, cooled aft optics module, multiple-stage passive cooler, and attached electronics assembly"]
-[3.7395453453063965, 4.536182403564453, "[FF] Imaging of the RADARSAT-1 = Radar Imagery"]
-[5.5330047607421875, 5.540818691253662, "[TT] Type of the Computers = Military specification 31750a (dual-redundant silicon-on-sapphire)"]
-[9.355513572692871, 7.388655662536621, "[FF] Spatial Resolution of the IRS = Halved with regard to IRMSS"]
-[7.981461524963379, 3.5389552116394043, "[FF] Location of the Slot Region = Gap between two of Earth\u2019s vast radiation belts"]
-[4.563580513000488, 7.746715545654297, "[FF] Uplink Frequency of the DCP Retransmission System = Unknown"]
-[5.786964416503906, 2.717863082885742, "[FF] Collaboration Partners of the \u00d8rsted satellite = Danish Technical University, University of Copenhagen, Aalborg University, Terma A/S, CRI, Copenhagen Optical Company, DDC International, Innovision, Per Udsen Co., Rescom, Ticra, DNSC, DMI, NASA, ESA, CNES, DLR, and more than 40 universities and research institutes"]
-[8.19362735748291, 4.8610358238220215, "[FF] Temperature at which it stopped working of the Home Switch = Unknown"]
-[3.8870928287506104, 4.023416519165039, "[TT] Validity of the SARSAT instrument package = Up to SARSAT-10 (NOAA-18, launch May 20, 2005)"]
-[13.903216361999512, 2.9772801399230957, "[TT] Mass of the STRV spacecraft = 52 kg"]
-[9.85000991821289, 7.81574010848999, "[TT] Imaging Spatial Resolution of the Telescope's PSF = Less than 0.22\u00b0"]
-[7.919690132141113, 2.1751296520233154, "[FF] pH of the Marine Chemistry = Unknown"]
-[9.408100128173828, -0.9303927421569824, "[TT] Orbit Altitude of the EDRS = 35,800 km"]
-[11.93625545501709, 4.889743804931641, "[TT] Dimensions of the ECS = 27.5 cm x 20 cm x 17.5 cm"]
-[6.4045491218566895, -0.16293597221374512, "[TT] Attitude Manoeuvring Time of the ALOS-2 = Up to 2 minutes from the Earth pointing attitude to right- or left-looking"]
-[3.957847833633423, 2.0357091426849365, "[TT] Launch Vehicle of the GFO = Taurus launcher"]
-[10.395834922790527, 2.3624696731567383, "[TT] Energy Range of the X-ray Satellite Navigation = 1-15 keV"]
-[10.564264297485352, 3.372706890106201, "[TT] Power Distribution of the ALBus 3U CubeSat = 100 W"]
-[4.781677722930908, 0.6098995804786682, "[FF] Launch Date of the MMS = Spring 2015"]
-[8.361806869506836, 7.634792804718018, "[TT] Quantity of the pnCCD Detectors = 7"]
-[6.194106101989746, 3.894690752029419, "[FF] Data Distribution Service of the Meteosat = Available"]
-[8.905596733093262, 2.2006680965423584, "[FF] Composition of the Stardust Grain = Carbon-rich graphite grain with an embedded speck of oxygen-rich material"]
-[9.636404037475586, 7.410082817077637, "[TT] Pixel Size at Nadir of the POLDER-2 = 6 km x 7 km"]
-[8.159152030944824, 7.1198883056640625, "[TT] Camera Modes of the Optical Satellite = Multi-spectral pushbroom and RGB color video"]
-[6.86299467086792, 2.5638656616210938, "[FF] Imagery Type of the MODIS = IR"]
-[14.079574584960938, 7.198473930358887, "[TT] Voltage of the Power Distribution Bus = 28V"]
-[5.634748935699463, 7.114760398864746, "[TT] Data Rate of the LISS-4 = 105 Mbit/s"]
-[11.398807525634766, 3.4568088054656982, "[FF] NASA Participation of the DRACO = Goal of using nuclear thermal propulsion for long-duration human spaceflight missions"]
-[7.275918960571289, 3.161057949066162, "[FF] Mission Extension of the Envisat = Yes"]
-[8.773332595825195, 7.136340141296387, "[TT] Sensor of the CartoSat-2B = PAN Camera"]
-[4.57637882232666, 0.8348796963691711, "[TT] Routine Operational Phase End Date of the ADEOS = June 30, 1997"]
-[9.276090621948242, 6.994749546051025, "[FF] Resolution of the JWST MIRI = 1024 x 1024"]
-[7.075827121734619, 2.754791498184204, "[FF] Imaging Capability of the SEOSAT\u2013Ingenio = Sideways with access to any point on Earth within three days"]
-[7.7915802001953125, 1.9484237432479858, "[FF] Monitoring Method of the Ocean Acidification = Satellites"]
-[5.271670818328857, 3.5390918254852295, "[FF] Unknown of the MMA Design LLC = Unknown"]
-[5.5442795753479, 4.366720676422119, "[FF] In-orbit digital IP routing of the Heinrich Hertz = Enabled"]
-[4.907976150512695, 6.356451511383057, "[TT] Protocol of the Communication System = AX25 radio-amateur protocol"]
-[3.4718480110168457, -0.752364993095398, "[TT] Orbit of the Sentinel-1C = Sun-synchronous orbit with an altitude around 690 km"]
-[12.000394821166992, 7.610722541809082, "[TT] Instrument Size of the Imager = 3 m tall"]
-[4.873815059661865, 0.6750122308731079, "[FF] Launch Date of the MMS = Fall of 2014"]
-[10.866480827331543, -0.3275288939476013, "[TT] Launch Date of the TanDEM-X = Planned for Oct. 2009"]
-[5.777329921722412, -0.6545527577400208, "[TT] Lifetime of the OFEQ-1 = 6 months"]
-[4.67805814743042, 1.6118396520614624, "[FF] On-orbit commissioning date of the SkySat-3 = August 3, 2016"]
-[5.6094279289245605, -0.6094222068786621, "[TT] Operational Life of the GOES-R = 14 years"]
-[9.31037712097168, 3.2103958129882812, "[FF] Imaging Requirement of the NIRCam coronagraph = 0.8 arcsec (6\u03bb/D) of the star at \u03bb = 4.3 \u03bcm, 0.64 arcsec at \u03bb = 3.35 \u03bcm, and 0.4 arcsec at \u03bb = 2.1 \u03bcm"]
-[11.599844932556152, 5.034611225128174, "[TT] Width of the Graphite Spacers = 1.6 mm"]
-[4.344370365142822, 3.7535324096679688, "[TT] Services of the Galileo = Three Initial Services"]
-[8.239659309387207, 8.815691947937012, "[TT] Spectral Range of the MEGS = 5-105 nm"]
-[6.226670742034912, -0.039867572486400604, "[TT] Length of Observational Data Set of the Aeolus = 3 years"]
-[7.55959415435791, 1.1350603103637695, "[FF] Date of the The Changing Seas of the Florida Keys = 31 May 2022"]
-[4.8196868896484375, 3.028170347213745, "[TT] Developer of the GRACE-FO = Airbus in Friedrichshafen (Germany)"]
-[9.774754524230957, 8.090991973876953, "[FF] Main Cause of Residual Coupling of the Lens System = Different spatial profile of the two beams and residual beam misalignments"]
-[6.109354019165039, 2.4113526344299316, "[TT] Program Scientist of the New Horizons = Curt Niebur"]
-[7.848114967346191, 5.502352237701416, "[FF] Measurement Technique of the Biological Specimens = Optical absorbance and density"]
-[8.758777618408203, 9.406099319458008, "[TT] Spectral Bands of the TANSO-CAI = 4"]
-[5.660970211029053, -2.014758586883545, "[FF] Bus Technologies of the KOMPSAT-5 = Enhanced based on previous programs"]
-[7.996440887451172, 9.151073455810547, "[TT] Wavelengths of the MABEL = 532 nm and 1064 nm"]
-[13.870858192443848, 3.811117172241211, "[TT] Mass of the Integrated Sensor = ~ 4 g"]
-[6.129180908203125, 2.2481348514556885, "[FF] News Article of the Robotic satellite servicer = S. Clark, \"Robotic satellite servicer rehearsal underway in orbit,\" Spaceflight Now, April 3, 2007"]
-[4.938485622406006, 7.576307773590088, "[TT] Throughput of the SABR = Up to 180 W"]
-[6.783324241638184, -0.5449351668357849, "[TT] Orbital Period of the GNSS Satellites = About 12 hours"]
-[10.778265953063965, 1.4749237298965454, "[TT] Mass of the Supermassive Black Hole = About 78 million times the Sun\u2019s mass"]
-[10.119892120361328, 1.3483364582061768, "[TT] Number of Asteroids of the Gaia = 154,741"]
-[5.621860504150391, 3.3346939086914062, "[TT] Operating Status of the PARASOL = Nominal"]
-[7.981235027313232, -0.6482120752334595, "[TT] Instrument Type of the CryoSat = Precision orbit, Radar altimeters"]
-[5.429903030395508, 3.9587666988372803, "[TT] Number of Satellites in Orbit of the Satellogic = 8"]
-[8.264618873596191, 6.502608776092529, "[TT] Observation Rate of the SSM/T-2 = 7.5 scans/minute"]
-[7.215207576751709, 7.7458953857421875, "[TT] Leakage current balancing of the PHA = Up to 32 \u00b5A with 10-bit resolution"]
-[10.725675582885742, 1.5689268112182617, "[TT] Number of Retroreflectors of the STARLETTE and Stella = 60"]
-[5.023184776306152, 3.538461685180664, "[TT] Manufacturer of the CMC Transceiver = ClydeSpace"]
-[13.399889945983887, 6.900749683380127, "[TT] Output Power of the SAST-5000 = \u2265 3.2 kW"]
-[3.682769298553467, 4.426095008850098, "[TT] Quantity of the SAR-GLONASS = 2"]
-[9.209237098693848, 8.693670272827148, "[TT] Slit Width of the Short Wavelength Band = 150 \u00b5m"]
-[6.0836358070373535, 7.6661601066589355, "[TT] Internal Sampling Clock Frequency of the FIELDS Instrument = 150,000 Hz"]
-[5.745636940002441, 0.8919791579246521, "[FF] Launch Date of the Orbital ATK Mission = 21 May 2018"]
-[4.3949384689331055, -1.6573443412780762, "[FF] Formation of the Blue Ring Nebula = Product of two stars merging into one"]
-[13.155116081237793, 7.232844829559326, "[TT] Power Consumption of the Space Comb = Below 30 W"]
-[10.326951026916504, 1.9770407676696777, "[FF] Purpose of the eROSITA = View the Universe in X-rays"]
-[3.778012275695801, 7.149451732635498, "[TT] Gain of the Antenna = 11.2 dBi"]
-[8.522592544555664, 3.8586740493774414, "[TT] Number of Level 1b End-Products of the Space Weather Instruments = 8"]
-[5.190272808074951, 0.6302441954612732, "[TT] Launch Date of the Cesium Satellite 1 = 27 September 2021"]
-[7.602947235107422, -0.4652814567089081, "[FF] URL of the IceCube = https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=4063&context=smallsat"]
-[6.788193225860596, 4.638760089874268, "[FF] Purpose of the MONTE = Deep space navigation"]
-[5.741206645965576, 2.957542657852173, "[TT] Estimated Growth Opportunity of the Hiber = \u00a33.5B"]
-[4.701968669891357, 0.36687183380126953, "[TT] Launch Date of the Buccaneer = 18 November 2017"]
-[8.187684059143066, 1.9160805940628052, "[FF] Observation Data of the Shikisai = Boso Peninsula SST and the seine fishing ground"]
-[9.55611515045166, 7.633386611938477, "[TT] Swath Width of the Main Camera = 2250 km"]
-[4.607077598571777, 5.594603061676025, "[TT] User Identification of the Distress Beacons = Yes"]
-[14.50623893737793, 6.561779022216797, "[FF] Battery Operations Presentation of the TET-1 = SpaceOps 2014"]
-[6.418515205383301, -0.28571391105651855, "[TT] Observation Duration of the SPARCS = 1 day to 80 days"]
-[13.347699165344238, 7.2844157218933105, "[TT] Power of the UniSat-1 = Average power of 10 W"]
-[5.676321506500244, 5.699001789093018, "[TT] Data Interface of the GAMALINK = I2C, UART"]
-[14.274168968200684, 3.1008269786834717, "[TT] Mass of the Anand = Less than 15 kg"]
-[5.4147467613220215, 7.042995929718018, "[TT] ETM Output of the Landsat-6 = Two 85 Mbit/s serial composite streams"]
-[14.04529094696045, 6.315826892852783, "[TT] SDRAM of the GomSpace NanoMind A3200 = 32 MB"]
-[5.932890892028809, 4.892963886260986, "[FF] Service Interfaces of the LCRD = Link scheduling, data transmission and reception, in-event support status"]
-[8.720709800720215, 8.861431121826172, "[FF] Grating Type of the OCO-2 = Regularly-spaced series of grooves on a very flat surface"]
-[7.3024468421936035, 1.8016475439071655, "[FF] Cargo of the CRS-19 = Microscopic organism, rotifers"]
-[7.625616073608398, 5.698288440704346, "[FF] Information Type of the CATS LiDAR = Range-resolved"]
-[9.042860984802246, 4.4667277336120605, "[TT] Sun sensors of the ADCS = 6"]
-[3.8328981399536133, 3.3662664890289307, "[TT] Launch Date of the Galileo FOC-3 and FOC-4 satellites = 27 March 2015"]
-[13.624701499938965, 2.7813873291015625, "[TT] Launch Mass of the Almaz-1 = Over 18,500 kg"]
-[8.636967658996582, 1.0566402673721313, "[TT] Data Collection Duration of the Aquarius/SAC-D satellite = 35 months"]
-[9.540339469909668, 7.465932369232178, "[TT] Resolution of the SV-24 = 0.9-1.1 m"]
-[5.286927223205566, 7.617151260375977, "[TT] Received Eb/No of the Unit = 7.52 dB"]
-[14.069311141967773, 4.024109840393066, "[TT] Mass of the Total instrument = <125 kg"]
-[10.374610900878906, 6.965492248535156, "[TT] Effective Area for Pointed Observations of the Mirror System = 510 cm 2  @ 7 keV"]
-[7.699400424957275, 8.979138374328613, "[TT] Spectral Range (Band 4) of the MUX = 0.77-0.89 \u00b5m"]
-[12.155038833618164, 2.948122501373291, "[TT] Failure Reason of the Landsat-6 = Ruptured hydrazine manifold"]
-[5.762209892272949, 0.6419746279716492, "[FF] Mystery Solve Date of the Cluster = July 14, 2015"]
-[5.583970069885254, 6.103466987609863, "[TT] Processor MIPS of the MPM = 42 MIPS"]
-[10.298774719238281, 8.042876243591309, "[TT] Entrance Aperture Diameter of the Instrument = 29.5 x 24 mm2"]
-[18.798583984375, 3.4801695346832275, "[TT] Mean \u0394N (m) of the Kirkuk = -9.5"]
-[10.984646797180176, 0.858971893787384, "[TT] Satellite Separation of the LISA = Millions of kilometers"]
-[11.944937705993652, 4.477606773376465, "[TT] Body Height of the Spacecraft = 23.5 cm"]
-[6.9909443855285645, 3.1568984985351562, "[FF] Revisit Times of the HyperScout = Sub-daily"]
-[9.445602416992188, 2.291468858718872, "[FF] Elves of the ISUAL = 73.65%"]
-[12.717363357543945, 3.8915677070617676, "[FF] Properties of the Ion Dispersion = Provide information on the properties of magnetopause reconnection"]
-[8.360223770141602, 4.117837429046631, "[FF] Measurement Record of the Spectral Irradiance Monitor (SIM) = Unknown"]
-[6.108408451080322, 1.365583896636963, "[FF] Meeting Date of the Swarm = May 3-5, 2006"]
-[9.619071006774902, -0.5766985416412354, "[TT] Altitude of the Hodoyoshi-4 = 600 km"]
-[8.208950996398926, 2.5536842346191406, "[FF] Purpose of the CAPI = Cloud and Aerosol measurement"]
-[7.733747482299805, 8.037788391113281, "[FF] Function of the Instrument = Spectral determination of major minerals"]
-[6.884444713592529, 3.0343620777130127, "[TT] Planned Number of Satellites of the MethaneSAT = 1"]
-[10.45750617980957, 6.730222702026367, "[TT] Mirror Surfaces of the Limb Imager = Fully free-form"]
-[7.198647975921631, 1.2881587743759155, "[FF] Mission Overview of the ExoMars Trace Gas Orbiter = URL: http://exploration.esa.int/mars/46124-mission-overview/"]
-[9.862377166748047, -0.2889811098575592, "[TT] Altitude of the DMSP = 830 km"]
-[4.033324718475342, 6.17029333114624, "[FF] Antenna Orientation of the GPS Reflectometry Receiver = Zenith side and Nadir side"]
-[8.171942710876465, 4.56311559677124, "[FF] Ionising Doses of the TimePix radiation sensors = 4 to 5 krads"]
-[6.741611003875732, 5.858728408813477, "[TT] Quantity of the BCM = 3"]
-[5.21621036529541, 5.846099853515625, "[FF] Type of the SpaceWire router = SpaceWire router"]
-[8.400256156921387, 6.9241042137146, "[TT] Instrument Type of the AWiFS = High resolution optical imagers"]
-[6.981197834014893, 4.347845077514648, "[FF] Unknown of the SOVIM = Unknown"]
-[6.947230815887451, -0.6058144569396973, "[TT] Orbit Period of the HORYU-4 = 96.2 minutes"]
-[9.511590003967285, 6.921137809753418, "[TT] Resolution of the OPS = 30 m"]
-[6.237387657165527, 4.227288722991943, "[FF] Support of the Flight Segment System Engineer = Project System Engineer"]
-[5.897316932678223, -0.7668468952178955, "[TT] Orbital Lifetime of the InflateSail = 72 days"]
-[12.880056381225586, 5.020143032073975, "[TT] Dimensions of the SOHO = 4.3 m x 2.7 m x 3.65 m"]
-[7.677641868591309, 2.098362922668457, "[FF] Objectives of the Altimetry Mission = Ocean topographic mapping, measurements of sea surfaces, development of climate models"]
-[6.564856052398682, 7.678072929382324, "[TT] Pixel Quantization of the Spectral bands = 12 bit"]
-[13.097262382507324, 5.5916314125061035, "[TT] Quantity of the SOLID Panels = 4"]
-[9.636817932128906, 0.8628281354904175, "[TT] Projected Distance of the Newly Detected Source = 8 times the Earth-Sun distance"]
-[4.827108383178711, 5.199478626251221, "[FF] Message Forwarding of the LUT = Forwards the located distress message to a nearby Mission Control Center (MCC)"]
-[8.85123062133789, 4.971014022827148, "[FF] Impact of the Attitude Control System = Hindered the performance of the GPS receiver"]
-[9.282045364379883, 2.4341094493865967, "[TT] Red Sprites Percentage of the ISUAL = 6.54%"]
-[12.805658340454102, 7.594715595245361, "[TT] Power Consumption of the Instrument = 32 W"]
-[7.269746780395508, 4.679478645324707, "[TT] Location of the OPSE = Close to the center of the disk"]
-[9.897797584533691, 0.05301652476191521, "[TT] Data Resolution of the GRACE-FO = 1/8th degree of latitude, or about 8.5 miles"]
-[3.337524652481079, 2.314927101135254, "[FF] Level 1 Products of the Sentinel-6 = Instrument measurements converted into recognized engineering units, calibration data (radiometric and spectral calibration as well as geometric registration to geodetic Earth coordinates) are appended (Level 1a) or applied (Level 1b), geolocation data are also appended"]
-[2.9395499229431152, 4.431236267089844, "[FF] Components of the PALSAR-2 Electric Unit (ELU) = System Controller (SC), Data Processor (DP)"]
-[9.741887092590332, 4.2490973472595215, "[TT] Controlled Axes of the Permanent Magnets = Two"]
-[8.947306632995605, 5.689019203186035, "[TT] Pointing Knowledge of the ADCS = 540 arcsec"]
-[6.304670810699463, 8.075882911682129, "[TT] Number of Passbands of the Channel 6 = 1"]
-[5.438998699188232, 1.050930142402649, "[FF] Launch Date of the BlackSky Pathfinder Satellite = 26 Sept. 2016"]
-[8.53162670135498, 6.789849281311035, "[TT] Cost (sensor + spacecraft) of the Pushbroom Scanner = High"]
-[11.265453338623047, 5.348002910614014, "[TT] Quantity of Scintillators of the Scatterer = 64"]
-[4.399557113647461, 7.846203327178955, "[TT] Downlink Frequency of the RF communications = 437.465 MHz"]
-[4.477506160736084, 7.881669044494629, "[TT] Frequency of the Ka-band = Near 32 GHz"]
-[6.032825469970703, 1.2035202980041504, "[FF] Mission Start Date of the Deep Space Atomic Clock = Oct. 9, 2012"]
-[4.2143988609313965, 0.1955563873052597, "[FF] Falcon 1e Launch Date of the FormoSat-5 = June 15, 2010"]
-[3.3719959259033203, 6.391876697540283, "[TT] Antenna Length of the OPAL = About 17.5 cm"]
-[6.183319091796875, 4.774891376495361, "[FF] Level 0-1b & Level 2 processing facility of the PDGS = Hosted"]
-[6.455450534820557, 1.1475608348846436, "[FF] Presentation Date of the WINDS = Oct. 11-13, 2005"]
-[12.448524475097656, 3.202289581298828, "[TT] Propellant Quantity of the Propulsion System = 103.5 kg"]
-[3.7621853351593018, 6.400874614715576, "[TT] Type of the Antenna = 1024-element passive microstrip-based arrays antenna, linearly polarized"]
-[3.806469678878784, 1.1454529762268066, "[TT] Booster Recovery Count of the Falcon 9 = 75"]
-[5.1388349533081055, 6.44383430480957, "[TT] Power of the Spacecraft 406 MHz Processor = 33 W"]
-[10.359396934509277, 5.781391143798828, "[TT] Temperature Range of the SST = 200-320K"]
-[3.296945810317993, 2.260030746459961, "[FF] Product Levels of the Sentinel-3 = Level 1, Level 2/3"]
-[8.06213665008545, 1.8672221899032593, "[TT] Coastal Zones Swath of the HY-1C = More than 950 km"]
-[7.488158702850342, 7.017300605773926, "[TT] Cadence of the XRS = \u22643 s"]
-[9.559552192687988, 8.418865203857422, "[TT] Field of View of the UVS Instrument = 0.071\u00ba x 0.75\u00ba"]
-[9.793999671936035, 7.796027660369873, "[TT] Frame Time of the Telescope = 25 minutes for normal mode"]
-[10.426857948303223, 5.755476474761963, "[TT] Temperature of the Eureka Station = 21.9\u00b0C"]
-[9.297274589538574, 5.827077388763428, "[TT] Orientation of the G-switch sensors = Inverted"]
-[6.340867042541504, 5.2129902839660645, "[FF] Microcontroller of the Big Apple board = Controls the operations, power distribution, and data saving"]
-[8.655437469482422, 3.929783582687378, "[FF] Mission of the CSSWE = Measure outer belt electrons and SEP protons"]
-[8.14974594116211, -0.2596892714500427, "[TT] Extent Trend of the Sea Ice = Downward"]
-[7.896831035614014, 9.020589828491211, "[TT] Wavelength of the VIS (red) = 0.65 \u00b5m"]
-[4.142849922180176, 0.1377076357603073, "[TT] Launch Date of the Falcon-Heavy (Block 5) = 2017"]
-[13.27167797088623, 5.445882320404053, "[TT] Installation Location of the Solar Arrays = On top of the existing solar panels"]
-[13.675677299499512, 5.85525369644165, "[FF] Solar Panel Connection of the Phoenix EPS = COTS buck/boost voltage regulator"]
-[5.8892927169799805, 2.38456654548645, "[TT] Principal Investigator Affiliation of the NuSTAR = Caltech in Pasadena, California"]
-[11.290855407714844, 4.2533979415893555, "[FF] Size of the IPEX = 1U"]
-[9.989980697631836, 5.633209705352783, "[FF] Function of the PC5 = Supplies power to the detector, including low voltages for the preamps, high voltage to bias the detector, and a supply for the thermoelectric cooler which provides closed loop control with a maximum temperature differential of 85 \u00b0C"]
-[9.556463241577148, 0.3185060918331146, "[TT] Distance Traveled of the Yutu 2 = 600 meters"]
-[6.033593654632568, 7.1660332679748535, "[TT] Data Rate of the MIS Instrument = 500 kbit/s"]
-[6.505413055419922, 0.586347758769989, "[TT] Earth Explorer of the FORUM = Ninth"]
-[6.949581623077393, 0.8082495927810669, "[FF] Conference Date of the InSight Mars Mission = May 28-June 1, 2018"]
-[7.677521228790283, 0.8075985312461853, "[FF] Purpose of the Broadband InfraRedCompact High-resolution Exploration Spectrometer = Lunar Volatile Dynamics"]
-[5.192260265350342, 4.896266460418701, "[TT] Ground Outage Period of the INTEGRAL = 4 to 6 h"]
-[5.411926746368408, 0.5095774531364441, "[TT] Planned Ejection Date of the PICOSAT1.1 = July 2001"]
-[8.983621597290039, 7.099663257598877, "[TT] Swath of the DMC-2G imager = >600 km"]
-[10.005615234375, 0.8459581732749939, "[TT] Antenna Length of the Cluster spacecraft = 88 m"]
-[2.616513729095459, 0.13861313462257385, "[TT] Pulse period (ms) of the B0531+21 (Crab) = 33.085"]
-[8.30697250366211, 8.24637508392334, "[TT] Technology of the VNIR detector = 0.35 \u00b5m CMOS technology"]
-[5.602181911468506, 6.885283470153809, "[TT] Bit Rates of the EDRS = 600 Mbit/s and higher"]
-[11.254467964172363, 5.8120951652526855, "[TT] Material of the RX-M2 Tower = CFRP skins"]
-[5.6319990158081055, 3.262078046798706, "[TT] Contract Amount of the TSIS-2 = $18,044,280"]
-[11.627555847167969, 3.4031481742858887, "[FF] Force of the ESP Thrusters = Provides force in the normal direction"]
-[7.002349853515625, -0.7804165482521057, "[TT] Orbital Period of the HD 21749c = Just under eight days"]
-[9.227364540100098, -1.0123140811920166, "[TT] Orbit of the INSAT-3D = Geostationary orbit of 35,786 km"]
-[6.412632465362549, 5.2821855545043945, "[FF] Performance Improvement of the FY-4 Series = Data amount, network transmission bandwidth, product type and quantity, archiving data and applications"]
-[9.177033424377441, 3.162818193435669, "[FF] Unique Capability of the HPCA = Uses radio frequency oscillations to sweep the majority of solar wind protons away from the detector, without affecting the magnetospheric oxygen"]
-[3.188886880874634, 2.30279541015625, "[FF] Mission Type of the Sentinel-2 = Optical High Resolution"]
-[5.759520053863525, -0.9816176295280457, "[TT] Design Life of the Kanopus-V = 5 years"]
-[13.436734199523926, 6.8088555335998535, "[TT] Power Generation of the GOSAT-2 = 5 kW"]
-[10.066936492919922, 5.5686469078063965, "[FF] Thermal Design of the SWAP = Unknown"]
-[11.688765525817871, 0.22161902487277985, "[FF] Discovery of the TESS = Young Neptune-size world orbiting AU Microscopii"]
-[13.205902099609375, 7.699073314666748, "[TT] Transmit Power Level of the ALScat = 200 W"]
-[11.727527618408203, 3.278874158859253, "[TT] Quantity of the Thrusters = 24"]
-[3.5064642429351807, 1.5931278467178345, "[FF] Mission Date of the Sentinel-2 = July 23-27, 2007"]
-[10.42711067199707, 1.799878716468811, "[FF] Orientation Effect of the Doughnut = Blocks black hole if viewed edge-on, allows detection if viewed face-on"]
-[11.665032386779785, 4.239927291870117, "[TT] Fairing Extension Length of the TerraSAR-X = 1.5 m"]
-[6.16855525970459, -0.37924668192863464, "[TT] Station Keeping Duration of the PARASOL = > 10 years"]
-[7.978638648986816, 8.43235969543457, "[FF] Moving Parts of the Spatial Heterodyne Spectroscopy (SHS) = None"]
-[10.325679779052734, 2.664910316467285, "[TT] Time to Reach Same Altitude of the NanoSat-1B = About 3 months"]
-[6.177367687225342, -0.4474264979362488, "[TT] Forecast Mode Duration of the C/NOFS = 3 months required, 27 month goal"]
-[8.381062507629395, 4.2286248207092285, "[FF] Function of the Deployable Robotic Arms = Orientate the satellite's electric propulsion thrusters, and control thrust direction and attitude during different phases of the mission"]
-[5.293260097503662, 7.731272220611572, "[TT] Timing Pulse Frequency of the SAMPEX = 1 Hz"]
-[5.131527900695801, -0.5989609360694885, "[FF] Phase B Start Year of the TARANIS = 2009"]
-[6.719809532165527, 5.523657321929932, "[TT] Control Type of the Jerry = Passive"]
-[7.341990947723389, 8.94865894317627, "[TT] Filter Type of the OTD = Narrow band"]
-[11.004131317138672, 0.8288829326629639, "[TT] Lissajous Orbit Dimensions of the LISA Pathfinder = 500,000 km x 800,000 km"]
-[9.19786548614502, 6.05996036529541, "[TT] Moving Cold Start Acquisition Time of the Antenna Subsystem = < 720 s"]
-[3.658949136734009, -0.8212763071060181, "[TT] Orbit Type of the ABEX = Super-synchronous"]
-[7.362063407897949, 0.23860576748847961, "[TT] Return Date to Earth of the OSIRIS-REx = September 24, 2023"]
-[11.291308403015137, 5.9464430809021, "[TT] Material of the Bushings = Polyimide plastic with impregnated graphite"]
-[5.910545825958252, 7.034791469573975, "[TT] Data Rate of the Solar Wind Monitors = <1 kbit/s"]
-[11.895186424255371, 3.0649797916412354, "[TT] \u0394V of the Propulsion System = Up to 200 m/s"]
-[6.53617000579834, 6.052267074584961, "[FF] States of the LCRD Payload = S1 - LCRD Optical Space Terminal initialized but not illuminated by the beacon or uplink beam, S2 - LCRD Optical Space Terminal illuminated by the beacon, S3 - LCRD Optical Space Terminal illuminated by the uplink beam, S4 - LCRD Optical Space Terminal receiving data frames"]
-[10.321138381958008, 5.904715061187744, "[TT] Temperature of the MWIR = 700 K (max)"]
-[7.037519454956055, 8.168173789978027, "[FF] SNR Improvement of the PAIS = When the subaperture area is increased"]
-[8.639826774597168, 7.029256820678711, "[TT] Image Quality of the Imaging System = Good"]
-[6.9942755699157715, -0.3624984920024872, "[TT] Observation Period of the SORCE = Two solar minima"]
-[5.9604082107543945, 0.16068720817565918, "[TT] Wake-up Date of the Rosetta = 20 January 2014"]
-[11.990104675292969, 6.301523685455322, "[FF] Flux Behavior of the AMS = Increases, levels out, increases again, tendency to decrease"]
-[4.54738712310791, 7.651061534881592, "[FF] Uplink of the Communication Subsystem = VHF at 9.6 kbit/s, frequency = 155 MHz, bandwidth = 16 kHz"]
-[13.736729621887207, 5.394834041595459, "[TT] Solar Cells of the Solar Panel = 20 TJ GaAs solar cells in series"]
-[4.722331523895264, 0.7080410122871399, "[TT] PFM Manufacture Status of the MSASI = Started"]
-[6.052305698394775, 0.8955983519554138, "[FF] Swath Mapping of the UV/VIS Camera = First and second month"]
-[6.917097568511963, 0.7815996408462524, "[TT] Development Time of the GP-B probe = Over 40 years"]
-[11.628029823303223, 6.517476558685303, "[FF] Energy Range of the NuSTAR = Three times higher than Chandra detects"]
-[5.293783187866211, 2.977048873901367, "[FF] Development of the LRI = Joint US-German development with additional contributions from Australia"]
-[8.607644081115723, 5.631110668182373, "[TT] Components of the FLLS = Lateral system and longitudinal system"]
-[10.854024887084961, -0.27731457352638245, "[TT] Imaging Capability of the Tandem-L = Exceeds that of TanDEM-X by a factor of 100"]
-[6.196334362030029, 5.186892032623291, "[FF] Patching Capability of the OBSW = Included in this version"]
-[4.857584476470947, 1.041318416595459, "[TT] Date of the PDR = Jan. 20-24, 2014"]
-[4.35957670211792, 0.7907940745353699, "[TT] Launch Date of the HY-1C = 7 September 2018"]
-[3.827098846435547, 6.937821865081787, "[TT] Antenna Polarization of the TUC Transponder = Circular"]
-[7.656192779541016, 6.5991597175598145, "[TT] Purpose of the Optical Benches = Core of the laser interferometry measurement system"]
-[4.625856399536133, 8.010820388793945, "[TT] Operating Frequency of the Altimeter = 13.56 GHz"]
-[7.473108768463135, 2.9377381801605225, "[TT] View Path Width of the MethaneSAT = 200 kilometers"]
-[10.180974006652832, 7.454550743103027, "[TT] Image Size of the FCI = 17.7 degree diameter circle"]
-[3.38071870803833, 6.441731929779053, "[TT] Diameter (mm) of the Antenna = 600"]
-[4.993260860443115, 3.548943281173706, "[TT] Manufacturer of the ADPMS = Qinetiq Space"]
-[6.872247695922852, 9.512662887573242, "[TT] NEDT at 300 K of the Band 7 = 0.15 K"]
-[6.346721172332764, 1.4705770015716553, "[TT] Observation Date of the eROSITA = 17 to 18 October 2019"]
-[8.710400581359863, -0.1706429123878479, "[TT] Lunar Working Orbit of the Chang'e-1 = 200 km x 200 km"]
-[13.476747512817383, 2.8903238773345947, "[TT] Mass of the Capella's Satellites = 110 kg (Whitney-class satellites), less than 197 kg (Acadia-class satellites)"]
-[8.184396743774414, 4.372176170349121, "[FF] Measurement Uncertainties of the Active Cavity Radiometer Irradiance Monitors = Unknown"]
-[6.418394565582275, 3.9513332843780518, "[FF] Development Status of the CIMR = Proposed"]
-[4.853023052215576, 0.73000168800354, "[FF] Launch Date of the TeLEOS-1 = Unknown"]
-[9.259610176086426, 3.0938446521759033, "[FF] Objective of the Genesis = Monitor the solar wind and to collect particles of the solar wind by ion implantation into the collector materials for a duration of two years, and to return these samples for isotopic and chemical analysis in terrestrial laboratories"]
-[7.98281717300415, 8.947983741760254, "[TT] Transmitted Wavefront Distortion of the Optical Window = \u03bb/8 at 633 nm"]
-[5.424102306365967, 0.7880740165710449, "[FF] Launch Date of the Five Spacecraft = April 23, 2013"]
-[10.20203685760498, 4.4569854736328125, "[TT] Torque of the Canopus Pipper = 1.6 x 10 -4 Nm"]
-[6.2148332595825195, 8.038604736328125, "[FF] Channel Set of the MWI = Unknown"]
-[4.974318027496338, 5.8710856437683105, "[TT] Acquisition Mode of the TDX and TSX Satellites = Dual Receive Antenna configuration"]
-[9.820551872253418, 7.737278938293457, "[TT] Time Lost for Maneuvering of the Telescope = Significant for tens of thousands of satellites"]
-[8.694967269897461, 4.518838405609131, "[FF] Attitude Sensing of the ADCS = 3-axis magnetometer, a 3-axis gyroscope, 4 sun sensors, 2 ST (Star Trackers)"]
-[4.150163173675537, 4.061355113983154, "[FF] Earth Observation Mission of the INTA\u00b5Sat-1 = First"]
-[11.22822380065918, 2.8329696655273438, "[TT] Mass of the SERB Nanosatellite = 4.5 kg"]
-[7.943114280700684, 4.549563407897949, "[FF] Presentation Date of the Long-term stable internal calibration chain for a space-borne Integrated Path Differential Absorption LIDAR system = Oct. 3-7, 2011"]
-[10.142273902893066, 5.547889232635498, "[TT] IR Detector Cooling of the Instrument = Two-stage passive radiative cooler with retractable earth shield"]
-[7.632466793060303, 7.787885665893555, "[TT] Sensitivity of the MTVZA-GY = Better sensitivity (factor 2) over a conventional Dicke-switched system"]
-[5.191290855407715, 2.6189749240875244, "[TT] Electromagnetic Interference Chamber Testing Location of the Crew Dragon = SpaceX factory in Hawthorne, California"]
-[5.2661943435668945, 0.5433084964752197, "[TT] Launch Date of the Satellite = 18 Dec 1999"]
-[7.845088481903076, -0.39083796739578247, "[TT] Duration of the Drift Ice Season = January to March"]
-[5.155810356140137, 0.8087993264198303, "[TT] Operational Date of the WSF-M Satellites = Fiscal Year 2024"]
-[6.412045478820801, -0.6540518999099731, "[TT] Revisit Rate of the CBERS-4A = 5 days"]
-[6.345154762268066, 1.8755183219909668, "[FF] URL of the ExoMars = http://www.russianspaceweb.com/exomars2018-2017.html"]
-[9.679450988769531, 2.5449960231781006, "[FF] Parameter of the Chandrayaan M3 = Value"]
-[10.120345115661621, 6.414090633392334, "[TT] NEDT of the NIRST = Better than 0.5 K at 400 K in the MWIR range and better than 0.4 K at 300 K in the TIR range"]
-[12.459223747253418, 0.5620318055152893, "[FF] Date of the Plato\u2019s cave = 01 June 2022"]
-[14.692002296447754, 6.647843360900879, "[TT] Nominal Capacity of the Battery = 14.4 Ah"]
-[8.357972145080566, 6.696598052978516, "[FF] Far-Field Pattern Irradiance Drop of the OGS = Does not exceed 3dB"]
-[5.241277694702148, 6.980262756347656, "[TT] Downlink Lock Time of the LLCD PAT Systems = Within seconds"]
-[4.530785083770752, 6.775259017944336, "[FF] Function of the S-band antenna = Reception of uplinked command stream"]
-[8.743789672851562, 4.859034061431885, "[TT] Location Accuracy of the Autonomous star tracker = Less than 50 m"]
-[8.946528434753418, 6.20082950592041, "[TT] Instrument Type of the SSJ/5 = Electrostatic analyzer detector"]
-[6.649921417236328, -0.49322715401649475, "[FF] Orbit Duration of the EDRS-A = 1 month"]
-[5.411225318908691, -0.3088301718235016, "[TT] Launch Timeframe of the Block 5B/C satellites = 1971 to 1976"]
-[8.831551551818848, 5.461714267730713, "[TT] Control Accuracy of the CALIPSO = \u00b1 10 km at equator crossing"]
-[5.506145477294922, 5.594786643981934, "[TT] Device Type of the Raspberry Pi 3 = Raspberry Pi 3"]
-[7.461529731750488, 2.1224191188812256, "[FF] Objective of the CBERS-4A = Provide remote sensing images to observe and monitor vegetation, deforestation in the Amazon region, water resources, agriculture, urban growth, land use and education"]
-[8.000984191894531, 2.0602598190307617, "[TT] Spatial Resolution of the Ocean Color Scanner = 1 km"]
-[6.780666828155518, 5.263757228851318, "[FF] Components of the Drum = Digital data subsystem, power and the signal transfer assembly"]
-[5.8287858963012695, 1.5107314586639404, "[FF] Conference Presentation Date of the RISESAT = August 13-16, 2012"]
-[13.832772254943848, 2.985067129135132, "[TT] Weight of the GOES-T = Over 6,000 pounds (~3000 kg)"]
-[12.03547477722168, 6.9832587242126465, "[FF] Output Energy of the InnoSlab amplifier = About 30 mJ"]
-[9.187385559082031, 7.105188846588135, "[TT] Recording Resolutions of the SPOT-4 = 2.5 - 20 m"]
-[14.465004920959473, 6.565658092498779, "[TT] Battery Capacity of the Spacecraft = 50 Ah"]
-[6.452478885650635, 3.7715370655059814, "[FF] Expected Full Recovery of the GOES-17 = On track for a full recovery with no lasting effects to the satellite"]
-[9.764265060424805, 4.189462184906006, "[TT] Detection Threshold of the DICE body-mounted magnetometer = >100 nT"]
-[9.76087760925293, -0.6007044911384583, "[TT] Orbit Altitude of the Corvus-BC = Ranging from 481 - 585 km"]
-[1.767899513244629, 4.544273376464844, "[FF] N/A of the Control Software = N/A"]
-[4.238253116607666, 0.7648515701293945, "[TT] Launch Date of the EDRS = Feb. 1, 2016"]
-[6.8613080978393555, -0.5936219096183777, "[TT] ToO Nominal Duration of Observation of the SVOM = 1 orbit"]
-[6.242568016052246, -1.0893843173980713, "[TT] Mission Duration of the GRACE-FO = 5 years"]
-[8.316985130310059, 7.988945484161377, "[TT] SWIR Detector Material of the GLI = InGaAs"]
-[6.902018070220947, 7.79811429977417, "[TT] Diameter of the Reflector = 1 m"]
-[10.03075122833252, -1.5518776178359985, "[TT] Inclination of the Molniya Orbit = 63.4\u00b0"]
-[7.9141645431518555, 2.3070011138916016, "[FF] Sensor Type of the SeaWiFS = Scanning telescope"]
-[6.45607328414917, -0.4355226755142212, "[TT] Period of the SMDC-ONE = 88.1 minutes"]
-[9.201560974121094, 8.000162124633789, "[TT] Focal Plane of the R3 Sensor = ON Semiconductor LUPA 1300-2 Si:CMOS focal plane"]
-[5.514008045196533, 7.760989665985107, "[TT] EIRP of the Isolated Spot Beams = 65 dBW"]
-[5.62747859954834, 4.575963020324707, "[FF] Communication Status of the YES = Not Re-established"]
-[10.337520599365234, 5.876181125640869, "[TT] Temperature of the MWIR = 300 K (min)"]
-[3.1936447620391846, 1.8341362476348877, "[TT] Data Accuracy of the Sentinel-2 = Timely and accurate"]
-[8.930343627929688, 7.605424404144287, "[TT] Spatial Resolution of the CCD Camera = 30 m"]
-[5.382797718048096, 3.9398751258850098, "[TT] Number of Operational Satellites of the HY-2 = 3"]
-[8.44741439819336, 5.25741720199585, "[FF] AOI Sensitivity of the Etalon = Unknown"]
-[3.5937891006469727, 4.41389799118042, "[FF] Application Topics of the Cross-track SAR Interferometry = Land environment, Navigation, Crisis and security management, Urban areas, Glaciology/hydrology Ice and snow, Sea-ice, Morphology/hydrology Geology Geological mapping/morphology, Earthquakes/volcanoes, Landslides, Subsidence (land and urban areas) Land cover and vegetation Land cover/surface parameters, Forestry, Oceanography Wind and waves/ocean dynamics, Ship detection, Coastal zones Along-track SAR interferometry Oceanography Ocean currents, Coastal zones, Ship detection, Wind and waves Traffic Traffic flow monitoring, Development of new SAR techniques Glaciology Ice flow monitoring Hydrology River flow monitoring, Development of new SAR techniques New SAR techniques Multistatic processing Bistatic/multistatic processing, Land cover, Development of new SAR techniques Pol-InSAR (polarimetric SAR interferometry) Forest, Agriculture, Snow and ice, Ship detection, Wind and waves, Geological mapping, Urban areas, Landslides/subsidence, Earthquakes/volcanoes, Development of new SAR techniques Digital beam forming (DBF) Wide swath imaging and ambiguity suppression, Development of new SAR techniques Super resolution Development of new SAR techniques InSAR processing Development of new SAR techniques, Ultra high resolution DEM with multiple baselines Formation flying Development of new SAR techniques, Precise baseline determination and orbit control"]
-[9.989005088806152, 0.6487223505973816, "[TT] Separation Distance from Earth of the Reentry Vehicle = Around 5,000 km"]
-[4.8732590675354, 0.5846704244613647, "[TT] Year of the Launch Date = 2015"]
-[4.751035213470459, 0.43969935178756714, "[TT] Rescheduled Launch Date of the OFT-2 = No earlier than Aug. 3"]
-[5.088728427886963, 8.397843360900879, "[TT] Bandwidth of the Antenna = 1.1 GHz"]
-[10.061136245727539, 8.171546936035156, "[TT] Telescope of the VIRUS-W = McDonald Observatory\u2019s 2.7-meter Harlan J. Smith Telescope"]
-[7.701408386230469, -2.5272634029388428, "[TT] Observation Duration of the GOLD = About two hours"]
-[13.866903305053711, 3.096313238143921, "[TT] Mass (kg) of the TanDEM-X = 1340"]
-[5.614664554595947, 2.3756394386291504, "[TT] Separated Teams of the Upgrade Team = Three"]
-[8.38979721069336, 1.929634690284729, "[FF] Measurement Swath of the ISS-RapidScat = Smaller by a factor of two compared to QuikSCAT"]
-[6.652184009552002, 4.100481033325195, "[FF] Eclipse Period of the QuakeSat = Current"]
-[7.038701057434082, 8.39116382598877, "[TT] Band of the ROSAT All-Sky Survey (RASS) = 1/4 keV"]
-[6.385228157043457, 4.052535533905029, "[FF] Unknown of the Space Cube 2 Software Design Kit (SDK) = Unknown"]
-[5.528537273406982, 3.039844036102295, "[TT] Sponsorship of the AMS-02 = DOE"]
-[3.8833587169647217, 4.247064113616943, "[TT] Sensor Module Mission Objectives of the RADARSAT-2 = Glacier cover, motion, and topography; ice sheet and land surface topography; and sea-ice cover and type"]
-[7.0299506187438965, 3.5064775943756104, "[FF] URL of the ASPIICS/PROBA-3 = http://congrex.nl/ICSO/Papers/Session%209a/FCXNL-10A02-1987947-1-LANDINI_ICSO_PAPER.pdf"]
-[3.474559783935547, -0.9139119386672974, "[TT] Orbit Type of the Aalto-1 = Sun-synchronous near-circular orbit"]
-[5.4536285400390625, 2.6845669746398926, "[TT] Managed by of the NuSTAR = Goddard"]
-[9.528264045715332, 0.8363682627677917, "[TT] Closest Pass Distance to the Sun of the Solar Orbiter = 0.32 au"]
-[10.684746742248535, 8.309638977050781, "[TT] Main Beam 3 dB Footprint of the ICIR = 10 \u2013 20 km"]
-[9.992534637451172, 7.763883590698242, "[TT] Celestial Sphere Coverage of the Telescope = Continuous within 5\u00ba of ecliptic poles"]
-[3.6879677772521973, 3.846431255340576, "[TT] Launch Date of the RISAT-1A = February 2022"]
-[6.460147380828857, 1.463654637336731, "[FF] Workshop Date of the COSMO-SkyMed = June 12-13, 2007"]
-[4.786767959594727, 0.3736734390258789, "[TT] Arrival Date at ISS of the HTV-7 = 27 September"]
-[6.914924144744873, 2.225005865097046, "[FF] IEEE Transactions on Geoscience and Remote Sensing of the SAMPEX = Vol. 31, No. 3, May 1993, pp. 531-541"]
-[4.262185096740723, 0.31079211831092834, "[TT] Period of Performance of the JPSS-3 and -4 = Through 2026"]
-[7.428199768066406, 2.1541810035705566, "[FF] Mission of the Biomass = Biomass Monitoring Mission for Carbon Assessment"]
-[4.640710830688477, 7.328975200653076, "[TT] Downlink Modulation of the NEMO-AM = Variable"]
-[9.76356029510498, 7.5946149826049805, "[TT] Time Resolution of the NICER = Highest of any astronomy instrument flown"]
-[10.025359153747559, 0.9005824327468872, "[TT] Distance from Earth of the AU Mic = 31.9 light-years"]
-[6.636882781982422, 0.5582285523414612, "[TT] Observations per Day of the Sapphire = More than 3000"]
-[13.27068042755127, 5.424880027770996, "[TT] Deployment of the Solar Panels = Automatic"]
-[8.674891471862793, 7.522372245788574, "[TT] Detector Assembly of the Sounder = 4"]
-[5.578551292419434, 4.575125217437744, "[FF] Communication Status of the MarCO = Loud and Clear"]
-[5.670599937438965, 3.801727771759033, "[FF] Experimental Payloads of the DoT-1 satellite = Flying further experimental payloads as part of SSTL\u2019s ongoing R&D program"]
-[14.188397407531738, 3.2739481925964355, "[TT] Mass of the OTU = 45 kg"]
-[7.511582851409912, 8.148451805114746, "[FF] Change for DSX of the CEASE = CEASE will capture and downlink the full dose spectra from each dosimeter"]
-[8.808777809143066, 7.486614227294922, "[TT] Detector Thickness of the RAMIS = 300 \u00b5m"]
-[7.75644063949585, 6.651031017303467, "[TT] Image Capture Time of the Monitoring Camera 3 = 23:44:57 UTC"]
-[4.680683612823486, 8.237031936645508, "[TT] Center Frequency (GHz) of the Antenna = 23.8"]
-[10.216085433959961, 8.136909484863281, "[TT] Telescope Focal Length of the XMM = 7.5 m"]
-[9.514700889587402, 7.935453414916992, "[TT] LI Optical Head Envelope of the LI = 718 mm x 1200 mm x 1456 mm"]
-[8.788493156433105, 7.510948657989502, "[TT] Coverage of the Imager = Cross-track: \u00b135\u00ba, Along-track: \u00b120\u00ba"]
-[8.911870002746582, 4.464332103729248, "[TT] Scientific Sensors of the SAMPEX = 4"]
-[8.96723747253418, 6.34524393081665, "[TT] Scan Capability of the Argus = None"]
-[8.68127155303955, 3.0392038822174072, "[FF] Source of Uncertainty of the CADRE = Lack of understanding of the upper atmospheric response to energy input near the poles"]
-[5.554238796234131, 0.2677794396877289, "[FF] Anomaly Date of the RapidScat Team = Sept. 9, 2016"]
-[6.1233673095703125, 0.8224439024925232, "[FF] Selection Date of the Lobster-Inspired Mirror = Oct. 27, 2015"]
-[5.108984470367432, 4.378743648529053, "[TT] Number of Satellites of the Starlink = 422"]
-[7.126341819763184, 7.249377727508545, "[TT] Photons Sent per Pulse of the ATLAS = 300 trillion"]
-[5.506746768951416, 0.3932649791240692, "[TT] Launch Year of the ATHENA = 2031"]
-[5.86454439163208, 3.3650543689727783, "[FF] Initial Launch Service Procurement Plan of the Transport Layer Tranche 1 = Under commercial contracts"]
-[13.781200408935547, 5.356285572052002, "[TT] Power Generation Technology of the GaInP2/GaAs/Ge solar arrays = GaInP2/GaAs/Ge"]
-[5.463363170623779, 1.532077431678772, "[FF] Anniversary Symposium Date of the TRMM = Nov. 12, 2012"]
-[5.9133501052856445, -0.43425238132476807, "[TT] Mission Duration of the TSIS-1 = 5 years"]
-[4.899986743927002, 0.5664669275283813, "[TT] Operation Period of the ALT = From launch to July 1979"]
-[10.372747421264648, 2.2854299545288086, "[TT] Energy Range (Blue) of the Chandra X-ray Observatory = 3,000 to 10,000 eV"]
-[8.283337593078613, 7.780079364776611, "[TT] Number of Detectors of the MHS = 4"]
-[11.824247360229492, 3.3646275997161865, "[FF] Category of the PPS-1350-G = Hall-effect thrusters"]
-[9.147871017456055, 4.6491618156433105, "[FF] Attitude Control Strategy of the Microsatellite = Interactive spacecraft pointing for event monitoring support"]
-[4.923623085021973, 0.5284864902496338, "[FF] Start Time of the Planning Process = About three years before launch"]
-[12.880046844482422, 7.530904293060303, "[TT] 2.5 W/sensor head of the Instrument Power = Instrument power 2.5 W/sensor head"]
-[8.558156967163086, 6.127505302429199, "[TT] XY Accuracy of the Planimetric Accuracy Assessment = <0.2 m"]
-[6.371117115020752, -1.1541937589645386, "[TT] Mean LTAN of the KOMPSAT-3 = 13:30 hours"]
-[4.50857400894165, 2.8752129077911377, "[TT] Location of the NGSLR = Maryland, USA"]
-[9.283233642578125, 3.183767795562744, "[FF] Function of the Fabry-Perot etalon interferometer = Analyzing the bi-dimensional distribution of the spectral profiles of several coronal emission lines (CEL)"]
-[5.63627815246582, 3.2550206184387207, "[FF] Development Lead of the GFO satellite system = JPL"]
-[8.287172317504883, 6.881873607635498, "[FF] Sensor Type of the OSA = Optical"]
-[4.91413688659668, 8.065431594848633, "[FF] Center Frequency of the Satellite Device = 89.0 GHz"]
-[4.281557559967041, 2.3345024585723877, "[TT] Launch Site of the BlackSky-1 = Satish Dhawan Space Center"]
-[5.0946245193481445, 8.653432846069336, "[FF] Center Frequency of the Channel = 36.75 \u03bd, h"]
-[4.9674882888793945, 3.115124225616455, "[TT] Manufacturer of the Euclid space telescope = Airbus"]
-[7.52161169052124, -0.8891645073890686, "[TT] Primary Mission Duration of the ICESat-2 = Three years"]
-[5.147892475128174, 2.9200620651245117, "[TT] Affiliation of the IASI = CNES and EUMETSAT"]
-[5.352121829986572, 5.978147983551025, "[FF] Latency of the Space Based AIS Receiving System = Present"]
-[7.138971328735352, 7.0878190994262695, "[TT] Wavelength Accuracy Requirement of the HeNe laser = Less than 3 x 10-7"]
-[13.853829383850098, 5.648377895355225, "[TT] Average Efficiency of the Dual-junction solar cells = 21%"]
-[10.158661842346191, 3.228893518447876, "[FF] Instrument Type of the TROPICS CubeSat = Microwave Spectrometer"]
-[13.952393531799316, 2.7641170024871826, "[TT] Launch Mass of the RASAT = 95 kg"]
-[6.040821552276611, 0.19696331024169922, "[TT] Orbit Lowering Manoeuvre Date of the PARASOL = December 2, 2009"]
-[8.23353385925293, 3.532249689102173, "[FF] Objective of the OCO-2 = Measure sunlight reflected off the Earth's surface"]
-[4.56760835647583, 1.903529167175293, "[TT] Mission Development Start of the RCM (RADARSAT Constellation Mission) = 2005"]
-[4.782522678375244, 7.378711700439453, "[TT] Command UHF-band of the RF communications = 1.2 kbit/s"]
-[7.523408889770508, 3.3673923015594482, "[FF] Contents of the Level-1A = Granule scene sensor output data with geolocation and radiometric correction information"]
-[5.816429138183594, 3.758943557739258, "[FF] Number of Satellites in 2024 of the Sateliot IoT nanosatellite constellation = 64"]
-[7.971194267272949, -0.9184066653251648, "[FF] Freeboard Measurement Data Source of the A-68A = ESA\u2019s CryoSat mission, US ICESat-2 mission"]
-[10.275129318237305, 5.3603129386901855, "[FF] Heat Management of the BepiColombo = Heat generated by spacecraft subsystems and payload components, as well as heat that comes from the Sun and Mercury and \u2018leaks\u2019 through the blankets into the spacecraft, will be conducted to the radiator by heat pipes and ultimately radiated into space"]
-[5.939648151397705, 4.996712684631348, "[FF] Data Transmission of the Ground Station Contact = Occurs above the corresponding minimum elevation"]
-[8.273347854614258, 6.689911842346191, "[TT] Uncertainty of the RSI instrument = 5%"]
-[9.762516975402832, 8.507659912109375, "[TT] IFOV of the SSULI = 0.1\u00ba vertical and 2.4\u00ba horizontal"]
-[10.206686973571777, 5.970059871673584, "[TT] OZA of the Instrument = 55\u00ba"]
-[13.842656135559082, 2.664667844772339, "[TT] Launch Mass of the Spacecraft = 3375 kg"]
-[5.607292652130127, 5.609933376312256, "[TT] Architecture of the Control Computer (CC) = i86"]
-[6.49749755859375, 3.617722749710083, "[FF] Cost Savings of the Integrated recycling/3D printing capability = Reducing the launch mass and volume required for printer feedstock"]
-[12.038480758666992, -0.40213534235954285, "[TT] Final Thruster Burn Date of the TESS = May 30"]
-[13.947234153747559, 7.104227066040039, "[TT] Power Buses of the Data & Power Module = 3.8, 5, 8 and 12 Volts"]
-[8.652661323547363, 3.4791247844696045, "[FF] Importance of the Lithosphere-Atmosphere-Ionosphere Coupling = Fundamental for Earth remote sensing, monitoring of the near-Earth electromagnetic environment and studying of natural hazards"]
-[7.501959800720215, 3.488828659057617, "[TT] Tracking Support of the Debris = Joint Force Space Component Command"]
-[3.8785951137542725, 0.16898946464061737, "[FF] Mission Status Presentation Date of the SMART-1 = March 13-17, 2000"]
-[10.756258964538574, 3.471529245376587, "[TT] Size of the Aalto-1 = 3U CubeSat"]
-[7.875158309936523, 8.437005996704102, "[TT] Pan (panchromatic) of the Spectral bands = 420-890 nm"]
-[7.719096660614014, -0.8459115028381348, "[FF] Global Data Release Date of the ICESat-2 = 28 May 2019"]
-[8.457013130187988, 8.024484634399414, "[TT] Spectral Band (MS B4) of the Pushbroom imager = 0.76-0.89 \u00b5m"]
-[4.775136470794678, 6.4211554527282715, "[TT] Frequency of the LAGRANGE receiver = Dual-frequency"]
-[14.091740608215332, 7.191446781158447, "[TT] Voltage of the Power bus = Regulated 28V \u00b1 2%"]
-[9.704450607299805, 8.293312072753906, "[TT] Lens FOV of the Imager = \u00b18\u00ba"]
-[6.254956245422363, 2.2370011806488037, "[TT] Principal Investigator of the EFI = F. Mozer"]
-[5.2373833656311035, 8.438804626464844, "[TT] Channel Bandwidth of the DCS = 3 kHz"]
-[11.834819793701172, 3.043578863143921, "[FF] Mission Productivity of the Clementine = Scientifically Productive"]
-[14.749063491821289, 6.614326000213623, "[TT] Capacity of the Li-ion battery = 7700 mAh"]
-[9.982998847961426, -1.5825486183166504, "[TT] Orbit Inclination of the CBAS = 0\u00ba"]
-[4.884863376617432, 0.6457161903381348, "[TT] Completion Date of the CMIP5 = 2010 to 2014"]
-[8.44505500793457, 7.71511697769165, "[TT] Imaging Spectrometers of the CASA-212-200 aircraft = Three"]
-[4.468790054321289, 2.857957601547241, "[TT] Location of the STScI = Baltimore, Maryland"]
-[3.475581169128418, -0.9051523804664612, "[TT] Orbit Type of the DMSP = Sun-synchronous"]
-[5.409461498260498, 3.3572840690612793, "[FF] Industries of the OSG = Aerospace, automotive, die/mold, and many others"]
-[9.504069328308105, 1.201831579208374, "[FF] Actual Speed of the Heliosphere = Roughly 7,000 miles per hour slower than previously thought"]
-[5.893486499786377, 1.618324875831604, "[FF] Conference Date of the Oculus-ASR = Sept. 11-14, 2012"]
-[13.234769821166992, 5.2201457023620605, "[TT] Total Area of the Solar Cells = 2 m2"]
-[7.224915027618408, 4.649067401885986, "[FF] Purpose of the XRD = Simulate GRB detection"]
-[8.351978302001953, 7.328202724456787, "[TT] Dynamic Range of the FGM = \u00b10.01 to \u00b1600 nT"]
-[4.175937175750732, 5.867080211639404, "[TT] Data-Handling Time of the ADS-B Receiver = Only a few tenths of a second"]
-[5.578129291534424, -1.9530125856399536, "[FF] Program Update of the GEO-KOMPSAT-2 = Unknown"]
-[6.886063575744629, 0.6873414516448975, "[FF] Livestream Date of the InSight = July 23"]
-[14.185874938964844, 3.2324931621551514, "[TT] Mass of the CAI = 8 kg"]
-[9.575170516967773, 8.210622787475586, "[FF] Field of View of the Trigger Camera = Wide"]
-[14.187089920043945, 3.2943222522735596, "[TT] Mass of the MAG = 40 g"]
-[6.765018939971924, 5.864197731018066, "[TT] Hibernation Mode of the EDM = Yes"]
-[10.410821914672852, 5.688952922821045, "[TT] Temperature (Eclipse Periods) of the Spacecraft = Roughly -50\u00ba C"]
-[10.897404670715332, 2.087601661682129, "[FF] Sensitivity of the XMM-Newton = Incredibly sensitive to signals"]
-[14.283044815063477, 3.196074962615967, "[TT] Total Mass of the WCOM = 1300-1500 kg"]
-[13.693778991699219, 2.8920814990997314, "[TT] Mass of the COSMO-SkyMed spacecraft = 1700 kg"]
-[9.132895469665527, 7.027332782745361, "[TT] CAVIS Ground Resolution of the WorldView-3 = 30 m"]
-[9.240633964538574, -0.32316502928733826, "[TT] Apogee of the COMPASS-2 = 494 km"]
-[18.79961585998535, 3.4775400161743164, "[TT] \u0394r (m) of the Jomo Kenyatta = 11.5"]
-[7.503231525421143, 0.9681947827339172, "[FF] Bulk Density and Porosity Estimates of the GRAIL = Average over the entire crust"]
-[10.464615821838379, 6.868515491485596, "[TT] Focal Length of the Mirror = 10.15 m"]
-[9.253488540649414, 6.916590690612793, "[TT] Spatial Resolution of the JL-1-GF03B = 1 m"]
-[12.729302406311035, 3.8997461795806885, "[FF] Stability of the Reconnection Process = Stable and single"]
-[10.157247543334961, 5.367000102996826, "[FF] Loop Heat Pipe Blockage of the ABI = Caused the instrument to overheat"]
-[6.527384281158447, 1.8509302139282227, "[FF] Content of the VN-rapport = Methaanreductie een van de meest kosteneffectieve maatregelen tegen opwarming"]
-[5.352158546447754, 0.7337464094161987, "[TT] Reorganization Date of the Maxar Space Solutions = February"]
-[8.487785339355469, 6.196570873260498, "[TT] Field of Regard of the TEMPO = Sixth of North America"]
-[6.995938777923584, 6.576684474945068, "[TT] Component Type of the Waveguide switches = Switch"]
-[9.579760551452637, 7.085410118103027, "[TT] Resolution (VIS) of the VHRR = 2.75 km"]
-[2.350140333175659, 1.3257313966751099, "[FF] Attitude Stabilization Method of the NanoSail-D2 = Passive attitude stabilization of the spacecraft will be achieved using permanent magnets to detumble and orient the body with the magnetic field lines and then rely on atmospheric drag to passively stabilize the sailcraft in an essentially maximum drag attitude"]
-[6.774682521820068, 5.264019966125488, "[FF] AFE Type of the F-FEE = Integrated analog front-end (AFE) electronics"]
-[3.333904504776001, 1.4956556558609009, "[TT] Scheduled Launch Date of the Sentinel-1C = March 2024"]
-[6.031334400177002, 3.1432864665985107, "[FF] Management of the GOES-R = Collaborative effort between NOAA and NASA"]
-[7.173689842224121, 4.477800369262695, "[FF] Mounting of the OCSE = JAWSAT payload"]
-[5.845165252685547, -0.32376906275749207, "[TT] Maximum In-Storage Period of the MWI Instrument = 19 years"]
-[10.623340606689453, 7.346900939941406, "[TT] Swath Width of the OBRC instrument = 450-600 km"]
-[8.346803665161133, 5.424427032470703, "[TT] Spectral Calibration Accuracy of the Satellite = < 0.02 nm"]
-[6.6071319580078125, 2.1514482498168945, "[FF] Mission of the PanFTS = GEO-CAPE"]
-[10.779155731201172, 2.9546897411346436, "[TT] Mission Duration of the O/OREOS nanosatellite = 6 months"]
-[9.859260559082031, 4.72095251083374, "[TT] Spin Rate of the Genesis spacecraft = One revolution in 37.5 seconds"]
-[9.174236297607422, -0.5534075498580933, "[TT] Coverage of the SpinKF = Every orbit perigee-to-perigee"]
-[9.6128568649292, 3.77168869972229, "[TT] Magnetic Field Strength of the Rho Ophiuchi A = 500 times stronger than that of the Sun"]
-[5.321568965911865, 7.011116981506348, "[FF] Data Communication Speed of the KIZUNA = 1.2 Gbit/s"]
-[5.441527843475342, 3.4922778606414795, "[TT] Operator of the SES-14 = SES, a Luxembourg-based satellite operator"]
-[5.6035614013671875, 0.45601946115493774, "[TT] End of Operations Date of the GEOS-3 = July 1979"]
-[5.566834449768066, -2.0257792472839355, "[FF] Imaging Objective of the KOMPSAT-1 = Collect wide-swath multispectral imagery of the ocean and coastal zones"]
-[3.8340506553649902, 7.206457614898682, "[TT] Gain of the Antennas = \u20134 dBic minimum"]
-[6.385751247406006, -0.2738461494445801, "[TT] Observation Period Duration of the SORCE = 11 years"]
-[8.10451602935791, 1.192162275314331, "[FF] URL of the SMAP = http://www.nasa.gov/press-release/nasa-soil-moisture-mission-begins-science-operations"]
-[5.131526947021484, -0.5930694341659546, "[FF] Mission Failure of the TARANIS = 16 November 2020"]
-[7.169943332672119, 4.484771251678467, "[FF] Stowed Configuration of the LF spacecraft = Illustrated in Figure 2(b)"]
-[10.143352508544922, 9.991241455078125, "[TT] Final Reentry Process of the Vega = Direct reentry and burn up high in the atmosphere over the ocean"]
-[9.103653907775879, 3.872404098510742, "[FF] Passive Temperature Control of the SVM = Mirror solar reflectors on the Sun-side, white paint on the anti-sun side"]
-[6.720711708068848, 1.1366956233978271, "[FF] Media Showing Date of the Mercury Magnetosphere Orbiter = March 19, 2015"]
-[7.397951602935791, 2.345249652862549, "[TT] Global Mapping Achievement of the Satellite = 36.1%"]
-[4.738389492034912, 1.821454644203186, "[FF] Symposium Date of the Geosat Follow-On = March 13-18, 2006"]
-[10.621577262878418, 1.3840653896331787, "[TT] Energy Absorption of the Open ocean water = 90 percent of the Sun\u2019s energy"]
-[8.267752647399902, 8.684952735900879, "[TT] Launch Date of the Multi-band UV/VIS Spectrometer (ACE) = 21 November 2013"]
-[6.286914348602295, 3.0315513610839844, "[FF] Regions of the Data Nodes = Asia, Europe and Africa, North and South America, Australia and Oceania"]
-[5.5354838371276855, 5.675765037536621, "[FF] Reliable file transfer of the TCP protocols = Yes"]
-[10.671018600463867, 3.3070337772369385, "[FF] Objective of the Micro-gravity experiment = Investigate the coupling between heat capillary convection and buoyancy convection, and other phenomena"]
-[6.082090854644775, 0.5591456294059753, "[TT] Communication Status of the ASTERIA = Lost"]
-[8.472677230834961, 6.806767463684082, "[TT] Carries of the Beijing-3B = Larger and higher resolution optical imager"]
-[11.310914039611816, 5.070608615875244, "[TT] Length of the NuSTAR instrument = 10 m"]
-[9.200902938842773, -0.8158836364746094, "[FF] Location of the ETC = 31\u00b0 31' South and 64\u00b0 27' West"]
-[6.754533767700195, 4.595473289489746, "[FF] Function of the IBS LR = Act as a load bypass mechanism for the bearings contained within the SMA and provide a direct load path for the supported mass into the spacecraft interface"]
-[12.181159019470215, 3.0097262859344482, "[TT] Propulsion System of the EAGLE ESPAStar = Hydrazine-based monopropellant"]
-[9.340092658996582, 0.07230734080076218, "[TT] Circumference of the Aso Caldera = 120 km"]
-[4.858179569244385, 4.453940391540527, "[TT] Platform Data Rates of the Argos System = Higher"]
-[11.077862739562988, 5.016556262969971, "[TT] Measurement Difference of the CDN1 transponder = Less than 2 mm"]
-[5.365893363952637, 0.2393798530101776, "[TT] Launch Date of the STS-66 = Nov. 3-14, 1994"]
-[10.09773063659668, 8.077275276184082, "[TT] Depth of Focus of the Telescope = 10 \u00b5m"]
-[9.023682594299316, 8.534073829650879, "[TT] Spectral Sampling of the Telescope = 2.55 nm"]
-[10.523175239562988, 6.572329521179199, "[TT] Number of Shells of the ART-XC's mirrors = Seven sets of 28 nested shells"]
-[14.090912818908691, 3.215385913848877, "[TT] Mass of the X50M = Approximately 100 kg"]
-[9.359709739685059, 4.781521797180176, "[TT] Attitude Control Subsystem of the DMSP-19 = New"]
-[12.722990989685059, 3.894596815109253, "[FF] Reconnection Lines of the Magnetopause = Multiple"]
-[4.2994537353515625, 2.5523362159729004, "[TT] Launch Location of the Orion = Cape Canaveral, Florida"]
-[4.755290985107422, 5.822940349578857, "[FF] Transmission Overlap of the Stensat Beacon = Observed"]
-[5.467311859130859, 0.8287045359611511, "[FF] Arrival Date of the European Data Relay System = 18 June 2019"]
-[8.882914543151855, 9.471426963806152, "[TT] Improvement Factor of the TANSO-FTS-2 = 2.3 times"]
-[5.469069957733154, 6.649190425872803, "[TT] Message Volume of the Onboard data collection and transmission system = 250 bit"]
-[8.811026573181152, 5.843667030334473, "[TT] Measurement Range of the ADCs = 0 - 4.096 V"]
-[12.087118148803711, 4.346126079559326, "[TT] Height of the DubaiSat-1 = 1.35 m"]
-[7.669650077819824, 8.442689895629883, "[FF] NIR/SWIR Bands of the MSI = Additional NIR/SWIR bands"]
-[10.224087715148926, 8.109014511108398, "[TT] Aperture Diameter of the Geoton-L1 imager = 50 cm"]
-[4.9344611167907715, 8.328466415405273, "[TT] Frequency Range of the MWNIR = 6.6 GHz - 37 GHz"]
-[5.5531325340271, 5.684512138366699, "[TT] Processor of the C&DH = Sharp LH79520 ARM microprocessor"]
-[8.085236549377441, 4.564256191253662, "[FF] Mission Focus of the CUMULOS = Operation of passively cooled COTS sensors and cameras, weather and environmental monitoring"]
-[6.188945293426514, 5.991734981536865, "[TT] Function of the TCU = Controls all 24 TR modules on a tile"]
-[14.34976863861084, 3.112691879272461, "[TT] Mass of the S/C structure = About 8 kg"]
-[13.978374481201172, 3.1909332275390625, "[TT] Mass of the Module = ~ 2.5 kg"]
-[4.198009967803955, 0.15501129627227783, "[TT] Launch Date of the SpaceX Falcon-9 Block 5 = 3 December 2018"]
-[14.103778839111328, 4.011939525604248, "[TT] Mass of the Instrument = ~ 10 kg"]
-[9.672743797302246, 7.177052974700928, "[TT] Spatial Resolution in Low Resolution Mode of the OBRC instrument = 700-1000 m"]
-[8.579936981201172, 7.067481517791748, "[TT] Image Quality of the Payload = Maintained at consistent levels for more than 14 years"]
-[6.612410068511963, 3.580880880355835, "[FF] NESZ of the Capella = Unknown"]
-[5.767509460449219, -0.8799428343772888, "[TT] S/C Design Life of the Payload = Up to 12 years"]
-[7.747965335845947, 2.123520612716675, "[TT] Maximum Latitude Coverage of the ISS = \u00b154.33\u00ba"]
-[9.655296325683594, 5.025336742401123, "[TT] Drift Rate of the AOCS = \u00b1 3.0 x 10 -4 \u00ba/s"]
-[4.734099388122559, -1.178227424621582, "[TT] Launch Date of the Beijing-3B = 24 August 2022"]
-[10.016490936279297, -1.5695770978927612, "[TT] Orbit Inclination of the Rocket 3.3 = 86\u00ba"]
-[5.384907245635986, 2.584038496017456, "[FF] Managing Agency of the ADEOS = NASDA, the National Space Development Agency of Japan"]
-[6.265476703643799, 8.630610466003418, "[TT] Polarization of the SASS = Dual-polarised"]
-[6.583102703094482, -2.0632948875427246, "[FF] Operation Start Date of the T2L2/Jason2 = Unknown"]
-[8.914883613586426, 9.441397666931152, "[TT] Spatial Resolution of the TANSO-FTS-2 = Higher than TANSO-CAI-2"]
-[5.673648834228516, 11.349467277526855, "[FF] Approx. peak sensitivity altitude of the Channel 3 = Unknown"]
-[5.720131874084473, 1.1269786357879639, "[FF] Launch Date of the EROS-C = Not set so far"]
-[5.055593013763428, 1.6858896017074585, "[TT] Operating Status of the Odin = Nominal"]
-[5.745115756988525, 1.4059951305389404, "[FF] Authors of the HyperScout = Michael Soukup, Janis Gailis, Daniele Fantin, Arnoud Jochemsen, Christina Aas, Pieter-Jan Baeck, Iskander Benhadj, Stefan Livens, Bavo Delaur\u00e9, Massimo Menenti, Ben Gorte, Seyed Enayat Hosseini Aria, Marco Esposito, Chris van Dijk"]
-[5.442691802978516, 6.393855571746826, "[TT] Data Storage Capacity of the Data Transmission Subsystem = 128 Gbit"]
-[7.5921101570129395, 5.420989990234375, "[FF] Components of the Telescope = M1A (Primary Mirror Assembly), M2 A (Secondary Mirror Assembly), CLA (Correction Lens Assembly), the metering structure"]
-[4.6861090660095215, 6.962789535522461, "[TT] Uplink Band of the Spacecraft = S-band (2 kbit/s)"]
-[8.594219207763672, 0.17460322380065918, "[FF] Activity of the Comet = Increased around the closest approach to the Sun"]
-[12.17632007598877, 4.559677600860596, "[TT] Parking Orbit Dimensions of the Spacecraft and Propulsion Module = 200 km x 1600 km"]
-[6.453022003173828, 3.535926342010498, "[FF] Use of the DMSP = Strategic and tactical weather prediction for the US military"]
-[10.55135440826416, 5.800872325897217, "[TT] Battery Temperature Range of the HORYU-2 = 10 to 12\u00baC"]
-[13.313590049743652, 6.8871026039123535, "[TT] Power of the Spacecraft = ~1.5 W"]
-[9.332418441772461, 7.583021640777588, "[FF] Imaging Capability of the Kestrel Eye-2M = Spot objects on Earth's surface about the size of a car"]
-[7.935917854309082, 0.6419411897659302, "[TT] Glacier and Ice Cap Surface Velocity Spatial Resolution of the ROSE-L = 10 m"]
-[5.109526634216309, -0.3687771260738373, "[TT] Retirement Date of the CBERS-2 = Late 2007"]
-[13.971893310546875, 3.7135303020477295, "[TT] Mass of the Lens Assembly = 266 g"]
-[5.056590557098389, 3.5835275650024414, "[TT] Instrument Type of the GovSat-1 = Communications"]
-[5.84523868560791, 1.0286933183670044, "[FF] Press Release Date of the AgNeo = 6 March 2020"]
-[11.023159980773926, 6.195337772369385, "[TT] Material of the Optical Window = Fused Silica"]
-[11.01031494140625, 5.693040370941162, "[FF] Composition of the Avcoat = Heat-retardant substance similar to what the Apollo missions used, with the exception of toxic materials like asbestos"]
-[8.89058780670166, -0.9070972204208374, "[TT] Orbit Type of the GNSS Satellites = Medium Earth Orbit (MEO)"]
-[7.703634738922119, 6.908304214477539, "[TT] Pixel Exposure Time of the Instrument = 2.0, 4.1, 8.2 ms (VIS); 6.6, 13.2, 26.4 ms (NIR)"]
-[8.979750633239746, 0.7622628808021545, "[TT] Surface Mobility of the MASCOT = Tungsten swing arm accelerated and decelerated by a motor"]
-[13.850234031677246, 3.0477652549743652, "[FF] Mass of the Sacred = Unknown"]
-[7.10187292098999, 7.214456558227539, "[TT] Pulse Width of the ATLAS = 6-7 ns"]
-[13.35451602935791, 6.601691722869873, "[TT] Power of the CICERO satellites = Around 21 W"]
-[7.3420586585998535, 6.321498394012451, "[TT] Data Collection Frequency of the ABI = Every 10-15 minutes"]
-[14.640562057495117, 6.660301685333252, "[TT] Capacity of the Battery = 12 Ah"]
-[7.945418834686279, 0.3450305461883545, "[FF] Data Usage of the GRACE = Hydrological variations monitoring"]
-[8.695069313049316, 3.90653395652771, "[FF] Measurement of the EFP = DC and AC electric fields"]
-[9.784255981445312, 4.484964847564697, "[TT] Attitude Control of the CubeSats = Passive magnetic"]
-[5.910367965698242, 6.503218650817871, "[TT] Data Availability of the CATS = Freely available"]
-[13.031384468078613, 7.61044454574585, "[TT] Power Dissipation of the LCT = Varies"]
-[9.716139793395996, 5.185583591461182, "[FF] Connection Type of the Lower Barrel and Inner Sleeve = Double lap shear bonded connection"]
-[4.939773082733154, 3.4777817726135254, "[FF] Manufacturer of the OLA = MDA (MacDonald Dettwiler & Associates) and Optech Inc."]
-[5.261500835418701, 3.3109004497528076, "[FF] Center Locations of the DSDS = CSSAR, Beijing, China; IWF (Institut f\u00fcr Weltraumforschung), Graz, Austria; RAL (Rutherford Appleton Laboratory), Didcot, UK; French DSP Data Center, at CNES, Toulouse, France"]
-[5.982396602630615, 2.456144094467163, "[TT] Launch Schedule of the Worldview Legion = First quarter of 2021"]
-[3.878066062927246, 6.200599193572998, "[FF] Health Check Experiment of the Active Phased Array Antenna Elements = Conducted"]
-[7.515632629394531, 7.011443614959717, "[TT] Pulse Duration of the SIRAL = 50 \u00b5s"]
-[12.016875267028809, 3.022883415222168, "[TT] Thrusters of the Satellite Bus = 12 hydrazine thrusters"]
-[5.979349136352539, 2.0143561363220215, "[FF] Mission Status of the SwRI Small Satellite = Forward"]
-[3.91536545753479, 6.368165493011475, "[TT] Antenna Usage of the Ground Segment = Transmitting and Receiving"]
-[12.033270835876465, 6.510105609893799, "[TT] Energy Range of the AMS-02 = Up to multi-TeV"]
-[9.420019149780273, 0.9030267000198364, "[TT] Distance from Sun of the Oort Cloud = About 185 billion miles"]
-[4.557097434997559, -0.8866259455680847, "[TT] Mission Status of the Dragon spacecraft = Mission complete"]
-[10.719165802001953, 3.84488582611084, "[TT] Deployment Date of the Drag de-orbit sail = June 23, 2017"]
-[6.194753646850586, 4.296526908874512, "[FF] Capability of the Remote Agent = Detected, diagnosed and fixed simulated problems"]
-[11.401034355163574, 4.2832770347595215, "[TT] Size of the EagleSat-2 = 3U"]
-[7.437479496002197, 3.061880111694336, "[TT] Sensor Type of the MethaneSat = Spectrometer"]
-[5.665104389190674, 5.553962230682373, "[TT] Microcontroller of the CDHS = PIC24"]
-[9.404075622558594, 7.411883354187012, "[TT] Nadir image size (1000 km altitude) of the 16 mm camera = 110 km x 120 km x 92.8 km"]
-[4.7002692222595215, 0.5255298018455505, "[TT] Generation of the GOES 2nd generation spacecraft = 2nd"]
-[10.040566444396973, 6.545033931732178, "[FF] Mirror Type of the SeaWiFS = Rotating half-angle mirror"]
-[4.447826385498047, 4.585730075836182, "[FF] Ground Segment Components of the COSPAS-SARSAT = Local User Terminals (LUTs), Mission Control Centres (MCCs), Rescue Coordination Centres (RCCs)"]
-[8.102764129638672, 8.510856628417969, "[TT] Spectral Bands of the Geoton-1 = 8 bands in the VNIR spectral range"]
-[7.828437805175781, 7.5425286293029785, "[TT] Bit Depth of the MSS Instrument = 6 bit per pixel"]
-[14.608235359191895, 6.634778022766113, "[TT] Type of the Batteries = Lithium-ion 18650"]
-[4.865365028381348, 3.1175239086151123, "[TT] Manufacturer of the JUICE = Airbus"]
-[9.533320426940918, 6.450104236602783, "[TT] Observation Directions of the MSU-100 = \u00b18.7\u00ba, 0\u00ba"]
-[7.716156005859375, 7.1846842765808105, "[TT] Frame Rate of the Detector = 500 Hz (ROI function), 30 Hz (full frame)"]
-[4.410851001739502, 3.069195032119751, "[TT] Location of the GSC = Guildford (UK)"]
-[7.759074687957764, -2.5512020587921143, "[TT] Mission of the GOLD = Global-scale Observations of the Limb and Disk"]
-[13.610522270202637, 3.001060724258423, "[TT] Payload Capacity of the LEOStar-2 = Up to 500 kg"]
-[5.248286247253418, 1.056727409362793, "[FF] Meeting Date of the TriG = September 22-25, 2009"]
-[2.8972134590148926, 1.939003825187683, "[FF] Image Capture Date of the Copernicus Sentinel-2 = June 2022"]
-[8.009944915771484, 6.302929878234863, "[TT] Instrument Type of the SPOT-5 = Imaging multi-spectral radiometers (vis/IR), High resolution optical imagers, Precision orbit"]
-[7.822192192077637, 7.0926618576049805, "[FF] On-axis Unapodized Spectral Resolution Requirement of the Michelson Interferometer = \u2264to the values given in Table 5"]
-[5.134459018707275, 4.907660484313965, "[TT] Type of the GPS receiver = SGR-20 model"]
-[7.885534286499023, 8.00600528717041, "[TT] Spectral Bands of the HSC-III optics subsystem = 61"]
-[5.895950794219971, 0.9137503504753113, "[FF] Observation Data Acquisition Date of the SHIKISAI = Jan. 12, 2018"]
-[9.4946928024292, 7.2787861824035645, "[TT] Infrared Subsystem Resolution of the Westinghouse OLS = 3.7 km at the surface day and night"]
-[14.317481994628906, 6.479086875915527, "[TT] Battery Charging Time of the NextSat = Within a single orbit"]
-[9.327455520629883, 2.5192065238952637, "[FF] Speed of the Solar Energetic Particles = Close to the speed of light"]
-[7.246927261352539, 0.9513047933578491, "[TT] Launch Date of the SeaSat = January 1975"]
-[4.984274864196777, -0.4079383611679077, "[TT] Launch Time of the SOCRATES = 03:05 UTC"]
-[5.636110782623291, 5.6636643409729, "[TT] Microprocessor of the OBC = MPC860T"]
-[8.44387149810791, 1.1451270580291748, "[TT] Spatial Resolution of the Solid Earth Tectonic motions = 100 km"]
-[4.876707553863525, 4.300385475158691, "[FF] Miniaturization of the ARGOS-NEO payload = In progress"]
-[3.6250619888305664, 2.653977155685425, "[TT] Remaining Launches of the Iridium NEXT = 2 of 10 satellites each"]
-[10.946449279785156, 7.566962242126465, "[TT] Swath Width of the TopSAR narrow = 100 - 150 km"]
-[9.893264770507812, -0.3964461386203766, "[TT] Altitude of the Satellite = 681-709 km"]
-[9.554289817810059, 0.3115101158618927, "[TT] Location of the Yutu-2 = Arrived at preset location A"]
-[13.698675155639648, 3.4314894676208496, "[TT] Mass of the S-band transceiver = 1.6 kg"]
-[9.506772994995117, 5.532691955566406, "[TT] Maximum Slew Rate of the APM = 4\u00ba/s"]
-[13.727231979370117, 2.86063814163208, "[TT] Mass of the Spacecraft = 521 kg"]
-[5.618127822875977, 4.034929275512695, "[TT] Type of the GGAK-M = Space environment"]
-[14.173660278320312, 3.2898762226104736, "[TT] Mass of the MHX-2400 = 75 g"]
-[7.845364093780518, 6.005136013031006, "[TT] Device Type of the SSM/T-1 = Radiometer"]
-[4.838331699371338, 4.290928840637207, "[TT] Data Collection System of the ADEOS-II = Argos-Next"]
-[13.086723327636719, 5.553771495819092, "[FF] Subsystem Selection Aspects of the MERLIN = Power consumption, mass and volume allocations, thermal behaviour, radiation hardness"]
-[9.077868461608887, 7.166139125823975, "[FF] Resolution of the EXI = High resolution"]
-[10.844836235046387, 0.9630012512207031, "[TT] Number of Accurately Characterized of the Brown Dwarfs = About 30"]
-[9.338743209838867, 5.302972793579102, "[TT] Mechanism of the HGA = Two-axis gimbal"]
-[5.318404197692871, 4.021096229553223, "[TT] Number of Satellites of the T1TL Prototype Constellation = 42"]
-[8.985079765319824, 4.400546073913574, "[TT] Sensor Type of the CubeSense = Integrated sun and nadir sensor"]
-[5.079167366027832, -0.7880324721336365, "[TT] Reentry Burn Duration of the First Stage = 19 seconds"]
-[6.518948554992676, -0.3085401654243469, "[TT] Standard Deviation of Time Between Resets of the BRMM = 6 days"]
-[9.953714370727539, 0.42866867780685425, "[TT] Formation Control Accuracy of the PRISMA = Decimeter level"]
-[11.846124649047852, 4.955132484436035, "[TT] Dimensions of the FENIX micropropulsion device = 10 cm long and 2 cm wide"]
-[6.028148651123047, 6.5917768478393555, "[TT] Throughput of the QLP/NRTP = Real-time (QLP) to max 45 minutes (NRTP) per scene, 10-15 GFLOPS"]
-[7.63481330871582, 4.68432092666626, "[FF] Function of the TRD = Identify electrons and positrons"]
-[8.111756324768066, -1.032412052154541, "[FF] Objective 2 of the ICESat-2 = Determine the seasonal cycle and topographic character of ice sheet changes"]
-[7.216320991516113, 3.452544689178467, "[FF] Purpose of the Proba-3 = Creating an artificial solar eclipse every day"]
-[8.254566192626953, 6.5809855461120605, "[TT] Scan Rate of the MSU-E = 200 lines/s"]
-[5.17941427230835, 3.293384552001953, "[TT] Manufacturer of the Landsat 9 = NASA"]
-[5.91258430480957, 3.5437307357788086, "[FF] Deployment of the DSX = Attached to the ESPA ring"]
-[7.826733112335205, 8.12917709350586, "[TT] Band 6 of the R3 Sensor = Green"]
-[9.851953506469727, 8.780407905578613, "[TT] Swath/FOV of the GOSAT-2 = Band 4, 786 km (60\u00ba)"]
-[8.609854698181152, 7.670163631439209, "[TT] Power of the CCD Camera = <50 W"]
-[9.44315242767334, -0.34459641575813293, "[TT] Perigee of the SCD-2 = 743 km"]
-[4.9260663986206055, 1.9907866716384888, "[FF] Project and Mission Overview of the GOSAT = Not provided"]
-[10.273326873779297, 8.416781425476074, "[TT] Entrance Pupil Diameter of the TESS Lens = 10.5 cm"]
-[10.699054718017578, 3.9090423583984375, "[FF] Purpose of the Bigelow Aerospace BEAM = Provide operational experience with inflatable modules in a crewed environment"]
-[7.944843769073486, 8.06070613861084, "[FF] Imaging Sensor of the Landsat-5 = Combines infrared, red, and green wavelengths"]
-[3.8368797302246094, 6.4885759353637695, "[TT] Antenna Position of the SIR-C = 38\u00ba"]
-[3.7157931327819824, 6.474842548370361, "[TT] Isolation Method of the KaRIn = Offset feed reflectarray antennas"]
-[5.0135345458984375, 0.5888045430183411, "[TT] Launch Date of the ESAIL = 12 June 2020"]
-[8.304418563842773, 8.754927635192871, "[TT] Slit 1 Spectral Range of the MEGS-A = 5-20 nm"]
-[11.14005184173584, 0.5223100185394287, "[TT] Number of Exoplanets of the TOI 2076 and TOI 1807 = Four"]
-[9.378856658935547, 5.315680980682373, "[TT] Expected Initial Tumbling Rates of the Satellite = Less than 30\u00ba/s"]
-[5.205776214599609, 1.4696121215820312, "[FF] Initial Products of the INSAT-3D = http://www.isro.org/pdf/insat-3d-imager.pdf"]
-[9.795513153076172, 4.510861873626709, "[FF] Control Methods of the Attitude Control = Magnetorquer-assisted gravity gradient, 3-axis reaction wheels and 3 magnetorquers"]
-[5.426349639892578, 5.633859157562256, "[TT] Number of Processors of the RISAT-1 = 300"]
-[8.886730194091797, 4.78264856338501, "[FF] Detection Target of the SVOM Attitude = GRB on the night side"]
-[7.655281066894531, 6.523757457733154, "[FF] Image Delivery Time of the 24/7 Emergency Image Delivery Service = Averaging two hours after acquisition"]
-[6.825209140777588, 1.5701117515563965, "[TT] Ground Testing of the Galaxy = Underway"]
-[13.600269317626953, 1.736585259437561, "[TT] Payload Delivery of the Dragon = More than 5,600 pounds of science and supplies"]
-[3.4461019039154053, -0.4852495789527893, "[TT] Orbit Type of the JL-1-GF03B = SSO"]
-[11.701510429382324, 6.499480724334717, "[TT] Detects of the JADE = Energetic electrons"]
-[6.566277503967285, 5.910353183746338, "[FF] Conference Presentation of the Laser Communications Relay Demonstration Project = URL: http://www.spaceops2012.org/proceedings/documents/id1261897-paper-001.pdf"]
-[3.643876075744629, -1.0321862697601318, "[TT] Injection Trajectory of the Launch Segment = Earth-Sun L2 (ES-L2)"]
-[4.342968463897705, 3.283376455307007, "[TT] Antenna Test Location of the EDRS-C = CATR (Compact Antenna Test Range) at Airbus in Ottobrunn Germany"]
-[7.25111722946167, 2.9781930446624756, "[FF] Payload of the MethaneSAT = DigitalGlobe"]
-[7.014120101928711, 9.31302547454834, "[TT] NEDT of the Instrument = 0.2 K@300 K"]
-[4.6590495109558105, 7.117076873779297, "[TT] X-band Downlink Transmission Data Rates of the CBERS-2B = 60 Mbit/s"]
-[13.081740379333496, 7.243268013000488, "[TT] Power of the Horizon sensor = 2.8 W"]
-[6.786919116973877, 4.141397476196289, "[TT] Function of the OPS = Observation"]
-[5.601507186889648, 6.0870466232299805, "[FF] Memory Type of the DSU = Non-volatile memory"]
-[7.031692981719971, 6.098820209503174, "[TT] Instrument Suite of the FY-4B = Four instruments"]
-[7.827902793884277, 8.615910530090332, "[TT] Channel Band (\u00b5m) of the LWIR (Longwave Infrared) = 8.0-9.0"]
-[1.6048730611801147, 3.7598586082458496, "[FF] Purpose of the Beesat-5,-6,-7,-8 smallsats = Unknown"]
-[6.726741313934326, 6.02285623550415, "[TT] Number of Subapertures of the SMART = 8"]
-[4.664862632751465, 1.0936217308044434, "[TT] Operation Status of the FY-3B = Operating in 2016"]
-[7.875112533569336, 2.5502264499664307, "[TT] Measurement Domain of the ZACUBE-2 = Land"]
-[7.706579208374023, 3.4584763050079346, "[FF] Contribution to Debris of the Net and Harpoon = Not contribute to the production of further debris in space"]
-[6.8088250160217285, 5.9539384841918945, "[TT] Quantity in ADCS controller of the StrongARM SA1110 = 1"]
-[8.176481246948242, 8.783552169799805, "[TT] Wavelengths of the Spectrometer = 1020, 940, 600, 525, 453, 448, and 385 nm"]
-[9.941459655761719, 8.198155403137207, "[TT] Focal Length of the MS1/2, MS3/4 = 220 mm"]
-[5.3301191329956055, 1.088706612586975, "[FF] First Image Date of the SMOS = Feb. 23, 2010"]
-[7.011897087097168, 4.386380672454834, "[FF] Unknown of the Vulcan Wireless = Unknown"]
-[5.374428749084473, 6.11942195892334, "[TT] Program Memory of the Memory = 4 MByte TMR protected SRAM"]
-[4.861978530883789, -1.7661833763122559, "[TT] Landing Site of the Chang'e-4 = Von Karman crater in the South-Pole-Aitken (SPA) basin"]
-[12.131534576416016, 3.4629478454589844, "[FF] Propellant of the IES = Xenon gas"]
-[6.630380153656006, 0.30815452337265015, "[TT] Documented On-Orbit Anomalies of the BRMM = 24"]
-[3.4503543376922607, 1.8535672426223755, "[FF] Mission Status of the Sentinel-1 = Current"]
-[10.401339530944824, 5.745400905609131, "[TT] Total Temperature Range of the EO Module = 25\u00b110\u00b0C"]
-[10.4793062210083, 3.271192789077759, "[TT] Form Factor of the Ubotica CogniSAT-XE1TM CubeSat Board = PC/104"]
-[7.833656311035156, 2.7597341537475586, "[FF] Purpose of the KBR = Measure Earth's gravity field"]
-[10.39201545715332, 2.110071897506714, "[TT] Observed Parts of X-ray Light Spectrum of the NuSTAR = High-energy"]
-[5.163370132446289, 3.8109073638916016, "[FF] Operation of the EDR-2 = Run in parallel with the original European Drawer Rack"]
-[5.653924465179443, 5.002239227294922, "[FF] Function of the EDRS-C = Second node in the European Data Relay System"]
-[9.182331085205078, 7.3320698738098145, "[TT] Spatial Resolution of the WorldView-1 = 0.5 m panchromatic"]
-[5.514052391052246, 2.897529125213623, "[FF] Design Teams of the QSP-1 = Germany, Sweden, and the US"]
-[10.472858428955078, 2.909670114517212, "[TT] Communication Frequencies of the Nanosatellite = UHF, VHF"]
-[14.189738273620605, 3.1804585456848145, "[TT] Mass of the CBNT-1 (Carbonite-1) = 91 kg"]
-[7.560001373291016, 4.875810623168945, "[TT] Data Transmission Frequency of the Instrument = About once a month"]
-[4.816450595855713, 8.562931060791016, "[TT] Center Frequency of the Channel 5 = 36.5 GHz"]
-[8.991379737854004, 2.8557169437408447, "[FF] Purpose of the SWAP and LYRA = Space Weather Observation"]
-[4.388779640197754, 7.864936351776123, "[TT] Downlink Frequency of the DCS = 460-470 MHz"]
-[7.2023420333862305, 1.2550033330917358, "[FF] Function of the Mars Ascent Vehicle = Launch samples into orbit around Mars"]
-[7.192344665527344, 6.804605484008789, "[TT] Low-Energy Transmitter Range of the OLA = 500 m to 1 km"]
-[9.612977981567383, -0.4744517505168915, "[TT] Altitude of the Beijing-1 = 686 km"]
-[5.044926166534424, 4.444282054901123, "[TT] Operation of the DASS = Independent GPS-III payload"]
-[8.077301979064941, 2.1052303314208984, "[FF] Objectives of the NIRST = Hot spot events, SST (Sea Surface Temperature) measurements"]
-[5.419097423553467, 4.195751667022705, "[TT] Bus Type of the DSP satellites = CAST968"]
-[10.330086708068848, 5.536743640899658, "[TT] Temperature of the Solar Corona = More than a million degree Kelvin"]
-[8.436727523803711, 8.076414108276367, "[TT] Number of Pixels of the TDI Array = Four lines of 1750 pixels for the MS (multispectral) bands"]
-[12.117151260375977, 4.544011116027832, "[TT] Wing Span of the Spacecraft bus = 13.7 m"]
-[5.64059591293335, 3.23591685295105, "[TT] Contract Value of the JPSS-3 and -4 = $460 million"]
-[9.858386039733887, 4.271849155426025, "[TT] Magnet Configuration of the AMS-02 = Permanent"]
-[10.8259859085083, 2.114353656768799, "[TT] X-ray Observations of the XMM-Newton = March 2014 and June 2016"]
-[10.027887344360352, 2.7750766277313232, "[TT] Manufacturer of the NanoSatC-Br1 = Southern Regional Space Research Center and of INPE"]
-[9.85621452331543, 8.806292533874512, "[TT] Swath/FOV of the GOSAT-2 = Band 1-3, 1002 km (72\u00ba)"]
-[10.283577919006348, 0.896894633769989, "[TT] Distance from Earth of the Kepler-442b = 1,100 light-years"]
-[3.7546820640563965, 6.620843410491943, "[TT] Characteristic Impedance of the Sprite\u2019s antenna = 50 ohm"]
-[9.932879447937012, 5.531785488128662, "[FF] Function of the Heater Control System = Maintains thermal control of the focal planes when pointing the instrument at off-nadir ground targets"]
-[7.009750843048096, 7.139101982116699, "[TT] Pulse Width of the Micropulse Laser Transmitter = 1 ns"]
-[6.274002552032471, 6.09645938873291, "[TT] Performance of the APW = Exceptional"]
-[8.20124340057373, 2.2153944969177246, "[FF] Mission of the INCUS = Provide the first tropics-wide investigation of the evolution of the vertical transport of air and water by convective storms"]
-[10.051334381103516, 1.9105747938156128, "[FF] Orbit Phase Orbit Determination Date of the Chandrayaan-1 = Oct. 12-16, 2009"]
-[4.711245536804199, 5.333037853240967, "[FF] Function of the ISM = Registers the pulse from the Mire Beacons on CSC to synchronize the integration of the WAC and NAC with the pulsed Beacon"]
-[5.678021430969238, 11.362378120422363, "[FF] Approx. peak sensitivity altitude of the Channel 6 = Unknown"]
-[13.777480125427246, 2.873270273208618, "[TT] Mass of the Lunar Pathfinder = 280 kg"]
-[5.401676654815674, 2.446958303451538, "[TT] Launch Configuration of the OSIRISv3 = Soft-stowed"]
-[9.263784408569336, 3.1124022006988525, "[FF] Objectives of the WISPR = 1. Understand the morphology, velocity, acceleration, and density of evolving solar wind structures when they are close to the Sun. 2. Derive the 3D structure of the solar corona through which in-situ measurements are made to determine the sources of the solar wind. 3. Determine the roles of turbulence, waves, and pressure-balanced structures in the solar wind. 4. Measure the physical properties of SEP (Solar Energetic Particle)-producing shocks and their CME drivers as they evolve in the corona and inner heliosphere."]
-[4.912399768829346, 3.3365840911865234, "[TT] Manufacturer of the FLLS = Neptec UK (NUK) and Neptec Design Group Canada (NDG)"]
-[5.661290645599365, 0.7728955149650574, "[FF] Calibration Date of the SSBUV = 1989 to 1993"]
-[6.39206600189209, 4.996322154998779, "[FF] Application of the CMT = Local Mapping"]
-[5.875492572784424, 5.429028511047363, "[TT] Software of the TIE = BASH"]
-[5.571465015411377, 2.1657683849334717, "[FF] Mission Status of the YES = Failure"]
-[9.747367858886719, 7.085927963256836, "[TT] Cross-Track Resolution of the MLS = 5 km"]
-[9.891210556030273, 2.679386854171753, "[TT] Angular Resolution of the HaloSat = 15\u00b0 or less"]
-[13.361342430114746, 2.8921332359313965, "[TT] Mass of the PRESat = ~4.5 kg"]
-[9.79886531829834, -0.6474454402923584, "[TT] Orbital Altitude of the QuickBird-2 = 450 km"]
-[9.4611177444458, 0.5652797818183899, "[TT] Operation Duration of the Schiaparelli = Few days"]
-[5.727548122406006, 5.286952495574951, "[FF] Real-time telemetry delivery of the UDP protocols = Yes"]
-[7.161346912384033, 4.530284404754639, "[TT] Accommodation Location of the Scientific Payload = North Radiator Panel"]
-[7.371591091156006, 4.147090435028076, "[FF] Sensor Complement of the MASCOT Sample Return Capsule = Unknown"]
-[11.756991386413574, 4.796540260314941, "[TT] Dimensions of the Research Facility = 26 inches high, 35 inches wide, 24 inches deep"]
-[4.725891590118408, 8.282291412353516, "[TT] Center Frequency of the GFO-RA = 13.5 GHz"]
-[8.808073997497559, 6.428892612457275, "[TT] Pulse Time Interval Measurement Precision of the SLA altimeter = ~ 5 ns"]
-[7.5804667472839355, 8.641314506530762, "[TT] Number of Bands of the Spectral bands = 8 (threshold), 12 (goal)"]
-[7.144134044647217, 3.78914737701416, "[FF] Formation Flying Navigation of the PROBA-3 = Design"]
-[4.205694198608398, 7.255509853363037, "[TT] Frequency Band of the TTC = S-band"]
-[6.781814098358154, 0.4095589220523834, "[TT] True Anomaly of the Satellite = Arbitrary"]
-[11.463382720947266, 5.802467346191406, "[TT] Structure of the Spacecraft = Aluminium honeycomb H-structure"]
-[9.525247573852539, 0.7994046807289124, "[TT] Current Position of the Solar Orbiter = Between the orbits of Venus and Mercury"]
-[6.899944305419922, 4.2649078369140625, "[FF] Flexibility of the TriG = Greater to accommodate future requirements"]
-[3.6764206886291504, 4.837900161743164, "[TT] Nominal Swath Width of the RADARSAT-1/2 = 100 km, 150 km, 170 km, 70 km, 50 km, 500 km, 300 km"]
-[4.891580581665039, 7.491153240203857, "[TT] OCTS Data Rate of the RF communications = 3.0 Mbit/s"]
-[10.110837936401367, 5.353275299072266, "[TT] Thermal Cooling System of the SES-17 = Two-phase mechanically pumped loop"]
-[6.279724597930908, 4.427471160888672, "[FF] Purpose of the End-to-End Simulator = Assess the performance of the mission/instrument configuration, retrieval algorithms, and influence of instrumental errors on the retrieval accuracies"]
-[5.639538764953613, 6.8054304122924805, "[TT] Data Volume of the SEIS Instrument = ~38 Mbit/day"]
-[6.914037704467773, 5.834812164306641, "[TT] Probability of the NSTT = 99.9%"]
-[8.553430557250977, 5.644323825836182, "[TT] Positioning Precision of the Galileo = 20 cm"]
-[7.456692695617676, 2.9291961193084717, "[TT] Spatial Resolution of the MethaneSAT = ~100 x 400 m"]
-[6.408300399780273, 1.8942646980285645, "[FF] URL of the ASNARO-1 = http://www.wmo-sat.info/oscar/satellites/view/467"]
-[8.019671440124512, 1.513156771659851, "[FF] Instrument Type of the SEIS = Seismic"]
-[11.742870330810547, 0.1269163340330124, "[TT] Mass of the TESS = Holds between three and 16 times Earth\u2019s mass"]
-[4.680768966674805, 7.334184169769287, "[TT] Data Transfer Frequency of the SSRNI = X-band at 8.2 GHz"]
-[6.579206943511963, 6.610589504241943, "[TT] Communication Method of the EDRS-C = Laser communication"]
-[6.457381725311279, 4.79533576965332, "[FF] Assembly Options of the HISat = Flexible assembly options resulting in multiple possible configurations"]
-[4.648576736450195, 6.512502670288086, "[TT] Bus Type of the Spacecraft = MMS (Multimission Modular Satellite), Fairchild RF communication"]
-[9.821470260620117, -0.6018689274787903, "[TT] Orbit Altitude of the ICESat-2 = Approximately 500 km"]
-[5.443384647369385, 7.093505382537842, "[TT] Data Transmission Speed of the Chang'e-2 = 12 Mbit/s"]
-[6.3104400634765625, -0.7478634119033813, "[FF] Spacewalk Duration of the UrtheCast Cameras = Six Hours"]
-[10.696505546569824, 3.939436674118042, "[FF] Intersatellite Communication System of the CanX-4&5 = Must relay position, velocity and attitude information"]
-[13.49744701385498, 5.851024627685547, "[TT] Power of the Solar arrays = 400 W (EOL)"]
-[5.990139484405518, 6.980489253997803, "[TT] GEO-to-ground Communication Link Speed of the Optical Ground Station = 2.8 Gbit/s"]
-[9.089946746826172, 3.100688934326172, "[FF] Objectives of the SEM-2 = 1. To determine the energy deposited by solar particles in the upper atmosphere 2. To provide a solar storm warning system"]
-[6.390894889831543, 5.390006065368652, "[FF] Interface of the MMFU = VCU (Video Compression Unit)"]
-[11.79654598236084, 4.814942359924316, "[TT] Tray Dimensions of the UniSat-3 = Octagonal plates of 150 mm side with an overall height of 250 mm"]
-[10.82187557220459, 3.013327121734619, "[TT] Cone Half-Angle of the O/OREOS nanosatellite = Less than 13o"]
-[6.71208381652832, 0.9071961045265198, "[TT] Observation Date of the Solar-B/Hinode spacecraft = February 6, 2018"]
-[6.682150840759277, 5.89541482925415, "[FF] Conference Date of the Quasi-optical multiplexer = July 22-27, 2012"]
-[9.171272277832031, 7.325572967529297, "[TT] Panchromatic Band Ground Resolution of the WorldView-3 = 31 cm"]
-[7.339989185333252, 4.680675506591797, "[FF] Mounting Location of the SPS head = In front of the instrument Tube, under the lid of the FDA (Front Door Assembly)"]
-[5.922757148742676, 1.077186942100525, "[FF] Mission Start Date of the Deep Space 1 = Unknown"]
-[6.774342060089111, -0.6620911955833435, "[TT] Orbital Period of the PROBA-3 = 19 hr 38 minutes"]
-[8.963178634643555, 0.6128374338150024, "[TT] Type of the Artemis-I = Non-EO"]
-[6.28108549118042, 8.109126091003418, "[FF] Not Applicable of the Channel Nr. = Not Applicable"]
-[7.785038471221924, 1.9821999073028564, "[FF] Function of the Phytoplankton = Absorbing atmospheric carbon dioxide into solution at the sea surface, using carbon dioxide to create their organic biomass via photosynthesis"]
-[12.13495922088623, 6.302099704742432, "[FF] Number of positrons collected of the PM = Expected to be a factor 2 to 6 greater to the SCM configuration"]
-[10.63744068145752, 8.881979942321777, "[TT] Pixel size of the Channel 1 = 32 km x 32 km"]
-[5.000735759735107, 3.4602067470550537, "[TT] Preamplifier Manufacturer of the SCM = 3D Plus"]
-[4.925153732299805, 8.318753242492676, "[TT] Radio frequency (GHz) of the SMMR = 6.6"]
-[4.61978006362915, 7.911366939544678, "[TT] Frequency Band of the RF communications = UHF (435 MHz)"]
-[9.685249328613281, 6.331632614135742, "[TT] Return Time of the Moving Mirror Alignment and Suspension Control System = 3 seconds"]
-[6.626265048980713, 4.949304103851318, "[FF] Performance of the GPSP = Same or better as on Jason-2"]
-[4.64265251159668, 7.967464923858643, "[TT] Frequency of the UHF = 435 MHz"]
-[7.879645824432373, 2.439565420150757, "[FF] Mission of the TEMPEST-D = Test new, low-cost technology for gathering weather data"]
-[4.713468074798584, 0.9172144532203674, "[TT] Qualification Date of the SUM = April 24-25, 2013"]
-[11.276700973510742, 5.950622081756592, "[TT] Material of the Antenna Assembly = Graphite epoxy"]
-[4.317417144775391, 3.1999783515930176, "[TT] TT&C stations of the GIOVE-A and GIOVE-B = Oxford (UK), Santiago (Chile), Kuala Lumpur (Malaysia), Fucino (Italy), Kiruna (Sweden)"]
-[5.210143566131592, 0.1230044960975647, "[TT] Operational Date of the Ikonos-2 = December 1999"]
-[5.807765007019043, -0.8582207560539246, "[TT] Design Lifetime of the Spacecraft = 5 years"]
-[4.386319637298584, 7.797727108001709, "[TT] Uplink Frequency of the RF communications system = 2.025-2.12 GHz"]
-[11.922947883605957, 5.409214496612549, "[TT] Instrument Size of the Hyperion = 39 cm x 75 cm x 66 cm"]
-[4.54530143737793, 5.735195636749268, "[FF] Purpose of the GomX-4B = Testing a micro-propulsion system, testing an inter-satellite radio link, carrying a hyperspectral imager"]
-[4.724491596221924, 8.396120071411133, "[TT] Center Frequency of the 7 = 59.4 GHz"]
-[3.926118850708008, 6.411129474639893, "[TT] Antenna Scan of the MSR = Oscillating 10\u00b0 either side of nadir"]
-[14.554801940917969, 6.591424942016602, "[TT] Battery Support for Nominal Operations of the RapidEye = After 2020"]
-[9.13763427734375, 5.6398162841796875, "[TT] Jitter of the SPARCS = 1\u03c3 ~6\" over 10 minutes"]
-[1.7522480487823486, 6.157698154449463, "[FF] Dark Matter Particles of the AMS-2 = Possibility of Arising from"]
-[7.599173069000244, -2.521131992340088, "[TT] Observation Date of the GOLD = 2 July 2019"]
-[9.691061973571777, 4.009688377380371, "[TT] Magnetic Field Tilt of the MGF = Up to 2\u00ba or 3\u00ba"]
-[7.183343410491943, -0.5239383578300476, "[TT] Rotation Period of the Pulsars = Every few milliseconds to seconds"]
-[14.196002006530762, 3.1832988262176514, "[TT] Mass of the COPS = 316 kg"]
-[8.244237899780273, 7.890365123748779, "[TT] Focal Planes of the Multispectral Imager = Two large visible near-infrared and shortwave infrared focal planes"]
-[8.859498023986816, 4.251476287841797, "[FF] Target of the Cal_doppler = Sun"]
-[5.589540481567383, 3.3101847171783447, "[FF] Integration, Testing, Launch Support and Space Vehicle Commissioning Services Provider of the Northrop Grumman = Airbus"]
-[8.94076919555664, 5.633907318115234, "[TT] Pointing Accuracy of the ADCS = \u22640.01\u00ba (3\u03c3, 3-axis)"]
-[5.635944843292236, 6.684018135070801, "[TT] Daily Volume of the LDCM = 400 scenes"]
-[8.445900917053223, 6.529919147491455, "[TT] Precision of the TOF = Around 120 ps"]
-[8.133767127990723, 2.52591609954834, "[FF] Function of the Multibeam Thermal Infrared Camera = Measure the height and motion of clouds"]
-[6.997689247131348, 7.101292610168457, "[TT] Power of the LISA Laser Prototype = 2 watts"]
-[10.159985542297363, 5.924654006958008, "[TT] Full-Aperture Reference Surface Temperature of the TIR Subsystem = 340 K"]
-[10.51672649383545, 2.7085635662078857, "[TT] Orbit Inclination of the CADRE nanosatellite = 51.6\u00ba"]
-[5.473289489746094, 6.295849800109863, "[TT] Size of the Mass Memory System = L: 302 x W: 345 x H: 240 mm"]
-[7.699248313903809, -2.5515332221984863, "[TT] Scanning Cadence of the GOLD = ~15 min"]
-[9.678546905517578, 3.969179391860962, "[TT] Magnetic Footprint Displacement of the MGF = Up to 5 km for every 100 km of altitude"]
-[14.033090591430664, 7.104702472686768, "[TT] Output Voltages of the EPS = 8.4 V, 5 V, 3.3 V"]
-[8.655410766601562, 3.6875970363616943, "[FF] Measurement of the ACRIM = Total Solar Irradiance"]
-[4.995365142822266, 3.7355618476867676, "[TT] Manufacturer of the LF Receiver = Sierra Lobo Inc."]
-[10.015589714050293, 2.9928884506225586, "[FF] Orbit of the CuPID CubeSat Observatory = Modeled"]
-[10.428163528442383, 2.324354887008667, "[TT] X-ray Spectrum of the AXP = Extends up to energies of at least 150 keV"]
-[9.01239013671875, 8.558829307556152, "[FF] Strehl Ratio of the Optical Telescope = < 0.5 at wavelength of 450 nm"]
-[7.971014499664307, 3.3138556480407715, "[FF] Operation of the ISUAL = Alternately in eclipsed and sunlight times"]
-[10.755621910095215, 0.9415557384490967, "[TT] Size of the KELT-11b = About 30% larger in size than Jupiter"]
-[9.265631675720215, 5.089664936065674, "[TT] Sun Angle of the Legion Constellation = Above 15\u00ba"]
-[4.479572296142578, 2.7115368843078613, "[TT] Location of the XAS = Hsinchu, Taiwan"]
-[9.72933292388916, 7.519103527069092, "[TT] Cross-track Swath of the Nadir total column spectrometer = 50 km x 2800 km"]
-[5.2486772537231445, 0.6736115217208862, "[TT] Status of the CanX-6/NTS = Retired, R&D"]
-[8.110612869262695, 2.227614164352417, "[FF] Instrument Function of the SMMR = Provide necessary corrections for the SeaSat altimeter and scatterometer measurements"]
-[3.710799217224121, 6.655487060546875, "[TT] Beamwidth of the Antenna = 2.7\u00ba"]
-[7.853443622589111, 7.802104473114014, "[TT] Sensitivity of the HSC-III = 350 \u00b5rad/mV"]
-[6.174829006195068, 5.344888687133789, "[FF] Type of the First FPGA = GNSS receiver core functions"]
-[8.776012420654297, 5.084931373596191, "[FF] Mission Objective of the OICETS = Conduct on-orbit demonstrations of high-accuracy pointing, acquisition and tracking technologies"]
-[9.867475509643555, 8.25728702545166, "[FF] Page Numbers of the Coded aperture correlation holography system = F67-F77"]
-[7.310632228851318, 6.152511119842529, "[TT] Timing Accuracy of the BOSS = 1 ms"]
-[9.528336524963379, 0.8674531579017639, "[TT] Distance from the Sun of the New Horizons = Almost 5 billion miles (7.5 billion kilometers)"]
-[7.738407135009766, 7.5857696533203125, "[TT] Output Resolution of the Detector = 12 bits"]
-[7.981700420379639, 0.1239684671163559, "[FF] Purpose of the GRACE = Measure gravity and show how mass is distributed around the planet"]
-[8.154240608215332, 2.553852081298828, "[FF] Objective of the BIRD = Observe thermal processes on the Earth\u2019s surface"]
-[4.508406162261963, -0.8907790780067444, "[TT] Splashdown Date of the Dragon cargo spacecraft = April 7, 2020"]
-[6.430878639221191, 7.995853424072266, "[TT] Channels of the GOES Sounder = 19"]
-[5.747989177703857, 4.356562614440918, "[FF] IOV Activities of the LCT = LCT self-test, IOV with an OGS Optical Ground Station, IOV with LEO user satellite"]
-[14.27554702758789, 3.243081569671631, "[TT] Mass of the EPDP = 2.3 kg"]
-[10.218482971191406, 5.464747905731201, "[FF] Performance of the ABI Cooler System = Unknown"]
-[5.191904067993164, -1.225459337234497, "[FF] Launch Date of the Kondor-E1 = January 1, 2020"]
-[10.397847175598145, 2.1378464698791504, "[TT] On-axis Resolution of the eROSITA X-ray telescope = 15 arc seconds HEW"]
-[7.999216079711914, 8.831390380859375, "[TT] Spectral Range of the 1.61 and 2.06 \u00b5m CO2 channel = 1.594 to 1.619 \u00b5m and 2.042 to 2.082 \u00b5m"]
-[6.642167091369629, 1.7288017272949219, "[FF] Overview URL of the Orbital ATK CRS-4 = http://www.nasa.gov/sites/default/files/atoms/files/orbital_atk_crs-4_mission_overview-2.pdf"]
-[9.96026611328125, -1.531659722328186, "[TT] Orbit Inclination of the ABEX = 27\u00ba"]
-[5.314291954040527, 0.6666809320449829, "[FF] Release Date of the ITRF2014 = 18 July 2016"]
-[11.817155838012695, 6.751832008361816, "[TT] Ion energy of the Microdosimeter B = > 50 keV"]
-[9.483146667480469, 3.9226956367492676, "[FF] Type of the Magnetometers = Unknown"]
-[5.4830145835876465, 7.360712051391602, "[FF] Bandwidth of the ODTML = Higher than Argos DCS"]
-[9.175868034362793, 7.484655380249023, "[TT] Multispectral Resolution of the EROS-C = 2.8 m GSD"]
-[8.454734802246094, 6.2492570877075195, "[TT] Data Transmission Rate of the Coarse Lateral Sensor = 10 Hz"]
-[14.765301704406738, 6.730789661407471, "[TT] Quantity of the NiH2 Batteries = 5"]
-[3.248141288757324, 5.087480545043945, "[TT] Spotlight High Resolution (HS) Spectral Resolution of the TSX-SAR = 1m"]
-[5.631503582000732, 1.5553120374679565, "[TT] Path of the ALOS-2 = 135"]
-[7.822641849517822, 6.969826698303223, "[FF] Interface of the ROE = 3 CCDs"]
-[8.84208869934082, 7.5121660232543945, "[TT] Detector Separation of the Detector = Less than 12.06 mm"]
-[4.1911115646362305, 6.680783271789551, "[TT] UHF-VHF transceiver of the SMDC-ONE = Custom"]
-[8.540667533874512, 1.7557551860809326, "[TT] Range of Values of the Cloud water = 0 - 1"]
-[6.728384494781494, -0.3485252559185028, "[TT] Traditional Delivery Time of the Polar Satellite Data = 2 to 6 hours after the time of measurement"]
-[6.669432163238525, 1.756622552871704, "[FF] URL of the ExoplanetSat = https://dspace.mit.edu/handle/1721.1/61644"]
-[9.205306053161621, 7.0507917404174805, "[TT] Resolution of the SHIROP = High"]
-[10.424738883972168, 2.3378679752349854, "[FF] XNAV Type of the SEXTANT = X-ray Pulsar-based Navigation"]
-[7.125911235809326, 7.085928440093994, "[FF] Optical Cavity Layout of the GEDI Laser = 22 bounce slab and a GRM"]
-[8.313362121582031, 7.583356857299805, "[TT] CCD Detectors of the COR1 = EEV 42-40, 2k x 2K, 13.5 \u03bcm pixels, backside illuminated, AR coated (except EUVI), >100 k e -  full well"]
-[12.086654663085938, 7.633492946624756, "[TT] Mass of the CCD Camera = <55 kg"]
-[7.465245723724365, 2.951735734939575, "[TT] Swath Width of the MethaneSAT = 1990 pixels"]
-[8.15578842163086, 6.048856735229492, "[TT] Sensor Type of the SSAS = Spin-type"]
-[8.021924018859863, 6.204465389251709, "[FF] Type of the LAICA = Lyman Alpha Imaging Camera"]
-[9.037093162536621, 5.215722560882568, "[TT] Components of the IRU (Inertial Reference Unit) = 4 gyros, 2 processing units, 2 power supplies"]
-[10.36264705657959, 2.1235811710357666, "[TT] Observation Date of the eROSITA X-ray telescope = 17 and 18 October 2019"]
-[7.143213272094727, 3.7937967777252197, "[FF] Purpose of the RemoveDebris = Performing key ADR demonstrations"]
-[8.985265731811523, 0.46298035979270935, "[TT] Size of the New Boulders = 30 cm to 3 m"]
-[12.131790161132812, 1.979609489440918, "[TT] Status of the CartoSat-2B = Operational"]
-[6.878195762634277, 5.943558216094971, "[TT] Quantity of the ADELIS-SAMSON = 3"]
-[14.232499122619629, 3.139131784439087, "[TT] Mass of the CEASE = 1 kg"]
-[6.823023319244385, 5.083326816558838, "[FF] Function of the PIU = Provides the power supply for the FEE and SiPMs"]
-[8.703740119934082, 7.73738431930542, "[TT] Detector Size of the SIS = 16 pixels in along-track and 160 pixels in the cross-track direction"]
-[14.263385772705078, 6.794930458068848, "[TT] Battery Charge Current of the SBVR = Up to 40 A"]
-[4.782835006713867, 0.38173335790634155, "[TT] Powering Up Start Date of the Prichal = October 11"]
-[8.200246810913086, 8.407243728637695, "[TT] Resolution of the SSULI = 1.5 nm"]
-[6.190698623657227, 2.567763566970825, "[FF] Consortium of the P3RVX = DEIMOS, Technical University of Denmark (DTU), University Politehnica of Bucharest/Institute of Space Sciences (UPB/ISS)"]
-[9.91616439819336, -0.09709510952234268, "[TT] Altitude at Launch of the GRACE Satellite = 485 km"]
-[4.12109375, 6.226650238037109, "[FF] Effects Modeled of the GRASP (Geodetic Reference Antenna in Space) = FOV changes as the antenna rotates, reflector and boom thermal distortions, dynamic distortions from spacecraft"]
-[11.697593688964844, 7.470895767211914, "[FF] Global Observation Frequency of the TOMS = Daily"]
-[13.352069854736328, 7.836316108703613, "[TT] X-band Tx Power of the RF communications = 6 W"]
-[6.537807464599609, 6.94942569732666, "[TT] Repeater Mode Data Rate of the LaserCom = 270 - 1000 Mbit/s"]
-[14.033282279968262, 4.000305652618408, "[TT] Instrument Mass of the SBVR = 54.5 kg"]
-[6.596210479736328, 4.172248363494873, "[FF] Ground Segment of the QuakeSat = Unknown"]
-[5.49704647064209, 3.0177345275878906, "[TT] Responsible Agency of the DWSS = DoD"]
-[6.559176921844482, 6.950517177581787, "[TT] Duty Cycle of the DORIS = 100%"]
-[5.0858283042907715, 8.358609199523926, "[TT] Bandwidth of the GAMALINK = 40 MHz"]
-[5.467625141143799, 6.359376430511475, "[TT] Capacity of the MMU = 16 Gbit"]
-[7.989846706390381, 8.622004508972168, "[TT] Spectral Range of the SIM = 0.2~50 \u00b5m"]
-[5.922524452209473, -0.4665459990501404, "[TT] Mission Duration of the FY-4 = 7 years"]
-[7.092803001403809, 2.8641719818115234, "[TT] Mission Operations Management of the MethaneSAT = Rocket Lab"]
-[4.63523006439209, 6.714249134063721, "[FF] Data Transmission of the X-band ground TT&C station = X-band deep space transponder"]
-[6.176207542419434, 3.713263511657715, "[FF] Operation of the DMC Constellation = Independently owned and operated by one nation or organization"]
-[4.82305908203125, -1.847311019897461, "[TT] Earth-to-Moon Cruise Time of the Chang'e-2 = 5 days"]
-[12.125601768493652, 3.4730796813964844, "[FF] Maximum Fuel Budget of the RVX = Unknown"]
-[9.173232078552246, 1.3202226161956787, "[TT] Launch Date of the New Horizons = January 19, 2006"]
-[7.468361854553223, 2.9751040935516357, "[TT] Observing Swath of the MethaneSAT = About 200 km"]
-[9.100835800170898, -1.2227966785430908, "[FF] Release of the HPA = Not until a geostationary transfer orbit is attained"]
-[6.026889801025391, 5.762725353240967, "[TT] Model of the Second FPGA = Virtex 4"]
-[4.778464317321777, 0.4711464047431946, "[TT] Launch Date of the MEV-1 = October 2019"]
-[3.7071080207824707, 6.317706108093262, "[TT] Design Location of the Printed Antenna Aperture = ISRO"]
-[3.5236384868621826, 1.762485146522522, "[FF] Conference Location of the Sentinel-3 = Oslo, Norway"]
-[7.59636116027832, 6.8654561042785645, "[TT] Large Window Time Resolution of the CCD = 0.6 seconds"]
-[8.480680465698242, 7.630037307739258, "[TT] Detector Array of the POLDER = 2-D"]
-[9.41623592376709, 3.7981245517730713, "[FF] Function of the MAG = Measure magnetic fields"]
-[9.787734031677246, 2.3338429927825928, "[FF] Image Detail of the NuSTAR = High"]
-[11.870606422424316, 3.284952163696289, "[TT] Thruster Type of the GPIM = Aerojet Rocketdyne GR-1 1-N class"]
-[4.752793788909912, 0.5960695147514343, "[TT] Launch Date of the MetOp-B = Sept. 17, 2012"]
-[3.3333959579467773, 5.0899810791015625, "[TT] Imaging Modes of the SAR instrument = Co- and cross-polarization"]
-[14.114527702331543, 7.219200611114502, "[TT] Main Bus Voltage of the MRU = 28 V"]
-[7.917531490325928, 9.153473854064941, "[TT] Wavelength of the MC-U = 762 nm for sprite and 777 nm for lightning"]
-[8.339399337768555, 4.511279106140137, "[TT] Calibration Method of the XGRE = LED sources"]
-[6.144638538360596, 2.2692294120788574, "[TT] Principal Investigator of the Juno = Scott Bolton"]
-[6.622713565826416, 6.872058391571045, "[TT] Downlink Speed of the Compact Laser Comms Terminals (CLCT) = Up to 10 Gbit/s"]
-[5.398379325866699, 5.525728702545166, "[FF] Technology Options of the ORS Communication Bus = Firewire, SpaceWire, and Ethernet"]
-[10.139718055725098, -1.3890058994293213, "[TT] Off-nadir Angle of the Cartosat-2E = Up to 45\u00b0"]
-[7.900090217590332, 7.215584754943848, "[TT] Spectral Resolution of the FTS Interferometer = <0.028, 0.056, 0.11, 0.55 cm -1"]
-[5.9686102867126465, 0.9813234210014343, "[FF] Development Date of the Compact Infrared Camera (CIRC) = Oct. 4-8, 2010"]
-[5.957045555114746, 1.5704699754714966, "[FF] URL of the IBEX = http://www.swri.org"]
-[6.436145305633545, 3.183737277984619, "[FF] Delivery Time of the BlackSky Gen-2 satellites = 90-minute average delivery times"]
-[8.548432350158691, 2.1843185424804688, "[FF] Geolocation and Pointing Accuracy of the WindSat = Not provided"]
-[6.279245376586914, 0.2058243602514267, "[TT] On-Orbit Operations of the FormoSat-2 = Over 11 years"]
-[4.917855739593506, 7.246246814727783, "[TT] Max Data of the S-band Transmitter = 2 MB/day"]
-[10.282423973083496, 4.398259162902832, "[FF] Attitude Control of the QuickBird-2 = Low-vibration reaction wheels, three torque rods, and four hydrazine thrusters"]
-[13.813932418823242, 5.664823055267334, "[FF] Efficiency of the XTJ Prime solar cells = Not specified"]
-[5.917668342590332, 3.0269765853881836, "[TT] Annualized cost to collect 10 6  km 2 /day of the Legion = < $10 million"]
-[8.761367797851562, -0.15844228863716125, "[FF] Elliptical Lunar Orbit of the Chang'e-2 = 100 km x 15 km (apoapsis x periapsis)"]
-[8.161722183227539, 1.6768434047698975, "[TT] Spatial Resolution (km) of the Land surface temperature = 25"]
-[12.074931144714355, 3.78432559967041, "[TT] Gas Pressure of the Detector = 1.0 bar absolute"]
-[5.242620468139648, 1.2744389772415161, "[FF] Conference Presentation Date of the THEMIS = Aug. 14-17, 2006"]
-[7.152170181274414, 1.935913324356079, "[TT] Coverage of the MEOSAR = Large portion of Earth's surface"]
-[5.374634742736816, 2.410789966583252, "[TT] Grappling Astronaut of the SpaceX CRS-17 = David Saint-Jacques"]
-[10.629839897155762, 0.9333577156066895, "[TT] Diameter of the Kepler-438b = Less than 1.5 times the diameter of Earth"]
-[6.959610939025879, 4.4846296310424805, "[FF] Function of the Exo-Brake = Enable Safe Return for Small Spacecraft"]
-[8.331476211547852, 5.379354476928711, "[TT] Spectrometric Calibration Accuracy of the TanSat = Absolute accuracy of 5%, and a relative accuracy of 3%"]
-[5.537652969360352, 5.84904146194458, "[TT] Processor of the OBC = transputer T805 @ 20 MHz"]
-[7.8904128074646, 7.544158935546875, "[TT] Transmit Frequency (MHz) of the Imager data = 1677.0"]
-[6.61302375793457, 8.113192558288574, "[TT] Cross-Polar Operation of the Instrument = Available"]
-[5.297043800354004, 3.848294258117676, "[TT] Number of Satellite Pairs of the MetOp-SG = 3"]
-[7.68080472946167, 2.9628288745880127, "[FF] Purpose of the GOSAT-GW = Monitor greenhouse gases in the atmosphere and improve understanding of the water cycle"]
-[4.868236064910889, 4.240450859069824, "[FF] Ground Station Transmission of the CanX-7 = Next Access"]
-[6.479626178741455, 1.0982723236083984, "[FF] Image of the Day Date of the NASA Earth Observatory = 21 May 2022"]
-[10.453886985778809, 5.784172534942627, "[TT] Temperature Range of the GOES-T = -67\u00ba Fahrenheit to 188\u00ba Fahrenheit"]
-[6.3805832862854, 0.46062710881233215, "[TT] Profiles Per Day Goal of the FormoSat-7 / COSMIC-2 mission = 10,000"]
-[4.700925827026367, 8.383596420288086, "[TT] Center Frequency of the 6 = 57.29 GHz"]
-[10.141769409179688, 5.976543426513672, "[TT] Operating Temperature of the Mid-infrared detectors = 7 K"]
-[5.515880584716797, 3.094339609146118, "[TT] Manufacturer of the Deep Space Atomic Clock = NASA Jet Propulsion Laboratory"]
-[5.515870094299316, 6.826879501342773, "[TT] Data Volume of the SSM/T-1 = 1.5 MByte per satellite"]
-[10.561689376831055, 6.530837535858154, "[TT] Mirror Modules of the ART-XC = 7"]
-[5.629771709442139, 5.737837791442871, "[TT] Blade Servers Cores of the GS (Ground System) = 3,632"]
-[7.9913835525512695, 0.8321183323860168, "[FF] Data Usage of the GRACE-FO = Track drought across the United States"]
-[7.9861345291137695, 7.248440265655518, "[FF] Input and Output of the CCD (Charge-Coupled Device) = LVDS (Low Voltage Differential Signaling)"]
-[3.785541534423828, 2.39691424369812, "[TT] Design Life of the Iridium NEXT bus platform = 12.5 years"]
-[5.148074150085449, 3.1212351322174072, "[TT] Patented By of the iMESA = USAFA"]
-[10.461941719055176, 2.382047414779663, "[TT] Calibration Facility of the X123 X-ray Spectrometer = SURF (Synchrotron Ultraviolet Radiation Facility) of NIST (National Institute of Standards and Technology)"]
-[13.424688339233398, 7.733359336853027, "[TT] Output Power of the XBT = 10.5 W"]
-[7.271750450134277, 3.385707139968872, "[FF] Inputs of the SCOPE = ABI sensor data from GOES-R satellites, ambient temperature, relative humidity at the ground"]
-[6.300903797149658, 5.081157207489014, "[FF] Interface Type of the X50 platform = Directly interface with the launch box via braces"]
-[6.049582004547119, 1.7575180530548096, "[FF] URL of the MEIDEX = http://irc-iamas.org/files/MEIDEX.doc"]
-[9.869180679321289, 4.2791337966918945, "[FF] Magnetorquers of the NEMO-AM = Quantity: 3, Manufacturer: SFL, Current-Controlled up to 100 mA"]
-[4.513340473175049, 3.823425054550171, "[TT] Number of orbital planes of the GALILEO = 3"]
-[8.505170822143555, 7.1289520263671875, "[TT] Camera Type of the CASPR = 8U binocular camera"]
-[6.161627769470215, 7.045527458190918, "[FF] Data of the Potential Instrument = Included in TT&C data"]
-[10.364349365234375, 1.8401601314544678, "[TT] Function of the NuSTAR = Seeing through the gas and dust around black holes"]
-[5.349216461181641, 6.538521766662598, "[TT] Data Storage Capacity of the ICESat-2 = 580 Gbits/day"]
-[8.10488510131836, 8.982828140258789, "[TT] Wavelength Range (VIS) of the Sentinel-4/UVN = 400-500 nm"]
-[8.5413179397583, 3.6677169799804688, "[FF] Tracking of the TSIS TPS = The sun each orbit with a two-axis gimbal"]
-[13.961663246154785, 7.168604373931885, "[TT] Voltage of the MTM main power bus = 100 V"]
-[8.263171195983887, 6.691588401794434, "[FF] Medical Capabilities of the Butterfly IQ Ultrasound = Provided to crews on long-term spaceflights where immediate ground support is not an option"]
-[7.366943836212158, 4.125192165374756, "[FF] Frequency of the ASASSN-14ko = Most predictable and frequent recurring"]
-[6.116288185119629, 0.20392420887947083, "[TT] Daily Reset of the Dellingr = Part of daily operations"]
-[4.882012367248535, 1.0105268955230713, "[TT] CDR Date of the SMOS = Nov. 2005"]
-[6.251537799835205, 2.358325242996216, "[TT] Purpose of the MPCV = Crewed missions to the Moon, asteroids and Mars"]
-[5.053164482116699, 4.531896114349365, "[TT] Radio Systems of the CanX-2 = SFL-designed"]
-[14.075560569763184, 4.035837650299072, "[TT] Instrument Mass of the Instrument = 177 kg"]
-[8.002720832824707, 2.1976511478424072, "[FF] Objective of the MSU-MR = Global and regional cloud cover mapping, SST (Sea Surface Temperature), and LST (Land Surface Temperature)"]
-[6.143313407897949, -0.20554675161838531, "[FF] Mission Duration of the FORMOSAT = Not specified"]
-[7.056534290313721, 3.768019914627075, "[FF] Formation of the Formation Flying = A-train (Aqua in the lead and Aura at the tail)"]
-[10.13398551940918, -1.5944136381149292, "[TT] Orbit Inclination of the HY-1C = 98.6\u00ba"]
-[6.184900283813477, 2.2509610652923584, "[TT] Principal Investigator of the ECOSTRESS = Simon J. Hook"]
-[9.692699432373047, 4.20781946182251, "[TT] Number of Magnetometers of the FIELDS suite = 3"]
-[9.053067207336426, -1.3652676343917847, "[TT] Orbit Type of the GEMS = Geostationary orbit over equator"]
-[6.360941410064697, 4.5541558265686035, "[FF] Components of the NLS-2 = QuakeSat"]
-[8.565834045410156, 4.548820495605469, "[FF] Objective of the ASTERIA = Demonstrate new technologies for studying nearby stars"]
-[7.394670486450195, 3.1960346698760986, "[FF] Altimeter of the Envisat = Yes"]
-[3.61376690864563, 4.732835292816162, "[TT] Imaging Modes of the RADARSAT-2 = 15 Stripmap modes, 4 ScanSAR modes, and a Spotlight mode"]
-[9.657950401306152, 4.024356842041016, "[TT] Vector Components Stability of the Magnetic Field = Better than 1 nT/year"]
-[8.851919174194336, 0.9823806881904602, "[TT] Lead Author of the Parker Solar Probe = Justin Kasper"]
-[7.535633087158203, 1.8665661811828613, "[FF] Impact of the Argo = Change our understanding of the world's oceans, opening in fact a new era of oceanography"]
-[7.7202677726745605, 2.7122445106506348, "[FF] Primary Purpose of the Kanopus-V-IK = Detecting sources of fire"]
-[7.098094463348389, -0.15330958366394043, "[TT] Number of Independent Systems of the Precision Orbit = 3"]
-[11.990516662597656, 5.011950969696045, "[TT] Size of the PLC = 285 mm x 235 mm x 165 mm"]
-[4.347807884216309, 3.1220178604125977, "[FF] Ground Station of the LCT = ESA\u2019s OGS on Tenerife Island (Spain), DLR\u2019s mobile OGS"]
-[8.407560348510742, 7.568418979644775, "[TT] Conversion Factor of the Photodetector = ~16 r (3\u03bb)-1"]
-[4.968665599822998, 3.3096084594726562, "[TT] Data Management Center of the VIRR = GSFC"]
-[7.060635566711426, 8.183661460876465, "[TT] SNR (Signal to Noise Ratio) of the Instrument = 6"]
-[6.49381160736084, 7.592269420623779, "[TT] Parameter of the A/D quantization = 12 bit"]
-[4.546280860900879, 5.859544277191162, "[TT] Quantity in Use of the 406 MHz Beacons = About 350,000"]
-[10.739505767822266, 3.1707603931427, "[TT] Attitude System of the Microsatellite = \u00b110\u00ba"]
-[7.531087875366211, 8.681507110595703, "[TT] Bands of the AEISS = 5"]
-[7.933547496795654, 9.172935485839844, "[TT] Operating Wavelength of the IRS = Millimeter"]
-[13.385462760925293, 7.580205917358398, "[TT] Peak RF Power of the T/R module = 10 W"]
-[6.422855854034424, 1.895912528038025, "[FF] URL of the ROSE-L = https://www.airbus.com/en/newsroom/press-releases/2020-12-airbus-to-deliver-radar-instrument-for-new-copernicus-rose-l"]
-[4.624998092651367, 7.03578519821167, "[TT] X-band of the Downlink communications = 800 Mbit/s (16 QAM), 400/200 Mbit/s (QPSK)"]
-[4.589875221252441, 6.241879463195801, "[TT] Communication Function of the APAA = SS-TDMA (Satellite Switched Time Division Multiple Access)"]
-[8.810172080993652, 3.327359199523926, "[FF] Mission of the Patch Antenna = Maintain an artificial eclipse of the Sun"]
-[7.434247970581055, 5.305765628814697, "[FF] Components of the COB = Optics, detector, radiator, FDA (Front Door Assembly), FWA (Filter Wheel Assembly), SHM (Shutter Mechanism)"]
-[3.617223024368286, 6.281195640563965, "[TT] Quantity of the ESA\u2019s three 35 m dish antennas = 3"]
-[6.841052055358887, 0.9299988150596619, "[FF] Mission Date of the Solar Probe Plus = Sept. 27-Oct. 1, 2010"]
-[7.649569034576416, 9.228135108947754, "[TT] Wavelength Range of the Band 6 = 2.225-2.275 \u00b5m"]
-[9.935140609741211, -0.3491595983505249, "[TT] Altitude of the Satellites = 35,786 km"]
-[8.431694984436035, 6.770323753356934, "[TT] Observation Method of the NTSIC = Pushbroom"]
-[10.573343276977539, 5.693042755126953, "[TT] Maximum Temperature of the Heat Shield = 2200\u00ba C"]
-[9.163544654846191, 7.261631488800049, "[TT] Altitude Range of the Detector = Limited to 30 km"]
-[13.287467002868652, 7.406229019165039, "[TT] Power of the NSCAT = 240 W"]
-[4.8384108543396, -0.9776433706283569, "[TT] Launch Date of the Fengyun 4B = 6 June 2021"]
-[9.178004264831543, 2.853888511657715, "[FF] Flare Intensity of the Solar Dynamics Observatory = X1"]
-[3.256319761276245, 1.5419251918792725, "[TT] Planned Overlap of the Sentinel-6 = At least 6 months"]
-[13.376821517944336, 7.380730628967285, "[TT] Peak Power of the TRMs = >150W"]
-[3.4368503093719482, 6.4282402992248535, "[TT] Size of the 2.5 m dish antenna = 2.5 m"]
-[7.838738918304443, 3.177769899368286, "[TT] Operation of the ISUAL = Nighttime (eclipse period)"]
-[6.528352737426758, 0.0646209642291069, "[FF] Observation Period of the BRITE satellites = Hours to Months"]
-[10.000550270080566, 1.365781307220459, "[TT] Frequency of the Supernovae = Happen every 100 years or so"]
-[8.569430351257324, 2.2192909717559814, "[TT] Accuracy of Wind Velocity (Troposphere) of the Aeolus = 2-3 m/s"]
-[6.7840070724487305, 2.2758359909057617, "[FF] URL of the Appliqu\u00e9 Sensor Interface Module = http://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=1494&context=smallsat"]
-[5.749277114868164, 5.092550754547119, "[FF] Optional Data Protection Mechanism of the SCPS = Assure end-to-end security and integrity of message exchange"]
-[12.721549034118652, 3.896312952041626, "[FF] Evidence of the Ion Dispersion = A single steady ion dispersion in the cusp may be evidence for a single steady reconnecting separator at the dayside magnetopause"]
-[8.919270515441895, 6.637991905212402, "[FF] Objective of the CAVIS = Monitor the atmosphere and provide correction data to improve WorldView-3's high-resolution imagery"]
-[10.078580856323242, 1.9109941720962524, "[FF] Planned Landing of the Chandrayaan-3 = 2020"]
-[7.741516590118408, 4.423804759979248, "[FF] Observation Data of the AMSR2 = SHIZUKU"]
-[5.491494178771973, 0.26842400431632996, "[TT] Launch Date of the COMPASS-1 = Dec. 10, 2001"]
-[8.849459648132324, -0.9288085699081421, "[TT] Orbit Type of the LAGEOS = MEO (Mean Earth Orbit)"]
-[5.456075668334961, 4.298687934875488, "[TT] Quad-stack of the Satellite Bus = True"]
-[3.0140223503112793, 4.727938652038574, "[TT] DASS POC Band of the GISAR = 2226.42 \u2013 2226.52 MHz"]
-[7.970449447631836, -2.583913803100586, "[TT] Band Wavelength of the GOLD = 135.6 nm"]
-[4.895359992980957, 3.329822301864624, "[FF] Manufacturer of the Gaia spacecraft = EADS Astrium"]
-[8.528253555297852, 1.3353321552276611, "[FF] Sea Surface Salinity Monitor of the Aquarius = Global monitoring"]
-[6.762984752655029, -0.46187669038772583, "[TT] Total Cruise Phase Duration of the Solar Orbiter = < 3 years"]
-[9.410808563232422, 2.304257392883301, "[TT] Total of the Blue Jets = 4239"]
-[7.079219818115234, 8.418498039245605, "[TT] Nominal SNR of the Band 3 = 1170"]
-[3.8328096866607666, -1.0956956148147583, "[TT] Orbit Type of the LARES-2 = Circular MEO"]
-[7.365891933441162, 8.809285163879395, "[TT] Number of Narrow-Band Filters of the MEIDEX = 6"]
-[7.81279993057251, 5.677473545074463, "[FF] Changes of the iMESA-R Flights = New electrostatic analyzer (ESA) design, Improved temperature measurements, Reduces number of plates, Switchable range on ESA, Programmable gain amplifier, Higher transimpedance amplifier gain, New power supply design, Added dosimeter, Rewritten software"]
-[4.585885524749756, 6.785609722137451, "[FF] S-band Downlink of the Spacecraft = Completed"]
-[8.11005687713623, -1.2364997863769531, "[FF] Instrument Optimization Procedures of the ICESat-2 = Ensure the laser is pointing at the precisely correct angle and lasing at the precisely correct wavelength"]
-[6.731581211090088, 1.0949366092681885, "[FF] Arrival Date of the Mercury Magnetosphere Orbiter = May 12, 2015"]
-[7.878450870513916, 6.7956390380859375, "[TT] Repetition Cycle of the WiFS camera = 5 days"]
-[2.954503297805786, 4.462240695953369, "[TT] Ground Resolution (Mosaic mode) of the XSAR = 1.8 m"]
-[6.159786224365234, 3.0251572132110596, "[TT] Image Quality of the WorldView Legion sensor = High"]
-[8.440042495727539, 7.401356220245361, "[TT] Array Configuration of the Cameras = 1 x 4"]
-[4.675240993499756, 6.227381706237793, "[FF] Operation Modes of the BSC = APAA health confirmation mode, fixed beam direction mode"]
-[10.046159744262695, 1.34074068069458, "[TT] Observable Time of the Hoinga supernova remnant = About 100,000 years"]
-[8.183453559875488, 1.139757513999939, "[FF] Workshop Date of the Soil Moisture Active and Passive Mission (SMAP) = Nov. 18-20, 2009"]
-[5.138644695281982, 8.173722267150879, "[FF] Affiliation of the IMM = LPC2E (Laboratoire de Physique et de Chimie de l'Environnement, Orleans) of CNRS, France and the Stanford Very Low Frequency (VLF) Group, Stanford University, Stanford, CA, USA"]
-[7.029303550720215, 3.451655864715576, "[FF] URL of Presentation of the PROBA-3 = http://www.sffmt2013.org/PPAbstract/4056pr.pdf"]
-[14.284796714782715, 3.2860422134399414, "[TT] Mass of the IMS-1 = 83 kg"]
-[4.633161544799805, 0.6166939735412598, "[TT] Launch Date of the GOES-R = Nov. 4"]
-[6.578620910644531, -0.3775627017021179, "[TT] Repeat Cycle of the TecSAR = 36 days"]
-[7.484812259674072, 2.5515341758728027, "[TT] Measurement Category of the SkySat Constellation = Multi-purpose imagery (ocean), Multi-purpose imagery (land)"]
-[12.081775665283203, 4.555578708648682, "[TT] Spacecraft Size of the QSat = 492 mm x 503 mm x 502 mm"]
-[7.93763542175293, 5.94490909576416, "[FF] Purpose of the IMAX camera = Filming during four increments"]
-[7.824886322021484, 8.991703033447266, "[TT] Wavelengths of the OLI-2 = Nine"]
-[8.127601623535156, 6.64233922958374, "[FF] Image Location of the ABI = Provided in Table 9"]
-[7.587985992431641, 6.6106696128845215, "[FF] Export Formats of the OpenMCT = PNG, JPEG, CSV, JSON, tab-delimited"]
-[10.117313385009766, 3.0089263916015625, "[FF] AI Integration of the PhiSat-1 = AI chip including the first AI algorithms for cloud screening"]
-[12.423968315124512, 3.1912786960601807, "[TT] Propulsion System Fuel Capacity of the EAGLE ESPAStar = Up to 310 kg"]
-[4.925103187561035, -0.8778629302978516, "[TT] Deorbit Burn Duration of the Dragon = Up to 10 minutes"]
-[8.620320320129395, 4.711114406585693, "[TT] Catalog of the Star Tracker = 3746 stars"]
-[8.003972053527832, 9.09544849395752, "[TT] Wavelengths Monitored of the TOMS = 312, 317.5, 331.3, 339.9, 360.0 and 380 nm"]
-[9.752297401428223, -0.2590519189834595, "[TT] Altitude at Final Breakup of the S/C = Little more than 100 km"]
-[8.131819725036621, 6.630153179168701, "[TT] Manufacturer of the MWIR Imager = Leonardo"]
-[5.127133369445801, 6.825444221496582, "[TT] LISS-2A/B Data Downlink Transfer Rate of the Satellite = 10.4 Mbit/s"]
-[4.773488521575928, 6.392850875854492, "[FF] Data Reception of the X-band ground stations = Other data continues to be received"]
-[5.033729553222656, 3.193519353866577, "[TT] Manufacturer of the SkySat = Terra Bella"]
-[10.931154251098633, 4.013027191162109, "[FF] Operation Principle of the EMP (Electromagnetic Pump) = Utilizes the Lorentz body force to propel the electrically conductive fluid inside the toroidal channel"]
-[6.350795269012451, 0.7984640598297119, "[FF] Data Release 3 and Data Release 4 of the Gaia = In production"]
-[11.05844783782959, 0.5334581732749939, "[FF] Number of Planets of the HD 260655 system = 2"]
-[13.905193328857422, 7.142645835876465, "[TT] Primary Input Voltage of the Kiku-8 PPU = 100 V"]
-[10.824435234069824, 3.4768660068511963, "[TT] CubeSat Size of the PhiSat-1 = 6U"]
-[9.267105102539062, 5.1188273429870605, "[TT] Attitude Pointing Accuracy of the Spacecraft = 0.1\u00ba"]
-[7.5197038650512695, 1.2762879133224487, "[TT] Development Period of the Neutrally Buoyant Floats = Mid-1950s"]
-[5.527690410614014, 6.920440196990967, "[FF] Maximum Telemetry Rate of the Telemetry bus = Based on typical 1 minute snapshots with additional attitude control data saved at 1 Hz"]
-[4.878444671630859, 1.9226322174072266, "[FF] Information of the GeoSat Follow-On = http://enterprise.spawar.navy.mil/UploadedFiles/gfo_fs.pdf"]
-[5.876731872558594, 1.5503647327423096, "[FF] Presentation Location of the INDEX (REIMEI) = Hyderabad, India"]
-[7.49009370803833, 1.731852412223816, "[FF] Application Areas of the ResourceSat-2 = Agricultural crop discrimination and monitoring, crop acreage/yield estimation, precision farming, water resources, forest mapping, rural infrastructure development, disaster management"]
-[6.742729187011719, 1.0477794408798218, "[FF] First Capture Date of the Owens Valley Solar Array (EOVSA) = Sept. 10, 2017"]
-[9.278691291809082, 0.9935027360916138, "[TT] Size of the DART = About the size of a small car"]
-[9.844437599182129, 4.930688381195068, "[TT] Antenna Rotation Speed of the IRS = 1\u00ba/s"]
-[5.5753607749938965, 5.5687432289123535, "[TT] Interface Type of the Bus Interface = PCI"]
-[6.060530662536621, 4.8924994468688965, "[FF] Data Processing Requirement of the SVOM = Super-computers to process the data in real-time and smart algorithms to broker which transients to focus on with follow-up facilities"]
-[8.109389305114746, 2.9283456802368164, "[FF] Products of the GLI = Forecasting and warning of convection precipitation, and studying of Earth's electric field"]
-[10.848530769348145, 7.469429969787598, "[TT] Swath of the IIR = 64 km x 64 km"]
-[11.944210052490234, 5.041537761688232, "[TT] Dimensions of the APAA = 1420 mm x 920 mm x 1500 mm"]
-[8.230162620544434, 3.2902379035949707, "[FF] Measurement Type of the FTS = Amount of direct sunlight absorbed by atmospheric gases"]
-[8.056939125061035, 1.6730154752731323, "[FF] Orbit Altitude of the GOCE = Varies"]
-[4.942231178283691, 1.7070966958999634, "[TT] Mission Status of the OSCAR-QUBE = Operational (nominal)"]
-[14.257461547851562, 3.2442123889923096, "[TT] Mass of the MSU-50 = 2.3 kg"]
-[5.6146464347839355, 4.842980861663818, "[FF] Equipment of the GPS Spoofing = GSE (Ground Support Equipment)"]
-[14.521891593933105, 6.672919750213623, "[TT] Type of the Power Storage = NiCd"]
-[14.17189884185791, 3.180224657058716, "[TT] Mass of the CU = 5 kg"]
-[8.483073234558105, 1.9246447086334229, "[TT] Survival Heaters Status of the RapidScat = On"]
-[3.730924129486084, -0.9115366339683533, "[TT] Orbit Type of the ABEX = Highly eccentric orbit"]
-[5.587458610534668, -0.8313949108123779, "[TT] Design Life of the GOMS-1 = 3 years"]
-[9.13392162322998, 3.1153788566589355, "[FF] Method of the Cluster spacecraft = 3D electric field measurements"]
-[6.7285003662109375, 6.480328559875488, "[TT] Data Processing Time of the Spectra AI = 90 minutes"]
-[5.728187561035156, 6.309459686279297, "[TT] Capacity of the High capacity solid-state recorder = 9 Tbit"]
-[10.100886344909668, 1.4599602222442627, "[FF] Star Formation Rate of the M83 = A handful of new stars being born every year"]
-[6.955613136291504, 6.999025821685791, "[TT] Quantity of the Laser Diodes = 2"]
-[2.8633408546447754, 4.276662826538086, "[TT] Emergency Observation Time of the PALSAR-2 = 5:59 (GMT) on July 2, 2015"]
-[5.982563018798828, 0.6833362579345703, "[FF] Mission Date of the ASTERIA Space Telescope = Aug. 4-9, 2018"]
-[5.032467842102051, 3.3808743953704834, "[TT] Manufacturer of the Phi-Sat-1 = \u03a6 Department of the Earth Observation Directorate"]
-[3.4418368339538574, -0.9165893793106079, "[TT] Orbit of the SARAL spacecraft = Sun-synchronous near-circular dawn-dusk orbit"]
-[5.597423076629639, 5.643306255340576, "[TT] Processor of the OBC = 386 based computer"]
-[5.640859127044678, 0.7423074245452881, "[TT] Launch Dates of the GeoOptics = June 2017 and January 2018"]
-[5.7075581550598145, -0.9287397265434265, "[TT] Goal of the Design Life = 7.5 years"]
-[8.701515197753906, 4.7193217277526855, "[TT] Number of Star Images of the Star Tracker = One or two"]
-[8.021742820739746, 2.9304606914520264, "[FF] Function of the PACO = Perform atmospheric and topographic processing"]
-[12.002813339233398, 4.72042179107666, "[TT] Dimensions of the GCOM-W1 = 5.1 m (X) x 17.5 m (Y) x 3.4 m (Z)"]
-[6.461908340454102, 8.327643394470215, "[FF] Cross-polarization of the Instrument = Less than\u00d7-20 dB"]
-[5.687536716461182, 7.1190595626831055, "[TT] Data Rate of the ARM A8 Linux-based onboard computer = 19.2kbps"]
-[13.328112602233887, 7.1016998291015625, "[FF] Power of the PPS-1350-G = Nominal input power (in Watt)"]
-[7.796308517456055, -0.8756017684936523, "[FF] Deputy Project Scientist of the ICESat-2 = Tom Neumann"]
-[4.692362308502197, 6.470719337463379, "[FF] Electromagnetic Waves of the Tether = ULF, ELF, VLF"]
-[4.920434474945068, 5.0958123207092285, "[TT] CCSDS ID of the GSAT-0211 = 26B"]
-[4.371365547180176, 0.46303480863571167, "[TT] Observation End Time of the INTEGRAL = 22:14:36 on 25 January"]
-[8.768913269042969, 7.6137375831604, "[TT] Thermal IR Channels Resolution of the Imager = 4 km"]
-[13.389127731323242, 6.824498176574707, "[TT] Power of the Spacecraft = Up to 1065 W"]
-[11.834209442138672, 0.01941649802029133, "[TT] Number of Stars Observed of the TESS = 400,000"]
-[4.821755886077881, 3.069159984588623, "[TT] Members of the SPEXone Steering Committee = Two Airbus DS NL and two SRON members including the Principle Investigator"]
-[12.021125793457031, 4.784739971160889, "[TT] Envelope Dimensions of the RemoveSat = 0:65 m x 0:65 m x 0:72 m"]
-[7.11668586730957, 7.00761604309082, "[TT] Volume of the Laser = < 40 cm x 25 cm x 15 cm"]
-[6.338846206665039, -1.2816057205200195, "[TT] Launch Date of the GRACE-FO Satellites = December"]
-[5.520705699920654, 1.2664209604263306, "[FF] Announcement Date of the Mapping System = Aug. 18, 2014"]
-[7.755659103393555, 2.378462553024292, "[FF] Goal of the VIRR = Provide low-resolution visible and infrared images of oceans, coasts, and clouds"]
-[3.034475564956665, 4.51253604888916, "[FF] Observation Modes of the PALSAR-2 = Spotlight, 3/6/10-m resolution stripmap, and ScanSAR"]
-[8.068142890930176, 0.8377335667610168, "[FF] Impact of the Asia\u2019s Summer Monsoon = Refilling aquifers, generating hydroelectric energy, providing water for crops"]
-[5.009629249572754, 3.6171233654022217, "[TT] Manufacturer of the OBC = Intel"]
-[6.730451583862305, 4.478304862976074, "[FF] Manufacturing Process Controls of the Frangible Joint System = Sufficient to assure that variability in materials properties and hardware component dimensions, within both maximum and minimum tolerances, will not invalidate design performance requirements"]
-[6.027057647705078, -0.17152687907218933, "[TT] In Orbit Operations Duration of the RapidEye Constellation = 10 years"]
-[8.642326354980469, 1.1240888833999634, "[TT] Data Processing Location of the Aquarius = GSFC"]
-[5.375704288482666, 2.978424310684204, "[TT] Data Management Center of the SMMR = JPL"]
-[7.610116481781006, 5.547883987426758, "[FF] Detection Chain Components of the NAOMI = Detectors, F2EM, MEV"]
-[5.352749347686768, 0.24936586618423462, "[TT] Launch Date of the STS-95 = Oct. 29 - Nov. 7, 1998"]
-[5.631400108337402, 3.7712795734405518, "[FF] Spare Satellite of the NSPO = Provided in space depending on the launch vehicle capability"]
-[9.576189041137695, 7.167566299438477, "[TT] Spatial resolution at nadir of the TOU = 50 km"]
-[6.418543815612793, 8.623323440551758, "[FF] Polarization of the Wide Fine Quad-Pol and Wide Standard Quad-Pol modes = Quad-pol"]
-[9.918542861938477, 7.279778003692627, "[TT] Image Scene Length of the Geoton-1 = Up to 2000 km"]
-[11.841080665588379, 3.132166862487793, "[TT] Total Delta V of the NanoPS = > 35 m/s"]
-[4.978420257568359, 0.7797797918319702, "[FF] Program Start Date of the DRACO = Over a year ago"]
-[8.205101013183594, 8.83237361907959, "[TT] Spectral Resolution of the MAHRSI = 0.018 nm at 310 nm"]
-[4.8510284423828125, 2.922205686569214, "[TT] Prime Contractor of the SEOSAT-Ingenio = Spain"]
-[4.824625015258789, 2.64003849029541, "[TT] Antenna Type of the Eutelsat Quantum = Electronically steerable"]
-[1.7592179775238037, 6.1581339836120605, "[TT] Dark Matter Particle Mass of the AMS-02 = Approximately 40 and 60 GeV/c2"]
-[8.669445037841797, 3.785247325897217, "[FF] Instruments of the Solar Orbiter = In-situ instruments and Remote sensing equipment"]
-[6.074490547180176, 4.674859523773193, "[FF] Purpose of the GomSpace Sensor Bus (GSSB) = Allow interstage boards to act as intermediaries between sensors and the ADCS computer"]
-[4.4554057121276855, 2.860295534133911, "[FF] Location of the WCOM = Qu\u00e9bec, Canada"]
-[13.767457008361816, 3.0532171726226807, "[TT] Maximum Possible Value (MPV) Mass of the PUNCH Mission = 54.9 kg"]
-[10.348407745361328, 4.5138726234436035, "[TT] Reaction Wheels of the LEOStar-2 bus = Four"]
-[7.463423728942871, 1.2011489868164062, "[FF] Launch Date of the Global Surface Water Survey Mission = Unknown"]
-[16.557783126831055, 3.6442461013793945, "[TT] Number of Satellites in Orbit of the OneWeb = 254"]
-[9.178922653198242, -0.4397088587284088, "[TT] Apogee of the Orbit = 804.6 km"]
-[11.635108947753906, 3.7313616275787354, "[TT] Firing Duration of the X-axis Bang-Bang Maneuver = 10 s"]
-[9.566499710083008, 9.169063568115234, "[FF] Quantity of the IRIS = Unknown"]
-[18.79966163635254, 3.4795899391174316, "[TT] Mean \u0394N (m) of the Mosul = 4.6"]
-[8.877644538879395, 9.575708389282227, "[FF] Band 1 Wave Numbers of the TANSO-FTS-2 = 12,950 - 13,250"]
-[11.787202835083008, 4.734999656677246, "[TT] Size of the ASTERIA = ~10 x 20 x 30 cm"]
-[4.937028884887695, -1.7975257635116577, "[TT] Lunar Orbit Period of the Chang'e-1 = 127 minutes"]
-[9.7442626953125, 4.821930408477783, "[TT] Number of Electrodes of the TPS = 3"]
-[8.047060012817383, 5.008085250854492, "[FF] Observation Purpose of the SXS = Measure the velocity, density and dynamics of the material"]
-[5.49285364151001, 6.298905849456787, "[TT] Capacity of the OBR = 256 Gbit"]
-[13.889301300048828, 3.1586005687713623, "[TT] Mass of the MicroMAS-2a = 3.8 kg"]
-[7.92288875579834, 8.914554595947266, "[TT] Wavelength of the HSRL receiver = 532 nm"]
-[5.501284599304199, -1.8186784982681274, "[TT] Launch Date of the KOMPSAT-3 = May, 2012"]
-[13.447420120239258, 2.880011558532715, "[TT] Mass of the Satellite = 180 kg"]
-[7.8552985191345215, 8.564215660095215, "[TT] Spectral Bands of the IRIS Instrument = Green (520 - 600 nm), red (630 - 690 nm), and NIR (760 - 890 nm)"]
-[5.778151035308838, 7.53681755065918, "[FF] Bus Components of the Jason-2 = Altimeter and the DORIS receiver"]
-[7.888107776641846, 5.027628421783447, "[FF] Typical Value of the BrO = 5 x 10 -2"]
-[7.435504913330078, 6.985178470611572, "[TT] Sampling Period of the ScaRaB = 62.5 ms"]
-[9.144655227661133, 2.207474708557129, "[FF] Air Traffic Volume Scenario of the Model = 10 times higher than actual"]
-[7.597357749938965, 2.7991697788238525, "[FF] Purpose of the Carbon Mapper = Pinpoint, quantify and track point-source methane and CO2 emissions"]
-[4.416883945465088, 4.127694606781006, "[FF] Signal Tracking Capacity of the GETR = 4 general Galileo signals + 1 wideband AltBOC (Alternate Binary Offset Carrier) signal + 9 GPS satellites (L1+L2)"]
-[13.611279487609863, 1.7442866563796997, "[TT] Total Cargo Mass of the Dragon Resupply Vehicle = 2490 kg"]
-[6.998119354248047, 2.044970989227295, "[FF] URL of the SXI = http://www.research.noaa.gov/spotlite/archive/spot_sxi.html"]
-[5.650325775146484, 4.921971797943115, "[TT] Operation of the PH-U = Plugged into the MEXIC module"]
-[5.234498023986816, 3.2152748107910156, "[TT] Spacecraft of the MHS = MetOp-A spacecraft of EUMETSAT"]
-[7.798830032348633, 0.007878012955188751, "[TT] Latency of the ATL08 Land Water Vegetation Elevation = 45 days"]
-[8.453520774841309, 7.4074578285217285, "[TT] Optical Imager of the DebriSat = 1"]
-[5.1140971183776855, 4.7905402183532715, "[TT] Passes per Day of the Ground Station = 5.0"]
-[7.907797813415527, -0.5205766558647156, "[FF] Demonstration Date of the Polar Sea Ice Detection = 3 February 2020"]
-[7.972175598144531, 6.230074882507324, "[FF] Type of the Imaging multi-spectral radiometers = Vis/IR"]
-[8.339198112487793, 3.7274088859558105, "[FF] Function of the Machine Learning Algorithm = Compare specific structures across the wavelengths and strengthen its assessments"]
-[10.699021339416504, 2.83332896232605, "[TT] Design Life of the GaoJing / SuperView minisatellites = 8 years"]
-[8.813203811645508, 3.488565444946289, "[FF] Plasma Particle Data Analysis of the Reimei = URL:\u00a0 https://web.archive.org/web/20161222025705/http://www.iugonet.org/meetings/2010-02-25/05_Reimei_EISA_Hirahara_20100225.pdf"]
-[3.22625732421875, 5.515102386474609, "[TT] Range Resolution of the SAR Antenna = 3 m / 6 m / 10 m / 100 m"]
-[7.640021800994873, 1.3514642715454102, "[FF] Function of the ShadowCam = Capture images in lunar orbit"]
-[4.715956687927246, 3.158991813659668, "[TT] Developer of the PLEGPAY = Thales Alenia Space"]
-[7.050869464874268, 7.815527439117432, "[TT] Reflector Aperture of the Biomass = 12 m circular projected aperture"]
-[4.922706127166748, 2.5133163928985596, "[FF] Development Support of the Eutelsat Quantum = ESA and the UK Space Agency"]
-[4.774636268615723, 8.07817554473877, "[TT] Band of the LNA = 7145 to 7235 MHz"]
-[5.732148170471191, 12.150629043579102, "[TT] Wavelength FWHM of an unresolved line of the Spectrometer = 0.021 \u00b5m"]
-[12.167070388793945, 4.769845008850098, "[TT] S/C Bus of the IRS-1C and IRS-1D = Central cylinder (930 mm diameter x 1123 mm)"]
-[6.479176044464111, 3.69792103767395, "[FF] Status of the MEOLUTs = In the definition/prototype phase as of 2008"]
-[5.23986291885376, 1.0282419919967651, "[FF] Presentation Date of the Dave Williamson = April 3-6, 2017"]
-[7.994667053222656, 8.446514129638672, "[TT] Spectral Region Visible Channel of the VIRR = 0.49 - 0.94 \u00b5m"]
-[7.785129070281982, 1.2215508222579956, "[TT] Expected Duration of Effects of the Australian Wildfires = At least a year"]
-[8.736809730529785, 2.1517348289489746, "[FF] Altitude Range of the CO2 VMR = 50 - 100 km"]
-[6.780700206756592, 3.241494655609131, "[TT] Daily Deep-Space Observations of the SBSS-1 = 12,000"]
-[9.015036582946777, 5.5526814460754395, "[TT] Spacecraft pointing capability of the ALOS-3/PRISM-2 = \u00b160\u00ba (cone, max)"]
-[6.588557720184326, 4.806478977203369, "[FF] Unknown of the Test receivers = Unknown"]
-[10.969743728637695, 7.586782932281494, "[TT] Swath Width of the MR-2000M1 = 3100 km"]
-[9.063441276550293, 5.806790828704834, "[TT] Boresight Pointing Mechanism of the NIRST instrument = Yes"]
-[16.509557723999023, 3.5953311920166016, "[FF] Next OneWeb Launch of the Arianespace = ST30"]
-[13.431429862976074, 6.914690971374512, "[TT] Power Capability of the GOES-R = > 4 kW (EOL)"]
-[10.367027282714844, 2.278855562210083, "[FF] Design of the EPIC = Capture both low- and high-energy X-rays"]
-[3.44700026512146, 6.360898971557617, "[TT] Antenna Mounting Plane Clearance of the KySat-1 = 6.5 mm"]
-[8.735030174255371, 5.949212074279785, "[TT] Tracking Capability of the Coarse Lateral Sensor = 0.5 arcdeg/s"]
-[11.701898574829102, 3.394395589828491, "[TT] Nominal Thrust of the Ion Propulsion System = 1.24 mN"]
-[6.431284427642822, 4.133277893066406, "[FF] Communication System of the SPOT-6 & SPOT-7 = AstroTerra system"]
-[9.628202438354492, 8.469191551208496, "[FF] Field of View (FOV) of the SSM/I = Varies with frequency about 15 km at 85.5 GHz about 60 km at 19.4 GHz"]
-[7.800575256347656, 4.8244218826293945, "[FF] Type of the EPC (Electric Power Conditioner) = Miniaturized pulsed"]
-[10.158845901489258, 5.218204021453857, "[FF] Cryocooler Development Leads of the MIRI = JPL, Northrop Grumman, NASA's Goddard Space Flight Center"]
-[5.779573917388916, -0.8801836371421814, "[TT] Operational Lifetime of the Satellite = More than 20 years"]
-[8.716349601745605, 0.3843085765838623, "[TT] Neap Tide Height of the Gulf of Khambhat = 10 meters (33 feet)"]
-[9.182523727416992, 7.013914585113525, "[FF] Global 3 m resolution mosaic of the Biosphere = Global 3 m resolution mosaic"]
-[14.662111282348633, 6.680871963500977, "[TT] Battery Model of the PSU = Lithium-ion battery of Saft (France), model: MP144350"]
-[10.384130477905273, 4.485461711883545, "[TT] Quantity of the Scanwheel assemblies = Two"]
-[7.421072959899902, 2.925724506378174, "[FF] Monitoring Capability of the Satellite Constellation = Daily facility-scale methane monitoring"]
-[12.104509353637695, 6.268911838531494, "[FF] Boron-to-Carbon Ratio Study of the AMS-2 = Conducted"]
-[9.18249797821045, 5.068284511566162, "[TT] Operational Mode of the AOCS = Stellar yaw-steering"]
-[6.569756984710693, 7.669680118560791, "[TT] Data Quantization of the TeLEOS-1 Imager = 10 bit"]
-[10.045719146728516, 3.2153513431549072, "[FF] Purpose of the CubeSat = Lower cost, allowing the democratization of space"]
-[3.263183355331421, 5.702493667602539, "[TT] Aperture Size of the SAR Antenna = 15 m x 1.37 m"]
-[7.826716899871826, 2.487354040145874, "[FF] Effect of the South Atlantic Anomaly = Affects the amount of cosmic radiation reaching the passengers and crew of any plane and spacecraft led to cross it"]
-[7.9413275718688965, 2.7217392921447754, "[FF] Correction Types of the Atmospheric Correction = Flat and rugged terrain, haze/cirrus detection"]
-[5.993263244628906, -0.7300044894218445, "[TT] In-Orbit Lifetime of the AstroBus-L = Up to 10 years"]
-[9.47441291809082, 6.3238935470581055, "[TT] Scan Path of the Two-axis gimbaled mirror scan system = Predominantly E/W"]
-[8.02725887298584, 8.878396034240723, "[FF] Wavelength of the FAI = Near infrared (650-1100 nm)"]
-[10.26077938079834, 4.57030725479126, "[TT] Nominal Torque Setting of the Reaction Wheels = 1mNm"]
-[4.346736431121826, 2.1301088333129883, "[TT] Launch Date of the DubaiSat-1 = July 29, 2009"]
-[5.44074821472168, 6.920687198638916, "[TT] Data Transmission Rate of the SpaceDataHighway = 1.8 Gbit/s"]
-[9.822608947753906, -0.5922284126281738, "[TT] Orbit Altitude of the CBERS-4 = 778 km"]
-[14.491243362426758, 6.644256114959717, "[TT] Failure Cause of the BILSAT = Battery system failure"]
-[8.63265609741211, 7.250798225402832, "[TT] Temporal Resolution of the Imager = 2 ms"]
-[8.68738842010498, 6.999340534210205, "[TT] Spatial Resolution at Nadir of the WV60 imager = 0.50 m"]
-[7.479231834411621, 8.73452377319336, "[TT] Band 3 of the Instrument = 0.8 - 0.9 \u00b5m"]
-[12.144368171691895, 6.164362907409668, "[TT] Leptons Identified of the AMS-02 = 10.6 million"]
-[4.129199028015137, 6.3747053146362305, "[FF] Antenna Requirement of the CITRIS = Unobstructed hemisphere"]
-[6.6869120597839355, 5.47954797744751, "[FF] Power Modes of the dsPIC33F microcontroller = Unknown"]
-[5.855320930480957, 0.18447493016719818, "[TT] Join Date of the PARASOL = Early February 2005"]
-[9.01268482208252, -0.43620020151138306, "[TT] Orbit of the Spacecraft = 1km circular \u201cSafe Home\u201d orbit about the asteroid"]
-[6.297876358032227, 2.5533618927001953, "[FF] Purpose of the Orion Multi-Purpose Crew Vehicle = Safe, Reliable Human Transport to Deep Space"]
-[9.035563468933105, 5.144925117492676, "[FF] Objectives of the TDP = Position, velocity and time determination, inertial angular velocity"]
-[5.315403938293457, 0.9833938479423523, "[FF] Launch Date of the SSOT = Unknown"]
-[11.644164085388184, 4.7249274253845215, "[TT] Structure Shape of the Clementine = Octagonal prism"]
-[8.145244598388672, -1.054604172706604, "[FF] Volume of the ICESat-2 = Volume125"]
-[5.187634468078613, 1.488095760345459, "[TT] Development Status of the SMAP = Under development"]
-[5.437787055969238, -0.0633910521864891, "[TT] Project Start Date of the Heinrich Hertz = Mid-2009"]
-[5.327101230621338, 3.9679527282714844, "[TT] Quantity of the Active Satellites = More than 5,000"]
-[4.593405246734619, 6.6108078956604, "[FF] Components of the Ground Station = 9.1m S-band antenna, 4.6 m C-band antenna, antenna controllers"]
-[4.657495498657227, 1.6604067087173462, "[TT] General Manager of the GHGSat-C2 = Marc Corriveau"]
-[7.5212931632995605, 6.316922187805176, "[TT] Relative Time Accuracy of the TARANIS Instruments = Less than 10 ns"]
-[4.812729835510254, 0.6215333938598633, "[TT] Launch Date of the BeiDou-3S = 2015/2016"]
-[9.414222717285156, 6.282474040985107, "[TT] Cross-Track Angle of the MSI-0 and MSI-1 = 3\u00ba"]
-[7.768097877502441, 8.541521072387695, "[TT] Spectral Range of the GOME-2 = 240-790 nm"]
-[4.190896511077881, 1.9060145616531372, "[TT] Launch Date of the NigeriaSat-X = 17 Aug 2011"]
-[7.637829780578613, 8.990093231201172, "[TT] Spectral Range (\u00b5m) of the Band 1 = 0.58 - 0.68"]
-[9.453692436218262, 5.666411876678467, "[TT] Angle of the Satellite Slew = 30\u00ba"]
-[5.222235679626465, 4.709317207336426, "[TT] GNSS of the TriG-RO = GPS+ Galileo+GLONASS"]
-[8.86157512664795, 9.465993881225586, "[TT] SNR (Signal-to-Noise Ratio) of the Harris TANSO-FTS-2 = Very high"]
-[6.620371341705322, 1.7015786170959473, "[FF] URL of the Rosetta = http://www.esa.int/Our_Activities/Space_Science/Rosetta/Rosetta_overview"]
-[5.727035999298096, 6.199155330657959, "[TT] Model of the IXV Recorder = COTS SSR-500"]
-[9.544355392456055, 4.862901210784912, "[TT] Roll Axis Control of the GNB = Not controlled"]
-[5.746166706085205, -0.016743483021855354, "[TT] Operational Period of the ISS = Until 2028"]
-[5.0881853103637695, 4.410952091217041, "[TT] Number of Deorbited Prototypes of the Starlink = 2"]
-[8.31645679473877, 7.482377529144287, "[TT] Detector Type of the ASTERIA = Complementary metal-oxide-semiconductor (CMOS)"]
-[7.031085014343262, 6.255590438842773, "[TT] Science Modes of the CATS = Mode 1, Mode 2, Mode 3, Mode 4, Mode 5, Mode 6"]
-[8.29855728149414, 7.507406711578369, "[FF] Technology of the CMOS Imagers = Chosen over CCD technology because of their power efficiency and performance"]
-[3.646714925765991, 4.4318695068359375, "[FF] Monitoring of the L-band Synthetic Aperture Radar (SAR) = Land, ice and oceans"]
-[9.88442325592041, -0.38960716128349304, "[TT] Launch Altitude of the James Webb Space Telescope = Approximately 870 miles (1,400 km)"]
-[8.087778091430664, 2.786475419998169, "[FF] Purpose of the BCU = Measuring in-situ space weather conditions"]
-[8.747259140014648, 5.927333354949951, "[TT] Precision of the Support Structure = 0.1 mm"]
-[7.7577619552612305, 2.776773691177368, "[FF] Subaperture Area Percentage of the PAIS = Above some value"]
-[8.498530387878418, 1.767946720123291, "[FF] Data Usage of the SSM/T-2 = Determine water vapor mass in seven layers, and specific and relative humidity at six levels"]
-[6.4321513175964355, 5.167913913726807, "[FF] Components of the OBDH = Microcontroller and the other circuits needed for data storage, communication, conversions, timing and execution of the tasks"]
-[3.6387319564819336, 5.213503360748291, "[TT] Velocity Resolution of the MMW Radar = <50 m/s"]
-[9.803874015808105, 8.388249397277832, "[TT] Field of View of the AVHRR/3 = \u00b155.37\u00ba about nadir"]
-[5.5391740798950195, 0.7900122404098511, "[FF] Survey Date of the Hera = Unknown"]
-[5.652785778045654, 4.361203670501709, "[FF] IoT Services of the Astrocast = Track, measure, manage, communicate and control IoT assets"]
-[8.0641508102417, 2.641077756881714, "[TT] Measurement Domain of the CHORUS = Ocean, Land, Snow & Ice"]
-[9.272591590881348, 7.466058731079102, "[TT] Distance from Mercury of the Monitoring Camera 3 = 2687 km"]
-[8.194969177246094, 0.69364333152771, "[FF] Creation Method of the 3D Model of the Asteroid = Inferred the shape based on multiple photo angles"]
-[8.347041130065918, -0.501849889755249, "[FF] Width of the Pluto's Glacier = 1,000 kilometers"]
-[7.074680328369141, 1.0588316917419434, "[FF] Objective of the MarCO = Relay back InSight data as it enters the Martian atmosphere and lands"]
-[12.758230209350586, 1.97477126121521, "[FF] Measurement Types of the SAGE-III = UV and visible light"]
-[4.98675012588501, 3.3841233253479004, "[TT] Manufacturer of the ESAJECT Mechanism = Verhaert of Kruibeke, Belgium"]
-[7.587472915649414, 8.623818397521973, "[TT] Spectrum Bands of the CAPI = 5"]
-[9.263113975524902, 6.861289978027344, "[TT] System Complexity of the IMI = Lower than two-dimensional interferometric radiometers"]
-[6.244616985321045, 4.48971700668335, "[FF] Function of the Satellite primary structure = Carries the different satellite components and payloads"]
-[10.446924209594727, 5.507910251617432, "[TT] Surface Temperature of the Companion Star = 40% hotter than the Sun"]
-[8.525471687316895, 5.371035575866699, "[TT] Position Accuracy (RMS orbit) of the S-3 STC = 4 cm threshold with a target of 3 cm (radial)"]
-[5.931403160095215, 5.394084930419922, "[TT] Athermalized of the APIS = Yes"]
-[5.052300453186035, 3.2651960849761963, "[TT] Manufacturer of the GMAG = NASA\u2019s Goddard Space Flight Center"]
-[4.507859706878662, 3.0899834632873535, "[TT] New Factory Location of the Satellogic = Netherlands"]
-[8.73141860961914, 5.542662143707275, "[TT] Pointing Accuracy of the DMSP satellites = 0.01\u00ba"]
-[6.346863269805908, 1.4460393190383911, "[TT] Observation Date of the eROSITA = 18 to 19 October 2019"]
-[12.083155632019043, 2.9705276489257812, "[FF] Propulsion System of the TanSat = Four 1N hydrazine thrusters with 10 kg of propellant on board"]
-[7.464179515838623, 0.9455026984214783, "[FF] Effect of the Moonlight = Reducing the design complexity and weight of individual missions"]
-[5.251278400421143, 2.5687499046325684, "[TT] Launch Agency of the ERG (Arase) spacecraft = JAXA (Japan Aerospace Exploration Agency)"]
-[6.106410980224609, 4.615285873413086, "[TT] Communication of the SOLCON-3 = General Orbiter services, including power control, command, and telemetry"]
-[1.743607759475708, 4.56418514251709, "[FF] N/A of the fluidics connections = N/A"]
-[6.339256763458252, 6.863779067993164, "[TT] Data Inputs of the Front End Electronics = 5"]
-[8.8090181350708, 0.44386449456214905, "[TT] Coordinates of the Tohoku-Kanto earthquake = 38.32\u00baN, 142.37\u00baE"]
-[8.041419982910156, 5.21514368057251, "[FF] Calibration Accuracy of the FY-4A = 1.5 K (3\u03c3) radiation, 1.0 K (3\u03c3), 10 ppm (3\u03c3) spectrum, 5 ppm (3\u03c3)"]
-[9.928016662597656, 4.424966335296631, "[FF] Functionality of the Torquers = Apply counter dipoles"]
-[7.743565559387207, 6.857266426086426, "[TT] Number of Exposures of the Exposures = 3"]
-[3.946176290512085, 9.700983047485352, "[TT] Frequency (GHz) of the ICI-1 = 183.31\u00b18.4"]
-[5.141287326812744, -0.26963821053504944, "[FF] Activation Time of the Launch Abort System = Milliseconds"]
-[4.761880874633789, 0.5208327770233154, "[FF] Launch Date of the SARAL = Feb. 25, 2013"]
-[7.011319160461426, -0.7906613349914551, "[TT] Orbital Period of the HD 21749b = 36 days"]
-[6.1580376625061035, 0.10851850360631943, "[FF] Validation Tests of the OCK (Orbit Control Kit) = Three short tests lasting up to several days, followed by a 4th extended test that lasted two weeks"]
-[9.437457084655762, 7.432055473327637, "[TT] Panchromatic GSD at Nadir of the NAOMI = 0.7 m to 2.5 m"]
-[7.731160640716553, 7.982583999633789, "[TT] Sensitivity of the MWR = 0.5 K"]
-[10.40364933013916, 7.361013412475586, "[TT] Support Component Material of the TX Telescope = Invar"]
-[10.554020881652832, 7.3695478439331055, "[TT] Near Edges of the SASS = 200 km from subsatellite track"]
-[10.20600700378418, 1.1517444849014282, "[TT] Diameter of the Cas A = 10 light years"]
-[4.52776575088501, 5.876939296722412, "[FF] Additional Component of the GomX-4B = Extra transceiver in the Software Defined Radio for ISL operations"]
-[8.37028980255127, -0.4626176953315735, "[TT] Spatial Resolution of the Sea Ice Concentration (SIC) = 5 km"]
-[6.531343460083008, 4.009983062744141, "[FF] Ground Segment of the PARASOL = Unknown"]
-[5.973299026489258, 2.4820539951324463, "[FF] Recipient Prize of the Marcel Grossmann Award = Silver casting of the T. E. S. T. sculpture"]
-[10.117411613464355, 5.632806777954102, "[FF] Temperature of the CrIS-based passive detector cooler = Achieves temperatures needed for IR detectors"]
-[6.514185905456543, 5.181954383850098, "[FF] Function of the ETB/DHS = Provides a large number of general-purpose interface ports, analog sampling, isolated power conversion, and expanded memory management capability"]
-[9.311851501464844, 4.889762878417969, "[TT] Idle Spacecraft Guidance and Attitude Control of the RBA = True"]
-[4.5724287033081055, 2.717984676361084, "[FF] Location of the Richat Structure = Mauritania"]
-[6.88215446472168, 1.0461556911468506, "[FF] Installation Date of the Solar Panels = 20 June 2021"]
-[5.705333709716797, 1.6640572547912598, "[FF] Mission of the ALADIN = AEOLUS"]
-[3.9367620944976807, 4.293371200561523, "[FF] Application of the RISAT-2 = Earth observation"]
-[8.236750602722168, 4.901689052581787, "[FF] Sensor Complement of the CubeRRT = Specialized digital-based spectrometer equipped with sophisticated algorithms"]
-[3.118492603302002, 3.9047677516937256, "[FF] Symposium Date of the NISAR = 21-26 July 2013"]
-[7.163429260253906, 1.2413800954818726, "[TT] Potential Mission Services Value of the Mars Ascent Propulsion System (MAPS) = $60.2 million"]
-[10.295175552368164, 3.113507032394409, "[TT] Reaction Wheel Test of the SONATE CubeSat = Successful"]
-[4.899542808532715, 7.330521583557129, "[TT] Data Rate of the L-band HRPT = 665,400 bit/s"]
-[7.166118144989014, 5.101690769195557, "[FF] Components of the SIR-2 = Sensor unit, power unit, ICU"]
-[7.28147554397583, 4.996352672576904, "[FF] Purpose of the MPPT = Improve the performance of the onboard power generation system"]
-[8.178725242614746, -0.615815281867981, "[FF] Monitoring Purpose of the SMOS = Antarctic ice sheet"]
-[4.496115684509277, 3.0226006507873535, "[TT] Location of the MCF = CSA in Saint-Hubert, Quebec"]
-[8.171611785888672, 7.580724716186523, "[TT] Detector Type of the FUV Instrument = Intensified CCD"]
-[5.280921936035156, 1.2793575525283813, "[FF] Conference Presentation Date of the STSat-2 = Aug. 11-14, 2003"]
-[10.1530179977417, -1.4564162492752075, "[TT] Inclination of the GOSAT-2 = 97.84\u00b0"]
-[10.71487045288086, 7.40278959274292, "[TT] Swath (nadir) of the Payload = \u226530 km"]
-[1.723524570465088, 6.149317264556885, "[FF] Dark Matter Content of the Leo I = Not much"]
-[9.020978927612305, 5.218435287475586, "[TT] Gyro Configuration of the IRU (Inertial Reference Unit) = Four gyros in a tetrahedron configuration"]
-[5.378210067749023, 8.787108421325684, "[TT] Bandwidth of the Band 1 = 0.281 \u00b5m (13 cm -1)"]
-[11.069222450256348, 4.602290630340576, "[TT] Drill Depth of the Rosalind Franklin = Up to two meters"]
-[11.686637878417969, 0.17217862606048584, "[TT] Size of the TESS = Three times larger than Earth"]
-[7.703186988830566, 9.203239440917969, "[TT] Wavelength Range of the Band 9 = 6.75-7.15 \u00b5m"]
-[7.0528435707092285, 4.680136680603027, "[TT] Location of the REM = Outside, on the front panel"]
-[8.747810363769531, 8.824666023254395, "[TT] Groove Density of the Grating = ~646 grooves/mm at the center"]
-[8.187356948852539, 2.2800021171569824, "[FF] Cloud-Contaminated of the FTS-2 = Value"]
-[11.36683464050293, 5.847734451293945, "[TT] Material of the Spacecraft Structure = Aluminum 7075-T6"]
-[10.338096618652344, 3.2103843688964844, "[FF] Record Load of the Minotaur I Rocket = 28 CubeSats"]
-[4.862935543060303, 6.2891645431518555, "[TT] Protocol of the RF Communications = AX.25"]
-[14.03007698059082, 6.2967448234558105, "[FF] Power Storage of the Satellite = Batteries"]
-[7.869922637939453, 4.604273319244385, "[FF] Position of the EFS = Below the Landsat-9 and above the top of Centaur"]
-[7.5406060218811035, 1.8881337642669678, "[FF] Purpose of the Veggie = Cultivate leafy greens"]
-[4.436392784118652, 7.720883846282959, "[TT] Frequency band of the Feeder Link = Ka-band (20 / 30 GHz)"]
-[13.855599403381348, 5.680721759796143, "[TT] Maximum Efficiency of the Solar Cell Assemblies = 25%"]
-[6.693609237670898, 4.712334156036377, "[FF] Function of the HemoCue = Provide quick and accurate counts of total and differentiated white blood cells"]
-[9.221176147460938, 5.270110130310059, "[TT] Pointing Precision of the HY-2A = < 0.1\u00ba in pitch, roll and yaw"]
-[6.929158687591553, 3.6677663326263428, "[FF] Enshrouded of the AGN = Yes"]
-[4.989905834197998, 3.848904609680176, "[TT] Developer of the NorSat-3 = FFI in collaboration with Kongsberg Seatex"]
-[6.81250524520874, 6.445033550262451, "[TT] Time of the Test Modes = 60 minutes"]
-[5.572966575622559, 0.4758840799331665, "[TT] Launch Date of the GEOS-3 = 9 April 1975"]
-[10.981063842773438, 4.783045768737793, "[FF] Accuracy Influence of the HCS = Free release of the tether"]
-[9.809090614318848, 7.474216461181641, "[TT] Ground Sample Distance of the Imager = 8-14 km"]
-[1.7517247200012207, 4.559144496917725, "[FF] N/A of the control unit = N/A"]
-[13.362689971923828, 2.8660953044891357, "[TT] Mass of the DubaiSat-1 = 12 kg"]
-[11.835165977478027, 6.710934162139893, "[TT] Energy Range of the GRS = 300 keV - 9 MeV"]
-[6.152273178100586, 0.4279178977012634, "[TT] Data Availability of the ATMS = Within 180 minutes of observation"]
-[14.057064056396484, 3.0584144592285156, "[TT] Weight of the SPOT-3 = 1800 kg"]
-[4.710707187652588, 0.8689166903495789, "[TT] End of Mission of the PROBA-V = April 20, 2020"]
-[5.241089344024658, 5.659107208251953, "[FF] Version of the CCSDS Space Data Link Security Protocol = 355.0-R-2"]
-[7.8972601890563965, 6.44935941696167, "[TT] Type of the ACE-FTS = Limb-scanning infrared spectrometer"]
-[8.843013763427734, 7.766124248504639, "[TT] Over-sampling Ratio of the INSAT-3D Imager = 1.75 for all channels except WV, 3.5 for WV channel"]
-[8.015780448913574, 5.164566993713379, "[FF] Geometric Accuracy and Stability of the PROBA-V = Unknown"]
-[8.751543045043945, 6.755239963531494, "[TT] Generation of the DMC-3 = Next"]
-[10.93813419342041, 7.53848934173584, "[TT] Swath Width of the MWHS-II = 2600 km"]
-[11.743110656738281, 7.521886348724365, "[TT] Years on Orbit of the Megha-Tropiques = 3"]
-[5.128275394439697, 2.370339870452881, "[TT] Mission Type of the CHORUS = EO"]
-[4.543960094451904, 0.8542107939720154, "[TT] Routine Operational Phase Start Date of the ADEOS = November 26, 1996"]
-[4.934636116027832, 7.310328960418701, "[TT] Data Rate of the S-band transmitter = Up to 144 kbit/s"]
-[2.9628024101257324, -0.37569570541381836, "[TT] Altitude of the OneWeb = 1,200 kilometers"]
-[11.222504615783691, 5.0679030418396, "[TT] Wire Harness Length of the Integrated Sensor = 500 mm"]
-[5.979309558868408, -0.413505494594574, "[TT] Mission Duration of the TSIS = Five years"]
-[8.095401763916016, 4.145666122436523, "[FF] Test Range of the LARES, LAGEOS and LAGEOS 2 satellites = 12,270 km"]
-[5.459181785583496, 6.048179626464844, "[TT] Static RAM of the OBDH = 256 kB"]
-[8.352803230285645, 7.628280162811279, "[TT] Detector Type of the Spectral Channels = Silicon"]
-[8.918354988098145, 7.4163126945495605, "[TT] Imaging Resolution of the FormoSat-2 = 2 m (panchromatic), 8 m (multispectral)"]
-[9.729308128356934, -0.5180961489677429, "[TT] Final Orbit Altitude of the Aquarius = 657 km above Earth"]
-[13.383439064025879, 7.314622402191162, "[TT] Power of the BIT-3 = 70 W"]
-[5.372067928314209, 3.033012866973877, "[FF] Manufacturer of the InSight = Lockheed Martin Space in Denver"]
-[8.949969291687012, 5.506054401397705, "[FF] Issue of the BPP (Bi-axial Pointing Platform) = Difficulties in achieving the pointing control precision"]
-[7.961116313934326, -0.5928681492805481, "[TT] Instrument 2 of the CryoSat-2 = LRR"]
-[5.034029006958008, -0.31519463658332825, "[TT] Launch Time of the KazSTSAT = 18:34:05 GMT"]
-[8.527743339538574, 2.032607078552246, "[FF] Gaps of the WSF-M = Ocean surface vector winds (OSVWs), tropical cyclone intensity (TCI) and LEO energetic charged particles"]
-[8.561530113220215, 1.9192174673080444, "[TT] Temperature Range of the Silicate Clouds = Between about 1,900 degrees Fahrenheit and 3,100 degrees Fahrenheit"]
-[7.410420894622803, 4.831058979034424, "[TT] Mounting of the M1 = Central fixture at back side"]
-[4.866306781768799, 3.3029539585113525, "[FF] Manufacturer of the LPT/CANDOS = ITT-AES (Advanced Engineering & Sciences), Reston, VA, a division of ITT Industries Inc"]
-[13.536336898803711, 5.860785484313965, "[TT] Solar Arrays Power of the Electrical Power Subsystems (EPS) = Over 330 W"]
-[5.246217250823975, 7.716492176055908, "[TT] E5 to E1 Port Isolation of the Antenna = Higher than 40 dB"]
-[7.767598628997803, 2.1403119564056396, "[FF] Purpose of the ALT = Produced the first global view of the variability of the surface geostrophic currents"]
-[6.100099563598633, 7.017800331115723, "[TT] Acceleration of the iCPS engine = 0.5 g"]
-[4.868500232696533, -0.04085730388760567, "[TT] End of Life Date of the JERS-1 = 12 Oct 1998"]
-[4.352645397186279, 4.394748687744141, "[FF] Ground Segment Providers of the COSPAS-SARSAT = 24"]
-[5.061201572418213, 7.8865966796875, "[FF] LO Precision of the Satellite Device = 50 MHz"]
-[8.999716758728027, 6.480226516723633, "[TT] Image Capture Location of the CaSSIS = 26.8\u00baS/34.8\u00baW"]
-[9.842466354370117, 4.793083667755127, "[TT] Spin of the Satellite = Up to 5 rpm"]
-[6.824046611785889, -0.5295496582984924, "[TT] Orbit Period of the Harmony = 98.74 minutes"]
-[8.431660652160645, 2.60705828666687, "[FF] Purpose of the MAIA = Measure particulate matter to allow correlation with adverse human health issues"]
-[9.231754302978516, -0.5497008562088013, "[TT] Cube Size of the Orbit Your Thesis! 2019 program = 1U"]
-[9.563093185424805, 0.6672449111938477, "[TT] Rate of Movement Away from Earth of the Moon = 3.8 cm/year"]
-[7.577208518981934, 8.764214515686035, "[TT] Optics Type of the LISS-3 = Refractive optics in four spectral bands"]
-[7.561594486236572, 5.586453914642334, "[FF] Configuration of the MICAP = L-band scatterometer and different frequencies for radiometer"]
-[7.183651447296143, 4.783890724182129, "[FF] Self-identification of the SPA Components = Provide information about their functions and use to the system"]
-[14.570694923400879, 6.60203742980957, "[TT] Battery Depth of Discharge of the RADARSAT-2 = Less than 8%"]
-[14.102045059204102, 3.1928396224975586, "[TT] Mass of the STX-01 = 80 g"]
-[6.560667037963867, 0.3565657138824463, "[TT] Monitoring Duration of the Landsat probes = Since 1972"]
-[11.422648429870605, 4.341040134429932, "[TT] Size of the Centauri-1 = 3U"]
-[11.963554382324219, 4.841894149780273, "[TT] Form Factor of the GPS Receiver = 46 mm x 71 mm"]
-[4.602016925811768, 1.1609867811203003, "[TT] Development Time of the SAOCOM-1A = since 2011"]
-[9.655011177062988, 8.392058372497559, "[TT] FOV of the Microdosimeter B = 32\u00ba"]
-[10.843121528625488, 1.3670977354049683, "[TT] Mass of the Companion Star = About half the mass of the Sun"]
-[8.547235488891602, 5.527585029602051, "[TT] Initial Position Accuracy of the Transit Navigation = Few hundred meters"]
-[7.551056385040283, 3.546626567840576, "[FF] Data of the NightPod = Images of natural and human-made events on Earth"]
-[7.473816394805908, 6.6040825843811035, "[TT] Image Acquisition Order Acceptance Time of the PDC (PASCO Data Center) = Before AOS -30 minutes"]
-[6.945930004119873, -0.7515241503715515, "[FF] Orbital Period of the B binary = About every eight days"]
-[8.893136978149414, 5.794711112976074, "[TT] EW (3\u03c3) of the Navigation = \u00b121 \u00b5rad"]
-[5.676897048950195, 5.61872673034668, "[TT] Model of the OBC = 80C386EX"]
-[3.6141862869262695, 5.1576642990112305, "[FF] Radar of the ALOS-2 = L-band radio waves"]
-[11.627208709716797, 3.2567641735076904, "[TT] Travel Time to Destination of the RF Ion BIT-3 thruster = About three months"]
-[5.470163822174072, 6.179408073425293, "[FF] Data Storage of the SOLID Panels = The data regarding registered impacts on the panels will be stored by the satellite's on-board computer for a subsequent downlink"]
-[7.903946876525879, 4.220061302185059, "[FF] Purpose of the SET = Survey the slot region and study radiation damage to instruments"]
-[8.907453536987305, 5.5261969566345215, "[TT] Pointing Accuracy of the Spacecraft = Better than 0.05\u00ba (3\u03c3)"]
-[6.7612762451171875, 3.17730975151062, "[FF] Revisit Time of the Satellite Constellation = Much better in higher latitudes"]
-[13.845390319824219, 7.07592248916626, "[TT] Voltage Output of the PPU = 800 V"]
-[8.761232376098633, 1.931754469871521, "[TT] Internet Connection Speed of the WINDS = 155 Mbit/s"]
-[9.724679946899414, 1.4268385171890259, "[TT] Moon Image Resolution of the Pleiades-1A and Pleiades-1B = ~300 m"]
-[6.572765350341797, 6.9940361976623535, "[TT] Duty Cycle of the Instrument = 100%"]
-[8.36144733428955, 3.3276052474975586, "[TT] Ozone Limb Sounding of the LORE = 88%"]
-[7.302047252655029, 9.130132675170898, "[TT] Number of Wavelength Positions of the FG (Filtergraph) = Six"]
-[7.573177814483643, 8.864641189575195, "[TT] Radiometric Accuracy of the Spectral Band A = 3"]
-[7.210853576660156, 1.2519606351852417, "[FF] Detection of the NOMAD-TGO = Green line emission in the dayside atmosphere of Mars"]
-[4.746711730957031, 7.293282985687256, "[FF] Signal Generation of the SE (Sensor Electronics) = Low power transmit signal pulses at C-band"]
-[13.297470092773438, 2.9254679679870605, "[TT] Mass of the ZASat-002 = 82 kg"]
-[6.025506496429443, 0.11768607050180435, "[FF] Time Reference of the GESS = IEN time"]
-[7.206186771392822, 2.3053083419799805, "[FF] Image Type of the Landsat-8 Operational Land Imager (OLI) = Natural color image"]
-[13.854625701904297, 5.671224594116211, "[TT] Nominal Efficiency of the Solar Cell Experiment = 15%"]
-[7.480715751647949, 6.897762775421143, "[TT] Data Product Cadence of the MAG Sensor = 1 message per 0.874 seconds"]
-[6.071804046630859, 1.6519824266433716, "[FF] Date of the Symposium on Small Satellite Systems and Services (4S) = May 31-June 4, 2010"]
-[5.815374851226807, 1.9246357679367065, "[TT] Contact Email of the eoPortal = eoportal@symbios.space"]
-[9.716681480407715, -0.4700099229812622, "[TT] Pointing Altitude of the FAI = 110-km"]
-[4.898245334625244, 3.344783067703247, "[TT] Manufacturer of the TecSAR = Israel Aerospace Industries Ltd (IAI)"]
-[12.10592269897461, 3.5786781311035156, "[TT] Preload Force at South Pole of the Separation System = About 140000 N"]
-[14.549043655395508, 6.678299427032471, "[TT] EPS of the SCARAB = Clyde Space 1U EPS w/Lithium-polymer battery"]
-[10.415234565734863, 7.117465019226074, "[TT] CONUS Rectangle Size of the ABI = 4.81\u00ba 8.02\u00ba"]
-[7.650559902191162, 0.5706532001495361, "[FF] Internal Water Evidence Date of the Moon = August 27, 2013"]
-[4.8376970291137695, -0.9887030124664307, "[TT] Age of the FengYun-1C = Modern"]
-[3.473914861679077, 4.7707600593566895, "[TT] Imaging Frequency Band of the COSMO-SkyMed = X"]
-[7.498645782470703, 7.003312110900879, "[FF] Cadence of the EUVS = \u226430 s, 27 s"]
-[4.347529888153076, 7.134300708770752, "[FF] Components of the Ka-band payload = Multi beam antenna, on-board switching transponder subsystem"]
-[6.713469505310059, 4.849522590637207, "[FF]  of the CubeSense = "]
-[10.212591171264648, 5.463770866394043, "[FF] Thermal Performance of the SAS = Analyzed for design limits and thermal ranges"]
-[10.922568321228027, 7.5645036697387695, "[TT] Swath Width of the StriX-\u03b1 = More than 10-30 km"]
-[7.975389003753662, 1.692138433456421, "[FF] Imaging of the DPR (Dual-frequency Precipitation Radar) = A three-dimensional cross-section of the storm"]
-[4.607576370239258, 1.4875341653823853, "[TT] Agreement Date of the COMSAT, Inc. = February 19, 2018"]
-[6.167783737182617, 2.925842046737671, "[TT] Imaging Frequency of the WorldView Legion Constellation = Every 20 to 30 minutes"]
-[10.944327354431152, 0.8381076455116272, "[TT] Orbit of the LISA = Earth-trailing heliocentric orbit about 50 million km from Earth"]
-[10.540534973144531, 2.8188304901123047, "[FF] Purpose of the Kaber = Deploy microsatellites from the ISS orbit"]
-[3.330415725708008, 2.2534024715423584, "[FF] Product Levels of the Sentinel-3 = Level 1, Level 2"]
-[7.501373767852783, 3.7772510051727295, "[FF] Usage of the NightPod = Align to ISS local nadir direction, keep desired target steady in the camera's FOV, manually point at off-track targets"]
-[6.562920570373535, 8.670682907104492, "[TT] Polarization Sensitivity of the WPM = < 7.0 %"]
-[5.209408760070801, 2.3754947185516357, "[TT] Mission Type of the CXBN-2 = Non-EO"]
-[3.62756085395813, 4.619840145111084, "[FF] Data Product Levels of the SAR Processor = Raw Signal Products (level-0), Geo-Tagged Products (level-1), Terrain-corrected Geocoded Products (level-2)"]
-[9.983230590820312, 5.727766990661621, "[TT] PT-type Thermistors of the TCS = 36"]
-[12.460285186767578, 0.5661672353744507, "[FF] Proposal Selection Date of the PLATO = 25 April 2018"]
-[6.1231255531311035, 5.310096740722656, "[FF] Processor Configuration of the CFTP = Reconfigurable"]
-[8.551647186279297, 3.6201694011688232, "[TT] Radiation Source of the Extinctive Stellar Occultations = Star"]
-[11.288055419921875, 5.838597297668457, "[FF] Composition of the SCM = Flour-polymer resin over a copper substrate"]
-[7.358326435089111, 4.9464592933654785, "[FF] Recovery of the VBS = Automatic and optimized for robustness and speed"]
-[5.901233196258545, 0.9336599111557007, "[TT] Image Acquisition Date of the Menara = 24 Feb. 2013"]
-[7.1989898681640625, 4.773728847503662, "[FF] Function of the WTS = Samples the angular distribution"]
-[5.3086700439453125, 2.035029411315918, "[TT] Mission Status of the SOHLA-1 = Retired"]
-[8.055549621582031, -2.3901195526123047, "[TT] Altitude Range of the GOLD = 80-600 km"]
-[7.27298641204834, 5.133790016174316, "[FF] TLEs Recorded of the ISUAL = 31,369"]
-[14.130354881286621, 3.3679707050323486, "[TT] Mass of the TIDM = 30 g"]
-[4.72789192199707, 8.339956283569336, "[TT] Center Frequency of the 2 = 52.8 GHz"]
-[6.072364330291748, 2.2928099632263184, "[FF] Leading Scientist of the IASI = Cathy Clerbaux"]
-[6.164933681488037, 3.6034188270568848, "[FF] Roadmap of the DG constellation = Extends industry leadership well into the next decade"]
-[13.482512474060059, 2.823312759399414, "[TT] Dry Mass of the Meteosat = 322 kg"]
-[14.130782127380371, 6.80946683883667, "[TT] Battery Charging Voltage Range of the SABR = 5-34 V"]
-[4.935263156890869, 5.994276523590088, "[TT] Communication Mode of the LLITED satellites = Receive only"]
-[10.53196907043457, 2.4865293502807617, "[FF] Diagnostic of the Microdosimeter Suite = Identify when X-ray measurements may be contaminated from charged particles"]
-[10.115520477294922, -2.7090399265289307, "[FF] Technology of the MMFU = NAND-Flash memory devices"]
-[6.3658127784729, -0.48626258969306946, "[TT] Period of the STRV-1a = 10 hours and 27 minutes"]
-[9.3643798828125, 6.901905059814453, "[TT] Along-Track Resolution of the SIRAL = 250 m"]
-[10.367011070251465, 2.3349249362945557, "[TT] X-Ray Sensor (XRS) of the EXIS = Measures soft X-rays"]
-[9.667450904846191, 3.911249876022339, "[TT] Magnetometer Collections of the QuakeSat = Nearly 2000"]
-[7.57670783996582, 6.915444850921631, "[TT] FPA NEDT of the CIRiS = < 50 mK"]
-[6.3114705085754395, -1.2406724691390991, "[FF] Complementary Missions of the GOCE = CHAMP (launch July 15, 2000) and GRACE (launch March 17, 2002) missions"]
-[5.208611488342285, 2.106873035430908, "[TT] Mission Status of the SPOT-5 = Mission complete"]
-[10.463090896606445, 1.6213144063949585, "[TT] Luminosity of the NGC 5907 ULX = 1,000 times more than the maximum thought possible for an accreting neutron star"]
-[7.709063529968262, 6.537561416625977, "[TT] Scan Mode 4 (Continuous Full Disk) of the ABI = 5 minutes"]
-[6.319936275482178, 7.1514892578125, "[TT] Onboard Compression of the DACS = 2-6 bit BAQ"]
-[10.026082992553711, 0.18265219032764435, "[TT] Spacing of the EDSN Swarm = ~20 km"]
-[3.372166395187378, 5.880015850067139, "[TT] Number of Radiating Element Groups per Tile of the SAR antenna subsystem = 24"]
-[10.192288398742676, 2.523282527923584, "[FF] Authors of the ART-XC Instrument = M. Pavlinsky, V. Akimov, V. Levin, I. Lapshov, A. Tkachenko, N. Semena, V. Arefiev, A. Glushenko, A. Yaskovich, R. Burenin, S. Sazonov, M. Revnivtsev, M. Buntov, S. Grebenev, A. Lutovinov, M. Kudelin, S. Grigorovich, D. Litvin, V. Lazarchuk, I. Roiz, M. Garin, M. Gubarev, B. Ramsey, K. Kilaru, S. L. O'Dell, R. Elsner"]
-[7.9234538078308105, 6.422303199768066, "[TT] Instrument Types of the Sich-2 = Imaging multi-spectral radiometers (vis/IR), High resolution optical imagers"]
-[7.728639602661133, 9.085567474365234, "[TT] Wavelength Range of the Spectral band 3 = 0.2 - 50 \u00b5m"]
-[10.791418075561523, 3.5066633224487305, "[TT] Size of the SurfSat = 2U"]
-[11.537672996520996, 2.75822377204895, "[TT] Mass of the KazEOSat-2 minisatellite = 185 kg"]
-[5.032990455627441, 4.273634433746338, "[TT] Number of Stations of the DRDC Ground Station Network = 6"]
-[6.551849842071533, 1.432144045829773, "[FF] URL of the MERTIS = https://www.researchgate.net/publication/224798007_Thermal_infrared_spectroscopy_to_investigate_the_composition_of_mercury_-_The_MERTIS_instrument_on_BepiColombo"]
-[13.875848770141602, 5.663712024688721, "[TT] Efficiency of the Solar Cells = 24%"]
-[5.405383110046387, 5.958468437194824, "[TT] RAM of the STRV-2 DHS = 512 k"]
-[4.365810871124268, 7.067551136016846, "[TT] TT&C Communication Band of the TTCS = S-band"]
-[8.5288667678833, 5.656086444854736, "[TT] Accuracy of the Navigation Receiver = Less than one meter"]
-[6.537489414215088, -0.35112717747688293, "[TT] Period of the ALOS-2 = 97 minutes"]
-[8.283358573913574, 4.5325798988342285, "[TT] Primary Payload of the LARES-2 = Yes"]
-[4.64178466796875, 0.1248774379491806, "[FF] Final Mission Report Date of the FREESTAR = March 20, 2003"]
-[7.559203624725342, 8.347268104553223, "[TT] Bands of the GOES Imager = 1 VIS band, 2 MWIR bands, 2 TIR bands"]
-[2.901092767715454, 4.380005836486816, "[TT] Observation Frequency of the PALSAR-2 = Once a year"]
-[6.667362689971924, -0.23985843360424042, "[FF] Exchange Time with Interplanetary Space of the Exosphere = Monthly time scale"]
-[10.303831100463867, 5.717329978942871, "[TT] Temperature of the Filter Wheel = 213K"]
-[7.838332176208496, 7.012657642364502, "[TT] Configuration of the Michelson Interferometer = Flat-mirror Michelson"]
-[5.417706489562988, 8.694869041442871, "[TT] Spectral Bandwidth of the Spectral Bandwidth = 8 nm <1000 nm and 16 nm >1000 nm"]
-[5.646298885345459, 4.495599746704102, "[FF] Communication Improvement of the EDRS = Significantly improve the stringent timeliness requirements of demanding Earth observation missions"]
-[4.797412872314453, 3.9003069400787354, "[TT] Ground Stations of the Gokturk-2 = One fixed and one mobile"]
-[5.499803066253662, 6.2165374755859375, "[TT] Speed of the ODHS Processor Module = Up to 200 MIPS"]
-[11.602882385253906, 6.640506744384766, "[TT] HST Measurement of the LCI = 100 \u2013 500 keV electrons"]
-[10.832664489746094, -0.31605684757232666, "[TT] Acquisition Year of the Amptek X123 SDD = 2012"]
-[6.4393696784973145, 3.1618261337280273, "[FF] Participation of the Vision-1 = International Disasters Charter"]
-[8.42008113861084, 3.2024195194244385, "[TT] Vertical Cell Size of the Ozone Measurement Instrument = 3 km"]
-[9.57304859161377, 9.21664810180664, "[TT] Launch Date of the IRIS = June 28, 2013"]
-[3.8741488456726074, 6.176974296569824, "[TT] Mission of the 3D-printed metal antenna = PROBA-3"]
-[13.403331756591797, 6.890409469604492, "[TT] Ion Emitter Type of the ASPOC = Liquid metal type"]
-[9.097565650939941, 3.319159746170044, "[FF] Purpose of the GEOTAIL = Determine the role of the distant and near-Earth tail in substorm phenomena and in the overall magnetospheric energy balance and relate these phenomena to external triggering mechanisms"]
-[5.922854900360107, 2.9926233291625977, "[FF] Project Priority of the UNITEC-1 = Safety and simplicity"]
-[8.706392288208008, 5.500525951385498, "[TT] Landing Accuracy of the Autonomous spaceport drone ship = Within 10 m"]
-[9.066303253173828, 3.8342607021331787, "[FF] Testing of the MEMS solar sensor = For satellite applications"]
-[5.850651264190674, -0.7636944055557251, "[FF] Lifetime of the MetOp-B = Unknown"]
-[5.190467834472656, 5.681955337524414, "[TT] Purpose of the Dynamic Source Routing = Routing in the network layer protocol"]
-[7.878633975982666, 3.138200283050537, "[TT] Absorption at 1.42 \u00b5m of the Carbon Dioxide (CO2) = 10 -22 mol cm -2"]
-[7.47429084777832, 6.224363327026367, "[TT] Timing Precision of the NICER = < 100 ns"]
-[12.192764282226562, -0.25745856761932373, "[TT] Data Transmission Frequency of the TESS = Every two weeks"]
-[5.17600154876709, 0.7810853719711304, "[FF] Date of the Data Distribution Policy Agreement = 2008"]
-[8.934477806091309, 6.540229320526123, "[TT] Imaging System of the CaSSIS = Color and Stereo Surface Imaging System"]
-[7.89649772644043, 6.445982456207275, "[FF] Time of Image Acquisition of the Advanced Baseline Imager (ABI) = 1:20 p.m. Eastern Standard Time (17:20 Universal Time)"]
-[9.993314743041992, 4.361237525939941, "[TT] Quantity of the Magnetic torquers = 3"]
-[3.9212424755096436, 9.738897323608398, "[TT] Bandwidth (GHz) of the ICI-2 = 3"]
-[7.278132915496826, 6.377171039581299, "[TT] Operator of the TIMED = Johns Hopkins University Applied Physics Laboratory (JHU/APL)"]
-[9.435327529907227, 7.000338077545166, "[TT] Resolution of the SMOS = 100 m"]
-[10.369213104248047, 2.0405349731445312, "[TT] Number of All-Sky Surveys of the eROSITA X-ray telescope = 8"]
-[8.666326522827148, 3.154967784881592, "[FF] Image Processing of the NASA's Solar Dynamics Observatory = Reduce noise"]
-[3.434891939163208, -0.9233130812644958, "[TT] Orbit Type of the FASat-Alfa = Sun-synchronous near-circular orbit"]
-[2.549335479736328, 0.16151432693004608, "[TT] Pulse period (ms) of the B1617-155 (Sco X-1) = 3.200"]
-[10.225003242492676, 1.7943174839019775, "[FF] Science Goals of the NuSTAR = Mapping of the central regions of our Milky Way galaxy, studying the remnants of exploded stars in our galaxy, and surveys of several well-studied extragalactic fields"]
-[7.480664253234863, 3.021425724029541, "[TT] Detection Threshold of the MethaneSAT = At least 10 times more sensitive than the current GHGSat satellite"]
-[9.286239624023438, 6.3050994873046875, "[TT] TFOV of the Scan mechanism assembly = \u00b113\u00ba in the E-W and \u00b110\u00ba in the N-S direction"]
-[7.0606207847595215, 4.76668119430542, "[FF] Electrical Interfaces of the AMS-02 = Power, LRDL (Low Rate Data Link), HRDL (High Rate Data Link)"]
-[4.5781168937683105, 0.5369454622268677, "[TT] Launch Date of the CIMON-2 = 5 December 2019"]
-[7.922886371612549, -0.40924882888793945, "[TT] Time Period of the Sea Ice Extent = 1981-2010"]
-[7.421472549438477, 8.498259544372559, "[TT] Spectral Sensitivity (Minimum Detectable Photon Radiance) of the SXI = 7, 132 photon cm -2  arcsec -2  s -1"]
-[4.383622169494629, 7.761702060699463, "[TT] Downlink Frequency of the TT&C = 2.2 GHz"]
-[6.028174877166748, 0.05450166016817093, "[TT] Mission Duration of the IBEX = Seven years"]
-[6.078899383544922, 2.0457189083099365, "[FF] Purpose of the Advance Power Technology Experiment = Provide advance power technology for the Starshine 3 Satellite"]
-[6.074774742126465, 1.6643238067626953, "[FF] Symposium Date of the SWOT Mission = Sept. 24-29, 2012"]
-[13.460922241210938, 7.438660621643066, "[TT] Power of the COPS = 1077 W"]
-[6.06570291519165, 1.910093903541565, "[TT] Habitable Zone Status of the TOI 700 d = Confirmed"]
-[13.882709503173828, 5.665482997894287, "[TT] Nominal Efficiency of the Solar Cell Experiment = 21%"]
-[7.262254238128662, -0.23103547096252441, "[TT] Orbit Period of the G\u00f6kt\u00fcrk-2 = 98.3 minutes"]
-[6.9671502113342285, 6.323085784912109, "[TT] Number of Feeds of the MBA = 19"]
-[4.788443565368652, -1.8786879777908325, "[TT] Number of Lunar Landings of the Chang'e-5 = 3"]
-[6.780849933624268, 8.48189926147461, "[FF] SNR @Lref [BOL] of the Spectral Channel = 211-390"]
-[5.14681339263916, 7.585362911224365, "[TT] G/T of the Reception Station = 22.7 dB/K"]
-[4.828396797180176, 8.54964828491211, "[TT] Center Frequency of the Channel 9 = 53.30 GHz"]
-[9.669617652893066, 0.2791380286216736, "[TT] Inter Satellite Distance of the PROBA-3 = About 150 m"]
-[12.152946472167969, 3.6987714767456055, "[TT] Maximum Temperature of the Xenon Gas Tank = 50\u00baC"]
-[5.635156631469727, 3.149432420730591, "[TT] Contract Award of the York Space = $382 million"]
-[9.449003219604492, 4.180758953094482, "[TT] Noise Level at 1 Hz of the Field Measurement Device = \u2264 10 pT Hz -1/2"]
-[9.531240463256836, 2.8808796405792236, "[TT] Position of the Inmarsat S \u2013 Europasat / Hellas-Sat 3 = 39\u00b0 East"]
-[7.649254322052002, 8.76798152923584, "[TT] Channel Wavelength of the SAM-II = 0.98-1.02 \u00b5m"]
-[5.022170543670654, 1.8145302534103394, "[TT] Operating Status of the Envisat = Nominal"]
-[6.079873085021973, 3.3663489818573, "[FF] Not Selected for Development of the Daedalus = Due to the strict adherence to the cost constraints established by the PB-EO"]
-[10.12267780303955, 1.4659521579742432, "[FF] Typical Number of Stars of the Young Moving Groups = Only a few tens of stars"]
-[4.828351974487305, -1.806506872177124, "[TT] Mission Duration of the Chang'e-4 = 2019"]
-[4.383589267730713, 0.11582069844007492, "[TT] Starlink Satellites Launch Date of the SpaceX = 11 March 2021"]
-[3.915053606033325, 7.884401321411133, "[TT] Data Format of the Optical link = 1064 nm, BPSK (Bi-Phase Shift Keying) modulated, homodyne"]
-[6.832955837249756, -0.5670361518859863, "[FF] Orbit of the ISS = Diurnal and sub-diurnal cycles"]
-[5.35201358795166, 2.6687374114990234, "[TT] Integration Location of the LightSail-2 = Air Force Research Laboratory (AFRL) in Albuquerque, New Mexico"]
-[6.797872543334961, -0.34600600600242615, "[TT] Ground Station Passes of the Astro Digital Satellites = 11 minutes"]
-[5.996433734893799, -0.06830571591854095, "[TT] Duration of Human Presence of the International Space Station = More than 18 years"]
-[6.998643398284912, 4.482560634613037, "[FF] Complement of the MWR = Unknown"]
-[4.770845413208008, -1.137615442276001, "[FF] Orbit Reach Date of the Shenzhou-13 = 15 October 2021"]
-[5.622608661651611, 2.2432305812835693, "[TT] Alignment Requirement of the SPIDER = Not required"]
-[6.632296085357666, 4.448485374450684, "[FF] Qualification and Test Activity of the Taurus Frangible Joint System = Based on the results of an extensive failure analysis (for example, detailed fault tree or failure mode analysis) and with consideration for the environments in which the joint is operated"]
-[9.610201835632324, 0.7298403382301331, "[TT] Moving Target Distance of the EDRS-A = Up to 45 000 km"]
-[4.772249698638916, 1.4864681959152222, "[FF] Debut Date of the Opti-SAR = Unknown"]
-[6.9307026863098145, -1.7615588903427124, "[FF] Globally Averaged Sea Level Measurement Goal of the Jason-3 = Zero bias \u00b11 mm (standard error)"]
-[5.602484226226807, 3.5554897785186768, "[TT] Platform of the DSX = ESPA (EELV Secondary Payload Adapter)"]
-[6.736979007720947, 2.1330204010009766, "[FF] Data Collection of the ASTRO-H = Gas dynamics, particle acceleration, maximum energy of the accelerated particles"]
-[14.52867317199707, 6.565263748168945, "[TT] Battery Depth of Discharge of the RADARSAT-2 = Less than 10% of the battery capacity"]
-[5.957352161407471, 3.4409971237182617, "[FF] SSBUV Instrumentation Flights of the Space Shuttle = Multiple"]
-[7.640634536743164, 8.497920989990234, "[TT] Number of Bands of the CIRiS = 3"]
-[9.68532943725586, 8.370701789855957, "[TT] Field-of-View (FOV) Defining Apertures of the TR = 2"]
-[4.76967191696167, 7.941634654998779, "[TT] Time-Delay Resolution of the Linear FM Transmitter = 3.125 ns"]
-[6.312363147735596, -0.4248111844062805, "[TT] Onboard Autonomy of the F-15 and F-16 DMSP satellites = 60 days"]
-[9.847471237182617, -0.6476719975471497, "[TT] Orbit Altitude of the SAR/Galileo VOV-3, IOV-4 = 23,222 km"]
-[2.0671305656433105, -0.30170705914497375, "[FF] URL of the Van Allen Probes = http://www.nasa.gov/feature/goddard/2016/nasa-s van-allen-probes-revolutionize-view-of-radiation-belts"]
-[7.762504577636719, 1.7636218070983887, "[FF] Response to Global Climate Changes of the Coral Reefs = Increased sea surface temperature (SST), ultraviolet radiation (UV) and acidification of seawater"]
-[13.761616706848145, 3.0887975692749023, "[TT] Payload Mass of the STS-85 = 11,200 kg"]
-[7.648031234741211, 6.931001663208008, "[TT] Operation Mode of the CCDs = Frame-transfer mode"]
-[4.767922878265381, -1.743569254875183, "[TT] End of Life Date of the Chang'e-2 = 2029"]
-[5.706413745880127, 7.005161762237549, "[TT] Information Rate of the DPU = 300 Mbit/s"]
-[11.142489433288574, 5.935610771179199, "[TT] Baffle Material of the TX Telescope = CFRP"]
-[5.965129852294922, 4.750665187835693, "[FF] Purpose of the Ground Station = Send commands or receive data"]
-[6.271670818328857, 0.35469385981559753, "[TT] Lifetime of the ROSE-L Mission = 7.5 years"]
-[6.607916355133057, -0.6012800335884094, "[TT] Mission Period of the Corvus-BC 3 = 3 minutes"]
-[9.837047576904297, -0.36398693919181824, "[TT] Altitude Range of the LEO Altitudes = 150 km to 800 km"]
-[8.661245346069336, 6.700488567352295, "[FF] Cadence of Images of the OSIRIS Narrow Angle and Wide Angle Cameras = Increased in each observation"]
-[5.60606050491333, 0.2567497789859772, "[TT] Installation Date of the ISS-RapidScat = October 6, 2014"]
-[9.314797401428223, 6.343269348144531, "[TT] Scan Pattern of the Sensor = Conical at 45\u00ba from nadir"]
-[7.077669143676758, 1.2539353370666504, "[FF] News Release Date of the Spitzer Space Telescope = 19 December 2019"]
-[7.4514479637146, 3.2479259967803955, "[FF] Ability of the GHGSat = Pinpoint the source of even small leaks"]
-[6.1347198486328125, 3.1487069129943848, "[TT] Bus Integration and Testing Location of the Neutron-1 = Hawaii Space Flight Laboratory (HSFL)"]
-[7.636630058288574, 9.056674003601074, "[TT] Spectral Range (\u00b5m) of the Band 7 = 0.43 - 0.48"]
-[6.3510918617248535, 4.340338230133057, "[FF] Operational Parameters of the ICPS = Data needed for the secondary payload deployment system avionics unit to perform the correct skit for the mission based on trip time to the moon and when the payloads need to be deployed"]
-[7.068778991699219, 5.900949954986572, "[TT] Time Uncertainty of the Deep Space Atomic Clock = One nanosecond"]
-[6.940108299255371, -0.7517374753952026, "[TT] Orbit Period of the S/C = 6.2 years"]
-[7.46945333480835, 3.5659053325653076, "[TT] Number of Atmospheric Occultations of the GNOS-2 = Less than 1000 per day"]
-[7.706491947174072, 5.845962047576904, "[FF] Components of the Interactive Operation Mode = Video camera mode"]
-[10.128499984741211, 6.8557209968566895, "[TT] Ground Track of the Orbit = \u00b1 2 km"]
-[9.121118545532227, 5.175765037536621, "[TT] Minimum Elevation Horizon Mask of the Panama ground station = 3\u00ba"]
-[3.8224220275878906, 4.446959018707275, "[FF] Definitive Orbits of the RADARSAT-2 = To be made available routinely for SAR data processing"]
-[5.324357986450195, 1.350205898284912, "[FF] Instrument Installation Start Date of the GOES-R Series Weather Satellite = July 30, 2014"]
-[6.164243221282959, 3.1432249546051025, "[TT] Revenue Forecast for 2021 of the BlackSky = $30 to $34 million"]
-[13.651615142822266, 5.826822280883789, "[TT] Power Output of the Solar Panel = 1164 W"]
-[5.937918663024902, 1.629170536994934, "[FF] Presentation Date of the MEIDEX = June 9-13, 2003"]
-[13.27172565460205, 2.9269206523895264, "[TT] Mass of the 3U CubeSat = ~5 kg"]
-[8.01956844329834, 2.0105926990509033, "[FF] Altitude of the FY-3 (FengYun-3) = +105"]
-[10.948253631591797, 5.099440097808838, "[TT] No of CCRs of the LARES-2 = 303"]
-[6.435410022735596, 3.7128121852874756, "[TT] Requirement of the RV and FF experiments = Totally complementary, without duplicating effort and results"]
-[5.3478803634643555, 4.000775337219238, "[TT] Number of Satellites in Payload of the Starshine-3 = 4"]
-[10.080231666564941, 5.429542064666748, "[FF] Objectives of the ACC = Better thermal stability, Improvement of thermal characterization, On-ground characterization of differential bias and scale factor"]
-[4.81906795501709, 7.243656158447266, "[FF] Communication Configuration of the CanX-2 = UHF in uplink and the S-band in downlink"]
-[13.384773254394531, 6.882004261016846, "[TT] Payload Power of the Spacecraft = 40 W"]
-[11.89200496673584, -0.07888438552618027, "[TT] Target Stars Distance of the TESS = Less than 300 light-years"]
-[7.1461663246154785, 3.5029263496398926, "[TT] Purpose of the OPS = Earth observation"]
-[6.785849571228027, 1.773526668548584, "[FF] URL of the MEOSAR = http://tinyurl.com/k82lepc"]
-[10.964022636413574, 4.031879901885986, "[TT] Sail Shape of the Drag Sail Modules = Trapezoidal"]
-[5.612105369567871, 6.771815299987793, "[TT] Upload Frequency of the IXPE = Once every three days"]
-[5.643048286437988, 6.781416893005371, "[FF] Data Rate Adjustment of the Electra = Can maximize data volume by actively adjusting the data rate to be slower when the orbiter is near the horizon from the surface robot's perspective, faster when it is overhead"]
-[6.698901653289795, 4.216481685638428, "[FF] Equipment Modules of the Terra = Populated on the zenith face of the spacecraft"]
-[12.148673057556152, 4.5795674324035645, "[TT] Spacecraft Bus Size of the QuickBird-2 = 3 m x 1.6 m \u00d8"]
-[7.615273475646973, 1.9896366596221924, "[FF] Potential Data of the Tandem-L = Forest height, structure, and biomass"]
-[8.157999992370605, 3.6530158519744873, "[FF] Components of the OCO-2 MIP = Four different transport models with varying configurations, multiple different data assimilation frameworks, and diverse prior fluxes and uncertainties"]
-[5.311800003051758, 6.648774147033691, "[TT] Daily Data Collection of the TRACE spacecraft = About 700 MByte"]
-[5.34363317489624, 0.9032225012779236, "[FF] Evaluation Date of the Evaluation = 8 December 2021"]
-[8.149102210998535, 8.449219703674316, "[TT] Band-to-Band Registration of the WPM = < 5.2 \u00b5m"]
-[13.635456085205078, 7.022982120513916, "[TT] Power of the EPS = 3 W (paddles closed), 5.9 W (paddles open)"]
-[7.17546272277832, 5.274616718292236, "[TT] Mounting Interface of the Active Pointing Control Mechanism = Invar ring"]
-[6.671088695526123, 0.7653636336326599, "[FF] Image of the Week Date of the Herschel = Dec. 21, 2015"]
-[11.132146835327148, 1.0881907939910889, "[TT] Development of the Telescopes = Pre-developed by ESA, NASA and the LISA consortium of ESA member states"]
-[4.717995643615723, 0.4634912610054016, "[TT] Booked for Launch Date of the SpIRIT = Early 2023"]
-[5.543465614318848, 1.4052883386611938, "[TT] Presentation Date of the AMS-02 = 2\u20139 July, 2013"]
-[14.324440956115723, 3.2780652046203613, "[TT] Mass of the LRR = 2 kg"]
-[6.37343692779541, 4.904000282287598, "[FF] Hardware of the ACS = Controlled by ACS flight software"]
-[9.65517520904541, 8.328607559204102, "[TT] FOV of the Particle Detector = \u00b121.8\u00ba"]
-[6.029738426208496, 1.8673288822174072, "[TT] Flight Test Duration of the Orion = 4.5 hours"]
-[5.772250652313232, 5.442939758300781, "[FF] Functions of the DFU = CCSDS formatting, Reed-Solomon encoding"]
-[10.863312721252441, 7.422483444213867, "[TT] Swath of the Scatterometer = 1800 km"]
-[7.455364227294922, 5.389585018157959, "[TT] Instrument of the Spacelab-1 = SOLCON-1"]
-[4.633323669433594, 6.6046462059021, "[FF] Features of the DVB-S2 standard with adaptive coding and modulation = All the DVB-S2 features have been implemented"]
-[5.520679473876953, 5.0519304275512695, "[FF] CAN Bus of the Avionics System = Distributed data interface"]
-[10.606539726257324, 2.7686209678649902, "[TT] Altitude of the 46 nanosatellites = 530 km"]
-[6.443600177764893, 0.6219337582588196, "[TT] Launch Date of the Landsat-9 = December of 2020"]
-[6.705643177032471, -0.31254270672798157, "[TT] Average Latency of the GPS Ephemerides = About 4 hours, 17 hours, 12 days"]
-[5.634519577026367, 0.7986921668052673, "[TT] Arrival Date in Europe of the ExoMars Lander Platform = March 21, 2019"]
-[9.615849494934082, 8.333174705505371, "[FF] Field of View (FOV) of the LCT = Unobstructed"]
-[4.799172878265381, 7.29824161529541, "[TT] Downlink Data Rate of the RF Communications = 16.8 Mbit/s"]
-[9.77530288696289, -0.6446627974510193, "[TT] Initial Orbit Altitude of the Bion-M1 = ~300 km"]
-[7.047939777374268, 7.2451276779174805, "[TT] Pulse Rate of the ATLAS = 10,000 pulses per second"]
-[7.190917015075684, 8.690070152282715, "[TT] Passband of the NUV channel = >159 nm"]
-[5.691182613372803, -0.40933215618133545, "[TT] Life Expectancy of the RapidEye = 6 years of operations, with full image performance for another 5 or more operational years"]
-[4.458527565002441, 7.6800312995910645, "[TT] Frequency of the VHF-band communications = 145.825 MHz"]
-[12.616880416870117, 9.092798233032227, "[TT] Revisit Time at Equator of the HyperScout\u00ae = Around 45 days"]
-[6.849759101867676, 6.200515270233154, "[TT] Type of the DBCP = Pseudo-depolarizer"]
-[11.73271369934082, 7.526400566101074, "[TT] Launch Date of the Megha Tropiques = Oct. 12, 2011"]
-[12.153196334838867, 6.117031574249268, "[TT] Cosmic Ray Events Recorded of the AMS-02 = Over 60 billion"]
-[7.534389019012451, 6.511439323425293, "[TT] Single Point Acquisition Time of the Instrument = Less than 0.3 seconds"]
-[9.279891967773438, 7.352409362792969, "[FF] Panchromatic Resolution of the EROS-C = Comparable to EROS B"]
-[9.88456916809082, 1.345108985900879, "[TT] Sky Area of the Perseus galaxy cluster = Roughly the size of two full Moons"]
-[11.594780921936035, 4.868410587310791, "[TT] Diameter of the Marman ring = 0.97 m"]
-[4.948126792907715, 3.4645893573760986, "[TT] Manufacturer of the PIC = Elbit Systems/ElOp (Electro-Optics Industries Ltd.)"]
-[7.443080902099609, 4.826116561889648, "[FF] Location of the FLGS = Not specified"]
-[7.04240608215332, 8.271074295043945, "[TT] Signal-to-Noise Ratio of the SNR in bands 1 and 2, in band 3 = \u2265 200, \u2265 100"]
-[14.297403335571289, 3.290146589279175, "[TT] Mass of the AMU = 8 kg"]
-[14.264236450195312, 3.0782546997070312, "[TT] Mass of the GEISAT Precursor = 17.4 kg"]
-[7.824731826782227, 2.137338876724243, "[FF] Purpose of the Ocean Color and Temperature Scanner = Measure ocean color and temperature"]
-[6.530449390411377, -1.2458268404006958, "[FF] Science Data Collection of the GRACE-FO = Nearly continuous"]
-[8.057305335998535, 1.9084128141403198, "[TT] Spatial Resolution of the Coastal Zone Scanner = 80 m"]
-[8.032818794250488, 4.020554542541504, "[FF] Design Requirement 1 of the OCO-3 PMA = Allow quick movement through a large range of angles"]
-[4.673469066619873, 3.209700345993042, "[TT] Manufacturer of the SES-17 = Thales Alenia Space"]
-[14.072365760803223, 7.088133811950684, "[TT] Output Voltage Levels of the CS-XUEPS2-41 = 3.3, 5, or 12 V"]
-[6.848891735076904, 5.801323890686035, "[TT] Quantity of the Fragments = In excess of 115 k"]
-[7.517374038696289, 3.72556471824646, "[FF] Selection Criteria of the Hexapod = Lifetime and lubrication tests"]
-[7.5887556076049805, 8.818828582763672, "[TT] Typical Radiance of the COCTS = 41.1 mW/cm2 \u00b5m sr"]
-[5.522812366485596, 0.588374674320221, "[FF] Configuration Change of the NIRISS = Summer of 2011"]
-[8.274272918701172, 5.3167877197265625, "[TT] Calibration Status of the Satellite = Calibrated"]
-[7.543806076049805, 8.61831283569336, "[TT] Number of Spectral Bands of the Instrument = Up to 200"]
-[6.284997463226318, 8.0994234085083, "[TT] Number of Channels of the SMMR = 10"]
-[3.5080997943878174, 4.799905776977539, "[FF] Operating Modes of the RISAT-1 = SAR operating modes, including Sliding Spotlight mode"]
-[9.201921463012695, 0.05057257413864136, "[TT] Height of the Tvashtar Volcano Plume = 290 km (180 miles)"]
-[4.943264484405518, 6.05911922454834, "[TT] Link Loss Behavior of the LLITED satellites = Try up to 3 seconds to complete the last packet transmitted"]
-[4.911482334136963, 0.34028512239456177, "[FF] Presentation Date of the CXBN-2 = April 22-24, 2015"]
-[8.41203784942627, -0.6417832970619202, "[TT] Height of the Iceberg A-76 = About 35 meters (100 feet) above sea level"]
-[7.987008571624756, 0.2085307389497757, "[FF] Method of the GRACE and GRACE-FO = Tease out the gravitational signal associated with the movement of water by evapotranspiration"]
-[8.592537879943848, 0.14379723370075226, "[TT] Size of the Comets = Roughly 5 km"]
-[7.839219570159912, 2.438133478164673, "[FF] Impact of the South Atlantic Anomaly = Allows charged particles to dip closer to the surface than normal"]
-[8.096155166625977, 5.749453067779541, "[TT] Calibration Source of the LISS-3 camera = LEDs (1.55 \u00b5m)"]
-[6.780701160430908, -0.5936747193336487, "[TT] Observation Time of the Tri-TIP = Night-side portion of the orbit"]
-[5.746582508087158, 4.379650115966797, "[FF] Configurations of the SATSIM = GAS, SATLAB"]
-[6.5066633224487305, 0.07093033194541931, "[TT] Revisit Times of the Constellation = Few hours or less"]
-[8.71981430053711, -0.2623348832130432, "[TT] Apogee (km) of the Meteor-1-2 = 690"]
-[8.011493682861328, 2.238738536834717, "[FF] Purpose of the FY-2 = Cloud profile and rain radars"]
-[9.01128101348877, 0.4015973210334778, "[TT] Diameter of the Haydn crater = 251 km"]
-[6.519373893737793, 3.166393756866455, "[FF] Concept and International Collaboration of the Chinese Environment and Disaster Monitoring Satellite System (EDMSS) = UNESCAP Meeting, Bangkok, Thailand, June 22-24, 2005"]
-[3.8271169662475586, 0.8658757209777832, "[TT] Launch Date of the PSLV-C38 = June 23, 2017"]
-[4.590748310089111, 4.7750163078308105, "[FF] Purpose of the Proof-of-Concept Prototype = Test future options for maritime autonomous vessel navigation"]
-[8.487460136413574, 8.414448738098145, "[TT] Resolving Power of the Spectrometers = 3 x 10^5 for the narrowband ones"]
-[9.569990158081055, 4.733575820922852, "[FF] Function of the Y-axis aligned reaction wheel = Absorb the angular momentum of the spinning satellite"]
-[10.361376762390137, 5.516785144805908, "[TT] Cooler of the Astro-APS = Peltier cooler"]
-[8.97706413269043, 7.092826843261719, "[TT] Optical Axis of the Metric Camera = Vertically down to the Earth's surface"]
-[6.498223304748535, 4.69533109664917, "[FF] Function of the ICPS = Image Collection Planning"]
-[8.524316787719727, 8.295445442199707, "[TT] Spectral Resolution of the Instrument = FWHM (Full Width Half Maximum) 0.5 cm -1"]
-[9.634783744812012, -0.3715965747833252, "[TT] Altitude of the Tatiana-2 = 825 km"]
-[4.926401615142822, 1.3346059322357178, "[TT] Switched On Date of the MIRAS = Nov. 17, 2009"]
-[4.529991626739502, 6.207767486572266, "[TT] Beacon Transmission Frequency of the ELFIN-A = 437.450 MHz"]
-[7.423255443572998, 4.526304721832275, "[FF] Objective of the Guidance = Provide the appropriate references to ensure that the S/C follow the nominal trajectory profile for the RVX"]
-[9.310432434082031, 4.878528118133545, "[TT] Safe Mode Attitude of the AOCS = Earth-oriented"]
-[4.9631171226501465, 3.414583444595337, "[TT] Manufacturer of the EXObox = Exolaunch"]
-[7.697608470916748, 2.3532700538635254, "[FF] Operation Focus of the CFTP = Recording SEEs near the SAA (South Atlantic Anomaly)"]
-[10.15104866027832, 3.212559223175049, "[FF] Measurement Frequency of the TROPICS CubeSat = Higher than previous satellites"]
-[4.7794365882873535, 3.03955340385437, "[TT] Owner of the SAOCOM constellation = CONAE (Comision Nacional de Actividades Espaciales)"]
-[6.3416032791137695, 2.9309422969818115, "[TT] Satellite of the MODIS = NASA\u2019s Terra"]
-[12.016708374023438, -0.15997707843780518, "[FF] Ground Station Contribution of the TESS-L5 = Significant private contribution"]
-[6.299189567565918, 3.8969886302948, "[FF] Objective of the OTV = ADR mission scenarios"]
-[5.040033340454102, 1.2219163179397583, "[FF] Date of the GIOVE Signal and Sensor Station = Sept. 22-25, 2009"]
-[10.33435344696045, 5.467415809631348, "[TT] Corona Temperature of the Sun = On average 1 million degrees Celsius"]
-[9.917613983154297, 8.1138277053833, "[TT] Optics Unit Focal Length of the Imager = 10.5 cm"]
-[7.711967945098877, 1.4139410257339478, "[FF] Mission of the ROSE-L = Environmental monitoring, land management, ocean monitoring"]
-[7.407344341278076, 6.928247928619385, "[TT] Laser Footprint Spacing of the SLA sensor package = 700 m"]
-[6.45961856842041, 1.4616039991378784, "[FF] Purpose of the COSMO-SkyMed = Military and civil (research and commercial) data use"]
-[14.237479209899902, 3.048375129699707, "[TT] Mass of the Sterkh-2 = ~ 171 kg"]
-[6.138359546661377, 5.201300144195557, "[TT] Features of the INSPIRE-2 = m-NLP"]
-[8.362146377563477, 8.239532470703125, "[FF] Dimensions of the Data Cube = samples_wide X number of spectral_data_lines X number_of_frames"]
-[6.792803764343262, -0.7597721219062805, "[TT] Time in Halo Orbit of the S/C = About 2 years"]
-[5.135120868682861, 2.3268535137176514, "[TT] Heritage of the OMPS = SBUV/2, TOMS and GOME"]
-[9.169838905334473, 8.549507141113281, "[TT] Wavelength of the Lens 6 = 1.64 \u00b5m @ 120\u00ba"]
-[4.389228343963623, 0.6691762208938599, "[TT] Launch Date of the DMSP-20 = Aug. 23, 1962"]
-[5.390735149383545, 6.898508071899414, "[TT] Peak Detection Rate of the Complex Receiver = 19 Messages/s"]
-[5.252163887023926, 1.899970293045044, "[TT] Mission Status of the EO-1 = Operational"]
-[8.262219429016113, 8.13590145111084, "[TT] Scan Lines of the Visible Spectral Band = 2500 x 4"]
-[4.799817085266113, 0.8819831013679504, "[FF] Launch Date of the PROBA-V-CC = October 9, 2023"]
-[8.7865629196167, 9.404860496520996, "[TT] Bands of the TANSO-CAI-2 = Forward- and backward-looking bands (\u00b120\u00ba)"]
-[8.015482902526855, 8.511812210083008, "[TT] Number of Bands of the VNIR = 40"]
-[9.67000961303711, -0.6644245982170105, "[TT] Orbit Altitude of the Dragon = ~ 400 km"]
-[7.770803451538086, 4.5514397621154785, "[FF] Performance of the AMS-02 transition radiation detector = Unknown"]
-[5.640366077423096, 8.762473106384277, "[TT] Filter Bandwidth of the MCE = 10 nm FWHM"]
-[5.707090377807617, 0.6175134778022766, "[TT] Days of data collection of the VIRR = 94.2"]
-[7.333564281463623, 4.61025333404541, "[FF] Function of the S/C Guidance (GNC-GDC) = Computes the attitude profiles to be followed by the spacecraft"]
-[6.27902889251709, 2.2173593044281006, "[FF] Principal Investigator of the SEOPS-PGTIDE (P&G Tide in Space) = Dr. Mark Sivik"]
-[8.328777313232422, 1.2348535060882568, "[TT] Pulse Repetition Interval of the RainCube = 1660 \u00b5s"]
-[6.500398635864258, 4.577737808227539, "[FF] Function of the Satellite Management Unit = Provides both the command and control of the spacecraft and the attitude and orbit control functions"]
-[13.82022476196289, 6.7201247215271, "[TT] Power Source of the Distress Transmitters = Low-powered battery"]
-[9.208356857299805, 3.851057291030884, "[FF] Function of the SADE (Solar Array Drive Electronics) = Process signals from sun sensors and control the array drive motor speed"]
-[4.2738037109375, 2.628357410430908, "[TT] Launch Site of the STPSat-3 = MARS (Mid-Atlantic Regional Spaceport)"]
-[11.168391227722168, 6.08366060256958, "[TT] Number of the Graphite Spacers = 5 per glass segment"]
-[6.344573974609375, 5.566068172454834, "[TT] Function of the CDS = Controls the overall operation of the instrument"]
-[7.930368900299072, 5.660918712615967, "[FF] VBN Demonstration of the DSAT-3 = Capturing images of DSAT-3 from various distances and over large duration"]
-[10.168992042541504, 5.401001453399658, "[FF] Design Changes of the ABI loop heat pipes = Address thermal control issues detected on GOES-16 and -17"]
-[3.37121844291687, 1.449670433998108, "[TT] Launch Date of the Sentinel-2A = June 23, 2015"]
-[11.352075576782227, 2.7673981189727783, "[TT] Cables, Connectors Mass of the Microsatellite = 5.1 kg"]
-[10.122326850891113, 1.685918927192688, "[FF] Science Objectives of the IMAP = LISM (Local Inter-Stellar Medium) Properties and Composition"]
-[13.405313491821289, 2.9390177726745605, "[FF] Mass of the PolySat-1, -2 = Unknown"]
-[5.319321155548096, 6.9172773361206055, "[FF] Global Average Detection Rate of the Simple Receiver = 2 to 3 Messages/s"]
-[7.79134464263916, 2.945913553237915, "[FF] Mission of the MicroCarb = MicroCarb mission: a CNES initiative for monitoring the CO2 exchanges"]
-[6.300873279571533, 2.676518678665161, "[TT] Institute of the DAXSS = LASP (Laboratory for Atmospheric and Space Physics)"]
-[7.464702129364014, 8.7933349609375, "[TT] Passband of the VIS = 550-900 nm"]
-[3.2696855068206787, 5.00944709777832, "[TT] Mode of the SAR Sensor Subsystem = WS (Wide Swath)"]
-[8.302558898925781, 7.730077743530273, "[TT] Number of Detectors of the Spectrometer = 4"]
-[9.164884567260742, 7.493372440338135, "[TT] Camera Resolution of the DMSP Block 4 = 1.5 km at image center to about 5.5 km at the edge of a picture"]
-[7.240346431732178, 4.48984432220459, "[TT] Information Source of the VBS = RVX (RendezVous Experiment)"]
-[5.568765640258789, 2.7469468116760254, "[FF] Consortia of the Moonlight = Telespazio leads the first consortium"]
-[6.455845832824707, 4.127760887145996, "[FF] Design of the SWiPS = Compact"]
-[5.3677544593811035, 4.946380138397217, "[FF] On-board Receivers of the Sentinel-3 = Two GPS Receivers, LRR, DORIS"]
-[5.0833845138549805, 1.1791081428527832, "[FF] Presentation Date of the UniSat-3 = July 27, 2005"]
-[11.397892951965332, 4.384607315063477, "[TT] Size of the Alpha = 1U"]
-[3.8805747032165527, 1.974973440170288, "[TT] New Launch Vehicle of the GRACE-FO = Falcon-9 rocket"]
-[9.272634506225586, 5.147329330444336, "[TT] Yaw Maneuver Capability of the ADCS = \u00b190\u00ba/180\u00ba"]
-[7.184023380279541, 5.433567047119141, "[TT] Mode of the VBS = Cooperative and non-cooperative"]
-[3.624134063720703, 6.5343708992004395, "[TT] Mirror Type of the Short Wavelength Band = Off-axis parabolic cylinder"]
-[8.653410911560059, 7.694055080413818, "[TT] Pixel Size of the Detector Array = 13.5 \u00b5m"]
-[4.465360641479492, 7.876785755157471, "[TT] Uplink Frequency of the TT&C Data = 2089 MHz"]
-[8.191512107849121, 8.263540267944336, "[TT] Sensitivity of the Spectrometers = Detect concentrations as low as two parts per billion"]
-[7.65911865234375, 0.23293842375278473, "[TT] Critical Design Review End Date of the Lucy = Oct. 18"]
-[10.09521770477295, -2.7378737926483154, "[FF] Launch Date of the SLC NAND-Flash = Unknown"]
-[14.306760787963867, 3.180746078491211, "[TT] Mass of the CPD = 2.3 kg"]
-[4.745061874389648, -0.4163304567337036, "[TT] Docking Time of the Soyuz MS-17 = Three hours later"]
-[9.665872573852539, 8.357928276062012, "[TT] FOV of the GLI = \u00b143\u00b0"]
-[12.076570510864258, 3.1631691455841064, "[TT] Propellant of the NanoPS = Sulfur hexafluoride (SF6)"]
-[6.07286262512207, 2.4167821407318115, "[TT] Directing Entity of the New Horizons = Southwest Research Institute"]
-[8.1740083694458, 7.467922210693359, "[TT] CCD Detector of the PS0 = 11MP"]
-[11.482261657714844, 3.7118146419525146, "[TT] Firing Duration of the CUS = Approximately 720 seconds"]
-[5.1270365715026855, 2.1688249111175537, "[TT] Operator of the ITASat-1 = ITA ground team in S\u00e3o Jos\u00e9 dos Campos"]
-[3.5554568767547607, 1.984610915184021, "[TT] Mission of the OLCI = Sentinel-3"]
-[13.766152381896973, 2.9673678874969482, "[TT] Payload Mass of the ADEOS = 1300 kg"]
-[5.316799163818359, 1.5696032047271729, "[FF] Partner of the ELSA-d = SSTL"]
-[8.64172077178955, 2.7031338214874268, "[FF] Measurement Proxy of the ClO = Dynamical effects on the high-latitude upper stratosphere"]
-[4.790307998657227, 3.1584460735321045, "[TT] Manufacturer of the Sentinel-2A = Airbus DS"]
-[10.326517105102539, 5.794916152954102, "[FF] Problem of the NISP = Stopped working in a cold vacuum state"]
-[9.763496398925781, 8.50445556640625, "[TT] EW FOV: max FPM of the AHI = 33,203 \u00b5rad"]
-[7.592883586883545, 8.868403434753418, "[TT] Radiometric Accuracy of the Spectral Band C = 3"]
-[4.321655750274658, 2.8891427516937256, "[TT] Tracking Station Location of the HTV-7 = Guam"]
-[9.983809471130371, -0.5032921433448792, "[TT] Orbit Altitude of the GHGSat-C2 (Hugo) = 560 km"]
-[4.7140583992004395, 7.3962907791137695, "[TT] Data Rate of the X-band transmitter = 800 Mbit/s"]
-[5.456146240234375, 0.3672446608543396, "[FF] Operating Date of the ISS ship-tracker = Aug. 26, 2010"]
-[10.08307933807373, 7.718984127044678, "[TT] Offset Pointing of the Telescope = Disk center \u00b11\u00ba"]
-[4.251175880432129, 2.5480146408081055, "[TT] Launch Site of the NPP = VAFB, CA"]
-[5.900683879852295, 2.132765054702759, "[FF] Number of the Columbus ESA ISS Science & System = 79"]
-[7.772793292999268, -0.38159433007240295, "[TT] Age of the Ice = 0-100"]
-[4.068897724151611, 3.471766471862793, "[TT] Agency of the Galileo = ESA"]
-[4.2990522384643555, 7.283596038818359, "[TT] Downlink Frequency of the ABEX Telemetry, Tracking, & Command (TT&C) subsystem = X-band"]
-[3.8566598892211914, 6.530155658721924, "[TT] Type of the VHF receiving antenna = Dipole"]
-[7.995345592498779, 6.386443138122559, "[TT] Type of the OCI = Hyperspectral radiometer"]
-[6.581719398498535, 4.4746856689453125, "[FF] Function of the AutoConTM = Automated EO-1's maneuver planning and formation control"]
-[7.687498569488525, 6.944969177246094, "[TT] Detection Capability of the MEOSAR = Near-instantaneous"]
-[9.725740432739258, 8.316341400146484, "[TT] FOV Angle of the Lenses = 2.7\u00ba"]
-[5.865741729736328, 0.7879922389984131, "[TT] Date of Measurement of the Satellites = February 21"]
-[8.720674514770508, 0.0158332958817482, "[TT] Observation Region (Winter) of the WNISAT-1 = Northern latitude range of 40-50\u00ba"]
-[4.463383674621582, -0.02172240801155567, "[FF] Orbital Flight Test Date of the Starliner = Unknown"]
-[10.854548454284668, 6.379134178161621, "[TT] Coating Smoothness of the ART-XC's mirrors = 0.5 nanometers"]
-[7.888957977294922, 2.1016652584075928, "[TT] Main Measurement Objective of the POLDER = Ocean colour"]
-[5.2086615562438965, 3.438432455062866, "[TT] Owner of the Hosted Payload = German Federal Ministry of Defense (BMVg)"]
-[10.020960807800293, 2.8144619464874268, "[FF] CubeSat Deployment of the Cygnus = Three CubeSats via the NanoRacks External Cygnus Deployer at two different altitudes and two CubeSats from the Slingshot CubeSat Deployer System"]
-[5.642777442932129, -0.8128870725631714, "[TT] Design Life of the GOSAT-2 = Five years"]
-[7.233331680297852, 8.848708152770996, "[TT] Axial Ratio of the NAVANT = < 0.6 dB at low band, and < 0.7 dB at high band"]
-[4.889557361602783, 3.0687780380249023, "[TT] Prime Contractor of the EDRS-C = Airbus"]
-[4.834654808044434, 4.309251308441162, "[FF] Unknown of the Argos-3 = Unknown"]
-[11.620523452758789, 3.4109137058258057, "[TT] Propulsion of the EUTELSAT KONNECT = All-electric"]
-[5.672967433929443, 7.11135196685791, "[TT] Data Rate of the Data rate = 800, 400, or 200 Mbit/s"]
-[6.109824180603027, 1.118537425994873, "[FF] Public Data Availability of the NuSTAR = Aug. 29, 2013"]
-[5.933959007263184, -0.18638676404953003, "[TT] Operation Period of the S-193 = Over 600 days"]
-[7.00672721862793, 7.510297775268555, "[FF] 3dB Beam Width of the Instrument = 1.8\u00ba, 1.2\u00ba, 0.65\u00ba, 0.75\u00ba, 0.35\u00ba, 0.25\u00ba, 0.25\u00ba, 0.15\u00ba, 0.15\u00ba"]
-[3.776211738586426, 6.461710453033447, "[TT] Antenna Shape of the Satellite = Umbrella"]
-[9.866637229919434, -0.2590298354625702, "[TT] Altitude of the ALL-STAR-1 = ~350-400 km"]
-[9.268865585327148, 1.7558895349502563, "[TT] Firing Speed of the Harpoon = 20 m/s"]
-[6.416865348815918, 2.040259838104248, "[FF] URL of the ARTEMIS satellite = http://telecom.esa.int/telecom/www/object/index.cfm?fobjectid=31816"]
-[4.464808940887451, 2.686789035797119, "[TT] Imagery of the DubaiSat-1 = Panchromatic and multispectral"]
-[10.317861557006836, 5.857199192047119, "[TT] Operating Temperature of the MWIR = 80 K"]
-[5.750895977020264, 2.0889625549316406, "[TT] Technology Readiness Levels of the KaRIn = 3 to 5"]
-[4.785372257232666, 5.733829498291016, "[TT] Frequency (MHz) of the GPS L1 C/A = 1575.42"]
-[6.320706844329834, -0.3659406006336212, "[TT] Revisit time of the FTS = 3 days"]
-[13.360221862792969, 7.398710250854492, "[TT] Power of the Transponder = 5 W"]
-[9.776323318481445, 4.2107391357421875, "[TT] Placement of the Magnetorquers = 2 on x, 2 on y, and 1 on z-axis"]
-[7.625204086303711, 9.210039138793945, "[TT] Band 3 Wavelength of the AEISS = 520 nm - 600 nm"]
-[6.776058673858643, 6.171228408813477, "[TT] Operation Mode of the LEDs = Pulse mode at higher currents"]
-[9.59831714630127, -0.07423694431781769, "[TT] Height of the Cliff = 50 m"]
-[5.982147216796875, 2.5504024028778076, "[TT] Affiliation of the Participating Scientists = Space Science Institute, Boulder, CO"]
-[4.853812217712402, 1.9643702507019043, "[FF] Symposium Date of the Universat-Tatyana-2 = Sept. 21-24, 2010"]
-[7.566661834716797, 5.5629496574401855, "[FF] Interferometric Radiometer of the SMOS = L-band"]
-[8.103632926940918, -1.098075270652771, "[FF] Surface Wave Structure of the ICESat-2 = Unknown"]
-[5.645816802978516, 0.6607975363731384, "[TT] Image Date of the TRACE = Nov. 6, 1999"]
-[6.1765923500061035, 4.870693206787109, "[FF] Function of the TMTC Interface = Telemetry and telecommand interface"]
-[5.971388339996338, 1.4496865272521973, "[TT] Period of Performance of the Joint Polar Satellite System Common Ground System contract = September 30, 2022"]
-[5.86721658706665, 5.017055034637451, "[FF] Architecture of the EDRS = LEO spacecraft optically uplink their data to GEO stations which feed the data via conventional Ka-band links to the ground segment"]
-[9.814879417419434, 5.53627347946167, "[FF] Temperature Correlation of the Temperature Sensors = <0.5\u00baC"]
-[12.43924331665039, 0.5781760811805725, "[TT] Mission Duration of the PLATO = 4 \u00bd years"]
-[6.009206771850586, 3.992248773574829, "[FF] Technology Demonstrator of the SIMBA Satellite = Intended"]
-[7.171874523162842, 1.235740065574646, "[TT] Discovery Date of the ExoMars Trace Gas Orbiter = February 10, 2021"]
-[9.783961296081543, -0.5867514610290527, "[TT] Orbit Altitude of the Alba Cluster 3 = 500 to 600 km"]
-[5.185181617736816, 8.124248504638672, "[TT] Frequency Range of the Electric antennas (IME) = 100 kHz - 30 MHz"]
-[7.269552707672119, 5.647215366363525, "[FF] Detection Time of the MEOLUT = Unprecedented"]
-[7.752424716949463, 5.150928020477295, "[TT] Reference Frame of the FF-N = Local Vertical Local Horizontal (LVLH)"]
-[5.739778995513916, 4.43140172958374, "[FF] Use Cases of the 3D Maps = 5G signal propagation, autonomous vehicles, smart cities and internet of things (IoT), guided munitions and disaster response planning and mitigation"]
-[6.124983787536621, 2.271479368209839, "[TT] Principal Investigator of the NuSTAR = Fiona Harrison"]
-[6.379265308380127, 4.103674411773682, "[FF] Post-Flight Analysis Recommendations of the Automated Transfer Vehicle = 130 technical recommendations"]
-[3.928624391555786, 6.702532768249512, "[TT] Band Design of the Antenna = L-band: circularly polarized dual-patch antenna, UHF-band : array of four inverted F antennas with capacitive loading"]
-[10.223587989807129, 7.551845550537109, "[TT] Telescope Type of the AGRI = Off-axis"]
-[5.385998249053955, 3.098665475845337, "[FF] Operating Capability of the Teledyne\u2019s MUSES Platform = Full"]
-[6.777839660644531, 1.912703275680542, "[FF] URL of the ICARE = http://wwwe.onecert.fr/craterre/radiation_monitors/ICARE.html"]
-[10.015130996704102, -1.5202754735946655, "[TT] Inclination of the Orbit = ~120.5\u00ba"]
-[7.043813228607178, 3.27872371673584, "[FF] Project of the Microwave Remote Sensing Small Satellite = Unknown"]
-[5.635924816131592, 1.3535082340240479, "[TT] Post-flight Inspection Date of the IXV = Autumn 2015"]
-[8.176300048828125, 1.2476345300674438, "[FF] Effect on Climate of the El Ni\u00f1o = Above-average winter rainfall in California, drier-than-normal winters in Oregon and Washington"]
-[8.175773620605469, 1.172422170639038, "[FF] Workshop Date of the Soil Moisture Active and Passive (SMAP) Mission = Sept. 22-23, 2008"]
-[4.266899108886719, 0.5299209952354431, "[TT] Unexpected Observation Date of the Integral = 10 November 2015"]
-[10.485323905944824, 1.2912013530731201, "[TT] UV Light Intensity of the TOI 1807 b = Around 22,000 times more than Earth"]
-[8.030292510986328, 4.494693756103516, "[FF] Object Observation of the STARE satellite = AFSPC catalog"]
-[8.142618179321289, 6.443310260772705, "[FF] Parameter of the ULTRACAM = Unknown"]
-[7.128138542175293, 2.141000986099243, "[TT] Imaging Instrument of the Landsat-8 = Operational Land Imager (OLI)"]
-[7.0223002433776855, 4.338497161865234, "[FF] Unknown of the LUTs = Unknown"]
-[5.187262058258057, 6.899280548095703, "[TT] Data Downlink of the LORE = About 70% of the data"]
-[5.593827247619629, 7.02248477935791, "[TT] Input Buffer Size of the Transmission Module = 1115 bytes"]
-[12.116087913513184, 3.6830384731292725, "[TT] Gas Mixture of the Detector = Xenon and methane"]
-[5.193575382232666, 2.7560904026031494, "[TT] Affiliation of the MHS = EUMETSAT-funded"]
-[7.443862438201904, 7.151591777801514, "[TT] Signal Strength of the Robusta = Weak"]
-[10.026555061340332, -1.534834861755371, "[TT] Orbit Inclination of the P35 series = 100.5\u00ba"]
-[6.422766208648682, 4.345682621002197, "[FF] Development Approach of the Service Module = Parallel development, assembly, integration and test of the service and payload modules"]
-[10.190699577331543, 1.6292977333068848, "[FF] Image Content of the eROSITA = Distribution of the diffuse hot gas, supernova remnants, foreground stars, distant Active Galactic Nuclei"]
-[7.736770153045654, 2.990990400314331, "[TT] Measurement of the GOSAT-2 = CO2 and methane"]
-[8.037824630737305, 4.291695594787598, "[TT] Chamber of the TVAC = Thermal Vacuum"]
-[7.85495662689209, 5.119631290435791, "[FF] Components of the Inner Calibration Unit (ICU) = RF switches, delayed and non-delayed RF paths"]
-[4.24977445602417, 2.158099889755249, "[TT] Launch Site of the AlSat-2A and -2B = Satish Dhawan Space Centre (SDSC) in India"]
-[11.452801704406738, 4.662341117858887, "[FF] Main Structure of the RISAT-1 = Cuboid module"]
-[8.780202865600586, 4.672996520996094, "[FF] Function of the Star tracker/mapper = Identify star constellations and retrieve absolute attitude"]
-[5.735014915466309, 0.49861136078834534, "[FF] Time of the Georegistered CUMULOS data = 19:19 UT"]
-[10.430155754089355, 5.820944309234619, "[TT] Operating Temperature Range of the LCPR Control System = 10-30 degrees Celsius"]
-[11.588136672973633, 3.323976516723633, "[FF] Destruction Cause of the SEOSat = Thruster control issue led to loss of trajectory"]
-[10.066737174987793, -1.5546681880950928, "[TT] Orbit of the Tsikada = 989 km x 1028 km, 83\u00ba inclination"]
-[6.745490550994873, 4.553841590881348, "[FF] Use of the MBOC = Civilian"]
-[6.275592803955078, 6.9604644775390625, "[TT] Experiment Duration of the SIOS Optical Link Demonstration Board = 3-5 years"]
-[5.446529865264893, 2.625117540359497, "[FF] Collaboration of the MAYA-1 = DOST-ASTI, KIT"]
-[9.858907699584961, 6.4406585693359375, "[TT] Channels of the Earth Radiation Budget Experiment (ERBE) = Total radiance (0.3 to 100 \u00b5m); Shortwave (0.3 to 5 \u00b5m); Window (8 to 12 \u00b5m)"]
-[5.453951358795166, 6.248786449432373, "[TT] Total Capacity of the Memory = 7 Gbit"]
-[6.9392266273498535, 3.2647576332092285, "[FF] Purpose of the National Operational Meteorological Satellite System (NOMSS) = Provide accurate and timely meteorological forecasts"]
-[4.412530899047852, 7.063309192657471, "[FF] Functions of the G/S = S- and X-band functions for signal modulation/demodulation"]
-[10.368297576904297, 1.8665202856063843, "[FF] Detection of the REXIS = Newly flaring black hole in the constellation Columba"]
-[5.497407913208008, 6.3693461418151855, "[TT] Science Data Storage Capability of the Spacecraft = 48 Gbit"]
-[3.758378028869629, -0.7638947367668152, "[FF] Orbit of the SET = Near-Earth space"]
-[8.732857704162598, 8.620064735412598, "[TT] Pixels per FWHM of the Spectrometer = 1650"]
-[8.209327697753906, 3.1253914833068848, "[TT] TGF Association of the RHESSI = Intracloud lightning"]
-[8.278650283813477, 5.719247341156006, "[TT] Precision of the SAGE-III = 0.1 % to 10 %"]
-[9.74576187133789, 7.507076740264893, "[TT] GSD (Ground Sample Distance) of the Camera = 1 m"]
-[5.466457843780518, 6.092972755432129, "[TT] RAM of the protos = 8 kB of RAM"]
-[7.6245622634887695, 7.837350368499756, "[TT] -1 Order Diffraction Angle (677 nm) of the Diffracted Beam = 21.3\u00ba"]
-[5.94390869140625, -0.796599268913269, "[TT] Operational Lifetime of the Kanopus-V-IK = Up to five years"]
-[6.273231506347656, 8.196474075317383, "[TT] No of bands/channels of the MERSI = 20"]
-[6.535097599029541, 3.242060899734497, "[TT] Imaging Frequency of the BlackSky Satellite Constellation = Multiple times a day"]
-[9.74202823638916, 8.3640775680542, "[FF] FOV of the STAFF/DWP = \u00b13\u00bax 180\u00ba(IIMS), \u00b117.5\u00ba x 180\u00ba (IES)"]
-[11.150235176086426, 3.847673177719116, "[FF] Balloon Status of the AeroCube-3 = Ejected but did not inflate"]
-[10.437211036682129, 5.7771100997924805, "[TT] Temperature Range of the WPM = 15\u00baC \u2013 20\u00baC"]
-[5.856489181518555, -0.7432541847229004, "[TT] Lifetime of the Spacecraft = 3 years"]
-[8.045639991760254, 0.9129073619842529, "[FF] Importance of the Groundwater = Source of water for crop irrigation, sustains streams during dry periods, and is a useful indicator of extended drought"]
-[10.665767669677734, 1.6018275022506714, "[FF] Production Dependency of the Neutrons = Variable high-energy charged particle fluxes and properties of the upper atmosphere"]
-[7.728616714477539, -0.03803382068872452, "[TT] Daily Downlink Time of the Arctic Ground Station = About 93 minutes"]
-[7.683247089385986, 9.276172637939453, "[TT] Band 7 Wavelength of the OCM = From 760 nm to 740 nm"]
-[7.247082710266113, 1.2738919258117676, "[FF] Purpose of the ExoMars Trace Gas Orbiter = Hunting for atmospheric gases linked to biological or geological activity, as well as understanding the past and present water inventory of the planet"]
-[4.748596668243408, 0.011806591413915157, "[TT] End of Life Date of the PSat-2 = June, 2025"]
-[9.75098991394043, 5.1377692222595215, "[FF] Quantity of the CMT assembly = Six (two per axis) MTMs (Mass Trim Mechanisms)"]
-[7.837730407714844, 5.936037063598633, "[TT] Observation Types of the MWI = Microwave, Electrooptical, Infrared"]
-[6.570059776306152, 4.982537269592285, "[FF] Provides the next increment \u201cSlot List\u201d of the LCT MCC = During the execution of increment N-1, the LCT MCC at GSOC provides the next increment \u201cSlot List\u201d"]
-[4.624894142150879, 7.965422630310059, "[TT] Range of the L-band = 1675-1696 MHz"]
-[11.44272232055664, 4.954039096832275, "[TT] Picosat Distribution of the OPAL = 4 short and 2 long"]
-[4.913721561431885, 0.27618375420570374, "[TT] Impact Date of the DART = 2022"]
-[6.875027179718018, -0.5908670425415039, "[TT] LTDN of the CBERS-3 = Local solar Time on Descending Node) at 10:30 hours"]
-[1.3240444660186768, 1.8996795415878296, "[TT] Cargo Mass of the HTV-3 = About 4600 kg"]
-[7.2491679191589355, 6.608420372009277, "[FF] Steering Range of the Laser Beam = Relative to the S/C"]
-[6.680106163024902, 5.5695343017578125, "[TT] Action of the Degraded Mode = Flight computer powers off"]
-[9.035420417785645, 2.816835641860962, "[FF] Mission Focus of the ACE = Solar wind and ICME (Interplanetary Coronal Mass Ejections), solar and interplanetary energetic particles, cosmic rays and heliosphere/interstellar interactions, and space weather"]
-[9.67167854309082, 4.838275909423828, "[TT] Stabilization of the SAST-5000 = Three-axis stabilization"]
-[14.310713768005371, 3.2231814861297607, "[TT] Mass of the POLDER-P = 32 kg"]
-[7.070600509643555, 7.212093830108643, "[TT] Energy per Pulse of the ATLAS = 50 mJ"]
-[6.60746431350708, 3.8111250400543213, "[FF] Scrapped of the DMSP F-20 = Due to limited funding"]
-[7.119056224822998, 1.324365258216858, "[FF] Collaboration of the Mars Express and ExoMars TGO = At the forefront of the international fleet investigating the Red Planet"]
-[10.931845664978027, 7.545780658721924, "[TT] Swath width of the MWHS = 2700 km"]
-[7.1727495193481445, 2.4992058277130127, "[FF] Publication Year of the Observation of the Earth and Its Environment: Survey of Missions and Sensors = 2002"]
-[6.630816459655762, -0.4315837025642395, "[TT] Period of the SpinSat = 89.4 minutes"]
-[9.95374870300293, 8.029115676879883, "[TT] Focal Ratio of the Optical Telescope Assembly = f/14.3"]
-[8.487820625305176, 1.8286489248275757, "[TT] Climate Accuracy of the RAVAN = Better than 0.3 W m-2 absolute"]
-[7.045693874359131, 8.326227188110352, "[TT] Estimated SNR of the Band 8 = 308.10 \u00b1 130.92"]
-[7.1718573570251465, 7.152824878692627, "[TT] Laser Power of the Triple Mirror = 25 mW"]
-[5.097807884216309, 8.350139617919922, "[TT] Bandwidth of the C-band = 160 MHz"]
-[10.825911521911621, 1.46124267578125, "[TT] Size Comparison to Milky Way of the Leo I = 30 times smaller"]
-[8.744298934936523, 8.139055252075195, "[FF] Status of the NIRSpec instrument = Prepped for Micro-Shutter Array and Focal Plane Assembly replacement"]
-[7.85613489151001, -2.4768564701080322, "[FF] Observation of the GOLD = Thermosphere-Ionosphere System"]
-[8.89583969116211, 3.5211315155029297, "[FF] Measurement Comparison of the Science Question Methodology = Plasma density profile at different latitudes in the target longitude region from radio occultation may be compared with the latitude profile of the plasma density, drift and structures observed later in time by the satellite's in-situ instruments"]
-[8.104839324951172, 8.040982246398926, "[TT] Spectral Band of the TIR camera = 10.4-11.3 \u00b5m (band 2) and 11.4-12.3 \u00b5m (band 3)"]
-[6.575750827789307, 4.786495685577393, "[FF] Ability of the ODTS = Provide accurate estimation of GIOVE and GPS orbits and clocks"]
-[9.571632385253906, 8.257527351379395, "[TT] FOV of the Limb Imager = 5.67\u00b0 x 0.91\u00b0"]
-[10.171490669250488, 7.448222637176514, "[TT] Image Size of the AHI = 17.8 degree diameter circle"]
-[10.52038288116455, 2.360384941101074, "[FF] Operation of the SEXTANT XFSW = Observes MSPs, processes photon events, updates spacecraft state"]
-[9.578591346740723, 8.199806213378906, "[TT] Field of View of the Channels = 45'"]
-[8.585334777832031, 5.611841678619385, "[TT] SIS/URE of the QZS-1 = 34 cm (rms)"]
-[7.085991859436035, 0.23353831470012665, "[FF] Follow-up Studies of the Swift = Performed quick follow-up studies"]
-[6.3585662841796875, 5.362798690795898, "[TT] Type of the Lab-on-a-chip device = BioCDs"]
-[7.124404430389404, 2.2138612270355225, "[TT] Number of Packaged Transistors of the Biomass = 3 per SSPA"]
-[6.124368190765381, 4.136915683746338, "[FF] Contributions of the NASA = SIR-C hardware, the Shuttle launch, ground systems, mission operations and data processing support"]
-[9.417228698730469, -1.1428300142288208, "[TT] Orbit Position of the BeiDou-1E = GEO, 160\u00ba E"]
-[7.916970729827881, 5.047000408172607, "[FF] Status of the Damping Mechanical System = Currently under consideration"]
-[3.151848077774048, 1.680490493774414, "[TT] Geometrical Revisit of the Sentinel-2 = 5 days"]
-[6.864659786224365, 1.9012253284454346, "[FF] Event of the MATS = SPIE Astronomical Telescopes + Instrumentation, 2018, Austin, Texas, United States"]
-[9.732514381408691, 7.301065921783447, "[TT] Spatial Sampling of the Instrument = 1 arcmin"]
-[8.21831226348877, 3.3307647705078125, "[FF] Measurement of the GeoCARB = Solar-induced fluorescence"]
-[7.752267837524414, 5.709866046905518, "[FF] Image Re-sampling Methods of the Product Level 1C (L1C) = Bi-cubic convolution interpolation and nearest neighbor"]
-[8.072251319885254, 5.909524917602539, "[TT] Time Standard Synchronisation Accuracy of the LASSO = One nanosecond"]
-[11.87492847442627, 4.970287799835205, "[TT] Dimensions of the Plastic Sled = 8 feet wide and 60 feet long"]
-[9.931324005126953, 8.251419067382812, "[TT] Paraxial Focal Length (mm) of the FCI-TA = 1650"]
-[10.976288795471191, 7.559500694274902, "[TT] Swath of the MSU-S = 1380 km"]
-[9.695900917053223, 8.238415718078613, "[TT] Field of View of the Genesis Electron Monitor = 10\u00ba-170\u00ba with respect to the spin axis by 30\u00ba in azimuth"]
-[6.172651767730713, 0.6634787321090698, "[TT] Geostationary Orbit Reach Date of the GOLD = June 2018"]
-[14.174422264099121, 3.11955189704895, "[TT] Mass of the DX-1 (Dauria Experimental-1) = 22 kg"]
-[4.8395490646362305, 7.326761722564697, "[TT] Downlink Data Rate of the RF communications = 9.6 or 38.4 kbit/s"]
-[5.557605743408203, 3.5796775817871094, "[FF] Future Satellite of the TIM and SIM instruments = NPOESS series spacecraft"]
-[5.683125972747803, 3.7571613788604736, "[TT] Constellation Size of the Kleos Space = Up to 20 clusters"]
-[5.565882682800293, 5.6518988609313965, "[TT] CPU of the OBC = ERC-32"]
-[8.777320861816406, 4.037896156311035, "[FF] Components of the IVM = Two planar thermal ion sensors, a RPA (Retarding Potential Analyzer) and an IDM (Ion Drift Meter)"]
-[3.703367233276367, 6.600081920623779, "[TT] VDES Antenna Dimensions of the NorSat-2 = 62 x62 x 73 cm"]
-[10.322843551635742, 3.2144827842712402, "[FF] URL of the TOPCAT = https://web.archive.org/web/20120306134448/http://www.bis.gov.uk/assets/bispartners/ukspaceagency/docs/space%20science/cubesats/astrium%20payload%20text%20and%20picture.pdf"]
-[9.882311820983887, 2.516569137573242, "[FF] Purpose of the SIXS = To enable modeling of X-ray fluorescence and scattering on the planet's surface"]
-[10.434823989868164, 7.051971912384033, "[TT] Primary Mirror Diameter of the Optics Assembly = 200 mm"]
-[10.557295799255371, 6.482229709625244, "[FF] Mirror Module Assemblies URL of the IXPE = https://doi.org/10.1117/12.2531956"]
-[7.571606636047363, 5.519278049468994, "[FF] Development Status of the IASI-NG = Critical Design Reviews for Instrument and System aspects completed"]
-[13.09525203704834, 7.47489595413208, "[TT] Power of the GPS receiver = 5-7 W"]
-[7.002212047576904, 0.8030180335044861, "[FF] Presentation Date of the Gravity Probe B = June 23-29, 1991"]
-[9.142980575561523, 6.008301734924316, "[TT] Static Warm Start Acquisition Time of the Antenna Subsystem = < 300 s"]
-[10.541540145874023, 5.6834330558776855, "[TT] Testing Position of the Electro-L1 = 167\u00baE"]
-[5.520247936248779, -0.43476518988609314, "[TT] Operational Duration of the Odin = 21 years"]
-[13.462923049926758, 6.844841957092285, "[TT] Power Generation of the iROSA = 215 kW"]
-[5.760270595550537, 2.8160271644592285, "[FF] TU Graz Team of the OPS-SAT = Composed of GMV and the Space Research Center Warsaw (Poland)"]
-[5.910033702850342, 8.130783081054688, "[TT] Beam size of the Submillimeterwave receiver = 7 arcmin"]
-[7.015712261199951, 5.816610336303711, "[TT] Clocks of the GIOVE-B = 10 ns per day"]
-[5.230567455291748, 6.553753852844238, "[TT] Reception Rates of the AIS Receiver = Above 13,000 AIS messages per hour"]
-[7.730050086975098, 6.8989081382751465, "[TT] Gating Time of the Camera = 1, 1/125, 1/250, 1/500, 1/1000 s"]
-[13.864670753479004, 7.173616409301758, "[TT] Under Voltage Cut Off of the DC-DC converter = Yes"]
-[11.821648597717285, 4.532229900360107, "[TT] Length of the Spacecraft = 7.3 m"]
-[7.8799967765808105, 5.178884983062744, "[FF] Operation of the SSF = Static Earth viewing"]
-[10.03702163696289, -1.5320801734924316, "[TT] Inclination of the Orbit = ~98\u00ba"]
-[5.148407936096191, 4.972249984741211, "[TT] Fix Frequency of the Novatel OEMV-1 GPS receiver = Approximately once every 25 hours"]
-[13.372989654541016, 2.9071733951568604, "[TT] Mass of the SkySat-14 and -15 = 100 kg"]
-[7.719439506530762, 5.409952640533447, "[FF] Measurement Frequency of the Special Sensor Microwave Imager Sounder (SSM/IS) = Unknown"]
-[5.533628463745117, 4.0080132484436035, "[TT] Bus Type of the AlSat-2A and -2B = AstroSat-100"]
-[9.486739158630371, 8.942402839660645, "[TT] Aspect Ratio of the Iris Video Camera = 16:9"]
-[10.41977596282959, 5.725438594818115, "[TT] Operational Temperature Range of the Payload Platform = -10\u00b0C to +30\u00b0C"]
-[4.3125176429748535, 7.3205671310424805, "[TT] Frequency Bands of the RF communications = S-band, UHF/VHF bands"]
-[5.283344745635986, 5.179695129394531, "[TT] Tracking Capabilities of the Phoenix receiver = Good"]
-[8.65035343170166, 7.40552282333374, "[TT] Gain of the Camera = 1 or 4"]
-[6.345563888549805, -1.3462947607040405, "[TT] Launch Date of the GRACE-FO = May 2018"]
-[5.550051689147949, 3.785198450088501, "[FF] Number of Satellites of the PSLV = 6"]
-[6.894489288330078, 4.739741802215576, "[FF] Functionality Demonstration of the RemoveDebris = Vision Based Navigation"]
-[11.838685035705566, 0.04436349868774414, "[TT] Star Temperature of the TESS = 2,700 to 5,000 degrees Kelvin"]
-[13.600576400756836, 1.786295771598816, "[TT] Cargo Capacity of the Canadarm2 = About 4500 kg"]
-[5.776018142700195, 0.33929750323295593, "[TT] Launch Date of the WINDS/Kizuna = 2008"]
-[7.676294326782227, 6.590819358825684, "[TT] Time to Scan a Full Disk of the GK-2A = About one-fifth of the current 28 minutes"]
-[5.94899845123291, 8.717111587524414, "[TT] Modulation Transfer Function of the MTF = \u2265 15% (@Nyquist frequency)"]
-[4.8439764976501465, 2.922861099243164, "[TT] Location of the Science Operations Center (SOC) = LASP"]
-[4.739012241363525, 0.4915381968021393, "[TT] Launch Date of the Anand = 26 November 2022"]
-[10.791507720947266, 2.11675763130188, "[TT] Number of Publicly Released X-ray Source Catalogues of the XMM-Newton Survey Science Center = 6"]
-[5.410860538482666, 1.6942752599716187, "[FF] Development Status of the ALOS-2 = Unknown"]
-[8.214400291442871, 2.1099560260772705, "[FF] Ephemeris Goal of the SeaSat = Submeter accuracy for the vertical component"]
-[6.015835762023926, 1.5038570165634155, "[FF] Presentation Date of the SWOT Mission = 2012"]
-[14.255621910095215, 3.16652512550354, "[TT] Mass of the SOCRATES = 48 kg"]
-[5.131234169006348, 3.1649224758148193, "[TT] Manufacturer of the SAGE-II = Ball Aerospace"]
-[6.5532636642456055, 5.814983367919922, "[TT] Equipment Storage of the Shelter Room = 3 racks"]
-[9.913042068481445, 7.758374214172363, "[TT] Spatial Resolution & Stability of the Telescope = Encircled Energy of 75% at 1 \u00b5m for 150 mas radius"]
-[7.117390155792236, -0.0007439808105118573, "[FF] Debris Disk Age of the Beta Pictoris system = 20 million years"]
-[5.001494884490967, 6.621275424957275, "[TT] Max Bandwidth of the Spacecraft 406 MHz Processor = 80 kHz"]
-[13.29662036895752, 5.354043006896973, "[TT] Articulation Mechanism Resolution of the Solar Panels = 1/64\u00ba"]
-[6.913532733917236, -1.777342438697815, "[FF] Mean Sea Level Change Error Budget of the Jason-3 = External geophysical correction: 0.1 mm/yr, Orbit drift: 0.1 mm/yr, Microwave radiometer wet troposphere correction: 0.7 mm/yr, Sigma naught (\u03c3\u03bf) drift impact on sea state bias through wind speed): 0.1 mm/yr"]
-[8.391127586364746, 7.810680389404297, "[TT] Detector Array of the ISIR = Uncooled"]
-[9.101693153381348, 7.015242576599121, "[TT] Resolution of the TeLEOS-1 = Down to one-meter"]
-[6.296839237213135, 4.586184024810791, "[FF] Interface of the MOC = Coordinates the overall mission"]
-[7.790106296539307, 4.946191787719727, "[FF] Error Sources of the Monte Carlo Analysis = Departure state errors, maneuver execution errors, lidar instrument bias and noise, surface roughness effects on lidar measurements, spacecraft attitude errors, gravity model errors, solar radiation pressure errors, and asteroid spin state errors"]
-[8.407013893127441, 2.767143726348877, "[FF] Measurement of the ROSA = Atmospheric temperature and humidity profiles"]
-[7.621093273162842, 4.867008686065674, "[FF] Horizontal and Vertical Direction of the CATS = Illustrated"]
-[8.079304695129395, 0.11913836002349854, "[FF] Frequency of the Winter Warming Event = More frequent and more intense"]
-[4.88194465637207, 2.641193151473999, "[TT] Coverage of the MBA = Japan and south-east Asia"]
-[4.205830097198486, 4.294548034667969, "[FF] Meeting Date of the Cospas-Sarsat = 06 \u2013 10 July 2015"]
-[5.505115032196045, 0.6647565960884094, "[TT] Arrival Date of the NIRSpec = Sept. 30, 2013"]
-[4.68605899810791, 0.8907415866851807, "[TT] Technology Development Start Year of the MOMS = 1979"]
-[7.00038480758667, -0.231752410531044, "[TT] Eclipse Duration of the Alpha Draconis = 6 hours"]
-[14.334029197692871, 6.548933506011963, "[TT] Maximum Battery Power in Uncontrolled Tumble of the Satellite = 3 hrs"]
-[10.916157722473145, 5.519984722137451, "[TT] Diameter of the Heat Shield = 5 m"]
-[13.028741836547852, 7.05355167388916, "[TT] Housekeeping Power Requirement of the WCOM = 25 W"]
-[5.6941986083984375, 0.5631861090660095, "[FF] Measurement Date of the NuSTAR = Unknown"]
-[14.00023078918457, 3.7178232669830322, "[TT] Mass of the SILEX Optical Terminal = 157 kg"]
-[3.9036457538604736, 4.442857265472412, "[TT] Operational Capacity of the RADARSAT-2 = Above mission specified parameters"]
-[7.291231155395508, 3.6115670204162598, "[FF] Radio Occultation Data Purchase of the NOAA = Expanded on 19 February 2021"]
-[5.1098246574401855, 1.3437899351119995, "[FF] Conference Proceedings Year of the MAHRSI and CRISTA = 2001"]
-[9.448391914367676, 7.006585597991943, "[TT] DEM Resolution of the SRTM = 30 m"]
-[8.669595718383789, 6.331362724304199, "[FF] Optical Path of the IASI-NG = Refractive material which thickness changes with the OPD"]
-[7.499470233917236, 5.226730823516846, "[FF] Operation Mode of the VBS = Cooperative tracking, non-cooperative tracking"]
-[5.303308963775635, 8.429198265075684, "[TT] Bandwidth of the Radiometers = 10 kHz"]
-[10.27112865447998, 2.0242624282836914, "[FF] Gamma Rays of the Magnetars = Have been known to release great bursts of gamma rays"]
-[5.292343616485596, 1.2777663469314575, "[FF] IAC Presentation Date of the SMOS = Oct. 12-16, 2009"]
-[6.047835350036621, -0.4969926178455353, "[TT] Duration of the Field Campaign = 6 days"]
-[5.990204334259033, 5.931114673614502, "[FF] Requirements of the ISL = Lower latencies and transmission error rates"]
-[4.89462423324585, 0.5975958108901978, "[FF] Launch Date of the WFIRST = Mid-2020s"]
-[10.545133590698242, 2.3040006160736084, "[FF] Data Product of the Dosimeter and X-ray telescope = 10 s averaged counts"]
-[7.658465385437012, 6.485575199127197, "[TT] Image Capture Time of the ABI = As often as every 30 seconds"]
-[8.760461807250977, 8.810582160949707, "[TT] Density of the Grating = 300 lines/mm"]
-[6.669702053070068, -0.18026259541511536, "[TT] Period of the Landsat 9 = 99 minutes"]
-[8.461383819580078, 1.8617950677871704, "[TT] Latitude of the Noctilucent Clouds = Between 56 and 60 degrees north latitude"]
-[3.869699716567993, 7.8881916999816895, "[TT] Modulation of the OPS (Onboard Packet Switch) = 512 k symbol/s, \u03c0/4 QPSK"]
-[4.778092384338379, 0.5613124370574951, "[TT] Date of the CGMS46-CMA-WP-01 = 2 June 2018"]
-[10.107662200927734, 7.6922478675842285, "[TT] Distance of M1 of the Image Surface = -1050 mm"]
-[13.6307954788208, 2.749518632888794, "[TT] Launch Mass of the NigeriaSat-2 = 286 kg"]
-[8.826299667358398, 3.2475996017456055, "[FF] Measurement Technique of the ICON = Combines remote optical imaging and in situ measurements of the plasma"]
-[9.622488021850586, 7.022539138793945, "[TT] Spatial Resolution of the TES = 0.43 km x 5.3 km"]
-[10.511412620544434, 4.920407295227051, "[FF] Function of the Langmuir Probe = Provide on-orbit in-situ measurements"]
-[3.8962759971618652, 3.4328715801239014, "[FF] Contribution Date of the Galileo = June 18, 2015"]
-[9.275146484375, -0.41000548005104065, "[TT] Apogee Height of the P3RVX = 60,530 km"]
-[4.990167140960693, 0.7108139991760254, "[FF] Launch Date of the ELaNa V = March 2014"]
-[5.647365570068359, 3.948624610900879, "[TT] Payloads of the Kick Stage = 34 smallsats"]
-[6.6642913818359375, 5.02412748336792, "[FF] Technology Types of the CFESat = Supercomputer, power supply, antennas, booms, launch-vehicle separation system, lithium-ion batteries"]
-[3.9729397296905518, 7.835268497467041, "[FF] Operation Basis of the LCT = Coherent (homodyne digital receiver and BPSK modulation)"]
-[8.067728042602539, 8.515307426452637, "[TT] Spectral Range of the Sensor = 800-1700 nm"]
-[7.856135845184326, 9.171560287475586, "[TT] Band Center Wave of the VNIR = 0.70 \u00b5m"]
-[7.953371047973633, 8.455695152282715, "[FF] Spectral Bands of the Spectrometer = VIS and IR"]
-[6.024466037750244, 5.033021926879883, "[TT] Data Processing of the Satellite = Real-time"]
-[8.429533958435059, 2.02394700050354, "[FF] Noctilucent Cloud Observation Locations of the AIM = Arctic, Antarctica, Utah, Colorado"]
-[7.719011306762695, 4.400081157684326, "[FF] Drivers for the selection of the RVX execution dates and illumination conditions of the RVX = Part B2 to be performed with illuminated perigee, while Parts A+B1 are to be performed with eclipse in perigee. Part B2 to be performed after Part A. Earth cannot be within the VBS FoV when it is used in non-cooperative mode"]
-[4.410835266113281, 5.432157039642334, "[FF] Mission Duration of the GomX-3 = Six months"]
-[9.306244850158691, 1.772840142250061, "[TT] Deorbit Time of the Net and Harpoon = Within 25 years"]
-[3.9205479621887207, 3.459057569503784, "[FF] Operations Start of the Galileo Second Generation (G2) = Later in this decade"]
-[3.801211357116699, -0.7160913348197937, "[FF] Relay of the SpaceDataHighway = In Orbit"]
-[10.474128723144531, 2.3473896980285645, "[FF] Location of the X-ray Telescope = Takes up approximately half of the chassis volume"]
-[6.575701713562012, 0.8994494080543518, "[FF] Observation Date of the Planck = Unknown"]
-[4.813108921051025, 1.177572250366211, "[TT] Launch Date of the Delfi-n3Xt = Nov. 21, 2013"]
-[6.976919651031494, 7.06316614151001, "[TT] Frequency Range of the Laser = 10 mHz to 100 mHz"]
-[6.87418270111084, 4.494661808013916, "[FF] Location of the VIS = Service Module"]
-[6.299433708190918, 8.647078514099121, "[TT] Polarization of the 1 = Horizontal"]
-[4.883413791656494, 2.739147663116455, "[TT] Payload and Ground Segment Responsible Parties of the SEOSAT-Ingenio = SENER & INDRA"]
-[3.4527339935302734, 4.901356220245361, "[TT] Data Management Center of the SAR = JPL"]
-[9.69199275970459, 2.608452796936035, "[TT] Image Capture Date of the AlSat Nano = January 9, 2017"]
-[5.89460563659668, 7.193934440612793, "[TT] Data Rate of the DUST sensor = 8 bit/s"]
-[11.351120948791504, 3.5697314739227295, "[FF] Maneuvers of the ESP Thrusters = Spin-up (de-spin) maneuver and a normal thrust maneuver"]
-[8.326983451843262, 4.72684383392334, "[FF] Components of the ADCS = Wheels, gyroscopes, magnetic control system, magnetorquers, magnetometer"]
-[5.321878910064697, 4.5997209548950195, "[FF] Backwards compatibility of the Open5GCore Rel. 4 = Maintaining backwards compatibility with LTE and NB-IoT [IDD and NIDD]"]
-[8.719887733459473, 6.936267852783203, "[FF] Nodal Position of the PICO20 = Unknown"]
-[11.216535568237305, 1.5710088014602661, "[TT] Total Mass of the FREESTAR = 2,000 kg"]
-[7.229640483856201, 3.8462026119232178, "[FF] Unknown of the TROPOMI satellite instrument = Unknown"]
-[7.862617015838623, 1.1798975467681885, "[FF] Date of the NASA's IMERG Shows Devastating Rainfall Over East Africa = 4 May 2018"]
-[11.701197624206543, 3.400897264480591, "[TT] Thrust of the Ion engine = 10-28 mN"]
-[6.284559726715088, -0.46427783370018005, "[TT] Routine Phase Operations Duration of the RADARSAT-2 = Over three years"]
-[8.692511558532715, 1.8893916606903076, "[TT] Operating Conditions of the Antenna = Category 2 hurricane"]
-[5.309386253356934, -0.16160759329795837, "[TT] Lock Establishment Time of the STEREO-B = 6:27 p.m. EDT"]
-[3.8744964599609375, 1.8002454042434692, "[TT] Launch Pad of the PSLV-C19 = FLP (First Launch Pad) of SDSC"]
-[7.8361945152282715, 9.145609855651855, "[TT] Doubled Wavelength of the LOM = 532 nm"]
-[13.917325019836426, 2.999908924102783, "[TT] Mass of the Space Comb = Below 10 kg"]
-[9.014598846435547, 5.522599220275879, "[TT] Pointing Capability of the Spacecraft = \u00b145\u00ba from nadir in any direction"]
-[13.78280258178711, 5.331691265106201, "[TT] Sensor Type of the CSS = GaAs cells and experimental porous Si cells"]
-[10.187751770019531, 9.39444351196289, "[TT] Nominal IGFOV of the Band 13 = 2 km"]
-[10.642545700073242, 1.6124743223190308, "[FF] Spinning Speed of the Neutron Star = Thousands of miles per hour"]
-[13.62714672088623, 2.763293504714966, "[TT] Launch Mass of the Satellite = 2208 kg"]
-[7.792791366577148, 2.3808882236480713, "[TT] Data Focus of the ABI = Atmospheric, ocean, and land data"]
-[8.307873725891113, -0.844028890132904, "[TT] Dimensions of the Carbon Dioxide Ice Patch = 80 m x 60 m"]
-[5.042425632476807, 3.2946181297302246, "[TT] Manufacturer of the TRXU = Space Quest"]
-[6.458808898925781, 5.31828498840332, "[FF] Communication Experiment of the CubeSat = Optical, or laser"]
-[5.684070110321045, -0.11704950779676437, "[FF] Deployment Repeatability of the RDA = Not provided"]
-[1.3609929084777832, 2.7829251289367676, "[TT] Principal Absorbing Constituents of the Band 4 = CO2"]
-[10.467864036560059, 5.807713508605957, "[TT] Temperature Range of the CIRC = -15\u00ba to 50\u00baC"]
-[4.755122661590576, 1.5733559131622314, "[TT] Launch Date of the SkySat Constellation = 21 Nov 2013"]
-[10.25114917755127, 0.9874759316444397, "[TT] Distance from Earth of the HIP 67522 b = About 490 light-years"]
-[4.5178117752075195, 3.0555474758148193, "[FF] Ground Station of the Enxaneta = Montsec Observatory (OAdM)"]
-[6.588235378265381, 0.22087103128433228, "[TT] End of Life Date of the CryoSat = 08 Oct 2005"]
-[6.925322532653809, 4.634205341339111, "[FF] Optimization Problem of the LUMIO = Nonlinear Programming Problem (NLP) method"]
-[7.941775321960449, 7.378077983856201, "[TT] Data Transmission Rate of the Pan Imager = 15.36 or 61.44 or 122.88 Mbit/s"]
-[7.524415969848633, 6.953125953674316, "[TT] Cadence of the BRITE = < 100 minutes"]
-[7.569143295288086, 1.6114741563796997, "[FF] EarthCARE-ROSES Call of the CloudSat = Recommendation"]
-[14.115110397338867, 2.917135238647461, "[TT] Mass of the Schiaparelli = 600 kg"]
-[5.162765979766846, 2.6950221061706543, "[TT] Affiliation of the Eugene Parker = University of Chicago"]
-[8.959967613220215, 3.922499179840088, "[TT] Stray Light/Disk Light Rejection of the COR1 = 10 -6  B sun"]
-[10.68153190612793, -0.25339436531066895, "[TT] Orbital Tube Diameter of the Tandem-L = 500 m"]
-[9.491231918334961, 0.5086597204208374, "[TT] Altitude of the Schiaparelli module = About 3.7 km"]
-[5.763516902923584, 4.918684005737305, "[FF] Data Relay Method of the GeneSat-1 = Encrypted communications through the public Internet"]
-[10.228673934936523, 7.519216537475586, "[TT] Receiver Telescope Type of the DIAL Instrument = Cassegrain"]
-[7.00174617767334, 8.169197082519531, "[TT] Noise performance of the Channel = 0.5 K at 300 K"]
-[6.122865676879883, 4.513122081756592, "[FF] Tasks of the Ground Station = Tracking of the satellite, Telemetry operations, Command operations, Data processing operations"]
-[4.3916916847229, 7.827261924743652, "[TT] Downlink Frequency of the RF Communication System = 437.490 MHz"]
-[6.885834693908691, 2.8185970783233643, "[FF] Mission Leader of the MethaneSAT = United States-based NGO Environmental Defense Fund (EDF) and its subsidiary MethaneSAT LLC"]
-[4.8388519287109375, 0.5159810781478882, "[TT] Launch Date of the M6P and M12P = Early 2023"]
-[3.9849157333374023, 7.829617500305176, "[FF] Coherent Tracking Capability of the LPT Demodulator = Symbols, carrier and, when necessary, PN code"]
-[6.258238315582275, 4.227066993713379, "[TT] Resource Impact of the SWx = Low"]
-[9.12366008758545, 7.741277694702148, "[TT] Size of the LinkSprite JPEG color VGA camera = 32 mm x32 mm"]
-[4.881454944610596, 3.2385005950927734, "[TT] Manufacturer of the AlSat-2 = EADS Astrium SAS"]
-[4.936466693878174, 3.2226078510284424, "[TT] Manufacturer of the Strela-3/Rodnik = NPO Prikladnoi Mekhaniki"]
-[10.929927825927734, 7.5615386962890625, "[TT] Swath Width of the TIRS-2 = 185 km"]
-[8.142477989196777, 7.322972297668457, "[TT] Number of Photo MOSFET Switches of the DLP System = 5"]
-[14.280077934265137, 3.1489551067352295, "[TT] Total Mass of the SZ-7 = ~7800 kg"]
-[13.570401191711426, 2.943084239959717, "[TT] Satellite Mass of the TanDEM-X = 1350 kg"]
-[4.905651092529297, 0.4396931529045105, "[TT] Insertion Date of the P1 = August 23rd, 2010"]
-[10.365772247314453, 5.721379280090332, "[FF] Temperature Sensitivity of the SOHO's EIT = 1 million, 1.5 million, 2 million and 60,000\u201380,000\u00baC"]
-[12.368263244628906, 0.5917569994926453, "[FF] URL of the PLATO satellite = https://iafastro.directory/iac/proceedings/IAC-18/IAC-18/A7/3/manuscripts/IAC-18,A7,3,5,x42024.pdf"]
-[6.4869704246521, 1.953505039215088, "[FF] URL of the SWOT Satellite = http://scienceandtechnology.jpl.nasa.gov/newsandevents/newsdetails/?NewsID=3201"]
-[4.107890605926514, 6.8992462158203125, "[TT] Antenna Types of the Ground Station = S-band, C-band"]
-[10.4183988571167, 5.959353923797607, "[TT] Brigthness Temperature (BT) Sensitivity of the Antenna = \u00b10.43 K"]
-[4.569239616394043, 7.838594913482666, "[TT] Operating Band of the AstroDev Lithium 2 = UHF band at 400.5 MHz"]
-[5.545123100280762, 7.2241363525390625, "[TT] Data Rate of the Continuous Rebroadcast = Up to 31 Mbit/s"]
-[5.606781005859375, 6.57740592956543, "[FF] Transmission Format of the WEFAX = Start signal (300 Hz), 3 seconds; Phasing signal, 5 seconds; Image (800 lines), 200 seconds; Stop signal (450 Hz), 5 seconds"]
-[13.593145370483398, 7.064775466918945, "[TT] Power of the EPS = 0.2 W"]
-[4.838315010070801, 7.6910247802734375, "[TT] Frequency of the MosaicGNSS receiver = Single"]
-[12.00098991394043, 3.23468279838562, "[TT] Propellant of the X50 series propulsion system = Butane cold gas"]
-[7.954648017883301, 8.012679100036621, "[FF] Sensor Types of the Corvus = Three imagers for different spectral filters. A green band, a red band, and a near infrared band."]
-[8.308603286743164, 8.711779594421387, "[TT] Spectral Resolution of the UV-2 = 0.45 nm"]
-[6.223853588104248, 4.352375030517578, "[FF] Unknown of the GomSpace = Unknown"]
-[11.727520942687988, 0.1215701550245285, "[TT] Number of Candidate Planets of the TESS = More than 1,000"]
-[8.689067840576172, 2.031923532485962, "[TT] Accuracy Range of the Wind speed = 2 m/s or 10%"]
-[6.504555702209473, 0.8726165890693665, "[FF] Anomalies of the FormoSat-2 = 43 AROs (Automatic Reconfiguration Orders) and lots of error events"]
-[8.616156578063965, 4.733349800109863, "[TT] Star Trackers of the ADCS = 2"]
-[9.773059844970703, 7.083714962005615, "[TT] Spatial Resolution of the Atmospheric-sounding instrument = Better than 50 km2 over several across-track pixels"]
-[14.259456634521484, 3.0776526927948, "[TT] Mass of the SPROUT = ~7 kg"]
-[3.359544038772583, 6.45925760269165, "[TT] Antenna Diameter of the AMSR = 2.0 m"]
-[5.519515037536621, 5.743677139282227, "[TT] CPU of the C&DH Subsystem = RAD750"]
-[10.009163856506348, 2.970396041870117, "[FF] Ready for Flight Date of the CubeSats = Dec. 16, 2011"]
-[8.616154670715332, 7.959033012390137, "[TT] Spectral Pixel Size after Binning (x3) of the ISRF = 84 \u00b5m"]
-[6.4266839027404785, -0.26183199882507324, "[TT] LEOP Duration of the TeLEOS-1 = Two weeks"]
-[8.331522941589355, 2.0344390869140625, "[FF] Measurement of the SMMR = Sea-surface temperature, wind speed, and liquid water"]
-[7.714486598968506, 5.918062210083008, "[TT] Performance Improvement of the IASI-NG Instrument = 2 times"]
-[7.741029262542725, 9.565346717834473, "[TT] Center Wavelength of the B5 = 705 nm"]
-[7.9711079597473145, 5.2824883460998535, "[TT] Test Location of the FLLS = RAL Space, in Harwell, UK"]
-[11.785482406616211, 3.2902421951293945, "[TT] Thrust of the Actuators = 2 N"]
-[9.419513702392578, 7.338196277618408, "[TT] Spatial Resolution of the Pan = 2.5 m"]
-[6.154385566711426, 2.179743528366089, "[FF] Design and Development of the eROSITA = MPE (Max-Planck-Institut f\u00fcr Extraterrestrik), Garching, Germany"]
-[3.471606969833374, 5.334649085998535, "[TT] Frequency of the SARP-3 = 406.05 MHz"]
-[8.185982704162598, 1.211335301399231, "[FF] Data of the SMAP = Soil moisture status, timing and extent of potential frost damage"]
-[5.333658695220947, 8.315909385681152, "[FF] Frequency Bandwidth of the Channelizer = Smoothly increased as expected"]
-[5.019949436187744, 8.127175331115723, "[TT] Frequency of the Aquarius = 1.41 GHz"]
-[3.3551199436187744, 5.108149528503418, "[TT] CP Mode Polarization of the SAR instrument = Linear polarization oriented at 45\u00ba or circular (LHCP or RHCP)"]
-[13.666520118713379, 5.570098876953125, "[FF] Objective of the SCTE = To measure the IV curves of up to 47 new solar cell and coverglass technologies"]
-[5.896933555603027, 5.7705912590026855, "[TT] Number of Applications of the C&DH Subsystem = 17"]
-[8.158299446105957, 4.446767807006836, "[FF] Thermal Vacuum Test Environment of the Flight Model = Vacuum"]
-[5.101917266845703, 4.171411037445068, "[TT] Number of the NASA Ground Stations = 3"]
-[5.7283525466918945, 4.798221111297607, "[FF] Purpose of the In-Space Relay Network = Allow continuous communications from space to ground"]
-[10.181076049804688, 3.0870137214660645, "[FF] Deployment of the CubeSats = Use of 9 ISIPODs of ISIS, 3 XPODs of UTIAS/SFL, 2 PEPPODs of GAUSS, and 1 MRFOD of MSU"]
-[10.401885032653809, 5.683414459228516, "[TT] Golf Course Temperature of the ECOSTRESS = 23 F (13 C) cooler"]
-[5.894529819488525, 6.147024631500244, "[TT] Data Reception of the Tactical Terminals = Realtime"]
-[6.301703453063965, 1.3500412702560425, "[FF] Mission Difficulty of the BepiColombo = Most difficult"]
-[6.457985877990723, 0.9391689896583557, "[FF] Data Source of the Gaia spacecraft = New data from ESA\u2019s Gaia spacecraft"]
-[13.79861068725586, 6.980616092681885, "[TT] Qualification Status of the High Voltage Electrical Power System = Qualified for flight"]
-[8.178255081176758, 5.144032955169678, "[TT] Calibration Target of the MAC = Special ground targets"]
-[10.496891021728516, 3.3476998805999756, "[TT] Power Requirement of the CubeSats = None"]
-[8.174628257751465, 2.956840991973877, "[FF] Purpose of the GLI = Observe regional lightning activity in China"]
-[7.554217338562012, 3.842933416366577, "[FF] Door Activation of the PEPPOD #3 = Resulting in the deployment of E-ST@r-2"]
-[7.809998035430908, 1.4087517261505127, "[FF] Mission Objective of the Juice = Study the potential habitability and the underground oceans of Ganymede, Callisto and Europa"]
-[8.02420425415039, 8.093012809753418, "[FF] Sensor Types of the Trishna = Thermal InfraRed (TIR) telescope, optical Visible and Near Infrared (VNIR)/Short Wave InfraRed (SWIR) sensor (VSWIR)"]
-[5.421508312225342, 6.347392559051514, "[TT] Maximum Capacity of the DSU = Up to 8 Tbit at EOL"]
-[6.2861433029174805, 1.8532013893127441, "[FF] URL of the eROSITA = http://arxiv.org/PS_cache/arxiv/pdf/1001/1001.2502v2.pdf"]
-[7.452491283416748, 6.489072799682617, "[FF] Detection Method of the Tianqin satellites = Inter-spacecraft laser interferometry"]
-[9.773563385009766, 2.463365316390991, "[TT] Mission of the NuSTAR = Nuclear Spectroscopic Telescope Array"]
-[11.734231948852539, 7.5301361083984375, "[FF] Workshop Date of the Megha-Tropiques = 17-20 November 2014"]
-[9.155542373657227, 7.288972854614258, "[TT] Spatial Resolution of the Wide Field Imager = 55 m"]
-[6.92746639251709, 7.753118991851807, "[TT] Reflector Size of the Biomass satellite = 12 m across"]
-[5.06121826171875, 1.2686415910720825, "[FF] Mission Date of the INSAT-3D = April 2008"]
-[5.446188926696777, 6.991461753845215, "[TT] Data Transmission Speed of the SpaceDataHighway = 1.8 Gbit/s"]
-[5.972369194030762, -0.5205499529838562, "[TT] Deorbiting Timeframe of the Mothercraft = Next couple of years"]
-[5.127594470977783, 6.984915256500244, "[TT] Downlink Rate of the ResourceSat-1 = 1-16 kbit/s"]
-[14.083979606628418, 4.020025253295898, "[TT] Instrument Mass of the EIC = 2.5 kg"]
-[5.90120792388916, 1.5018876791000366, "[TT] Instrument System Testing Status of the IXPE observatory = Completed"]
-[6.856799125671387, 6.92946720123291, "[TT] Sampling of the Radiometers = 7 samples during 120 ms"]
-[8.359391212463379, 2.1307384967803955, "[FF] Measurement Range of the Cloud Top Pressure = 200-900 hPa"]
-[6.312877655029297, 8.075191497802734, "[TT] Number of Channels of the ScaRaB = 4"]
-[6.061708450317383, 5.714522838592529, "[TT] In-flight Reconfigurable FPGA of the CCM = Xilinx Virtex"]
-[4.11368989944458, 1.1277921199798584, "[FF] Launch Date of the H-II Transfer Vehicle \"KOUNOTORI3\" (HTV3) = July 20, 2012"]
-[8.347114562988281, 6.11873197555542, "[FF] Magnitude of the FGS = Brighter than the magnitude of 15 (MV)"]
-[13.232107162475586, 5.2552337646484375, "[TT] Solar Array Span of the Resurs-DK1 = about 14 m"]
-[10.83022689819336, -0.21169118583202362, "[TT] Formation Type of the TanDEM-X = Bistatic interferometric"]
-[5.559151649475098, 7.267665386199951, "[TT] Symbol Rate of the Channel = 76.8 Msps"]
-[10.041132926940918, 2.9719009399414062, "[FF] Orbit Type of the CuPID CubeSat Observatory = Passing through the magnetospheric cusp"]
-[6.7552571296691895, 8.47463607788086, "[TT] Total Channels of the Spectral Bands = 713"]
-[11.995807647705078, 4.968489170074463, "[TT] Volume of the AMU = 325 x 305 x 250 mm"]
-[6.689584255218506, 6.020163059234619, "[TT] New Avionics of the TDS-1 = 25"]
-[8.260176658630371, 2.554520606994629, "[FF] Optical Property Retrievals of the CATS = Particulate backscatter product, extinction product, ice water content product"]
-[7.772957801818848, 7.4361748695373535, "[FF] Purpose of the TDI = Boosting object signal-to-noise ratio (SNR) by coherently adding the outputs of detectors aligned in the scan direction of the sensor"]
-[8.346980094909668, 5.635760307312012, "[TT] Position Knowledge of the GPS Receiver = \u00b160 m"]
-[11.954442977905273, 4.98587703704834, "[TT] Volume of the DPU = 0.0186 m3"]
-[9.698005676269531, 8.02174186706543, "[FF] Telescopes of the ScaRaB = Four parallel telescopes, one telescope per channel"]
-[9.700386047363281, 1.396684169769287, "[TT] Daily Image Acquisitions of the Pleiades-1A = Approximately 1300"]
-[3.406672954559326, 5.23242712020874, "[TT] Band Coverage of the SARP = 406 MHz"]
-[12.126859664916992, 1.9782027006149292, "[FF] Evaluation Paper of the CartoSat-1 = \"Evaluation of CartoSat-1 Multi-Scale Digital Surface Modelling Over France\""]
-[11.352679252624512, 5.8503923416137695, "[TT] Structure Material of the STRV-2 = All-aluminum"]
-[9.48281192779541, 8.135807037353516, "[TT] Field of View of the CMOS Camera = 58\u00ba"]
-[7.311961650848389, 2.9737143516540527, "[TT] Total CO2 Equivalent Mitigated of the GHGSat = Over 10 million tons"]
-[8.419492721557617, 7.411480903625488, "[TT] CMOS Image Sensor Data Retrieval of the Imager = Field gate programmable array with 32 MB RAM"]
-[6.280815124511719, 4.584446907043457, "[FF] Payload Data System of the KazSTSAT = Delivered"]
-[4.880843639373779, 7.3810200691223145, "[TT] Data Rate of the S-band transceivers = 38.4 kbit/s (low rate), 2-4 Mbit/s (high rate)"]
-[6.3133544921875, 5.1814446449279785, "[FF] Mission of the Parallel Processing Unit (PPU) = Secondary"]
-[7.807211875915527, -2.435208320617676, "[FF] Purpose of the GOLD instrument = Study the upper atmosphere and the impact of space weather on Earth"]
-[12.9868745803833, 7.4766621589660645, "[TT] Power Consumption of the GPS Receiver = Low"]
-[1.748322606086731, 4.558273792266846, "[FF] N/A of the N/A = N/A"]
-[5.214992523193359, 5.7706193923950195, "[FF] Compatibility of the Kenwood THD-7 = with the downlink"]
-[9.511923789978027, 4.72146463394165, "[TT] Attitude Control of the ADCS unit = Satellite detumbling"]
-[3.892188310623169, 4.464258193969727, "[TT] Monitoring Capabilities of the RADARSAT-2 = Global"]
-[4.124293327331543, 0.19170695543289185, "[TT] Launch Date of the Falcon 9 = March 4, 2021"]
-[6.741106033325195, -0.6410056948661804, "[TT] Orbit of the DMSP Follow-on program = Early morning (05:30 hours)"]
-[11.553861618041992, 6.465851783752441, "[TT] Energy Range of the NuSTAR = 8 to 24 keV"]
-[5.172491073608398, 3.2451653480529785, "[TT] Manufacturer of the Orion spacecraft = Lockheed Martin"]
-[5.618489742279053, 5.665305137634277, "[TT] Processor of the C&DH = Innoflight CFC-300"]
-[9.254744529724121, 1.8631809949874878, "[FF] Data Intercomparison of the HARP-2 = Multi-angle, polarized"]
-[9.118073463439941, 7.202631950378418, "[TT] Imaging Resolution of the Resurs-DK1 = 1 m"]
-[3.2595338821411133, 5.687857627868652, "[TT] Radar Reflector Antenna Boom Length of the NISAR = 30 feet (9 meters)"]
-[6.704298496246338, -0.3603269159793854, "[TT] Yaw Flip Frequency of the Spacecraft = Twice during the one-year mission"]
-[8.092808723449707, 8.450632095336914, "[TT] Sensitivity of the VNIR = S/N \u2265 90"]
-[6.9084672927856445, 3.3998281955718994, "[FF] Purpose of the MVP Cell-03 = Examine whether microgravity increases the production of heart cells from human-induced pluripotent stem cells (hiPSCs)"]
-[8.992844581604004, 10.26198959350586, "[TT] Pixel Resolution of the SPIM2 = 14 bit"]
-[4.664312839508057, 6.942140102386475, "[FF] Downlink Limitations of the MSU-SK = Four out of five bands may be downlinked simultaneously"]
-[6.294692516326904, 4.809791564941406, "[FF] Operation of the SPEQS = Autonomic system"]
-[5.1584553718566895, -1.1764075756072998, "[TT] Market of the Kondor = Worldwide customers as well as institutional users in Russia"]
-[9.130298614501953, 7.602215766906738, "[TT] Spatial Resolution of the Multispectral Instrument (MSI) = 10 m"]
-[9.894537925720215, 4.747921466827393, "[TT] Spin Motion of the GMS = 100 rpm"]
-[9.298144340515137, -1.0416388511657715, "[FF] Phase Difference Adjustment Method of the SJ-9A and SJ-9B = Adjusting the orbit semi-major axis and changing the phase relative drift ratio"]
-[9.391852378845215, -0.412983238697052, "[TT] Perigee Height of the P3RVX = 600 km"]
-[11.023871421813965, 3.6884427070617676, "[TT] Size of the Trisat-R = Shoebox-sized"]
-[5.74028205871582, 7.171424865722656, "[TT] Safe Mode Data Rate of the LunaH-Map = 62.5 bit/s"]
-[7.747169017791748, 1.5369601249694824, "[FF] Patrick Blau of the Global Precipitation Measurement (GPM) = GPM Core - Mission & Spacecraft Overview"]
-[5.13897705078125, 6.856350421905518, "[TT] Performance of the TRAM = Within 0.7 dB of theoretical projections"]
-[8.743950843811035, -0.15027253329753876, "[TT] Perigee of the Chang'e-1 = 200 km"]
-[9.838369369506836, 0.6032578945159912, "[TT] Distance to LPF of the LPF Spacecraft = Approximately 1:5 million km"]
-[11.601314544677734, 6.8395819664001465, "[TT] Sensitivity of the ART-XC = 3 x 10-13 erg s-1 cm-2 keV-1"]
-[5.813718318939209, 3.4710700511932373, "[TT] Number of Springs and Flaps of the Dellingr mission = One"]
-[5.630450248718262, 5.284163475036621, "[FF] Purpose of the NanoDock ADCS = House the OEM615 adjacent to a dedicated A3200 ADCS computer"]
-[5.045711994171143, 0.518950343132019, "[TT] Payload Fairing Installation Date of the ICON = 17 October 2018"]
-[5.71928071975708, 0.7234487533569336, "[FF] Data Retrieval of the LIRIS = 29 August"]
-[8.565421104431152, 6.907243251800537, "[TT] Type of the PRISM-2 = Stereo high-resolution instrument"]
-[6.828806400299072, 4.549834728240967, "[FF] Sensitivity of the GMOD = Simulated"]
-[10.174141883850098, 3.3003182411193848, "[TT] Remote Sensing System of the CubeSat = VIS, SWIR, LWIR"]
-[8.832341194152832, 4.451601982116699, "[FF] Operation Modes of the New Horizons = Spin-stabilized mode, three-axis \u201cpointing\u201d mode"]
-[9.743481636047363, -0.6105636358261108, "[TT] Orbit Altitude of the CBAS = 39,000 km"]
-[5.063466548919678, 5.017233371734619, "[TT] Quantity of the GPS = Single unit"]
-[5.116168975830078, 1.7853546142578125, "[FF] Conference Presentation of the TacSat-4 = Space, Propulsion and Energy Sciences International Forum (SPESIF 2009)"]
-[8.239740371704102, 2.8559939861297607, "[TT] Measurement Domain of the CubeRRT = Atmosphere"]
-[13.700830459594727, 2.7377560138702393, "[TT] Launch Mass of the Satellite = 2778 kg"]
-[3.2591028213500977, 5.703022480010986, "[TT] Size of the SAR Antenna = 15 m by 1.5 m"]
-[3.2604873180389404, 4.046566963195801, "[FF] Objectives of the NISAR = Study solid Earth, ice masses, and ecosystems"]
-[18.799306869506836, 3.479686975479126, "[TT] Mean \u0394E (m) of the Mosul = 6.2"]
-[7.233453750610352, 5.516623497009277, "[FF] Instrument Operation Modes of the TARANIS = Survey mode, Event mode"]
-[8.569193840026855, 5.453165054321289, "[TT] Orbit Accuracy of the Gaia = Within 150 m at 1.5 million km"]
-[5.0940260887146, 5.071619987487793, "[TT] Quantity of the GPS receiver = 1 unit"]
-[8.721681594848633, 2.3755807876586914, "[TT] Altitude Range of the Thermosphere = 90 \u2013 1000 km"]
-[5.632210731506348, 1.9678200483322144, "[FF] Mission Status of the CHIPS = Unknown"]
-[14.268296241760254, 3.3190228939056396, "[TT] Mass of the SpinSat = 57 kg"]
-[8.135769844055176, 6.481538772583008, "[FF] Support Mode of the SLIM6 = Window Pseudo Real-Time Imaging"]
-[7.30558967590332, 2.559915781021118, "[FF] Imaging Capabilities of the KMSS = Land and sea surfaces, and ice cover"]
-[7.11817741394043, 7.005650997161865, "[TT] Beam Diameter of the Lasers = 14-meter"]
-[9.869112968444824, 0.7728771567344666, "[TT] Spatial Scale of the GOSAT = 100-1000 km"]
-[4.713575839996338, 7.31885290145874, "[FF] RSSI of the UHF Radio = Parameter Value"]
-[8.499051094055176, 5.162688732147217, "[FF] Output of the GFO Accelerometer = Analog voltages"]
-[9.853344917297363, 5.189470291137695, "[TT] Control Stability of the ACS = < 0.016 \u00ba/s"]
-[8.361186027526855, 8.032118797302246, "[FF] IM Glass of the Optic = Blue"]
-[4.791430473327637, 3.18247389793396, "[TT] Manufacturer of the MEOLUT Next = Thales Alenia Space"]
-[6.0867018699646, -0.44631901383399963, "[TT] Design Storage Time of the Valves = Up to 60 days"]
-[3.8145720958709717, -1.1536825895309448, "[TT] Type of the Orbit = Halo orbit into the Lagrangian point L1"]
-[14.068279266357422, 6.341233253479004, "[FF] Batteries of the IRIS spacecraft = Spares from the GRAIL program"]
-[8.496630668640137, 3.279698371887207, "[FF] Measured Parameters of the Special Sensor Ultraviolet Limb Imager (SSULI) = Vertical profiles from the natural airglow radiation from atoms, molecules and ions in the upper atmosphere and ionosphere"]
-[7.952760696411133, 7.2374420166015625, "[TT] Detection Efficiency of the Sensor = >90%"]
-[4.770191192626953, 5.700667381286621, "[FF] GPS Signal Detection of the Stensat Beacon = Observed"]
-[6.929073810577393, 1.5346150398254395, "[FF] Launch Year of the James Webb Space Telescope = Recently launched"]
-[4.119753837585449, 6.389671325683594, "[FF] Performance Parameters of the Antenna = Gain, half-power beamwidth, sidelobe and cross-polarization levels, electrical pointing"]
-[5.150189399719238, 3.2696919441223145, "[TT] Manufacturer of the TEMPEST-D = NASA/JPL"]
-[9.819330215454102, 7.428595542907715, "[TT] Ground Sample Distance of the Satellite = \u2264 2.5 m (Pan), \u2264 10 m (MS)"]
-[8.310871124267578, -0.6650620102882385, "[TT] Acceleration of the Getz Glaciers = Almost 25% on average"]
-[6.9736456871032715, 7.0707807540893555, "[TT] Instantaneous Optical Power of the Laser diode = 40 W"]
-[4.8397088050842285, -1.7920883893966675, "[FF] Visible and Near-Infrared Imaging Spectrometer (VNIS) of the Chang\u2019e-4 Rover = Payload"]
-[9.089244842529297, -1.2209818363189697, "[TT] Orbit of the EDRS-A = Geostationary"]
-[3.3399531841278076, 2.2239837646484375, "[FF] Instruments of the Sentinel-3 = OLCI and SLSTR"]
-[4.741088390350342, 0.9314946532249451, "[TT] Final Acceptance Review Date of the PROBA-V = December 2012"]
-[6.132848262786865, -0.5558417439460754, "[FF] On-orbit Lifetime of the Global-1 = Unknown"]
-[2.874309539794922, 4.226361274719238, "[TT] Observation Image Date of the ALOS-2 PALSAR-2 = 1st September 2017"]
-[9.98608684539795, -0.20177820324897766, "[TT] Orbit Altitude of the DMSP Block 5D-2 spacecraft = 833 km"]
-[8.372549057006836, 8.759462356567383, "[TT] FWHM at 80 nm of the EUV Simulation = 7 arcmin"]
-[8.84753704071045, 9.482240676879883, "[TT] Spectral Range of the TANSO-FTS-2 = 0.755 - 14.29 \u00b5m"]
-[8.91575813293457, 9.534638404846191, "[FF] Spectral Coverage of the TANSO-FTS = Unknown"]
-[13.675368309020996, 7.033248424530029, "[TT] PPTs Max Current of the EPS = 2.5 A"]
-[7.604304790496826, 2.244887113571167, "[TT] Coverage of the GIIRS = 4500 x 4500 km (China area mode), 1000 x 1000 km (Mesoscale mode)"]
-[7.674083709716797, 5.699058532714844, "[TT] Technology of the Vision-based navigation system = 2D and 3D LiDaR (light detection and ranging)"]
-[4.492090702056885, 7.579413890838623, "[TT] Encoding of the VHF-band communications = NRZ"]
-[7.479103088378906, 2.320970058441162, "[TT] Coverage of the Coverage = 2-day global coverage at 1 km resolution"]
-[14.2059965133667, 3.1751902103424072, "[TT] Mass of the LAGEOS = 411 kg"]
-[7.781622409820557, 2.0153400897979736, "[FF] Data Distribution Network of the SeaSat = NRT (Near-Real-Time)"]
-[6.964895248413086, 4.359828948974609, "[FF] Unknown of the LRR = Unknown"]
-[4.716599464416504, 0.8924370408058167, "[TT] Presentation Date of the PROCYON = August 6-11, 2016"]
-[11.236712455749512, 5.081849098205566, "[TT] Length of the Graded Index Multimode Fiber = 30 meters"]
-[14.240425109863281, 3.138822555541992, "[TT] Mass of the NTSIC = 96.7 kg"]
-[4.904292583465576, 0.553729772567749, "[TT] Start Date of the ColAIS = Summer of 2010"]
-[6.267807960510254, 6.619953155517578, "[TT] Number of Transmission Attempts of the Fixed Platforms = 3"]
-[9.247777938842773, 7.527815818786621, "[TT] Spatial resolution (km) of the VNIR = 1"]
-[8.093587875366211, 5.17822265625, "[FF] Optimization of the AMS STD = Extend the lever arm of the tracking measurement"]
-[11.531537055969238, 6.500555515289307, "[FF] Particle Measurement Ranges of the STAFF/DWP = Electrons = 20 keV - 400 keV; Protons = 40 keV - 1500 keV; Helium = 40 keV - 150000 keV; Oxygen = 40 keV - 4000 keV"]
-[5.898921966552734, -1.1332021951675415, "[TT] Exceeded Design Life of the TRMM = Yes"]
-[12.771951675415039, 1.9950265884399414, "[TT] Vertical Resolution of the SAGE-III = 0.75 km (solar measurements), 1.5 km (lunar measurements)"]
-[9.76424789428711, -0.2913796305656433, "[TT] Initial Altitude of the NRCSD = 385-400 km"]
-[8.944849967956543, 2.7308692932128906, "[TT] Auroral Potentials of the Earth = Several thousands of volts"]
-[8.025671005249023, 3.952066659927368, "[FF] Purpose of the SEISS = Monitor the near-Earth particle and electromagnetic environment in real-time"]
-[9.109315872192383, 8.090081214904785, "[TT] Output Data Rate of the LLNL imaging system = < 50 kbit/s"]
-[6.590939998626709, 0.9454054236412048, "[FF] Agility of the FormoSat-2 = Reduced to ~50%"]
-[9.50963306427002, 4.017343997955322, "[TT] Magnetic Field Measurement Frequency Range of the IOF = 40 Hz to 1.78 kHz"]
-[4.5896759033203125, 3.1073660850524902, "[TT] Operations Location of the Ground Segment = ESOC (Darmstadt, Germany)"]
-[10.696430206298828, 1.3445922136306763, "[TT] Energy from Star of the TOI 700 d = 86% of the energy that the Sun provides to Earth"]
-[9.465522766113281, -0.4209167957305908, "[FF] Kinematic properties of the IPD = < 77 km/s"]
-[9.96104907989502, 0.7418750524520874, "[TT] Separation of the GOSAT-2 = About 150 km"]
-[8.205951690673828, -0.20787353813648224, "[FF] Sea Level Rise Calculation of the GRACE = 1000 gigatons of land ice into the ocean raises global sea level by 2.8 millimeters"]
-[10.181902885437012, 5.334772109985352, "[TT] Compressor Units of the Stirling Cycle Cooler = Pair of linear motor reciprocating compressor units"]
-[6.501423358917236, 1.0637938976287842, "[FF] Mission of the Beowulf Cluster = First in Space"]
-[6.393815040588379, 2.1810038089752197, "[TT] Management Location of the Nancy Grace Roman Space Telescope = NASA\u2019s Goddard Space Flight Center in Greenbelt, Maryland"]
-[5.467350482940674, 6.821591377258301, "[TT] Number of Data Channels of the AMS-02 = Over 300,000"]
-[4.407217979431152, 2.680608034133911, "[TT] Location of the WINDS earth station = Higashimatsushima"]
-[5.132641315460205, 0.6308611035346985, "[FF] Launch Date of the Minotaur I Rocket = Nov. 19, 2013"]
-[4.183992385864258, 7.026284694671631, "[TT] HSTX of the IOD-1 GEMS = CPUT HSTX (High-Speed S-Band Transmitter) with SANT (S-band Patch Antenna)"]
-[3.7024388313293457, 4.525819301605225, "[FF] Data Product Levels of the RISAT-1 SAR = Raw Signal Products (level-0), Geo-Tagged Products (level-1), Terrain-corrected Geocoded Products (level-2)"]
-[7.71138858795166, 6.5599846839904785, "[TT] Image Capture Time of the EUI = More than four hours"]
-[9.803625106811523, 2.6848671436309814, "[TT] Upgrade of the Nano View = Yes"]
-[8.570771217346191, 1.4709134101867676, "[FF] Measurement of the Aquarius Scatterometer = Surface Roughness"]
-[10.363492012023926, 0.5442913174629211, "[FF] Orbital Decay of the Starshine-2 = Occurred"]
-[11.85994815826416, 6.611336708068848, "[FF] Proton Energy of the GALS-VE = > 800 MeV"]
-[8.184706687927246, 8.315690994262695, "[FF] Spectral Bands of the Focal Plane Array = Multiple"]
-[3.240098476409912, 5.032890796661377, "[TT] Full SAR Access Range of the SAR = Ten swaths in quad-pol (QP) mode and nine swaths in dual-pol mode"]
-[14.267492294311523, 3.039200782775879, "[TT] Mass of the PEACE = 6.5 kg"]
-[6.9098219871521, 4.114716053009033, "[FF] Mission of the Team Miles = Fly autonomously using a sophisticated onboard computer system"]
-[6.312563896179199, 8.048352241516113, "[TT] Channel Nr. of the SSMIS = 1-5"]
-[6.584400177001953, -2.0573854446411133, "[TT] Launch Date of the Jason 2 = June 20, 2008"]
-[14.082550048828125, 3.9844489097595215, "[TT] Instrument Mass of the ScaRaB = 40 kg"]
-[5.75816535949707, -0.4999295771121979, "[TT] Lifetime of the Laser = > 5 years"]
-[5.385490417480469, 7.026513576507568, "[TT] Data Transmission Rate of the RISAT-1 = 640 Mbit/s"]
-[12.053990364074707, 6.27778959274292, "[TT] Antiprotons with Energies Above 100 Billion Electron Volts of the AMS = 2200"]
-[6.7788238525390625, 5.902480125427246, "[TT] Quantity of the LROC = 2"]
-[10.181827545166016, 5.3882222175598145, "[FF] Operation of the Thermal Control Louvers = Open up when the satellite needs to dissipate heat from its interior and close when the craft needs to warm up"]
-[13.23766803741455, 5.234020709991455, "[TT] Area of the Solar panels = 23 m2"]
-[11.803960800170898, 6.726356029510498, "[TT] Ion Blockage Energy of the Dosimeter A = Below 1 MeV"]
-[9.359395980834961, 6.371823310852051, "[FF] Directly Controlled by and only depends on the steering mirror of the Steering Mirror = The angle of the local oscillator beam w.r.t. the optical bench"]
-[10.2687406539917, 3.0928640365600586, "[TT] Duty-Cycle of the CubeSat = Minimum 25%"]
-[10.191265106201172, 7.787038326263428, "[TT] Housing Location of the SMA = First optic within the telescope optical assembly"]
-[5.977281093597412, 2.2331647872924805, "[TT] Next Flight of the Orion = Exploration Mission-1"]
-[6.701287746429443, 0.27115243673324585, "[TT] Launch Date of the CryoSat = Oct. 08, 2005"]
-[10.008306503295898, 6.821825981140137, "[TT] Depth Range of the Acoustic Sensors = 0 to 10 meters"]
-[9.72963809967041, 5.202746868133545, "[TT] Configuration of the Pin-Puller = Double-shear"]
-[9.106101036071777, 0.4967450499534607, "[FF] Number of Near-Perigee and Apogee Maneuvers of the ARTEMIS = 5 near-perigee and 3 apogee maneuvers"]
-[5.942483901977539, -0.3176846504211426, "[TT] Operation Duration of the MWI = Over 5 years"]
-[8.982293128967285, 1.1384363174438477, "[TT] Range of values of the Surface type = 25 km"]
-[6.073857307434082, 3.1375350952148438, "[TT] Number of the Participating Scientists = Nine"]
-[14.294047355651855, 3.2082605361938477, "[TT] Mass of the SGLS = 1.5 kg"]
-[2.969498634338379, 4.452515125274658, "[TT] Viewing Acquisition of the XSAR = 20 - 45\u00b0"]
-[7.012451171875, 6.362202167510986, "[FF] Data Processing of the Proton400 k = Extracts subarrays from each 2 min summed image, compresses them and stores them in the SSB"]
-[10.37608814239502, 2.302042245864868, "[TT] Low-energy Response of the X-ray Satellite Navigation = Down to 1 keV"]
-[10.366049766540527, 5.813225746154785, "[TT] Operating Temperature of the NIR = 257 K"]
-[12.160966873168945, 3.495152235031128, "[TT] Quantity of the Propellant Tanks = 2"]
-[7.807583332061768, 5.850698471069336, "[TT] Radiometer Type of the SMMR = Dicke-type"]
-[7.565565586090088, 6.906388759613037, "[TT] Measuring Cadence of the CLARA Instrument = 30 s"]
-[4.784180164337158, 7.7881317138671875, "[TT] Stiffness of the Antenna = > 20 Hz (during launch in lateral direction)"]
-[13.99989128112793, 7.137697696685791, "[TT] Bus Voltage of the SBVR = 100 V"]
-[13.537817001342773, 5.46794319152832, "[TT] Solar Array Type of the TacSat-2 = Thin-film"]
-[9.777459144592285, 2.6508214473724365, "[FF] Launch Status of the Nano-JASMINE = Ready to Launch"]
-[4.782186031341553, 7.2048444747924805, "[TT] S-band Uplink Data Link of the RF communications = 64 kbit/s"]
-[6.271853446960449, 6.380402565002441, "[TT] Data Delivery Time of the SafetyNetTM = 75% within 15 minutes, 95% within 26 minutes"]
-[4.676367282867432, 6.9824299812316895, "[TT] Ground Stations Downlink Data Rate of the Payload = X-band at 800, 400, or 200 Mbit/s"]
-[8.641531944274902, 1.082911491394043, "[FF] Commissioning Phase End Date of the SAC-D/Aquarius = End of July"]
-[8.088547706604004, 8.070731163024902, "[TT] Spectral Band of the Band Cameras = 391.4 nm"]
-[10.103179931640625, -1.5463343858718872, "[TT] Inclination of the Tandem-L satellites = 98.4\u00ba"]
-[13.88912296295166, 6.386595726013184, "[FF] Power Source of the Integrated Firing Test = Battery"]
-[10.028635025024414, 8.190461158752441, "[TT] Focal Length of the STORM = 27.5 cm"]
-[3.1081299781799316, 2.233100414276123, "[FF] Mission Purpose of the Copernicus Sentinel-2 = Monitor changes in plant health and growth"]
-[4.904596328735352, 6.469152927398682, "[TT] Receiver Frequency of the CTECS-A = L1"]
-[7.038697242736816, 3.960784435272217, "[FF] System of the Anti-Coincidence Counter = AMS-02"]
-[8.23499584197998, 4.073059558868408, "[FF] Function of the Microdosimeter Suite = Monitor energetic particle populations and the spacecraft's radiation exposure"]
-[10.400346755981445, 5.190217018127441, "[FF] Secondary Structure Components of the S/C = N/S radiators, E/W panels, Earth-facing panel"]
-[6.487114429473877, 4.871457576751709, "[FF] Function of the MIU = Receives payload commands and spacecraft telemetry from the FC and forwards those to the CEU"]
-[4.872297763824463, 6.864547252655029, "[TT] Type of the RF communication subsystem = Non-coherent, half-duplex, 20K00F1D"]
-[9.413805961608887, 6.13877534866333, "[TT] Impact Angle of the WISPR Optics = 0\u00ba, 45\u00ba, 70\u00ba"]
-[11.731879234313965, 3.303530216217041, "[TT] Thruster Pairs of the CGS = 2 redundant pairs of thrusters mounted on the satellite in each of the \u00b1 flight directions"]
-[4.7469305992126465, 7.872906684875488, "[TT] IF Frequency of the Receiver = 112.5 MHz"]
-[12.011921882629395, 4.519452095031738, "[TT] Width of the Spacecraft = 2.3 m"]
-[4.574215412139893, 7.25225305557251, "[FF] Signal Frequencies of the QZS = L1-band, L2-band, L5-band, E6-band"]
-[5.409754276275635, 1.5462843179702759, "[TT] Image Acquisition Date of the ALOS satellite = 29 March 2011"]
-[3.880723714828491, 3.430168867111206, "[FF] Discovery Date of the Galileo = January 7, 1610"]
-[7.1776628494262695, 4.508608341217041, "[FF] Orbit Calculation Technique of the GPS System = Reduced-dynamic"]
-[7.424004077911377, 7.377784729003906, "[TT] Average Passes per Day of the CHORUS = 8.6"]
-[6.330679893493652, 4.496598243713379, "[FF] Data Provider of the IDE = Provides the stream of science data to the C&DHS"]
-[9.655696868896484, 8.467609405517578, "[TT] Sampling Interval for WV of the Telescope = 3.5 samples / IFOV"]
-[6.799044609069824, 8.037476539611816, "[FF] Electron Density of the RAX-1 = Very quiet"]
-[7.283870697021484, 6.680950164794922, "[TT] Laser System Position Accuracy of the LAGEOS = About 10 cm"]
-[9.860607147216797, 2.9155471324920654, "[FF] Type of the ExoCube = Space weather nanosatellite"]
-[14.19152545928955, 3.3141725063323975, "[TT] Mass of the RCU = 2.3 kg"]
-[8.347294807434082, 1.5066373348236084, "[TT] Uncertainty of the Sea Surface Salinity (SSS) = <0.3 pss"]
-[8.094671249389648, -1.0419350862503052, "[FF] Mission Goal of the ICESat-2 = Estimate the flux of low-salinity ice out of the Arctic basin into the marginal seas"]
-[11.919087409973145, 4.636458396911621, "[TT] Dimensions of the GOMX-1 = 10 cm x 10 cm x 20 cm"]
-[5.957122325897217, -0.4979255199432373, "[TT] Prime Mission Duration of the EMIT = One year"]
-[6.133406639099121, 5.894397258758545, "[TT] Data/Pilot of the L1-B = Data"]
-[7.196183681488037, 2.1525166034698486, "[TT] Imaging Instrument of the Landsat-7 = ETM+ (Enhanced Thermal Mapper Plus)"]
-[5.724949359893799, 6.9919610023498535, "[TT] Telemetry of the DPU = Two 8-bit words/TIP minor frame"]
-[7.987796306610107, 8.812299728393555, "[TT] Spectral Range of the Spectral Range = ~380/400 to 2400 nm"]
-[6.24747896194458, -1.1347904205322266, "[TT] Minimum Mission Life of the GRACE-FO = 5 years"]
-[4.82719612121582, 7.295291900634766, "[TT] Downlink Data Rates of the RF Communications = 9.6 or 38.4 kbit/s"]
-[7.978322982788086, 7.367511749267578, "[TT] Data Digitization of the CCD Camera = 10 bits"]
-[5.624179363250732, 4.836437225341797, "[FF] Tool of the GPS Spoofing = STK (Satellite Tool Kit)"]
-[10.651939392089844, 8.879288673400879, "[TT] Pixel size of the Channel 5 = 32 km x 32 km"]
-[9.089885711669922, -0.5425732731819153, "[TT] Orbit Perigee of the ABEX = 300 km"]
-[5.194268703460693, 1.0431095361709595, "[TT] Live Demonstration Date of the OPS-SAT = 11 January 2022"]
-[4.570045471191406, 1.094660758972168, "[TT] Launch Date of the SAOCOM-1A = 2014"]
-[4.5795087814331055, 1.0438048839569092, "[TT] Launch Date of the SAOCOM-1A = October 2018"]
-[11.08707046508789, 5.925698757171631, "[TT] Material of the Membranes = Calcium-silicate (C-S)"]
-[10.967120170593262, 2.082106351852417, "[TT] Number of Observations of the XMM-Newton = 1,789"]
-[10.448967933654785, 2.3057501316070557, "[FF] Function of the Position Sensing Imager = Record and telemeter the position and time of each X-ray photon detection"]
-[7.843284606933594, 2.0961172580718994, "[FF] Publication Date of the Ocean Color and Temperature Scanner = April 1991"]
-[12.184021949768066, -0.2819673418998718, "[TT] Antenna Pointing Interruption of the TESS = No more than 16 hours"]
-[2.911696672439575, 4.448596000671387, "[TT] Stripmap Mode Swath of the PALSAR-2 = 70 km, 70 km, and 50 km"]
-[7.4129462242126465, 6.567018032073975, "[TT] Product Delivery Time of the PDC (PASCO Data Center) = Within an hour from imagery acquisition"]
-[5.424119472503662, 6.436709403991699, "[TT] Payload Data Storage Capacity of the BRITE spacecraft = up to 256 MB"]
-[13.332832336425781, 7.307788372039795, "[TT] Power of the S/C = 330 W (EOL, 100 W average)"]
-[9.707056045532227, -0.9976137280464172, "[TT] Orbital Separation from SPOT-5 of the SPOT-4 = 138\u00ba"]
-[13.891745567321777, 3.8008623123168945, "[TT] Mass of the Sensor Complement = \u2264140 kg"]
-[5.468006134033203, 6.115982532501221, "[TT] Capacity of the Flash memory = 4 MByte"]
-[4.527753829956055, 2.96242094039917, "[FF] Location of the GESS = IEN (Istituto Elettrotecnico Nazionale), Torino, Italy"]
-[7.829416275024414, 1.4357235431671143, "[TT] Principal Investigator of the SEIS Instrument = Philippe Lognonn\u00e9"]
-[7.673183917999268, 5.958533763885498, "[TT] Instrument Type of the POLDER-P = Multiple direction/polarisation radiometers"]
-[5.229095458984375, 0.8420429229736328, "[TT] Launch Date of the ASNARO = 6 November 2014"]
-[7.348442077636719, 4.823747634887695, "[FF] Type of the NISP = Instrument"]
-[7.183643341064453, 4.34217643737793, "[FF] Mission of the P3RVX = In-orbit demonstrations of the GNC subsystem, the operations, the autonomy approach, and the VV"]
-[7.890374660491943, 4.494863033294678, "[FF] Phases of the In-orbit Calibration and Validation = Two"]
-[13.790395736694336, 5.344438552856445, "[TT] Solar Cells Type of the Solar Array = High-efficiency dual-junction gallium-arsenide (GaAs)"]
-[12.35669231414795, 0.6054908037185669, "[FF] Modular Architecture of the PLATO Satellite = Optimal solution"]
-[5.817741870880127, 2.8712024688720703, "[TT] Development Program of the DIAL Instrument = NASA Earth Science Technology Office's IIP (Instrument Incubator Program)"]
-[8.191632270812988, 7.1080851554870605, "[TT] Susceptibility of the CMOS Sensors = SEU and latchup effects"]
-[10.933759689331055, 6.253448486328125, "[TT] Optical Windows Coatings of the Instrument = Broadband AR coatings with R < 2%"]
-[10.070097923278809, -1.567399263381958, "[TT] Inclination of the STPSat-3 = 40.5\u00ba"]
-[6.1154279708862305, 3.7000393867492676, "[FF] Lead of the Science Office = \u201cScience Systems Engineering\u201d effort"]
-[13.393648147583008, 5.686143398284912, "[FF] Current of the Solar Array = Unknown"]
-[3.972306489944458, 0.2173440307378769, "[TT] Number of Investigations of the SMART-1 = 10"]
-[6.711639404296875, 1.0426630973815918, "[FF] Presentation Date of the SCARLET Solar Array = 2000"]
-[8.224760055541992, 0.7279053330421448, "[FF] Hypothesized Origin of the Psyche = Nickel-iron heart or exposed core of an early planet"]
-[7.602069854736328, 3.1389405727386475, "[FF] Spectrometer-based Methane Sensing System Developer of the Ball Aerospace = Unknown"]
-[11.396310806274414, 8.928675651550293, "[TT] Capture Date of the MODIS = June 16, 2022"]
-[4.435877799987793, 3.148416519165039, "[TT] Location of the Ground Segment = University of Ljubljana and Pomjan"]
-[10.863245964050293, 7.435185432434082, "[TT] Swath Width of the ALOS-4 = 200 km"]
-[9.704580307006836, 5.84908390045166, "[TT] Type of the LCPR Control System = Capacitance tracking based"]
-[9.422590255737305, 8.58797550201416, "[TT] IFOV diameter of the Spectrometer = 14 km"]
-[3.3971219062805176, 5.2352294921875, "[TT] SAR Payload Peak Power Consumption of the RCM = Approximately 1270 W"]
-[7.94752836227417, 7.5776238441467285, "[FF] Conference Presentation Date of the EnMAP Hyperspectral Imager = Sept. 2006"]
-[8.617607116699219, 4.541472911834717, "[FF] Purpose of the STR = Propagating star centroids with a reasonable shape"]
-[3.994779109954834, 2.0982182025909424, "[TT] Launch Vehicle of the Aeolus = Vega vehicle"]
-[8.402851104736328, 1.9372044801712036, "[TT] Measurement Domain of the ISS-RapidScat = Ocean"]
-[9.307794570922852, 3.1551449298858643, "[FF] Purpose of the Solar Wind Concentrator = Enhance the flow of solar wind onto a small target to make possible oxygen and nitrogen measurements"]
-[13.63797378540039, 2.9894115924835205, "[TT] Mass of the Dove Satellites = 4.7 kg each"]
-[4.683984279632568, 0.6704509854316711, "[TT] Launch Date of the GOES-R = October 2016"]
-[4.348349094390869, 7.790096282958984, "[TT] Downlink Frequency of the LLMS/IRIS = 400.6 MHz"]
-[7.592210292816162, 1.9357109069824219, "[FF] Potential Forest Map Frequency of the Tandem-L = Weekly basis"]
-[11.823502540588379, 6.736715316772461, "[FF] Energy Range of the ULEIS = About 20 keV/n to 10 MeV/n"]
-[13.221762657165527, 7.244590759277344, "[TT] Background Energy Consumption of the FLP = 40 W"]
-[10.051774978637695, -1.552448034286499, "[TT] Orbit Inclination of the Corvus-BC = Approximately 97\u00b0"]
-[13.706554412841797, 7.013216018676758, "[TT] Average Power Supply of the EPS = 50 W"]
-[9.18167781829834, 4.578607559204102, "[FF] Attitude Control System of the NorSat-3 = Star tracker, attitude sensors and reaction wheels"]
-[9.491727828979492, 0.8583604097366333, "[TT] Closest Approach to Sun's Surface of the Solar Orbiter = Within 48 million km"]
-[4.816180229187012, 7.45448637008667, "[TT] Transmission Speed of the CW transmitter = 20 wpm"]
-[3.7745628356933594, 6.454479694366455, "[TT] Antenna Type of the PR = 2 m slotted waveguide (WG) antenna"]
-[9.44696044921875, 6.945995330810547, "[TT] Spatial Resolution - ScanSAR of the ALOS-2 = 100 m"]
-[10.11750316619873, -1.2981690168380737, "[TT] Orbit Inclination of the MightySat II.1 (Sindri) = 97.3\u00ba"]
-[3.310281991958618, 1.4398773908615112, "[TT] Design Life of the Sentinel-2A = Seven years"]
-[5.85062313079834, 0.9095754623413086, "[FF] Presentation Date of the OCAMS = March 18-22, 2013"]
-[7.056248664855957, 4.990324974060059, "[FF] Avionics of the ESPA Ring = Independent set"]
-[14.027512550354004, 2.749565839767456, "[TT] Launch Mass of the CartoSat-2D = 714 kg"]
-[9.9896240234375, 4.83676815032959, "[FF] Cooling Pumps of the AMS-02 = 3 out of 4 stopped working"]
-[3.5601181983947754, 4.016350269317627, "[FF] SAR Image of the Sentinel-1A = Over La Reunion Island"]
-[13.351806640625, 7.828336238861084, "[TT] X-band Transmitter Output Power of the RF Communications = +30 dBm (1 W)"]
-[13.72142505645752, 7.030507564544678, "[TT] Capacitor Voltage of the PPTs = 800 V"]
-[7.1042094230651855, 8.212301254272461, "[TT] SNR of the VSSC = Around 100"]
-[4.521866321563721, -0.8657712340354919, "[TT] Splashdown Location of the Dragon spacecraft = 259 miles southwest of Long Beach, California"]
-[6.968777179718018, -0.7810414433479309, "[TT] Orbit Period of the TOI 270 c = 5.7 days"]
-[5.838590621948242, 7.179149627685547, "[TT] Data Rate of the Severyanin-M = 10 kbit/s"]
-[6.3199615478515625, 1.0535911321640015, "[FF] Launch Date of the WINDS = June 2-8, 2013"]
-[5.127365589141846, 2.8214635848999023, "[FF] Locations of the POCs = Navel Research Laboratory in Washington, DC (SECCHI); the University of California, Berkeley (IMPACT), the University of Minnesota, Minneapolis (SWAVES); and the University of New Hampshire, Durham (PLASTIC)"]
-[13.323001861572266, 6.344580173492432, "[FF] Technology Demonstration of the HORYU-2 = High-voltage"]
-[-4.065072536468506, 4.48240852355957, "[FF] Support Phase Time Period of the Mango Tango = 15.06 to 19.06.2010"]
-[4.5689568519592285, 2.814850091934204, "[TT] Archive Location of the SeaSat = ASF (Alaska Satellite Facility)"]
-[3.3147153854370117, 5.104583263397217, "[FF] CP Mode Polarization of the SAR instrument = Selectable by command"]
-[5.291681289672852, 3.4410769939422607, "[FF] Manufacturer of the FF-GNC = Unknown"]
-[9.01261043548584, 4.872631549835205, "[TT] Number of AMR Sensors of the SOSMAG = 2"]
-[11.206068992614746, 0.9833294749259949, "[TT] Development Location of the LISA Telescope = Goddard Space Flight Center"]
-[7.043729782104492, 7.11672306060791, "[TT] Power of the Communications Lasers = 125mW"]
-[13.281710624694824, 7.524700164794922, "[TT] SSPA Power of the VSAT = 40 W"]
-[5.55002498626709, 0.5736351609230042, "[TT] Scanner Portion Failure Date of the ERBE = Feb. 28, 1990"]
-[5.469534873962402, 3.3605732917785645, "[TT] Manufacturing Environment of the MakerSat = Microgravity"]
-[7.760231018066406, 5.237464904785156, "[FF] Focus of the Characterization Process = Utilize automation to expedite fragment characterization process and minimize human-in-the-loop"]
-[8.632224082946777, 1.9115333557128906, "[TT] Sustained Winds of the RapidScat = 45 m/s (162 km/hr)"]
-[10.467336654663086, 1.8146754503250122, "[FF] Description of the Small Black Holes = Small black holes that slowly feed off their companion stars, radiating X-rays as material plummets down into their bottomless pits"]
-[8.162925720214844, 2.776378631591797, "[TT] Measurement Domain of the JPSS-2/NOAA-21 = Atmosphere, Land"]
-[6.05152702331543, 4.6376051902771, "[TT] Developer of the Onboard flight software module = Tatung System Technologies Corp."]
-[3.315293788909912, 1.4493457078933716, "[TT] Nominal Lifetime of the Sentinel-5P = 7 years"]
-[6.00633430480957, -0.5303620100021362, "[TT] Mission Duration of the AIST-2 = 3 years"]
-[9.61097240447998, 8.073887825012207, "[TT] Lens Material of the Primary Objective = BK7G18 and SF6G05"]
-[9.799235343933105, 7.585686206817627, "[TT] Off-nadir Capability of the Telescope = \u00b1 15\u00ba"]
-[11.81119441986084, 6.611469745635986, "[TT] Neutron Energy Range of the MGNS = Thermal to 10 MeV"]
-[6.298399925231934, 8.12998104095459, "[TT] No of Passbands of the Channel 8 = 1"]
-[10.451492309570312, 2.266798257827759, "[FF] X-rays of the Magnetars = Can emit X-rays"]
-[8.349658012390137, 2.4828603267669678, "[FF] Data of the Aeolus = Vertical distribution of aerosol and cloud layers"]
-[9.567561149597168, -0.37225398421287537, "[TT] Altitude of the SCD-2 = 750 km"]
-[11.897290229797363, 6.687980651855469, "[TT] Kinetic Energy of Iron (Fe) of the Mass Spectrometer = ~18 eV"]
-[12.32479190826416, 3.238598346710205, "[FF] Propellant Consumption Rate of the RapidEye = Lower than assumed during the design phase"]
-[9.505362510681152, 6.122097015380859, "[TT] Incidence Angle of the AMSR = Approximately 55\u00ba"]
-[10.771355628967285, 1.400956630706787, "[TT] Primary Star Mass of the M51-ULS = 20 to 30 times the mass of the Sun"]
-[8.578906059265137, 5.3241424560546875, "[TT] Instrument of the Block 5B/C satellites = Constant-speed rotary-scan radiometer"]
-[8.25277042388916, -0.4746491611003876, "[FF] February Extent of the Arctic Sea Ice = 13.95 million km2"]
-[4.257156848907471, 6.378924369812012, "[TT] Helical Antenna Gain of the GOMX-3 = 10 dB"]
-[6.413512706756592, 5.654377460479736, "[TT] Location of the CDU = One on each column"]
-[5.454268932342529, 5.6194353103637695, "[TT] Processors of the RISAT-1 = 300"]
-[9.215425491333008, 6.224025249481201, "[TT] Orientation of the Image = North is 45\u00ba on the upper left"]
-[9.820785522460938, 8.480751991271973, "[TT] FOV (50% resp.) at 10 keV of the Instrument = 10 arcmin"]
-[9.30775260925293, 5.045528411865234, "[TT] Attitude Accuracy of the Spacecraft = 0.4\u00ba in roll and pitch, 0.5\u00ba in yaw"]
-[5.459517002105713, -0.09033170342445374, "[TT] Next Operations Phase of the SHIKISAI and TSUBAME = Three-month period"]
-[8.700041770935059, 5.0434370040893555, "[TT] Star Magnitude of the Normal Cameras = Fainter than mV = 8"]
-[8.895326614379883, 7.671620845794678, "[TT] Pixel size of the 16 mm camera = 8 \u03bcm x 8 \u03bcm"]
-[4.627435684204102, 7.836156845092773, "[TT] Received Frequency of the DCP = 401.65 MHz"]
-[9.715750694274902, 7.188481330871582, "[TT] Spatial Resolution of the Observation Instrument = 0.16\u00ba (Airglow Port), 0.06\u00ba (High-spatial-resolution Port)"]
-[6.620047569274902, -0.5787760019302368, "[TT] Time in Lunar Orbit of the Service Module = 6-7 days"]
-[8.980669021606445, 7.447948932647705, "[TT] Pan Camera of the Payload = 0.45~0.89 \u00b5m"]
-[7.887892723083496, 1.604390025138855, "[TT] Optimal Ground Condition of the HP3 (Heat Flow and Physical Properties Package) = Level ground without rocks larger than about 1.5 cm"]
-[8.466984748840332, 5.587676525115967, "[TT] Measurement Accuracy of the GPS Receiver = < 10 m (95%, 3Drss)"]
-[9.589797019958496, -1.6762287616729736, "[TT] Inclination of the Swarm-A and Swarm-C = 87.35 \u00ba"]
-[6.334352016448975, -0.4740723967552185, "[TT] Attitude Control Time of the PSSCT-2 = Two months"]
-[7.756665229797363, 5.151681900024414, "[TT] Location of the SPIRE = RAL (Rutherford Appleton Laboratory, Didcot, UK"]
-[8.707008361816406, 1.8222615718841553, "[TT] Wind Speed of the Hurricane Laura = 150 miles (240 kilometers) per hour"]
-[7.075380325317383, 7.166891574859619, "[TT] Doubled Pulse Width of the LOM = < 1.5 ns"]
-[8.613282203674316, 0.10970393568277359, "[TT] Affordability of the Comet = Available"]
-[9.91203498840332, -0.34812605381011963, "[TT] Altitude of the Satellite = ~ 700 km"]
-[4.308598041534424, 7.389876365661621, "[TT] Band of the LICEF = L-band"]
-[3.8376989364624023, 3.3861653804779053, "[TT] Launch Date of the Galileo satellites = 21 October 2011"]
-[13.242260932922363, 7.232208251953125, "[TT] Power Consumption of the ASPOC = Up to 2.7 Watt"]
-[5.852411270141602, 4.427584648132324, "[TT] Validation Data Source of the CYGNSS = SFMR"]
-[4.592286586761475, 1.8148930072784424, "[TT] 3TECS Test Dates of the NorSat-2 = August 24th, 2017 and March 14th, 2018"]
-[8.604323387145996, 6.804929733276367, "[FF] Observation Technique of the SHIMMER FTS = Limb scanning can be avoided since the detector simultaneously records interferograms in each horizontal row of the CCD, corresponding to discrete altitudes in the range subtended by the field-of-view (FOV) of the instrument"]
-[3.1894145011901855, 1.6863707304000854, "[TT] Revisit Time of the Sentinel-2 satellites = 5 days"]
-[6.930312633514404, -0.5591734647750854, "[TT] Time in Orbit of the Vesselsat-1 & -2 = 3 years"]
-[6.056156635284424, 2.2898900508880615, "[FF] Launch Vehicle of the SLS = Orion's launch vehicle of choice"]
-[10.121511459350586, -2.7142446041107178, "[TT] Technology of the CoReCi = NAND flash memory"]
-[7.685283184051514, 9.280320167541504, "[TT] Wavelength Range of the Band 11 = 8.3-8.7 \u00b5m"]
-[11.534004211425781, 4.88864278793335, "[TT] Diameter of the RRA = 57 cm"]
-[6.28853178024292, 7.017780303955078, "[TT] User Data Rate of the SILEX Optical Terminal = 0.05 Gbit/s"]
-[5.756758213043213, -2.052020788192749, "[TT] No of revolutions of the KOMPSAT-3 = 14.6 revolutions/day"]
-[9.6221342086792, 6.809654235839844, "[FF] Distortion Measurement of the Test Masses = Affects the fabric of spacetime on the minuscule scale of a few millionths of a millionth of a meter over a distance of a million kilometers"]
-[5.181920051574707, 6.787229537963867, "[TT] Downlink Data Rate of the Spacecraft = 150 Mbit/s"]
-[10.995748519897461, 2.0654494762420654, "[TT] Launch Date of the XMM-Newton = 10 December 1999"]
-[4.97973108291626, 1.411197304725647, "[TT] Operational Phase Start Date of the Himawari-8 = 7 July 2015"]
-[9.852730751037598, 7.1240363121032715, "[FF] Imaging Areas of the RSI = One 3000 km x 24 km continuous strip, two 100 km x 24 km stereo pairs, four 100 km x 24 km strips, or eight scenes"]
-[5.293848991394043, 1.4558656215667725, "[TT] Launch Date of the ABEX = Planned for 2024"]
-[5.517437934875488, 5.7123918533325195, "[FF] Perform reliable file transfer over both two-way and one-way communication links of the Multicast Dissemination Protocol (MDP) = Yes"]
-[10.324270248413086, 2.068838119506836, "[TT] Image Resolution of the eROSITA X-ray telescope = About 10\u201d"]
-[6.418436527252197, 3.274686813354492, "[FF] Purpose of the UN Disaster Charter = Gives front-of-the-line access to information needed to respond to major disasters"]
-[8.139666557312012, 3.0393636226654053, "[FF] Next Step Date of the Air Quality Monitoring = March 28, 2014"]
-[8.658252716064453, 7.032943248748779, "[FF] Imagery Throughput of the Deimos-1 = Order of magnitude more than the first generation DMC"]
-[9.673564910888672, 0.16256307065486908, "[FF] Parachute Size of the ExoMars 2020 = Largest ever to fly on a Mars mission"]
-[13.484004974365234, 5.569817543029785, "[TT] Deployable Solar Array Angle of the UK-DMC-2 = 110\u00ba"]
-[3.117605447769165, 2.233562707901001, "[FF] Data Collection of the Copernicus Sentinel-2 = Optical data"]
-[7.968298435211182, 6.0364203453063965, "[FF] Optics and Resolution of the COTS Cameras = Different"]
-[5.343583106994629, 0.3756803274154663, "[TT] Founding Date of the Timbuktu = 5th century"]
-[5.037295341491699, 5.582249641418457, "[TT] Radio of the OPS-SAT = Software-defined"]
-[5.975845813751221, 4.957232475280762, "[TT] Data Processing of the Ground System = Process 60 times more data than today\u2019s GOES satellites"]
-[10.577720642089844, 3.3324315547943115, "[TT] Form Factor of the CADRE = 3U CubeSat"]
-[7.532446384429932, 8.803457260131836, "[FF] Band-3 Data of the LISS-4 = Nominally observed and transmitted in mono mode"]
-[2.8019144535064697, 0.08346554636955261, "[TT] J2000 right ascension (deg) of the B0531+21 (Crab) = 83.63303"]
-[13.418563842773438, 6.7197794914245605, "[TT] Average Power Consumption of the Satellite = 580 W"]
-[8.10916805267334, 1.0253037214279175, "[FF] Soil Moisture Measurement of the ROSE-L = Volumetric soil moisture (%)"]
-[8.861645698547363, 7.466774940490723, "[TT] Detector Dimensions of the NINA = 60 mm x 60 mm"]
-[6.972956657409668, 0.7443139553070068, "[TT] Percentage of InSight EDL Data Sent of the MarCO-B = 97%"]
-[8.67519760131836, 2.0431771278381348, "[TT] Wind Speed Measurements Accuracy of the SMMR = 2 m/s"]
-[10.30832576751709, 8.022164344787598, "[TT] Aperture Diameter of the Korsch telescope = 0.64 m"]
-[10.332426071166992, 4.146394729614258, "[FF] Common Methods of the Deployment Mechanisms = Nichrome burn wires, breakable links made of plastic retaining bars"]
-[7.958281993865967, 8.190760612487793, "[TT] Vibration Tolerance of the IES = > 20 G rms"]
-[12.064867973327637, 6.287393093109131, "[TT] Antiproton to Proton Ratio of the AMS-02 = Constant from 20 GeV to 450 GeV kinetic energy"]
-[4.37640380859375, 1.8513513803482056, "[TT] Failure Date of the SAR antenna CDU = 2012"]
-[12.214225769042969, -0.21868285536766052, "[TT] New Observing Strategy of the TESS = Full images every 10 minutes"]
-[5.941309928894043, 2.3262720108032227, "[TT] Mission Type of the Orion MPCV = Non-EO"]
-[3.784079074859619, 6.838829040527344, "[TT] Dual-frequency of the Altimeter Antenna = Ku, C"]
-[7.639513969421387, 5.8393073081970215, "[FF] Instrument Type of the CREDO-II = Compact, low power monitor housed on a single board"]
-[9.561078071594238, 9.109724044799805, "[FF] Mission Type of the IRIS = Solar Study"]
-[3.4591870307922363, -0.8845497965812683, "[TT] Orbit of the MWI = Sun-synchronized 833 km"]
-[11.343670845031738, 5.887490272521973, "[FF] Structure Material of the HIT-Sat = Aluminum alloys, AL2219 and AL5052"]
-[6.472334861755371, 1.9767714738845825, "[FF] URL of the NuSTAR = http://www.nustar.caltech.edu/uploads/updates/NuSTAR_2009oct_update.pdf"]
-[5.95684289932251, 7.535216808319092, "[TT] Sampling Rate of the ILAS = 12 Hz"]
-[3.659653902053833, 5.2254157066345215, "[TT] Radar Measurement Detail of the SMAP = 1 km by 3 km"]
-[6.091464996337891, 5.509899139404297, "[TT] Redundancy of the ICUs = Cold redundancy"]
-[10.296161651611328, 4.5996880531311035, "[TT] Bias-Momentum of the Momentum Wheel = 0.84 Nms"]
-[13.51379680633545, 6.778268337249756, "[TT] Energy Storage of the Spacecraft = 52.7 Whr"]
-[11.557607650756836, 3.969494104385376, "[FF] Value of the RCS = Smaller than the IES"]
-[8.728155136108398, 2.0869171619415283, "[TT] Residential User Terminal Diameter of the WINDS = 45 cm"]
-[8.808428764343262, 5.705755233764648, "[TT] Pointing Error of the Tracking Sensor (TS) = 1200-1500 \u00b5rad"]
-[7.634674549102783, 1.9547728300094604, "[FF] Purpose of the Global Monitoring of Tropical Rain Forests = Identify carbon sinks"]
-[7.758539199829102, 2.6651506423950195, "[FF] Application of the Lidar Instrument = Measure canopy depth"]
-[7.201024055480957, 2.1348190307617188, "[FF] Imagery Use of the SPOT 6/7 = Improved efficiency of US agriculture"]
-[9.603907585144043, 4.634130001068115, "[TT] Attitude Control of the ADCS unit = Magnetic detumbling"]
-[7.1142120361328125, 6.658368110656738, "[FF] False Event Rate of the GLM = Evenly distributed"]
-[8.244362831115723, -0.44753608107566833, "[FF] Minimum Extent of the Arctic Sea Ice = 4 million square kilometers"]
-[7.6657915115356445, 0.24251006543636322, "[TT] Contract Award Date of the Lucy = 31 January 2019"]
-[10.104832649230957, 5.459619522094727, "[FF] Purpose of the Thermal Shrouds = Isolate the cold detector plate from the warm ROEs"]
-[5.607792377471924, 6.527963638305664, "[TT] Data Download of the TARANIS Instruments = Up to about 2 GB of high-resolution data (event mode) will be downloaded per day"]
-[7.059887409210205, 2.244128942489624, "[FF] Designed for of the Landsat-7 = Earth-observing"]
-[9.214186668395996, 7.468087673187256, "[TT] Panchromatic of the Medium resolution = 5 \u00b5m x 5 \u00b5m"]
-[10.032560348510742, -1.5192246437072754, "[TT] Orbit Inclination of the Starlink Group 4-14 = 53.2\u00ba"]
-[11.829418182373047, 0.01706613041460514, "[TT] Expected Discovery of the TESS = New planets"]
-[10.72767448425293, 2.7472457885742188, "[TT] Orbit Period of the BlackSky microsatellite = 90.00 min"]
-[3.1026031970977783, 2.216606616973877, "[FF] Mission Purpose of the Copernicus Sentinel-2 = Provide images for distinguishing crop types and data on plant indices"]
-[11.108346939086914, 1.3198332786560059, "[TT] Gravitational Wave Detection of the LISA = Low-frequency"]
-[11.588581085205078, 4.075550556182861, "[TT] Size of the AeroCube-8A = 1.5U"]
-[14.284326553344727, 3.2761688232421875, "[TT] Mass of the SMMR = 53.9 kg"]
-[4.751905918121338, 8.00112533569336, "[TT] Frequency of the TT&C = 437.385 MHz"]
-[6.709733963012695, 8.334087371826172, "[FF] Spectral Channels of the HSI = Variable"]
-[9.186834335327148, -0.5829594135284424, "[TT] Orbit Apogee of the Beijing-3B = 627 km"]
-[11.929417610168457, 5.3095703125, "[TT] Volume of the Instrument = 100 mm x 100 mm x 50 mm"]
-[6.1624650955200195, 4.598198890686035, "[FF] User Platform Simulator of the LCRD = UPS"]
-[8.290103912353516, 0.777769148349762, "[TT] Containment of the Calf Canyon-Hermits Peak Fire = 40 percent"]
-[6.869558334350586, 2.6907379627227783, "[FF] Function of the UrtheCast = Offer near-live images of Earth"]
-[13.80279541015625, 3.9339661598205566, "[TT] Sensor Mass of the Vector Magnetometer = 300 g"]
-[5.215160846710205, 2.3654897212982178, "[TT] Mission Type of the DICE = EO"]
-[4.823270320892334, 0.06001397222280502, "[FF] Launch Date of the SpaceX CRS-24 = 21 December 2021"]
-[5.586879253387451, 0.4355909526348114, "[FF] Acquisition Date of the ATLAS = October 19, 2018"]
-[5.298070907592773, 2.556471586227417, "[FF] Development Partners of the ZACube-2 = CPUT, French South African Institute of Technology, South African Council for Scientific and Industrial Research (CSIR)"]
-[12.117639541625977, -0.28235870599746704, "[TT] Observation Period of the TESS = 27 days"]
-[3.657548666000366, 2.8144664764404297, "[TT] Number of Atomic Clocks of the IRNSS = 4 per satellite"]
-[6.306859970092773, 3.144599199295044, "[TT] Orbit Duration of the BlackSky-1 = About 3 years"]
-[9.543628692626953, 4.739160060882568, "[TT] Attitude Control of the KOMPSAT-6 = 3-axis attitude control with zero momentum bias"]
-[9.988485336303711, 2.8758554458618164, "[TT] Launch Date of the Sunstorm CubeSat = August 27, 2021"]
-[9.56787109375, 8.327013969421387, "[FF] Image Quality of the TOU = 90% enclosed energy within 2.532.5 pixel 2  for 95% of nominal camera FoV"]
-[5.903280735015869, 1.5332664251327515, "[FF] Presentation Date of the PRISMA = July 23-27, 2018"]
-[6.053251266479492, 5.725427150726318, "[TT] Programming Interface of the Xilinx XCV600 FPGA = JTAG (Joint Test Action Group)"]
-[10.111603736877441, 1.4282938241958618, "[FF] Circumstellar Gas Disk of the HD 172555 = Contains Exocomets"]
-[7.238712787628174, 6.78787088394165, "[TT] Data Compression Algorithm of the HRC Instrument = JPEG2000"]
-[8.612800598144531, 2.6783695220947266, "[FF] Observation Goal of the SHIMMER = Observe the equatorward edge of the polar mesospheric cloud (PMC) region"]
-[9.67021369934082, 1.4019156694412231, "[FF] System Status of the Pleiades = Unknown"]
-[11.934175491333008, 3.087042808532715, "[TT] Maximum \u0394V of the Spacecraft = 85 m/s"]
-[6.657755374908447, 4.493111610412598, "[FF] Failure Detection System of the SMART-1 = FDIR system"]
-[4.540776252746582, -0.8668563961982727, "[FF] Payloads of the Dragon spacecraft = New solar arrays, new science investigations, supplies, and equipment for the international crew"]
-[9.147645950317383, -0.35242959856987, "[TT] Apogee of the PROBA-3 = 60,530 km"]
-[3.828831911087036, 0.8989148736000061, "[FF] Launch Provider of the TecSAR = Indian PSLV"]
-[10.100936889648438, 5.72920036315918, "[TT] Passive Cooling Temperature of the Focal Plane = 0-5\u00baC"]
-[11.799235343933105, 6.649407863616943, "[TT] Incident Flux Energy Spread of the GEMS = \u0394Einc of approximately 18 eV"]
-[6.633890151977539, 8.837533950805664, "[FF] Design Improvement of the HARP = Advance over POLDER\u2019s (POLarization and Directionality of the Earth's Reflectances) filter wheel system"]
-[7.207747459411621, 5.99757194519043, "[TT] Instrument Type of the CATS = Lidars"]
-[7.618573188781738, 8.414283752441406, "[TT] Number of Bands of the SWIR Filter Assembly = 3"]
-[4.648009300231934, 0.5282831192016602, "[TT] Landing Date of the CIMON-1 = 27 August 2019"]
-[11.063064575195312, 6.122037887573242, "[TT] Material of the Optical Bench = Low-expansion glass (Zerodur)"]
-[6.120334625244141, 4.175509929656982, "[FF] Purpose of the CIL = Interoperate the French \u201dComposante Spatiale Optique\u201d and the Italian CSG systems"]
-[6.773334980010986, -0.6628380417823792, "[TT] Responsible Orbit of the DWSS = Early Morning"]
-[12.371569633483887, 0.6323356628417969, "[TT] Accuracy of Stellar Mass Measurement of the PLATO = Up to 10%"]
-[10.397608757019043, 1.8453235626220703, "[FF] Function of the NuSTAR = Identify black holes and neutron stars"]
-[5.147932529449463, 6.891836166381836, "[FF] Data Downlink Start Condition of the LCS = When the received intensity is over a threshold value"]
-[8.642056465148926, 4.769495487213135, "[TT] No of Stars Observed of the STOs and STAEs = 10 x 2 (acquisition), 5 x 2 (tracking)"]
-[9.94981575012207, 3.0783474445343018, "[FF] Project of the Firefly Satellite = NSF CubeSat Project"]
-[7.028533458709717, 5.110680103302002, "[FF] Orbit Data of the Satellite = Medium Laser orbit data"]
-[9.552733421325684, 6.0664873123168945, "[TT] Tilt of the PAN-F = 26\u00ba"]
-[9.40776252746582, 3.578597068786621, "[FF] Expected Location of Strongest Magnetic Field of the Sunspot = In the dark part of the umbra"]
-[10.224472999572754, 8.398874282836914, "[TT] Entrance Pupil Diameter of the TOU = 120 mm"]
-[8.183025360107422, 6.613140106201172, "[FF] Type of the ASPIICS = Giant, White Light and Emission Line"]
-[5.875466346740723, 2.419076681137085, "[TT] Affiliation of the ALICE = SwRI (Southwest Research Institute)"]
-[4.485691547393799, 2.9164271354675293, "[TT] Location of the GPC = ESA/ESTEC in Noordwijk, The Netherlands"]
-[9.118792533874512, 7.615841865539551, "[TT] Pan at nadir of the Pushbroom imager = 6-10 m"]
-[4.578427314758301, 7.498099327087402, "[TT] Data Transmission Rate of the VHF-band data transmission = 80 kbit/s"]
-[4.607585430145264, 7.851174831390381, "[TT] Antenna Frequency of the SDR = 1592 MHz"]
-[4.653234958648682, 7.056770324707031, "[TT] X-band Downlink Capacity of the PDHT = 520 Mbit/s"]
-[5.021423816680908, 3.362762689590454, "[TT] Manufacturer of the HWQLP = MRSA/SAC team"]
-[9.02227783203125, -0.5352259278297424, "[TT] Thruster Operation of the ABEX = Below 1,600 km, which only represents 25 minutes of the 19.3-hour orbital period"]
-[14.672603607177734, 6.687657356262207, "[TT] Capacity of the NiH2 batteries = 12 Ah"]
-[14.070924758911133, 4.031389236450195, "[TT] Mass of the MIS Instrument = 475 kg"]
-[5.252824783325195, 2.8360981941223145, "[TT] Operator Action of the ASNARO spacecraft = Nominally no operator action is required"]
-[4.541475772857666, 7.6563215255737305, "[TT] Link margin of the Uplink (VHF) = 4 dB"]
-[3.5847315788269043, 6.326376438140869, "[TT] Length of the Antenna Booms = 80 meters"]
-[13.485106468200684, 6.983408451080322, "[TT] Max Power of the PM = 24 kW"]
-[8.069222450256348, 9.03151798248291, "[TT] Wavelength of the UVSP = About 2760 \u00c5 in first order"]
-[9.45842170715332, 6.624955654144287, "[TT] Azimuth Resolution of the Stripmap = 3.3 m (single pol.), 6.6 m (dual pol.)"]
-[7.105274677276611, 2.9781205654144287, "[FF] 1st-Light Data of the NASA Missions = Unknown"]
-[5.564380168914795, 5.651906967163086, "[TT] CPU Model of the OBC = LEON2-FT"]
-[4.876183986663818, 0.14081774652004242, "[TT] Launch Date of the SpaceX CRS-19 = 5 December 2019"]
-[3.2163197994232178, 4.99714469909668, "[TT] Spatial Resolution of the RISAT-SAR = 1 - 50 m"]
-[9.011567115783691, 0.5343649387359619, "[FF] Laser Link Date of the Artemis = Dec. 6, 2001"]
-[6.456650257110596, -0.8423035144805908, "[TT] LTAN of the DMC-3 Constellation = 10:30 hours"]
-[9.801814079284668, -0.6743987202644348, "[TT] Orbit Altitude of the SCATSat-1 = 720 km"]
-[6.085416793823242, 5.597221374511719, "[TT] Implementation of the CCSDS-IDC = Reconfigurable core in a high density, space qualified reconfigurable FPGA"]
-[10.064474105834961, 0.19812370836734772, "[TT] Inter-satellite Distance Changes of the GRACE-FO = Can be as large as hundreds of microns"]
-[5.305309295654297, 1.1160013675689697, "[FF] Launch Date of the OPAL = Not provided"]
-[6.799549579620361, 1.9272876977920532, "[FF] URL of the ASTERIA Space Telescope = https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=4067&context=smallsat"]
-[2.9375932216644287, 2.3927931785583496, "[FF] Pollutants Monitored of the Copernicus Sentinel-5P = Nitrogen dioxide, ozone, formaldehyde, sulphur dioxide, carbon monoxide, methane"]
-[10.31926441192627, 4.026270866394043, "[TT] Mounting of the SCM = 1 m deployable boom"]
-[5.875982761383057, -0.8084455132484436, "[TT] Design Life of the COSMO-SkyMed spacecraft = 5 years"]
-[4.936645984649658, 2.704348087310791, "[FF] Testing Location of the Gaia SVM = EMC chamber at Intespace, Toulouse"]
-[11.826902389526367, 5.004877090454102, "[TT] Size (mm) of the M1 = 442 x 190"]
-[4.98251485824585, 8.16771411895752, "[TT] Data Band of the GimmeRF = 0-30 MHz"]
-[7.834649562835693, 5.997922420501709, "[FF] Design of the E-THEMIS = Infrared camera"]
-[9.479711532592773, 0.537254273891449, "[FF] Type of the Schiaparelli = Entry, Descent and Landing Demonstrator"]
-[9.58977222442627, 6.266067028045654, "[TT] Swing Angle of the Scan Mirror Mechanism = \u00b14.5\u00b0 (mechanical)"]
-[9.858975410461426, -0.38640156388282776, "[TT] Altitude of the Satellite = 619km"]
-[7.0042548179626465, 8.3885498046875, "[TT] Nominal SNR of the Band 6 = 870"]
-[10.810969352722168, 7.4388041496276855, "[TT] Border Width of the Turbulent Swirls = 20 km"]
-[5.612316608428955, 3.7042899131774902, "[TT] # satellites to collect 106 sqkm/day @ 50 cm GSD of the SkySat = 75"]
-[4.3466997146606445, 4.03849458694458, "[FF] Purpose of the GETR = Verify the acquisition, tracking and noise characteristics of all Galileo signals"]
-[6.162600517272949, 4.041337490081787, "[TT] FDIR Concept of the AstroBus-L = Hierarchically structured and can easily be adapted to specific mission needs"]
-[4.778029441833496, 6.189925193786621, "[FF] Purpose of the Frontier Radio Lite = Communication"]
-[6.680148124694824, 7.869225978851318, "[TT] Channels of the MIS Instrument = 39"]
-[6.245460510253906, 2.200035810470581, "[FF] Mission Purpose of the Euclid = Investigate dark matter and dark energy"]
-[7.276354789733887, 9.133761405944824, "[TT] Filter Wavelength of the ISUAL instrument = 557.7 nm"]
-[4.709441661834717, 7.4636125564575195, "[FF] Modulation Indices of the Transponder = Command and ranging (for uplink), telemetry and ranging (for downlink)"]
-[4.493469715118408, 5.5747389793396, "[TT] Compatibility of the GPS-SAR = Full with existing and future 406 MHz beacons"]
-[6.528507709503174, -0.716550350189209, "[TT] Time to Point to the Sun and Balance Electrical Power of the TSUBAME = Within 33873 seconds after rocket separation"]
-[4.557167053222656, 0.5976703763008118, "[FF] Launch Date of the ANGELS = 18 December 2019"]
-[8.317327499389648, -0.5970489978790283, "[TT] Spatial Resolution (km) of the Ice: edge location = 25"]
-[11.790044784545898, 4.484923362731934, "[TT] Height of the Spacecraft = 6 m"]
-[3.164185047149658, 4.987915515899658, "[TT] Swath Width of the RISAT-SAR = 10 - 240 km"]
-[5.185251235961914, 0.6750507354736328, "[TT] Deorbit Mission Start Date of the CanX-7 = May 3, 2017"]
-[6.726396560668945, 5.900928974151611, "[TT] Number of NMGU of the GIOVE-A = 1"]
-[6.37001895904541, 4.1674346923828125, "[FF] Resource Requirements of the SWiPS = Low"]
-[9.24410629272461, 3.231715202331543, "[FF] Stray Light Analyses Model of the ASPIICS coronagraph = ASAP model"]
-[4.986971855163574, 0.5714998245239258, "[FF] Development Status of the Pelican = Expected to begin launching early next year"]
-[6.661043167114258, 2.5706193447113037, "[TT] Number of Published Images of the MoonKAM = Nearly 120,000"]
-[4.735650539398193, 2.840301990509033, "[FF] Operation Center of the GRACE-FO = German Space Operations Center in Oberpfaffenhofen, Germany"]
-[9.163642883300781, 7.012900352478027, "[TT] Nadir resolution of the WorldView-4 = 31 cm"]
-[10.385110855102539, 5.786314487457275, "[TT] Operational Temperature Range of the Instrument = 293.15 K \u00b1 2 K"]
-[13.834174156188965, 7.197727203369141, "[TT] Power of the Voltage 4 = 1.38"]
-[4.708797931671143, 7.312499523162842, "[TT] X-band Data Rate of the RF Communications = 7.68 Mbit/s"]
-[8.061080932617188, 6.008735179901123, "[TT] Time Standard Synchronization Accuracy of the LASSO = 10-9 s"]
-[6.135034084320068, 2.7836740016937256, "[FF] Funding Source of the Atmospheric Science Program = Catalyst: Strategic"]
-[5.830534934997559, -0.811301589012146, "[TT] Spacecraft Design Life of the FY-4 spacecraft series = 5-7 years"]
-[11.37458324432373, 5.874733924865723, "[TT] Material of the Spacecraft structure = Aluminum"]
-[9.591507911682129, 7.089634895324707, "[TT] Spatial Resolution of the CAPI = 0.5 km"]
-[7.207672595977783, 5.13607120513916, "[FF] Test Modules (TM) of the SAMMES = LEO environmental monitor module, a \u201dram\u201d (direction in face of flight) calorimeter module, a \u201dwake\u201d (direction at the rear of flight) calorimeter module, a Temperature-controlled Quartz Crystal Microbalance (TQCM)/actinometer module, and a solar photovoltaic module"]
-[5.485134124755859, -1.8210303783416748, "[TT] Funding Source of the KOMPSAT-1 = Government of Korea"]
-[5.0737104415893555, 8.150946617126465, "[TT] Frequency of the Sub-mm = 0.35 THz"]
-[10.358111381530762, 1.9398140907287598, "[TT] Brightness of the SS 433 = Appears to be about 1,000 times dimmer than the minimum threshold to be considered a ULX"]
-[9.246219635009766, -0.7305737733840942, "[TT] Orbit of the Trisat-R = MEO (~ 5900 km)"]
-[13.43592643737793, 6.792321681976318, "[TT] Power Generation of the GOSAT-2 = 5kW"]
-[5.558294296264648, 0.6809501051902771, "[FF] Data Mapping Period of the Envisat = 1994 to 2010"]
-[3.900995969772339, 4.379664897918701, "[FF] Data Processing Levels of the RISAT-1 = Standard products, Value added products"]
-[8.132872581481934, 8.51656723022461, "[TT] VNIR Spectral Range of the GLI = 380 - 830 nm"]
-[3.6421589851379395, 4.701983451843262, "[TT] Instrument Type of the ICEYE-X2 = SAR (Synthetic Aperture Radar)"]
-[7.559627056121826, 6.6630730628967285, "[FF] Function of the TDC = Processing valid photon events and rejecting subthreshold or incomplete events"]
-[6.4592461585998535, 5.4640021324157715, "[FF] Function of the Memory Upset Monitor = Looking for single-event upset errors in a known memory pattern in the memory of a test RAM"]
-[6.5981340408325195, 4.329111099243164, "[FF] Function of the Data Integration and Solution System = Integrates the satellite image data with other data sources and provides the analyzed data"]
-[5.630146503448486, 0.7404831647872925, "[TT] First Launch Date of the GeoXO = Early 2030s"]
-[9.703681945800781, 7.537559509277344, "[TT] Resolution of the Nadir Sensor Wide-Field Telescope = 0.42 nm"]
-[7.412003517150879, -0.15781570971012115, "[TT] Communication Loss Time of the Philae = 09:58 GMT"]
-[6.2097296714782715, 0.2883804142475128, "[TT] Number of Open Seats of the Crew-4 = 1"]
-[6.116769790649414, -0.13408708572387695, "[TT] Mission Duration of the FormoSat-2 = 10 years"]
-[14.326404571533203, 3.193802833557129, "[TT] Mass of the Rubin-8-AIS = 7 kg"]
-[7.300414085388184, 8.635664939880371, "[TT] Quantity of the Output filters and diplexer = 1"]
-[9.684028625488281, 5.4089860916137695, "[TT] Sky Circle Radius of the GIM = ~24\u00ba"]
-[5.811526298522949, -0.764975905418396, "[TT] Design Life of the Satellite = 10 years"]
-[8.812829971313477, 2.733858585357666, "[TT] Error of the Atmosphere = \u00b15.0 mm/h"]
-[2.3425071239471436, 2.7906699180603027, "[TT] PI of the IVM = Rod Heelis"]
-[9.423855781555176, 5.740816116333008, "[TT] Ground Track Distribution of the TanSat = -30\u00b0 ~ 10\u00b0"]
-[8.192285537719727, -1.1079859733581543, "[TT] Bathymetry Measurement Depth of the ICESat-2 = Up to 25 meters"]
-[8.71170425415039, 0.16253280639648438, "[TT] Collector Head Depth of the OSIRIS-REx = 1.6 feet (48.8 cm)"]
-[6.041487693786621, 6.652584075927734, "[TT] Key Size of the AES Algorithm = 128-bit"]
-[5.96079158782959, 2.5716946125030518, "[FF] Educational Objective of the ESEO = For university students to acquire hands-on experience of the full life cycle of a real space project"]
-[5.379495143890381, 8.782188415527344, "[TT] Bandwidth of the Band 12 = 0.255 \u00b5m (60 cm -1)"]
-[14.127705574035645, 3.2759270668029785, "[TT] Mass of the APM = 4.4 kg"]
-[8.797526359558105, 4.495126724243164, "[FF] Star Sensor Requirement of the TARANIS = Low temperature and a FOV (Field of View) without any sun parasitic illumination"]
-[7.492404460906982, 4.864365577697754, "[TT] Mounting Location of the Camera Sensor = On the OSC"]
-[4.879732608795166, 0.8893769979476929, "[TT] Satellite Launch Date of the AMSU/HSB = May 4, 2002"]
-[7.220893383026123, 1.3238246440887451, "[TT] Solar Array Deployment Time of the Solar Orbiter = 06:24 CET"]
-[8.39117431640625, 1.7115428447723389, "[TT] 34 GHz Channel Function of the JMR = Correction for non-raining clouds"]
-[7.646724700927734, 3.2660739421844482, "[FF] Observation Capability of the MIGHTI = Day and night"]
-[5.1307549476623535, 2.4171206951141357, "[TT] Chair of the Independent Enquiry Commission = Toni Tolker-Nielsen"]
-[2.8958754539489746, 1.9403239488601685, "[FF] Image Capture Date of the Copernicus Sentinel-2 = June 24, 2022"]
-[14.214942932128906, 2.959094285964966, "[TT] Mass of the OceanSat-2 = 970 kg"]
-[8.230021476745605, 5.271971225738525, "[TT] Calibration Status of the Satellite = Uncalibrated"]
-[5.577360153198242, 6.313355922698975, "[TT] Data Storage of the SPAS carrier = Tapes"]
-[11.695271492004395, 3.3043482303619385, "[FF] Thruster Configuration of the GPIM = Single primary divert thruster centered on an upper deck topping the payload\u2019s box-like primary structure flanked by four attitude-control thrusters mounted one each at the adjacent corners"]
-[9.26000690460205, 2.8059043884277344, "[TT] Solar Wind Speed and Beta of the ACE = ~38% lower on average from 2009 through the day 79 of 2013"]
-[3.7887096405029297, 7.94478178024292, "[FF] Modulation Waveforms of the Argos-3 = BPSK (Bi-Phase Shift Keying), QPSK (Quadra-Phase Shift Keying) and GMSK (Gaussian Minimum Shift Keying)"]
-[4.765851974487305, 7.394175052642822, "[TT] Data Rate of the X-band transmitter = 42.22 Mbit/s"]
-[8.107970237731934, 6.833369731903076, "[TT] Image Interval of the DECA = 1.5 s"]
-[9.490606307983398, 4.679346561431885, "[FF] Function of the ADCC = Interfaces with the attitude sensors and actuators and runs the attitude control algorithms"]
-[9.691330909729004, -0.4424169659614563, "[TT] Orbit Altitude of the LARES-2 = 5893 km"]
-[10.602588653564453, 7.614403247833252, "[TT] Swath of the Beam Modes = 105 to 170 km"]
-[6.002411842346191, 0.7315826416015625, "[TT] Launch Date of the FormoSat-7 / COSMIC-2 = 25 June 2019"]
-[7.571981430053711, 6.469527244567871, "[FF] Potential of the ORS = Rapidly fly a spare replacement instrument to provide continued temporal measurements"]
-[9.049199104309082, 6.6404500007629395, "[TT] Image Resolution of the CaSSIS = 5 x 10 km"]
-[3.2523250579833984, 5.574504852294922, "[TT] Unit Failure of the SAR Antenna CDU = 2012"]
-[11.72076416015625, 4.5768351554870605, "[TT] Dimensions of the Atlantic Basin Facility = 75 m long, 9 m wide"]
-[6.673357963562012, 4.497696399688721, "[FF] Cardframe Structure of the Avionics System = Grown and split into two separate units"]
-[4.713819980621338, 2.447122812271118, "[TT] Launcher of the GPM Core spacecraft = JAXA"]
-[8.837766647338867, 7.493653774261475, "[TT] Size of the Full Image = 600-700 kB"]
-[7.817216396331787, 4.78457498550415, "[TT] Type of the SSM/T-1 = Atmospheric temperature and humidity sounders"]
-[12.791565895080566, 7.229317665100098, "[TT] Main Beam Efficiency (%) of the Antenna = 85"]
-[7.9041290283203125, 5.514768600463867, "[FF] Components of the STP-H6-NISTEx II = Sun-shade, optical shutter, interferometric components, housing for the Stingray custom designed optics, electronics processing and power interface using a radiation hardened BAE CIS1910 detector"]
-[14.275979995727539, 3.2073307037353516, "[TT] Mass of the AVNIR = 250 kg"]
-[11.371901512145996, 3.627110481262207, "[FF] Main hollow-cathode activation of the ACTV_M = PS-4 on, high level"]
-[11.849139213562012, 4.879027843475342, "[TT] PCB Size of the GAMALINK = 95.9 x 90.2 x 11 (mm)"]
-[4.60995626449585, 4.7865376472473145, "[FF] Consortium Members of the Maritime AI-NAV = FGI, Aalto University\u2019s Sensor Informatics and Medical Technology group, Fleetrange Ltd"]
-[8.560476303100586, 1.8201748132705688, "[TT] Range of values of the Cloud amount = 0-100%"]
-[9.147444725036621, 7.794227600097656, "[FF] Focal Plane of the Telescope = Four large-format CCD sensors"]
-[8.057173728942871, 9.32262897491455, "[FF] Meteoritic Origin of NLCs of the AIM spacecraft = About 3% of each ice crystal"]
-[11.109111785888672, 5.888009071350098, "[TT] Shielding of the Radiator = Specially shaped titanium fins"]
-[5.4291300773620605, 0.06609895825386047, "[FF] Launch Date of the RapidEye = Unknown"]
-[5.86240816116333, -0.8567655086517334, "[TT] Design Life of the Spacecraft = 4 years"]
-[5.142435073852539, 5.997552394866943, "[TT] Technology of the AOCS = SpaceWire"]
-[8.063940048217773, 4.299235820770264, "[FF] Objective of the SEE Experiments = Measure and evaluate the effects of the high radiation environment on electronic devices"]
-[5.091036796569824, 3.3188393115997314, "[TT] Manufacturer of the MakerSat = Made In Space"]
-[4.067526340484619, 3.3126871585845947, "[TT] Budget Allocation of the Galileo = 8 billion euros"]
-[5.764350414276123, 5.6342034339904785, "[TT] Components of the IDA = QWIP FPA, cryocooler, motherboard ROIC"]
-[10.488785743713379, 4.358340740203857, "[TT] Reaction Wheel Operation of the CanX-2 = Long-duration"]
-[7.539312839508057, 6.871109485626221, "[TT] Frame Store Transfer Time of the CCD = 200 \u00b5s"]
-[3.9652445316314697, 2.0260865688323975, "[TT] Launch Vehicle of the COSMO-SkyMed-1 = Delta-2"]
-[13.318388938903809, 7.378011703491211, "[TT] Power of the TMR = 25 W"]
-[5.545077323913574, 5.520437240600586, "[TT] Type of the OBC = RCM3400 of Z-World based on the microcontroller Rabbit 3000"]
-[13.889216423034668, 7.006335258483887, "[TT] Voltage of the HVSA = 350 V"]
-[13.52691650390625, 7.145569324493408, "[TT] Power Supply of the Readout Electronics = Individual"]
-[1.7444692850112915, -2.0758652687072754, "[FF] Reentry Capsule Recovery Date of the Hayabusa-2 = 6 December 2020"]
-[13.374236106872559, 2.8959407806396484, "[TT] Total Mass of the QuakeSat = about 4.5 kg"]
-[12.512903213500977, 3.1553940773010254, "[TT] Fuel Mass of the Chemical propulsion engine = 34 kg (N 2 H 4 )"]
-[18.648454666137695, 3.9402153491973877, "[TT] NE\u0394T of the 4 = 0.4 K"]
-[10.67292308807373, 5.321240425109863, "[FF] Operation of the ELF = Electrons are emitted from the conductor surface"]
-[14.276041984558105, 3.2846598625183105, "[TT] Mass of the EPE = 3.3 kg"]
-[5.747164249420166, -0.8981472253799438, "[TT] Design Lifetime of the EO-1 = 1.5 years"]
-[4.599996566772461, 2.8032329082489014, "[TT] Control Center Location of the Odin = Esrange"]
-[4.516491413116455, 1.5863523483276367, "[TT] Launch Date of the TanSat = December 21, 2016"]
-[7.834412574768066, 4.6440815925598145, "[TT] Observation Frequency of the EPIC instrument = About 13 times per day"]
-[5.668877124786377, 7.014842987060547, "[TT] Output Buffer Size of the Transmission Module = 1115 bytes"]
-[4.433464050292969, -0.23895438015460968, "[FF] Initial Launch Date of the Nauka = 2007"]
-[9.692818641662598, -0.44312945008277893, "[TT] Altitude of the TEMPO = 35,786 km"]
-[4.773592948913574, 8.089509010314941, "[TT] Center Frequency of the L1-C/A = 1575.42 MHz"]
-[5.947854518890381, 5.181009292602539, "[FF] Function of the LPT = Demonstrate communications links"]
-[9.668537139892578, 1.3964961767196655, "[TT] Revisit Capacity of the Pl\u00e9iades Neo = Twice"]
-[6.9665703773498535, -0.7803454399108887, "[TT] Orbit Period of the TOI 270 d = 11.4 days"]
-[12.08018970489502, -0.3958546221256256, "[TT] Mission Duration of the TESS = Initial two-year mission"]
-[3.852917194366455, 4.515660762786865, "[TT] Orbit of the RADARSAT-2 = In one of the most populated debris zones"]
-[9.481971740722656, 4.979527950286865, "[TT] Attitude Knowledge of the ACS = \u00b10.02\u00ba"]
-[4.00209903717041, 1.684417963027954, "[TT] Launch Vehicle of the TechEdSat = H-II Transfer Vehicle \"KOUNOTORI3\" (HTV3) Aboard the H-IIB Launch Vehicle No. 3"]
-[5.172571182250977, 0.6785861253738403, "[FF] Publication Date of the Onboard Processing = 27 February 2018"]
-[10.147798538208008, 8.061858177185059, "[TT] Entrance Slit Width of the Telescope = 2.6 mm"]
-[7.276822566986084, 6.246872901916504, "[TT] Operating Mode of the TOMS = Scan mode"]
-[7.809268951416016, 6.363210678100586, "[TT] Image Capture Time of the Long Range Reconnaissance Imager (LORRI) = 11:04 Universal Time on February 28, 2007"]
-[5.274689197540283, 3.4669055938720703, "[TT] Manufacturer of the Terminator Tape Deorbit Module = TUI (Tethers Unlimited Inc.)"]
-[3.4527344703674316, 3.6931312084198, "[TT] Ground Control Segment Provider of the PAZ = Indra"]
-[10.232434272766113, 3.2592554092407227, "[FF] Configuration of the FENIX micropropulsion device = Can be at each corner of the CubeSat or doubled up on either side"]
-[5.532745361328125, 4.258805751800537, "[FF] Services of the ALTAIR bus = Navigation, propulsion, data processing and communications for the five TRACERS science instruments"]
-[5.2298431396484375, 4.168231010437012, "[TT] Number of active satellites of the GPS-DASS = 2/24"]
-[13.542637825012207, 5.814359664916992, "[TT] Solar Array Power of the LEOStar-2 bus = 415 W"]
-[7.588165760040283, 3.1644675731658936, "[FF] Image of the SJ-5 = Fluid two-layer flow liquid-bath"]
-[12.466232299804688, 0.5777778625488281, "[TT] Long Pointing Phase Duration of the PLATO = Up to 3 years"]
-[7.079879283905029, 7.191628456115723, "[TT] Laser Pulses Distance of the ATLAS = 480 km"]
-[9.762361526489258, 5.712307929992676, "[FF] Thermal Coupling of the Optical System = Common opticalbench that thermally couples both sensors"]
-[6.895111560821533, -0.2117437869310379, "[TT] Repeat Cycle of the OceanSat-1 = 2 days"]
-[5.435552597045898, 6.096479892730713, "[TT] Memory of the protos = 128 kB of flash memory"]
-[4.8027262687683105, 0.6813326478004456, "[FF] Development Start Date of the MOMS-02 = Unknown"]
-[7.97114372253418, 4.607596397399902, "[FF] Design Hypothesis of the Geometric Calibration System = Change within an orbit can be sufficiently modelled with a 3rd order polynomial against the time since the eclipse\u2019s exit"]
-[13.3162260055542, 2.8675239086151123, "[TT] Mass of the HawaiiSat-1 = 80 kg"]
-[5.75423002243042, 2.487837791442871, "[FF] Project Partners of the TRACERS = University of Iowa (UI), SwRI, MSS, UCB, UCLA"]
-[6.891958236694336, 9.500977516174316, "[TT] NEDT at 300 K of the Band 8 = 0.15 K"]
-[6.308103084564209, 8.011285781860352, "[TT] Channel Nr. of the SSM/T-2 = 1-7"]
-[10.34719467163086, 2.3127498626708984, "[FF] X-ray Instruments of the AstroSat = 3 co-aligned X-ray instruments"]
-[12.144798278808594, 3.1723618507385254, "[TT] Propellant of the CGMS = Argon"]
-[9.107478141784668, 1.3765168190002441, "[FF] Interstellar Space Entry Date of the Voyager 2 = 10 December 2018"]
-[8.602335929870605, 7.701070785522461, "[TT] Spatial Data Pixels of the Detector = 1000 pixels"]
-[8.874565124511719, -0.03163827583193779, "[TT] Orbit Latitude Range of the NICER/SEXTANT = \u00b151.6 \u00ba"]
-[9.133264541625977, 5.6898603439331055, "[TT] Orbital Navigation Solution of the NEMO-AM = Position: 12 m (2\u03c3), Velocity: 6 cm/s (2\u03c3)"]
-[3.818258047103882, 7.923134803771973, "[TT] Modulation of the TREX-823 X-band transmitter = QPSK/OQPSK (selectable)"]
-[10.516605377197266, 5.493533611297607, "[TT] Heat Probe of the InSight Lander = HP3 (Heat Flow and Physical Properties Probe)"]
-[9.493370056152344, 0.6257400512695312, "[TT] Distance from Earth of the Moon = 384,000 km"]
-[8.158059120178223, 4.314701557159424, "[TT] Test Type of the EDRS-C terminal = Thermal vacuum test"]
-[5.055771350860596, 8.170843124389648, "[TT] Type of the SSALT = Single-Frequency Solid-State"]
-[10.804317474365234, 6.847755432128906, "[TT] Effective Received Power (b) of the Triple Mirror = > 25 pW"]
-[14.081461906433105, 4.0433855056762695, "[TT] Instrument Mass of the CoReCi = 14 kg"]
-[5.310361862182617, 0.5624682903289795, "[TT] Next Spacewalk Date of the iROSA = Sunday, June 20"]
-[8.996111869812012, 8.040165901184082, "[TT] CCD Line Pixel Pitch of the FPM (Focal Plane Module) = 6.5 \u00b5m"]
-[9.323877334594727, 6.274117469787598, "[FF] Incidence Angle of the ScanSAR Wide beam mode = Unknown"]
-[8.169941902160645, 1.2015461921691895, "[TT] Soil Moisture Refresh Rate of the SMAP = 3 days"]
-[9.207120895385742, 0.8856378197669983, "[FF] Density of the Venus' Orbital Dust = About 10% more dense than in neighboring regions"]
-[4.904359340667725, 3.3691604137420654, "[TT] Manufacturer of the Focal Plane = e2v for Astrium"]
-[9.424717903137207, 7.2253336906433105, "[TT] Resolution of the COSI = 0.7 m (Pan)"]
-[8.313511848449707, 0.8922713398933411, "[TT] Absolute Accuracy of the Snow water content = \u00b1 3 cm"]
-[7.564010143280029, 3.7048470973968506, "[TT] Quantity of the Debris = More than 250 pieces"]
-[5.969543933868408, -0.22364115715026855, "[TT] Support Duration of the Commercial Crew Vehicle Emergency Breathing Air Assembly (CEBAA) Regulator Manifold Assembly (RMA) = Up to one hour"]
-[6.97542667388916, 2.8750345706939697, "[TT] Mission Type of the MethaneSAT = EO"]
-[3.5472211837768555, 4.170894622802734, "[FF] SAR Image of the Sentinel-1A = Over La Reunion Island and its coastal area"]
-[12.156850814819336, 4.688692092895508, "[TT] Size of the Bus Structure = ~2 m x 0.8 m in diameter"]
-[7.595798015594482, 8.843116760253906, "[TT] Spectral Band of the MSU-E = 0.6 - 0.7 \u00b5m"]
-[4.51323127746582, 7.426329135894775, "[TT] VHF-band FSK Channels of the UoSAT-12 = 3"]
-[10.967926979064941, 7.573205947875977, "[TT] Swath Width of the AMSR = 1600 km"]
-[3.7913753986358643, -0.7066965103149414, "[TT] Operation Environment of the SSTI = Low-Earth orbit"]
-[9.103813171386719, 7.690354824066162, "[TT] MS (Multispectral) of the Medium resolution = 0.43-0.51 \u00b5m (blue)"]
-[5.482564926147461, 2.521575689315796, "[FF] Development Partners of the JJ-FAST = JICA (Japan International Cooperation Agency) and JAXA"]
-[6.029417991638184, 5.3195366859436035, "[FF] Interoperable Signals of the QZS = L1C, L1-C/A, L2C, L5"]
-[6.2844014167785645, 5.2899169921875, "[FF] Project Overview Author of the Optical Inter-orbit Communications Engineering Test Satellite (OICETS) = Katsuyoshi Arai"]
-[4.640509605407715, 1.5454087257385254, "[TT] Launch Date of the GHGSat-D = June 22, 2016"]
-[14.632512092590332, 6.576598644256592, "[TT] Battery Type of the UK-DMC-2 = Li-ion battery"]
-[7.978003978729248, 4.229638576507568, "[TT] Instrument Type of the RIS = Precision orbit"]
-[11.587285995483398, 6.66732120513916, "[TT] Energy Channels of the Telescopes = E0, E1, E2, E3, E4, E5, E6, E7, E8"]
-[5.927745342254639, 4.994978427886963, "[TT] Data Processing Chains of the TRISHNA = Indian and French payload ground segments"]
-[13.355856895446777, 7.325180530548096, "[TT] Power of the OCM = 134 W"]
-[3.742363452911377, 5.954220294952393, "[FF] Antenna Facilities of the DSN = Goldstone, Madrid, and Canberra"]
-[7.990723133087158, 1.1061155796051025, "[FF] History of the Lanzarote = Long history of eruptions"]
-[13.108241081237793, 7.1769938468933105, "[FF] Output Power of the MPA = Unknown"]
-[10.877029418945312, -0.3114921748638153, "[TT] Conference Date of the TanDEM-X = May 29-31, 2013"]
-[5.263831615447998, 0.7025997638702393, "[TT] Launch Date of the Tandem-L satellites = End of 2022"]
-[5.472114562988281, 5.353693962097168, "[TT] Main Processor of the Command and Data Handling Subsystem = Nexus S smartphone"]
-[14.17406940460205, 3.3773608207702637, "[TT] Weight of the Dosimeter Suite = 70 grams"]
-[9.196603775024414, 2.4474833011627197, "[TT] Nickname of the SpriteSat = Rising"]
-[14.304566383361816, 3.142587900161743, "[TT] Mass of the Baumanets = 80 kg"]
-[6.240185260772705, 0.6842208504676819, "[TT] Actual Launch Date of the Gaia = December 19, 2013"]
-[6.502940654754639, 4.885595321655273, "[FF] Data Destination of the Control Units = SCU"]
-[6.225213050842285, 4.769845962524414, "[FF] Layer 2 Components of the MCS = LMS (Link Management System) and interface to the MOC"]
-[2.0231263637542725, -0.32934218645095825, "[FF] New Discovery of the Van Allen Probes = Temporary third radiation belt, acceleration energy within the belts themselves, and a nearly impenetrable barrier"]
-[11.04554271697998, 6.203442096710205, "[TT] Prism Material of the LAGEOS = 422 fused silica glass, 4 germanium"]
-[9.041845321655273, 7.483706951141357, "[TT] Field of View of the Point-source Detectors = 12km"]
-[13.025217056274414, 7.056019306182861, "[TT] Power Supply Power Requirement of the WCOM = 50 W"]
-[8.003988265991211, 7.194643497467041, "[TT] PID 238 Implementation of the Spacecraft C&DH = Same specification as instruments"]
-[11.205698013305664, 1.5711283683776855, "[TT] Mass of the D-Star One = 3 kg"]
-[4.71255350112915, 0.43154677748680115, "[TT] Launch Year of the S3C = 2024"]
-[7.033802032470703, 4.997300624847412, "[FF] Modes of the AOCS subsystem = MLT, MAS, MGT, MNO, MCO"]
-[6.333893775939941, 7.154484272003174, "[TT] Data Input of the Data Handling System = 11-bit"]
-[4.743106842041016, -1.1378117799758911, "[FF] Predicted Reentry Date of the Chinese Rocket Stage = May 8, 2021"]
-[4.9808759689331055, 0.6956283450126648, "[FF] Service Start Date of the SpaceDataHighway = Nov. 23, 2016"]
-[11.435762405395508, 3.4835453033447266, "[FF] Purpose of the EP (Electric Propulsion) system = Testing"]
-[6.501869201660156, 3.5275144577026367, "[FF] Launch Box Purpose 2 of the RemoveDebris satellite = Protect astronauts from protrusions and sharp edges during handling aboard the ISS"]
-[9.322891235351562, 6.446725845336914, "[TT] FSH Pitch Angle Distribution of the LCI = 130\u00ba x 10\u00ba"]
-[6.823176383972168, 0.6199682950973511, "[TT] Launch Year of the Kepler Space Telescope = 2009"]
-[6.908016204833984, 0.4988940954208374, "[TT] Operation Status of the Kepler = Nominal"]
-[8.383075714111328, 7.290322303771973, "[TT] Instrument Roll Stability of the MBA detector = 0.01\u00ba/s"]
-[5.100619792938232, 2.3226451873779297, "[TT] Destination of the Queqiao = EML-2"]
-[5.302999019622803, 2.69814395904541, "[TT] Operator of the Resurs-P1 = Roskosmos"]
-[14.146028518676758, 3.2548177242279053, "[TT] Mass of the HIRES = 1.12 kg"]
-[8.354593276977539, 8.998297691345215, "[TT] Detector of the Argus = InGaAs with diffractive optics"]
-[3.9907751083374023, 1.9270591735839844, "[TT] Launch Vehicle of the ALOS-2 = Mitsubishi vehicle - an H-IIA F24 bus"]
-[10.996100425720215, 7.640374660491943, "[TT] Swath Width of the Wide Ultra-Fine Mode = At least 50 km"]
-[8.918793678283691, 4.371191501617432, "[TT] Yaw Knowledge of the GFO = Sun sensors"]
-[5.998862266540527, -0.43711185455322266, "[TT] Mission Extension of the WIND = 10 years"]
-[9.580743789672852, -0.48652419447898865, "[TT] Parking Orbit Altitude of the FormoSat-2 = 723 km"]
-[5.625776290893555, 2.0063748359680176, "[TT] Re-entry Location of the Starshine = Atlantic Ocean off the coast of Brazil"]
-[6.248299598693848, -0.018435673788189888, "[TT] Data Distribution of the Aeolus = Near-real time"]
-[7.448369979858398, 3.634918212890625, "[TT] Atmospheric Penetration Depth of the GNSS-RO Instrument = Greater than other radio occultation instruments"]
-[5.03397798538208, 0.7068759202957153, "[FF] System Development Date of the PRARE = April-Mei 1991"]
-[14.517122268676758, 6.752739429473877, "[TT] Voltage of the Li-ion battery (Saft, France) = 24 V"]
-[10.7340726852417, 3.273186683654785, "[FF] Complexity of the Micro-gravity experiment = Most complex one so far"]
-[13.992731094360352, 3.2062361240386963, "[TT] Mass of the MERLIN = 400 kg"]
-[7.412701606750488, 0.9898626804351807, "[FF] URL of the GRAIL = http://discovery.nasa.gov/grail.cfml"]
-[11.94583511352539, 5.020023345947266, "[TT] Size of the OBCom module = 25 mm x 15 mm x 14 mm"]
-[8.651464462280273, 7.6601457595825195, "[TT] Pixel Resolution of the 4-band CCD Imager = 250 m"]
-[13.418389320373535, 5.473542213439941, "[TT] Solar Panels of the IOD-1 GEMS = CSL Double Deploy Solar Panels"]
-[13.004982948303223, 7.066198825836182, "[TT] PMI Power Requirement of the WCOM = 250 W"]
-[6.035806179046631, 4.886587619781494, "[FF] Function of the GPS Receiver = Provide ECEF position and velocity solutions to GNC SW"]
-[6.379599094390869, 1.861954927444458, "[FF] Symposium Date of the eROSITA = June 16-19, 2014"]
-[9.750964164733887, 8.444402694702148, "[TT] Cross Track Full FOV of the ISIR = Approximately 15\u00ba"]
-[5.550949573516846, 6.247056484222412, "[TT] Mass memories of the Data Handling Unit = MM0, MM1, MM2, MM4"]
-[5.767538070678711, 7.179922103881836, "[TT] Comments of the L6 (LEX) = Experimental signal with higher data rate message (2 kbit/s)"]
-[8.028386116027832, 2.1596455574035645, "[FF] Function of the MSU-MR = Global and regional cloud cover mapping, SST (Sea Surface Temperature), and LST (Land Surface Temperature)"]
-[4.942896842956543, 1.9471362829208374, "[TT] Mission Status of the HORYU-2 = Operational (nominal)"]
-[6.238674640655518, 5.303139686584473, "[FF] Brochure URL of the Optical Inter-orbit Communications Engineering Test Satellite (OICETS) = http://global.jaxa.jp/activity/pr/brochure/files/sat09.pdf"]
-[6.206912517547607, 2.2762179374694824, "[TT] Principal Investigator of the LROC = Mark Robinson"]
-[6.366420745849609, 8.067317962646484, "[TT] Number of Channels of the ERB = 22"]
-[6.339235305786133, 7.119717597961426, "[TT] Sampling Rate of the GPS/MET = 50 times per second"]
-[6.78154182434082, 5.834574222564697, "[TT] Quantity of the PDM = 2"]
-[13.338894844055176, 2.9674532413482666, "[TT] Weight of the GRACE-FO Satellites = 600 kg"]
-[10.594480514526367, 2.7834343910217285, "[TT] Expected Lifetime of the NanoSatellite-1B = 5 years"]
-[6.508151054382324, 6.062360763549805, "[TT] Output of the NGAVGS = Real-time video"]
-[7.769905090332031, 2.951059103012085, "[TT] SO2 Emissions of the San Nicolas refinery = Roughly 350 kilotons per year"]
-[6.457736968994141, 6.10919713973999, "[FF] Ground Network Compatibility of the LCT (Laser Communications Terminals) = Tesat LCT DTE and the BridgeSat optical communications ground network"]
-[13.762764930725098, 3.697329044342041, "[TT] Mass of the SAR antenna panel = 290 kg"]
-[5.789114952087402, 3.345386028289795, "[TT] Revenue of the Satellogic = $4.2 million"]
-[10.215913772583008, 5.406921863555908, "[TT] Nominal Cooling Capacity of the Stirling-cycle cryocooler = 780 mW at 75 K"]
-[5.546526908874512, 0.7110011577606201, "[FF] Publication Date of the ASASSN-19bt = 26 September 2019"]
-[9.2684965133667, 4.999460220336914, "[TT] Type of Temperature Sensors of the DSX = 47 AD590s, 16 PRT (Platinum Resistance Thermometers)"]
-[7.435567855834961, 3.396106004714966, "[FF] Maps of the Free-air and Bouguer Gravity Anomaly = Free-air (left), Bouguer (right)"]
-[10.802680969238281, 1.3883798122406006, "[TT] Wind Mass of the Massive Stars = Equivalent of Earth\u2019s mass in a month"]
-[13.968003273010254, 7.195578098297119, "[TT] Voltage of the Voltage 4 = 5.5\u00b12%"]
-[7.967665672302246, 2.37493896484375, "[FF] Sensing Ability of the TEMPEST = Atmospheric moisture and its vertical distribution"]
-[7.991997718811035, 2.369849681854248, "[FF] Purpose of the GCOM-W = Ocean surface evaporation, snow, ice and soil moisture"]
-[3.804788827896118, 4.336043357849121, "[FF] Data Utilization of the RISAT-1 = Agriculture, Disaster Management and other ancillary applications related to oceanography, urban mapping, forest cover"]
-[8.174901008605957, 5.805642127990723, "[FF] Enclosure of the DarkCarb image sensor = Cooled Dewar"]
-[6.174644947052002, 4.589179039001465, "[FF] Objectives of the MCP = To identify and characterize the TLEs (sprites, halos, elves, etc.), to locate the source regions of TLEs over the world, to identify and characterize the strongest lightning flashes, and to trigger other TARANIS instruments which may point out associated events"]
-[10.839326858520508, 7.463676452636719, "[TT] Swath of the DPS = 1000 km"]
-[7.051901817321777, -0.5235179662704468, "[TT] Ascending Node Crossing Time of the CALIPSO = Around 13:30 hours"]
-[3.464679718017578, 4.829926490783691, "[FF] Modes of the RISAT-SAR = Conventional stripmap, ScanSAR, quad polarization stripmap, sliding spotlight"]
-[14.319602966308594, 6.619579315185547, "[TT] On-orbit Maximum Battery Voltage of the Power Subsystem = Within 0.13 V of the predicted value"]
-[3.5770835876464844, 4.772527694702148, "[TT] Primary Payload of the RADARSAT-1 = Synthetic Aperture Radar (SAR) sensor"]
-[6.134250164031982, 6.931782245635986, "[TT] Dataset Rate of the GEOSAT = 10 Hz"]
-[2.959251642227173, 4.440090179443359, "[TT] Ground Resolution (Stripmap mode) of the XSAR = 3 m"]
-[9.37672233581543, -0.4130266010761261, "[TT] Perigee of the STRV-1c and -1d = 620 km"]
-[5.435791492462158, 6.406778812408447, "[TT] Storage of the SDR Host Computer = 250 GB SSD"]
-[10.372293472290039, 2.147510290145874, "[TT] Capability of the NuSTAR = Focusing high-energy X-rays into sharp pictures"]
-[9.016586303710938, 8.128543853759766, "[TT] Number of Focal Plane Modules of the OLI = 14"]
-[8.074814796447754, 9.282690048217773, "[TT] Wavelength of the Ice = 2 \u00b5m"]
-[5.669193744659424, 4.7073540687561035, "[FF] Purpose of the EDRS = Relay user data between LEO satellites, as well as UAVs (Unmanned Aerial Vehicles) in the future, and ground stations"]
-[11.227655410766602, 1.0293391942977905, "[TT] Cube Size of the LISA Pathfinder = 46 mm"]
-[6.092668533325195, 2.3357765674591064, "[FF] Team Lead of the Airborne Topographic Mapper (ATM) = Michael Studinger"]
-[7.722780227661133, 6.683423042297363, "[FF] Image Formats of the C3D2 = Compressed and uncompressed"]
-[9.793436050415039, -1.4591118097305298, "[TT] Space Segment of the Galileo = 30 MEO satellites in 3 planes inclined at 56\u00ba"]
-[8.047361373901367, 1.8275150060653687, "[FF] Measurement of the OCI = Precise measurements of the ocean surface"]
-[8.971789360046387, 5.589344501495361, "[TT] Determination Requirement of the ADCS = 0.5\u00ba"]
-[4.368790626525879, 7.6192402839660645, "[TT] Frequency Range of the GAMALINK = UHF to S-band"]
-[4.179519176483154, 1.933295488357544, "[FF] Orbit of the NigeriaSat-X = Unknown"]
-[9.018563270568848, 4.757357120513916, "[FF] Flight Software Capabilities of the XACT = Autonomously detumbling the spacecraft, searching for the sun, maintaining a sun-pointed coarse attitude, slew to an inertial attitude, maintain 3-axis pointing with relatively high precision over long durations"]
-[5.071533203125, -0.3924262821674347, "[FF] Launch Date of the CBERS 3 = November 2012"]
-[12.804553985595703, 7.597271919250488, "[TT] Instrument Power of the Instrument = 220 W"]
-[8.008308410644531, 1.2413315773010254, "[TT] Quasi-Periodic Eruptions (QPEs) Frequency of the GSN 069 = Every nine hours"]
-[8.159955978393555, -0.6713394522666931, "[TT] Land Ice (large scale) Measurement Accuracy of the CryoSat = 0.17 cm/year"]
-[6.159905433654785, 3.1245181560516357, "[FF] Affected Activities of the CPOM = Shipping, tourism, Arctic exploration, search and rescue"]
-[11.515603065490723, 5.098668575286865, "[TT] Collection Area of the CUTE = 20 cm x 8.5 cm"]
-[4.86236047744751, 0.5923588871955872, "[TT] Year of Launch of the SORCE = 2003"]
-[7.93051290512085, 6.4865498542785645, "[FF] Measurement of the ATLAS = Elevation"]
-[13.451858520507812, 6.780527591705322, "[TT] Electric Power of the Satellite = 2.8 kW"]
-[9.050564765930176, 9.977846145629883, "[TT] Data Quantization of the Eastman Kodak KLI14403 linear CCD sensor = 8 bit or 10 bit"]
-[9.66215705871582, 4.114030361175537, "[TT] Sensitivity of the Magnetic Field Sensor = Sub-picotesla"]
-[8.80652904510498, 2.357863664627075, "[FF] Dust Velocity Distribution Analysis of the GIADA = Dust ejection velocity depends both on the grain size and on time"]
-[4.08107852935791, 6.693068981170654, "[FF] Antenna Gain Requirement of the FormoSat-5 = Unknown"]
-[7.164610385894775, 2.789414644241333, "[TT] Launch Date of the MethaneSAT = 2022"]
-[8.767912864685059, 3.612966537475586, "[TT] Objective of the UVSTAR = Study extended sources of EUV bands"]
-[6.6852498054504395, 1.832014560699463, "[FF] URL of the NASA/JPL = https://www.jpl.nasa.gov/news/news.php?feature=6938&utm_source=iContact&"]
-[8.625236511230469, 4.022146224975586, "[FF] Detected Particles of the SREM = Electrons, protons, and cosmic rays"]
-[7.942906379699707, 9.13357925415039, "[TT] Wavelength Threshold of the CFOSAT = Larger than about 70 m"]
-[9.75057315826416, 2.40143084526062, "[FF] Effective Area of the NuSTAR = Function of off-axis angle, as a fraction of on-axis area, for several energies"]
-[11.958688735961914, 5.077535629272461, "[TT] Vacuum Chamber Volume of the SEIS Instrument = 3 liters"]
-[7.689359188079834, 3.927675485610962, "[FF] Geographical Coverage of the EARS = Large"]
-[3.5779075622558594, 4.880710601806641, "[FF] Features of the Poseidon-4 = Higher performance than the previous generation, new \"interleaved\" SAR operating mode, new architecture improving the role of the digital functions"]
-[6.0286431312561035, 0.8290221691131592, "[FF] Separation Date of the Spektr-RG observatory = Unknown"]
-[8.339203834533691, 7.680708408355713, "[TT] Type of the LWIR and MWIR detectors = HgCdTe detectors"]
-[10.136736869812012, 5.393627643585205, "[FF] Operation of the SIMBA = Measures how much extra energy we need to put in to maintain a fixed temperature"]
-[4.715266227722168, 0.4920346736907959, "[TT] Removal from Service Date of the Monitor-E = August 2008"]
-[11.728278160095215, 6.72256326675415, "[TT] Energy Range of the Instrument = 5-79 keV"]
-[4.34379768371582, 0.9198793768882751, "[TT] Launch Date of the Argos ANGELS = 18 December 2019"]
-[4.888736248016357, 0.5408055186271667, "[TT] Launch Date of the Pathfinder 1 = 2016"]
-[5.142782211303711, 0.17866981029510498, "[TT] Launch Date of the POLAR = Feb 24, 1996"]
-[9.07678508758545, 1.51948881149292, "[FF] Design of the SMP = Small projectile to be shot as soon as the tip of a cylinder-shaped horn touches the asteroid surface"]
-[5.780855178833008, 3.371385097503662, "[TT] SPAC Valuation of the Satellogic = $1.1 billion"]
-[13.59838581085205, 1.7987107038497925, "[TT] Cargo Return of the Starliner = 600 pounds"]
-[7.950657367706299, 2.5968596935272217, "[FF] Function of the AMI = Provides continuous monitoring capability for the near real-time generation of high-resolution meteorological products and long-term change analysis of sea surface temperature and cloud coverage"]
-[9.79804515838623, 4.5617451667785645, "[FF] Components of the Spacecraft Stabilization System = Combination flywheel and magnetic control coil system"]
-[5.987585067749023, 1.0172696113586426, "[FF] Capture Date of the WorldView-1 = 19 August 2021"]
-[8.154861450195312, -0.023378852754831314, "[TT] End of Life Date of the TOPEX/Poseidon = 18 Jan 2006"]
-[5.592939376831055, 7.429980754852295, "[TT] Types of the VSATs = HDR-VSAT and SA-VSAT"]
-[14.118243217468262, 2.967413902282715, "[TT] Mass of the SeaSat = Nearly 2300 kg"]
-[3.2030856609344482, 3.869788885116577, "[TT] Data Supply Agreement of the TerraSAR-X = Until the end of 2020"]
-[4.652339458465576, 0.7602117657661438, "[TT] Contract Award Date of the SBSS-1 Pathfinder = March 2004"]
-[5.04907751083374, 8.429410934448242, "[TT] Spectral range of the MWRI = 10.65-150 GHz"]
-[10.339003562927246, 4.523418426513672, "[TT] Reaction Wheels of the AlSat-2 = 4"]
-[11.228496551513672, 5.397449970245361, "[TT] LYSO crystals of the Range Calorimeter = Side of 5 cm"]
-[5.618890762329102, 0.8576297163963318, "[FF] Test Date of the ISIM = April 2013"]
-[9.848858833312988, 8.280576705932617, "[TT] FOV of the Telescope = 18o (0.314 rad)"]
-[5.82570743560791, 6.0673604011535645, "[TT] Number of Partitions of the SDRAM based memory module = 4"]
-[4.510998725891113, 2.9029922485351562, "[TT] Workshop Location of the SSETI Express = Noordwijk at ESA/ESTEC"]
-[7.426271438598633, 2.901796340942383, "[TT] Capability of the MethaneSAT = Measure emissions from industrial agriculture and other human-made methane sources"]
-[8.074535369873047, 2.6956868171691895, "[FF] Objective of the Experiment = Demonstrate global and real-time space weather observations of near-Earth space"]
-[6.2960920333862305, -0.28070029616355896, "[TT] Operational Span of the ASPOC = 32,000 hours"]
-[8.434553146362305, 7.922861099243164, "[TT] Detector Pitch of the FLIR Boson camera = 12 \u00b5m"]
-[7.084283828735352, 0.2330467700958252, "[TT] Trail Time from Aqua of the CloudSat = \u2264 120 s"]
-[5.383513450622559, 4.796271800994873, "[FF] Design Cycle of the SpooQySat = Shorter development cycle"]
-[5.3157196044921875, 6.213690280914307, "[TT] Data Bus Width of the SDR-SDRAM = 8 bit"]
-[14.248976707458496, 3.194206953048706, "[TT] Mass of the HXT-C = 13.5 kg"]
-[5.746434688568115, 2.1624603271484375, "[TT] Number of Technologies of the CFESat = 8"]
-[6.382595062255859, -0.25592154264450073, "[TT] Communication Attempt Duration of the ALOS = About three weeks"]
-[8.813079833984375, 6.40625524520874, "[TT] Height Measurement Precision of the ALT = 10 cm (rms)"]
-[5.314700603485107, 4.06538724899292, "[TT] Bus Type of the BILSAT-1 = MicroSat-100 bus"]
-[7.026796817779541, 1.8519028425216675, "[FF] Image Credit of the Aqua = NASA Earth Observatory"]
-[4.279979705810547, 4.339349269866943, "[TT] Cost of the COSPAS-SARSAT system = Free"]
-[5.431148529052734, 4.217630863189697, "[TT] Bus Provider of the TRACERS = Millennium"]
-[5.4666523933410645, 7.119093418121338, "[TT] Data Transmission Rate of the MarCO = 8 kbit/s"]
-[7.125292778015137, 4.861011505126953, "[FF] Modes of the CSC Position Guidance = Boost Mode, Coast Mode, Forced Motion Mode"]
-[8.170860290527344, 7.794824600219727, "[FF] Quantum Efficiency (QE) of the NISP IR Detector = Mean specified values"]
-[6.415770530700684, -0.5016008019447327, "[TT] Thrust Duration of the LightSail-2 = One month"]
-[3.2164981365203857, 5.092218399047852, "[TT] Pixel Size of the SAR = 25 x 25 m"]
-[13.259509086608887, 5.3124237060546875, "[TT] Solar Arrays Span of the Spacecraft = Over 40 m"]
-[9.038871765136719, 3.2136175632476807, "[FF] Design Requirements of the Swarm Spacecraft = Magnetic cleanliness, Magnetic field vector attitude knowledge, Ballistic coefficient, Accelerometer proof-mass vs satellite CoG location"]
-[5.919182777404785, 0.3064444661140442, "[FF] Ground Control Development Start Date of the JUICE = 16 January 2018"]
-[6.01153564453125, 1.2004835605621338, "[FF] Review Date of the NASA = June 11, 2015"]
-[5.903547286987305, 4.824952125549316, "[FF] Radio Glitch of the AeroCube-3 = The satellite radio suffered a glitch where it would not acknowledge that the ground station was talking to it"]
-[5.474409580230713, 6.33296537399292, "[TT] Storage Memory of the Satellite = > 512 Gbit"]
-[6.969089984893799, 1.3691126108169556, "[FF] Storm System Analysis Date of the NASA = March 7, 2016"]
-[5.847996234893799, -0.7673208713531494, "[TT] Mission Design Life of the ADEOS spacecraft = 3 years"]
-[10.953231811523438, 6.178511619567871, "[TT] Coating of the Grating = 200 nm gold"]
-[6.162539958953857, -0.36136430501937866, "[TT] Duration of the Simulation = About 11 days"]
-[8.200746536254883, 6.557384967803955, "[FF] Images Taken of the RASAT = 13,362 images"]
-[9.052655220031738, 7.248193264007568, "[TT] Resolution of the Imaging Device = 30 cm"]
-[6.080352783203125, 0.7524459362030029, "[FF] Publication Date of the SphinX = Nov. 2008"]
-[8.506452560424805, 1.3234716653823853, "[TT] 3-Year Prime Salinity Measurement Mission of the Aquarius/SAC-D = November"]
-[5.237216949462891, 3.366640567779541, "[FF] Manufacturer of the SREM = Contraves"]
-[10.745610237121582, 1.461565375328064, "[FF] Mass of the Supermassive Black Hole = Millions to billions times the mass of our sun"]
-[5.673595428466797, 6.499739646911621, "[TT] Raw Data Capacity of the Temporary storage = 30 hrs"]
-[11.508193969726562, 3.3440194129943848, "[FF] Effect of Failure of the AVUM Thrust Vector Control (TVC) system = Inversion of electrical connections, not detected through the different control steps and tests"]
-[14.31875228881836, 3.198904037475586, "[TT] Mass of the VIRR = 8.1 kg"]
-[8.388192176818848, 1.5467638969421387, "[TT] Absolute Accuracy of the Precipitation over water = \u00b1 5 mm/hr"]
-[6.163657188415527, 3.159006357192993, "[TT] Manufacturer of the BlackSky 7 = LeoStella"]
-[5.2619171142578125, 0.6312947869300842, "[TT] First Entry Date of the BEAM = June 6, 2016"]
-[10.230462074279785, 4.465266227722168, "[FF] Function of the Actuator Manager (ACT-MNG) = Distributes the actuations computed by the SC-GNC/FF-GNC (force and torque) to each single thruster and reaction wheels mounted in the spacecraft depending on their configuration"]
-[5.413417816162109, 4.082611083984375, "[TT] Minimum Visible Satellites of the Satnav Receiver = 4"]
-[8.31471061706543, 2.473133087158203, "[TT] Number of Substorms Caught of the THEMIS Constellation = More than five dozen"]
-[9.627215385437012, 5.708690166473389, "[FF] Components of the TM Thermal Calibration System = Single onboard cavity blackbody, black, highly emissive shutter, toroidal mirror, thermistors"]
-[3.073077440261841, -0.04864630103111267, "[TT] Orbital Slot of the GSAT-0103 = C04"]
-[9.660538673400879, 8.247088432312012, "[TT] Pixel Size of the IFOV = 44.6 km x 39.3 km"]
-[8.969223976135254, 5.580944538116455, "[TT] Field of Regard of the AOCS = \u00b126\u00ba"]
-[3.3983957767486572, 6.425414085388184, "[TT] Volume of the Radio and Antenna = 0.25U (2.5 cm x 2.5 cm x 10 cm)"]
-[9.671407699584961, 2.4145257472991943, "[FF] Data Representation of the NuSTAR = Orange circles"]
-[4.985941410064697, -0.35244059562683105, "[TT] Release Time of the Canadarm2 = 6:33 p.m. EST"]
-[5.72048807144165, -0.7580634355545044, "[TT] Number of Long-life Follow-on Satellites of the Block 5D-2 satellite = 9"]
-[9.444069862365723, 4.736587047576904, "[TT] Attitude Control of the ADCS unit = Only attitude sensor during eclipse"]
-[4.955588340759277, 3.933759927749634, "[TT] Developers of the Argos-Next = NASDA and CNES"]
-[7.14103889465332, 3.160295009613037, "[FF] Operation Mode of the GeoSTAR = Continuous"]
-[3.7858407497406006, 6.335064888000488, "[FF] Inflation Issue of the Antenna Mast = Only one of the three antenna masts inflated correctly"]
-[7.51035213470459, 3.7537052631378174, "[TT] Battery Life of the NightPod = More than 6 hours"]
-[10.043085098266602, -1.5321189165115356, "[TT] Orbit Inclination of the ASNARO-1 = 97.4\u00ba"]
-[8.521827697753906, 3.2287378311157227, "[FF] Effect of the SAA = Causing technical disturbances in satellites"]
-[5.642021179199219, 6.593240737915039, "[TT] Usable Cloud-Free Data Collection of the TANSO-FTS-2 = 20% to 46%"]
-[3.304098129272461, 1.5147416591644287, "[TT] Launch Dates of the Sentinel-6 = 2020 and 2026"]
-[13.385173797607422, 7.323246479034424, "[TT] Power Output of the SAC = 37 W (BOL, 27.5 W EOL)"]
-[10.947587966918945, 7.545713901519775, "[TT] Spatial Coverage of the SMOS = Lower at the edges of the swath"]
-[7.903118133544922, 1.3570046424865723, "[FF] Observation Focus of the WCOM = Water cycle and global change"]
-[9.488191604614258, 3.968311309814453, "[FF] Connection to Electronics Boards of the MAG Sensor = Accomplished by a tuned circuit, including the harness"]
-[8.381756782531738, 6.410202980041504, "[TT] Cross-Track Scan Positions of the SSM/T-1 = 7"]
-[7.087581157684326, 5.2852559089660645, "[FF] Components of the KBR = USO (Ultra Stable Oscillator), MWA (Microwave Assembly), horn, IPU (Instrument Processing Unit), SPU (Signal Processing Unit)"]
-[5.892076015472412, 4.739831924438477, "[FF] Navigation Message of the GIOVE-A = Consistent with the transmission protocol"]
-[8.336283683776855, 3.324289083480835, "[TT] Scan Mode of the SSULI = Forms vertical images of the Earth's atmosphere from 750 km to 50 km"]
-[6.255257606506348, 3.312065839767456, "[TT] Function of the WSF-M = Provide critical and actionable environmental intelligence to military operations"]
-[9.228601455688477, 1.8762518167495728, "[FF] Cloud Area Coverage of the HARP = < 4 km x 4 km"]
-[6.948179721832275, -0.38687512278556824, "[TT] Orbits Per Day of the ASTERIA = 15"]
-[10.038969993591309, 7.519280910491943, "[TT] Ground Area of the Pan Scene = 30.7 km x 30.7 km"]
-[4.407132625579834, -0.06857608258724213, "[FF] Readiness of the Starliner = Ready to go"]
-[4.511805057525635, 0.6505377888679504, "[TT] Transfer Date of the DMSP spacecraft = December 23, 1999"]
-[6.304627895355225, 8.637831687927246, "[TT] Polarisation Asymmetry of the CCRs = Eliminated"]
-[6.1619343757629395, 6.960202693939209, "[FF] Reception Stability of the GETR = Stable"]
-[9.020126342773438, 0.5122305154800415, "[TT] Quantity of the Impact Craters = 77"]
-[5.411901950836182, 1.042128562927246, "[TT] Constellation Full Operational Date of the Arktika-M N1 = 2025"]
-[9.232075691223145, 8.078723907470703, "[TT] Time Resolution of the Focal Plane Module = 2 \u00b5s"]
-[7.423300743103027, 2.3956525325775146, "[FF] Purpose of the Landmapper-BC3 = Provide multispectral imagery of 22 m resolution on a swath of 220 km"]
-[7.616637706756592, 3.95054030418396, "[FF] Instruments of the MTSAT = Imager, JAMI, MTSAT DCS, MTSAT Comms, GPS receiver"]
-[6.076436996459961, -0.08363713324069977, "[TT] Testing Duration of the JUICE = 1 month"]
-[10.13230037689209, 9.982945442199707, "[TT] Mission Number of the Vega = 19"]
-[7.406978607177734, 0.25023260712623596, "[FF] Mission Status of the OSIRIS-REx = Rehearsal Time for NASA\u2019s Asteroid Sampling Spacecraft"]
-[8.549514770507812, 4.65136194229126, "[FF] Components of the WINCS = Four electrostatic analyzers (two for ions and two for neutrals) and two mass spectrometers (one for ions and one for neutrals)"]
-[5.48945426940918, 2.4662716388702393, "[FF] Composition of the CAM Core Team = 2 MSc students, 3 PhD students, 3 MSc graduates"]
-[13.756916046142578, 2.860853672027588, "[TT] Mass of the LEO Vantage = 70 kg"]
-[6.165299892425537, 6.343373775482178, "[TT] Delivery Latency of the Tactical Mode = Less than 30 minutes"]
-[12.40579891204834, 0.5947359204292297, "[TT] Orbit Distance of the PLATO = 1.5 million km beyond Earth"]
-[10.08261775970459, -1.569724678993225, "[TT] Inclination of the ADEOS = 98.6\u00ba"]
-[9.744256019592285, 7.076649188995361, "[TT] Ground Cross-Track Range Resolution of the KaRIn = 70 m to 10 m"]
-[8.943520545959473, 3.400775671005249, "[FF] Sun's Activity of the ICON = Quiet phase during solar minimum"]
-[6.174109935760498, 0.2342728227376938, "[FF] Visibility of the Event = About 2,000 years"]
-[6.367201805114746, -0.24901863932609558, "[TT] SIC Temporal Sampling Period of the CIMR = Sub-daily"]
-[3.4237422943115234, 1.8602657318115234, "[FF] GMES Operational services of the Sentinel-2 = Sentinel-2, Optical High Resolution Mission for GMES Operational services"]
-[8.834834098815918, 9.485445022583008, "[TT] Spectral Bands of the TANSO-FTS-2 = 5"]
-[6.049776077270508, 3.45565128326416, "[TT] Number of Experiments of the SMART-1 = 7"]
-[8.349569320678711, 2.5552213191986084, "[FF] In-Track Error of the Ephemeris = Within \u00b1 500 m"]
-[6.9116315841674805, 2.0935170650482178, "[FF] Collaboration URL of the Hinode = http://www.jaxa.jp/article/special/solar-b/1/index_e.html"]
-[6.423702716827393, -0.40298759937286377, "[TT] Period of the SAOCOM-1A and -1B = 97.1 minutes"]
-[7.076220512390137, 7.194286823272705, "[TT] Laser Wavelengths of the CATS = 355, 532, 1064 nm"]
-[8.173370361328125, 6.286702632904053, "[FF] Scan Modes of the CERES on TRMM = Cross-track, along-track, and rotating azimuth plane (RAP) mode"]
-[12.189009666442871, 3.6523494720458984, "[TT] Capacity of the XTA = 60 liters"]
-[4.842256546020508, 7.491719722747803, "[TT] Antenna (Gr/T) of the Unit = -17.4"]
-[6.617928981781006, -0.38294392824172974, "[FF] Lead Time of the Cirrus Plumes = 10 minutes or more"]
-[6.2215495109558105, 2.635716438293457, "[FF] Integration Partner of the Delta IV Heavy = Orion spaceflight vehicle"]
-[7.938821792602539, 7.911970138549805, "[TT] Communication Interface of the HSC-III optics subsystem = Camera Link\u00ae"]
-[3.5516579151153564, 5.217645645141602, "[TT] Look Direction of the Radar = Right or left"]
-[10.727890968322754, 1.5920480489730835, "[FF] Flux and Energy Spectrum of the Neutrons = Variable"]
-[13.729593276977539, 5.391657829284668, "[TT] Solar Cell Type of the Solar Cell Experiment = Monocrystalline silicon"]
-[12.117924690246582, 4.492162227630615, "[TT] Dimensions of the SPOT satellite constellation = 3.5 m x 15.6 m"]
-[3.6746249198913574, 4.920391082763672, "[TT] Deployment Switches of the Radar = 4"]
-[4.31821346282959, 7.202068328857422, "[TT] RF Frequency of the Spacecraft = Ka-band"]
-[4.993992328643799, 3.814896583557129, "[TT] Supplier of the Argos-Next = NASDA/CNES"]
-[8.869544982910156, -0.577724814414978, "[TT] Orbit Period of the P35 series = 98.7 min"]
-[10.947179794311523, 7.556705474853516, "[TT] Swath Width of the NAOMI = 17.5 km"]
-[14.35114860534668, 6.548558235168457, "[TT] Battery Energy of the Satellite = 60 Ah"]
-[4.729976177215576, 6.09185791015625, "[TT] Architecture of the Frontier Radio = SDR (Software Defined Radio)"]
-[10.602470397949219, 7.401922225952148, "[TT] Gap Width of the NSCAT = 330 km"]
-[5.018189907073975, 0.4217086732387543, "[TT] Launch Date of the RHESSI = February 5, 2002"]
-[11.82202434539795, 6.7300872802734375, "[TT] Electron Energy Range of the CPD = 50 keV - 1 MeV"]
-[5.6259870529174805, 1.3719260692596436, "[TT] Mission Control of the IBEX = Boston University"]
-[10.294614791870117, 4.0244317054748535, "[TT] Longitudinal Deployable Boom of the DSAT#1 = Deployed as planned"]
-[14.22429370880127, 3.277052164077759, "[TT] Mass of the iQPS-2 = ~100 kg"]
-[8.137822151184082, 5.774607181549072, "[FF] Output of the DarkCarb image sensor = Proportional to the radiance it receives"]
-[13.425081253051758, 6.843812942504883, "[TT] Power of the INSAT-2A/2B = 1.18 kW"]
-[8.187237739562988, 1.1958658695220947, "[FF] Parameter of the PMI = Snow water equivalence - Soil surface parameters"]
-[4.932056903839111, 7.3373918533325195, "[TT] TT&C Uplink Data Rate of the RF Communications = 125 kbit/s"]
-[7.900468826293945, 7.378480434417725, "[TT] Timing Capabilities of the Detectors = Yes"]
-[8.171778678894043, 7.742210388183594, "[TT] Detector Elements of the SPIRIT-III = 6"]
-[5.074872970581055, 0.6750460863113403, "[FF] Year of the WISE = 2000 and 2001"]
-[4.896116256713867, 5.1807146072387695, "[FF] Communication of the INMCC = Linked to the RCCs and other international MCCs through automatic telex and Aeronautical Fixed Telecommunication Network (AFTN)"]
-[4.5143723487854, 0.11145545542240143, "[TT] Launch Date of the ALL-STAR-1 = April 18, 2014"]
-[10.565600395202637, 2.753551721572876, "[TT] Orbit Altitude of the CADRE nanosatellite = ~400 km"]
-[10.077173233032227, 7.897068977355957, "[TT] Telescope of the Tyvak-0130 = One with a wide field of view"]
-[8.305386543273926, 2.403891086578369, "[FF] Mission Objective of the CALIPSO = Assess the impact of aerosols on Earth\u2019s radiation budget through the aerosol direct and indirect effects"]
-[8.989119529724121, 7.33639669418335, "[TT] Video Resolutions of the NEMO-HD = 1920 x 1080 pixels, 2.8 m GSD, 75 m GSD"]
-[10.16043472290039, 8.074932098388672, "[TT] Telescope WV and IR Focal Length of the MVIRI = 535 mm"]
-[7.1158246994018555, 0.021864263340830803, "[TT] Age of the HD 166191 = 10 million years"]
-[13.749932289123535, 5.359500885009766, "[FF] Solar Array of the Helios-2A and -2B = Two Gallium Arsenide panels and three silicon panels"]
-[5.3921074867248535, 4.055304050445557, "[TT] Number of Satellites of the CIMR = Three"]
-[9.90123176574707, 6.326654434204102, "[TT] Detector Quantity of the D-CIXS = 24"]
-[5.53591251373291, 2.693049430847168, "[TT] Flight Preparation Contributors of the SAPPHIRE = Students at Washington University (WU) in St. Louis, MO"]
-[4.193026065826416, 5.778750896453857, "[TT] Signal Type of the Receiver = ADS-B (Automatic Dependent Surveillance\u2013Broadcast)"]
-[5.387946128845215, 4.943257808685303, "[TT] Contact Initiation Time of the Microhard Ground Station = Five to ten minutes after the expected scheduled contact"]
-[6.214702606201172, 2.3300538063049316, "[TT] Deputy Principal Investigator of the AMS-02 = Stefan Schael"]
-[6.395437240600586, -0.7659372687339783, "[TT] LTAN of the AlSat-2B = 9:30 hours"]
-[11.032195091247559, 6.294164180755615, "[TT] Mirror Material of the Limb Imager = Aluminium"]
-[7.615718841552734, 8.67931842803955, "[TT] Spectral Bands of the Anand = Over 150"]
-[6.788827896118164, 8.75060749053955, "[TT] Type of the POLAS-128 = Polarization-sensitive Acousto-optic Spectrometer"]
-[11.586047172546387, 4.939183712005615, "[TT] Diameter of the M1 = 415 mm"]
-[8.179482460021973, 6.627779006958008, "[TT] Imaging Frequency of the AgCam/ISSAC = 2-4 images per orbit for 4 consecutive orbits"]
-[4.389970779418945, 7.815110683441162, "[TT] Uplink Frequency of the Communication System = 145.95 MHz"]
-[18.799116134643555, 3.478625535964966, "[TT] Mean \u0394N (m) of the Marctan = 1.9"]
-[7.123101711273193, 6.674221038818359, "[TT] False Event Rate of the GLM = Less than 100 events/sec"]
-[5.433941841125488, 6.2344560623168945, "[TT] Memory of the Onboard Computer = 1 GB"]
-[9.361529350280762, 3.6575844287872314, "[FF] Field Location of the Sunspot = Always located at the boundary between the bright region and the umbra"]
-[6.799649238586426, 1.8262372016906738, "[FF] URL of the MEOSAR = http://searchandrescue.gsfc.nasa.gov/dass/index.html"]
-[5.104336261749268, 0.6720477938652039, "[TT] Deployment Date of the AMS-02 = 19 May 2011"]
-[10.646302223205566, 7.318778991699219, "[FF] Swath of the CAVIS = Slightly wider than main instrument"]
-[7.132728576660156, 4.7867865562438965, "[TT] Instrument Builder of the TEMPEST-D = JPL"]
-[6.825254917144775, 2.9334146976470947, "[FF] Components of the Look-Up Table = GFS (Global Forecast System) of the NCEP (National Center for Environmental Prediction)"]
-[8.39493179321289, 7.9459614753723145, "[TT] Scan Step Increment of the Visible Spectral Band = 140 \u00b5rad (N-S scanning)"]
-[8.753002166748047, 1.845968246459961, "[TT] Strongest Winds of the Tropical Cyclone Nathan = 40 knots"]
-[7.730022430419922, 8.779192924499512, "[TT] Spectral Bands of the Optical Arrangement = 36 bands between 0.4 and 14.5 \u00b5m"]
-[9.483848571777344, -0.5840706825256348, "[TT] Altitude of the ICEYE-X1 = 505 km"]
-[18.798931121826172, 3.4793920516967773, "[TT] Mean \u0394E (m) of the Marctan = 6.2"]
-[4.398436069488525, -1.657594919204712, "[FF] Motion of the Blue Ring Nebula = One cone moving almost directly toward Earth, while the other is moving almost directly away"]
-[5.12456750869751, -0.22265011072158813, "[TT] Countries of the CBERS program = Brazil and China"]
-[9.979203224182129, 7.979064464569092, "[TT] Field of View of the STARE telescope = 2.08\u00ba x 1.67\u00ba"]
-[10.677019119262695, 7.36297607421875, "[TT] Swath Width of the OSCAT-3 = 1440 km"]
-[9.561491966247559, 8.976889610290527, "[FF] Topographic Analysis of the Sinus Iridum = Proposed"]
-[7.040282726287842, 1.4240115880966187, "[FF] Purpose of the Proving Ground = Practice with, innovate on, and demonstrate the technologies and capabilities needed to send humans to Mars"]
-[10.044533729553223, 1.290865182876587, "[TT] Capture Time of the Sagittarius dwarf galaxy = 4-5 billion years ago"]
-[9.46368408203125, 0.9198435544967651, "[FF] Distance from Sun of the New Horizons = Unknown"]
-[11.082386016845703, 5.821178913116455, "[TT] Shielding Thickness of the TIDM = 2 mm"]
-[7.143187522888184, 1.2600005865097046, "[FF] Image Acquisition Date of the ExoMars Trace Gas Orbiter = 27 June 2018"]
-[5.289026737213135, 3.2037434577941895, "[TT] Provider of the YouthSat = ISRO"]
-[6.8813605308532715, 8.531183242797852, "[TT] Spectral Sample of the SUCHI = Seven wave channels between 7 and 14 \u00b5m"]
-[5.579346179962158, 4.58462381362915, "[TT] Purpose of the TTP = Technology Transfer Program"]
-[4.6848225593566895, 1.6461234092712402, "[FF] Release Date of the GOSAT-2 = Dec. 12, 2013"]
-[12.365379333496094, 0.58126300573349, "[FF] Unknown of the Plato = Unknown"]
-[4.736716270446777, -1.232397437095642, "[TT] Launch Date of the Beijing-1 = Oct. 27, 2005"]
-[5.3954925537109375, 1.151302456855774, "[FF] Conference Date of the Kaguya (SELENE) = March 10-14, 2008"]
-[5.186872959136963, 0.5297713875770569, "[TT] Activation Date of the LAXPCs = October 2015"]
-[9.919455528259277, -0.31320762634277344, "[TT] Orbit Altitude of the Sentinel-2A = 786 km"]
-[14.267679214477539, 3.1816914081573486, "[TT] Mass of the UNITE = 4 kg"]
-[9.097073554992676, 1.3659206628799438, "[TT] Operation Start Year of the Voyager 2 = 1973"]
-[8.367951393127441, 8.298084259033203, "[TT] Spectral Resolution of the Channels = 0.0002 \u00c5/pixel"]
-[6.655117034912109, 0.482094943523407, "[TT] Age of the Cassiopeia A (Cas A) = 320 years"]
-[4.245630264282227, 7.399106502532959, "[TT] Frequency of the Transmitter = X-band"]
-[6.597302436828613, 5.268402576446533, "[FF] Function of the PD = Provide data and products to the appropriate entities"]
-[6.516501426696777, 1.936395525932312, "[FF] URL of the NuSTAR = http://www.nustar.caltech.edu/uploads/files/helio_decadal_WP_10nov.pdf"]
-[7.146493434906006, 4.380946636199951, "[FF] Purpose of the Switch Matrix = On-Orbit-Verification"]
-[9.647628784179688, 7.20055627822876, "[TT] Spatial Resolution of the Instrument = 28 m x 30 m"]
-[6.6845293045043945, 1.8890148401260376, "[FF] URL of the JPL = https://www.jpl.nasa.gov/news/news.php?release=2017-314"]
-[13.223752975463867, 5.234090328216553, "[TT] Size of the Solar Array = 3 m x 4.9 m"]
-[4.871842861175537, 7.05251407623291, "[TT] Communication System of the CanX-2 = Full-duplex dual-band"]
-[14.087577819824219, 4.051063537597656, "[TT] Mass of the Instrument = 18.20 kg"]
-[11.093517303466797, 1.2978841066360474, "[FF] Technology Demonstration of the LISA Pathfinder = Detect gravitational waves from space"]
-[9.339231491088867, 3.5755271911621094, "[FF] Formation Mechanism of the Sunspot = Mystery of the formation mechanism of a stronger field outside an umbra than in the umbra"]
-[10.837923049926758, -0.27422240376472473, "[FF] Mission Design of the TanDEM-X = Not provided"]
-[5.20480489730835, 1.9858810901641846, "[TT] SOC Deputy Head of the Roman = Cristina Oliveira"]
-[10.061504364013672, 4.403331279754639, "[TT] Torque Coils of the ACS = Six"]
-[14.313035011291504, 2.77203106880188, "[TT] Mass of the KOMPSAT-3 = ~1000 kg"]
-[7.336361408233643, 6.167372703552246, "[FF] Timing Precision of the NICER = Few \u00b5s"]
-[10.869138717651367, -0.31662631034851074, "[TT] First Image Transmission Date of the TanDEM-X = June 24, 2010"]
-[5.394219875335693, 1.7093557119369507, "[FF] Ground Segment Design Team of the EnMAP = M. Habermeyer, T. Storch, S. Eberle, C. Makasy, S. Maslin, A. de Miguel, K.-D. Missling , H. M\u00fchle, R. M\u00fcller, S. Engelbrecht, J. Gredel, U. Heiden"]
-[10.378683090209961, 7.219147205352783, "[TT] Primary Mirror Type of the Shafer Telescope = Scanning mirror"]
-[7.116579055786133, 8.24063491821289, "[TT] SNR for CH4 of the Instrument = \u2265400"]
-[8.526612281799316, 3.143813133239746, "[FF] Measurements of the MAHRSI = Nitric oxide"]
-[5.559458255767822, 3.7393600940704346, "[TT] Quantity of the GOES satellites of NOAA = 2"]
-[7.938067436218262, 3.0905160903930664, "[TT] CO2 Emission Source Resolution of the CO2Image = Below 1 Mt/year"]
-[9.957647323608398, -0.5282406806945801, "[TT] Orbit Altitude of the QSat = 500-700 km"]
-[5.492534637451172, 6.979959964752197, "[TT] Data Download of the STRaND-1 = 372 kB in 5 weeks and 1 day"]
-[8.3524751663208, 5.457667827606201, "[TT] Geolocation Knowledge of the QuickBird-2 = < 15 m (3?) after ground processing"]
-[7.468804836273193, 1.367608666419983, "[FF] Award Date of the Reef Support = 10 December 2020"]
-[8.381658554077148, -0.3903437554836273, "[TT] Range of Values of the Ice: area covered = 0 - 100"]
-[11.440169334411621, 2.1475064754486084, "[TT] \u0394V (cm/s) of the Cosmos 2251 Debris = 2.0"]
-[7.406723976135254, 2.8916752338409424, "[TT] Number of Leaks of the Kayrros Studies = Around 100"]
-[5.43661642074585, 4.001403331756592, "[FF] Quantity of the IoT Devices = More than 50 billion globally"]
-[10.169024467468262, 1.3939783573150635, "[TT] Target Stars of the Gaia = > 1000 million"]
-[5.30190896987915, 0.2985105812549591, "[TT] Mission Status of the RAVAN = Still operating"]
-[6.2185187339782715, 4.551180839538574, "[FF] Functions of the Ground System = MOC (Mission Operations Center) and DPDC (Data Processing and Distribution Center)"]
-[5.99508810043335, 0.8944553136825562, "[FF] Image Capture Date of the Small Monitor Camera = April 16, 2018"]
-[9.586758613586426, 0.8369085192680359, "[TT] Closest Approach Distance of the Rosetta = 3162 km"]
-[5.022933483123779, 0.6382703185081482, "[TT] Start of Science Operations of the NICER-SEXTANT = 17 July"]
-[8.633915901184082, 1.112975001335144, "[TT] Meeting Date of the Aquarius Instrument = Nov. 11-14, 2014"]
-[12.087803840637207, 4.212103843688965, "[TT] Size of the GRACE-FO satellites = 3 m x 3 m x 0.8 m"]
-[9.651385307312012, -1.0498586893081665, "[TT] Orbit Drift of the PARASOL = Eastward"]
-[6.066622734069824, 5.500894546508789, "[TT] Redundancy of the SGR-10 = Redundant pair"]
-[4.8894524574279785, 0.616675853729248, "[TT] Launch Year of the DSAC = 2015"]
-[9.213918685913086, -0.655869722366333, "[TT] Orbit of the AVUM = Transfer Orbit"]
-[6.943369388580322, 6.240860462188721, "[FF] Integration Time of the PROBA-V = Continuously updated"]
-[6.402812957763672, 1.5373077392578125, "[TT] Expected Result Publication Date of the MICROSCOPE = End of 2019"]
-[1.939762830734253, -0.39996206760406494, "[FF] Observation Date of the Van Allen Probes = March 17, 2015"]
-[5.564288139343262, -0.5879907608032227, "[TT] Design Life of the INSAT-3D = 7.7 years"]
-[5.148228168487549, 3.17525577545166, "[TT] Operator of the GeoEye-1 = Maxar Technologies"]
-[9.575504302978516, 3.841672897338867, "[FF] Magnetization of the Rosetta = Not magnetized"]
-[10.229658126831055, 1.571560263633728, "[FF] Specialty of the Brian Metzger = Cosmic mergers \u2013 collisions between a variety of objects, whether they be planets and stars or two black holes"]
-[5.902420997619629, -1.0988825559616089, "[TT] Exceeded Design Life of the SORCE = Yes"]
-[10.086827278137207, 7.01312780380249, "[TT] Along-Track Distance of the MWR = 13.1 km"]
-[7.909668445587158, 1.0184035301208496, "[FF] Eruption Date of the Hunga Tonga-Hunga Ha\u2018apai = 19 January 2022"]
-[9.529541015625, 6.03912353515625, "[TT] Collimator Half Angle of the CID = 5.7\u00ba"]
-[4.957277297973633, -0.23593053221702576, "[TT] Launch Time of the RemoveDebris = 20:30 UTC"]
-[10.345039367675781, 4.0599188804626465, "[TT] Load Range of Shaker Tests of the Boom = 0.048 to 0.00055 kg"]
-[5.106666088104248, 7.064441680908203, "[FF] Transmission Rates of the TT&C subsystem = Uplink: 4 kbit/s, Downlink: Up to 500 kbit/s"]
-[5.065892696380615, 7.27764892578125, "[TT] Data Sampling Capacity of the NorAIS-2 Receiver = Up to 512 MByte"]
-[9.542628288269043, 4.745690822601318, "[TT] Attitude Control of the JL-1-GF03B = 3-axis, 4 flywheels"]
-[7.8122334480285645, 2.785262107849121, "[FF] Emissive Band Uses of the VIIRS = Cloud imagery, precise geolocation, surface temperature determination, cloud top pressure determination, fire detection"]
-[13.152481079101562, 5.397602081298828, "[FF] Deployment of the Sunshield = Folded against the payload module during launch, deployed around the fixed solar array after separation from the launch vehicle"]
-[13.97667121887207, 7.140538692474365, "[TT] Voltage of the Voltage 3 = 5.5\u00b12%"]
-[8.31438159942627, 6.083653450012207, "[TT] Measurement Error of the Overall relative measurement error of radiance in bands 1-3 = 10%"]
-[5.4361701011657715, 6.435820579528809, "[TT] Storage Capacity of the Mission Operation System = More than 2.5 PB"]
-[6.123155117034912, 3.188913106918335, "[FF] Operational Phase of the DSAT-1 = Start of the operational phase"]
-[7.023965835571289, 6.070538520812988, "[TT] Quantity of the CCE = 2"]
-[8.05190372467041, 8.451257705688477, "[FF] Field-Widened Gains of the Spatial Heterodyne Spectroscopy (SHS) = Typically 100"]
-[5.073428630828857, 4.9775590896606445, "[TT] GPS Receivers of the NigeriaSat-2 = 2 SGR-10 (Space GPS Receiver-10) units"]
-[13.929157257080078, 3.061511278152466, "[FF] Mass of the DSX = Unknown"]
-[6.210973739624023, 5.397606372833252, "[TT] Design of the ACC = Modular"]
-[7.245302677154541, 1.1862787008285522, "[FF] Function of the Perseverance = Acquire Mars samples, cache them into sample tubes, and leave the tubes in one or more depots"]
-[6.991836071014404, 6.121898651123047, "[TT] Number of Instruments of the WINCS = 4"]
-[6.252898693084717, 2.5287349224090576, "[FF] Purpose of the European Service Module = Propel NASA\u2019s Orion spacecraft to the Moon"]
-[9.665669441223145, 0.17197348177433014, "[FF] Testing Completion Date of the Parachute System = Unknown"]
-[10.796578407287598, 7.495621681213379, "[TT] Swath Width of the NSCAT = 600 km"]
-[3.1966097354888916, 5.10296630859375, "[TT] Radiometric Resolution of the SAR = 5-bit"]
-[7.103072166442871, 3.0620665550231934, "[FF] Application of the Satellite-based EO = Earth Observation"]
-[4.064204692840576, 7.09066104888916, "[TT] Antenna Coverage of the CXS-810C = Approximately 4\u03c0 steradian"]
-[9.117448806762695, 5.550432205200195, "[FF] Function of the ISS (Image Stabilization System) = Provides jitter removal to < 0.1 arcsec rms"]
-[10.103304862976074, 1.3311553001403809, "[TT] Thick Disc Star Formation End of the Milky Way = Around 6 billion years after the Big Bang"]
-[8.576333999633789, 5.653750419616699, "[TT] Ranging Accuracy of the Galileo = Better than 1.07 m"]
-[4.577231407165527, 3.869781017303467, "[TT] Number of Spare Satellites of the Galileo Constellation = 6"]
-[6.975769996643066, 7.800143241882324, "[TT] Radius of Curvature of the Secondary Reflector = 345.2 mm"]
-[8.023423194885254, 6.5385565757751465, "[FF] Unknown of the Multi-Spectral Optical Scanners = Unknown"]
-[4.217918872833252, 4.3033366203308105, "[FF] Management of the Cospas-Sarsat = National Oceanic and Atmospheric Administration"]
-[4.925405502319336, 0.41290074586868286, "[TT] Launch Date of the VRSS-1 = Sept. 29, 2012"]
-[7.03703498840332, 5.224590301513672, "[FF] Advantages of the DST = Low-cost, stable, easier to collimate"]
-[4.215486526489258, 2.7155141830444336, "[TT] Location of the Pre-CHUVA = Alc\u00e2ntara Launching Center in northeastern Brazil"]
-[9.666916847229004, 7.304851055145264, "[TT] Spatial Resolution of the CO2Image = 50 m x 50 m"]
-[6.969756126403809, 6.908580303192139, "[TT] Model of the Diode Pumped Nd:YAG Laser = RLU"]
-[8.977252006530762, 7.07712459564209, "[TT] Orientation of the Metric Camera = Open cargo bay oriented towards Earth"]
-[9.55884075164795, 4.180666446685791, "[TT] Type of the TAM = Three-Axis Magnetometer"]
-[4.812253475189209, 7.758084774017334, "[TT] Main Processor Frequency of the NSat = 100 MHz"]
-[8.324950218200684, 7.36802339553833, "[TT] Detector Design of the APIS = CMOS"]
-[10.914084434509277, -0.25447893142700195, "[FF] Conference Presentation Date of the TanDEM-X = April 23-26, 2012"]
-[8.069748878479004, 4.253021717071533, "[FF] Measurement Capabilities of the CEASE = Radiation dose, dose rate, surface dielectric charging, deep dielectric charging, and single event effects"]
-[5.8423566818237305, 3.1174674034118652, "[TT] New Fundraising Goal of the Inspiration4 = $200 million"]
-[14.107096672058105, 7.1238555908203125, "[TT] Voltage of the Voltages Available = 28 V, 12 V, 5 V, 3.3 V"]
-[5.559372425079346, 5.342837810516357, "[TT] Type of the BEU = Plug-and-Play"]
-[14.035805702209473, 7.188724994659424, "[TT] Power Supply of the RAMIS = 12 V (M1), 28 V (M2)"]
-[11.885139465332031, 5.410415172576904, "[TT] Size of the Instrument = 45 cm x 20 cm x 20 cm"]
-[8.31054401397705, 2.307046890258789, "[FF] Objective of the Stratus = Measure cloud fraction, cloud top height, and cloud top wind"]
-[3.2800488471984863, 4.782501220703125, "[FF] Conference Presentation of the CSG System = EUSAR 2016, 11th European Conference on Synthetic Aperture Radar, Hamburg, Germany, June 6-9, 2016"]
-[9.733811378479004, 4.480737209320068, "[TT] Attitude Control of the UniSat-3 = Passive magnetic attitude control"]
-[5.65620231628418, 4.862769603729248, "[FF] Objective of the SMDC-ONE = Over-the-horizon communications of unattended ground station (UGS) data"]
-[5.636895656585693, 6.739849090576172, "[TT] Performance Data Transfer of the LPT = Successful"]
-[9.19316577911377, 5.406621932983398, "[TT] Pointing Accuracy of the ACS (Attitude Control Subsystem) = 3.2 arcsec control, 2.7 arcsec knowledge"]
-[6.141026020050049, 7.927420616149902, "[FF] Function of the Shaping Circuit = Reduce the length of the impulses and modify them to allow a numerical encoding"]
-[6.250557899475098, 4.703671455383301, "[FF] Responsibility of the STOC = Payload scheduling, quick-look data analysis, data processing and archiving"]
-[6.320280075073242, 5.3701982498168945, "[FF] Components of the MDHS = FPGA, mass memory and some peripheral components"]
-[14.259846687316895, 3.0389270782470703, "[TT] Mass of the BRITE-PL-1 = 7 kg"]
-[6.4938507080078125, -1.9421058893203735, "[TT] Exceeded Design Life of the Jason-2 = Yes"]
-[11.760427474975586, 3.2020010948181152, "[TT] Thruster Type of the Coronagraph Spacecraft = Monopropellant"]
-[3.6626129150390625, 4.749959468841553, "[TT] Instrument of the Harmony Satellite = Synthetic Aperture Radar"]
-[10.686765670776367, 2.757481336593628, "[TT] Orbit of the PSSCT Nanosatellite = 200 km x 35,786 km x 7\u00ba GTO"]
-[10.456396102905273, 3.2848970890045166, "[FF] CubeSat of the ExoplanetSat = Three-Unit"]
-[14.578743934631348, 6.606122016906738, "[FF] Battery Type of the TacSat-4 = Lithium ion"]
-[4.818361759185791, 7.372014999389648, "[TT] Radio Link Speed of the Ground Station Equipment = 9.6 kbaud"]
-[5.991565704345703, 5.749475955963135, "[TT] FPGA of the PCU = Actel RTSX32SU-CQ84B"]
-[7.076430797576904, 3.7285754680633545, "[FF] Formation Flying of the PROBA-3 = Unknown"]
-[5.493738651275635, -1.8279552459716797, "[TT] Launch Year of the KOMPSAT-5 = 2013"]
-[9.386739730834961, 2.3937435150146484, "[TT] Halos Percentage of the ISUAL = 5.81%"]
-[4.995812892913818, 8.152877807617188, "[TT] Bandwidth of the Ka-band Channels = 900 MHz each channel, 2.7 GHz total"]
-[6.158376216888428, 6.997811794281006, "[TT] Bit Error Rate of the Optical link = 10 -8"]
-[5.1203436851501465, 2.30108380317688, "[TT] Mission Type of the GIOVE = Non-EO"]
-[13.234883308410645, 5.632045745849609, "[FF] Purpose of the Solar Panel = Environment test"]
-[3.7047677040100098, 4.628494739532471, "[FF] Reflector Technology of the SARah = Based on SAR-Lupe and enhanced for SARah"]
-[6.915011882781982, 7.526956081390381, "[TT] A/D Converter of the HSC-III = 14 bit"]
-[11.742853164672852, 4.925421714782715, "[TT] Dimensions of the MTF Target = 48 m x 48 m"]
-[10.374480247497559, 2.0614867210388184, "[FF] Agreement Date of the eROSITA X-ray telescope = Aug. 18, 2009"]
-[7.612504005432129, 4.734304428100586, "[FF] Instrument Suite of the EPI-Hi = IMPACT"]
-[10.868864059448242, 7.505985260009766, "[TT] Swath Width of the MUX = 95 km"]
-[5.081640243530273, 0.4015706181526184, "[FF] Date of the Divine Providencia = 27 March 2022"]
-[5.768795013427734, 0.7382866144180298, "[TT] End Date of the IMAGE = Dec. 2005"]
-[12.498934745788574, 7.489893436431885, "[TT] Power Generation of the Imager = Over 1 W"]
-[3.7954437732696533, 4.720224857330322, "[TT] Accuracy of Cross-Track Velocity Components of the RADARSAT-2 = \u00b10.3 m/s"]
-[6.465900421142578, -1.9139083623886108, "[TT] Exceeded Design Life of the Jason-1 = Yes"]
-[13.439841270446777, 2.88230299949646, "[TT] Tango Satellite Mass of the PRISMA = 50 kg"]
-[10.716423988342285, 3.90171480178833, "[FF] Purpose of the CanX-7 = Deorbit mission"]
-[8.092513084411621, 2.5818212032318115, "[TT] Measurement Domain of the SARAL = Atmosphere, Ocean"]
-[5.489146709442139, 7.354385852813721, "[TT] Bandwidth of the ODTML = > 50 kbit per node per day"]
-[12.449597358703613, 0.597638726234436, "[TT] Measurement Interval of the PLATO CCDs = Every 25 seconds"]
-[8.556502342224121, 7.654087543487549, "[TT] Detector Size of the HSC-III = 1084 x 1024 pixels"]
-[13.26046371459961, 5.506365776062012, "[TT] Installation Date of the ISS Roll-Out Solar Arrays (IROSA) = Summer 2021"]
-[4.807765483856201, 1.1256598234176636, "[TT] Public Listing Date of the Satellogic = Dec. 22"]
-[5.458964824676514, 1.9499903917312622, "[FF] Mission Status of the LADEE = Completed"]
-[9.830137252807617, 8.264752388000488, "[TT] Total Subtended FOV of the Focal Plane Module = 13 arcmin on a side"]
-[10.035494804382324, -1.5263762474060059, "[TT] Inclination of the SAOCOM-1A and -1B = 97.86\u00b0"]
-[6.312500953674316, -0.2727296054363251, "[TT] Duration of the Computer System = 10 hours"]
-[8.884477615356445, 5.674493789672852, "[TT] Pointing Accuracy of the Pointing Mechanism = Better than 0.03\u00ba (500 \u00b5rad)"]
-[5.1567606925964355, 1.1492244005203247, "[FF] Restructured Program Date of the NPOESS = Nov. 2006"]
-[9.293351173400879, 4.796132564544678, "[FF] Operation of the THEIA = Attitude Control"]
-[13.266140937805176, 5.294195652008057, "[TT] Thickness of the Solar Panels = Less than one millimeter"]
-[5.806022644042969, 3.348489284515381, "[FF] Ground System Manager of the JPSS = NOAA"]
-[8.340338706970215, 2.481630563735962, "[FF] Mission of the PARASOL = Observe clouds and aerosols in the A-train"]
-[7.012097358703613, 7.204797267913818, "[TT] Laser Beam Strength of the ATLAS = Decreased by 13 orders of magnitude"]
-[16.50089454650879, 3.586919069290161, "[TT] Commercial Connectivity Services Start of the OneWeb = Late 2021"]
-[9.712834358215332, 4.993422985076904, "[TT] Performance of Rotation Equipment of the Satellite = No degradation"]
-[6.34041690826416, 5.415409088134766, "[FF] Data Format of the VectorSol = Analog or digital"]
-[14.274774551391602, 3.0255582332611084, "[TT] Mass of the VesselSat-1 = 29 kg"]
-[4.388004302978516, 5.430348873138428, "[TT] Launch Date of the GomX-4B = 2 February 2018"]
-[11.986804008483887, -0.11929477006196976, "[TT] Peak Magnitude of the TESS telescope = 15.1"]
-[7.82763671875, 8.134614944458008, "[TT] Band 5 of the R3 Sensor = Red"]
-[5.299234390258789, 2.1619255542755127, "[TT] Mission Type of the ABEX = Non-EO"]
-[10.313474655151367, 5.387289524078369, "[TT] Thermal Reservoir of the Thermal Management Subsystem = 1"]
-[5.747771739959717, 0.9585747718811035, "[TT] Loss Date of the Worldview-4 = January of this year"]
-[4.419271469116211, 7.667275428771973, "[TT] Frequency of the S-band Downlink = 2239.250 MHz"]
-[9.471710205078125, 4.088229656219482, "[TT] Technology of the Magnetometers = Fluxgate sensor by Applied Physics Systems"]
-[4.291316032409668, 2.4863674640655518, "[TT] Launch Center of the FY-3E = Jiuquan Space Launch Center"]
-[6.495614051818848, 5.813117980957031, "[TT] PRN of the GSAT-0103 = 19"]
-[6.553371429443359, -0.4707834720611572, "[TT] Period of the RADARSAT-2 = 100.7 minutes"]
-[10.480768203735352, 4.851396083831787, "[FF] Challenges of the Langmuir Probe = Ground handling equipment and testing methods"]
-[6.585418224334717, -2.056776762008667, "[FF] Meeting Date of the T2L2/Jason2 = Nov. 16-19, 2009"]
-[12.085363388061523, 3.7261974811553955, "[TT] Pressure of the Inflation Pressure = 20,600 bar (3 x 104 psi)"]
-[8.504278182983398, 5.708645343780518, "[TT] Geometric Accuracy of the L1C Products = About 15 m (linear Root Mean Square)"]
-[8.268855094909668, 5.390998840332031, "[TT] Geolocation Accuracy of the RADARSAT-2 = < 10 m"]
-[8.535510063171387, 8.929305076599121, "[TT] Spectroscopy Resolution of the PACS = ~ 75-300 km/s"]
-[7.7220330238342285, -0.8546268343925476, "[TT] Data Collection Start Date of the ICESat-2 = December 11, 2018"]
-[13.268569946289062, 2.9265682697296143, "[TT] Wet Mass of the Standard 3U CubeSat = < 3.78 kg"]
-[8.960467338562012, 7.533512115478516, "[TT] Pixel Size of the TROPOMI = 7000 x 7000 m"]
-[11.688657760620117, 5.602344512939453, "[TT] Wafer Shape of the Collector Array = 10 cm (point-to-point) hexagonal"]
-[9.633125305175781, 4.718491077423096, "[TT] Attitude Control of the SOHLA-1 = Spin-stabilized"]
-[12.201366424560547, -0.20361202955245972, "[TT] Imaging Mode of the TESS = Continuous"]
-[14.14560317993164, 2.9704973697662354, "[TT] Mass of the WNISat-1 = 10 kg"]
-[5.466912746429443, 1.9808107614517212, "[FF] Tool of the ABEX = Cameo Enterprise Architecture"]
-[7.715780258178711, 6.3969879150390625, "[TT] Mesoscale #1 of the ABI = 1 minute"]
-[6.576940059661865, -0.5435755252838135, "[TT] Expected Duration of the Lunar Orbit = Minimum of 6 months"]
-[5.365026950836182, 8.656942367553711, "[TT] Optimum Bandwidth of the Etalon = 80-120 m\u00c5"]
-[8.381131172180176, 5.501298427581787, "[FF] Geolocation Accuracy of the MEOSAR = Unknown"]
-[7.042386531829834, 3.505113363265991, "[FF] URL of paper of the PROBA-3 = http://www.sffmt2013.org/PPAbstract/4111.pdf"]
-[10.288223266601562, 4.484806060791016, "[TT] Torque Coil Power of the Canopus Pipper = ~ 500 mA"]
-[6.924712657928467, 7.775001525878906, "[TT] Reflector Size of the DPS = 1.8 m diameter"]
-[9.723904609680176, 8.440638542175293, "[TT] Range of Observable Flow Angles of the FSU = 56\u00ba FOV"]
-[9.000575065612793, 5.6119866371154785, "[TT] Pointing Accuracy of the iADCS-100 = Well below 1\u00b0"]
-[8.82423210144043, 3.4327008724212646, "[FF] Mission Goal of the ExoCube = Measure the densities of all significant neutral and ionized atom species in the ionosphere"]
-[14.230754852294922, 3.256218671798706, "[TT] Mass of the OBC = 3 kg"]
-[9.3776273727417, 6.266445159912109, "[FF] Best Measurement Position of the IMAP = He 58.4 glow from the crosswind position"]
-[5.987732887268066, 2.858191967010498, "[FF] Deployment From of the DIWATA-1 = ISS Kibo"]
-[14.172224998474121, 3.1209630966186523, "[TT] Mass of the Mayak = 4kg"]
-[5.627769470214844, 6.690025806427002, "[TT] Signal Conditioning Modules of the MnACQ-2000 Miniature Network Data Acquisition System = Included"]
-[4.154105186462402, 0.17727451026439667, "[FF] Launch Date of the Falcon Heavy = 25 June 2019"]
-[9.797796249389648, -0.3507631719112396, "[TT] Altitude of the Quango = About 600 km"]
-[7.0320725440979, 3.7985165119171143, "[FF] URL of the Proba-3 Formation Flying System = https://iafastro.directory/iac/proceedings/IAC-18/IAC-18/A7/3/manuscripts/IAC-18,A7,3,2,x47061.pdf"]
-[8.431243896484375, 6.969812393188477, "[TT] Image Acquisition Request of the ASNARO = Available"]
-[4.146473407745361, 1.3581147193908691, "[TT] End of Service of the Meteosat-7 = End of 2016 or possibly 1st quarter of 2017"]
-[6.674624919891357, 2.153934955596924, "[FF] URL of the H. Kuninaka = http://www.nasa-usa.de/pdf/604314main_6-GER_WS_JAXA-RoboticPrecursor-Kuninaka.pdf"]
-[6.324670791625977, 5.425206184387207, "[FF] Controller of the MMFU = Memory System Supervisor"]
-[4.381061553955078, 2.1237406730651855, "[FF] Objectives of the DubaiSat-2 = Further develop the space program and associated sectors in the UAE, provide continuity and major improvements to the previous DubaiSat mission"]
-[3.879647731781006, 1.9266048669815063, "[TT] Launch Provider of the Falcon-9 V1.1 = SpaceX"]
-[5.451829433441162, 6.8875203132629395, "[TT] Data Connection of the AMS-02 = 2 MB/s"]
-[10.14769458770752, 8.100342750549316, "[TT] Telescope Focal Length of the ASTRO-H = 5.6 m"]
-[13.113323211669922, 7.306277275085449, "[TT] Power Consumption of the Power = 43.5 W"]
-[7.607755184173584, 0.5661906003952026, "[FF] Stability Requirement of the Lunar Orbit = Orbit where the spacecraft doesn\u2019t impact the surface for at least 6 months"]
-[5.18819522857666, 0.4327421486377716, "[TT] Activation Date of the TOR = February 16, 2009"]
-[9.15475845336914, 7.516822814941406, "[FF] Design Requirement of the Camera Boom = Small as it can be within the tiny satellite for launch, then extend from it as far as possible when in space"]
-[2.9101343154907227, 1.955751657485962, "[TT] Image Capture Date of the Copernicus Sentinel-2 = 28 December 2021"]
-[6.42831563949585, 3.4320755004882812, "[FF] Robotic Precision Assembly of the OSAM-1 = Yes"]
-[10.822138786315918, 0.6605666875839233, "[TT] Orbits of Planets of the Kepler-11 = Smaller than Venus and Mercury's"]
-[6.146963596343994, 7.013397216796875, "[TT] Individual Subchannel Data Rate of the Optical Downlink = 38.55Mbit/s"]
-[5.070964336395264, 7.034419059753418, "[TT] High-Gain Dish Link Speed of the TGO = 2 Mbit/s"]
-[5.0767598152160645, 5.266731262207031, "[TT] Tracking Capability of the OEM628 Receiver = Up to 120 signals (60 dual frequency satellites) at any time"]
-[9.667664527893066, 8.184736251831055, "[TT] Lens of the LinkSprite JPEG color VGA camera = 131o FOV wide angle lens"]
-[6.071020603179932, -1.952204704284668, "[TT] Member of the Richard Miller = True"]
-[6.536959171295166, 0.07435529679059982, "[TT] Mission Duration of the CryoSat = Over 10 years"]
-[9.89119815826416, -0.3363868296146393, "[TT] Orbit Altitude of the STARS spacecraft = 666 km"]
-[10.019728660583496, 8.225971221923828, "[TT] Apertures per Channel of the SOLCON = 2"]
-[3.473842144012451, -0.9024246335029602, "[FF] Nominal Operation of the G-EPS = Sunlit part of the orbit"]
-[9.380955696105957, 6.96613883972168, "[TT] Spatial Resolution - MS of the Spacecraft = 4 m GSD"]
-[10.708189010620117, 7.152570724487305, "[TT] Footprint of the 7 = 25.8 x 17.5 km"]
-[5.046173572540283, 0.6331303715705872, "[TT] Mission End of the F-1 = 17.9.1979"]
-[8.083203315734863, 6.559545040130615, "[FF] Purpose of the MWIR = Detect and classify military aircraft"]
-[5.447805404663086, 5.930198669433594, "[TT] Bidirectional Port Protocol of the NIC = UART (Universal Asynchronous Receiver/Transmitter)"]
-[7.263711452484131, 4.895341396331787, "[FF] Instrument Lead of the TEMPEST-D = Sharmila Padmanabhan"]
-[9.813592910766602, 8.626294136047363, "[TT] IFOV of the GLI = 1.25 mrad"]
-[7.696131706237793, 1.3394466638565063, "[FF] Distinction Capability of the ROSE-L = Between vegetated and non-vegetated areas"]
-[7.850851058959961, 7.001106262207031, "[TT] Dynamic Alignment System of the Michelson Interferometer = Equipped"]
-[6.791310787200928, 1.2635517120361328, "[FF] Date of the Satellites Spot Tornado Tracks Across Midwest = 14 December 2021"]
-[10.449382781982422, 5.778059482574463, "[TT] Operating Temperature of the ATLAS = -30 C to 50 C"]
-[7.475570201873779, 6.384013652801514, "[TT] Quantity of the MCP-MC = 2 MicroCameras"]
-[6.514700412750244, 1.8310526609420776, "[FF] URL of the ExoMars = http://m.esa.int/spaceinimages/Images/2016/10/Thumbs_up"]
-[10.945974349975586, 7.5479817390441895, "[TT] Swath Width of the SMMR = About 600 km"]
-[6.252169132232666, 5.589934825897217, "[FF] Function of the FPGA = Receive commands from the CCM, generate all the clocks necessary for driving the CCD and drive the DACs responsible for providing the bias voltages"]
-[9.262960433959961, -1.268056869506836, "[FF] Ideal Geosynchronous orbit located at the GOES east or GOES west station longitude of the Fixed Grid Frame = -"]
-[13.17448902130127, 7.381054401397705, "[TT] Power Consumption of the OBC-Combo = 10 W"]
-[7.745115756988525, 0.950954258441925, "[FF] Date of the Plugging-in Sub-Saharan Africa = 22 March 2021"]
-[6.821624279022217, -0.3481234610080719, "[TT] Roll Maneuver Frequency of the EarthCARE satellite = Once a month"]
-[7.907719612121582, 8.848967552185059, "[TT] Wavelength of the HSC = 0.45 - 0.9 \u00b5m"]
-[10.210637092590332, 0.9915715456008911, "[FF] Distance from Earth of the Kepler supernova remnant = About 20,000 light years"]
-[8.501238822937012, 7.49462366104126, "[TT] Pixel Size of the CMOSIS CHR70M Image Sensor = 3.1 \u03bcm x 3.1 \u03bcm"]
-[5.653204917907715, 7.165748596191406, "[TT] Data Rate of the GEZGIN-2 = 100 Mbit/s"]
-[6.991445541381836, 2.0578155517578125, "[FF] Mission of the Landsat 9 = Monitor Earth's Landscapes"]
-[3.657229423522949, 5.557922840118408, "[TT] PRF of the LRM = 1-4 kHz"]
-[4.7315239906311035, 7.814943790435791, "[TT] Frequency 1 of the Onboard Receiver = 2036.25 MHz"]
-[8.37846565246582, 6.91240930557251, "[FF] Thermal Channels of the Imager = Unknown"]
-[6.1756911277771, 4.66015625, "[FF] Purpose of the GEO = Global Positioning Systems (GPS) and communications"]
-[9.661040306091309, 1.4093847274780273, "[TT] Constellation Quantity of the Pleiades Neo-3 = 4"]
-[10.376007080078125, 2.2381372451782227, "[FF] Function of the HXI = Produce images of the high-energy X-ray universe"]
-[10.537397384643555, 5.753517150878906, "[TT] Surface Temperature of the Thuban = Around 17,500\u00ba Fahrenheit (9,700\u00baC)"]
-[5.95369815826416, 0.8950579762458801, "[FF] Manufacturing Date of the Spaceborne Camera Mirrors = Oct. 4-8, 2010"]
-[14.025958061218262, 3.4013421535491943, "[TT] Mass (kg) of the SARLupe = 770"]
-[9.770763397216797, 8.438892364501953, "[FF] Span of the DSX = Nearly the length of a football field"]
-[12.936153411865234, 7.734334468841553, "[TT] Optical Power Amplifier of the LCT = 5 W"]
-[13.530787467956543, 5.786036014556885, "[TT] Solar Array Power of the Orion = 11.1 kW"]
-[12.97187328338623, 2.926734447479248, "[FF] Mass Range of the CubeSats and nanosatellites = 1-10 kg"]
-[10.479660987854004, 5.787665843963623, "[TT] Temperature Range of the TR Module = -10\u00baC to 60\u00baC"]
-[8.38234806060791, 7.742428302764893, "[TT] Number of Arrays of the Detector Arrays = 2"]
-[4.316163063049316, 0.7947551012039185, "[FF] Launch Date of the EDRS = 29 May 2020"]
-[5.423675060272217, 1.2297866344451904, "[FF] SpaceOps 2010 Conference Date of the Resourcesat-1 = April 25-30, 2010"]
-[8.199692726135254, 4.419722557067871, "[TT] Measurement Objective of the SRM = Measure the total ionizing dose from the population of charged particles at the orbital altitude"]
-[4.402838706970215, 4.267626762390137, "[TT] Number of Satellites of the SAR-Lupe = 5"]
-[5.486972332000732, 3.881112575531006, "[TT] NIIRS of the Satellite = 5 or better"]
-[10.591387748718262, 3.445981025695801, "[TT] Configuration of the Spacecraft = 3U CubeSat carrying a Ka-band payload"]
-[8.64578914642334, 3.0141584873199463, "[FF] Mission Objectives of the Picard = Solar Diameter, Irradiance, Climate, Differential Rotation, Solar Constant and their variations"]
-[9.787189483642578, -0.633280873298645, "[TT] Orbit Altitude of the CBERS-4A = 629 km"]
-[8.821279525756836, 3.3374388217926025, "[FF] Application of the DORIS = All-weather global tracking, ground-beacon positioning, estimate of the total content of ionospheric free electrons"]
-[4.774235248565674, 7.391177654266357, "[TT] Antenna Switch Loss of the Transceivers = 4.5 dB"]
-[10.846595764160156, 7.513055801391602, "[TT] Swath Width of the OCTS = 1400 km"]
-[8.143941879272461, -0.6276148557662964, "[FF] Content of the MERLIN and POLAR science freezers = Biological samples"]
-[5.29836368560791, 0.8929249048233032, "[FF] Launch Date of the SSO-A = 3 December 2018"]
-[9.948023796081543, 2.766964912414551, "[TT] Deployment Tool of the NanoRacks = NRCSD (NanoRacks CubeSat Deployer)"]
-[13.54414176940918, 5.737922191619873, "[FF] Power Source of the LEOStar-3 = Solar Panels"]
-[7.455718040466309, 2.8554089069366455, "[FF] Quote of the ESA's Director of Earth Observation Programs = \"In the public sector, the use of observed data on methane emissions instead of untested assumptions on methane intensity, will improve the accuracy of annual inventories of greenhouse emissions. For governments and regulators, this technology will enable better decisions on energy policy if they can establish a baseline for methane emissions and monitor changes in carbon intensity as they happen.\""]
-[9.033464431762695, 7.26361083984375, "[TT] Effective Sensitive Area of the HXT-C = 70 cm2"]
-[6.322249412536621, 0.5688398480415344, "[TT] Observation Frequency of the ALOS-4 = Once every two weeks"]
-[8.424761772155762, 5.097378730773926, "[FF] CDR Date of the GFO accelerometer = September 2014"]
-[13.365548133850098, 7.760597229003906, "[TT] Output Power of the CC1101 UHF transceiver = Up to 10 mW"]
-[5.036098480224609, 4.367262363433838, "[TT] Active Starlink Terminals Target in India of the Starlink = 200,000"]
-[4.6425299644470215, 1.540926456451416, "[TT] Operational Start Date of the GCOM-W1 = Mid-2013"]
-[9.610922813415527, 8.39629077911377, "[TT] Instantaneous Field of View (IFOV) of the Detector = 0.182 mrad"]
-[8.724190711975098, 0.42368337512016296, "[TT] Intertidal Area Width of the Gulf of Khambhat = Up to 5 km (3 miles)"]
-[14.267657279968262, 3.1981585025787354, "[TT] Total Mass of the PHM = 18 kg"]
-[6.238485336303711, 3.6318931579589844, "[TT] Generation of the DMC (Disaster Monitoring Constellation) = 2nd"]
-[6.628634452819824, 0.5826839208602905, "[TT] Possible Potential Rate of the FORMOSAT-2 = 195"]
-[3.7920522689819336, 6.770672798156738, "[TT] Specific Features of the Altimeter Antenna = Dual-frequency for ionospheric correction"]
-[5.77475643157959, 0.7959461808204651, "[FF] Observation Date of the MAXI = July 13, 2011"]
-[5.688687801361084, -0.9384965896606445, "[TT] Design Lifetime of the SIMBA = 3 years"]
-[9.087721824645996, 5.934381484985352, "[TT] In-Track Look Capability of the NEMO-AM = Slightly less than 90\u00ba"]
-[11.763297080993652, 6.787159442901611, "[TT] Energy Range of the SEM-2 = 42.9 - 300 KeV"]
-[3.8913016319274902, 4.443732261657715, "[TT] Fuel Budget of the RADARSAT-2 = Enough for extensive COLA manoeuvres and de-orbit services"]
-[8.624037742614746, 4.824926376342773, "[FF] Data Correction of the Aeolus = Corrected certain biases"]
-[4.391577243804932, 7.763269901275635, "[TT] Downlink Frequency of the Trisat = UHF"]
-[8.460168838500977, 6.859159469604492, "[FF] Image Size of the ABI = Provided in Table 8"]
-[13.37747859954834, 6.890554904937744, "[FF] Power Consumption Monitoring of the Propulsion System = Of the total propulsion system, of the CGG igniters and the main valve"]
-[5.270483493804932, 3.1148061752319336, "[TT] Manufacturer of the SPIDER = Lockheed Martin"]
-[4.012115478515625, 4.318639755249023, "[FF] Mission Planning of the RADARSAT-2 = Continuous improvement"]
-[7.695414066314697, 8.46505069732666, "[TT] Bands of the MVIRI = 3"]
-[14.630290031433105, 6.655854225158691, "[TT] Battery Configuration of the Canopus Pipper = 1S4P"]
-[7.708863735198975, 0.865382969379425, "[FF] Function of the MRM (Microwave Radiometer, Moon) = Explore the lunar soil properties"]
-[6.192476749420166, 2.399346113204956, "[TT] Principal Investigator of the JEM-X = S\u00f8ren Brandt"]
-[6.835987567901611, -0.6624937057495117, "[TT] Period of the Orbit = 99.31 min"]
-[5.46436882019043, 6.387887477874756, "[TT] Storage Capacity of the Mass Memory System = 2400 Gbit"]
-[6.247326850891113, 4.079528331756592, "[FF] Purpose of the MUSIS = Surveillance, reconnaissance and observation"]
-[5.710309028625488, 6.845946788787842, "[TT] Data Size of the Raw Science Data Packet = 256 bytes"]
-[4.818650722503662, 7.215936660766602, "[TT] Data Transmission Rate of the S-band downlink antenna = 2-4 Mbit/s"]
-[5.084061145782471, 8.667067527770996, "[FF] Center Frequency of the Channel = 10\u03bd, 10h"]
-[8.924362182617188, 5.399651527404785, "[TT] Attitude of the GOMX-3 = Primarily ram-pointing"]
-[8.08264446258545, 0.6327119469642639, "[TT] Groundwater Storage Measurement Date of the GRACE-FO satellites = March 29, 2021"]
-[14.265924453735352, 3.1945619583129883, "[TT] Mass of the Granada = 5 kg"]
-[5.349999904632568, 0.3775339722633362, "[FF] Presentation Date of the CHEOPS = April 20-24, 2015"]
-[8.672738075256348, 2.0294010639190674, "[TT] Wind Speed Measurement Accuracy of the SeaWinds = 2 m/s"]
-[5.5891313552856445, 0.9065997004508972, "[TT] Testing Timeline of the ECP sensors = Within 12 months of launch"]
-[6.958975791931152, 2.121598243713379, "[FF] Mission 1 of the Planet = Ability to image all of Earth\u2019s landmass every day"]
-[8.33019733428955, 3.619575262069702, "[FF] Objective of the AOE = Measurement of atomic oxygen (AO) by silver loss determination in different material specimens"]
-[9.059057235717773, 7.548181056976318, "[TT] Hyperspectral Imagery Resolution of the Satellogic = 30 meters"]
-[6.021137237548828, 4.957679271697998, "[FF] Function of the Inter Satellite Link (ISL) = Range measurement and transfer of data between the two S/C"]
-[10.071768760681152, 7.558166980743408, "[TT] Swath Width of the Imager = 23 km"]
-[8.70141315460205, 4.758930683135986, "[FF] Precision of the Star Tracker = Autonomous"]
-[6.454522132873535, 3.2671780586242676, "[FF] Imagery Delivery of the BlackSky's Satellites = Real-time"]
-[5.1313982009887695, 0.47251221537590027, "[TT] Venting Date of the SXT = October 2015"]
-[10.279219627380371, 1.6943140029907227, "[FF] Number of Isolated Neutron Stars Detected of the eROSITA = Unknown"]
-[9.91518783569336, 7.788473129272461, "[TT] Scan Step Angle of the Telescope = 10 km E-W, every 0.1 s, and 40 km N-S"]
-[7.1170501708984375, 2.6726558208465576, "[FF] Purpose of the SkySat = Provide high-resolution panchromatic and multispectral imagery of any place on Earth multiple times a day"]
-[5.1915507316589355, 2.328207015991211, "[FF] Mission Type of the AEM-2 = EO"]
-[4.408061981201172, 7.175098896026611, "[TT] RF Communications Band of the Kanopus-V 1 = X-band"]
-[8.374813079833984, 7.075204849243164, "[TT] Type of the Imager = Pushbroom with TDI capability"]
-[14.199935913085938, 3.185157060623169, "[TT] Mass of the CanX-6 / NTS = 6.5 kg"]
-[5.886742115020752, 4.753686904907227, "[FF] Transmission Security of the Satellite = Used polarization as a means of transmission security"]
-[4.450167179107666, 1.9713811874389648, "[TT] Launch Provider of the RADARSAT-2 = Starsem"]
-[9.486571311950684, 7.583033084869385, "[TT] GSD (nadir) of the Payload = Pan = \u22642.5 m, MS = \u226410 m"]
-[14.545369148254395, 6.604905128479004, "[TT] Battery Capacity of the IMPS = 45 mAh"]
-[10.511524200439453, 1.2837555408477783, "[TT] UV Light Intensity of the TOI 2076 b = 400 times more than Earth"]
-[12.620027542114258, 9.096982955932617, "[TT] Local Equator Crossing Time of the UniSat-3 = 22:30 hours"]
-[7.0715131759643555, 3.7032856941223145, "[TT] Formation Flying Operation of the PROBA-3 = Several hours"]
-[9.132140159606934, 2.8810153007507324, "[FF] Method of the Cluster spacecraft = Triangulation"]
-[10.334004402160645, 2.3111836910247803, "[FF] Camera Function of the Imaging X-ray Polarimetry Explorer (IXPE) = Measure the polarization of cosmic X-rays"]
-[7.707034111022949, 0.7980204224586487, "[FF] Neutron Production of the Lunar Surface = Constant bombardment by cosmic ray protons"]
-[5.389593124389648, 2.1047890186309814, "[FF] Mission Status of the ST5 = Mission complete"]
-[7.528834342956543, 2.37031626701355, "[FF] Detection Capability of the Microwave and Optical Instruments = Increases in signal levels when marine plastic waste is present"]
-[3.8911190032958984, 6.704350471496582, "[FF] Antenna Type of the RF communications = Monopoles with circular polarization"]
-[9.274085998535156, 4.912498474121094, "[TT] Maneuver of the Satellite = Sinusoidal about 1\u00b0"]
-[8.07053279876709, -1.0354419946670532, "[FF] Data Analysis of the ICESat-2's instrument = Model to convert volume change to mass change"]
-[13.388514518737793, 7.1511311531066895, "[TT] Energy Storage Margin (120 minute window) of the RASP = 71.1%"]
-[3.1895995140075684, 3.817124605178833, "[TT] Design Lifetime of the TerraSAR-X = 5 years"]
-[5.389555931091309, 6.209228038787842, "[TT] Microcontroller Clock Speed of the On-board Computer = 16 MHz"]
-[8.24757194519043, 0.15624193847179413, "[TT] Purpose of the Meteor-M-2 = Weather observation"]
-[5.463242530822754, 6.6495680809021, "[TT] Data Download of the EDRS-SpaceDataHighway = More than 500 terabytes"]
-[8.06573486328125, 4.998992919921875, "[FF] Additional Calibration of the Mini-RF = Conducted on the flight instrument during thermal vacuum temperature ramp cycles"]
-[7.705000400543213, 9.33822250366211, "[TT] Minimum Lower Band Edge of the MS8 (NIR2) = 856 nm"]
-[7.178717613220215, 5.052811622619629, "[FF] Components of the JEM = Pressurized Module (JEM-PM), Exposed Facility (JEM-EF), Experiment Logistics Module-Pressurized Section (ELM-PS), Experiment Logistics Module-Exposed Section (ELM-ES), Remote Manipulator System (JEM-RMS), Inter-orbit Communication System (JEM-ICS)"]
-[4.126440525054932, 5.903641700744629, "[TT] Frequency of the ADS-B = 1090 MHz"]
-[3.4764208793640137, -0.8928972482681274, "[TT] Orbit of the SEOSAT-Ingenio = Sun-synchronous circular orbit"]
-[3.821012258529663, 1.2881275415420532, "[TT] Landing Location of the Falcon 9 first stage = Autonomous spaceport drone ship"]
-[3.8409931659698486, 0.9312118291854858, "[FF] Launch Date of the PSLV-C26 = Unknown"]
-[5.605505466461182, 4.016513347625732, "[TT] Number of DMSP Satellites in Service of the DMSP-F13 = 6"]
-[6.409958362579346, -0.4571384787559509, "[TT] Autonomy of the Satellite = 2 weeks"]
-[5.884214401245117, 3.483916759490967, "[TT] Number of Flights of the Foton = 2"]
-[6.370728969573975, 1.8959343433380127, "[FF] URL of the SCD-2 = https://www.wmo-sat.info/oscar/satellites/view/392"]
-[4.996231555938721, -0.37516239285469055, "[TT] Launch Time of the BRO-1 = 00:12 NZST"]
-[8.623835563659668, 7.673732280731201, "[TT] Pixel Count of the Detector Array (PAN) = 13,500 pixels cross-track"]
-[14.016242980957031, 3.124408483505249, "[TT] Estimated Ejected Material of the Wirtanen = About one million kilograms"]
-[13.372655868530273, 7.565358638763428, "[TT] Peak Pulse Output Power (High Power Mode) of the T/R module = +40 dBm (10 watts)"]
-[6.939979553222656, 9.044564247131348, "[TT] Band Center of the POLDER-1/2 = 565 nm"]
-[8.458374977111816, 4.632550239562988, "[FF] Frame-Dragging Accuracy of the LAGEOS = 2%"]
-[4.87094259262085, 1.7682485580444336, "[TT] Operation Status of the AlSat-2A = Nominal"]
-[5.146429538726807, 0.6130524277687073, "[TT] Date of the Close Approach Event = April 9, 2015"]
-[5.067372798919678, 0.3334386944770813, "[TT] Deployment Date of the MABEL = April 2012"]
-[3.5385866165161133, 6.371603965759277, "[TT] Antenna Baseline of the KaRIn = 10 m"]
-[5.956003189086914, 0.8938696384429932, "[TT] Image Acquisition Date of the Nellis = 17 Aug. 2014"]
-[5.7544169425964355, 3.0428152084350586, "[TT] Annual Spending on Commercial Data of the NASA = Roughly $30 million"]
-[10.05370807647705, 9.178850173950195, "[TT] IGFOV of the MIR, TIR-1 and TIR-2 = 112 \u00b5rad"]
-[5.471805572509766, 2.2324986457824707, "[FF] Affiliation of the Clement Dudal = Unknown"]
-[10.909416198730469, 7.527454853057861, "[TT] Swath width of the MWRI = 1400 km"]
-[9.562618255615234, 9.174880981445312, "[FF] Image Credit of the IRIS = LMSAL"]
-[7.063017845153809, 3.7473061084747314, "[FF] URL of the Proba-3 Formation Flying System = http://www.esa.int/Our_Activities/Space_Engineering_Technology/"]
-[5.868208885192871, 3.199869394302368, "[FF] Number of Spaceships of the Cargo Dragon = 2"]
-[10.417633056640625, 5.717453956604004, "[TT] Temperature Range of the ExoMars Analytical Laboratory Drawer = -120\u00b0C to -60\u00b0C"]
-[6.248939037322998, 4.614431381225586, "[FF] Firing Control of the Picosat Launcher = Ground commandable"]
-[7.129831790924072, 4.54949426651001, "[TT] Mounting Location of the Radiation shielding = Avionics box"]
-[6.070082664489746, -1.960986852645874, "[TT] Member of the Susan Ustin = True"]
-[4.763391494750977, 0.5559942126274109, "[TT] End Year of the MDPP-2 = 2003"]
-[6.4693403244018555, 4.472927093505859, "[FF] Modules of the CBERS-4A = Service Module and a Payload module"]
-[8.517477035522461, 1.357211947441101, "[TT] Salinity Measurement Units of the Aquarius = grams per kilogram"]
-[8.676682472229004, 1.1286896467208862, "[FF] First Map Release Date of the Aquarius = Sept. 22, 2011"]
-[14.705050468444824, 6.6533684730529785, "[TT] Capacity of the Battery = 10.5 Ah"]
-[13.741155624389648, 2.868490695953369, "[TT] Payload Mass of the Resurs-O1 spacecraft = Up to 600 kg"]
-[5.109323978424072, 0.5361798405647278, "[TT] Launch Date of the Dnepr Cluster Mission 2013 = Nov. 21, 2013"]
-[8.702160835266113, -0.6808611750602722, "[TT] Resolution (Initial) of the ICEYE = 10 x 10 meter"]
-[10.959843635559082, 1.5202168226242065, "[TT] Size of the Elysium Star-2 = 1U"]
-[13.2290620803833, 7.2385573387146, "[TT] Initial Heater Power of the CAE System = 80 W"]
-[5.155163288116455, 3.276653289794922, "[TT] Manufacturer of the Dove-4 = Planet Labs Inc. (formerly Cosmogia Inc.)"]
-[4.614462375640869, 7.124853610992432, "[TT] Data Transfer of the NEXTAR-300L = S-band communications"]
-[8.608592987060547, 1.1290217638015747, "[FF] Workshop Date of the Aquarius/SAC-D = May 15-17, 2006"]
-[9.315881729125977, 5.064154148101807, "[TT] Attitude Determination Accuracy of the CADRE = 0.1\u00b0"]
-[6.0955023765563965, 2.176961660385132, "[FF] Caption Author of the VIIRS = Adam Voiland"]
-[5.191407203674316, 2.46785569190979, "[TT] Mission Type of the Monitor-E = EO"]
-[7.849735260009766, 4.885036945343018, "[FF] Sensor of the DMSP Block 4 = Low-resolution VIS (0.4 - 4 \u00b5m) and infrared (8.0 - 12 \u00b5m) sensor"]
-[9.000494003295898, 6.5037760734558105, "[TT] Coordinates of the Image = 230.77\u00baE/73.95\u00baN"]
-[6.40490198135376, 2.329805374145508, "[TT] Wide Survey Coverage of the Euclid Reference Survey = 15000 deg2"]
-[14.197264671325684, 3.1653387546539307, "[TT] Mass of the OPS = 1.9 kg"]
-[9.172626495361328, -0.4582192301750183, "[TT] Orbit Apogee of the PROBA-3 = 60,500 km"]
-[5.720939636230469, 4.316038131713867, "[FF] Development Tools of the EDSN = JIRA, static analysis tools, peer reviews, central repository with subversion tracking, virtual machines"]
-[13.416792869567871, 5.464536190032959, "[TT] Solar Panels of the MicroMAS-1 = Four 3U double-sided deployable solar panels oriented at 120\u00ba angles to the structure"]
-[10.922039985656738, 7.5403947830200195, "[TT] Width Swath of the PMI = >1000 km"]
-[6.004834175109863, 0.9494763612747192, "[FF] Imager Start Date of the IBEX = Late 2016"]
-[7.699106216430664, 9.419353485107422, "[TT] Center Wavelength of the Band 5 = 13.37 \u00b5m (749 cm -1)"]
-[8.500143051147461, 3.8602094650268555, "[FF] Operation of the SIMBA = Turns to the Sun, measuring the amount of radiation coming in"]
-[6.587906360626221, 5.117570877075195, "[FF] Function of the ICDS (Instrument Command and Data Subsystem) = Perform digital data processing of the received signal"]
-[5.170772552490234, 2.294405221939087, "[TT] Mission Type of the WNISAT-1 = EO"]
-[5.215829372406006, 3.2144274711608887, "[TT] Operator of the Beijing-2 = SSTL and DMC International Imaging Ltd (DMCii)"]
-[7.990166664123535, 8.848673820495605, "[FF] Planned Algorithm of the GeoCarb = OCO-2 algorithm, modified to include the longest wavelength band"]
-[10.693408966064453, 4.44183874130249, "[FF] CT Scans of the Valves = Scheduled"]
-[9.928254127502441, -0.061826251447200775, "[TT] Altitude after Five Years of the GRACE Satellite = About 300 km"]
-[4.692608833312988, 2.160989761352539, "[FF] Vicarious Validation Campaign Location of the Deimos-2 = Greenland, Dome-C, Stennis Space Flight Center, Salon de Provence, Baotou"]
-[5.717787265777588, 5.197378158569336, "[TT] Software of the ASPIICS = RTOS (Real-Time Operating System)"]
-[9.724503517150879, 1.5494933128356934, "[FF] Location of the Hoinga = Very far off the galactic plane"]
-[5.448410987854004, 0.6413499712944031, "[TT] Discovery Date of the LIGO = 2015"]
-[5.165262222290039, 6.9212775230407715, "[TT] Command Uplink Speed of the NorSat-3 = Up to 32 kbit/s"]
-[10.216598510742188, 6.616766929626465, "[FF] Shape of the Master = Negative of the final reflective surface of the mirror"]
-[5.95483922958374, 2.382167339324951, "[FF] Conference Date of the WorldView Legion = August 1-6, 2020"]
-[8.507523536682129, 8.838668823242188, "[FF] Sensitivity of the FY-4A = LWIR: 0.5 -1.1 mW/m2 sr cm -1, S/MIR: 0.1-0.14 mW/m2 sr cm -1, VIS: S/N> 200(\u03c1=100%), LWIR: 0.3 mW/m2 sr cm -1, S/MIR: 0.06 mW/m2 sr cm -1"]
-[8.479381561279297, 7.25341272354126, "[TT] Imaging Modes of the Carbonite-2 = Stripmap, Stereo pair and mosaic imaging"]
-[10.030736923217773, 4.757983207702637, "[TT] Speed of the Flywheel = 4500 rpm"]
-[18.79631233215332, 3.479703664779663, "[TT] \u0394r (m) of the Dyess = 5.8"]
-[8.305893898010254, 4.171734809875488, "[FF] Stray Light Mitigation of the DST = Baffles"]
-[8.36906909942627, 4.602790355682373, "[FF] Function of the BEESAT-4 = Gather precise position and orbit determination information, as well as take series of photographs and individual images of Earth's surface with a special camera to confirm the position of the satellite"]
-[7.887282848358154, 0.72711580991745, "[TT] Sea Ice Development Spatial Resolution of the ROSE-L = 20 m"]
-[5.508243560791016, 7.232248783111572, "[TT] Data Rate of the Information data rate per channel = 450 Mbit/s"]
-[9.54796314239502, 4.279662609100342, "[TT] Magnetometer of the ADCS = 3-axes"]
-[11.76850700378418, 3.284609794616699, "[TT] Thruster Thrust of the Propulsion Module = 1 N"]
-[4.584417343139648, 1.6303188800811768, "[TT] Re-entry Date of the HaloSat = 4 January 2021"]
-[8.750060081481934, 2.3442256450653076, "[FF] Dust Flux Measurement of the GIADA = Direct and Reflected Grains"]
-[9.514167785644531, 7.035019397735596, "[FF] Data Resolution of the RAVAN = 10\u00b0 x 10\u00b0 latitude\u2013longitude geographic grid"]
-[7.633574485778809, -2.5000813007354736, "[FF] Data Availability of the GOLD = Continuous, real time"]
-[5.867141246795654, 2.0612752437591553, "[FF] Team of the LightSail-2 = Planetary Society-led team"]
-[4.813571929931641, -1.858983039855957, "[FF] Advanced Small Analyzer for Neutrals(ASAN) of the Chang\u2019e-4 Rover = International Joint Collaboration Payload"]
-[9.927755355834961, -0.38785672187805176, "[TT] Orbit Altitude of the Secondary Payloads = ~410 km"]
-[6.613820552825928, 0.20730319619178772, "[FF] Aggregation Time of the Satellite Measurements = Months or even years"]
-[7.9922308921813965, 5.052915096282959, "[FF] In-Flight Calibrations of the OCI = Repetitive reflectance measurements on reference target sites"]
-[4.961740970611572, -0.3320045471191406, "[TT] Time Between Launches of the Falcon 9 = a little more than 72 hours"]
-[7.218236446380615, 2.5612387657165527, "[TT] Author of the Observation of the Earth and Its Environment: Survey of Missions and Sensors = Herbert J. Kramer"]
-[8.865079879760742, 8.443853378295898, "[TT] Mass of the Miniature High-Resolution Imaging Spectrometer = 5.4 kg"]
-[6.507043361663818, -0.0630587488412857, "[TT] TLE Update Frequency of the ASNARO = Twice per day"]
-[4.013729572296143, 3.484926223754883, "[FF] URL of the Galileo = http://www.gsa.europa.eu/galileo-implementation-search-and-rescue-interfaces"]
-[4.290177345275879, 0.6912018060684204, "[TT] Launch Date of the EDRS-C = 24 July"]
-[5.676197052001953, 4.479025840759277, "[FF] Issue Resolution of the EDSN = Eliminating unnecessary connections and ensuring no floating or undefined values in the software"]
-[8.531645774841309, 4.680908679962158, "[FF] Components of the ADCS = 3-axis gyro sensor, 3-axis magnetometer, sun sensor, Earth sensor"]
-[9.21330738067627, 7.664999485015869, "[TT] Footprint of the LWIR Cameras = 9911 km2"]
-[8.145271301269531, 4.0248870849609375, "[FF] Purpose of the AMS Experiment = Studies charged particles and nuclei in the cosmos"]
-[5.473519802093506, 0.9375500679016113, "[FF] Launch Date of the NINA = Unknown"]
-[7.596527099609375, 3.5356695652008057, "[FF] Observation Scheme of the GLI = Figure 7"]
-[5.627661228179932, 2.4830214977264404, "[FF] Phases of the Euro-Argo ERIC = 2011-2013, 2014+"]
-[4.486691474914551, 1.348239779472351, "[FF] Program Overview of the AlSat-2 = 1 year from launch"]
-[11.985787391662598, -0.1949373334646225, "[FF] Pointing Stability of the TESS spacecraft = Excellent"]
-[11.242459297180176, 5.30468225479126, "[TT] Sample Diameter of the Microcalorimeter = 2.5 cm"]
-[3.759981632232666, 4.5099196434021, "[TT] Imaging Conditions of the RADARSAT-2 = Regardless of weather conditions and the time of day or night"]
-[4.85645866394043, 0.5284141302108765, "[TT] Permanent Failure Date of the B1 Segment = January 2011"]
-[9.95361328125, -1.1056526899337769, "[TT] Slew Rate of the NigeriaSat-2 = 6\u00b0/s"]
-[7.307588577270508, 6.889944076538086, "[FF] Function of the ATLAS = Sends pulses of laser light toward Earth\u2019s ice, land, and water surfaces and derives height from the amount of time it takes for photons to bounce back"]
-[4.767765998840332, 5.203774452209473, "[FF] Tasks of the MCC = Receive data from national LUTs and foreign MCCs, Attempt to match signals coming from the same beacon source, Merge beacon signals from the same source to improve location accuracy, Geographically sort data to determine appropriate recipient of alert message, Transmit alert messages to search and rescue authorities"]
-[8.020256996154785, 6.447869300842285, "[FF] Development Date of the High-resolution Optical Imager = July 5-12, 2009"]
-[3.1781444549560547, 2.3925459384918213, "[TT] Red Edge Bands of the Sentinel-2 = 3"]
-[4.398283958435059, 7.909297466278076, "[TT] Downlink Frequency of the DMSP = 2222.5 MHz"]
-[13.25100040435791, 5.254260540008545, "[TT] Area of the Solar Arrays = 18.3 m^2"]
-[9.90588665008545, 1.7740535736083984, "[FF] Velocity before being Swallowed up by the Hole of the Earth-sized clump of matter = A third of the velocity of light"]
-[8.876203536987305, 2.862338066101074, "[TT] Yearly Trajectory Deflection of the Solar System = Around 115 km"]
-[7.995963096618652, 4.6132001876831055, "[FF] Length of Operation of the Full Calibration of HIS = 1 day accumulated"]
-[3.912353754043579, -1.2773833274841309, "[FF] Potential Locations of the MiniCOR = L1 (Lagrangian Point 1), L4 and L5"]
-[11.593981742858887, 3.4768264293670654, "[FF] Force of the ESP Thrusters = Provides a tangential component force on the exterior"]
-[3.703968048095703, 3.8452908992767334, "[TT] End of Service Date of the RISAT-1 = March 2017"]
-[6.458175182342529, 1.9837664365768433, "[FF] URL of the SARah project = https://www.ohb.de/en/news/2019/satellite-based-radar-reconnaissance-for-germany"]
-[3.4256458282470703, 4.920965671539307, "[FF] Processing Technique of the SAR Images = Analogue techniques, incorporating optical lenses and photographic film"]
-[6.4159345626831055, 3.3810200691223145, "[FF] Goal of the CRS-5 mission = Safely deliver NASA's contracted cargo to the ISS"]
-[5.665345191955566, 2.368039846420288, "[FF] Educational Mission of the ABEX = Publish work on ABEX to conferences and journals"]
-[3.6579666137695312, 5.231705665588379, "[TT] Altitude Range of the MMW Radar = 600 to 1300 km"]
-[6.895964622497559, 1.4501152038574219, "[TT] Expected Release of First Full-Resolution Imagery and Science Data of the Webb = Summer"]
-[5.058016300201416, 1.9093085527420044, "[TT] Status of the CARMEN-1 = Operating nominally"]
-[9.350356101989746, 3.182745933532715, "[FF] Unknown of the Solar Wind Concentrator = Unknown"]
-[9.164881706237793, 3.458650588989258, "[FF] Purpose of the GEOTAIL = Study plasma entry, energization, and transport processes in interaction regions such as the inner edge of the plasma sheet, the magnetopause and the bow shock, and investigate associated boundary layer regions"]
-[5.629395484924316, 0.8846089839935303, "[FF] Terra Carta Supporter Date of the Satellite Vu = September 21, 2022"]
-[5.35657262802124, 3.9462878704071045, "[TT] Quantity of the ICEYE US Satellites = 2"]
-[3.862647771835327, 5.162717819213867, "[TT] Polarization Modes of the RADARSAT-2 = Fully polarimetric quad-polarization (quad-pol)"]
-[7.088863849639893, 9.067644119262695, "[TT] Interference Filter Bandwidth of the GLM instrument = 1 nm"]
-[7.788612365722656, 9.18766975402832, "[TT] Wavelength of the PH2 = 337 \u00b1 5 nm"]
-[10.631845474243164, 7.365865707397461, "[TT] Ground Swath of the TIRS = 185 km"]
-[4.90755558013916, -0.5796674489974976, "[TT] Phase Transition Date of the SLATS = June 1, 2018"]
-[10.244990348815918, -1.3835567235946655, "[TT] Beta Angle of the R3 = -30\u00b0"]
-[7.696835517883301, 9.348458290100098, "[TT] Wavelength of the S-band = 12 cm"]
-[8.022489547729492, 5.29262113571167, "[TT] Calibration Location of the FLLS = SSC (Surrey Space Centre), at the University of Surrey"]
-[6.238409519195557, 2.2213964462280273, "[TT] Principal Investigator of the ShadowCam = Mark Robinson"]
-[9.220792770385742, 6.8894853591918945, "[FF] Mass Resolution of the INMS sensor = The mass resolution is limited by uncertainties in energy dispersion, time resolution and time of flight path"]
-[9.667335510253906, 4.228053569793701, "[TT] Quantity of the 3-axis Magnetometer = 2"]
-[5.143900394439697, 8.639747619628906, "[FF] Center Frequency of the Channel = 89 \u03bd, h"]
-[6.468443870544434, -0.6508772373199463, "[TT] Revisit Period of the TanSat = 16 days"]
-[8.896771430969238, 7.023191452026367, "[TT] Future Test Source Magnitude of the CGI = V=5"]
-[3.7556350231170654, 7.036200523376465, "[TT] Gain of the 23 dBiC circularly polarised quad Yagi antenna = 23 dBiC"]
-[10.777763366699219, -1.0618151426315308, "[FF] Attitude Mode of the SLATS = NM-Z"]
-[3.87178373336792, 4.430083274841309, "[TT] Number of Scenes Annually of the RADARSAT-2 = Up to 10,000"]
-[5.569577693939209, 7.179844379425049, "[TT] Data Rate of the NEXTAR-300L = 800 Mbit/s"]
-[9.968560218811035, -1.4400966167449951, "[FF] URL of the TriG = http://authors.library.caltech.edu/21729/1/"]
-[9.866830825805664, -0.35137251019477844, "[TT] Altitude of the GEO Satellite = About 35,800 km"]
-[8.797869682312012, 2.7234342098236084, "[TT] Error of the Atmosphere = \u00b11.5 K"]
-[7.918294906616211, 8.544435501098633, "[TT] Spectral Range of the HSC-1700 = 400-800 nm"]
-[6.637958526611328, 3.90118145942688, "[FF] Functionality of the HISats = Independent and fully functional with their own propulsion, power, navigation, data processing, communications and payload accommodations"]
-[6.111502647399902, -0.2572653293609619, "[FF] Development Time of the SCIP = Too long"]
-[5.140894889831543, 1.2465859651565552, "[FF] Conference Date of the GOMS = 1991"]
-[11.039406776428223, 0.5821256637573242, "[FF] Effect of the Star-planet tides = Brought the planet inward from its original, wider orbit"]
-[8.348721504211426, 7.202107906341553, "[TT] Funding Source of the Small Monitor Camera (CAM-H) = Contributions from the public"]
-[5.246820449829102, 0.6293606758117676, "[FF] Heritage of the SUSIM = Spacelab-2 (STS-19, July 29-August 6, 1985) and on UARS"]
-[9.08180046081543, 4.56967830657959, "[FF] Capability of the Attitude & Orbit Control Subsystem (AOCS) = Orienting the dual-gimballed data transmission antenna to point towards the required data reception station during the overpass of the CartoSat-2"]
-[11.426552772521973, 5.544535160064697, "[TT] Hardness of the Haynes 242 = 32 HRC"]
-[4.405319690704346, 7.737338542938232, "[TT] Ka-band frequency of the Transmitter/Receiver EMC = 34.4 GHz"]
-[13.867999076843262, 2.790222406387329, "[TT] On-orbit Mass of the FY-2F = 680 kg"]
-[4.340682506561279, 3.146099090576172, "[TT] Ground Control Location of the SSOT = Chile"]
-[5.468535900115967, 6.9994215965271, "[TT] Demodulator Data Rate of the RISAT-1 DRS = 320 Mbit/s"]
-[13.606040000915527, 1.7409496307373047, "[TT] Cargo Weight of the Crew Dragon = More than 500 pounds"]
-[9.689187049865723, 8.394877433776855, "[TT] IFOV of the Imager = 10.5 km"]
-[10.812588691711426, -0.29226914048194885, "[TT] Observation Date of the TWINS = April 6, 2010"]
-[7.813230037689209, 6.534692764282227, "[TT] Imaging Outage Duration of the Satellite = 10 minutes"]
-[7.827469825744629, 2.6940908432006836, "[FF] Purpose of the GOES-West = Provide an infrared look at the clouds"]
-[3.488191604614258, 5.167985916137695, "[TT] Operating Band of the SAR = L-band"]
-[9.692558288574219, 0.16017656028270721, "[FF] Coverage Area of the Parachute System = Almost an entire football field"]
-[7.214083194732666, 6.85981559753418, "[FF] Size of the APD = Very small"]
-[6.2956061363220215, -1.1104934215545654, "[TT] Operation Duration of the GRACE-FO = 1 year"]
-[7.424668788909912, 8.437254905700684, "[TT] Bands of the GOES Sounder = 1 VIS band, 3 SWIR bands, 6 MWIR bands, 9 TIR bands"]
-[3.2313039302825928, 5.780091762542725, "[TT] Dimensions of the SAR Antenna = 2.2 m x 1.5 m panels, measuring 2.2 m x 11.9 m in total"]
-[11.236129760742188, 6.357263088226318, "[TT] Bulk Velocity of the Proton Component Measurement Accuracy of the DSCOVR = 20%"]
-[8.370221138000488, -0.062221214175224304, "[TT] Orbit Altitude of the TOPEX/Poseidon = 158 km apart at the equator"]
-[3.885991334915161, 0.19082006812095642, "[FF] Crash Date of the SMART-1 = 3 September 2018"]
-[6.235507488250732, -0.21557550132274628, "[TT] Unavailability Period of the SST = Up to 20 minutes"]
-[6.014387130737305, 1.4695004224777222, "[TT] Loss Date of the BlackSky Earth-observing satellites = 15 May 2021"]
-[6.778994560241699, 5.923666000366211, "[TT] Quantity of the DPCC = 1"]
-[14.093716621398926, 7.243368148803711, "[TT] Power Supply of the RM = Single unregulated 28 V supply"]
-[5.630450248718262, 7.113195419311523, "[TT] Data Rates of the ODU = 24 and 155 Mbit/s"]
-[8.437000274658203, 8.420974731445312, "[TT] Spectral Resolution of the NOAA/AVHRR-2 = Ch1: .55-0.68 \u00b5m, Ch2: .725-1.0 \u00b5m, Ch3: 3.55-3.93 \u00b5m, Ch4: 10.30-11.30 \u00b5m, Ch5: 11.50-12.50 \u00b5m"]
-[4.882944583892822, -0.23747989535331726, "[TT] Launch Time of the Global-9 = 11:11 UTC"]
-[5.385045528411865, 8.70792007446289, "[TT] Bandwidth of the M3 = 0.02 \u00b5m"]
-[9.565881729125977, 4.283576488494873, "[TT] Magnetometer of the ADCS = 1"]
-[8.154024124145508, 8.476850509643555, "[TT] Spectral Region of the FTS = 665 - 780 cm -1"]
-[6.472989082336426, 7.609903335571289, "[FF] Quantization of the POLDER = 12-bit"]
-[8.195795059204102, 0.6371375322341919, "[TT] Target of the Psyche spacecraft = Psyche, a metal-rich asteroid"]
-[6.334056377410889, -1.235365390777588, "[TT] LST of the KOMPSAT-3 = 1050 hours"]
-[7.174445152282715, 2.524510383605957, "[TT] Author of the Observation of the Earth and Its Environment = Herbert J. Kramer"]
-[10.573692321777344, 3.3575847148895264, "[TT] CubeSat of the Satellite = 1U"]
-[9.121676445007324, 0.7211392521858215, "[TT] Distance Traveled of the InSight = 172 million miles (277 million kilometers)"]
-[3.909578561782837, 4.422747611999512, "[FF] System and Operations Performance of the RADARSAT-2 = Met and surpassed system requirements"]
-[9.568357467651367, 0.581608772277832, "[TT] Lunar Orbit Distance of the Probes = Approximately 400,000 km"]
-[10.95682430267334, 7.346714019775391, "[TT] Swath Width of the Satellite = 80 km"]
-[5.186751365661621, 2.182739734649658, "[TT] Version of the GIQE version 5 = 5"]
-[6.770599842071533, 7.469639778137207, "[TT] Beamwidth of the AMSU = 3.3\u00ba"]
-[7.1412858963012695, 7.84361457824707, "[TT] Noise of the Radiometry = < 0.8 Wm -2  sr -1"]
-[5.77905797958374, 3.191859006881714, "[TT] Support and Maintenance Provider of the GOES = NASA's SAR team"]
-[5.370863914489746, 3.925199270248413, "[TT] Number of Satellites of the COSMO-SkyMed = 4"]
-[6.7001519203186035, -0.4629998803138733, "[TT] Orbit Synchronization Time of the Observatories = About 2 months after launch"]
-[10.14466667175293, 6.92537784576416, "[TT] Satellite Ground Track Range of the TUC Transponder = 3-5 km"]
-[7.603165626525879, 2.3165788650512695, "[TT] Measurement Domain of the Biomass = Land"]
-[7.357440948486328, 0.32446813583374023, "[TT] Principal Investigator of the OSIRIS-REx = Dante Lauretta"]
-[4.285740852355957, 4.298766613006592, "[FF] Formal Understanding with ISRO of the COSPAS-SARSAT = Concerning the long-term provision of INSAT GEOSAR services"]
-[6.76148796081543, 8.430357933044434, "[TT] Total Channels of the Spectral Bands = 159"]
-[5.400320529937744, 0.5716229677200317, "[TT] Launch Date of the IMAGE = 25 March 2000"]
-[5.75425910949707, 6.969292640686035, "[TT] Useful Data Rate of the DPU = 600 Mbit/s"]
-[6.433859348297119, -0.6808507442474365, "[TT] LTDN of the AlSat-2A = 21:30 hours"]
-[11.01030158996582, 2.8921031951904297, "[TT] Size of the SERB Nanosatellite = 10 x 10 x 33 cm"]
-[9.224495887756348, 6.394130706787109, "[TT] Incidence Angles of the PROBA-1 = Five different"]
-[6.847440242767334, 3.475461006164551, "[FF] Development Status of the ALTIKA = Unknown"]
-[7.95651388168335, 8.11016845703125, "[TT] Spectral Band of the Band Photometers = 762.4 nm"]
-[4.952709674835205, 8.343034744262695, "[TT] Center Frequency (GHz) of the SSM/I = 19.35, 19.35, 22.235, 37.0, 37.0, 85.0, 85.0"]
-[5.948542594909668, 4.827827453613281, "[FF] Function of the Thales MissionLINKTM = Provides a reliable connection for voice, satellite internet, cellular data, Land Mobile Radio (LMR) and location-based applications"]
-[9.110405921936035, 7.4123969078063965, "[TT] Resolution of the Camera 2 = 0.3 km/pixel"]
-[6.934534072875977, 4.7215375900268555, "[FF] Interface of the Central Cylinder = Interface with the launch vehicle"]
-[6.28548526763916, 6.113706111907959, "[FF] Provides of the Receiver subsystem = Low noise figures and very good stability for excellent radiometric performance"]
-[4.86392068862915, 8.255748748779297, "[TT] Frequency Conversion of the Poseidon-1 = 13.65 GHz"]
-[5.552661418914795, 0.925865113735199, "[FF] Test Completion Date of the ExoMars Analytical Laboratory Drawer = Unknown"]
-[6.753848075866699, 0.5735071301460266, "[TT] Mission Completion Date of the Kepler = Nov. 14, 2012"]
-[5.316822528839111, 3.6441872119903564, "[TT] Reflector Manufacturers of the Biomass = Harris Corporation (HC) and Northrop Grumman (NG)"]
-[7.383059978485107, 7.964136123657227, "[TT] Dynamic Range of the Instrument = 35 dB"]
-[9.104679107666016, 2.6089162826538086, "[FF] Potential Damage of the Geomagnetic Storm = Collapse the whole telegraph system in North America and Europe"]
-[5.428431510925293, 0.671220064163208, "[FF] Transfer Date of the BEAM = 21 January 2022"]
-[5.662071704864502, 6.782488822937012, "[TT] Data Volume of the Ground Segment = 750 Mbit per orbit"]
-[4.765244007110596, 7.375568389892578, "[TT] Data Transmission Rate of the RF Communications = 9.6 to 500 kbit/s in Ku-band"]
-[8.160956382751465, 7.508328914642334, "[TT] Data Rate of the 4-band CCD Imager = 2.67 Mbit/s"]
-[9.2581148147583, 4.8360748291015625, "[TT] Apogee of the Activity Attitude = 180\u00ba"]
-[8.533743858337402, 5.063858985900879, "[FF] Accelerometer of the Satellite = Femto-g accurate electrostatic differential accelerometer"]
-[5.962042331695557, -0.4836449921131134, "[TT] Mission Duration of the FY-4 = 5 years"]
-[11.603602409362793, 3.5014145374298096, "[TT] Propulsion of the Al Yah-3 = All-electric"]
-[11.31295108795166, 4.771819114685059, "[TT] Inflatable Structure Shape of the DSAT-1 = Octahedron tensegrity"]
-[5.5398783683776855, 2.3125596046447754, "[TT] Team Members of the HORYU-4 = More than 30"]
-[7.5071821212768555, 3.4323253631591797, "[FF] Description of the Level-2 (L2) = Geometric corrected image (the effects of world curvature and state angle are eliminated, image generated using the imaging geometry model without ground control points)"]
-[7.559519290924072, 3.511124610900879, "[TT] Purpose of the Google Earth = Earth surface image generator"]
-[6.39520788192749, 5.4082560539245605, "[TT] Type of the Dione = Prototype"]
-[10.460617065429688, 4.630853652954102, "[TT] Material of the Reaction Wheels = Mu-metal"]
-[3.4677844047546387, -0.8995380997657776, "[TT] Orbit Type of the Beijing-1 = Sun-synchronous circular orbit"]
-[1.7541799545288086, 6.159493446350098, "[TT] Dark Matter Particle Mass of the AMS = 1 TeV"]
-[5.303958415985107, 0.6113142967224121, "[FF] Presentation Date of the SRP SC \u201cTsSKB-Progress\u201d = 2011"]
-[9.13525676727295, 7.435927867889404, "[TT] Multispectral Bands Off-nadir Resolution of the WorldView-3 = 1.38 m"]
-[5.367408275604248, 1.6041735410690308, "[FF] Anomaly of the ALOS-3 = Ignition signals for the SRB-3s were not sent"]
-[14.338812828063965, 3.2929725646972656, "[TT] Mass of the POLDER-2 = 32 kg"]
-[14.269430160522461, 2.885216236114502, "[TT] Mass of the CINEMA-2 = 4 kg"]
-[5.394023895263672, 0.8601730465888977, "[TT] Launch Date of the EFT-1 = December 5, 2014"]
-[9.431113243103027, 3.7342288494110107, "[FF] Function of the Scalar Magnetometer (OVM) = Measure Earth's magnetic field"]
-[9.139250755310059, 7.705181121826172, "[TT] MS (Multispectral) of the Medium resolution = 0.7-0.9 \u00b5m (NIR1)"]
-[13.76156997680664, 2.931870222091675, "[TT] Payload Mass of the ADEOS spacecraft = 1300 kg"]
-[6.180817604064941, 5.764540195465088, "[TT] Type of the CGA = Column Grid Array Packaging"]
-[5.417976379394531, 0.3995510935783386, "[TT] Launch Date of the Cheollian 2B satellite = February 19"]
-[6.3203277587890625, 6.087451934814453, "[TT] Levels of the Data products = 0 and 1"]
-[6.088261127471924, 5.641881465911865, "[FF] Function of the SSR = Data storage and retrieval"]
-[6.802758693695068, 5.893600940704346, "[TT] Quantity of the OMPS = 3"]
-[9.734607696533203, -0.35533764958381653, "[TT] Altitude of the WV-1 = 496 km"]
-[6.341769218444824, 5.088390350341797, "[FF] Function of the OBDH-software = Implements a man-in-the-middle application to manipulate housekeeping data before passing it to ADIA-L"]
-[7.967630863189697, 4.155003547668457, "[FF] Purpose of the Multiple direction/polarisation radiometers = Atmosphere and Ocean observation"]
-[8.418959617614746, 3.217841863632202, "[TT] Accuracy of the Ozone Measurement Instrument = Greater of (20%, 0.1 ppmv) below 15 km"]
-[7.881969928741455, 0.8625456094741821, "[FF] Date of the Maui\u2019s Iconic Waves = 16 May 2022"]
-[9.326932907104492, 5.089837074279785, "[FF] Yaw Control of the Spacecraft = Up to 6\u00ba"]
-[6.670180320739746, 5.223016738891602, "[FF] Type of the PDUs = Bus power distributors using a capacitor bank"]
-[13.386045455932617, 6.740355014801025, "[TT] Power of the Satellite = 2200 W"]
-[9.610095977783203, 1.039766550064087, "[TT] Light Levels of the Rosetta = 4% of those on Earth"]
-[8.169048309326172, -1.1027084589004517, "[FF] Data Correlation of the ICESat-2 = Satellite-derived bathymetry results were correlated with field measurements of the lake taken via boat, helicopter, and land surveyors between June 1974 and September 1976"]
-[6.524886608123779, 3.1747474670410156, "[TT] Revisit Rate of the BlackSky Satellite Constellation = Hourly"]
-[3.7551982402801514, 4.704667091369629, "[TT] Alternate Downlink Locations of the RADARSAT-2 = Up to four"]
-[6.419239521026611, 5.02885627746582, "[FF] Architecture of the FSW = Components and ports"]
-[5.154541969299316, 6.374638080596924, "[TT] SpaceWire Transfer Rate of the OBC = 10 Mbit/s"]
-[14.05744743347168, 3.1248979568481445, "[TT] Weight of the CHRIS = 14 kg"]
-[7.590050220489502, 4.513679504394531, "[FF] Control Authority in Forced-motion Phases of the RVX = Limited"]
-[6.646729946136475, 3.8698995113372803, "[FF] Deployment Method of the Instruments = From boats and ships"]
-[9.599276542663574, 8.071914672851562, "[TT] Number of Lenses of the MOMS-02 = 5"]
-[9.755134582519531, -0.604544997215271, "[TT] Altitude of the Orbit = 628km"]
-[5.1474289894104, 1.2670540809631348, "[FF] Conference Date of the NPOESS Preparatory Project (NPP) = May 26, 2005"]
-[13.219602584838867, 7.205665588378906, "[TT] Power Consumption of the SOLSPC = 32 W"]
-[8.262227058410645, 7.156598091125488, "[TT] Device Type of the IMS/NMS = Mass Spectrometer"]
-[8.076543807983398, 8.829180717468262, "[TT] Wavelength Range (Ultraviolet) of the SOLSPEC = 165 to 370 nm"]
-[4.364802360534668, 6.709341049194336, "[FF] Operating Band of the AIS = VHF maritime band"]
-[10.920341491699219, 10.088640213012695, "[FF] Publication Date of the Alpha Magnetic Spectrometer = Sept. 18, 2014"]
-[3.4813733100891113, -0.8922167420387268, "[TT] Orbit of the CHORUS = Non-sun-synchronous"]
-[9.332723617553711, 0.5290691256523132, "[TT] Maximum Rock Height of the Schiaparelli = 40 cm"]
-[5.200234413146973, 5.957300186157227, "[FF] Nodes of the SpaceWire Link on TacSat-4 = PDH (Payload Data Handler) module in the CDE (Command and Data Electronics) on the bus side and the UIE (Universal Interface Electronics) on the payload side"]
-[6.438572883605957, 2.2141454219818115, "[TT] Deep Survey Coverage of the Euclid Reference Survey = ~40 deg2"]
-[9.956804275512695, -0.41047701239585876, "[TT] Orbit Altitude of the MethaneSAT = 526 km"]
-[11.796401977539062, 6.760780334472656, "[TT] Energy Range of the XRD = 2-15 keV"]
-[10.108694076538086, 7.927058696746826, "[TT] Field of View of the DST (Dobson Space Telescope) = Up to 10 km"]
-[10.987513542175293, 1.3595184087753296, "[FF] Tumbling Behavior of the Starshine = Initially not as expected"]
-[9.411574363708496, -1.379055380821228, "[TT] Eccentricity of the LAGEOS = 0.0045"]
-[6.9218244552612305, -0.2860225439071655, "[FF] Radio Signals of the Hitomi = 3/26 23:49~23:52 (for 3 min) @USC,23:48~23:51(for 3 min) @ KTU"]
-[6.3904595375061035, 4.039363861083984, "[FF] Primary Payload of the NROL-36 = NRO/MSD classified spacecraft"]
-[7.884758472442627, -2.462960958480835, "[FF] Imaging of the GOLD = Ionosphere"]
-[6.594539165496826, 1.5407496690750122, "[FF] Purpose of the Europa Clipper = Measure Europa's gravity field"]
-[7.864865779876709, 2.14182186126709, "[FF] Measurement of the Ocean Colour and Temperature Scanner (OCTS) = Ocean colour and sea surface temperature"]
-[4.442722320556641, 2.9387409687042236, "[TT] Location of the NOAA Fairbanks, AK Tracking Station = Fairbanks, AK"]
-[7.04066801071167, 5.962571620941162, "[TT] Units of the SET-1 = CEM (Correlative Environment Monitor) and CCA (Central Carrier Assembly)"]
-[10.010080337524414, 2.847414016723633, "[TT] Launch Time of the COPPER CubeSat = 01:15:00"]
-[13.338556289672852, 2.944614887237549, "[TT] Mass (kg) of the RADARSAT-1 = 2200"]
-[11.251729965209961, 5.993712902069092, "[TT] Technology of the SMARD = Shape-memory alloy (Nitinol)"]
-[7.6730055809021, -2.5335233211517334, "[TT] Power On Time of the GOLD instrument = Jan. 28, 7:23 p.m. EST"]
-[13.830832481384277, 5.3083295822143555, "[TT] Technology of the Solar array = Triple junction GaAs cell"]
-[4.291231155395508, 6.428948402404785, "[FF] Parameter Derivation of the Antenna = Ta = Tref - \u03b7 Tn"]
-[8.893016815185547, -0.36148619651794434, "[TT] Inclination of the Meteor-M2-3 = 98.8\u00ba"]
-[3.8086721897125244, 4.893586158752441, "[FF] Signal Field Strength Graph of the LituanicaSat-1 = Data"]
-[9.498005867004395, 2.898481607437134, "[TT] Peak Energy Deposition Separation of the Solar SXR Spectra = About 5 km"]
-[7.3609161376953125, 4.650577068328857, "[FF] Component of the TRD gas supply system = Unknown"]
-[12.152454376220703, 4.459877014160156, "[TT] Spacecraft size (main body) of the GOSAT-2 = 5.3 x 2.0 x 2.8 m"]
-[7.594912528991699, 1.443864345550537, "[FF] Data Release of the SeaSat = Open release of all data to all interested scientists and engineers"]
-[5.221471786499023, 4.372250556945801, "[TT] Number of Tracked Satellites of the GPS/MET = Up to eight GPS satellites"]
-[9.796638488769531, 2.667295455932617, "[TT] Location of the NanoRacks LLC = Houston, TX"]
-[5.571465969085693, 0.933989942073822, "[FF] Satellite Launches of the Space Flight Laboratory = Five in Two Weeks"]
-[5.271700859069824, 2.825146436691284, "[TT] Operator of the Arktika-M N1 = ROSCOSMOS"]
-[6.392761707305908, 7.008763790130615, "[TT] Modulation Type of the SILEX Optical Terminal = OOK-NRZ / 2-PPM"]
-[3.8956387042999268, 7.875882148742676, "[TT] Modulation of the Transmitter = 1200 bit/s FSK / 1 bit/s CW"]
-[5.925037384033203, 6.191709518432617, "[TT] Data Transfer Time from Satellite to Ground of the EDRS = More than an hour"]
-[6.487398624420166, 5.313769817352295, "[FF] Role of the DCS = Unknown"]
-[7.721815586090088, 9.031582832336426, "[TT] Wavelength Range of the Band 1 = 0.45-0.49 \u00b5m"]
-[9.797135353088379, -0.3751315772533417, "[TT] Altitude of the MICROSCOPE = 710 km"]
-[8.645913124084473, 8.803236961364746, "[TT] Wavelength Range of the Grating Reflection Unit = 750nm to 775nm"]
-[9.365776062011719, 0.3666979670524597, "[TT] Additional Gathering Line Length of the PHMSA Rule = 20,336 miles"]
-[7.304438591003418, 9.027092933654785, "[TT] SBF (Solar Blocking Filter) Spectral Width of the GLM = ~3 nm FWHM"]
-[13.039689064025879, 6.200695037841797, "[FF] Structural Thermal Model of the HORYU-2 = -"]
-[8.167437553405762, -0.6561808586120605, "[FF] New Applications of the SMOS = Permafrost and thawing monitoring in the boreal forest, ice thickness determination in the Arctic Ocean, hurricane wind observations"]
-[10.225345611572266, 7.589554786682129, "[TT] Telescope Type of the SBSS = Two-axis, gimballed optical telescope"]
-[7.016233921051025, 1.9142155647277832, "[FF] On-Orbit Geometric Calibration of the Landsat-7 = Four Years"]
-[6.480381965637207, 3.1168503761291504, "[TT] Remapping Frequency of the 90-satellite constellation = Weekly"]
-[8.146620750427246, 2.7739386558532715, "[TT] Measurement Domain of the GOSAT-2 = Atmosphere, Land"]
-[6.662484169006348, 6.040617942810059, "[TT] Quantity of the TRC = 288"]
-[6.36147403717041, 4.010015487670898, "[FF] ReBroadcast (GBR) of the GOES-R = Volume 4"]
-[6.048327445983887, 3.843777656555176, "[FF] Architecture of the AstroSat-250 = AstroBus-L"]
-[11.884624481201172, -0.13073329627513885, "[FF] URL of the TESS = https://www.nasa.gov/feature/goddard/2020/nasa-s-tess-enables-breakthrough-study-of-perplexing-stellar-pulsations"]
-[14.489949226379395, 6.602373123168945, "[TT] Battery Capacity of the Spacecraft = > 30Ah @ EOL"]
-[12.25152587890625, 2.9586877822875977, "[TT] Hydrazine Consumption of the Envisat = 25.8 kg on average per year"]
-[11.881304740905762, 6.69861364364624, "[TT] Electron Energy Range of the HEPS = 1.5-20 MeV"]
-[4.613071918487549, 7.428165435791016, "[TT] UHF Downlinks Data Rate of the UoSAT-12 = 9.6 and 38.4 kbit/s"]
-[8.191784858703613, 8.405303955078125, "[TT] Emissivity (\u03b5) of the FCA = 0.8"]
-[14.629858016967773, 6.750585556030273, "[TT] Battery Packs Quantity of the EPS = 3"]
-[5.100709915161133, 3.3545687198638916, "[TT] Manufacturer of the SpaceEye-T = Satrec Initiative"]
-[9.1907377243042, 7.519175052642822, "[TT] Field Size of the Optical Payload = 2.08\u00ba x 1.67\u00ba"]
-[5.090116024017334, 2.355496644973755, "[TT] Mission Type of the RemoveDebris Mission = Non-EO"]
-[8.888394355773926, 7.245389461517334, "[TT] Limb-Viewing Section Pixels of the SIS = 24 cross-track pixels and 8 along-track pixels"]
-[4.877684593200684, 7.308318614959717, "[TT] Data Rate of the S-band = 66.54 kbit/s"]
-[11.7802734375, 3.2980825901031494, "[TT] Thrust of the Thrusters = ~10 \u00b5N"]
-[6.644476890563965, 1.1140937805175781, "[FF] Image Date of the Extratropical Cyclones = 26 October 2021"]
-[4.65848970413208, 6.977573394775391, "[TT] Payload Data Downlink of the PRISMA = X-band"]
-[7.118093013763428, 6.650693416595459, "[FF] Optics Fiber Channel of the FIBOS = Transfer the light from the laser"]
-[9.566988945007324, 4.760830879211426, "[TT] ADCS of the IOD-1 GEMS = Attitude Determination and Control Subsystem"]
-[10.784196853637695, 1.3873655796051025, "[TT] Mass of the SS 433 = About 10 times the mass of our Sun"]
-[6.605366230010986, 6.302854061126709, "[FF] Laser Link of the Sentinel-1A = Excellent stability and robustness"]
-[5.870112419128418, 1.352769136428833, "[FF] Initiative Date of the Small GEO Satellite = April 16, 2007"]
-[4.81929349899292, 4.741506099700928, "[FF] Signal Data Provider of the AMBER IOD-3 = National Maritime Information Centre (NMIC)"]
-[3.6182467937469482, 4.5789971351623535, "[TT] Operation of the Synthetic Aperture Radar (SAR) = Day or night, when skies are cloudy or clear"]
-[11.167710304260254, 5.70168399810791, "[TT] Thickness of the Device = 100 \u00b5m"]
-[7.140341758728027, 7.396646022796631, "[FF] Type of the MABEL = Photon-counting Altimetry"]
-[5.332162380218506, 3.9515891075134277, "[TT] Number of Satellites of the Constellation = 10"]
-[4.002401828765869, 7.831990718841553, "[TT] Modulation Type of the Low-rate Modulation = 9 kbit/s residual carrier PM"]
-[6.523815155029297, 2.217637538909912, "[FF] URL of the Advanced Communication Technology Satellite (ACTS) = http://acts.grc.nasa.gov/technology/spacecraft/specs.shtml"]
-[6.712172985076904, 4.527217388153076, "[FF] Description of the Orthorectified Product (L1C) = The product is derived from the L1 product and geometrically corrected (correction of sensor, satellite motion and terrain related distortions) and re-sampled to a specified grid (orthorectified)"]
-[6.380550384521484, -0.02615252137184143, "[TT] Production Frequency of the SST Product = Every 10 minutes"]
-[10.082804679870605, -1.5507944822311401, "[TT] Inclination of the GOMS-1 = < 0.5\u00ba"]
-[13.404757499694824, 7.78239107131958, "[TT] Power of the RF output power = +5 dBm \u00b1 1 dB"]
-[6.4447455406188965, 1.0994080305099487, "[FF] Interface Requirement Document of the FORMOSAT-7/COSMIC-2 = FS7-IRD-0002"]
-[6.080594539642334, 2.559654712677002, "[TT] Mission of the COWVR = Space Test Program-Houston 8 (STP-H8)"]
-[7.836277008056641, 9.083666801452637, "[TT] Wavelength Range of the LOM = >50 pm"]
-[6.493290901184082, 7.603886127471924, "[TT] Data Quantization of the Instrument = 10 bits"]
-[5.913370132446289, 2.7433114051818848, "[FF] Funding Status of the Worldview Legion = Fully able to fund"]
-[9.454984664916992, 6.948405742645264, "[TT] Resolution of the Angular resolution = 1.2 +0.2 mrad"]
-[6.440675258636475, 4.112527847290039, "[FF] Validation Facilities of the SWOT = Efficient"]
-[8.124356269836426, 3.9543771743774414, "[FF] Purpose of the Carmen-2 = Study the influence of space radiation on advanced components"]
-[14.020474433898926, 3.731674909591675, "[TT] Mass of the LaserCom = 14.3 kg"]
-[5.96343469619751, 0.7017762660980225, "[TT] Discovery Year of the W\u2013 boson = 1983"]
-[7.616538047790527, 8.25527572631836, "[TT] Number of MS bands of the FPA = 4"]
-[10.070649147033691, -1.5182808637619019, "[TT] Orbit Inclination of the PAZ = 98\u00ba"]
-[5.455587863922119, 6.403591156005859, "[TT] Onboard Storage Capability of the OceanSat-1 = 320 Mbit"]
-[13.502521514892578, 5.759974956512451, "[TT] Power Generation of the SPOT-1 = Solar array"]
-[3.345916986465454, 4.945455551147461, "[FF] Polarimetric SAR Interferometry of the TDX/TSX = Combines interferometric with polarimetric measurements"]
-[4.930226802825928, 6.159466743469238, "[FF] Telemetry Packet Forwarding of the Delfi-n3Xt = Worldwide amateur radio community"]
-[13.401477813720703, 5.646013259887695, "[TT] Solar Array Output of the IMPS = Nearly 7 V"]
-[13.351479530334473, 7.347834587097168, "[TT] Power of the MTQ = 1 W/unit"]
-[5.569614887237549, 0.7729899287223816, "[TT] Arrival Date at Europe\u2019s Spaceport of the BepiColombo = May 11, 2018"]
-[6.1589179039001465, 3.4528632164001465, "[FF] Mission Objective of the Flying Laptop = Test ten different small-satellite technologies"]
-[8.686725616455078, 3.506463050842285, "[TT] Extreme Ultraviolet Sensors (EUVS) of the EXIS = Measure extreme ultraviolet light"]
-[11.281769752502441, 0.9896596074104309, "[TT] Mission Status of the LISA = Feasible for final technology development and design before adoption"]
-[13.88270378112793, 7.146599292755127, "[TT] Power of the Voltage 3 = 1.93"]
-[5.253063678741455, 5.5957865715026855, "[TT] Data Compression of the Payload = CCSDS 120.1-G-1E"]
-[7.439726829528809, 3.587224245071411, "[FF] Function of the GNSS-RO Instrument = Track navigation satellite radio signals as they dip below, or rise from, the horizon and detect tiny changes in the radio signal related to the density of the atmosphere"]
-[11.09365177154541, 0.6686263680458069, "[FF] Types of the Exoplanet = Small, rocky worlds like Earth, gas giants many times larger than Jupiter, hot Jupiters, super-Earths, mini-Neptunes, planets orbiting two stars at once, planets orbiting the collapsed remnants of dead stars"]
-[14.192501068115234, 3.2127015590667725, "[TT] Mass of the ASPOC = 2.5 kg"]
-[11.395923614501953, 4.3736958503723145, "[TT] Size of the TSAT = 2U"]
-[3.3729372024536133, 2.5637712478637695, "[FF] Applications of the Sich-2 = Monitoring of natural resources, rational nature management, Agriculture, land use, town building, environment pollution monitoring and evaluation, mapping, Diagnosis and forecast of technogenic and natural cataclysms, Monitoring of ionosphere parameters"]
-[5.748183727264404, -0.6182110905647278, "[TT] Operational Lifetime of the Jugnu mission = 1 year"]
-[7.706709384918213, 5.255837917327881, "[FF] Subassemblies of the ASTERIA payload = OTA (Optical Telescope Assembly) and the PEA (Payload Electronics Assembly)"]
-[4.050992488861084, 1.874051570892334, "[TT] Launch Site of the Global-9 = New Zealand"]
-[5.622629165649414, -0.06689263135194778, "[TT] Measurement Period of the TSX-5 = June 2000 through July 2006"]
-[8.946762084960938, 4.531836986541748, "[FF] Primary Pointing Reference of the CHOMPTT = Sun's orientation measured by the sun sensors"]
-[9.790813446044922, 8.224882125854492, "[TT] FOV Resolution of the HSRS = 2.22 arcmin"]
-[5.706753253936768, 2.6146867275238037, "[FF] Purpose of the BeaverCube = Educational mission to introduce students worldwide to aerospace science and technology"]
-[4.458873748779297, 1.323915719985962, "[FF] Presentation Date of the GMES Contributing Missions (GCM) = June 6-7, 2012"]
-[7.045060634613037, 5.765097141265869, "[TT] Quantity of the Tri-TIP = 4"]
-[4.670529842376709, 2.6062939167022705, "[TT] Imaged Region of the HyperScout = Scotland"]
-[5.279046058654785, 0.019753411412239075, "[FF] Departure from Space Station of the Cygnus NG-10 = Unknown"]
-[11.955841064453125, 5.175757884979248, "[TT] Volume of the Total instrument = <0.8 m 3"]
-[7.607727527618408, -2.5308172702789307, "[TT] Image Acquisition Date of the GOLD = December 19, 2018"]
-[6.0106611251831055, -0.4248553514480591, "[FF] Mission Duration of the RASAT = Initially projected for a mission duration of three years"]
-[11.773134231567383, 6.369626998901367, "[FF] Energy Loss of the Neutron-Hydrogen Collisions = About half its energy"]
-[7.855612754821777, 4.626106262207031, "[FF] Illumination Conditions of the RVX = Define the relative position of the chaser"]
-[4.839724540710449, 5.320838928222656, "[TT] Number of the Polar Epsilon Reception Stations = 2"]
-[6.588625907897949, 0.08602248877286911, "[TT] Coolant Supply Duration of the Herschel = More than three years"]
-[8.077115058898926, 8.372479438781738, "[TT] Imaging Spectrum of the Elektro-L = Infrared (MWIR, TIR) and VNIR"]
-[9.63680362701416, 5.077427864074707, "[TT] Stability of the AOCS = 5 x 10-5 \u00ba/s"]
-[1.9360733032226562, -0.4026089012622833, "[TT] Expected Re-entry of the Van Allen Probes = In about 15 years"]
-[6.189379692077637, 1.8666229248046875, "[FF] URL of the ExoMars = https://iafastro.directory/iac/proceedings/IAC-18/IAC-18/A3/3A/manuscripts/IAC-18,A3,3A,10,x42850.pdf"]
-[12.131059646606445, 4.620812892913818, "[TT] Size of the SpaceCube 2 = 71 mm(W) x 220.5 mm(D) x 177.5 mm (H)"]
-[10.3333158493042, 5.7999749183654785, "[TT] Operating Temperature of the OHIS = 90 K"]
-[5.489402770996094, 6.565201282501221, "[FF] Data Archive Size of the Gaia = 1000 1 TB hard drives from a top-end home PC"]
-[6.48237419128418, 4.653317451477051, "[FF] Refit Purpose of the ERNO-Box = Serve as a data relay for the ColAIS experiment"]
-[6.623276710510254, 3.669011354446411, "[FF] Data Allocation of the Remote Sensing Instruments = Insufficient to downlink the full raw data"]
-[7.425062656402588, 4.3194499015808105, "[FF] Along-Track Separation of the ATI Experiments = Optimal observation conditions"]
-[6.169045925140381, 4.81254768371582, "[FF] Process of the Personal Computer = Plug-and-play"]
-[10.3178129196167, 3.178372859954834, "[TT] Number of CubeSats of the Spire = More than 70"]
-[10.122122764587402, -1.6179612874984741, "[TT] Inclination of the HY-1D = 98.6\u00ba"]
-[11.339678764343262, 2.7851181030273438, "[TT] Construction and Temperature Control System Mass of the Microsatellite = 9.3 kg"]
-[5.2609052658081055, 8.408071517944336, "[TT] Bandwidth of the Radiometer = 22 MHz"]
-[5.338253021240234, 0.7718453407287598, "[TT] EFI Deployment Completion Date of the THEMIS Constellation = 14 January 2008"]
-[8.65996265411377, 8.738905906677246, "[TT] Wavelength Ranges of the CaSSIS = Four"]
-[9.001057624816895, 6.080173969268799, "[TT] Target Reflectivity of the NEMO-HD = 30%"]
-[9.923649787902832, -0.3893759250640869, "[TT] Altitude of the QuakeSat = 820 km"]
-[5.514599323272705, 1.1196324825286865, "[TT] Launch Date of the IXPE = December 2021"]
-[5.813802719116211, -0.7650334239006042, "[TT] Operational Life of the Kestrel Eye II = Greater than one year in low earth orbit"]
-[6.076789379119873, 0.43132585287094116, "[FF] Prime Mission Duration of the ASTERIA = 90 days"]
-[5.840132713317871, 6.010753631591797, "[TT] Performance of the Communications and Tracking = As expected"]
-[10.092864036560059, -1.6021950244903564, "[TT] Inclination of the RESURS-O1-4 = 98.7\u00ba"]
-[10.072290420532227, 8.070235252380371, "[TT] Optics Focal Length of the Sun Sensor = 2.5 mm"]
-[7.186009407043457, 6.459563255310059, "[TT] Type of the FPA = Linear"]
-[5.123753070831299, 0.1479235589504242, "[TT] Launch Date of the QuickBird-2 = Oct. 21, 2001"]
-[13.109659194946289, 7.254431247711182, "[TT] Power Consumption of the Coarse Lateral Sensor = < 8 W"]
-[6.470980167388916, 4.877717018127441, "[FF] Functions of the FMC = Segment monitoring and G/S interfacing"]
-[9.207375526428223, 3.886645555496216, "[FF] Attitude Sensor of the PSSCT Nanosatellite = Two-axis sun sensor and a single pixel infrared Earth sensor"]
-[7.975988388061523, -0.5086733102798462, "[TT] Estimates of the CryoSat-2 = Could be high"]
-[6.437040328979492, 5.060786724090576, "[FF] Function of the ESPA Ring = Multifunctional integrating element"]
-[14.424835205078125, 6.583885669708252, "[TT] Battery Power Duration of the IXV = 1h 43 min"]
-[6.584365367889404, 2.3020174503326416, "[TT] Additional Lateral Displacement for the Fourth Exposure of the Euclid Reference Survey = 50 arcsec"]
-[8.153363227844238, 1.2762502431869507, "[FF] Purpose of the SMAP = Measuring the water content of soils"]
-[8.673945426940918, 2.4054641723632812, "[FF] Systems of the WIND = Equipped with heavy shielding and double-redundant systems"]
-[6.280468940734863, 4.23520040512085, "[TT] Autonomy of the F-DUGS = Operated by French personnel"]
-[9.759931564331055, 8.589740753173828, "[TT] IFOV (Instantaneous FOV) of the Instrument = 4 km"]
-[9.042095184326172, 4.274341106414795, "[FF] Measurement of the SSAS = Sun angle"]
-[8.176621437072754, 1.1997466087341309, "[TT] Preliminary Soil Moisture and Freeze/Thaw Products Availability of the SMAP = November"]
-[5.351036548614502, 7.302396774291992, "[TT] Radio-link Data Transfer Rate of the OBRC instrument = Not more than 10 kbit/s"]
-[10.9844331741333, 5.166633129119873, "[FF] Function of the NANOhpm of SkyLabs = Performs measurements of GNSS scintillations"]
-[8.710342407226562, 8.440666198730469, "[TT] Spectral Resolution of the Miniature High-Resolution Imaging Spectrometer = 0.1 nm"]
-[8.659690856933594, 8.752655982971191, "[TT] Development Location of the Grating Reflection Unit = Fraunhofer IOF (Institute of Applied Optics and Precision Engineering), Jena, Germany"]
-[6.298017501831055, 2.323018789291382, "[FF] Producing Team of the Visualization = Space Telescope Science Institute (STScI) in Baltimore, Maryland; the Caltech/IPAC in Pasadena, California; and the Center for Astrophysics, Harvard & Smithsonian (CfA) in Cambridge. Massachusetts"]
-[4.3994550704956055, 0.1174311488866806, "[TT] Delivery Start Date of the Starlink Premium = Second quarter of 2022"]
-[2.034597873687744, -0.32656756043434143, "[FF] New Discovery of the Van Allen Probes = ULF (Ultra-Low Frequency) plasma waves transport the outer part of the belt radiation harmlessly into interplanetary space and create the previously unexplained feature of the third belt"]
-[3.0485918521881104, 4.437655925750732, "[FF] Data Type of the PALSAR-2 = Radar and visible satellite data"]
-[4.991801738739014, 3.283099412918091, "[TT] Manufacturer of the GIIRS = National Space Science Center of CAS"]
-[6.84855842590332, 6.041822910308838, "[TT] NEDT of the CIRC = 40 mK"]
-[9.327116966247559, 4.077169418334961, "[FF] Redundant Attitude Determination of the Magnetometers = Method"]
-[5.758647441864014, 2.426805019378662, "[TT] Deployment Readiness of the DoD Human Space Flight Support Office Rescue Division = Prepared to deploy at a moment\u2019s notice"]
-[9.229879379272461, 3.041079044342041, "[FF] Operating Capability of the CCOR = During intense solar storms and flares"]
-[11.827054023742676, 6.62528133392334, "[TT] Gd Electron Energies of the LND = 29, 72, 78, and 132 keV"]
-[9.868927955627441, 1.9850515127182007, "[FF] URL of the Chandra X-Ray Observatory = https://www.nasa.gov/mission_pages/chandra/"]
-[6.368704795837402, 6.431451797485352, "[TT] Data Filters of the CRAMS = PoC, miss distance, time to TCA"]
-[4.4660773277282715, 0.9213742017745972, "[TT] Start Date of the GNSS Network = About 2010 onwards"]
-[14.261000633239746, 3.055938243865967, "[TT] Mass of the Jason-3 = 550 kg"]
-[8.70565128326416, 4.813819408416748, "[TT] Accuracy of the Star sensor = +1.0-6.0 m v 0.02\u00ba (3\u03c3)"]
-[5.368179798126221, 1.2260428667068481, "[FF] Topical Team Meeting Date of the ASIM = June 26-27, 2006"]
-[5.784327030181885, 6.133557319641113, "[TT] Contacts per Day of the DCS = 2"]
-[6.78493595123291, 2.4517033100128174, "[TT] Image Source of the DCT = Sloan Digital Sky Survey"]
-[9.814468383789062, -0.27786365151405334, "[TT] Peaking altitude (km) of the SSM/T-2 = 0, 2, 6, 10, 30, 16, 22"]
-[9.473063468933105, 7.840227127075195, "[TT] Focal Length of the spaceCam c4000 = 600 mm"]
-[4.876006603240967, 3.0961196422576904, "[TT] Manufacturer of the SAOCOM-1A = ArSat"]
-[6.244340896606445, 5.780115127563477, "[TT] Unique Identifiers of the LT = J and K"]
-[6.128387451171875, 2.576653242111206, "[TT] Agency of the HAUSat-2 = SSRL (Space Systems Research Laboratory)"]
-[6.989958763122559, 3.2182505130767822, "[TT] Number of Hosted Payloads in Testing of the GHGSat = 3"]
-[14.708976745605469, 6.7258687019348145, "[TT] Batteries Capacity of the Tsubame = 16.2 Ah"]
-[5.13905143737793, 5.023785591125488, "[TT] Communication Status of the Robusta = No further communication has been received"]
-[3.4540133476257324, 4.914870262145996, "[TT] SAR Antenna Deployment Mechanism of the RISAT-1 = Employed"]
-[5.172379493713379, 0.605383038520813, "[TT] Launch Date of the BEAM = 8 April 2016"]
-[2.987126111984253, 2.258390188217163, "[TT] Ground Resolution of the Copernicus Sentinel-2 = Up to 10 m"]
-[6.864800930023193, 4.1701202392578125, "[TT] Mounting Location of the HDEV = External Payload Facility of the European Space Agency\u2019s Columbus module"]
-[4.742112159729004, -0.8531776070594788, "[TT] Splashdown Time of the Dragon = Monday at 12:15 a.m."]
-[14.145995140075684, 2.9685230255126953, "[TT] Mass of the Deimos-2 minisatellite = 310 kg"]
-[5.648371696472168, 5.693452835083008, "[TT] Processor Type of the SCS750 = PowerPC 750FX"]
-[8.798351287841797, 3.6403212547302246, "[TT] Objective of the EHIS = Measure the proton, electron, and alpha particle fluxes at GEO"]
-[6.905206680297852, -0.3453429937362671, "[TT] Revisit Time of the Tandem-L satellites = 16 days"]
-[8.645177841186523, 5.7859578132629395, "[TT] Accuracy of the ARI = Better than 0.1 K 3\u03c3"]
-[8.186484336853027, 8.035274505615234, "[FF] Next Alignment Step of the Webb = Near-Infrared Spectrograph, Mid-Infrared Instrument, and Near InfraRed Imager and Slitless Spectrograph"]
-[9.250923156738281, 5.037256240844727, "[TT] Attitude Knowledge of the GFO = Derived from horizon scanners"]
-[10.515265464782715, 6.884418487548828, "[TT] Smallest mirror diameter of the Mirror = 76 mm"]
-[4.989912986755371, 1.7425968647003174, "[TT] Operating Status of the RISING-2 = Nominal"]
-[3.4088213443756104, -0.8539099097251892, "[TT] Orbit of the Cartosat-2F = 505 km sun-synchronous type orbit"]
-[5.747178077697754, 6.521454811096191, "[TT] Daily Scenes of the System = More than 30"]
-[13.32728099822998, 7.129246234893799, "[FF] Power Range of the Modular Power System = 1W to 1kW"]
-[8.39651870727539, 6.311873912811279, "[FF] Components of the TEMPO = Off-axis reflective Schmidt telescope and an Offner spectrometer"]
-[10.089935302734375, -1.4803078174591064, "[TT] Inclination of the QuakeSat = 98.73\u00ba"]
-[10.773528099060059, 1.351302981376648, "[FF] Weight of the BL Lacertae = 200 million times the mass of our Sun"]
-[9.367856979370117, 7.845609664916992, "[TT] Imaging Payload of the NEA Scout = Optical"]
-[9.817293167114258, 8.239856719970703, "[TT] FOV (Filed of View) of the Mirror = 61 arcmin"]
-[5.100544452667236, 0.8184334635734558, "[FF] Development Date of the PRARE = 1990"]
-[8.449199676513672, 1.9474321603775024, "[FF] Measurement Range of the Cloud Fraction = 0-1"]
-[9.31844425201416, 5.011699199676514, "[TT] Accuracy of the Attitude Control = \u2264\u00b11\u00ba (3\u03c3)"]
-[5.874819278717041, 3.2411582469940186, "[FF] Activities of the Coast Guard, Navy and Air Force = Search and rescue"]
-[6.43858528137207, 8.104363441467285, "[TT] Parameters of the Convolutional Coding = k=7, R= \u00bd"]
-[10.971339225769043, 2.02693772315979, "[TT] Expected End of Mission of the XMM = Into 2023"]
-[5.823678493499756, 3.616647958755493, "[FF] Development Scope of the Neosat program = In-orbit validation of the new satellite product lines"]
-[7.386610507965088, 5.217818260192871, "[FF] Purpose of the SOLCON-3 = Determine the SARR coefficients of ACRIM-III on ACRIMSAT and to verify the VIRGO coefficients on SOHO"]
-[8.386256217956543, 7.276229381561279, "[TT] Components of the MDM = Material samples and the optical camera"]
-[9.50752067565918, 4.148627281188965, "[TT] Quantity of the Eddy Current-Type Detection Gap Sensors = 8"]
-[8.367300987243652, 7.0981831550598145, "[TT] BW Film Type of the Metric Camera = KODAK Double-X Aerographic Film 2405"]
-[5.312261581420898, 6.777162551879883, "[TT] Command & Data Handling of the Spacecraft = 240 MIPS, 128 MB, 128 MB"]
-[6.846358299255371, 6.974476337432861, "[TT] Number of Beams of the SWIM Instrument = 6"]
-[6.70217752456665, 0.8551862835884094, "[TT] Launch Date of the Solar Orbiter = 2017"]
-[5.312961101531982, 3.959533929824829, "[TT] Total Satellites of the ICEYE Satellite Constellation = 21"]
-[11.7223539352417, 6.638092994689941, "[TT] Energy of the VNIR = 1.17 eV"]
-[7.409222602844238, 4.563525199890137, "[FF] Purpose of the VCST = Provide independent evaluation of the VIIRS calibration and SDR product quality"]
-[10.241372108459473, -1.3515751361846924, "[TT] Orbit Inclination of the CINEMA satellites = High"]
-[7.841204643249512, 0.5863772630691528, "[TT] Spatial Resolution of the SELENE/SP = 0.5\u00ba grid meshes in lunar latitude and longitude"]
-[7.996921062469482, 0.5729807019233704, "[FF] Conference Presentation of the Near Earth Asteroid Scout = 2019 IEEE Aerospace Conference"]
-[5.4091033935546875, 7.073226451873779, "[TT] Data Rate of the Instrument data downlink = 2.62 Mbit/s"]
-[5.503265857696533, 3.7639410495758057, "[TT] Responsible Organization of the SWEM (SWEAP Electronics Module) = UCB/SSL (University of California, Berkeley /Space Sciences Laboratory)"]
-[12.258810043334961, 6.932833671569824, "[TT] Energy Range for H of the LEICA = 0.76 - 6.1 - - 18 - 250 MeV"]
-[8.43418025970459, 7.178699493408203, "[TT] Quantity of the Micro-CMOS Cameras = 4"]
-[3.108804225921631, 2.4528958797454834, "[FF] Purpose of the Copernicus Sentinel-2 = Methane hotspot detection"]
-[10.172181129455566, 1.36087965965271, "[TT] Previous Catalogue Object Count (1957) of the Gaia Catalogue of Nearby Stars = 915 objects"]
-[4.645618438720703, 7.0817975997924805, "[TT] X-band Downlink Transmission Data Rates of the CBERS-2B = 2 x 53 Mbit/s"]
-[11.339692115783691, 2.7649357318878174, "[TT] Mass of the Microsatellite = 47 kg"]
-[8.246996879577637, 2.284978151321411, "[TT] Cloud Top Imaging Resolution of the ISIR = Near \u00bc km"]
-[5.005083084106445, 3.5144267082214355, "[TT] Manufacturer of the SGLS CXS-810C radio = L-3 Communications Inc."]
-[8.075637817382812, 6.0050554275512695, "[FF] Function of the LASSO = Demonstrate high accuracy time standard synchronisation over large distances"]
-[10.280729293823242, 4.107057094573975, "[TT] Frequency Range of Shaker Tests of the Boom = 9-300 Hz"]
-[7.618921756744385, 4.01715087890625, "[FF] Objectives of the C3D Instrument = Provide a technology demonstrator to improve the TRL of new CMOS sensors, Correlate the effects of space radiation with ground based testing, Capture images of the Earth"]
-[4.286202907562256, 4.176366806030273, "[TT] Observables of the Galileo = Code Pseudorange, Carrier-Phase Measurement, Doppler (or Range Rate), C/N0 (Carrier-to-Noise Ratio)"]
-[7.390948295593262, 2.4740114212036133, "[FF] Observation Coverage of the GLM sensor = Most of the western hemisphere, including the Atlantic and Eastern Pacific tropical basins"]
-[6.690617084503174, 7.555029392242432, "[TT] Telemetry Amplitude Digitization of the SXI = 12 bit"]
-[5.2155022621154785, 3.206005811691284, "[TT] Manufacturer of the NRCSD = NanoRacks"]
-[5.375612735748291, 7.046836853027344, "[FF] Data Downlink of the AAUSat-1 = Limited amount"]
-[7.175781726837158, 1.2100765705108643, "[TT] Arrival at Mars of the ExoMars Trace Gas Orbiter = 2016"]
-[5.655368328094482, 7.107843399047852, "[TT] Data Rate of the LIAU = 600 Mbit/s"]
-[7.440502166748047, 6.401968955993652, "[TT] Datation Triggers of the XGRE = 300 ns relative time accuracy"]
-[7.152733325958252, 0.7715855836868286, "[TT] Seismometer Deployment Date of the InSight Lander = December 19, 2018"]
-[13.645432472229004, 5.738100051879883, "[TT] Solar Panels Power Generation (Average) of the EURECA = 1 kW"]
-[5.150041580200195, 0.30721035599708557, "[TT] Deployment Order of the PCSat = After SAPPHIRE"]
-[7.8940558433532715, 8.828344345092773, "[FF] Spectra of the SP = Dual-line (Fe i 630.25 nm and Fe i 630.15 nm)"]
-[5.585593223571777, 2.184319257736206, "[TT] Deployment Contract of the Diwata-1 = JAXA and Tohoku University"]
-[6.161911964416504, 6.858985900878906, "[FF] Data Compression of the NMS = Yes"]
-[7.816572189331055, 6.983829975128174, "[TT] Sample Frequency of the Fast Cameras = Every 2.5s"]
-[9.302703857421875, -0.8904090523719788, "[TT] Location of the INSAT-3D = 82\u00b0E over the equator"]
-[6.428783416748047, -0.014599304646253586, "[TT] Coverage of the Active Schedule = Next fourteen 24-hour operational days"]
-[6.3918938636779785, 5.487404823303223, "[TT] Provider of the DCS = INPE"]
-[10.225512504577637, 1.5494074821472168, "[TT] Number of Brightest Stars Recorded of the Project = 100"]
-[3.1850602626800537, 3.8276498317718506, "[FF] 10 Year Anniversary Date of the TerraSAR-X = June 14, 2017"]
-[7.883219242095947, 6.545065402984619, "[FF] Function of the CEB = Operate the CCD, digitize the image data and transfer it to the CCM"]
-[7.819693088531494, 8.400731086730957, "[TT] Bands of the SV-24 = Visible Pan / Color"]
-[5.560207843780518, 2.6003189086914062, "[TT] Population of the Kolkata = Over 14 million inhabitants"]
-[8.49057388305664, 6.217274188995361, "[TT] Preferred Location of the TEMPO = 90-110\u00ba W"]
-[10.124241828918457, -0.4810383915901184, "[TT] Orbit Altitude of the ALBus CubeSat = 500 km"]
-[7.218825817108154, 3.2656047344207764, "[FF] Function 2 of the PUNCH = Yield the first maps of the evolving shape of the Alfv\u00e9n surface"]
-[6.46878719329834, 4.047914028167725, "[TT] Docking of the Pirs = Autonomously docked to the Zvezda service module\u2019s nadir"]
-[8.572813034057617, 3.8207733631134033, "[TT] Detected Particles of the IBEX = Energetic Neutral Atoms (ENAs)"]
-[7.984059810638428, 8.182652473449707, "[TT] Spectral Band of the Band Photometers = 337.0 nm"]
-[8.61578369140625, 8.731306076049805, "[TT] Grating Order of the Spectrometer = 1"]
-[8.407194137573242, 7.934845447540283, "[TT] Imaging Length of the SWIR Detector = Over 2700 pixels"]
-[10.039462089538574, 8.15191650390625, "[TT] Focal Length of the TIR Subsystem = 31.14 mm"]
-[14.029850006103516, 3.254746913909912, "[TT] Weight of the TxU = 8 kg"]
-[9.084546089172363, 5.715245246887207, "[TT] Cone Angle of the Pointing Mechanism = 4\u00ba"]
-[3.6131157875061035, 2.705531120300293, "[TT] Number of Satellites of the Iridium Satellite LLC = 66"]
-[9.399384498596191, 7.170877456665039, "[TT] Image Resolution of the WFI = 55 m"]
-[13.486233711242676, 7.401014804840088, "[TT] Electrical Power of the TXS = 4 W"]
-[8.226571083068848, 5.573630332946777, "[FF] Performance of the OCE = Spectral calibration accuracy of 0.02 nm"]
-[9.587531089782715, 6.0218682289123535, "[TT] Actuator of the HSC-III = Coreless DC motor"]
-[7.923430919647217, 8.550080299377441, "[TT] Spectral Range of the ISO Instrument = 30-1300 nm"]
-[6.5557146072387695, -0.7303983569145203, "[FF] Mission of the Neutron-1 = Study low energy neutron flux in Low Earth Orbit (LEO) as a function of time and location"]
-[5.353275775909424, 1.1141091585159302, "[TT] Ready Date of the Instrument = March 2018"]
-[5.72731351852417, -0.5832000374794006, "[TT] Expected Lifetime of the TIRS = At least three years"]
-[10.946935653686523, 7.572216510772705, "[TT] Swath Width of the TopSAR narrow = > 150 km"]
-[3.691499710083008, 5.0317912101745605, "[TT] Imaging Frequency Band of the TecSAR = X"]
-[5.505625247955322, 7.23772668838501, "[TT] Data Rate of the Information data rate per channel = 300 Mbit/s"]
-[12.132340431213379, 3.2598066329956055, "[TT] Propellant of the FENIX micropropulsion device = Solid"]
-[7.703547477722168, 4.4360857009887695, "[FF] Deployment of the AstroMesh Reflector = Deployed"]
-[4.9321441650390625, 5.4454450607299805, "[TT] Frequency Bands of the GPS Receiver = L1 and L2"]
-[13.846004486083984, 7.142571926116943, "[TT] Regulation (%) of the PS-2 = \u00b15"]
-[5.42244291305542, 6.344507694244385, "[TT] Capacity of the UPM-1T card = 800 Gbit"]
-[11.996760368347168, 3.4545950889587402, "[TT] Pressure of the Steam Propulsion Unit = Atmospheric pressure"]
-[7.586866855621338, 5.103470802307129, "[FF] Components of the C2B = Radio, batteries, attitude control unit, solar panels"]
-[4.61027717590332, 7.877004146575928, "[TT] Receive Frequency (MHz) of the HRIT HiRID = 2029.1"]
-[9.043336868286133, 0.8833371996879578, "[TT] Number of Venus Flybys of the V7GA = 7"]
-[8.429624557495117, 7.562895774841309, "[FF] Quantity of Silicon Detectors of the NICER/SEXTANT = Not provided"]
-[7.288444519042969, 7.9303693771362305, "[TT] Sound Impact of the GRACE-FO satellites = 140 decibels (dB)"]
-[9.820778846740723, -0.38821497559547424, "[TT] Altitude of the Spacecraft = 677 km x 586 km"]
-[8.314319610595703, 7.308410167694092, "[FF] Image Sensor Supplier of the Teledyne e2v = Unknown"]
-[8.010098457336426, -1.061536192893982, "[FF] Use of the Radar Altimeter = Monitoring glaciers"]
-[8.344407081604004, 5.483994960784912, "[FF] Spectral Sampling Rate of the TanSat = Unknown"]
-[10.843636512756348, 3.0078275203704834, "[TT] Microgravity Environment of the O/OREOS nanosatellite = Below 500 \u00b5g"]
-[7.873220443725586, 5.1807861328125, "[TT] Use Case of the FLLS = Monitoring the relative positions between craft in the constellation"]
-[9.026130676269531, 3.3281500339508057, "[FF] Characteristic of the Plasmapause = Sudden drop in plasma density by the order of one magnitude"]
-[4.144665718078613, 1.453101396560669, "[FF] Conference Date of the Meteosat Second Generation (MSG) Radiometer/Imager = May 16-20, 2016"]
-[9.598880767822266, 1.445570707321167, "[TT] Communication Bandwidth of the Pl\u00e9iades Neo = Up to 1.8 Gbit/s"]
-[9.732054710388184, 0.20260018110275269, "[FF] Parachute System Qualification Team of the ExoMars = ESA, TASinI, TASinF, Vorticity, Arescosmo"]
-[4.792488098144531, 0.07331255078315735, "[TT] End of Life Date of the HJ-1 = 31 Dec 2022"]
-[3.3709816932678223, 6.515334129333496, "[TT] Antenna Diameter of the ALT = 1 m"]
-[10.828996658325195, 4.031796455383301, "[TT] Position Control of the CanX-4&5 = 10 cm"]
-[8.305069923400879, 7.926760673522949, "[TT] Type of the SWIR detectors = InSb detectors"]
-[7.719116687774658, 1.0486727952957153, "[FF] URL of the Airborne Lunar Spectral Irradiance (air-LUSI) Instrument = https://www.nist.gov/measuring-cosmos/airborne-lunar-spectral-irradiance-air-lusi-instrument"]
-[12.101709365844727, 4.5075836181640625, "[TT] Size of the Spacecraft = Approximately 2.5 m x 3.5 m x 3.2 m (deployed)"]
-[9.2860746383667, 3.8040194511413574, "[TT] Main Instruments of the \u00d8rsted spacecraft = CSC and Overhauser magnetometers"]
-[5.486341953277588, 0.6156271696090698, "[FF] Anniversary Date of the ENVISAT-1 = 1 March 2022"]
-[9.223756790161133, 1.0402618646621704, "[TT] Arrival Date at Jupiter of the Juno spacecraft = 2016"]
-[4.110096454620361, 6.533998489379883, "[FF] Advantages of the Q/V-bands = Larger bandwidth, Smaller antenna for fixed gain, Higher gain for fixed antenna, Enhanced directivity for spot beams systems"]
-[5.625446319580078, 6.684795379638672, "[TT] Data Volume of the Aleph Satellite = Around 50 MB per scene"]
-[3.8870022296905518, 0.18085764348506927, "[FF] Operational Concept Presentation Date of the SMART-1 = Sept. 29, - Oct. 3, 2003"]
-[7.324718952178955, 4.962408542633057, "[TT] Type of the MPPT = Step-up DC/DC converter"]
-[10.045808792114258, -1.560075283050537, "[FF] Orbit Inclination of the Colorado Student Space Weather Experiment (CSSWE) = Highly Inclined"]
-[5.917515277862549, 1.1380897760391235, "[FF] Development Start Date of the Satellites around the Moon = 20 May 2021"]
-[4.74424409866333, 3.267080545425415, "[TT] Manufacturer of the SES-17 and Syracuse-4E = Thales Alenia Space"]
-[5.750068664550781, 1.1562761068344116, "[FF] Launch Date of the Earth-Observation Satellite = Nov. 6, 2010"]
-[7.842912673950195, 4.711801052093506, "[FF] Challenges of the ADCS = Calibrating and monitoring this subsystem across a large constellation, complexities introduced by distributed launches and multiple hardware revisions, resource constraints"]
-[12.131863594055176, 0.5801039934158325, "[FF] Catalogue Content of the PLATO = Confirmed and characterized planets in habitable zones with known mean densities, compositions, and evolutionary ages/stages"]
-[8.703725814819336, 7.6601715087890625, "[TT] No of Strips of the Detector = 41 x 41"]
-[11.938648223876953, 4.975975036621094, "[TT] Honeycomb core thickness of the Bus structure = t = 10. 8 mm"]
-[7.2625203132629395, 8.162825584411621, "[TT] Sensitivity of the Channel 5 = 0.3 K/pixel"]
-[13.347747802734375, 7.254117488861084, "[TT] Power of the ASPOC = 3.0 W"]
-[6.146439552307129, 2.176422595977783, "[TT] Location of the Euclid Consortium = Institut de Ci\u00e8ncies de L\u2019Espai (ICE, IEEC-CSIC) and Port d\u2019Informaci\u00f3 Cient\u00edfica (PIC) in Barcelona"]
-[7.033588409423828, 4.422131061553955, "[FF] Unknown of the CP-9 = Unknown"]
-[4.669206142425537, 8.073896408081055, "[TT] Frequency RX of the USAT (Ultra Small Aperture Terminal) = 18.25 GHz\u00b1550 MHz"]
-[4.773508071899414, 0.013603984378278255, "[TT] End of Life Date of the MidSTAR-1 = 30 April 2009"]
-[3.1706461906433105, 3.9908533096313477, "[TT] Data Collected of the TerraSAR-X = 1.34 petabytes"]
-[10.128304481506348, -2.73453426361084, "[TT] NAND Flash of the Stamp9G20 = 128 MB"]
-[13.335734367370605, 6.739416599273682, "[FF] Energy Comparison of the Lightning = 1 bolt of ordinary lightning = enough energy to charge 20 electric cars"]
-[8.052979469299316, 8.647509574890137, "[FF] Spectral Sampling of the LR Bands (500\u2013697 nm) = Equal to the slit with (84 \u00b5 )"]
-[5.4637041091918945, 4.976225852966309, "[FF] GPS Receiver of the AlSat-2 = Onboard location and time services"]
-[7.035387992858887, 8.375701904296875, "[TT] Nominal SNR of the Band 5 = 1010"]
-[8.165672302246094, 4.448556900024414, "[FF] Type of the Timepix = Space Radiation micro-Tracker"]
-[6.464458465576172, -0.8239338994026184, "[TT] LTAN of the Satellite = 18:00 hours"]
-[9.532341003417969, 6.925236225128174, "[TT] Raw Resolution of the DPS = 50 m (azimuth) x 15 km (elevation)"]
-[8.091338157653809, -0.9175925850868225, "[FF] Coverage of the ICESat-2 = More southern latitudes than ever before"]
-[8.241288185119629, 5.399715900421143, "[FF] Accuracy of the MEMS Rate Sensor = High"]
-[10.469245910644531, 2.3668322563171387, "[TT] Micropore Array of the CuPID X-ray telescope = 20 x 20 \u00b5m square-hole micropores"]
-[13.683335304260254, 6.989856719970703, "[FF] Current-Limiting Resistor of the PPPT = Unknown"]
-[9.858810424804688, 8.74571704864502, "[TT] FOV of the S-band = 1000 km"]
-[4.385781288146973, 7.820886135101318, "[TT] Uplink Frequency of the RF communications = 145.848 MHz"]
-[7.972108840942383, 4.083193778991699, "[TT] Instrument Types of the Megha-Tropiques = Earth radiation budget radiometers, Imaging multi-spectral radiometers (passive microwave), Atmospheric temperature and humidity sounders"]
-[9.605594635009766, 0.6462777853012085, "[TT] Earth-Moon Transfer Distance of the Probes = Up to 1.6 million km"]
-[8.221597671508789, 6.6583685874938965, "[FF] Image Captures of the C3D2 = >100"]
-[9.48015308380127, 6.14902400970459, "[TT] Incidence Angle of the MWR = 52\u00ba and 58\u00ba"]
-[11.719888687133789, 6.770791053771973, "[TT] Energy Range of the LAXPCs = 3-80 keV"]
-[5.9096269607543945, 2.819948434829712, "[TT] Design of the Legion = Fully redundant"]
-[4.742519378662109, 7.326022624969482, "[TT] Data Rate of the X-band antenna = 800 Mbit/s"]
-[4.807111740112305, -1.8442440032958984, "[FF] Mission Tasks of the Chang'e-4 = Low-frequency radio astronomical observation, surveying the terrain and landforms, detecting the mineral composition and shallow lunar surface structure, and measuring neutron radiation and neutral atoms"]
-[6.689138889312744, 1.3078795671463013, "[TT] Image Revisit Time of the Landmapper BC = Daily"]
-[6.564236640930176, -0.5367682576179504, "[TT] Flight Duration of the INSAT-3D = 32 minutes and 48 seconds"]
-[9.219788551330566, 4.810813903808594, "[FF] Description of the Inertial Attitude Control Mode (IRC) = Provided spacecraft control using a propagated inertial quaternion"]
-[13.574111938476562, 6.861053466796875, "[TT] Power of the Spacecraft bus = 3.8 kW"]
-[8.632135391235352, 1.155551552772522, "[TT] Operation Mode of the Aquarius = Nominal science mode"]
-[10.307491302490234, 4.055165767669678, "[TT] Instrument Mounting of the OVM = Boom-mounted at a distance of 8 m"]
-[7.817590236663818, 4.951539039611816, "[FF] Testing Status of the Calibration Targets = Completed"]
-[2.343384027481079, 1.3132487535476685, "[TT] Launch Date of the NanoSail-D = Aug. 2 2008"]
-[9.69084644317627, -0.543839156627655, "[TT] Altitude of the WorldView-3 = 617 km"]
-[4.731438159942627, 1.8646416664123535, "[FF] Readiness Date of the EUMETSAT ground segment = 5 December 2017"]
-[10.206764221191406, 5.386314868927002, "[TT] Performance of the Active Cooling System = Nominal"]
-[9.652486801147461, -0.6395246982574463, "[TT] Orbit Altitude of the DSX = 6-12,000 km"]
-[8.764358520507812, 8.355539321899414, "[FF] Publication Date of the Envisat's Medium-Resolution Imaging Spectrometer = November 1993"]
-[11.00383186340332, 0.580467700958252, "[TT] Number of Planets of the Kepler space telescope = Billions"]
-[4.966475009918213, 5.406027793884277, "[TT] Frequency of the IGOR GPS receiver = Dual"]
-[7.336806297302246, 0.9742643237113953, "[FF] Data Release Date of the GRAIL = 2014"]
-[7.308067798614502, 2.159069061279297, "[FF] Mission Phase of the Biomass = Last phases of development"]
-[10.269048690795898, 5.653542995452881, "[TT] Thermal Control of the CCRR = \u00b11\u00b0C"]
-[5.203459739685059, 0.20387567579746246, "[TT] Previous Planned Launch Year of the NEMO-AM = 2017"]
-[8.67664909362793, 5.719287872314453, "[TT] Tracking accuracy of the Antenna = <\u00b10.2\u00ba"]
-[7.429725646972656, 6.205774307250977, "[FF] Purpose of the Laser Tracking Instrument = Provide the plane information of the antenna plane"]
-[8.487166404724121, 4.597498893737793, "[FF] Sensors of the AOCS = CESS (Coarse Earth Sun Sensor), IMU (Inertial Measurement Unit), fluxgate magnetometer, STR (Star Tracker Assembly), GNSS receiver"]
-[7.549463748931885, 0.30673980712890625, "[TT] Dry Condition Frequency of the GRACE-FO satellites = 2 percent of the time (about once every 50 years)"]
-[4.946389198303223, 0.9769591093063354, "[FF] Shutdown Date of the IMP-8 = Oct. 31, 2001"]
-[11.744600296020508, 3.292792320251465, "[TT] Pulse Trains of the LM thruster = Pulses on the order of 500 ms"]
-[4.828330039978027, 0.4842076003551483, "[TT] Communication Issues of the STARE-A = Spring/Summer of 2013"]
-[7.755728244781494, 7.8150129318237305, "[TT] Sensitivity of the NICER = 30 times the sensitivity of RXTE to background-dominated sources"]
-[6.107183933258057, -0.3641377389431, "[TT] Science Mission Duration of the LRO = 9/17/2010 - 9/16/2012"]
-[8.179527282714844, -0.0053384206257760525, "[FF] Development Time of the TOPEX/Poseidon Project = 25 Years"]
-[13.548578262329102, 6.904310703277588, "[TT] Average Power Generation of the EPS = 2 kW"]
-[9.062661170959473, -0.7856951355934143, "[TT] Orbit Period of the Beijing-3B = 96.8 minutes"]
-[4.238533020019531, 7.253305435180664, "[TT] Monitoring and Control Frequency of the RF Communications = S-band"]
-[5.672487735748291, 4.399942398071289, "[FF] Key Technologies of the SATis5 = Distributed NFV orchestration, distributed, edge oriented 5G control plane, diverse, dynamic data path support, local offload, multicast, efficient small messages distribution, device management for slice-selection, secure and isolated multi-slice environment using service function chaining extensions, end-to-end network management, slice programmability and customization to applications, integration with legacy and 3rd party services, integration of edge intelligence and Multi-access Edge Computing (MEC) node, functional split and synchronization with central nodes, New Radio (NR) integration with satellite"]
-[7.6053924560546875, 3.082041025161743, "[TT] Secondary Mission Goal of the GOSAT = Thermal infrared observation"]
-[10.94791030883789, 7.6012983322143555, "[TT] Nominal Swath Width of the Wide multi-look fine = 90 km"]
-[14.647174835205078, 6.66223669052124, "[TT] Quantity of the Battery = 1"]
-[8.971055030822754, 3.536313772201538, "[TT] Operation Time of the High-voltage solar array = More than 50 hours"]
-[6.778566837310791, 1.8434301614761353, "[TT] Launch Date of the Nancy Grace Roman Space Telescope = Mid-2020s"]
-[5.395333766937256, 0.9237188696861267, "[FF] Launch Date of the BRITE-Austria = Unknown"]
-[10.045372009277344, 1.3465673923492432, "[TT] Asteroid Survey of the Gaia = 156 thousand rocky bodies"]
-[5.757954120635986, 2.0928404331207275, "[FF] Mission Status of the CAPSTONE = Unknown"]
-[3.4221725463867188, 1.4077316522598267, "[TT] Launch Date of the Sentinel-3A = 2013"]
-[7.161881446838379, 2.0313892364501953, "[TT] Launch Date of the Biomass = April 2024"]
-[6.599320888519287, 4.2746968269348145, "[FF] Download Time of the QuakeSat = Premium"]
-[5.99330997467041, 0.955634593963623, "[FF] Date of the XGOHI = April 4, 2007"]
-[5.862349510192871, -1.0416353940963745, "[TT] Exceeded Design Life of the Terra = Yes"]
-[5.759329319000244, 6.216596603393555, "[TT] Number of Subscribers of the SecureWatch = 20"]
-[5.761476993560791, 3.143193006515503, "[TT] Funding Round Amount of the Satelles = $26 million"]
-[7.14798641204834, 3.1599931716918945, "[FF] Sensing Amazon Seasonality of the Satellite = Unknown"]
-[4.796144962310791, 0.43088585138320923, "[TT] Launch Date of the MSG-1 = Aug. 28, 2002"]
-[8.705933570861816, 8.552300453186035, "[TT] Number of Optical Elements of the Grating Wheel Assembly = 8"]
-[7.534561634063721, 0.9630612134933472, "[FF] Map Resolution of the GRAIL Probes = Highest resolution"]
-[13.44399642944336, 2.867192268371582, "[TT] Mass of the Satellite = 19.6 kg"]
-[5.627078056335449, 4.911396503448486, "[TT] Geostationary Data Relay System of the Sentinel-1, -2 = EDRS (European Data Relay System)"]
-[5.035345554351807, 0.4451052248477936, "[TT] Launch Date of the Aeolus satellite = July 23, 2018"]
-[4.463598251342773, 7.770402431488037, "[TT] Uplink Frequency of the RF Communications = VHF (145 MHz)"]
-[3.462843656539917, 4.898133277893066, "[FF] Performance Verification of the SAR Sensor = Ground test results, in-orbit tests and evaluations"]
-[6.577992916107178, 5.569509506225586, "[TT] Quantity of the Circuit Board Experiments = 3"]
-[10.224481582641602, 2.0992531776428223, "[FF] Imaging of the Chandra X-ray Observatory = Andromeda"]
-[4.071778774261475, 7.266540050506592, "[TT] Gain of the Low Noise Amplifier (LNA) = Up to 39 dB"]
-[4.853382587432861, 7.906286239624023, "[TT] Data Transmission Frequency of the Sensor = 8000 MHz"]
-[9.139077186584473, 5.35288143157959, "[TT] Pointing Accuracy of the QuickBird-2 = \u00b10.016o (3? steady state in all three axes)"]
-[6.895384311676025, 3.1945745944976807, "[FF] Formation of the MMS = Four spacecraft flown around Earth in a pyramid formation"]
-[6.453956604003906, -0.5348034501075745, "[TT] Power Off Period of the Spacecraft = Until Aug. 30"]
-[10.930571556091309, 6.287643909454346, "[TT] Internal Surface Treatment of the Instrument = Flat-black surface treatments, e.g. Z306 paint with diffuse reflectance Rdiff ~ 5%"]
-[7.769839763641357, 5.710467338562012, "[FF] Testing Support of the Vision-based sensor system = Supported the testing remotely"]
-[18.665424346923828, 3.9382619857788086, "[TT] NE\u0394T (K) of the ICI-5 = 1.1"]
-[7.493283748626709, 2.2134029865264893, "[FF] Purpose of the Normalised Difference Vegetation Index = Measure of health and status of plant growth"]
-[12.21873950958252, 3.6861188411712646, "[TT] Xenon Critical Density of the CVX\u20132 Device = 1.1 times that of water"]
-[7.902000427246094, 5.894154071807861, "[FF] Function of the Center of Mass Algorithm = Determines where the center of the beam on the lateral detector is"]
-[5.885061740875244, -0.7677387595176697, "[TT] Mission Life of the Electrical Power Subsystem = 6 months"]
-[4.5068678855896, 2.9488604068756104, "[FF] Remote Operations Location of the ExoMars = France"]
-[9.249731063842773, 5.453362464904785, "[TT] Required Spacecraft Stability of the Push Frame Framer with a fast steering mirror = Low"]
-[9.518733024597168, 4.173305988311768, "[TT] Sensor Type of the MAGIC = Dual, 3-axis AMR (Anisotropic MagnetoResistive) sensor"]
-[5.1076765060424805, 2.3223392963409424, "[TT] Products in Nominal Phase of the Mission Operation System = About 2 PB"]
-[10.12148666381836, 8.084344863891602, "[TT] Telescope Focal Length of the PIC = 3.45 m"]
-[7.685975551605225, 0.8152744770050049, "[FF] Function of the XRS (X-Ray Spectrometer) = Explore the lunar soil properties"]
-[14.302326202392578, 2.7604901790618896, "[TT] Mass of the KOMPSAT-3 = 970 kg"]
-[5.019285202026367, 3.248481512069702, "[TT] Manufacturer of the Resurs-P1 = TsSKB Progress (Progress State Research and Production Space Center)"]
-[3.2768189907073975, 3.8472063541412354, "[TT] Number of Observations per Year of the 3XMM Catalogue = 600-700"]
-[9.369060516357422, 7.136878490447998, "[TT] Resolution of the EIC = 250 m x 250 m"]
-[12.0947265625, 4.4097161293029785, "[TT] Capacity of the General spacecraft parameters = 12 Ah"]
-[6.843048095703125, -0.63816237449646, "[TT] Period of the Orbit = 97.4 minutes"]
-[8.15034294128418, 5.228402614593506, "[TT] Calibration Algorithm Version of the MWR = v2.0"]
-[6.664370536804199, 8.837028503417969, "[FF] Measurement of the Polarisation and Directionality of Earth\u2019s Reflectance (POLDER) = Earth\u2019s Reflectance"]
-[9.078758239746094, 3.3919076919555664, "[FF] Effect on Neutrals of the Ions = Exert both a frictional drag and a frictional heating on the neutrals"]
-[10.265936851501465, 8.050470352172852, "[TT] Aperture of the Telescope = 400 mm (primary), 140 mm (secondary)"]
-[10.58061408996582, 2.2152698040008545, "[FF] Publication Date of the S056 X-ray telescope = April 1977"]
-[7.3050336837768555, 6.230029582977295, "[FF] Operation of the Optical Instruments = MWIR and Lasercom"]
-[8.762267112731934, 7.756312847137451, "[TT] Pixel Scale of the Detector = 4.13 arcsec/pixel"]
-[5.789011001586914, 3.091677188873291, "[TT] Computing Resource of the 'Fight club' asteroid simulations = Bluecrab supercomputer cluster"]
-[8.289790153503418, 6.686004161834717, "[FF] f/3.4 Number (Spatial) of the Camera = Unknown"]
-[4.3313188552856445, 2.1901955604553223, "[TT] Launch Location of the MySat-1 = United Arab Emirates (UAE)"]
-[5.545577526092529, 0.3607622981071472, "[TT] Launch Date of the ATLAS-1 = March 24, 1992"]
-[10.99211311340332, 6.314373970031738, "[TT] Substrate Material of the Grating = SiC"]
-[3.3631649017333984, 5.045643329620361, "[FF] Measurement Requirements of the SAR System = Each selected beam will be measured during two passes (ascending and descending). Furthermore, two receive polarization combinations per operation mode are to be measured simultaneously"]
-[6.7775774002075195, 5.9012370109558105, "[TT] Quantity of the Tyvak 61C = 1"]
-[6.866002082824707, 2.712946891784668, "[FF] Functionality of the UrtheCast Website = Fast-forward, pause, rewind and skip the near-live footage"]
-[6.156614303588867, -0.3628408908843994, "[TT] Mission Time of the ROBUSTA picosatellite = Up to three years"]
-[8.233473777770996, 2.771111011505127, "[TT] Measurement Category of the ST5 = Atmospheric Temperature Fields, Gravity, Magnetic and Geodynamic measurements, Atmospheric Humidity Fields, Atmospheric Winds"]
-[8.11674690246582, 3.9996302127838135, "[FF] Objectives of the CARMEN-1 = Effects of cosmic radiation in electronic devices, distribution of micro-particles and space debris Measure the high-energy radiation environment (ICARE). Measure the size distribution of micro- particles and space debris (SODAD)"]
-[6.508375644683838, 4.125516414642334, "[FF] Architecture Elements of the FORUM = Platform, payload and main mission performance"]
-[7.25268030166626, 1.7354350090026855, "[FF] Function of the bioCD = Measures the fern spores"]
-[5.605264186859131, 2.2288503646850586, "[FF] Mission Status of the OSIRISv3 = Unknown"]
-[8.5678129196167, 3.894777774810791, "[FF] Operating Modes of the SFx and specifically the SET-1 instrument = Dependent on solar activity and position in the orbit"]
-[7.6806535720825195, -0.8519849181175232, "[TT] SRR Date of the ICESat-2 = May 25, 2011"]
-[8.937167167663574, 7.407443046569824, "[TT] Electron Detector Surface Area of the REM = 25 mm2"]
-[9.997150421142578, 7.762025833129883, "[TT] GSD of the Optical telescope = 15 m"]
-[5.812474727630615, 7.224027156829834, "[TT] Data Transmission of the GT = Five 250-Hz samples every 20 ms"]
-[6.582834243774414, 8.243057250976562, "[TT] Number of Channels of the Spectral Channels = 5"]
-[6.666406631469727, 3.7374446392059326, "[FF] URL of the SPOT 7 = http://www.astrium-geo.com/files/pmedia/edited/r18072_9_spot_6_technical_sheet.pdf"]
-[14.177061080932617, 3.2362239360809326, "[TT] Mass of the Sapphire = 148 kg"]
-[12.302937507629395, 2.9404752254486084, "[TT] Hydrazine Tank Capacity of the AOCS = 4.7 kg"]
-[8.813270568847656, 3.6889519691467285, "[FF] Onboard Instruments of the Voyager 2 = Cosmic ray subsystem, low energy charged particle instrument, magnetometer"]
-[6.776832103729248, 1.855614185333252, "[FF] URL of the NASA Earth Observatory = https://earthobservatory.nasa.gov/images"]
-[10.476181983947754, 2.154257297515869, "[FF] First Measurements of the APXS = The first X-ray and alpha spectra will be recorded"]
-[9.67320728302002, -0.40822288393974304, "[TT] Altitude of the ASTERIA = 400 km"]
-[7.1017608642578125, 7.203557014465332, "[TT] Number of Photons Returning to Telescope of the ATLAS = Only a dozen or so"]
-[3.0908803939819336, 2.212204933166504, "[FF] Coastline Length of the Copernicus Sentinel-2 = Around 800 km"]
-[8.721783638000488, 8.631422996520996, "[TT] Pixels per FWHM of the Spectrometer = 3030"]
-[4.433205604553223, 6.917610168457031, "[TT] Communication System of the TanDEM-X = S-band receiver"]
-[6.400051593780518, -0.2442726045846939, "[TT] Minimum Interval of In-Plane Manoeuvres of the ALOS-2 = 1.5 days"]
-[5.451198577880859, 7.181931018829346, "[TT] Rate of the Data Transmission = 6 Mbit/s"]
-[8.398014068603516, 7.751728534698486, "[TT] Detector Array of the Micro-spectrometer = Linear InGaAs photodiode array with 256 high-quantum efficiency pixels"]
-[8.51067066192627, 1.7539253234863281, "[TT] Absolute Accuracy of the Integrated water vapor = \u00b1 2.0 kg/m 2"]
-[14.329151153564453, 3.223613977432251, "[TT] Mass of the Iraz\u00fa = 1 kg"]
-[5.64663028717041, 1.1538892984390259, "[TT] Imaging Date of the MRO = Nov. 1, 2016"]
-[6.8010053634643555, -0.6291841864585876, "[TT] Orbital period of the PROBA-3 = 19 hr 38 minutes"]
-[12.219319343566895, 3.6014931201934814, "[TT] Volume of the Propellant Tanks = 1106 liter"]
-[13.572279930114746, 5.839964866638184, "[TT] Minimum Power of the Solar Arrays = 4kW"]
-[4.159932613372803, 4.1952128410339355, "[FF] Founders of the COSPAS\u2013SARSat = Canada, France, Russia and the US"]
-[11.220992088317871, 0.6007986664772034, "[FF] Target of the Cheops = Stars hosting planets in the Earth-to-Neptune size range"]
-[11.445749282836914, 5.532443523406982, "[TT] Yield of the Haynes 242 = 1031 MPa"]
-[13.36500358581543, 7.775382995605469, "[TT] RF Output Power of the Wide Beam = 60 W"]
-[6.685837745666504, -0.5214570760726929, "[TT] Orbit Period of the SuperView-1 01 and Superview-1 02 = 97 minutes"]
-[9.503310203552246, 8.13134479522705, "[TT] Field of View of the Z-panel camera = 25o"]
-[14.249585151672363, 3.206533670425415, "[TT] Mass of the RIS = 43 kg"]
-[7.576386451721191, 8.864606857299805, "[TT] VIS Bands Wavelength of the Instrument = 0.47 \u00b5m & 0.64 \u00b5m"]
-[7.936025142669678, 6.303744792938232, "[TT] Instrument Type of the RDSA, PSA = Imaging multi-spectral radiometers (vis/IR)"]
-[8.09533977508545, 6.462172985076904, "[TT] Cross-track Scan of the TOMS = 111\u00ba (37 3\u00ba steps)"]
-[7.679581642150879, 6.840307235717773, "[TT] Exposure Time of the Camera System = 800 ms"]
-[7.198996067047119, 1.9062608480453491, "[TT] Design Life of the Carbonite-2 = 5 years"]
-[7.852497100830078, 0.040484342724084854, "[TT] Start Time of the Asteroid Day TV = 30 June at 12:00 CEST"]
-[9.547959327697754, 5.015358924865723, "[TT] Long Term Stability of the AOCS = 112 \u00b5rad"]
-[8.749946594238281, 4.508948802947998, "[TT] Attitude Sensor Types of the ACS = DSS (Digital 2-axis Sun Sensor), SSS (Spinning Sun Sensor), ST (Star Tracker)"]
-[8.313726425170898, -0.8668105602264404, "[TT] Thickness of the Carbon Dioxide Ice Patch = 9 cm"]
-[7.413389205932617, 2.9734396934509277, "[TT] Source Tank Content of the RRM3 module = Liquid methane"]
-[6.741389274597168, 8.452984809875488, "[TT] Spectral Channels of the CERES = 3"]
-[4.999607086181641, 8.214491844177246, "[TT] Bandwidth of the UHF Band = 20 kHz"]
-[4.783647537231445, 0.04884359985589981, "[TT] End of Life Date of the GIOVE = November 24, 2021"]
-[6.088161468505859, 1.8495357036590576, "[FF] Mission of the FLORIS = ESA FLEX"]
-[5.307018280029297, 3.858593463897705, "[FF] Number of Satellites of the HawkEye 360 = Not Provided"]
-[4.751178741455078, -1.7970023155212402, "[TT] Sample Collection Location of the Chang'e-5 = Siziwang Banner, Inner Mongolia"]
-[5.496933460235596, 7.121696949005127, "[TT] Data Transmission Speed of the LCTs = 600 Mbit/s"]
-[7.898044586181641, 7.1671648025512695, "[FF] Data Interface of the CCD (Charge-Coupled Device) = Special-purpose serial interface using data/strobe arrangement"]
-[13.513999938964844, 6.826862812042236, "[TT] Power Generation of the EAGLE ESPAStar = 1.2 kW"]
-[10.402523040771484, 3.229036808013916, "[TT] Quantity of the LightSail CubeSat = 1 of 10"]
-[9.64512825012207, 7.00171422958374, "[TT] Resolution of the ABI = 2 km"]
-[8.880966186523438, 4.932623863220215, "[TT] Pointing Modes of the TanSat = Eleven"]
-[5.535677909851074, 5.790848731994629, "[TT] CPU of the C&DH = RAD6000 CPU @ 20 MIPS"]
-[7.9352006912231445, 3.97031569480896, "[FF] Emission Detection of the ABEX = Lower energy emission"]
-[11.131302833557129, 5.8523688316345215, "[TT] Shielding Material of the EPI-Lo = Aluminum flashing of ~2 \u00b5m thickness"]
-[5.7008256912231445, 5.227321624755859, "[TT] Handling of the High Priority Commands = Directly by the telecommand decoder and by-passes all OBC software"]
-[9.80468463897705, -0.6574039459228516, "[TT] Orbit Altitude of the STP-S26 mission = 650 km"]
-[6.11478328704834, 7.02081823348999, "[TT] Data Rate of the Optical ISL return service = 600 Mbit/s or 1.8 Gbit/s"]
-[5.57206916809082, 2.028609037399292, "[FF] Mission Status of the BeiDou-2 = Unknown"]
-[5.040336608886719, 2.2308411598205566, "[TT] Mission Status of the STPSat-3 = Unknown"]
-[5.829358100891113, 0.5307063460350037, "[TT] Tandem Mission Completion Date of the ERS-1 and ERS-2 = May/June 1996"]
-[14.265398979187012, 3.2275917530059814, "[TT] Mass of the SMDC-ONE 2.1 = 4.1 kg"]
-[10.434198379516602, 2.068134307861328, "[TT] X-ray Source Distance of the NuSTAR = 12 million light years"]
-[10.13859748840332, 3.1168689727783203, "[FF] Observation Type of the DICE CubeSats = Plasma"]
-[5.399264812469482, 0.23185518383979797, "[TT] Operation Start Date of the SAMPEX = Before 1997"]
-[8.718997955322266, 3.185615301132202, "[FF] Data Collection of the Geospace Dynamics Constellation = Earth\u2019s ionosphere and thermosphere"]
-[7.770076751708984, 5.073666572570801, "[FF] Publication Date of the GRACE K-band ranging instrument = 2009"]
-[12.15909481048584, 2.956594705581665, "[TT] Default Propulsion Module of the Myriade Bus = Hydrazine propulsion module provided by Airbus Defense and Space"]
-[5.820450305938721, 6.332561016082764, "[TT] Information Transmission of the EDRS = Quasi-real time"]
-[6.479020118713379, 1.997309923171997, "[FF] URL of the Satellite = http://library01.gsfc.nasa.gov/gdprojs/projinfo/sage.pdf"]
-[6.097581386566162, 5.261729717254639, "[FF] Functions of the LCT = Relay Earth observation data from LEO satellites and verify the bidirectional optical link"]
-[10.313166618347168, 5.611933708190918, "[TT] Thermal Cycle Test of the ETFE Film = -100 to +70\u00baC, 15 cycles, N2 atmosphere"]
-[8.84110164642334, 3.3908884525299072, "[FF] Variable of the F-region ionosphere = Yes"]
-[12.1207275390625, 7.616885662078857, "[TT] Mass of the Imager = 135 kg"]
-[5.654277801513672, 3.170771598815918, "[TT] Contract Amount of the HawkEye 360 = $15.5 million"]
-[11.51672077178955, 3.651890277862549, "[TT] Ignition Duration of the T3\u00b5PS = 10 seconds"]
-[11.958005905151367, -0.33380982279777527, "[TT] Managed By of the TESS = MIT in Cambridge, Massachusetts, and managed by NASA's Goddard Space Flight Center"]
-[5.051141738891602, 7.03310489654541, "[TT] Uplink Rate of the ResourceSat-1 = 100 bit/s"]
-[5.915905952453613, 0.9253520965576172, "[TT] Image Acquisition Date of the GIIRS = 1 February 2019"]
-[5.376764297485352, 0.20335471630096436, "[TT] Launch Date of the STS-46/57 = Jul. 31, 1992 - Jun. 21, 1993"]
-[4.800500392913818, 6.055527687072754, "[FF] Function of the SDR (Software Defined Radio) = Dynamically change its receive and transmit frequencies"]
-[14.192627906799316, 2.799015998840332, "[TT] Mass of the KazSTSAT = <100 kg"]
-[9.500060081481934, -0.381046861410141, "[TT] Radius of the Orbital Phase 1 = Ca. 29 km"]
-[8.862741470336914, 6.984663009643555, "[TT] GSD of the HSC-III = 15 m"]
-[4.928546905517578, 1.898868441581726, "[FF] Mission Results and Anomaly Investigation of the HORYU-II = Unknown"]
-[8.583248138427734, 0.28857848048210144, "[FF] Comet Discoveries of the SOHO = 3000"]
-[5.950918674468994, 0.28995633125305176, "[TT] Final Maneuver Date of the Rosetta = 29 September 2016"]
-[10.77637767791748, 1.361114263534546, "[TT] Star Masses of the Iota Orionis = 23 and 13 times the Sun's mass"]
-[4.8042192459106445, -0.015867367386817932, "[TT] End of Life Date of the THEOS-2 = 2031"]
-[13.443415641784668, 2.9952540397644043, "[TT] Mass of the OPSAT-1000 satellite bus = 178 kg"]
-[6.267518520355225, 8.086246490478516, "[TT] Channels of the TopStar-3000 G1 = 12"]
-[13.971139907836914, 7.157472133636475, "[TT] Current of the Voltage 6 = 200"]
-[10.884953498840332, 3.5903518199920654, "[FF] Type of the Microwheel 10SP-M = Small Satellite"]
-[9.322124481201172, 3.62943172454834, "[FF] Model Input of the Satellite Magnetic Field Data = Field-Aligned Currents"]
-[4.737179279327393, 2.2744383811950684, "[TT] Launch Date of the Eutelsat Quantum = 2019"]
-[7.503157615661621, 2.946519136428833, "[FF] Detection Threshold of the MethaneSAT = Much lower than a point-source system"]
-[7.472777843475342, 1.837226390838623, "[FF] Application of the LISS-3 = Land and water resources management"]
-[3.875253915786743, -1.2537176609039307, "[TT] Lagrange Point of the Gaia = Lagrange point 2"]
-[10.806014060974121, 0.7184988856315613, "[FF] Composition of the TRAPPIST-1 Planets = Similar Stuff"]
-[9.154292106628418, 5.593071460723877, "[TT] Position Jitter of the Instrument = < 1 \u00b5rad rms"]
-[4.376253128051758, 7.580364227294922, "[TT] Frequency of the Microhard MHX-2420 = S-band"]
-[5.281247615814209, 2.789062261581421, "[TT] Operator of the MANTIS = Open Cosmos"]
-[9.449775695800781, 4.781918048858643, "[TT] Attitude Control of the Deimos-2 = Three-axis"]
-[8.63684368133545, 4.553496837615967, "[FF] Star Tracker (STR) of the PARASOL = Main instrument used to verify the satellite orientation"]
-[5.609651565551758, 7.285910606384277, "[TT] Frequency Ratio of the KBR = Exact 3-to-4 ratio"]
-[3.1613543033599854, 1.6568737030029297, "[TT] Revisit Time of the Sentinel-2 = 5 days"]
-[8.399904251098633, 8.113054275512695, "[TT] MS Pixels of the Spectral bands = 3,000 pixels"]
-[4.5641632080078125, 2.817086935043335, "[TT] Location of the SOCC = Hsinchu, Taiwan"]
-[3.845974922180176, 3.45196270942688, "[TT] End of Life Date of the Galileo Second Generation (G2) = 31 December 2039"]
-[11.908875465393066, 6.634041786193848, "[TT] Energy Range of the HIPS = 1-30 MeV"]
-[9.289783477783203, 3.233473539352417, "[FF] Science Goal of the TRACE = Explore the relation between diffusion of the surface magnetic fields and changes in heating and structure throughout the transition region and corona"]
-[7.001988887786865, -0.22992178797721863, "[TT] Earth Mapping Cycle of the OCO-2 = 32 days"]
-[5.450575828552246, 2.2644588947296143, "[FF] Mission of the OSIRIS = Odin"]
-[6.91585111618042, 9.043961524963379, "[TT] Band Center of the POLDER-1/2 = 670P nm"]
-[7.1659836769104, 1.2696422338485718, "[TT] Data Relay Services Start of the ExoMars Trace Gas Orbiter = 2023"]
-[12.45647144317627, 0.5618524551391602, "[TT] Launch Date of the PLATO = December 2026"]
-[14.027644157409668, 3.2268240451812744, "[TT] Mass of the Cabling/harness = 0.1 kg"]
-[6.432952404022217, -0.6756306290626526, "[TT] Orbital Operations Duration of the CubeRRT = ~1 year"]
-[7.343878269195557, 5.547812461853027, "[FF] Components of the FEE = FPPE (Focal Plane Proximity Electronics) and VAU (Video Acquisition Unit)"]
-[3.5859181880950928, 6.109794616699219, "[TT] Number of Dual Polarized Linear Arrays per Tile of the Active Antenna = 24"]
-[4.614009380340576, 7.833215713500977, "[TT] Data Transmission Frequency of the DCP = 1691, 1694.5 MHz"]
-[5.759664058685303, 4.674433708190918, "[FF] Communication Capability of the Prometheus Satellite = Transfer audio, video, and data files from man-portable, low-profile, remotely located field units to deployable ground stations terminals using over-the-horizon satellite communications"]
-[7.773940563201904, 2.9838995933532715, "[FF] Purpose of the TROPOMI = Map a multitude of trace gases such as nitrogen dioxide, ozone, formaldehyde, sulphur dioxide, methane, carbon monoxide and aerosols"]
-[8.735852241516113, 7.663305759429932, "[TT] Size of the CCD = 1024 x 1024 pixels"]
-[8.676651954650879, 2.6011037826538086, "[FF] Objective of the LIMS = Measurement of vertical gas concentrations and temperature profiles in the stratosphere"]
-[12.154584884643555, 3.267289638519287, "[FF] Propellant of the Burner IIA upper stage = Solid-propellant"]
-[9.884653091430664, 4.254641056060791, "[FF] Magnet Types of the AMS-01 = Seven magnets for field calculation, leakage and dipole moment; Three full-size magnets for space qualification, destructive testing and flight"]
-[11.43882942199707, 3.9376089572906494, "[FF] Proximity Operations Plan of the AeroCube-OCSD-B and -C = Co-orbital corkscrew orbit"]
-[4.788473606109619, -1.8735039234161377, "[FF] Mission Overview of the Chang'e 4 = Unknown"]
-[6.002636432647705, -0.16866444051265717, "[TT] Mission Duration of the Rosetta = 2 years"]
-[8.055059432983398, 4.572648525238037, "[TT] Radiation tolerance of the PHA = >100 krad"]
-[8.127802848815918, -0.20197159051895142, "[FF] Impact of Climate Change of the Arctic = Longer unfrozen seasons"]
-[6.3703694343566895, 2.0842902660369873, "[FF] URL of the ARTEMIS satellite = http://www.esa.int/Our_Activities/Operations/Artemis_the_ATV_whisperer"]
-[3.4769389629364014, 4.776885509490967, "[FF] Project Partners of the SIR-C/X-SAR = NASA/JPL, DARA/DLR, and ASI (Agenzia Spaziale Italiana)"]
-[5.578847408294678, 7.518791198730469, "[TT] Specific Impulse of the HET-X = 1300 - 2200 ISP"]
-[3.779177188873291, -0.7414942979812622, "[TT] Orbit Type of the Space Station = Low-Earth orbit"]
-[4.167391777038574, 4.47760534286499, "[FF] Operation of the SAR-VTB = Independent of COSPAS-SARSAT system"]
-[3.8266711235046387, -1.1748127937316895, "[TT] Orbit of the eROSITA = Halo orbit around the L2 point"]
-[9.997560501098633, -1.4902936220169067, "[TT] Orbit Inclination of the PROBA-3 = 59\u00ba"]
-[7.0525617599487305, 4.277773380279541, "[FF] Unknown of the ECS = Unknown"]
-[7.589014530181885, 8.685662269592285, "[TT] GSD of the Spectral Band A = 5"]
-[8.020400047302246, 0.1787436455488205, "[TT] Contact with Asteroid Surface of the MASCOT = Approximately 20 minutes after separation"]
-[9.83742904663086, 6.4667534828186035, "[TT] Instrument Pointing Requirements of the Earth Radiation Budget Experiment (ERBE) = Control Knowledge Stability 720 arcsec 180 arcsec 79 arcsec/6.6 sec"]
-[8.07313060760498, 4.488023281097412, "[FF] Radiation Tolerance of the \u00b5ASC = Total-dose radiation, dose-rate for SEU (Single Event Upset), and SEL (Single Event Latch-up)"]
-[7.405327796936035, 6.137266159057617, "[FF] Operation Principle of the Radar and laser altimeters = Sending radio or laser light pulses toward Earth\u2019s surface and recording the reflections as they bounce back"]
-[8.640267372131348, 1.048370361328125, "[TT] Survey Time of the Aquarius = 8 days"]
-[9.052754402160645, 6.508244514465332, "[TT] Viewing Angles of the PROBA-1 = Five different"]
-[8.598001480102539, 1.304423451423645, "[FF] Function of the ADPS = Automatically retrieves raw downlink files of Aquarius science data from the CONAE database and processes this data into time-ordered salinity data files"]
-[4.336155414581299, 7.222029685974121, "[TT] Transmitter of the OBRC instrument = Klystron"]
-[14.167975425720215, 2.9547278881073, "[TT] Mass of the PICOSAT = 0.275 kg"]
-[8.135149955749512, -0.3301111161708832, "[TT] Ice Spread of the Arctic Ocean = Slowed"]
-[8.403425216674805, -0.37833142280578613, "[TT] Range of Values of the Ice: edge location = 0 - 100"]
-[9.681443214416504, -0.10251204669475555, "[TT] Altitude of the Tsubame = 271.5 km and 216.8 km"]
-[5.5318708419799805, -0.5119428038597107, "[TT] Study Duration of the Odin = Over 20 years"]
-[8.281794548034668, 6.651424407958984, "[TT] Ground System Provider of the Advanced Baseline Imager = L3Harris Technologies"]
-[8.617086410522461, 0.15707889199256897, "[TT] Small Lobe Dimensions of the Comet = 2.6 x 2.3 x 1.8 km"]
-[7.423440933227539, 0.18927054107189178, "[TT] Travel Time to Asteroid of the OSIRIS-REx = About two years"]
-[7.0210442543029785, 6.625270843505859, "[FF] Type of the Laser = Unknown"]
-[8.520873069763184, 6.443113327026367, "[TT] Scanning Rate of the ATM = 20 Hz"]
-[9.217681884765625, 3.7679100036621094, "[FF] Performance Measurement of the Solar Array = Current-voltage (I-V) sweeps"]
-[10.28382396697998, 5.292497158050537, "[FF] Heat Transport System of the FUS (Frame Unit System) = Collecting power to be dissipated externally to the LCT"]
-[8.028060913085938, -0.3030739724636078, "[FF] Data Usage of the GRACE-FO = Measure mass changes in the thick ice sheets of Greenland and Antarctica"]
-[7.7723002433776855, -0.41560906171798706, "[FF] Article Date of the Micro cold traps = 26 October 2020"]
-[12.153568267822266, 3.0073184967041016, "[TT] Propellant of the Propulsion Module = Hydrazine"]
-[8.755258560180664, 3.5484766960144043, "[FF] Measurement of the Gaia = The acceleration of the Solar System"]
-[7.092441082000732, 5.896890640258789, "[FF] Enhancement of the Onboard Atomic Clocks = More precise"]
-[5.143316268920898, 7.052934646606445, "[TT] TT&C Downlink Rate of the MERLIN = 625 kbit/s"]
-[6.288885116577148, 8.094247817993164, "[TT] Channels of the MTVZA-GY = 29"]
-[9.812438011169434, 5.633205890655518, "[FF] Thermal Stability of the Doublet = Relaxes the thermal stability requirements of the optical bench"]
-[4.753178596496582, -1.8597586154937744, "[TT] Launch Vehicle of the Chang'e-5 = Long March 5 (CZ-5)"]
-[7.8170647621154785, 2.604356527328491, "[FF] Objective of the Optical Payload = Detection and quantitative analysis of HTE (High Temperature Events) like wildfires and volcanoes"]
-[6.428004264831543, 4.348288536071777, "[FF] Management Responsibility of the Mini Centrifugal Subsystems = NASA/ARC"]
-[4.878297805786133, 5.167818069458008, "[FF] Tasks of the MCCs = Receive data from nationally associated LUTs and international MCCs, match signals originating from the same signal source, merge beacon signals from identical sources, geographically sort data and transmit data and alerts to relevant RCCs"]
-[5.812191486358643, 3.546391010284424, "[TT] Measurement Continuity of the PARASOL = Until the end of September 2013"]
-[9.528862953186035, 0.4386323392391205, "[TT] Altitude of Rear Heatshield and Parachute Jettison of the Schiaparelli = 1.3 km above the surface"]
-[6.8870625495910645, 0.8092642426490784, "[TT] Image Span of the Herschel = Over 1\u00ba on the long side"]
-[6.494906425476074, 5.545641899108887, "[FF] Function of the Optical Communication Payload = Transmit data via laser to satellites in geostationary orbit"]
-[6.257491111755371, 8.100932121276855, "[TT] Channels of the SSM/I = 7"]
-[4.770305156707764, 8.230443000793457, "[TT] Frequency of the GFO-RA = 13.5 GHz"]
-[8.603821754455566, 3.3978431224823, "[TT] Measurement of the SSUSI = Visible radiation (airglow and terrestrial albedo)"]
-[8.202300071716309, -1.052559494972229, "[TT] Sea Ice Thickness Measurement of the ICESat-2 = Up to 5 meters"]
-[8.855633735656738, 6.516571044921875, "[TT] Image Acquisition Files of the PROBA-V = 1.392"]
-[6.741631984710693, 6.373856544494629, "[TT] Processing Time of the Level 1B = 60 s"]
-[6.1545634269714355, 3.1329100131988525, "[TT] Manufacturer of the BlackSky\u2019s Global-4 = BlackSky"]
-[7.219646453857422, 1.2652533054351807, "[TT] Propulsion of the Mars Ascent Vehicle (MAV) = Solid rocket motors"]
-[4.926084995269775, 0.7221879959106445, "[FF] Approval Date of the STD-8719.14A = 2011-12-08"]
-[9.885454177856445, 5.685268402099609, "[TT] Focal Plane Temperature Control of the ASTERIA = Highly stable"]
-[7.447660446166992, 1.6296627521514893, "[FF] Purpose of the Kepler Mission = Detecting other planetary systems"]
-[4.772679805755615, -1.8619434833526611, "[FF] Mission Tasks of the Chang'e-5 = Number of Firsts for China"]
-[7.91792631149292, 8.886813163757324, "[TT] Operating Wavelength of the Coarse Lateral Sensor = Around 980 nm"]
-[7.601360321044922, 9.244254112243652, "[TT] Band 1 of the CIRiS = 7.4 \u00b5m to 13.72 \u00b5m"]
-[9.774301528930664, 7.097355365753174, "[TT] Ground Resolution of the SiPD = 1m"]
-[8.472804069519043, 5.576847076416016, "[TT] Accuracy of the MEOLUT = 2\u20135 km"]
-[10.114049911499023, -2.7353663444519043, "[TT] Data Retention of the SLC NAND-Flash = 10 years"]
-[6.8426408767700195, -0.6107321977615356, "[TT] Orbit Period of the ExoMars TGO = Every two hours"]
-[9.264948844909668, 3.2056195735931396, "[TT] Observation Duration of the Coronagraph Instrument = Minimum 1,000 hours"]
-[8.357675552368164, 1.6966804265975952, "[TT] Measurements of the MicroMAS-2 = Precipitation, temperature, and humidity"]
-[5.620420455932617, -1.981496810913086, "[TT] Bus Design of the KOMPSAT-3 = 3-axis stabilized"]
-[8.134188652038574, 3.7338876724243164, "[FF] Observation Type of the OCO-3 PMA = Non-nadir"]
-[7.967794418334961, 7.920699119567871, "[TT] Data Digitization of the HSC-III optics subsystem = 8 or 10 bit"]
-[5.174155235290527, 1.4807283878326416, "[FF] Date of the 30th Annual AIAA/USU SmallSat Conference = August 6-11, 2016"]
-[12.620122909545898, 9.09626579284668, "[TT] Local equator crossing time of the GOSAT-2 = 13:00 \u00b1 0:15 hour"]
-[10.722455024719238, 2.8385565280914307, "[FF] Mission Design of the CICERO = Microsatellite to a 6U CubeSat Form Factor"]
-[5.963917255401611, 1.523754358291626, "[TT] Detector Units Status of the IXPE observatory = Complete"]
-[10.409220695495605, 3.3230671882629395, "[TT] Microcontroller of the SCARAB = PIC24-based CubeSat Kit"]
-[7.523769855499268, 2.9294614791870117, "[TT] Methane Detection Threshold of the iSIM-90 = 150 kg/h"]
-[5.54753303527832, 0.5775675177574158, "[TT] Launch Year of the ERS-2 = 1995"]
-[5.555638313293457, 4.168964862823486, "[TT] Functionality of the MEOSAR = Effective"]
-[10.507149696350098, 5.864906311035156, "[TT] Inside Temperature Range of the HORYU-2 = 0 to 18\u00baC"]
-[7.810762882232666, 8.327722549438477, "[TT] Spectral Bands of the Imager = 6"]
-[10.31884765625, 7.3614726066589355, "[TT] Ground Swath of the IRFS-2 = 1,000 to 2,500 km"]
-[3.795318365097046, 6.87300443649292, "[FF] Type of the Beacon station antenna = 7-element Yagi antenna"]
-[5.611992359161377, 1.3733437061309814, "[FF] Information Kit Date of the Columbus = January 2008"]
-[5.453973770141602, 2.2306034564971924, "[FF] Affiliation of the Santiago Urue\u00f1a = Unknown"]
-[8.105096817016602, 6.609135627746582, "[TT] Operation Mode of the Camera Sensor = Snapshot or staring mode"]
-[6.956530570983887, 5.20268440246582, "[FF] Components of the EPS = COTS (Commercial-off-the-Shelf) components, MPTT (Maximum Power Point Tracking) ICs, FRAM (Ferroelectric Random Access Memory), AVR microcontroller"]
-[7.610950946807861, -0.5994135737419128, "[FF] URL of the ICESat-2-ND-Presentation = http://www.scribd.com/doc/76177455/ICESat-2-ND-Presentation-4-18-11"]
-[5.948943614959717, 4.1557087898254395, "[FF] Cooperation Paradigms of the Multisensory feature = Federation and Expansion"]
-[10.576200485229492, 7.4458417892456055, "[TT] Swath Width of the Optical Sensor (OPS) = 10 km"]
-[6.343371391296387, 4.331089496612549, "[FF] Location of the MOC = UCB/SSL"]
-[8.488471031188965, 7.35212516784668, "[TT] Image Resolution of the Supervision Cameras = 1280 x 1024 pixels"]
-[8.349522590637207, -0.7644643783569336, "[TT] Annual surface elevation change rates accuracy of the ATLAS = Better than 0.25 m/yr"]
-[6.386363983154297, 1.5165433883666992, "[FF] Presentation Date of the MICROSCOPE = Oct.12-16, 2015"]
-[8.069416046142578, 5.771499156951904, "[FF] Usage of the CAM = Used for the intelligent pointing system"]
-[18.665767669677734, 3.935915231704712, "[TT] NE\u0394T (K) of the ICI-7 = 1.4"]
-[7.068058967590332, 7.082023620605469, "[TT] Laser Technology of the DIAL Instrument = 2.05 \u00b5m"]
-[6.608115196228027, -0.034403156489133835, "[TT] Operation Duration of the Cooling System = More than 15 years"]
-[5.691424369812012, 7.083314895629883, "[TT] Measurement Speed of the OLA = Up to 10,000 measurements/s"]
-[6.278748989105225, 3.76771879196167, "[FF] Satellite Configuration of the RADARSAT Constellation = Orbiting in formation, each dephased by 120\u00b0"]
-[9.01174259185791, 2.5969667434692383, "[TT] Particle Detection Location of the IBEX = Outer heliosphere"]
-[7.728603363037109, 7.933041572570801, "[FF] Function of the Instrument = Understanding of current dynamics of volatile sources, sinks, and processes"]
-[4.157036781311035, 4.828372478485107, "[TT] Spatial Acquisition Duration of the Alphasat TDP1 = Reliably achieved within 7 s"]
-[4.390268802642822, 1.8374004364013672, "[TT] Launch Date of the RADARSAT-2 = 2007"]
-[5.49689245223999, 2.340855598449707, "[TT] EMC Test Locations of the MPO spacecraft = ESTEC laboratories"]
-[10.629545211791992, 1.4230257272720337, "[TT] Energy Reflection of the Bright sea ice = 80 percent of the Sun\u2019s energy"]
-[9.15591049194336, 7.575399875640869, "[TT] Multispectral Spatial Resolution of the DMAC = 5 m"]
-[6.844466209411621, -0.5202482342720032, "[TT] Revisit Time of the Orbit = 14 days"]
-[5.5446343421936035, 5.072258472442627, "[TT] Connector Type of the Satellite = 51-pin connector"]
-[7.367301940917969, 5.892823219299316, "[FF] Transmission Method of the Imagettes = Raw data to ground or processed on-board"]
-[7.948062419891357, 5.502045631408691, "[FF] Instrument Type of the METIS = Multi-Element Telescope for Imaging and Spectroscopy"]
-[7.9129862785339355, 5.3835225105285645, "[TT] Range-dependent Biases of the FLLS = Dimensionless"]
-[6.4789509773254395, 2.873647689819336, "[TT] De-aliasing of the Constellations = Not Needed"]
-[6.114948272705078, -0.569226861000061, "[TT] Operation Duration of the RADARSAT-2 = 10 years"]
-[6.116525650024414, 1.3317703008651733, "[FF] Presentation Date of the LIDAR = March 16-20, 2015"]
-[14.678563117980957, 6.65772008895874, "[TT] Capacity of the FS-5 battery = 24 Ah"]
-[5.846030235290527, 3.709402084350586, "[TT] First Flight of the SIMBA Satellite = 2016"]
-[6.5548882484436035, 5.768137454986572, "[TT] Maximum Number of Racks of the JEM/Kibo = Up to 23 racks"]
-[9.765222549438477, -0.23028001189231873, "[TT] Altitude of the GPS Signal Environment = Up to geosynchronous orbit (35,900 km)"]
-[5.283078670501709, 4.084935665130615, "[TT] Integration of the MEOSAR = GNSS (Global Navigation Satellite Systems) constellations"]
-[9.783116340637207, -0.645381510257721, "[TT] Orbit Altitude of the GRIFEX = ~ 650 km"]
-[7.999733924865723, 5.843173503875732, "[FF] Deployment Camera Verification of the Spacecraft = Completed"]
-[6.3883891105651855, 6.4905314445495605, "[TT] Message Repeat Interval of the ODB = 10 seconds"]
-[6.403717041015625, 2.502220392227173, "[FF] URL of the Space Wire = http://spacewire.computing.dundee.ac.uk"]
-[6.64326810836792, 0.7266968488693237, "[FF] Publication Date of the Herschel = Aug. 20, 2013"]
-[6.487311363220215, -0.7950851321220398, "[TT] LTAN of the SARAL spacecraft = 6:00 hours"]
-[9.7099027633667, -0.16839665174484253, "[TT] Orbital Altitude of the TSUBAME = 167.4 km"]
-[6.667140007019043, 1.678409457206726, "[FF] URL of the Rosetta = http://sci.esa.int/rosetta/55295-getting-to-know-rosetta-s-comet/"]
-[7.348445892333984, 5.4952073097229, "[FF] Components of the LRI = Single frequency laser, Fabry Perot reference cavity, triple mirror assembly (TMA), OBS (Optical Bench Subsystem), instrument electronics"]
-[7.942842960357666, 9.059273719787598, "[TT] Wavelength of the ATLAS = 1064 nm"]
-[7.816391944885254, 5.090238094329834, "[FF] Purpose of the CAL switches = Onboard calibration"]
-[7.601237773895264, -0.804360568523407, "[TT] Operation Period of the ICESat = 2003-2010"]
-[10.985152244567871, 2.8687634468078613, "[TT] Dimensions of the Microsatellite = 52 cm x 52 cm x 45 cm"]
-[13.328980445861816, 7.840040683746338, "[TT] RF Output Power of the S-band transmitter = Adjustable from 27 to 33 dBm"]
-[3.6952457427978516, 4.490214824676514, "[FF] Mission Purpose of the RISAT-1 = Utilise all-weather, day-and-night SAR (Synthetic Aperture Radar) for applications in agriculture, geology, flood monitoring, and more"]
-[3.3796751499176025, 3.673948287963867, "[FF] URL of the PAZ and TerraSAR-X = http://www.dlr.de/dlr/en/desktopdefault.aspx/tabid-10081/151_read-7994/year-2013/%23gallery/12103#gallery/12103"]
-[3.7883188724517822, 1.1334456205368042, "[TT] Height of the Falcon-9 first stage = 14 stories"]
-[6.780941963195801, 1.0124706029891968, "[FF] Article Release Date of the Solar Orbiter = 27 April 2021"]
-[4.004966735839844, 2.1264967918395996, "[TT] Launch Vehicle of the ORS-3 Mission = Minotaur I"]
-[7.875736713409424, 8.024012565612793, "[TT] Spectral Range of the HSC-III optics subsystem = 400-1000 nm"]
-[11.892648696899414, 5.445582389831543, "[TT] Housing Size of the NIRST instrument = 35 cm x 40 cm x 50 cm"]
-[3.817166805267334, 0.8773173689842224, "[FF] Launch Date of the PSLV-C34 = June 22, 2016"]
-[10.982236862182617, 2.0406594276428223, "[TT] Data Collection Period of the XMM-Newton = 2016 and 2018"]
-[3.6806938648223877, -1.0514757633209229, "[TT] Orbit Type of the Secondary Payloads = Elliptical"]
-[3.8223235607147217, 7.199467182159424, "[TT] Antenna Gain (dB) of the Antenna = >37"]
-[8.58619213104248, 2.097759246826172, "[TT] Swath Width of the SeaWinds scatterometer = 1600 km"]
-[7.648865222930908, 9.034479141235352, "[TT] Spectral Range (\u00b5m) of the Band 10 = 0.90 - 0.965"]
-[10.881170272827148, 7.579615116119385, "[TT] Observation Swath of the POLDER-2 = 2400 km"]
-[4.503683567047119, 1.3956537246704102, "[FF] Symposium Date of the AlSAT-1 = Sept. 20-24, 2004"]
-[13.363208770751953, 5.5016350746154785, "[FF] Quantity of the Roll-out solar arrays = 6"]
-[8.733258247375488, 8.018035888671875, "[FF] Spacers of the Optic = Gray"]
-[5.425283432006836, 1.519550085067749, "[FF] Ground Segment Coordination Body Workshop Date of the RapidEye = June 6-7, 2012"]
-[11.398541450500488, 5.804414749145508, "[TT] Material of the Decks = Aluminum honeycomb sandwich bonded between Gr/E skins"]
-[6.124150276184082, 2.5763776302337646, "[FF] Project Role of the AU = Orbital Analysis, Flight Software, Structures and Mechanisms, Thermal & Radiation Design & Analysis"]
-[3.8551244735717773, 2.0001742839813232, "[TT] Launch Vehicle of the GovSat-1 = SpaceX Falcon 9 Rocket"]
-[5.003750801086426, 4.157257080078125, "[FF] Software Packages of the GeoSat-2 = User4EO, Plan4EO, Fly4EO, Control4EO, Track4EO, Archive4EO, Process4EO, Monitor4EO and CalVal4EO"]
-[8.303112983703613, 3.1114468574523926, "[FF] Purpose of the MLS = Chemistry of the middle and upper stratosphere, Monitoring of ozone chemistry, Measuring radicals, reservoirs, and source gases in chemical cycles which destroy ozone, Measuring SO2 and other gases in volcanic plumes"]
-[5.1209001541137695, 2.250082015991211, "[TT] Mission Type of the CubeRRT = EO"]
-[6.921612739562988, 6.519113540649414, "[TT] Interruption Frequency of the Sounding Operation = Every 30 minutes"]
-[5.2172722816467285, 2.277472496032715, "[TT] Mission Lead of the THEMIS = Vassilis Angelopoulos"]
-[5.2415995597839355, 8.017154693603516, "[TT] Frequency Response of the SCM = ELF/VLF range"]
-[10.195335388183594, 5.88905143737793, "[TT] Detector Array Operating Temperature of the Radiometer = 11 and 12 K"]
-[6.790810585021973, 7.388689041137695, "[TT] ADCs Resolution of the DAQ electronics = 14 bit"]
-[8.898833274841309, 0.9448213577270508, "[TT] Project Scientist Affiliation of the Parker Solar Probe = Johns Hopkins University Applied Physics Laboratory"]
-[8.990236282348633, 5.8316240310668945, "[FF] Altitude Measurement of the OMPS = Yes"]
-[10.263126373291016, 4.4897003173828125, "[TT] Actuators of the AOCS = 4 reaction wheels and two sets of eight thrusters"]
-[13.43985366821289, 5.490488052368164, "[TT] Solar Panels of the NSat = 4"]
-[9.065657615661621, 9.974150657653809, "[TT] FOV per channel of the Eastman Kodak KLI14403 linear CCD sensor = 26.6\u00ba"]
-[6.311577796936035, -1.389892339706421, "[TT] Launch Year of the GRACE Follow-On = 2018"]
-[6.494091987609863, 1.878061294555664, "[FF] URL of the Unknown = http://www.dso.org.sg/cmsresource/20110309337087956336.pdf"]
-[8.36228084564209, 4.633605003356934, "[FF] Surface-to-Mass Ratio of the LARES = Optimal"]
-[10.907873153686523, 2.9695122241973877, "[TT] Stabilization of the Picard microsatellite = Three-axis"]
-[5.2707905769348145, 4.017824649810791, "[TT] Number of Satellites of the OHB-SSTL consortium = 8"]
-[5.662558078765869, 3.706655740737915, "[TT] Total Impulse of the SkySat-4 = 57 Ns"]
-[14.132912635803223, 7.194504261016846, "[TT] Voltage of the EPS = 28 V and 5 V"]
-[5.896678447723389, 0.8423914313316345, "[FF] Image Shooting Date of the IKAROS = June 16, 2010"]
-[13.524822235107422, 5.505341529846191, "[TT] Number of Cells per String of the Solar Array = 39"]
-[10.50491714477539, 2.1888349056243896, "[FF] Purpose of the ROSAT X-ray telescope = Confirm the nature of Hoinga"]
-[7.237204551696777, 6.456870079040527, "[FF] Function of the Reference Gaussian Profile = Used to determine the quality of the laser beam and monitor potential degradation of the beam shape over the mission lifetime"]
-[4.0693039894104, 6.242724895477295, "[TT] Source of the Printed antenna array = Indigenous"]
-[7.4058637619018555, 5.965461730957031, "[FF] Challenge of the Synchronization = Major"]
-[4.691653251647949, 3.2773284912109375, "[TT] Manufacturer of the Ka-band Transmission Assembly = Thales Alenia Space in Spain"]
-[10.953177452087402, 2.059852361679077, "[TT] Reconfiguration Year of the XMM = 2017"]
-[6.711849689483643, 0.8433237075805664, "[TT] Next Close Pass of the Sun of the Solar Orbiter = March 2022"]
-[7.149235248565674, 6.807816982269287, "[FF] Response Speed of the APD detector = High"]
-[9.4523286819458, 5.033200740814209, "[FF] Sailboat (SB) Mode of the ICESat = YG axis (plus or minus) is closely coincident with the satellite velocity vector"]
-[8.684550285339355, 1.2170041799545288, "[TT] Beam Resolution of the Aquarius = Three beams: 76 km x 94 km, 84 km x 120 km, 96 km x 156 km"]
-[11.431974411010742, 2.1644227504730225, "[TT] \u0394V (cm/s) of the Cosmos 2251 Debris = 0.17"]
-[6.78053092956543, 7.449884414672852, "[TT] Yaw Coupling Factor of the Beamsplitter = 2.2 mm/rad"]
-[10.914511680603027, 10.100074768066406, "[FF] Publication Date of the Alpha Magnetic Spectrometer = 28 January 2021"]
-[6.049819469451904, -0.4469732642173767, "[TT] Planned Duration of the Science Operations = At least 2 years"]
-[5.564947605133057, 1.5205000638961792, "[FF] Conference Presentation Date of the Trailblazer = March 29-31, 2011"]
-[8.092570304870605, -0.4903298318386078, "[FF] Result of the SAR = Large-area maps of sea-ice movement in the Arctic"]
-[1.7447096109390259, -2.0763614177703857, "[TT] Separation Time from Hayabusa-2 of the MASCOT = 03:58 CEST"]
-[5.135944843292236, 2.733037233352661, "[TT] Affiliation of the Verner Suomi = University of Wisconsin-Madison"]
-[7.785900115966797, 1.3201961517333984, "[FF] Measurement Capabilities of the ROSE-L = Vegetation, ice, and ocean parameters"]
-[7.662929058074951, 1.007175326347351, "[TT] DOI of the Gravity Recovery and Interior Laboratory (GRAIL) = 10.1126/science.1231507"]
-[6.818291187286377, 6.060431480407715, "[TT] High-sensitive of the Mode = -"]
-[7.950366497039795, 4.7665252685546875, "[FF] Typical Value of the C2H2O2 = 0.2"]
-[10.149066925048828, 9.32172966003418, "[TT] IGFOV at Nadir for Broadband Visible of the Instrument = 0.5 km"]
-[7.20259428024292, -0.2554780840873718, "[TT] Orbits of the DSLP = 5500"]
-[6.812742710113525, 5.976999282836914, "[TT] Modes of the OCM = Real-time and playback"]
-[4.3160810470581055, 7.428570747375488, "[TT] Spectrum of the Lightspeed = Ka-band"]
-[7.174464225769043, 4.363278388977051, "[FF] Unknown of the SOLCON = Unknown"]
-[5.132424354553223, 2.3835089206695557, "[TT] Agency of the Kondor-E = NPOMash"]
-[9.508370399475098, 6.1736578941345215, "[FF] Degree of Coverage of the Partially Overlapping Contrails of the Model = Four times greater"]
-[10.476768493652344, 2.324737310409546, "[TT] Detection Type of the X-ray Detectors = Single incoming X-ray photons"]
-[9.409221649169922, 0.542835533618927, "[TT] Semimajor Axis of the SMART-1 = 3416.853 km"]
-[5.83463191986084, -0.6512706875801086, "[FF] Orbital Decay Prediction of the POPACS = Three years after launch"]
-[8.088059425354004, 8.128965377807617, "[TT] 1 km to 1 km, 0.5 km (wavelength/detector dependent) of the Channel-to-Channel Registration = \u00b1 5.2 \u00b5rad"]
-[1.6048839092254639, 3.7647628784179688, "[TT] Fault-tolerant satellite design of the BEESAT-1 = Yes"]
-[5.523379802703857, 0.35630324482917786, "[TT] Launch Date to ISS of the Flock 1a = January 9, 2014"]
-[6.708380222320557, 1.6158709526062012, "[FF] URL of the Emirates Mars Mission = https://aetoswire.com/en/news/emirates-mars-mission-hope-probe-ready-for-launch-from-japans-tanegashima-space-centre"]
-[14.649868965148926, 6.750985622406006, "[TT] Battery Capacity of the EPS = 1.8 Ah"]
-[13.188082695007324, 7.237151145935059, "[TT] Power Consumption of the RM = ~1.4 W"]
-[7.452475547790527, 2.9174740314483643, "[TT] Field of View of the MethaneSAT = Hundreds of kilometres wide"]
-[11.795583724975586, 4.38868522644043, "[TT] Size of the SporeSat = 10 cm x 10 cm x 34 cm"]
-[5.460106372833252, 6.246973514556885, "[TT] Capacity of the CoReCi = 850 Gbit (EOL) with Flash technology"]
-[5.282333850860596, 7.525901794433594, "[TT] Margin of the Unit = 2.52 dB"]
-[7.783738136291504, 2.1907148361206055, "[FF] Purpose of the CZCS = Ocean colour measurements"]
-[7.349032402038574, 8.848186492919922, "[TT] Filter Type of the NUV channel = Fused Silica Window"]
-[8.57826042175293, 5.205244541168213, "[TT] Measurement Range YACC and ZACC axes of the GFO Accelerometer = \u00b15 x 10-5ms-2"]
-[5.118273735046387, 0.7183206677436829, "[TT] Data Collection Start Date of the SIM = March 4th"]
-[5.52189826965332, 5.563830852508545, "[TT] Processor of the CryoSat = Sparc ERS 32"]
-[7.0774149894714355, 1.2750146389007568, "[FF] Shutdown Date of the Spitzer Space Telescope = January 30, 2020"]
-[5.497459411621094, 7.055004119873047, "[TT] Data Transmission Speed of the CubeLCT = Up to 100 Mbit/s"]
-[9.1182222366333, 2.68991756439209, "[FF] Release Date of the Giant solar flare = Sept. 15, 2014"]
-[10.46989917755127, 5.812074661254883, "[TT] Minimum Temperature of the GOES-R satellite = -55\u00baC"]
-[14.207658767700195, 3.261941432952881, "[TT] Mass of the CMG = 500 g"]
-[9.350749015808105, 5.332671642303467, "[TT] Azimuth Alignment of the Inertial Reference Systems = 70 degrees"]
-[8.426053047180176, 8.220749855041504, "[FF] On-axis Unapodized Spectral Resolution of the CrIS Instrument = \u2264 Values given in Table 5"]
-[3.834629774093628, 0.8924541473388672, "[TT] Launch Date of the PSLV-C19 = April 26, 2012"]
-[5.646523952484131, 3.702368974685669, "[TT] Number of Maneuvers of the SkySat-5 = 5"]
-[13.593491554260254, 5.831193447113037, "[TT] Power of the Solar panels = about 35 W/panel (BOL)"]
-[8.977617263793945, 4.447632789611816, "[TT] Sun Sensors of the ADCS = 4"]
-[3.8372366428375244, 1.1452618837356567, "[TT] Number of Successful Landings of the Falcon-9 = 20"]
-[11.93181324005127, 4.914255619049072, "[TT] Dimensions of the SSTL-X50 = 65 x 65 x 72 cm"]
-[8.133256912231445, -1.0629196166992188, "[FF] Mission Goal of the ICESat-2 = Provide high-accuracy altimetry for making long-sought repeat estimates of sea ice freeboard and hence sea ice thickness change"]
-[10.033221244812012, 7.191176891326904, "[TT] Spatial Coverage of the Instrument = 10 - 60 km"]
-[3.925630807876587, 4.3344950675964355, "[FF] Traffic Monitoring Capability of the RADARSAT-2 = Efficient detection of moving objects and accurate estimation of their parameters"]
-[3.83573317527771, 7.889369010925293, "[TT] Modulation of the RF communication subsystem = AFSK (Audio Frequency Shift Keying)"]
-[7.645095348358154, 1.495877981185913, "[FF] Launch Date of the Global Precipitation Measurement (GPM) Mission = Unknown"]
-[8.109556198120117, 0.7420149445533752, "[FF] Groundwater Pumping Percentage of the Tulare Basin = More than 80% in drought years"]
-[9.55171012878418, -1.3792189359664917, "[FF] Current Orbit of the Galileo FOC satellites = Elliptical, with an eccentricity of 0.23, a semi major axis of 26,200 km and inclined at 49.8\u00ba"]
-[7.11773681640625, 0.02048402838408947, "[FF] Age of the Beta Pictoris system = Few million years old"]
-[4.501150131225586, -0.9088945388793945, "[TT] Departure Date of the Dragon = January 2018"]
-[8.234748840332031, 2.490615129470825, "[FF] Capability of the TRUTHS = Determine Aerosol optical depth and water vapor"]
-[7.1777191162109375, 2.7877049446105957, "[TT] Launch Date of the MethaneSAT = No earlier than Oct. 1, 2022"]
-[5.418946266174316, 6.221076965332031, "[TT] SDRAM with ECC functionality of the Memory = 2 Gbyte"]
-[7.641135215759277, 2.349567413330078, "[FF] Purpose of the TOPEX = Advanced altimeter satellite for ocean circulation"]
-[10.518972396850586, 3.3434500694274902, "[TT] Power Requirement of the GEMS = Low-power operation in the CubeSat"]
-[4.873934268951416, 3.072922706604004, "[TT] Developer of the RUBI = Airbus"]
-[3.7148165702819824, 2.397352695465088, "[FF] Launch Date of the Iridium-4 NEXT Mission = December 2017"]
-[9.57682991027832, 0.8807005286216736, "[TT] Final Image Distance of the Rosetta = 24 meters"]
-[11.397669792175293, 8.929636001586914, "[FF] Image Acquisition Date of the MODIS = March 2002 and February 2022"]
-[7.092578887939453, 4.282057285308838, "[FF] Integration of the OCSE = Minotaur rocket"]
-[10.272747993469238, -1.3843092918395996, "[TT] Ecliptic Inclination of the TESS = About 40\u00ba"]
-[7.652822494506836, 1.217313528060913, "[FF] Date of the Phytoplankton Productivity Down in Gulf of Maine = 8 June 2022"]
-[10.344354629516602, 5.670475959777832, "[FF] Temperature Variations of the Orbit = <0.1\u00baC /hr for 90% of the orbit, and <2\u00baC/hr throughout the entire orbit"]
-[9.803149223327637, -0.35207265615463257, "[TT] Altitude of the LEO Platform = Up to 1000 km"]
-[4.860949993133545, 8.062938690185547, "[FF] Frequencies of the DORIS = 2.03625 GHz, 401.25 MHz"]
-[10.449458122253418, 6.357523441314697, "[TT] Measurement Depth of the SMAP = 5 cm"]
-[9.252036094665527, 5.227433204650879, "[TT] Pointing Stability of the MTG-S Spacecraft = Over 10 s"]
-[4.753261089324951, 0.8099097013473511, "[TT] Completion Date of the Canberra DSN station = January 2021"]
-[9.580426216125488, 5.098874092102051, "[TT] Mean Motion of the AC4-B = Higher"]
-[6.360778331756592, 4.110771656036377, "[FF] Secondary Payloads of the SONATE satellite = Star sensor, reaction wheel, amateur radio payload"]
-[14.290985107421875, 3.1838085651397705, "[TT] Mass of the DECA = 0.6 kg"]
-[9.331876754760742, -0.5095641613006592, "[TT] Perigee of the Geotail = About 10 Re"]
-[3.441089391708374, 6.429227828979492, "[TT] Antenna Diameter of the Galileo = 13 m"]
-[10.119514465332031, -1.5880167484283447, "[TT] Inclination of the WV-1 = 97.2\u00b0"]
-[13.612582206726074, 1.7521133422851562, "[TT] Cargo Weight of the SpaceX Dragon CRS-14 = More than 2630 kg"]
-[10.123048782348633, 6.026837348937988, "[TT] Temperature Resolution at 2.5% albedo of the VNIR = \u2265 6.5"]
-[14.20014762878418, 3.1934168338775635, "[TT] Mass of the ASPOC = 1.9 kg"]
-[8.661861419677734, 0.9095890522003174, "[TT] Launch Date of the Parker Solar Probe = 2018"]
-[10.9706449508667, 2.0733437538146973, "[FF] Expected Lifespan of the Automation System = Another decade of safe operations with XMM-Newton"]
-[5.519253730773926, 1.5775797367095947, "[FF] Qualification Status of the LED = Expected to take place well into the 2017"]
-[6.829995155334473, 5.959911823272705, "[TT] Quantity of the SCC = 1"]
-[12.235843658447266, 3.1126046180725098, "[TT] Sizing Duration of the Propellant = 12 years"]
-[7.47032356262207, -0.11551252752542496, "[TT] Arrival Date of High-energy Neutrino of the IceCube Neutrino Observatory = 22 September 2017"]
-[8.78718090057373, 5.43095588684082, "[FF] Pointing System of the Harris TANSO-FTS-2 = IP (Intelligent Pointing) system"]
-[10.317564010620117, 5.404868125915527, "[TT] Function of the Plumbing Instruments = Cut into the cooling lines"]
-[9.869392395019531, 7.542381286621094, "[FF] Sensor Complement of the AstroSat = Five co-aligned telescopes"]
-[8.254681587219238, 4.348557472229004, "[FF] Design of the Microdosimeter Suite = Custom designed for the mission"]
-[9.311954498291016, 8.047907829284668, "[FF] Publication Year of the Introduction to Fourier Optics = 2017"]
-[7.950917720794678, 8.355286598205566, "[FF] Correlation of the Spectral Angle = With the white panel when the yellow coupon is used as a reference"]
-[9.15286922454834, 5.420547008514404, "[TT] Slew Time, 180\u00ba pitch of the ADCS = \u2264 14 minutes"]
-[13.600825309753418, 5.8380303382873535, "[TT] Sun-pointing mode OAP of the Solar Panels = 5.8 W"]
-[12.071120262145996, 3.4519288539886475, "[TT] Burst Pressure of the PPCU ion thruster = 2.0(tank), 2.5(valve), 4.0(tube etc.) x MEOP"]
-[13.669727325439453, 2.8640050888061523, "[TT] Gravitational Stability of the Spacecraft = < 5 x 10-11 g"]
-[5.799060821533203, 6.765871524810791, "[TT] Number of Links per Day of the Automator = Up to 400"]
-[7.969690799713135, 8.548544883728027, "[TT] Spectral Range of the HIRDLS = 6 - 18 \u03bcm"]
-[3.838317394256592, 1.9727058410644531, "[TT] Launch Vehicle of the Polar Vigilance Mission = SpaceX Falcon 9"]
-[6.531280994415283, 3.4675731658935547, "[FF] Publication Journal of the Telerobotics = Science Robotics"]
-[11.055876731872559, 6.040204048156738, "[TT] Material of the Optical Cavity = Zerodur or ULE"]
-[10.118746757507324, 8.179885864257812, "[TT] Aperture of the Medium resolution = 1:4"]
-[10.926815032958984, 6.303584575653076, "[TT] Material of the Heat Rejection Mirror = Vacuum deposited silver"]
-[6.850924968719482, 1.766713261604309, "[FF] URL of the MEOSAR = http://searchandrescue.gsfc.nasa.gov/dass/groundsystem.html"]
-[3.8085312843322754, 7.941776752471924, "[TT] Modulation of the VBR = OQPSK"]
-[5.4300103187561035, 3.887967586517334, "[TT] Number of Satellites of the JL-1-GF03D = 3"]
-[9.246846199035645, 6.372791290283203, "[TT] Movement of the InSight's robotic arm = Helped \"the mole\" dig nearly 2 cm over the past week"]
-[5.734255313873291, 7.16004753112793, "[TT] Data Rate of the GeoCarb = 10 Mbit/s"]
-[9.522432327270508, 6.827017307281494, "[FF] Resolution of the Wide Fine Quad-Pol and Wide Standard Quad-Pol modes = Good"]
-[11.518994331359863, 6.586243152618408, "[TT] Measurement Range of the Particle Detector = Helium-3 : 21 MeV/n ~ 84 MeV/n"]
-[9.132731437683105, 4.921079635620117, "[TT] Magnitude of the Trajectory Correction Maneuver = 22 cm/s"]
-[8.8888521194458, 7.618192195892334, "[TT] Pixel Size of the Acquisition and Tracking Camera (ATC) = 20 \u00b5m x 20 \u00b5m"]
-[9.579671859741211, 6.769808292388916, "[TT] Resolution of the Gravity Models = 360 km"]
-[7.181859970092773, 1.2470368146896362, "[TT] Maximum Potential Value of the Mars Ascent Propulsion System (MAPS) = $84.5 million"]
-[9.622698783874512, -0.24283897876739502, "[TT] Altitude of the Yubileyniy-2/MiR = ~ 1400 km"]
-[3.179476261138916, 5.002596378326416, "[TT] Off-Nadir Distance of the RISAT-SAR = 107 km"]
-[7.070686340332031, 4.221460819244385, "[FF] Value of Information (VOI) of the COS = Computed by IGW-SCC"]
-[6.919310092926025, 3.4008889198303223, "[FF] Purpose of the Microage = Examine synthetic muscle cells in orbit"]
-[7.030081272125244, 7.527616024017334, "[TT] Bit Depth of the fADC = 14 bits"]
-[9.859551429748535, 8.196670532226562, "[TT] FOV (Field of View) of the Telescope = 41.3 x 41.3 arcmin"]
-[12.787214279174805, 7.230821132659912, "[TT] Main Beam Efficiency (%) of the Antenna = 89"]
-[10.9127197265625, 10.104891777038574, "[FF] Repair Completion Date of the Alpha Magnetic Spectrometer = 25 January 2020"]
-[4.497514247894287, 2.888077735900879, "[TT] Location of the GLPG = La Plata Argentina"]
-[5.156685829162598, 3.38158917427063, "[TT] Manufacturer of the WorldView-1 = DigitalGlobe Inc."]
-[9.2356595993042, 3.161834955215454, "[FF] Components of the SWEA = SWEA (Solar Wind Electron Analyzer) and STE (Suprathermal Electron Telescope)"]
-[6.110930919647217, 1.8739460706710815, "[FF] Development Status of the SwRI Small Satellite = Unknown"]
-[6.975454807281494, 6.93521785736084, "[TT] Quantity of the TEA-CO2 lasers = 2"]
-[10.071098327636719, 7.983537673950195, "[TT] Telescope of the GLM instrument = Fast f/1.2"]
-[6.485387802124023, 2.0369789600372314, "[FF] Map Accuracy of the eROSITA = Most accurate"]
-[9.670328140258789, 0.3069867789745331, "[FF] Relative Drift Velocity of the PROBA-3 = 50-60 cm/s"]
-[7.075600624084473, 3.266280174255371, "[FF] Function of the Vricon = Create photo-realistic, 3D accurate data models overnight"]
-[11.893176078796387, 4.103708267211914, "[TT] Volume of the GHGSat-D = 20 x 30 x 42 cm"]
-[11.755542755126953, 4.7620038986206055, "[TT] Shape of the Vacuum Tank = Toroidal"]
-[7.038377285003662, 8.363442420959473, "[TT] Nominal SNR of the Band 4 = 1070"]
-[4.344934463500977, 3.0977704524993896, "[TT] Ground Stations of the Herschel = New Norcia (Australia) and Cebreros (Spain)"]
-[10.596872329711914, 5.494180679321289, "[TT] Probe Type of the Electron Temperature Part = Three simple circular planar probes with guarding rings"]
-[10.689743995666504, 1.5877273082733154, "[FF] Class of the Neutron Star = Ultraluminous neutron stars"]
-[9.637176513671875, 8.337526321411133, "[TT] FOV (Field of View) of the Imager = > 1.28\u00ba"]
-[12.54057502746582, 7.534229278564453, "[TT] Instrument Power of the Imager = 290 W"]
-[8.678149223327637, 5.724903106689453, "[TT] Pointing Error Requirement of the Antenna = \u00b10.2\u00b0 peak"]
-[9.991562843322754, 2.009051561355591, "[FF] URL of the Chandra X-Ray Observatory = https://arxiv.org/ftp/arxiv/papers/1110/1110.4020.pdf"]
-[6.163238048553467, 2.198371171951294, "[TT] Data Center Members of the Euclid = 1000+ members of the Euclid Consortium"]
-[7.014540195465088, -0.3443882465362549, "[TT] UHF Carrier Detection Time of the MarCO-B = 11:41 am"]
-[14.648067474365234, 6.672943592071533, "[TT] Capacity of the NiCd batteries = 6 Ah"]
-[6.330442905426025, -0.418378084897995, "[TT] EVA Duration of the AMS-02 = 6 hr 19 min"]
-[6.359315872192383, -1.2655029296875, "[TT] Leading Satellite Date of the GRACE-2 = January 2006"]
-[5.1683526039123535, 3.964911937713623, "[TT] Ground Stations of the DICE Mission = NASA Wallops field, Stanford Research International"]
-[5.930309772491455, 1.725508213043213, "[FF] Presentation Date of the VIIRS = April 28, 2015"]
-[5.500189781188965, 3.3393208980560303, "[FF] Mission Purpose of the Heinrich Hertz satellite = Test the behavior of new technologies under extreme conditions in space"]
-[5.69695520401001, 2.7959511280059814, "[TT] AI Technology of the CIMON = Watson from IBM Cloud"]
-[10.398351669311523, 2.1248230934143066, "[FF] Data Source of the NuSTAR = High-energy X-ray data"]
-[9.579367637634277, 9.216229438781738, "[FF] Integration Date of the IRIS = Jan. 18, 2013"]
-[7.102128028869629, 2.39707088470459, "[FF] Purpose of the SIMBA smallsat = Monitoring of wildlife behavior"]
-[8.662064552307129, 3.522278308868408, "[FF] Instrument Suite of the EUI = Two HRI (High Resolution Imagers), one at Lyman \u03b1 and one dual-band in the extreme UV, and one dual-band FSI (Full Sun Imager) working alternatively at the two 174 \u00c4 and 304 \u00c4 EUV passbands"]
-[11.822126388549805, 3.382388114929199, "[TT] Thrust of the PROP unit = 130 mN"]
-[4.9943108558654785, 1.6852471828460693, "[TT] Operating Status of the MIRAS = Nominal"]
-[3.4962236881256104, 5.014694690704346, "[TT] Imaging Frequency Band of the SARLupe = X"]
-[8.707758903503418, 2.1616573333740234, "[TT] Antenna Diameter of the SeaWinds = 1 m"]
-[4.416143417358398, 7.047633647918701, "[FF] Product of the Kymeta = u8 broadband terminal"]
-[7.813413143157959, 1.6384148597717285, "[TT] Peatland Area of the Indonesia = Over 14 million hectares (140,000 km2)"]
-[10.070775032043457, -1.5186506509780884, "[TT] Orbit Inclination of the HY-2C = 66\u00ba"]
-[5.824295520782471, -0.796601414680481, "[TT] Design Life of the Spacecraft = 3 years (goal of 5 years of operations)"]
-[9.6045560836792, 7.145440101623535, "[TT] Spatial resolution at nadir of the MWTS = 50/75 km"]
-[11.357128143310547, 5.864677906036377, "[TT] Material of the LAGEOS = Aluminium sphere with a brass core"]
-[10.205070495605469, 3.653928756713867, "[TT] Stabilization of the 3U CubeSat = 2-axis (optionally 3-axis)"]
-[9.687466621398926, -0.07285590469837189, "[TT] Maximum Depth of Discharge of the TSUBAME = Estimated at no more than 50%"]
-[5.084475517272949, 3.263948678970337, "[TT] Manufacturer of the ZY-3 = CAST/BISSE (China's Academy of Space Technology/Beijing Institute of Spacecraft System Engineering)"]
-[9.626703262329102, 6.992062091827393, "[TT] Spatial Resolution at Nadir of the SSM/T-1 = 174 km diameter"]
-[8.190053939819336, 4.55759859085083, "[TT] Total Ionizing Dose Tolerance of the ECS = 100 kRad"]
-[10.092599868774414, 8.221612930297852, "[FF] Operation of the FDA = Several shot closing/opening of the entrance aperture"]
-[8.453873634338379, 7.3975629806518555, "[TT] Resolution of the CMOSIS CHR70M Image Sensor = 10000 by 7096 pixels"]
-[5.909835338592529, 0.2904665172100067, "[FF] Launch Date of the JUICE = Unspecified"]
-[4.9787373542785645, 0.9853627681732178, "[TT] Phase C/D Start Date of the SMOS = Mid-2004"]
-[7.288792133331299, 3.19378924369812, "[FF] Purpose of the Joint Polar Satellite System (JPSS) = Collection of global multi-spectral radiometry and other specialized meteorological and oceanographic data"]
-[8.834859848022461, 4.370214462280273, "[FF] Recovery Method of the Kepler Space Telescope = Maneuvering the spacecraft so that the solar pressure is evenly distributed across the surfaces of the spacecraft"]
-[3.49019193649292, 6.438363075256348, "[TT] Surface Error of the Antenna = Less than 2.4 mm rms"]
-[10.539145469665527, 4.370561122894287, "[FF] Redundancy of the FDA = One-shot wax actuator"]
-[9.582351684570312, -1.4560343027114868, "[TT] Eccentricity of the SMART-1 = 0.359146"]
-[5.636099815368652, 6.333784103393555, "[TT] Data Transfer of the ASAP-Light = Ground station communication passes"]
-[12.059428215026855, 4.278606414794922, "[TT] Quantity of the Spacecraft = 64"]
-[3.0889084339141846, 2.2568140029907227, "[FF] Sea Level Rise of the Copernicus Sentinel-6 = 4.8 mm per year"]
-[7.052921772003174, 5.961487293243408, "[TT] Range of the NGAVGS = Up to 3000 meters"]
-[4.973493576049805, 0.6317463517189026, "[TT] Launch Date of the ESAIL = 3 September 2020"]
-[7.271146774291992, 7.84752082824707, "[TT] Integral non-linearity of the PHA = <0.05% of full scale"]
-[13.375882148742676, 2.9255611896514893, "[TT] Propellant for Station Keeping of the Geo Satellite = 1 ton"]
-[5.551244258880615, 7.096954822540283, "[TT] Data Rate of the TT&C = 9600 baud"]
-[10.968840599060059, 7.482173919677734, "[TT] Swath Width of the Sentinel-2C = 290 km"]
-[8.994917869567871, 5.324047565460205, "[FF] Pointing System of the ASTERIA = Coarse pointing control, two-stage fine pointing control"]
-[14.247180938720703, 3.2181448936462402, "[TT] Mass of the AMS-02 = ~7,000 kg"]
-[12.050073623657227, -0.18855322897434235, "[TT] Sky Division of the TESS = 13 sectors"]
-[11.850892066955566, 2.9157872200012207, "[TT] \u0394V of the Deimos-1 = ~ 20 m/s"]
-[7.132527828216553, 5.294399261474609, "[FF] Components of the REPT = Stack of high-performance silicon solid-state detectors, collimation aperture, thick case, charge-sensitive amplifiers, pulse-shaping circuits, field-programmable gate array, low- and high-voltage power boards"]
-[8.829792022705078, 7.5687947273254395, "[TT] Pixel Size of the Imager = 6.5 \u00b5m square"]
-[10.758683204650879, 3.8784661293029785, "[TT] Deployment Timing of the CanX-7 Drag Sail = End of a six-month phase of secondary payload operation"]
-[13.217247009277344, 5.440995216369629, "[FF] Structure of the DSAT-3 = Panels deploy in the same cross shape"]
-[9.52242374420166, 8.185402870178223, "[TT] Field-of-View of the PanCam HRC = 5\u00b0 x 5\u00b0"]
-[13.320329666137695, 6.129034519195557, "[FF] Eclipse Depth-of-Discharge of the Power Subsystem = Only slightly higher than the LOI (Lunar Orbit Insertion) depth-of-discharge"]
-[5.26499605178833, 8.442143440246582, "[TT] Servo Bandwidths of the Guider = 0 to a few Hz (platform), <50 Hz (prime mirror fine guiding)"]
-[5.383205890655518, 0.661176860332489, "[TT] Mini-commissioning Phase of the Envisat = November and December 2010"]
-[4.938571929931641, 5.837026596069336, "[FF] Prime Objective of the ZACube-2 = Demonstrate AIS (Automatic Identification System) message reception"]
-[6.73921012878418, 0.5973533391952515, "[TT] Discovery Date of the Kepler-1649c = April 15, 2020"]
-[7.971668720245361, 4.941354751586914, "[FF] Calibration Method of the TRUTHS = Pre-flight calibration/characterization and during the commissioning phase"]
-[4.356827259063721, 1.28200101852417, "[FF] Development Date of the GMV = 24 June 2021"]
-[9.580988883972168, 8.240023612976074, "[TT] Field of View of the Camera 2 = 36.8\u00ba"]
-[6.690231800079346, 4.87854528427124, "[FF] Function of the PMS = Product Management"]
-[5.6125407218933105, 1.8732035160064697, "[TT] Landing Location of the Orion = Pacific Ocean off the west coast of the United States"]
-[8.847384452819824, 4.674612045288086, "[FF] Attitude Measurements of the Star Sensor = Roll, pitch, and yaw"]
-[5.239715576171875, 2.2987890243530273, "[TT] Chief Strategy Officer of the HawkEye 360 = Kari Bingen"]
-[13.1998872756958, 7.256702899932861, "[TT] Power Consumption of the WPM = 80 W"]
-[4.03150749206543, 3.410071849822998, "[TT] Industrial Consortium of the GOME = Officine Galileo, Laben, British Aerospace, TPD"]
-[10.105912208557129, 4.07810115814209, "[TT] Booms of the Spacecraft = Two 5 m booms in the spin plane for the magnetometers"]
-[7.260135650634766, 2.5494728088378906, "[TT] Imagery of the Kondor = SAR imagery and eventually also optical imagery"]
-[13.39844036102295, 6.853747844696045, "[TT] Electric Power of the SES-14 = 16 kW"]
-[2.9808318614959717, 0.06716165691614151, "[FF] Wave-Like Patterns Location of the Warm-Core Ring = J2 to J5"]
-[5.999819278717041, 0.9652292728424072, "[TT] Image Acquisition Date of the RASAT = April 13, 2016"]
-[10.702428817749023, -0.16906724870204926, "[TT] Horizontal Distance of the TerraSAR-X and TanDEM-X = 600 m to 1200 m"]
-[3.728774070739746, 4.542819976806641, "[FF] Recent Efforts of the ICEYE = Tracking and analyzing flood events globally, launching new SAR satellites"]
-[7.749115467071533, 9.127985954284668, "[TT] Wavelength Range of the Band 1 = 365-408 nm"]
-[7.019352436065674, 7.16686487197876, "[TT] Output Pulse Energy of the InnoSlab laser = About 30 mJ"]
-[9.999905586242676, 2.8085649013519287, "[TT] Deployment Time of the NRCSD (NanoRacks CubeSat Deployer) = May 16, 2016"]
-[13.301115036010742, 5.445462703704834, "[TT] Articulation of the Solar Arrays = 2-axis"]
-[13.249125480651855, 5.4793548583984375, "[FF] Solar Array Deployment of the SLATS = Confirmed"]
-[3.4219846725463867, 5.604488372802734, "[TT] Type of the Synthetic Aperture Radar Antenna = Large deployable"]
-[5.187501907348633, 0.7611489295959473, "[FF] Mishap Investigation Board Creation Date of the Glory = March 7, 2011"]
-[7.35630989074707, 4.020736217498779, "[FF] Instrument of the Satellites = Unknown"]
-[9.694720268249512, 4.077908992767334, "[FF] Testing of the Magnetorquers = Prototypes of the design have been successfully tested with excellent performance"]
-[4.316793441772461, -0.1290341317653656, "[FF] Launch Date of the P35-3 = 19.2.19963"]
-[5.256195545196533, 1.0353367328643799, "[TT] Status of the NIRST = Still in the commissioning phase"]
-[6.975679397583008, 2.8698313236236572, "[FF] Mission Objective of the DIDO-3 = Gather data by researching the effects of a microgravity environment on biological materials"]
-[11.932490348815918, 3.4391722679138184, "[TT] Propellant Status of the CanX-4 = Close to a full tank"]
-[6.676455497741699, 3.543931007385254, "[FF] Data Latency of the MetOp Satellite = 130 minutes"]
-[4.120666980743408, 5.7288665771484375, "[FF] Mandatory Installation Date of the ADS-B Receiver = 2015 for high-performance aircraft, 2020 for all aircraft"]
-[5.919397830963135, 3.1912930011749268, "[TT] Number of Commands of the Admiral Paul F. Zukunft = 8"]
-[8.981366157531738, 5.08334493637085, "[FF] Components of the SIA = Four quartz gyroscopes aligned in a fused-quartz block"]
-[5.280578136444092, 0.7103095054626465, "[TT] Arrival Date at RRSW of the MSV bus and payloads = May 2013"]
-[5.110988140106201, 3.2227494716644287, "[TT] Manufacturer of the NTS (Nanosatellite Tracking of Ships) = COM DEV / UTIAS/SFL, Toronto, Canada"]
-[4.888027667999268, 1.5351066589355469, "[TT] Radiometric Calibration of the G\u00f6kt\u00fcrk-2 = CEOS network Tuz G\u00f6l\u00fc (Salt Lake) in Turkey"]
-[11.837226867675781, 6.694606781005859, "[FF] Omni-directional Proton Energy Ranges of the MEPED = > 16 MeV, > 35 MeV, > 70 MeV and > 140 MeV"]
-[7.574998378753662, -2.480368137359619, "[TT] End of Life Date of the GOLD = 2033"]
-[8.104403495788574, 0.7746555209159851, "[FF] Land Area in Drought of the Drought Monitor = More than 93 percent of the land area in Utah, Colorado, Nevada, and New Mexico"]
-[5.3074188232421875, 7.216421604156494, "[TT] Image Telemetry Link of the SPOT-3 = 50 Mbit/s at 8 GHz"]
-[4.565962314605713, 7.841982841491699, "[TT] Range of the UHF-band = 402.0-402.2 MHz"]
-[6.217514514923096, 4.46571683883667, "[FF] Telemetry Downlink of the WSF-M = EGS Operations Center"]
-[4.549824237823486, 5.734783172607422, "[TT] Location Accuracy of the Distress Beacons = Within 2 km"]
-[5.22841215133667, -0.027377324178814888, "[TT] Launch Date of the TSUBAME = 27 October, 2017"]
-[7.258065700531006, 4.455738544464111, "[FF] Purpose of the FLexRX = In-orbit test, demonstration, and qualification of a product"]
-[8.733460426330566, 1.9534671306610107, "[TT] Wind Speeds of the Global Models = Higher than 20 m/s"]
-[13.093744277954102, 7.243838310241699, "[TT] Power Consumption of the CMS = 26 W"]
-[6.172798156738281, 5.857519626617432, "[TT] Quantity of the Payload Data Interface Controller = 1"]
-[11.32107162475586, 3.689828872680664, "[FF] Energy Forms of the Cygnus A jet = Kinetic energy, heat or radiation"]
-[8.909948348999023, 4.386002063751221, "[FF] Brightness Sensor Issue of the MarCO = Affecting ability to stay pointed at the Sun and recharge their batteries"]
-[8.154557228088379, 0.02604755572974682, "[TT] Mission Start Year of the TOPEX/Poseidon = 1987"]
-[10.121121406555176, 5.534844398498535, "[FF] Constraint of the Instrument = Keep the instrument radiators away from Nadir direction for thermal stability purposes"]
-[5.558758735656738, 2.2374207973480225, "[FF] Affiliation of the Andreas Jung = Unknown"]
-[5.51736307144165, 2.053327798843384, "[FF] Mission Status of the OCSE = Completed"]
-[4.814347743988037, 7.294031620025635, "[TT] Downlink Data Rate of the RF Communication System = 1.2 kbit/s"]
-[5.2083353996276855, 0.6433896422386169, "[FF] Publication Date of the JB2008 = 18-21 August 2008"]
-[9.956830978393555, 0.8632251024246216, "[TT] Adapter and Separation System Type of the ALMASat-1 = 2-clamp separation method"]
-[5.988641262054443, 1.5975021123886108, "[TT] Deployment Date of the EURECA = Aug. 2, 1992"]
-[5.993021488189697, 4.729381561279297, "[FF] Function of the Enabling Inter-Satellite Link platform = Enable inter-satellite communication"]
-[9.576461791992188, 7.149353981018066, "[TT] Ground Spatial Resolution of the POLDER-P = 6 km x 7 km at nadir"]
-[6.113645076751709, 0.9935515522956848, "[FF] First Light Image Date of the SeaHawk-1 = 22 March 2019"]
-[11.351399421691895, 2.781163215637207, "[TT] Construction and Thermo-Regulation System Mass of the Microsatellite = 5.3 kg"]
-[6.0595293045043945, 5.681718349456787, "[FF] Technology of the FPGAs = Six Sigma SolderQuik\u00ae"]
-[7.691039562225342, 0.4794740676879883, "[FF] GNC System of the Lunar IceCube = Highly-capable micronized GNC (Guidance, Navigation and Control) system"]
-[4.972299098968506, 1.1077301502227783, "[TT] Release Date of the BEESAT-4 = Sept. 9, 2016"]
-[11.644416809082031, 6.719620227813721, "[TT] Energy Resolution of the Detectors = About 10% above 10 keV"]
-[7.854629039764404, 3.3614766597747803, "[FF] Function of the Low-Frequency Radio Spectrometers = Detect the 21 cm hydrogen line radiation"]
-[6.141009330749512, 6.4307684898376465, "[TT] Data Transmission Time of the COSIMA = About 40 minutes"]
-[4.407362461090088, 0.942693293094635, "[FF] Launch Date of the IRNSS-1D = March 28, 2015"]
-[5.778701305389404, -0.7172528505325317, "[TT] Original Lifetime of the Geotail = 4 years"]
-[8.53968334197998, 0.18659494817256927, "[FF] Components of the Comet = Nucleus, coma, hydrogen envelope, dust and plasma tails"]
-[4.3633527755737305, 3.9391982555389404, "[FF] Objective of the GATE = Monitor Galileo signals from the GIOVE, IOV, and Galileo spacecraft series"]
-[4.978658676147461, 0.45865771174430847, "[TT] Launch Date of the SWFO-L1 = 31 October 2024"]
-[6.801424980163574, 5.8910064697265625, "[TT] Quantity of the Mandrels = 27"]
-[5.805703163146973, -0.862809419631958, "[TT] Design Life of the QuikTOMS spacecraft = Three years"]
-[9.792454719543457, 8.084368705749512, "[TT] Focal length of the 50 mm camera = 50 mm"]
-[6.741524696350098, 1.2708772420883179, "[FF] Solar Corona Observation Date of the PROBA-2 = March 16, 2015"]
-[7.6800336837768555, 8.601799011230469, "[TT] Spectral Bands of the OLCI = 21"]
-[9.44149112701416, 5.322926998138428, "[TT] Sun Angle Constraint of the CHEOPS = Larger than 120\u00ba"]
-[10.90869140625, 7.565409183502197, "[TT] Swath Width of the VIRR = 2280 km"]
-[13.740608215332031, 2.8515162467956543, "[TT] Spacecraft Mass of the GeoEye-1 = ~2000 kg"]
-[10.068878173828125, -1.5559496879577637, "[TT] Inclination of the SSMIS = 98.8\u00ba"]
-[7.516820430755615, 3.762275218963623, "[TT] Maximum Integration Time of the NightPod = 10 seconds"]
-[11.992805480957031, 3.858715772628784, "[TT] Back Pressure of the Test Setup = 1 x 10-3 Pa"]
-[6.538963794708252, 4.313081741333008, "[FF] High Performance Computing and Application Flexibility of the Spacecraft Payload = Unknown"]
-[10.345691680908203, 5.432811260223389, "[TT] Thermal Control of the S/C = Passive"]
-[9.280054092407227, 2.860487222671509, "[FF] Justification of the ACE = Better understand the consequences of the declining phase of the solar cycle and a very low solar minimum"]
-[6.893594741821289, 3.7178468704223633, "[FF] Advantages of the Short Baseline DOR Interferometry = Time synchronization problem between the stations is effectively solved by using the same source of time and frequency; The transmission media errors included troposphere, ionosphere and solar plasma are approximately the same between the two tracking stations"]
-[7.955645561218262, 7.663069248199463, "[FF] Type of the SUCHI (Space Ultra-compact Hyperspectral Imager) = Much smaller"]
-[6.692936420440674, -0.445550799369812, "[TT] Period of the ADEOS-II = 101 minutes"]
-[3.9313817024230957, 1.9330545663833618, "[TT] Launch Vehicle of the Global-9 = Rocket Lab\u2019s Electron"]
-[8.281461715698242, 2.1359546184539795, "[FF] Data Output of the WTS = Raw data to obtain the neutral wind vector, the neutral temperature and the O and N2 densities"]
-[6.340585231781006, 6.2971320152282715, "[TT] Number of Loops about the L1 point of the S/C = 4"]
-[5.499969005584717, 7.692005157470703, "[TT] EIRP of the Contiguous Sectors = 60-65 dBW"]
-[9.388030052185059, 5.020176887512207, "[TT] Attitude Measurement Periodicity of the ISS = ~\u00b10.5\u00ba in each axis over one orbit"]
-[3.489528179168701, 4.5772881507873535, "[TT] Backup Location of the PAZ SAR Processor = Maspalomas (Canary Islands)"]
-[13.69914722442627, 3.2483699321746826, "[TT] Mass of the AeroCube-4.5 = 1.3 kg"]
-[14.066509246826172, 4.05094051361084, "[TT] Instrument Mass of the RA-1 = 96 kg"]
-[5.723691463470459, 5.172293663024902, "[FF] Antennas of the ROSA = One navigation antenna, Two radio occultation antennas"]
-[9.005833625793457, -0.5280596017837524, "[TT] Orbit Perigee of the P35 series = 578 km"]
-[8.094575881958008, 6.314955711364746, "[FF] Payload of the CBERS = Multisensor with imaging sensors of different spatial resolutions and collection frequencies"]
-[9.437824249267578, 5.449487209320068, "[TT] Slew Rate of the Spacecraft = 0.25 to 1.0\u00ba/s"]
-[3.6080095767974854, 2.704800605773926, "[TT] Certainty Improvement of the Iridium constellation of satellites = Four orders of magnitude"]
-[6.40514612197876, 6.4806318283081055, "[TT] Data Collection Interval of the CANDOS = 10 seconds"]
-[4.818426132202148, 3.7017831802368164, "[TT] Structure of the Sojourner 2020 = Three-layer telescoping structure"]
-[3.4939069747924805, 6.419192314147949, "[TT] Antenna Diameter of the Satellite = 1.2 m, 1.84\u00ba (Ku-band), 6.2\u00ba (S-band)"]
-[8.70118236541748, 6.28743839263916, "[TT] Sensitivity (6 - 10 keV) of the Instrument = 2 x 10 -15  erg/cm 2 /s"]
-[7.0468339920043945, 4.544188499450684, "[TT] Mounting Method of the Avionics and Payloads = Directly onto three equipment radiator panels"]
-[8.301019668579102, 7.238045692443848, "[TT] Camera Module Interface of the Frame Grabber = Correct interface to the camera module"]
-[6.109996795654297, 5.551149368286133, "[TT] Components of the PDHS = FPGAs (Field-Programmable Gate Arrays)"]
-[9.999798774719238, -1.450347661972046, "[TT] Orbital Plane Tilt of the Orbital Phase 1 = 60\u00ba away from the Sun direction"]
-[7.903806686401367, 4.769308567047119, "[FF] Purpose of the Advanced Microwave Scanning Radiometer (AMSR) = Earth observation"]
-[8.282395362854004, 7.544290542602539, "[TT] CCD Detector Type of the MEGS = Back-thinned, back-illuminated"]
-[11.78618335723877, 6.720125198364258, "[TT] Electron energy of the Microdosimeter A = > 50 keV"]
-[5.759730339050293, 2.6905605792999268, "[FF] Manufacturer of the NuSTAR = NASA"]
-[7.7521233558654785, -0.8879359364509583, "[FF] Science Team Lead of the ICESat-2 = Lori Magruder"]
-[10.375809669494629, 3.2229433059692383, "[TT] Quantity of the CubeSats = Two"]
-[5.512010097503662, 7.896092891693115, "[FF] Design Features of the Channelizers/filters = 4 channel input multiplexer @ 4 GHz, 4 channel filter @ 4GHz, 5 channel input multiplexer @ 8 GHz"]
-[10.79439926147461, 6.316159725189209, "[FF] Construction of the Focal Plane Structure = Complex 3d structures built rapidly from sheet metal primitives"]
-[8.372506141662598, -0.8149600028991699, "[TT] Surface elevation change rates accuracy of the ATLAS = 0.4 m/yr"]
-[5.672544002532959, 5.159300804138184, "[TT] Operating System of the OBC = FreeRTOS"]
-[4.682267665863037, 6.597839832305908, "[FF] Data Transfer of the S-band link = NASA Ground Network"]
-[8.265119552612305, 3.0982275009155273, "[FF] Purpose of the ASIM = Measures electric events in Earth\u2019s upper atmosphere with cameras, photometers and X- and gamma-ray detectors"]
-[9.04358196258545, 5.803884506225586, "[TT] Linearity of the Position Sensing and Actuation = Along the instrument sensitive axis"]
-[13.624763488769531, 6.98745584487915, "[TT] Power Output of the EPS = 550 W"]
-[4.317783832550049, 2.3075923919677734, "[TT] Launch Site of the DubaiSat-2 = Dombarovsky launch site in Russia"]
-[3.386414051055908, 6.441704273223877, "[TT] Antenna Diameter of the LET = 5 m"]
-[5.031360626220703, 0.6263728737831116, "[TT] Start Date of the EMOC = 2004"]
-[8.953927993774414, 5.387426376342773, "[TT] Attitude Manoeuvring of the GomX-3 = Up to 7 target changes per orbit"]
-[5.678874969482422, 5.847771644592285, "[FF] Technology of the EEPROM = Unknown"]
-[7.479581832885742, 2.352999687194824, "[TT] Coverage of the GOES-R = Full hemispheric"]
-[5.371757507324219, 3.9272878170013428, "[TT] Number of Satellite Overpasses of the Inuvik Satellite Station Facility = More than 30,000 in 11 years"]
-[5.29215145111084, 0.8720914125442505, "[TT] Commissioning Phase of the Monitor-E = November 2005"]
-[4.030430793762207, 6.663717746734619, "[TT] PRF of the Antenna = 1464 to 1640 Hz"]
-[5.755100727081299, 0.9499683380126953, "[TT] Launch Date of the WorldView-1 = Oct. 18, 2001"]
-[4.981164932250977, 0.2361626774072647, "[TT] Launch Time of the BlackSky 7 = 22:30 UTC, March 22, 2021"]
-[8.66126537322998, 7.656978607177734, "[TT] Pixel Size of the 4-band CCD Imager = 10 x 10 \u00b5m"]
-[8.959383964538574, -0.20571568608283997, "[TT] Altitude of the Meteor-M2-2 = 816.4 km"]
-[13.234607696533203, 7.230142593383789, "[TT] Power of the Power consumption = < 800 W"]
-[7.812553882598877, 8.107884407043457, "[FF] Tuning of the Focal Plane Skew Settings of the R3 System = Possible cause of noise in the NIR band"]
-[7.048771858215332, -0.7802711725234985, "[TT] Orbital Period of the Kepler-442b = 112 days"]
-[8.78482723236084, 1.907654047012329, "[TT] Transmission Speed of the WINDS = 155 Mbit/s"]
-[8.57111644744873, 6.837579727172852, "[TT] Imaging Solution of the Stereo Camera = Single lens and two angles of view in the same track"]
-[9.712510108947754, -0.1307542771100998, "[TT] Altitude of the Tsubame = 180 km"]
-[5.2653398513793945, 4.495654582977295, "[FF] Close Approach Coordination of the Starlink = With multiple government and commercial satellite operators"]
-[11.156108856201172, 4.312138557434082, "[TT] TID Requirement of the PSB = 2.9 krad (Si)"]
-[13.341594696044922, 7.801084518432617, "[TT] Power of the S-band Transmitter = 0.5 W"]
-[8.51974105834961, 6.9923858642578125, "[FF] Purpose of the SCAR = Improve the long-term stability of TSI measurements"]
-[14.599733352661133, 6.618846416473389, "[TT] Power Storage of the CS-XUEPS2-41 = Rechargeable 30 W hr lithium polymer batteries"]
-[14.731225967407227, 6.637582302093506, "[TT] Capacity of the Battery System = Four 3.2 Ah lithium-ion battery cells"]
-[11.028066635131836, 3.706458806991577, "[FF] Objective of the PLEGPAY = Study of spacecraft/space environment interactions in LEO with reference to electrostatic charging/discharging phenomena"]
-[8.684252738952637, 1.2553082704544067, "[TT] Observation Field of the Kepler = Constellation Aquarius"]
-[10.217681884765625, 5.573726177215576, "[FF] Thermal Cycle Test Environment of the Flight Model = -20 to 50 degrees"]
-[6.728335857391357, 6.0593485832214355, "[TT] Number of Subapertures of the PAIS = 4"]
-[7.120635032653809, 1.2372583150863647, "[TT] Vision Date of the Spitzer = 1946"]
-[4.498493194580078, 6.1750993728637695, "[TT] Frequency of the S-band Beacon = 2250 MHz"]
-[14.513736724853516, 6.573355197906494, "[FF] Battery Design of the TacSat-4 = Rapid, in the field replacement without spacecraft disassembly"]
-[4.910551071166992, 1.7448071241378784, "[FF] Observation Applications of the G\u00f6kt\u00fcrk-2 = Emergency response, land monitoring, disaster management"]
-[13.86160945892334, 6.952284336090088, "[FF] Potential of the 300 V system = Negative"]
-[11.751582145690918, 3.2644941806793213, "[FF] Thrusters of the RCS = 1 N thruster and 20 N thruster"]
-[9.1918363571167, 3.865002155303955, "[FF] Mounting of the Solar Cell = Modified mirror mount"]
-[6.763432025909424, 1.8277995586395264, "[FF] URL of the Dellingr = https://www.nasa.gov/feature/goddard/2017/nasa"]
-[5.862799644470215, 3.3513717651367188, "[TT] Amortized unit cost of the SkySat = $5 million"]
-[5.747389316558838, 2.945408582687378, "[TT] Organization of the NROL-36 = National Reconnaissance Organization"]
-[7.59262752532959, 3.3496787548065186, "[FF] Purpose of the Global Imager (GLI) = Earth observation"]
-[5.046577453613281, 3.3833682537078857, "[TT] Manufacturer of the ENPULSION Micro R3 = ENPULSION of Wiener Neustadt, Austria"]
-[9.285362243652344, 6.846855163574219, "[TT] Spatial Resolution of the JL-1-GF03D = 0.75 m"]
-[6.465252876281738, 5.7714996337890625, "[TT] PRN of the GSAT-0209 = 9"]
-[10.761122703552246, 1.4267020225524902, "[TT] Smaller Black Hole Mass of the OJ 287 galaxy = About 150 million times the mass of our Sun"]
-[9.254538536071777, 5.1495256423950195, "[TT] Attitude Command of the MicroSCOPE = Inertial"]
-[9.919530868530273, 7.873116970062256, "[TT] Aperture Diameter of the Pushbroom imager = 200 mm"]
-[7.996647357940674, -0.9951231479644775, "[TT] Elevation Data Collection of the ICESat-2 = Ongoing"]
-[5.204167366027832, 8.421425819396973, "[TT] Bandwidth of the Channel 1 = 100 MHz"]
-[6.440113067626953, 5.7520318031311035, "[FF] Execution Time of the Payload routine configuration request = Unknown"]
-[14.189340591430664, 3.278409719467163, "[TT] Mass of the MWIR = 23 kg"]
-[6.5225419998168945, 5.363131999969482, "[FF] Type of the DCS = Data collection"]
-[11.753549575805664, 5.125341892242432, "[TT] Microchannel Plate Area of the FlaPS = 25 cm2"]
-[7.917708396911621, 3.0979137420654297, "[FF] Measurement Type of the TanSat = Carbon Dioxide"]
-[9.6072359085083, 8.289462089538574, "[FF] Field of View Map of the EPI-Lo = Unknown"]
-[10.625659942626953, 4.996458053588867, "[TT] Mass of the Langmuir Probe = 4.5 kg"]
-[4.816765785217285, 2.9683029651641846, "[FF] Partner Countries of the T/P = USA and France"]
-[8.553585052490234, 0.27509546279907227, "[FF] Depth of the Uzynaral Strait = Around 6 m"]
-[8.047674179077148, 5.8596296310424805, "[FF] Brighter Areas Indicator of the Image = Changes in amplitude"]
-[6.260436534881592, 1.8816667795181274, "[TT] URL of the TOI-178 = https://arxiv.org/pdf/2101.09260.pdf"]
-[3.0540292263031006, 1.841388463973999, "[TT] Image Capture Date of the Sentinel-2 = 20 January 2022"]
-[5.690372467041016, 6.86700963973999, "[TT] Data Consumption of the EAN = 150 MB"]
-[13.234416007995605, 5.41312313079834, "[FF] Unpressurized Trunk of the SpaceX Cargo Dragon = New pair of solar arrays"]
-[8.497690200805664, 1.4096745252609253, "[TT] Measurement of the Aquarius = Rain rates, surface wind speeds, water vapor and cloud liquid water, over the oceans"]
-[10.42148494720459, 2.3149986267089844, "[FF] Horizon Sensing of the X-ray Navigation = Only the upper atmosphere is traversed by a ray grazing the effective horizon"]
-[5.2242350578308105, 8.377721786499023, "[TT] Maximum Bandwidth of the T/R module = 100 MHz"]
-[9.091525077819824, 2.8699538707733154, "[FF] Author of the Can ripples on the sun help predict solar flares? = Robert Sanders"]
-[4.9452972412109375, 0.6201191544532776, "[FF] Launch Date of the Dauria Aerospace and Samsung = Oct. 15, 2013"]
-[8.655706405639648, 2.2239487171173096, "[TT] LOS Wind Error Requirement of the Mie Channel = 0.6 m/s"]
-[9.940401077270508, 9.015405654907227, "[TT] Effective FOV of the Channel 2 = 52 x 16 km"]
-[11.351597785949707, 4.968791484832764, "[TT] Total Path Length of the Gaia = 35 m"]
-[6.611977577209473, 6.865864276885986, "[TT] Laser Terminal Speed of the EDRS-A = 1.8 Gbit/s"]
-[4.481863975524902, 4.896616458892822, "[TT] Ship Detection Data Processing Time of the EDRS = 18 minutes"]
-[4.898483753204346, 3.8853931427001953, "[TT] Manufacturer of the CanX-2 = UTIAS/SFL"]
-[7.768287181854248, 5.853616237640381, "[TT] Instrument of the Odin = SMR (Sub-Millimeter Radiometer)"]
-[7.544748783111572, 0.8798936605453491, "[FF] Effect of the Moonlight = Lowering the ticket price to lunar exploration"]
-[5.160895824432373, 7.136938095092773, "[TT] Data Handling Capacity of the Radio Terminal = Up to 300 Mbit/s"]
-[4.8695292472839355, 7.193227767944336, "[TT] Data downlink of the ALOS/PRISM = 277.52 Mbit/s (Ka-band)"]
-[4.9449896812438965, -0.26870545744895935, "[TT] Launch Time of the GOES-T = 4:38 p.m. EST"]
-[11.358607292175293, 0.6875022649765015, "[TT] Orbital Period of the Planet Orbiting AU Microscopii = Just over a week"]
-[8.519553184509277, 6.021369934082031, "[TT] Absolute Radiometric Accuracy of the Hyperion = <6% (1\u03c3)"]
-[10.015661239624023, 2.8879995346069336, "[TT] Launch Date of the ALBus CubeSat = December 16, 2018"]
-[8.312019348144531, 3.1453497409820557, "[FF] Purpose of the Prime Instrument = Monitor the distribution of ozone"]
-[9.497899055480957, 7.07991886138916, "[TT] Spatial Resolution at 6.6 GHz of the SMMR = About 100 km"]
-[8.789773941040039, 0.9620888233184814, "[FF] URL of the Parker Solar Probe = https://iopscience.iop.org/article/10.3847/2041-8213/ac4015/pdf"]
-[4.434572696685791, 5.9692769050598145, "[TT] Communication Links of the GomX-4A and GomX-4B = UHF and S-band"]
-[4.936270236968994, 8.211784362792969, "[TT] Center Frequencies of the Bandpass Filters = 1.5, 4.5, 7.5, 10.5, 13.5, 16.5, 19.5, 22.5, 25.5, 28.5, 31.5 and 34.5 MHz"]
-[4.8601393699646, 0.4431542754173279, "[TT] Deployment Date of the CRISTA-SPAS-2 = Aug. 7"]
-[6.771631240844727, 1.0073015689849854, "[FF] Unfurling Date of the Solar Arrays = 20 June 2021"]
-[14.170462608337402, 3.2166171073913574, "[TT] Mass of the PCDU = < 21.6 kg"]
-[8.715174674987793, 4.996544361114502, "[TT] Star Magnitude Range of the Fast Cameras = 4 to 8"]
-[8.613486289978027, 1.1367114782333374, "[TT] Instrument Data Distribution Facility Location of the SAC-D/Aquarius = Buenos Aires, Argentina"]
-[6.921255111694336, 4.369132041931152, "[FF] Unknown of the TPF = Unknown"]
-[5.847951889038086, 2.156820058822632, "[FF] Website of the Roman = Interactive"]
-[9.968062400817871, 6.797220230102539, "[TT] Ground Spacing of the ATM = ~85 m"]
-[5.050971984863281, 7.306451320648193, "[TT] Data Rate of the RF Communications = 280 Mbit/s"]
-[7.171743869781494, 3.3986644744873047, "[FF] Number of Alerts Per Day of the SKA = Unknown"]
-[10.061419486999512, 1.9262654781341553, "[FF] Initial Imaging and Observations Date of the Chandrayaan-2 = October 22, 2019"]
-[13.445038795471191, 6.926222324371338, "[TT] Electrical Power of the ASNARO-2 = 1300 W (EOL)"]
-[10.29423713684082, 5.4396209716796875, "[FF] Thermal Management Requirement of the Invar = Careful attention to thermal management"]
-[9.63879680633545, 2.3051798343658447, "[FF] Proprietary Period of the NuSTAR = None"]
-[6.218302249908447, -0.2273985892534256, "[TT] System AI&T Duration of the RRSW = Six months"]
-[8.262382507324219, 5.749351978302002, "[TT] Accuracy of the FFRF Sensor = 1 cm and 1\u00b0"]
-[11.246159553527832, 5.889875888824463, "[TT] Surface Composition of the Ryugu = Two different types of material, one slightly redder and the other slightly bluer"]
-[6.747158050537109, 3.514849901199341, "[FF] Purpose of the SM = Provides in-space power, propulsion capability, attitude control, thermal control, water and air for the astronauts"]
-[6.3372039794921875, 4.782889366149902, "[FF] Function of the EGS = Run from any Space Operations Center and work with the Air Force Satellite Control Network or Universal Space Network ground stations"]
-[6.742735862731934, 7.598280906677246, "[TT] Beam Width of the Channel = 0.66 \u00ba"]
-[8.932121276855469, 4.399001598358154, "[FF] Sun Sensors, Star Sensors, Magnetometer of the AOCS = Provide attitude data in the form of absolute attitude errors"]
-[8.023337364196777, 2.210231304168701, "[FF] Purpose of the FY-3 (FengYun-3) = Cloud profile and rain radars"]
-[3.883437395095825, 6.346537113189697, "[TT] Quantity of the KhalifaSat Antennas = 2"]
-[4.413136005401611, 2.5358991622924805, "[TT] Launch Center of the BeiDou/Compass satellites = XSLC (Xichang Satellite Launch Center)"]
-[4.512864112854004, -0.8513527512550354, "[FF] Design Baseline of the SpaceX's Crew Dragon = Manufacture its Crew Dragon spacecraft and Falcon 9 v.1.1 rocket, then launch, fly, land and recover the crew"]
-[6.386579990386963, 1.0172594785690308, "[TT] First Light Observations Date of the MIRIS = Dec. 23, 2013"]
-[4.6014404296875, 1.7461040019989014, "[FF] Presentation Date of the RazakSAT = Nov. 7-11, 2005"]
-[9.443384170532227, 1.0234110355377197, "[TT] Speed Before Jettisoning of the Orion = 480 km/hr"]
-[10.73326301574707, -0.2604082226753235, "[TT] Horizontal Baselines of the Tandem-L = 1 km to 18 km"]
-[11.138625144958496, 5.021223545074463, "[TT] Circle Radii of the SPS = 42 and 52 mm"]
-[1.7671345472335815, -2.0629398822784424, "[FF] Mission of the Hayabusa 2 = Ryugu, a carbonaceous asteroid"]
-[9.375329971313477, 4.775163173675537, "[FF] Control of the Satellite = Full 3-axes and continuous drag-free satellite control"]
-[10.758047103881836, 0.8887585401535034, "[TT] Radius of the TOI-148, TOI-587, TOI-681, TOI-746, TOI-1213 = 0.81 to 1.66 times that of Jupiter"]
-[10.864184379577637, 4.008602142333984, "[FF] Examples of the Passive Deorbiting Devices = Tethers and drag sails"]
-[3.387056827545166, 5.139625072479248, "[TT] Frequency Band of the L-band SAR = L-band"]
-[6.610903263092041, -0.08111732453107834, "[FF] Observation Duration of the BRITE satellites = 15 minutes"]
-[8.29568862915039, 7.17959451675415, "[TT] Lens Type of the Supervision Cameras = High performance machine vision lens"]
-[9.082789421081543, 4.815817356109619, "[TT] Sensor Quantity of the OPSE = 8"]
-[6.724398136138916, -0.2691182494163513, "[TT] Period of the Satellite = 103.2 minutes"]
-[12.037701606750488, 3.2821314334869385, "[FF] Trajectory of the EP (Busek BIT-3 Iodine engine) = Low energy manifold"]
-[6.680688381195068, 5.920997619628906, "[FF] Meeting Date of the Optical Wireless = October 14th, 2008"]
-[7.396049976348877, 2.6670620441436768, "[FF] Secondary Objectives of the PROBA = Space environment investigation and Earth observation"]
-[10.160405158996582, 3.724940299987793, "[FF] Design of the CubeSat = Dual-spinner design"]
-[4.964174747467041, 0.8652322888374329, "[TT] Flight Demonstration Goal of the DRACO = Fiscal year 2026"]
-[7.885614395141602, 8.561508178710938, "[TT] Spectral Bands of the HyperScout = 45 visible and near-infrared spectral bands"]
-[10.328186988830566, 5.307314395904541, "[TT] Control Type of the Thermal Control Subsystem = Passive"]
-[8.983960151672363, 7.242440700531006, "[TT] Spatial Resolution of the Imager = High"]
-[8.697800636291504, 9.045379638671875, "[TT] Sensitivity of the NIRSpec MIRI = 12 nJy (1.1 \u03bcm, \u03c4 i =10,000 s, and \u03bb/\u0394\u03bb= 4)"]
-[5.6089863777160645, 5.368346214294434, "[TT] Interface Compatibility of the Spacecraft Avionics EDU = Matches the power and data interfaces of the flight spacecraft, and the command interface of the flight system"]
-[11.433589935302734, 5.732397556304932, "[TT] Main Metal Percentage of the Cobalt Alloy = 45%"]
-[5.157203197479248, 2.4075534343719482, "[TT] Mission Type of the PW-Sat = Non-EO"]
-[5.143528938293457, 7.007389545440674, "[TT] Regenerative Mode Downlink of the Communication Modes = 155 Mbit/s"]
-[11.989026069641113, 5.037351608276367, "[TT] Size of the LALT-TR = 360 mm x 450 mm x 408 mm"]
-[8.7373628616333, 0.38483262062072754, "[TT] Spring Tide Height of the Gulf of Khambhat = 11.6 meters (38 feet)"]
-[4.508028984069824, 3.837695598602295, "[TT] Number of Satellites of the Galileo = 8"]
-[6.713510513305664, 5.935696601867676, "[TT] Quantity of the TCU = 12"]
-[7.716210842132568, 8.756872177124023, "[TT] Spectral Ranges of the MSU-E = 0.5 - 0.6 \u00b5m, 0.6 - 0.7 \u00b5m, 0.8 - 0.9 \u00b5m"]
-[8.397540092468262, 1.9020919799804688, "[TT] Type of the Scatterometers = Scatterometers"]
-[7.96904182434082, 5.248313903808594, "[FF] Function of the FLLS = Read the associated displacement error for that temperature from the look-up table, and subtract it from the displacement measurement"]
-[13.835936546325684, 2.6963937282562256, "[TT] Mass of the Spacecraft = ~2500 kg (launch mass)"]
-[3.939431667327881, 6.340806484222412, "[TT] Antennas of the RF Communications = Two existing two-axis gimbaled directional antennas"]
-[7.500965595245361, 2.9439806938171387, "[FF] Usage of the SOFIE and MLS = Categorized the inter-annual variability of winter and springtime upper stratospheric methane (CH4)"]
-[9.750678062438965, -0.3308885395526886, "[TT] Viewing Altitude of the SSULI = Approximately 50 km to 750 km"]
-[4.750735282897949, 0.38986846804618835, "[TT] Launch Date of the Project = May 2017"]
-[9.629032135009766, 8.34402084350586, "[TT] Field of View (FOV) of the TIRS = 15\u00ba"]
-[9.74656867980957, 8.092611312866211, "[TT] Focal length of the Medium resolution = 40 mm"]
-[4.8407769203186035, 6.143245697021484, "[FF] Purpose of the Fox-1D = Radio amateur and technology research"]
-[13.348511695861816, 7.801827907562256, "[TT] Transmitter Output Power of the S-band transponder = 5 W"]
-[3.4711060523986816, 5.316714286804199, "[TT] Pulse Width of the CSG-SAR = Programmable (5-100 \u00b5s)"]
-[4.508846282958984, 1.9225529432296753, "[FF] Contract Award Date of the RADARSAT Constellation Mission = May 29, 2009"]
-[13.873832702636719, 3.071277618408203, "[FF] Mass of the ANTELSAT = 2U"]
-[7.86358642578125, 8.72628402709961, "[TT] Spectral Range of the CLARREO = 5 to 50 \u00b5m"]
-[5.8546013832092285, 0.5166279077529907, "[TT] Data Averaging Period of the ELS-A = 4 months from November 2008 to February 2009"]
-[13.281686782836914, 7.272034168243408, "[TT] Power of the Capability = 24 W"]
-[8.1350679397583, 0.5631806254386902, "[FF] Damage of the Yellowstone River = Cut a new course"]
-[8.864693641662598, 8.052785873413086, "[TT] Maximum Field Distortion of the TOU = 3.84%"]
-[11.7722806930542, 3.281132459640503, "[TT] Noise of the Thrusters = 0.1 \u00b5N / Hz"]
-[9.836392402648926, 4.546916961669922, "[TT] Attitude Control of the ACS = Reaction wheels and magnetic torquers"]
-[6.331669807434082, 4.192645072937012, "[FF] Components of the SEXTANT = 1) the NICER XTI, 2) the flight software and algorithms, 3) the ground testbed, and 4) the ground system"]
-[5.3504743576049805, 7.1883368492126465, "[TT] Data Rate of the Flight Modem = 72 Mbit/s to 2.88 Gbit/s"]
-[7.376739978790283, 6.487618446350098, "[TT] Median Delivery Time of the Ground Network = Under 1 hour for high-priority imagery"]
-[8.531867980957031, 7.886884689331055, "[TT] Array Size of the SWIR = 80 x 640"]
-[4.009206771850586, 2.1485824584960938, "[TT] Launch Vehicle of the INSAT-3D = Ariane-5 ECA"]
-[2.2707266807556152, 2.7801196575164795, "[TT] Co-PI of the EPI-Lo = Tycho von Rosenvinge"]
-[8.356158256530762, -0.6060077548027039, "[TT] Size of the Iceberg A-76 = 1,500 square miles (4,000 km2)"]
-[8.215132713317871, 5.845387935638428, "[TT] Accuracy Assured Rate of the STOs and STAEs = 0.0608 \u00b1 0.0008\u00ba/s (H); 0.005\u00ba/s (V)"]
-[5.808145999908447, 2.950145959854126, "[TT] Funding of the GeoXO = NOAA"]
-[3.4967970848083496, -0.8835520148277283, "[TT] Orbit Type of the ADEOS = Sun-synchronous polar descending"]
-[10.327248573303223, 6.713398456573486, "[FF] Round-Trip Path Length of the Three Mirrors = Twice the distance between the beam starting point and a plane normal to the beam direction and intersecting the vertex"]
-[8.187760353088379, 7.390895843505859, "[TT] Type of the Metrology Detectors = PSD (Position Sensitive Detectors)"]
-[8.606047630310059, 7.615413665771484, "[TT] Detector Size of the MPID = 4 cm x 8 cm"]
-[12.823039054870605, 7.607874393463135, "[TT] Instrument Power of the GGAK-M = 80 W"]
-[4.899168014526367, 3.4568307399749756, "[TT] Manufacturer of the NETCAM = Airbus DS, Bremen"]
-[7.090949535369873, 4.469180107116699, "[FF] Design Strategy of the RVX Profile = Non-drifting injection"]
-[6.932196617126465, 6.941189289093018, "[TT] Quantity of the Laser Transmitters = 2"]
-[9.272212982177734, 5.221815586090088, "[TT] Solar Elevation Angle in TC Operation of the Instrument = < 40\u00ba"]
-[4.460255146026611, 6.7120041847229, "[TT] RF Communications of the Spacecraft = X-band for science data acquisition"]
-[5.668576717376709, 3.2241597175598145, "[TT] Provider of the DMSP = NOAA"]
-[5.796911239624023, 1.079892873764038, "[FF] Presentation Date of the BepiColombo = Feb. 28-March 4, 2011"]
-[8.046833038330078, 6.579589366912842, "[FF] Usage of the Spectral Imager = Not used"]
-[5.332047462463379, 5.999553680419922, "[TT] CPU Operating Frequency of the OBC = 50 MHz"]
-[5.656527042388916, 2.090421199798584, "[FF] Quality Checks of the Launcher Mission Parameters = Not detected during the standard quality checks"]
-[5.677371978759766, 1.0362720489501953, "[FF] Mission Start Date of the IBEX = Unknown"]
-[3.4095818996429443, -0.9202606678009033, "[TT] Orbit Type of the COMPASS-1 = Sun-synchronous circular polar orbit"]
-[6.493831157684326, 4.84896993637085, "[FF] Function of the MIU = Interface between the SCB (Spacecraft Bus) and the CEU (Combined Electronics Unit) in the payload"]
-[9.256524085998535, 2.302699327468872, "[TT] Auroral Potentials of the Jupiter = Up to 400,000 electron volts"]
-[8.913110733032227, 3.078310251235962, "[FF] Impact of the Solar Flares = Capable of severely disrupting technologies on Earth such as satellite operations, GPS navigation and communication systems"]
-[13.250807762145996, 5.389348983764648, "[FF] Features of the Prometheus Block 2 CubeSats = Four deployable solar panels, an active attitude control system with stellar sensors, and a SDR (Software Defined Radio) with a footprint sufficiently small for tactical operations"]
-[12.118578910827637, 7.628232955932617, "[TT] Mass of the Imager = ~ 130 kg"]
-[9.462512969970703, 7.057713508605957, "[TT] Spatial Sampling Distance of the MSI = 10 m, 20 m, 60 m"]
-[11.383683204650879, 3.325416088104248, "[TT] Purpose of the ENPULSION MICRO R3 = Orbit raising"]
-[12.923882484436035, 6.753683090209961, "[TT] Predicted Specific Impulse of the Future PPT Module = 76.3 m/s"]
-[8.85700511932373, 1.4355977773666382, "[FF] Gravity Levels of the Centrifuge = 0 and 1g"]
-[3.4001362323760986, 5.3399176597595215, "[TT] Peak Power of the SAR instrument = 1000 W"]
-[4.738399982452393, 3.1866157054901123, "[TT] Manufacturer of the EUTELSAT KONNECT = Thales Alenia Space"]
-[5.123980522155762, 0.1967715471982956, "[FF] Publication Date of the CYGNSS = 19 June 2018"]
-[6.0761189460754395, 7.904301166534424, "[TT] Receiver Channels of the Jason 2 = 8 channels"]
-[9.277908325195312, 3.2083353996276855, "[TT] Type of the Solar Coronagraph Instrument = Distributed over the Formation"]
-[8.86918830871582, 0.9862609505653381, "[TT] Lead Author Affiliation of the Parker Solar Probe = BWX Technologies, Inc. and University of Michigan"]
-[5.3775200843811035, 3.2188398838043213, "[TT] Machining Technique of the Satellite = WEDM (Wire Electrical Discharge Machining)"]
-[6.4616875648498535, 1.8197600841522217, "[FF] URL of the SIXS = http://www.cosmos.esa.int/web/bepicolombo/sixs"]
-[5.132616996765137, 3.228308916091919, "[TT] Manufacturer of the Clementine = US Naval Research Laboratory (NRL)"]
-[10.9500093460083, 5.6763997077941895, "[TT] Material of the Thermal Isolation Components = Delrin"]
-[7.015330791473389, 0.8062902092933655, "[FF] Presentation Date of the Gravity Probe B = 1991"]
-[9.069354057312012, 6.629275798797607, "[TT] Data Acquisition Spacing of the SARAL/AltiKa = ~ every 180 m"]
-[5.125808238983154, -0.6064648628234863, "[FF] URL of the TARANIS = http://www.cnes.fr"]
-[8.767271995544434, 4.705817699432373, "[FF] Technical Verification of the STARS = URL: http://robotics.estec.esa.int/i-SAIRAS/isairas2008/Proceedings/POSTER%20SESSION/m003-Nohmi.pdf"]
-[5.653831481933594, 5.854999542236328, "[TT] MIPS of the SCS750 = 1500"]
-[9.778533935546875, -0.6246197819709778, "[TT] Orbit Altitude of the JAWSAT = 753 km x 805 km"]
-[12.021724700927734, -0.3566969931125641, "[TT] Discovery Date of the TESS = 14 April 2021"]
-[6.861382484436035, 5.806623935699463, "[TT] Quantity of the RW = 4"]
-[7.684136867523193, 9.285041809082031, "[TT] Wavelength Range of the Band 5 = 1628-1654 nm"]
-[7.335225582122803, 1.1627554893493652, "[FF] Announcement Date of the Water mission = Sept. 3, 2010"]
-[10.953803062438965, 2.125504732131958, "[FF] Mission of the XMM-Newton = ESA"]
-[13.366195678710938, 5.541332721710205, "[FF] Solar Panels of the Lander = Vertical panels"]
-[10.195727348327637, 5.7677226066589355, "[TT] Temperature Uncertainty of the Instrument = 0.1K at the bottom of the limb to 13 K at 140 km"]
-[7.1219706535339355, 6.608175754547119, "[FF] Threshold-to-Noise Ratio of the GLM = Unknown"]
-[5.6530866622924805, 0.959621250629425, "[FF] Date of the GAUSS Satellite Launch = Nov. 21, 2013"]
-[9.64379596710205, 7.049829483032227, "[TT] Resolution of the MWR = 40 km"]
-[7.278740882873535, 1.3994715213775635, "[TT] Solar Arrays Deployment Time of the GOES-T = 8:28 p.m. EST"]
-[9.704567909240723, 1.8540680408477783, "[FF] Contribution Date of the Hubble = 30 December 2018"]
-[11.7191801071167, 4.902863025665283, "[TT] Transverse Dimensions of the HXT-S = 465 mm x 392 mm"]
-[4.041777610778809, 6.708669185638428, "[TT] Quantity of the X-band ground stations = 4"]
-[8.034997940063477, -1.018813967704773, "[TT] Instrument of the ICESat-2 = Ice, Cloud and land Elevation Satellite-2"]
-[9.8123197555542, 5.438978672027588, "[TT] SRP Acceleration of the M1S/M2S = 138 nm/s2"]
-[11.211700439453125, 5.401715278625488, "[TT] LYSO crystals of the Range Calorimeter = 9"]
-[6.109073162078857, 4.126813888549805, "[TT] Component Reuse of the COSMOS Software = A number of Agents are used in every aspect of operations"]
-[3.483893871307373, 1.8198107481002808, "[FF] Launch Vehicle of the Sentinel-1C = Vega-C"]
-[11.739937782287598, 3.2983314990997314, "[TT] Reaction Chamber Pressure of the Microthrusters = 0.3 MPa"]
-[7.631870269775391, 2.168808937072754, "[TT] Primary Use of the Band 6 = Soil humidity, provision of ice/snow cover distinguishing capability"]
-[4.177670001983643, 7.205779552459717, "[TT] Ku-band antennas of the Spire Global = High-capacity"]
-[10.892518997192383, 1.4247876405715942, "[TT] Mass of the Delta Scuti stars = 1.5-2.5 times the Sun\u2019s mass"]
-[6.931081295013428, 1.5053660869598389, "[FF] Test Date of the James Webb Space Telescope = Summer 2014"]
-[7.297191619873047, 3.199627161026001, "[FF] User Services of the Envisat = Unknown"]
-[7.957542896270752, 7.774565696716309, "[FF] TDI Mode of the NAOMI = Enabled in the Pan band"]
-[6.271563529968262, 4.290654182434082, "[FF] Technology of the DSX = Planning System Inc. (PSI) Network Data Acquisition System (NDAS)"]
-[10.182156562805176, 3.184983968734741, "[FF] Subsystem Microprocessor of the CubeSat = Each subsystem has its own microprocessor"]
-[9.713763236999512, 4.577244758605957, "[TT] Type of the Attitude control = Passive control via permanent magnet and hysteresis dumper"]
-[9.50337028503418, 7.045289993286133, "[TT] Resolution of the MR-2000M1 = 0.7 km x 1.4 km"]
-[5.882464408874512, 4.989861965179443, "[TT] Software of the OBC = FOS (Flight Operations Segment)"]
-[9.805961608886719, 5.605836391448975, "[TT] Tilt of the M2 = 10 \u00b5rad"]
-[4.405671119689941, 3.0534589290618896, "[TT] Data Receiving and Processing Stations Locations of the Kolibri-2000 = Tarusa, Obninsk (Russia), and Sydney (Australia)"]
-[9.489311218261719, 3.537376880645752, "[FF] Value of the PUI Pressure = Unknown"]
-[5.959300994873047, -0.41922929883003235, "[TT] Operation Duration of the e-POP RRI = Three Years"]
-[7.021827697753906, 7.1461334228515625, "[TT] Pulse Width of the NSCAT = 5 ms"]
-[9.541576385498047, 4.754856586456299, "[FF] Torque Input of the Attitude Control System = Minute and continuous"]
-[4.897162437438965, 7.110009670257568, "[TT] S-band Downlink Data Rates of the Payload = 15, 128, 512 kbit/s"]
-[7.2605180740356445, 4.867972373962402, "[FF] Connection of the Leg Assemblies = Connected to the head by two interfaces"]
-[8.557123184204102, 1.679673671722412, "[TT] Rainfall of the Hurricane Laura = 5 to 10 inches"]
-[7.994173526763916, 9.057818412780762, "[TT] Wavelength Range of the BEO = 400-1100 nm"]
-[8.692197799682617, 3.856478452682495, "[TT] Number of Instrument Units of the Solar Orbiter = 33"]
-[9.576102256774902, 4.6740827560424805, "[FF] Control Modes of the ADCS = De-tumbling, nadir and inertial pointing"]
-[2.291940212249756, 2.764625310897827, "[TT] SSM of the EPI-Lo = Edmond Roelof"]
-[6.216883182525635, 4.397660255432129, "[FF] User Mission Operations Center Simulator of the LCRD = UMS"]
-[5.030393123626709, 7.400330543518066, "[TT] AVNIR (P) Data Rate of the RF communications = 60 Mbit/s"]
-[11.669057846069336, 4.772555828094482, "[TT] Structure Height of the Clementine = 1.88 m"]
-[8.486886024475098, 2.1421597003936768, "[FF] Observation of the SASS = Ocean winds"]
-[9.513021469116211, -0.3263653516769409, "[TT] Radius of the Orbital Phase 2 = Ca. 19 km"]
-[4.837828159332275, 4.513293266296387, "[FF] Technology of the Cesium Mission 1 = Electronically steerable, multibeam APA (Active Phased Array)"]
-[11.757596015930176, 4.997000217437744, "[TT] Dimensions of the IPEX-II boom = 2.35 m x 0. 3 m x 0.3 m"]
-[10.160064697265625, 3.154043197631836, "[FF]  of the CubeSat Deployer = "]
-[9.470084190368652, 4.10438871383667, "[TT] Channels of the Electric Field Measurement System = 16"]
-[9.489502906799316, 7.372675895690918, "[TT] Resolution of the PAN = 0.65 m"]
-[8.42424488067627, 5.524972438812256, "[TT] RMS Absolute Error of the Geolocation Testing = 1-2 m"]
-[9.56494140625, 9.08191967010498, "[TT] Spatial Resolution of the IRIS = Between 0.33 and 0.44 arcseconds"]
-[9.308911323547363, 6.8068952560424805, "[TT] Spatial Resolution of the GF-3 = 3.5 m in azimuth and 5.5 m in range"]
-[7.411390781402588, 5.530013084411621, "[FF] Objective of the LRI = Measure the same range fluctuations as the KBR instrument, but with less noise, and provide precise measurements of the relative pointing of the satellites to each other"]
-[9.81857681274414, 4.4534912109375, "[TT] Attitude Control of the EURECA = Magnetorquers"]
-[8.822729110717773, 7.463351726531982, "[TT] Field of Regard of the Pushbroom imager = \u00b130\u00ba"]
-[5.8922438621521, 7.0156731605529785, "[TT] Telemetry Format of the Instrument = PCM (Pulse Code Modulation)"]
-[7.503780364990234, 6.821000099182129, "[TT] Number of Channels of the Scanning Radiometer = 12"]
-[3.477916717529297, -0.8884274363517761, "[TT] Orbit of the SeaHawk-1 = Sun-synchronous"]
-[13.382245063781738, 6.747460842132568, "[TT] Array Power of the Spacecraft = 650 W, 790 W"]
-[9.205340385437012, 3.221890449523926, "[TT] Observation Target of the Aditya-1 = Solar corona"]
-[13.46021556854248, 7.378885269165039, "[TT] Power of the TOMS = 24 W"]
-[6.509583473205566, 3.535315752029419, "[FF] Launch Box Purpose 1 of the RemoveDebris satellite = Protect spacecraft during shipping, launch, and handling aboard the ISS"]
-[6.58738374710083, 3.8015024662017822, "[FF] Data Use of the DMS = Helps scientists identify features that are also detected by radar, laser, and gravity instruments"]
-[12.07256031036377, 4.508429527282715, "[TT] Size of the Spacecraft = \u00d8 1,500 x 1,940 mm height"]
-[7.557164192199707, 3.461906671524048, "[FF] Data of the NightPod = Events such as storms, floods, fires and volcanic eruptions"]
-[8.097246170043945, 6.30959939956665, "[TT] Type of the MSU-E = Sensor"]
-[12.157522201538086, 4.696020126342773, "[TT] Bus Dimensions of the PRISMA = 1.751 x 1.545 x 3.4 m"]
-[10.733644485473633, 7.5517897605896, "[TT] Swath Width of the Altimeter = 2.4 to 12 km"]
-[7.012225151062012, 5.869872570037842, "[TT] Quantity of the PIRATA = 15"]
-[7.8257904052734375, 6.9706292152404785, "[TT] EFL of the COR1 = f/20"]
-[7.3924384117126465, 5.4321465492248535, "[FF] Components of the Antenna/Drive/Calibration Subsystem = Conical corrugated horn-fed shrouded reflector, multiplexer, closed-loop antenna scan drive assembly and closed path calibration assembly"]
-[6.039548873901367, 5.979025840759277, "[TT] Number of Modules of the Memory Module = 3"]
-[9.917970657348633, 4.597548961639404, "[TT] Spinner Assembly Rotation of the MicroMAS-2 CubeSat = 30 rpm"]
-[5.117973804473877, 1.092998743057251, "[FF] Conference Date of the MicroMAS Project = August 13-16, 2012"]
-[10.411523818969727, 5.6963582038879395, "[TT] Cooling Temperature of the IRFPA = 70 K"]
-[5.725442886352539, 6.354249477386475, "[TT] Solid State Recorder Capacity of the C&DH = 4 TB @ BOL and 3.1 TB @ EOL"]
-[6.394080638885498, 3.3990695476531982, "[FF] Cargo Transportation Services Requirement of the ISS = Resupply and return"]
-[14.074628829956055, 4.061219215393066, "[FF] Mass of the Instrument = 1 kg"]
-[6.269100189208984, 8.188610076904297, "[TT] No of bands/channels of the MWRI = 6"]
-[11.563718795776367, 3.4489684104919434, "[FF] Objective of the VAT (Vacuum Arc Thruster) = On-orbit demonstration of a trigger-less vacuum arc thruster"]
-[5.279877662658691, 1.5964106321334839, "[FF] Partnership Date of the CICERO = Dec. 4, 2009"]
-[14.1233491897583, 7.19289493560791, "[TT] Input Voltage Range of the SLATS PPCU = 24 V to 32 V"]
-[11.386883735656738, 4.389747619628906, "[TT] Size of the CP-9 = 2U"]
-[10.196073532104492, 1.5029547214508057, "[TT] Redshifts of the NISP Spectrograph = About 30 million emission line galaxies"]
-[3.2189598083496094, 3.8706295490264893, "[TT] Science Mission End of the TanDEM-X and TerraSAR-X = End of 2015"]
-[3.913733720779419, 3.3253462314605713, "[FF] Testing Duration of the Galileo Satellites 13 and 14 = Lengthy"]
-[5.407710552215576, 0.4155280590057373, "[FF] Launch Date of the Apollo 15, 16, 17 = 1960s"]
-[8.422359466552734, 7.359968185424805, "[TT] Number of Images per CME of the CCOR = At least two"]
-[1.6134923696517944, 3.759596824645996, "[TT] Reaction wheels of the BEESAT-2 = Yes"]
-[6.104851245880127, 4.760499477386475, "[FF] Type of the Telemetry = Spacecraft health and safety information (engineering telemetry) and raw instrument data"]
-[5.5792236328125, -1.9888705015182495, "[FF] Function of the Kodiak system = Provide real-time images and distance-ranging information"]
-[3.599684476852417, -0.9794498085975647, "[TT] Orbit of the GRACE-FO = Near-polar"]
-[7.490628719329834, 6.818578243255615, "[TT] Full Frame Integration Time of the CCD = 2.6 seconds"]
-[12.146724700927734, 3.66853666305542, "[TT] Maximum Operating Pressure of the Xenon Gas Tank = 150 bar"]
-[9.024683952331543, 5.687751293182373, "[TT] Pointing Tolerance of the SAC = 20\u00ba"]
-[8.514776229858398, 3.0659499168395996, "[FF] Purpose of the VWFC = Take wide-angle ultraviolet-light photographs of vast regions of sky not observable from Earth"]
-[9.638736724853516, 4.093002796173096, "[FF] Advantages of the Magnetic Capture Technology = Improves on the shortcomings of both tethered systems and robotic systems"]
-[9.521671295166016, 7.107140064239502, "[TT] Resolution of the VIIRS = 750 m"]
-[6.733144283294678, 6.452503681182861, "[TT] On-Board Processing Time of the HyperScout 1 = About one minute"]
-[10.696629524230957, 7.552044868469238, "[TT] Swath Width of the Optoelectronic System = 15 km"]
-[7.35940408706665, 0.24532797932624817, "[TT] Last Flyover Date of the OSIRIS-REx = April 7, 2021"]
-[9.377655029296875, 7.067945957183838, "[TT] Spatial Resolution of the Hyperion = 30 m"]
-[7.938046932220459, 8.750255584716797, "[TT] Spectral Coverage of the NIR (Near Infrared) = 760-850 nm"]
-[8.682454109191895, 7.469340801239014, "[TT] Current Detection Scale Sizes of the MGF = 100 m or larger"]
-[6.810902118682861, 2.7842321395874023, "[TT] Developer of the MethaneSAT = Environmental Defense Fund (EDF)"]
-[6.970642566680908, 4.917476654052734, "[FF] Purpose of the Optical Ground Station = Initial thrust testing"]
-[6.1302924156188965, -0.22017242014408112, "[TT] Operation Status of the Genesis-2 = Nominal in 2013"]
-[3.460918664932251, -0.9121009111404419, "[FF] Orbit of the AERO and VISTA = Sun-synchronous polar orbit"]
-[12.184274673461914, 2.920804023742676, "[TT] Propellant Mass of the Hydrazine propulsion system = 120 kg"]
-[5.0504302978515625, 0.9726988077163696, "[TT] Operation Period of the GEM and GIM = Since shortly after launch in August 2001 until August 4, 2004"]
-[4.931761264801025, 0.3401225209236145, "[TT] Launch Date of the SAC-B = Nov. 4, 1996"]
-[7.852283477783203, 8.624619483947754, "[FF] Bands of the Spectral bands = 0.52 - 0.60 \u00b5m (green), 0.63 - 0.69 \u00b5m (red), 0.76 - 0.89 \u00b5m (NIR)"]
-[6.828951835632324, 5.920112133026123, "[TT] Quantity of the XBAA = 2"]
-[4.620949745178223, 1.5833266973495483, "[TT] Launch Date of the SkySat-4-7 = September 16, 2016"]
-[4.1857991218566895, 0.19954177737236023, "[FF] Launch Date of the Falcon 9 = Jan. 6, 2014"]
-[12.199700355529785, 3.622394561767578, "[TT] Xenon Quantity of the XTA = 110 kg"]
-[9.7117338180542, -0.18557532131671906, "[FF] Orbital Altitudes of the TSUBAME = Seven different orbital altitudes"]
-[6.303381443023682, 4.268614768981934, "[FF] Functionality Testing of the EDU Lab = Mission capable code"]
-[12.792604446411133, 2.011906147003174, "[TT] Vertical Range of the SAGE-III = 0 km to 100 km"]
-[7.849223613739014, -2.484783887863159, "[TT] Observation Type of the GOLD = Earth's Upper Atmosphere"]
-[8.526972770690918, 7.793269634246826, "[FF] Size of the Subarray = 400 mm x 22 m"]
-[11.059012413024902, 5.862544059753418, "[TT] Shielding Efficiency of the MLI Design = 23 dB"]
-[4.0189971923828125, 2.165476083755493, "[TT] Launch Vehicle of the SES-17 = Ariane 5 ECA"]
-[6.371652126312256, -0.21979773044586182, "[TT] Maintenance Schedule of the COSIMA = Checkouts every 6 months"]
-[5.363749027252197, 0.5689643621444702, "[TT] Mission End Date of the Envisat = May 9, 2012"]
-[11.309867858886719, 4.640171527862549, "[TT] Min. Depth of the GTSPP = 1 m"]
-[11.721773147583008, 5.069838047027588, "[TT] Module Section of the ECAL = 648 mm x 648 mm"]
-[7.41572380065918, 5.120611190795898, "[TT] Rigidly Mounted of the LRI = Yes"]
-[7.54744291305542, 2.8413407802581787, "[FF] Mission of the FY-4 Series = Imagery, sounding, lightning mapping, and space environment monitoring"]
-[13.10422420501709, 7.554800510406494, "[FF] Computing Power of the AMS-02 = Four 750 MHz PowerPC computers running Linux"]
-[9.434624671936035, 7.103909015655518, "[TT] Spatial Resolution of the COR1 = \u2264 16.0 arcsec"]
-[7.6860432624816895, 5.30600643157959, "[FF] Acoustic Testing of the MSA = Performed in the NIRSpec ETU"]
-[9.318496704101562, -0.423690527677536, "[TT] Apogee of the STRV-1c and -1d = 36,000 km"]
-[5.636465072631836, 6.461920738220215, "[TT] Storage Capacity of the 50 Ah = 50 Ah"]
-[4.515449523925781, -0.8075059056282043, "[TT] Installation Date of the SpaceX CRS-13 Dragon = 17 Dec. 2017"]
-[5.249281883239746, 5.926893711090088, "[TT] Data Bus Interface of the PCU = SpaceWire type"]
-[8.14202880859375, 5.8913702964782715, "[FF] Precision of the LASSO = Better than 100 ps"]
-[5.71372127532959, 7.719123840332031, "[TT] Number of High-Gain Stages of the DNB = 2"]
-[6.461099624633789, -0.8684723377227783, "[TT] LTAN of the QSat = 10:00 - 14:00 hours"]
-[4.937524795532227, 7.343260765075684, "[TT] Data Rate (Uplink) of the S-band transmitter = 4 kbit/s"]
-[11.582765579223633, 3.795232057571411, "[TT] Rotation Angle of the Y-axis Bang-Bang Maneuver = 130\u00ba"]
-[7.902346134185791, 8.36858081817627, "[TT] Spectral Bands of the TrueColour Imager = 9 bands"]
-[8.653572082519531, 1.1118789911270142, "[FF] Science Team Meeting of the Aquarius = Nov. 11-14, 2014"]
-[7.849482536315918, 4.878012657165527, "[TT] Radiation Tolerance of the GPS Receiver = Up to 50 kRads"]
-[6.341114521026611, 5.603529930114746, "[FF] Function of the FPGA = Generates all the clocks necessary for driving the 4 CCDs and drives the DACs responsible for providing the bias voltages"]
-[11.38425064086914, 4.968820571899414, "[TT] Size of the BioSentinel = 6U"]
-[7.088710308074951, 1.1939237117767334, "[FF] Launch Date of the ExoMars Trace Gas Orbiter = 2016"]
-[7.966269016265869, 3.1587398052215576, "[FF] Algorithm of the OCO, GOSAT, OCO-2 = Atmospheric Carbon Observing System (ACOS)"]
-[5.635919570922852, 6.643885612487793, "[TT] Data Volume Reduction of the RMC = About half"]
-[4.84724235534668, -0.9755104184150696, "[FF] Launch Date of the Fengyun-4A = Dec. 10, 2016"]
-[7.050398349761963, 7.762670993804932, "[TT] Cube Corner Reflectors (CCRs) of the LARES = 92"]
-[10.387184143066406, 4.57434606552124, "[FF] Properties of the Cryogenic Fluid = Keeps spacecraft operational and can prolong their lifespan by years"]
-[6.782015323638916, 6.108295440673828, "[TT] Ultra-fine of the Mode = -"]
-[4.49492073059082, 1.4218149185180664, "[TT] Reentry Date of the TechEdSat-1 = May 5, 2013"]
-[3.846221923828125, 4.229171276092529, "[FF] Mission Objectives of the SAR-RCM = Monitoring of glacier cover, motion and topography, ice sheet and land surface topography, and sea-ice cover and type"]
-[4.906626224517822, 0.1776580512523651, "[TT] End of Life Date of the CXBN = 31 January 2013"]
-[5.093337535858154, 2.6188888549804688, "[TT] Managing Center of the Chandra = NASA's Marshall Space Flight Center"]
-[5.763914585113525, -0.8492615818977356, "[TT] Design Life of the Mission = 7.7 years"]
-[9.121405601501465, 5.507537364959717, "[TT] Pointing Accuracies of the AOCS = \u00b10.05\u00ba in all axes"]
-[8.641629219055176, 6.774534225463867, "[TT] Observation Efficiency of the FY-4 spacecraft series = 85%"]
-[6.214494228363037, 4.166195869445801, "[FF] Function of the Remote Agent = Planned DS1 activities on-board and carried out the plan without ground intervention"]
-[7.740796089172363, 5.015183448791504, "[FF] Observation Purpose of the MIRIS = Functional test purposes without any proper calibration process"]
-[10.889931678771973, 0.8935078382492065, "[FF] Lifespan of the Red Dwarfs = Generally do not live long enough for complex life to evolve"]
-[14.060907363891602, 3.594815731048584, "[TT] Mass of the Aquarius instrument assembly = 375 kg"]
-[4.966750621795654, 0.3541591763496399, "[TT] Adoption Year of the SASAR = 2004"]
-[8.271307945251465, 8.396021842956543, "[TT] Absolute radiometric uncertainty of the Spectrometer = <0.8% (SWIR), <0.6% (MWIR), <0.45% (TIR)"]
-[10.449145317077637, 6.6172966957092285, "[TT] Mirrors Quantity of the Starshine-3 = 1500"]
-[8.845653533935547, 7.269059658050537, "[TT] Threshold of the Low LET Detector = 0.2 MeV"]
-[12.181930541992188, -0.0659998208284378, "[TT] Red Limit of the TESS Lens = 1000 nm"]
-[10.375880241394043, 4.568121433258057, "[FF] Permanent Failures of the FormoSat-2 = IRU malfunction and gyro-A noise"]
-[5.5460205078125, 7.100742340087891, "[TT] Rate of the Data Transmission = 750 kbit/s"]
-[6.821782112121582, 1.0806572437286377, "[FF] Article Release Date of the Solar Orbiter = 17 May 2021"]
-[10.913135528564453, 2.1350255012512207, "[FF] Energy Range of the XMM-Newton = Broad"]
-[11.059412956237793, 3.693480968475342, "[TT] Size of the Trisat-R = 3 standardised 10-cm boxes"]
-[9.135910987854004, 5.81437349319458, "[TT] Instrument Pointing (Control/Knowledge) of the Instrument = 0.15\u00ba/0.15\u00ba"]
-[6.774702548980713, 1.3106032609939575, "[FF] Data Gathering Start Date of the Space-Based Weather Instruments = 8 February 2022"]
-[4.571521759033203, 7.9134135246276855, "[FF] Data Header of the THD-7 radios = STRSHN3 N7YTK"]
-[6.944474697113037, 2.133922576904297, "[FF] Image Stack of the DInSAR = 8 TOPS and 8 stripmap images"]
-[11.172416687011719, 1.2756515741348267, "[TT] Gravitational Wave Measurement Range of the LISA = 10 seconds to more than half a day"]
-[5.487674713134766, 3.193118095397949, "[TT] Contract Award of the Northrop Grumman = $692 million"]
-[5.479721546173096, 2.235588788986206, "[FF] Affiliation of the Aur\u00e9lie Moussi = Unknown"]
-[5.499993801116943, 1.664645791053772, "[FF] Precision of the ALOS-4 = Five times more than ALOS-2"]
-[9.46822738647461, -1.1217557191848755, "[TT] Longitude of the Mission Orbit = 75\u00ba W and 137\u00ba W (and possible 105\u00ba W for reduced operations)"]
-[7.442705154418945, -0.6517925262451172, "[TT] Duration of the Operation IceBridge = Late October to late November 2017"]
-[6.846033096313477, 6.024803638458252, "[TT] Decade-Daily Global Composite Products of the PROBA-V = 36"]
-[5.967397689819336, -0.5144087076187134, "[TT] Mission Duration of the BEAM = Two years"]
-[8.535222053527832, 0.035291049629449844, "[TT] Water Ice Abundance of the Comet = 10-15%"]
-[5.770994186401367, 6.887843132019043, "[TT] Header Size of the Raw Science Data Packet = 23 bytes"]
-[10.3355712890625, 3.201394557952881, "[TT] Quantity of the Secondary Payloads = 4 nanosatellites and 1 CubeSat"]
-[5.28554630279541, 8.028898239135742, "[TT] Frequency Range of the VLF narrowband receiver = 3 kHz to 750 kHz"]
-[6.758522987365723, 4.353582859039307, "[FF] Parameter of the SWID = Value"]
-[4.9314680099487305, 5.093554496765137, "[TT] CCSDS ID of the GSAT-0103 = 3A7"]
-[9.772944450378418, 2.6606500148773193, "[TT] Deployment Services Start Date of the NanoRacks LLC = October 2012"]
-[5.0275092124938965, 1.1828668117523193, "[TT] Launch Date of the UniSat-3 = June 29, 2004"]
-[4.8235602378845215, 6.376494884490967, "[TT] Communication Protocols of the RF communications = ECSS E 70, ECSS- E 41"]
-[9.426475524902344, 2.308607339859009, "[TT] Elves Percentage of the ISUAL = 73.93%"]
-[9.810980796813965, 8.727521896362305, "[TT] IFOV of the Instrument = 40 mrad x 40 mrad"]
-[9.586566925048828, 8.271746635437012, "[TT] Field of View of the ELENA = Nadir pointing 1-D FOV"]
-[6.0548224449157715, 2.9144375324249268, "[TT] Funding of the GHGSat = $10 million"]
-[5.205132484436035, 3.135023355484009, "[TT] Manufacturer of the TEMPO = Ball Aerospace"]
-[10.921388626098633, 2.869663715362549, "[TT] Knowledge of the PARASOL microsatellite = 0.02\u00ba"]
-[6.809905529022217, 2.704946517944336, "[FF] Mission of the INSAT-3DR = Provide service continuity to earlier ISRO meteorological missions"]
-[10.00818920135498, 2.875040292739868, "[TT] Launch Date of the CeREs CubeSat = 16 December 2018"]
-[7.263929843902588, 2.5520684719085693, "[TT] Global Average Detection Rate of the exact Earth Satellite = 42 Messages/s"]
-[13.414093017578125, 2.8361122608184814, "[TT] AD-SS Mass of the ALMASat-1 = 6.54 kg"]
-[8.110204696655273, 0.9865640997886658, "[TT] Irrigation Efficiency Threshold of the IAS = 20 percent"]
-[7.9796881675720215, 9.122633934020996, "[TT] Wavelength of the LSA = 532.272 nm"]
-[4.980402946472168, 0.4206984043121338, "[TT] Deployment Date of the SDA Transport Layer = Late 2022"]
-[3.5212886333465576, 5.355287075042725, "[TT] Sampling Rate of the SAR = 250 MHz 83.3 MHz 41.67 MHz 20.83 MHz"]
-[7.558019638061523, 6.866578102111816, "[TT] Exposure Time of the Channels = 0.01-600"]
-[11.986590385437012, -0.3427157402038574, "[TT] Project Management Provider of the TESS = NASA/GSFC (Goddard Space Flight Center)"]
-[9.763166427612305, 7.1812896728515625, "[FF] Spatial Resolution of the Instrument = 40x70 km, 27x46 km, 14x25 km, 17x29 km, 8x14 km, 6x10 km, 6x10 km, 3x6 km, 3x6 km"]
-[6.458275318145752, 0.3198140561580658, "[TT] Observation Frequency of the ULX-4 = Multiple times in quick succession"]
-[6.271711826324463, 4.975131511688232, "[FF] Functionality of the Software = Networking, file I/O operations, low-level hardware configuration, and many basic commands"]
-[11.775115966796875, 6.781744480133057, "[TT] Energy Range of the HXD = 10-60 keV"]
-[9.558297157287598, 7.046876907348633, "[TT] Spatial Resolution (km) of the SMMR = 18.0"]
-[13.421257972717285, 5.5107035636901855, "[TT] Quantity of the Smart Solar Panels = 5"]
-[5.4199442863464355, 2.8341805934906006, "[TT] Designers of the Oculus-ASR = Undergraduate students of MTU (Michigan Technological University)"]
-[4.8622727394104, 0.6575573086738586, "[FF] Launch Date of the MetOp-3 = Unknown"]
-[5.865789890289307, -0.19535420835018158, "[TT] Operational Timelines of the ABI = Continuous Full Disk (CFD), Flex Mode (aka Storm Watch)"]
-[7.593232154846191, 3.51086163520813, "[FF] Size of the DSAT#1 = Representative of the size of a large space debris"]
-[8.990166664123535, 7.486152172088623, "[TT] Resolution of the Comedia C328 = VGA"]
-[11.423145294189453, 0.7819327712059021, "[TT] Mass of the AU Mic b = Smaller than 58 Earths"]
-[13.780759811401367, 3.120985269546509, "[TT] Mass of the GOMX-3 = ~3 kg"]
-[5.686375141143799, -0.27938318252563477, "[TT] Installation Time of the DESIS = One day"]
-[5.04848051071167, 7.177235126495361, "[TT] Ka-band Communication Link Speed of the GEO LCT = 600 Mbit/s"]
-[4.236012935638428, 7.50398063659668, "[TT] Output Frequency of the TREX-823 X-band transmitter = 8.23 GHz"]
-[4.386419773101807, 2.921977996826172, "[TT] Location of the GOUS = Dunedin New Zealand"]
-[9.889652252197266, 5.341685771942139, "[FF] Purpose of the Structural Model (SM) = Embedding STM or Mass Thermal Dummies (MTD) units"]
-[10.859735488891602, 3.921140432357788, "[TT] Purpose of the Drag sail = Cause the orbit of the spacecraft to rapidly decay"]
-[7.930512428283691, -0.4439879059791565, "[FF] Principal Investigators of the Multiple Sclerosis and Parkinson\u2019s Disease Cryovial Study = Dr. Andres Bratt-Leal and Dr. Valentina Fossati"]
-[13.137657165527344, 7.302646636962891, "[TT] Power Consumption of the POLDER-2 = 50 W"]
-[8.282116889953613, 8.509944915771484, "[TT] Surface Roughness of the Mandrels = Better than 4 \u00c5 (0.4 nm)"]
-[8.222526550292969, -0.44167378544807434, "[TT] Temporal Sampling of the Sea Ice Concentration (SIC) = Sub-daily"]
-[8.871668815612793, 7.694733142852783, "[TT] MS B4 of the Pushbroom imager = 0.76-0.89 \u00b5m"]
-[4.911696910858154, 0.6740684509277344, "[FF] Launch Date of the Bion-M1 = April 19, 2013"]
-[4.844155311584473, 0.5114269256591797, "[TT] Launch Date of the AltiKa = 2011/12"]
-[8.089183807373047, -0.8591776490211487, "[FF] Purpose of the Microwave Sensor = Help avoid a dangerous gap in Arctic sea ice data"]
-[11.46263313293457, 5.125340461730957, "[TT] Ceiling Height Requirement of the ETB sub-experiment = Less than 54 mm"]
-[8.09427261352539, 4.418360710144043, "[FF] Operation Modes of the VBS = 6DoF solutions for spacecraft flying in close proximity, and inertial LOS solutions for any spacecraft reflecting more light than an Mv7 star"]
-[7.1356730461120605, 5.954699516296387, "[FF] Purpose of the Ultra Stable Oscillator (USO) = Precise time tagging"]
-[3.382298469543457, 5.322238445281982, "[TT] Frequency of the SAR-10 = 3.13 GHz"]
-[4.913424968719482, 3.2437121868133545, "[TT] Shareholder of the AIS = Hisdesat"]
-[4.405551910400391, 1.8252614736557007, "[TT] Reprogramming Date of the RADARSAT-2 = May 2013"]
-[7.857765197753906, 5.87969446182251, "[TT] Maximum Acquisition Rate of the STOs and STAEs = 0.1\u00ba/s"]
-[10.0547513961792, 7.904794692993164, "[FF] Full Aperture Blackbody and Space Views of the Telescope = Scan modes Full, normal and programmable sector for quick repetivity"]
-[7.693287372589111, 9.20547866821289, "[TT] Broad-band Window of the ISIR = 7 to 13 \u00b5m"]
-[6.816458702087402, 4.2639384269714355, "[FF] Type of the AIDA = Advanced"]
-[10.318063735961914, 3.8352317810058594, "[TT] Acceleration of the Microgravity Regime = <10-4 g for all directions"]
-[9.655296325683594, 1.386850118637085, "[FF] Mythological Names of the Pleiades = Alcyone, Maia, Electra, Merope, Taygete, Celaeno, and Sterope"]
-[6.975714206695557, 1.6887482404708862, "[FF] Architecture of the Instrument Carrier = Leverages GSFC recent experience with the James Webb Space Telescope ISIM (Integrated Science Instrument Module) structure"]
-[3.473665952682495, -0.8894205093383789, "[TT] Orbit of the MicroMAS-2 = 505 km sun-synchronous type"]
-[9.813425064086914, 8.581244468688965, "[TT] IFOV of the Telescope = 280 \u00b5rad x 280 rad"]
-[10.091012001037598, 1.4219084978103638, "[FF] Purpose of the Gaia = Precisely measuring the distance and movement of more than a billion stars in our galaxy"]
-[10.80489730834961, 7.457500457763672, "[TT] Swath of the AlSat-2A = 17.5 swath"]
-[4.1383056640625, 0.15700751543045044, "[TT] Launch Date of the SpaceX Falcon 9 = Nov. 14"]
-[10.65936279296875, 2.191739082336426, "[TT] Number of Unique X-ray Sources of the 3XMM Catalogue = 372 728"]
-[5.386518478393555, 6.345092296600342, "[TT] Data bus width of the SDR-SMM = 128+16 bit"]
-[10.28356647491455, 6.278391361236572, "[TT] Pulse Rate of the NuSTAR = 1.37 seconds"]
-[7.469152927398682, 0.8657679557800293, "[FF] Mission of the Lunar Flashlight = Exploration Mission 1"]
-[11.837432861328125, 3.4256746768951416, "[FF] Thrust of the IES = Exceeds atmospheric drag"]
-[6.069733142852783, 3.0646579265594482, "[TT] Ticker Symbol of the BlackSky Holdings, Inc. = BKSY.W"]
-[9.132591247558594, -1.190130591392517, "[TT] Orbit of the EDRS-C = Higher than Earth observation satellites"]
-[3.92966365814209, 4.342389106750488, "[FF] Surveillance Capabilities of the RADARSAT-2 = All-weather, day/night persistent surveillance"]
-[6.766994476318359, 1.8148841857910156, "[FF] Mission Concept of the FLuorescence EXplorer = ESA\u2019s Earth Explorer 8"]
-[9.939960479736328, 6.916734218597412, "[TT] False Alarm Rate of the Tool = 2 per 3600 km along-track"]
-[8.369450569152832, 5.458011150360107, "[TT] Localization Accuracy of the TanSat = Better than one pixel"]
-[5.135354995727539, 6.503427982330322, "[FF] Function of the XPWR = Provides the power required for the whole downlink chain"]
-[3.081996440887451, 1.8201340436935425, "[TT] Measurement Interval of the Copernicus Sentinel-6 Poseidon-4 = Every 10 days"]
-[5.482480525970459, 2.7047812938690186, "[TT] Operators of the SAPPHIRE = Students at the USNA (US Naval Academy) and at SCU (Santa Clara University)"]
-[5.751131534576416, 0.7697575688362122, "[FF] Capital Market Day of the Small GEO = February 11, 2009"]
-[5.884188175201416, -0.46399447321891785, "[TT] Mission Duration of the GOCE = More than four years"]
-[6.497914791107178, 4.982037544250488, "[FF] Data Processing Levels of the SMC = N0, N1, N2"]
-[5.96021842956543, -0.7356059551239014, "[TT] Heritage of the LET = More than 14 years of successful operation in space"]
-[8.40333366394043, 4.723550319671631, "[FF] Components of the ADCS = Magnetometers, Solar array sensors, Magnetorquers, Gyroscope"]
-[8.106096267700195, 0.6670717597007751, "[FF] Groundwater Storage Measurement of the GRACE-FO = Wetness Percentile"]
-[4.012896537780762, 7.762143135070801, "[FF] Signal Generation of the Modulators = Generate the corresponding RF (Radio Frequency) signal"]
-[3.046278715133667, 4.460238933563232, "[TT] Resolution of the TerraSAR-X = 3 m or better in stripmap and spotlight mode"]
-[6.46599817276001, 7.590878009796143, "[TT] Data Quantization of the VIS = 12 bit"]
-[11.989097595214844, 6.214542388916016, "[FF] Matter/Antimatter Separation of the AMS-02 PM = Left-positive, right-negative"]
-[9.587315559387207, 0.8373799324035645, "[TT] Maximum Distance from the Sun of the Rosetta = Over 850 million km"]
-[5.176446914672852, 2.4350922107696533, "[TT] Mission Mode of the SST = MNO"]
-[11.531373023986816, 3.453372001647949, "[TT] Propulsion of the DSX = None"]
-[7.728571891784668, 0.538447916507721, "[FF] Measurement of the Lunar IceCube = Completely encompass the broad 3 \u00b5m band resulting from absorption by water in the solid and vapor states"]
-[4.4751057624816895, 7.7817702293396, "[TT] Frequency Range of the VHF-band data transmission = 137-138 MHz"]
-[10.331524848937988, 2.3056256771087646, "[TT] Optics Presentation Date of the Imaging X-ray Polarimetry Explorer = 2017"]
-[7.517117023468018, 5.022134304046631, "[TT] Moving Parts of the LORRI = No"]
-[5.771749496459961, 5.281496047973633, "[FF] Send UDP command packets to LPT over one-way uplink without Mobile IP or a two-way link of the UDP Blind Commanding = Yes"]
-[5.318617820739746, 0.2763442099094391, "[TT] Test Date of the Space-Borne Clock = 1979"]
-[7.762900352478027, 2.9741930961608887, "[FF] Detection Type of the Spaceborne Detection System = Localized carbon dioxide sources"]
-[5.997852802276611, 4.594372749328613, "[FF] Services of the Infrastructure = Network fabric, consolidated storage, database services, enterprise service bus"]
-[6.003621578216553, 5.708214282989502, "[FF] Generation of the Xilinx Zynq Ultrascale+ MPSoC ZU9EG = Latest"]
-[7.7777419090271, 6.637848854064941, "[TT] Time of the Imaging = 25 minutes"]
-[6.963937282562256, 1.7313292026519775, "[FF] URL of the Juno = https://www.nasa.gov/feature/jpl/findings-from-nasas-juno-update-jupiter-water-mystery"]
-[11.236165046691895, 3.3979132175445557, "[FF] Technology of the MARIN = Microelectromechanical systems (MEMS)"]
-[5.41659688949585, 5.334486484527588, "[FF] Technologies Tested of the STRV-1a and -1b = Advanced structural materials, radiation hardened computers, sensors, solar cells, vibration suppression on a cryogenic cooler, measurements of the ion and electron environment, spacecraft charging, and microelectronics"]
-[5.353175640106201, 3.170952558517456, "[TT] Contract Type of the WSF-M = Predominantly fixed price"]
-[13.271988868713379, 5.660421848297119, "[FF] Function of the C2B = Communication with the ground, controls the solar panels, distributes power to the various components, and provides attitude control"]
-[6.0560302734375, -0.5281286835670471, "[TT] In-Orbit Operations Duration of the Alphasat = 7 years"]
-[8.138453483581543, -1.2041321992874146, "[TT] Laser Altimeter of the ICESat-2 = Height Measurement Down to about an inch"]
-[7.002657413482666, 3.8636021614074707, "[FF] URL of the Anti-Coincidence Counter = http://www.srl.utu.fi/AuxDOC/kocharov/ICRC2009/pdf/icrc1064.pdf"]
-[14.688015937805176, 6.6783671379089355, "[TT] Type of the Battery storage = Large"]
-[12.050628662109375, 4.498826503753662, "[TT] Size of the Spacecraft = 2.8 m x 1.98 m x 2.57 m"]
-[8.461161613464355, 8.3534517288208, "[TT] Spectral Resolution of the Observation Instrument = <0.6 nm (point source), <1.2 nm (extended source)"]
-[10.462400436401367, 5.798784255981445, "[TT] Range of the Temperature = -50 to +600\u00baC"]
-[9.528345108032227, 6.775884628295898, "[TT] Z-axis Scan Capability of the Scanner = 20 cm"]
-[5.346235275268555, 0.06478781253099442, "[TT] Retirement Date of the TSX-5 = Late July 2006"]
-[6.996330261230469, 4.107884407043457, "[FF] Unknown of the COIN Collaboration = Unknown"]
-[8.497176170349121, 5.678206443786621, "[FF] Position Determination Accuracy of the XNAV = Expected to be on the order of hundreds of meters"]
-[6.1735382080078125, 4.658286094665527, "[FF] Processor of the SWEM = Coldfire"]
-[7.728978633880615, 8.52137565612793, "[TT] Spectral Sensitivity of the WUPPE = 1400 to 3200 \u00c5"]
-[6.229772090911865, 5.002591133117676, "[FF] Processing of the LMS = Automatic requests received from the MOC"]
-[9.013222694396973, 3.325819730758667, "[FF] Ion Composition of the Plasma Sheet = Mainly H"]
-[5.880160808563232, 0.22382603585720062, "[TT] Launch Date of the PARASOL = 18 Dec 2004"]
-[4.181342601776123, 7.2796149253845215, "[TT] Band of the SES-17 = Ka-band"]
-[6.037433624267578, -0.5764925479888916, "[TT] On-Orbit Duration of the AIM spacecraft = 7 years"]
-[6.038768291473389, 7.136319160461426, "[TT] Data Rate of the Instrument = 883 kbit/s"]
-[13.733685493469238, 3.053518056869507, "[TT] Total Mass of the APIS Device = 120g"]
-[5.75927734375, 0.8795812726020813, "[FF] Publication Date of the G11.2-0.3 = 16 August 2016"]
-[8.177847862243652, 7.419783115386963, "[TT] Detector Type of the Observation Instrument = 2D MCP (solar blind), Csl photocathode, cross-delay-line (XDL) readout, full array size 4096 spectral x 4096 spatial x 256 PHD"]
-[8.980563163757324, 3.0004453659057617, "[FF] Purpose of the PIMS = Measure the plasmas in Europa's ionosphere and Jupiter's magnetosphere"]
-[7.983709335327148, 2.916327953338623, "[FF] Detection Capability of the OMI = Volcano Emissions"]
-[4.8459367752075195, 8.561481475830078, "[TT] Center Frequency of the Channel 3 = 1695.7562 MHz"]
-[10.339981079101562, 2.2602531909942627, "[TT] Energy Range of the Chandra X-ray Observatory = Lower-energy X-rays"]
-[16.561559677124023, 3.6437690258026123, "[TT] Number of Satellites of the OneWeb = 110"]
-[12.051126480102539, 4.975690841674805, "[TT] Volume of the Electronics volume = 320 mm x 210 mm x 150 mm"]
-[10.504758834838867, 1.3801714181900024, "[FF] Infrared Brightness of the TOI 451 = Unusually bright at wavelengths of 12 and 24 micrometers"]
-[7.775381088256836, 2.5397140979766846, "[FF] Fire scar of the Disaster = Using time-differentiation of the slope-corrected HV, fire risk areas will be detected"]
-[14.26085376739502, 3.2187678813934326, "[TT] Mass of the SAOCOM-1B = 3050 kg"]
-[3.1778790950775146, 2.4834392070770264, "[FF] Level-2 Ocean products of the Sentinel-1 = Ocean wind field, swell wave spectra and surface currents information as derived from SAR data"]
-[5.946413993835449, 7.53347110748291, "[TT] Sampling Rate of the TRSR = 10 Hz"]
-[8.719491004943848, 4.677389144897461, "[FF] Components of the OSP = One boresighted fixed-head star tracker and two skewed fixed-head star trackers"]
-[10.621171951293945, 5.050870895385742, "[TT] Proton Suppression Factor of the CuPID Sweeping Magnets and Filter System = 105"]
-[4.571976184844971, 8.14556884765625, "[TT] Center Frequency of the Radar = 1.26 GHz"]
-[8.63764762878418, 5.632551193237305, "[FF] Accuracy Range of the GOCE = 0.002 - 0.03 m"]
-[7.107692718505859, 2.63973331451416, "[FF] Application of the Observation Target = Maritime, Disaster Monitoring, Water Conservancy, Meteorology"]
-[5.547317981719971, 0.8939620852470398, "[TT] NLC Observation Start Date of the AIM spacecraft = May 13, 2013"]
-[9.41888427734375, 5.344162940979004, "[FF] Azimuth Rotation Speed of the Two-axes mechanism = Varies"]
-[5.351531028747559, 3.2317278385162354, "[TT] Platform of the Tsikada = Nadezda (Hope) satellite platform"]
-[3.2316811084747314, 1.6904029846191406, "[TT] Global Coverage Frequency of the Sentinel-2 = Every 10 days with one satellite, every 5 days with two satellites"]
-[3.286547899246216, 2.2556118965148926, "[FF] Ground-level Changes Data Provider of the GRACE-FO = ESA (European Space Agency) Sentinel-1 satellite"]
-[7.533080101013184, -0.6131040453910828, "[FF] Flight Lines of the NASA P-3B aircraft = Proposed during the 2017 Antarctic Field Campaign of Operation IceBridge"]
-[7.1996541023254395, 5.484310626983643, "[FF] Mass Classes of the STAFF/DWP = 1, 4, 12-16, 28-56 amu"]
-[10.958953857421875, 7.381404876708984, "[TT] Swath Width (Reduced Performance) of the Satellite = 550 km"]
-[5.466200351715088, 1.4807950258255005, "[TT] Orbit Maintenance Success Rate of the ALOS-2 = 99.7%"]
-[6.890353202819824, 4.415297985076904, "[FF] Mounting of the iROSA = Plugs into the station\u2019s power channels and rotary joints"]
-[7.069924354553223, 2.4104676246643066, "[FF] Publication Year of the Observation of the Earth and Its Environment = 2002"]
-[6.050069808959961, 1.3865047693252563, "[FF] Re-entry Date of the SENSE Satellites = May 4, 2015"]
-[8.06026840209961, -1.222781777381897, "[FF] Instruments of the IceBridge Aircraft = Elevation-mapping lasers, ice-penetrating radars, optical and infrared cameras, gravimeters, magnetometers"]
-[5.193756103515625, 0.8423744440078735, "[TT] Launch Date of the ASNARO-1 = November 6, 2014"]
-[10.363170623779297, 0.3128952383995056, "[FF] Formation Geometry of the TDX and TSX Satellites = Pursuit Monostatic Far formation"]
-[11.123722076416016, 0.9383782148361206, "[TT] Sky Scanning of the LISA = Continuous"]
-[5.317915439605713, 5.447761058807373, "[FF] Communication Links of the BILGE = 2 ports of 1 Mbit/s CAN bus, 2 ports of 1 Mbit/s MIL-STD-1553B bus, 3 ports of 130 Mbit/s SpaceWire bus, Up to 8 duplex ports of 8 Mbit/s HDLC over opto-isolated or LVDS (Low Voltage Differential Signaling) channels, 3 ports of 25 Mbit/s DATA-CLK-DV raw data over LVDS"]
-[11.57962703704834, 3.457660436630249, "[TT] Propulsion Systems of the MEV-1 = Hybrid chemical and electric"]
-[7.852063179016113, 2.224200963973999, "[FF] Satellite Ocean-Color Data Record of the NASA = Data"]
-[5.704594135284424, 4.21665620803833, "[FF] Purpose of the Hiber-3 smallsat = Provide satellite connectivity to \u201cinternet-of-things\u201d (IOT) devices"]
-[8.852520942687988, 7.149265289306641, "[TT] Imagery Quality of the AlSat-2A = Outstanding"]
-[3.9433906078338623, 3.4327123165130615, "[FF] Data Collection of the Galileo = Flyby of Europa in 2000"]
-[9.763097763061523, 6.937957286834717, "[TT] Geometric Factor of the ELENA = 2 x 10 -5 cm 2 sr"]
-[4.492969512939453, -0.9013708829879761, "[TT] Arrival Date of the Dragon CRS-14 = April 4, 2018"]
-[13.759297370910645, 3.064364433288574, "[TT] Payload Mass of the Ariane 5 = 10,264 kg"]
-[4.632149696350098, 7.923587322235107, "[TT] Frequency of the L-band Transmitter = 1700 MHz"]
-[9.169219970703125, 2.9341187477111816, "[TT] Ripple Amplification of the Solar Dynamics Observatory = Three times"]
-[11.750785827636719, 3.303825855255127, "[TT] Thrusters of the ALTIUS = Four 1N thrusters"]
-[3.474364757537842, 4.8808393478393555, "[TT] Instrument of the Sentinel-1 = C-band SAR (Synthetic Aperture Radar)"]
-[3.958603620529175, 4.225363254547119, "[FF] Information Use of the RADARSAT-2 = Ice monitoring, pollution monitoring, disaster management, agricultural monitoring, forest management"]
-[6.485889434814453, 7.633537292480469, "[TT] Signal Quantization of the Telescope = 10 bit/sample"]
-[7.1312408447265625, 6.491370677947998, "[TT] Number of FPMs of the FPA = 6"]
-[6.590788841247559, 5.139989852905273, "[FF] Architecture of the On-Board Controller Digital ASIC = Unknown"]
-[10.1759614944458, 6.932918548583984, "[TT] Cross-Track Separation of the ANDESITE = 5 km"]
-[6.6702656745910645, 8.751253128051758, "[TT] Polarized Filters of the POLDER = 3"]
-[9.116483688354492, 1.5377591848373413, "[TT] Plasma Instrument of the Voyager 2 = Will provide the first-ever plasma measurements of the interstellar medium"]
-[5.001230716705322, 4.391096591949463, "[TT] Hardware Cost of the Starlink = $499"]
-[6.788186550140381, -0.6417725682258606, "[TT] Responsible Orbit of the JPSS = Afternoon"]
-[14.58676528930664, 6.610876560211182, "[TT] Battery Type of the Power Subsystem = Ni-Cd"]
-[5.483172416687012, 1.8183009624481201, "[FF] Development Status of the ABEX = Unknown"]
-[5.4468560218811035, 5.4427385330200195, "[TT] Software Standard of the OBC = PUS (Packet Utilization Standard)"]
-[10.357503890991211, 3.2080605030059814, "[TT] Payloads of the SLS = 13 CubeSats/Nanosatellites"]
-[10.870184898376465, 0.9685511589050293, "[FF] Brightness of the Red Dwarfs = Much less than our Sun"]
-[4.177665710449219, 2.589177131652832, "[TT] Launch Site of the Sentinel-1C = Guiana Space Center, Europe\u2019s Spaceport in French Guiana"]
-[4.725334167480469, 0.46648508310317993, "[TT] Launch Date of the ARIEL = 2029"]
-[8.204645156860352, -0.672960638999939, "[TT] Rates of Ice Thinning of the Austfonna = Exceeded 25\u2009m/yr"]
-[5.781817436218262, 6.066570281982422, "[TT] Bit Size of the FPGA = 32 bit"]
-[13.395520210266113, 7.3387651443481445, "[TT] Electrical Power of the MHX-2400 = 4.85 W"]
-[2.9013617038726807, 1.9601274728775024, "[FF] Image Capture Dates of the Copernicus Sentinel-2 = 15 October 2021, 24 November 2021, 13 January 2022"]
-[7.661998748779297, 0.24244017899036407, "[TT] Critical Design Review Start Date of the Lucy = Oct. 15"]
-[9.269089698791504, 5.013485431671143, "[TT] Number of Temperature Sensors of the DSX = 63"]
-[6.097784519195557, -0.1946127712726593, "[TT] Expected Extended Lifetime of the Aeolus = Another year"]
-[7.449635028839111, 5.202946662902832, "[FF] Critical Design Review (CDR) of the Instrument = Late 2018"]
-[5.976922035217285, 5.931673049926758, "[TT] Data/Pilot of the E5b-Q = Pilot"]
-[8.309120178222656, 7.929136276245117, "[TT] Detector Size of the SWIR Band = 26 \u00b5m"]
-[9.203587532043457, 3.265376329421997, "[FF] Stray Light Rejection of the Giant Externally-Occulted Solar Coronagraphs = Experimental Developments"]
-[7.143914699554443, 3.8704988956451416, "[FF] Unknown of the ZY-1( 02C) Satellite = Unknown"]
-[6.12687349319458, 0.3248963952064514, "[FF] Ground-Based Test Duration of the Modern ICs = More than 40 days per mode"]
-[6.490564346313477, -0.7677018642425537, "[TT] LTAN of the HY-1D = 13:30 \u00b130 min"]
-[8.702879905700684, -0.6584259867668152, "[TT] Imaging Frequency of the ICEYE = Many times a day"]
-[8.911038398742676, 3.695842981338501, "[FF] DC electric field measurement of the Geotail spacecraft = Unknown"]
-[7.62437105178833, 2.9784858226776123, "[FF] Function of the Radar System = Generate three-dimensional deformation maps of the Earth's surface and calculate topographical changes at volcanoes"]
-[8.360876083374023, 4.0153889656066895, "[TT] Observation Frequency of the Solar Calibration Target = Approximately every two weeks"]
-[7.067684650421143, 3.479018211364746, "[FF] URL of presentation of the PROBA-3 = http://www.sffmt2013.org/PPAbstract/4111pr.pdf"]
-[7.889962673187256, 8.794337272644043, "[TT] Wavelength Range of the SWIR = 1.58 - 2.49 \u03bcm"]
-[6.625722885131836, 0.7178630828857422, "[FF] Article Date of the Herschel = July 1, 2014"]
-[9.63496208190918, 5.008899211883545, "[TT] Wing Status of the AC4-A = Closed"]
-[9.45751953125, 1.5830265283584595, "[TT] Wind Speed of the Massive Stars = Millions of km/hour"]
-[5.588176250457764, 2.692488431930542, "[TT] Funding of the QARMAN = European Space Agency"]
-[5.434460163116455, 1.3211920261383057, "[FF] Workshop Date of the e-st@r program = Oct. 26-27, 2009"]
-[8.983896255493164, 3.246248960494995, "[FF] Measurement Objectives of the Cluster = Study of small-scale plasma structures and current densities"]
-[11.00515365600586, 6.300812721252441, "[TT] Lens Materials of the CIRC = Germanium and chalcogenide glass (GASIR)"]
-[13.56722640991211, 5.904312610626221, "[TT] Solar Array Power of the MicroMAS-2 = Approximately 3 W"]
-[3.9728481769561768, 6.301877498626709, "[FF] Configuration of the SGR-ReSI antenna = Nadir and zenith dual frequency antennas, two L1-only zenith antennas"]
-[4.897176265716553, 7.753763198852539, "[TT] Locking Time of the Carrier Offset Frequency = T0+84 s"]
-[11.239164352416992, 5.905430793762207, "[TT] Material of the Master = Gold"]
-[14.308563232421875, 3.2988743782043457, "[TT] Mass of the VELOX-PII = 1.33 kg"]
-[6.144404411315918, 0.9952571988105774, "[TT] First Light Images Date of the Landsat-9 = October 31"]
-[3.8405253887176514, -1.1627384424209595, "[TT] Observation Point of the eROSITA = L2"]
-[5.26038122177124, 1.9229663610458374, "[TT] Operator of the OrbView-2 = ORBIMAGE"]
-[8.993186950683594, 4.398890495300293, "[TT] Sun Sensors of the S/C = 8"]
-[6.454541206359863, 6.2756667137146, "[FF] Interference Source Characteristics of the SMOS RFI Team = Topology, Power, Behaviour"]
-[6.3815813064575195, 3.410001516342163, "[FF] Purpose of the Automated Transfer Vehicle (ATV) = Provided reliable cargo deliveries to the Space Station"]
-[4.019201278686523, 1.659737229347229, "[FF] Launch Failure Tweet of the Global-9 = The issue occurred shortly after stage two ignition"]
-[10.371915817260742, 7.980844020843506, "[TT] Diameter of the Schmidt-Cassegrain telescope = 13.8 cm"]
-[5.72735595703125, 6.2425665855407715, "[TT] Architecture of the GATE signal generator = Flexible"]
-[13.307548522949219, 6.7449469566345215, "[TT] Wave Energy of the STEREO spacecraft = 2400 megatons of TNT (1022 joule)"]
-[8.549050331115723, 8.803130149841309, "[TT] Slit 2 Material of the MEGS-A = Si"]
-[11.782719612121582, 3.2859036922454834, "[TT] Thrust Range of the CGM = Up to 560 \u00b5N"]
-[6.205371856689453, 4.38932991027832, "[FF] Ordering follow-up of the CSK GS = Allow the FM to keep S-IM informed about the progression of the order"]
-[10.729339599609375, 3.5241620540618896, "[TT] CubeSat Size of the InflateSail = 3U"]
-[10.000391960144043, -0.5152629613876343, "[FF] Altitude of the MySat-1 = 300 km"]
-[7.710629940032959, 5.309796333312988, "[FF] Acoustic Test of the BepiColombo = 12 June 2017"]
-[7.620624542236328, 4.300384521484375, "[FF] Light Tightness of the Chassis = Three-bounce"]
-[7.849491596221924, 2.073819398880005, "[FF] Map of Surface Gravity and Earthquakes of the SeaSat = Data"]
-[8.062192916870117, 3.2050743103027344, "[FF] Objective of the TANSO-FTS-2 = Measure the density of greenhouse gases in the atmosphere"]
-[13.410094261169434, 6.704551696777344, "[TT] Required Power at EOL of the KOMPSAT-6 = 2,250 W"]
-[4.905703544616699, -0.6044705510139465, "[FF] Operation Period of the SLATS = From launch to the end of initial operation (March 2018)"]
-[8.650949478149414, 7.113107204437256, "[FF] L1 Detectors Purpose of the HIT = Sensitive to electrons"]
-[5.197615146636963, 7.011470794677734, "[TT] Data Rates of the Downlink = 1.024 to 1048.576 kbit/s"]
-[9.673356056213379, 1.8705546855926514, "[FF] Additional Evidence Gathering of the Hubble Space Telescope = A few years later"]
-[10.883737564086914, 4.9996843338012695, "[TT] Measured optical cross-section of the LARES-2 = 2.7 x 10^6 m^2"]
-[8.273932456970215, 9.058229446411133, "[FF] Wavelengths of the NGC 7538 = 70 \u00b5m (blue), 160 \u00b5m (green) and 250 \u00b5m (red)"]
-[4.759133338928223, -0.02294975332915783, "[TT] End of Life Date of the PW-Sat = October 28, 2014"]
-[13.557945251464844, 5.68335485458374, "[TT] Deployable Solar Array Power of the UK-DMC-2 = 65 W at AM0 and 28\u00baC"]
-[5.8693389892578125, -0.48635637760162354, "[TT] In-Orbit Nominal Lifetime of the MWI Instrument = 7.5 years"]
-[11.935649871826172, 6.687022686004639, "[TT] Incoming Energy Range of the INMS = 0-50 eV"]
-[11.800568580627441, 0.049997713416814804, "[TT] Number of Stars Monitored of the TESS = More than 200,000"]
-[4.476892471313477, 7.749640941619873, "[TT] Frequency Bands of the ELT (Emergency Locator Transmitter) = 121.5 MHz, 406.025 MHz"]
-[5.918370723724365, -0.4505538046360016, "[TT] Mission Duration of the TSIS-1 = Five years"]
-[3.7851004600524902, 4.496430397033691, "[FF] Daily SAR Imaging Requirement of the RADARSAT-2 = All required daily SAR imaging"]
-[5.116482257843018, 3.2549538612365723, "[FF] Manufacturer of the CesiumAstro = Full-scale manufacturer advancing airborne and next-generation aerospace platforms"]
-[10.349839210510254, 5.386491298675537, "[TT] Thermal Control of the DMAC = Active"]
-[7.984846591949463, 8.29598617553711, "[FF] Advantage of the FTHSI = Can record the full spectra without any time delay and can decouple the spatial and spectral signatures"]
-[5.470626354217529, 5.074661731719971, "[TT] Interface of the RM = CAN bus"]
-[13.385371208190918, 6.82667350769043, "[TT] Power of the Spacecraft = 350 W"]
-[9.407681465148926, 6.367808818817139, "[TT] Scanning Geometry of the AGRI = Two-axis"]
-[13.601205825805664, 6.780038833618164, "[FF] EPS Board of the MinXSS = Unknown"]
-[5.542403697967529, 3.4502153396606445, "[FF] Platform Bus Supplier of the Blue Canyon Technologies = Unknown"]
-[14.367924690246582, 3.3025269508361816, "[TT] Mass of the SRMSat = 10.9 kg"]
-[5.734384536743164, 3.960331916809082, "[TT] Bus Type of the F-15 and F-16 DMSP satellites = Block 5D-3"]
-[6.55363130569458, -0.013675583526492119, "[TT] Revisit Period of the Constellation = 24 hours"]
-[6.2583231925964355, -0.3590964376926422, "[TT] Operation Period of the Remote Agent = Three days"]
-[7.317492485046387, 2.128539562225342, "[FF] Data Availability of the Carbon Mapper = Freely available"]
-[14.00117301940918, 7.152092456817627, "[TT] Voltage of the 60V link = 60V"]
-[13.469087600708008, 2.8178324699401855, "[TT] Dry Mass of the Spacecraft = 1400 kg"]
-[9.874429702758789, 2.705117702484131, "[TT] Small Satellite Deployment Count of the NanoRacks = 228"]
-[5.579935073852539, 5.735366344451904, "[TT] CPU of the C&DHS = 32 bit RISC, MPU (SH4)"]
-[9.52367877960205, -0.4682864546775818, "[TT] Mean Altitude of the MEO Constellation = 23616 km"]
-[4.552519798278809, 7.502523899078369, "[TT] Gain of the Uplink Receiver = > 40 dB"]
-[6.415066242218018, 4.776821136474609, "[FF] Function of the ISSAC SOC = Uplink image acquisition and other ISSAC operational commands to the ISSAC payload software"]
-[6.014222145080566, 5.515317440032959, "[TT] Redundancy of the C&DH Subsystem = One OBC is redundant, two TMC are redundant"]
-[5.859902381896973, 3.0156118869781494, "[TT] Amortized unit cost of the Legion = $100 million"]
-[5.267617225646973, 1.0136955976486206, "[FF] Mission Date of the LCROSS = May 31-June 4, 2010"]
-[4.761862754821777, -0.27630501985549927, "[TT] Launch Time of the Falcon 9 rocket = 06:17 Pacific Time (14:17 UTC) on 22 February 2018"]
-[7.137322902679443, 6.600924491882324, "[TT] Detection Threshold of the GLM = Low"]
-[6.643199443817139, -0.5016546249389648, "[FF] Expected Orbit Duration of the Solar Array = Several months"]
-[8.1325101852417, -1.0310909748077393, "[FF] Purpose of the Gravimeter = Map the seafloor underneath the ice shelves"]
-[10.746441841125488, 3.2701659202575684, "[FF] Technology of the Micro-gravity experiment = Important for developing the methods of space crystal material growth"]
-[9.146682739257812, 7.476843357086182, "[TT] Imagery Collection of the Satellogic = 10 times as much imagery"]
-[5.120507717132568, -0.8432825803756714, "[TT] Berth Duration of the Kounotori = Until November"]
-[7.200082778930664, 7.521007537841797, "[TT] Radiometric Resolution of the OLI-2 = 14-bit"]
-[8.882773399353027, 0.6942166686058044, "[TT] Descent Path Length of the Lander = 450 km"]
-[7.283707141876221, 8.1527099609375, "[TT] Sensitivity of the Channel 3 = 0.3 K/pixel"]
-[10.820690155029297, 1.395995855331421, "[TT] Mass of the MAXI J1820+070 = About eight times that of the Sun"]
-[9.463168144226074, 3.8151838779449463, "[FF] Unknown of the Billingsley magnetometer = Unknown"]
-[11.150529861450195, 4.988692760467529, "[TT] Radius of the LARES-2 = 212 mm"]
-[11.529436111450195, 4.985411167144775, "[TT] Diameter of the Torus/Strut Structures = 61 cm and 46 cm"]
-[7.163546562194824, 2.833322048187256, "[FF] Data Combination of the IMBIE = Data from 13 NASA and ESA missions"]
-[14.29067325592041, 3.306375503540039, "[TT] Mass of the See Me = ~22 kg"]
-[11.85608959197998, -0.1935044825077057, "[FF] URL of the TESS = https://www.nasa.gov/feature/goddard/2019/nasa-s-tess-mission-spots-its-1st-star-shredding-black-hole"]
-[1.7164963483810425, 6.144287586212158, "[FF] Composition of the Universe = ~68% dark energy, ~27% dark matter, ~5% normal matter"]
-[4.66330099105835, 0.7915008068084717, "[TT] Launch Date of the PROBA-3 = Late 2020"]
-[11.679973602294922, 6.720322608947754, "[TT] Sensitive Range of the XRD = 15 keV \u2013 1 MeV"]
-[5.453960418701172, 6.214539527893066, "[TT] Capacity of the Platform memory = 2 MByte per computer"]
-[9.16756820678711, 4.527733325958252, "[FF] Attitude Control Subsystem of the TUBSAT-N = CCD star sensor, 3-D magnetic compass, two magnetic coils, reaction wheel"]
-[8.655891418457031, 2.071563959121704, "[FF] Potential Impact of the SXS = Revolutionizing our understanding by determining the launch radius of these winds"]
-[4.379600524902344, 7.098819255828857, "[FF] Function of the Ka-band payload = Receive, switch, amplify and transmit microwave signals"]
-[10.632990837097168, 8.881338119506836, "[TT] Pixel Size of the Channel 2 = 32 x 32 km"]
-[7.3394975662231445, 3.725217819213867, "[FF] Radio Occultation Payload of the Sentinel-6 = GPS and GLONASS satellites"]
-[7.152198791503906, 1.2904651165008545, "[FF] URL of the ExoMars Trace Gas Orbiter = http://exploration.esa.int/mars/46124-mission-overview/"]
-[6.581844329833984, 4.945358753204346, "[FF] Design of the GPSP = Blackjack"]
-[9.347291946411133, 7.661487579345703, "[TT] Dimensions of the ShadowCam = 118 cm long and 27 cm in diameter"]
-[8.738426208496094, 7.951103210449219, "[FF] Intermediate Mandrel (IM) of the Optic = Unknown"]
-[12.113877296447754, 7.625102519989014, "[TT] Mass of the 4-band CCD Imager = 15 kg"]
-[6.114951133728027, 7.327375411987305, "[TT] Sample Rate of the Acceleration = 125 Hz"]
-[9.386977195739746, 5.522069454193115, "[TT] Latitude Range for Surface Target Detection of the TanSat = -43\u00b0 to 46\u00b0"]
-[7.098587989807129, 3.759866952896118, "[FF] Formation Flying of the ASPIICS/PROBA-3 = Yes"]
-[5.480670928955078, -0.5744104981422424, "[TT] Scheduled Work Resume Date of the Yutu-2 = March 10"]
-[7.524639129638672, 7.204354763031006, "[TT] Frame Rate of the Hyperion = 225 Hz"]
-[6.334592819213867, 4.679668426513672, "[FF] Operational Goals of the ISERV = Reduce the amount of time required for each step"]
-[4.764702796936035, 0.39725959300994873, "[TT] Launch Date of the STREAK = Sept. 23, 2005"]
-[14.611420631408691, 6.602903366088867, "[TT] Provider of the Lithium Polymer battery = ASP Equipment GmbH"]
-[8.974418640136719, 4.519236087799072, "[TT] Quantity of the Adcole sun sensors = 3"]
-[4.3582048416137695, 0.09859605878591537, "[FF] Public Beta Test Plan of the Starlink = Before the end of the year"]
-[10.384598731994629, 5.399616241455078, "[TT] Type of the Passive heaters = Passive"]
-[6.131157398223877, 3.119626998901367, "[TT] Gross Proceeds of the BlackSky Holdings, Inc. = $283 million"]
-[5.5768256187438965, 2.454000473022461, "[FF] Number of Islands of the LAPAN-A3/IPB = More than 17,500 islands"]
-[7.409300327301025, 2.3042027950286865, "[TT] Global Coverage of the Infrared Bands = 2 Days"]
-[9.348725318908691, -1.6927849054336548, "[TT] Spatial Resolution of the Swarm = About 2000 km"]
-[6.826900005340576, 3.167179584503174, "[FF] Service Provision of the MetOp program = Continuous broadcast of its meteorological data to the worldwide user community"]
-[8.364659309387207, 2.435053825378418, "[FF] Authors of the Aerosol Polarimetry Sensor = Richard J. Peralta, Carl Nardell, Brian Cairns, Edgar E. Russell, Larry D. Travis, Michael I. Mishchenko, Bryan A. Fafaul, Ronald J. Hooker"]
-[5.721919059753418, -0.29160642623901367, "[TT] Deployment Duration of the RBA = Within 40 minutes"]
-[7.408679962158203, 3.8833491802215576, "[TT] Function of the Satellite = Performs radio occultation (RO)"]
-[5.365335464477539, 1.1318962574005127, "[FF] Presentation Date of the ASIM = Jan. 21, 2009"]
-[9.005197525024414, 5.313596248626709, "[FF] Pointing Ability of the ASTERIA = Two-stage fine pointing control"]
-[8.471714973449707, 8.053633689880371, "[TT] Resolution of the IR Systems = 7\u201314 \u00b5m"]
-[9.007975578308105, 7.421103477478027, "[TT] Image Size of the NAVCAM = 866 x 866 m"]
-[6.933752059936523, 7.125135898590088, "[TT] PRF of the Laser = 10 kHz"]
-[5.524014949798584, 2.529507637023926, "[FF] Population of the Dhaka = Unknown"]
-[4.658902168273926, 0.6359067559242249, "[TT] Launch Date of the GOES\u20107 = Feb. 26, 1987"]
-[5.728569984436035, 2.716362476348877, "[FF] Affiliated Organizations of the MANTIS = ESA, UK Space Agency, Open Cosmos, Satlantis, Terrabotics"]
-[12.09238338470459, 6.007917881011963, "[FF] Authors of the Cosmic Ray Isotope Spectrometer = E. C. Stone, C. M. S. Cohen,W. R. Cook, A. C. Cummings, B. Gauld, B. Kecman, R. A. Leske, R. A. Mewaldt, M. R. Thayer, B. L. Dougherty, R. L. Grumm, B. D. Milliken, R. G. Radocinski , M. E. Wiedenbeck, E. R. Christian, S. Shuman, H. Trexel, T. T. von Rosenvinge, W. R. Binns, D. J. Crary, P. Dowkontt, J. Epstein, P. L. Hink, J. Klarmann, M. Lijowski, M. A. Olevitch"]
-[8.38308334350586, 2.1474380493164062, "[FF] Geophysical Evaluation of the SeaSat-A Satellite Scatterometer = Remotely Sensed Wind Vectors Over the Ocean"]
-[4.005500316619873, 2.1816303730010986, "[TT] Launch Vehicle of the Deployment Systems = Dnepr-1"]
-[5.216277599334717, 5.631077289581299, "[FF] Objective of the ECSE = Demonstrate a prototype secure CCSDS packet TM/TC system in an operational environment"]
-[5.692176342010498, 5.7944135665893555, "[TT] Number of Processors of the QC40 = 4"]
-[7.161761283874512, 8.392056465148926, "[TT] Revolution Count of the Filter Wheel = 1216"]
-[9.060036659240723, 0.5278170108795166, "[FF] Mission of the ARTEMIS = Transfer of P1 and P2 from Earth orbits to lunar orbits"]
-[9.228212356567383, 5.554760932922363, "[FF] Principle-plane Nadir Observation of the Satellite = Scanning the ground targets with the instrument boresight within 5\u00ba of the principal plane"]
-[7.750797748565674, 6.910113334655762, "[TT] Deployment Time of the NETCAM = Approximately 100 s"]
-[5.36674690246582, 7.05881929397583, "[TT] Data Packet Loss Rate of the Analog-1 = 1%"]
-[11.6954927444458, 4.689463138580322, "[TT] Height of the Canister = 38 cm"]
-[6.72776985168457, 5.92681884765625, "[TT] Quantity of the NODES = 2"]
-[6.879265308380127, -0.6585206389427185, "[TT] Orbital Period of the Thuban = 51.4 days"]
-[5.460737228393555, -0.5595348477363586, "[TT] Malfunction Date of the Yutu = March 3, 2014"]
-[13.403412818908691, 2.886002779006958, "[TT] Mass of the NEXTSat-1 = ~100 kg"]
-[3.48087739944458, 6.41256046295166, "[TT] Antenna Systems Length of the DRS = 7.5 m"]
-[10.7987642288208, 2.068704843521118, "[FF] Follow-up Studies Date of the XMM-Newton observatory = Unknown"]
-[13.85132884979248, 2.954803943634033, "[FF] Unknown of the Reference Mass = Material that will not degrade in a LEO"]
-[8.667814254760742, 4.884066104888916, "[FF] Capabilities of the Procyon star tracker = Excellent rate estimates, \u2018lost in space' capability"]
-[8.264443397521973, 4.082371234893799, "[FF] Objective of the NINA-2 = Measure fluxes of charged particles, in particular to detect cosmic ray nuclei of galactic, solar, or other origin from hydrogen to iron, between 10 and 200 MeV/n (contained particles) and 1 GeV/n (outside containment)"]
-[6.240800857543945, -0.5601604580879211, "[TT] Orbit Maintenance Capabilities of the PACE = 10 years"]
-[5.481805801391602, 6.570580959320068, "[TT] Data Collection Capacity of the Gaia = 100 TB"]
-[10.20566177368164, 8.187955856323242, "[TT] Entrance Aperture Location of the INMS = +Y 2U face"]
-[3.9040887355804443, 4.68910551071167, "[FF] Design Basis of the NRD = Experimental terrestrial navigation radar detector systems developed by FFI"]
-[7.151651859283447, 1.3608272075653076, "[FF] Observation Type of the Spitzer = Eddington Flare from Blazar OJ 287"]
-[5.406183242797852, 2.731851100921631, "[TT] Operator of the INSAT-3DR = ISRO (Indian Space Research Organisation)"]
-[5.21215295791626, 3.1457908153533936, "[TT] Contract Value of the Thales Alenia Space = \u20ac482 million"]
-[4.215872764587402, 4.292900085449219, "[FF] Document of the COSPAS-SARSAT LEOSAR System = C/S T.003, Issue 4, Oct.. 2008"]
-[5.175304889678955, 1.2047115564346313, "[FF] Calibration Conference Date of the GOMS = March 15\u201319, 1999"]
-[9.82117748260498, 3.7527496814727783, "[TT] Mounting of the Magnetometer = Opposite side of the spacecraft from the X-ray telescope's optics"]
-[8.666938781738281, -0.639914333820343, "[TT] Processing Format of the ICEYE-X1 = GeoTIFF"]
-[8.88143253326416, 7.288838863372803, "[TT] Optical Payloads of the CBERS-4A = Operating in the visible spectrum with resolutions in the range of 2 to 60 meters"]
-[5.505147457122803, 0.6903359293937683, "[TT] Release Date of the SCI = April 5"]
-[9.243756294250488, 2.650562286376953, "[FF] Observation Type of the RHESSI = Flare"]
-[9.372346878051758, -1.7086427211761475, "[TT] Altitude Difference of the Swarm-A and Swarm-C = Less than 5 km"]
-[3.9727113246917725, 9.678894996643066, "[TT] Frequency (GHz) of the ICI-5 = 325.15\u00b19.5"]
-[9.222585678100586, 2.881915330886841, "[FF] Goal of the RHESSI = Investigating particle acceleration and energy release in solar flares"]
-[9.495405197143555, 6.7250847816467285, "[TT] Azimuth Resolution of the Wide multi-look fine = 4.6-7.6 m"]
-[9.472590446472168, 5.404725551605225, "[TT] Maximum Slew Rate of the TanSat = 0.6\u00b0/s"]
-[9.002686500549316, 5.369722843170166, "[FF] Requirement of the Focus Mechanism = Independent feedback on movement"]
-[9.538331985473633, 0.9580249190330505, "[TT] Relative Speed of the EDRS-A = Up to 28,000 km per hour"]
-[13.317387580871582, 7.114255428314209, "[TT] Peaks of the Payload Power = 180 W"]
-[5.311268329620361, 0.9009336829185486, "[TT] Launch Date of the BioSentinel = Second half of 2021"]
-[8.101844787597656, 5.675020217895508, "[TT] Calibration Cycle of the LISS-3 camera = 2048 scan lines"]
-[14.065752983093262, 2.9901247024536133, "[TT] Mass Budget of the ALBus = Under 4 kg"]
-[8.281096458435059, 7.135566234588623, "[FF] Attachment Optimization of the Supervision Cameras = Provide the best possible view of all of the demonstrations"]
-[12.177632331848145, 3.0797841548919678, "[FF] Presentation Date of the A Stable Liquid Mono-Propellant based on ADN = May 11-14, 2009"]
-[6.55690860748291, 1.7417141199111938, "[FF] Workshop Date of the Skybox Imaging = March 26-28, 2014"]
-[8.434920310974121, 8.06804084777832, "[TT] Total Number of Pixels of the MS Bands = 7,500"]
-[14.348599433898926, 3.086575984954834, "[TT] Mass of the ICEYE-X2 = ~ 80 kg"]
-[5.8719964027404785, 6.215326309204102, "[TT] Memory Boards Capacity of the SSR = 50 Gbit"]
-[4.513794422149658, 1.6205511093139648, "[TT] Flight Experiment Date of the TUBSAT = Sept. 25-29, 2006"]
-[8.255048751831055, 4.494142532348633, "[FF] Mission Objective of the LARES-2 = Look for subtle distortions in spacetime caused by Earth's own mass"]
-[10.521005630493164, 3.1151585578918457, "[FF] Purpose of the KMSL smallsat = Experiments in microgravity"]
-[6.796357154846191, 5.75364351272583, "[TT] Number of Non-Separating Components of the ORS-3 = 2"]
-[9.761821746826172, 6.441255569458008, "[FF] Function of the Steering Mirror = Optimizes the interferometer contrast in the receive path as well as the transmit beam pointing"]
-[5.27065896987915, 5.377355575561523, "[FF] Technologies of the IXV Communications Network = Serial leased lines, Ethernet lines, ISDN, IP Satellite Networks"]
-[7.584835529327393, -2.4644672870635986, "[FF] Data Release Date of the GOLD = 12 March 2019"]
-[9.397211074829102, 7.3701019287109375, "[TT] Spatial Resolution of the AVNIR = 8 m (PAN Band), 16 m (MS Band)"]
-[8.922173500061035, 5.624453067779541, "[TT] Pointing Requirement of the FIPEX sensor = Along the velocity vector to within 10 degrees"]
-[6.160811901092529, 3.529855251312256, "[TT] Number of Experiments of the SEM-14 = 10"]
-[7.979720115661621, -0.3566679060459137, "[FF] Decline Start Date of the Arctic Sea Ice = 4 February 2020"]
-[6.886551380157471, 9.066856384277344, "[TT] Band Center of the POLDER-1/2 = 444.5 P nm"]
-[8.930158615112305, 9.429821968078613, "[TT] Cross-track Coverage of the TANSO-FTS-2 = \u00b135\u00b0"]
-[13.077241897583008, 3.0024054050445557, "[TT] Propellant Mass of the Satellite = \u2264 80 kg"]
-[11.070819854736328, 1.519286036491394, "[TT] Structure Diameter of the Starshine-3 = 94 cm"]
-[3.6678056716918945, 4.685204982757568, "[TT] Sensor Module of the RADARSAT-2 = C-band SAR (Synthetic Aperture Radar) imager"]
-[6.23751163482666, 8.007593154907227, "[TT] Number of Channels of the RF D/L channels = 4"]
-[3.2500813007354736, 2.2463462352752686, "[FF] Service Provision of the EDRS = Copernicus program"]
-[12.214835166931152, 4.555253982543945, "[TT] Bus Size of the Spacecraft = 1.4 m x 1.4 m x 2 m"]
-[4.211565971374512, 6.410261154174805, "[TT] Use of the Turnstile antennas = Communications with the spacecraft bus"]
-[9.921966552734375, 8.95506763458252, "[TT] IGFOV of the WV channel = 224 \u00b5rad"]
-[9.433428764343262, -0.6350950002670288, "[TT] Orbit of the AVUM = Final Orbit (1450 km x 1450 km, i=69.5\u00ba)"]
-[9.24634838104248, 6.152058124542236, "[TT] Scanning Beams of the OSCAT-3 = 2 conical scanning beams"]
-[8.001176834106445, 8.443316459655762, "[TT] Waveband of the CO2Image = Shortwave infrared (SWIR): 1100 nm - 3000 nm"]
-[12.774805068969727, 7.61913537979126, "[TT] Power of the Instrument = 20 W operating, 120 W during cold calibration"]
-[7.425961017608643, 2.373476982116699, "[TT] Sampling of the Satellite = Excellent sampling of one region of the globe"]
-[8.922189712524414, 4.280404567718506, "[FF] Presentation Location of the Micro Digital Sun Sensor = Banff, Alberta, Canada"]
-[9.569418907165527, -1.6870025396347046, "[TT] Inclination of the Swarm-B = 87.75\u00ba"]
-[6.06458854675293, -1.9595054388046265, "[TT] Member of the Jennifer Comstock = True"]
-[7.017415523529053, 0.8033974170684814, "[FF] Mission Update of the Gravity Probe B = Sept. 26, 2008"]
-[9.316701889038086, 2.460378646850586, "[FF] Type of the FIREBIRD-2 A and B = Focused Investigations of Relativistic Electron Burst Intensity, Range, and Dynamics"]
-[7.658924579620361, 7.368244647979736, "[TT] Sampling Rate of the HSC-1700 = 30 frames/s"]
-[5.459656238555908, 0.1225416511297226, "[TT] Operation Start Date of the RAIDS = June 2010"]
-[4.6922478675842285, 7.997950553894043, "[TT] Modulation Frequencies of the CCRR = 500 MHz, 100 MHz, 0.5 MHz"]
-[2.919128894805908, 1.9671845436096191, "[TT] Image Capture Date of the Copernicus Sentinel-2 = 13 August 2021"]
-[10.737516403198242, -1.1422359943389893, "[TT] IOC Operation Period Altitude of the SLATS = 250 km"]
-[8.353414535522461, 3.734786033630371, "[FF] Purpose of the RAVAN = Measure Earth outgoing radiation"]
-[3.095604658126831, 2.2884178161621094, "[FF] Range of Spectral Bands of the Copernicus Sentinel-2 = Unknown"]
-[5.653207778930664, 7.103404521942139, "[TT] Data Rates of the CDL = Up to 274 Mbit/s"]
-[5.499808311462402, 0.5285891890525818, "[FF] Development Date of the HEFT and NuSTAR = 2005"]
-[3.4534671306610107, -0.9257206320762634, "[TT] Orbit Type of the Satellite = Sun-synchronous near-circular polar orbit"]
-[7.55153751373291, 6.749368667602539, "[TT] Integration Time of the Photometric Observations = 60 seconds"]
-[6.976973056793213, 4.082019329071045, "[FF] Unknown of the Anticoincidence Counter = Unknown"]
-[7.3605828285217285, -0.06680971384048462, "[TT] Orbits Completed of the Gokturk-2 = 5344"]
-[7.777409553527832, 9.424633026123047, "[TT] Band Center Wave of the M3 = 0.488 \u00b5m"]
-[12.195566177368164, 3.8501687049865723, "[TT] Volume of the PHM = 28 liters"]
-[7.875378131866455, 7.654606342315674, "[FF] Technology Demonstration Mission of the TAIKI = Hyperspectral imaging, experimental high-rate optical (laser) data transmissions"]
-[5.126672744750977, 2.3006091117858887, "[TT] Deployment Status of the PhoneSat 2.5 = Successful"]
-[7.657052040100098, -0.8698610067367554, "[TT] Mission Critical Design Review Date of the ICESat-2 = February 18, 2014"]
-[7.081119060516357, 5.839076519012451, "[TT] Clock Frequency Stability of the Spacecraft = PHM (Passive Hydrogen Maser):<4.5 x 10 -14  at 30000 s"]
-[8.383454322814941, 7.669033050537109, "[TT] Detector Array Elements of the IRIS Instrument = 5000 active elements"]
-[7.19838809967041, 7.129169464111328, "[TT] Number of Beams for Standard Imaging Mode of the COSI = 31"]
-[8.620853424072266, 8.757692337036133, "[TT] Design of the Atmospheric-sounding instrument = Dispersive spectrometer, using a reflexive grating for spectral bands dispersion"]
-[3.3764612674713135, 6.406210422515869, "[TT] High-Gain Dish Diameter of the TGO = 2.2 m"]
-[12.146383285522461, 3.0576953887939453, "[TT] Propellant of the SVM = Hydrazine and Cold Gas"]
-[4.410144805908203, 2.4365711212158203, "[TT] Launch Site of the ADEOS-II = TNSC (Tanegashima Space Center), Japan"]
-[8.170839309692383, -0.716393768787384, "[FF] Objective of the CRISTAL = Simultaneously monitor snow depth and sea-ice thickness change over the Arctic"]
-[7.543624401092529, 5.409223556518555, "[FF] Components of the EOS = Telescope, FPA (Focal Plane Assembly), SPM (Signal Processing Module)"]
-[7.97092342376709, 7.28380012512207, "[TT] FOV of the FTS Interferometer = 1.25 mrad"]
-[10.815220832824707, 5.9243268966674805, "[TT] Extension Above Detector of the CsI(Na) Shield = 20 cm"]
-[5.454259395599365, 6.734469413757324, "[TT] Data Relay Capacity of the SpaceDataHighway = 40 terabytes per day"]
-[12.73242473602295, 3.8993842601776123, "[FF] Spatially Localized of the Reconnection Regions = True"]
-[9.406582832336426, 5.318387031555176, "[FF] Bearing Assemblies Configurations of the Central Bulkhead Assembly = 2 and 3 degree-of constraint"]
-[10.355310440063477, 5.144954204559326, "[FF] Purpose of the Sunshield Panels = Passive Radiant Cooler"]
-[7.930777549743652, 5.074974060058594, "[FF] Geometric Error Types of the PROBA-V Mission = Absolute, inter-band and multi-temporal"]
-[3.362633466720581, 5.290309906005859, "[TT] Boom Length of the L-band SAR instrument = 9-m"]
-[7.4966559410095215, 2.352797269821167, "[FF] Temporal Resolution of the FY-4A = China area < 1 hr, Mesoscale area < \u00bd hr"]
-[5.619046211242676, 7.096174716949463, "[TT] Data Stream Speed of the Suomi-NPP = 15 Mbit/s"]
-[4.29525089263916, 2.217827558517456, "[TT] Contractor of the NigeriaSat-2 = National Space Research and Development Agency (NASRDA) of Nigeria"]
-[6.444033145904541, 0.6284996271133423, "[FF] Launch Date of the Landsat 9 = Unknown"]
-[8.865111351013184, 6.232203006744385, "[FF] Antenna Scan Rate of the Instrument = 40 rpm (1.5 s/scan)"]
-[7.600107669830322, 5.807831287384033, "[FF] Operation Power Level of the Scanning LIDAR = Not operated at its highest power-level"]
-[8.53151798248291, 6.1630754470825195, "[FF] ToA Measurements of the TRUTHS = SI-traceable ToA measurements"]
-[10.666873931884766, 2.8087446689605713, "[FF] Mission Status of the Tsubame microsatellite = Stopped receiving uplink commands"]
-[6.470857620239258, -0.02147587575018406, "[TT] Monitoring Frequency of the SMAP = Every two days"]
-[6.242781162261963, 1.6108098030090332, "[FF] Publication Date of the Shuttle Radar Topography Mission = 2003"]
-[14.036694526672363, 3.1822688579559326, "[TT] Cion Mass of the CICERO-6 = 1.2 kg"]
-[9.721905708312988, 7.090704917907715, "[TT] Along-Track Resolution of the MLS = 500 km"]
-[5.184471607208252, 6.030949592590332, "[TT] Data Links of the OBC = ESA standard SpaceWire connections"]
-[8.684527397155762, 7.670957088470459, "[TT] Detector Size of the Color Imager = 1280 x 1024 pixels"]
-[7.566901206970215, -0.9061406254768372, "[TT] Retirement of the Delta II = After ICESat-2 launch"]
-[10.281322479248047, 5.76211404800415, "[TT] Measurement Duration of the Temperature = 420 s"]
-[13.749635696411133, 2.890720844268799, "[TT] Mass of the Spacecraft = ~165 kg"]
-[10.391841888427734, 4.497548580169678, "[TT] Number of Wheels of the Yutu 2 = 6"]
-[6.875952243804932, -0.7042568325996399, "[TT] Orbital Period of the ZTF J1539+5027 = 7 minutes"]
-[9.328292846679688, 5.054647922515869, "[TT] Attitude Determination Accuracy of the AOCS = \u2264 0.2\u00ba (3\u03c3)"]
-[6.001150608062744, 1.5631568431854248, "[FF] Conference Date of the Operationally Responsive Space = August 8-13, 2015"]
-[4.016922950744629, 3.5117740631103516, "[FF] Deployment Framework of the Galileo = FOC (Full Operational Capability)"]
-[7.800172805786133, 8.32989501953125, "[TT] Measurement Spectral Region of the Sounder Instrument = 4-5 \u00b5m"]
-[8.430604934692383, 7.649898052215576, "[TT] Pixel Size of the HSC-III = 10.8 \u00b5m"]
-[9.675152778625488, 4.1692728996276855, "[TT] Quantity of the Magnetic Field Sensor = 5"]
-[8.075968742370605, 8.70086669921875, "[TT] Measurement Range of the OCI = Ultraviolet to the shortwave infrared"]
-[11.581311225891113, 3.212773561477661, "[TT] Lifetime of the Kiku-8 ion thruster = 16,000 hours"]
-[8.41682243347168, 3.208672523498535, "[FF] Parameter Measured of the Ozone Mapping Profiler Suite = Ozone"]
-[4.920644283294678, 7.336122035980225, "[TT] Uplink Rate of the RF communications system = 125 bit/s"]
-[18.79905128479004, 3.479288339614868, "[TT] Mean \u0394E (m) of the Bandari = 1.8"]
-[9.989109992980957, 4.521418571472168, "[TT] Magnetic Flux Density of the Cryomag = 0.86 TeV"]
-[5.7497992515563965, 7.93522310256958, "[FF] Performance Degradation of the Channelizer = Small enough for a useful disaster support"]
-[7.749866485595703, 1.9243643283843994, "[FF] Characterized Processes of the Models of the Oceans and Land Biosphere = Photosynthesis, respiration, nutrient uptake and transport, fire, and chemical cycling, as well as fossil fuel inventories"]
-[10.486660957336426, 1.7377192974090576, "[TT] Luminosity of the \"pulsars\" = Much fainter than ULXs"]
-[4.148754596710205, 6.990556240081787, "[TT] LGA (Low Gain patch Antennas) of the S/C Communication Subsystem = 4"]
-[5.596457481384277, 1.0015894174575806, "[TT] Removal Date of the Heat Shield = Feb. 27, 2015"]
-[5.067842483520508, 4.431161403656006, "[TT] Number of Deorbited Relay Stations of the Starlink = 3"]
-[9.988058090209961, -0.37285116314888, "[TT] Altitude Usage of the IES (Ion Engine System) = Above 220 km"]
-[4.215812683105469, 4.588852882385254, "[FF] Services of the SAR/Galileo = FLS (Forward Link Service), RLS (Return Link Service)"]
-[7.822154521942139, 8.716035842895508, "[TT] Spectral Bands of the EXI = 205-234 nm, 245-275 nm, 305-335 nm, 405-469 nm, 506-586 nm and 625-645 nm"]
-[5.312962055206299, 6.995274543762207, "[TT] Speed of the Internet Connection = At least 25 Mbit/s"]
-[8.315847396850586, 7.653453350067139, "[TT] Detector Type of the SIS (Scanning Imaging Spectrograph) = Photon-counting"]
-[10.308984756469727, 7.356799602508545, "[TT] Primary Mirror Diameter of the Cassegrain telescope = 310 mm"]
-[8.251500129699707, 0.035929977893829346, "[TT] Rebound Distance of the Philae Lander = A kilometer above the comet"]
-[10.508506774902344, 4.664586544036865, "[TT] Release Method of the Sail Closeout Panels = Spring-loaded hinges"]
-[9.905389785766602, -0.34899261593818665, "[TT] Altitude of the Satellite = 35,786 km"]
-[8.743465423583984, 3.9112727642059326, "[FF] Measurement Task of the SIXS = Perform measurements of fluxes and spectra of protons and electrons"]
-[5.170661926269531, 6.249457836151123, "[FF] Link Protocol of the MDD = X.25 (CCITT)"]
-[4.246367454528809, 0.33045315742492676, "[TT] Launch Date of the JPSS = March 2017"]
-[8.443283081054688, 7.690266132354736, "[TT] CCD Detection Array of the POLDER-P = 274 x 242 pixels"]
-[4.525149822235107, 6.266307830810547, "[TT] Basis of the MLFMM (Multilevel Fast Multipole Method) = Method of Moments"]
-[6.48222017288208, 4.335484981536865, "[FF] Design Status of the LRI = Flight model production has started"]
-[6.985191822052002, 0.7547852993011475, "[TT] Total Number of Names of the InSight = 2,429,807"]
-[8.545099258422852, 3.1118218898773193, "[FF] Publication Date of the Very-Wide-Filed Ultraviolet Sky Survey = July 13, 1984"]
-[10.921277046203613, 7.548567295074463, "[TT] Swath Width of the WAOSS-B = 533 km"]
-[9.417074203491211, 3.6255574226379395, "[FF] Value of the Magnetic Pressure = Unknown"]
-[8.153970718383789, 8.464420318603516, "[FF] Gain Stability of the VNIR Channels = Far slower than the MWIR and LWIR channels"]
-[9.008533477783203, 3.2144832611083984, "[FF] Description of the Solar Disk = Finite set of non-coherent source points"]
-[6.4528608322143555, -0.6331697106361389, "[TT] Period of the FY-3D = 101.49 min"]
-[5.89816427230835, -0.7812750935554504, "[TT] Lifetime of the Mass Memory System = 7.5 years"]
-[5.621142387390137, 6.991767406463623, "[TT] Data Rates of the Command and data handling subsystem = 20 MByte/s"]
-[8.146040916442871, 3.1306142807006836, "[FF] Temporal Filtering of the GLM = Takes advantage of the difference in lightning pulse duration which is on the order of 400 \u00b5s versus the background illumination which tends to be constant on the time scale of seconds"]
-[11.530346870422363, 5.6737260818481445, "[TT] Wafer Thickness of the Collector Array = 0.5 mm"]
-[13.437033653259277, 7.332830905914307, "[TT] Power of the Prime Power Generated = 120 W"]
-[9.05789566040039, 7.426111221313477, "[TT] Resolution of the Optical Payload = 6.100/pixel"]
-[11.19152545928955, 0.6054723262786865, "[TT] Mission Type of the Cheops = Study of exoplanets"]
-[6.966631889343262, -0.7897076606750488, "[TT] Orbit Period of the TOI 700 d = 37 days"]
-[8.488372802734375, 5.051894187927246, "[FF] Launch Date of the GFO accelerometer = August 2017"]
-[12.085618019104004, 3.521716356277466, "[FF] Function of the XFS = Stores xenon gas in a high pressure vessel and provides the xenon gas for the thruster head"]
-[7.908919811248779, 2.1561877727508545, "[TT] Spatial Sampling of the LI = < 10 km @ latitude 45\u00ba and subsatellite longitude"]
-[5.694788932800293, 5.725057125091553, "[TT] Type of the QC40 = Quad-TMS320C40"]
-[5.177999973297119, 0.7644974589347839, "[FF] Approval Date of the WFIRST = 02 March 2020"]
-[7.79418420791626, 5.039258003234863, "[FF] Recognition of the ITRF = Global Geodetic Reference Frame (GGRF)"]
-[9.531736373901367, -0.42949751019477844, "[TT] Perigee Altitude of the Satellite Orbit = Above 7.3 RE"]
-[8.548972129821777, 6.123285293579102, "[TT] Calibration Stability of the CERES on TRMM = 0.25%"]
-[9.83590316772461, 8.138958930969238, "[TT] Lens Focal Length of the Imager = 134 mm"]
-[4.535938739776611, 5.858549118041992, "[FF] Population of the 406 MHz beacon = Unknown"]
-[7.801640033721924, 4.885824203491211, "[FF] Side Effect of the SPS = High repetition rate"]
-[9.461779594421387, -1.0654737949371338, "[TT] Longitude of the GOES-R = 75\u00ba W"]
-[6.364883899688721, 0.19644536077976227, "[FF] Beam-Out Events of the IPA = 2 per day (nominal), less than one per week on average"]
-[5.666069984436035, 3.5069921016693115, "[FF] Design and Operational Concept of the Mission Operations Facility = The Mission Operations Facility design and operational concept for EUMETSAT\u2019s next generation geostationary satellite program (MTG)"]
-[8.936572074890137, 6.512060642242432, "[FF] TVR of the SLA altimeter = Total Vertical Roughness"]
-[8.605537414550781, 7.76531457901001, "[TT] Pixels per Line of the CCDs = 740"]
-[5.458835601806641, 3.3579161167144775, "[TT] Constellation Builder of the UrtheCast = SSTL (Surrey Satellite Technology Ltd.),UK"]
-[6.009195327758789, 2.11470103263855, "[FF] Conference Presentation Date of the Stuttgart Micro Satellite = May 5-9, 2014"]
-[8.224029541015625, 8.709444999694824, "[FF] Spectral Resolution of the EUVS = From 5-35 nm: 10 nm bins, From 35-115 nm: 40 nm bins, Lyman-\u03b1 (121.6 nm): 10 nm (FWHM), 5-115 nm; 5 nm bins, 117-127 nm; 10 nm bin"]
-[8.53758430480957, 7.26294469833374, "[TT] Quantity of the VBS (Vision Based Sensor) = 1"]
-[9.170428276062012, 7.49263858795166, "[TT] Hyperspectral Instrument Resolution of the Satellogic = 30 meters"]
-[5.03828763961792, 0.5221371054649353, "[TT] Launch Date of the THEOS-2 = 9 October 2023"]
-[8.928722381591797, -0.8069624304771423, "[FF] Orbital Geometry of the R3 = Favorable"]
-[4.189623832702637, 1.9933687448501587, "[TT] Stabilization of the NigeriaSat-2 = 3-axis"]
-[11.128164291381836, 0.5474677085876465, "[FF] Mission of the ARIEL = Study the composition of exoplanets, how they formed and how they evolve"]
-[10.285162925720215, 5.7500901222229, "[TT] Operating Temperature of the CCDs = Near -75\u00baC"]
-[8.32325553894043, 5.502608299255371, "[FF] Pointing Accuracy of the VectorSol = Unknown"]
-[5.666957378387451, 0.8282721638679504, "[FF] Testing Period of the ExoMars = Since April"]
-[5.589065074920654, -2.0305538177490234, "[TT] Imaging Frequency Band of the KOMPSAT-5 = X"]
-[12.135339736938477, -0.12270235270261765, "[FF] Bright Limit of the TESS = IC~4 or perhaps even brighter"]
-[13.336483001708984, 7.358733654022217, "[TT] Power of the FSS = 0.1 W"]
-[3.0878705978393555, 2.3415071964263916, "[TT] Spectral Bands Resolution of the Sentinel-2 = 10 to 60 m"]
-[11.309490203857422, 4.6904191970825195, "[TT] Min. Depth of the Argo buoys = 5 m"]
-[10.997236251831055, 2.057088851928711, "[FF] Launch Date of the XMM-Newton = December 1999"]
-[5.136920928955078, 0.6859380006790161, "[TT] Test Date of the Aireon = May 3, 2017"]
-[4.996581077575684, 3.0255136489868164, "[TT] Agency of the CAS500 = KARI"]
-[3.8338053226470947, 4.396461486816406, "[FF] Imaging Satellite of the ROCSat-2 = High-resolution optical imaging"]
-[9.118597984313965, 7.530795574188232, "[TT] Spatial Resolution of the Visible Spectral Band = 1.25 km x 1.25 km"]
-[8.189750671386719, 9.35094165802002, "[TT] Wavelength of the Responsivity Measurement = 1990 nm"]
-[13.830129623413086, 3.754225969314575, "[TT] Mass of the SAR instrument = 147 kg"]
-[4.348655700683594, 7.904682159423828, "[TT] Downlink Frequency of the Communication System = 437.325 MHz"]
-[10.989556312561035, 2.871657371520996, "[TT] Dimensions of the Microsatellite = 315 mm x 315 mm x 260 mm"]
-[14.355629920959473, 3.0953798294067383, "[TT] Mass of the ChubuSat-1 = 50 kg"]
-[8.845867156982422, 9.526569366455078, "[FF] Band 1 Spectral Range of the TANSO-FTS-2 = 0.755 - 0.772 \u00b5m"]
-[13.637998580932617, 3.416083335876465, "[TT] Current Quantity of the Artificial Objects = 22,000"]
-[6.699569225311279, 2.3276100158691406, "[TT] Average Daily Acquisition Capability of the COSMO-SkyMed = 1800 images"]
-[7.960684299468994, 8.641524314880371, "[TT] Spectral Range WV of the MVIRI = 5.7 - 7.1 \u00b5m"]
-[6.780609130859375, 1.6800956726074219, "[TT] Launch Partner of the James Webb = European Space Agency"]
-[8.572569847106934, 7.691157817840576, "[TT] CCD Line Array of the MSU-E = 1024 pixels"]
-[5.477102279663086, 3.8832695484161377, "[FF] Number of Satellites of the LARES = Smaller with respect to the ones of GNSS"]
-[8.206671714782715, 5.876096725463867, "[TT] Operating Range of the FFRF Sensor = 3 m-30 km"]
-[6.772495746612549, 3.5108375549316406, "[FF] Purpose of the Oxygen Generator Assembly (OGA) Pump Assembly = Critical spare to a support oxygen generation capability in support of the crew on board the International Space Station"]
-[5.7374091148376465, 5.276284217834473, "[TT] Type of the Operating System = Salvo Real Time Operating System"]
-[5.855748653411865, 0.854919970035553, "[TT] International Image Distribution Contract Start Date of the FormoSat-2 = June 2004"]
-[4.433493137359619, 3.0384528636932373, "[TT] Locations of the TT&C stations = Saint-Hubert and in Saskatoon, Saskatchewan"]
-[4.046708583831787, 4.068563461303711, "[FF] Mission of the Arktika-M N1 = Monitor the Earth\u2019s atmosphere and surface in the Arctic, collect and relay information from Arctic facilities, monitor cosmic rays, and assist in the international search and rescue service, COSPAR-SARSAT"]
-[3.4091317653656006, 6.438279628753662, "[TT] Aperture Diameter of the Antenna = 2.5 m"]
-[13.448441505432129, 2.860623836517334, "[TT] Spacecraft Dry Mass of the Telescope = 4059 kg"]
-[5.7478485107421875, 3.185952663421631, "[FF] Affiliated Institutions of the Bluecrab supercomputer cluster = Johns Hopkins University and University of Maryland"]
-[4.543753623962402, 1.736160397529602, "[FF] Conference Presentation Date of the JC2Sat-FF = 18 - 21 August 18-21, 2008"]
-[3.84482741355896, 3.4469034671783447, "[TT] End of Life Date of the Galileo = 22 August 2026"]
-[7.9797043800354, 13.687308311462402, "[TT] SSD of the B2 = 10 m"]
-[6.485206127166748, 7.027129173278809, "[TT] Zones of the AEM = 2"]
-[7.609808921813965, 2.749234437942505, "[FF] Data Sources of the Tool = ESA\u2019s Swarm magnetic field mission and data stored in Movebank"]
-[11.778247833251953, 6.653590202331543, "[TT] Energy Range of the Visible Light = About 2 to 3 eV"]
-[7.053806304931641, 2.760819673538208, "[TT] Launch Provider of the MethaneSAT = Not yet been selected"]
-[10.40030574798584, 5.844265937805176, "[TT] Temperature Difference of the WISPR = 85 degrees Fahrenheit"]
-[7.906373977661133, 0.22591036558151245, "[FF] Data Source of the GRACE-FO = Satellite gravimetry data"]
-[14.232539176940918, 3.2386860847473145, "[TT] Total Mass of the CMGs = 261.6 kg"]
-[5.050697326660156, 1.176387906074524, "[TT] Full Operational Capability of the NPOESS = 2015"]
-[5.191247463226318, 0.9370903968811035, "[TT] Launch Date of the ResourceSat-2A = December 7, 2016"]
-[8.126811981201172, -0.5645791888237, "[TT] Mountain Glaciers Ice Loss of the GRACE = 200 gigatons per year"]
-[7.343630313873291, 4.516928195953369, "[FF] Instruments of the ERS-2 = MWR, ATSR/M, AMI/SAR/Image, AMI/Scatterometer, ERS Comms, AMI/SAR/Wave, RA, GOME, ATSR-2"]
-[12.082100868225098, 4.544365882873535, "[TT] Stowed Dimensions of the Spacecraft = 1.1 m x 0.8 m x 0.8 m"]
-[9.925871849060059, -0.36458316445350647, "[TT] Altitude of the First Batch of Satellites = 550 km"]
-[6.084514141082764, 6.154374599456787, "[TT] 1 Second Labels of the SSRNI = Yes"]
-[5.61167573928833, 1.0681452751159668, "[FF] Calibration Date of the HISUI = 10-15 July 2016"]
-[4.649199485778809, 8.002882957458496, "[TT] Frequency of the Skylab S-194 = 1.4 GHz"]
-[6.779175758361816, 5.998870849609375, "[TT] Quantity of the Companies = 21"]
-[10.674073219299316, 7.5323567390441895, "[TT] Swath width of the Optical System = 2000 km"]
-[4.608169078826904, 5.56013822555542, "[FF] Lifesaving of the NASA Emergency Beacons = Yes"]
-[5.865649700164795, 3.9060864448547363, "[TT] Phase B Payload Design Completion of the SMOS = Oct. 2003"]
-[3.8488869667053223, 0.8951259851455688, "[FF] Launch Date of the PSLV-C32/IRNSS-1F = March 10, 2016"]
-[8.295217514038086, 4.178913116455078, "[FF] Measurement of the Microdosimeter Suite = Intensity of energetic particles"]
-[5.31441593170166, 8.06966495513916, "[TT] Frequency Range of the IMM = 5Hz \u2013 20kHz"]
-[7.5410380363464355, 5.627171516418457, "[TT] Manufacturer of the Scanning LIDAR = Jena-Optronik GmbH"]
-[4.362128734588623, 0.6349266767501831, "[TT] Integration Date of the BRK = May 29"]
-[4.49175500869751, 7.4121413230896, "[TT] Modulation of the Downlink = IM/DD (Intensity Modulation / Direct Detection)"]
-[9.803627967834473, -0.6763968467712402, "[TT] Orbit Altitude of the Bion-M1 = 575 km"]
-[6.3991289138793945, 4.440714359283447, "[FF] Purpose of the Zarya control module Kurs electronics unit = Cosmonaut remote-control docking of Russian spacecraft"]
-[8.31200885772705, 6.887641429901123, "[FF] Type of the WFI = High resolution optical imagers"]
-[9.65365982055664, 8.166287422180176, "[TT] Field of View (Cross-track) of the MSU-50 = 62\u00ba"]
-[6.266256332397461, 4.202000617980957, "[FF] Ground Segment Elements of the SAMPEX = Ground stations, POCC, PACOR, UMSOC"]
-[11.55267333984375, 3.45322585105896, "[TT] Operating Mode of the Solar Electric Propulsion System (SEPS) = Twin thruster mode"]
-[8.486953735351562, 7.415311336517334, "[FF] Photometric Precision of the PicSat = Sub-milimag"]
-[7.729680061340332, 6.434361934661865, "[TT] Mesoscale Image Collection Interval of the ABI = 30 seconds"]
-[5.162001609802246, 1.002865195274353, "[FF] Joining Date of the SPOT 6 = Sept. 9, 2012"]
-[5.39619255065918, 5.709352970123291, "[TT] RS-422 Serial Interfaces of the PIC = Primary and redundant"]
-[8.71023178100586, 3.910313844680786, "[FF] Ion Analysis of the Time-of-flight/position sensing section = Mass, energy, and angle"]
-[8.474289894104004, 3.1637215614318848, "[FF] Atmospheric Species of the UVS = K, Na, Al, Si, Ca, Li, OH, H2O"]
-[4.923534870147705, 0.4718441069126129, "[TT] Launch Date of the BILSAT = Sept. 27, 2003"]
-[10.155145645141602, 7.467483043670654, "[TT] Optics Design of the NFOV Imagers = Cassegrain design"]
-[6.115503311157227, 5.8473711013793945, "[TT] Components of the GS (Ground System) = 2,100 servers, 149 racks of network equipment, 317 workstations, and storage services totaling three petabytes (3 PB)"]
-[14.589510917663574, 6.541197776794434, "[TT] Number of Cells of the Battery = 24"]
-[4.766013145446777, 2.3901233673095703, "[TT] Development Location of the RASAT = Turkey"]
-[5.768611907958984, 5.151949405670166, "[TT] Processing of the Normal telecommands = By the OBC on-board software"]
-[13.4166259765625, 5.465942859649658, "[TT] Type of the Solar array = Fixed, 3 panels, 1 body"]
-[12.161115646362305, 2.990999460220337, "[TT] Propellant of the Propulsion System = Hydrazine"]
-[4.054363250732422, 3.5339274406433105, "[FF] PRS Access of the Galileo = Available for government agencies, armed forces and emergency services"]
-[8.283354759216309, 6.280307769775391, "[FF] Cross Section of the CCR = Averaged around a circle at each velocity aberration"]
-[5.114121437072754, 7.0420002937316895, "[TT] Uplink Rates of the LLCD PAT Systems = Up to 20 Mbit/s"]
-[11.578302383422852, 3.4706177711486816, "[TT] Propulsion of the SES-14 = All-electric"]
-[9.314391136169434, 10.74227523803711, "[TT] Polarization of the ICI-6 = V"]
-[8.009600639343262, 3.1577138900756836, "[FF] Measured Gases of the GeoCarb = CO2, CH4, CO"]
-[6.314209938049316, 4.548179626464844, "[FF] Functions of the MOC = Mission operations planning and design, Science and instrument operations support, Command planning, verification and uploads, Ground station interaction, Observatory health monitoring and housekeeping trending, Observatory navigation and orbit maintenance maneuver implementation"]
-[5.1587233543396, 0.5318182706832886, "[TT] Launch Date of the AERO-VISTA mission = April 7, 2021"]
-[10.713534355163574, -0.3682495951652527, "[TT] Mission Time of the Tandem-L = > 10 years"]
-[4.754911422729492, 7.504049777984619, "[TT] Data Rate of the UHF Band = 9.6 kbit/s"]
-[13.953144073486328, 3.056046962738037, "[FF] Mass of the SEEDS = Unknown"]
-[6.228747844696045, 5.195296764373779, "[FF] Behavior of the Interfaces = Nominally"]
-[11.946054458618164, 5.051352500915527, "[TT] Size of the MSU-50 = 210 x 200 x 140 mm"]
-[12.808416366577148, 7.599547386169434, "[TT] Instrument Power of the Instrument = 66/60 W (peak/average)"]
-[12.020792961120605, -0.37114208936691284, "[FF] Discovery Date of the TESS = 24 June 2020"]
-[13.983083724975586, 3.1490204334259033, "[TT] Mass of the Corvus-BC 2 = 10 kg"]
-[5.807096004486084, 4.055778503417969, "[TT] Experimental Mission of the FY-3 = FY-3A"]
-[7.782250881195068, 1.9954229593276978, "[FF] Objectives of the SeaSat = Demonstrate techniques to monitor Earth's oceanographic phenomena and features from space on a global scale, Provide timely oceanographic data to scientists studying marine phenomena and users of the oceans as a resource, Determine the key features of an operational full-time ocean-monitoring system"]
-[7.391707420349121, 5.549294948577881, "[FF] Architecture of the LRI = Single frequency laser, Fabry Perot reference cavity, triple mirror assembly (TMA), OBS (Optical Bench Subsystem), instrument electronics"]
-[14.239919662475586, 3.2770729064941406, "[TT] Mass of the Card Mass = <0.6 kg"]
-[5.4206342697143555, 3.517953395843506, "[TT] Engineering Activities of the TDP Operations = Not performed by Inmarsat"]
-[7.7616658210754395, 5.614626407623291, "[FF] Advantages of the LED = High energy efficiency, long life, small size, design flexibility"]
-[7.913464546203613, 0.7955394983291626, "[FF] Date of the \"Catastrophic Flooding in Yellowstone\" = 23 June 2022"]
-[5.097225189208984, 3.2606630325317383, "[TT] Manufacturer of the AMSU-A = Aerojet, a subsidiary of GenCorp"]
-[13.60430908203125, 1.750032901763916, "[TT] Weight of the Cargo Dragon = 6,553 pounds (2,972 kg)"]
-[10.979166984558105, 5.629414081573486, "[TT] Charring of the Heat Shield Avcoat = Consistent with expectations"]
-[3.3919517993927, 6.440914154052734, "[TT] Antenna Diameter of the Transmitter = 0.7 m"]
-[3.787738084793091, 4.4814348220825195, "[FF] Image Quality of the RADARSAT-2 = Stable and well within operating objectives"]
-[8.97803020477295, 4.564148426055908, "[TT] Quantity of the Sun sensors = 4"]
-[4.267655372619629, 6.481746673583984, "[FF] Operating Frequency of the Antennas = Not specified"]
-[11.72624397277832, 4.426143646240234, "[TT] Lower Tray Height of the SUNSAT = 12 cm"]
-[9.770673751831055, -0.5772141218185425, "[TT] Orbit Altitude of the Almaz-1B = ~ 600 km"]
-[14.0712251663208, 4.0608415603637695, "[TT] Plate Scale of the EXI instrument = 0.85 mm/\u00ba"]
-[1.7260915040969849, 6.148218631744385, "[FF] Characteristics of the Dark Matter = Weird, unexpected"]
-[6.19320011138916, 7.025008201599121, "[TT] Data Rate of the GLM = 5 Gbit/s"]
-[10.099504470825195, 4.701444149017334, "[TT] Control Speed of the Wheels = 1500 rpm"]
-[6.312721252441406, -0.7395259737968445, "[TT] Duration of the Spacewalk = About five-and-a-half hours"]
-[3.8736300468444824, 4.395957946777344, "[TT] Daily Imagery Usage of the RADARSAT-1 = 3000-4000 scenes"]
-[4.685343265533447, 2.6033337116241455, "[TT] Funding Date of the BRITE Satellites = January 2011"]
-[6.212442398071289, 3.1367948055267334, "[FF] Pricing Options of the BlackSky = Variety of pricing and utilization options"]
-[13.876130104064941, 3.954451560974121, "[TT] Mass of the Particle Detectors = 2.5 kg"]
-[8.356185913085938, 3.170661449432373, "[TT] Number of Atmospheric Profiles Collected of the CRISTA Telescopes = 38"]
-[7.184520244598389, 2.1833343505859375, "[TT] Number of SSPAs of the Biomass = 6"]
-[4.074596405029297, 5.569741249084473, "[FF] Definition of the dBZ = Z is the equivalent radar reflectivity that gives a mean power equal to the standard deviation after integration and noise subtraction"]
-[9.176709175109863, 2.473444938659668, "[TT] Sprites of the MEIDEX = 100%"]
-[5.274011611938477, 8.487688064575195, "[TT] Bandwidth of the DRT = \u00b1 100 kHz"]
-[14.44647216796875, 6.6202898025512695, "[TT] Function of the IMPS = Power generation and power storage for microelectronic applications"]
-[7.566956996917725, 6.383967876434326, "[TT] Blackbody Observation Frequency of the ABI = At least every 15 minutes"]
-[3.3763444423675537, 1.5050880908966064, "[FF] Launch Date of the Sentinel-3A = Unknown"]
-[4.932733535766602, 3.287822723388672, "[TT] Manufacturer of the NIRSpec = Astrium GmbH"]
-[9.616362571716309, 8.12468433380127, "[TT] Field of View of the FY-4 GLI = 9,000 km diagonal"]
-[11.815739631652832, 6.720411777496338, "[TT] Range of Relativistic Electrons of the XGRE = 1 MeV - 10 MeV"]
-[6.737294673919678, -0.470284104347229, "[FF] Activation Time of the NGC Lander = Before the separation from orbiter"]
-[8.202396392822266, 5.718174934387207, "[FF] Geographical Mapping Accuracy of the Primary Imager = Automatic"]
-[5.708366870880127, -0.9236337542533875, "[TT] Design Life of the ASNARO-2 = 5 years"]
-[13.350532531738281, 5.596695899963379, "[FF] Power Supply of the ISS Roll-out Solar Arrays (iROSA) = Increase in energy available for research and station activities"]
-[8.94232177734375, 5.423408508300781, "[TT] Pointing Capability of the GOMX-3 = 1-degree"]
-[7.1528425216674805, 2.0413520336151123, "[TT] Imaging Sensor of the Landsat-5 = Thematic Mapper (TM)"]
-[5.563855171203613, 4.689793586730957, "[TT] Technology of the Digital Electronics = Cutting edge"]
-[9.292448997497559, 8.411735534667969, "[FF] Band Separation of the Telescope = Beam splitter, interference filters"]
-[8.082416534423828, 4.394962787628174, "[FF] Purpose of the ShadowCam = Reduce stray light from making its way to the detector"]
-[7.854722023010254, 1.97654390335083, "[FF] Fishing Spot of the Shikisai = Japanese pilchard (Sardinops melanostictus)"]
-[6.438335418701172, -0.2708037495613098, "[TT] Period of the CSC and OSC = About 19.7h"]
-[7.983409881591797, 5.169008731842041, "[FF] Components of the Instrument = SEDF (Spatial Response), Alignment Parameters, ISRF Shape, SSI, SR, Smile, CU, Radiance Calibration Coefficients, Response Linearity, Noise, Detector PRNU, Detector DSNU"]
-[10.714556694030762, 1.5211565494537354, "[FF] Black Hole Mass of the Leo I = Nearly as massive as the Milky Way's"]
-[3.5963125228881836, 6.433759689331055, "[TT] Antenna Sizes of the Ground Station = 9.1m, 4.6m"]
-[8.890395164489746, 7.409993648529053, "[TT] Resolution of the Raw Video Product = 2560 x 1080 pixels"]
-[11.34670639038086, 4.216105937957764, "[FF] Size of the Sunshade = Large"]
-[4.959508895874023, 1.0002847909927368, "[TT] Launch Date of the ALOS-3 = 7 March 2023"]
-[6.2578654289245605, 4.416551113128662, "[FF] Role of the COSMIAC = Build the satellite and collect the data from it"]
-[9.241908073425293, 7.659521579742432, "[TT] Swath Width of the CCD Camera = 700 km"]
-[6.840137481689453, 6.256053447723389, "[FF] Deliverables of the Laser Team = ETU laser, three flight units, and a flight spare"]
-[8.07530403137207, -1.046876311302185, "[TT] Data Collection of the ICESat-2 = Fresh ice is totally flat to within a couple centimeters"]
-[7.759453296661377, 3.1569204330444336, "[FF] Measurement of the Imaging Spectrometer = Light absorbed by methane"]
-[6.496606826782227, 4.486810207366943, "[TT] Design Location of the ASIC = In-house"]
-[13.400243759155273, 6.924018383026123, "[TT] Payload Power of the SmallGEO = Up to 3 kW"]
-[8.282153129577637, 2.8320412635803223, "[TT] Measurement Category of the STARSHINE = Atmospheric Temperature Fields, Atmospheric Humidity Fields, Atmospheric Winds"]
-[12.39418888092041, 0.616886556148529, "[TT] Accuracy of Stellar Age Measurement of the PLATO = Up to 10%"]
-[13.167116165161133, 7.243221759796143, "[TT] Power Consumption of the CEASE = <1.5 W"]
-[6.43964147567749, 4.840883731842041, "[FF] Module Type of the TRAM = Flex-based HDI"]
-[11.7047119140625, 3.313535690307617, "[TT] Accumulated Firing Time of the LM thruster = Over 6.0 minutes"]
-[5.666186809539795, 5.701801300048828, "[TT] Processor of the Proton P400K-SGMII-2-PCI104S-SD Space Computer = Freescale advanced 45 nm dual-core microprocessor"]
-[8.362655639648438, 8.246600151062012, "[TT] Bands of the HawkEye = 8-band multispectral"]
-[8.521343231201172, 6.3020219802856445, "[TT] Window Spectral Region of the CERES = 8 - 12 \u00b5m"]
-[7.238892555236816, 4.357916831970215, "[FF] Purpose of the SEM = Monitor the space environment"]
-[14.2045316696167, 3.348423480987549, "[TT] Total Mass of the SILEX = 150 kg"]
-[6.799535274505615, 6.954610347747803, "[TT] Number of Beams of the Eutelsat Quantum = 8"]
-[13.298338890075684, 7.332651138305664, "[TT] Weight of the mvBlueFOX-IGC (200w) = 80 g"]
-[9.51760482788086, 3.620584726333618, "[FF] Short wavelength Magnetizations of the Vertically-integrated magnetization model = Dominated by seafloor spreading"]
-[8.298198699951172, 2.4590702056884766, "[TT] Number of Wire Boom Deploys of the THEMIS Constellation = 20"]
-[9.668030738830566, -0.3804524540901184, "[TT] Latitude Range of the PRISMA Payload = 70\u00b0S - 70\u00b0N"]
-[11.843802452087402, 6.749094009399414, "[TT] Energy Range for Electrons of the MagEIS = 30 keV to 4 MeV"]
-[8.585556983947754, 6.908895015716553, "[FF] Image Quantity of the LROC = Over 3,000"]
-[8.856389045715332, 7.035506725311279, "[TT] GSD of the DMC-2G imager = 22 m"]
-[4.360410213470459, 7.072986602783203, "[TT] Function of the MEXIC = Format and date data, both scientific and housekeeping in X-band"]
-[7.493910789489746, 1.9588426351547241, "[FF] URL of the Global Ocean Observing System (GOOS) = http://www.gosic.org/goos/Argo-data-access.htm"]
-[5.000077724456787, 6.021726131439209, "[FF] Application of the SDR = Space applications"]
-[9.50026798248291, 3.546306610107422, "[FF] Value of the Pickup H+ Pressure = Unknown"]
-[10.499770164489746, 6.981192588806152, "[TT] Primary Mirror Diameter of the WUPPE = 0.5 m"]
-[8.005058288574219, 8.790889739990234, "[TT] Wavelength Range (Infra-red) of the SOLSPEC = 800 to 3080 nm"]
-[5.9603071212768555, 3.8832504749298096, "[TT] IMU of the DSX = Present"]
-[3.9036195278167725, 2.0947155952453613, "[TT] Launch Vehicle of the CanX-2 = PSLV"]
-[5.336625099182129, 1.074874997138977, "[FF] Meeting Date of the AMPERE = December 14, 2010"]
-[5.968327045440674, 0.29261860251426697, "[FF] Arrival Date of the Rosetta = August 6, 2014"]
-[8.059072494506836, 1.6893517971038818, "[FF] Parameter of the DPS = Sea surface evaporation - Corrections for sea surface roughness"]
-[6.146327972412109, 7.230700492858887, "[TT] BAQ Data Compression of the CSG-SAR = 10:6, 10:5, 10:4, 10:3, 10:2, 10:1, 10:10"]
-[4.665456295013428, 1.6034802198410034, "[TT] Development Timeline of the GHGSat-D = Spring 2013 to Summer 2015"]
-[5.381418228149414, 7.268218994140625, "[TT] Channel Data Rate of the Communication System = 310 Mbit/s"]
-[8.029155731201172, 0.6201876401901245, "[TT] Peak Time of the Water Production = Between the end of August and early September 2015"]
-[6.075085639953613, 5.6062798500061035, "[FF] Type of the COVE Payload = Reconfigurable FPGA-Based"]
-[11.885919570922852, 5.405819892883301, "[TT] Dimensions - Sensor head assembly of the Instrument = 20 x 37 cm"]
-[6.359420299530029, -1.1877515316009521, "[TT] Measurement Date of the GRACE-FO satellites = March 29, 2021"]
-[7.771938800811768, 2.369196653366089, "[FF] Applications of the SARAL = Altimetric applications in oceanography, cryospheric sciences, hydrology and geodesy"]
-[6.212005615234375, 3.828173875808716, "[FF] Mission Objective of the TechEdSat = Evaluate SPA (Space Plug-and-play Avionics) designed by \u00c5AC Microtec, and to perform a communications experiment utilizing the Iridium and Orbcomm satellite phone network"]
-[10.232593536376953, 2.163635015487671, "[FF] Image Resolution of the eROSITA telescope = High"]
-[10.732783317565918, 7.1980814933776855, "[TT] Footprint (km) of the SSM/I = 68.9 x 44.3, 69.7 x 43.7, 59.7 x 39.6, 35.4 x 29.2, 37.2 x 28.7, 15.7 x 13.9, 15.7 x 13.9"]
-[10.991971969604492, 5.747491359710693, "[TT] Shielding Thickness of the Trisat-R = 7 mm"]
-[10.1265287399292, 2.8889551162719727, "[TT] Observation Time per Pass of the ISARA CubeSat = 3-5 minutes"]
-[13.204230308532715, 7.2694292068481445, "[TT] Power Consumption of the OTU = 15 W"]
-[10.03244400024414, -1.5366169214248657, "[TT] Orbit Inclination of the JAWSAT = 100.2\u00ba"]
-[8.228476524353027, 4.459505081176758, "[FF] Orbital Predictions of the LARES = Unknown"]
-[4.125120162963867, 7.144497871398926, "[TT] Frequency of the S-band patch Rx/Tx antennas = 2 GHz"]
-[10.015284538269043, -1.572556734085083, "[TT] Inclination of the Orbit = 97.8o"]
-[4.820408821105957, 3.9118218421936035, "[TT] Number of Satellites of the GalileoSat = 4"]
-[8.188637733459473, 4.446557998657227, "[FF] Orbit Control of the MEV-1 = Controlled the orbit of the customer satellite"]
-[7.7562150955200195, 8.9275484085083, "[TT] Spacing Between Consecutive Lines of the MS Bands = 936 \u00b5m"]
-[3.4545934200286865, 4.959167957305908, "[FF] Polarimetry Mode of the RISAT-SAR = Circular or hybrid polarimetry"]
-[8.2318754196167, 7.51339864730835, "[FF] Mounting of the PSD Detector = On a PCB (Printed Circuit Board) along with 4 operational amplifiers"]
-[13.772697448730469, 7.251332759857178, "[TT] Efficiency of the Pulsed Diode Driver = 85%"]
-[5.428314208984375, 7.190557956695557, "[TT] Transmission Rate of the Demodulator = 1.5 Mbit/s"]
-[5.080410480499268, 8.100677490234375, "[FF] Bandwidth of the Aquarius = Not specified"]
-[6.701589584350586, 6.0119948387146, "[TT] Number of Components of the JEM = 6"]
-[8.265454292297363, 6.329195976257324, "[TT] Longitudinal Movement of the CCRR = Less than 1 m"]
-[6.626235485076904, 5.9322052001953125, "[TT] Update Frequency of the Ground Sensors = Every 30 minutes"]
-[8.290091514587402, 2.481051206588745, "[FF] Measurement Capabilities of the ALADIN = Cloud characteristics, aerosol measurements, cloud top height, cloud cover, cloud and aerosol extinction and optical thickness, multi-layer clouds identification, lower troposphere aerosol stratification, height of the tropopause, height of the PBL"]
-[6.378939151763916, 0.6795461773872375, "[FF] Launch Date of the Landsat = Unknown"]
-[10.147032737731934, 8.100037574768066, "[TT] Focal Length of the Telescope = 234.5 mm"]
-[9.133105278015137, 7.375166893005371, "[TT] MS Resolution at Nadir of the QuickBird-2 = 2.4 m - 1.8 m (8 bands)"]
-[10.04488754272461, 2.831108331680298, "[FF] Announcement Date of the X-ray Navigation CubeSat Mission = 3 May 2018"]
-[8.909625053405762, 5.228277683258057, "[TT] Pointing Control of the LEOStar-3 = 13.3 arcsec (3\u03c3)"]
-[9.44271183013916, 5.4837236404418945, "[TT] Ideal Slew Rate of the ADCS = 0.25\u00ba/s"]
-[14.236506462097168, 3.220475673675537, "[TT] Total Mass of the DORIS = 17 kg"]
-[8.690997123718262, 7.659005641937256, "[TT] 0.47, 0.64, 0.865, and 1.61 \u00b5m channels of the Frame-to-Frame Registration = \u00b116 \u00b5rad"]
-[7.35837984085083, 3.601511240005493, "[FF] Debris Field Location of the DMSP-F13 = Near the satellite"]
-[3.7779769897460938, 4.70414924621582, "[TT] Ground Range Resolution of the RADARSAT-2 = Stable"]
-[11.958789825439453, 5.010143280029297, "[TT] Size of the ICARE-NG = 116 mm x 202 mm x 90 mm"]
-[5.810701847076416, 1.5917373895645142, "[FF] Date of the 28th Annual AIAA/USU Conference on Small Satellites = August 2014"]
-[6.141651630401611, -0.11204585433006287, "[TT] Orbit Delivery of the Aeolus = 55 minutes later"]
-[13.375809669494629, 7.315488338470459, "[TT] Power of the STAFF/DWP = 5.0 W"]
-[4.831081867218018, 0.6504305005073547, "[TT] Launch Date of the ORS-3 Mission = August 2013"]
-[6.942239761352539, 1.5264015197753906, "[FF] Mission Status Date of the James Webb Space Telescope = Dec. 5. 2012"]
-[8.416696548461914, 3.2093777656555176, "[TT] Horizontal Cell Size of the Ozone Measurement Instrument = 50 km @ nadir"]
-[5.655394077301025, 0.4557609558105469, "[TT] Operation Extension Deadline of the Cluster = October 1, 2010"]
-[9.531311988830566, 4.853527545928955, "[TT] Attitude Control of the STPSat-1 = Momentum-biased about the pitch axis"]
-[6.926331520080566, -0.680833637714386, "[TT] Period of the Molniya Orbit = 11 hours and 58 minutes"]
-[5.410329341888428, 0.4830814301967621, "[TT] Reentry Date of the MaSat-1 = January 9, 2015"]
-[4.887599945068359, 7.297285556793213, "[TT] TT&C Downlink Data Rate of the RF Communications = 1.6 - 4 Mbit/s"]
-[10.439326286315918, 3.2937324047088623, "[TT] Quantity of the Power Board = 1 per CubeSat"]
-[8.02668285369873, 9.254609107971191, "[TT] Wavelength of the Carbonate = 2.35 \u00b5m"]
-[8.795382499694824, 7.1586785316467285, "[TT] L1 Detectors Active Area of the HIT = 2 cm2"]
-[7.536995887756348, 0.7760574221611023, "[FF] Location of the Gateway = Orbiting the Moon"]
-[6.200383186340332, 1.1340126991271973, "[FF] Image Acquisition Date of the NOAA-20 = June 5"]
-[6.884408473968506, 7.131064414978027, "[TT] Number of Beams of the ATLAS instrument = 9"]
-[8.369165420532227, 6.941046237945557, "[TT] Instrument Type of the TUBSAT = High resolution optical imagers, Other, Data collection, Hyperspectral imagers"]
-[5.031252384185791, 1.2383427619934082, "[FF] Implementing Arrangement Date of the INSAT-3D = Sept. 11, 2008"]
-[6.158821105957031, -0.18682841956615448, "[TT] Temporal Matchup Window of the CYGNSS = 3 hours"]
-[9.536075592041016, 0.8584225177764893, "[TT] Distance from Sun of the Kuiper Belt = 5 billion kilometers (and beyond)"]
-[7.836328029632568, 0.5635753870010376, "[TT] Moon Illumination of the CUMULOS = 74%"]
-[7.860334873199463, 8.847097396850586, "[TT] Number of Wavelength Bands of the OCO-2 = 3"]
-[6.268325328826904, 6.522578239440918, "[TT] Number of Timeslots per Hour of the DCPs = 40"]
-[10.360383033752441, 2.1611015796661377, "[FF] Capability of the NuSTAR = Seeing high-energy X-ray light from the decay of titanium-44"]
-[1.7451237440109253, -2.076106548309326, "[TT] Sample Return Date of the Hayabusa-2 = December 2020"]
-[4.8649773597717285, 4.260836601257324, "[FF] URL of the Argos-3 = https://web.archive.org/web/20110814035457/http://www.argos-system.org/html/system/enhancements_en.html"]
-[3.1947929859161377, 2.0831589698791504, "[TT] Orbit Altitude of the Copernicus Sentinel-1A and -1B = 600 and 700 km"]
-[3.439424991607666, -0.9251850843429565, "[TT] Orbit Type of the PACE = Sun-synchronous near-circular orbit"]
-[7.761653900146484, 4.215203762054443, "[FF] Unknown of the Thermotive = Unknown"]
-[8.161280632019043, 0.1373888999223709, "[TT] Delayed Launch Date of the Meteor-M2 spacecraft = Mid-December 2013"]
-[9.476845741271973, 0.665081799030304, "[TT] Line-of-Sight Distance to Mars of the ExoMars TGO = 41 million km"]
-[5.369546413421631, 2.778350353240967, "[TT] Flagship of NASA's EOS Program of the Terra = True"]
-[4.316844940185547, 0.6451555490493774, "[TT] Launch Date of the DMSP-F13 = March 24, 1995"]
-[5.108633995056152, 3.1995675563812256, "[TT] Manufacturer of the DWP = University of Sheffield"]
-[6.472362041473389, 6.032041549682617, "[FF] RFI Mitigation Capability of the Low-Noise Detector = Unknown"]
-[7.493533134460449, -0.07971468567848206, "[TT] Orbit Altitude of the G\u00f6kt\u00fcrk-2 = 684 km"]
-[7.403554916381836, 2.2805049419403076, "[FF] Observation Coverage of the GEO Satellite = About 40% of the Earth's surface"]
-[12.859292030334473, 2.0548481941223145, "[FF] Alignment of the Hexapod = Used for aligning SAGE-III"]
-[4.883683681488037, 5.53429651260376, "[TT] GPS Receiver Frequency of the SPS = L1 (1575.42 MHz)"]
-[4.667232513427734, 0.08427181094884872, "[TT] End of Life Date of the AstroSat = 28 September 2025"]
-[14.005703926086426, 3.252967596054077, "[TT] Mass of the KickSat-2 = Just a few grams"]
-[5.932155609130859, 3.829926013946533, "[TT] Success Rate of the SOLSE-2 = 80%"]
-[5.874777793884277, 4.796566963195801, "[TT] Performance of the Development Flight Instrumentation (DFI) = Worked well throughout the entire flight"]
-[9.106512069702148, 4.29702091217041, "[FF] Attitude Sensing of the ACS = 3-axis magnetometer and a solar panel current algorithm"]
-[10.7113037109375, 5.57050085067749, "[FF] Composition of the Thermal Insulation = Several layers of metal-evaporated polyimide film"]
-[8.970247268676758, 4.526334285736084, "[TT] Quantity of the Sun Sensors = 4"]
-[12.455960273742676, 0.5599643588066101, "[TT] Launch Date of the PLATO = 2017\u20132018"]
-[5.8663177490234375, -0.77626633644104, "[TT] Lifetime of the Spacecraft Platform = 7 years"]
-[5.459800720214844, 3.0111334323883057, "[FF] Partner Organizations of the OPS-SAT = BST (Berlin Space Technologies) and MEW Aerospace (Germany), GOMSPACE (Denmark) as well as MAGNA STEYR Engineering and Unitel (Austria)"]
-[4.500815391540527, -0.23211513459682465, "[FF] Docking Date of the Starliner = 20 May 2022"]
-[7.774777412414551, 9.312512397766113, "[FF] Bragg Condition of the Multilayer = n \u03bb = 2d sin(\u03b8)"]
-[1.9387922286987305, -0.4032280743122101, "[TT] Mission Duration of the Van Allen Probes = 3 years"]
-[8.199092864990234, 4.521581172943115, "[FF] Design Objective of the LARES-2 = Achieve specific orbit with high accuracy"]
-[5.120542049407959, -0.5952810049057007, "[FF] PDR Date of the TARANIS = June 2009"]
-[11.22404956817627, 4.940072059631348, "[TT] Diameter of the LARES-2 = 0.424 m"]
-[5.843344688415527, 2.2678472995758057, "[TT] Launch Vehicle of the ArgoMoon = NASA's Orion EM-1"]
-[8.390359878540039, 0.05210741609334946, "[FF] Instruments of the Meteor-1/Meteor-2/Meteor-Priroda Series = 174-K, MR-900B, RMK-2, Chaika, MR-2000, MR-900"]
-[8.969792366027832, 5.811699390411377, "[TT] Direction of the Comedia C328 = Pointing in the direction of the balloon"]
-[11.680363655090332, 3.3732190132141113, "[TT] Position of the VACCO MiPS cold gas thruster = Aft end (\u2013y)"]
-[9.4348726272583, 1.262021541595459, "[TT] Drift Speed of the DSAT#1 = Approximately 7.5m/s"]
-[5.846109390258789, -0.19209575653076172, "[TT] On-Orbit Operations of the LS-7 = 11 years"]
-[5.529067039489746, 4.38844108581543, "[FF] Ground Stations of the Spacecraft = AFSCN (Air Force Satellite Control Network) and the USN (Universal Satellite Network)"]
-[5.258042812347412, 8.11712646484375, "[TT] Frequency Range of the Magnetic antennas (IMM) = DC-20 kHz"]
-[8.486091613769531, 8.095396041870117, "[TT] Spectral Resolution of the IMG = < 0.15 cm -1 (band 3); <0.25 cm -1 (band 2)"]
-[7.655272483825684, 8.67570972442627, "[TT] Spectral Bands of the CHRIS = Up to 63"]
-[5.823824882507324, 1.564500331878662, "[TT] Retraction Status of the ROSA = Unsuccessful"]
-[9.690434455871582, -0.0729518011212349, "[TT] Altitude of Deployment of the Drogue Chutes = Around 7 \u00bd km"]
-[4.566125869750977, 7.576459884643555, "[TT] Data Rate of the VHF Transmitter = 64 kbit/s"]
-[9.735288619995117, 0.438213050365448, "[TT] Accuracy of positioning of the PROBA-3 = Around a few mm"]
-[8.426875114440918, 7.629843711853027, "[TT] Array Size of the CCD Detector Matrix = 576 lines x 780 columns"]
-[8.185394287109375, 6.855410575866699, "[TT] Number of Images of the DECA = 15"]
-[6.835753440856934, -0.6356889605522156, "[TT] Orbit Period of the ADEOS-II = 101 minutes"]
-[13.851339340209961, 3.7152247428894043, "[TT] Mass of the GPS OEM Sensor = About 22 g"]
-[12.450611114501953, 0.5762590169906616, "[TT] Short-Term Pointing Stability of the PLATO = 25 s"]
-[7.136382579803467, -0.5803956389427185, "[FF] Rotation Period of the Stars = Ranged from one to as many as 11 Earth-days"]
-[4.630373477935791, 2.770498275756836, "[TT] Mission Control Center Location of the Odin = Solna, Sweden"]
-[7.724797248840332, 8.640697479248047, "[FF] Spectral Index of the AMS = Single, constant"]
-[6.503007888793945, 4.879856109619141, "[FF] Function of the GAMCATS = Monitoring, control, and test functionality for the antenna control unit, receive elements, transmit elements, control ports of the switching system, RF switching, BITE (Built-In Test Equipment), environmental and fire suppression system monitoring, waveguide dehydrator, and other related equipment"]
-[12.52586841583252, 3.199129343032837, "[TT] Propellant Capacity of the Spacecraft = 23 kg"]
-[6.283807754516602, 5.261897563934326, "[FF] System Architecture of the SOHLA-1 = ACS, COM, EPS, Experiment connected to CCU and ECU"]
-[12.29060173034668, 4.733602523803711, "[TT] Size of the Miniaturized X-band transponders = 5 cm x 5 cm x 7.6 cm"]
-[2.8937907218933105, 4.585463047027588, "[TT] Maximum Data Rate of the PALSAR-2 = 800 Mbit/s"]
-[13.195467948913574, 7.280799865722656, "[TT] Power Consumption of the CubeLCT = Less than 8.5 W"]
-[7.175489902496338, 5.44094705581665, "[TT] Topology of the FODB = Ring"]
-[8.65848159790039, 3.882965087890625, "[FF] Function of the SDEA instrument = Can be utilized for ions or neutrals"]
-[6.51140022277832, 0.2720256447792053, "[TT] Exceeded Design Life of the Landsat-7 = Yes"]
-[8.784812927246094, 4.479558944702148, "[FF] Attitude Measurement Devices of the AOCS = Two fine-pointing sun sensors (FPSS), two star trackers also referred to as SSU (Star Sensor Unit), and three gyros"]
-[8.021450996398926, 1.1384090185165405, "[TT] Last Measurable Rainfall Date of the Las Vegas = Mid-April"]
-[6.097012519836426, 3.4963746070861816, "[FF] Experiment Types of the OPS-SAT = Artificial intelligence, advanced communication protocols and compression techniques, software-defined radio, optical communication, advanced autonomous planning, web services in space"]
-[4.411784648895264, 4.272789001464844, "[TT] Number of Satellites of the Capella X-SAR Constellation = 9"]
-[4.79495906829834, 0.7650645971298218, "[FF] Launch Confirmation Date of the Telesat LEO Phase 1 = 12 Jan. 2018"]
-[7.251789093017578, 1.4243886470794678, "[FF] Rover Task of the ExoMars = Seek out geologically interesting sites to drill below the surface"]
-[13.99842357635498, 6.467494010925293, "[FF] Protection of the Batteries = Integrated over current protection"]
\ No newline at end of file
+[5.160096645355225, 8.793096542358398, "The Celestial Sphere Coverage of the Spacecraft Satellite is 64% during the first two years of the mission."]
+[7.0774712562561035, 7.163238525390625, "The PM Mass of the DSX Spacecraft Payload Module Satellite is 180 kg."]
+[5.213613510131836, 9.70866584777832, "The Recovery Status of the NEOSSat Satellite is Successful."]
+[6.722851276397705, 8.410761833190918, "The Nadir resolution of the WorldView-4 Satellite is 31 cm."]
+[10.049193382263184, 10.660056114196777, "The Number of Channels of the ICI Instrument is 11."]
+[7.769374847412109, 10.191213607788086, "The Software of the OBC On-Board Computer is FOS (Flight Operations Segment)."]
+[7.9796857833862305, 10.03935718536377, "The Number of Computer Consoles of the Control Room Facility is 9."]
+[13.489581108093262, 11.322863578796387, "The Number of Normal Cameras of the PLATO Telescope is 24."]
+[15.67857837677002, 9.751118659973145, "The Spectral Range of the SOLSPEC-ATLAS Spectrometer is 210-2400 nm."]
+[10.594514846801758, 9.524298667907715, "The Number of Load Cells of the Truss Structure is 6."]
+[13.232380867004395, 9.833312034606934, "The FOV for VNIR-P pushbroom scanning of the VNIR-NP Imager is 55\u00ba."]
+[12.79001235961914, 8.936933517456055, "The SRAMs Quantity of the RADMON Radiation Monitor is 16."]
+[15.81900691986084, 10.898445129394531, "The SNR of the Band 5 Spectral Band is 110."]
+[5.137787818908691, 11.00347900390625, "The Start of Science Operations Date of the RAIDS Experiment is October 22, 2009."]
+[6.342623710632324, 7.217489719390869, "The Mass of the KOMPSAT-3 Satellite is 970 kg."]
+[6.91657829284668, 8.864730834960938, "The Number of satellites per system of the WorldView-4 Satellite is 1."]
+[5.3203840255737305, 10.977248191833496, "The Launch Date of the OrbView-2 Satellite is August 1, 1997."]
+[5.879562854766846, 8.664878845214844, "The Altitude of the GRACE-FO satellites Satellite is ~490 km."]
+[7.398259162902832, 9.378195762634277, "The Type of the DERA-patented carbon-composite joint Spacecraft Structure is Novel."]
+[6.366792678833008, 7.2023234367370605, "The Mass of the GCOM-W1 Satellite is ~1990 kg."]
+[13.718896865844727, 8.532347679138184, "The Data Bandwidth of the RTEPs On-board Image Processing System is 6 Mbit/s."]
+[15.050607681274414, 10.356934547424316, "The Bands of the SCIAMACHY Spectrometer is 8."]
+[11.595527648925781, 8.611761093139648, "The Range of the Magnetometer Sensor is \u00b160 \u00b5T."]
+[10.968829154968262, 10.364007949829102, "The Architecture of the MM Radiometer Sensor is Direct-detection."]
+[9.638128280639648, 11.992239952087402, "The Polarizations of the SAR antenna Antenna is HH,VV,HV,VH."]
+[5.8429059982299805, 9.71168041229248, "The Ground Station of the LightSail Satellite is Cal Poly San Luis Obispo."]
+[8.920283317565918, 10.307063102722168, "The Mounting of the S-band receive and transmit antenna Antenna is Nadir-facing deployable boom."]
+[10.522212028503418, 9.240019798278809, "The Altitude Range of the Air Density Measurement Device Instrument is ~200 km."]
+[5.617391109466553, 8.022897720336914, "The Pointing Accuracy of the PARASOL microsatellite Satellite is 0.1\u00ba."]
+[13.606268882751465, 11.67286205291748, "The Focal Length of the Primary Mirror Telescope Component is 120 mm."]
+[11.14919662475586, 10.465819358825684, "The Operational Mode of the Aquarius Radiometer System is  Survival."]
+[4.740350246429443, 8.908326148986816, "The Observation Duration of the TESS Satellite is 27 days."]
+[13.286141395568848, 10.495755195617676, "The Field of View (FOV) of the Genesis Ion Monitor Instrument is 26\u00ba starting along the spin axis by about 3\u00ba in azimuth."]
+[12.440320014953613, 11.031539916992188, "The Power Consumption of the Photometer Instrument Instrument is \u2264 3.5 W."]
+[6.346927165985107, 8.38167667388916, "The Orbit Inclination of the Max Valier Satellite is 98\u00ba."]
+[8.860692024230957, 10.099541664123535, "The Downlink Frequency of the Payload Communication System is Ka-band."]
+[5.83266019821167, 7.08033561706543, "The Mass of the Flock-1c CubeSat is 5 kg."]
+[10.706134796142578, 11.238208770751953, "The Resolution of the Stripmap mode (SM) Operational Mode is 5 m x 5 m."]
+[5.910017967224121, 8.004257202148438, "The Size of the Lake Atat\u00fcrk Dam Reservoir is 817 km2."]
+[7.68474817276001, 11.186182022094727, "The Optics Type of the ALTIUS Instrument Satellite Instrument is Reflective optics."]
+[6.774994373321533, 7.5821967124938965, "The Fuel of the IRS-1A Satellite is Hydrazine."]
+[12.099600791931152, 8.829174041748047, "The Range of the Rate sensor Sensor is \u00b185\u00ba/s."]
+[10.864994049072266, 11.099488258361816, "The Spatial Resolution of the MSU-SK Radiometer is 170 m (in VIS)."]
+[7.24807596206665, 8.944290161132812, "The Radiation Hardness of the Satellite Satellite is MEO compliant."]
+[5.42183256149292, 9.971244812011719, "The Launch Date of the ABEX CubeSat is Planned for 2024."]
+[14.03488540649414, 8.523229598999023, "The Full Well Charge of the Image Sensor Imaging is 60,000 e-."]
+[8.526232719421387, 9.554194450378418, "The Total Data Volume per Orbit of the Satellite Satellite is 77.7 Gbit."]
+[6.444128513336182, 8.352531433105469, "The Orbit Inclination of the Monitor-E Spacecraft is 97.5\u00ba."]
+[13.415156364440918, 9.258988380432129, "The Nadir Resolution of the OLS Imaging Sensor is 0.55 km in the VIS range."]
+[5.951899528503418, 8.116546630859375, "The Embankment Height of the Ataturk Dam Dam is 184 m."]
+[6.622605323791504, 10.398540496826172, "The Objective of the TanSat Satellite is Retrieve the atmosphere column-averaged CO2 dry air mole fraction (XCO2) with precisions of 1% (4 ppm) on national and global scales."]
+[4.382018566131592, 8.49315071105957, "The TLE Accuracy of the Orbit Dynamic System System is Low distance difference of the appropriate time zone."]
+[10.43503475189209, 10.478239059448242, "The Frequencies of the MM Radiometer Sensor is 89, 165, 176, 180 and 182 GHz."]
+[14.95477294921875, 10.375517845153809, "The Spectral Band of the Instrument Spectrometer is TIR."]
+[13.555585861206055, 8.62687873840332, "The Data Size of the Camera Imaging Device is 14 bit/pixel."]
+[14.654851913452148, 8.559353828430176, "The Spectral Range of the Current GOES imager Sensor is 5.77-6.6."]
+[13.824504852294922, 9.345141410827637, "The IFOVs of the Detectors Photovoltaic Detectors is 14 km."]
+[-3.41005802154541, 11.290103912353516, "The Latency of the ATL16 ATLAS Atmosphere Weekly Data is 45 days from receipt of last data in product."]
+[15.629551887512207, 10.851266860961914, "The Wavelength Range of the Band 5 Spectral Band is 1628-1654 nm."]
+[7.921444416046143, 10.161150932312012, "The CPU of the OBC On-Board Computer is ERC-32."]
+[14.201400756835938, 9.956999778747559, "The Spectral Resolution (86 keV) of the Detector Instrument is 1.2 keV."]
+[12.070205688476562, 11.866439819335938, "The Height of the Instrument Instrument is 140 mm."]
+[4.679254055023193, 9.367592811584473, "The Operational Duration of the Meteosat-7 Satellite is 17 years."]
+[12.2689790725708, 9.751506805419922, "The Developer of the Temperature Sensor Sensor is High School Students of Geymonat (Tradate, VA, Italy)."]
+[7.854793548583984, 10.160037994384766, "The Software of the Control Room Facility is SCOS-2000."]
+[9.777933120727539, 8.497748374938965, "The Computer of the ADCS Attitude Determination and Control System is ARM 7 MCU."]
+[6.605367183685303, 9.80349349975586, "The Payload of the SV-2 Satellite is WINCS (Winds-Ion-Neutral Composition Suite)."]
+[5.86375617980957, 9.563419342041016, "The Measurement Type of the GRACE-FO Satellite is Groundwater Storage and Root Zone Soil Moisture."]
+[6.924582004547119, 9.19796371459961, "The Shape of the DebriSat Satellite is Hexagonal Prism."]
+[9.548651695251465, 10.730969429016113, "The Output Power of the RF communications Communication System is ~ 1W."]
+[4.585187911987305, 8.894729614257812, "The Cycle Length of the Satellite Imaging Satellite is 175 days."]
+[10.126951217651367, 11.149032592773438, "The Measurement Accuracy of the D2P Radar Altimeter Altimeter is 1-3 cm average."]
+[6.864468574523926, 9.138318061828613, "The Number of Operational Satellites of the DMSP (Defense Meteorological Satellite Program) Satellite Program is 3."]
+[7.498497009277344, 7.599887847900391, "The voltage of the Bus Bus is  28\u00b15 V."]
+[13.559179306030273, 8.68116569519043, "The Capacity of the Image Storage Data Storage is 8 GB + 32 GB of science data."]
+[9.990972518920898, 12.172272682189941, "The Dimensions of the SAR antenna Antenna is 3 m x 1 m."]
+[15.701606750488281, 9.735536575317383, "The UV Spectral Range / Bandwidth of the SOLSPEC-ATLAS Spectrometer is 210-370/1.2/0.4."]
+[6.49804162979126, 10.347076416015625, "The Managed By of the GFO Satellite is METOC (Meteorological/Oceanographic) Program Office of SPAWAR."]
+[6.946427822113037, 7.586665153503418, "The Hydrazine Capacity of the Propulsion Subsystem Propulsion is Up to 28 kg."]
+[6.914608955383301, 9.522472381591797, "The Sponsor of the DebriSat project Satellite is NASA and DoD."]
+[8.294392585754395, 9.369707107543945, "The Relative Positioning Accuracy of the PRISMA Satellite is Sub-centimeter level."]
+[6.653614521026611, 10.891180038452148, "The Instruments of the Meteor-M-2 Satellite is DCS, KMSS, IKFS-2, MTVZA-GY, MSU-MR, GGAK-M, Severyanin-M."]
+[9.553693771362305, 11.580619812011719, "The Mass of the SeaWinds scatterometer Scatterometer is 205 kg."]
+[9.07041072845459, 9.460245132446289, "The Mass of the TRSR GPS Receiver is 4 kg."]
+[15.051236152648926, 9.74234390258789, "The Spectral Range of the HR Spectrometer Spectrometer is 677\u2013697nm."]
+[6.382015705108643, 9.706700325012207, "The Role of UNM of the SORTIE Satellite is Integrators of the CubeSat."]
+[10.041069030761719, 2.539804458618164, "The SCI ports of the STRV-2 DHS Data Handling System is Six RS-422, MIL-STD-1553 S/C bus."]
+[5.2679948806762695, 11.112994194030762, "The Launch Date of the Monitor-E Spacecraft is Aug. 26, 2005."]
+[10.66110897064209, 11.617879867553711, "The Antenna Aperture in the Azimuth of the P Mode Observation Mode is 7.5 m."]
+[12.044234275817871, 11.912369728088379, "The Width of the Instrument Instrument is 413 mm."]
+[11.162038803100586, 10.510860443115234, "The Operational Mode of the Aquarius Radiometer System is Standby."]
+[13.697237014770508, 11.668417930603027, "The Components of the TOU Telescope Optical Unit is 6 lenses."]
+[14.445659637451172, 10.453365325927734, "The Size of the Optical Scanning Design Imaging Spectrometer is 1.3 m3."]
+[10.15044116973877, 2.428910493850708, "The Analog channel of the STRV-1d DHS Data Handling System is Sixteen."]
+[12.382368087768555, 11.078174591064453, "The Power Consumption of the Photometer Instrument is \u2264 3.5 W."]
+[11.163553237915039, 9.000425338745117, "The Quantity of the Magnetotorquers AOCS Actuators is 3."]
+[8.756118774414062, 9.886247634887695, "The Transmission Speed of the KIZUNA Satellite Communication Technology is 3.2 Gbit/s."]
+[6.943386554718018, 10.019278526306152, "The Project Partners of the DSP Satellite Project is ESA (European Space Agency), CNSA (China National Space Administration)."]
+[4.471925258636475, 8.708005905151367, "The Occultation Duration of the CTECS Satellite is 6 minutes."]
+[7.637027740478516, 8.270540237426758, "The Attitude of the ISS Space Station is Torque Equilibrium Attitude (TEA)."]
+[9.351034164428711, 12.352873802185059, "The Impulse Peak Power of the X-band Radar is 100 kW."]
+[14.602285385131836, 10.35653305053711, "The Focal Plane Cooling of the Spectrometers Instrument is Passively cooled."]
+[11.996116638183594, 10.006928443908691, "The Outer Shell Temperature of the Dewar Component is ~254.5 K."]
+[5.921841144561768, 11.021142959594727, "The Remarks/Sensors of the OrbView-1 Satellite is OTD."]
+[14.76645278930664, 10.15434741973877, "The ILS Spectral Resolution of the Instrument Spectrometer is \u226411 nm, \u226416 nm."]
+[9.53110122680664, 8.22138500213623, "The RAAN Accuracy of the Bloostar Launch Vehicle is \u00b10.05\u00ba."]
+[12.357943534851074, 11.515833854675293, "The Mass of the ST (Star Tracker) Instrument is 1.2 kg."]
+[11.275270462036133, 10.867402076721191, "The Components of the DBCP Pseudo-depolarizer is Four wedges of birefringent material."]
+[7.972769260406494, 10.78974723815918, "The Manufacturer of the SEPAC Instrument is SwRI (Southwest Research Institute), San Antonio, TX, USA."]
+[12.359211921691895, 9.915292739868164, "The IR Detector Temperature of the OCTS Sensor is 100 K."]
+[4.385530471801758, 9.496411323547363, "The Lifespan of the Satellite Satellite is 11/12 years."]
+[7.342367649078369, 7.697451114654541, "The Dimensions of the Bus Bus is 1.6 m x 1.6 m x 1.5 m."]
+[9.434774398803711, 12.23922348022461, "The Transmitting Pulses of the Instrument Radar Instrument is H or V."]
+[11.576210975646973, 8.539445877075195, "The Sensor Distance of the MAG Magnetometer is 80 cm apart."]
+[4.365478038787842, 8.680691719055176, "The LTAN of the Max Valier Satellite is 17:00 hours."]
+[15.74410343170166, 9.783935546875, "The IR Spectral Range / Bandwidth of the SOLSPEC-ATLAS Spectrometer is 800-2400/20./4."]
+[15.59556770324707, 9.782958984375, "The Number of Spectrometers of the SOLSPEC-SOLAR Spectrometer is 3."]
+[15.071813583374023, 10.40484619140625, "The Spectral Band of the Instrument Spectrometer is MWIR."]
+[7.435940742492676, 9.143534660339355, "The Bus Structure Material of the QSat-EOS bus Microsatellite bus is Aluminum alloy (A5052-H32)."]
+[5.605102062225342, 9.898505210876465, "The Mission Status of the ABEX CubeSat is Planned."]
+[6.433426380157471, 7.248165130615234, "The Mass of the UniSat-1 Satellite is 12 kg."]
+[7.792321681976318, 10.612394332885742, "The Manufacturer of the Hardware Quick Look SAR Processor SAR Processor is MRSA/SAC team."]
+[13.676198959350586, 11.575826644897461, "The Focal Length of the ART-XC Instrument Telescope is 2700 mm."]
+[5.087607383728027, 11.082085609436035, "The Launch Date of the Orion/ EFT-1 Spacecraft is 5 Dec 2014."]
+[6.077634811401367, 9.400678634643555, "The Solar Panel Deployment of the LightSail Satellite is Possibly ajar or deployed."]
+[8.26583480834961, 9.459506034851074, "The Range Measurement Precision of the Satellite Satellite is Few decimeters."]
+[6.897006034851074, 9.192547798156738, "The Number of Spacecraft of the DSP Satellite Project is 2."]
+[6.725813865661621, 8.290311813354492, "The Slew Angle of the MiRaTA Satellite is 90-105\u00b0."]
+[14.41946792602539, 9.062312126159668, "The Dynamic Range of the Limb Sensor Sensor is 4-5 orders in magnitude variation."]
+[13.48880672454834, 10.787184715270996, "The Resolution of the Photometer Optical Instrument is 26.52 arcsec/pixel."]
+[12.01410961151123, 11.15613842010498, "The Power of the MW Instrument is 1 W."]
+[12.03378677368164, 11.864235877990723, "The Length of the Instrument Instrument is 204 mm."]
+[10.931357383728027, 7.396880149841309, "The Area Collection Rate of the Pushbroom Sensor is Very high."]
+[12.270676612854004, 9.17584228515625, "The Angle Resolution of the FSS Fine Sun Sensor is Up to 0.03\u00ba."]
+[6.342413425445557, 7.192549228668213, "The Dry Mass of the HY-1C Satellite is 429 kg."]
+[9.471738815307617, 12.363591194152832, "The Sigma 0 Range of the Radar Radar is HH, VV: +15~-25 dB."]
+[12.445260047912598, 10.036439895629883, "The Sensor Operating Pressure of the FIPEX Instrument is Down to 10-10 mbar."]
+[4.721188068389893, 9.330305099487305, "The Operational Duration of the OPAL Satellite is 29 months."]
+[12.794580459594727, 8.921799659729004, "The Channels Quantity of the REM Radiation Environment Monitor is 16."]
+[11.669095993041992, 11.81408977508545, "The Project Manager of the TEMPO Instrument is Stephen Hall."]
+[12.275263786315918, 11.629364967346191, "The Mass of the CSS Instrument is 48 gram."]
+[14.948543548583984, 10.492237091064453, "The Optical Configuration of the Spectrometer Spectrometer is Czerny-Turner."]
+[7.426318645477295, 9.5260009765625, "The specification of the Bus Satellite Component is  MethaneSAT."]
+[5.710006237030029, 10.554675102233887, "The Launch Center of the RASAT Satellite is Jiuquan Satellite Launch Center in China."]
+[10.5198392868042, 10.216409683227539, "The Frequency Range of Shaker Tests of the Boom Structure is 9-300 Hz."]
+[5.228344440460205, 8.203409194946289, "The Goal Mission Life of the PARASOL microsatellite Satellite is Two years."]
+[11.480545997619629, 9.475042343139648, "The Sampling Interval of the sADC A/D Converter is 12 \u00b5s."]
+[5.853919506072998, 8.901268005371094, "The Spacing of the GRACE-FO satellites Satellite is 220 km."]
+[7.303127288818359, 7.504171371459961, "The Propulsion System of the Lunar IceCube Spacecraft is Busek\u2019s miniaturized electric thrusters."]
+[12.127361297607422, 8.874866485595703, "The Error (RMS) of the Coarse sun sensor Sensor is <10\u00ba."]
+[11.818132400512695, 11.302936553955078, "The Weight of the MESSR Radiometer is 140 kg."]
+[5.735576152801514, 8.832063674926758, "The Swath of the Sentinel-2 satellites Satellite is 290 km."]
+[11.01970386505127, 10.717521667480469, "The Polarization of the MWR Radiometer is V."]
+[14.978857040405273, 9.898324012756348, "The Spectral Coverage of the AIRS Atmospheric Infrared Sounder is 3.74 - 15.4 \u00b5m for the array grating spectrometer (IR bands)."]
+[5.498622417449951, 10.6070556640625, "The Goal of the RASAT Satellite Mission is to test the equipments."]
+[9.2610445022583, 9.745402336120605, "The Frequency L2 of the GPS receiver Receiver is 1227.6 MHz."]
+[9.076078414916992, 10.117782592773438, "The Modulation of the RF communications Communication System is FSK."]
+[-3.314413547515869, 11.193037033081055, "The Latency of the ATL21 Arctic/Antarctic Gridded Sea Surface Height within Sea Ice Data is 45 days from receipt of last data in product."]
+[5.143564701080322, 10.315106391906738, "The Launch Announcement Date of the MethaneSAT Satellite is 13 January 2021."]
+[5.755834579467773, 10.506547927856445, "The Launch Location of the RASAT Satellite is Orenburg Region, Russia."]
+[5.213666915893555, 10.24316120147705, "The First Image Download Date of the LightSail Satellite is June 2, 2015."]
+[11.126191139221191, 10.171893119812012, "The Manufacturer of the MM Radiometer Sensor is NASA/JPL."]
+[5.989739894866943, 8.457914352416992, "The Orbit (Orbit control) of the Spacecraft Satellite is \u2264 \u00b1 500 m."]
+[7.479466438293457, 9.200087547302246, "The Material of the Outer Panels Satellite is CFRP (EX-1515/M55J + Redux 312L)."]
+[4.987025737762451, 10.965943336486816, "The Delivery Date of the FSS Fine Sun Sensor is June 2015."]
+[11.333869934082031, 8.672128677368164, "The Manufacturer of the Vector Magnetometer Instrument is DTU (Danish Technical University)."]
+[15.48817253112793, 10.344453811645508, "The Spectral Band of the Infrared Channel is approx. 3.6 km at nadir."]
+[7.042409896850586, 7.174941539764404, "The Total Mass of the DSX Spacecraft Payload Module Satellite is 600 kg."]
+[13.253203392028809, 9.717259407043457, "The Non-Polarized Channels of the VNIR Sensor is 11."]
+[7.114739418029785, 7.510867595672607, "The Stowed Dimensions of the DSX Spacecraft Payload Module Satellite is 3.6 m x 2 m x 1.1 m."]
+[5.606970310211182, 7.046834945678711, "The Size of the DTUSat-2 CubeSat is 1U."]
+[5.521392822265625, 9.744874000549316, "The Mission Operations Location of the OPAL Satellite is SSDL ground station at Stanford University."]
+[4.868631839752197, 10.83409595489502, "The End of life date of the Meteor-M-2 Satellite is 31 Dec 2030."]
+[10.250150680541992, 10.502394676208496, "The Frequency of the Millimeterwave receiver radiometer is 190 GHz."]
+[9.82589340209961, 10.37723159790039, "The Frequency of the  Submillimeterwave receiver receiver is 562 GHz."]
+[5.8091888427734375, 8.521637916564941, "The Distance from Milky Way of the Andromeda Galaxy is 2.5 million light-years."]
+[13.567039489746094, 11.218006134033203, "The Slit Width of the IRIS instrument Instrument is 1/3 arcsec."]
+[4.442694664001465, 8.665857315063477, "The Time to Full Control of the Satellite Spacecraft is Three hours."]
+[4.251345634460449, 8.876701354980469, "The Duration of the Chirp Signal is ~100us."]
+[11.728598594665527, 8.671799659729004, "The Error (RMS) of the Magnetometer Sensor is <40 nT."]
+[10.958373069763184, 11.187036514282227, "The Spatial Resolution of the Multispectral Instrument (MSI) Instrument is 60 m."]
+[5.273264408111572, 11.090415000915527, "The Launch Date of the Monitor-E Spacecraft is June 30, 2003."]
+[7.896325588226318, 10.128472328186035, "The Operating System of the Control Room Facility is Linux."]
+[14.507939338684082, 10.105809211730957, "The Smile and Keystone of the Instrument Spectrometer is \u22641 image pixel."]
+[10.105875968933105, 10.924386978149414, "The Operating Frequency of the ALT Experiment Altimeter is 13.56 GHz."]
+[7.653151035308838, 9.217400550842285, "The Material of the Boom Assembly Assembly is CFRP (Carbon Fiber Reinforced Plastic)."]
+[7.407333850860596, 7.128470420837402, "The Array Power Peak of the DSX Spacecraft Payload Module Satellite is 790 W."]
+[12.796865463256836, 8.939889907836914, "The p-FETs Quantity of the RADMON Radiation Monitor is 4."]
+[10.95672607421875, 12.176361083984375, "The Tank Length of the Launcher Test Facility is 283.5 m."]
+[4.4042816162109375, 9.591080665588379, "The Goal Life of the Gokturk-2 Satellite is 7 years."]
+[11.255477905273438, 10.015278816223145, "The Accuracy of the SCM Satellite Charging Monitor is \u22640.01 pA/cm2."]
+[12.376460075378418, 11.543069839477539, "The Mass of the FSS Instrument is 87.5 g."]
+[9.210993766784668, 9.668400764465332, "The Tracking of the TRSR GPS Receiver is Dual-frequency code and cross-correlation, data output of up to eight GPS satellites simultaneously."]
+[13.325787544250488, 11.84492015838623, "The Size of the Instrument Telescope is 107 cm diameter x 360 cm in length."]
+[8.992422103881836, 9.867226600646973, "The Downlink Frequencies of the Satellite Satellite is S-band, UHF, C-band, L-band, 2048 MHz, 2225 MHz, 406 MHz, 5005 MHz, 1191.795 MHz, 1278.75 MHz, 1575.42 MHz, 1544 MHz."]
+[14.095479011535645, 10.129441261291504, "The Energy Range of the Electron Spectrometer Instrument is 1 eV to 1400 eV."]
+[13.165937423706055, 9.59516429901123, "The Radiometer of the OLS Imaging Sensor is VIS/IR."]
+[4.509152412414551, 8.7814359664917, "The Revisit Time of the Sentinel-2 satellites Satellite is 5 days."]
+[5.388509750366211, 9.509608268737793, "The Daughterships Shape of the OPAL Satellite is Similar to a hockey puck."]
+[4.287035942077637, 9.150896072387695, "The Orbit Repeat Cycle of the MSU-SK Radiometer is 21 days."]
+[5.193656921386719, 10.898002624511719, "The Delivery Date of the \u00b5CAT Hardware is Sept. 2015."]
+[13.502224922180176, 11.43808364868164, "The F-number of the Telescope Optical Instrument is 2.2."]
+[10.280084609985352, 10.391194343566895, "The Frequency Conversion of the Microwave Assembly Signal Processing Device is 24 and 32 GHz."]
+[11.485516548156738, 10.447860717773438, "The Brightness Temperature Stability of the MWR Dicke Radiometer is 1 K."]
+[12.59445571899414, 9.231788635253906, "The Time Resolution of the Electrostatic Analysers Sensor is Up to 0.5 s."]
+[-3.4303112030029297, 11.309901237487793, "The Latency of the ATL17 ATLAS Atmosphere Monthly Data is 45 days from receipt of last data in product."]
+[7.080682277679443, 10.042250633239746, "The Developer of the MSG Satellite Fleet is Airbus Defence and Space."]
+[13.760883331298828, 9.75301456451416, "The Spectral Region of the QWIP Detector Detector is 11-17 \u03bcm."]
+[15.672872543334961, 9.737008094787598, "The UV Spectral Range / Bandwidth of the SOLSPEC-SOLAR Spectrometer is 165-370/1.2."]
+[4.915860652923584, 11.216517448425293, "The Pioneering Mission Concluded Date of the LISA Space Observatory is June 2017."]
+[6.04250431060791, 8.415105819702148, "The Off-Nadir Pointing Duration of the MicroSat-70 Satellite is Up to half an orbit."]
+[12.218916893005371, 9.876409530639648, "The Cooling Temperature of the QWIP Detector Detector is 150 K."]
+[10.108541488647461, 8.616222381591797, "The Operational Ranges for non-main windows position of the NightPod Tracking Device is 1st:Yaw \u00b160\u00ba, 2nd:Roll +40\u00ba/-20\u00ba (constrained by NightPod geometry), 3rd:Pitch nodding \u00b120\u00ba."]
+[5.309390544891357, 10.668620109558105, "The First Contact Date of the RASAT Satellite is August 17, 2011."]
+[7.5916876792907715, 9.830825805664062, "The Additional Payloads of the SENSE Satellite is CTECS (Compact Total Electron Content Sensor) and a micro dosimeter."]
+[14.100861549377441, 8.447340965270996, "The Peak Quantum Efficiency of the Imager Camera is 50%."]
+[4.997089385986328, 8.78598403930664, "The Sky Coverage of the TESS Satellite is 85 percent."]
+[10.653327941894531, 10.958159446716309, "The Swath Width of the RM-08 Passive Microwave Scanning Radiometer is 550 km."]
+[9.645551681518555, 11.934769630432129, "The Polarization of the ICI instrument Receiver is V and H."]
+[6.801848411560059, 10.222935676574707, "The Leader of the Marsquake Service Service is ETH Zurich."]
+[11.913637161254883, 12.585083961486816, "The Required Accuracy of the Mie co-polar channel Channel is 50%."]
+[5.207622051239014, 9.542856216430664, "The Duty Cycle Reduction of the NEOSSat Satellite is Modest."]
+[13.710501670837402, 9.338905334472656, "The GIFOV of the VIS Detector is 1 km."]
+[13.438462257385254, 8.862582206726074, "The Field of View of the VIS Camera Camera is 30\u00ba x 19\u00ba."]
+[4.43515157699585, 9.641039848327637, "The Design Life of the Gokturk-2 Satellite is 5 years."]
+[6.942398548126221, 8.821035385131836, "The Number of satellites per system of the WorldView Legion Satellite System is 6."]
+[12.047128677368164, 8.793904304504395, "The Error (RMS) of the Nadir sensor Sensor is <0.2\u00ba."]
+[9.303439140319824, 11.182528495788574, "The Ocean Current Speed Accuracy of the Satellite System Earth Observation is 0.2 m/s."]
+[14.883822441101074, 10.537781715393066, "The Type of the Spectrograph Instrument is Rowland Circle style imaging spectrograph."]
+[11.384782791137695, 8.373710632324219, "The Magnetic Field Strength of the Pulsar Celestial Object is 70 quadrillion times stronger than that of Earth."]
+[14.778029441833496, 8.754900932312012, "The Central Wavelength of the Spectrally modified current sounder Sensor is 8.5."]
+[11.219854354858398, 9.629395484924316, "The Sampling Frequency of the fADC A/D Converter is 80 MHz."]
+[5.751567363739014, 9.720815658569336, "The Launch Site of the HORYU-2 Nanosatellite is TNSC (Tanegashima Space Center), Japan."]
+[9.770458221435547, 10.83584976196289, "The Data Rate of the RA-1 Antenna Antenna is \u2264 15 kbit/s."]
+[14.546160697937012, 8.480364799499512, "The Dark Current of the Image Sensor Imaging is 4 e- /s/pixel."]
+[11.225763320922852, 10.961448669433594, "The Data Quantization of the MI Radiometer Instrument is 10 bit."]
+[6.909453392028809, 10.647334098815918, "The Mission Scientist of the Aeolus Satellite is Anne Grete Straume."]
+[4.413280010223389, 8.579604148864746, "The Time Between Satellites of the A-Train Satellite Constellation is About 15 seconds."]
+[5.705171585083008, 8.77957820892334, "The Continental Crust Thickness of the Earth Planet is Averages from 35 to 40 kilometers."]
+[13.804780960083008, 11.879230499267578, "The Telescope Type of the ISAMS Instrument is Movable off-axis reflecting telescope."]
+[5.873701572418213, 10.969820022583008, "The Remarks/Sensors of the OrbView-1 Satellite is GPS."]
+[15.696736335754395, 10.787728309631348, "The Number of Pixels of the Band 3 Spectral Band is 1600."]
+[6.54173469543457, 10.767234802246094, "The Agency of the Meteor-M-2 Satellite is ROSKOSMOS, ROSHYDROMET."]
+[9.500255584716797, 11.510964393615723, "The Data Rate of the SeaWinds scatterometer Scatterometer is 40 kbit/s."]
+[10.077492713928223, 2.4982943534851074, "The Total mass of assembly of the STRV-2 DHS Data Handling System is 2 kg."]
+[13.52574634552002, 9.039642333984375, "The Object Detection Capability of the Imaging System Imaging System is Objects as small as 2 mm in length."]
+[12.493341445922852, 9.811412811279297, "The Designer of the BGO Calorimeter Detector is Prof. AN Qi from USTC."]
+[7.612236976623535, 7.1753315925598145, "The Power Generation of the Spacecraft Satellite is 5.2 kW."]
+[15.339902877807617, 10.02209758758545, "The Chopper Wheels Frequency of the SBUV Spectrometer is 25 Hz."]
+[9.110654830932617, 11.759284973144531, "The Mode of the RADARSAT-2 Satellite is ScanSAR Wide mode."]
+[14.06657600402832, 10.907039642333984, "The length of the toroidal holographic diffraction grating grating is 50 mm."]
+[6.979630947113037, 8.56508731842041, "The Daily system capacity of the WorldView Legion Satellite System is 3x."]
+[6.662741184234619, 10.038772583007812, "The Developer of the skCube Satellite is SOSA (Slovak Organization for Space Activities ) ."]
+[13.29963207244873, 10.506032943725586, "The FOV of the . Microdosimeter B Instrument is 32\u00ba."]
+[4.124392986297607, 9.4144868850708, "The Data Collected of the GP-B mission Mission is Over 1 TByte."]
+[13.513205528259277, 8.225120544433594, "The Dynamic Range of the Kodak KAI-11002 CCD CCD is 66 dB."]
+[10.418835639953613, 10.539933204650879, "The Operating Frequencies of the SMMR Microwave Radiometer is 10.7 GHz."]
+[7.198341369628906, 7.240704536437988, "The Launch Vehicle compatibility of the DSX Spacecraft Payload Module  Payload Module is 12 months."]
+[5.209664344787598, 9.652078628540039, "The Torque Rods Status of the NEOSSat Satellite is Failed."]
+[6.318807601928711, 9.860243797302246, "The Ground Segment Chain of the Deimos-2 Satellite is Flight operations chain."]
+[9.544986724853516, 11.57639217376709, "The Power of the SeaWinds scatterometer Scatterometer is 250 W."]
+[4.1469573974609375, 9.337703704833984, "The Science Phase Duration of the GP-B mission Mission is 50 weeks."]
+[7.313488006591797, 10.274517059326172, "The User of the STK Scheduler Software is NASA."]
+[10.05776596069336, 8.781721115112305, "The Mounting Angle of the AST Autonomous Star Tracker is 10\u00ba from the spin axis."]
+[14.825891494750977, 10.715245246887207, "The Spectrometer Type of the SPEXone Spectrometer is Compact and lightweight all-reflective imaging grating spectrometer."]
+[6.737939357757568, 8.078080177307129, "The Dimensions of the INTEGRAL Satellite is (5 x 2.8 x 3.2) m."]
+[6.4768171310424805, 8.398782730102539, "The Orbit Inclination of the ISS Space Station is 51.6\u00ba."]
+[14.508143424987793, 9.1673583984375, "The Spectral Range of the Limb Sensor Sensor is 290 to 1000 nm."]
+[9.225127220153809, 9.699993133544922, "The Operation Modes of the TRSR GPS Receiver is C/A and P code, P-codeless (cross-correlation)."]
+[11.903236389160156, 9.810955047607422, "The Stages of the Cooler Passive Cooler is 4."]
+[8.729466438293457, 9.829487800598145, "The Data Transfer Capacity of the Satellite Communication is 100 MByte/day."]
+[6.172170639038086, 9.513636589050293, "The Type of the skCube Satellite is 1U CubeSat."]
+[15.835960388183594, 10.886035919189453, "The SNR of the Band 3 Spectral Band is 400."]
+[4.366244316101074, 8.610603332519531, "The TLE Maintenance of the Orbit Dynamic System System is 5.5 hours to 10 hours."]
+[15.114264488220215, 9.876450538635254, "The Spectral Range of the HR Spectrometer Spectrometer is 740\u2013780 nm."]
+[13.997224807739258, 11.445253372192383, "The Coating of the FPI Mirrors Component is Silver coating (thickness 50 nm)."]
+[11.201385498046875, 10.468995094299316, "The Pointing Requirements (Control and Stability) of the Aquarius Radiometer System is 0.5\u00ba."]
+[4.958402156829834, 10.964829444885254, "The Observation Start Date of the LIGO/Virgo sensors Sensors is Late 2018."]
+[13.732284545898438, 8.511211395263672, "The Raw Video Data Bandwidth of the Camera Imaging Device is 12.5 Gbit/s."]
+[12.949241638183594, 9.745607376098633, "The Similar To of the VIIRS Sensor is MODIS."]
+[8.969450950622559, 10.209210395812988, "The TT&C Frequency of the Payload Communication System is S-band."]
+[5.672436714172363, 7.152994155883789, "The Deployable Drag Sail Area of the 3U CubeSat Satellite is 10m2."]
+[5.412521839141846, 11.012004852294922, "The Launch Date of the OrbView-3 Satellite is June 26, 2003."]
+[10.691354751586914, 10.930635452270508, "The Swath Width of the MWR Dicke Radiometer is 380 km."]
+[11.430184364318848, 8.531909942626953, "The Principle of the Magnetometer Instrument is Magneto-inductive."]
+[13.662469863891602, 11.611343383789062, "The Number of Mirror Modules of the ART-XC Instrument Telescope is 7."]
+[-3.3695642948150635, 11.247933387756348, "The Latency of the ATL20 Arctic/Antarctic Gridded Sea Ice Freeboard Data is 45 days from receipt of last data in product."]
+[15.691960334777832, 9.764430046081543, "The Visible Spectral Range / Bandwidth of the SOLSPEC-ATLAS Spectrometer is 350-880/1.4/1."]
+[9.473875999450684, 12.40328598022461, "The Sigma 0 Range of the Radar Radar is HV, VH: +5~-35 dB."]
+[7.5093302726745605, 9.192745208740234, "The Material of the Bus Structure Satellite is Aluminum (AA2024-T3)."]
+[4.225706577301025, 9.088676452636719, "The Potential Repeat Cycle of the MSU-SK Radiometer is 3-5 days."]
+[10.570002555847168, 10.83587646484375, "The Swath Width of the SMMR Microwave Radiometer is Approximately 600 km."]
+[14.100336074829102, 9.83696174621582, "The Parasitic Bias of the Keithley 6430 Femtoammeter is <1 mV."]
+[5.8366618156433105, 7.417463779449463, "The Type of the SUCHAI-1 Satellite is 1U CubeSat."]
+[11.015266418457031, 10.73041820526123, "The Type of the POLDER-P Instrument is Radiometer/Polarimeter."]
+[12.23501968383789, 8.985971450805664, "The Surface Area of the CSS Coarse Sun Sensor is 2 cm2."]
+[5.086528301239014, 10.261551856994629, "The Launch Date of the 3U CubeSat Satellite is 23rd June 2017."]
+[7.293787479400635, 11.073139190673828, "The Flights of the AEPI Instrument is ATLAS-1."]
+[12.420886993408203, 10.033926963806152, "The Sensor Operating Temperature of the FIPEX Instrument is Approximately 660\u00b0C."]
+[13.573619842529297, 11.58632755279541, "The Effective Focal Length of the Telescope Optical Instrument is 1150 mm."]
+[7.022240161895752, 7.984255313873291, "The Dimensions of the QSat-EOS bus Microsatellite bus is 492 mm x 503 mm x 502 mm."]
+[9.294792175292969, 12.333179473876953, "The Frequency of the Radar Radar is X-Ku dual-frequency."]
+[6.3149237632751465, 9.330942153930664, "The Mission Number of the CubeSat Satellite is 17."]
+[9.454339027404785, 12.457252502441406, "The Bandwidth of the Radar Radar is 5 MHz."]
+[9.105140686035156, 9.986401557922363, "The Transmit and Receive Frequencies Offset of the Satellite Communication Device is 0.5 MHz in the 24 GHz channel, and by 0.67 MHz in the 32 GHz channel."]
+[5.216396808624268, 7.588404655456543, "The Type of the Aalto-1 Nanosatellite is 3U CubeSat."]
+[8.705029487609863, 9.912809371948242, "The Downlink Data Rate of the Payload Communication System is 278 Mbit/s."]
+[13.075519561767578, 10.891095161437988, "The Field of View of the A Photometer Instrument is 0.1o x 2.1o."]
+[5.969750881195068, 9.481391906738281, "The Operator of the Meteosat-7 Satellite is EUMETSAT."]
+[5.600190162658691, 7.008810043334961, "The Size of the MySat-1 CubeSat is 1U."]
+[11.539173126220703, 8.562687873840332, "The Range of the MAG Magnetometer is -350 nT to +350 nT."]
+[10.179871559143066, 11.075897216796875, "The Backscatter Coefficient Accuracy of the ALT Experiment Altimeter is 1.0 dB."]
+[11.669811248779297, 8.585314750671387, "The Time Resolution of the MAG Magnetometer is \u22640.1 s."]
+[12.352147102355957, 10.920621871948242, "The Power Consumption of the VIRR Instrument is 7.3 W."]
+[12.70262622833252, 9.34394645690918, "The Dose Measurement Range of the DDM Instrument Dosimetry System is Rad to Mrad."]
+[14.881813049316406, 10.15645694732666, "The Spectral Resolution of the Instrument Spectrometer is 10 nm, 12.5 nm."]
+[7.35366678237915, 11.490269660949707, "The Impact of the CATS Lidar Instrument is Enabled more accurate aerosol modeling and forecasting."]
+[6.124013900756836, 10.101569175720215, "The Ground Stations of the HYPSO-1 Satellite is NTNU Trondheim."]
+[12.599796295166016, 10.518514633178711, "The Dynamic Range (Infrared Channel) of the VIRR Instrument is 180-330 K (scene temperature)."]
+[11.894584655761719, 12.579032897949219, "The Horizontal Resolution of the Mie co-polar channel Channel is 10 km."]
+[7.452359676361084, 8.262816429138184, "The Type of the S/C Satellite is three-axis stabilized, zero-momentum satellite."]
+[13.305672645568848, 10.910041809082031, "The Field of View of the Lens Optical Instrument is 24\u00ba x 96\u00ba."]
+[11.314752578735352, 8.739217758178711, "The Manufacturer of the GMAG Magnetometer is NASA\u2019s Goddard Space Flight Center."]
+[6.437399864196777, 8.40946102142334, "The Orbit (Inclination) of the Spacecraft Satellite is 97.9\u00ba."]
+[6.922518253326416, 9.065657615661621, "The Number of Satellites of the MSG Satellite Fleet is 6."]
+[11.405776977539062, 8.639702796936035, "The Angular Resolution of the Vector Magnetometer Instrument is 1 arcsec."]
+[15.184808731079102, 9.822419166564941, "The Magnification of the HSC Spectrometer Spectrometer is 1:1."]
+[12.04770278930664, 11.15046215057373, "The Power Usage of the Instrument Device is < 4 W."]
+[6.032876014709473, 10.08953857421875, "The Ground Stations of the HYPSO-1 Satellite is KSAT Puertollano, Spain."]
+[7.636641025543213, 6.89119815826416, "The Li-ion Battery Capacity of the PARASOL microsatellite Satellite is 15 Ah."]
+[13.74215030670166, 11.634145736694336, "The Number of Mirror Shells per Module of the ART-XC Instrument Telescope is 28."]
+[7.458486080169678, 8.364785194396973, "The Mass of the SS 433 Cosmic Object is Millions to billions of times the mass of the Sun."]
+[10.153023719787598, 2.457470655441284, "The SCI ports of the STRV-1d DHS Data Handling System is Eleven RS-422."]
+[10.13938045501709, 2.434790849685669, "The PROM of the STRV-2 DHS Data Handling System is 32 k PROM."]
+[14.486538887023926, 10.186901092529297, "The Field of View Length of the Spectrometer Spectrometer is ~0.0146 radians."]
+[11.353559494018555, 8.731298446655273, "The Developer of the Magnetometer Sensor is GAUSS team."]
+[7.645576477050781, 7.349422931671143, "The Power Capacity of the Bus Satellite Component is 140 W."]
+[5.976139545440674, 10.914321899414062, "The Location of the ORBIMAGE Satellite Operations Center Satellite Operations Center is Dulles, VA."]
+[5.638443946838379, 7.004404067993164, "The Size of the CHEFSat-2 CubeSat is 3U."]
+[6.269775390625, 9.667622566223145, "The Launch Vehicle of the ALOS-2 Satellite is Mitsubishi vehicle - an H-IIA F24 bus."]
+[14.854314804077148, 10.397740364074707, "The Instrument Type of the AIRS Atmospheric Infrared Sounder is Multi-aperture, non-Littrow echelle array grating spectrometer configuration."]
+[5.576288223266602, 8.808899879455566, "The Fixed Distance from CALIPSO of the CloudSat Satellite is About 460 km."]
+[6.720043659210205, 9.45787239074707, "The Control Algorithm of the SV-1 Satellite is Problematic."]
+[5.772569179534912, 9.863324165344238, "The Operational Position of the GOES-S Satellite is 137.2\u00b0 West."]
+[5.779994964599609, 8.591657638549805, "The Orbit Altitude of the A-Train Satellite Constellation is Approximately 705 km."]
+[9.834748268127441, 10.978752136230469, "The Power of the RA-1 Antenna Antenna is \u2264 134.5 W."]
+[9.817276954650879, 8.44359016418457, "The Attitude Knowledge of the ACS Attitude Control Subsystem is \u00b10.02\u00ba."]
+[4.99134635925293, 11.407735824584961, "The Detector Type of the LISA Space Observatory is Gravitational Waves."]
+[10.370805740356445, 10.506312370300293, "The Operating Frequencies of the SMMR Microwave Radiometer is  37.0 GHz."]
+[7.681744575500488, 6.9010701179504395, "The Battery Type of the SENSE Satellite is Li-Ion."]
+[7.132443428039551, 7.713043212890625, "The Propellant of the Busek\u2019s miniaturized electric thrusters Propulsion System is Iodine."]
+[4.985674858093262, 10.57045841217041, "The Launch Date of the Sentinel-3 Satellite is 2013."]
+[6.905584335327148, 7.672305107116699, "The Isp of the Hydrazine system Orbit control subsystem is 210 s."]
+[11.952669143676758, 11.842048645019531, "The Standard Interface of the CEASE-2 Instrument is RS-422 or MIL-STD-1553B."]
+[7.442075729370117, 7.102433204650879, "The Payload Power of the DSX Spacecraft Payload Module Satellite is 350 W, 1.1 kW."]
+[11.399296760559082, 8.586665153503418, "The Range of the Magnetometers Actuator is \u00b10.2 Am 2."]
+[6.023452281951904, 7.486289024353027, "The Mass at Launch of the PARASOL microsatellite Satellite is 120 kg."]
+[9.17806625366211, 7.133257865905762, "The Carbon Temperature of the Sun's Lower Atmosphere Celestial Body is 32,000\u00baC."]
+[-3.366084575653076, 11.240883827209473, "The Latency of the ATL11 Antarctica/Greenland Ice Sheet H(t) Series Data is 45 days from receipt of last data in product."]
+[5.214427471160889, 7.550863742828369, "The Developer of the Venta-1 Nanosatellite is OHB Systems."]
+[-3.369811773300171, 11.251057624816895, "The Latency of the ATL08 Land Water Vegetation Elevation Data is 45 days."]
+[9.496746063232422, 8.188162803649902, "The Inclination Accuracy of the Bloostar Launch Vehicle is \u00b10.05\u00ba."]
+[5.29998254776001, 10.2389497756958, "The Launch Date of the Meteosat-1 Satellite is November 23, 1977."]
+[11.861496925354004, 12.56618881225586, "The Vertical Resolution of the Mie co-polar channel Channel is 100 m."]
+[10.998292922973633, 12.110445976257324, "The Interchangeable Barrels Sizes of the Launcher Test Facility is 84 mm, 102 mm, and 203 mm."]
+[5.9860687255859375, 8.664400100708008, "The Orbit Altitude of the Monitor-E Spacecraft is 540 km."]
+[4.960476875305176, 10.354517936706543, "The Full Year in Orbit of the COMS Satellite is Late summer of 2011."]
+[10.087667465209961, 2.4861648082733154, "The Radiation hardness of the STRV-2 DHS Data Handling System is about 100 krad."]
+[13.595698356628418, 8.892559051513672, "The Pixel Size of the Detector Imaging Device is 15 \u00b5m."]
+[9.22030258178711, 10.237798690795898, "The RF Output Power of the EWC31 S-band transceiver module Communication Module is +27 to +33 dBm."]
+[7.622848033905029, 10.247567176818848, "The Fault Tolerant Software Developer of the FPGA Component is UFRGS (Universidade Federal do Rio Grande do Sul)."]
+[11.658487319946289, 11.787705421447754, "The Principal Investigator of the TEMPO Instrument is Kelly Chance."]
+[8.78550910949707, 9.953723907470703, "The Downlink Speed of the Communication links Communication System is 9.6 - 38.4 kbit/s."]
+[13.89235782623291, 8.547196388244629, "The Cadence of the Fast Cameras Camera is 2.5 seconds."]
+[10.841185569763184, 7.7265191078186035, "The Testing Environment of the CuPID spacecraft Spacecraft is Helmholtz cage."]
+[8.793587684631348, 10.033756256103516, "The Ground Stations Downlink Data Rate of the Payload Communication System is X-band at 800, 400, or 200 Mbit/s."]
+[10.72891902923584, 11.316265106201172, "The Resolution of the Interferometric Wide Swath mode (IWS) Operational Mode is 25 m x 80 m."]
+[11.923393249511719, 11.756105422973633, "The Telemetry of the CEASE-2 Instrument is 10 byte/min."]
+[7.805972576141357, 10.18423843383789, "The Software of the OBC On-Board Computer is FCS (Flight Control Software)."]
+[6.260527610778809, 7.232937335968018, "The Weight of the SUCHAI-1 Satellite is 1 kg."]
+[12.681922912597656, 10.573090553283691, "The Ground Resolution (Infrared Channel) of the VIRR Instrument is 4.4 km."]
+[8.17611026763916, 7.471858501434326, "The Mass of the PCU Power Control Unit is Low."]
+[10.63465690612793, 11.298810005187988, "The Swath of the Interferometric Wide Swath mode (IWS) Operational Mode is 240 km."]
+[13.099251747131348, 10.170113563537598, "The Optical System of the OCTS Sensor is Catoptric."]
+[6.713723182678223, 10.125221252441406, "The Mission Lead of the SORTIE Satellite is ASTRA LLC."]
+[10.888400077819824, 7.402174472808838, "The Area Collection Rate of the Push Frame Framer with a fast steering mirror Sensor is Low."]
+[6.660415172576904, 9.853011131286621, "The Manufacturer of the CIRiS CubeSat is Utah State University."]
+[5.144225597381592, 7.658329486846924, "The Developer of the Aalto-1 Nanosatellite is Aalto University."]
+[11.99315071105957, 11.403101921081543, "The Mass of the MI Radiometer Instrument is 139 kg."]
+[14.4146728515625, 10.624497413635254, "The Slit Width of the Spectrometer Spectrometer is 25 \u00b5m."]
+[6.498829364776611, 7.707671642303467, "The Printed Circuit Board Area of the Sprite Tiny Spacecraft is 3.5 by 3.5 cm."]
+[9.526679992675781, 12.497429847717285, "The Swath Width of the X-band Radar is 450 km."]
+[5.904399871826172, 11.026244163513184, "The Operator of the OrbView-1 Satellite is Orbital Imaging Corporation (ORBIMAGE)."]
+[4.5272064208984375, 8.85575008392334, "The Repeat Cycle of the Satellite Imaging Satellite is 12 days."]
+[10.778535842895508, 9.517716407775879, "The Number of Accelerometers of the Truss Structure is 22."]
+[12.258586883544922, 11.20245361328125, "The Performance of the CSS Instrument is \u00b10.115\u00ba."]
+[15.667539596557617, 10.84660530090332, "The Wavelength Range of the Band 3 Spectral Band is 862-877 nm."]
+[11.937835693359375, 11.982367515563965, "The Size of the Instrument Device is 9.7 cm x 9.7 cm x 4.8 cm."]
+[5.0732903480529785, 11.258610725402832, "The Landing Date of the Falcon 9 first stage Rocket is Jan. 11, 2015."]
+[4.41957426071167, 8.523179054260254, "The TLE Generation of the Orbit Dynamic System System is By mean processing of a 6 lap orbit."]
+[8.334870338439941, 9.793526649475098, "The Processing Capability of the Processor Satellite Component is 14 MIPS."]
+[8.337577819824219, 9.466005325317383, "The Downlink of the Image Location Knowledge Satellite Component is < 300 m."]
+[7.307912349700928, 11.43868350982666, "The Mission Duration of the CATS Lidar Instrument is 33 months."]
+[9.145583152770996, 10.152865409851074, "The Operating Frequency Range (TM) of the EWC31 S-band transceiver module Communication Module is 2200-2290 MHz."]
+[6.4292311668396, 10.068713188171387, "The Launch Provider of the MethaneSAT Satellite is SpaceX."]
+[4.649653911590576, 9.030119895935059, "The Frequency of the EMOC Process is Monthly."]
+[14.065587997436523, 8.5401611328125, "The Power Consumption of the Image Sensor Imaging is 1 W."]
+[10.113598823547363, 2.4677047729492188, "The Analog channel of the STRV-2 DHS Data Handling System is None."]
+[10.905383110046387, 11.177901268005371, "The Resolution of the MSU-M Multispectral Scanner is 1.0 km x 1.7 km."]
+[8.595170021057129, 9.72777271270752, "The Downlink Data Rate of the Satellite Satellite is 115.2 kbit/s."]
+[10.894381523132324, 7.379129409790039, "The Cost (sensor + spacecraft) of the Pushbroom Sensor is High."]
+[10.925212860107422, 10.77657413482666, "The Type of the MLS Instrument is Microwave radiometer."]
+[7.118892192840576, 7.19118595123291, "The Payload Mass (max) of the  DSX Spacecraft Payload Module Satellite is 170 kg."]
+[10.372629165649414, 10.499131202697754, "The Operating Frequencies of the SMMR Microwave Radiometer is 6.6 GHz."]
+[7.892512321472168, 10.528523445129395, "The Build Location of the Hardware Quick Look SAR Processor SAR Processor is Ahmedabad."]
+[14.04973030090332, 9.9652681350708, "The Spectral Resolution (60 keV) of the Detector Instrument is 1.0 keV."]
+[7.033503532409668, 7.1204094886779785, "The AM Mass of the DSX Spacecraft Payload Module Satellite is  180 kg."]
+[11.04295825958252, 10.171162605285645, "The Provider of the STM Sensor is MSSL (Mullard Space Science Laboratory) of Belgium."]
+[12.07686996459961, 8.840686798095703, "The Error (RMS) of the Sun sensor Sensor is <0.2\u00ba."]
+[10.949775695800781, 11.04215145111084, "The Spatial Resolution of the SLSTR Imaging Device is 500 m."]
+[9.151094436645508, 7.141051769256592, "The Peak Temperature of the Orion Spacecraft is 2,200\u00b0C."]
+[6.587214946746826, 10.55461597442627, "The Manager of the Chandra Program is NASA's Marshall Space Flight Center."]
+[14.536222457885742, 10.224752426147461, "The Dynamic Range of the Instrument Spectrometer is Saturated at \u226570% albedo."]
+[14.400742530822754, 9.0703125, "The Optical Gains of the Limb Sensor Sensor is Two."]
+[7.647380352020264, 6.957327842712402, "The Battery Capacity of the Spacecraft Bus (Avionics Module=AM) Satellite is 60 Ah."]
+[6.883225917816162, 9.192205429077148, "The Number of Verified Fragments of the DebriSat project Satellite is Close to 3,000."]
+[6.500030517578125, 8.013810157775879, "The Solar Panels Span of the INTEGRAL Satellite is 16 m."]
+[13.451350212097168, 11.098478317260742, "The Focal Ratio of the Lens Optical Instrument is f/1.4."]
+[6.517206192016602, 10.67325496673584, "The Landing Site of the InSight Spacecraft is Homestead hollow in Elysium Planitia."]
+[7.357885360717773, 11.476505279541016, "The Data Availability of the CATS Lidar Instrument is Freely available."]
+[5.2917399406433105, 11.187143325805664, "The ADCS Malfunction Date of the Monitor-E Spacecraft is Feb. 2007."]
+[4.49998140335083, 9.484174728393555, "The Mission Design Life of the ADEOS spacecraft Satellite is 3 years."]
+[9.495792388916016, 12.136600494384766, "The Reception of the Receive Chain Radar Instrument is Either H or V."]
+[4.338364601135254, 9.51796817779541, "The Lifetime of the Mission Satellite Mission is 3 years."]
+[9.486071586608887, 11.72555923461914, "The Radar Frequency of the SeaWinds Scatterometer Scatterometer is 110 W pulse at 189 Hz pulse repetition frequency (PRF)."]
+[6.637529373168945, 10.409335136413574, "The Scientific Goal of the TanSat Satellite is Improve the understanding on the global CO2 distribution and its contribution to the climate change, and also to monitor the CO2 variation on seasonal time scales."]
+[10.750490188598633, 11.87102222442627, "The Diameter of the Antenna Instrument is 1 m."]
+[7.263508319854736, 9.880142211914062, "The Platform of the Intelsat 40e Satellite is Maxar's 1300-class."]
+[7.576113224029541, 6.853225231170654, "The Battery Capacity of the DSX Spacecraft Payload Module Satellite is 60 Ah."]
+[15.720667839050293, 10.919445991516113, "The Wavelength Range of the Band 4 Spectral Band is 1360-1390 nm."]
+[7.81427526473999, 10.570953369140625, "The Manufacturer of the Near Real Time SAR Processor SAR Processor is MRSA/SAC team."]
+[4.428524494171143, 9.551565170288086, "The Design Life of the S/C Satellite is One year."]
+[14.861248970031738, 10.5675630569458, "The Type of the Spectrographs Optical Instrument is Aberration-corrected Offner-type."]
+[7.436295986175537, 11.226533889770508, "The Manufacturer of the ATLID Lidar Instrument is Airbus DS."]
+[4.359434127807617, 8.705906867980957, "The LTAN of the Satellite Satellite is 10:00 - 14:00 hours."]
+[-3.4024977684020996, 11.281938552856445, "The Latency of the ATL09 ATLAS Atmosphere Cloud Layer Characteristics Data is 45 days."]
+[9.755657196044922, 12.313796043395996, "The Transmission Frequency of the SAR Synthetic Aperture Radar is 1.275 GHz."]
+[11.477326393127441, 8.970182418823242, "The Quantity of the Magnetometers AOCS Sensors is 2."]
+[15.18237590789795, 10.614325523376465, "The Number of Bands of the Optical Scanning Design Imaging Spectrometer is 21 bands (nominal Earth View)."]
+[-3.2827608585357666, 11.161430358886719, "The Latency of the ATL06 Land Ice Height Data is 45 days."]
+[9.816468238830566, 8.428653717041016, "The Attitude Accuracy of the Attitude and Orbit Control Subsystem Subsystem is 0.4\u00ba in roll and pitch."]
+[9.194917678833008, 7.1163177490234375, "The Neon Temperature of the Sun's Lower Atmosphere Celestial Body is 630,000\u00baC."]
+[-3.4699792861938477, 11.3525390625, "The Latency of the ATL01 Reformatted Telemetry Data is 2 days."]
+[5.8218255043029785, 8.8209810256958, "The Altitude of the Meteosat-7 Satellite is 35,786 km."]
+[11.019890785217285, 11.206377029418945, "The Bands of the Multispectral Instrument (MSI) Instrument is 13."]
+[12.908315658569336, 8.888078689575195, "The SRAMs Memory of the RADMON Radiation Monitor is 4-kbit each."]
+[6.064524173736572, 10.26134967803955, "The Location of the CryoVEx Campaign is Arctic."]
+[13.964300155639648, 11.008376121520996, "The Gap of the Slits Optical Instrument is 30 \u00b5m."]
+[11.059178352355957, 10.424962997436523, "The Uniformity of Absorber Surface of the HTS/AMSR2 Microwave Absorber is 2.5\u00baCp-p."]
+[11.192997932434082, 10.514093399047852, "The Pointing Requirements (Knowledge) of the Aquarius Radiometer System is 0.1\u00ba."]
+[11.621280670166016, 8.605585098266602, "The Error (RMS) of the Magnetometers Actuator is <0.0005 Am 2."]
+[9.823351860046387, 12.269463539123535, "The Look Angle of the SAR Synthetic Aperture Radar is 20\u00ba."]
+[4.4855146408081055, 9.756009101867676, "The Storage Capacity of the GOES-R Access System Data Distribution System is Seven days."]
+[5.43716287612915, 11.389233589172363, "The Sensitivity of the LIGO/Virgo sensors Sensors is Improved."]
+[10.687745094299316, 10.588519096374512, "The Bandwidth of the MWR Radiometer is 1 GHz."]
+[5.104822635650635, 11.381239891052246, "The Landing Location of the Falcon 9 first stage Rocket is Autonomous spaceport drone ship."]
+[5.626133918762207, 6.965139389038086, "The Size of the Flock-1c CubeSat is 3U."]
+[7.720932483673096, 6.806289196014404, "The Type of the Lithium ion battery Power Source is Rechargeable."]
+[15.210299491882324, 10.467508316040039, "The Number of Individual Scans of the SPICE Instrument is 25."]
+[13.465202331542969, 11.478103637695312, "The Spatial Scale of the Telescope Optical Instrument is 2.8 arcsec/pixel."]
+[8.953163146972656, 10.185979843139648, "The Frequency Band of the RF Communications Communication System is X-band for the payload data downlink."]
+[4.87570858001709, 10.184639930725098, "The Launch Date of the Gokturk-2 Satellite is Dec. 18, 2012."]
+[6.740358352661133, 10.665684700012207, "The Mission Scientist of the CO2M Satellite is Yasjka Meijer."]
+[5.298573970794678, 8.704933166503906, "The Celestial Sphere Coverage of the Spacecraft Satellite is 50% during the extended mission phase."]
+[13.305961608886719, 10.542604446411133, "The FOV of the Microdosimeter A Instrument is 38\u00ba."]
+[6.125550746917725, 10.744498252868652, "The Flight Operations Location of the Chandra X-ray Center Center is Burlington, Massachusetts."]
+[12.08852481842041, 11.02083683013916, "The Performance of the MTQ Instrument is 0-4 Nms."]
+[13.550725936889648, 11.662055969238281, "The Stray Light/Sun Disk Light Rejection of the Telescope Optical Instrument is 5 x 10^8."]
+[9.462935447692871, 12.411211013793945, "The Frequency of the Radar Radar is 17 GHz."]
+[13.719099044799805, 8.643136024475098, "The Field of View of the Z-panel camera Camera is 25o."]
+[12.440836906433105, 11.521865844726562, "The Mass of the VIRR Instrument is 8.1 kg."]
+[10.8066987991333, 11.412978172302246, "The Azimuth Resolution of the P Mode Observation Mode is 1 m."]
+[6.067477226257324, 10.089332580566406, "The Earth Station Location of the WINDS Satellite is Higashimatsushima."]
+[14.63593864440918, 8.514625549316406, "The Central Wavelength of the Current GOES imager Sensor is 3.90."]
+[4.4657158851623535, 9.429015159606934, "The Operational Duration of the Jason-3 Satellite is More than 25 years."]
+[11.917952537536621, 11.945276260375977, "The Size of the CEASE-1 Instrument is 10 cm x 10 cm x 8.2 cm."]
+[11.490863800048828, 8.498414039611816, "The DC Measurement Uncertainty of the Magnetometer Instrument is 14 nT."]
+[5.499654769897461, 8.781346321105957, "The Footprint Distance of the CloudSat and CALIPSO Satellites is Always within 2 km."]
+[10.106511116027832, 2.47300386428833, "The CPU of the STRV-2 DHS Data Handling System is 8086 rad-hard."]
+[4.680650234222412, 8.502764701843262, "The Speed Before Jettisoning of the Orion Spacecraft is 480 km/hr."]
+[14.341279983520508, 10.652607917785645, "The Slit Length of the Spectrometer Spectrometer is 3 mm."]
+[10.845643997192383, 10.67050838470459, "The Bandwidth of the MWR Radiometer is 500 MHz."]
+[12.29744815826416, 11.627640724182129, "The Mass of the CEASE-1 Instrument is 1 kg."]
+[11.070022583007812, 10.667134284973145, "The Incidence Angles of the MWR Dicke Radiometer is between 52\u00ba and 58\u00ba."]
+[6.620798110961914, 8.152864456176758, "The Size of the GRACE-FO satellites Satellite is 3 m x 3 m x 0.8 m."]
+[11.874436378479004, 12.587934494018555, "The Backscatter of the Mie co-polar channel Channel is 8 x 10 -7 sr -1 m -1."]
+[6.728351593017578, 10.752805709838867, "The Testing Facility of the CO2M Satellite is Largest satellite test facility in Europe."]
+[14.651077270507812, 8.46476936340332, "The Central Wavelength of the Current GOES imager Sensor is 6.95."]
+[15.306021690368652, 10.507566452026367, "The Wavelength Region of the Instrument Spectrometer is 400-970 nm (57 bands), 900-2500 nm (128 bands)."]
+[8.417240142822266, 9.40461540222168, "The Position Knowledge of the GPS Receiver Satellite Component is \u00b160 m."]
+[7.164712429046631, 10.197486877441406, "The Reorganization Date of the Maxar Space Solutions Company is February."]
+[10.659883499145508, 9.38418960571289, "The Number of Sub-Processes of the EMOC Process is Five."]
+[9.814216613769531, 12.38553237915039, "The Swath Width of the SAR Synthetic Aperture Radar is 100 km."]
+[6.335693836212158, 8.390819549560547, "The Orbit Inclination of the 3U CubeSat Satellite is 97.44\u00ba."]
+[9.919548988342285, 12.146316528320312, "The Wavelength of the SAR antenna Antenna is ~ 10 cm."]
+[4.740056037902832, 8.848058700561523, "The Image Frequency of the TESS Satellite is Every 30 minutes."]
+[15.739895820617676, 10.79514217376709, "The Number of Pixels of the Band 5 Spectral Band is 800."]
+[6.476768493652344, 9.946317672729492, "The Ground Segment Chain of the Deimos-2 Satellite is Data processing chain."]
+[13.547468185424805, 8.62680721282959, "The Number of Pixels of the Image Sensor Imaging is 4008 x 2672."]
+[13.813944816589355, 11.468047142028809, "The Field of View of the ART-XC Instrument Telescope is 0.3\u00ba x 0.3\u00ba."]
+[13.860174179077148, 10.737822532653809, "The Smile of the System Optical System is Less than 0.5 \u00b5m."]
+[7.623797416687012, 7.215390682220459, "The Payload Power of the Spacecraft Bus (Avionics Module=AM) Satellite is 350 W, 1.1 kW."]
+[6.10625696182251, 10.08885383605957, "The Ground Station of the HYPSO-1 Satellite is KSAT Svalbard, Norway."]
+[13.597115516662598, 8.601181983947754, "The Resolution of the Z-panel camera Camera is 3 Mpixel."]
+[4.516439914703369, 8.806196212768555, "The Observation Duration of the Integral Satellite is Four weeks."]
+[14.613469123840332, 10.132969856262207, "The Radiometric Accuracy of the Optical Scanning Design Imaging Spectrometer is <2% with reference to the sun."]
+[5.20883846282959, 10.814143180847168, "The Launch Date of the OSCAT Scatterometer is September 2009."]
+[10.095885276794434, 2.4777915477752686, "The Radiation hardness of the STRV-1d DHS Data Handling System is about 100 krad."]
+[13.389976501464844, 9.692355155944824, "The Spectral Range of the VNIR-NP channels Sensor is 380 nm to 865 nm."]
+[4.57551383972168, 8.856449127197266, "The Orbit (number of cycles/day) of the Spacecraft Satellite is 15 3/14."]
+[10.85307788848877, 7.427433967590332, "The Required Spacecraft Stability of the Push Frame Framer with a fast steering mirror Sensor is Low."]
+[5.635546684265137, 8.001260757446289, "The Solar Array Efficiency of the PARASOL microsatellite Satellite is 26%."]
+[15.111175537109375, 9.883849143981934, "The Spectral Sampling Interval of the HSC Spectrometer Spectrometer is 5 nm."]
+[14.64799690246582, 8.848957061767578, "The Central Wavelength of the AVHRR/3 Sensor is 2.25."]
+[13.201055526733398, 9.784247398376465, "The FOV for SWIR/TIR for whiskbroom scanning of the VNIR-NP Imager is 80\u00ba."]
+[10.866898536682129, 7.40427827835083, "The Required Spacecraft Stability of the Pushbroom Sensor is High."]
+[7.154776096343994, 7.967470169067383, "The Slew Rate of the  Spacecraft Bus (Avionics Module=AM) Satellite is 0.25 to 1.0\u00ba/s."]
+[5.15792989730835, 10.17712116241455, "The Release Date of the CubeSat Satellite is February 19."]
+[5.594318866729736, 10.590376853942871, "The Year of the CryoVEx Campaign is 2003."]
+[6.729969501495361, 10.269261360168457, "The Prime Contractor of the Spacecraft Satellite is Alenia Spazio."]
+[15.671765327453613, 10.945526123046875, "The Polarization Angle of the Band 2 Spectral Band is 0/60/120 \u00ba."]
+[13.52432918548584, 8.29407024383545, "The Pixel Count of the Kodak KAI-11002 CCD CCD is 11M pixel."]
+[9.846056938171387, 12.12514591217041, "The Number of Phase Centers of the SAR antenna Antenna is 18."]
+[11.518082618713379, 8.543910026550293, "The Absolute Measurement Error of the Vector Magnetometer Instrument is Less than 1 nT."]
+[9.703205108642578, 12.435840606689453, "The Aperture Dimension of the Radar Radar is Approximately 1.5 m."]
+[5.600825309753418, 6.98784065246582, "The Size of the PACE CubeSat is 2U."]
+[5.741037368774414, 8.748109817504883, "The Oceanic Crust Thickness of the Earth Planet is About 6 to 7 kilometers."]
+[15.729065895080566, 10.771007537841797, "The Number of Pixels of the Band 2 Spectral Band is 1600."]
+[14.680290222167969, 8.943588256835938, "The Spectral Range of the AVHRR/3 Sensor is 2.225-2.275."]
+[5.1793951988220215, 7.617570400238037, "The Developer of the Venta-1 Nanosatellite is Ventspils University College."]
+[6.748240947723389, 10.777422904968262, "The Test Location of the CO2M Satellite is ESA\u2019s Test Centre in the Netherlands."]
+[9.830160140991211, 12.32256031036377, "The Pixel Size of the SAR Synthetic Aperture Radar is 25 x 25 m."]
+[13.755834579467773, 8.668726921081543, "The Star Magnitude Range of the Normal Cameras Camera is Fainter than mV = 8."]
+[13.894489288330078, 10.411571502685547, "The Active Area of the X123-SDD X-ray Spectrometer is 25 mm2."]
+[4.299398422241211, 9.526701927185059, "The Mission Lifetime of the Instrument Spectrometer is 7.5 years."]
+[5.103696823120117, 10.398615837097168, "The Launch Date of the RADARSAT-2 Satellite is 2007."]
+[5.777065277099609, 11.368762969970703, "The Deployment Date on Mars of the Seismic Experiment for Interior Structure (SEIS) Seismometer is Late 2018."]
+[13.536375045776367, 8.54842472076416, "The Ground Pixel Size of the VIS Camera Camera is ~100 m."]
+[10.960094451904297, 7.379672527313232, "The Area Collection Rate of the Framer Sensor is Very low."]
+[12.4454345703125, 10.025128364562988, "The Sensor Type of the FIPEX Instrument is Solid oxide electrolyte micro-sensors."]
+[7.463082790374756, 7.549223899841309, "The Instrument Support Capacity of the Bus Satellite Component is Up to 206 kg."]
+[8.955547332763672, 10.026519775390625, "The Data Rates (TM) of the EWC31 S-band transceiver module Communication Module is 10 kbit/s to 1 Mbit/s."]
+[7.664377689361572, 10.483123779296875, "The Designer of the Driver on/off IC Component is Santa Maria Design House."]
+[9.081605911254883, 9.858967781066895, "The Phase Change Sample Rate of the Satellite Communication Device is 10 Hz."]
+[10.672977447509766, 9.902037620544434, "The Number of Micro-g Accelerometers of the Boom Structure is 24."]
+[5.24627685546875, 8.164335250854492, "The Mission Design Life of the PARASOL microsatellite Satellite is One year."]
+[5.105140686035156, 11.442380905151367, "The Sensitivity of the LISA Space Observatory is Lower frequency than LIGO."]
+[11.801376342773438, 11.839027404785156, "The Telemetry of the CEASE-1 Instrument is 10 byte/min."]
+[6.881435394287109, 10.862138748168945, "The Payload Instruments of the Chibis-M Microsatellite is \"Thunderstorm\" and \"Wave Package\"."]
+[6.0339579582214355, 11.061286926269531, "The Remarks/Sensors of the OrbView-2 Satellite is SeaWiFS."]
+[13.785260200500488, 11.304204940795898, "The Energy Range of the ART-XC Instrument Telescope is 5 to 30 keV."]
+[10.133650779724121, 2.447614908218384, "The PROM of the STRV-1d DHS Data Handling System is 32 k PROM."]
+[4.962613105773926, 10.885973930358887, "The Launch Date of the Meteor-M-2 Satellite is 08 Jul 2014."]
+[7.594475269317627, 7.254329204559326, "The Power Consumption of the Satellite Satellite is 270 W."]
+[11.438047409057617, 11.797698974609375, "The Mass of the IPEX-II boom ADAM mast is 112 kg."]
+[7.328379154205322, 11.371968269348145, "The Development Location of the ATLID Lidar Instrument is Selex-Galileo, Florence, Italy."]
+[6.663399696350098, 7.953660488128662, "The Size of the ADEOS spacecraft Satellite is 4 m x 4 m x 5 m."]
+[12.523274421691895, 11.422812461853027, "The Performance of the ST (Star Tracker) Instrument is 10 arcsec."]
+[9.51911735534668, 11.676609992980957, "The Radar Frequency of the SeaWinds Scatterometer Scatterometer is 13.4 GHz (Ku-band)."]
+[7.654936790466309, 10.423910140991211, "The Designer of the Driver IC Component is Brazilian software house located on the campus of UFSM (Federal University of Santa Maria)."]
+[12.41240119934082, 9.988226890563965, "The Provider of the FIPEX Sensor is Institute of Aerospace Engineering of TU Dresden, Germany."]
+[4.9796600341796875, 11.219447135925293, "The Expected Launch Date of the LISA Space Observatory is 2034."]
+[7.702376842498779, 9.74725341796875, "The Model of the Processor Satellite Component is TEMIC TSC695 32-bit RISC processor."]
+[5.802175045013428, 7.962484836578369, "The Solar Power of the PARASOL microsatellite Satellite is 180 W."]
+[5.802975654602051, 8.677255630493164, "The Altitude of the Satellite Satellite is 500-700 km."]
+[6.455306529998779, 10.352858543395996, "The Prime Minister of India of the OneWeb Satellite Communications Company is Narendra Modi."]
+[11.523757934570312, 8.476438522338867, "The Magnetic Field Strength of the 1E1547.0-5408 Magnetar is 1014G -1015G."]
+[10.08272647857666, 2.4951205253601074, "The CPU of the STRV-1d DHS Data Handling System is 8051 rad-hard."]
+[13.492916107177734, 8.243391990661621, "The Size of the Kodak KAI-11002 CCD CCD is 37.25 mm (H) by 25.7 mm (V)."]
+[14.260503768920898, 9.83365535736084, "The Detector Array of the SCIAMACHY Spectrometer is 1024-pixel."]
+[13.455792427062988, 9.192402839660645, "The Swath Width of the OLS Imaging Sensor is 2960 km."]
+[8.108019828796387, 7.523984432220459, "The Data Bus Interface of the PCU Power Control Unit is SpaceWire type."]
+[5.941228866577148, 11.017667770385742, "The Remarks/Sensors of the OrbView-3 Satellite is commercial imaging PAN +MS."]
+[13.228608131408691, 9.762913703918457, "The FOV for VNIR-NP pushbroom scanning of the VNIR-NP Imager is 70\u00ba."]
+[7.494126796722412, 7.5821213722229, "The Delta-V Capacity of the Bus Satellite Component is More than 154 m/s."]
+[13.529953956604004, 10.242350578308105, "The Electron energy of the Microdosimeter B Instrument is > 50 keV."]
+[6.622016906738281, 8.04008674621582, "The Size of the Spacecraft Satellite is 9.9 m (x) x 16.5 m (y) x 3.7 m (z)."]
+[13.793069839477539, 11.830718040466309, "The Type of the Telescope Optical Instrument is Off-axis three mirror anastigmat type (TMA)."]
+[6.843441486358643, 10.806921005249023, "The Testing Location of the CO2M Satellite is ESA\u2019s ESTEC testing facilities in the Netherlands."]
+[15.866662979125977, 10.883936882019043, "The SNR of the Band 2 Spectral Band is 160."]
+[13.95823860168457, 10.4383544921875, "The TEC of the X123-SDD X-ray Spectrometer is Active 2 stage."]
+[10.129316329956055, 2.4483282566070557, "The Power of the STRV-1d DHS Data Handling System is 3 W."]
+[7.226920127868652, 10.108001708984375, "The Acquisition of the Maxar Technologies Company is Vricon."]
+[7.47189474105835, 7.121188640594482, "The Array Power Average of the DSX Spacecraft Payload Module Satellite is 650 W."]
+[5.13744592666626, 7.639079570770264, "The Developer of the ROBUSTA-1B Nanosatellite is University of Montpellier students."]
+[4.688625335693359, 9.046000480651855, "The Reentry Time of the 3U CubeSat Satellite is 72 days."]
+[9.038959503173828, 10.270069122314453, "The Frequency Band of the RF Communications Communications is S-band."]
+[11.078444480895996, 8.775235176086426, "The Range of the Pitch momentum wheel Actuator is \u00b11.7 mNms."]
+[7.353240489959717, 8.585897445678711, "The Type of the Andromeda Galaxy is Spiral."]
+[5.417891979217529, 11.011696815490723, "The Launch Date of the OrbView-1 Satellite is April 1, 1995."]
+[13.507237434387207, 8.907143592834473, "The Size of the Detector Imaging Device is 2048 x 2048 pixels."]
+[7.335653781890869, 11.459756851196289, "The Funding Source of the CATS Lidar Instrument is International Space Station Program."]
+[6.5901994705200195, 10.890104293823242, "The Role of the Jason-3 Satellite is High Precision Ocean Altimetry reference mission."]
+[11.27595329284668, 8.6846342086792, "The Manufacturer of the Vector Magnetometer Instrument is DRSI (Danish Space Research Institute)."]
+[9.382192611694336, 12.422921180725098, "The Wavelength/Frequency of the X-band Radar is 32 mm/9.7 GHz."]
+[14.470532417297363, 9.245548248291016, "The Spectral Resolutions (FWHM) of the Limb Sensor Sensor is 0.75 nm at 290 nm to 25 nm at 1000 nm."]
+[14.489992141723633, 10.190027236938477, "The Field of View Width of the Spectrometer Spectrometer is ~0.0001 radians."]
+[15.202220916748047, 9.884175300598145, "The Spectral Range of the HSC Spectrometer Spectrometer is 450-1000 nm."]
+[13.46418285369873, 8.494839668273926, "The Image Size of the Imager Camera is 37.25 mm x 25.70 mm."]
+[6.7889628410339355, 9.964509963989258, "The Mission Funding of the SORTIE Satellite is NASA Heliophysics Technology and Instrument Development (H-TIDeS) program grant."]
+[7.367756366729736, 11.49196720123291, "The Purpose of the CATS Lidar Instrument is Measure clouds and aerosols."]
+[5.042651176452637, 10.208467483520508, "The Launch Date of the GOES-S Satellite is March 2018."]
+[11.43454647064209, 10.809776306152344, "The Power Consumption of the MWR Dicke Radiometer is 96 W."]
+[15.694415092468262, 10.789447784423828, "The Number of Pixels of the Band 4 Spectral Band is 800."]
+[14.6277494430542, 8.559752464294434, "The Spectral Range of the Current GOES imager Sensor is 7.24-7.44."]
+[14.083369255065918, 8.498541831970215, "The Peak Quantum Efficiency of the Image Sensor Imaging is 50%."]
+[6.782419204711914, 10.90981388092041, "The Instrument type of the Meteor-M-2 Satellite is Imaging multi-spectral radiometers (vis/IR), Space environment, Imaging multi-spectral radiometers (passive microwave), Data collection, Imaging microwave radars, Atmospheric temperature and humidity sounders."]
+[7.93440055847168, 10.615683555603027, "The Build Location of the Near Real Time SAR Processor SAR Processor is Ahmedabad."]
+[7.838009834289551, 10.152995109558105, "The Redundancy of the C&DH Subsystem Control System is One OBC is redundant, two TMC are redundant."]
+[14.019241333007812, 10.188793182373047, "The Detector Array of the X-ray Spectrometer Spectrometer is 36-pixel."]
+[6.355932235717773, 8.535771369934082, "The Orbit Inclination of the Sentinel-2 satellites Satellite is 98.6\u00b0."]
+[4.133683204650879, 9.397769927978516, "The Data Analysis and Validation Duration of the GP-B mission Mission is Approximately 1 1/2 years."]
+[11.99585247039795, 10.06268310546875, "The Atomic Clock Panel Temperature Control of the Thermal Control Subsystem Thermal Control is Within 0.4\u00ba C."]
+[12.321175575256348, 11.613055229187012, "The Mass of the Instrument Device is 600 g."]
+[5.074887275695801, 10.800557136535645, "The Operational Date of the Scanning Sky Monitor (SSM) Payload is October 12th, 2015."]
+[11.94093132019043, 10.07855224609375, "The Cryogen Volume of the Instrument Dewar/Heat Exchanger is 944 liter."]
+[5.286269664764404, 8.198351860046387, "The Hydrazine Duration of the PARASOL Satellite is > 10 years."]
+[6.192719459533691, 10.71839714050293, "The Science Control Location of the Chandra X-ray Center Center is Cambridge, Massachusetts."]
+[8.710400581359863, 9.870180130004883, "The Downlink communications (X-band) of the Spacecraft Satellite is 800 Mbit/s (16 QAM), 400/200 Mbit/s (QPSK)."]
+[5.040052890777588, 11.115403175354004, "The Splashdown Date of the Orion Spacecraft is Dec. 5, 2014."]
+[4.766293525695801, 9.235886573791504, "The Data Release of the TESS Satellite is Sectors 1 and 2, observed between July 25 and September 20, 2018."]
+[10.864816665649414, 7.428022861480713, "The Required Spacecraft Stability of the Framer Sensor is Low."]
+[9.510407447814941, 11.491579055786133, "The Direction Accuracy of the SeaWinds scatterometer Scatterometer is 20\u00ba."]
+[5.244386672973633, 7.952053070068359, "The Spacecraft Controller of the TNS-0 Nanosatellite is Single chip microcontroller (C8051F022) of the Silicon Laboratories Company."]
+[7.457245826721191, 9.128731727600098, "The Structure Material of the IRS-1A Satellite is Aluminum/aluminum honeycomb."]
+[5.959441661834717, 8.072160720825195, "The Embankment Length of the Ataturk Dam Dam is 1,820 m."]
+[6.003028392791748, 7.154946327209473, "The Mass of the 3U CubeSat Satellite is 3.2 kg."]
+[5.016834259033203, 11.154729843139648, "The Launch Date of the Falcon 9 Rocket is Early 2018."]
+[6.9940185546875, 8.625653266906738, "The Total system cost of the WorldView Legion Satellite System is $600 million."]
+[5.063137531280518, 11.35501766204834, "The Landing Attempt of the Falcon 9 first stage Rocket is Mostly successful."]
+[4.393076419830322, 8.707233428955078, "The Track Duration of the CTECS Satellite is 30.6 minutes."]
+[5.942197799682617, 11.467912673950195, "The Data Monitor of the Seismic Experiment for Interior Structure (SEIS) Seismometer is Marsquake Service."]
+[6.063287258148193, 8.799363136291504, "The Longitude of the Meteosat-7 Satellite is 57.5 \u00b0E."]
+[10.8143310546875, 10.936446189880371, "The Resolution of the MWR Radiometer is 40 km."]
+[-3.450103521347046, 11.33076286315918, "The Latency of the ATL19 Mean Sea Surface (MSS) Data is 45 days from receipt of last data in product."]
+[13.317440032958984, 10.923323631286621, "The Field of View of the Lens Optical Instrument is 24\u00ba x 24\u00ba."]
+[6.656648635864258, 7.2753496170043945, "The Payload Mass of the INTEGRAL Satellite is 2 t."]
+[6.735960006713867, 9.64422607421875, "The Payload of the SV-1 Satellite is CTIP (Compact Tiny Ionospheric Photometer)."]
+[5.165804862976074, 10.945208549499512, "The Launch Date of the Genesis Satellite is August 8, 2001."]
+[15.250055313110352, 10.595813751220703, "The Number of Bands of the Optical Scanning Design Imaging Spectrometer is 45 bands (spectral campaigns)."]
+[7.200080394744873, 10.049456596374512, "The Acquisition Date of the Maxar Technologies Company is June 24, 2020."]
+[7.584720134735107, 7.168663024902344, "The Power of the ADEOS spacecraft Satellite is 4.5 kW."]
+[5.774611949920654, 8.021843910217285, "The Solar Array Length of the PARASOL microsatellite Satellite is 1.7 m."]
+[5.813788890838623, 9.47756290435791, "The GPS Data Collection Location of the ICESat-2 Satellite is 88 degrees south."]
+[4.416927337646484, 9.571144104003906, "The Design Life of the HY-1C Satellite is 5 years."]
+[5.706141471862793, 7.090084075927734, "The Circuit Board Area of the ChipSat CubeSat is 3.5 cm2."]
+[12.132318496704102, 11.116381645202637, "The Power of the CSS Instrument is 0.1 W."]
+[10.558523178100586, 11.278572082519531, "The Swath of the Stripmap mode (SM) Operational Mode is 80 km."]
+[14.289108276367188, 9.101181030273438, "The Vertical Resolution of the Limb Sensor Sensor is 2.2 km."]
+[10.079991340637207, 2.501278877258301, "The RAM of the STRV-2 DHS Data Handling System is 512 k."]
+[5.495207786560059, 8.883488655090332, "The Orbit Formation of the CloudSat Satellite is Tight formation with CALIPSO."]
+[5.25371789932251, 11.116917610168457, "The Removal from Service Date of the Monitor-E Spacecraft is August 2008."]
+[6.628697395324707, 9.971736907958984, "The Partner of the TanSat Satellite Mission is University of Edinburgh."]
+[9.866643905639648, 8.460712432861328, "The Attitude Knowledge Accuracy of the MCS Magnetic Control System is Within 0.1\u00ba."]
+[14.867735862731934, 9.828665733337402, "The Spectral Sampling Interval of the VNIR Spectrometer Spectrometer is 6.5 nm."]
+[8.904963493347168, 10.169997215270996, "The Function of the Antenna System Communication System is Receive GRB and legacy GVAR downlinks."]
+[5.612361907958984, 7.009798049926758, "The Size of the NanoSatC-Br1 CubeSat is 1U."]
+[14.685630798339844, 10.304931640625, "The Stability Requirements of the Individual Spectrometers Instrument is 15 pm."]
+[10.417880058288574, 10.501173973083496, "The Operating Frequencies of the SMMR Microwave Radiometer is 21.0 GHz."]
+[5.193699359893799, 10.568156242370605, "The Launch Date of the GRACE-FO Satellite is Early 2018."]
+[6.079738140106201, 8.393004417419434, "The Pointing of the MicroSat-70 Satellite is Nadir pointing."]
+[10.159236907958984, 10.44156265258789, "The Center Frequencies of the Bandpass Filters Signal Processing is 1.5, 4.5, 7.5, 10.5, 13.5, 16.5, 19.5, 22.5, 25.5, 28.5, 31.5 and 34.5 MHz."]
+[5.601933479309082, 7.0463786125183105, "The Size of the POPSat-HIP-1 CubeSat is 3U."]
+[6.541430950164795, 7.532245635986328, "The Mass of the Monitor-E Spacecraft is 700 kg."]
+[6.911925315856934, 9.239646911621094, "The Number of Collected Fragments of the DebriSat project Satellite is Over 20,000."]
+[5.754552364349365, 9.733039855957031, "The Spacecraft Type of the ABEX CubeSat is 12U CubeSat."]
+[11.654568672180176, 8.841659545898438, "The Performance of the MAG Instrument is \u00b130 nT."]
+[5.629031658172607, 8.705758094787598, "The Orbit Altitude of the Sentinel-2 satellites Satellite is 786 km."]
+[6.585992813110352, 8.265044212341309, "The Slew Maneuvers of the MicroSat-70 Satellite is Within \u00b115\u00ba about the roll axis (or \u00b1180\u00ba about the yaw axis)."]
+[10.987581253051758, 9.082898139953613, "The Quantity of the Reaction Wheels AOCS Actuators is 4."]
+[10.622003555297852, 10.650349617004395, "The Wavelength/Frequency of the RM-08 Passive Microwave Scanning Radiometer is 0.8 cm / 36.6 GHz."]
+[6.1873345375061035, 9.262539863586426, "The Camera Position of the LightSail Satellite is Mounted to two of the four deployable solar panels."]
+[10.951826095581055, 10.175907135009766, "The Scanning Capability of the ISAMS Instrument is Vertically and to either side of the UARS observatory."]
+[7.462709903717041, 8.422008514404297, "The Movement of the SS 433 Cosmic Object is Wobbles on its axis - precession."]
+[14.986153602600098, 9.873934745788574, "The Spectral Sampling Interval of the HR Spectrometer Spectrometer is 0.0933 nm/pixel."]
+[15.14370059967041, 9.91710376739502, "The Spectral Sampling Interval of the HSC Spectrometer Spectrometer is 1.2 nm \u2013 16 nm."]
+[14.426395416259766, 9.095951080322266, "The Spectra Captured of the Limb Sensor Sensor is Six."]
+[13.322999000549316, 11.14196491241455, "The Footprint Shape of the CNSCAT Scatterometer is Rosette-shaped."]
+[5.167573928833008, 7.671116352081299, "The Country of the Aalto-1 Nanosatellite is Finland."]
+[6.726785182952881, 9.829360961914062, "The Developer of the KickSat-2 CubeSat is Stanford University and NASA/Ames."]
+[7.371356010437012, 8.765280723571777, "The Pulsation Patterns of the Delta Scuti stars Star Type is Regular."]
+[11.286739349365234, 8.697381019592285, "The Error (RMS) of the Pitch momentum wheel Actuator is <0.001 mNms."]
+[13.95280647277832, 9.39616870880127, "The Array of the Detectors Photovoltaic Detectors is 3 x 3."]
+[4.433145999908447, 8.666827201843262, "The Time to Stabilize of the Satellite Spacecraft is More than six hours."]
+[7.813870429992676, 10.15859317779541, "The Database of the Payload Data Processing Software is MongoDB."]
+[14.264202117919922, 10.861041069030762, "The entrance slit width of the Spectrograph Instrument is  6\u00ba."]
+[6.614800453186035, 7.524022102355957, "The Per spacecraft mass of the WorldView-4 Satellite is 2500 kg."]
+[12.66813850402832, 10.599540710449219, "The Spectral Region (Visible Channel) of the VIRR Instrument is 0.49 - 0.94 \u00b5m."]
+[8.805734634399414, 10.158978462219238, "The Data Path of the Antenna System Communication System is Primary path for L1b data from WCDAS to NSOF."]
+[13.406110763549805, 11.078463554382324, "The Ensquared Energy of the Lens Optical Instrument is 90% within 60 x 60 \u00b5m."]
+[13.57928466796875, 8.502358436584473, "The Pixel Size of the Imager Camera is 9.0 \u00b5m x 9.0 \u00b5m."]
+[14.62900447845459, 10.291072845458984, "The Calibration Accuracy of the Instrument Spectrometer is Absolute: \u00b1 5%."]
+[5.325923442840576, 9.666329383850098, "The Primary Mission Status of the OPAL Satellite is Successful."]
+[14.020723342895508, 11.345268249511719, "The Wavelengths of the Telescope Optical Instrument is Fe XIV 530.3 nm; He I 587.6 nm."]
+[11.426055908203125, 9.463264465332031, "The Bit Depth of the fADC A/D Converter is 14 bit."]
+[6.950901985168457, 8.230467796325684, "The Slew Rate of the Spacecraft Satellite is 0.25 to 1.0\u00ba/s."]
+[11.635908126831055, 8.632561683654785, "The Range of the . Magnetometer Instrument is \u00b1 100,000 nT."]
+[5.452382564544678, 8.876351356506348, "The Footprint Overlay of the CloudSat and CALIPSO Satellites is About 50%."]
+[13.892560958862305, 11.45617389678955, "The Bandpass of the Telescope Optical Instrument is 540\u2013590 nm."]
+[11.439077377319336, 11.36184024810791, "The Sounder Type of the MLS Instrument is Three-channel heterodyne limb sounder."]
+[10.152436256408691, 2.4219465255737305, "The Power to sub-experiments of the STRV-1d DHS Data Handling System is +5 V, \u00b112 V."]
+[9.453231811523438, 12.400456428527832, "The Frequency of the Radar Radar is 9.6 GHz."]
+[12.113656044006348, 9.99178409576416, "The Detector Temperature of the ATSR-1 Instrument is < 95 K."]
+[15.393608093261719, 9.945961952209473, "The Wavelength Bands of the SBUV Spectrometer is 0.250 - 0.340 \u00b5m."]
+[5.730397701263428, 8.737903594970703, "The Crust Thickness of the Mars Planet is Between 24 and 72 kilometers."]
+[5.780267238616943, 8.614614486694336, "The Orbit (Altitude) of the Spacecraft Satellite is 628km."]
+[7.766521453857422, 10.112513542175293, "The Language of the Payload Data Processing Software is Java."]
+[13.617817878723145, 8.516905784606934, "The Number of Pixels of the Imager Camera is 4008 x 2672."]
+[7.205597877502441, 7.46866512298584, "The S/C Pointing of the DSX Spacecraft Payload Module Satellite is 1.0\u00ba, 1.0\u00ba."]
+[14.621285438537598, 8.493671417236328, "The Central Wavelength of the Current GOES imager Sensor is 7.34."]
+[6.999453067779541, 8.670042991638184, "The Daily system capacity of the WorldView-4 Satellite is 1x."]
+[11.586642265319824, 8.712867736816406, "The Sensor Quantity of the MAG Magnetometer is 2."]
+[8.728164672851562, 9.888072967529297, "The Downlink communications (Ka-band) of the Spacecraft Satellite is 278 Mbit/s (QPSK)."]
+[14.721805572509766, 10.068096160888672, "The Spectral Resolution Element Sampling of the Spectrometer Instrument is 2.5-3.0 detector pixels."]
+[9.479002952575684, 12.497906684875488, "The Resolution of the X-band Radar is 2.1 - 2.8 km in flight direction, 1.2 - 0.7 km in cross track direction."]
+[13.976371765136719, 8.503085136413574, "The Power Consumption of the Imager Camera is 1 W."]
+[9.133098602294922, 10.135880470275879, "The Operating Frequency Range (TC) of the EWC31 S-band transceiver module Communication Module is 2025-2110 MHz."]
+[12.584617614746094, 10.994421005249023, "The Performance of the FSS Instrument is \u00b10.35\u00ba."]
+[10.414776802062988, 10.522080421447754, "The Operating Frequencies of the SMMR Microwave Radiometer is 18.0 GHz."]
+[5.812553882598877, 8.89718246459961, "The Bathymetry Measurement Depth of the ICESat-2 Satellite is 10 meters or more."]
+[13.710067749023438, 11.508785247802734, "The Angular Resolution of the ART-XC Instrument Telescope is HPD~ 30\u201d on-axis at 8 keV."]
+[13.689495086669922, 11.607419967651367, "The Field of View of the ART-XC Instrument Telescope is 36' diameter."]
+[10.626420021057129, 10.185586929321289, "The Load Range of Shaker Tests of the Boom Structure is 0.048 to 0.00055 kg."]
+[7.565817832946777, 11.149303436279297, "The Manufacturer of the ALTIUS Instrument Satellite Instrument is Optique et Instruments de Pr\u00e9cision (OIP) Sensor Systems."]
+[5.794037342071533, 9.855910301208496, "The Mission Type of the ABEX CubeSat is Non-EO."]
+[11.193113327026367, 10.879470825195312, "The Crystal Axes Orientation of the DBCP Pseudo-depolarizer is Crossed and rotated by 45\u00b0."]
+[13.797741889953613, 10.340765953063965, "The Detector Type of the X-ray Spectrometer Spectrometer is Microcalorimeter."]
+[5.811054706573486, 9.284188270568848, "The Orbit of the GRACE-FO satellites Satellite is Co-planar polar orbit."]
+[15.666090965270996, 10.858591079711914, "The Wavelength Range of the Band 2 Spectral Band is 660-685 nm."]
+[13.705548286437988, 10.623273849487305, "The Grasp (500 eV) of the X-ray Imager Instrument is 27.5 cm 2 deg 2."]
+[15.066679000854492, 9.844974517822266, "The Spectral Range of the Hyperspectral Imager Radiometer is 0.4 \u2013 2.5 \u00b5m."]
+[11.341877937316895, 9.877449035644531, "The Range of the SCM Satellite Charging Monitor is -3 pA/cm2 to +3 pA/cm2."]
+[13.3901948928833, 9.988351821899414, "The Type of the Detector Instrument is 2D microchannel plate."]
+[13.850812911987305, 10.953261375427246, "The Transmitted Wavefront Distortion of the VPW42 Optical Window is \u03bb/8 at 633 nm."]
+[5.746104717254639, 11.4107666015625, "The First Marsquake Detection Date of the Seismic Experiment for Interior Structure (SEIS) Seismometer is April 6, 2019."]
+[9.768400192260742, 12.322952270507812, "The Wavelength of the SAR Synthetic Aperture Radar is 23.5 cm."]
+[-3.440621852874756, 11.32334041595459, "The Latency of the ATL02 Science Unit Data is 2 days."]
+[13.47836685180664, 8.256658554077148, "The Effective Pixel Dimensions of the Kodak KAI-11002 CCD CCD is 4008 x 2672."]
+[13.500041007995605, 11.653836250305176, "The Entrance Aperture Diameter of the Telescope Optical Instrument is 50 mm."]
+[13.514766693115234, 10.368990898132324, "The Ion energy of the Microdosimeter A Instrument is > 1 MeV."]
+[14.602071762084961, 8.555014610290527, "The Spectral Range of the Current GOES imager Sensor is 3.80-4.00."]
+[13.34168529510498, 8.761261940002441, "The Number of Cameras of the Imaging System Imaging System is 6."]
+[11.43429183959961, 8.600841522216797, "The Magnet Configuration of the AMS-02 Instrument is Permanent."]
+[4.79476261138916, 9.854451179504395, "The Operation Status of the Gokturk-2 Satellite is Nominal."]
+[10.042973518371582, 10.567609786987305, "The Center Frequencies of the ICI instrument Receiver is 183 GHz, 243 GHz, 325 GHz, 448 GHz and 664 GHz."]
+[6.483429908752441, 7.289212226867676, "The Mass of the SDS-4 Satellite is ~48 kg."]
+[5.044840335845947, 10.248456954956055, "The Data Release Date of the ICESat-2 Satellite is May 2019."]
+[12.366230964660645, 10.278692245483398, "The Interface Temperature Requirement of the LCT Optical Instrument is Lower than 15\u00baC."]
+[6.269553184509277, 8.433460235595703, "The Viewing Constraint of the Spacecraft Satellite is Cannot point to sources closer than 50\u00ba to the sun and to the anti-sun during nominal lifetime, 60\u00ba if eclipse seasons and extended lifetime."]
+[7.123553276062012, 7.482320785522461, "The Bus Mass of the Spacecraft Bus (Avionics Module=AM) Satellite is 180 kg."]
+[9.59070873260498, 12.548781394958496, "The Spatial Resolution (Elevation) of the Radar Radar is 15 km."]
+[4.532344341278076, 8.774338722229004, "The Orbit Period of the Sentinel-2 satellites Satellite is 101 minutes."]
+[11.922764778137207, 12.586236953735352, "The Cirrus Optical Depth of the Mie co-polar channel Channel is 0.05."]
+[6.943756103515625, 9.106648445129395, "The Number of Satellites of the DMSP (Defense Meteorological Satellite Program) Satellite Program is 19."]
+[13.305171966552734, 11.323241233825684, "The Aperture of the Instrument Optical Instrument is 8 cm."]
+[14.963770866394043, 10.331268310546875, "The Spectral Band of the Instrument Spectrometer is SWIR."]
+[10.111148834228516, 2.467137575149536, "The Power of the STRV-2 DHS Data Handling System is 6 W."]
+[9.49729061126709, 8.153088569641113, "The \u0394V Decrease of the Bloostar Launch Vehicle is ~8%."]
+[14.170470237731934, 9.94654655456543, "The Electronic Noise Contribution to Energy Resolution of the Detector Instrument is 400 eV."]
+[13.39123821258545, 11.238879203796387, "The Number of Fast Cameras of the PLATO Telescope is 2."]
+[4.856205463409424, 9.329216003417969, "The Mission Duration of the SORTIE CubeSat is 6 months."]
+[13.242450714111328, 11.251909255981445, "The Footprint Size of the CNSCAT Scatterometer is 19 km x 24 km."]
+[13.475272178649902, 10.689264297485352, "The FOV of the X-ray Imager Instrument is 4.6\u00ba x 4.6\u00ba."]
+[6.424333572387695, 9.65278148651123, "The developer of the UniSat-1 Satellite is GAUSS (Gruppo di Astrodinamica dell' Universita degli Studi \u201cla Sapienza\u201d)."]
+[9.452948570251465, 8.149321556091309, "The Payload Spin of the Bloostar Launch Vehicle is Up to 10 rpm."]
+[5.28245210647583, 10.121244430541992, "The Launch Date of the Meteosat-7 Satellite is September 1997."]
+[13.597977638244629, 8.589237213134766, "The Pixel Size of the Image Sensor Imaging is 9.0 \u00b5m x 9.0 \u00b5m."]
+[12.127470016479492, 11.077865600585938, "The Average Power Consumption of the Instrument Instrument is 5.6 W."]
+[13.258841514587402, 9.671625137329102, "The Polarized Channels of the VNIR Sensor is 2."]
+[7.1294708251953125, 8.078058242797852, "The Deployment Velocity of the Dispensers Satellite Component is 1 to 2 m/s."]
+[5.044108867645264, 10.589359283447266, "The Re-entry Date of the Satellite Satellite is 8 December 2011."]
+[7.4077067375183105, 8.26365852355957, "The ADCS of the MiRaTA Satellite is 3-axis stabilized."]
+[12.561196327209473, 11.351466178894043, "The Mass of the Photometer Instrument is \u2264 0.9 kg."]
+[14.807600021362305, 10.632169723510742, "The Type of the Optical Scanning Design Imaging Spectrometer is Pushbroom."]
+[10.832533836364746, 9.187236785888672, "The Altitude Range of the Atomic Oxygen (AO) Density Measurement Device Instrument is 180-200 km."]
+[15.689209938049316, 9.741772651672363, "The Visible Spectral Range / Bandwidth of the SOLSPEC-SOLAR Spectrometer is 285-910/1.6."]
+[13.123100280761719, 10.684224128723145, "The Field-of-view of the Photometer Optical Instrument is 24\u00ba."]
+[5.891653060913086, 8.692788124084473, "The Altitude of the EFT-1 Spacecraft is Approximately 5800 km."]
+[5.179220199584961, 7.5941314697265625, "The Developer of the Venta-1 Nanosatellite is Bremen University of Applied Sciences."]
+[10.659603118896484, 11.134550094604492, "The Area of the . Wave mode (WM) Operational Mode is 20 km x 20 km."]
+[13.969365119934082, 11.240602493286133, "The Wavelength Range of the Lens Optical Instrument is 600 - 1000 nm."]
+[9.540489196777344, 12.452350616455078, "The Incident Angle of the Radar Radar is ~39\u00ba."]
+[12.006439208984375, 10.01710033416748, "The Inner Temperature of the Dewar Component is ~ 256.6 K."]
+[6.208641052246094, 8.328917503356934, "The Solar Array Normal Vector and Sun Vector Difference of the Spacecraft Satellite is Up to 40 degrees during the first two years of operations."]
+[5.792110919952393, 9.713272094726562, "The Launch Vehicle of the HORYU-2 Nanosatellite is H-IIA of Japan."]
+[12.289958000183105, 11.645589828491211, "The Mass of the CEASE-2 Instrument is 1.3 kg."]
+[6.720803737640381, 10.654611587524414, "The Project Manager of the CO2M Satellite is Valerie Fernandez."]
+[9.073890686035156, 9.884952545166016, "The Flexible Mode Frequency of the Payload Satellite Component is Below 10 Hz."]
+[6.815080165863037, 9.163243293762207, "The Solar Panels of the DebriSat Satellite is 3 deployable."]
+[-3.4540746212005615, 11.334879875183105, "The Latency of the ATL00 Telemetry Data Data is Downlinked 8 times/day."]
+[13.217084884643555, 9.717317581176758, "The Channels of the VNIR Sensor is 14."]
+[13.420473098754883, 11.626507759094238, "The Ground Sampling Distance of the Telescope Optical Instrument is 30 m."]
+[7.683620452880859, 6.848094463348389, "The Capacity of the Battery Power is 12 Ah."]
+[12.037242889404297, 11.08703899383545, "The Power of the Travelling Wave Tube Amplifier Device is 20 W."]
+[9.863699913024902, 8.467371940612793, "The Attitude Error of the AOCS Attitude Control System is <0.3\u00ba."]
+[14.750810623168945, 10.234354019165039, "The Spectral Knowledge of the Individual Spectrometers Instrument is 1.5 pm."]
+[13.502411842346191, 8.49593448638916, "The Image Size of the VIS Camera Camera is 1910 x 1270 pixels."]
+[13.171509742736816, 10.698626518249512, "The ACT FOV Incidence Angles of the Sentinel-5 instrument Instrument is Up to 54\u00b0."]
+[15.617781639099121, 10.70144271850586, "The FOV of the Band 1 Spectral Band is 400 km x 0.5 km."]
+[10.50623607635498, 10.659855842590332, "The Spatial Resolution of the SMMR Microwave Radiometer is Ranged from 22 km at 37 GHz to 100 km at 6.6 GHz."]
+[13.430184364318848, 11.118871688842773, "The Ensquared Energy of the Lens Optical Instrument is 50% within 15 x 15 \u00b5m."]
+[11.717079162597656, 11.283860206604004, "The Mass of the MWR Dicke Radiometer is 99 kg."]
+[15.597323417663574, 9.709741592407227, "The Spectral Range of the SOLSPEC-SOLAR Spectrometer is 165-3080 nm."]
+[7.145090103149414, 7.214734077453613, "The Orbit Capability of the DSX Spacecraft Payload Module Satellite is 6,000 km to 12,000 km any inclination."]
+[6.890065670013428, 10.007593154907227, "The Manufacturer of the ELSA-d Satellite is Astroscale UK Ltd."]
+[7.581003189086914, 10.674802780151367, "The Developer of the MWS, SCA, RO, MWI, ICI, 3MI Instruments is ESA."]
+[7.49424409866333, 8.162853240966797, "The  Spacecraft control of the  Spacecraft Bus (Avionics Module=AM) Satellite is 3-axis stabilized."]
+[13.836299896240234, 11.556289672851562, "The Mirror Shell Material of the ART-XC Instrument Telescope is Nickel-cobalt alloy with iridium coating."]
+[6.024698734283447, 10.09231948852539, "The Launch Vehicle of the OneWeb Satellite Communications Company is PSLV (Polar Satellite Launch Vehicle) and GSLV-MkIII (Geosynchronous Satellite Launch Vehicle)."]
+[4.689237594604492, 8.948774337768555, "The Image Capture Time of the TESS Satellite is Over the course of 17 hours on July 25."]
+[13.037601470947266, 10.020074844360352, "The Scanning Method of the OCTS Sensor is Mechanical rotating with a mirror."]
+[10.472110748291016, 9.72433090209961, "The Boresight Direction of the MIRO Instrument is Aligned with the Rosetta payload line of sight."]
+[11.240914344787598, 9.42529582977295, "The Quantity of the Rx Channels Receiver is 2."]
+[11.96802806854248, 11.734450340270996, "The Backscatter Sensitivity of the Core Instrument Instrument is 8 x 10-7 m-1 sr-1."]
+[4.910613536834717, 10.324543952941895, "The Launch Date of the GOES-T Satellite is March 2022."]
+[12.311891555786133, 11.582016944885254, "The Mass of the MTQ Instrument is 225 g."]
+[7.497620582580566, 8.09904956817627, "The  Spacecraft control of the DSX Spacecraft Payload Module Satellite is 3-axis stabilized."]
+[10.068761825561523, 10.715827941894531, "The Frequency Range of the ICI Instrument is 183 GHz up to 664 GHz."]
+[12.599294662475586, 10.519625663757324, "The Sensitivity (Infrared Channel) of the VIRR Instrument is 4 K with a scene at 185 K, 1 K with a scene at 300 K."]
+[15.608346939086914, 9.822853088378906, "The Number of Spectrometers of the SOLSPEC-ATLAS Spectrometer is 3."]
+[6.884424209594727, 10.447722434997559, "The owner of the Insight lander lander is NASA."]
+[10.78502082824707, 11.006612777709961, "The Resolution of the MWR Dicke Radiometer is 50 km."]
+[13.498641014099121, 10.325061798095703, "The Ion energy of the Microdosimeter B Instrument is > 50 keV."]
+[9.482173919677734, 8.185039520263672, "The Altitude Accuracy of the Bloostar Launch Vehicle is \u00b15 km."]
+[13.946146011352539, 10.686774253845215, "The Polarization Sensitivity of the Grating Optical Component is Less than 20%."]
+[4.12044095993042, 9.33609390258789, "The Instrument Calibration Phase Duration of the GP-B mission Mission is 7 weeks."]
+[9.276162147521973, 9.631958961486816, "The Power of the TRSR GPS Receiver is 7-15 W."]
+[12.50588321685791, 11.375752449035645, "The Mass of the Photometer Instrument Instrument is \u2264 0.9 kg."]
+[5.612968444824219, 8.937010765075684, "The Mean Sea Level Rise Measurement of the Jason-3 Satellite is About 3mm per year."]
+[11.560832977294922, 8.561098098754883, "The Accuracy of the MAG Magnetometer is \u22641 nT."]
+[12.308913230895996, 11.554125785827637, "The Mass of the MAG Instrument is 40 g."]
+[7.269690990447998, 9.96947956085205, "The New Debt Issued of the Maxar Technologies Company is $150 million."]
+[4.451965808868408, 8.656377792358398, "The Orbit (Local Sun Time) of the Spacecraft Satellite is 12:00 \u00b1 15 min."]
+[6.636789321899414, 7.219947814941406, "The Payload Mass of the ADEOS spacecraft Satellite is 1300 kg."]
+[6.898748397827148, 8.221158981323242, "The Per spacecraft mass of the  WorldView Legion Satellite System is 750kg."]
+[6.535378932952881, 7.4452409744262695, "The Fuel Quantity of the IRS-1A Satellite is 80 kg."]
+[10.146117210388184, 8.751709938049316, "The Operational Ranges for alignment / pointing of the NightPod Tracking Device is 1st:Yaw \u00b120\u00ba, 2nd:Roll \u00b120\u00ba, 3rd:Pitch nodding \u00b120\u00ba."]
+[-3.4189019203186035, 11.299360275268555, "The Latency of the ATL03 Global Geolocated Photon Data Data is 21 days."]
+[5.5002946853637695, 7.356303691864014, "The Weight of the Venta-1 Nanosatellite is ~5 kg."]
+[4.809281826019287, 8.49517822265625, "The Revisit Time of the BlackSky's Satellites Microsatellites is Every 30 minutes."]
+[6.608928680419922, 9.964653968811035, "The COSMIAC Role of the SORTIE Satellite is Build the satellite and collect the data from it."]
+[15.131094932556152, 10.012895584106445, "The Grating Frequency of the HSC Spectrometer Spectrometer is 30 lines/mm."]
+[5.6308274269104, 7.0026655197143555, "The Size of the Duchifat-1 CubeSat is 1U."]
+[11.919058799743652, 11.759965896606445, "The Standard Interface of the CEASE-1 Instrument is RS-422 or MIL-STD-1553B."]
+[11.59193229675293, 9.032145500183105, "The Number of Sensor Elements of the Chem-sensor housing Sensor is 32."]
+[6.090561389923096, 9.87446117401123, "The Launch of the Spacecraft Satellite is H-IIA launch vehicle from TNSC."]
+[15.429485321044922, 9.860101699829102, "The Field of View of the SBUV Spectrometer is 0.20 rad."]
+[12.708205223083496, 8.948272705078125, "The Detectors Quantity of the REM Radiation Environment Monitor is 2."]
+[9.54555606842041, 12.023602485656738, "The Polarization of the Antenna Radar Antenna is Dual (H and V)."]
+[10.654620170593262, 10.013837814331055, "The In-flight Operation Start of the NIRST Instrument Radiometer is Winter of 2012."]
+[7.268013954162598, 8.867204666137695, "The Number of Identified Stars of the Delta Scuti stars Star Type is 60."]
+[15.745017051696777, 10.959611892700195, "The Polarization Angle of the Band 5 Spectral Band is 0/60/120 \u00ba."]
+[9.532820701599121, 12.070168495178223, "The Polarization of the Radar Radar is HH, VV, HV/VH."]
+[4.464895725250244, 8.761331558227539, "The Estimated Time Before Blackout of the Spacecraft Satellite is Just three hours."]
+[15.498085975646973, 9.815498352050781, "The Solar-Spectral Scan Range of the SBUV Spectrometer is 0.16 - 0.4 \u00b5m."]
+[11.498903274536133, 11.994157791137695, "The Dimensions of the InP amplifier Amplifier is 900 x 560 \u00b5m2."]
+[6.489041328430176, 7.393270969390869, "The Mass of the GRACE-FO satellites Satellite is ~600 kg."]
+[5.259932041168213, 10.708566665649414, "The Commissioning End Date of the RASAT Satellite is Late December 2011."]
+[13.913920402526855, 10.832052230834961, "The Keystone of the System Optical System is Less than 0.4 \u00b5m."]
+[6.920817852020264, 8.502762794494629, "The Nadir resolution of the WorldView Legion Satellite System is 29 cm."]
+[7.660322666168213, 6.840956687927246, "The Capacity of the BAT Battery is 50 Ah."]
+[4.353417873382568, 9.133870124816895, "The Orbit Determination Frequency of the ASNARO Ground Segment Ground Station is Twice per day."]
+[6.785257816314697, 10.263919830322266, "The Head of the Astronomy Missions Division of the Integral Satellite is Andreas Rudolph."]
+[12.47930908203125, 9.909461975097656, "The Designer of the BGO Calorimeter Detector is Prof. LIU Shubin from USTC."]
+[7.478323459625244, 10.300766944885254, "The Developers of the MR-FOD Deployer is Morehead University, Morehead, KY, USA and GAUSS."]
+[11.591780662536621, 11.79588794708252, "The Manufacturer of the TEMPO Instrument is Ball Aerospace."]
+[15.153183937072754, 9.961868286132812, "The Spectral Range of the LR Spectrometer Spectrometer is 500\u2013758 nm."]
+[5.255766868591309, 10.697040557861328, "The Operational Start Date of the RASAT Satellite is Start of 2012."]
+[5.665377616882324, 7.145657539367676, "The Inflatable Mast Length of the 3U CubeSat Satellite is 1 m."]
+[10.749067306518555, 10.937467575073242, "The Resolution of the RM-08 Passive Microwave Scanning Radiometer is 15 km x 20 km."]
+[11.001550674438477, 10.582857131958008, "The Testing of the TEMPEST-D Radiometer Instrument is Passed."]
+[5.812084197998047, 10.404545783996582, "The Development Locations of the POPSAT-HIP1 Satellite is Italy, Japan, and Singapore."]
+[5.141363143920898, 7.826972484588623, "The Presentation Date of the SERB Nanosatellite is Sept. 26-30, 2016."]
+[10.50728702545166, 11.568900108337402, "The Size of the  Submillimeterwave receiver receiver is 0.5 mm."]
+[13.804916381835938, 11.004228591918945, "The Diameter of the VPW42 Optical Window is 1.5\u201d."]
+[14.124430656433105, 11.469252586364746, "The Protective Layer of the FPI Mirrors Component is 50 nm layer of silicon dioxide (SiO2)."]
+[8.949708938598633, 10.022309303283691, "The Data Rates (TC) of the EWC31 S-band transceiver module Communication Module is 8 kbit/s to 256 kbit/s."]
+[9.732572555541992, 8.352560997009277, "The Attitude Accuracy of the Attitude and Orbit Control Subsystem Subsystem is 0.5\u00ba in yaw."]
+[5.343495845794678, 11.036091804504395, "The Launch Date of the OrbView-4 Satellite is Sept. 21 2001."]
+[10.219791412353516, 8.80045223236084, "The Rotation Range of the Pointer Mirror Device is 0 to 360\u00ba."]
+[6.502208232879639, 7.249185085296631, "The Mass at Launch of the INTEGRAL Satellite is 4 t."]
+[9.088850975036621, 9.922961235046387, "The Frequency of the Satellite Communication is 435 MHz."]
+[8.12413215637207, 7.505126476287842, "The Functionality of the PCU Power Control Unit is High."]
+[4.820075988769531, 10.937600135803223, "The Observation Date of the NICER Telescope Telescope is 8 March 2022."]
+[5.921825885772705, 10.010825157165527, "The Launch Vehicle of the Meteosat-1 Satellite is Thor-Delta."]
+[12.253560066223145, 10.921639442443848, "The Power Dissipation of the LCT Optical Instrument is Varies."]
+[5.551555633544922, 10.911606788635254, "The Launch Status of the OrbView-4 Satellite is Failure."]
+[4.747359752655029, 10.538711547851562, "The Image Capture Date of the Sentinel-2 Satellite is 25 January 2022."]
+[14.16102409362793, 9.90849781036377, "The Spectral Resolution (5-30 keV) of the Detector Instrument is 500 eV FWHM."]
+[13.321203231811523, 11.277345657348633, "The Design Review Date of the IRIS instrument Instrument is December 2010."]
+[13.40057373046875, 11.669954299926758, "The Footprint of the Telescope Instrument is Smaller than 30 m."]
+[11.474595069885254, 8.528159141540527, "The Uncertainty of the . Magnetometer Instrument is \u00b114 nT."]
+[6.4517436027526855, 7.1461567878723145, "The Launch Mass of the HY-1C Satellite is 442 kg."]
+[7.154745101928711, 10.17748737335205, "The CEO of the Maxar Space Solutions Company is Jablonsky."]
+[9.913318634033203, 12.143550872802734, "The Payload Data Memory of the SAR antenna Antenna is 544 GByte."]
+[5.954639434814453, 10.598021507263184, "The Location of the IMGEOS Ground Segment Facility is NRSC (National Remote Sensing Center), Shadnagar, Hyderabad Complex."]
+[13.631782531738281, 10.649848937988281, "The Resolution of the X-ray Imager Instrument is < 0.22\u00ba."]
+[8.748528480529785, 10.271638870239258, "The Radio Type of the SENSE Satellite is S-band."]
+[11.181272506713867, 9.433717727661133, "The Quantity of the Zenith antennae Antenna is 2."]
+[10.989496231079102, 12.190157890319824, "The Tank Diameter of the Launcher Test Facility is 3 m."]
+[13.765759468078613, 9.45410442352295, "The GIFOV of the SWIR Detector is 4 km."]
+[13.08946704864502, 10.921667098999023, "The Field of View of the A Photometer Instrument is 0.2o x 2.1o."]
+[11.687350273132324, 10.991896629333496, "The Power Consumption of the MI Radiometer Instrument is < 195 W."]
+[13.83343505859375, 10.040946006774902, "The Low-Energy Threshold of the Detector Instrument is 2.5 keV."]
+[5.8078813552856445, 9.187718391418457, "The Orbit Type of the Satellite Imaging Satellite is Sun-synchronous near-polar orbit."]
+[6.594167709350586, 7.227591514587402, "The Satellite Mass of the ADEOS spacecraft Satellite is 3560 kg."]
+[10.592278480529785, 11.308886528015137, "The Swath of the Extra Wide Swath mode (EWS) Operational Mode is 400 km."]
+[6.534427165985107, 10.321526527404785, "The Investment Minister of the OneWeb Satellite Communications Company is Gerry Grimstone."]
+[13.488168716430664, 8.248006820678711, "The Pixel Size of the Kodak KAI-11002 CCD CCD is 9 \u00b5m x 9 \u00b5m."]
+[9.832107543945312, 12.115913391113281, "The Duty Cycle of the SAR antenna Antenna is 2-3 minutes per orbit."]
+[-3.446207284927368, 11.327305793762207, "The Latency of the ATL12 Ocean Elevation Data is 45 days from receipt of last data in product."]
+[11.272475242614746, 10.67664909362793, "The Sensitivity of the MWR Dicke Radiometer is 0.5 K."]
+[7.679623603820801, 8.189443588256836, "The Attitude Control of the UniSat-1 Satellite is Spin-stabilized at 5 rpm with the spin-axis normal to the orbital plane."]
+[10.90565013885498, 10.733107566833496, "The Polarization of the MWR Radiometer is V and H."]
+[7.0449604988098145, 7.1106743812561035, "The ESPA Ring Mass of the DSX Spacecraft Payload Module Satellite is  240 kg."]
+[14.721014022827148, 10.187093734741211, "The MTF of the Instrument Spectrometer is \u22650.2, \u22650.3."]
+[5.34713077545166, 11.149481773376465, "The Failure Date of the ISAMS Instrument is Late July 1992."]
+[5.184425354003906, 9.694828987121582, "The Status in 2004 of the OPAL Satellite is Semi-operational."]
+[10.920204162597656, 11.242477416992188, "The Spatial Resolution of the Multispectral Instrument (MSI) Instrument is 20 m."]
+[14.86605167388916, 10.612865447998047, "The Spectral Band of the VIS Channel is 0.4 - 1.1 \u00b5m."]
+[13.825775146484375, 8.671567916870117, "The Cadence of the Normal Cameras Camera is 25 seconds."]
+[13.44223690032959, 8.964128494262695, "The Bit Size of the Event Data Structure is 64-bit."]
+[11.506256103515625, 8.439064025878906, "The DC Measurement Accuracy of the Magnetometer Instrument is 0.05% of the field in CuPID's orbit."]
+[13.556988716125488, 9.12903118133545, "The Resolution of the OLS Imaging Sensor is 2.8 km."]
+[13.415651321411133, 11.752283096313477, "The Aperture Diameter of the Instrument Telescope is 35 cm."]
+[14.925975799560547, 10.061888694763184, "The Spectral Sampling Distance of the SWIR Spectrometer Spectrometer is 10 nm."]
+[15.742721557617188, 10.78184700012207, "The Resolution of the spectral band band is 240 m."]
+[6.467785835266113, 9.779218673706055, "The Satellite Integrator of the SORTIE CubeSat is COSMIAC."]
+[5.887185573577881, 8.588489532470703, "The Orbit Altitude of the Max Valier Satellite is 600 km."]
+[6.571033477783203, 7.246738910675049, "The Mass of the Spacecraft Satellite is 2120 kg."]
+[5.706549167633057, 9.810066223144531, "The Development Status of the ABEX CubeSat is In development."]
+[13.344042778015137, 10.5452299118042, "The Field of View (FOV) of the Electron Spectrometer Instrument is 10\u00ba-170\u00ba with respect to the spin axis by 30\u00ba in azimuth."]
+[6.742588996887207, 10.112493515014648, "The Funding Provider of the TanSat Satellite Mission is CAS (Chinese Academy of Sciences)."]
+[5.259795188903809, 10.734113693237305, "The launch date of the RASAT Satellite is August 17, 2011."]
+[6.848518371582031, 8.688730239868164, "The Funding Status of the Worldview Legion Satellite Constellation is Fully able to fund."]
+[-3.3665335178375244, 11.244632720947266, "The Latency of the ATL10 Arctic/Antarctic Sea Ice Freeboard Data is 45 days."]
+[13.317948341369629, 11.867067337036133, "The Telescope Size of the ASTERIA Satellite is 2.4-inch (6-centimeter)."]
+[4.5038251876831055, 9.39256763458252, "The Age of the Integral Spacecraft is 18 years."]
+[5.336774826049805, 10.142642974853516, "The Deployment Date of the CubeRRT, EQUiSat, HaloSat, MemSat, RadSat-g, RainCube, TEMPEST-D, EnduroSat One, Radix Satellites is July 15th."]
+[11.935860633850098, 8.749469757080078, "The Error (RMS) of the Rate sensor Sensor is <0.05/s."]
+[10.14216423034668, 2.4922804832458496, "The RAM of the STRV-1d DHS Data Handling System is 1024 k."]
+[12.069232940673828, 9.963310241699219, "The Temperatures of the Cooler Passive Cooler is 81 K for LWIR patch."]
+[5.39450740814209, 8.19064712524414, "The Frequency Range of the Chibis-M Microsatellite is ULF-VLF."]
+[9.45124626159668, 12.41615104675293, "The Peak Power of the Radar Radar is 200 W/150 W."]
+[7.613325595855713, 9.202319145202637, "The Material of the IDA Dewar is Titanium."]
+[6.320382118225098, 10.996213912963867, "The Cross-Calibration Partner of the QuikSCAT Satellite is Indian Space Research Organization (ISRO) Oceansat-2 scatterometer known as OSCAT."]
+[15.267559051513672, 9.826664924621582, "The F Number of the HSC Spectrometer Spectrometer is 3.0."]
+[12.042220115661621, 11.11446475982666, "The Power of the MTQ Instrument is 1 W/unit."]
+[7.6636223793029785, 11.187542915344238, "The Channels of the ALTIUS Instrument Satellite Instrument is Three channels."]
+[13.776941299438477, 11.77918815612793, "The Type of the Telescope Optical Instrument is Zeiss 1 m \u2205 Ritchey-Chr\u00e9tien/Coud\u00e9 telescope."]
+[14.623455047607422, 8.547155380249023, "The Spectral Range of the Current GOES imager Sensor is 6.75-7.15."]
+[5.86185884475708, 8.58067512512207, "The Orbit Altitude of the ISS Space Station is ~400 km."]
+[10.964938163757324, 12.139806747436523, "The Tank Pressure Range of the Launcher Test Facility is 0.2 torr to 1.7 atmospheres."]
+[12.11181354522705, 11.154373168945312, "The Power Consumption of the CEASE-1 Instrument is 1 W."]
+[5.779201507568359, 8.495023727416992, "The Distance from Sun of the Solar Orbiter Satellite is Roughly 75 million km."]
+[4.372979164123535, 9.639965057373047, "The Operational Lifetime of the GOES-R Satellite is 10 years."]
+[4.493587493896484, 8.876592636108398, "The Orbit (Revisit Time) of the Spacecraft Satellite is 14 days."]
+[15.73450756072998, 9.73537826538086, "The IR Spectral Range / Bandwidth of the SOLSPEC-SOLAR Spectrometer is 650-3080/8."]
+[4.909766674041748, 10.566099166870117, "The Measurement Date of the GRACE-FO Satellite is 22 June 2020."]
+[13.81738567352295, 11.847563743591309, "The Type of the Primary Mirror Telescope Component is Off-axis paraboloid."]
+[4.454073429107666, 9.091084480285645, "The Orbit Transition Duration of the WorldView-1 Satellite is 18 months."]
+[10.947007179260254, 11.103972434997559, "The Spatial Resolution of the MSU-SK Radiometer is 600 m (TIR)."]
+[4.844451427459717, 10.657085418701172, "The Image Capture Date of the Copernicus Sentinel-2 Satellite is January 28, 2022."]
+[10.735494613647461, 10.627347946166992, "The Frequency of the MWR Radiometer is 36.5 GHz."]
+[11.246665954589844, 10.163077354431152, "The Detector Type of the MM Radiometer Sensor is Schottky diode detectors."]
+[6.005282402038574, 8.092557907104492, "The Volume of the Lake Atat\u00fcrk Dam Reservoir is 48.7 km3."]
+[15.466590881347656, 9.809796333312988, "The Number of Detectors of the SBUV Spectrometer is 3."]
+[5.934875011444092, 11.483515739440918, "The Provider of the Seismic Experiment for Interior Structure (SEIS) Seismometer is Centre National d'\u00c9tudes Spatiales (CNES)."]
+[15.845552444458008, 10.917404174804688, "The SNR of the Band 4 Spectral Band is 180."]
+[5.070298671722412, 8.72441291809082, "The Sky Coverage of the INTEGRAL Satellite is Almost full-sky coverage for brief events."]
+[9.17669677734375, 7.135531902313232, "The Hydrogen Gas Temperature of the Sun's Lower Atmosphere Celestial Body is 10,000\u00baC."]
+[7.029536724090576, 7.6980204582214355, "The Number of Thrusters of the Propulsion Subsystem Propulsion is 8 (2 x 4)."]
+[7.308314800262451, 7.860782146453857, "The S/C Pointing of the Spacecraft Bus (Avionics Module=AM) Satellite is 1.0\u00ba, 1.0\u00ba."]
+[6.5074968338012695, 9.00222110748291, "The Sensitivity of the INTEGRAL Satellite is High sensitivity to gamma rays."]
+[7.55148983001709, 7.320511817932129, "The Array Power Peak of the Spacecraft Bus (Avionics Module=AM) Satellite is 790 W."]
+[7.194683074951172, 7.840656280517578, "The Mission Design Life of the Spacecraft Bus (Avionics Module=AM) Bus is 12 months."]
+[12.66895580291748, 10.601027488708496, "The Spectral Region (Infrared Channel) of the VIRR Instrument is 10.5 - 12.5 \u00b5m."]
+[5.220023155212402, 9.734161376953125, "The Magnetometer Status of the NEOSSat Satellite is Failed."]
+[9.031155586242676, 10.24651050567627, "The Frequency Band of the Telemetry, Tracking and Command System Telemetry, Tracking and Command System  is S-band."]
+[11.335941314697266, 8.591087341308594, "The Type of the Vector Magnetometer Instrument is CSC (Compact Spherical Coil) triaxial fluxgate magnetometer."]
+[4.743441581726074, 10.640064239501953, "The Image Capture Date of the Sentinel-2 Satellite is 20 January 2022."]
+[4.404681205749512, 8.769023895263672, "The Overhead Pass Time of the WorldView-1 Satellite is Approximately 13:30 hours local time."]
+[13.568559646606445, 9.126398086547852, "The width of the Detector Instrument is 32 pixels."]
+[7.337461948394775, 10.755874633789062, "The Developer of the Sentinel-5 Instrument is ESA."]
+[5.839921951293945, 9.74073314666748, "The Mission of the GRACE-FO Satellite is Gravity Recovery and Climate Experiment Follow-On."]
+[9.812564849853516, 8.431541442871094, "The Attitude Stability of the AOCS Attitude Control System is <0.003\u00ba/s."]
+[5.528534889221191, 8.618962287902832, "The Comet Distance from Earth of the TESS Satellite is About 29 million miles (48 million km)."]
+[12.442733764648438, 10.011185646057129, "The Sensor Operating Temperature Range of the FIPEX Instrument is 600-700\u00baC."]
+[6.465989112854004, 7.4936137199401855, "The Printed Circuit Board Mass of the Sprite Tiny Spacecraft is A few grams."]
+[9.592649459838867, 12.064828872680664, "The Polarization of the SAR Synthetic Aperture Radar is HH."]
+[4.902251720428467, 10.50187873840332, "The Image Capture Date of the Solar Orbiter Satellite is 7 March."]
+[13.558367729187012, 9.076458930969238, "The Dynamic Range of the Detector Imaging Device is 16 bit."]
+[13.505579948425293, 8.631956100463867, "The Resolution of the CMOS Camera Sensor is 3000 x 2000 pixels."]
+[-3.4160521030426025, 11.296463012695312, "The Latency of the ATL13 Inland Water Elevation Data is 45 days from receipt of last data in product."]
+[11.262786865234375, 8.804252624511719, "The Provider of the MAG Instrument is SwRI (Southwest Research Institute) and the University of New Hampshire in cooperation with the Austrian Academy of Sciences."]
+[11.268631935119629, 9.082757949829102, "The Number of Mini-Solenoid Valves of the NCSU Nano ChemSensor Unit is 3."]
+[12.000886917114258, 11.069581031799316, "The Performance of the MW Instrument is 0-4 Nms."]
+[14.80115032196045, 10.271699905395508, "The Spectral Resolution of the Optical Scanning Design Imaging Spectrometer is 1.25 nm."]
+[7.514828681945801, 10.665155410766602, "The Manufacturer of the IREM Radiation Environment Monitor is ESA."]
+[13.41213607788086, 11.624106407165527, "The Aperture Diameter of the Telescope Optical Instrument is 30 cm."]
+[6.477023124694824, 7.142940521240234, "The Launch Mass of the Gokturk-2 Satellite is ~ 450 kg."]
+[-3.3402013778686523, 11.218297004699707, "The Latency of the ATL15 Antarctica/Greenland Ice Sheet dh/dt Gridded Data is 45 days from receipt of last data in product."]
+[6.257089614868164, 8.333409309387207, "The Solar Array Normal Vector and Sun Vector Difference of the Spacecraft Satellite is Up to 30 degrees during the extended mission phase."]
+[6.892853260040283, 9.244118690490723, "The Number of Characterized Fragments of the DebriSat project Satellite is Over 13,000."]
+[10.886385917663574, 11.987048149108887, "The Boom Length of the AstroTube Payload is 1.5m."]
+[4.9742913246154785, 10.350268363952637, "The Launch Date of the GOSAT-2 Satellite is October 2018."]
+[4.417548656463623, 9.281231880187988, "The Test Duration of the D-Orbit Company is Four months."]
+[10.544244766235352, 11.646095275878906, "The Thickness of the RF Section Subsystem is 5 cm."]
+[13.967565536499023, 11.70989990234375, "The Telescope Assembly of the SPEXone Spectrometer is Three-mirror segmented telescope assembly."]
+[13.488096237182617, 8.880705833435059, "The Resolution of the Detector CMOS Sensor is 2048 x 2048 pixels."]
+[12.179927825927734, 9.107389450073242, "The Quantity of the Electrostatic Analysers Sensor is 2."]
+[6.6445746421813965, 10.859400749206543, "The Measurement domain of the Meteor-M-2 Satellite is Atmosphere, Ocean, Land, Gravity and Magnetic Fields, Snow & Ice."]
+[7.549448013305664, 8.545772552490234, "The X-ray Light of the SS 433 Cosmic Object is Enough to officially call SS 433 a ULX."]
+[7.283924579620361, 8.080163955688477, "The Orbit Capability of the Spacecraft Bus (Avionics Module=AM) Satellite is LEO, MEO."]
+[9.212170600891113, 10.056442260742188, "The Frequency of the RF communications Communication System is 437.27 MHz."]
+[5.277626991271973, 10.027462005615234, "The Launch Date of the HORYU-2 Nanosatellite is May 17, 2012."]
+[14.541315078735352, 9.799070358276367, "The Wavelength of the SWIR Detector is 3.75 \u00b5m."]
+[8.24077320098877, 10.161569595336914, "The Interface Type of the GOES-R Access System Data Distribution System is Subscription-based and ad hoc data requests."]
+[14.64515495300293, 8.498844146728516, "The Central Wavelength of the Current GOES imager Sensor is 6.19."]
+[9.641021728515625, 12.460892677307129, "The Antenna Aperture of the Radar Radar is 1.5 m x 1.5 m."]
+[-3.46409273147583, 11.345073699951172, "The Latency of the ATL04 Calibrated Backscatter Profiles Data is 21 days."]
+[6.736572265625, 10.772188186645508, "The Test Type of the CO2M Satellite is Shaker test."]
+[8.596485137939453, 9.713149070739746, "The Data Rate of the Satellite Satellite is 25 Mbit/s."]
+[5.265244483947754, 10.368999481201172, "The Launch Date of the OneWeb Satellite Communications Company is From 2022."]
+[13.995759010314941, 11.327159881591797, "The Calibration Lamp Wavelength of the Telescope Optical Instrument is 546.1 nm."]
+[8.324509620666504, 9.416586875915527, "The Processed Imagery of the Image Location Knowledge Satellite Component is < 100 m."]
+[11.985716819763184, 10.00625228881836, "The Temperatures of the Cooler Passive Cooler is 98 K for MWIR/SWIR patch."]
+[12.83617115020752, 8.948993682861328, "The Detectors Type of the REM Radiation Environment Monitor is 300 Tm silicon diode detectors."]
+[8.992558479309082, 9.711543083190918, "The PSD Limit Frequency of the Payload Satellite Component is Until 6.5Hz."]
+[5.654971599578857, 7.9474968910217285, "The Structure Size of the PARASOL microsatellite Satellite is 60 cm x 60 cm x 80 cm."]
+[9.258624076843262, 9.789588928222656, "The Frequency L1 of the GPS receiver Receiver is 1575.42 MHz."]
+[8.532623291015625, 9.627571105957031, "The SGSD Goal of the HYPSO-1 Satellite is Better than 100 m/pixel."]
+[10.98736572265625, 12.119502067565918, "The Projectile Diameter of the Launcher Test Facility is Up to 203 mm."]
+[6.980175971984863, 7.623225688934326, "The Thrusters of the Hydrazine system Orbit control subsystem is Four 1 N thrusters."]
+[11.361339569091797, 9.15908432006836, "The Quantity of the Star Trackers AOCS Sensors is 2."]
+[-3.365891695022583, 11.243979454040527, "The Latency of the ATL07 Arctic/Antarctic Sea Ice Elevation Data is 45 days."]
+[8.17353630065918, 7.526778221130371, "The Voltage Conversion Level of the PCDM Power Conditioning Module is \u00b15 V level."]
+[-3.381193161010742, 11.259157180786133, "The Latency of the ATL14 Antarctica/Greenland Ice Sheet H(t) Gridded Data is 45 days from receipt of last data in product."]
+[10.88411808013916, 7.398514747619629, "The Cost (sensor + spacecraft) of the Push Frame Framer with a fast steering mirror Sensor is Low."]
+[7.361536026000977, 10.240713119506836, "The Developer of the Space Launch System Spacecraft  is NASA/MSFC."]
+[10.349785804748535, 9.700900077819824, "The Mounting Location of the MIRO Instrument is On the spacecraft payload plane."]
+[13.844677925109863, 10.967808723449707, "The Parallelism of the VPW42 Optical Window is \u22645 arcsec."]
+[9.170659065246582, 12.007190704345703, "The Bands of the SRAL SAR Radar Altimeter is C+Ku."]
+[10.588519096374512, 9.693418502807617, "The Number of Physical Modules of the MIRO Instrument is 4."]
+[14.3579740524292, 9.066183090209961, "The Electronic Gains of the Limb Sensor Sensor is Two."]
+[12.328946113586426, 11.63868522644043, "The Mass of the Instrument Instrument is 2.7 kg."]
+[9.915227890014648, 12.324004173278809, "The Average Sigma Naught of the SAR Instrument is -7.5 dB."]
+[12.163846969604492, 11.083773612976074, "The Power of the FSS Instrument is 0.1 W."]
+[7.893083572387695, 10.887701034545898, "The Manufacturer of the ATSR-1 Instrument is RAL, UK (British Aerospace as prime contractor); CRPE, France, and CSIRO, Australia."]
+[12.116974830627441, 11.162065505981445, "The Power Consumption of the CEASE-2 Instrument is 1.7 W."]
+[13.533087730407715, 8.630171775817871, "The Image Size of the Image Sensor Imaging is 37.25 mm x 25.70 mm."]
+[14.969594955444336, 9.990121841430664, "The Spectral Sampling Interval of the LR Spectrometer Spectrometer is 0.6 nm/pixel."]
+[11.547364234924316, 10.207385063171387, "The Thermal Measurement Accuracy of the HTS/AMSR2 Microwave Absorber is 0.4\u00baC (3\u03c3)."]
+[7.579023361206055, 11.249598503112793, "The Instrument of the CryoSat Satellite is Radar altimeter."]
+[5.022721767425537, 8.352093696594238, "The Manoeuvre Frequency of the PARASOL Satellite is Nearly every month."]
+[10.152523040771484, 11.063641548156738, "The Wave Height Measurement Accuracy of the ALT Experiment Altimeter is 10% or 0.5 m, whichever was greater."]
+[13.945993423461914, 10.444385528564453, "The Be Filter Thickness of the X123-SDD X-ray Spectrometer is 8 \u00b5m."]
+[5.107936382293701, 10.242574691772461, "The 3D-HDTV Broadcasting and Broadband VSAT Communication Trial Services of the COMS Satellite is Summer of 2011."]
+[14.913115501403809, 10.033541679382324, "The Spectral Overlap of the VNIR and SWIR bands Spectrometer is 900 nm to 1000 nm."]
+[6.845589637756348, 8.898089408874512, "The Dimensions of the Fragments Space Debris is 2-D or 3-D."]
+[10.699373245239258, 11.308609962463379, "The Resolution of the Interferometric Wide Swath mode (IWS) Operational Mode is 5 m x 20 m."]
+[15.213622093200684, 9.856386184692383, "The Wavelength Range of the HSC Spectrometer Spectrometer is 450-900 nm."]
+[9.652660369873047, 12.555415153503418, "The Swath of the Radar Radar is > 1000 km."]
+[6.955555438995361, 7.67061185836792, "The Hydrazine Quantity of the Hydrazine system Orbit control subsystem is 4.5 kg."]
+[7.234899520874023, 7.540593147277832, "The Power of the solar panels solar panels is Average power of 10 W."]
+[8.968085289001465, 10.205516815185547, "The Frequency Band of the RF Communications Communication System is S-band for TT&C data."]
+[14.399212837219238, 9.702760696411133, "The Wavelength of the VIS Detector is 0.675 \u00b5m."]
+[12.489544868469238, 11.630969047546387, "The Mass of the Instrument Telescope is 967 kg."]
+[13.644109725952148, 9.246737480163574, "The length of the Detector Instrument is 1024 pixels."]
+[9.536197662353516, 12.521890640258789, "The Spatial Resolution (Azimuth) of the Radar Radar is 50 m."]
+[5.143174171447754, 7.749214172363281, "The Presentation Location of the SERB Nanosatellite is Guadalajara, Mexico."]
+[10.755362510681152, 11.196606636047363, "The Swath Width of the MSU-M Multispectral Scanner is 1900 km."]
+[12.208568572998047, 11.513941764831543, "The Mass of the MW Instrument is 1.625 kg."]
+[10.933664321899414, 11.224905967712402, "The Spatial Resolution of the Multispectral Instrument (MSI) Instrument is 10 m."]
+[7.665226459503174, 11.013579368591309, "The Mission Heritage of the POLDER-P Instrument is ADEOS and ADEOS-II."]
+[6.2151994705200195, 10.46434211730957, "The Operations Center of the GIOVE-B Satellite is Telespazio's Fucino Space Center in Italy."]
+[11.643088340759277, 11.763113975524902, "The Measurement Frequency of the TEMPO Instrument is Hourly."]
+[12.65039348602295, 9.958698272705078, "The Cross-Track Detection Range of the Spectrometer Instrument is -30\u00ba to 10\u00ba."]
+[9.198994636535645, 11.95886516571045, "The Operating Modes of the SRAL SAR Radar Altimeter is Conventional radar-altimeter mode, advanced SAR mode."]
+[13.958924293518066, 11.250996589660645, "The Wavelengths of the NuSTAR X-ray Telescope is Almost the whole range of X-ray wavelengths."]
+[9.096192359924316, 11.748388290405273, "The Modes of the RADARSAT-2 Satellite is Spotlight mode, Five wider coverage stripmap modes, Two higher resolution ScanSAR modes for maritime surveillance, Extra wide swath 5 m resolution mode (Extra Fine)."]
+[7.488155364990234, 8.420351028442383, "The Cone Tilt of the SS 433 Cosmic Object is Periodically tilts slightly toward Earth."]
+[11.867919921875, 10.090048789978027, "The Cryogen Lifespan of the Instrument Dewar/Heat Exchanger is 15 months."]
+[4.378889560699463, 9.597188949584961, "The On-Orbit Spare Lifetime of the GOES-R Satellite is 5 years."]
+[15.813898086547852, 10.859501838684082, "The SNR of the Band 1 Spectral Band is 260."]
+[12.283738136291504, 9.89958381652832, "The Operating Temperature of the Detector Imaging Device is < 60\u00baC."]
+[5.221879482269287, 10.929848670959473, "The Launch Year of the RemoveDebris Mission is 2018."]
+[12.211138725280762, 11.20852279663086, "The Power of the ST (Star Tracker) Instrument is 6.5 W."]
+[6.154189109802246, 9.85428524017334, "The Mission Type of the Genesis Satellite is Non-EO."]
+[9.872889518737793, 8.48237133026123, "The Attitude Control of the ACS Attitude Control Subsystem is \u00b10.05\u00ba."]
+[13.999764442443848, 10.457123756408691, "The Effective Si Thickness of the X123-SDD X-ray Spectrometer is 0.5 mm."]
+[5.140544891357422, 10.91005802154541, "The Commissioning Completion Date of the RAIDS Experiment is October 22, 2009."]
+[-3.4222066402435303, 11.301932334899902, "The Latency of the ATL18 Land/Canopy Gridded Data is 45 days from receipt of last data in product."]
+[6.839138984680176, 9.123373985290527, "The Number of Retired Satellites of the DMSP (Defense Meteorological Satellite Program) Satellite Program is 16."]
+[6.2495527267456055, 8.332784652709961, "The Solar Array Normal Vector and Sun Vector Difference of the Spacecraft Satellite is Up to 30 degrees during eclipse seasons."]
+[12.743595123291016, 9.541136741638184, "The FOV of the FSS Fine Sun Sensor is 128\u00ba x 128\u00ba."]
+[6.464479446411133, 7.654724597930908, "The Printed Circuit Board Thickness of the Sprite Tiny Spacecraft is A few millimeters."]
+[10.66247272491455, 11.842103958129883, "The Size of the Antennas Communication Equipment is 9.1 m."]
+[14.840283393859863, 8.88157844543457, "The Spectral Range of the Spectrally modified current sounder Sensor is 8.3-8.7."]
+[9.25527572631836, 9.714035034179688, "The Sampling Rate of the TRSR GPS Receiver is 10 Hz."]
+[13.233922958374023, 9.716176986694336, "The Field of View of the VNIR-NP channels Sensor is 70\u00ba."]
+[5.383727073669434, 9.600213050842285, "The Designation of the OPAL Satellite is OPAL OSCAR-38 (OO-38) by AMSAT."]
+[12.223865509033203, 8.897442817687988, "The Short Circuit Current of the CSS Coarse Sun Sensor is 34 mA."]
+[11.634186744689941, 11.7870512008667, "The Gases Measured of the TEMPO Instrument is Ozone, nitrogen dioxide and formaldehyde."]
+[10.625988006591797, 11.301362991333008, "The Size of the Millimeterwave receiver radiometer is ~ 1.6 mm."]
+[11.42934799194336, 8.54069709777832, "The Sampling Coordination of the Magnetometer Instrument is Coordinated with pulsing by the magnetorquers."]
+[5.167954921722412, 7.612765789031982, "The Developer of the Venta-1 Nanosatellite is VVentspils High Technology Park."]
+[15.201959609985352, 10.413644790649414, "The SNR of the Instrument Spectrometer is \u2265450 @ 620 nm, \u2265300 @ 2100 nm, \u2265200 (for each band)."]
+[6.4073872566223145, 10.074787139892578, "The Country of the skCube Satellite is Slovakia."]
+[11.130558013916016, 10.632835388183594, "The Type of the MWR Radiometer is Dicke."]
+[11.343026161193848, 11.964462280273438, "The Dimensions of the IPEX-II boom ADAM mast is 2.35 m x 0. 3 m x 0.3 m."]
+[9.280665397644043, 12.437976837158203, "The Pulse Repeat Frequency of the X-band Radar is 100 Hz."]
+[9.65592098236084, 11.844711303710938, "The Peak RF Power of the SAR antenna Antenna is 1.8 kW."]
+[5.855989456176758, 8.697894096374512, "The Altitude of the GPS Signal Environment Mapping is Up to geosynchronous orbit (35,900 km)."]
+[5.087477684020996, 11.398820877075195, "The Height of the Falcon 9 first stage Rocket is 42 m."]
+[12.54359245300293, 9.157597541809082, "The Interval of the Observation and Calibration Process is 1.8s."]
+[7.244229793548584, 9.685826301574707, "The Manufacturer of the Bus Satellite Component is  Blue Canyon Technologies."]
+[15.661553382873535, 10.8281831741333, "The Number of Pixels of the Band 1 Spectral Band is 1600."]
+[6.6015753746032715, 10.203643798828125, "The Ground Support Provider of the TanSat Satellite Mission is NSMC (National Satellite Meteorological Center)."]
+[10.900877952575684, 7.3780517578125, "The Cost (sensor + spacecraft) of the Framer Sensor is Very low."]
+[12.684427261352539, 10.611515045166016, "The Ground Resolution (Visible Channel) of the VIRR Instrument is 2.3 km."]
+[6.450353145599365, 7.883915424346924, "The Solar Panels Area of the IRS-1A Satellite is 8.6 m2."]
+[9.178979873657227, 7.135402202606201, "The Corona Temperature of the Sun Celestial Body is On average 1 million degrees Celsius."]
+[12.723000526428223, 10.596232414245605, "The Dynamic Range (Visible Channel) of the VIRR Instrument is 65 - 10,000 fL (scene brightness)."]
+[13.289729118347168, 11.904863357543945, "The Telescope Size of the MOST Satellite is 5.9-inch (15-centimeter)."]
+[10.095562934875488, 2.4821293354034424, "The Total mass of assembly of the STRV-1d DHS Data Handling System is 1.2 kg."]
+[13.57879638671875, 11.251554489135742, "The FOV of the Telescope Optical Instrument is 1.02 R sun \u00b1 2.7/3 R sun."]
+[15.615864753723145, 10.767512321472168, "The Range of the spectral band band is 0.58 - 1.0 \u00b5m."]
+[4.705271244049072, 8.841259002685547, "The Snapshot Frequency of the TESS Satellite is Every two minutes."]
+[11.94526481628418, 11.951455116271973, "The Size of the CEASE-2 Instrument is 10 cm x 10 cm x 8.2 cm."]
+[13.790571212768555, 8.511749267578125, "The Frame Rate of the Camera Imaging Device is 500 frames/s."]
+[4.771536827087402, 10.65407943725586, "The Next Phase Decision Date of the Copernicus Satellite Program is Second half of 2021."]
+[13.784302711486816, 10.554699897766113, "The Energy Range of the X-ray Imager Instrument is 0.1\u20132 keV."]
+[13.600295066833496, 10.25511646270752, "The Electron energy of the Microdosimeter A Instrument is > 50 keV."]
+[9.77546501159668, 12.321592330932617, "The Radiometric Resolution of the SAR Synthetic Aperture Radar is 5-bit raw data."]
+[9.493067741394043, 11.473965644836426, "The Accuracy of the SeaWinds scatterometer Scatterometer is 2 m/s."]
+[9.447279930114746, 8.162076950073242, "The Launch Location of the Bloostar Launch Vehicle is Above 99% of the mass of the atmosphere."]
+[6.719266414642334, 10.194459915161133, "The Partner of the TanSat Satellite Mission is University of Leicester."]
+[7.503034591674805, 8.467692375183105, "The X-ray Light Source of the SS 433 Cosmic Object is Bright."]
+[7.137270927429199, 7.783786296844482, "The Stowed Dimensions of the Spacecraft Bus (Avionics Module=AM) Satellite is 1.1 m x 0.8 m x 0.8 m."]
+[12.671541213989258, 10.603555679321289, "The Scan Rate of the VIRR Instrument is 48 rpm."]
+[13.69447135925293, 11.832578659057617, "The Mount Type of the Telescope Optical Instrument is English mount."]
+[14.254220008850098, 10.123774528503418, "The Energy Steps of the Electron Spectrometer Instrument is 24."]
+[13.396119117736816, 11.306976318359375, "The Entrance Pupil Diameter of the Lens Optical Instrument is 10.5 cm."]
+[13.523970603942871, 11.157811164855957, "The Lens of the TV Camera Camera is Augeniux 50 mm f/0.95 lens."]
+[11.155289649963379, 12.006802558898926, "The Length of the Boom Assembly Assembly is 1.2 m."]
+[13.961908340454102, 8.443631172180176, "The Full Well Charge of the Imager Camera is 60,000 e -."]
+[14.626866340637207, 10.229532241821289, "The Shape Knowledge of the ISRF Instrument Spectral Response Function is Within 1%."]
+[14.711909294128418, 10.64043140411377, "The Mass of the Optical Scanning Design Imaging Spectrometer is 150 kg."]
+[7.645064830780029, 9.222638130187988, "The Type of the Sun Sparc microprocessor Microprocessor is Radiation-hardened."]
+[4.982762336730957, 10.6317138671875, "The Launch Date of the COSMO-SkyMed Di Seconda Generazione Satellite is 18 December 2019."]
+[7.291834831237793, 10.01327133178711, "The Acquisition Cost of the Maxar Technologies Company is $140 million."]
+[9.181617736816406, 7.130015850067139, "The Oxygen Temperature of the Sun's Lower Atmosphere Celestial Body is 320,000\u00baC."]
+[13.668624877929688, 8.718851089477539, "The Star Magnitude Range of the Fast Cameras Camera is 4 to 8."]
+[5.214899063110352, 10.247152328491211, "The Communication Restoration Date of the LightSail Satellite is May 31, 2015."]
+[4.893171310424805, 11.086445808410645, "The Observation Date of the XMM-Newton Space Observatory is June 17, 2020."]
+[10.881545066833496, 11.130374908447266, "The Spatial Resolution of the MSU-SK Radiometer is 170 m (in VIS) and 600 m (TIR)."]
+[6.0224738121032715, 7.295022964477539, "The Mass of the HORYU-2 Nanosatellite is 7.1 kg."]
+[6.908534526824951, 9.05173110961914, "The Number of Satellites of the Iridium Communications Inc. Company is 5."]
+[12.78267765045166, 9.448790550231934, "The Energy Range of the Electrostatic Analysers Sensor is 0.2 to 20 keV."]
+[12.118268966674805, 11.10279655456543, "The Power of the MAG Instrument is 0.2 W."]
+[7.5565338134765625, 7.24811315536499, "The Array Power Average of the Spacecraft Bus (Avionics Module=AM) Satellite is 650 W."]
+[15.647149085998535, 10.801715850830078, "The Wavelength Range of the Band 1 Spectral Band is 365-408 nm."]
+[6.5083208084106445, 10.775384902954102, "The Mission Type of the Meteor-M-2 Satellite is EO."]
+[8.129314422607422, 7.532272815704346, "The Size of the PCU Power Control Unit is Compact."]
+[5.0009684562683105, 10.74543571472168, "The End of Life Date of the Genesis Satellite is September 8, 2004."]
+[6.735851764678955, 10.333953857421875, "The Mission Scientist of the Sentinel-6 Satellite is Craig Donlon."]
+[14.96151351928711, 9.801443099975586, "The Spectral Coverage of the AIRS Atmospheric Infrared Sounder is 0.4 - 1.0 \u00b5m for photometer (4 VNIR bands at: 0.41-0.44, 0.58-0.68, 0.71-0.92, 0.49-0.."]
+[10.093849182128906, 2.4331092834472656, "The Power to sub-experiments of the STRV-2 DHS Data Handling System is 28 V isolated."]
+[7.440987586975098, 11.074554443359375, "The Flights of the AEPI Instrument is Spacelab-1."]
+[10.189579010009766, 11.06013011932373, "The Swath Width of the ALT Experiment Altimeter is Varies from 2.4 to 12 km."]
+[7.139035701751709, 10.07258415222168, "The Manufacturer of the Restore-L Satellite is Maxar."]
+[5.803857326507568, 8.520896911621094, "The Orbit Altitude of the 3U CubeSat Satellite is 505 km."]
+[9.365021705627441, 12.46368408203125, "The Impulse Duration of the X-band Radar is 3 \u00b5s."]
+[10.66039752960205, 11.910616874694824, "The Antenna Size of the DART Spacecraft is 4.5 m."]
+[13.731229782104492, 10.36569595336914, "The X-ray Systems Interval of the Diagnostic Instruments Test Facility is 2 \u00b5s."]
+[8.774873733520508, 9.979043960571289, "The Uplink Speed of the Communication links Communication System is 9.6 kbit/s."]
+[5.272494792938232, 9.686714172363281, "The Operation Status of the NEOSSat Satellite is Operating well."]
+[14.84384536743164, 10.493947982788086, "The Disperser Type of the Instrument Spectrometer is Prism."]
+[5.623279571533203, 7.95869255065918, "The Knowledge of the PARASOL microsatellite Satellite is 0.02\u00ba."]
+[7.064216613769531, 8.586318969726562, "The Total system cost of the WorldView-4 Satellite is $850 million."]
\ No newline at end of file