[3.582620620727539, 6.542792320251465, "The S-band TxRx Data Rate (TM) of the RF communications Communication System is 1.91 Mbit/s or 329 kbit/s."]
[5.563470363616943, 4.098793983459473, "The Ground Station of the SAOCOM-1A Satellite is ETC (Estaci\u00f3n Terrena de C\u00f3rdoba), Argentina."]
[3.9000236988067627, 4.549216270446777, "The Main Tasks of the OBDH OnBoard Data Handling is 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 va."]
[4.651007652282715, 3.5106523036956787, "The Prime Objective of the ZACube-2 Satellite is Demonstrate AIS (Automatic Identification System) message reception."]
[8.43667221069336, 7.742218971252441, "The Detector Orientation of the DIDM Instrument is Facing the S/C ram direction."]
[6.4109296798706055, 3.4768989086151123, "The Type of the Cesium Mission 1 Satellite is On-orbit testbed."]
[6.169034004211426, 4.470922946929932, "The Sensor Complement of the QSat Satellite is 2-band CMOS camera (VNIR) 3000 x 2000 pixels."]
[4.453282356262207, 3.6428134441375732, "The Receiver Type of the AIS Automatic Identification System is Dual polarization."]
[7.308815956115723, 4.583254814147949, "The Imaging Capabilities of the NewSat-6 Satellite is Multispectral and hyperspectral."]
[10.48249626159668, -1.0029314756393433, "The Mass of the ICEYE-X2 Microsatellite is ~ 80 kg."]
[7.007889747619629, 6.348310947418213, "The Data of the Tropomi Satellite Instrument is Used to combine with GHGSat's unique fleet of high-resolution satellites."]
[10.541933059692383, 7.546205043792725, "The Structure Material of the ESTCube-1 & -2 CubeSat is Aluminum (alloy AW 6082-T6)."]
[6.9125657081604, 5.453921794891357, "The Purpose of the SMOS Satellite is Measure soil moisture and ocean salinity."]
[8.029504776000977, 1.7143056392669678, "The Test Location of the Orion Spacecraft Spacecraft is Plum Brook Station in Sandusky, Ohio."]
[8.365066528320312, 3.7572784423828125, "The Alignment Requirement of the SPIDER Telescope is Not required."]
[7.519863605499268, 0.4783822298049927, "The Launch Date of the JPSS-1 Satellite is 2016."]
[7.1358842849731445, 2.411696195602417, "The URL of the SARah project Satellite Project is https://www.army-technology.com/news/newsastrium-german-third-sarah-reconnaissance-satellite/."]
[6.4819512367248535, 4.68360710144043, "The Product Levels of the Sentinel-3 Ocean Surface Topography Mission is Level 1, Level 2/3."]
[11.742390632629395, -0.9629697203636169, "The Mass of the OWLS Payload is 0.5 kg."]
[7.802796363830566, 4.576704978942871, "The Image Resolution of the SPOT-6 Satellite is 1-5 m."]
[5.983508110046387, 1.6180574893951416, "The Ground Control Segment Provider of the PAZ Satellite is Indra."]
[5.416953086853027, 4.077820301055908, "The Functionality Testing of the EDU Lab Testing Facility is Mission capable code."]
[7.948126792907715, 9.05972671508789, "The Observation Wavelength of the NACO Instrument is 3.6 \u00b5m."]
[7.74066686630249, 3.8793375492095947, "The Velocity Regime of the Austfonna Ice Cap is Predominantly slow (~ 101\u2009m/yr) to fast (~ 103\u2009m/yr)."]
[1.1231876611709595, 4.204751491546631, "The Type of the Lithium iron phosphate (LiFePO4) battery Battery is Secondary power source."]
[5.0584564208984375, 3.4505727291107178, "The Mounting Method of the Avionics Satellite Components is Built up into stacks based on a generic SSTL module box design."]
[3.405888319015503, 4.832280158996582, "The Bit Size of the FPGA Processor is 32 bit."]
[4.110743999481201, 3.1676182746887207, "The Integration with 5G New Radio of the Open5GCore Rel. 4 5G Core Network is NSA [S1-MME, S1-U] and SA [N1, N2, N3]."]
[3.5663862228393555, 4.553163051605225, "The Reprogrammable of the FPGA based parallel computing Processing Technology is Yes."]
[8.68093490600586, 5.952870845794678, "The Function of the Magnetic Field Geomagnetic Field is Protecting Earth from cosmic radiation and charged particles."]
[10.626673698425293, 2.5957865715026855, "The Orbit Altitude of the GHGSat-C2 (Hugo) Nanosatellite is 560 km."]
[8.298504829406738, 4.742537021636963, "The Remaining ?V Capability of the PRISMA Satellite is More than 50 m/s."]
[4.2779436111450195, 7.148793697357178, "The Weight of the OSDP Onboard Signal Data Processor is 18 kg."]
[7.916297435760498, 4.615108966827393, "The Camera Resolution of the PhoneSats Satellite is 5 Mpixel."]
[7.024740219116211, 3.2371926307678223, "The Status of the WorldView-1 Satellite is Operational."]
[9.324159622192383, 1.7342151403427124, "The Experiments per Day of the Satellite Satellite is 2-3."]
[9.616021156311035, 9.46840763092041, "The Testing Duration of the SAGE-III Instrument is Nearly five years."]
[9.820464134216309, -0.6287866830825806, "The Attitude System of the Microsatellite Satellite is \u00b110\u00ba."]
[10.692421913146973, 5.281798362731934, "The Intersatellite Link Range of the CNAPS Propulsion System is 5 km."]
[4.329195976257324, 6.669696807861328, "The Frequency of the ICOM-9100 transceiver Transceiver is 144 MHz (Tx), 434MHz (Rx)."]
[12.096471786499023, 2.2293546199798584, "The Science Team Leader of the OSIRIS-REx Spacecraft is University of Arizona, Tucson."]
[6.589810371398926, 0.6729154586791992, "The Launch Date of the TechEdSat Satellite is March 21, 2012."]
[6.609980583190918, 3.516509532928467, "The Collection Areas of the HawkEye 360 Satellite Constellation is Mediterranean, South China Sea, Korean Peninsula."]
[11.033534049987793, -1.4276636838912964, "The Mass of the Diamond nanosatellites CubeSats is 6 kg."]
[3.239841938018799, 5.146830081939697, "The Data Storage of the ASAP-Light Camera System is Non-volatile memory."]
[7.258047103881836, 7.928459644317627, "The Ground Track of the MOMS-2P Instrument is 2000 km."]
[6.617420196533203, 3.7380712032318115, "The Purpose of the ZACube-2 Satellite is Track boats along South Africa's coasts and detect forest fires."]
[6.675207614898682, 4.180708408355713, "The Program of the Sentinel-1C Satellite is Copernicus, a joint European Union and European Space Agency (ESA) Earth Observation program."]
[1.9110701084136963, 4.031091690063477, "The Manufacturer of the Solar Panels Electrical Power Subsystem is Spectrolab."]
[6.651743412017822, 8.326104164123535, "The Main Mode Frequency of the MRSE Instrument is X-band (9.6 GHz)."]
[4.606826305389404, 3.454749584197998, "The Procedure Scripts of the SATLAB Configuration is PLUTO procedure scripts."]
[8.5519437789917, 6.799666404724121, "The Manufacturer of the 3-axis magnetometer Sensor is Honeywell."]
[3.2947607040405273, 5.173652172088623, "The Data Storage of the MAC Memory System Module is 32 Gbit."]
[9.642298698425293, 2.6779696941375732, "The Number of Orbits of the Quasi-Halo Orbits Orbit is 14."]
[10.501195907592773, 2.395087957382202, "The Apogee (km) of the Meteor-3-1 Satellite is 1263."]
[5.61834716796875, 3.744922637939453, "The Objective of the MidSTAR-1 Satellite is Fly two payloads: ICSat (Internet Communications Satellite) and CFTP (Configurable Fault Tolerant Processor)."]
[8.053340911865234, 9.350483894348145, "The Wavelength Range of the InSb Detector is 1.55 - 1.75 \u00b5m."]
[3.9874486923217773, 5.7755327224731445, "The Data Rate of the LEO-LEO Inter-satellite Link Communication System is 5.625 Gbit/s."]
[8.205865859985352, 7.842982769012451, "The Nominal Pointing Range of the Guider Instrument is \u00b130 arcsec."]
[6.555241584777832, 5.389586925506592, "The Spatial Resolution of the TerraSAR-X NG Satellite is Down to 0.25 meters."]
[7.780478477478027, 8.952115058898926, "The Spectral resolution of the UV/VIS Spectrometer Spectrometer is 0.89 nm."]
[7.143970966339111, 2.9526686668395996, "The Operation Mode of the STEREO Mission is Autonomous operation - beacon mode."]
[7.588586807250977, -0.28638380765914917, "The Launch Time of the Rocket 3.3 Rocket is 1:16 a.m. EST (06:16 UTC)."]
[11.760326385498047, -0.8628294467926025, "The Mass of the MERLIN Satellite is 400 kg."]
[5.524207592010498, 3.9163947105407715, "The Estimated Code Reuse of the VMOC Mission Operations Center is Soon approach 95%."]
[6.531408786773682, 0.3766486644744873, "The Mission Status Presentation Date of the SMART-1 Satellite is March 13-17, 2000."]
[7.061800956726074, 4.435874938964844, "The Measurement Domain of the CASSIOPE Satellite is Gravity and Magnetic Fields."]
[7.766236782073975, 3.5275840759277344, "The Interferometric Baseline of the ERS-2 Satellite is Optimal with 30 min. separation."]
[6.142375946044922, 5.009433746337891, "The Host of the OSIRISv2 Instrument is BiROS satellite."]
[9.298637390136719, 6.477035999298096, "The Position of the Star Tracker Device is Left."]
[6.169120788574219, 9.66016674041748, "The Mass of the Photometer Instrument is \u2264 0.9 kg."]
[9.393928527832031, 6.00474739074707, "The Accuracy of the SpinKF Attitude Determination System is Best available attitude accuracy."]
[9.519975662231445, 9.515816688537598, "The Size of the SAGE-III Instrument is 73 cm x 45 cm x 93 cm."]
[7.319084167480469, 0.388381689786911, "The Launch Date of the ASTRO-H Satellite is Feb. 17, 2016."]
[4.609774589538574, 0.2284696400165558, "The Number of Satellites in Orbit of the OneWeb Low-Earth-Orbit Broadband Venture is 254."]
[5.5940117835998535, 9.114873886108398, "The Power Consumption of the Instrument Satellite Instrument is < 24 W."]
[10.1882963180542, 4.264619827270508, "The Bipropellant System Lunar Departure \u0394V of the Clementine Spacecraft is About 540 m/s."]
[7.582159519195557, 5.439512729644775, "The Drought Impact of the OCO-2 Satellite is Increased carbon dioxide release."]
[4.480778217315674, 4.39353084564209, "The Recommendation of the Connector Savers Component is Future projects should consider their implementation for external access ports."]
[10.384618759155273, 5.658825397491455, "The Orbit Inclination of the ProSEDS Tether Demonstration Experiment is 35\u00ba."]
[8.519938468933105, 1.6701185703277588, "The Announcement Date of the Photon Sieve Optics Technology is June 4, 2012."]
[4.011570930480957, 6.334964275360107, "The Data Transmission of the LT Device is Lithium radio."]
[6.175261974334717, 2.8659403324127197, "The SOC Deputy Head of the Roman Space Mission is Cristina Oliveira."]
[6.104167938232422, 2.884716749191284, "The Manufacturer of the Icarus-1 Drag Sail is Cranfield University."]
[2.249481678009033, 4.4347615242004395, "The Power of the Spacecraft Satellite is ~1.5 W."]
[8.715288162231445, 8.103389739990234, "The Location of the RADFET dosimeters Dosimeters is ESS (Experiment Support System) PCB."]
[9.155294418334961, 1.239363670349121, "The Data Collected of the GP-B mission Mission is Over 1 TByte."]
[6.6182403564453125, -0.32700249552726746, "The Launch Date of the QZS-3 Satellite is June 16, 2017."]
[6.155975341796875, 0.6361681222915649, "The Pilot Program Start Date of the CubeSat Satellite is Nov. 10, 2010."]
[8.635104179382324, 10.632593154907227, "The MTF of the CCD Camera Imaging System is <=0.23."]
[6.940118789672852, 8.77150821685791, "The Field of View of the LISS-IIM Instrument is \u00b15\u00ba."]
[2.253594160079956, 3.8161709308624268, "The Solar Generator Configuration of the MicroSCOPE Satellite is Two identical wings of one panel each, mounted on Y panels and directed toward +X."]
[7.262267112731934, 9.615006446838379, "The Power of the S-192 optomechanical scanner Scanner is 266 W."]
[6.963586807250977, 2.4982948303222656, "The URL of the D-Sat Satellite is https://www.dsat.space/."]
[11.710285186767578, 3.0053751468658447, "The Orbit Inclination of the LitianicaSAT-2 Nanosatellite is 97.44\u00ba."]
[6.502622604370117, 3.1895751953125, "The Objectives of the YouthSat Satellite is 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."]
[9.419093132019043, 7.792202472686768, "The Measurement Range of the Particle Detector Instrument is Helium-4 : 10 MeV/n ~ 400 MeV/n."]
[11.42887020111084, -1.2092663049697876, "The Spacecraft Mass of the QSat Satellite is < 50 kg."]
[8.039628028869629, 6.342118263244629, "The PUI Measurement Resolution of the IMAP Satellite is < 1 min."]
[2.016991138458252, 7.846899509429932, "The Solar Wind Speed and Beta of the ACE Satellite is ~38% lower on average from 2009 through the day 79 of 2013."]
[11.134283065795898, 4.011954307556152, "The Publication Date of the TOI-178 Exoplanet System is 25 January, 2021."]
[4.3813581466674805, 7.7697834968566895, "The Center Frequency of the Channel 2 Sensor is 18.7 GHz."]
[7.469083309173584, 8.970359802246094, "The Interference Nadir Gap of the NNI Synthetic Aperture Nadir Altimeter is \u00b14 km."]
[7.526816368103027, 5.490228176116943, "The Reliability of the Aeolus Satellite is 95%."]
[6.806169509887695, 1.2881256341934204, "The Topical Team Meeting Date of the ASIM Payload System is June 26-27, 2006."]
[9.399215698242188, 9.195202827453613, "The Entrance Pupil Diameter (mm) of the FCI-TA Instrument is 300."]
[6.625052452087402, 0.5827991366386414, "The SEVIRI HRV Image Date of the Meteosat-10 Satellite is 19 July 2016."]
[7.76301908493042, 0.7322468757629395, "The Launch Date of the SLS with Orion Space Launch System is 8 March 2018."]
[6.132759094238281, 5.614477157592773, "The Amazon Basin Size of the Biomass satellite Satellite is Over six million km2."]
[7.119155406951904, 2.685299873352051, "The URL of the SWOT Satellite is http://smsc.cnes.fr/SWOT/."]
[6.808901786804199, 4.738008975982666, "The Mission Type of the Sentinel-4 Satellite is Geostationary component of European (EC, ESA) operational atmospheric composition monitoring missions."]
[6.385383605957031, 4.865598201751709, "The GNSS-RO of the Sentinel-6 Satellite is Instrument."]
[11.767715454101562, 3.366734743118286, "The Proposed Rate of Change of the Delta in Solar Phase of Apsides Orbital Parameter is 3.6\u00ba/ year."]
[6.040909290313721, 3.948321580886841, "The Location of the HIFI Instrument Control Center is SRON Netherlands Institute for Space Research, Groningen, the Netherlands."]
[9.498696327209473, 1.4918091297149658, "The Initial Staffing of the LMOC and OGSs Ground Segment is 8 hours per day, 5 days per week."]
[10.229273796081543, 1.7855761051177979, "The Period (min) of the Cosmos-1066 (Astrofizika) Satellite is 102.2."]
[7.487600326538086, 3.949059247970581, "The Observation of the STSat-1 Satellite is Airglow."]
[4.447035312652588, 4.949477672576904, "The ITR (Integrate-Than-Read) and IWR (Integrated-While-Read) of the Device Operation Modes is In ITR mode, the signal integration and the read-out cycle are separated in time, whereas in IWR mode, the device starts already a new integration cycle while the information of the previous line is read out."]
[6.116029262542725, 6.317524433135986, "The Orbit Inclination of the TecSAR SAR is 41\u00b0."]
[11.549192428588867, 4.439474582672119, "The Type of the AU Microscopii Star is M dwarf."]
[10.308913230895996, 7.126797199249268, "The Flaps Material of the Thermal Control Louvers Thermal Regulation Device is Aluminum."]
[6.728857040405273, 0.7452351450920105, "The Launch Year of the SARLupe Satellite is 2006."]
[11.822787284851074, 1.0328278541564941, "The Number of Lunar Landings of the Chang'e-5 Spacecraft is 3."]
[4.420223712921143, 6.046086311340332, "The Control Type of the Dual-channel Receiver Unit (DRU) Receiver is Manual or Automatic."]
[8.951321601867676, 2.9178359508514404, "The Science Objectives of the LRO Lunar Reconnaissance Orbiter is Bombardment history of the Moon, Lunar geologic processes, The processes that have shaped the global lunar regolith."]
[5.519450664520264, 7.456553936004639, "The Tx Bandwidth of the KaRIn Instrument is 200 MHz."]
[5.172196388244629, 6.595539569854736, "The Surface Error of the Antenna Communication is Less than 2.4 mm rms."]
[11.78829574584961, 3.338456153869629, "The Contact Attempt Elevation Angle of the Polar Scout Satellite is Above 10 \u00ba."]
[9.779537200927734, 3.159893751144409, "The Orbit Parameters of the GEOS-1 Satellite is 1,114 x 2,273 km x 59.4\u00ba."]
[8.526869773864746, 5.4693121910095215, "The Off Nadir Acquisition Capability of the Satellite Imaging Satellite is Up to 1 path off nadir."]
[7.577358245849609, 4.708925724029541, "The Nominal Scenario Orbit Phases of the PROBA-V Satellite is Geodetic attitude with yaw steering correction, Sun-bathing mode, Geodetic pointing mode, Reactivated to reach thermal stability."]
[6.405793190002441, 4.118740081787109, "The Testing Facility of the CO2M Satellite is Largest satellite test facility in Europe."]
[8.400421142578125, 4.217206001281738, "The Topics Addressed of the INTEGRAL Satellite is 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 h."]
[10.027259826660156, 4.610836029052734, "The Attempted ?V Maneuver of the Satellite Spacecraft is 7 m/s."]
[9.64051342010498, 2.249730348587036, "The Cross-Track Motion Control of the CloudSat Satellite is Within \u00b11 km of the CALIPSO ground track."]
[7.699184417724609, 3.7356784343719482, "The Data Access of the Pl\u00e9iades Neo constellation Satellite Constellation is Immediate."]
[10.076512336730957, 6.973116874694824, "The MLI Area Ratio of the MLI Thermal Control Device is Unknown."]
[8.195087432861328, 4.512295246124268, "The Swath of the Sentinel-2 satellites Satellite is 290 km."]
[7.055541038513184, 4.944783687591553, "The Importance of the Satellites Observation Tool is Crucial for monitoring climate-related phenomena."]
[11.13163948059082, 2.0169994831085205, "The Drill Length of the Rosalind Franklin ExoMars rover Rover is 2 m."]
[4.0077290534973145, 5.692720890045166, "The Data Transmission of the CubeRRT Satellite is On-board filtering requires 99% less data to be downlinked."]
[8.657748222351074, 0.15696527063846588, "The Crew Size of the Skylab-1 Space Station is Three astronauts."]
[4.54911470413208, 2.1217756271362305, "The Number of Orbited Satellites since May of the Starlink Communication Satellite is 420."]
[10.027729988098145, 3.0976734161376953, "The Orbit Altitude of the GF-3 Satellite Satellite is 755 km."]
[3.516446828842163, 5.123896598815918, "The Data Storage of the LIRIS Laser Infrared Imaging Sensors is Hard disks in ATV's cargo hold."]
[7.991393566131592, 7.462165832519531, "The New York Second (NY sec) of the FIELDS Instrument Instrument is 217/150,000 ~ 0.873813 sec."]
[10.087772369384766, 1.5168977975845337, "The Period of the LAGEOS Satellite is 225 min."]
[6.910820960998535, 0.8832656741142273, "The Launch Date of the SmallGEO Satellite is Jan. 28, 2017."]
[8.066890716552734, 7.388303279876709, "The Internal Sampling Clock Frequency of the FIELDS Instrument Instrument is 150,000 Hz."]
[5.148111343383789, 1.6839725971221924, "The Planned Launches in 2018 of the ICEYE Company is At least two additional missions."]
[6.786172389984131, 0.5647143721580505, "The Contract Announcement Date of the Transport Layer Tranche 1 Satellite System is By the end of the month."]
[6.912230491638184, 5.565540790557861, "The Ocean Salinity Measurement of the SMOS Satellite is Unknown."]
[11.742044448852539, 7.483800411224365, "The Stability of the Deep Space Atomic Clock Atomic Clock is Time deviation of less than four nanoseconds after more than 20 days of operation."]
[9.550149917602539, 0.43686264753341675, "The Design Life of the Optsat-3000 Satellite is 7 years."]
[10.573419570922852, 4.891356468200684, "The Placement of the Test Masses Components is Float freely within the spacecraft."]
[8.77178955078125, 5.253750324249268, "The Angular Velocity Stabilization Accuracy of the Resurs-DK1 Spacecraft is 0.005o/s."]
[7.759179592132568, 8.925297737121582, "The Channels of the VISSR Instrument is Water vapor (6.5 - 7.0 \u00b5m), Infrared (10.5 - 11.5 \u00b5m), Infrared (11.5 - 12.5 \u00b5m)."]
[6.372663497924805, 9.227105140686035, "The Housing Dimensions of the MuREM Radiation Monitor is 10 x 6 x 6 cm."]
[7.22213077545166, 3.0123586654663086, "The Mission Status of the Kaber Spacecraft is Unknown."]
[6.3993144035339355, 1.1511640548706055, "The Constellation Maintenance Presentation Date of the COSMO-SkyMed Satellite Constellation is Feb. 24-26, 2003."]
[4.877157211303711, 6.017638206481934, "The Frequency Range of the CubeRRT Satellite is 6-40 GHz."]
[4.962350845336914, 6.186827659606934, "The Frequency (MHz) of the Compass-BeiDou B2a Signal Carrier is 1175.00."]
[12.06820297241211, 3.3196589946746826, "The Inclination of the COMPASS-1 Satellite is 98.85\u00ba."]
[9.796650886535645, 6.681751728057861, "The Operating Temperature Range of the CubeSat Satellite is -5\u00baC to 20\u00baC."]
[6.649490833282471, 0.9828453063964844, "The Progress Update and Launch Plan Date of the FORMOSAT-7/COSMIC-2 Satellite Constellation is April 16-22, 2015."]
[4.864897727966309, 9.027420043945312, "The Heat Probe of the InSight Lander Lander is HP3 (Heat Flow and Physical Properties Probe)."]
[9.131492614746094, 9.158285140991211, "The FOV of the FSI dual EUV 174 \u00c5 and 304 \u00c5 alternatively Passband center is 5.2\u00ba x 5.2\u00ba."]
[9.275927543640137, 9.091753959655762, "The f/D of the Limb Imager Telescope is 7.3."]
[10.136213302612305, 4.339059829711914, "The Bipropellant System Lunar Insertion \u0394V of the Clementine Spacecraft is About 550 m/s."]
[9.173142433166504, 4.133090972900391, "The Size of the Flight Unit Satellite Component is About the size of a desktop computer."]
[8.721202850341797, 4.85772180557251, "The Orbital Navigation Solution of the NEMO-AM Satellite is Position: 12 m (2\u03c3), Velocity: 6 cm/s (2\u03c3)."]
[6.274003505706787, 7.4059367179870605, "The Components of the DBCP Dual Babinet Compensator Pseudo-depolarizer is Four wedges of birefringent material arranged in pairs."]
[3.2295384407043457, 4.184618949890137, "The VHF-UHF Transceiver of the IOD-1 GEMS Satellite is CPUT (Cape Peninsula University of Technology) VHF-UHF Transceiver (VUTRX) with CSL ADM (Antenna Deployment Mechanism)."]
[8.043303489685059, 0.8648030161857605, "The Launch Date of the Landsat 9 Satellite is Unknown."]
[10.320391654968262, 7.042873859405518, "The Mass Budget of the ALBus R&R Design is Under 4 kg."]
[5.050769329071045, 4.55288028717041, "The Coverage Area of the Ground Segment Ground Control Infrastructure is Alps, Pannonian Plain, and Mediterranean region."]
[7.219963550567627, 5.588998317718506, "The Objective of the SeaWiFS Satellite is Measurement of reflected visible sunlight from the ocean surface for the derivation of ocean-color data."]
[7.376004219055176, 3.811453104019165, "The Price of the Landsat-7 Satellite is The price tag for Landsat-7 imagery is substantially lower than for the commercial products of Landsat-4 and -5."]
[4.230865478515625, 6.962306499481201, "The 1st LO of the HRIT HiRID Data Receiver is 1900."]
[4.407445430755615, 3.8135428428649902, "The Input of the Onboard Neural Network Artificial Intelligence is Magnetic or electric component in the VLF range."]
[8.574626922607422, 2.334101915359497, "The Specialty of the Brian Metzger Theoretical Astrophysicist is Cosmic mergers \u2013 collisions between a variety of objects, whether they be planets and stars or two black holes."]
[7.57135009765625, 2.2948319911956787, "The URL of the DeorbitSail Spacecraft Mission is http://www.athena-spu.gr/projects/DeOrbit."]
[11.503042221069336, 2.1621663570404053, "The URL of the Hayabusa2 Asteroid Explorer is http://www.jspec.jaxa.jp/e/activity/hayabusa2.html."]
[10.206564903259277, 4.83795690536499, "The Presentation Date of the Miniature Ion Propulsion System Propulsion System is Oct. 10-13, 2012."]
[6.530559062957764, 4.356061935424805, "The Telescope Type of the R3 spacecraft CubeSat is Refractive."]
[5.9431633949279785, 3.0132882595062256, "The Agency of the SMART Satellite is Ben-Gurion University (BGU)."]
[10.794517517089844, 7.295036315917969, "The Energy Band of the JEM-X X-Ray Monitor is 3 - 35 keV."]
[7.936965465545654, 0.46708235144615173, "The Operation Start Date of the CryoSat-2 Satellite is April 8, 2010."]
[6.155976295471191, 9.86638355255127, "The Mass of the VPU Video Processing Unit is 3.2 kg."]
[5.333741664886475, 3.1302452087402344, "The | of the EnMAP Satellite Bus Satellite Bus is EnMAP Satellite Bus - A Cost Effective Platform for Advanced Earth Observation Missions."]
[12.104927062988281, 3.2725861072540283, "The Orbit Inclination of the Landsat-9 Satellite is 98.2\u00b0."]
[7.990086078643799, -0.6862012147903442, "The Overview URL of the Dragon SpX-3 Cargo spacecraft is http://www.spaceflight101.com/dragon-spx-3-cargo-overview.html."]
[2.1112170219421387, 4.6763410568237305, "The Projected EOL of the Payload Power Power Generation is 140 W."]
[8.23559284210205, 7.281002998352051, "The Detection of the FIELDS Instrument is Natural, low-frequency radio signal."]
[7.241992950439453, 0.968830406665802, "The Launch Date of the M3MSat Satellite is April 28, 2008."]
[7.054716110229492, 1.690573811531067, "The Meeting Date of the Swarm Satellite is June 24-26, 2009."]
[6.084413528442383, 3.5524094104766846, "The Service of the Spire Global UK Company is Manage busy docks safely and market traders to price the goods carried aboard."]
[7.545194149017334, 7.493025779724121, "The Gimbal Tracking of the SOTA Satellite is \u00b1100 \u00b5radians."]
[6.500792503356934, -0.07798606157302856, "The Atomic Clocks of the Indian Regional Navigation Satellite System (IRNSS) Satellite System is Replacement."]
[7.7250142097473145, 13.5758695602417, "The Resolution \u0394\u03bb (0.10\u00ba slit) of the SPIM5 Spectrometer is 4.3 nm."]
[12.133444786071777, 5.375805854797363, "The Dark Energy Percentage of the Universe Cosmology is 70 percent."]
[8.4880952835083, 8.923503875732422, "The -1 Order Diffraction Angle (780 nm) of the Diffracted Beam Light is 30.9 \u00ba."]
[9.13177490234375, 4.440497875213623, "The Telescope Size of the MOST Satellite is 5.9-inch (15-centimeter)."]
[8.819839477539062, 7.308687686920166, "The Number of Instruments of the PIMS Plasma Instrument is 2."]
[8.63976764678955, 10.522564888000488, "The CCD Array Elements of the LISS-4 Camera is 12,288 elements for each band."]
[6.5730462074279785, 7.7638936042785645, "The Heat Dissipation of the Power Laser Head Subsystem is ~150 W."]
[8.314125061035156, 3.1800825595855713, "The Mission Objectives of the TanDEM-X Satellite is Generating a global HRTI-3 DEM."]
[7.679635047912598, 9.212915420532227, "The Spectral Range of the Spectral Band D Spectrometer is 0.76 - 0.86 \u00b5m."]
[4.006651878356934, 2.315558671951294, "The Size of the Dellingr Nanosatellite is 6U."]
[6.562317848205566, 3.5702550411224365, "The Mission Type of the GEOSAT Satellite is EO."]
[7.042036533355713, 7.394734859466553, "The Long-Term Stability of the MIRAS Radiometer is 0.18 K/year."]
[6.426921844482422, 5.464648723602295, "The Function of the Satellite STRATOS is Performs POD (Precise Orbit Determination)."]
[7.127077579498291, 0.6978536248207092, "The Attitude Control System Testing Date of the Odin Satellite is Oct. 18-21, 1999."]
[8.275782585144043, 1.549540400505066, "The Launch Date of the Kepler Mission Space Telescope is March 7, 2009."]
[6.4513654708862305, 0.58184814453125, "The Reentry Date of the HaloSat Satellite is January 4, 2021."]
[8.475916862487793, 7.485006332397461, "The Purpose of the Refocus Mechanism Assembly Mechanism is Fine-tune the instrument focus."]
[9.134191513061523, 10.551587104797363, "The GSD (Ground Sample Distance) of the Camera Payload is 1.5 m at an altitude of 650 km."]
[6.810032367706299, 3.8529818058013916, "The Concept Purpose of the Dedicated Satellite Constellation Satellite Service is Exclusive control over a number of satellites over a specific geographical region."]
[6.641134738922119, 0.6038933992385864, "The Arrival Date of the Meteosat-8 Satellite is 21 September, 2016."]
[10.910696029663086, -1.4207909107208252, "The Cargo Mass of the SpaceX Cargo Resupply Mission is 2,910 kg."]
[7.866004943847656, 5.403976917266846, "The Testbed for Precise Onboard Orbit Determination of the SAC-C Satellite is Unknown."]
[7.070672512054443, 2.924791097640991, "The Development Status of the MULA Satellite is In progress."]
[7.66471529006958, 8.89193344116211, "The Wavelength of the Responsivity Measurement Instrument is 1495 nm."]
[4.056990146636963, 4.584787845611572, "The Bus Type of the PIC microcontroller Microcontroller is SPI (Serial Peripheral Interface)."]
[8.485873222351074, 4.371678352355957, "The Differential Photometry of the BRITE Satellite is < 0.1%."]
[9.322747230529785, 5.217567443847656, "The Effect of Earth's magnetic field of the Reaction Wheels Satellite Component is Causes a weak drag."]
[7.898392200469971, 9.69959831237793, "The Spatial Resolution of the Optical Arrangement Imaging System is 250 m, 500 m, and at 1 km at nadir."]
[9.380419731140137, 2.8303511142730713, "The Maneuvers of the OMOTENASHI Satellite is Two deterministic maneuvers."]
[7.997696876525879, 7.2724223136901855, "The Master Clock Frequency of the FIELDS Instrument Instrument is 38.4 MHz."]
[5.397762775421143, 5.896306037902832, "The Antenna Shape of the Satellite Communication Satellite is Umbrella."]
[7.2098565101623535, 4.228731155395508, "The Signal Strength of the Robusta Satellite is Weak."]
[8.49474811553955, 8.264421463012695, "The Detector Type of the ELENA Instrument is MCP (Micro-Channel Plate) detectors."]
[11.307625770568848, 1.30344820022583, "The Distance from Mars of the Tianwen-1 Mars Mission is 2.2 million kilometers (1.4 million miles)."]
[3.775556802749634, 6.151474952697754, "The Modulation of the Optical Downlink Communication System is 16-ary PPM format."]
[9.30023193359375, 10.1384916305542, "The Focal Length of the Kowa LM16JC lens Lens is 16mm."]
[11.680733680725098, -1.0821373462677002, "The Maximum Possible Value (MPV) Mass of the PUNCH Mission Satellite is 54.9 kg."]
[6.2080488204956055, 1.7430152893066406, "The Founding Year of the Kleos Space Company is 2017."]
[7.538422584533691, 1.4500367641448975, "The Data Return of the IXPE Satellite is March 22, 2022."]
[11.620790481567383, 2.0506949424743652, "The Confirmation of the MASCOT Asteroid Lander is Small fragments of carbon-rich asteroids are too fragile to survive entry into Earth\u2019s atmosphere."]
[10.315132141113281, 5.299073696136475, "The Maximum Capacity of the Xenon Gas Tank Propellant Storage is 82 kg."]
[3.9922659397125244, 6.424048900604248, "The Design Purpose of the Data Processing Pipeline System is Accommodate both products in each of the six spectral bands."]
[8.307052612304688, 3.668867349624634, "The Engineering Activities of the TDP Operations Satellite Operations is Not performed by Inmarsat."]
[7.4191741943359375, 5.582107067108154, "The Effect of the Deep Ocean Trenches Natural Feature is Producing a dip on the sea surface."]
[7.857543468475342, 4.590560436248779, "The Measurement Rate of the Claire Satellite is 500th measurement on 09 December 2016."]
[7.44996452331543, 8.196778297424316, "The Altitude Range of the Temperature Ch. 4 difference & ch. 7 difference Measurement Device is 50 - 100 km."]
[3.976895570755005, 6.473133563995361, "The Modulation of the S-band Transmitter Transmitter is DQPSK (Differential Quadrature Phase Shift Keying)."]
[5.088429927825928, 1.9404114484786987, "The Telemetry Frames Received of the SONATE CubeSat Satellite is More than 5000."]
[7.919308185577393, 7.153121471405029, "The Principal Investigator of the SIMPL Investigation is Talbot Jaeger."]
[6.858216285705566, 2.6632802486419678, "The URL of the VRSS-1 Satellite is http://cn.cgwic.com/VRSS-1/english/satellite.html."]
[9.159199714660645, 5.053484916687012, "The Stabilization of the Picard microsatellite Satellite is Three-axis."]
[8.421150207519531, 3.8994455337524414, "The Performance of Rotation Equipment of the Satellite Spacecraft is No degradation."]
[8.915114402770996, 10.499975204467773, "The Pixel Size of the Imager Camera is 9.0 \u00b5m x 9.0 \u00b5m."]
[8.209855079650879, 6.8128533363342285, "The Function of the SWEM Instrument is 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."]
[6.224938869476318, 2.026582956314087, "The Designation of the OPAL Satellite is OPAL OSCAR-38 (OO-38) by AMSAT."]
[6.25029993057251, 6.8832173347473145, "The Capability of the ARC Active Radar Calibrator is Change the transmit frequency for the evaluation of the Doppler processing."]
[10.346643447875977, 7.666674613952637, "The Young's Modulus of the Aluminum foil layers Material is 68 GPa."]
[6.312841415405273, 2.592238426208496, "The Operator of the Bluecrab supercomputer cluster Supercomputer Cluster is Maryland Advanced Research Computing Center."]
[9.343003273010254, 5.702172756195068, "The Initial Design of the DFACS Attitude Control System is FEEP (Field Emission Electric Propulsion)-type system."]
[7.2010016441345215, 5.755349159240723, "The Wind Velocity Range (Stratosphere) of the Aeolus Satellite is 2 - 16 km."]
[9.56475830078125, 0.47949352860450745, "The Design Life of the GCOM-W1 Satellite is 5 years."]
[7.305560111999512, 10.173133850097656, "The Revisit Times of the HyperScout Imager is Sub-daily."]
[4.537352085113525, 6.0590033531188965, "The Uplink Frequency of the SCD-2 Satellite is 401.650 MHz and 401.620 MHz."]
[4.787974834442139, 5.071054458618164, "The Ground-Station Uplink Passes of the SpinSat Satellite is Several."]
[7.3731608390808105, 0.6328871250152588, "The Camera Deployment Date of the TechDemoSat-1 Satellite is 31 May 2019."]
[8.62354850769043, 8.807699203491211, "The Central Output Angle of the Long Wavelength Band Spectrometer is -5.28\u00ba."]
[6.732361316680908, 4.436588764190674, "The Land-surface Temperature Imaging of the Copernicus Sentinel-3 Satellite is Data."]
[9.151937484741211, 3.2387566566467285, "The Orbit of the Satellite Imaging Satellite is Sun-synchronous dawn-dusk."]
[5.8113884925842285, 0.7554783225059509, "The Operation Start Date of the AlSat Nano Satellite is July 24, 2017."]
[6.0075554847717285, 3.110664129257202, "The Program Partners of the SloshSat-FLEVO Satellite is ESA, the (Dutch) Ministry of Economic Affairs, NIVR (Netherlands Agency for Aerospace Programs), and NRL (National Aerospace Laboratory)."]
[9.69522476196289, 8.20447063446045, "The Effective Area of Main CsI Crystal of the GRS Gamma-Ray Spectrometer is 118 mm."]
[4.773877143859863, 2.423485279083252, "The Spacecraft Type of the ABEX CubeSat is 12U CubeSat."]
[9.475708961486816, 3.0569615364074707, "The Orbit of the SkySat 3 Satellite is Sun-synchronous orbit of ~ 500 km."]
[7.9663872718811035, 7.405404090881348, "The Purpose of the GOLF Instrument is Study of the internal structure of the sun by measuring the spectrum of free global oscillations."]
[9.020318984985352, 3.6055991649627686, "The Orbit Position of the BeiDou-1E Satellite is GEO, 160\u00ba E."]
[8.610709190368652, 8.858434677124023, "The Dispersed Images of the HETG Grating is Form a shallow X centered at the undispersed (zeroth order) position."]
[6.426440715789795, 5.349534034729004, "The Operation of the GRAS Global Navigation Satellite System Receiver for Atmospheric Sounding is Supplies atmospheric soundings of the temperature and humidity of the Earth\u2019s atmosphere."]
[6.928005218505859, 1.648488163948059, "The Launch Date of the GPM Core spacecraft Satellite is 2014."]
[9.591192245483398, 5.970296382904053, "The Attitude Determination Accuracy of the ADCS Attitude Determination and Control Subsystem is \u22640.03\u00ba (3\u03c3, 3-axis)."]
[4.928501605987549, 4.755878925323486, "The Operational of the GENSO Ground Station Network is By the time that Delfi-n3Xt is launched."]
[3.369140625, 6.4743971824646, "The Power Supply of the MnACQ-2000 Miniature Network Data Acquisition System Data Acquisition System is Radiation tolerant."]
[5.9770894050598145, 6.078436851501465, "The Multi-Look of the Capella SAR System is 20."]
[3.5727462768554688, 5.711202621459961, "The Data Transport of the SPA-S Interface is 400~600 Mbit/s."]
[7.851334095001221, 4.062932968139648, "The Melting Effect of the Ice Material is Earth re-adjusts and immediately rises by a few millimeters."]
[6.163735866546631, 3.3655526638031006, "The Led by of the Space component Component is ESA (European Space Agency)."]
[8.484726905822754, 7.135673522949219, "The Purpose of the CIP Instrument is In-situ measurements of the ionospheric plasma compositions, ion concentrations, velocities, and temperatures."]
[5.909112453460693, 4.591454982757568, "The Design of the Cupola Windows Space Station Component is Four layered front to potential impactors: a debris pane, two pressure panes, and an inner scratch pane."]
[9.437315940856934, 0.6116532683372498, "The Study Duration of the Odin Satellite is Over 20 years."]
[6.220302581787109, 2.422523021697998, "The Operating Organizations of the Jason-3 Satellite is NOAA, NASA, CNES, EUMETSAT."]
[9.861159324645996, 3.952688694000244, "The Launch Vehicle of the NanoSail-D Satellite is Falcon-1."]
[3.5195634365081787, 4.070011138916016, "The Power to sub-experiments of the STRV-2 DHS Data Handling System is 28 V isolated."]
[9.18659782409668, 3.219561815261841, "The Orbit of the AERO and VISTA Satellites is Sun-synchronous polar orbit."]
[6.241743087768555, 3.534259557723999, "The Managing Organization of the SWEAP Investigation Investigation is SAO (Smithsonian Astrophysical Observatory)."]
[10.565169334411621, 7.515029430389404, "The Bus Structure Material of the QSat-EOS bus Microsatellite bus is Aluminum alloy (A5052-H32)."]
[8.01004695892334, 5.222578525543213, "The SNR of the ALOS/PRISM Satellite is >70."]
[6.955865859985352, 2.1350297927856445, "The Leaders of the Cosmological Simulations Working Group Organization is Pablo Fosalba (ICE, IEEC-CSIC) and Romain Teyssier (Institute for Computational Science at the University of Zurich)."]
[7.1982245445251465, 3.458981990814209, "The Unknown of the Sensor System Satellite Component is Unknown."]
[5.798163890838623, 3.671178102493286, "The Pipeline Software Developer of the GBOT Project is GBOT group in Paris."]
[7.02280855178833, 3.5349183082580566, "The Location of the High-Latitude Cold-Season Snowfall Campaign Field Campaign is Ontario, Canada."]
[3.7523396015167236, 6.425196647644043, "The Coding of the Channel Communication System is 1/4 to 9/10 FEC."]
[5.254000663757324, 4.6402997970581055, "The Location of the Ground Station Ground Station is Kaluga (Russia)."]
[6.347827434539795, 2.217437744140625, "The Receiver Type of the Envisat Satellite is 2nd generation receiver (11 kg), a bi-frequency system in 2 channels."]
[8.18471622467041, 9.299957275390625, "The Wavelength Range of the HgCdTe Detector is 10.4 - 12.5 \u00b5m."]
[7.769327163696289, 9.119511604309082, "The NER of the Spectral Band B Spectrometer is 6.0 x 10^-6 W/(cm^2 sr \u00b5m)."]
[5.827645301818848, 6.773444175720215, "The Swath Width of the C-RADAR Phased Array Antenna System is 225 km."]
[8.307071685791016, 3.58522629737854, "The Mission Overview and Status of the TanDEM-X Satellite is Not Provided."]
[6.958469390869141, 9.185901641845703, "The Azimuth Resolution of the P Mode Observation Mode is 1 m."]
[9.542560577392578, 5.521522521972656, "The Control Type of the AOCS Attitude and Orbit Control Subsystem is Bias-wheel and magnetic torquer control."]
[9.0897798538208, 7.064301013946533, "The Reference Vector of the Sun Sensor Sensor is Coarse sun model from an astronomical almanac."]
[7.750082969665527, 10.789167404174805, "The Data Input of the Data Handling System System is 11-bit."]
[13.08167552947998, 4.068182945251465, "The Data Distribution of the Gaia Satellite is ESAC."]
[5.171773910522461, 5.885061740875244, "The Dish Size of the Chilbolton Site IOT Station is 25 m."]
[6.598217010498047, 2.6879005432128906, "The Components of the SPIDER Robot is Communications antenna and MakerSat."]
[6.092532157897949, 6.420510292053223, "The Wind Direction Blur of the SAR Image Synthetic Aperture Radar Image is 180\u00b0."]
[6.072502136230469, -0.055308807641267776, "The Testing Start Date of the Galileo Second Generation Satellite is 19 July 2021."]
[6.835761547088623, 4.454431533813477, "The Manufacturer of the spaceCam c4000 Video Camera is Theta System Elektronik GmbH."]
[7.675090789794922, 8.49907112121582, "The Spectral Coverage of the AIRS Atmospheric Infrared Sounder is 3.74 - 15.4 \u00b5m for the array grating spectrometer (IR bands)."]
[7.846783638000488, 9.102434158325195, "The Spectral Band Centers of the Instrument Spectrometer is 415,750,900,950,1000 nm (VIS); 1000,1050,1250,1550 nm (NIR)."]
[9.439119338989258, 5.047720432281494, "The Spin Rate of the DSP satellites Satellite is 15 rpm."]
[8.99323844909668, 6.953909397125244, "The Mass of the PAP Plasma Analyzer is 7 kg."]
[4.365781307220459, 2.4791316986083984, "The Type of the TechEdSat-10 Satellite is 6U CubeSat."]
[8.323567390441895, 1.0412914752960205, "The Operation Start Date of the RAIDS Instrument is June 2010."]
[2.0291106700897217, 4.058244705200195, "The Solar Panels of the EURECA Spacecraft is Twin deployable/retractable panels of silicon solar cells."]
[4.011120796203613, 4.53742790222168, "The Security Perimeter of the DCU Data Control Unit is Excludes OBSW."]
[8.974886894226074, 10.655674934387207, "The Spatial Resolution of the LISS-3 Camera is 23.5 m."]
[5.994210720062256, 9.591569900512695, "The Mass of the SGR-ReSI Interface Unit is 1.5 kg."]
[5.118692874908447, 6.971194744110107, "The Center Frequency (GHz) of the Antenna Reflector is 23.8."]
[8.774704933166504, 0.20046505331993103, "The Space Walk Duration of the Skylab Space Station is Three and a half hours."]
[7.608875751495361, 8.287164688110352, "The Objective of the OMPS UV Hyperspectral Imaging Spectrometer is Measure the total amount of ozone in the atmosphere and the ozone concentration variation with altitude."]
[6.9920854568481445, 7.697444915771484, "The Calibrations of the HARP-2 Polarimeter is Frequent lunar and solar."]
[6.454611778259277, 6.271286487579346, "The Operating Frequency of the OSCAT-3 Radar Scatterometer is 13.515 GHz."]
[7.6558966636657715, 4.896277904510498, "The Reaction wheels of the BEESAT-2 Satellite is Yes."]
[7.060711860656738, 9.235906600952148, "The Incidence Angle of the P Mode Observation Mode is 20\u00ba~50\u00ba."]
[10.15222454071045, 4.8722310066223145, "The Propulsion Type of the Eurostar E3000 Satellite Platform is Electric (plasma) propulsion."]
[11.690906524658203, -1.1685206890106201, "The Propellant Mass of the Satellite Satellite is \u2264 80 kg."]
[12.076786041259766, 3.3255534172058105, "The Inclination of the Satellite Spacecraft is 56.2\u00ba."]
[7.84825325012207, 8.946718215942383, "The Wavelength Range (VIS) of the Sentinel-4/UVN Instrument is 400-500 nm."]
[5.2281365394592285, 4.830801486968994, "The Antenna Facilities of the DSN Communication System is Goldstone, Madrid, and Canberra."]
[6.276564121246338, 4.2823967933654785, "The Sample Rate of the QuakeSat Satellite is Unknown."]
[7.039926528930664, 0.45723140239715576, "The Launch Date of the Unicorn-2L, -2M and -2N Satellites is December 1, 2023."]
[11.556412696838379, 6.248558521270752, "The Exposures of the XMM-Newton X-ray Telescope is Long, uninterrupted, detailed."]
[9.95201301574707, 1.509189248085022, "The Ground Outage Period of the INTEGRAL Satellite is 4 to 6 h."]
[9.44942569732666, 10.512391090393066, "The Altitude of the Iris Video Camera Camera is 360-460 km."]
[6.825881481170654, 10.028879165649414, "The Bandwidth of the Band 2 Spectral Band is 433-453 nm."]
[9.151268005371094, 9.266279220581055, "The FOV Azimuth of the SAGE-III Instrument is \u00b1 185\u00ba."]
[4.928083419799805, -3.21186900138855, "The | of the Eduard P. Kontar Author is Eduard P. Kontar."]
[6.6228556632995605, 3.6152570247650146, "The Technology and Resource Legacy of the ZACUBE-1 Satellite is Leveraged for ZACUBE-2."]
[4.05927038192749, 5.653881072998047, "The Downlink Capacity of the Tandem-L Satellite is ~ 8 TB/day."]
[10.034756660461426, 2.8854331970214844, "The Altitude of the Atmospheric Chemistry Experiment (ACE) satellite Satellite is Low."]
[4.785155296325684, 1.7750545740127563, "The Satellite Count of the Dnepr Rocket Rocket is 37."]
[6.716531753540039, 7.043781757354736, "The Main Challenges of the MERLIN Satellite is Implementing a complex LIDAR instrument on a small satellite platform with limited resources."]
[4.668605327606201, 4.309025287628174, "The Data Processing Unit of the SAMPEX Satellite is Common DPU."]
[6.333967685699463, 5.476309776306152, "The Function of the GNSS-RO Instrument Instrument is 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."]
[9.098963737487793, 7.38139009475708, "The Measurement Error of the Temperature Sensor is \u00b13\u00baC (-50 to +400\u00baC), \u00b18\u00baC (+400 to +600\u00baC)."]
[7.115804195404053, 9.013815879821777, "The Function of the MSU-MR Instrument is Global and regional cloud cover mapping, SST (Sea Surface Temperature), and LST (Land Surface Temperature)."]
[1.7031484842300415, 4.752358913421631, "The Total Power Requirement of the EPS Electrical Power Subsystem is Around 679 W."]
[6.2364373207092285, 3.203430652618408, "The Agency of the SVOM Satellite is CNES, CNSA."]
[10.444073677062988, -0.9663520455360413, "The Maximum Weight of the MS-2 Minisatellite is 200 kg."]
[5.838199615478516, 3.337822914123535, "The Architecture of the ICE Satellite Electronics is Modular design with integrated RF and digital design technologies."]
[6.309352874755859, 8.230880737304688, "The Operating Frequencies of the SMMR Microwave Radiometer is  37.0 GHz."]
[6.593545913696289, 0.9233430027961731, "The Flight Experience Presentation Date of the BIRD Onboard Navigation System Navigation System is Dec. 3-7, 2001."]
[2.0588910579681396, 4.047527313232422, "The Power Production with One Wing Failed of the SAWs Solar Array Wings is Unknown."]
[8.280421257019043, 9.607425689697266, "The Number of Bands of the NIR Detector is 80."]
[11.631597518920898, -1.0101215839385986, "The SRP Acceleration of the M1S/M2S Satellite is 138 nm/s2."]
[6.338514804840088, 11.862730026245117, "The Measurement of the Electrostatic Gravity Gradiometer (EGG) Instrument is Gravitational field of the Earth."]
[4.168182373046875, 5.663424015045166, "The Global Capacity of the Telesat Lightspeed Satellite Constellation is 15 terabit/s (Tbit/s)."]
[10.667033195495605, -1.570565938949585, "The Cargo Weight of the Crew Dragon Spacecraft is More than 500 pounds."]
[5.3490495681762695, 3.6854496002197266, "The Type of the On-board Computer Processing Systems Satellite is Powerful complement."]
[8.96888256072998, 0.5419238805770874, "The Test Duration of the Tianzhou 2 Robotic Cargo Spaceship is 47 minutes."]
[7.663082122802734, 8.486534118652344, "The Vertical Resolution Requirement of the OMPS UV Hyperspectral Imaging Spectrometer is Not provided."]
[8.01860523223877, -0.717232346534729, "The Cargo of the CRS-19 SpaceX Dragon Mission is Microscopic organism, rotifers."]
[6.125736236572266, 6.089480400085449, "The Spatial Resolution of the SAR Sensor Subsystem SAR Sensor is 3 m x 3 m."]
[7.185763359069824, 0.5691267848014832, "The Launch Date of the Simon Bolivar Satellite (VeneSat-1) Communication Satellite is October 29, 2008."]
[7.2114996910095215, 4.204007625579834, "The Chinese Optical instruments of the CBERS Satellite is URL: http://dragon2.esa.int/landtraining2008/pdf/D1L3b_Optical_Li.pdf."]
[6.443159580230713, -0.6582623720169067, "The Tracking Stations of the QZS-1/Michibiki Satellite is Chofu, Singapore, Sydney, Maui, and Tahiti."]
[10.44541072845459, 5.903935432434082, "The Purpose of the Microage Experiment is Examine synthetic muscle cells in orbit."]
[8.213951110839844, 5.3518242835998535, "The Purpose of the GEOTAIL Satellite is 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."]
[7.601670265197754, 1.016588807106018, "The Observation Period of the RECCAP-2 Satellite Mission is 2009-2018."]
[10.92738151550293, 4.176840305328369, "The Purpose of the Next-generation telescopes Telescopes is Directly image Earth-size exoplanets."]
[5.418827056884766, 4.194393634796143, "The User Interface of the CMS Constellation Management System is Simple and robust."]
[11.340583801269531, 6.341167449951172, "The Energy Source of the Pulsar Neutron Star is Emission seen by all three telescopes."]
[11.619437217712402, -1.219282627105713, "The Mass of the Sapphire Satellite is 148 kg."]
[9.267487525939941, 8.466931343078613, "The Mirror Type of the SeaWiFS Satellite is Rotating half-angle mirror."]
[9.611823081970215, -0.7097377777099609, "The Development of the RISING-2 Microsatellite is By Tohoku University and Hokkaido University."]
[6.834590435028076, 4.307648658752441, "The References of the CIMR Satellite Mission is Climate change resulting in ocean warming, sea level rise, and sea ice melting has consequences for the global economy, navigation, and security."]
[11.40627384185791, 5.92438268661499, "The Presentation Date of the ASIM Gamma-ray Detector is Jan. 21, 2009."]
[7.818806171417236, 6.919471740722656, "The Unknown of the Ground-based experimental facility Facility is Unknown."]
[8.400228500366211, 8.682256698608398, "The Transmission Profile FWHM of the Lyot-Michelson Filter System Optical Instrument is 76 m\u00c5."]
[8.435709953308105, 0.3849027454853058, "The Demonstration Duration of the BEAM Expandable Habitat is Two years."]
[6.667710304260254, 7.476491451263428, "The Laser Technology of the DIAL Instrument LIDAR is 2.05 \u00b5m."]
[9.400477409362793, 9.225037574768066, "The Aperture Diameter of the Geoton-L1 imager Optical Subsystem is 50 cm."]
[5.85513162612915, 8.594932556152344, "The IFOV/line (pixels/scan line) of the MWHS Microwave Humidity Sounder is 98."]
[3.540571928024292, 4.075654983520508, "The Total mass of assembly of the STRV-1d DHS Data Handling System is 1.2 kg."]
[8.18670654296875, 9.95991325378418, "The PFM Manufacture Status of the MSASI Imager is Started."]
[7.740838050842285, 8.29658031463623, "The Manufacturer of the OMPS UV Hyperspectral Imaging Spectrometer is BATC (Ball Aerospace & Technologies Corp.)."]
[5.466391086578369, 4.412684440612793, "The Usage of the GHOST Software Package is Routinely to support many missions (GRACE, CHAMP, TerraSAR-X, TanDEM-X, PROBA-2)."]
[9.297226905822754, 10.21268081665039, "The Optics Field of View of the Wide-angle camera Camera is 65.8\u00b0."]
[7.74202299118042, 9.161856651306152, "The GSD of the Spectral Band A Spectrometer is 5."]
[9.062867164611816, 7.565959930419922, "The Field of View (FOV) of the Sun Sensor Sensor is 4\u00ba."]
[4.443459510803223, 2.2611541748046875, "The Number of Satellites of the Starlink Satellite Constellation is 835."]
[7.831066131591797, 10.051660537719727, "The MS B1 of the Pushbroom imager Spectral Band is 0.45-0.52 \u00b5m."]
[6.367609977722168, 8.066452026367188, "The Operating Bands of the RCU Radiometer Calibration Unit is K- and Ka-bands."]
[5.237787246704102, 5.936866283416748, "The Deployable Antennas of the Satellite Communication Satellite is Four."]
[10.066333770751953, 2.4135630130767822, "The Ground speed of the KOMPSAT-3A Satellite is 7.02 km/second."]
[6.8704047203063965, 3.1525416374206543, "The Mission Status of the SARAL Satellite is Operational (extended)."]
[6.771613121032715, 2.6617960929870605, "The Document URL of the EUMETSAT Satellite Data Service is http://www.eumetsat.int/website/wcm/idc /idcplg?IdcService=GET_FILE&dDocName=PDF_DMT_112370&."]
[10.53246784210205, 7.458937644958496, "The Material of the Flywheel Satellite Component is Silicon nitride."]
[9.345113754272461, -0.7977975606918335, "The Launch Site of the SOCRATES Microsatellite is TNSC (Tanegashima Space Center), Japan."]
[3.3126566410064697, 4.430722236633301, "The Size of the PCU Power Control Unit is Compact."]
[6.721221923828125, 1.1656935214996338, "The Installation Date of the Cupola Window is Feb. 2010."]
[8.767230033874512, 6.969971179962158, "The Purpose of the PLS Plasma Instrument is Measure plasma and ionized particles around the outer planets and to measure the solar wind\u2019s influence on those planets."]
[9.796894073486328, 9.693293571472168, "The Stowage Date of the ShadowCam Instrument is 12 August 2021."]
[9.591282844543457, 1.2237389087677002, "The Mission Extension of the TIMED Satellite is Fourth Time."]
[9.78022289276123, 7.145339012145996, "The Charge / Discharge Cycles of the Supercapacitor Energy Storage Device is Millions."]
[8.010396003723145, 2.1029562950134277, "The Launch Date of the Himawari-8 Satellite is October 7, 2014."]
[7.431545734405518, 7.425657749176025, "The Data Collection Period of the Ozone Monitoring Instrument (OMI) Instrument is March 25 through April 25 for 2020."]
[12.130839347839355, 2.1717514991760254, "The Sample Collection Date of the OSIRIS-REx Spacecraft is Oct. 20, 2020."]
[7.868258476257324, 2.020219326019287, "The Builder of the ISEE-1 Spacecraft is NASA."]
[8.11052131652832, 4.011691093444824, "The Images Acquired of the Pleiades Satellite is More than 150."]
[7.363215446472168, 6.700789928436279, "The Data of the MODIS Satellite is NDVI anomaly: it contrasts vegetation health from March 29 to April 5, 2016, against the long-term average from 2000\u20132015."]
[10.926332473754883, 3.1065101623535156, "The Length of the Nix Moon is 42 km."]
[3.602008104324341, 6.599023342132568, "The Data Transfer Rate of the XCOM X-ray Communication System is Gigabits per second."]
[9.427868843078613, 5.105679512023926, "The Spin Rate of the Y-Thomson mode Control Mode is 2\u00ba/s."]
[7.016756534576416, 6.042492389678955, "The Spatial Resolution of the Sea Surface Salinity (SSS) Measurement is 5 km."]
[7.74137020111084, 0.6771116256713867, "The Mission Session Date of the OceanSat-2 Satellite is February 08-19, 2010."]
[2.2661359310150146, 4.512717247009277, "The Array Power Peak of the DSX Spacecraft Payload Module Satellite is 790 W."]
[6.26400899887085, 0.8597633242607117, "The Delivery Date of the Argos-3 Onboard Instrumentation is 2002."]
[6.515503883361816, 6.196024417877197, "The Instrument Manufacturer of the OSCAT-3 Radar Scatterometer is ISRO."]
[7.111802101135254, 0.21394875645637512, "The Creation Date of the 3D Map Map is 13 January 2021."]
[7.514642715454102, 7.471002578735352, "The Detection Capability of the OMI Satellite Instrument is Volcano Emissions."]
[5.776393413543701, 1.75007963180542, "The Spacecraft of the Orbital ATK Launch Provider is Cygnus."]
[8.978886604309082, 9.73740005493164, "The Coordinates of the Image Data is 230.77\u00baE/73.95\u00baN."]
[12.010680198669434, 2.256261110305786, "The Travel Time to Asteroid of the OSIRIS-REx Spacecraft is About two years."]
[7.962825298309326, 8.977388381958008, "The IFOV motion (jitter) of the Spectrometer Spectrometer is < 50 \u00b5rad/axis."]
[9.09764575958252, 4.147781848907471, "The Size of the BRITE spacecraft Satellite is 200 mm x 200 mm x 200 mm."]
[3.8110082149505615, 0.296551376581192, "The URL of the GRAIL Mission is http://discovery.nasa.gov/grail.cfml."]
[11.585311889648438, -1.2419788837432861, "The Mass of the GEISAT Precursor Satellite is 17.4 kg."]
[5.980891227722168, 3.2005794048309326, "The Use of the Lemur-2 Satellite is Track maritime, aviation, and weather activity from space."]
[6.468631267547607, 6.24171257019043, "The Operating Frequency of the OSCAT Scatterometer is Ku-band of 13.515 GHz."]
[9.642559051513672, 4.262255668640137, "The Single Shot Accuracies of the TOR Payload is 3-4 cm."]
[5.015857696533203, 5.029847145080566, "The Components of the Ground Station Ground Station is 9.1m S-band antenna, 4.6 m C-band antenna, antenna controllers."]
[6.012035369873047, 2.665658950805664, "The CEO of the SpaceLink Satellite Network is David Bettinger."]
[11.400839805603027, 4.557053565979004, "The Hydrogen Gas Temperature of the Sun's Lower Atmosphere Celestial Body is 10,000\u00baC."]
[11.265275001525879, 6.709107398986816, "The URL of the SEXTANT X-ray Timing and Navigation Technology is http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20150001327.pdf."]
[4.308964252471924, 5.5879034996032715, "The Interface of the S-band transceiver Communication Device is UART link with the RIU, 1553 RIU interface with the OBC."]
[3.2049660682678223, 6.631274700164795, "The RF Power of the Ka-band Channels Communication System is 46 W/channel."]
[6.678590297698975, 0.6720437407493591, "The Launch Date of the EyeSat Smallsat is 2019."]
[12.20479965209961, 5.340635299682617, "The Hot, Diffuse Gas in the Haloes Percentage of the Universe Cosmology is 5 percent."]
[9.389921188354492, 8.641791343688965, "The Coating Material of the Primary Mirror Optical Component is Boron carbide (B4C)."]
[7.213587760925293, 0.656321108341217, "The Installation Date of the SpaceChain's multisignature blockchain payload Blockchain Payload is 2020."]
[11.313416481018066, 6.535743236541748, "The Launch Date of the IXPE Satellite is December 2021."]
[4.895506381988525, 9.171506881713867, "The First Marsquake Detection Date of the Seismic Experiment for Interior Structure (SEIS) Seismometer is April 6, 2019."]
[6.216305255889893, 5.864893436431885, "The Temporal Baseline of the GF-3 SAR Satellite is Nearly 4 months."]
[7.934337139129639, 1.920082449913025, "The Release Date of the HimawariCast Newsletter Document is 8 November 2016."]
[4.658179759979248, 0.24794124066829681, "The Production Capacity of the OneWeb Satellites Satellite Manufacturer is Two satellites a day."]
[10.026643753051758, 1.5595942735671997, "The Orbit Period of the ALMASat-1 Satellite is 103 minutes."]
[8.320266723632812, 9.702603340148926, "The Number of Detectors of the OLI Imaging System is 6500 per multispectral band, 13000 for the panchromatic band."]
[8.366201400756836, 10.592117309570312, "The Data Output of the CCD (Charge-Coupled Device) Imaging Device is 10 bits."]
[9.54670238494873, 7.516899585723877, "The Cooling Temperature of the Radiative Cooler Cooling System is 83 K."]
[3.59468150138855, 6.322175979614258, "The Downlink Data Rate of the Frontier Radio Radio is Up to 2 Mbit/s."]
[6.120291233062744, 6.217207431793213, "The Abbreviation of the HRWS SAR Instrument is High-Resolution Wide-Swath SAR."]
[11.34359359741211, 6.453995704650879, "The Purpose of the Model Scientific Model is Predict whether pulsars detected in gamma-rays could also be expected to appear in X-rays."]
[4.321957588195801, 2.541156530380249, "The ITU Approval of the Starlink Satellite Network is Required."]
[7.907968044281006, 1.8576858043670654, "The Arrival Date in Europe of the ExoMars Lander Platform Lander Platform is March 21, 2019."]
[9.912361145019531, 1.3987704515457153, "The Nadir Orientation Duration of the PSSCT-2 Satellite is 4 hours."]
[10.394477844238281, 4.739157199859619, "The Specific Impulse of the Chemical Propulsion Thrusters Orbit Maintenance is 291 seconds."]
[3.4223151206970215, 6.699672222137451, "The Interface of the CPUT STX S-band Transmitter is 7 dBi S-band patch antenna."]
[10.5457181930542, 6.021681785583496, "The Complexity of the Micro-gravity experiment Experiment is Most complex one so far."]
[8.25363540649414, 3.649115562438965, "The Data Acquisition Plan of the TanDEM-X Satellite is Not provided."]
[8.678217887878418, 1.9486714601516724, "The Vision of the James Webb Space Telescope Space Telescope is Improved."]
[3.912498712539673, 4.435929775238037, "The Original Design Application of the Sabertooth Parallel Processing Unit is Machine-learning."]
[11.630496978759766, -0.9936138987541199, "The Mass of the Neutrinos Subatomic Particles is Nearly massless."]
[7.311076641082764, 1.1647357940673828, "The Mission Start Date of the MMS (Magnetospheric Multiscale) Mission Satellite is 2014."]
[7.580138206481934, 4.054672718048096, "The Measurement Purpose of the CryoSat-2 Satellite is Collect measurements for scientific research."]
[6.13931941986084, 8.019349098205566, "The Number of Channels of the MTVZA-GY Radiometer is 29."]
[13.724870681762695, 1.6101949214935303, "The Announcement Date of the Vega Flight VV17 Rocket is 18 December 2020."]
[7.5965375900268555, 7.93453311920166, "The Accuracy of the CERES Instrument is 0.5%."]
[9.825200080871582, 4.206460952758789, "The Deorbit System of the Spacecraft Satellite is Sail."]
[13.732558250427246, 1.6193878650665283, "The Failure Date of the Vega Flight VV17 Rocket is 17 November 2020."]
[10.682612419128418, -1.5671907663345337, "The Return Cargo Weight of the Cargo Dragon Spacecraft is 5,200 pounds."]
[9.813387870788574, 4.871608257293701, "The Total Firing Time of the Y-axis Bang-Bang Maneuver Satellite Maneuver is 60 seconds."]
[6.717031002044678, 8.489376068115234, "The Ground Sample Distance (GSD) of the MESSR Radiometer is 50 m."]
[11.651355743408203, 5.066138744354248, "The Energy Forms of the Cygnus A jet Black Hole Jet is Kinetic energy, heat or radiation."]
[7.1922197341918945, 0.6218568682670593, "The Launch Date of the SOHO Satellite is December 2, 1995."]
[8.697854042053223, 2.6047768592834473, "The Maximum Range of the ARTEMIS Spacecraft is 1.5 million km."]
[8.349108695983887, 3.9031131267547607, "The Thermal Control of the LARES Satellite is None."]
[8.011734962463379, 1.3498204946517944, "The Image Capture Date of the SOHO Satellite is Jan. 14, 2014."]
[7.916398048400879, 3.694204092025757, "The Structure of the Sentinel-5P Satellite is Hexagonal."]
[5.208131790161133, 2.5413873195648193, "The Development Status of the ABEX CubeSat is In development."]
[7.842377185821533, 3.8411943912506104, "The Visits per Day of the Pl\u00e9iades Neo constellation Satellite Constellation is Doubles the number of visits per day anywhere on Earth."]
[8.773792266845703, 10.426531791687012, "The Detector Resolutions of the FLIR Boson camera Thermal Imaging Camera is 640 x 512 or 320 x 256."]
[7.576408863067627, 1.5558018684387207, "The Development Status Presentation Date of the Spacecraft Fire Experiment (Saffire) Experiment is July 13-17, 2014."]
[7.648324966430664, 3.1312029361724854, "The Structure of the KOMPSAT-6 Satellite is Integrated structure with hexagonal cross section."]
[10.513141632080078, 7.668915748596191, "The Material of the SPEQS Baseplate is Titanium."]
[10.249537467956543, 2.943892240524292, "The Altitude of the Satellite PAZ is 514 km."]
[7.197366714477539, 3.732403039932251, "The Data Throughput of the BIROS Satellite is Unknown."]
[8.765780448913574, 7.0578155517578125, "The Configuration of the NGAVGS Sensor is One box."]
[6.95324182510376, 11.288506507873535, "The Wavelength FWHM of an unresolved line of the Spectrometer Instrument is 0.111 \u00b5m."]
[9.480911254882812, 1.5919725894927979, "The Global Coverage Time for Altimetry Observations of the Sentinel-3B Satellite is After completion of the reference ground track of 27 days."]
[5.934709548950195, 6.2261481285095215, "The SAR Payload Orbital Altitude of the RCM Satellite is 600 km."]
[8.653672218322754, 10.523711204528809, "The Image Processing Rate of the ASAP-Light Camera System is 100 images/s."]
[8.509117126464844, 7.040159702301025, "The Data Product Cadence of the MAG Sensor Sensor is 1 message per 0.874 seconds."]
[8.935720443725586, 7.478085041046143, "The Angle Resolution of the FSS Fine Sun Sensor is Up to 0.03\u00ba."]
[6.080940246582031, 8.189315795898438, "The Frequency of the MWHS-2 Satellite Instrument is 183 GHz."]
[9.642871856689453, 1.2307435274124146, "The Transmission Duration of the Galileo probe Space Probe is 57 minutes."]
[3.5508060455322266, 2.2828896045684814, "The Size of the CP5 Satellite is 1U."]
[8.620462417602539, 6.869151592254639, "The Type of the Space Magnetometer Sensor is Anisotropic magnetoresistive hybrid sensor."]
[6.656296253204346, 4.431302070617676, "The Additional Payloads of the SENSE Satellite is CTECS (Compact Total Electron Content Sensor) and a micro dosimeter."]
[4.8856635093688965, 1.9348894357681274, "The Quantity of the Dove Satellites CubeSats is 88."]
[9.249490737915039, 1.780422568321228, "The BAA Framework Issuance Frequency of the NRO National Reconnaissance Office is Multiple times per year."]
[6.04973840713501, 0.7120562791824341, "The Deployment Date of the QARMAN CubeSat is 2019."]
[9.425296783447266, 4.928274631500244, "The Slew Rate of the ISS Platform Platform is 0.067\u00ba/s."]
[9.909544944763184, 3.9848263263702393, "The Conference Presentation of the NanoSail-D Satellite is April 9-11, 2008."]
[6.495937824249268, -0.009530678391456604, "The Launch Date of the IRNSS-1D Satellite is March 27, 2015."]
[4.627070903778076, 5.844712257385254, "The RF Communications of the Spacecraft Satellite is 0.1 W (VHF beacon)."]
[5.802459239959717, 2.958627462387085, "The Syndicate Members of the Heinrich Hertz Satellite is Tesat-Spacecom GmbH, Audens Telecommunications Consulting, DLR/GSOC, SciSys Deutschland GmbH, HPS, INVENT, Astrium, Inradios GmbH, Dresden, and DLR/IKN."]
[7.298492431640625, 7.449181079864502, "The Measurement Category of the VHRR Instrument is 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."]
[9.368741989135742, 2.6963298320770264, "The Objective of the DART Mission is Demonstrate a kinetic impact on a small asteroid."]
[7.622334003448486, 0.848080039024353, "The Last ?V Maneuver Date of the Satellite Spacecraft is July 8, 2014."]
[6.022961139678955, 2.897519588470459, "The Researchers of the SMART Satellite is Ben-Gurion University (BGU) researchers."]
[7.0735883712768555, 2.3263309001922607, "The URL of the Shuttle Radar Topography Mission Satellite Mission is http://www2.jpl.nasa.gov/srtm/."]
[9.191817283630371, 3.243011236190796, "The Orbit Type of the Satellite Imaging Satellite is Sun-synchronous near-polar circular orbit."]
[5.168167591094971, 6.231039047241211, "The Enhancement of the Navigation Antenna Antenna is More powerful."]
[8.851133346557617, 10.433693885803223, "The Number of Pixels of the Imager Camera is 4008 x 2672."]
[3.7941207885742188, 6.519441604614258, "The Telemetry Ku-band of the RF communications Communication Subsystem is 0.1 W, 500 kbit/s."]
[4.874855995178223, -3.278686046600342, "The | of the John H. Perepezko Individual is Fred A. Best, Douglas P. Adler, Claire Pettersen, Henry E. Revercomb, P. Jonathan Gero, Joseph K. Taylor, Robert O. Knuteson, John H. Perepezko."]
[9.15977954864502, 5.178065299987793, "The  Spacecraft control of the DSX Spacecraft Payload Module Satellite is 3-axis stabilized."]
[7.0073723793029785, 1.5625178813934326, "The Launch Date of the Vigilance Mission (KSF1) Satellite Cluster is End of June."]
[6.008482933044434, 6.524925708770752, "The Polarization of the StriX-\u03b1 SAR Satellite is Single polarized (VV)."]
[7.933119297027588, 7.273786544799805, "The Operational Cadence of the Instrument Satellite Instrument is Rotate 120\u00ba in < 2 minutes to space view."]
[8.358453750610352, 6.224256992340088, "The Test Location of the EMC Testing Test Type is Anechoic chamber either at USSC or SSTL premises."]
[6.565622329711914, 6.5133843421936035, "The Polarization Channels of the SGLI Imager is 2."]
[9.17549991607666, 7.373528480529785, "The Developer of the Temperature Sensor Sensor is High School Students of Geymonat (Tradate, VA, Italy)."]
[3.3196957111358643, 5.3257598876953125, "The Bit Size of the Event Data Structure is 64-bit."]
[1.9509655237197876, 3.815793514251709, "The Provider of the Next generation solar cells / Azur Solar Cells is Azur Space GmbH."]
[3.851954221725464, 6.061957836151123, "The Data Rate of the OGS Optical Ground Station is 80 Mbit/s."]
[9.930214881896973, 6.480850696563721, "The Orbital Position of the Meteosat-11 Geostationary Satellite is 0 \u00ba."]
[6.032952785491943, 6.634189605712891, "The Frequency Bands of the RA/HY-2 Radar Altimeter is Ku-band and C-band."]
[10.438017845153809, 7.593194007873535, "The Material of the Mandrels Manufacturing Component is Aluminum."]
[8.679703712463379, 10.31564712524414, "The Application of the LISS-3 Linear Imaging Self-Scanning Sensor is Land and water resources management."]
[9.541251182556152, 0.5478222370147705, "The Design Life of the S/C Satellite is One year."]
[6.586957931518555, 0.3764672577381134, "The Launch Date of the SMART-1 Satellite is 27 September 2003."]
[5.850944519042969, 8.60244369506836, "The Sensitivity of the MWHS-II Microwave Humidity Sounder is 1.1 K."]
[9.164938926696777, 10.306693077087402, "The Star Magnitude Range of the Fast Cameras Camera is 4 to 8."]
[8.730707168579102, 9.895858764648438, "The Design of the Cameras Imaging System is Monochromatic with optical filters."]
[6.623640060424805, 10.663582801818848, "The Nominal SNR of the Band 1 Spectral Band is 1000."]
[7.812312602996826, 2.216278076171875, "The Publication Year of the Observation of the Earth and Its Environment Book is 2002."]
[5.336162567138672, 2.9413111209869385, "The Principal Investigator of the TROPICS Constellation of CubeSats is William Blackwell of MIT/LL (Massachusetts Institute of Technology'/Lincoln Laboratory)."]
[4.785072326660156, 2.128021717071533, "The Satellite Quantity of the CM1 Satellite is 2."]
[7.2421183586120605, 5.407590389251709, "The Source of Mid-tropospheric CO2 of the AIRS Satellite is Airflow into the mid-troposphere from the near surface."]
[8.787461280822754, 7.187623977661133, "The Sensor Quantity per Spacecraft of the Tri-TIP Instrument is 2."]
[7.3207197189331055, 10.09048080444336, "The Launch Date of the HISUI Hyperspectral Imager is Unknown."]
[7.873131275177002, 6.05444860458374, "The Radiometric Calibration of the Payload Satellite Payload is Continues to be maintained."]
[7.087457656860352, 2.7885663509368896, "The Contact Email of the MEVI\u00b5S Satellite is eoportal@symbios.space."]
[11.7575101852417, 4.482786655426025, "The Age of the Cosmic Microwave Background (CMB) Remnant of the Big Bang is 380,000 years."]
[8.039974212646484, 4.075252056121826, "The Growth Requirement of the Space Moss Moss is Only a small area for growth."]
[6.211938381195068, 0.5241057276725769, "The Launch Time of the GRIFEX 3U CubeSat is 14:22:00 UTC."]
[1.9408671855926514, 4.075690746307373, "The Power Supply of the SI-300 Satellite Bus is Li-ion battery and four deployable solar panels."]
[6.167818546295166, 2.2502567768096924, "The Operator of the TacSat-2 Satellite is US military."]
[6.633599281311035, 3.0015246868133545, "The Components of the Orion spacecraft Spacecraft is Avionic computers, harnesses, propulsion system, 12 engines, 11 parachutes, 16-foot-diameter heat shield, forward bay cover and numerous other systems and components."]
[6.806080341339111, 5.507636547088623, "The Data Usage of the SMAP Satellite is Analyzing this moisture can tell you whether there is enough water for plants to function properly and to achieve an optimal yield."]
[9.27010440826416, 2.232398509979248, "The Autonomous Maneuver Capability of the BIROS Minisatellite is Yes."]
[4.177828311920166, 4.6991729736328125, "The Protocol Version of the DCPS Data Control and Processing System is SSP protocol version 2.1."]
[4.458104133605957, 5.736887454986572, "The Downlink Frequency of the EROS-A Satellite is X-band."]
[8.264585494995117, 3.6422994136810303, "The Performance Prediction of the TanDEM-X Satellite is Not provided."]
[6.734327793121338, 1.752487063407898, "The Conference Session of the PSAT Satellite is Pre-Workshop Session 4: Lessons Learned."]
[6.737692832946777, 7.1757493019104, "The Function of the Kodiak system Lidar is Provide real-time images and distance-ranging information."]
[11.463044166564941, 4.4352874755859375, "The Study Location of the Stardust Grain Particle is University of Arizona."]
[7.324484825134277, 5.6992692947387695, "The Identification Method of the Small- and Meso-scale Ocean Features Oceanic Phenomenon is Solely using sea surface temperature properties."]
[8.72881031036377, 6.915815353393555, "The Error (RMS) of the Magnetometers Actuator is <0.0005 Am 2."]
[6.083578586578369, 6.141270160675049, "The Coverage Area of the Satellite SAR Instrument is Varies."]
[6.305215835571289, 8.25033187866211, "The Dicke Load Measurement of the MWR Noise Injection Radiometer is During the second half of the Dicke cycle."]
[8.36694622039795, 6.656085014343262, "The Launch Date of the NewMag Magnetometer is Aug. 21, 1996."]
[9.179193496704102, 7.85772705078125, "The Interface Temperature Requirement of the LCT Optical Instrument is Lower than 15\u00baC."]
[4.551102161407471, 5.8025736808776855, "The Backscatter Coefficient of the Satellite Satellite is -10 dB to +50 dB."]
[6.08392333984375, 9.586111068725586, "The Total Mass of the LALT Laser Altimeter is 19.1 kg."]
[1.8236382007598877, 4.278764247894287, "The Power Sources of the PSU Power Supply Unit is Solar panels, battery."]
[4.356961727142334, 7.0277791023254395, "The DSB noise temperature of the Millimeterwave receiver Receiver is 1000 K."]
[9.551993370056152, 6.543757915496826, "The Hinge Type of the Closeout Panels Satellite Components is Spring loaded."]
[9.937310218811035, 1.45322585105896, "The Separation Time from Launch Vehicle of the Mey-Lin (C6), Gaspard (C7), and Oc\u00e9ane (C8) Satellites is Around 63 minutes."]
[6.364292144775391, 7.814474105834961, "The In-flight Operation Start of the NIRST Instrument Radiometer is Winter of 2012."]
[9.520441055297852, 0.5600103139877319, "The Lifetime of the HaloSat Satellite is Two and a half years."]
[6.927101135253906, 4.315583229064941, "The Imagers of the HySIS Satellite is Two pushbroom imagers."]
[5.3909478187561035, 4.693985939025879, "The Status of the LCTs Data Relay System is In orbit."]
[9.210002899169922, 7.2839813232421875, "The Pointing Requirement of the FIPEX sensor Sensor is Along the velocity vector to within 10 degrees."]
[8.468839645385742, 9.092982292175293, "The F Number of the HSC Spectrometer Spectrometer is 3.0."]
[7.632940769195557, 1.0014114379882812, "The Liftoff Date of the Sentinel-1B Satellite is 22 April."]
[7.228847980499268, 2.498894453048706, "The Date of the SWOT Hydrology Workshop Workshop is Sept. 15-17, 2008."]
[9.105873107910156, 5.133398532867432, "The Attitude of the Spacecraft Satellite is Spin-stabilized and nominally sun-pointing."]
[4.955972194671631, 1.9307194948196411, "The Number of Sprite satellites of the KickSat Satellite is 104."]
[8.326602935791016, 8.10568904876709, "The Primary Detector of the Spectrometer Instrument is Electrical Substitution Radiometer (ESR)."]
[11.476278305053711, -1.336105227470398, "The Mass of the TEPCE Satellite is 3 kg."]
[6.082978248596191, 5.356136798858643, "The Purpose of the GNC Technology is 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."]
[4.424942493438721, 7.700287818908691, "The Bandwidth of the Channel 2 Sensor is 200 MHz."]
[3.8522040843963623, 5.6828413009643555, "The Data Download Rate of the First DMC generation Satellite is 8 Mbit/s."]
[8.576112747192383, 6.813918590545654, "The Measurement of the MFI Magnetometer is Intensity and direction of magnetic field vector."]
[10.097555160522461, 5.662344455718994, "The Actuation of the FDV Fill & Drain Valve is Opened using its torquing mechanism."]
[8.038728713989258, 1.2262572050094604, "The Image of the Day Date of the NASA Earth Observatory Satellite is 20 May 2022."]
[6.110705375671387, 6.064602851867676, "The Field of Regard of the L-SAR Satellite is 320 km."]
[8.360822677612305, 1.8816661834716797, "The Launch Year of the Voyager 2 Spacecraft is 1977."]
[0.9731148481369019, 4.234517574310303, "The Capacity of the NiH2 Batteries Power Subsystem is 8 Ah."]
[4.578648090362549, 3.42484450340271, "The Control Software of the SATLAB Configuration is RAMSES software."]
[12.140596389770508, 5.383174419403076, "The Expansion of the Universe Cosmology is Speeding up."]
[6.588685512542725, 4.075737476348877, "The Imaging Payload of the NEA Scout CubeSat is Optical."]
[7.887567520141602, 4.418755531311035, "The SWIR Range Ground Resolution of the WorldView-3 Satellite is 3.7 m."]
[10.232613563537598, 5.3247480392456055, "The Maximum Sulphur Dioxide Content of Ship Fuels of the International Shipping Emission Regulations Regulation is 0.5%."]
[7.080520153045654, 0.9504752159118652, "The Launch Date Control of the ORS-6 Satellite Mission is Not have the ability to dictate launch date."]
[11.641678810119629, -1.1382776498794556, "The Fuel Quantity of the IRS-1A Satellite is 80 kg."]
[4.743885517120361, 5.210966110229492, "The Function of the Thales MissionLINKTM Terminal is Provides a reliable connection for voice, satellite internet, cellular data, Land Mobile Radio (LMR) and location-based applications."]
[2.264766216278076, 3.8368701934814453, "The Camera Position of the LightSail Satellite is Mounted to two of the four deployable solar panels."]
[4.341552734375, 6.698291778564453, "The Signal Frequency of the Matrix Switch Signal Routing Equipment is 1.2 GHz or 720 MHz."]
[3.923250198364258, 6.580955505371094, "The Components of the Group Delay Parameter is Clock, code generator, modulator, up-converter, transmitter, satellite antenna."]
[5.125685214996338, 4.6001410484313965, "The Main Control Station of the Rumpin Ground Station is True."]
[10.445300102233887, 7.637092590332031, "The Material of the FSU FC Sensor Unit is Titanium."]
[13.079209327697754, 4.084125518798828, "The Data Archive Size of the Gaia Satellite is 1 PB."]
[7.3100810050964355, 8.480539321899414, "The Sensitivity of the SIM Solar Irradiation Monitor is 0.2 W m-2."]
[11.893038749694824, 3.0887012481689453, "The Inclination of the Swarm-A and Swarm-C Satellite Constellation is 87.35 \u00ba."]
[3.9427812099456787, 4.405162811279297, "The Operating System of the OBC On-Board Computer is VxWorks RTOS."]
[6.938636302947998, 0.740695059299469, "The Launch Dates of the iMESA Technology is MISSE-7(ISS), iMESA 2009-2011."]
[7.333619117736816, 7.352424144744873, "The Components of the SLOSU Instrument Unit is OME (Opto-Mechanical Enclosure), thermal radiators, FEE (Front End Electronics), the cooling system, and DA (Detection Assembly)."]
[6.550326824188232, 6.162869930267334, "The Launch Date of the OSCAT Scatterometer is September 2009."]
[6.469884872436523, 6.290887832641602, "The Spatial Resolution of the OSCAT-3 Radar Scatterometer is 25 km."]
[6.041992664337158, 1.8473330736160278, "The Operation End Year of the SAR-Lupe Satellite System is 2017."]
[9.67067813873291, 8.953612327575684, "The Clear Aperture of Telescope of the DubaiSat-2 Satellite is 40 cm."]
[8.179342269897461, 9.201475143432617, "The Ground Coverage of the Detector Sensor is 79 m."]
[6.0415568351745605, 2.786620855331421, "The Technology Development Funding of the MAST Satellite is NASA Small Business Technology Transfer (STTR) contract."]
[9.23916244506836, 3.2210657596588135, "The Orbit of the SARAL spacecraft Satellite is Sun-synchronous near-circular dawn-dusk orbit."]
[7.144838809967041, 7.154348373413086, "The Unknown of the SOVIM Instrument is Unknown."]
[7.6712188720703125, 0.6141544580459595, "The Mission End Date of the DSCOVR Satellite is Unknown."]
[6.965290546417236, 5.592378616333008, "The Impact of the Argo Ocean Observation System is Provided data for climate projections."]
[7.640263080596924, 0.48476189374923706, "The Period of Performance of the JPSS-3 and -4 Satellite is Through 2026."]
[8.119270324707031, 4.72382116317749, "The Spatial Resolution of the Geodesy Inertial navigation system Satellite is 100-1000 km."]
[12.033466339111328, 3.2440598011016846, "The Orbit Inclination of the 3U CubeSat Satellite is 97.44\u00ba."]
[7.532801628112793, 4.779834270477295, "The SWIR Resolution of the PROBA-V Satellite is 1024 pixels."]
[8.877684593200684, 7.3547797203063965, "The Instrument Suite of the EPI-Hi Particle Measurement Instrument is IMPACT."]
[3.2522637844085693, 4.831638813018799, "The SRAM of the OBC On Board Computer is 2 MB."]
[3.293489933013916, 4.794859886169434, "The Control Handover of the Stamp9G20 microcontroller Microcontroller is Acquires control of the shared flash memory."]
[6.404827117919922, 5.889645099639893, "The Radar Measurements Spatial Resolution of the L2SMAP Soil Moisture Product is About 9 km."]
[9.278996467590332, -0.8438277244567871, "The Launch Vehicle of the SOCRATES Microsatellite is H-IIA."]
[2.436380386352539, 6.346264839172363, "The Latency Requirement of the S-1 NTC Product is Within 20 days."]
[7.324986457824707, 7.2497100830078125, "The Developers of the SoloHI Instrument is 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, D."]
[8.296547889709473, 9.545175552368164, "The Type of Array of the NIR Detector is HgCdTe."]
[7.847520351409912, 6.969536781311035, "The Measurement Cadence of the DSCOVR Satellite is 1 sample per minute."]
[10.301053047180176, -0.8097841143608093, "The Cone Half-Angle of the O/OREOS nanosatellite Satellite is Less than 13o."]
[6.89232063293457, 0.21857212483882904, "The Viasat Partnership Date of the Satellite Vu Company is 28 September, 2022."]
[5.891201019287109, 5.126063346862793, "The Failure Cause of the MRSE Instrument is Arcs of the high-voltage cathode supply at the TWTA connections in the low-pressure environment (vacuum) of the Shuttle orbit."]
[9.008749961853027, 8.691811561584473, "The Detector Temperature of the TIR Subsystem Imaging System is 80 K."]
[5.771599292755127, 2.712782144546509, "The Funding of the GIDAS Project is Co-funded basis."]
[7.492003917694092, 5.679722785949707, "The Experiment of the IRT Saint Exup\u00e9ry Research Institute is Using a form of artificial intelligence called \u2018deep learning\u2019 to recognize patterns such as cloud formations or fires on Earth."]
[6.132002353668213, 1.8802587985992432, "The Launch Contractor of the OCO-2 Spacecraft is ULA (United Launch Services LLC)."]
[8.26216983795166, 8.780071258544922, "The Redshifts of the NISP Spectrograph Instrument is About 30 million emission line galaxies."]
[8.905561447143555, 4.881349563598633, "The Control Algorithm of the EIRSAT-1 Satellite is \u2018Wave based control' algorithm."]
[8.370055198669434, 7.130712509155273, "The Mass of the IOF Plasma Wave Instrumentation is 12 kg."]
[5.250673770904541, 3.1339190006256104, "The Bus Name of the NorSat-1 Satellite is GNB (Generic Nanosatellite Bus)."]
[9.404718399047852, 8.167237281799316, "The Retroreflectors of the Ralph and Norton Satellite Components is Mounted on the exterior surfaces."]
[5.71646785736084, 3.528703451156616, "The Deployment Sequence of the Drag Augmentation Device Satellite Component is 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 d."]
[5.653228282928467, 7.2508158683776855, "The Antenna Size of the KaRIn Instrument is 5 m x 0.25 m."]
[8.86596393585205, 7.2412495613098145, "The Error (RMS) of the Nadir sensor Sensor is <0.2\u00ba."]
[6.9772515296936035, 1.0092459917068481, "The Congress Date of the BEESAT-3 Satellite is Sept. 10-12, 2012."]
[7.440722465515137, 1.3642767667770386, "The Establishment Date of the Sentinel Asia Disaster Risk Management System is May 2005."]
[9.230887413024902, 10.58031940460205, "The Nadir ground resolution (IFOV) of the 16 mm camera Camera is 370 m x 370 m."]
[6.826225280761719, 7.290961265563965, "The Manufacturer of the ATSR-1 Instrument is RAL, UK (British Aerospace as prime contractor); CRPE, France, and CSIRO, Australia."]
[10.4970703125, 6.103976726531982, "The Subject of the Micro-gravity experiment Experiment is Multi-layer heat capillary convection."]
[6.4694318771362305, -0.6256171464920044, "The Implementation Date of the QZSS L1-SAIF Message Generator Device is Jan. 28-30, 2008."]
[9.166815757751465, 8.364633560180664, "The Active Diameter of the L3 Detector Detector is Large enough to intercept even the widest-angle trajectories defined by the L1\u2022L2 coincidence."]
[10.67667007446289, 5.26688814163208, "The Minimum Impulse Bit of the CNAPS Propulsion System is 0.7 mNs."]
[9.57928466796875, 8.697437286376953, "The Field of View of the HPT High Precision Telescope is 1.9 km x 1.4 km."]
[12.100561141967773, 3.2867355346679688, "The Orbit Inclination of the Rocket 3.3 Rocket is 86\u00ba."]
[9.63110065460205, 5.942190170288086, "The Attitude Control Algorithms of the ADCS Attitude Determination and Control Subsystem is Runs."]
[11.621338844299316, 4.342592239379883, "The Spin Axis Inclination of the Zeta Puppis Star is (24 \u00b1 9)\u00ba."]
[4.0837602615356445, 6.358406066894531, "The Modulation of the Payload Imagery Imaging is OQPSK (Offset Quadrature Phase Shift Keying)."]
[3.1902832984924316, 4.933011531829834, "The ROM of the OBC Onboard Data Handling is 16 kB."]
[6.8558669090271, 7.644350528717041, "The Telescope Diameter of the DIAL Instrument LIDAR is 40 cm."]
[11.675145149230957, -1.0429335832595825, "The Maximum Mass of the Payload Satellite Payload is Up to 600 kg."]
[9.30353832244873, 10.146289825439453, "The Direction of the Comedia C328 Camera is Pointing in the direction of the balloon."]
[5.292100429534912, 2.1917836666107178, "The Number of Geographic Sites of the PUTC Program is 69."]
[6.038023948669434, 2.1836700439453125, "The Conceptualized Name of the KhalifaSat Satellite is DubaiSat-3."]
[11.048064231872559, 7.020623683929443, "The Affiliation of the JEM-X X-Ray Monitor is DSRI (Danish Space Research Institute), Copenhagen, Denmark."]
[9.18421459197998, 9.691413879394531, "The Field of View (FOV) of the WISPR Imager is 180\u00ba."]
[9.798351287841797, 7.729539394378662, "The Telescope Energy Range of the ASTRO-H Mission is E ~ 0.3-12 keV."]
[5.778748512268066, 2.937333583831787, "The Manufacturer of the NOAA-20 Satellite is Ball Aerospace."]
[10.849119186401367, 5.72968864440918, "The Diagnostic Technique of the Solar Flare Solar Event is Helioseismic holography."]
[8.40008544921875, 10.420058250427246, "The Focal Length of the 4-band CCD Imager Instrument is 32 mm."]
[8.368911743164062, 0.21693915128707886, "The Time on ISS of the CIMON-1 Prototype is 14 months."]
[6.72959041595459, 2.5635766983032227, "The Launch Center of the BeiDou/Compass satellites Satellite is XSLC (Xichang Satellite Launch Center)."]
[12.077674865722656, 5.33049201965332, "The Existence of the Dark Radiation Hypothetical Radiation is Possible in the early cosmos."]
[9.49544620513916, 7.815051555633545, "The Energy Range of the Electron Spectrometer Instrument is 1 eV to 1400 eV."]
[4.775905132293701, 0.8590589761734009, "The Funding Round Amount of the Satelles PNT Service Provider is $26 million."]
[6.073161602020264, 1.5447263717651367, "The Constellation Concept of the PAZ-TerraSAR Constellation Satellite Constellation is Coordinated Constellation Concept (CCC)."]
[7.655540466308594, 1.4817038774490356, "The Launch Date of the Hera Mission is Unknown."]
[10.023538589477539, 9.953612327575684, "The Pointing Platform Provider of the Iris video camera Camera is RSC Energia of Kaliningrad, Russia."]
[12.02303409576416, 4.47427225112915, "The Study Importance of the Blue Ring Nebula Nebula is Show us what they look like so we can identify more of them."]
[4.711951732635498, 1.7667419910430908, "The Number of Satellites of the Galileo Satellite Constellation is 8."]
[4.977149963378906, 7.6269683837890625, "The Energy of the W-band Band is 0.3 meV."]
[3.1585419178009033, 5.318714618682861, "The Storage Capacity of the SSR Solid State Recorder is 3.1 Tbit @ EOL."]
[6.257706642150879, 5.905646324157715, "The Spotlight High Resolution (HS) Spectral Resolution of the TSX-SAR Satellite is 1m."]
[8.662660598754883, 8.047567367553711, "The Sensor Type of the MuREM Dosimeter is RADFET (Radiation-sensitive Field Effect Transistor) solid-state dosimeters."]
[6.8450727462768555, 3.886334180831909, "The Platform of the Deimos-2 Satellite is SpaceEye-1."]
[5.4390177726745605, 6.388922214508057, "The Antenna Beamwidth of the Satellite Satellite is 1.33\u00ba (Ku-band), 5.25\u00ba (S-band)."]
[5.127173900604248, 2.9010891914367676, "The Flight Software of the SOURCE 3U CubeSat Satellite is Being developed and tested in parallel."]
[7.840203762054443, 0.5919787883758545, "The Launch Date of the Aeolus Satellite is 2018."]
[7.987363815307617, 8.545877456665039, "The Calibration Method of the OVIRS Spectrometer is Using NIST traceable calibrated blackbodies and flood sources."]
[6.287911891937256, 0.5491167902946472, "The Launch Vehicle of the SMART-1 Satellite is Ariane-5G."]
[1.989066243171692, 3.853785276412964, "The Deployable Solar Array Type of the UK-DMC-2 Satellite is Emcore triple-junction InGaP/InGaAs/Ge solar cells."]
[9.492517471313477, 1.6214083433151245, "The SAR Interferometry Image Pair Time Interval of the Sentinel-1A and Sentinel-1B Satellites is 6 days."]
[11.186084747314453, 4.207335472106934, "The Number of Planet Candidates Identified of the Kepler Satellite is 1,235."]
[7.254334926605225, 9.450666427612305, "The In-Flight Calibration of the MSU-E Multispectral Scanner is Not Performed."]
[7.554925918579102, 2.5962772369384766, "The Servicer Capture Mechanism of the ELSA-d Mission is Magnetic."]
[7.918635845184326, 1.6145837306976318, "The URL of the SCARLET Advanced Array Solar Array is http://nmp.nasa.gov/ds1/tech/scarlet.html."]
[3.190661668777466, 5.19738245010376, "The Data Storage of the SSMM Solid State Mass Memory is Unknown."]
[6.749812126159668, 3.905275583267212, "The Operational Modes of the VRSS-1 Satellite is Real-time imaging mode, Quasi real-time imaging mode, Recording mode, Replay mode."]
[5.962101459503174, 6.778468132019043, "The Azimuth Resolution of the Radar Sensor is Approximately 400 m."]
[8.206830978393555, 6.659733295440674, "The Target of the External Calibration Calibration is Sky in an inertial attitude."]
[5.7767157554626465, 1.830970048904419, "The Vehicle of the Orbital ATK Launch Provider is Antares."]
[5.200082778930664, 6.154984951019287, "The Alignment Type of the Helical Antenna Antenna is Self-Aligning."]
[7.48781681060791, 5.997973918914795, "The Spectral Range of the CLARREO Satellite is 5 to 50 \u00b5m."]
[4.75273323059082, 0.8326777219772339, "The Value of the Agreement with ABDAS Imaging Satellite Access is $38 million."]
[6.879458427429199, 1.0414247512817383, "The Presentation Date of the DLR FireBird Constellation Satellite Constellation is May 30-June 3, 2016."]
[11.740941047668457, 7.502255439758301, "The Clock Stability Requirement of the DSAC Demonstration Unit is AD of at most 2.0 x 10-14 at one day."]
[10.052940368652344, -0.8963158130645752, "The Size of the TurkSat-3USat Nanosatellite is 10 cm x 10 cm x 30 cm."]
[6.347245693206787, 2.5443356037139893, "The Mean Sea Level Change Error Budget of the Jason-3 Satellite is 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."]
[6.26760721206665, 3.3205058574676514, "The Collaboration with Other Government Agencies of the NASA Organization is National Oceanic and Atmospheric Administration (NOAA) and the National Reconnaissance Office (NRO)."]
[10.429937362670898, 4.962850093841553, "The Input Power of the HET-X Hall-effect Thruster is 350 - 2500 W."]
[7.1373610496521, 2.525757074356079, "The URL of the NASA Satellite Satellite is http://www.nasa.gov/press-release/nasa-satellite-finds-unreported-sources-of-toxic-air-pollution."]
[4.609139442443848, 5.553740978240967, "The Link Establishment of the LLITED satellites Satellite is Beacon and proper serial number code."]
[11.60848331451416, 2.573256254196167, "The Diameter of the Asteroid 1999JU3 Asteroid is About 900 m."]
[1.3060781955718994, 4.257842063903809, "The Minimum Battery Voltage of the IXV Spacecraft is 30.8 V."]
[9.376703262329102, -0.6221312284469604, "The Sensor Complement/Experiment of the TechnoSat Nanosatellite is Camera, Fluiddynamic Actuator, S-band transmitter HISPICO, Laser Retroreflectors, Solar Generator Impact Detector, Star Tracker STELLA, Reaction Wheel System."]
[11.604903221130371, 6.203012466430664, "The Commissioning Start Date of the XRS instrumentation Instrumentation is End of November 2007."]
[9.050453186035156, 10.534430503845215, "The Pixel Pitch of the PamCam Panoramic Camera is 6.7 \u00b5m."]
[6.6901116371154785, 0.4060888886451721, "The Launch Date of the CBERS-2 Satellite is Oct. 21, 2003."]
[7.5620622634887695, -0.4871698319911957, "The Next Launch Date of the Falcon 9 Rocket is February 5."]
[6.341014385223389, 11.866488456726074, "The Measurement Data Noise of the EGG Gradiometer is Slightly higher-than-expected."]
[5.252943992614746, 2.52150297164917, "The Mission Type of the QBITO CubeSat is EO."]
[6.914143085479736, 0.6074723601341248, "The Launch Date of the SEEDS-2 Satellite is April 28, 2008."]
[5.026219844818115, 4.833561897277832, "The Availability of the Matera ground station Ground Station is For L-band SAR imagery downlinks."]
[7.017392158508301, 5.167681694030762, "The Impact of the Climate Models Computer Models is Helped scientists separate natural changes in the Earth's climate from human influences."]
[9.803559303283691, 4.238119602203369, "The Packaging and Mass Efficiency of the Drag Sail Modules Satellite Component is Superior or competitive to state-of-the-art solar sails."]
[10.062355041503906, 2.438326597213745, "The Ground Target Distance Between Adjacent Passes of the KOMPSAT-5 Satellite is 95 km (at equator)."]
[8.664800643920898, 8.726783752441406, "The Field of View of the UVS Instrument Spectrometer Telescope is 0.071\u00ba x 0.75\u00ba."]
[11.540386199951172, 4.4573893547058105, "The Spin Rate of the Stars Celestial Bodies is Varies."]
[9.533848762512207, 8.119335174560547, "The Scintillator Size of the Gamma-ray Counter Detector is 12 cm x cm."]
[7.602922439575195, 4.545072078704834, "The Pixel Size of the Copernicus Sentinel-1 Satellite is About 30 m."]
[4.229077339172363, 3.7345378398895264, "The Peak Detection Rate of the COM DEV NTS Receiver AIS Receiver is 35 Messages/s."]
[7.660986423492432, 1.4430605173110962, "The Logo Release Date of the Hera Mission is 3 May 2019."]
[13.174962043762207, 4.007840633392334, "The Data Gathering Period of the Gaia Satellite is Full nominal mission plus the first 6 months of the mission extension (66 months in total)."]
[6.730352401733398, 7.754727840423584, "The Interface Temperature of the Power Laser Head Subsystem is 0.5 K."]
[4.3228888511657715, 6.713335990905762, "The Frequency of the Transmitter Communication Device is 5.84 GHz."]
[10.117956161499023, 3.6319963932037354, "The Orbit Eccentricity of the Gravity Gradient Stabilization Attitude Control System is About 0.07."]
[10.032395362854004, 4.0450897216796875, "The Maximum \u0394V of the Spacecraft Satellite is 85 m/s."]
[10.185518264770508, 2.996995687484741, "The Altitude of the Satellite Imaging Satellite is 681-709 km."]
[11.574373245239258, -0.97027987241745, "The Propulsion System Capacity of the ESPA Ring Interface is 344 kg."]
[5.68881893157959, 2.987975835800171, "The Platform Type of the SSTL-300 Satellite is EO Small Satellite."]
[5.968758583068848, 8.489351272583008, "The Vertical Scan Emphasis of the MLS Microwave Limb Sounder is Lower stratosphere and upper troposphere."]
[8.076339721679688, 1.4506187438964844, "The Seasonal Cycle of the Carbon Dioxide Ice Substance is Unfolds over the comet's 6.5 year orbit."]
[6.7658586502075195, 3.3208911418914795, "The Mission Status of the Sentinel-5P Satellite is Pre-operational."]
[7.613014221191406, 3.9543869495391846, "The Storage Capacity of the KazEOSat-2 Satellite is Up to 4000 km."]
[7.534542560577393, 8.177727699279785, "The Altitude Range of the RAIDS Instrument is 100 to 200 km."]
[6.016619682312012, 3.3046352863311768, "The Development Partners of the Telerobotics Space Technology is ESA, DLR."]
[7.298258304595947, 3.519341230392456, "The Bus Type of the SPOT-6 & SPOT-7 Satellite Constellation is AstroBus-L (or AstroSat250)."]
[10.573899269104004, 8.516242027282715, "The EFL of the COR1 Coronagraph1 imager is f/20."]
[7.089548110961914, 2.441084146499634, "The URL of the Microsat Satellite is https://web.archive.org/web/20180125015338/https://www.isro.gov.in/Spacecraft/microsat-0."]
[6.979892730712891, 1.2345455884933472, "The Conference Date of the European Re-entry Program Program is Aug. 19-22, 2013."]
[7.208242416381836, 4.658664703369141, "The Potential Forest Map Frequency of the Tandem-L Satellite is Weekly basis."]
[5.960577487945557, 1.6223747730255127, "The Imaging Modes of the PAZ Satellite is Four."]
[9.45931339263916, 7.792747497558594, "The Energy Range of the EPI-Hi Particle Measurement Instrument is MeV."]
[5.8324785232543945, 2.9468770027160645, "The Operator of the SORCE Satellite is LASP (Laboratory for Atmospheric & Space Physics) of the University of Colorado."]
[1.1205790042877197, 4.374173641204834, "The Battery Cells of the EPS Electric Power Subsystem is 4."]
[12.941008567810059, 4.836329460144043, "The Perigee of the IBEX Spacecraft is 7,000 km."]
[8.807660102844238, 10.412064552307129, "The Spatial Resolution of the LISS III Sensor is 23.5 m."]
[7.836440563201904, 8.320982933044434, "The Sample Exposure Time of the METIS Investigation is More than 200 days."]
[9.328211784362793, -0.3471308648586273, "The Reentry Date of the SMDC-ONE Nanosatellite is January 12, 2011."]
[6.67680025100708, 3.795450210571289, "The LRIT and HRIT Broadcasting Service Start Date of the GK2A satellite Satellite is 2011."]
[6.412328243255615, 6.36608362197876, "The Radar Frequency of the SeaWinds Scatterometer Scatterometer is 13.4 GHz (Ku-band)."]
[4.099030017852783, 5.084787368774414, "The Messaging Capability of the ODTML Data Collection System is Two-way delay-tolerant."]
[8.098885536193848, 3.9930059909820557, "The Total Imaging Area of the Pleiades Satellite is 40,000 km2."]
[9.470133781433105, 10.235267639160156, "The Inclination of the Iris Video Camera Camera is 51.6\u00ba."]
[7.65252161026001, 8.068321228027344, "The Type of the VHRR Instrument is Imaging multi-spectral radiometers (vis/IR)."]
[7.365253448486328, 6.40920877456665, "The Instruments of the Variant Satellite is Split Langmuir probe, Rogovsky coil, Faraday cup."]
[12.018200874328613, 2.2384533882141113, "The Mission Duration of the OSIRIS-REx Spacecraft is Two years."]
[8.473575592041016, 2.556473731994629, "The Orbit Maneuvers of the THEMIS (and ARTEMIS) spacecraft Satellite is 19 maneuvers between Sept. 25 and Oct. 22, 2013."]
[9.551774978637695, 7.735591411590576, "The Mass of the EPE Energetic Particle Experiment is 3.3 kg."]
[9.043132781982422, 6.974687099456787, "The Ion Temperature of the PAP Plasma Analyzer is 500 ~ 10,000 K."]
[10.322230339050293, 1.270336389541626, "The LTAN of the QSat Satellite is 10:00 - 14:00 hours."]
[8.702003479003906, 5.55722713470459, "The Tensional Force Criterion of the Marman Clamp band SRC Separation Mechanism is Design condition change."]
[8.466174125671387, 3.6428561210632324, "The Deployment Over Operating Temperature of the RDA Deployment System is Not provided."]
[8.584973335266113, 9.441006660461426, "The Sensitivity of the NIRSpec MIRI Optical Instrument is 12 nJy (1.1 \u03bcm, \u03c4 i =10,000 s, and \u03bb/\u0394\u03bb= 4)."]
[9.795060157775879, -1.0257169008255005, "The Swath Width of the JL-1-GF03D Microsatellite is 17 km."]
[11.744573593139648, 7.498057842254639, "The Stability of the DSAC Atomic Clock is Orders of magnitude more stable than current spaceborne navigation clocks."]
[6.82757568359375, 2.012079954147339, "The Rainfall Measurement of the IMERG Satellite Data Product is Greater than 160 mm."]
[7.867667198181152, 9.697861671447754, "The Manufacturer of the OHRIS Imaging System is Northrop Grumman."]
[10.29251480102539, 1.3045964241027832, "The LTAN of the Satellite Satellite is 10:00 - 14:00 hours."]
[11.335946083068848, 6.416525840759277, "The X-ray Light of the SS 433 Cosmic Object is Enough to officially call SS 433 a ULX."]
[8.097843170166016, 0.9454163312911987, "The Development Start Date of the Landsat-9 Satellite is Oct. 25, 2016."]
[3.681098461151123, 6.270071506500244, "The Frequency Range of the SGLS Link Communication System is 1755-1850 MHz."]
[5.577700138092041, 5.9847798347473145, "The SAR Antenna of the KOMPSAT-6 Satellite is Fixed SAR antenna on a panel."]
[6.616100788116455, 10.676942825317383, "The Estimated SNR of the Band 8 Spectral Band is 308.10 \u00b1 130.92."]
[7.750959396362305, 7.695064067840576, "The Measurement Concept of the OCO-3 Instrument is OCO-3 will measure the intensity of the sunlight reflected from the presence of CO2 in a column of air."]
[9.473270416259766, 8.831184387207031, "The Optical System of the PAN Camera Imaging Device is Three-mirror off-axis reflective telescope with an off-axis concave hyperboloidal primary mirror and an off-axis concave ellipsoidal tertiary mirror."]
[11.748868942260742, 1.1820608377456665, "The Lunar Penetrating Radar (LPR) of the Chang\u2019e-4 Rover Rover is Payload."]
[8.828971862792969, 5.14434289932251, "The Pointing and Stabilization System of the ExoplanetSat Satellite is Sub-arcsecond."]
[8.603252410888672, 8.77862548828125, "The Mirror Type of the Short Wavelength Band Spectrometer is Off-axis parabolic cylinder."]
[1.7494707107543945, 4.0355610847473145, "The Production Speed Improvement of the Solar Cells Energy Device is More than 20 times faster than the process now commonly used."]
[8.180448532104492, 9.414986610412598, "The IFOV of the InSb Detector is 42.5 \u00b5rad."]
[3.92586612701416, 5.720648288726807, "The Command Uplink Speed of the NorSat-3 Satellite is Up to 32 kbit/s."]
[4.408486843109131, 7.682921886444092, "The Bandwidth of the Channel 4 Sensor is 1000 MHz."]
[2.1092381477355957, 4.113833427429199, "The Deployable Solar Array Power of the UK-DMC-2 Satellite is 65 W at AM0 and 28\u00baC."]
[8.45802116394043, 1.8494677543640137, "The Mission Selection Date of the Euclid Space Telescope is October 2011."]
[8.59704875946045, 1.6349259614944458, "The Second Reaction Wheel Failure Date of the Kepler Space Telescope Space Telescope is Unknown."]
[8.976177215576172, 9.953692436218262, "The Components of the Multispectral Camera Camera is Electrooptical assembly, management and control unit, signal processing unit."]
[10.535881996154785, 2.3194971084594727, "The Inclina. (\u00ba) of the Meteor-1-2 Satellite is 81.2."]
[10.557564735412598, 7.520724296569824, "The Bus Structure Material of the StudSat Picosatellite is High grade aluminum alloy (Al 7075 T6)."]
[8.95311164855957, 7.188256740570068, "The Type of the Horizon sensor Sensor is 2 axis IR pyro array & chopper."]
[8.659435272216797, 6.259284019470215, "The Associated Density Perturbation of the Plasma Drifts Phenomenon is Indicated by the circled arrow."]
[6.534308433532715, 7.572911739349365, "The Sub-contractor of the Laser Transmitter Laser is Quantel."]
[6.7778496742248535, 3.1420867443084717, "The Status of the Vesselsat-1 & -2 Satellite is Still counting."]
[8.210196495056152, 0.5204373002052307, "The Readiness of the Starliner Commercial Crew Vehicle is Ready to go."]
[2.0398077964782715, 3.8977251052856445, "The Type of the Solar Array Power Subsystem is Single panel."]
[7.329422473907471, 0.590294361114502, "The Launch Date of the AFSPC-11 Satellite Mission is 14 April 2018."]
[12.131481170654297, 3.308504104614258, "The Inclination of the COMPASS-2 Satellite is 78.9\u00ba."]
[9.202507972717285, 4.142717361450195, "The Dimensions of the Satellite Communication Satellite is 6m high with a width of 2 m x 2.4 m."]
[10.269587516784668, 6.826658725738525, "The Function of the TCU Thermal Control Unit is Ensure the management of the TCS and of the CSS."]
[9.99406909942627, 1.4818965196609497, "The Time Between Satellites of the A-Train Satellite Constellation is About 15 seconds."]
[7.940423011779785, 6.936420440673828, "The Length of Operation of the Monitoring of HIS Calibration Process is Few minutes."]
[6.833199977874756, 2.7407045364379883, "The Phase of the OPS-SAT Satellite is A-B1."]
[9.187602043151855, 3.2422707080841064, "The Orbit Type of the Satellite Imaging Satellite is Sun-synchronous near-polar orbit."]
[9.546483993530273, 1.0921286344528198, "The Duration of the Mission of the BRITE Satellite is Longer than 2 years."]
[8.175833702087402, 10.48160171508789, "The Data Rate of the TDI Detector Detector is 3.5 Gbit/s total."]
[5.032434940338135, 1.9427335262298584, "The Number of CubeSat P-PODs of the CubeSat - Launch 4 Satellite is 3."]
[8.313097953796387, 3.161151885986328, "The Formation Flying Concept Presentation Date of the TanDEM-X Satellite is Jan. 23-27, 2005."]
[6.0774922370910645, 2.397002696990967, "The Potential Rocket Launch Provider of the Spacety Company is Indian rockets."]
[8.578287124633789, 9.431000709533691, "The Sensitivity of the NIRSpec MIRI Optical Instrument is 10.4 nJy (2.0 \u03bcm, \u03c4 i =10,000 s, and \u03bb/\u0394\u03bb = 4)."]
[7.750376224517822, 8.638333320617676, "The Instantaneous spectral coverage of the Spectrometer Instrument is 1.53 km/s."]
[7.5651960372924805, 5.268959045410156, "The Observation Location of the Orbiting Carbon Observatory-2 (OCO-2) Satellite is Las Vegas."]
[11.891139030456543, 3.354959011077881, "The Inclination of the GOMS-1 Satellite is < 0.5\u00ba."]
[10.22853946685791, 3.234347105026245, "The Height of the Rocket and Payload Launch Vehicle is 196 feet."]
[3.8540773391723633, 5.6359968185424805, "The Data Transmission Rate of the OCM Data Transmission System is 0.3 Mbit/s."]
[4.792847156524658, 2.549365758895874, "The Total Racks of the PM Satellite Component is 23."]
[5.750646591186523, 2.245312452316284, "The Beam Reconfiguration of the Eutelsat Quantum Satellite is Enabled."]
[7.587730884552002, 3.8441619873046875, "The Compression Ratio of the KazEOSat-2 Satellite is 2.5:1."]
[13.098286628723145, 4.073066711425781, "The Magnitude of the Gaia Space Astrometric Mission is G=20."]
[7.004203796386719, 4.304646015167236, "The Measurement Domain of the Kolibri-2000 Satellite is Atmosphere, Gravity and Magnetic Fields."]
[7.7437262535095215, 13.558480262756348, "The Resolution \u0394\u03bb (0.10\u00ba slit) of the SPIM3 Spectrometer is 1.8 nm."]
[7.357943058013916, 9.441702842712402, "The Swath Width of the TopSAR wide Imaging Mode is 220 - 350 km."]
[9.172769546508789, -0.6146276593208313, "The Launch Date to ISS of the Flock 1b Nanosatellites is July 13, 2014."]
[7.511014461517334, 4.487719535827637, "The Multispectral Imagery Collection of the R3 System Satellite is Successful."]
[8.174336433410645, 1.1290394067764282, "The Data Release Date of the EPIC Earth Polychromatic Imaging Camera is July 20, 2016."]
[9.481245040893555, 6.15638542175293, "The Digital Sun Sensor FOV of the AOCS Attitude and Orbit Control System is 37\u00ba."]
[8.198299407958984, 8.600654602050781, "The Specialization of the LET spectrometer Spectrometer is Highly specialised."]
[5.312058925628662, 10.398868560791016, "The Objective of the LI System Lightning Information System is Deliver information on total lightning over the full disk."]
[3.7982711791992188, 4.908868789672852, "The Calibration Target of the MAC Memory System Module is Special ground targets."]
[9.24821949005127, 4.1766252517700195, "The Dimensions of the Spacecraft Satellite is 2.4 m (cylinder height), 3.7 m total height, 3.2 m diameter."]
[6.511413097381592, 2.7220730781555176, "The URL of the Galileo Satellite System is http://m.esa.int/Our_Activities/Navigation/Android_smartphone_app_connects_you_to_Galileo."]
[8.665898323059082, 7.983205318450928, "The Function of the MCP Multi-Channel Plate is Multiplier."]
[5.912469387054443, 3.7376961708068848, "The Operator of the Bartolomeo Platform is Airbus."]
[3.5888869762420654, 6.406990051269531, "The Antenna Switch Loss of the Transceivers Communication Device is 4.5 dB."]
[6.343127727508545, 10.071653366088867, "The Mass of the ROLIS Imaging Camera is 1.4 kg."]
[4.902589797973633, 1.9703353643417358, "The Number of Satellites of the Iridium-4 NEXT Mission Satellite Mission is 10."]
[9.404844284057617, -0.6518566608428955, "The URL of the FedSat Microsatellite is https://web.archive.org/web/20110603203559/http://www.ips.gov.au/IPSHosted/NCRS/wars/wars2000/invited/fraser.pdf."]
[7.8748626708984375, 4.019790172576904, "The Average Daily Acquisition Capability of the COSMO-SkyMed Satellite Constellation is 1800 images."]
[9.872562408447266, 7.729677200317383, "The PI of the CRaTER Cosmic Ray Telescope is Harlan E. Spence."]
[9.645927429199219, 5.947976112365723, "The Secondary Attitude Sensor of the ADCS Attitude Determination and Control System is SCDM."]
[10.372743606567383, 3.3331522941589355, "The Deployment Velocity of the BEESAT-4 CubeSat is 1.5 m/s."]
[7.282790184020996, -0.4952004849910736, "The Next Starlink Launch Date of the SpaceX Company is February 15."]
[8.814980506896973, 6.4794840812683105, "The Composition of the Plasmasphere Plasma Region is Low-energy (low-temperature) plasma."]
[7.716269493103027, 7.63657283782959, "The Observed Phenomena of the ASIM Observation Instrument is Wide variety of phenomena in Earth's upper atmosphere."]
[10.289230346679688, 6.85914421081543, "The Design of the TCS Thermal Control Subsystem is Passive methods with MLI (Multi-Layered Insulation) blankets and thermal coatings."]
[6.6771464347839355, 4.24120569229126, "The Former Name of the Copernicus Program is GMES (Global Monitoring for Environment and Security) program."]
[9.324522972106934, -0.662337601184845, "The Developer of the Venta-1 Nanosatellite is Ventspils University College."]
[11.737432479858398, 1.215210199356079, "The Altitude of the Chang'e-3 lander Lander is 4 m."]
[7.874299049377441, 8.26345443725586, "The Measurement of the IASI Infrared Atmospheric Sounding Interferometer is Infrared radiation emitted from Earth\u2019s surface."]
[9.408209800720215, 1.3137648105621338, "The Timeliness of Data Availability of the Aeolus Satellite is 3 hours."]
[8.020180702209473, 4.49783182144165, "The Imaging Resolutions of the PanGeo Fleet Satellite Fleet is From 20 m to 75 cm/ pixel."]
[8.062568664550781, 9.361412048339844, "The Wavelength Range of the InSb Detector is 2.08 - 2.35 \u00b5m."]
[9.418519020080566, 8.653221130371094, "The Material of the Optical Window Component is Fused Silica."]
[8.263507843017578, 7.868337631225586, "The Cryocooler Development Leads of the MIRI Instrument is JPL, Northrop Grumman, NASA's Goddard Space Flight Center."]
[4.011902332305908, 5.725426197052002, "The Uplink Data Rate of the Spacecraft Satellite is 9.6 or 19.2 kbit/s."]
[9.151121139526367, 10.596687316894531, "The Cadence of the Normal Cameras Camera is 25 seconds."]
[10.361307144165039, 9.586277961730957, "The Launch Date of the IRIS Spacecraft is June 28, 2013."]
[10.153374671936035, 3.0991363525390625, "The Orbit (Orbit control) of the Spacecraft Satellite is \u2264 \u00b1 500 m."]
[6.19445276260376, 0.41452696919441223, "The End of Life Date of the QBITO CubeSat is 16 February 2019."]
[7.005798816680908, 3.486027479171753, "The Mission Status of the DMC-3 Satellite Constellation is Operational (nominal)."]
[3.795198678970337, 4.288512706756592, "The CPU of the C&DH Command & Data Handling is RAD750."]
[9.428756713867188, 2.4944417476654053, "The Number of Propulsive Maneuvers of the ICE (International Cometary Explorer) Spacecraft is 15."]
[10.00357437133789, 2.8441648483276367, "The Targeted Orbit Altitude of the OneWeb satellites Satellites is Roughly 450 km above Earth."]
[6.099154949188232, 0.008362023159861565, "The Launches of the Galileo Satellite Satellite is 11 in 10 years."]
[10.981054306030273, 5.363210678100586, "The Field Strength of the Sunspot Solar Phenomenon is More than 6,000 gauss."]
[8.096833229064941, 8.31283950805664, "The Authors of the Solar-B EUV Imaging Spectrometer Spectrometer is J. L. Culhane, L. K. Harra, G. A. Doschek, J. T. Mariska, T. Watanabe, H. Hara."]
[4.681282997131348, 9.047286033630371, "The Landing Date of the InSight Spacecraft is 26 November."]
[6.735223293304443, 1.7331674098968506, "The Launch Date of the Kleos Patrol Mission (KSF2) Satellite is April 2022."]
[3.9936702251434326, 5.633631706237793, "The Data Stream Speed of the Suomi-NPP Satellite is 15 Mbit/s."]
[7.141721725463867, 2.723051071166992, "The URL of the Sentinel Data Hub Data Hub is https://senthub.esa.int/."]
[7.631757736206055, 1.5025410652160645, "The Status Presentation Date of the SMOS Mission is Nov. 18-20, 2009."]
[9.173552513122559, 3.261909246444702, "The Orbit Type of the Meteor-M2 Satellite is Sun-synchronous circular orbit."]
[6.2727556228637695, 5.183608055114746, "The Function of the Coprocessor Satellite Component is Real-time processing of the raw reflected GNSS data into DDMs."]
[7.090001106262207, 0.7330459356307983, "The Construction Completion Date of the BDS-3 Satellite System is June 2020."]
[6.683537006378174, 7.198728084564209, "The Integration Status of the ALADIN Laser is Second flight model integration was prepared."]
[7.926274299621582, 9.72810173034668, "The Relative Geometric Accuracy of the GCP Extraction Approach Image Processing is 10 m RMSE."]
[7.7456512451171875, 9.41143798828125, "The Wavelength Range of the Visible Channel Imaging Device is 0.4-1.0 \u00b5m."]
[8.283594131469727, 3.091032028198242, "The First Global Coverage Completion Date of the TanDEM-X Satellite is January 2012."]
[5.956602096557617, 0.2747311294078827, "The Flight Name of the Galileo FOC-3 and FOC-4 satellites Satellite is VS-11."]
[10.770686149597168, 3.441554069519043, "The Closest Approach to the Sun of the Parker Solar Probe Spacecraft is Within 4 million miles."]
[6.85028600692749, 5.486995220184326, "The Potential Impact of the SMAP Satellite is Improve the accuracy of the soil moisture characterization in the Air Force systems."]
[8.387649536132812, 7.343870639801025, "The Radiation Hardness of the Space Comb Spectroscopy Setup is Some critical fiber components will be more deeply inspected for radiation hardness."]
[9.23088264465332, 8.388824462890625, "The Detector Separation of the Detector Instrument is Less than 12.06 mm."]
[10.299138069152832, 3.62764573097229, "The Altitude Range of the MEOSAR Search and Rescue System is 19 000 to 24 000 km."]
[6.67319393157959, 1.079563856124878, "The Ground Stations of the Genesis-2 Satellite is Las Vegas, Virginia, Alaska, Hawaii."]
[4.938416004180908, -3.2002904415130615, "The | of the N. Vilmer Author is N. Vilmer."]
[4.089682102203369, 3.1592354774475098, "The Backwards compatibility of the Open5GCore Rel. 4 5G Core Network is Maintaining backwards compatibility with LTE and NB-IoT [IDD and NIDD]."]
[11.543543815612793, 6.29516077041626, "The X-ray Map of the XMM-Newton Satellite is Extensive."]
[8.048717498779297, 7.035837173461914, "The Training Data of the Machine Learning Algorithm Calibration Tool is Images from sounding rocket calibration flights."]
[9.506831169128418, 0.18938712775707245, "The Mission Duration of the O/OREOS nanosatellite Satellite is 6 months."]
[4.3590312004089355, 4.406313896179199, "The Router External Links of the SpaceWire ASIC Application-Specific Integrated Circuit is 4."]
[10.740274429321289, 5.605917453765869, "The Impact of the Solar Flares Solar Phenomenon is Capable of severely disrupting technologies on Earth such as satellite operations, GPS navigation and communication systems."]
[7.4992170333862305, 1.7250438928604126, "The Calibration Plan Presentation of the Microscope Space Mission is Oct. 1-5, 2012."]
[6.537484645843506, 5.015534400939941, "The Instrument of the Copernicus Sentinel-6 Satellite is Advanced Microwave Radiometer."]
[8.842191696166992, 2.2189383506774902, "The Navigation of the New Horizons Spacecraft is State-of-the-art."]
[6.697658061981201, 7.389262676239014, "The Field-of-View of the Scanning LIDAR LIDAR is Ranging between 1\u00b0 x 1\u00b0 and 40\u00b0 x 40\u00b0 degrees maximum."]
[7.143834590911865, 3.265303373336792, "The Recovery Status of the NEOSSat Satellite is Successful."]
[6.996129989624023, 4.217990875244141, "The Measurement Domain of the Sich-2 Satellite is Ocean, Land, Snow & Ice."]
[8.544700622558594, 8.549221992492676, "The Reflector Half Cone Angle of the AMSR-E Instrument is 47.4\u00ba."]
[10.883044242858887, 3.9415442943573, "The Field of View of the Nancy Grace Roman Space Telescope Space Telescope is Nearly 100 times larger than Hubble Space Telescope."]
[4.942076206207275, 2.200712203979492, "The Quantity of the CubeSat Yonsei team Team is 1."]
[8.824668884277344, 6.976169586181641, "The Quantity of the Magnetometers AOCS Sensors is 2."]
[6.750777721405029, 4.452706336975098, "The Data Source of the Climate Change Initiative Program is Copernicus Sentinel-1 mission, Envisat\u2019s ASAR instrument, JAXA\u2019s Advanced Land Observing Satellite (ALOS-1 and ALOS-2)."]
[9.769676208496094, -0.48848965764045715, "The Photometer Resolution of the Nanosatellite Satellite is 26.52 arcsec/pixel."]
[8.771407127380371, 7.375673770904541, "The Measurement of the LYRA Sensor is Sun's energy intensity."]
[10.568928718566895, 8.534406661987305, "The Image Sequence Acquisition Time of the COR1 Coronagraph1 imager is \u2264 8 s."]
[11.728116989135742, 4.6422200202941895, "The Star Formation Rate of the Cluster XDCPJ0044.0-2033 Galaxy Cluster is Almost two thousand solar masses per year."]
[6.256896495819092, 5.972385883331299, "The Spotlight (SL) Image Size of the TSX-SAR Satellite is 10km x 10km."]
[3.873929977416992, 2.325850009918213, "The Form Factor of the Ultra-Compact Radiometer Radiometer is 1U CubeSat."]
[8.556513786315918, 5.579291343688965, "The Payload Weight Capacity of the IPS Pointing System is Up to 7,000 kg."]
[8.29044246673584, 3.0996923446655273, "The Science Phase of the TanDEM-X Satellite is 2014 to mid of 2016."]
[7.2746429443359375, 0.6731851696968079, "The Launch Date of the Spacecraft Satellite is 2019."]
[6.1748552322387695, 1.8777055740356445, "The Launch Site of the OCO-2 Spacecraft is VAFB, CA."]
[7.727268695831299, 2.0386388301849365, "The Project Manager of the Europa Clipper Spacecraft is Jan Chodas."]
[5.735091209411621, 2.268676280975342, "The Launch Provider of the Eutelsat Quantum Satellite is Arianespace."]
[7.76037073135376, 1.0411649942398071, "The Next Phase Decision Date of the Copernicus Satellite Program is Second half of 2021."]
[5.6227898597717285, 6.232813835144043, "The Antenna Diameter of the Galileo Satellite System is 13 m."]
[9.322484970092773, 6.401035308837891, "The Acceleration Tolerance of the Procyon Star Tracker is 1\u00b0/s2."]
[7.245205402374268, 5.590184211730957, "The Effect of the Rain Clouds Weather Phenomenon is Changes ocean's temperature and salinity profiles, affects the circulation of deep water and can even affect global climate events like El Ni\u00f1o."]
[7.297804832458496, 4.586328506469727, "The Imaging System of the NewSat Satellite is Visible and near-infrared spectrum."]
[6.817036151885986, 5.486603260040283, "The Workshop Date of the Soil Moisture Active and Passive Mission (SMAP) Satellite Mission is Nov. 18-20, 2009."]
[8.619640350341797, 5.342843055725098, "The Pointing Accuracy of the Spacecraft Satellite is 360 arcsec."]
[5.559700012207031, 2.855687379837036, "The Platform of the Intelsat 40e Satellite is Maxar's 1300-class."]
[4.293880462646484, 5.111555576324463, "The Redundancy of the Data Handling Unit Subsystem is Half Satellite."]
[7.520725250244141, 8.142691612243652, "The Observed Altitudes of the MIGHTI Instrument is 200-300 km altitude, ~100 km altitude, 100 km altitude region."]
[4.802647590637207, 0.9034494161605835, "The Build, Deployment, and Operations Cost of the RainCube Satellite is Less than $10 million."]
[1.1469695568084717, 4.203880786895752, "The Battery Type of the PCU Power Conditioning Unit is Li-ion."]
[8.051321029663086, 9.731918334960938, "The Operation of the OHRIS Imaging System is Can be operated in parallel with OHIS."]
[9.588939666748047, 8.705086708068848, "The Design of the Limb Imager Telescope is Single off-axis three-mirror reflective telescope."]
[6.974987506866455, 8.0789213180542, "The Global Coverage Time of the MESSR Radiometer is 17 days."]
[11.63908863067627, 6.193077564239502, "The Mission Extension Period of the XMM-Newton X-ray observatory is 1 January 2015 \u2013 31 December 2016."]
[8.95507526397705, 2.7423644065856934, "The Presentation Date of the GCOM-W1 Satellite is June 5-12, 2011."]
[8.423059463500977, 5.689757823944092, "The Number of Off-Source Pointings of the Mode 2 Pointing Mode is 24."]
[9.215070724487305, 1.3063753843307495, "The Beam-Out Events of the IPA Engine is 2 per day (nominal), less than one per week on average."]
[2.0281083583831787, 4.3976945877075195, "The Solar Array Power of the MTM Transfer Module is 13 kW."]
[7.679680347442627, 0.9797968864440918, "The Launch Dates of the Sentinel-6 Satellite is 2020 and 2026."]
[6.109174728393555, 3.086164712905884, "The Prime Contractor of the Jason-CS / Sentinel-6 Satellite Mission is Airbus Defence and Space."]
[9.660440444946289, 5.6151018142700195, "The ADCS System of the DeorbitSail Satellite is First demonstration of the CubeAIM system."]
[6.079501628875732, -0.041947271674871445, "The Testing Start Date of the Galileo Second Generation Hardware Hardware is July 19, 2021."]
[11.599102973937988, -0.9811015129089355, "The Mass of the S/C Structure Satellite Structure is 191.4 kg."]
[8.574844360351562, 1.4242987632751465, "The Age of the Rosetta Spacecraft is Over 12 years."]
[3.87923002243042, 6.166696071624756, "The Data Rate of the Payload Imagery Imaging is 32.72 Mbit/s."]
[5.093717098236084, 6.941720962524414, "The RF Bandwidth (MHz) of the Antenna Reflector is 400."]
[1.9767389297485352, 4.335762023925781, "The Up to 11 kW of the MTM Solar Arrays Power Output is The MTM solar arrays are sized to provide up to 11 kW for operating the electric propulsion system."]
[6.94265079498291, 2.8653013706207275, "The Affiliation of the Scientists General is UK Committee for Antarctic Place-Names."]
[7.25673246383667, 9.942935943603516, "The Data Comparison of the HyperScout\u00ae Satellite is Copernicus data, in-situ ground truth measurements and an airborne campaign."]
[7.335848331451416, 3.5163636207580566, "The Unknown of the ZY-1( 02C) Satellite Satellite is Unknown."]
[7.011129856109619, 5.152976036071777, "The Operational Modes of the GIS Instrument Satellite Instrument is Simultaneous panchromatic and multispectral (pan-sharpened), Panchromatic only, Multispectral only."]
[7.366105556488037, 0.5819862484931946, "The Launch Date of the Solar-B / Hinode Satellite is 23 September 2006."]
[4.915390968322754, 1.7190395593643188, "The Number of MFUU of the GIOVE-A Satellite is 2."]
[7.056695938110352, 9.642546653747559, "The Band 6 of the MSS Instrument Spectral Band is 0.7 - 0.8 \u00b5m."]
[5.439871788024902, 3.8752875328063965, "The Developer of the Deep-space Communications Communications System is UK."]
[9.09718132019043, 10.502031326293945, "The Exposure Time of the Camera System Sensor is 800 ms."]
[11.512600898742676, -1.299707293510437, "The Weight of the Satellite Satellite is 770 kg."]
[9.338386535644531, 7.801164150238037, "The Detector Cooling Temperature of the SWIR Spectrometer Spectrometer is 120 K."]
[9.452593803405762, 5.075916767120361, "The Spin Rate of the SCD-2 Satellite is 32 - 36 rpm."]
[11.657489776611328, 6.1392927169799805, "The Planned Lifetime of the XMM-Newton Satellite is 10 years."]
[7.512103080749512, 1.269619345664978, "The Integration Time of the PROBA-V Satellite is Continuously updated."]
[6.126555919647217, 6.878337860107422, "The Antenna Type of the Altimetry Instrument Instrument is Dual-band C/Ku center-fed antenna."]
[5.968972682952881, 1.6262130737304688, "The Purpose of the PAZ Satellite is 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."]
[7.43773078918457, 10.029481887817383, "The Spectral Bands of the High-Resolution Hyperspectral Imager Imager is 220 bands."]
[8.522943496704102, 10.564074516296387, "The Pixel Size of the Kruiz CCD Detector is 9 \u00b5m x 9 \u00b5m."]
[8.797331809997559, 5.011728286743164, "The Operation of the THEIA Satellite is Attitude Control."]
[5.741908073425293, 2.787919044494629, "The | of the LEOBUS-1000 Small Satellite Platform is A Generic Small Satellite Platform for High Performance LEO Missions - LEOBUS-1000."]
[9.92027473449707, 6.773036956787109, "The Temperature Range of the Juice Spacecraft is -180\u00baC to 250\u00baC."]
[10.415237426757812, 4.627863883972168, "The Delta-Velocity of the Onboard Propulsion System Propulsion System is 17 m/s."]
[9.416146278381348, 9.870382308959961, "The Purpose of the ShadowCam Instrument is Reduce stray light from making its way to the detector."]
[6.174045562744141, 2.085084915161133, "The Destruction Cause of the SEOSat Satellite is Thruster control issue led to loss of trajectory."]
[2.440938949584961, 6.35060453414917, "The Latency Requirement of the S-3 STC Product is Within 1,5 days (36 hr)."]
[8.245169639587402, 6.313492774963379, "The Required Spacecraft Stability of the Push Frame Framer with a fast steering mirror Sensor is Low."]
[8.927972793579102, 6.77509069442749, "The Actuation Method of the Electrodes Position Control is Electrostatic force."]
[8.801019668579102, 4.954373836517334, "The Attitude Navigation Solution of the NEMO-AM Satellite is 0.036\u00b0 (2\u03c3)."]
[11.782282829284668, -1.1419870853424072, "The Launch Mass of the ResourceSat-2A Satellite is 1235 kg."]
[7.399683952331543, 2.4822230339050293, "The URL of the Rosetta Satellite is http://www.esa.int/spaceinimages/Images/2015/08/Rosetta_thermal_louvres."]
[6.432808876037598, 4.774260997772217, "The Instruments of the CASSIOPE Satellite is CER, IRM, NMS, SEI, GAP, RRI, MGF, FAI."]
[6.856447219848633, 1.2125391960144043, "The Meeting Date of the FalconSAT-3 Satellite is Oct. 12-16, 2009."]
[7.644336223602295, 1.5936474800109863, "The Project Date of the Small Explorer (SMEX) Satellite is March 28, 1994."]
[11.480789184570312, 4.235377311706543, "The Orbital Distance of the Planet Candidate Exoplanet is Tens of times the Earth-Sun distance."]
[10.09487533569336, 1.3412482738494873, "The Equator Crossing Time of the SMAP Satellite is 6:00 a.m. and 6:00 p.m. local time."]
[8.125551223754883, 9.198826789855957, "The Spectral Resolution (5-30 keV) of the Detector Instrument is 500 eV FWHM."]
[6.058694839477539, -0.06156730279326439, "The End of Life Date of the Galileo Satellite Navigation System is 22 August 2026."]
[9.24535846710205, 8.124092102050781, "The Set Point Temperature of the OPAL Camera is ~10\u00baC."]
[7.153090953826904, 2.2365310192108154, "The URL of the High Spatio-Temporal Resolution Land Surface Temperature Mission Satellite is https://web.archive.org/web/20220808212453/https://ieeexplore.ieee.org/document/8517433."]
[9.49090576171875, 5.808046817779541, "The Attitude Knowledge of the ACS Attitude Control Subsystem is \u00b10.02\u00ba."]
[7.441437244415283, 8.21596908569336, "The Integration Time of the Instrument Spectrometer is 12 s."]
[9.133655548095703, 3.2070562839508057, "The Orbit of the EarthDaily Constellation Satellite Constellation is Sun-synchronous."]
[10.432527542114258, 7.606563091278076, "The Material of the Pin-Puller Mechanism is 17-4 PH H900 stainless steel."]
[8.949474334716797, 1.9483474493026733, "The Assessment Presentation of the BepiColombo MMO spacecraft Spacecraft is 44th ICES ( International Conference on Environmental Systems), Tucson, Arizona, 13-17 July 2014."]
[8.994997024536133, 9.955720901489258, "The Function of the Video Proximity Electronics Unit Sensor Component is Conversion of the analog signal coming from the focal plane assembly into digital signals."]
[6.582411766052246, -0.07144108414649963, "The Launch Date of the PSLV Satellite is 12 Jan. 2018."]
[1.257698655128479, 4.1803741455078125, "The Battery of the Spacecraft Satellite is 78 AH Li-ion battery."]
[4.570245742797852, 4.051291465759277, "The Components of the Spacecraft Plug-n-Play Avionics (SPA) Standards is Special test bypass interface."]
[10.565284729003906, 7.514974117279053, "The Material of the Bus Structure Satellite is Aluminum (AA2024-T3)."]
[13.097149848937988, 4.060874938964844, "The VO Protocols of the Gaia Satellite is TAP for table, Simple Access Protocol for spectra."]
[7.235116481781006, 5.055073261260986, "The Measurement Precision of the GHGSat's New Satellites Satellite is 1% of background for methane."]
[7.41883659362793, 8.26014232635498, "The Spatial Resolution of the CERES Scanner is 20 km."]
[8.101080894470215, 4.036090850830078, "The Image Resolution of the Pl\u00e9iades Neo constellation Satellite Constellation is 30 cm."]
[10.366877555847168, 9.419578552246094, "The Orbit Type of the IRIS Spacecraft is Sun-synchronous orbit."]
[10.188444137573242, 2.9939310550689697, "The Orbit Altitude of the Tomorrow-R1 and -R2 Satellite is 550 km."]
[9.511475563049316, 0.7668591141700745, "The Lifetime of the Mission Satellite Mission is 3 years."]
[7.263523101806641, 3.473375082015991, "The Unknown of the INDEX Satellite Satellite is Unknown."]
[5.726104736328125, 9.14911937713623, "The Power of the Instrument power Spectrometer is \u2264 25 W."]
[5.846864223480225, 3.8459033966064453, "The Data Routing of the EV-9 Satellite is From Panama to the NOC (Network Operations Center) located at the exactEarth facilities in Cambridge, Ontario."]
[8.798002243041992, 6.7128143310546875, "The Discoveries of the MAP-PACE Plasma Analyzer is 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."]
[8.312942504882812, 10.58915901184082, "The Data Rate of the 4-band CCD Imager Instrument is 2.67 Mbit/s."]
[9.658852577209473, 8.617809295654297, "The Quantity of Mirrors of the LRA Laser Retroreflector Array is 100."]
[3.8385064601898193, 6.6837663650512695, "The Bandwidth of the DRT Data Relay Transponder is \u00b1 100 kHz."]
[7.883543968200684, 4.008854389190674, "The Position of the DSCOVR Satellite is L1."]
[3.880033016204834, 2.3012890815734863, "The CubeSat Size of the BRRM Satellite is 3U."]
[7.779402732849121, 2.290613889694214, "The Rover Task of the ExoMars Mission is Seek out geologically interesting sites to drill below the surface."]
[8.851130485534668, 3.3197600841522217, "The Operation Environment of the SSTI GPS Receiver is Low-Earth orbit."]
[7.954980850219727, 7.195985317230225, "The Calibration Capabilities of the Instrument Calibration System is Spectral behavior, relative and absolute radiometric properties."]
[11.548443794250488, 6.2973151206970215, "The Telescope of the XMM-Newton X-ray Satellite is Large Binocular Telescope (LBT) in Arizona."]
[9.897717475891113, 5.280995845794678, "The RCS Thrusters of the AOCS Attitude and Orbit Control System is 16."]
[10.495939254760742, 2.393871545791626, "The Perigee (km) of the Meteor-3-1 Satellite is 1235."]
[6.951032638549805, 1.2790839672088623, "The Workshop Date of the FASTRAC Satellite is April 21-23, 2010."]
[7.207167625427246, 4.527860641479492, "The Band 2 of the Landsat TM Satellite is Green reflectance, peak of healthy vegetation, plant vigor."]
[10.233896255493164, 8.722776412963867, "The Full Sun FOV of the EUVI Extreme Ultraviolet Imager is \u00b11.7 Rsun."]
[5.471647262573242, 4.898359775543213, "The Developer of the NRD Navigation Radar Detector is Norwegian Defence Research Establishment (FFI) with partners."]
[8.992015838623047, 5.150549411773682, "The Cold Face Offset of the SVOM Attitude Satellite Attitude is 45\u00b0 with respect to the antisolar direction."]
[4.673548221588135, 2.27962064743042, "The Quantity of the Perseus-M1 and M2 6U CubeSats is 2."]
[9.690884590148926, 1.3070409297943115, "The Characterization Duration of the SpinSat Satellite is Within the first four months."]
[8.466073036193848, 3.653367042541504, "The Deployed Stiffness of the RDA Deployment System is Not provided."]
[6.4073357582092285, 8.077805519104004, "The RIN Performance of the ASM Instrument Instrument is -140 dB (Hz)^1/2."]
[6.004138946533203, 2.0005428791046143, "The Launch Vehicle of the TerraSAR-X Satellite is Russian/Ukrainian Dnepr-1."]
[7.258876323699951, 1.6467490196228027, "The Senior Review Date of the TRMM Satellite is 2011."]
[4.934985160827637, -3.19895601272583, "The | of the Jayant Sharma, Grant H. Stokes, Curt von Braun, George Zollinger, Andrew J. Wiseman Authors is Jayant Sharma, Grant H. Stokes, Curt von Braun, George Zollinger, Andrew J. Wiseman."]
[7.795293807983398, 4.052236080169678, "The Imaging Capacity of the Satellite Satellite is 2.5 x 10^6 km^2 / day."]
[7.3247270584106445, 3.7209434509277344, "The Memory Use Capability of the SPOT-4 Satellite is Lost."]
[8.874634742736816, 10.726300239562988, "The Data Rate of the LISS-3 Camera is 52.5 Mbit/s."]
[5.620413303375244, 5.5236592292785645, "The GPS Receiver of the ACS Attitude Control Subsystem is NovAtel OEMV-1."]
[9.316597938537598, 3.245859384536743, "The Orbit Shape of the LRO Satellite is Elliptical."]
[8.1334228515625, 7.250552177429199, "The Digitization Accuracy of the Experiment Unknown is \u00b1 0.14 nT."]
[9.452532768249512, 5.5454840660095215, "The Operational Mode of the AOCS Attitude Control System is Stellar yaw-steering."]
[9.483419418334961, 1.7703843116760254, "The Near-Global Coverage of the Satellite Orbit is Every three days."]
[5.901345252990723, 2.955811023712158, "The Manufacturer of the LunIR Satellite is Lockheed Martin."]
[6.864224910736084, 4.4620490074157715, "The Hyperspectral Instruments of the 90-satellite constellation Satellite Constellation is Yes."]
[5.205516338348389, 5.542965412139893, "The Frequency Band of the MEOSAR satellite constellations Satellite Constellations is 406 MHz."]
[9.338733673095703, 6.399582386016846, "The Acquisition Mode Duration of the Star Tracker Attitude Determination System is 2-3 seconds."]
[6.973382949829102, 0.049248140305280685, "The End of Life Date of the GeoEye-1 Satellite is September 2023."]
[2.8946173191070557, 5.305222511291504, "The Mass of the OBIS Onboard Information System is 20 kg."]
[8.890436172485352, 10.53690242767334, "The Frame Rate of the Camera Imaging Device is 500 frames/s."]
[7.158753395080566, 3.2958946228027344, "The Operation Status of the WIND Satellite is Nominally."]
[8.073002815246582, 2.264651298522949, "The Goal of the Artemis Program Space Exploration Program is Land the first woman and next man on the Moon by 2024."]
[8.133859634399414, 10.03409481048584, "The Minimum Lower Band Edge of the MS1 (NIR1) Imager is 765 nm."]
[8.242966651916504, 3.0040948390960693, "The Science Mission Start of the TanDEM-X and TerraSAR-X Satellites is September/October 2014."]
[11.630406379699707, 0.8942134976387024, "The Orbiter Weight of the Chang\u2019e-5 Lunar Lander is Nearly 2,000 kg."]
[8.288044929504395, 8.819734573364258, "The Spectral Line of the Deployable Membrane Telescope Telescope is Hydrogen-alpha spectral line of 656.46 nm."]
[6.143249034881592, 0.43214988708496094, "The End of Life Date of the Buccaneer CubeSat is 18 November 2022."]
[7.781944274902344, 9.951810836791992, "The Detector Element Spacing of the VNIR FPA Focal Plane Array is 12 \u00b5m."]
[8.029078483581543, 4.146631240844727, "The Goal Image Resolution of the Satellite Constellation Satellite Constellation is 1 meter."]
[12.066329956054688, 3.2966322898864746, "The Orbit Precession of the TRUTHS Satellite is 90 degrees."]
[9.460948944091797, 0.5747095942497253, "The Lifetime of the PM Satellite Component is More than 10 years."]
[3.5790791511535645, 6.635817527770996, "The Digital Recorder Dump Rate of the X-band Communication Band is 15.36 Mbit/s."]
[9.781110763549805, 8.682336807250977, "The Telescope of the Tyvak-0130 Satellite is One with a wide field of view."]
[7.834990978240967, 2.2661404609680176, "The Author of the Observation of the Earth and Its Environment Documentation is Herbert J. Kramer."]
[9.175922393798828, 9.10959243774414, "The Angular resolution (2 px) of the FSI dual EUV 174 \u00c5 and 304 \u00c5 alternatively Passband center is 9 arcsec."]
[8.514891624450684, 9.343480110168457, "The Microshutter Arrays of the NIRSpec Spectroscopy Instrument is More than 200 spectra."]
[9.319092750549316, 5.74400520324707, "The Performance of the DFACS System is Excellent."]
[7.935415267944336, 3.282562255859375, "The Research Paper of the Picard Satellite is Advances in Space Research, Vol. 24, No 2, July 1999, pp. 205-214."]
[9.166953086853027, 8.295978546142578, "The L1 Detectors Purpose of the HIT Sensor is Sensitive to electrons."]
[7.205690860748291, 1.5800682306289673, "The Finding Date of the Cluster Satellite is 2017."]
[8.902649879455566, 5.656083583831787, "The Accelerometer of the Satellite Spacecraft is Femto-g accurate electrostatic differential accelerometer."]
[9.271247863769531, -0.5957670211791992, "The Target Market of the ANGELS Nanosatellite is Small satellite market for in orbit operational missions."]
[9.847708702087402, 1.7510957717895508, "The Exposure Time of the SPARCS Satellite is \u224810 min."]
[10.197378158569336, 3.0092382431030273, "The Altitude of the CanX-6/NTS Satellite is 630 km."]
[8.051304817199707, -0.7218599915504456, "The Purpose of the SpaceX Crew Dragon Spacecraft is Transporting astronauts to and from the International Space Station."]
[9.364901542663574, 8.151031494140625, "The Detector Active Area of the RAMIS Radiation Detector is 0.5 cm2."]
[7.755308151245117, 3.8863542079925537, "The Rates of Ice Thinning of the Austfonna Ice Cap is Exceeded 25\u2009m/yr."]
[7.7838263511657715, 2.4619569778442383, "The Launch Year of the NovaSAR-1 Satellite is 2018."]
[12.051663398742676, 4.476000785827637, "The Formation of the Blue Ring Nebula Nebula is Product of two stars merging into one."]
[9.318940162658691, 6.554590702056885, "The Cooler of the Astro-APS Star Tracker is Peltier cooler."]
[6.870243072509766, 6.212971210479736, "The Wind Speed Range of the SCAT Wind Measurement System is 2 m/s - 24 m/s."]
[9.505621910095215, 0.8376946449279785, "The Service Duration of the ZY-3 Satellite is Eight years."]
[7.069974422454834, 3.3213610649108887, "The Mission Status of the TEMPO Satellite is Commissioning."]
[8.219889640808105, 7.244518756866455, "The Components of the VEFI Instrument is DC and AC electric fields instrumentation, burst memory, onboard signal processing, filter bank, magnetometer sensor, lightning detector, fixed-bias Langmuir probe."]
[5.145801067352295, 5.46101713180542, "The Manufacturer of the GATR-TRAC ground station antenna Antenna is GATR Technologies."]
[4.726301193237305, 2.052788496017456, "The Quantity of the Flock-4v Satellite is 4."]
[7.408971786499023, 4.041058540344238, "The Imagery Use of the SPOT 6/7 Satellite is Improved efficiency of US agriculture."]
[7.29327392578125, 0.1468837857246399, "The Launch Date of the HJ-1 Satellite is 06 Sep 2008."]
[7.613740921020508, 1.5815231800079346, "The Data Collection Dates of the SMAP satellite Satellite is May 27\u201331, 2015."]
[8.991023063659668, 7.139796257019043, "The Measurement Parameters of the SWOOPS Instrument is Density, speed and direction of the solar wind in three dimensions."]
[9.096144676208496, 9.06860637664795, "The Output Signal of the THD Horizon Detector is Analog signal."]
[9.66576099395752, 2.8923838138580322, "The Orbit of the CAPSTONE 12U CubeSat is Near rectilinear halo orbit."]
[9.733853340148926, 5.363768100738525, "The Function of the CDRA Orbital Replacement Unit is Maintains the carbon dioxide partial pressure at under 5.3mm Hg for up to nine crew members."]
[3.6953537464141846, 4.7737507820129395, "The Purpose of the Texas Instruments MSP-430 Microcontroller is Count clock cycles over the entire lifetime of the mission."]
[7.649722099304199, 7.047922134399414, "The | Investigation Opportunities for Future Users of the MUSES Facility is MUSES facility enables investigation opportunities for future users."]
[6.478121280670166, 3.1088035106658936, "The Payloads of the DarkCarb Small Satellite is MWIR."]
[4.569629669189453, 7.126606464385986, "The Frequency of the  Submillimeterwave receiver receiver is 562 GHz."]
[10.383138656616211, 4.3818511962890625, "The Altitude Maintenance Duration of the Electric Thruster Thruster is One year."]
[7.582416534423828, 2.274961471557617, "The URL of the Remote Sensing Activities Activity is http://www.oosa.unvienna.org/pdf/pres/stsc2012/tech-24E.pdf."]
[9.076953887939453, 9.708181381225586, "The Monitoring Frequency of the OSIRIS Narrow Angle and Wide Angle Cameras Imaging System is Weekly."]
[5.878749370574951, 4.2891950607299805, "The Data Handling of the Iridium NEXT Satellite is Near real-time transport of mission data and sensor telemetry."]
[9.070280075073242, 1.2696048021316528, "The Apogee Drift Period of the Van Allen Probes Satellite is About 2 years."]
[6.203214168548584, 3.001209259033203, "The Project Team of the MiRaTA Satellite is Blackwell, Cahoy, Rebecca Bishop."]
[6.534192085266113, 0.6140404939651489, "The Decommission Date of the RADARSAT-1 Satellite is 29 March 2013."]
[3.70093035697937, 4.755460262298584, "The Setup of I/O Ports of the dsPIC33F microcontroller Microcontroller is Unknown."]
[9.370429992675781, 8.493983268737793, "The Manufacturer of the TESIS Telescope-spectrometer is LPI (Lebedev Physical Institute)."]
[6.580835342407227, 8.035760879516602, "The Function of the MiniRad Microwave Radiometer is Measure temperature at different levels of the atmosphere."]
[13.070945739746094, 4.081465244293213, "The Image Object Density of the Gaia Satellite is 750,000 objects/deg2."]
[6.92056941986084, 1.0949851274490356, "The Presentation Date of the Quasi-Zenith Satellite System Satellite System is July 5-12, 2009."]
[8.554652214050293, 4.179226875305176, "The Fuel Consumption of the Attitude Control System Satellite System is None."]
[4.446407318115234, 5.473715782165527, "The AOCS Guidance List of the TTTC Satellite System is Included in each data take."]
[4.782190799713135, 1.0006831884384155, "The Development Cost Reduction of the Software System is Large."]
[8.339882850646973, 10.229779243469238, "The Width of the Spectral Block Focal Plane Component is 100 pixels."]
[6.4213175773620605, 5.4961018562316895, "The Function of the GNSS-RO GNSS- Radio Occultation Instrument is Provide (with high vertical resolution) all-weather atmospheric and ionospheric soundings by tracking GNSS satellites."]
[5.6954731941223145, 6.363863945007324, "The Stripmap Scene Size of the SAR Antenna Antenna is 60 km x 8 km."]
[6.814439296722412, 10.05967903137207, "The Bandwidth of the Band 8 Spectral Band is 845-885 nm."]
[6.347992897033691, 10.049878120422363, "The Total Mass of the Model 1000 Camera System Imaging System is <100 kg."]
[7.979470252990723, 7.014739990234375, "The Authors of the Multichannel Autocalibration Process is 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."]
[9.043675422668457, 10.213507652282715, "The Objective of the CMOS Camera Camera is Take occasional snapshot imagery of Earth and to use the camera for onboard event verification."]
[7.62452507019043, 7.173533916473389, "The Internal Calibration of the Mini-RF Instrument is 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."]
[8.415867805480957, 3.2395412921905518, "The Formation Flight Mode of the TanDEM-X Satellite is Close formation."]
[2.2098119258880615, 1.7312300205230713, "The CCSDS ID of the GSAT-0204 Satellite is 264."]
[4.913112163543701, 6.071829795837402, "The Timing Pulse Frequency of the SAMPEX Satellite is 1 Hz."]
[5.776937007904053, 3.682713270187378, "The Led by of the In-situ component Component is EEA (European Environmental Agency)."]
[7.134025573730469, 7.126051425933838, "The Unknown of the SCIAMACHY Instrument is Unknown."]
[6.974077224731445, 2.5001230239868164, "The URL of the AstroSat Satellite is http://www.isro.gov.in/Spacecraft/astrosat."]
[9.036293983459473, 6.562480449676514, "The Accuracy of the Rate gyro Sensor is 0.02\u00ba/s."]
[4.0882954597473145, 4.395420551300049, "The Components of the CDMS Command and Data Management Subsystem is SCP (Spacecraft Process Controller), SCC (Serial Communication Card), DAC (Data Acquisition Card), HSF (High Speed Formatter)."]
[9.883492469787598, 7.088724613189697, "The Cut-out Depth of the Heater Thermal Control Device is 0.4 mm."]
[7.623861312866211, 6.371059417724609, "The Test Type of the Konnect satellite Satellite is Vibration."]
[7.796907901763916, 10.139400482177734, "The MS B2 of the Pushbroom imager Spectral Band is 0.53-060 \u00b5m."]
[5.290487289428711, 2.476116895675659, "The Mission of the ArgoMoon CubeSat is Deep-space."]
[4.893204212188721, 2.11651611328125, "The Total Number of Names of the InSight Satellite is 2,429,807."]
[5.693648815155029, 9.192662239074707, "The Power of the MAG Instrument is 0.2 W."]
[8.537778854370117, 6.84484338760376, "The Type of the Vector Magnetometer Instrument is CSC (Compact Spherical Coil) triaxial fluxgate magnetometer."]
[5.071631908416748, 1.0974801778793335, "The Backlog Value of the Terran R Launch Vehicle is More than $1.2 billion."]
[10.596433639526367, 7.490829944610596, "The Detection Area of the Solar X-ray monitor Detector is 0.75 mm2."]
[7.3557209968566895, 3.588656425476074, "The Ground Segment of the SPOT-6 & SPOT-7 Satellite Constellation is CGS (control ground segment) and EGS (exploitation ground segment)."]
[8.248677253723145, 3.0607588291168213, "The First Image Transmission Date of the TanDEM-X Satellite is June 25, 2010."]
[4.293244361877441, 6.407606601715088, "The Downlink Frequency of the RF Communications System is X-band."]
[8.182344436645508, 8.59028148651123, "The Calibration Views of the CIRiS Infrared Imaging System is 1) deep space 2) an on-board source at a selectable and controlled temperature and 3) an on-board source at the instrument temperature."]
[7.259328365325928, 6.9934611320495605, "The Image Credit of the VIIRS Imaging Radiometer is NASA Earth Observatory image by Lauren Dauphin, using VIIRS data from NASA EOSDIS LANCE, GIBS/Worldview, and the Joint Polar Satellite System (JPSS)."]
[7.854238986968994, 8.714498519897461, "The Minimum Value of the Spectral Angle Measurement is Achieved when the red panel is prominent on the satellite."]
[3.9756274223327637, 6.247256755828857, "The Modulation Format of the Flight Modem Modem is DPSK (Differential Phase Shift Keying)."]
[6.673579692840576, 6.242905139923096, "The Image Types of the SGLI Satellite Instrument is True color composite, Near-ultraviolet, Degree of polarization."]
[4.784347057342529, 1.79224693775177, "The Number of Satellites in Orbit of the Satellogic Satellite Company is 60+."]
[9.396060943603516, 9.085967063903809, "The Size of the Instrument Telescope is 107 cm diameter x 360 cm in length."]
[9.901326179504395, 8.039417266845703, "The Depth of the HXT-S Detector Modules is 223 mm."]
[8.372000694274902, 6.326168537139893, "The Measurement of the Conducted EMC Test Test is Conducted emissions."]
[6.487938404083252, 1.3336772918701172, "The Tester of the ISIM Compartment is Randy Kimble."]
[12.0969820022583, 3.303028106689453, "The Inclination of the NEMO-AM Satellite is 97.64\u00ba."]
[3.2954697608947754, 5.292837619781494, "The On-board data storage of the Second generation spacecraft UK-DMC-2 and Deimos-1 Satellite is HSDR (High Speed Data Recorder) capable of storing up to 8 GByte worth of data."]
[9.824761390686035, 2.683504343032837, "The Planned Quantity of the Kinetic Impact/Crater Generation Maneuver is One."]
[7.9365057945251465, 8.520506858825684, "The Number of Wavelength Bands of the OCO-2 Spectrometer is 3."]
[4.692996501922607, 1.7648978233337402, "The Number of Satellites of the Eurostar E3000 Satellite Platform is 7."]
[3.926288366317749, 6.500919342041016, "The Group Delay of the Receiver Communication System is \u2264 13 \u00b5s."]
[4.857305526733398, 6.014599323272705, "The Signal Power of the Clementine Satellite is 6 W."]
[9.247061729431152, 4.83477783203125, "The Solar b-angles of the SPARCS Satellite is Up to 40\u00b0."]
[6.658938884735107, 2.2072346210479736, "The Number of Satellites of the GPM (Global Precipitation Measurement) Mission Satellite Constellation is 12."]
[6.314598560333252, 8.239217758178711, "The 23.8 GHz Channel Function of the JMR Microwave Radiometer is Primary water vapor sensor."]
[4.274313449859619, 2.5151913166046143, "The Preorder Count of the Starlink Satellite Internet Service is Over 750,000."]
[9.033039093017578, 8.643136024475098, "The Design of the Optical Benches Optomechanical System is Truss-type."]
[8.567748069763184, 6.893040657043457, "The Data Transmission of the Magnetometer Instrument is Real-time."]
[5.020111560821533, 3.6991653442382812, "The Modules of the Spacecraft Satellite is Service module (bus) and payload module."]
[7.481625556945801, 9.095773696899414, "The Swath Width of the Swath width Spectrometer is 50 km."]
[4.626343727111816, 6.213379383087158, "The X-band Frequency of the MSX Satellite is 8475 MHz."]
[9.88471508026123, -0.9290758967399597, "The Structure of the TurkSat-3USat Nanosatellite is 3U CubeSat."]
[11.806133270263672, 4.840269088745117, "The Energy Release of the Ophiuchus Galaxy Cluster Galaxy Cluster is Factor of five more than the previous record holder."]
[6.972692489624023, 1.4230520725250244, "The Symposium Date of the Small Satellites Satellite is May 4-7, 2009."]
[9.982633590698242, -0.7103068232536316, "The Dimensions of the Picard microsatellite Satellite is 90 cm x 80 cm x 110 cm."]
[10.962576866149902, 3.3598568439483643, "The Transit Time to Jupiter of the Juno spacecraft Spacecraft is About three years."]
[12.063738822937012, 3.2997210025787354, "The Orbit Inclination of the CartoSat-2D Satellite is 97.44\u00ba."]
[10.199387550354004, 3.060115098953247, "The Baseline Altitude of the SPARCS Satellite is 550 km."]
[7.017385959625244, 7.154713153839111, "The Design Improvements of the SRC Instrument is New HK telemetry, backup timer."]
[2.378352165222168, 5.589766025543213, "The Power of the GaN-based Power Transistors Transistors is 15W and 80W."]
[6.9113993644714355, 5.880771160125732, "The Deployment Priority of the Argo Floats Oceanographic Instrument is World ocean as their highest priority."]
[6.196606159210205, 3.6591744422912598, "The COSMIAC Role of the SORTIE Satellite is Build the satellite and collect the data from it."]
[7.654901027679443, 1.0462688207626343, "The Launch Date of the Sentinel-1D Satellite is First half of 2024."]
[9.029261589050293, 5.424820899963379, "The Architecture of the Attitude Control System Satellite System is FPGA Based."]
[7.507249355316162, 8.146069526672363, "The FSR of the Radiometry Sensor is 240 Wm -2  sr -1."]
[7.60508394241333, 7.700758934020996, "The Function of the HemoCue Blood Cell Counting Device is Provide quick and accurate counts of total and differentiated white blood cells."]
[7.397749423980713, 0.4504469335079193, "The Deployment Date from ISS of the Light-1 Satellite is February 3, 2022."]
[5.575417518615723, 1.407128930091858, "The Landing Location of the Falcon 9's first stage Rocket Stage is \"Just Read the Instructions\" droneship, which was stationed in the Pacific Ocean."]
[9.526564598083496, 5.496887683868408, "The Stabilization of the AOCS Attitude and Orbit Control Subsystem is 3-axis."]
[4.8589887619018555, 5.228153228759766, "The Communication Ability of the Propulsion System Satellite Component is With the satellite to get instructions and to send telemetry data."]
[9.1157865524292, 4.2070112228393555, "The 2.0 m (L) x 2.1 m (W) x 1.9 m (D) of the Spacecraft Bus Size is Bus size - 2.0 m (L) x 2.1 m (W) x 1.9 m (D)."]
[7.948451995849609, 4.512173175811768, "The Spatial Resolution of the Ice sheets Ice vertical movements Satellite is 100-1000 km."]
[10.436224937438965, -1.125518560409546, "The Mass of the CINEMA-3 Nanosatellite is 4 kg."]
[6.0938639640808105, 1.9706377983093262, "The Launch Vehicle of the Gravity Probe A Satellite is Scout-D."]
[9.170740127563477, 9.081133842468262, "The FOV of the HRI dual EUV 174 \u00c5 and 335 \u00c5 alternatively Passband center is 1000 arcsec x 1000 arcsec."]
[3.584657907485962, 6.5999345779418945, "The Max Data of the S-band Transmitter Transmitter is 2 MB/day."]
[9.511090278625488, 1.668853998184204, "The Programming Loop Operation of the Helios-2 Satellite is Daily."]
[6.614538669586182, 10.673728942871094, "The Noise Performance of the Visible Spectral Band Spectral Band is SNR=6.5 (albedo=2.5%)."]
[7.50731086730957, 1.4535393714904785, "The Expected Result Publication Date of the MICROSCOPE Satellite is End of 2019."]
[7.468705177307129, 2.2708473205566406, "The URL of the Foton-M3 Mission Mission is http://esamultimedia.esa.int/docs/foton/FOTON-M3_brochure.pdf."]
[9.624390602111816, 5.9575090408325195, "The Modes of Operation of the ADCS Attitude Determination and Control Subsystem is Magnetic control, 3-axis control."]
[10.559456825256348, 7.539791584014893, "The Coating of the Aluminum Spheres Satellite is Space-rated flat white paint (AZ-93 white paint)."]
[7.48099422454834, 0.037038907408714294, "The Launch Date of the SAOCOM-1A Satellite is October 2018."]
[7.625342845916748, 1.0258052349090576, "The Solar Corona Observation Date of the PROBA-2 Satellite is March 16, 2015."]
[8.607348442077637, 2.3308305740356445, "The Flyby Imaging of the Parker Solar Probe Satellite is Bonus data."]
[4.132903099060059, 6.526177883148193, "The Downlink Frequency of the CMC Transceiver Communication Device is 430-440 MHz."]
[9.996829986572266, 1.330282211303711, "The Parachute Deployment Time of the MarCO-B Satellite is 11:51 am."]
[5.816640377044678, 3.217417001724243, "The Structure Integration and Builder of the Biomass Satellite is Airbus in the UK."]
[9.7003755569458, 7.6003618240356445, "The Electron Isotropy Boundaries Energy Range of the ELFIN Satellite is 0.5-5 MeV."]
[10.033411026000977, 3.026747226715088, "The Altitude of the WV-1 Satellite is 496 km."]
[6.974342346191406, 1.1376742124557495, "The Launch Date of the Resourcesat-2A Satellite is Unknown."]
[9.4647798538208, 9.019584655761719, "The Aperture of the Optical Parabolic Mirror or Telescope Optical Instrument is ~1 m."]
[7.969099521636963, 4.667555332183838, "The Spatial Resolution of the Maps Data is 0.5\u00b0 to 2\u00b0."]
[11.843631744384766, -1.1206979751586914, "The Launch Mass of the Spacecraft Satellite is ~310 kg."]
[9.095157623291016, 9.123674392700195, "The DOI of the Spaceborne Frequency Comb Metrology Metrology System is 10.1364/optica.3.001380."]
[8.24334716796875, 7.434110164642334, "The Purpose of the SEM Space Environment Monitor is Monitor the space environment."]
[4.4044270515441895, 4.455487251281738, "The Usage of the IU Guidance and Sequencing Unit is Only during launch and the initial phases of operation."]
[10.539111137390137, 7.560450077056885, "The Material of the Decks Satellite Component is Aluminum honeycomb sandwich bonded between Gr/E skins."]
[6.030141830444336, 3.1169862747192383, "The Participants of the SRTM Shuttle mission is NASA, DoD/NGA, DLR, ASI."]
[6.7661004066467285, 1.2445939779281616, "The Mission Presentation Date of the FalconSat-7 Satellite is Oct. 1-5, 2012."]
[9.53350830078125, 5.584805011749268, "The Components of the AOCS Attitude and Orbit Control Subsystem is Four reaction wheels, a dual redundant AIM (AOCS Interface Module), dual redundant gyros, dual redundant ST (Star Trackers) and four sun sensors."]
[9.412806510925293, 0.9023584127426147, "The Mission Duration of the SciSat/ACE spacecraft Satellite is 10 years."]
[7.121848106384277, 2.379085063934326, "The URL of the SARah-1 Earth Observation Satellite is https://www.airbus.com/en/newsroom/press-releases/2022-06-airbus-built-earth-observation-satellite-sarah-1-ready-for-launch."]
[7.942418098449707, 8.899279594421387, "The GSD of the CIRiS Instrument is 0.166 km."]
[7.8712663650512695, 2.004316568374634, "The URL of the SP-402 A New Sun Book is http://history.nasa.gov/SP-402/ch4.htm."]
[6.449178218841553, 8.202452659606934, "The Sensitivity of the MWR Dicke Radiometer is 0.5 K."]
[9.95059585571289, 1.5294106006622314, "The Orbital Period of the Landsat-9 Satellite is 99 minutes."]
[8.453224182128906, 2.1903235912323, "The Mission of the Voyager Spacecraft is Outer heliosphere research."]
[8.959919929504395, 0.8868545293807983, "The Campaign Duration of the CryoSat-2 Satellite is Up to four months."]
[5.591653823852539, 1.4104007482528687, "The Landing Location of the Falcon 9 Rocket is \"Just Read the Instructions\" droneship, which was stationed in the Pacific Ocean."]
[4.110416889190674, 5.673657417297363, "The UHF Downlinks of the UoSAT-12 Satellite is 3."]
[9.230969429016113, 2.6323354244232178, "The Authors of the Double Asteroid Redirection Test (DART) Mission is 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."]
[6.830190181732178, 7.099409580230713, "The Purpose of the CATS Lidar Instrument is Measure clouds and aerosols."]
[7.03641414642334, 1.629092812538147, "The Collision Avoidance Date of the Swarm Satellite Constellation is 14 July 2022."]
[7.362175464630127, 6.7711896896362305, "The Planned Operation Date of the METimage Instrument is 2021."]
[11.717290878295898, 5.084273338317871, "The Brightness of the Sw J1644+57 Supermassive Black Hole is Exceptionally bright for a few weeks."]
[4.2149505615234375, 2.4141037464141846, "The Size of the Cesium Satellite 1 Satellite is Six-unit CubeSat."]
[7.276042461395264, 8.084144592285156, "The Relation to Single-Detector Integration Time of the Integration Time Detector Array is m times longer, where m is the number of stages in a row."]
[11.444863319396973, 6.5820722579956055, "The Number of Unique X-ray Sources of the 3XMM Catalogue X-ray Source Catalogue is 372 728."]
[5.136232852935791, 4.573267459869385, "The Contract Release of the JPSS Common Ground System Ground System is C18-10."]
[8.418205261230469, 3.0898661613464355, "The Formation Time of the TanDEM-X and TerraSAR-X Satellites is ~ 3 seconds."]
[9.402993202209473, 1.3565952777862549, "The Shift Length of the On-call Operations Operations is 12 hours."]
[7.030788898468018, 6.593520641326904, "The Measurement of the TROPOMI Instrument is Trace gases, aerosol and cloud properties."]
[5.520660877227783, 0.4020870327949524, "The 2021 Acres Burned of the U.S. Drought Monitor Report is 124,000 acres."]
[4.755469799041748, 2.447787046432495, "The Intersatellite Link of the CM1 and CM2 6U CubeSats is In LEO."]
[2.1706650257110596, 3.7971715927124023, "The Solar Panels of the LF spacecraft Spacecraft is Four."]
[8.427523612976074, 5.5204854011535645, "The Particle Contamination Level of the VSSC Satellite is Maximum of 300 ppm."]
[10.903084754943848, 2.7864058017730713, "The Date of the Tohoku-Kanto earthquake Earthquake is March 11, 2011."]
[6.212414741516113, 2.263423204421997, "The Prime Contractor of the G\u00f6kt\u00fcrk-1 Satellite is Telespazio of Italy."]
[6.874209403991699, 3.8268086910247803, "The URL of the DEIMOS-2 Satellite is http://www.elecnor.es/en/press/press/elecnor-deimos-inaugurates-its-puertollano-integration-and-satellite-operation-centre-and-presents-its-deimos-2-satellit."]
[8.627054214477539, 0.18266378343105316, "The Maximum Crew Duration of the OWS Space Station is 84 days."]
[8.368494033813477, 7.462207317352295, "The Type of the EDI Instrument is Electron Drift Instrument."]
[7.8364667892456055, 9.848930358886719, "The Spectral range of the MERSI Medium Resolution Spectral Imager is 0.41-12.5 \u00b5m."]
[6.599641799926758, 0.40472668409347534, "The Image Release Date of the SMART-1 Satellite is Oct. 5, 2015."]
[6.611067771911621, 10.681160926818848, "The Estimated SNR of the Band 3 Spectral Band is 745.12 \u00b1 92.15."]
[5.040955543518066, 3.18454647064209, "The Onboard System of the CAPSTONE 12U CubeSat is Communications system."]
[7.859975337982178, 8.891366004943848, "The Spectral Responsivity of the SPIRIT-III Interferometer-Spectrometer is 2.5 to 28.0 \u00b5m."]
[10.848763465881348, 5.62800931930542, "The Date of Event of the Solar Flare Solar Event is September 6, 2017."]
[8.521082878112793, 2.2573401927948, "The Published Article Date of the Eugene Parker Astrophysicist is 1958."]
[8.933771133422852, 2.4311628341674805, "The Purpose of the Herschel Telescope is Map the star formation in clusters by measuring the far-infrared emission from the particles of dust."]
[7.2108988761901855, 1.6970943212509155, "The Publication Date of the Shuttle Radar Topography Mission Satellite Mission is 1998."]
[9.1878080368042, -0.6188749670982361, "The Launch Date of the HORYU-2 Nanosatellite is May 17, 2012."]
[10.587602615356445, 7.545180320739746, "The Material of the LAGEOS Satellite is Aluminium sphere with a brass core."]
[10.902430534362793, 6.840404510498047, "The Attitude Determination Accuracy of the X-ray Telescope Telescope is 0.5\u00ba."]
[8.006401062011719, 4.617875099182129, "The Linear Resolution of the Satellite Imaging Satellite is 34 m x 24 m."]
[4.917549133300781, 4.551877498626709, "The Developers of the Level 2 products Data Products is KNMI, SRON, DLR and BIRA."]
[5.954578399658203, 1.8892229795455933, "The Launch Vehicle of the CHOMPTT Satellite is Rocket Lab USA Electron."]
[11.754058837890625, -1.1067264080047607, "The Total Mass of the DSP satellites Satellite is 330 kg at launch."]
[8.001802444458008, 7.7332658767700195, "The Orthorectification Requirement of the EROS-A PIC Instrument is Required."]
[7.8852152824401855, 0.5649612545967102, "The Launch Date of the Aeolus Satellite is August 2018."]
[8.18159008026123, 10.32967472076416, "The Spectral Band of the Band Cameras Camera is 336.2 nm."]
[5.20229959487915, 6.01190185546875, "The Designs of the Antenna Satellite Component is Omnidirectional, high gain and arrays."]
[7.725193977355957, 3.002415418624878, "The Data Reception and Distribution Agreement Date of the CartoSat-1 Satellite is January 14, 2008."]
[10.429173469543457, 4.79625129699707, "The Tank Type of the ACE propulsion system Propulsion System is Blow-down hydrazine tanks."]
[6.614787578582764, 4.269908428192139, "The Data Uses of the RADARSAT-1 Satellite is Disaster management, interferometry, agriculture, cartography, hydrology, forestry, oceanography, ice studies and coastal monitoring."]
[7.354640007019043, 1.0842411518096924, "The Evaluation Date of the CrIMSS OPS-EDR Product Data Product is 02/24/2012."]
[9.064128875732422, 5.206740379333496, "The Attitude Control System Stability of the CFESat Satellite is Up to 60% of the orbit."]
[10.665167808532715, -1.5640008449554443, "The Cargo Weight of the Dragon CRS-14 Spacecraft is More than 2630 kg."]
[4.001015663146973, 4.391728401184082, "The Flash ROM of the OBC On-Board Computer is Updated applications."]
[5.90662145614624, 7.5737128257751465, "The On-Orbit Performance of the ATMS Instrument is All performance parameters are within expected values."]
[9.688400268554688, 3.834165573120117, "The Drag Sail Deployment Date of the CanX-7 Satellite is May 4, 2017."]
[5.676270961761475, 6.934754371643066, "The Definition of the dBZ Unit is Z is the equivalent radar reflectivity that gives a mean power equal to the standard deviation after integration and noise subtraction."]
[7.177873611450195, 0.3227059841156006, "The Launch Date of the Vigil Spacecraft is Mid-2020's."]
[3.695953845977783, 6.289280891418457, "The Data Rate of the Communication links Communication subsystem is 3 single channel RCV, 2 synthesized RCV 2 synthesized transmitters."]
[10.922345161437988, 4.187199592590332, "The Clarity of the EPIC Data Exoplanet Imaging Data is Exceptionally clear view of Earth, largely unfettered by light from other sources."]
[5.903946399688721, 6.7331929206848145, "The Predicted Target Error of the LRR Radar is Below 6 mm."]
[8.244568824768066, 8.745898246765137, "The Tuning Positions Separation of the Lyot-Michelson Filter System Optical Instrument is 69 m\u00c5."]
[9.043344497680664, 10.017312049865723, "The Function of the Camera Sensor Imaging System is Anti-blooming and electronic integration control."]
[9.2582368850708, 5.239794731140137, "The Rotation Speed of the Antenna Subsystem Satellite Component is 5.6 rpm."]
[9.322466850280762, 6.428238868713379, "The Manufacturer of the Star Trackers Attitude Sensing is CAL Corp, Canada."]
[8.575135231018066, 9.281121253967285, "The Color of the Electronics Mainboard Electronic Component is Green."]
[5.636416912078857, 3.4045445919036865, "The Components of the European Service Module Spacecraft Module is Built and integrated in Italy and Germany, with smaller components delivered from several European nations, including the solar arrays from the Netherlands."]
[10.980109214782715, 2.8543853759765625, "The Size of the Lake Atat\u00fcrk Dam Reservoir is 817 km2."]
[13.803162574768066, 0.7695835828781128, "The Orbital Slot of the GSAT-0203 Satellite is B08."]
[5.049561500549316, 4.655052661895752, "The Data Downlink of the GNOMES Instrument is Via commercial ground station networks."]
[7.069077014923096, 7.190913200378418, "The Deployment of the MUPUS-PEN Instrument is Will be deployed."]
[5.66294527053833, 2.5036940574645996, "The Funding of the QARMAN CubeSat is European Space Agency."]
[5.066336154937744, 7.503785610198975, "The Signal Delay of the Analog-1 Experiment is More than 0.8 seconds."]
[4.6267313957214355, 0.2418295294046402, "The Number of Satellites Launched of the OneWeb Satellite Constellation is 36."]
[7.612736225128174, 3.98915696144104, "The Observation Data of the CryoSat-2 Satellite is Arctic sea-ice thickness measurements."]
[9.278661727905273, 1.7729606628417969, "The Planning Cycle of the TDP Operations Satellite Operations is Weekly incremental cycle."]
[6.725568771362305, 4.311183452606201, "The Operator of the Copernicus Programme Earth Observation Program is European Commission."]
[7.46122407913208, 3.1510417461395264, "The Instruments of the GEO-KOMPSAT-2B Satellite is Geostationary Environment Monitoring Spectrometer (GEMS) and the Advanced Geostationary Ocean Colour Imager-II (GOCI-II)."]
[10.310758590698242, 2.895050048828125, "The Perigee of the FASat-Alfa Satellite is 651 km."]
[5.412066459655762, 10.4044189453125, "The Spatial Resolution of the LIS Lightning Image Sensor is 4km."]
[6.459619045257568, 2.3002469539642334, "The URL of the TSU Telescience Support Unit is http://www.prismasatellites.se/?id=8202."]
[8.083513259887695, 1.4805784225463867, "The Discovery Date of the Kepler-1649c Exoplanet is April 15, 2020."]
[11.7236967086792, 4.544010639190674, "The Contamination Distance of the Sun and Galactic Glint Optical Phenomenon is Up to 1000 km from the coastlines."]
[11.768033027648926, 4.886813640594482, "The Mass of the MAXI J1820+070 Black Hole is About eight times that of the Sun."]
[12.030945777893066, 2.261143922805786, "The Sampling Mechanism Duration of the OSIRIS-REx Spacecraft is Approximately five seconds."]
[11.183809280395508, 6.459066390991211, "The URL of the NICER Neutron star Interior Composition Explorer is https://smd-prod.s3.amazonaws.com/science-red/s3fs-public/atoms/files/nicer-factsheet-final.pdf."]
[6.774953842163086, 1.1860785484313965, "The Restructure Date of the NPOESS Satellite Program is February 2010."]
[9.29292106628418, 10.265657424926758, "The Average Cabin Temperature of the Metric Camera Camera is 22\u00ba C."]
[3.640702486038208, 6.396028995513916, "The Uplink Data Rate of the RF Communication System Communication System is 1.2 kbit/s."]
[8.487821578979492, 7.711548328399658, "The Components of the LENA Instrument is Collimator, conversion unit, extraction lens, dispersive energy analyzer, time-of-flight mass analyzer with position-sensitive particle detection."]
[8.76711654663086, 10.656271934509277, "The Time Resolution of the CCD Image Sensor is 2.6 seconds."]
[6.110672473907471, 6.832764148712158, "The Type of the Tranet Tracking System is Two-frequency Doppler."]
[3.838543176651001, 6.482022285461426, "The FEC Coding Scheme of the Transmitter Communication Device is 5/6 TCM."]
[5.775886535644531, 2.851426124572754, "The Purpose of the Bigelow Aerospace BEAM Inflatable Module is Provide operational experience with inflatable modules in a crewed environment."]
[7.58052396774292, 1.1418946981430054, "The Operation Date of the Analog-1 Experiment is Late 2019."]
[7.865785598754883, 9.557854652404785, "The Spectral Resolution of the Instrument Spectral Imager is 0.625 cm -1."]
[3.224998712539673, 5.248457908630371, "The Ring Memory (RM) of the Groza Instrument is Fixed size sufficient to record a few events."]
[9.403026580810547, 9.735557556152344, "The Focal Length of the VSSC Camera is 1.75 m."]
[7.8368449211120605, 7.922730445861816, "The Information Provided of the \u00b5SCIA Monitoring Instrument is Total column amount."]
[4.4447922706604, 4.55565071105957, "The Functions of the ICU Instrument Control Unit is 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."]
[9.584181785583496, 2.3004353046417236, "The FY22 Budget of the CloudSat Satellite is Unknown."]
[7.619473934173584, 8.808481216430664, "The Resolution of the Nadir Sensor Wide-Field Telescope Sensor is 0.42 nm."]
[10.092029571533203, 1.5743921995162964, "The Orbital period of the Satellite LEO (Low Earth Orbit) is 98.8 minutes."]
[11.460664749145508, 4.156739234924316, "The Planet Sizes of the TRAPPIST-1 Star System is Very close to the size of Earth."]
[7.854133605957031, 0.18259619176387787, "The Launch Date of the NASA Space Station Cargo Resupply Mission is April 18, 2017."]
[5.778219223022461, 2.25009822845459, "The Scientific Objective of the QUESS satellite Satellite is Provide insight into the strangest phenomenon in quantum physics \u2014 quantum entanglement."]
[6.13317346572876, 5.191455841064453, "The Radar Type of the Biomass satellite Satellite is Fully polarimetric P-band synthetic aperture radar."]
[11.372328758239746, 1.3808187246322632, "The Mode of the Yutu-2 Lunar Rover is \"Napping\" mode."]
[8.020033836364746, -0.10904794186353683, "The URL of the Docking Module Space Station Module is https://blogs.nasa.gov/spacestation/2021/11/26/russias-new-docking-module-arrives-at-station/."]
[8.620716094970703, 6.92750358581543, "The Accuracy of the MAG Magnetometer is \u22641 nT."]
[2.2125582695007324, 1.7333993911743164, "The International ID of the SpriteSat Satellite is 2009-002C 33494."]
[10.734277725219727, 6.820317268371582, "The URL of the Solar X-ray Imager Imager is http://goes.gsfc.nasa.gov/text/databook/section06.pdf."]
[11.808415412902832, -1.1440846920013428, "The Spacecraft Mass at Launch of the QuickBird-2 Satellite is 931 kg."]
[3.9270858764648438, 2.29543137550354, "The Size of the Standard 3U CubeSat Satellite is 100 x 100 x 340.5 mm."]
[4.310336589813232, 4.487998008728027, "The Software of the TriTel CPU Central Processing Unit is CAN communication protocol."]
[10.369182586669922, 8.081965446472168, "The Design of the EPIC CCD Cameras is Capture both low- and high-energy X-rays."]
[3.4149158000946045, 5.257589340209961, "The Data Storage of the EPICHyper Constellation Satellite Constellation is At least 4 GB on platform and 128 GB on payload."]
[8.153855323791504, 8.664067268371582, "The Total of the IASI-NG Instrument Optical Path Difference (OPD) is About 8 cm."]
[4.986574649810791, 7.505697727203369, "The Data Packet Loss Rate of the Analog-1 Experiment is 1%."]
[8.335068702697754, 0.6202909350395203, "The Health Status of the Hitomi Satellite is Not Confirmed."]
[5.792922496795654, 3.4649875164031982, "The Objectives of the COTS 2/3 Mission is Complete Licenses and Certifications, Rocket Launch and Spacecraft Inserted into Orbit, On-Orbit Operations, De-orbit Burn & Separation, Controlled Entry, Descent, and Landing, Recovery."]
[6.590388774871826, 0.6302735805511475, "The Program Date of the Meteosat Third Generation (MTG) Satellite is Oct. 1-5, 2012."]
[4.052213191986084, 6.4985504150390625, "The Type of the RF communication subsystem Communication is Non-coherent, half-duplex, 20K00F1D."]
[8.590230941772461, 8.503471374511719, "The Detector Type of the Observation Instrument Telescope/Spectrograph is 2D MCP (solar blind), Csl photocathode, cross-delay-line (XDL) readout, full array size 4096 spectral x 4096 spatial x 256 PHD."]
[5.041389465332031, 2.064840793609619, "The Awarded Funding of the OPS-SAT CubeSat is 12."]
[7.151146411895752, 2.115471601486206, "The Mission Requirements Document of the Next Generation Gravity Mission Satellite is URL:\u00a0https://www.asi.it/wp-content/uploads/2021/03/MAGIC_NGGM_MCDO_MRD_v1_0-signed2.pdf."]
[3.14487361907959, 5.1842241287231445, "The Memory Card Capacity of the DSU Data Storage Unit is 1 Tbit at EOL."]
[9.40499496459961, 7.092530727386475, "The Initial Plenum Pressure of the T3\u00b5PS Pressure Sensor is 1 bar."]
[5.433722496032715, 5.598178386688232, "The Maximum Signals Tracked of the BlackJack GPS Instrument is 48."]
[10.871575355529785, 5.12039041519165, "The Impact on Thrust of the Solar Activity Natural Phenomenon is Isolated peaks of IPA thrust."]
[8.233355522155762, 10.172100067138672, "The Pixel Pitch (MS) of the Pushbroom imager Detectors is 48 \u00b5m x 48 \u00b5m."]
[8.518680572509766, 8.508930206298828, "The Earth Incidence Angle of the AMSR-E Instrument is 55.0\u00ba."]
[7.529389381408691, 8.845213890075684, "The Performance Area of the Nadir Profile Spectrometer Spectrometer is 250 km x 250 km."]
[5.3646368980407715, 4.666391849517822, "The Management of the EDRS Data Relay Satellite System is Managed through a dedicated segment."]
[9.178342819213867, 9.987683296203613, "The Field of View of the WFI Wide Field Imager is ~40\u00ba."]
[3.8989241123199463, 2.304377555847168, "The Size of the SPACE HAUC CubeSat is 3U."]
[7.948680877685547, 10.000621795654297, "The Resolution of the HRMX Imaging System is 2 m."]
[9.931468963623047, 2.435178518295288, "The Predicted Pmp at BOL of the KOMPSAT-6 Satellite is 2,874 W."]
[11.480783462524414, 6.400294303894043, "The Sensitivity of the XMM-Newton X-ray Telescope is Incredibly sensitive to signals."]
[5.679844856262207, 2.4015471935272217, "The New Debt Issued of the Maxar Technologies Company is $150 million."]
[9.547317504882812, 7.280721187591553, "The Low Temperature Limit of the Batteries Power System is -10\u00b0C."]
[7.348911762237549, 3.5730233192443848, "The Communication System of the SPOT-6 & SPOT-7 Satellite Constellation is AstroTerra system."]
[4.205470085144043, 5.531072616577148, "The Link Loss Behavior of the LLITED satellites Satellite is Try up to 3 seconds to complete the last packet transmitted."]
[11.570812225341797, 6.245216369628906, "The Article URL of the XMM-Newton Satellite is https://doi.org/10.1051/0004-6361/201832664."]
[8.231951713562012, 6.2956061363220215, "The | of the VIRGO Helioseismology and Solar Irradiance Monitoring Experiment is VIRGO: Experiment for Helioseismology and Solar Irradiance Monitoring."]
[9.493426322937012, -0.7475515604019165, "The Design Presentation URL of the Microsatellites Satellite is http://cddis.nasa.gov/lw13/docs/presentations/target_nicholas_1p.pdf."]
[5.363964557647705, 3.284398317337036, "The In-flight Disconnect of the CSD Satellite Component is Unknown."]
[4.82430362701416, 1.6678022146224976, "The Number of Pristine Vantage Points of the THEMIS Constellation Satellite Constellation is 12."]
[6.768422603607178, 7.35323429107666, "The Measurements of the RA-1 Instrument is Precise altitude, Significant wave height, Ocean surface wind speed, Various ice parameters."]
[3.5245890617370605, 4.070647239685059, "The Radiation hardness of the STRV-1d DHS Data Handling System is about 100 krad."]
[8.229918479919434, 10.085206985473633, "The Resolution of the Visual Imager Instrument is More than 600 mega pixels."]
[7.032921314239502, -0.10861720144748688, "The End of Life Date of the EXPORTS Satellite Mission is July, 2025."]
[7.483820915222168, 1.344167947769165, "The Publication Date of the Cluster STAFF experiment Experiment is 1997."]
[9.188131332397461, 3.6618144512176514, "The Elevation Mask of the GNOMES-1 Satellite is 5 degrees."]
[6.016176700592041, 8.494274139404297, "The Temporal Coverage of the Geostationary Infrared Sounder Satellite Instrument is Good."]
[9.239686965942383, 3.1926634311676025, "The Orbit Type of the GEISAT Precursor Satellite is Sun-synchronous."]
[7.209349155426025, 8.926138877868652, "The Swath Width of the PP Instrument is Approximately 28 km."]
[11.702916145324707, -1.065014123916626, "The Mass of the Satellite Payload is 180 kg."]
[7.502955913543701, 0.6834983825683594, "The Launch Date of the Monitor-E Spacecraft is Aug. 26, 2005."]
[6.680929183959961, 4.45816707611084, "The Function of the U-GEO Algorithm is Combines Copernicus Sentinel data with urban planning, resource management, and green infrastructure."]
[3.7040810585021973, 6.414513111114502, "The Max. Data Rate of the RF Communications Communication Subsystem is 100 kbit/s."]
[7.028749942779541, 0.9705458283424377, "The Open Call Year of the OPS-SAT Satellite is 2013."]
[9.447328567504883, 0.8807788491249084, "The Fuel Endurance of the Wind Satellite is Until 2074."]
[6.06758451461792, 8.952407836914062, "The Power Consumption of the RM Radiation Monitor is ~1.4 W."]
[9.20602798461914, 4.189115047454834, "The Stowed Dimensions of the DSX Spacecraft Payload Module Satellite is 3.6 m x 2 m x 1.1 m."]
[5.263248920440674, 5.021710395812988, "The Conference Date of the Laser Communication Terminals Communication Device is 8-13, 2007."]
[4.061636447906494, 6.334662914276123, "The Modulation Schemes of the Transponder Communication Device is PCM/PSK/PM, PSK."]
[6.026329517364502, 0.628818929195404, "The Submission Date of the MinXSS CubeSat is August 15, 2013."]
[5.2521586418151855, 4.097399711608887, "The Functions of the FOS Flight Operations Segment is Operation and control of the satellite, provision of telemetry."]
[7.330599308013916, 5.1227521896362305, "The CO2 Annual Flux Estimation Error of the GOSAT Satellite is 0.54GtC/yr to 0.27GtC/yr."]
[9.114031791687012, 7.897291660308838, "The Counting Ability of the Particle Detector Instrument is 5 x10 4  event/s."]
[7.291255950927734, 2.502938985824585, "The URL of the Cluster Satellite is http://www.esa.int/Our_Activities/Operations/Rejigging_the_Cluster_quartet."]
[6.654031276702881, 2.9555258750915527, "The Avionics of the STRaND-1 Satellite is Smartphone."]
[7.720930099487305, 9.790719032287598, "The Wavelength of the VNIR Band is 1.06 \u00b5m."]
[7.6269731521606445, 3.6431586742401123, "The On-board Orbit Computation of the DORIS-DIODE Satellite System is Operational."]
[8.257749557495117, 9.957983016967773, "The Operation Mode of the NAOMI Imaging Instrument is TDI (Time Delay Integration) mode in the Pan band."]
[9.342384338378906, 4.793880939483643, "The Slew Rate of the NigeriaSat-2 Satellite is 6\u00b0/s."]
[11.663496971130371, -1.088550329208374, "The Payload Mass of the DSP satellites Satellite is 30 kg."]
[5.274649143218994, 3.8269054889678955, "The Development Tools of the EDSN Organization is JIRA, static analysis tools, peer reviews, central repository with subversion tracking, virtual machines."]
[7.060100555419922, 0.6612616777420044, "The Launch Date of the Pl\u00e9iades Satellite is Dec. 17, 2011."]
[11.655914306640625, 1.7960350513458252, "The Conference Presentation of the MASCOT Lander Lander is May 16-20."]
[5.099030017852783, 7.223940372467041, "The Daily Data Volume of the Instrument Satellite Instrument is 50 Gbit."]
[9.1940279006958, 3.0807807445526123, "The North Polar Region Name of the Charon Moon is Mordor Macula."]
[8.568416595458984, 10.484354019165039, "The Data Bandwidth of the RTEPs On-board Image Processing System is 6 Mbit/s."]
[9.674765586853027, -0.5889034867286682, "The Mission Type of the High-Resolution Microsatellite Satellite is Earth Monitoring and Observation."]
[9.629439353942871, 1.5979446172714233, "The Revisit Frequency of the Spacecraft Orbit is Maximum of 4 days."]
[5.527329921722412, 1.8501629829406738, "The Satellite Cluster Quantity of the Kleos S.A. Company is 4."]
[11.928827285766602, 3.2441484928131104, "The Inclination of the PhoneSat-2.5 1U CubeSat Satellite is 51.6\u00b0."]
[8.40546989440918, 9.07404613494873, "The Sensor Type of the OSA Optical Sensor Assembly is Optical."]
[8.641569137573242, 7.127198219299316, "The Sample Rate of the Angular Rate Sensor is 125 Hz."]
[5.058900356292725, 5.211888790130615, "The Antenna Type of the Knudsen Station Ground Station is Quad array 436CP42UG cross polarized UHF Yagis."]
[8.250252723693848, 10.165629386901855, "The Absolute Pointing Uncertainty of the Spectral Block Focal Plane Component is \u00b10.25\u00ba."]
[9.597138404846191, 3.8830277919769287, "The Ground Station Transmission of the CanX-7 Satellite is Next Access."]
[6.620162010192871, 2.7781271934509277, "The URL of the Sierra Nevada Corporation Corporation is https://www.sncorp.com/press-releases/snc-hardware-on-nasa-insight-mission/."]
[7.560245990753174, 4.880032539367676, "The Sun sensors of the BEESAT-1 Satellite is Yes."]
[7.553657054901123, 5.461552143096924, "The Purpose of the OCO-2 Satellite is 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."]
[6.968400955200195, 0.03682020679116249, "The End of Life Date of the AstroSat Astronomy Satellite is 28 September 2025."]
[9.815925598144531, 6.676027297973633, "The Top Temperature of the Meteosat-10 Satellite is 33.5 \u00b0C."]
[8.463956832885742, 10.584078788757324, "The Data Interface of the CCD (Charge-Coupled Device) Imaging Device is Special-purpose serial interface using data/strobe arrangement."]
[5.102972030639648, 4.066359519958496, "The Model of the IXV Recorder Recorder is COTS SSR-500."]
[7.475579261779785, 3.08931827545166, "The Type of the KOMPSat-5 Satellite is SAR."]
[5.314849853515625, 9.602805137634277, "The Maximum Tracking Rate of the STOs and STAEs Analog Electronic units is 0.1\u00ba/s."]
[5.635547637939453, 4.221155166625977, "The ARGOS Support of the ESEX Satellite is Attitude control, communications, radiation-hardened data storage, and housekeeping power."]
[7.175647258758545, 5.700089931488037, "The Purpose of the Aeolus Satellite is Measure Earth's wind on a global scale."]
[7.121243000030518, 2.22796893119812, "The URL of the Shuttle Radar Topography Mission Satellite Mission is http://www.shuttlepresskit.com/STS-99/payload56.htm."]
[9.262994766235352, 1.0044209957122803, "The Software Shutdowns of the IPA Engine is Twice in 20 months of operation."]
[11.466378211975098, 4.881756782531738, "The Rotation Rate of the Pulsar Neutron Star is 30 times per second."]
[7.535489559173584, 0.9439259767532349, "The Article Date of the INTEGRAL Satellite is 26 Jan. 2016."]
[11.764065742492676, 1.670540452003479, "The Hibernation Start Time of the Philae Lander is 00:36 GMT."]
[6.505253314971924, 5.1327924728393555, "The Coherence Change Detection of the TerraSAR-X Satellite is Significantly Enhanced."]
[6.996769428253174, 4.952358245849609, "The Purpose of the Copernicus Sentinel-2 Satellite is Methane hotspot detection."]
[2.2918033599853516, 5.725364685058594, "The Amplifier Type of the SSPA Solid-State Power Amplifier is S-band power amplifier."]
[10.566880226135254, 7.5006866455078125, "The Platform Type of the G\u00f6kt\u00fcrk-1A Satellite is Aluminium chassis with honeycomb panels."]
[8.488389015197754, 2.1690165996551514, "The Launch Date of the Parker Solar Probe Satellite is 2018."]
[6.418227195739746, 2.9484376907348633, "The Mounting of the OCSE Satellite is JAWSAT payload."]
[5.753190040588379, 1.876399278640747, "The Launch Provider of the MethaneSAT Satellite is SpaceX."]
[8.294685363769531, 2.0362064838409424, "The Mission Name of the Solar Probe Plus Satellite is Solar Probe Plus."]
[10.366995811462402, 5.630764007568359, "The Orbital Altitude Decay of the ProSEDS Tether Demonstration Experiment is At least 5-15 km in altitude per day."]
[11.764693260192871, -1.11263906955719, "The Launch Mass of the MSG-3 Satellite is ~2000 kg."]
[8.392885208129883, 10.279621124267578, "The Light Sensitivity of the DNB Sensor is Up to 10 million times fainter than daylight."]
[7.033107757568359, 0.6691869497299194, "The Deployment Date of the LDEF Satellite is April 7, 1984."]
[4.246057033538818, 5.485235214233398, "The Downlink Contact Duration of the IXPE Satellite is 8 minutes."]
[9.261781692504883, 0.9786716103553772, "The Planned Duration of the Science Operations Satellite Phase is At least 2 years."]
[4.398949146270752, 4.763514518737793, "The User Interface Manual Version of the DAPS Data Collection System is 1.1."]
[7.863412380218506, 5.595894813537598, "The Activation of the AutoNav Autonomous Navigation System is Immediate upon activation of the S/C."]
[6.464715003967285, 4.358537673950195, "The Laser Link of the Sentinel-1A Satellite is Excellent stability and robustness."]
[7.532145023345947, 1.137852668762207, "The Failure Date of the Sensor Flipper Unknown is March 23, 1978."]
[2.6569228172302246, 5.346673488616943, "The Power Consumption of the OSDP Onboard Signal Data Processor is 28 W."]
[8.216118812561035, 4.761286735534668, "The Imaging Resolution of the NEMO-HD Satellite is 2.8 m GSD."]
[7.145940780639648, 8.976621627807617, "The Spatial Resolution (MS) of the PP Instrument is 10 m."]
[7.053469657897949, 9.76792049407959, "The Wavelength Range of the Band No 1 Spectral Band is 0.50 \u00b1 0.2 - 0.70 \u00b1 0.2 \u00b5m."]
[9.624773979187012, 4.056099891662598, "The Number of Retroreflectors of the STARLETTE and Stella Satellites is 60."]
[6.044978141784668, 5.94371223449707, "The Application of the SAR Sensor Sensor is Counting parked vehicles."]
[1.5534217357635498, 4.442940711975098, "The Low Voltage Occurrence of the SpriteSat Satellite is After the deployment of the gravity mast."]
[6.890671730041504, 2.963587999343872, "The Managing Office of the IMAP Satellite is Heliophysics Program Office at NASA's Goddard Space Flight Center."]
[11.46090316772461, -0.868665874004364, "The Orbit Capability of the DSX Spacecraft Payload Module Satellite is 6,000 km to 12,000 km any inclination."]
[5.239383220672607, 3.668607473373413, "The Mounting Method of the Avionics and Payloads Satellite Components is Directly onto three equipment radiator panels."]
[6.591167449951172, 0.6098412275314331, "The Launch Date of the SkySat-16 to -18 Satellite is 13 June 2020."]
[7.104438304901123, 3.3426127433776855, "The Ground Segment Location of the KazEOSat-2 Satellite is Astana, Kazakhstan."]
[8.684487342834473, 10.676382064819336, "The Test Image Time of the WFC CCD Imager is Almost 12 hours before the boom deployment."]
[2.967853307723999, 6.5596418380737305, "The Power Consumption of the Transmitter Communication Device is 61.1 W (max)."]
[9.022177696228027, 10.633210182189941, "The GSD (Multispectral) of the EOS Camera is 4 m."]
[9.930822372436523, 8.308721542358398, "The URL of the Solar Orbiter/METIS Coronagraph/Spectrometer is http://congrex.nl/icso/2012/papers/FP_ICSO-089.pdf."]
[6.77755069732666, 6.432018280029297, "The Spatial Resolution of the Nighttime SST Product Dataset is 2 km."]
[8.766578674316406, 0.18395908176898956, "The URL of the EP-107 Skylab Space Station is http://history.nasa.gov/EP-107/ch5.htm."]
[10.371353149414062, 7.235844135284424, "The Function of the TEMBOTM EMC Material is Both the primary deployment mechanism and the principal structural members of the boom."]
[9.585918426513672, 1.4101587533950806, "The Revisit Time of the Tandem-L Satellite is 16 days."]
[9.535508155822754, 0.5566390156745911, "The Mission Life of the QSat Satellite is 2 years."]
[3.9227898120880127, 5.506509304046631, "The Redundancy of the Telemetry Data is High."]
[10.256295204162598, 3.010234832763672, "The Orbit Altitude of the Almaz-1B Satellite is ~ 600 km."]
[7.897128105163574, 3.6032767295837402, "The Impact of Satellite Constellations of the ESO Telescopes Telescope is Not specified."]
[6.572483539581299, 5.233693599700928, "The Measurement Type of the GEOSAT Radar Altimeter (GRAS) Instrument is High-precision range measurements between the satellite and the subsatellite point at nadir."]
[11.508538246154785, -0.8749253153800964, "The Mass of the Prichal Module Docking Port is 4 metric tons."]
[5.834478855133057, 2.958641767501831, "The Industries of the OSG Company is Aerospace, automotive, die/mold, and many others."]
[7.76349401473999, 2.9460299015045166, "The Launch Date of the CartoSat-2 Satellite is Jan. 10. 2007."]
[5.052771091461182, 3.352553129196167, "The Payload of the MDASat-1 Satellite is SDR-based payload that will provide AIS and VDES services."]
[1.048885464668274, 4.323849201202393, "The Battery System of the EPS Electrical Power Subsystem is 2 NiCd batteries of 19 Ah each."]
[10.530471801757812, -1.0200613737106323, "The Mass of the LEO Vantage Microsatellite is 70 kg."]
[7.202364921569824, 9.964682579040527, "The Calibration Date of the HISUI Hyperspectral Imager is 10-15 July 2016."]
[6.012109279632568, 3.8965771198272705, "The Payload Space of the Bartolomeo Platform is 50+ liters."]
[7.908254146575928, 5.9781317710876465, "The Purpose of the Unresolved Imagery Data is Observe and characterize orbiting objects with the goal of determining their attitude and detecting configuration changes."]
[7.116387844085693, 0.6956762075424194, "The Launch Date of the Pleiades-1B Satellite is More than one and a half years before October 2013."]
[9.45914077758789, -0.5527705550193787, "The Design Purpose of the Compact Intersatellite Link Communication System Communication System is For satellites operating in swarms."]
[4.366145133972168, 4.26152229309082, "The Interface Type of the MSV Combined Router and Power Distribution Unit is SPA-S (SPA-SpaceWire) compliant."]
[5.363095760345459, 1.3351469039916992, "The Number of Successful Landings of the Falcon-9 Rocket is 20."]
[7.01886510848999, 3.2740256786346436, "The Operating Status of the RISING-2 Satellite is Nominal."]
[8.732320785522461, 10.015483856201172, "The Impact on Results of the Subapertures Imaging System Component is Larger subapertures yield better results than smaller subapertures."]
[9.657548904418945, 1.4495148658752441, "The Revisit Time of the S/C Satellite is One day."]
[3.020761489868164, 6.610714435577393, "The Transmitter Power of the Radio Communication Device is 5 W."]
[5.916408538818359, 3.5246798992156982, "The Goal of the Neosat program Satellite Program is Build a European supply chain which optimizes costs and guarantees on-time delivery of satellites."]
[4.092503547668457, 2.3735456466674805, "The Platform Size of the 6U CubeSat Satellite is 6U."]
[5.026519775390625, -0.15406890213489532, "The Launch Date of the OneWeb Satellite Constellation is 14th of October."]
[2.250396490097046, 3.792278289794922, "The Solar Panels of the Picard microsatellite Satellite is Single."]
[8.736839294433594, 8.068891525268555, "The Components of the PowerCell Hardware is 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 acceler."]
[6.130224704742432, 2.9739811420440674, "The Heat Shield Manufacturer of the Orion Spacecraft is Lockheed Martin."]
[10.542098045349121, 8.469554901123047, "The Instrument Type of the COR1 Coronagraph1 imager is Internally occulted Lyot coronagraph."]
[9.337581634521484, 4.924199104309082, "The Proton Dynamic Pressure of the ACE Satellite is ~2.4 nPa."]
[10.342363357543945, 2.909531354904175, "The Altitude of the Rideshare mission Satellite is 560 km."]
[2.064891815185547, 4.540927410125732, "The Power Output of the IPS Pointing System is Up to 1.25 kW."]
[9.768838882446289, 3.6353304386138916, "The Quantification Method of the Lunar Meteoroid Impact Flash Detection Detection System is Using the apparent magnitude of the light flash."]
[9.250357627868652, 4.122581481933594, "The Size of the Spacecraft Satellite is 9.9 m (x) x 16.5 m (y) x 3.7 m (z)."]
[6.7755208015441895, 1.780304193496704, "The Presentation Date of the Global Climate Observing System (GCOS) Climate Observing System is July 21, 1999."]
[7.001086235046387, 6.79175329208374, "The Development Time Frame of the GOME Instrument is 1990-1994."]
[8.128345489501953, 3.4021222591400146, "The Size of the Debris Spacecraft Debris is About 1.3 meter pixels."]
[11.708206176757812, 4.618784427642822, "The Distance from Earth of the GSN 069 Black Hole is About 250 million light years."]
[5.212047576904297, 4.606506824493408, "The Segments of the ICU Container is Bottom, Middle, Top."]
[8.394998550415039, 4.698809623718262, "The Geolocation Knowledge of the QuickBird-2 Satellite is < 15 m (3?) after ground processing."]
[7.414486885070801, 10.109986305236816, "The Type of the THI (Thermal Hyperspectral Imager) Payload is Relatively large."]
[4.244058609008789, 6.2879533767700195, "The Uplink Frequency of the Iris Radio Communication Device is Standard X-band."]
[8.935491561889648, 7.60161018371582, "The Ionising Doses of the TimePix radiation sensors Sensor is 4 to 5 krads."]
[5.304187774658203, 4.3231201171875, "The Ground System of the FormoSat-7 / COSMIC-2 mission Satellite Mission is High degree of automation."]
[10.049079895019531, 3.082061290740967, "The Altitude of the ICEYE-X14 and ICEYE-X16 Satellites is Approximately 500 km."]
[2.353998899459839, 3.779808282852173, "The Solar Array Deployment of the TSUBAME Satellite is Automatically deployed after the rocket separation."]
[9.544071197509766, 5.473819255828857, "The Capability of the Attitude & Orbit Control Subsystem (AOCS) Control System is Orienting the dual-gimballed data transmission antenna to point towards the required data reception station during the overpass of the CartoSat-2."]
[10.433053970336914, 5.871452331542969, "The Type of the Micro Systems Technology Experiment is In-Orbit."]
[6.58298397064209, 3.3087942600250244, "The Testing Environment of the CuPID spacecraft Spacecraft is Helmholtz cage."]
[7.606297492980957, 1.6080683469772339, "The Date of the SMAPVEX12 Experiment is 2012."]
[8.280762672424316, 10.50780963897705, "The Peak Power of the 4-band CCD Imager Instrument is 30 W."]
[3.914731502532959, 6.76300048828125, "The SASAR System of the DRT Data Relay Transponder is Not Carried."]
[10.469395637512207, 4.776183128356934, "The Propulsion of the Schiaparelli Module is 3 clusters of 3 hydrazine engines (400 N each), operated in pulse-modulation."]
[1.1787842512130737, 3.8049702644348145, "The Structure of the XI-IV Picosatellite is Conforms to the requirements of the CubeSat program in size and mass."]
[5.6208648681640625, 5.464602470397949, "The Manufacturer of the GPS/MET GPS Receiver is Allen Osborne Associates Inc.."]
[4.346473217010498, 5.200873374938965, "The Avionics Redundancy of the TDS-1 Satellite is Fully redundant."]
[6.768813133239746, 3.3766403198242188, "The | of the SSO-A SmallSat Express is Spaceflight - Introducing SSO-A: The smallsat express."]
[8.541961669921875, 9.83885669708252, "The length of the Detector Instrument is 1024 pixels."]
[5.446069717407227, 5.78676176071167, "The Antenna Type of the Tandem-L Satellite is Digital radar antenna."]
[6.936882972717285, 3.5203683376312256, "The Failure Analysis of the Taurus Frangible Joint Design Satellite Component is Detailed fault tree or failure mode analysis."]
[9.480809211730957, 0.5492116808891296, "The Mean Mission Life of the SBSS Satellite System is 5.5 years."]
[9.501724243164062, 8.736227989196777, "The Type of the Primary Mirror Telescope Component is Off-axis paraboloid."]
[8.977544784545898, 7.118222236633301, "The Quantity of the Sun sensors Sensor is 4."]
[4.269700527191162, 6.649755477905273, "The IF Frequency of the Receiver Communication System is 112.5 MHz."]
[7.041807651519775, 0.5483980774879456, "The Launch Date of the SPOT-6 Satellite is September 2012."]
[9.143790245056152, 10.705713272094727, "The Observation Area of the T1 Trigger Camera is 160 km x 160 km."]
[10.475519180297852, 7.365776538848877, "The Protection of the Flywheel Housing Satellite Component is Capton tape."]
[4.093329906463623, 6.470763206481934, "The Modulation Indices of the Transponder Communication Device is Command and ranging (for uplink), telemetry and ranging (for downlink)."]
[6.926881790161133, 2.3389573097229004, "The URL of the Xatcobeo CubeSat is http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20100021944_2010023813.pdf."]
[8.362181663513184, 6.935405254364014, "The Data Integration of the CDE Sensor is Over several days."]
[10.845332145690918, 7.241683483123779, "The Energy Range of the X-ray Background Spectrum Spectrum is 3-300 keV."]
[9.0205717086792, 5.301315784454346, "The Pointing Accuracy of the IRS-1C and IRS-1D Spacecraft is Roll and pitch = \u00b10.15\u00ba, yaw = \u00b10.2\u00ba."]
[8.522855758666992, 8.92288589477539, "The Filter Type of the VIS channel Spectrometer is VIS 3."]
[7.141413688659668, 4.508767604827881, "The Example of the Coordinated Observations Satellite Mission Activity is 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."]
[8.86886978149414, 7.289850234985352, "The Accuracy of the Sun sensors Sensor is 0.2\u00ba (3\u03c3)."]
[7.768672943115234, 8.448043823242188, "The Resolution of the CHRIS Imaging Spectrometer is 17 to 34 meter."]
[6.683221817016602, 0.5502203106880188, "The Launch Date of the Meteosat-7 Satellite is September 1997."]
[7.111046314239502, 9.090411186218262, "The Ground Footprint of the RA Imaging System is 16 km."]
[7.599976062774658, 1.0729186534881592, "The Image Capture Date of the ALOS satellite Satellite is February, 2014."]
[7.212331295013428, 5.760081768035889, "The Data of the Aeolus Satellite is Altitude and vertical extent of the aerosol layer."]
[1.0032308101654053, 4.3890604972839355, "The Battery unit of the EPS Electrical Power Subsystem is 8 series NiMH (750 mAh, 9.6V)."]
[7.567973613739014, 7.426296710968018, "The Platform of the SOVA Experiment is Eureca."]
[9.057489395141602, 5.24367094039917, "The Attitude of the Satellite Spacecraft is BBQ-attitude."]
[10.355734825134277, 4.912472248077393, "The Thrusters of the LISA Pathfinder Spacecraft is \u00b5N."]
[7.166645526885986, 0.4121803045272827, "The First Flight of the SIMBA Satellite RMIB SIMBA program is 2016."]
[5.963539123535156, 8.463727951049805, "The Operation Mode of the GeoSTAR Atmospheric Microwave Sounder is Nowcasting and very short range weather forecasts."]
[6.837568759918213, 4.742842674255371, "The Information Provided of the Copernicus Sentinel-4 and Sentinel-5 Satellite Missions is Air quality, solar radiation and climate monitoring."]
[9.570245742797852, 3.974393129348755, "The Position Control of the CanX-4&5 Satellite is 10 cm."]
[7.761485576629639, 2.1456024646759033, "The Parachute Quantity of the ExoMars mission Mars Mission is Two main parachutes."]
[11.32226276397705, 4.168278694152832, "The Confirmed Transiting Planets of the Kepler-11 Star System is 6."]
[5.984567642211914, 3.0611140727996826, "The Satellite of the Spire Global UK Company is Nanosatellites."]
[10.50282096862793, -1.0229809284210205, "The Mass of the SOCRATES Microsatellite is 48 kg."]
[7.756763935089111, 6.024233818054199, "The Calibration Method of the Meteosat Second Generation (MSG) Radiometer/Imager Satellite is Dedicated Moon/Sun/Deep-space Scans."]
[4.726817607879639, 7.366480827331543, "The Footprint of the Millimeterwave receiver Receiver is 15 m."]
[5.840251445770264, 8.59184741973877, "The Scanning Period of the MWHS-II Microwave Humidity Sounder is 2.667 s \u00b1 50 ms."]
[2.6239073276519775, 5.41320276260376, "The Power Usage of the Microelectronic device Device is 20 times less than proven technology."]
[6.106255531311035, 3.599059820175171, "The Operator of the GovSat-1 Communication Satellite is LuxGovSat S.A.."]
[6.974883556365967, 2.5029098987579346, "The URL of the TOPCAT Satellite is https://web.archive.org/web/20120306134448/http://www.bis.gov.uk/assets/bispartners/ukspaceagency/docs/space%20science/cubesats/astrium%20payload%20text%20and%20picture.pdf."]
[9.408138275146484, 5.124467372894287, "The Attitude Control of the SCD-2 Satellite is Spin-stabilized."]
[5.180860996246338, 3.6419708728790283, "The Equipment Modules of the Terra Satellite is Sized and partitioned to facilitate pre-launch integration and test of the spacecraft."]
[7.674785137176514, 1.2403545379638672, "The Name Change Date of the Copernicus Program is December 11, 2012."]
[10.288981437683105, 9.343310356140137, "The Solar Array Dimensions of the IRIS Satellite is 0.6 m x 1.3 m."]
[8.541799545288086, 6.871438980102539, "The Absolute Accuracy of the OVM Overhauser scalar magnetometer is 0.5 nT."]
[6.842967987060547, 2.9957008361816406, "The Ops Renewal Contract of the SeaHawk-1 Satellite is Received."]
[8.097935676574707, 5.07857084274292, "The Statistical Accuracy Goal of the HaloSat Satellite is \u00b10.5 LU."]
[9.435392379760742, 5.5465850830078125, "The Pointing Accuracy of the AOCS Attitude and Orbit Control Subsystem is < 36 arcsec for the Z-axis."]
[10.737961769104004, 3.266763925552368, "The Separation Distance from Earth of the Reentry Vehicle Vehicle is Around 5,000 km."]
[6.939889430999756, 1.2448375225067139, "The Conference Date of the WorldView-1 Satellite is Nov. 11-14, 2007."]
[7.207438945770264, 4.505944728851318, "The Potential Data of the Tandem-L Satellite is Forest height, structure, and biomass."]
[3.596266746520996, 6.439330101013184, "The Data Rate of the S-band Communication Band is 66.54 kbit/s."]
[1.9102169275283813, 4.170196533203125, "The Power of the solar panels solar panels is Average power of 10 W."]
[6.078428268432617, 6.115965843200684, "The Spatial Resolution of the SAR Sensor Subsystem SAR Sensor is 1 m x 1 m."]
[9.124381065368652, 3.143230438232422, "The Orbit Type of the EURECA Satellite is Low Earth Orbit (LEO) circular."]
[9.285834312438965, -0.7473605871200562, "The Launch Site of the KazSTSAT Microsatellite is VAFB (Vandenberg Air Force Base) in California."]
[7.873560905456543, 7.571320056915283, "The Purpose of the SCAR TSI Calibration Device is Improve the long-term stability of TSI measurements."]
[6.894759178161621, 1.8765695095062256, "The End of Life Date of the Kolibri-2000 Satellite is 3 May 2002."]
[7.312615394592285, 1.0503559112548828, "The Launch Date of the M3MSat Satellite is 2016."]
[6.820752143859863, 3.9643256664276123, "The Mission Type of the SEOSAT-Ingenio Satellite is Optical Earth-observation."]
[6.921758651733398, 8.040037155151367, "The SIC Temporal Sampling Period of the CIMR Radiometer Imager is Sub-daily."]
[6.060978412628174, 9.731389045715332, "The Mass of the CALET Telescope is 650 kg."]
[6.844437599182129, 4.49860954284668, "The Mission Phase of the Biomass Satellite is Last phases of development."]
[8.70698356628418, 7.6206865310668945, "The Number of Sensors of the Rosetta Plasma Consortium Instrument Suite is Five."]
[5.0678510665893555, 7.568179607391357, "The Data Rate of the SAGE-III Instrument is 115 kbit/s."]
[7.797222137451172, 1.8442820310592651, "The Launch Date of the Mars Hope probe Spacecraft is February 2021."]
[8.110060691833496, 7.133387565612793, "The Purpose of the Matroshka AstroRad Radiation Experiment (MARE) Radiation Experiment is Provide valuable data on radiation levels during missions to the Moon and test the effectiveness of the new vest."]
[4.933014869689941, -3.206535577774048, "The | of the D. M. Smith Author is D. M. Smith."]
[7.221724987030029, 4.403000831604004, "The Science Instruments of the Landsat-9 Satellite is Operational Land Imager 2 (OLI-2) and the Thermal Infrared Sensor 2 (TIRS-2)."]
[5.829441070556641, 3.0460731983184814, "The Manufacturer of the XMM-Newton Satellite is ESA."]
[9.746112823486328, 8.799448013305664, "The Number of Mirrors of the Korsch telescope Telescope is 5."]
[9.8330078125, 6.919998645782471, "The Constraint of the Instrument Payload is Keep the instrument radiators away from Nadir direction for thermal stability purposes."]
[8.613426208496094, 8.812846183776855, "The Mirror Type of the Long Wavelength Band Spectrometer is Off-axis parabolic cylinder."]
[10.243218421936035, 5.573976039886475, "The Principle of the Momentum-exchange Tethers Space Propulsion System is Based on the gravity gradient force."]
[7.090928077697754, 5.402957439422607, "The Data Usage of the Aeolus Satellite is Climate Research, Weather Forecasting."]
[10.106252670288086, 6.9158525466918945, "The Sewing of the MLI Thermal Control Device is Connection Method."]
[6.960160732269287, 1.4572004079818726, "The Presentation Date of the CNES Satellite is Feb. 16-18, 2010."]
[6.814595699310303, 4.350365161895752, "The Applications of the LAPAN-TUBSAT Satellite is Disaster monitoring, vegetation monitoring."]
[7.285933971405029, 2.4526479244232178, "The URL of the Kepler Satellite is https://kepler.nasa.gov/news/nasakeplernews/index.cfm?FuseAction=ShowNews&NewsID=226."]
[5.919480800628662, 2.947521209716797, "The Composition of the SloshSat Investigators' Working Group (IWG) Team is Academic researchers from Groningen State University (NL), Delft Technical University (NL), Technion (Israel), and investigators from ESA, NASA and NLR."]
[7.893315315246582, 4.430400848388672, "The Panchromatic Band Ground Resolution of the WorldView-3 Satellite is 31 cm."]
[8.737446784973145, 8.929497718811035, "The Filter Thickness of the VIS channel Spectrometer is 3.00 mm."]
[9.356146812438965, -0.7717359662055969, "The Launch Time of the KazSTSAT Microsatellite is 18:34:05 GMT."]
[6.302089214324951, 8.515523910522461, "The Nr. of spectral or frequency bands of the Microwave System Microwave System is 22 MW channels."]
[7.27725887298584, 2.9538514614105225, "The Science and Mission Overview of the STEREO Satellite is  URL: http://www.jhuapl.edu/techdigest/TD/td2802/Kaiser.pdf."]
[7.502383708953857, 1.879125952720642, "The Operation Start Date of the ICE-Cubes facility Research Facility is December."]
[8.46247673034668, 10.230194091796875, "The Detector Type of the Instrument Satellite Instrument is 1D CCD (4098 pixels)."]
[8.97612190246582, 8.316368103027344, "The Emissivity of the Calibration Mirror TIR Subsystem Component is Near-perfect zero radiance reference."]
[8.296165466308594, 6.069486141204834, "The Pointing Requirements (Knowledge) of the Aquarius Radiometer System is 0.1\u00ba."]
[9.447778701782227, 0.7922960519790649, "The Battery Life of the AAUSat-1 CubeSat is Two and a half months."]
[9.214887619018555, 0.7666821479797363, "The Mission Duration of the BEAM Module is Two years."]
[8.650716781616211, 3.1804375648498535, "The Contribution of the GOCE Satellite is New view of the remnants of lost continents hidden deep under the ice sheet of Antarctica."]
[5.296412467956543, 1.5339655876159668, "The Number of Rocket Motors of the Super Strypi rocket Rocket is 3."]
[8.786674499511719, 1.3905688524246216, "The Observation Date of the Van Allen Probes Satellite is March 17, 2015."]
[6.9598259925842285, 2.530235528945923, "The Head of the Astronomy Missions Division of the Integral Satellite is Andreas Rudolph."]
[6.593467712402344, 1.2818102836608887, "The Operation Start Date of the SARah system Satellite System is End of 2019."]
[6.493416786193848, 1.3335903882980347, "The Designers of the ISIM Compartment is Matthew Garrison, Keith Parrish, Charles Perrygo."]
[8.465475082397461, 10.46525764465332, "The Element Size of the CCD Detector Matrix Detector is 22.5 \u00b5m x 22.5 \u00b5m."]
[6.603433609008789, 6.449902057647705, "The Production Frequency of the Nighttime SST Product Dataset is Hourly."]
[8.85695743560791, 1.7760074138641357, "The Launch Date of the BepiColombo Satellite is October 2018."]
[10.320712089538574, 9.474596977233887, "The Mission Type of the IRIS Satellite is Solar Study."]
[7.588359832763672, 5.84483528137207, "The Solar Calibration Components of the SeaWiFS Satellite is Solar radiation diffuser, input port."]
[10.468605041503906, -1.0012407302856445, "The Mass of the KazSTSAT Microsatellite is <100 kg."]
[8.303468704223633, 8.932146072387695, "The Open Pores Fraction of the MXT Instrument is 50."]
[9.278850555419922, 10.253050804138184, "The FOV of the 16 mm camera Camera is 6.9\u00ba x 5.336\u00ba."]
[4.876070022583008, 7.483080863952637, "The Energy of the UHF Band is 1.8 \u00b5eV."]
[11.760087966918945, -1.2173385620117188, "The Launch Mass of the QZS-1 Satellite is 4100 kg."]
[10.35981559753418, 2.6871774196624756, "The Orbit Altitude of the Beijing-3A Satellite is 500 km."]
[7.121037006378174, 6.8700270652771, "The Mounting Date of the IASI-NG PFM instrument Instrument is 2022."]
[7.847217082977295, 9.045763969421387, "The Passbands of the HIRES Instrument is 395 - 435 nm, 535 - 585 nm, 625 - 675 nm, 725 - 775 nm, and 450 - 800 nm."]
[6.363725662231445, 3.1660842895507812, "The Program of the MiRaTA Satellite is In-Space Validation of Earth Science Technologies."]
[7.632792949676514, 5.427107810974121, "The Cal_limb data Collection of the OCO-2 Satellite is Solar and Atmospheric Absorption Lines."]
[7.033324241638184, 9.878437995910645, "The Center Wavelength of the Band No. 4 Spectral Band is 504.96 nm."]
[8.2886381149292, 6.444889545440674, "The Area Collection Rate of the Framer Sensor is Very low."]
[6.679538726806641, 2.990429401397705, "The Program of the SMAP Satellite is ESSP (Earth System Science Pathfinder)."]
[7.593847274780273, -0.4720701277256012, "The Last-Second Abort Date of the Falcon 9 Rocket is Oct. 2."]
[8.092074394226074, 5.329751968383789, "The Positioning Precision of the Galileo Satellite System is Meter-scale."]
[9.13801383972168, 6.762031078338623, "The Type of the Star sensor Sensor is CCD matrix."]
[11.076902389526367, 2.5579776763916016, "The Altitude of Rear Heatshield and Parachute Jettison of the Schiaparelli Lander is 1.3 km above the surface."]
[5.606191158294678, 3.8926830291748047, "The Location of the BSOCC Satellite Operation Control Center is Just about 10 miles northeast of the GSFC."]
[9.200624465942383, 10.1307373046875, "The Manufacturer of the LISS-I Camera Imaging Device is ISRO."]
[10.436052322387695, -0.9592837691307068, "The Mass of the IDEA OSG-1 Microsatellite is 22 kg."]
[7.897708892822266, 4.726020336151123, "The Resolution of the Spotlight-1A Satellite is Finest."]
[3.3729844093322754, 5.893576622009277, "The Track Duration of the DSN Communication System is 3.5-5 hours."]
[11.840500831604004, 0.9753140807151794, "The Number of Scientific Payloads of the Chang\u2019e-4 Mission is 6."]
[7.580568790435791, 0.4586157202720642, "The Launch Date of the DSCOVR Satellite is Feb. 9, 2015."]
[5.326372146606445, 10.388785362243652, "The Data Delivery of the LIS Lightning Imaging Sensor is Once operations begin."]
[9.786930084228516, 3.6281473636627197, "The Measurement Quality of the Lunar Meteoroid Impact Flash Detection Detection System is High signal-to-noise ratios (SNR)."]
[7.354473114013672, 4.324041843414307, "The Map Area Coverage of the Copernicus Sentinel-1 Satellite is 176 km by 170 km."]
[9.58897590637207, 5.661768436431885, "The ADCS of the IOD-1 GEMS Satellite is Attitude Determination and Control Subsystem."]
[7.150295257568359, 2.5311014652252197, "The URL of the ALOS PRISM Satellite is http://www.isprs-ann-photogramm-remote-sens-spatial-inf-sci.net/II-4/71/2014/isprsannals-II-4-71-2014.pdf."]
[9.007996559143066, 9.302555084228516, "The Thickness of the GDS Light Curtain is 3 mm."]
[11.440683364868164, -1.361402988433838, "The Mass of the ITUpSat-1 Satellite is \u2264 1 kg."]
[6.839670658111572, 5.815636157989502, "The Application of the TEMPEST Sensor is Numerical models and characterizing the moisture surrounding tropical cyclones."]
[5.0981221199035645, 7.6288628578186035, "The Data Rate of the ASPOC Instrument is 0.13 kbit/s."]
[5.9905900955200195, 4.925478935241699, "The Processing Location of the OSIRIS Data Processing is University of Saskatchewan, Saskatoon, Canada."]
[7.697446823120117, 0.22643689811229706, "The Next Launch Date of the Soyuz Spacecraft is Spring of 2022."]
[5.210109710693359, 6.702280521392822, "The Size of the Antennas Communication Equipment is 9.1 m."]
[5.351095199584961, 5.352108478546143, "The Owner of the Deep Space Tracking Antenna Antenna is China."]
[3.613865613937378, 6.369152545928955, "The Back-up Channel Data Rates (Downlink) of the RF Communications Communication System is 38.8 kbit/s."]
[6.244404315948486, 3.5081679821014404, "The Operator of the Meteosat-7 Satellite is EUMETSAT."]
[6.177016258239746, 6.592793941497803, "The Polarization of the ICEYE-X1 Satellite is Single VV."]
[1.2998415231704712, 4.503454208374023, "The Voltage of the Battery Power System is Unknown."]
[10.384496688842773, 9.591588020324707, "The Integration Date of the IRIS Satellite is Jan. 18, 2013."]
[1.7832422256469727, 4.388543605804443, "The Solar Power of the EPS Electrical Power Subsystem is at BOL: 1390 W (max), at EOL: 1100 W."]
[8.159021377563477, 4.402580261230469, "The Resolution of the ASTRO-H Satellite is 30-50% of the hard X-ray Cosmic Background."]
[7.91184663772583, 0.5542059540748596, "The Re-Entry Date of the Aeolus Satellite is Before the end of August."]
[10.630329132080078, -1.684931755065918, "The Cargo Capacity of the HTV-9 Cargo Transfer Spacecraft is Up to six tons."]
[7.716117858886719, 8.096405982971191, "The Objective of the CAVIS Imager is Monitor the atmosphere and provide correction data to improve WorldView-3's high-resolution imagery."]
[11.49549674987793, 5.768455982208252, "The Travel Path of the X-ray emission Phenomenon is Towards us through dusty regions of our Galaxy."]
[6.157001972198486, 8.155172348022461, "The Bandwidth of the Radiometer Instrument is 22 MHz."]
[5.970648288726807, 4.240750789642334, "The Location of the Reykjav\u00edk City is Seltjarnarnes Peninsula, in southwest Iceland."]
[7.0787248611450195, 3.7874767780303955, "The Usage of the Pelican Satellites Satellite is Mapping services, environmental tasks, defense, support rescue operations."]
[4.058322906494141, 5.778346061706543, "The VHF-band FSK Channels Data Rate of the UoSAT-12 Satellite is 9.6 kbit/s."]
[5.722352027893066, 3.7720322608947754, "The Content of the High-level Activity Schedule Product is Times the LCRD payload will operate and any operational events that may impact host spacecraft flight or ground operations."]
[8.446142196655273, 10.229399681091309, "The Data rate of the Optical System Imaging System is 665.4 kbit/s."]
[11.35091781616211, 6.941714763641357, "The Time Resolution of the NICER X-ray Timing Instrument is Highest of any astronomy instrument flown."]
[4.728520393371582, 1.5835707187652588, "The Number of Phase-B Contracts of the Galileo Second Generation Satellite System is 11."]
[11.318872451782227, 3.0544486045837402, "The Composition of the Rocklea Dome Geological Formation is Light-colored granites."]
[7.856399059295654, 8.220733642578125, "The Pixel Exposure Time of the Instrument Satellite Instrument is 1.625, 3.25, or 6.5 ms."]
[6.811669826507568, 2.1005756855010986, "The Rainfall Data URL of the TRMM Satellite is http://pmm.nasa.gov/TRMM/realtime-3hr-7day-rainfall."]
[6.053040504455566, 9.625882148742676, "The Mass of the SD2 Sample Drill and Distribution System is 4.8 kg."]
[9.260761260986328, 7.995940208435059, "The Plastic Scintillator Counters of the Veto System Particle Detector is 5."]
[6.568772315979004, 3.3090896606445312, "The Launch Site of the Sentinel-1B Satellite is Kourou."]
[7.775213241577148, 7.220742225646973, "The Measurement Precision of the SOFIE Instrument is T 0.2 K, O3 11 ppbv, H2O 70 ppbv, CH4 5 ppbv, PMC extinction 5 x 10 -8 km -1."]
[9.941121101379395, -0.7904154658317566, "The Imaging Capability of the Kestrel Eye-2M Microsatellite is Spot objects on Earth's surface about the size of a car."]
[9.556587219238281, 1.4349911212921143, "The Operating Hours of the LMOC Ground Segment is 24 hours per day, seven days per week."]
[9.126853942871094, 8.749757766723633, "The Correction Factor of the Sun and Galactic Glint Optical Phenomenon is 0.98."]
[8.021639823913574, 4.855576038360596, "The Ground Instantaneous Field of View (GIFOV) of the Climate Observatory Satellite is ~250 m spatial resolution."]
[9.303168296813965, 3.303866386413574, "The Orbit of the TRUTHS Satellite is Asynchronous."]
[9.401756286621094, 7.756311416625977, "The Temperature Sensitivity of the SOHO's EIT Extreme-ultraviolet Imaging Telescope is 1 million, 1.5 million, 2 million and 60,000\u201380,000\u00baC."]
[9.822661399841309, -0.7451497912406921, "The Main Imager Spectral Wavelengths of the PROBA-1 Microsatellite is 18 programmable visible and near-infrared wavelengths."]
[8.620221138000488, 3.6756508350372314, "The Location of the GOMS-1 Satellite is 76.5\u00ba East."]
[4.70482873916626, 2.5713722705841064, "The Capacity of the Node-3 Module is Up to eight ISS equipment racks."]
[8.717681884765625, 5.431177616119385, "The Pointing Requirement of the Imaging Payload Satellite Component is Towards nadir."]
[10.141092300415039, 4.870413780212402, "The Manufacturer of the T6 thrusters Ion Thrusters is QinetiQ."]
[9.308731079101562, 6.3894524574279785, "The Use Case of the Specialized Asset Trackers Tracking Device is Big productivity gains with a specific asset type."]
[7.217051982879639, 5.705117702484131, "The Wind Velocity Range (Troposphere) of the Aeolus Satellite is 0 - 2 km."]
[6.5788774490356445, 0.42862892150878906, "The Presentation Date of the CBERS Satellite is Feb. 4, 2009."]
[7.398797988891602, 4.8602824211120605, "The Purpose of the TOPCAT Payload is Ionospheric study based on GPS measurements."]
[7.704590320587158, 7.709816932678223, "The Sensitivity to Multipath of the FFRF Sensor Instrument is 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."]
[10.198822021484375, 1.0947887897491455, "The LTDN of the SuperView-1 01 and Superview-1 02 Satellite is 10:30 hours."]
[3.8102529048919678, 4.614024639129639, "The Type of the Sun Sparc microprocessor Microprocessor is Radiation-hardened."]
[3.2727739810943604, 5.9604878425598145, "The Function of the SDR (Software Defined Radio) Communication Device is Dynamically change its receive and transmit frequencies."]
[6.512592792510986, 0.831440269947052, "The Launch Date of the GOSAT Satellite is 23 Jan 2009."]
[6.481191635131836, 1.9263217449188232, "The Design Requirements of the Swarm Spacecraft Satellite is Magnetic cleanliness, Magnetic field vector attitude knowledge, Ballistic coefficient, Accelerometer proof-mass vs satellite CoG location."]
[5.973646640777588, 5.1329216957092285, "The Type of the CRATEX (C-band Radar Transponder Experiment) Payload is Eliminated."]
[9.022648811340332, 8.444770812988281, "The Sweep Angle of the Sensor Sensor is 10.4\u00ba."]
[3.875473737716675, 6.392648220062256, "The Downlink Frequency of the TT&C Data Communication is 2089 MHz."]
[7.72238826751709, 7.156180381774902, "The Planned Position of the TEMPO Satellite is 91\u00b0 West, above the equator."]
[7.591503143310547, 6.579970359802246, "The Typical Value of the NO2 Satellite Instrument is 6."]
[5.31281852722168, 10.391960144042969, "The Coverage of the ISS-LIS Lightning Detection Instrument is CONUS (CONtinental US)."]
[6.260469436645508, 5.112292289733887, "The Conference Presentation of the MMS Phase 2B Navigation Performance Navigation Performance is AAS/AIAA Astrodynamics Specialist Conference."]
[10.367671012878418, 4.686044692993164, "The Delta V of the Propulsion Subsystem Propulsion is 20 m/s."]
[1.5364960432052612, 4.912849426269531, "The Operating Voltage of the Herley MD2000C-1 Transponder Module is 22\u201332 VDC."]
[1.5726544857025146, 4.640928268432617, "The Soft Start Up of the DC-DC converter Power Converter is Typically greater than 1ms/V."]
[6.620300769805908, 10.67989444732666, "The Nominal SNR of the Band 8 Spectral Band is 750."]
[10.746182441711426, 3.3627285957336426, "The Operating Distance from the Sun of the Rosetta Spacecraft is Over 800 million km."]
[4.939250946044922, 4.599969387054443, "The Operation Mode of the Ground Segment Communication System is Store-and-forward."]
[6.635190010070801, 0.8140586614608765, "The Calibration and Validation Date of the DubaiSat-2 Satellite is Early March 2014."]
[4.16254186630249, 1.3546223640441895, "The Mission Type of the Buccaneer CubeSat is Non-EO."]
[11.75922679901123, 4.3940911293029785, "The Age of the Chamaeleon I Star-forming Region is Two million years-old."]
[8.36605167388916, 10.149118423461914, "The Array of the Fluidic Card Device is 4 x 12."]
[7.622064590454102, 5.46402645111084, "The On Board Calibrator (OBC) of the OCO-2 Satellite is Calibration Data Collection."]
[9.268216133117676, 1.0557441711425781, "The Mission Duration of the Solar Maximum Mission Satellite is 14 Oct.. 1984 - 15 April 1986."]
[8.053275108337402, 1.293471336364746, "The Date of the Cloud-free Iceland Weather Phenomenon is 28 August 2020."]
[1.7775193452835083, 5.360015869140625, "The Current of the Voltage 4 Modulator is 250."]
[17.728219985961914, 7.1627726554870605, "The J2000 declination (deg) of the GROJ1744-28 Pulsar is -28.741."]
[6.059469699859619, 2.913594961166382, "The Consortia of the Moonlight Lunar Telecommunications and Navigation Satellite Network is 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 (ALT."]
[6.3611907958984375, 5.399410247802734, "The SAR Techniques of the TanDEM-X Satellite is Digital beamforming (DBF) with two satellites, single-pass polarimetric SAR interferometry, single-pass along-track interferometry with varying baseline."]
[6.9686055183410645, 4.300908088684082, "The Measurement Domain of the Satellite EO is Atmosphere, Ocean, Land, Gravity and Magnetic Fields, Snow & Ice."]
[9.544806480407715, 5.946390628814697, "The Pointing Accuracy of the iADCS-100 ADCS System is Well below 1\u00b0."]
[11.162084579467773, 3.530036211013794, "The Comet of the Rosetta Spacecraft is 67P/Churyumov-Gerasimenko."]
[8.69975757598877, 9.675119400024414, "The Brighter Areas Indicator of the Image Data is Changes in amplitude."]
[11.176019668579102, 6.886845588684082, "The Function of the MXS Modulated X-ray Source is Demonstration of X-ray communication in space."]
[6.286984920501709, 8.257102966308594, "The Operating Frequencies of the SMMR Microwave Radiometer is 18.0 GHz."]
[7.376583576202393, 9.642666816711426, "The Energy of the VIS (red) Band is 1.9 eV."]
[8.76240348815918, 2.2003931999206543, "The Principal Investigator of the New Horizons Spacecraft is Alan Stern."]
[6.696542263031006, 8.439193725585938, "The Spectral Bands of the CIMR Radiometer Imager is 1.4, 6.9, 10.65, 18.7, and 36.5 GHz."]
[8.276564598083496, 6.323476791381836, "The Cost (sensor + spacecraft) of the Push Frame Framer with a fast steering mirror Sensor is Low."]
[9.535307884216309, -0.5621886253356934, "The Payload Data of the ASAP Nanosatellite is High-resolution image data, in the order of 100 MB/day."]
[11.67983341217041, 2.9947381019592285, "The Orbit Inclination of the GHGSat-C2 (Hugo) Nanosatellite is 97.6\u00ba."]
[10.017470359802246, 4.325003623962402, "The Propulsion of the CAPSTONE Satellite is Solar and the Sun\u2019s gravity."]
[7.850705146789551, 9.911590576171875, "The Swath Width of the HRMX Imaging System is 10 km."]
[9.165781021118164, 5.160365581512451, "The Coarse Stabilization of the S/C Satellite is Gravity gradient boom (actuator, 6 m long)."]
[5.777003288269043, 5.407654285430908, "The Performance of the GPSP Instrument is Same or better as on Jason-2."]
[5.963937282562256, 5.516809940338135, "The GNSS Signals of the Pyxis-RO Instrument is 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)."]
[8.52428913116455, 6.382380485534668, "The Solar Wind Measurements of the IMAP Satellite is Electron, proton, heavy ion, and magnetic field."]
[6.034937381744385, 1.7876218557357788, "The Launch Vehicle of the ETS-VIII Spacecraft is H-IIA F11."]
[8.472572326660156, 7.125347137451172, "The Wide Band Receiver Tunable Frequencies of the IOF Plasma Wave Instrumentation is 2000, 500, 125, and 31.1 kHz."]
[9.436331748962402, 1.4110076427459717, "The Imaging Opportunities of the TeLEOS-1 Satellite is Up to 6 within a day."]
[4.303826332092285, 6.490480899810791, "The Downlink Frequency of the RF Communications Communication System is UHF band (437.5 MHz)."]
[5.666125774383545, 5.082723617553711, "The Manufacturer of the Near Real Time SAR Processor SAR Processor is MRSA/SAC team."]
[6.9208664894104, 4.2578277587890625, "The Objective 2 of the EPS (EUMETSAT Polar System) Satellite System is Provide enhanced monitoring capabilities (complimentary to ENVISAT) to fulfil the requirements to study the Earth climate system."]
[8.615228652954102, 10.325389862060547, "The Type of the DU Detector Unit is CMOS APS (Active Pixel Sensor)."]
[5.288444519042969, 5.351590633392334, "The Coherence of the Optical Terminal Communication Device is True."]
[9.474997520446777, 7.641064167022705, "The Temperatures of the Cooler Passive Cooler is 98 K for MWIR/SWIR patch."]
[7.760581016540527, 8.308844566345215, "The Image Production of the SECCHI Instrument is About 7 images/hour."]
[9.188673973083496, -0.45471519231796265, "The URL of the Galassia Nanosatellite Satellite is http://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=3418&context=smallsat."]
[5.583261013031006, 2.8215432167053223, "The Platform of the GaoJing / SuperView minisatellites Satellite is CAST3000B light agile platform."]
[6.958164691925049, 1.3017538785934448, "The Date of the 30th Annual AIAA/USU SmallSat Conference Conference is August 6-11, 2016."]
[11.495525360107422, -0.7314324975013733, "The Hydrazine Usage of the SPOT-4 Satellite is 2.8 kg."]
[11.449644088745117, -1.3376590013504028, "The Weight of the Satellite Communication is 95 grams."]
[3.776745080947876, 2.3808653354644775, "The Power of the COPPER CubeSat is 2 W."]
[8.842169761657715, 9.321965217590332, "The Fiber Optic Cable Type of the Detector Box Instrument is Various lengths."]
[9.382715225219727, -0.5065545439720154, "The Platform of the MANTIS Satellite is Nanosatellite."]
[10.226423263549805, 1.0375531911849976, "The LTDN of the ALOS-3 Satellite is 1030 hours."]
[4.017856597900391, 5.894076824188232, "The Channels of the Communication System Data Transmission is Two."]
[5.58096981048584, 2.9410998821258545, "The Bus Design of the Restore-L Satellite is Maxar's decades-proven 1300-class platform."]
[9.488738059997559, 4.3080291748046875, "The Main Body Volume of the Solar Orbiter Spacecraft is 2 m3."]
[6.129741668701172, 4.42626428604126, "The Origin of the ERA Robotic Arm is Europe."]
[6.110502243041992, 7.954222679138184, "The Sensitivity of the MTVZA-GY Radiometer is Factor 2."]
[10.278217315673828, 9.400796890258789, "The Emission Detection Capability of the Iris Satellite is 100 times smaller than any other satellite."]
[8.119900703430176, 0.30195561051368713, "The Anomaly Date of the RapidScat Team Investigation Team is Sept. 9, 2016."]
[4.8125996589660645, 1.8841301202774048, "The Rotation of the Captain Role Satellite Operation is Every spacecraft holding the role of Captain at least once and one spacecraft being Captain twice."]
[9.528785705566406, 0.472167044878006, "The Battery Endurance of the Satellite Spacecraft is 5 years."]
[2.242454767227173, 3.7984793186187744, "The Solar Panels of the Microsatellite Satellite is Four deployable solar panels of 0.5 m2."]
[10.028011322021484, 2.170356035232544, "The No of revolutions of the KOMPSAT-3 Satellite is 14.6 revolutions/day."]
[9.603025436401367, 6.649111747741699, "The Wear-in Test Cycles of the Redesigned SMA Component is 15 cycles."]
[8.247419357299805, 0.17588387429714203, "The Landing Date of the CIMON-1 Prototype is 27 August 2019."]
[5.997655868530273, -0.24909000098705292, "The Launch Date of the Oculus-ASR Satellite is Unknown."]
[7.729029655456543, 8.822663307189941, "The SNR of the Imager Satellite Instrument is PAN: \u226548 dB, MS: \u226548 dB."]
[6.137906551361084, 5.9657673835754395, "The Ground Resolution (Spotlight mode) of the XSAR SAR is Less than 1 m."]
[9.456395149230957, 0.875562310218811, "The Mission Duration of the LLITED Spacecraft is One year."]
[6.902915954589844, 0.7030068635940552, "The Re-entry Date of the SENSE Satellites Satellite is May 4, 2015."]
[11.333197593688965, 6.728503704071045, "The Operation Mode of the IXAE X-ray Astronomy Experiment is Pointed mode observations."]
[3.8520097732543945, 4.402298450469971, "The Microcontroller of the OBC On Board Computer is ARM7."]
[3.5983877182006836, 5.952241897583008, "The Data Consumption of the EAN Connectivity System is 150 MB."]
[5.345170497894287, 2.6226909160614014, "The Development Workshop of the UNISAT Satellite is 5th Annual CubeSat Developers' Workshop."]
[7.175277233123779, 1.1031099557876587, "The Operational Date of the Scanning Sky Monitor (SSM) Payload is October 12th, 2015."]
[5.654488563537598, 3.3063018321990967, "The Mission of the IOV (In-Orbit Verification) Payload Payload is Developing system capability for communications payloads on small geostationary satellites."]
[6.183773517608643, 8.178175926208496, "The Bandwidth of the MWR Radiometer is 1 GHz."]
[4.809678077697754, 1.985238790512085, "The Number of Gyroscopes of the SloshSat Satellite is 3."]
[5.9461140632629395, 1.853287696838379, "The Launch Vehicle of the Aditya-L1 Satellite is PSLV-XL."]
[9.55449390411377, 0.5148118734359741, "The Mission Design Life of the Spacecraft Bus (Avionics Module=AM) Bus is 12 months."]
[9.247186660766602, 7.8437957763671875, "The Detector Temperature Range of the MSU-E Multispectral Scanner is -30 to -50\u00baC."]
[4.826105117797852, 6.09423303604126, "The LO Precision of the Satellite Device Unknown is 50 MHz."]
[5.6174774169921875, 1.515808343887329, "The Location of the Pre-CHUVA Field Campaign is Alc\u00e2ntara Launching Center in northeastern Brazil."]
[9.203672409057617, 4.111487865447998, "The Platform Size of the Satellite Satellite is 2.26 m x 1.9 m x 2.53 m."]
[9.479226112365723, 0.5568280220031738, "The Lifetime of the MTG-S satellite Satellite is Around 8.5 years."]
[6.046449661254883, 4.386178493499756, "The Data Access of the Twinkle Spaceborne Telescope is Exclusive access, via encrypted transfer, to the data within days of the observation."]
[13.118295669555664, 4.052199363708496, "The Data Set of the Gaia Satellite is Third."]
[9.250746726989746, 6.032919883728027, "The Error (RMS) of the Pitch momentum wheel Actuator is <0.001 mNms."]
[5.073368072509766, 6.066201210021973, "The Frequency L1 of the GPS receiver Receiver is 1575.42 MHz."]
[6.692771911621094, 3.6034398078918457, "The Operator of the MANTIS Satellite is Open Cosmos."]
[5.445387363433838, 4.728579998016357, "The Unknown of the Argos-3 Data Collection and Location System is Unknown."]
[8.82181167602539, 6.505988121032715, "The Ion Composition of the Plasma Sheet Space Phenomenon is Mainly H."]
[8.397110939025879, 6.535550594329834, "The Frequency Range of Shaker Tests of the Boom Structure is 9-300 Hz."]
[7.238257884979248, 4.866311550140381, "The Air Pollution Observation of the GOSAT Satellite is December 2016."]
[6.772570610046387, 2.174294948577881, "The URL of the GPM Core Satellite is http://www.spaceflight101.com/gpm-core-mission-updates.html."]
[11.766898155212402, 4.63123083114624, "The Distance from Milky Way of the Andromeda Galaxy is 2.5 million light-years."]
[4.004620552062988, 6.4059624671936035, "The Uplink Modulation of the Iris Radio Communication Device is BPSK."]
[11.706221580505371, 2.5941221714019775, "The Primary Diameter of the Didymos Binary System is 780 m."]
[8.034886360168457, 4.109383583068848, "The Freeboard Definition of the A-68A Iceberg is The height of the ice above the sea surface."]
[4.997626781463623, 4.926826000213623, "The Repetition Rate of the Fixed Platforms Ground Segment is 200 seconds."]
[8.395193099975586, 5.209733963012695, "The On-Ground Postprocessing Requirements of the Satellite Spacecraft is < 5 cm 3D rms."]
[6.765656471252441, 2.742483139038086, "The URL of the SCD-2 Satellite is http://www.inpe.br/programas/mecb/ingl/satellite/scd2/scd2.htm."]
[7.418255805969238, 1.0490583181381226, "The Product Specification Date of the Planet Imagery Satellite Imagery is April 2017."]
[7.714556694030762, 1.0127313137054443, "The Application Date of the Sentinel-5P Satellite is 18 September 2020."]
[6.3323540687561035, 7.199622631072998, "The Data Processing of the Delay/Doppler Altimeter Altimeter is Unknown."]
[7.655545711517334, 0.47431057691574097, "The Launch Date of the Meteor-3-1 Satellite is 24.10.1985."]
[7.785787105560303, 10.839632987976074, "The Data Quantization of the AATSR Instrument is 12 bit."]
[9.7805814743042, 7.160287857055664, "The Temperature of the Infinity-shaped loop Gas and Dust Formation is 15 degrees above absolute zero."]
[6.9743242263793945, 1.0552119016647339, "The Debut Date of the Opti-SAR Satellite is Unknown."]
[7.726012229919434, 13.574390411376953, "The Resolution \u0394\u03bb (0.05\u00ba slit) of the SPIM3 Spectrometer is 1.5 nm."]
[8.13524341583252, 1.1998430490493774, "The Date of the Seroja Slams Australia Image is 13 April 2021."]
[7.523961544036865, 5.195193290710449, "The Cloud Albedo Measurement of the AIM Satellite is Yes."]
[5.451687335968018, 6.090985298156738, "The Location of the GPS patch antenna Antenna is Wake surface of the satellite."]
[6.236540794372559, 9.0878267288208, "The Volume of the Herley MD2000C-1 Transponder Module is 13.8 cm3."]
[8.423473358154297, 6.623432636260986, "The Mounting of the MFI Magnetometer is 12 m radial boom."]
[4.899097442626953, 5.815770149230957, "The Purpose of the FLexRX Flexible Receiver is In-orbit test, demonstration, and qualification of a product."]
[6.699354648590088, 1.2887052297592163, "The Satellite Launch Date of the Capella Space And Rocket Lab Companies is Not Provided."]
[8.40272045135498, 7.615322113037109, "The Usage of the Tiny Ionospheric Photometer (TIP) Instrument is Not provided."]
[9.594871520996094, -0.9039360284805298, "The Launch Date of the JL-1-GF03D Microsatellite is 03 July 2021."]
[8.293558120727539, 10.022675514221191, "The Pixel Pitch of the MS Bands Detector Line Arrays is 52 \u00b5m."]
[11.711155891418457, 7.514957427978516, "The Ovenized Crystal USO Stability of the DSAC Demonstration Unit is Between 1 \u2013 100 seconds."]
[7.956640720367432, 8.863577842712402, "The Temperature Derivation Samples of the Instrument Spectrometer is 20 samples per spectrum."]
[6.050803184509277, 3.510255813598633, "The Developer of the Sentinel-5 Instrument is ESA."]
[9.076882362365723, 1.1569815874099731, "The Mission Extension Period of the Aura spacecraft Satellite is Ongoing."]
[3.6756703853607178, 3.513057231903076, "The Manufacturer of the CICERO-4 Satellite is Tyvak Nanosatellite Systems."]
[8.815877914428711, 8.599065780639648, "The Along-Track of the WAOSS-B Sensor is \u00b125\u00b0."]
[8.120084762573242, 4.060060977935791, "The Resolution of the Pleiades-1A Satellite is 50 cm."]
[7.978888988494873, 4.859889984130859, "The Tracking Targets of the Hexapod Tracking Device is Sun and Moon."]
[7.351889610290527, 4.6210713386535645, "The Instruments of the Almaz-1B Satellite is 2 Ekor-A, a 4-band optical imager, etc.."]
[5.650271415710449, 9.134637832641602, "The Output Power of the Instrument Power Unit Power Converter is 463 W."]
[7.6451096534729, 6.558279514312744, "The Required Precision of the O3 Profile Satellite Instrument is FT (ppbv)."]
[10.178681373596191, 5.626195907592773, "The Heaters Addition of the Valves Spacecraft Component is Under Consideration."]
[6.987730026245117, 4.5762786865234375, "The Imaging Modes of the SPOT satellite constellation Satellite Constellation is Multispectral and panchromatic."]
[3.7240352630615234, 6.196819305419922, "The Individual Subchannel Data Rate of the Optical Downlink Communication System is 38.55Mbit/s."]
[5.816831111907959, 1.9434478282928467, "The Launch Location of the Orbital ATK Launch Provider is Wallops Flight Facility in Virginia."]
[11.4271821975708, -1.320300817489624, "The Mass of the TechEdSat Satellite is 1.2 kg."]
[5.914909362792969, 6.193849563598633, "The SAR Payload Imaging Time of the RCM Satellite is 12 minutes per orbit."]
[4.052794933319092, 4.526191711425781, "The Interface of the Personal Computer Computer is USB."]
[4.986301898956299, 2.127143144607544, "The Inter-satellite Links of the Iridium PRIME Satellite Platform is 4."]
[11.751810073852539, -1.0915132761001587, "The Client Mass of the ELSA-d Mission is ~17 kg."]
[7.247580528259277, 5.555942535400391, "The Effect on Pteropods of the Ocean Acidification Environmental Phenomenon is Shell damage has been observed."]
[9.033945083618164, 5.170567512512207, "The Attitude Control of the GFO Satellite is Three-axis stabilized."]
[11.532964706420898, 4.450283050537109, "The Debris Disk of the AU Microscopii Star is Yes."]
[9.224729537963867, 8.299908638000488, "The URL of the SIXS Spectrometer is http://www.cosmos.esa.int/web/bepicolombo/sixs."]
[8.291027069091797, 6.3220133781433105, "The Required Spacecraft Stability of the Pushbroom Sensor is High."]
[9.78372859954834, 8.005576133728027, "The Energy Range of the GRS Gamma-Ray Spectrometer is 300 keV - 9 MeV."]
[7.5469441413879395, 1.3186413049697876, "The Date of the JAXA Earth Observation Missions Workshop is March 8, 2013."]
[6.992804527282715, 7.6738152503967285, "The Global Coverage of the HARP-2 Polarimeter is 2 days."]
[9.44785213470459, 9.244734764099121, "The Pre-Flight Performance Characterization of the Medium-sized Aperture Camera Camera is Unknown."]
[6.293392181396484, 6.902586460113525, "The Frequency of the AltiKa Altimeter is 35.75 GHz."]
[5.9159345626831055, 1.3697798252105713, "The Launch Manifest of the Ariane Launch Vehicle is Unknown."]
[9.800782203674316, 7.789956092834473, "The Energy Measurement Range for Protons of the Telescope 2 Telescope is 0.8-4 MeV."]
[12.028512001037598, 3.143831253051758, "The Lunar Orbit Inclination of the Chang'e-1 Satellite is 90\u00ba."]
[5.242690086364746, 3.1237306594848633, "The Project Management of the Communication subsystem Satellite Subsystem is Kagoshima University Soka University, Akita University."]
[6.473602771759033, 5.203022480010986, "The Scintillation Climatology Model of the C/NOFS Satellite is Improve scintillation climatology model."]
[6.380502700805664, 3.6089706420898438, "The Data Processing Center Lead of the INCUS Satellite is Phil Partain."]
[8.791653633117676, 1.6178200244903564, "The Mission Expansion Date of the Juno Spacecraft is 13 January 2021."]
[3.199338912963867, 6.109824180603027, "The Frequency Range of the APL\u2019s Frontier radio Radio is Wide range of frequencies."]
[5.860812187194824, 6.246958255767822, "The Number of Radar Beams of the COSI SAR Mission is 50."]
[3.352257013320923, 4.891851902008057, "The Power of the Spacecraft 406 MHz Processor Processor is 33 W."]
[11.745978355407715, -1.053737759590149, "The Payload Mass of the Heinrich Hertz Satellite is 435 kg."]
[8.348990440368652, 2.119868040084839, "The Plasma Instrument of the Voyager 2 Spacecraft is Will provide the first-ever plasma measurements of the interstellar medium."]
[6.154433250427246, 3.742197036743164, "The Autonomy of the ESEX Satellite is Somewhat autonomous."]
[1.9670168161392212, 3.839571714401245, "The Solar Cells of the GNB Satellite is Up to six triple-junction solar cells on each face."]
[3.8500025272369385, 2.3348982334136963, "The CubeSat Size of the MiRaTA Satellite is 3U."]
[7.534453868865967, 7.900594711303711, "The Accuracy of the CERES Instrument is 0.3 Wm -2  sr -1."]
[7.451536655426025, 7.447957992553711, "The Image Credit of the OMI Instrument is KNMI."]
[11.351694107055664, 6.724701881408691, "The Number of X-ray detector arrays of the IXPE observatory X-ray Observatory is 3."]
[7.3972907066345215, 2.353792667388916, "The URL of the Emirates Mars Mission (Hope) Satellite is https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=EMM-HOPE."]
[7.77464485168457, 8.98967170715332, "The Interference filter - Wavelength of the Instrument Sensor is 777.4 nm."]
[7.517590522766113, 2.296511650085449, "The Utilization of the ICI-11 Radiometer is Quasi-window, cirrus clouds, cloud ice water path."]
[3.812775135040283, 5.608094215393066, "The Data Bus Speed of the Spacecraft Satellite is 1 Mbit/s."]
[8.427863121032715, 4.510370254516602, "The Ground Sampling Distance of the TET-1 Satellite is 160 m."]
[11.989404678344727, 4.417069911956787, "The Image Release Date of the Crab Nebula Nebula is May 10, 2017."]
[10.290278434753418, 3.0404324531555176, "The Orbit Altitude of the Monitor-E Spacecraft is 540 km."]
[7.508452892303467, -0.10814107209444046, "The Launch Date of the Kounotori Spacecraft is August 19, 2015."]
[8.089730262756348, 5.243215560913086, "The Orbit Determination Accuracy of the LEO Satellites Satellite is Sub-decimeter."]
[6.714285373687744, 3.912781238555908, "The Purpose of the Proposed Constellations Satellite Constellations is Enhance Arctic weather observations."]
[11.685869216918945, -1.2196242809295654, "The Mass of the OceanSat-2 Satellite is 970 kg."]
[10.10466480255127, 3.9614980220794678, "The Orbit Raise Rate of the LightSail-2 Spacecraft is Several hundred meters per day."]
[7.310140132904053, 3.809223175048828, "The Image Capture of the Worldview-4 Satellite is SpaceX's first stage."]
[7.110116958618164, 2.269181489944458, "The URL of the Shuttle Radar Topography Mission Satellite Mission is http://www.shuttlepresskit.com/sts-99/payload57.htm."]
[9.307167053222656, 0.5382296442985535, "The Orbit Decay Time of the MicroMAS-1 Satellite is Within the required 25 year time period."]
[11.822653770446777, -1.1194102764129639, "The Launch Mass of the Spacecraft Satellite is 2040 kg."]
[4.589540481567383, 5.528073787689209, "The Data Path of the Antenna System Communication System is Primary path for L1b data from WCDAS to NSOF."]
[7.024520397186279, 9.799148559570312, "The Wavelength Range of the Band No 6 Spectral Band is 11.5 \u00b1 0.50 - 12.5 \u00b1 0.50 \u00b5m."]
[10.264739036560059, 4.901938438415527, "The Fuel of the Propulsion System Satellite Component is Green monopropellant fuel blend based on ADN (Ammonium Dinitramide)."]
[8.764542579650879, 3.399390935897827, "The Relevance of the MinXSS mission Satellite is NSF Division of Atmospheric and Geospace Sciences (AGS)."]
[7.357773303985596, 5.7499895095825195, "The Temperature of the Japan Current Ocean Current is High."]
[7.391470909118652, 7.274603366851807, "The Manufacturer of the COWVR Radiometer is NASA\u2019s Jet Propulsion Laboratory."]
[7.92374849319458, 4.464147090911865, "The SWIR Off-nadir Resolution of the WorldView-3 Satellite is 4.1 m."]
[5.377771854400635, 3.8477609157562256, "The Produces of the Services component Component is Information services in response to European policy priorities in environment and security."]
[8.441329956054688, 8.476432800292969, "The Number of Filter Windows of the Filter Wheel Optics Subsystem is 18."]
[11.749673843383789, -1.064327597618103, "The Printed Circuit Board Mass of the Sprite Tiny Spacecraft is A few grams."]
[9.346768379211426, 2.787559986114502, "The Impact Speed of the DART Spacecraft is Around 24,000 km/h."]
[8.551356315612793, 10.646126747131348, "The Power Consumption of the FLIR Boson camera Thermal Imaging Camera is Low."]
[4.31508731842041, 6.2221574783325195, "The Bandwidth of the Dual-channel Receiver Unit (DRU) Receiver is Variable."]
[8.628839492797852, 4.208157062530518, "The Design and Test of the BRITE Constellation Space Telescope Telescope is Wide Field, High Resolution, Low Noise."]
[8.319960594177246, 5.43637228012085, "The Orbit Reconstruction Accuracy of the GBOT Ground Based Orbit Tracking is 150 m in position and 2.5 mm/s in motion."]
[8.826264381408691, 5.276800632476807, "The Attitude Determination of the BRITE spacecraft Satellite is 10 arcseconds."]
[8.811406135559082, 7.023645401000977, "The Moisture Sensors per Site of the Sensor Node Data Collection System is 3."]
[7.059186935424805, 5.353074073791504, "The Data Uses of the Aeolus Satellite is Predicting the weather, improving climate models, tracking events in near-realtime."]
[6.107285022735596, 3.305293321609497, "The Tracking Support of the ESA Organization is Essential to Chinese mission."]
[7.253952980041504, 1.5110418796539307, "The Publication Date of the Cluster and Phoenix Missions Satellite Missions is 1997."]
[10.431666374206543, 4.729776859283447, "The Operating Hours of the Electric Thruster Thruster is More than 1000."]
[6.965001106262207, 4.6817121505737305, "The Focus of the RECCAP-2 Satellite Mission is Global stocktake and tracking towards net zero emissions."]
[7.835846900939941, 6.985298156738281, "The Unknown of the SUSIM Experiment is Unknown."]
[5.108911037445068, 1.86564040184021, "The Number of Scientists and Engineers of the ASTRO-H Mission is 266."]
[7.837482929229736, 8.607248306274414, "The Instantaneous spectral coverage of the Spectrometer Instrument is 2.37 km/s."]
[7.308141231536865, 2.9476802349090576, "The Installation of the MSPR-2 Rack is Already installed to Kibo."]
[8.629905700683594, 1.4776325225830078, "The Launch Date of the Juno Spacecraft is Aug. 5, 2011."]
[10.15657901763916, 6.73214054107666, "The Active Temperature Control of the SVM Service Module is Heaters controlled by thermostats."]
[10.273958206176758, 6.842933654785156, "The Kapton Heaters of the Thermal Management Subsystem Thermal Management System is Multiple."]
[8.048933982849121, 8.659586906433105, "The Spectral Resolution of the FTS Interferometer Interferometer is <0.028, 0.056, 0.11, 0.55 cm -1."]
[6.836556911468506, 2.727235794067383, "The Operational Status of the Carbonite-2 Satellite is Operational."]
[9.994287490844727, 2.8554916381835938, "The Operational Orbit Altitude of the OneWeb satellites Satellites is 1,200 km."]
[7.967230796813965, 8.242186546325684, "The Designers of the CHRIS Imaging Spectrometer is M. A. Cutter, D. R. Lobb."]
[5.390289306640625, 6.048446178436279, "The Antenna Composition of the SAOCOM-1A Satellite is 140 smaller antennas."]
[8.782204627990723, 10.335665702819824, "The Signal-to-Noise Ratio of the GOCI-II CMOS Imaging Sensor CMOS Imaging Sensor is Not provided."]
[9.290205001831055, 0.8067061305046082, "The Years in Orbit of the Landsat 7 Satellite is 20 Years."]
[7.961421489715576, 9.884303092956543, "The Channels of the FCI Optical Imager is 16."]
[6.113063812255859, 6.517465114593506, "The Operating Modes of the SRAL SAR Radar Altimeter is Conventional radar-altimeter mode, advanced SAR mode."]
[6.766097545623779, 3.327910900115967, "The Launch Agency of the ERG (Arase) spacecraft Satellite is JAXA (Japan Aerospace Exploration Agency)."]
[6.862974166870117, 3.187135934829712, "The Operational Status of the CDH and EPS subsystems Satellite Subsystems is Always ON."]
[2.0573432445526123, 4.38090181350708, "The Topology of the Power Subsystem Subsystem is DET (Direct Energy Transfer)."]
[8.21912670135498, 10.454870223999023, "The Purpose of the TDI Signal Processing Technique is Boosting object signal-to-noise ratio (SNR) by coherently adding the outputs of detectors aligned in the scan direction of the sensor."]
[9.177741050720215, -0.6229596734046936, "The Launch Date to ISS of the Flock 1a Nanosatellites is January 9, 2014."]
[6.682100772857666, 0.6620713472366333, "The Loss Date of the SEOSAT-Ingenio Satellite is 17 November 2020."]
[7.345991134643555, 8.63131332397461, "The Sampling Distance of the HIRS/4 Infrared Sounder is 18 km."]
[9.463784217834473, 8.799599647521973, "The Radiometric Linearity of the Telescope Optical Instrument is >95%."]
[9.687015533447266, 7.039003849029541, "The Temperature of the Verkhoyansk Town is 38\u00b0C."]
[6.9384684562683105, 3.535463809967041, "The Development Status of the GeoXO Satellite System is In progress."]
[5.087799549102783, 7.588417053222656, "The Data Rate of the DUST sensor Cosmic Dust Sensor is 8 bit/s."]
[8.494085311889648, 1.9203811883926392, "The Observation Date of the Herschel Space Observatory Space Observatory is September 24, 2018."]
[10.287759780883789, 6.889779567718506, "The Atomic Clock Panel Temperature Control of the Thermal Control Subsystem Thermal Control is Within 0.4\u00ba C."]
[2.127734899520874, 4.162583827972412, "The Solar Array Power of the UK-DMC-2 Satellite is 65 W at AM0 and 25\u00baC."]
[2.254521131515503, 6.498945713043213, "The Latency of the ATL04 Calibrated Backscatter Profiles Data is 21 days."]
[6.777440071105957, 1.1718733310699463, "The Conference Date of the GPS Receivers Receiver is August 13-16 2007."]
[7.038538932800293, 1.402388572692871, "The Conference Presentation Date of the Imaging System Satellite System is Sept. 15-18, 2015."]
[6.371781826019287, 8.538060188293457, "The Spectral range of the MWRI Microwave Radiation Imager is 10.65-150 GHz."]
[7.9217963218688965, 5.910319805145264, "The Execution Location of the Image acquisition and HSI calibration Task is Anywhere on the satellite orbit."]
[7.087919235229492, 2.7886199951171875, "The Funding of the SPOT-6 Satellite is Government funding or pre-sales agreements."]
[10.016162872314453, 3.0949413776397705, "The Ground Track of the Orbit Satellite Orbit is \u00b1 2 km."]
[10.20982551574707, 5.046248912811279, "The Propellant of the Cold Gas System Attitude and Orbit Control Subsystem is Nitrogen."]
[9.273575782775879, -0.5695586800575256, "The Conference Date of the CanX-4 & CanX-5 Nanosatellites is April 25-27, 2006."]
[7.546538352966309, 4.9094696044921875, "The Stray Light of the GHGSat-D Satellite is Up to 5%."]
[9.613860130310059, 6.0077290534973145, "The Proportional Control of the ADCS Attitude Determination and Control System is Magnetic field value or sun vector error."]
[5.3834733963012695, 4.096673011779785, "The Ground Stations of the Colony I Satellite is Melbourne, Florida, and Fort Huachuca, Arizona."]
[3.854266405105591, 6.654313564300537, "The Downlink Frequency of the DRT Data Relay Transponder is 4506.05 MHz."]
[7.460408687591553, 3.7672507762908936, "The Platform of the InnoSat Satellite is Mesospheric Tomography and Spectroscopy."]
[7.543573379516602, 4.800904750823975, "The Imaging Subject of the PROBA-V Satellite is Drakensberg mountains."]
[8.099839210510254, 7.808556079864502, "The Magnetic Field Tilt of the MGF Instrument is Up to 2\u00ba or 3\u00ba."]
[6.444638252258301, 2.9484593868255615, "The Producing Team of the Visualization Product is 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."]
[9.4816255569458, 0.5952466726303101, "The Operating Lifetime of the SPOT-6 Satellite is 10 years."]
[8.830074310302734, 7.891351699829102, "The Principle of Operation of the INMS sensor Ion Mass Spectrometer is Neutral particles are first ionized with compact thermionic filament ionizer. Post acceleration by voltage V gives all ions same energy E=qV, much greater than initial energy dispersions dE. Thus, the ions are ordered in velocity according to their mass o."]
[7.375593662261963, 6.730648040771484, "The Image Credit of the MODIS Instrument is NASA Earth Observatory image by Lauren Dauphin."]
[9.726744651794434, 1.1354886293411255, "The Operational Autonomy of the COSMO-SkyMed spacecraft Satellite is 24 hours."]
[6.183504581451416, 0.7603123188018799, "The Launch Time of the Iridium-5 Satellite Launch is 7:17 am PDT (14:17 UTC)."]
[9.52810287475586, 0.5232771039009094, "The Design Life of the SARAL spacecraft Satellite is 5 years."]
[4.0095014572143555, 5.559638977050781, "The Uplink of the STRaND-1 Satellite is Not optimal during the first two weeks."]
[6.227362155914307, 8.504867553710938, "The Feedhorns of the MIS Instrument Microwave Radiometer is 12."]
[6.489946365356445, 1.339308738708496, "The Launch Date of the G\u00f6kt\u00fcrk-1 Satellite is 2015."]
[8.553316116333008, 6.187073707580566, "The Boom Length of the CHAMP Satellite is 4 m."]
[7.60865592956543, 9.022139549255371, "The Resolving Power of the O2 A-band channel Spectrometer is > 17,000."]
[11.14316177368164, 4.2483391761779785, "The Heat Emission of the Magma Ocean Planets Planets is Enough to be observed with the next generation of infrared telescopes."]
[8.579980850219727, 9.419412612915039, "The Sensitivity of the NIRSpec MIRI Optical Instrument is 5000 nJy (21 \u03bcm, \u03c4 i =10,000 s, and \u03bb/\u0394\u03bb = 4.2)."]
[9.031737327575684, 9.722003936767578, "The Experiment of the Toshiba Co. Organization is Vision data processing experiment."]
[9.044703483581543, 10.653656005859375, "The Size of the MSU-50 Camera is 210 x 200 x 140 mm."]
[9.675055503845215, 7.708881855010986, "The Neutrino Energy of the Glashow Resonance Phenomenon is 6.3 PeV."]
[9.676411628723145, 9.516388893127441, "The Mass of the SAGE-III Instrumentation is Unknown."]
[5.803889751434326, 2.8311824798583984, "The Designers of the Small Satellite Platform Satellite Platform is F. Dannemann, M. Jetzschmann."]
[4.966630935668945, 5.591639518737793, "The Location of the Transponder Device is Australia."]
[5.984489440917969, 0.6955221891403198, "The Return Date of the NRCSD CubeSat Deployer is Mid-September."]
[5.292827129364014, 2.3835997581481934, "The Operators of the SAPPHIRE Satellite is Students at the USNA (US Naval Academy) and at SCU (Santa Clara University)."]
[8.887240409851074, 3.3566932678222656, "The Mission Unique Feature of the EQUULEUS Satellite is Measure the LIF at the far side of the moon from EML2 and control trajectory within the Sun-Earth-Moon region."]
[9.783798217773438, 8.819785118103027, "The Design of the Herschel Telescope Telescope is Classic Cassegrain with a 3.5 m primary mirror."]
[7.3924760818481445, 3.9894542694091797, "The AOCS of the MERLIN Satellite is Improved."]
[6.847020149230957, 2.6397979259490967, "The Quote of the Ericson Unknown is \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."]
[6.695561408996582, 0.533765971660614, "The Launch Date of the STPSat-3 Satellite is November 20, 2013."]
[10.96140193939209, 3.3947956562042236, "The Planned Trajectory Correction Maneuvers of the Juno spacecraft Spacecraft is 13."]
[9.338692665100098, 3.7638776302337646, "The Size of the DART Spacecraft is About the size of a small car."]
[6.258942127227783, 1.9567980766296387, "The Reentry Outcome of the InflateSail Satellite is Destroyed."]
[6.689299583435059, 7.162407398223877, "The Instrument Status of the GEDI Lidar is Operational."]
[5.148489952087402, 3.281928062438965, "The Objective of the PSat-2 CubeSat is 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."]
[9.881122589111328, 4.058220386505127, "The Attitude Controller Design Presentation Date of the IKAROS Solar Sail Demonstrator is July 20-22, 2010."]
[3.0095410346984863, 6.760610580444336, "The Electrical Power of the STX-01 S-band Transmitter/Transceiver is 6 W."]
[10.887455940246582, 5.717614650726318, "The Publication Date of the Kappa Scheme Flare Prediction Method is July 31, 2020."]
[7.647036552429199, 9.935506820678711, "The Unknown of the JSS Multispectral Imagers Imaging System is Unknown."]
[7.735128402709961, 7.997010231018066, "The Measurement Types of the MSX/UVISI Instrument is Refraction and Extinction."]
[6.7658586502075195, 2.225783586502075, "The Status of the Teledesic Program is Cancelled."]
[8.946487426757812, 10.637650489807129, "The Spatial Resolution of the CCD Camera Optical Device is 30 m."]
[10.175629615783691, 4.955214500427246, "The Apogee Motor Type of the Propulsion Subsystem Satellite is Bipropellant liquid."]
[10.261316299438477, 3.620896100997925, "The Orbit Type of the XMM-Newton Satellite is Highly eccentric."]
[7.824876308441162, 10.778575897216797, "The Data Quantization of the Visible Spectral Band Spectral Band is 6 bit."]
[3.982529878616333, 6.4644904136657715, "The Modulation of the RF Communications Transmitter is BPSK."]
[3.20930814743042, 4.914262294769287, "The External RAM of the OBC Onboard Data Handling is 524 kB."]
[9.73737907409668, 8.088794708251953, "The Effective Area of the GMOD Detector is Function of off-axis angle and azimuth of the source GRB."]
[10.067906379699707, 5.013674736022949, "The Gas Storage Capability of the Propulsion System Satellite Component is Until it is used for thrusting."]
[7.713989734649658, 10.22035026550293, "The Instrument Power of the SEVIRI Imager is 123 W."]
[7.082912445068359, 4.226544380187988, "The Measurement Category of the SPOT-5 Satellite is Multi-purpose imagery (ocean), Multi-purpose imagery (land), Vegetation, Albedo and reflectance, Landscape topography, Sea ice cover, edge and thickness, Ice sheet topography."]
[5.47744607925415, 3.87384033203125, "The Location of the ISSAC SOC Space Operations Center is UND."]
[7.856950283050537, 4.603821277618408, "The Vertical Resolutions of the SciSat-1/ACE Satellite is One of the world\u2019s highest."]
[11.607547760009766, -0.7801151275634766, "The Cube Mass of the LISA Pathfinder Spacecraft is 2 kg."]
[8.343428611755371, 7.257011890411377, "The Purpose of the FIELDS Instrument is Measure electric and magnetic fields in the Sun's atmosphere."]
[9.212516784667969, 3.2243545055389404, "The Orbit Type of the STARS spacecraft Satellite is Sun-synchronous near-circular orbit."]
[9.981910705566406, 4.189441680908203, "The Operation of the E-Sail Electric Solar Sail is Repelled charged plasmas found in space."]
[6.637065410614014, 2.4626052379608154, "The URL of the Eutelsat Quantum Satellite is https://www.eutelsat.com/en/news.html#/blog_posts/four-things-you-should-know-about-eutelsat-quantum-69078."]
[6.931994438171387, 3.562673568725586, "The Offices of the EROS-B Satellite is Limassol, Cyprus, and in Tel Aviv, Israel."]
[8.516413688659668, 9.308100700378418, "The Sensitivity of the NIRSpec MIRI Optical Instrument is 3.1 x 10 -20  Wm -2  (22.5 \u00b5m, \u03c4 i =10,000 s, R=1200)."]
[5.7558913230896, 6.68314266204834, "The Polarization of the Radar Radar is HH, VV, HV/VH."]
[9.73198413848877, 8.972249031066895, "The Primary Mirror Diameter of the WUPPE Spectrophotometer is 0.5 m."]
[8.464181900024414, 9.136187553405762, "The Band 3 of the R3 Sensor Sensor is CA."]
[9.716498374938965, 8.066888809204102, "The Sensitivity of the GMOD Detector is Simulated."]
[10.468807220458984, 2.894185781478882, "The Orbit Altitude of the Polar Scout 6U CubeSat Satellite is 575 km."]
[5.020259857177734, 9.23263931274414, "The Recording Date of the SEIS Seismometer is July 25, 2019."]
[9.420943260192871, 1.7791883945465088, "The Pass Frequency of the Satellite Orbit Type is 16 passes per day."]
[8.107447624206543, 4.313404083251953, "The Imager Stabilization Requirement of the ExoplanetSat Satellite is Same fraction of a pixel."]
[6.762541770935059, 7.533686637878418, "The Detector Size of the DIAL Instrument LIDAR is 200 \u00b5m."]
[7.7430524826049805, 10.28325366973877, "The Channels of the SEVIRI Imager is VIS 0.6 \u00b5m, VIS 0.8 \u00b5m, IR 1.6 \u00b5m, HRV (High Resolution Visible), IR 3.9 to IR 13.4 \u00b5m."]
[5.340652942657471, 2.6942782402038574, "The CubeSat Structure Manufacturer of the Iraz\u00fa CubeSat Satellite is Costa Rica."]
[6.119304180145264, 5.727952480316162, "The Function of the SGR-ReSI Interface Unit is Platform GNSS receiver."]
[8.570961952209473, 10.849639892578125, "The Dynamic Range of the Kodak KAI-11002 CCD CCD is 66 dB."]
[6.997570514678955, 0.5568997263908386, "The Launch Date of the Genesis-2 Satellite is June 28, 2007."]
[9.375150680541992, 5.018645286560059, "The Mirror Angle of the SUNSAT Satellite is 45\u00ba."]
[6.720576763153076, 7.799593925476074, "The Quantity of the PMDs Polarization Measurement Device is 2."]
[9.62540054321289, 3.885634183883667, "The Propellant Status of the CanX-5 Satellite is Very large fraction remaining."]
[4.775985240936279, 3.813967704772949, "The Support Program of the Maritime AI-NAV Program is Navigation Innovation and Support Program (NAVISP)."]
[8.96464729309082, 10.276567459106445, "The Unknown of the PMS Camera Camera is Unknown."]
[8.533047676086426, 7.189552307128906, "The Shaken but not disturbed of the Inertial Sensor Head Sensor is \"Inertial Sensor Head shaken but not disturbed,\" ESA, Dec. 12, 2013."]
[6.5274457931518555, 7.816110610961914, "The Output Energy of the InnoSlab amplifier Laser Amplifier is About 30 mJ."]
[9.19440746307373, 7.101204872131348, "The Function of the DLP Double Langmuir Probe is Surface cleaning."]
[7.623276710510254, 0.9139093160629272, "The Launch Date of the Foton Spacecraft is May 31, 2005."]
[8.189866065979004, 8.804091453552246, "The Field of View Length of the Spectrometer Spectrometer is ~0.0146 radians."]
[7.304413318634033, 1.3370758295059204, "The Advisory Group Call Date of the EarthCARE Mission is April 4, 2017."]
[5.455367088317871, 3.2397687435150146, "The Hardware Modification of the TBIRD Satellite is Modified for the extreme environment of space."]
[6.454756259918213, 4.2423014640808105, "The General Environmental Verification Specification of the Drag-free CubeSat Satellite is 14.1 g-rms for the lightest satellites."]
[4.253588676452637, 4.229422569274902, "The Development and Flight Results of the On-Board Computer Computer System is Unknown."]
[9.332914352416992, 1.0358902215957642, "The Mission Duration of the OPAL Satellite is > 9 months."]
[10.506049156188965, 8.249798774719238, "The Publication Date of the High Altitude Observatory white-light coronagraph Coronagraph is April 1977."]
[9.796236991882324, 8.390545845031738, "The Celestial Sphere Coverage of the Telescope Optical Instrument is 39.7% at any given time."]
[10.31982707977295, 3.116152286529541, "The Orbit Altitude of the Secondary Payloads Satellite is ~410 km."]
[10.050969123840332, 1.5191792249679565, "The Orbit Period of the ResourceSat-2A Satellite is 101.35 minutes."]
[3.8915655612945557, 5.963871955871582, "The Transmission Rates of the TT&C subsystem Satellite Subsystem is Uplink: 4 kbit/s, Downlink: Up to 500 kbit/s."]
[7.424525737762451, 2.1723504066467285, "The Development Status of the SMAP Satellite is Under development."]
[10.337061882019043, 2.969404458999634, "The Altitude Data Set of the GEOSAT Satellite is 5 cm orbits based on GRACE gravity model."]
[6.44027042388916, 2.720461368560791, "The Experiment Types of the OPS-SAT Satellite is Artificial Intelligence (AI), data compression, and even financial transactions."]
[10.051789283752441, 2.203287363052368, "The Orbit of the SkySat-16 to -18 Satellite is Sun-synchronous circular orbit with an altitude of 575 km, inclination of ~98\u00ba, LTDN (Local Time of Descending Node) of 10:30 hours."]
[10.31331729888916, 2.9819273948669434, "The Mission Altitude of the MicroSat-2a Satellite is 1125 km."]
[5.424233913421631, 3.0264952182769775, "The Avionics of the AstroSat-250 Satellite is Astrium AS250 new generation avionics."]
[9.413002967834473, 5.85350227355957, "The Type of the ACS Attitude Control Subsystem is Passive magnetic attitude control system."]
[7.516168117523193, 1.9137465953826904, "The Surface Velocities of the Wilkins Ice Shelf Ice Shelf is 1994\u201396 and between 2006 and 2010."]
[9.224982261657715, 5.4602460861206055, "The Control Systems of the ANUSat Satellite is Magnetic torquers."]
[6.650019645690918, 7.6605329513549805, "The Location of the Avionics Stack Device is Below the laser."]
[9.526067733764648, 3.6798512935638428, "The Previous Observations of the Lunar Flashlight Satellite is Surface reflectance variations measured by the LOLA 1064 nm laser altimeter and the ice-like reflectance spectra measured by M3."]
[6.937891006469727, -0.03662882372736931, "The End of Life Date of the MTSAT Satellite is 31 Dec 2018."]
[5.926417827606201, 3.3851349353790283, "The Coordination Responsibilities of the Executive Position is Coordination with EC and GSA, analysis of operational requirements, dissemination of joint information papers at IMO and IALA."]
[4.796118259429932, 0.8324565887451172, "The Contract Value of the Northrop Grumman Company is $692 million."]
[7.757009029388428, 1.029852271080017, "The Launch Date of the Sentinel-5P Satellite is October 2017."]
[3.4963996410369873, 4.592711448669434, "The Type of the COVE Payload Processor is Reconfigurable FPGA-Based."]
[8.224320411682129, 8.077162742614746, "The Publication Date of the Extreme UV spectroheliometer Spectroheliometer is April 1977."]
[8.685959815979004, 3.2618794441223145, "The Coverage of the Satellite GEO (Geostationary Earth Orbit) is Not global: observes only one region of globe."]
[7.108217716217041, 1.5161802768707275, "The Conference Date of the GMES-Sentinels System is April 25-30, 2010."]
[9.599990844726562, 5.947874069213867, "The Attitude Knowledge Error of the ADCS Attitude Determination & Control Subsystem is \u2264 29 \u00b5rad."]
[12.942862510681152, 4.843324661254883, "The Purpose of the IBEX Spacecraft is Examine how our heliosphere interacts with interstellar space."]
[8.588688850402832, 8.998814582824707, "The Resolution of the Photometer Optical Instrument is 26.52 arcsec/pixel."]
[6.641406536102295, 3.979645013809204, "The Ground Segment Chain of the Deimos-2 Satellite is Data processing chain."]
[2.6706998348236084, 5.417160511016846, "The Power Consumption of the AIM Reconfigurable Computing Hardware Device is 1.5 to 5 W."]
[7.428163528442383, 1.8043895959854126, "The Presentation Date of the Gravity Probe B Satellite is June 23-29, 1991."]
[1.2663397789001465, 4.119418621063232, "The Battery Type of the UK-DMC-2 Satellite is Li-ion battery."]
[7.771134376525879, 7.17779541015625, "The Developer of the TEMPO Instrument is Ball Aerospace."]
[8.781805038452148, 8.058917045593262, "The Radiation Monitoring of the SPA-1 Dosimeter Dosimeter is Depletion mode, p-channel RADFET from REM."]
[10.651835441589355, -1.1693181991577148, "The Mass of the NanoACE Satellite is 5.2 kg."]
[8.977837562561035, 2.5581459999084473, "The Observation Wavelengths of the Herschel Satellite is 70 \u00b5m (blue), 160 \u00b5m (green) and 250 \u00b5m (red)."]
[7.579102516174316, 0.4218924343585968, "The Launch Date of the Meteor-M-2 Satellite is 08 Jul 2014."]
[6.549075603485107, 4.12813138961792, "The Type of the VISION Instrument is CubeSat optical payload."]
[6.59029483795166, 1.1390726566314697, "The Commissioning Date of the PRISMA POD Facility is Fall of 2010."]
[4.774626731872559, 7.153860569000244, "The Dimensions of the RPU Receiver Processor Unit is 195 mm x 280 mm x 365 mm."]
[11.20641040802002, 4.263210773468018, "The Number of Stars Observed of the Kepler Telescope is Approximately 1,000."]
[6.960415840148926, 0.12928929924964905, "The Launch Date of the Satellite Vu\u2019s first satellite Satellite is June 2023."]
[11.642634391784668, 1.2601505517959595, "The Number of Checkouts of the EDM Lander is Three."]
[7.8824005126953125, 4.424992084503174, "The Planned Measurement Rate of the Claire Satellite is Double as of early 2017."]
[8.92628288269043, 8.490328788757324, "The Rotation of the Scan Assembly Assembly is 360\u00ba."]
[4.579010009765625, 5.776699066162109, "The Signal Bands of the BeiDou-3S Satellite is Legacy B1 signals, modernized signals in the L1, E5, and B3 band."]
[10.145854949951172, 4.014134407043457, "The Flyby Speed of the NEA Scout Solar Sail Technology Demonstration Spacecraft is Less than 100 feet [30 meters] per second."]
[8.441640853881836, 2.9499356746673584, "The Location of the Gateway Outpost is Orbiting the Moon."]
[6.850047588348389, 0.46425220370292664, "The End of Operations Date of the GEOS-1 Satellite is January 1968."]
[1.7434234619140625, 4.643678188323975, "The Size of the EPS Electrical Power Subsystem is 96 x 90 x 20 mm."]
[9.457818031311035, -0.7055019736289978, "The Deployment From of the DIWATA-1 Microsatellite is ISS Kibo."]
[1.7255820035934448, 4.228665828704834, "The Solar Arrays of the EPS Electrical Power Subsystem is 6."]
[6.619656562805176, 3.4721789360046387, "The Mission Type of the MOMS Satellite is EO."]
[4.0670390129089355, 4.815659046173096, "The Behavior of the Interfaces Communication is Nominally."]
[8.292037963867188, 7.437122344970703, "The Noise Level at 1 Hz of the Field Measurement Device Sensor is \u2264 10 pT Hz -1/2."]
[7.200645923614502, 5.450767517089844, "The Monitoring Method of the Ocean Acidification Environmental Phenomenon is Satellites."]
[9.170145034790039, 7.008930683135986, "The Purpose of the WISPR Wide-field Imager for Solar Probe is Study the solar wind."]
[8.36703109741211, 3.389274835586548, "The Global Absolute Height Error of the TanDEM-X Satellite is 0.9 m."]
[4.819375038146973, 1.058868408203125, "The Business Model of the Astrocast Satellite Manufacturer is Monthly subscription fee for every device connected."]
[6.518892765045166, 3.8920862674713135, "The Sensor Types of the EO ASI Satellite is SAR and hyperspectral."]
[6.94359016418457, 4.5492353439331055, "The Imaging Frequency Band of the ERS-1 Satellite is C."]
[4.18797492980957, 6.525663375854492, "The Uplink Frequency of the Astrodev Lithium 2 Radio RF Communication Device is 449.75 MHz."]
[7.967512130737305, 8.02743911743164, "The Current Detection Range of the MGF Instrument is 0.1 \u00b5Am-2 or stronger."]
[3.679863214492798, 6.0532755851745605, "The Data Rate of the Payload Downlink Communication System is 20 Mbit/s."]
[9.16633415222168, 8.38652229309082, "The Margin for Smear of the BAE Detector Detector is 473%."]
[6.091452121734619, 2.579538583755493, "The Payload of the SLS Rocket is Orion spacecraft, astronauts, and supplies."]
[8.342398643493652, 4.6189165115356445, "The Swath Width of the ALOS-4 Satellite is 200 km."]
[10.507925987243652, -1.0233386754989624, "The Mass of the UNISat-6 Microsatellite is 26 kg."]
[7.4204421043396, 3.245079278945923, "The Lunar gravity field detection of the Kaguya (SELENE) Satellite is Unknown."]
[2.008380174636841, 4.211895942687988, "The Maximum Electrical Power Production of the SAWs Solar Array Wings is 11.2 kW."]
[6.4383721351623535, 9.85278034210205, "The Instrument Mass of the ERIP Earth Remote-Sensing Imaging Package is 1.80 kg."]
[11.715445518493652, -0.8074107766151428, "The Platform Mass of the MERLIN Satellite is 260 kg."]
[8.265844345092773, 8.297677040100098, "The Temperature Stabilization of the UVNS Spectrometer is Better than 1oK during one orbit."]
[6.161287784576416, 3.169729709625244, "The Development Support Programs of the Galileo Second Generation Satellite System is ESA European Global Navigation Satellite System Evolutions Program (EGEP), EU's GNSS and Horizon 2020 HSNAV Programs."]
[4.970203399658203, 6.183272838592529, "The Frequency (MHz) of the GLONASS L5 OC Signal Carrier is 1176.45."]
[8.96590805053711, 9.808874130249023, "The Components of the PIC Device is Back-illuminated scene, projector, lenslets, PIC interferometers, detector, thermoelectric phase modulators, Fast-Steering Mirror, three-row mask."]
[8.052324295043945, 1.4115828275680542, "The First Data Release Date of the Solar Orbiter Satellite is September 30, 2020."]
[4.126192569732666, 5.846750736236572, "The RF Wideband Downlink of the QuickBird-2 Satellite is 320 Mbit/s."]
[10.028148651123047, 1.545515537261963, "The Period of the COMPASS-1 Satellite is 102 minutes."]
[4.236310958862305, 6.648554801940918, "The UHF Band Frequency of the RF Communications Communication Subsystem is 430 MHz."]
[9.412944793701172, 8.735589981079102, "The Design Basis of the OAP (Off-Axis Parabola) mirrors Optical System is COTS (Commercial Off-The-Shelf ) diamond-turned."]
[7.206083297729492, 3.3052480220794678, "The Duty Cycle Reduction of the NEOSSat Satellite is Modest."]
[6.725546836853027, 0.5356940031051636, "The Planned Launch Year of the ProSEDS Satellite is 2003."]
[9.775153160095215, 6.690757751464844, "The Attachment Method to Radiator of the Superelastic Springs Mechanical Component is Attached to the radiator with screws."]
[7.841694355010986, 3.975961446762085, "The Projected Quantity of the Artificial Objects Satellite is Double."]
[10.42934513092041, -1.0096684694290161, "The Magnetic-Gravitational Stabilization and One-Axis Orientation System Mass of the Microsatellite Satellite is 2.7 kg."]
[8.693879127502441, 10.210805892944336, "The Dark Current of the Image Sensor Imaging is 4 e- /s/pixel."]
[5.286171913146973, 4.181460380554199, "The Components of the MCS Mission Control Software is Database and associated programs."]
[6.078061580657959, 0.5534644722938538, "The Launch Date of the ALBus CubeSat Satellite is 16 December 2018."]
[5.367166996002197, 3.588197708129883, "The Technology Types of the CFESat Satellite is Supercomputer, power supply, antennas, booms, launch-vehicle separation system, lithium-ion batteries."]
[8.138350486755371, 4.948174476623535, "The Grasp of the HaloSat Satellite is 26 cm2deg2."]
[9.687882423400879, -0.6645246148109436, "The Payload Instruments of the Chibis-M Microsatellite is \"Thunderstorm\" and \"Wave Package\"."]
[4.80842924118042, 0.16431939601898193, "The OneWeb Business of the Hughes Company is More than $300 million."]
[5.848143577575684, 3.2104289531707764, "The Prime Contractor of the CHEOPS Satellite is Airbus in Spain."]
[9.822452545166016, 6.6574788093566895, "The Temperature Range of the ANUSat Satellite is 10\u00ba C \u2013 30\u00ba C."]
[9.329910278320312, 4.940937519073486, "The Spin Axis Tilt Angle of the Cluster spacecraft Satellite is 45\u00ba."]
[10.60275936126709, 3.5453381538391113, "The Speed of the Rosetta Spacecraft is 8.6 km/s."]
[7.236639499664307, 2.785478353500366, "The Operating Status of the SMOS mission Satellite Mission is Nominally."]
[11.733858108520508, -1.169176459312439, "The Mass of the Monitor-E Spacecraft is 700 kg."]
[4.714376926422119, 5.605547904968262, "The Communication of the GPM Core Satellite is S-band RF."]
[11.825939178466797, -1.1651276350021362, "The Launch Mass of the Resurs-DK1 Spacecraft is about 6570 kg."]
[6.043596267700195, 1.6709966659545898, "The Launch Site of the SkySat-16 to -18 Satellite is Cape Canaveral."]
[4.803958892822266, 4.405543327331543, "The Function of the Housekeeping Computer On Board Computer is Responsible for communications with the ground station and collecting satellite telemetry."]
[5.206396579742432, 5.460354328155518, "The Spectrum of the Lightspeed Satellite Constellation is Ka-band."]
[4.06982421875, 6.631136894226074, "The Capability of the LRO Mini-RF Transmitter Transmitter is Dual-band."]
[7.641372203826904, 1.5690641403198242, "The Session of the \"Report of the Committee on the Peaceful Uses of Outer Space Report is Sixty-second."]
[4.9850873947143555, 5.258701324462891, "The Radius of the Ground Station Coverage Ground Station is 2000 km."]
[11.799262046813965, 4.533635139465332, "The Observation Time of the Tycho Supernova Remnant is More than four centuries."]
[11.727560997009277, -1.0796414613723755, "The Mass of the Deimos-2 Satellite is 300 kg."]
[7.974610805511475, 9.907370567321777, "The Spatial Resolution at Nadir of the Imager Imaging System is 0.46 m GSD."]
[7.721244812011719, 0.7397861480712891, "The Scheduled Lift Off of the EM-1 Exploration Mission-1 is November 2018."]
[7.910325527191162, 1.2164058685302734, "The Eruption Date of the Calbuco volcano Volcano is April 22, 2015."]
[10.690155982971191, 5.2723708152771, "The Minimum Relative Distance of the CNAPS Propulsion System is 50 m."]
[3.2163147926330566, 6.116559982299805, "The Operation Environment of the Frontier Radio Telecommunications System is Very harsh environment."]
[11.559526443481445, 5.679267406463623, "The Continuum Spectrum of the GRS 1915+105 X-ray Binary with a Black Hole is Figure 6."]
[8.176114082336426, 10.509206771850586, "The Data Rate of the TDI Detector Detector is 700 Mbit/s per detector."]
[7.773010730743408, 0.3440623879432678, "The Year of the CryoVEx Campaign is 2003."]
[4.031217575073242, 2.3828554153442383, "The Size of the CubeSats Satellite is About the size of a boot box."]
[5.451624393463135, 1.8130426406860352, "The Constellation Size of the Kleos Space S.A. Company is Up to 20 clusters."]
[6.4670281410217285, 9.161165237426758, "The Size of the LCT instrument Instrument is 0.6 m x 0.6 m x 0.7 m."]
[9.308356285095215, 9.439607620239258, "The f/Number of the Custom design lens Lens is f/5."]
[9.93407917022705, 2.516636610031128, "The Planned Quantity of the Touch Downs/Sample Collections Maneuver is Three."]
[4.6629791259765625, 4.09730339050293, "The Designer of the Driver on/off IC Component is Santa Maria Design House."]
[9.187067031860352, 7.080740928649902, "The Operation Duration of the m-NLP system Langmuir Probe System is 10 years."]
[8.371641159057617, 0.6532001495361328, "The Telemetry Data of the Hitomi Satellite is Not Received."]
[8.687716484069824, 1.5138019323349, "The Update Date of the Juno Spacecraft is 11 December 2020."]
[10.13162899017334, 3.083042860031128, "The Orbit Altitude of the GeoCARB Satellite is Approximately 35,786 km above the equator."]
[4.82909631729126, 1.9909789562225342, "The Number of Maneuvers of the SkySat-3 Satellite is 13."]
[7.966745853424072, 6.962141513824463, "The Design Hypothesis of the Geometric Calibration System Calibration System is Thermoelastic distortions change slowly, smoothly and not a lot."]
[9.41843318939209, 1.8353559970855713, "The Retargeting Frequency of the Platform Satellite is Twice per orbit."]
[7.761610984802246, 1.6100083589553833, "The Phase B of the SMOS Satellite is 2002."]
[5.045180320739746, 5.95978307723999, "The Spectrum Observation of the CubeRRT Satellite is 1 GHz wide portion of the electromagnetic spectrum."]
[9.745495796203613, 3.103935480117798, "The Orbit Parameters of the GEOS-3 Satellite is 816 km x 850 km x 115.0\u00ba."]
[6.4076762199401855, 8.531320571899414, "The Swath Width of the RM-08 Passive Microwave Scanning Radiometer is 550 km."]
[5.330102920532227, 5.777947425842285, "The Antenna Version of the BlackJack GPS Instrument is 4-antenna."]
[8.77068042755127, 1.932904839515686, "The Suitability of the DarkCarb Mission is Well suited."]
[8.570209503173828, 8.683601379394531, "The Temporal Resolution of the EIS Sensor is 30 s."]
[9.167938232421875, 5.278502941131592, "The Objective of the Slew Mode Satellite Mode is 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."]
[5.727367877960205, 3.030540943145752, "The Prime Contractor of the Swarm Spacecraft Satellite is EADS Astrium GmbH, Friedrichshafen, Germany."]
[4.3403801918029785, 2.6667988300323486, "The Form Factor of the Ubotica CogniSAT-XE1TM CubeSat Board Satellite Device is PC/104."]
[7.6083784103393555, 0.9915928840637207, "The Launch Date of the Sentinel-1B Satellite is April 25, 2016."]
[5.591906547546387, 3.067511558532715, "The Closure Reason of the Factory Facility is Pandemic."]
[5.171572685241699, 4.8145036697387695, "The Location of the Ground Station Ground Station is Panska Ves (Czech Republic)."]
[6.99253511428833, -0.0626031830906868, "The End of Life Date of the NigeriaSat-X Satellite is 31 Dec 2021."]
[7.277925968170166, 4.323178291320801, "The Mission Purpose of the Tandem-L Satellite is Climate research and environmental monitoring."]
[6.920453071594238, 1.210608720779419, "The Presentation Date of the Small Satellites Satellite is Oct. 2-6, 2006."]
[6.654274940490723, 1.4568355083465576, "The Launch Date of the RapidEye Earth Observation Constellation is August 2008."]
[4.908263206481934, -3.2440314292907715, "The | of the P. Jonathan Gero Individual is Fred A. Best, Douglas P. Adler, Claire Pettersen, Henry E. Revercomb, P. Jonathan Gero, Joseph K. Taylor, Robert O. Knuteson, John H. Perepezko."]
[11.83230209350586, -1.2144867181777954, "The Launch Mass of the CartoSat-2D Satellite is 714 kg."]
[3.527207374572754, 2.5865254402160645, "The Array of the Spacecraft Satellite is 3 panel/Si with GaAs/articulating/5.25 m."]
[8.676950454711914, 3.208191156387329, "The Purpose of the GOCE Satellite is Measure the pull of Earth's gravity."]
[6.030571460723877, 9.58121395111084, "The Packaging Weight of the MRM Magnetometer is 1.6 kg."]
[7.180414199829102, 4.183815002441406, "The Sensor complement / remarks of the Meteor-3-1 Satellite is MR-2000M, MR-900B, IR, SM, RMK-2."]
[7.155539512634277, 6.980004787445068, "The Measurement Capabilities of the ALADIN Instrument is 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."]
[13.114021301269531, 4.058659076690674, "The Unique Capability of the Gaia Satellite Mission is Performing the most precise astrometric survey ever realized."]
[9.896184921264648, 4.085941314697266, "The Subsystem of the NanoSail-D2 Satellite is Sail."]
[7.804770469665527, 9.10993766784668, "The Spectral Range of the TIR Thermal Infrared region is 8.4-8.5, 10.3-11.3, 11.5-12.5 \u00b5m."]
[11.324042320251465, 6.712096214294434, "The Observation Mode of the IXPE Satellite is Pointed viewing of known X-ray sources."]
[6.666938781738281, 3.8034915924072266, "The Status of the RESOURCESAT-2 Satellite is Functioning Satisfactorily."]
[5.823265075683594, 4.8195977210998535, "The Role of the MONTE Software is Independent check of GIPSY-OASIS results."]
[9.05013370513916, 10.254914283752441, "The Detector Array Temperature of the LWIR Camera Camera is 65 K."]
[5.635361671447754, 1.0544630289077759, "The Deployment Services Start Date of the NanoRacks LLC Company is October 2012."]
[9.870382308959961, 4.3660993576049805, "The Attitude Stabilization Method of the NanoSail-D2 Satellite is 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 a."]
[11.575580596923828, 6.2974324226379395, "The Publication Date of the S056 X-ray telescope X-ray Telescope is April 1977."]
[8.260468482971191, 10.153779029846191, "The Instrument Size of the Imager Imaging System is 3 m tall."]
[9.456321716308594, 9.36197566986084, "The Ratio of the Aperture Function Image Processing is D/a."]
[4.789997577667236, 4.2316718101501465, "The Functionality of the Software Control System is Object recognition, satellite alignment, fine pointing, target recognition, stage recognition, image capture, image transmission, attitude acquisition."]
[5.371579647064209, 4.215521812438965, "The Purpose of the ETB Electronics Test Bed is Evaluate and demonstrate a number of new electronic components, processors, and memory devices."]
[5.242209434509277, 3.3824570178985596, "The Initiation Connector of the CSD Satellite Component is Unknown."]
[5.950248718261719, 5.834475517272949, "The Processing Mode of the SAR Processor Data Processor is Complete processing for the trigger application and possibly repeated processing for other applications."]
[10.66054630279541, 2.7605855464935303, "The Radio Link Testing Distance of the GomX-4A and GomX-4B Satellites is Up to 750 km."]
[7.280590534210205, 7.036707878112793, "The Use of the Thermal Waveband Imaging System is Track cold clouds in the upper atmosphere as well as forest fires on the Earth's surface."]
[7.482365131378174, 8.967718124389648, "The Spectral Band of the Infrared Channel is approx. 3.6 km at nadir."]
[8.980081558227539, 0.6652897596359253, "The Duration of the OSCAR-QUBE Experiment is 8 months."]
[13.16639518737793, 4.027720928192139, "The Third Full Data Release (DR3) Date of the Gaia Satellite is 13 June."]
[7.693235874176025, 9.26905345916748, "The Spectral Resolution of the Instrument Sensor is Better than 0.01\u00c5 (resolving power 105)."]
[9.13759994506836, 5.155208587646484, "The Stabilization of the Spacecraft Satellite is 3-axis."]
[7.952456951141357, 1.2999440431594849, "The Article Date of the Lunar Reconnaissance Orbiter Spacecraft is 11 February 2021."]
[10.648298263549805, 3.351757287979126, "The Closest Approach Distance of the Rosetta Spacecraft is 800 km."]
[4.78352165222168, 0.8456509113311768, "The Funds Raised of the Inspiration4 Mission is $29.2 million."]
[4.933155536651611, 4.146500587463379, "The Software Glitches of the Starliner Spacecraft is Major software error, communications dropouts, another software mistake."]
[7.562438011169434, -0.4778525233268738, "The Launch Date of the Falcon 9 Rocket is February 4, 2021."]
[8.380340576171875, 8.33985424041748, "The Effective Area at 80 nm of the EUV Simulation Simulation is 6 cm2."]
[11.116259574890137, 5.476904392242432, "The Sensitivity of the LISA Space Observatory is Lower frequency than LIGO."]
[10.468177795410156, 8.406888961791992, "The Components of the Coronagraph Instrument is Four coaxial occulting discs and photodetectors."]
[11.228751182556152, -1.4930686950683594, "The Mass of the 3U CubeSat Satellite is 3.2 kg."]
[9.685311317443848, 6.031322002410889, "The Responsible Teams of the ADCS Attitude Determination and Control Subsystem is Mission Operations (health monitoring and reporting), ADCS team (performance maintenance)."]
[9.165392875671387, 9.045969009399414, "The FOV of the SXI Spacecraft is 42 arc min x 42 arcmin."]
[5.401235103607178, 5.694514751434326, "The Frequency of the IGOR GPS receiver GPS Receiver is Dual."]
[8.212970733642578, 4.364272117614746, "The User Locations of the OUFTI-1 Satellite is Must be within the footprint of the satellite."]
[9.063199996948242, 9.238456726074219, "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."]
[9.10196590423584, 8.222432136535645, "The Temperature of the SWAP Imager is One million degrees."]
[3.2345480918884277, 4.832098960876465, "The EEPROM Capacity of the RAD750 SBC Single Board Computer is 4 MB."]
[8.520517349243164, 10.517485618591309, "The Pixels per Line of the CCDs Detector is 740."]
[7.054626941680908, 4.36993408203125, "The Measurement Category of the ST5 Satellite is Atmospheric Temperature Fields, Gravity, Magnetic and Geodynamic measurements, Atmospheric Humidity Fields, Atmospheric Winds."]
[5.887909889221191, 9.106651306152344, "The Power of the DUST sensor Cosmic Dust Sensor is 2.2 W."]
[6.0225958824157715, 6.598337173461914, "The Band of the SWIM Instrument Radar is Ku-band."]
[5.162301540374756, 6.989427089691162, "The Swath Width of the Antenna Conically-scanning reflector is 1000 km."]
[11.689175605773926, -1.127368450164795, "The Mass of the GCOM-W1 Satellite is About 1991 kg at launch."]
[8.667158126831055, 8.174050331115723, "The Detector Telescope Head of the DOSTEL Radiation Detector is Two PIPS detectors and one PIN diode."]
[9.288137435913086, 8.26822280883789, "The CCD Detector Temperature of the MEGS Spectrograph is -100\u00ba C."]
[8.19226360321045, 1.3762221336364746, "The Observation Date of the Lake Okeechobee Lake is July 3, 2022."]
[5.429282188415527, 4.072726249694824, "The Construction Completion of the Emergency Egress System Safety System is TBD."]
[3.6864161491394043, 6.574189186096191, "The Data Rates (TM) of the EWC31 S-band transceiver module Communication Module is 10 kbit/s to 1 Mbit/s."]
[6.0588603019714355, 9.61967945098877, "The Mass of the Instrument Spectrometer is 9.4 kg."]
[1.4400858879089355, 4.262309551239014, "The Power Source of the EAGLE ESPAStar Satellite is 96 Ahr battery."]
[12.059255599975586, 3.2874579429626465, "The Orbit Inclination of the GPM Core spacecraft Satellite is 65\u00ba."]
[9.395389556884766, 0.5093132853507996, "The Operational Lifetime of the MicroMAS-1 Satellite is One year."]
[8.367419242858887, 7.673756122589111, "The Components of the TM Thermal Calibration System Calibration System is Single onboard cavity blackbody, black, highly emissive shutter, toroidal mirror, thermistors."]
[5.196754455566406, 2.121565341949463, "The Number of Experiments of the OPS-SAT Satellite is Over 100."]
[7.228425979614258, 5.718789100646973, "The Purpose of the WIND Satellite is Measure the plasma and fields around the spacecraft, including energetic particles and radio waves."]
[7.199697971343994, 6.9365553855896, "The Presentation Date of the 3MI Instrument is October 16, 2013."]
[4.819344520568848, 1.7972744703292847, "The Number of Satellites of the EarthDaily Constellation Satellite Constellation is 10."]
[7.444484710693359, 1.409082055091858, "The Expected End of Operations of the MICROSCOPE Satellite is Autumn 2018."]
[1.4677937030792236, 4.354772567749023, "The Battery Temperature of the SpriteSat Satellite is Can go up to a critical level."]
[9.828667640686035, -0.9932523965835571, "The Phase Angle of the JL-1-GF03B Microsatellite is 60\u00ba."]
[6.421296119689941, 4.655420780181885, "The Payloads of the FY-3E Satellite is Microwave and infrared sounders, instrument to derive atmospheric conditions and ocean winds, spectral imager."]
[6.066532135009766, 0.846333384513855, "The Purpose of the RAVAN Satellite is Measure Earth outgoing radiation."]
[9.136958122253418, 2.180751323699951, "The Number of Additional Containers of the BepiColombo Spacecraft is 15."]
[5.117366313934326, 3.5088813304901123, "The Panel 5 Function of the CSTB1 Satellite is Payload panel."]
[7.5844526290893555, -0.4754720628261566, "The Launch Date of the SpaceX Falcon-9 Rocket is Jan. 14, 2017."]
[7.5203423500061035, 1.8955237865447998, "The Observation Date of the Wilkins Ice Shelf Ice Shelf is Dec. 1, 2016."]
[10.32722282409668, 3.125814914703369, "The Altitude at Launch of the GRACE Satellite Satellite is 485 km."]
[6.726988315582275, 6.415952205657959, "The Presentation Date of the GNSS Reflectometry Instrument Instrument is Sept 18-20, 2012."]
[5.078021049499512, 8.726344108581543, "The Position Accuracy (RMS orbit) of the S-2 NRT Product is < 10 m (2D) 3-sigma."]
[7.03527307510376, 0.918942391872406, "The Start Date of the ELFIN Satellite is 2012."]
[6.9758477210998535, 2.5519161224365234, "The URL of the AAUSat3 Satellite is http://www.space.aau.dk/aausat3/index.php?n=Tech.AAUSAT3InDetails."]
[9.94374942779541, 1.6252762079238892, "The Orbital Period of the MPO Spacecraft is 2.3 hours."]
[8.04000186920166, 1.2516682147979736, "The Image of the Day Date of the NASA Earth Observatory Satellite is 17 May 2022."]
[7.145318984985352, 8.892781257629395, "The Swath Width of the Instrument Satellite Instrument is 17.5 km (half mode)."]
[8.348243713378906, 2.90959095954895, "The Destination of the MoonLIGHT Satellite is Reiner Gamma region of the Moon."]
[3.276855230331421, 5.343028545379639, "The Storage Capacity of the PDHT Payload Data Handling and Transmission is 1410 Gbit."]
[4.463664531707764, 3.9181692600250244, "The Purpose of the Avionics Air Assembly (AAA) Fans Hardware is 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."]
[6.818080902099609, 6.074555397033691, "The Purpose of the RapidScat Satellite Instrument is Spying tropical-storm-force winds."]
[4.061435222625732, 5.755505561828613, "The Ka-band Data Rate of the CASCADE Satellite Communication System is Up to 2.1 Gbit/s using higher order modulations."]
[7.265683174133301, 3.4274742603302, "The Destination of the Queqiao Communication Satellite is EML-2."]
[7.064530372619629, 0.43418651819229126, "The Launch Date of the MidSTAR-1 Satellite is 9 March 2007."]
[8.317296981811523, 5.1838226318359375, "The Image Geolocation Accuracy of the SSTL-300 bus system Satellite Bus System is < 35 m (CE90 = Circular Error 90%)."]
[13.71252155303955, 1.6083712577819824, "The Mission Number of the Vega Launch Vehicle is 19."]
[9.477706909179688, 0.6308576464653015, "The On-Orbit Useful Life of the SXI Spacecraft is 3 years with a goal of 5 years."]
[10.334272384643555, 4.9133524894714355, "The Propellant Quantity of the Propulsion System Propulsion Subsystem is 103.5 kg."]
[10.41299819946289, 4.86406135559082, "The Propellant of the DMC Propulsion Subsystem Electric Propulsion is Butane."]
[10.127568244934082, 4.0630340576171875, "The Thrust Duration of the LightSail-2 Spacecraft is One month."]
[5.205916881561279, 3.355722665786743, "The Bus Configuration of the QuikTOMS spacecraft Satellite is Two rings stacked together vertically."]
[9.481443405151367, -0.7260738611221313, "The Development Date of the FedSat Microsatellite is 1998."]
[7.519567966461182, 8.102014541625977, "The Altitude Range of the RAIDS Instrument is 75-220 km."]
[7.607221603393555, 0.7108375430107117, "The Date of the Pre-CHUVA Field Campaign is 3-24 March 2010."]
[7.454209327697754, 5.219674587249756, "The Manufacturer of the OCO-2 Satellite is JPL."]
[9.722448348999023, 6.031110763549805, "The Controller of the ADCS Attitude Determination and Control System is Kalman Estimator."]
[11.746024131774902, -1.1771066188812256, "The Mass of the GOMS-1 Satellite is 2580 kg."]
[11.768051147460938, 4.644183158874512, "The Distance from Earth of the M83 Galaxy is 15 million light-years."]
[10.9764986038208, 5.051042556762695, "The Centrifugal Force Cause of the LISA Pathfinder Spacecraft is 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."]
[8.77082347869873, 2.8157975673675537, "The Image Credit of the Kepler Mission Space Mission is NASA."]
[6.671634197235107, 3.800286293029785, "The Mission Type of the Biomass Satellite is EO."]
[2.9419772624969482, 6.530936241149902, "The Power Consumption of the Receiver Communication Device is 0.125 W."]
[9.781576156616211, 1.5055022239685059, "The Observation Duration of the SPARCS Satellite is 1 day to 80 days."]
[7.064596652984619, 9.7621488571167, "The Spectral Range (\u00b5m) of the Band 10 Spectral Band is 0.90 - 0.965."]
[4.747373580932617, 1.8104593753814697, "The Number of Satellites of the Planet SkySats Satellite Constellation is 21."]
[5.827112674713135, 5.0167460441589355, "The Contributions of the DLR Agency is X-SAR hardware, ground systems, mission operations and data processing support."]
[9.266716957092285, 3.1588761806488037, "The Orbit of the CHORUS Satellite is Non-sun-synchronous."]
[5.299188613891602, 3.129828929901123, "The Purpose of the BeaverCube Satellite is Educational mission to introduce students worldwide to aerospace science and technology."]
[8.793252944946289, 8.991189956665039, "The Groove Density of the Grating Optical Component is ~646 grooves/mm at the center."]
[11.655108451843262, 1.6849766969680786, "The Debris Field Location of the Vikram Lander Lander is About 750 meters northwest of the main crash site."]
[6.193725109100342, 1.4973680973052979, "The Start of Operations of the CCC (Coordinated Constellation Concept) Satellite Constellation is 2014."]
[6.819925308227539, 4.808366775512695, "The Function of the Transponder Device is Track the Biomass satellite."]
[7.537161827087402, 1.1746288537979126, "The SAR Data Acquisition Date of the Copernicus Sentinel-1 Satellite is 2 September 2019."]
[5.883355140686035, 2.9430081844329834, "The Manufacturer of the RTAFSAT-1 Satellite is Royal Thai Air Force."]
[6.385910511016846, 1.4178544282913208, "The Main Port Mechanism of the PRISMA Satellite is Unknown."]
[4.103553295135498, 5.7344970703125, "The Telemetry Downlink Data Rate of the NEMO-HD Satellite is 8 kbit/s."]
[10.313483238220215, 4.953863143920898, "The Engine Type of the IES Ion Engine System is Xe microwave discharge ion engine system."]
[6.757976531982422, 8.519852638244629, "The Spatial Resolution of the MSU-SK Radiometer is 170 m (in VIS)."]
[4.4242658615112305, 6.188752174377441, "The Back-up Channel of the RF Communications Communication System is S-band."]
[11.467451095581055, 2.5757689476013184, "The Discovery Year of the Itokawa Asteroid is 1999."]
[10.467649459838867, 4.8039116859436035, "The \u03c1Isp of the Thruster Propulsion System is 50% greater than hydrazine."]
[8.89331340789795, 5.369799613952637, "The Attitude Command of the MicroSCOPE Satellite is Inertial."]
[4.178273677825928, 5.166898250579834, "The Redundancy of the SSTL Signal Generator Chain Signal Generator is One chain."]
[12.97908878326416, 4.858477592468262, "The URL of the IBEX Spacecraft is http://www.swri.org."]
[9.763285636901855, 7.285367488861084, "The Failure Cause of the COPV Pressure Vessel is Accumulation of oxygen between the COPV liner and over-wrap in a void or a buckle in the liner."]
[5.67266845703125, 9.15081787109375, "The Instrument Power of the Instrument Sensor is 35 W."]
[9.330302238464355, 6.4469194412231445, "The Manufacturer of the MST Star Tracker Star Tracker is TU Graz."]
[7.568851470947266, 1.6063029766082764, "The Publication Date of the Iridium engineering magnetometer Magnetometer is December 15, 2000."]
[9.6373929977417, -0.5290701389312744, "The Photometer Field-of-View of the Nanosatellite Satellite is 24\u00ba."]
[6.844109535217285, 8.503994941711426, "The SST Spatial Resolution of the CIMR Radiometer Imager is 15 km."]
[4.822639465332031, 6.051418304443359, "The Improvement Factor of the ELFIN Satellite is Two."]
[9.91256332397461, 3.971381902694702, "The Sponsors of the NanoSail-D2 Satellite is Army Space and Missile Defense Command, the Von Braun Center for Science and Innovation, Dynetics Inc."]
[12.001562118530273, 3.2493693828582764, "The Orbit Inclination of the ALBus CubeSat Satellite is 85\u00ba."]
[6.141051769256592, 4.023415565490723, "The Mission Scientist of the Aeolus Satellite is Anne Grete Straume."]
[7.365260601043701, 4.1287760734558105, "The Data Application of the DAICHI Satellite is Compilation of Global Digital 3D Map with World's Best Precision."]
[6.8945183753967285, 4.596660614013672, "The Workshop Location of the RECCAP-2 Activity is Gotemba, Japan."]
[7.512594223022461, 3.747969388961792, "The Orbital Separation from SPOT-5 of the SPOT-4 Satellite is 166\u00ba."]
[9.342247009277344, 5.263479232788086, "The Momentum Wheels of the NigeriaSat-2 Satellite is 4 Microwheel 10SP."]
[8.099451065063477, 8.485970497131348, "The Self-apodisation effect of the Michelson Interferometer Interferometer is Reduces the signal level when increasing the FOV and the OPD range."]
[8.58389949798584, 5.206136226654053, "The Pointing Accuracy of the Spacecraft Satellite is \u2264 3\u00ba."]
[9.594369888305664, 5.949036121368408, "The Magnetometer of the ADCS Attitude Determination and Control Subsystem is 3-axes."]
[11.115756034851074, 7.053187847137451, "The Presentation Date of the An Efficient Photoelectric X-ray Polarimeter Device is 2001."]
[3.9610345363616943, 6.0701727867126465, "The Components of the Downlink Optical Communication System is 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."]
[3.7910287380218506, 6.101014614105225, "The Telecommand Data Rate Range of the TTCS Telemetry & Telecommand Subsystem is 2-8 kbit/s."]
[6.921082019805908, 3.8563084602355957, "The Mission Type of the HySIS Satellite is Earth Observation."]
[10.13007640838623, 4.859963893890381, "The Provider of the Picosatellite propulsion system Propulsion System is Aerospace Innovation GmbH."]
[11.870379447937012, 0.9900205731391907, "The Resumed Work Days of the Chang'e-4 Lunar Probe is 21."]
[9.559399604797363, 7.728754043579102, "The Ion Energy Range of the SWEPAM Particle Detector is 0.26 - 35 keV."]
[7.568332195281982, 0.046091627329587936, "The Launch Date of the Cheops Satellite is 18 December 2019."]
[9.756486892700195, 1.3305330276489258, "The Contact Time of the STSAT-3 Satellite is 89 minutes after lift-off."]
[10.435874938964844, 2.6677510738372803, "The Apogee of the RBSP spacecraft Satellite is ~ 5.8 RE."]
[6.300344467163086, 8.24698257446289, "The Operating Frequencies of the SMMR Microwave Radiometer is 10.7 GHz."]
[6.259481906890869, 5.783127784729004, "The Spatial Resolution of the GF-3 SAR Satellite is 3.5 m in azimuth and 5.5 m in range."]
[7.647515773773193, 1.7961208820343018, "The Conference Presentation of the Near Earth Asteroid Scout Satellite is AIAA Space 2014 Conference and Exposition."]
[9.567987442016602, 7.811287879943848, "The Omni-directional Proton Energy Ranges of the MEPED Particle Detector is > 16 MeV, > 35 MeV, > 70 MeV and > 140 MeV."]
[4.039622783660889, 2.3825600147247314, "The Type of the SUCHAI-1 Satellite is 1U CubeSat."]
[12.987828254699707, 4.859480857849121, "The NASA Feature Date of the IBEX Satellite is 5 August 2020."]
[3.9973905086517334, 6.166252613067627, "The Performance of the S-band link Communication Link is Successfully established even in elevations below 20 degrees."]
[9.155508995056152, 0.4192289710044861, "The End of Life Date of the Odin Satellite is Dec 2023."]
[4.549056529998779, 3.959455728530884, "The Conference Presentation Date of the Space Plug-and Play Avionics Avionics is April 25\u201328, 2005."]
[7.3414626121521, 9.937078475952148, "The Spatial Resolution of the Hyperion Imaging Spectrometer is 30 m."]
[7.961362838745117, 7.220880508422852, "The Scan Mechanism Assembly of the TEMPO Instrument is Provides high-precision pointing."]
[9.327826499938965, -0.6947075128555298, "The Developer of the ROBUSTA-1B Nanosatellite is University of Montpellier students."]
[11.745132446289062, -1.2208738327026367, "The Mass of the CartoSat-2E Satellite is ~712 kg."]
[6.733313083648682, 2.1772141456604004, "The Presentation of the GPM Satellite is 14th European Space Mechanisms & Tribology Symposium \u2013 ESMATS 2011."]
[8.936145782470703, 1.8129364252090454, "The Arrival Date of the BepiColombo Spacecraft is 2024."]
[7.428787708282471, 0.24036216735839844, "The Press Release Date of the Smile Satellite is 30 July 2019."]
[7.3387885093688965, 0.3091152310371399, "The Launch Date of the SpIRIT Satellite is 2023."]
[4.3564887046813965, 5.3343963623046875, "The Redundancy of the TT&C Receiver Communication Device is Half Satellite."]
[5.192286491394043, 3.1482927799224854, "The Design of the QuakeSat Satellite is CubeSat."]
[9.116304397583008, 10.54099178314209, "The Exposure Time of the VIS Camera is 565 seconds."]
[7.129710674285889, 8.258399963378906, "The Time Resolution of the FREND Instrument is From 1 second."]
[11.546490669250488, 2.645329713821411, "The Orbital Range of the Ryugu Asteroid is Mostly between Earth and Mars."]
[5.848108768463135, 6.750616073608398, "The Frequency of the Radar Radar is X-Ku dual-frequency."]
[10.974517822265625, 5.4243340492248535, "The Typical Magnetic Field Strength of the Sunspot Solar Phenomenon is 3,000 gauss."]
[9.608011245727539, 5.809224605560303, "The Stabilization of the ADCS Attitude Determination and Control Subsystem is 3-axis."]
[3.581822156906128, 5.453122615814209, "The Data Acquisition of the PROBA-V Satellite is >1015 bytes."]
[8.610581398010254, 6.832597732543945, "The Type of the Magnetometer Sensor is Flux gate."]
[6.608939170837402, 3.6966071128845215, "The Mission Type of the LAPAN-A2 Satellite is EO (Earth Observation)."]
[11.272078514099121, 3.494281053543091, "The Width of the Deir el-Medina Pit on Comet 67P/Churyumov\u2013Gerasimenko is 130 m."]
[6.061715126037598, 4.111912250518799, "The Affiliation of the IASI Instrument is CNES and EUMETSAT."]
[7.198430061340332, 3.9850409030914307, "The Facilities of the Coordinated Observations Satellite Mission Activity is Magnetic and optical observatories, radars, receivers and heaters."]
[7.280490875244141, 2.199159622192383, "The Observation Date of the Orbiting Carbon Observatory-2 (OCO-2) Satellite is 8 February 2018."]
[8.066132545471191, 5.272402763366699, "The Data Delivery of the GBOT Ground Based Orbit Tracking is One set of data per day."]
[4.0392937660217285, 5.038284778594971, "The Data Recorders Redundancy of the Vital Layer Data System Component is Two redundant recorders."]
[8.460171699523926, 9.937174797058105, "The Subaperture Radius of the SMART Imaging System is 0.8 to 0.2 mm."]
[1.501109004020691, 4.943534851074219, "The Voltage of the MTM main power bus Power Bus is 100 V."]
[6.959906578063965, -0.15359683334827423, "The End of Life Date of the ARMADILLO Satellite is 25 June 2024."]
[11.621037483215332, -0.9037246704101562, "The Total Mass of the Bus Satellite Component is 128 kg."]
[7.001782417297363, 4.3118367195129395, "The Measurement Domain of the CAS500 Satellite is Land."]
[8.979138374328613, 3.2927308082580566, "The Satellite Orbit Types of the BeiDou-2 Satellite Constellation is 5 geostationary orbit (GEO) satellites and 30 medium Earth orbit (MEO) satellites."]
[5.090975284576416, 5.991635322570801, "The Height Data Echo Rate of the GEOSAT Satellite is 10 Hz."]
[8.054634094238281, 0.8396978378295898, "The Launch Date of the Landsat-9 Satellite is September 2021."]
[7.800586700439453, 9.81543254852295, "The Bandwidth of the Band Photometers Photometer is 5.0 nm."]
[9.699811935424805, 6.891894817352295, "The Flow Rate Set Points of the FCA Flow Control Assembly is Two."]
[12.049747467041016, 3.2872917652130127, "The Inclination of the Primary Payload Unknown is 69.5\u00ba."]
[7.621833801269531, 6.525272846221924, "The Required Precision of the H2CO Satellite Instrument is 10.0."]
[4.794536113739014, 1.840669870376587, "The Number of Satellites of the Capella X-SAR Constellation Satellite Constellation is 9."]
[8.37582015991211, 2.3553860187530518, "The Communication Status of the Voyager 2 Spacecraft is Without receiving commands from Earth."]
[7.318276882171631, 2.6302132606506348, "The URL of the Hinode Satellite is http://www.isas.ac.jp/home/solar/."]
[6.263836860656738, 6.348034381866455, "The Tandem Flight Duration of the Copernicus Sentinel-6 Poseidon-4 Radar Altimeter is 12 months."]
[6.693019390106201, 1.3934764862060547, "The Deactivation Date of the RapidEye Earth Observation Constellation is March 2020."]
[4.821479797363281, 1.8857024908065796, "The Quantity of the SuperDove satellites Next-generation satellites is 150."]
[7.6879191398620605, 9.12275218963623, "The Spectral Range of the IIM instrument Imaging Spectrometer is 0.48-0.96 \u00b5m."]
[7.594920635223389, 1.543418049812317, "The IGARSS Presentation Date of the SMOS Satellite is July 26-31, 2015."]
[7.49047327041626, 9.921625137329102, "The Spectral Band Interval of the SMI Spaceborne Multispectral Imager is 13 nm."]
[9.565286636352539, 6.8156046867370605, "The URL of the Wide-Field Imager for Solar Probe Plus Imager is http://www.nrl.navy.mil/ssd/branches/7680/WISPR."]
[8.696727752685547, 3.1690735816955566, "The Mission Name of the GOCE Satellite is Gravity field and steady-state Ocean Circulation Explorer."]
[8.628988265991211, 1.7683172225952148, "The Observation Type of the Spitzer Satellite is Eddington Flare from Blazar OJ 287."]
[6.428452968597412, 4.6502814292907715, "The Mission of the OLCI Instrument is Sentinel-3."]
[5.193301200866699, 6.096112251281738, "The Installation of the ISL Antennas Antennas is +X surface and -X surface."]
[4.121696949005127, 5.612959384918213, "The Downlink Data Rate of the IXPE Satellite is 2.0 Mbit/s."]
[9.010831832885742, 2.501014232635498, "The Launch Date of the DART Space Probe is Last November."]
[5.34024715423584, 3.2749979496002197, "The Data Applications of the BeaverCube Satellite is Improving the understanding of regional biological productivity and the effects of extreme weather events."]
[10.018342018127441, 1.486027479171753, "The Lag Period of the Pelican Satellites Satellite is Less than two hours."]
[4.59302282333374, 6.038031578063965, "The Beacon Transmission Rate of the ELFIN-A Satellite is 9600 baud."]
[5.294476509094238, 2.123142957687378, "The Launch Vehicle of the CubeStack Multi CubeSat Adapter is Minotaur I."]
[9.260924339294434, 0.9587148427963257, "The Development Cycle of the CubeSats Satellite is Six to twelve months."]
[8.884900093078613, 6.527698993682861, "The Micro-switches of the Mechanism Position Indicator is Array of micro-switches."]
[10.130757331848145, 3.568716287612915, "The Spacecraft Separation of the Tri-TIP Instrument is 250-500 km."]
[7.843615531921387, 3.1291451454162598, "The Development Status of the TerraSAR-NG System Satellite System is Preliminary Design Phase."]
[6.679577350616455, 0.7770126461982727, "The Launch Date of the SkySat Constellation Satellite Constellation is 21 Nov 2013."]
[8.004019737243652, 8.246452331542969, "The Overall Accuracy of the ARI Infrared Spectrometer is <0.1 K 2\u03c3."]
[7.0913190841674805, 0.7396566867828369, "The Test Period of the TOR Payload is January 15 through February 15, 2008."]
[6.843300819396973, 8.457258224487305, "The Ground Track Velocity of the ICIR Radiometer is Approximately 7 km/s."]
[6.647878170013428, 0.5565074682235718, "The Launch Date of the Meteosat-1 Satellite is November 23, 1977."]
[6.310060024261475, 4.877889633178711, "The Quality Information of the L1C Products Satellite Data is Included."]
[9.537714958190918, 5.973682403564453, "The Attitude Sensing of the ADCS Attitude Determination and Control Subsystem is Magnetometers, gyros and photodiodes."]
[6.183660984039307, 4.955193042755127, "The Application of the GPS Satellite-based Service is Navigation."]
[9.824504852294922, 3.9036011695861816, "The Re-entry Date of the Drag de-orbit sail De-orbit Device is 72 days later."]
[8.866971015930176, 8.836441993713379, "The Field-of-view of the Photometer Optical Instrument is 24\u00ba."]
[9.640534400939941, 7.120850563049316, "The Temperature Range of the Battery Energy Storage is -5\u00ba to +25\u00ba C."]
[11.419262886047363, 2.4984281063079834, "The Discovery Year of the 1999JU3 Asteroid is 1999."]
[3.635509729385376, 4.828007221221924, "The Power Modes of the dsPIC33F microcontroller Microcontroller is Unknown."]
[10.258502006530762, 5.61726188659668, "The Power Requirement of the Electrodynamic Tether (Thrust System) Propulsion Device is Requires power to be injected into the tether system from an on-board power supply."]
[4.779262065887451, 5.343751430511475, "The Communication Protocol of the Deployment Systems Satellite is RF, UHF/VHF, S-band."]
[5.878077507019043, 4.681506156921387, "The Content of the L1-SAIF+ Satellite Message is Differential correction information, information for correcting orbital position and clock errors for 10 satellites, short messages for emergency cases."]
[9.60715103149414, 5.944418907165527, "The Drift Angle Correction Accuracy of the ADCS Attitude Determination and Control Subsystem is \u2264 0.1\u00ba (3\u03c3, correction based on nadir camera)."]
[8.29558277130127, 10.084399223327637, "The Pan of the Pushbroom imager GSD is 1.45 m."]
[5.2038397789001465, 4.1137309074401855, "The Support of the Flight Segment System Engineer Engineer is Project System Engineer."]
[5.927709102630615, 3.078505516052246, "The Developer of the Unicorn-2D PocketQube is Alba Orbital UG (Germany)."]
[6.31212043762207, 9.694211959838867, "The Instrument Mass of the MSU-E Multispectral Scanner is 17 kg."]
[7.640505313873291, 2.3224287033081055, "The URL of the ExoMars Mars Orbiter is http://m.esa.int/Our_Activities/Space_Science/ExoMars/Schiaparelli_crash_site_in_colour."]
[5.077648162841797, 4.533013820648193, "The Main Operations Tasks of the LMOC Ground Segment is 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."]
[6.017010688781738, 3.4359140396118164, "The Location of the LRAC Reference Archive Center is Kiruna."]
[6.482547760009766, 4.371401309967041, "The Data Delivery of the SENSE Satellite is Air Force Research Laboratory at Kirtland Air Force Base."]
[8.379862785339355, 7.332172870635986, "The Measurement Type of the Logarithmic Electrometers Instrument is Current."]
[9.25210189819336, 2.308753728866577, "The Trajectory Correction Maneuver of the MarCO-B CubeSat is Completed with Unexpected Challenges."]
[7.963342189788818, 3.5740456581115723, "The Phase of the SPARCS Satellite is Phase B."]
[9.104931831359863, 6.868007659912109, "The Range of the Star sensor Sensor is 14.4\u00ba x 19.2\u00ba."]
[8.782197952270508, 9.696898460388184, "The Information Usage of the IIS Integrated Imaging Subsystem is Co-registration with the AVHRR."]
[8.476122856140137, 4.3077192306518555, "The Science Objective of the BRITE Constellation Satellite is Provide milli-magnitude (0.1% error) differential photometry of bright stars."]
[8.106106758117676, -0.6282306909561157, "The Docking Time of the Crew Dragon Spacecraft is Around a day later."]
[9.982158660888672, 2.967925786972046, "The Maximum Depth of Discharge of the TSUBAME Satellite is Estimated at no more than 50%."]
[9.127188682556152, 9.401683807373047, "The FOV (Field of View) of the Imager Imaging System is > 1.28\u00ba."]
[10.668280601501465, 9.207907676696777, "The Image Content of the CaSSIS Instrument is Light-toned bedrock."]
[6.9402689933776855, 3.6530351638793945, "The Manufacturer of the EROS-B Satellite is ImageSat International N.V.."]
[11.554293632507324, 6.2820234298706055, "The Observation Date of the XMM-Newton X-ray observatory is June 2013."]
[5.919407367706299, 2.825969934463501, "The Prime Contractor of the THEMIS Satellite Constellation is Swales Aerospace."]
[9.185364723205566, 3.2072465419769287, "The Orbit of the PAMELA Instrument is Semi-polar Resurs orbit."]
[7.302501678466797, 5.342996120452881, "The Measurement Frequency of the GeoCARB Satellite is Daily."]
[1.5902888774871826, 4.995676517486572, "The Voltage Output of the PSU Power Supply Unit is 5 V to supply the RF power amplifiers in C&CS."]
[7.029906272888184, 7.696227550506592, "The Swath of the HARP-2 Polarimeter is Wide."]
[9.588519096374512, 7.855130672454834, "The Electron energy of the Microdosimeter B Instrument is > 50 keV."]
[7.926812171936035, 4.4423828125, "The Nadir resolution of the WorldView Legion Satellite System is 29 cm."]
[9.440337181091309, 5.451488494873047, "The Operation Start Date of the AOCS Attitude and Orbit Control System is Day 5."]
[5.157491683959961, 3.160836696624756, "The Function of the CAPSTONE 12U CubeSat is Demonstration of spacecraft-to-spacecraft navigation services."]
[7.472901344299316, 1.8752548694610596, "The URL of the Spacecraft Fire Experiment (Saffire) Experiment is http://orbit.dtu.dk/ws/files/97737980/2014_ICES_SFS_Demo_Paper_265_5_16_2014.pdf."]
[8.016569137573242, 1.2453216314315796, "The Date of the Super Typhoon Rai Image is 18 December 2021."]
[8.632377624511719, 6.921541213989258, "The Mounting Interface Requirement of the SOSMAG Magnetometer is None."]
[8.177618026733398, 5.314078330993652, "The Purpose of the GEOTAIL Satellite is Measure the flow of energy and its transformation in the magnetotail created by the interaction between the solar wind and the Earth."]
[5.366816520690918, 6.05597448348999, "The Configuration of the Reflectarray Antenna Antenna is Three panels, electrically tied together through hinges, with an array of printed circuit board patches on them."]
[6.1064133644104, 4.8463640213012695, "The Location of the OSIRIS Instrument is Odin."]
[9.458104133605957, 0.013268190436065197, "The Expected Orbit Duration of the SMDC-ONE Nanosatellite is Approximately 30 days."]
[6.481226444244385, 3.015932083129883, "The California Institute of Technology Infrared Processing and Analysis Center, Pasadena, California, USA of the NASA Herschel Science Center Location is An additional center is the NASA Herschel Science Center, located at the California Institute of Technology Infrared Processing and Analysis Center, Pasadena, California, USA."]
[7.304170608520508, 3.7212891578674316, "The Data Delivery of the SPOT-4 Satellite is Unreliable."]
[5.892157554626465, 8.590849876403809, "The Unknown of the Millimeter Wave Atmospheric Sounder (MAS) Sounder is Unknown."]
[6.350041389465332, 2.961229085922241, "The Mission Design of the Geosat ERM Satellite is G. H. Born, J. L. Mitchell, G. A. Heyler."]
[7.925131797790527, 4.418275833129883, "The Image Resolution of the Ikonos-2 Satellite is 1 m."]
[7.826133728027344, 8.978547096252441, "The Spectral Range of the Spectrometer Instrument is 5-28.5 \u00b5m."]
[4.241415977478027, 6.900045394897461, "The LO Frequency (MHz) of the HRIT HiRID Data Receiver is 1900."]
[8.221003532409668, 10.310812950134277, "The Number of Bands of the WFI Camera is 4."]
[10.72024917602539, 10.279446601867676, "The Preamp full scale output swing of the PHA Detector is 4.0 V."]
[5.053910255432129, 1.918165922164917, "The Tube Capacity of the Picosa Launcher Satellite Component is 2 short picosats or 1 long picosat."]
[9.689984321594238, -0.5005102157592773, "The Fault Location of the Tsubame microsatellite Satellite is Peripheral circuit for communication."]
[2.2413063049316406, 4.441895961761475, "The Power of the Average Payload Satellite is < 100 W."]
[7.285335540771484, 8.093097686767578, "The Mean Revisit Time of the TeLEOS-1 Imager Imaging Device is 12 to 16 hours."]
[3.9892711639404297, 6.6956000328063965, "The Expected Level of the TRL Technology Readiness Level is 6."]
[2.251769781112671, 4.443011283874512, "The Wave Energy of the STEREO spacecraft Satellite is 2400 megatons of TNT (1022 joule)."]
[13.130106925964355, 4.044443130493164, "The User Interface of the Gaia Satellite is GUI (Graphical User Interface)."]
[3.8932626247406006, 4.6278204917907715, "The Purpose of the OBDH On-Board Data Handling subsystem is Load the software experiment."]
[6.618934631347656, 1.1618767976760864, "The Operation Date of the PRISMA Satellite is Sept. 27-Oct. 1, 2010."]
[11.761025428771973, 4.730688095092773, "The Mass of the The Horse and the Dragon Pair of distinct massive galaxies is Roughly as massive as our Milky Way."]
[6.071115016937256, 6.2475714683532715, "The Swath Width (ScanSAR mode) of the XSAR SAR is Up to 100 km."]
[7.0585126876831055, 0.5158725380897522, "The Launch Date of the SPOT-7 Satellite is Late 2013."]
[3.251521110534668, 5.275832176208496, "The Data Storage Capacity of the Data Handling System System is 64 Gbit."]
[7.486121654510498, 1.2039822340011597, "The Antenna Deployment Date of the Radar Instrument is July 28, 2018."]
[11.343690872192383, 6.964532852172852, "The Measurement Capability of the NICER X-ray Instrument is General-relativistic Shapiro delay in binary systems."]
[11.473669052124023, 2.177994728088379, "The Sample Return Date of the Hayabusa-2 Spacecraft is December 2020."]
[11.517409324645996, 6.360994815826416, "The Operation of the XMM-Newton X-ray Telescope is Must be told exactly where to point."]
[3.412855863571167, 5.283945560455322, "The Data Storage Capacity of the RISAT-2 Satellite is 240 Gbit."]
[7.03416109085083, 2.552194356918335, "The URL of the Satellite Satellite is http://journals.ametsoc.org/doi/pdf/10.1175/1520-0477%281979%29060%3C1038%3ASSOTSA%3E2.0.CO%3B2."]
[7.21206521987915, 8.010035514831543, "The Integration Time of the Scanner Assembly Instrument is About 15 seconds."]
[6.044942855834961, 9.596348762512207, "The Mass of the Field Measurement Device Electronic Unit is < 0.5 kg."]
[7.187665939331055, 1.046087622642517, "The Publication Date of the RadCalNet Calibration Network is 16 October 2019."]
[7.436654090881348, 8.482425689697266, "The MTF of the Instrument Satellite Instrument is > 0.2 @ Nyquist frequency."]
[6.055954933166504, 2.303684949874878, "The Launch Site of the STPSat-3 Satellite is MARS (Mid-Atlantic Regional Spaceport)."]
[5.837395191192627, 4.0491132736206055, "The Application of the AutoConTM Technology is Orbit maintenance of single spacecraft or constellations and formations."]
[6.984198093414307, 4.3306474685668945, "The Measurement Category of the GF-3 Satellite is Multi-purpose imagery (land), Landscape topography."]
[7.491734981536865, 3.7362818717956543, "The Observation Data of the Shikisai Satellite is Boso Peninsula SST and the seine fishing ground."]
[8.06818962097168, 8.51535701751709, "The Unapodized Spectral Resolution Requirement of the Michelson Interferometer Interferometer is I/(2L)."]
[7.273426055908203, 0.6566047668457031, "The Inauguration Date of the DEIMOS-2 Satellite is October 8, 2013."]
[6.928408622741699, 3.254859209060669, "The Mission Status of the Satellite HY-1B is Operational."]
[7.272838592529297, 1.5619611740112305, "The Publication Date of the Cluster Mission Satellite Mission is Oct. 1988."]
[8.010793685913086, 4.515745639801025, "The Image Resolution of the Solar Orbiter Satellite is 9148 x 9112 pixels."]
[4.942412853240967, 3.762056350708008, "The Modules of the PRIMA Satellite Bus is Propulsion module (PPM), service module (SVM), payload module (PLM)."]
[5.820549488067627, 6.778660297393799, "The Antenna Rotation Speed of the IRS Interferometric Radar System is 1\u00ba/s."]
[8.217267990112305, 2.5845370292663574, "The Pre-flight Calibration Target of the ARTEMIS Satellite is Specially-coated panel with known absorption features."]
[8.245747566223145, 10.187459945678711, "The Dimensions of the Data Cube Data Structure is samples_wide X number of spectral_data_lines X number_of_frames."]
[7.243355751037598, 0.613441526889801, "The Launch Date of the OrbView-4 Satellite is Sept. 21 2001."]
[6.932024002075195, 4.776815414428711, "The Measurement Category of the Biomass Satellite is Vegetation."]
[8.821023941040039, 10.741657257080078, "The Side-viewing Capability of the CCD Pushbroom Camera Camera is \u00b132\u00ba."]
[6.303858280181885, 4.91971492767334, "The Type of the NOSS-36A Satellite is Navy Ocean Surveillance Satellite."]
[5.023776531219482, 4.634333610534668, "The Antenna Usage of the Ground Segment Ground Control Infrastructure is Transmitting and Receiving."]
[7.504127502441406, 2.2894794940948486, "The Utilization of the ICI-4 Radiometer is Quasi-window, cloud ice retrieval, cirrus clouds."]
[4.525450706481934, 6.651159286499023, "The Frequency of the Ka-band Signal is 32 GHz."]
[10.190774917602539, 2.989234685897827, "The Orbit of the Spacecraft Satellite is 600-850 km altitude."]
[7.6662726402282715, 0.658194899559021, "The End of Life Date of the Sentinel-5P Satellite is September 2027."]
[12.952920913696289, 4.14414119720459, "The Previous Catalogue Distance Limit of the Gaia Catalogue of Nearby Stars Stellar Census is 82 light years."]
[10.22131633758545, 4.951507568359375, "The Number of Reaction Control Thrusters of the Propulsion Subsystem Satellite is 16."]
[7.158087253570557, 5.746738433837891, "The Wind Velocity Range (PBL) of the Aeolus Satellite is \u00b1150 m/s."]
[6.5454535484313965, 2.0229668617248535, "The News Article of the Robotic satellite servicer Satellite is S. Clark, \"Robotic satellite servicer rehearsal underway in orbit,\" Spaceflight Now, April 3, 2007."]
[5.266468048095703, 5.336061477661133, "The Manufacturer of the FR-lite satellite radio Communication Device is Johns Hopkins University Applied Physics Laboratory."]
[9.005980491638184, 3.192232608795166, "The De-orbit of the Gnome Chompski Space Component is With Electron\u2019s Kick Stage."]
[2.288896322250366, 4.461244583129883, "The Power Consumption of the Satellite Satellite is 270 W."]
[5.315876007080078, 7.436522483825684, "The Data Volume of the Mini-RF Instrument is 60 TB."]
[9.746091842651367, 4.0496907234191895, "The Sail Area of the CanX-7 Drag Sail Payload is Approximately 5 m2."]
[10.21849250793457, 2.9857654571533203, "The Orbit Altitude of the CartoSat-2D Satellite is 505 km."]
[1.904315710067749, 5.5017008781433105, "The Voltage of the Voltage 1 Power Amplifier is 22-28 adjustable."]
[9.048852920532227, 6.550974369049072, "The Quantity of the Rate gyro Sensor is 1 unit."]
[6.479187488555908, 2.9272425174713135, "The | of the Adam Szabo and Keith W. Ogilvie Individuals is Information provided by Adam Szabo and Keith W. Ogilvie of NASA/GSFC."]
[4.873170375823975, 3.7301220893859863, "The Upper Module Components of the Merlin Satellite Device is `sensor board', detectors, associated front-end electronics."]
[7.021159648895264, 2.4917919635772705, "The URL of the MidSTAR-1 Satellite is http://en.wikipedia.org/wiki/MidSTAR-1."]
[5.235983371734619, 6.87869119644165, "The Thickness of the RF Section Subsystem is 5 cm."]
[11.772297859191895, -0.9738426208496094, "The Mass of the Eristo/Osteo Payload is 66 kg."]
[11.393308639526367, 6.547013759613037, "The Telescope Type of the ASTRO-H Mission is SXTs (Soft X-ray Telescopes)."]
[6.8949151039123535, 0.6549569964408875, "The Shutdown Date of the IMP-8 Satellite is Oct. 31, 2001."]
[6.730965614318848, 7.574549674987793, "The Transmitter Wavelength of the DIAL Instrument LIDAR is 2 \u00b5m."]
[8.498868942260742, 4.896518707275391, "The MTF of the NEMO-HD Satellite is 0.10."]
[11.959101676940918, 3.170816659927368, "The Inclination of the 7 microsatellites Satellite is 97.45\u00ba."]
[7.573005676269531, 1.9718364477157593, "The Mission Status of the LADEE Satellite is Completed."]
[10.100336074829102, 5.026402950286865, "The Thruster System of the BeaverCube CubeSat is Tiled Ionic Liquid Electrospray (TILE 2) thruster system technology, developed and manufactured by Accion Systems, Inc."]
[8.273377418518066, 3.070188283920288, "The Mission Operations Segment Date of the TanDEM-X Satellite is April 25-30, 2010."]
[9.318236351013184, 10.241778373718262, "The Field of View of the EIC Camera is \u00b18.5\u00ba."]
[5.9933648109436035, 3.4569671154022217, "The Affiliation of the STScI Science Operations Center is Association of Universities for Research in Astronomy (AURA)."]
[8.597646713256836, 5.299752712249756, "The Pointing Accuracy of the PARASOL microsatellite Satellite is 0.1\u00ba."]
[6.358871936798096, 2.795593500137329, "The Manufacturer of the Lucy Discovery Program Mission is Lockheed Martin."]
[1.5941046476364136, 4.598459720611572, "The Configuration of the SABR DC/DC Converter is Synchronous buck converter."]
[4.704760551452637, 6.594682693481445, "The Operating Frequency of the Antennas Communication is Not specified."]
[7.157588481903076, 8.715251922607422, "The Spatial Resolution of the Instrument Satellite Instrument is 10 m."]
[8.381783485412598, 9.203390121459961, "The Detectors of the NIRSpec Spectroscopy Instrument is Two."]
[9.314202308654785, 6.38938045501709, "The Attitude Update Mode Rate of the Star Tracker Attitude Determination System is 1.7 Hz."]
[9.711316108703613, 7.968001842498779, "The Neutron Energy Range of the Natalya-2M High energy radiation spectrometer is 20 \u2013 300 MeV."]
[6.91018009185791, 0.5028164386749268, "The Launch Date of the Sich-2 Satellite is 17 Aug 2011."]
[7.098752975463867, 0.9622541069984436, "The Transmitter Fault Date of the MicroMAS-1 Satellite is August 2015."]
[10.397639274597168, 2.7214291095733643, "The Perigee of the SCD-2 Satellite is 743 km."]
[6.453794956207275, 8.23019790649414, "The Primary Function of the JMR Microwave Radiometer is Measure brightness temperatures."]
[7.701535224914551, 1.5566078424453735, "The CDR Date of the SMOS Satellite is Nov. 2005."]
[2.0648443698883057, 4.520754814147949, "The Power Generation of the EAGLE ESPAStar Satellite is 1.2 kW."]
[5.887557506561279, 6.733282089233398, "The Measurement of the KaRIn Radar Interferometer is Water level."]
[7.386955738067627, 0.7079389691352844, "The Announcement Date of the 30 Doradus in LMC Satellite is Jan. 30, 2000."]
[9.057684898376465, 6.672578811645508, "The Energy Resolution of the IMAP Satellite is 100 eV."]
[5.854430675506592, 8.57578182220459, "The Viewing Angle of the MWHS-II Microwave Humidity Sounder is \u00b153.35\u00ba."]
[9.47390365600586, 6.737407207489014, "The Electrical Conduction Method of the Fasteners Mechanical Component is Conduct the electricity to a copper lug."]
[8.212221145629883, 9.083740234375, "The Projected Counting Rate of the Instrument Spectrometer is 0.5 counts/pixel/exp/R."]
[1.7360254526138306, 4.706606864929199, "The Open Circuit Voltage (Voc) of the Solar Panel Satellite Component is Variable."]
[10.213181495666504, 2.9849190711975098, "The Orbit Altitude of the OPAL Satellite is ~ 370 km."]
[10.281338691711426, 4.942345142364502, "The Development Date of the Resistojet Thruster Propulsion Systems Propulsion Systems is Aug. 11-14, 2003."]
[4.036614418029785, 1.2067774534225464, "The Mission Type of the Solar-A / Yohkoh Satellite is Non-EO."]
[10.671880722045898, 5.269349098205566, "The Performance of the CNAPS Propulsion System Propulsion System is Out-performed expectations."]
[1.47641122341156, 4.900025844573975, "The Eclipse Power Conversion Efficiency of the SBVR Power Supply is 97%."]
[9.089180946350098, 9.841767311096191, "The Output of the DarkCarb image sensor Photon Detector is Proportional to the radiance it receives."]
[7.28164529800415, 1.4511971473693848, "The Conference Presentation Date of the EO-1 Satellite is Aug. 13-16, 2007."]
[6.562081813812256, 0.37724876403808594, "The Image Release Date of the SMART-1 Satellite is March 03, 2008."]
[7.937376022338867, 7.311516761779785, "The Test Locations of the FG Calibration Device is Air, vacuum conditions, 10000-class clean room, solar telescope."]
[8.524014472961426, 10.471409797668457, "The CCD Line Pixel Count of the Focal Plane Module Imaging Device is 12,000 pixels."]
[7.672492980957031, 9.238844871520996, "The Measurement Spectral Region of the Sounder Instrument Instrument is 4-5 \u00b5m."]
[8.059575080871582, 0.8930708765983582, "The Launch Year of the Landsat-7 Satellite is 1999."]
[3.8222873210906982, 2.3007378578186035, "The Cube Size of the Orbit Your Thesis! 2019 program Education Program is 1U."]
[7.26136589050293, 5.684759616851807, "The pH of the Marine Chemistry Study Parameter is Unknown."]
[7.143825054168701, 4.380795001983643, "The Measurement Domain of the Badr-B Satellite is Gravity and Magnetic Fields."]
[11.191834449768066, -1.5286405086517334, "The Mass of the ASTERIA CubeSat is 12 kg."]
[11.624938011169434, 0.4555705487728119, "The Total Rock Mass Returned of the Apollo Missions Lunar Sample Return Missions is 382 kg."]
[6.981348037719727, 4.388838768005371, "The Observation Target of the Satellite Satellite is 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, droug."]
[8.872987747192383, 7.129531383514404, "The Measurement of the WISPR Instrument is Solar Wind Structures."]
[4.079623222351074, 5.810178756713867, "The S-band Downlink Modulation of the UoSAT-12 Satellite is BPSK."]
[9.42313003540039, 8.633633613586426, "The Material of the Heat Rejection Mirror Optical Component is Vacuum deposited silver."]
[8.097410202026367, 0.8678687214851379, "The Article Date of the Landsat 9 Satellite is 9 January 2020."]
[3.922744035720825, 2.296661376953125, "The Size of the CAPSTONE 12U CubeSat is Small microwave oven."]
[11.84411907196045, -1.073159098625183, "The Mass of the SA-200HP Spacecraft Platform is Launch mass of 2780 kg; dry mass of 1512 kg."]
[6.92533016204834, 1.1843504905700684, "The Presentation Date of the SI-200 Mini-Satellite Platform Satellite Platform is Oct. 12-16, 2009."]
[6.009476661682129, 9.032946586608887, "The Power of the Sun sensors Sensor is < 0.1 W."]
[6.266502857208252, 2.1775152683258057, "The Inherited Features of the Jason-3 Satellite is Orbit, instruments and measurement accuracy."]
[12.139107704162598, 3.290428876876831, "The Inclination of the Satellite PAZ is 97.44\u00ba."]
[8.356123924255371, 9.586812019348145, "The Detector Pixel Size of the Instrument Spectrometer is 13 \u00b5m x 13 \u00b5m (VIS); 40 \u00b5m x 40 \u00b5m (NIR)."]
[4.378444194793701, 5.669787883758545, "The TT&C of the Spacecraft Satellite is S-band (32 kbit/s in up- and downlink)."]
[6.240542888641357, 6.062335968017578, "The Calibration Modes of the SAR Instrument SAR Instrument is Interferometric calibration mode, Amplitude/phase distortions measurement mode."]
[7.966968536376953, 1.3762776851654053, "The Publication Date of the Lunar Flashlight Satellite is 15 July 2015."]
[8.072731971740723, 8.03215503692627, "The Microbe Types of the Experiment Microbiology is Halorubrum chaoviatoris and Bacillus subtilis."]
[8.925211906433105, 8.88138484954834, "The Line of Sight Range of the TIR Subsystem Imaging System is \u00b1 8.54\u00ba in the cross-track direction of nadir."]
[4.542868137359619, 3.692939043045044, "The Payload Location of the AIS Automatic Identification System is On board PAZ."]
[9.227396011352539, 6.234736442565918, "The Purpose of the Camera System Attitude Determination and Observation is 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."]
[6.9485650062561035, 8.908858299255371, "The Spectral Bands of the LISS-IIM Instrument is 0.45-0.52 \u00b5m, 0.52-0.59 \u00b5m, 0.62-0.68 \u00b5m, 0.77-0.86 \u00b5m."]
[9.386017799377441, 4.048976898193359, "The Diameter of the LAGEOS Satellite is 60 cm."]
[4.637062072753906, 5.497252464294434, "The Communication System of the TRMM Satellite is Four radio frequency (RF) links."]
[6.94413948059082, 4.675859451293945, "The Objective of the Experiment Satellite is Demonstrate global and real-time space weather observations of near-Earth space."]
[8.456522941589355, 8.355914115905762, "The Size of the Integrated Sensor Sensor is 8 mm x 3 mm x 19 mm."]
[7.850633144378662, 6.904360771179199, "The Operation End of the Experiment Unknown is Mid-1975."]
[6.9219818115234375, 4.645606994628906, "The Data Types of the Cheollian 2B Satellite is Marine image data, Ocean color images."]
[7.832055568695068, 6.195384502410889, "The In-flight Calibration of the SOSP Satellite is Provided."]
[6.547458171844482, 2.1043314933776855, "The Data Usage of the EnviSat Satellite is Studying and monitoring the Earth's environment."]
[7.267371654510498, 9.87647819519043, "The Instrument Power of the Hyperion Imaging Spectrometer is 78 W."]
[8.568246841430664, 3.7120749950408936, "The Latitude Coverage of the ERS-1 Satellite is \u00b1 81.5\u00ba."]
[5.930085182189941, 2.8728222846984863, "The Consortium Lead of the Satellites around the Moon Satellite Constellation is SSTL Lunar."]
[4.787006855010986, 0.8263644576072693, "The Contract Value of the HDEV High-Definition Earth-Viewing System is US$65 million."]
[10.477396965026855, 8.439840316772461, "The Image Recording of the Coronagraph Instrument is 35 mm film."]
[6.907392978668213, 4.959019184112549, "The Threat of the U.S. Midwest Region is Agricultural productivity is being threatened by climate change."]
[4.38705587387085, 5.318540096282959, "The Redundancy of the SGR-10 Space GPS Receiver is Redundant pair."]
[6.790384769439697, 4.509374618530273, "The Purpose of the Nimbus-7 Satellite is Testing of advanced systems for sensing and collecting data in the atmospheric, oceanographic and meteorological disciplines."]
[9.137368202209473, 9.362554550170898, "The Angle of the Nadir FOV Field of View is 75\u00ba."]
[7.774086952209473, 2.148591995239258, "The Function of the Exo-Brake Parachute is Enable Safe Return for Small Spacecraft."]
[9.787153244018555, 6.634181976318359, "The Function of the TechEdSat-10 Satellite is High temperature, accurate deorbit reentry."]
[10.420295715332031, 2.5044949054718018, "The Orbit Apogee of the Beijing-3B Satellite is 627 km."]
[4.443729877471924, 6.022493839263916, "The Function of the Electra Radio is Relay data from a rover or stationary lander to an orbiter passing overhead."]
[9.581086158752441, -0.7158986330032349, "The Purpose of the IDEA OSG 1 Microsatellite is Tracking and mapping of space debris."]
[7.851358413696289, 4.092219352722168, "The Imagery Collection of the Satellogic Satellite Imaging Company is 10 times as much imagery."]
[1.042592167854309, 4.337576389312744, "The Battery Configuration of the EPS Electric Power Subsystem is 8 in series."]
[5.961190223693848, 9.5689115524292, "The Mass of the OCM Instrument is 78 kg."]
[8.211384773254395, 9.423826217651367, "The Key Technology Elements of the MWIR Sensor Sensor is Integrated micro-cryocooler and a high temperature nBn based 1-Megapixel focal plane."]
[6.078590393066406, 3.8444716930389404, "The Operations Approach of the Twinkle Satellite is Streamlined, robust, safe, and high availability."]
[3.862722158432007, 5.717259407043457, "The Realtime Access Link Speed of the IRIS Satellite is 81 Mbit/s."]
[6.933152198791504, 3.037567138671875, "The Student Collaboration Goal of the IMAP Mission is Develop hands-on research experience for students."]
[11.323090553283691, 1.466962456703186, "The Number of Solar Panels of the Yutu 2 Lunar Rover is 2."]
[7.250751972198486, 5.124420166015625, "The CO2 Emission Source Resolution of the CO2Image Satellite is Below 1 Mt/year."]
[4.717212200164795, 1.681815266609192, "The Number of Satellites of the Galileo Satellite Navigation System is 26."]
[9.935493469238281, 7.7854695320129395, "The Energy Range of the HXD Detector is 10-60 keV."]
[7.369965076446533, 8.000845909118652, "The Average Concentrations in 1960s of the Ozone Layer Atmospheric Layer is 260 to 320 Dobson Units."]
[10.411444664001465, 7.879297733306885, "The Resolution of the X-ray Imager Instrument is < 0.22\u00ba."]
[5.663759231567383, 6.35725212097168, "The Length of the RF Antenna Mast Satellite Component is Nearly 12 m."]
[4.043893814086914, 6.525488376617432, "The Base Frequency of the DSN Link Signal is Approximately 9.6 MHz."]
[7.913256645202637, 9.982341766357422, "The Multispectral Bands Detector Array of the WV-3 Imager Imager is 9,300 pixel."]
[3.9759795665740967, 6.650345802307129, "The Telescope Aperture of the LCT Laser Communication Terminal is 135 mm."]
[5.471516132354736, 5.9416303634643555, "The Connection of the ROSA Radio Occultation Antenna Antenna is 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."]
[7.573741912841797, 8.058897972106934, "The Altitude of the LIMS Instrument is 153 km."]
[10.061110496520996, 3.0094451904296875, "The Orbit Height of the TerraSAR-X Satellite is 514 km."]
[5.925375461578369, 9.042815208435059, "The Power of the Star sensor Sensor is 4 W."]
[5.67872953414917, 2.81272029876709, "The Manufacturer of the NewSat-6 Satellite is Satellogic S.A.."]
[7.932734489440918, 9.731146812438965, "The Instrument Type of the AaSI Spectral Imager is Fabry-P\u00e9rot Interferometer (FPI)."]
[4.412665367126465, 4.719571113586426, "The Functions of the DFU Data Formatter Unit is CCSDS formatting, Reed-Solomon encoding."]
[4.618303298950195, 0.21678254008293152, "The Number of Satellites of the OneWeb Satellite Constellation is 650."]
[4.953096866607666, 6.46622371673584, "The Primary Structure Stiffness of the COMMx Payload is 50 Hz."]
[9.003256797790527, 5.2258501052856445, "The Pointing Locations of the SVOM Attitude Satellite Attitude is Near the equator, areas observable from both Hawaii, Chile and the Canary."]
[7.6372222900390625, 0.47495391964912415, "The Launch Date of the Meteor-M-1 Spacecraft is Sept. 17, 2009."]
[9.148232460021973, 4.228686809539795, "The Dimensions of the Node-3 Module is Diameter of 4.5 m and length almost 7 m."]
[7.050089359283447, 4.232815265655518, "The Measurement Category of the IRS-P6 Satellite is Multi-purpose imagery (land), Vegetation, Albedo and reflectance, Landscape topography, Sea ice cover, edge and thickness, Snow cover, edge and depth."]
[11.581564903259277, 6.173102378845215, "The Observation Date of the XMM-Newton Space Observatory is June 17, 2020."]
[7.87367582321167, 6.703008651733398, "The Observation of the FAUST Instrument is Large Magellanic Cloud galaxy."]
[7.095821857452393, 6.744257926940918, "The CDR Date of the TROPOMI Instrument is End of 2012, early 2013."]
[9.299226760864258, 5.712823390960693, "The Software of the ACS Attitude Control System is ACS flight software (FSW)."]
[11.070821762084961, -1.2580138444900513, "The Total Mass of the StudSat Picosatellite is 1.3 kg."]
[9.884967803955078, 4.414253234863281, "The ?V Capability of the ISEE-3 Spacecraft is About 310 m/s."]
[7.950125217437744, 8.214120864868164, "The Coil Cross-Sectional Area of the VLF Experiment Scientific Experiment is 42 cm2."]
[9.167946815490723, 3.2051918506622314, "The Orbit Type of the SPOT 1-5 Satellite is Sun-synchronous."]
[1.8011568784713745, 4.831784725189209, "The Power of the EPS Electrical Power Subsystem is 3 W (paddles closed), 5.9 W (paddles open)."]
[6.084283828735352, 3.1141250133514404, "The Funding Provider of the TanSat Satellite Mission is CAS (Chinese Academy of Sciences)."]
[7.586357593536377, 2.87162709236145, "The URL of the Picard Satellite is http://solarnet.projet.latmos.ipsl.fr/fichiers_pdf/pro_picard_SOLSPA.pdf."]
[9.675692558288574, 1.1652476787567139, "The Operation Duration of the SloshSat Satellite is 57.5 hours."]
[8.404393196105957, 10.117484092712402, "The Central Wavelength of the Current GOES imager Sensor is 3.90."]
[7.741567611694336, 9.096794128417969, "The Spectral Bands of the MESSR Radiometer is One visible (VIS) band and three thermal infrared (TIR) bands."]
[8.37137222290039, 9.248016357421875, "The TDI Lines of the R3 Sensor Sensor is 11, 19, 21, 21, 21, 21."]
[9.014518737792969, 4.819892406463623, "The Orientation of the Solar Panels Power Generation is Roll direction of the satellite."]
[6.673046112060547, 0.9701723456382751, "The Presentation Date of the FORMOSAT-3/COSMIC Follow-On Mission Satellite Mission is Aug. 11-14, 2008."]
[7.632987022399902, 7.983179569244385, "The Range of the SCM Satellite Charging Monitor is -3 pA/cm2 to +3 pA/cm2."]
[9.831438064575195, -1.0125168561935425, "The Number of Satellites of the JL-1-GF03D Microsatellite is 3."]
[11.125389099121094, 2.497357130050659, "The Diameter of the Schiaparelli Module is 2.4 m with heatshield, 1.65 m without heatshield."]
[5.022365570068359, 4.9696478843688965, "The Communication Capability of the Prometheus Satellite Satellite is 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."]
[10.189400672912598, 3.196971893310547, "The Data Acquisition Spacing of the SARAL/AltiKa Satellite is ~ every 180 m."]
[9.658210754394531, 3.9242794513702393, "The Thrust of the CanX-4&5 Satellite is 5 mN."]
[9.150815963745117, 9.160196304321289, "The Number of Elements of the Collecting Optics Lens Assembly is 8."]
[4.09134578704834, 1.220598816871643, "The Mission Type of the IDEA OSG 1 Satellite is Non-EO."]
[5.770462512969971, 6.870526313781738, "The Minimum Radar Reflectivity of the CPR Millimeter-Wave Radar is -35 dBZ."]
[7.319248676300049, -0.122504323720932, "The Launch Date of the H-IIB Launch Vehicle No. 6 Launch Vehicle is Oct. 7, 2016."]
[6.002288818359375, 6.367643356323242, "The Look Angle of the SAR Synthetic Aperture Radar is 20\u00ba."]
[6.655624866485596, 0.6379708051681519, "The Launch Year of the UWE-2 Satellite is 2006."]
[8.229840278625488, 10.235974311828613, "The Spectral Bands of the WFI Camera is VIS to NIR."]
[6.396260738372803, 4.213308334350586, "The Designation of the MTSAT Satellite is CNS/ATM system."]
[10.16551685333252, 6.89899206161499, "The Operation of the Thermal Control Louvers Thermal Regulation Device is Open up when the satellite needs to dissipate heat from its interior and close when the craft needs to warm up."]
[10.240042686462402, 2.975187301635742, "The Deployment Altitude of the Stingray Satellite is Approximately 500 km."]
[6.253628253936768, 0.8317410945892334, "The Operation Start Year of the Argos Satellite System is 1978."]
[6.647055149078369, 4.403249263763428, "The Measurement Category of the MTSAT Satellite is Cloud type, amount and cloud top temperature, Liquid water and precipitation rate, Surface temperature (ocean), Atmospheric Humidity Fields, Atmospheric Winds."]
[6.813614845275879, 4.335680961608887, "The Mission of the CRISTAL Satellite is Measure and monitor sea-ice thickness, overlying snow depth and ice-sheet elevations."]
[7.332335948944092, 0.6574820876121521, "The Launch Date of the PROBA-V-CC Satellite is October 9, 2023."]
[2.128730297088623, 4.639206886291504, "The Power Demand of the CMA/CM Component is 7.3 kW."]
[7.608564853668213, 3.9905004501342773, "The Observation Target of the Tandem-L Satellite is Earth\u2019s surface."]
[7.096261024475098, 2.447984457015991, "The Documentation Provider of the Aalto-1 Satellite is Herbert J. Kramer."]
[4.879181861877441, 4.7926130294799805, "The Better Uplink Verification Method of the Ground System Satellite Ground System is Recording the uplink RF signal at the ground site using a software-defined radio."]
[10.533157348632812, 7.5219879150390625, "The Material of the Gimbal Satellite Component is Silicon nitride."]
[7.410702705383301, 8.617136001586914, "The IFOV of the HIRS/4 Infrared Sounder is 10 km (0.7\u00ba)."]
[1.744829773902893, 4.801358222961426, "The Average Power Generation of the EPS Electrical Power Subsystem is 2 kW."]
[9.189994812011719, 6.306499481201172, "The Function of the Star Sensors Autonomous Star Sensors is Measure and report the S/C orientation relative to an inertial reference frame."]
[6.05922269821167, 0.9157835841178894, "The Deployment Timeframe of the Iridium NEXT Satellite Constellation is 2015-2017."]
[11.297934532165527, 4.205825328826904, "The Type of the Hot Jupiters Exoplanets is Star-hugging, superheated giants."]
[7.454337120056152, 0.8620108962059021, "The First Light Date of the Storm Hunter Satellite is 23 May 2018."]
[8.965906143188477, 7.348975658416748, "The Calibration of the MAG Sensor Sensor is Performed over a wide range of temperatures."]
[10.19549560546875, -0.8067883849143982, "The Imaging System Resolution of the GOMX-1 Nanosatellite is 35 m."]
[4.058626651763916, 4.517906188964844, "The Function of the Arduino-based processors Processors is Run other activity tasks such as interfacing with the payload, polling sensor data, and interfacing with the GPS."]
[5.05101203918457, 7.63054895401001, "The Energy of the Sub-mm Band is 1.4 meV."]
[9.629012107849121, 7.784245491027832, "The Energy Channels of the GALS-VE Particle Energy Measurement Device is > 600 MeV, > 800 MeV, > 1200 MeV."]
[5.087053298950195, 9.237574577331543, "The Principal Investigator of the SEIS Instrument Seismometer is Philippe Lognonn\u00e9."]
[7.196185111999512, 3.7109248638153076, "The System Name of the Whale Ecology Observation Satellite Satellite is Kanta-kun."]
[9.082703590393066, 9.187323570251465, "The Spatial Scale of the Telescope Optical Instrument is 2.8 arcsec/pixel."]
[3.743648052215576, 6.684189796447754, "The EIRP of the DRT Data Relay Transponder is 21 dBW (min)."]
[6.998028755187988, 4.665653705596924, "The Purpose of the LIRIS Rendezvous Sensor is Technology demonstration for future non-cooperative rendezvous applications."]
[7.873425006866455, 9.163022994995117, "The Wavelength Region of the Instrument Spectrometer is 400-970 nm (57 bands), 900-2500 nm (128 bands)."]
[11.239046096801758, 3.5195717811584473, "The Boulder Strength of the Comet 67P/C-G Comet is One hundred times weaker than freshly packed snow."]
[11.354132652282715, 4.480754375457764, "The Survey Density of the VIS Visual Instrument is At least 30 galaxies per arcmin2."]
[3.970823049545288, 4.577138900756836, "The Bus Type of the OBDH On Board Data Handling is ESA standard."]
[11.791330337524414, 1.6926343441009521, "The Imprint Size of the Philae Lander is 25 cm."]
[7.721579074859619, 0.33594685792922974, "The Launch Date of the Crew-3 Mission is Oct. 31."]
[10.291217803955078, 9.401311874389648, "The Observation Target of the IRIS Observatory is Sun's lower atmosphere just above the surface (chromosphere)."]
[11.68565845489502, -1.1545766592025757, "The Mass of the Spacecraft Satellite is 2.66 kg."]
[4.906670570373535, -3.2479612827301025, "The | of the Henry E. Revercomb Individual is Fred A. Best, Douglas P. Adler, Claire Pettersen, Henry E. Revercomb, P. Jonathan Gero, Joseph K. Taylor, Robert O. Knuteson, John H. Perepezko."]
[7.701270580291748, 3.1213698387145996, "The Series of the CartoSat-2E Satellite is Cartosat-2."]
[10.29551887512207, 4.922556400299072, "The Reaction Control Assembly of the EURECA Spacecraft is 6 x 21 mN nitrogen thrusters."]
[10.638904571533203, 9.210320472717285, "The Image Type of the CaSSIS instrument Imaging Instrument is Stereo pairs."]
[6.360138893127441, 1.7616126537322998, "The Conference Date of the Space-based ADS-B Surveillance System is Nov. 19-30, 2012."]
[5.204750061035156, 2.355515241622925, "The Team Structure of the HORYU-4 Satellite is Professors-staff, and students."]
[6.6309614181518555, 0.4463111460208893, "The Joint Tests Date of the CBERS 3 Satellite is March 29, 2011."]
[7.5340800285339355, 1.275517463684082, "The Operation Period of the S-193 Radar System is May 1973 to Feb. 1974."]
[4.484850883483887, 6.5438055992126465, "The Frequency of the Communication Payload Payload is Ka-band (27.0-31.0 GHz and 18.1-21.2 GHz)."]
[7.815793514251709, 8.828354835510254, "The GSD of the Instrument Satellite Instrument is 32m to 22m."]
[7.7811713218688965, 1.587031364440918, "The Conference Presentation Date of the Near Earth Asteroid Scout Satellite is 1 Aug 2014."]
[3.6656737327575684, 6.652161121368408, "The Data Rate of the X-band Transmitter Transmitter is 105 Mbit/s."]
[9.337151527404785, 1.7389249801635742, "The Conference Frequency of the JFCT Team is Once a week."]
[9.364542961120605, 1.8928006887435913, "The Global Coverage of the HARP-2 Satellite is 2 days."]
[3.846036434173584, 6.29326868057251, "The Channel Bandwidth of the TT&C Telemetry, Tracking and Command Subsystem is 25 kHz."]
[5.955488204956055, 6.223670482635498, "The Polarization Channel Transition of the SAR Processor Data Processor is 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."]
[9.307751655578613, -0.6780885457992554, "The Developer of the Venta-1 Nanosatellite is VVentspils High Technology Park."]
[1.7690494060516357, 5.292832374572754, "The Current of the Voltage 3 Digital is 350."]
[3.681459665298462, 6.0200886726379395, "The X-band Downlink Capacity of the PDHT Payload Data Handling and Transmission is 520 Mbit/s."]
[9.405482292175293, 5.116781711578369, "The Z-axis Rotation Rate of the Satellite Spacecraft is 1 rotation per minute (rpm)."]
[8.226820945739746, 3.207287311553955, "The Data Acquisition and Processing Concepts Presentation Date of the TanDEM-X Satellite is July 4-6, 2006."]
[3.302704334259033, 5.927493572235107, "The Technology of the Ground Station Communication System is SDR (Software Defined Radio)."]
[1.8726168870925903, 4.16071891784668, "The Area of the Solar Arrays Power Source is 18.3 m^2."]
[6.713075637817383, 2.1698861122131348, "The Launch Status of the FormoSat-7/COSMIC-2 Satellite Satellite is Cancelled."]
[8.074972152709961, 7.7595391273498535, "The Tracking Method of the Payload Measurement Device is Time-resolved optical density and absorbance measurements."]
[8.431727409362793, 0.17237646877765656, "The Operational Period of the ISS Space Station is Until 2028."]
[9.342972755432129, 7.424838542938232, "The Operation Sensitivity of the Electron Temperature Probe Instrument is Less sensitive to the potential sheath structure of its enveloped electrodes."]
[10.264827728271484, 8.712217330932617, "The ISS Components of the EUVI Extreme Ultraviolet Imager is EUVI secondary mirror as the actuator and GT as the high-accuracy angular motion sensor."]
[5.435513973236084, 3.4151604175567627, "The Operation Start Year of the CFESat Satellite is 2009."]
[5.44236946105957, 3.9249069690704346, "The Experiment of the CNES Space Agency is Automatic spacecraft maneuver planning and collision prediction in space."]
[6.18308162689209, 5.698593616485596, "The Data Service of the SGR-ReSI Interface Unit is Rapidly collect and invert the data into sea state."]
[6.951789855957031, 9.170926094055176, "The Azimuth Resolution of the Spotlight Imaging Mode is 3.4 m (dual pol.)."]
[9.63779067993164, 0.7439935207366943, "The Balloon Status of the AeroCube-3 Satellite is Ejected but did not inflate."]
[10.725085258483887, 10.280243873596191, "The Radiation tolerance of the PHA Detector is >100 krad."]
[8.775184631347656, 6.589982032775879, "The Function of the Translation Stage Actuator is Shift the alignment of the center of mass relative to the center of pressure."]
[7.716892719268799, 9.752574920654297, "The Spectral Bandwidth of the VNIR Spectrometer Spectrometer is 10 nm."]
[4.96399450302124, 4.792433261871338, "The Control Method of the Antenna Satellite Component is Commanded from ground station."]
[7.719427108764648, 13.591384887695312, "The Passband Range of the SPIM1 Spectrometer is 113-173 nm."]
[9.544873237609863, 1.022196650505066, "The Total Cruise Phase Duration of the Solar Orbiter Satellite is < 3 years."]
[6.434913158416748, 8.616456985473633, "The Spatial resolution at nadir of the MWRI Microwave Radiation Imager is 15-70 km."]
[17.728086471557617, 7.1627726554870605, "The J2000 declination (deg) of the B1509-58 Pulsar is -59.13583."]
[5.843711853027344, 4.7661333084106445, "The Role of the GIPSY-OASIS Software Package is Simulating DSAC\u2019s expected PCD performance."]
[7.385350227355957, 1.2373299598693848, "The Failure Date of the ISAMS Instrument is Late July 1992."]
[8.069108009338379, 0.8704236745834351, "The Year of Launch of the Landsat-7 Satellite is 1999."]
[9.153820037841797, 8.847715377807617, "The Scan Period of the Rotating Telescope Scanner Optical Instrument is 1.729 s."]
[8.802329063415527, 6.443648815155029, "The Solution of the BPP (Bi-axial Pointing Platform) Pointing Platform is Use existing gyroscopes on the HRC to improve the BPP pointing control."]
[9.677266120910645, -0.16947858035564423, "The Mission Design Life of the PARASOL microsatellite Satellite is One year."]
[7.548779010772705, 1.1958224773406982, "The Return Date of the Metcomp experiment Materials Science Experiment is SpaceX CRS-21."]
[1.840843677520752, 4.048138618469238, "The Manufacturer of the Solar Panels Power Generation is PrecizikaMET SC."]
[5.69728946685791, 3.2818105220794678, "The Payloads of the Satellite Satellite is IOV, Communication Payload of the German Ministry of Defense."]
[7.668355941772461, 1.5518262386322021, "The Date of the NASA Adds Up Alberto's Soaking Rainfall Event is 31 May 2018."]
[6.899488925933838, 4.387646198272705, "The Measurement Domain of the MTSAT Satellite is Atmosphere, Ocean."]
[1.1628519296646118, 4.223114490509033, "The Battery Model of the PSU Power Supply Unit is Lithium-ion battery of Saft (France), model: MP144350."]
[7.845141410827637, -0.5751309990882874, "The Press Kit URL of the SpaceX CRS-6 Mission is http://www.nasa.gov/sites/default/files/files/SpaceX_NASA_CRS-6_PressKit.pdf."]
[4.98996639251709, 4.565657138824463, "The Check-Conflict (National Harmonization) of the CSK GS Ground Segment is Verify if any sensing request is conflicting with any others and submit the final harmonized Service Request list to the FM GS."]
[7.65741491317749, 8.906740188598633, "The Observed Emissions of the MIGHTI Instrument is O(1D)@630.0 nm, O(1S) @ 557.7 nm, 0-0 band of O2(b1Sg+) @762.0 nm."]
[7.25229549407959, 8.323875427246094, "The Type of the PHI Instrument is Diffraction limited, wavelength tunable, quasi-monochromatic, polarization sensitive imager."]
[4.067751884460449, 2.249617099761963, "The Size of the GRIFEX Satellite is 3U CubeSat."]
[9.239934921264648, 9.16690444946289, "The Normalization at 1 keV of the First Broken Powerlaw Model Component is 5.7 photon cm-2 s-1 keV-1 ster-1."]
[8.228015899658203, 5.238797187805176, "The Objective of the GEOS-2 Satellite is Measurement of fluctuations in the magnetic field."]
[8.58974838256836, 1.7634468078613281, "The Mirror Technology Workshop Date of the JWST Telescope is June 16-18, 2009."]
[11.117177963256836, 5.1428422927856445, "The Expected Launch Date of the LISA Space Observatory is 2034."]
[7.807403087615967, 9.082969665527344, "The Value of the Spectral Stability Performance Requirement is Better than 0.02 nm."]
[9.481314659118652, 5.690036296844482, "The ADCS Systems of the OPS-AT Satellite is Two."]
[11.012832641601562, 7.176575183868408, "The Effective Sensitive Area of the HXT-C X-ray Optics is 70 cm2."]
[7.101079940795898, 0.1526767909526825, "The Launch Time of the BRO-6 Satellite is 6:49 p.m. Eastern."]
[5.213430404663086, 2.1747400760650635, "The Number of Students of the University of Sankore Educational Institution is 25,000."]
[5.734356880187988, 3.2704572677612305, "The Cooperation Agreement of the SSOT Satellite is Includes provision for Chilean engineers to work alongside the Astrium development team."]
[9.684109687805176, 7.633117198944092, "The Ion Isotropy Boundaries Energy Range of the ELFIN Satellite is 100-500 keV."]
[4.183514595031738, 4.903957843780518, "The Function of the HSM High-Speed Multiplexer is Collects ISP (Instrument Source Packets) in CCSDS format."]
[4.439049243927002, 5.302276611328125, "The Communication of the CICERO satellites Satellite is UHF up/downlink for TTC data."]
[11.560425758361816, 6.35127067565918, "The First Light Image Date of the SXT Soft X-ray Telescope is October 26, 2015."]
[5.809829235076904, 3.0167388916015625, "The Manufacturer of the GF-2 Satellite is CAST (China Academy of Space Technology)."]
[9.350826263427734, 2.1725106239318848, "The Trajectory Correction Maneuver of the MarCO-A CubeSat is Completed."]
[8.520587921142578, 7.378607273101807, "The Components of the DLRE Instrument is Instrument optics bench assembly (OBA), elevation/azimuth yoke, instrument mount."]
[11.638973236083984, -1.2225979566574097, "The Mass (kg) of the TanDEM-X Satellite is 1340."]
[9.398695945739746, 0.34072399139404297, "The Exceeded Design Life of the QuikSCAT Satellite is Yes."]
[8.397602081298828, 7.130378246307373, "The Channels of the Magnetic Field Measurement System Instrument is 8."]
[3.7252390384674072, 5.29329252243042, "The Downlinked Data of the Mission Operation System Data Processing System is 100 GB/day."]
[2.979550838470459, 6.589780807495117, "The Power of the GPS receiver Receiver is 5-7 W."]
[4.186424732208252, 1.3991754055023193, "The Mission Type of the ABEX CubeSat is Non-EO."]
[5.941186428070068, 3.8692898750305176, "The Components of the Look-Up Table Model is GFS (Global Forecast System) of the NCEP (National Center for Environmental Prediction)."]
[5.4533843994140625, 4.0229105949401855, "The Design Phase Start of the Emergency Egress System Safety System is 2019."]
[7.194995403289795, 3.461404800415039, "The Unknown of the Myriade Satellite Platform is Unknown."]
[9.282206535339355, 7.863131046295166, "The Operating Temperature of the Mid-infrared detectors Detector is 7 K."]
[11.697632789611816, -1.2010825872421265, "The Mass (kg) of the ALOS-1 Satellite is 4000."]
[9.101038932800293, 7.583643436431885, "The Form Factor of the LINAS Ionization Gauge is 1U CubeSat."]
[5.969560623168945, 0.7699217796325684, "The Presentation Date of the NANOSATC-BR Cubesat Program Satellite Program is Oct. 10-13, 2012."]
[7.853680610656738, 0.47167807817459106, "The International Space Station Operations Update Date of the UrtheCast Company is April 3, 2014."]
[1.167171597480774, 3.8203461170196533, "The Radiation Protection of the CUTE-1.7 Picosatellite is Mentioned."]
[10.04122257232666, 4.892860412597656, "The Propulsion Systems Quantity of the MTG Satellites Satellite is 6."]
[8.186156272888184, 2.4935097694396973, "The Resupply Mission of the ARTEMIS Satellite is Successful."]
[7.49427604675293, 9.918913841247559, "The Scene Size of the Instrument Hyperspectral Imager is 5 km x 20 km."]
[10.493868827819824, 2.5052807331085205, "The Apogee (km) of the Cosmos-1066 (Astrofizika) Satellite is 908."]
[9.849610328674316, 1.4918938875198364, "The Receiver Recovery Time of the RAX-1 Satellite is Within 100 microseconds."]
[8.150553703308105, 2.0691990852355957, "The Launch Date for Artemis 1 of the SLS Rocket Rocket is Unknown."]
[5.777368545532227, 3.1386525630950928, "The Manufacturer of the TRMM Satellite is NASA\u2019s Goddard Space Flight Center."]
[8.80981731414795, 3.6921355724334717, "The Nominal Along-Track Separation of the EO-1 Satellite is One-minute (450 km), \u00b1 6 s (42.5 km)."]
[6.633211135864258, 4.551419258117676, "The Data Transmission Mode of the Satellite Imaging Satellite is Recording (R) with subsequent reproduction(DR)."]
[6.3232197761535645, 6.3219313621521, "The Types of the Data Products Data is 3-hourly, 6-hourly and daily products."]
[5.513060092926025, 3.479673385620117, "The Design Approach of the Satellite Bus Satellite Component is Commercial-off-the-shelf (COTS) products."]
[9.488313674926758, 1.8430256843566895, "The Imaging Frequency of the Pelican Satellites Satellite is More than 10 photographs a day."]
[6.5807905197143555, 0.7840321660041809, "The Meeting Date of the GOSAT TANSO-FTS Spectrometer is June 18-20, 2012."]
[5.767519950866699, 6.491992950439453, "The Signal Wavelength of the S-band SAR Radar is About 4 inches (10 cm)."]
[10.006307601928711, 3.090944290161133, "The Altitude of the ICEYE-X10 Satellite is 500 km."]
[10.142719268798828, 7.000341892242432, "The Function of the TET Radiator Thermal Interface is It is small enough to prevent an out cooling of the system during \"cold\" phases."]
[9.454391479492188, 1.3396683931350708, "The Temporal Sampling of the Aeolus Satellite is 12 hours."]
[9.62621021270752, 8.617051124572754, "The Number of Flat Mirrors of the Refocus Mechanism Assembly Mechanism is 2."]
[8.100358963012695, 8.193839073181152, "The Modules of the IASI-NG Instrument Spectrometer is Optical Head (I-OH) and Electronics Module (I-EM)."]
[3.9747016429901123, 2.3403067588806152, "The Platform Space of the ITASat CubeSat Satellite is 4U."]
[12.103981971740723, 2.164066791534424, "The Last Flyover Date of the OSIRIS-REx Spacecraft is April 7, 2021."]
[11.264893531799316, 6.748410224914551, "The Operation Modes of the NICER X-ray telescope Telescope is 2-axis gimbal, tracking celestial X-ray sources, pointing towards ELC 3."]
[7.236918926239014, 1.544364094734192, "The Publication Date of the Cluster Satellite is 19 December 2014."]
[7.591776371002197, 8.190350532531738, "The Noise of the Radiometry Sensor is < 0.8 Wm -2  sr -1."]
[8.519632339477539, 9.013775825500488, "The Spatial Sampling of the Instrument Spectrometer is 1 arcmin."]
[8.63035774230957, 10.616870880126953, "The Data Quantization of the WiFS camera Camera is 7-bit (radiometric resolution of 128 grey levels)."]
[1.0049879550933838, 4.308833599090576, "The Quantity of the NiH2 Batteries Power Subsystem is 5."]
[5.297358512878418, 6.41569709777832, "The Dimensions of the VDES Antenna Antenna is 62 x 62 x 73 cm."]
[6.9936041831970215, 1.6880043745040894, "The Conference Date of the Swarm Satellite is Oct. 4-8, 2010."]
[11.600066184997559, 6.112115383148193, "The Distance of X-ray jet from the Manatee\u2019s head of the XMM-Newton X-ray Observatory is Approximately 300 light years."]
[6.911181449890137, 4.7204437255859375, "The Support Initiative of the Copernicus program Satellite Program is Stocktaking exercise with a new observation-based service to monitor CO2 emissions resulting from human activities."]
[7.5875468254089355, 9.797811508178711, "The Beam width of the VNIR Band is 5.5 \u00b5rad."]
[8.302638053894043, 7.65725564956665, "The Design and Operation of the Tiny Ionospheric Photometer (TIP) Instrument is Not provided."]
[9.515058517456055, 0.5783714652061462, "The Operational Lifetime Requirement of the SST Satellite is 7.5 years."]
[11.175344467163086, 2.8986213207244873, "The Sampleability of the Site Nightingale Crater is High."]
[8.081421852111816, 8.839485168457031, "The GSD at nadir of the Imager Satellite Instrument is PAN: \u22642.5 m, MS: \u226410 m."]
[7.4011430740356445, 7.39954137802124, "The Cloud Imager of the Atmospheric-sounding instrument Spectrometer is Built-in."]
[4.077235221862793, 5.688683032989502, "The Downlink Data Rate of the NEMO-AM Satellite is 2Mbit/s."]
[6.4546589851379395, 3.3868112564086914, "The Agency of the ZACUBE-2 Satellite is SANSA, CPUT."]
[4.955430030822754, 2.1911885738372803, "The Number of Satellites of the EDSN Swarm Satellite Network is 8."]
[9.9181547164917, 9.549662590026855, "The Measured Quantity of the SAGE-III Instrument is Chemical composition of the atmosphere and the vertical distribution of aerosols and gaseous compounds."]
[11.71731185913086, 4.556623935699463, "The Distance from Earth of the NGC 3603 Star Cluster is 20,000 light-years."]
[5.241453170776367, 2.6987602710723877, "The Manufacturer of the POPSat-HIP-1 3U CubeSat is Microspace Rapid Pte Ltd.."]
[7.679520606994629, 9.606953620910645, "The Spectral Bands of the Geoton-1 Imaging Instrument is 8 bands in the VNIR spectral range."]
[11.339507102966309, 3.7859461307525635, "The Time to Reach Oort Cloud of the Voyager 2 Space Probe is About 300 years."]
[6.07669734954834, 3.150533437728882, "The Mission Lead of the SPARCS Satellite is Arizona State University."]
[8.149375915527344, 10.639010429382324, "The Single Shot Precision of the TDC-GPX Time-to-digital converter is 10 ps."]
[8.667393684387207, 3.3868508338928223, "The EPS Board of the MinXSS Satellite is Unknown."]
[11.68901252746582, 4.6306681632995605, "The Primary Star Mass of the M51-ULS X-ray Binary is 20 to 30 times the mass of the Sun."]
[5.009954452514648, 6.090407371520996, "The Flexible Mode Frequency of the Payload Satellite Component is Below 10 Hz."]
[10.27083683013916, 4.734170913696289, "The Fuel Tank Distribution of the Advanced Composition Explorer Spacecraft is One pair having approximately 20% more propellant than the other pair."]
[9.403935432434082, 0.9448745250701904, "The Nominal Lifetime of the TanDEM-X Satellite is 5.5 years."]
[7.289487361907959, 2.9951579570770264, "The Unknown of the Super Dual Auroral Radar Network Radar Network is Unknown."]
[8.142633438110352, 8.911354064941406, "The Spatial Resolution of the EO System Earth Observation System is ~50 m (goal)."]
[5.145500183105469, 1.6831215620040894, "The Deployment of the KickSat CubeSat is about 250 femtosatellites into LEO (Low Earth Orbit)."]
[1.4309452772140503, 4.395260334014893, "The Quantity of the BCR Battery Charge Regulator is 6."]
[8.946867942810059, 4.565659523010254, "The Secondary Structure Components of the S/C Satellite is N/S radiators, E/W panels, Earth-facing panel."]
[8.62865924835205, 10.563563346862793, "The Full Well Charge of the Imager Camera is 60,000 e -."]
[6.718876838684082, 7.112249851226807, "The Biomass Estimate Comparison of the GEDI Lidar Instrument is 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."]
[9.19455337524414, 7.497494220733643, "The Flux Limitation of the Sensor Gas Sensor is Limits the oxygen flux to the cathode."]
[8.778620719909668, 6.4278740882873535, "The Guidestar Selection of the Spacelab Instrument Pointing System Pointing System is Improvements."]
[7.198750972747803, 4.521795749664307, "The Data Validation of the TanDEM-X Satellite is Used additional remote sensing data to validate the calculated results and differentiate forest areas from non-forested regions."]
[5.381280422210693, 5.583185195922852, "The Minimum Number of Satellites for Navigation Fix of the T3000G2 receiver GPS Receiver is 4."]
[2.0157594680786133, 4.162437915802002, "The Design Life of the Solar Panels Power Source is Up to 15 years."]
[7.361187934875488, 8.840295791625977, "The Spectral Range (VIS) of the VHRR Very High-Resolution Radiometer is 0.55 - 0.75 \u00b5m."]
[5.826921463012695, 1.5343506336212158, "The Source of the Induced Pluripotent Stem Cells Cell Type is Adult cells genetically programmed to return to an embryonic stem cell-like state."]
[8.854028701782227, 8.19845962524414, "The 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 Sensor is 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]."]
[4.202416896820068, 5.8116607666015625, "The Data Rate of the Radio Subsystem Satellite Subsystem is Varying based on the channel capacity."]
[3.863032102584839, 5.697786808013916, "The Data Distribution Telemetry of the MTG SpaceWire Architecture Satellite Architecture is 295 Mbit/s (Imager S/C) and 557Mbit/s (Sounder S/C)."]
[7.75862455368042, -0.5330620408058167, "The End of Life Date of the SpaceX CRS-19 Mission is 7 January 2020."]
[5.355523586273193, 6.540613651275635, "The Antenna Array Size of the PR Phased Array System is 2 m x 2 m."]
[5.307080268859863, 6.762956619262695, "The 3 dB Beamwidth of the Satellite Device Unknown is 2.0\u00ba\u00b10.1\u00ba."]
[4.893191337585449, 6.9887895584106445, "The Type of the CITRIS Receiver is Tri-frequency."]
[7.636255264282227, 1.6579256057739258, "The Operation Start Date of the SMAP Satellite is May 19, 2015."]
[6.96174955368042, 8.672257423400879, "The Surface Resolution of the FREND Instrument is ~40 m."]
[6.254591464996338, 2.886007308959961, "The Owner of the RADARSAT Constellation Satellite Constellation is Canadian Space Agency (CSA)."]
[8.819026947021484, 10.232572555541992, "The CMOS Image Sensors of the C3D Instrument Imaging Device is 2."]
[8.414322853088379, 8.115907669067383, "The Detector Type of the DIDM Instrument is MCP (Microchannel Plate)."]
[7.353204250335693, 0.43350452184677124, "The Launch Date of the Aalto-1 Satellite is End of 2016."]
[7.589900493621826, 2.736455202102661, "The Capture and De-Orbit Capabilities of the ELSA-M Spacecraft Servicer is Innovative rendezvous, capture and de-orbit capabilities with a full-size constellation client."]
[5.989348411560059, 9.063525199890137, "The Power Consumption of the Photometer Instrument is \u2264 3.5 W."]
[8.251139640808105, 4.173159599304199, "The Coverage Area of the HawkEye 360 Satellite Constellation is Millions of square kilometers."]
[9.01333999633789, 7.765442848205566, "The Temperature of the Deep Space Calibration Reference is Approximately 4 K."]
[11.54097843170166, 3.8867435455322266, "The Bedrock Formation Age of the CaSSIS Instrument is Between 3.7 and 4.1 billion years ago."]
[6.173272132873535, 8.041146278381348, "The Platform of the 118 GHz Radiometer Radiometer is Aircraft."]
[6.5937113761901855, 3.0343127250671387, "The URL of the Resurs-P1 Satellite is http://www.russianspaceweb.com/resurs_p.html."]
[7.481969356536865, 9.90151596069336, "The Spatial Resolution of the SMI Spaceborne Multispectral Imager is 80 m."]
[5.246000289916992, 3.1152713298797607, "The Bus Name of the NorSat-1 Satellite is NEMO platform."]
[4.768682956695557, 5.435461044311523, "The Data Transmission Subsystem of the Sentinel-1, -2, and -3 Satellites is X-band TXA (Transmission Assembly)."]
[2.056303024291992, 3.879448413848877, "The Solar Arrays of the UK-DMC-2 Satellite is Three body-mounted heritage solar arrays."]
[8.21414852142334, 2.2045845985412598, "The Test Flight of the Orion Spacecraft is Artemis I."]
[5.970097541809082, 8.470052719116211, "The System Type of the GeoSTAR Atmospheric Microwave Sounder is 2-D spatial interferometric system."]
[4.893238067626953, 4.75685977935791, "The Data Transmission of the McMurdo Ground Station Ground Station is Real-time."]
[3.6736257076263428, 4.302810192108154, "The Compression Type of the DHU Data Handling Unit is Online lossless and lossy."]
[8.908021926879883, 10.317890167236328, "The Modes of the Payload 2 CMOS Camera is VGA/QVGA."]
[8.29075813293457, 0.3221192955970764, "The Project Team Size of the CIMON Astronaut Assistant is Approximately 50."]
[6.333240032196045, 11.88387680053711, "The Sensitivity of the Three-axis diagonal gradiometer Gradiometer is < 10 -12  m s -2  Hz -1/2."]
[9.218172073364258, 3.205613851547241, "The Orbit Type of the Satellite Communication is Sun-synchronous near-circular polar orbit."]
[1.2149814367294312, 4.158317565917969, "The Battery Type of the Sail Power Source is Lithium-ion."]
[6.231167793273926, 1.8127720355987549, "The International Headquarters Establishment Date of the Spacety Company is 2019."]
[8.566347122192383, 2.7658562660217285, "The Role of the Martin Popek Individual is His photos add another dimension to the research."]
[4.057260990142822, 1.2080254554748535, "The Mission Type of the CHOMPTT Satellite is Non-EO."]
[2.005084991455078, 3.939732789993286, "The Power Source of the GHGSat-D Microsatellite is Body-mounted solar cells."]
[7.527880668640137, 9.931573867797852, "The Spectral Bands of the SMI Spaceborne Multispectral Imager is Visible (420\u2013700 nm) and near infrared (650\u20131050 nm)."]
[11.621734619140625, 2.626368999481201, "The Diameter of the Ryugu Asteroid is 900 m."]
[10.743868827819824, 3.3764684200286865, "The Distance from the Sun of the Voyager 1 Space Probe is Beyond the heliosphere."]
[10.2472505569458, 6.822741985321045, "The Control Type of the Thermal Control Subsystem Subsystem is Passive."]
[5.4016313552856445, 4.134178638458252, "The Components of the MOC Mission Operations Center is Mission planning software, data management system, spacecraft ground terminal."]
[10.740884780883789, 5.510349750518799, "The Effect of the Solar Storms Natural Phenomenon is Affected a variety of technological systems around the world."]
[7.6584882736206055, 8.499690055847168, "The Limb-Sounding Concept/Technology Test of the OMPS UV Hyperspectral Imaging Spectrometer is ISIR (Infrared Spectral Imaging Radiometer) flown on Shuttle flight STS-85 (Aug. 7-19, 1997)."]
[7.287636756896973, 7.837792873382568, "The Observation Time of the MOMS-2P Instrument is 3 minutes/day."]
[8.763177871704102, 1.509130597114563, "The Whistler Waves Energy Transfer of the Van Allen Probes Satellite is From copious low-energy particles to sparse high-energy particles."]
[11.537239074707031, 6.024346828460693, "The Science Outcomes of the NICER X-ray Timing Instrument is 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."]
[6.685713768005371, 1.2027281522750854, "The Contract Date of the Capella Company is 17 June 2021."]
[9.550758361816406, 7.897881984710693, "The Energy Range of the ULEIS Spectrometer is About 20 keV/n to 10 MeV/n."]
[10.675293922424316, -1.5546106100082397, "The Cargo Load for Return of the SpaceX Dragon Spacecraft is ~720 kg."]
[5.420175075531006, 2.3161566257476807, "The Mission Status of the QBITO CubeSat is Mission complete."]
[3.391568899154663, 4.35054874420166, "The Power Lines for SVM-PDU and FPA-PDU of the MRU Main Regulator Unit is 2 x 2."]
[4.601156234741211, 5.979020118713379, "The Unknown of the FlexRX Receiver Communication Device is Unknown."]
[8.0863676071167, 1.3230571746826172, "The Date of the Volcanic Eruption Lights Up Iceland Image is 23 March 2021."]
[10.637289047241211, 9.205439567565918, "The Image Capture Date of the CaSSIS camera Camera is 13 June 2021."]
[10.016016006469727, -0.742225170135498, "The Maximum Microsatellite Dimensions of the NanoRacks Microsat Deployer Satellite Deployer is 95 cm x 83 cm x 64 cm."]
[7.489918231964111, 9.931696891784668, "The Conference Presentation of the EarthCARE Multi Spectral Imager Imaging System is SPIE Remote Sensing Conference, Toulouse, France, Sept. 20-23, 2010."]
[5.280830383300781, 4.6930670738220215, "The Platform Data Rates of the Argos System Data Collection System is Higher."]
[11.986042976379395, 3.3973302841186523, "The Orbit Inclination of the ISS Space Station is 51.6\u00ba."]
[9.525288581848145, 0.41134965419769287, "The Design Life of the GaoJing / SuperView minisatellites Satellite is 8 years."]
[7.176568031311035, 5.79201602935791, "The Accuracy of Wind Velocity (PBL) of the Aeolus Satellite is 2 m/s."]
[9.003880500793457, 3.236738920211792, "The Satellite Orbit of the Satelles PNT Service Provider is LEO."]
[9.747077941894531, 1.4890598058700562, "The Growth Rate Approximation of the C/NOFS Satellite is Linear."]
[7.334864139556885, 3.6329243183135986, "The Observation Geometry of the Satellite Unknown is Limb."]
[10.361849784851074, 2.889709234237671, "The Orbit Altitude of the GRIFEX 3U CubeSat is ~ 650 km."]
[10.935087203979492, 4.219852924346924, "The Purpose of the WFIRST Telescope is Directly image exoplanets by blocking out the light of their host stars."]
[7.438610076904297, 1.3769230842590332, "The Approval Date of the Sentinel Asia Disaster Risk Management System is October 2005."]
[5.140995025634766, 1.2172188758850098, "The Number of Terran R launches of the Terran R Launch Vehicle is More than 20."]
[7.525847434997559, 8.134601593017578, "The Polarization Measurement of the TANSO-FTS Sensor is P and S polarization."]
[9.636693000793457, -0.31297534704208374, "The Mission Design Life of the Microsatellite Satellite is \u2265 2 years."]
[5.633672714233398, 2.801501989364624, "The Purpose of the Hiber-3 smallsat Satellite is Provide satellite connectivity to \u201cinternet-of-things\u201d (IOT) devices."]
[8.25274658203125, 8.82424545288086, "The Optical Configuration of the Spectrometer Spectrometer is Czerny-Turner."]
[9.603307723999023, 8.65746784210205, "The Mirror Surfaces of the Limb Imager Telescope is Fully free-form."]
[8.66355037689209, 9.722813606262207, "The Synergy products of the OLCI Camera Assembly is Based on combination of OLCI and SLSTR data."]
[11.966530799865723, 4.466681003570557, "The Observation Date of the Orion A Nebula is 18 November 2019."]
[5.977948188781738, 9.497899055480957, "The Mass of the LISS-IIM Instrument is 80.8 kg."]
[9.169381141662598, 8.789619445800781, "The Material of the Focal Plane Array Detector Array is SiC."]
[7.805478096008301, 2.78432035446167, "The Origin of the Sample Return Capsule Capsule is NASA Stardust mission."]
[7.050853252410889, 0.08762418478727341, "The End of Life Date of the Solar-A / Yohkoh Satellite is 23 April 2004."]
[4.121199131011963, 7.2884297370910645, "The Mass of the MHX-2400 S-band Transmitter/Transceiver is 75 g."]
[4.391860008239746, 5.710659027099609, "The IFOV of the Satellite Communication is Very large."]
[6.414205074310303, 8.23314380645752, "The Frequency Range of the Copernicus Imaging Microwave Radiometer (CIMR) Radiometer is 1.4\u201336.5 GHz."]
[7.260217189788818, -0.7331342697143555, "The Mission Status of the CYGNSS Satellite Constellation is On Track."]
[7.748275279998779, 8.702969551086426, "The Vertical Range of the SAGE-III Spectrometer is 0 km to 100 km."]
[9.427813529968262, -0.27890390157699585, "The Mission Objective of the FASTRAC Satellite is Investigate enabling technologies crucial for satellite formations, including on-orbit micro-thrust capability, relative navigation, attitude determination, and satellite crosslink communications."]
[6.756011486053467, 5.511368274688721, "The Radar of the Soil Moisture Active Passive (SMAP) Satellite is L-band."]
[7.652734279632568, 7.29343843460083, "The Complementarity of the IMAP-Ultra Instrument is Complements the measurements of IMAP-Lo and IMAP-Hi."]
[5.251769065856934, 4.712731838226318, "The Location of the DRS Data Reception Station is Shadnagar, Hyderabad."]
[4.907000541687012, 6.02621603012085, "The Frequency Range of the Variant Satellite is 0.1 Hz to 40 kHz."]
[9.197216033935547, 4.165327072143555, "The Dimensions of the ALTIUS Satellite is 800 x 800 x 1200 nm."]
[6.868027210235596, 6.2130632400512695, "The Wind Speed Accuracy of the SCAT Wind Measurement System is 10%."]
[7.344353199005127, 2.2348310947418213, "The Publication Date of the Orbiting Carbon Observatory Satellite is 2004."]
[4.86887788772583, 1.056016206741333, "The Estimated Growth Opportunity of the Hiber Satellite Network is \u00a33.5B."]
[7.263762474060059, 9.69472599029541, "The Instrument Size of the Hyperion Imaging Spectrometer is 39 cm x 75 cm x 66 cm."]
[5.162893772125244, 6.236943244934082, "The Experiment of the GeReLEO Smart Antenna Antenna is Test."]
[6.092103958129883, 0.5970129370689392, "The Launch Date of the ELaNa V CubeSat is March 2014."]
[8.005576133728027, 9.725671768188477, "The Bands of the PMC Imager is NIR and three visible (blue, green and red)."]
[9.65063762664795, 1.360189437866211, "The Forecast Mode Duration of the C/NOFS Satellite is 3 months required, 27 month goal."]
[2.131162166595459, 4.553786277770996, "The Payload Power of the Heinrich Hertz Satellite is 3.6 kW."]
[7.510850429534912, 7.026243686676025, "The Launch Provider Announcement Date of the TEMPO Pollution Monitoring Instrument is 18 March 2020."]
[5.362926483154297, 2.1434032917022705, "The Plaque Content of the LAGEOS Satellite is Binary numbers, Earth orbiting the sun, Maps of Earth at different epochs."]
[2.011296510696411, 3.8804192543029785, "The Solar Cells of the SCARAB 1U CubeSat bus is Spectrolab triple-junction CIC solar cells (body-mounted)."]
[6.065647125244141, 3.482755184173584, "The Operational Requests Management of the TDP Operations Satellite Operations is Managed at a top level by ESA."]
[7.684416770935059, 7.615447521209717, "The Instrument Type of the OCO-3 Instrument is Atmospheric chemistry."]
[4.752419471740723, 1.8221757411956787, "The Orbital Planes of the T1TL Prototype Constellation Satellite Constellation is 2."]
[6.934878349304199, 9.181910514831543, "The Azimuth Resolution of the Spotlight Imaging Mode is 1.7 m (single pol.)."]
[6.403091907501221, 8.522956848144531, "The Spatial resolution of the Microwave System Microwave System is 19-260 km."]
[8.918984413146973, 7.118132591247559, "The Measurement of the WISPR Instrument is Solar Wind Properties."]
[10.499271392822266, 6.092743396759033, "The Technology of the Micro-gravity experiment Experiment is 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."]
[9.83486270904541, 2.550321340560913, "The Planned Quantity of the Surface Rovers Deployment Maneuver is Four."]
[5.694228172302246, 3.112316846847534, "The Owner of the Hosted Payload Satellite Payload is German Federal Ministry of Defense (BMVg)."]
[6.326436996459961, 1.8496495485305786, "The Deployment Status of the Aireon Air Traffic Surveillance System is Closer to Complete."]
[5.067089557647705, 7.564311504364014, "The Data Rate of the LEID Instrument is 1 kbit/s."]
[5.278920650482178, 6.890510559082031, "The IFOV (beam width) of the Antenna Reflector is 5.3\u00ba."]
[7.145366191864014, 0.7630236744880676, "The Announcement Date of the Nearby star HR1099 Satellite is Jan. 30, 2000."]
[8.506491661071777, 7.476996898651123, "The Function of the SES Instrument is Confirm predictions of thermionic and photoelectric emission."]
[10.049546241760254, 1.5288925170898438, "The Orbit Period of the Primary Mission Satellite is 101 minutes."]
[4.877588748931885, 1.9567571878433228, "The Number of Satellites of the SkySat-16 to -18 Satellite is 3."]
[9.552988052368164, 8.697345733642578, "The Ground Sample Distance of the HPT High Precision Telescope is 3 m."]
[5.6268839836120605, 5.101009845733643, "The Build Location of the Hardware Quick Look SAR Processor SAR Processor is Ahmedabad."]
[1.9760313034057617, 5.5552659034729, "The Voltage of the Voltage 2 Power Amplifier is -5.5\u00b15%."]
[9.459498405456543, 9.040122032165527, "The Focal Length of the Telescope Optical Instrument is 2000 mm."]
[8.774222373962402, 10.05923080444336, "The Subaperture Quantity of the SMART Imaging System is Four and eight."]
[9.07060432434082, 10.582123756408691, "The Resolution of the M-CAM 1 Monitoring Camera is 1024 x 1024 pixels."]
[8.061466217041016, 8.751870155334473, "The Observables of the LIMS Limb Infrared Monitor is O3, H2O, NO2, HNO3 and temperature."]
[10.09451961517334, 2.1130564212799072, "The Stability Requirement of the Lunar Orbit Orbital Phase is Orbit where the spacecraft doesn\u2019t impact the surface for at least 6 months."]
[11.589385032653809, 6.017024517059326, "The Image Interval of the IBIS X-ray Imager is Roughly eight minutes."]
[6.948112964630127, 4.009655475616455, "The Objective of the Sich-2 Satellite is Obtain high-resolution imaging data in the visible and infrared region."]
[8.030769348144531, 8.70582103729248, "The Sensitivity of the LDEX Instrument is Especially sensitive to the metallic compounds of minerals and any species which easily form ions (e.g. water)."]
[7.764649391174316, 9.159449577331543, "The GSD of the Spectral Band B Spectrometer is 5."]
[7.9719319343566895, 1.4661720991134644, "The Observation Date of the Solar Dynamics Observatory Satellite is July 30, 2011."]
[11.65485954284668, -1.1377400159835815, "The Launch Mass of the HY-1C Satellite is 442 kg."]
[6.819674491882324, 7.589570045471191, "The Modes of the MRSE Instrument is SAR, Scatterometer, Radiometer."]
[6.342029571533203, 4.345820426940918, "The Science Objectives of the TROPICS Constellation of CubeSats is Relate the retrieved environmental moisture measurements to coincident measures of storm structure (including size) and intensity."]
[6.1231865882873535, 6.503963470458984, "The Frequency Bands of the Copernicus Sentinel-6 Poseidon-4 Radar Altimeter is C- and Ku-band."]
[4.020435810089111, 6.490468978881836, "The Bandwidth of the Spacecraft Repeater Communication Device is 25 kHz."]
[4.496534824371338, 6.55893611907959, "The Components of the Receiver Communication System is Low noise preamplifier with BFS17, LNA (Low Noise Amplifier), first mixer NE602, crystal filter, intermediate frequency amplifier A281D, last mixer NE602."]
[6.94175386428833, 0.48739737272262573, "The Launch Date of the GEOS-2 Satellite is Jan. 11, 1968."]
[5.7906270027160645, 6.354908466339111, "The SAR Payload Orbit Average Power Consumption of the RCM Satellite is Approximately 200 W."]
[7.503541946411133, 1.8054925203323364, "The On-ground and In-orbit Calibration Presentation of the Microscope Space Mission is 2010."]
[7.046806812286377, 0.3990189731121063, "The Launch Date of the SPOT-2 Satellite is January 1990."]
[11.767303466796875, 4.963705062866211, "The Distance to Galaxy of the GRB 031203 Gamma-Ray Burst is Less than 1300 million light years."]
[5.691714286804199, 9.205296516418457, "The Power of the STAFF/DWP Instrument is 5.0 W."]
[8.784090042114258, 6.989816665649414, "The Mounting of the SEP Solar Energetic Particles Instruments is On the spacecraft body."]
[6.997869968414307, 0.9854171276092529, "The Launch Year of the ALOS-2 Satellite is 2014."]
[5.825205326080322, 6.827692985534668, "The Sensitivity of the Radar Instrument is 1.7 dB."]
[10.093440055847168, 3.102726459503174, "The Orbit Altitude of the Aalto-1 Satellite is 505 km."]
[7.286472320556641, 7.871561527252197, "The Purpose of the Scale Factor Measurements System (SFMS) Measurement System is Measurement of the absolute laser frequency."]
[1.8574875593185425, 5.431015491485596, "The Power of the Voltage 1 Power Amplifier is 28 @ 28 V worst-case."]
[4.925123691558838, 1.6060270071029663, "The Production Rate of the Factory Facility is About one satellite per week."]
[11.046439170837402, 2.5694756507873535, "The Altitude of the Schiaparelli module Spacecraft is About 3.7 km."]
[7.057086944580078, 6.523626327514648, "The Flights of the AEPI Instrument is ATLAS-1."]
[9.635262489318848, 5.950169086456299, "The Attitude Stability of the ADCS Attitude Determination and Control Subsystem is \u22640.001\u00ba/s (3\u03c3, 3-axis)."]
[10.004851341247559, 1.520289421081543, "The Occultation Duration of the CTECS Satellite is 6 minutes."]
[4.823580265045166, 0.8443320989608765, "The Grant Amount of the SpaceChain Company is $596,000."]
[7.050689220428467, 2.597649574279785, "The URL of the Satellite Satellite is http://library01.gsfc.nasa.gov/gdprojs/projinfo/sage.pdf."]
[6.268012046813965, 2.9305694103240967, "The Manufacturer of the InSight Lander is Lockheed Martin Space in Denver."]
[9.129107475280762, 5.780703544616699, "The Components of the G&C system Guidance and Control System is Sun sensors, a ST (Star Tracker), redundant IMUs (Inertial Measurement Units), the GT, reaction wheel assemblies, and a monopropellant hydrazine propulsion system."]
[4.806405067443848, 0.8973862528800964, "The Goal Unit Cost of the Super Strypi Launch System is $12 million."]
[8.571215629577637, 8.367627143859863, "The Incident Angle of the Reflection Diffuser Calibration Device is \u03b8 inc. = 65\u00ba."]
[7.853628158569336, 1.928341269493103, "The Publication Date of the ISEE-1 Spacecraft is July 1978."]
[6.138153076171875, 5.462032318115234, "The Development Date of the PALSAR Ground Data System Ground Data System is 2004."]
[6.354736804962158, 3.267249822616577, "The Mission Goals of the ARMADILLO Satellite is Train students in best systems engineering practices by executing a complete spacecraft life cycle from concept design to mission operations."]
[8.128085136413574, 9.965813636779785, "The Manufacturer of the MWIR Imager Imaging Device is Leonardo."]
[4.518352508544922, 6.038833141326904, "The Beacon Transmission Rate of the ELFIN-B Satellite is 9600 baud."]
[9.157444953918457, 3.08789324760437, "The Orbit of the LunaH-Map Spacecraft is Stable circular orbit."]
[2.7225873470306396, 5.2759480476379395, "The Power Consumption of the OBIS Onboard Information System is 32 W."]
[6.3791913986206055, 1.6096283197402954, "The Meeting Date of the Jason-3 Satellite is Oct. 18-20, 2010."]
[8.532755851745605, 10.39865779876709, "The Signal Processing of the CCD Detector Detector is Fast electronics near the detector head."]
[7.987483024597168, -0.7235262989997864, "The Arrival Date of the Dragon CRS-14 Spacecraft is April 4, 2018."]
[5.058653831481934, 2.272690534591675, "The Number of Instruments of the ISEE-3 Satellite is 13."]
[8.133036613464355, 4.646042823791504, "The Swath Width of the Spotlight-2B Satellite is 10km."]
[6.245629787445068, 7.780930519104004, "The Polarization of the ICI-7 Radiometer is V."]
[7.644009590148926, 9.520793914794922, "The Swath of the SLSTR Spectral Imaging Instrument is 750 km."]
[9.520657539367676, 5.545966148376465, "The Design Concept of the AOCS Attitude and Orbit Control System is 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 contro."]
[7.424109935760498, 5.7814812660217285, "The Temperature Range of the Silicate Clouds Atmospheric Phenomenon is Between about 1,900 degrees Fahrenheit and 3,100 degrees Fahrenheit."]
[4.284862518310547, 6.077812194824219, "The Uplink Beacon of the RF Communications Communication System is CW (Continuous Wave) UHF beacon."]
[6.881965637207031, 1.1059021949768066, "The Capital Market Day of the Small GEO Satellite is February 11, 2009."]
[9.104336738586426, 10.194457054138184, "The Quantity of the Cameras Imaging is 2."]
[11.62024974822998, -1.1988801956176758, "The Mass of the exactView-1 Satellite is 100 kg."]
[2.211495876312256, 4.357795238494873, "The Payload Power of the Solar Orbiter Satellite is 180 W."]
[6.983829021453857, 0.18156419694423676, "The Launch Date of the VRSS-1 Satellite is September 29, 2012."]
[7.044261932373047, 2.4913289546966553, "The Report URL of the AAUSAT3 Satellite is http://zcuba.dk/reports/08gr633.pdf."]
[5.714049816131592, 2.9642837047576904, "The Bus Manufacturer of the THEMIS Probes Satellite is Swales Aerospace."]
[11.499706268310547, 4.172525405883789, "The Diameter Uncertainty of the KELT-11b Planet is Just under 4300 km."]
[5.6354594230651855, 3.8846256732940674, "The Operator of the BSOCC Satellite Operation Control Center is Bowie State University."]
[6.616096019744873, -0.10384602099657059, "The Launch Date of the PSLV Satellite Launch Vehicle is Dec. 16, 2015."]
[6.751916408538818, 3.566636800765991, "The Mission Type of the CryoSat Satellite is EO."]
[2.3293795585632324, 4.451454162597656, "The Operational Capability of the SSPIDR Project is Power 'on demand' anywhere on the globe regardless of weather or latitude, day or night and without vulnerable logistics lines."]
[7.4963908195495605, 4.162008762359619, "The Instrument 1 of the CryoSat-2 Satellite is DORIS."]
[5.640137672424316, 2.786792755126953, "The Development and Build Contractor of the SAR-Lupe Satellite System is OHB System AG."]
[6.824400424957275, 1.2988319396972656, "The Project Agreement Date of the YouthSat Satellite is January 25, 2007."]
[4.794393062591553, 1.8649373054504395, "The Number for Coverage Match of the LEO Satellites Satellite is Around 300."]
[8.745759963989258, 10.380311965942383, "The Image Sensor Pixel Size of the CMV4000 CMOS Color Detector is 5.5 \u00b5m."]
[7.9224934577941895, 6.7941389083862305, "The Frequency of the Full Calibration of HIS Calibration Process is Bimonthly."]
[2.27355694770813, 4.455376148223877, "The Power of the Spacecraft Satellite is 357 W (long-term), 1350 W (short-term)."]
[5.907355308532715, 9.11348819732666, "The Power of the Magnetometer Sensor is < 0.8 W."]
[8.367627143859863, 10.585244178771973, "The Power Consumption of the Image Sensor Imaging is 1 W."]
[7.890177249908447, 1.963867425918579, "The Arrival Date of the Europa Clipper Spacecraft is Early June 2022."]
[9.579360008239746, 5.96931791305542, "The Attitude Knowledge Stability of the ADCS Attitude Determination & Control Subsystem is \u2264 0.12 \u00b5rad in 2.5 seconds."]
[9.579777717590332, 5.516047477722168, "The Safe Mode Attitude of the AOCS Attitude and Orbit Control System is Earth-oriented."]
[9.425725936889648, 0.9403048753738403, "The Mission Duration of the RBSP spacecraft Satellite is 2 years."]
[11.568495750427246, -1.249540090560913, "The Satellite Mass of the Terra Bella Satellite Constellation is ~120 kg."]
[7.251121520996094, 7.0413079261779785, "The NEdT Performance of the VIIRS Instrument is Excellent."]
[7.682916641235352, 4.091067790985107, "The Observation of the ALOS/PALSAR Satellite is Magnitude-9.0 Earthquake off the Pacific coast of Tohoku-Kanto District in Japan in 2011."]
[7.624893665313721, 9.080135345458984, "The Total Channels of the Spectral Bands Spectrometer is 713."]
[7.24886417388916, 9.409697532653809, "The Swath Width of the MSU-E Multispectral Scanner is 28 km."]
[9.129810333251953, 6.304481029510498, "The Data Delivery Speed of the Quasar 3000 IMU Inertial Measurement Unit is 100Hz."]
[5.2761616706848145, 6.376616954803467, "The Type of the VDES Antenna Antenna is Folded dipole Yagi-Uda antenna with three elements in crossed configuration."]
[3.7044241428375244, 6.297244548797607, "The TT&C Downlink Data Rate of the RF Communications Communication Subsystem is 1.6 - 4 Mbit/s."]
[6.261528968811035, 0.3853681981563568, "The End of Life Date of the PSat-2 CubeSat is June, 2025."]
[8.022492408752441, 4.230461597442627, "The Scene Size of the ICEYE-X1 Satellite is 40 x 83.3 km."]
[9.43501091003418, 0.8676937222480774, "The Development Time of the CubeSat Satellite is 2 years."]
[6.830963134765625, 0.8609176874160767, "The Launch Date of the GFO Satellite is Feb. 10, 1998."]
[6.03633975982666, 2.650228977203369, "The | of the Capella Space Satellite Company is Capella Space Is First American Company to Send Advanced Commercial Radar Satellite to Space."]
[7.928017616271973, 4.387146949768066, "The Development Location of the LHASA Model Landslide Hazard Assessment Model is NASA/GSFC (Goddard Space Flight Center) in Greenbelt, Maryland."]
[8.22807502746582, 8.86482048034668, "The Operating Bands of the GAS Grating Spectrometer is Four NIR/SWIR bands."]
[8.327911376953125, 3.6090919971466064, "The Mission Overview of the GCOM-W Satellite is Not provided."]
[6.928069591522217, 0.6050377488136292, "The Image Capture Date of the ICEYE-X2 Satellite is Four days after the satellite's launch."]
[8.488648414611816, 9.488678932189941, "The Incident Angle Dependence of the Scanning Systems Optical System is Problematic."]
[7.651678085327148, 8.085362434387207, "The Extinction Cross Sections of the Species Atmospheric is Wavelength Dependent."]
[9.333540916442871, 10.225837707519531, "The Field of View of the MSC Camera is 6\u00b0 x 0.3\u00b0."]
[3.836374282836914, 0.3133524954319, "The Map Resolution of the GRAIL Probes Spacecraft is Highest resolution."]
[7.265129089355469, 7.453404903411865, "The Type of the REIS (JSS-56) instrument Instrument is REIS (JSS-56)."]
[6.49819803237915, 5.699960231781006, "The BeiDou Occultations of the GNOS Instrument Occultation Measurement Device is About 200 per day."]
[8.909233093261719, 1.8882488012313843, "The URL of the BepiColombo Mission is http://www.issfd22.inpe.br/S10-Orbit.Determination-OD/S10_P4_ISSFD22_PF_065.pdf."]
[9.585671424865723, 3.98844313621521, "The Position Control of the CanX-4&5 Satellite is 1 m."]
[8.608881950378418, 1.6939562559127808, "The Observation Date of the Spitzer Satellite is 28 April 2020."]
[3.66858172416687, 5.151650905609131, "The Timing Accuracy of the BOSS Real-time operating system is 1 ms."]
[4.845975875854492, 1.883995532989502, "The Number of Operational Satellites of the DMSP (Defense Meteorological Satellite Program) Satellite Program is 3."]
[3.2897424697875977, 5.449766635894775, "The Data Rate of the HSDR High-Speed Data Recorder is 80 Mbit/s."]
[7.082269668579102, 9.534602165222168, "The Spectral Bands of the MSI-0 and MSI-1 MSI Instruments is 0.45 - 0.52 \u00b5m, 0.52 - 0.60 \u00b5m, 0.63 - 0.69 \u00b5m, 0.76 - 0.90 \u00b5m."]
[6.308565616607666, 7.779386520385742, "The Test Equipment of the ICI Instrument Instrument is Unknown."]
[4.992945194244385, -0.1202331930398941, "The Launch Plan of the Arianespace Launch Provider is Launch the rest of OneWeb\u2019s constellation this year."]
[7.331528186798096, -0.16435490548610687, "The Launch Vehicle of the Kounotori Spacecraft is H-IIB vehicle of MHI (Mitsubishi Heavy Industries, Ltd.)."]
[7.798293113708496, -0.5443189144134521, "The Booster Landing of the SpaceX CRS-24 Mission is Successful."]
[11.487119674682617, 4.119903564453125, "The Atmosphere Mass of the Earth Planet is Less than one millionth of the total mass of Earth."]
[11.506928443908691, 2.7122488021850586, "The Mission Objective of the Psyche spacecraft Spacecraft is Explore a metal-rich asteroid in the main asteroid belt between Mars and Jupiter."]
[6.927987098693848, 1.5640490055084229, "The Expected Mission Duration of the RapidEye Satellite Constellation is Through 2020."]
[6.948880672454834, 0.435282438993454, "The Launch Date of the ITUpSat-1 Satellite is 23 September 2009."]
[9.154047966003418, 4.11439847946167, "The Size of the Satellite Payload Module is 954 mm x 954 mm x 1218 mm."]
[6.7020063400268555, 2.843738555908203, "The Location of the Dasht-e Lut salt desert Desert is Iran."]
[6.335465431213379, 8.237725257873535, "The Frequency Band of the AMSU Microwave Radiometer is 50 to 60 GHz."]
[3.686249256134033, 4.61395263671875, "The Processor of the SCB Spacecraft Bus is Motorola 68302."]
[5.168445587158203, 5.952122688293457, "The Number of Auxiliary Signals for ECCM of the Complete Solution Antenna Configuration is 4."]
[3.3002381324768066, 4.8444719314575195, "The RAM of the OBC On-Board Computer is 2MByte payload data."]
[7.726529598236084, 8.54627799987793, "The Field of View of the OMPS Nadir Profile Spectrometer Spectrometer is 16.6\u00b0."]
[4.994137287139893, 1.989893913269043, "The Number of Spacecraft of the THEMIS Satellite is Three."]
[10.18610954284668, 4.961930274963379, "The Redundancy of the EPPS Electric Propulsion Subsystem is Fully redundant system."]
[10.172667503356934, 6.792067527770996, "The Thermal Control of the KOMPSAT-6 Satellite is Passive & processor-controlled thermal control."]
[7.778038024902344, 3.4930927753448486, "The Purpose of the ICON Space Mission is Retrieve all of the properties of the system that both influence and result from the dynamical and chemical coupling of the atmosphere and ionosphere."]
[7.71981954574585, 7.240798473358154, "The Constellation of the TEMPO Instrument is Instruments measuring air quality over the Northern Hemisphere."]
[6.891385078430176, 2.467318296432495, "The URL of the Dellingr Satellite is http://spaceflight101.com/dragon-spx12/dellingr/."]
[3.602900266647339, 2.2991318702697754, "The Size of the CINEMA Satellite is 3U."]
[10.237865447998047, 6.875601291656494, "The Thermal Management Requirement of the Invar Material is Careful attention to thermal management."]
[10.174158096313477, 8.584237098693848, "The Exposure Time of the Solar Flare Sites Imaging Device is < 10 ms."]
[9.254743576049805, 3.1976208686828613, "The Type of the Satellite Orbit is Elliptical polar orbit."]
[5.466292381286621, 7.038692951202393, "The Data Rate of the RA-1 Antenna Antenna is \u2264 15 kbit/s."]
[9.551912307739258, 6.072375774383545, "The Provider of the ADCS System is CNES."]
[7.693012237548828, 8.863698959350586, "The PI of the MAHRSI Instrument is R. Conway."]
[1.986446499824524, 5.566160678863525, "The Power of the Voltage 2 Power Amplifier is 0.055."]
[7.569784641265869, 0.5292465090751648, "The Leading Satellite Date of the GRACE-2 Satellite is January 2006."]
[8.433686256408691, 11.015761375427246, "The Number of Available Rows per Filter Band of the QWIP Array Sensor Array is 32."]
[10.34620189666748, 3.0827877521514893, "The Altitude of the Satellites Communication is 550 km."]
[7.520643711090088, 6.9500908851623535, "The Manufacturer of the TEMPEST-D Radiometer Instrument is NASA/JPL."]
[10.967984199523926, 5.3294997215271, "The Field Location of the Sunspot Solar Phenomenon is Always located at the boundary between the bright region and the umbra."]
[7.216455459594727, 5.323629379272461, "The Measurement Uncertainty of the CO2 Greenhouse Gas is Unknown."]
[5.773132801055908, 7.000348091125488, "The Pulse Repetition Frequency of the RA-1 Radar Altimeter is 1020 Hz."]
[6.133759498596191, 2.2753026485443115, "The Launch Site of the BioSentinel 6U CubeSat is Kennedy Space Center, Cape Canaveral, FL."]
[7.704960346221924, 7.762353420257568, "The Purpose of the MSX/UVISI Instrument is Probe the atmospheric composition accurately."]
[1.9851877689361572, 3.8538191318511963, "The Solar Cell Material of the LFSA Photovoltaic Solar Array System is Copper Indium Diselinide (CuInSe2)."]
[7.0204291343688965, 2.4846391677856445, "The URL of the TOPCAT Satellite is https://web.archive.org/web/20120306134438/http://www.bis.gov.uk/assets/bispartners/ukspaceagency/docs/space%20science/cubesats/cmos%20imager%20text.pdf."]
[5.598909854888916, 5.389556407928467, "The Manufacturer of the SSTI GPS Receiver is Laben, Milan, Italy."]
[5.89151668548584, 6.838001728057861, "The Pulse Width of the RainCube Radar is Variable."]
[10.397783279418945, 4.944890975952148, "The Propellant Mass of the RCS Reaction Control System is 320 kg."]
[10.55003833770752, 8.506399154663086, "The FOV of the COR1 Coronagraph1 imager is 1.25 - 4 R sun."]
[9.828598022460938, 1.4525229930877686, "The Orbital Repeat Time of the OrbView-2 Satellite is 16 days."]
[11.03115463256836, 4.441536903381348, "The Documented On-Orbit Anomalies of the BRMM Spacecraft is 24."]
[6.881256103515625, 4.928655624389648, "The Mission Objective of the Sentinel-5 Satellite is Operational monitoring of trace gas concentrations for atmospheric chemistry and climate applications."]
[9.944906234741211, 1.4803470373153687, "The Period of the ALOS-3 Satellite is 98 minutes."]
[10.313405990600586, 1.9630112648010254, "The Period of the Meteor-M2 Satellite is 101.41 minutes."]
[8.775121688842773, 10.66875171661377, "The Small Window Time Resolution of the CCD Image Sensor is 0.3 seconds."]
[6.747315883636475, 0.7734043002128601, "The Loss Date of the EgyptSat-2 Satellite is Unknown."]
[8.386754989624023, 1.6373445987701416, "The Launch Date of the Kepler Space Telescope is March 7, 2009."]
[8.35318660736084, 3.6208908557891846, "The Availability of the GPS Simulator Equipment is Not available."]
[5.005117416381836, 4.54902458190918, "The Commanding Management of the Ground Schedule Execution System System is Nominal."]
[7.715371608734131, 3.242112398147583, "The Focus of the Characterization Process Satellite Debris Analysis is Utilize automation to expedite fragment characterization process and minimize human-in-the-loop."]
[5.559875011444092, 1.4075621366500854, "The URL of the NanoRacks Airlock Module Airlock Module is http://nanoracks.com/wp-content/uploads/NanoRacks-Airlock-Presentation.pdf."]
[7.756711483001709, 13.162677764892578, "The Pixel Resolution of the SPIM5 Spectrometer is 14 bit."]
[6.19539737701416, 4.545701503753662, "The Data Delivery of the ICEYE Satellite Constellation is Near real-time."]
[8.178996086120605, 4.238823413848877, "The Speed of the ICEYE-X1 Satellite is More than 7.5 km/s."]
[9.197487831115723, 4.056130886077881, "The Dimensions of the G\u00f6kt\u00fcrk-1A Satellite is 4.2 m x 2.5 m x 1.6 m."]
[8.731603622436523, 9.1668119430542, "The Slit Height of the Short Wavelength Band Spectrometer is 2.75 cm; 1/33 for bright target."]
[3.6527116298675537, 2.3091063499450684, "The Volume of the DeMi Satellite is ~4.5U."]
[3.9929490089416504, 5.636472225189209, "The Download Transmission Rate of the DubaiSat-1 Satellite is 30 Mbit/s."]
[9.686856269836426, 2.5707521438598633, "The Orbits of the Odin Satellite is > 60,000."]
[8.913372993469238, 10.29793643951416, "The Sensor Model of the Camera System Sensor is Aptina MT9P031 5 Mpixel CMOS sensor."]
[7.536044597625732, 5.2954583168029785, "The First Noctilucent Cloud Observation of the AIM Satellite is 2007."]
[8.239938735961914, 3.1409358978271484, "The Conference Presentation Date of the X-Sat Satellite is Nov. 22-26, 2004."]
[9.121323585510254, 5.136922836303711, "The Stabilization of the ZY-3 Satellite is 3-axis."]
[10.242330551147461, 3.0394816398620605, "The Apoapsis Altitude of the Satellite Spacecraft is 21813.2 km."]
[10.198555946350098, 4.840724468231201, "The Type of the Propulsion System Satellite Propulsion is Chemical bi-propellant."]
[7.068462371826172, 9.715930938720703, "The Spectral Range (\u00b5m) of the Band 5 Spectral Band is 11.5 - 12.5."]
[7.400490760803223, 7.815192222595215, "The PIs of the SOVA Radiometer is D. Crommelynck, IRMB, Brussels, Belgium; C. Fr\u00f6hlich, PMOD/WRC Davos, Switzerland."]
[7.243905544281006, 8.481752395629883, "The Dust Grain Width of the COSIMA Mass Spectrometer is About 50 \u00b5m and 70 \u00b5m."]
[9.700876235961914, 3.6089425086975098, "The Event Cause of the LROC Camera System is Hit by a tiny meteoroid."]
[9.782245635986328, 6.649669647216797, "The Temperature of the PM Satellite Component is 18.3~26.7\u00ba."]
[5.835896968841553, 4.368968963623047, "The Purpose of the Secure Communications Satellite Satellite is Provide secure and resilient satellite communications."]
[5.6747212409973145, 3.7186617851257324, "The Service Infrastructure of the Airbus Defence and Space Service Provider is Commercial data exploitation and customer interfaces."]
[4.806459426879883, 1.8124996423721313, "The Number of Satellites of the ICEYE Constellation Satellite Constellation is Approximately 18."]
[3.6196203231811523, 6.643923759460449, "The Data Rate of the X-band Transmitter Transmitter is Up to 210 Mbit/s."]
[7.804599761962891, -0.521563708782196, "The Launch Date of the SpaceX CRS-6 Mission is April 7, 2015."]
[4.7786149978637695, 1.7826602458953857, "The Number of Satellites of the OHB-SSTL consortium Satellite Manufacturers is 8."]
[4.494158744812012, 4.191216468811035, "The Onboard Network Specification of the JWST Avionics Spacecraft Avionics is SpaceWire."]
[8.794757843017578, 0.7499222755432129, "The Purpose of the JUICE Satellite is Explore Callisto, Europa and Ganymede."]
[8.519684791564941, 7.526230812072754, "The URL of the Spaceborne Frequency Comb Metrology Metrology System is https://www.osapublishing.org/DirectPDFAccess/DBE99771-B99B-C7D3-BC1981AC3BB40F6B-354726/optica-3-12-1381.pdf?da=1&id=354726-&seq=0&mobile=no."]
[9.571672439575195, 5.793442249298096, "The Original Purpose of the CRS Cosmic Ray Subsystem is Measure planetary systems."]
[9.352971076965332, 7.693180084228516, "The Data Averaging Period of the ELS-A Electron Measurement Instrument is 4 months from November 2008 to February 2009."]
[9.209687232971191, 3.228121280670166, "The Orbit Type of the PACE Satellite is Sun-synchronous near-circular orbit."]
[8.12968921661377, 7.604106903076172, "The Calibration Method of the OMPS Sensor is Solar illuminated diffusers."]
[3.57796311378479, 4.134562015533447, "The CPU of the STRV-1d DHS Data Handling System is 8051 rad-hard."]
[7.226770401000977, 7.888489246368408, "The Ground Pixel Sizes of the MOMS-02 Instrument is Unknown."]
[3.812276601791382, 6.421054840087891, "The Ka-band of the RF Communications Communication Subsystem is 350 Mbit/s."]
[12.124994277954102, 2.171355724334717, "The Sample Return to Earth of the OSIRIS-REx Spacecraft is Sept. 24, 2023."]
[4.976415634155273, 4.0949177742004395, "The Parallel to DOTCam of the SHU Software Application Development is True."]
[8.964735984802246, 5.9056501388549805, "The Rotation Speed of the AMSR-E Instrument is 40 rpm."]
[9.677797317504883, 7.697432041168213, "The Cooling Method of the Telescope Tube Assembly Telescope is Passively cooled."]
[6.793566703796387, 2.0841054916381836, "The Calibration Data of the GPM Mission is Measurements from the GPM Core Observatory and rain gauge networks around the world."]
[4.817119121551514, 2.4598450660705566, "The OBCs of the CubeSat Satellite is 2."]
[8.342888832092285, 7.381047248840332, "The Location of the ISIS Instrument is As far aft on the spacecraft body as possible, on the ram side, just inside the umbra line."]
[6.633007049560547, 8.29397201538086, "The Uniformity of Absorber Surface of the HTS/AMSR2 Microwave Absorber is 2.5\u00baCp-p."]
[5.419673442840576, 3.889894962310791, "The Testing Tools of the EDSN Organization is DevSats, Flatsats, EDUs."]
[4.894441604614258, 5.598690986633301, "The Signal Frequency of the Ground Station Antenna System Antenna System is 8200.5 MHz."]
[8.257281303405762, 1.3824007511138916, "The Outburst Date of the Comet 67P Comet is 2016 July 03."]
[8.97075366973877, 2.9592161178588867, "The Mission Name of the LunaH-Map Satellite is LunaH-Map."]
[9.078274726867676, 9.21181869506836, "The Iron Particle Distributions of the WISPR Optics Optical System is 0.5 \u2013 3 \u00b5m."]
[3.729919195175171, 6.759166240692139, "The Form Factor Dimensions of the Myriad RF board RF Board is 50 mm x 55 mm."]
[6.754627227783203, 6.16154670715332, "The Calibration and Validation Duration of the RapidScat Instrument is Two weeks."]
[7.845228672027588, 9.153298377990723, "The Swath of the OLCI Spectral Imaging Instrument is 1270 km."]
[10.30102825164795, 6.933065414428711, "The Components of the TCS Thermal Control Subsystem is 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."]
[9.096572875976562, 2.9504804611206055, "The Orbit Transition of the LunaH-Map Spacecraft is Several months."]
[7.472073078155518, -0.34408342838287354, "The Reentry Date of the Long March 5B Rocket Stage is May 8."]
[5.611137866973877, 3.069572925567627, "The Lead Contractor of the Heinrich Hertz Satellite is OHB System AG."]
[10.843954086303711, 5.805788993835449, "The Size of the Solar Flare Natural Phenomenon is X8.2-sized."]
[4.837106227874756, 6.046849727630615, "The Main Processor Frequency of the NSat Satellite is 100 MHz."]
[6.686193466186523, 7.276183605194092, "The Data Density of the Scanning LIDAR LIDAR is Provided data at a reasonable density for the last 30 m."]
[11.619050979614258, 4.697537422180176, "The Accretion Disc Width of the V404 Cygni Black Hole is 10 million kilometers."]
[5.993457317352295, 7.908354759216309, "The Clock Signals of the CIB Interface is 1 Hz and 220 Hz."]
[6.627131938934326, 1.0059068202972412, "The Antenna Gain Requirement of the FormoSat-5 Satellite is Unknown."]
[9.424793243408203, 7.974277973175049, "The Cadence of the Proton Energy Spectra Measurement is Up to around 20 MeV."]
[7.247180461883545, 1.6839375495910645, "The Presentation Date of the Jaan Praks Person is Sept. 22-24, 2014."]
[7.0170512199401855, 1.639452576637268, "The PNAS Publication Date of the Swarm Satellite Constellation is March 21, 2022."]
[1.6416758298873901, 4.564094543457031, "The Manufacturer of the EPS Electrical Power Subsystem is GomSpace."]
[8.230624198913574, 5.643105506896973, "The Leading Noise Terms of the Satellite Spacecraft is TM-to-satellite stiffness coupling to satellite motion."]
[6.079504489898682, 4.10952091217041, "The Mission Control Location of the Odin Satellite is Stockholm."]
[9.878801345825195, -0.7469649910926819, "The Dimensions of the PACE nanosatellite Satellite is 100 mm x 100 mm x 243 mm."]
[7.634953022003174, 7.891088008880615, "The Products of the CERES Instrument is Solar-reflected and Earth-emitted radiation from the top of the atmosphere to the Earth's surface."]
[5.680629253387451, 9.160309791564941, "The Power of the HIRES Instrument is 10 W."]
[8.9179105758667, 9.23041820526123, "The IFOV N/S x E/W (\u00ba) of the FCI-TA Instrument is 0.40 x 0.40."]
[5.973373889923096, 3.3019957542419434, "The Managing Center of the Eu:CROPIS Satellite is DLR (German Aerospace Center)."]
[5.449038028717041, 2.948603630065918, "The Platform of the exactView-1 Satellite is SSTL-100."]
[6.86834716796875, 9.18818473815918, "The Dimensions of the Instrument Spectrometer is 445 x 327 x 182 mm3."]
[9.45804214477539, 2.310224771499634, "The Total Travel Distance of the BepiColombo Spacecraft is Nine billion kilometers."]
[11.843976974487305, -1.1383658647537231, "The Launch Mass of the Spacecraft Satellite is 3375 kg."]
[6.643557548522949, 8.484638214111328, "The Resolution of the MWR Dicke Radiometer is 50 km."]
[7.822352886199951, -0.043305106461048126, "The Launch Date of the Nauka Development Satellite is Unknown."]
[12.04309368133545, 3.312901496887207, "The Inclination of the ALL-STAR-1 Satellite is 51.6o."]
[9.494446754455566, 9.022866249084473, "The Telescope/Spectrograph Assembly of the MAHRSI Instrument is f/7.5 Czerny-Turner spectrograph with a 75 cm focal length behind a 50 cm focal length telescope (57 cm2 aperture)."]
[5.755258560180664, 3.7786166667938232, "The Data Center of the GBOT Project is Observatoire de Paris."]
[5.661077976226807, 5.35425329208374, "The Supplier of the GPSP Instrument is NASA."]
[7.170524597167969, 1.5721957683563232, "The Mission Extension of the Cluster Satellite Constellation is December 2005 to December 2009."]
[11.190370559692383, 2.38118052482605, "The Depth of the Holes Drill Holes is 2,450 meters."]
[5.957805633544922, 2.9264278411865234, "The Mission Leader of the ASTRA LLC Organization is ASTRA LLC."]
[5.738260269165039, 5.088059425354004, "The Backup Station Frequency Bands of the PAZ SAR Processor Ground Segment Processor is S/X-band."]
[8.460662841796875, 3.8642473220825195, "The Propulsion System of the Spacecraft Satellite is None."]
[6.841819763183594, 2.0235917568206787, "The URL of the China High-resolution Earth Observation System (CHEOS) Satellite System is http://www.nasaspaceflight.com/2013/04/china-back-in-action-long-march-2d-gaofen-1/."]
[7.876457691192627, 9.644704818725586, "The Number of Pixels of the Band 2 Spectral Band is 1600."]
[3.551764726638794, 2.287905693054199, "The Size of the CXBN Satellite is 2U."]
[7.412747383117676, 5.529819488525391, "The Effect of the Water Cycle Natural Process is Moves heat."]
[6.107494831085205, 0.6095938682556152, "The Announcement Date of the X-ray Navigation CubeSat Mission CubeSat Mission is 3 May 2018."]
[7.434783458709717, 9.307958602905273, "The Field of View of the A Photometer Instrument is 0.2o x 2.1o."]
[7.140063285827637, 0.5145642161369324, "The Launch Date of the SuperView-1 01 and Superview-1 02 Satellite is December 28, 2016."]
[7.229516983032227, 5.624792575836182, "The Response to Stresses of the Phytoplankton Marine Organism is Varying greatly in size, function, and response to environmental and ecosystem changes or stresses such as ocean acidification."]
[5.0814995765686035, 4.835718154907227, "The Ground Stations of the PRISMA Satellite Network is DLR antennas at Weilheim and the antennas operated by SSC in Sweden."]
[6.723348140716553, 1.7712047100067139, "The Commissioning Phase Date of the Envisat Satellite is June 2001."]
[9.464311599731445, 9.078688621520996, "The Footprint of the Telescope Instrument is Smaller than 30 m."]
[3.0142476558685303, 6.627861022949219, "The RF Output Power of the Transmitter Communication Device is 12 W."]
[7.815180778503418, 9.605131149291992, "The Normalized to of the PRI Photochemical Reflectance Index is 570 nm."]
[2.1338467597961426, 4.517929553985596, "The Spacecraft Power of the QuickBird-2 Satellite is 1.14 kW (EOL)."]
[8.147781372070312, 10.294058799743652, "The Bandwidth of the Band Cameras Camera is 5.0 nm."]
[5.337728023529053, 10.368090629577637, "The Data of the LI Lightning Imager is Real-time data on the location and intensity of lightning flashes."]
[9.252006530761719, 8.602867126464844, "The Material of the Optical Benches Optomechanical System is Composite tubes with titanium fittings."]
[8.757004737854004, 6.415327072143555, "The Issue of the BPP (Bi-axial Pointing Platform) Pointing Platform is Difficulties in achieving the pointing control precision."]
[5.72931432723999, 2.2215003967285156, "The Quantum Communication of the Micius Satellite is Enabled."]
[7.718389987945557, 13.590744018554688, "The Passband Range of the SPIM4 Spectrometer is 377-582 nm."]
[9.315942764282227, 8.226907730102539, "The Thickness of the Low LET Detector Detector is 1000 \u00b5m."]
[5.137532711029053, 2.0438766479492188, "The Award Abstract Number of the OPAL CubeSat is 1242901."]
[8.109588623046875, 1.2066130638122559, "The Imaging Location of the Landsat 8 Satellite is British Columbia and Alberta."]
[7.0551862716674805, 3.8283488750457764, "The Mission of the INSAT-3DR Satellite is Improve upon observation capabilities of its predecessors."]
[7.699341773986816, 7.747129917144775, "The Purpose of the SBUV Instrument is 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."]
[7.8731689453125, 7.081941604614258, "The Measurement Calibration Technique of the SAM-II Instrument is Langley technique."]
[3.6439428329467773, 4.762277126312256, "The Microcontroller Speed of the CDHS Command and Data Handling Subsystem is 16 MIPS when run at 32 MHz."]
[6.775071620941162, 0.40202897787094116, "The Launch Date of the GF-3 Satellite Satellite is 9 August 2016."]
[7.5208330154418945, 4.263949871063232, "The Function of the Light Sensor Sensor is Confirm when the optical beacon is impinging on the satellite."]
[8.43449592590332, 5.759390354156494, "The Number of Off-Source Pointings of the Mode 1 Pointing Mode is 6."]
[9.456463813781738, 8.514212608337402, "The Mirror Material of the ALI Telescope is Silicon carbide (SiC)."]
[5.777236461639404, 1.369399905204773, "The Launch Site of the SpaceX CRS-13 Mission is Cape Canaveral SLC-40."]
[4.830026149749756, 1.7283109426498413, "The Number of Substorms Observed from Excellent Vantage Point of the THEMIS Constellation Satellite Constellation is 6-10."]
[4.912815570831299, 1.5695332288742065, "The Profiles Per Day of the FormoSat-7 / COSMIC-2 mission Satellite Mission is 8,000 (threshold)."]
[6.428577899932861, 3.313049077987671, "The Conference Presentation of the Space Test Program-1 Satellite is 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."]
[6.2675395011901855, 8.195775032043457, "The Channel Bands of the AMSU Microwave Radiometer is 50 to 60 GHz, 183.3 GHz."]
[5.233232021331787, 4.72063684463501, "The Location of the RF Ground Station Ground Station is Shinshu University in Nagano."]
[3.8651959896087646, 7.1653852462768555, "The Digital Data Handling Subsystem Mass of the SIR-C Phased Array is 145 kg."]
[7.686872482299805, 2.13757586479187, "The URL of the Europa Clipper Spacecraft is https://europa.nasa.gov/spacecraft/instruments/eis/."]
[8.447550773620605, 5.572464466094971, "The Reporting Frequency of the GT Fine-Pointing Error Signal Provider is 250 Hz."]
[9.540444374084473, 1.0354487895965576, "The Testing Duration of the QUESS satellite Satellite is Four months."]
[5.621467590332031, 4.1242899894714355, "The Support of the Test Station Testing Equipment is Ops testing and training support."]
[8.19743537902832, 1.541333556175232, "The Date of the Proximity Flyby Maneuver is June 3, 2018."]
[4.065647125244141, 4.929751396179199, "The Redundancy of the C&DH Subsystem Control System is One OBC is redundant, two TMC are redundant."]
[11.203145980834961, -1.5130360126495361, "The Mass of the ZACUBE-1 CubeSat is 1.2 kg."]
[10.005321502685547, 3.9899842739105225, "The Sail Deployment Time of the LightSail-2 Spacecraft is Roughly two minutes."]
[8.160940170288086, 3.690584659576416, "The Payload Volume of the STACEM Satellite is Not provided."]
[9.498340606689453, -0.7413433790206909, "The Deployment Success of the DIWATA-1 Microsatellite is Yes."]
[9.101456642150879, 9.78108024597168, "The Field of View of the DarkCarb image sensor Photon Detector is Restricted."]
[7.159650802612305, 7.021495342254639, "The Publication Date of the Superconducting Submillimeter-Wave Limb-Emission Sounder Sounder is Dec. 7, 2010."]
[7.52322244644165, 6.749808311462402, "The Purpose of the SWAP and LYRA Instruments is Space Weather Observation."]
[7.907841205596924, 5.199039459228516, "The Accuracy of the Satellite Tracking Tracking System is Centimeter-scale orbital checks."]
[4.490845203399658, 3.664133071899414, "The Shareholder of the AIS Automatic Identification System is Hisdesat."]
[5.058424949645996, 5.115915298461914, "The Receiving Antenna Location of the Bukittinggi Ground Station is To cover the far Northwest of Indonesia such as the Aceh province."]
[8.840970039367676, 3.2489242553710938, "The Orbit of the PhoneSat 2.5 Satellite is Low Earth Orbit."]
[10.187071800231934, 3.0102627277374268, "The Altitude of the Meteosat-7 Satellite is 35,786 km."]
[7.3518266677856445, 8.16471004486084, "The Spectral range of the TOU Total Ozone Unit is 308-361 nm."]
[4.936157703399658, 3.8246476650238037, "The Purpose of the NAVISP Project is Strengthening European competitiveness in the navigation arena."]
[4.2685112953186035, 6.509517669677734, "The Uplink Frequency of the RF Communications Communication System is UHF band (437.5 MHz)."]
[5.113061904907227, 5.562650680541992, "The Size of the DSN Antennas Ground Antennas is 34 m."]
[8.156904220581055, 0.4504854381084442, "The Orbit Delivery of the Aeolus Spacecraft is 55 minutes later."]
[8.92143440246582, 8.305967330932617, "The Function of the Calibration Mirror TIR Subsystem Component is Block the cold space aperture during Earth view."]
[5.034088611602783, 5.394908905029297, "The Antenna Size of the Ground Station Ground Station is 3.7 m."]
[9.19107723236084, 3.2215263843536377, "The Orbit Type of the Beijing-1 Satellite is Sun-synchronous circular orbit."]
[9.324419021606445, 6.402925491333008, "The Measurement Performances of the Star Tracker Attitude Determination Device is Better measurement performances than the current baseline Myriade's Star Tracker."]
[11.851423263549805, 0.999418318271637, "The Sample Collection Goal of the Chang'e-5 Moon Surface Sampling Probe is Around two kilograms of lunar samples."]
[5.673431873321533, 9.092118263244629, "The Power Consumption of the OTU Optical Telescope Unit is 15 W."]
[9.789246559143066, 2.873272180557251, "The Landing Speed of the OMOTENASHI Satellite is Approximately 30 m/s."]
[6.513765335083008, 4.549426555633545, "The Type of the FY-1C Satellite is Feng Yun-1C."]
[7.785755157470703, 8.603185653686523, "The Solar-Spectral Scan Range of the SBUV Spectrometer is 0.16 - 0.4 \u00b5m."]
[8.199630737304688, 3.2057199478149414, "The Formation Control of the TerraSAR-X Satellite is Yes."]
[8.47974967956543, 8.364707946777344, "The Number of Individual Scans of the SPICE Instrument is 25."]
[8.583136558532715, 6.562265396118164, "The Reference Vector of the Magnetometer Sensor is Truncated IGRF-11 (International Geomagnetic Reference Field-11) model of the Earth's magnetic field with 2010 coefficients."]
[3.935558795928955, 4.329723358154297, "The Microcontroller of the CDHS Command and Data Handling Subsystem is PIC24."]
[6.841804504394531, 2.4546444416046143, "The URL of the COMS Satellite is http://cimss.ssec.wisc.edu/cimss25th/presentations/chung.pdf."]
[8.781031608581543, 4.780416011810303, "The Eccentricity and Argument of Perigee Adjustment Method of the SJ-9A and SJ-9B Satellites is Adjusting the speed increment (position and time) and the semi-major axis."]
[2.415796995162964, 3.9042351245880127, "The Solar Array Length of the PARASOL microsatellite Satellite is 1.7 m."]
[6.364837646484375, 8.212723731994629, "The Type of the MWR Radiometer is Dicke."]
[7.118067741394043, 0.9835089445114136, "The Phase B2/C/D/E1 Contract of the OPS-SAT Satellite is Kicked off in February 2015."]
[11.344232559204102, 3.634881019592285, "The Components of the Comet Celestial Body is Nucleus, coma, hydrogen envelope, dust and plasma tails."]
[11.722397804260254, -0.9723799824714661, "The Mass of the Polizon Payload is 144 kg."]
[4.968302249908447, 6.544158935546875, "The Stiffness of the Antenna Communication is > 20 Hz (during launch in lateral direction)."]
[7.643824577331543, 2.162350654602051, "The Mission Completion Date of the ELSA-d Satellite is 4 May 2022."]
[8.37476921081543, 9.931294441223145, "The Array Size of the B1 Band Detector is 4 x 4."]
[7.382871150970459, 6.771551609039307, "The Image Acquisition Date of the MODIS Instrument is May 16, 2022."]
[3.7219464778900146, 6.342971324920654, "The CW Beacon Data Rate of the RF Communications Communication Subsystem is GMSK 9.6 kbit/s / AFSK 1.2 kbit/s."]
[5.8615875244140625, 3.1300716400146484, "The Annual Production of the APL\u2019s Research and Exploratory Development Department (REDD) Department is Thousands of boards, cables and assemblies."]
[12.142650604248047, 2.234018564224243, "The Full Name of the REXIS Spectrometer is Regolith X-ray Imaging Spectrometer."]
[8.275671005249023, 0.6049032807350159, "The Launch Date of the Hitomi Satellite is February 17, 2016."]
[6.16579532623291, 9.607770919799805, "The Mass of the Particle Detectors Instrument is 2.5 kg."]
[8.103333473205566, 4.124330043792725, "The Area Coverage of the RADARSAT-2 Satellite is 23% over the identified area."]
[5.0842814445495605, 4.545466423034668, "The Firing Control of the Picosat Launcher Satellite Component is Ground commandable."]
[7.172865867614746, 0.7635550498962402, "The Launch Date of the Satellite Spacecraft is Unspecified."]
[7.863109111785889, 8.007939338684082, "The Number of Atmosphere Passes of the OCO-3 Spectrometer is 2."]
[9.881028175354004, 1.482417106628418, "The Contact Time after Launch of the Mey-Lin (C6), Gaspard (C7), and Oc\u00e9ane (C8) Satellites is Within 90 minutes."]
[8.868876457214355, 9.886547088623047, "The Image Type of the Long-Range Reconnaissance Imager (LORRI) Camera is Color."]
[8.951231002807617, 3.223217010498047, "The Location of the NCLE Instrument is Low Earth Orbit."]
[1.8888300657272339, 3.845996141433716, "The Type of the Solar Cells Power Generation is GaInP/GaAs/Ge triple junction solar cells."]
[6.823629856109619, 1.3601950407028198, "The Conference Presentation Date of the JC2SAT-FF Satellite is Aug 20-24, 2007."]
[5.957906723022461, 3.9567556381225586, "The Affiliation of the MHS Instrument is EUMETSAT-funded."]
[8.545952796936035, 5.509446144104004, "The Pointing Accuracy of the SILEX Terminal is Better than 1 arc second."]
[6.636948108673096, 3.9783990383148193, "The Ortho-rectification Methods of the Deimos' ground segment Ground Segment is Automatic, Human-driven."]
[3.9485042095184326, 4.896667957305908, "The Redundancy of the Onboard Computer Computer is One computer is nominally off as a cold spare."]
[11.244091987609863, -1.4336787462234497, "The Weight of the CubeSats Satellite is 14 kg."]
[1.6141622066497803, 4.059324741363525, "The Battery Recharge Method of the Sloshsat-FLEVO Satellite is Using the solar panels."]
[7.0747456550598145, 0.5514419078826904, "The Joining Date of the SPOT 6 Satellite is Sept. 9, 2012."]
[4.41505765914917, 5.204041481018066, "The Downlink Chains of the ResourceSat-2 Satellite is 2."]
[9.160117149353027, 5.792328834533691, "The Attitude Sensing of the OceanSat-2 Satellite is Earth horizon sensors, digital sun sensors, triaxial magnetometers and a gyroscope-based inertial reference unit."]
[4.7128376960754395, 5.750144958496094, "The RF Communications of the Spacecraft Satellite is X-band for science data acquisition."]
[7.136168956756592, 8.63900375366211, "The No of bands/channels of the SBUS Solar Backscattering UV Sounder is 12."]
[8.319955825805664, 8.418403625488281, "The Alignment Tools of the Interferometer Alignment Process is Personnel from the OPC (Optical Physics Company), custom goniometer, collimated light source."]
[9.926025390625, 4.250771522521973, "The Maneuvering Principle of the NEA Scout Solar Sail Technology Demonstration Spacecraft is Tipping and tilting its sail to change the angle of sunlight."]
[11.72386646270752, -1.1845331192016602, "The Mass at Launch of the Geo Satellite Satellite is 6 tonnes."]
[5.1783223152160645, 6.2221784591674805, "The Number of Consecutive Deployments of the VDES Antenna Antenna is Over 100."]
[3.628795862197876, 4.537374496459961, "The Generation of the Xilinx Zynq Ultrascale+ MPSoC ZU9EG Processor is Latest."]
[7.513078689575195, 5.765915393829346, "The Calibration Techniques of the SMOS Satellite is Initial Guess based Techniques (\u2018Gibbs\u2019 approaches), the Floor Error Mask, the Pre-Distorted G-matrix and the Average Pattern Reconstruction."]
[6.623047828674316, 3.5999631881713867, "The Mission Type of the SciSat-1/ACE Satellite is EO."]
[8.56002426147461, 3.251253843307495, "The Mission Objectives of the LADEE Satellite is 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 a."]
[7.2005815505981445, 7.076296806335449, "The Status of the Carmen-2 Instrument is Performing well."]
[5.563601493835449, 2.873068332672119, "The Bus Manufacturer of the Restore-L Satellite is Maxar."]
[8.902897834777832, 5.712421417236328, "The Alignment of the Hexapod Mounting System is Used for aligning SAGE-III."]
[7.83379602432251, 5.998988151550293, "The HIS Calibrations Frequency of the TRUTHS Satellite is On occasions, particularly during commissioning phase."]
[7.914714813232422, 2.1461288928985596, "The Publication Date of the Star-circling bubble of gas Unknown is 11 June 2018."]
[11.759923934936523, 1.6689804792404175, "The Initial Rotation of the Philae Lander is Slow."]
[4.077879428863525, 6.605111598968506, "The Operating Frequency Range (TM) of the EWC31 S-band transceiver module Communication Module is 2200-2290 MHz."]
[4.734631061553955, 2.0123045444488525, "The Quantity of the Flock-3p x 4 Satellite is 4."]
[3.3351473808288574, 4.956961154937744, "The Solid-State Recording Capacity of the Onboard Data Handling Subsystem (OBDH) Data Handling System is 90 Gbit."]
[7.8229875564575195, 1.1719655990600586, "The Flood Mapping Date of the Satellites Satellites is 16 July 2021."]
[6.063169956207275, 9.733030319213867, "The Mass of the Telescope Telescope is 315 kg."]
[9.365015983581543, 9.70715618133545, "The Focal Length of the Custom design lens Lens is 155.9 mm."]
[9.279051780700684, 1.702916145324707, "The Revisit Time of the Terra Bella Satellite Constellation is Three times per day."]
[1.1482101678848267, 3.841155529022217, "The Power of the XI-IV Picosatellite is Average power of 1.2 W."]
[7.217012405395508, 1.4451195001602173, "The Presentation Date of the ESTCube-1 Satellite is May 30, 2012."]
[7.755952835083008, 0.9874917268753052, "The Application Date of the Sentinel-5P Satellite is 19 October 2020."]
[6.479455471038818, 6.217188358306885, "The PDU of the ASCAT Scatterometer is Power Distribution Unit."]
[10.276934623718262, 2.9403440952301025, "The Altitude of the BeaverCube Satellite is 410 km."]
[6.964250087738037, 0.7212518453598022, "The Constellation Proposal Date of the ICEYE Satellite is September 14, 2022."]
[7.4784417152404785, -0.048466265201568604, "The Launch Date of the SpaceX Satellite Satellite is July 14, 2009."]
[8.404106140136719, 3.7736687660217285, "The Thruster Quantity of the Eutelsat 172B Satellite is Not provided."]
[9.407811164855957, 9.983920097351074, "The Response Speed of the APD detector Experiment is High."]
[5.984810829162598, 1.8273003101348877, "The Launch Vehicle of the TechEdSat Satellite is H-II Transfer Vehicle \"KOUNOTORI3\" (HTV3) Aboard the H-IIB Launch Vehicle No. 3."]
[10.303177833557129, 4.914332389831543, "The Conference Date of the \u00b5CAT Micro-Propulsion Solution Propulsion System is August 6-11, 2016."]
[4.415270805358887, 6.701654434204102, "The Quantization of the LICEF Receiver is 1 or 0."]
[3.695431709289551, 6.273054122924805, "The Data Rates of the Channel Communication System is Variable from 37 Mbit/s to 336 Mbit/s."]
[4.329273223876953, 5.2696943283081055, "The Connection of the USRP Transceiver is Interfaced with a PC."]
[8.07667350769043, 4.744185924530029, "The GSD (Multispectral) of the GF-2 Satellite is 3.24 m."]
[8.863996505737305, 6.490816116333008, "The New Finding of the Plasma Sheet Space Phenomenon is Higher-energy O+ (1\u201310 keV) ions."]
[8.332718849182129, 3.3277435302734375, "The Effective Baselines of the TanDEM-X Satellite is Required for DEM acquisition at different latitudes."]
[11.366653442382812, 1.3663991689682007, "The Scheduled Work Resume Date of the Yutu-2 Rover is March 10."]
[9.557015419006348, 1.1022249460220337, "The Orbit Repeat Time of the SeaHawk-1 CubeSat is About 18-days."]
[10.372344017028809, 5.004051208496094, "The Specific Impulse of the HET-X Hall-effect Thruster is 1300 - 2200 ISP."]
[7.251067638397217, 6.882441997528076, "The Image Source of the NOAA-20 Satellite is VIIRS."]
[4.019391059875488, 4.876903057098389, "The Redundancy of the OBC On-Board Computer is Redundant."]
[6.3754754066467285, 1.080808401107788, "The Conference Date of the COSMO-SkyMed Satellite is March 17-18, 2004."]
[9.220459938049316, 3.102928638458252, "The Exploration Mission Orbit of the LRO Satellite is Quasi-circular polar orbit (50 \u00b1 15km)."]
[7.0449137687683105, 9.841753959655762, "The Wavelength Range of the Band 1 Spectral Band is 365-408 nm."]
[6.472417831420898, 4.49765157699585, "The Instruments of the FedSat Satellite is Communications payload (Ka and UHF band), GPS receiver, Fluxgate magnetometer."]
[2.301182270050049, 4.421164512634277, "The Power Consumption of the Total Satellite is < 75 W."]
[7.837484359741211, 9.773310661315918, "The Spectral Range of the TrueColour Imager Optical Imager is 433 nm - 907 nm."]
[6.76033353805542, 7.148037433624268, "The Biomass Estimate Accuracy of the GEDI Lidar Instrument is Well-described uncertainty for its estimates using advanced statistical models."]
[11.562121391296387, 6.298123359680176, "The Fact Sheet URL of the XMM-Newton Satellite is http://sci.esa.int/xmm-newton/47370-fact-sheet/."]
[7.3081254959106445, 7.18745756149292, "The Flight Performance of the MOPITT Instrument is Unknown."]
[5.580560207366943, 4.0386247634887695, "The Communication Methods of the SSETI Express Satellite is Internet, chat sessions, e-mail, news postings, dedicated news server, Internet Relay Chats (IRCs), SSETI website."]
[6.751023292541504, 2.6938414573669434, "The URL of the EUMETSAT Satellite Data Service is http://www.eumetsat.int/website/home/Data/RegionalDataServiceEARS/index.html."]
[6.88060188293457, 1.0163954496383667, "The Mission End Date of the GFO Satellite is October 22, 2008."]
[10.074359893798828, 4.05115270614624, "The Solar Sail Area of the NEA Scout Spacecraft is 85 m2."]
[10.799756050109863, 3.256122350692749, "The Distance from Earth of the Vigil Spacecraft is 1.5 million km."]
[8.87912654876709, 7.6984124183654785, "The Ion Velocity Components of the DIDM Instrument is Normal and perpendicular."]
[7.118946075439453, 4.685728073120117, "The Purpose of the GOES-West Satellite is Provide an infrared look at the clouds."]
[7.020874977111816, -0.05327075719833374, "The End of Life Date of the CAS500 Satellite is 2029."]
[11.357590675354004, 3.924762487411499, "The Orbit Period of the Beta Pictoris b Planet is 21 years."]
[9.449370384216309, -0.38086751103401184, "The Mission Goal of the FASTRAC Satellite is Demonstrate enabling technologies for nanosatellites that work together in space."]
[8.492022514343262, 7.24961519241333, "The Probe Orientation of the TPMU Device is In the direction of the velocity vector."]
[-4.981034278869629, 4.407583713531494, "The Support Phase Time Period of the Mango Tango Satellite Formation is 03.08 to 10.08.2010."]
[10.0053129196167, 5.198277950286865, "The Components of the Electric Propulsion Test Subsystem Monitoring Unit is Quartz crystal microbalance, Langmuir probe and retarding potential analyzer."]
[9.56347942352295, 0.887212872505188, "The Time to Reach Intelsat 901 of the MEV-1 Satellite is Approximately four months."]
[9.385138511657715, 0.8334783911705017, "The Original Design Orbit Duration of the ESEO Satellite is 6 months."]
[3.6119394302368164, 6.063162326812744, "The Bandwidth of the Communication Bus Data Communication is 100 Mbit/s."]
[8.195798873901367, 2.5289642810821533, "The Support Tools of the ARTEMIS Satellite is Tools developed under multiple airborne experiments."]
[12.098421096801758, 3.297480821609497, "The Orbital Inclination of the Long March 5B Rocket Stage is 41.5 degrees."]
[5.661321640014648, 3.9348161220550537, "The Location of the MOC Mission Operations Center is ESOC (Darmstadt, Germany)."]
[5.132964134216309, 2.974928617477417, "The Role of UNM of the SORTIE Satellite is Integrators of the CubeSat."]
[9.174020767211914, 10.612479209899902, "The GSD (Ground Sample Distance) of the Camera Payload is 1 m."]
[10.111787796020508, 1.3820463418960571, "The Equator Crossing Time of the OceanSat-1 Satellite is 12:00 hours on the descending node."]
[6.662840366363525, 0.7400054931640625, "The Launch Date of the RADARSAT-2 Satellite is 2007."]
[5.855490684509277, 5.36467170715332, "The Control Method of the GSS GPS Signal Generator is Attitude and orbit commands from SATSIM."]
[5.367621898651123, 6.602875232696533, "The Angle Bin Interval of the PR Phased Array System is 0.71\u00ba."]
[9.799933433532715, 8.48410415649414, "The Observing Opportunity of the Ground-based Telescopes Telescopes is Only brief windows exist near the Sun as the Earth rotates through 15\u00ba every hour."]
[11.790250778198242, -1.116494059562683, "The Mass at Launch of the INTEGRAL Satellite is 4 t."]
[9.436779022216797, 8.809759140014648, "The Mount Type of the Telescope Optical Instrument is English mount."]
[4.956820011138916, -3.1160969734191895, "The Affiliation of the Kazaya Yoshida Author is Unknown."]
[6.6028571128845215, 4.766531467437744, "The Peatland Area of the Indonesia Country is Over 14 million hectares (140,000 km2)."]
[9.000218391418457, 7.674821853637695, "The Components of the REPT Instrument is 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."]
[3.958702325820923, 5.689788341522217, "The Downlink Data Rate of the EROS-A Satellite is 70 Mbit/s."]
[7.171754360198975, 8.585272789001465, "The Number of Channels of the Filter Wheel Optics Subsystem is LWIR (7 channels), SWIR (6 channels) and the MWIR (5 channels)."]
[11.341525077819824, 1.5183241367340088, "The Antenna and Camera Temperature of the Yutu Lunar Rover is Below -180\u00baC."]
[13.085079193115234, 4.079899311065674, "The General Theory of Relativity of the Gaia Space Astrometric Mission is Test."]
[9.30236530303955, 7.255679607391357, "The Measurement Range - Electron Temperature of the ISL Instrument Langmuir Probe is 500-3000 K."]
[5.30611515045166, 9.602873802185059, "The Star Sensitivity Range of the STOs and STAEs Analog Electronic units is 4 ~6.5 magnitude."]
[7.532984256744385, 5.573228359222412, "The Effect of the Undersea Mountain Natural Feature is Attract a mound of water several meters high over the seamount."]
[7.33336877822876, 0.8744038939476013, "The Activation Date of the HDEV High-Definition Earth-Viewing System is April 30, 2014."]
[6.615262508392334, 6.084982872009277, "The URL of the SWIM Scatterometer is http://smsc.cnes.fr/CFOSAT/GP_swim.htm."]
[10.848094940185547, 4.2460761070251465, "The Imaging Capability of the Hubble Space Telescope Space Telescope is Shows only blurry patches of light and dark materials on Pluto\u2019s surface."]
[7.5241546630859375, 1.138898253440857, "The Article Date of the INTEGRAL Satellite is 2016 April 1."]
[4.343763828277588, 5.604406833648682, "The TT&C Subsystem of the CBERS-1 Satellite is S-band and UHF-band data transmission."]
[6.040640354156494, 4.329193592071533, "The Back Up User of the Canadarm2 Robotic Arm is ESA astronaut Thomas Pesquet."]
[7.43276309967041, 6.868638515472412, "The Platform of the DESIS Instrument is Multiple User System for Earth Sensing (MUSES)."]
[8.144391059875488, 1.0133867263793945, "The Imaging Date of the Landsat 8 Satellite is October 31, 2021."]
[11.938056945800781, 2.341918706893921, "The Launch of the OSIRIS-REx Spacecraft is Required considerable power."]
[8.393841743469238, 7.380747318267822, "The Frequency Range of the EZ probe Electric Field Probe is 0 - 1000 Hz."]
[6.226861000061035, 8.214532852172852, "The Bandwidth of the MWR Radiometer is 500 MHz."]
[7.457148551940918, 6.536387920379639, "The Satellite of the MODIS Imaging Spectroradiometer is NASA\u2019s Terra."]
[4.195381164550781, 2.7877326011657715, "The Download Speed of the Starlink Satellite Internet Service is 100-200 Mbit/s."]
[7.148199558258057, 7.0787177085876465, "The Presentation Date of the MIPAS Instrument Instrument is Jan 1999."]
[7.15128231048584, 2.655905246734619, "The URL of the InSight Mars Lander Mars Lander is https://www-robotics.jpl.nasa.gov/projects/InSight.cfm?Project=7."]
[11.049290657043457, 5.101931571960449, "The Launch of the Coronal Mass Ejections Solar Phenomenon is Launched in sequence one after another from the same active region."]
[9.090533256530762, 5.0281500816345215, "The Stabilization of the NigeriaSat-2 Satellite is 3-axis."]
[8.06558609008789, 8.955310821533203, "The Spectral Bands of the TIR Instrument Telescope is 8-12 \u00b5m range."]
[6.230823516845703, 7.792679309844971, "The Polarization of the ICI-1 Radiometer is V."]
[7.400625705718994, 0.8770530819892883, "The Launch Date of the Sentinel-3 Satellite is 2013."]
[7.846689224243164, 5.9937214851379395, "The Description of the CEASE-III-RR Experiment is CEASE-III-RR will use a suite of instruments to identify conditions in the space environment that could affect the operation of a satellite. Consisting of high and low-energy proton/electron telescopes and an electrostatic analyzer, CEASE will measure the."]
[8.146514892578125, 3.310598850250244, "The Data Mode of the TanDEM-X Satellite is Stripmap single polarization (HH) mode."]
[4.872610092163086, 3.8955345153808594, "The Function of the Node-3 Module is Accommodates the items necessary for the distribution of commands and data, audio, video, electrical power, atmosphere, water and thermal energy to adjacent elements."]
[9.326273918151855, 10.319143295288086, "The Field-of-View of the PanCam WAC Camera is 37\u00b0 x 37\u00b0."]
[9.47299861907959, 5.573553085327148, "The Pointing Accuracies of the AOCS Attitude and Orbit Control Subsystem is \u00b10.05\u00ba in all axes."]
[9.44664192199707, 4.860006809234619, "The Solar Array of the Orion Spacecraft is Designed to bend up to 60\u00ba forward and backward."]
[4.664915561676025, 4.400610446929932, "The Control Functions of the MECA Electronics Controller Assembly is Management of the command data interface, control of the dust door, scanning mirror, rotating polarizing filter, and scanned grating."]
[5.076709747314453, 2.2430174350738525, "The Height of the CubeStack Multi-Payload Adapter is 10 inches (25 cm)."]
[3.2477006912231445, 5.308416843414307, "The Storage Capacity of the Data Buffer Board Data Storage Device is Up to 46+46 averaged frames with telemetry and ancillary data."]
[9.235692024230957, 9.351542472839355, "The FOV Elevation of the SAGE-III Instrument is -24.81 to -31.02\u00ba."]
[6.853822231292725, 2.3149750232696533, "The URL of the Beidou Satellite Navigation System is http://www.globalsecurity.org/space/world/china/beidou.htm."]
[5.131014823913574, 3.1761574745178223, "The Parts of the CubeSat Satellite is 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."]
[7.688421726226807, 1.759032964706421, "The Event of the SMOS Satellite is SMOS MIRAS - return to nominal data quality."]
[10.43127155303955, -1.0790050029754639, "The Mass of the SERB Nanosatellite Satellite is 4.5 kg."]
[10.06054973602295, 4.974865913391113, "The Purpose of the HEMPT Thruster Assembly Electric Propulsion Thruster is Satellite position maintenance."]
[7.667813301086426, 2.3412373065948486, "The URL of the MMO Orbiter is http://www.stp.isas.jaxa.jp/mercury/p_mmo.html."]
[7.006742477416992, -0.04357805848121643, "The End of Life Date of the CASSIOPE Satellite is 01 Apr 2024."]
[7.075660228729248, 6.709036350250244, "The Image Source of the PLEGPAY Instrument is ESA."]
[10.563531875610352, 7.498624324798584, "The Structure of the Spacecraft Satellite is Aluminium honeycomb H-structure."]
[10.525226593017578, 2.3185908794403076, "The Inclina. (\u00ba) of the Cosmos-1066 (Astrofizika) Satellite is 81.2."]
[3.3982937335968018, 6.5485639572143555, "The EIRP of the Contiguous Sectors Communication System is 60-65 dBW."]
[9.559744834899902, 5.916117191314697, "The Attitude Control of the ADCS unit Satellite Component is Only attitude sensor during eclipse."]
[8.502981185913086, 10.465752601623535, "The Resolution of the CUTE CCD Array is 2048 x 515 pixel."]
[10.777933120727539, 3.4771947860717773, "The Closest Approach to the Sun of the SOHO Spacecraft is 1,165,000 km."]
[6.383510589599609, 3.352149248123169, "The Operational Goals of the ISERV Satellite is Reduce the amount of time required for each step."]
[10.414623260498047, 4.741069793701172, "The Number of Activation Cycles of the Electric Thruster Thruster is About 2500."]
[10.045368194580078, 3.2540531158447266, "The Eccentricity of the Secondary Payloads Unknown is 0.075."]
[6.118197917938232, 1.760637879371643, "The Retirement Date of the SAR-Lupe Constellation Satellite Constellation is After November 2017."]
[4.784579277038574, 1.9732435941696167, "The Number of Ranging Stations of the LAGEOS Satellite is 183."]
[7.77040958404541, 8.864641189575195, "The Spectral Range of the Instrument Satellite Instrument is 450-700 nm."]
[1.3335455656051636, 4.3047027587890625, "The Minimum Battery Voltage of the IXV Spacecraft is 30.4 V."]
[4.301237106323242, 4.597009658813477, "The Function of the Instrument Control Unit (NI-ICU) Control Unit is General power supply."]
[3.172273874282837, 5.310489177703857, "The Capacity of the High capacity solid-state recorder Recorder is 9 Tbit."]
[7.77547550201416, 5.891154766082764, "The Solar Irradiance Measurements of the TRUTHS Satellite is Direct measurements of Earth incident solar irradiance, total and spectrally resolved."]
[11.437681198120117, -1.331214189529419, "The Weight of the SUCHAI-1 Satellite is 1 kg."]
[1.2861415147781372, 4.193220138549805, "The Li-ion Battery Capacity of the PARASOL microsatellite Satellite is 15 Ah."]
[5.1861958503723145, 4.735745906829834, "The Location of the Ground Station Ground Station is Montpellier University campus."]
[8.220654487609863, 8.602486610412598, "The Quantity of the VIS Unit is 5."]
[6.240325927734375, 9.693286895751953, "The Instrument mass of the Spectrometer Spectrometer is 152 kg."]
[5.263341426849365, 3.487746477127075, "The Activation Sequence of the ISM Satellite Component is Two diagonal corners, then the other two."]
[4.041860580444336, 1.2004916667938232, "The Mission Type of the Rosetta Spacecraft is Non-EO."]
[3.480464458465576, 5.324570655822754, "The Data Returned of the Clementine Satellite is ~ 330 Gbit total."]
[3.8774404525756836, 6.4711503982543945, "The Ka-band Communication Link Speed of the GEO LCT Laser Communication Terminal is 600 Mbit/s."]
[10.009778022766113, -0.7708172798156738, "The Structure Dimensions of the Baumanets-2 Microsatellite is 460 mm in diameter and 530 mm high."]
[6.110212326049805, 3.2453696727752686, "The Development Collaboration of the Satellite Platform is ESA and CNES."]
[7.8339433670043945, 5.169272422790527, "The Orbit Determination Goals of the GEOSAT Follow-On Satellite is High Accuracy and Near-Real-Time Processing."]
[3.2839179039001465, 5.375100135803223, "The Data Capacity of the MOMS-2P Instrument is 4 Gbyte."]
[4.146912574768066, 5.737555503845215, "The TT&C Communications of the Spacecraft Satellite is 4 kbit/s (uplink), 32 kbit/s to 6.25 Mbit/s (downlink)."]
[4.022046089172363, 5.555520534515381, "The Optical Link Bandwidth (Downlink) of the OICETS satellite Satellite is 50 Mbit/s."]
[8.861957550048828, 6.414180278778076, "The Mounting Interface of the Active Pointing Control Mechanism Mechanism is Invar ring."]
[7.259511470794678, 1.4442684650421143, "The Conference Presentation Date of the EO-1 Satellite is Mar. 6-13, 2004."]
[5.720478534698486, 2.3563120365142822, "The Predecessor of the SAR-Lupe system Satellite System is SARah system."]
[7.18596076965332, 0.6980391144752502, "The Launch Date of the CHAMP Satellite is July 15, 2000."]
[8.792503356933594, 1.488134741783142, "The Measurement of the Van Allen Probes Satellite is Sudden pulse of electrons energized to extreme speeds."]
[7.702756404876709, 7.180175304412842, "The Storage Location of the TEMPO Instrument is Maxar\u2019s satellite manufacturing facility in Palo Alto, California."]
[6.1868109703063965, 8.531298637390137, "The Scanning of the MIS Instrument Microwave Radiometer is Conical scanning at 31.6 rpm."]
[11.448199272155762, 3.7916486263275146, "The Extinction of the Ichthyosaurs Marine Reptiles is The creatures are now extinct."]
[5.960058212280273, 6.426011562347412, "The Near Incidence Angle of the Instrument SAR is >23\u00ba."]
[5.5912981033325195, 2.331159830093384, "The Monitoring Capability of the SBSS Satellite System is Objects as small as a 1 m cube all the way out to the Geosynchronous belt at 35, 786 km from Earth."]
[8.04457950592041, 8.485166549682617, "The On-axis Unapodized Spectral Resolution Requirement of the Michelson Interferometer Interferometer is \u2264to the values given in Table 5."]
[4.349941253662109, 5.604695796966553, "The TT&C Communication Band of the TTCS Telemetry & Telecommand Subsystem is S-band."]
[6.192982196807861, 3.399261474609375, "The Mounting Location of the HDEV High-Definition Earth-Viewing System is External Payload Facility of the European Space Agency\u2019s Columbus module."]
[8.680658340454102, 10.045928955078125, "The Number of Subapertures of the PAIS Imaging System is 8."]
[11.114420890808105, 5.11732292175293, "The Extended Mission Duration of the LISA Pathfinder Spacecraft is Seven months."]
[8.104792594909668, 0.8884589672088623, "The Liftoff Date of the Landsat-9 Satellite is Sept. 27."]
[5.10389518737793, 5.459747314453125, "The Quantity of the DSN Antennas Ground Antennas is 7."]
[10.239891052246094, 9.392950057983398, "The Spatial Resolution of the IRIS Satellite is 0.33 arcsec."]
[4.842535972595215, 0.8698486685752869, "The Development Cost of the FORUM Satellite Mission is \u20ac160 million."]
[7.567800521850586, 1.6664586067199707, "The Article Publication Date of the Magnetospheric Multiscale Mission Satellite is 3 Jan. 2018."]
[7.210197925567627, 2.470550537109375, "The URL of the NASA's Spaceborne Carbon Counter Satellite is http://www.jpl.nasa.gov/news/news.php?release=2014-435."]
[4.808793067932129, 4.7786993980407715, "The Data Compression of the Ground Segment Communication System is Prior to transmission to the ground."]
[4.440537452697754, 3.0005078315734863, "The PRN of the GSAT-0203 Satellite is 26."]
[9.22554874420166, 7.38565731048584, "The Temperature of the Primary Sensor Sensor is >1300\u00baC."]
[4.370398998260498, 7.227055072784424, "The Volume of the X-band Transmitter Transmitter is 240 mm x 196 mm x 185 mm."]
[7.286174297332764, 7.0500874519348145, "The Emissive Band Uses of the VIIRS Satellite is Cloud imagery, precise geolocation, surface temperature determination, cloud top pressure determination, fire detection."]
[9.926484107971191, -0.5562166571617126, "The Orbit Type of the Tsubame Microsatellite is Sunynchronous."]
[7.122990131378174, 0.5986258387565613, "The International Astronautical Congress Date of the Odin Satellite is October 6-10, 1997."]
[6.8340983390808105, 5.544807434082031, "The Soil Moisture Resolution of the SMAP Satellite is 10-km."]
[4.433170318603516, 4.059474468231201, "The Interface Compatibility of the Spacecraft Avionics EDU Avionics is Matches the power and data interfaces of the flight spacecraft, and the command interface of the flight system."]
[10.159128189086914, 4.80834436416626, "The Diameter of the T5 thruster Ion Thruster is 10 cm."]
[10.400068283081055, 4.270349979400635, "The Launch Location of the Bloostar Launch Vehicle is Above 99% of the mass of the atmosphere."]
[1.8268667459487915, 3.9894497394561768, "The Solar Cells Type of the EPS Electric Power Subsystem is Triple-junction surface-mounted."]
[9.621548652648926, 1.752300500869751, "The Imaging Frequency of the Meteosat-11 Geostationary Satellite is Every 15 minutes."]
[8.68384838104248, 9.158258438110352, "The Tolerable Misalignment of the Spectrometer Channel Optical System is On the order of the slit width."]
[9.151310920715332, 4.064320087432861, "The Dimensions of the NorSat-3 Satellite is 0.62 m x 0.56 m x 0.33 m."]
[7.467626094818115, 8.925056457519531, "The Spatial Resolution of the Instrument Spectrometer is 20 m (VIS); 62 m (NIR)."]
[7.612444877624512, 2.8662452697753906, "The Fly Over Precipitation of the RainCube Satellite is 6\u03c3 certainty within the first two days of payload operations."]
[7.8326921463012695, 8.687033653259277, "The Wavelength of the UVSP Instrument is About 1380 \u00c5 in second order."]
[6.991743564605713, -0.0883898138999939, "The Expected End of Life Date of the STARLETTE and Stella Satellites is At least 2050."]
[7.011653900146484, 4.346153736114502, "The Measurement Domain of the Megha-Tropiques Satellite is Atmosphere, Ocean."]
[11.830930709838867, -1.1157448291778564, "The Launch Mass of the IMP-8 Spacecraft is 410 kg."]
[7.44097375869751, 3.6253504753112793, "The Wing Status of the AC4-A Satellite is Closed."]
[6.901472091674805, 0.45487430691719055, "The Technology Demonstrator Mission of the Delfi-C3 Satellite is April 6-8, 2005."]
[9.140809059143066, 4.242903709411621, "The Stowed Dimensions of the Spacecraft Bus (Avionics Module=AM) Satellite is 1.1 m x 0.8 m x 0.8 m."]
[8.224522590637207, 7.293194770812988, "The Precision Measurement Method of the Servo-system Instrument Component is Measurement of the electrical power applied to each channel for the two cases."]
[8.488741874694824, 10.376830101013184, "The Array Size of the Detector Array CCD is 2048 x 4096 square pixels."]
[7.976086139678955, 1.4506629705429077, "The Validation Date of the SCARLET Advanced Array Solar Array is Aug. 2, 1999."]
[4.362563610076904, 3.290837526321411, "The Use Cases of the Satellite for 5G Satellite is Disaster response, relieving ground network congestion, serving areas with poor terrestrial links."]
[8.834685325622559, 10.261568069458008, "The Technology of the C3D Instrument CMOS Sensor is CMOS."]
[7.525720119476318, 8.965222358703613, "The Channel Centre Wavelengths of the LIMS Limb Infrared Monitor is 6.25, 6.75, 9.65, 11.35, 15.25 \u00b5m and one broad channel from 13.3 - 17.2 \u00b5m."]
[7.392237663269043, 9.144482612609863, "The Swath Width of the IIM instrument Imaging Spectrometer is 25.6 km."]
[8.49774169921875, 4.721426010131836, "The Operating Mode of the Sich-2 Satellite is Program tilt mode during imaging."]
[6.899022102355957, 5.4312849044799805, "The Mission of the SMOS Satellite is Soil moisture and ocean salinity data."]
[4.166463851928711, 6.580917835235596, "The Operation Basis of the LCT Laser Communication System is Coherent (homodyne digital receiver and BPSK modulation)."]
[5.384675979614258, 5.890796184539795, "The Deployment of the Reflectarray Antenna Antenna is Can be folded down against the CubeSat."]
[8.128277778625488, 8.396878242492676, "The Dynamic Alignment System of the Michelson Interferometer Interferometer is Equipped."]
[6.147014141082764, 2.726682424545288, "The Mission Funding of the SORTIE Satellite is NASA Heliophysics Technology and Instrument Development (H-TIDeS) program grant."]
[9.543353080749512, 9.883319854736328, "The Mounting Location of the ShadowCam Instrument is Korean Aerospace Research Institute (KARI)."]
[6.56913948059082, -0.08697358518838882, "The Launch Date of the PSLV-C33/IRNSS-1G Satellite is April 28, 2016."]
[3.3736770153045654, 5.122367858886719, "The Data Transfer of the ASAP-Light Camera System is Ground station communication passes."]
[1.9188218116760254, 4.201972961425781, "The Power of the Solar Panels Power Subsystem is 14 W (max)."]
[12.1082181930542, 3.2835662364959717, "The Inclination of the Main Payload Satellite is 98\u00ba."]
[8.989965438842773, 7.385317325592041, "The Objective of the EPAM Electron, Proton, and Alpha-particle Monitor is Measurement of solar and interplanetary particle fluxes with a wide dynamic range and a directional coverage of nearly a full unit sphere."]
[5.806640625, 3.7042298316955566, "The Lead Organization of the LCRD Payload is NASA\u2019s Goddard Space Flight Center."]
[5.2642822265625, 9.277939796447754, "The VBB Performance of the SEIS Instrument Seismometer is -9 m s-2 Hz-\u00bd from 10-3 up to 10 Hz."]
[6.852263450622559, 1.5096343755722046, "The Testing Completion Date of the RapidEye Satellite is Unknown."]
[7.967376708984375, 8.663911819458008, "The Spectral Resolution of the FTS Fourier Transform Spectrometer is 0.04 to 1 cm-1."]
[5.076179027557373, 7.482062339782715, "The Average Data Rate Over Ocean of the KaRIN Instrument is ~3 Mbit/s."]
[5.453023433685303, 2.6060330867767334, "The Mission Name of the XI-V CubeSat is X-factor Investigator-V."]
[8.541350364685059, 6.521182060241699, "The Metrology Metric of the Drag-Free Technology Technology is Measurement of the absolute position of a drag-free test mass or the differential measurement of the distance between two drag-free test masses."]
[8.114075660705566, 2.909662961959839, "The Bistatic X-band Experiment Date of the TerraSAR-X Satellite is November 2007."]
[6.793291091918945, 1.2305785417556763, "The Conference Presentation Date of the GIOVE-A Satellite is June 11-14, 2006."]
[11.224645614624023, 6.794707775115967, "The Wavelengths of the NuSTAR X-ray Telescope is Almost the whole range of X-ray wavelengths."]
[9.666326522827148, -0.8431673049926758, "The Size of the Aalto-1 Nanosatellite is 3U CubeSat."]
[7.166637897491455, 8.911418914794922, "The Swath Width of the EOS-T Instrument is 14 km."]
[5.169593334197998, 6.20072603225708, "The Number of Linear Arrays of the Radiating Board Antenna Component is 8."]
[6.74655294418335, 5.799635887145996, "The Evaluation Data of the AVTP and AVMP retrievals Data Products is Global ECMWF analysis fields, radiosonde (RAOB) measurements, and AIRS (Aqua-Atmospheric Infrared Sounder) heritage algorithm retrievals."]
[2.2648472785949707, 5.0691046714782715, "The Maximum of the Power Consumption System is 12 W."]
[6.435696125030518, 2.5936410427093506, "The Globally Averaged Sea Level Measurement Goal of the Jason-3 Satellite is Zero bias \u00b11 mm (standard error)."]
[10.35448932647705, 4.910334587097168, "The Function of the Resistojets Propulsion System is Acts as a vaporizer to ensure no liquid propellant is expelled, as well as increasing the specific impulse of the system."]
[11.274775505065918, 3.533900022506714, "The Water Vapor Emission of the Patch on Comet Surface Surface Feature is 3% of the total amount."]
[6.06652307510376, 2.732665777206421, "The CEO of the HawkEye 360 Company is John Serafini."]
[7.263484477996826, 0.26101410388946533, "The Launch Date of the SWFO-L1 Satellite is 31 October 2024."]
[8.71053695678711, 6.568991184234619, "The Number of Micro-g Accelerometers of the Boom Structure is 24."]
[7.789433002471924, 3.180964469909668, "The Wheel Configuration of the CartoSat-2 Satellite is Tetrahedral."]
[7.909826278686523, 2.9502274990081787, "The MSP/MGN Operation Data of the Hitomi X-ray Astronomy Satellite is Only HK data during visible time."]
[4.588388442993164, 5.037813186645508, "The Objective of the FITSat-1 Satellite is Demonstrate a high-speed transmission module for a small satellite and a visible light communication experiment using high power LEDs."]
[6.479488849639893, 7.32461404800415, "The Polarization of the ScanSAR Imaging Mode is Single."]
[10.734759330749512, 10.291683197021484, "The Shaping of the PHA Detector is Bipolar, 1.9 \u00b5s to peak."]
[9.312764167785645, 8.046063423156738, "The Angle Measurements of the TED Particle Detector is 0\u00ba and 30\u00ba from the local vertical."]
[6.696971416473389, 7.186537265777588, "The Measurement of the GEDI Lidar Instrument is Forest canopy height, canopy vertical structure, and surface elevation."]
[6.365163326263428, 3.3963680267333984, "The Operations Manager of the GOES-N Satellite is United States Space Force (USSF)."]
[1.5668678283691406, 4.877397060394287, "The Bus Voltage of the EPS Power Subsystem is 28 to 33 V."]
[5.389209270477295, 5.6244096755981445, "The Channels of the TopStar-3000 G1 GPS Receiver is 12."]
[11.186927795410156, -1.523049235343933, "The Mass of the KickSat CubeSat is ~5.5 kg."]
[3.7087955474853516, 6.250304698944092, "The Uplink Baud Rate of the CMC Transceiver Communication Device is 1200 baud."]
[4.357742786407471, 4.892796039581299, "The Design of the Signal Processing System Signal Processing System is High performance and ultra low-power analog VLSIs that can processes multi signals simultaneously."]
[4.4827680587768555, 2.4336860179901123, "The Satellite Type of the LEMUR-2 constellation Satellite Constellation is 3U CubeSats."]
[3.6788489818573, 6.311794757843018, "The Baud Rates of the High-speed link Radio Link is 600 - 19200 baud."]
[4.6737799644470215, 2.6866371631622314, "The Maximum Number of Racks of the JEM/Kibo Japanese Experiment Module is Up to 23 racks."]
[7.5616302490234375, 7.823672771453857, "The Data Gathered of the MAHRSI Instrument is New vertical profile data on the distribution of OH in the mesosphere and upper stratosphere."]
[5.007893085479736, 4.621264457702637, "The Purpose of the Optical Ground Station Ground Station is Initial thrust testing."]
[6.49113655090332, 1.1044139862060547, "The Period of Performance of the Joint Polar Satellite System Common Ground System contract Contract is September 30, 2022."]
[8.085105895996094, 1.340400218963623, "The Peak Time of the Water Production Comet Activity is Between the end of August and early September 2015."]
[5.838503360748291, 6.408066272735596, "The PRF of the CSG-SAR Synthetic Aperture Radar is Programmable (500-7000 Hz)."]
[9.022298812866211, 4.772153377532959, "The Solar Panel Orientation of the X-Sat Satellite is Pointed towards the sun, except during imaging or downlinking operation during certain orbits over a small portion of its period."]
[9.085164070129395, 5.015146255493164, "The Roll Tilt Capability of the Satellite Satellite is \u00b135\u00ba."]
[6.97471284866333, 4.505879878997803, "The Instrument Type of the TUBSAT Satellite is High resolution optical imagers, Other, Data collection, Hyperspectral imagers."]
[11.140454292297363, 2.3305394649505615, "The Depth of the Firn Drill Drilling Tool is About 50 meters."]
[4.86676025390625, 0.8869065642356873, "The Net Present Value (NPV) of the Climate Damages N/A is Tens of trillions of US dollars."]
[7.808830261230469, 8.736218452453613, "The MTF of the Telescope Optical Instrument is < 3 nm."]
[8.476078033447266, 2.902531385421753, "The Source of the Most Intense Auroras of the Jupiter Planet is Not the observed electric potentials."]
[13.157386779785156, 4.007613658905029, "The Scriptable Interface of the Gaia Satellite is Python, C, Java."]
[6.94009256362915, 8.219048500061035, "The Transmit Pulse Length of the SCA Calibration System is 600 \u00b5s."]
[6.70729398727417, 2.2791590690612793, "The Data Source of the GPM Satellite Mission is IMERG."]
[8.53089714050293, 1.10359525680542, "The Timeframe of the Operation Practice/Rehearsal Activity is Year 2017."]
[9.1256103515625, 5.721353530883789, "The Primary Sensor of the SpinSat Spacecraft is The spacecraft itself."]
[12.890860557556152, 4.162868976593018, "The Distance Limit of the Gaia Catalogue of Nearby Stars Stellar Census is 326 light years."]
[3.45940899848938, 5.457047462463379, "The Onboard Data Storage of the RF Communication System Communication System is Up to 64 kbyte."]
[3.852296829223633, 6.527375221252441, "The Bandwidth of the HDR Terminal Communication Equipment is 900 MHz."]
[7.986167907714844, 7.488509654998779, "The Components of the Spectral Calibration Calibration is ISRF Shape, SSI, SR, Smile, CU."]
[9.389851570129395, 0.9770658612251282, "The Duration of the Inspiration4 Mission is Three days."]
[8.13936996459961, 0.36124086380004883, "The Mission Status of the ISS-RapidScat Instrument is Mission complete."]
[7.825920104980469, -0.032032232731580734, "The Docking Status of the ATV-5 Satellite is De-docked."]
[10.393390655517578, 9.645533561706543, "The Launch Date of the IRIS Satellite is June 27, 2013."]
[5.410655975341797, 4.898226261138916, "The Additional Downlink Subsystem of the Sentinel-1, -2 Satellites is Optical Communications Payload (OCP)."]
[7.607895374298096, 1.174797534942627, "The Image Acquisition Date of the Sentinel-1A Satellite is 2014."]
[9.04771614074707, 10.648726463317871, "The Intensity Levels of the LISS-3 camera Camera is Six."]
[8.329121589660645, 4.599413871765137, "The Swath Width of the ALOS-4 Satellite is 50 km."]
[8.06620979309082, 10.009886741638184, "The Spatial Resolution of the MWIR Imager Imaging Device is 3.5 m."]
[9.15104866027832, 10.245755195617676, "The Attachment Method of the LWIR Camera Camera is Room temperature vulcanizing silicone-566 (RTV)."]
[4.176394462585449, 6.373147964477539, "The Development, Test and Flight Results of the RF Systems Communication Systems is Unknown."]
[9.935234069824219, 2.9195990562438965, "The Orbit of the Spacecraft Satellite is SSO, altitude of 623 km x 650 km, inclination = 98\u00ba, LTDN= 10:30 hours."]
[10.200126647949219, 1.0108985900878906, "The LTDN of the SEOSAT-Ingenio Satellite is 10:30 hours."]
[7.7232255935668945, 1.6729189157485962, "The Event of the SMOS Satellite is SMOS gains clearer view as illegal transmitters shut down."]
[2.127809524536133, 4.549864292144775, "The Navigation Payload Power of the GNSS Satellites Satellite is Kilowatt."]
[8.30909538269043, 4.574051380157471, "The Swath Width of the Satellite Imaging Satellite is 63 km."]
[5.8717360496521, 6.464332103729248, "The Bandwidth of the Instrument SAR is 6 MHz."]
[9.488736152648926, 0.9564960598945618, "The Duration of the Passivation Phase Spacecraft is About 700 s."]
[8.739018440246582, 7.911498069763184, "The Mass Resolution of the INMS Ion and Neutral Mass Spectrometer is Approximately 12."]
[6.349074840545654, 5.0112810134887695, "The Description of the At-Sensor-Radiance Product (L1B) Data Product is The product is radiometrically calibrated, spectrally characterized, geometrically characterized, quality controlled and annotated with preliminary pixel classification (usability mask)."]
[4.737477779388428, 0.8138013482093811, "The Adjusted EBITDA of the Satellogic Satellite Company is \u2013$30.7 million."]
[7.185612201690674, 5.779441833496094, "The Purpose of the OCI Instrument is Derive optical properties of chlorophyll-sensitive species in the ocean and ocean color."]
[12.104575157165527, 3.279907464981079, "The Orbit Inclination of the Max Valier Satellite is 98\u00ba."]
[6.790835380554199, 4.512288570404053, "The Areas of Focus of the Copernicus Programme Earth Observation Program is Climate change and global warming."]
[9.377235412597656, 2.695152521133423, "The Inter-Orbit Communication Experiment of the Eureca Satellite is Unknown."]
[7.674659252166748, 7.865705966949463, "The Measurement Principle of the OLME Ozone Monitor is Solar Backscatter Ultraviolet (SBUV)."]
[7.120275020599365, 3.1057348251342773, "The Mission Status of the LAICE Satellite is Planned."]
[7.284065246582031, -0.7432824373245239, "The Contact Success of the CYGNSS Satellite Constellation is 100%."]
[10.70688247680664, 10.303776741027832, "The ADC resolution of the PHA Detector is 11 bits, 12th bit overflow."]
[7.656049728393555, 1.6152104139328003, "The Mission End Date of the SMOS Satellite is Unknown."]
[7.372228145599365, 6.922970294952393, "The Data Release Start Date of the RPW Radio and Plasma Waves Instrument is After 15 June."]
[9.45374584197998, 9.03173828125, "The Focal Length of the Telescope Optical Instrument is 2626 mm."]
[9.595136642456055, 8.100212097167969, "The Accuracy of Position Determination of the Gamma-ray Counter Detector is < 5\u00ba."]
[9.048151969909668, 8.367559432983398, "The Rotation of the Calibration Mirror TIR Subsystem Component is Rotatable."]
[10.205462455749512, 3.0409233570098877, "The Altitude of the SARAL/AltiKa Satellite is 800 km."]
[5.798266410827637, 0.8239090442657471, "The ADCS Status of the AlSat Nano Satellite is Verified and activated."]
[9.349994659423828, 10.474958419799805, "The Pointing Altitude of the FAI Camera is 110-km."]
[5.849809169769287, 8.12743091583252, "The Frequency (GHz) of the ICI-8 Radiometer is 448\u00b17.2."]
[3.5443708896636963, 5.399804592132568, "The Fiber Core Diameter of the Data Storage System Satellite Component is 200 \u00b5m."]
[8.026385307312012, 2.900393009185791, "The Operation Status of the TerraSAR-X Satellite is Nominal as of 2010."]
[7.026003360748291, -0.007215258199721575, "The End of Life Date of the MidSTAR-1 Satellite is 30 April 2009."]
[9.564773559570312, 5.506442070007324, "The Pointing Stability of the AOCS Attitude and Orbit Control Subsystem is 10 \u00b5rad (N/S and E/W) peak to peak over 8 s period."]
[6.109058856964111, 4.034425735473633, "The Data Relay of the Trace Gas Orbiter (TGO) Satellite is NASA\u2019s Curiosity Mars rover and InSight lander."]
[8.938067436218262, -0.39589381217956543, "The Collision Avoidance Requirement of the IDEA OSG 1 Satellite is 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."]
[8.558269500732422, 10.522388458251953, "The CCD Line Read-Out Rate of the Focal Plane Module Imaging Device is 6.5 MHz."]
[11.794303894042969, 4.829599857330322, "The Black Hole Mass of the Leo I Galaxy is Nearly as massive as the Milky Way's."]
[9.168601036071777, 3.2379748821258545, "The Orbit Type of the SPARCS Satellite is Sun-synchronous terminator orbit."]
[3.959947109222412, 4.463284015655518, "The Protocol of the OBC On-Board Computer is CSP (CubeSat Space Protocol)."]
[1.7683684825897217, 4.688424587249756, "The Power Generation of the IRIS Satellite is 28 V."]
[2.036292791366577, 4.4494500160217285, "The Solar Array Demand of the MTM Transfer Module is 2 x 5 kW."]
[7.9698805809021, 7.597562789916992, "The Spectrometer of the The Rossi Explorer Satellite is Device used to uncover properties of the light source, such as speed and rapid variations in the order of milliseconds."]
[6.42097282409668, 1.6681346893310547, "The Planning Start of the Jason-CS Satellite Mission is 2009/10."]
[8.96583080291748, 7.547638893127441, "The Purpose of the S-WPIA Wave Particle Interaction Analyzer is Measure the wave-particle interactions."]
[8.26164436340332, 8.32590103149414, "The Detector Assembly of the Sounder Satellite Instrument is 4."]
[7.307285785675049, 0.2719172239303589, "The Launch Date of the Tandem-L satellites Satellite is End of 2022."]
[6.464838027954102, 3.9439942836761475, "The Deployment Test Location of the Copernicus Sentinel-1C Satellite is Airbus\u2019 facilities in Germany."]
[4.497664928436279, 5.376127243041992, "The Issue of the TT&C System Satellite System is Spacecraft ignoring commands from the ground stations."]
[7.989301681518555, 1.4285049438476562, "The Water Detection Date of the Bullialdus Crater Lunar Crater is August 25, 2013."]
[10.598091125488281, -1.1165400743484497, "The Mass of the NanoRacks Kaber Microsat Deployer Satellite Deployer is 10 kg."]
[5.8089728355407715, 3.6025400161743164, "The Location of the STScI Science Operations Center is Baltimore, Maryland."]
[7.452980995178223, 0.7758355736732483, "The Removal from Service Date of the Monitor-E Spacecraft is August 2008."]
[8.413678169250488, 7.668173789978027, "The Provider of the MORE Memory Orbit Radiation Experiment is IDA TU Braunschweig."]
[7.7839436531066895, 8.472378730773926, "The Dust Measurement Altitude of the UVS Instrument is Down 300 m."]
[4.777101993560791, 5.316479682922363, "The Machining Technique of the Satellite Communication is WEDM (Wire Electrical Discharge Machining)."]
[5.066970348358154, 8.723591804504395, "The Position Accuracy (RMS orbit) of the S-3 STC Product is 4 cm threshold with a target of 3 cm (radial)."]
[4.979221343994141, 4.822390079498291, "The Functions of the G/S Ground Station is S- and X-band functions for signal modulation/demodulation."]
[9.344645500183105, -0.7818281650543213, "The Launch Time of the SOCRATES Microsatellite is 03:05 UTC."]
[8.947893142700195, 2.7699856758117676, "The Presenter of the GCOM-W Satellite is Toru Fukuda."]
[7.3811211585998535, 8.361734390258789, "The Image Downlink Time of the AgCam/ISSAC Imaging System is Several hours of powered operations immediately following collection."]
[7.427626609802246, 7.435172080993652, "The Conference Date of the OMI Ozone Monitoring Instrument is Oct. 14-17, 2008."]
[12.14079475402832, 2.164663314819336, "The Sample Delivery Date to Earth of the OSIRIS-REx Spacecraft is September 24, 2023."]
[8.950028419494629, 3.2858757972717285, "The Flight Path of the Gravity Probe A Satellite is Ballistic (sub-orbital)."]
[5.2984089851379395, 3.237614631652832, "The Purpose of the BeaverCube CubeSat is Gather important ocean and atmospheric measurements."]
[6.023801326751709, 3.9533772468566895, "The Instrument Type of the GovSat-1 Communication Satellite is Communications."]
[9.907083511352539, 3.992166757583618, "The Conference Presentation of the NanoSail-D Satellite is Aug. 11-14, 2008."]
[9.12824821472168, 3.12599778175354, "The TLE Generation of the Orbit Dynamic System System is By mean processing of a 6 lap orbit."]
[9.220110893249512, 4.784232139587402, "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."]
[7.365375995635986, 0.8470604419708252, "The Lunar Swing-by Date of the Queqiao Communication Satellite is May 25, 2018."]
[10.111858367919922, 3.06351900100708, "The Altitude of the Satellite Imaging Satellite is 619km."]
[8.879312515258789, 10.366490364074707, "The Image Size of the Imager Camera is 37.25 mm x 25.70 mm."]
[9.175910949707031, 3.136971950531006, "The Orbit Type of the WV-1 Satellite is Sun-synchronous circular."]
[8.77670669555664, 10.283358573913574, "The Image Size of the Image Sensor Imaging is 37.25 mm x 25.70 mm."]
[7.271224498748779, 2.6659867763519287, "The Operator of the Hinode Spacecraft is JAXA/NASA."]
[10.264973640441895, 5.678431034088135, "The Electric Charge of the Tether Tether is 500 V."]
[6.186694622039795, 3.2802231311798096, "The Focus of the EIAST Organization is Satellite development, manufacturing, integration and application utilization."]
[8.283523559570312, 8.513510704040527, "The Detector Type of the Spectral Channels Satellite Instrument is Silicon."]
[7.514770984649658, 7.549741268157959, "The Performance of the MAG Instrument is \u00b130 nT."]
[7.403724193572998, 0.7033566236495972, "The Launch Date of the PROBA-V Satellite is Before July 2013."]
[11.184520721435547, 9.346877098083496, "The URL of the Nimbus Earth Radiation Budget (ERB) Experiment Satellite Experiment is http://badc.nerc.ac.uk/data/gedex/detail/erb_soli.det."]
[8.375585556030273, 0.6215453147888184, "The Observations for Performance Verification Dates of the Hitomi X-ray Astronomy Satellite is March 25 & 26, 2016."]
[7.505010604858398, 8.513947486877441, "The SNR for CH4 of the Instrument Spectrometer is \u2265400."]
[12.079657554626465, 3.2891457080841064, "The Inclination of the Orbit Satellite is 123\u00ba."]
[4.4550089836120605, 5.518062591552734, "The TT&C Transmission of the PRISMA Satellite is S-band."]
[7.595829010009766, 4.772390842437744, "The Primary Images of the PROBA-V Satellite is 8.345."]
[10.548182487487793, 7.533139705657959, "The MLI Surface Material of the ERG Satellite is Black polyimide film."]
[10.248209953308105, 6.842991828918457, "The Heater Lines of the OTC Thermal Control System is 13."]
[6.548952102661133, 3.5463144779205322, "The Space Segment of the Sentinel-6 Satellite is Two successive Jason-CS satellites (A and B)."]
[11.740864753723145, 1.6768035888671875, "The Initial Touchdown Point of the Philae lander Lander is Agilkia."]
[3.469639539718628, 4.6744303703308105, "The Dimensions of the FPGA Processing Device is 42.5 mm x 42.5 mm."]
[7.624826431274414, 4.872622966766357, "The S-band transmitter of the BEESAT-3 Satellite is Yes."]
[7.286853313446045, 8.564568519592285, "The Wavelength of the Laser Instrument is 1570 nm."]
[5.63252592086792, 2.037261724472046, "The Deployment System of the GeneSat-1 Satellite is P-POD (Poly\u00bfPicosatellite Orbital Deployer)."]
[8.781135559082031, 3.414966344833374, "The Purpose of the MinXSS-2 Satellite is Study how coronal soft X-rays vary over solar cycle timescales and what impact those variations have on the earth's upper atmosphere."]
[8.546955108642578, 6.446798801422119, "The Objective of the VEFI Instrument is 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."]
[7.640382766723633, 7.085652828216553, "The Dust Flux Measurement of the GIADA Contamination Monitor is Direct and Reflected Grains."]
[2.236677646636963, 4.451573371887207, "The Power Source of the RapidScat Satellite Instrument is Columbus module power circuit."]
[9.411965370178223, 0.34816470742225647, "The Exceeded Design Life of the ACRIMSat Satellite is Yes."]
[6.352059841156006, 9.22697639465332, "The Housing Mass of the MuREM Radiation Monitor is 0.5 kg."]
[11.682942390441895, 4.552393436431885, "The Star Masses of the Iota Orionis Binary Star System is 23 and 13 times the Sun's mass."]
[6.357706546783447, 3.244903087615967, "The Educational Objective of the ESEO Satellite is For university students to acquire hands-on experience of the full life cycle of a real space project."]
[4.88438606262207, 1.6574046611785889, "The Number of Planes of the FormoSat-3/COSMIC-1 Satellite Constellation is 6."]
[6.476075649261475, 0.5393708348274231, "The Launch Date of the SkySat 3 Satellite is June 22, 2016."]
[8.500856399536133, 10.483402252197266, "The CCD Line Pixel Pitch of the Focal Plane Module Imaging Device is 6.5 \u00b5m."]
[5.61609411239624, 1.4462796449661255, "The Launch Site of the Falcon 9 rocket Rocket is Vandenberg Air Force Base."]
[9.378059387207031, 8.199617385864258, "The Temperature of the CCD Imager is As low as -110\u00baC."]
[6.180150508880615, 2.2575907707214355, "The Partners of the TacSat-3 Satellite is 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."]
[8.533061981201172, 9.062751770019531, "The Band 1 of the R3 Sensor Sensor is Pan."]
[8.262969017028809, 2.4702107906341553, "The Birth Year of the Max Valier Person is 1895."]
[9.568584442138672, 0.5588698983192444, "The Operational Lifetime of the Jugnu mission Satellite Mission is 1 year."]
[11.361429214477539, -0.709290087223053, "The Total Mass of the BA 330 module Space Module is 23,000 kg."]
[4.95523738861084, 1.9390816688537598, "The Number of Maneuvers of the Swarm-A Satellite is 9."]
[8.413349151611328, 9.760903358459473, "The Detector Type of the FUV Instrument Spectrometer is Intensified CCD."]
[7.911045551300049, 0.45361602306365967, "The Data Merge Start Year of the CryoSat-2 and SMOS Satellites is 2010."]
[7.074197769165039, 4.489625453948975, "The Camera Type of the Gaia Satellite is CCDs."]
[8.77119255065918, 8.560745239257812, "The Scanning Angle of the Scanning geometry Instrument is 108\u00ba, 54\u00ba."]
[9.385977745056152, 9.958669662475586, "The Size of the APD detector Experiment is Very small."]
[9.113950729370117, 2.1266162395477295, "The Mission Difficulty of the BepiColombo Satellite is Most difficult."]
[8.84854793548584, 7.660706043243408, "The Components of the IVM Ion Velocity Meter is Two planar thermal ion sensors, a RPA (Retarding Potential Analyzer) and an IDM (Ion Drift Meter)."]
[3.23504900932312, 6.071719169616699, "The Purpose of the Frontier Radio Lite Radio is Communication."]
[7.885743141174316, 8.788359642028809, "The Spectral Resolutions (FWHM) of the Limb Sensor Sensor is 0.75 nm at 290 nm to 25 nm at 1000 nm."]
[11.559345245361328, -1.2853026390075684, "The Mass of the BILSAT-1 Satellite is Around 120 kg."]
[8.831806182861328, 9.409733772277832, "The Keystone of the System Optical System is Less than 0.4 \u00b5m."]
[7.229094982147217, 0.8424070477485657, "The Launch Preparation Date of the Rain and Snow Satellite Satellite is Jan. 27, 2014."]
[7.100528240203857, 5.086649417877197, "The Methane Emissions of the Hugo Satellite is Approximately 4000 kg per hour."]
[5.758914470672607, 1.6546756029129028, "The Purpose of the GomX-4B Satellite is Testing a micro-propulsion system, testing an inter-satellite radio link, carrying a hyperspectral imager."]
[8.12109088897705, 4.925594329833984, "The DEM Generation of the ALOS PRISM Satellite is Precise."]
[4.914847373962402, 1.849325180053711, "The Number of Satellites of the Pl\u00e9iades Neo Satellite Constellation is 4."]
[11.637563705444336, 1.2727174758911133, "The Image Credit of the Analog-1 rover Rover is ESA\u2013A. Koehler."]
[10.166176795959473, 5.109532356262207, "The Thrust Capability of the MICROSCOPE Satellite is Micronewton."]
[10.155094146728516, 1.6607415676116943, "The Period (min) of the Intercosmos- Bulgaria 1300 (Intercosmos-22) Satellite is 101.9."]
[10.073019027709961, 4.0482611656188965, "The Solar Sail Deployment Test Location of the NEA Scout Spacecraft is NeXolve, a space materials company near Marshall Space Flight Center in Huntsville, Alabama."]
[3.763803005218506, 4.473616123199463, "The CPU of the OBC On-Board Computer is 16-bit CPU of Siemens."]
[6.753384113311768, 2.7002077102661133, "The URL of the OPS-SAT Satellite is http://esamultimedia.esa.int/docs/gsp/C4000108683ExS.pdf."]
[6.7129106521606445, 7.666562557220459, "The Laser Transmitter Range of the OLA Instrument is ~7.5 km down to ~1km."]
[11.613158226013184, 4.3635711669921875, "The Energy Received from Star of the Kepler-186f Exoplanet is One-third of the energy Earth gets from the sun."]
[6.576487064361572, 0.592316746711731, "The Launch Date of the GEOSAT Satellite is 12 March 1985."]
[8.802809715270996, 7.934625148773193, "The Ionization Efficiency of the MCP Multi-Channel Plate is 80-120 eV."]
[3.1054880619049072, 6.636477947235107, "The Output Power of the CC1101 UHF transceiver Transceiver is Up to 10 mW."]
[3.7775588035583496, 6.130511283874512, "The Bit Error Rate of the Optical link Communication System is 10 -8."]
[9.048052787780762, 9.283470153808594, "The Drawback of the Photon Sieve Optic is Limited bandwidth."]
[4.940214157104492, 6.189088821411133, "The Frequency (MHz) of the Compass-BeiDou B1 Signal Carrier is 1575.42."]
[9.579233169555664, 3.6393845081329346, "The Purpose of the LDEX Instrument is Detect presence of water ice in the permanently shadowed lunar craters."]
[6.664770603179932, 3.9362120628356934, "The Applications of the TRISHNA Satellite is 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 an."]
[3.2020976543426514, 5.409232139587402, "The Operation Commands of the SSRNI Data Acquisition and Registration System is Yes."]
[7.827878952026367, 5.9525465965271, "The Purpose of the GIRO GSICS Implementation of the ROLO model is Address the increasingly challenging calibration needs for the next generation of satellite instruments."]
[7.950387954711914, 10.212445259094238, "The Imagery Geolocation Accuracy without GPCs of the WV60 imager Imaging System is 5.8 m-7.6 m."]
[7.072000980377197, 0.9289082288742065, "The launch date of the RASAT Satellite is August 17, 2011."]
[7.435914993286133, 9.312986373901367, "The Bands of the GOES Sounder Sounder is 1 VIS band, 3 SWIR bands, 6 MWIR bands, 9 TIR bands."]
[10.063203811645508, 5.137936115264893, "The Thruster Type of the Cold Gas System Attitude and Orbit Control Subsystem is 16 attitude control thrusters, 4 orbit control thrusters."]
[7.811243057250977, 9.069849014282227, "The Spectral Sampling Distance of the VIS Spectrometer is 0.21 nm."]
[4.627898216247559, 5.560969352722168, "The Data Downlink Band of the SWFO-L1 Satellite is X-band."]
[6.070221424102783, 4.397514820098877, "The Purpose of the ERA Robotic Arm is 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."]
[6.09928035736084, 0.585565447807312, "The End Date of the CubeRRT mission CubeSat is 30 November 2020."]
[11.697325706481934, 4.8637495040893555, "The Radiation Diminishment of the The Teacup Quasar is 50 to 600 times over the last 40,000 to 100,000 years."]
[11.74660587310791, 1.1929545402526855, "The Visible and Near-Infrared Imaging Spectrometer (VNIS) of the Chang\u2019e-4 Rover Rover is Payload."]
[6.803585052490234, 2.808976173400879, "The Managing Center of the SMAP Satellite is NASA's Jet Propulsion Laboratory in Pasadena, California."]
[9.137970924377441, 8.724655151367188, "The Substrate Material of the Grating Optical Component is SiC."]
[4.906565189361572, -3.2472386360168457, "The | of the Robert O. Knuteson Individual is Fred A. Best, Douglas P. Adler, Claire Pettersen, Henry E. Revercomb, P. Jonathan Gero, Joseph K. Taylor, Robert O. Knuteson, John H. Perepezko."]
[11.4747896194458, 2.173153877258301, "The Arrival Date of the Hayabusa-2 Space Probe is December 7, 2020."]
[9.306365013122559, 0.8548792004585266, "The Lifetime of the Instrument Satellite Instrument is 3.25 years."]
[10.513643264770508, 8.452230453491211, "The Objective of the COR2 Coronagraph2 Imager is Explore the outer corona (2-15 Rsun) in white light and pB with high spatial and temporal resolutions."]
[4.7635884284973145, 0.8699702024459839, "The Total Addressable Market of the Satellogic Satellite Imaging Company is $140 billion."]
[9.459580421447754, 7.749996185302734, "The Ion Energy Range of the EPAM Particle Detector is Ei \u227350 keV."]
[7.486453533172607, 0.4514836370944977, "The Mission Profile Presentation Date of the SVOM Satellite is 10-15 April 2016."]
[7.771410942077637, 9.030508995056152, "The Spectral Resolution of the Instrument Spectrometer is 1200 (lambda/delta lambda)."]
[7.777163505554199, 0.009090792387723923, "The Launch Date of the IDEA OSG 1 Satellite is 28 November 2017."]
[11.544621467590332, 4.423696041107178, "The Composition of the White Dwarf Celestial Body is Rich in helium."]
[5.6548871994018555, 9.121474266052246, "The Power Consumption of the MIRAD Instrument is 500 mW."]
[9.58447551727295, 5.880162715911865, "The Control Loop Input of the ADACS Attitude Determination and Control Subsystem is GPS position knowledge."]
[5.2835164070129395, 2.603935718536377, "The Purpose of the ArgoMoon CubeSat is Demonstrate the ability to perform operations in close proximity of the ICPS."]
[4.706258296966553, 4.652616500854492, "The Services of the General Purpose Communication Network Communication Network is Data exchange with any other external system."]
[8.544397354125977, 8.269506454467773, "The Magnitude of the FGS Sensor is Brighter than the magnitude of 15 (MV)."]
[11.149149894714355, 4.076847076416016, "The Resonance of the TOI-178 Exoplanet System is Laplace."]
[7.132260799407959, 5.0469160079956055, "The Number of Detections of the Methane Leak Environmental Event is 12."]
[3.580212354660034, 6.630753517150879, "The X-band Transmitter Data Rate of the Measurement Data Data Transmission is 10 Mbit/s."]
[5.653512954711914, 1.9601914882659912, "The Launch Vehicle of the ORS-3 Mission Satellite Mission is Minotaur I."]
[8.488377571105957, 4.236128807067871, "The Orientation Accuracy of the GOMS-1 Satellite is \u00b12-5 arcmin."]
[9.819210052490234, -1.0013465881347656, "The LTDN of the JL-1-GF03B Microsatellite is 09:20."]
[7.828083038330078, 0.6317571401596069, "The Announcement Date of the UrtheCast Company is July 16, 2014."]
[4.263576507568359, 5.110167980194092, "The Redundancy of the Star Sensors Autonomous Star Sensors is Redundant units may be implemented with some minor penalties."]
[10.512048721313477, -1.0572717189788818, "The Total Mass of the Microsatellite Satellite is 20.5 kg."]
[8.563678741455078, 1.3655951023101807, "The Planned Image Production of the GOCI Geostationary Ocean Color Imager is 8 times per day."]
[7.596651077270508, 7.759787559509277, "The Spectral Calibration of the SUCHI Instrument is On orbit using atmospheric absorption features."]
[6.227211952209473, 2.9542911052703857, "The Developer of the Carruthers Geocorona Observatory Spacecraft is Ball Aerospace."]
[9.479263305664062, 8.920058250427246, "The Separation of the OB Optical Bench is About 40 cm."]
[9.100521087646484, 10.256800651550293, "The C3D2 Camera Images of the AlSat Nano Satellite is 105 image files downloaded in total so far, including 16 full size images."]
[4.799562454223633, 4.516022682189941, "The Purpose of the Inter-satellite Links Communication System is Routinely cross-check their performance and reduce their dependency on the availability of ground installations."]
[12.060707092285156, 3.281106948852539, "The Orbit Inclination of the CanX-6/NTS Satellite is 97.83\u00ba."]
[4.478952884674072, 5.171840190887451, "The BDH Subsystem of the ResourceSat-2 Satellite is Baseband Data Handling."]
[1.767263412475586, 4.163374900817871, "The Hydropower of the Glen Canyon Dam Dam is Electricity to about 5 million people in seven states."]
[10.260574340820312, 4.523309230804443, "The Maneuvers Performance of the Advanced Composition Explorer Spacecraft is Periodically underperform by as much as 50% in 2014."]
[9.664706230163574, 1.4812638759613037, "The Revisit Time of the Landsat-9 Satellite is 16 days."]
[9.607926368713379, 7.8119096755981445, "The Energy Range for Electrons of the Spectrometer Instrument is 250 keV to 4 MeV."]
[9.37917709350586, 8.132603645324707, "The Detector Thickness of the RAMIS Radiation Detector is 300 \u00b5m."]
[12.047035217285156, 3.2787904739379883, "The Inclination of the DSX spacecraft Satellite is 43\u00ba."]
[6.4761576652526855, 3.4001054763793945, "The Provider of the Megha Tropiques Satellite is CNES and ISRO."]
[8.153655052185059, 0.3274126350879669, "The End of Life Date of the ISS-RapidScat Instrument is 19 Aug 2016."]
[7.530796051025391, 8.578503608703613, "The SNR in SO of the ELVIS Spectrometer is >1000."]
[6.030652046203613, 9.635173797607422, "The Mass of the LEID Instrument is 3.1 kg."]
[8.47358512878418, 1.919863224029541, "The Operation Period of the Herschel Space Telescope is 2009 until 2013."]
[7.301072120666504, 2.288499116897583, "The Launch Date of the Carbon Mapper Satellite is April 2021."]
[3.8070785999298096, 5.551766872406006, "The Data Downlink of the BRITE spacecraft Satellite is up to 256 kbit/s."]
[7.626025676727295, 7.673894882202148, "The Objective of the LIMS Limb Infrared Monitor is Measurement of vertical gas concentrations and temperature profiles in the stratosphere."]
[5.724309921264648, 4.666074752807617, "The Application of the Argos DCS Satellite System is Environmental monitoring, Wildlife monitoring, Oceanography, Climatology."]
[7.300798416137695, -0.7257859706878662, "The Validation Data Source of the CYGNSS Satellite is GPS dropsondes."]
[5.069372653961182, 2.293997049331665, "The Number of Science Instruments of the IMAP Satellite is 10."]
[9.565898895263672, 0.5224088430404663, "The Design Life of the GOMS-1 Satellite is 3 years."]
[7.302881240844727, 8.879210472106934, "The Angular Resolution of the Scanning geometry Instrument is 1.2 +0.2 mrad."]
[7.455542087554932, 0.05373242869973183, "The Launch Date of the SAOCOM-1B Satellite is August 2020."]
[3.239619016647339, 5.318808078765869, "The On-board SSRs Compact Flash Cards of the Telemetry Data Recovery is Successful."]
[5.155115604400635, 5.948122024536133, "The Tracking Frequencies of the GPS/MET GPS Receiver is L1 and L2."]
[6.5442891120910645, 8.15293025970459, "The Derived Parameters of the MiniRad Microwave Radiometer is 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."]
[7.881691932678223, 0.5453360676765442, "The End of Nominal Operations of the Aeolus Satellite is 30 April 2023."]
[4.749751091003418, 2.125518321990967, "The Quantity of the KickSat CubeSat is 1."]
[4.994237899780273, 4.578657627105713, "The Operation of the Monitoring and Control Segment Ground Segment Component is 24/7 monitoring."]
[6.224861145019531, 5.4703369140625, "The Application of the PPT System is SAR application such as interferometry, ATI/GMTI, the fusion of SAR data with AIS data."]
[6.359569072723389, 1.0980448722839355, "The Control Presentation Date of the COSMO-Skymed Satellite Constellation is Oct. 4-8, 2004."]
[6.531012058258057, 3.770068883895874, "The Satellite of the Sentinel-5 Mission is MetOp-SG."]
[9.743444442749023, 6.844484806060791, "The Operational Temperature Range of the Payload Platform Satellite Component is -10\u00b0C to +30\u00b0C."]
[3.4079172611236572, 5.281017303466797, "The On-board Data Storage of the Spacecraft Satellite is 2 GByte."]
[3.285309314727783, 4.83936882019043, "The EEPROM of the Model calculator Data Handling and Processing is 256 kB."]
[-4.981055736541748, 4.407588005065918, "The Proximity GPS Approach of the Mango and Tango Satellites is 2 m in Dec. 2010."]
[9.356616973876953, 3.18959903717041, "The Orbit Insertion of the Periselene-1 Spacecraft is Lunar orbit."]
[6.054516315460205, 4.587141513824463, "The Considered Data of the NOAA Agency is Microwave Sounding Data."]
[4.98090934753418, 4.754894256591797, "The Ground Station Operator of the RF Communications Communication System is TI-Tech."]
[8.550566673278809, 10.164704322814941, "The Number of Megapixels of the HAWAII-2RG 4 Megapixel array Infrared Sensor Array is 4."]
[9.439207077026367, 9.154679298400879, "The Telescope Aperture of the Pan Camera Imaging System is 0.5 m."]
[4.034181594848633, 10.34963321685791, "The NE\u0394T (K) of the ICI-7 Radiometer is 1.4."]
[7.986433506011963, 9.851112365722656, "The Spectral Range of the Imager Imaging System is 450-800 nm."]
[7.550992488861084, 4.7464141845703125, "The Study Topic of the MSI and Proba-V Satellite is Radiation Influence."]
[5.846675872802734, 6.765854358673096, "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."]
[7.662109851837158, 3.0770058631896973, "The Launch of the SEEDS-2 Satellite is Secondary payload to the CartoSat-2A primary spacecraft of ISRO."]
[13.172040939331055, 4.023194313049316, "The Measurement Date of the Gaia Satellite is 3 December 2020."]
[7.0087361335754395, 0.6401342153549194, "The Unveiling Date of the ZACUBE-01 Satellite is Oct. 1, 2011."]
[10.709815979003906, 3.4537858963012695, "The Heliocentric Orbit Distance of the Observatories Satellite is Nearly 1 AU."]
[9.342116355895996, 0.7547564506530762, "The Nominal Lifetime of the TerraSAR-X Satellite is 5.5 years."]
[8.881589889526367, 7.4539361000061035, "The Time Resolution of the Electrostatic Analysers Sensor is Up to 0.5 s."]
[6.0597028732299805, 5.838884353637695, "The Beam Steering of the XSAR SAR Sensor Subsystem is Electronic scanning capabilities in the azimuth and the elevation planes."]
[7.957722187042236, 7.188343524932861, "The Calibration Method of the On Board Calibrator Calibration Device is Flat fielding."]
[7.404038906097412, 3.533378839492798, "The Operation Status of the SPOT-4 Satellite is Nominal."]
[7.144342422485352, 2.6521661281585693, "The URL of the Unknown Satellite is http://www.dso.org.sg/cmsresource/20110309337087956336.pdf."]
[11.028606414794922, 4.105416297912598, "The Website of the Roman Satellite is Interactive."]
[10.456669807434082, 7.7350993156433105, "The Material of the SPEQS Optical Unit is Titanium."]
[3.906341314315796, 4.366507530212402, "The Manufacturer of the OBC On-Board Computer is EADS Astrium SAS."]
[6.825448036193848, 2.0462265014648438, "The Rainfall Totals of the IMERG Rainfall Analysis Tool is Over 8 inches (203 mm)."]
[9.231722831726074, 5.917692184448242, "The Attitude Sensing of the ACS Attitude Control Subsystem is Sun sensors, star sensors and gyroscopes."]
[4.162890434265137, 5.669732093811035, "The Data Delivered of the LRO Satellite is 325 TB."]
[4.012357234954834, 6.757214069366455, "The TRL of the ROIC Read-Out Integrated Circuit is 7."]
[5.4389448165893555, 2.5760293006896973, "The Department of Defense Users of the Iridium Certus(SM) Broadband Service is True."]
[4.840969085693359, 2.1301441192626953, "The Free Flyers Quantity of the CubeStack Multi CubeSat Adapter is 26."]
[6.345639705657959, 10.040979385375977, "The Mass of the PPL1 and PPL2 Hyperspectral Camera Systems is 5.96 kg."]
[10.34163761138916, 9.34360122680664, "The Flare Class of the IRIS Observatory is M-class."]
[4.040465831756592, 4.963136672973633, "The Redundancy of the TCU Control Unit is Internally redundant."]
[4.149580001831055, 4.347862243652344, "The Function of the Peregrine Electronics Electronics is Provide C&C (Command and Control) of the payload, as well as data handling."]
[8.405157089233398, 9.405771255493164, "The Instrument Type of the OSIRIS Optical, Spectroscopic, and Infrared Remote Imaging System is Imaging System."]
[6.447991371154785, 4.663306713104248, "The Instrument of the Sentinel-1 Satellite is C-band SAR (Synthetic Aperture Radar)."]
[10.55541706085205, 7.486958980560303, "The Coatings of the EIRSAT-1 Satellite is Protective oxide coatings."]
[7.476093292236328, 7.114246845245361, "The Arrival Date of the ECOSTRESS Science Payload is 17 April 2018."]
[4.760653018951416, 1.8398979902267456, "The Maximum Number of Satellites of the Telescope Observation Equipment is Feasible if there are 1,000 satellites."]
[9.279678344726562, 3.186452627182007, "The Orbit Type of the Argos-4 Satellite Instrument is Sun-synchronous orbit."]
[10.143211364746094, 3.4845917224884033, "The Eccentricity of the LAGEOS Satellite is 0.0045."]
[7.373229026794434, 0.9793055057525635, "The Detector Annealing Date of the RHESSI Satellite is Jan. 16, 2008."]
[9.445834159851074, 0.5105687975883484, "The On-Orbit Life of the NigeriaSat-2 Satellite is 5th year."]
[4.441050052642822, 2.99822735786438, "The PRN of the GSAT-0204 Satellite is 22."]
[4.691636562347412, 2.140751361846924, "The Number of Switches of the DLP System Satellite System is 5."]
[11.492480278015137, 5.86305570602417, "The Burst Alert System Response Time of the INTEGRAL High Energy Observatory is Within a record 18 seconds."]
[8.720735549926758, 9.731592178344727, "The Optics Design of the UV WFOV Imager Imaging System is Off-axis three-mirror design."]
[6.06306266784668, 9.6649808883667, "The Instrument Mass of the Instrument Sensor is 25 kg."]
[10.002010345458984, 1.401720404624939, "The Signal Reception Time of the MarCO-B Satellite is 11:31 am."]
[4.93356990814209, 2.1662070751190186, "The Microphone Quantity of the Megastar Satellite is Trio."]
[7.176276206970215, 0.8281152844429016, "The Founding Date of the Timbuktu City is 5th century."]
[7.51304292678833, 1.807790756225586, "The Collision Date of the A-74 iceberg Iceberg is 20 August 2021."]
[7.650050163269043, 4.877221584320068, "The Multi-function component assembly of the BEESAT-1 Satellite is Yes."]
[9.26793098449707, 6.1603827476501465, "The Design and Testing Duration of the Gyro Unit Attitude Control is Three and a half years."]
[6.583563327789307, 4.117528438568115, "The Mission Objective of the OICETS Satellite is Conduct on-orbit demonstrations of high-accuracy pointing, acquisition and tracking technologies."]
[9.625940322875977, 0.15376105904579163, "The Hydrazine Duration of the PARASOL Satellite is > 10 years."]
[11.675100326538086, -1.2012600898742676, "The Total of the Satellite Mass is 500 kg."]
[5.822800159454346, 2.4954140186309814, "The Planned System of the SARah Satellite System is SARah."]
[6.814653396606445, 5.46530294418335, "The Participants of the Soil Moisture Active Passive (SMAP) Mission is Dara Entekhabi, Eni G. Njoku, Peggy E. O'Neill, Kent H. Kellogg, Wade T. Crow, Wendy N. Edelstein, Jared K. Entin, Shawn D. Goodman, Thomas J. Jackson, Joel Johnson, John Kimball, Jeffrey R. Piepmeier, Randal D. Koster, Neil Martin, Kyle C. McDonald, Maht."]
[7.025588035583496, 3.177685022354126, "The Orbit Confirmation of the YES Satellite is Confirmed."]
[6.885728359222412, 0.21657992899417877, "The Article Date of the AstroSat Satellite is February 25, 2013."]
[7.384104251861572, 7.954691410064697, "The Accuracy of the Ozone Measurement Instrument Atmospheric Measurement Device is 15 DU or better."]
[11.075958251953125, 4.413944721221924, "The Actual Speed of the Heliosphere Interstellar Medium is Roughly 7,000 miles per hour slower than previously thought."]
[8.152832984924316, 3.7493698596954346, "The Radiation Effects of the THEMIS (and ARTEMIS) spacecraft Satellite is No permanent effects, occasional resets due to Single Event Upsets."]
[11.852994918823242, 1.0061604976654053, "The Mission Tasks of the Chang'e-5 Lunar Probe is Number of Firsts for China."]
[3.458730697631836, 4.553983211517334, "The Model of the Second FPGA FPGA is Virtex 4."]
[7.925447463989258, 4.483240604400635, "The Nadir resolution of the WorldView-4 Satellite is 31 cm."]
[7.633122444152832, 7.5983967781066895, "The Architecture of the MM Radiometer Sensor is Direct-detection."]
[7.1959147453308105, 5.321744441986084, "The Effect of the CH4 Chemical Compound is Lower summertime CH4."]
[9.393255233764648, 9.971702575683594, "The Functionality of the UrtheCast Website User Interface is Fast-forward, pause, rewind and skip the near-live footage."]
[8.597604751586914, 3.7289206981658936, "The Type of the Astrolabe Rupes Feature is Lobate scarp."]
[9.496053695678711, 7.8433074951171875, "The Energy Range of the TED Particle Detector is 0.05 to 20 keV."]
[10.059215545654297, 4.9883832931518555, "The Propulsion of the EUTELSAT KONNECT Satellite is All-electric."]
[10.28746223449707, 5.261097431182861, "The Xenon Quantity of the XTA Xenon Tank Assembly is 110 kg."]
[8.540796279907227, 8.849478721618652, "The -1 Order Diffraction Angle (677 nm) of the Diffracted Beam Light is 21.3\u00ba."]
[9.549118995666504, 5.535326957702637, "The Attitude Stability of the AOCS Attitude and Orbit Control Subsystem is \u2264 0.01\u00ba/s (3\u03c3)."]
[8.59967041015625, 6.163455963134766, "The Navigation Purposes of the Vision Based Sensors Instrument is Long distance detection and tracking of a moving target (VBS FR), relative position/attitude estimation of a cooperative target (VBS CR)."]
[6.846334457397461, 3.718686580657959, "The Mission of the MANTIS Satellite is Demonstration."]
[5.8654913902282715, 6.788017272949219, "The Antenna Footprint of the SIRAL Radar is 15 km."]
[6.8473076820373535, -0.0005312426947057247, "The Fifth Flight Date of the MEPSI Satellite is 2007."]
[11.275863647460938, 3.049079179763794, "The Composition of the Layered Mounds Geological Formation is Nearly pure water ice."]
[5.903518199920654, 6.023423671722412, "The Redundancy Management Software of the S-193 Radar System is Yes."]
[7.35045862197876, 1.0961766242980957, "The Deployment Date of the Gravity Boom and VLF Antenna Satellite Components is Feb. 4, 2009."]
[9.254729270935059, 9.24337100982666, "The Parallelism of the VPW42 Optical Window is \u22645 arcsec."]
[6.861680507659912, 1.0142813920974731, "The Presentation Date of the ASIM Payload Facility is Sept. 24-28, 2007."]
[7.078422546386719, 2.6092655658721924, "The URL of the ISS-RapidScat Satellite is URL: http://www.nasa.gov/jpl/rapidscat/nasas-new-winds-mission-installed-gathers-first-data/."]
[7.2561774253845215, 1.0766985416412354, "The Regional Service Start Date of the BeiDou-2 Navigation Satellite System Satellite System is Unknown."]
[6.801159381866455, 5.300606727600098, "The Instrument of the SMOS Satellite is Microwave instrument."]
[6.886595249176025, 0.3397246301174164, "The Operation Status of the FY-3B Satellite is Operating in 2016."]
[5.84187650680542, 6.865866184234619, "The Frequency of the CPR Millimeter-Wave Radar is 94GHz."]
[3.300952434539795, 5.293580055236816, "The Capacity of the HSDR High-Speed Data Recorder is 8 GByte."]
[9.25314998626709, 0.8659483790397644, "The Orbit Duration of the SMOS Satellite is Almost 10 years."]
[7.57333517074585, 0.945228636264801, "The Launch Date of the Sentinel-3B Satellite is 25 April 2018."]
[7.414279460906982, 2.493928909301758, "The URL of the Rosetta Satellite is http://www.esa.int/spaceinimages/Images/2014/11/Rosetta_solar_wing."]
[6.903946876525879, 0.5631540417671204, "The Launch Date of the OTB-1 Satellite is 2015."]
[8.217668533325195, 7.177802562713623, "The Responsible Organization of the SPAN (Solar Probe Analyzers) Instrument is UCB/SSL (University of California, Berkeley /Space Sciences Laboratory)."]
[8.437795639038086, 8.195746421813965, "The Manufacturer of the TIRS Sensor is Northrop Grumman."]
[6.636544227600098, 7.771214485168457, "The Turn-On Time of the GEDI Laser Laser System is Not specified."]
[7.114158630371094, 2.7079615592956543, "The URL of the SWOT Satellite Satellite is http://scienceandtechnology.jpl.nasa.gov/newsandevents/newsdetails/?NewsID=3201."]
[4.839118957519531, 1.8615673780441284, "The Public Archive Images of the ICEYE Satellite Operator is Nearly 18,000 images taken between mid-2019 and the present."]
[8.144797325134277, 10.005345344543457, "The Center Wavelength of the MS8 (NIR2) Imager is 908 nm."]
[9.082181930541992, 9.21367359161377, "The Surface Requirements of the Reflector Optic is 60 times more stringent than a photon sieve."]
[11.597963333129883, 2.626108407974243, "The Diameter of the Ryugu asteroid Asteroid is 1-km."]
[7.623302936553955, 7.3603692054748535, "The Data Analysis Lead of the ROMAP Instrument is Philip Heinisch."]
[9.32292366027832, 6.403258800506592, "The Practicality of the Specialized Asset Trackers Tracking Device is Not always the most practical solution."]
[10.851849555969238, 3.4573960304260254, "The Operating Distance from Earth of the Euclid Space Telescope is 1.5 million km."]
[9.84842586517334, 3.9044764041900635, "The Deployment Date of the Drag de-orbit sail De-orbit Device is June 23, 2017."]
[4.4302473068237305, 7.705239295959473, "The Bandwidth of the Channel 8 Sensor is 400 MHz."]
[5.155655384063721, 4.641059875488281, "The Location of the Ground Segment Ground Station is Huntsville AL."]
[7.81533145904541, 9.738197326660156, "The Spectral Bands of the Optical Arrangement Imaging System is 36 bands between 0.4 and 14.5 \u00b5m."]
[9.95569896697998, 5.182158470153809, "The Maneuvers of the ESP Thrusters Maneuvering System is Spin-up (de-spin) maneuver and a normal thrust maneuver."]
[9.087555885314941, 5.020776271820068, "The Stabilization of the Microsatellite Satellite is 3-axis stabilized + passive stabilization of the gravity gradient boom."]
[7.49094295501709, 2.4752750396728516, "The Mission Overview of the Hinode Satellite is June 2007."]
[12.069633483886719, 3.2749135494232178, "The Orbit Inclination of the Electron rocket Launch Vehicle is 85\u00ba."]
[8.021652221679688, 8.773629188537598, "The View Swath of the TIR Instrument Telescope is 68 degrees-wide nadir cross-track swath."]
[8.691213607788086, 1.0141401290893555, "The Start of Operation of the LS-7 Satellite is 2010."]
[4.918422222137451, 3.1748108863830566, "The Architecture of the QSP-1 Satellite is 4-Tray."]
[11.077532768249512, 4.825473785400391, "The Speed of the Solar Wind Phenomenon is Up to 800 km/s."]
[7.796781539916992, 8.62951946258545, "The Instantaneous spectral coverage of the Spectrometer Instrument is 1.06 km/s."]
[8.324650764465332, 9.737001419067383, "The URL of the Medium Energy Neutral Atom (MENA) Imager Imager is http://twins.swri.edu/pubs/MENA.pdf."]
[9.980460166931152, 2.3362677097320557, "The Repeated ground track of the KOMPSAT-3 Satellite is 28days/423revolutions."]
[8.39078140258789, 7.256232261657715, "The Mounting Location of the MIRO Instrument is On the spacecraft payload plane."]
[7.331665992736816, 10.093835830688477, "The Conference Presentation Date of the EnMAP Hyperspectral Imager Imaging Satellite is Sept. 2006."]
[12.017770767211914, 2.261524200439453, "The Flyby Duration of the OSIRIS-REx Spacecraft is 5.9 hours."]
[4.131288051605225, 5.135891437530518, "The Bandwidth of the ODTML Data Collection System is Higher than Argos DCS."]
[10.385025024414062, 5.426158905029297, "The Minimum Impulse Bit of the T3\u00b5PS Micropropulsion System is 30\u00b5Ns."]
[6.605565071105957, 3.913158655166626, "The Payload of the ResourceSat-2 Satellite is LISS-3, LISS-4 and AWiFS."]
[5.179851055145264, 5.048871994018555, "The Possibility of Cross-Tagging of the UFF TLE Data Product is Good."]
[7.099072456359863, -0.06347279250621796, "The End of Life Date of the JPSS-2/NOAA-21 Satellite is 10-11-2029."]
[5.8227033615112305, 8.639689445495605, "The Instrument Power of the MWHS-II Microwave Humidity Sounder is 116 W."]
[8.47321605682373, 3.2147507667541504, "The Function of the Formation Flying Application is Precise baseline determination and orbit control."]
[1.703507661819458, 4.189975738525391, "The Solar Cells Efficiency of the EPS Electric Power Subsystem is 28%."]
[5.80645751953125, 1.9249881505966187, "The Payload of the Atlas V Launch Vehicle is Classified NROL-39 & 12 CubeSats."]
[9.871220588684082, 4.084468364715576, "The Sail Size of the Solar Cruiser Solar Sail Mission is 16 times larger."]
[11.332351684570312, 1.3772010803222656, "The Expected Wake Up Date of the Yutu-2 Rover is 28 April."]
[10.089423179626465, 1.3838119506835938, "The Equatorial Crossing Time of the Orbit Satellite is 12:00 hours."]
[8.811452865600586, 9.14480972290039, "The Focal Length of the Short Wavelength Band Spectrometer is 12.5 cm (f/2.2)."]
[5.802135467529297, 2.9179069995880127, "The Manufacturer of the NigeriaSat-2 Satellite is SSTL (Surrey Satellite Technology Ltd.)."]
[7.951714515686035, 4.701057434082031, "The Resolution of the Spotlight-2B Satellite is 1m."]
[9.15317153930664, 9.260135650634766, "The Ensquared Energy of the Lens Optical Instrument is 50% within 15 x 15 \u00b5m."]
[9.441847801208496, 0.6188505291938782, "The Orbital Decay Prediction of the POPACS Satellite is Three years after launch."]
[11.693483352661133, 4.570148944854736, "The Lifespan of the Red Dwarfs Star Type is Generally do not live long enough for complex life to evolve."]
[7.276642322540283, 3.7106449604034424, "The Role of the CE-4R satellite Satellite is Relay satellite for a rover."]
[7.757400035858154, 1.440605640411377, "The Date of the Severe Rainfall and Flooding in Japan Event is 10 July 2018."]
[10.771769523620605, 3.2438366413116455, "The Distance from Earth of the Voyager 1 Spacecraft is About 5.9 billion km."]
[9.341904640197754, 9.445367813110352, "The Photodetector Pixel Size of the Optical Head Optical Device is 5.2 \u00b5m x 5.2 \u00b5m."]
[8.936927795410156, 7.296228885650635, "The Range of the Sun sensors Sensor is \u00b150\u00ba."]
[9.591240882873535, 5.998509883880615, "The Magnetometer of the ADCS Attitude Determination and Control System is 1."]
[7.214966297149658, 5.5929059982299805, "The Bloom Intensity Change of the Phytoplankton Microorganism is Rose considerably in 48 out of the 71 lakes (68 percent)."]
[9.673345565795898, 1.62546706199646, "The Electric Fields Forecast of the C/NOFS Satellite is Pre-reversal enhancement strength."]
[10.85567569732666, 7.229593753814697, "The Spectral Resolution of the XSM X-Ray Detector is ~ 250 eV at 6 keV."]
[9.154854774475098, 9.583536148071289, "The Lens Configuration of the WISPR Imager is Split into two separate imaging assemblies."]
[7.738329887390137, 2.1821136474609375, "The Parachute Manufacturer of the ExoMars mission Mars Mission is Airborne Systems."]
[9.396333694458008, 0.3377269208431244, "The Exceeded Design Life of the SORCE Satellite is Yes."]
[7.806008815765381, 1.4783976078033447, "The Date of the Asteroid Day Awareness Campaign is 30 June."]
[5.338486194610596, 4.645496845245361, "The Location of the Goonhilly Earth Station Earth Station is UK."]
[11.531776428222656, 3.817450761795044, "The Deposition Time of the Fortescue, Hamersley, and Turee groups Rock Groups is Between 2.7 billion and 2.3 billion years ago."]
[6.539428234100342, 9.154943466186523, "The Size of the SIR-2 Instrument is 260 mm x 171 mm x 143 mm (EO module), 146 mm x 125 mm x 33.5 mm (electronics box)."]
[8.047735214233398, 4.857860088348389, "The Yaw Knowledge of the GFO Satellite is Sun sensors."]
[7.986312389373779, 6.93014669418335, "The Calibration Frequency of the OMPS Sensor is Weekly for working diffuser, Twice annually for reference diffuser."]
[8.85879898071289, 9.22768497467041, "The FOV of the Long Wavelength Band Spectrometer is 8\u00ba x 5'."]
[4.117676258087158, 4.476401329040527, "The Components of the HPS Bus System is OBC (On-Board Computer), TCTM (Telecommand & Telemetry) module, PDU (Power Distribution Unit)."]
[4.743496417999268, 1.7937660217285156, "The Number of Satellites in Constellation of the Satellogic Satellite Company is 34."]
[11.717992782592773, 4.75249719619751, "The Distance from Earth of the The Teacup Quasar is 1.1 billion light years."]
[7.720970153808594, 1.2920690774917603, "The Article Date of the NASA Organization is 23 July 2021."]
[5.301277160644531, 6.907015800476074, "The Incidence Angle of the Antenna Conically-scanning reflector is 40.0\u00ba."]
[5.06057071685791, 4.844361305236816, "The Geographical Coverage of the EARS Data Service is Large."]
[6.014222621917725, 9.625731468200684, "The Mass of the HIA Instrument is 3.0 kg."]
[4.953460693359375, 9.202987670898438, "The Optimal Ground Condition of the SEIS (Seismic Experiment for Interior Structure) Seismometer is Level ground without rocks larger than about 1.5 cm."]
[5.047637939453125, 1.916593313217163, "The Number of Recommendations of the Starliner Spacecraft is 60."]
[8.092852592468262, 2.178683280944824, "The End of Life Date of the Artemis-I Mission is 11 December 2022."]
[7.617094039916992, 9.046283721923828, "The Ground Resolution of the IIM instrument Imaging Spectrometer is 200 m/pixel."]
[10.229987144470215, 6.965810298919678, "The Shielding of the Radiator Thermal Control System is Specially shaped titanium fins."]
[8.08240795135498, 8.863987922668457, "The Field of View Width of the Spectrometer Spectrometer is ~0.0001 radians."]
[6.0024590492248535, 1.5472564697265625, "The Sovereignty of the PAZ and TerraSAR Satellites is Independent."]
[5.317654132843018, 9.612507820129395, "The Head Switch-over Time of the STOs and STAEs Analog Electronic units is 3 s."]
[9.112335205078125, 2.8254849910736084, "The Constellation of the GCOM-W1 Satellite is A-Train."]
[9.473603248596191, -0.695778489112854, "The Purpose of the Delfi-n3Xt Nanosatellite is Space Weather Research and Qualification of Microtechnology."]
[5.551059246063232, 2.1790573596954346, "The Manufacturer of the NRCSD CubeSat Deployer is NanoRacks."]
[4.493192672729492, 6.779191017150879, "The Log Amp Bias of the Signal Processing System is Log Amp termination mode."]
[7.689070701599121, 1.2609119415283203, "The Launch Date of the LADEE Lunar Mission is Fall 2013."]
[9.50642204284668, 4.1009111404418945, "The Attitude Control of the CanX-4&5 Satellite is 0.5\u00ba."]
[7.2291951179504395, 7.580109119415283, "The Manufacturer of the ALTIUS Instrument Satellite Instrument is Optique et Instruments de Pr\u00e9cision (OIP) Sensor Systems."]
[5.081266403198242, 5.203237533569336, "The Default Mode of the TRXU Communication System is Receive mode."]
[4.572882175445557, 6.339388370513916, "The Band of the KaRPDA Antenna is Ka-band."]
[7.810055255889893, 7.772552013397217, "The Measurement Target of the OCO-2 Spectrometer is Gases."]
[7.7953619956970215, 3.2472240924835205, "The Number of Characterized Fragments of the DebriSat project Satellite is Over 13,000."]
[6.87122917175293, 5.336883068084717, "The Data Usage of the SMOS Satellite is All-weather microwave data."]
[8.666717529296875, 10.297505378723145, "The Dark Current of the Instrument CCD Imaging Camera is Can be kept insignificant for normal instrument operating temperatures."]
[8.00507640838623, 9.245518684387207, "The Spectral Resolution (60 keV) of the Detector Instrument is 1.0 keV."]
[4.413057327270508, 5.859618186950684, "The Band of the RF Communications TT&C is S-Band."]
[6.712961673736572, 7.621899604797363, "The Unknown of the LRR Laser Retroreflector is Unknown."]
[7.123736381530762, 8.844773292541504, "The Spatial resolution at nadir of the VIRR Visible and Infrared Radiometer is 1.1 km."]
[5.262613296508789, 1.3645555973052979, "The Orbits Completed of the MaSat-1 CubeSat is 10,000."]
[5.865753173828125, 6.2640790939331055, "The Number of Beams for HR Mode of the COSI SAR Mission is 19."]
[7.979018211364746, 7.853643894195557, "The Constraint of the Instrument Payload is Avoid the sunlight intrusion in the payload CCD."]
[5.161675453186035, 2.061807870864868, "The Experiment Proposals of the OPS-SAT CubeSat is 55."]
[6.09835147857666, 3.070714235305786, "The Development Organizations of the NINA-2 Telescope is INFN (Italian National Institute of Nuclear Physics) of Rome, Italy and MEPhI (Moscow Engineering and Physics Institute)."]
[7.870456695556641, -0.14374029636383057, "The Arrival Year of the Nauka mini-research module Module is 2021."]
[5.5764031410217285, 6.310280799865723, "The Length of the Antenna Satellite Component is 0.5m."]
[1.6112388372421265, 4.927047252655029, "The Power Supply of the RM Radiation Monitor is Single unregulated 28 V supply."]
[6.914567947387695, 3.1552577018737793, "The Payload of the Satellite Spacecraft is Unknown."]
[4.417897701263428, 6.523179531097412, "The Frequency of the Ka-band payload Communication System is 30 GHz (receive) and 20 GHz (transmit)."]
[1.0961740016937256, 4.234703540802002, "The Type of the Batteries Electrical Power Subsystem is Lithium-ion 18650."]
[5.349492073059082, 4.270900249481201, "The Location of the PDAS Data-Acquisition Station is Fucino (Italy)."]
[7.890799522399902, 6.6862263679504395, "The Design Hypothesis of the Geometric Calibration System Calibration System is Change within an orbit can be sufficiently modelled with a 3rd order polynomial against the time since the eclipse\u2019s exit."]
[4.199178695678711, 5.747817039489746, "The X-band Downlink of the Satellite Satellite is 280 Mbit/s."]
[8.359034538269043, 3.8362958431243896, "The Lagrange Point of the SWFO Satellite is Lagrange Point 1."]
[5.291248321533203, 4.412383556365967, "The Ground Stations of the DICE Mission Satellite is NASA Wallops field, Stanford Research International."]
[8.395276069641113, 10.129569053649902, "The Spectral Range of the Current GOES imager Sensor is 3.80-4.00."]
[8.317797660827637, 9.978925704956055, "The Design of the SLIM6 Line Scan Imager Imager is COTS (Commercial Off The Shelf) optics design and a COTS detector."]
[9.214164733886719, 6.347653388977051, "The Configuration of the Star Sensors Autonomous Star Sensors is Hot redundant, cross-strapped."]
[7.904839515686035, 7.44754695892334, "The Components of the GOLF Instrument is Sodium vapor resonance scattering filter, Longitudinal magnetic field."]
[7.158422470092773, 5.211059093475342, "The Additional Information Source of the Remote Sensing Observation Method is Emission of fluorescence from the chlorophyll of assimilating leaves."]
[4.603029251098633, 4.084802150726318, "The Design of the SILEX Communication System is ESA."]
[9.412303924560547, 1.8362735509872437, "The Observation Frequency of the ALOS-4 Satellite is Once every two weeks."]
[7.695666313171387, 1.5896060466766357, "The PFM Delivery Date of the SMOS Satellite is End of 2006."]
[10.239599227905273, 5.622778415679932, "The Current Flow of the Electrodynamic Tether Propulsion and Power Generation Device is Determines if the interaction contributes to drag or to propulsion."]
[9.080615997314453, 8.302390098571777, "The Control Method of the SMA Scan Mechanism Assembly is Close-loop controlled using realtime attitude data supplied by the host spacecraft."]
[10.296632766723633, -0.6822299361228943, "The Rotation Rate of the O/OREOS nanosatellite Satellite is 1 to 2 rpm."]
[11.19705867767334, 4.178226947784424, "The Number of Confirmed Planets of the Kepler spacecraft Spacecraft is 2,650."]
[5.580787658691406, 4.379659175872803, "The Function of the BJ3A1 satellite ground pre-processing system Data Processing System is Receives raw data received by the ground station for processing."]
[9.766125679016113, 1.5935826301574707, "The Imaging Time of the CHORUS Satellite is About 20 minutes earlier each day."]
[6.968125343322754, 0.012451187707483768, "The End of Life Date of the PhoneSat-1 and -2 Satellite is 27 April 2013."]
[9.409546852111816, 11.505254745483398, "The Effective FOV of the Channel 3 Sensor is 42 km x 94 km."]
[8.782946586608887, 5.323025703430176, "The Control Accuracy of the Mango Satellite is Within 0.3 m from the commanded approach."]
[5.9180121421813965, 2.4438023567199707, "The Operation of the Antonov 124 Aircraft is Carry the spacecraft."]
[9.52397632598877, 2.754701852798462, "The Retrieval Altitude of the EURECA Satellite is 476 km."]
[9.272542953491211, 3.2259671688079834, "The Orbit Type of the ALL-STAR-1 Satellite is Near-circular orbit."]
[11.133761405944824, 5.148680210113525, "The Conference Date of the LISA Pathfinder Satellite is Oct. 17-20, 2005."]
[2.641094446182251, -1.4453336000442505, "The Antenna Temperature of the WISPR Imager is ~1800\u00baC."]
[6.8898138999938965, 4.948471546173096, "The Nitrogen Dioxide Concentrations Change of the Copernicus Sentinel-5P Satellite is Beijing: -35%, Chongqing: -45%."]
[9.621252059936523, 5.653620719909668, "The ADCS System of the DeorbitSail Satellite is Second use of CubeSense after STRaND-1."]
[5.257857322692871, 4.598114490509033, "The Location of the Ground Station Ground Station is Villafranca, Spain."]
[7.1528520584106445, 9.209552764892578, "The Resolution of the Interferometric Wide Swath mode (IWS) Operational Mode is 25 m x 80 m."]
[6.213615417480469, 1.9374221563339233, "The Launch Vehicle of the G\u00f6kt\u00fcrk-1 Satellite is Vega VV08."]
[6.6738972663879395, 0.6806393265724182, "The Launch Date of the UWE-1 Satellite is Unknown."]
[10.249874114990234, -0.8984540700912476, "The Nominal Operating Voltage of the GHGSat-D Microsatellite is 12.3 V."]
[7.499324321746826, 1.9156721830368042, "The First 883-GHz Cloud Radiance Map Date of the ICIR IceCube Cloud\u2013Ice Radiometer is June 20, 2017."]
[6.8976359367370605, 0.16299879550933838, "The Altitude Decay Date of the InflateSail Satellite is 3 September 2017."]
[4.184328079223633, 6.493160724639893, "The Telemetry of the CEASE-2 Instrument is 10 byte/min."]
[8.351903915405273, 7.4163498878479, "The Power Consumption of the Space Comb Spectroscopy Setup is Below 30 W."]
[2.26932692527771, 4.440444469451904, "The Orbit Average Power of the Power System Satellite Subsystem is 65 W."]
[7.483541011810303, 8.756793022155762, "The Along-Track Resolution of the Nadir Sensor Wide-Field Telescope Sensor is 50 km at nadir."]
[8.54666805267334, 5.439642906188965, "The Drift Accuracy of the DPU Data Processing Unit is ~ 0.1 arcsec."]
[9.348570823669434, 3.109718084335327, "The Orbit Type of the PhoneSat-2.5 1U CubeSat Satellite is Near-circular orbit."]
[8.577666282653809, 6.949568271636963, "The DC Measurement Uncertainty of the Magnetometer Instrument is 14 nT."]
[9.40488338470459, 8.386148452758789, "The Retroreflector Coating of the Ralph Satellite Component is Reflects only one of the two transmitted laser wavelengths."]
[6.501190662384033, 5.653789043426514, "The Radio Occultation Data Purchase of the NOAA Organization is Expanded on 19 February 2021."]
[3.191788911819458, 5.353090286254883, "The Function of the SSR Solid State Recorder is Data storage and retrieval."]
[8.543414115905762, 9.312512397766113, "The Status of the NIRSpec instrument Instrument is Prepped for Micro-Shutter Array and Focal Plane Assembly replacement."]
[9.063779830932617, 0.7808528542518616, "The Ground-Based Test Duration of the Modern ICs Electronic Components is More than 40 days per mode."]
[9.15473747253418, 9.137018203735352, "The Impact Angle of the WISPR Optics Optical System is 0\u00ba, 45\u00ba, 70\u00ba."]
[6.5525126457214355, -0.5152763724327087, "The Clock 2 Anomaly Date of the QZS-1 Satellite is Dec. 19, 2012."]
[5.953999042510986, 6.759907245635986, "The Spatial Resolution (Elevation) of the Radar Radar is 15 km."]
[11.535569190979004, -1.2994846105575562, "The ALMASat-1 Mass of the ALMASat-1 Satellite is 13.56 kg."]
[5.766056537628174, 3.6133322715759277, "The Operation Status of the Paraguan\u00e1 Refinery Complex Refinery Complex is In limbo."]
[6.763573169708252, 10.149675369262695, "The Primary Use of the Band 9 Spectral Band is Ocean color."]
[10.236329078674316, 3.001218795776367, "The Altitude of the FY-3E Satellite is ~ 800 km."]
[9.792095184326172, 1.5123401880264282, "The Science Phase Duration of the EQUULEUS Satellite is At least 180 days."]
[7.458381652832031, 8.82841968536377, "The Spectral Channel 3 of the Satellite Imaging Satellite is 0.79 - 0.92 \u00b5m."]
[9.272832870483398, 4.142411708831787, "The Size of the ADEOS spacecraft Satellite is 4 m x 4 m x 5 m."]
[5.313025951385498, 10.390735626220703, "The Instrument Type of the ISS:LIS Lightning Imaging Sensor is Lightning sensors."]
[4.483114719390869, 6.643360137939453, "The Components of the LF Receiver Receiver is Laser diodes, collimation lenses, electrical and mechanical hardware, copper heatsink, aluminum-alloy chassis, PCM module."]
[8.808841705322266, 1.4160552024841309, "The Revolutionize View Date of the Van Allen Probes Satellite is Jan. 19, 2016."]
[7.94569730758667, 10.214149475097656, "The Spatial Resolution at 20\u00b0 off-nadir of the WV60 imager Imaging System is 0.55 m."]
[7.355454921722412, 4.257295608520508, "The Camera Position of the PSSCT-2 Satellite is +Z face."]
[6.754151344299316, 1.157370686531067, "The Delivery Date of the BRITE Satellites Satellite is June 2011."]
[10.730619430541992, 10.286128044128418, "The High/Low gain ratio of the PHA Detector is 68 or 40."]
[11.418268203735352, 5.129467010498047, "The Distance from Neutron Star to Companion of the Absorption Signatures Spectral Feature is 0.04% of the distance from the neutron star to the companion."]
[6.966542720794678, 6.351574897766113, "The Objectives of the AATSR Instrument is Continuation of precise measurement of Sea Surface Temperature (SST) started with ATSR-1 and ATSR-2."]
[5.085760116577148, 7.555207252502441, "The Rate of the Data Sensor is 50.6 kbit/s."]
[5.304759979248047, 1.3729772567749023, "The Mission Count of the NanoRacks Satellite Deployment System is 17."]
[11.894476890563965, -1.1664849519729614, "The Launch Mass of the QuikTOMS spacecraft Satellite is 166 kg."]
[8.879505157470703, 7.289815425872803, "The Error (RMS) of the Sun sensor Sensor is <0.2\u00ba."]
[7.600124359130859, 1.7736077308654785, "The Conference Presentation of the Near Earth Asteroid Scout Satellite is 2019 IEEE Aerospace Conference."]
[4.325685024261475, 6.23399543762207, "The Uplink Frequency of the Communication Communication System is S-band."]
[9.52975845336914, 0.46027982234954834, "The Design Life of the VEN\u00b5S Satellite is 4 and a half years."]
[8.784423828125, 5.186906814575195, "The Pointing Stability of the MTG-S Spacecraft Satellite is Over 10 s."]
[10.216293334960938, 1.0398097038269043, "The LTDN of the SkySat-16 to -18 Satellite is 10:30 hours."]
[8.940335273742676, 8.036362648010254, "The Designer of the BGO Calorimeter Detector is Prof. AN Qi from USTC."]
[9.654176712036133, 8.45101547241211, "The Thermal Gradients of the Etalon Etalon is Unknown."]
[6.381920337677002, 3.337162494659424, "The Subsystems of the TRISHNA Satellite is French Space Agency (CNES)."]
[8.211913108825684, 10.312819480895996, "The Spectral Band of the Band Cameras Camera is 650-740 nm."]
[6.557159900665283, 0.9229702353477478, "The Launch Date of the OPAL CubeSat is Not provided."]
[5.118968963623047, 7.528065204620361, "The Data Rate of the Instrument Spectrometer is 1.27 Mbit/s."]
[7.696854114532471, 7.948874473571777, "The Detector Type of the CERES Instrument is Thermistor bolometers."]
[7.807570934295654, 9.426860809326172, "The Number of Spectral Bands of the ALI Telescope is 10."]
[8.962437629699707, 7.173712253570557, "The Quantity of the Horizon sensor Sensor is 1."]
[7.876033782958984, 2.032982587814331, "The Study of the ISEE-1/2 spacecraft Spacecraft is An unusual flux transfer event."]
[7.9286274909973145, 5.131418704986572, "The ICRA Requirement of the MTG-I Satellite is Inter-Channel Co-registration Accuracy."]
[8.537718772888184, 2.2985260486602783, "The Affiliation of the Eugene Parker Astrophysicist is University of Chicago."]
[5.01971960067749, 4.751766681671143, "The Ground Segment Component of the Delfi-C3 Satellite is Radio amateur network."]
[9.655208587646484, 0.49739697575569153, "The Design Life of the FY-3 series spacecraft Satellite is 3 years."]
[6.8221306800842285, 4.096343040466309, "The Purpose of the APSS-1 Satellite is Monitor electrical activity in Earth\u2019s upper atmosphere to test whether ionospheric disturbances can predict earthquakes."]
[4.926955699920654, 2.02372670173645, "The Microchip Quantity of the InSight Satellite is 2."]
[10.335105895996094, 9.50284481048584, "The Components of the IRIS spacecraft Satellite is 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."]
[8.428267478942871, 8.00261402130127, "The Additional Lateral Displacement for the Fourth Exposure of the Euclid Reference Survey Survey is 50 arcsec."]
[7.666746139526367, 2.8143444061279297, "The Plasma Particle Data Analysis of the Reimei Satellite is URL:\u00a0 https://web.archive.org/web/20161222025705/http://www.iugonet.org/meetings/2010-02-25/05_Reimei_EISA_Hirahara_20100225.pdf."]
[9.104324340820312, 1.3436295986175537, "The Data Stream Availability of the Sentinel-6 Satellite is A couple of days after collection."]
[6.640175819396973, 2.268326759338379, "The Deputy Project Scientist for Applications of the GPM Satellite is Dalia Kirschbaum."]
[2.143336534500122, 3.810014247894287, "The Type of the Solar panel release mechanism Deployment System is New implementation method."]
[5.869571685791016, 6.768163681030273, "The Integration Distance of the Radar Instrument is 10 km."]
[4.014159202575684, 4.385450839996338, "The Capability of the Payload OBC On-Board Computer is Support of payloads with FPGA computing capability."]
[11.204866409301758, 2.872771739959717, "The Diameter of the Crater Surface Feature is 11 km."]
[9.003274917602539, 4.738059043884277, "The Orbit Control of the MEV-1 Satellite is Controlled the orbit of the customer satellite."]
[4.8412580490112305, 1.9016828536987305, "The Number of Prisms of the LAGEOS Satellite is 426."]
[8.573141098022461, 6.62294864654541, "The | of the Absolute Scalar Magnetometer Magnetometer is Magnetic Cleanliness and thermomagnetic effect: Case staudy of the Absolute Scalar Magnetometer and its environment on Swarm satellites."]
[7.29250431060791, 5.463099002838135, "The December 2015 Value of the CO2 Concentration Atmospheric Parameter is 400.2 ppm."]
[7.2391791343688965, 0.15571919083595276, "The Projected Growth of the Arctic vessel traffic Maritime Traffic is 250 percent by 2025."]
[8.943055152893066, 2.768052339553833, "The Partners of the Kepler Mission is 6."]
[6.622833251953125, 3.6677663326263428, "The Mission Type of the Sentinel-5P Satellite is EO."]
[6.87375545501709, 0.8091116547584534, "The De-orbit Date of the GFO Satellite is End of 2008."]
[6.2022600173950195, 0.5391477346420288, "The Launch Date of the SeaHawk-1 CubeSat is 3 December 2018."]
[9.546426773071289, 0.6599822044372559, "The Orbit Lifetime of the NRCSD Payload is 8-12 months."]
[6.179046630859375, 3.714569091796875, "The Orbit Maintenance of the JERS-1 Satellite is TACC."]
[9.4274320602417, 8.89317512512207, "The Field of View of the Telescope Optical Instrument is Below 75 \u00b5rad."]
[9.729530334472656, 8.028066635131836, "The Detectable Minimum Energy of the Gamma-ray Counter Detector is < 30 keV."]
[9.080410957336426, 4.824619293212891, "The S/C Pointing of the Spacecraft Bus (Avionics Module=AM) Satellite is 1.0\u00ba, 1.0\u00ba."]
[8.028979301452637, 8.543478012084961, "The Disperser Type of the Instrument Spectrometer is Prism."]
[6.182533264160156, 8.504749298095703, "The Data Rate of the MIS Instrument Microwave Radiometer is 500 kbit/s."]
[7.756595611572266, -0.4950709939002991, "The Launch Time of the SpaceX CRS-19 Mission is 17:29:24 UTC."]
[4.328583717346191, 5.2041144371032715, "The Performance Characteristics of the Small Optical Transponder (SOTA) Optical Transponder is Unknown."]
[4.369874477386475, 4.396423816680908, "The Functionalities of the PMS System is Catalog data generation, product generation status control and monitoring, standard product generation."]
[4.612234592437744, 0.3467445373535156, "The Satellite Bus of the EarthDaily Constellation Satellite Constellation is Modified OneWeb satellite buses."]
[9.136897087097168, 4.139317512512207, "The Side Panels Surface Area of the UniSat-5 Satellite is 50 cm x 50 cm."]
[6.586338043212891, 4.185887336730957, "The Data Access of the Sentinel-1 Satellite is Full and open access."]
[10.65709400177002, -1.5686079263687134, "The Weight of the Cargo Dragon Spacecraft is 6,553 pounds (2,972 kg)."]
[9.345155715942383, -0.6333019137382507, "The URL of the TechnoSat Nanosatellite is http://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=2986&context=smallsat."]
[4.528703689575195, 5.89860200881958, "The Purpose of the Alinco UHF Transceiver Transceiver is Monitor the spacecraft beacon messages."]
[10.359050750732422, 5.120635986328125, "The Firing Direction of the Micronozzle Propulsion System is +Y."]
[8.066788673400879, 9.99026107788086, "The Minimum Lower Band Edge of the Pan (WorldView-1) Imager is 400 nm."]
[11.757185935974121, 3.262294054031372, "The Side to Side of the S-193 Ground Coverage is 48\u00ba."]
[7.288181304931641, 9.473350524902344, "The Spectral Ranges of the MSU-E Multispectral Scanner is 0.5 - 0.7 \u00b5m, 0.7 - 0.8 \u00b5m, and 0.8 - 1.0 \u00b5m."]
[7.021718502044678, 2.8677101135253906, "The Circuitry of the SWEM Satellite is Standard designs used extensively in previous missions."]
[8.129554748535156, 1.682679295539856, "The Study Date of the Small Sun Structures Space Phenomenon is 19 January 2021."]
[4.992974758148193, 2.139806032180786, "The Mission Payloads of the HORYU-4 Satellite is Multiple."]
[7.663999080657959, 4.1800856590271, "The Observation of the ALOS/PALSAR Satellite is Magnitude-6.5 Earthquake in Southeastern Iran, 2010."]
[8.330763816833496, 9.723682403564453, "The Wavelength Interval of the PAN Imaging System is 0.50 - 0.85 \u00b5m."]
[6.843139171600342, 5.454831600189209, "The Application of the SMAP Satellite is Flood potential forecasting, drought monitoring."]
[11.532155990600586, 4.47419548034668, "The Maximum Distance of Galaxies of the Euclid Space Telescope is Up to 10 billion light years away."]
[7.804459571838379, 9.438407897949219, "The Imaging Bands of the EOS-T Instrument is Five bands, one panchromatic as well as four multispectral."]
[3.141861915588379, 4.406842231750488, "The Mass of the PCU Power Control Unit is Low."]
[8.960986137390137, 2.4874651432037354, "The Emission Band of the Herschel Telescope is Far-infrared (at 100 \u00b5m)."]
[5.70319938659668, 2.0396528244018555, "The Team of the LightSail-2 Solar Sailing CubeSat is Planetary Society-led team."]
[9.14210319519043, 5.36726188659668, "The Attitude Hardware of the BRITE satellites Satellite is Reaction wheels and star trackers."]
[8.345141410827637, 9.191073417663574, "The Spectra of the SP Spectrograph is Dual-line (Fe i 630.25 nm and Fe i 630.15 nm)."]
[7.625720977783203, 6.4611005783081055, "The Required Precision of the Cloud Top Pressure Satellite Instrument is 100."]
[8.440452575683594, 7.695003032684326, "The URL of the ICARE Radiation Monitor is http://wwwe.onecert.fr/craterre/radiation_monitors/ICARE.html."]
[7.7213873863220215, 8.303053855895996, "The Frequency Range of the VLF Experiment Scientific Experiment is 3-30 kHz."]
[12.09214973449707, 3.297848701477051, "The Inclination of the SCD-2 Satellite is 25.0o."]
[11.668889045715332, -1.1338239908218384, "The Mass of the M1S/M2S Satellite is ~1000 kg."]
[7.022800922393799, 3.6253952980041504, "The Purpose of the Muninn Satellite is Expand the geographical regions that we are testing in, and also test more advanced user scenarios on the ground with multiple satellites in view."]
[10.257838249206543, 5.600703716278076, "The Type of the Tethered System Space Propulsion System is Momentum-exchange."]
[8.526406288146973, 10.694295883178711, "The Power of the PPL1 and PPL2 Hyperspectral Camera Systems is 30 W peak power."]
[6.734288692474365, 3.9428882598876953, "The Ground Segment Chain of the Deimos-2 Satellite is Flight operations chain."]
[6.49667501449585, -0.6921971440315247, "The Supporting GPS/GLONASS Multi-Constellation Augmentation of the QZSS L1-SAIF System is ITM 2013 (International Technical Meeting) of The Institute of Navigation, San Diego, Ca, USA, January 28-30, 2013."]
[6.167481899261475, 3.2536661624908447, "The Regional Hubs of the SERVIR Program is CATHALAC in Panama, RCMRD in Nairobi, ICIMOD in Kathmandu."]
[6.733851432800293, 1.0642263889312744, "The 3D-HDTV Broadcasting and Broadband VSAT Communication Trial Services of the COMS Satellite is Summer of 2011."]
[3.5217268466949463, 4.5469889640808105, "The Computational Units of the Electrical System System is Distributed processors and FPGAs."]
[6.301152229309082, 4.118206024169922, "The Location of the Hertz Chamber Test Chamber is ESA's ESTEC technical heart in the Netherlands."]
[7.869727611541748, 5.706045627593994, "The Image Acquisition Frequency of the AutoNav Autonomous Navigation System is About once per week."]
[3.838730573654175, 4.567435264587402, "The Role Assignment of the OBDH OnBoard Data Handling is Assigned to a specific OBDH-board."]
[11.346314430236816, 3.908250331878662, "The Orbit Period of the AU Mic b Planet is 8.5 days."]
[5.0500311851501465, 6.803397178649902, "The Antenna Gain (dB) of the Antenna Reflector is 29.3."]
[11.225549697875977, 2.8549108505249023, "The Maximum Distance from Crater Center of the Disturbed Areas Geological Feature is Up to 15 m."]
[5.378149509429932, 2.1240458488464355, "The Number of Processors of the EnMAP Satellite is 4."]
[6.019218444824219, 8.125073432922363, "The Bandwidth of the Radiometers Instrument is 3 kHz."]
[11.769128799438477, 1.6831618547439575, "The Flight Above the Surface of the Philae Lander is More than an hour."]
[7.8286261558532715, 4.540604591369629, "The Detector Line Array of the SLIM6 Satellite is 10,000 silicon element cells in cross-track."]
[8.402581214904785, 1.5775341987609863, "The Hibernation Duration of the Rosetta Satellite is 2010-2014."]
[7.908364772796631, 8.727033615112305, "The Field of View of the SBUV Spectrometer is 0.20 rad."]
[6.821142196655273, 4.269470691680908, "The Benefits of the Mission Satellite Mission is Ecological forecast, water quality, air quality."]
[4.871687412261963, 7.017297267913818, "The Scintillation Data Frequencies of the CITRIS Receiver is VHF, UHF, and at L-band frequencies."]
[6.047025680541992, 4.038468837738037, "The Operator of the Odin Satellite is OHB Sweden, on behalf of the Swedish National Space Agency (SNSA) and the Swedish Space Corporation (SSC)."]
[10.734183311462402, 10.302727699279785, "The Chip size of the PHA Detector is 7.4 mm x 7.4 mm."]
[9.345673561096191, 5.807769775390625, "The Components of the ACS Attitude Control Subsystem is 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)."]
[7.052336692810059, 0.5471286773681641, "The End of Operations of the Resurs-P2 Satellite is 2018."]
[8.112088203430176, 1.4669255018234253, "The Publication Date of the Solar Mass Ejection Imager Imager is Jan. 22, 2002."]
[5.952667713165283, 6.3724212646484375, "The Swath Width of the SAR Synthetic Aperture Radar is Larger than 40 km."]
[8.067222595214844, 8.848811149597168, "The Minimum Value of the Spectral Angle Measurement is Achieved when the blue panel is prominent."]
[5.904650688171387, 1.4902688264846802, "The Launch Vehicle of the MSG-3 Satellite is Ariane-5 ECA."]
[9.624783515930176, 6.032890796661377, "The Control Algorithms Implementation of the Coarse ADCS ADCS System is Nanomind OBC."]
[7.3290534019470215, 0.34408512711524963, "The Launch Date of the Dauria Aerospace and Samsung Satellite is Oct. 15, 2013."]
[9.410642623901367, -0.5561918020248413, "The Communication Frequencies of the Nanosatellite Satellite is UHF, VHF."]
[17.727998733520508, 7.162730693817139, "The J2000 right ascension (deg) of the B0531+21 (Crab) Pulsar is 83.63303."]
[6.654284954071045, 0.5522732138633728, "The Launch Date of the NorSat-1 Satellite is July 2017."]
[9.132389068603516, 9.310210227966309, "The Field of View of the FOV Satellite is 0.08\u00ba along track and 1.42\u00ba cross track."]
[10.71496295928955, -1.5669869184494019, "The Pressurized Cargo Bay Mass of the Dragon Resupply Vehicle Resupply Vehicle is 1530 kg."]
[9.051349639892578, 9.910368919372559, "The Shutter Requirement of the AgCam/ISSAC Imaging System is US Laboratory Window external shutter to be open."]
[4.9386467933654785, 4.641463756561279, "The Function of the MC3 Ground Station is Signal for assistance if a ground engineer was needed to resolve a problem."]
[7.224992275238037, 1.634286642074585, "The Symposium Date of the Air Force Academy Department of Physics Space Technologies Development and Research Research Project is May 19-22, 2014."]
[10.055870056152344, 1.395711064338684, "The Period of the WorldView-3 Satellite is 97 minutes."]
[10.152078628540039, 3.5570712089538574, "The Eccentricity of the Satellite Spacecraft is 0.8."]
[8.406694412231445, 10.076435089111328, "The Spectral Range of the Current GOES imager Sensor is 6.75-7.15."]
[8.34633731842041, 7.532957553863525, "The Name of the CERN Radiation Testing Facility is VESPER (Very energetic Electron facility for Space Planetary Exploration missions in harsh Radiative environments)."]
[7.972058296203613, 1.408085584640503, "The Article Date of the Tooley Crater Lunar Crater is 26 January 2021."]
[8.882892608642578, 3.2581639289855957, "The Orbit Type of the LEO Satellites Satellite is Low Earth Orbit (LEO)."]
[9.520326614379883, 8.73160171508789, "The Primary Mirror Type of the Shafer Telescope Optical System is Scanning mirror."]
[5.147027969360352, 4.546239376068115, "The Location of the Monitoring and Control Segment Ground Segment Component is Troms\u00f8, Norway."]
[9.37855052947998, 8.877477645874023, "The Field of View of the Telescope Optical Instrument is 0.5\u00ba x 0.5\u00ba."]
[9.134393692016602, 0.7948105335235596, "The Experiment Duration of the SIOS Optical Link Demonstration Board Technology Demonstration Board is 3-5 years."]
[4.681087493896484, 6.340525150299072, "The Antenna (Gr/T) of the Unit Communication System is -17.4."]
[7.183927059173584, 2.617476463317871, "The URL of the H. Kuninaka Individual is http://www.nasa-usa.de/pdf/604314main_6-GER_WS_JAXA-RoboticPrecursor-Kuninaka.pdf."]
[11.590484619140625, 4.390857219696045, "The Difference in Radius of the Kepler 11145123 Star is 3 km."]
[7.622461795806885, 6.412747383117676, "The Measurement Range of the Cloud Fraction Satellite Instrument is 0-1."]
[5.173152923583984, 6.101534843444824, "The Sampling Rate of the TRSR GPS Receiver is 10 Hz."]
[8.569384574890137, 1.9385621547698975, "The Views of Star Formation Date of the Herschel and Planck Telescopes is 5 July 2020."]
[9.885526657104492, 4.005676746368408, "The Launch Site of the NanoSail-D Satellite is Omelek Island in the Kwajalein Atoll."]
[7.653614521026611, 9.09323501586914, "The Spectral Passband of the Miniature High-Resolution Imaging Spectrometer Imaging Spectrometer is 1600-1700 nm."]
[7.769880294799805, 2.325061798095703, "The Publisher of the Observation of the Earth and Its Environment: Survey of Missions and Sensors Documentation is Springer Verlag."]
[5.926524639129639, 8.609475135803223, "The IFOV/line (pixels/scan line) of the MWTS Microwave Temperature Sounder is 15."]
[6.445127964019775, 3.9403722286224365, "The Data Location of the JERS-1 Satellite is ESA Earth Online website and the OpenSearch Datasets on NASA Earthdata website."]
[10.703361511230469, 3.416874885559082, "The Perihelion Radius of the Solar Orbiter Satellite is < 0.25 AU and > 0.20 AU."]
[9.531208038330078, 0.5100244879722595, "The Design Life of the Satellite Satellite is Ten years."]
[5.2339606285095215, 3.0738937854766846, "The Signal Processing System of the NorSat-3 Satellite is Zynq Ultrascale+ system-on-chip."]
[7.463861465454102, 4.213303565979004, "The Instruments of the CryoSat Satellite is DORIS-NG, Laser Reflectors (ESA), SIRAL."]
[7.145500659942627, 0.41471901535987854, "The Launch Date of the Intercosmos- Bulgaria 1300 (Intercosmos-22) Satellite is 07.08.1981."]
[10.153742790222168, 5.083837032318115, "The Quantity of the Thrusters Attitude Control is 24."]
[9.118569374084473, 5.1357035636901855, "The Stabilization of the JAWSAT Satellite is Three-axis."]
[7.67746639251709, 2.3206381797790527, "The URL of the Radiation Belt Storm Probes Satellite is http://rbsp.jhuapl.edu/index.php."]
[7.069467544555664, 1.5011606216430664, "The Conference Presentation Date of the THEMIS Satellite is Aug. 14-17, 2006."]
[9.557939529418945, 3.999103307723999, "The Intersatellite Communication System of the CanX-4&5 Satellite is Must relay position, velocity and attitude information."]
[8.70353889465332, 6.949234485626221, "The Type of the Fluxgate Sensors Sensor is Ring core-types."]
[11.057483673095703, 6.451473236083984, "The Navigation Method of the Interplanetary spacecraft Spacecraft is Pulsars."]
[10.684645652770996, 5.266666889190674, "The Total \u0394V of the CNAPS Propulsion System is 12 m/s."]
[9.83290958404541, 7.8373212814331055, "The Energy Measurement Range for Electrons of the Telescope 1 Solid-State Telescope is >0.15, 0.35, 0.75 MeV."]
[10.458089828491211, -0.9813740849494934, "The Mass of the AIST-2 Microsatellite is 39 kg."]
[7.9225921630859375, 1.4117076396942139, "The Test Schedule of the Orion Spacecraft Spacecraft is Accelerated."]
[8.303563117980957, 7.258821964263916, "The Frequency Range of the Electric Field Measurement System Instrument is 20 Hz - 100 kHz."]
[10.164348602294922, 4.775622844696045, "The Onboard Propulsion of the QuickBird-2 Satellite is 4 x 4.4 N hydrazine thrusters."]
[4.005198001861572, 5.662278652191162, "The Data downlink of the ALOS-3/PRISM-2 Satellite is 800 Mbit/s (X- and Ka-band)."]
[9.399741172790527, 5.809942245483398, "The Pointing Performance of the ACS Attitude Control Subsystem is \u2264 150 arcsec."]
[11.705609321594238, -1.0711476802825928, "The Payload of the Solar Orbiter Satellite is 180 kg."]
[3.86649227142334, 6.448745250701904, "The Number of Digital Delays of the TTDL Component is 5."]
[6.439018249511719, 4.957968711853027, "The Instrument Type of the GF-3 Satellite is Imaging microwave radars."]
[11.517305374145508, -1.2159936428070068, "The Mass of the Jugnu Satellite is ~ 3 kg."]
[1.8810629844665527, 4.017467021942139, "The Quantity of the Solar Panels Power Subsystem is 4."]
[9.64867115020752, 4.226870536804199, "The Diameter at Launch of the Genesis-2 Spacecraft is 1.9 m."]
[7.648510456085205, 7.155673980712891, "The Measurement Category of the TEMPO Satellite is Ozone, Trace gases (excluding ozone)."]
[7.040615558624268, 0.5084528923034668, "The Launch Timeframe of the Aditya-L1 Satellite is 2019 \u2013 2020."]
[9.842264175415039, 4.435826778411865, "The Examples of the Passive Deorbiting Devices Deorbiting Devices is Tethers and drag sails."]
[11.848909378051758, 1.0202341079711914, "The Discovery Date of the Chang'e-4 Lunar Probe is 21 July 2020."]
[3.865355968475342, 4.509928226470947, "The Microprocessor of the Beresheet lander Lander is LEON3 cores."]
[9.233306884765625, 10.323517799377441, "The Focal Length of the LWIR Cameras Camera is 13.5 mm."]
[6.671996593475342, 4.734683036804199, "The Imaging Frequency Band of the COSMO-SkyMed Satellite is X."]
[5.674896240234375, 1.9557805061340332, "The Fairing Manufacturer of the Ariane 5 Launch Vehicle is RUAG Space."]
[10.52425479888916, 3.205707550048828, "The Distance to EML-2 of the Queqiao Communication Satellite is 60-80,000 km."]
[9.354310035705566, 8.648995399475098, "The Design of the Rotating Telescope Scanner Optical Instrument is 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."]
[8.203289985656738, 5.622521877288818, "The Leading Noise Terms of the Satellite Spacecraft is Electric disturbances."]
[9.647347450256348, 7.862399101257324, "The Energy Range for Protons of the Spectrometer Instrument is 8 to 120 MeV/(mg/cm2)."]
[7.95488977432251, 6.80159330368042, "The Frequency of the External Calibration Calibration is Two events every two weeks."]
[6.594930648803711, 1.1864045858383179, "The Brochure Date of the GOCE Satellite is June 2006."]
[7.581536769866943, 2.4573440551757812, "The Design Factors of the ELSA-d Mission is Mission safety, market leadership, engagement in discussions for doctrine, standards, and regulation, interface with legal structures."]
[7.886752128601074, 10.246139526367188, "The Imagery Geolocation Accuracy with GPCs of the WV60 imager Imaging System is 2 m."]
[3.9074745178222656, 4.499938011169434, "The Image Credit of the CU Control Unit is GWU, USNA."]
[5.841695308685303, 6.729604244232178, "The Swath Width of the X-band Radar is 450 km."]
[7.7368597984313965, 9.514151573181152, "The Bands of the Spectral Bands Sensor is 2."]
[5.2232184410095215, 6.499979496002197, "The Material of the Sprite\u2019s antenna Antenna is Nitinol."]
[3.2576186656951904, 5.849123001098633, "The Data Collection Period of the CPT Data Processing System is Fixed period of time."]
[8.71192741394043, 7.785771369934082, "The Event Identification of the CZTI Instrument is Compton scattering criteria."]
[9.606565475463867, 3.933687686920166, "The Drag Sails of the CanX-7 Satellite is Four."]
[7.6689229011535645, 4.684459686279297, "The Contribution of the LARES Satellite is Laser Relativity Satellite."]
[5.696013927459717, 4.061618804931641, "The Data Retrieval Location of the FOS Satellite is Ground stations."]
[9.214118003845215, 2.622326135635376, "The Impact Date of the DART Spacecraft is 2022."]
[5.564236164093018, 1.7805567979812622, "The Conference Location of the PnP Cube Satellite CubeSat is Big Sky, Montana, USA."]
[8.37843132019043, 9.266867637634277, "The Spectral Sampling of the LR Bands (500\u2013697 nm) Spectral Bands is Equal to the slit with (84 \u00b5 )."]
[9.15838623046875, 4.21213960647583, "The Dimensions of the Spacecraft bus Satellite is 2.0 m x 1.8 m x 3.7 m."]
[5.306560039520264, 4.134119033813477, "The Storage Location of the Processed science data Data is DAAC located at GSFC."]
[7.080573558807373, 4.327986717224121, "The Measurement Domain of the ST5 Satellite is Atmosphere, Gravity and Magnetic Fields."]
[5.86014461517334, 9.200794219970703, "The Power of the LISS-IIM Instrument is 34 W."]
[8.491067886352539, 10.277107238769531, "The Number of CCDs of the Focal Plane Array Detector Array is 36."]
[7.77031135559082, 3.967550754547119, "The GPS Data Collection Location of the ICESat-2 Satellite is 88 degrees south."]
[7.102189540863037, 4.805838108062744, "The Purpose of the GOSAT-GW Satellite is Monitor greenhouse gases in the atmosphere and improve understanding of the water cycle."]
[6.824858665466309, 7.797230243682861, "The Data Collection of the ECOSTRESS ECOsystem Spaceborne Thermal Radiometer is Morning data for the summer season."]
[9.057782173156738, 3.2391457557678223, "The Orbit Type of the LAGEOS Satellite is MEO (Mean Earth Orbit)."]
[2.204474687576294, 4.333999156951904, "The Power of the DubaiSat-2 Satellite is 100 W."]
[7.240026473999023, 6.029553413391113, "The Effect Size of the Aerosol Direct Radiative Effect Atmospheric Phenomenon is Unknown."]
[7.462484359741211, 0.5312261581420898, "The Launch Date of the ESAIL Satellite is 12 June 2020."]
[4.889745235443115, 1.9076271057128906, "The Number of Satellites Waiting to be Launched of the GHGSat Company is Two."]
[11.838034629821777, 1.0199594497680664, "The Unknown of the Chang'E-1 Lunar Probe is Unknown."]
[11.235377311706543, 2.861138105392456, "The Displacement Resolution of the Boulders Geological Feature is ~1 cm."]
[5.986741065979004, 6.227896213531494, "The Daily Scenes of the System SAR is More than 30."]
[11.731588363647461, -1.014892578125, "The Mass of the STP-H5 Payload Package is Unknown."]
[6.766311168670654, 6.103912353515625, "The Sustained Surface Winds of the RapidScat Scatterometer is 46.9 mph (21 meters per second/75.6 kph)."]
[8.113736152648926, 2.2767882347106934, "The Operational Phase Start Date of the Himawari-8 Geostationary Satellite is 7 July 2015."]
[7.80092716217041, 7.329862117767334, "The Calibration Equipment of the Monochromator Instrument is \u201cYokogawa AQ6376\u201d."]
[8.274239540100098, 3.6142585277557373, "The Project and Mission Overview of the GOSAT Satellite is Not provided."]
[9.513694763183594, -2.5284998416900635, "The Power of the LEICA Particle Detector is 4.9 W."]
[9.403877258300781, 1.7772302627563477, "The Pass Frequency of the Satellite Orbit Type is Three to five times per day."]
[10.815152168273926, 1.9750303030014038, "The Altitude of the Swarm-B Satellite is Circa 516 km."]
[8.12210750579834, -0.6997851729393005, "The Attachment Duration of the Cargo Dragon Spacecraft is About one month."]
[4.451535224914551, 2.9997339248657227, "The PRN of the GSAT-0101 Satellite is 11."]
[11.628483772277832, 6.077738285064697, "The Typical Short Outburst Duration of the X-ray Source Celestial Object is Unknown."]
[7.268152236938477, 4.938648700714111, "The Purpose of the RAIDS Instrumentation is Acquire a global database of airglow intensities."]
[9.985509872436523, 1.58018159866333, "The Operation Mode of the ASAR Sensor is High-rate mode for up to 30 minutes per orbit, including 10 minutes in the eclipse phase."]
[7.012115478515625, 1.698215365409851, "The Conference Presentation Date of the Radio Aurora Explorer Satellite is Aug. 8-11, 2011."]
[8.648921966552734, 5.8161773681640625, "The Temperature of the Proton Component Measurement Range of the DSCOVR Satellite is 40,000 \u2013 2,000,000 Kelvin."]
[3.265716791152954, 5.0700764656066895, "The Memory of the Transceivers Communication Device is 2 Mbit."]
[10.576135635375977, 8.509953498840332, "The Entrance Aperture Diameter of the COR2 Coronagraph2 Imager is 30.5 mm."]
[9.704840660095215, 8.668001174926758, "The Contracting Company of the PP Twin Telescopes Telescope is SENER."]
[8.289655685424805, 9.728443145751953, "The On-board Processing Procedures of the Optical Payload Imaging System is Radiometric correction, Inter-channel co-registration, Geo-referencing, Background classification, Hotspot detection, Consolidation of hot pixels, Extraction of attributes of hot clusters."]
[10.434017181396484, -1.0127971172332764, "The Payload Mass of the GHGSat-D Microsatellite is 9 kg."]
[8.77808666229248, 6.531191825866699, "The Composition of the Ionosphere Atmospheric Layer is Electrically charged gases or plasma."]
[9.123990058898926, 5.161348819732666, "The Attitude Stabilization of the Spacecraft Satellite is 3-axis stabilized."]
[8.212964057922363, 7.626965045928955, "The Target of the Cal_doppler Observation Instrument is Sun."]
[6.022594451904297, 3.288619041442871, "The Contributions of the NASA Agency is SIR-C hardware, the Shuttle launch, ground systems, mission operations and data processing support."]
[8.338303565979004, 3.389004707336426, "The Deployment Status of the InflateSail Satellite is Not Deployed."]
[7.233778476715088, 9.517159461975098, "The Operation of the MSS Multispectral Scanner is Opto-mechanical scanning instrument (whiskbroom technique, unidirectional operation)."]
[7.870545864105225, 5.845367431640625, "The Phases of the In-orbit Calibration and Validation Satellite Process is Two."]
[6.002402305603027, 5.458832263946533, "The Data Link Subsystem of the XSAR SAR Sensor Subsystem is DLS."]
[7.820981979370117, 10.82049560546875, "The Data Quantization of the VIS Visible region of spectrum is 12 bit."]
[9.798230171203613, 4.662709712982178, "The Tank Length of the Launcher Test Facility is 283.5 m."]
[7.925581455230713, 4.485810279846191, "The Vertical Resolution of the Tomorrow-R1 and -R2 Satellite is 250 m."]
[5.487375736236572, 3.5758936405181885, "The Use of Commercial off the Shelve subsystems or subsystems composed of automotive grade parts of the Development Approach Satellite Instrument Development is Sometimes a choice is made to implement Commercial off the Shelve subsystems or subsystems composed of automotive grade parts, rather than state-of-the-art dedicated space applications."]
[9.347214698791504, 11.60067081451416, "The Pixel size of the Channel 1 Sensor is 32 km x 32 km."]
[8.534629821777344, 10.55977725982666, "The Spectral Bands of the CCD Camera Imaging System is 0.62 - 0.68 \u00b5m, 0.77 - 0.86 \u00b5m, 1.55 - 1.69 \u00b5m."]
[9.459997177124023, 3.853404998779297, "The ADCS Suite of the CanX-4 or CanX-5 Satellite is Tray Housing."]
[4.7510504722595215, 2.0158743858337402, "The Number of Maneuvers of the SkySat-5 Satellite is 5."]
[3.588176727294922, 2.2901010513305664, "The Margin of the EV-9 Satellite is 3 dB."]
[10.341141700744629, 3.7328693866729736, "The High-Gain Dish Diameter of the TGO Trace Gas Orbiter is 2.2 m."]
[9.737845420837402, 1.6136209964752197, "The Earth Mapping Cycle of the OCO-2 Satellite is 32 days."]
[8.817676544189453, 8.749682426452637, "The Material of the HiRAIS Optical Instrument is Zerodur."]
[9.398194313049316, 5.756437301635742, "The Processor of the ACS Attitude Control Subsystem is Dedicated."]
[1.208417534828186, 4.167575836181641, "The Battery Type of the S/C Satellite is Lithium-iodine."]
[8.650691986083984, 8.117196083068848, "The Sensor Type of the MuREM Dosimeter is Dose rate sensitive photodiode."]
[3.274320363998413, 4.930345058441162, "The EEPROM of the OBDH Data Handling and Processing is 128 kB."]
[8.13529109954834, 2.0440263748168945, "The Mission Status of the Herschel Satellite is Ongoing."]
[9.969175338745117, 7.8056159019470215, "The Energy Resolution of the HXD Detector is \u2264 10% at 59.5 keV."]
[7.618389129638672, 5.417692184448242, "The Spatial Variations in XCO2 of the OCO-2 Satellite is <2%."]
[7.133553504943848, 0.3611598312854767, "The End-of-life Date of the SPOT-4 Satellite is June 29th, 2013."]
[7.393505096435547, 3.576767921447754, "The Magnetic Onboard Recorders of the SPOT-4 Satellite is Operational."]
[10.341404914855957, 2.83014178276062, "The Orbit Altitude of the Alba Cluster 3 Satellite Cluster is 500 to 600 km."]
[9.297337532043457, 9.038064002990723, "The Focal Length of the Instrument Satellite Instrument is 72.5 mm."]
[2.0501554012298584, 3.858027219772339, "The Type of the Solar Arrays Power System is Surface-mounted."]
[6.611565113067627, 3.6981194019317627, "The Function of the EON-IR Satellite is Earth Observation Nanosatellite -Infrared."]
[12.114142417907715, 3.2795472145080566, "The Inclination of the Tandem-L Satellite is 98.4\u00ba."]
[9.011398315429688, 7.173539161682129, "The Type of the Sun sensors Sensor is 2 axis slit & photo cell."]
[8.301743507385254, 7.2888407707214355, "The Channels of the Electric Field Measurement System Instrument is 16."]
[10.922249794006348, 3.375420093536377, "The Distance from Sun of the New Horizons Spacecraft is Unknown."]
[1.955098032951355, 3.9586727619171143, "The Body-mounted solar cells of the CLAVIS Power Generation is True."]
[1.4525748491287231, 4.971010684967041, "The Battery Voltage of the SBVR Power Supply is 55 to 96 V."]
[9.477561950683594, 0.11269555240869522, "The Operation Duration of the CanX-7 Nanosatellite is Approximately six months."]
[7.300840854644775, 9.376968383789062, "The 185 km x 185 km of the RBV Instrument Image Size is Image of 185 km x 185 km."]
[6.063498497009277, 3.313321352005005, "The Instrument Provider of the SPARCS Satellite is NASA's Jet Propulsion Laboratory."]
[10.129572868347168, 7.73139762878418, "The Function of the Baffle Telescope Component is Thermal."]
[8.176026344299316, 8.454767227172852, "The Configuration of the Michelson Interferometer Interferometer is Flat-mirror Michelson."]
[3.7703161239624023, 4.513210773468018, "The Processor of the OBC On-Board Computer is ERC-32 processor of ATMEL."]
[5.919538497924805, -0.27652615308761597, "The Model Validation of the Oculus-ASR Satellite is Successful."]
[4.581369400024414, 3.116117477416992, "The External Panels of the GNB Satellite Platform is 6."]
[5.454554080963135, 1.3002971410751343, "The Landing Attempt of the Falcon 9 first stage Rocket is Mostly successful."]
[8.052428245544434, 4.104517459869385, "The Freshwater Release of the A-68A Iceberg is 152 billion (152 x 10^9) tonnes."]
[7.098834037780762, 3.148387908935547, "The Mission Operation Concept of the VEN\u00b5S Satellite is Unknown."]
[7.219914436340332, 0.5936421155929565, "The Communication Restoration Date of the LightSail Satellite is May 31, 2015."]
[1.0792118310928345, 4.184344291687012, "The Number of Cells of the Battery Energy Storage is 24."]
[8.77330207824707, 5.171682834625244, "The Pointing Restrictions of the CHIPSat Satellite is Sun, Earth, moon and in the orbital RAM direction."]
[6.07547664642334, 4.5761494636535645, "The Signal Augmentation of the MTSAT Satellite is GPS wide-area signal augmentation."]
[9.600319862365723, 7.77114725112915, "The Count Rate of the EPD-E Energetic Particle Detector - Electrons is 10,000 to 50,000 counts/s."]
[9.26848030090332, 10.148077011108398, "The Purpose of the Low-Resolution Video Camera Camera is Spot the general location of interest."]
[7.627842426300049, 3.365825653076172, "The Tracking Support of the Debris Satellite Components is Joint Force Space Component Command."]
[7.417029857635498, 5.846916675567627, "The Altitude of the Noctilucent Clouds Atmospheric Phenomenon is 50 miles (80 km)."]
[7.128422737121582, 0.42298412322998047, "The Launch Date of the SwissCube Satellite is 2009."]
[7.339800834655762, 2.266188144683838, "The Symbolism of the Emirates Mars Mission Mission is Named as a symbol of hope for all Arab youth."]
[8.040367126464844, 8.892300605773926, "The Pixel Exposure Time of the Instrument Spectrometer is 2.0, 4.1, 8.2 ms (VIS); 6.6, 13.2, 26.4 ms (NIR)."]
[10.353260040283203, 2.777418613433838, "The Altitude Range of the LEMUR-2 constellation Satellite Constellation is 400-600 km."]
[5.7097392082214355, 4.151385307312012, "The Critical Activities of the Spacecraft Satellite is Performed in contact with the ground."]
[8.234543800354004, 1.5688152313232422, "The Observation Period of the SoloHI Heliospheric Imager is 17-19 December."]
[7.890661716461182, 10.758916854858398, "The Data Quantization of the Imager Imaging System is 11 bit."]
[7.699051380157471, 4.0252861976623535, "The Daily Acquisition Capacity of the SPOT-6 Satellite is 3 million km2."]
[11.058144569396973, 4.163722991943359, "The Influence on Exoplanets of the Stars Celestial Bodies is Can influence the climates and habitability of a star\u2019s hosted exoplanets."]
[6.0436625480651855, 4.644770622253418, "The Imaging Capability of the NovaSAR-1 Satellite is SAR and AIS (Automatic Identification System) data."]
[5.275544166564941, 4.784675598144531, "The Location of the TT&C Station Ground Station is Kiruna, Sweden."]
[6.872775077819824, 2.5558037757873535, "The URL of the BioSentinel Satellite is http://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=3453&context=smallsat."]
[7.723180294036865, 7.890421390533447, "The URL of the Solar Backscatter Ultraviolet/Total Ozone Mapping Spectrometer (SBUV/TOMS) Spectrometer is http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1978-098A-09."]
[10.220335006713867, 3.016035318374634, "The Altitude of the Tatiana-2 Satellite is 825 km."]
[7.4229416847229, 0.22827140986919403, "The Travel Date of the Smile Satellite is 16 March 2022."]
[12.953889846801758, 4.858404159545898, "The Observed Atoms of the IBEX Spacecraft is Hydrogen, oxygen, neon and helium."]
[6.403806209564209, 0.6458187103271484, "The Launch Date of the GHGSat-D Satellite is June 22, 2016."]
[9.030526161193848, 4.7827019691467285, "The Off-nadir Angle of the ICESat Satellite is 0.3\u00ba."]
[7.037970066070557, -0.011115656234323978, "The End of Life Date of the IMAGE Satellite is 18 December 2005."]
[7.86167049407959, 8.829427719116211, "The Spectral Resolution of the OVIRS Spectrometer is R>2,000."]
[9.326692581176758, 7.713826656341553, "The Inner Temperature of the Dewar Component is ~ 256.6 K."]
[6.7298760414123535, 4.497139930725098, "The Land Measurements of the Copernicus Sentinel-3 Satellite is Maps land, provides indices of vegetation state and measures the height of rivers and lakes."]
[10.133663177490234, 3.0324981212615967, "The Altitude of the SPOT-1, -2 and -3 Satellites is 832 km."]
[11.198698997497559, 4.225456714630127, "The Number of Candidate Planets of the Kepler Space Telescope Space Telescope is More than 4,000."]
[4.222336769104004, 4.889359474182129, "The Presentation Date of the Agile data downlink solutions Data Communication System is June 4-8, 2012."]
[4.953439712524414, 6.168708801269531, "The Frequency (MHz) of the Galileo E1-B/C Signal Carrier is 1575.42."]
[7.24729061126709, 2.5931897163391113, "The Nickname of the SpriteSat Satellite is Rising."]
[9.774506568908691, 10.043195724487305, "The Technology Development Start Year of the MOMS Optical Camera is 1979."]
[8.468120574951172, 8.021036148071289, "The Deep Survey Coverage of the Euclid Reference Survey Survey is ~40 deg2."]
[4.848818302154541, 9.11083984375, "The Detection Capability of the InSight Seismic Experiment for Interior Structure (SEIS) is Marsquakes every day."]
[11.75936222076416, 1.1732287406921387, "The Terrain Camera (TCAM) of the Chang\u2019e-4 Lander Lander is Payload."]
[3.9008991718292236, 5.675015926361084, "The Data Transmission Speed of the OceanSat-2 Satellite is 4 kbit/s."]
[9.179615020751953, 5.420691013336182, "The Attitude Control of the Payload Satellite Payload is Star Tracker, Gyroscopes & Control Moment Gyros."]
[9.477728843688965, 9.055706977844238, "The Aperture of the Telescope Assembly Optical Instrument is 45 cm."]
[9.943923950195312, 1.476711392402649, "The Global UTC Time Dissemination of the Galileo Satellite Navigation System is Within 30 billionths of a second."]
[9.389842987060547, 7.899649143218994, "The Cooling System of the Focal Plane Assembly Sensor Component is Active cooling subsystem."]
[10.164176940917969, 6.7394890785217285, "The Radiator Function of the BepiColombo Spacecraft is Reflect heat directionally."]
[5.241666793823242, 6.0421671867370605, "The ECCM Configurations of the Complete Solution Antenna Configuration is SPAN 5, SPAN 4 through digital beamforming, SPAN 2b, SPAN 3b+3, STRX."]
[7.972429275512695, 9.565991401672363, "The Wavelength of the FAI Auroral Imager is Near infrared (650-1100 nm)."]
[6.216797828674316, 4.051969528198242, "The Testing Purpose of the Flying Laptop Satellite is New technologies and scientific Earth observation."]
[8.619040489196777, 0.15519684553146362, "The Crew Capacity of the OWS Space Station is 3-person."]
[10.370434761047363, 2.899193525314331, "The Altitude Range of the Cluster Satellite Constellation is 25 000 km to 125 000 km."]
[3.929527759552002, 6.027218818664551, "The Components of the Uplink Optical Communication System is Slow tip/tilt mirror, dichroic mirror."]
[6.218997478485107, 0.494153767824173, "The Launch Date of the 3U CubeSat Satellite is 23rd June 2017."]
[3.930171489715576, 6.282948970794678, "The Bandwidth of the RF Ground Network Ground Network is Up to ten times the UHF radio."]
[4.486231327056885, 3.652665853500366, "The Features of the AIS Automatic Identification System is Simultaneous reception and decoding of any two channels in the maritime VHF band, as well as a software-defined radio architecture."]
[7.009300708770752, 5.2488112449646, "The Parameter Representation of the GEOS Model Weather and Climate Model is Mathematical equations that represent physical processes."]
[7.591127872467041, 2.3367607593536377, "The URL of the Terrestrial Imaging Spectroscopy Missions Missions is doi:10.1109/IGARSS.2013.6723584."]
[8.009803771972656, 8.85960865020752, "The Vertical Resolution of the Limb Sensor Sensor is 2.2 km."]
[7.846858501434326, 7.479339122772217, "The Calibration Aim of the SODISM Solar Imaging Instrument is Provide long term sensitivity calibration."]
[3.6210293769836426, 6.200441837310791, "The Downlink Speed of the ColKa Communication Device is Up to 50 Mbit/s."]
[7.940829277038574, 1.4178199768066406, "The Announcement Date of the NASA Mission Asteroid Mining is August 8, 2013."]
[5.90250301361084, 1.547208309173584, "The Conference Presentation Date of the GOMX-1 Satellite is May 26-30, 2014."]
[4.587070941925049, 6.721406936645508, "The Frequency of the X-band phased array antenna Antenna is 8125 MHz."]
[7.378335475921631, 0.31935274600982666, "The Launch Date of the FORUM Mission is 2026."]
[5.791079044342041, 1.6938451528549194, "The Product Assurance/Quality Assurance Standards of the GomX-4 Satellite is ESA on nanosatellite missions."]
[4.332616806030273, 5.956375598907471, "The S-band antenna of the TT&C Tracking, Telemetry, and Command is 1."]
[5.816389560699463, 6.856968879699707, "The Impulse Duration of the X-band Radar is 3 \u00b5s."]
[11.565991401672363, 6.2970380783081055, "The Cataloged X-ray Sources of the XMM-Newton X-ray Satellite is 71,951."]
[9.90369701385498, -0.6400493383407593, "The Apogee Altitude of the IDEA-OSG 1 Microsatellite is 800 km."]
[7.46116828918457, 1.2369136810302734, "The NLC Observation Start Date of the AIM spacecraft Satellite is May 13, 2013."]
[3.26170015335083, 5.632653713226318, "The Size of the Raw Science Data Packet Data Packet is 280 bytes."]
[9.992159843444824, 3.1590750217437744, "The Orbit Distance from Earth of the SWFO-L1 Satellite is Approximately 1.5 million kilometers."]
[7.6935248374938965, 0.875093936920166, "The Information Kit Date of the OasISS Space Module is May 2009."]
[3.411663770675659, 4.73606538772583, "The Bus Speed of the RAD750 SBC Single Board Computer is 66 MHz."]
[9.238972663879395, 0.7427178621292114, "The Current Policy of the Meteosat Satellites Geostationary Satellites is 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."]
[9.777705192565918, -0.9673076868057251, "The Number of Satellites of the JL-1-GF03B Microsatellite is 6."]
[10.463528633117676, -1.1395732164382935, "The Weight of the Venta-1 Nanosatellite is ~5 kg."]
[9.529899597167969, 0.5156409740447998, "The Design Life of the Spacecraft Satellite is 7 years."]
[7.250946998596191, 0.6866467595100403, "The Launch Date of the IMAGE Satellite is 25 March 2000."]
[3.347864866256714, 5.273103713989258, "The SSDR Capacity of the SLIM6 Satellite is 1.5 GB."]
[7.619248867034912, 9.158781051635742, "The Function of the ND Neutral Density Filter is Adjust the transmission of each spectral channel."]
[4.463482856750488, 4.27085018157959, "The Function of the Interface Modules Software Layer is Interface to the hardware components and the ONS module."]
[4.760146141052246, 4.280150413513184, "The Role of the MiWarS Device is Backup."]
[10.582347869873047, 8.518424034118652, "The FPA of the COR1 Coronagraph1 imager is 1024 x 1024 (2k x 2k array summed 2 x 2)."]
[4.637444019317627, 0.20005320012569427, "The Number of Gateway Stations of the OneWeb Satellite Constellation is Unknown."]
[5.9662861824035645, 2.988018751144409, "The Market of the EarthSTAR Inc. Company is People's Republic of China, including Hong Kong and Macao."]
[5.132082939147949, 6.449461936950684, "The Type of the Sprite\u2019s antenna Antenna is Half-wave V-dipole."]
[9.680012702941895, 2.1024341583251953, "The Trail Time from Aqua of the CloudSat Satellite is \u2264 120 s."]
[3.348350763320923, 6.682138442993164, "The RF Output Power of the VHF COTS transmitter Transmitter is 22 dBm."]
[8.40604019165039, 3.222930908203125, "The Science Phase of the TanDEM-X Satellite is Three consecutive periods of different formation geometries."]
[8.45059871673584, 7.98492956161499, "The Number of Instruments of the ISIM Instrument Module is 4."]
[7.145157814025879, 1.4929819107055664, "The Symposium Date of the WatER Satellite Mission is March 13-16, 2006."]
[5.276736259460449, 6.786876201629639, "The Beamwidth of the Onboard Antenna Antenna is 20\u00ba."]
[6.232700347900391, 5.114811420440674, "The Band of the TerraSAR-X SAR Satellite is X-band."]
[8.921126365661621, 10.786824226379395, "The Spatial Resolution of the WFC CCD Camera is 1 km."]
[9.29262924194336, 6.410897731781006, "The Object Detection Threshold of the Star Tracker Attitude Determination Device is Visual (or apparent) magnitude Mv 11."]
[6.959686279296875, 0.47642186284065247, "The Launch Date of the Odin Satellite is February 2001."]
[6.244340896606445, 6.340097904205322, "The Measurement Interval of the Copernicus Sentinel-6 Poseidon-4 Radar Altimeter is Every 10 days."]
[8.472713470458984, 8.699589729309082, "The Grating Order of the Spectrometer Instrument is 2."]
[3.9275662899017334, 6.365661144256592, "The Modulation Scheme of the High-speed link Radio Link is GFSK (Gaussian Frequency Shift Keying)."]
[5.242470741271973, 6.08870792388916, "The Placement of the Patch Antennas Antennas is On opposite side of the spacecraft."]
[5.851865768432617, 4.060917377471924, "The Responsibilities of the ITF Instrument Test Facility is Instrument builds and tests, building a repository of engineering information."]
[7.93039083480835, 6.7905778884887695, "The On Orbit Star Calibration of the Instrument Spectrometer is Once per week."]
[9.085494041442871, 8.357157707214355, "The Prototype of the L1 Detector Detector is Photograph."]
[5.4972968101501465, 7.492821216583252, "The Transmit Power of the KaRIN Instrument is ~1.5 kW."]
[11.73735237121582, 1.1642076969146729, "The Operation Status of the Chang'e-3 Moon Lander is Devices still work well."]
[6.85029935836792, 2.3475441932678223, "The URL of the Chinese satellite Satellite is http://www.spaceflightinsider.com/."]
[4.507091999053955, 2.252735137939453, "The Number of Deorbited Prototypes of the Starlink Communication Satellite is 2."]
[9.439835548400879, 1.852482795715332, "The Imaging Frequency of the Dove Satellites Satellite is Once a day for the entire planet, up to 10 times a day for a particular location."]
[10.60082721710205, 9.28635311126709, "The Image Resolution of the CaSSIS camera Camera is Unknown."]
[7.69102668762207, 1.2045586109161377, "The First Image Transmission Date of the LADEE Satellite is Feb. 13, 2014."]
[6.425364971160889, 0.9788277745246887, "The Vibration Test Completion Date of the Quantum Satellite is 2 March 2020."]
[6.754961013793945, 2.08359432220459, "The Brochure URL of the Global Precipitation Measurement (GPM) Satellite is http://www.nasa.gov/sites/default/files/files/GPM_Mission_Brochure.pdf."]
[3.247269868850708, 4.194644927978516, "The Switched Lines for MTCU of the MRU Main Regulator Unit is 1 x 2."]
[9.040549278259277, 10.453364372253418, "The Calibration Status of the HRC (High-Resolution Camera) Camera is Ongoing."]
[12.108548164367676, 3.282562494277954, "The Inclination of the DMC-3 Constellation Satellite Constellation is 97.8\u00ba."]
[10.907423973083496, 3.4006333351135254, "The Depth of Spectrometer Measurements of the Galileo probe Space Probe is About 75 miles (120 kilometers)."]
[6.264374732971191, 1.8538352251052856, "The Operation of the ADS-B Surveillance Technology is Aircraft determines its position via satellite navigation and periodically broadcasts it."]
[4.523750305175781, 5.601736068725586, "The Data Downlink of the Payload Satellite Payload is X-band."]
[8.923815727233887, 10.325356483459473, "The f/No of the CMOS Camera Camera is 2.8."]
[10.27436637878418, 6.848342418670654, "The Heater Systems of the TCS Thermal Control Subsystem is HM and HS."]
[11.55948543548584, 6.266786575317383, "The Anniversary of the X-ray Astronomy Field of Study is 50th anniversary in June 2012."]
[9.386463165283203, 0.9303168654441833, "The Contract Period of the ELSA-d Mission is 12 months."]
[6.528949737548828, 2.892947196960449, "The Promoter of the SOHLA-1 Satellite is NEDO."]
[8.086333274841309, 1.0141959190368652, "The Image Acquisition Date of the Landsat-8 Satellite is May 21, 2022."]
[1.8561924695968628, 4.857115745544434, "The Power Dissipation of the IEC ISIM Electronics Compartment is 200 W."]
[11.493722915649414, 6.561715602874756, "The Number of Observations per Year of the 3XMM Catalogue X-ray Source Catalogue is 600-700."]
[5.679567813873291, 9.172274589538574, "The Power Consumption of the CEASE-2 Instrument is 1.7 W."]
[8.969676971435547, 5.179944038391113, "The Design Tolerance of the D3 D-Orbit Decommissioning Device is The alignment of the motor with the spacecraft's center of gravity resulted to be outside the designed tolerance."]
[7.640347003936768, 9.08951473236084, "The Resolving Power of the Spectrometer Instrument is R = 100."]
[5.756554126739502, 6.5355072021484375, "The Signal Wavelength of the L-band SAR Radar is Around 10 inches (25 cm)."]
[7.2435221672058105, -0.37445199489593506, "The Launch Date of the Starlink Communication Satellite is March 18, 2020."]
[7.724445819854736, 3.8103020191192627, "The Area of the Vatnaj\u00f6kull Glacier Glacier is 8400 km2."]
[10.648104667663574, 9.259089469909668, "The Image Location of the CaSSIS Imaging System is Melas Chasma."]
[7.819453239440918, 8.468523025512695, "The IR Spectral Range / Bandwidth of the SOLSPEC-ATLAS Spectrometer is 800-2400/20./4."]
[1.9574642181396484, 4.172186374664307, "The Power of the Solar Panels Power Generation is About 230 W."]
[7.0600905418396, 0.4859968423843384, "The Launch Status of the DirecTV 15 Satellite is To be launched in a few weeks."]
[8.110268592834473, 9.954597473144531, "The Video Capability of the MWIR Imager Imaging Device is Yes."]
[5.1205549240112305, 6.586098670959473, "The Characteristic Impedance of the Sprite\u2019s antenna Antenna is 50 ohm."]
[9.580163955688477, 5.877752780914307, "The Pointing Angle of the ADACS Attitude Determination and Control Subsystem is 21.5\u00ba below the orbital normal."]
[9.276103019714355, 1.8858027458190918, "The Crosses the Equator of the JPSS-1/NOAA-20 Satellite is About 14 times daily."]
[9.320600509643555, 0.7868857383728027, "The Duration of the Nimbus Earth Radiation Budget (ERB) Experiment Satellite Experiment is 1975 to 1992."]
[10.187493324279785, 4.953057765960693, "The Propulsion Subsystem of the Spacecraft Satellite is > 10 mN of thrust, > 1000 s of I sp, 3 kg of Xenon."]
[11.567864418029785, -0.8065549731254578, "The Fuel of the IRS-1A Satellite is Hydrazine."]
[7.588222503662109, 8.551911354064941, "The SNR in Nadir of the ELVIS Spectrometer is >500."]
[8.383167266845703, 8.274197578430176, "The Effective Area at 40 nm of the EUV Simulation Simulation is 28 cm2."]
[7.80197286605835, 9.633021354675293, "The Usage of the Spectral Imager Instrument is Not used."]
[9.445967674255371, 9.170150756835938, "The Telescope Aperture of the Pan Camera Imaging System is 0.7 m."]
[9.396415710449219, 8.708860397338867, "The Surface of the Flight Mirror Assemblies Optical System is Non-reflective surfaces are procured un-anodized and will be wrapped in polyimide tape for increased emissivity."]
[7.807309627532959, -0.5380343198776245, "The Launch Date of the SpaceX CRS-19 Mission is 5 December 2019."]
[11.248576164245605, 4.1334404945373535, "The Habitability of the Planet Candidate Exoplanet is Uninhabitable by life as we know it on Earth."]
[11.11893367767334, 4.947969913482666, "The Speed Range of the Coronal Mass Ejections Solar Phenomenon is 100 to 3500 km/s."]
[7.046337127685547, 0.02471053972840309, "The End of Life Date of the SWFO-L1 Satellite is 31 December 2029."]
[7.095358848571777, 5.068364143371582, "The Number of Leaks of the Kayrros Studies Methane Leak Detection is Around 100."]
[8.054608345031738, 7.563486576080322, "The Measurement Accuracy - Time of the Instrument Sensor is Tag at frame rate."]
[1.1261098384857178, 4.227271556854248, "The Type of the Energy Storage Power System is NiCd batteries."]
[5.870095729827881, 10.879121780395508, "The No of Passbands of the Channel 5 Sensor is 1."]
[9.074301719665527, 1.2950665950775146, "The Mission Duration of the Van Allen Probes Satellite is 2 years."]
[2.350799083709717, 3.647045373916626, "The Earth Pointing Mode Function of the H3 and H4 Spacecraft is PZ-Surface faces into the nadir direction during observations."]
[9.397632598876953, 0.9641112089157104, "The On-Orbit Duration of the ACE Mission Satellite is 18 years."]
[8.028849601745605, 9.411352157592773, "The Central Wavelength of the AVHRR/3 Sensor is 2.25."]
[9.298929214477539, 6.423610687255859, "The Mounting Angle of the AST Autonomous Star Tracker is 10\u00ba from the spin axis."]
[6.33247184753418, 11.88681697845459, "The Resolution of Accelerometer Measurements of the Three-axis diagonal gradiometer Gradiometer is < 2.0 x 10 -12  m s -2  Hz -1/2."]
[4.996913909912109, -0.1297682374715805, "The Second-Generation Network Launch of the OneWeb Satellite Constellation is 2025."]
[7.227626800537109, 0.4026569128036499, "The Launch Date of the Lunar Pathfinder Comsat Communication Satellite is End of 2023."]
[8.397967338562012, 3.669182538986206, "The Mission Concept of the TanDEM-X Satellite is Not provided."]
[2.262819528579712, 4.4203081130981445, "The Power of the Spacecraft Satellite is 600 W."]
[5.172119140625, 6.18734884262085, "The Deployment Type of the Helical Antenna Antenna is Self-Deploying."]
[9.132613182067871, 2.9335215091705322, "The Orbit Type of the GCOM-W1 Satellite is Sun-synchronous orbit."]
[2.100642204284668, 4.720585346221924, "The Peaks of the Payload Power Power Generation is 180 W."]
[7.054577350616455, 3.004819393157959, "The Responsible Organization of the SWEM (SWEAP Electronics Module) Module is UCB/SSL (University of California, Berkeley /Space Sciences Laboratory)."]
[7.396710395812988, 0.7174602746963501, "The Launch Date of the Explorer 36 Satellite is Jan. 11, 1968."]
[11.431455612182617, -1.2961814403533936, "The Mass of the RISAT-2 Satellite is 300 kg (including a payload mass of 100 kg)."]
[7.6516032218933105, 1.66361665725708, "The Phase B Payload Design Completion of the SMOS Satellite is Oct. 2003."]
[6.763244152069092, 8.555797576904297, "The Size of the Nightingale site Sample Collection Site is The size of a small parking lot."]
[3.8008720874786377, 4.4614763259887695, "The Quantity of the OBC On Board Computer is 3."]
[1.4970629215240479, 4.953489780426025, "The Unregulated Bus Voltage of the Power Subsystem Subsystem is 14 V."]
[8.627949714660645, 6.447022914886475, "The Tip Mass of the Gravity-Gradient Boom Stabilization Device is 3 kg."]
[7.74643087387085, 4.535326957702637, "The Instrument Banks of the SLIM6 Satellite is 2."]
[9.468300819396973, 1.7676438093185425, "The Orbit Frequency of the HyperScout\u00ae Satellite is 15 times a day."]
[7.816570281982422, 10.883125305175781, "The Telemetry Amplitude Digitization of the SXI Spacecraft is 12 bit."]
[4.146327972412109, 5.800567626953125, "The X-band, Downlink Data Rate of the Data Transmission Subsystem Satellite Subsystem is 190 Mbit/s."]
[9.795125961303711, 5.60014009475708, "The Manufacturer of the Lee Solenoid Valve Flow Control Valve is Lee."]
[11.24496841430664, -0.6631011366844177, "The Launch Timeframe of the BA 330 module Space Module is 2012/14."]
[9.241430282592773, 10.1886625289917, "The Manufacturer of the DECA Camera is OIP (Optique et Instruments de Pr\u00e9cision)."]
[10.4048433303833, 7.577627182006836, "The Material of the Boom Assembly Assembly is CFRP (Carbon Fiber Reinforced Plastic)."]
[9.310420036315918, 5.197783946990967, "The Function of the Y-axis aligned reaction wheel Reaction Wheel is Absorb the angular momentum of the spinning satellite."]
[8.058709144592285, 9.953243255615234, "The Output Signal of the Tunneling Infrared Sensor Sensor is 3.0 V signal + 1/400 of the tunneling high voltage + the tunneling signal disturbance."]
[4.743948936462402, 2.348233461380005, "The Data Downlink Volume of the EPICHyper Constellation Satellite Constellation is 20-100 times the downlink volume as a traditional cubesat."]
[11.077986717224121, 2.947706460952759, "The Size Discrepancy of the Impact Basins Lunar Surface Feature is Up to twice the diameter."]
[7.101822853088379, 4.312225818634033, "The Event Probability of the Safe Mode Satellite Mode is Sufficiently low and only possible under very special initial conditions."]
[9.508567810058594, 0.48411670327186584, "The Design Lifetime of the Eutelsat Quantum Satellite is 15 years."]
[9.14234447479248, 10.604942321777344, "The Rotation Time of the M-CAM 1 Monitoring Camera is Less than two minutes."]
[10.008991241455078, 1.5402511358261108, "The Period of the Satellite Orbit Orbit is 9.03 days."]
[5.5133562088012695, 2.8238096237182617, "The Manufacturer of the Prometheus Block 2 CubeSats Satellite is LANL (Los Alamos National Laboratory)."]
[2.618434190750122, 6.2925286293029785, "The Wait Time of the LT Device is 120 seconds."]
[10.08399486541748, 1.5245106220245361, "The Orbital Period of the Shakuntala Satellite is 94.0 minutes."]
[7.774118423461914, 5.959204196929932, "The Detector Readouts of the ASTERIA Satellite is 20 Hz."]
[9.18234634399414, 6.614349365234375, "The Quantity of the Star Trackers AOCS Sensors is 2."]
[8.785085678100586, 3.9539809226989746, "The Latitude and Longitude of the Gulfstream Supersite Experiment Location is 42\u00ba N, 75\u00ba W; 36\u00ba N, 65\u00ba W; 30\u00ba N, 73\u00ba W."]
[9.770371437072754, 1.8763576745986938, "The Integration Time of the EyeSat Satellite is 15 seconds."]
[10.359055519104004, 3.334002733230591, "The Orbital Separation of the Sapphire and NEOSSat Satellites is Approximately 4700 km."]
[9.283940315246582, 10.280306816101074, "The IFOV of the 16 mm camera Camera is 9.2 x 10 -3  degrees."]
[9.9984130859375, 8.478229522705078, "The Co-aligned Telescopes of the ASTRO-1 Satellite Mission is 3."]
[8.794654846191406, 8.878937721252441, "The Band Reflection and Transmission of the Dichroic Filter Optical Filter is 400 to 1,000 nm reflected, 900 to 2,500 nm transmitted."]
[6.200676441192627, 2.117759943008423, "The Imagery Assessment of the TacSat-2 Minisatellite is Useful to the tactical operator."]
[7.286303520202637, 7.05861234664917, "The Calibration Performance of the VIIRS Instrument is Continuously Assessed."]
[10.45713996887207, 2.536468982696533, "The Apogee of the Deimos-1 Satellite is 680 km."]
[4.1795735359191895, 5.668579578399658, "The X-band Downlink Transmission Data Rates of the CBERS-2B Satellite is 2 x 53 Mbit/s."]
[9.622589111328125, 7.726701259613037, "The Electron Energy Range of the SWEPAM Particle Detector is 1 - 1240 eV."]
[7.269623756408691, 7.074793338775635, "The Complementary Data Source of the VIIRS Instrument is AIS and VMS data."]
[8.129412651062012, 5.11371374130249, "The Location Knowledge Accuracy of the GFO Satellite is 10 cm (radial component)."]
[11.457616806030273, 4.366015434265137, "The Composition of the Stardust Grain Particle is Carbon-rich graphite grain with an embedded speck of oxygen-rich material."]
[7.872349739074707, 1.8406918048858643, "The Launch Date of the ExoMars 2020 Mission is July 2020."]
[6.537215709686279, 5.645187854766846, "The Number of Atmospheric Occultations of the GNOS-2 Satellite is Less than 1000 per day."]
[11.373933792114258, 6.674011707305908, "The Instrument System Testing Status of the IXPE observatory X-ray Observatory is Completed."]
[5.936668395996094, 2.7761731147766113, "The Team Members of the Galileo 2nd Generation Satellites Satellite is Thales, Spaceopal, Leonardo and other partners."]
[8.182666778564453, 8.507105827331543, "The Aberrations of the SHS Interferometer is Introduce field of view limitations."]
[9.371554374694824, 4.158537864685059, "The Diameter of the Torus/Strut Structures Satellite Component is 61 cm and 46 cm."]
[11.592297554016113, -1.319102168083191, "The Mass of the FY-1C Satellite is Unknown."]
[7.280533313751221, 10.198629379272461, "The Data Downlink Time from Nanosatellite of the HyperScout 1 Hyperspectral Imager is Several weeks."]
[8.962738037109375, 2.1209144592285156, "The Mission of the New Horizons Space Probe is Explore the Kuiper Belt."]
[8.929559707641602, 10.14647102355957, "The Number of CMOS Cameras of the CubeSense Attitude Determination and Control Subsystem is 2."]
[8.343332290649414, 8.555953025817871, "The Detector of the Spectral Band C Spectrometer is Si-PIN."]
[1.7993680238723755, 5.383443355560303, "The Current of the Voltage 5 Digital is 525."]
[9.403776168823242, 5.011645317077637, "The Spin Axis Orientation of the IMP-8 Spacecraft is Normal to the ecliptic plane within 1\u00ba."]
[4.882744789123535, 6.547266483306885, "The Frequency Band of the Antenna Low-Gain Antenna is 8.025-8.400 GHz."]
[8.590752601623535, 3.149550676345825, "The Purpose of the Queqiao Relay Satellite is Bridge between Earth and the far side of the moon."]
[7.636118412017822, 0.8838356733322144, "The First Earth Imagery Sent Date of the Kanopus-V Satellite is Sept. 3, 2012."]
[6.329510688781738, 2.7766904830932617, "The Missions of the Solar Terrestrial Probes (STP) Program Program is STEREO, MMS, Hinode, TIMED."]
[11.466300010681152, 5.775371551513672, "The Observation Date of the Planck Telescope is Unknown."]
[5.292269706726074, 3.87520170211792, "The Development Lessons Learned of the EDSN Satellite is Unknown."]
[2.1545333862304688, 4.84985876083374, "The Power Range of the Modular Power System Power System is 1W to 1kW."]
[6.517937660217285, 3.1772782802581787, "The Hosting Service of the EUTELSAT 5 West B Satellite is EGNOS."]
[7.910762786865234, 7.176879405975342, "The Objective of the CVE Calibration and Verification Element is Calibration of the COSI payload and maintaining its long-term system performance."]
[10.001996040344238, 1.4594155550003052, "The Off-Nadir Pointing Duration of the MicroSat-70 Satellite is Up to half an orbit."]
[9.744634628295898, 3.6495959758758545, "The Detection Method of the Lunar Meteoroid Impact Flash Detection Detection System is 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."]
[7.49767541885376, 0.9491978883743286, "The Arrival Date of the Messenger Spacecraft is 18 March 2011."]
[8.316095352172852, 1.8539938926696777, "The Launch Year of the Voyager 1 Spacecraft is 1977."]
[8.437535285949707, 1.9651589393615723, "The Launch Date of the Herschel Telescope Telescope is May 14, 2009."]
[11.34334945678711, 6.715837478637695, "The Background Noise Reduction Method of the IXAE X-ray Astronomy Experiment is Mutual anti-coincidence fashion."]
[11.573225021362305, 6.198376655578613, "The Operation Start Date of the NICER X-ray telescope Telescope is June 2017."]
[6.737295627593994, 2.8005354404449463, "The Ground Control Complex Location of the Kolibri-2000 Satellite is Kaluga (Russia)."]
[8.942750930786133, 1.8013298511505127, "The Start of Full-Scale Simulations of the BepiColombo Spacecraft is May 28, 2018."]
[6.008833885192871, 6.364837646484375, "The Polarimetry of the SAR-RCM Synthetic Aperture Radar is Hybrid."]
[8.3236722946167, 2.750001907348633, "The Mission of the JPSS-1 through JPSS-4 Satellites is Provide operational continuity of satellite-based observations and products from NOAA's POES and S-NPP satellites."]
[2.963606834411621, 6.526247978210449, "The Power of the Transponder Communication System is 5 W."]
[6.749438285827637, 3.282989025115967, "The | of the HISDESAT Satellite Operator is HISDESAT: PNOTS operator."]
[6.750359058380127, 4.6628193855285645, "The Observation Objective of the Sentinel-4 Satellite is Observing the diurnal cycle of the tropospheric composition over Europe and North Africa."]
[9.5032377243042, 0.571894109249115, "The Image Quality of the Payload Satellite Payload is Maintained at consistent levels for more than 14 years."]
[10.822961807250977, 7.273629188537598, "The Energy Range of the XSM X-Ray Detector is 1-20 keV."]
[1.2194492816925049, 4.199520111083984, "The Battery Capacity of the S/C Satellite is 920 mAh."]
[9.941512107849121, 6.461724281311035, "The Temperature of the Eureka Station Weather Station is 21.9\u00b0C."]
[7.788876056671143, 9.084124565124512, "The Linearity of the UV/VIS Spectrometer Spectrometer is 0.5%."]
[5.5100579261779785, 4.742127418518066, "The Spatial Acquisition Duration of the Alphasat TDP1 GEO-relay is Reduced from 240 s at the very first tests to 34 s for default links."]
[7.7508544921875, 6.9859724044799805, "The Deployment Location of the ECOSTRESS Instrument is JEM (Japanese Experiment Module) External Facility on the ISS."]
[8.590211868286133, 5.495027542114258, "The Accuracy of the GT Fine-Pointing Error Signal Provider is 0.4 arcsec, 3\u03c3."]
[2.3022103309631348, 4.567957401275635, "The Power Consumption Monitoring of the Propulsion System Satellite Component is Of the total propulsion system, of the CGG igniters and the main valve."]
[7.809744834899902, 9.052359580993652, "The Spectral Range of the TES Spectrometer is 3.2 \u03bcm to 15.4 \u03bcm."]
[6.786318302154541, 1.2500933408737183, "The Conference Presentation Date of the STSat-2 Satellite is March 3-5, 2005."]
[6.419761657714844, 0.9351724982261658, "The Radio-Frequency Test Completion Date of the Quantum Satellite is 27 July 2020."]
[9.471909523010254, 5.998388767242432, "The Function of the Sun-seeking precession controller Controller is Precess the solar panel normal vector to the sun vector."]
[2.2927582263946533, 5.726926326751709, "The Design of the OTA Operational Transconductance Amplifier is Truly differential amplifier."]
[6.121164321899414, 9.187252044677734, "The Mass of the MWR Dicke Radiometer is 99 kg."]
[8.707673072814941, 8.840653419494629, "The Viewing Angle of the SCIAMACHY Spectrometer is 55\u00ba."]
[3.536959409713745, 4.046442031860352, "The SCI ports of the STRV-1d DHS Data Handling System is Eleven RS-422."]
[8.525459289550781, 9.303677558898926, "The Color of the Driver Electronics Electronic Component is Green."]
[11.174057006835938, 3.5442566871643066, "The Activity of the Comet Celestial Body is Increased around the closest approach to the Sun."]
[8.69620418548584, 3.1675710678100586, "The Mission Objectives of the GOCE Satellite is Obtain a portrait of Earth's most intimate features."]
[9.16251277923584, 5.060708522796631, "The Spin Frequency of the MicroSCOPE Satellite is Twice the Orbital Frequency."]
[7.797024250030518, 5.919421672821045, "The Filters of the Water Machines Water Filtration System is Ultrafiltration and reverse osmosis."]
[9.842784881591797, 7.788235664367676, "The Energy Measurement Range for Electrons of the Telescope 3 Telescope is 2-12 MeV."]
[7.013979911804199, 0.4336366653442383, "The Launch Date of the MOMS Satellite is 18 June 1983."]
[8.894403457641602, 10.67580795288086, "The Camera Type of the CASPR Experiment is 8U binocular camera."]
[4.9705376625061035, 6.054520606994629, "The Phase Change Sample Rate of the Satellite Communication Device is 10 Hz."]
[7.902228355407715, 8.805025100708008, "The Spectral Knowledge of the Individual Spectrometers Instrument is 1.5 pm."]
[6.389589786529541, 2.955796480178833, "The Location of the NASA's Jet Propulsion Laboratory Organization is Pasadena, California."]
[7.793299198150635, 8.985806465148926, "The Wavelength Range of the SUSIM Spectrometer Instrument is 110 to 410 nm."]
[4.826233863830566, 1.8803648948669434, "The Quantity of the ICEYE SAR Satellites Satellite is 5."]
[6.8552327156066895, 9.091364860534668, "The Size of the Instrument Sensor is 45 cm x 20 cm x 20 cm."]
[7.498477935791016, 7.282309055328369, "The Contribution of the SPEXone Instrument is PACE mission."]
[8.480051040649414, 3.2985618114471436, "The Helix-Formation Distance of the TanDEM-X Satellite is Less than 1 km."]
[5.347907543182373, 4.218780994415283, "The Ground System of the ORS-6 Satellite is EGS (Enterprise Ground System)."]
[5.127438545227051, 3.035083293914795, "The Purpose of the CAPSat CubeSat is Perform quantum annealing experiments."]
[7.673248291015625, 8.79153823852539, "The Vertical Resolution of the SAGE-III Spectrometer is 0.75 km (solar measurements), 1.5 km (lunar measurements)."]
[9.412812232971191, 7.811530590057373, "The Power of the Particle Detectors Instrument is 20 - 50 V."]
[5.920406341552734, -0.2674753963947296, "The Mission Goal of the Oculus-ASR Satellite is Exercise and validate techniques for determining an orbiting object's pose using unresolved ground imagery."]
[2.127695322036743, 4.274617671966553, "The Solar Panel Peak Power of the NSat Satellite is 28.8 W."]
[5.56969690322876, 3.0124905109405518, "The Technology Management Contractor of the Heinrich Hertz satellite Communication Satellite is OHB."]
[9.632133483886719, 1.4032776355743408, "The Solar Array Deployment Time of the Solar Orbiter Spacecraft is 06:24 CET."]
[6.105656147003174, 3.047198534011841, "The Manufacturer of the Pearl White-1 Satellite is United States Air Force Space Command."]
[10.031378746032715, 1.4598219394683838, "The Local Time of Ascending Node of the COMPASS-1 Satellite is 9:15 AM."]
[9.719717025756836, 6.820176124572754, "The Survival Heaters Status of the RapidScat Satellite Instrument is On."]
[6.757483959197998, 3.0705912113189697, "The Mission Status of the PhoneSat-1 and -2 Satellite is Mission complete."]
[5.209598541259766, 9.27939510345459, "The SP Performance of the SEIS Instrument Seismometer is < 5 x 10-8 m s-2 Hz-\u00bd from 10-2 up to 100 Hz."]
[6.394514083862305, 3.392643451690674, "The Launch Site of the SMART-1 Satellite is Kourou, French Guiana."]
[1.9721025228500366, 3.946878671646118, "The Power Source of the S/C Satellite is Surface-mounted triple-junction solar cells."]
[9.03347110748291, 3.4184470176696777, "The Control Mode of the NEOSSat Satellite is Sun-Point."]
[9.264904975891113, 7.82520055770874, "The Cooling Temperature of the Filter Wheel Optics Subsystem is 213K."]
[9.122307777404785, 8.04471206665039, "The LYSO crystals of the Range Calorimeter Particle Detector is Side of 5 cm."]
[4.50481653213501, 2.98134183883667, "The PRN of the GSAT-0211 Satellite is 2."]
[4.741781711578369, 1.7720630168914795, "The Number of Satellites to Launch in 2022 of the Satellogic Satellite Company is Up to 12."]
[4.782327175140381, 3.1390233039855957, "The Internal Trays of the GNB Satellite Platform is 2."]
[8.595455169677734, 10.363434791564941, "The Lens System of the Instrument CCD Imaging Camera is f/4 telecentric lens system with a 5:1 fiber-optic taper."]
[5.617389678955078, 6.171145915985107, "The Antenna Length of the OPAL Satellite is About 17.5 cm."]
[12.05759048461914, 3.2908360958099365, "The Orbit Inclination of the NRCSD Payload is 51.6\u00ba."]
[4.7942280769348145, 4.116557598114014, "The Future Enhancements of the EDSN Data Network is Implementation of an ACK/NACK system, or via delay tolerant networks."]
[7.544787883758545, 6.720628261566162, "The Vibration Testing of the TEMPEST-D Radiometer Instrument is Passed."]
[2.9977757930755615, 6.640649795532227, "The RF Transmit Power of the Transmitter Communication Device is 9.6 W."]
[5.215519428253174, 5.977221488952637, "The Quantity of the Zenith antennae Antenna is 2."]
[6.37933874130249, 8.508273124694824, "The Resolution of the RM-08 Passive Microwave Scanning Radiometer is 15 km x 20 km."]
[5.90858268737793, 9.076399803161621, "The Power Consumption of the Field Measurement Device Sensor is < 0.5 W."]
[6.0749311447143555, 3.2865254878997803, "The Plans of the ESA Organization is Develop a range of \u2018in-orbit servicing\u2019 technologies that will refuel, refurbish and de-orbit spacecraft."]
[6.765796661376953, 4.344290733337402, "The Conference Location of the High Spatio-Temporal Resolution Land Surface Temperature Mission Satellite is Valencia, Spain."]
[5.893165111541748, 5.285782337188721, "The Operation of the Satellite to Satellite Tracking Instrument (SSTI) Instrument is Provide Satellite-to-Satellite Tracking."]
[3.9670538902282715, 2.3378591537475586, "The Payload Space of the ITASat CubeSat Satellite is 2U."]
[8.933222770690918, 5.1053900718688965, "The Attitude Angle Error of the Satellite Satellite is Occurs after 15-20 minutes."]
[9.921481132507324, 4.784327507019043, "The Tank Pressure Range of the Launcher Test Facility is 0.2 torr to 1.7 atmospheres."]
[7.982066631317139, 0.4632977247238159, "The Time Reference of the CryoSat-2 Satellite is TAI (International Atomic Time)."]
[3.199002981185913, 5.202762126922607, "The Capacity of the DDR2 SDRAM Memory is 1 GByte."]
[10.204728126525879, 1.0621088743209839, "The LTDN of the WorldView-3 Satellite is 13:30 hours."]
[6.481930732727051, 3.200486660003662, "The Information Provider of the SwissCube Satellite is Muriel Richard of EPFL."]
[9.45092487335205, 0.9074659943580627, "The Orbit Duration of the QARMAN CubeSat is Around four months."]
[7.049455642700195, 3.524697780609131, "The TDRSS Support of the Landsat-5 Satellite is No."]
[11.763314247131348, 1.6744438409805298, "The Final Location Time of the Philae Lander is 17:32 GMT."]
[5.772878646850586, 9.154690742492676, "The Average power of the Spectrometer Spectrometer is 124 W."]
[9.147059440612793, 8.98304271697998, "The Telescope Focal Length of the SIS (Scanning Imaging Spectrograph) Spectrograph is 75 mm."]
[7.080531120300293, 7.463035583496094, "The Autonomy of the MPO-MAG instrument Instrument is Largely autonomous."]
[7.362099647521973, 4.467611789703369, "The Imagers of the BILSAT-1 Satellite is Medium resolution panchromatic and multispectral."]
[4.258098125457764, 6.3705878257751465, "The Uplink Frequency of the RF Communications Communication System is S-band (2025-2110 MHz)."]
[6.0922675132751465, 5.179529666900635, "The Conference Presentation of the GPS Navigation Navigation System is 22nd International Technical Meeting of The Satellite Division of the Institute of Navigation (ION GNSS 2009)."]
[8.508279800415039, 11.031384468078613, "The Total Imaging Swath of the Eastman Kodak KLI14403 linear CCD sensor Sensor is > 600 km."]
[9.256021499633789, -0.5963755249977112, "The Agreement Date of the Nanosatellite And Plug-and-play Architecture (NAPA) Project Project is Sept. 17, 2010."]
[6.548399925231934, 1.402542233467102, "The Conference Date of the GOMS Geostationary Operational Meteorological Satellite is 1991."]
[6.180876731872559, 9.705031394958496, "The Mass of the APXS Spectrometer is 1.3 kg."]
[5.952571868896484, 1.626521348953247, "The Operation of the HTV Spacecraft is Reentry."]
[12.120834350585938, 3.303192377090454, "The Orbit Inclination of the SuperView-1 01 and Superview-1 02 Satellite is 98\u00ba."]
[10.391108512878418, 5.708531856536865, "The Number of Flights of the SEDS Tether Experiment Demonstration Program is Two."]
[6.8057332038879395, 2.232306957244873, "The Data Update Frequency of the GPM Satellite is Every half-hour."]
[4.8314361572265625, 1.7966004610061646, "The Number of Satellites of the Satellite Constellation Constellation is 3-5."]
[7.520425319671631, 2.6761186122894287, "The URL of the Cluster Satellite is http://www.esa.int/Our_Activities/Space_Science/Cluster/Origin_of_high-latitude_auroras_revealed."]
[10.307580947875977, 9.509366035461426, "The Purpose of the IRIS Satellite is Observe the transition region."]
[11.80339241027832, 1.0783802270889282, "The Number of Lunar Days of the Chang'e-3 Moon Lander is 28."]
[9.050048828125, 6.471900939941406, "The Mounting Configuration of the Honeywell QA2000-030 accelerometers Accelerometer is One measures spin rate and the other measures nutation."]
[4.407852649688721, 6.417402267456055, "The Frequency Band of the Ka-band transmitter Transmitter is Ka-band."]
[4.783491134643555, 7.371067523956299, "The Size of the  Submillimeterwave receiver receiver is 0.5 mm."]
[6.194173812866211, 8.182217597961426, "The Frequencies of the MSR Radiometer is 24 GHz and 31 GHz."]
[9.970056533813477, 6.6832051277160645, "The Thermal Condition of the Satellite Spacecraft is Stable."]
[11.748764991760254, 4.678536415100098, "The Star Formation Rate Discrepancy of the Cluster XDCPJ0044.0-2033 Galaxy Cluster is Four times the rate found in its outer regions."]
[8.023639678955078, 5.889254093170166, "The Involvement of the HSI payload, the mass memory and coding unit (DSHA) and the AOCS (Attitude and Orbit Control Subsystem) Subsystems is Image acquisition and calibration."]
[6.515035152435303, 2.708571672439575, "The Constellation Status of the Astrocast Satellite Operator is Up and running in space."]
[7.3165693283081055, 0.9005045890808105, "The Payload Fairing Installation Date of the ICON Satellite is 17 October 2018."]
[6.677985668182373, 5.808943271636963, "The Producing Instruments of the AVTP and AVMP retrievals Data Products is Cross-track Infrared Sounder and the Advanced Technology Microwave Sounder suite (CrIMSS)."]
[8.37441635131836, 6.610021114349365, "The Design of the SWiPS Sensor is Compact."]
[8.997097969055176, 9.840703964233398, "The Function of the Photo MOSFET Switch Component is Capacitor discharge."]
[7.496487617492676, 7.660677909851074, "The Global Observation Frequency of the TOMS Total Ozone Mapping Spectrometer is Daily."]
[8.035958290100098, -0.7429874539375305, "The Certification Date of the SpaceX Crew Dragon Spacecraft is November 11, 2020."]
[9.512495994567871, 0.5142367482185364, "The Design Lifetime of the SIMBA Satellite is 3 years."]
[9.752485275268555, 5.5615925788879395, "The Components of the CDRA Orbital Replacement Unit is Two beds known as a Desiccant/Adsorbent Bed Orbital Replacement Unit."]
[5.909106731414795, 6.756857872009277, "The Intrinsic Range Resolution of the KaRIn Radar is 75 cm."]
[4.437468528747559, 6.309179782867432, "The Flight Heritage of the HiSPiCO S-band Transmitter/Transceiver is Sounding rocket."]
[7.715429782867432, 9.94705581665039, "The Polarized Channels of the VNIR Sensor is 2."]
[6.963927268981934, 2.5386483669281006, "The Thesis URL of the AAUSAT3 Satellite is 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."]
[6.385852336883545, 1.6764038801193237, "The Project Status Meeting Date of the Jason-1 Satellite is Oct. 18-20, 2010."]
[7.817531585693359, 8.667226791381836, "The Instantaneous spectral coverage of the Spectrometer Instrument is 3.58 km/s."]
[8.151461601257324, 4.089337348937988, "The Dimensions of the Iceberg B-22 Iceberg is 85 km long and 64 km wide."]
[9.514760971069336, 0.562938392162323, "The Operational Lifetime of the GOES-R Satellite is 10 years."]
[7.036159992218018, 9.777891159057617, "The Spectral Range (\u00b5m) of the Band 3 Spectral Band is 3.55 - 3.93."]
[4.377957820892334, 5.718103408813477, "The Components of the Command Communications System Communication System is VHF command receiver, pair of redundant UHF command and telemetry transceivers."]
[8.167280197143555, 4.980033874511719, "The Movement of the Telescope System Satellite Component is Along-track, across-track, or both."]
[5.141261100769043, 4.258716583251953, "The Data Management of the COSMOS Mission Operations System is Data transfer, data processing, data archiving."]
[6.2282633781433105, 4.198441028594971, "The Signal Types of the QuakeSat Satellite is Approximately 25."]
[4.738178730010986, 2.600400686264038, "The ISPR of the PM Satellite Component is 12."]
[8.835511207580566, 3.253960609436035, "The Purpose of the LEO Low Earth Orbit is Weather and reconnaissance."]
[4.977806091308594, -0.12795673310756683, "The Global Service Availability of the OneWeb Satellite Constellation is 2022."]
[6.8313140869140625, 8.53496265411377, "The Resolution of the Radiometer Instrument is 40 km."]
[11.727245330810547, -0.9933779835700989, "The Mass of the YES-2 Payload is 36 kg."]
[5.741813659667969, 6.73427152633667, "The Steering of the C-RADAR Phased Array Antenna System is 2-D electronic."]
[4.311335563659668, 6.632687091827393, "The Frequency of the L-band Transmitter Radio Transmitter is 1700 MHz."]
[10.818429946899414, 2.0083975791931152, "The Altitude of the Swarm-A and Swarm-C Satellite Constellation is 468 km."]
[9.811724662780762, 4.388064384460449, "The Volume Occupation of the Sail Subsystem is Lower 2/3 of the spacecraft."]
[12.008050918579102, 3.2456214427948, "The Orbit Inclination of the GRIFEX 3U CubeSat is 99.12\u00ba."]
[3.5748891830444336, 4.7218122482299805, "The Processor MIPS of the MPM Main Processor Module is 42 MIPS."]
[6.472362995147705, 4.37989616394043, "The Wavebands of the R3 spacecraft CubeSat is Visible to near-IR."]
[10.328790664672852, -0.7928152680397034, "The Nutation Rate of the O/OREOS nanosatellite Satellite is 4-5 rpm."]
[8.901985168457031, 7.214633941650391, "The Measurement of the WISPR Instrument is Solar Corona Structure."]
[8.353872299194336, 3.406805992126465, "The Height Error Requirement of the TanDEM-X Satellite is 10 m."]
[11.1976900100708, 6.714542388916016, "The Position Determination Accuracy of the SEXTANT Technology is Expected to be on the order of hundreds of meters."]
[10.150714874267578, 5.498292922973633, "The Desiccant Addition of the Valves Spacecraft Component is Done."]
[9.329511642456055, 6.294309616088867, "The Star Trackers of the ADCS Attitude Determination and Control System is 2."]
[12.94062328338623, 4.847403049468994, "The Mission of the IBEX Spacecraft is Outer heliosphere research."]
[8.686759948730469, 4.503770351409912, "The Longitude Range of the PRISMA Payload Satellite Payload is 180\u00b0W - 180\u00b0E."]
[8.787762641906738, 6.226874828338623, "The Rotation Rate of the MWI Instrument is 45 rpm."]
[8.16823959350586, 9.874778747558594, "The TDI Mode of the NAOMI Imager is Enabled in the Pan band."]
[6.837015151977539, 4.929276943206787, "The Purpose of the Sentinel-5P Satellite is Deliver a key set of atmospheric composition, cloud and aerosol data products for air quality and climate applications."]
[11.806153297424316, 4.511618614196777, "The Distance from Earth of the Chamaeleon I Star-forming Region is Around 550 light-years."]
[5.92360782623291, 6.868376731872559, "The Vertical Accuracy of the In-flight simulated radar interferometry experiment Experiment is 1 m."]
[6.182153224945068, 1.5321193933486938, "The Operation al Concept Presentation Date of the PAZ Ground Segment Ground Segment is June 3-5, 2014."]
[5.969459533691406, 8.48875904083252, "The Latitude Coverage of the MLS Microwave Limb Sounder is Complete each orbit."]
[3.685823678970337, 6.245455741882324, "The Data Rate of the HDR Terminal Communication Equipment is Up to 622 Mbit/s."]
[8.855148315429688, 9.973417282104492, "The Image Type of the Multispectral Visible Imaging Camera (MVIC) Camera is Color."]
[8.718353271484375, 8.97121810913086, "The Material of the Primary Sensor Sensor is Niobium C-103."]
[4.333114147186279, 5.4704365730285645, "The Upload Frequency of the IXPE Satellite is Once every three days."]
[3.217674493789673, 5.602395057678223, "The Header Size of the Processed Science Data Packet Data Packet is 23 bytes."]
[9.544769287109375, 5.9118123054504395, "The Attitude Knowledge Accuracy of the MCS Magnetic Control System is Within 0.1\u00ba."]
[5.174066066741943, 6.4347639083862305, "The Polarization of the TEC Antennas Antennas is Right, circular."]
[8.108659744262695, 3.989971399307251, "The Planned Imaging Area of the Pleiades Satellite is 150,000 km2."]
[9.023828506469727, 4.422871112823486, "The Total Geometrical Area of Solar Arrays of the CHEOPS Satellite is About 2.7 m2."]
[6.394853115081787, 6.930365085601807, "The Manufacturer of the SSP Altimeter Altimeter is SSTL/Astrium."]
[7.226024627685547, 1.055813193321228, "The Launch Date of the EROS-B Satellite is April 25, 2006."]
[10.315402030944824, 5.028585433959961, "The Plenum Pressure Threshold of the Thruster Propulsion System is 80% of the current main tank pressure."]
[3.7796859741210938, 6.168333053588867, "The Radio Link Speed of the Ground Station Equipment Communication System is 9.6 kbaud."]
[9.029741287231445, 1.8473466634750366, "The Ultimate Fate of the BepiColombo Spacecraft is To circle the Sun indefinitely in the vicinity of the planet."]
[3.521406888961792, 4.632786750793457, "The Configuration Bitstream Source of the V5QV FPGA FPGA is PROMs."]
[10.23527717590332, 2.9531004428863525, "The Orbit Altitude of the Bion-M1 Spacecraft is 575 km."]
[7.611740589141846, 0.8183584809303284, "The Launch Date of the KANOPUS-V-IK Satellite is July 14, 2017."]
[-4.981041431427002, 4.407583713531494, "The Support Phase Time Period of the Mango Tango Satellite Formation is from 09.09 onwards."]
[7.7136454582214355, 13.596099853515625, "The No. of Bins of the SPIM3 Spectrometer is 68, 136, or 272."]
[10.075735092163086, 1.3801605701446533, "The Equator Crossing Time of the OrbView-2 Satellite is 12:00 hours on descending node."]
[9.29928970336914, 1.2231872081756592, "The Expected Deployment Duration of the Spaceflight SSO-A: SmallSat Express Satellite is Over a period of six hours."]
[3.879551649093628, 6.097720623016357, "The Ground Stations Downlink Data Rate of the Payload Communication System is X-band at 800, 400, or 200 Mbit/s."]
[5.104088306427002, 3.713366985321045, "The Mounting Points of the Bus Structure Satellite Component is Star tracker, gyroscopes, High Gain Antenna, Low Gain Antennae, maneuvering thrusters."]
[5.895211696624756, 5.4711833000183105, "The Signal Tracking of the TriG receiver GNSS Receiver is GPS, Galileo, CDMA GLONASS, Compass."]
[9.002111434936523, 2.8117918968200684, "The Provider of the GCOM-W1 Satellite is JAXA."]
[2.2858688831329346, 4.439053535461426, "The Power of the Total Satellite is 13.9 W."]
[6.511358261108398, 0.6402395367622375, "The Establishment Year of the RADARSAT International Ltd. Company is 1989."]
[3.3322246074676514, 5.526764392852783, "The Output Buffer Size of the Transmission Module FPGA Module is 1115 bytes."]
[9.716607093811035, 1.4551892280578613, "The Deployment Time of the Secondary Mirror Support Structure Support Structure is Approximately 1 hour and 36 minutes."]
[7.652349948883057, 7.754011631011963, "The Absolute Accuracy of the FFRF sensor Metrology Instrument is 1 cm on distance."]
[7.138564586639404, 5.004146099090576, "The Annual Methane Release of the Kayrros Studies Methane Leak Detection is 20 megatons."]
[6.324189186096191, 5.446853160858154, "The SAR Interferometry Techniques of the TanDEM-X Satellite is Digital beamforming, single-pass polarimetric SAR interferometry, ATI with varying baseline, or super-resolution."]
[4.299112796783447, 6.43745231628418, "The Ku-band beams of the Repeater subsystem Communication System is 4 Ku-band beams using a receive-only direct radiating phased array antenna (DRA)."]
[6.770930290222168, 1.2501178979873657, "The Presentation Date of the FalconSAT-7 Satellite is Sept. 13-16, 2011."]
[11.719332695007324, 1.1576818227767944, "The Sample Collection Amount of the Chang'e-5 Lander Lander is 0.5 kg from drilling and 1.5 kg scooped from the surface."]
[7.072113513946533, 7.729439735412598, "The Image Capture Frequency of the MSU-GS Imager is Every 15 minutes."]
[7.949252605438232, -0.17309559881687164, "The Docking Date of the Tianzhou-2 Cargo Spacecraft is 29 May 2021."]
[2.114305019378662, 4.027698516845703, "The Power Output of the Solar Array Power Generation is Meets the satellite operation requirements."]
[6.451068878173828, 2.7269692420959473, "The Location of the GPM Core spacecraft ground segment Ground Segment is JAXA."]
[6.858950614929199, 3.4783759117126465, "The Data Production of the INCUS Satellite is About 15 times the data of CloudSat."]
[7.170054912567139, 4.498934268951416, "The Sensor Complement of the HJ-1A Satellite is Wide View CCD Cameras (WVC), Hyperspectral Imager(HSI)."]
[8.512415885925293, 10.719873428344727, "The Power Consumption of the MSU-50 Camera is 6.8 W."]
[3.5306763648986816, 4.067302227020264, "The Analog channel of the STRV-2 DHS Data Handling System is None."]
[10.288056373596191, 9.564799308776855, "The Signal Processing and Control Module Architecture of the IRIS Satellite is PowerPC."]
[6.664387226104736, 3.255958080291748, "The Software of the HISat Satellite is App-based, open-source approach to core resource-sharing cellular firmware."]
[6.7566022872924805, 6.140120029449463, "The Calibration Standard of the ISS-RapidScat Scatterometer is Golden standard."]
[8.853801727294922, 5.29316520690918, "The Attitude Measurement Accuracy of the Spacecraft Satellite is 1-2\u00ba."]
[9.54842758178711, 6.00177526473999, "The SciC Mode Operation of the ADCS Attitude Determination and Control System is +X of the spacecraft towards the velocity direction with +Y of the spacecraft pointing as close as possible towards nadir direction."]
[9.576811790466309, 3.6898436546325684, "The Water Ice Concentration Measurement Range of the Lunar Flashlight Spacecraft is 5 wt% or less to 0.5 wt%."]
[6.340524196624756, 8.52280330657959, "The Swath Width of the MIS Instrument Microwave Radiometer is ~1,700 km."]
[9.199501991271973, 4.164108753204346, "The Volume of the PROBA-1 Satellite is 1 m3."]
[1.5318024158477783, 4.991003513336182, "The Variable Retardance with Applied Voltage of the LCVR Liquid Crystal Variable Retarder is Unknown."]
[8.847010612487793, 9.978180885314941, "The Components of the SIM Science Instrument Module is Focal-plane cameras, ACIS, HRC."]
[5.339570045471191, 3.6375436782836914, "The URL of the IXV Spacecraft is http://www.esa.int/Our_Activities/Launchers/IXV/IXV_spacecraft."]
[6.786212921142578, 0.6983471512794495, "The Start of Imagery Download of the TDRSS Satellite System is April 2010."]
[8.571741104125977, 6.981239318847656, "The Dynamic Range of the Magnetic Field Sensor Sensor is fT - mT."]
[10.277412414550781, 6.840364933013916, "The Power of the TCS Thermal Control Subsystem is 2 W."]
[6.557680606842041, -0.10527711361646652, "The Launch Date of the PSLV-C41 Satellite is April 12, 2018."]
[10.88947868347168, 5.70302152633667, "The Publication Date of the Submerged Sources of Transient Acoustic Emission from Solar Flares Research Paper is 20 September 2020."]
[5.678378105163574, 9.192298889160156, "The Power of the CSS Instrument is 0.1 W."]
[8.21922779083252, 3.215167284011841, "The Bus Design of the TanDEM-X Satellite is Extended to allow the formation flight of both satellites."]
[6.763726234436035, 5.922302722930908, "The Data Usage of the ISS-RapidScat Satellite Instrument is Tropical Cyclone Forecasting."]
[4.727039813995361, 0.16036809980869293, "The Prime Contractor of the OneWeb Satellite Constellation is OneWeb Satellites \u2013 a joint venture between OneWeb and Airbus Defence and Space."]
[11.520349502563477, 3.2041015625, "The \u03b2 Angle Variation of the NanoRacks-QB50 CubeSats Satellite is 0-75\u00ba."]
[6.5657267570495605, 2.4737815856933594, "The URL of the Space Cube 2 Onboard Computer is http://spacewire.computing.dundee.ac.uk/.../takahashi.pdf."]
[8.48271369934082, 6.792760848999023, "The Heritage of the NewMag Magnetometer is MFI (Magnetic Fields Instrument)."]
[6.968473434448242, 0.16651348769664764, "The Launch Date of the VRSS-1 Satellite is Sept. 28, 2012."]
[8.663467407226562, 7.863118648529053, "The Developer of the Small Analyzer for Neutrals Analyzer is Sweden."]
[8.231205940246582, 9.043620109558105, "The Swath Width of the Sensor Sensor is 72.4 km."]
[7.263023853302002, 7.891888618469238, "The Number of Tapes of the MOMS-2P Instrument is 19."]
[8.517693519592285, 5.3033766746521, "The Pointing Accuracy of the GP-B satellite Satellite is 0.97 \u00b5rad RMS (0.2 arcsec RMS)."]
[8.237666130065918, 9.167329788208008, "The Count Rate of the Instrument Sensor is From 200/s (IP) to 104 /s (solar corona) per pixel."]
[7.927251815795898, 7.079821586608887, "The Range of the Experiment Unknown is 36 nT."]
[8.217240333557129, 8.933514595031738, "The Angular Resolution of the S-020 XUV Spectrograph is Modest."]
[8.9003324508667, 9.264033317565918, "The Structure Material of the Infrared Imager Sensor is CeSiC (Carbon-fiber reinforced Silicon Carbide)."]
[6.743118762969971, 6.009523868560791, "The Primary Usage of the QuikSCAT Scatterometer is Measure winds inside distant hurricanes."]
[7.413219451904297, 0.6927157044410706, "The Launch Date of the Polar Scout 6U CubeSat Satellite is December 3, 2018."]
[10.533110618591309, 7.811432361602783, "The | of the GOES-12 SXI Instrument Instrument is Coronal Imaging with the GOES-12 SXI Instrument."]
[7.484324932098389, 9.055266380310059, "The Size of the Miniature High-Resolution Imaging Spectrometer Imaging Spectrometer is 360 x 260 x 180 mm."]
[2.2952451705932617, 4.375970363616943, "The Maximum Power Budget of the SERB Nanosatellite Satellite is 20 W."]
[9.449483871459961, 5.06003475189209, "The Spin Rate of the ELFIN Satellite is 20 rpm."]
[4.747776031494141, 6.611292362213135, "The Frequency Ranges of the TEC Antennas Antennas is 1250 MHz and 1600 MHz."]
[11.760845184326172, 4.7425007820129395, "The Mass of the SS 433 Cosmic Object is Millions to billions of times the mass of the Sun."]
[4.977656841278076, 1.8694210052490234, "The Number of Free Flyers of the ORS-3 Mission Satellite Mission is 26."]
[7.09330415725708, 6.9532856941223145, "The Anomaly Start Date of the GOMOS instrument Instrument is August 2011."]
[11.068947792053223, 4.843252182006836, "The Image Span of the NGC 7538 Star Factory is About 50 x 50 arc minutes."]
[9.588507652282715, 6.014421463012695, "The Components of the ADCS Attitude Determination and Control Subsystem is 3 magnetorquers: two torque rods and one air coil torquer."]
[9.450874328613281, 0.6355361938476562, "The Age of the Integral Spacecraft is 18 years."]
[9.692111015319824, 1.5055930614471436, "The Data Collection to Estimate Extension of the C/NOFS Satellite is 24 hours."]
[5.219203948974609, 5.056437015533447, "The T1 - Ground Station or User Platform initialized but not illuminated by the downlink, T2 - Ground Station or User Platform illuminated by the (optionally dithered) downlink beam, T3 - Ground Station or User Platform synchronized clock to downlink beam str of the Ground Stations or User Platform States is The Ground Stations or User Platform states are: T1 - Ground Station or User Platform initialized but not illuminated by the downlink T2 - Ground Station or User Platform illuminated by the (optionally dithered) downlink beam T3 - Ground Station or User P."]
[7.811407566070557, 8.539870262145996, "The Visible Spectral Range / Bandwidth of the SOLSPEC-SOLAR Spectrometer is 285-910/1.6."]
[7.86575984954834, 3.3254756927490234, "The Number of Data Takes of the TerraSAR-X Satellite is Over 12000."]
[8.559657096862793, 7.917075157165527, "The Cadence of the Electron Spectrum Measurement is 5 minutes."]
[5.213466644287109, 1.6182206869125366, "The Number of Upper-Stage Engine Burns of the STP-2 Mission is Four."]
[6.559164047241211, 4.3520331382751465, "The Imaging Type of the R3 spacecraft CubeSat is Multispectral."]
[8.834189414978027, 7.680304050445557, "The Collector Segments Arrangement of the IDM Ion Drift Meter is Along the satellite nadir and the orbit normal."]
[8.621423721313477, 7.891005516052246, "The Function of the ToF (Time-of-Flight) counter Instrument Component is Measure the velocity of particles."]
[7.6588053703308105, 1.571139931678772, "The Full Implementation Approval Date of the SMOS Satellite is Nov. 2003."]
[4.803489685058594, 0.8882436752319336, "The Cost of the NPOESS Satellite Program is Exceed $14 billion."]
[7.288896560668945, 3.725534439086914, "The Advancements of the Pelican Satellite Constellation is Higher revisit and higher spatial resolution, faster data access and delivery."]
[7.5173869132995605, 8.858190536499023, "The Spatial Resolution of the Instrument Spectrometer is 13.5 km horizontal at nadir for IR bands."]
[6.181956768035889, 9.701333045959473, "The Mass of the SSRNI Data Acquisition and Registration System is 9 kg."]
[9.296928405761719, 5.540768146514893, "The Control Methods of the Attitude Control Satellite Subsystem is Magnetorquer-assisted gravity gradient, 3-axis reaction wheels and 3 magnetorquers."]
[10.334059715270996, 4.944952487945557, "The Thrust Level Increase of the IES Ion Engine System is 25%."]
[6.514337062835693, 5.6557722091674805, "The GPS Occultations of the GNOS Instrument Occultation Measurement Device is More than 500 per day."]
[4.381407260894775, 7.776611328125, "The Center Frequency of the Channel 5 Sensor is 36.5 GHz."]
[8.065683364868164, 7.310625076293945, "The Data Collection Focus of the CIP Instrument is Eclipse time and the transition time from sunlight to eclipse time."]
[7.72900915145874, 8.364273071289062, "The Instrument Type of the AIRS Atmospheric Infrared Sounder is Multi-aperture, non-Littrow echelle array grating spectrometer configuration."]
[9.560855865478516, 1.4390692710876465, "The Downlink Time of the Sentinel-3 Satellite is Approximately 6 minutes per orbit."]
[7.133334159851074, -0.0192609503865242, "The End of Life of the S3B Satellite is 2028."]
[6.565044403076172, -0.07168879359960556, "The Launch Date of the PSLV-C35 / SCATSAT-1 Satellite is Sept. 26, 2016."]
[0.9261534810066223, 4.211033821105957, "The Capacity of the Lithium-ion battery Power Source is 60 Ah."]
[5.930954456329346, 3.5897433757781982, "The Coordination of the Commercial Partners Hisdesat and Airbus DS is Required."]
[10.084229469299316, 1.5174825191497803, "The Orbit Period of the HORYU-4 Nanosatellite is 96.2 minutes."]
[8.954305648803711, 10.456676483154297, "The Image Resolution of the ASAP-Light Camera System is 4 Mpixels."]
[6.056495666503906, 2.7207891941070557, "The CEO of the Iridium Satellite Operator is Matt Desch."]
[1.380758285522461, 4.163974761962891, "The Battery Charging Time of the NextSat Satellite is Within a single orbit."]
[9.0781831741333, 8.183389663696289, "The Sensitive Area of the IS Diaphragm is 100 cm2."]
[8.274992942810059, 2.221116304397583, "The Presentation Authors of the Lunar Reconnaissance Orbiter Satellite is Jan McGarry, Tom Zagwodzki, Ron Zellar, Carey Noll, Greg Neumann, Mark Torrence, Julie Horvath, Bart Clarke, Randy Ricklefs, Mike Pearlman."]
[9.975011825561523, 4.81877326965332, "The Function of the Ion Propulsion Assembly (IPA) Propulsion System is Compensated for the drag force experienced by the satellite\u2019s orbit in real-time."]
[7.875437259674072, 7.848276138305664, "The Measurement Accuracy - Intensity of the Instrument Sensor is 10%."]
[9.077788352966309, 10.799535751342773, "The Swath Width of the MSC Camera is 51 km."]
[6.233745098114014, 7.092094898223877, "The Telemetry Data Rate of the AltiKa Altimeter+ Radiometer is 43 kbit/s."]
[8.690614700317383, 10.646648406982422, "The Small Window Imaging Area Pixels of the CCD Image Sensor is 100 x 100."]
[10.288802146911621, 7.595133304595947, "The Material of the Baffles Instrument Component is Same material as the heatshield first layer."]
[10.956987380981445, 5.041248798370361, "The Test Masses Relative Acceleration of the LISA Pathfinder Spacecraft is Lower than ten millionths of a billionth of Earth's gravity."]
[3.93664288520813, 2.29706072807312, "The Deployable Drag Sail Area of the 3U CubeSat Satellite is 10m2."]
[7.09812593460083, 9.018685340881348, "The Spatial Resolution of the MSU-MR Instrument is 1 km."]
[9.562350273132324, 6.064701080322266, "The Sun Sensors of the ADCS Attitude Determination and Control System is 4."]
[5.980355739593506, 1.995160460472107, "The Launch Provider of the NPP Satellite is ULA."]
[3.9570915699005127, 5.6697821617126465, "The Downlink Speed of the AprizeSat-3 and AprizeSat-4 Satellites is Up to 300 kbit/s."]
[9.314276695251465, 6.3815999031066895, "The Accuracy of the Star Tracker Attitude Determination Device is < 7 arcsec RMS cross-boresight, < 70 arcsec RMS around boresight."]
[4.800597190856934, 5.04176664352417, "The Transmission Protocol of the UHRIT Data Dissemination System is DVB-S2 (Digital Video Broadcasting-Satellite-Second Generation)."]
[11.774171829223633, -1.078542709350586, "The Total Weight of the ExoMars 2016 Trace Gas Orbiter and Schiaparelli Spacecraft is 4.300 kg."]
[4.640298843383789, 5.018762588500977, "The Modules of the TSCT Terminal is Data enquiry, data purchase, data acceptance, and the personal center."]
[8.803558349609375, 8.986635208129883, "The Flatness of the Grating Optical Component is 10 \u03bb (6348 nm)."]
[9.40944766998291, 7.81116247177124, "The Detector Type of the EPI-Lo Electron Detector is SSDs (Solid State Detectors)."]
[10.093621253967285, 4.341912269592285, "The Structure Height of the Clementine Spacecraft is 1.88 m."]
[5.081531524658203, 6.059019565582275, "The Dynamical Disturbances of the Test Masses Satellite Component is < 3 x 10-14 m s-2 Hz1/2 @ 1 mHz."]
[9.135567665100098, 9.170260429382324, "The FOV of the Limb Imager Telescope is 5.67\u00b0 x 0.91\u00b0."]
[9.51422119140625, 8.281315803527832, "The Effective Si Thickness of the X123-SDD X-ray Spectrometer is 0.5 mm."]
[11.474533081054688, 4.090394973754883, "The Mass of the Jupiter Planet is Over 300 times that of Earth."]
[4.9677958488464355, 2.050183057785034, "The Number of Payloads of the FY-3E Satellite is 11."]
[3.984900951385498, 4.898870468139648, "The Redundancy of the OBC On-Board Computer is Cold dual-redundant."]
[6.253418445587158, 4.090702533721924, "The Program Motivation of the ISERV Satellite is Timely access to data."]
[5.5503740310668945, 4.241825103759766, "The Function of the MMO Mission Management Office is Plan user requests for payload (SAR) tasking."]
[7.197589874267578, 0.28136441111564636, "The Launch Date of the Arachne Satellite is Early 2025."]
[2.2697863578796387, 4.463607311248779, "The Predicted Power Levels of the IXV Spacecraft is 700 W."]
[1.7887166738510132, 5.34161901473999, "The Power of the Voltage 3 Digital is 1.93."]
[6.388975620269775, 2.96309757232666, "The Developer of the ROLO Robotic Lunar Observatory is USGS (United States Geological Survey)."]
[11.547234535217285, 6.278374671936035, "The Ground Stations of the XMM-Newton Satellite is Perth, Kourou, Villafranca, Santiago."]
[8.041839599609375, 7.490229606628418, "The Development Start Date of the Airborne Lunar Spectral Irradiance (Air-LUSI) Instrument is 28 October 2020."]
[6.689314365386963, 7.366117477416992, "The Principal Investigator of the LOLA Lunar Orbiter Laser Altimeter is David E. Smith."]
[9.646970748901367, 0.708255410194397, "The Orbit Life With Balloon of the AeroCube-3 Satellite is 2-3 months."]
[10.32991886138916, 2.648660659790039, "The Perigee of the Deimos-1 Satellite is ~ 642 km."]
[9.495848655700684, 2.6907997131347656, "The Key Unknown of the Kinetic Impactor Technique Asteroid Deflection Method is Beta."]
[12.072765350341797, 2.1016812324523926, "The Launch Date of the REXJ Astrobot is July 21, 2012."]
[9.56647777557373, 5.971403121948242, "The Components of the ADCS Attitude Determination and Control Subsystem is Three magnetorquers, a single momentum wheel, a translation stage."]
[7.24737024307251, 3.8721201419830322, "The Tracking Reliability of the CHOMPTT Satellite is Only reliable when the SLR facility is in darkness."]
[5.895875453948975, 8.618009567260742, "The Number of Channels of the HSB Humidity Sounder is 4."]
[9.819108009338379, -1.015463948249817, "The Orbit Type of the JL-1-GF03B Microsatellite is SSO."]
[11.324652671813965, 3.521845579147339, "The Water Ice Abundance of the Comet Celestial Body is 10-15%."]
[4.558196067810059, 6.722259998321533, "The Frequencies of the DOR Tones Signal is Typically at 1 MHz and 2f0."]
[9.427197456359863, 1.4423860311508179, "The Revisit Period of the Constellation Satellite Constellation is 24 hours."]
[11.40499210357666, 5.035646915435791, "The Distance from Neutron Star of the Gaseous Atmosphere Atmospheric Feature is 1,500 miles."]
[3.6530182361602783, 6.127167701721191, "The Data Rate of the Data downlink Data Transmission is 2 x 50 Mbit/s."]
[6.876224040985107, 3.9652504920959473, "The Objective of the HJ-1 minisatellite constellation Satellite Constellation is 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."]
[4.4888997077941895, 4.339207172393799, "The Function of the EPC Layer Software Layer is Control task."]
[9.088473320007324, 0.9608569741249084, "The Working Life of the Copernicus Sentinel-1 Satellite is Exceeded."]
[11.171651840209961, 9.343101501464844, "The Power of the Earth Radiation Budget Experiment (ERBE) Instrument is 50 W (average) per scanner."]
[11.6991548538208, -1.1717807054519653, "The Mass (kg) of the COSMO-SkyMed Satellite is 1700."]
[4.472670555114746, 6.318420886993408, "The Function of the Ka-band payload Communication System is Receive, switch, amplify and transmit microwave signals."]
[4.445920467376709, 4.213250160217285, "The Components of the MEX Experiment Module is Memories, linear and optoelectronic devices, power MOSFETs."]
[3.883816957473755, 5.702490329742432, "The Fiber Optics Link Speed of the MIRAS Satellite Payload is 110 Mbit/s."]
[7.265076637268066, 4.161681175231934, "The Instrument of the DMC-3 Satellite Constellation is PAN (BJ-2)."]
[9.060138702392578, 9.857779502868652, "The Junction Type of the Device Photo Diodes is P-type in an n-type substrate."]
[6.45797061920166, 0.6751188039779663, "The Contract Date of the Ball Aerospace Company is Feb. 12, 2014."]
[6.073973178863525, 3.836866617202759, "The Data Distribution of the Satellite GFO is NOAA (and NASA) for distribution and use by the civilian community."]
[4.828971862792969, 4.056130886077881, "The Components of the Spacecraft Emulator Testing Equipment is Flight representative STRx Transceiver, OBC emulator development board, Antennas."]
[7.525722503662109, 3.8866240978240967, "The Coverage of the TeLEOS-1 Satellite is Equatorial belt."]
[7.151973724365234, 1.6868971586227417, "The Test Phase of the D-Sat Satellite is LEOP (Launch and Early Operations Phase)."]
[6.788374900817871, 7.113213062286377, "The Modes of the RA-1 Instrument is Ocean mode and ice mode."]
[8.083800315856934, 8.369566917419434, "The Test Status of the Interferometer Subsystem is Completed."]
[9.6854887008667, 9.034113883972168, "The Telescope Primary Mirror Aperture Diameter of the WV-3 Imager Imager is 110 cm."]
[9.506423950195312, 0.546855092048645, "The Nominal Life of the Spacecraft Satellite is 1 year."]
[5.482541084289551, 0.39594072103500366, "The Area of the Yaguas National Park National Park is 2 million acres (809,370 ha)."]
[7.925264358520508, 4.490146636962891, "The CAVIS Ground Resolution of the WorldView-3 Satellite is 30 m."]
[9.478111267089844, 8.144243240356445, "The Gd Foil Thickness of the LND Particle Telescope is 20 \u00b5m."]
[6.598771095275879, 0.4063129425048828, "The Launch Date of the CBERS 3 Satellite is November 2012."]
[11.662545204162598, -1.2539794445037842, "The Mass of the Kolibri-2000 Satellite is 20.5 kg."]
[1.5331659317016602, 4.313825607299805, "The Power Source of the Spacecraft Satellite is 28V battery."]
[4.7678351402282715, 7.180037498474121, "The Wavelength of the UHF Band is 69 cm."]
[4.411276817321777, 7.641116142272949, "The Bandwidth of the Channel 1 Sensor is 100 MHz."]
[7.062182903289795, 9.244270324707031, "The Size of the Rosetta Stone Artifact is 114.4 cm x 72.3 cm x 27.93 cm."]
[10.283698081970215, 6.853117942810059, "The Thermal Reservoir of the Thermal Management Subsystem Thermal Management System is 1."]
[9.243577003479004, -0.5991630554199219, "The Presentation Date of the NEMO Bus Nanosatellite is April 4-8, 2011."]
[7.2872114181518555, 6.1464948654174805, "The Purpose of the MAIA Multi-Angle Imager for Aerosols is 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."]
[3.3782832622528076, 5.440706729888916, "The Data Storage Capacity of the SGR-ReSI GNSS Reflectometry Instrument is 1 GByte."]
[9.380088806152344, 5.113875865936279, "The Reaction Wheel Rotation of the Integral Satellite is Roughly one rotation every 21 minutes."]
[9.534811973571777, -0.6460312008857727, "The Purpose of the MicroMAS Nanosatellite is Provide near-continuous views of severe weather."]
[8.578293800354004, 0.21790185570716858, "The Number of Open Seats of the Crew-4 Spacecraft is 1."]
[6.132093906402588, 4.180044651031494, "The Leading Scientist of the IASI Satellite Instrument is Cathy Clerbaux."]
[8.94229793548584, 6.635409832000732, "The Effectiveness of the Hollow Cathode Plasma Contactor Technology is Most effective technology for mitigating charging effects."]
[10.976699829101562, 3.361999988555908, "The Orbit Insertion Burn Duration of the Juno spacecraft Spacecraft is 30 minutes."]
[9.406152725219727, 7.3353352546691895, "The Modulator Grid of the FSU Faraday Cup Sensor Unit is High-voltage."]
[5.307375907897949, 3.2008602619171143, "The Type of the OTB-1 Satellite is Minisatellite."]
[9.102743148803711, 4.883303642272949, "The Once per orbit of the Solar Array Rotation is The solar array rotates once per orbit to maintain a nominally normal orientation to the sun."]
[13.809408187866211, 0.7666704654693604, "The Orbital Slot of the GSAT-0209 Satellite is C02."]
[7.539318561553955, 0.7980881333351135, "The Scheduled Date of the Launch Mission Event is 14 March."]
[7.117949485778809, 4.113687515258789, "The Imaging Mission of the SEOSAT-Ingenio Satellite is High-resolution land imaging."]
[7.110394477844238, 4.086564064025879, "The Instruments of the Meteor-1/Meteor-2/Meteor-Priroda Series Satellite Mission is 174-K, MR-900B, RMK-2, Chaika, MR-2000, MR-900."]
[8.897705078125, 7.966590881347656, "The Temperature Range of the Miniature High-Resolution Imaging Spectrometer Imaging Spectrometer is -40\u00b0C to +80\u00b0C."]
[11.035309791564941, 7.038548469543457, "The X-ray Instruments of the AstroSat Astronomy Satellite is 3 co-aligned X-ray instruments."]
[5.436568737030029, 3.1816513538360596, "The Number of TMTC Interfaces of the Heinrich Hertz Satellite is 1150."]
[6.598778247833252, 3.0334787368774414, "The Centers of Expertise Locations of the YES2 Satellite is 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."]
[7.194286346435547, 5.016411781311035, "The Data Usage of the GOSAT Satellite is CO2 levels in all layers of the atmosphere."]
[5.853204727172852, 9.104995727539062, "The Power of the Sensor Device is 2.24 W."]
[7.071356773376465, 3.9122374057769775, "The Concept Interest of the Satellite Constellation Earth Observation is High."]
[3.2741191387176514, 6.089308261871338, "The Communication Subsystem Radio of the Hope Probe Spacecraft is APL\u2019s Frontier radio."]
[5.762339115142822, 2.931429862976074, "The Satellite Manufacturer of the Airbus Company is True."]
[11.731120109558105, -1.0027035474777222, "The Mass of the Granada Payload is 5 kg."]
[11.246554374694824, 1.2488645315170288, "The Deployment Date of the Jade Rabbit Rover is Dec. 14, 2013."]
[2.22375750541687, 6.528579235076904, "The Latency of the ATL14 Antarctica/Greenland Ice Sheet H(t) Gridded Data is 45 days from receipt of last data in product."]
[4.751133441925049, 3.752901554107666, "The Consortium Members of the Maritime AI-NAV Program is FGI, Aalto University\u2019s Sensor Informatics and Medical Technology group, Fleetrange Ltd."]
[9.832277297973633, 7.91341495513916, "The Neutron Energy Range of the MGNS Neutron and Gamma-ray Spectrometer is Thermal to 10 MeV."]
[8.174162864685059, 4.138683319091797, "The Swath Width of the Pl\u00e9iades Satellite is Larger."]
[7.566372394561768, 5.016258239746094, "The Imaging Spectrometer of the PROBA Satellite is CHRIS."]
[7.661240577697754, 8.612931251525879, "The Purpose of the SPDC Quantum Optical Effect is Trace the solar spectral irradiance to Planck\u2019s constant and photon count number."]
[3.1717662811279297, 4.871312141418457, "The NAND Flash of the Stamp9G20 Microcontroller is 128 MB."]
[7.431707859039307, 0.7491641640663147, "The Handover Date of the PROBA-V Satellite is April 30, 2014."]
[8.808534622192383, 9.565569877624512, "The Lens System of the EXI instrument Imaging Instrument is 48 mm, f/3.6."]
[7.22445011138916, 9.18126392364502, "The Tuning Range of the FG (Filtergraph) Instrument is \u00b10.6 \u00c5."]
[8.561487197875977, 0.1522291600704193, "The Number of Countries with Researchers of the International Space Station Space Station is 106 countries."]
[7.019573211669922, 9.733348846435547, "The Wavelength of the Sub-mm Band is 860 \u00b5m."]
[7.9085516929626465, 4.853516101837158, "The Orbit Localization Interval of the WEOS Satellite is 10 s."]
[3.611689329147339, 5.754148006439209, "The Data Input Rate of the Data Handling System System is 336 Mbit/s."]
[4.3154377937316895, 4.521047592163086, "The Components of the MCCM Control Unit is Digital/analogue ASIC electronics."]
[6.67941951751709, 9.072038650512695, "The Size of the FREND Instrument is 465 x 380 x 370 mm."]
[6.545690059661865, 2.058012008666992, "The Launch Center of the RASAT Satellite is Jiuquan Satellite Launch Center in China."]
[7.418832778930664, 5.609712600708008, "The Latitude of the Noctilucent Clouds Atmospheric Phenomenon is Between 56 and 60 degrees north latitude."]
[5.008261680603027, 2.2234466075897217, "The Feeder Links of the Iridium PRIME Satellite Platform is 2."]
[6.67712926864624, 4.75404167175293, "The Instruments of the Megha-Tropiques Satellite is ROSA, ScaRaB, SAPHIR, MADRAS."]
[7.853042125701904, 1.242889404296875, "The Date of the Medicane Ianos Weather Phenomenon is 18 September 2020."]
[11.372722625732422, 3.689253091812134, "The Age of the Comets Celestial Bodies is 4.6 billion years."]
[7.208232402801514, 0.8596879243850708, "The Launch Date of the Deep Space 1 Satellite is Unknown."]
[7.306442737579346, 5.462492942810059, "The January 2016 Value of the CO2 Concentration Atmospheric Parameter is 401.1 ppm."]
[4.732010841369629, 4.441173553466797, "The Development of the SOLISS Satellite Optical Communication System is Collaboratively developed by Sony Computer Science Laboratories, Inc. and JAXA Space Exploration Innovation Hub Center."]
[9.157294273376465, 4.299662113189697, "The Dimensions of the MPA Structure is 71 cm x 71 cm x 76 cm."]
[10.727622032165527, 4.868229389190674, "The Cube Size of the LISA Pathfinder Spacecraft is 46 mm."]
[5.118748188018799, 4.408860206604004, "The Functions of the Ground System Ground System is MOC (Mission Operations Center) and DPDC (Data Processing and Distribution Center)."]
[9.132372856140137, 8.048051834106445, "The Operating Temperature of the NIR Detector is 257 K."]
[11.391742706298828, 3.9228556156158447, "The Orbital Period of the Kepler-186f Exoplanet is 130 days."]
[9.442959785461426, 5.998225688934326, "The Axis of the ISA Accelerometer is Three."]
[7.2876763343811035, 2.9813601970672607, "The Mission Status of the BeiDou-1 Satellite is Unknown."]
[10.022125244140625, 3.9441168308258057, "The \u0394V of the Deimos-1 Satellite is ~ 20 m/s."]
[12.007665634155273, 3.2613909244537354, "The Inclination of the GCOM-W1 Satellite is 98.2\u00ba."]
[8.46269416809082, 7.89108419418335, "The Quantity of the Tri-TIP Instrument is 4."]
[7.834733009338379, 2.9317197799682617, "The Revisit Time of the Cartosat-2E Satellite is Four-day."]
[1.9217991828918457, 3.8766696453094482, "The Type of the Solar Arrays Power System is Triple junction solar cells (GaAs)."]
[5.035752773284912, -2.3688888549804688, "The Affiliation of the Bruno N. Calvo Engineer is Unknown."]
[6.568440914154053, 4.386801719665527, "The Test Type of the CO2M Satellite is Shaker test."]
[11.120070457458496, 5.168285846710205, "The DRS Duration of the LISA Pathfinder Satellite is 90 days."]
[9.134452819824219, 5.3184075355529785, "The Attitude Control Components of the STPSat-1 Satellite is Momentum wheel, two smaller reaction wheels."]
[8.752395629882812, 0.19346193969249725, "The Spacewalk Elapsed Time of the Poisk ISS Module is 7 hours 19 minutes."]
[11.397809982299805, 6.506284713745117, "The M-CDR Date of the IXPE observatory X-ray Observatory is July 10, 2019."]
[12.102629661560059, 3.295400857925415, "The Inclination of the SARAL spacecraft Satellite is 98.538\u00ba."]
[6.201101303100586, 6.545929908752441, "The Mode of Operation of the Poseidon 4 Radar Altimeter is SAR and pulse-width limited modes."]
[4.9845099449157715, 3.8067026138305664, "The Formation of the Formation Flying Navigation Strategy is A-train (Aqua in the lead and Aura at the tail)."]
[5.237904071807861, 4.952219486236572, "The Inputs of the TAFF Software Package is GPS data provided by the GPS receiver onboard TDX and, through the ISL, also from the GPS receiver data onboard the TSX."]
[8.289387702941895, 10.53246784210205, "The SNR of the 4-band CCD Imager Instrument is 641."]
[4.416775703430176, 3.949023723602295, "The Operation of the Automated Beacon Network Anomaly Detection System is Broadcasts a health message periodically."]
[7.411261081695557, -0.6045117378234863, "The Scheduled Deployment Date of the Cygnus spacecraft Spacecraft is Sunday, July 15th."]
[7.50033712387085, 0.6476589441299438, "The Instrument Delivery of the CLARREO Pathfinder Satellite is 6/2022."]
[6.706094264984131, 0.8776997327804565, "The Separation Date of the ASTRO and NextSat Satellites is April 17, 2007."]
[8.156607627868652, 1.7967069149017334, "The Telemetry Data Investigation Start Date of the Voyager 1 Satellite is 18 May 2022."]
[8.286128044128418, 8.285164833068848, "The Mission of the MERTIS Thermal Infrared Spectrometer is BepiColombo."]
[6.554667949676514, 5.519843101501465, "The Function of the GNSS-POD Precise Orbit Determination Instrument is 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."]
[8.025524139404297, 0.5072516202926636, "The Mission Duration of the CryoSat-2 Satellite is October 2010 to April 2013."]
[6.846887588500977, 8.711301803588867, "The Main Mode Ground Resolution of the MRSE Instrument is 25 m."]
[3.6137869358062744, 6.527424335479736, "The Data Transmission Rate of the RF Communications Transmitter is 1.2 kbit/s for the UHF band."]
[4.809643745422363, 0.1438220590353012, "The Investment Minister of the OneWeb Satellite Communications Company is Gerry Grimstone."]
[10.180229187011719, 6.7641143798828125, "The Thermal Control Type of the CASSIOPE spacecraft Satellite is Passive, supplemented with software-controlled operational heaters."]
[9.727642059326172, -0.6601106524467468, "The Mission of the NEOSSat Microsatellite is Asteroid astronomy and Space Situational Awareness experimentation."]
[6.695618629455566, 1.2917753458023071, "The Approval Date of the BRITE-PL Satellite Project is Early 2010."]
[5.466626167297363, 3.0215976238250732, "The Bus Functions of the Restore-L Satellite is Structural support, propulsion, attitude control, data and communications interface and power."]
[9.326813697814941, 6.384318828582764, "The Attitude Data Acquisition Time of the Procyon Star Tracker is 8 seconds from power-on."]
[4.221867561340332, 4.812702655792236, "The Data Format of the Modem Processor Signal-Processing Chain is CCSDS AOS (Advanced Orbiting Systems) Transfer Frames."]
[11.74422550201416, 7.491680145263672, "The Demonstration Requirement of the DSAC Atomic Clock is In-orbit demonstration of the precision timing and navigation capabilities."]
[8.60690975189209, 5.018087863922119, "The Coarse Pointing Accuracy of the NEMO-AM Satellite is Better than 5\u00b0."]
[7.407803058624268, 0.46821391582489014, "The Launch Date of the SVOM Satellite is No earlier than 2020."]
[7.50840950012207, 0.8583018779754639, "The ADCS Malfunction Date of the Monitor-E Spacecraft is Feb. 2007."]
[9.089217185974121, 8.837665557861328, "The Off-nadir Capability of the Telescope Optical Instrument is \u00b1 15\u00ba."]
[8.774312973022461, 2.196934700012207, "The Program Scientist of the New Horizons Spacecraft is Curt Niebur."]
[10.866846084594727, 3.3155431747436523, "The Main Rocket Motor Usage of the Juno spacecraft Spacecraft is Twice."]
[9.577370643615723, 3.8598673343658447, "The Formation Ranges of the CanX-4 Satellite is 50 m."]
[7.93255090713501, 0.9063568711280823, "The Arrival Date at NASA Plum Brook of the Orion Spacecraft is November 22, 2019."]
[5.557240009307861, 2.766559600830078, "The developer of the UniSat-1 Satellite is GAUSS (Gruppo di Astrodinamica dell' Universita degli Studi \u201cla Sapienza\u201d)."]
[9.611400604248047, 4.369231224060059, "The Flatness Target of the Euclid Spacecraft is Less than 50 microns."]
[6.096263408660889, 0.5410586595535278, "The Launch Time of the CANYVAL-X CubeSats CubeSats is 03:59 UTC."]
[8.044868469238281, 8.882649421691895, "The Sensitivity of the CHIPS Spectrometer is High."]
[8.367243766784668, 0.8231087327003479, "The Sampling of the Megha-Tropiques Satellite is At 13\u00baN,the various orbits come in one single packet following each other ~100 min apart."]
[9.096880912780762, 4.15020751953125, "The Dimensions of the ALOS-3 Satellite is 9.9 m x 16.6 m x 3.7 m."]
[10.533723831176758, 7.5249505043029785, "The Material of the Desiccant Bed Component is Silica gel."]
[11.341843605041504, 1.3629847764968872, "The Design Life Span of the Yutu Lunar Rover is Three months."]
[11.571174621582031, 4.416060924530029, "The Host Star Size of the Kepler-186 Star System is Half the size of the sun."]
[6.8538007736206055, 3.2188785076141357, "The Operation Status of the AISSat-1 Satellite is Nominal."]
[9.250866889953613, 8.909510612487793, "The F/No of the Telescope Optical Instrument is 2.8."]
[5.085904598236084, 4.412298679351807, "The Purpose of the Flight Dynamics Tool Ground Segment Component is Evaluate the navigation data and provides essential data for mission planning."]
[9.673542022705078, 1.5922499895095825, "The Earth Mapping Cycle of the OCO Satellite is 32 days."]
[5.157858371734619, 6.714488506317139, "The Installation of the Antenna Communication is In a cavity equal to half of a 4U standard volume (211 x 211 x 43 mm)."]
[7.028151035308838, 8.015586853027344, "The Climate Accuracy of the RAVAN Radiometer is Better than 0.3 W m-2 absolute."]
[1.2797596454620361, 4.17481803894043, "The Battery Capacity (BOL) of the CubeSat power module Power Control is 7.2 Whr."]
[8.601204872131348, 9.306790351867676, "The Instantaneous Field of View of the IFOV Spectrometer is 14.60 \u00b5rad."]
[10.329898834228516, 3.010315179824829, "The Orbit Altitude of the Electron rocket Launch Vehicle is 500 km."]
[5.3263068199157715, 3.9413557052612305, "The Function of the ISSAC SOC Space Operations Center is Downlink resultant imagery data and transfer to UND for processing and quick delivery to image requestors."]
[11.414810180664062, -1.3109465837478638, "The Instrument Mass of the DubaiSat-2 Satellite is 50 kg."]
[7.0852861404418945, 6.8444132804870605, "The Operational Period of the Trasser AOS Instrument is Until 1990."]
[8.510087013244629, 2.7007598876953125, "The Role of the Martin Popek Individual is Scientific team member."]
[7.524111270904541, 2.9134552478790283, "The Bus Design, Development and Integration of the KOMPSAT-5 Spacecraft is Led by KARI."]
[6.886847019195557, 3.241497755050659, "The Mission Status of the Odin Satellite is Operational (extended)."]
[1.883700966835022, 3.8775007724761963, "The Type of the Solar Cells Power Generation is Triple junction GaAs (Gallium Arsenide)."]
[4.961052894592285, -3.0954620838165283, "The Affiliation of the Yoshihiro Tomioka Author is Unknown."]
[2.9606821537017822, 6.735821723937988, "The Electrical Power of the HiSPiCO S-band Transmitter/Transceiver is 5 W."]
[11.804412841796875, -1.1519596576690674, "The Launch Mass of the IRNSS-1D Satellite is 1425.4 kg."]
[5.687838077545166, 3.227827548980713, "The Patented By of the iMESA Technology is USAFA."]
[5.06805419921875, 6.07400369644165, "The Frequency in Rotating Mode of the FEP Satellite Device is 1.0 x 10-3 Hz."]
[10.066303253173828, 1.6346241235733032, "The Orbital Period of the ALL-STAR-1 Satellite is ~ 91 minutes."]
[7.744865417480469, 4.361290454864502, "The Observation Purpose of the SWFO-L1 Satellite is Continuous unobstructed observation of the corona."]
[8.241214752197266, 7.720829010009766, "The Unknown of the DDCM Dielectric Deep Charge Monitor is Dielectric Deep Charge Monitor (DDCM)."]
[9.37583065032959, 0.957150936126709, "The Expected Data Transmission of the GRIFEX Satellite is Many months."]
[4.688181400299072, 6.8454389572143555, "The Module Size of the Wireless Compose-2 Wireless Network Infrastructure is Roughly the size of a small smartphone."]
[4.982236862182617, 7.105621814727783, "The Mass of the ORA Offset Reflector Antenna is 16 kg."]
[8.524677276611328, 0.21564258635044098, "The Backup Crew Member of the Crew-4 Spacecraft is Assigned to fill that seat."]
[9.283778190612793, 0.8991667032241821, "The Instrument Lifetime of the Telescope Optical Instrument is 5 years."]
[6.412572383880615, -0.7254102826118469, "The Positioning Errors Reduction with QZSS of the QZS-1 Satellite is More than 30%."]
[7.290276527404785, 0.2948733866214752, "The Launch Date of the Arktika-M N1 Satellite is February 2021."]
[12.980664253234863, 4.859412670135498, "The Launch Date of the IBEX Spacecraft is 2008."]
[8.891411781311035, 9.25118637084961, "The FOV Resolution of the WAOSS-B Sensor is 1.11 arcmin."]
[9.105588912963867, 10.637129783630371, "The Resolution of the Visible Camera Camera is < 0.5 km."]
[6.0638322830200195, 6.686592102050781, "The Spatial Resolution of the SRAL Radar Altimeter is 300 m."]
[4.270214080810547, 4.444215297698975, "The Data Interface of the ESEO-TriTel EQM Satellite Instrument is CAN (Controller Area Network) open protocol."]
[7.560309886932373, 8.689413070678711, "The Publication Date of the Atlas zur Interpretation von kosmischen Scanneraufnahmen Book is 1989."]
[6.995796203613281, 3.62095308303833, "The Geographic Coverage of the POPACS Satellite is Data."]
[3.5592703819274902, 5.177140235900879, "The Storage Capacity of the Mission Operation System Data Processing System is More than 2.5 PB."]
[6.313718318939209, 10.072668075561523, "The Mass of the DECA Camera is 0.6 kg."]
[11.849625587463379, -1.1303150653839111, "The Launch Mass of the Spacecraft Satellite is 730 kg."]
[9.505770683288574, 6.088294982910156, "The Sensors of the ADCS Attitude Determination and Control System is Redundant set of sun sensors and magnetometers."]
[7.142272472381592, 1.5882351398468018, "The Scheduled Launch of the Patrol Mission Satellite Cluster is End of 2021."]
[6.31794548034668, 4.206382751464844, "The Data Access of the Vision-1 Satellite is Access to a full archive and new acquisition data."]
[1.9558552503585815, 4.284056663513184, "The Solar Panels Power Generation of the EURECA Spacecraft is 1.5 kW at 28 VDC."]
[7.557374477386475, 0.5284321904182434, "The Trailing Satellite of the GRACE-1 Satellite is December 10, 2005."]
[11.206884384155273, 2.6312313079833984, "The Height of the Pas Moraine Moraine is About 30 meters (100 feet)."]
[7.154667854309082, 1.8228977918624878, "The Duration of the SJ-10 Satellite Satellite is About two weeks."]
[4.808511734008789, 0.8822658658027649, "The Cost of the Full-size Earth-observing satellite Satellite is Hundreds of millions of dollars to build, launch, and operate."]
[6.482320308685303, 6.224364757537842, "The Scanning Beams of the OSCAT-3 Radar Scatterometer is 2 conical scanning beams."]
[7.625925540924072, 7.793856143951416, "The Calibration of the CERES Instrument is Highly calibrated."]
[10.357769012451172, 2.9041717052459717, "The Altitude of the NanoRacks-QB50 CubeSats Satellite is ~ 400 km."]
[11.446170806884766, -1.3364579677581787, "The Mass of the HawaiiSat-1 Satellite is 80 kg."]
[5.8745317459106445, 6.15823221206665, "The Duty Cycle of the SAR antenna Antenna is 2-3 minutes per orbit."]
[6.96684455871582, 1.005733609199524, "The Symposium Date of the Flying Laptop Satellite is April 4-8, 2005."]
[4.499447822570801, 4.747890949249268, "The Data Delivery of the DPE Data Processor Element is HDF-5 formatted file."]
[8.582723617553711, 1.6263056993484497, "The Contract Signing Date of the BepiColombo Mercury Probe is Dec. 5, 2012."]
[6.417714595794678, 2.9593582153320312, "The TU Graz Team of the OPS-SAT Satellite is Composed of GMV and the Space Research Center Warsaw (Poland)."]
[9.077544212341309, 9.451457977294922, "The 4\u00ba x 300\u00ba of the FOV Sensor is FOV (Field of View) 4\u00ba x 300\u00ba."]
[6.373561382293701, 8.424817085266113, "The Channels of the MWRI Microwave Radiometer Imager is 10 channels."]
[7.560512065887451, 4.767023086547852, "The Geometric Accuracy and Stability of the PROBA-V Satellite is Unknown."]
[7.887999534606934, 3.3328700065612793, "The Mission Objective of the THEMIS Probes Spacecraft is Determine what physical process in near-Earth space initiates the auroras."]
[4.385141849517822, 5.76393461227417, "The RF Communications of the Spacecraft Satellite is 32 to 256 kbit/s."]
[12.128827095031738, 2.218587636947632, "The X-ray Spectrometer of the OSIRIS-REx Spacecraft is REXIS."]
[12.06124210357666, 2.112931966781616, "The Docking Date of the REXJ Astrobot is July 28, 2012."]
[10.183516502380371, 5.011490821838379, "The System of the Onboard Propulsion System Propulsion System is Dual-redundant."]
[8.114879608154297, 1.9713917970657349, "The Mars Atmosphere Entry of the Schiaparelli Lander is 19 October, 14:42 GMT."]
[7.13385534286499, 9.69969654083252, "The Range of the spectral band band is 0.58 - 1.0 \u00b5m."]
[9.808768272399902, -0.7077419757843018, "The Imaging Frequency of the PROBA-V Microsatellite is Every two days."]
[5.0583815574646, 8.711296081542969, "The Position Accuracy (RMS orbit) of the S-3 NRT Product is 10 cm threshold with a target of 8 cm (radial)."]
[6.023933410644531, 4.28012752532959, "The Commercial Weather Data Program of the NOAA Agency is Operational."]
[12.104345321655273, 3.280777931213379, "The Inclination of the Satellite Satellite is 99.049\u00ba."]
[7.768385887145996, 10.85544490814209, "The Data Quantization of the MI Radiometer Instrument is 10 bit."]
[9.52988052368164, 7.776721954345703, "The Energy Threshold of the EPISEM Instrument is Specific energy threshold is different for electrons and protons."]
[5.019088268280029, 4.293015956878662, "The Adaptability of the COSMOS Software System is Easily adaptable for adding spacecraft, interfacing with external software, and porting to MOCs."]
[9.080039024353027, 10.551225662231445, "The Exposure Time of the M-CAM 1 Monitoring Camera is 20 ms."]
[7.250951766967773, 1.6153507232666016, "The Presentation Date of the Hiroyuki Shindou Unknown is Oct. 6-7, 2008."]
[9.564867973327637, 6.025195598602295, "The Actuators of the ADCS Attitude Determination and Control System is Three in-house designed magnetorquer coils."]
[7.221912860870361, 1.5041368007659912, "The Operation End Date of the Cluster Satellite Mission is December 2014."]
[1.904866337776184, 4.03151273727417, "The Weight per Unit Area of the Solar Panels Power Source is Half of the traditional solar arrays."]
[11.508123397827148, 4.158971786499023, "The Diameter of the KELT-11b Planet is 181,600 km."]
[5.021343231201172, 6.113031387329102, "The Frequency (MHz) of the GPS L1 C/A Signal Carrier is 1575.42."]
[6.033680438995361, 3.2233970165252686, "The Debut Mission of the Grid Fins Control Surface is SpX-5."]
[9.408269882202148, 1.2299829721450806, "The Mission Duration of the Kepler Space Telescope is Three-and-a-half years."]
[3.820629119873047, 5.576119422912598, "The Telemetry Transfer of the Interfaces Communication is Flawless."]
[6.091490745544434, 2.791222095489502, "The Ground Segment Ownership of the Helios-2 Satellite is Belgium, Spain, Italy, Greece, Germany."]
[7.959024429321289, 9.841310501098633, "The GCP Density of the GCP Extraction Approach Image Processing is About 450 GCP per 1000 km2."]
[10.715423583984375, 10.27163028717041, "The Preamp feedback capacitance of the PHA Detector is 5\u201375 pF."]
[9.812078475952148, 8.619738578796387, "The Number of Mirror Shells per Module of the ART-XC Instrument Telescope is 28."]
[11.860581398010254, 1.0045398473739624, "The Launch Date of the Chang'e-5 Moon Surface Sampling Probe is Late November 2020."]
[9.909357070922852, 2.3094308376312256, "The Repeated ground track of the KOMPSAT-3A Satellite is 28days/409revolutions."]
[9.263697624206543, 8.928580284118652, "The FMC Mode Rotation Speed of the Telescope Optical Instrument is 1.5\u00ba/s."]
[11.0820894241333, 6.945146560668945, "The Ability of the X-rays Communication Medium is Pierce the hot plasma sheath."]
[7.3224663734436035, 0.18592950701713562, "The Launch Year of the Tandem-L Satellite is 2022."]
[9.293566703796387, 1.2238303422927856, "The Instrument Calibration Phase Duration of the GP-B mission Mission is 7 weeks."]
[4.0365986824035645, 6.668865203857422, "The Technology Readiness Level of the OEM628 Receiver Receiver is TRL5."]
[6.7488884925842285, 3.0911917686462402, "The Mission Status of the NigeriaSat-X Satellite is Operational (extended)."]
[8.384031295776367, 8.548474311828613, "The Problem of the NISP Near Infrared Spectrometer and Photometer is Stopped working in a cold vacuum state."]
[6.339605808258057, 4.036481857299805, "The Data Receiving Stations of the JERS-1 Satellite is 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 Researc."]
[7.1762919425964355, 1.9084031581878662, "The Experiment Focus of the SJ-10 satellite Satellite is Study on the pre-ignition characteristics, soot emission, and smoke distributions of the overload wire insulation."]
[8.122194290161133, 8.149101257324219, "The Technology of the EMIT Imaging Spectrometer is Image spectrometer."]
[12.01799201965332, 2.2785160541534424, "The Signal Travel Time of the OSIRIS-REx Spacecraft is Just over 18.5 minutes."]
[6.6593852043151855, 0.6642332673072815, "The Testing Start Date of the TET-1 Satellite is July 24, 2012."]
[5.180905818939209, 6.593465328216553, "The HPBW EL of the Antenna ADS-B Antenna is 73\u00ba."]
[8.588194847106934, 1.739388108253479, "The Launch Date of the James Webb Space Telescope Telescope is Later this year."]
[5.9157586097717285, 3.615509510040283, "The Managing Organization of the SWEAP Science Operations Center (SOC) Center is SAO (Smithsonian Astrophysical Observatory)."]
[6.8967671394348145, 8.439681053161621, "The Spatial Resolution Calculation of the Radiometer Sensor is Geometric mean of the minor and major axes of the ellipse projected on the earth, also accounting for earth curvature."]
[9.579251289367676, 7.1842756271362305, "The Operational Temperatures of the FPM Instrument is -40 \u00b0C and -10 \u00b0C."]
[7.382917881011963, -0.30152055621147156, "The Tracking Station Location of the HTV-7 Cargo Vessel is Guam."]
[7.045705795288086, 8.20288372039795, "The Noise Measurement Window Length of the SCA Calibration System is 8.5 ms and 10.8 ms."]
[9.570991516113281, 5.949646949768066, "The Momentum wheel of the ADCS Attitude Determination and Control Subsystem is 0.002 Nms at 2000 rpm."]
[4.895772933959961, 3.944976806640625, "The Purpose of the Commercial Crew Vehicle Emergency Breathing Air Assembly (CEBAA) Flight Support Equipment (FSE) and Air Recharge Tank Assembly (RTA) Hardware is 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."]
[7.191561698913574, 2.364748239517212, "The URL of the Mass Change (MC) Satellite Mission is URL:\u00a0https://science.nasa.gov/earth-science/decadal-mc."]
[7.163837432861328, 0.8673496842384338, "The Launch Date of the CALIPSO Satellite is Unknown."]
[9.60425090789795, 1.133489727973938, "The Commissioning Duration of the Spacecraft Satellite is 30 days."]
[7.713634967803955, 6.4552788734436035, "The Testing Status of the Euclid Satellite is Thermal qualification tests completed, mechanical vibration tests upcoming."]
[11.078537940979004, 6.909853458404541, "The Low-energy Response of the X-ray Satellite Navigation Navigation System is Down to 1 keV."]
[9.351213455200195, 11.605951309204102, "The Pixel size of the Channel 4 Sensor is 32 km x 32 km."]
[6.813466548919678, 1.201767921447754, "The Conference Date of the Joint Polar Satellite System Satellite System is June 11-15, 2012."]
[8.354710578918457, 7.376413345336914, "The Operation of the Space Comb Spectroscopy Setup is Under vacuum conditions."]
[9.092814445495605, 9.207294464111328, "The Parallelism of the Optical Window Component is \u22645 arcsec."]
[9.5050687789917, 0.9833323359489441, "The Mission Duration of the Spacecraft Satellite is Minimum of 3 years."]
[9.31989860534668, 0.7279341816902161, "The In-Orbit Design Life of the Aeolus Satellite is 36 months."]
[6.1624321937561035, 5.948709487915039, "The Image Stack of the DInSAR Differential SAR Interferometry is 8 TOPS and 8 stripmap images."]
[6.191686153411865, 8.522420883178711, "The Usage of the CST Microwave Studio\u00ae Software is Electric field calculation."]
[8.921470642089844, 8.09107494354248, "The Plane Orientation of the Imaging Calorimeter Calorimeter is x-plane, y-plane."]
[3.733395576477051, 6.188748359680176, "The Downlink Data Rate of the Telemetry, Tracking, and Command (TT&C) Communication is 6 Mbit/s."]
[6.450959205627441, 3.418281078338623, "The Required Thesis Level of the Experiment Space Station Experiment is Master or PhD."]
[10.02283763885498, 6.6495256423950195, "The Thermal Environment Before Separation of the MMO Spacecraft is Low temperature, not illuminated by sunlight."]
[6.177388668060303, 2.992359161376953, "The Purpose of the GPLTBs Navigation Payloads is Development models of the navigation payloads intended for the Galileo Second Generation (G2) satellites."]
[5.905104160308838, 6.8865532875061035, "The Speed Estimation Accuracy of the In-flight simulated radar interferometry experiment Experiment is 0.05 m/s."]
[5.530909538269043, 4.226292610168457, "The Regions of the Data Nodes Data Center is Asia, Europe and Africa, North and South America, Australia and Oceania."]
[3.990431308746338, 4.366875171661377, "The Function of the ESPA Ring Interface is Multifunctional integrating element."]
[9.04013442993164, 10.612112045288086, "The Spatial Resolution of the MSU-100 Camera is 60 m."]
[9.064372062683105, 5.3793511390686035, "The Attitude Control Computers of the GNB Satellite is 2 ARM7."]
[9.41252613067627, 11.521406173706055, "The Effective FOV of the Channel 7 Sensor is 24 km x 43 km."]
[5.912944793701172, 2.9006495475769043, "The Manufacturer of the STACEM Satellite is SDL (Space Dynamics Laboratory) of USU (Utah State University)."]
[10.267533302307129, 9.459845542907715, "The Spectral Signatures of the IRIS Satellite is Oxygen and heavier silicon ions."]
[8.368460655212402, 10.503134727478027, "The Pixel Resolution of the 4-band CCD Imager Instrument is 250 m."]
[7.605512619018555, 3.527611017227173, "The Revisit Frequency of the Satellite Constellation Constellation is Near the edge of the scan > Near nadir."]
[9.510575294494629, 3.5395028591156006, "The Regions of Interest of the Lunar Flashlight Satellite is Permanently shadowed and occasionally sunlit regions poleward of 80\u00ba S latitude."]
[5.05311393737793, 7.554514408111572, "The Data Rate of the STAFF/DWP Instrument is 3.00 kbit/s."]
[5.044676780700684, 4.644093036651611, "The Functionality of the Ground Station Ground Station is Collect satellite telemetry data, send satellite tasking requests, retrieve relayed data, and extract ground sensor data."]
[12.048532485961914, 3.287976026535034, "The Inclination of the Molniya Orbit Orbit is 63.4\u00b0."]
[5.327550888061523, 10.395548820495605, "The Unknown of the Lightning Imaging Sensor (LIS) Sensor is Unknown."]
[7.844607353210449, 1.3659043312072754, "The Data Gathering Start Date of the Space-Based Weather Instruments Weather Instruments is 8 February 2022."]
[4.740169048309326, 6.061585903167725, "The Ground Interference Frequency of the RAVAN CubeSat is 450 MHz."]
[7.46410608291626, 4.203319549560547, "The Observation Capabilities of the BILSAT-1 Satellite is Wide Field of Regard."]
[9.597867965698242, 2.308387279510498, "The Footprint Overlay of the CloudSat and CALIPSO Satellites is About 50%."]
[9.5449857711792, 0.9215760231018066, "The Time to Reach Intelsat 10-02 of the MEV-2 Satellite is Nearly eight months."]
[10.421309471130371, 7.567716598510742, "The Material of the Chimney Structure is CFRP (Carbon Fiber Reinforced Polymer)."]
[10.089707374572754, 2.5387027263641357, "The Altitude of the KOMPSAT-6 Satellite is 505 km."]
[6.0038228034973145, 6.377162456512451, "The Radiometric Bias of the Instrument SAR is \u2264 0.3 dB."]
[4.472820281982422, 4.789467811584473, "The Function of the DPU Data Processing Unit is Image processing and non-destructive compression."]
[8.350278854370117, 9.623492240905762, "The Pixel Response Time of the Detector Instrument Component is < 6 ms."]
[5.091182708740234, 6.957183837890625, "The IF Bandwidth (MHz) of the Antenna Reflector is 200."]
[9.028620719909668, 3.3324930667877197, "The SMIM Location of the LUMIO Satellite is Periselene of the transition orbit."]
[9.687467575073242, 3.064622402191162, "The Orbit Altitude of the GOCE Satellite is ~260 km."]
[9.618041038513184, 7.616521835327148, "The Electric Charge of the Neutrinos Subatomic Particles is Neutral."]
[8.875120162963867, 10.600787162780762, "The Number of Lines of the Calibration Cycle Camera Calibration is 2048."]
[6.611218452453613, 10.687553405761719, "The Nominal SNR of the Band 3 Spectral Band is 1170."]
[3.7638323307037354, 6.174022197723389, "The Energy Efficiency of the Optical Downlink Communication System is -4.6 dB detected photons/bit or 25-100 \u00b5J/bit."]
[7.701552867889404, 3.327265977859497, "The Data Availability of the Landsat 1-5 Satellites is All MSS data January 2009."]
[6.145610332489014, 2.737964391708374, "The Goal of the EIAST Organization is Establish a complete Space Industry within the UAE."]
[7.283285140991211, 9.326398849487305, "The Angle of Incidence of the TopSAR wide Imaging Mode is 20\u00b0 - 45\u00b0."]
[1.9248027801513672, 4.260729789733887, "The Power Output of the Solar Panels Power Source is 20 KW."]
[7.00098991394043, 5.316202640533447, "The Measurement Coverage of the SMOS Satellite is Arctic."]
[4.277750492095947, 6.639058589935303, "The Frequency of the UHF Transceiver Transceiver is 437.365MHz."]
[8.787979125976562, 9.150138854980469, "The Projection of the CUTE Spectrograph Entrance Slit is 23 arcminutes (23')."]
[11.721574783325195, 1.0938929319381714, "The Lunar Orbit Altitude of the Chang'e-1 Satellite is 200 km."]
[7.635258197784424, 6.556642055511475, "The Required Precision of the AOD Satellite Instrument is 0.05."]
[4.7354865074157715, 1.9273953437805176, "The Quantity Launched of the SuperDoves Satellite is 12."]
[8.58790397644043, 5.129293918609619, "The Spacecraft pointing capability of the ALOS/PRISM Satellite is \u00b11.5\u00ba (in cross-track)."]
[8.477137565612793, 8.03993034362793, "The Percentage of Sky Observed in Four Exposures of the Euclid Reference Survey Survey is 50%."]
[8.304044723510742, 10.41096305847168, "The Field of View of the 4-band CCD Imager Instrument is 36\u00ba, or 500 km swath width."]
[10.203779220581055, 4.666285037994385, "The Perturbation Forces of the Space Environment Satellite Environment is Solar pressure, drag."]
[4.334162712097168, 5.894432544708252, "The UHF/VHF omnidirectional antennas of the TT&C Tracking, Telemetry, and Command is 2."]
[7.786861896514893, 9.019803047180176, "The Spectral Resolution of the Spectrometer Spectrometer is <0.625 cm -1."]
[9.61534309387207, 2.1920695304870605, "The Cross-Calibration Frequency of the CloudSat Satellite is Once in 3 days."]
[10.577338218688965, 8.511021614074707, "The Overall Length of the COR2 Coronagraph2 Imager is 1348 mm."]
[11.210539817810059, -1.5207599401474, "The Mass of the ITASat-1 Cubesat is ~8kg."]
[3.975780963897705, 6.544281482696533, "The Modulation of the X-band Transmitter Transmitter is QPSK."]
[10.38179874420166, 2.794708013534546, "The Optimal Radial Distance of the PIXIE Satellite is 6 RE."]
[6.729130744934082, 3.8891470432281494, "The Purpose of the SAOCOM constellation Satellite Constellation is 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."]
[7.465783596038818, 8.215877532958984, "The Altitude Range of the Water Vapor VMR Measurement Device is 50 - 110 km."]
[7.608267307281494, 1.0038247108459473, "The Lift-off Date of the Foton microgravity mission Mission is Sept. 14, 2007."]
[8.274690628051758, 8.095524787902832, "The Exposure of the Observation Data is 40 ks."]
[2.3402090072631836, 3.6533007621765137, "The PZ-Surface Function of the H3 and H4 Spacecraft is Location of major mission instruments."]
[3.2028541564941406, 4.904210567474365, "The RAM of the protos Software is 8 kB of RAM."]
[5.411213397979736, 3.299370765686035, "The Use Case of the CubeSats Satellite is Atmospheric calibration objects."]
[6.0405449867248535, 3.5940968990325928, "The Developer of the PHI Instrument is Consortium with major contributions from institutes in Germany, Spain and France, and smaller contributions from Sweden, Norway and Switzerland."]
[9.337072372436523, 4.9936418533325195, "The Required Rotation Rate Knowledge of the ANDERR-MAA spacecraft Satellite is Yes."]
[5.986343860626221, 3.0837857723236084, "The Mission Consortium of the CHEOPS Satellite is University of Geneva and University of Bern."]
[4.914270877838135, 1.8609777688980103, "The Number of Satellites of the Pl\u00e9iades Neo constellation Satellite Constellation is 4."]
[1.3481603860855103, 4.186408519744873, "The Maximum Battery Power Before 100% Depletion in Orbits of the Satellite Spacecraft is 6 orbits."]
[6.347311019897461, 3.7294528484344482, "The Mission Objective of the Flying Laptop Satellite is Test ten different small-satellite technologies."]
[6.8248291015625, 3.3583998680114746, "The Mission Status of the GF-3 Satellite is Operational (nominal)."]
[11.375044822692871, 4.362212181091309, "The Measured Upper Atmosphere Temperature of the Jupiter Planet is Around 800\u00ba Fahrenheit (426\u00ba Celsius)."]
[9.132573127746582, 10.592156410217285, "The Picture Interval of the M-CAM 1 Monitoring Camera is Six seconds."]
[9.4334077835083, -0.07800044864416122, "The Functionality Duration of the SMDC-ONE Nanosatellite is Until reentry on 12 January 2011."]
[8.22769546508789, 8.008819580078125, "The Manufacturer of the MicrOmega Infrared Spectrometer is ESA."]
[3.458326578140259, 5.2668280601501465, "The Data Storage Capacity of the ResourceSat-2 Satellite is 400 GB."]
[10.0889253616333, 1.5212388038635254, "The Orbit Period of the Odin Satellite is 97.6 minutes."]
[8.430486679077148, 7.381659030914307, "The Measurement Rate of the SPAN Sensors Sensor is Constant."]
[7.108026027679443, 1.4631754159927368, "The Industry Day Date of the GMES Sentinel-1 Satellite is Nov. 2007."]
[5.989489555358887, 5.326235294342041, "The Function of the Global Positioning System (GPS) Receiver Instrument is Receives tracking signals transmitted by GPS satellites."]
[7.870419502258301, 8.404882431030273, "The Citation of the SOLSPEC Spectrometer is E. Hilsenrath, in Optical Remote Sensing of the Atmosphere, 1990 Technical Digest Series of the Optical Society of America, Vol. 4, pp. 409-412."]
[4.6217942237854, 0.19560009241104126, "The Number of Satellites of the OneWeb Satellite Constellation is 428."]
[8.355051040649414, 8.092493057250977, "The Development Date of the USNA MIDN Microdosimeter Instrument Microdosimeter is Unknown."]
[11.754491806030273, -0.962300181388855, "The Moving Part Mass of the SILEX Terminal is 70 kg."]
[7.672313690185547, 2.9744200706481934, "The Debris Removal Capability of the ELSA-M Spacecraft Servicer is Multiple defunct satellites in a single mission."]
[6.58091402053833, 0.5508268475532532, "The Launch Date of the TechEdSat Satellite is July 31, 2012."]
[5.04340934753418, 3.400519371032715, "The Project Management of the C&DH subsystem Satellite Subsystem is University of Tokyo, Hokkaido Institute of Technology, Tokyo Metropolitan College."]
[8.925965309143066, 5.592463970184326, "The Mounting Location of the RCS Pods Reaction Control System is Externally."]
[8.844002723693848, 7.882330894470215, "The Calibration Frequency of the TIR Instrument Telescope is Every 5 seconds."]
[9.275529861450195, 3.2339255809783936, "The Orbit Stability of the EQUULEUS Satellite is Quasi-periodic."]
[8.516988754272461, 9.896753311157227, "The Quantum Efficiency (QE) of the NISP IR Detector Detector is Mean specified values."]
[6.119891166687012, 3.5144882202148438, "The Deployment Location of the J-SSOD Satellite Deployer is ISS/JEM ( Japanese Experiment Module)/ Kibo."]
[4.824763774871826, 3.205604076385498, "The Payload of the Perseus-M1 and M2 6U CubeSats is AIS for ship tracking."]
[8.140826225280762, 11.110272407531738, "The Environment of the Linear Encoder Sensor is Vacuum-rated."]
[3.603553295135498, 4.722029685974121, "The Quantity in ADCS controller of the StrongARM SA1110 Processor is 1."]
[5.081507205963135, 5.4582014083862305, "The Antenna Dish Size of the ATLAS Space Operations Ground Station is 3.4 m to 9.1 m."]
[5.805901050567627, 3.247007131576538, "The Development Responsibility of the \u00b5RTU Software Application is SRL."]
[5.754359245300293, 7.044790744781494, "The Max. Data Rate of the RA-1 Radar Altimeter is 15 kbit/s."]
[6.870357513427734, 4.229604244232178, "The Camera Supplier of the OPTSAT 3000 Satellite is Elop."]
[3.1225860118865967, 5.9157328605651855, "The Multi-mode Capability of the MTP Transponder is True."]
[7.228884220123291, 1.0683567523956299, "The Testing Date of the EO-1 Satellite is Oct. 18, 2004."]
[7.0583086013793945, 4.431131839752197, "The Measurement Domain of the FORUM Satellite is Atmosphere, Gravity and Magnetic Fields."]
[6.942515850067139, 0.8084499835968018, "The Permanent Failure Date of the B1 Segment Antenna Segment is January 2011."]
[9.203872680664062, 6.1185808181762695, "The Momentum Envelope of the CMG Control Moment Gyroscope is 0.8 mNms."]
[5.249701976776123, 6.374873161315918, "The Size of the Receive Antenna Antenna is 2.2 m dish."]
[10.96815299987793, 4.909998416900635, "The Locations of the Shocks Phenomenon is Universe around stars, supernova remnants, comets, and planets."]
[8.34299373626709, 4.867122173309326, "The Digital Resolution of the Cluster S/C Satellite is 7.813 x 10 -3 nT, 3.125 x 10 -2 nT, 0.125 nT, 0.5 nT, 8 nT."]
[2.218599796295166, 6.525193214416504, "The Latency of the ATL11 Antarctica/Greenland Ice Sheet H(t) Series Data is 45 days from receipt of last data in product."]
[8.658123016357422, 9.140701293945312, "The Slit Length of the Instrument Spectrometer is 150 arcmin."]
[10.342769622802734, 3.12622332572937, "The Altitude of the Secondary Payloads Satellites is ~325 km."]
[12.943520545959473, 4.844788551330566, "The Purpose of the IBEX Satellite is Provide images of the solar system's boundaries."]
[11.763500213623047, 1.7349495887756348, "The Crevice Width of the Philae Lander is 1\u20131.5 m."]
[6.937859535217285, 2.5617127418518066, "The URL of the SCD-2 Satellite is https://www.wmo-sat.info/oscar/satellites/view/392."]
[8.553047180175781, 5.789369583129883, "The Bulk Velocity of the Proton Component Measurement Accuracy of the DSCOVR Satellite is 20%."]
[11.370063781738281, 4.053393840789795, "The Orbital Distances of the TRAPPIST-1 Star System is Within the orbital distance of Mercury."]
[7.045777797698975, 5.2439374923706055, "The Monoscopic Collection Capacity of the GIS Instrument Satellite Instrument is Up to 700,000 km2 of panchromatic imagery, Up to 350,000 km2 of pan-sharpened multispectral imagery."]
[9.162071228027344, 8.29146957397461, "The L1 Detectors Thickness of the HIT Sensor is 24 \u00b5m."]
[7.164780139923096, -0.029268372803926468, "The End of Life Date of the IDEA OSG 1 Satellite is 28 November 2017."]
[7.532248497009277, 2.382570505142212, "The Collaboration of the Mars Express and ExoMars TGO Mars Missions is At the forefront of the international fleet investigating the Red Planet."]
[10.134849548339844, 9.45090389251709, "The Far-UV Channel Range of the IRIS Observatory is 133.0\u2013141.0 nm."]
[7.756720066070557, 13.182304382324219, "The Pixel Resolution of the SPIM4 Spectrometer is 14 bit."]
[8.58959674835205, 5.271053791046143, "The Pointing Accuracy of the DSP satellites Satellite is <5\u00ba."]
[8.144062042236328, 1.3211551904678345, "The Date of the West Lothian Shale Bings Image is 21 March 2022."]
[4.009330749511719, 4.418771266937256, "The Functions of the OBC On-Board Computer is Processing, reconfiguration and timing."]
[7.2295708656311035, 1.0892384052276611, "The Development Date of the Strategic Sites Monitoring Solution Monitoring Solution is 8 October 2020."]
[6.729470729827881, 5.660043716430664, "The Number of Soundings of the GNOS-2 Satellite is 1000 per day."]
[6.7933268547058105, 0.5835228562355042, "The Launch Date of the STPSat-3 Satellite is 20 Nov 2013."]
[8.379916191101074, 6.7710723876953125, "The Location of the SCM Device is In the shade of the spacecraft, at the end of the magnetometer boom."]
[8.220702171325684, 2.5400662422180176, "The Data Collection Time of the TerraSAR-X Satellite is 60 years."]
[12.178706169128418, 5.329382419586182, "The Hot Gas in Galaxy Clusters Percentage of the Universe Cosmology is 4 percent."]
[9.031458854675293, 10.627406120300293, "The Spatial Resolution of the WFI Camera is 16 m."]
[4.773617744445801, 4.107527256011963, "The TT&C of the Bus Satellite Bus is Nominal operations."]
[9.368463516235352, 4.837854385375977, "The Canting Angle of the SAWs Satellite Component is +55\u00ba / 0\u00ba."]
[10.457996368408203, 2.516368865966797, "The Apogee (km) of the Meteor-1-2 Satellite is 690."]
[9.4585542678833, 5.853598117828369, "The CMG Assembly of the ACS Attitude Control Subsystem is IMPACT 1.1."]
[7.838624477386475, 8.704802513122559, "The Data Compression of the NMS Neutral Mass Spectrometer is Yes."]
[7.744898796081543, 8.641831398010254, "The Instantaneous spectral coverage of the Spectrometer Instrument is 1.38 km/s."]
[6.260804653167725, 7.503509998321533, "The Crystal Axes Orientation of the DBCP Pseudo-depolarizer is Crossed and rotated by 45\u00b0."]
[4.479825973510742, 5.920650005340576, "The S-band of the RF Communications Communication Subsystem is TT&C + ePOP."]
[7.9914069175720215, 8.924620628356934, "The Wavelength Range of the Telescope Optical Instrument is 600 -1000 nm."]
[4.977292537689209, 3.738809108734131, "The Function of the Bus Satellite Component is Provides the structural, power, and communications interfaces to the payload."]
[8.697105407714844, 4.666977405548096, "The TAG Site Flexibility of the Spacecraft Satellite is Maximum."]
[10.805506706237793, 3.4633266925811768, "The Distance from the Sun within the orbit of Mercury of the Solar Orbiter Satellite is Around 42 million kilometers."]
[3.9783670902252197, 6.515078544616699, "The Data Rate of the L-band HRPT High Resolution Picture Transmission is 665,400 bit/s."]
[7.261295318603516, 1.8673381805419922, "The Collaboration Invitation Date of the SWOT Satellite is 2 January 2019."]
[5.045156955718994, 6.987145900726318, "The Main Beam Efficiency (%) of the Antenna Reflector is 85."]
[9.36690616607666, 0.9818907380104065, "The Duration of the TAKE5 mission Satellite Mission is Jan. 31, 2013 - June 19, 2013."]
[9.157119750976562, 8.874170303344727, "The Visible Energy Transmission of the Optics Assembly Dichroic Mirror is 75%."]
[11.278336524963379, 3.5242884159088135, "The Size of the Comet Leonard Comet is About a kilometer across."]
[0.9346604347229004, 4.193478584289551, "The Capacity of the Battery Assembly Energy Storage is 15 Ahr."]
[7.590768337249756, 2.9153919219970703, "The Role of the Hinode Spacecraft is Sun-watching."]
[9.165048599243164, -0.6047805547714233, "The Launch Date of the ANGELS Nanosatellite is 2019."]
[8.481708526611328, 2.2659189701080322, "The Solar Wind Source Prediction of the Parker Solar Probe Satellite is Daily."]
[4.2478346824646, 6.48238468170166, "The Downlink Frequency of the RF Communications Communication System is X-band (8345.968-8346.032 MHz)."]
[9.924958229064941, 4.009965419769287, "The Deployment Time of the NanoSail-D2 Solar Sail is 30-45 seconds."]
[7.233719348907471, 7.5065016746521, "The Affiliation of the MAHRSI Instrument is NRL (Naval Research Laboratory)."]
[8.14795207977295, 0.21009542047977448, "The Time Extension Date of the BEAM Space Station Module is 4 Dec. 2017."]
[11.180859565734863, 9.345149993896484, "The Size of the Earth Radiation Budget Experiment (ERBE) Instrument is 60 cm x 60 cm x 57.6 cm/unit."]
[5.5733466148376465, 7.540366172790527, "The Orbital Average Power of the KaRIN Instrument is ~810 W."]
[5.301034450531006, 10.401054382324219, "The Missed Lightning in Northern Hemisphere of the TRMM LIS Lightning Detection Instrument is Up to 30% in the warm season months."]
[6.193536281585693, 5.164632320404053, "The Type of the NorAIS Sensor is Norwegian Automatic Identification System."]
[4.933134078979492, 2.2986433506011963, "The Number of Instruments of the JWST Satellite is 4."]
[4.77534818649292, 1.8082828521728516, "The Quantity of the Dove satellites Satellite is 88."]
[4.808574676513672, 1.6747214794158936, "The Number of Probe Conjunctions of the THEMIS Constellation Satellite Constellation is 154 hours."]
[6.6557536125183105, 5.123677730560303, "The Altimeter Observations of the Geosat Satellite is L. Miller, R. E. Cheney, B. C. Douglas."]
[6.771727561950684, 2.1016643047332764, "The Data Source of the IMERG Rainfall Estimation System is Integrated Multi-Satellite Retrievals for GPM (IMERG)."]
[10.552122116088867, -1.1115758419036865, "The Mass of the SRMSat Nanosatellite is 10.9 kg."]
[4.7971906661987305, 1.9728946685791016, "The Quantity Needed of the Amazonia-1 Satellite is At least 30."]
[8.813963890075684, 8.557303428649902, "The Incidence Angle Range of the Scatterometer Sensor is 0 to 48\u00ba."]
[12.141332626342773, 3.2599315643310547, "The Inclination of the KOMPSAT-3 Satellite is 98.13\u00ba."]
[7.821711540222168, -0.442632794380188, "The Establishment Date of the Yaguas National Park National Park is January 2018."]
[6.765700817108154, 0.004390767775475979, "The End of Life Date of the Tatiana-2 Satellite is 16 January 2010."]
[7.451362133026123, 3.639272451400757, "The Unknown of the EROS-B Satellite is Unknown."]
[5.016448020935059, -0.15299515426158905, "The Announcement Date of the OneWeb Satellite Constellation is January 15, 2015."]
[8.09121322631836, 4.00490665435791, "The Image Quality of the Pleiades 1B Satellite is Unknown."]
[4.6277995109558105, 5.882072925567627, "The RF Communications of the Spacecraft Satellite is 2234.4 MHz."]
[8.928321838378906, 7.3094658851623535, "The Accuracy of the Horizon sensor Sensor is 0.06\u00ba (3\u03c3)."]
[7.790185451507568, 1.7903904914855957, "The Observation Date of the ISEE-1 and ISEE-2 Satellites is 29 September 1978."]
[9.327593803405762, 10.034749984741211, "The Response of the APD Avalanche Photodiode is High-speed."]
[9.967775344848633, 9.539485931396484, "The Observation of the SAGE-II Satellite is Stratospheric ozone decline over the Antarctic."]
[6.462791919708252, 3.4570202827453613, "The Spare Satellite of the NSPO Satellite Provider is Provided in space depending on the launch vehicle capability."]
[10.59089469909668, 3.171773672103882, "The Entanglement Distance of the Satellite Satellite is Approximately 500 to 1,400 km."]
[6.584813117980957, -0.08041229099035263, "The Launch Date of the PSLV-C31/IRNSS-1E Satellite is January 20, 2016."]
[4.944915294647217, 3.7013399600982666, "The Functionality of the XB1 Bus is GN&C, EPS, Thermal, C&DH, RF Comm, and SSR."]
[5.178825855255127, 5.480546474456787, "The Spectrum of the Starlink and OneWeb Satellite Constellations is Ka-band."]
[5.7856059074401855, 3.0981273651123047, "The Manufacturer of the JUICE Satellite is Airbus."]
[6.603587627410889, 3.658829927444458, "The Electrical/Functional Allocation of the Sentinel-5P Satellite is Classical architecture."]
[11.794241905212402, 1.015779733657837, "The Launch Date of the Chang'e-1 Satellite is Oct. 24, 2007."]
[5.438597679138184, 5.608410835266113, "The Channels of the GPS Receiver Payload Module is 12."]
[8.757526397705078, 9.020480155944824, "The Polarization Sensitivity of the Grating Optical Component is Less than 20%."]
[7.733358860015869, 7.222201347351074, "The Type of the TEMPO Instrument is Spaceborne ultraviolet/visible light air quality spectrometer."]
[8.828965187072754, 3.5996882915496826, "The Formation Geometry of the TDX and TSX Satellites Satellites is Pursuit Monostatic Far formation."]
[8.6759672164917, 10.327543258666992, "The Number of Pixels of the Image Sensor Imaging is 4008 x 2672."]
[7.955319404602051, 10.22897720336914, "The Spatial Resolution at Nadir of the WV60 imager Imaging System is 0.50 m."]
[7.9980645179748535, 8.718106269836426, "The Point Spread Function Assessment of the OVIRS Spectrometer is Using collimated point and extended sources."]
[9.940287590026855, -0.7586904168128967, "The Structure Shape of the Baumanets-2 Microsatellite is Regular hexagon."]
[7.673178672790527, -0.4456774592399597, "The Launch Time of the Falcon 9 rocket Rocket is 06:17 Pacific Time (14:17 UTC) on 22 February 2018."]
[8.43400764465332, 9.737160682678223, "The Detector Pixel Size of the Instrument Satellite Instrument is 7 \u00b5m x 7 \u00b5m."]
[9.642443656921387, 6.068150043487549, "The Function of the ADCC Attitude Determination and Control Computer is Interfaces with the attitude sensors and actuators and runs the attitude control algorithms."]
[8.171029090881348, 9.862371444702148, "The Moving Mirror Unit Location of the MSASI Imager is Russia."]
[9.916678428649902, 7.38268518447876, "The Reflecting Performances Evaluation of the Cube Corner Reflectors (CCRs) Satellite Component is Through the analysis of the FFDP (Far Field Diffraction Pattern)."]
[6.564720153808594, -0.11653795093297958, "The Launch Date of the PSLV-C38 / Cartosat-2 Series Satellite Mission Satellite Mission is June 23, 2017."]
[8.012295722961426, 1.3519798517227173, "The Encounter Date of the Solar Orbiter Satellite is 4 June."]
[11.704394340515137, -1.1438511610031128, "The Mass of the Spacecraft Satellite is 447 kg."]
[7.687095642089844, 4.894709587097168, "The Tracking Method of the Aluminum Spheres Satellite is 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."]
[6.1862030029296875, 5.1477437019348145, "The SAR Bands of the SAR Satellite Satellite is X-band and L-band."]
[9.251486778259277, 5.409999847412109, "The Attitude Control of the QuickBird-2 Satellite is Low-vibration reaction wheels, three torque rods, and four hydrazine thrusters."]
[7.2888102531433105, -0.45552894473075867, "The Starlink Satellites Launch Date of the SpaceX Company is 4 March 2021."]
[5.991970062255859, 7.586857795715332, "The On-Orbit Performance of the ATMS Instrument is Superior to AMSU."]
[9.193602561950684, 4.1508378982543945, "The Size of the ROBUSTA picosatellite Satellite is 10 cm sidelength."]
[4.972404956817627, 4.496137619018555, "The Purpose of the Computer Ground Station Equipment is Provide the interface between COSMOS and the ground station for data management, monitor and possibly control the operations of the ground station."]
[7.205519199371338, 3.2347779273986816, "The Project of the Microwave Remote Sensing Small Satellite Satellite is Unknown."]
[5.715419769287109, 4.231584072113037, "The Population of the Dhaka City is Unknown."]
[7.796552658081055, 9.566668510437012, "The Number of Bands of the Optical Scanning Design Imaging Spectrometer is 45 bands (spectral campaigns)."]
[11.759855270385742, 4.793472766876221, "The Orbiting Black Hole Mass of the OJ 287 galaxy Galaxy is About 150 million times the Sun's mass."]
[2.0169143676757812, 4.0816168785095215, "The Power Source of the Spacecraft Module Satellite Module is Solar arrays and three nickel-hydrogen batteries."]
[7.0474162101745605, 4.543464183807373, "The Rendezvous Sensor Test Date of the ATV-5 Spacecraft is March 18, 2014."]
[12.13689136505127, 5.374850273132324, "The Composition of the Universe Cosmological Model is ~68% dark energy, ~27% dark matter, ~5% normal matter."]
[5.064479827880859, 8.70185661315918, "The Position Accuracy (RMS orbit) of the S-1 NTC Product is 5 cm (3D)."]
[7.862170219421387, 0.5760079026222229, "The Information Kit Date of the Columbus Space Module is January 2008."]
[7.471198081970215, 8.150148391723633, "The Test Mass Relative Displacement Measurement of the Laser Interferometer Measurement Device is High resolution."]
[5.911046504974365, 7.938109397888184, "The Resonant Frequency of the 3D Printed Polymers Material is Unknown."]
[10.488937377929688, -0.9803320169448853, "The Mass of the ChubuSat-1 Microsatellite is 50 kg."]
[6.867783546447754, 8.795151710510254, "The Required Accuracy of the Mie co-polar channel Channel is 50%."]
[7.085631370544434, 8.904888153076172, "The Swath Width of the Instrument Satellite Instrument is 35 km (nominal mode)."]
[8.179343223571777, 4.07329797744751, "The Resolution of the Pleiades-1A Satellite is 70 cm."]
[12.074109077453613, 2.236098527908325, "The Departure Date from Bennu of the OSIRIS-REx Spacecraft is 2021."]
[7.3382344245910645, 2.632181167602539, "The URL of the Chandra X-Ray Observatory Satellite is https://www.nasa.gov/mission_pages/chandra/."]
[9.469127655029297, 5.97886848449707, "The Bias Estimation of the Overall System System is Use of surface return."]
[7.553142547607422, 3.483511209487915, "The Sensor Complement of the ERS-2 Satellite is Unknown."]
[7.054765701293945, 0.00104735407512635, "The End of Life Date of the JERS-1 Satellite is 12 Oct 1998."]
[4.766308784484863, 1.8100663423538208, "The Access to Satellites of the Satellogic Satellite Constellation is 10 satellites."]
[7.572344779968262, 2.6569511890411377, "The Launch Year of the KOMPSAT-5 Satellite is 2013."]
[7.667144298553467, 3.9333901405334473, "The Ice Volume of the CryoSat Satellite is 1Gt corresponds to a volume of 1 km3."]
[6.873395919799805, 2.7178616523742676, "The | of the IASI-NG Satellite is IASI-NG (Next Generation),\u201d CNES, URL: http://smsc.cnes.fr/IASI-NG/index.htm."]
[6.926488399505615, 1.7842682600021362, "The Meeting Date of the Swarm Satellite Mission is May 3-5, 2006."]
[6.244476795196533, 7.418709754943848, "The Type of the DBCP Dual Babinet Compensator Pseudo-depolarizer is Pseudo-depolarizer."]
[9.439867973327637, 5.8046135902404785, "The Stabilization Accuracy of the Attitude Control System Control System is \u00b110\u00ba."]
[6.976783752441406, 1.144248366355896, "The Conference Date of the MTG Satellites Satellite is June 10 - 14, 2013."]
[9.748294830322266, 8.353392601013184, "The Truss Structure Material of the ALI Telescope is Invar."]
[7.327218055725098, 0.9762064218521118, "The System Development Date of the PRARE Satellite Observation System is April-Mei 1991."]
[6.364546298980713, 3.248520851135254, "The Project Philosophy of the ESEO Satellite is Maximize student participation in AIV activities and spacecraft operations."]
[7.749075889587402, 6.971322536468506, "The Unknown of the SPIRALE Space-based Early Warning Demonstrator is Unknown."]
[7.126449108123779, 0.8809935450553894, "The Review Date of the RHESSI Satellite is August 3, 2003."]
[7.379148006439209, 1.5114541053771973, "The Campaign of the Sentinel-1 Satellite is AgriSAR 2009."]
[9.452754974365234, 1.8621636629104614, "The Manoeuvre Frequency of the PARASOL Satellite is Nearly every month."]
[4.219004154205322, 2.466665744781494, "The Bus Assembly Type of the LunIR Satellite is 6U CubeSat."]
[8.87575626373291, 3.2842280864715576, "The Orbit of the CM1 Satellite is Low Earth Orbit (LEO)."]
[4.0376458168029785, 5.654225826263428, "The Bandwidth Savings of the PhiSat-1 Satellite is About 30%."]
[6.057224273681641, 3.0091402530670166, "The Satellite Navigation Company of the GMV-NSL Company is British."]
[7.139894008636475, 2.808516502380371, "The Development Schedule of the SWOT Satellite is Optimised."]
[8.454041481018066, 8.356755256652832, "The Authors of the Cosmic Ray Isotope Spectrometer Spectrometer is 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 Rose."]
[2.088984966278076, 4.813347816467285, "The Continuous Operation of the Fission Surface Power System Power System is At least 10 years."]
[10.367579460144043, 1.3309217691421509, "The Mean LTAN of the KOMPSAT-3A Satellite is 13:30 hours."]
[10.917182922363281, 7.199437141418457, "The Gas Purification of the LAXPCs X-ray Proportional Counters is Onboard purifier."]
[9.127917289733887, 10.680791854858398, "The Resolution of the T2 Zoom-in Camera is 5 km x 5 km."]
[9.138421058654785, 5.90194034576416, "The Attitude Control of the CeREs Satellite is Precision star tracker and two Sun pointers."]
[8.003046035766602, 3.4697508811950684, "The Components of the Sundancer Spacecraft is Life support systems, attitude control, three windows, on-orbit maneuverability, reboost, and de-orbit capability."]
[4.218653678894043, 2.7659218311309814, "The Download Speed of the Starlink Premium Satellite Internet Service is 150-500 Mbit/s."]
[6.895745277404785, 4.982443332672119, "The Measurement of the Copernicus Sentinel-5P Satellite is Nitrogen dioxide and other trace gases."]
[6.527123928070068, 5.063302516937256, "The Primary Instrument of the GEOSAT Satellite is GEOSAT Radar Altimeter (GRAS)."]
[8.113190650939941, 10.11575698852539, "The Function of the On-board Processor Data Processing Device is Real-time radiometric/geometric calibration and image compression for all imaging data."]
[11.74443531036377, 7.496466636657715, "The Enhancement of the Onboard Atomic Clocks Clocks is More precise."]
[7.154130935668945, 4.817437171936035, "The Function of the Docking Plate Rendezvous Suite Component is Provides a point of contact on the target for a magnetic capture system, and also provides an optically controlled surface for GNC."]
[7.027240753173828, -0.1056726947426796, "The End of Life Date of the ITUpSat-1 Satellite is 2030."]
[9.785357475280762, 1.6940641403198242, "The System Latency of the DSCOVR Satellite is No more than 5 minutes."]
[11.842347145080566, 1.0150765180587769, "The Orbit Entry Time of the Chang'e-5 Spacecraft is Around 21:45 UTC."]
[8.569803237915039, 8.25976276397705, "The Length of the Primary Sensor Sensor is 2 m."]
[9.51215934753418, 5.5113935470581055, "The Nominal Attitude of the AOCS Attitude and Orbit Control System is Nadir orientation."]
[6.726168155670166, 8.046232223510742, "The Function of the OMS Radiometer Radiometer is Deliver highly-accurate temperature, humidity, and precipitation data."]
[7.683409214019775, 0.45904257893562317, "The Launch Date of the Meteor-1-1 Satellite is 26.03.1969."]
[6.5673980712890625, 1.6382713317871094, "The Test Date of the Aireon Air Traffic Surveillance System is May 3, 2017."]
[5.097259521484375, 6.961172580718994, "The Center Frequency (GHz) of the Antenna Reflector is 37."]
[7.591008186340332, 9.249267578125, "The Image Scene Length of the Image scene length Spectrometer is 500 km."]
[9.269848823547363, 3.29057240486145, "The Initial Orbit Type of the Observatories Satellite is Highly elliptical orbits."]
[8.389232635498047, 9.144004821777344, "The Detection Range of the VIIRS Sensor is Green to near-infrared."]
[7.22637939453125, 7.137696743011475, "The Emissive Band Wavelengths of the VIIRS Satellite is 3.74, 11.45, 3.75, 4.05, 8.55, 10.76, and 12.01 \u00b5m."]
[6.840305805206299, 1.8621573448181152, "The Launch Date of the Kolibri-2000 Satellite is 20 March 2002."]
[7.932201862335205, 3.708286762237549, "The Geophysical Products of the Tandem-L Satellite is 26."]
[6.910107612609863, 7.025619983673096, "The Type of the GOES Sounder Instrument is Sounder."]
[7.964279651641846, 1.4107707738876343, "The Investigation Date of the ASGA Solar Cell Experiment Solar Cell Experiment is Dec. 05 - 09, 1994."]
[6.612453937530518, 8.778573989868164, "The Performance of the MTQ Instrument is 0-4 Nms."]
[7.21426248550415, 1.4070031642913818, "The Workshop Date of the COSMIC-II Satellite is October 21-22, 2010."]
[9.310308456420898, 6.3831377029418945, "The Personnel Needs of the Specialized Asset Trackers Tracking Device is Full time employees for monitoring."]
[9.511002540588379, 0.5965813398361206, "The Lifetime of the SmallGEO Satellite Platform is Up to 15 years."]
[4.932840824127197, 6.2396111488342285, "The Design of the Antenna Communication is Square array of tunable inverted F UHF antennas, and of one stacked circularly polarized L-band patch."]
[6.815948486328125, 4.2751617431640625, "The Objectives of the NISAR Satellite is Study solid Earth, ice masses, and ecosystems."]
[9.28475570678711, 10.183613777160645, "The Field of View of the Camera System Sensor is 15\u00b0 x 20.2\u00b0."]
[4.933027267456055, -3.2058260440826416, "The | of the G. J. Hurford Author is G. J. Hurford."]
[9.347505569458008, 6.450610160827637, "The | of the SI Star Tracker Star Tracker is SI star tracker."]
[7.0827412605285645, 1.2444396018981934, "The Public Listing Date of the Astrocast Satellite Operator is August 2021."]
[9.706050872802734, 2.1489744186401367, "The Maneuver Time ahead of CALIPSO of the CloudSat Satellite is 15 s."]
[7.028496265411377, 0.7599671483039856, "The Operation Status of the Genesis-2 Satellite is Nominal in 2011."]
[8.723048210144043, 3.694706678390503, "The Geographical Coverage of the Satellite Satellite is World coverage, with latitudes from 83\u00baN to 56\u00baS."]
[7.866698265075684, 5.620810031890869, "The Unbalance of the Land and Sea Contamination Signal Anomaly is 2%."]
[6.281981945037842, 0.5144312977790833, "The Launch Date of the CeREs CubeSat Satellite is 16 December 2018."]
[6.668468952178955, 2.8885650634765625, "The Type of the Dione Spacecraft is Prototype."]
[7.757561206817627, 4.952890396118164, "The 3-axis stabilization of the BEESAT-1 Satellite is Yes."]
[7.334042072296143, 7.870656490325928, "The Total Observation Time of the MOMS-2P Instrument is 25 hours."]
[7.386443138122559, 9.943191528320312, "The Spectral Bands of the Hyperion Imaging Spectrometer is 220."]
[4.005019187927246, 5.689964294433594, "The LISS-I Data Downlink Transfer Rate of the Satellite Satellite is 5.4 Mbit/s."]
[10.26158618927002, 2.9671382904052734, "The Orbit Altitude of the KySat-1 Satellite is 705 km."]
[9.274969100952148, 10.276825904846191, "The Focal Length of the spaceCam c4000 Video Camera is 600 mm."]
[7.775755882263184, 9.02902889251709, "The Operating Frequency of the Passive Microwave Spectrometer Spectrometer is Near the 118.75 GHz oxygen absorption line."]
[9.386082649230957, 3.6287665367126465, "The Status of the CanX-6/NTS Satellite is Retired, R&D."]
[9.098483085632324, 5.370931148529053, "The Function of the Attitude Control System Satellite Subsystem is Pointing of the satellite."]
[5.872251510620117, 8.13827133178711, "The Bandwidth (GHz) of the ICI-11 Radiometer is 10."]
[6.390230178833008, 0.7547330856323242, "The Launch Date of the RAVAN Satellite is Nov. 11, 2016."]
[10.337425231933594, 5.246275424957275, "The Xenon Pressure of the XTA Xenon Tank Assembly is 186 bar."]
[1.3955172300338745, 4.1624321937561035, "The Power Source of the Lander Spacecraft is Lithium ion battery."]
[6.767946243286133, 2.743626832962036, "The URL of the VRSS-1 Satellite is http://cn.cgwic.com/VRSS-1/english/focus.html#."]
[6.012478828430176, 3.8458669185638428, "The Purpose of the Transport Layer Tranche 1 Satellite Network is Support military communications, surveillance and tracking of enemy targets."]
[1.2432936429977417, 4.302454471588135, "The Battery Recharge of the Safe-mode System System is Possible while it is in operation."]
[8.443485260009766, 2.142759323120117, "The Current Location of the Voyager 2 Spacecraft is Interstellar space."]
[1.8303992748260498, 5.3635711669921875, "The Voltage of the Voltage 5 Digital is 3.8\u00b12%."]
[8.989198684692383, 5.2188544273376465, "The Attitude Stabilization Margin of the HIT-Sat Satellite is About 10\u00ba."]
[11.292036056518555, 6.541638374328613, "The Imaging Capability of the Chandra X-ray Telescope is Capturing intricate details in X-rays."]
[10.197738647460938, 2.995403289794922, "The Orbit (Altitude) of the Spacecraft Satellite is 628km."]
[9.46473503112793, 0.6106507778167725, "The Lifespan of the Satellite Satellite is 11/12 years."]
[7.39112663269043, 0.9651929140090942, "The Launch Date of the Sentinel-3B Satellite is Unknown."]
[7.231270790100098, 1.8959393501281738, "The Publication Date of the Shuttle Radar Topography Mission Satellite Mission is 2003."]
[7.813534736633301, 4.074225425720215, "The Bathymetry Measurement Depth of the ICESat-2 Satellite is 10 meters or more."]
[9.074736595153809, 10.792479515075684, "The Swath of the LISS-3 Camera is 140 km."]
[2.009655237197876, 3.8011584281921387, "The Solar Array of the Helios-2A and -2B Satellite is Two Gallium Arsenide panels and three silicon panels."]
[7.51381254196167, 2.0603816509246826, "The Operation Status of the ICIR IceCube Cloud\u2013Ice Radiometer is Normal."]
[10.04759693145752, 1.559288501739502, "The Period of the Satellite Orbit is 103 minutes."]
[9.033034324645996, 5.288602828979492, "The Roll/Pitch Pointing Accuracy of the Attitude Control Satellite Subsystem is \u00b10.3\u00ba."]
[9.423453330993652, 5.762639999389648, "The Quantity of the Reaction Wheels AOCS Actuators is 4."]
[6.900402545928955, 0.38885781168937683, "The End of Operations Date of the GEOS-2 Satellite is January 1970."]
[7.49611234664917, 1.1291052103042603, "The Imaging Date of the MRO Mars Reconnaissance Orbiter is Nov. 1, 2016."]
[7.636270523071289, 5.018074035644531, "The Observation Modes of the Trace Gas Orbiter Satellite is Solar occultation, Nadir, Nightside."]
[6.210042953491211, 2.942584276199341, "The Managing Institution of the Carruthers Geocorona Observatory Spacecraft is University of California, Berkeley (UC Berkeley)."]
[3.779262065887451, 6.172698020935059, "The GEO-to-ground Communication Link Speed of the Optical Ground Station Ground Station is 2.8 Gbit/s."]
[2.2110772132873535, 1.733612298965454, "The CCSDS ID of the GSAT-0205 Satellite is 265."]
[4.000372886657715, 2.3438308238983154, "The Size of the EXOpod CubeSat deployers Deployer is 12U and 16U."]
[11.583192825317383, 4.398975372314453, "The Rotation Period of the Zeta Puppis Star is 1.78 d."]
[9.21831226348877, 10.240961074829102, "The Field of View of the NAC Narrow-Angle Camera is Smaller portions of the landscape."]
[7.332263469696045, 7.632439136505127, "The Operational Modes of the MOMA Instrument is 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 inter."]
[6.934478282928467, 0.5396592617034912, "The Launch Date of the Resurs-P1 Satellite is June 2013."]
[4.714066505432129, 5.5451459884643555, "The Radio Frequency of the PhoneSat-2.5 Satellite is S-band."]
[8.464696884155273, 3.7016241550445557, "The Torque Margin of the RDA Deployment System is Not provided."]
[1.2525782585144043, 4.150018692016602, "The Battery Capacity of the NSat Satellite is 5.2 Ah."]
[5.126427173614502, 1.7335344552993774, "The Number of CubeSats of the PSLV-C37 Launch Vehicle is 88."]
[8.896208763122559, 7.063990592956543, "The Quantity of the Temperature Sensors Sensors is 2."]
[11.635575294494629, 4.826687335968018, "The Surrounding Gas Temperature of the Black Holes Astronomical Object is More than a million degrees."]
[8.819445610046387, 10.411748886108398, "The Seeing Diameter of the Acquisition and Tracking Camera (ATC) Camera is 1 arcsec = 65 \u00b5m."]
[8.273162841796875, 10.518424987792969, "The Power Dissipation of the Focal Plane Detector is Less than 1 watt."]
[9.2160005569458, 1.4563934803009033, "The Mission Duration of the Euclid Space Telescope is 6 years."]
[9.890790939331055, 6.652260780334473, "The Equipment Temperatures of the Satellite Spacecraft is Stable."]
[7.017344951629639, -0.02755826897919178, "The End of Life Date of the ZACUBE-2 Satellite is 27 Dec 2022."]
[8.075567245483398, 4.541023254394531, "The Mission of the CuSP Satellite is Measure particles and magnetic fields in space, testing the practicality for a network of stations to monitor space weather."]
[5.332162380218506, 10.375584602355957, "The End of Life Date of the ISS:LIS Lightning Imaging Sensor is 30 Sep 2023."]
[7.748034477233887, 1.4102270603179932, "The Release Date of the SCI Spacecraft is April 5."]
[5.667503356933594, 3.6064844131469727, "The Accommodation Location of the Hosted Military Payload Satellite Payload is South Panel."]
[8.763297080993652, 5.315528392791748, "The Pointing Precision of the HY-2A Satellite is < 0.1\u00ba in pitch, roll and yaw."]
[3.1415188312530518, 6.80419397354126, "The Output Power of the CanX-2 S-band Transmitter/Transceiver is 27 dBm."]
[11.784286499023438, -0.9097599983215332, "The Mass of Payloads of the FAST Program Technology Demonstration Program is Starting at just 1 kg."]
[8.438708305358887, 0.8414772748947144, "The Observation Frequency of the Megha-Tropiques Satellite is Up to 6 overpasses per day."]
[6.462217330932617, 4.316097259521484, "The Sensor Types of the Pico Dragon CubeSat is Gather data of the temperature, voltage and current of the satellite systems."]
[7.074490070343018, 3.2638072967529297, "The Utilization Plan of the KIBO Payload is Unknown."]
[11.342808723449707, 1.5441919565200806, "The Closest Distance to Stone of the Yutu-2 Rover is 1.2 meters."]
[4.434126377105713, 2.7452054023742676, "The NN Frameworks of the Ubotica CogniSAT-XE1TM CubeSat Board Satellite Device is TensorFlow, PyTorch, Caffe."]
[7.4143853187561035, 1.491829514503479, "The Operation Completion Date of the KIKU No. 8 Satellite is January 11, 2017."]
[6.935652732849121, 1.0150561332702637, "The Magnetometer Installation Date of the Iridium Constellation Satellites Satellite is February 1999."]
[10.858722686767578, 3.727102756500244, "The Yearly Trajectory Deflection of the Solar System Celestial System is Around 115 km."]
[9.965079307556152, -0.7271389961242676, "The Dimensions of the Microsatellite Satellite is 52 cm x 52 cm x 45 cm."]
[6.061509132385254, 9.678804397583008, "The Mass of the SESAME Experiments is 1.8 kg."]
[9.427546501159668, 9.053092956542969, "The Area of the Effective Collecting Area Telescope is 767.93 cm2."]
[4.9574055671691895, 3.651021718978882, "The Components of the Merlin Satellite Device is Two `card-frame' modules, printed circuit boards, lid, base, EMC screen."]
[4.103256702423096, 5.269021034240723, "The Modes of the OCM Data Transmission System is Real-time and playback."]
[5.293515682220459, 4.706989288330078, "The Proximity to Sentinel-3A of the CDN2 Site Ground Station is 100 m east."]
[6.590548038482666, 3.5477893352508545, "The Mission Type of the FormoSat-1 Satellite is EO."]
[7.044465065002441, 0.7876447439193726, "The Launch Date of the MANTIS Earth Observation Satellite is 11 November 2023."]
[10.12328052520752, 3.0297186374664307, "The Altitude of the SAOCOM-1A and -1B Satellites is 619.6 km."]
[11.578957557678223, -0.8259465098381042, "The Bus Mass of the Spacecraft Bus (Avionics Module=AM) Satellite is 180 kg."]
[8.03141975402832, 3.8052585124969482, "The Unknown of the Pleiades Satellite is Unknown."]
[3.6355600357055664, 4.447624683380127, "The Function of the Power Distributor Unit (PDU) Subsystem is 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."]
[5.201785087585449, 4.698416233062744, "The Downlink Function of the Argos System Satellite Communication System is Acknowledge uplink messages, increase system capacity, transmit broadcasting messages, modulate message length or repetition period."]
[6.330773830413818, 11.888859748840332, "The Absolute / Relative Scale Factors of the Three-axis diagonal gradiometer Gradiometer is 10 -3  / 10 -5."]
[6.57763147354126, 8.542876243591309, "The Swath Width of the MESSR Radiometer is 100 km."]
[6.19696044921875, 7.7786431312561035, "The Polarization of the ICI-9 Radiometer is V."]
[11.874760627746582, 4.579672813415527, "The Authors of the The Global Dynamical Atlas of the Milky Way Mergers Research Paper is 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."]
[10.571414947509766, 7.566507816314697, "The Trays Material of the QSP-1 Satellite is Aluminum."]
[8.583778381347656, 7.900704383850098, "The Detectors Quantity of the REM Radiation Environment Monitor is 2."]
[4.082504749298096, 4.853184700012207, "The Redundant Chain of the TMCU Subsystem is QPSK-B / ATOP-B."]
[4.027839183807373, 1.203394889831543, "The Type of the Artemis-I Mission is Non-EO."]
[8.057204246520996, 2.66567325592041, "The Launch Date of the TerraSAR-X Satellite is June 15, 2007."]
[11.092828750610352, 2.5105018615722656, "The Final Impact Velocity of the Schiaparelli Lander is Just under 11 km/h."]
[4.9705047607421875, 1.9915008544921875, "The Number of CubeSats of the EM-1 Mission is 13."]
[11.298796653747559, 3.674239158630371, "The Insight of the Comets Celestial Bodies is Planetary construction yard at these early times."]
[6.348522186279297, 9.974516868591309, "The Camera Mass of the Pushbroom imager Optics is 13 kg."]
[9.092693328857422, -0.5294658541679382, "The Launch Vehicle of the Jugnu Nanosatellite is ISRO PSLV launcher."]
[9.1939115524292, 4.131239891052246, "The Dimensions of the INTEGRAL Satellite is (5 x 2.8 x 3.2) m."]
[5.6700239181518555, 9.289021492004395, "The Power of the PEACE Instrument is 5.0 W."]
[7.12596321105957, 8.843729972839355, "The IFOV/line (pixels/scan line) of the VIRR Visible and Infrared Radiometer is 2048."]
[10.606926918029785, 2.7720584869384766, "The Orbit Shift Distance of the GomX-4B Satellite is 300 km."]
[4.394535541534424, 4.015739917755127, "The Power Delivery of the Spacecraft Plug-n-Play Avionics (SPA) Standards is Separate 28V power delivery."]
[12.146748542785645, 3.3074214458465576, "The Orbit Inclination of the Genesis-2 Satellite is 64.5\u00ba."]
[6.4386820793151855, 8.504534721374512, "The Spatial Resolution of the MWRI Microwave Radiometer Imager is 15-85 km."]
[17.728321075439453, 7.162668228149414, "The J2000 right ascension (deg) of the B1813-140 Pulsar is 274.006."]
[7.270221710205078, 9.528139114379883, "The Manufacturer of the MSS Multispectral Scanner is SBRC (Santa Barbara Research Center) of Hughes."]
[5.694821834564209, 3.2962281703948975, "The Manufacturer of the Drag Augmentation Device Satellite Component is Ryokeiso CO., Ltd.."]
[7.7985310554504395, 2.836644172668457, "The Landing Site of the Capsule Sample Container is Southern Australian desert."]
[9.772174835205078, 1.7967307567596436, "The Orbit (number of cycles/day) of the Spacecraft Satellite is 15 3/14."]
[7.642612457275391, 2.197763204574585, "The Mission of the Mars Hope probe Spacecraft is Orbit Mars."]
[7.571539402008057, 7.603891372680664, "The Operation Mode of the Radiometer Sensor is Integrate-while-scanning."]
[8.025412559509277, 5.200579643249512, "The Accuracy of the SubWave+ Underground Geolocation System is Few meters."]
[7.395112991333008, -0.21187865734100342, "The Scheduled Flight Date of the HTV-7 Cargo Vessel is Sept. 10."]
[4.488896369934082, 6.3077073097229, "The Bands of the High Gain Antenna Communication System is Ka-band and S-band."]
[7.574740409851074, -0.4680420458316803, "The Launch Date of the Falcon 9 Rocket is 21 April 2022."]
[7.470028877258301, 3.4635772705078125, "The Sensor Complement of the Satellite Spacecraft is Unknown."]
[11.165189743041992, 6.554418563842773, "The Post-flight Inspection Date of the IXV Spacecraft is Autumn 2015."]
[7.399444580078125, 1.0195831060409546, "The Opening Date of the ESA Facility Facility is 9 November 2018."]
[7.263119220733643, 2.3108346462249756, "The Launch Year of the Carbonite-2 Satellite is 2018."]
[9.292121887207031, 3.0796878337860107, "The Moon Orbit of the Chandrayaan-2 Spacecraft is 100 km circular polar orbit."]
[3.3471508026123047, 5.630252361297607, "The Data Packet Length of the Science Data Interface Interface is 1024 bytes."]
[7.725815773010254, 13.578132629394531, "The Resolution \u0394\u03bb (0.05\u00ba slit) of the SPIM4 Spectrometer is 2.1 nm."]
[3.268521547317505, 5.904855728149414, "The Transaction Time of the CPT Data Processing System is Allocated time."]
[1.8584126234054565, 4.850395202636719, "The Current-Limiting Resistor of the PPPT Circuit is Unknown."]
[11.132369041442871, 2.499332904815674, "The Descent Duration of the Schiaparelli Lander is Just under six minutes."]
[11.10954475402832, 6.99794340133667, "The Potential Applications of the STP-H6-XCOM X-ray communications system is Deep space probes, communicating with hypersonic vehicles."]
[11.771722793579102, 3.4526662826538086, "The Orbital Plane Tilt of the Orbital Phase 1 Orbit is 60\u00ba away from the Sun direction."]
[4.1282196044921875, 5.101594924926758, "The Redundancy of the CFI Signal Generator Chains Signal Generator is Two chains."]
[7.776503086090088, 0.31788522005081177, "The Launch Date of the Crew-1 Mission is Oct. 31."]
[1.015945315361023, 4.231329917907715, "The Battery Capacity of the MTM Transfer Module is 12 Ah."]
[6.39802885055542, 0.6479483842849731, "The Launch Date of the GHGSat's Second Satellite Satellite is August."]
[6.037225723266602, 6.359722137451172, "The Nominal Looking Direction of the SAR Synthetic Aperture Radar is Right."]
[8.720243453979492, 10.599396705627441, "The Data Rate of the Camera Imaging Device is 336 Mbit/s."]
[7.794862270355225, 1.3576736450195312, "The Date of the Bristol Abloom Natural Event is 4 June 2022."]
[9.400811195373535, 11.494014739990234, "The Effective FOV of the Channel 2 Sensor is 52 km x 16 km."]
[6.8755340576171875, 0.8939287662506104, "The Presentation Date of the TeLEOS-1 Satellite is Feb. 11-13, 2015."]
[7.877695083618164, 8.823655128479004, "The Imaging Wavelength of the Solar Orbiter Satellite is 17 nm."]
[5.724920749664307, 3.513761043548584, "The Operator of the CSSS Canadian Space Surveillance System is DND."]
[6.224353313446045, 9.671622276306152, "The Weight of the CHRIS Imaging Spectrometer is 14 kg."]
[5.67337703704834, 4.13925313949585, "The Support Level of the Test Station Testing Equipment is Subsystem to SV (Space Vehicle) I&T (Integration and Test) level."]
[6.377762794494629, 9.21505355834961, "The Housing Dimensions of the MuREM Radiation Monitor is 10 cm x 10 cm x 4.5 cm."]
[3.862046957015991, 2.305198907852173, "The Side Length of the ESTCube-1 & -2 CubeSat is 10 cm."]
[3.6929922103881836, 4.704911231994629, "The Timers of the MCU Microcontroller Unit is Three 16-bit timers."]
[6.694927215576172, 9.779078483581543, "The Instrument Mass of the Hyperion Imaging Spectrometer is 49 kg."]
[10.486137390136719, -1.0049355030059814, "The Mass of the Carbonite-2 Microsatellite is ~100 kg."]
[10.054073333740234, 5.105109691619873, "The Attitude Control Thrusters of the INSAT-2A/2B Satellite is 16."]
[9.884024620056152, 1.473167061805725, "The Payload Interaction Window of the SOC Satellite Operations Center is Up to 20 minutes before each contact."]
[6.968094348907471, 8.45655345916748, "The Field of View of the LI Instrument is 16\u00ba \u00d8 shifted northward or 84% of visible Earth disk."]
[7.0548295974731445, 4.371217250823975, "The Measurement Domain of the LAICE Satellite is Atmosphere."]
[8.339620590209961, 8.495111465454102, "The Operation of the OCO-2 Spectrometer is Employ a diffraction grating to separate the inbound light energy into a spectrum of multiple component colors."]
[5.988266468048096, 9.582779884338379, "The Mass of the CEASE-2 Instrument is 1.3 kg."]
[7.771341323852539, 2.09496808052063, "The Publication Year of the Observation of the Earth and Its Environment Documentation is 2002."]
[6.00056791305542, 4.837240695953369, "The Launch of the OSIRISv3 System is Unknown."]
[8.96200180053711, 2.7285850048065186, "The PDR Date of the GCOM-W1 Satellite is March 2008."]
[11.45722484588623, -1.3250374794006348, "The Mass of the NorSat-2 Satellite is 16 kg."]
[9.876810073852539, -0.7513782978057861, "The Size of the ASAP Nanosatellite is 175 x 245 x 100 mm3."]
[9.102368354797363, 8.286486625671387, "The Housing Location of the SMA Scan Mechanism Assembly is First optic within the telescope optical assembly."]
[5.474157333374023, 1.7766762971878052, "The Constellation Type of the OptiSAR\u2122 Constellation Satellite Constellation is Paired, tandem configuration."]
[8.853286743164062, 1.7837449312210083, "The Image Capture Date of the BepiColombo Spacecraft is 10 April."]
[8.110754013061523, 3.5898332595825195, "The Characteristic Wavelength of the Tandem-L Satellite is 236 mm."]
[9.94075870513916, 3.9889655113220215, "The Full Deployment Time of the NanoSail-D2 Solar Sail is Within just five seconds."]
[8.277591705322266, 3.082501173019409, "The Bistatic Phase of the TanDEM-X Satellite is March 2015 to September 2015."]
[7.705705165863037, 8.632305145263672, "The Dust Measurement Concentration of the UVS Instrument is As low as 10-4 per cc."]
[5.03696870803833, 2.2016148567199707, "The Team Members of the HORYU-4 Satellite is More than 30."]
[7.5996832847595215, 1.6778942346572876, "The Duration of the Drift Ice Season Natural Phenomenon is January to March."]
[11.187470436096191, 9.340871810913086, "The Data Collection Start of the ERBE Experiment is 1984."]
[9.868162155151367, 4.109950065612793, "The Delta-V Capacity of the Bus Satellite Component is More than 154 m/s."]
[9.564241409301758, 7.744933128356934, "The Ion Energy Channels of the EPE Energetic Particle Experiment is 0.05 - 0.20 MeV, 2.1 - 4.5 MeV."]
[7.69985294342041, 3.9266819953918457, "The Imaging Capacity of the KazEOSat-2 Satellite is Up to 1,000,000 km2 per day."]
[12.129746437072754, 3.2681779861450195, "The Orbit Inclination of the ResourceSat-2 Satellite is 98\u00ba."]
[9.033618927001953, 8.761849403381348, "The Sensitivity of the THD Horizon Detector is 1,500 V/W."]
[4.304474353790283, 6.971526622772217, "The Data collection rate of the Millimeterwave receiver Receiver is 0.23 \u2013 2.53 kbit/s."]
[5.3911452293396, 4.886519908905029, "The Downlink Method of the Sentinel-1 Satellite is Laser Communication Terminal unit allowing downlink of recorded data via the EDRS."]
[8.6270112991333, 10.315022468566895, "The Image Captures of the C3D2 Payload is >100."]
[8.058504104614258, 5.219505310058594, "The Objectives of the S 321 Satellite is Measurement of the pitch-angle distribution for electrons (20-300 keV) and protons (20 keV - 3 MeV)."]
[9.334319114685059, 0.5728002786636353, "The Design Life of the EO-1 Satellite is 2 years."]
[9.883031845092773, -0.7012856602668762, "The Structure Type of the Microsatellite Satellite is Hexagonal prism."]
[3.7587244510650635, 6.14812707901001, "The PPM Slot Rates of the Optical Downlink Communication System is 0.311 \u2013 5 GHz."]
[6.874794960021973, 10.02535629272461, "The Bandwidth of the Band 6 Spectral Band is 675-685 nm."]
[3.7359018325805664, 6.245728015899658, "The Uplink Data Rate of the Telemetry, Tracking, and Command (TT&C) Communication is 4 kbits/s."]
[7.335775852203369, 10.117071151733398, "The Imaged Region of the HyperScout Imaging System is Scotland."]
[11.18410587310791, 4.780235290527344, "The Type of the Orphan Cloud Phenomenon is Isolated cloud in a galaxy cluster."]
[10.507572174072266, 6.155846118927002, "The Instrument of the RHESSI Satellite is X-ray and \u03b3-ray imaging spectroscopy."]
[5.724492073059082, 6.831864833831787, "The Operating Wavelength of the IRS Interferometric Radar System is Millimeter."]
[7.897283554077148, 9.779399871826172, "The Spectral Range of the Instrument Spectral Imager is 5.71-8.26 \u00b5m."]
[6.458707809448242, 7.3214640617370605, "The Polarization of the Stripmap Imaging Mode is Single or dual."]
[9.31210708618164, 4.238719940185547, "The Volume of the Spacecraft Satellite is 20 cm x 20 cm x 20 cm."]
[6.81410026550293, 3.8519446849823, "The Common Ground System of the JPSS and DWSS Satellites is Yes."]
[4.8552446365356445, 4.988863468170166, "The Required Processing System of the UHRIT Data Dissemination System is Processing system including DVB-S2 equipment."]
[6.634512424468994, 3.6230740547180176, "The Agency of the Sich-2 Satellite is NSAU."]
[11.182581901550293, 6.748742580413818, "The Capabilities of the X-ray Navigation Navigation System is Position, attitude, and timekeeping."]
[8.521903038024902, 2.557102918624878, "The Number of Near-Perigee and Apogee Maneuvers of the ARTEMIS Spacecraft is 5 near-perigee and 3 apogee maneuvers."]
[7.219164848327637, 6.883982181549072, "The Operation Timeframe of the AaSI Instrument is June-August growing season."]
[7.673803329467773, 1.0943583250045776, "The Image Capture Date of the Copernicus Sentinel-3 Satellite is 3 January."]
[3.859191417694092, 6.236804008483887, "The Data Streams of the Baseband Processor Processor is Two 110 Mbit/s TDMA/DAMA data streams assignable in increments of 64 kbit/s."]
[3.8744728565216064, 5.517941474914551, "The Internet Access Speed of the EUTELSAT KONNECT Satellite is Up to 100 Mbit/s."]
[8.00290298461914, 4.4328179359436035, "The Field of Regard of the Resurs-P1 Imaging Satellite is 950 km."]
[6.133181095123291, 8.152332305908203, "The Channel Frequency of the MHS Instrument is 183.311 GHz."]
[8.095242500305176, 2.305144786834717, "The Mission Start Date of the ARTEMIS Satellite is 2010."]
[4.801810264587402, 7.209507942199707, "The Wavelength of the X-band Band is 2.9 cm."]
[7.022779941558838, 1.277716875076294, "The Presentation Date of the ERG Satellite Satellite is June 5-12, 2011."]
[12.936264991760254, 4.831325531005859, "The Observation Location of the IBEX Satellite is About 30 degrees south of the interstellar upwind direction."]
[7.804385662078857, 2.264241933822632, "The Publisher of the Observation of the Earth and Its Environment Documentation is Springer Verlag."]
[8.54742431640625, 4.639595031738281, "The Objective of the Cluster Satellite Mission is Observation of key interaction processes between two cosmic plasmas."]
[11.332162857055664, 1.556169867515564, "The Accumulated Travel of the Yutu-2 Rover is 178.9 meters."]
[8.64383602142334, 8.33106803894043, "The Ultraviolet Spectrograph of the Juno Spacecraft is Instrument."]
[8.496959686279297, 6.424286365509033, "The Measurement Data of the Solar Orbiter Satellite is Solar wind, coronal mass ejection."]
[5.006355285644531, 5.014701843261719, "The Antenna Types of the Ground Station Ground Station is S-band, C-band."]
[7.490368843078613, 2.8916096687316895, "The Observation Location of the RainCube Satellite is Sierra Madre Oriental, near Monterrey, Mexico."]
[8.186145782470703, 10.112804412841797, "The IFOV of the SGLI Imager is 250 m."]
[6.8296589851379395, 8.531214714050293, "The Main Beam 3 dB Footprint of the ICIR Radiometer is 10 \u2013 20 km."]
[4.644955635070801, 9.05390739440918, "The Launch Date of the InSight Mars Lander Mars Lander is May 5, 2018."]
[10.088692665100098, 4.530157089233398, "The Heat Shield Diameter of the Orion Spacecraft is 5 m."]
[5.052032470703125, 6.700109958648682, "The Isolation Between Ports of the Array Radiator Antenna is Better than -22 dB."]
[6.058898448944092, 4.913152694702148, "The Purpose of the OSIRIS Device is Attitude control system and satellite performance testing."]
[6.930602550506592, 0.7936360239982605, "The Functional Demonstration Date of the OHB Telecommunications Satellite Satellite is June 2, 2017."]
[5.348913669586182, 6.513319969177246, "The Pulse Repetition Frequency (PRF) of the PR Phased Array System is 2776 Hz."]
[6.598540782928467, 4.553155422210693, "The Instrument Type of the CHORUS Satellite Constellation is Imaging microwave radars."]
[8.649676322937012, 10.73724365234375, "The Power Consumption of the STL-11000M SBIG Camera CCD Camera is Low."]
[4.463319778442383, 6.35732889175415, "The Components of the Ka-band payload Communication System is Multi beam antenna, on-board switching transponder subsystem."]
[5.275362491607666, 4.770545482635498, "The Proximity to Sentinel-3B of the CDN2 Site Ground Station is 300 m west."]
[8.456467628479004, 8.950719833374023, "The Field of View of the Spectrometer Instrument is 3.5 x 3.5 to 7 arcsec x 7 arcsec."]
[1.7364227771759033, 4.286637306213379, "The Solar Array Size of the EPS Electrical Power Subsystem is 5.661 m 2."]
[8.423568725585938, 8.117146492004395, "The Manufacturer of the UL 03041 pixel ULIS microbolometer array Microbolometer Array is ULIS."]
[3.8859317302703857, 5.72525691986084, "The Data Downlink Speed of the Payload Satellite Payload is 128/256 kbit/s."]
[7.7983622550964355, 6.480884552001953, "The Radiometric Stability of the Satellite Sensors Instrument is Crucial."]
[7.139937877655029, 5.313837051391602, "The Characterized Processes of the Models of the Oceans and Land Biosphere Earth Science is Photosynthesis, respiration, nutrient uptake and transport, fire, and chemical cycling, as well as fossil fuel inventories."]
[6.736597061157227, 4.663714408874512, "The Imaging Frequency Band of the RADARSAT-2 Satellite is C."]
[5.716433525085449, 9.194253921508789, "The Power of the LIMS Instrument is 27 W."]
[8.728485107421875, 5.311652660369873, "The Attitude Knowledge Error of the Spacecraft Satellite is 5 arcsec (95%)."]
[10.639034271240234, -1.7005778551101685, "The Cargo Storage of the HTV-8 Spacecraft is 3.5 metric tons in the PLC, 1.9 metric tons in the ULC."]
[7.7459492683410645, 2.287551164627075, "The URL of the Observation of the Earth and Its Environment: Survey of Missions and Sensors Documentation is http://link.springer.com/article/10.1007/s12273-015-0241-8."]
[3.1980581283569336, 5.426202774047852, "The Number of Supported Devices of the SSRNI Data Acquisition and Registration System is Up to 24."]
[1.1576215028762817, 4.150321960449219, "The Battery Type of the Canopus Pipper Satellite is Molicel 18650 Li-ion batteries."]
[11.466452598571777, -0.8426958322525024, "The Mass of the Nauka module Module is 20 tons."]
[10.055387496948242, 3.0400054454803467, "The Radius of the Orbital Phase 1 Orbit is Ca. 29 km."]
[5.51542854309082, 7.0666656494140625, "The Power of the RA-1 Antenna Antenna is \u2264 134.5 W."]
[6.6621317863464355, 8.479294776916504, "The Swath of the MERSI-RM Radiometer is 2900 km."]
[4.778056621551514, 0.8672969937324524, "The Cost per Satellite of the Satellogic Satellite Constellation is $2 million dollars per year."]
[9.255098342895508, 8.178709030151367, "The Temperature of the Optics Subsystem Camera Subsystem is 20 \u00b13\u00baC."]
[6.582058429718018, 0.6833127737045288, "The Deorbit Date of the ICESat Satellite is Sept. 2, 2010."]
[9.073342323303223, 9.337811470031738, "The Pixel Size of the Telescope Optical Instrument is 24 x 24 \u00b5m."]
[8.087930679321289, 5.182705879211426, "The Objectives of the S 329 Satellite is Measurement of DC electric field grad |B|."]
[7.656155586242676, 6.751094341278076, "The Sensor Complement of the MMO Spacecraft is MERMAG, MPPE, PWI, MSASI, MDM."]
[10.582822799682617, -1.331112027168274, "The Cargo Capacity of the Tianzhou-2 Cargo Spacecraft is 4.69 tons."]
[8.58890438079834, 5.222512245178223, "The Pointing Precision of the FY-3 series spacecraft Satellite is 50 m on the ground."]
[5.773458480834961, 3.037933349609375, "The Purpose of the Hiber Satellite Constellation is Track and monitor machines and devices for a wide range of IoT solutions in some of the world's hardest-to-reach places."]
[3.3362393379211426, 5.257908821105957, "The Image Data Storage of the ISERV Satellite is Compact Flash memory, WORF laptop hard disk."]
[7.660099029541016, 8.745919227600098, "The Velocity Resolution of the Spectrometer Instrument is ~100 km/s."]
[5.415014743804932, 4.9325032234191895, "The Additional Downlink Subsystem of the Sentinel-1, -2 Satellites is Laser Communication Terminal (LCT)."]
[7.5260090827941895, 9.769301414489746, "The Frequency of the VNIR Band is 283 THz."]
[10.863968849182129, 2.0079727172851562, "The Mean Anomaly at Epoch of the Swarm-C (Charlie) Satellite is N/A."]
[6.337489128112793, 3.7777059078216553, "The Data Processing Challenge of the INCUS Satellite is Technical challenge that\u2019s really fun."]
[8.540574073791504, 2.178861141204834, "The Arrival Date of the Parker Solar Probe Satellite is April 28, 2021."]
[11.602185249328613, 1.9012452363967896, "The Science Levels of the MASCOT Science Landing Package is Context Science."]
[8.988895416259766, 7.040109157562256, "The Objectives of the WISPR Instrument is 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 ."]
[8.577590942382812, 9.80700969696045, "The Components of the Optical Payload Payload is Wide-angle camera (primary) and a telescopic camera (secondary)."]
[8.041619300842285, 1.4482581615447998, "The Observation Date of the Solar-B/Hinode spacecraft Spacecraft is February 6, 2018."]
[7.806648254394531, 5.989107131958008, "The Calibration Method of the TRUTHS Satellite is Pre-flight calibration/characterization and during the commissioning phase."]
[6.0985894203186035, 3.6912176609039307, "The Minimum Required Functionality of the Development Approach Satellite Instrument Development is Kept strictly to the minimum required functionality to fulfill the science goal."]
[7.4820098876953125, 7.450460910797119, "The Algorithm Improvement of the OMI Satellite is OMI O2\u2013O2 operational cloud algorithm."]
[4.816830158233643, 0.8642676472663879, "The Procurements Cost of the Galileo Second Generation (G2) Satellite Constellation is Up to approximately 950 million euros."]
[2.0467326641082764, 4.0523200035095215, "The Power Source of the Lander Spacecraft is Body mounted solar panels."]
[7.849682331085205, -0.5741142630577087, "The URL of the SpaceX CRS-6 Mission is http://blogs.nasa.gov/spacex/wp-content/uploads/sites/227/2015/04/SpaceX_CRS-6_Mission_Overview.pdf."]
[9.669931411743164, 8.725995063781738, "The Unknown of the Metal mirror TMA Telescope is Unknown."]
[8.176600456237793, 5.649489879608154, "The Leading Noise Terms of the Satellite Spacecraft is Self gravitation to the satellite."]
[7.780996799468994, 8.965958595275879, "The Performance Range of the UV-2 Spectrometer is 310 - 365 nm."]
[4.738789081573486, 1.7931071519851685, "The Constellation Number of the PlanetiQ satellites Weather Satellites is 20."]
[8.431565284729004, -0.01640612818300724, "The Firing Duration of the CUS Cryogenic Upper Stage is Approximately 720 seconds."]
[12.043489456176758, 2.2591335773468018, "The Mission Status of the OSIRIS-REx Spacecraft is One Step Closer to Touching Asteroid Bennu."]
[6.246184349060059, 2.011582374572754, "The Conference Date of the TacSat-4 Satellite is Aug. 11-14, 2008."]
[8.29603099822998, 8.674725532531738, "The Funding of the NIRSpec Near-Infrared multi-object Spectrograph is ESA."]
[9.061259269714355, 5.038027763366699, "The Attitude Orientation of the ICESat Satellite is -ZG axis is 0.3\u00ba from geodetic nadir."]
[4.914153099060059, 7.450573444366455, "The 205 kbit/s for each sensor (uncompressed case) of the Data Rate Sensor is Data rate 205 kbit/s for each sensor (uncompressed case)."]
[9.542285919189453, 6.5323920249938965, "The Manufacturer of the Maeva Hinges Deployment Mechanism is CNES."]
[3.560962200164795, 2.291588306427002, "The Size of the PolyITAN-2-SAU Satellite is 2U."]
[5.258209705352783, 6.308844089508057, "The Configuration of the VDES Antenna Antenna is Stowed and deployed."]
[6.084869861602783, 11.24538516998291, "The Approx. peak sensitivity altitude of the Channel 3 Sensor is Unknown."]
[8.960052490234375, 10.36215591430664, "The Image Capture Method of the WAC Camera is Moderate resolution images using filters."]
[6.897339344024658, 7.320173740386963, "The Manufacturer of the NIRSpec Instrument is Astrium GmbH."]
[3.828850269317627, 6.389407157897949, "The Data Rate of the Astrodev Lithium 2 Radio RF Communication Device is 9.6 kbit/s."]
[5.908931255340576, 3.307063579559326, "The Manufacturer of the Gaia Space Telescope is ESA."]
[6.890881538391113, 9.17349624633789, "The Azimuth Width of the Transmitting Beam of the UF Mode Observation Mode is Broadened 1.7 times."]
[8.362531661987305, 3.6258528232574463, "The Mission Design of the TanDEM-X Satellite is Not provided."]
[8.246315002441406, 3.611180543899536, "The Deployment Date of the HawkEye 360 Satellite Constellation is Not Provided."]
[6.657100200653076, 1.8567471504211426, "The Monitoring Period of the Envisat Satellite is 2008-2009."]
[6.99210262298584, 7.703192234039307, "The Ground Resolution of the HARP-2 Polarimeter is Narrow."]
[7.682112693786621, 1.045933485031128, "The Anomaly Date of the Sentinel-1B Satellite is 23 December 2021."]
[6.0329270362854, 2.7370858192443848, "The Mission Lead of the THEMIS Satellite Constellation is Vassilis Angelopoulos."]
[6.7376604080200195, 2.1212501525878906, "The Mission Type of the GPM Satellite is Rainfall Measurement."]
[6.62313985824585, 10.664945602416992, "The SNR of the Band 1 Spectral Band is 260."]
[9.458536148071289, 8.892539024353027, "The Telescope Type of the R3 Sensor Imaging System is 1-inch refractive optical telescope."]
[7.5355424880981445, 2.1280572414398193, "The DOI of the Near Earth Asteroid Scout Satellite is https://doi.org/10.2514/6.2014-4435."]
[10.920251846313477, 4.997219085693359, "The Maneuver of the LISA Pathfinder Spacecraft is Keep test masses away from the housing walls."]
[9.405387878417969, 2.8413166999816895, "The Trajectory Analysis and Design Presentation of the OMOTENASHI Satellite is 31st ISTS (International Symposium on Space Technology and Science)."]
[7.137362480163574, 3.1668012142181396, "The Communication Status of the MarCO CubeSat is Loud and Clear."]
[0.9644762277603149, 4.189776420593262, "The Mass of the Battery Energy Storage is About 3.5 kg."]
[5.1189703941345215, 7.622080326080322, "The Data Compression Rate of the Instrument Spectrometer is < 80%."]
[6.878876209259033, 2.9428558349609375, "The Status of the SwissCube Satellite is Active."]
[7.758823394775391, 10.322444915771484, "The Channel Detectors of the SEVIRI Spectral Imager is 42."]
[2.8637747764587402, 6.5089898109436035, "The Input Voltage of the Transmitter Communication Device is +12 V DC."]
[9.289884567260742, 9.100934982299805, "The PSF (Point Spread Function) of the Telescope Optical Instrument is 1.5 - 2.5 arcmin (rms)."]
[6.335279941558838, 8.320385932922363, "The Channels of the GOES Sounder Radiometer is 19."]
[8.65638542175293, 8.554239273071289, "The Optical System of the PS0 Optical Instrument is 2 element Maksutov Cassegrain."]
[7.214834690093994, 1.2910830974578857, "The Launch Date of the EarthCARE Mission is Unknown."]
[8.617955207824707, 4.902635097503662, "The Drag Levels of the S/C Satellite is Several N."]
[6.479726791381836, 6.287574291229248, "The Swath Width of the OSCAT-3 Radar Scatterometer is 1440 km."]
[12.013679504394531, 3.374194622039795, "The Orbit of the Kounotori-5 Spacecraft is Near-circular orbit, altitude of ~400 km to ISS, inclination =51.6\u00b0."]
[7.4086503982543945, 2.516568660736084, "The URL of the Kepler Satellite is http://www.nasa.gov/mission_pages/kepler/news/41-new-transiting-planets.html."]
[10.23996353149414, 6.815816402435303, "The Control Mode of the HM Heater System is Measurement and Calibration Modes and controlled through CCU-CMN (Correlator and Control Unit-Control and Monitoring Node) chain."]
[6.521581649780273, 8.497989654541016, "The Performance of the MW Instrument is 0-4 Nms."]
[9.83713436126709, 4.294095516204834, "The Function of the Drag Sail Satellite Component is Deorbit the satellite."]
[6.410543918609619, 4.41478967666626, "The Instrument Type of the TROPICS CubeSat Satellite is Microwave Spectrometer."]
[3.4151341915130615, 5.280282974243164, "The Onboard Storage Capacity of the NigeriaSat-2 Satellite is 16 gigabytes."]
[6.828207969665527, 3.164095401763916, "The Mission Status of the FITSat-1 Satellite is Mission complete."]
[11.331575393676758, -0.6772289276123047, "The Interior Volume of the BA 330 module Space Module is 330 m3."]
[11.681904792785645, -0.7000343203544617, "The Power Distribution of the MERLIN Satellite is Unknown."]
[7.315951824188232, 0.6298003792762756, "The Selection Date of the Lobster-Inspired Mirror Satellite Component is Oct. 27, 2015."]
[1.8862833976745605, 3.9957468509674072, "The Surface Area of the CSS Solar Cells is 2 cm2."]
[2.2529916763305664, 4.37345552444458, "The Power of the RISAT-2 Satellite is 750 W."]
[6.65459680557251, 3.466695785522461, "The Mission Objectives of the ZACUBE-2 Satellite is Aligned with those of MDASat-1."]
[7.650364875793457, 5.041412353515625, "The Absolute Radiometric Calibration Accuracy of the PROBA-V Satellite is Unknown."]
[3.552711009979248, 2.2896034717559814, "The Size of the CP-9 Satellite is 2U."]
[11.148548126220703, 6.643956661224365, "The Spectral Range of the SphinX X-ray Photometer is 1-12 \u00c5."]
[10.023207664489746, 1.4132205247879028, "The Period of the Satellite SuperView Constellation is 97 minutes."]
[1.4849671125411987, 4.962670803070068, "The Voltage of the Antenna Power Supply Antenna Power Supply is 100 V."]
[8.363872528076172, 8.99811840057373, "The Apogee of the BUV Sensor is 1108 km."]
[5.334573745727539, 6.048240661621094, "The Configuration of the SGR-ReSI antenna Antenna is Nadir and zenith dual frequency antennas, two L1-only zenith antennas."]
[5.374765396118164, 2.1515755653381348, "The Number of Student Images of the MoonKAM Education and Public Outreach Program is Over 70,000."]
[9.472661018371582, 8.993597984313965, "The Target Altitude of the CHEOPS Telescope is Equal or higher than 100 km."]
[5.685183048248291, 6.467889308929443, "The SAR Antenna Size of the CSG-SAR Synthetic Aperture Radar is ~7.5 m^2."]
[5.040884017944336, 6.371810436248779, "The Radiation Pattern of the Antenna Low-Gain Antenna is Broad-beam."]
[8.154473304748535, 0.7300323843955994, "The Workshop Date of the Megha-Tropiques Satellite is 17-20 November 2014."]
[7.955906391143799, 7.26120138168335, "The Update Method of the Spectral Calibration Calibration is Vicarious techniques using the measurement of the atmospheric gas and/or the sun Fraunhofer lines."]
[11.69146728515625, 0.9277562499046326, "The Ascender Weight of the Chang\u2019e-5 Lunar Lander is 300 to 400 kg."]
[10.15674877166748, 3.900728702545166, "The \u0394V of the NEA Scout CubeSat is Up to 2km/s."]
[11.34223747253418, 4.175909519195557, "The Observation Reach of the Roman Satellite is More than 13 billion years of cosmic history."]
[7.737429141998291, 3.9375205039978027, "The Daily Coverage of the ZY-3A Satellite is 150,000 km2."]
[5.377490997314453, 3.5869927406311035, "The Unknown of the IXV Spacecraft is Unknown."]
[12.944488525390625, 4.858371257781982, "The Imaging Technology of the IBEX Spacecraft is ENA (Energetic Neutral Atom) imaging."]
[8.29541015625, 7.884863376617432, "The Components of the Camera Unit Calibration Assembly is Filters, spectral calibration sources (PTFE sun diffusers)."]
[8.008357048034668, 10.050235748291016, "The Bands of the WFI Camera is Three visible bands and one NIR band."]
[3.999783754348755, 6.442746639251709, "The Beacon modulation of the RF communication subsystem Communication is OOK 15 WPM."]
[2.6338701248168945, -1.455215573310852, "The Brigthness Temperature (BT) of the Antenna Reflector is 100~300 K."]
[2.1964070796966553, 4.218661785125732, "The Energy Supply of the Payload Satellite Payload is Solar generator."]
[6.774965763092041, 2.607597827911377, "The URL of the SCD-2 Satellite is http://www.las.inpe.br/~veissid/eng18.html."]
[13.706266403198242, 1.6057008504867554, "The Stages of the Vega Launcher Launch Vehicle is Three SRM stages, a liquid propulsion upper module."]
[3.9872708320617676, 4.513103485107422, "The Communication Interface of the DCU Data Control Unit is Mil-STD-1553 bus."]
[7.88612699508667, 0.9737525582313538, "The Year of Launch of the Terra Satellite is 1999."]
[7.300730228424072, 8.202804565429688, "The Beacon Period of the Spectrum Analyzer Device is 15 seconds."]
[7.293903827667236, 7.766726970672607, "The Single Point Acquisition Time of the Instrument Satellite Instrument is Less than 0.3 seconds."]
[5.307811737060547, 4.540573596954346, "The Locations of the LAPAN Ground Station Network is Rumpin and Rancabungur (Bogor), Bukittinggi (West Sumatra), Pontianak (West Borneo)and Biak (Papua)."]
[7.603082656860352, 6.368001937866211, "The Mechanical Tests of the Biomass Satellite is Sine vibration, acoustic, shock and clamp-band release tests."]
[1.508072853088379, 4.916806221008301, "The Operating Voltage of the LVPS Board Power Supply is 28 V."]
[9.173152923583984, 7.422276496887207, "The Current Dependence of the Sensor Gas Sensor is Linear dependence on the oxygen partial pressure."]
[8.983101844787598, 10.677654266357422, "The Calibration Source of the LISS-3 camera Camera is LEDs (1.55 \u00b5m)."]
[8.64719295501709, 9.068243026733398, "The Grating Type of the MEGS Spectrograph is Dual, holographic, spherical grating."]
[8.517147064208984, 2.3226349353790283, "The Affiliation of the Parker Solar Probe Spacecraft is Johns Hopkins University Applied Physics Laboratory."]
[10.089594841003418, 1.3517181873321533, "The Equator Crossing Time of the ResourceSat-2A Satellite is 10:30 AM."]
[4.99262809753418, 4.364922523498535, "The Command Execution Method of the Spacecraft Satellite is Immediate or Time-tag queue."]
[11.682059288024902, 4.862577438354492, "The Handle Distance from Center of the The Teacup Quasar is Around 30,000 light years."]
[9.838349342346191, 8.732011795043945, "The Field of View of the ART-XC Instrument Telescope is 36' diameter."]
[8.611076354980469, 6.095302581787109, "The Symmetry of the Earth's main magnetic field Magnetic Field is Not Geometrically Opposite."]
[7.925559043884277, 0.4350404441356659, "The Launch Date of the CryoSat-2 Satellite is April 8, 2010."]
[2.632756233215332, -1.4567021131515503, "The Brigthness Temperature (BT) Sensitivity of the Antenna Reflector is \u00b10.18 K."]
[7.547846794128418, 8.099609375, "The Pseudo-sounding Capability of the AMI Imager is Provides atmospheric instability information."]
[10.018682479858398, 3.0878071784973145, "The Altitude of the MICROSCOPE Satellite is 710 km."]
[9.118752479553223, 9.307868957519531, "The Application of the Scanning Shack Hartmann Sensor Wavefront Measurement Device is Measurement of the human eye."]
[8.423343658447266, 10.527029037475586, "The Maximum Quantum Efficiency of the Kruiz CCD Detector is 0.33."]
[5.1053595542907715, 4.4099016189575195, "The Objective of the DRR Data Routing and Retrieval is Deliver global SMD (Stored Mission Data) to four US Operational Processing Centers."]
[7.1305460929870605, 0.5929486751556396, "The Technical Commissioning Completion Date of the SPOT 6 Satellite is January 2013."]
[7.4800214767456055, 8.00102710723877, "The Performance Independence of the Instrument Unknown is Independent of variations of the receiver gain."]
[10.389809608459473, 3.1020119190216064, "The Secondary Orbit Altitude Goal of the HAPS Hydrazine Auxiliary Propulsion System is 1200 km."]
[3.9672529697418213, 4.389219284057617, "The Provider of the RTOS Real Time Operating System is VxWorks."]
[9.3623685836792, 8.491604804992676, "The Components of the TESIS Telescope-spectrometer is TESIS-BD, TESIS-BE, TESIS-OD."]
[9.7994384765625, 5.5495476722717285, "The Maneuver Execution Time (240 minute window) of the RASP Maneuver Planning System is 143.36 minutes."]
[4.363003253936768, 4.876160144805908, "The Function of the TMTC Interface Software Layer is Telemetry and telecommand interface."]
[10.259658813476562, 6.841997146606445, "The Heater Lines of the STC Survival Thermal Control is 8."]
[9.316429138183594, 8.942817687988281, "The Objective Type of the Optics Subsystem Camera Subsystem is Ritchey-Chr\u00e9tien type with auxiliary lenses."]
[8.640868186950684, 6.2223687171936035, "The Deployment Status of the AstroTubeTM Boom Boom is Deployed to full length."]
[7.717384338378906, 9.130163192749023, "The GSD of the Spectral Band C Spectrometer is 5."]
[8.234054565429688, 2.2673466205596924, "The Mission of the SOHO Satellite is Solar and Heliospheric Observatory."]
[8.18061351776123, 2.9565961360931396, "The Authors of the Interstellar Boundary Explorer Satellite is 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, ."]
[8.775891304016113, 8.822943687438965, "The Grating Angle of the UVS Instrument Spectrometer Telescope is 22.7\u00ba."]
[4.774867534637451, 5.190371513366699, "The Ground Segment Antennas of the IXPE Satellite is 10 m antennas at Malindi (primary) and Singapore (backup)."]
[0.9453322887420654, 4.226711273193359, "The Capacity of the Batteries Power subsystem is 7 Ah."]
[10.192709922790527, 2.9608983993530273, "The Altitude of the SkySat-16 to -18 Satellite is 575 km."]
[9.17812728881836, 3.2355942726135254, "The Orbit Type of the Satellite Constellation Satellite Constellation is Elliptical sun-synchronous dawn-dusk."]
[3.2951090335845947, 5.665489673614502, "The Data Size of the Processed Science Data Packet Data Packet is 36 bytes."]
[11.396673202514648, 5.1603827476501465, "The Distance from Earth of the Pulsar Neutron Star is Unknown."]
[7.347142219543457, -0.2248777598142624, "The Launch Date of the HTV-7 Cargo Vessel is 22 September 2018."]
[5.529179573059082, 3.8722944259643555, "The Autonomy of the F-DUGS Center is Operated by French personnel."]
[3.646596670150757, 3.4974653720855713, "The Mission Design of the CICERO Satellite is Microsatellite to a 6U CubeSat Form Factor."]
[8.48118782043457, 3.8677871227264404, "The Celestial Sphere Coverage of the Spacecraft Satellite is 50% during the extended mission phase."]
[7.802724361419678, 2.2322731018066406, "The Edition of the Observation of the Earth and Its Environment: Survey of Missions and Sensors Documentation is 4th."]
[4.656413555145264, 5.908305644989014, "The RF Communications of the Spacecraft Satellite is 437.365 MHz."]
[2.2509260177612305, 4.405569553375244, "The Power of the SCD-2 Satellite is 110 W."]
[8.169161796569824, 10.284524917602539, "The Spectral Band of the Camera Imaging Device is 744-826 nm."]
[6.045552730560303, 1.5644748210906982, "The Status of the PAZ Satellite is In launch preparation."]
[6.393554210662842, 2.873772621154785, "The Mission Management Provider of the Lucy Satellite is Goddard."]
[6.527021408081055, 0.549030065536499, "The Launch Date of the TUBSAT Satellite is September 13-16, 1993."]
[4.051308631896973, 1.207102656364441, "The Mission Type of the ZACUBE-2 Satellite is Non-EO."]
[11.281272888183594, 6.61925745010376, "The Observation Target of the NICER/SEXTANT Instrument is Neutron stars and pulsars."]
[4.893891334533691, 7.369175910949707, "The Telemetry Format of the Instrument Sensor is PCM (Pulse Code Modulation)."]
[10.359939575195312, 3.3894691467285156, "The Separation Distance of the Satellite Constellation Satellite Constellation is 100-1000 km."]
[9.56884479522705, 2.1072771549224854, "The Radio and Reaction Wheels Current of the MarCO-B Satellite is Significantly more."]
[7.197032451629639, 6.898742198944092, "The Presentation Date of the SEDA-AP Instrument is August 3-6, 2010."]
[8.24431324005127, 5.812005043029785, "The Vector Components Random Error of the Ion Drift Velocity Satellite System is < 200 m/s."]
[7.924092769622803, -0.6570647358894348, "The Launch Date of the SpaceX-CRS-4 Dragon capsule Cargo Capsule is Sept. 21, 2014."]
[4.46331262588501, 6.165449619293213, "The Flight Heritage of the MHX-2400 S-band Transmitter/Transceiver is 4 missions."]
[7.1584930419921875, 0.6894820928573608, "The Launch Date of the BeiDou-1A Satellite is Oct. 31, 2000."]
[5.802530765533447, 3.018399477005005, "The Manufacturer of the SARah-1 Earth Observation Satellite is Airbus."]
[9.758810997009277, 4.24424934387207, "The Sail Shape of the Drag Sail Modules Satellite Component is Trapezoidal."]
[6.255413055419922, 4.643264293670654, "The Data of the ICEYE Satellite is Used to monitor oil wells and measure global oil storage."]
[8.35688591003418, 0.3418765962123871, "The Expansion Time of the BEAM Expandable Habitat is Seconds."]
[7.7911763191223145, 3.4752037525177, "The In-situ Measurements of the ICON Space Mission is Provide the ability to explain how energy and momentum from the lower atmosphere propagate into the space environment."]
[9.354606628417969, 1.5333261489868164, "The Global Ocean Color Data Recording Time of the Sentinel-3B Satellite is Less than 1.9 days at the equator, and in less than 1.4 days at latitudes higher than 30\u00ba."]
[1.8313791751861572, 4.073836326599121, "The Energy Source of the Electric Power Subsystem Power System is Solar cells."]
[9.371660232543945, 5.982433795928955, "The Sensor Type of the CubeSense Attitude Determination and Control Subsystem is Integrated sun and nadir sensor."]
[4.855380058288574, 1.8424760103225708, "The Quantity of the ICEYE US Satellites Satellite is 2."]
[3.7551095485687256, 2.295356035232544, "The Spacecraft Type of the CHOMPTT Satellite is 3U."]
[7.421710968017578, 1.135287880897522, "The Discovery Date of the Integral Satellite is 20 Oct. 2003."]
[9.343819618225098, 5.8429131507873535, "The Effect of the Galactic Cosmic Rays Cosmic Phenomenon is Penetrate Earth's magnetic fields and interact with the atmosphere."]
[11.44286060333252, 5.84647798538208, "The Discovery of the ASIM Instrument is Recently detected a unique gamma-ray burst from outer space."]
[7.864524841308594, 6.921143531799316, "The Operation Start of the Experiment Unknown is Launch."]
[7.806042671203613, 9.134743690490723, "The Spectral Range of the Spectrometer Instrument is 5-11 \u00b5m."]
[9.081315994262695, 0.7134434580802917, "The Years on Orbit of the EO-1 Satellite is 13."]
[11.542343139648438, 5.99643087387085, "The Role of the INTEGRAL and XMM-Newton Satellite Missions is Follow-up of recent gravitational wave detections."]
[5.931726455688477, 4.70108699798584, "The Categories of the L1-SAIF+ Satellite Message is \"SBAS-compatible\" and \"SBAS-incompatible\"."]
[7.194125652313232, 7.1187238693237305, "The Observation Date of the ADONIS Instrument is 1996."]
[8.161736488342285, 1.2775413990020752, "The Date of the Long-lasting Dust Storm from Chihuahua Image is 18 March 2021."]
[9.067999839782715, 8.86698055267334, "The Along-track FOV of the TIR Subsystem Imaging System is \u00b10.65\u00ba."]
[5.47733211517334, 3.750669240951538, "The Object Match of the CSpOC Catalog Catalog is Correct."]
[6.025788307189941, 4.074428081512451, "The Prime Instrument Contractor of the IASI Instrument is Alcatel Space."]
[5.291015625, 3.429978132247925, "The Number of Technologies of the CFESat Satellite is 8."]
[6.368474960327148, 1.1434860229492188, "The Conference Date of the COSMO-SkyMed Satellite is Nov. 27-29, 2006."]
[9.488168716430664, -2.506754159927368, "The Energy Range for He of the LEICA Particle Detector is 0.45 - 6.1 4.3 - 38 7 - 20 18 - 350 MeV/n."]
[8.307084083557129, 8.685916900634766, "The Funding of the NIRCam Near-Infrared Camera is NASA."]
[7.937577724456787, 4.720444679260254, "The Spatial Resolution of the GHGSat-D Satellite System is 100 x better than the current state-of-the-art."]
[9.612850189208984, 1.2356460094451904, "The Initial Acquisition Time of the CAPSTONE Spacecraft is Six days."]
[7.726993083953857, 6.20869255065918, "The Analysis of the Unresolved Imagery Data is Analyzing the spectral frequencies and temporal changes in the intensity."]
[7.627274036407471, 4.474984645843506, "The Sea-Level Rise Contribution of the Greenland and Antarctica Locations is About 11 mm."]
[8.452851295471191, 8.414628982543945, "The Detector Systems of the Spectrometer Instrument is 7."]
[5.975881099700928, 1.8932251930236816, "The Launch Vehicle of the KANOPUS-V-IK Satellite is Soyuz-2.1a."]
[9.10721206665039, 4.158361911773682, "The Size of the StudSat Picosatellite is 10 cm x 10 cm x 13.5 cm."]
[9.757116317749023, 1.272995114326477, "The Test Period of the Sloshsat-FLEVO Satellite is About a week."]
[3.2280259132385254, 4.926722526550293, "The Internal RAM of the OBC Onboard Data Handling is 4 kB."]
[9.407889366149902, -0.7375528812408447, "The Launch Time (CEST) of the ESAIL Microsatellite is 03:51."]
[7.26032829284668, 1.7988255023956299, "The Development Prize Date of the Global Change Observation Mission 1st \u2013 Water \u201cSHIZUKU\u201d Satellite is October 17, 2013."]
[5.673641681671143, 9.403295516967773, "The Sensitivity of the STROFIO Instrument is 0.14 counts/s when the density is 1 particle/cm3."]
[7.152770519256592, 2.388383150100708, "The URL of the Evaluation Process is https://spacenews.com/nasa-continues-csda-program/."]
[10.540566444396973, 2.599198341369629, "The Apogee of the Explorer 36 Satellite is 1570 km."]
[10.573647499084473, 7.576979160308838, "The Material of the Adsorbent Bed Component is Zeolite."]
[1.8193767070770264, 4.148098945617676, "The Solar Array of the EPS Electric Power Subsystem is Articulated, 1 wing, 2-axis tracking."]
[4.398639678955078, 7.002600193023682, "The Antenna Weight of the PRARE ground transponder Ground Station Equipment is 42 kg including gearing unit."]
[8.569624900817871, 5.5125579833984375, "The Attitude Determination and Control Subsystem Calibration of the Spacecraft Satellite is Ongoing."]
[9.263053894042969, 8.3386869430542, "The Segmentation of the LET Detector is Central bull\u2019s-eye surrounded by a wide annular region."]
[6.797488212585449, 3.342738628387451, "The Data Processing Provider of the CloudSat Satellite is CIRA (Cooperative Institute for Research in the Atmosphere) of CSU (Colorado State University)."]
[9.076074600219727, 9.747342109680176, "The Time Between Monitoring Campaigns of the OSIRIS Narrow Angle and Wide Angle Cameras Imaging System is Reduced to a few days."]
[11.188023567199707, 9.346726417541504, "The IFOV of the Earth Radiation Budget Experiment (ERBE) Instrument is 14 mrad."]
[7.252932548522949, 4.199553966522217, "The Instrument Type of the DMC-3 Satellite Constellation is Imaging multi-spectral radiometers (vis/IR)."]
[6.371425151824951, 5.394701957702637, "The Bistatic Imaging of the TDX/TSX Satellite is Provides additional observables for the extraction of new scene and target parameters."]
[9.178525924682617, 7.9388651847839355, "The Geometry Factor of the LEICA Particle Detector is 0.8 cm^2 sr."]
[6.428036212921143, 4.734851837158203, "The Planned Instruments of the FY-3RM Satellite is Ku/Ka band radar, microwave sounding and imaging instruments."]
[7.290902614593506, 9.480989456176758, "The Swath Width of the TopSAR narrow Imaging Mode is 100 - 150 km."]
[8.496554374694824, 7.411664962768555, "The Operation of the ULF Sensor Sensor is Continuous."]
[11.740099906921387, 1.6746665239334106, "The Landing Accuracy of the Philae Lander Spacecraft is Less than 100 m from the planned Agilkia site."]
[11.083290100097656, 4.043514728546143, "The Kinematic properties of the \u03b2 meteoroid Interplanetary Dust is > 77 km/s."]
[11.68804931640625, -0.7960687279701233, "The Total Mass of the MERLIN Satellite is 430 kg."]
[7.095815181732178, 1.7550863027572632, "The Mission of the Beowulf Cluster Computing Cluster is First in Space."]
[5.179009437561035, 6.605474948883057, "The Antenna Type of the Antenna Reflector is Dual Paraboloidal Reflector."]
[2.135586738586426, 4.573350429534912, "The Power Capacity of the Platform Satellite is 3 kW."]
[7.291347503662109, 5.431392192840576, "The Reproduction of the Bdelloids Species of Rotifers is Produce offspring from unfertilized eggs."]
[9.19611644744873, -0.6571650505065918, "The Launch Date of the Aalto-1 Nanosatellite is Feb, 5, 2012."]
[7.703033924102783, 7.201008319854736, "The Function of the TEMPO Instrument is Provide near-real-time North American air quality information."]
[5.117030143737793, 1.3589266538619995, "The Aviation Market Ranking of the India Country is Third largest."]
[9.462525367736816, 0.9110461473464966, "The Tracking Duration of the TiPS Assembly Satellite is One year."]
[5.3195271492004395, 9.60352611541748, "The Configuration of the STOs and STAEs Analog Electronic units is 3 on but 2 in operation."]
[3.510026454925537, 5.707365989685059, "The Test Number of the File Transfer Test Communication is 4."]
[7.189586639404297, 5.731414794921875, "The Influence on Storm Growth of the Drop Size Distribution Meteorological Phenomenon is Changes the rate of evaporation of rain, affects storm structure and behavior."]
[4.019726753234863, 10.363948822021484, "The NE\u0394T (K) of the ICI-8 Radiometer is 1.3."]
[6.803377151489258, 0.6410028338432312, "The Launch Confirmation Date of the Telesat LEO Phase 1 Satellite is 12 Jan. 2018."]
[11.809311866760254, -1.0999791622161865, "The Launch Mass of the FY-3 series spacecraft Satellite is 2450 kg."]
[12.081853866577148, 5.348057746887207, "The Characteristics of the Dark Matter Hypothetical Matter is Weird, unexpected."]
[11.27880573272705, 3.785815477371216, "The Comet Discoveries of the SOHO Satellite is 2000."]
[17.72833824157715, 7.162677764892578, "The J2000 right ascension (deg) of the GROJ1744-28 Pulsar is 266.138."]
[11.627286911010742, 0.7012717127799988, "The Combined Weight of the Tiangong Space Station is Nearly 70 metric tons."]
[9.001605033874512, 2.764604091644287, "The Launch Date of the GCOM-W1 Satellite is May 17, 2012."]
[6.63131856918335, 8.396806716918945, "The Cross-Track Scanning Technique of the MERSI-RM Radiometer is 4096 samples."]
[7.482785701751709, 0.9458394050598145, "The Development Date of the ETS-VIII Satellite Satellite is 2003."]
[9.659146308898926, 5.966046333312988, "The Microprocessor of the ADCS Attitude Determination and Control Subsystem is 32-bit ARM."]
[13.182689666748047, 4.0129289627075195, "The Launch Window of the Gaia Satellite is 17 December to 5 January 2014."]
[11.390363693237305, 1.0672085285186768, "The Lander/Rover Soft Landing Time of the Tianwen-1 Probe is 2\u20133 months after arrival of the spacecraft."]
[4.0081939697265625, 6.925367832183838, "The Mass of the Spacecraft Repeater Communication Device is 24 kg."]
[1.6111843585968018, 4.343585968017578, "The Power Source of the EPS Electrical Power Subsystem is Solar cells and lithium-ion battery."]
[12.084538459777832, 3.3037407398223877, "The Inclination of the Spacecraft Orbit is 98\u00b0."]
[7.509009838104248, 8.99987506866455, "The Channel Wavelength of the SAM-II Instrument is 0.98-1.02 \u00b5m."]
[7.4862961769104, 9.611359596252441, "The Wavelength of the VIS (red) Band is 0.65 \u00b5m."]
[7.915236473083496, 7.254922866821289, "The Operational Cadence of the Instrument Satellite Instrument is Rotate 120\u00ba in < 2 minutes to blackbody view."]
[7.7112507820129395, 7.854541301727295, "The Publication Date of the Solar Backscatter Ultraviolet/Total Ozone Mapping Spectrometer (SBUV/TOMS) Spectrometer is 1975."]
[6.20227575302124, 3.009403944015503, "The Responsible Agency of the DWSS Satellite is DoD."]
[11.21542739868164, 3.990004062652588, "The Drift Speed of the Great Red Spot Atmospheric Anticyclone on Jupiter is Circling the planet in about four-and-a-half years."]
[6.24778413772583, 1.824934482574463, "The Frequency of the ADS-B Air Traffic Surveillance System is 1090 MHz."]
[7.401401519775391, 2.5102241039276123, "The URL of the Rosetta Satellite is http://www.esa.int/Our_Activities/Space_Science/Rosetta/Rosetta_factsheet."]
[1.514079213142395, 4.804016590118408, "The Under Voltage Cut Off of the DC-DC converter Power Converter is Yes."]
[4.814929485321045, 9.00859260559082, "The Sensor Types of the InSight Mars Lander is Wind, temperature, pressure, magnetometer."]
[5.436631679534912, 3.6750965118408203, "The Accommodation Location of the ASIM Payload is Starboard deck of the CEPF."]
[7.29656457901001, 0.5292545557022095, "The Launch Date of the Claire Satellite is February 2018."]
[6.125607967376709, 4.110641956329346, "The Collaboration of the TES Satellite Instrument is Close collaboration with the IASI scientists."]
[6.563320159912109, 3.9774436950683594, "The AWiFS Data Access of the Resourcesat-1 Satellite is Unknown."]
[7.610830307006836, 1.7298961877822876, "The Arrival Date of High-energy Neutrino of the IceCube Neutrino Observatory Neutrino Detector is 22 September 2017."]
[11.711979866027832, -1.0739563703536987, "The Mass of the Genesis-2 Spacecraft is 1360 kg."]
[7.014931678771973, 0.3796411156654358, "The Launch Date of the SPOT-2 Satellite is Jan. 22, 1990."]
[7.287908554077148, 7.111415386199951, "The Data Usage of the AVHRR/3 Visible and Infrared Spectral Bands Instrument is Provide image data in the visible and infrared spectral bands, information on cloud coverage within the footprints of the various sounding instruments."]
[5.125339508056641, 5.1945600509643555, "The Antenna Type of the Knudsen Station Ground Station is Two phased 2MCP8A circularly polarized VHF yagis with polarizer switching capabilities."]
[0.9156599640846252, 4.191532135009766, "The Capacity of the Power Storage Battery is 5 Ah."]
[5.98039436340332, 0.7234826683998108, "The Launch Date of the NRCSD CubeSat Deployer is January 9, 2014."]
[9.207598686218262, 7.100568771362305, "The Operational Environment of the m-NLP system Langmuir Probe System is LEO up to 1000 km altitude."]
[7.545087814331055, 2.9036030769348145, "The Support Plan of the KOMPSAT-2 Satellite is Support key technologies for application in the private sector and to promote the relevant industries."]
[7.189032077789307, 0.3018766939640045, "The Launch Date of the Biomass Satellite is April 2024."]
[10.543517112731934, 2.2600550651550293, "The Inclina. (\u00ba) of the Meteor-1-1 Satellite is 81.2."]
[6.561969757080078, 0.4875330328941345, "The Data Record Start of the CERES FM6 Satellite is 1997."]
[5.423150062561035, 4.066005706787109, "The Data Archiving Site of the Deployment Systems Satellite is Las Vegas."]
[3.711866617202759, 5.955212116241455, "The Nominal Average of the Data Generation Rate Full Payload is 120 kbit/s."]
[3.789807081222534, 4.528031349182129, "The Data Storage of the SCP Spacecraft Process Controller is Half of programming space."]
[8.480138778686523, 8.003532409667969, "The Mass-Cage Contact of the Inertial Sensors Sensor is 5 \u00b5m diameter gold wire."]
[9.262642860412598, 5.180537700653076, "The Life-Test Status of the NIRISS Dual Wheel Cryogenic Mechanism Mechanism is Not Provided."]
[7.013791561126709, 0.19026562571525574, "The Launch Time of the BRO-1 Satellite is 00:12 NZST."]
[7.459248065948486, 8.419696807861328, "The Fly on of the HIRS/4 Infrared Sounder is NOAA-N, NOAA-N', and MetOp 1 and 2."]
[11.487865447998047, 2.1737444400787354, "The Reentry Capsule Recovery Date of the Hayabusa-2 Spacecraft is 6 December 2020."]
[5.894493103027344, 1.915079951286316, "The Launch Vehicle of the Galileo FOC satellites Satellite is Soyuz ST-B/Fregat-MT."]
[5.934384822845459, 0.9824082851409912, "The Announcement Date of the Iridium Certus service providers Service Providers is February 28, 2018."]
[5.116429805755615, 4.448154449462891, "The Development Status of the Mission Control System Ground Segment Component is Currently being developed."]
[6.411160945892334, 2.2862939834594727, "The Number of Collision Warnings Provided in 2014 of the JSpOC Joint Space Operations Center is 671,727."]
[10.501192092895508, 7.675518035888672, "The Enclosure Material of the VLF Antenna Antenna is Plastic."]
[4.7232232093811035, 5.134718418121338, "The Function of the PTT Platform Transmitter Terminal is Collect and process relevant environmental data and transmit them to the NOAA-POES satellites."]
[8.519790649414062, 9.93507194519043, "The Number of Arrays of the FPA (Focal Plane Assembly) Detector Arrays is 4."]
[11.07359790802002, 4.1117844581604, "The Kinematic properties of the ISD Interstellar Dust is 25 km/s, ecliptic longitude of 252\u00ba & ecliptic latitude of 5\u00ba."]
[9.200103759765625, 3.231840133666992, "The Orbit Type of the Landsat 9 Satellite is Sun-synchronous near-circular orbit."]
[9.064825057983398, -0.5612786412239075, "The Launch Date of the M6P and M12P Nanosatellite Buses is Early 2023."]
[5.178317546844482, 4.24772834777832, "The Autonomy of the X-UGS UGS is Full."]
[6.710503101348877, 0.6866499185562134, "The Launch Date of the EyeSat Satellite is 18 December 2019."]
[5.891695499420166, 1.5593507289886475, "The Conference Presentation Date of the GOMX-1 Satellite is April 23-25, 2014."]
[5.350313186645508, 5.659992694854736, "The Frequency of the MosaicGNSS receiver GPS Receiver is Single."]
[9.520413398742676, 8.791261672973633, "The Function of the Optical Telescopes Instrument is Determine the trajectory of an orbiting object, determine the object's attitude, physical profile, and features."]
[4.3869781494140625, 3.9236605167388916, "The Operation of the Automated Beacon Network Anomaly Detection System is Notifies on-call operators and initiates response actions."]
[9.806119918823242, 8.61323356628418, "The Number of Mirror Modules of the ART-XC Instrument Telescope is 7."]
[11.572067260742188, 5.136275768280029, "The Point of No Return of the Event Horizon Black Hole Feature is The point of no return."]
[6.070477485656738, 9.542182922363281, "The Total Mass of the PHM Instrument is 18 kg."]
[9.003212928771973, 1.085892677307129, "The Science Mission Duration of the LRO Satellite is 9/17/2010 - 9/16/2012."]
[4.056519031524658, 1.2858887910842896, "The Mission Type of the AstroSat Astronomy Satellite is Non-EO."]
[7.498760223388672, 0.7418813109397888, "The Birthday of the PROBA-V Satellite is May 7, 2014."]
[9.42905330657959, 0.9115250706672668, "The On-Orbit Duration of the AIM spacecraft Satellite is 7 years."]
[3.462407350540161, 6.721839427947998, "The Data Rate (max) of the STX-01 S-band Transmitter/Transceiver is 2000 kbit/s."]
[4.353338718414307, 5.3246235847473145, "The Signal Loss of the Schiaparelli module Spacecraft is After one housekeeping data packet."]
[7.711900234222412, 1.0504978895187378, "The Launch Date of the Sentinel-1C Satellite is First half of 2023."]
[4.364593029022217, 4.5201096534729, "The Communication Network of the TTCS Telemetry & Telecommand Subsystem is CAN (Controller Area Network) bus."]
[6.674045085906982, 3.0487658977508545, "The Mission Objectives Achievement of the Alexander PhoneSat is More than 100%."]
[8.660083770751953, 6.875410556793213, "The Sensor Type of the MAGIC Magnetometer is Dual, 3-axis AMR (Anisotropic MagnetoResistive) sensor."]
[11.861254692077637, 1.004741907119751, "The Mission Expectations of the Chang'e-5 Lunar Probe is Major Contributions."]
[6.857096195220947, 1.4977787733078003, "The Workshop Date of the GIRO GSICS Implementation of the ROLO model is November 2017."]
[8.846043586730957, 9.388279914855957, "The Optical Efficiency of the Overall System is 0.4."]
[6.875726699829102, 1.0541965961456299, "The Presentation Date of the STSat-1 Satellite is Dec. 13-17, 2004."]
[9.242902755737305, 4.155856132507324, "The Size of the Spacecraft Satellite is 10 cm x 10 cm x 10 cm."]
[6.808486461639404, 3.1611950397491455, "The Mission Status of the NigeriaSat-2 Satellite is Operating nominally."]
[2.452911615371704, 6.330336570739746, "The Latency Requirement of the S-1 NRT Product is Within 3 hours."]
[6.714463710784912, 1.1837167739868164, "The Conference Date of the NPOESS Preparatory Project (NPP) Satellite is May 26, 2005."]
[7.60835075378418, 4.33624792098999, "The Sensor of the WorldView-3 Satellite is SWIR."]
[6.916618824005127, 3.976170778274536, "The Environmental Testing of the Deimos-2 Satellite is Verified."]
[7.180715560913086, 4.123671054840088, "The Image of the SJ-5 Satellite is Fluid two-layer flow liquid-bath."]
[6.325842380523682, 3.171098232269287, "The Operator of the Gonets-M No.3 Communication Satellite is Gonets Satellite Company."]
[10.307233810424805, 7.664721965789795, "The Main Structure Material of the UVNS Spectrometer is CFRP (Carbon Fiber Reinforced Polymer)."]
[6.071055889129639, 9.619853019714355, "The Instrument Mass of the Instrument Spectrometer is 177 kg."]
[3.6542446613311768, 6.645515441894531, "The Coded Data Rate of the X-band transmitter Transmitter is 441.625 Mbit/s."]
[7.6990838050842285, 1.5753494501113892, "The Survey Date of the Hera Spacecraft is Unknown."]
[5.638597011566162, 9.135004043579102, "The Power Consumption of the LEID Instrument is 2.9 W."]
[9.078693389892578, 5.804560661315918, "The Attitude Sensors of the ANUSat Satellite is Tri-axial magnetometer and an optical TWSS (Twin Slit Sun Sensor)."]
[3.873318910598755, 2.2740352153778076, "The Inflatable Mast Length of the Spacecraft 3U CubeSat is 1 m."]
[4.010609149932861, 4.497167110443115, "The Software Standard of the OBC On-Board Computer is PUS (Packet Utilization Standard)."]
[8.655171394348145, 0.1850534975528717, "The Crew Capacity of the Shenzhou-11 Spacecraft is 2."]
[10.518396377563477, 7.541136741638184, "The Material of the Outer Panels Satellite is CFRP (EX-1515/M55J + Redux 312L)."]
[9.18448543548584, 7.173457622528076, "The Purpose of the MSPR-2 Rack is Conduct a variety of experiments."]
[5.783769607543945, 6.832489013671875, "The Pulse Repeat Frequency of the X-band Radar is 100 Hz."]
[11.748559951782227, 1.6250319480895996, "The Instrument Operation Time of the Philae Lander is First 60 hours following the touch-down."]
[9.05439567565918, 10.101529121398926, "The Provider of the IR-Camera Camera is DLR-OS."]
[9.53780460357666, 9.041641235351562, "The Telescope Focal Length of the XMM Spacecraft is 7.5 m."]
[9.999100685119629, -0.5862410664558411, "The Inclination of the Tsubame Microsatellite is 97.4\u00ba."]
[9.894850730895996, 6.69417667388916, "The Objective of the BIRD Satellite is Observe thermal processes on the Earth\u2019s surface."]
[8.669567108154297, 9.843491554260254, "The Optics Type of the Imager Suite Imaging System is All-reflective."]
[7.999459266662598, 4.563791751861572, "The Image Resolution of the MTG-S Spacecraft Satellite is 0.5 to 2 km."]
[10.071508407592773, 1.4800454378128052, "The Period of the Tatiana-2 Satellite is 101.3 minutes."]
[5.922633647918701, 6.781363487243652, "The Data of the LPR Radar is Electromagnetic image of the far side subsurface structure."]
[9.317938804626465, 8.732850074768066, "The Telescope Type of the TIR Subsystem Imaging System is Newtonian catadioptric system with aspheric primary mirror and lenses for aberration correction."]
[8.128140449523926, 0.8795949816703796, "The Lifted atop launcher Date of the Landsat-9 Satellite is 21 September 2021."]
[6.833455562591553, 0.04020456597208977, "The Transition Point of the STP-H8 and H7 Missions is Unknown."]
[11.788909912109375, -1.1554356813430786, "The Launch Mass of the Gokturk-2 Satellite is ~ 450 kg."]
[6.421148777008057, 3.681145429611206, "The Re-use of Electronic Equipment of the Sentinel-5P Satellite is From several suppliers."]
[13.175485610961914, 4.021598815917969, "The Survey Date of the Gaia Satellite is 23 March 2022."]
[6.973004341125488, 7.318295001983643, "The Publication Date of the Nimbus-7 SBUV radiometer Radiometer is 1988."]
[12.122156143188477, 2.2115142345428467, "The Sample Stowage of the OSIRIS-REx Spacecraft is Expedited."]
[7.925623416900635, 9.18712043762207, "The Bands of the Spectral bands Spectrometer is 0.52 - 0.60 \u00b5m (green), 0.63 - 0.69 \u00b5m (red), 0.76 - 0.89 \u00b5m (NIR)."]
[5.1685791015625, 4.752638339996338, "The Ground Station of the RF Communications Communication System is SPIV (San Pietro in Vincoli)."]
[9.402457237243652, 4.918523788452148, "The Rotation Rate of the Satellite Spacecraft is Less than 1\u00ba/s."]
[6.656119346618652, 3.1354894638061523, "The Simulation of the YES2 satellite Satellite is Space Tether Deployment on Earth."]
[6.790988445281982, 3.3898446559906006, "The | of the SSO-A SmallSat Express Mission is Spaceflight SSO-A: SmallSat Express Mission."]
[6.620736122131348, 0.6885319352149963, "The Launch Date of the KySat-2 Satellite is 20 November 2013."]
[6.422595500946045, -0.7220099568367004, "The GPS/QZSS Differential Code Biases Stability of the QZS-1 Satellite is Better than 1 ns."]
[5.623703479766846, 3.215139865875244, "The Development Contractor of the SSOT Satellite is EADS Astrium SAS."]
[1.6274967193603516, 4.75137186050415, "The PPTs of the EPS Electrical Power Subsystem is 4 independent PPTs."]
[7.945862770080566, 3.9970014095306396, "The Placement of the Aditya-L1 Satellite is Lagrangian point L1."]
[8.366066932678223, 7.004237174987793, "The Bandwidth of the NewMag Magnetometer is 10Hz."]
[9.232357025146484, 5.334747791290283, "The Attitude Control of the PhoneSat-2.5 Satellite is Reaction wheels."]
[11.3749418258667, 6.494584083557129, "The Future Investigator of the Athena X-ray observatory X-ray Observatory is ESA\u2019s future Athena X-ray observatory."]
[13.218221664428711, 3.981856346130371, "The Last Eclipse Avoidance Maneuver Date of the Gaia Satellite is 16 July 2019."]
[7.254319190979004, 7.495129585266113, "The Contribution of the HARP-2 Instrument is PACE mission."]
[6.017755031585693, 0.8771957755088806, "The Launch Date of the Iridium NEXT Satellite is January 8, 2017."]
[7.238128662109375, 5.6352715492248535, "The Monitoring Method of the Ocean Acidification Environmental Phenomenon is Measurements of seawater pH."]
[4.1411824226379395, 6.431208610534668, "The Ka-band Repeater of the Repeater subsystem Communication System is 5/3 simultaneously operating transponders at saturation."]
[5.974093437194824, 8.5775146484375, "The Spectral range of the MWTS Microwave Temperature Sounder is 50-57 GHz."]
[10.232096672058105, 4.850553035736084, "The Ground Qualification Completion of the Aquajet Satellite Propulsion System is 2009."]
[10.337859153747559, 3.197033643722534, "The Altitude of the Primary Payload Unknown is 1450 km."]
[9.438926696777344, 7.381377220153809, "The Temperature of the IEC ISIM Electronics Compartment is Room temperature."]
[4.721314430236816, 5.539491176605225, "The Communication Link of the Bus Satellite Component is S-band radio frequency (RF) link."]
[7.881282329559326, 4.471498966217041, "The Spatial Resolution of the Sentinel-2 Satellite is 10, 20 or 60 m."]
[9.576531410217285, -0.664819598197937, "The Sensor of the ESAIL Microsatellite is VDES (VHF Data Exchange System)."]
[7.570044040679932, 8.43355941772461, "The Altitude range of the UV/VIS Spectrometer Spectrometer is 20 - 100 km."]
[7.976544380187988, 8.202615737915039, "The Accuracy of the ARI Infrared Spectrometer is Better than 0.1 K 3\u03c3."]
[10.375476837158203, 5.659121990203857, "The Orbit Altitude of the ProSEDS Tether Demonstration Experiment is 400 km."]
[10.244216918945312, 3.2777998447418213, "The Orbit of the INTEGRAL Satellite is Highly eccentric 64-hour orbit, coming as close as 10,000 km and as distant as 140,000 km from Earth."]
[9.207921028137207, 9.299302101135254, "The FOV Angle of the Lenses Optical System is 2.7\u00ba."]
[10.736838340759277, 10.284207344055176, "The Design of the PHA HiLRS is Small, low power."]
[7.640625, 7.215759754180908, "The RF Labs Equipment of the CesiumAstro Company is High performance test equipment, multiple RF chambers, antenna ranges, and environmental test stands."]
[6.05402946472168, 5.786800861358643, "The Reflector Illumination of the Biomass Satellite is 3 x 2 array of cavity-backed circular microstrip radiators."]
[10.35781478881836, 9.630208969116211, "The Launch Date of the Iris Satellite is 2nd September 2020."]
[4.771604537963867, 0.8766310214996338, "The Revenue of the Satellogic Satellite Company is $4.2 million."]
[10.195277214050293, 1.664853572845459, "The Orbital Period of the Beijing-1 Satellite is About 97.7 minutes."]
[7.711903095245361, 9.020807266235352, "The Spectral Range of the Ma_MISS Spectrometer is 0.4\u20132.2\u2009\u00b5m."]
[5.802615642547607, 4.160860061645508, "The Simulation Levels of the SEXTANT ground testbed architecture Testbed is Level 0, Level 1, Level 2."]
[3.5014657974243164, 5.07877254486084, "The Max Bandwidth of the Spacecraft 406 MHz Processor Processor is 80 kHz."]
[4.867485046386719, 1.8168330192565918, "The Water Points Connection Goal of the Astrocast Satellite Operator is 150 water points in 2022 in Senegal."]
[5.208433151245117, 4.794361591339111, "The Components of the NRD Electronics is Industrial, or in some cases automotive, grade commercial off-the-shelf components."]
[3.912039279937744, 4.431413173675537, "The OBC OS of the Spacecraft Satellite is VxWorks."]
[1.7687020301818848, 4.437092304229736, "The Solar Power Generation of the EPS Electrical Power Subsystem is 48 W."]
[7.657711029052734, 5.446485996246338, "The Cal_solar data Collection of the OCO-2 Satellite is Absolute and Relative Instrument Response Calibration."]
[7.634156227111816, 2.2847142219543457, "The Purpose of the Mars Terrain Simulator Simulator is Validate and simulate ExoMars Rover Operations and to support the ExoMars Surface Mission."]
[7.762491226196289, 3.8314614295959473, "The Acceleration of the Getz Glaciers Glaciers is Almost 25% on average."]
[12.031937599182129, 4.476415634155273, "The Hypothesis of the Blue Ring Nebula Nebula is Composed of debris from two stars that collided and merged into a single star."]
[8.583560943603516, 6.810264587402344, "The Instrument Type of the MFI Magnetometer is Dual triaxial fluxgate magnetometers."]
[1.8042120933532715, 4.024046421051025, "The Number of Cells of the Photo-Voltaic Array Power Generation is 25 strings, 18 cells per string."]
[5.275157451629639, 2.4030954837799072, "The Manufacturer of the CubeStack Multi CubeSat Adapter is LoadPath LLC of Albuquerque, NM."]
[9.214200973510742, 7.7324113845825195, "The Measurement Range of the EIS Sensor is ~45 keV to 500 keV."]
[7.29358434677124, 7.766657829284668, "The Geometric Accuracy of the Atmospheric Correction Processor Image Processing is ~10 m RMSE linear."]
[1.4839857816696167, 4.328371524810791, "The Connection of the BCR Battery Charge Regulator is One half of the solar cell strings on two opposite sides of the spacecraft."]
[6.312220573425293, 2.669809103012085, "The Partner Levels of the Planet Orbit Partner Program is Gold and Platinum."]
[8.436418533325195, 8.949341773986816, "The Number of Detectors of the Scanner Assembly Instrument is 96."]
[9.263648986816406, 4.18172025680542, "The Lower Tray Height of the SUNSAT Satellite is 12 cm."]
[7.746135711669922, 0.97626131772995, "The Application Date of the Sentinel-5P Satellite is 17 September 2020."]
[9.23342514038086, 3.1689951419830322, "The Orbit of the SeaHawk-1 CubeSat is Sun-synchronous."]
[4.87479305267334, 1.0014163255691528, "The Funding Status of the Worldview Legion Satellite Constellation is Fully able to fund."]
[3.2302794456481934, 4.8906660079956055, "The Memory Storage of the CPU Board Processor is 128 MB of DRAM for data memory storage and cache memory storage."]
[10.392268180847168, 2.939790725708008, "The Altitude of the BEESAT-4 CubeSat is 515 km."]
[9.757493019104004, 3.0124943256378174, "The Trajectory of the Periselene-1 Spacecraft is One loop around the Earth with perigee > 100,000 km altitude."]
[8.39510440826416, 9.266115188598633, "The IFOV diameter of the Spectrometer Spectrometer is 14 km."]
[11.573208808898926, -0.8228347897529602, "The Instrument Support Capacity of the Bus Satellite Component is Up to 206 kg."]
[7.125132083892822, 4.9978156089782715, "The Microwave Scatterometer of the HY-2A Satellite Satellite is Unknown."]
[5.27837610244751, 7.354381561279297, "The Data Volume of the Mini-RF Instrument is 200 GB."]
[9.435362815856934, 0.3887859582901001, "The Design Life of the QZS-1 Satellite is > 10 years."]
[5.360078811645508, 5.681798934936523, "The GPS Receiver of the KOMPSAT-6 Satellite is Dual-frequency GPS receiver for POD generation."]
[5.857921600341797, 6.7721991539001465, "The Sigma 0 Range of the Radar Radar is HH, VV: +15~-25 dB."]
[9.514226913452148, 1.0476189851760864, "The Orbit Duration of the International Gamma-Ray Astrophysics Laboratory Satellite is 1 Year."]
[9.810086250305176, 4.15628719329834, "The Reentry Outcome of the Drag Sail Satellite Component is Disintegrate."]
[4.252575874328613, 5.738903999328613, "The TT&C Uplink of the QSat Satellite is S-band, 1 kbit/s."]
[11.664400100708008, -1.1349960565567017, "The Mass of the Spacecraft Satellite is 47 kg."]
[11.208078384399414, 4.492518424987793, "The Speed of the Material from Exploded Star Unknown is Faster than 20 million miles per hour."]
[5.704388618469238, 2.5042686462402344, "The Manufacturer of the Eutelsat Quantum Satellite is Airbus Defence and Space and Surrey Satellite Technology Limited."]
[7.981412887573242, 5.498223304748535, "The SNR at Maximum Radiance of the Satellite Imaging Satellite is 100."]
[7.225451946258545, 0.4465475082397461, "The Launch Date of the ALL-STAR Satellite is 18 April 2014."]
[8.497122764587402, 9.354226112365723, "The IFOVs of the Detectors Photovoltaic Detectors is 14 km."]
[9.067500114440918, 5.608625411987305, "The Gyroscope of the Pico Dragon CubeSat is 3-axis."]
[7.565830230712891, 9.060249328613281, "The Total Channels of the Spectral Bands Spectrometer is 1305."]
[3.8026936054229736, 4.304601669311523, "The CPU of the C&DH Subsystem Command & Data Handling is RAD750."]
[5.798854827880859, 6.830343723297119, "The NESZ of the Radar Instrument is -29 dB."]
[7.395183086395264, 8.857176780700684, "The Spatial Resolution of the Spectral Channels Satellite Instrument is 28 \u00b5rad (1 km x 1 km at nadir) (+0-10%)."]
[12.099702835083008, 3.288485050201416, "The Inclination of the Tandem-L satellites Satellite is 98.4\u00ba."]
[4.715732097625732, 5.764491081237793, "The Number of RF Signals of the Antenna Subsystem Satellite Component is 6."]
[5.181758403778076, 3.1234638690948486, "The AIS Receiver of the NorSat-3 Satellite is ASR x50."]
[5.094655990600586, 5.262583255767822, "The Number of Antennas of the KSAT Ground Station Network is Over 200."]
[7.76576042175293, 3.649669647216797, "The Design Approach of the Constellation Satellite System is Low cost and low risk, doesn't sacrifice performance."]
[4.833345413208008, 0.9499362111091614, "The Budget of the Copernicus Programme Satellite Programme is EUR 4.3 billion."]
[4.339993476867676, 2.4787940979003906, "The Active Starlink Terminals Target in India of the Starlink Satellite Internet Service is 200,000."]
[6.5597758293151855, 7.584698677062988, "The Type of the Laser Device is Unknown."]
[4.904411792755127, 1.7606679201126099, "The Number of Holes of the Deployment Specialists Personnel is 86."]
[7.557730197906494, 2.885646343231201, "The Bus Technologies of the KOMPSAT-5 Spacecraft is Enhanced based on previous programs."]
[5.733611583709717, 3.1251490116119385, "The Manufacturer of the Gaia spacecraft Satellite is EADS Astrium."]
[6.735188007354736, 7.183168411254883, "The Status and Performance of the CALIOP Lidar is Unknown."]
[8.011093139648438, 1.125784158706665, "The Image Capture Date of the Earth Observation Satellite Satellite is 25 June 2021."]
[8.181245803833008, 7.774264335632324, "The Calibration Device Quantity of the OMPS Sensor is Two diffusers for each sensor."]
[9.813331604003906, 4.715376377105713, "The Projectile Diameter of the Launcher Test Facility is Up to 203 mm."]
[7.949123382568359, 1.4129048585891724, "The Delivery Date of the FSS Fine Sun Sensor is June 2015."]
[9.17048168182373, 9.139321327209473, "The FPA Size of the Telescope Optical Instrument is 1056 (spatial) x 256 (spectral) pixel."]
[8.946051597595215, 8.108305931091309, "The Absorber Material of the Imaging Calorimeter Calorimeter is Tungsten."]
[8.28122329711914, 1.6023484468460083, "The Mission Completion Date of the Kepler Satellite is Nov. 14, 2012."]
[7.732964038848877, 3.7844576835632324, "The Acceleration of the Getz Glaciers Glaciers is Over 44% for three glaciers."]
[5.003283977508545, 6.524965763092041, "The F/D of the Antenna Communication is 0.8."]
[7.828376770019531, 9.992695808410645, "The Type of Array of the VNIR Detector is Si."]
[11.607008934020996, 5.122565269470215, "The Quasi-Periodic Eruptions (QPEs) Frequency of the GSN 069 Black Hole is Every nine hours."]
[4.1502180099487305, 3.159358263015747, "The Coverage of the 5G Network Telecommunications Network is Global, always-on network."]
[4.044825553894043, 1.1940760612487793, "The Mission Type of the Galileo Satellite Navigation System is Non-EO."]
[6.7971954345703125, 3.2323975563049316, "The Functionality of the HISat Satellite is Complete satellite functionality in a nanosat-scale package."]
[9.561976432800293, 5.609622478485107, "The Attitude Determination Accuracy of the AOCS Attitude and Orbit Control Subsystem is \u2264 0.2\u00ba (3\u03c3)."]
[10.610997200012207, 7.368056297302246, "The | of the NOAA Goes-12 Solar X-Ray Imager Instrument is The NOAA Goes-12 Solar X-Ray Imager (SXI)."]
[8.502350807189941, 7.473974227905273, "The Number of Experiments of the TPMU Device is 3."]
[6.009631156921387, 3.1444332599639893, "The Science Payload Developer of the Neutron-1 Satellite is Arizona State University (ASU)."]
[7.494163990020752, 0.7317195534706116, "The Maneuver Date of the P2 Satellite is Early May 2012."]
[7.718454837799072, 7.494250774383545, "The Observation Contribution of the MAHRSI Instrument is Help quantify the contribution of water vapor exhaust injected into the upper atmosphere from the space shuttle to PMCs."]
[8.928729057312012, 7.484094142913818, "The Purpose of the GRIDS Ion Sensor is Measure the distribution, motion, and velocity of ions."]
[7.963288307189941, 3.4573214054107666, "The Mission Phases of the Solar Orbiter Satellite is Cruise phase and Science phase."]
[7.551595687866211, -0.4739171862602234, "The Booster's Previous Flight Date of the Falcon 9 Rocket is Jan. 20."]
[2.735992908477783, 4.159908771514893, "The Electrical Power System of the IOD-1 GEMS Satellite is CSL FlexU Electrical Power System (EPS)."]
[11.86725902557373, 0.9984056949615479, "The Sample Collection Location of the Chang'e-5 Spacecraft is Siziwang Banner, Inner Mongolia."]
[4.793311595916748, 6.024688243865967, "The Optical Beacons Modulation of the CHOMPTT Satellite is 1 Hz."]
[6.62440299987793, 6.11451530456543, "The Cross-Calibration Partner of the QuikSCAT Satellite is Indian Space Research Organization (ISRO) Oceansat-2 scatterometer known as OSCAT."]
[3.1495378017425537, 6.80296516418457, "The Output Power of the HiSPiCO S-band Transmitter/Transceiver is 27 dBm."]
[7.152687072753906, 6.4179253578186035, "The Flights of the AEPI Instrument is Spacelab-1."]
[7.751753807067871, 8.24326229095459, "The Development Challenges of the Infrared Sounder (IRS) Sounder is 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."]
[5.400420188903809, 0.3066845238208771, "The Burned Area of the Calf Canyon-Hermits Peak Fire Fire is Exceeded 300,000 acres."]
[8.784791946411133, 8.608664512634277, "The Cross-Track of the WAOSS-B Sensor is 50\u00b0."]
[6.249581813812256, 7.075443744659424, "The Function of the DDA Delay-Doppler Altimeter is Measure the along-track position of the range measurement."]
[3.881706476211548, 5.642520904541016, "The Debut Speed of the Iridium Certus Satellite Communication Service is 352 kbit/s."]
[8.174725532531738, 4.535461902618408, "The Resolution of the Satellite GEO (Geostationary Earth Orbit) is \u0394x = 62 km for \u0394\u03b8 = 0.1\u00ba."]
[7.0446648597717285, 1.1298373937606812, "The Presentation Date of the Attitude Control Module Small Satellite Component is August 13-16, 2012."]
[13.173274993896484, 4.020172595977783, "The Data Release Dates of the Gaia Satellite is 2016, 2018."]
[5.676644325256348, 5.501389026641846, "The GPS Receiver of the AOCS Attitude and Orbit Control System is Dual frequency GPS receiver (GPSR)."]
[7.706887245178223, 9.630304336547852, "The Spatial Resolution of the SLSTR Spectral Imaging Instrument is 500 m."]
[2.145163059234619, 4.569512844085693, "The Power of the Satellite Bus Spacecraft Component is Approximately 1.9 kW."]
[7.853079319000244, 8.491312026977539, "The Design Drivers of the ACE-FTS Instrument is Sensitivity (SNR), Spectral Resolution, Large Spectral Coverage."]
[9.243803024291992, 10.335864067077637, "The BW Film Type of the Metric Camera Camera is KODAK Double-X Aerographic Film 2405."]
[8.110213279724121, 4.669336795806885, "The Spatial Resolution of the Solid Earth Lithosphere and upper mantle density structure Satellite is 100 km."]
[8.708900451660156, 4.430543899536133, "The Latitude Observation Point of the SHIMMER Satellite is Around 55\u00ba."]
[7.925885200500488, 7.039820194244385, "The Purpose of the BEAT experiment Ballistocardiography for Extraterrestrial Applications and long-Term missions is Measure an astronaut\u2019s ballistocardiographic data, including pulse and blood pressure."]
[12.136701583862305, 3.317337989807129, "The Inclination of the CICERO-4 Satellite is 85\u00ba."]
[6.576013565063477, 0.6586135625839233, "The Test Date of the SpinSat Satellite is May 21, 2015."]
[3.679330587387085, 6.052313804626465, "The BER (Bit Error Rate) of the Payload Downlink Communication System is <10-9."]
[7.025838851928711, 5.186742782592773, "The Mission of the PanFTS Panchromatic Fourier Transform Spectrometer is GEO-CAPE."]
[6.7667083740234375, 7.259179592132568, "The Manufacturer of the OLA LIDAR Instrument is MDA (MacDonald Dettwiler & Associates) and Optech Inc.."]
[8.555299758911133, 2.328491449356079, "The Project Scientist of the Parker Solar Probe Spacecraft is Nicola Fox."]
[6.598725318908691, 0.8228453993797302, "The Commissioning Completion Date of the DubaiSat-2 Satellite is April 14, 2014."]
[10.887983322143555, 2.008229970932007, "The \u0394RAAN of the Swarm-C (Charlie) Satellite is ~0-135\u00ba difference wrt mean plane of A/B."]
[6.30903959274292, 9.895628929138184, "The Instrument Mass of the Pushbroom imager Optics is 18.5 kg."]
[12.0277681350708, 5.269817352294922, "The Dark Matter Content of the Leo I Galaxy is Not much."]
[9.84025764465332, 9.472882270812988, "The Band-to-Band Alignment of the IRIS Instrument Spectral Scanner is 0.1 pixels."]
[8.670888900756836, 5.336419582366943, "The Robotic Arms of the Satellite Platform is Deployable."]
[5.847464084625244, 8.1270112991333, "The Frequency (GHz) of the ICI-5 Radiometer is 325.15\u00b19.5."]
[10.090225219726562, 3.1324868202209473, "The Longitude of the Meteosat-7 Satellite is 57.5 \u00b0E."]
[5.201414585113525, 3.088634967803955, "The Function of the Juventas CubeSat CubeSat is Perform the first radar probe of an asteroid."]
[1.4551849365234375, 4.904049873352051, "The Voltage Output of the PSU Power Supply Unit is 4.1 V for safe battery charging."]
[12.109481811523438, 3.3414418697357178, "The Inclination of the S/C Spacecraft is 80.2\u00ba."]
[10.032797813415527, 1.4835103750228882, "The Orbital Period of the OceanSat-1 Satellite is 99.31 min."]
[4.010312080383301, 6.537242412567139, "The AGC Time Constant of the Receiver Communication System is \u2264 40 x10 -9 ms."]
[2.2536182403564453, 4.459474563598633, "The Power of the Payload Satellite Subsystem is 3.5 W."]
[9.085302352905273, 7.307010173797607, "The Quantity of Faraday Cup Ion Detectors of the SWE Instrument Sensor is 2."]
[12.12659740447998, 3.341498374938965, "The Inclination of the Satellite SuperView Constellation is 98\u00ba."]
[8.532369613647461, 8.105728149414062, "The Type of the ULEIS Spectrometer is Time-of-flight (TOF) mass spectrometer."]
[4.973816394805908, 4.498995304107666, "The Ordering follow-up of the CSK GS Ground Segment is Allow the FM to keep S-IM informed about the progression of the order."]
[9.741186141967773, 3.8947501182556152, "The Deployment Timing of the CanX-7 Drag Sail Payload is End of a six-month phase of secondary payload operation."]
[10.166173934936523, 3.0359227657318115, "The Orbit Altitude of the JAWSAT Satellite is 753 km x 805 km."]
[3.010828971862793, 6.690756797790527, "The RF Output Power of the X-band Transmitter Transmitter is 6 W."]
[1.3849120140075684, 4.18769645690918, "The Maximum Battery Power Before 100% Depletion in Orbits of the Satellite Spacecraft is 2 orbits."]
[11.333240509033203, 6.724879264831543, "The Number of X-ray mirror module assemblies of the IXPE observatory X-ray Observatory is 3."]
[7.026188373565674, 2.5529181957244873, "The URL of the AstroSat Satellite is http://www.tifr.res.in/~laxpcworkshop14/presentations/LAXPC_WORKSHOP%20%20_3-k%20s%20sharma.pdf."]
[7.203122138977051, 0.8961790800094604, "The Launch Date of the Integral Satellite is 2002."]
[8.269526481628418, 3.1349117755889893, "The Mission Observation Period of the TanDEM-X Satellite is 21 September 2017 until June 2020."]
[4.9161787033081055, 1.0283377170562744, "The Funding Requirement of the 90-satellite constellation Satellite Constellation is Another equity funding round, cash flow from operations and debt."]
[6.224881172180176, 7.792359828948975, "The Polarization of the ICI-2 Radiometer is V."]
[10.19459342956543, 1.8118473291397095, "The Orbit Period of the Beijing-3B Satellite is 96.8 minutes."]
[9.272290229797363, 10.193998336791992, "The Field of View of the WAC Wide-Angle Camera is Large portions of Europa's landscape."]
[10.779230117797852, 3.4717178344726562, "The Distance from Sun of the Solar Orbiter Satellite is Roughly 75 million km."]
[10.716935157775879, 7.365347385406494, "The Energy Range of the CXBN-2 X-ray Detector is 30-50 keV."]
[8.16492748260498, 4.024144172668457, "The Orbit Type of the SWFO-L1 Satellite is L1."]
[7.287286758422852, 2.572742462158203, "The URL of the Magnetospheric Multiscale Mission Satellite is https://www.nasa.gov/feature/goddard/2018/nasa-s-magnetospheric-multiscale-mission-locates-elusive-electron-act."]
[6.823019504547119, 3.146970748901367, "The Mission Status of the Resurs-P1 Satellite is Operational."]
[12.905062675476074, 4.789721965789795, "The Apogee of the IBEX Spacecraft is 319,000 km."]
[8.815812110900879, 8.144916534423828, "The Cu Foil Thickness of the RADFET Dosimeters Dosimeter is 50 \u00b5m."]
[8.718489646911621, 1.5239249467849731, "The Detection of the Van Allen Probes Satellite is Increased number of even higher energy electrons."]
[5.99639368057251, 3.0317177772521973, "The Prime Contractor of the SloshSat-FLEVO Satellite is NRL (National Aerospace Laboratory)."]
[7.37758207321167, 8.00190544128418, "The Area in 2016 of the Ozone Hole Atmospheric Phenomenon is 23 million km2."]
[10.38729190826416, 7.703793525695801, "The Material of the Outer Shield Instrument Component is Aluminum."]
[10.232548713684082, 6.806362152099609, "The Total Number of Solar Cells of the TCS Thermal Control System is 190."]
[10.196048736572266, 1.0457390546798706, "The LTDN of the Aalto-1 Satellite is 9:30 hours."]
[10.394003868103027, 4.93341064453125, "The Water Capacity of the Steam Propulsion Unit Propulsion is Up to 30 grams."]
[6.034386157989502, 9.629015922546387, "The Mass of the Instrument Satellite Instrument is 15 kg."]
[4.953743934631348, -3.1233150959014893, "The Affiliation of the Yuji Sakamoto Author is Unknown."]
[7.9450483322143555, 5.476938247680664, "The Calibration Activities of the GCOM-C Satellite is On-orbit."]
[12.128853797912598, 3.293531894683838, "The Inclination of the Satellite HY-1B is 98.8\u00ba."]
[8.889379501342773, 4.958022594451904, "The Reaction Wheels of the NEMO-AM Satellite is Quantity: 3, Manufacturer: SI, Momentum Storage: 60 Nms, Maximum Torque: 2 mNm, Maximum Torque Jitter: 5 x 10-5Nm."]
[5.0053911209106445, 6.57632303237915, "The Measurement of the HGA High Gain Antenna is HGA gain."]
[5.601274013519287, 1.5725680589675903, "The Booster of the Falcon 9 Rocket is B1060."]
[5.80208158493042, 8.113178253173828, "The Bandwidth (GHz) of the ICI-5 Radiometer is 6."]
[10.223531723022461, 5.078180313110352, "The Position of the VACCO MiPS cold gas thruster Thruster is Aft end (\u2013y)."]
[7.352099418640137, 9.968480110168457, "The Spectral Coverage of the Hyperion Imaging Spectrometer is 400 - 2500 nm."]
[10.454499244689941, 2.618281841278076, "The Apogee of the FASat-Alfa Satellite is 682 km."]
[4.776748180389404, 0.8951815962791443, "The Cost of the Prometheus Block 2 CubeSats Satellite is Less than $100,000."]
[7.294118881225586, 4.570422172546387, "The Imaging System of the NewSat Satellite is Multispectral imager."]
[6.285670280456543, 4.242157936096191, "The Data Processing of the Satellite Satellite is Real-time."]
[9.606197357177734, 7.7648234367370605, "The Bias Voltages of the EPE Energetic Particle Experiment is 1.25-1.5 times the values required for full depletion."]
[9.045883178710938, 1.126906394958496, "The Map Production Time of the SMOS Satellite is Within 24 hours."]
[6.729950428009033, 7.460109710693359, "The Operational Modes of the MIRAS Instrument is Dual-polarization or full-polarimetric."]
[9.607319831848145, 0.6964569687843323, "The Orbit Life Without Balloon of the AeroCube-3 Satellite is 1-3 years."]
[3.5424041748046875, 4.513096809387207, "The ROM/RAM of the SHU Science Handling Unit is EEPROM(128KB x 2), SRAM(8MB x 4), FROM(128MB)."]
[6.941771507263184, 0.02779310755431652, "The End of Life Date of the GEOSAT Satellite is January 1990."]
[9.424931526184082, 9.118572235107422, "The Effective Area of the Telescope Optical Instrument is ~ 15 cm2 for FUV channel, 15-40 cm2 for NUV & VIS channels."]
[9.216708183288574, 1.7653664350509644, "The Inputs of the Active Schedule Planning Product is Mission Timeline, LMOC downtimes, OGS availability schedules, external interfaces availability, predictive avoidance constraints, experiment plans, user service requests."]
[1.3409005403518677, 4.126572132110596, "The Battery of the IOD-1 GEMS Satellite is CSL 30 Whr Battery."]
[8.87686538696289, 9.118938446044922, "The Separation Distance of the Slits Optical Instrument is 4.5 mm."]
[8.649609565734863, 10.786596298217773, "The Power of the LISS-4 Camera is 216 W."]
[8.133027076721191, 7.7015700340271, "The Purpose of the MGF Instrument is Measure deviations of the magnetic fields during space storms."]
[7.9576945304870605, 3.1828081607818604, "The Status of the X-SAT Satellite is Functioning Satisfactorily."]
[9.119568824768066, 9.21872329711914, "The Field of View of the ELENA Instrument is Nadir pointing 1-D FOV."]
[8.351656913757324, 8.18656063079834, "The Effective Area of the EUV Simulation Simulation is 43 cm2."]
[6.165670871734619, 5.835583209991455, "The Data Used of the DInSAR Differential SAR Interferometry is TOPS (Terrain Observation with Progressive Scan)."]
[9.740248680114746, 3.8562302589416504, "The Drag Sails Deployment Date of the CanX-7 Satellite is May 3, 2017."]
[8.499815940856934, 8.47158145904541, "The Absolute Solar Shape Precision of the Instrument Optical Instrument is Better than 10 marcsec (milli-arcseconds)."]
[9.387365341186523, 5.736779689788818, "The Hardware of the ACS Attitude Control System is Controlled by ACS flight software."]
[6.496426582336426, 4.054624557495117, "The Acquirer of the JPSS-1 Satellite is NOAA (National Oceanic and Atmospheric Administration)."]
[8.101838111877441, 1.4822341203689575, "The Mission Date of the Solar Probe Plus Satellite is Sept. 27-Oct. 1, 2010."]
[9.574152946472168, 5.969651222229004, "The Attitude Control of the ADCS Attitude Determination and Control Subsystem is Magnetorquers and reaction wheels."]
[6.947544097900391, 0.8396136164665222, "The Re-entry Date of the Satellite Satellite is 8 December 2011."]
[8.280745506286621, 3.091862916946411, "The Complete Global DEM Availability Date of the TanDEM-X Satellite is September 2016."]
[6.8067097663879395, 3.8954615592956543, "The Applications of the Sich-2 Satellite is 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."]
[7.796135425567627, 2.6392812728881836, "The Data Collection of the Rosetta Satellite is Comet's dust, gas and plasma environment, its surface characteristics and its interior structure."]
[4.981281280517578, -0.12994083762168884, "The Partial Services Start Year of the OneWeb Low-Earth-Orbit Broadband Venture is 2021."]
[10.234062194824219, 9.424969673156738, "The Spatial Resolution of the IRIS Observatory is Between 0.33 and 0.44 arcseconds."]
[9.34370231628418, 9.452994346618652, "The Pupil Diameter of the NAOMI Imager is No longer sized to comply with SNR requirements."]
[9.464347839355469, 8.716429710388184, "The Protective Layer of the FPI Mirrors Component is 50 nm layer of silicon dioxide (SiO2)."]
[9.557304382324219, 0.8772498965263367, "The Technology Demonstration Phase Duration of the GomX-4B Satellite is 6 months."]
[9.757040977478027, 1.4508469104766846, "The Anomaly Investigation Duration of the NextSat Satellite is Additional week."]
[12.163599014282227, 2.20621395111084, "The TAG Date of the OSIRIS-REx Spacecraft is Up to asteroid departure in March 2021."]
[11.718878746032715, -1.1410541534423828, "The Mass of the Spacecraft Satellite is 2120 kg."]
[9.13265323638916, 4.086919784545898, "The Size of the PhiSat-1 Satellite is About the size of a cereal box."]
[5.409613132476807, 4.173198223114014, "The Responsibilities of the MC Mission Center is 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."]
[6.268919467926025, 9.82652759552002, "The Mass of the Geoton-L1 imager Instrument is 310 kg."]
[7.020529270172119, 1.7875144481658936, "The Tandem Mission End Date of the Envisat / ERS-2 SAR Satellite is Late April 2009."]
[6.614903450012207, 3.1337950229644775, "The Design of the Resurs-P Satellite is Modular."]
[7.568597316741943, 1.7703391313552856, "The Collision Date of the A-74 iceberg Iceberg is 19 May 2021."]
[6.4237799644470215, 4.579593181610107, "The Product Type of the Sentinel-1 Satellite is GRD (Ground Range Detected)."]
[7.7734479904174805, 7.977766513824463, "The Purpose of the Spectrometer Instrument is Separation of atmospheric extinction along the line-of-sight due to Rayleigh scattering, aerosols, ozone, nitrogen dioxide, water vapor concentration profiles, and aerosol detection."]
[8.707595825195312, 8.086213111877441, "The Function of the NuDose ASIC is Force a specified current through the RADFET."]
[5.318464756011963, 10.394108772277832, "The Location of the LIS Lightning Imaging Sensor is ISS."]
[5.9896016120910645, 9.606300354003906, "The Total Mass of the HREP Instrument is 381 kg."]
[9.740653038024902, 1.5526562929153442, "The Repeat Cycle of the OceanSat-1 Satellite is 2 days."]
[4.770620346069336, 9.131263732910156, "The Seismometer Deployment Date of the InSight Lander Lander is December 19, 2018."]
[7.741872310638428, 7.672417163848877, "The Measurement of the OCO-3 Instrument is CO2 Mole Fraction."]
[5.49922513961792, 3.487046480178833, "The Manufacturer of the ERNO-Box Computer is Astrium Space Transportation in Germany."]
[6.184658527374268, 3.0122289657592773, "The Developing Entity of the MoonLIGHT Satellite is Italian National Institute of Nuclear Physics (INFN) in Frascati."]
[6.21029806137085, 3.2296321392059326, "The Participating Countries of the Euclid Mission Consortium Consortium is Italy, France, Germany, Denmark, Portugal, Spain, The Netherlands, Norway, Romania, United Kingdom, Finland."]
[3.5333375930786133, 4.590930461883545, "The Type of the First FPGA FPGA is GNSS receiver core functions."]
[10.392861366271973, 4.856326103210449, "The Total Firings of the LM thruster Thruster is More than 85."]
[7.154362678527832, 4.585113048553467, "The Measurement of the SKIM Satellite Mission is Ocean-surface currents."]
[1.2691833972930908, 4.293498516082764, "The Function of the Battery Holder Electrical Power Subsystem is Battery control, battery overcharge protection and bus voltage regulation."]
[6.855623722076416, 1.6715606451034546, "The Launch Date of the Kleos Scouting Mission (KSM1) Satellite is November."]
[6.128566741943359, 5.986838340759277, "The Ground Resolution (ScanSAR mode) of the XSAR SAR is Varying between 8 m and 20 m."]
[4.92097806930542, -3.2110719680786133, "The | of the Juan Yin, Yuan Cao, Yu-Huai Li, Ji-Gang Ren, Sheng-Kai Liao, Liang Zhang, Wen-Qi Cai, Wei-Yue Liu, Bo Li, Hui Dai, Ming Li, Yong-Mei Huang, Lei Deng, Li Li, Qiang Zhang, Nai-Le Liu, Yu-Ao Chen, Chao-Yang Lu, Rong Shu, Cheng-Zhi Peng, Jian-Yu Wang, and Jia Authors is | False."]
[3.6474978923797607, 4.810417175292969, "The Clock Frequency of the dsPIC33F microcontroller Microcontroller is Unknown."]
[3.458158016204834, 4.902176856994629, "The Storage Capacity of the Spacecraft 406 MHz Processor Processor is 324 kbit."]
[6.907020568847656, 1.031131625175476, "The Announcement Date of the SmallGEO Extension Satellite Extension is Sept. 30, 2011."]
[6.029531478881836, 4.301756858825684, "The Operator of the Canadarm2 Robotic Arm is Astronauts."]
[3.7277019023895264, 6.083765029907227, "The Duration of the TTTC Imaging System is Longer than the data take itself."]
[11.467806816101074, 6.0006022453308105, "The Anomaly Date of the Chandra X-ray Observatory X-ray Observatory is Aug. 24."]
[8.771925926208496, 10.35672664642334, "The Analog Outputs of the GOCI-II CMOS Imaging Sensor CMOS Imaging Sensor is 10."]
[10.100086212158203, 2.868028402328491, "The Orbit Altitude of the Odin Satellite is 600 km."]
[5.894223213195801, 9.517215728759766, "The Mass of the TriG GNSS-RO payload Instrument is 115 kg."]
[8.506620407104492, 8.458759307861328, "The Guard Angle of the MXT Instrument is 20\u00b0."]
[11.742463111877441, 7.504703998565674, "The Stability of the DSAC Clock is 100 times more stable than today's best navigation clocks."]
[8.47663402557373, 9.851261138916016, "The Number of Channels of the Interferometer Arrays Imaging Technology is Same as a digital camera."]
[7.055467128753662, 0.8793131113052368, "The Launch Date of the OPAL Satellite is Jan. 27, 2000."]
[9.610215187072754, 4.202813625335693, "The Length of the Genesis-2 Spacecraft is 4.4 m."]
[6.691093444824219, 4.605841159820557, "The Instruments of the HJ-1 Satellite is S-Band SAR."]
[9.630352973937988, 5.918442249298096, "The Pointing Accuracy of the ADCS Attitude Determination and Control Subsystem is \u2264 0.1\u00ba (triaxial, 3\u03c3)."]
[8.69055461883545, 6.952292442321777, "The Quantity of the Magnetic Field Sensor Sensor is 5."]
[8.248771667480469, 5.400369167327881, "The Surface Accuracy Goal of the Reflector Assembly Satellite Component is 1.0 mm rms."]
[10.390592575073242, 4.603096008300781, "The Propellant Duration of the Butane Propulsion System Propulsion System is 3-4 years."]
[10.462416648864746, -1.136499047279358, "The Mass of the CINEMA-2 Nanosatellite is 4 kg."]
[8.801526069641113, 0.7281744480133057, "The Mission Objective of the Juice Spacecraft is Study the potential habitability and the underground oceans of Ganymede, Callisto and Europa."]
[6.736537456512451, 1.522902011871338, "The Presentation Date of the RapidEye Earth Observation Constellation is Sept. 29 to Oct. 3, 2008."]
[5.060309410095215, 4.191749095916748, "The Management of the CTDA Component is Counts with a central management point for the tasking and cataloguing of information."]
[9.300848007202148, 0.7098692655563354, "The Mission Lifetime of the EarthDaily Constellation Satellite Constellation is 10 years."]
[10.065786361694336, 4.15352725982666, "The Thrust Source of the LightSail-2 Spacecraft is Solar sails."]
[5.322664737701416, 1.6513649225234985, "The Upper Stage Payloads of the Rocket Launch Vehicle is 114."]
[7.247934341430664, 2.3410935401916504, "The URL of the Jaan Praks Person is https://web.archive.org/web/20160304222738/http://tstc2014.to.ee/download/m5429b9e5144f8."]
[8.053540229797363, 9.528414726257324, "The Filter Spectral Bands of the EXI instrument Imaging Instrument is UV1: 245-275 nm, UV2: 305-335 nm Blue: 427-447 nm, Green: 536-556 nm, Red: 625-645 nm."]
[3.2838635444641113, 6.700662612915039, "The Power Consumption of the Myriad RF board RF Board is > 4 W."]
[8.0384521484375, 8.634857177734375, "The Sweep Duration of the FTS Interferometer Interferometer is 2, 1, 0.5, 0.1 s."]
[4.972290992736816, 4.1480183601379395, "The Components of the Antenna/Drive/Calibration Subsystem Subsystem is Conical corrugated horn-fed shrouded reflector, multiplexer, closed-loop antenna scan drive assembly and closed path calibration assembly."]
[6.948782444000244, 5.993130683898926, "The Measurement of the ALACE Floats Oceanographic Instrument is Global subsurface circulation."]
[7.607208728790283, 5.376586437225342, "The Components of the OCO-2 MIP Project is Four different transport models with varying configurations, multiple different data assimilation frameworks, and diverse prior fluxes and uncertainties."]
[6.837597846984863, 1.2203460931777954, "The Presentation Date of the COMS Satellite is July 12, 2005."]
[8.016219139099121, -0.7194305062294006, "The Berthing Date of the Dragon spacecraft Spacecraft is 2 July 2018."]
[3.973285675048828, 2.377549648284912, "The Cion Size of the CICERO-6 6U CubeSat is 30 x 10 x 6 cm."]
[7.608128070831299, 7.284785270690918, "The Additional Calibration of the Mini-RF Instrument is Conducted on the flight instrument during thermal vacuum temperature ramp cycles."]
[11.313411712646484, 6.732989311218262, "The Measurement Capability of the NICER X-ray Instrument is Cooling histories of young neutron stars."]
[12.007527351379395, 3.2668135166168213, "The Inclination of the Secondary Payloads Unknown is 69.5\u00ba."]
[4.8753275871276855, 4.844594478607178, "The Purpose of the Wireless Compose-2 Wireless Network Infrastructure is Conduct and execute low-power, low-weight, and wireless experiments on the International Space Station (ISS)."]
[7.481226444244385, 1.7962526082992554, "The In-Orbit Calibration Plan Presentation of the Microscope Space Mission is Sept. 23-27, 2013."]
[9.141345977783203, 10.109816551208496, "The Function of the NAC Camera is Highlights variations in soil moisture content and vegetation density."]
[9.123868942260742, 5.715120792388916, "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."]
[6.744040489196777, 4.169187545776367, "The Data Usage of the Satellite Earth Observation Satellite is Critical role in the resiliency mindset."]
[7.231374740600586, 5.421446800231934, "The Location of the WIND Satellite is L1 halo upstream of Earth."]
[6.218418598175049, 5.897531986236572, "The Observation Modes of the StriX-\u03b1 SAR Satellite is Stripmap and Sliding Spotlight mode."]
[5.274850845336914, 3.9156980514526367, "The Purpose of the Remote Agent Software is Reduce the cost of future S/C operations."]
[6.62769079208374, 0.41716036200523376, "The Image Release Date of the SMART-1 Satellite is Sept. 29, 2014."]
[5.9554924964904785, 6.644195079803467, "The Detection Capability of the Satellite-based Radar Radar is Ripples and splashes caused by falling raindrops."]
[9.356204986572266, 0.75238037109375, "The Program Duration of the SOHLA-1 Satellite is 5 years."]
[8.157156944274902, -0.0547381229698658, "The Docking Time of the Starliner Spacecraft is 26 hours after launch."]
[7.2909746170043945, 5.495800971984863, "The Data Impact of the Aeolus Satellite is Positive impact of the data obtained in 2019 was roughly twice as big as it is now."]
[10.013175010681152, 1.4433234930038452, "The Orbit Period of the SuperView-1 01 and Superview-1 02 Satellite is 97 minutes."]
[12.113446235656738, 3.2892520427703857, "The Orbit Inclination of the Argos-4 Satellite Instrument is 98\u00ba."]
[6.086867809295654, 2.4212045669555664, "The Primary Payload of the NROL-36 Satellite is NRO/MSD classified spacecraft."]
[7.92430305480957, 4.5389275550842285, "The Spatial Resolution of the SLIM6 Satellite is 32 m GSD."]
[7.285754203796387, 7.373534679412842, "The Same Instrument as of the MAHRSI Instrument is STS-66 mission (CRISTA-SPAS-1)."]
[3.4272801876068115, 6.461166858673096, "The Quantity of the MnACQ-2000 Miniature Network Data Acquisition System Data Acquisition System is 9 units."]
[4.2612481117248535, 6.614776611328125, "The Frequency of the Unit Communication System is 435 MHz."]
[8.614840507507324, 9.60374927520752, "The Field of View of the EXI instrument Imaging Instrument is 19.0\u00ba."]
[11.493036270141602, 2.142171621322632, "The Solar Conjunction Operation Period of the Hayabusa-2 Spacecraft is Late November 2018 until the end of December 2018."]
[9.508292198181152, 0.6434662938117981, "The Passes in 1-year mission lifetime of the Satellite Satellite is ~1000."]
[7.973519802093506, 9.456076622009277, "The Wavelengths of the PACS Far-infrared camera is 70 \u00b5m (blue)."]
[9.193899154663086, 4.125490665435791, "The Size of the RainCube Satellite is About the size of a cereal box to a toaster oven."]
[6.055662631988525, 3.3332695960998535, "The Bus Integration and Testing Location of the Neutron-1 Satellite is Hawaii Space Flight Laboratory (HSFL)."]
[7.718515396118164, 0.5097824335098267, "The First Flight Date of the SLS Rocket is 2020."]
[3.6898810863494873, 4.655544281005859, "The Processor of the MPM Main Processor Module is LEON2-E Sparc V8 processor."]
[4.027734756469727, 4.329339981079102, "The Software of the OBC On-Board Computer is FCS (Flight Control Software)."]
[9.924681663513184, 4.058764457702637, "The Mission Status of the NanoSail-D2 Solar Sail is Active."]
[12.962806701660156, 4.841487407684326, "The Mission of the IBEX Satellite is Interstellar Boundary Explorer."]
[4.446183681488037, 6.418424129486084, "The Modules of the TTC Rx Receiver is LNA (Low Noise Amplifier), 208F Frequency Synthesiser, 10M7 Phase Detector, Power Supply."]
[6.745452404022217, 8.482263565063477, "The Spatial Resolution of the MSU-SK Radiometer is 600 m (TIR)."]
[8.990464210510254, 9.127262115478516, "The FOV of the CIRiS Instrument is 12.2\u00ba x 9.2\u00ba."]
[7.240426540374756, 4.332170486450195, "The Sensor complement / remarks of the Intercosmos- Bulgaria 1300 (Intercosmos-22) Satellite is Bulgarian sensors on Meteor-2 satellite technology (ionospheric plasma and high-energetic fluxes of charged particles, electric and magnetic fields, etc.)."]
[4.640254974365234, 4.630841255187988, "The Communication Protocol of the Ground Software Architecture System is TCP/IP."]
[6.387498378753662, 2.168275833129883, "The Launch Provider of the TecSAR Satellite is Indian PSLV."]
[4.595763683319092, 5.701560974121094, "The RF Communications Band of the Kanopus-V 1 Satellite is X-band."]
[5.573416709899902, 1.8327499628067017, "The Conference Location of the Trailblazer CubeSat is St. Louis, Missouri, USA."]
[5.218016624450684, 1.4774926900863647, "The Number of Operational RAFS Clocks of the GIOVE-A Satellite is 1."]
[9.102472305297852, 5.016376972198486, "The Spin Frequency of the Myriade series spacecraft Satellite is Orbital Frequency."]
[10.376836776733398, 4.747184753417969, "The Default Propulsion Module of the Myriade Bus Satellite Bus is Hydrazine propulsion module provided by Airbus Defense and Space."]
[6.937066555023193, 4.12349796295166, "The Future Mission of the GEO-CAPE Geostationary Coastal and Air Pollution Events satellite is Yes."]
[9.427708625793457, 5.894214153289795, "The In-Flight Pointing Control Accuracy of the EFI (Electrical Field Instrument) Instrument is 5\u00ba."]
[3.822685480117798, 4.3147735595703125, "The Processor of the Controller card C&DH Subsystem Component is PowerPC processor."]
[11.628875732421875, -1.1825639009475708, "The Dry Mass of the EAGLE ESPAStar Satellite is 430 to 470 kg."]
[5.815654277801514, 2.8073391914367676, "The Contract of the Thales Alenia Space Company is Won the first Spacebus Neo commercial satellite contract for a Broadband for Africa mission with Eutelsat (BB4A) to be launched in 2019."]
[4.410247802734375, 5.579160213470459, "The Data Transmission Mode of the Satellite Imaging Satellite is Direct transmission (DD)."]
[7.955916404724121, 9.670382499694824, "The MWIR Band of the OHIS Imaging System is Cancelled in 2000."]
[8.03872299194336, 1.1162747144699097, "The Release Date of the Figure 7 Image is Sept. 29, 2015."]
[5.534550189971924, 3.600910186767578, "The Accommodation Location of the Scientific Payload Satellite Payload is North Radiator Panel."]
[5.471865177154541, 3.512057304382324, "The Micro-Switch Location of the ISM Satellite Component is Adjacent to the ISM."]
[5.580904960632324, 0.4511483311653137, "The 2022 Fires of the U.S. Drought Monitor Report is 211."]
[5.288796424865723, 2.570371627807617, "The Data Speed Options of the Iridium Certus Satellite Communication Service is Multiple."]
[8.869592666625977, 2.7761242389678955, "The Support of the LRO Satellite is Future human missions to the moon."]
[10.327669143676758, 3.0589065551757812, "The Orbit Altitude of the Hubble Satellite is 350 miles."]
[6.636963367462158, 4.677794456481934, "The Data Contribution of the Sentinel-6 Satellite is Sea state and wind speed measurements."]
[5.656521320343018, 3.6127915382385254, "The Operations Center of the GIOVE-B Satellite is Telespazio's Fucino Space Center in Italy."]
[6.625988483428955, 2.6170036792755127, "The URL of the RADARSAT Constellation Mission Satellite Constellation is http://www.asc-csa.gc.ca/eng/search/images/watch.asp?id=4247."]
[7.452390670776367, 3.1869380474090576, "The Imaging Frequency Band of the KOMPSAT-5 Satellite is X."]
[3.4648993015289307, 4.874220848083496, "The Size of the Spacecraft 406 MHz Processor Processor is 0.034 m3."]
[8.5933837890625, 1.7028089761734009, "The Mission of the Spitzer Space Telescope Telescope is 2003 - 2020."]
[9.539244651794434, 9.108859062194824, "The Primary Diameter of the Telescope Optical Instrument is 120 mm."]
[9.546825408935547, 0.46928247809410095, "The Design Life of the WorldView-1 Satellite is 7.25 years."]
[11.313248634338379, 4.224661827087402, "The Classification of the HAT-P-7 Exoplanet is Hot Jupiter."]
[6.04578971862793, -0.015220957808196545, "The Launch Date of the Galileo FOC satellites Satellite is 22 August 2014."]
[7.296119689941406, 1.4604978561401367, "The IAC Presentation Date of the GMES Sentinel-1 Satellite is Oct. 12-16, 2009."]
[11.748559951782227, 4.446293830871582, "The Age of the Hyades Star Cluster is 600\u2013700 million years."]
[4.7548017501831055, 0.09369322657585144, "The Target Coverage of the OneWeb Satellite Constellation is All regions north of 50 degrees latitude."]
[8.443656921386719, 6.820216178894043, "The Manufacturer of the NewMag Magnetometer is UCLA (C. T. Russell)."]
[3.901387929916382, 4.336243152618408, "The Operating System of the OBC On-Board Computer is CANOE (Canadian Advanced Nanospace Operating Environment)."]
[9.446283340454102, 9.318900108337402, "The Diameter of the Aperture Function Image Processing is D."]
[4.502248764038086, 5.512402057647705, "The Payload Data Downlink of the PRISMA Satellite is X-band."]
[10.432995796203613, -1.1013611555099487, "The Mass of the PACE nanosatellite Satellite is < 2 kg."]
[9.606680870056152, 7.763125419616699, "The Thermally Isolated of the HyperScout\u00ae Telescope Telescope is Yes."]
[8.12401008605957, 8.452733039855957, "The Instrument Concept of the IASI-NG Interferometer is Mertz Interferometer allowing to assess the Self Apodization issue by a Field Effect Compensation."]
[9.545284271240234, 5.497822284698486, "The Stability of the AOCS Attitude and Orbit Control Subsystem is 5 x 10-5 \u00ba/s."]
[4.954758644104004, 3.653169631958008, "The Propulsion System of the MERLIN Satellite is Newly adapted."]
[4.074665546417236, 5.7606682777404785, "The Data Rate of the Satellite Satellite is 100 kbit/s."]
[8.534327507019043, 8.099064826965332, "The Wire Harness Length of the Integrated Sensor Sensor is 500 mm."]
[8.00918197631836, 3.675255537033081, "The Earth Observation Applications of the Aurora Satellite is Energy, mining and defence sectors, oil and gas pipeline monitoring, methane mapping, clean-energy resource exploration, sustainable mining practices and wildfire risk mitigation."]
[6.017269611358643, 9.629661560058594, "The Mass of the MIRAD Instrument is 0.5 kg."]
[9.071511268615723, 7.995206832885742, "The Measurement Error of the Particle Detectors Instrument is < 1%."]
[3.6523654460906982, 6.348250865936279, "The Data Rate of the RF Communications Data Transmission is 280 Mbit/s."]
[12.145543098449707, 2.195101499557495, "The Detection Date of the REXIS Spectrometer is Last fall."]
[4.278979778289795, 4.2635955810546875, "The Manufacturer of the MAC-200 Configuration is Bristol Aerospace."]
[7.970717906951904, 1.4211095571517944, "The Measurement Date of the Solar Storm Natural Phenomenon is February 2014."]
[6.702314376831055, 3.4389147758483887, "The Mission Status of the Sentinel-1 Satellite is Current."]
[12.103795051574707, 2.207160711288452, "The Departure from Bennu of the OSIRIS-REx Spacecraft is Mid-2021."]
[7.8189287185668945, 0.42086082696914673, "The Initial Imaging and Observations Date of the Chandrayaan-2 Satellite is October 22, 2019."]
[7.266976833343506, 7.875709056854248, "The Earth Scanning Time (FDC) of the Instrument Satellite Instrument is Less than 10 minutes."]
[6.464096546173096, 3.374174118041992, "The Operator of the COMS Satellite is Korean Meteorological Association (KMA)."]
[5.707269668579102, 1.7682139873504639, "The Launch Vehicle of the GovSat-1 Satellite is SpaceX Falcon 9 Rocket."]
[4.874480247497559, 5.6129069328308105, "The Signal Frequency of the Ground Station Antenna System Antenna System is 1.2 GHz or 720 MHz."]
[9.311590194702148, 8.948575019836426, "The BRDF Angle of the Telescope Optical Instrument is \u00b140\u00ba."]
[11.98653793334961, 3.422685146331787, "The Inclination of the ISS Space Station is 51.6\u00ba."]
[6.023198127746582, 5.978525161743164, "The Receive Chain Selection of the SAR Instrument SAR Instrument is Chain 1 or 2."]
[9.148367881774902, 8.026673316955566, "The LYSO crystals of the Range Calorimeter Particle Detector is 9."]
[3.5443029403686523, 2.2788662910461426, "The Size of the Eagle-2 ($50SAT) FemtoSat is 2.5U."]
[5.141106128692627, 7.666730880737305, "The Data Compression of the Instrument Spectrometer is DPCM (Differential Pulse Code Modulation) method."]
[9.196906089782715, 4.120405197143555, "The Dimensions of the EIRSAT-1 Satellite is 22 by 10 by 10 cm."]
[9.33984375, 7.748556613922119, "The Detector Cooling of the AVHRR/3 Instrument is <105 K."]
[8.29322338104248, 3.901656150817871, "The Regulatory Body for Satellite Light Pollution of the United States Country is None."]
[11.59634780883789, 4.367000102996826, "The Potential Mass of the White Dwarf Celestial Body is Similar to Jupiter."]
[3.8057689666748047, 5.991765975952148, "The TT&C Uplink Rates of the MERLIN Satellite is 16, 32 and 64 kbit/s."]
[10.555971145629883, 7.379687309265137, "The Requirement of the Candidate Materials Satellite Components is Resistant to the effects of AO."]
[9.172246932983398, -0.6160290837287903, "The Launch Date to ISS of the Flock 1d Nanosatellites is October 28, 2014."]
[4.171781063079834, 5.768632888793945, "The Rates of the Gimbal Satellite Component is 1 rad/s (max)."]
[9.391847610473633, 7.697991371154785, "The Detector Cooling of the FTS Interferometer Interferometer is Passive cooling <100 K."]
[4.535654544830322, 5.666276454925537, "The Ground Monitoring Frequency of the EROS-A Satellite is S-band."]
[4.3418426513671875, 6.158474922180176, "The Monitoring and Control Frequency of the RF Communications System is S-band."]
[11.262507438659668, 3.532766580581665, "The Tail Formation of the McNaught Comet is Two distinct tails: an ion tail carried by the solar wind and a dust tail."]
[6.622198104858398, 3.897787570953369, "The Application of the Satellite-based EO Satellite-based Service is Earth Observation."]
[11.206480026245117, 3.4958925247192383, "The Distance from Comet Center of the NAVCAM Camera is 9.9 km."]
[7.360070705413818, 8.542085647583008, "The IFOV/line (pixels/scan line) of the IRAS Infrared Atmospheric Sounder is 56."]
[6.69563102722168, 2.102277994155884, "The Data Type of the GPM Satellite is Three-dimensional snapshots of drop size distribution."]
[5.074956893920898, 6.265987873077393, "The Connector Type of the Antennas Communication is SMA male."]
[5.6291937828063965, 2.874652624130249, "The Antenna Chips Sales of the Astrocast Satellite Manufacturer is Sells the antenna chips to the clients."]
[7.795384883880615, 8.975111961364746, "The Instrument Payload of the Sentinel-4 Satellite is Passive UVN (Ultraviolet-Visible-Near-Infrared) hyperspectral imaging spectrometer."]
[5.565598487854004, 2.8459255695343018, "The Manufacturer of the Restore-L Satellite is Maxar."]
[8.859451293945312, 7.944672584533691, "The Shielding Material Transparency of the CZTI Instrument is More transparent above 100 keV."]
[7.644866943359375, 8.785223007202148, "The Range of the Solar band Sensor is 0.32 \u00b5m to \u2265 100 \u00b5m."]
[9.019906997680664, 10.743185043334961, "The Calibration Period of the LISS-3 camera Camera is Eclipse period of the satellite pass."]
[8.685942649841309, 1.555922031402588, "The New Discovery of the Van Allen Probes Satellite is Temporary third radiation belt, acceleration energy within the belts themselves, and a nearly impenetrable barrier."]
[4.136834144592285, 6.219662666320801, "The Protocol of the High-speed link Radio Link is AX.25 packet protocol."]
[11.688735008239746, 1.0907964706420898, "The Landing Date of the Zhurong Mars Rover Rover is Last week."]
[8.813809394836426, 3.1344943046569824, "The Orbit of the Satellites Satellite is Geostationary."]
[10.130843162536621, 4.901071548461914, "The Importance of the Stepper Motor Motor is Mission critical part."]
[8.403264999389648, 9.188984870910645, "The Passband of the FUV channel Spectrometer is >125 nm."]
[6.719137191772461, 0.9148458242416382, "The Development Status of the FormoSat-5 Satellite is In process of developing."]
[8.724407196044922, 6.902853965759277, "The Range of the Magnetometers Actuator is \u00b10.2 Am 2."]
[9.987770080566406, 6.732953071594238, "The Handling Safety of the Soft Stack Satellite Assembly is Can be handled safely for thermal cycling."]
[8.423534393310547, 8.45900821685791, "The Detector Elements of the SPIRIT-III Interferometer-Spectrometer is 6."]
[6.510856628417969, 4.794183254241943, "The Measurement Technique of the Sentinel-6 Michael Freilich Satellite is Synthetic aperture radar."]
[6.103126049041748, 3.7633042335510254, "The Software Packages of the GeoSat-2 Satellite is User4EO, Plan4EO, Fly4EO, Control4EO, Track4EO, Archive4EO, Process4EO, Monitor4EO and CalVal4EO."]
[7.189889907836914, 2.859023332595825, "The Action of the UK Committee for Antarctic Place-Names Committee is Named 28 mountains, glaciers and bays after modern-day scientists."]
[6.074035167694092, 2.3361034393310547, "The Chief Scientist of the QUESS Satellite is Jianwei Pan from the University of the Science and Technology of China."]
[10.824891090393066, 1.861496090888977, "The Swarm Size of the Desert Locusts Insect is 1 km2."]
[4.141903877258301, 4.31091833114624, "The Manufacturer of the RAD6000 Flight Processor is Unknown."]
[6.835899353027344, 3.212303638458252, "The Operation Status of the PREMOS Instrument is Continuously operating since the launch, except for mission interruption due to operational constraints."]
[9.541873931884766, 0.49803099036216736, "The Design Life of the Satellite Spacecraft is 10 years."]
[8.852228164672852, 8.344527244567871, "The Velocity Resolution of the ELENA Sensor is Down to 10%."]
[8.910183906555176, 8.199203491210938, "The Calorimeter Diameter of the Microcalorimeter Microcalorimeter is 5.6 cm."]
[8.156196594238281, 8.437159538269043, "The Instrument Elements of the SHIMMER FTS Fourier Transform Spectrometer is Telescope, relay optics, interferometer, CCD camera."]
[1.975056767463684, 4.035675525665283, "The Function of the Space Solar Power System Power System is Collect solar energy, convert it to RF and beam it to a receiving station on the ground for conversion to clean, usable power."]
[4.717806339263916, 7.363903522491455, "The Footprint of the Submillimeterwave receiver Receiver is 5 m."]
[7.768288612365723, 10.297611236572266, "The HRV Channel Detectors of the SEVIRI Spectral Imager is 9."]
[7.831889629364014, 8.87135124206543, "The Radiometric Accuracy of the Spectral Band C Spectrometer is 3."]
[9.228279113769531, 5.324754238128662, "The Control Capability of the Attitude Control System Satellite Subsystem is Full three-axis control."]
[7.241710186004639, 0.6086359024047852, "The Launch Date of the CHOMPTT Satellite is 16 Dec 2018."]
[8.55195426940918, 6.832818031311035, "The Components of the MIAS Magnetometer Package is Overhauser scalar magnetometer (OVM), two fluxgate vector magnetometers (FGM), and two-star imagers."]
[6.251115322113037, 1.801337480545044, "The URL of the Automatic Dependent Surveillance-Broadcast (ADS-B) Surveillance System is http://www.faa.gov/nextgen/implementation/programs/adsb/."]
[7.315253734588623, 7.7517409324646, "The Observation Time of the Band-1 and Band-64 Satellite Instruments is 37.68 seconds."]
[7.680634498596191, -0.2943601608276367, "The Launch Time of the Kounotori Spacecraft is 11:50:49 UTC."]
[7.756931304931641, 9.289651870727539, "The Wavelength of the VIS Visible region of spectrum is 20 nm."]
[7.535484790802002, -0.4145018756389618, "The Launch Date of the Electron rocket Launch Vehicle is November 11, 2018."]
[11.292871475219727, 6.693309307098389, "The Conference Location of the SEXTANT X-ray Timing and Navigation Technology is Kissimmee, FL, USA."]
[12.14426326751709, 2.172883987426758, "The URL of the OSIRIS-REx Asteroid Sample Return Mission is http://arc.aiaa.org/doi/pdf/10.2514/6.2014-1721."]
[10.177886962890625, 2.98773193359375, "The Orbit Altitude of the KSM-1 satellites Satellite is 500 km."]
[10.356393814086914, 9.531275749206543, "The Eclipse-Free Viewing of the IRIS Spacecraft is 7 months per year."]
[6.655064105987549, 3.523080587387085, "The Mission Type of the CAS500 Satellite is EO."]
[7.928060054779053, 4.3848185539245605, "The Resolution of the ICEYE-X1 Satellite is 3 m."]
[8.553943634033203, 8.264870643615723, "The Diameter of the Primary Sensor Sensor is 1/8\u201d."]
[5.99343729019165, 6.373517990112305, "The Channel Imbalance of the Instrument SAR is \u2264-34 dB."]
[8.871438980102539, 2.8666656017303467, "The Meeting Location of the LunaH-Map Satellite is Columbia, Maryland."]
[8.981246948242188, 8.829544067382812, "The Detector Quantity of the TIR Subsystem Imaging System is 50."]
[8.641619682312012, 6.154923915863037, "The Intensity of the Earth's main magnetic field Magnetic Field is Not the same in the north as in the south."]
[8.512053489685059, 6.522430896759033, "The Length of the Current Sheet Magnetic Field Structure is More than 40,000 kilometers."]
[8.783167839050293, 10.414737701416016, "The Pixel Size of the Image Sensor Imaging is 9.0 \u00b5m x 9.0 \u00b5m."]
[8.60405445098877, 6.960858345031738, "The DC Measurement Accuracy of the Magnetometer Instrument is 0.05% of the field in CuPID's orbit."]
[8.708054542541504, 10.724088668823242, "The Noise and Dark Current Performance of the STL-11000M SBIG Camera CCD Camera is Very good even at room temperature."]
[6.0062127113342285, 9.619328498840332, "The Cargo Weight of the CREAM Cosmic-Ray Instrument is 1,258 kg."]
[7.712369441986084, 1.0008385181427002, "The Launch Year of the Sentinel-5P Satellite is 2016."]
[4.409738540649414, 5.761412620544434, "The Ka-band System of the STPSat-6 Satellite is SpaceWire command, control, and telemetry to the spacecraft."]
[7.7904863357543945, 3.939836263656616, "The Sea Ice Coverage of the Global Change Observation Mission 1st \u2013 Water \u201cSHIZUKU\u201d Satellite is 19.47 million km2."]
[8.46646785736084, 7.46700382232666, "The Function of the SES Instrument is Verify that the instrument high voltage performance as expected over temperature."]
[4.077334403991699, 4.090445041656494, "The Components of the Core-DHS Avionics Module is S-band Transmitter and Receiver, Global Positioning System, Attitude & Orbit Control System, Interface Module and Bridge and On Board Computer."]
[8.649160385131836, 5.287517070770264, "The Primary Pointing Reference of the CHOMPTT Satellite is Sun's orientation measured by the sun sensors."]
[5.847588539123535, 6.536942481994629, "The PRF of the SAR Radar is About 9 kHz."]
[6.014368534088135, 2.4547173976898193, "The Launch Vehicle of the GFO Satellite is Taurus launcher."]
[6.1820220947265625, 0.7826407551765442, "The Operation Start Date of the RAVAN Satellite is Jan. 25."]
[10.474164962768555, 2.4718456268310547, "The Apogee (km) of the Meteor-2-1 Satellite is 906."]
[9.012436866760254, 3.2463531494140625, "The Orbit of the Beidou-3M/G/I satellites Satellite is MEO (Medium Earth Orbit) and GEO (Geosynchronous Orbit)."]
[8.273112297058105, 3.2259609699249268, "The Available DEM Geocells of the TanDEM-X Satellite is Over 15,000 geocells or nearly 80%."]
[4.249075889587402, 5.14404296875, "The ICDS Redundancy of the ARTEMIS Satellite Subsystem is All units have a redundancy."]
[6.63838529586792, 7.768373012542725, "The Output Energy of the GEDI Laser Laser is 10 mJ."]
[9.476189613342285, 9.280109405517578, "The Diameter of the Entrance Pupil Optical Component is 320 mm."]
[7.258419513702393, 1.2093677520751953, "The Milestone Date of the EGNOS V3 Satellite System is March 28, 2017."]
[7.150187015533447, 8.790335655212402, "The Footprint Shape of the CNSCAT Scatterometer is Rosette-shaped."]
[6.88804817199707, 8.79848861694336, "The Vertical Resolution of the Mie co-polar channel Channel is 100 m."]
[11.746926307678223, 7.500938415527344, "The Manufacturer of the DSAC Atomic Clock is SST-US."]
[7.003169536590576, 8.814653396606445, "The Swath of the LISS-IIM Instrument is 131 km."]
[5.833609104156494, 1.6773141622543335, "The Size of the GomX-4B Satellite is Cereal-box-sized."]
[10.325441360473633, 4.981948375701904, "The Components of the IEPS Ion Electric Propulsion System is 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)."]
[8.245540618896484, 0.6940828561782837, "The Observation Period of the Megha-Tropiques Satellite is December 28, 2013 to January 4, 2014."]
[9.781742095947266, 5.028489112854004, "The Requirement of the Caging System Mechanism is Prevent damage to the sphere during launch and to release the sphere after arrival of the satellite on orbit."]
[5.4212446212768555, 0.32108423113822937, "The Burned Area of the Black Fire Fire is More than 130,000 acres."]
[8.562420845031738, 7.8990583419799805, "The Detectors Type of the REM Radiation Environment Monitor is 300 Tm silicon diode detectors."]
[4.421818256378174, 5.627526760101318, "The Data Transmission of the Landsat-6 Satellite is X-band direct downlink."]
[8.380563735961914, 9.14626407623291, "The Measurement Types of the SAGE-III Spectrometer is UV and visible light."]
[11.071920394897461, 4.936745643615723, "The Speed of the CME (Coronal Mass Ejection) Solar Phenomenon is Tens of kilometres per second."]
[9.722452163696289, 3.6452691555023193, "The Background Noise of the Lunar Meteoroid Impact Flash Detection Detection System is Earthshine (Earth reflected light on the Moon surface) in the visible spectrum, and by thermal emissions of the Moon surface in the infrared spectrum."]
[8.105752944946289, 5.207304954528809, "The Range Measurement Precision of the Satellite Satellite is Few decimeters."]
[7.245378494262695, 7.470983505249023, "The Photo of the SREM Instrument is Figure 19: Photo of the SREM instrument."]
[10.316723823547363, 7.793732166290283, "The Active Area of the X123-SDD X-ray Spectrometer is 25 mm2."]
[13.112862586975098, 4.054214954376221, "The Oscillation Modes Frequency Shift of the Gaia Satellite is 8.6 million times."]
[7.02639102935791, 8.608072280883789, "The Sample Size of the Vera C. Rubin Observatory Observatory is Very large."]
[8.255485534667969, 4.903286933898926, "The Measurement Resolution of the Cluster S/C Satellite is >= 6 pT."]
[6.960667610168457, 3.8427841663360596, "The Technology of the MANTIS Earth Observation Satellite is Native multispectral Earth Observation."]
[10.109950065612793, 8.306081771850586, "The Sensor Complement of the AstroSat Astronomy Satellite is Five co-aligned telescopes."]
[4.16798210144043, 6.591887474060059, "The Image Rejection of the Receiver Communication System is 60 dB."]
[11.781172752380371, 1.0511019229888916, "The Re-Entry Speed of the Chang\u2019e-5 Lunar Lander is Approximately 40,000 km/hr."]
[8.661894798278809, 2.1857521533966064, "The Chief Scientist of the Hubble Space Telescope Telescope is Ed Weiler."]
[3.8719613552093506, 5.0593061447143555, "The Requirement of the Data Processing System Computer System is Complex and robust."]
[7.669526100158691, 8.788801193237305, "The Measurements of the MAHRSI Instrument is Nitric oxide."]
[8.135786056518555, 7.2844767570495605, "The Purpose of the NASA Instrument Instrument is Determines Hazards of Deep-Space Radiation."]
[9.456469535827637, 1.636459231376648, "The Mode of the Sentinel-1 Satellite is Complete coverage of Earth in six days."]
[9.77333927154541, 1.59511399269104, "The Cycle Length of the Satellite Imaging Satellite is 175 days."]
[1.6445392370224, 4.7958526611328125, "The Power Bus of the Payload Instruments Satellite Components is 28 V unregulated, switched."]
[7.22000789642334, 1.0909672975540161, "The Mission Start Date of the MANTIS Earth Observation Satellite is September 11, 2019."]
[7.508645057678223, 8.163097381591797, "The Transmission Spectra of the Altitude Range Atmospheric is 1 to 99%."]
[3.5826914310455322, 4.520750045776367, "The Technology of the FPGAs Electronic Components is Six Sigma SolderQuik\u00ae."]
[8.351482391357422, 1.8900210857391357, "The Article URL of the Herschel Satellite is http://sci.esa.int/herschel/54252-young-suns-violent-history-solves-meteorite-mystery/."]
[6.713625907897949, 2.2127773761749268, "The Data Access of the GPM Satellite is Free and available to the public."]
[6.924261093139648, -0.06033647060394287, "The End of Life Date of the OSCAR-QUBE Satellite is 29 August 2026."]
[11.562898635864258, 2.6681604385375977, "The Orbit of the Lutetia Asteroid is Main asteroid belt between Mars and Jupiter."]
[8.325943946838379, 9.964377403259277, "The Detector Pixel Size of the Imager Satellite Instrument is Pan: 10\u00b5m x 10\u00b5m, MS: 40 \u00b5m\u00d740 \u00b5m."]
[8.920446395874023, 4.468683242797852, "The Structure of the MTG-S Spacecraft Satellite is Two-winged satellite configuration."]
[3.8340442180633545, 0.2945420444011688, "The Conference Presentation Date of the Gravity Recovery and Interior Laboratory (GRAIL) Satellite is March 18-22, 2013."]
[7.610199451446533, 5.384319305419922, "The Data Collection of the OCO-3 Satellite is Denser data set than OCO-2."]
[9.401331901550293, 3.919278144836426, "The OBC of the Spacecraft Satellite is LEON3 FT."]
[8.255555152893066, 3.112823009490967, "The Earth's Entire Land Mass Mapping Completion Date of the TanDEM-X Satellite is By the end of 2014."]
[7.504049301147461, 1.0638598203659058, "The First Light Observations Date of the MIRIS Satellite is Dec. 23, 2013."]
[8.278074264526367, 3.0951430797576904, "The Global DEM Acquisition Start Date of the TanDEM-X Satellite is December 2010."]
[12.10167121887207, 3.296234369277954, "The Orbit Inclination of the STP-S26 mission Satellite Mission is 72\u00ba."]
[8.757376670837402, 10.541396141052246, "The Resolution of the True Color Composite Image Image is 250 m."]
[11.780464172363281, -0.9956338405609131, "The Booster Segments Weight of the SLS Rocket is 180 tons."]
[8.876762390136719, 5.0739288330078125, "The Roll Motion Range of the GF-2 spacecraft Satellite is \u00b135\u00ba."]
[8.064335823059082, 8.500513076782227, "The Noise Equivalent Radiance of the FTS Interferometer Interferometer is <0.5% of the radiance of a blackbody at 5800 K."]
[8.937042236328125, 6.696169376373291, "The Configuration of the Inertial Sensors Sensor is Concentric coaxial cylinders."]
[10.191773414611816, 1.1099354028701782, "The LTDN of the CBERS-4 Satellite is 10:30 hours."]
[7.321666240692139, 8.088479995727539, "The Sampling Duration of the TAGSAM Sample Acquisition Mechanism is About five seconds."]
[7.759872913360596, 2.3174185752868652, "The Rover Name of the ExoMars Mission is Rosalind Franklin."]
[10.123576164245605, 5.128281116485596, "The Ignition Capability of the Propulsion System Satellite Component is All CGGs individually upon request."]
[7.752671241760254, 3.438552141189575, "The Measurement Technique of the ICON Space Mission is Combines remote optical imaging and in situ measurements of the plasma."]
[7.718405246734619, 7.128421306610107, "The Measurement Range of the IMAP-Ultra Instrument is Extends the measurements through the range covered previously by Cassini/INCA."]
[6.9777655601501465, 1.0858845710754395, "The Conference Date of the Resurs-P1 Satellite is Feb. 28 - March 2, 2007."]
[7.819012641906738, 8.752239227294922, "The Wavelengths of the EPIC instrument Instrument is 10."]
[9.996255874633789, 9.563652038574219, "The Data Usage of the SAGE-III on ISS Satellite Instrument is Help the scientific community identify the cause and assess the threat of any new threats to the ozone layer."]
[9.320500373840332, 4.179646968841553, "The Body Height of the Spacecraft Satellite is 23.5 cm."]
[5.696898937225342, 2.91163969039917, "The Manufacturer of the Hugo Satellite is ABB."]
[6.389297008514404, 1.0745490789413452, "The Workshop Date of the Skybox Imaging Company is March 26-28, 2014."]
[10.231578826904297, 4.912147045135498, "The Thrusters of the ALTIUS Satellite is Four 1N thrusters."]
[6.906233787536621, 5.541726112365723, "The Soil Moisture Accuracy of the SMOS Satellite is 4%."]
[6.920524597167969, 8.803060531616211, "The Cirrus Optical Depth of the Mie co-polar channel Channel is 0.05."]
[11.820420265197754, -1.110715389251709, "The Launch Mass of the Helios-2 satellites Satellite is Approximately 4200 kg."]
[4.77068567276001, 0.8350560069084167, "The Net Loss of the Satellogic Satellite Company is $117.7 million."]
[7.524184703826904, 9.584128379821777, "The SNR @Lref [BOL] of the Spectral Channel Detector is 211-390."]
[8.879571914672852, 10.33143138885498, "The FPN Measurement Method of the Sensor Image Sensor is Capturing and averaging a series of 50 dark images, each containing 10 \u00b5s exposure time."]
[9.19516372680664, -0.617524266242981, "The Launch Date of the HORYU-4 Nanosatellite is Feb. 17, 2016."]
[3.783517360687256, 5.821754455566406, "The Data Rate of the MBEI Data Source is ~184 Mbit/s."]
[9.302330017089844, 8.195145606994629, "The Detector Type of the RAMIS Radiation Detector is Two silicon detectors."]
[9.792872428894043, 8.860638618469238, "The Diameter of the RRA Retroreflector Array is 57 cm."]
[5.719359874725342, 2.4091250896453857, "The Plaque Designer of the LAGEOS Satellite is Carl Sagan."]
[5.375485897064209, 4.120236396789551, "The Ground Segment Components of the JUICE Mission Mission is Mission Operation Center (MOC) and the Science Operation Center (SOC)."]
[7.137279510498047, 0.7822680473327637, "The Availability of the European Aviation Network Inflight Broadband is 18 July 2019."]
[8.38169002532959, 7.762257099151611, "The Cadence of the Pulse Height Analysis Measurement is 1 minute."]
[6.87059211730957, 5.67188835144043, "The Sea Surface Salinity Accuracy Goal of the SMOS Satellite is 0.1 psu."]
[7.650418281555176, 4.099547863006592, "The Radiation Hardness of the Satellite Satellite is MEO compliant."]
[9.534414291381836, 5.590051651000977, "The Control Systems of the AVUM Upper Module is RACS (Roll and Attitude Control System) and the LPS (Liquid Propulsion System)."]
[7.142020225524902, 3.157363176345825, "The Operation Management of the CAPSTONE Satellite is Advanced Space and Terran Orbital."]
[10.718021392822266, 3.4458656311035156, "The Orbit Location Distance of the ACE Mission Satellite is About 1% of the way toward the sun on the sun-Earth line."]
[2.1032443046569824, 4.601454734802246, "The Payload Power of the Inmarsat S \u2013 Europasat / Hellas-Sat 3 Satellite is About 12.3 kW."]
[10.956661224365234, 3.0866992473602295, "The Length of the Hydra Moon is 55 km."]
[3.681529998779297, 6.044353485107422, "The Bandwidth Impact of the Telemetry Data is Limited."]
[9.6090726852417, 1.2826184034347534, "The Aggregation Time of the Satellite Measurements Data is Months or even years."]
[8.290122985839844, 9.559967041015625, "The IFOV of the PAN Detector is 0.45 - 0.52 \u00b5rad."]
[8.14301586151123, 8.16463565826416, "The Application of the Infrared Sensors Sensor is Astronomical observations."]
[7.262206554412842, 5.589877128601074, "The NWP Impact of the Aeolus Satellite is Positive."]
[12.097986221313477, 3.356076955795288, "The Orbit Inclination of the PRISMA Satellite is 98.19\u00b0."]
[3.911736488342285, 2.3012876510620117, "The CubeSat Size of the RadCube Satellite is 3U."]
[5.350185871124268, 1.3511216640472412, "The Fairing Reuse of the Falcon 9 Rocket is Half of which flew on two previous missions."]
[4.564666271209717, 4.34662389755249, "The Function of the Strain Relief Connector Saver Component is Alleviate issues and protect the access port."]
[7.557442665100098, 7.214804172515869, "The Meeting Date of the ECOSTRESS Instrument is 15 - 17 May 2017."]
[8.844474792480469, 1.9487992525100708, "The URL of the BepiColombo Mission is http://www.lpi.usra.edu/meetings/lpsc2013/pdf/2172.pdf."]
[7.725485801696777, 0.23166470229625702, "The Mission Flexibility Demonstration of the Soyuz Spacecraft is April 26, 2016."]
[6.927379608154297, 3.7185935974121094, "The Mission Type of the Meteor-M-2 Satellite is EO."]
[11.747446060180664, 1.7542691230773926, "The Crevice Length of the Philae Lander is 2.5 m."]
[11.732093811035156, 2.57468581199646, "The Size of the Didymos A Asteroid is About one-half mile."]
[7.322851657867432, 10.120185852050781, "The Data Volume Requirement of the HyperScout Imaging System is 1.5 MB."]
[10.243560791015625, 2.921035051345825, "The Orbit Altitude of the HY-2A Satellite is 971 km."]
[7.737350940704346, 8.863564491271973, "The Horizontal Onboard Accumulation Length of the Detector Instrument is 1.0 km and 3.5 km."]
[11.774499893188477, 4.558614730834961, "The Diameter of the Cas A Supernova Remnant is 10 light years."]
[7.086127281188965, 7.032627582550049, "The Unknown of the GOMOS Instrument is Unknown."]
[8.346534729003906, 5.595921993255615, "The Impact on Satellites of the Earth's Magnetic Field Natural Phenomenon is Can cause big headaches for satellites."]
[7.895922660827637, 2.0866427421569824, "The Number of Instruments of the ISEE-1 Spacecraft is Unknown."]
[5.204339981079102, 1.9192568063735962, "The Switches of the P-POD Poly-Picosatellite Orbital Deployer is 2."]
[8.144493103027344, 3.4574897289276123, "The Shape of the DebriSat Satellite is Hexagonal Prism."]
[7.587718486785889, 8.730128288269043, "The Vertical Resolution of the VISION Instrument is 2 km."]
[9.067025184631348, 9.76055908203125, "The Modes of the Camera System Observation Modes is Automatic target pointing, Interactive operation."]
[6.6090407371521, 10.687112808227539, "The SNR of the Band 2 Spectral Band is 160."]
[9.505160331726074, 0.5733769536018372, "The Expected Lifetime of the MetOp-SG Satellite is 7.5 years."]
[10.510698318481445, -1.1511056423187256, "The Mass of the Jugnu Nanosatellite is 3 kg."]
[9.807534217834473, 1.312411904335022, "The Stable Electricity Supply Duration of the TSUBAME Satellite is At least 80 days."]
[4.806308269500732, 1.6898750066757202, "The New Factory Production Capacity of the Satellogic Satellite Company is 25 satellites a quarter."]
[3.5676491260528564, 6.514409065246582, "The Data Rates of the CC1101 UHF transceiver Transceiver is Up to 500 kbit/s."]
[8.65031623840332, 2.0535736083984375, "The Retired Date of the Herschel and Planck Telescopes is Unknown."]
[11.443807601928711, -1.3533722162246704, "The Mass of the HawaiiSat-1 Satellite is 40 kg."]
[10.473499298095703, -1.154201865196228, "The Mass of the D-Star One Nanosatellite is 3 kg."]
[12.160436630249023, 3.2023942470550537, "The Inclination of the Meteor-M2 Satellite is 98.8\u00ba."]
[6.8320112228393555, 1.1891676187515259, "The Commissioning Date of the Small Satellite Constellation Satellite Constellation is Aug. 9-12, 2004."]
[6.017009258270264, 6.3869147300720215, "The ISLR of the Instrument SAR is \u2264-9 dB."]
[9.530733108520508, 8.172759056091309, "The Scintillation Module Layers of the Natalya-2M High energy radiation spectrometer is Two layers (4 crystals in each)."]
[9.61076831817627, 3.625488042831421, "The Measurement Goal of the Lunar Flashlight Spacecraft is Identify locations where water ice is present at the surface of the Moon as a frost."]
[7.6871018409729, 0.5149398446083069, "The Launch Date of the SLS Rocket is Four years from now."]
[8.6548433303833, 4.206454753875732, "The Development Cost of the BRITE Telescope is Minimized."]
[7.229511260986328, 3.144882917404175, "The Mission Status of the CHIPS Satellite is Unknown."]
[6.00084114074707, 3.4338653087615967, "The Development Partnership of the MIRI Instrument is 50-50 partnership between NASA and ESA."]
[8.081072807312012, 11.140795707702637, "The Sensitivity of the Channel 6 Sensor is 0.4 K/pixel."]
[11.61632251739502, -1.2008386850357056, "The Mass of the Satellite Communication Satellite is 2500 kg."]
[4.081676483154297, 4.548814296722412, "The Communication Interface of the EC Digital Signal Processor is Serial port."]
[10.547258377075195, 7.564692974090576, "The Material of the Reflector Film Satellite Component is 1/4 mil aluminized mylar."]
[7.088329792022705, 0.7553988695144653, "The Sent to NASA Date of the Diwata-1 Satellite is January 18, 2016."]
[9.20328140258789, 4.109426975250244, "The Solar Cell Dimensions of the TUBSAT-N Satellite is 6 cm x 4 cm."]
[12.156798362731934, 3.2343204021453857, "The Orbit Inclination of the JAWSAT Satellite is 100.2\u00ba."]
[8.6512451171875, 1.6962453126907349, "The Launch of the Telescope Optical Instrument is 2019."]
[7.3317365646362305, 0.14163343608379364, "The Launch Date of the Rocket 3.3 Rocket is 20 November 2021."]
[6.798473358154297, 1.2213557958602905, "The Conference Presentation Date of the GIOVE-A Satellite is Sept. 26-29, 2006."]
[7.268266677856445, 0.9356117248535156, "The Year of Launch of the EO-1 Satellite is 2000."]
[5.536383152008057, 6.347224235534668, "The Downlink Frequency Band of the SAR/Galileo and SAR/GLONASS payloads Payloads is 1544 \u2013 1545 MHz (L-band)."]
[4.744840621948242, 2.714097738265991, "The Control Type of the Jerry 1U CubeSat is Passive."]
[7.880180835723877, 9.340639114379883, "The Spectral Sampling Distance of the SWIR Spectrometer Spectrometer is 10 nm on average."]
[5.769696235656738, 3.667379140853882, "The Development Center of the GeoXO Satellite System is NASA's Goddard Space Flight Center in Greenbelt, Maryland."]
[9.283699989318848, 5.46458101272583, "The Attitude Accuracy of the Attitude and Orbit Control Subsystem Subsystem is 0.5\u00ba in yaw."]
[7.6956024169921875, 3.2936530113220215, "The Evaluation Paper of the CartoSat-1 Satellite is \"Evaluation of CartoSat-1 Multi-Scale Digital Surface Modelling Over France\"."]
[6.981529235839844, 0.7335294485092163, "The Arrival Date at Launch Site of the OHB Communications Satellite Communications Satellite is Dec. 1, 2016."]
[6.51608419418335, 9.198892593383789, "The Size of the STAFF/DWP Instrument is 351 mm x 200 mm x 208 mm."]
[8.642953872680664, 9.533915519714355, "The EW FOV: max FPM of the AHI Scanner is 33,203 \u00b5rad."]
[8.850905418395996, 3.313344717025757, "The Orbit of the TET-1 Satellite is Low Earth Orbit."]
[6.613794326782227, 10.679750442504883, "The Nominal SNR of the Band 7 Spectral Band is 860."]
[8.72854995727539, 3.1959879398345947, "The Impact on ILRS of the GOCE Satellite is Negative."]
[6.38872766494751, 0.6307836174964905, "The Generation of the GOES 2nd generation spacecraft Satellite is 2nd."]
[10.06633186340332, 2.39233660697937, "The Orbit velocity of the KOMPSAT-3 Satellite is 7.51 km/second."]
[9.53191089630127, 0.5177154541015625, "The Design Life of the COSMO-SkyMed spacecraft Satellite is 5 years."]
[11.525030136108398, 3.041126251220703, "The Orientation of the SERB Nanosatellite Satellite is +Z pointing to the Sun, +Y along the longitudinal nanosatellite axis, and +X along the deployed solar arrays."]
[7.144400596618652, 0.36934900283813477, "The Launch Date of the Ikonos-2 Satellite is 24 Sep 1999."]
[8.069328308105469, 9.802494049072266, "The Position of the CASI-1500i Compact Airborne Spectrographic Imager is Left."]
[6.067182540893555, 2.414428234100342, "The Launch Location of the Italian mini-satellite Satellite is Russia."]
[6.792883396148682, 3.274977207183838, "The Mission Status of the ZACUBE-2 Satellite is Operational (nominal)."]
[7.127252101898193, 7.072504997253418, "The Status of the MADRAS Instrument is Unknown."]
[7.027962684631348, 9.842805862426758, "The Wavelength Range of the Band 2 Spectral Band is 660-685 nm."]
[7.249275207519531, 9.040587425231934, "The Swath Width of the PanMUX Instrument is 60 km."]
[9.387717247009277, 6.057932376861572, "The Inertia Tensor of the AGS Attitude Determination System is Best available."]
[7.1401190757751465, 0.7369898557662964, "The Launch Date of the RHESSI Satellite is February 5, 2002."]
[9.708388328552246, 1.5895402431488037, "The Repeat Cycle of the SPOT-1, -2 and -3 Satellites is 26 days."]
[9.990885734558105, 1.524154782295227, "The Length of Operation of the Internal Satellite Diffuser Calibration Device is 30 min, one or two wavelengths per orbit."]
[5.9538893699646, 0.6274963617324829, "The Deployment Date of the CubeRRT, EQUiSat, HaloSat, MemSat, RadSat-g, RainCube, TEMPEST-D, EnduroSat One, Radix Satellites is July 15th."]
[5.304573059082031, 9.606289863586426, "The No of Stars Observed of the STOs and STAEs Analog Electronic units is 10 x 2 (acquisition), 5 x 2 (tracking)."]
[8.40172290802002, 0.6337159276008606, "The Radio Signals of the Hitomi Satellite is 3/29 00:33 (for about 6 sec) @ SNT."]
[6.056833267211914, 6.187082767486572, "The L0 and L1A Processing Time of the SAR Synthetic Aperture Radar is About 3 days."]
[7.854641914367676, 9.04537296295166, "The Exposure Time of the Channels Spectrometer is 0.01-600."]
[4.405335426330566, 5.285299777984619, "The Cross-Strapping of the KazEOSat-2 Satellite is Provides Redundancy."]
[9.64476490020752, 7.853599548339844, "The Energy Range for Electrons of the MagEIS Magnetic Electron Ion Spectrometer is 30 keV to 4 MeV."]
[6.58696174621582, 0.5301177501678467, "The Current Status of the AeroCube-3 Satellite is Operating nominally as of summer 2009."]
[6.086096286773682, 9.670149803161621, "The Mass of the Sensor Unit Sensor is 4.815 kg."]
[12.033517837524414, 2.1346940994262695, "The Movement of the REXJ Astrobot is Can theoretically move around the space station."]
[9.307332992553711, -0.6475920677185059, "The Target Industry of the MANTIS Nanosatellite is Oil and gas sector."]
[8.653935432434082, 1.9273854494094849, "The Observatory Presentation of the James Webb Space Telescope Space Telescope is Rob Garner, \"The James Webb Space Telescope Observatory,\" NASA, July 28, 2013."]
[4.323427200317383, 6.445505619049072, "The Amplifier Efficiency of the Ka-band Signal is 13%."]
[7.1419148445129395, 5.059865951538086, "The Percentage from Oil and Gas Sector of the Kayrros Studies Methane Leak Detection is Around 50%."]
[7.807130813598633, 9.588930130004883, "The Spectral Bandpass of the Instrument Photometer is 400 nm to 850 nm."]
[9.587396621704102, 4.198330879211426, "The Primary Cube Structure Side Length of the COMMx Payload is 0.93 m."]
[6.099491119384766, 3.857771873474121, "The Partner Agencies of the Odin Satellite is Canada, Finland and France."]
[7.336277484893799, 5.496984004974365, "The Effect of the Space Traffic Spacecraft Launches is Controls the year-to-year variability of mid-latitude noctilucent clouds."]
[7.706486225128174, 1.4922606945037842, "The First Image Date of the SMOS Satellite is Feb. 23, 2010."]
[4.6556010246276855, 5.6831955909729, "The RF Communications of the Spacecraft Satellite is S-band."]
[6.845445156097412, 0.4169781506061554, "The Launch Date of the GEOS-3 Satellite is April 9, 1975."]
[8.723079681396484, 3.094477415084839, "The Release of the HPA Satellite is Not until a geostationary transfer orbit is attained."]
[8.539746284484863, 3.956645965576172, "The Roll Axis Control of the GNB Satellite is Not controlled."]
[8.001630783081055, 0.31141385436058044, "The Launch Time of the Aeolus Spacecraft is 21:20 GMT."]
[4.046820163726807, 4.492559432983398, "The Manufacturer of the Microprocessor Component is PIC."]
[10.209360122680664, 6.885483741760254, "The Design of the Thermal Subsystem Satellite Subsystem is Largely passive solution using MLI (Multi-Layered Insulation) and surface coatings."]
[7.6967926025390625, 0.5148109793663025, "The Launch Date of the DSCOVR Spacecraft is February, 11, 2015."]
[11.990030288696289, 3.2535622119903564, "The Orbit Inclination of the R3 CubeSat Satellite is 85\u00b0."]
[11.684165000915527, -1.1998603343963623, "The Mass (kg) of the KOMPSAT-5 Satellite is 1400."]
[7.094122886657715, 3.9599807262420654, "The Agency of the Meteor-M-2 Satellite is ROSKOSMOS, ROSHYDROMET."]
[9.333532333374023, 4.831738471984863, "The Solar Array Normal Vector and Sun Vector Difference of the Spacecraft Satellite is Up to 30 degrees during the extended mission phase."]
[7.790318489074707, -0.41737374663352966, "The Launch Time of the Soyuz MS-17 Spacecraft is 1:45 a.m. Eastern Oct. 14."]
[10.335187911987305, 2.90529465675354, "The Apoherm of the MMO Spacecraft is 12,000 km."]
[4.810329914093018, 1.8603743314743042, "The Number of Satellites of the MetOp-SG Satellite is 6."]
[9.577999114990234, 1.447338342666626, "The Repeat Coverage of the Landsat 9 Satellite is 16 days."]
[5.23447322845459, 1.6681596040725708, "The Number of Secondary Payloads of the PSLV-C37 Launch Vehicle is 103."]
[8.670600891113281, 1.6080834865570068, "The New Discovery of the Van Allen Probes Satellite is 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."]
[6.730844020843506, 7.744974136352539, "The Survival Temperature Range of the GEDI Laser Laser System is 50\u00baC to -10\u00baC."]
[6.125384330749512, 9.647516250610352, "The Mass of the Instrument mass Spectrometer is 12 kg (max)."]
[3.434377670288086, 6.480732440948486, "The Signal Conditioning Modules of the MnACQ-2000 Miniature Network Data Acquisition System Data Acquisition System is Included."]
[8.534934997558594, 10.471266746520996, "The CCD Lines per Package of the Focal Plane Module Imaging Device is 3."]
[7.378665924072266, 7.3544182777404785, "The Phase of the OLCI Instrument is PDR (Preliminary Design Review)."]
[7.696239471435547, 8.965981483459473, "The Manufacturer of the Miniature High-Resolution Imaging Spectrometer Imaging Spectrometer is MPB Communications Inc.."]
[1.8179445266723633, 4.0032219886779785, "The Array of the Detectors Photovoltaic Detectors is 3 x 3."]
[6.114177703857422, 0.6899359226226807, "The Design Date of the CubeSat Guidance, Navigation, and Control Module CubeSat Component is August 2011."]
[9.626805305480957, 7.7816386222839355, "The Proton Energy of the GALS-VE Particle Energy Measurement Device is > 800 MeV."]
[7.361093044281006, 8.876359939575195, "The Spectral Channel 1 of the Satellite Imaging Satellite is 0.50 - 0.59 \u00b5m."]
[7.739736080169678, 4.0721659660339355, "The Principal Investigators of the Multiple Sclerosis and Parkinson\u2019s Disease Cryovial Study Research Project is Dr. Andres Bratt-Leal and Dr. Valentina Fossati."]
[12.976948738098145, 4.842173099517822, "The Mission Control of the IBEX Satellite is Boston University."]
[6.590143203735352, 7.607474327087402, "The Quantity of the Laser Transmitter Device is 1."]
[11.563197135925293, 5.296567440032959, "The Article Date of the H1743-322 Black Hole Binary is July 2016."]
[9.80282974243164, 4.664656639099121, "The Interchangeable Barrels Sizes of the Launcher Test Facility is 84 mm, 102 mm, and 203 mm."]
[7.444240570068359, 0.6449776291847229, "The Launch of the CLARREO Pathfinder Satellite is 11/2022."]
[9.530244827270508, 6.007104873657227, "The Primary Attitude Sensor of the ADCS Attitude Determination and Control System is Magnetometer."]
[6.2363810539245605, 7.775680065155029, "The Polarization of the ICI-10 Radiometer is V."]
[1.05460786819458, 4.3577165603637695, "The Battery Capacity of the EPS Electrical Power Subsystem is ~ 10 Whr."]
[8.80087947845459, 10.153159141540527, "The Latchup Event of the CMOS Sensors Sensor is Produces an increase in current consumption, and the device becomes un-responsive."]
[5.046442985534668, 7.556812286376953, "The Data Rate of the PEACE Instrument is 3.54 kbit/s."]
[4.606070041656494, 4.5558857917785645, "The Methods of Communication of the MCS Communication System is Point-to-point client-server communication and communication on a message bus."]
[8.75553035736084, 0.7586584687232971, "The Impact on Ganymede's Surface of the Juice Spacecraft is Late 2035."]
[6.384611129760742, 3.2968528270721436, "The Mission Operator of the SPOT 1-5 Satellite is CNES."]
[6.428292751312256, 5.541971683502197, "The Function of the Satellite STRATOS is Performs radio occultation (RO)."]
[6.152090549468994, 1.5447111129760742, "The Document Date of the Paz ground segment Ground Segment is May 31, 2011."]
[4.840661525726318, 1.8528650999069214, "The Number of Satellites of the RADARSAT Constellation Satellite Constellation is 3."]
[6.804884910583496, 3.2230401039123535, "The Operational Status of the MTSAT-1R Satellite is Standby."]
[6.864542484283447, 3.949101448059082, "The Registration Process of the Sentinel-1 Satellite is Online self-registration accessible via the Sentinel Data Hub."]
[9.170289993286133, 7.0782599449157715, "The Development Date of the Multi-Needle Langmuir Probe System Probe System is May 25, 2009."]
[9.296452522277832, 6.399120807647705, "The Robustness of the Star Tracker Attitude Determination Device is Better robustness to Moon-blinding and to temperature constraints."]
[8.181805610656738, 10.40627670288086, "The Bandwidth of the Band Cameras Camera is 90 nm."]
[4.578938007354736, 4.732295989990234, "The Functions of the DAQLB Data Acquisition and Quicklook Browsing is Quicklook display, browse generation, calibration analysis and ADIF generation."]
[9.55018424987793, 0.6354615092277527, "The Design Life of the S/C Spacecraft is 2 years."]
[10.563760757446289, 3.2435128688812256, "The Maximum Distance of the Inter-satellite link Communication System is 2-5 km."]
[4.877750873565674, 0.9256247878074646, "The Cost of the Radiation Effects Tests Testing Process is On the order of $400,000."]
[10.52407455444336, -0.9663401246070862, "The Mass of the SaudiSat-4 Microsatellite is 112 kg."]
[9.821076393127441, 7.970654487609863, "The Sensitivity of the High-Altitude Water Cherenkov Observatory (HAWC) Observatory is Very high energy gamma-ray photons."]
[3.6919445991516113, 6.256234645843506, "The Uplink Data Rate of the TT&C S-band Communications Communication System is 4 kbit/s."]
[6.703104019165039, 4.841300964355469, "The Data Provided of the CFOSAT Satellite is Co-located wind vector fields, directional spectra of ocean waves, normalized radar cross-section."]
[8.466997146606445, 10.497374534606934, "The Command Interface of the CCD (Charge-Coupled Device) Imaging Device is UART type."]
[6.072934627532959, 9.674118995666504, "The Total Mass of the Instrument Sensor is 13.25 kg."]
[7.54680871963501, 8.059638023376465, "The Field of View of the CERES Scanner is \u00b178\u00b0."]
[11.168927192687988, 4.254464626312256, "The Brightness of the Venus' Orbital Dust Ring Space Dust Feature is At least a hundred times brighter than the solar wind."]
[3.4637203216552734, 6.168254852294922, "The Frequency Band of the TOTEM SDR SDR Platform is 400-440 MHz."]
[10.196993827819824, -0.904302179813385, "The Volume of the PROBA-1 Microsatellite is 1 m3."]
[5.881649494171143, 6.439100742340088, "The Observation Capability of the SIR-C/X-SAR Radar System is Two-frequency."]
[11.762118339538574, 4.666876792907715, "The Light Travel Time to Earth of the OJ 287 galaxy Galaxy is 3.5 billion years."]
[8.070218086242676, 4.078769207000732, "The Keel Depth of the A-68A Iceberg is 141 metres below the ocean surface."]
[4.333250045776367, 4.420496463775635, "The Arbitration System of the CAN Bus Data Communication is Yes."]
[8.143327713012695, 8.446903228759766, "The Optical System of the SHS Interferometer is Similar to the Twyman-Green interferometer."]
[7.636230945587158, 7.155958652496338, "The Measurement Domain of the TEMPO Satellite is Atmosphere."]
[7.193081378936768, 3.0502257347106934, "The Mission Status of the FORUM Satellite is Planned."]
[6.898317337036133, 0.08129898458719254, "The End of Life Date of the GF-3 Satellite is 10 Aug 2024."]
[6.9311113357543945, 5.015625953674316, "The Emissions Contribution in 2019 of the Sudd wetlands in South Sudan Wetlands is Over a quarter of the growth in global emissions."]
[10.087888717651367, -1.0238598585128784, "The Nadir Pointing of the Dove-1 Nanosatellite is Twice per orbit."]
[6.56349515914917, 6.772399425506592, "The Test Date of the AltiKa Radar Altimeter is Nov. 17-18, 2009."]
[7.01232385635376, 4.956386566162109, "The Source of Carbon of the Northern Forests Ecosystem is Potential future outcome."]
[6.983338832855225, 2.5801124572753906, "The URL of the Radio Aurora Explorer Satellite is http://rax.sri.com/index.html."]
[8.74030590057373, 0.7737063765525818, "The Arrival at Jupiter of the Juice Spacecraft is July 2031."]
[4.421849250793457, 4.575414180755615, "The Function of the ICU Instrument Control Unit is FCI and IRS management and data-processing."]
[11.151506423950195, 6.926563262939453, "The Spectrum of the Sco X-1 X-ray Source is Soft X-ray."]
[8.861063003540039, 4.826900959014893, "The Control Algorithm of the SV-1 Satellite is Problematic."]
[6.500078201293945, 4.8637213706970215, "The Role of the Copernicus Sentinel-6 Michael Freilich Satellite is Radar altimetry reference mission."]
[7.358306407928467, 1.462587594985962, "The Date of the Senior Review 2013 Review is June 13, 2013."]
[9.899784088134766, 1.55754554271698, "The Observation Time of the Satellite Orbit is Approximately 10 minutes per orbit."]
[7.126455307006836, 7.124449253082275, "The Function of the PACO Software is Perform atmospheric and topographic processing."]
[9.274452209472656, -0.7478722333908081, "The Launch Vehicle of the KazSTSAT Microsatellite is SpaceX Falcon-9 Block 5."]
[5.882650375366211, 6.511435031890869, "The Transmission Frequency of the SAR Synthetic Aperture Radar is 1.275 GHz."]
[7.260993003845215, 3.8236303329467773, "The Cloud Cover Impact of the CHOMPTT Satellite is Preventing lasing from the Mount Stromlo site."]
[9.818305015563965, 5.053886413574219, "The Orbit Control System of the Payload Satellite Payload is Propulsion."]
[9.28727912902832, 0.806469202041626, "The In-Orbit Nominal Lifetime of the MWI Instrument Instrument is 7.5 years."]
[5.7069926261901855, 7.066234588623047, "The Antenna Diameter of the RA-1 Radar Altimeter is 1.2 m."]
[5.5863566398620605, 2.7024717330932617, "The Partners of the Hiber Satellite Network is Amazon Web Services, IBM Watson and Actility."]
[6.756895542144775, 3.575960397720337, "The Mission Type of the HJ-1 Satellite is EO."]
[5.148364543914795, 4.31427526473999, "The Alert Production of the Ground Software Data Processing is Produce and distribute alerts to the world-wide astronomical community."]
[6.0643134117126465, 9.624906539916992, "The Mass of the CION Instrument is 1.5 kg."]
[7.021462440490723, 2.0310869216918945, "The URL of the Swarm Mission is http://pcwww.liv.ac.uk/~holme/RAS/haagmans.pdf."]
[11.241896629333496, 2.9887704849243164, "The Material of the Site Kingfisher Crater is Fresher, minimally-altered."]
[9.321946144104004, 1.1568208932876587, "The Operation Period of the Remote Agent Software is Three days."]
[7.070069789886475, 2.6487443447113037, "The URL of the SWOT Satellite Satellite is https://swot.jpl.nasa.gov/flight_systems.htm."]
[8.424728393554688, 10.079217910766602, "The Capability of the TDI Feature Imaging Device Feature is Low-light observations of imagery."]
[5.986998558044434, 4.939060688018799, "The Purpose of the GIPSY-OASIS Software is Earth orbit determination using GPS data."]
[9.43580150604248, 7.310116767883301, "The Grids of the FSU Solar Wind Faraday Cup is Monolithic grids etched from single wafers of high purity W."]
[4.261531829833984, 5.703780174255371, "The X-band Downlink Transmission Frequency of the CBERS-2B Satellite is 8103 and 8321 MHz."]
[10.080362319946289, 1.4208425283432007, "The Equator Crossing Time of the Satellite Satellite is 10:26 hours."]
[5.795283794403076, 6.487190246582031, "The Pulse Width of the CSG-SAR Synthetic Aperture Radar is Programmable (5-100 \u00b5s)."]
[6.213935852050781, 4.707462787628174, "The Processing Format of the ICEYE-X1 Satellite is GeoTIFF."]
[7.798715591430664, 10.874479293823242, "The Data quantization of the ALOS/PRISM Satellite is 8 bit."]
[7.90707540512085, 8.27871322631836, "The Manufacturer of the CHRIS Imaging Spectrometer is Space Group of Sira Electro-Optics."]
[9.272995948791504, 10.249011993408203, "The f/number of the 50 mm camera Camera is f/1.8."]
[4.557551860809326, 2.0597357749938965, "The Total Impulse of the SkySat-3 Satellite is 1,732 Ns."]
[7.40485143661499, -0.6084083318710327, "The Berthing Date of the Cygnus Satellite is July 16, 1014."]
[5.116911888122559, 2.3725290298461914, "The Unknown Failure Rate of the CubeSats Satellite is 33%."]
[6.081533432006836, 4.114535808563232, "The Data Downlink of the ISERV Satellite is Via TDRSS."]
[3.6251285076141357, 6.060787677764893, "The Max Transmission Rate of the DTS Data Transmission Subsystem is 320 Mbit/s."]
[9.699071884155273, 6.491634845733643, "The Humidity of the PM Satellite Component is 25~70%."]
[12.103280067443848, 3.3075201511383057, "The Inclination of the ICEYE-X10 Satellite is 97.4\u00ba."]
[7.4338531494140625, 1.0745270252227783, "The Launch Date of the PlanetiQ satellites Weather Satellites is Early 2020."]
[6.62100076675415, 3.3052709102630615, "The Control Center of the Chandra X-ray Observatory is Smithsonian Astrophysical Observatory's Chandra X-ray Center."]
[7.710313320159912, 3.9313082695007324, "The Data Transfer of the Pl\u00e9iades Neo Satellite Constellation is Up to 40 terabytes per day."]
[7.712404727935791, 7.08413553237915, "The Critical NASA Review Date of the TEMPO Pollution Monitoring Instrument is May 6, 2015."]
[6.14854621887207, -0.04900413751602173, "The End of Life Date of the Galileo Second Generation (G2) Satellite Constellation is 31 December 2039."]
[9.020539283752441, 8.847472190856934, "The Exit Slit of the UVS Instrument Spectrometer Telescope is 2 x 4 mm."]
[7.888463497161865, 8.43976879119873, "The Precision of the SAGE-III Spectrometer is 0.1 % to 10 %."]
[7.582211017608643, 4.095092296600342, "The Panchromatic Resolution of the EROS-C Satellite is Comparable to EROS B."]
[6.848771095275879, 3.986105442047119, "The Evaluation of the Disaster Monitoring Constellation Satellite Constellation is Utility in Support of Earth Observation Applications."]
[11.730595588684082, 7.477704048156738, "The Atomic Clock Accuracy of the Galileo Satellite System is Accurate to a few nanoseconds."]
[6.774766445159912, 0.0231251772493124, "The Data Production Start Date of the Tatiana-2 Satellite is Early January 2010."]
[9.221128463745117, 9.138875007629395, "The Break Energy of the First Broken Powerlaw Model Component is 1.2 keV."]
[8.60612964630127, 10.070560455322266, "The Quality Comparison of the Imaging Methods System is SMART > PAIS > Direct."]
[6.057055473327637, 6.623302459716797, "The Operating Bands of the SRAL Radar Altimeter is C-band and Ku-band."]
[5.432301998138428, 1.9223707914352417, "The Picosatellite Capacity of the OPAL Satellite is 6."]
[8.289875030517578, 7.470760822296143, "The Manufacturer of the EXObox Electrical Management Unit is Exolaunch."]
[10.04904556274414, 1.522002935409546, "The Period of the Explorer 36 Satellite is 112 minutes."]
[7.05838680267334, 4.460818290710449, "The Infrared Multispectral Scanner of the HJ-1B Satellite is 1."]
[6.503523826599121, 3.687809944152832, "The Mission Objective of the OSMA-1 Satellite is Refuel Landsat-7 spacecraft."]
[8.115711212158203, 3.840311288833618, "The Imagery of the Pleiades Satellite is Not Free."]
[5.660853385925293, 4.126251697540283, "The Ground Testing of the Galaxy Spacecraft is Underway."]
[8.993182182312012, 2.743659019470215, "The Full Operational Service Start Date of the GCOM-W1 Satellite is May 17, 2013."]
[6.951663970947266, 1.2858742475509644, "The Date of the Space Tethers and Small Satellites Presentation is Unknown."]
[10.623330116271973, 6.026668548583984, "The Flare List Events of the RHESSI Satellite is Over 70,000."]
[12.077059745788574, 3.3358190059661865, "The Path Offset/Revolution of the Satellite Communication is 26.334\u00ba."]
[10.194625854492188, 3.0183823108673096, "The Altitude of the Satellite Orbit Orbit is ~666 km."]
[9.369047164916992, 1.8478171825408936, "The Satellite Configuration Frequency of the HyperScout\u00ae Satellite is Once per day."]
[8.988844871520996, 10.619366645812988, "The Resolution of the MUX Camera is 20 m."]
[8.604620933532715, 10.543295860290527, "The Data Rate of the Imager Imaging System is ~3.9 Mbit/s."]
[5.722173690795898, 3.8059728145599365, "The Operation Center of the SAOCOM-1A Satellite is Mission Operation Center in CETT (Centro Espacial Te\u00f3filo Tabanera), CONAE \u2013Cordoba."]
[9.421669960021973, 8.125814437866211, "The Instrument Mass of the RAMIS Radiation Detector is 540 g."]
[9.698165893554688, 7.13673210144043, "The Thermal Operating Range of the SAGE-III Instrument is 10-30\u00ba C."]
[5.813615322113037, 8.182875633239746, "The Bandwidth (GHz) of the ICI-7 Radiometer is 3.2."]
[7.571046352386475, 3.7288084030151367, "The Mission 1 of the Planet Satellite Operator is Ability to image all of Earth\u2019s landmass every day."]
[5.879856586456299, 8.555815696716309, "The Launch Year of the MicroWave Humidity Sounder-2 Sounder is 2013."]
[8.225837707519531, 4.980853080749512, "The Cross-Track Direction Body-Pointing Capability of the Kanopus-V 1 Satellite is Yes."]
[1.8843932151794434, 3.8980515003204346, "The Type of the Power System Satellite is Dual battery, gallium arsenide triple-junction solar cell based."]
[10.072004318237305, 3.0595340728759766, "The Altitude of the SuperView 1A and 1B Satellite is 514 km."]
[10.875304222106934, 5.717308521270752, "The Author of the Can ripples on the sun help predict solar flares? News Article is Robert Sanders."]
[8.588417053222656, 6.736405372619629, "The Purpose of the Spaceborne scalar magnetometers Instrument is Map the Earth\u2019s magnetic field."]
[3.774972915649414, 6.178427696228027, "The Data Rate of the OGS Optical Ground Station is 40 Mbit/s."]
[9.396042823791504, 8.804642677307129, "The Pointing of the Telescope Optical Instrument is Within a 40\u00ba cone centered around the anti-sun vector."]
[7.630889415740967, 6.606723785400391, "The Required Precision of the O3 Profile Satellite Instrument is 10, 10, 5%."]
[7.602076053619385, 0.777637779712677, "The International Astronautical Congress Date of the ETS-VII Satellite is Sept.28-0ct.2, 1998."]
[13.807552337646484, 0.767737627029419, "The Orbital Slot of the GSAT-0102 Satellite is B06."]
[10.79726791381836, 3.499345302581787, "The Closest Approach to Sun of the Parker Solar Probe Satellite is 4 million miles."]
[8.517168998718262, 10.444965362548828, "The Type of the Focal Plane Receiver CCD is Multi-chromatic TDI."]
[5.445746421813965, 4.355444431304932, "The Data Transmission of the Himawari-8/9 Ground Segment Ground Segment is HOPE to JMA."]
[7.3381028175354, 1.393484354019165, "The Conference Date of the Sentinel-1 Satellite is June 7-10, 2010."]
[8.150100708007812, 3.2238683700561523, "The Operation Status of the TanDEM-X Satellite is Nominal."]
[5.559615135192871, 2.340099811553955, "The Data Tile Size of the EnMAP Satellite is 1000 x 1024 pixels."]
[9.176325798034668, 4.217012405395508, "The Solar Array Size of the DSP satellites Satellite is 6.33 m2."]
[8.177918434143066, 4.029778003692627, "The Observation Content of the MIRIS Satellite is Images of M42 (Orion Nebula) and the Rosette Nebula."]
[7.498281478881836, -0.605472981929779, "The Installation Date of the Cygnus Cargo Spacecraft is 14 Nov. 2017."]
[2.672562837600708, 5.382640361785889, "The Power Usage of the Micro-electromechanical system chip Chip is 8.5 times less than proven systems."]
[9.139534950256348, 10.328989028930664, "The Mounting Ring Location of the LWIR Camera Camera is Blue."]
[6.079517364501953, 0.6819851398468018, "The Failure Date of the NRCSD CubeSat Deployer is August 2014."]
[4.7483415603637695, 6.065481185913086, "The Morse Code Beacon Frequency of the OSSI-1 CubeSat is 145.980 MHz."]
[7.034691333770752, 8.258891105651855, "The Lifetime Revolutions of the MWI Instrument Scan Mechanism Assembly is 180 million cycles."]
[6.836270809173584, 3.666588306427002, "The Primary Missions of the MEOSAR Search and Rescue System is Global Navigation Satellite Systems (GPS, Galileo and GLONASS)."]
[6.984602928161621, 0.9873136878013611, "The Commissioning End Date of the RASAT Satellite is Late December 2011."]
[6.019869327545166, 3.176683187484741, "The Design Teams of the QSP-1 Satellite is Germany, Sweden, and the US."]
[9.546051025390625, 3.2037246227264404, "The Orbit Type of the Secondary Payloads Unknown is Elliptical."]
[9.20899486541748, 10.320721626281738, "The Field of View of the Z-panel camera Camera is 25o."]
[4.663434982299805, 4.409381866455078, "The Provider of the Level 0-1b software Software is KNMI."]
[9.397564888000488, 9.116852760314941, "The Focal Length of the Telescope Optical Instrument is 522 mm."]
[3.3826918601989746, 5.815710544586182, "The Data Transfer Time of the Data Transfer Interface Communication System is Approximately twenty-four hours."]
[5.254360198974609, 6.903934478759766, "The IFOV (beam width) of the Antenna Reflector is 1.81\u00ba."]
[6.3143630027771, 3.096328020095825, "The Program of the InSight Lander is Manages by JPL."]
[9.136737823486328, 3.2026569843292236, "The Type of the Satellite Orbit is Sun-synchronous dawn/dusk."]
[6.0472307205200195, 9.593416213989258, "The Mass of the CSS Instrument is 48 gram."]
[5.0139875411987305, 3.9775807857513428, "The Issue Resolution of the EDSN Organization is Eliminating unnecessary connections and ensuring no floating or undefined values in the software."]
[6.2488226890563965, 3.0373165607452393, "The Affiliation of the ITUpSat-1 Satellite is Istanbul Technical University."]
[5.66745138168335, 7.119424343109131, "The RF Transmit Power of the RA-1 Radar Altimeter is 55 W peak."]
[12.165750503540039, 5.377861976623535, "The Cold Interstellar Gas Percentage of the Universe Cosmology is 1.8 percent."]
[7.966097831726074, 2.0915563106536865, "The Mission of the ISEE-2 Spacecraft is Mother/daughter/heliocentric."]
[3.8617238998413086, 2.2792398929595947, "The Size of the Flock-1c CubeSat is 3U."]
[7.933818340301514, 4.1951069831848145, "The Number of Public Images of the Ikonos Imaging Satellite is 597,802."]
[9.031688690185547, 7.874684810638428, "The Counting Ability of the Particle Detector Instrument is 5\u00d710 4  event/s."]
[10.394562721252441, 4.789760589599609, "The Thruster System of the ERG Satellite is Hydrazine."]
[12.102584838867188, 3.300208568572998, "The Inclination of the Satellite Orbit is 80\u00ba."]
[9.378077507019043, 10.102936744689941, "The Position of the Earth Imaging Camera Device is Bottom Middle."]
[4.410024166107178, 6.66810941696167, "The Output Frequency of the PRARE space segment oscillator Quartz-Crystal Oscillator is 5 MHz."]
[8.066522598266602, 7.143678665161133, "The Manufacturer of the AstroRad vest Radiation Protection is ISA."]
[7.620408058166504, 0.4487525522708893, "The Launch Date of the Inspiration4 Mission is Mid-September."]
[5.827289581298828, 2.7769811153411865, "The Role of the Thales Alenia Space Company is On-board Galileo 2nd Generation."]
[7.619155406951904, 4.215765953063965, "The Image Content of the ALOS satellite Satellite is Al Jawf oasis, city, large, irrigated agricultural plots, Kufra Airport."]
[5.250617504119873, 4.306035041809082, "The Instrument Commands of the Spacecraft Satellite is Queued up at the MOC remotely from the SOCs, and uploaded to the spacecraft during the next regular contact."]
[9.153508186340332, 5.244331359863281, "The Attitude Pointing Control of the Spacecraft Satellite is 1\u00ba in pitch, roll, yaw."]
[4.409783840179443, 4.590228080749512, "The Functions of the CMN Interface is 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."]
[5.979130744934082, 3.33565354347229, "The Payload of the SV-2 Satellite is WINCS (Winds-Ion-Neutral Composition Suite)."]
[9.279335021972656, 6.015347957611084, "The Torque of the CMGs Attitude Control is Up to 6.1 Nm."]
[6.264817237854004, 3.4874680042266846, "The Company Type of the Spire Satellite Constellation is Provider of space-based data, analytics, and space services."]
[6.682469844818115, 7.581655979156494, "The Accuracy of the Rangefinder Module Laser Altimeter is 20 cm."]
[4.362375259399414, 4.633678913116455, "The Functionality of the DMFC Digital Signal Processing Card is Perform a variety of mission specific functions."]
[4.571901321411133, 4.68991231918335, "The Functions of the DPS Data Processing System is 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."]
[3.8069376945495605, 6.3034987449646, "The Telemetry Rate of the FREND Instrument is 50 Mbit/day."]
[6.133968353271484, 3.29356050491333, "The Operator of the SEOSAT-Ingenio Satellite is ESA."]
[7.003340721130371, 3.676575183868408, "The On-Orbit Performance and Application of the HJ-1A and HJ-1B Satellites is Proceedings of the 60th IAC (International Astronautical Congress), Daejeon, Korea, Oct. 12-16, 2009."]
[4.719851016998291, 9.005097389221191, "The Landing Site of the InSight Spacecraft is Homestead hollow in Elysium Planitia."]
[10.371787071228027, 3.0003204345703125, "The Altitude of the Secondary Payloads Nanosatellites and CubeSat is ~325 km."]
[6.976746559143066, 5.087621688842773, "The RFI Source Levels of the SMOS Satellite Satellite is Moderate, Strong, Very Strong."]
[6.742055892944336, 0.908908486366272, "The Launch Date of the FormoSat-5 Satellite is Unknown."]
[5.1427788734436035, 3.9823596477508545, "The Subsystems of the SVM Service Module is Thermal environment control, power generation and storage, orbit path control, payload data handling and transmission (PDHT)."]
[6.535250186920166, 6.358027935028076, "The Data Rate of the SeaWinds scatterometer Scatterometer is 40 kbit/s."]
[12.94361686706543, 4.859571933746338, "The Imager of the IBEX Satellite is Energetic Neutral Atom Imager."]
[7.834789752960205, 2.260650634765625, "The Author of the Observation of the Earth and Its Environment Book is Herbert J. Kramer."]
[9.39706802368164, 6.18257999420166, "The Number of Algorithms of the Attitude Determination Quaternion Filter Experiment is Four."]
[9.225491523742676, 2.6093032360076904, "The Impact Date of the DART Spacecraft is Coming September."]
[7.799920558929443, 4.439643859863281, "The Imagery Resolution of the ALOS-3 Satellite is 0.8 m."]
[12.977241516113281, 4.136391639709473, "The Previous Catalogue Object Count (1957) of the Gaia Catalogue of Nearby Stars Stellar Census is 915 objects."]
[7.652600288391113, 8.859636306762695, "The Along-Track Slit Width of the Nadir Sensor Wide-Field Telescope Sensor is 0.27\u00ba."]
[9.250947952270508, 0.9938825368881226, "The Normal Operations Duration of the SELENE/Kaguya Satellite is 10 months."]
[7.689813137054443, -0.4461900591850281, "The Launch Time of the Falcon 9 Launch Vehicle is 12:16 UTC."]
[7.820127487182617, 8.873729705810547, "The Spectral Range of UVIS of the ELVIS Spectrometer is 200-650 nm."]
[9.87158203125, 1.8162462711334229, "The Orbit Revolutions/Day of the ALMASat-1 Satellite is 14."]
[1.2725447416305542, 4.155068874359131, "The Battery Status of the Grace Mission Satellite is Degraded."]
[6.86949348449707, 0.8690199851989746, "The Third Birthday of the SmallGEO Satellite is 14 September 2020."]
[11.040314674377441, 5.1560797691345215, "The Magnetic Field Strength of the CME (Coronal Mass Ejection) Solar Phenomenon is Double that of a normal CME."]
[5.333240509033203, 2.029118299484253, "The Age of the Iridium 33 Satellite is Modern."]
[9.087616920471191, 9.24666976928711, "The Field of View (FOV) of the Instrument Instrument is 52\u00ba."]
[7.547461032867432, 4.494449615478516, "The Observation Modes of the ALOS-3 Satellite is Nadir-looking and backward-looking panchromatic imager."]
[9.632180213928223, 1.6886085271835327, "The Orbit Repeat Cycle of the Altimetry Satellites Satellites is Every ten days."]
[6.38218879699707, 0.769912600517273, "The Patent Award Date of the GHGSat-D Satellite System is January 2016."]
[7.857309341430664, 6.427313327789307, "The Frequency of the Internal Satellite Diffuser Calibration Device is Potentially every orbit."]
[9.326047897338867, -0.5538087487220764, "The Primary Goals of the Dellingr Nanosatellite is 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."]
[8.217667579650879, 7.612302780151367, "The Sun Tracking Device of the ORA Instrument Atmospheric Measurement Instrument is No."]
[11.988227844238281, 2.2124838829040527, "The URL of the OSIRIS-REx Spacecraft is https://www.asteroidmission.org/asteroid-operations/."]
[11.155778884887695, 2.429769515991211, "The Separation Date of the Schiaparelli Lander is 16 October."]
[5.650168418884277, 2.3833398818969727, "The Ground Station of the SAR-Lupe Satellite System is 1."]
[5.619841575622559, 5.029109001159668, "The Coordination Partner of the PAZ SAR Processor Ground Segment Processor is IGS (Ingenio Ground Segment)."]
[9.711662292480469, 1.435891032218933, "The Start Time of the Solar Eclipse Event is 11:00 UTC."]
[11.524619102478027, 6.585509777069092, "The Number of X-ray Source Detections of the 3XMM Catalogue X-ray Source Catalogue is 531 261."]
[6.611119270324707, 10.683634757995605, "The Estimated SNR of the Band 7 Spectral Band is 388.29 \u00b1 153.69."]
[7.248018264770508, 2.4517250061035156, "The Loss of Momentum and Expertise of the RISESAT Project is True."]
[10.228609085083008, 8.727540969848633, "The Telescope Type of the EUVI Extreme Ultraviolet Imager is Small Ritchey-Chretien telescope."]
[5.254297256469727, 4.143028736114502, "The Provides the next increment \u201cSlot List\u201d of the LCT MCC Control Center is During the execution of increment N-1, the LCT MCC at GSOC provides the next increment \u201cSlot List\u201d."]
[7.679546356201172, 3.9840142726898193, "The Data Quality of the Landsat Satellite is Unmatched in quality, detail, coverage, and length."]
[9.20634651184082, 6.447649955749512, "The Performance of the ST (Star Tracker) Instrument is 10 arcsec."]
[6.915261268615723, 3.291534185409546, "The Mission Status of the HJ-1 Satellite is Operational (extended)."]
[9.150755882263184, 8.02496337890625, "The Size of the Particle Detectors Instrument is 95 mm x 122 mm x 217 mm."]
[10.353296279907227, 1.3122341632843018, "The LTAN of the SARAL spacecraft Satellite is 6:00 hours."]
[8.783080101013184, 10.658897399902344, "The Compressed Data Rate of the Camera Imaging Device is 105 Mbit/s."]
[7.549091815948486, 1.427157998085022, "The Impact Date of the LADEE Satellite is April 18, 2014."]
[5.842447757720947, 3.0391061305999756, "The Manufacturer of the GFO Satellite is BATC (Ball Aerospace & Technology Corporation)."]
[9.656998634338379, 6.701361656188965, "The Development and Qualification of the LISA Pathfinder Cage and Vent Mechanism Mechanism is 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-."]
[10.819625854492188, 5.869082927703857, "The Effect of Gravity of the Light Electromagnetic Radiation is Energy loss, lower frequency, longer wavelengths."]
[6.889302730560303, 1.0276902914047241, "The Bulletin Publication Date of the GPS/MET Satellite is April 1998."]
[7.032910346984863, 9.775437355041504, "The Wavelength Range of the Band No 5 Spectral Band is 10.5 \u00b1 0.50 - 11.5 \u00b1 0.50 \u00b5m."]
[5.218087196350098, 1.8406453132629395, "The P-POD Deployment of the CubeSat - Launch 4 Satellite is Successful."]
[4.818184852600098, 9.016661643981934, "The Movement of the InSight's robotic arm Robotic Arm is Helped \"the mole\" dig nearly 2 cm over the past week."]
[6.033506393432617, 2.9152684211730957, "The Design Copyright of the BRITE-PL Satellite Project is SFL."]
[7.773252010345459, 10.80005168914795, "The Analog to Digital Conversion of the Front End Electronics Electronics is 12 bit."]
[6.944110870361328, 2.242035388946533, "The Authors of the Hokkaido Satellite Project Satellite is 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."]
[8.382034301757812, 0.6433366537094116, "The Health Check Completion Date of the Hitomi X-ray Astronomy Satellite is March 26, 2016."]
[6.356281757354736, 8.465960502624512, "The Radar Sensitivity of the JPL Microwave Radiometer Radiometer is 12 dBZ."]
[10.284526824951172, 3.067997694015503, "The Launch Altitude of the James Webb Space Telescope Space Telescope is Approximately 870 miles (1,400 km)."]
[2.1149802207946777, 3.885305404663086, "The Solar Arrays Type of the Power Subsystem Satellite is Sun-tracking."]
[4.80818510055542, 4.302223205566406, "The Project Overview Author of the Optical Inter-orbit Communications Engineering Test Satellite (OICETS) Satellite is Katsuyoshi Arai."]
[9.498895645141602, 10.506915092468262, "The File Format of the Iris Video Camera Camera is MPEG-4."]
[8.146754264831543, 7.701139450073242, "The Data Cadence of the IMPACT and PLASTIC Instruments is Approximately 1 minute."]
[6.036613941192627, 3.6928627490997314, "The Lean and Collaborative of the Development Approach Satellite Instrument Development is The instrument builder and PI can openly discuss and trade available margins on design and science requirements during instrument development."]
[6.156437397003174, 0.7340365648269653, "The Launch Date of the RAVAN CubeSat is November 2016."]
[7.754298686981201, -0.4541950523853302, "The Launch Time of the SpaceX CRS-13 Mission is 15:36 GMT."]
[9.62206745147705, 9.835061073303223, "The Launch Location of the ShadowCam Instrument is Cape Canaveral."]
[6.157106876373291, 3.471442222595215, "The Service of the Spire Global UK Company is Predictive analysis for global shipping, aviation and weather forecasting."]
[5.9604172706604, 6.303024768829346, "The Swath Width of the StriX-\u03b1 SAR Satellite is More than 10-30 km."]
[5.77471399307251, 1.6131521463394165, "The Conference Presentation of the GOMX-1 Satellite is 11th Annual CubeSat Developers\u2019 Workshop."]
[5.870743751525879, 5.875130653381348, "The Antenna Size of the Biomass Satellite is 12 m diameter."]
[7.262397766113281, 6.145695686340332, "The Authors of the Case studies of aerosol retrievals Study is J. B. Chowdhury, B. Cairns, L. D. Travis."]
[6.003905296325684, 4.4436492919921875, "The Technology of the MSAS Satellite-based Augmentation System is Advanced technologies such as satellite orbit ranging, and ionospheric and tropospheric delay estimation assumption."]
[8.50147533416748, 1.0276275873184204, "The Operation Duration of the RAIDS Instrument is Eight months."]
[9.496164321899414, 0.977132260799408, "The Operation Duration of the QB50 CubeSat Constellation Satellite Constellation is 3 months."]
[8.28283405303955, 9.053098678588867, "The Swath Width of the HSRS Sensor is 190 km."]
[4.082085132598877, 4.036993980407715, "The Functionality of the Core-DHS Avionics Module is Same level as heritage equivalent avionics stack."]
[4.248514652252197, 6.957189083099365, "The Transmit Frequency (MHz) of the HRIT HiRID Data Receiver is 1558."]
[7.54040002822876, 7.529460430145264, "The | of the Atmospheric Turbulence Monitoring System Monitoring System is Atmospheric turbulence monitoring at DLR."]
[11.290312767028809, 1.2953745126724243, "The Design Life of the Jade Rabbit Moon Rover is 3 months."]
[1.5213009119033813, 4.9524922370910645, "The Output Voltage (Redundant) of the LVPS Board Power Supply is +1.5 V."]
[9.07326889038086, 5.124492645263672, "The Stabilization of the FORTE Spacecraft is Momentum-biased, gravity-gradient stabilized (nadir-pointing)."]
[4.023693561553955, 5.723280906677246, "The Telemetry Downlink Data Rate of the GIOVE-B Satellite is 31.250 kbit/s."]
[9.012983322143555, 4.626049041748047, "The NLC Observation Peak of the AIM spacecraft Satellite is During solar minimum."]
[6.965346813201904, -0.06427116692066193, "The End of Life Date of the KySat-2 Satellite is 28 February 2014."]
[8.302802085876465, 10.0635347366333, "The Total Number of Pixels of the MS Bands Detector Line Arrays is 7,500."]
[9.772136688232422, 3.1320860385894775, "The Orbit of the ETS-VIII Spacecraft is Geostationary orbit at 146\u00ba E longitude."]
[9.607322692871094, 7.804995059967041, "The Proton Energy of the GALS-VE Particle Energy Measurement Device is > 600 MeV."]
[8.151082992553711, 0.18698948621749878, "The Extension Date of the International Space Station Space Station is April 27, 2023."]
[11.6967191696167, 6.209962368011475, "The Launch Date of the XMM-Newton X-ray Space Observatory is 10 December 1999."]
[5.3701019287109375, 10.372761726379395, "The Revisit Time of the LIS Lightning Image Sensor is 4 days."]
[5.312401294708252, 4.666833877563477, "The Data Reception Station of the Ground Segment Satellite Ground Segment is Svalbard (Spitzbergen)."]
[6.953397274017334, 0.4941587746143341, "The Launch Date of the FITSat-1 Satellite is 21 July 2012."]
[10.383746147155762, 5.093533992767334, "The Firing Direction of the Micronozzle Propulsion System is -X."]
[6.810509204864502, 7.075638294219971, "The Funding Source of the CATS Lidar Instrument is International Space Station Program."]
[6.599209308624268, 3.9233579635620117, "The Status of the ResourceSat-2 Satellite is Production."]
[7.220316410064697, 4.521328449249268, "The Band 1 of the Landsat TM Satellite is Coastal water mapping, soil/vegetation differentiation, deciduous/coniferous differentiation, chlorophyll absorption."]
[5.272310256958008, 1.4420528411865234, "The Clocks of the GIOVE-B Satellite is Better than 1 ns per day."]
[11.429861068725586, 3.8783068656921387, "The Water Decomposition Time Scale of the Mars Planet is Centuries."]
[6.904271602630615, 4.746333599090576, "The Multispectral Mode Bands of the SPOT satellite constellation Satellite Constellation is Red, green and infrared bands of the visible spectrum."]
[10.342734336853027, 8.368371963500977, "The Purpose of the Telescope-coronagraph 304 \u00c5 Telescope is Imaging hot plasma (T ~ 10 MK) of the solar corona."]
[9.234487533569336, 6.11591911315918, "The Role of the IMU Inertial Measurement Unit is Determine initial attitude at de-boost."]
[7.08783483505249, 4.453217506408691, "The Measurement Domain of the GF-3 Satellite is Land."]
[9.265225410461426, 10.211372375488281, "The Observation Directions of the MSU-100 Camera is \u00b18.7\u00ba, 0\u00ba."]
[7.249214172363281, 1.3085322380065918, "The Conference Presentation Date of the EO-1 Satellite is June 22-24, 2004."]
[6.915631294250488, 9.160676956176758, "The Azimuth Resolution of the High Resolution Spotlight Imaging Mode is 1.1 m (single pol.)."]
[7.584803581237793, 1.1302485466003418, "The Release Date of First 13 Photos of the Gaofen-1 Satellite is June 6, 2013."]
[9.14863109588623, 9.142180442810059, "The Field of View of the Lens Optical Instrument is 24\u00ba x 96\u00ba."]
[7.118549346923828, 1.4843947887420654, "The Meeting Date of the GMES Sentinel-3 Satellite is Sept. 16, 2010."]
[7.38515567779541, 9.297685623168945, "The Field of View of the A Photometer Instrument is 0.1o x 2.1o."]
[5.027626991271973, 3.5641021728515625, "The Function of the System satlets Satellite Subsystem Type is Designed so each satlet constitutes a complete standalone system."]
[6.115415096282959, 0.04528498277068138, "The Launch Date of the Galileo FOC-3 and FOC-4 satellites Satellite is 27 March 2015."]
[10.496299743652344, 7.483166217803955, "The Properties to Investigate of the Bricks Building Material is Number and orientations of protein bridges, compressive strength, and porosity."]
[11.690208435058594, -1.1682246923446655, "The Mass of the IRS-1B Satellite is 975 kg."]
[3.741490364074707, 6.574297904968262, "The Interference Source Characteristics of the SMOS RFI Team Team is Topology, Power, Behaviour."]
[7.281051158905029, 0.7755658626556396, "The Planned Launch Date of the Heinrich Hertz Satellite is 2016."]
[8.786853790283203, 10.22034740447998, "The CMOS Image Sensor Type of the Imager Payload is Radiation-hardened."]
[8.895620346069336, 7.372822284698486, "The Quantity of the Electrostatic Analysers Sensor is 2."]
[9.851401329040527, 1.4794615507125854, "The Traditional Delivery Time of the Polar Satellite Data Data is 2 to 6 hours after the time of measurement."]
[5.132185935974121, 6.060652732849121, "The Rx Channels of the Complete Solution Antenna Configuration is 5."]
[5.595740795135498, 1.5389764308929443, "The | of the Falcon 9 Launch Vehicle is Spaceflight gears up for dedicated Falcon 9 launch."]
[5.97334623336792, 6.227736949920654, "The SAR Payload Spatial Resolution of the RCM Satellite is 5 - 50 m."]
[7.818280220031738, 4.000778675079346, "The Mission Type of the Aditya-L1 Satellite is Study the Sun."]
[5.56212854385376, 6.6663031578063965, "The Polarization of the Antenna Radar Antenna is Dual (H and V)."]
[7.282545566558838, 0.3655116558074951, "The Mission Launch Date of the PACE Satellite is 2023."]
[3.611469030380249, 4.609071731567383, "The Data Processing Algorithm of the V5QV FPGA FPGA is MSPI algorithm."]
[9.948397636413574, 1.4894354343414307, "The MLST Excursion of the Envisat Satellite is 10 minutes."]
[8.704927444458008, 5.667179107666016, "The Magnetometer Suite of the RAX-1 Satellite is Two internally mounted tri-axial magnetometers and four dual axis magnetometers mounted on external faces of the satellite."]
[5.810245513916016, 5.898130893707275, "The Antenna Size of the Biomass satellite Satellite is 5 m diameter."]
[4.298279762268066, 7.127933502197266, "The Weight of the PowerCell Hardware is 4.3 kg."]
[4.846269130706787, 5.481356143951416, "The Data Transmission Bands of the ICEYE-X1 Satellite is S- and X-band."]
[7.47138786315918, 2.432969331741333, "The Phase of the ELSA-d Satellite Mission is AIT (Assembly, Integration and Test)."]
[6.2817912101745605, 3.091707706451416, "The Contribution to the Orion Program of the European Service Module Spacecraft Module is IAC 2015."]
[7.777270793914795, 9.729825019836426, "The Spatial Resolution of the IRS Imager is Halved with regard to IRMSS."]
[6.214641571044922, 8.216052055358887, "The Dicke Load Phases of the MWR Noise Injection Radiometer is Three."]
[9.392311096191406, 6.073232650756836, "The Performance of the SpinKF Attitude Determination System is Very well."]
[11.69649600982666, -1.1418685913085938, "The Remaining Useable Propellant of the OrbView-3 Satellite is 22.98 kg."]
[3.5926713943481445, 2.3093128204345703, "The Size of the OptiCube-2 Satellite is 3U."]
[5.931551933288574, 1.8490313291549683, "The Launch Vehicle of the ResourceSat-2A Satellite is PSLV-C36."]
[8.456523895263672, 4.738929271697998, "The Objective of the Cluster S/C Satellite is Provision of intercalibrated measurements of the magnetic field vector B."]
[8.996288299560547, 6.6950297355651855, "The Mounting Orientation of the OPS systems Sensor is Not flat to the surface but shifted inside the body of MASCOT."]
[3.296722173690796, 4.785594463348389, "The Start-up ROM Capacity of the RAD750 SBC Single Board Computer is 64 KB."]
[6.339564323425293, 7.238596439361572, "The Backscatter Coefficient Accuracy of the ALT Experiment Altimeter is 1.0 dB."]
[3.2184128761291504, 5.371665000915527, "The Storage Capacity of the SSRNI Data Acquisition and Registration System is 4 Gbit."]
[1.255745768547058, 4.160000801086426, "The Battery Capacity of the DSX Spacecraft Payload Module Satellite is 60 Ah."]
[11.363619804382324, 1.3648018836975098, "The Wake Up Time of the Yutu-2 Rover is 1:45 p.m. Sunday."]
[11.77079963684082, 4.718356132507324, "The Type of the Andromeda Galaxy is Spiral."]
[11.536216735839844, -1.274535059928894, "The Weight of the ALTIUS Satellite is 266 kg."]
[5.844306468963623, 8.088272094726562, "The Center Frequencies of the ICI instrument Receiver is 183 GHz, 243 GHz, 325 GHz, 448 GHz and 664 GHz."]
[1.7669318914413452, 4.785879611968994, "The Power of the EPS Electric Power Subsystem is < 8.6 W."]
[8.06789493560791, -0.6481521725654602, "The Docking Location of the Cargo Dragon Spacecraft is Harmony module."]
[7.337906360626221, 0.7741605639457703, "The Mishap Investigation Board Creation Date of the Glory Satellite is March 7, 2011."]
[3.1710262298583984, 4.993772983551025, "The RAM of the SDR Host Computer Computer is 8 GB."]
[3.6611955165863037, 6.6526055335998535, "The Transmission Rates of the XBT X-band Transmitter is 12.5, 25, or 50 Mbit/s."]
[7.206025123596191, 6.897328853607178, "The Arrival Date of the NIRSpec Instrument is Sept. 30, 2013."]
[7.823024272918701, 8.86708927154541, "The Performance Range of the UV-1 Spectrometer is 270 - 310 nm."]
[8.967761039733887, 5.212677478790283, "The Attitude Accuracy of the DubaiSat-1 Satellite is 0.2\u00ba."]
[9.140251159667969, 7.40645170211792, "The Measurement Duration of the Temperature Sensor is 420 s."]
[10.581960678100586, 7.524814128875732, "The Material of the WISA Woodsat Satellite is Plywood."]
[7.218577861785889, 1.2253203392028809, "The Publication Date of the Orbital Formation-Keeping System System is Jan.\u2013 Feb. 1989."]
[4.77871561050415, 0.8275762796401978, "The Contract Award of the Lockheed Martin Company is $700 million."]
[5.668734550476074, 3.465628147125244, "The Manufacturer of the NAOMI Imager is Airbus DS (former EADS Astrium SAS)."]
[7.90750789642334, 4.622528553009033, "The Camera Resolution of the Shakuntala Satellite is One of the highest."]
[2.243828773498535, 6.500542640686035, "The Latency of the ATL18 Land/Canopy Gridded Data is 45 days from receipt of last data in product."]
[5.816486358642578, 3.4899697303771973, "The Operation Center Location of the Cheops Satellite is Torrej\u00f3n, near Madrid, Spain."]
[9.799737930297852, 3.841939687728882, "The Sail Deployment Time of the InflateSail Satellite is Approximately one hour after ejection."]
[9.413993835449219, 3.4945151805877686, "The Mission of the Lunar Flashlight Satellite is Exploration Mission 1."]
[4.852301120758057, 4.699687480926514, "The Connection Type of the Ground Station Communication System is Ethernet over IP (Internet)."]
[8.608981132507324, 10.615559577941895, "The Quantum Efficiency of the Instrument CCD Imaging Camera is 0.8 at 630 nm."]
[9.198958396911621, 5.240105628967285, "The Attitude Control of the Deimos-2 Satellite is Three-axis."]
[4.5215373039245605, 6.967072010040283, "The ADC Sampling Rate of the Rx Module Digital Receiver is 40 Msamples/s."]
[7.214925289154053, 5.123290061950684, "The Purpose of the GeoCarb Satellite is Distinguish between man-made and natural emissions."]
[9.919547080993652, 1.5492030382156372, "The Length of Operation of the Solar Measurements Instrument is 5\u201310 min per orbit."]
[1.8785730600357056, 3.9119882583618164, "The GaAs of the Solar Array Type is The EPS (Electrical Power Subsystem) uses GaAs solar cells."]
[4.154129981994629, 5.0102458000183105, "The Developer of the ODTML Data Collection System is Praxis Inc.."]
[9.171293258666992, 4.21963357925415, "The Bus Size of the Spacecraft Satellite is 1.4 m x 1.4 m x 2 m."]
[5.275908946990967, 10.2536039352417, "The Instruments of the MTG-I Satellite is Flexible Combined Imager (FCI) and Lightning Imager (LI)."]
[4.891188144683838, 12.098394393920898, "The Responsivity Requirement of the Responsivity Measurement Instrument is >0.89 A/W."]
[9.936994552612305, 5.17311429977417, "The Review of the Electric Propulsion Space Experiment (ESEX) Space Experiment is Journal of Propulsion and Power, Vol.18 No.4, 2002, pp. 723-730."]
[7.0558929443359375, 1.4819402694702148, "The Date of the IGARSS Symposium is July 21-26, 2013."]
[9.385527610778809, 5.178295612335205, "The Rotation Rate of the Reaction Wheels Satellite Component is Up to 60,000 rpm."]
[9.426435470581055, 2.71976900100708, "The Dosimetric Results of the Eureca Satellite is Unknown."]
[10.268340110778809, 4.637852191925049, "The Propellant Expulsion of the Advanced Composition Explorer Spacecraft is The pair of the tanks with less fuel expelled all of its propellant by 2014."]
[10.116157531738281, 6.865084171295166, "The Thermal Modeling Supporter of the Edison Demonstration of Smallsat Networks Project Project is Robert F. Coker."]
[10.451027870178223, 4.782948970794678, "The Pulse Trains of the LM thruster Thruster is Pulses on the order of 500 ms."]
[6.156121730804443, 5.976109027862549, "The Resolution of the SAR Image Satellite Image is 3-meter."]
[5.063724040985107, 5.300475597381592, "The Number of Antennas of the KSAT Company is More than 130."]
[7.771823406219482, 9.132218360900879, "The Spectral Channels of the SAGE-III Instrument is 9 solar 290-1550 nm."]
[5.976776599884033, 4.453066825866699, "The Funding of the GPSP Instrument is NOAA."]
[8.105891227722168, 8.72493839263916, "The Exposure Time of the NISP Photometer Instrument is About 100 seconds per filter."]
[4.400669097900391, 7.764735698699951, "The Center Frequency of the Channel 1 Sensor is 10.6 GHz."]
[4.559567451477051, 5.4173102378845215, "The Communication of the TT&C System Satellite System is Effective and reliable UHF communication with BRMM."]
[7.623577117919922, -0.4976692199707031, "The Arrival Time at Space Station of the Cygnus Cargo Spacecraft is Around 6:10 a.m. Thursday, Aug. 12."]
[12.125069618225098, 2.1725237369537354, "The Launch Date of the OSIRIS-REx Spacecraft is September 2017."]
[7.047990798950195, 4.157818794250488, "The Measurement Domain of the KySat-2 Satellite is Ocean, Land, Snow & Ice."]
[10.002450942993164, -0.6104168891906738, "The Altitude of the 7 microsatellites Satellite is 515 km."]
[4.857796669006348, 1.7072912454605103, "The Number of Satellites of the FormoSat-7/COSMIC-2 Satellite Constellation is 6."]
[10.286566734313965, 2.992762804031372, "The Target Orbit Altitude of the Bion-M1 Spacecraft is 575 km."]
[7.327363014221191, 6.8920135498046875, "The Publication Date of the DESIS Instrument is October 2019."]
[7.050516128540039, 2.8478832244873047, "The Data Interface and Control Design of the SWEM Satellite is Derived from the MAVEN DCB."]
[6.636179447174072, 0.8194580078125, "The Launch Date of the NigeriaSat-1 Satellite is Sept. 27, 2003."]
[7.002810478210449, 1.1480563879013062, "The Contract Win Date of the Spire, GeoOptics Companies is Sept. 16, 2016."]
[10.541708946228027, 2.2900211811065674, "The Inclina. (\u00ba) of the Meteor-2-1 Satellite is 81.3."]
[9.600040435791016, 5.513868808746338, "The LAM Thrust of the AOCS Attitude and Orbit Control System is 440 N."]
[10.708612442016602, -1.5353407859802246, "The Cargo Delivery of the SpaceX Cargo Resupply Mission is More than 2,910 kg."]
[7.579665184020996, 0.022444695234298706, "The Launch Date of the CHEOPS Satellite is 2017."]
[7.993307590484619, 1.3271969556808472, "The Unboxing Date of the Mercury Magnetospheric Orbiter Spacecraft is April 29, 2015."]
[4.581197261810303, 4.121143341064453, "The Conference Presentation Date of the Appliqu\u00e9 Sensor Interface Module Sensor Interface Module is Aug. 13-16, 2007."]
[9.05877685546875, 4.817503929138184, "The Observation Capability of the STEREO spacecraft Satellite is More than 270\u00ba of solar longitude."]
[9.148438453674316, 4.232032299041748, "The Dimensions of the Bus Bus is 1.6 m x 1.6 m x 1.5 m."]
[7.488149642944336, 3.1483871936798096, "The Sensor Complement of the RaInCube Satellite is Unknown."]
[5.380340099334717, 2.659118890762329, "The Project Partners of the SPORT CubeSat is NASA, the Brazilian National Institute for Space Research (INPE), and the Technical Aeronautics Institute under the Brazilian Air Force Command Department (DCTA/ITA)."]
[6.527854919433594, 0.7617517709732056, "The On-Orbit Verification Mission of the TET-1 Spacecraft is IAC 2013."]
[11.23266887664795, 5.761416912078857, "The Theory of Gravity of the General Theory of Relativity Physics is Needs a modification."]
[10.220571517944336, 2.980679988861084, "The Orbit Altitude of the STSAT-3 Satellite is ~600 km."]
[8.281862258911133, 4.8829498291015625, "The Operating Ranges of the Cluster S/C Satellite is 64 to + 63.992 nT, 256 to + 255.97 nT, 1024 to + 1023.9 nT, 4096 to + 4095.5 nT, 65536 to + 65528 nT."]
[5.759939670562744, 3.217500925064087, "The Developer of the Flight Computer Satellite is GSFC."]
[4.341692924499512, 4.880257606506348, "The Data Transfer Protocol of the Ground Support System System is TFTP (Trivial File Transfer Protocol)."]
[7.099195957183838, 0.6221678853034973, "The Launch Date of the Odin Satellite is 20 Feb 2001."]
[4.443865776062012, 2.9950203895568848, "The PRN of the GSAT-0208 Satellite is 8."]
[5.219503402709961, 4.155993938446045, "The Provider of the Mission Control System Control System is GomSpace."]
[9.168082237243652, 10.294210433959961, "The Number of Images Captured of the PolyCam Camera is 7000 images."]
[7.7174072265625, 4.526763439178467, "The Mounting of the ATLAS Sensor Sensor is Spacelab pallet(s)."]
[9.543131828308105, 7.549356460571289, "The Temperatures of the Cooler Passive Cooler is 81 K for LWIR patch."]
[7.042766571044922, 8.289522171020508, "The Power Transfer of the MWI Instrument Scan Mechanism Assembly is 200 W."]
[4.174115180969238, 3.1497607231140137, "The Connectivity of the 5G Network Telecommunications Network is Reliable connection for people and devices, anytime and anywhere, with increased security."]
[2.3049094676971436, 5.738100528717041, "The Peak RF Power of the HPA High Power Amplifier is 120 W."]
[9.989380836486816, -0.5628710389137268, "The Orbit Type of the Vstar Gravity-field Measurement Microsatellite is Near-circular."]
[5.421716213226318, 3.911834478378296, "The Number of Elements of the Ground Segment Satellite Ground Segment is 2."]
[10.114349365234375, 2.9426984786987305, "The Altitude of the IRS-1B Satellite is 904 km."]
[8.875189781188965, 9.04969596862793, "The Beam Focal Length of the Spectrometer Instrument is 400 mm."]
[9.44123363494873, 1.1433264017105103, "The Mission Time of the Tandem-L Satellite is > 10 years."]
[6.317440032958984, 9.226932525634766, "The Mass of the MuREM Radiation Monitor is ~400 g."]
[5.885784149169922, 3.009006977081299, "The Manufacturer of the CAPSTONE Satellite is Rocket Lab."]
[11.531269073486328, -1.266850233078003, "The Total Mass of the Eutelsat 172B Satellite is 9,969 kg."]
[5.932906150817871, 8.517402648925781, "The Measurement Altitude Range of the MLS Microwave Limb Sounder is Upper troposphere to the lower thermosphere."]
[4.64484167098999, 6.796961784362793, "The Electronics Unit Dimensions of the PRARE ground transponder Ground Station Equipment is 560 x 560 x 300 mm."]
[8.173731803894043, 10.485780715942383, "The Data Storage of the TDI Signal Processing Technique is TDI chain."]
[9.59350299835205, -0.864567220211029, "The Launch Date of the JL-1-GF03B Microsatellite is 15 September 2020."]
[3.631108045578003, 4.88247013092041, "The Analog to Digital Conversion (ADC) of the dsPIC33F microcontroller Microcontroller is Unknown."]
[6.827198028564453, 10.035181045532227, "The Bandwidth of the Band 7 Spectral Band is 735-755 nm."]
[5.895816802978516, 6.6003031730651855, "The Frequency Bands of the SIR-C Radar System is C-band, L-band, X-band."]
[9.130131721496582, 10.205520629882812, "The Temperature Range of the LWIR Cameras Camera is -59\u00b0C to 113\u00b0C."]
[8.63825511932373, 8.387223243713379, "The Type of the FPP Telescope Component is Housing two filtergraphs and a spectro-polarimeter."]
[11.575014114379883, 4.340220928192139, "The Distance from Earth of the HAT-P-7 Exoplanet is About 1,000 light years."]
[10.062169075012207, 4.094346523284912, "The Solar Sail Deployment Test Environment of the NEA Scout Spacecraft is Large, low-friction table."]
[5.45085334777832, 3.4818689823150635, "The Architecture of the Instrument Carrier Carrier is Leverages GSFC recent experience with the James Webb Space Telescope ISIM (Integrated Science Instrument Module) structure."]
[2.0197255611419678, 7.844825744628906, "The Change Date of the ACE Realtime Solar Wind Lists Data Service is Feb. 21, 2015."]
[8.107629776000977, 9.468427658081055, "The Radiometric Resolution of the OLI-2 Instrument is 14-bit."]
[4.9661383628845215, 4.540117263793945, "The Level 0-1b & Level 2 processing facility of the PDGS Payload Data-processing Ground Segment is Hosted."]
[5.222489833831787, 1.664961814880371, "The Deployment Count of the J-SSOD (JEM Small Satellite Orbital Deployer) CubeSat Deployment System is 10."]
[12.011612892150879, 3.2515926361083984, "The Orbit Inclination of the Lunar Landing Vehicle Vehicle is 45\u00ba."]
[7.3806843757629395, 10.030282020568848, "The Technology Basis of the Hyperspectral Imaging Remote Sensing Technology is High spectral resolution measurements of light interacting with matter."]
[7.4811906814575195, 6.000339031219482, "The Spectral Range of the CLARREO Satellite is 0.32 to 2.3 \u00b5m."]
[5.498030662536621, 3.7760050296783447, "The Function of the PASTEC Payload System is Study the orbital environment, studying concepts such as the measurement of satellite dynamics (MEDY) and electrostatic potentials outside the SPOT spacecraft (SILLAGE)."]
[5.753721237182617, 2.764376163482666, "The Agreement of the ABB Technology Company is Signed with GHGSat to deliver the payloads for GHGSat\u2019s next 3 methane detecting satellites."]
[2.9753124713897705, 6.596259117126465, "The Power Amplifier of the Navigation Antenna Antenna is 50 W."]
[9.290461540222168, 7.2261199951171875, "The Ignition Duration of the T3\u00b5PS Pressure Sensor is 10 seconds."]
[6.566496849060059, 3.36436128616333, "The Payload of the MPQ442 Satellite is Qubduino."]
[7.157549858093262, 0.20751242339611053, "The Launch Year of the MTG-S satellite Satellite is 2024."]
[9.086235046386719, 1.574064016342163, "The Revisit Time for CCD Camera of the Satellite HY-1B is Seven days."]
[8.886448860168457, 2.842331647872925, "The Alternate Name of the GCOM-C Satellite is SHIKISAI."]
[5.075223922729492, 1.9030470848083496, "The Number of Fixed Experiments of the EAGLE Spacecraft is 4."]
[6.196557998657227, 1.2521308660507202, "The Revenue Start of the Eutelsat Quantum Satellite is Fiscal 2021."]
[9.680657386779785, 8.60041618347168, "The Number of Mirrors of the Laser Retroreflector Array (LRA) Instrument is 9."]
[9.313919067382812, 3.1672840118408203, "The Orbit of the GF-3 Satellite Satellite is Sun-synchronous orbit."]
[9.49699592590332, 4.300026893615723, "The Diameter of the SpinSat Spacecraft is 558 mm."]
[5.696758270263672, 2.8514552116394043, "The Manufacturer of the NewSat Satellite is Satellogic."]
[4.2460036277771, 4.558793544769287, "The Function of the Organ-Chips Device is Study organ physiology and diseases in a laboratory setting."]
[7.575971603393555, 1.7250913381576538, "The Availability of the Segments Program Segments is Via AsteroidDay.org, via SES Satellite, via ESA Web TV, ESA\u2019s YouTube channel."]
[7.893908500671387, 9.049151420593262, "The Wavelengths of the ATOMMS Spectrometer is Centimeter and millimeter."]
[6.841216564178467, 5.483676433563232, "The Measurement Coverage of the SMAP Satellite is Global land area, excluding regions of snow and ice, mountainous topography, open water, and areas of extremely dense vegetation such as tropical forests."]
[5.917272090911865, 6.766058921813965, "The Field of View of the LRR Radar is \u00b157.6\u00b0."]
[7.865730285644531, 5.048898220062256, "The Position Accuracy of the PROBA-2 Satellite is 200 m (2\u03c3) on each axis."]
[11.41242504119873, 2.252999782562256, "The Hill Coordinate System of the Hayabusa-2 Spacecraft is The Sun is always to the left and outside the figure."]
[8.409723281860352, 9.793139457702637, "The Field of Regard of the Pushbroom imager Optics is \u00b130\u00ba."]
[7.815228462219238, 2.2537684440612793, "The Publisher of the Observation of the Earth and Its Environment: Survey of Missions and Sensors Documentation is Herbert J. Kramer."]
[5.356156349182129, 5.609682083129883, "The Number of GPS Satellites of the T3000G2 receiver GPS Receiver is 8."]
[4.893059253692627, 6.4622273445129395, "The Stiffness of the Antenna Communication is > 0.1 Hz (in orbit)."]
[7.363936901092529, 0.525164783000946, "The Launch Date of the STARS spacecraft Satellite is January 23, 2009."]
[7.541064739227295, -0.04268014803528786, "The Manufacturing Start Date of the CHEOPS Instrument is Mid-2013."]
[9.715751647949219, 8.095580101013184, "The Spacecraft Attitudes Range of the GMOD Detector is From zenith (0\u00ba) to nadir (180\u00ba)."]
[8.740556716918945, 6.591757774353027, "The Purpose of the Nexus S magnetometer Attitude Determination Device is Measuring the local magnetic field."]
[6.318508148193359, 4.37324333190918, "The Type of the RADARSAT-1 Satellite is Earth-imaging radar satellite."]
[5.587603569030762, 2.8635153770446777, "The Function of the Restore-L servicer Robotic spacecraft is Extend a satellite's lifespan."]
[9.900703430175781, 1.6357120275497437, "The Data Latency of the MetOp Satellite Satellite is 65 minutes."]
[9.5684175491333, 5.945080757141113, "The Manufacturer of the CubeSense Attitude Determination and Control Subsystem is University of Stellenbosch, South Africa."]
[7.234910011291504, 5.6276021003723145, "The Description of the Sudden Stratospheric Warming Meteorological Event is 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."]
[8.246395111083984, 5.261176109313965, "The Real-Time Orbit Determination Accuracy of the GF-3 Satellite Satellite is Better than 10 m (1\u03c3)."]
[7.388771057128906, 0.9575275778770447, "The Launch Date of the Philae Spacecraft is Unknown."]
[4.025852680206299, 2.389599561691284, "The Size of the CIRAS Satellite is 6U."]
[7.250922679901123, 2.5825960636138916, "The Mission of the Orbiting Carbon Observatory Satellite is Unknown."]
[9.62753963470459, 8.128212928771973, "The Affiliation of the Gamma-ray Spectrometer Experiment Experiment is University of New Hampshire."]
[8.224360466003418, 0.1777477264404297, "The AI Deployment Date of the CIMON-1 Prototype is 15 November 2018."]
[4.023545265197754, 4.984181880950928, "The Redundancy Type of the RPU Receiver Processor Unit is Cold internal redundancy."]
[9.313764572143555, 6.466538429260254, "The Anomaly Compensation of the Astro-APS Star Tracker is White spots."]
[8.430795669555664, 8.947819709777832, "The Angular Resolution of the CIRiS Instrument is 0.00122 radians."]
[3.5722010135650635, 4.5533223152160645, "The Fault Tolerant Software Developer of the FPGA Component is UFRGS (Universidade Federal do Rio Grande do Sul)."]
[6.75131893157959, 0.8394604325294495, "The Launch Date of the NigeriaSat-X Satellite is Unknown."]
[9.029969215393066, 8.944165229797363, "The OPD for Shortest Wavelength of the Telescope Optical Instrument is Stays below a quarter of a wave."]
[6.043687343597412, -0.0001290939108002931, "The Full Operational Capability Date of the Galileo Satellite Satellite is Unknown."]
[8.64785385131836, 8.570318222045898, "The Optical System of the PS2 Optical Instrument is Five element."]
[8.182735443115234, 8.492253303527832, "The Design Concept of the SHIMMER FTS Fourier Transform Spectrometer is 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."]
[4.539458274841309, 7.389095783233643, "The Mass of the DataLogger Payload is 2 kg."]
[7.034499645233154, 3.1276936531066895, "The Mission Programming of the VEN\u00b5S Satellite is Unknown."]
[7.716987133026123, 7.200610160827637, "The Principal Investigator of the ECOSTRESS Instrument is Simon J. Hook."]
[5.142302989959717, 6.878269672393799, "The Peak Gain of the Antenna Conically-scanning reflector is 36 dBi."]
[11.044249534606934, 5.11068058013916, "The Types of Eruptions of the Sun Star is Coronal mass ejection, jet, partial eruption."]
[6.446264266967773, 0.7453561425209045, "The Patent Filing Date of the GHGSat-D Satellite System is May 2015."]
[6.744235992431641, 4.270305633544922, "The Data License of the Copernicus Sentinel-3 Satellite is CC BY-SA 3.0 IGO."]
[6.003856658935547, 5.255837917327881, "The GPS Receiver of the S/C Satellite is Provides S/C location data for accurate orbit determinations and onboard time delivery."]
[7.68803596496582, 0.9525830149650574, "The Launch Year of the Sentinel-1A/B Satellite is 2016."]
[3.6243743896484375, 6.167447090148926, "The Uplink Speed of the ColKa Communication Device is Up to 2 Mbit/s."]
[6.545510292053223, -0.10016265511512756, "The Launch Date of the IRNSS-1C Satellite is Oct. 15, 2014."]
[11.234889030456543, 2.9142134189605713, "The Mass of the Boulder Geological Feature is 230 tons."]
[10.451918601989746, -1.1439673900604248, "The Mass of the Corvus-BC-3 Nanosatellite is 11 kg."]
[5.987435817718506, 9.601150512695312, "The Mass of the Instrument General is 15 kg."]
[4.991530895233154, -0.12780912220478058, "The Global Service Target of the OneWeb Satellite Constellation is 2021."]
[9.665205001831055, 6.072080612182617, "The Manufacturer of the ADCS Attitude Determination & Control Subsystem is XACT, Blue Canyon Technology."]
[6.767833232879639, 4.464812278747559, "The Journal Article of the Demeter Satellite is Chorus and chorus-like emissions."]
[7.963530540466309, 2.0020925998687744, "The Arrival at Mars of the ExoMars Trace Gas Orbiter Orbiter is 2016."]
[9.16694450378418, 5.967956066131592, "The Control Precision of the PCS Pointing Control System is One thousandth of a degree."]
[7.870912075042725, 8.311728477478027, "The Design Date of the CHRIS Imaging Spectrometer is Unknown."]
[11.638835906982422, 6.164361476898193, "The Article Date of the XMM-Newton Satellite is 20 January 2020."]
[9.455109596252441, 2.8608648777008057, "The Trajectory Analysis and Design Presentation of the OMOTENASHI Satellite is 26th International symposium on Space Flight Dynamics."]
[11.695647239685059, 5.147458553314209, "The Discovery of the MAXI J1820+070 Black Hole is Newly discovered."]
[6.575227737426758, 0.7581258416175842, "The Operation Start Date of the TET-1 Satellite is Oct. 16, 2012."]
[6.055681228637695, 3.0174081325531006, "The Funding of the SRTM Shuttle mission is NIMA."]
[8.084661483764648, 7.144652366638184, "The Developer of the AstroRad vest Radiation Protection is StemRad."]
[11.47970199584961, 4.159752368927002, "The Mass of the HAT-P-7 Exoplanet is Somewhat larger than the planet Jupiter."]
[7.190356254577637, 7.91604471206665, "The Registration Time of the DUV Instrument is 100 ms."]
[7.131052494049072, 4.854648590087891, "The Purpose of the EXPORTS Satellite Mission is Advance the utility of NASA ocean color assets to predict how changes in ocean primary production will impact the global carbon cycle."]
[7.449127197265625, 0.8881776332855225, "The Status Update Date of the SeaWiFS Satellite is Jan. 24, 2011."]
[3.812969923019409, 0.2797716557979584, "The Spacedaily Article Date of the GRAIL Mission is Dec. 12, 2007."]
[6.770783424377441, 3.3202295303344727, "The Operators of the SATis5 Satellite is Unknown."]
[4.905537128448486, -3.248931646347046, "The | of the Joseph K. Taylor Individual is Fred A. Best, Douglas P. Adler, Claire Pettersen, Henry E. Revercomb, P. Jonathan Gero, Joseph K. Taylor, Robert O. Knuteson, John H. Perepezko."]
[8.063873291015625, 10.007734298706055, "The Spatial Resolution of the EarthDaily Optical Imager Optical Imager is 5 m."]
[7.158219814300537, 0.9166259169578552, "The Launch Date of the Satellite Spacecraft is Unknown."]
[7.042068004608154, 0.7931144833564758, "The Operational Start Date of the RASAT Satellite is Start of 2012."]
[6.572288990020752, 7.466333866119385, "The Manufacturer of the LALT Laser Altimeter is NEC Corporation."]
[9.159162521362305, 9.82819652557373, "The Field of View of the NFI Near Field Imager is ~2\u00ba."]
[12.939863204956055, 4.8596110343933105, "The Detected Particles of the IBEX Spacecraft is Energetic Neutral Atoms (ENAs)."]
[7.698043346405029, 9.467024803161621, "The Spatial Resolution of the VIS Visible region of spectrum is 400 m (at nadir)."]
[5.870511531829834, 2.743330240249634, "The Considering Deals of the Rocket Lab Aerospace Company is True."]
[5.374875545501709, 1.3631672859191895, "The Launches in 2021 of the Falcon 9 Rocket is 8."]
[5.950526237487793, 1.6420490741729736, "The Payload of the PAZ Satellite is X-band SAR (Synthetic Aperture Radar)."]
[9.04962158203125, 0.6974968314170837, "The Growth Test Times of the Experiment Microbiology is Within 1-2 weeks, three months, six months after launch."]
[6.53410005569458, 5.702409744262695, "The Sensitivity to Instrument Degradation of the Occultation Techniques Atmospheric Study Method is Less sensitive than other remote sensing methods."]
[5.851019859313965, 1.854839563369751, "The Launch Vehicle of the Galileo FOC-3 and FOC-4 satellites Satellite is Soyuz-STB/Fregat-MT."]
[11.566831588745117, 3.982077121734619, "The Formation Time of the Pilbara and Yilgarn Cratons is About 2.2 billion years ago."]
[17.728055953979492, 7.16274356842041, "The J2000 declination (deg) of the J1846-0258 Pulsar is -2.97503."]
[7.5750508308410645, 4.9614176750183105, "The Purpose of the CIRCE Mission is Understanding the dynamics of the ionosphere."]
[5.59669828414917, 0.41794514656066895, "The Annual Salt Extraction of the Saltworks Salt Production Facility is 9 million metric tons."]
[9.825145721435547, 4.891712188720703, "The Firing Pressure of the X-axis Bang-Bang Maneuver Satellite Maneuver is 1.56 bar."]
[9.422588348388672, 2.687521457672119, "The Deployment and Retrieval of the Eureca Satellite is Unknown."]
[9.226134300231934, 8.381823539733887, "The Coupling Ratio of the OGS Data Detector Detector is 90% reach the fiber and 10% the ACT."]
[8.471357345581055, 2.9185731410980225, "The Most Powerful Auroras of the Jupiter Planet is Yes."]
[10.25722885131836, 3.0084047317504883, "The Orbital Height of the HyperScout\u00ae Satellite is 500 km."]
[7.274416446685791, 0.19291704893112183, "The Launch Date of the Restore-L Satellite is 2025."]
[9.005609512329102, 10.410635948181152, "The Lens of the LinkSprite JPEG color VGA camera Camera is 131o FOV wide angle lens."]
[9.138680458068848, 3.233065128326416, "The Type of the Orbit Centaur AV-042 upper stage is SSO."]
[7.2158989906311035, 0.949914276599884, "The Announcement Date of the European Commission Satellite Technology Acquirer is 8 October 2018."]
[4.466590881347656, 3.7006194591522217, "The Function of the Onboard Neural Network Artificial Intelligence is Detecting whistlers."]
[5.522849082946777, 4.050691604614258, "The Purpose of the MUSIS System is Surveillance, reconnaissance and observation."]
[11.901333808898926, 3.4190921783447266, "The Orbit of the OCO-3 Satellite is Mounted on the exterior of the space station, which circles between 52\u00ba north and 52\u00ba south latitude."]
[5.798463344573975, 2.8949460983276367, "The Manufacturer of the Tyvak 61C Satellite is Tyvak Inc.."]
[10.148554801940918, 5.443388938903809, "The Ignition of the CGG Cool Gas Generator is By a glow plug, avoiding the use of pyrotechnics."]
[8.406177520751953, 1.5629149675369263, "The Trajectory Change Start Date of the Rosetta Spacecraft is August."]
[11.846831321716309, -1.0340120792388916, "The Total Mass of the PSLV-C38 Launch Vehicle is ~955 kg."]
[9.325671195983887, -0.7473957538604736, "The | of the Miniature Imaging Spectrometer Imaging Spectrometer is Miniature Imaging Spectrometer for Aalto-1 Nanosatellite."]
[4.876150131225586, 5.008345603942871, "The Pass Duration of the Ground Stations Ground Station is 2.5 hours."]
[11.659266471862793, -1.1928991079330444, "The Mass of the SCD-2 Satellite is 117 kg."]
[9.169867515563965, 5.36122465133667, "The Control System of the S/C Satellite is Four reaction wheels and gyro-stellar attitude determination."]
[11.444721221923828, 6.119636058807373, "The Number of Main Sections of the XMM-Newton spacecraft Satellite is 4."]
[8.582609176635742, 6.2672576904296875, "The Boom Length of the AstroTube Payload is 1.5m."]
[5.138632297515869, 7.562809467315674, "The Source Data Rate of the Instrument Sensor is 200 bit/s."]
[6.0860395431518555, -0.03997078910470009, "The Development Date of the New maritime Galileo receiver Device is 24 June 2021."]
[9.976435661315918, 5.3195295333862305, "The Atmospheric Pressure of the Galileo probe Space Probe is About 320 pounds per square inch (22 bar)."]
[8.778352737426758, 9.018912315368652, "The Field of View of the AVHRR/3 Instrument is \u00b155.37\u00ba about nadir."]
[6.208416938781738, 6.17571496963501, "The Mode of the SAR Sensor Subsystem SAR Sensor is ST (Standard Mode)."]
[9.326430320739746, 6.339792728424072, "The Accuracy of the Star Trackers Attitude Determination Device is >99.45% per orbit."]
[5.375161647796631, 2.712376356124878, "The Manufacturer of the PACE 2U CubeSat is NCKU (National Cheng Kung University)."]
[7.81267786026001, -0.5419543385505676, "The Launch Date of the SpaceX CRS-24 Mission is 21 December 2021."]
[3.9126298427581787, 2.3289923667907715, "The Circuit Board Area of the ChipSat CubeSat is 3.5 cm2."]
[9.155112266540527, 1.1882272958755493, "The Data Processing Time of the CryoSat-2 Satellite is Within two days of acquisition."]
[8.959587097167969, 5.843719959259033, "The Components of the IMS-2 System Satellite System is 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."]
[6.78690767288208, 5.498950004577637, "The Data of the SMAP Satellite is Soil moisture status, timing and extent of potential frost damage."]
[8.478103637695312, 8.552282333374023, "The Detector Type of the SIS (Scanning Imaging Spectrograph) Spectrograph is Photon-counting."]
[9.619312286376953, 7.768829345703125, "The Energy Range of the HOPE Helium Oxygen Proton Electron is From less than or equal to 20 eV or spacecraft potential (whichever is greater) to greater than or equal to 45 keV."]
[6.439139366149902, 2.8315887451171875, "The Heat Shield of the Orion Spacecraft is Manufacturer Location."]
[7.806493759155273, 6.664088726043701, "The Measurement Frequency of the Global Oil Storage Monitoring Product is Weekly."]
[9.185195922851562, 2.92121958732605, "The Sea Ice Extent of the GCOM-W1 Satellite is 19.47 million km2."]
[10.290644645690918, 8.711647033691406, "The Exposure Time of the Coronal Hole Boundaries Imaging Device is < 10 seconds."]
[1.6363112926483154, 5.049133777618408, "The Voltage Conversion Level of the PCDM Power Conditioning Module is \u00b15 V level."]
[7.509711742401123, 4.772088527679443, "The SWIR Channels of the PROBA-V Satellite is 3."]
[8.149528503417969, 5.41720724105835, "The Control Electronics of the Lander Spacecraft is Provide the interface to all the sensors and the actuator drives."]
[12.91311264038086, 4.166019439697266, "The Percentage of Stars within 100 parsecs of the Gaia Catalogue of Nearby Stars Stellar Census is 92%."]
[10.597803115844727, 5.953963279724121, "The Goal of the RHESSI Satellite is Investigating particle acceleration and energy release in solar flares."]
[6.686975955963135, 6.075663089752197, "The Data Coverage of the QuikSCAT Scatterometer is Over 90% of the global ocean."]
[7.356151580810547, 7.523197174072266, "The Potential Locations of the MiniCOR Instrument is L1 (Lagrangian Point 1), L4 and L5."]
[12.984650611877441, 4.85826301574707, "The Mission Update Date of the IBEX Satellite is Nov. 14, 2011."]
[8.881012916564941, 7.297710418701172, "The Measurement of the SSAS Sensor is Sun angle."]
[7.40325403213501, 1.5972418785095215, "The Symposium Date of the MICROSCOPE Satellite is June 4-8, 2012."]
[12.10951042175293, 3.287609815597534, "The Inclination of the Rideshare mission Satellite is 97.6\u00ba."]
[7.1614298820495605, 2.9503848552703857, "The EarthCARE-ROSES Call of the CloudSat Satellite is Recommendation."]
[7.306862831115723, 1.015809416770935, "The Development Date of the PRARE Satellite Observation System is 1990."]
[3.638932943344116, 6.255011081695557, "The Nominal Rate of the S-band Downlink Communication System is 40 kbit/s."]
[7.29340124130249, 8.150196075439453, "The Time of the Imaging Process is 25 minutes."]
[6.260639190673828, 2.950110673904419, "The Manager of the WFIRST Mission is NASA's Goddard Space Flight Center."]
[7.31855583190918, 6.979093551635742, "The Similar To of the VIIRS Sensor is MODIS."]
[7.463682651519775, 0.19169139862060547, "The Test Campaign Date of the Smile Satellite is 21 April 2022."]
[7.171334266662598, 0.9072884321212769, "The Launch Date of the SSOT Satellite is Unknown."]
[9.305163383483887, 1.8996227979660034, "The Global Coverage of the JPSS-1/NOAA-20 Satellite is Twice a day."]
[6.2102508544921875, 7.787302017211914, "The Polarization of the ICI-3 Radiometer is V."]
[9.373265266418457, 5.833665370941162, "The Components of the Drag-free control system Control System is Shadow sensor, small cold gas thruster, ADACS."]
[10.559813499450684, 7.548001289367676, "The Structure Material of the CeREs Satellite is Aluminum."]
[10.019887924194336, 1.5736867189407349, "The Measurement Datation of the Satellite Satellite is \u00b1100 \u03bcs with respect to UTC."]
[7.124457836151123, 4.011148452758789, "The Imaging Mission of the SEOSAT\u2013Ingenio Satellite is High-resolution images of Earth's land cover."]
[5.858921051025391, 3.1186580657958984, "The Full Form of the Lemur-2 Satellite is Low Earth Multi-Use Receiver-2."]
[10.999982833862305, 3.4564340114593506, "The Relative Velocity at Closest Approach of the Juno Spacecraft is 41,600 mph (67,000 km/h)."]
[6.14756965637207, 6.005779266357422, "The Modes of Operation of the XSAR SAR Sensor Subsystem is High resolution mode by sliding spotlight, Standard mode by stripmap technique and Wideswath mode by TOPS (Terrain Observation with Progressive Scan) technique."]
[9.089856147766113, 9.796895980834961, "The Cadence of Images of the OSIRIS Narrow Angle and Wide Angle Cameras Imaging System is Increased in each observation."]
[5.027162075042725, 4.029198169708252, "The Experiment of the Airbus Aerospace Company is Testing a completely new onboard software system in the space environment."]
[4.9427595138549805, 4.506035327911377, "The Function of the VT Data Processing is Provide GRB alerts with sub-arcsec accuracy."]
[7.806925296783447, 7.745336055755615, "The Operation of the OCO-2 Spectrometer is Pass through the atmosphere twice."]
[1.3188971281051636, 4.369831562042236, "The Battery Nominal Voltage of the S/C Satellite is 3.7 V."]
[13.073448181152344, 4.0860419273376465, "The Star Detection Rate of the Gaia Satellite is Up to 10,000 stars/s."]
[10.8538818359375, 5.2367262840271, "The Activity Level of the Solar Activity Natural Phenomenon is Exceptionally low and practically constant."]
[10.396249771118164, 4.790196895599365, "The Propulsion System of the EAGLE ESPAStar Satellite is Hydrazine-based monopropellant."]
[7.853966236114502, 9.623369216918945, "The Resolving Power of the Visible Channel Imaging Device is 300."]
[6.45541524887085, 1.0061849355697632, "The Delay Announcement Date of the Quantum Satellite is 6 August 2019."]
[7.214773654937744, 2.6341946125030518, "The URL of the Super Dual Auroral Radar Network Radar Network is http://www.superdarn.ac.uk/archive/Chisham_et_al_2007.pdf."]
[9.225597381591797, 9.07658576965332, "The Resolution of the SXI Spacecraft is 7 arcsec (on axis)."]
[7.693471431732178, 6.055410385131836, "The Value of the Atmospheric Pressure Weather Parameter is 1051.6 hPa."]
[5.176936626434326, 4.94067907333374, "The Type of the Tatara Bridge Bridge is Cable-stayed."]
[7.106159210205078, 1.4229096174240112, "The Presentation Date of the GMES Contributing Missions (GCM) Satellite Constellation is June 6-7, 2012."]
[1.9524476528167725, 5.072417259216309, "The Regulated Voltages of the COVE Board Data Transfer Device is 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."]
[5.700646877288818, 1.3514665365219116, "The Launch Vehicle of the SpaceX CRS-13 Mission is Falcon-9 FT."]
[11.72439193725586, -1.1947643756866455, "The Mass at Launch of the Satellite Satellite is Dry mass = 750 kg."]
[9.198760986328125, 5.234518051147461, "The Actuation Control of the Canopus Pipper Satellite is 3-axis."]
[5.876583099365234, 2.9497125148773193, "The Manufacturer of the SpaceEye-T Satellite is Satrec Initiative."]
[7.67350959777832, 0.27573058009147644, "The Article Date of the CXO Satellite is 29 January 2019."]
[7.143204212188721, 8.300009727478027, "The SST Accuracy of the AATSR Instrument is Better than 0.3 K."]
[10.30853271484375, 4.952838897705078, "The Test Results of the IEPS Ion Electric Propulsion System is All 21 tests were completed faultlessly, except for the break-down protection test."]
[7.676247596740723, 7.213084697723389, "The Project Manager of the TEMPO Instrument is Stephen Hall."]
[7.598050117492676, 0.5988690257072449, "The Launch Date of the EM-1 Mission is 2019."]
[6.064113140106201, 3.1292595863342285, "The Developer of the EMIT Satellite is NASA\u2019s Jet Propulsion Laboratory."]
[10.459585189819336, -0.9823181629180908, "The Mass of the BugSat-1 Microsatellite is 22 kg."]
[7.452151775360107, 3.6121418476104736, "The Agility of the SPOT-6 & SPOT-7 Satellite Constellation is Pitch and roll forward, backwards and sideways by 45\u00b0."]
[6.628695011138916, 10.65103816986084, "The SNR of the Band 5 Spectral Band is 110."]
[11.076386451721191, 4.152115821838379, "The Heat Production of the XO-3b Exoplanet is Unknown."]
[9.407066345214844, 11.498970985412598, "The Effective FOV of the Channel 1 Sensor is 89 km x 198 km."]
[8.686685562133789, 4.928272247314453, "The In-Track Look Capability of the NEMO-AM Satellite is Slightly less than 90\u00ba."]
[4.522568702697754, 4.4396257400512695, "The Nodes of the SpaceWire Link on TacSat-4 Communication Link is 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."]
[7.427465438842773, 7.924136638641357, "The Vertical Cell Size of the Ozone Measurement Instrument Atmospheric Measurement Device is 3 km."]
[6.396491050720215, 0.9897266030311584, "The Technology Presentation Date of the Quantum Satellite is 21 November 2019."]
[13.127108573913574, 4.055655479431152, "The Early Data Release 3 (EDR3) of the Gaia Satellite is Data processed, validation ongoing."]
[4.417496681213379, 6.382185935974121, "The Frequency of the S-band Band is 2.45 GHz."]
[2.049875497817993, 4.194204330444336, "The Solar Panel Power Output of the AprizeSat Satellite is 7.7 W."]
[7.6386494636535645, 4.78346586227417, "The Imaging Wavelength of the PROBA-2 Satellite is Extreme ultraviolet."]
[9.513309478759766, 9.31287670135498, "The Slit Width of the IRIS instrument Instrument is 1/3 arcsec."]
[4.958447456359863, -3.1100943088531494, "The Affiliation of the Toshinori Kuwahara Author is Unknown."]
[7.59483003616333, 6.920494079589844, "The Operating Capability of the Teledyne\u2019s MUSES Platform Platform is Full."]
[5.814144134521484, 5.179699897766113, "The Program Start of the SIR-C/X-SAR Payload is Seasat Synthetic Aperture Radar (SAR) in l978."]
[5.98992395401001, 9.590627670288086, "The Mass of the HIRES Instrument is 1.12 kg."]
[9.033064842224121, 3.0393283367156982, "The Mission of the LunaH-Map Spacecraft is Lunar Polar Hydrogen Mapper."]
[5.199753284454346, 4.875109672546387, "The Architecture of the NRD Electronics System is Multi-board with specific functions."]
[9.612427711486816, 7.806589126586914, "The Composition Energy Range of the ECT Suite Instrument Suite is Up to 50 keV for ions, from a few to 50 MeV/nucleon for ions."]
[5.335792064666748, 6.566317081451416, "The Enclosure Size of the XPAA Phased Array Antenna is 30.5 cm x 33 cm x 7.4 cm."]
[10.251879692077637, 2.9641222953796387, "The Altitude of the Spacecraft Orbit is 645 km."]
[9.802030563354492, 7.015041351318359, "The Emissivity (\u03b5) of the FCA Flow Control Assembly is 0.8."]
[9.698999404907227, 9.507999420166016, "The Operational Status of the SAGE-III Instrument is Operational."]
[5.776947021484375, 6.329086780548096, "The SAR Payload Chirp Bandwidth of the RCM Satellite is 100 MHz."]
[4.240383625030518, 6.667332649230957, "The Channel of the Broadband Applications Experiment Communication System is 450 MHz broadband channel."]
[5.671833515167236, 0.37637749314308167, "The Start Date of the Cooks Peak fire Wildfire is April 17."]
[7.558414936065674, 1.686765193939209, "The Presentation Date of the Magnetospheric Multiscale (MMS) Mission is Feb. 24-27, 2014."]
[8.927035331726074, 5.079120635986328, "The Stabilization of the Resurs-P1 Satellite is 0.005\u00ba/s."]
[5.719643592834473, 2.3097174167633057, "The Beam Tracking of the Eutelsat Quantum Satellite is Enabled."]
[4.751379489898682, 1.953037977218628, "The Satellite Tracking Capacity of the MEOLUT Next Local User Terminal is Up to 30 satellites."]
[7.924043655395508, 5.525241851806641, "The Orbit Determination Accuracy of the AutoNav Autonomous Navigation System is <1000 km in position and <0.4 m/s in the velocity vector."]
[7.500734329223633, 8.888899803161621, "The Ground Projection of the Spectrometer Instrument is 0.4 km x 12 km."]
[9.025025367736816, 8.86583137512207, "The Thickness of the Dobson Unit Unit of Measurement is 0.01 mm."]
[6.795815467834473, 4.249846458435059, "The Data Contribution of the Copernicus Sentinel-1 Satellite is Included in the research."]
[5.840809345245361, 6.6825270652771, "The Length of the LMAG (Lunar Magnetometer) mast Instrument is 12 m."]
[4.1111979484558105, 4.86870002746582, "The Conference Presentation Date of the On-Board Data Handling System Data Handling System is Nov. 22-26, 2004."]
[9.097537994384766, 5.329761505126953, "The Attitude Control of the Payload Satellite Payload is Slew Acceleration."]
[7.998824596405029, 9.095282554626465, "The Speed of the Spectrometer Channel Optical System is Relatively slow (f/14)."]
[5.668920993804932, 9.105743408203125, "The Power Consumption of the CMS Instrument is 26 W."]
[10.831168174743652, 4.1817145347595215, "The Mission Objective of the CHEOPS Satellite is Study the structure of exoplanets smaller than Saturn and measure the bulk density of super-Earths and Neptunes."]
[9.575030326843262, 9.018952369689941, "The Optical Bench Length of the Telescope System X-ray Telescope is 10 m."]
[7.645987033843994, 8.883467674255371, "The Wavelength of the Responsivity Measurement Instrument is 1850 nm."]
[4.684580326080322, 6.1473517417907715, "The Beacon Frequency of the CUTE-1.7+APD Satellite is UHF (437.385 MHz)."]
[6.913209915161133, 4.813612937927246, "The Mission Type of the CO2M Satellite is Monitoring and Tracking Carbon Dioxide Emissions."]
[2.2045726776123047, 4.436398506164551, "The Average Payload Power of the QuikTOMS spacecraft Satellite is 107 W."]
[5.619231224060059, 9.1406888961792, "The Power Consumption of the VIRR Instrument is 7.3 W."]
[6.280821800231934, 1.88759446144104, "The Status of the Microsat-R Satellite is Destroyed."]
[4.75624942779541, 2.0028607845306396, "The Number of Referred Papers Produced of the HaloSat Satellite is 7."]
[8.001798629760742, 7.276952266693115, "The Calibration Types of the ICU Internal Calibration Unit is Absolute and relative radiometric calibrations and spectral calibrations."]
[5.614074230194092, 4.964755058288574, "The Interface of the PAZ SAR Processor Ground Segment Processor is HMA (Heterogeneous Mission Access)."]
[6.485361576080322, 2.8995726108551025, "The Agency of the FalconSat-3 Satellite is USAF."]
[5.3143157958984375, 10.386942863464355, "The Monitoring of the ISS LIS Lightning Imaging Sensor is Occurrence and changes in extreme storms."]
[8.713013648986816, 7.913969993591309, "The Range of Radiation Temperature Measured in Bands 4-6 of the Scanning geometry Instrument is 213-313 K."]
[7.04714298248291, 2.5427138805389404, "The URL of the Satellite Satellite is http://badc.nerc.ac.uk/data/gedex/detail/aem2sag1.det."]
[3.5802783966064453, 4.113323211669922, "The Layout of the DHS Data Handling System is Not Applicable."]
[5.975554943084717, 9.600837707519531, "The Mass of the LIMS Instrument is 68.4 kg."]
[10.083005905151367, 1.5277647972106934, "The Target of Opportunity Duration of the INTEGRAL Satellite is 100,000 seconds."]
[8.853967666625977, 7.034661293029785, "The Aperture Size of the SWAP Instrument is Largest ever used to measure the solar wind."]
[7.936141014099121, 6.765088081359863, "The Frequency of the Monitoring of HIS Calibration Process is Daily."]
[7.14474630355835, 0.28777801990509033, "The Launch Date of the Beijing-3A Satellite is 11 June 2021."]
[11.565054893493652, -1.3180031776428223, "The Mass of the Sentinel-1C Satellite is 2.3 tons."]
[7.77523946762085, 7.392209053039551, "The Vibration Test Frequencies of the FPM Instrument is 5 Hertz and 2000 Hertz."]
[6.515512466430664, 3.5830507278442383, "The Mission Type of the FedSat Satellite is EO."]
[6.34064245223999, 2.9608371257781982, "The Mission Status of the Galileo Satellite Navigation System is Operational (nominal)."]
[5.814042568206787, 6.421193599700928, "The Wavelength of the SAR Synthetic Aperture Radar is 23.5 cm."]
[10.228292465209961, 3.108285665512085, "The Altitude Increase of the SARAL/AltiKa Satellite is 1 km."]
[4.638406753540039, 3.9256956577301025, "The Avionics Architecture of the TechEdSat Satellite is SPA (Space Plug-and-Play Avionics)."]
[7.4505534172058105, 5.482839584350586, "The Bias Requirements of the Aeolus Satellite is Can be expected to be met after further optimization of the instrument calibration and data processing."]
[6.606874942779541, 7.689927577972412, "The Pump Module of the GEDI Laser Laser is Below the layout."]
[9.34212589263916, 5.370328426361084, "The | of the SI Reaction Wheel Reaction Wheel is SI reaction wheel."]
[3.2167346477508545, 5.27840518951416, "The Storage Capacity of the PLCDHS Data Handling System is 2 GByte."]
[11.053366661071777, 3.431035041809082, "The Distance from Jupiter's Cloud Tops of the Juno Spacecraft is 2,100 miles (3,400 km)."]
[4.676085948944092, 5.637019157409668, "The Function of the SCP Satellite Communications Payload is Provide a UHF link for the ODTML services and to function as an internal S&F subsystem."]
[8.476173400878906, 7.1381683349609375, "The Electric Field Measurement Frequency Range of the IOF Plasma Wave Instrumentation is 40 Hz and 178 kHz."]
[9.44461727142334, 0.6845889687538147, "The Design Life of the SPOT-1 Satellite is Three years."]
[5.748969078063965, 2.0834157466888428, "The Telemetry Submission Method of the GeneSat-1 Satellite is Web site."]
[5.059484481811523, 2.9889585971832275, "The Purpose 2 of the PW-Sat CubeSat is Demonstration of a satellite deorbit structure."]
[6.055286884307861, 2.88362717628479, "The Deployment Framework of the Galileo Satellite System is FOC (Full Operational Capability)."]
[7.614366054534912, 4.924282550811768, "The Sun sensors of the BEESAT-3 Satellite is Yes."]
[11.333218574523926, 6.974563121795654, "The Number of Telescopes of the NICER XTI X-ray Timing Instrument is 56."]
[9.353591918945312, 9.978751182556152, "The Objective of the APD Avalanche Photodiode is Observe the low energy charged particle density distribution in LEO (Low Earth Orbit)."]
[7.787442684173584, 4.916123867034912, "The Measurement of the Global Positioning System Satellite System is Geopotential Heights."]
[8.75230884552002, 8.681547164916992, "The Stereo Angles of the Instrument Satellite Instrument is \u00b115\u00ba (fore and aft)."]
[9.297675132751465, 1.6317301988601685, "The Frequency of Issuing Requests for Information of the NASA Organization is About once a year to once every 18 months."]
[9.282095909118652, 4.818317413330078, "The Separation Angle of the STEREO spacecraft Satellite is 90\u00ba."]
[11.378438949584961, 6.66453742980957, "The MMAs Status of the IXPE observatory X-ray Observatory is Three of four MMAs is built."]
[8.114805221557617, 0.32374346256256104, "The Launch Date of the ISS-RapidScat Instrument is 20 Sep 2014."]
[9.697879791259766, 4.95014762878418, "The Rotation Angle of the Y-axis Bang-Bang Maneuver Satellite Maneuver is 130\u00ba."]
[6.303415775299072, 3.2821359634399414, "The Launch Site of the SEOSAT-Ingenio Satellite is Europe's Spaceport in Kourou, French Guiana."]
[9.151083946228027, 1.8524749279022217, "The Delivery of Operational Requests of the TDP Operations Satellite Operations is Weekly."]
[5.077237129211426, 1.9587041139602661, "The Payloads of the Kick Stage Rocket Stage is 34 smallsats."]
[4.190906047821045, 4.695640563964844, "The Interface of the Modem Processor Signal-Processing Chain is SPI (Serial Peripheral Interface) running at 1 MHz line rate."]
[10.19885540008545, 6.8235931396484375, "The Battery Thermal Regulating System of the Neutron-1 Spacecraft is Active internal system with a sensor, heater, and controller."]
[10.593385696411133, 7.493170261383057, "The Material of the Torus/Strut Structures Satellite Component is 12 mil thick neoprene coated Kevlar."]
[8.136646270751953, 4.049702167510986, "The Agility Range of the Pleiades-1A Satellite is Up to 1500 km on either side of their path."]
[8.50575065612793, 7.066103458404541, "The Dynamic Range of the Magnetometer Instrument is 160 dB (ELF/VLF range), 130 dB (LF/MF range)."]
[6.600110054016113, 8.69347095489502, "The Ground Resolution of the MWNIR Imaging System is 100 km - 18 km."]
[6.81311559677124, 3.644688367843628, "The Mission Type of the Meteor-1/Meteor-2/Meteor-Priroda Series Satellite Mission is EO."]
[3.595857620239258, 6.064794540405273, "The Maximum Operating Speed of the DCU-S(TC) module Communication Module is 128 kbit/s."]
[4.920793056488037, 3.175145387649536, "The Bus Connection of the CubeSat Satellite is I2C or CAN."]
[4.204535484313965, 6.509955406188965, "The Frequency of the S-band Transmitter Transmitter is 2234.4 MHz."]
[5.246414661407471, 1.9601706266403198, "The Orbit Count of the Genesis-2 Satellite is 10,000."]
[7.743314266204834, 4.886418342590332, "The Reaction Wheel Momentum Offloading of the PROBA-V Satellite is Autonomously performed when the instrument is not imaging."]
[13.806538581848145, 0.7668923139572144, "The Orbital Slot of the GSAT-0208 Satellite is C07."]
[7.266317844390869, 0.6851615309715271, "The Clearing Date of the Aalto-1 Satellite is June 21, 2018."]
[8.01220417022705, 8.39139175415039, "The Spectrometer Type of the ACE-FTS Instrument is Adapted version of the classical Michelson interferometer."]
[2.019853115081787, 7.8458380699157715, "The Solar Wind Speed and Beta of the ACE Satellite is ~40% lower on average from 2009 through the day 79 of 2013."]
[5.333804130554199, 2.468946933746338, "The Project Manager of the HORYU-4 Satellite is Professional staff."]
[10.89515209197998, 7.223657608032227, "The Sensitivity of the XSM X-Ray Detector is ~ 7000 cps at flux level of 10-4 W m-2 in the range 1-8 \u00c5."]
[4.40969181060791, 4.448859214782715, "The Function of the MIU Interface is Receives payload commands and spacecraft telemetry from the FC and forwards those to the CEU."]
[4.080386161804199, 6.456949234008789, "The Modulation of the RF Communications Communication System is Bell 202."]
[7.557770252227783, 4.031712532043457, "The Orbit Determination of the CryoSat-2 Satellite is Real-time orbit determination for spacecraft attitude and orbit control (on-board)."]
[8.555461883544922, 1.3259100914001465, "The Data Collection Duration of the GOCI Geostationary Ocean Color Imager is Eight hours."]
[7.350611209869385, 1.7067557573318481, "The Online Availability Date of the TRUTHS Satellite is 13 February 2004."]
[10.367974281311035, 4.964627742767334, "The Manufacturer of the PPS-1350-G Hall-effect thruster is SNECMA of France."]
[4.041162490844727, 10.340105056762695, "The NE\u0394T (K) of the ICI-10 Radiometer is 1.9."]
[6.293123245239258, 1.1029279232025146, "The Launch Date of the COSMO-SkyMed-1 Satellite is June 8, 2007."]
[10.2791109085083, 8.73695182800293, "The Objectives of the EUI Extreme UV Imager is 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 inacce."]
[8.882173538208008, 7.502150535583496, "The Potential Generation of the SenPot Amplifier is Maintains the IVM reference ground at the floating potential with respect to the plasma."]
[5.831997871398926, 2.0651631355285645, "The Components of the NLS-2 Launch System is QuakeSat."]
[7.948275566101074, 10.714622497558594, "The Processed Resolution of the Detector Sensor is 10 bits or 8 bits."]
[5.065506935119629, 4.467065334320068, "The CGA Implementation of the MC3 Ground Station is Allowed for the ground stations to be unmanned 24/7."]
[11.494730949401855, -1.3217507600784302, "The Mass of the LituanicaSAT-2 Satellite is 3 kg."]
[6.053389072418213, 9.242362022399902, "The Mass of the AMU Altimeter Microwave Unit is 8 kg."]
[8.466898918151855, 10.379720687866211, "The CCD Detector of the NMS Neutral Mass Spectrometer is 256 x 256 elements."]
[9.818796157836914, 7.084677219390869, "The Loading Temperature Change of the Helium Gas is To allow warmer temperature helium to be loaded."]
[9.57316780090332, 6.6866912841796875, "The Components of the Maeva Hinges Deployment Mechanism is Carpentier elastic blades, SMA strings, Cerafil heater wires."]
[10.449956893920898, -1.142266869544983, "The Mass of the Pegasus Nanosatellite is Unknown."]
[3.610581636428833, 6.173376560211182, "The Data Rate of the Unit Communication System is 1000 bit/s."]
[7.108835220336914, 4.929619312286377, "The Purpose of the Carbon Mapper Satellite Constellation is Pinpoint, quantify and track point-source methane and CO2 emissions."]
[9.4544677734375, 0.7289962768554688, "The Operational Duration of the Odin Satellite is 21 years."]
[11.08826732635498, 5.114336013793945, "The Location of the LISA Pathfinder Spacecraft is L1 (Lagrangian Point 1)."]
[8.299424171447754, 8.302799224853516, "The Type of the MIRI Instrument is Mid-Infrared Camera-Spectrograph."]
[7.447769641876221, 1.2925007343292236, "The Observation Date of the OMI Satellite is 15 Dec. 2016."]
[8.050339698791504, 7.031195163726807, "The Calibration Task of the Machine Learning Algorithm Calibration Tool is Recognize solar structures and determine calibration needed."]
[9.49548053741455, -0.5397860407829285, "The Configuration of the SONATE nanosatellite Satellite is ASAP-L (light)."]
[7.38358736038208, 0.7835445404052734, "The Integration Test Date of the PROBA-V Satellite is April 15, 2013."]
[6.033746719360352, 3.2909600734710693, "The Prime Contractor for A satellites of the MetOp-SG Satellite Program is Airbus Defence and Space of France."]
[11.592148780822754, 2.6461715698242188, "The Purpose of the OLA Instrument is 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."]
[9.066515922546387, 6.495205879211426, "The Saturation of the Honeywell QA2000-030 accelerometers Accelerometer is Around 27.5 rpm."]
[3.7681188583374023, 4.701136112213135, "The Processor of the SWEM Satellite is Coldfire."]
[7.917148113250732, 1.1630206108093262, "The Data Stream of the Copernicus Sentinel-6 Satellite is Slated for distribution later this year or early next year."]
[3.5247342586517334, 4.758754730224609, "The Microcontroller Clock Speed of the CC430 SoC System on Chip is 8 MHz."]
[9.739864349365234, 1.4060434103012085, "The Observation Duration of the Roman Satellite is Several days."]
[4.800319671630859, 5.513376712799072, "The RF Communications of the exactView-1 Satellite is S-band TM/TC (Telemetry/Telecommand) for satellite operations."]
[7.192902088165283, 5.767270565032959, "The Purpose of the OCI Ocean Color Instrument is Examine and monitor phytoplankton communities in the ocean."]
[8.851491928100586, 4.899188041687012, "The Sensor Suite of the NEMO-AM Satellite is SFL sun sensors, SFL magnetometer, SI star tracker."]
[4.232861518859863, 6.536200046539307, "The Frequency of the RF communications Communication System is 437.27 MHz."]
[5.9929938316345215, 9.596728324890137, "The Mass of the MSI-0 and MSI-1 MSI Instruments is 3 kg."]
[10.457080841064453, -1.0145556926727295, "The Mass of the Microsatellite Satellite is 47 kg."]
[9.107767105102539, 10.565882682800293, "The Resolution of the PamCam Panoramic Camera is 1280 x 1024 pixels."]
[6.265090465545654, 2.951002359390259, "The Location of the Lockheed Martin Sensing and Exploration Systems Systems is USA."]
[11.575796127319336, 4.541163444519043, "The Wind Speed of the Massive Stars Stars is Millions of km/hour."]
[11.714254379272461, 4.555073261260986, "The Distance from Solar System of the Pleiades Open Cluster is About 400 light years."]
[8.94698429107666, 2.130340814590454, "The Data Transmission of the New Horizons Spacecraft is Ongoing."]
[11.706863403320312, -0.7023594975471497, "The Payload Data Storage of the MERLIN Satellite is Increased."]
[7.937418460845947, 6.950581073760986, "The Data Acquisition Start Timing of the ARC Calibration System is Adequate."]
[5.050568103790283, 4.613441467285156, "The Instrument Configuration of the Ground Segment Communication System is Based on predicted crossing times of magnetospheric regions of interest in combination with various on-board trigger algorithms."]
[4.72261381149292, 3.8707540035247803, "The Components of the AAE Experiment is Appliqu\u00e9 sensor network, adaptive wiring manifold, high-performance computing on-orbit, and software definable radio."]
[10.169265747070312, 5.180304527282715, "The Configuration of the FENIX micropropulsion device Micropropulsion Device is Can be at each corner of the CubeSat or doubled up on either side."]
[8.285505294799805, 8.551519393920898, "The Detector of the Spectral Band B Spectrometer is Si-PIN."]
[8.601112365722656, 4.3649773597717285, "The Solar Array Span of the QuickBird-2 Satellite is 5.2 m."]
[9.03032112121582, 3.655716896057129, "The Image Capture of the NASA's Solar Dynamics Observatory Satellite is Full-disk Sun and the left side of the inset image."]
[7.639184474945068, 0.8886427879333496, "The Mission Overview and Status Date of the WindSat Satellite is June 5, 2006."]
[7.398806095123291, 10.110857963562012, "The Instrument Size of the HySI Hyperspectral Imager is 275 mm x 275 mm x 205 mm."]
[7.2716474533081055, 9.255537033081055, "The Width of the Penumbra Shadow is 100+ km."]
[6.842740058898926, 1.2360620498657227, "The Conference Date of the GIOVE-B Satellite is May 3-6, 2009."]
[11.235602378845215, 3.5222249031066895, "The Interaction of the Solar Orbiter Spacecraft is Crossed one of the comet\u2019s two tails."]
[8.568279266357422, 6.9452128410339355, "The Absolute Measurement Error of the Vector Magnetometer Instrument is Less than 1 nT."]
[10.165574073791504, 5.079379081726074, "The Thrust Measurement Method of the AQT-D Propulsion System is Direct."]
[11.631969451904297, 6.165803909301758, "The Article Date of the XMM-Newton Satellite is July 12, 2016."]
[8.530379295349121, 10.994548797607422, "The FOV per channel of the Eastman Kodak KLI14403 linear CCD sensor Sensor is 26.6\u00ba."]
[11.609573364257812, -1.1478521823883057, "The Mass of the GCOM-W1 Satellite is ~1990 kg."]
[5.8920698165893555, 5.4501471519470215, "The Purpose of the IGOR+ GPS Receiver is Allows the tracking of occulting signals."]
[10.139557838439941, 6.771682262420654, "The Thermal Control of the Satellite Spacecraft is Milli-Kelvin (mK) passive thermal control of the payload."]
[10.593409538269043, 2.7699038982391357, "The Extended Range Testing Distance of the GomX-4A and GomX-4B Satellites is Up to 4500 km."]
[8.142693519592285, 4.916522979736328, "The Angular Resolution of the HaloSat Satellite is 15\u00b0 or less."]
[5.489569664001465, 4.275882244110107, "The Operator of the Himawari-8/9 Ground Segment Ground Segment is Himawari Operation Enterprise Corporation (HOPE)."]
[10.354193687438965, 3.4762139320373535, "The Pericenter Distance of the SMART-1 Satellite is 2189.702 km."]
[6.885239124298096, 0.4204394221305847, "The Launch Date of the IRS-1B Satellite is August 29, 1991."]
[4.003268718719482, 6.570887088775635, "The Telemetry of the CEASE-1 Instrument is 10 byte/min."]
[7.294619560241699, 0.3769833743572235, "The Expected Return near to Earth of the Satellite Spacecraft is 2029."]
[6.6525559425354, 0.6309863924980164, "The Launch Date of the COMPASS-1 Satellite is Dec. 10, 2001."]
[5.571471214294434, 6.149935245513916, "The Antenna Diameter of the Satellite Communication Satellite is 4.2 meters."]
[8.441418647766113, 6.951928615570068, "The Location of the Receiver Sensor Sensor is Back side of the terminal."]
[7.478697299957275, 9.554621696472168, "The Polarization Angle of the Band 2 Spectral Band is 0/60/120 \u00ba."]
[3.582163095474243, 6.140728950500488, "The Baud Rate of the RS-422 UARTs Communication Interface is 115 kbit/s."]
[5.225929260253906, 3.10577392578125, "The Auxiliary Payload of the NorSat-3 Satellite is Navigation Radar Detector (NRD)."]
[11.01973819732666, 4.171510219573975, "The Mission Type of the Hubble Satellite is Discovery of Diverse Exoplanets."]
[6.770078182220459, 0.06940127164125443, "The Mission Status of the Tatiana-2 Satellite is Finished."]
[8.328845977783203, 5.2686638832092285, "The Accuracy of the Gravity Satellite is mgal."]
[11.101995468139648, 2.2482705116271973, "The Maximum Drill Depth of the SD2 Instrument is About 0.2 m."]
[6.823939800262451, 9.054768562316895, "The Size of the SHS Instrument Spectroscopic Instrument is Small."]
[8.10312271118164, 4.665656566619873, "The Spatial Resolution of the Geodesy Orbits Satellite is 100-1000 km."]
[9.233132362365723, 5.446784019470215, "The Attitude Accuracy of the Attitude and Orbit Control Subsystem Subsystem is 0.4\u00ba in roll and pitch."]
[7.024442195892334, 7.594845294952393, "The Imaging Capabilities of the HARP-2 Satellite is Wide swath, polarization, and multi-angular sampling."]
[11.329910278320312, 1.3782788515090942, "The Malfunction Date of the Yutu Lunar Rover is March 3, 2014."]
[9.550127983093262, 0.6684547662734985, "The Mission Goal of the MinXSS-2 Satellite is 5 years."]
[8.25761604309082, 0.17509454488754272, "The Construction Start Year of the China\u2019s space station Space Station is 1992."]
[5.384568214416504, 1.8733758926391602, "The User of the P-POD Deployer is Unknown."]
[3.657416343688965, 4.559110641479492, "The CPU Operating Frequency of the OBC On-Board Computer is 50 MHz."]
[10.29410457611084, 6.814047336578369, "The Mass of the TCS Thermal Control Subsystem is 0.15 kg."]
[9.48827838897705, -2.5070533752441406, "The Energy Range for H of the LEICA Particle Detector is 0.76 - 6.1 - - 18 - 250 MeV."]
[7.311241149902344, 7.42136812210083, "The Focal Point of the SWAVES Instrument is University of Minnesota."]
[6.764893531799316, 4.903303146362305, "The Polarization Measurement of the Sentinel-5 Satellite is First three elements of the M\u00fcller matrix."]
[11.325356483459473, 3.8912193775177, "The Diameter of the Mars' Core Seismic Analysis is About 3,660 kilometers."]
[10.75379467010498, 3.3969900608062744, "The Closest Approach Distance of the Solar Orbiter Satellite is 460 km."]
[1.7581698894500732, 5.082058906555176, "The Power Input Voltage Range of the COVE Board Data Transfer Device is 6.0-8.4 V."]
[6.868828296661377, 2.9752378463745117, "The Status of the YOUTHSAT Satellite is Functioning Satisfactorily."]
[4.90830659866333, 1.840803623199463, "The Number of Spacecraft of the DSP Satellite Project is 2."]
[6.850949764251709, 6.121632099151611, "The Orbit Inclination of the ISS-RapidScat Scatterometer is Lower than polar sun-synchronous satellites."]
[8.796574592590332, 4.31091833114624, "The Configuration of the SARAL spacecraft Satellite is Overview shown in Figure 2."]
[11.595074653625488, 2.6630778312683105, "The Albedo of the Lutetia Asteroid is Unusually low."]
[11.75481128692627, 1.678118348121643, "The Collision with Cliff of the Philae Lander is 45 minutes after landing."]
[12.160143852233887, 2.1410250663757324, "The Sample Delivery Date to Earth of the OSIRIS-REx Spacecraft is September 2023."]
[10.779580116271973, 3.4347527027130127, "The Closest Approach to the Sun of the Rosetta Satellite is Perihelion."]
[6.804300308227539, 8.331448554992676, "The LOS Wind Error Requirement of the Rayleigh Channel Instrument is Below a certain value."]
[3.94919753074646, 5.706851482391357, "The Data Rate of the Spacecraft Satellite is 100 Mbit/s."]
[3.2832043170928955, 5.606815338134766, "The Header Size of the Raw Science Data Packet Data Packet is 23 bytes."]
[3.4522533416748047, 4.7078328132629395, "The Memory of the AIM Reconfigurable Computing Hardware Device is 4 M x 16 Flash for storage of multiple Xilinx configurations."]
[4.775068759918213, 1.973128318786621, "The Current Quantity of the Artificial Objects Satellite is 22,000."]
[10.067623138427734, 4.338746547698975, "The Manufacturer of the Clementine Spacecraft is US Naval Research Laboratory (NRL)."]
[7.953163146972656, 2.025425434112549, "The Mission Overview of the ExoMars Trace Gas Orbiter Orbiter is URL: http://exploration.esa.int/mars/46124-mission-overview/."]
[11.610389709472656, -1.1842012405395508, "The Mass of the Tether Satellite Component is 5.5 kg."]
[6.880612373352051, 3.201834201812744, "The Mission Status of the GeoEye-1 Satellite is Operational (extended)."]
[7.387389659881592, 9.067633628845215, "The Swath Width at Nadir of the Telescope Optical Instrument is 30 km."]
[7.200581073760986, 6.91066837310791, "The Observation Date of the MAXI Instrument is July 13, 2011."]
[1.6315284967422485, 4.689844131469727, "The 28 \u00b16 VDC of the Solar Array Power Generation is A regulated 28 \u00b16 VDC power bus distributes energy to all S/C subsystems and instruments."]
[11.442622184753418, 2.2254741191864014, "The Conjunction Transition Orbit of the Hayabusa-2 Spacecraft is Placed slightly further away from the asteroid."]
[8.28197193145752, 3.1700072288513184, "The Data Acquisition Period of the TanDEM-X Satellite is 2011 and 2015."]
[7.648965358734131, 9.16334342956543, "The Spatial Resolution of the ETM+ Enhanced Thermal Mapper Plus is 15 m (PAN band), 30 m (VNIR/SWIR bands), 60 m (TIR band)."]
[7.414761066436768, 1.8123022317886353, "The NASA Announcement of the Gravity Probe B Satellite is May 4, 2011."]
[6.491027355194092, 1.0708091259002686, "The Operation Start Date of the OptiSAR\u2122 Constellation Satellite Constellation is 2022."]
[4.875644207000732, 4.4698872566223145, "The Location of the DCS Data Collection System is LEO."]
[11.183138847351074, 2.8833866119384766, "The Hazard of the Site Nightingale Crater is Building-size boulder on the eastern rim."]
[9.226370811462402, 9.83119010925293, "The Number of Normal Cameras of the PLATO Telescope is 24."]
[8.334887504577637, 6.43522310256958, "The Conference Presentation of the Sensor Web Sensing System is First IEEE International Conference on Sensors 2002."]
[6.164394378662109, 2.379028558731079, "The Manufacturer of the G\u00f6kt\u00fcrk-1 Satellite is Telescpazio."]
[11.191631317138672, 9.349891662597656, "The URL of the Nimbus Earth Radiation Budget (ERB) Experiment Satellite Experiment is http://journals.ametsoc.org/doi/pdf/10.1175/1520-0477%281993%29074%3C0815%3ATNERBE%3E2.0.CO%3B2."]
[1.8038917779922485, 4.036523342132568, "The Goal of the Solar Cells Energy Device is Enable high-efficiency space solar cells and panels to be produced in large quantity and at lower cost."]
[8.529393196105957, 1.9655961990356445, "The Online Publication Date of the Herschel and Planck Telescopes is 12 September 2019."]
[7.6351776123046875, 3.926487684249878, "The Mission Goal of the Tandem-L Satellite is Set new standards in Earth observation."]
[1.6008902788162231, 4.892392158508301, "The Unregulated Bus Voltage of the EPS Electric Power Subsystem is 28V \u00b16 V DC."]
[11.644508361816406, -1.2238246202468872, "The Mass of the NEOSSat Satellite is ~74 kg."]
[8.205265998840332, 8.535442352294922, "The Team Members of the CIRiS Infrared Radiometer is A. Amparan, A. Ghandour, T. Kampe, P. Kerrigan, J. Necas, D. Piqueira, G. Reavis, R. Rohrschneider, M. Veto, R. Warden."]
[5.9051947593688965, 10.848837852478027, "The No of Passbands of the Channel 3 Sensor is 1."]
[10.972039222717285, 3.393064260482788, "The Orbit Altitude of the Rosetta Spacecraft is Less than 10 km from the comet's surface."]
[10.34725570678711, 7.153200149536133, "The Material of the Heatshield Thermal Protection is Al honeycomb structure."]
[3.7230076789855957, 6.234817028045654, "The Operational Data Rates of the ACTS Mobile Terminal Mobile Terminal is 2.4, 4.8, 9.6, 64, to 128 kbit/s."]
[9.672725677490234, 2.1613199710845947, "The Mean Separation Time from CALIPSO of the CloudSat Satellite is 15 seconds."]
[10.458319664001465, -1.1480685472488403, "The Mass of the AprizeSat-9 Nanosatellite is 12 kg."]
[11.329976081848145, 7.015570640563965, "The Timing Precision of the NICER X-ray timing instrument is < 100 ns."]
[6.913391590118408, 5.047635078430176, "The Radar Altimeter of the HY-2A Satellite Satellite is Unknown."]
[8.449846267700195, 2.945850372314453, "The Auroral Potentials of the Jupiter Planet is Up to 400,000 electron volts."]
[7.618968486785889, 4.871457576751709, "The Fault-tolerant satellite design of the BEESAT-2 Satellite is Yes."]
[6.521259307861328, 2.0587260723114014, "The URL of the PSLV Launch Vehicle is https://www.isro.gov.in/2018press15.html."]
[10.309593200683594, 2.999613046646118, "The Initial Orbit Altitude of the Bion-M1 Spacecraft is ~300 km."]
[7.6707634925842285, 8.880704879760742, "The Wavelength of the Responsivity Measurement Instrument is 1990 nm."]
[8.141545295715332, 9.045571327209473, "The Resolution of the OLS Imaging Sensor is 2.8 km."]
[7.541697978973389, 8.453617095947266, "The SNR of the Instrument Spectrometer is > 100."]
[8.537040710449219, 10.467301368713379, "The Pixel Size of the Detector Array CCD is 13.5 \u00b5m."]
[12.050183296203613, 3.223426580429077, "The Orbital Inclination of the LDEF Satellite is 28.5\u00ba."]
[6.6572651863098145, 3.62380313873291, "The Mission Type of the Sich-2 Satellite is EO."]
[8.759016990661621, 10.662435531616211, "The Imaging Rate of the Instrument CCD Imaging Camera is About 60 0.1 second exposures per minute with the NIR camera, and 1/2 second exposure per minute with the VIS camera."]
[6.5526041984558105, 4.866971492767334, "The Imaging Frequency Band of the SARLupe Satellite is X."]
[8.284351348876953, 8.545431137084961, "The Location of the VIS Unit is Service Module."]
[9.155232429504395, 4.110140323638916, "The Size of the QuakeSat Satellite is 10 cm x 10 cm x 30 cm."]
[8.188923835754395, 2.476130247116089, "The Nationality of the Max Valier Person is Italian."]
[9.513042449951172, 5.57687520980835, "The Software Architecture of the AOCS Attitude and Orbit Control System is Object-oriented and modular with a static architecture."]
[7.230337619781494, 1.1166727542877197, "The Development Date of the Microsized Microwave Atmospheric Satellite (MicroMAS) Satellite is April 28, 2013."]
[4.049489974975586, 6.598924160003662, "The Minimum Trigger Level of the Receiver Communication Device is -96 dBm."]
[5.92875862121582, 6.80112886428833, "The Operational Modes of the SIR-C Phased Array is ScanSAR and Spotlight."]
[4.229007720947266, 2.8537635803222656, "The Latency of the Starlink Satellite Internet Service is 20 milliseconds."]
[5.882171630859375, 5.744330406188965, "The Deployment of the AstroMesh Reflector Reflector is Deployed."]
[6.623373031616211, 3.873178005218506, "The Purpose of the SSIKLOPS Launcher is Provide means to release small satellites from the ISS."]
[3.2276175022125244, 4.470153331756592, "The Power Consumption of the Safe-mode System System is Very low."]
[9.212735176086426, 5.252048969268799, "The Axes of the Attitude Determination and Control System Satellite is Full 3-axis."]
[7.135836124420166, 1.033223271369934, "The Decommissioning Date of the Midcourse Space Experiment Satellite is 2010."]
[12.139050483703613, 3.2556018829345703, "The Inclination of the Shakuntala Satellite is 97.4\u00b0."]
[4.102570056915283, 7.293550491333008, "The Mass of the HiSPiCO S-band Transmitter/Transceiver is 75 g."]
[7.56564474105835, 6.197578430175781, "The Additional Test of the Biomass Satellite is Thermal elastic distortion test."]
[7.64375638961792, 0.7864986062049866, "The Launch Date of the MESA Technology is Aug. 2013."]
[6.111422061920166, 5.967687606811523, "The Ground Resolution (Mosaic mode) of the XSAR SAR is 1.8 m."]
[8.750822067260742, 9.006592750549316, "The Energy Optimization of the HEG Grating is High."]
[8.587159156799316, 5.533817768096924, "The Accuracy for 2000 kg payload of the IPS Pointing System is 0.5 arcseconds lateral and 41 arcseconds roll in sun mode."]
[9.585086822509766, 8.999292373657227, "The Length of the TT Telescope Tube is 6.80 m."]
[5.9873857498168945, 9.59852123260498, "The Mass of the Instrument Device is < 7 kg."]
[6.753452301025391, 2.1503491401672363, "The Impact of the Asia\u2019s Summer Monsoon Weather Phenomenon is Refilling aquifers, generating hydroelectric energy, providing water for crops."]
[7.24224853515625, 0.7223033905029297, "The Delivery Date of the CUTE Satellite is Mid-September 2021."]
[6.27957820892334, 7.905821323394775, "The Polarization of the MWR Radiometer is V and H."]
[8.227326393127441, 9.789444923400879, "The Spectral Region of the QWIP Detector Detector is 11-17 \u03bcm."]
[5.077158451080322, 7.590176582336426, "The Data Rate of the HEED Instrument is 0.19 kbit/s."]
[7.302420616149902, 1.2755392789840698, "The Conference Date of the Sentinel-3 Satellite is 5-9 September 2011."]
[7.830874919891357, 5.073668003082275, "The Laser System Position Accuracy of the LAGEOS Satellite is About 10 cm."]
[9.754249572753906, 7.137736797332764, "The Loading Temperature of the Helium Gas is Cold."]
[6.580748081207275, 3.894136428833008, "The Payload of the SEOSat/Ingenio Satellite is Optical."]
[6.671369552612305, 7.171710014343262, "The Observation Date of the HSRL-2 Lidar is 10 October 2014."]
[7.787670612335205, 8.185561180114746, "The Instrument Architecture of the OMPS Sensor is Staring spectrometer."]
[8.407383918762207, 9.252793312072754, "The Spectral Resolution of the MEGS Spectrograph is 0.1 nm."]
[3.33296275138855, 6.659607887268066, "The P/L Power of the Repeater subsystem Communication System is < 3500 W (EOL)."]
[9.29535961151123, 8.487164497375488, "The Housing Material of the Detector Stack Instrument Component is Tungsten."]
[3.849050760269165, 5.719013214111328, "The Test Transmission Data Rate of the Herschel Spacecraft is 1.5 Mbit/s."]
[9.293061256408691, 4.15527868270874, "The Spacecraft Size of the QSat Satellite is 492 mm x 503 mm x 502 mm."]
[3.963667154312134, 5.5286736488342285, "The Transmission Configuration of the Data Download System Satellite System is All files (already downloaded and not yet downloaded) or only not yet downloaded files."]
[5.731013298034668, 0.9114835858345032, "The International Space Station Arrival Date of the NanoRacks CubeSat Deployer Missions CubeSat Deployer is April 18, 2017."]
[7.5217390060424805, 1.3132107257843018, "The Last Accessed Date of the JAXA Missions Satellite Missions is March 2015."]
[7.9639787673950195, 4.0240159034729, "The Presence of the Carbon Dioxide Ice Patch Surface Feature is Isolated rare case."]
[10.263930320739746, 2.982804775238037, "The Altitude of the SARAL spacecraft Satellite is ~800 km."]
[9.03773307800293, 2.375119686126709, "The Venus Flyby Types of the V7GA Mission is Resonant and non-resonant."]
[5.289906024932861, 3.5133931636810303, "The Internal Harness Connectors of the ASM Satellite Component is Removed."]
[9.948352813720703, 4.824670791625977, "The Orbit Maneuver Support of the INSAT-2A/2B Satellite is Integral apogee boost motor."]
[5.27966833114624, 1.4258952140808105, "The Clocks of the GIOVE-B Satellite is PHM (Passive Hydrogen Maser)."]
[11.814830780029297, -1.0447667837142944, "The Launch Mass of the Bion-M1 Spacecraft is ~6,840 kg."]
[4.678964614868164, 0.15806429088115692, "The Number of Planned Satellites of the OneWeb Satellite Constellation is 1980."]
[7.864762783050537, 4.721480369567871, "The Spatial Resolution of the GHGSat's New Satellites Satellite is < 25 m."]
[3.5597329139709473, 4.681727886199951, "The Processor FLOPS of the MPM Main Processor Module is 10 FLOPS."]
[8.296594619750977, 2.6128358840942383, "The Orbit of the Himawari-9 Satellite is Geostationary."]
[4.3903913497924805, 7.782436847686768, "The Center Frequency of the Channel 7 Sensor is 48 GHz."]
[12.02280044555664, 4.510109901428223, "The Time Since Formation of the Blue Ring Nebula Nebula is Millennia."]
[9.830193519592285, 4.55823278427124, "The Image of the Terminator Tape Deorbit Module Deorbit Device is Prototype version of the Terminator Tape Deorbit Module."]
[5.302237510681152, 1.3651803731918335, "The Reusability of the Terran R Launch Vehicle is Both stages and its payload fairing will be reusable."]
[6.578296661376953, 7.641452789306641, "The Design of the ATLID Power Laser Head Laser Head is Sealed and pressurized."]
[2.21738862991333, 1.734616994857788, "The CCSDS ID of the GSAT-0206 Satellite is 266."]
[6.675971031188965, 0.5444161891937256, "The Launch Confirmation Date of the MeteoSat Third Generation Satellite is 23 March 2021."]
[8.612208366394043, 9.254159927368164, "The Field of View of the Limb Imager Instrument is 75 to 110 km tangent altitudes, 300 km across the track."]
[5.121104717254639, 4.4339919090271, "The Location of the DPS Data Processing System is Balanagar."]
[6.652285099029541, 4.781411170959473, "The Type of the MTG-S Satellite is Sounder."]
[6.417870998382568, 2.0924015045166016, "The Purpose of the Swarm Satellite Constellation is Space science studies."]
[11.451143264770508, 4.175212860107422, "The Dayside Temperature of the 55 Cancri e Exoplanet is 4,400\u00ba Fahrenheit (about 2,400\u00ba Celsius)."]
[9.365535736083984, 5.907215118408203, "The Purpose of the Aerothermodynamics Technology is Validation of design tools and improvement of design performance."]
[4.072451591491699, 5.7301225662231445, "The L-band Receivers Data Rate of the UoSAT-12 Satellite is 1 Mbit/s."]
[10.466644287109375, 7.61683988571167, "The Material of the Ribbon Cable Component is Unknown."]
[6.034905433654785, -0.04981647804379463, "The Launch Date of the Galileo Satellites Satellite is July 25, 2018."]
[4.540106773376465, 3.543900966644287, "The Connection of the SATLAB Configuration is SATSIM is connected with the OBC through the CAN bus."]
[5.76765251159668, 3.18501615524292, "The Manufacturer of the ACLS Air and Oxygen System is Airbus."]
[8.254776954650879, 10.129843711853027, "The Pixel Pitch (Pan) of the Pushbroom imager Detectors is 12 \u00b5m x 12 \u00b5m."]
[7.68314266204834, 8.72623062133789, "The Mapping accuracy of the Spectrometer Spectrometer is < 1.5 km."]
[8.026251792907715, 1.3686904907226562, "The Comet Encounter Date of the ICE (International Cometary Explorer) Spacecraft is September 11, 1985."]
[9.822381973266602, 6.7109856605529785, "The Orbit Latitude Range of the NICER/SEXTANT Instrument is \u00b151.6 \u00ba."]
[7.840600967407227, 6.173705101013184, "The Side Slither Calibration Frequency of the Satellite Imaging Satellite is Quarterly."]
[5.7882184982299805, 6.401773452758789, "The SAR Payload Peak Power Consumption of the RCM Satellite is Approximately 1270 W."]
[11.189356803894043, -1.5217746496200562, "The Mass of the TSAT CubeSat is Unknown."]
[5.304970741271973, 6.777263164520264, "The Satellite Ground Track Range of the TUC Transponder Microwave Transponder is 3-5 km."]
[6.258655071258545, 1.864652156829834, "The Founding Date of the Spacety Company is 2016."]
[8.466604232788086, 2.2942471504211426, "The Lead Author of the Parker Solar Probe Satellite is Justin Kasper."]
[3.879971742630005, 5.6448564529418945, "The Data Downlink Speed of the Payload Satellite Payload is 800 Mbit/s."]
[10.565865516662598, 7.531555652618408, "The Material of the Satellite Structure Satellite Component is Aluminum 6061."]
[1.1085984706878662, 4.258429050445557, "The Battery type of the EPS Electric Power Subsystem is Li-ion."]
[7.648056983947754, 4.753076076507568, "The Viewing Angles of the PROBA-1 Satellite is Five different."]
[10.844712257385254, 2.026289224624634, "The Orbital Altitude of the Swarm-C (Charlie) Satellite is \u2264 530 km."]
[4.761026382446289, 6.125319957733154, "The Data Communications Transceiver Frequency of the OSSI-1 CubeSat is 437.525 MHz."]
[6.4630208015441895, 6.156088829040527, "The Data Product Format of the OSCAT-2 Instrument is HDF 5 (Hierarchical Data Format 5)."]
[8.017003059387207, 1.0938689708709717, "The Image Date of the AWiFS Imaging System is May 4, 2011."]
[9.876736640930176, 3.976489782333374, "The Conference Date of the Deorbitsail Deployable Sail is April 8-11, 2013."]
[9.20411205291748, 8.836990356445312, "The IR Energy Reflection of the Optics Assembly Dichroic Mirror is 85%."]
[12.114192008972168, 2.2241921424865723, "The Camera Suite of the OSIRIS-REx Spacecraft is OCAMS (PolyCam, MapCam, and SamCam)."]
[7.33993673324585, 4.388566493988037, "The Camera Type of the SLIM6 Satellite is Multispectral scanning camera."]
[3.1885390281677246, 5.131409645080566, "The Memory Type of the DSU Data Storage Unit is Non-volatile memory."]
[3.437856912612915, 4.597284317016602, "The Qualification Program of the Virtex-4 FPGA Data Processing Unit is Undergoing vibration and thermal cycling tests."]
[3.521677017211914, 4.073376655578613, "The PROM of the STRV-1d DHS Data Handling System is 32 k PROM."]
[6.067251205444336, 11.222005844116211, "The Approx. peak sensitivity altitude of the Channel 2 Sensor is Unknown."]
[5.518155574798584, 2.4462711811065674, "The Constellation of the UrtheCast Satellite System is Optical and SAR satellites."]
[8.80473518371582, 7.399820804595947, "The Operation of the MERIS Sensor is Only out of eclipse."]
[6.809317111968994, 0.961225688457489, "The End Year of the MDPP-2 Program is 2003."]
[10.024113655090332, 2.810462713241577, "The Orbit Altitude of the GPM Core spacecraft Satellite is 400 km."]
[11.336337089538574, 1.410302758216858, "The Operation Duration of the Yutu Lunar Rover is 972 days."]
[9.504690170288086, 8.951282501220703, "The Earth Illumination Angle Constraint of the CHEOPS Telescope is Larger than 35\u00ba."]
[7.332767486572266, 6.595269680023193, "The Instrument Builder of the TEMPEST-D Satellite is JPL."]
[6.823230743408203, 2.0515267848968506, "The Rainfall Measurement of the IMERG Satellite Data Product is Over 310 mm."]
[9.334572792053223, 10.234929084777832, "The Focal length of the 1000 mm camera Camera is 1000 mm."]
[5.196714878082275, 6.980490684509277, "The Integration Time (ms) of the Antenna Reflector is 100."]
[9.553396224975586, 8.998491287231445, "The Aperture of the NESSI Telescope is 15 cm."]
[8.628281593322754, 9.850556373596191, "The Area of the GDS Light Curtain is 100 cm2."]
[6.385159492492676, 5.12994909286499, "The Data Input of the Coprocessor Satellite Component is PRN, estimated delay, and estimated Doppler of the reflection."]
[9.373512268066406, 10.155460357666016, "The Filming Locations of the UrtheCast\u2019s Proprietary HD Video Camera Camera is More than 10 countries across four continents."]
[5.379312992095947, 5.644186496734619, "The Fix Interval of the NovAtel OEMV-1 GPS receiver GPS Receiver is Approximately once every 25 hours."]
[7.191678524017334, 3.842970371246338, "The Configurations of the Satellite Constellation Imaging Satellite Constellation is Nominal orbital configuration, Interferometric orbital configuration."]
[5.915459632873535, 2.448502779006958, "The Reorganization Date of the Maxar Space Solutions Company is February."]
[3.676706075668335, 6.0513458251953125, "The Data Transfer Rate of the SpW Data Transfer Protocol is 135 Mbit between 2 consecutive image acquisitions."]
[7.699442386627197, -0.49805155396461487, "The Departure Time from Space Station of the Cygnus Cargo Spacecraft is About three months after arrival."]
[7.047832012176514, 7.459969997406006, "The Operation Modes of the MPO-MAG instrument Instrument is Set of science operations modes."]
[7.232872009277344, 0.2824803292751312, "The Launch Date of the Anand Satellite is 26 November 2022."]
[5.30034875869751, 4.6752424240112305, "The Receiver Sensitivity of the Argos System Data Collection System is Increased."]
[10.87558364868164, 3.7598650455474854, "The Trajectory Deflection of the Solar System Celestial System is Diameter of an atom every second."]
[5.034376621246338, 6.112684726715088, "The Frequency (MHz) of the GPS L1C Signal Carrier is 1575.42."]
[5.951382637023926, 2.900883197784424, "The Prime Contractor of the Spacecraft Satellite is Alenia Spazio."]
[1.061499834060669, 4.321186542510986, "The Battery Type of the EPS Electric Power Subsystem is NiH 2  battery."]
[8.00355339050293, 4.545193672180176, "The Panchromatic Resolution of the SuperView 1A and 1B Satellite is 0.5 m."]
[6.280152320861816, 0.7547072768211365, "The Launch Date of the Argos ANGELS Satellite is 18 December 2019."]
[4.503968238830566, 3.893069267272949, "The Heritage of the Avionics Core Satellite Component is Multi-mission version of avionics."]
[6.06526517868042, 9.673050880432129, "The Mass of the DPU Digital Processing Unit is 14 kg."]
[5.907145023345947, 4.289595603942871, "The Ground Earth Stations of the MSAS Satellite-based Augmentation System is Kobe Aeronautical Satellite Center and the Hitachi-Ota Aeronautical Center."]
[13.106822967529297, 4.057151794433594, "The Purpose of the Gaia Satellite is Measure the positions and motions of stars in our Milky Way galaxy."]
[10.186901092529297, 2.9955825805664062, "The Orbit Altitude of the CartoSat-2D Satellite is 506 km."]
[10.001073837280273, -0.699874222278595, "The Dimensions of the NanoRacks Kaber Microsat Deployer Satellite Deployer is 40 cm x 42 cm x 31 cm."]
[7.986343860626221, -0.7095851302146912, "The Arrival Date of the SpaceX Dragon Spacecraft is 4 April 2018."]
[3.60760235786438, 6.298253536224365, "The Data Rate of the Transmitter Communication Device is 500 Mbit/s."]
[6.593749523162842, 0.3887144923210144, "The | of the Long March 4B Launch Vehicle is \"China and Brazil to launch CBERS 3 satellite in November 2012\"."]
[7.672608375549316, 0.11605855822563171, "The Launch Date of the CXBN-2 Satellite is 18 April 2017."]
[8.513669967651367, 3.541140556335449, "The Orbit Estimator of the NigeriaSat-2 Satellite is Recursive orbit estimator."]
[8.308804512023926, 9.87149715423584, "The Detector Type of the IIR Imager is Microbolometer."]
[4.029743671417236, 10.355535507202148, "The NE\u0394T (K) of the ICI-5 Radiometer is 1.1."]
[10.060235977172852, 4.807319164276123, "The Propulsion System of the SkySat-3 Satellite is HPGP (High Performance Green Propulsion) system."]
[7.341699600219727, 7.824857711791992, "The Objectives of the AMSU-A Instrument is Atmospheric temperature profile measurements from the surface up to about 50 km in 15 channels."]
[8.851384162902832, 7.070713996887207, "The Impact Detection of the Apollo seismometers Seismometers is Large impacts."]
[11.359542846679688, 6.577230930328369, "The Launch Date of the IXPE observatory X-ray Observatory is 2021."]
[6.41160249710083, 9.164620399475098, "The Electronics Package Volume of the FlaPS Instrument Package is 290 cm3."]
[9.493656158447266, 6.095713138580322, "The Sensor Quantity of the ADS Attitude Determination Subsystem is 3-axis magnetometer."]
[7.9173197746276855, 0.4089551270008087, "The Launch Date of the CryoSat Satellite is Oct. 08, 2005."]
[4.648221492767334, 9.062064170837402, "The Next Dust Clearing Date of the InSight Mars lander Spacecraft is June 5, 2021."]
[8.036731719970703, 1.3441686630249023, "The Mission Start Date of the Solar Orbiter Spacecraft is February 14, 2020."]
[7.540244102478027, 7.961981773376465, "The Accuracy of the CERES Instrument is 0.6 Wm -2  sr -1."]
[9.640042304992676, 6.577223777770996, "The Attachment Method to SA panel of the Superelastic Springs Mechanical Component is Riveted and directly soldered."]
[8.026397705078125, 10.184638977050781, "The Field of View of the WV60 imager Imaging System is 2.12\u00b0."]
[7.1791205406188965, 0.5212962627410889, "The Launch Date of the Ven\u00b5s Satellite is Aug. 2, 2017."]
[6.672701835632324, 0.672895073890686, "The Launch Date of the TET-1 Satellite is 2012."]
[7.510542869567871, 9.563291549682617, "The Spectral Band Wavelengths of the ERIP Earth Remote-Sensing Imaging Package is 252.0, 273.5, 283.0, 292.2, 301.9, 320.0, 340.0 nm."]
[6.556634902954102, 2.1687710285186768, "The Operating Status of the Envisat Satellite is Nominal."]
[7.311761856079102, -0.11617156863212585, "The Launch Date of the H-IIA launch vehicle No. 37 Launch Vehicle is 23 December 2017."]
[9.242527961730957, 9.17458438873291, "The Photon Index Above the Break of the First Broken Powerlaw Model Component is 1.4."]
[8.00866985321045, -0.692514181137085, "The Launch Date of the Crew Dragon Spacecraft is 2:40 a.m. EDT Oct. 31."]
[9.422837257385254, 5.519798755645752, "The Pointing Error of the AOCS Attitude and Orbit Control Subsystem is \u00b1 0.05\u00ba in roll and pitch."]
[9.520524024963379, 1.020858883857727, "The Approximate Time to Deorbit of the Spacecraft 3U CubeSat is 5-20 days."]
[7.340148448944092, 10.118681907653809, "The Development Lead of the HyperScout Hyperspectral Imager is cosine."]
[8.802562713623047, 10.166872024536133, "The Onset of Latchup of the CMOS Sensors Sensor is Occurs at LET values typically 16 MeV cm-2/mg and higher."]
[9.62739372253418, 7.850536823272705, "The Measurement Type of the NINA-2 Experiment is Light high-energy ions."]
[10.2555513381958, 5.192890644073486, "The Design Pressure of the Cylinders Pressure Vessel is More than double normal operation pressure - 1000 times atmospheric pressure."]
[7.842687606811523, 9.949102401733398, "The Swath Width (Individual) of the HRV Imager is 60 km."]
[2.217600107192993, 4.567825794219971, "The Payload Power of the DSX Spacecraft Payload Module Satellite is 350 W, 1.1 kW."]
[11.820794105529785, 1.1149348020553589, "The Advanced Small Analyzer for Neutrals(ASAN) of the Chang\u2019e-4 Rover Rover is International Joint Collaboration Payload."]
[10.611294746398926, 6.146474838256836, "The Objective of the RHESSI Imaging Instrument is Obtain high fidelity color movies of solar flares in X-rays and gamma rays."]
[6.988554954528809, 4.916855335235596, "The Planned Observational Capabilities of the FengYun LEO satellites Satellite is WindRAD for sea winds, GAS for greenhouse gases absorption measurement."]
[6.794763565063477, 4.231119632720947, "The Application of the Observation Target Satellite is Maritime, Disaster Monitoring, Water Conservancy, Meteorology."]
[10.372760772705078, 2.677072048187256, "The Apogee Alignment of the MMS and THEMIS Satellites is 180\u00ba apart."]
[7.829987049102783, -0.0062147327698767185, "The Launch Date of the Prichal Module Docking Port is 24 November 2021."]
[2.260279417037964, 4.3681206703186035, "The Power of the Minisatellite Satellite is 50 W."]
[11.406329154968262, 1.0308035612106323, "The Components of the Tianwen-1 Mars Mission is Mars orbiter, a lander and a rover."]
[4.483619213104248, 6.860057353973389, "The Antialiasing Filter Poles of the Rx Module Digital Receiver is 19."]
[8.254098892211914, 8.77500057220459, "The Objective of the S-020 XUV Spectrograph is 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."]
[10.126609802246094, 4.960163116455078, "The Purpose of the Electric Propulsion Propulsion System is Propel the satellites from the orbit in which they will be launched to the final operational orbits."]
[11.753640174865723, 3.5589280128479004, "The Location of the Eureka Station Weather Station is Canadian Arctic at 80 degrees north latitude."]
[5.333736896514893, 4.762358665466309, "The Experiment of the ISL Tracking Antenna Antenna is Bidirectional TM/TC data relay to a LEO satellite."]
[7.592352390289307, 2.6840505599975586, "The Operation of the CAPSTONE Spacecraft is Return humans to the Moon."]
[8.02808666229248, 1.9971147775650024, "The URL of the Orion Spacecraft is http://www.nasa.gov/feature/orion-passes-the-pressure-test."]
[7.015065670013428, 3.9775779247283936, "The Long-Term Tracking of the LAGEOS Satellite is Yes."]
[8.78413200378418, 8.544185638427734, "The Cross-Track of the HORUS Sensor is 1.6\u00b0."]
[5.647303104400635, 3.5275466442108154, "The Purpose of the GMDSS Global Maritime Distress and Safety System is Rescue mariners in emergency situations while at sea."]
[5.900855541229248, 6.697293281555176, "The Incident Angle of the Radar Radar is ~39\u00ba."]
[6.00653076171875, 8.027047157287598, "The Frequency of the Millimeterwave receiver radiometer is 190 GHz."]
[8.894640922546387, 9.344400405883789, "The Advantages of the Diffracting Optic Optic is Easing of engineering constraints, reduction in mass."]
[7.115426063537598, 7.2991251945495605, "The Operation of the Frontier Radio Instrument is Hardened to continue working even in the harshest conditions."]
[11.123151779174805, 2.537156105041504, "The Maximum Rock Height of the Schiaparelli Lander is 40 cm."]
[8.22574234008789, 4.308703422546387, "The Magnetic Field of the SWFO-L1 Satellite is +10."]
[11.484611511230469, -1.2919539213180542, "The Weight of the SPOT-1 Satellite is 1800 kg."]
[7.907937049865723, 5.667766571044922, "The Behavior of the SAA South Atlantic Anomaly is Gradually weakening."]
[8.84477424621582, 10.768240928649902, "The Spatial Resolution of the HSC CCD Imaging Camera is 300 m."]
[7.921721458435059, 4.607386112213135, "The Recording Resolutions of the SPOT-4 Satellite is 2.5 - 20 m."]
[5.970433712005615, 6.106899738311768, "The Multi-Look of the Capella SAR System is 30."]
[9.005497932434082, 7.120837688446045, "The Quantity of the Coarse Sun Sensor Cells Sun Sensor is 8."]
[3.896047353744507, 2.3279173374176025, "The CubeSat of the Satellite PhoneSat-2.5 is 1U."]
[11.029959678649902, 5.1529011726379395, "The Associated Event of the Solar Flare Natural Phenomenon is Fast coronal mass ejection (CME)."]
[2.0190834999084473, 7.845723628997803, "The Solar Wind Speed and Beta of the ACE Satellite is ~41% lower on average from 2009 through the day 79 of 2013."]
[11.479430198669434, -1.3110356330871582, "The Mass (kg) of the IceEye-1 Satellite is 80."]
[11.629658699035645, -1.2442395687103271, "The Mass of the UKube-1 Satellite is < 1080 g."]
[9.955890655517578, 2.44404935836792, "The Predicted Pmp at EOL of the KOMPSAT-6 Satellite is 2,258 W."]
[5.444404602050781, 5.59922456741333, "The Channels of the BlackJack GPS Instrument is 16."]
[6.827493667602539, 1.279131293296814, "The Conference Date of the PSAT Satellite is Aug. 5-10, 2017."]
[11.755900382995605, 4.424558639526367, "The Age of the HD 166191 Star is 10 million years."]
[7.025819778442383, 1.765536904335022, "The Completion Date of the CMIP6 Climate Model is Recent."]
[10.426520347595215, 4.66111421585083, "The Delta-V of the Water Propulsion System Propulsion System is More than 130 m/s."]
[7.054469585418701, 8.894469261169434, "The | 185 km of the MSS Instrument Swath is Swath 185 km."]
[4.7098917961120605, 3.88032865524292, "The Mission Objective of the TechEdSat Satellite is 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."]
[6.4076642990112305, 1.3644351959228516, "The Formation Flying Demonstration of the PRISMA Satellite is Unknown."]
[6.150452136993408, 6.725362300872803, "The Required Tracking Interval of the TIRA Radar Tracking Station is 12 hours."]
[8.85684871673584, 5.316732406616211, "The Attitude Pointing Accuracy of the CHIPSat Satellite is \u00b12\u00ba."]
[10.04823112487793, 5.136099338531494, "The Testing Method of the ESP Thruster Thruster is Firing in pairs and measuring the changes to the spin rate via on-board rate instrumentation."]
[7.946932315826416, 1.221163034439087, "The Launch Date of the LunaH-Map Spacecraft is Second half of 2021."]
[11.224406242370605, 7.0400519371032715, "The Quantity of X-ray Optics of the NICER/SEXTANT Instrument is 56."]
[8.629438400268555, 6.880121231079102, "The Spatial Resolutions of the FGM Fluxgate Magnetometer is About 200 or 100 m."]
[7.199686050415039, 1.4457683563232422, "The Launch Year of the ERS-2 Satellite is 1995."]
[6.554573059082031, 1.7233555316925049, "The Satellite Launch Date of the Kleos S.A. Company is Mid-2021."]
[7.801108360290527, 9.051875114440918, "The Wavelength of the TIR Thermal Infrared region is 0.5, 1.0, 1.0 \u00b5m."]
[6.161591529846191, 6.179220676422119, "The Purpose of the TOPSAR SAR Mode is Wide swath imaging."]
[7.762414932250977, 2.7188334465026855, "The Imaging Filters of the MRO Mars Reconnaissance Orbiter is Three."]
[7.1344075202941895, 8.641423225402832, "The Swath width of the SBUS Solar Backscattering UV Sounder is ."]
[7.4879865646362305, 1.1723124980926514, "The Telescience Support Unit Presentation Date of the Foton Spacecraft is Oct. 2-6, 2006."]
[11.311400413513184, 3.977196455001831, "The Rotation Rate Measurement of the Exoplanet Celestial Body is Two to three times per orbital period for about seven orbital periods."]
[8.275623321533203, 8.57198429107666, "The Detector of the Spectral Band D Spectrometer is Si-PIN."]
[10.069173812866211, 9.442068099975586, "The Near-UV Channel Range of the IRIS Observatory is 278.0\u2013284.0 nm."]
[9.25240421295166, 3.1773478984832764, "The Orbit Type of the WorldView-3 Satellite is Sun-synchronous orbit."]
[7.129209518432617, 1.513779640197754, "The Status Update Date of the Cluster Satellite Constellation is July 2015."]
[10.313570022583008, 7.7039995193481445, "The Baffles Material of the Collimator Instrument Component is Tantalum (Z=73)."]
[8.027297973632812, 8.902443885803223, "The Spectral Sampling of the Telescope Optical Instrument is 2.55 nm."]
[9.004044532775879, 7.4984660148620605, "The Resolution of the FSS Fine Sun Sensor is 0.005\u00ba."]
[5.26473331451416, 6.430637836456299, "The Polarizations of the Communication System Data Transmission is RHCP (Right-Hand Circular Polarization) and LHCP (Left-Hand Circular Polarization)."]
[7.572977542877197, 9.608278274536133, "The Spatial Resolution (IFOV) of the ERIP Earth Remote-Sensing Imaging Package is 170 km x 70 km."]
[11.479866027832031, 4.382409572601318, "The Origin of the Stardust Grain Particle is Nova explosion more than 4.5 billion years ago."]
[11.579046249389648, -1.2626595497131348, "The Mass of the CICERO satellites Satellite is Approximately 10 kg."]
[1.9200758934020996, 3.885427474975586, "The Solar Panel Type of the Canopus Pipper Satellite is Triple-junction 26% efficient solar cells."]
[3.768606662750244, 4.54802942276001, "The Processor of the CryoSat Satellite is Sparc ERS 32."]
[5.042061805725098, 2.6246373653411865, "The Collaboration of the MAYA-1 1U CubeSat is DOST-ASTI, KIT."]
[9.250446319580078, 7.897514343261719, "The Operating Temperature of the SWIR Detector is 257 K."]
[8.07078742980957, 8.62082576751709, "The Spectral Range of the FTS Interferometer Interferometer is 2.4-13.3 \u00b5m (or 750-4100 cm -1)."]
[5.853446960449219, 8.584152221679688, "The Data Usage of the MHS Microwave Humidity Sounder is Provides the operational microwave sounding capability for the NOAA-N, -N' meteorological satellites."]
[9.4745454788208, 0.6969755291938782, "The Mission Tenure of the RHESSI Satellite is 10 Years."]
[9.213555335998535, 3.229609966278076, "The Orbit Type of the JAWSAT Satellite is Sun-synchronous near-circular orbit."]
[8.97063159942627, 9.651745796203613, "The Components of the SWIR Camera System Camera System is Integrated detector cooler assembly, MCT photodiode array, ROIC, pulse tube cooler."]
[7.841869831085205, 8.363828659057617, "The Publication Date of the Envisat's Medium-Resolution Imaging Spectrometer Spectrometer is November 1993."]
[8.179093360900879, 9.194310188293457, "The Swath Width of the TIRS-2 Sensor is 185 km."]
[5.319697856903076, 6.451450824737549, "The Polarizations of the Antenna Communication System is Ch 0, 1, 2: RHCP, Ch 3, 4, 5: LHCP."]
[7.802505970001221, 9.642744064331055, "The Spectral Bands of the EarthDaily Optical Imager Optical Imager is 6 bands in each of the visible, near-infrared (NIR) and shortwave infrared (SWIR) spectrums, and 4 in the thermal infrared (TIR) spectrum."]
[9.52089786529541, 0.9753850102424622, "The Operation Duration of the SPOT-VEGETATION Satellite is 16 years."]
[6.815165042877197, 3.6287667751312256, "The Modes of Operation of the CXBN-2 Spacecraft is Failure recovery, standby/uplink, downlink, and full science modes."]
[10.348995208740234, 5.0608954429626465, "The Firing Duration of the Micronozzle Propulsion System is 10 s x 3."]
[4.502832889556885, 3.649719715118408, "The Antenna Footprint of the AIS Automatic Identification System is Has narrower size due to lower satellite orbit altitude."]
[2.0184743404388428, 7.846619606018066, "The Solar Wind Speed and Beta of the ACE Satellite is ~48% lower on average from 2009 through the day 79 of 2013."]
[9.966863632202148, 1.4392191171646118, "The Time to Point to the Sun of the TSUBAME Satellite is 33873 seconds after the separation."]
[8.355791091918945, 6.427931308746338, "The Environment of the Functional Tests Testing is Ambient (and gravity)."]
[7.761622428894043, 8.395134925842285, "The Images per Capture of the EPIC Instrument is 10."]
[7.350671291351318, 0.3538847267627716, "The Launch Date of the NeuSAR Satellite is June 30, 2022."]
[8.364563941955566, 1.8990745544433594, "The Conference Presentation of the SWAP EUV Telescope is March 30-April 2, 2004."]
[6.737388610839844, 5.163886547088623, "The Spectral Bands of the Sentinel-2 Satellite is 13."]
[8.413403511047363, 6.622167587280273, "The Design Basis of the SWiPS Sensor is IES (Ion and Electron Sensor) flown on ESA's comet mission, Rosetta."]
[8.86545467376709, 6.660656452178955, "The Accuracy of the Lateral Shearing Angular Period Device is 206 mas."]
[8.380695343017578, 3.733403444290161, "The Integration of Physical Components of the Cooperation by Federation Data Exchange is Not Required."]
[4.872632026672363, 5.502338409423828, "The Radio Frequency of the Reception Station Ground Station is 7.8 GHz."]
[4.7194318771362305, 1.6562968492507935, "The Number of Satellites of the Galileo Satellite System is 14."]
[6.417043685913086, 8.61898136138916, "The Frequency Range of the MWNIR Imaging System is 6.6 GHz - 37 GHz."]
[6.168667316436768, 7.874175548553467, "The Polarization of the MTVZA-GY Radiometer is Vertical and Horizontal."]
[11.581133842468262, 5.103244781494141, "The Ability of the Black Hole Cosmic Object is Pulling things toward it and blasting material away from itself."]
[6.27661657333374, 8.196975708007812, "The Operating Bands of the MWR Microwave Radiometer is K-band and Ka-band."]
[3.592193365097046, 4.470202445983887, "The ROM/RAM of the ACU Attitude Control Unit is EEPROM(1MB x 2), SRAM(1MB x 2) for C&DH EEPROM(1MB), SRAM(1MB), MRAM(512KB) for HSS."]
[8.445687294006348, 10.650671005249023, "The Power of the CCD Camera Imaging System is <50 W."]
[7.826248645782471, 5.811089992523193, "The Sea Surface Calibration Mode of the EarthCARE satellite Satellite is CPR in Sea Surface Calibration mode."]
[7.377162933349609, 3.9144375324249268, "The Mission Objective of the EROS-B Satellite is Provide high-resolution imagery to the customer base."]
[7.942225456237793, 8.947336196899414, "The Spectral Range of the Telescope Optical Instrument is 400-1000 nm."]
[4.080514430999756, 4.6294636726379395, "The Software of the TPMU Device is 8051 Pascal mode."]
[6.009551525115967, 3.3387880325317383, "The Partnership of the ESA and EDA Organizations is Solid."]
[11.837156295776367, 3.1507813930511475, "The Inclination of the 46 nanosatellites Satellite is 97.51\u00ba."]
[4.316827297210693, 6.539614200592041, "The Frequency Bands of the DCS Data Collection System is UHF (401.9 MHz), S-band (1694.5 MHz), S-band (2034.9 MHz), UHF (468.8 MHz)."]
[9.329910278320312, 9.268455505371094, "The Diameter of the VPW42 Optical Window is 1.5\u201d."]
[7.873785972595215, 4.990462779998779, "The Orbit Determination Method of the WEOS Satellite is Uses the Keplerian elements of the satellite which are estimated from its locations measured by the onboard GPS receiver."]
[8.455114364624023, 9.907992362976074, "The CCD Array Size of the MEGS Spectrograph is 1024 x 2048 pixels."]
[4.242668628692627, 5.7652482986450195, "The Downlink Transmission of the X-band telemetry subassembly Telemetry Device is Stored image data."]
[6.624599933624268, 4.537065505981445, "The Application Categories of the Sentinel-3 Ocean Surface Topography Mission is Numerical weather prediction, Climate change."]
[6.072761535644531, 6.22808313369751, "The Spatial Resolution of the Instrument SAR is \u2264 60 m x 50 m."]
[6.029533863067627, 5.3284592628479, "The Objective of the RARS Regional ATOVS Retransmission Services is Expand the RARS concept to other data types in support of a wider range of applications."]
[7.22786283493042, 8.63586711883545, "The Spectral range of the SBUS Solar Backscattering UV Sounder is 250-340 nm."]
[9.16749095916748, 2.155724287033081, "The Image Transmission Time of the New Horizons Spacecraft is More than four hours."]
[9.946412086486816, 4.130162715911865, "The Propulsion Method of the LightSail-2 Solar Sailing CubeSat is Solar sailing."]
[5.650630474090576, 4.994856357574463, "The Launch Lock of the OSIRISv3 Laser Communication Terminal is Not required."]
[8.59444522857666, 1.741622805595398, "The Update #6 Date of the JWST Telescope is April 2009."]
[5.730854511260986, 9.130085945129395, "The Power of the Instrument Spectrometer is < 17 W."]
[4.735284805297852, 1.687247633934021, "The Number of Satellites of the Galileo Satellite Constellation is 26."]
[11.303903579711914, 6.668324947357178, "The Mirror Module Assemblies Presenter of the IXPE Satellite is Brian Ramsey."]
[10.216532707214355, 4.772581100463867, "The URL of the \u00b5CAT Micro-Propulsion Solution Propulsion System is https://digitalcommons.usu.edu/cgi/viewcontent.cgi?referer=&httpsredir=1&article=3374&context=smallsat."]
[9.388829231262207, 0.4553914964199066, "The Design Life of the Jason-1 Satellite is 5 years."]
[5.745783805847168, 0.40970468521118164, "The Date of the The Black Fire Blows Up in New Mexico Image is 24 May 2022."]
[8.656885147094727, 8.888631820678711, "The Mounting of the HETG Grating is Concurrent."]
[9.750258445739746, 8.478287696838379, "The Mounting of the Solar Orbiter /PHI Full Disk Telescope Telescope is Unknown."]
[6.166027545928955, 3.3062949180603027, "The New Program Segments Languages of the ESA European Space Agency is Dutch, French, German, Italian and Spanish."]
[9.65774917602539, 7.395061016082764, "The Displacer Unit of the Stirling Cycle Cooler Cooler is Single, similarly driven, displacer unit orthogonal to the compressor axis."]
[5.8765788078308105, 3.5408871173858643, "The Location of the RADARSAT MMO Mission Management Office is CSA in Saint-Hubert, Quebec."]
[9.425990104675293, -0.16029781103134155, "The Technology Readiness Level of the SMDC-ONE Nanosatellite is TRL-7."]
[10.557547569274902, 8.4768705368042, "The Optical Design of the COR2 Coronagraph2 Imager is Externally occulted Lyot design."]
[7.077546119689941, 5.623215198516846, "The Spectral Bands of the SLIM6 Satellite is 0.52-0.62 \u00b5m, 0.63-0.69 \u00b5m, and 0.76-0.9 \u00b5m."]
[10.278818130493164, 3.026076316833496, "The Altitude for Satellite Release of the Falcon-9 Rocket Rocket is 450 km."]
[7.422565937042236, 4.85543155670166, "The Objective of the SENSE Satellite is Provide data for ionospheric prediction models."]
[3.7848265171051025, 4.508886337280273, "The Processor Type of the SCP Spacecraft Process Controller is Honeywell VHSIC MIL-STD-1750A microprocessor."]
[6.674795150756836, 0.866466224193573, "The Launch Date of the FormoSat-3/COSMIC-1 Satellite Constellation is April 15, 2006."]
[1.7613071203231812, 4.799715042114258, "The Power of the EPS Electrical Power Subsystem is ~ 2 W."]
[6.792667865753174, 7.6026458740234375, "The Purpose of the LRF-S2 Laser Device is Measure the distance to the tip of the sampler horn."]
[5.115152835845947, 4.668628692626953, "The Data Transmission of the McMurdo Ground Station Ground Station is NOAA in Suitland."]
[9.42487907409668, 9.055757522583008, "The Length of the Telescope Optical Instrument is 2465 mm."]
[10.434624671936035, 2.639653205871582, "The Apogee of the Gravity Probe A Satellite is 10,000 km."]
[3.936889886856079, 2.3270020484924316, "The Size of the POPSat-HIP-1 CubeSat is 3U."]
[5.684855937957764, 5.16656494140625, "The Build Location of the Near Real Time SAR Processor SAR Processor is Ahmedabad."]
[5.639463901519775, 6.552045822143555, "The Deployed Antenna Size of the IAE Experiment Satellite Component is Roughly the size of a tennis court."]
[4.998394012451172, 1.8494246006011963, "The Number of Satellites of the Cluster Satellite Constellation is 4."]
[9.575072288513184, 7.18245267868042, "The Temperature Increase Objective of the Paris Agreement International Agreement is Well below 2\u00b0C above pre-industrial levels and pursuing efforts to limit the temperature increase to 1.5\u00b0C above pre-industrial levels."]
[4.352950096130371, 5.606776237487793, "The Usage of the USRP Transceiver is Access the RF signals, demodulate, and decode the signals."]
[6.680866241455078, 0.5843440890312195, "The Launch Year of the RISAT-1 Satellite is 2012."]
[10.236103057861328, 2.9879841804504395, "The Orbit Altitude of the HTV-8 Spacecraft is ~400 km."]
[7.849637508392334, 0.796859085559845, "The Orbital Flight Test Date of the Starliner Spacecraft is Unknown."]
[-4.981083393096924, 4.407583236694336, "The Support Phase Time Period of the Mango Tango Satellite Formation is 15.06 to 19.06.2010."]
[3.827211618423462, 6.401181697845459, "The Locking Time of the Comb Oscillator Oscillator is Reached within seconds."]
[4.029326438903809, 5.6934590339660645, "The ETM Output of the Landsat-6 Satellite is Two 85 Mbit/s serial composite streams."]
[6.474884986877441, 5.677436828613281, "The Presentation Date of the GPS Radio Occultation Instrument Instrument is April 3-6, 2017."]
[3.955524206161499, 4.324202060699463, "The Manufacturer of the CDHS Command and Data Handling Subsystem is University of Tartu."]
[7.81867790222168, 0.7361882925033569, "The Bulletin Release Year of the OceanSat-2 Satellite is 2010."]
[9.276826858520508, 10.310029983520508, "The Field of View (Cross-track) of the MSU-50 Camera is 62\u00ba."]
[7.212525844573975, 1.0643142461776733, "The First Picture Acquisition Date of the D-Sat Satellite is June 26, 2017."]
[5.980306625366211, 8.453556060791016, "The System Type of the GeoSTAR Atmospheric Microwave Sounder is Sparse array synthetic aperture radiometry."]
[10.00712776184082, 5.294174671173096, "The Pressure of the Inflation Pressure Satellite Component is 20,600 bar (3 x 104 psi)."]
[7.791380405426025, 7.715273380279541, "The CRISM Spectrometer of the Mars Reconnaissance Orbiter Satellite is Spectrometer."]
[9.530661582946777, 9.074201583862305, "The Focal Length of the Telescope Optical Instrument is 167 cm."]
[2.2107551097869873, 1.731909990310669, "The CCSDS ID of the GSAT-0203 Satellite is 263."]
[6.606342792510986, 2.5506458282470703, "The Team Members of the Dellingr Satellite is 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, S."]
[7.294250965118408, 5.60187292098999, "The Horizontal Domain of the Aeolus Satellite is Global coverage."]
[4.226917266845703, 4.545680999755859, "The Function of the Interface Chip Chip is Provides a convenient breakout interface."]
[6.205277919769287, 4.845007419586182, "The Imagery Type of the SAR Satellites Satellite is SAR."]
[7.717068672180176, 8.238761901855469, "The Coil Windings of the VLF Experiment Scientific Experiment is 1000."]
[7.839297771453857, 9.848248481750488, "The Swathwidth of the PAN Imaging System is 9.6 km."]
[8.255749702453613, 7.044455528259277, "The Location of the ISS-EMIT Instrument is Onboard the International Space Station\u2019s (ISS) primary forward-facing hub for externally mounted instruments."]
[5.9168219566345215, 7.778915882110596, "The Telemetry Bit Rates of the MPO-MAG instrument Instrument is 64, 32, 16, 8, 4, 2, 1, and 0.5 Hz."]
[8.162619590759277, -0.6806325912475586, "The Orbit Altitude of the Crew Dragon Spacecraft is Approximately 575 kilometers."]
[1.901416301727295, 3.8626625537872314, "The Power Generation Technology of the GaInP2/GaAs/Ge solar arrays Solar Arrays is GaInP2/GaAs/Ge."]
[8.131292343139648, 9.128918647766113, "The Imaging Concept of the OCM Instrument is Extension of the imaging concept adopted for the IRS LISS instruments."]
[8.463568687438965, 8.322205543518066, "The Number of Detectors of the Spectrometer Instrument is 4."]
[10.007842063903809, 1.5599631071090698, "The Orbital period of the Satellite GEO (Geostationary Earth Orbit) is 24 hours."]
[7.321410655975342, 0.6454043388366699, "The Launch Preparations Date of the Mission Extension Vehicle Satellite is 30 June 2020."]
[8.957982063293457, 10.231042861938477, "The Brightness Comparison of the Newly Detected Source Object is More than 1000 times fainter than Beta Pictoris."]
[9.651503562927246, 6.000751495361328, "The Challenges of the ADCS Attitude Determination and Control Subsystem is Calibrating and monitoring this subsystem across a large constellation, complexities introduced by distributed launches and multiple hardware revisions, resource constraints."]
[4.691320419311523, 5.560057640075684, "The Communication Mode of the LLITED satellites Satellite is Receive only."]
[6.631082057952881, 3.744523048400879, "The Purpose of the TRISHNA Satellite is Climate monitoring and operational applications."]
[7.200932502746582, 5.9700188636779785, "The Measurement Range of the OCI Ocean Color Instrument is Ultraviolet to the shortwave infrared."]
[6.975437641143799, 0.8752951622009277, "The Launch Date Risk of the ORS-6 Satellite Mission is Adds risk to the program."]
[8.954400062561035, 10.442648887634277, "The Size of the LinkSprite JPEG color VGA camera Camera is 32 mm x32 mm."]
[9.323539733886719, 2.5224947929382324, "The Mission Start Date of the EURECA Satellite is August 7, 1992."]
[5.217728614807129, 4.620672225952148, "The Location of the Ground Segment Ground Station is Roof of the research lab IES (Institut d'Electronique du Sud) building located on the campus of UM2 (University Montpellier 2)."]
[7.5629048347473145, 4.75295877456665, "The Justification of the ACE Satellite is Providing context and supporting data to nearly all other solar, heliosphere, magnetosphere, and ionosphere/thermosphere missions both current and planned."]
[9.188179969787598, 6.172040939331055, "The Operation Principle of the Gyro Unit Attitude Control is Electrically-excited vibration of a solid cylindrical element."]
[8.373429298400879, 2.790844202041626, "The Satellite Bus of the JPSS Joint Polar Satellite System is \"NPP-like\"."]
[5.622956275939941, 2.3391356468200684, "The Daily Deep-Space Observations of the SBSS-1 Satellite System is 12,000."]
[8.931626319885254, 2.389805316925049, "The Observation Results of the Herschel Space Observatory is Intricate network of gas filaments and dark bubbles interspersed by bright hotspots."]
[4.726943016052246, 2.180145025253296, "The Quantity of the FIREBIRD-I CubeSats is 2."]
[7.154648780822754, 6.88762903213501, "The Critical Design Review Date of the Instrument Satellite Instrument is Early 2020."]
[10.367066383361816, 2.65803599357605, "The Apogee Alignment of the THEMIS Satellite is Opposing."]
[9.493577003479004, 0.6692325472831726, "The Mission Lifetime of the CHIPSat Satellite is One year."]
[7.379333019256592, 8.676718711853027, "The Data Rate of the Scanning geometry Instrument is 660 kbit/s."]
[8.95215129852295, 10.475546836853027, "The Detector Array of the WiFS camera Camera is 2 x 2048 pixels."]
[8.340991020202637, 8.642855644226074, "The Detectors of the Visible Spectral Band Spectral Band is Si photodiode."]
[4.044568061828613, 5.690456867218018, "The Image Telemetry Link of the SPOT-1 Satellite is 50 Mbit/s at 8 GHz."]
[5.84694242477417, 6.785224437713623, "The Bandwidth of the SWIM Instrument Radar is 320 MHz."]
[8.729449272155762, 7.71441125869751, "The Calibration of the Scanning Optical Thermopile Calibration Device is NIST-traceable."]
[5.652316093444824, 7.5380940437316895, "The Stowed Configuration Size of the KaRIN Instrument is 3.0 m x 2.8 m x 2.8 m."]
[4.760161399841309, 5.009119510650635, "The Function of the TSCT Terminal is 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."]
[7.202882766723633, 8.925882339477539, "The Image Size of the CIPS Instrument is 1440 km x 960 km."]
[8.429017066955566, 9.625067710876465, "The Performance Characterization of the EarthCARE BBR Detectors Instrument is Unknown."]
[4.000680923461914, 6.465065002441406, "The Modulation of the RF Communications Transmitter is FSK."]
[7.724885940551758, 4.146154880523682, "The Number of Images of the SPOT-6 Satellite is More than 100 million km2."]
[9.137299537658691, 9.196891784667969, "The Field of View of the Lens Optical Instrument is 24\u00ba x 24\u00ba."]
[2.298719644546509, 5.750051021575928, "The Duty Cycle of the HPA High Power Amplifier is 12%."]
[7.935262203216553, 2.186979293823242, "The URL of the Radiation Belt Storm Probes Satellite is http://vanallenprobes.jhuapl.edu/common/content/pdfs/VanAllenProbes_FS_Press.pdf."]
[7.067089080810547, 9.749863624572754, "The Spectral Range (\u00b5m) of the Band 8 Spectral Band is 0.48 - 0.53."]
[8.782931327819824, 10.726570129394531, "The Source Data Rate per Band of the MSU-100 Camera is 9.8 Mbit/s."]
[12.975550651550293, 4.13537073135376, "The Previous Catalogue of the Gaia Catalogue of Nearby Stars Stellar Census is Gliese Catalogue of Nearby stars."]
[4.669799327850342, 2.855865955352783, "The AI Model Testing of the \u03a6sat-2 Satellite is 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."]
[8.531759262084961, 5.02208948135376, "The Pointing Accuracy of the NEMO-HD Satellite is 1.5 arcmin."]
[3.608436107635498, 6.362561225891113, "The Data Rate of the S-band Uplink Communication System is 9.6 kbit/s."]
[7.03492546081543, 0.17151837050914764, "The Launch Date of the Satellite Vu\u2019s second satellite Satellite is Early 2024."]
[7.697104454040527, 9.004167556762695, "The Spectral Range of the 1.61 and 2.06 \u00b5m CO2 channel Spectrometer is 1.594 to 1.619 \u00b5m and 2.042 to 2.082 \u00b5m."]
[11.74094009399414, -1.1234670877456665, "The Per spacecraft mass of the WorldView-4 Satellite is 2500 kg."]
[8.107516288757324, 3.2288095951080322, "The Communication System of the TanDEM-X Satellite is S-band receiver."]
[5.354294300079346, 10.40893268585205, "The Latitude Coverage of the LIS Lightning Image Sensor is \u00b154.33\u00ba."]
[11.592399597167969, -0.9742046594619751, "The Body Size of the M1S/M2S Satellite is 2.0 m x 2.5 m x 3.6 m."]
[6.254569053649902, 4.728261947631836, "The SAR Constellation Frequency of the Spacety Company is Day and night."]
[5.889078617095947, 2.9512779712677, "The Platform of the Heinrich-Hertz satellite Satellite is SmallGEO (SGEO)."]
[10.26784896850586, -0.6766303777694702, "The Orbit Altitude of the GOMX-1 Nanosatellite is 600 km."]
[6.18170690536499, 8.396125793457031, "The Type of the MLS Instrument is Microwave radiometer."]
[9.232494354248047, 10.350565910339355, "The Purpose of the High-Resolution Video Camera Camera is Zoom in on the actual target of interest."]
[7.014595985412598, 1.9889754056930542, "The URL of the Swarm Mission is https://earth.esa.int/c/document_library/get_file?folderId=131556&name=DLFE-3101.pdf."]
[6.972206115722656, 4.380993366241455, "The Measurement Domain of the SARAL Satellite is Atmosphere, Ocean."]
[6.539361476898193, 1.1187188625335693, "The Propulsion System Commissioning Date of the PRISMA Satellites Satellite is June 24, 2010."]
[7.179823875427246, 0.576507031917572, "The Launch Date of the SRL-1 (STS-59) Mission is April 9, 1994."]
[6.776487827301025, 4.186629295349121, "The Purpose of the EPS GRAS Mission is Operational GPS Meteorology."]
[9.16787338256836, 4.223114967346191, "The Bus Dimensions of the Helios-2 satellites Satellite is 3.4 m x 3.1 m x 6 m."]
[7.098228454589844, 5.007540702819824, "The Start Date of the Methane Leak Environmental Event is 4 July 2020."]
[8.319462776184082, 8.580242156982422, "The Type of the Spectrograph Instrument is Rowland Circle style imaging spectrograph."]
[6.6855082511901855, 2.6256885528564453, "The Secretariat Location of the Joint Project Team (JPT) Project Team is JAXA."]
[7.895068645477295, 8.607012748718262, "The Scanning Technique of the PRISM-2 Instrument is Pushbroom."]
[9.506183624267578, 3.5659966468811035, "The Pages of the Lunar Flashlight Satellite is 58\u201369."]
[3.838301420211792, 6.017300128936768, "The Data Link Speed of the CMS Instrument is 4 Mbit/s."]
[4.3467183113098145, 5.387669563293457, "The Function of the TTC Rx Receiver is Acquire the residual carrier from the ground station and extract the 16 kHz subcarrier for the telecommand demodulator inside the CCSDS processor."]
[4.293734073638916, 6.253596305847168, "The Intersatellite Link Frequency of the Communication Communication System is S-band."]
[5.339641094207764, 1.4399456977844238, "The Deployment Rounds of the NanoRacks CubeSat Deployer is 3."]
[6.700772762298584, 9.114156723022461, "The Size of the Instrument Device is 9.7 cm x 9.7 cm x 4.8 cm."]
[5.252540111541748, 3.0893404483795166, "The Funding of the NorSat-3 Satellite is Norwegian Ministry of Defence."]
[7.888594150543213, 9.0857572555542, "The Wavelength Range of the S3 Spectrophotometer is 300-800 nm."]
[8.359851837158203, 3.424008846282959, "The Spatial Resolution of the TanDEM-X Satellite is 0.4 arcseconds (12 m at the equator)."]
[8.609172821044922, 10.768165588378906, "The Power Consumption of the LISS-3 Camera is 70 W."]
[7.8973388671875, 4.506670951843262, "The Imaging Resolution of the Resurs-DK1 Earth Observation Satellite is 1 m."]
[9.707608222961426, 1.4506412744522095, "The Forecast Duration of the HWRF Model is 120 hours."]
[10.864791870117188, 5.699504375457764, "The URL of the Can ripples on the sun help predict solar flares? News Article is https://news.berkeley.edu/2020/09/21/can-ripples-on-the-sun-help-predict-solar-flares/."]
[6.790380954742432, 8.306295394897461, "The Number of Flight Models of the MWI Instrument Instrument is Three."]
[6.293210029602051, 3.5091893672943115, "The Location of the Margarita Island Landmark is Venezuela."]
[9.16724967956543, 3.245917558670044, "The Orbit of the CSG and CSK satellites Satellite is Circular sun-synchronous."]
[9.506257057189941, -0.7557321190834045, "The Launch Date of the Tsubame Microsatellite is November 6, 2014."]
[6.7609782218933105, 4.9384541511535645, "The Instruments of the CFOSAT Satellite is SWIM (Surface Waves Investigation and Monitoring), SCAT."]
[4.780172824859619, 0.851518988609314, "The Contract Value of the ICON Satellite is $50 Million."]
[9.313613891601562, 0.3536124527454376, "The Exceeded Design Life of the Jason-2 Satellite is Yes."]
[9.517369270324707, 0.5888842940330505, "The Mission Design Life of the ADEOS spacecraft Satellite is 3 years."]
[6.954965114593506, 5.146703720092773, "The Spectral Bands of the Satellite Satellite is Panchromatic band, 4 MS (Multispectral) bands Pan B, G, R and NIR."]
[1.0419905185699463, 4.324385166168213, "The Li-ion Battery Capacity of the EPS Electrical Power Subsystem is 30 Ah."]
[8.6353178024292, 7.914371013641357, "The Interface of the Tertiary Collimator Assembly Assembly is Optically and mechanically interfaces with the FOA."]
[6.713751316070557, 4.227925777435303, "The Mission Objective of the RADARSAT-1 Satellite is Monitor environmental change and the planet's natural resources."]
[8.055914878845215, 0.40183940529823303, "The Announcement Date of the Thales Alenia Space Ground Station Builder is 9 October 2018."]
[8.169454574584961, 10.23878288269043, "The System Dynamic Range of the PMC-2 Imagers Imaging System is 20~800 DN."]
[9.360518455505371, 0.9087156653404236, "The Actual Orbit Duration of the ESEO Satellite is Almost two years."]
[3.2995715141296387, 4.824789047241211, "The ROM of the Model calculator Data Handling and Processing is 64kB."]
[10.451070785522461, -1.03830885887146, "The Maximum Mass of the O/OREOS nanosatellite Satellite is 5.5 kg."]
[5.965819358825684, 3.9683408737182617, "The Servicing Concept of the Bartolomeo Platform Satellite Platform is Fully robotically serviceable."]
[7.760777950286865, 7.562291145324707, "The Function of the NICER Instrument is Measure light echoes."]
[7.555141448974609, 0.5372913479804993, "The Re-Entry Date of the GRACE 1 Satellite is 11 March 2018."]
[7.414863109588623, 0.26116064190864563, "The Meeting Date of the HY-1B Satellite is Feb. 12-14, 2008."]
[7.595167636871338, 3.87481689453125, "The Imaging Satellite of the KazEOSat-2 Satellite is Medium resolution."]
[7.641816139221191, 4.427618503570557, "The Sensor of the WorldView-3 Satellite is CAVIS."]
[4.41143274307251, 7.679795265197754, "The Bandwidth of the Channel 6 Sensor is 1000 MHz."]
[7.70452880859375, 10.548787117004395, "The Data Quantization of the Hyperion Imaging Spectrometer is 12 bit."]
[9.614049911499023, 1.1578930616378784, "The Attitude Control Time of the PSSCT-2 Satellite is Two months."]
[3.644017219543457, 5.71589994430542, "The Data Rate of the Data Flow System is 2.2 Gbit/day."]
[9.41573429107666, 4.162029266357422, "The Radius of the Spacecraft Satellite is 21 cm."]
[7.95265531539917, 1.045987844467163, "The Image Acquisition Date of the NOAA-20 Satellite is June 5."]
[7.396894931793213, 7.472606182098389, "The First Flight Date of the TOMS Total Ozone Mapping Spectrometer is Oct. 24, 1978."]
[7.941342353820801, 3.8916711807250977, "The Daily Acquisition Capacity of the Pl\u00e9iades Neo Satellite is More than double."]
[5.716382026672363, 3.6239702701568604, "The Control Node Locations of the GeneSat-1 Satellite is 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."]
[5.746768951416016, 2.9103384017944336, "The Manufacturer of the CHIPSat Satellite is SpaceDev, Inc.."]
[5.99507474899292, 0.6223875880241394, "The Operational Date of the MaSat-1 CubeSat is Feb. 2014."]
[8.309870719909668, 8.232277870178223, "The Entrance Slits Alignment of the OCO Instrument Spectrometer is Co-aligned."]
[10.15397834777832, 1.3651028871536255, "The Period of the NEMO-AM Satellite is 97.4 minutes."]
[9.283217430114746, 1.0852293968200684, "The Data Collection Duration of the GPM Satellite is Last 19 years."]
[7.425961494445801, 3.281449794769287, "The Mission Status of the ERS-2 Satellite is Unknown."]
[6.745309352874756, 0.02237343229353428, "The Operation Start Date of the Tatiana-2 Satellite is Sept. 20, 2009."]
[7.061646461486816, 4.055834770202637, "The ACNS Units of the PROBA-2 Satellite is 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."]
[8.756170272827148, 8.558220863342285, "The Forward Used Angle of the Scan Assembly Assembly is 110\u00ba."]
[4.308718681335449, 4.3361287117004395, "The Components of the TAMU MEMS Technology Demonstration Package is 8051 microcontrollers, 4 Mbit Magnetic RAM, and CAN-bus interface."]
[11.138575553894043, 2.8657636642456055, "The Lighting Conditions of the Site Nightingale Crater is Create additional challenges for spacecraft navigation."]
[10.317010879516602, 5.938776969909668, "The Observation Type of the RHESSI Satellite is CME ejection."]
[8.217962265014648, 4.928030967712402, "The Objective of the Variant Satellite is Investigation of the lithosphere-atmosphere-ionosphere-magnetosphere coupling."]
[7.823718547821045, 1.0939840078353882, "The Image Capture Date of the Sentinel-2 Satellite is 20 January 2022."]
[11.531993865966797, 6.298255443572998, "The Number of Observations of the XMM-Newton X-ray Satellite is 1,789."]
[4.192300319671631, 6.511535167694092, "The Band of the Transceivers Communication Device is DSSS 2.4 GHz."]
[7.7180047035217285, 7.208829879760742, "The Preferred Location of the TEMPO Instrument is 90-110\u00ba W."]
[9.278459548950195, 9.261238098144531, "The Spatial Frequency of the Collecting Optics Lens Assembly is 70 l/mm."]
[10.200257301330566, 5.036270618438721, "The System of the Onboard Propulsion System Propulsion System is Split into two modular units."]
[7.228655815124512, 7.041897773742676, "The Pre-launch Performance of the VIIRS Instrument is Unknown."]
[11.627453804016113, -1.1649160385131836, "The Payload Mass of the Eutelsat 172B Satellite is 10,865 kg."]
[7.935789585113525, 5.267044544219971, "The Positioning Accuracy of the Lunar Pathfinder's Receiver Satellite Receiver is Around 100 m."]
[5.689255237579346, 6.576583385467529, "The Lifetime Mechanism of the SWIM RMA Antenna is Unknown."]
[5.193175792694092, 4.128161907196045, "The Mission Analysis of the COSMOS Mission Operations System is Analysis and trending of spacecraft and ground network SOH data, orbital and trajectory data, and mission accomplishment data."]
[5.749639511108398, 6.843904495239258, "The Transmit Bandwidth of the Radar Instrument is 1 MHz."]
[12.091980934143066, 2.2142415046691895, "The URL of the OSIRIS-REx Spacecraft is http://www.spacedaily.com/reports/OSIRIS_REx_cruising_towards_rendezvous_with_Asteroid_Bennu_999.html."]
[8.951754570007324, 5.293115615844727, "The Attitude Knowledge of the STPSat-1 Satellite is 0.03\u00ba."]
[11.256080627441406, 5.252284526824951, "The Movement of the SS 433 Cosmic Object is Wobbles on its axis - precession."]
[8.755411148071289, 10.596982955932617, "The Compression Algorithm Ratio of the Camera Imaging Device is 3.2 : 1."]
[7.004666328430176, 1.7059732675552368, "The Magnetic Waves Discovery Date of the Swarm Satellite Constellation is 23 May 2022."]
[5.031946182250977, 7.535940647125244, "The Data Rates of the STAFF/DWP Instrument is 1.024 kbit/s, or 4.627 kbit/s."]
[6.262938022613525, 3.177854061126709, "The Affiliated Organizations of the InSight Lander Lander is NASA, German Aerospace Center (DLR)."]
[7.229163646697998, 0.3756316900253296, "The Launch Date of the Mey-Lin (C6) Satellite is 15th April."]
[6.393588066101074, 7.99248743057251, "The Satellite Launch of the AMSU Microwave Radiometer is NOAA-15."]
[7.818860054016113, 8.573551177978516, "The UV Spectral Range / Bandwidth of the SOLSPEC-SOLAR Spectrometer is 165-370/1.2."]
[7.1914963722229, -0.38157182931900024, "The Beta Test of the Starlink Satellite Constellation is Ongoing."]
[9.224100112915039, 0.9404542446136475, "The Mission Life of the Telescope Optical Instrument is Commissioning in < 6 months."]
[7.248625755310059, 6.568832874298096, "The Amplifier Technology of the TEMPEST-D Satellite is High-frequency microwave."]
[7.861529350280762, 1.1499133110046387, "The Date of the Winter in the Appalachians Image is 25 February 2022."]
[7.894981861114502, 1.323323369026184, "The Date of the Flooding in Eastern Australia Image is 11 April 2022."]
[8.561476707458496, 8.01356315612793, "The Modification of the OCO-2 Instrument Optical Bench Assembly Process is Implemented."]
[8.015097618103027, 1.3842649459838867, "The First Measurements Date of the Solar Orbiter Satellite is February 17, 2020."]
[7.457404136657715, 2.958658218383789, "The Mission Status of the Solar-B / Hinode Satellite is Unknown."]
[12.124475479125977, 3.294019937515259, "The Inclination of the WV-1 Satellite is 97.2\u00b0."]
[8.57578182220459, 10.024547576904297, "The Number of Pixels of the Optics and detector assembly Assembly is 900."]
[8.346268653869629, 10.456144332885742, "The CCD Detector Light-Sensitive Areas of the DNB Spectral Band is 4."]
[7.498074531555176, 2.370255470275879, "The URL of the Mars Terrain Simulator Simulator is https://iafastro.directory/iac/proceedings/IAC-18/IAC-18/B6/3/manuscripts/IAC-18,B6,3,5,x42837.pdf."]
[13.057394027709961, 4.076436519622803, "The Number of Asteroids of the Gaia Satellite is 150,000."]
[9.027616500854492, 6.523596286773682, "The Manufacturer of the Accelerometer Sensor is Analog Devices."]
[4.258476257324219, 5.828878402709961, "The Ka-band System of the STPSat-6 Satellite is Receive up to 64 Mbit/s."]
[6.330063343048096, 1.931101679801941, "The Launch Date of the TacSat-4 Satellite is Unknown."]
[5.3100457191467285, 6.520084381103516, "The Antenna Aperture of the XPAA Phased Array Antenna is 8 x 8 array of modules."]
[1.2582306861877441, 4.149494171142578, "The Battery Capacity of the UK-DMC-2 Satellite is 15 Ah."]
[8.288039207458496, 9.180185317993164, "The Pixels per FWHM of the Spectrometer Instrument is 1340."]
[4.092117786407471, 7.262903690338135, "The Mass of the Receiver Communication Device is 200 g."]
[9.458797454833984, 5.966049671173096, "The Components of the iADCS100 Attitude Determination and Control System is ST200 star tracker, RW200-series of reaction wheels, MTQ200 series of magnetorquers."]
[6.680306434631348, 3.836984157562256, "The Purpose of the TRISHNA Satellite is Increasing understanding of ecosystem stress and water use, coastal and inland waters, urban microclimate monitoring, solid earth, the cryosphere, and the atmosphere."]
[11.66088581085205, 1.6974215507507324, "The Image Credit of the Vikram Lander Lander is NASA/Goddard/Arizona State University."]
[2.014012336730957, 7.849451065063477, "The ACE News No 165, Dec. 2, 2013 of the Weakest Solar Wind of the Space Age Solar Wind Event is URL: http://www.srl.caltech.edu/ACE/ACENews_curr.html."]
[6.606780529022217, 4.043783187866211, "The Application of the RISAT-2 Satellite is Earth observation."]
[6.996926307678223, 4.363267421722412, "The Measurement Domain of the IMAGE Satellite is Atmosphere."]
[1.7163225412368774, 5.172321319580078, "The Power Supply Voltage of the Big Apple board Electronic Board is 5 V."]
[3.623120069503784, 6.2557053565979, "The Telemetry Downlink Rate of the SGLS Link Communication System is 32 kbit/s."]
[6.072916507720947, 2.3618030548095703, "The Partnership of the LOFTID Project is NASA's Space Technology Mission Directorate and United Launch Alliance (ULA)."]
[8.578269958496094, 2.34197735786438, "The Field of Research of the Parker Solar Probe Spacecraft is Heliophysics."]
[4.929440498352051, -3.2064013481140137, "The | of the Anna MariaMassone Author is Anna MariaMassone."]
[8.070897102355957, 9.91946792602539, "The Resolution of the MI Meteorological Imager is 500 m."]
[9.253691673278809, 0.9300400614738464, "The Sampling Duration of the CREAM Cosmic-Ray Instrument is At least three years."]
[9.390341758728027, 0.48445188999176025, "The Design Lifetime of the Jason-3 Satellite is 5 years."]
[8.2756986618042, 9.217436790466309, "The Pixels per FWHM of the Spectrometer Instrument is 1420."]
[5.592805862426758, 4.439807891845703, "The Creation Technique of the Synthetic Galaxy Catalog Data is Halo Occupation Distribution technique."]
[7.313798427581787, 9.863253593444824, "The Objective of the MSS Multispectral Scanner is 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."]
[8.928450584411621, 8.114834785461426, "The Number of Scintillating Fibers of the Imaging Calorimeter Calorimeter is 448."]
[9.076749801635742, 7.589722633361816, "The Data Provided of the REPT Instrument is Energy bins, pulse heights, space weather packets, housekeeping telemetry."]
[10.823265075683594, 5.901811122894287, "The Spatial Resolution of the HXR Flare Ribbons Solar Phenomenon is ~2 arcsec."]
[7.763386249542236, 10.43565845489502, "The ADC Resolution of the SEVIRI Spectral Imager is 12 bit."]
[8.260175704956055, 4.541614532470703, "The Swath Width of the SPOT 1-5 Satellite is 60 km."]
[6.0803632736206055, 3.593843460083008, "The Managing Organization of the Solar Probe Cup (SPC) Instrument is SAO (Smithsonian Astrophysical Observatory)."]
[9.46504020690918, 7.751953601837158, "The Additional Mode of the EPI-Lo Electron Detector is Requires a Start pulse along with the SSD pulse."]
[2.238135814666748, 4.0992045402526855, "The Solar Power of the PARASOL microsatellite Satellite is 180 W."]
[8.638002395629883, 6.9256792068481445, "The Vector Components Stability of the Magnetic Field In-Situ Sensor is Better than 1 nT/year."]
[7.851625919342041, -0.5684601068496704, "The URL of the SpaceX CRS-2 Mission Mission is http://www.spacex.com/downloads/crs2-press-kit.pdf."]
[5.102419376373291, 4.294729232788086, "The Architecture of the COSMOS Software System is Provides a number of software tools to serve well defined operational roles and applications."]
[4.174808025360107, 5.717649459838867, "The Mission Data Downlink of the QSat Satellite is Ku-band, 30 Mbit/s."]
[11.276667594909668, 2.3907415866851807, "The Discovery Year of the LINEAR Project is 1999."]
[10.434101104736328, 6.165224075317383, "The Purpose of the Heat Transfer Host Experiment is Investigate convection and heat transfer through air and liquids."]
[6.178272724151611, 9.837581634521484, "The Mass of the HXT-C X-ray Optics is 13.5 kg."]
[7.02181339263916, 4.632742404937744, "The Secondary Mission Goal of the GOSAT Satellite is Thermal infrared observation."]
[9.375548362731934, 4.933298587799072, "The Angle of the Satellite Slew Satellite Maneuver is 30\u00ba."]
[10.684734344482422, -1.599193811416626, "The Cargo Delivery of the Starliner Spacecraft is 500 pounds."]
[7.680756568908691, 9.727989196777344, "The Spectral Sampling Interval of the VNIR Spectrometer Spectrometer is 6.5 nm."]
[9.84754467010498, 8.367682456970215, "The Celestial Sphere Coverage of the Telescope Optical Instrument is 100% of sphere has at least 51 contiguous days visibility."]
[3.5074806213378906, 5.770632266998291, "The Baud Rate of the Science Data Interface Interface is 1 Mbit/s."]
[6.559293270111084, 2.708911418914795, "The Conference Presentation of the SPIDER Imaging System is 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."]
[5.802103042602539, 3.473254442214966, "The Goal of the IRAS project Technology is Reduce manufacturing costs for satellites by using commercial components."]
[5.194221496582031, 2.3334434032440186, "The Launch Status of the TROPICS cubesats Satellite is Failed."]
[6.589036464691162, 3.569080114364624, "The Mission Type of the COMS Satellite is EO."]
[7.621796607971191, 1.128322720527649, "The Launch Date of the Copernicus Sentinel-6 Michael Freilich Satellite is 10 November."]
[11.671992301940918, -1.1944249868392944, "The Mass of the COSMO-SkyMed spacecraft Satellite is 1700 kg."]
[7.9770402908325195, 4.663627624511719, "The Spatial Resolution of the SeaHawk-1 CubeSat is 130 meters."]
[7.961425304412842, 5.506406307220459, "The SNR of the Spacecraft Satellite is > 100:1."]
[10.454828262329102, -1.0003025531768799, "The Mass of the CE-SAT-1 Microsatellite is 50 kg."]
[8.15951919555664, 9.029789924621582, "The Grating Frequency of the HSC Spectrometer Spectrometer is 30 lines/mm."]
[6.132837772369385, 9.69123649597168, "The Mass of the Integrated Sensor Sensor is ~ 4 g."]
[7.910329341888428, 6.8554792404174805, "The Design Hypothesis of the Geometric Calibration System Calibration System is Change across the swath can be modelled with 8th order polynomials."]
[6.519589900970459, 4.623640537261963, "The Application of the FY-3 (FengYun-3) Satellite is Atmosphere."]
[8.539945602416992, 1.2791143655776978, "The Start Time of the Quasi-Halo Orbits Orbit is 2020 August 30 00:00:00.00 dynamical barycentric time (TDB)."]
[9.233065605163574, 10.336945533752441, "The Number of CIR Photographs of the Metric Camera Camera is 546."]
[8.911810874938965, 5.290525436401367, "The Attitude Pointing Knowledge of the QuickBird-2 Satellite is \u00b10.0008o (3? steady state in all three axes)."]
[6.322165489196777, 5.023497104644775, "The Location of the SAGE-III Instrument is International Space Station's ExPRESS Logistics Carrier platform."]
[6.130525588989258, 3.160177230834961, "The Partnership of the Unicorn-1 PocketQube is European Space Agency (ESA)."]
[12.101279258728027, 2.2214503288269043, "The Mission Management of the OSIRIS-REx Spacecraft is Goddard."]
[1.4942727088928223, 4.875906944274902, "The Input Voltage of the LVPS Board Power Supply is 26 - 29 V."]
[11.700427055358887, -1.247029423713684, "The Mass of the NewSat-6 Satellite is 43.5 kg."]
[8.568313598632812, 7.90659761428833, "The SRAMs Quantity of the RADMON Radiation Monitor is 16."]
[10.387789726257324, -1.1273200511932373, "The Mass of the Delfi-n3Xt Nanosatellite is 3.5 kg."]
[5.8379082679748535, 7.5904974937438965, "The Data Availability of the ATMS Instrument is For at least 98% of all observations over an annual basis."]
[9.372804641723633, 7.868685245513916, "The Measurement Range of the Particle Detector Instrument is Tritium : 9.2 MeV/n ~ 21 MeV/n."]
[3.4197633266448975, 6.718203067779541, "The Intensity of the RFI Sources Interference is Very strong power emitters."]
[3.7309584617614746, 6.560912132263184, "The Command UHF-band of the RF communications Communication Subsystem is 1.2 kbit/s."]
[10.929695129394531, 2.6436216831207275, "The Topographic Elevation Difference of the Lander Spacecraft is 3 km to 7 km."]
[7.634212493896484, 1.0243239402770996, "The Mission End Date of the Sentinel-1B Satellite is 3 August 2022."]
[5.199497699737549, 5.988819599151611, "The Number of Antennas of the ADM Antenna Deployment Module is 2."]
[5.032238483428955, 4.59500789642334, "The Sovereignty of the Ground Segments Ground Stations is Independent."]
[10.518543243408203, 3.342301607131958, "The Link Distance of the Optical link Communication System is > 45,000 km."]
[5.778568744659424, 3.067164421081543, "The Structure Manufacturer of the Biomass Satellite is APCO Technologies in Switzerland."]
[7.340221881866455, 1.4628156423568726, "The Conference Presentation Date of the Sentinel-1 Satellite is July 22-27, 2012."]
[7.251298427581787, 0.6146610379219055, "The Reentry Date of the OrbView-3 Satellite is March 13, 2011."]
[3.7363765239715576, 4.19392204284668, "The Solar Array of the ESPA Ring Interface is Single-panel body mounted."]
[9.363895416259766, 0.8224356770515442, "The Years of Service of the Admiral Paul F. Zukunft Coast Guard Commandant is 41 years."]
[5.723600387573242, 9.1774263381958, "The Power of the Instrument General is 30 W."]
[11.576180458068848, -0.9030773639678955, "The Hydrazine Mass of the Satellite Satellite is 80 kg."]
[6.546941757202148, -0.08532673865556717, "The Launch Date of the PSLV-C38 Launch Vehicle is June 23, 2017."]
[2.3080368041992188, 4.3743767738342285, "The Power Distribution of the ALBus 3U CubeSat Satellite is 100 W."]
[6.626160144805908, -0.03863663598895073, "The Mission Date of the PSLV-21 Satellite is Sept. 4, 2012."]
[7.853670120239258, 0.5527883768081665, "The Launch Date of the Aeolus satellite Satellite is July 23, 2018."]
[3.2149293422698975, 5.506065845489502, "The Model of the SDR Host Computer Computer is Intel Core i5."]
[5.699948310852051, 9.164311408996582, "The Power of the MTQ Instrument is 1 W/unit."]
[5.87851619720459, 3.389697551727295, "The Number of Formal Cooperation Projects of the ESA and EDA Organizations is Eight."]
[6.910211563110352, 9.15567398071289, "The Volume of the Optics volume Spectrometer is 180 mm diameter x 530 mm."]
[6.463875770568848, 3.7078986167907715, "The Launch Location of the Copernicus Sentinel-6 Michael Freilich Satellite is Vandenberg Air Force Base in California."]
[5.407950401306152, 3.525629758834839, "The Technologies of the CFESat Satellite is 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."]
[5.092309951782227, 7.055771827697754, "The Diameter (mm) of the Antenna Reflector is 760."]
[4.5545172691345215, 2.2666409015655518, "The Fiber Optics Links of the MIRAS Satellite Payload is 144."]
[6.792956829071045, 3.784090995788574, "The Host for Sentinel-4 of the MTG-S Satellite is True."]
[5.961364269256592, 8.57681655883789, "The No of bands/channels of the MWHS Microwave Humidity Sounder is 5."]
[7.489731788635254, 6.152815818786621, "The Impact of the EMIT Imaging Spectrometer is Help climate scientists better understand the impact of airborne dust particles in heating and cooling the planet\u2019s atmosphere."]
[10.520808219909668, -1.0721435546875, "The Construction and Thermo-Regulation System Mass of the Microsatellite Satellite is 5.3 kg."]
[10.238972663879395, 4.940581321716309, "The Thrust of the Propulsion System Satellite Component is 0.3 N."]
[4.424540042877197, 6.701012134552002, "The Receiver Type of the LICEF Receiver is Frequency-selective."]
[4.122579574584961, 6.201096534729004, "The Protocol of the RF Communications Communication System is AX.25 or SRLL."]
[6.060164451599121, -0.034442029893398285, "The Launch Date of the Galileo satellites Satellite is 12 October 2012."]
[4.941751003265381, 1.8426231145858765, "The Number of Flights of the Foton Spacecraft is 2."]
[5.769579887390137, 5.161640644073486, "The Data Link Subsystem of the X-band SAR payload system Payload System is Included."]
[9.50946044921875, 8.920062065124512, "The Focal Length of the UVIT Telescope Telescope is ~4750 mm."]
[9.290714263916016, 3.1024997234344482, "The Orbit of the Vigilance Mission (KSF1) Satellite Cluster is 525 km Sun Synchronous orbit."]
[10.03365707397461, 5.1823906898498535, "The Force of the ESP Thrusters Maneuvering System is Provides a tangential component force on the exterior."]
[9.008272171020508, 9.204595565795898, "The Core Diameter of the Graded Index Multimode Fiber Fiber is 200 \u00b5m."]
[5.21000862121582, 3.9210236072540283, "The Configuration of the OPSIM Operational Simulator is One RTU in the loop and the other RTUs are simulated."]
[5.5968523025512695, 6.093695163726807, "The Antenna Diameter of the Satellite Satellite is 1.5 m."]
[8.895598411560059, 7.302393913269043, "The Accuracy of the Sun Sensors Sensor is ~1\u00ba."]
[7.851563930511475, 3.4398279190063477, "The Propellant Consumption Rate of the RapidEye Satellite Constellation is Lower than assumed during the design phase."]
[6.678135871887207, 4.588288307189941, "The Instruments of the Sentinel-3 Satellite is Measure oceans, land, ice and atmosphere."]
[6.634018898010254, 5.084616184234619, "The Feasibility of the Global Satnav System Satellite Navigation System is Unfeasible."]
[4.579052925109863, 2.0484423637390137, "The Total Impulse of the SkySat-7 Satellite is 317 Ns."]
[8.289721488952637, 7.559485912322998, "The Tests of the FG Calibration Device is Optical, electrical and mechanical."]
[9.635616302490234, -0.6649596691131592, "The Mission Purpose of the PACE Satellite is Establish more confident simulation models for nanosatellites and/or CubeSats of similar configuration in LEO."]
[4.174814701080322, 6.73898458480835, "The Frequency of the XBT X-band Transmitter is 8.3025 GHz."]
[5.743912696838379, 3.550431728363037, "The Developer of the CIP Instrument is Space Payload Laboratory at NCU (National Central University) of Taiwan."]
[6.891585350036621, 1.6795557737350464, "The Conference Date of the NASA Optical Communications and Sensor Demonstration Program Program is Aug. 4-9, 2018."]
[9.09365177154541, 9.705585479736328, "The Enclosure of the DarkCarb image sensor Photon Detector is Cooled Dewar."]
[5.850998401641846, 8.1372709274292, "The Frequency (GHz) of the ICI-3 Radiometer is 183.31\u00b12.0."]
[2.246107578277588, 1.7597074508666992, "The CCSDS ID of the GSAT-0101 Satellite is 3A5."]
[5.396271705627441, 5.574615001678467, "The Number of Tracked Satellites of the GPS/MET GPS Receiver is Up to eight GPS satellites."]
[6.716702938079834, 6.1277618408203125, "The Instrument of the ISS-RapidScat Scatterometer is QuikSCAT scatterometer."]
[9.481000900268555, 8.541522026062012, "The Polishing, Coating, Integration of the SiC mirrors Space Telescope Component is Unknown."]
[3.1742982864379883, 5.292606353759766, "The Storage Capacity of the CEU Solid-State Recorder is Much larger than 3 MB."]
[7.114346504211426, 5.916504859924316, "The Measurement of the OCI Ocean Color Instrument is Precise measurements of the ocean surface."]
[9.374795913696289, 7.420902729034424, "The Pressure Range of the DN probe Neutral Particle Probe is 10^-7 - 10^-2 Pa."]
[9.196447372436523, 9.088680267333984, "The FOV of the . Microdosimeter B Instrument is 32\u00ba."]
[7.23373556137085, 0.6096222996711731, "The Launch Date of the CASSIOPE Satellite is 29 Sep 2013."]
[4.769444942474365, 0.8484470248222351, "The Current Backlog of the Satellogic Satellite Imaging Company is $38 million."]
[7.786590576171875, 10.28663444519043, "The Operating Principle of the SEVIRI Imager is 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."]
[6.652684211730957, 2.225619077682495, "The Consortium Members of the Swarm Spacecraft Satellite is EADS Astrium Ltd., UK; GFZ Potsdam, Germany; DTU Space, Copenhagen, Denmark."]
[7.279815673828125, 0.31671473383903503, "The Launch Date of the PACE Satellite is January 2024."]
[4.836425304412842, 7.488414287567139, "The Telescope Diameter of the Millimeterwave receiver Receiver is 30 cm."]
[4.757154941558838, 6.088598251342773, "The Beacon Frequency of the OSSI-1 Satellite is 145 Mhz."]
[3.6852943897247314, 6.782867431640625, "The Operating Temperature of the Myriad RF board RF Board is -40\u00b0C to 85\u00b0C."]
[8.505838394165039, 7.18043851852417, "The Electric Field Measurement Range of the Plasma Wave Instrument Instrument is 0.5 Hz to 400 kHz."]
[4.352302074432373, 6.421915531158447, "The Frequency of the S-band Frequency Band is 2067 MHz."]
[5.736414432525635, 6.415374755859375, "The Spotlight Scene Resolution of the SAR Antenna Antenna is 0.5 m."]
[6.234513282775879, 3.4055898189544678, "The Headquarters Locations of the SAR Satellites Satellite is San Francisco, California; Denver, Colorado; Washington, D.C.."]
[7.0759148597717285, 0.14836271107196808, "The Launch Date of the BRO-1 Satellite is 20 August 2019."]
[11.767867088317871, -0.9174519777297974, "The Mass of the Biobox Payload is 64 kg."]
[7.2095770835876465, 4.259079933166504, "The Purpose of the Resurs-DK1 Earth Observation Satellite is Multispectral and spectrozonal mapping of the Earth's surface in the visible and near IR bands."]
[7.8188300132751465, 9.774296760559082, "The Position of the AHS Airborne Hyperspectral System is Left-hand port."]
[7.986555576324463, -0.685302734375, "The Launch Date of the Dragon Satellite is 3 April 2018."]
[1.7939714193344116, 5.388729572296143, "The Power of the Voltage 6 Modulator is 0.93."]
[1.7496657371520996, 4.812700271606445, "The Power of the EPS Electrical Power Subsystem is 0.2 W."]
[3.1627092361450195, 5.299068450927734, "The Storage Capacity of the SSR Solid State Recorder is 4 Tbit @ BOL."]
[5.583284378051758, 9.10910701751709, "The Operating Power of the Satellite Observation Instrument is 8.5 W."]
[7.736554145812988, 9.199471473693848, "The Wavelength Bands of the Hrr. chaoviatoris Microorganism is 470, 525, and 615 nm."]
[8.751422882080078, 7.851043224334717, "The Mass Range of the MIPA Ion Mass Analyzer is Optimized to cover accelerated ionospheric ions."]
[10.084756851196289, 3.0435240268707275, "The Altitude of the WorldView-3 Satellite is 617 km."]
[4.2443342208862305, 4.430419445037842, "The Data Destination of the Control Units Satellite Component is SCU."]
[6.24289083480835, 4.335254669189453, "The Primary Payload of the RADARSAT-1 Satellite is Synthetic Aperture Radar (SAR) sensor."]
[7.359291076660156, -0.21555624902248383, "The Launch Date of the H-II Transfer Vehicle \"KOUNOTORI6\" Spacecraft is Oct. 7, 2016."]
[9.253331184387207, 0.5228134989738464, "The Orbit Duration of the Jason-2 Satellite is Three years."]
[8.297225952148438, 3.5601279735565186, "The Development Status of the GCOM Satellites Satellite is Not provided."]
[4.087358474731445, 7.300570964813232, "The Mass of the CanX-2 S-band Transmitter/Transceiver is Unknown."]
[7.712491035461426, 7.245540142059326, "The Acceptable Location of the TEMPO Instrument is 80-120\u00ba W."]
[2.2174594402313232, 3.7205488681793213, "The MZ-Surface Function of the H3 and H4 Spacecraft is Location of solar cells."]
[6.111013412475586, 6.099698066711426, "The Gridding Size of the SAR Image Satellite Image is 2000 x 2000."]
[6.9950761795043945, 1.6763505935668945, "The Presentation Date of the Swarm Satellite Constellation is March 20-24, 2017."]
[8.432113647460938, 7.834413051605225, "The Cadence of the Dose Rate Measurement is 1 minute."]
[7.90436315536499, 8.38028335571289, "The Type of the ACE-FTS Instrument is Limb-scanning infrared spectrometer."]
[7.976598739624023, 1.152491807937622, "The Orbit Raise Maneuver No. 2 Completion Date of the CloudSat Satellite is 27 May, 2006."]
[7.4653449058532715, 3.2986574172973633, "The Mass Spectrometer of the Kaguya Satellite is Present."]
[6.276821136474609, 1.932530403137207, "The Deployment Date of the TacSat-4 Satellite is October 8, 2011."]
[6.635349750518799, 9.11122989654541, "The Size of the LEID Instrument is 330 mm x 150 mm x 130 mm."]
[9.216092109680176, 3.150195837020874, "The Orbit Type of the FASat-Alfa Satellite is Sun-synchronous near-circular orbit."]
[5.835610389709473, 3.486915111541748, "The Developer of the MWS, SCA, RO, MWI, ICI, 3MI Instruments is ESA."]
[10.264323234558105, 2.9404895305633545, "The Orbit Altitude of the PACE Satellite is 600-800 km."]
[4.765134334564209, 0.8560681343078613, "The Constellation Cost of the Lightspeed Satellites Satellite is $5 billion."]
[5.35515832901001, 1.3716747760772705, "The Small Satellite Deployments of the NanoRacks Company is 217th overall."]
[8.367756843566895, 0.35962116718292236, "The Diameter Increase of the BEAM Expandable Habitat is 40%."]
[11.678642272949219, -1.0935850143432617, "The Mass of the Deimos-2 Satellite is 310 kg."]
[6.662724494934082, 1.2437340021133423, "The Workshop Date of the GIOVE-A and GIOVE-B Satellites is October 13, 2008."]
[11.57331657409668, 4.405377388000488, "The Future Evolution of the Star and its Orbit Celestial Body is More circular and grow in size."]
[5.235933780670166, 4.967021942138672, "The Communication Method of the OUFTI-1 Satellite is Direct communication."]
[4.795495510101318, 0.9036773443222046, "The Funding Amount of the Pixxel Company is $25 million."]
[4.937948703765869, -3.1838104724884033, "The | of the T. Kumar Pant, R. Sridharan Authors is T. Kumar Pant, R. Sridharan."]
[7.053470611572266, 5.1801533699035645, "The Number of Parameters of the PEM (Parameterized Exospheric Model) Theoretical Model is 30 parameters."]
[8.748003005981445, 0.1584864854812622, "The Reentry Location of the Skylab-1 Space Station is Indian Ocean and parts of sparcely-populated western Australia."]
[4.725054740905762, 6.098873138427734, "The Beacon Transmission Frequency of the ELFIN-A Satellite is 437.450 MHz."]
[4.656882286071777, 4.002809047698975, "The Development Program of the HSB Hybrid Sensor Bus is ESA-ARTES program."]
[5.758101940155029, 3.6304361820220947, "The Development Partner of the Land Information System Software is NASA's Goddard Space Flight Center."]
[6.509515285491943, 1.2496200799942017, "The Full Operational Service Date of the SARah Satellite Constellation is By the end of 2019."]
[5.455133438110352, 2.1288795471191406, "The Target Audience of the MoonKAM Education and Public Outreach Program is Fifth- to eighth-grade students."]
[7.650413513183594, 8.440815925598145, "The Transmission Spectra of the Optical Depth Range Atmospheric is 0.01\u20134.5."]
[8.085975646972656, 8.971268653869629, "The GIFOV of the VIS Detector is 1 km."]
[7.33272647857666, 1.5118732452392578, "The Operation Extension Date of the Cluster Satellite Mission is June 2009."]
[8.993330001831055, 9.202264785766602, "The Bump Height of the Photon Sieve Optic is h< 8\u2205(f/D)2."]
[7.1236891746521, 7.331092834472656, "The Operational Mode of the REPT Instrument is Continuous."]
[10.345810890197754, 1.2755153179168701, "The LTAN of the Satellite PAZ is 18:00 hours."]
[11.28951358795166, 7.035433769226074, "The Collecting Area of the NICER X-ray timing instrument is > 1800 cm2."]
[9.244433403015137, 10.319705963134766, "The Field of View (Cross-track) of the MSU-100 Camera is 31\u00ba."]
[7.90155553817749, 4.522557258605957, "The Hyperspectral Instrument Resolution of the Satellogic Satellite is 30 meters."]
[11.059515953063965, 7.060431957244873, "The First Measurements of the APXS Instrument is The first X-ray and alpha spectra will be recorded."]
[5.66949462890625, 2.078068256378174, "The Integration Location of the LightSail-2 Solar Sailing CubeSat is Air Force Research Laboratory (AFRL) in Albuquerque, New Mexico."]
[1.2274552583694458, 4.16695499420166, "The Battery Capacity of the TUBSAT-N Satellite is 5 Ah."]
[6.7928466796875, 1.120142936706543, "The Conference Date of the LCROSS Satellite is April 25-30, 2010."]
[8.890861511230469, 9.91828441619873, "The Components of the FEE Front End Electronic is FPPE (Focal Plane Proximity Electronics) and VAU (Video Acquisition Unit)."]
[11.428153038024902, 2.2235803604125977, "The Capsule Drop Location of the Hayabusa-2 Spacecraft is Australian Outback."]
[7.329617977142334, 2.514504909515381, "The URL of the Cupola Window is https://web.archive.org/web/20131207132529/http://thalesaleniaspace-issmodules.com/index.php/cupola."]
[7.111896991729736, 3.8361246585845947, "The Disposal of the Monitor-E mock-up Payload is De-orbit together with Breeze into the atmosphere."]
[3.982423782348633, 5.144866466522217, "The Ionospheric Plasma Survey Hours of the DSLP Data Acquisition System is 10 thousand hours."]
[6.910157680511475, 0.42157915234565735, "The Launch Date of the MetOp-B Satellite is Sept. 17, 2012."]
[8.79786491394043, 7.363670825958252, "The Objective of the HI-SCALE Instrument is Measurement of interplanetary ions and electrons."]
[7.499088287353516, 2.330416440963745, "The URL of the ExoMars Mission is https://iafastro.directory/iac/proceedings/IAC-18/IAC-18/A3/3A/manuscripts/IAC-18,A3,3A,10,x42850.pdf."]
[7.712494373321533, 1.677297592163086, "The Event of the SMOS Satellite is SMOS Results and MIRAS Evolution Studies."]
[6.408492088317871, 6.912360668182373, "The Platform of the AltiKa Altimeter is Myriade."]
[7.845820426940918, 10.81025505065918, "The Data Quantization of the Imager Satellite Instrument is 10 bit."]
[8.692168235778809, 3.2069709300994873, "The Purpose of the GEO Geostationary Orbit is Global Positioning Systems (GPS) and communications."]
[5.927724361419678, -0.26977017521858215, "The Simulation and Materials Database of the Oculus-ASR Satellite is Improved."]
[8.285285949707031, 6.4247541427612305, "The Sensitivity of the LIGO/Virgo sensors Sensors is Improved."]
[7.848523139953613, 4.6063127517700195, "The Pixel-Binning Spatial Resolution of the EyeSat Satellite is 0.5\u00b0-2\u00b0."]
[10.962006568908691, 7.122767448425293, "The Principal Investigator of the JEM-X X-Ray Monitor is S\u00f8ren Brandt."]
[8.142922401428223, 4.66491174697876, "The Spatial Resolution of the Geodesy Levelling by GPS Satellite is 100-1000 km."]
[8.604666709899902, 8.797131538391113, "The Telescope Aperture of the SIS (Scanning Imaging Spectrograph) Spectrograph is 25 x 50 mm."]
[11.353029251098633, 3.8844211101531982, "The Oceanic Crust Thickness of the Earth Planet is About 6 to 7 kilometers."]
[3.832510471343994, 2.3019282817840576, "The Size of the RSP-00 CubeSat is 1U."]
[4.480774402618408, 2.516648054122925, "The Type of the skCube Satellite is 1U CubeSat."]
[7.693325042724609, 9.66630744934082, "The Spectral Overlap of the VNIR and SWIR bands Spectrometer is 900 nm to 1000 nm."]
[5.67629861831665, 2.780540704727173, "The Manufacturer of the Planet SkySats Satellite is Maxar Technologies."]
[7.738589286804199, 7.1962785720825195, "The Principal Investigator of the TEMPO Instrument is Kelly Chance."]
[5.136031150817871, 4.706974029541016, "The Number of Simultaneous Message Processing of the Argos Communication System is Up to four (eight in next series) messages."]
[5.419161796569824, 1.3500794172286987, "The Deployment Services of the NanoRacks LLC Company is J-SSOD (JEM-Small Satellite Orbital Deployer) of JAXA."]
[7.767922878265381, 8.416955947875977, "The URL of the SOLSPEC Spectrometer is http://www.ioccg.org/groups/Thuillier.pdf."]
[6.071902751922607, 8.036731719970703, "The Number of Channels of the ICI Instrument is 11."]
[3.62524676322937, 6.219053268432617, "The Data Rates of the CDL Common Data Link is Up to 274 Mbit/s."]
[9.427943229675293, -0.0908123031258583, "The Qualification Nanosat Quantity of the SMDC-ONE program Satellite Program is 1."]
[6.844089984893799, 0.6892416477203369, "The Launch Date of the EarthDaily Constellation Satellite Constellation is January 2024."]
[9.87479305267334, 1.3854504823684692, "The S-band Transmitter Activation Time of the Satellite Spacecraft is 30 minutes after separation."]
[8.397123336791992, 4.288756847381592, "The Accuracy Range of the GOCE Satellite is 0.002 - 0.03 m."]
[8.063836097717285, 8.680886268615723, "The Electronic Gains of the Limb Sensor Sensor is Two."]
[8.319865226745605, 1.8861935138702393, "The Service Module Commissioning Start Date of the Herschel Spacecraft is May 15, 2009."]
[6.149684429168701, 6.031713008880615, "The Viewing Acquisition of the XSAR SAR is 20 - 45\u00b0."]
[7.9474687576293945, 7.150534629821777, "The Calibration Step of the Sensor Counts to Radiance Conversion Process is May be applied for calibration."]
[5.813582897186279, 2.8645732402801514, "The Manufacturer of the BEAM Module is Bigelow Aerospace."]
[6.790262222290039, 5.296420574188232, "The Types of the Output Products Data is Ground reflectance cube, maps of the aerosol optical thickness and atmospheric water vapor, masks of land, water, haze, cloud, shadow and snow."]
[7.846157073974609, 9.406930923461914, "The Spectral Bands of the Pixxel\u2019s planned satellites Satellite is 300 including Visible to Near Infrared (VNIR) and Short Wave Infrared (SWIR)."]
[7.640771865844727, 0.9288336038589478, "The Operational Since of the PVA Photovoltaic Assembly is Late 2013."]
[9.257225036621094, 5.261363983154297, "The Reaction Wheels of the S/C Satellite is Four."]
[11.68924617767334, -1.167258381843567, "The Mass of the GRACE-FO satellites Satellite is ~600 kg."]
[2.2085928916931152, 1.7311551570892334, "The CCSDS ID of the GSAT-0211 Satellite is 26B."]
[7.693126201629639, 5.247344493865967, "The Observation Mode Switching of the OCO Satellite is Alternate 16-day global ground-track repeat cycles."]
[7.439072608947754, 8.265666007995605, "The SNR Ratio of the Instrument Satellite Instrument is Increased."]
[9.093080520629883, 8.355422019958496, "The Wavelengths of the SOHO's EIT Extreme-ultraviolet Imaging Telescope is 171 \u00c5, 195 \u00c5, 284 \u00c5 and 304 \u00c5."]
[1.6356606483459473, 4.6036248207092285, "The Manufacturer of the EPS Electrical Power Subsystem is Tiger Innovations."]
[5.06380558013916, 4.442789554595947, "The Function of the Ground Software Data Processing is Make finding charts with source lists."]
[5.39906120300293, 2.776310443878174, "The Platform of the ExoplanetSat Satellite is CubeSat."]
[6.594432353973389, 4.800030708312988, "The Imaging Frequency Band of the TecSAR Satellite is X."]
[7.920357704162598, 10.060811996459961, "The VNIR Spatial Resolution of the iSIM-90 Imager is 1.65 m."]
[8.509567260742188, 2.198073625564575, "The Renamed Name of the Solar Probe Plus Spacecraft is Parker Solar Probe."]
[8.191884994506836, 9.74649429321289, "The Design of the NAOMI Imaging Instrument is High-resolution pushbroom imager."]
[6.956273078918457, 8.633427619934082, "The Resolution (VIS) of the VHRR Very High-Resolution Radiometer is 2.75 km."]
[6.029979228973389, 2.942619562149048, "The Designer/Developer of the PROBA Satellite is Verhaert Design and Development N. V.."]
[7.08488655090332, 4.4033002853393555, "The Measurement Domain of the OSCAR-QUBE Satellite is Gravity and Magnetic Fields."]
[6.1967010498046875, 4.640702724456787, "The On-board Receivers of the Sentinel-3 Satellite is Two GPS Receivers, LRR, DORIS."]
[8.05787181854248, 0.30055859684944153, "The Installation Date of the ISS-RapidScat Satellite Instrument is October 6, 2014."]
[11.439424514770508, 6.016576766967773, "The Return to Science Operations Date of the Chandra X-ray Observatory X-ray Observatory is 24 October 2018."]
[6.944712162017822, 1.1460474729537964, "The Conference Date of the Dellingr Satellite is Aug. 5-10, 2017."]
[7.27736234664917, 10.06588077545166, "The Mission Regions of Interest of the HyperScout\u00ae Satellite is Identified by the consortium partners."]
[6.413663387298584, 3.7763211727142334, "The Purpose of the HawkEye 360 Satellite Constellation is Deliver RF data and analytics to the agency and combatant commands."]
[11.786243438720703, -1.191599726676941, "The Payload Mass of the Resurs-DK1 Spacecraft is 1200 kg."]
[8.96308708190918, 4.544805526733398, "The Structure of the S/C Satellite is Box-shaped three-axis bus."]
[8.62279224395752, 1.904664158821106, "The Expected Coolant Exhaustion of the Herschel Space Observatory is March 2013."]
[7.558902263641357, 3.234011650085449, "The Tracking Organization of the Debris Satellite Components is U.S. Air Force's 18th Space Control Squadron."]
[5.0227203369140625, 3.0427284240722656, "The Purpose 1 of the PW-Sat CubeSat is System test of a flexible solar generation system."]
[5.086005210876465, 4.637661457061768, "The Downlink Verification Method of the Ground System Satellite Ground System is Playing back the recorded signal to the flight unit or an engineering unit and verifying the uplinked commands."]
[5.950901508331299, 1.5512131452560425, "The Access of the HTV Spacecraft is ISS crew will be able to enter and remove the supplies."]
[7.913115501403809, 6.720122337341309, "The Design Hypothesis of the Geometric Calibration System Calibration System is Seasonal change can be sufficiently modelled for a pair of months with a 1st order polynomial against sun \u03b2 angle."]
[8.094749450683594, 8.778813362121582, "The | of the Miniature Integrated Camera Spectrometer (MICAS) Spectrometer is Miniature Integrated Camera Spectrometer (MICAS)."]
[10.432138442993164, 8.379007339477539, "The Components of the Coronagraph Instrument Instrument is Optical Bench Assembly (CGI-OBA) and the Tertiary Collimator Assembly (TCA)."]
[9.16327953338623, 5.40407133102417, "The Torque Type of the Attitude Control System Satellite System is Attitude control torque."]
[11.856368064880371, 2.392477512359619, "The Flyby Distance of the OSIRIS-REx Spacecraft is 2.1 miles (3.5 km)."]
[10.367323875427246, 5.263453006744385, "The Quantity of the XTA Xenon Tank Assembly is 2."]
[3.520794153213501, 4.664411544799805, "The Processor Speed of the MPM Main Processor Module is 50 MHz."]
[5.035895347595215, -2.374629259109497, "The Affiliation of the Andreas Jung Engineer is Unknown."]
[8.610132217407227, 1.7578011751174927, "The Data Archive Location of the Spitzer Space Telescope Telescope is Infrared Science Archive at IPAC at Caltech in Pasadena, California."]
[9.659697532653809, 9.008010864257812, "The Focal Length of the Primary Mirror Telescope Component is 120 mm."]
[8.724014282226562, 7.26536750793457, "The Range of the Rate sensor Sensor is \u00b185\u00ba/s."]
[6.656789779663086, 5.3699846267700195, "The Instrument of the SMAP satellite Satellite is Radar and radiometer."]
[4.764270782470703, 1.9683103561401367, "The Number of Sensors of the SloshSat Satellite is 270."]
[8.179093360900879, 9.935247421264648, "The Temporal Resolution of the MSASI Imager is 2 ms."]
[11.613924980163574, 0.7534265518188477, "The Weight of the Chang'e-5 Spacecraft is 8.2 tons."]
[7.325188159942627, 0.5740001797676086, "The Launch Date of the Hugo Satellite is Later this year."]
[4.61474084854126, 5.828014850616455, "The Supported Navigation Signals of the Signal Generator Subsystem Signal Generation System is E5, E6, and L1-bands."]
[7.134590148925781, 6.887813568115234, "The International Astronautical Congress Date of the 3MI Instrument is 25-29 Sept. 2017."]
[7.974918365478516, 9.651394844055176, "The Wavelengths of the Mid-IR Imagers Camera is 7 and 12.3 \u00b5m."]
[10.288936614990234, 4.828651428222656, "The Presentation Date of the A Stable Liquid Mono-Propellant based on ADN Propellant is May 11-14, 2009."]
[11.616617202758789, 6.235388278961182, "The First Observation of the XMM-Newton X-ray Observatory is June 1962."]
[9.722875595092773, 6.952247619628906, "The Diameter of the Heat Shield Parker Solar Probe Component is 8 feet (2.44 m)."]
[11.769792556762695, 1.6789554357528687, "The Main Rotation Period of the Philae Lander is 24 seconds."]
[7.310879230499268, 0.8451561331748962, "The Launch Year of the ALOS-1 Satellite is 2006."]
[9.490200996398926, 7.802036762237549, "The Directional and Omni-directional Measurements of the MEPED Particle Detector is Available."]
[8.192620277404785, 10.551387786865234, "The Video Data Output Frequency of the MS Detectors Detectors is 58 Mpixel/s."]
[5.306827545166016, 7.228055000305176, "The Beam width of the W-band Band is 20 mrad."]
[7.079530239105225, 0.17523688077926636, "The End of Life Date of the Genesis Satellite is September 8, 2004."]
[9.362507820129395, 8.626473426818848, "The Telescope Assembly of the SPEXone Spectrometer is Three-mirror segmented telescope assembly."]
[7.012365341186523, 4.978849411010742, "The Mission Focus of the Aqua Satellite is Multidisciplinary study of the Earth's water cycle."]
[5.250321865081787, 4.506285190582275, "The Regional Components of the DBNet Data Collection Network is 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."]
[3.700529098510742, 6.277817249298096, "The Downlink Data Rate of the TT&C S-band Communications Communication System is 722.116 kbit/s."]
[7.089044570922852, 0.08881574124097824, "The End of Life Date of the SPOT-5 Satellite is 30 Mar 2015."]
[6.91662073135376, 4.692393779754639, "The Instrument Type of the GOSAT Satellite is Imaging multi-spectral radiometers (vis/IR), Atmospheric chemistry."]
[5.622036457061768, 3.4004881381988525, "The Operation Status of the AprizeSat-3 and AprizeSat-4 Satellites is Nominal."]
[6.750269412994385, 3.769935131072998, "The URL of the Sentinel-1 Satellite is http://earth.eo.esa.int/workshops/fringe09/participants/1197/pres_1197_Rosich.pdf."]
[11.657405853271484, -1.0858538150787354, "The Mass of the Total Payload Satellite is < 100 kg."]
[7.723601341247559, 3.293928384780884, "The Oversight of the Characterization Process Satellite Debris Analysis is Human oversight to ensure the integrity of the data."]
[6.872552394866943, 0.5909126400947571, "The Bulletin Date of the GEOS-1 Satellite is Feb. 2004."]
[10.41429615020752, 4.28663444519043, "The RAAN Accuracy of the Bloostar Launch Vehicle is \u00b10.05\u00ba."]
[8.18004322052002, 10.263279914855957, "The Spectral Range of the TAC Camera is 500 - 800 nm."]
[9.555883407592773, 8.719273567199707, "The Components of the Electro-optical assembly Assembly is Off-axis TMA (Three Mirror Anastigmat) optical telescope unit, focal plane assembly, baffle."]
[5.9923415184021, 9.568951606750488, "The Mass of the CU Cabling Unit is 5 kg."]
[7.876671314239502, 1.1570062637329102, "The Image Date of the Copernicus Sentinel-5P Satellite is 2 July 2018."]
[6.456088066101074, 5.495831489562988, "The Daily Radio Occultation Profiles of the Spire Satellite Operator is 5,000."]
[6.247009754180908, 7.350658893585205, "The Pair Orientation of the DBCP Dual Babinet Compensator Pseudo-depolarizer is 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."]
[11.463628768920898, 2.193204641342163, "The Impact Date of the Hayabusa-2 Spacecraft is 30 October 2020."]
[11.51815414428711, 2.143389940261841, "The Sampler Room A Close Command Date of the Hayabusa-2 Spacecraft is February 22, 2:20 UT."]
[11.108271598815918, 2.4464547634124756, "The Operation Duration of the Schiaparelli Lander is Few days."]
[9.201313018798828, 0.7693139314651489, "The On-Orbit Geometric Calibration of the Landsat-7 Satellite is Four Years."]
[8.055546760559082, 7.0186543464660645, "The Function of the Machine Learning Algorithm Calibration Tool is Recognize a solar flare and determine how much degradation is affecting AIA's current images and how much calibration is needed."]
[6.143650054931641, 3.506213426589966, "The GPS Receivers of the NigeriaSat-2 Satellite is 2 SGR-10 (Space GPS Receiver-10) units."]
[3.3970589637756348, 6.556971549987793, "The EIRP of the Isolated Spot Beams Communication System is 65 dBW."]
[8.55508804321289, 10.231837272644043, "The Detector of the DubaiSat-2 Satellite is TDI CCD detectors."]
[8.863018035888672, 10.751753807067871, "The Spatial Resolution of the CCD Camera Imaging System is 1 km x 1 km."]
[9.054012298583984, 2.403470277786255, "The Observation Results of the Herschel Space Observatory is Filaments in nearby star-forming clouds seem to be roughly all the same width \u2013 about a third of a light-year."]
[4.782271385192871, 0.8812840580940247, "The Cost Savings of the Satellogic Satellite Imaging Company is 100 times cheaper than competitors."]
[10.26665210723877, 4.960077285766602, "The Thruster Type of the Starlink Satellite Satellite is Hall thrusters powered by krypton."]
[6.693921089172363, 2.978492498397827, "The Onboard Computer of the PhoneSat 2 Satellite is Samsung Nexus S phone."]
[8.580299377441406, 8.248702049255371, "The View of the SWIR/MWIR/TIR Calibration is Blackbody."]
[12.11060905456543, 2.192777633666992, "The NASA's upcoming asteroid sample return mission of the Rosetta spacecraft Spacecraft is OSIRIS-REx."]
[11.322516441345215, 2.5488736629486084, "The Height of the Prometheus Volcano Plume Volcanic Plume is 60 km (40 miles)."]
[7.831153392791748, 8.552482604980469, "The UV Spectral Range / Bandwidth of the SOLSPEC-ATLAS Spectrometer is 210-370/1.2/0.4."]
[12.11978530883789, 3.2819697856903076, "The Inclination of the Satellite Orbit is 98\u00ba."]
[3.4043657779693604, 5.2927165031433105, "The Data Storage of the NSat Satellite is 2 GB SD card."]
[5.702963829040527, 2.999627113342285, "The Manufacturer of the SIMBA Satellite is Royal Meteorological Institute Belgium."]
[9.11783504486084, 7.598729610443115, "The Quantity of Cylindrical Electrostatic Deflection Analyzers of the VEIS Vector Electron Ion Spectrometers is 6."]
[10.462692260742188, 4.679013729095459, "The Duration Pulses of the LM thruster Thruster is Up to 8.0 sec."]
[7.743875980377197, 6.948761940002441, "The Data Transmission Frequency of the HRC Instrument Camera is At least once per orbit, or every 90 minutes."]
[1.3339288234710693, 4.226106643676758, "The Battery Power Duration of the IXV Spacecraft is 1h 43 min."]
[7.946451663970947, 5.214223861694336, "The Receiver Sensitivity of the Galileo Satellite is Millions of times weaker than the ones received on Earth."]
[7.078785419464111, 1.1873360872268677, "The Workshop Date of the MTG Mission Team (MMT) Team is Dec.3-5, 2007."]
[10.09609603881836, 9.65699291229248, "The Objective of the IRIS Imager Camera is Provide multispectral imagery in the visible and near-infrared wavelength range."]
[7.556186676025391, 1.1624037027359009, "The Scheduled Launch Date of the Sentinel-6 Michael Freilich Ocean Science Satellite is Nov. 10."]
[10.494821548461914, 8.218993186950684, "The Presentation Date of the Next-Generation Formation Flying Solar Coronagraph Solar Coronagraph is May 27-28, 2014."]
[7.769536972045898, 10.774991989135742, "The Resolution of the A/D converter Data Converter is 5 bit."]
[8.421036720275879, 10.107181549072266, "The Central Wavelength of the Current GOES imager Sensor is 7.34."]
[8.130781173706055, 4.675410747528076, "The Spatial Resolution of the Solid Earth Sedimentary basins Satellite is 20-100 km."]
[9.2251615524292, 4.168467998504639, "The Dimensions of the LLITED Spacecraft is Approximately 100 x 100 x 170 mm."]
[10.641756057739258, 9.177267074584961, "The Image Capture Date of the CaSSIS Instrument is 15 January 2019."]
[7.394740104675293, 1.47850501537323, "The Operation Stop Date of the ERB Radiometer is Jan. 4, 1994."]
[6.054853916168213, -0.023173877969384193, "The Contract Award Date of the Galileo Satellite System is January 7, 2010."]
[9.437935829162598, 5.67108678817749, "The Processor of the AOCS Attitude and Orbit Control Subsystem is MIL-STD 31750."]
[6.602817058563232, 5.572132110595703, "The L-band Radiometer Frequency of the SMAP Satellite is 1.4 GHz."]
[8.672309875488281, 8.038816452026367, "The Dose Measurement Range of the DDM Instrument Dosimetry System is Rad to Mrad."]
[7.292356014251709, 1.660032868385315, "The OceanObs'09 Presentation Date of the SWOT Satellite is Sept. 21-25, 2009."]
[9.306499481201172, 1.7755544185638428, "The Plan Generation of the MPF System is Daily."]
[6.121427536010742, 4.416208267211914, "The Length of the ERA Robotic Arm is Over 11 m."]
[7.258045673370361, 7.930375576019287, "The Earth Surface Area Observed of the MOMS-2P Instrument is 65 million km 2."]
[10.18456745147705, 1.3737396001815796, "The Ascending Node Time of the Odin Satellite is 18:00 hrs."]
[9.188636779785156, 10.336258888244629, "The Image Interval of the DECA Descent Camera is 1.5 s."]
[10.562658309936523, 7.531702041625977, "The Primary Structure of the Terra Satellite is Truss-like structure built of graphite-epoxy tubular members."]
[6.031740665435791, 2.1385293006896973, "The Launch Locations of the OneWeb Satellite Constellation is Baikonur Cosmodrome in Kazakhstan, and Vostochny Cosmodrome in Russia."]
[7.822935104370117, 5.222594738006592, "The Mission of the RSP-00 CubeSat is Demonstrate technology aimed at electron density measurement and three-dimensional mapping of ionosphere and chip scale (ultra-small) atomic clock for CubeSats."]
[5.937125205993652, 3.055243968963623, "The Manufacturer of the GFO Satellite is Unknown."]
[7.734386444091797, 9.08616828918457, "The Parameter of the Channels Spectrometer is Value."]
[3.813063144683838, 6.252344131469727, "The Bandwidth of the RF Ground Network Ground Network is 500 kbit/s."]
[3.905635356903076, 2.29298734664917, "The Spacecraft Volume (Before Inflatable and Sail Deployment) of the Spacecraft 3U CubeSat is 34 cm x 10 cm x 10 cm."]
[6.907438278198242, 5.360867977142334, "The Interferometric Radiometer of the SMOS Satellite is L-band."]
[6.650846481323242, 0.599417507648468, "The Launch Date of the TUBSAT Satellite is 17 July 1991."]
[9.432621002197266, 7.900782585144043, "The Range of the LET Range Parameter is 0.2 - 7 MeV/\u00b5m."]
[7.357442378997803, 1.3696048259735107, "The Presentation Date of the Sentinel-1 Satellite is Nov. 30-Dec. 4, 2009."]
[10.372038841247559, 5.704112529754639, "The Developer of the SEDS Tether Experiment Demonstration Program is NASA/MSFC and Tether Applications Co. of San Diego."]
[7.650864124298096, 4.896238327026367, "The Development Team of the BEESAT-3 Satellite is Merlin F. Barschke, Frank Baumann, Klaus Briess, Christian Nitzschke."]
[7.032956123352051, 3.962662696838379, "The Payload of the STACEM Satellite is Miniaturized multi-spectral payload for the acquisition of imagery in the visible and near infrared wavelengths and hyperspectral channels."]
[10.555914878845215, -1.0713272094726562, "The Transmitter/Receiver and the Buffer Store Mass of the Microsatellite Satellite is 12.5 kg."]
[6.539915561676025, 7.771187782287598, "The Output Power of the InnoSlab amplifier Laser Amplifier is Scalable."]
[7.908266067504883, 9.556449890136719, "The Number of Pixels of the Band 3 Spectral Band is 1600."]
[7.75443172454834, 3.063694953918457, "The Number of ERS SAR Pairs of Data of the ERS Tandem Mission Satellite Mission is About 110,000."]
[7.830946922302246, 0.622218906879425, "The On-Station Time of the DSCOVR Spacecraft is 110 days."]
[9.767237663269043, 8.672110557556152, "The Design of the Telescope Telescope is Cassegrain design."]
[12.08987808227539, 3.2980597019195557, "The Inclination of the ICEYE-X14 and ICEYE-X16 Satellites is 97.4\u00ba."]
[5.239932537078857, 4.255187034606934, "The Components of the JUICE Science Ground Segment (SGS) Ground Segment is Science Operation Center (SOC) and the PI instrument teams."]
[4.208536148071289, 3.8694264888763428, "The Doppler Shift of the AIS System Communication System is - 4 kHz to + 4 kHz."]
[11.209293365478516, 1.0101540088653564, "The Expected Mars Orbit Entry Date of the Tianwen-1 Mars Mission is February 10."]
[8.392404556274414, 7.907668113708496, "The URL of the JWST Fine Guidance Sensor Sensor is http://www.stsci.edu/jwst/instruments/fgs."]
[7.300492763519287, 2.487664222717285, "The URL of Paper of the RISESAT Satellite is http://tinyurl.com/q5hq42e."]
[8.434163093566895, 10.351805686950684, "The CCD Pixel Measurements of the Nadir Sensor Wide-Field Telescope Sensor is Summed into 35 bins."]
[9.076894760131836, 10.678312301635742, "The Spatial Resolution of the TAC Camera is 3.5 m."]
[6.95517635345459, 0.8556332588195801, "The Launch Date of the LambdaSat Satellite is Unknown."]
[5.081486701965332, 7.132503509521484, "The Pixel Size (km x km) of the Antenna Reflector is 8."]
[5.849836826324463, 6.8940935134887695, "The Accuracy of Cloud Echoes of the CPR Millimeter-Wave Radar is 1 m/s."]
[7.020350933074951, 4.755738735198975, "The Mission of the NIRS Instrument is RAIDS (Remote Atmospheric and Ionospheric Detection System)."]
[10.213883399963379, 2.8650972843170166, "The Altitude of the FormoSat-3/COSMIC-1 Satellite Constellation is 800 km."]
[5.400884628295898, 3.9625446796417236, "The Deployment of the Sunshield Satellite Component is Folded against the payload module during launch, deployed around the fixed solar array after separation from the launch vehicle."]
[1.8800243139266968, 4.010104179382324, "The Number of Panels of the Solar Array Power Source is 8."]
[12.625039100646973, 6.917423725128174, "The Pulse period (ms) of the B0531+21 (Crab) Pulsar is 33.085."]
[6.021177768707275, 2.2353320121765137, "The Number of Sensors and Systems of the SSA Space Situational Awareness System is 375."]
[6.025867938995361, 6.8869524002075195, "The Location Technique of the PTT-HD or PMT-HD High Data-rate Transmitters is Not designed to be autonomously located by Doppler technique."]
[11.739547729492188, -1.1336840391159058, "The Mass of the DeMi Satellite is 2.5 kg."]
[6.875730991363525, 0.5626792907714844, "The Commercial Operation Start Date of the Hiber Satellite Network is Q1 2019."]
[5.569394588470459, 3.1493241786956787, "The Platform of the BRITE Satellites Satellite is GNB (Generic Nanosatellite Bus)."]
[7.880574703216553, 7.082597732543945, "The Signal Assessment Modes of the Hertz Facility is Local \u2018near-field' or as if the signal has crossed thousands of kilometers of space."]
[8.469367027282715, 1.9364612102508545, "The Observation Date of the Herschel Telescope is 24 September 2018."]
[5.379098892211914, 5.689428329467773, "The Fix Frequency of the Novatel OEMV-1 GPS receiver GPS Receiver is Approximately once every 25 hours."]
[11.38125991821289, 6.659442901611328, "The Solar Array Status of the IXPE observatory X-ray Observatory is Not delivered."]
[3.9353392124176025, 6.6525163650512695, "The Technology of the LRO Mini-RF Transmitter Transmitter is MPM combines a solid state RF driver/preamplifier with a traveling wave tube amplifier."]
[6.951268672943115, 4.6179518699646, "The Instrument Type of the IMAGE Satellite is Atmospheric chemistry, Communications, Data collection."]
[8.716544151306152, 4.270179748535156, "The Telescope FOV of the BRITE Satellite is 24\u00ba diameter."]
[5.584489822387695, 3.8628106117248535, "The Tracking and Cataloging of the CSpOC Space Operations Center is Immediate."]
[5.501588821411133, 6.514647483825684, "The Antenna Angle of the SWOT Satellite is \u00b1 60\u00ba."]
[7.643052101135254, 3.9786555767059326, "The Observation Data of the CryoSat-2 Satellite is Changes in ice thickness for October/November 2011, 2012 and 2013."]
[8.433959007263184, 8.960177421569824, "The Type of the NIR Camera Camera is Near Infrared."]
[4.116413116455078, 5.710416793823242, "The VHF-band FSK Channels of the UoSAT-12 Satellite is 3."]
[10.288294792175293, 2.898719549179077, "The Orbit Altitude of the A-Train Satellite Constellation is Approximately 705 km."]
[7.8971076011657715, 9.961917877197266, "The Bands of the CAVIS Imager is 7 VNIR + 5 SWIR."]
[5.952382564544678, 3.261420965194702, "The IoT Services of the Astrocast Satellite Manufacturer is Track, measure, manage, communicate and control IoT assets."]
[6.736429691314697, 6.451016426086426, "The Path Length Ratio of the SST Retrieval Algorithm Algorithm is 1.54."]
[7.316424369812012, 0.2236405313014984, "The Launch Date of the HY-1B Satellite is October 4, 2007."]
[5.405099868774414, 5.4686279296875, "The Acquisition Mode of the TDX and TSX Satellites Satellites is Dual Receive Antenna configuration."]
[10.345973014831543, 3.0028858184814453, "The Orbit Altitude of the Envisat Satellite is ~783 km."]
[7.794050693511963, 3.9287631511688232, "The Imaging Capacity of the RapidEye Satellite Constellation is 5 million km2 per day."]
[8.302423477172852, 2.3139922618865967, "The URL of the Parker Solar Probe Satellite is https://blogs.nasa.gov/parkersolarprobe/2021/11/10/space-dust-presents-opportunities-challenges-as-parker-solar-probe-speeds-back-toward-the-sun/."]
[7.447545528411865, -0.2391800433397293, "The Launch Date of the Minotaur-C rocket Rocket is Nov. 1, 2017."]
[5.067240238189697, 5.430044651031494, "The Antenna Mast Height of the ASAL Ground Station Ground Station is 10 m."]
[9.175780296325684, 6.118783473968506, "The Total Mass of the CMGs Attitude Control is 261.6 kg."]
[3.9909982681274414, 6.51811408996582, "The Modulation of the X-band Transmitter Transmitter is BPSK or QPSK."]
[9.468131065368652, 0.9408858418464661, "The Deorbiting Time of the IDEAS Deorbiting System is Within about 25 years."]
[6.541799545288086, 3.890220880508423, "The Mission Scientist of the Sentinel-6 Satellite is Craig Donlon."]
[10.828940391540527, 4.225665092468262, "The Observation Targets of the Twinkle Spaceborne Telescope is Astrophysical objects (e.g. exoplanets, solar system bodies, stars, disks)."]
[5.856700897216797, 7.593358516693115, "The Team Size of the ATMS Instrument is 100 people."]
[8.770752906799316, 10.366368293762207, "The Resolution of the GOCI-II CMOS Imaging Sensor CMOS Imaging Sensor is 2720 rows by 2718 columns."]
[8.18651294708252, 7.586113929748535, "The Interval of the Observation and Calibration Process is 1.8s."]
[5.109719276428223, 6.061336517333984, "The Frequency Range of the ISEE-3 Satellite is 0.3 Hz to 100 kHz."]
[7.568172454833984, 7.062595844268799, "The Utilized Atmospheric Emissions of the MATS Satellite Instrument is O2 Atmospheric Band airglow and scattering of sunlight by NLC."]
[8.193750381469727, 1.5486606359481812, "The Mission Extension Approval Date of the Kepler Satellite is April 4, 2012."]
[10.49091911315918, 7.600290298461914, "The Material of the Wire Component is Teflon-coated 29 gauge copper-stranded wire."]
[6.699426651000977, 0.8670108914375305, "The Contract Signing Date of the FormoSat-5 Satellite is June 17, 2010."]
[11.021076202392578, 4.252114295959473, "The Atmospheric Phenomenon of the Planets with One Side Permanently Facing Their Star Exoplanets is Clouds of different compositions might be visible, depending on the side observed."]
[9.340269088745117, 4.957611083984375, "The Required Spacecraft Orientation for Stability of the Kepler Space Telescope Space Telescope is Nearly parallel to its orbital path around the sun."]
[5.727073669433594, 6.918377876281738, "The Impulse Peak Power of the X-band Radar is 100 kW."]
[6.950442314147949, 0.40184035897254944, "The Presentation Date of the Delfi-n3Xt Satellite is June 3-5, 2013."]
[6.366459846496582, 5.887661457061768, "The SAR Measurements Spatial Resolution of the L2SMA Soil Moisture Product is About 3 km."]
[9.20652961730957, 0.8648723363876343, "The Operation Duration of the Experiments Payload is 1 year to 3 years."]
[6.685136318206787, 9.138786315917969, "The Size of the GeoCarb Instrument is 1.3 m x 1.14 m x 1.3 m."]
[13.165512084960938, 3.984787940979004, "The Date of the GAUSS Satellite Launch Satellite Launch is Nov. 21, 2013."]
[6.121072769165039, 0.5868517756462097, "The Release Date of the CubeSat Satellite is February 19."]
[8.013240814208984, 9.648750305175781, "The Spectrum of the FCI Optical Imager is Visible, near-infrared and infrared."]
[6.8546342849731445, -0.03932454064488411, "The Third Flight Date of the MEPSI Satellite is Nov. 24 to Dec. 7, 2002."]
[7.631163120269775, 0.9936286807060242, "The Launch Date of the Sentinel-5P Satellite is 13 October 2017."]
[8.969236373901367, 3.278071165084839, "The Applicable Orbits of the AutoConTM Technology is Variety of orbits ranging from LEO to non-Keplerian trajectories such as libration orbits."]
[9.963533401489258, 2.807137966156006, "The Data Collection Altitude of the RainCube Satellite is About 310 km."]
[8.848030090332031, 7.163936614990234, "The Accuracy of the SSAS Sensor is 0.1\u00ba to 1\u00ba."]
[10.638163566589355, 2.744205951690674, "The Orbit Altitude of the GomX-4B Satellite is 500 km."]
[7.2875518798828125, 4.498986721038818, "The Band 7 of the Landsat TM Satellite is Hydrothermal mapping, geology."]
[3.577162027359009, 6.225649356842041, "The Data Downlink Rate of the TDRSS Communication System is 20 kbit/s."]
[10.164363861083984, 4.87681770324707, "The Propulsion of the Hisea-1 Satellite is ThrustMe iodine electric propulsion."]
[10.363591194152832, 5.309439659118652, "The Thrust of the T3\u00b5PS Micropropulsion System is Up to 6 mN."]
[10.48166275024414, -1.1235401630401611, "The Mass of the Nanosatellites Satellite is < 10 kg."]
[2.210416078567505, 6.520287990570068, "The Latency of the ATL06 Land Ice Height Data is 45 days."]
[11.1265230178833, 5.132819175720215, "The Mission End Date of the LISA Pathfinder Spacecraft is 25 June 2016."]
[11.29082202911377, 6.8337321281433105, "The Number of Pointed Proportional Counters of the IXAE X-ray Astronomy Experiment is 3."]
[9.081157684326172, 9.327486038208008, "The FOV (Field of View) of the Instrument Sensor is 80\u00ba x 80\u00ba."]
[4.923441410064697, 6.605700492858887, "The Parameter Derivation of the Antenna Unknown is Ta = Tref - \u03b7 Tn."]
[12.076666831970215, 3.2755050659179688, "The Orbit Inclination of the DubaiSat-2 Satellite is 97.8\u00ba."]
[5.9235639572143555, 6.814630508422852, "The Azimuth Dwell Time of the Radar Instrument is 42 ms."]
[9.491523742675781, 3.5241024494171143, "The Mission Accomplished Date of the CanX-4 & CanX-5 Satellites is Nov. 5, 2014."]
[8.240355491638184, 5.07768440246582, "The Location Accuracy of the SPOT-6 Satellite is 11.9 m CE90 @30\u00ba."]
[5.249794960021973, 3.231053590774536, "The Platform Type of the Satellite Vu Satellite is DarkCarb satellite bus."]
[9.206733703613281, 5.553254127502441, "The Control Method of the Attitude Control System Satellite System is Solar radiation pressure, Optical parameters control."]
[5.413830757141113, 4.552278518676758, "The Locations and Operators of the Sentinel-1 PDGS centers Ground Segment is 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 th."]
[9.199406623840332, 6.146029472351074, "The Mass of the Gyro Unit Attitude Control is 1.5 kg."]
[9.303168296813965, 5.313654899597168, "The Quantity of Reaction Wheels of the Earth Observation Compartment Compartment is 3."]
[11.593473434448242, 4.453202724456787, "The Size Comparison to Sun of the HD 93396 Star is Three times larger."]
[6.752218246459961, 4.274207592010498, "The Payload of the VisionCube-1 Satellite is Multi-anode photon multiplier tube(MaPMT), a camera, and a real-time image processing engine."]
[6.742798328399658, 5.188355445861816, "The Purpose of the Advanced Satellite Navigation Receiver Receiver is Perform the first ever satnav positioning fix in lunar orbit."]
[6.802681922912598, 1.332882046699524, "The Workshop Date of the GIOVE-B Satellite is October 13, 2008."]
[5.98652982711792, 5.4618988037109375, "The Components of the XSAR Instrument is 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)."]
[8.055730819702148, 0.7139499187469482, "The Congress Date of the Megha-Tropiques Satellite Mission is Sept. 29 to Oct. 3, 2008."]
[11.744351387023926, 1.1867491006851196, "The Panorama Camera (PCAM) of the Chang\u2019e-4 Rover Rover is Payload."]
[6.549772262573242, 3.5719189643859863, "The Manufacturer of the Sich-2 Satellite is Yuzhnoye SDO."]
[8.972691535949707, 10.81187915802002, "The Swath Width of the HSC CCD Imaging Camera is 700 km."]
[8.210636138916016, 10.484984397888184, "The Data Output of the TDI Detector Detector is 290 Mpixel/s total."]
[7.583177089691162, 1.5829821825027466, "The Presentation Date of the PROCYON Deep Space Probe is August 6-11, 2016."]
[7.108569622039795, 6.191246032714844, "The Instrument Type of the OCI Instrument is Ocean colour instruments."]
[7.346183776855469, 0.6775950193405151, "The Launch Date of the Beresheet Spacecraft is Mid-February."]
[7.848774433135986, 10.802790641784668, "The Pixel Quantization of the Telescope Optical Instrument is 12 bit plus 1 bit for low and high gain setting."]
[7.924004077911377, 9.083355903625488, "The Wavelength/Passband of the Instrument Spectrometer is 135.6; 155 nm."]
[4.773101806640625, 5.582221984863281, "The G/T of the Reception Station Ground Station is 22.7 dB/K."]
[6.7474684715271, 7.5874152183532715, "The Phototransistor Sensitive Area Diameter of the DIAL Instrument LIDAR is 200 \u00b5m."]
[7.357362270355225, 2.7647063732147217, "The Mission Status of the Gravity Probe B Satellite is Unknown."]
[9.852692604064941, 6.602489471435547, "The Thermistor Telemetry Data of the Satellite Spacecraft is Stable."]
[5.83062744140625, 2.4785995483398438, "The Acquisition Date of the Maxar Technologies Company is June 24, 2020."]
[6.612485408782959, 1.1775212287902832, "The Conference Date of the TBIRD Program Data Transfer System is August 3-8, 2019."]
[9.580221176147461, 6.619355201721191, "The Electrical Power Transfer Method of the Hinge Mechanical Component is Conducting electricity through the superelastic springs."]
[3.407228708267212, 5.684498310089111, "The Test Number of the File Transfer Test Communication is 1, 2, 3."]
[8.8616361618042, 8.475310325622559, "The TFOV of the Scan mechanism assembly Assembly is \u00b113\u00ba in the E-W and \u00b110\u00ba in the N-S direction."]
[7.241634845733643, 1.5298738479614258, "The Date of the Dnepr Cluster Mission 2013 Satellite Cluster Mission is Nov. 21, 2013."]
[5.747617721557617, 3.844841718673706, "The SCOS-2000 Version of the Ground Segment Satellite Ground Segment is Version 5."]
[9.352670669555664, 1.2239561080932617, "The Ready Time of the 90-satellite constellation Satellite Constellation is 24 months later."]
[9.281951904296875, 9.035189628601074, "The Aperture Diameter of the GMI Instrument is 1.22 m."]
[7.375587463378906, 6.323780536651611, "The Type of the EOVSA's Images Data is Radio emissions."]
[7.4217071533203125, 10.101844787597656, "The Type of the SUCHI (Space Ultra-compact Hyperspectral Imager) Payload is Much smaller."]
[7.633114814758301, 9.00388240814209, "The Resolving Power of the 1.61 and 2.06 \u00b5m CO2 channel Spectrometer is > 20,000."]
[9.584388732910156, 0.7557235360145569, "The Functionality Duration of the S/C and ground segment Satellite and Ground System is Up to 1 orbit before the final breakup."]
[11.439957618713379, 3.791114091873169, "The Resemblance of the Ichthyosaurs Marine Reptiles is Modern-day porpoises."]
[6.934046268463135, 4.705807685852051, "The Mission of the Biomass Satellite is Deliver crucial information on how the world's forests are changing."]
[10.117462158203125, 4.755268573760986, "The Propulsion System of the Lunar IceCube Spacecraft is Busek\u2019s miniaturized electric thrusters."]
[8.81975269317627, 7.029658317565918, "The Quantity of the LEP Sensor Units Sensor Units is Three."]
[11.894635200500488, -0.9394184947013855, "The Lift-off Mass of the GSLV-F05 Rocket is 415.2 tons."]
[6.769123554229736, 1.5749038457870483, "The Operation Start Date of the RapidEye Satellite Constellation is Unknown."]
[7.556820392608643, 2.9069950580596924, "The Participating Companies of the KOMPSAT-5 Spacecraft is Korea Aerospace Industries, Korean Air, Hanwha, Doowon Heavy Industries, and SI (Satrec Initiative)."]
[7.912887096405029, 9.107104301452637, "The Passband of the VIS channel Spectrometer is 400-500 nm."]
[4.793060779571533, 1.7033109664916992, "The Number of Devices Served of the Galileo Satellite Navigation System is More than 1.5 billion smartphones and devices."]
[10.236120223999023, 1.0353425741195679, "The LTDN of the Resurs-P1 Satellite is 10:30 hours."]
[9.249971389770508, 4.104443073272705, "The Body Size of the Spacecraft Satellite is 2.5 m x 1.2 m x 1.1 m."]
[10.433233261108398, 4.7702155113220215, "The Delta-V of the DMC Propulsion Subsystem Electric Propulsion is 10 m/s."]
[6.94163703918457, 4.181803226470947, "The Operation of the THEIA Satellite is Image Capture."]
[6.303040027618408, 8.123774528503418, "The RIN Performance Frequency of the ASM Instrument Instrument is 1 kHz."]
[5.547975063323975, 4.378137588500977, "The Ground Stations of the GIOVE-B Satellite is Dongara (Australia), Kiruna (Sweden), Santiago de Chile (Chile), South Point Hawaii (USA), and Fucino (Italy)."]
[7.576684474945068, 2.729304075241089, "The Calibration Workshop Date of the KOMPSAT-5 Satellite is Aug. 25-27, 2010."]
[10.374727249145508, 3.458832263946533, "The Impact Speed of the SMART-1 Satellite is 2 km/s."]
[9.401833534240723, 3.1339948177337646, "The Orbit Type of the Yubileyniy-2/MiR Satellite is Near-circular orbit."]
[8.955340385437012, 4.133485317230225, "The Dimensions of the SPOT satellite constellation Satellite Constellation is 3.5 m x 15.6 m."]
[9.053417205810547, 8.275458335876465, "The Mechanism Type of the SMA Scan Mechanism Assembly is Two-axis mechanism involving two flex pivots per axis."]
[8.974178314208984, 4.4713850021362305, "The Structure Size of the S/C Satellite is 4 m x 3 m x 2 m."]
[7.562263011932373, -0.5003324151039124, "The Launch Campaign Thread Date of the Falcon Heavy Rocket is 3 June 2019."]
[7.862841606140137, 7.870091915130615, "The Calibration Accuracy of the Instrument Spectrometer is Absolute: \u00b1 5%."]
[10.56065845489502, 1.5800342559814453, "The LTAN Evolution of the Swarm-A (Alpha) Satellite is 24 hours of local time coverage every 7-10 months."]
[9.045376777648926, 6.527291297912598, "The Backup Function of the BEI Systron Donner QRS100 Rate Gyro is Nutation measurement."]
[4.624777317047119, 5.623673439025879, "The LISS-2A/B Data Downlink of the Satellite Satellite is X-band."]
[10.788004875183105, 6.738651275634766, "The Attitude Determination Sensors of the X-ray Telescope Telescope is Fine sun sensor, 3-axes magnetometer."]
[10.736170768737793, 10.29370403289795, "The Dynamic range of the PHA Detector is Up to 23000."]
[7.937219142913818, 1.8460148572921753, "The Publication Date of the ISEE-C Spacecraft is July 1978."]
[6.446649551391602, 2.831700563430786, "The Principal Investigator Institution of the Lucy Satellite is Southwest Research Institute in Boulder, Colorado."]
[7.017004013061523, 1.6080546379089355, "The Completion Date of the CMIP5 Climate Model is 2010 to 2014."]
[11.582620620727539, 2.220553159713745, "The URL of the NASA Mission Asteroid Mining is http://www.nasa.gov/content/goddard/new-nasa-mission-to-help-us-learn-how-to-mine-asteroids/#.U4s2hXbwUkA."]
[12.078969955444336, 2.172919511795044, "The Mission Purpose of the REX-J Robot is Demonstrate technologies for Astronaut support robots."]
[4.023219585418701, 4.394643306732178, "The Operating System of the OBC On-Board Computer is FreeRTOS."]
[6.104343414306641, 4.129900932312012, "The Data Utilization and Applications Program of the RCM Satellite is Provides technical assistance to federal departments to upgrade their applications and develop new ones exploiting data generated by the RCM."]
[3.8142642974853516, 2.2991855144500732, "The Size of the IPEX CubeSat is 1U."]
[6.033569812774658, 6.076939582824707, "The Radar Imagery Capability of the SIR-C/X-SAR Radar System is Multifrequency (3) and multipolarization."]
[6.694207191467285, 6.882246971130371, "The Operation Period of the ALT Instrument is From launch to July 1979."]
[5.652571201324463, 0.9754999876022339, "The Mission Date of the NanoRacks Satellite Deployment Service is 13 July 2018."]
[6.43851375579834, 8.066534042358398, "The Incidence Angles of the MWR Dicke Radiometer is between 52\u00ba and 58\u00ba."]
[4.796419143676758, 0.8855576515197754, "The Cost of the Brexit Satellite Unknown is BS billions."]
[11.871758460998535, -1.1313531398773193, "The Launch Mass of the Kanopus-V Satellite is ~ 450 kg."]
[2.27553391456604, 4.42417573928833, "The Maximum Power Consumption of the ROBUSTA picosatellite Satellite is 1 W."]
[3.9011619091033936, 2.305337905883789, "The Size of the SNaP CubeSat is 3U."]
[8.513124465942383, 9.77570629119873, "The Model of the ICON FUV Instrument CCD is Dalsa FTT1010M."]
[10.43779182434082, 3.5016930103302, "The Ascending Node of the SMART-1 Satellite is 237.721\u00ba."]
[7.727838516235352, 13.557868003845215, "The Resolution \u0394\u03bb (0.05\u00ba slit) of the SPIM5 Spectrometer is 2.9 nm."]
[9.719159126281738, 9.477246284484863, "The Spectral Bands of the IRIS Instrument Spectral Scanner is Green (520 - 600 nm), red (630 - 690 nm), and NIR (760 - 890 nm)."]
[7.456391334533691, 5.553488254547119, "The Bias Correction of the Aeolus Satellite is Temperature variations across the instrument's telescope."]
[9.081507682800293, 10.159085273742676, "The Application of the WiFS camera Camera is Vegetation index mapping."]
[7.869462013244629, 9.81466293334961, "The Swath Width of the TeLEOS-1 Imager Imaging Device is 12 km."]
[5.67899227142334, 3.975785970687866, "The Service Spectrum of the NPOESS Program is NPOESS ground segment will acquire and store global and regional environmental imagery, specialized meteorological, climatic, terrestrial, oceanographic, solar-geophysical, and other data."]
[8.951042175292969, 9.908632278442383, "The Function of the Photo MOSFET Switch Component is DLP mission."]
[13.10883903503418, 4.045600891113281, "The Power Source of the Gaia Satellite is Solar power."]
[5.934912204742432, 1.628304123878479, "The Payloads of the PAZ Satellite is 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."]
[4.633661270141602, 6.556013107299805, "The Equipped Devices of the Low Noise Amplifier Amplifier is Temperature sensor, switched load."]
[3.2151269912719727, 5.196340084075928, "The Capacity of the Flash Memory Card Data Storage is 8GB."]
[9.217114448547363, 10.33258056640625, "The Aperture of the LWIR Camera Camera is 131 mm."]
[1.625557541847229, 4.64909553527832, "The Throughput of the SABR DC/DC Converter is Up to 180 W."]
[9.324602127075195, 5.283327102661133, "The Reaction Wheels of the NigeriaSat-2 Satellite is 4 SSTL Smallwheel 200SP wheels."]
[8.17894172668457, 2.211054563522339, "The Parking Orbit Achievement Date of the ARTEMIS Spacecraft is Aug. 24, 2001."]
[4.592091083526611, 4.223297119140625, "The Function of the CPOD Service Data Service is Generating precise orbital products and auxiliary data files."]
[6.968692779541016, 6.042932987213135, "The Uncertainty of the Sea Surface Salinity (SSS) Measurement is <0.3 pss."]
[7.090023994445801, 0.043227292597293854, "The End of Life Date of the DeMi Satellite is 8 March 2022."]
[8.777016639709473, 6.3920745849609375, "The Associated Plasma Dynamics of the Plasma Blobs Phenomenon is Investigated in the topside ionosphere."]
[7.225246906280518, 2.9396753311157227, "The Debut Location of the Visualization Product is American Astronomical Society meeting in Honolulu, Hawaii."]
[9.653258323669434, 5.873480796813965, "The ADCS of the NEMO-HD Satellite is Attitude Determination and Control System."]
[7.492466926574707, 8.07978630065918, "The Absolute Accuracy of the Radiometry Sensor is < 2.4 Wm -2  sr -1."]
[9.25876235961914, 7.904235363006592, "The Thermal Design of the SWAP Instrument is Unknown."]
[8.941106796264648, 9.169731140136719, "The FPA Format of the CIRiS Instrument is 640 x 480."]
[8.008061408996582, -0.7349796295166016, "The Capture Date of the Dragon Spacecraft is 8 December."]
[7.63930082321167, -0.043821368366479874, "The Docking Attempt Date of the MEV-2 Servicer is 10 March 2021."]
[10.258099555969238, 6.828873157501221, "The Control Mode of the HS Heater System is SHM (Safe Hold Mode) and controlled through Proteus platform."]
[5.066565990447998, 6.995922088623047, "The RF Bandwidth (MHz) of the Antenna Reflector is 800."]
[8.877008438110352, 7.023534774780273, "The Mounting of the SWEA Solar Wind Electron Analyzer is STEREO boom."]
[7.245059967041016, 4.546750068664551, "The Band 5 of the Landsat TM Satellite is Vegetation moisture measurement, snow/cloud differentiation."]
[8.12277603149414, 9.282844543457031, "The Middle Wavelength Infrared (MWIR) and Thermal Infrared (TIR) band wavelengths of the HSRS Sensor is ."]
[5.955591201782227, 4.476083278656006, "The Population of the Timbuktu City is About 55,000."]
[8.127959251403809, 4.019855976104736, "The Moon Images Acquired of the Pleiades-1A and Pleiades-1B Satellites is More than 800 images."]
[4.134790897369385, 5.741061687469482, "The UHF Downlinks Data Rate of the UoSAT-12 Satellite is 9.6 and 38.4 kbit/s."]
[5.7261176109313965, 2.467872142791748, "The Manufacturer of the NanoPower Modules Satellite Component is GomSpace."]
[11.34859561920166, 6.439124584197998, "The Spectrum of the X-ray pulsars Astronomical Objects is Almost the same as predicted by the model."]
[7.953871250152588, 4.645792484283447, "The Spatial Resolution of the CO2Image Satellite is 50 m x 50 m."]
[7.254936695098877, 2.581658363342285, "The URL of the Communications with Earth Communication System is https://mars.nasa.gov/insight/mission/communications/."]
[1.9685184955596924, 5.555533409118652, "The Current of the Voltage 2 Power Amplifier is 10."]
[7.150648593902588, 6.8442583084106445, "The Satellite Environment Test Campaign Date of the IASI-NG PFM instrument Instrument is 2022 and 2023."]
[9.974282264709473, 9.551234245300293, "The Data Usage of the SAGE-III on ISS Satellite Instrument is Assess the performance of OMPS flying on the Suomi-NPP satellite."]
[8.130202293395996, 10.31265926361084, "The Spectral Band of the Band Cameras Camera is 391.4 nm."]
[7.037635326385498, -0.02711125649511814, "The End of Life Date of the Sich-2 Satellite is 12 Dec 2012."]
[4.333308219909668, 6.482544422149658, "The Receiver Operation of the LCT Laser Communication System is Optically adding a locally generated field to the receiver field prior to photodetection."]
[11.064623832702637, 3.5148115158081055, "The Total Mass of Jet Streams of the Juno Spacecraft is About 1% of Jupiter's mass."]
[6.561136245727539, 3.8199403285980225, "The Purpose of the Spire Satellite Constellation is Collect global weather data."]
[6.758682727813721, 0.48167553544044495, "The Launch Date of the VNREDSat-1A Satellite is January 08,2013."]
[8.405923843383789, 9.132829666137695, "The Detector of the SAGE-III Spectrometer is CCD and photodiode."]
[2.121614933013916, 4.534597873687744, "The Power of the INSAT-2A/2B Satellite is 1.18 kW."]
[7.239818572998047, 1.5741969347000122, "The Operation Extension Date of the Cluster Satellite Mission is December 31, 2009."]
[6.491511344909668, 6.388010501861572, "The Power of the SeaWinds scatterometer Scatterometer is 250 W."]
[4.584808349609375, 2.104335069656372, "The Quantity of the MP6 6U CubeSat Satellite is 4."]
[6.8123698234558105, 2.9241907596588135, "The Development Status of the Intermediate Experimental Vehicle Spacecraft is Unknown."]
[5.984949588775635, 6.442716598510742, "The Off-nadir Angle of the SAR Synthetic Aperture Radar is 35\u00ba to the right side of the satellite."]
[4.165735721588135, 4.5186686515808105, "The Function of the Interface Chip Chip is Provides a compliant implementation of the USB standard."]
[6.933774471282959, 2.7018184661865234, "The URL of the POPSAT-HIP1 Satellite is http://blog.isilaunch.com/?p=885."]
[1.5431464910507202, 4.87551736831665, "The Voltage of the 28V main bus Power Bus is 28V."]
[6.6528639793396, 1.3143181800842285, "The Launch Date of the GOCE Satellite is Unknown."]
[7.306117057800293, 8.01158618927002, "The Mosaic Image Tile Time of the EUI Instrument is About 10 minutes."]
[7.927131652832031, 7.398956298828125, "The Pre-Flight Characterization of the TRUTHS Reference Sensor is Good level of pre-flight characterization of the sensor under test."]
[5.951003074645996, 9.524286270141602, "The Mass of the FGM Instrument is 3.0 kg."]
[3.8331587314605713, 2.3088936805725098, "The Size of the MySat-1 CubeSat is 1U."]
[4.738665580749512, 1.814678430557251, "The Number of Satellites of the Unseenlabs constellation Satellite Constellation is Between 20 and 25 by 2025."]
[9.32117748260498, 4.750992774963379, "The Angle Between Fixed Panels of the CHEOPS Satellite is 67 degrees."]
[5.672950744628906, 2.547834634780884, "The Subcontractor of the SBSS Satellite System is Ball Aerospace & Technologies Corp.."]
[7.6217780113220215, 0.8273409605026245, "The Insertion Date of the P1 Spacecraft is August 23rd, 2010."]
[5.6121087074279785, 6.189142227172852, "The Panel Quantity of the SAR Antenna Antenna is 32 slotted waveguides."]
[9.416826248168945, 11.521697998046875, "The Effective FOV of the Channel 5 Sensor is 30 km x 67 km."]
[6.802861213684082, 0.41424673795700073, "The Launch Date of the BeiDou-3S Satellite is 2015/2016."]
[5.169863700866699, 6.11763858795166, "The Purpose of the JIB Antennas Antennas is Support Ship ID Capability."]
[9.673833847045898, 8.193709373474121, "The Anticoincidence CsI Crystal Thickness of the GRS Gamma-Ray Spectrometer is 30 mm."]
[9.124262809753418, 9.170731544494629, "The FOV of the Observation Instrument Telescope/Spectrograph is 0.1\u00ba x 7.3\u00ba + 0.2\u00ba x 0.2\u00ba (7.5\u00ba full length)."]
[7.652308940887451, 6.539882183074951, "The Measurement Error of the Instrument Satellite Instrument is Slightly deteriorated when no ground echo was retrieved."]
[7.108466625213623, 8.075536727905273, "The Integration Time of the Radiometer Instrument is 65 ms."]
[8.049701690673828, 1.4623746871948242, "The Discovery Date of the Solar Dynamics Observatory Satellite is 24 years ago."]
[9.165704727172852, 4.233895778656006, "The Honeycomb core thickness of the Bus structure Satellite Structure is t = 10. 8 mm."]
[5.902127265930176, 6.059831619262695, "The Bandwidth Transition Processing of the SAR Processor Data Processor is 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."]
[10.076502799987793, 1.9841063022613525, "The Orbital period of the KOMPSAT-3 Satellite is 98.5 minutes."]
[5.566335678100586, 5.517467975616455, "The GPS Antennas of the NOX Payload Satellite Payload is 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."]
[8.37197208404541, 7.521668434143066, "The Instrument Heritage of the EPI-Hi Particle Measurement Instrument is LET (Low Energy Telescope) and HET (High Energy Telescope)."]
[8.840410232543945, 10.699527740478516, "The Data Rate of the WiFS camera Camera is 2.06 Mbit/s."]
[8.743952751159668, 0.7472138404846191, "The Orbital Insertion at Ganymede of the Juice Spacecraft is December 2034."]
[6.186338901519775, 7.708566665649414, "The Polarization of the ICI instrument Receiver is V and H."]
[7.0326690673828125, 0.4693388044834137, "The Launch Date of the ANUSat Satellite is April 20, 2009."]
[8.0494384765625, 8.226449966430664, "The Components of the Atmospheric Chemistry Suite Spectrometer is Three infrared spectrometers."]
[9.645465850830078, -0.06503468006849289, "The Goal Mission Life of the PARASOL microsatellite Satellite is Two years."]
[11.735581398010254, 1.0944750308990479, "The Laser Altimetry Data Processing of the Chang\u2019E-1 Satellite is 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."]
[9.235077857971191, 4.1869001388549805, "The Dimensions of the QSat-EOS bus Microsatellite bus is 492 mm x 503 mm x 502 mm."]
[7.1996283531188965, 7.978952884674072, "The Registration Time of the RGD Instrument is 20 ms."]
[5.098038673400879, 6.440245151519775, "The Type of the Antenna ADS-B Antenna is Planar with two elements."]
[7.095077037811279, 5.617091655731201, "The Impact of the Argo Oceanographic Program is Change our understanding of the world's oceans, opening in fact a new era of oceanography."]
[5.219459533691406, 4.687802791595459, "The Location of the Ground Station Ground Station is Tarusa (Russia)."]
[10.381860733032227, 4.963865756988525, "The Category of the PPS-1350-G Hall-effect thruster is Hall-effect thrusters."]
[11.758167266845703, 4.640833854675293, "The Distance from Earth of the Ophiuchus galaxy cluster Galaxy Cluster is 390 million light years."]
[6.909940242767334, 1.2893437147140503, "The Conference Date of the Multi-satellite Operations System System is April 25-30, 2010."]
[4.342430591583252, 4.6097564697265625, "The Components of the Instrument Control Unit (ICU) Control Unit is 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)."]
[7.274194717407227, 0.4296153783798218, "The Launch Date of the PACE Satellite is 19 June 2014."]
[7.5888752937316895, 8.805249214172363, "The Vertical resolution of the UV/VIS Spectrometer Spectrometer is 1.7 km."]
[8.17119026184082, 0.9453839063644409, "The Historical Record Publication Date of the Landsat-7 Satellite is Oct. 2006."]
[4.3760986328125, 3.2398922443389893, "The Technology Integration of the SATis5 Testbed is 5G communication environment including satellite and terrestrial components."]
[7.150452613830566, 2.3838984966278076, "The URL of the Grace Mission Satellite is https://web.archive.org/web/20230406203004/http://www.csr.utexas.edu/grace/operations/."]
[8.962235450744629, 3.2862210273742676, "The Fuel Tank Status of the Kepler spacecraft Spacecraft is Running very low."]
[10.582550048828125, 5.9845685958862305, "The Observation Type of the RHESSI Satellite is Flare."]
[6.824443340301514, 3.0061399936676025, "The Student Collaboration Goal of the IMAP Mission is Provides students of diverse backgrounds with hands-on experience designing and building a CubeSat and two scientific instruments."]
[7.100070953369141, 2.547203540802002, "The URL of the Deep Space 1 Satellite is http://nmp.jpl.nasa.gov/ds1/NewsConference/04_06_99DS1.pdf."]
[5.326189994812012, 5.7453107833862305, "The Antennas of the GPS receiver Receiver is 4 antennas."]
[12.999903678894043, 4.1546525955200195, "The Data Archive Size of the Gaia Satellite is 1000 1 TB hard drives from a top-end home PC."]
[7.137405872344971, 1.3432953357696533, "The Workshop Date of the MXGS Apparatus is May 19-22, 2009."]
[5.406402111053467, 0.29608282446861267, "The Containment of the Calf Canyon-Hermits Peak Fire Fire is 40 percent."]
[4.477662086486816, 3.2265477180480957, "The EPS of the SCARAB 1U CubeSat bus is Clyde Space 1U EPS w/Lithium-polymer battery."]
[9.28381633758545, 0.8289018869400024, "The Mission Life of the Telescope Optical Instrument is 5-year minimum lifetime."]
[4.247757434844971, 3.695523500442505, "The Signal Processing of the NTS AIS Receiver Communication Receiver is Attempt to unravel the overlapping messages."]
[10.4757661819458, -1.144029140472412, "The Total Mass of the ASAP Nanosatellite is About 3 kg."]
[11.419652938842773, 3.875981569290161, "The Bulk Water Inventory of the Mars Planet is Global Equivalent Layer (GEL) of ~30 m."]
[9.334467887878418, 3.190822124481201, "The Orbit Type of the CeREs CubeSat Satellite is Circular."]
[10.423416137695312, 4.13239860534668, "The Altitude Accuracy of the Bloostar Launch Vehicle is \u00b15 km."]
[7.340571403503418, 7.44230318069458, "The Design of the OMI Instrument is Conceptual."]
[7.646854877471924, 2.2287957668304443, "The Expected Completion Date of the ELSA-d Mission is April 2020."]
[5.949704170227051, 4.514456272125244, "The Operator of the TIM and SIM instruments Instruments is NOAA."]
[8.091294288635254, 8.388740539550781, "The Detector Function of the Conventional Interferometers Interferometer is Collects light over the full aperture of the critical optical components."]
[9.998430252075195, 1.3633451461791992, "The UHF Carrier Detection Time of the MarCO-B Satellite is 11:41 am."]
[7.732624530792236, 4.909754276275635, "The 3-axis stabilization of the BEESAT-3 Satellite is Yes."]
[7.72193717956543, 3.652911424636841, "The Event of the Land Glacier Glacier is Part of the glacier\u2019s ice tongue crumbled away."]
[11.136127471923828, 6.90735387802124, "The X-ray Spectrum of the AXP Anomalous X-ray Pulsar is Extends up to energies of at least 150 keV."]
[6.55180549621582, 2.6560916900634766, "The Location of the Richat Structure Landmark is Mauritania."]
[3.5859010219573975, 6.258009433746338, "The Maximum Data Rate of the Channel Communication System is 1674 Mbit/s."]
[8.244058609008789, 10.171417236328125, "The GSD of the DMC-2G imager Imager is 22 m."]
[8.097966194152832, 5.33475399017334, "The Accuracy of the GPS-fed high-accuracy ephemerides Data is ~5 m."]
[5.979224681854248, 1.7613416910171509, "The Launch Provider of the COSMO-SkyMed-1 Satellite is ULA."]
[4.890857696533203, 12.098414421081543, "The Responsivity Measurement of the Responsivity Measurement Instrument is 1.37 A/W."]
[6.193375587463379, 2.0081167221069336, "The Launch Site of the OPAL Satellite is VAFB, CA."]
[4.380347728729248, 6.402457237243652, "The Frequency Band of the COM Communications System is VHF/UHF."]
[7.279841423034668, -0.4409058690071106, "The Starlink Satellites Launch Date of the SpaceX Company is 14 March 2021."]
[3.8149778842926025, 4.427303314208984, "The Type of the OBC On-Board Computer is High-grade main OBC."]
[9.487241744995117, -2.5074028968811035, "The Charge Range for Isotopes of the LEICA Particle Detector is 2 - 16."]
[9.159116744995117, -0.5721612572669983, "The End of Life Date of the TechnoSat Nanosatellite is Operational as of February 2023."]
[6.777817726135254, 4.800571918487549, "The Data Products of the Sentinel-4 Satellite is 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 thickn."]
[5.9859843254089355, 8.590733528137207, "The No of bands/channels of the MWTS Microwave Temperature Sounder is 4."]
[10.63790225982666, -1.6984624862670898, "The Waste Capacity of the HTV-6 Spacecraft is Up to 6 metric tons."]
[5.835777759552002, 3.578242063522339, "The Location of the SPIE Office is NASA/MSFC (Marshall Space Flight Center) in Huntsville, Alabama."]
[4.770782470703125, 0.8249197602272034, "The Contract Award of the Northrop Grumman Company is $692 million."]
[9.062796592712402, 6.5467448234558105, "The Type of the Rate gyro Sensor is Gyro chip."]
[6.212990760803223, 3.017341375350952, "The Manufacturer of the Gonets-M No.3 Communication Satellite is JSC Academician M.F. Reshetnev Information Satellite Systems."]
[7.117878437042236, 7.594991683959961, "The Distribution of the MET data Data is HRIT/LRIT transmission within 15 minutes after image acquisition."]
[9.396038055419922, -0.7711402177810669, "The Launch Time of the IDEA-OSG 1 Microsatellite is 05:41 UTC."]
[8.940083503723145, 2.206498146057129, "The Observation of the New Horizons Spacecraft is Fluxes of charged particles in Jupiter's magnetotail."]
[13.10165786743164, 4.051567554473877, "The Measurement of the Gaia Satellite is The acceleration of the Solar System."]
[6.938997745513916, 2.488281488418579, "The URL of the Earth Observation Constellation Satellites Satellite Constellation is http://www.nspo.narl.org.tw/ICGPSRO2013/."]
[3.5527892112731934, 2.2813069820404053, "The Size of the QBus-4 Satellite is 2U."]
[7.506821155548096, 3.674776077270508, "The Wing Status of the AC4-B Satellite is Open."]
[10.951177597045898, 2.8276610374450684, "The Magnitude of the Tohoku-Kanto earthquake Earthquake is 9.0."]
[7.448453426361084, 7.949265480041504, "The Number of Ozone Altitude Profiles of the UVSP Instrument is Approximately 20,000."]
[8.035746574401855, 1.4959125518798828, "The Close-Up Date of the Arrokoth Celestial Body is 13 February 2020."]
[11.871557235717773, 0.9817755222320557, "The Launch Vehicle of the Chang'e-5 Spacecraft is Long March 5 (CZ-5)."]
[8.451661109924316, 7.482454776763916, "The Components of the ULF Sensor Sensor is Search coil, calibration coil, amplifier/filter circuit."]
[6.256404876708984, 2.1625924110412598, "The Design Considerations and Programme Status of the TecSAR Satellite is Y. Sharay, U. Naftaly, \u201cTecSAR: design considerations and programme status,\u201d IEE proceedings of Radar, Sonar & Navigation, Vol. 153, No 2, 2006."]
[7.029943466186523, 2.425691843032837, "The URL of the TOPCAT Satellite is http://www.bath.ac.uk/elec-eng/invert/topcat.html."]
[4.600311756134033, 2.351234197616577, "The Hosted Payloads of the Prometheus Satellite Satellite is 1.5U payload module can be added to each satellite."]
[9.645370483398438, 6.026060581207275, "The Manufacturer of the ADCS Attitude Determination and Control Subsystem is Stellenbosch University."]
[8.020946502685547, 10.023542404174805, "The Bandpass Filters of the EXI Camera is 3 UV bands and 3 visible (RGB) bands."]
[4.930228233337402, -3.210477352142334, "The | of the Justin C. Kasper, Bennett A. Maruca, Michael L. Stevens, Arnaud Zaslavsky Authors is Justin C. Kasper, Bennett A. Maruca, Michael L. Stevens, Arnaud Zaslavsky."]
[11.482928276062012, 4.244316101074219, "The Orbit Distance of the 55 Cancri e Exoplanet is 0.015 astronomical units from its Sun-like star."]
[7.791004657745361, 10.878772735595703, "The Data quantization of the ALOS-3/PRISM-2 Satellite is 11 bit."]
[6.060965538024902, -0.0543353371322155, "The Announcement Date of the Galileo Second Generation Satellite is 27 May 2021."]
[9.66116714477539, 1.4400403499603271, "The Ground-Station Uplink Passes of the SpinSat Satellite is Within the preceding 5 days."]
[6.26723051071167, 3.6296896934509277, "The Mounting Satellite of the METimage Instrument is MetOp-SG-A."]
[6.53657865524292, 3.7461748123168945, "The Mission Objective of the OSMA-1 Satellite is Conduct a series of demonstrations of in-space robotic assembly of an antenna and a boom."]
[3.949711561203003, 4.565521717071533, "The Microprocessor of the TPMU Device is ADuC845."]
[7.681822776794434, 9.967313766479492, "The Operating Temperature of the VNIR Detector is 257 K."]
[3.893728017807007, 6.933012008666992, "The Power of the COPS Ka-band Communication Payload is 1077 W."]
[11.467637062072754, 5.8852949142456055, "The Black Hole Jet Discovery Date of the Chandra X-ray Observatory X-ray Observatory is 9 January 2019."]
[9.797689437866211, 3.8479669094085693, "The Launch Date of the NanoSail-D Satellite is Aug. 2 2008."]
[4.87831974029541, 1.7341985702514648, "The Number of Satellites of the FORMOSAT-7/COSMIC-2 Satellite Constellation is 6."]
[7.729691982269287, 9.087183952331543, "The Spectral Sampling of the Ma_MISS Spectrometer is About 20\u2009nm."]
[5.136199951171875, 2.209148645401001, "The Primary-Spacecraft Interfaces of the CubeStack Multi-Payload Adapter is 98.5 cm \u00d8 and 61 cm \u00d8."]
[9.690166473388672, 2.4677839279174805, "The Closest Approach Distance of the BepiColombo Spacecraft is 199 km."]
[11.705025672912598, -1.169843077659607, "The Payload Mass of the INTEGRAL Satellite is 2 t."]
[9.10810375213623, 10.53295612335205, "The Pixel Size of the Main Camera Camera is 100 m in its central field of view."]
[3.994492530822754, 6.659134864807129, "The Value of the Group Delay Uncertainty Parameter is Few nanoseconds (1-3 ns)."]
[10.12207317352295, 6.783090114593506, "The Thermal Control of the ITASat CubeSat Satellite is Passive."]
[5.502141952514648, 3.209573268890381, "The Objective of the MarCO CubeSat is Relay back InSight data as it enters the Martian atmosphere and lands."]
[7.100106239318848, 0.43533000349998474, "The Launch Date of the ALL-STAR-1 Satellite is April 18, 2014."]
[9.614912033081055, 4.0752177238464355, "The Length of the Tianhe Space Station Module is 16.6 meters."]
[3.9818475246429443, 5.671104431152344, "The LISS-2A/B Data Downlink Transfer Rate of the Satellite Satellite is 10.4 Mbit/s."]
[5.466099262237549, 4.293242454528809, "The Ground-Based Observation Sites of the ExoCube Satellite is Arecibo, Wisconsin, Kitt Peak, and Cerro Tololo."]
[6.050185680389404, 1.5472462177276611, "The Components of the CCC (Coordinated Constellation Concept) Satellite Constellation is German TerraSAR-X/TanDEM-X and the Spanish PAZ satellite."]
[9.195084571838379, 3.2509496212005615, "The Orbit Type of the Rideshare mission Satellite is SSO (Sun-Synchronous Orbit)."]
[6.409191131591797, 4.133851051330566, "The Ground Segment of the QuakeSat Satellite is Unknown."]
[7.140844345092773, 5.802770614624023, "The Accuracy of Wind Velocity (Stratosphere) of the Aeolus Satellite is 3 m/s."]
[7.398272514343262, 4.073887348175049, "The Measurement Category of the FormoSat-1 Satellite is Ocean colour/biology."]
[5.866513252258301, 8.576172828674316, "The Calibration Method of the MWHS-II Microwave Humidity Sounder is Two points periodically."]
[7.136398792266846, 3.7024457454681396, "The Operator of the OrbView-2 Satellite is ORBIMAGE."]
[8.588134765625, 1.2639963626861572, "The Observation End Time of the INTEGRAL Satellite is 22:14:36 on 25 January."]
[7.844727039337158, 4.505337238311768, "The Multispectral Bands Off-nadir Resolution of the WorldView-3 Satellite is 1.38 m."]
[9.038026809692383, 4.193959712982178, "The Height Envelope of the UKube-1 Satellite is < 108 mm."]
[5.611726760864258, 3.037019968032837, "The Manufacturer of the Heinrich-Hertz satellite Satellite is DLR-RfM (German Aerospace Center \u2013 Space Administration)."]
[11.323261260986328, 6.055720329284668, "The Interaction with Matter of the Neutrinos Subatomic Particles is Incredibly rarely."]
[9.072792053222656, 7.996408939361572, "The Plastic Scintillator of the Range Calorimeter Particle Detector is Side of 15 cm."]
[7.0093584060668945, 4.995014190673828, "The Carbon Sink of the Northern Forests Ecosystem is Yes."]
[10.359315872192383, 3.2315216064453125, "The Altitude of the GRACE-FO satellites Satellite is ~490 km."]
[8.597761154174805, 5.360837459564209, "The Pointing Accuracy of the Resurs-P1 Satellite is 0.2 arcmin."]
[6.470193386077881, 6.152468204498291, "The Measurement Capability of the ASCAT C-band radar is Day and night."]
[9.493270874023438, 9.044926643371582, "The Length of the Telescope Assembly Optical Instrument is 100 cm."]
[8.525073051452637, 6.8396148681640625, "The Resolution of the OVM Overhauser scalar magnetometer is 0.1 nT."]
[10.337700843811035, 5.302237510681152, "The Capacity of the XTA Xenon Tank Assembly is 60 liters."]
[5.8459391593933105, 8.660543441772461, "The Beamwidth of the HSB Humidity Sounder is 1.1\u00ba."]
[7.08448600769043, 8.544942855834961, "The Ion Masses of the COSIMA Mass Spectrometer is Above 28 Daltons."]
[13.078792572021484, 4.070781707763672, "The Function of the Gaia Space Telescope is Scans the sky."]
[7.076773643493652, 1.3663824796676636, "The Conference Date of the LPT9310 COTS cooler Cooler is May 23-27, 2016."]
[6.993209362030029, 3.2887072563171387, "The Duty Cycle of the VRSS-1 Satellite is 10%."]
[10.409341812133789, 5.65394926071167, "The Length of the Hoytether Tether is 10 m."]
[9.296467781066895, 10.052597999572754, "The Power Consumption of the APD Avalanche Photodiode is Low."]
[9.594782829284668, 0.9696635007858276, "The Flight Time Before Reentry of the RainCube Satellite is No more than twelve months."]
[7.433507442474365, 1.4721601009368896, "The Calibration Approach Date of the MICROSCOPE Satellite is 2003."]
[7.897568225860596, -0.2256852686405182, "The Orbit Reach Date of the Shenzhou-13 Spacecraft is 15 October 2021."]
[3.9831528663635254, 6.593803405761719, "The Dynamic Range of the Receiver Communication System is \u2264 15 dB."]
[7.655401706695557, 8.454983711242676, "The Heritage of the OMPS UV Hyperspectral Imaging Spectrometer is SBUV/2, TOMS and GOME."]
[5.723928451538086, 0.8986322283744812, "The Interface Control Document Date of the NanoRacks CubeSat Deployer Deployer is Dec. 10, 2013."]
[7.431466579437256, 7.968003273010254, "The Range of the Ozone Measurement Instrument Atmospheric Measurement Device is 50-650 Dobson Units (DU)."]
[9.47269344329834, 9.233187675476074, "The Objective Aperture Diameter of the VSSC Camera is 0.25 m."]
[7.415340900421143, -0.527522623538971, "The Launch Year of the CYGNSS Satellite Mission is 2016."]
[10.613758087158203, 3.372009515762329, "The Closest Approach Distance of the Rosetta Spacecraft is 75,000 km."]
[8.034852981567383, 9.614951133728027, "The Wavelengths of the OSIRIS Infrared Imager is 1263 nm, 1273 nm, 1530 nm."]
[11.767102241516113, 3.3828446865081787, "The Rate of Change of the Delta in Solar Phase of Apsides Orbital Parameter is 0.8\u00ba/year."]
[9.6477632522583, 2.2687246799468994, "The Fixed Distance from CALIPSO of the CloudSat Satellite is About 460 km."]
[11.66959285736084, -1.1903079748153687, "The Mass of the Flight Unit Satellite Component is 8.5 kg."]
[8.426033020019531, 6.326159477233887, "The Test Location of the Thermal Testing Test Type is Thermal vacuum chamber on USSC premises."]
[7.537479400634766, 7.844792366027832, "The Objective of the CERES Instrument is Provide continuity of the top-of-the-atmosphere radiant energy measurements."]
[10.121908187866211, 6.955416202545166, "The Outer Edge Length of the MLI Thermal Control Device is Unknown."]
[9.070773124694824, 3.221255302429199, "The Orbit Type of the NigeriaSat-2 Satellite is Sun-synchronous circular orbit."]
[8.579095840454102, 2.709380865097046, "The Responsible Orbit of the JPSS Satellite is Afternoon."]
[6.96394157409668, 0.12150907516479492, "The Contract Date of the Satellite Vu\u2019s first satellite Satellite is December 16, 2021."]
[12.031708717346191, 3.230921506881714, "The Orbit Inclination of the Optsat-3000 Satellite is 98.28\u00ba."]
[6.479270935058594, 8.111139297485352, "The Mission Objective of the AMSU Microwave Radiometer is Obtain global temperature and humidity profiles."]
[8.358367919921875, 5.500452041625977, "The Stability of the Electrical Field Satellite System is < 1 mV/m over 1 month."]
[11.687084197998047, -1.1634345054626465, "The Total Mass of the SZ-7 Spaceship is ~7800 kg."]
[8.212114334106445, 4.518938064575195, "The Loch-in Zone of the Satellite Imaging Satellite is 800 km."]
[6.944449424743652, 1.0908839702606201, "The Presentation Date of the UniSat-5 Satellite is April 23-25, 2014."]
[5.306423187255859, 1.3846638202667236, "The Number of Launches of the Falcon 9 Rocket is Three."]
[7.953640460968018, 10.77993392944336, "The Data Quantization of the 4-band CCD Imager Instrument is 12 bit."]
[5.12808084487915, 3.1759486198425293, "The Communication Architecture of the BioSentinel Spacecraft is 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-ban."]
[8.035289764404297, 1.4735088348388672, "The Presentation Date of the Micro Digital Sun Sensor Sensor is Aug 25-27, 2004."]
[6.952813625335693, 11.298958778381348, "The Wavelength FWHM of an unresolved line of the Spectrometer Instrument is 0.039 \u00b5m."]
[7.965018272399902, 1.4856311082839966, "The Operation Period of the SAM-II Sun Photometer is 1978 to 1995."]
[5.224405288696289, 2.632591724395752, "The Manufacturer of the DTUSat-2 1U CubeSat is DTU (Technical University of Denmark)."]
[2.260862112045288, 4.398228168487549, "The Power of the Microsatellite Satellite is 30 W (max)."]
[8.22531509399414, 7.7740478515625, "The Accuracy of Atmospheric Temperature Profiles of the CrIMSS Instrument Suite is 1 K."]
[5.014463901519775, 1.8631240129470825, "The Number of Experiments of the ORS-3 Mission Satellite Mission is 2."]
[8.106718063354492, 9.609602928161621, "The Resolution of the NAOMI Imaging Instrument is 2.5 m."]
[4.384678840637207, 4.296447277069092, "The Microcontroller of the Sensor Suite Payload is Shared."]
[7.695359230041504, 9.883665084838867, "The Spectral Range of the VNIR-NP channels Sensor is 380 nm to 865 nm."]
[8.392818450927734, 6.651615619659424, "The Resource Requirements of the SWiPS Sensor is Low."]
[12.00614070892334, 3.248549699783325, "The Orbit Inclination of the CubeSats Satellite is 97.6\u00ba."]
[9.615038871765137, 5.993194580078125, "The Actuators of the ADCS Attitude Determination and Control Subsystem is Magnetorquers."]
[11.637893676757812, -0.9766010046005249, "The Bus Dry Mass of the Spacecraft Satellite is 410 kg."]
[6.313340187072754, 10.077921867370605, "The Total Mass of the LWIR Camera Camera is 2.1 kg."]
[2.3047893047332764, 4.2463579177856445, "The Solar Array Power of the THEMIS (and ARTEMIS) spacecraft Satellite is Barely moved below BOL values."]
[11.324445724487305, 1.5190714597702026, "The Number of Wheels of the Yutu 2 Lunar Rover is 6."]
[9.172035217285156, 3.2328295707702637, "The Orbit Type of the Satellite Spacecraft is Sun-synchronous orbit."]
[7.868966102600098, 7.284116268157959, "The Calibration Equipment of the Monochromator Instrument is \u201cHP 70950A\u201d."]
[11.53064250946045, 5.2457194328308105, "The Article Date of the Black Hole Celestial Object is July 12, 2016."]
[2.32546067237854, 4.480656623840332, "The Power of the Spacecraft Satellite is Up to 1065 W."]
[5.903741359710693, 6.7780609130859375, "The Antenna Rotation Speed of the SWIM Real Aperture Radar is ~6 rpm."]
[10.328706741333008, 4.860040664672852, "The Propellant Type of the Chemical Propulsion Thrusters Orbit Maintenance is Monomethylhydrazine and nitrogen tetroxide."]
[8.349761962890625, 8.746274948120117, "The Sensitivity of the Interferometric Spectroscopic Instruments Spectroscopic Instruments is Typically 100 times those of conventional grating spectroscopic instruments of similar size."]
[3.585627317428589, 2.2891769409179688, "The Size of the StangSat Satellite is 1U."]
[8.25326156616211, 10.344202995300293, "The Spectral Ranges of the WorldView-110 camera Camera is Eight bands of the short-wave infrared range."]
[8.150214195251465, 8.785531997680664, "The Correlation of the Spectral Angle Measurement is With the white panel when the yellow coupon is used as a reference."]
[4.033536911010742, 10.348812103271484, "The NE\u0394T (K) of the ICI-11 Radiometer is 1.5."]
[7.582411766052246, 1.1150375604629517, "The Arrival Date of the Sentinel-1B Satellite is March 22, 2016."]
[9.395760536193848, 6.016528606414795, "The Sun Sensor Field of View of the ACS Attitude Control Subsystem is \u00b145\u00ba."]
[9.192090034484863, 9.495306968688965, "The Angle of the Zenith FOV Field of View is 35\u00ba."]
[6.69552755355835, 7.869009971618652, "The Laser Type of the Laser Head Unit (LHU) Laser Unit is Narrow linewidth NPRO laser."]
[7.895044803619385, 4.444099426269531, "The Imagery Resolution of the WorldView-3 Satellite is 30 cm."]
[11.762712478637695, 4.658158779144287, "The Outflow Length of the Milky Way Galaxy is Hundreds of light years."]
[3.6818583011627197, 4.534957408905029, "The Supported RTOS of the RAD750 SBC Single Board Computer is VxWorks (versions 5.4, 5.5, and 6.2)."]
[5.561455249786377, 2.7826032638549805, "The Developer of the FSSCat Satellite is Universitat Polit\u00e8ctica de Catalunya (UPC)."]
[5.571334362030029, 4.971399307250977, "The Manufacturer of the Hardware Quick Look SAR Processor SAR Processor is MRSA/SAC team."]
[12.10466480255127, 2.2212085723876953, "The Camera Suite of the OSIRIS-REx Mission is OCAMS."]
[7.751906871795654, 0.37529221177101135, "The Launch Date of the Inspiration4 Crewed Mission is Sept. 15."]
[8.83743667602539, 7.301295757293701, "The Impact on Measurements of the Thermal Effects Phenomenon is Systematic errors."]
[4.105195999145508, 7.266939640045166, "The Mass of the Transmitter Communication Device is 700 g."]
[10.023822784423828, 1.5322864055633545, "The Cadence of the BRITE Satellite is < 100 minutes."]
[11.691267013549805, -1.1492576599121094, "The Mass of the DebriSat Satellite is 56 kg."]
[6.047077655792236, -0.05684955418109894, "The Integration Dates of the Galileo Satellites Satellite is July 11, 2018."]
[9.688300132751465, 8.997645378112793, "The Size of the Secondary Mirror Optical Component is 2.4-foot (0.74 m)."]
[9.400327682495117, 9.981334686279297, "The Power Consumption of the APD detector Experiment is Low."]
[8.009422302246094, 9.547032356262207, "The Spectral Range of the AVHRR/3 Sensor is 2.225-2.275."]
[7.4588727951049805, 8.460588455200195, "The Value of the MTF Performance Requirement is Better than 0.3 Nyquist."]
[9.617859840393066, 5.960988998413086, "The Attitude Control Error of the ADCS Attitude Determination & Control Subsystem is \u2264 30 \u00b5rad."]
[7.253349304199219, 7.207909107208252, "The Internal Calibration Modes of the MIRAS Instrument is Short duration, full orbit."]
[4.751702785491943, 6.01930570602417, "The Radio Type of the ELFIN-A Satellite is AstroDev Helium radio."]
[1.5519171953201294, 4.921694755554199, "The Secondary Voltages of the PCM Power Control Module is +28 V, \u00b15 V, \u00b115 V, and \u00b112 V."]
[7.73564338684082, 7.363779544830322, "The Altitude of the TEMPO Instrument is 35,786 km."]
[9.233468055725098, 10.19497013092041, "The Number of Published Images of the MoonKAM Camera System is Nearly 120,000."]
[3.487013339996338, 5.283288955688477, "The Data Collected of the TerraSAR-X Satellite is 1.34 petabytes."]
[7.119389057159424, 0.7920573353767395, "The Asia-Pacific Region Service Start Date of the BDS Satellite is 2012."]
[10.074483871459961, 4.108599662780762, "The Solar Sail Deployment Test Support of the NEA Scout Spacecraft is Helium balloons."]
[9.205657005310059, 4.193545341491699, "The Structure Dimensions of the DSP satellites Satellite is 2.1 m diameter and 1.23 m in height."]
[8.328812599182129, 4.5834126472473145, "The Swath Width of the GF-2 Satellite is 45 km."]
[8.539795875549316, 5.726566314697266, "The Temperature of the Proton Component Measurement Accuracy of the DSCOVR Satellite is 50%."]
[8.667278289794922, 9.5715913772583, "The Plate Scale of the EXI instrument Imaging Instrument is 0.85 mm/\u00ba."]
[5.231828212738037, 5.979495525360107, "The Antennas of the R3 Spacecraft Satellite is Two patch antennas."]
[7.364939212799072, 7.878012180328369, "The Observation Geometry of the MOMS-02 Instrument is Stereo Triplets."]
[5.1962890625, 6.122949123382568, "The Antennas of the RF Communications Data Transmission is Two existing two-axis gimbaled directional antennas."]
[7.400300979614258, 3.597766876220703, "The Controller Modes of the GOCE Satellite is FPM and higher DFACS modes."]
[11.665154457092285, 2.617873430252075, "The Width of the Dimorphos Asteroid is 160 meters."]
[6.139387607574463, 5.931844711303711, "The Ground Resolution (Stripmap mode) of the XSAR SAR is 3 m."]
[10.274224281311035, 6.832968235015869, "The Operation of the TCU Thermal Control Unit is 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."]
[8.6176176071167, 8.854338645935059, "The Filter Type of the VIS channel Spectrometer is Block with Aluminum."]
[2.209639549255371, 6.523780345916748, "The Latency of the ATL09 ATLAS Atmosphere Cloud Layer Characteristics Data is 45 days."]
[10.151613235473633, 9.551587104797363, "The Data Rate for Images of the IRIS Observatory is Every 5\u201310 s."]
[4.944516181945801, 2.113368511199951, "The Payload Complement of the ALBus CubeSat Satellite is 13 CubeSats."]
[11.062652587890625, 2.625694990158081, "The Descent Path Length of the Lander Spacecraft is 450 km."]
[8.813159942626953, 8.422207832336426, "The Temporal Resolution of the ELENA Sensor is 40 s."]
[7.666345119476318, 1.7335456609725952, "The Report Release Date of the SMAP Satellite is January 2007."]
[4.9590229988098145, 8.916240692138672, "The X-band radio of the InSight Spacecraft is Measure the \"wobble\" of Mars as it spins."]
[7.7750396728515625, 9.891326904296875, "The No of bands/channels of the MERSI Medium Resolution Spectral Imager is 20."]
[7.754050254821777, 10.792654991149902, "The Bit Depth of the fADC A/D Converter is 14 bit."]
[8.761178016662598, 7.089783191680908, "The Range of the Acceleration Sensor is -50 to +50 G (3-axis)."]
[7.746554374694824, 7.986426830291748, "The Accuracy of the SCM Satellite Charging Monitor is \u22640.01 pA/cm2."]
[11.144795417785645, 2.4783360958099365, "The Diameter of the Holes Drill Holes is 60-centimeter."]
[7.816001892089844, 2.2467942237854004, "The Edition of the Observation of the Earth and Its Environment Documentation is 4th."]
[5.843000411987305, 6.824817180633545, "The Frequency of the Radar Radar is 17 GHz."]
[8.47780990600586, 1.8938933610916138, "The Date of NASA Feature of the Jupiter's Auroras Natural Phenomenon is 6 September 2017."]
[5.402651786804199, 0.2935106158256531, "The Burned Area of the Calf Canyon-Hermits Peak fire Fire is 270,000 acres."]
[9.732303619384766, 1.5533337593078613, "The Repeat Cycle of the Resurs-P1 Satellite is 3 days."]
[5.959195613861084, 2.6116960048675537, "The Affiliation of the Ayyoob Sharifi Associate Professor is Urban Knowledge-Action Network."]
[8.300762176513672, 8.12096118927002, "The Reflectance of the Reflection Diffuser Calibration Device is \u03c1=100%."]
[8.7736177444458, 9.988862991333008, "The Number of Subapertures of the SMART Imaging System is 8."]
[7.264217853546143, 0.6571608185768127, "The Launch Date of the Deployment Systems Satellite is July 12, 2006."]
[1.0141973495483398, 4.315349578857422, "The NiH (Nickel Hydrogen) of the Battery System Type is A NiH (Nickel Hydrogen) battery system provides power for eclipse phase operations."]
[10.345206260681152, 5.97930383682251, "The TGFs Detected of the RHESSI Satellite is Over 1000."]
[11.649535179138184, 6.150251865386963, "The Announcement Date of the XMM Newton Satellite is 04 February, 2000."]
[6.937551975250244, 0.9178726077079773, "The Mission Date of the FireBird Satellite is May 11-15, 2015."]
[9.072627067565918, 2.9628841876983643, "The Rock Deposits Size of the LRO Satellite is Less than 500 m across."]
[6.95512056350708, 11.288949012756348, "The Wavelength FWHM of an unresolved line of the Spectrometer Instrument is 0.013 \u00b5m."]
[4.472174167633057, 6.317300319671631, "The Configuration of the \u00b5SDTN transponder Transponder is Core transponder on the left; diplexer, RF switch and test couplers on the right."]
[6.390215873718262, 8.554060935974121, "The Swath Width of the JPL Microwave Radiometer Radiometer is 9 km."]
[7.142025470733643, 3.9769322872161865, "The Operation of the DMC Constellation Satellite Constellation is Share unused capacity with other Members."]
[6.205403804779053, 2.7472803592681885, "The Funding Source of the NASA Heliophysics Technology and Instrument Development (H-TIDeS) Program is NASA."]
[10.224956512451172, 2.9956467151641846, "The Orbit Altitude of the STARS spacecraft Satellite is 666 km."]
[7.272652626037598, 0.5073710680007935, "The Launch Time of the NeuSAR Satellite is 0832 EDT."]
[5.927789688110352, 3.0776216983795166, "The Prime Contractor of the Spacecraft Satellite is Airbus UK."]
[7.36887788772583, 10.093154907226562, "The Conference Presentation Date of the EnMAP Hyperspectral Imager Imaging Satellite is July 31-Aug. 4, 2006."]
[5.3586273193359375, 2.950385093688965, "The Transmission Capacity of the IOV Payload Satellite Payload is Dynamic allocation."]
[10.357795715332031, 1.9666812419891357, "The Period (min) of the Meteor-1-2 Satellite is 97.7."]
[4.57049560546875, 6.872762203216553, "The Frequency of the X-band Band is 10.2 GHz."]
[6.838314056396484, 1.2752642631530762, "The Conference Date of the RazakSAT Satellite is Aug. 14-17, 2006."]
[6.093943119049072, 0.5469208359718323, "The Launch Date of the QBITO CubeSat is 18 April 2017."]
[11.614218711853027, 4.372859001159668, "The Distance from Earth of the Kepler-442b Exoplanet is 1,100 light-years."]
[5.7354583740234375, 5.415255546569824, "The GPS receiver of the TDX/TSX Satellite is IGOR GPS receiver."]
[4.619315147399902, 3.615777015686035, "The Objective of the Lemur-2 Satellite Constellation is Ship tracking via AIS (Automatic Identification System) with SENSE."]
[7.5756120681762695, 8.957845687866211, "The Depth Range of the Ma_MISS Spectrometer is Between 0 and 2\u2009m."]
[12.021921157836914, 3.2530884742736816, "The Inclination of the CeREs CubeSat Satellite is 85\u00ba."]
[7.369321823120117, 8.745501518249512, "The Spectral Channel 2 of the Satellite Imaging Satellite is 0.61-0.69 \u00b5m."]
[6.750879287719727, 0.9908623695373535, "The Meeting Date of the Nigerian National Geospatial Data Infrastructure Programme Programme is March 1-2, 2007."]
[7.941459655761719, 9.306941986083984, "The Ground Resolution at Apoapsis / Priapsis of the EXI instrument Imaging Instrument is 4.9 / 2.3 km per pixel."]
[4.297396183013916, 4.349309921264648, "The Interface of the CEPA Adapter is FRAM (Flight Releasable Attachment Mechanism)."]
[3.6224637031555176, 6.572701454162598, "The Data Rate of the VHF COTS transmitter Transmitter is 1200 to 9600 bit/s."]
[3.8141019344329834, 6.489712715148926, "The Downlink Speed of the Compact Laser Comms Terminals (CLCT) Communication Device is Up to 10 Gbit/s."]
[8.6346435546875, 6.132308483123779, "The Upward Drift of the Plasma Blobs Phenomenon is Invoked away from the magnetic equator."]
[8.717089653015137, 7.791220188140869, "The Function of the Electromagnetic Calorimeter Instrument Component is Measure the energy of particles interacting in its sensitive volume and image the shape of these interactions."]
[10.86607837677002, 3.1519477367401123, "The Width of the Nix Moon is 36 km."]
[8.442018508911133, 6.342426776885986, "The Drag-Free Performance Metric of the Drag-Free Technology Technology is Residual acceleration of the test mass in units of m/(s2Hz1/2)."]
[3.029897451400757, 6.628156661987305, "The Power of the RF Output Power Communication System is 3 W."]
[7.724659442901611, 8.427079200744629, "The Type of the PRISM-2 Instrument is Stereo high-resolution instrument."]
[5.783279895782471, 3.458390235900879, "The Institute of the DAXSS Payload is LASP (Laboratory for Atmospheric and Space Physics)."]
[1.5326659679412842, 4.779317855834961, "The Output Open Circuit Protection of the DC-DC converter Power Converter is Yes."]
[6.1847124099731445, 3.886941432952881, "The Orbit Data of the Satellite GFO is Medium Laser orbit data."]
[7.382469177246094, 1.0894378423690796, "The Project Start Date of the Heinrich Hertz Satellite is Mid-2009."]
[7.4917731285095215, 1.726527214050293, "The Demonstration Date of the Polar Sea Ice Detection Satellite is 3 February 2020."]
[5.494661808013916, 6.298038482666016, "The Diameter of the Antenna Satellite Component is 0.1m."]
[6.16208553314209, 6.483489513397217, "The Polarization of the Sentinel-1 Satellite is Selectable dual polarization."]
[8.423029899597168, 7.815991401672363, "The Usage of the RADMON Instrument is Used sporadically and depending on the system's instantaneous power demands."]
[2.0377373695373535, 3.806058406829834, "The Solar Arrays of the TacSat Satellite is Thin Film."]
[9.931639671325684, 3.671156167984009, "The Capture Box Separation of the ASTRO Satellite is < 1 m."]
[8.04538345336914, 8.104266166687012, "The Measurement Technique of the Biological Specimens Samples is Optical absorbance and density."]
[6.264296054840088, 5.796189308166504, "The Spatial Baseline of the GF-3 SAR Satellite is 250 m."]
[3.002702474594116, 6.684541702270508, "The X-band Tx Power of the RF communications Communication System is 6 W."]
[6.8254523277282715, 7.214189052581787, "The Data Update Frequency of the IMERG Algorithm is Every half-hour."]
[9.41642951965332, 5.882802486419678, "The Function of the Magnetorquer Attitude Actuation Device is Allows full 3-axis attitude control experimentation to be performed."]
[8.257964134216309, 10.321887969970703, "The Image Gain of the PMC-2 Imagers Imaging System is 1~5 levels."]
[2.41055965423584, 4.3428449630737305, "The Electrical Power System of the ESTCube-1 Satellite is COTS solution."]
[4.9453535079956055, 6.654108047485352, "The Gain of the Antenna Communication System is Maximum gain normal to the spin axis of the bus."]
[1.507112741470337, 5.024101734161377, "The Voltage Output of the PSU Power Supply Unit is 3.3 V."]
[7.68262243270874, 7.254729270935059, "The Scan Mirror of the TEMPO Instrument is Included."]
[5.369477272033691, 7.275929927825928, "The Beam width of the Sub-mm Band is 4.5 mrad."]
[10.856311798095703, 4.155672073364258, "The Purpose of the Kepler Mission Space Telescope is Detection of extra-solar planetary systems."]
[8.582230567932129, 8.844316482543945, "The Input Angle alpha of the Long Wavelength Band Spectrometer is 21.9\u00ba."]
[7.992091655731201, 9.058446884155273, "The Bandpass of the Short Wavelength Band Spectrometer is 900-1150 \u00c5."]
[3.897156000137329, 6.479031562805176, "The Modulation Scheme of the VHF COTS transmitter Transmitter is BPSK."]
[5.523103713989258, 3.8186757564544678, "The Identification Time of the CSpOC Catalog Catalog is 8 days after launch."]
[3.6987104415893555, 6.6073737144470215, "The Data Transmission Rate of the X-band Communication Band is 25 Mbit/s."]
[6.352602005004883, 1.947034239768982, "The Development Status of the G\u00f6kt\u00fcrk-1 Satellite is Stuck in a production facility in France."]
[6.5895280838012695, 0.35862404108047485, "The Retirement Date of the CBERS-2 Satellite is Late 2007."]
[10.321568489074707, 3.739447832107544, "The Orbit Shape of the XO-3b Exoplanet is Eccentric (oval)."]
[8.83309555053711, 5.329504489898682, "The Role of the Central Bulkhead Assembly Satellite Component is Facilitate connectivity of the imager instrument to the spacecraft platform in the desired semi-kinematic configuration."]
[4.633575439453125, 4.3889546394348145, "The Platform of the Ground Software Architecture System is Windows or Linux PCs."]
[8.810258865356445, 10.224949836730957, "The Objectives of the C3D Instrument CMOS Sensor is 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."]
[11.665313720703125, 1.804048776626587, "The URL of the MASCOT Lander Lander is http://arc.aiaa.org/doi/pdf/10.2514/6.2016-2386."]
[8.272123336791992, 9.116656303405762, "The Image Displacement of the Quad-cell Instrument is <10 -2\u03c0 sensitivity."]
[6.646493434906006, 1.7894216775894165, "The Data Mapping Period of the Envisat Satellite is 1994 to 2010."]
[7.324945449829102, 5.598891735076904, "The Location of the Polar Vortex Meteorological Phenomenon is High above the North Pole in the polar stratosphere."]
[7.845170974731445, 1.5329370498657227, "The Crime Scene Investigation Start Date of the Hera Spacecraft is Late 2026."]
[9.281458854675293, 6.251911163330078, "The Attitude Determination Device of the ACS Attitude Control Subsystem is Commercial star tracker, AST (Autonomous Star Tracker)."]
[9.916486740112305, 8.549748420715332, "The Sensitivity of the VT Telescope is High sensitivity, in particular at long wavelength."]
[5.234860420227051, 2.7993738651275635, "The Hardware Maintenance Costs of the MEOLUT Next Local User Terminal is The lowest on the market."]
[7.622610569000244, 1.4490395784378052, "The Mission Extension Announcement Date of the LADEE Satellite is Jan. 31, 2014."]
[3.130429267883301, 6.826115608215332, "The Output Power of the TXS S-band Transmitter/Transceiver is 28 dBm."]
[5.615269660949707, 6.6091508865356445, "The Lunar Axial Tilt of the DSN Stations Antenna is 4.5\u00ba to 5.5\u00ba."]
[7.019632816314697, 0.13032694160938263, "The End of Life Date of the MOMS Satellite is 16 August 1999."]
[8.190865516662598, 3.2239770889282227, "The Communication System of the TanDEM-X Satellite is X-band inter-satellite link."]
[5.103456020355225, 6.0596089363098145, "The Clock Frequency Stability of the Spacecraft Satellite is PHM (Passive Hydrogen Maser):<4.5 x 10 -14  at 30000 s."]
[10.347490310668945, 9.432680130004883, "The Mission Type of the IRIS Satellite is 3-axis stabilized, sun-pointed."]
[8.50705623626709, 2.5807132720947266, "The Maneuvers per Year of the ARTEMIS Satellite is Approximately two."]
[10.050846099853516, 4.071388244628906, "The Solar Sail Size of the NEA Scout Solar Sail Technology Demonstration Spacecraft is 925 square feet (86 m2)."]
[7.325352191925049, 7.117771148681641, "The Boat Detection of the VIIRS Instrument is 10,000 to 20,000 boats every night."]
[13.061201095581055, 4.096185684204102, "The Target Stars of the Gaia Space Astrometric Mission is > 1000 million."]
[6.064735412597656, -0.031920790672302246, "The Launch Date of the Galileo satellites Satellite is 21 October 2011."]
[6.615334987640381, 2.645775079727173, "The Mission Type of the FalconSat-7 Satellite is Proof-of-concept."]
[7.276787281036377, 7.052428245544434, "The Purpose of the VCST Team is Provide independent evaluation of the VIIRS calibration and SDR product quality."]
[6.6108012199401855, 7.996699333190918, "The Pulse Width of the Lasers Light Source is 1 to 6 ms."]
[7.701481342315674, 0.1427495777606964, "The Kurs-NA Radio System Test Start Date of the Prichal Module is October 20."]
[6.012030124664307, 3.148275852203369, "The Developer of the Space Launch System Spacecraft  is NASA/MSFC."]
[8.528892517089844, 9.23051929473877, "The Ground Pixel Size of the WAOSS-B Sensor is 185 m."]
[4.801681041717529, 0.8975681662559509, "The Fundraising Goal of the Inspiration4 Mission is $100 million."]
[9.424385070800781, 6.656564235687256, "The Radial Position Control of the OAP to Housing Connection is Close-fitting sleeve."]
[11.707314491271973, 7.414888381958008, "The Mission Start Date of the Deep Space Atomic Clock Clock is Oct. 9, 2012."]
[6.948270320892334, -0.03136426955461502, "The End of Life Date of the FedSat Satellite is 14 Dec 2005."]
[6.717159271240234, 4.257163047790527, "The Affiliation of the CRISTAL Satellite Mission is Copernicus program."]
[5.3237175941467285, 6.677026748657227, "The Look Angles of the Antenna Subsystem Communication is 42.62\u00ba and 49.38\u00ba."]
[6.061249732971191, 2.63874888420105, "The Affiliation of the Shuaib Lwasa Professor is Urban Action Lab, Makerere University."]
[11.720613479614258, 5.350200176239014, "The Discovery Date of the GRB 150101B Gamma Ray Burst is January 2015."]
[4.8749518394470215, 1.952102541923523, "The Number of Operational Satellites of the HY-2 Satellite is 3."]
[4.444039344787598, 7.071659088134766, "The Size of the Miniaturized X-band transponders Communications System is 5 cm x 5 cm x 7.6 cm."]
[4.857959270477295, 2.5985820293426514, "The Communication System of the CM1 and CM2 6U CubeSats is Phased array communication system."]
[4.101932048797607, 5.644801616668701, "The Data downlink of the ALOS/PRISM Satellite is 277.52 Mbit/s (Ka-band)."]
[9.328898429870605, 0.7019698023796082, "The Expected Extended Lifetime of the Aeolus Satellite is Another year."]
[8.893610000610352, 1.7666035890579224, "The Last Chance to View of the BepiColombo Satellite is 14 June 2017."]
[6.3986945152282715, 1.3288360834121704, "The Presentation of the PRISMA Satellite is Flight Results from PRISMA Formation Flying and Rendezvous Demonstration Mission."]
[4.832823276519775, 0.9106962084770203, "The Funding from ESA of the Copernicus Environmental Monitoring Satellites is 2.55 billion euros."]
[9.087026596069336, 7.435895919799805, "The Detection Capability of the TimePix radiation sensors Sensor is Able to detect radiation flux spikes of over 1000 times the background level during a single solar particle event (SPE)."]
[5.857545852661133, 6.415119647979736, "The Frequency of the SAR Synthetic Aperture Radar is L-band (1.275 GHz)."]
[5.18164587020874, 4.718267917633057, "The Location of the RF Backup Station Ground Station is Matsumoto."]
[9.452213287353516, 8.624069213867188, "The Material of the X-ray mirrors Optical Instrument is Nickel."]
[5.012423038482666, -0.1606292575597763, "The Launch Date of the OneWeb Satellite Constellation is 7 February 2020."]
[5.475062847137451, 6.43587589263916, "The Length of the Spin Plane Dipole Antenna Antenna is 90 m."]
[6.247605323791504, 5.935429096221924, "The FPGA Co-processor of the SGR-ReSI GNSS Reflectometry Instrument is Virtex 4."]
[3.2446370124816895, 5.310227394104004, "The Capacity of the Image Storage Data Storage is 8 GB + 32 GB of science data."]
[6.45433235168457, 2.399611473083496, "The Computing Resource of the 'Fight club' asteroid simulations Simulation is Bluecrab supercomputer cluster."]
[8.537026405334473, 6.461103916168213, "The 2.5 m of the MPO Boom Length is The 2.5 m long boom carrying the magnetometer sensors onboard ESA\u2019s BepiColombo MPO."]
[6.9233012199401855, 4.1069746017456055, "The Operational Modes of the Tsubame microsatellite Satellite is Detumbling mode, Safe mode, Standby mode, Camera mode, Gamma-ray mode."]
[9.44893741607666, 7.289427757263184, "The Range of Observable Flow Angles of the FSU Solar Wind Faraday Cup is 56\u00ba FOV."]
[6.242948055267334, 6.379415035247803, "The 3 km of the Radar Data Spatial Resolution is The radar data will provide the freeze/thaw measurement with 3 km spatial resolution."]
[11.676752090454102, 2.601900815963745, "The Secondary Body Diameter of the Didymos Asteroid is About 150 m."]
[5.603605270385742, 6.454940319061279, "The Dimensions of the SAR Antenna Antenna is 1.5 m x 15 m."]
[9.778742790222168, 1.4105170965194702, "The Deployment Wait Time of the Payloads Satellite Components is 15 seconds."]
[9.970414161682129, 1.2996512651443481, "The Lock Establishment Time of the STEREO-B Satellite is 6:27 p.m. EDT."]
[7.851253032684326, 4.418747425079346, "The Image Resolution of the DEIMOS-2 Satellite is 0.75 m per pixel."]
[5.28412389755249, 2.339329481124878, "The Flight Preparation Contributors of the SAPPHIRE Satellite is Students at Washington University (WU) in St. Louis, MO."]
[8.2672758102417, 10.518073081970215, "The Average Power of the 4-band CCD Imager Instrument is 6 W."]
[9.569555282592773, 5.7437543869018555, "The Manufacturer of the Torque Rod Attitude Control Device is SSTL."]
[5.816992282867432, 8.557313919067383, "The Band Frequency of the MicroWave Humidity Sounder-2 Sounder is 118 GHz."]
[4.884665012359619, 8.935297966003418, "The Wind Measurement of the InSight Spacecraft is Continuous."]
[2.2685117721557617, 4.089076519012451, "The Number of Load Cells of the Truss Structure is 6."]
[4.935909271240234, -3.1837921142578125, "The | of the Zhongkan Tang, Rakhitha Chandrasekara, Yue Chuan Tan, Cliff Cheng, Kadir Durak & Alexander Ling Authors is | False."]
[9.654326438903809, 5.957059383392334, "The Control Method of the ADCS Attitude Determination and Control Subsystem is Magnetic torque coils (magnetorquers)."]
[8.043062210083008, 1.381385087966919, "The Conference Date of the Solar Orbiter Mission is Oct. 14-17, 2008."]
[6.827125549316406, 7.451992511749268, "The Operational Modes of the MIRAS Instrument is Dual-polarization mode, Full polarimetric mode, Calibration modes."]
[5.693024158477783, 6.915834903717041, "The Antenna Diameter of the DORIS Instrument is 160 mm."]
[7.652548313140869, 7.864861488342285, "The Z Accuracy of the Planimetric Accuracy Assessment Assessment is <0.3 m."]
[1.0654233694076538, 4.3089094161987305, "The Battery Type of the EPS Electric Power Subsystem is 2 x 66 Ah Li-ion batteries."]
[7.639713764190674, 8.784335136413574, "The Spectral Resolution of the SOSP Satellite is 1 nm in UV/VIS, 20 nm in IR."]
[9.236391067504883, 4.208995819091797, "The Solar Wings Span of the Satellite Spacecraft is 25 m."]
[6.964451789855957, 0.2532867193222046, "The Launch Date of the AstroSat Satellite is Unknown."]
[5.353094100952148, 3.263524055480957, "The Bus Type of the DSP satellites Satellite is CAST968."]
[5.866613864898682, 1.5527759790420532, "The Launch Vehicle of the Galileo Satellite Constellation is Ariane 5."]
[12.144394874572754, 5.388889789581299, "The Expansion Rate of the Universe Cosmological Entity is Accelerating."]
[6.068082332611084, 1.9515070915222168, "The Additional Experiments of the Kounotori H-II Transfer Vehicle is 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)."]
[3.8152120113372803, 4.513173580169678, "The FPGA of the OBC On-Board Computer is Radiation-hardened."]
[5.939323425292969, 3.9070284366607666, "The Data Fusion Center of the Satellite GFO is ADFC (Altimeter Data Fusion Center) also located at NavOceano."]
[8.695172309875488, 5.313315391540527, "The Pointing Stability of the Spacecraft Satellite is 0.3 arcsec/s."]
[8.840866088867188, 3.295518398284912, "The Orbit Type of the Unicorn-2L, -2M and -2N Satellites is Low-Earth."]
[7.4819111824035645, 6.884599685668945, "The Image Capture Date of the DESIS Instrument is 29 November 2019."]
[11.413952827453613, 3.888941526412964, "The Phosphine Upper Limit of the Mars Planet is Unknown."]
[5.1349873542785645, 5.985835075378418, "The Quantity of the S&F antennas Communication is 4."]
[9.497366905212402, 4.3771867752075195, "The Width of the Large Space Simulator (LSS) Vacuum Chamber is 10 m."]
[6.61833381652832, 7.971333026885986, "The Pulse Width of the Laser Instrument is 1~999 \u00b5s."]
[8.570260047912598, 8.681672096252441, "The Alignment and Testing of the NIRSpec Filter and Grating Wheel Assembly Space Mechanism is Unknown."]
[7.1714043617248535, 0.37452003359794617, "The Launch Contract Date of the Muninn Satellite is Early 2023."]
[4.216370105743408, 6.616089820861816, "The VHF Band Frequency of the RF Communications Communication Subsystem is 144 MHz."]
[11.606873512268066, 5.849874019622803, "The Description of the Gravitational Lensing Method Space Exploration Tool is Photons deviate from the rectilinear direction when passing near a massive body under the influence of its gravitational field."]
[6.672708511352539, 2.2952523231506348, "The Instruments of the GPM Constellation Satellite Constellation is Radiometers."]
[8.282478332519531, 5.2644853591918945, "The Objective of the NanoSatC-BR Satellite is 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)."]
[6.532933712005615, 7.505422115325928, "The Prime Developer of the Laser Transmitter Laser is Selex Galileo."]
[4.148209571838379, 5.047029972076416, "The Provider of the ODTML Data Collection System is ONR (Office of Naval Research)."]
[3.7506320476531982, 5.965790271759033, "The Downlink Capacity of the Bartolomeo Payload Communication System is Up to 1 GB per day."]
[7.4967193603515625, 7.507169723510742, "The Type of the OCI Instrument is Hyperspectral radiometer."]
[5.311413288116455, 4.605175971984863, "The Locations of the IOT Stations Ground Station is Redu, Belgium and Chilbolton, UK."]
[6.028561592102051, 9.641095161437988, "The Electronic Unit Mass of the Instrument Sensor is 2.82 kg."]
[6.342174053192139, 7.239272594451904, "The Swath Width of the ALT Experiment Altimeter is Varies from 2.4 to 12 km."]
[5.019521713256836, 6.042455673217773, "The ELF Signal Energy of the QuakeSat Satellite is Between 10 Hz and 150 Hz."]
[6.42041015625, -0.7180616855621338, "The SIS/URE of the QZS-1 Satellite is 34 cm (rms)."]
[6.813043594360352, 3.295163869857788, "The Mission Status of the NeuSAR Satellite is Operational (nominal)."]
[6.864282131195068, 4.050175666809082, "The Application Fields of the HJ-1 minisatellite constellation Satellite Constellation is 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 mo."]
[10.314902305603027, 9.347073554992676, "The Flare Class of the IRIS Observatory is X-class."]
[8.565674781799316, 5.547670841217041, "The Fine-Pointing Range of the GT Fine-Pointing Error Signal Provider is Approximately 70 arcsec."]
[7.307163715362549, 2.251577377319336, "The Launch Date of the Orbiting Carbon Observatory-2 Satellite is Unknown."]
[9.989798545837402, -0.8465480208396912, "The Orbit of the Kestrel Eye-2M Microsatellite is Near the ISS."]
[4.668560028076172, 7.18398380279541, "The Data Download Capacity of the GimmeRF Radio Instrument is About 10 Mbit per orbit."]
[7.626636028289795, 0.9786010384559631, "The Announcement Date of the New Method Process is 20 July 2021."]
[7.897850513458252, 9.99463939666748, "The Calibration of the Advanced Land Imager Imaging Device is Spatial."]
[10.169663429260254, 3.506296157836914, "The Eccentricity of the Satellite Communication is 0.0024."]
[5.696944236755371, 2.366304636001587, "The Antenna Type of the Eutelsat Quantum Satellite is Electronically steerable."]
[6.241395950317383, 8.24071216583252, "The Frequency Conversion of the Microwave Assembly Signal Processing Device is 24 and 32 GHz."]
[3.853998899459839, 2.3061821460723877, "The Side Panel Thickness of the ESTCube-1 & -2 CubeSat is 1 mm."]
[8.520249366760254, 7.441488265991211, "The Search Coil Length of the ULF Sensor Sensor is 20 cm."]
[8.814105987548828, 8.156817436218262, "The Al Shielding Thickness of the RADFET Dosimeters Dosimeter is 165 \u00b5m."]
[8.884711265563965, 5.292672157287598, "The Capability of the AeroCube-4 Satellite is Can slew and maintain pointing at a specific ground target."]
[3.6373653411865234, 6.33987283706665, "The Nominal Rate of the S-band Uplink Communication System is 16 kbit/s."]
[7.223502159118652, 0.7113694548606873, "The Launch Date of the SPARCS Satellite is Not earlier than October 2021."]
[6.118309020996094, 6.2783403396606445, "The Function of the Digital Beam Forming (DBF) Application is Wide swath imaging and ambiguity suppression."]
[7.370458126068115, 4.049654960632324, "The Type of the SPOT-6 Satellite is Optical imaging specialist."]
[7.6191511154174805, 8.886798858642578, "The Wavelength of the Responsivity Measurement Instrument is 1064 nm."]
[9.254316329956055, 6.550843715667725, "The Field of View of the Star Tracker Optical Sensor is 2\u00ba x 2\u00ba."]
[8.086849212646484, 5.6721882820129395, "The Stabilization Rate of the FORTE Spacecraft is 1 Hz."]
[8.96396255493164, 8.808741569519043, "The Cross-track FOV of the TIR Subsystem Imaging System is \u00b111.5\u00ba."]
[2.2083945274353027, 4.457807540893555, "The Power Source of the CubeSats Satellite is Does not require any extra power from the rocket."]
[10.048382759094238, 1.562150239944458, "The Orbital Period of the Suomi-NPP Satellite is 101 minutes."]
[7.79336404800415, 3.972817897796631, "The Orbital Phase of the Sentinel-1A and Sentinel-1B Satellites is 180\u00ba."]
[5.170119285583496, 2.2269012928009033, "The Ride Capability of the CubeStack Multi CubeSat Adapter is Tertiary canisterized."]
[9.386068344116211, -0.6789348721504211, "The Presentation Date of the Delfi-n3Xt Nanosatellite is Sept. 29 to Oct. 3, 2008."]
[9.93847942352295, 9.54383659362793, "The Science Objectives of the SAGE-III Instrument is Characterize tropospheric and stratospheric aerosols and upper tropospheric and stratospheric clouds."]
[4.977634429931641, 6.083423614501953, "The Frequency Bands of the Antenna for Navigation Antenna is L1/L2."]
[3.6484246253967285, 6.280983924865723, "The Data Rate of the Uplink Communication System is 1 kbit/s."]
[11.133113861083984, 6.241786003112793, "The Interaction in Atmosphere of the Neutrons Radiation is Absorption by nuclear reactions, decay, Earth albedo neutron flux."]
[10.215274810791016, 3.98884654045105, "The Speed of the Proximity Flyby Maneuver is 800 m/day."]
[6.668155670166016, 6.289924621582031, "The Accuracy of the SeaWinds scatterometer Scatterometer is 2 m/s."]
[9.038657188415527, 8.851073265075684, "The Design Purpose of the CrIS Optical System is Provide an optimum combination of optical performance and compact packaging."]
[3.830385446548462, 6.147036552429199, "The Average Download Capacity of the Panama ground station Ground Station is 1.2 GB/day."]
[6.063987731933594, -0.07804278284311295, "The Orbit Placement Date of the Galileo 2nd Generation Satellites Satellite is End of 2024."]
[7.704641342163086, 3.3530778884887695, "The Data Availability of the Landsat 7 ETM+ SLC-off and Landsat 5 TM Satellites is New global acquisitions July 2008."]
[8.655277252197266, 10.337361335754395, "The Image Resolution of the Visual Sensor Array Sensor Array is 13376 x 10000 pixels."]
[3.490936040878296, 2.3461756706237793, "The Size of the PSat-2 Satellite is 1.5U."]
[10.238842010498047, 5.71115255355835, "The Positive and Negative of the Tether Charging Modes Test Procedure is Both positive and negative tether charging modes will be tested during this phase."]
[11.6637601852417, 1.7884283065795898, "The Expected Operation Duration of the MASCOT Lander is Approximately 16 hours."]
[8.374974250793457, 9.28844165802002, "The FWHM at 80 nm of the EUV Simulation Simulation is 7 arcmin."]
[9.27425479888916, 5.741544723510742, "The Capability of the iADCS100 Attitude Determination and Control System is Precisely pointing and slewing a 3U CubeSat."]
[9.387248992919922, 7.321527481079102, "The Electric Field of the FSU Faraday Cup Sensor Unit is Set up between the modulator grid and the adjacent ground grids."]
[7.293620586395264, 7.568788528442383, "The Measurement Detailed of the VHRR Instrument is 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)."]
[6.22102689743042, 0.9117648005485535, "The Project Start Date of the Argos-3 Onboard Instrumentation is 1997."]
[10.053723335266113, 2.736138105392456, "The Ballistic Coefficient of the PUNCH Mission Satellite is Increased by adding ballast."]
[4.9711384773254395, 4.728683948516846, "The Requirements of the KE Ground Station Ground Station is 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)."]
[7.608889579772949, 7.620121955871582, "The Detection of the MOMA Instrument is Direct detection of indigenous martian organic molecules and some thermally released inorganic molecules or laser-desorbed fragments of inorganic minerals."]
[7.321829795837402, 1.907543659210205, "The Overview Seminar of the Gravity Probe B Satellite is June 17, 2009."]
[6.615082263946533, 2.8095874786376953, "The Video Capabilities of the Carbonite Series Small Satellite Platforms is High-performance."]
[11.785444259643555, -0.9654598832130432, "The Payload Capacity of the Super Strypi launcher Launcher is 300 kg."]
[9.381857872009277, 2.6199257373809814, "The Retrieval Date of the EURECA Satellite is June 21 - July 1, 1993."]
[6.001775741577148, 4.2433247566223145, "The Manufacturer of the Canadarm-1 Remote Manipulator System is Canadian Space Agency."]
[7.797125816345215, 9.864632606506348, "The Spectral Bands of the TrueColour Imager Optical Imager is 9 bands."]
[6.124906063079834, 3.154017210006714, "The Assembly Location of the BRITE Satellites Satellite is Space Research Center in Warsaw."]
[6.519379615783691, 2.6824562549591064, "The URL of the Galileo Satellite Navigation System is https://www.esa.int/Applications/Navigation/406_Day_celebrating_Galileo_saving_lives."]
[10.343721389770508, -1.1506396532058716, "The Mass of the Dove-1 Nanosatellite is ~ 5.8 kg."]
[5.401304244995117, 1.3605118989944458, "The Fairing Recovery of the Falcon 9 Rocket is Two recovery vessels were dispatched to sea to retrieve the fairing halves from Tuesday night\u2019s mission."]
[6.398820400238037, 3.7666280269622803, "The Operations Manager of the GOES-O Satellite is National Oceanic and Atmospheric Administration (NOAA)."]
[4.193423271179199, 4.457017421722412, "The Components of the PMS System is TPU (Thermal Power Unit) and MMU (Memory Management Unit)."]
[6.067241668701172, 2.412700653076172, "The Program of the TacSat-3 Satellite is ORS (Operational Responsive Space)."]
[5.309816360473633, 4.881842613220215, "The Communication Relay Terminals of the Pl\u00e9iades-Neo satellites Satellite is Tesat Spacecom laser."]
[8.149949073791504, 7.588284015655518, "The Calibration Steps of the Detector Calibration Process is Apply bad pixel map, followed by gain and offset correction to flat-field the sensor output."]
[12.176791191101074, 3.296092987060547, "The Orbit Inclination of the Odin Satellite is 97.77\u00ba."]
[10.082324028015137, 3.0311038494110107, "The Operational Altitude of the GNOMES-1 Satellite is 650 km."]
[4.717532634735107, 2.0946197509765625, "The Quantity of the Flock-4v CubeSats is 14."]
[9.677910804748535, 8.184309005737305, "The Main Detector of the GRS Gamma-Ray Spectrometer is 12 cm diameter x 7.6 cm long CsI (Tl) crystal."]
[11.085610389709473, 4.968214988708496, "The Coronal Mass Ejections Observed of the SOHO Satellite is More than 20,000."]
[7.730164051055908, 7.307794094085693, "The Angular Resolution of the IMAP-Ultra Instrument is Comparable or better angular resolution than IMAP-Hi."]
[8.447092056274414, 9.1128568649292, "The Band 6 of the R3 Sensor Sensor is Green."]
[12.065664291381836, 3.2307863235473633, "The Inclination of the Yubileyniy-2/MiR Satellite is 82.5\u00ba."]
[8.801189422607422, 1.9509387016296387, "The Launch Date of the New Horizons Spacecraft is January 19, 2006."]
[9.323846817016602, 7.4478983879089355, "The Concentration Range of the DE probe Charged Particle Probe is 10^4 - 10^7 cm^-3."]
[7.761038303375244, 9.028308868408203, "The Spectral Resolution of the Spectrometer Spectrometer is <1.25 cm -1."]
[7.355522155761719, 1.028083324432373, "The Mission End Date of the Deep Space 1 Satellite is Unknown."]
[8.7103853225708, 8.067708969116211, "The Detector Unit of the DOSTEL Radiation Detector is Five silicon sensors."]
[11.683944702148438, -1.1905796527862549, "The Launch Mass of the Satellite Communication Satellite is ~5.8 tons."]
[4.33693265914917, 5.64475679397583, "The S-band Usage of the CBERS-2B Satellite is TT&C services."]
[3.907703399658203, 5.4408087730407715, "The Levels of the CSI Data Communication is 4."]
[11.626564979553223, 0.7694649696350098, "The Rocket Weight of the Chang'e-5 Lunar Mission is 870 metric tons."]
[3.884031295776367, 6.548923015594482, "The Types of the RFI Sources Interference is In-band emissions, Excessive out-of-band emissions, Spurious emissions."]
[4.930830001831055, 1.8961397409439087, "The Number of Deployable Subsatellites of the EAGLE Spacecraft is 1."]
[6.764997959136963, 0.6670486330986023, "The Launch Date of the GOES-T Satellite is March 2022."]
[7.3913798332214355, 0.9284511804580688, "The Launch Date of the Sentinel-3A Satellite is Unknown."]
[7.25429105758667, 6.146361351013184, "The Publication Year of the Case studies of aerosol retrievals Study is 2002."]
[7.051051616668701, 0.7514593005180359, "The Development Start Date of the BDS Satellite is 1990s."]
[7.624839782714844, 4.838716506958008, "The Calibration Images of the PROBA-V Satellite is 2.622."]
[4.244142532348633, 4.8507184982299805, "The Data Transmission Protocols of the ETS-VIII Spacecraft is CCSDS."]
[2.9976048469543457, 6.618138313293457, "The Output Power of the RF communications Communication System is ~ 1W."]
[8.910331726074219, 8.705885887145996, "The Moving Parts of the LORRI Imaging Instrument is No."]
[5.526061534881592, 1.3592904806137085, "The First Stage Landing Location of the Falcon 9 Rocket is Atlantic Ocean."]
[10.196134567260742, 4.796017646789551, "The Propellant of the Busek\u2019s miniaturized electric thrusters Propulsion System is Iodine."]
[6.08190393447876, -0.04361771047115326, "The Launch Date of the Galileo Second Generation (G2) Satellite Constellation is 31 December 2024."]
[8.865543365478516, 10.255099296569824, "The Detector Type of the Camera Imaging Device is CMOS."]
[8.880363464355469, 7.722403049468994, "The Measurement Objective of the EPISEM Instrument is Measure the omnidirectional integral flux."]
[10.300508499145508, 5.475857734680176, "The Maximum Temperature of the Xenon Gas Tank Propellant Storage is 50\u00baC."]
[5.93474817276001, 0.7755295038223267, "The Presentation Date of the NANOSATC-BR Cubesat Program Satellite Program is Oct. 1-5, 2012."]
[9.311691284179688, 8.185948371887207, "The Internal Data Storage of the RAMIS Radiation Detector is 2."]
[1.0078016519546509, 4.397251605987549, "The Battery Capacity of the EPS Electrical Power Subsystem is 108 Wh."]
[8.4861421585083, 8.04492473602295, "The Exposures per Field of the Euclid Reference Survey Survey is 4."]
[8.736674308776855, 9.089608192443848, "The IFOV of the AVHRR/3 Instrument is 1.1 km at nadir."]
[0.9819064140319824, 4.329607009887695, "The Battery pack capacity of the EPS Electric Power Subsystem is 3.6 Ah."]
[7.6918625831604, 7.429044723510742, "The Instrument Types of the Instruments EO is Multiple direction/polarisation radiometers, Imaging multi-spectral radiometers (vis/IR), High resolution optical imagers, Earth radiation budget radiometers, Atmospheric chemistry."]
[5.357001304626465, 1.3972654342651367, "The Booster Reuse of the Falcon 9 Rocket is 7 trips to space and back."]
[7.394800662994385, 10.094514846801758, "The Instrument Power of the HySI Hyperspectral Imager is 16 W."]
[7.563417911529541, 6.61726188659668, "The B/H of the Instrument Satellite Instrument is 0.57."]
[4.704565525054932, 1.8842884302139282, "The Number of Satellites of the Spire Satellite Constellation is Over 100."]
[6.6462249755859375, 4.489040374755859, "The Data Applications of the NISAR Satellite is Monitoring of agricultural biomass, assessing disasters, studying snow and glaciers, studying Indian coastal and near-shore oceans."]
[11.73768424987793, 1.6588003635406494, "The Touchdown Time of the Philae Lander is 17:25:26 GMT."]
[8.106149673461914, 10.017372131347656, "The Maximum Upper Band Edge of the Pan (WorldView-1) Imager is 900 nm."]
[13.046029090881348, 4.103012561798096, "The Binary Star Catalogue of the Gaia Satellite is More than 800 thousand binary systems."]
[8.10629653930664, 5.232448577880859, "The Accuracy of the SubWave Underground Geolocation System is 10m."]
[9.03559684753418, 7.9555487632751465, "The Time Resolution of the Particle Detector Instrument is 1 s."]
[11.16583251953125, 6.765604496002197, "The Area of the X-ray Satellite Navigation Navigation System is 2000 cm2."]
[7.6480326652526855, 4.991143226623535, "The Signal Health of the Galileo Satellite Navigation System is 97.33%."]
[9.430621147155762, 9.089103698730469, "The Effective Focal Length of the Telescope Optical Instrument is 1150 mm."]
[8.932174682617188, 10.469566345214844, "The Image Sensor Resolution of the Wide-angle camera Camera is VGA resolution (640 x 480 pixels)."]
[10.458736419677734, 7.65783166885376, "The Material of the IDA Dewar is Titanium."]
[7.9300336837768555, 6.7019219398498535, "The Frequency of the Solar Calibration Calibration is Daily."]
[6.0531182289123535, 9.473625183105469, "The Mass of the UVS Instrument is 3.98 kg."]
[10.824077606201172, 3.8328640460968018, "The Data Stack Height of the Nancy Grace Roman Space Telescope is 330 miles (530 km) high after a single day."]
[5.330422401428223, 4.648951530456543, "The Location of the TIRA Radar Tracking Station is FGAN site in Wachtberg near Bonn, Germany."]
[5.955499172210693, 3.0982720851898193, "The Owner of the Lemur-2 Satellite is Spire Global."]
[9.472192764282227, 9.202500343322754, "The Pupil Diameter of the Telescope Optical Instrument is 75.6 mm."]
[8.188547134399414, 9.515691757202148, "The Type of Array of the SWIR Detector is HgCdTe."]
[9.012484550476074, 8.794859886169434, "The Detector Quantity of the TIR Subsystem Imaging System is 10."]
[8.686639785766602, 7.1153564453125, "The Measurement Error of the Acceleration Sensor is Random <0.1 G (1\u03c3), Bias < 0.25 G, Nonlinearity < 2%."]
[3.8862390518188477, 5.69706916809082, "The Transmission Speed of the KIZUNA Satellite Communication Technology is 3.2 Gbit/s."]
[6.539135456085205, -0.08826681226491928, "The Launch Date of the IRNSS-1E Satellite is January 20, 2016."]
[7.980584621429443, 5.3299055099487305, "The GPS/UTC Accuracy of the Data Handling Subsystem Subsystem is 100 \u00b5s."]
[8.7316255569458, 7.921145439147949, "The Mass Resolution of the INMS sensor Ion Mass Spectrometer is The mass resolution is limited by uncertainties in energy dispersion, time resolution and time of flight path."]
[1.867040753364563, 4.218085765838623, "The Solar Panels Power Generation (Average) of the EURECA Spacecraft is 1 kW."]
[6.390986442565918, 3.0137932300567627, "The Partners of the Rosalind Franklin Rover is ESA and the Russian State Space Corporation, Roscosmos."]
[1.5917744636535645, 4.4837775230407715, "The Efficiency of the 28 V Regulator Regulator is 93%."]
[10.8646879196167, 2.0067567825317383, "The Orbital Altitude of the Swarm-A (Alpha) Satellite is \u2264 460 km."]
[4.852373123168945, 1.6113719940185547, "The Profiles Per Day of the FormoSat-3 / COSMIC mission Satellite Mission is 1,600~1,800."]
[8.504459381103516, 6.883949279785156, "The Stated Capabilities of the Honeywell Sensor Sensor is Unknown."]
[13.808835983276367, 0.7662830352783203, "The Orbital Slot of the GSAT-0103 Satellite is C04."]
[7.55010461807251, 4.057702541351318, "The Orbit of the Sentinel-1C Satellite is Sun-synchronous orbit with an altitude around 690 km."]
[5.935299873352051, 6.475311756134033, "The Incidence Angle Range of the SAR Synthetic Aperture Radar is 32\u00ba at the near range and 38\u00ba at the far range."]
[6.783668518066406, 0.6387368440628052, "The Sensor Update Date of the ROCSat-1 Satellite is Unknown."]
[7.124844074249268, 1.5230954885482788, "The Exploration Start Date of the Cluster Satellite Constellation is July 1, 2015."]
[4.808889389038086, 0.9121229648590088, "The Prize Amount of the Google Lunar X-Prize Competition is $20 million."]
[9.119325637817383, 0.9939756393432617, "The Potential of the ORS Office is Rapidly fly a spare replacement instrument to provide continued temporal measurements."]
[10.309087753295898, 2.9465458393096924, "The Periherm of the MMO Spacecraft is 400 km."]
[5.570367813110352, 3.3742659091949463, "The Purpose of the European Service Module Spacecraft Module is Propel NASA\u2019s Orion spacecraft to the Moon."]
[6.80499792098999, 9.063294410705566, "The Dimensions of the TEP Absorber 1 Absorber is 5.4 cm cylinder."]
[4.595195770263672, 7.676168918609619, "The Bandwidth of the FIELDS suite Sensor Suite is 20 MHz."]
[6.702359676361084, 2.975863218307495, "The Launcher of the Sentinel-1B Satellite is Soyuz-STA/Fregat vehicle (VS 14) of Arianespace."]
[6.272982120513916, 4.2721710205078125, "The Science Objectives of the TROPICS Constellation of CubeSats is Relate the occurrence of intense precipitation cores (convective bursts) to storm intensity evolution."]
[9.9050931930542, 1.3785109519958496, "The Response Time of the Pleiades-1A Satellite is Within four hours."]
[6.436791896820068, 5.631801128387451, "The Atmospheric Penetration Depth of the GNSS-RO Instrument Instrument is Greater than other radio occultation instruments."]
[9.961085319519043, 9.604826927185059, "The Departure Date from MSSS of the ShadowCam Instrument is 13 August 2021."]
[6.516621112823486, 6.048492908477783, "The Data Collection of the Radar Altimeters Instruments is Monitor ocean surface topography."]
[10.302495956420898, 2.987588405609131, "The Orbit Altitude of the SpaceX CRS-17 Mission is ~ 400 km."]
[9.330530166625977, 6.320924758911133, "The Mass of the Star Tracker Attitude Determination Device is ~90 gram."]
[1.9474431276321411, 5.532979488372803, "The Current of the Voltage 1 Power Amplifier is 1000."]
[5.35195779800415, 10.365766525268555, "The Launch Date of the ISS:LIS Lightning Imaging Sensor is 19 Feb 2017."]
[5.663141250610352, 1.567238688468933, "The Payload of the Falcon 9 rocket Rocket is Spain\u2019s PAZ satellite."]
[8.88104248046875, 10.44516658782959, "The Size of the PAN Camera Imaging Device is 150 cm x 850 cm x 100 cm."]
[7.871334552764893, 6.212028980255127, "The Lunar Calibration Frequency of the Satellite Imaging Satellite is Monthly."]
[8.275293350219727, 3.0644912719726562, "The Launch Year of the TanDEM-X Satellite is 2010."]
[7.49283504486084, 5.261148452758789, "The Deputy Project Scientist of the OCO-2 Satellite is Annmarie Eldering."]
[7.949236869812012, 5.032408714294434, "The Mission Goal of the ExoCube Satellite is Measure the densities of all significant neutral and ionized atom species in the ionosphere."]
[6.047933578491211, 2.157557249069214, "The Launch Site of the Deployment Systems Satellite is Dombarovsky Missile Site, Yasny."]
[9.218092918395996, 10.5468168258667, "The Mounting Height of the Panoramic Camera system Camera is 2 m above ground level."]
[3.2214534282684326, 4.836025238037109, "The Microcontroller RAM of the On-board Computer Computer is 1 MB."]
[6.313828468322754, 4.309193134307861, "The Measurement Parameters of the TROPICS CubeSat Satellite is Temperature, Humidity, Precipitation."]
[6.07191276550293, 4.689671039581299, "The Function of the NGA Organization is Ensures safety of navigation in the air and on the seas."]
[6.996469497680664, 7.862421035766602, "The SSS Temporal Sampling Period of the CIMR Radiometer Imager is Once per month."]
[7.915769100189209, 10.685344696044922, "The Data Quantization of the WV60 imager Imaging System is 11-bit."]
[6.12351131439209, 3.6291418075561523, "The Installation Location of the EMIT Satellite is International Space Station."]
[7.1809468269348145, 5.86637020111084, "The Air Traffic Volume Scenario of the Model Atmospheric Model is 10 times higher than actual."]
[8.018499374389648, 9.345130920410156, "The Ground Resolution of the InSb Detector is 30m."]
[5.9367804527282715, 6.784426689147949, "The Ground Range Resolution of the Radar Sensor is Approximately 250 m."]
[9.554941177368164, 2.840078115463257, "The Orbital Period of the Solar Orbiter Satellite is 3:2 resonance with Venus."]
[9.376595497131348, -0.5374235510826111, "The Image Credit of the CanX-7 nanosatellite Nanosatellite is UTIAS/SFL."]
[2.2054898738861084, 3.8574917316436768, "The Partner of the ROSA Roll-Out Solar Array is Deployable Space Systems."]
[7.343658924102783, 4.22509241104126, "The Spectral Resolution of the DMC-3 Satellite Constellation is Four bands."]
[6.318526268005371, 2.0102438926696777, "The Primary Mission Status of the OPAL Satellite is Successful."]
[6.730526924133301, 3.072873115539551, "The Deployment Status of the PhoneSat 2.5 Satellite is Successful."]
[5.621862411499023, 4.144906520843506, "The Launch Date of the EuTEF European Technology Exposure Facility is Feb. 7 2008."]
[9.548663139343262, 0.4891078472137451, "The Design Life of the Iridium NEXT bus platform Satellite Bus is 12.5 years."]
[6.229496955871582, 4.733063220977783, "The Civil SAR System of the SAR spacecraft Satellite is First of China."]
[4.406520843505859, 7.697660446166992, "The Bandwidth of the Channel 5 Sensor is 1000 MHz."]
[5.996322154998779, 9.608339309692383, "The Mass of the HI-SCALE Instrument is 5.8 kg."]
[4.666825771331787, 3.9287619590759277, "The IEEE Transactions on Geoscience and Remote Sensing of the SAMPEX Satellite is Vol. 31, No. 3, May 1993, pp. 531-541."]
[4.607868194580078, 0.20046168565750122, "The Number of Satellites of the OneWeb Satellite Constellation is 322."]
[4.889997959136963, 12.099970817565918, "The Responsivity Requirement of the Responsivity Measurement Instrument is >0.47 A/W."]
[6.610081672668457, 6.018008232116699, "The Presentation Date of the SWIM Scatterometer is Sept. 23-27, 2013."]
[5.639523506164551, 9.175426483154297, "The Power Consumption of the STAFF/DWP Instrument is 4.5 W."]
[9.390687942504883, 9.30175495147705, "The Diameter of the Focal Plane Optical Instrument is 11.23 mm."]
[9.321149826049805, 5.393375396728516, "The Actuation of the OceanSat-2 Satellite is Four reaction wheels in a tetrahedral configuration, two magnetic torquer coils and monopropellant hydrazine thrusters."]
[7.470715045928955, 8.479853630065918, "The Wavelength of the SOTA Satellite is 1.5 \u00b5m."]
[9.345043182373047, 10.244149208068848, "The Position of the Side-Looking Camera Device is Right Side."]
[9.367545127868652, 9.275697708129883, "The Relative Aperture of the Lenses Optical System is 1/10."]
[1.9648115634918213, 4.181678771972656, "The Solar Panel Power of the Canopus Pipper Satellite is 15 W."]
[10.268994331359863, 4.735547065734863, "The Thruster Burn Arcs of the BepiColombo Spacecraft is 22."]
[11.870925903320312, 0.9864018559455872, "The Sample Transfer Date of the Chang'e-5 Spacecraft is Around Dec. 15-16."]
[7.730254650115967, 3.9799964427948, "The Peak Daily Acquisition Capability of the COSMO-SkyMed Satellite Constellation is 10 minutes of continuous operation in Stripmap or ScanSAR modes or alternatively 20 spotlight images."]
[2.326995372772217, 4.406129837036133, "The Power System of the GNB Satellite is Direct energy-transfer."]
[10.328338623046875, 6.7696027755737305, "The Spacecraft Size of the TCS Thermal Control System is 64.7 cm diameter, 40.3 cm height."]
[8.396702766418457, 3.229193925857544, "The Vertical Separation of the TanDEM-X Satellite is Achieved by a relative shift of the eccentricity vectors of the satellites."]
[11.763494491577148, -0.9587545394897461, "The Total Mass of the FOTINO Capsule is 6 kg."]
[7.255977630615234, 0.9746271371841431, "The Imaging Date of the OPS-SAT Satellite is 14 August 2020."]
[5.016059398651123, -0.14700666069984436, "The Test Service Start of the OneWeb Satellite Constellation is Late 2021."]
[4.550753593444824, 5.831100940704346, "The Navigation Signal Bandwidth of the Spacecraft Satellite is 3 bands (E5, E6, L1)."]
[8.015437126159668, 4.655664443969727, "The Resolution of the Optical Satellite Satellite is 0.5 m GSD."]
[7.93972110748291, 3.7942566871643066, "The Revisit Capacity of the Pl\u00e9iades Neo Satellite is Twice."]
[7.708489894866943, 9.078047752380371, "The Pan-Sharpening Capability of the Hyperion Spectral Instrument is 10 m."]
[6.800632953643799, 0.04465009644627571, "The Launch Date of the Tatiana-2 Satellite is 17 September 2009."]
[7.009162902832031, 0.4153198301792145, "The Launch Date of the LDEF Satellite is April 6, 1984."]
[3.609809637069702, 6.284383296966553, "The Data Rates (Downlink) of the RF Communications Communication System is 9.6 kbit/s."]
[6.810739517211914, 0.6645058989524841, "The Launch Date of the ROCSat-1 Satellite is Unknown."]
[5.525928974151611, 4.751306533813477, "The Link Performance of the Alphasat TDP1 GEO-relay is More than 200 successful links."]
[9.00912094116211, 4.474516868591309, "The Structure of the S/C Satellite is Cube (60 cm x 60 cm x 60 cm)."]
[5.705879211425781, 6.351997375488281, "The Spotlight Scene Size of the SAR Antenna Antenna is 5.5 km side."]
[2.128455877304077, 4.541779518127441, "The Power Range of the Small-GEO Satellite is 2.5 kW to 7.5 kW."]
[7.402172565460205, 8.429123878479004, "The Definition of the Signal to Noise Ratio (SNR) Performance Metric is Commensurate with the overall uncertainty required by the application and its observational characteristics."]
[8.39540958404541, 5.926486968994141, "The Pointing Requirements (Control and Stability) of the Aquarius Radiometer System is 0.5\u00ba."]
[11.696487426757812, -1.1522331237792969, "The Mass of the Spacecraft Satellite is 138 kg."]
[7.185102462768555, 6.959197998046875, "The Power On Date of the Carmen-2 Instrument is June 22, 2008."]
[7.385632038116455, 0.6938515901565552, "The Launch Date of the Glory Satellite is March 4, 2011."]
[8.358508110046387, 9.432435035705566, "The Detector Elements of the Imager Satellite Instrument is 8."]
[4.752775192260742, 4.986599445343018, "The Data Reception of the DRS Data Reception Station is Real-time and playback from the onboard memory."]
[5.294384479522705, 2.8097445964813232, "The Development Team of the BeaverCube CubeSat is Undergraduate and graduate students at the Massachusetts Institute of Technology."]
[10.225984573364258, 2.9904260635375977, "The Orbit Altitude of the BRO-4 Satellite is 551 km."]
[8.334230422973633, 6.98486852645874, "The Expected Parameter Measurement of the CDE Sensor is Cosmic dust influx, PMC nucleation sites."]
[7.30226993560791, 2.504883050918579, "The URL of the Arctide2017 Tidal Model is https://tinyurl.com/y2axpw8c."]
[8.961499214172363, 9.081582069396973, "The Focal Length of the Instrument Spectrometer is 65 mm."]
[7.796326160430908, 8.429824829101562, "The URL of the SOLSPEC Spectrometer is http://lasp.colorado.edu/sorce/workshops/09_19_06/pdf_presentations/14_Thuillier_SOLSPEC-ISS.pdf."]
[6.177560329437256, 6.1418986320495605, "The Mode of the SAR Sensor Subsystem SAR Sensor is WS (Wide Swath)."]
[7.333024501800537, 2.0645947456359863, "The Funding of the IceCube Radiometer is Co-funded by ESTO (Earth Science Technology Office)."]
[9.421255111694336, 10.508625030517578, "The GSD of the Iris Video Camera Camera is Resampled to 1 meter."]
[6.17658805847168, 2.31217622756958, "The Usage of the TacSat-4 Satellite is SATCOM between many platforms."]
[5.318020820617676, 5.137145042419434, "The Coverage of the Predictive Avoidance Request Message Product is Next few days of laser activity by the LCRD payload optical terminal."]
[9.530289649963379, -0.8000615239143372, "The Launch Year of the Kent Ridge 1 Microsatellite is 2013."]
[8.447905540466309, 7.991921901702881, "The Displacement between Exposures of the Euclid Reference Survey Survey is 100 arcsec."]
[7.003039836883545, 3.578322649002075, "The Launch Vehicle of the OrbView-2 Satellite is Pegasus XL rocket."]
[9.865049362182617, 7.80871057510376, "The Energy Measurement Range for Nuclei of the Telescope 3 Telescope is 20-500 MeV/n."]
[7.614056587219238, 3.9746854305267334, "The Measurement Coverage of the CryoSat-2 Satellite is Arctic."]
[7.1756415367126465, 2.560405731201172, "The Purpose of the Proving Ground Space is Practice with, innovate on, and demonstrate the technologies and capabilities needed to send humans to Mars."]
[5.864248275756836, 6.664641857147217, "The Aperture Dimension of the Radar Radar is Approximately 1.5 m."]
[8.59782600402832, 6.902255058288574, "The Time Resolution of the MAG Magnetometer is \u22640.1 s."]
[9.185049057006836, -0.5951563119888306, "The Launch Date of the PISAT nanosatellite Nanosatellite is July 2016."]
[0.9291625022888184, 4.229726791381836, "The Capacity of the Battery Power Source is 40 Ah NiCd."]
[12.077075004577637, 3.28922176361084, "The Inclination of the Explorer 36 Satellite is 105.8\u00ba."]
[5.088437080383301, 4.018670082092285, "The Engineering Model Availability of the EDR-2 European Drawer Rack is Available at CADMOS."]
[7.919032096862793, -0.3952924609184265, "The Proposed Doubleheader Launch Time of the Falcon 9 Rocket is Less than four and a half hours apart."]
[7.426292419433594, 1.3627122640609741, "The Development Completion Date of the S-band SAR Synthetic Aperture Radar is March 9, 2021."]
[5.978504180908203, 6.531505107879639, "The | of the Poker Flat Incoherent Scatter Radar Radar is Initial results from Poker Flat Incoherent Scatter Radar (PFISR)."]
[10.228827476501465, 2.9306483268737793, "The Altitude of the SEOSAT-Ingenio Satellite is 670 km."]
[7.523346900939941, 6.8439130783081055, "The Data Storage of the Instrument Photometer is On the spacecraft."]
[10.51246452331543, 2.423898935317993, "The Apogee (km) of the Meteor-1-1 Satellite is 713."]
[9.061846733093262, 8.769413948059082, "The Thickness of the IS Diaphragm is 0.5 mm."]
[11.636666297912598, -1.2272214889526367, "The Mass of the Spacecraft Satellite is < 2 kg."]
[8.08350658416748, 9.125160217285156, "The Swath Width of the OLS Imaging Sensor is 2960 km."]
[7.040876388549805, 4.274758815765381, "The Measurement Domain of the CHORUS Satellite Constellation is Ocean, Land, Snow & Ice."]
[7.887628078460693, 4.489444732666016, "The Camera Resolution of the Change-2 Satellite Satellite is One Meter."]
[12.071364402770996, 3.3151235580444336, "The Inclination of the INTEGRAL Satellite is 52.246\u00ba."]
[17.7282657623291, 7.162693023681641, "The J2000 right ascension (deg) of the J1846-0258 Pulsar is 281.60392."]
[7.915493011474609, 10.756047248840332, "The Data Depth of the Infrared Sensors Sensor is 8 bit."]
[8.016353607177734, 1.239433765411377, "The Image of the Day Date of the NASA Earth Observatory Satellite is 11 May 2022."]
[9.396580696105957, 5.5469818115234375, "The Effect of the Hysteresis (Memory) Material Attitude Control is Provides the needed damping effect to stabilize KySat-2 on the two control axes, and resist changes on the uncontrolled axis as well."]
[6.410299301147461, 5.841617584228516, "The SAR Measurements Grid Resolution of the L2SMA Soil Moisture Product is 3 km EASE-2."]
[5.150335788726807, 2.7158823013305664, "The Fundraising of the Iraz\u00fa CubeSat Satellite is Aluminum plate is placed on one of the sides of the CubeSat and another one inside of the spacecraft for fund-raising purposes."]
[1.2433820962905884, 4.170903205871582, "The Batteries of the IRIS spacecraft Satellite is Spares from the GRAIL program."]
[7.499438762664795, 0.5510382652282715, "The Date of the MC3E Field Campaign is April 15 -June 1, 2011."]
[7.614985466003418, 3.9047000408172607, "The Optical Imager of the DebriSat Satellite is 1."]
[5.020529747009277, 6.781557559967041, "The Antenna Gain (dB) of the Antenna Reflector is >37."]
[5.400359153747559, 0.2908072769641876, "The Wind Speed of the Calf Canyon-Hermits Peak fire Fire is 65 miles (105 km) per hour."]
[9.350245475769043, 7.783463954925537, "The Cooling Method of the SWIR Detectors Detector is Cryocooler."]
[5.959206581115723, 1.624672770500183, "The Launch Vehicle of the HTV Spacecraft is H-IIB."]
[7.9287896156311035, -0.22628098726272583, "The Launch Date of the Tianzhou-2 Cargo Spacecraft is 29 May 2021."]
[4.628666400909424, 4.48971700668335, "The Function of the SLCPE Instrument Unit is Controls all subsystems and manages the data interface with the satellite."]
[5.470483303070068, 2.6024179458618164, "The Land-Mobile Service Providers of the Iridium Certus(SM) Broadband Service is True."]
[4.219522476196289, 5.748077869415283, "The Uplink Receivers of the UoSAT-12 Satellite is 5."]
[11.7398681640625, 4.792054176330566, "The Flash Brightness of the OJ 287 galaxy Galaxy is Brighter than a trillion stars."]
[8.555721282958984, 6.87734842300415, "The Resolution of the NewMag Magnetometer is 16 bit (\u00b10.2 nT)."]
[5.321791648864746, 4.5461931228637695, "The Ground Stations of the GimmeRF Radio Instrument is Puerto Rico, Florida, Texas, California, Hawaii, and Guam."]
[8.277729034423828, 1.0188677310943604, "The Observation Record of the Landsat-9 Satellite is Last half-century."]
[9.530595779418945, 5.973095417022705, "The Inertial Measurement Unit of the ADCS Attitude Determination and Control System is 1."]
[5.826170921325684, 5.100187301635742, "The Project Partners of the SIR-C/X-SAR Payload is NASA/JPL, DARA/DLR, and ASI (Agenzia Spaziale Italiana)."]
[9.095526695251465, 3.209336280822754, "The Orbit of the DELPHINUS Satellite is Halo orbit around the EML2."]
[5.102904796600342, 9.24511432647705, "The Quake Magnitude of the SEIS Seismometer is 3.3."]
[4.747289180755615, 3.919154644012451, "The Purpose of the ISS Power Augmentation (IPA) Mod Kit Hardware is 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."]
[10.697257995605469, 7.426340103149414, "The Energy Resolution of the SXD and Solar X-ray monitor Detector is \u2264 600 eV at 5.95 keV."]
[5.637338638305664, 2.8652241230010986, "The Satellite Network Provider of the SES Company is True."]
[6.215529918670654, 3.1635775566101074, "The Affiliation of the Michel Sarthou CNES Argos Project Manager is CNES."]
[6.877316474914551, 2.8845343589782715, "The Image Content of the OPS-SAT Satellite is Uninhabited island north of Russia."]
[8.537470817565918, 4.392776012420654, "The Orbital Altitude of the QuickBird-2 Satellite is 450 km."]
[5.009174823760986, 6.431008338928223, "The Frequency of the Antenna ADS-B Antenna is 1090 MHz."]
[11.64181137084961, 6.142877578735352, "The Article Date of the XMM-Newton Satellite is 21 November 2018."]
[6.680068492889404, 2.4053633213043213, "The Launcher of the GPM Core spacecraft Satellite is JAXA."]
[9.412358283996582, 10.5281400680542, "The Frame Rate of the Iris Video Camera Camera is 30 frames/s."]
[10.000201225280762, 5.561923980712891, "The Number of Mini-Solenoid Valves of the NCSU Nano ChemSensor Unit is 3."]
[5.782539367675781, 9.253015518188477, "The Power of the OCM Instrument is 134 W."]
[6.705446720123291, 0.4079023599624634, "The Contract Award Date of the SBSS-1 Pathfinder Satellite is March 2004."]
[8.224616050720215, 2.843031406402588, "The Image Date of the TWINS Satellite is June 15, 2008."]
[5.667785167694092, 5.433382511138916, "The Manufacturer of the GPS Receiver Device is Surrey."]
[7.8220720291137695, 6.8152756690979, "The Frequency of the Dark Current Measurements Measurement is Twice a day."]
[8.748035430908203, 0.7413093447685242, "The Launch Window of the Juice Spacecraft is 5\u201325 April 2023."]
[4.120729923248291, 5.705038547515869, "The X-band Data Rate of the VRSS-1 Satellite is 190 Mbit/s."]
[6.056522369384766, 3.0772154331207275, "The Contractor of the NigeriaSat-2 Satellite is National Space Research and Development Agency (NASRDA) of Nigeria."]
[8.582703590393066, 8.208467483520508, "The PI of the ULEIS Spectrometer is G. Mason, U. of Maryland, R. Gold, JHU/APL."]
[8.697492599487305, 10.423766136169434, "The Image Sensor Resolution of the CMV4000 CMOS Color Detector is 2048 x 2048 pixels."]
[11.83205795288086, 2.3956480026245117, "The Altitude at Checkpoint of the OSIRIS-REx Spacecraft is Approximately 410 feet (125 m)."]
[4.8794097900390625, 1.9290162324905396, "The Number of Planned Satellites of the HY-2 Satellite is 4."]
[6.1102776527404785, 3.4390549659729004, "The Data Authorization of the Satellite GFO is Unconditional (and unclassified) release."]
[8.153474807739258, 9.919161796569824, "The Spatial resolution of the Optical System Imaging System is 1.1 km."]
[7.934947490692139, 4.731465816497803, "The Image Resolution of the On-board Image Processing Satellite System is Better than 100 m/pixel."]
[7.813260555267334, 9.119220733642578, "The Spectral Resolution of the Channels Spectrometer is 0.0002 \u00c5/pixel."]
[7.3253397941589355, 7.379323959350586, "The Development Team of the MiniCOR Instrument is NRL (Naval Research Laboratory), NASA/JPL, the University of Michigan, and JHU/APL (Johns Hopkins University/Applied Physics Laboratory)."]
[7.628512382507324, 6.471256256103516, "The Required Precision of the NO2 Satellite Instrument is 1.00."]
[5.130680561065674, 7.5777459144592285, "The Data Rate of the Instrument General is 600 kbit/s."]
[6.475888252258301, 4.164804935455322, "The Test Location of the CO2M Satellite is ESA\u2019s Test Centre in the Netherlands."]
[4.9459547996521, 6.847790241241455, "The Antenna Requirement of the CITRIS Receiver is Unobstructed hemisphere."]
[7.940490245819092, 8.545560836791992, "The Detector Array Bands of the FTS Fourier Transform Spectrometer is 194-324 \u00b5m and 316-672 \u00b5m."]
[7.6218953132629395, 3.997894048690796, "The Five-Year Average Arctic Sea Ice Volume of the CryoSat-2 Satellite is Relatively stable."]
[5.246866226196289, 2.0777297019958496, "The Number of Runs of the Monte Carlo Simulation Analysis Tool is 3000."]
[10.381658554077148, 2.7988884449005127, "The Altitude of the ISS Space Station is ~400 km."]
[4.1840033531188965, 5.707328796386719, "The L-band Receivers of the UoSAT-12 Satellite is 2."]
[11.476592063903809, 4.150414943695068, "The Size of the Planet Orbiting AU Microscopii Exoplanet is About as large as Neptune."]
[7.164047718048096, 8.810887336730957, "The Swath Width of the AMSR-E Instrument is 1445 km."]
[4.151191234588623, 6.690313339233398, "The Calibration Method of the Ranging Channel Communication System is 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."]
[11.499638557434082, 5.5620269775390625, "The Completeness of the Einstein's theory of gravity Scientific Theory is May be incomplete."]
[9.503815650939941, 6.098205089569092, "The Sensor Quantity of the ADS Attitude Determination Subsystem is 6 sun sensors."]
[9.300850868225098, 0.8378010392189026, "The Planning Duration of the MOPITT Satellite Instrument is 12 Years."]
[9.596701622009277, -0.6522709131240845, "The Design Options of the Microsatellite Satellite is NFI + STEAM, or a WFI."]
[9.906331062316895, 8.668706893920898, "The Field of View of the ART-XC Instrument Telescope is 0.3\u00ba x 0.3\u00ba."]
[7.564815044403076, 4.81756591796875, "The Geometric Calibration/Validation of the PROBA-V Satellite is Implemented."]
[7.524724960327148, 6.1158013343811035, "The Objective 1 of the EMIT Mission is Deliver a new improved assessment of the heating and cooling effects of mineral dust in the Earth\u2019s atmosphere."]
[7.836223602294922, 8.8032808303833, "The Ground Sample Distance (GSD) of the GIS Instrument Satellite Instrument is 41 cm for Pan and 1.64 m for MS."]
[8.586636543273926, 1.763161063194275, "The Mission Operations Location of the Spitzer Space Telescope Telescope is NASA\u2019s Jet Propulsion Laboratory, a division of Caltech."]
[7.7975053787231445, 9.03693962097168, "The Passband of the Instrument Spectrometer is 4 nm."]
[11.650046348571777, 4.504305839538574, "The Distance from Earth of the HD 93396 Star is 320 light-years."]
[5.678035259246826, 2.222052574157715, "The Function of the QKD Quantum Key Distribution is Generate private random encryption keys and share them between only two parties."]
[4.410013675689697, 7.689920902252197, "The Bandwidth of the Channel 3 Sensor is 400 MHz."]
[3.0608038902282715, 6.628270626068115, "The RF output power (max) of the RF communication subsystem Communication is 1 W."]
[5.449560642242432, 10.253654479980469, "The Demonstration Date of the LIRIS Sensor is March 19, 2014."]
[9.398022651672363, 4.094357013702393, "The Diameter of the Aluminum Spheres Satellite is 10 cm."]
[6.767714023590088, 2.47243332862854, "The Affiliation of the Hiroyuki Shindou Unknown is JAXA."]
[3.9743545055389404, 5.748983860015869, "The Bit Error Rate of the LEO-LEO Inter-satellite Link Communication System is < 10-9."]
[8.369929313659668, 3.1348788738250732, "The Conference Presentation Date of the CANYVAL-X Satellite is 28 May - 1 June 2018."]
[2.457608699798584, 6.334609031677246, "The Latency Requirement of the S-3 NRT Product is Within 30 minutes."]
[4.88259744644165, 5.024584770202637, "The Telemetry Packet Forwarding of the Delfi-n3Xt Satellite is Worldwide amateur radio community."]
[6.143039226531982, 8.101405143737793, "The Antenna Type of the MSR Radiometer is Offset Cassegrain-type antenna."]
[9.500041007995605, 1.4601975679397583, "The Observation Duration of the Kepler Telescope is 72 days."]
[5.942444324493408, 2.2326483726501465, "The Entanglement Test Performer of the QUESS Satellite is Chinese team."]
[6.997199535369873, 0.37090376019477844, "The Launch Date of the SPOT-3 Satellite is September 1993."]
[8.176534652709961, 4.902126789093018, "The Field of View of the HaloSat Satellite is Near 100 square degrees."]
[4.738570690155029, 1.7701252698898315, "The Number of Satellites of the 90-satellite constellation Satellite Constellation is 90."]
[3.850604772567749, 4.969921588897705, "The Calibration of the MAC Memory System Module is In-orbit radiometric calibration."]
[9.02106761932373, 5.322515964508057, "The Attitude Control of the Payload Satellite Payload is Pointing Agility."]
[7.811221122741699, 9.042141914367676, "The Spectral Domains of the Sentinel-4/UVN Instrument is UV (305-400 nm), VIS (400-500 nm) and NIR (750-775 nm)."]
[9.163559913635254, 10.514547348022461, "The Communication of the DCAM3 Camera is One-way to the mother ship."]
[5.321232795715332, 2.5622241497039795, "The Director of the ArgoMoon CubeSat is David Parker."]
[7.711702346801758, 1.6559503078460693, "The Phase A Feasibility Study of the SMOS Satellite is 2000-2001."]
[6.674800872802734, 9.128133773803711, "The Dimensions of the Instrument Interface Module Interface Module is 90 mm x 95 mm x 12 mm."]
[3.1495020389556885, 4.859434604644775, "The Size of the Nanoracks BlackBox Platform is Locker-sized."]
[9.495068550109863, 0.942907452583313, "The Journey Duration of the NEA Scout Spacecraft is Approximate two years."]
[7.045646667480469, 4.419387340545654, "The Measurement Domain of the TUBSAT Satellite is Atmosphere, Ocean, Land, Gravity and Magnetic Fields."]
[6.770475387573242, 1.0825048685073853, "The Transition Date of the Pilot Program Program is CSDA."]
[10.793305397033691, 3.6361541748046875, "The Planet Diameter of the ExoMars TGO Trace Gas Orbiter is 34 arcseconds."]
[6.792653560638428, 4.46872615814209, "The Data Transmission of the British Antarctic Survey (BAS) Customer is Remote measurement stations."]
[7.568186283111572, 7.930983543395996, "The Window Spectral Region of the CERES Instrument is 8 - 12 \u00b5m."]
[8.91019344329834, 7.08120059967041, "The Objective of the SWEA Solar Wind Electron Analyzer is 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."]
[9.569416999816895, 5.484638214111328, "The Stability of the AOCS Attitude and Orbit Control Subsystem is 2 arcmin/s about the Z-axis."]
[12.155574798583984, 2.21433162689209, "The Detection of the REXIS Spectrometer is Newly flaring black hole in the constellation Columba."]
[5.963736534118652, 3.702728271484375, "The Workshop Location of the SSETI Express Satellite is Noordwijk at ESA/ESTEC."]
[3.215858221054077, 6.056725025177002, "The Purpose of the Frontier Software Defined Radio Radio is Communication."]
[3.823120594024658, 4.5163373947143555, "The Microcontroller of the Big Apple board Electronic Board is Controls the operations, power distribution, and data saving."]
[5.415916442871094, 0.30318182706832886, "The Evacuated People of the Calf Canyon-Hermits Peak fire Fire is Thousands."]
[7.541203022003174, 1.0608289241790771, "The Image Acquisition Date of the ALOS satellite Satellite is 29 March 2011."]
[10.271419525146484, 2.9789772033691406, "The Nominal Altitude of the DubaiSat-2 Satellite is 600 km."]
[9.451533317565918, 0.9927127957344055, "The Nominal Mission Duration of the Vega Rideshare Mission Satellite Launch is 1 hour, 44 minutes and 56 seconds."]
[4.692054271697998, 5.000344753265381, "The Detection Time of the Ground System Communication System is 7 days."]
[4.8905863761901855, 4.81067419052124, "The Data Processing Time of the Ground Segment Ground System is Within an hour."]
[7.804591178894043, 8.939172744750977, "The Radiometric Accuracy of the Spectral Band A Spectrometer is 3."]
[5.270916938781738, 6.620200157165527, "The Aperture Size of the Antenna Communication is 13 m."]
[2.9118731021881104, 6.372318267822266, "The Power of the SILEX Terminal is 130 W."]
[3.1039366722106934, 6.609463691711426, "The Beacon Power of the RF Communication System Communication System is 100mW."]
[3.891059637069702, 4.351471900939941, "The MCU of the C&DH Command and Data Handling is Freescale MCU (HCSX12)."]
[7.638446807861328, 3.3076233863830566, "The Connection of the ICON Satellite is Physical connection between our world and the immediate space environment around us."]
[7.557427406311035, 10.060332298278809, "The Data Compression of the Instrument Hyperspectral Imager is None."]
[9.67431640625, 1.4596441984176636, "The Mean Time Between Resets of the BRMM Spacecraft is 8 days."]
[4.280998229980469, 4.484289169311523, "The Communication Protocol of the PIC microcontroller Microcontroller is CAN bus."]
[7.304995536804199, 3.2506022453308105, "The Geopotential Mission of the CHAMP Satellite is Unknown."]
[3.2778139114379883, 4.465775489807129, "The Functionality of the PCU Power Control Unit is High."]
[9.491945266723633, 0.530619204044342, "The De-Orbit Lifetime of the Secondary Payloads Satellite is 25 years."]
[6.365966796875, 3.5146567821502686, "The Location of the HSC Herschel Science Center is ESAC (ESA/European Space Astronomy Centre) in Villafranca, Spain."]
[8.48880386352539, 6.850606441497803, "The Manufacturer of the Vector Magnetometer Instrument is DTU (Danish Technical University)."]
[1.1788641214370728, 3.8475866317749023, "The Power Source of the XI-IV Picosatellite is Body-mounted solar cells."]
[9.732215881347656, 3.115816593170166, "The Orbit of the AVUM Spacecraft is Transfer Orbit."]
[7.817224502563477, 9.06902027130127, "The Wavelength Range of the OMI Spectrograph is 270 nm to 500nm."]
[7.640023708343506, 0.8764063715934753, "The Operational Declaration Date of the Kanopus-V Satellite is Jan. 29, 2013."]
[3.6194205284118652, 6.55683708190918, "The Data Rate of the L-band Transmitter Radio Transmitter is 1 Mbit/s."]
[6.560421943664551, 7.409078598022461, "The Polarization Modes of the Coronagraph Instrument is Unpolarized light or one of three possible orientations of plane polarized light."]
[6.839442729949951, 10.062117576599121, "The Bandwidth of the Band 5 Spectral Band is 650-670 nm."]
[4.324994087219238, 5.99960994720459, "The X-band antenna of the TT&C Tracking, Telemetry, and Command is 1."]
[6.485650062561035, 4.701883792877197, "The Level-2 Ocean products of the Sentinel-1 Satellite is Ocean wind field, swell wave spectra and surface currents information as derived from SAR data."]
[8.687424659729004, 10.403738021850586, "The Effects of the CCD Imager is Noise, and dark current."]
[7.913624286651611, 3.6907286643981934, "The Number of Preliminary Geophysical Products of the Tandem-L Satellite is 26."]
[6.954065322875977, 11.294721603393555, "The Wavelength FWHM of an unresolved line of the Spectrometer Instrument is 0.021 \u00b5m."]
[9.990921020507812, 3.0316147804260254, "The Orbit Altitude of the PRISMA Satellite is 614 km."]
[9.802336692810059, 8.043127059936523, "The Gamma-ray Energy Resolution of the MGNS Neutron and Gamma-ray Spectrometer is Approximately 3.5% at the energy of 662 keV."]
[5.991443634033203, 8.919683456420898, "The Power Consumption of the RMU Radiometer Microwave Unit is < 4 W."]
[5.797727108001709, 2.927018880844116, "The Manufacturer of the Landsat-9 Satellite is Northrop Grumman Innovation Systems."]
[8.685762405395508, 0.21767176687717438, "The Period of the ISS Space Station is ~ 93 minutes."]
[6.128592491149902, 6.247805595397949, "The Advantage of the Staggered SAR Radar Mode is Allows the imaging of a wide continuous swath without the need for a long antenna with multiple apertures."]
[5.901031017303467, 4.716495037078857, "The Window Damage of the Cupola Space Station Module is Minor."]
[2.045745372772217, 5.6014227867126465, "The Amplification Factor of the Op-amp Operational Amplifier is 2.4."]
[11.605256080627441, -1.069667935371399, "The Launch Loads of the SRMSat Satellite is \u00b1 11 g longitudinal and \u00b1 6 g lateral."]
[9.201864242553711, 6.514904022216797, "The Configuration of the Pin-Puller Mechanism is Double-shear."]
[3.5295350551605225, 4.512911796569824, "The Quantity of the FPGAs Electronic Components is 6."]
[2.321197509765625, 4.472229480743408, "The Average Power Consumption (Standby Mode) of the COMIS Satellite is 8 W."]
[6.3058085441589355, 10.06493854522705, "The Weight of the HRC High-Resolution Camera is 2.1 kg."]
[7.107178688049316, 0.4021313488483429, "The Launch Date of the FY-2 Satellite is May 29, 2012."]
[13.808097839355469, 0.7670063376426697, "The Orbital Slot of the GSAT-0206 Satellite is A05."]
[7.145920753479004, 0.8129462599754333, "The Launch Date of the EROS-C Satellite is Not set so far."]
[9.870675086975098, 1.6438071727752686, "The Solar Eclipses Duration of the SPARCS Satellite is 25 minutes per year."]
[4.121728420257568, 6.464976787567139, "The Ku-band repeater of the Repeater subsystem Communication System is 24 (BOL) / 20 (EOL) simultaneously operating transponders at saturation."]
[8.71672248840332, 1.9189316034317017, "The Heritage of the LET Low Energy Telescope is More than 14 years of successful operation in space."]
[6.851071834564209, 8.562270164489746, "The SIC Spatial Resolution of the CIMR Radiometer Imager is 5 km."]
[7.328965663909912, -0.6313350796699524, "The Mission Presentation Date of the CYGNSS Satellite Constellation is March 2-9, 2013."]
[4.617411136627197, 6.19935417175293, "The Frequency of the Satellite Communication is 435 MHz."]
[4.805797576904297, 1.7725095748901367, "The Number of Satellites of the BeiDou-2 Satellite Constellation is 35."]
[9.534172058105469, 9.10257625579834, "The Aperture of the NUV & VIS Channels Telescope Channels is ~380 mm."]
[6.549167633056641, 0.7114809155464172, "The Launch Date of the GOSAT-GW Satellite is 2024."]
[8.037713050842285, 3.9627883434295654, "The Image Acquisition Capability of the Pleiades System Satellite System is More than 500 images per day and per satellite."]
[10.503175735473633, 6.09874963760376, "The Purpose of the SUBSA-BRAINS Brazing Alloy Solidification Experiment is Examine differences in capillary flow, interface reactions, and bubble formation during the solidification of brazing alloys in microgravity."]
[11.815990447998047, 1.03170645236969, "The Journey Time to the Moon of the Chang'e-5 Spacecraft is Estimated 112 hours."]
[8.481468200683594, 2.3171420097351074, "The Responsible Team of the Parker Solar Probe Satellite is Modeling teams."]
[7.63339900970459, 7.437703609466553, "The Objectives of the WISDOM Instrument is 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."]
[7.831949710845947, 9.250553131103516, "The Spectral Sampling Interval of the HSC Spectrometer Spectrometer is 5 nm."]
[3.5275142192840576, 4.710348129272461, "The Core Speed of the Stamp9G20 Microcontroller is 400 MHz."]
[7.029473304748535, 0.766503095626831, "The Funding Approval Year of the MiRaTA Satellite is 2013."]
[6.7244768142700195, 0.6724786162376404, "The Year of Launch of the ACRIMSat Satellite is 1999."]
[11.731236457824707, 1.1944150924682617, "The Sampling Time of the Chang'e-5 Lander Lander is 48 hours."]
[5.515052318572998, 9.622244834899902, "The Instrument Mass of the STOs and STAEs Analog Electronic units is 39.8 kg (for 3 STO configuration)."]
[8.886127471923828, 8.334497451782227, "The Integral Geometric Factor of the ELENA Sensor is 6 x 10 -4 cm 2 sr."]
[7.5352301597595215, 4.882236480712891, "The Heat Up Monitoring of the S/C Satellite is Yes."]
[7.663320064544678, 8.628678321838379, "The MTF of the Imager Satellite Instrument is \u22650.18(PAN), \u22650.2(MS)."]
[4.590982913970947, 6.165788650512695, "The S-band Uplink Frequency of the MSX Satellite is 1827.8 MHz."]
[8.515012741088867, 7.166225910186768, "The Components of the BSA Beam Steering Assembly is BSMFE, BSME, BSH."]
[5.910249710083008, 1.9783883094787598, "The Rocket of the Landsat-9 Satellite is United Launch Alliance Atlas 5."]
[6.788046836853027, 3.2533481121063232, "The Mission Status of the GovSat-1 Communication Satellite is Operational (nominal)."]
[7.470474720001221, 9.990377426147461, "The Manufacturer of the Instrument Hyperspectral Imager is Northrop Grumman."]
[7.296509742736816, 5.588000297546387, "The Partial Pressure of Carbon Dioxide in the Water of the Marine Chemistry Study Parameter is Unknown."]
[10.47468376159668, -1.1475757360458374, "The Mass of the BLITS Nanosatellite is 7.53 kg."]
[9.395509719848633, 7.859888076782227, "The Cooling of the FPA Focal Plane Array is Cryogenic module (three-stage radiative cooler)."]
[4.236702919006348, 2.597503423690796, "The Hardware Cost of the Starlink Premium Satellite Internet Service is $2,500."]
[8.767148971557617, 7.871225357055664, "The Function of the Charge Sensitive Preamplifier Instrument is Convert total charge Q created by the passage of ionizing radiation to an electric impulse."]
[7.863271236419678, 9.11247444152832, "The Wavelength Range of the MIRI Spectrometer Spectrometer is 4.8-29 \u00b5m."]
[8.62325382232666, 10.032651901245117, "The Subaperture Radius of the PAIS Imaging System is 0.2 mm."]
[12.129448890686035, 3.3184778690338135, "The Orbit Inclination of the KSM-1 satellites Satellite is 37\u00ba."]
[5.267305850982666, 4.352075099945068, "The Ground Stations of the Spacecraft Satellite is AFSCN (Air Force Satellite Control Network) and the USN (Universal Satellite Network)."]
[10.971589088439941, 3.3481109142303467, "The Distance from Sun of the Kuiper Belt Celestial Object is 5 billion kilometers (and beyond)."]
[7.600698471069336, 3.4673683643341064, "The Revisit Time of the Satellite Constellation Constellation is Much better in higher latitudes."]
[6.6048970222473145, 8.384202003479004, "The Contract Volume of the MWI Instrument Instrument is \u20ac 134 million."]
[11.705199241638184, 4.633893013000488, "The Gas Temperature of the Cassiopeia A (Cas A) Supernova Remnant is 50 million degrees."]
[2.234957456588745, 3.8333802223205566, "The Solar Arrays of the Satellite Communication Satellite is Two arrays with a total wingspan of 37 m."]
[8.78519058227539, 8.491342544555664, "The Cross-Track Detection Range of the Spectrometer Instrument is -30\u00ba to 10\u00ba."]
[9.485949516296387, -0.808589518070221, "The Type of the Aalto-1 Nanosatellite is 3U CubeSat."]
[6.515997409820557, 3.157721519470215, "The Payload Development Manager of the CloudSat Satellite is NASA/JPL."]
[8.135689735412598, 9.535564422607422, "The Imager Ranges of the HySIS Satellite is Visible Near Infrared (VNIR) range and the other in the Shortwave Infared (SWIR) range."]
[7.876115798950195, 4.612267971038818, "The Imager Resolution of the Satellite Vu Satellite is 3.5 m."]
[3.4124691486358643, 5.276223659515381, "The 2 Gbit of the Satellite Data Storage Capacity is Data storage capacity of 2 Gbit (EOL)."]
[9.750041961669922, 1.4175344705581665, "The Deployment Time of the SpinSat Satellite is Few minutes after the plunger inhibit switches disengage from the Cyclops pusher plate."]
[7.10470724105835, 4.4708123207092285, "The Hyperspectral Imager of the HJ-1A Satellite is 1."]
[9.741252899169922, -0.6910762786865234, "The International Code of the BX-1 Microsatellite is 2008-047G."]
[7.907094955444336, 9.323474884033203, "The Waveband of the CO2Image Satellite is Shortwave infrared (SWIR): 1100 nm - 3000 nm."]
[7.533798694610596, 7.154504299163818, "The Preamplifier Manufacturer of the SCM Device is 3D Plus."]
[6.201259136199951, 5.592613697052002, "The SAR Data Acquisition of the X-UGS UGS is Absence of acquisition and processing functionalities."]
[8.316508293151855, 0.6361368298530579, "The ESA Announcement Date of the Hitomi Satellite is July 6, 2016."]
[11.178935050964355, 9.346363067626953, "The Number of Channels of the ERB Earth Radiation Budget Experiment is 22."]
[6.694549560546875, 3.0706939697265625, "The Mission Objectives of the SOHLA-1 Satellite is Completed."]
[7.110227108001709, 8.896416664123535, "The Spatial Resolution of the ECOSTRESS Instrument is 38 m in-track by 69 m cross-track."]
[6.838254451751709, 1.523069143295288, "The Presentation Date of the Disaster Monitoring Constellation Imagers Satellite is Oct. 3-7, 2011."]
[1.8863962888717651, 3.856863498687744, "The Cell Type of the Solar Arrays Power Generation is Triple-junction GaAs design."]
[10.07925033569336, 3.6625802516937256, "The Effect of the Solar Storms Natural Phenomenon is Cause the regolith in the moon's PSRs to accumulate charge in two layers until explosively released."]
[6.909337520599365, 2.452244758605957, "The DOI of the Onboard Processing Satellite System is https://doi.org/10.1109/JPROC.2018.2802438."]
[11.6633939743042, -1.180588722229004, "The Mass of the Spacecraft Satellite is 6.5 kg."]
[4.874520778656006, 0.9486121535301208, "The Total Budget of the ESA Space19+ ministerial conference Conference is \u20ac14.5 billion for ESA for the next three years."]
[9.134366035461426, 9.349130630493164, "The Field of View of the RRA RetroReflector Array is More than 30\u00ba."]
[8.008177757263184, 5.267273426055908, "The Sensitivity of the ASTRO-H Satellite is 2 orders of magnitude better than previous instruments."]
[6.961124897003174, 0.46434319019317627, "The Reaction Wheel Problem Start Date of the SARAL/AltiKa Satellite is July 2016."]
[8.664789199829102, 8.594762802124023, "The Cross-Track of the HSRS Sensor is 19\u00b0."]
[11.526387214660645, 2.6852686405181885, "The Distance from Earth of the Ryugu Asteroid is 300 million km."]
[7.54279088973999, 7.7602996826171875, "The Data Products of the TOMS Instrument is 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."]
[9.171010971069336, 10.315260887145996, "The Number of Images Selected of the PolyCam Camera is Just over 2,100 images."]
[5.527901649475098, 3.1861319541931152, "The Bus Type of the MEV-1 Satellite is GEOStar 3."]
[9.344679832458496, 7.694908142089844, "The Maximum Operating Temperature of the RDM Sensor Radiation Damage Monitor is +80\u00baC."]
[2.7107372283935547, 4.073729991912842, "The Project Manager of the Fission Surface Power System Power System is Todd Tofil."]
[8.691471099853516, 5.174884796142578, "The Body-pointing Capability of the Spacecraft Satellite is Up to \u00b145\u00ba."]
[9.274718284606934, 5.346111297607422, "The Rotation Speed of the Filter Wheel Optics Subsystem is 600 rpm."]
[8.085947036743164, 0.8759447336196899, "The Mission Status of the Landsat-9 Satellite is Continuing the legacy - 2020 and beyond."]
[6.936439514160156, 4.776463508605957, "The Straylight Measurement of the Sentinel-5 Satellite is Laser and filter measurements."]
[7.390002250671387, -0.24010923504829407, "The End of Life Date of the HTV-9 Cargo Transfer Spacecraft is 20 August 2020."]
[4.297410488128662, 4.491562366485596, "The Function of the Microcontroller Controller is Collects data from the OSL, from the temperature sensors and from measurements issued from the DUTs."]
[11.473655700683594, -1.2899136543273926, "The Weight of the SPOT-3 Satellite is 1800 kg."]
[5.891822338104248, 3.7885985374450684, "The Mission Operations Center of the XMM-Newton Satellite is ESA/ESOC (European Spacecraft Operations Center) in Darmstadt, Germany."]
[11.940473556518555, 3.2243494987487793, "The Orbit Inclination of the CANYVAL-X CubeSats CubeSats is 97.55\u00ba."]
[5.95380163192749, 9.57382583618164, "The Mass of the HEED Instrument is 2.2 kg."]
[8.079849243164062, 4.987124919891357, "The Science Goal of the HaloSat Satellite is Estimate the mass of the hot halo surrounding the Milky Way galaxy."]
[7.444456577301025, 1.3637391328811646, "The Observation Date of the SGLI Polarimetric Radar Radar is 23 March 2018."]
[11.05750560760498, 6.965196132659912, "The Spectral Band of the AstroSat Astronomy Satellite is Hard X-ray to visible bands."]
[6.631044864654541, 0.4988551437854767, "The Launch Date of the SciSat-1/ACE Satellite is 12 August 2003."]
[4.413486480712891, 6.639091968536377, "The Signal Filtering of the LICEF Receiver is RF and IF."]
[11.333165168762207, 6.244199275970459, "The Non-Thermal Radiation Creation Processes of the Pulsars Neutron Stars is Synchrotron emission and curvature emission."]
[8.740281105041504, 8.854658126831055, "The Ground Area Coverage of the TIR Subsystem Imaging System is 156 km by 8 km."]
[10.329347610473633, 9.511076927185059, "The Design Reference of the IRIS spacecraft Satellite is Prior missions and design studies."]
[3.1439714431762695, 4.834883689880371, "The Built-in Flash of the GomSpace NanoMind A3200 Onboard Computer is 512 kB."]
[6.418198108673096, 3.483506202697754, "The Risk of the ASAP Autonomous System is Loss of Mission."]
[3.9945616722106934, 5.6851806640625, "The Uplink Data Rate of the NSat Satellite is 1.2 kbit/s."]
[9.449931144714355, 5.961304187774658, "The Advantages of the Magnetic Capture Technology Capture Technology is Improves on the shortcomings of both tethered systems and robotic systems."]
[5.217066764831543, 6.143731594085693, "The Array of the Onboard Antenna Antenna is 2 x 2 patch array."]
[6.217031002044678, 2.4939217567443848, "The Mission Status of the STPSat-3 Satellite is Unknown."]
[11.216485977172852, -1.5034911632537842, "The Cion Mass of the CICERO-6 6U CubeSat is 1.2 kg."]
[7.679714679718018, 1.0527031421661377, "The Launch Date of the SPIRRAL Experiment is 2023."]
[6.9730448722839355, 0.8971193432807922, "The Presentation Date of the Indian Remote Sensing Satellite Missions (IRS) Satellite is Sept. 24-28, 2007."]
[5.997247219085693, 3.0032434463500977, "The Manufacturer of the CHORUS Satellite Constellation is MDA Ltd. (MacDonald, Dettwiler and Associates Ltd.)."]
[11.397284507751465, 2.1381826400756836, "The Location of the Sandpiper Sample Collection Site is Bennu\u2019s southern hemisphere."]
[4.58113956451416, 4.256865501403809, "The Language of the Payload Data Processing Software is Java."]
[10.392210006713867, 3.3093583583831787, "The High Energy Particle Strikes of the Computer System Payload is 2."]
[9.63193416595459, 8.498193740844727, "The AOI Sensitivity of the Etalon Etalon is Unknown."]
[6.570693492889404, 0.8207790851593018, "The Contract Award Date of the RADARSAT Constellation Mission Satellite is May 29, 2009."]
[4.380419731140137, 6.3384928703308105, "The Downlink Frequency of the Payload Communication System is Ka-band."]
[4.164838790893555, 4.5752644538879395, "The Command Types of the DCU Data Control Unit is Plain TCs, authenticated and encrypted messages."]
[11.315592765808105, 6.755321979522705, "The Camera Function of the Imaging X-ray Polarimetry Explorer (IXPE) Space Telescope is Measure the polarization of cosmic X-rays."]
[8.20743465423584, 9.688736915588379, "The Array Size of the SWIR Detector is 80 x 640."]
[7.569248199462891, 0.07397483289241791, "The In Orbit Commissioning (IOC) End Date of the CHEOPS Satellite is March 26, 2020."]
[9.799883842468262, 3.9974453449249268, "The Total \u0394V of the CanX-4&5 Satellite is 14 m/s."]
[10.154170989990234, 7.64196252822876, "The Function of the BCA Baffle and Cover Assembly is Minimizes stray-light and includes a protective cover and release mechanism."]
[10.31237506866455, 4.951926231384277, "The Thruster of the S/C Satellite is 100 mN resistojet."]
[9.849781036376953, 8.307703971862793, "The Mission of the Spectrometer Telescope Telescope is Solar Orbiter."]
[11.488202095031738, 4.577929496765137, "The Corona Temperature of the Sun Celestial Body is On average 1 million degrees Celsius."]
[3.4089841842651367, 5.279049396514893, "The Mass Data Storage of the DubaiSat-1 Satellite is 32 Gbit."]
[5.923907279968262, 5.399687767028809, "The Software of the Phoenix GPS Receiver GPS Receiver is eXtended Navigation System (XNS)."]
[8.92876148223877, 2.6951353549957275, "The Observation Campaign of the Kepler spacecraft Spacecraft is 18th."]
[7.608072280883789, 4.808080196380615, "The Calibration Images of the PROBA-V Satellite is 2.674."]
[7.596207141876221, 6.535370826721191, "The On-Board Calibrators Performance Duration of the Terra MODIS Satellite Instrument is Not Provided."]
[8.413786888122559, 10.541325569152832, "The TDI Stages of the Kruiz CCD Detector is 128, 64, 32, 16, 8."]
[5.241942882537842, 4.099123477935791, "The Ground Control Network of the R3 spacecraft CubeSat is Multi-station."]
[7.906915664672852, 5.0837082862854, "The Data Acquisition Sites of the VSSC Satellite is Existing or planned experimental sites with sizes ranging from 27 km x 27 km to 27 km x 54 km or more."]
[7.85102653503418, 9.131512641906738, "The Spectral Resolution of the HPT Sensor is Multispectral."]
[5.823321342468262, 8.149785041809082, "The Bandwidth (GHz) of the ICI-4 Radiometer is 6."]
[2.1258490085601807, 4.728294372558594, "The Power of the EPDP Technology Payload is 18 W."]
[8.059618949890137, 7.450676918029785, "The Calibrators of the Instrument Calibration is Solar diffuser, solar diffuser stability monitor, blackbody."]
[4.286581516265869, 5.607572078704834, "The Downlink Transmission of the CBERS-1 Satellite is X-band."]
[6.067941665649414, 9.59850788116455, "The Mass of the CLARA Instrument Satellite Instrument is 2.63 kg."]
[7.24238920211792, 7.999088287353516, "The Scan Time of the VISSR Mirror Instrument is 30 minutes."]
[7.7418928146362305, 4.079741477966309, "The Image Archive of the SPOT-4 Satellite is 100 billion km2."]
[6.560170650482178, 1.1570379734039307, "The Rocket Engine Test Date of the PRISMA Satellites Satellite is June 24, 2010."]
[7.809301376342773, 7.208430290222168, "The Scan Mirror Controller of the TEMPO Instrument is Closed-loop control."]
[7.3255791664123535, 0.7493012547492981, "The Launch Date of the Monitor-E Spacecraft is June 30, 2003."]
[6.961212635040283, 0.947012722492218, "The Collaboration Date with Turkey of the SPOT 6 & 7 Satellite Constellation is Dec. 20, 2012."]
[5.618214130401611, 5.486179351806641, "The Chip Set of the GPS receiver Receiver is MITEL chip set."]
[5.499244689941406, 9.353434562683105, "The Vacuum Chamber Volume of the SEIS Instrument Seismometer is 3 liters."]
[8.17489242553711, 10.443500518798828, "The Video Data Conversion Rate of the MS Detectors Detectors is 7 Mpixel/s."]
[6.469233512878418, 7.853961944580078, "The Pulse Peak Output Power of the Laser Instrument is 500~1000 W."]
[7.343637466430664, 4.407186985015869, "The Imagery of the Landsat-8 OLI Satellite is Data."]
[9.031076431274414, 3.0228729248046875, "The Orbit of the Kleos Patrol Mission (KSF2) Satellite is Sun synchronous."]
[5.768383502960205, 2.87925386428833, "The Manufacturer of the SkySat Satellite is Terra Bella."]
[9.350848197937012, 1.7090636491775513, "The Data Collection Frequency of the Sentinel-6/Jason-CS Satellite is Every 10 days."]
[8.578495025634766, 9.105611801147461, "The Value of the Polarization Sensitivity Performance Requirement is Less than 2%."]
[6.750916957855225, 3.60514760017395, "The Mission Aim of the NeuSAR Satellite is Pathfinder mission for a potential constellation of small SAR satellites."]
[11.383474349975586, 3.867034912109375, "The Crust Thickness of the Mars Planet is Between 24 and 72 kilometers."]
[5.340073585510254, 3.6059470176696777, "The Retention Mechanism of the Deployment Systems Satellite is Pyro cutters."]
[5.5565714836120605, 2.9626147747039795, "The Power Subsystem Manufacturer of the MicroMAS-1 Satellite is Clyde Space."]
[3.1428747177124023, 5.933030605316162, "The Data Processing Time of the PDS Data Services is Within 3 hours after sensing."]
[10.23183536529541, 9.337126731872559, "The Solar Array Surface Area of the IRIS Satellite is 1.7 m2."]
[6.456543922424316, 3.593904495239258, "The Payload of the ZACube-2 Satellite is Medium resolution matrix imager and a number of communication subsystems."]
[7.230122089385986, 5.800897598266602, "The Spectral Range and Resolution of the OCI Ocean Color Instrument is Advance the ability to distinguish between different species of phytoplankton compared to predecessor satellite instruments."]
[6.709714889526367, 0.6102375388145447, "The Launch Time of the SEOSAT-Ingenio Satellite is 02:52 CET / 22:52 local time on 16 November."]
[7.677937030792236, 5.387423515319824, "The Applications of the NIDEM Elevation Model is Coastal risk mitigation, ecological conservation, habitat mapping, hydrographic surveying."]
[5.060102939605713, 6.621598720550537, "The Antenna Gain of the GPSRO Sensor Sensor is Over 10 dBi."]
[10.414976119995117, 2.6476690769195557, "The Apogee of the SCD-2 Satellite is 768 km."]
[9.572885513305664, 8.655084609985352, "The Type of the VIIRS Telescope Assembly is Three Mirror Anastigmatic."]
[5.248333930969238, 4.445663928985596, "The Installation Location of the Wireless Compose module Communication Module is Space Station."]
[8.091597557067871, 9.277587890625, "The Wavelength of the VIS Detector is 0.675 \u00b5m."]
[3.988048553466797, 5.818030834197998, "The Instrument Package Data Rate of the LCROSS Satellite is 554.5 kbit/s."]
[4.702286720275879, 5.640395164489746, "The Components of the Satellite Communication Satellite is More than 600 electronic and radio-frequency units."]
[7.739438533782959, 1.1115225553512573, "The Anomaly Updates of the Copernicus Sentinel-1B Satellite is 2."]
[6.08509635925293, 4.102480888366699, "The Data Relay of the TGO Satellite is Second ExoMars mission."]
[4.120396137237549, 1.231115460395813, "The Mission Type of the FormoSat-7 / COSMIC-2 Satellite Constellation is Non-EO."]
[1.47739577293396, 4.815095901489258, "The Voltage levels of the EPS Electric Power Subsystem is 3.3 V, 5 V, battery output (nominal 3.7 V)."]
[9.217053413391113, 4.164956092834473, "The Structure Dimensions (Stowed) of the FY-3 series spacecraft Satellite is 4.4 m x 2.0 m x 2.0 m."]
[9.784272193908691, 8.161307334899902, "The Total Energy Channels of the GRS Gamma-Ray Spectrometer is 512."]
[3.2093708515167236, 5.313949108123779, "The Capacity of the Onboard Mass Data Storage Data Storage is 24 GByte."]
[9.141841888427734, 0.8224868178367615, "The Duration of the Radiation Effects Tests Testing Process is Months to execute."]
[1.5028899908065796, 4.932936191558838, "The Operating Voltage of the C&DH Subsystem Subsystem is 3.3 V."]
[11.360217094421387, 6.421557426452637, "The Detection of the X-ray pulsars Astronomical Objects is Detected."]
[7.658573150634766, 1.86708402633667, "The Date of the Superresolution Far-field Imaging Imaging Technique is 18 December 2018."]
[7.192869186401367, 1.3482905626296997, "The Workshop Date of the Brazilian EO Satellite Program Satellite Program is April 17-19, 2012."]
[8.656112670898438, 10.075081825256348, "The Image Quality of the SMART Imaging System is Better than direct imaging and PAIS."]
[8.440117835998535, 9.359575271606445, "The Micro-Roughness of the Primary Optics Optics is Better than 0.2 nm."]
[8.481390953063965, 11.044336318969727, "The IFOV of the Eastman Kodak KLI14403 linear CCD sensor Sensor is 32.07 \u00b5m."]
[10.20026969909668, 2.9919025897979736, "The Orbital Altitude of the LDEF Satellite is 477 km."]
[6.613513469696045, 6.430349826812744, "The Production Frequency of the SST Product Dataset is Every 10 minutes."]
[7.843591213226318, 2.9075746536254883, "The Conference Presentation Date of the DebriSat Fragments Space Debris is 25-29 Sept. 2017."]
[8.376007080078125, 2.9744722843170166, "The Years in Orbit of the TanDEM-X Satellite is 8 years."]
[4.411637783050537, 2.73877215385437, "The Interface Options of the Ubotica CogniSAT-XE1TM CubeSat Board Satellite Device is Gigabit Ethernet or USB2.0/3.0."]
[7.432086944580078, 7.110276699066162, "The URL of the GIADA Instrument is http://sci.esa.int/rosetta/35061-instruments/?fbodylongid=1639."]
[7.905380725860596, 9.646770477294922, "The Spectral Resolution of the Instrument Spectral Imager is 1.25 cm -1."]
[7.147184371948242, 7.405189514160156, "The Long-Term Stability Drift of the MIRAS Radiometer is 0.49 K or 1.46 K."]
[5.974850177764893, 2.9170725345611572, "The Partnership of the Astrocast and iWire Group Companies is Development and production of devices equipped with both Sigfox terrestrial connectivity and Astrocast Satellite IoT (SatIoT) services."]
[6.335203647613525, 4.026188850402832, "The Image Credit of the GOES 2nd generation spacecraft Satellite is NOAA."]
[1.7845872640609741, 4.184231281280518, "The Solar Array of the EPS Electric Power Subsystem is Single deployable with single-axis articulation capability."]
[11.627277374267578, 4.9904022216796875, "The Accretion of the V404 Cygni Black Hole is Material from a companion star."]
[4.276613235473633, 6.690024375915527, "The Processing Frequency of the RPU Receiver Processor Unit is 401.6 MHz."]
[6.444180488586426, 5.633022308349609, "The Mission Objective of the GNOS GNSS Occultation Sounder is Remote sensing of Earth\u2019s neutral atmosphere and the ionosphere."]
[6.144093036651611, 4.332870006561279, "The Data Access of the Airbus Satellite Satellite is Near real-time."]
[5.84801721572876, 8.11661148071289, "The Frequency (GHz) of the ICI-2 Radiometer is 183.31\u00b13.4."]
[5.9929609298706055, 3.4026718139648438, "The Led by of the GMES Initiative is EC (European Commission)."]
[8.586837768554688, 7.65086030960083, "The Operation Principle of the LENA Instrument is 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 ."]
[3.9932878017425537, 6.470443248748779, "The Architecture of the DPSK Transmitter Transmitter is MOPA."]
[6.2943806648254395, 6.887245178222656, "The Usage of the Doppler Velocity Sensor Velocity Measurement Device is Terminal landing phase."]
[7.776791095733643, 8.677704811096191, "The Instantaneous spectral coverage of the Spectrometer Instrument is 1.37 km/s."]
[7.93383264541626, 9.296034812927246, "The Spectral Resolution (86 keV) of the Detector Instrument is 1.2 keV."]
[6.192200660705566, 8.504965782165527, "The Measurement Range of the MIS Instrument Microwave Radiometer is 6 GHz to 183 GHz."]
[6.348041534423828, 3.065999746322632, "The Location of the Astrobiology Analytical Laboratory Laboratory is NASA\u2019s Goddard Space Flight Center in Greenbelt, Maryland."]
[8.057299613952637, 4.461700439453125, "The Spatial Resolutions of the GOCE Satellite is Half-wavelength."]
[8.270544052124023, 9.402405738830566, "The IFOV of the HgCdTe Detector is 170 \u00b5rad."]
[9.822771072387695, 6.677525997161865, "The Thermal Vacuum Test Environment of the Flight Model Satellite Model is Vacuum."]
[8.974000930786133, 9.870462417602539, "The Function of the Photo MOSFET Switch Component is Probe cleaning."]
[7.263324737548828, 9.280721664428711, "The Thermo-elastic Stability of the FG Filtergraph is Unknown."]
[5.320967674255371, 10.380548477172852, "The Detection of the LI Lightning Imager is Cloud to cloud, cloud to ground, and intra-cloud flashes."]
[9.300429344177246, 6.390084743499756, "The Use Case of the Specialized Asset Trackers Tracking Device is Knowing where your assets are and how your assets are being treated."]
[4.960868835449219, 3.8901288509368896, "The Function of the Spacecraft Bus Satellite Component is 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 ."]
[3.9277331829071045, 4.34413480758667, "The Development Time of the SCIP Processor is Too long."]
[8.52840518951416, 6.889776229858398, "The Vector Sample Rates of the NewMag Magnetometer is Internal = 1000/s, Standard = 10/s, Burst mode = 100/s."]
[8.078497886657715, 8.432679176330566, "The Observation Technique of the SHIMMER FTS Fourier Transform Spectrometer is 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."]
[2.466130495071411, 6.328705787658691, "The Latency Requirement of the S-2 NRT Product is Within 30 minutes."]
[8.722345352172852, 10.30523681640625, "The Manufacturer of the CMV4000 CMOS Color Detector is CMOSIS."]
[3.789581060409546, 6.0774970054626465, "The Data Delivery of the SWAP Payload is About 70 images per contact, delivered within 30 minutes to the SOC."]
[6.844376564025879, 5.836025238037109, "The Baseline of the Wind Speed Retrieval Algorithm Algorithm is Extension of one previously developed for the UK-DMC spaceborne mission."]
[9.478521347045898, 5.850212574005127, "The Orientation Accuracy of the Tethered System Attitude Control System is Within \u00b110 degrees of the vertical."]
[7.857302665710449, 10.794976234436035, "The Bit Depth of the Signal Digitization Process is 10 bit."]
[7.480695724487305, 9.753813743591309, "The SNR @Lref [EOL] of the Spectral Channel Detector is 202-408."]
[6.509883403778076, 1.3030074834823608, "The URL of the ISIM Compartment is http://www.jwst.nasa.gov/isim.html."]
[7.9239821434021, 10.259561538696289, "The Revisit Time at 20\u00b0 off nadir or less (0.51 m GSD) of the WV60 imager Imaging System is 5.9 days."]
[6.867922306060791, -0.038886599242687225, "The Second Flight Date of the MEPSI Satellite is July 2001."]
[7.240941047668457, 6.1092529296875, "The Measurement Range of the Aerosol Index (AI) Satellite Instrument is -1 to +5."]
[8.566174507141113, 7.556260585784912, "The Search Coil Diameter of the ULF Sensor Sensor is 5 cm."]
[2.545680522918701, 5.436163425445557, "The Power Consumption of the SGR-ReSI Interface Unit is 10 W."]
[7.870082378387451, 8.978589057922363, "The Wavelength Range of the Instrument Sensor is 115-180 nm."]
[4.369624614715576, 6.293410301208496, "The Frequency of the S-band Transmitter Transmitter is S-band."]
[3.194098472595215, 5.890983581542969, "The Data Retrieval Time Improvement of the SafetyNet Ground Data Receptor Network is More than 32 minutes."]
[6.586968898773193, 4.338559150695801, "The Imaging of the RADARSAT-1 Satellite is Radar Imagery."]
[1.7823007106781006, 5.353869915008545, "The Voltage of the Voltage 6 Modulator is 3.8\u00b12%."]
[5.651754856109619, 2.083822727203369, "The Deployment Mechanism of the STRaND-1 Satellite is ISIPOD CubeSat dispenser of ISIS."]
[1.5313920974731445, 4.840161323547363, "The Output Voltages of the EPS Electrical Power Subsystem is 8.4 V, 5 V, 3.3 V."]
[6.333576679229736, 3.134434461593628, "The Joint Endeavor of the ExoMars Mission is ESA and Roscosmos."]
[7.396059513092041, 0.31619054079055786, "The Launch Date of the CO2M Satellite is 2025."]
[4.272607803344727, 6.351769924163818, "The Purpose of the RF Crossover Switch Switch is Hedge against loss of one of the redundant UHF command and telemetry transceivers."]
[7.684288501739502, 10.457340240478516, "The ADC Resolution of the MuREM Radiation Monitor is 10 bit."]
[5.169974327087402, 4.009509086608887, "The Description of the SV-6 System Resource Flow Matrix DoDAF 2 Viewpoint is Tabular description of each data element exchange between two system function actions."]
[8.757440567016602, 0.7408378720283508, "The Arrival Date of the JUICE Spacecraft is 2029."]
[2.130154848098755, 4.538125514984131, "The Power of the Spacecraft Satellite is 2.5 kW (EOL)."]
[9.34977912902832, -0.5928274393081665, "The Conference Presentation Date of the TechnoSat Nanosatellite is Aug. 10-15, 2013."]
[7.798693656921387, 9.108007431030273, "The NER of the Spectral Band C Spectrometer is 1.7 x 10^-5 W/(cm^2 sr \u00b5m)."]
[9.18996524810791, 7.942022323608398, "The Focal Plane Temperature of the TIR Instrument Telescope is 60 K."]
[6.808518886566162, 8.585068702697754, "The Area of the . Wave mode (WM) Operational Mode is 20 km x 20 km."]
[5.182618141174316, 4.435007095336914, "The Subsystems of the IRPE Image Reception and Processing Element is 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)."]
[8.9556303024292, 2.884469747543335, "The Mission of the Lunar Reconnaissance Orbiter Satellite is LRO mission."]
[7.073911190032959, 9.743699073791504, "The Spectral Range (\u00b5m) of the Band 1 Spectral Band is 0.58 - 0.68."]
[9.456799507141113, 8.780135154724121, "The Mirrors of the Telescope Optical Instrument is Conics with a fourth-order aspherical term."]
[8.819511413574219, 6.866716384887695, "The Operation of the MAP-PACE Plasma Analyzer is Continuous."]
[10.220321655273438, 9.424478530883789, "The Resolution of the Iris Satellite is 100 times higher than any other satellite."]
[5.662890434265137, 3.00724196434021, "The Manufacturer of the Suomi-NPP Satellite is Ball Aerospace and Technologies Corporation (BATC)."]
[1.5878355503082275, 4.880539894104004, "The Power Input of the PDC Power/Data Controller is 28 VDC."]
[9.87740421295166, 1.465101957321167, "The Revisit Time at Equator of the HyperScout\u00ae Satellite is Around 45 days."]
[4.97712516784668, 4.726369857788086, "The Far-Field Pattern Irradiance Drop of the OGS Ground Station is Does not exceed 3dB."]
[9.94787311553955, -0.6014369130134583, "The Telescope Aperture of the Nanosatellite Satellite is 30 mm."]
[9.663334846496582, 2.147369861602783, "The Cross-Calibration Time Difference of the CloudSat Satellite is 30 minutes."]
[7.338993072509766, 3.0485329627990723, "The Unknown of the Kaber Spacecraft is Unknown."]
[3.5441625118255615, 4.713421821594238, "The Address Space of the LEON3 Processor is >24 bit."]
[8.294559478759766, 1.5389864444732666, "The Discovery Date of the Rosetta Satellite is 26 Oct. 2017."]
[5.270017623901367, 1.4095194339752197, "The Clocks of the GIOVE-B Satellite is 2 RAFS (Rubidium Atomic Frequency Standard)."]
[8.239593505859375, 1.4724242687225342, "The Observation Period of the STEREO-A Spacecraft is May 25 \u2013 June 1."]
[6.562573432922363, 3.3946053981781006, "The Disciplines of the Spacelab-1 Satellite Mission is Atmospheric science, solar science, materials science, space plasma physics, the life sciences, astrophysics."]
[2.12781023979187, 4.545495986938477, "The Power of the GOMS-1 Satellite is 1.5 kW."]
[3.532008171081543, 4.082763671875, "The Power of the STRV-1d DHS Data Handling System is 3 W."]
[10.87243366241455, 4.160537242889404, "The Target Stars of the CHEOPS Satellite is Small exoplanets previously detected by accurate Doppler surveys and known transiting Neptune-size planets detected by ground-based photometric surveys."]
[10.34528923034668, 2.9126904010772705, "The Altitude of the LLITED CubeSat Satellite is Lower altitudes."]
[6.611235618591309, 4.0370588302612305, "The Mission of the Arktika-M N1 Satellite is 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."]
[5.534447193145752, 3.187483787536621, "The Bus Type of the GF-2 Satellite is CAST-CS-L3000A."]
[12.044631958007812, 3.3003528118133545, "The Orbit Inclination of the DubaiSat-1 Satellite is 98.13\u00ba."]
[11.1041259765625, 2.837775230407715, "The Length of the Scandinavian Peninsula Landform is Approximately 1850 km."]
[11.472596168518066, 4.429921627044678, "The Study Level of the Stardust Grain Particle is Atomic."]
[11.720023155212402, 4.62113618850708, "The Distance from the Sun of the Galactic Center Center of the Milky Way is Almost 30,000 light years."]
[8.925939559936523, 3.283820152282715, "The Orbit of the Spacecraft Satellite is MEO."]
[7.688542366027832, 8.978192329406738, "The Spectral Resolution of the MAHRSI Instrument is 0.018 nm at 310 nm."]
[8.081127166748047, 10.017142295837402, "The Spatial Resolution of the GOES Imager Imager is 4 km x 4 km on MWIR and TIR bands, 1 km x 1 km on VIS band."]
[10.41452693939209, 8.33340072631836, "The Authors of the Proposed visible emission line space solar coronagraph Solar Coronagraph is 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. Sri."]
[4.528521537780762, 4.33999490737915, "The Subsystems of the AVUM Upper Module is GNC (Guidance Navigation and Control), SAS (Electric Safeguard Subsystem), TMS (Telemetry Subsystem)."]
[6.853675365447998, 2.676469326019287, "The Data Usage of the Carbonite-2 Satellite is UK\u2019s Royal Air Force (RAF) for use by the Joint Force Command National Centre for Geospatial Intelligence."]
[7.232773303985596, -0.4041183590888977, "The Anticipated Global Connectivity Timeline of the Starlink Satellite Constellation is A few months after the 28th launch."]
[7.83693265914917, 7.552051544189453, "The Sensitivity of the GOLF Instrument is 1 mm/s."]
[9.078035354614258, 6.253529071807861, "The Location of the MEMS 3-axis Gyro Device is Zenith end assembly."]
[9.145161628723145, 5.831950664520264, "The Attitude Sensors of the SUNSAT Satellite is 3-axis fluxgate magnetometer, 2-axis horizon sensor, fine slit sun sensor, second star sensor."]
[11.693565368652344, 4.5863471031188965, "The Number of Stars of the M33 galaxy Galaxy is Forty billion."]
[4.2999725341796875, 4.8183794021606445, "The Standard of the OOK Modulated Optical Satellite Communications System Communication System is CCSDS."]
[12.937765121459961, 4.818842887878418, "The Orbit Type of the IBEX Spacecraft is Highly Elliptical Orbit."]
[6.347305774688721, 7.916840553283691, "The Satellite Launch Date of the AMSU/HSB Advanced Microwave Sounding Unit/Humidity Sounder for Brazil is May 4, 2002."]
[8.78927993774414, 7.958514213562012, "The Data Processing of the EPD Sensors Sensors is Manual for first data release, future automation planned."]
[11.576727867126465, 6.224267959594727, "The Observation Speed of the XMM-Newton X-ray Observatory is Speeded up for illustration purposes."]
[8.220338821411133, 9.147281646728516, "The 15% FWHM of the Energy Resolution Sensor is Energy resolution (delta E/E) 15% FWHM (Full Width Half Maximum)."]
[5.982804298400879, 1.9333826303482056, "The Operation Start Year of the SAR-Lupe Satellite System is 2008."]
[7.526979923248291, 8.900579452514648, "The Resolution Cell, Vertical of the Instrument Spectrometer is 4 km."]
[5.863770008087158, 5.678863525390625, "The Function of the ROSA Radio Occultation Antenna Antenna is Receive signals from the GPS constellation during their occultation time window."]
[6.124673843383789, 3.31217885017395, "The Design Verification of the ESA Young Engineers Satellite 2 Satellite is FEM Analysis."]
[10.46953296661377, 4.676429748535156, "The Accumulated Firing Time of the LM thruster Thruster is Over 6.0 minutes."]
[7.765122413635254, 8.218935012817383, "The Sensor Type of the TANSO-FTS Sensor is Fourier Transform Spectrometer."]
[8.876238822937012, 3.284442186355591, "The Orbit of the SEOSAT/Ingenio Satellite is Low Earth Orbit."]
[8.009998321533203, 2.9097657203674316, "The Mission Principal Investigator of the IMAP Interstellar Mapping and Acceleration Probe is David McComas."]
[8.10692024230957, 2.191788911819458, "The Launch Year of the Himawari-9 Satellite is 2016."]
[6.536105632781982, -0.07431097328662872, "The Location of the IRNSS-1C Satellite is 83\u00baE."]
[6.352064609527588, 3.119997024536133, "The Operation of the Sentinel-6 Satellite is Fly in tandem with the Jason-3 spacecraft."]
[6.015645503997803, 6.343799114227295, "The Full SAR Access Range of the SAR Synthetic Aperture Radar is Ten swaths in quad-pol (QP) mode and nine swaths in dual-pol mode."]
[7.85805082321167, 6.092747211456299, "The Star Calibration Frequency of the Satellite Imaging Satellite is During commissioning."]
[4.10067081451416, 5.703940391540527, "The Data Capture Rate of the MinXSS-2 Satellite is At least 6%."]
[6.9501423835754395, 4.5967116355896, "The Data Collection of the Mission Satellite Mission is Atmospheric and oceanic data."]
[10.196493148803711, 2.9505386352539062, "The Initial Orbit Altitude of the Satellite PUNCH Mission is 570 km."]
[11.637779235839844, 6.113297939300537, "The Brightness Change Time Scales of the XMM-Newton X-ray Satellite is Up to 14.5 years."]
[8.283095359802246, 9.193639755249023, "The Pixels per FWHM of the Spectrometer Instrument is 580."]
[7.075189590454102, 4.451943397521973, "The Sensor Type of the TET-1 Satellite is Mid-wave and longwave infrared."]
[8.01809024810791, 4.069685459136963, "The Purpose of the Switch Matrix Experiment is On-Orbit-Verification."]
[5.263149738311768, 4.254849910736084, "The Benefits of the EGS-CC Space Control System is 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 t."]
[4.355506420135498, 7.210026264190674, "The Size of the X-band transmitter Transmitter is m3-sized."]
[9.50754451751709, 0.6041567325592041, "The Mission Lifetime of the NEMO-HD Satellite is One year."]
[6.778613567352295, 2.1035118103027344, "The Data Update Frequency of the GPM Global Precipitation Measurement mission is Every 30 minutes."]
[4.954288482666016, 6.666104316711426, "The Gain of the Antennas Antenna is \u20134 dBic minimum."]
[9.547511100769043, 0.5348328351974487, "The Design Lifetime of the CIMR Satellite is 7 years."]
[8.786714553833008, 10.339299201965332, "The Pixel Pitch of the GOCI-II CMOS Imaging Sensor CMOS Imaging Sensor is 6.8\u03bcm."]
[11.99820327758789, 3.356560230255127, "The Orbital Inclination of the Solar Orbiter Spacecraft is 17\u00ba (by 2025), 33\u00ba (by the end of the decade)."]
[8.279138565063477, 9.560107231140137, "The Ground Sample Distance (GSD) of the PAN Imaging System is 1 m."]
[5.856766700744629, 2.9511678218841553, "The Manufacturer of the WorldView-1 Satellite is DigitalGlobe Inc.."]
[7.6885905265808105, 9.009387016296387, "The Bandwidth of the Instrument Spectrometer is 20 nm (for 415, 750, 900,950 nm); 30 nm (for 1000, 1050, 1250 nm)  50 nm (1550 nm)."]
[4.994109630584717, 6.6881794929504395, "The Gain of the Onboard Antenna Antenna is 13.5 dBi."]
[9.850860595703125, -0.6505424380302429, "The Orbit Perigee of the BX-1 Microsatellite is 280 km."]
[6.5608344078063965, 2.6792852878570557, "The Funding Source of the SPIDER Telescope is DARPA (Defense Advanced Research Projects Agency)."]
[6.937170028686523, 2.7070722579956055, "The Regions of the AAI Air Navigation Service Provider is Mumbai, Chennai and Kolkata's oceanic airspaces."]
[6.851621627807617, 7.453517913818359, "The Operation of the Laser Retro Reflector (LRR) Tracking Device is Enabled tracking by ground-based satellite laser ranging stations."]
[8.822105407714844, 9.010819435119629, "The Dimensions of the Grating Optical Component is 10 cm x 20 cm."]
[7.1342339515686035, 4.2447309494018555, "The Coverage of the Copernicus Sentinel-5P Satellite is Global."]
[8.487584114074707, 11.073516845703125, "The GSD of the Eastman Kodak KLI14403 linear CCD sensor Sensor is 22 m."]
[8.210474014282227, 9.092169761657715, "The Swath Width of the OLI-2 Sensor is 185 km."]
[4.374727249145508, 5.734540939331055, "The Payload Uplink of the Dove-2 Satellite is 30 kbit/s over 2.4 GHz radio."]
[7.341759204864502, 0.05252877622842789, "The Program Start Date of the DRACO Demonstration Rocket is Over a year ago."]
[6.099044322967529, 9.707254409790039, "The Mass of the CONSERT Experiment is 1.8 kg."]
[10.79260540008545, 3.4755985736846924, "The Closest Approach to Sun's Surface in 2022 of the Solar Orbiter Satellite is Within 48 million km."]
[3.4994864463806152, 4.688948154449463, "The Microcontroller Clock Speed of the On-board Computer Computer is 16 MHz."]
[7.400801181793213, 3.424086332321167, "The Sensor of the SWOT Satellite is KaRIn (Ka-band Radar Interferometer)."]
[9.337478637695312, -0.6955535411834717, "The Conference Presentation Date of the Delfi-C3 Nanosatellite is June 9-11, 2005."]
[6.647397518157959, 0.5956740975379944, "The Launch Year of the GOES-U Satellite is 2024."]
[4.829566478729248, -3.3994927406311035, "The Member of the Ana Barros Individual is True."]
[8.899359703063965, 8.95647144317627, "The Orientation Deviation of the Collimator Optical Device is -0.27\u00b0 to -0.25\u00b0 in horizontal and 0.40\u00b0 to 0.48\u00b0 in vertical direction."]
[12.071839332580566, 3.2440969944000244, "The Orbit Inclination of the KySat-1 Satellite is 98.2\u00ba."]
[10.430727005004883, -1.122436761856079, "The Mass of the NIUSAT Nanosatellite is 15 kg."]
[6.923429489135742, 1.163364291191101, "The Presentation Date of the Small Satellites Satellite is April 3-6, 2017."]
[9.500788688659668, 7.674597263336182, "The Cryocooler of the WFIRST Observatory is Eliminated in favor of passive cooling of the WFI cold electronics."]
[8.23331069946289, 2.618889331817627, "The On-orbit Calibration Target of the ARTEMIS Satellite is Panel with relatively flat spectral reflectance and measured reflectance characteristics."]
[8.034130096435547, 1.2508195638656616, "The Image of the Day Date of the NASA Earth Observatory Satellite is 21 May 2022."]
[9.146289825439453, 4.525033950805664, "The Transfer Phase Start of the LUMIO Satellite is Stable Manifold Injection Maneuver."]
[7.083034515380859, 4.366945743560791, "The Video Camera Assembly of the LAPAN-A2 Satellite is Two cameras, featuring analog and digital outputs respectively."]
[4.712636947631836, 3.900376796722412, "The Data Distribution Center of the SAMPEX Satellite is UMSOC (University of Maryland Science Operation Center)."]
[3.966326951980591, 4.341074466705322, "The Components of the C&DH subsystem Command & Data Handling Subsystem is Controller card (CC), data handling card, Power Supply Card (PSC), Input/Output Card (IOC), Mission Interface Card (MIC)."]
[5.515608787536621, 2.928504705429077, "The Bus Platform of the Restore-L Satellite is 1300-class."]
[5.966038227081299, 6.2822418212890625, "The Quad Pol Swath Width of the SAR Processor Data Processor is 175 km."]
[5.1656928062438965, 4.364635467529297, "The Manager of the CGS Ground System is Raytheon."]
[5.541379928588867, 5.55811882019043, "The Design of the GPSP Instrument is Blackjack."]
[12.122980117797852, 3.291780948638916, "The Inclination of the FY-3E Satellite is 98.7\u00ba."]
[9.705642700195312, 1.2821367979049683, "The Deployment Confirmation Time of the STSAT-3 Satellite is About 6 hours after lift-off."]
[6.144023895263672, 0.5880229473114014, "The First Signal Reception Date of the Pico Dragon CubeSat is Nov. 20, 2013."]
[4.694287300109863, 7.075805187225342, "The Dimensions of the Card Size Communication System is 15.3 cm x 23 cm."]
[5.347500324249268, 6.731045722961426, "The Duration of the Chirp Signal is ~100us."]
[9.517641067504883, 0.505908727645874, "The Design Life of the Kanopus-V Satellite is 5 years."]
[8.467840194702148, 7.091988563537598, "The Dipole Antenna Length of the IOF Plasma Wave Instrumentation is 121.8 m."]
[7.6739702224731445, 7.658997058868408, "The Measurement Category of the OCO-3 Instrument is Trace gases (excluding ozone)."]
[2.0561845302581787, 4.774561882019043, "The Power Conversion of the PPM Power Processing Module is 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."]
[11.175774574279785, -1.5164141654968262, "The Mass of the Flock-1c CubeSat is 5 kg."]
[8.373720169067383, 3.3807897567749023, "The Horizontal Sampling of the TanDEM-X Satellite is 12 m by 12 m."]
[9.204031944274902, 2.000464916229248, "The Sampling of the Satellite LEO (Low Earth Orbit) is Poor spatial and temporal sampling: each point on globe sampled just once every day on dayside, once nightside."]
[3.421416997909546, 5.379968643188477, "The Tx-TNC Cache Memory of the RF Communication System Communication System is 128 byte."]
[8.848607063293457, 8.878138542175293, "The Coating of the Grating Optical Component is 200 nm gold."]
[7.673044204711914, 7.015255928039551, "The Data Transmission Frequency of the Instrument Photometer is About once a month."]
[7.933400630950928, 3.7392334938049316, "The Size of the Pelican Constellation Satellite Constellation is Not revealed."]
[6.574078559875488, 0.6601522564888, "The Launch Date of the EgyptSat-2 Satellite is May 5, 2014."]
[6.707374095916748, 4.225851058959961, "The User Consultation Working Groups of the Sentinel-1 Satellite is Marine Core Services, Land Monitoring and Emergency Services."]
[3.827244758605957, 0.2888379693031311, "The DOI of the GRAIL Satellite is 10.1038/nature13697."]
[9.367530822753906, 8.463532447814941, "The URL of the Spectrometer Telescope Telescope is http://www.esep.pro/sites/esep/IMG/pdf/poster_spie12_stix_8443-131_v3.pdf."]
[7.88062858581543, 9.375106811523438, "The Spectral Range of the SWIR bands Satellite is Shortwave (SW) infrared (IR) bands include: 940, 1038, 1250, 1378, 1615, 2130, and 2260 nm."]
[9.251389503479004, 10.766899108886719, "The Altitude of the MCAM-2 Camera is 200 km."]
[4.98967981338501, 1.8722869157791138, "The Number of Institutions of the ASTRO-H Mission is 58."]
[10.122897148132324, 9.471774101257324, "The Far-UV Channel Spectral Resolution of the IRIS Observatory is 4 x 10-3 nm."]
[10.872261047363281, 5.687495708465576, "The Publication Date of the Can ripples on the sun help predict solar flares? News Article is 21 September 2020."]
[11.519543647766113, 6.423042297363281, "The Number of Publicly Released X-ray Source Catalogues of the XMM-Newton Survey Science Center Consortium is 6."]
[1.859440565109253, 4.056745529174805, "The Light-Shade Cycle Frequency of the Solar Panels Power Source is 16 times per day."]
[3.775527238845825, 5.708433628082275, "The Data Rate of the MTG-S Spacecraft Satellite is 3 GByte/s at instrument output."]
[8.657050132751465, 4.088143348693848, "The Filter of the BRITE Telescope is Single Color."]
[7.559540271759033, 7.932477951049805, "The Shortwave Range of the CERES Instrument is 0.3 - 5.0 \u00b5m."]
[3.611300468444824, 6.560306072235107, "The BER (Bit Error Rate) of the S-band Transmitter Transmitter is 10 -5."]
[8.476439476013184, 7.836850166320801, "The Cadence of the Neutral Particle Dose Rate Measurement is 1 minute."]
[5.36030387878418, 6.341305255889893, "The Antenna Polarization of the GPS Reflectometry Receiver Instrument is RHCP (Right-Hand Circular Polarization) and LHCP (Left-Hand Circular Polarization)."]
[11.575305938720703, 6.310376167297363, "The Publication Date of the S-054 X-ray Telescope X-ray Telescope is Feb. 1977."]
[3.9649837017059326, 4.500979423522949, "The Data Interface of the OBC On-Board Computer is I2C bus."]
[8.299068450927734, 8.59438705444336, "The Sensor Provider of the Near-Infrared Spectroscopy and Photometry Instrument (NISP) Instrument is NASA."]
[8.490853309631348, 8.32264232635498, "The Number of Analyzers of the FlaPS Instrument Package is 16."]
[7.6950297355651855, 9.30290412902832, "The Spectral Bands of the Anand Satellite is Over 150."]
[5.980856418609619, 10.795703887939453, "The Transmission Profile of the PF2 Passband Filter is Unknown."]
[11.718387603759766, 4.577383041381836, "The Diameter of the Pleiades Open Cluster is About 35 light years."]
[7.534359455108643, 0.49010032415390015, "The Importance of Temporal Domain of the SVOM Satellite is Recognized in recent reports by the Chinese Space and Technology Roadmap, the European Union ASTRONET group and the USA National Research Council Decadal Survey."]
[7.0856099128723145, 0.835310161113739, "The Operation Status of the Genesis-2 Satellite is Nominal in 2012."]
[9.269523620605469, 10.02498722076416, "The Number of Lunar Transit Images of the EPIC Earth Polychromatic Imaging Camera is Two."]
[5.452749252319336, 7.292726993560791, "The Beam width of the S-band Band is 0.64 rad."]
[8.786784172058105, 8.985910415649414, "The Average Incidence Angle of the Convex Holographic Grating Grating is Approximately 38.2 \u00ba."]
[9.495943069458008, 8.944231033325195, "The Ground Sampling Distance of the Telescope Optical Instrument is 30 m."]
[10.372767448425293, 4.5929765701293945, "The Total Velocity Change of the Propulsion Subsystem Propulsion is \u0394V = 334 m/s."]
[11.533297538757324, 2.7052676677703857, "The Composition of the Psyche Asteroid is Mostly iron and nickel."]
[8.523768424987793, 7.18563985824585, "The Type of the BSA Beam Steering Assembly is 2-axis small range pointing mechanism."]
[6.331630706787109, 5.217190742492676, "The Usage of the INS Navigation System is First burn, second burn."]
[5.255410194396973, 3.8668155670166016, "The Location of the Payload Modules Satellite Components is Section close to the antenna."]
[7.745723247528076, 13.553397178649902, "The Resolution \u0394\u03bb (0.05\u00ba slit) of the SPIM2 Spectrometer is 0.9 nm."]
[6.732587814331055, 3.1295359134674072, "The Mission Status of the MOMS Satellite is Mission complete."]
[6.187506675720215, 3.045640230178833, "The Name Change of the SRTM Shuttle mission is NIMA (National Intelligence Mapping Agency) changed its name to NGA (National Geospatial-Intelligence Agency)."]
[8.250407218933105, 8.511561393737793, "The Fringe Distortions for Monochromatic Light of the SHS Interferometer is Provide a measure of the grating figure errors."]
[8.902400970458984, 5.327108860015869, "The Point-Spread-Function Hold Requirement of the Attitude System Satellite System is Within 3 pixels of the original point locations."]
[7.417820453643799, 0.7302942276000977, "The Last Launch Year of the Space Shuttle Spacecraft is 2011."]
[11.613812446594238, -1.251206636428833, "The Propellant for Station Keeping of the Geo Satellite Satellite is 1 ton."]
[8.729230880737305, 2.741741418838501, "The Orbit Type of the ARTEMIS Probes Spacecraft is Lissajous orbit near the Earth-Moon Lagrange points."]
[10.412163734436035, 7.217357635498047, "The Activation Method of the TEMBOTM EMC Material is Heat-activated."]
[8.637228965759277, 4.1585845947265625, "The Design of the BRITE Telescope is Low Cost and Risk Mitigation."]
[7.561439514160156, -0.49118655920028687, "The Launch Date of the Falcon Heavy Rocket is 25 June 2019."]
[3.0641844272613525, 6.652153491973877, "The Power of the VHF Transmitter Radio Transmitter is 8 W."]
[5.6915283203125, 6.783555507659912, "The Wavelength/Frequency of the X-band Radar is 32 mm/9.7 GHz."]
[7.525707721710205, -0.4628097414970398, "The Landing Date of the Falcon 9 first stage Rocket is Jan. 11, 2015."]
[8.062028884887695, 10.091614723205566, "The SWIR Spatial Resolution of the iSIM-90 Imager is 13 m."]
[6.16105318069458, 8.164422988891602, "The Center Frequency of the Radiometer Instrument is 1.41 GHz."]
[4.33507776260376, 2.4241864681243896, "The Satellite Type of the Hyper-Angular Rainbow Polarimeter Polarimeter is 3U CubeSat."]
[6.864589214324951, 3.228349447250366, "The Mission Status of the EO-1 Satellite is Operational."]
[7.430262088775635, 8.70689868927002, "The Spatial Resolution of the Atmospheric-sounding instrument Spectrometer is Better than 50 km2 over several across-track pixels."]
[7.296580791473389, 9.48398208618164, "The Swath Width of the S-192 optomechanical scanner Scanner is 72.4 km."]
[11.649495124816895, 4.306768894195557, "The Number of Transiting Super-Earths of the K2-155 M Dwarf Star is 3."]
[7.367271423339844, 5.548861503601074, "The Horizontal Integration of the Aeolus Satellite is 50 km."]
[8.950620651245117, 9.230025291442871, "The FOV of the Instrument Spectrometer is 11\u00ba."]
[5.979599475860596, 6.31658935546875, "The Polarization of the ICEYE SAR (Synthetic Aperture Radar) Sensor is Circular."]
[9.687251091003418, 8.868213653564453, "The Clear Aperture of Telescope of the DubaiSat-1 Satellite is 30 cm."]
[5.673032283782959, 3.858869791030884, "The Location of the MC3E Field Campaign is DOE-ASR Central Facility in Oklahoma."]
[9.406868934631348, 5.490608215332031, "The Actuators of the IRS-1C and IRS-1D Spacecraft is Four reaction wheels, two magnetic torquers, 16 one Newton hydrazine trusters, one 11 Newton thruster."]
[4.8085832595825195, 2.0854039192199707, "The Quantity of the AMICalSat Satellite is 1."]
[9.321500778198242, 7.77492094039917, "The Optimal PMT Temperature of the Detector Box Instrument is -20\u00b0C."]
[10.978378295898438, 5.011260032653809, "The Centrifugal Force of the LISA Pathfinder Spacecraft is Small."]
[9.362869262695312, 7.849028587341309, "The Measurement Range of the Particle Detector Instrument is Helium-3 : 21 MeV/n ~ 84 MeV/n."]
[11.137414932250977, 5.190736293792725, "The Journal Publication Date of the LISA Technology Package LTP Technology Package is 2006."]
[10.351720809936523, 2.8256967067718506, "The Perigee of the Satellite Orbit is 324 km."]
[8.395037651062012, 9.154659271240234, "The Panchromatic Image Data of the Optical Sensor Assembly (OSA) Instrument is 6500 lines/s."]
[11.320852279663086, 1.255234956741333, "The Distance from Mars of the Tianwen-1 Mars Mission is 1.1 million kilometers."]
[4.434333801269531, 5.233748435974121, "The Redundancy of the Phoenix GPS Receivers GPS Receiver is Cold redundant pair."]
[1.1651908159255981, 4.27435827255249, "The Power Source of the EPS Electrical Power Subsystem is Rechargeable Li-ion battery."]
[5.668783664703369, 2.804572343826294, "The Manufacturer of the EUTELSAT KONNECT Satellite is Thales Alenia Space."]
[3.8148701190948486, 0.2847599685192108, "The URL of the GRAIL Mission is http://science.nasa.gov/headlines/y2008/22may_grail.htm."]
[11.487629890441895, -1.2443498373031616, "The Total Mass of the GeneSat-1 Satellite is Not provided."]
[8.655324935913086, 6.895837783813477, "The Type of the Magnetic Field Sensor Sensor is Two-axis."]
[6.799408912658691, 1.4381190538406372, "The Conference Date of the NICT's New OGS Ground Station is May 16-20, 2016."]
[5.973678112030029, 10.797391891479492, "The Transmission Profile of the PF1 Passband Filter is Unknown."]
[4.472200870513916, 2.9892497062683105, "The PRN of the GSAT-0210 Satellite is 1."]
[8.456703186035156, 6.85300874710083, "The Manufacturer of the Vector Magnetometer Instrument is DRSI (Danish Space Research Institute)."]
[7.592388153076172, 5.472919464111328, "The Rainfall Impact of the OCO-2 Satellite is More carbon being released into the atmosphere."]
[2.632988452911377, -1.456423282623291, "The Brigthness Temperature (BT) Sensitivity of the Antenna Reflector is \u00b10.42 K."]
[9.567078590393066, 0.4317142367362976, "The Design Life of the HY-1C Satellite is 5 years."]
[9.542818069458008, 7.751486778259277, "The Energy Range of the EPD-I Energetic Particle Detector - Ions is 50 keV \u2013 300 keV."]
[7.12628173828125, 1.8804231882095337, "The SAR Tandem Mission Date of the ERS-2 Satellite is September 2007 to February 14, 2008."]
[3.9377756118774414, 4.393267631530762, "The Operating System of the OBC On Board Computer is CANOE (Canadian Advanced Nanospace Operating Environment)."]
[8.31739330291748, 6.54921817779541, "The Components of the SWE Sensor Web is SensorML, Observations and Measurements."]
[9.283646583557129, 0.9604595303535461, "The Data Collection Duration of the RAVAN CubeSat is 20 months."]
[5.803081035614014, 3.9033384323120117, "The PGDS Location of the FOS Satellite is ESRIN."]
[7.11219596862793, 5.15765905380249, "The Expected Nitrogen Dioxide Emissions Restriction of the International Shipping Emission Regulations Regulation is Coming years."]
[10.580934524536133, 7.498768329620361, "The Structure Material of the UniSat-5 Satellite is Aluminum honeycomb reinforced by aluminum internal panels."]
[9.650229454040527, 5.617044925689697, "The ADCS System of the DeorbitSail Satellite is First in-orbit demonstration of the CubeComputer."]
[8.174790382385254, 10.064533233642578, "The Pixel Size of the IIR Imager is 1 km."]
[11.599682807922363, -1.1974329948425293, "The Payload Volume of the Supernova-Beta Satellite is 7000 cm3."]
[0.9533331394195557, 4.236478805541992, "The Capacity of the Batteries Electrical Power Subsystem is 5.2 Ah."]
[7.212674617767334, 6.812705993652344, "The Development Status of the 3MI Instrument is PDR completed in October 2015, moving toward a CDR scheduled in January 2018."]
[9.486525535583496, 0.892605721950531, "The Mission Duration of the SPOT-3 Satellite is Three years."]
[3.595470428466797, 2.3105690479278564, "The Size of the OptiCube-3 Satellite is 3U."]
[3.78322434425354, 5.030375003814697, "The Products in Nominal Phase of the Mission Operation System Data Processing System is About 2 PB."]
[5.352468490600586, 3.6580121517181396, "The Communication Standard of the CFESat Satellite is IP (Internet Protocol)."]
[5.220759391784668, 6.067962169647217, "The Frequency of the Pyxis-RO Instrument is 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)."]
[4.12728214263916, 1.331365942955017, "The Mission Type of the PW-Sat CubeSat is Non-EO."]
[6.195965766906738, 4.080764293670654, "The Funding of the GeoXO Satellite System is NOAA."]
[11.687957763671875, 4.6026153564453125, "The Names of the Phantoms Mannequin Torsos is Helga and Zohar."]
[6.928947925567627, 1.9164365530014038, "The Data Set Duration of the Global Satellite Mapping of Precipitation (GSMaP) Satellite Data is Less than twenty years."]
[7.339303016662598, 2.524165391921997, "The URL of the SOHO Satellite is http://www.nasa.gov/content/goddard/soho-captures-jan-14-2014-cme/#.Uz0sNaKegkA."]
[6.8768486976623535, 7.291963577270508, "The Manufacturer of the ASIM Instrument is Danish company Terma, the Danish Technical University, the University of Bergen in Norway and the University of Valencia in Spain."]
[4.213677406311035, 4.906268119812012, "The Message Format of the SpW Data Transfer Protocol is ECSS PUS."]
[6.497748851776123, 0.7095714807510376, "The Battery Operations Presentation of the TET-1 Spacecraft is SpaceOps 2014."]
[5.3297343254089355, 3.650761842727661, "The Common Methods of the Deployment Mechanisms Satellite Component is Nichrome burn wires, breakable links made of plastic retaining bars."]
[7.924797058105469, 8.007416725158691, "The Measurement Accuracy of the ATOMMS Spectrometer is 1% or better."]
[8.886931419372559, 9.221158027648926, "The FOV of the STAFF/DWP Instrument is \u00b13\u00bax 180\u00ba(IIMS), \u00b117.5\u00ba x 180\u00ba (IES)."]
[6.280533790588379, 2.870927572250366, "The Principal Investigator of the Carruthers Geocorona Observatory Spacecraft is Lara Waldrop."]
[9.393813133239746, 5.129360198974609, "The Reaction Wheel Spin of the Integral Satellite is 5 times its maximum when under control."]
[7.289079189300537, 1.3047964572906494, "The De-orbiting End Date of the ERBS satellite Satellite is August 15, 2003."]
[10.391343116760254, 4.79386568069458, "The Propulsion System of the Jason-3 Satellite is Hydrazine."]
[3.469202756881714, 5.243439674377441, "The Data Storage of the Satellite Spacecraft is At least two and a half orbits of mission data."]
[7.099635124206543, 4.428886890411377, "The Imaging Camera of the DSCOVR satellite Satellite is Earth Polychromatic Imaging Camera."]
[7.36774206161499, 0.35720425844192505, "The Launch Date of the HySIS Satellite is 29 November 2018."]
[5.831591606140137, 2.487792491912842, "The Phased-Array Technology of the SARah Satellite Constellation is Developed by Airbus DS GmbH."]
[8.680274963378906, 10.069059371948242, "The SNR Improvement of the PAIS Imaging System is When the subaperture area is increased."]
[8.285207748413086, 8.35854721069336, "The Joint Instrument of the MIRI Mid-Infrared Camera-Spectrograph is JPL and ESA."]
[10.281394004821777, 9.454095840454102, "The Field of View of the IRIS Satellite is 171 arcsec."]
[4.673956871032715, 6.843568801879883, "The Accuracy of the DORIS Receiver is About 1m."]
[8.523378372192383, 8.143272399902344, "The Gain Control of the MCP (Microchannel Plate) Detector Detector is Voltage applied to the front surface."]
[8.891173362731934, 5.235705852508545, "The Attitude Subsystem Stability of the Spacecraft Satellite is 0.009\u00ba/s (3\u03c3)."]
[7.5202765464782715, 4.251522064208984, "The Spatial Resolution of the DMC-3 Satellite Constellation is 1 m."]
[8.545064926147461, 9.11510181427002, "The Band 2 of the R3 Sensor Sensor is Blue."]
[10.906084060668945, 4.002418518066406, "The Expected Data Collection of the Nancy Grace Roman Space Telescope Space Telescope is More than any of NASA\u2019s other astrophysics missions."]
[8.181018829345703, 0.2524102032184601, "The Debut Date of the CIMON Astronaut Assistant is 15 November 2018."]
[11.32521915435791, 2.360302209854126, "The Rotation Period of the Asteroid 1999JU3 Asteroid is Around 7.6 hours."]
[4.054442405700684, 4.025986671447754, "The Unknown of the LDRS-PEM Payload Electronics Module is Low Data Rate System - Payload Electronics Module (LDRS-PEM)."]
[8.364270210266113, 7.38777494430542, "The Publication Date of the Spaceborne Frequency Comb Metrology Metrology System is Dec. 2016."]
[5.917519569396973, 9.569568634033203, "The Mass of the ASPOC Instrument is 2.5 kg."]
[7.253542900085449, 2.2702407836914062, "The Launch Readiness of the Emirates Mars Mission Satellite is Ready for Launch."]
[4.809159278869629, 7.447763442993164, "The Telescope Diameter of the Submillimeterwave receiver Receiver is 30 cm."]
[5.280633926391602, 1.4399563074111938, "The Clocks of the GIOVE-B Satellite is 10 ns per day."]
[11.314796447753906, 1.0815144777297974, "The Design Lifetime of the Tianwen-1 Spacecraft is One Martian year, or 687 Earth days."]
[9.56694221496582, -0.5047460198402405, "The Communication of the BIROS Minisatellite is On board AVANTI experiment programs."]
[7.591005802154541, 3.57725191116333, "The Remapping Frequency of the 90-satellite constellation Satellite Constellation is Weekly."]
[5.492427349090576, 1.945533037185669, "The Picosat Distribution of the OPAL Satellite is 4 short and 2 long."]
[8.346362113952637, 1.5356850624084473, "The Arrival Date of the Rosetta Satellite is August 6, 2014."]
[6.530717372894287, 6.2771382331848145, "The Cell Resolution of the OSCAT Scatterometer is 25 km x 25 km."]
[9.45162582397461, 1.7329394817352295, "The Global Coverage Frequency of the Sentinel-2 Satellite is Every 10 days with one satellite, every 5 days with two satellites."]
[10.4500093460083, 2.6293232440948486, "The Apogee of the Molniya Orbit Orbit is 39750 km."]
[5.65805721282959, 2.3781659603118896, "The Space Situational Awareness Increase of the SBSS-1 Satellite System is Factor of three."]
[3.530463695526123, 4.546375274658203, "The Manufacturer of the Second FPGA FPGA is Xilinx."]
[9.159124374389648, 5.329267501831055, "The Vector Inputs of the Slew Mode Satellite Mode is Magnetometer and sun sensor vectors."]
[6.977616786956787, 1.0480148792266846, "The Initiative Date of the Small GEO Satellite Satellite is April 16, 2007."]
[11.745491981506348, 7.489130973815918, "The Time Delay of the Deep Space Atomic Clock Atomic Clock is About five times better than what the team reported in the spring of 2020."]
[11.57444953918457, -1.2760181427001953, "The Mass of the STRaND-1 Satellite is ~ 4.3 kg."]
[10.662067413330078, 9.174023628234863, "The Image Capture Date of the CaSSIS Instrument is 18 November 2018."]
[3.0236425399780273, 6.60458517074585, "The Downlink RF Output Power of the RF Communication System Communication System is 1 W."]
[7.133060455322266, 2.8023111820220947, "The Purpose of the SWOT Satellite is Study small-scale features of ocean surface."]
[5.916665077209473, 6.192398548126221, "The Number of Beams for Standard Imaging Mode of the COSI SAR Mission is 31."]
[8.504844665527344, 9.107609748840332, "The Band 4 of the R3 Sensor Sensor is NIR."]
[11.111283302307129, 5.143970966339111, "The LTP Duration of the LISA Pathfinder Satellite is 90 days."]
[7.208456993103027, 0.2794296443462372, "The Launch Date of the MULA Satellite is 2025."]
[6.684362888336182, 1.358992338180542, "The Partnership Date of the Capella Space Company is August 5, 2019."]
[7.2436323165893555, 8.799235343933105, "The Bandwidths of the AATSR Instrument is 20 nm, 300 nm, 1000 nm."]
[8.541337013244629, 9.56932258605957, "The Quantity of the LED-arrays Lighting System is 3."]
[4.761957168579102, 1.8655595779418945, "The Number of Ocean Regions of the RECCAP-2 Satellite Mission is 5."]
[7.941250324249268, 4.56625509262085, "The Spatial Resolution of the DubaiSat-1 Satellite is 2.5 m (Pan), 5 m (MS)."]
[9.404929161071777, 0.5279683470726013, "The Design Lifetime of the EO-1 Satellite is 1.5 years."]
[6.887230396270752, 9.116262435913086, "The Dimensions of the Instrument Optical Bench is 900 mm x 600 mm x 230 mm."]
[9.463949203491211, 7.838521480560303, "The Measurement Range of the Particle Detector Instrument is Proton : 1.5 MeV ~ 250 MeV."]
[4.713397979736328, 5.751558303833008, "The Communication of the Schiaparelli Module is UHF link with the ExoMars Orbiter (with 2 antennas)."]
[4.273011207580566, 4.887829303741455, "The Data Downlink Mechanism of the Experiment Layer Data Management System is Store and playback."]
[7.476966857910156, 4.314585208892822, "The Observation Continuity of the WFIRST Satellite is More-or-less continuously."]
[6.95713472366333, 1.7386537790298462, "The Anniversary Symposium Date of the TRMM Satellite is Nov. 12, 2012."]
[1.254071831703186, 4.251271724700928, "The Redundancy of the Battery Power Storage Device is 1 pack loss allowed."]
[9.106350898742676, 5.815499782562256, "The Attitude Determination of the S/C Satellite is Two STA (Star Tracker Assembly)."]
[4.326733589172363, 5.746090888977051, "The Data Rate Control of the Radio Subsystem Satellite Subsystem is Manual and Automatic."]
[10.863804817199707, 4.165929317474365, "The Mission of the ARIEL Satellite is Study the composition of exoplanets, how they formed and how they evolve."]
[9.545944213867188, 3.724243402481079, "The Volume of the Lunar Flashlight Satellite is 255."]
[6.854793548583984, 4.377526760101318, "The Camera Type of the OPTSAT 3000 Satellite is Unknown."]
[2.30611252784729, 3.7636375427246094, "The Features of the Prometheus Block 2 CubeSats Satellite is 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."]
[8.280555725097656, 8.516152381896973, "The Prime Contractor of the NIRSpec Near-Infrared multi-object Spectrograph is EADS Astrium GmbH."]
[8.564690589904785, 9.231513977050781, "The Ground Pixel Size of the HSRS Sensor is 372 m."]
[6.7342987060546875, 2.4212284088134766, "The Project Team Member of the SHIZUKU Satellite is Matsuaki Kato."]
[4.883571147918701, 1.5968815088272095, "The Profiles Per Day Goal of the FormoSat-7 / COSMIC-2 mission Satellite Mission is 10,000."]
[12.991168975830078, 4.131106853485107, "The Previous Catalogue Object Count (1991) of the Gaia Catalogue of Nearby Stars Stellar Census is 3803 celestial objects."]
[6.667604446411133, 7.620634078979492, "The Minimum Detectable Pulse of the Rangefinder Module Laser Altimeter is 6 photons."]
[7.756699085235596, 10.299470901489258, "The IR Channel Detectors of the SEVIRI Spectral Imager is HgCdTe."]
[1.7807791233062744, 4.11940336227417, "The Cell Efficiency of the Solar Arrays Power Generation is 27%."]
[7.799796104431152, 10.858716011047363, "The Data Quantization of the MI Radiometer Radiometer is 10 bit."]
[1.7324895858764648, 4.408778190612793, "The Function of the PSS Power Supply Subsystem is Stores, distributes and manages electrical power for all electrical equipment."]
[5.823986530303955, 3.639697551727295, "The Coordination Location of the GBOT Project is Heidelberg."]
[11.617056846618652, -1.2844176292419434, "The Mass of the Shakuntala Satellite is Less than 15 kg."]
[9.48306941986084, 8.98623275756836, "The Separation Distance of the Optics Assembly Telescope is 285 mm."]
[5.956789016723633, 2.576042652130127, "The Affiliation of the \u015eiir K\u0131lk\u0131\u015f Associate Professor is Urban Knowledge-Action Committee Network."]
[9.961112976074219, -0.970964789390564, "The Form Factor of the Dove-1 Nanosatellite is 3U CubeSat."]
[10.193817138671875, 3.001880168914795, "The Altitude Range of the LEO Altitudes Satellite Orbit is 150 km to 800 km."]
[8.280343055725098, 10.253290176391602, "The Spatial Resolution of the PMC Imager is 8 m."]
[8.098719596862793, 1.2885018587112427, "The Date of the Maui\u2019s Iconic Waves Image is 16 May 2022."]
[8.620896339416504, 8.894769668579102, "The Ellipse Axis C of the Short Wavelength Band Spectrometer is 242.6 mm."]
[8.407090187072754, 9.224119186401367, "The Spectral Range of the MEGS Spectrograph is 5-105 nm."]
[9.173420906066895, 6.145925045013428, "The Slew Capability of the CMG Control Moment Gyroscope is Up to \u00b130\u00ba."]
[9.893203735351562, 6.7784199714660645, "The Thermal Cycle Test Environment of the Flight Model Satellite Model is -20 to 50 degrees."]
[6.019501686096191, 9.507220268249512, "The Mass of the STAFF/DWP Instrument is 5.6 kg."]
[8.69495677947998, 5.4564385414123535, "The Attitude Calculation of the RAX-1 Satellite is Not yet been calculated."]
[6.540472984313965, 2.8963136672973633, "The Groundstation Pass Sharing of the Carbonite-1 Satellite is With other commercial satellites operated by SSTL."]
[10.482335090637207, -1.0164306163787842, "The Mass of the QSat-EOS Microsatellite is 49 kg."]
[7.418651580810547, 1.1099045276641846, "The Activation Date of the ISERV Pathfinder EO Sensor is March 3, 2013."]
[6.22790002822876, 1.0715795755386353, "The Launch Site of the GHGSat-D Satellite is Satish Dhawan Space Center (SDSC) in India."]
[5.8965559005737305, 3.8049206733703613, "The Flexibility of the Coprocessor Satellite Component is Can be programmed in orbit for different purposes."]
[7.602261543273926, 1.1682628393173218, "The Measurement Record Start Date of the Copernicus Sentinel-6 Michael Freilich Satellite is 1992."]
[9.892226219177246, 1.5537594556808472, "The Days in Space of the Genesis-2 Satellite is More than 150 days."]
[11.655017852783203, 6.158139705657959, "The Launch Date of the XMM-Newton Satellite is April 2, 2015."]
[11.212620735168457, -1.5206254720687866, "The Mass of the Arkyd-3 CubeSat is 4 kg."]
[7.0338215827941895, 9.78964614868164, "The Wavelength Range of the Band No 2 Spectral Band is 0.70 \u00b1 0.2 - 1.10 \u00b1 0.2 \u00b5m."]
[4.769720554351807, 1.7135225534439087, "The Number of Stacer Boom Systems of the THEMIS Constellation Satellite Constellation is 10."]
[7.263731002807617, 8.004592895507812, "The Distance IAR Duration of the Integer Ambiguity Resolution Process is Roughly 15 minutes."]
[13.72286605834961, 1.607465386390686, "The First European Mission to Launch Multiple Small Satellites Date of the Vega Launch Vehicle is 3 September 2020."]
[7.090664863586426, 0.34916776418685913, "The Operation Status of the Ikonos-2 Satellite is Nominal."]
[10.040526390075684, 3.0228121280670166, "The Orbit of the AVUM Spacecraft is Required Disposal Orbit (1450 km x 304 km, i=69.5\u00ba)."]
[10.113402366638184, 3.0336081981658936, "The Orbit Altitude of the WFIRST Satellite is One million miles."]
[8.749899864196777, 3.2163615226745605, "The Orbit of the GOMS-1 Satellite is Geostationary orbit."]
[6.571324825286865, 7.353506565093994, "The Unknown of the BepiColombo Laser Altimeter Instrument is Unknown."]
[3.867764949798584, 5.715822696685791, "The Data Downlink Speed of the Payload Satellite Payload is 4 Gbit/s."]
[11.823221206665039, -1.1690380573272705, "The Launch Mass of the IRNSS-1E Satellite is 1425.4 kg."]
[6.585172653198242, 2.633194923400879, "The Development Location of the SPIDER Telescope is Advanced Technology Center in Silicon Valley."]
[2.3027000427246094, 4.379364967346191, "The Power Transmission of the IOV Payload Satellite Payload is Flexible."]
[8.439887046813965, 7.545753002166748, "The Function of the SES Instrument is Confirm the energy resolution and measurement noise are unaffected by changes in light level and temperature."]
[4.964681625366211, 6.524058818817139, "The Stiffness of the Antenna Communication is > 40 Hz (during launch in longitudinal direction)."]
[3.2937519550323486, 4.900357723236084, "The ROM of the OBDH Data Handling and Processing is 64kB."]
[6.065040111541748, 9.680645942687988, "The Mass of the ST (Star Tracker) Instrument is 1.2 kg."]
[7.269505977630615, 6.710689067840576, "The Next Step Date of the Air Quality Monitoring Activity is March 28, 2014."]
[11.304951667785645, 1.2857226133346558, "The Design Lifetime of the Rover Rover is Around 90 Earth days."]
[6.45875358581543, 2.971831798553467, "The Ground Operations Provider of the CloudSat Satellite is USAF/STP (Space Test Program)."]
[9.550355911254883, 5.737614154815674, "The Attitude Control of the ADCS unit Satellite Component is Magnetic detumbling."]
[1.1606501340866089, 4.24454402923584, "The Type of the Lithium ion battery Power Source is Rechargeable."]
[8.993515968322754, 4.294460296630859, "The Length of the PM Satellite Component is 11.2 m."]
[10.477033615112305, 4.7096967697143555, "The Time to Reduce Pressure from 95% to 80% of the Thruster Propulsion System is Approximately two seconds."]
[6.184838771820068, 3.226781129837036, "The Managing Entity of the MoonLIGHT Satellite is ESA."]
[8.29958438873291, 7.292327404022217, "The Function of the BSA Beam Steering Assembly is Deviating a pulsed high-energy UV laser beam to compensate for the pointing misalignment between the emission and reception paths of ATLID."]
[10.056354522705078, 4.025857925415039, "The Solar Sail Deployment Test Date of the NEA Scout Spacecraft is 28 June 2018."]
[7.177245140075684, 3.433134078979492, "The Development Status of the Pelican Satellite Constellation is Expected to begin launching early next year."]
[6.071559906005859, 9.289741516113281, "The Mass of the SOLSPC Radiometer is 32 kg."]
[4.318701267242432, 4.472553253173828, "The Function of the AIU Subsystem is Monitors the operating state of the electronics subsystem and the operating state of the antenna subsystem."]
[6.554189682006836, 4.140024662017822, "The Instrument Type of the Satellite EO is 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 rada."]
[9.68940544128418, 7.058435440063477, "The Assembly of components of the Metering Truss Structural Component is Brazed assembly of components."]
[6.861701965332031, 2.4915971755981445, "The URL of the OPS-SAT Satellite is http://www.esa.int/ESA_Multimedia/Videos/2019/12/OPS-SAT_the_flying_laboratory."]
[12.021125793457031, 3.266645669937134, "The Orbit Inclination of the EAGLE Secondary Payload is 0\u00ba."]
[5.540721893310547, 6.858944892883301, "The Diameter of the Antenna Instrument is 1 m."]
[7.128499507904053, 5.769205570220947, "The Daily Coverage of the GeoCarb Instrument is CONUS > once per day."]
[7.434722900390625, 3.6566319465637207, "The Orbital Altitude of the SPOT-4 Satellite is Increased slightly."]
[8.876188278198242, 1.970453143119812, "The URL of the BepiColombo Mission is http://www.stp.isas.jaxa.jp/mercury/index-e.html."]
[7.609649658203125, 9.02161979675293, "The Total Channels of the Spectral Bands Spectrometer is 433."]
[8.2360258102417, 0.8828434348106384, "The Launch Delay of the Landsat-9 Satellite is Liquid nitrogen shortage."]
[9.492897987365723, 0.8879123330116272, "The Deorbit Timeline of the NRCSD Payload is Within 18 months."]
[6.173139572143555, 8.11956787109375, "The Bandwidth of the Radiometers Instrument is 10 kHz."]
[7.552953720092773, 2.9453091621398926, "The Pass Over of the RainCube Satellite is North-eastern edge."]
[8.42713451385498, 10.069061279296875, "The Binning of the ICON FUV Instrument CCD is 4 x 4."]
[11.371678352355957, 1.3604687452316284, "The 3rd Lunar Night Time Hibernation Period Start Date of the Yutu Lunar Rover is Feb. 22, 2014."]
[5.187534809112549, 3.7109477519989014, "The Presentation of the IXV Avionics is IXV avionics, from design to mission results."]
[5.644993305206299, 2.3767762184143066, "The Mission Objective of the SpooQy-1 CubeSat is Demonstrate an entangled photon light source."]
[12.150551795959473, 3.276616096496582, "The Inclination of the Resurs-P1 Satellite is 97.3\u00ba."]
[9.872507095336914, -0.5538790225982666, "The Perilune Altitude of the Rstar Data Relay Microsatellite is ~100 km."]
[9.844422340393066, 7.627326011657715, "The Components of the Look-Up Table Model is Radiative transfer simulations by MODTRAN."]
[8.902450561523438, 9.147007942199707, "The FOV of the Instrument Spectrometer is 4 x 150 arcmin."]
[11.097875595092773, 2.478749990463257, "The Type of the Schiaparelli Module is Entry, Descent and Landing Demonstrator."]
[8.938679695129395, 8.480308532714844, "The Cross-Track Orientation of the ISA Sensor is Up to 30\u00ba."]
[6.174062252044678, 1.528499960899353, "The Mission Date of the PAZ Satellite is Sept. 6-11, 2010."]
[7.305322647094727, 7.711923599243164, "The Purpose of the SPEXone Instrument is Improve OCI measurements."]
[11.753016471862793, 4.717289924621582, "The Structure of the Milky Way Galaxy is Warped galactic disc with hundreds of billions of stars."]
[6.039326190948486, -0.02007729560136795, "The Launch Date of the Galileo Satellite Navigation System is Unknown."]
[6.854258060455322, 4.1052117347717285, "The Key Applications of the GHOSt Satellite Constellation is 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,."]
[8.26938533782959, 5.400064945220947, "The Confidence Level of the IRS Sounder Satellite is 68.26%."]
[7.774415969848633, 10.903749465942383, "The Data Quantization of the DubaiSat-1 Satellite is 8 bit."]
[5.189176082611084, 3.740220546722412, "The Equipment Modules of the Terra Satellite is Populated on the zenith face of the spacecraft."]
[4.849017143249512, 1.7559478282928467, "The Number of Satellites of the FormoSat-3/COSMIC-1 Satellite Constellation is 6."]
[1.82439124584198, 4.024980545043945, "The Number of Panels of the Solar Array Power Generation is 3."]
[11.858272552490234, 3.0643975734710693, "The Inclination of the Swarm-B Satellite is 87.75\u00ba."]
[13.076990127563477, 4.059466361999512, "The Orbit Accuracy of the Gaia Satellite is Within 150 m at 1.5 million km."]
[11.487409591674805, 4.1622161865234375, "The Diameter of the 55 Cancri e Exoplanet is Almost twice that of Earth."]
[6.761709690093994, 3.227349042892456, "The Mission Status of the SkySat Constellation Satellite Constellation is Operational (nominal)."]
[5.681768417358398, 2.977339267730713, "The Manufacturer of the FASat-Alfa Satellite is SSTL."]
[7.14420747756958, 9.498467445373535, "The Band 3 of the CIRiS Instrument is 11.77 \u00b5m to 12.6 \u00b5m."]
[8.612947463989258, 10.084813117980957, "The Number of the TDI Stages Imaging System is 8."]
[5.499460220336914, 6.612605094909668, "The Azimuth Dimension of the Active Phased Array Antenna Antenna is 15 m."]
[7.5161004066467285, 0.5164764523506165, "The Launch Date of the JPSS-1/NOAA-20 Satellite is Nov. 18, 2017."]
[4.184832572937012, 3.755753755569458, "The Global Average Detection Rate of the COM DEV NTS Receiver AIS Receiver is 14.8 Messages/s."]
[4.8969011306762695, 2.0234055519104004, "The Quantity of the Secondary Payloads Satellites is 30."]
[10.515342712402344, 7.5026373863220215, "The Structure Material of the TUBSAT-N Satellite is Carbon fiber."]
[7.904953956604004, 7.404873847961426, "The Cadence of the Imaging Instrument Instrument is Fast."]
[4.049548149108887, 5.63923454284668, "The Downlink Data Rate of the NSat Satellite is 9.6 kbit/s."]
[7.283215522766113, 1.0266047716140747, "The Launch Date of the Weather Observation Satellite Satellite is April 17."]
[9.57363510131836, 9.112414360046387, "The Front Face Diameter of the MoonLIGHT Retroreflector Space Device is 100 mm."]
[8.38298511505127, 9.790818214416504, "The Number of Detectors of the Focal Plane Module Satellite Component is ~500 multispectral, 1000 panchromatic."]
[6.218738555908203, 1.5583020448684692, "The Design and Status Presentation Date of the PAZ Ground Segment Ground Segment is June 3-5, 2014."]
[8.435314178466797, 10.114359855651855, "The Object Detection Capability of the Imaging System Imaging System is Objects as small as 2 mm in length."]
[3.597837209701538, 5.4087419509887695, "The Payload Data Memory of the SAR antenna Antenna is 544 GByte."]
[7.718818187713623, 0.4462449848651886, "The Mission Date of the Chandrayaan-1 Satellite is April 25-30, 2010."]
[7.075496196746826, 1.1931289434432983, "The Award Date of the Reef Support Project is 10 December 2020."]
[2.7656726837158203, 5.277423858642578, "The Power Consumption of the UPM-1T card Mass Memory is 3 W on average."]
[5.952730655670166, 9.52236270904541, "The Mass of the SIR-2 Instrument is 2.3 kg."]
[7.617550373077393, 6.780746936798096, "The Next Testing Steps of the TEMPEST-D Radiometer Instrument is TVAC (Thermal Vacuum) testing and antenna radiation pattern testing."]
[7.345609188079834, 5.702026844024658, "The Effect of the Clouds Weather Phenomenon is Can cause scattered clouds resulting in links that are only partly available."]
[4.391273498535156, 6.106019496917725, "The Filter Banks of the Dual-channel Receiver Unit (DRU) Receiver is Same as LGU."]
[4.34348726272583, 6.633793354034424, "The Frequency of the UHF Band is 435 MHz."]
[8.87445068359375, 2.698856830596924, "The Imaging of the DAVINCI and VERITAS missions Missions is Near-infrared imaging."]
[7.12143611907959, 4.380232334136963, "The Instrument Type of the GeoEye-1 Satellite is High resolution optical imagers."]
[7.286499977111816, 0.8247854709625244, "The Launch Date of the MMS Satellite is Spring 2015."]
[10.101053237915039, 4.019374847412109, "The Solar Sail Flyby Velocity of the NEA Scout Spacecraft is Less than 100 feet, or 30 meters, per second."]
[6.635692119598389, 0.7465695738792419, "The Mission Operation Phase of the TET-1 Satellite is One Year."]
[8.092978477478027, 7.370433330535889, "The Function of the LFS (Low Frequency Spectrometer) Scientific Payload is 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."]
[7.401711463928223, 3.6740190982818604, "The Orbital Drift of the SPOT-4 Satellite is Tolerated."]
[5.290398120880127, 2.123901605606079, "The Compatible Launch Vehicles of the CubeStack Multi-Payload Adapter is Athena, Minotaur I, Taurus, Pegasus and Falcon 1."]
[8.908387184143066, 2.9241862297058105, "The Observation Field of the Kepler Spacecraft is Constellation Aquarius."]
[6.819830417633057, 4.160101890563965, "The Application of the HISEA-1 Satellite is Ocean and coastal observations."]
[12.931397438049316, 4.844433307647705, "The Observation Target of the IBEX Satellite is Heliosheath."]
[11.561135292053223, -1.2923917770385742, "The Mass of the UniSat-1 Satellite is 12 kg."]
[9.885518074035645, 3.9846081733703613, "The Article Publication of the NanoSail-D Satellite is October 2008."]
[8.918862342834473, 10.706140518188477, "The Panchromatic GSD of the CCD Pushbroom Camera Camera is 5m."]
[5.102745056152344, 4.455270290374756, "The Operation of the OGS Ground Segment is Ground segment laser communication experiment of SOTA/SOCRATES mission."]
[8.569059371948242, 10.42973804473877, "The CCD Line Pixel Pitch of the FPM (Focal Plane Module) Focal Plane is 6.5 \u00b5m."]
[7.237917423248291, 0.626002311706543, "The Launch Date of the AERO-VISTA mission Satellite Mission is April 7, 2021."]
[10.202593803405762, 3.494905710220337, "The Eccentricity of the Explorer 36 Satellite is 0.03165."]
[4.442243576049805, 2.9841127395629883, "The PRN of the GSAT-0103 Satellite is 19."]
[8.851410865783691, 7.692934989929199, "The Sensor Type of the IDM Ion Drift Meter is Planar sensor."]
[7.256572723388672, 9.309847831726074, "The Angle of Incidence of the TopSAR narrow Imaging Mode is 20\u00b0 - 45\u00b0."]
[7.38016414642334, 0.2852247357368469, "The Shipping Date of the ALD Flight Model Flight Model is 8 May."]
[5.993507385253906, 6.757864475250244, "The Boom Length of the RIME Radar is 16-m."]
[4.442004680633545, 6.226772308349609, "The Frequency Band of the RF Communications Communications is S-band."]
[8.436676979064941, 7.612884998321533, "The Operation Modes of the AIP (Advanced Ionospheric Probe) Probe is RPA and IT."]
[11.236164093017578, 6.560617446899414, "The Purpose of the NICER Payload is Provide both unique insights into neutron star physics and validation of a technology that may one day lead humanity into deep space."]
[9.39256763458252, 6.211093902587891, "The Designers of the Attitude Determination Quaternion Filter Experiment is Students of the Technical University of Delft."]
[8.593225479125977, 1.6985440254211426, "The Switched Off Date of the Spitzer Space Telescope Telescope is 2020."]
[8.224286079406738, 4.85667610168457, "The GSD (Ground Sample Distance) of the ALOS-3/PRISM-2 Satellite is 0.8 m."]
[7.296628475189209, 8.186139106750488, "The Swath width of the TOU Total Ozone Unit is ."]
[2.1780519485473633, 6.55728816986084, "The Latency of the ATL20 Arctic/Antarctic Gridded Sea Ice Freeboard Data is 45 days from receipt of last data in product."]
[7.973940849304199, 9.920441627502441, "The Number of Channels of the IIR Imager is 3."]
[8.835235595703125, 9.440427780151367, "The IFOV (Instantaneous FOV) of the Instrument Sensor is 4 km."]
[6.999040603637695, 0.2001020610332489, "The Launch Plan of the Pixxel Company is Commercial hyperspectral imaging constellation of 24 satellites in 2024 - 2025."]
[5.900694370269775, 10.853620529174805, "The No of Passbands of the Channel 8 Sensor is 1."]
[9.414822578430176, 1.5449901819229126, "The Global Land Color Data Recording Time of the Sentinel-3B Satellite is Less than 1.1 days at the equator, and less than 0.9 days in latitudes higher than 30\u00ba."]
[3.9381561279296875, 2.3769075870513916, "The PCB Size of the CubeSense Attitude Determination and Control Subsystem is PC104-sized."]
[10.377176284790039, 2.756617546081543, "The Perigee of the RBSP spacecraft Satellite is ~ 630 km."]
[5.026298999786377, 7.453853607177734, "The Data Rate of the GeoCarb Instrument is 10 Mbit/s."]
[5.615533351898193, 2.479891538619995, "The User Types of the Iridium NEXT Satellite Constellation is Commercial and government users."]
[4.782312870025635, 1.868450403213501, "The Number of Land Regions of the RECCAP-2 Satellite Mission is 10-14."]
[4.206151485443115, 5.950433254241943, "The Data Rate Adjustment of the Electra Radio is 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."]
[7.625657081604004, 7.700376987457275, "The Purpose of the Prime Instrument Ozone Monitor is Monitor the distribution of ozone."]
[6.718721389770508, 1.2221887111663818, "The Contract Signing Date of the Alphabus Telecommunications Platform is June 2005."]
[8.357034683227539, 8.700008392333984, "The Radiation Mitigation of the Observation Instrument Telescope/Spectrograph is Contiguous High-Z shielding (4\u03c0 sr @detector and electronics)."]
[8.879279136657715, 1.7594821453094482, "The Acoustic Test of the BepiColombo Satellite is 12 June 2017."]
[8.712048530578613, 7.567248344421387, "The Purpose of the Gallium Black Bodies Calibration Source is Track the long-term degradation of the radiometer sensors."]
[9.07369613647461, 4.747486591339111, "The NLC Observation Bottom-Out of the AIM spacecraft Satellite is During solar maximum."]
[4.177301406860352, 2.976440906524658, "The Harmful Interference to Starlink Users of the 5G Network Telecommunication Network is 77% of the time."]
[8.67578125, 0.7082750201225281, "The Launch Date of the JUICE Satellite is 2022."]
[8.486603736877441, 4.020218372344971, "The Avoided Objects of the Observation Restrictions Satellite is Earth and its atmosphere, the Moon, the bright planets, the Milky Way, the galactic band within \u00b1 30\u00b0 from the galactic plane."]
[6.476139545440674, 5.43557071685791, "The Use of the Radar Altimeter Spaceborne Sensor is Monitoring glaciers."]
[6.032773494720459, 9.579989433288574, "The Electronics Package Mass of the FlaPS Instrument Package is 0.5 kg."]
[10.033829689025879, 3.498399496078491, "The Argument of periapsis of the Satellite Spacecraft is 270\u00ba."]
[8.038407325744629, 9.079251289367676, "The Passband of the NUV channel Spectrometer is >159 nm."]
[11.356369018554688, 1.413134217262268, "The Operating Status of the Yutu 2 Lunar Rover is Operating."]
[12.026395797729492, 3.2316040992736816, "The Inclination of the FASat-Alfa Satellite is 82.5\u00ba."]
[9.15911865234375, 5.742417335510254, "The Three-axis accelerometer of the Spacecraft Attitude Determination and Control System is Mounted to the inside face of each solar panel."]
[5.23803186416626, 1.8490238189697266, "The Number of the Columbus ESA ISS Science & System Operations Report is 79."]
[8.667104721069336, 8.113509178161621, "The Number of Detectors of the MHS Instrument is 4."]
[11.215917587280273, 2.6149325370788574, "The Height of the Sand Dunes Landform is Up to 300 m."]
[7.237414836883545, 2.9695560932159424, "The Optimization Problem of the LUMIO Satellite is Nonlinear Programming Problem (NLP) method."]
[11.506478309631348, 5.963013172149658, "The Observation Date of the Giant Meterwave Radio Telescope (GMRT) Radio Telescope is Unknown."]
[7.6963210105896, 7.831869602203369, "The Phase of the UV2VIS SO Instrument is PDR (Preliminary Design Review)."]
[6.0402679443359375, 0.816490888595581, "The Purpose of the RAVAN Satellite is Measure the amount of reflected solar and thermal energy that is emitted into space."]
[5.29813814163208, 4.714540004730225, "The Location of the Svalbard Ground Station is 78\u00ba North."]
[4.144421577453613, 6.399496555328369, "The Operation Mode of the S-band transponder Communication Device is Full duplex."]
[0.9962875843048096, 4.195713520050049, "The Capacity of the NiCd Battery Energy Storage is 55Ah."]
[5.097268104553223, 6.009179592132568, "The Rx Channels of the Reduced Solution Antenna Configuration is 2."]
[2.6347827911376953, -1.4519587755203247, "The Brigthness Temperature (BT) of the Antenna Reflector is 100~330 K."]
[5.2545928955078125, 2.257349729537964, "The Number of Investigations of the SMART-1 Satellite is 10."]
[4.199239730834961, 6.40048885345459, "The Configuration of the Spare Lithium-1 Radio Radio is Reconfigured to monitor the crosslink activity."]
[12.105246543884277, 3.309263229370117, "The Orbit Inclination of the Colorado Student Space Weather Experiment (CSSWE) Satellite is Highly Inclined."]
[9.307401657104492, 7.794317722320557, "The Cooling Temperature of the Focal Plane Instrument Component is 150 K."]
[11.706709861755371, 2.598573684692383, "The Secondary Diameter of the Didymos Binary System is 160 m."]
[7.6615824699401855, 0.6138473153114319, "The Measurement Date of the GRACE-FO Satellite is 22 June 2020."]
[9.213648796081543, 7.788163661956787, "The Operating Temperature of the MIRI Instrument is 7K."]
[3.6492371559143066, 6.2536115646362305, "The Data Transmission Rate of the ITU Image Transmission Unit is 160 Mbit/s."]
[1.0571410655975342, 4.294411659240723, "The Power Storage of the CS-XUEPS2-41 Electrical Power Subsystem is Rechargeable 30 W hr lithium polymer batteries."]
[7.5149431228637695, 1.9359978437423706, "The Event Nickname of the IceCube Detector Particle Detector is Hydrangea."]
[1.2124390602111816, 4.169364929199219, "The Battery Type of the Spacecraft Satellite is Li-ion 12 Ah."]
[3.864241600036621, 2.30818247795105, "The CubeSat Size of the LEDSAT Satellite is 1U."]
[8.941822052001953, 5.207066535949707, "The Attitude Control Stability of the Spacecraft Satellite is 1 arcmin rms (or FWHM of ~2.2 arcmin)."]
[10.135252952575684, 6.80017614364624, "The Heat Rejection Method of the CASSIOPE spacecraft Satellite is From strategically placed radiator surfaces along the bus hex sidewalls."]
[7.779231071472168, 10.298443794250488, "The NIR Channel Detectors of the SEVIRI Spectral Imager is InGaAs photovoltaic diodes."]
[10.178410530090332, 3.508164644241333, "The Orbit Eccentricity of the UniCubeSat Satellite is About 0.07."]
[6.877627372741699, 2.6970930099487305, "The Coverage Area of the Kleos Scouting Mission (KSM1) Satellite is South China Sea and Strait of Hormuz."]
[6.89357852935791, -0.03210068494081497, "The First Flight Date of the MEPSI Satellite is February of 2000."]
[5.238490581512451, 1.684507131576538, "The Number of CubeSats Released of the NRCSD CubeSat Deployer is 33."]
[7.001159191131592, 0.7399969100952148, "The Launch Date of the TIMED Satellite is December 2010."]
[9.503155708312988, 0.4630667567253113, "The Design Life of the GRACE Satellite is 8 years."]
[9.673089027404785, 2.292846441268921, "The Orbit Formation of the CloudSat Satellite is Tight formation with CALIPSO."]
[12.63070297241211, 6.917786598205566, "The Pulse period (ms) of the B1617-155 (Sco X-1) Pulsar is 3.200."]
[8.224773406982422, 4.41942834854126, "The Pan Resolution at Nadir of the QuickBird-2 Satellite is 0.61 cm."]
[8.814783096313477, 1.4192326068878174, "The Fuel Consumption of the Van Allen Probes Satellite is Unknown."]
[6.9880547523498535, 4.4962382316589355, "The Measurement Domain of the GOSAT Satellite is Atmosphere, Land."]
[9.7527494430542, 8.983766555786133, "The Secondary Mirror Diameter of the Optics Assembly Telescope is 56 mm."]
[9.351577758789062, 6.113524436950684, "The Delivery Frequency of the SpinKF Attitude Determination System is Daily."]
[7.369219779968262, 8.624345779418945, "The Spatial resolution at nadir of the IRAS Infrared Atmospheric Sounder is 17 km."]
[6.639654636383057, 6.713545799255371, "The Design of the DDMI Instrument is Based on the SGR-ReSI design."]
[6.931809902191162, 6.799147129058838, "The Instrument of the CYGNSS observatory Observatory is DDMI (Digital Doppler Mapping Instrument)."]
[7.759799480438232, 6.089565277099609, "The Information of the Unresolved Imagery Data is Contains spectral and photometric information."]
[7.652164936065674, 1.6420490741729736, "The Launch Date of the SMAP Satellite is 2015."]
[11.606691360473633, -1.2184464931488037, "The Mass of the HY-2A Satellite is ~ 1500 kg."]
[1.7854557037353516, 4.853564262390137, "The Mass of the EPS Electrical Power Subsystem is 0.28 kg."]
[11.383142471313477, 3.79866886138916, "The Re-adjustment Time of the Earth Planet is Several thousand years."]
[7.0757269859313965, 7.520915508270264, "The Systematic Error of the MIRAS Radiometer is Several Kelvin."]
[3.191913366317749, 5.328965187072754, "The Redundancy Principle of the SSR Solid State Recorder is Division of the total storage space into several banks of memory."]
[6.383780479431152, 2.9584543704986572, "The Platform Type of the Carbonite Smallsat Satellite is High performance generic."]
[8.104500770568848, -0.7678883075714111, "The Training Location of the Crew Dragon Spacecraft is NASA\u2019s Neutral Buoyancy Laboratory near the Johnson Space Center in Houston."]
[5.698431491851807, 3.1700427532196045, "The Development Funding of the iMESA Technology is AFOSR and AFRL."]
[9.512777328491211, 0.5603513121604919, "The Lifetime of the OFEQ-1 Satellite is 6 months."]
[2.405287981033325, 3.761159658432007, "The Features of the Prometheus Satellite Satellite is Four deployable solar arrays and a deployable helix antenna."]
[4.707590103149414, 7.228115558624268, "The Data Rate of the GimmeRF Radio Instrument is Up to about 24 Tbit per orbit."]
[3.694957733154297, 5.334344863891602, "The Data Throughput of the AIS Data Collection System Data Collection System is 16 MB per day."]
[5.924379348754883, 3.3449130058288574, "The Payloads of the NSSL Phase 2 Launch Program is Large military and intelligence agency satellites."]
[5.252490997314453, 6.4713921546936035, "The Antenna Type of the PR Phased Array System is 2 m slotted waveguide (WG) antenna."]
[6.029448509216309, 2.9593112468719482, "The Manufacturer of the OSIRIS-REx Spacecraft is Lockheed Martin Space."]
[10.722503662109375, 10.27336311340332, "The Offset temperature coefficient of the PHA Detector is <0.1 channel/\u00baC."]
[11.727665901184082, -1.1423503160476685, "The Mass of the Jason-3 Satellite is 550 kg."]
[7.554007053375244, 2.115478277206421, "The Report Recommendation of the SMAP Satellite is Highest priority among all proposed missions."]
[5.950179100036621, 1.66325843334198, "The Owner of the PAZ Satellite is Ministry of Defence."]
[3.0821166038513184, 5.883718967437744, "The Operational Availability Improvement of the MTP Transponder is True."]
[8.494309425354004, 2.9950499534606934, "The Flight Path of the BioSentinel Satellite is Past the moon and then subsequently into an Earth trailing, Heliocentric orbit."]
[8.77447509765625, 10.684314727783203, "The Raw Video Data Bandwidth of the Camera Imaging Device is 12.5 Gbit/s."]
[12.151243209838867, 3.301497220993042, "The Orbit Inclination of the AFSPC-11 Satellite Mission is 0\u00ba."]
[8.17233657836914, 8.93570613861084, "The Spectral Sensitivity of the WUPPE Spectrophotometer is 1400 to 3200 \u00c5."]
[4.407277584075928, 6.305551528930664, "The Frequency of the S-band Communication Band is 1.67-1.71 GHz."]
[7.497722625732422, 4.173121452331543, "The PAN-F of the CartoSat-1 Satellite is Panchromatic Forward-pointing Camera."]
[9.958054542541504, -0.6863744258880615, "The Ground Resolution of the NIUSAT Nanosatellite is 25 m."]
[8.4229154586792, 11.069025039672852, "The Number of Occluded Rows per Filter Band of the QWIP Array Sensor Array is 76."]
[3.478778600692749, 5.338787078857422, "The Payload Data Storage Capacity of the BRITE spacecraft Satellite is up to 256 MB."]
[10.547369956970215, 7.550887584686279, "The Material of the Satellite structure Structure is Aluminum frame."]
[9.525182723999023, 0.5065431594848633, "The Design Lifetime of the Spacecraft Satellite is 5 years."]
[4.996505260467529, 1.5206236839294434, "The Demonstration Satellites of the Falcon 9 rocket Rocket is Two."]
[5.54742431640625, 2.7934210300445557, "The Manufacturer of the CubeSats Satellite is Technische Universit\u00e4t Berlin."]
[6.450124740600586, 3.079925537109375, "The Sponsor of the Diwata-1 Satellite is Philippine government."]
[4.96920919418335, 1.5497092008590698, "The Observation Area of the FORMOSAT-7/COSMIC-2 Satellite Constellation is Global meteorology, climate and ionosphere."]
[11.17198371887207, -1.483924150466919, "The Mass of the ESTCube-1 & -2 CubeSat is 1.050 kg."]
[7.745484352111816, 0.6450850963592529, "The Spacewalk Installation Date of the UrtheCast Satellite is Jan. 2014."]
[7.341540336608887, 10.113764762878418, "The Data Processing of the HyperScout Hyperspectral Imager is Onboard image processing and data compression."]
[3.335273504257202, 5.194305896759033, "The Lossy Compression Ratio of the HSDR FPGA Hardware is 4:1 or higher."]
[7.9149627685546875, 7.7829155921936035, "The False Event Rate of the Instrument Sensor is <5%."]
[6.890369892120361, 3.1971867084503174, "The Mission Status of the CASSIOPE Satellite is Operational (extended)."]
[8.7528715133667, 7.298856735229492, "The Manufacturer of the PIMS Plasma Instrument is Johns Hopkins Applied Physics Laboratory (APL)."]
[9.271261215209961, -0.625308632850647, "The Predecessor of the ROBUSTA-1B Nanosatellite is ROBUSTA satellite, which was launched in February 2012."]
[7.178216934204102, -0.34963276982307434, "The Launch Rate Goal of the Starlink Satellite Constellation is Roughly two Starlink launches a month."]
[6.511358261108398, 0.7764340043067932, "The Ground System of the TET-1 Satellite is Unknown."]
[6.979006767272949, 0.6188340783119202, "The Launch Date of the ICEYE X1 Satellite is 17 Jan. 2018."]
[1.9221924543380737, 4.046157360076904, "The Panel Size of the Solar Panels Power Subsystem is 432 mm x 243 mm."]
[8.780454635620117, 7.029860496520996, "The Configuration of the NGAVGS Sensor is Two box."]
[9.388144493103027, 0.9761611223220825, "The Mission Duration of the LCROSS Satellite is 26 months."]
[9.700135231018066, 1.2499521970748901, "The Commissioning Time of the AprizeSat-3 and AprizeSat-4 Satellites is 1 hour after separation."]
[7.361234664916992, 6.33167028427124, "The Performance of the GEOSAT Follow-On Water Vapor Radiometer Radiometer is Not Specified."]
[10.612932205200195, 9.267930030822754, "The Image Color Diversity of the CaSSIS Imaging System is Present."]
[11.748092651367188, -1.1239863634109497, "The Servicer Mass of the ELSA-d Satellite Mission is ~180 kg."]
[5.357580184936523, 5.0660905838012695, "The Conference Presentation of the Laser Communications Relay Demonstration Project Communication System is URL: http://www.spaceops2012.org/proceedings/documents/id1261897-paper-001.pdf."]
[7.865047931671143, 8.192269325256348, "The Design of the Atmospheric-sounding instrument Spectrometer is Dispersive spectrometer, using a reflexive grating for spectral bands dispersion."]
[6.580687999725342, 7.805084705352783, "The Peak Fluency of the InnoSlab laser Laser is Smaller than 2.5 J/cm2."]
[10.228551864624023, 2.9637582302093506, "The Altitude of the Orbit Satellite is 720 km."]
[10.72413158416748, 10.28441047668457, "The Number of dual-gain PHAs of the PHA Detector is 16."]
[7.674345970153809, 0.20257677137851715, "The Launch Date of the Soyuz-2.1b rocket Rocket is 6 February 2020."]
[9.382607460021973, 4.871884822845459, "The Slew Rate of the  Spacecraft Bus (Avionics Module=AM) Satellite is 0.25 to 1.0\u00ba/s."]
[10.10268497467041, 4.158829689025879, "The Maneuvering System of the NEA Scout Solar Sail Technology Demonstration Spacecraft is Small cold-gas thrusters."]
[11.244041442871094, 1.0079317092895508, "The Launch Date of the Tianwen-1 Mars Mission is July."]
[5.541167736053467, 3.920032024383545, "The Ground Station Location of the CFESat Satellite is LANL."]
[7.503172874450684, 7.494297504425049, "The Detection Capability of the OMI Satellite Instrument is Sulfur Dioxide."]
[4.315487384796143, 6.601320266723633, "The Linearity/Noise Level or Bias/NF of the Receiver Device is Use of noise sources."]
[6.681387424468994, 6.176042079925537, "The Grid Size of the ASCAT coastal winds Data Product is 12.5 km."]
[11.801873207092285, -0.9249471426010132, "The Mass of the Teplo Payload is 10 kg."]
[9.07454776763916, 7.210918426513672, "The Components of the PLS Plasma Instrument is Four Faraday cups."]
[10.383018493652344, 3.2614588737487793, "The Trigger Altitude of the Parachute System is About 5 km."]
[7.181985378265381, 0.41929787397384644, "The Launch Date of the Queqiao Relay Satellite is May 21, 2018."]
[9.971704483032227, 9.556597709655762, "The Science Objectives of the SAGE-III Instrument is Retrieve global profiles of atmospheric aerosols, ozone, water vapor, NO2, NO3, OClO, temperature and pressure."]
[7.526050090789795, 5.53143835067749, "The Slope Error of the Aeolus Satellite is 0.7%."]
[7.2151994705200195, 0.5953201055526733, "The Launch Date of the BIROS Satellite is 2016."]
[8.72677230834961, 6.515340328216553, "The Formation of the Ionosphere Atmospheric Layer is Photodissociation of thermospheric air by solar extreme ultraviolet radiation."]
[8.20888900756836, 1.172598123550415, "The Data Availability of the EPIC Earth Polychromatic Imaging Camera is June 2015 through the current day."]
[6.325687408447266, 1.14730703830719, "The Launch Date of the Eutelsat Quantum Satellite is 26 July 2021."]
[7.5088019371032715, -0.03212971240282059, "The Number of Computers of the SAOCOM-1A Satellite is 6."]
[7.101413249969482, 6.859654903411865, "The Launch Date of the Trasser AOS Instrument is July 5, 1988."]
[9.551400184631348, 6.595200538635254, "The Cycle Life Test of the SMA Hinge Spring Component is 130 cycles."]
[2.273730754852295, 3.849825620651245, "The Additional Solar Panel of the MicroMAS-1 Satellite is Another 2U solar panel will be body-mounted on the zenith side of the satellite bus."]
[10.093948364257812, 5.0902838706970215, "The Functions of the Electric Propulsion Test Subsystem Monitoring Unit is 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."]
[9.371374130249023, 10.3096284866333, "The Optical Axis of the Metric Camera Camera is Vertically down to the Earth's surface."]
[7.580782890319824, 2.694220781326294, "The Conference Date of the KOMPSAT-3A Satellite is May 16-20, 2016."]
[6.3404011726379395, 1.018201231956482, "The Launch Date of the COSMO-SkyMed Di Seconda Generazione Satellite is 18 December 2019."]
[7.632842540740967, 6.563933849334717, "The Micro Vibration Correction of the Instrument Satellite Instrument is Confirmed."]
[5.723183631896973, 7.074625015258789, "The Power of the RA-1 Radar Altimeter is 130 W."]
[11.644442558288574, -1.226133942604065, "The Dry Mass of the QZS-1 Satellite is 1800 kg."]
[11.574216842651367, 4.199149131774902, "The Shape of the Ceres Dwarf Planet is Almost spherical."]
[6.967977523803711, 6.088210582733154, "The Temporal Sampling of the Sea Surface Salinity (SSS) Measurement is Monthly."]
[4.83870267868042, 0.9225606918334961, "The Budget Allocation of the Copernicus Environmental Monitoring Satellites is 4.81 billion euros."]
[6.813014507293701, 6.959502220153809, "The Test Results of the ALTIKA Instrument is Unknown."]
[7.113745212554932, 1.4826263189315796, "The Date of the IGARSS Symposium is July 26-31, 2015."]
[8.317158699035645, 3.216096878051758, "The Baseline Determination of the TanDEM-X Satellite is Two years."]
[10.956875801086426, 7.161246299743652, "The Number of Instruments of the JEM-X X-Ray Monitor is 2."]
[7.467108726501465, 1.9655386209487915, "The Event of the Paris Glacier Memorial Glacier is Agreement of a legally binding treaty in 2015."]
[9.099064826965332, 3.289994955062866, "The Purpose of the HEO Highly Elliptical Orbits is Communications services and other uses at high northern latitudes."]
[6.916031837463379, 0.9346755146980286, "The Full Year in Orbit of the COMS Satellite is Late summer of 2011."]
[4.251174449920654, 6.444868087768555, "The Downlink Frequency of the SafetyNetTM Data Collection Architecture is Ka-band (26.7 GHz)."]
[9.312302589416504, 7.394234657287598, "The Range of the Temperature Sensor is -50 to +600\u00baC."]
[4.656970500946045, 5.719834327697754, "The Communication Signal of the FLP Satellite is S-band RF."]
[4.439260959625244, 2.993741035461426, "The PRN of the GSAT-0206 Satellite is 30."]
[7.566935062408447, 3.7444357872009277, "The Image Color Representation of the Shikisai Satellite is Coolest waters in blue, warmest temperatures in red."]
[7.317168235778809, 10.137466430664062, "The Image Calibration of the HyperScout Imaging System is Not yet calibrated."]
[8.354323387145996, 8.740262985229492, "The Lens Surfaces Coatings of the Instrument Spectrometer is Narrow-band AR coatings with R<0.2%."]
[7.858458995819092, 0.8064123392105103, "The Arrival Date of the European Service Module Spacecraft Module is November 7, 2018."]
[6.652028560638428, 3.5504045486450195, "The Mission Type of the Badr-B Satellite is EO."]
[10.357823371887207, 3.4811198711395264, "The Argument of Pericenter of the SMART-1 Satellite is 292.930\u00ba."]
[6.685030937194824, 8.941869735717773, "The Width of the Instrument Instrument is 413 mm."]
[11.353370666503906, 6.510614395141602, "The Imaging of the XRT X-Ray Telescope is Captured the black moon in the shape of a crescent in front of the solar corona brightened by X-rays."]
[3.588900327682495, 5.6697235107421875, "The Data Input Data Rate of the Data Handling System System is 336 Mbit/s."]
[7.968321323394775, 6.712723255157471, "The Basis of the MLFMM (Multilevel Fast Multipole Method) Algorithm is Method of Moments."]
[5.043132305145264, -0.14475615322589874, "The Launch Date of the OneWeb Satellite is 2022."]
[8.429848670959473, -0.03739042580127716, "The Upper Stage Deployment Time of the Rocket Launch Vehicle is More than a half-hour."]
[8.951188087463379, 1.496234655380249, "The Launch Date of the Ulysses Spacecraft is 1990."]
[7.920709609985352, 6.11309814453125, "The Volume of the CROP Filter Water Filtration System is 600 mL."]
[5.579768180847168, 2.8118367195129395, "The Developer of the KickSat-2 CubeSat is Stanford University and NASA/Ames."]
[8.291291236877441, 7.669175624847412, "The Functionality of the Active Calibration Source Calibration Equipment is Equivalent to a very large known reflector on the surface."]
[9.486591339111328, 10.529568672180176, "The Video Imaging Duration of the Iris Video Camera Camera is Up to 60 seconds."]
[8.095776557922363, 9.439048767089844, "The Ground Resolution of the PAN Detector is 1m."]
[6.037410736083984, 4.674984931945801, "The Transmission Security of the Satellite Satellite is Used polarization as a means of transmission security."]
[7.95533561706543, 7.8865203857421875, "The Accuracy of Moisture Profiles of the CrIMSS Instrument Suite is 15%."]
[7.221734046936035, 1.4292750358581543, "The Launch Year of the ERS-1 Satellite is 1991."]
[9.943109512329102, 1.6139202117919922, "The Orbital Period of the NigeriaSat-2 Satellite is About 99.5 min."]
[11.129169464111328, 7.000836372375488, "The URL of the An Efficient Photoelectric X-ray Polarimeter Device is https://doi.org/10.1038/35079508."]
[9.348554611206055, 10.259428977966309, "The Sun Elevation for Operations of the Metric Camera Camera is Never exceeded 30\u00ba."]
[6.73264217376709, 8.196772575378418, "The Manufacturer of the MWI Instrument Instrument is CGS (Carlo Gavazzi Space) S.p.A."]
[9.862439155578613, 8.026251792907715, "The Detection Area of the HXD Detector is 16cm2."]
[8.863382339477539, 7.2699666023254395, "The Short Circuit Current of the CSS Coarse Sun Sensor is 34 mA."]
[6.140143394470215, 4.102593898773193, "The Operational Protocols of the ISERV Satellite is Image data acquisition, storage, and downlink."]
[3.2709176540374756, 4.841047286987305, "The Memory of the Controller card C&DH Subsystem Component is Several MB of RAM and EEPROM."]
[9.332887649536133, 5.153750419616699, "The Attitude Control of the UniSat-1 Satellite is Spin-stabilized at 5 rpm with the spin-axis normal to the orbital plane."]
[7.523721694946289, 4.828375339508057, "The Justification of the ACE Satellite is New science that can be accomplished with three solar wind satellites near L1."]
[2.288245439529419, 4.426610469818115, "The Average Power of the JAWSAT Satellite is 80 W."]
[8.356782913208008, 3.5890109539031982, "The Program Overview of the GCOM-Al Satellite is Not provided."]
[4.176455497741699, 4.598611831665039, "The Data Input Interface of the Modem Processor Signal-Processing Chain is SpaceWire over LVDS (Low Voltage Differential Signaling) link with minimal NRE (Non-Recurring Engineering)."]
[5.792553901672363, 2.9784646034240723, "The Manufacturer of the GFO Satellite is BATC (Ball Aerospace &."]
[9.429909706115723, 9.088231086730957, "The Focal Length of the Telescope Optical Instrument is 320 mm."]
[8.065679550170898, 5.767849445343018, "The Thermomagnetic Perturbations of the ASM Satellite Component is 20-30 pT +/- 5 pT peak-to-peak range."]
[9.594133377075195, 5.919816493988037, "The Pointing Range of the ADCS Attitude Determination and Control Subsystem is \u00b132\u00ba."]
[5.84629487991333, 8.124798774719238, "The Frequency (GHz) of the ICI-10 Radiometer is 448\u00b11.4."]
[7.073358535766602, 8.951034545898438, "The | 80 m of the MSS Instrument Spatial Resolution is Spatial resolution 80 m."]
[7.540490627288818, 0.6067925691604614, "The Insertion Date of the P2 Spacecraft is October 22, 2010."]
[7.77232027053833, 9.238300323486328, "The Spectral Sampling Interval of the LR Spectrometer Spectrometer is 0.6 nm/pixel."]
[9.064798355102539, 8.028546333312988, "The Plastic Scintillator of the Range Calorimeter Particle Detector is 16 planes."]
[8.689376831054688, 9.715413093566895, "The Focal Plane Format of the EXI instrument Imaging Instrument is 12.6 MP 4:3 format."]
[7.6479058265686035, 4.022101879119873, "The Main Role of the CryoSat Satellite is Provide detailed measurements of the height of the world\u2019s ice."]
[8.160629272460938, -0.2396969497203827, "The Time Between Launches of the Falcon 9 Rocket is a little more than 72 hours."]
[5.481503486633301, 2.4661457538604736, "The Project of the Firefly Satellite Satellite is NSF CubeSat Project."]
[12.15576171875, 5.353747844696045, "The Stars in Galaxies Percentage of the Universe Cosmology is 7 percent."]
[7.542286396026611, 5.9672722816467285, "The Mission Goal of the EMIT Satellite is Map where the dust originates and estimate its composition."]
[7.270380973815918, 7.0364556312561035, "The TEB Detector Nonlinearity of the VIIRS Instrument is Excellent."]
[8.845573425292969, 2.6771485805511475, "The Responsible Orbit of the DWSS Satellite is Early Morning."]
[5.827162265777588, 1.6666202545166016, "The Radiation Qualification of the GomX-4 Satellite is 20 krad TID (Total Ionizing Dose)."]
[8.002152442932129, 9.918946266174316, "The Channel Wavelengths of the IIR Imager is 8.65 \u00b5m, 10.6 \u00b5m, 12.05 \u00b5m."]
[5.830404758453369, 8.142802238464355, "The Bandwidth (GHz) of the ICI-8 Radiometer is 6."]
[6.140458106994629, 9.789876937866211, "The Mass of the OTU Optical Telescope Unit is 45 kg."]
[8.168964385986328, 5.615144729614258, "The Electron Density of the RAX-1 Satellite is Very quiet."]
[7.789572715759277, 9.010987281799316, "The Channels of the Spectrometer Instrument is 385, 454, 600, 1020, 940, 448, 525 nm."]
[8.625250816345215, 1.7582809925079346, "The Science Operations Location of the Spitzer Space Telescope Telescope is Spitzer Science Center at IPAC at Caltech."]
[7.858150959014893, 3.1807615756988525, "The Quantity of the Fragments Debris is In excess of 115 k."]
[9.695906639099121, 1.5896265506744385, "The Exact Repeat Cycle of the Satellite Orbit is 8 days."]
[6.739614486694336, 8.226390838623047, "The Maximum Sustained Event Rate of the ISS-LIS Instrument is 300 events/s."]
[9.94156551361084, 9.529711723327637, "The Science Objectives of the SAGE-III Instrument is Provide atmospheric data essential for the calibration and interpretation/correction of other satellite sensors."]
[5.206849575042725, -0.09024329483509064, "The Alignment Milestone Date of the Webb Satellite is 16 March 2022."]
[3.708592414855957, 6.077233791351318, "The Data Delivery of the Command and Telemetry Interface Interface is 3-byte commands and 64-byte ancillary data."]
[7.954421043395996, 8.869722366333008, "The Wavelength Sensitivity of the Polarimeter Instrument is 1170 - 1800 \u00c5 in second order and up to 3600 \u00c5 in first order."]
[5.641664981842041, 3.7564120292663574, "The Location of the Science Operations Center (SOC) Data Center is LASP."]
[6.925139427185059, 4.288820743560791, "The Objective 1 of the EPS (EUMETSAT Polar System) Satellite System is Ensure continuity and availability for operational purposes of polar meteorological observations from the \"morning\" orbit to the global user community."]
[1.1179440021514893, 4.433273792266846, "The Nominal Voltage of the NiH2 Batteries Power Subsystem is 12.5 V."]
[9.654797554016113, 1.6441270112991333, "The Repeat Cycle of the Satellite Imaging Satellite is 12 days."]
[6.98028564453125, 1.398435354232788, "The Proposal Year of the Geospace Dynamics Constellation Mission is 2013."]
[3.529506206512451, 4.08012580871582, "The Power to sub-experiments of the STRV-1d DHS Data Handling System is +5 V, \u00b112 V."]
[6.6731486320495605, 3.1976659297943115, "The Principal Investigator of the NICER Payload is Keith Gendreau."]
[10.001395225524902, 1.454325795173645, "The Search Duration of the YES Satellite is About 96 hours."]
[8.643756866455078, 9.1385498046875, "The Slit Width of the Spectrometer Spectrometer is 25 \u00b5m."]
[11.395694732666016, 4.255756378173828, "The Atmosphere of the 55 Cancri e Exoplanet is Possibly made of oxygen or nitrogen, or a very thin atmosphere of mineral vapor, such as silicon oxide."]
[10.588418006896973, 3.331413745880127, "The Drift Distance of the ASTRO Satellite is More than 6 km."]
[6.138289451599121, 6.202399253845215, "The Function of the S-193 Radar System is Combination of passive microwave radiometer with an active scatterometer, and radar altimeter."]
[8.037086486816406, 5.873281002044678, "The Accuracy Specification of the ASM Satellite Component is 300 pT (2\u03c3)."]
[6.2059245109558105, 4.953860759735107, "The Levels of the Data products Data is 0 and 1."]
[8.098909378051758, 5.289244651794434, "The Orbit Accuracy of the DORIS-DIODE Satellite System is Ten Centimeters."]
[9.91047191619873, 4.034531116485596, "The Deployment of the NanoSail-D2 Satellite is Shortly after deployment of the NanoSail-D2, the solar sail will deploy."]
[10.402283668518066, 7.6562724113464355, "The Seal Material of the Sample Container Container is Aluminum metal."]
[6.2035231590271, 0.6090822219848633, "The Release Date of the BEESAT-4 CubeSat is Sept. 9, 2016."]
[8.149359703063965, 10.307533264160156, "The Spectral Band of the Camera Imaging Device is 762 nm."]
[7.022347927093506, 7.448516368865967, "The Design Concept Overview of the ASTER Instrument is Not Provided."]
[7.920281887054443, 6.983189105987549, "The Calibration Scheme of the In-flight Radiometric Calibration Calibration is Two points calibration."]
[7.890531539916992, 1.3442935943603516, "The Article Date of the Small Water Ice Reservoirs Lunar Surface Feature is 26 October 2020."]
[5.768533229827881, 6.934916019439697, "The Peak Power of the Radar Radar is 200 W/150 W."]
[6.890652179718018, 1.2778711318969727, "The Presentation Date of the Taiwan Weather Monitoring Satellites Satellite Constellation is March 1-8, 2008."]
[5.0731282234191895, 2.951838970184326, "The Mission Goals of the ALBus 3U CubeSat Satellite is Technology demonstration, Power distribution, Battery charging, Shape Memory Alloys deployment."]
[3.5881507396698, 6.496829509735107, "The Data Rate of the UHF Transceiver Transceiver is 4Kbps."]
[3.551863193511963, 4.097805500030518, "The CPU of the STRV-2 DHS Data Handling System is 8086 rad-hard."]
[5.329858303070068, 2.5654616355895996, "The Name of the CubeSat Satellite is Unknown."]
[9.183588027954102, 4.267421722412109, "The Outer Diameter of the PM Satellite Component is 4.4 m."]
[9.016134262084961, 10.632452964782715, "The Issue of the Medium-Resolution Camera Camera is Telemetry issues."]
[7.281679630279541, 6.823435306549072, "The Installation Date of the ACLS Air and Oxygen System is 2 November 2018."]
[4.501065731048584, 4.030492305755615, "The Components of the Spacecraft Plug-n-Play Avionics (SPA) Standards is Data transport, power delivery, time synchronization, single point ground connection, minimal \"hooks\" for self-description."]
[10.03687858581543, 1.3926501274108887, "The ECT (Equatorial Crossing Time) of the WV-1 Satellite is 1330 hours."]
[5.90845251083374, 3.5966389179229736, "The Developers of the MR-FOD Deployer is Morehead University, Morehead, KY, USA and GAUSS."]
[10.834857940673828, 4.139242649078369, "The Purpose of the CHEOPS Satellite is Search for transits of exoplanets by means of ultrahigh precision photometry on bright stars already known to host planets."]
[8.465662002563477, 7.301455020904541, "The Measurement Locations of the IMPACT Instrument is Two STEREO spacecraft locations."]
[8.828368186950684, 9.789497375488281, "The Unknown of the Automatic Registration Method Image Processing Method is Unknown."]
[3.6277387142181396, 6.129673480987549, "The Speed of the Internet Connection Communication is At least 25 Mbit/s."]
[3.640683650970459, 3.531484365463257, "The URL of the CICERO Satellite System is http://www.prweb.com/releases/2009/12/prweb3295414.htm."]
[8.009797096252441, 3.2422215938568115, "The Operator of the TanDEM-X Satellite is German Space Operations Center (GSOC)."]
[8.596696853637695, 7.951563835144043, "The p-FETs Quantity of the RADMON Radiation Monitor is 4."]
[5.14092493057251, 4.602493762969971, "The Location of the Ground Segment Ground Control Infrastructure is University of Ljubljana and Pomjan."]
[5.076466083526611, 7.142070770263672, "The Pixel Size (km x km) of the Antenna Reflector is 6."]
[9.366410255432129, -0.488925576210022, "The Observation Period of the BRITE Nanosatellite Network is Six-month."]
[10.835563659667969, 4.171083450317383, "The Capability of the CHEOPS Satellite is Determine accurate radii for exoplanets."]
[10.744522094726562, 7.350785732269287, "The Energy Range of the SXD and solar X-ray monitor Detector is 1-10 keV."]
[10.040342330932617, 9.948297500610352, "The Image Capture of the Iris Camera Camera is Barcelona, Spain."]
[10.09704875946045, 2.8571462631225586, "The Orbit Altitude of the ERBS Satellite is 610 km."]
[6.075179100036621, 3.6360080242156982, "The Transfer of the EMEA FleetBroadband Satellite Communication is To Alphasat."]
[6.5808515548706055, 0.9277735948562622, "The Development Contract Date of the Alphasat Satellite is November 2007."]
[7.986984729766846, 8.954927444458008, "The Wavelength Range of the Lens Optical Instrument is 600 - 1000 nm."]
[6.031312465667725, 0.6952956914901733, "The Launch Date of the ABEX CubeSat is Planned for 2024."]
[4.775344371795654, 3.7749288082122803, "The Challenges of the Maritime AI-NAV Program is Significant increases in transport volumes, more stringent environmental requirements and a shortage of seafarers in the future."]
[7.767465114593506, 9.189379692077637, "The Spectral Range of the HR Spectrometer Spectrometer is 677\u2013697nm."]
[7.917759418487549, 7.227141380310059, "The Function of the Instrument Calibration System is Monitor instrument response and enable high data quality and reliability."]
[5.345750331878662, 4.287676811218262, "The AIV System Reuse of the PROBA Project Satellite Project is Ground segment software is used both as the AIV system and as the operations system."]
[7.248437881469727, 7.818379878997803, "The East-West Scan Swath Time of the Instrument Satellite Instrument is Less than 10 seconds."]
[10.257883071899414, 4.984462261199951, "The Configuration of the IEPS Ion Electric Propulsion System is Single-string system."]
[4.7448859214782715, 1.8784533739089966, "The Number of Retired Satellites of the DMSP (Defense Meteorological Satellite Program) Satellite Program is 16."]
[11.623290061950684, -1.2185417413711548, "The Mass of the MEPSI Satellite is < 1 kg."]
[5.2256693840026855, 4.369582176208496, "The Establishment of the State Vectors Data is Using Deep Space Network (DSN), Orbit Determination and ground uplink."]
[9.282756805419922, 7.94637393951416, "The Spatial Resolution of the LEND Neutron Detector is 5 km."]
[9.159358978271484, 3.203768491744995, "The Orbit Type of the Shakuntala Satellite is Sun-synchronous."]
[11.66993522644043, -1.2065991163253784, "The Mass of the Ralph Satellite End-body is 37.7 kg."]
[6.21305513381958, 8.225923538208008, "The Filter Wheel Rotation Frequency of the GOES Sounder Radiometer is 10 times per second."]
[8.605504989624023, 1.731091856956482, "The Launch Date of the Nancy Grace Roman Space Telescope Space Telescope is Mid-2020s."]
[2.4555511474609375, 5.338995456695557, "The Power Consumption of the CU Cabling Unit is 10W."]
[5.302568435668945, 9.609823226928711, "The Exclusion Angles of the STOs and STAEs Analog Electronic units is \u00b135\u00ba (sun), \u00b125\u00ba (S/C secondary reflection) \u00b125\u00ba (moon), \u00b135\u00ba (Earth)."]
[7.019891738891602, 7.440730094909668, "The Data of the Potential Instrument Unknown is Included in TT&C data."]
[1.7092093229293823, 4.849635124206543, "The Power Input of the CU Control Unit is 6-36 VDC."]
[7.12658166885376, 9.226824760437012, "The Along-Track Coverage of the MSI-0 and MSI-1 MSI Instruments is 30 km."]
[8.50757884979248, 6.468267917633057, "The Change of the Test Profile Test Procedure is Started on a warm temperature plateau to enable a valid home command."]
[11.912105560302734, 0.9435186982154846, "The Lunar Orbit Entry Date of the Chang'e-5 Spacecraft is Nov. 28."]
[9.987396240234375, 9.30325984954834, "The Telescope Aperture of the IRIS Satellite is 20 cm."]
[2.035069465637207, 4.798371315002441, "The Power Output of the Fission Surface Power System Power System is At least 40 kilowatts."]
[9.370234489440918, 8.294608116149902, "The Be Filter Thickness of the X123-SDD X-ray Spectrometer is 8 \u00b5m."]
[4.69488525390625, 5.596930027008057, "The Modulation and Coding Scheme of the Sentinel-1, -2, and -3 Satellites is Accommodated within the 300 MHz X-band bandwidth."]
[3.0440773963928223, 6.605703830718994, "The RF Power of the Unit Communication System is 8 W."]
[4.7566328048706055, 1.7450898885726929, "The Number of Satellites of the Long March 6 Rocket is 13."]
[4.454679012298584, 5.416377544403076, "The Data Handling of the LT Satellite is Deletes SOH and science data from its crosslink queue."]
[4.064918041229248, 5.0530805587768555, "The Redundancy of the Data Recording System System is Dual-redundant."]
[5.027293682098389, 6.253629684448242, "The Band Design of the Antenna Communication is L-band: circularly polarized dual-patch antenna, UHF-band : array of four inverted F antennas with capacitive loading."]
[9.47458553314209, 0.5186337828636169, "The Design Life of the QuikSCAT Satellite is 2 years."]
[7.190025806427002, 7.478670120239258, "The Data Usage of the HIRS Infrared Spectral Radiance Instrument is Calculate atmospheric vertical temperature profiles, determine ocean surface temperatures, total atmospheric ozone, precipitable water, cloud height and coverage, and surface radiance."]
[10.196455955505371, 2.9102046489715576, "The Altitude of the PAZ Satellite is 514 km."]
[8.940947532653809, 6.085052013397217, "The Control Modes of the IPS Instrument Pointing System is Automatic, Manual."]
[5.177659511566162, 5.482693672180176, "The Spectrum of the Starlink and OneWeb Satellite Constellations is Ku-band."]
[7.361473083496094, 0.6284708976745605, "The Deployment Date of the Pulsar satellites Satellite is Early 2025."]
[8.791378021240234, 10.650485038757324, "The Full Frame Integration Time of the CCD Image Sensor is 2.6 seconds."]
[7.161522388458252, 1.591544508934021, "The Presentation of the Global Change Observation Missions Satellite is June 25-29, 2007."]
[6.852952480316162, 1.7962226867675781, "The Anniversary of the Swarm Satellite is 4th."]
[6.908971309661865, 0.600456714630127, "The Public Listing Date of the Astra Small Launch Vehicle Developer is July 1."]
[7.097434043884277, 4.847052574157715, "The | of the GOSAT Satellite is Space.based Carbon Monitoring by GOSAT and GOSAT-2."]
[6.939864635467529, 0.41103264689445496, "The Launch Date of the SARAL Satellite is Feb. 25, 2013."]
[9.56067943572998, 0.5458177328109741, "The Design Life of the MERLIN Satellite is Approximately three years."]
[9.063801765441895, 5.335013389587402, "The Roll Nadir Pointing Accuracy of the Attitude Control Satellite Subsystem is \u00b115\u00ba."]
[10.260186195373535, 6.278171539306641, "The TGF Energy of the RHESSI Satellite is Beyond 20 MeV."]
[1.6931021213531494, 4.974720001220703, "The Power Supply of the Readout Electronics Electronics is Individual."]
[5.144136905670166, 7.441786289215088, "The Daily Data Volume of the Instrument Spectrometer is 50 Gbit."]
[4.8508219718933105, 1.839115023612976, "The Number of Satellites per Mission of the Copernicus Environmental Monitoring Satellites is 2."]
[8.492168426513672, 11.024785995483398, "The Spectral Bands of the Eastman Kodak KLI14403 linear CCD sensor Sensor is 0.52-0.62 \u00b5m (green), 0.63-0.69 \u00b5m (red), and 0.76-0.9 \u00b5m (NIR)."]
[5.8306193351745605, 5.485645771026611, "The Manufacturer of the GNSS Receiver Navigation Device is Syrlinks."]
[7.251928329467773, 1.2278523445129395, "The Program Date of the European Student Earth Orbiter Satellite is Aug. 10-15, 2013."]
[9.761547088623047, 8.99563980102539, "The Telescope Diameter of the Euclid Space Telescope is 1.2 m."]
[8.317681312561035, 3.64085054397583, "The Development Status of the Webb Space Observatory is Not provided."]
[6.877857685089111, 2.523893356323242, "The URL of the GOCE Satellite is http://www.esa.int/Our_Activities/Observing_the_Earth/GOCE/Earth_s_gravity_scarred_by_earthquake."]
[6.250144958496094, 2.832888126373291, "The PRS Element of the Galileo Satellite Navigation System is Unknown."]
[7.2102484703063965, 2.769425630569458, "The URL of the STEREO Satellite is http://science.nasa.gov/science-news/science-at-nasa/2011/06feb_fullsun/."]
[2.129760980606079, 3.9685397148132324, "The Power Generation of the SPOT-2 Satellite is Solar array."]
[8.025688171386719, 0.07399579882621765, "The Vehicle Dockings Per Year of the Orion spacecraft Spacecraft is 12-15."]
[5.8973069190979, 10.85173511505127, "The No of Passbands of the Channel 9 Sensor is 1."]
[6.040186882019043, -0.05326183885335922, "The Launch Date of the Galileo Satellite Constellation is 25 July."]
[4.279915809631348, 6.337461471557617, "The Downlink Frequency of the Communication Communication System is X-band."]
[7.501492500305176, 4.770657062530518, "The Momentum Offloading Management of the PROBA-V Satellite is De-activated 10 s before the next imaging sequence."]
[7.322042942047119, 1.2076513767242432, "The Remote Sensing Image Record Change Date of the Tongzhou Beijing Location is 13 Oct. 2017."]
[9.066579818725586, 1.3371020555496216, "The Observation Start Time of the INTEGRAL Satellite is 15:30:59 on 24 January."]
[11.437154769897461, 2.1852571964263916, "The Travel Time of the Hayabusa-2 Space Probe is Six years."]
[4.669165134429932, 0.20160147547721863, "The In-Orbit Fleet of the OneWeb Company is 110 satellites."]
[10.538134574890137, -1.0825656652450562, "The Scientific Payload Mass of the Microsatellite Satellite is 10.8 kg."]
[8.218460083007812, 4.595393180847168, "The Swath Width of the CO2Image Satellite is 50 km."]
[6.321796417236328, 8.643403053283691, "The Volume of the RMU Radiometer Microwave Unit is 180 x 170 x 50 mm."]
[6.101579666137695, 6.49404239654541, "The Dimensions of the SGR-ReSI Interface Unit is Approx 300 x 160 x 30 mm."]
[4.74570369720459, 1.8016325235366821, "The Number of Satellites of the Flight Satellites Satellites is 8."]
[9.405143737792969, 0.7010754942893982, "The Mission Condition of the PROBA-V Mission Satellite Mission is Excellent after six months of operations and one year after launch."]
[9.019392967224121, 1.5813783407211304, "The Dust Measurement Period of the Ulysses Spacecraft is 1992 to 1998."]
[10.170317649841309, 6.746130466461182, "The Heat Shield Type of the Skylab Space Station is Temporary parasol-type."]
[5.355403900146484, 3.5172953605651855, "The Content of the VN-rapport Report is Methaanreductie een van de meest kosteneffectieve maatregelen tegen opwarming."]
[4.179928779602051, 3.720717191696167, "The Reception Rates of the AIS Receiver Device is Above 13,000 AIS messages per hour."]
[13.113081932067871, 4.0457000732421875, "The Oscillation Modes of the Gaia Satellite is Radial and Nonradial."]
[8.064277648925781, -0.7260186672210693, "The Acoustic Chamber Testing Location of the Crew Dragon Spacecraft is NASA\u2019s Plum Brook Station test facility at Glenn Research Center in Ohio."]
[5.033636093139648, 5.010946750640869, "The Downlink Frequency Band of the Svalbard Ground Station Ground Station is L-band."]
[10.009740829467773, 1.498900294303894, "The Orbital Period of the CBERS-4 Satellite is 100.26 minutes."]
[7.277729511260986, 3.3145532608032227, "The True Anomaly of the Satellite Spacecraft is Arbitrary."]
[6.491948127746582, 8.487457275390625, "The Swath of the MWRI Microwave Radiometer Imager is 1400 km."]
[7.4459919929504395, 0.7469483017921448, "The End of Observing Mission of the PROBA-V Satellite is June."]
[11.096420288085938, 2.5115673542022705, "The Impact Speed of the Schiaparelli module Spacecraft is 540 km/h."]
[9.427987098693848, 5.070963382720947, "The Spin Rate of the CINEMA satellites Satellite is 2 rpm."]
[8.425180435180664, 9.615755081176758, "The NS FOV: max channel of the AHI Scanner is 16,311 \u00b5rad."]
[7.1207170486450195, 0.8774416446685791, "The Launch Date of the PW-Sat Satellite is Unknown."]
[6.05510950088501, 9.225391387939453, "The Weight of the MESSR Radiometer is 140 kg."]
[3.9789655208587646, 4.303044319152832, "The Components of the C&DH Subsystem Command & Data Handling is IEM (Integrated Electronics Module), PIE (Payload Interface Electronics), SSR, and two OCXO (Oven Controlled Crystal Oscillators)."]
[7.2393412590026855, 1.7320055961608887, "The Launch Date of the SWOT Satellite is Unspecified."]
[6.8472981452941895, 3.017247438430786, "The Mission Status of the TUBSAT Satellite is Mission complete."]
[9.655275344848633, 1.431583046913147, "The Revisit Time of the Tandem-L satellites Satellite is 16 days."]
[5.958827495574951, 9.069771766662598, "The Power of the Horizon sensor Sensor is 2.8 W."]
[10.487394332885742, -1.005513310432434, "The Mass of the NewSat-6 Microsatellite is 43.5 kg."]
[9.153532028198242, 10.698081016540527, "The Frame Coverage of the spaceCam c4000 Video Camera is 12 km x 12 km."]
[6.733306407928467, 3.8209381103515625, "The Imager Manufacturer of the HySIS Satellite is ISRO\u2019s Space Application Centre (SAC)."]
[9.441495895385742, 9.929182052612305, "The Use of Shadows of the Bennu Global Mosaic Map is Needed to make the surface features pop."]
[10.983235359191895, 7.204609394073486, "The Effective Detector Area of the HXCP Hard X-ray Polarimeter is 7 cm 2."]
[5.1064133644104, 4.822762966156006, "The Network of Direct Readout Stations of the EARS Data Service is Around the Atlantic and Arctic Oceans."]
[10.904333114624023, 7.118780612945557, "The Energy Range of the X-ray Satellite Navigation Navigation System is 1-15 keV."]
[6.379922866821289, 2.829218626022339, "The Manufacturer of the Resurs-DK1 Spacecraft is TsSKB Progress."]
[1.685552954673767, 4.185747146606445, "The Solar Array Type of the EPS Electric Power Subsystem is Fixed."]
[5.267413139343262, 4.698498725891113, "The Avionics Unit of the ICPS Upper Stage is Unknown."]
[5.613611698150635, 6.961475849151611, "The Chirp Bandwidth of the RA-1 Radar Altimeter is 330 MHz (for ocean mode) and 82.5 MHz (for ice mode)."]
[6.832706928253174, 2.0781025886535645, "The Purpose of the IMERG Precipitation Product is Add up the large rainfall totals."]
[6.56420373916626, 3.5591204166412354, "The Mission Concept of the FLuorescence EXplorer Satellite is ESA\u2019s Earth Explorer 8."]
[7.044827938079834, 2.7017688751220703, "The Operational Status of the Carbonite-1 Satellite is Still operational after two years."]
[9.632331848144531, 8.95220947265625, "The Aperture of the UVIT Telescope Telescope is ~375mm."]
[8.555477142333984, 10.409181594848633, "The CCD Detector of the PS2 Optical Instrument is 29MP."]
[6.5294575691223145, 8.082265853881836, "The Sampling Rate of the CIP Instrument is 1 and 8 Hz."]
[7.168868541717529, 4.701571941375732, "The Data Collection of the Geospace Dynamics Constellation Mission is Earth\u2019s ionosphere and thermosphere."]
[7.431289196014404, 2.949079990386963, "The Mission Status of the RaInCube Satellite is Unknown."]
[7.6743245124816895, 2.223832845687866, "The Remote Operations Location of the ExoMars Mission is France."]
[6.224923610687256, 2.0734798908233643, "The Mission Operations Location of the OPAL Satellite is SSDL ground station at Stanford University."]
[9.725676536560059, 6.879489421844482, "The On-Orbit Temperatures of the TacSat-4 Satellite is \u00b1150o C."]
[7.055556774139404, 9.841090202331543, "The Wavelength Range of the Band 4 Spectral Band is 1360-1390 nm."]
[6.633946418762207, 9.698273658752441, "The Instrument Mass of the S-192 optomechanical scanner Scanner is 57 kg."]
[7.064869403839111, 9.189469337463379, "The Maximum Beam Scanning Angle of the P Mode Observation Mode is \u00b1 1.9\u00ba."]
[8.404561042785645, 4.843684196472168, "The Purpose of the MMS Satellite is Study magnetic reconnection in collisionless plasmas."]
[1.4759541749954224, 4.8401970863342285, "The Output Voltage of the Charge Regulator Power Management Device is Unregulated 14 V."]
[9.420280456542969, 10.321686744689941, "The Incidence Angle of the Iris Video Camera Camera is < 40\u00ba."]
[5.921925067901611, 2.426090717315674, "The Affiliation of the Shobhakar Dhakal Vice President is Asian Institute of Technology."]
[8.852947235107422, 7.140783309936523, "The Instrumentation of the IMPACT Instrument is Solar wind electron and solar energetic particle instrumentation."]
[9.663761138916016, -0.7019852995872498, "The System Architecture of the SOHLA-1 Microsatellite is ACS, COM, EPS, Experiment connected to CCU and ECU."]
[7.509331226348877, 1.1592309474945068, "The Date of the Geometric Calibration of the MICAS CCD Sensor Calibration is July 16-23, 2000."]
[1.0373321771621704, 4.18662166595459, "The Provider of the Lithium Polymer battery Battery is ASP Equipment GmbH."]
[7.0511016845703125, 0.5499296188354492, "The Launch Date of the ICEYE-X2 Satellite is December 2018."]
[7.246005535125732, 1.4578142166137695, "The Conference Date of the Operationally Responsive Space Concept is August 8-13, 2015."]
[4.624523162841797, 0.25574570894241333, "The Number of Satellites of the OneWeb Satellite is 34."]
[10.085485458374023, 1.999004602432251, "The Orbital period of the KOMPSAT-3A Satellite is 95.2 minutes."]
[5.974758148193359, 8.49085807800293, "The Purpose of the MLS Microwave Limb Sounder is 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."]
[8.344490051269531, 0.6041304469108582, "The Communication Recovery Efforts of the Hitomi Satellite is Ongoing."]
[5.204202175140381, 6.316807746887207, "The Deployment Time of the Antenna System Antenna is Few seconds."]
[6.538424491882324, 0.6860546469688416, "The Launch Date of the GOSAT-GW Satellite is Early 2024."]
[11.760721206665039, -0.9377250075340271, "The Mass of the Aquahab Payload is 18 kg."]
[4.334228992462158, 5.679591178894043, "The Data Transmission of the Landsat-5 Satellite is X-band direct downlink only."]
[5.154555797576904, 2.0486249923706055, "The Number of Missions of the Buccaneer CubeSat is 2."]
[7.665224552154541, 7.667781352996826, "The Objectives of the MAESTRO Instrument is Measuring ozone, nitrogen dioxide and aerosol/cloud extinction in the atmosphere."]
[7.328160762786865, 8.110941886901855, "The Image Capture Time of the EUI Instrument is More than four hours."]
[6.576467990875244, 7.7953901290893555, "The Optical Power of the Temperature-and-current-stabilized LD Laser Diode is Unknown."]
[6.078493118286133, 6.168211460113525, "The Response Time of the System SAR is Less than 36 hours."]
[11.398347854614258, 2.283684492111206, "The Ascent-Back \u0394V of the Hayabusa-2 Spacecraft is 0.64 m/s."]
[9.79568099975586, 1.3180493116378784, "The Observation Duration of the BRITE satellites Satellite is 15 minutes."]
[7.214400768280029, 2.5365540981292725, "The URL of the NASA Orbiting Carbon Observatory-2 Satellite is http://meetingorganizer.copernicus.org/EGU2015/EGU2015-6804.pdf."]
[8.520721435546875, 8.711724281311035, "The Development Location of the Grating Reflection Unit Spectrometer Component is Fraunhofer IOF (Institute of Applied Optics and Precision Engineering), Jena, Germany."]
[11.327116012573242, 6.757227420806885, "The Resolution of the Spacecraft Module Satellite Module is Eight-times greater than any previous X-ray telescope."]
[6.954034805297852, 11.288824081420898, "The Wavelength FWHM of an unresolved line of the Spectrometer Instrument is 0.126 \u00b5m."]
[8.645520210266113, 10.680398941040039, "The Noise Performance of the CCD Camera Imaging System is SNR <= 128 at 100% albedo."]
[5.222620487213135, 6.992656230926514, "The Wavelength of the Radio Waves Phenomenon is Decameter."]
[5.868840217590332, 2.8692073822021484, "The Prime Contractor of the Galileo 2nd Generation Satellites Satellite is Thales Alenia Space in Italy."]
[8.221311569213867, 4.59654426574707, "The Swath of the Satellite Satellite is 55 km."]
[11.82552719116211, 3.2046985626220703, "The Inclination of the NanoRacks-QB50 CubeSats Satellite is 51.6\u00ba."]
[3.256551742553711, 5.984768390655518, "The Data Uplink Bands of the SDR (Software Defined Radio) Communication Device is USB (Universal S-Band) and SGLS (Space Ground Link System, L-band)."]
[9.011131286621094, 10.795610427856445, "The Repetition Cycle of the WiFS camera Camera is 5 days."]
[6.005093097686768, 4.116427421569824, "The Control Center Location of the Odin Satellite is Esrange."]
[8.721135139465332, 8.069579124450684, "The Quantity of the OSL Dosimeter Dosimeter is 1."]
[4.675421714782715, 1.870456576347351, "The Number of Satellites of the Lightspeed Satellite Constellation is 198."]
[9.774290084838867, -0.5422370433807373, "The Knowledge of the PARASOL microsatellite Satellite is 0.02\u00ba."]
[7.977578163146973, 0.925230085849762, "The First Light Images Date of the Landsat-9 Satellite is October 31."]
[5.875922679901123, 6.696559429168701, "The Antenna Baseline of the KaRIn Radar is 10 m."]
[7.935353755950928, -0.6665517687797546, "The Launch Date of the SpaceX CRS-25 Dragon Spacecraft is 24 May 2022."]
[4.394796848297119, 4.466168403625488, "The Communication Approach of the CAN Bus Data Communication is Wait-on-send."]
[8.538762092590332, 8.138907432556152, "The Function of the Shutter Calibration System Component is Oscillates in synchronization with the scan mirror and crosses the optical axis at the end of each scan."]
[9.363495826721191, 7.921692371368408, "The Measurement Range of the SEI Electron Imager is 2-200 eV electrons or ions."]
[6.866668224334717, 6.062178611755371, "The Laser Transmitter of the Aeolus satellite Satellite is World's first."]
[5.818047523498535, 6.215047836303711, "The Conference Presentation of the CSG SAR instrument Synthetic Aperture Radar is EUSAR 2016, 11th European Conference on Synthetic Aperture Radar, Hamburg, Germany, June 6-9, 2016."]
[6.6590728759765625, 0.8859263062477112, "The Launch Year of the TecSAR Satellite is 2008."]
[7.543516635894775, -0.024257760494947433, "The Acquisitions per Day of the SAOCOM-1A Satellite is 225."]
[9.488619804382324, 3.2798585891723633, "The Shape of the Procellarum Lunar Region is Rectangular."]
[9.539719581604004, 3.7733726501464844, "The Precision Formation Flight of the CanX-4 & CanX-5 Nanosatellites is Demonstrated."]
[8.801676750183105, 3.9205210208892822, "The Structure Shape of the UniSat-5 Satellite is Cuboid."]
[9.364892959594727, 4.841040134429932, "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."]
[10.510741233825684, -1.0492908954620361, "The Analyzer of Particles and Electric Fields Mass of the Microsatellite Satellite is 0.8 kg."]
[6.274497032165527, 3.763683557510376, "The Operational Modes of the TechEdSat Satellite is Basic operation and computationally demanding payloads."]
[7.272302627563477, 4.025889873504639, "The References of the GeoSTAR-III Satellite System is Observation of the Earth and Its Environment: Survey of Missions and Sensors."]
[11.609272003173828, 6.061137676239014, "The Distance of X-ray jet from the Manatee\u2019s head of the XMM-Newton X-ray Observatory is About 100 light years."]
[5.694642066955566, 6.416304588317871, "The Wavelength of the SAR antenna Antenna is ~ 10 cm."]
[8.775017738342285, 10.640066146850586, "The Timing Time Resolution of the CCD Image Sensor is ~10 -3 seconds."]
[5.207514762878418, 4.078214168548584, "The Manufacturer of the IXV Recorder Recorder is Curtiss Wright."]
[4.537557601928711, 6.737841606140137, "The Frequency of the X-band Communication Band is 8.320, 8.064 or 8.192 GHz."]
[11.136815071105957, 4.194867134094238, "The Purpose of the Roman Satellite is Make similar measurements of stars in both the Milky Way and other galaxies."]
[8.06264591217041, 4.008778095245361, "The Daily Image Acquisitions of the Pleiades-1A Satellite is Approximately 1300."]
[7.899522304534912, 8.682398796081543, "The Orbit Altitude of the NMS Neutral Mass Spectrometer is 300-400 km."]
[6.092777252197266, 6.083738327026367, "The Type of the S-193 Radar System is Spaceborne Ku-band scatterometer."]
[7.791980266571045, 8.673628807067871, "The Wavelengths of the EPIC Instrument is 10."]
[6.735589504241943, 8.838614463806152, "The Standard Interface of the CEASE-1 Instrument is RS-422 or MIL-STD-1553B."]
[8.968018531799316, 2.4785616397857666, "The Observation Wavelengths of the Herschel Telescope is Far-infrared and sub-millimeter."]
[7.097232818603516, 2.4620778560638428, "The URL (presentation) of the Cute-1.7+APD Nano-Satellite is http://lss.mes.titech.ac.jp/ssp/cute1.7/paper/aca2007_p.pdf."]
[10.826845169067383, 3.498096466064453, "The Closest Pass Distance to the Sun of the Solar Orbiter Satellite is 0.32 au."]
[7.4626641273498535, 8.448447227478027, "The Precision of Ozone Density Profile Determination of the ERIP Earth Remote-Sensing Imaging Package is 10-15%."]
[8.780152320861816, 10.121929168701172, "The Data Output of the Mid-IR Imagers Camera is PAL format (384 H x 288 V pixels)."]
[9.52784538269043, 1.2380307912826538, "The Bus Calibration and Validation Duration of the TeLEOS-1 Satellite is Two weeks."]
[10.642631530761719, 9.218659400939941, "The First Light Date of the CaSSIS Imaging System is Unknown."]
[3.4982821941375732, 4.515660762786865, "The FPGA of the SCU Satellite Central Unit is XQ2V1000-4FG456N (Virtex2)."]
[7.7193498611450195, 4.764715671539307, "The Function of the Kazachok Lander Platform is Remain stationary to investigate the climate, atmosphere, radiation and possible presence of subsurface water."]
[8.21263599395752, 3.2056846618652344, "The Presentation Location of the TanDEM-X Satellite is Fort Worth, Texas, USA."]
[7.947734832763672, 9.407761573791504, "The Wavelength of the SWIR Short Wave Infrared region is 0.1 \u00b5m."]
[7.084792137145996, 1.578843355178833, "The Paper Number of the ERG Satellite Satellite is 2011-r-50."]
[5.966912269592285, 3.166701316833496, "The Contractor of the M3MSat Satellite is COM DEV International Ltd.."]
[4.004680156707764, 6.495651721954346, "The Duplex of the RF Communications Communication System is Half."]
[3.5738890171051025, 4.527598857879639, "The Operation Duration of the nanoRTUTM Safe Mode Computer is Six months."]
[4.218429088592529, 4.16144323348999, "The Number of Computer Consoles of the Control Room Facility is 9."]
[8.005254745483398, 4.4414215087890625, "The Spatial Resolution of the Global DEMs Digital Elevation Models is About 30 m."]
[6.452601909637451, -0.6349919438362122, "The Prime Contractor of the QZS-1 Satellite is MELCO (Mitsubishi Electric Corporation) Kamakura Works, Kamakura-City, Japan."]
[7.4009690284729, 0.9249853491783142, "The Power Generation Anomaly Date of the DAICHI (ALOS) Satellite is April 22, 2011."]
[7.6006083488464355, 6.597959041595459, "The Typical Value of the SO2 Satellite Instrument is 10."]
[8.873985290527344, 2.1409709453582764, "The Mission Objective of the New Horizons Spacecraft is Explore Pluto and its system of moons."]
[4.668650150299072, 3.6900124549865723, "The Components of the JEM Module is 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)."]
[3.5452094078063965, 4.081373691558838, "The Total mass of assembly of the STRV-2 DHS Data Handling System is 2 kg."]
[6.614354610443115, 3.5495784282684326, "The Operator of the Arktika-M N1 Satellite is ROSCOSMOS."]
[8.220901489257812, 4.538911819458008, "The Swath Width of the Sentinel-5P Satellite is 2600 km."]
[4.729970932006836, 5.455651760101318, "The AOCS Mode of the TTTC Satellite System is Precise mode."]
[10.296222686767578, 4.991496562957764, "The Function of the Resistojets Propulsion System is The gas is forced to spiral down the resistojet to increase the travel path and thus the heat transfer."]
[5.3048529624938965, 3.531339168548584, "The Hardware Changes of the Satellite Satellite is Addition of a bolt-hole pattern and two ruggedized connectors."]
[8.920537948608398, 10.845078468322754, "The Swath Width of the WFC CCD Camera is 61 km."]
[10.303973197937012, 8.736125946044922, "The ISS of the EUVI Extreme Ultraviolet Imager is Included."]
[5.021482944488525, 1.1995702981948853, "The Aviation Market Growth of the India Country is Sustained double-digit growth for the last 50 months."]
[9.504624366760254, 5.8454790115356445, "The Control Strategy of the Passive Attitude Control System Attitude Control System is Robust, simple."]
[5.660642623901367, 4.247652530670166, "The Type of the Test Facility Testing Equipment is Vertical test facility."]
[2.1213200092315674, 4.5388102531433105, "The Power Generation of the Spacecraft Satellite is 5.2 kW."]
[5.835323810577393, 7.581468105316162, "The Data Availability of the ATMS Instrument is Within 180 minutes of observation."]
[7.2232160568237305, 2.7806947231292725, "The Sample Image Locations of the NovaSAR-1 Satellite is Cebu city and the nearby Mactan-Cebu International Airport, Masbate Island in the Bicol region of the Philippines."]
[7.2896223068237305, 0.6755211353302002, "The Operational Phase End Date of the HyperScout\u00ae Satellite is 2018."]
[2.4515163898468018, 5.858253002166748, "The Power Amplifier of the Ka-band Signal is 2.2 W."]
[4.059266567230225, 5.680764198303223, "The Downlink Data Rates of the NEMO-AM Satellite is 32kbit/s to 2Mbit/s."]
[6.028162479400635, 1.7683547735214233, "The Founder of the Kleos Space Company is Luxembourg government."]
[7.777447700500488, 8.99170207977295, "The Spectral Sampling Distance of the UV-2 Spectrometer is 0.15 nm."]
[9.133662223815918, 5.1480326652526855, "The Stabilization of the ALTIUS Satellite is Three-axis."]
[11.20721435546875, 2.83388614654541, "The Boulder Width of the Tycho central peak Lunar Feature is Over 100 m."]
[8.601723670959473, 6.199760437011719, "The AstroTube Boom of the AlSat Nano Satellite is Deployed and stowed multiple times, including full 1.5 m length."]
[6.5831685066223145, 4.663632869720459, "The Imaging Frequency Band of the RADARSAT-1 Satellite is C."]
[5.036453723907471, -2.368293523788452, "The Affiliation of the Santiago Urue\u00f1a Engineer is Unknown."]
[7.859128952026367, 0.6921744346618652, "The Brochure Release Year of the OceanSat-2 Satellite is 2007."]
[7.010209560394287, 0.26453444361686707, "The Operational Date of the Ikonos-2 Satellite is December 1999."]
[4.668304920196533, 3.909221887588501, "The Scientific Sensors of the SAMPEX Satellite is 4."]
[8.758072853088379, 7.167664527893066, "The Purpose of the PIMS Plasma Instrument is Measure the plasmas in Europa's ionosphere and Jupiter's magnetosphere."]
[6.426599502563477, 3.3417062759399414, "The Location of the Euclid Consortium Organization is Institut de Ci\u00e8ncies de L\u2019Espai (ICE, IEEC-CSIC) and Port d\u2019Informaci\u00f3 Cient\u00edfica (PIC) in Barcelona."]
[10.031941413879395, 1.7663062810897827, "The Orbit of the HaloSat Satellite is 93-minute orbit around Earth."]
[11.323430061340332, 6.603683948516846, "The Mirror Module Assemblies Presentation Date of the IXPE Satellite is 2019."]
[6.202261924743652, 4.760210990905762, "The Constellation Type of the ICEYE Satellite Constellation is Synthetic-aperture radar (SAR)."]
[7.602447509765625, 9.138526916503906, "The Resolving Power of the Instrument Spectrometer is 10,000."]
[7.573948383331299, 0.7402309775352478, "The Launch Date of the Galaxy Spacecraft is Late 2008."]
[3.974435567855835, 5.67860746383667, "The Data Download of the STRaND-1 Satellite is 372 kB in 5 weeks and 1 day."]
[3.598637580871582, 6.623505592346191, "The Digital Recorder Dump Rate of the X-band Communication Band is 61.44 Mbit/s."]
[6.803841590881348, 5.449403762817383, "The Measurement of the SMAP Satellite is Land and ocean measurements."]
[9.084205627441406, 10.761892318725586, "The Swath Width of the WiFS camera Camera is 810 km."]
[7.463187217712402, 9.595757484436035, "The Swath Width of the ERIP Earth Remote-Sensing Imaging Package is 170 km."]
[5.482802391052246, 10.25540828704834, "The Data Return of the LIRIS Laser Infrared Imaging Sensors is September 2014."]
[7.20283317565918, 5.739435195922852, "The Purpose of the Aeolus Satellite is Measure wind from space."]
[5.0488409996032715, 4.4125800132751465, "The Number of Unmanned Global Ground Stations of the C3S Command, Control and Communications Segment is 15."]
[11.48642635345459, 2.6640102863311768, "The Creation Method of the 3D Model of the Asteroid Model is Inferred the shape based on multiple photo angles."]
[7.683929920196533, 7.236059665679932, "The Orbit of the TEMPO Instrument is Geostationary orbit."]
[8.249641418457031, 1.8896700143814087, "The Workshop Date of the Herschel Satellite is Dec. 17-18, 2009."]
[7.186026573181152, 2.329014778137207, "The Mission URL of the GRACE Satellite is https://www.nasa.gov/feature/jpl/wet-winters-may-not-dampen-small-wildfires."]
[8.003021240234375, 8.875643730163574, "The Bandpass of the Telescope Optical Instrument is 540\u2013590 nm."]
[8.050922393798828, -0.7470137476921082, "The Splashdown Date of the Crew Dragon spacecraft Spacecraft is Sept. 18, 2021."]
[6.144818305969238, 3.422300100326538, "The Service of the Spire Global UK Company is Track the identity, position, course and speed of each vessel."]
[8.322576522827148, 6.166053295135498, "The Signal Modulation Causes of the IMAP Satellite is 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)."]
[2.142638683319092, 4.5496978759765625, "The Power of the Spacecraft Satellite is 1.75 kW (EOL)."]
[9.487401962280273, 7.4289960861206055, "The Temperature Range of the ExoMars Analytical Laboratory Drawer Laboratory Drawer is -120\u00b0C to -60\u00b0C."]
[5.504056453704834, 5.909722328186035, "The Antenna Mounting Plane Dimensions of the KySat-1 Satellite is Maximum 10 x 10 x 10cm."]
[8.984989166259766, 7.395018100738525, "The Solar Environment of the Electric Field Antennas Sensor is More severe than all previous experience."]
[7.152904033660889, 0.36578840017318726, "The Launch Date of the DeMi Satellite is 15 February 2020."]
[4.607861042022705, 5.657423496246338, "The RF Trunkline of the LCRD Satellite Communication System is High data rate."]
[5.260465621948242, 4.838613033294678, "The Location of the CDN2 Site Ground Station is 35\u00b0 20.729' N, 23\u00b0 46.577'E."]
[9.521414756774902, 0.5305984020233154, "The Design Life of the Resurs-DK1 Spacecraft is 3 years."]
[9.702653884887695, 7.870826244354248, "The Gd Electron Energies of the LND Particle Telescope is 29, 72, 78, and 132 keV."]
[11.76758861541748, 4.696726322174072, "The Size Comparison to Milky Way of the Leo I Galaxy is 30 times smaller."]
[6.3440165519714355, 2.9495091438293457, "The Partnership of the Webb Space Observatory is European Space Agency ESA, US space agency NASA, and the Canadian Space Agency CSA."]
[10.87972354888916, 7.131267547607422, "The Energy Range of the Satellite Imaging Instrument is Hard X-ray."]
[7.594326972961426, 7.081584930419922, "The Capacity of the MUSES Platform is Up to four Earth observation instruments."]
[7.7782158851623535, 10.848806381225586, "The Data Quantization of the Instrument Spectrometer is 10 bit (VIS); 12 bit (NIR)."]
[12.143583297729492, 3.2451772689819336, "The Inclination of the QuakeSat Satellite is 98.73\u00ba."]
[5.744219779968262, 3.1882264614105225, "The Bus Type of the NigeriaSat-2 Satellite is SSTL-300."]
[4.870508670806885, 9.163204193115234, "The Livestream Date of the InSight Seismic Experiment for Interior Structure (SEIS) is July 23."]
[1.7035099267959595, 4.8403520584106445, "The PPTs Max Current of the EPS Electrical Power Subsystem is 2.5 A."]
[11.247023582458496, 6.76871395111084, "The Angular Resolution of the XRT X-Ray Telescope is Improved."]
[11.811981201171875, 3.267348289489746, "The Incidence at the ground about of the S-193 Altitude is 35\u00ba."]
[7.699089527130127, 9.93286418914795, "The Wavelength Range of the VNIR Detector is 0.45 - 0.905 \u03bcm."]
[10.326238632202148, 4.952864170074463, "The Propulsion Efficiency of the DRACO Demonstration Rocket is Two to five times the efficiency of chemical propulsion."]
[5.318157196044922, 4.974335193634033, "The Conference Presentation of the Lunar Laser Communication Demonstration Communication System is Unknown."]
[9.510763168334961, 5.483752727508545, "The Stabilization of the AOCS Attitude and Orbit Control Subsystem is 3-axis stabilized."]
[9.899057388305664, 1.3337265253067017, "The Temporal Matchup Window of the CYGNSS Satellite is 3 hours."]
[7.407488822937012, 1.4219030141830444, "The Implementation of the Sentinel Asia Pilot Project is First Step."]
[7.042614936828613, 5.030592441558838, "The Quote of the ESA's Director of Earth Observation Programs Director is \"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."]
[6.683345794677734, 1.0965023040771484, "The Presentation Date of the Quasi Zenith Satellite Bus System Satellite Bus System is June 1-8, 2008."]
[7.829411029815674, 7.14230489730835, "The Observation Time of the Tri-TIP Instrument is Night-side portion of the orbit."]
[7.957091331481934, 7.2074666023254395, "The Components of the Radiometric Calibration Calibration is Radiance Calibration Coefficients, Response Linearity, Noise, Detector PRNU, Detector DSNU."]
[8.133010864257812, 7.408084869384766, "The Dark Calibration of the ICU Internal Calibration Unit is Implemented by means of a lightweight shutter placed in front of the optical slit."]
[11.718799591064453, -1.0184600353240967, "The Mass of the Payload Satellite Component is 100 kg."]
[5.6811041831970215, 8.062870025634766, "The Bandwidth of the Crystal Filter Signal Processing Component is 3 kHz."]
[5.84647798538208, 8.172625541687012, "The Bandwidth (GHz) of the ICI-1 Radiometer is 6."]
[8.933560371398926, 1.8332748413085938, "The Presentation Date of the BepiColombo Mission is Feb. 28-March 4, 2011."]
[9.521059036254883, 0.5434818863868713, "The Orbital Lifetime of the KE-2M satellite Satellite is Approximately six months."]
[4.337158679962158, 4.509366035461426, "The Interface Types of the SGR-ReSI Interface Unit is CAN, RS422, SpaceWire."]
[7.6143083572387695, 3.293020725250244, "The Data Processing of the CartoSat-1 Satellite is Advanced."]
[8.927806854248047, 3.21872615814209, "The Orbit of the IRNSS-1C Satellite is GTO and then raised into GEO."]
[3.245915651321411, 5.226806640625, "The Capacity of the Data Storage System is Flash memory 8 Mbit x 2 (redundancy)."]
[8.832565307617188, 5.318016052246094, "The Attitude Determination and Control System Performance of the Claire Satellite is Exceeded specifications."]
[4.245774269104004, 5.953384876251221, "The Band of the Telemetry Data Data Transmission is X-band."]
[9.147257804870605, 4.602291107177734, "The Wave Height of the STEREO spacecraft Satellite is 100,000 km."]
[10.291280746459961, 5.670882701873779, "The Deployment Method of the Tether Spacecraft Component is Rolled up and housed within the end mass of the EDT system."]
[4.770340919494629, 4.04689884185791, "The Designer of the Driver IC Component is Brazilian software house located on the campus of UFSM (Federal University of Santa Maria)."]
[12.501411437988281, 6.890257835388184, "The Photon Energy Spectrum of the PSR B0531+21 Pulsar is 0.5-5 keV."]
[9.243874549865723, 4.1450958251953125, "The Size of the Assembly Satellite Component is 310 mm x 200 mm x 480 mm."]
[6.565222263336182, 4.7579264640808105, "The Instrument of the Sentinel-1 Satellite is Imaging microwave radar."]
[1.9518578052520752, 4.1707868576049805, "The Average Power of the Solar Cell Assemblies Power Source is ~1.5 W."]
[7.774582386016846, 10.88304328918457, "The Data Quantization of the Scanning geometry Instrument is 10 bit."]
[5.947456359863281, 6.838728904724121, "The Along-Track Resolution of the SIRAL Radar is 250 m."]
[11.342106819152832, 3.9083430767059326, "The Study Duration of the Exoplanets Celestial Bodies is More than 27 months."]
[10.675167083740234, 3.4212095737457275, "The Final Image Distance of the Rosetta Spacecraft is 24 meters."]
[10.22343921661377, 2.9952099323272705, "The Data Point Interval of the GEOSAT Satellite is 6.7 km."]
[9.356014251708984, 0.6907650232315063, "The Experience of the Keith Masback Individual is Over 30 years."]
[9.436483383178711, 9.0520601272583, "The Collection Area of the CUTE Telescope is 20 cm x 8.5 cm."]
[10.740306854248047, 5.605391025543213, "The Primary Science Objectives of the Solar-A / Yohkoh Satellite is 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."]
[1.4704124927520752, 4.9462890625, "The Bus Impedance of the SBVR Power Supply is <100 kHz."]
[7.589023590087891, 6.634334564208984, "The Typical Value of the O3 Profile Satellite Instrument is 40, 50, 8 x 10 3."]
[7.236470699310303, 0.4277517795562744, "The Service Start Date of the Lightspeed Satellites Satellite is 2023."]
[5.118193626403809, 3.7620298862457275, "The Transport Layer Protocols of the IXV Communications Network Network is TCP and UDP."]
[3.8980345726013184, 2.3172388076782227, "The Size of the SPATIUM-I CubeSat is 2U."]
[3.6577699184417725, 4.506697654724121, "The CPU of the SHU Science Handling Unit is HD64F7145FW50."]
[4.74490213394165, 2.086962938308716, "The Number of X-ray Sky Fields Observed of the HaloSat Satellite is 334."]
[4.428112030029297, 5.768733978271484, "The Planned Improvement of the Radio Subsystem Satellite Subsystem is Adapting the waveform for better channel capacity utilization."]
[7.411599636077881, 0.7228882312774658, "The Target Launch Date of the MMO Spacecraft is JFY 2016."]
[7.063612461090088, 8.791489601135254, "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."]
[3.494156837463379, 4.59196138381958, "The Type of the Second FPGA FPGA is Co-processor."]
[7.225005149841309, 1.260469675064087, "The Publication Date of the Experimental Satellite System for Earth Monitoring Satellite System is 1981."]
[8.60831069946289, 6.948774337768555, "The Resolution of the Magnetic Field Sensor Magnetoresistive Sensor is 100 pT."]
[4.338761806488037, 6.193353652954102, "The Type of the Space Micro \u00b5STDN S-band Transponder is Digitally intensive."]
[9.482616424560547, 0.5010457038879395, "The Design Cycle of the SpooQySat Satellite is Shorter development cycle."]
[11.464434623718262, 5.175701141357422, "The Time to be Pulled towards the Black Hole of the Earth-sized clump of matter Unknown is About a day."]
[7.778554916381836, 5.9486870765686035, "The Step 1 Operation of the TRUTHS Satellite is LDs illuminate (underfill) first the CSAR cavity and then the transfer radiometer (TR)."]
[10.391558647155762, 4.993866920471191, "The Predecessor of the PPS-1350-G Hall-effect thruster is SPT-100 (Stationary Plasma Thruster)."]
[12.114230155944824, 3.2940380573272705, "The Inclination of the Orbit Satellite is 98.28\u00ba."]
[7.727504253387451, 5.228950023651123, "The Observation Mode Switching of the OCO-2 Satellite is Alternate 16-day global ground-track repeat cycles."]
[8.361286163330078, 4.210240364074707, "The Polarization Measurements of the GOME-2 Satellite Instrument is Advanced."]
[8.18230152130127, 10.143094062805176, "The Resolution of the CAVIS Imager is 30 m."]
[8.021260261535645, 1.3068747520446777, "The Date of the Dynamic Dunes Phenomenon is 15 March, 2021."]
[1.992984652519226, 4.46646785736084, "The Power Generation of the MTM Transfer Module is More than 11 kW."]
[3.6916491985321045, 5.201841831207275, "The Handled Products of the Mission Operation System Data Processing System is Approximately 1 TB/day."]
[9.413495063781738, 7.355128288269043, "The Improved by of the Electron Temperature Probe Instrument is K. Oyama."]
[9.074644088745117, 5.414213180541992, "The Pointing Control of the Attitude System Satellite System is One arc-minute."]
[4.890664100646973, 12.098809242248535, "The Responsivity Measurement of the Responsivity Measurement Instrument is 1.36 A/W."]
[3.360574245452881, 5.231606483459473, "The Memory Capacity of the SLIM6 Satellite is 2 x 2 GByte."]
[7.032352924346924, 4.355142593383789, "The Measurement Domain of the SkySat Constellation Satellite Constellation is Ocean, Land."]
[7.711032390594482, 0.14069108664989471, "The Vacuum Test Completion Date of the Prichal Module is October 28."]
[7.555943489074707, 7.635363578796387, "The Purpose of the TIRS Sensor is Identify clouds and focus on the real land surface."]
[1.9425005912780762, 3.880175828933716, "The Solar Array Type of the UK-DMC-2 Satellite is GaAs/Ge single-junction solar cells."]
[5.409961223602295, 3.2651686668395996, "The Platform of the SAR spacecraft Satellite is CAST-2000 bus with necessary modifications and upgrades."]
[9.69702434539795, 7.7391743659973145, "The Type of the FIREBIRD-2 A and B Payload is Focused Investigations of Relativistic Electron Burst Intensity, Range, and Dynamics."]
[7.745849132537842, 8.22911262512207, "The Observation Frequency of the EPIC instrument Instrument is About 13 times per day."]
[6.630884170532227, 3.890866994857788, "The Image and Video Capture of the DoT-1 Satellite is Managed by Raspberry PI Camera."]
[5.286923885345459, 6.703929424285889, "The Antenna Thickness of the Subarray Array is 9 mm."]
[7.029690265655518, 1.3272441625595093, "The Conference Date of the Earth Observation Constellation Satellites Satellite Constellation is 14-16 May 2013."]
[9.55370807647705, 3.6704375743865967, "The Purpose of the Lunar Flashlight CubeSat is Detect naturally occurring surface ice believed to be at the bottom of craters on the Moon."]
[10.840145111083984, 3.911424398422241, "The Temperature at Closest Approach to the Sun of the Heat Shield Parker Solar Probe Component is Nearly 2,500 degrees Fahrenheit (1370 \u00baC)."]
[12.11152172088623, 3.2860021591186523, "The Orbit Inclination of the STARS spacecraft Satellite is 98.06\u00ba."]
[4.460925102233887, 8.872562408447266, "The Energy Gain of the InSight Mars lander Spacecraft is About 30 watt-hours per sol."]
[6.197498798370361, 2.513394832611084, "The Orbit of the STPSat-3 Satellite is Near-circular orbit."]
[9.458454132080078, 5.793614864349365, "The Flight Heritage of the Passive Attitude Control System Attitude Control System is Extensive."]
[4.586807727813721, 6.061784267425537, "The Number of Channels of the Dual-channel Receiver Unit (DRU) Receiver is 2."]
[9.070451736450195, 8.679089546203613, "The Mirror Oscillation Frequency of the TIR Subsystem Imaging System is About 7 Hz."]
[10.935943603515625, 3.793323516845703, "The Rate of the Material Release Rate Volcanic Activity is One ton per second."]
[4.002314567565918, 5.783554553985596, "The Nominal Mode Data Rates of the LunaH-Map Satellite is 1 kbit/s to 128 kbit/s."]
[9.102970123291016, 4.584711074829102, "The Wave Height of the Satellite Satellite is 0.5 m to 20 m."]
[7.70246696472168, 0.6537721753120422, "The Launch Date of the OceanSat-1 Satellite is May, 26, 1999."]
[10.840703964233398, 5.629364013671875, "The Release Date of the Giant solar flare Solar Event is Sept. 15, 2014."]
[7.15283727645874, 6.8890581130981445, "The Delivery Date of the IASI-NG Instrument is Early 2022."]
[10.071131706237793, 9.904996871948242, "The Designer and Builder of the IRIS Imager Camera is SI (Satrec Initiative Co. Ltd.) of Daejeon, Korea."]
[7.402943134307861, 4.2377400398254395, "The PAN-A of the CartoSat-1 Satellite is Panchromatic Aft-pointing Camera."]
[9.000086784362793, 10.62006664276123, "The GSD (Panchromatic) of the EOS Camera is 1 m."]
[5.9750447273254395, 3.213515043258667, "The Operator of the MSG-3 Satellite is Hughes Network Systems."]
[10.386027336120605, 1.3119752407073975, "The Mean LTAN of the KOMPSAT-3 Satellite is 13:30 hours."]
[7.971350193023682, 1.3610705137252808, "The Internal Water Evidence Date of the Moon Celestial Body is August 27, 2013."]
[7.857705116271973, 8.693533897399902, "The Spectral Sensitivity of the SXI Spacecraft is 6 to 20 \u00c5."]
[9.525858879089355, 7.383106708526611, "The Building Exterior Temperature of the ECOSTRESS Instrument is A few degrees cooler than paved surfaces."]
[7.132248878479004, 9.197375297546387, "The Swath of the Interferometric Wide Swath mode (IWS) Operational Mode is 240 km."]
[11.734243392944336, 7.499116897583008, "The Unknown of the Atomic Clock Timekeeping Device is Unknown."]
[6.600075721740723, 4.021912097930908, "The Mission Overview of the Sentinel-3 Satellite is Unknown."]
[1.5797654390335083, 4.47920036315918, "The Efficiency of the Solar Array Regulator Regulator is 94%."]
[1.5573172569274902, 4.634914398193359, "The Efficiency of the DC-DC converter Power Converter is Greater than 85% across load range of 75% to 100%."]
[4.456570148468018, 2.990753412246704, "The PRN of the GSAT-0209 Satellite is 9."]
[6.8662800788879395, 0.4878489077091217, "The Launch Date of the MetOp-A Satellite is Oct. 19, 2006."]
[8.978419303894043, 2.462313652038574, "The Field of View of the Herschel Space Observatory is Little more than two times the width of the full Moon."]
[5.911930084228516, 4.935179233551025, "The SAR antenna of the Payload Satellite Payload is Nominal operations."]
[8.541657447814941, 1.09298574924469, "The Operation Start Date of the LRO Satellite is 2009."]
[6.752950668334961, 6.101400852203369, "The Instrument Type of the ISS-RapidScat Instrument is Scatterometers."]
[4.042043209075928, 1.2018871307373047, "The Mission Type of the Solar-B / Hinode Satellite is Non-EO."]
[7.662515640258789, 0.9952509999275208, "The Launch Dates of the Sentinel-2 Satellite is 23 June 2015 (Sentinel-2A), end of 2016 (Sentinel-2B)."]
[6.035992622375488, 0.5923361778259277, "The Launch Date of the Buccaneer CubeSat is 18 November 2017."]
[11.780237197875977, 4.51991605758667, "The Number of Stars of the Upper Scorpius Star Cluster is 83."]
[3.1273727416992188, 4.429893970489502, "The Requirement of the Monitoring and shutdown system Power Protection is Detect and shutdown any power line which has encountered a fault."]
[9.606488227844238, 5.973306655883789, "The Sensors of the ADCS Attitude Determination and Control Subsystem is Magnetometers and gyroscopes."]
[9.449956893920898, 0.9838193655014038, "The Mission Duration of the Sentinel-2 Satellite is 20 years."]
[6.066537380218506, 0.5623685121536255, "The Launch Date of the QB50-ISS CubeSats Satellite is Dec. 9, 2016."]
[5.581810474395752, 3.799513578414917, "The Contact Check Frequency of the CSpOC Space Operations Center is Daily."]
[7.027230262756348, 8.634346008300781, "The Resolution of the IRMSS Instrument is 150 m."]
[9.39147663116455, 7.888256549835205, "The Sensitivity of the LEND Neutron Detector is 100 ppm or better."]
[5.942861080169678, 1.6146177053451538, "The Mission Type of the PAZ Satellite is Dual use (civil/defense)."]
[3.869842529296875, 6.3352580070495605, "The Modulation Type of the High-rate Modulation Communication System is 4 Mbit/s with DQPSK modulation."]
[9.259793281555176, 4.145797252655029, "The Size of the Spacecraft Satellite is 100 mm x 100 mm x 227 mm."]
[7.377941131591797, 9.65404987335205, "The Polarization Angle of the Band 5 Spectral Band is 0/60/120 \u00ba."]
[8.057506561279297, 9.721710205078125, "The Position of the SASI-600 Shortwave Infrared Airborne Spectrographic Imager is Right-hand port."]
[7.530631065368652, 7.549703121185303, "The Function of the TES Satellite Instrument is Collecting measurements of ozone's greenhouse effect."]
[9.402970314025879, -0.44942498207092285, "The Communication Protocol of the Nanosatellite Satellite is FMCW."]
[7.439319133758545, 4.790462970733643, "The Data Use of the PROBA-V Satellite is Global vegetation data for operational and scientific use."]
[7.416332721710205, -0.2868820130825043, "The Launch Date of the H-II Transfer Vehicle \"KOUNOTORI3\" (HTV3) Cargo Craft is July 20, 2012."]
[7.618872165679932, 8.291910171508789, "The Acquisition Range of the Guider Instrument is 1.2\u00ba."]
[8.222931861877441, 3.7295138835906982, "The Range of the AeroCube-OCSD-B and -C Satellites is Unknown."]
[6.0057148933410645, 9.627277374267578, "The Mass of the GeoCarb Instrument is 138 kg."]
[8.405872344970703, 7.113937854766846, "The Frequency Range of the Magnetic Field Measurement System Instrument is 20 Hz - 1 kHz."]
[7.345355033874512, 9.943524360656738, "The Absolute Radiometric Accuracy of the Hyperion Imaging Spectrometer is <6% (1\u03c3)."]
[6.907641410827637, 3.345682144165039, "The Operation of the NICER Satellite is Space Station Twist."]
[4.395428657531738, 6.359176158905029, "The Downlink Frequency of the S-band Frequency Band is 2.402 GHz."]
[4.837481498718262, -3.389634370803833, "The Member of the Richard Miller Individual is True."]
[7.770453929901123, 9.031756401062012, "The ILS Spectral Resolution of the Instrument Spectrometer is \u226411 nm, \u226416 nm."]
[9.050849914550781, 8.21006965637207, "The Energy Range of the ELENA Sensor is <0.02-5 keV."]
[9.610066413879395, 5.665432929992676, "The Attitude Control of the ADCS unit Satellite Component is Satellite detumbling."]
[7.839141368865967, 10.770156860351562, "The Signal Conversion of the MEV Electronics Module is 12 bit."]
[4.995726108551025, 5.0750885009765625, "The Downlink Frequency Band of the Svalbard Ground Station Ground Station is S-band."]
[6.551767349243164, 2.7373738288879395, "The Operations Concept of the OPS-SAT Satellite is Transition from supporting educational missions to supporting operational ones."]
[7.264840126037598, 0.5834252238273621, "The Launch Date of the Ax-1 mission Mission is No earlier than January 2022."]
[6.126038551330566, 0.8700305819511414, "The Data Set of the RAVAN Satellite is Episodic."]
[11.251570701599121, 6.706580638885498, "The Navigation Capability of the SEXTANT Technology Demonstration is GPS-like navigation."]
[7.018437385559082, 0.6074756383895874, "The Launch Date of the WorldView-3 Satellite is August 13, 2014."]
[7.4823198318481445, 4.434808731079102, "The Tracking Passes Occurrence of the CAPSTONE Satellite is When nearer to periapse."]
[7.0069684982299805, 1.000369668006897, "The Backup Laser Activation Date of the CALIPSO Satellite is March 12, 2009."]
[9.601786613464355, 4.4263129234313965, "The Flatness Target of the Euclid Spacecraft is 0.05 mm."]
[5.133505344390869, 3.4312994480133057, "The Technical Problems of the Nauka Module is Several."]
[10.954934120178223, 5.334085464477539, "The Expected Location of Strongest Magnetic Field of the Sunspot Solar Phenomenon is In the dark part of the umbra."]
[3.544928789138794, 2.296631336212158, "The Size of the Eagle-1 (BeakerSat) FemtoSat is 1.5U."]
[5.8926801681518555, 5.4273881912231445, "The Function of the GPS Receiver Receiver is Provide ECEF position and velocity solutions to GNC SW."]
[7.053022861480713, 4.440379619598389, "The Measurement Domain of the Myriade/AstroSat-100 Satellite is Atmosphere, Gravity and Magnetic Fields."]
[11.102492332458496, 6.236715793609619, "The Production Dependency of the Neutrons Radiation is Variable high-energy charged particle fluxes and properties of the upper atmosphere."]
[4.996209144592285, 4.308712482452393, "The Mission Goal of the OICETS Satellite is Conduct interorbit laser communications experiments with ARTEMIS of ESA."]
[10.260560989379883, 4.922341346740723, "The COVP of the Propulsion Subsystem Propulsion System is 1."]
[9.408097267150879, 11.503073692321777, "The Effective FOV of the Channel 4 Sensor is 35 km x 76 km."]
[6.123398780822754, 3.2677247524261475, "The Primary Objective of the SDA Agency is Speed."]
[6.622941493988037, 4.049126148223877, "The Field of Regard of the RISAT-2 Satellite is Wide."]
[8.348997116088867, 1.0786075592041016, "The Image Capture Date of the LRO Satellite is Jan. 29, 2014."]
[12.13770866394043, 2.1722586154937744, "The Departure Date from Bennu of the OSIRIS-REx Spacecraft is May 10."]
[7.599607467651367, 8.687694549560547, "The Cross-Track Swath of the OMPS Nadir Profile Spectrometer Spectrometer is 250 km."]
[11.158737182617188, 6.158543586730957, "The Volume of the The Astronomical Journal Journal is 155."]
[5.870116710662842, 6.775193691253662, "The Frequency of the Radar Radar is 9.6 GHz."]
[9.187376976013184, 9.09969425201416, "The Typical high cadence of the HRI dual EUV 174 \u00c5 and 335 \u00c5 alternatively Passband center is 2 s."]
[10.55662727355957, -1.0378118753433228, "The Mass of the BIROS Minisatellite is Roughly 130 kg."]
[9.393953323364258, -0.2934529185295105, "The Construction Time of the Nanosatellite Tracking Ships Nanosatellite is Seven Months."]
[9.218923568725586, 9.46392822265625, "The Focal Length of the Pushbroom imager Optics is 5131 mm."]
[7.5913801193237305, 1.768965482711792, "The Publication Year of the WMO World Meteorological Organization is 2016."]
[10.203852653503418, 2.9166011810302734, "The Altitude of the Satellite HY-1B is 798 km."]
[9.441329002380371, 3.089996099472046, "The Orbit of the NorSat-3 Satellite is 550-650 km sun synchronous."]
[11.486051559448242, 2.1796391010284424, "The Schematic of the Hayabusa and Hayabusa-2 Missions is Figure 3."]
[7.438192844390869, 4.181519508361816, "The Instrument of the CryoSat Satellite is Radar altimeter."]
[5.436007499694824, 3.203788995742798, "The Mission Purpose of the Heinrich Hertz satellite Communication Satellite is Test the behavior of new technologies under extreme conditions in space."]
[7.599870204925537, -0.5027823448181152, "The Proposed Doubleheader Launch Date of the Falcon 9 Rocket is February 4."]
[5.781215667724609, 5.153514385223389, "The Program Start of the SIR-C/X-SAR Payload is SIR-B in l984."]
[5.494217872619629, 5.94807243347168, "The Antenna Diameter of the Ground Segment Satellite Ground Segment is As small as 2.4 m."]
[9.433515548706055, 4.183488845825195, "The Dimensions of the Kubik Miniaturized Laboratory is 40 cm cube."]
[2.194413185119629, 4.408809661865234, "The Average Power of the S/C Power Satellite Power System is 171 W."]
[7.238260746002197, 2.509700059890747, "The URL of the Cluster Satellite is http://www.esa.int/Our_Activities/Operations/Cluster_satellite_catches_up."]
[12.158432960510254, 3.262143611907959, "The Orbit Inclination of the ResourceSat-2A Satellite is 98.78\u00ba."]
[10.832133293151855, 3.502356767654419, "The Closest Approach to Sun's Surface in 2021 of the Solar Orbiter Satellite is More than 20 million km."]
[8.84240436553955, 10.241121292114258, "The CMOS Image Sensor Data Retrieval of the Imager Payload is Field gate programmable array with 32 MB RAM."]
[4.054299831390381, 1.1935638189315796, "The Mission Type of the SVOM Satellite is Non-EO."]
[8.024147987365723, 2.8055765628814697, "The Mission Launch Year of the IMAP Interstellar Mapping and Acceleration Probe is 2024."]
[10.280439376831055, 8.755738258361816, "The Telescope Image Cadence of the EUVI Extreme Ultraviolet Imager is Higher image cadence."]
[10.48604965209961, 6.113513946533203, "The Objective of the RUBI Fluid Science Experiment is Investigate the fundamentals of boiling fluids in microgravity."]
[9.540335655212402, 0.5116938352584839, "The Design Life of the Spacecraft Satellite is 5 years."]
[6.930086612701416, 0.4990403354167938, "The Launch Date of the GEOS-1 Satellite is Nov. 6, 1965."]
[6.106101989746094, 5.6717424392700195, "The | of the SGR-ReSI GNSS Receiver is Remote Sensing Using GPS Signals \u2013 The SGR-ReSI Instrument."]
[5.590078353881836, 4.2987961769104, "The Services of the MSS Mobile Serving System is Power, video and data transfer functions, robotic manipulation."]
[3.3666739463806152, 5.285276889801025, "The Onboard Memory of the COSMO-SkyMed-1 Satellite is 300 Gbit."]
[11.455228805541992, 4.1397175788879395, "The Diameter of the Kepler-438b Exoplanet is Less than 1.5 times the diameter of Earth."]
[9.260847091674805, 7.297161102294922, "The Sensor Operating Temperature Range of the FIPEX Instrument is 600-700\u00baC."]
[7.893136501312256, 9.800446510314941, "The Spectral Range of the AaSI Spectral Imager is Visible."]
[4.1345038414001465, 6.532054901123047, "The Frequency of the Uplink Signal is 749f0."]
[8.427900314331055, 9.21888256072998, "The Slit 1 Spectral Range of the MEGS-A Spectrograph is 5-20 nm."]
[9.300524711608887, -0.6330631971359253, "The Conference Presentation Date of the CDHS Nanosatellite is Oct. 2-6, 2006."]
[5.174281597137451, 4.974474906921387, "The Ground Station of the ARTEMIS Satellite is UHF tactical communications ground station."]
[7.94012451171875, 1.0687898397445679, "The Image Capture Date of the TopSat Satellite is Unknown."]
[5.612929821014404, 5.489602565765381, "The Provider of the Two-frequency GPS (NOX) GPS is DLR/GSOC."]
[6.817300796508789, 1.5737475156784058, "The Battery Support for Nominal Operations of the RapidEye Satellite Constellation is After 2020."]
[10.763335227966309, 1.827779769897461, "The Food Consumption of the Desert Locusts Insect is Same amount of food in one day as about 35,000 people."]
[4.867368221282959, 1.9335289001464844, "The Number of CubeSats of the QB50 Project Satellite Constellation is 50."]
[12.120232582092285, 3.312018632888794, "The Inclination of the Satellite Constellation Satellite Constellation is 105.6\u00ba."]
[8.422592163085938, 10.443374633789062, "The Peak Quantum Efficiency of the Image Sensor Imaging is 50%."]
[11.006954193115234, 5.452536582946777, "The Magnetic Field Strength of the Pulsar Celestial Object is 70 quadrillion times stronger than that of Earth."]
[1.4870376586914062, 4.949480056762695, "The Output Voltage (Nominal) of the LVPS Board Power Supply is +3.3 V."]
[6.3147969245910645, 5.11642599105835, "The Image Recording Capability of the SAR Antenna Antenna is All weather conditions, both during the day and the night."]
[4.639232158660889, 9.049761772155762, "The Safe Mode Entry Date of the InSight Mars Lander is 11 January 2022."]
[7.20184850692749, 0.38351985812187195, "The Launch Date of the CAPSTONE Satellite is June 28, 2022."]
[10.296151161193848, 5.64613676071167, "The Edition of the Tethers In Space Handbook Handbook is Third."]
[10.559123992919922, 2.282245635986328, "The Inclina. (\u00ba) of the Meteor-3-1 Satellite is 82.5."]
[5.045764446258545, 3.5440750122070312, "The specification of the Bus Satellite Component is  MethaneSAT."]
[4.9272637367248535, -3.2160253524780273, "The | of the J. F. Carbary, D. Morrison, G. J. Romick, J.-H. Yee Authors is J. F. Carbary, D. Morrison, G. J. Romick, J.-H. Yee."]
[4.23649263381958, 6.624074459075928, "The Frequency of the RF communication subsystem Communication Subsystem is 435.325 MHz/145.95 MHz."]
[9.131589889526367, 4.216538906097412, "The Size of the Bus Structure Satellite Component is ~2 m x 0.8 m in diameter."]
[4.1891937255859375, 6.250161170959473, "The Communication Protocol of the UHF/VHF data frame Data Frame is AX.25."]
[7.607590198516846, 2.3177525997161865, "The URL of the ExoMars Mars Orbiter is http://www.jpl.nasa.gov/news/news.php?feature=6663&utm_source=iContact&."]
[3.9340038299560547, 4.3952555656433105, "The Number of Boards of the OBC On-Board Computer is 4."]
[12.116793632507324, 3.281676769256592, "The Inclination of the FormoSat-3/COSMIC-1 Satellite Constellation is 72\u00ba."]
[9.461161613464355, 4.20106840133667, "The Height of the Resurs-DK1 Spacecraft is 7.4 m."]
[8.371336936950684, 10.06719970703125, "The Resolution of the JWST MIRI Detector Array is 1024 x 1024."]
[8.77235221862793, 8.707100868225098, "The Boresight Look Angle of the KaRIn Instrument is \u00b12.7\u00ba."]
[11.769688606262207, -1.1366353034973145, "The Launch Mass of the ALOS-3 Satellite is 2120 kg."]
[6.5808024406433105, 0.5925652980804443, "The Mission Update Date of the GovSat-1 Satellite is 31 Jan. 2018."]
[8.38471794128418, 7.829871654510498, "The Cadence of the Housekeeping Measurement is 1 minute."]
[12.011958122253418, 4.484364032745361, "The Publication Date of the Blue Ring Nebula Nebula is Nov. 18."]
[7.925922870635986, 6.383174896240234, "The Solar Calibration Frequency of the Satellite Imaging Satellite is Roughly weekly."]
[4.516491413116455, 4.344857692718506, "The House-keeping (HK) Data of the Control Units Satellite Component is Voltage, current, and temperature."]
[10.166004180908203, 6.72537899017334, "The Insulation Purpose of the BepiColombo Spacecraft is Protect the spacecraft from extreme thermal conditions."]
[5.6164984703063965, 3.758331775665283, "The Agility Performance of the CSG System Satellite System is Very high."]
[9.259075164794922, 5.383008003234863, "The Attitude Control of the QSat Satellite is 3-axis stabilization by using RWs (nominal), magnetorquers (detumbling)."]
[6.115999698638916, 4.392508029937744, "The Control of the ERA Robotic Arm is Can be controlled from both inside and outside the Space Station."]
[4.7028117179870605, 1.668116807937622, "The Number of Satellites of the Galileo Constellation Satellite Constellation is 24."]
[7.794869422912598, 7.901715278625488, "The Accuracy of the VISION Instrument is 5%."]
[7.840709209442139, 8.607230186462402, "The Peak Energy Deposition Separation of the Solar SXR Spectra Solar Phenomenon is About 5 km."]
[8.135613441467285, 9.434401512145996, "The Type of the Optical Scanning Design Imaging Spectrometer is Pushbroom."]
[11.854219436645508, 1.008004903793335, "The Re-entry Module Verification of the Chang'e-5 Lunar Mission is Aerodynamic design, heat-resistant materials, flight control system."]
[6.165693283081055, 2.1376960277557373, "The Bus Components of the Jason-2 Satellite is Altimeter and the DORIS receiver."]
[11.757856369018555, 1.6823276281356812, "The Touchdown Time of the Philae Lander is 17:25 GMT."]
[11.228875160217285, 2.641956090927124, "The Width of the Pas Moraine Moraine is Up to 12 miles (20 km)."]
[7.603878021240234, 5.310051441192627, "The Characterization of the OCO-2 Satellite is Before Observatory launch."]
[8.397950172424316, 0.6076110601425171, "The Radio Signals of the Hitomi Satellite is 3/27 01:23~01:27 (for 4 min) @USC, 01:21~01:27 (for 6 min) @ KTU."]
[2.207576274871826, 6.526248931884766, "The Latency of the ATL10 Arctic/Antarctic Sea Ice Freeboard Data is 45 days."]
[7.4401535987854, -0.031231043860316277, "The Docking Date of the HTV-1 Spacecraft is Unknown."]
[8.354558944702148, 8.054317474365234, "The Detector Type of the MM Radiometer Sensor is Schottky diode detectors."]
[8.06441593170166, 2.6811485290527344, "The Operational Date of the TerraSAR-X Satellite is January 2011."]
[8.820465087890625, 7.525575637817383, "The Unique Capability of the HPCA Electrostatic Analyzer is Uses radio frequency oscillations to sweep the majority of solar wind protons away from the detector, without affecting the magnetospheric oxygen."]
[10.227356910705566, 2.998227119445801, "The Altitude of the SCI Spacecraft is Approximately 500 m."]
[11.633837699890137, 5.204242706298828, "The X-Ray Jet of the M87 Black Hole is Superluminal Motion."]
[9.33289623260498, -0.6800979971885681, "The Developer of the Venta-1 Nanosatellite is Bremen University of Applied Sciences."]
[5.464125633239746, 4.012711524963379, "The Automation Flexibility of the VMOC Mission Operations Center is Full automation to complete manual scheduling."]
[7.438726425170898, 1.3482224941253662, "The Extended Mission Start Date of the SELENE/Kaguya Satellite is November 2008."]
[5.142683506011963, 2.2355523109436035, "The Number of Members of the OSCAR-QUBE Team is 15 students."]
[11.327467918395996, 6.6667351722717285, "The Deployment Mechanism of the IXPE observatory X-ray Observatory is Deployable boom."]
[6.532276153564453, 3.067249298095703, "The Unknown of the NASA/JPL Organization is Unknown."]
[10.06256103515625, 1.5950790643692017, "The Orbit Period of the ERBS Satellite is 96.8 min."]
[7.114157199859619, 0.6861727833747864, "The Launch Date of the Earth-Observation Satellite Satellite is Nov. 6, 2010."]
[9.463682174682617, 7.54697847366333, "The Concentration Range of the DN probe Neutral Particle Probe is 10^5 - 10^12 cm^-3."]
[6.3404645919799805, 5.556212425231934, "The 3-D Structure Mode of the Tandem-L Satellite is Fully-polarimetric SAR interferometry."]
[8.28650951385498, 10.490541458129883, "The Power of the Pushbroom Imager Imaging Device is 250 W."]
[7.225992202758789, 2.2925045490264893, "The URL of the EO-1 Satellite is http://ase.jpl.nasa.gov/public/papers/chien_aamas2005_lessons.pdf."]
[5.978043079376221, 9.611989974975586, "The Mass of the VIRR Instrument is 8.1 kg."]
[4.455604553222656, 6.204568386077881, "The Frequency Band of the S-band radio frequency Communication is S-band."]
[3.7799785137176514, 6.534611225128174, "The Command S-band of the RF communications Communication Subsystem is 1.2 kbit/s."]
[9.652191162109375, 1.450079083442688, "The Observation Duration of the Cal_doppler Observation Instrument is One entire day side of the orbit."]
[11.32165241241455, 1.4037389755249023, "The Operation Duration of the Yutu 2 Lunar Rover is 321 Earth days."]
[9.94864273071289, -0.6281483173370361, "The Structure Size of the PARASOL microsatellite Satellite is 60 cm x 60 cm x 80 cm."]
[6.833395481109619, 1.2223643064498901, "The Mission Success Confirmation Date of the GIOVE-A Satellite is April 2, 2008."]
[9.714821815490723, 8.726218223571777, "The Number of Reflectors of the RRA Retroreflector Array is 264."]
[5.697096347808838, 9.148722648620605, "The Average Power Consumption of the Instrument Sensor is 11 W."]
[6.81903600692749, 3.7584547996520996, "The Comparison of the Variant Satellite is DEMETER mission."]
[4.019853115081787, 4.439974308013916, "The BSL Entry of the MCU Microcontroller Unit is Provides BSL (BootStrap Loader) entry for payload and EPS."]
[9.2565336227417, 5.431206703186035, "The Control Capability of the Attitude Control System Satellite Subsystem is Two axes at any given time."]
[7.154970169067383, 1.3119062185287476, "The Publication Date of the LARES satellite Satellite is December 2017."]
[9.317150115966797, 6.396608829498291, "The Manufacturer of the Star Tracker Attitude Determination Device is Sodern."]
[9.522037506103516, 1.48471999168396, "The Staffing of the On-call Operations Operations is Initially 24/7, eventually reduced to 8 hours on weekdays."]
[3.157877206802368, 5.362824440002441, "The Error Detection and Correction Scheme of the SSR Solid State Recorder is EDAC (Error Detection and Correction)."]
[6.06397008895874, 0.5846824049949646, "The AIV Completion Date of the IOD CubeSat Satellite is June 2017."]
[5.4768290519714355, 10.236465454101562, "The Data Retrieval of the LIRIS Laser Infrared Imaging Sensors is 29 August."]
[3.2001242637634277, 4.934053897857666, "The Memory of the Onboard Computer Computer is 1 GB."]
[11.533092498779297, -1.2909278869628906, "The Mass of the Cospas-Sarsat search and rescue package Device is 8 kg."]
[8.963373184204102, 7.683149814605713, "The Output Voltage Behavior of the OPS systems Sensor is Decreases for distances smaller than 10 mm."]
[6.421337127685547, 9.109389305114746, "The Performance of the FSS Instrument is \u00b10.35\u00ba."]
[12.075353622436523, 3.311378240585327, "The Orbit Inclination of the CHORUS Satellite is 53.5\u00b0."]
[9.807124137878418, -0.9457674026489258, "The Attitude Control of the JL-1-GF03D Microsatellite is 3-axis, 4 flywheels."]
[9.153918266296387, -0.7917098999023438, "The Mission of the SOTA Small Optical Transponder is SOCRATES (Space Optical Communications Research Advanced Technology Satellite) microsatellite mission of NICT."]
[9.15755844116211, 9.155254364013672, "The FOV of the HRI Lyman-\u03b1 1216 \u00c5 Passband center is 1000 arcsec x 1000 arcsec."]
[7.607903480529785, 9.11372184753418, "The Spectral Range of the O2 A-band channel Spectrometer is 0.758 to 0.772 \u00b5m."]
[9.663290977478027, 5.500271797180176, "The ADCS System of the DeorbitSail Satellite is Orientation Suitable for Sail Deployment."]
[5.12373685836792, 6.965258598327637, "The Center Frequency (GHz) of the Antenna Reflector is 6.6."]
[9.033641815185547, 7.463648796081543, "The Field of View of the FSS Fine Sun Sensor is \u00b132\u00ba."]
[5.605017185211182, 4.260751724243164, "The Sub-Experiments of the EuTEF European Technology Exposure Facility is DEBIE-2, DOSTEL, EuTEMP, EVC, EXPOSE, FIPEX, MEDET, PLEGPAY, TriboLab."]
[5.442248344421387, 3.184084892272949, "The Provider of the Next generation solar cells / Astrium Solar Cells is EADS Astrium GmbH."]
[3.3510732650756836, 6.962095737457275, "The Digital Data Handling Subsystem Power Consumption of the SIR-C Phased Array is 800 W."]
[10.879693984985352, 5.704269886016846, "The Technique Developer of the Solar Flare Solar Event is Francoise Roddier."]
[9.500690460205078, 0.05346621572971344, "The Duration of Proximity of the DICE nanosatellites Satellite is Up to six months."]
[5.115357875823975, 6.918657302856445, "The Volume Efficiency of the Reflectarray Antenna Antenna is Leaves plenty of room for payloads such as science instruments or imaging systems."]
[5.239918231964111, 6.638160228729248, "The Remote Operation of the TUC Transponder Microwave Transponder is Yes."]
[7.466559410095215, 4.15411901473999, "The Instrument Type of the CryoSat Satellite is Precision orbit, Radar altimeters."]
[9.92991828918457, 4.453524589538574, "The Variant of the Lunar Photon Spacecraft is High energy."]
[5.998823165893555, 9.618854522705078, "The Mass of the Phoka-D Instrument is 3 kg."]
[6.6312127113342285, 7.559060096740723, "The Distance Measurement Accuracy of the Laser Altimeter (LIDAR) Altimeter is Several hundred meters."]
[9.213215827941895, 7.300908088684082, "The Sensor Type of the FIPEX Instrument is Solid oxide electrolyte micro-sensors."]
[6.065465450286865, 8.913681030273438, "The Power Consumption of the SOLSPC Radiometer is 32 W."]
[6.805688381195068, 0.96016526222229, "The Start Year of the MDPP-2 Program is 2000."]
[3.5072758197784424, 4.589816570281982, "The Configuration of the FPGAs Electronic Components is Columnized FPGAs."]
[7.7988481521606445, 1.2155388593673706, "The Date of the North Pole Observations Observation is 23 and 24 April 1994."]
[6.5949625968933105, 4.23777437210083, "The Capability of the Unseenlabs\u2019 maritime monitoring system Satellite System is Monitor three different areas of interest simultaneously."]
[5.291635036468506, 5.958314418792725, "The Antenna Configuration of the Satellite Satellite is Two nadir antennas."]
[11.823590278625488, 1.0780524015426636, "The Age of Rocks in Landing Zone of the Chang\u2019e-5 Lunar Lander is Much younger than those returned by the Apollo astronauts."]
[1.5337865352630615, 4.70141077041626, "The Battery Charging Voltage Range of the SABR DC/DC Converter is 5-34 V."]
[7.917979717254639, 2.052673816680908, "The Average Stationkeeping Cost of the ISEE-3 Spacecraft is 8.5 m/s per year."]
[6.068828582763672, 2.5318405628204346, "The Area of the RESTEC Distributor is Asia and Russian area."]
[6.077536582946777, 2.8311431407928467, "The Effect of the Moonlight Lunar Telecommunications and Navigation Satellite Network is Lowering the ticket price to lunar exploration."]
[7.49161958694458, 1.1280509233474731, "The Operation End Date of the Midcourse Space Experiment Satellite is July 22, 2008."]
[7.1628923416137695, 0.9854543805122375, "The Public Listing Date of the Satellogic Satellite Company is Dec. 22."]
[10.605642318725586, -1.057909369468689, "The Payload Accommodation of the Minisatellite Satellite is 50 kg (max)."]
[9.600314140319824, 0.9507941007614136, "The Expected Lifetime of the SpinSat Satellite is >6 months."]
[5.4928741455078125, 2.372856855392456, "The Funding Agency of the OPAL CubeSat is National Science Foundation (NSF)."]
[11.305306434631348, 3.5710229873657227, "The Porosity of the Comet Celestial Body is 70-80%."]
[8.028168678283691, 4.83692741394043, "The Downlink of the Image Location Knowledge Satellite Component is < 300 m."]
[6.352562427520752, 3.670849084854126, "The Mission Objective of the PROBA Satellite is Address issues of on-board operational autonomy."]
[8.921677589416504, 7.333603382110596, "The Number of Sensor Elements of the Chem-sensor housing Sensor is 32."]
[9.449342727661133, 0.5767282843589783, "The Nominal Lifetime of the Sentinel-5P Satellite is 7 years."]
[7.881546497344971, 5.800713062286377, "The Calibration Status of the Satellite Spacecraft is Uncalibrated."]
[7.041011333465576, 5.8529205322265625, "The Function of the AMI Instrument is 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."]
[7.032171249389648, 1.2819366455078125, "The Conference Date of the IASI-NG Satellite is 4-8 February 2013."]
[7.301812648773193, 1.4774267673492432, "The Conference Presentation Date of the Sentinel-1 Satellite is June 7-10, 2010."]
[10.195467948913574, 1.1012165546417236, "The Access Availability of the Inmarsat BGAN Service Satellite Communication Service is 24/7."]
[3.580547571182251, 6.582470893859863, "The Data Rate of the S-band Transmitter Transmitter is 32 kbit/s to 256 kbit/s."]
[7.247503757476807, 9.399349212646484, "The Swath Width of the ETM+ Scanner Imaging Device is 185 km."]
[9.077156066894531, 10.558161735534668, "The Image Size of the VIS Camera Camera is 1910 x 1270 pixels."]
[7.125129699707031, 4.295138835906982, "The Imaging Frequency Band of the ERS-2 Satellite is C."]
[7.798397541046143, 8.489760398864746, "The Integrated Irradiance Values of the Solar SXR Spectra Solar Phenomenon is 0.1-7 nm."]
[4.970283508300781, 2.229604959487915, "The Number of Instruments of the Nimbus-7 Satellite is 9."]
[7.916701316833496, 4.505033493041992, "The Image Resolution of the Satellogic Satellite is 1 meter."]
[7.443051338195801, 8.112810134887695, "The SNR of the Instrument Satellite Instrument is > 100."]
[10.88642406463623, 3.459669351577759, "The Projected Distance of the Newly Detected Source Object is 8 times the Earth-Sun distance."]
[1.0274759531021118, 4.339598655700684, "The Nominal Voltage of the NiH2 batteries Power Source is 10 V."]
[9.97640609741211, 9.552812576293945, "The Observation Data of the SAGE-II Satellite is Stratospheric ozone, aerosol, water vapor, nitrogen dioxide."]
[6.636828422546387, 0.5765135288238525, "The Launch Date of the GovSat-1 Satellite is 31 Jan. 2018."]
[7.696387767791748, 8.998562812805176, "The Spectral Bandwidth of the MAHRSI Instrument is About 4 nm."]
[8.623941421508789, 9.242193222045898, "The Detector Size of the Short Wavelength Band Spectrometer is 2.5 cm x 2.5 cm."]
[4.916255474090576, 1.9699931144714355, "The Number of CubeSats of the CubeSat - Launch 4 Satellite is 7."]
[6.118644714355469, 2.2177836894989014, "The Renamed In Honor Of of the KhalifaSat Satellite is His Highness Sheikh Khalifa Bin Zayed Al Nahyan."]
[10.970354080200195, 5.2076096534729, "The Characteristics of the Eruption Solar Event is Ejection of a hot layer of solar material above a magnetically active region on the Sun's surface."]
[6.5617356300354, 3.6109983921051025, "The Configuration of the Propulsion System Satellite Component is ESPA and T2E-compatible."]
[9.225711822509766, 10.07219123840332, "The Function of the High-Resolution Camera Camera is Capture Earth imagery."]
[6.084939956665039, 2.222059965133667, "The Launch Site of the DubaiSat-2 Satellite is Dombarovsky launch site in Russia."]
[9.445131301879883, 9.89554500579834, "The Function of the ShadowCam Instrument is Acquire images of shadowed regions of the moon."]
[9.475998878479004, 5.550900936126709, "The Stationkeeping Accuracy of the AOCS Attitude and Orbit Control Subsystem is \u00b10.5\u00ba in longitude and latitude."]
[6.4993720054626465, 1.0665860176086426, "The Launch Date of the OptiSAR\u2122 Constellation Satellite Constellation is 2020-2021."]
[5.897991180419922, 7.598578929901123, "The Image of the ATMS Instrument is Figure 9: Danielle Gallegos, ATMS program manager for Northrop Grumman, with the ATMS instrument behind her."]
[7.352004528045654, 8.941431045532227, "The Infrared Channels of the AATSR Imaging Radiometer is 1.6, 3.7, 10.8, and 12.0 \u03bcm."]
[7.590716361999512, 3.6364541053771973, "The Staff Count of the GHOSt Constellation Satellite Constellation is Unknown."]
[4.4450764656066895, 6.78645658493042, "The Frequencies of the DORIS Receiver is 400 MHz and 2 GHz."]
[5.378626346588135, 3.8920323848724365, "The Developers of the FLEX Mission Performance Simulator is J. Vicent, N. Sabater, C. Tenjo, J. Acarreta, M. Manzano, J. Rivera, P. Jurado, R. Franco, L. Alonso, J. Verrelst, J. Moreno."]
[8.813634872436523, 6.357029438018799, "The Tip Mass of the Gravity Gradient Boom Attitude Actuation Device is 40 g."]
[8.65757942199707, 1.8511801958084106, "The Detection Announcement of the Hubble Space Telescope Space Telescope is 2013."]
[7.837193012237549, 9.93796157836914, "The Swath Width of the Imager Imaging System is 16.4 km."]
[7.561219692230225, 2.9802093505859375, "The Field of View of the Solar-B / Hinode Satellite is Unknown."]
[7.10985803604126, 8.9601469039917, "The | 80 m of the RBV Instrument Spatial Resolution is Spatial resolution 80 m."]
[4.249778747558594, 4.572201251983643, "The Function of the IM Interconnect Module is Combines and splits the RF energy and serves as the interface between the transmitter, receiver, and antenna."]
[9.126917839050293, 9.379435539245605, "The Field of View (FOV) of the BEO Back-End Optics is 0.32\u00ba."]
[7.220104694366455, 3.4699323177337646, "The Mission Phases of the Satellite Spacecraft is Commissioning phase, Science phase."]
[10.876158714294434, 3.0994412899017334, "The Travel Distance Requirement of the Google Lunar X-Prize Competition is 500 meters."]
[7.361930847167969, 4.2899909019470215, "The Area Coverage of the Copernicus Sentinel-3 Satellite is 100 000 km2."]
[11.490632057189941, 2.1612021923065186, "The Touchdown Date of the Hayabusa-2 Spacecraft is February 22, 2019."]
[3.905121088027954, 2.2629153728485107, "The Size of the ICE-Cap CubeSat is 3U."]
[5.422915935516357, 2.5037882328033447, "The Investment Focus of the UrtheCast Company is Constellation of Earth-imaging satellites."]
[4.8974456787109375, 12.088875770568848, "The Uncertainty of the Responsivity Measurement Instrument is \u00b1 5%, 2\u03c3 confidence level."]
[1.9511632919311523, 3.991074800491333, "The Power Source of the Rosetta Spacecraft is Solar cells."]
[8.808586120605469, 1.43263840675354, "The Data Return of the Van Allen Probes Satellite is More than twice the expected."]
[6.011966228485107, 2.9296936988830566, "The Unknown of the NRO/MSD Sponsor is Unknown."]
[6.688047885894775, 7.190782070159912, "The Observation Date of the HSRL-2 Lidar is TCAP 2012."]
[5.953463554382324, 5.524163722991943, "The Configurable GNSS Signals of the GNSS-RO Receiver Receiver is GPS, GLONASS, and additional GNSS signals."]
[7.793924808502197, 0.4167838990688324, "The Target Launch Date of the Crew-5 Spacecraft is Fall of '22."]
[10.21976089477539, 9.464814186096191, "The Observation Resolution of the IRIS Observatory is Unprecedented."]
[8.3564453125, 4.520849704742432, "The Ground Sample Distance of the Satellite Satellite is \u2264 2.5 m (Pan), \u2264 10 m (MS)."]
[8.222752571105957, 3.258835554122925, "The Data Acquisition of the TanDEM-X Satellite is 300 TByte."]
[5.573974132537842, 7.494699478149414, "The Center Frequency of the KaRIn Instrument is 35.75 GHz."]
[4.606474876403809, 0.20508696138858795, "The Number of Satellites with FCC Application of the OneWeb Satellite Constellation is 48000."]
[7.062121868133545, 2.5705440044403076, "The URL of the IPv6 and IPsec on a satellite in space Presentation is http://www.cisco.com/web/strategy/docs/gov/wood-iac-07-B-2-6-06-paper.pdf."]
[8.593737602233887, 9.281718254089355, "The Field of View of the Limb Channel Imaging Channel is Wide (along the limb) and short (in the vertical direction)."]
[3.5498411655426025, 4.730050086975098, "The Quantity in PPU of the StrongARM SA1110 Processor is 20."]
[6.0216240882873535, 6.265720367431641, "The Pixel Size of the SAR Synthetic Aperture Radar is 25 x 25 m."]
[8.123153686523438, 3.288285493850708, "The Data Type of the TanDEM-X Satellite is Quicklook images."]
[1.5474281311035156, 4.477334022521973, "The Power Capability of the Buck-Boost Converter Solar Array Regulator is 450 W per Converter."]
[3.5994791984558105, 4.49857759475708, "The ROM/RAM of the SCU Satellite Central Unit is EEPROM(128KB x 2), SRAM(512KB x 4, 8MB x 1)."]
[7.969433784484863, 8.370819091796875, "The Band of the IASI Infrared Atmospheric Sounding Interferometer is 2."]
[8.154863357543945, 3.261309862136841, "The Imaging Capability of the Tandem-L Satellite is Exceeds that of TanDEM-X by a factor of 100."]
[6.719206809997559, 1.6970843076705933, "The Operator of the RapidEye Earth Observation Constellation is BlackBridge."]
[7.161433219909668, 2.9002163410186768, "The Documentation Source of the MEVI\u00b5S Satellite is \"Observation of the Earth and Its Environment: Survey of Missions and Sensors\" (Springer Verlag)."]
[10.077576637268066, 7.001868724822998, "The Effective Absorption of the MLI Thermal Control Device is \u03b1 < 0.05."]
[8.363689422607422, 1.4823675155639648, "The Launch Date of the Rosetta Spacecraft is March 2, 2004."]
[4.636349678039551, 0.19382637739181519, "The Number of Satellites of the OneWeb Satellite Constellation is 110."]
[4.437194347381592, 4.149133205413818, "The Onboard Network of the JWST Avionics Spacecraft Avionics is FPE (Focal Plane Electronics)."]
[13.130647659301758, 4.098870277404785, "The Function of the Gaia Space Telescope is Measure the position, movement, distance, and characteristics of billions of stars."]
[7.574270248413086, 0.8049509525299072, "The Start of Science Operations of the NICER-SEXTANT Mission is 17 July."]
[11.266770362854004, 3.5063774585723877, "The Pit Diameter of the Ma'at Region on Comet 67P/Churyumov\u2013Gerasimenko is More than 100 m."]
[7.461180686950684, 8.218441009521484, "The Dynamic Range of the Radiometry Sensor is 0-380 Wm -2  sr -1."]
[11.717267036437988, -1.2252135276794434, "The Mass of the SAOCOM-1A Satellite is 3,000 kg."]
[9.148771286010742, 1.2866129875183105, "The Monitoring Duration of the NASA Organization is Several decades."]
[6.205642223358154, 6.553659439086914, "The Function of the Poseidon-4 Radar Altimeter is 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."]
[5.2380452156066895, 6.052482604980469, "The Integration of the Reflectarray Antenna Antenna is Solar cells have been added on the opposite side."]
[1.4718838930130005, 4.9651899337768555, "The Bus Voltage of the SBVR Power Supply is 100 V."]
[7.600466251373291, 0.9513476490974426, "The Launch Year of the Sentinel-4B Satellite is 2032."]
[4.38518762588501, 6.0808820724487305, "The Frequency Band of the TT&C Tracking, Telemetry, and Control is S-band."]
[11.006296157836914, 5.058962345123291, "The Proof Mass Distance of the LISA Pathfinder Satellite is 35 cm."]
[7.6504621505737305, 7.662064552307129, "The Measurement of the Vector Sensor Instrument is Amplitude and phase of radio emission."]
[5.037597179412842, 3.7281229496002197, "The Mission Objectives of the M3MSat Satellite is 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 technol."]
[6.734050273895264, 2.1127769947052, "The Rainfall Measurement of the GPM Satellite is Up to 50 mm per hour."]
[6.814748764038086, 2.511350393295288, "The Website of the GOCE Satellite is http://op.gfz-potsdam.de/champ/systems/main_SYSTEMS.html."]
[9.557040214538574, 0.3981529772281647, "The Design Life of the RISAT-2 Satellite is 5 years."]
[10.517448425292969, 6.021640777587891, "The Importance of the Micro-gravity experiment Experiment is Development of fluids, space material science, space life science."]
[5.982151985168457, 5.799877643585205, "The Reflector Size of the Biomass satellite Satellite is 12 m across."]
[7.735877990722656, 4.515002727508545, "The Field of Regard of the GF-2 spacecraft Satellite is Not specified."]
[5.891838073730469, 8.110400199890137, "The Frequency (GHz) of the ICI-7 Radiometer is 325.15\u00b11.5."]
[11.676176071166992, -1.2071284055709839, "The Mass of the CanX-6 / NTS Satellite is 6.5 kg."]
[3.8330581188201904, 2.3082854747772217, "The Maximum Cube Size of the Orbit Your Thesis! 2019 program Education Program is 4U."]
[4.954050064086914, -0.10184179246425629, "The Global Services Delivery of the OneWeb Company is 2022."]
[6.349826812744141, 3.589900255203247, "The Information of the GeoSat Follow-On Satellite is http://enterprise.spawar.navy.mil/UploadedFiles/gfo_fs.pdf."]
[6.548255443572998, -0.07836569100618362, "The Launch Date of the IRNSS-1D Satellite is March 28, 2015."]
[11.173861503601074, 2.7029783725738525, "The Depth of the Great Blue Hole Underwater Sinkhole is About 123 m."]
[7.962985992431641, 1.355669617652893, "The Article Date of the Micro cold traps Lunar Surface Feature is 26 October 2020."]
[7.0611724853515625, 0.6163749098777771, "The Launch Date of the Flying Laptop Satellite is 2017."]
[9.527223587036133, 5.836545467376709, "The Control Method of the ACS Attitude Control Subsystem is Magnetic control."]
[11.779496192932129, -0.9856322407722473, "The Mass of the Freqbone Payload is 10 kg."]
[8.863911628723145, 7.408515453338623, "The Photodiode Cant Angle of the Sun Sensor Suites Sensor is 45\u00ba."]
[1.7529391050338745, 4.803093433380127, "The Bus Rail Voltage of the Spacecraft Satellite is 26 \u00b16 V."]
[5.920248508453369, 6.5480570793151855, "The Band of the miniKaAR-C Radar is Ka-band."]
[10.038512229919434, 1.485324740409851, "The Time Resolution of the PIXIE Satellite is 60 seconds or better."]
[8.65280532836914, 8.83652114868164, "The Input Angle alpha of the Short Wavelength Band Spectrometer is 21.9\u00ba."]
[7.7312774658203125, 0.11838561296463013, "The Powering Up Start Date of the Prichal Module is October 11."]
[9.632786750793457, 2.295910596847534, "The Footprint Distance of the CloudSat and CALIPSO Satellites is Always within 2 km."]
[10.326151847839355, 8.707731246948242, "The Exposure Time of the Coronal Loops Imaging Device is < 1 second."]
[7.7987895011901855, 8.537408828735352, "The Time Between Observations of the SCIAMACHY Spectrometer is 150 seconds."]
[7.58439302444458, 8.354479789733887, "The Measurement Range of the SOLSPC Radiometer is 200-2400 nm."]
[7.24957799911499, 3.7962350845336914, "The Vision of the Eu:CROPIS Satellite is To derive the greatest benefit from long- term human space exploration."]
[5.947320461273193, 6.249685287475586, "The SAR Payload Accessible Swath Width of the RCM Satellite is 500 km."]
[7.955967903137207, 7.102287769317627, "The Pointing Stability Requirements of the TEMPO Instrument is High precision."]
[7.762053489685059, 1.267378807067871, "The Ticket Date of the Exoplanet mission Satellite is April 6, 2017."]
[7.891990661621094, 9.89327335357666, "The Detector Array of the VNIR Spectrometer Spectrometer is 60 x 250 pixels."]
[7.500120162963867, 9.588919639587402, "The Measurement Height of Atmosphere of the ERIP Earth Remote-Sensing Imaging Package is 0 - 55 km."]
[4.400622844696045, 2.7176876068115234, "The VPU Cores of the Ubotica CogniSAT-XE1TM CubeSat Board Satellite Device is 12 vector cores."]
[5.889433860778809, 4.30226993560791, "The Architecture Components of the MSAS Satellite-based Augmentation System is MRS (Monitor and Ranging Stations), GMS (Ground Monitor Stations), MCS (Master Control Stations)."]
[4.884708881378174, 4.459824085235596, "The Purpose of the SpaceLink Satellite Network is Provide real-time connectivity between space and the ground."]
[5.4449968338012695, 0.3198910057544708, "The Current Size of the Cerro Pelado fire Wildfire is More than 25,000 acres."]
[6.760893821716309, 2.2104227542877197, "The Status of the DWSS Satellite Program is Canceled."]
[7.755082607269287, 3.5883872509002686, "The Imaging Capability of the ICON Space Mission is Provide the ability to explain how these drivers set the stage for the extreme conditions of solar-driven magnetic storms."]
[6.684032440185547, 7.159718036651611, "The Function of the GEDI Lidar Instrument is Produces detailed observations of the three-dimensional structure of the Earth's surface."]
[5.942588806152344, 8.503945350646973, "The Data Resolution of the GeoSTAR Atmospheric Microwave Sounder is Very high temporal resolutions."]
[5.973843097686768, 2.474928379058838, "The Receiver Type of the SPOT-2 Satellite is 1st generation receiver (18 kg), a bi-frequency system in 1 channel."]
[7.9294633865356445, 7.450277328491211, "The URL of the Airborne Lunar Spectral Irradiance (air-LUSI) Instrument Instrument is https://www.nist.gov/measuring-cosmos/airborne-lunar-spectral-irradiance-air-lusi-instrument."]
[11.345287322998047, 1.5362621545791626, "The Driving Distance of the Yutu-2 Lunar Rover is 367.25 meters."]
[7.288290500640869, 0.9172484278678894, "The Launch Date of the MMS Satellite is Fall of 2014."]
[7.4982380867004395, 1.2477997541427612, "The Publication Date of the Ministers back ESA's bold ambitions for space with record 17% rise News Article is 23 November 2022."]
[6.824747085571289, 8.191237449645996, "The Thermal Measurement Accuracy of the HTS/AMSR2 Microwave Absorber is 0.4\u00baC (3\u03c3)."]
[6.002405166625977, 6.084535121917725, "The Multi-Look of the Capella SAR System is 10."]
[5.7058634757995605, 3.1696624755859375, "The Manufacturer of the ESAJECT Mechanism Satellite Deployment Mechanism is Verhaert of Kruibeke, Belgium."]
[7.318562984466553, 0.8722754716873169, "The Delivery Date of the \u00b5CAT Hardware is Sept. 2015."]
[6.21541166305542, 3.557915210723877, "The Provider of the MetOp-A Satellite is EUMETSAT."]
[10.101582527160645, 9.492799758911133, "The Near-UV Channel Spectral Resolution of the IRIS Observatory is 8 x 10-3 nm."]
[1.0167118310928345, 4.330901622772217, "The Li-ion Battery Capacity of the EPS Electrical Power Subsystem is ~20 Ah."]
[5.018165588378906, 1.6835790872573853, "The Operational of the Galileo Satellites 13 and 14 Satellites is Yes."]
[4.930030345916748, 3.870025157928467, "The Interface of the Service Module Satellite Module is Power and data handling bus."]
[6.273952007293701, 1.9769065380096436, "The URL of the Jason-2 Satellite is http://www.aviso.oceanobs.com/fileadmin/documents/newsstand/Newsletter/aviso_special_issue_3years_Jason2.pdf."]
[7.86228609085083, 8.993989944458008, "The Spectral Range of the Fourier transform spectrometer Infrared Spectrometer is 645 to 2760 cm-1."]
[9.782587051391602, 7.138597011566162, "The Application of the Supercapacitors Energy Storage is Space."]
[8.112728118896484, 10.046319007873535, "The Minimum Lower Band Edge of the MS8 (NIR2) Imager is 856 nm."]
[7.23621129989624, 8.305830001831055, "The Data Transmission Time of the COSIMA Mass Spectrometer is About 40 minutes."]
[6.752079963684082, 2.944427251815796, "The Mission Status of the FalconSat-3 Satellite is Mission complete."]
[3.6355667114257812, 6.312443733215332, "The Downlink Data Rate of the RF Communications Communication System is 32 kbit/s."]
[8.164761543273926, 0.22906862199306488, "The Blog Post Date of the International Space Station Space Station is 27 April 2023."]
[7.738678455352783, 7.1827521324157715, "The DOI of the SOFIE Satellite Instrument is 10.1002/2014JD021763."]
[4.199516296386719, 6.494591236114502, "The Bandwidth of the Ka-band Channels Communication System is 900 MHz each channel, 2.7 GHz total."]
[9.192023277282715, 0.7499232888221741, "The Service Continuity of the Pl\u00e9iades Neo Satellite Constellation is 15 years."]
[4.839186191558838, -3.387443780899048, "The Member of the Susan Ustin Individual is True."]
[4.201653480529785, 3.76690673828125, "The Operation Time of the NorAIS-2 Receiver AIS Receiver is Four and a half years."]
[4.908390045166016, 2.1123950481414795, "The Quantity of the SpaceBEE Picosatellites is 12."]
[6.920424461364746, 4.545860767364502, "The Type of the NigeriaSat X Remote Sensing Instrument is Imaging multi-spectral radiometers (vis/IR)."]
[7.234531402587891, -0.36746302247047424, "The Delivery Start Date of the Starlink Premium Satellite Internet Service is Second quarter of 2022."]
[11.047839164733887, 5.097981929779053, "The Interaction of the Coronal Mass Ejections Solar Phenomenon is Interacting in the interplanetary space with another Coronal Mass Ejection."]
[7.098699569702148, 3.76348614692688, "The Experiment Renewal of the SPOT-5 Satellite is TAKE5 experiment."]
[6.688873767852783, 8.349849700927734, "The Optical Pulse Dynamic Range of the LI Instrument is 6.7 - 670 mW/m 2 /sr."]
[7.238580703735352, 9.47281265258789, "The Spatial Resolution of the MSU-E Multispectral Scanner is 28 x 28 m."]
[8.05382251739502, 5.179577350616455, "The Flux Measurement Error of the HaloSat Satellite is 2.5%."]
[3.7311155796051025, 6.1991119384765625, "The Science Data Rates of the Ka-band Downlink Communication System is 7, 14, or 28 Mbit/s."]
[9.364469528198242, 4.823219299316406, "The Slew Angle of the MiRaTA Satellite is 90-105\u00b0."]
[12.112367630004883, 3.292142152786255, "The Orbit Inclination of the Monitor-E Spacecraft is 97.5\u00ba."]
[8.168720245361328, 10.628203392028809, "The Function of the TDC Time to Digital Converter is Processing valid photon events and rejecting subthreshold or incomplete events."]
[11.714428901672363, 2.5968077182769775, "The Primary Density of the Didymos Binary System is 2.1 g/cm3."]
[8.737614631652832, 0.16618163883686066, "The EREP Investigations of the Skylab Space Station is Unknown."]
[8.923426628112793, 10.084260940551758, "The Number of Cameras of the Imaging System Imaging System is 6."]
[9.258545875549316, 8.873637199401855, "The SNR of the Telescope Optical Instrument is 205."]
[10.424150466918945, 4.769286155700684, "The Delta Velocity of the Steam Propulsion Unit Propulsion is Up to 10 meter per second."]
[6.182077884674072, 1.392486572265625, "The Launch Control of the ORS-6 Satellite Mission is Not co-lead."]
[1.5659760236740112, 4.872377872467041, "The Voltage Range of the Suppressor Grid Grid is 0 to -12 V."]
[10.447467803955078, 6.204751014709473, "The Objective of the EFILE Experiment is Study the thermocapillary effect at the liquid-gas phase-change interface on evaporation in the space environment."]
[8.977313995361328, 5.123512268066406, "The Attitude Control Stability of the GF-2 spacecraft Satellite is 5 x10-4 \u00ba/s."]
[6.187783241271973, 7.873866081237793, "The Polarization of the MTVZA-GY Radiometer is Horizontal."]
[5.849853038787842, 3.6849875450134277, "The CONOPS and FDIR Features of the Twinkle Satellite is Robustness and redundancy; on-board autonomy and simple satellite safe-modes; extensive use of proven, off-the-shelf components; modularity."]
[7.95969295501709, 6.90412712097168, "The Overpass Timing Prediction Accuracy of the ARC Calibration System is Less than 1 second."]
[4.971724033355713, 2.1561331748962402, "The Payloads of the EIRSAT-1 Satellite is Trio of Irish payloads."]
[7.320274353027344, 1.9141770601272583, "The Publication Date of the TRUTHS Satellite is December 2003."]
[8.58759880065918, 8.065104484558105, "The Sensor Type of the MuREM Dosimeter is Two large area PIN diodes."]
[10.470853805541992, 9.268832206726074, "The Peak Season of the AgCam/ISSAC Imaging System is April - October."]
[8.779004096984863, 9.028903007507324, "The Value of the Straylight Performance Requirement is Less than 2%."]
[10.087606430053711, 2.496328830718994, "The Altitude of the KOMPSAT-3A Satellite is 528 km."]
[5.595451354980469, 1.5231317281723022, "The Vehicle of the SpaceX Launch Provider is Falcon 9."]
[9.058074951171875, 10.316743850708008, "The Image Capture Method of the NAC Camera is One line at a time."]
[7.532392978668213, 6.167413234710693, "The Impact of the EMIT Imaging Spectrometer is Help scientists understand which kinds of dust dominate each region and advance their understanding of dust\u2019s impact on climate and the Earth system."]
[4.409142971038818, 4.087444305419922, "The Formation Flying Algorithms of the Formation Flying Computer Computer is Runs."]
[7.785391807556152, 2.073063611984253, "The In-Orbit Demonstration Date of the ELSA-M Spacecraft Servicer is Late 2024."]
[5.084029197692871, 2.241271495819092, "The Number of Instruments of the MetOp Satellite is 11."]
[7.6752495765686035, 9.579002380371094, "The Spectral Bands of the SLSTR Spectral Imaging Instrument is 11."]
[7.3646650314331055, 4.51093053817749, "The Imaging Frequency Band of the ALOS-1 Satellite is L."]
[9.518552780151367, 8.969871520996094, "The Moon Angle Constraint of the CHEOPS Telescope is Larger than 5\u00ba."]
[9.204923629760742, 4.132135391235352, "The Dimensions of the Satellite Satellite is 4 m x 3 m x 2 m."]
[7.2090840339660645, 6.904975414276123, "The Presentation Date of the VIIRS Satellite Instrument is June 20-24, 2005."]
[4.080970287322998, 1.2380861043930054, "The Mission Type of the TechEdSat Satellite is Non-EO."]
[6.8012871742248535, 1.349269151687622, "The Conference Presentation Date of the JC2Sat & MIRAD Satellite is Sept. 29 to Oct. 3, 2008."]
[7.635979175567627, 7.866438388824463, "The Design Discussion of the MSX/UVISI Instrument is Three-paper series."]
[8.558765411376953, 5.048496723175049, "The Adapter and Separation System Type of the ALMASat-1 Satellite is 2-clamp separation method."]
[6.318037509918213, 9.638511657714844, "The Instrument Mass of the Scanning geometry Instrument is \u2264 70 kg."]
[17.72844696044922, 7.1628618240356445, "The J2000 declination (deg) of the B0540-69 Pulsar is -69.33171."]
[9.565028190612793, 7.852891445159912, "The Shielding Material of the EPI-Lo Electron Detector is Aluminum flashing of ~2 \u00b5m thickness."]
[7.175153732299805, 0.7478464841842651, "The Launch Date of the PROBA-V Satellite is Unknown."]
[7.8599772453308105, 0.36349040269851685, "The End of Life Date of the CryoSat Satellite is 08 Oct 2005."]
[10.46702766418457, -1.006855845451355, "The Mass of the UGATUSat Microsatellite is 30 kg."]
[7.2883620262146, 0.9121295809745789, "The Development Date of the PRARE-2 Satellite System is August 1995."]
[6.083432197570801, 4.027742862701416, "The Location of the Igloo Container is In front of the pallet."]
[6.85296106338501, 1.9832717180252075, "The URL of the China High-resolution Earth Observation System (CHEOS) Satellite System is http://www.oosa.unvienna.org/pdf/pres/stsc2014/tech-47E.pdf."]
[7.719077110290527, 13.593002319335938, "The Passband Range of the SPIM2 Spectrometer is 162-252 nm."]
[7.56546688079834, 0.8259868025779724, "The Team Members of the CLARREO Mission is 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. Hu."]
[5.447342872619629, 5.968217849731445, "The Ka-band Disadvantages of the SARAL/AltiKa Satellite is Attenuation due to water/water vapour in case of rain, resulting loss of data."]
[6.423971176147461, 0.424864798784256, "The Launch Date of the AAUSat-1 CubeSat is June 30, 2003."]
[5.184886932373047, 5.65854549407959, "The Dish Size of the NASA Wallops field Ground Station is 18.29 m."]
[5.289801120758057, 5.388717174530029, "The Ground Station Antenna of the KySat-1 Satellite is 21 m SPA (Space Tracking Antenna)."]
[7.865676403045654, 9.074029922485352, "The Wavelength of the Instrument Spectrometer is 2.3-3.8 \u00b5m."]
[7.5235185623168945, 0.25904226303100586, "The Debut Flight Date of the Rail-guided space launcher Space Launcher is October."]
[8.190584182739258, 9.852022171020508, "The Type of the Imager Imaging System is Pushbroom imager (or a line scan imaging system)."]
[6.882601261138916, 1.1617200374603271, "The Conference Presentation Date of the GPS/MET Satellite is Sept. 12-15, 1995."]
[4.082828044891357, 6.487860679626465, "The Noise Temperature of the System Communication System is Unknown."]
[3.7856621742248535, 4.472549915313721, "The OBC Processor of the X-Sat Satellite is StrongARM processor."]
[4.939541816711426, 6.363497257232666, "The Amplifier of the Phoenix GPS Receivers GPS Receiver is Independent low noise amplifier (LNA)."]
[7.576038360595703, 4.51487398147583, "The Observation Target of the PROBA-2 Satellite is Sun."]
[9.601195335388184, 6.140388011932373, "The Manufacturer of the iADCS-100 ADCS System is BST (Berlin Space Technologies) and Hyperion Technologies B.V.."]
[9.738243103027344, 7.240194797515869, "The Components of the Cooling System System is Pulse-tube cooler, symmetric compressor."]
[10.664813995361328, 5.025197505950928, "The Ejection Velocity of the ICU Container is At least 0.5 m/s."]
[8.882343292236328, 7.627546787261963, "The Mass Resolution of the HPCA Electrostatic Analyzer is Accurately separates and identifies the minute amounts of hydrogen, helium, and oxygen ions."]
[5.895026683807373, 6.346897602081299, "The SAR Payload Radar Center Frequency of the RCM Satellite is 5.405 GHz."]
[7.419665813446045, 5.458043575286865, "The Effect on Sea Levels of the El Ni\u00f1o Weather Phenomenon is More than a 30 cm higher than normal."]
[6.341336250305176, 5.108658313751221, "The Instrument Type of the Biomass Satellite is Imaging microwave radars."]
[4.448405742645264, 4.214146137237549, "The Data Bus of the OBDH Subsystem Satellite Subsystem is Dual redundant CAN bus."]
[11.610631942749023, -1.2642748355865479, "The Mass of the Capability Satellite is 14.0 kg."]
[10.886061668395996, 4.195132255554199, "The Purpose of the Kepler Mission Space Telescope is Detecting other planetary systems."]
[7.640875816345215, 7.500871658325195, "The Post-flight Calibration of the Gas Scintillation Proportional Counter Instrument is Unknown."]
[8.43847942352295, -0.041591159999370575, "The Attachment Time of the Centaur Second Stage and Spacecraft Rocket Components is 4 minutes, 33 seconds after launch."]
[6.297459125518799, 9.131309509277344, "The Power Consumption of the MuREM Radiation Monitor is ~1.4 W."]
[5.19362211227417, 1.7582905292510986, "The Constellation Size of the Kleos Space Satellite Operator is Up to 20 clusters."]
[9.893814086914062, 7.881563186645508, "The Instrument Performance Parameters of the HIT High-energy Ion Telescope is Summarized in Table 10."]
[5.333873271942139, 4.003370761871338, "The Responsibilities of the SSDC Space Science Data Center is Science data processing, managing, archiving, permanent preservation and distribution of data."]
[4.228592872619629, 6.219964981079102, "The Telemetry of the RF Communications Communication System is CW."]
[5.986282825469971, 10.819241523742676, "The AOI Sensitivity of the PF1 Passband Filter is Unknown."]
[6.129784107208252, 4.8564348220825195, "The Mission of the OSIRIS Instrument is Odin."]
[10.152057647705078, 6.744482517242432, "The Heat Management of the BepiColombo Spacecraft is 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."]
[7.494507312774658, 0.6288385987281799, "The Data Release Date of the Cheollian 2B Satellite is May 25, 2020."]
[8.884981155395508, 1.9379081726074219, "The Planned Mission Duration of the New Horizons Spacecraft is 2023 through 2025."]
[10.22921085357666, 4.935821533203125, "The Objective of the VAT (Vacuum Arc Thruster) Thruster is On-orbit demonstration of a trigger-less vacuum arc thruster."]
[6.003132343292236, 9.601973533630371, "The Mass of the Instrument Satellite Instrument is < 10 kg (with MI)."]
[12.112406730651855, 3.298215866088867, "The Inclination of the IRS-1B Satellite is 99.09\u00ba."]
[6.6382832527160645, 9.062627792358398, "The Dimensions of the Field Measurement Device Electronic Unit is 150 mm x 85 mm x 40 mm."]
[5.811081409454346, 2.9741122722625732, "The Manufacturer of the SEOSAT/Ingenio Satellite is Airbus."]
[7.491045951843262, 9.64305591583252, "The Number of Spectral Bands of the S-192 optomechanical scanner Scanner is 13."]
[10.719411849975586, 3.8110663890838623, "The Velocity Change of the Solar System Celestial System is 0.23 nm/s2."]
[7.375957012176514, 4.337160110473633, "The Output of the NGAVGS Sensor is Real-time video."]
[6.621892929077148, 2.403048276901245, "The Managing Center of the GPM Satellite is NASA's Goddard Space Flight Center in Greenbelt, Maryland."]
[10.343291282653809, 6.7011799812316895, "The Payload Mass of the TCS Thermal Control System is 7.26 kg."]
[9.62397575378418, 7.768283367156982, "The Field of View of the EPD-E Energetic Particle Detector - Electrons is < 28\u00b0."]
[7.025265693664551, 6.193771839141846, "The Temporal Sampling of the Sea Ice Concentration (SIC) Measurement is Sub-daily."]
[7.894050598144531, 1.1723144054412842, "The Date of the Satellites Spot Tornado Tracks Across Midwest Image is 14 December 2021."]
[9.584671020507812, 2.261326313018799, "The Cross-Calibration of the CloudSat Satellite is Additional Funds."]
[8.593114852905273, 6.8722076416015625, "The Resolution of the iMTQ Magnetorquer is 15 nT."]
[7.456615924835205, 9.957362174987793, "The Spectral Range of the Hyperspectral Imager Radiometer is 0.4 \u2013 2.5 \u00b5m."]
[11.491716384887695, -0.9798842668533325, "The ESPA Ring Mass of the DSX Spacecraft Payload Module Satellite is  240 kg."]
[4.018033027648926, 6.457304954528809, "The Modulation of the RF communication subsystem Communication Subsystem is AFSK (Audio Frequency Shift Keying)."]
[6.737181663513184, 0.753385066986084, "The RF Model Date of the MTG-I Satellite is 03 July 2019."]
[8.77696704864502, 3.32777738571167, "The Orbital Plane of the Orbital Phase 2 Orbit is Moved to the terminator plane."]
[8.940655708312988, 4.4972052574157715, "The S/C Structure of the Payload Satellite Payload is Main elements."]
[4.954410076141357, 1.805937647819519, "The Number of Doves Onboard of the PSLV-C37 Satellite Launch Vehicle is 88."]
[9.448774337768555, 7.80367374420166, "The Particle Measurement Ranges of the STAFF/DWP Instrument is Electrons = 20 keV - 400 keV; Protons = 40 keV - 1500 keV; Helium = 40 keV - 150000 keV; Oxygen = 40 keV - 4000 keV."]
[9.614057540893555, 6.626465797424316, "The Release Method of the Sail Closeout Panels Subsystem is Spring-loaded hinges."]
[8.838205337524414, 7.450159072875977, "The Surface Features of the WISPR Imaging Instrument is Aphrodite Terra, Tellus Regio plateau, Aino Planitia plains."]
[6.649416446685791, 0.37608838081359863, "The End of Mission Date of the SMART-1 Satellite is 3 September 2006."]
[8.797174453735352, 3.7190568447113037, "The Cross-Track Separation of the ANDESITE Satellite is 5 km."]
[8.801020622253418, 10.548785209655762, "The Data Size of the Camera Imaging Device is 14 bit/pixel."]
[8.919434547424316, 7.7756195068359375, "The Neutron Measurement of the SEDA-AP Instrument is Unknown."]
[9.496377944946289, 1.191244125366211, "The Payload Calibrations and Experiments Duration of the TeLEOS-1 Satellite is Five months."]
[5.889654636383057, 8.604893684387207, "The Swath width of the MWTS Microwave Temperature Sounder is ."]
[7.085944652557373, 6.939738750457764, "The Development Status of the IASI-NG Instrument is Critical Design Reviews for Instrument and System aspects completed."]
[5.9958815574646, 5.870230197906494, "The NESZ of the Capella SAR System is Unknown."]
[9.194513320922852, 4.145920276641846, "The Dimensions of the SSTL-X50 Satellite Platform is 65 x 65 x 72 cm."]
[6.079897880554199, 3.75380802154541, "The Managed By of the GFO Satellite is METOC (Meteorological/Oceanographic) Program Office of SPAWAR."]
[8.503350257873535, 1.6237932443618774, "The First Image Release Date of the Webb Telescope Telescope is 12 July 2022."]
[9.48352336883545, 7.770183563232422, "The Temperature Stability of the HyperScout\u00ae Telescope Telescope is Within 2.5\u00b0C."]
[6.61059045791626, 0.8802751302719116, "The Launch Date of the FormoSat-7 / COSMIC-2 Satellite Constellation is 25 June 2019."]
[2.2432444095611572, 4.442312240600586, "The Sunlit Average Power of the UKube-1 Satellite is < 1200 mW."]
[6.369218826293945, 2.751166343688965, "The Location of the GRNS Team is Applied Physics Laboratory at Johns Hopkins University."]
[4.788536548614502, 1.8224308490753174, "The Mission Count of the SSTL Company is 43."]
[6.599135875701904, 3.0262725353240967, "The URL of the Resurs-P1 Satellite is http://eng.ntsomz.ru/news/news_center/resurs-p_images_gallery_201505."]
[8.984086990356445, 4.071861267089844, "The Size of the SeaHawk-1 CubeSat is 30 x 10 x 10 cm."]
[9.200098991394043, 3.207970142364502, "The Orbit of the IRS-1B Satellite is Polar sun-synchronous orbit."]
[5.475431442260742, 2.9028677940368652, "The CubeSat Mounting of the Cygnus spacecraft Spacecraft is External."]
[6.057177543640137, 6.199972152709961, "The Orbits per Day of the TecSAR SAR is 15.22."]
[9.504295349121094, 0.5201338529586792, "The Lifetime of the Satellite Satellite is 15 years design after IOT."]
[8.701213836669922, 6.056036472320557, "The Purpose of the Upper Barrel Assembly Satellite Component is 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."]
[7.745216369628906, 6.8553314208984375, "The Orbit of the ECOSTRESS Instrument is Precessing orbit of the ISS."]
[6.978442668914795, 7.964894771575928, "The SST Temporal Sampling Period of the CIMR Radiometer Imager is Sub-daily."]
[8.929723739624023, 1.5588507652282715, "The Last Command Date of the Ulysses Spacecraft is June 30, 2009."]
[8.772058486938477, 0.1813230961561203, "The Repair Effectiveness of the Skylab Space Station is Exceeded expectations."]
[9.760415077209473, 1.5541731119155884, "The Repeat Cycle of the ResourceSat-1 Satellite is 24 days."]
[6.683044910430908, 6.843212604522705, "The Design of the BBR Instrument Instrument is Physically separated into two units: OU (Optics Unit) and the ICU (Instrument Control Unit)."]
[11.495248794555664, 4.210602283477783, "The Similarity to Earth of the Kepler-1649c Exoplanet is Earth in size and estimated temperature."]
[11.728960990905762, 7.498626708984375, "The Purpose of the Atomic Hydrogen-Maser Oscillator System Payload is Measure the effect of the gravitational potential on the frequency of a proper clock."]
[6.469733715057373, 8.293540000915527, "The Observation Parameters of the MWRI Microwave Radiometer Imager is Precipitation, cloud feature, vegetation, soil humidity, sea ice, etc."]
[10.61106014251709, 9.224493026733398, "The Image Date of the CaSSIS Imaging System is February 4, 2021."]
[4.8449249267578125, 1.6767812967300415, "The Number of Users of the FormoSat-3/COSMIC-1 Satellite Constellation is 3,000."]
[11.380843162536621, 4.208437442779541, "The Estimated End of the Oort Cloud Space Phenomenon is About 100,000 AU."]
[9.590073585510254, 5.991502285003662, "The Components of the ADCS Attitude Determination and Control System is Magnetometers, Solar array sensors, Magnetorquers, Gyroscope."]
[6.7676777839660645, 0.6940644383430481, "The Launch Time of the STPSat-3 Satellite is 01:15:00 UTC."]
[8.900259017944336, 9.278167724609375, "The FOV of the Band 1 Spectral Band is 400 km x 0.5 km."]
[8.844717979431152, 9.168863296508789, "The Gap of the Slits Optical Instrument is 30 \u00b5m."]
[7.852912902832031, 7.94276762008667, "The Objective of the OCO-2 Spectrometer is Measure sunlight reflected off the Earth's surface."]
[9.579120635986328, 1.4563734531402588, "The Downlink Time of the Sentinel-1, -2 Satellites is Approximately 16-18 minutes per orbit."]
[9.033894538879395, 0.6074373722076416, "The Planned Mission Duration of the Tiangong Space Lab Space Lab is 40 days."]
[4.75159215927124, 1.7724483013153076, "The Goal for Number of Satellites by 2025 of the Satellogic Satellite Company is 200 or more."]
[6.7339558601379395, 10.181069374084473, "The Primary Use of the Band 5 Spectral Band is SST, day/night clouds."]
[6.801852226257324, 7.6876749992370605, "The Replacement of the MHS Instrument is AMSU-B."]
[5.7957329750061035, 3.599456787109375, "The Experiment of the TU Graz University is Attempting to monitor signals emitted by devices in the 'Internet of Things' from space."]
[8.347467422485352, 7.995018482208252, "The Modification of the OCO-2 Instrument Verification Process is Seating Vibration followed by an alignment test."]
[7.653692722320557, 2.8342020511627197, "The Mission Type of the Hinode Satellite is Solar Study."]
[7.132048606872559, 4.5708208084106445, "The Instrument Types of the Sich-2 Satellite is Imaging multi-spectral radiometers (vis/IR), High resolution optical imagers."]
[5.955713272094727, 2.7311675548553467, "The Platform of the Alphasat Satellite is Alphabus."]
[8.92184829711914, 9.921533584594727, "The Type of the LAICA Camera is Lyman Alpha Imaging Camera."]
[3.6456422805786133, 6.656276226043701, "The Data Rate of the X-band transmitter Transmitter is 42.22 Mbit/s."]
[5.3063154220581055, 9.606855392456055, "The Star Intensity Accuracy (3\u03c3) of the STOs and STAEs Analog Electronic units is Random Bias -0.26 ~ +0.28 mag ((@ 6 mag) -0.4 ~ +0.65 mag (@ 6 mag)."]
[6.543933391571045, 2.6215338706970215, "The Critical Design Review End Date of the Lucy Discovery Program Mission is Oct. 18."]
[5.501144886016846, 5.534632205963135, "The Simultaneous Tracking of the SSTI GPS Receiver is Up to 12 GPS satellite signals."]
[4.733325958251953, 1.8486380577087402, "The Number of Satellites of the NSPO Satellite Provider is 12."]
[4.51533317565918, 4.2415924072265625, "The Manufacturer of the CEPA Adapter is Boeing."]
[8.559828758239746, 10.71840763092041, "The Pixel Count of the Kodak KAI-11002 CCD CCD is 11M pixel."]
[10.214509963989258, 3.0122082233428955, "The Altitude of the Satellite Satellite is 764 - 824 km."]
[11.542576789855957, 2.7018141746520996, "The Hypothesized Origin of the Psyche Asteroid is Nickel-iron heart or exposed core of an early planet."]
[6.217217445373535, 3.588149070739746, "The Agency of the MOMS Satellite is DLR."]
[4.256250858306885, 6.565546035766602, "The Beacon Frequency of the Life Raft Survival Equipment is 406 MHz."]
[5.657897472381592, 4.339967250823975, "The Data Relay Method of the GeneSat-1 Satellite is Encrypted communications through the public Internet."]
[8.553483963012695, 9.38699722290039, "The Sensitivity of the NIRSpec MIRI Optical Instrument is 5.2 x 10 -22  Wm -2  (2 \u00b5m, \u03c4 i =100,000 s, R=1000)."]
[6.650190830230713, 0.3676561713218689, "The Planned Launch Date of the CBERS-4 Satellite is 2013."]
[8.32520580291748, 4.55892276763916, "The Swath Width of the Satellite Imaging Satellite is 105 km."]
[4.968259334564209, 1.8433475494384766, "The Number of Spacecraft of the Pl\u00e9iades Satellite is 2."]
[8.009306907653809, 7.291843414306641, "The Co-Principal Investigator of the SIMPL Investigation is Walt Mirczak."]
[8.913804054260254, 2.777839183807373, "The Meeting Date of the Global Change Observation Mission (GCOM) Satellite is 24-26 April 2018."]
[6.622367858886719, 2.3453731536865234, "The Provider of the GPM Core spacecraft Satellite is NASA."]
[9.214910507202148, 2.2194440364837646, "The Flybys of the BepiColombo Spacecraft is One at Earth, two at Venus and six at Mercury."]
[7.241133689880371, 7.759525775909424, "The Backscatter Sensitivity of the Core Instrument Instrument is 8 x 10-7 m-1 sr-1."]
[10.615476608276367, -1.6842678785324097, "The Total Cargo Delivery of the HTV-7 Cargo spacecraft is 6.2 metric tons."]
[10.252070426940918, 2.9401967525482178, "The Altitude of the Satellite Orbit is 685 km."]
[6.3487019538879395, 5.02367639541626, "The Application Topics of the Pol-InSAR Application is Forest, Agriculture, Snow and ice, Ship detection, Wind and waves, Geological mapping, Urban areas, Landslides/subsidence, Earthquakes/volcanoes, Development of new SAR techniques."]
[10.679451942443848, 1.7071688175201416, "The LTAN Evolution of the Swarm-C (Charlie) Satellite is 9 hours of separation between lower pair and upper satellite at end of life."]
[10.26211166381836, -0.9079560041427612, "The Regulated Voltage of the GHGSat-D Microsatellite is 5 and 3.3 V."]
[9.35377025604248, 11.606986045837402, "The Pixel size of the Channel 7 Sensor is 32 km x 32 km."]
[9.09695816040039, 5.828010559082031, "The Components of the Attitude Sensing System Satellite System is Sun sensors, a three-axis magnetometer, and a star-tracker."]
[5.113890171051025, 5.514517307281494, "The Bands of the Star One D2 Satellite is Ku-, Ka-, C- and X-band."]
[6.09885835647583, 7.997413158416748, "The Design of the MTVZA-GY Radiometer is Total-power."]
[5.852017402648926, 8.123526573181152, "The Frequency (GHz) of the ICI-9 Radiometer is 448\u00b13.0."]
[10.3774995803833, 9.415287017822266, "The Orbit of the IRIS Observatory is Polar sun-synchronous orbit."]
[5.117186069488525, 4.340678691864014, "The Data Processing Levels of the SMC Center is N0, N1, N2."]
[7.16313362121582, 1.1573532819747925, "The Online Date of the Chinese Earth observation satellites Satellites is Jan. 12, 2017."]
[9.196707725524902, 5.9407806396484375, "The Accommodation Requirement of the ACC (Accelerometer) Instrument is Precise and stable in CoG (Center of Gravity)."]
[10.326726913452148, 5.188276290893555, "The MEOP of the Main Tank Propulsion Subsystem is 31 bar."]
[9.598087310791016, 7.813909530639648, "The Proton Energy of the GALS-VE Particle Energy Measurement Device is > 1200 MeV."]
[10.46468448638916, 3.358553171157837, "The Orbit Extent of the Observatories Satellite is Close to Earth to just beyond the moon's orbit."]
[3.7824814319610596, 5.591159820556641, "The Science Data Downlink Capacity of the Spacecraft Satellite is 105 Mbit/s."]
[8.220998764038086, 9.15668773651123, "The Spatial Resolution of the OLI-2 Sensor is 30 m."]
[10.765597343444824, 3.4677677154541016, "The Distance from Sun of the Solar Orbiter Satellite is About twenty percent of the way from the Earth to the Sun."]
[8.871071815490723, 10.620100975036621, "The Signal-to-Noise Ratio for Bright Objects of the MSU-100 Camera is 200."]
[10.931819915771484, 3.402148485183716, "The Distance from the Sun of the Juno Spacecraft is Orbiting Jupiter 10 times closer to the Sun than New Horizons."]
[7.810520648956299, 9.12275218963623, "The Spectral Resolution Element Sampling of the Spectrometer Instrument is 2.5-3.0 detector pixels."]
[8.547133445739746, 5.410600662231445, "The Relative Performance Error of the Spacecraft Satellite is < 1.5 arcsec over 1.5 s (95%)."]
[8.428333282470703, 6.124598026275635, "The Function of the MR LR Launch Restraint is Provide a stowed interface for the Main Reflector providing a load path through the composite structure to the spacecraft interface."]
[9.53612995147705, 0.4415956735610962, "The Design Life of the DubaiSat-1 Satellite is 5 years."]
[11.699210166931152, 1.7674216032028198, "The Landing Date of the MASCOT Lander is October 3, 2018."]
[5.843992233276367, 4.7375078201293945, "The Function of the L1-SAIF+ Satellite Message is Augmentation of satellite-positioning signal and shortening the TTFF (Time To First Fix)."]
[7.703341007232666, 9.066197395324707, "The Field of View of the Channels Spectrometer is 45'."]
[9.645465850830078, 3.888368606567383, "The Sail Deployment of the CanX-7 Satellite is Individual."]
[7.6212286949157715, 1.2116098403930664, "The Testing Start Date of the Parachute System Spacecraft Component is 2016."]
[8.324653625488281, 7.001163005828857, "The Mounting Location of the CREAM Cosmic-Ray Instrument is Externally to the ISS."]
[13.723861694335938, 1.6084282398223877, "The Launch Date of the Vega Launch Vehicle is 29 April 2021."]
[5.087812900543213, 4.096261501312256, "The Purpose of the Universal Waste Management System (UWMS) Installation and Spare Hardware Hardware is Critical installation and spare items to support operations of the next generation toilet system during the 2021 timeframe."]
[7.218979835510254, 9.44386100769043, "The Resolution of the MSU-M Multispectral Scanner is 1.0 km x 1.7 km."]
[7.553961753845215, 1.9265778064727783, "The Observation Period of the Wilkins Ice Shelf Ice Shelf is 2006\u20132009."]
[7.668107509613037, 0.9481894373893738, "The Image Capture Date of the Kanopus-V1 Satellite is 21.01.2013 - 27.01.2013."]
[7.049450874328613, 6.689619541168213, "The Spectral Range of the TROPOMI Instrument is Ultraviolet to visible and selected bands in near-infrared."]
[11.664172172546387, 5.309488296508789, "The X-ray Source of the MAXI J1820+070 Black Hole is Point source."]
[10.260709762573242, 9.464990615844727, "The Field of View of the IRIS Observatory is 120 arcseconds."]
[9.136336326599121, 9.897921562194824, "The Operational Orientation of the AgCam/ISSAC Imaging System is Local-Vertical-Local-Horizontal (LVLH)."]
[10.583827018737793, 2.5787477493286133, "The Altitude of the 46 nanosatellites Satellite is 530 km."]
[6.940004348754883, 1.3819677829742432, "The Agreement Date of the GMES-S Satellite is October 2014."]
[9.379927635192871, 7.314902305603027, "The Components of the FEU Faraday Cup Electronics Unit is Preamplifiers, FPGA, ADC, HMB."]
[11.393495559692383, 3.100346565246582, "The Composition of the Hamersley Group Rock Formation is Iron-rich rocks, banded iron formations, dolomites, shales, and volcanics."]
[5.020117282867432, 2.005862236022949, "The Payload Capacity of the ESPAStar Satellite Platform is Up to six hosted or 12 separable, free-flyer payloads."]
[6.052769660949707, 1.0631022453308105, "The Launch Site of the CANYVAL-X CubeSats CubeSats is SDSC (Satish Dhawan Space Center) SHAR (Sriharikota) on the east coast of India."]
[11.37170696258545, 3.933591365814209, "The Orbital Period of the Kepler-442b Exoplanet is 112 days."]
[7.5670552253723145, 2.7925515174865723, "The Conference Date of the Cross-calibration for KOMPSAT-2 MSC images using EO-1 Hyperion Calibration is April 16-18, 2014."]
[9.379656791687012, 10.256009101867676, "The Field-of-View of the PanCam HRC Camera is 5\u00b0 x 5\u00b0."]
[2.1095504760742188, 4.47714900970459, "The Solar Array Capacity of the KOMPSAT-6 Satellite is 2.250 kW."]
[7.26529598236084, 7.251487731933594, "The Manufacturer of the SEPAC Instrument is SwRI (Southwest Research Institute), San Antonio, TX, USA."]
[8.493766784667969, 8.682567596435547, "The Number of Holes of the Spectrometer Wheel Spectrometer is 14."]
[8.669255256652832, 3.7872447967529297, "The Global Coverage of the Antenna Subsystem Satellite Component is \u00b180\u00ba latitude."]
[5.889530181884766, 1.821875810623169, "The Launch Vehicle of the NPP Satellite is Delta-2-7920-10."]
[11.92783260345459, 3.2840473651885986, "The Orbit Inclination of the Polar Scout 6U CubeSat Satellite is ~98\u00ba."]
[8.577047348022461, 10.35070514678955, "The Resolution of the Detector CMOS Sensor is 2048 x 2048 pixels."]
[5.780094146728516, 0.408408522605896, "The Date of the Alaska Ablaze Natural Event is 15 June 2022."]
[8.499345779418945, 6.542534351348877, "The Boom Length of the MAGIC Magnetometer is 1 m."]
[8.413588523864746, 1.5362458229064941, "The Final Maneuver Date of the Rosetta Spacecraft is 29 September 2016."]
[7.920238494873047, 4.9702277183532715, "The Measurement Accuracy of the LARES satellite Satellite is Accurately reflects Earth's tidal perturbations."]
[4.3206939697265625, 5.326370716094971, "The Start of the Data Compression Imaging System Process is Autonomously as soon as the acquisition of data is stopped."]
[5.082661151885986, 1.8197988271713257, "The Number of Deployment Orbits of the STP-2 Mission is Three."]
[8.755392074584961, 6.925093650817871, "The Number of AMR Sensors of the SOSMAG Magnetometer is 2."]
[10.61001205444336, 6.03133487701416, "The Flare List Events with Emission above 12 keV of the RHESSI Satellite is Over 14,000."]
[7.6632280349731445, 9.574728012084961, "The Resolution of the spectral band band is 240 m."]
[5.377561569213867, 2.8366434574127197, "The Development Team of the Space Cube 2 Onboard Computer is T. Takahashi, T. Takashima, S. Fukuda, S. Kuboyama, M. Nomachi, Y. Kasaba, T. Tohma, H. Hihara, S. Moriyama, T. Tamura."]
[7.449844837188721, 0.08011451363563538, "The Launch Date of the SAOCOM-1A Satellite is 2014."]
[11.419378280639648, 4.361550331115723, "The Atmosphere Color of the Pluto Planet is Blue."]
[7.955659866333008, 8.532188415527344, "The Unknown of the CrIS Infrared Sounder is Unknown."]
[5.701237201690674, 4.608597755432129, "The Application of the Argos DCS Satellite System is Sustainable management of marine resources."]
[4.429625988006592, 3.9699435234069824, "The Architecture of the MicroStar avionics Avionics is Largely unchanged."]
[6.947084426879883, 2.50276780128479, "The URL of the TOPCAT Satellite is https://web.archive.org/web/20120306134455/http://www.bis.gov.uk/assets/bispartners/ukspaceagency/docs/space%20science/cubesats/topcat%20text%20and%20picture.pdf."]
[5.8881096839904785, 2.965312957763672, "The Manufacturer of the Orion spacecraft Spacecraft is Lockheed Martin."]
[6.684386253356934, 2.249488353729248, "The Evaluation of the GPM/DPR Satellite Instrument is Can be evaluated using ground validation observation network in Okinawa."]
[8.349759101867676, 5.272429466247559, "The Orbit Knowledge Accuracy of the Satellite Spacecraft is < 3 m rms in each axis."]
[0.9913384914398193, 4.328777313232422, "The Battery Capacity of the EPS Electrical Power Subsystem is 1.8 Ah."]
[10.295600891113281, 6.811244964599609, "The Payload Volume of the TCS Thermal Control System is 279 x 406 x 254 mm."]
[5.892888069152832, 6.891278266906738, "The Minimum Looks in Range of the Radar Sensor is 40 looks for 10 km cells."]
[8.555359840393066, 5.206355094909668, "The Roll Phase Error of the GP-B satellite Satellite is 0.13 mrad RMS."]
[8.71770191192627, 9.142098426818848, "The Slit Height of the Long Wavelength Band Spectrometer is 2.75 cm; 1/33 for bright target."]
[6.99946403503418, 0.5212005972862244, "The Launch Date of the Yubileyniy-2/MiR Satellite is July 28, 2012."]
[7.341192245483398, 10.084787368774414, "The Spectral Bands of the HyperScout Imaging System is 400-600 nm."]
[5.094666481018066, 5.96624755859375, "The Mean Height Values Rate of the GEOSAT Satellite is 1 Hz."]
[6.23325777053833, 7.810199737548828, "The Polarization of the ICI-8 Radiometer is V."]
[8.396475791931152, 6.1789445877075195, "The Usage of the Vision Aiding or Terrain Sensor Obstacle Avoidance System is Landing phase."]
[11.628890991210938, 4.500585556030273, "The Mass of the Stars Celestial Bodies is As little as a tenth of our sun\u2019s mass."]
[7.119173049926758, 4.234457015991211, "The Measurement Domain of the Meteor-1/Meteor-2/Meteor-Priroda Series Satellite Mission is Atmosphere, Snow & Ice."]
[9.74411678314209, -0.6488426923751831, "The Laboratory and Flight Testing of the Chibis-M Microsatellite Satellite is Unknown."]
[5.237781524658203, 6.571839332580566, "The Antenna Size of the HDR Terminal Communication Equipment is 3.4 m."]
[4.03224515914917, 10.352933883666992, "The NE\u0394T (K) of the ICI-4 Radiometer is 0.6."]
[8.908815383911133, 5.221829414367676, "The Mass Balance Usage of the Integrated Firing Test Test is Not used."]
[9.871810913085938, 6.580657482147217, "The Mission Purpose of the ASTRO-H Satellite is Give us a new view of the non-thermal processes taking place in the universe."]
[6.003592491149902, 3.6043689250946045, "The Measurement Domain of the QBITO CubeSat is Atmosphere."]
[9.497206687927246, 9.109380722045898, "The Aperture Diameter of the Telescope Optical Instrument is 5 cm."]
[4.269377708435059, 5.67955207824707, "The TT&C Downlink of the QSat Satellite is S-band with a data rate of 1 or 100 kbit/s."]
[5.822201728820801, 6.835265636444092, "The Bandwidth of the C-band Radar Altimeter Frequency Band is 160 MHz."]
[7.1580491065979, 5.272148132324219, "The Percentage of Global Warming of the CO2 and CH4 Greenhouse Gases is ~90%."]
[6.20637845993042, 5.374256134033203, "The Application of the Spaceborne GPS Instrument is Limb sounding and global monitoring."]
[12.00318717956543, 3.218254804611206, "The Inclination of the ELaNa-4 CubeSats Satellite is 40.5\u00ba."]
[8.83263874053955, 7.668557167053223, "The Aperture Shape of the IDM Ion Drift Meter is Square."]
[11.051963806152344, 4.082337856292725, "The Planetary Transits and Oscillations of stars of the PLATO Space Mission is Upcoming."]
[7.51995849609375, 3.8105392456054688, "The Orbital Separation from SPOT-5 of the SPOT-4 Satellite is 138\u00ba."]
[10.45736026763916, 4.2505974769592285, "The Inclination Accuracy of the Bloostar Launch Vehicle is \u00b10.05\u00ba."]
[10.03036117553711, 4.32078742980957, "The Structure Diameter of the Clementine Spacecraft is 1.14 m."]
[5.177447319030762, 3.5533599853515625, "The Contains of the Ralph Satellite End-body is SEDS (Small Expendable Tether Deployer System) box."]
[4.66034460067749, 6.178904056549072, "The S-band Downlink Frequency of the MSX Satellite is 2282.5 MHz."]
[6.308434009552002, 4.910661697387695, "The Contents of the Level-2 Data is Granule scene and global (tile) data of geophysical parameters."]
[5.014383316040039, 1.9368330240249634, "The Close Passes of the Messenger Spacecraft is 3."]
[7.401277542114258, 9.719176292419434, "The Frequency of the Sub-mm Band is 0.35 THz."]
[10.463595390319824, 6.109946250915527, "The Scientific Objectives of the EFILE Experiment is 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 evap."]
[7.998657703399658, 7.288736343383789, "The Calibration Procedure of the Radiometer System Instrument is 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."]
[6.734791278839111, 2.389573574066162, "The URL of the PSLV Satellite is https://www.isro.gov.in/2018press15.html."]
[6.7853851318359375, 3.9662702083587646, "The Measurement Domain of the ZACUBE-2 Satellite is Land."]
[4.255806922912598, 2.550016403198242, "The Hardware Cost of the Starlink Satellite Internet Service is $499."]
[7.56332540512085, 1.5539125204086304, "The IAC Presentation Date of the SMOS Mission is Oct. 12-16, 2009."]
[6.994045734405518, 8.392494201660156, "The Bands of the Advanced Spaceborne Thermal Emission and Reflection Radiometer (ASTER) Radiometer is 4-2-1."]
[3.4806437492370605, 5.32165002822876, "The Science Data Storage Capability of the Spacecraft Satellite is 48 Gbit."]
[10.768911361694336, 5.768730163574219, "The Ripple Amplification of the Solar Dynamics Observatory Satellite is Three times."]
[9.439327239990234, 1.1134958267211914, "The Mission Duration of the Tandem-L Satellite is 10 years."]
[6.293031692504883, 7.635865211486816, "The Polarization, Right Swath of the KaRIn Instrument is VV."]
[3.981281042098999, 4.609419822692871, "The Communication Interface of the EC Digital Signal Processor is 16-bit parallel port."]
[4.9514312744140625, 1.884207844734192, "The Number of Launch Tubes of the Picosa Launcher Satellite Component is 4."]
[6.084275722503662, 9.417902946472168, "The Mass Classes of the STAFF/DWP Instrument is 1, 4, 12-16, 28-56 amu."]
[5.472959995269775, 2.257906675338745, "The Number of Beams of the Eutelsat Quantum Satellite is 8."]
[10.300759315490723, 4.9154815673828125, "The Thrust of the Chemical Propulsion Thrusters Orbit Maintenance is 6 to 12.5 N."]
[6.751845359802246, 0.6706095933914185, "The Arrival Date at Guiana of the SEOSAT-Ingenio Satellite is September 25, 2020."]
[3.898750066757202, 2.287109613418579, "The Spacecraft Volume (After Inflatable and Sail Deployment) of the Spacecraft 3U CubeSat is 128 cm x 330 cm x 330 cm."]
[9.446207046508789, 1.0776373147964478, "The Duration of the BLT Transfer System is Three to four months."]
[6.064594268798828, 6.095439910888672, "The X-band Resolution of the SAR-XL Payload SAR Instrument is 1m class."]
[7.495439529418945, 4.079063415527344, "The Data Usage of the ESA's CryoSat mission Satellite Mission is Monitoring mountain glaciers."]
[13.038674354553223, 3.9891111850738525, "The Orbit of the Gaia Satellite is Second Lagrange point, L2, of the Sun-Earth system."]
[8.607301712036133, 6.225703716278076, "The Retraction Status of the AstroTubeTM Boom Boom is Retracted."]
[9.995882987976074, 8.57625675201416, "The Telescopes of the ASTRO-1 Satellite Mission is 4."]
[7.5397162437438965, 0.08029213547706604, "The Launch Date of the CHEOPS Satellite is 18 December 2019."]
[8.519001960754395, 5.979626178741455, "The Potential Adjustment of the Magnetic Field Models Geophysical Models is Send the pole back to Canada."]
[6.107345104217529, 6.395219326019287, "The Imaging Modes of the SAR-RCM Synthetic Aperture Radar is Single or dual polarisation, quad-polarisation."]
[8.282125473022461, 6.532474517822266, "The Chamber of the TVAC Testing is Thermal Vacuum."]
[7.439862251281738, 8.457679748535156, "The Impact of the Signal to Noise Ratio (SNR) Performance Metric is The higher the SNR, the smaller the bandwidth and the highest spatial resolution the better."]
[7.244627952575684, 8.129589080810547, "The Fast Imaging Time of the AMI Advanced Meteorological Imager is Within 10 minutes for FD (Full Disk) observations."]
[7.225622177124023, 3.032702922821045, "The Presentation of the Global Change Observation Mission Satellite is Unknown."]
[11.577439308166504, -1.2616690397262573, "The Mass of the OTB-1 Satellite is 138 kg."]
[11.201720237731934, 2.8768253326416016, "The Comparison of the Kuiper Belt Celestial Region is Big brother of the asteroid belt."]
[7.417566299438477, 8.937021255493164, "The Spectral Range (IR) of the VHRR Very High-Resolution Radiometer is 10.5 - 12.5 \u00b5m."]
[5.068061351776123, 2.0775012969970703, "The Number of Experiments of the D-Sat Satellite is 3."]
[8.181331634521484, 6.314321994781494, "The Observation Start Date of the LIGO/Virgo sensors Sensors is Late 2018."]
[5.64990234375, 9.16757583618164, "The Power of the HID Instrument is 2.0 W."]
[6.935247421264648, 8.809771537780762, "The Horizontal Resolution of the Mie co-polar channel Channel is 10 km."]
[8.201399803161621, 5.362554550170898, "The Purpose of the GEOTAIL Satellite is 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."]
[10.576929092407227, 9.15882682800293, "The Image Credit of the CaSSIS Instrument is ESA/Roscosmos/CaSSIS."]
[8.26486873626709, 9.094256401062012, "The Swath Width of the WAOSS-B Sensor is 533 km."]
[1.3694461584091187, 4.135718822479248, "The Battery Discharge of the Integral Satellite is Increased to more than six hours."]
[6.162327289581299, 5.896944999694824, "The Time Span of the GF-3 SAR Satellite is 29 days."]
[3.8318774700164795, 5.625566005706787, "The Data Download Rate of the Second generation spacecraft UK-DMC-2 and Deimos-1 Satellite is Up to 80 Mbit/s."]
[7.895118713378906, 0.2588406205177307, "The Operating Date of the ISS ship-tracker Satellite is Aug. 26, 2010."]
[8.939196586608887, 4.493160247802734, "The S/C Structure of the Payload Satellite Payload is Structure design."]
[5.7596917152404785, 2.905709743499756, "The Manufacturer of the Himawari-8 Satellite is Mitsubishi Electric Corporation."]
[9.047045707702637, 1.553278923034668, "The Interstellar Dust Measurement Period of the Ulysses Spacecraft is 16 years."]
[9.420403480529785, 11.547795295715332, "The Effective FOV of the Channel 6 Sensor is 26 km x 60 km."]
[7.004827976226807, 2.507894277572632, "The URL of the MidSTAR-1 Satellite is http://www.usna.edu/Satellite/midstar/downloads/main/PDRfinal.ppt."]
[7.814976692199707, 10.662867546081543, "The Complex Amplitude Resolution of the Digital Mixer Signal Processing Device is 16-bit."]
[6.744301795959473, 7.223219871520996, "The Data Generation Interval of the IMERG Data Processing System is Half hourly."]
[8.077530860900879, 7.8316192626953125, "The Sensitivity of the SCM Sensor is 100 nT."]
[7.4198198318481445, 0.1037907674908638, "The Launch Date of the SAOCOM-1A Satellite is 2019."]
[7.681995391845703, 7.542597770690918, "The | of the Canadian Electric Field Instrument (CEFI) Instrument is Overview of the Canadian Electric Field Instrument (CEFI) for Swarm."]
[6.931822776794434, 8.463582992553711, "The Spatial Sampling of the LI Instrument is < 10 km @ latitude 45\u00ba and subsatellite longitude."]
[2.02406644821167, 4.758849620819092, "The Maximum Power Point Tracking (MPPT) Mode of the NanoPower P60 Power Subsystem is Allows to gain around 20% of the input power."]
[9.457612037658691, 3.449010133743286, "The Coverage of the Permanently Shadowed Regions Lunar Surface Feature is About three percent of the moon's south pole."]
[11.626263618469238, 4.5479912757873535, "The Pulsation Patterns of the Delta Scuti stars Star Type is Regular."]
[6.579371929168701, 1.0909786224365234, "The Launch Dates of the GOES-N, -O, -P Satellite is May 2006, June 2009, March 2010."]
[8.384592056274414, 9.553647994995117, "The Image Types of the Optical System Instrument is Panchromatic, multispectral MWIR."]
[10.006028175354004, 1.473037838935852, "The Period of the FASat-Alfa Satellite is 98.7 minutes."]
[7.91067361831665, 9.062212944030762, "The Nadir Resolution of the OLS Imaging Sensor is 0.55 km in the VIS range."]
[7.848835468292236, 7.497959136962891, "The Purpose of the ASIM Observation Instrument is Shed more light on the lightning phenomena."]
[7.123216152191162, -0.032867372035980225, "The End of Life Date of the Badr-B Satellite is 2 years."]
[5.9528727531433105, 1.8011958599090576, "The Launch of the Spacecraft Satellite is H-IIA launch vehicle from TNSC."]
[8.898642539978027, 8.191102027893066, "The Function of the Mirror Calibration Component is Reflects cold 2.7 K cosmic background radiation into the feedhorn."]
[7.943904399871826, 4.010512351989746, "The Thickness of the Carbon Dioxide Ice Patch Surface Feature is 9 cm."]
[5.121512413024902, 3.0350027084350586, "The Satellite Integrator of the SORTIE CubeSat is COSMIAC."]
[8.780665397644043, 6.944881439208984, "The Quantity of the Magnetometer Sensor is 3 units."]
[8.188302040100098, 5.350428104400635, "The Purpose of the GEOTAIL Satellite is 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."]
[5.857248783111572, 5.303443908691406, "The Hardware Paths of the IRNSS Navigation Signal Signal is Main and redundant."]
[8.397784233093262, 9.710906982421875, "The Modes of the HRV Imager is Panchromatic (PAN) mode and Multispectral (MS) mode."]
[11.643239974975586, -1.2691235542297363, "The Mass of the Total Satellite is 7.49 kg."]
[4.402713298797607, 7.775073051452637, "The Center Frequency of the Channel 3 Sensor is 23.8 GHz."]
[9.64979362487793, 8.101922035217285, "The Scintillation Module Size of the Natalya-2M High energy radiation spectrometer is 4.5 cm x 8 cm x 36 cm."]
[4.931445121765137, 1.7267812490463257, "The Science Objectives of the THEMIS Satellite Constellation is Onset and evolution of the macroscale substorm instability, production of storm-time MeV electrons, control of the solar wind-magnetosphere coupling."]
[8.508699417114258, 10.495307922363281, "The Pixel Scale of the Detector E2V CCD-22 (Frame Store) is 4.13 arcsec/pixel."]
[4.822200775146484, 0.87895667552948, "The Total system cost of the WorldView-4 Satellite is $850 million."]
[8.871232032775879, 10.745835304260254, "The Spatial Resolution of the WFC CCD Camera is 125 m."]
[7.274059772491455, 10.156978607177734, "The Data Downlink Time from Larger Platforms of the HyperScout 1 Hyperspectral Imager is Several hours."]
[5.139250755310059, 4.406441688537598, "The Connectivity of the Ground Operations Networks Communication Networks is 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."]
[7.452335834503174, 8.123040199279785, "The Altitude Range of the Thermosphere Atmospheric Layer is 90 \u2013 1000 km."]
[9.803190231323242, 1.3513237237930298, "The Duration of the Computer System Payload is 10 hours."]
[7.987867832183838, 2.0600531101226807, "The Total Stationkeeping Cost of the ISEE-3 Spacecraft is ~30 m/s."]
[10.566924095153809, 3.3857574462890625, "The Closest Approach Distance of the GRACE Satellites Satellite is 406 meters."]
[9.66982650756836, 8.063775062561035, "The Signal Threshold of the GMOD Detector is 10 sigma."]
[4.719832420349121, 6.543766021728516, "The Nominal Input Level of the Antenna Communication System is Unknown."]
[8.22929573059082, 5.8806962966918945, "The Telescope Size of the ASTERIA Satellite is 2.4-inch (6-centimeter)."]
[9.242476463317871, 10.477909088134766, "The Calibration of the PIANO Airglow Camera Camera is Pre-Flight."]
[9.794803619384766, 5.304290294647217, "The Propulsion Subsystem of the AOCS Attitude and Orbit Control System is Cold gas propulsion subsystem and magnetic torquers."]
[4.031659126281738, 10.350545883178711, "The NE\u0394T (K) of the ICI-1 Radiometer is 0.6."]
[7.250918388366699, 6.11596155166626, "The URL of the Case studies of aerosol retrievals Study is http://glory.giss.nasa.gov/publications/2002_JAS_59_383.pdf."]
[8.348243713378906, 10.443646430969238, "The Pixel Size of the 4-band CCD Imager Instrument is 10 x 10 \u00b5m."]
[6.053067207336426, 0.6204392313957214, "The Launch Date of the CANYVAL-X CubeSats CubeSats is 12 January 2018."]
[11.400230407714844, 2.2499494552612305, "The Altitude at Touchdown of the Hayabusa-2 Spacecraft is 8.5 m."]
[8.067469596862793, 3.8506886959075928, "The Ice Cover of the Landsat 8 Satellite is 82 percent."]
[10.521867752075195, 3.186444044113159, "The Range of the Unit Communication System is 75000 km."]
[7.484365940093994, 8.221471786499023, "The Altitude Range of the Nitric Oxide VMR Measurement Device is 80 - 120 km."]
[4.1374077796936035, 7.169528484344482, "The Mass of the Miniaturized X-band transponders Communications System is < 0.300 kg."]
[6.868719577789307, 1.0865812301635742, "The Conference Date of the MTG Satellites Satellite is June 22-24, 2010."]
[3.1328511238098145, 5.200745105743408, "The Capacity of the UPM-1T card Mass Memory is 800 Gbit."]
[5.411253452301025, 4.589813709259033, "The Ground Stations of the HYPSO-1 Satellite is NTNU Trondheim."]
[9.551795959472656, 1.6312822103500366, "The Revisit Time of the Sentinel-2 satellites Satellite is 5 days."]
[8.896941184997559, 2.987121343612671, "The Unknown of the Lunah-Map Spacecraft is Unknown."]
[9.7315673828125, 1.2808246612548828, "The Orbit Synchronization Time of the Observatories Satellite is About 2 months after launch."]
[2.3606584072113037, 4.524530410766602, "The Power Consumption of the Cospas-Sarsat search and rescue package Device is 3% of onboard power."]
[4.949517726898193, 2.4363853931427, "The Data Downlink of the AAUSat-1 CubeSat is Limited amount."]
[8.133413314819336, 4.0425496101379395, "The Dimensions of the Iceberg B-22A Iceberg is 71 km by 45 km."]
[7.716036319732666, 8.56258487701416, "The Dust Measurement Particle Size of the UVS Instrument is 100 nm."]
[8.300374031066895, 0.04969584569334984, "The Decommissioned Status of the Pirs ISS Module is True."]
[9.937331199645996, 1.568313479423523, "The Majority Pass Time of the GNOMES-1 Satellite is Over 400 seconds."]
[4.629533290863037, 3.427332639694214, "The Number of Research Facilities of the JEM Module is 2."]
[12.14535140991211, 5.385727882385254, "The Dark Matter Percentage of the Universe Cosmology is 25 percent."]
[5.876857757568359, 6.770753860473633, "The Range Direction Beam Steering of the SIR-C Radar System is 123\u00ba."]
[8.273460388183594, 10.136395454406738, "The MS of the Pushbroom imager GSD is 5.8 m."]
[7.228210926055908, 0.3336203098297119, "The Launch Date of the ZY 1-02C Spacecraft is Dec. 22, 2011."]
[8.368703842163086, 2.761289596557617, "The Purpose of the Joint Polar Satellite System (JPSS) Satellite System is Collection of global multi-spectral radiometry and other specialized meteorological and oceanographic data."]
[6.975811004638672, 2.4667110443115234, "The URL of the ESTCube-1 Satellite is http://icubesat.files.wordpress.com/2012/06/icubesat-org-2012-c-1-3-_presentation_noorma_201205301151.pdf."]
[7.847570419311523, 9.715598106384277, "The Number of Pixels of the Band 4 Spectral Band is 800."]
[9.22107982635498, 3.231116771697998, "The Orbit Type of the Alba Cluster 3 Satellite Cluster is SSO (Polar)."]
[4.015188217163086, 6.505312919616699, "The Bandwidth of the RF communication subsystem Communication is 20 kHz."]
[6.679380893707275, 8.267773628234863, "The Minimum Optical Pulse Duration of the LI Instrument is 0.6 ms."]
[9.318528175354004, -0.4667406678199768, "The Communication Protocol of the NEMO-AM Satellite is SFL's nanosatellite protocol."]
[5.780784606933594, 2.812540054321289, "The Developer of the SATTLA-2 PocketQube is Ariel University (Israel)."]
[9.769311904907227, 8.442631721496582, "The Imaging Purpose of the Deployable Membrane Telescope Telescope is Narrow-band imaging of the sun's chromosphere."]
[7.884142875671387, 0.8694912195205688, "The Launch Date of the Landsat-8 Satellite is 2013."]
[8.25696086883545, 0.26846423745155334, "The Prototype Duration of the CIMON Astronaut Assistant is 2 July 2018 to 27 August 2019."]
[9.021031379699707, 9.508965492248535, "The Aperture Diameter of the Pushbroom imager Optics is 200 mm."]
[5.564684867858887, 6.065081596374512, "The Ka-band Frequency of the SARAL/AltiKa Satellite is 35.75 GHz."]
[2.1944165229797363, 4.391845226287842, "The Total Energy of the Station Keeping Satellite Maneuver is Roughly half the amount needed for initial orbit raising."]
[8.012429237365723, -0.6988298892974854, "The Launch Date of the Crew Dragon Spacecraft is 15 September 2021."]
[8.259798049926758, 4.527240753173828, "The Swath Width of the TeLEOS-1 Satellite is 12 km."]
[6.801024913787842, 2.395453929901123, "The URL of the Chinese satellite Satellite is http://www.nature.com/news/chinese-satellite-is-one-giant-step-for-the-quantum-internet-1.20329."]
[11.214821815490723, 2.8710153102874756, "The Size of the Boulder Geological Feature is 10 m-wide."]
[4.685364246368408, 1.7244828939437866, "The Constellation Size of the NewSat Satellite is 38 operating satellites."]
[9.373189926147461, 5.865329742431641, "The Operational Modes of the ACS Attitude Control System is Momentum biased stabilization, Nadir optimized pointing, Fixed scan angle."]
[2.308804512023926, 4.432762622833252, "The Average Power Consumption of the Satellite Satellite is 580 W."]
[13.80688762664795, 0.7674739956855774, "The Orbital Slot of the GSAT-0101 Satellite is B05."]
[6.4388346672058105, -0.6958037614822388, "The Bus Design of the QZS-1 Satellite is ETS-8 (Engineering Test Satellite-8) heritage."]
[6.418492317199707, -0.7028457522392273, "The Signal Frequencies of the QZS Satellite is L1-band, L2-band, L5-band, E6-band."]
[5.420633792877197, 5.9076619148254395, "The Sampling Rate of the GPS/MET GPS Receiver is 50 times per second."]
[8.273569107055664, 7.351245403289795, "The Unknown of the Auroral Particle Instrument Instrument is Unknown."]
[8.88061237335205, 8.881897926330566, "The Filter Thickness of the NUV channel Spectrometer is 3.00 mm."]
[11.319080352783203, 3.9106719493865967, "The Transit Duration of the KELT-11b Planet is Eight hours."]
[7.417511463165283, 10.109868049621582, "The Detector Array Size of the HySI Hyperspectral Imager is 512 x 512 pixels."]
[7.991713047027588, 9.938342094421387, "The Channel Spectral Widths of the IIR Imager is 0.9 \u00b5m, 0.6 \u00b5m, 1.0 \u00b5m."]
[8.337785720825195, 3.5086193084716797, "The Trajectory Phases of the EQUULEUS Satellite is Science phase, forward transfer phase, backward transfer phase."]
[7.783356189727783, 5.950047969818115, "The Step 2 Operation of the TRUTHS Satellite is HIS (Earth Radiance view) calibrated against the TR at each LD wavelength."]
[10.371438980102539, 3.2046327590942383, "The Altitude of the Computer System Payload is 90,000 feet."]
[9.65190315246582, -0.6684061288833618, "The Design Presentation Proceedings Page Numbers of the Microsatellites Satellite is pp. 20-33."]
[7.12722635269165, 4.828315734863281, "The Topic of the SCISAT Satellite is Ozone depletion."]
[7.211132049560547, 2.6807796955108643, "The URL of the NovaSAR-1 Satellite is http://www.eotechcluster.org.uk/eotechcluster/documents/novasar-overview-for-rspsoc-sep12.pdf."]
[7.497335910797119, 7.319729804992676, "The Calibration Function of the GMI Radiometer Radiometer is Transfer standard for the other radiometers of the GPM constellation."]
[9.278316497802734, 0.8947474956512451, "The Mission Life of the Telescope Optical Instrument is 11 years for fuel."]
[9.365044593811035, 8.826029777526855, "The Max Frame Rate of the Telescope Optical Instrument is 232 Hz."]
[10.42940902709961, 4.689248085021973, "The Time to Refill the Plenum back to 95% of the Thruster Propulsion System is Approximately three seconds."]
[11.493579864501953, 3.834824323654175, "The Existence Period of the Ichthyosaurs Marine Reptiles is 250 and 90 million years ago."]
[5.836317539215088, 8.658473014831543, "The Instrument Mass of the MWHS-II Microwave Humidity Sounder is 60 kg."]
[9.023669242858887, 10.548423767089844, "The Spatial Resolution of the EXI Camera is Better than 8 km."]
[6.11077880859375, 6.672536373138428, "The Data Collection Duration of the LPR Radar is 2 days."]
[4.190176486968994, 6.584185600280762, "The Narrow Band Mode of the Receiver Communication System is \u00b1 6.0 kHz (-1 dB)."]
[6.905815601348877, 4.261150360107422, "The Mission of the MTG-I Satellite is Imaging."]
[3.520899534225464, 6.285569190979004, "The Front-End Filters Bandwidth of the TOTEM SDR SDR Platform is 10 MHz."]
[2.0248935222625732, 4.5458598136901855, "The Power Voltage of the PM Satellite Component is 120 V DC."]
[8.893290519714355, 7.4227166175842285, "The Measurement Objective of the Potential Equipment Set is Measure neutral and charged particles in the ionosphere."]
[7.086112022399902, 9.67425537109375, "The Band 2 of the RBV Instrument Spectral Band is 0.58 - 0.68 \u00b5m."]
[10.648100852966309, 3.8615710735321045, "The Temperature of the Nearside Hemisphere Moon's Hemisphere is Hotter than that of the farside."]
[11.511083602905273, 4.779898166656494, "The Rotation Period of the Pulsars Neutron Stars is Every few milliseconds to seconds."]
[9.37070369720459, 7.899139881134033, "The Cooling Temperature of the QWIP Detector Detector is 150 K."]
[5.147674560546875, 2.5672607421875, "The Position of the Inmarsat S \u2013 Europasat / Hellas-Sat 3 Satellite is 39\u00b0 East."]
[9.030936241149902, 4.78814697265625, "The Orientation of the Solar Panels Satellite Component is Perpendicular to the sun direction."]
[11.723694801330566, 3.374432325363159, "The Definition of the Solar Phase of Apsides Angle Orbital Parameter is The angle between the line of apsides projected into the ecliptic plane and the Earth-Sun line."]
[9.453124046325684, 1.76240873336792, "The Tracking Station Passes of the Odin Satellite is 10 per day."]
[10.515195846557617, 1.4456232786178589, "The Lander Touchdown Time of the MarCO-B Satellite is 11:54 am, November 26th, 2018."]
[1.1831822395324707, 4.1508002281188965, "The Battery Type of the SENSE Satellite is Li-Ion."]
[9.791007995605469, 5.518118858337402, "The Planning Window Length of the RASP Maneuver Planning System is 240 minutes."]
[6.733913898468018, 4.856521129608154, "The Purpose of the Land Information System Software is Integrate satellite and ground-based data using advanced mathematical techniques to improve performance of weather and climate computer models."]
[9.489419937133789, 0.46044987440109253, "The Age of the FengYun-1C Satellite is Modern."]
[6.365004062652588, 1.388068675994873, "The Operational Concept of the PRISMA Satellite is Servicing a variety of experimental teams for the flight demonstration of formation flying technologies."]
[7.705331325531006, 2.489812135696411, "The Authors of the Rosetta Satellite is 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 Depp."]
[7.685786247253418, 1.5700585842132568, "The Development Start Date of the SMOS Satellite is 1992."]
[7.742217540740967, 7.193120956420898, "The Optical Path of the TEMPO Instrument is Yellow arrows through the block diagram."]
[9.543573379516602, 4.264846324920654, "The Usable Volume of the Galaxy Spacecraft is 16.7 m3."]
[6.831745624542236, 9.098694801330566, "The Size of the HawkEye Ocean Color Instrument is 10 x 10 x 10 cm."]
[9.741423606872559, 1.551960825920105, "The Repeat Cycle of the SEOSAT-Ingenio Satellite is 38 days."]
[3.923219680786133, 5.374654769897461, "The Realtime Storage of the Telemetry Data Transmission is Managed during the descent phase."]
[8.897790908813477, 7.329812049865723, "The Surface Area of the CSS Coarse Sun Sensor is 2 cm2."]
[4.836755275726318, 2.145653247833252, "The Quantity of the LightSail CubeSat CubeSat is 1 of 10."]
[2.040156364440918, 4.035367488861084, "The Power Source of the Psyche Spacecraft is Solar Arrays."]
[7.1721510887146, 4.418878555297852, "The Technical Specification of the Vegetation-2 Instrument is Identical to Vegetation flown on SPOT-4."]
[6.733556270599365, 8.486056327819824, "The Resolution of the MERSI-RM Radiometer is 500 m."]
[5.5636773109436035, 0.4619942307472229, "The Drought Percentage of the U.S. Drought Monitor Report is 99 percent."]
[9.539813995361328, 9.011421203613281, "The Telescope Focal Length of the ASTRO-H Mission is 5.6 m."]
[7.277810573577881, 1.0497628450393677, "The Funding Period of the AIM spacecraft Satellite is Through September 2018."]
[2.950225353240967, 6.5685715675354, "The Power of the DC Power Communication System is 12.7 W conditioned power (transmit)."]
[11.610566139221191, 6.004526138305664, "The Duration of Brightness Change of the X-ray Source Celestial Object is About five minutes."]
[9.602374076843262, 7.88201379776001, "The Energy Range of the ELENA Instrument is E ~20 eV up to E~5 keV."]
[6.071736812591553, 9.199403762817383, "The Mass of the MI Radiometer Radiometer is 139 kg."]
[1.375084400177002, 4.17172908782959, "The Battery Life of the Telemetry System System is Eight hours."]
[8.702113151550293, 10.612061500549316, "The Ground Resolution of the CCD Detector System Imaging System is 0.65 m."]
[8.575919151306152, 9.440535545349121, "The Sensitivity of the NIRSpec MIRI Optical Instrument is 560 nJy (10 \u03bcm, \u03c4 i =10,000 s, and \u03bb/\u0394\u03bb = 5)."]
[7.403390407562256, 6.695643424987793, "The Data Source of the MODIS Imaging Spectroradiometer is NASA EOSDIS LANCE and GIBS/Worldview."]
[9.514580726623535, 5.5785441398620605, "The Station keeping accuracy of the AOCS Attitude and Orbit Control System is Better than \u00b10.05\u00ba North-South/East-West."]
[8.516026496887207, 10.299873352050781, "The Detector of the DubaiSat-1 Satellite is CCD (Charged Coupled Device)."]
[7.019008159637451, 3.5806565284729004, "The Orbit Evolution of the POPACS Satellite is Data."]
[1.9192026853561401, 3.9058237075805664, "The Type of the Solar Panels Power Generation is Silicon solar cells."]
[4.959963321685791, -3.106924533843994, "The Affiliation of the K. Kondo, A. Kuze, T. Hamazaki Individuals is Unknown."]
[6.258065223693848, 6.914796352386475, "The Polarization of the Satellite Device Unknown is V."]
[9.2393159866333, 4.1372785568237305, "The Dimensions of the WISA Woodsat Satellite is 10 x 10 x 10 cm."]
[8.271167755126953, 9.62751293182373, "The Number of Detector Pixels of the Short Wavelength Band Spectrometer is 512 x 512."]
[2.9657483100891113, 6.734190464019775, "The Power of the S-band Transmitter Transmitter is 1 W."]
[9.149002075195312, 10.518038749694824, "The Spatial Resolution of the LWIR Cameras Camera is 348 m."]
[13.18073558807373, 4.010337829589844, "The Actual Launch Date of the Gaia Satellite is December 19, 2013."]
[2.1573455333709717, 3.9119791984558105, "The Technology of the ROSA Roll-Out Solar Array is Scalable solar power array."]
[9.242356300354004, 6.056509017944336, "The Power Consumption of the CMGs Attitude Control is 220 W."]
[5.846338272094727, 6.590224742889404, "The Boom Length of the L-band SAR instrument Instrument is 9-m."]
[3.501317024230957, 4.691244125366211, "The Speed of the ODHS Processor Module Onboard Data Handling System is Up to 200 MIPS."]
[7.400509357452393, 0.6576486825942993, "The Launch Date of the CLARREO Pathfinder Satellite is Late CY2022."]
[5.0743913650512695, 1.6730682849884033, "The Number of NMGU of the GIOVE-A Satellite is 1."]
[5.9527058601379395, 4.363343715667725, "The Provider of the DMSP Satellite is NOAA."]
[11.37495231628418, 6.4568986892700195, "The Description of the Model Scientific Model is Describes the gamma-ray emission of pulsars detected by Fermi and combines this information with three parameters that determine the pulsar emission."]
[8.210078239440918, 10.24089527130127, "The SNR of the PMC-2 Imagers Imaging System is 23~43 db for PAN and 25~43db for MS data."]
[11.666293144226074, -1.223504662513733, "The Mass (kg) of the SARLupe Satellite is 770."]
[8.924276351928711, 10.304729461669922, "The Control Interface of the Payload 2 CMOS Camera is I2C bus."]
[3.905292272567749, 4.332856178283691, "The Subsystem of the C&DH Command and Data Handling is Dedicated processor."]
[7.2945451736450195, 0.29587316513061523, "The Launch Date of the ARIEL Satellite is 2029."]
[5.035414695739746, -2.370598554611206, "The Affiliation of the Frank Preud'homme Engineer is Unknown."]
[6.332849025726318, 6.3109450340271, "The Data Availability of the Copernicus Sentinel-6 Poseidon-4 Radar Altimeter is Now."]
[5.7903265953063965, 5.050429821014404, "The Ground SAR Image Processor of the X-band SAR payload system Payload System is Included."]
[7.261993885040283, 7.876286506652832, "The Earth Scanning Time (LAC scenario) of the Instrument Satellite Instrument is 2.5 minutes."]
[8.597463607788086, 10.505514144897461, "The Detector Pitch of the FLIR Boson camera Thermal Imaging Camera is 12 \u00b5m."]
[9.121471405029297, 0.9980769753456116, "The Operation Duration of the LIMS Instrument is About 9 months."]
[4.907527446746826, 6.167727947235107, "The Frequency (MHz) of the Galileo E5a Signal Carrier is 1176.45."]
[6.064507961273193, 6.1672043800354, "The Repeat Cycle of the TecSAR SAR is 36 days."]
[4.50944709777832, 4.343595027923584, "The Integration Status of the Electronics Module Subsystem is Ongoing."]
[11.46937370300293, 5.227073669433594, "The Understanding of the Galactic Cosmic Rays Cosmic Phenomenon is Remains poorly understood and controversial."]
[11.739835739135742, 1.6782134771347046, "The Last Signal Date of the Philae lander Lander is 9 July 2015."]
[8.181496620178223, 1.130582571029663, "The Capture Date of the Image Data is 26 October 2019."]
[11.541343688964844, -1.2685675621032715, "The Maximum Mass of the Lunar Flashlight 6U CubeSat Satellite is 14 kg."]
[11.655061721801758, 4.405176639556885, "The Velocity of the Zeta Puppis Star is About 60 km/s."]
[8.046210289001465, 9.681748390197754, "The MWIR Band Wavelength Range of the OHIS Imaging System is 3.0 - 5.0 \u03bcm."]
[7.504997730255127, 7.870437145233154, "The Proportional Function of the Extinction Atmospheric is exp(\u2013\u03c4(\u03bb))."]
[8.583928108215332, 10.703475952148438, "The Average Power of the LWIR Camera Camera is 13 W."]
[8.414645195007324, 9.75541877746582, "The Resolution of the PAN Imaging System is 0.65 m."]
[9.329485893249512, 0.9510847330093384, "The Operations Budget of the Small space mission Mission Type is May have long since been exhausted at end of mission."]
[4.764873027801514, 1.9931614398956299, "The Quantity of the SpaceBEE Satellite is 12."]
[8.162755966186523, 5.6622819900512695, "The Noise in NIR Channel of the R3 System Satellite is Noticeable."]
[6.64616060256958, 2.5477113723754883, "The URL of the FalconSat-7 Satellite is http://www.usafa.edu/df/dfe/dfer/centers/lorc/docs/FalconSAT07.pdf."]
[8.560845375061035, 9.045795440673828, "The Pointing Angle of the FUV Instrument Spectrometer is 20\u00ba down towards nadir from the -Y axis."]
[6.386765480041504, 1.6349564790725708, "The Launch Date of the Jason-3 Satellite is January 17, 2016."]
[7.287141799926758, 5.287043571472168, "The Survival of the Bdelloids Species of Rotifers is Can survive year-long droughts in the Sahara desert as well as in the frozen plains of Antarctica."]
[4.105344295501709, 4.335201740264893, "The Software of the OBC On-Board Computer is FOS (Flight Operations Segment)."]
[6.243359565734863, 3.2286622524261475, "The Formation of the B612 Foundation Organization is Unknown."]
[4.8398261070251465, 1.6957448720932007, "The Number of Profiles of the FormoSat-3/COSMIC-1 Satellite Constellation is 10 million."]
[9.598772048950195, 1.518852949142456, "The Coverage Repeat Period of the S/C Satellite is 5.5 days."]
[2.531125545501709, 4.381397247314453, "The Power Interface of the ESEO-TriTel EQM Satellite Instrument is TriTel PS (Power Supply) board."]
[7.929274082183838, 5.675343036651611, "The Effect of the SAA South Atlantic Anomaly is Causing technical disturbances in satellites."]
[11.813166618347168, -1.1501884460449219, "The Launch Mass of the IRNSS-1C Satellite is 1425.4 kg."]
[9.14616870880127, 3.1889398097991943, "The Orbit Type of the OrbView-2 Satellite is Sun-synchronous polar circular orbit."]
[8.450139999389648, 7.467779159545898, "The Search Coil Mass of the ULF Sensor Sensor is 2 kg."]
[3.841233730316162, 5.140386581420898, "The Interface Type of the FODB Data Interface is Fiber Optic."]
[9.71208381652832, 3.043308973312378, "The Earth Parking Orbit of the Chandrayaan-2 Spacecraft is 170 km x 45,475 km."]
[11.613101959228516, -1.231110692024231, "The Dry Mass of the HY-1C Satellite is 429 kg."]
[7.529708385467529, 0.9143959283828735, "The Status Update Date of the SeaWiFS Satellite is Feb. 5, 2010."]
[8.206555366516113, 10.312433242797852, "The Total Number of Spectral Bands of the MSU-100 Camera is 6."]
[9.491178512573242, 9.057242393493652, "The f/number of the Imaging Subsystem Telescope is 4."]
[7.887509346008301, 8.093670845031738, "The Purpose of the ARI Infrared Spectrometer is Optimize measurement of the long-term changes of Earth\u2019s atmosphere and surface."]
[3.5326404571533203, 6.667675971984863, "The Downlink Rate of the CPUT STX S-band Transmitter is Up to 2 Mbit/s."]
[4.533918857574463, 4.323573589324951, "The Features of the Control Units Satellite Component is A/D (Analog-to-Digital) converters."]
[6.046534538269043, 6.4016876220703125, "The Dynamic Range of the Instrument SAR is 35 dB."]
[4.174607753753662, 3.2121424674987793, "The Impact on NGSO Terminals of the 5G Network Telecommunication Network is Fewer than 1%."]
[1.4787228107452393, 4.962509632110596, "The Bus Voltage Regulation of the SBVR Power Supply is 100 V \u00b1 1 V."]
[5.029581546783447, 9.227542877197266, "The Quake Duration of the SEIS Seismometer is Unknown."]
[7.079526901245117, 3.0282068252563477, "The Development Team of the Microsized Microwave Atmospheric Satellite (MicroMAS) Satellite is 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."]
[11.551791191101074, -1.2163480520248413, "The Mass of the SRMSat Satellite is 10.9 kg."]
[7.67617654800415, 2.2441883087158203, "The Launch Date of the ELSA-d Mission is March 2021."]
[6.384300231933594, 1.587937593460083, "The Year of Launch of the Jason-1 Satellite is 2001."]
[9.881962776184082, 3.9977681636810303, "The Designers of the NanoSail-D2 Satellite is NASA/MSFC, NASA/ARC, ManTech/NeXolve Corporation."]
[2.212432622909546, 6.523155212402344, "The Latency of the ATL15 Antarctica/Greenland Ice Sheet dh/dt Gridded Data is 45 days from receipt of last data in product."]
[7.906421184539795, 1.8468860387802124, "The Halo Orbit Duration of the ISEE-3 Spacecraft is Nov. 1978 to June 1982."]
[7.180737018585205, 5.555081367492676, "The Monitoring Importance of the Ocean Acidification Environmental Phenomenon is Important for climate and environmental policy-making."]
[7.469180583953857, 0.5650267601013184, "The Launch Date of the GRACE Satellite Satellite is March 17, 2002."]
[8.380023002624512, 3.5737154483795166, "The Material of the JUICE Spacecraft is Non-magnetic material."]
[12.120156288146973, 3.2817587852478027, "The Orbit Inclination of the SEOSat Satellite is 98\u00b0."]
[4.522499084472656, 3.297490119934082, "The Transceiver of the SCARAB 1U CubeSat bus is AstroDev Helium-100 UHF/VHF transceiver."]
[5.471091270446777, 6.090382099151611, "The Antenna Direction of the GPS/MET GPS Receiver is Anti-velocity direction."]
[11.413188934326172, -1.3736718893051147, "The Mass of the HIT-Sat Satellite is 3 kg."]
[6.377940654754639, 10.074467658996582, "The Mass of the CCD Camera Imaging System is <55 kg."]
[7.035446643829346, 1.0094025135040283, "The Facilities Launch Date of the UK space industry Industry is July 9, 2015."]
[7.778829097747803, 4.260054111480713, "The Observation Target of the Aditya-1 Satellite is Solar corona."]
[5.441097259521484, 5.882551193237305, "The Band Frequency of the SARAL/AltiKa Satellite is Ka-band."]
[9.43106460571289, 1.4483999013900757, "The Data Acquisition Duration of the CERES on TRMM Instrument is 9 months."]
[2.22572922706604, 4.450158596038818, "The Power Supply of the GNB Satellite is 8 W peak and 5.6 W nominal."]
[8.59078311920166, 5.058901786804199, "The Components of the PCS separation system Satellite Separation System is Two spring loaded rings and a motorized release mechanism."]
[2.224259376525879, 4.293403148651123, "The Solar Array Power of the MarCO CubeSats Satellite is Approximately 35 W (at 1AU)."]
[11.630437850952148, 4.482977390289307, "The Wind Mass of the Massive Stars Stars is Equivalent of Earth\u2019s mass in a month."]
[7.840534687042236, 10.125492095947266, "The MS B3 of the Pushbroom imager Spectral Band is 0.62-0.69 \u00b5m."]
[7.583070278167725, 6.565973281860352, "The Typical Value of the BrO Satellite Instrument is 5 x 10 -2."]
[12.150944709777832, 5.386989593505859, "The Composition of the Normal Matter Cosmological Component is ~5%."]
[6.661509990692139, 4.394819736480713, "The Presenter of the CO2Image Demonstrator Presentation is Andre Butz."]
[9.914386749267578, 1.5086873769760132, "The Exchange Time with Interplanetary Space of the Exosphere Atmospheric Layer is Monthly time scale."]
[10.184341430664062, 4.956401824951172, "The Ion Electric Propulsion of the Electric Propulsion Test Subsystem Satellite Subsystem is Isp = 3000 s \u00b1 300 s."]
[10.483566284179688, -1.1321425437927246, "The Mass of the Lemur-2 Nanosatellite is 4.5 kg."]
[4.029394149780273, 2.3554129600524902, "The Design Standard of the Neutron-1 Satellite is 3U CubeSat standard."]
[10.057058334350586, 8.501296043395996, "The CCD Detector Assembly Cooling of the EUVI Extreme Ultraviolet Imager is Passively cooled by a radiator."]
[4.605696201324463, 6.10267448425293, "The Uplink Frequency of the CUTE-1.7+APD Satellite is L-band (1268.500 MHz)."]
[10.569507598876953, -1.0329843759536743, "The Mass of the TabletSat-Aurora Microsatellite is 25 kg."]
[2.315582036972046, 4.478410720825195, "The Power Off Period of the Spacecraft Satellite is Until Aug. 30."]
[6.772236347198486, 9.033537864685059, "The | of the HEPD Instrument is HEPD."]
[5.391145706176758, 1.3614839315414429, "The Falcon Rocket Landings of the SpaceX Company is 75."]
[4.200793266296387, 4.367054462432861, "The Components of the SHU Control and Data Handling Subsystem is 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)."]
[8.820213317871094, 9.422852516174316, "The Smile of the System Optical System is Less than 0.5 \u00b5m."]
[9.395796775817871, 9.993268966674805, "The Signal to Noise Ratio of the APD Optical Radiation Detector is Good at room temperature."]
[3.2981605529785156, 5.039973258972168, "The Volume of the OSDP Onboard Signal Data Processor is 0.024 m3."]
[11.212478637695312, 2.94747257232666, "The Basalt Flows Fill Time of the Von K\u00e1rm\u00e1n crater Lunar Crater is ~3.35 Ga."]
[1.1595711708068848, 4.185970306396484, "The Battery Configuration of the Canopus Pipper Satellite is 1S4P."]
[9.49216365814209, 1.1829137802124023, "The Schedule of the NPOESS Satellite Program is Further delays."]
[4.13336706161499, 1.32335364818573, "The Mission Type of the PSat-2 CubeSat is Non-EO."]
[10.98861026763916, 6.351423740386963, "The Energy Loss of the Neutron-Hydrogen Collisions Particle Interaction is About half its energy."]
[7.904707908630371, 9.026883125305176, "The Cadence of the LET-Spectra Measurement is In the range 0.1-430 keV/\u00b5m."]
[7.527804851531982, 6.802185535430908, "The Testing of the TEMPEST-D Radiometer Instrument is Passed."]
[9.454017639160156, 5.475770950317383, "The Anomaly of the EAIM Subsystem is Occurred on the wheels command of satellite attitude control."]
[5.913952827453613, 2.9203238487243652, "The Manufacturer of the Landsat 9 Satellite is NASA."]
[8.889811515808105, 1.1729997396469116, "The Life Extension of the ESA's science missions Satellite is Extended."]
[6.724393844604492, 8.866960525512695, "The Standard Interface of the CEASE-2 Instrument is RS-422 or MIL-STD-1553B."]
[5.910524368286133, 3.153049945831299, "The Provider of the STM Sensor is MSSL (Mullard Space Science Laboratory) of Belgium."]
[4.780696392059326, 5.615902423858643, "The Radio Type of the SENSE Satellite is S-band."]
[7.2739577293396, 1.5601717233657837, "The Mapping Completion Date of the ERS-1 Satellite is March 1995."]
[3.849353790283203, 2.3027679920196533, "The Size of the ZACUBE-1 CubeSat is 1U."]
[8.63565444946289, 1.827560544013977, "The Attachment of the CALET Telescope is JEM-EF (Japanese Experiment Module Exposed Facility), Port #9."]
[6.543134689331055, 3.861999750137329, "The Digital Subsystem of the SCATSat-1 Satellite is Redesigned leveraging some of the recent efforts that have resulted in a smaller form factor for the digital system."]
[6.765558242797852, 2.547528028488159, "The URL of the RADARSAT Constellation Mission Satellite is http://www.asc-csa.gc.ca."]
[9.518453598022461, 0.4406861662864685, "The Design Lifetime of the RTAFSAT-1 Satellite is 3 years."]
[3.290696859359741, 5.3161773681640625, "The On-board data storage of the First DMC generation Satellite is SSDRs (Solid State Data Recorders) capable of storing up to 1.5 GByte of imagery."]
[10.51009750366211, 7.549158573150635, "The Nozzle Material of the Propulsion System Satellite Component is Aluminum."]
[8.608796119689941, 6.944950103759766, "The Detection Threshold of the DICE body-mounted magnetometer Magnetometer is >100 nT."]
[7.316415309906006, 8.759588241577148, "The Visible/Reflected Channels of the AATSR Imaging Radiometer is 0.55, 0.66, 0.87 \u03bcm."]
[4.046579360961914, 1.191956639289856, "The Mission Type of the LunIR Satellite is Non-EO."]
[7.91465425491333, 7.259908676147461, "The Design and Pre-Flight Characterization of the TRUTHS Reference Sensor is Will be optimized to fully utilize the benefits."]
[6.0522565841674805, 4.851100921630859, "The Orbit Determination Data Source of the WEOS Satellite is Onboard GPS receiver, TLE sets provided by NORAD."]
[9.501445770263672, 5.670612812042236, "The Attitude Stability of the AOCS Attitude Control System is <0.003\u00ba/s."]
[7.858428001403809, 4.454737663269043, "The Experiment Pointing System of the ATLAS-1 Satellite Mission is Orbiter."]
[6.578899383544922, 2.3840110301971436, "The URL of the Eutelsat Quantum Satellite is https://www.esa.int/Applications/Telecommunications_Integrated_Applications/Reprogrammable_satellite_is_ready_for_launch."]
[9.897271156311035, 3.9448039531707764, "The Image Shooting Date of the IKAROS Small Solar Power Sail Demonstrator is June 16, 2010."]
[6.075981140136719, 9.453946113586426, "The Mass Control Requirement of the Invar Material is Careful attention to mass control."]
[12.138556480407715, 3.285177230834961, "The Inclination of the OceanSat-1 Satellite is 98.28\u00ba."]
[4.995336055755615, 4.77427339553833, "The Network of the ATLAS Space Operations Ground Station is X- and S-band communications."]
[3.6937193870544434, 5.456353664398193, "The Raw Data Size of the QuakeSat Satellite is 500 MB."]
[9.231788635253906, 6.100439071655273, "The Activation of the Gyroscopes Attitude Control is Active."]
[6.517277717590332, 0.7098007202148438, "The Budget Lag Date of the ICESat Satellite is January 4, 2010."]
[8.546294212341309, 6.338175296783447, "The Mounting Method of the Propulsion Equipment Satellite Components is Mounted on a panel inside the launch adapter ring."]
[6.209025859832764, 4.909824371337891, "The X-band Synthetic Aperture Radar (SAR) of the CHORUS Satellite is ICEYE."]
[7.988295555114746, 7.572542667388916, "The Spectral Bands of the ROLO Robotic Lunar Observatory is 32."]
[7.678192615509033, 8.266456604003906, "The Altitude Measurement of the OMPS Sensor is Yes."]
[3.8218393325805664, 4.543179512023926, "The Model of the Processor Satellite Component is TEMIC TSC695 32-bit RISC processor."]
[10.21092414855957, 2.9949886798858643, "The Orbit Altitude of the Satellite Satellite is ~670 km."]
[1.856055736541748, 3.991673707962036, "The Cells in Series of the Solar Panels Power Source is 34."]
[8.362446784973145, 3.7299489974975586, "The Data Range of the SERVIR Program is Not entirely available through non-commercial entities."]
[9.317827224731445, 7.727818965911865, "The Temperature of the MIRIS Telescope is Around 200 K."]
[1.5316190719604492, 4.3947553634643555, "The Battery Charging System Design of the SpriteSat Satellite is Mistake."]
[9.216279029846191, 7.143060207366943, "The Measurement Range - Satellite Potential of the ISL Instrument Langmuir Probe is \u00b1 5 V."]
[8.161985397338867, 2.974428415298462, "The Design Basis of the Euclid Satellite is Experience gained with ESA\u2019s Herschel and Planck missions."]
[0.9584808945655823, 4.231198787689209, "The Battery Capacity of the Power Subsystem Subsystem is 7 Ah."]
[4.625319004058838, 2.8665292263031006, "The Onboard AI Processing Unit of the PhiSat-1 Satellite is Intel\u00ae Movidius\u2122 Myriad\u2122 2 Vision Processing Unit (VPU)."]
[9.850468635559082, 3.5853397846221924, "The Meteoroid Flux of the Lunar impact monitoring Monitoring System is Kilogram-sized."]
[9.448396682739258, 7.744019985198975, "The Energy Steps of the Electron Spectrometer Instrument is 24."]
[7.627255439758301, 4.898078918457031, "The Fault-tolerant satellite design of the BEESAT-1 Satellite is Yes."]
[5.7391486167907715, 3.5663487911224365, "The Location of the CSSS Canadian Space Surveillance System is 22 Wing in North Bay, Ontario."]
[3.571373224258423, 5.6570210456848145, "The Data Transport of the SPA-U Interface is USB 1.1 limited to 12 Mbit/s."]
[1.2737789154052734, 4.157808303833008, "The Li-ion Battery Capacity of the GNB Satellite is 5.3 Ah."]
[8.668899536132812, 1.9649457931518555, "The Project Status Presentation of the James Webb Space Telescope Space Telescope is Phil Sabelhaus, \"Project Status for the James Webb Space Telescope Partner's Workshop,\" JWST Partner's Workshop, Ottawa, Canada, May 19, 2009."]
[5.321747303009033, 3.2257487773895264, "The Tracking Area of the BeaverCube Satellite is Northeastern section of the US coast."]
[7.704061031341553, 4.345666408538818, "The Observation Capabilities of the TWINS Satellite is 3D spatial, energy, and pitch angle distributions of the terrestrial ring current (RC)."]
[10.279342651367188, 4.978001594543457, "The Thrusters of the Satellite Spacecraft is Micro-newton (\u00b5N) cold gas thrusters."]
[1.8980311155319214, 4.025601863861084, "The Thickness of the Solar Panels Power Source is Less than one millimeter."]
[11.410280227661133, 3.898780107498169, "The Liquid Core Diameter of the Mars Planet is Half the diameter of the planet."]
[6.705070972442627, 9.124895095825195, "The Base Dimensions of the CMS Instrument is 380 mm x 315 mm x 186 mm."]
[5.481897354125977, 4.390529632568359, "The Function of the CASPER Autonomy Software Component is Replan activities, including downlink, based on science observations in the previous orbit cycles."]
[8.837210655212402, 8.039067268371582, "The Thermal Control of the UVNS Spectrometer is Passive cooling to ensure that temperature conditions are adapted to the different requirements of the instrument modules."]
[9.009918212890625, 1.1064610481262207, "The Exploration Mission Duration of the LRO Satellite is 9/16/2009 - 9/16/2010."]
[5.850998401641846, 2.8973636627197266, "The Manufacturer of the Landsat-9 Satellite is Northrop Grumman."]
[0.9365378618240356, 4.177387714385986, "The Capacity of the Lithium-ion Polymer Batteries Energy Storage is 1.2 Ahr."]
[5.720261096954346, 3.0452158451080322, "The Manufacturer of the Payload Satellite Component is EADS Astrium Ltd. and partners."]
[8.046195983886719, 1.0726690292358398, "The Image Capture Date of the Landsat-8 Satellite is May 30, 2021."]
[6.037336349487305, 0.6799044609069824, "The Presentation Date of the Xatcobeo CubeSat is May 12-14, 2010."]
[10.334593772888184, 4.974565505981445, "The Manufacturer of the Safran/Snecma PPS-5000 Electric Propulsion is Safran/Snecma."]
[10.975101470947266, 4.9053778648376465, "The Effect of the Clusters Solar Phenomenon is Generates an enhanced particle acceleration compared to the isolated plasma cloud."]
[12.119050979614258, 2.2702975273132324, "The URL of the OSIRIS-REx Spacecraft is https://earthobservatory.nasa.gov/IOTD/view.php?id=91494&src=iotdrss."]
[7.58460807800293, 2.21994686126709, "The Copyright of the eoPortal Website is \u00a9 2024."]
[7.716296672821045, 13.615994453430176, "The Passband Range of the SPIM5 Spectrometer is 589-902 nm."]
[2.2038733959198, 3.8394384384155273, "The Solar Array of the KOMPSAT-6 Satellite is Fixed solar array with one deployable wing."]
[4.5496063232421875, 4.0631818771362305, "The Data Bus of the Payload Satellite Payload is LEON II FT MIL-STD-1553, CAN, SpaceWire."]
[6.103495121002197, 9.565203666687012, "The Sulfur Dioxide Content of the Dobson Unit Unit of Measurement is 0.0285 grams of sulfur dioxide/m2."]
[9.631295204162598, 4.185427665710449, "The Cone Structure Length of the COMMx Payload is ~1.85 m."]
[9.390130996704102, 1.5636199712753296, "The Global Surface Temperature Data Recording Time of the Sentinel-3B Satellite is Less than 0.9 days at the equator and in less than 0.8 days in latitudes higher than 30\u00ba."]
[9.296202659606934, 8.202091217041016, "The Data Rate of the RAMIS Radiation Detector is 10 MB / day."]
[6.950858116149902, 2.493396043777466, "The URL of the Dellingr Satellite is https://www.nasa.gov/feature/goddard/2017/nasa."]
[8.59997844696045, 6.832852840423584, "The | of the Fluxgate magnetometer Instrument is Fluxgate magnetometer."]
[8.146934509277344, 5.573334217071533, "The Accuracy of the Ion & Electron Temperature Satellite System is < 20% (\u03c1 >10 10  m -3 )."]
[8.642513275146484, 6.264599323272705, "The Relationship with Plasma Density of the Plasma Drifts Phenomenon is 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."]
[1.1360055208206177, 4.307345390319824, "The Battery Type of the EPS Electric Power Subsystem is Lithium-ion."]
[4.899625301361084, -3.254990577697754, "The | of the Claire Pettersen Individual is Fred A. Best, Douglas P. Adler, Claire Pettersen, Henry E. Revercomb, P. Jonathan Gero, Joseph K. Taylor, Robert O. Knuteson, John H. Perepezko."]
[5.097183704376221, 7.07844352722168, "The Diameter of the IOL Antenna Reflectors Antenna is 2.85 m."]
[6.977279186248779, 0.2578903138637543, "The Launch Date of the ASTROSAT Space Observatory is Sept. 28, 2015."]
[8.55514907836914, 6.822821617126465, "The Measurement Method of the OVM Overhauser scalar magnetometer is Proton Larmor precession in a weak magnetic field."]
[6.548334121704102, 5.364479064941406, "The Modes of the TerraSAR-X NG Satellite is Very high-resolution modes, heritage modes, wide swath modes."]
[7.992930889129639, 9.104146957397461, "The Spectral Signature of the Osprey Sample Collection Site is Carbon-rich material."]
[7.2176337242126465, 4.324532985687256, "The Instrument Type of the SPOT-5 Satellite is Imaging multi-spectral radiometers (vis/IR), High resolution optical imagers, Precision orbit."]
[7.237135410308838, 2.702644109725952, "The Conference Location of the NovaSAR-1 Satellite is University of Greenwich, London, UK."]
[8.916172981262207, 6.963204860687256, "The Sensitivity of the Instrument Photometer is Detects an Earth-size transit of an mv=12 G2V star at 4 \u03c3 in 6.5 hours of integration."]
[8.936230659484863, 2.1607043743133545, "The Observation of the New Horizons Spacecraft is Variations in particle fluxes over a wide range of energies and scales."]
[7.838415622711182, 9.174677848815918, "The Spectral Range of the HSC Spectrometer Spectrometer is 450-1000 nm."]
[2.2889251708984375, 6.4773101806640625, "The Latency of the ATL02 Science Unit Data is 2 days."]
[7.449971675872803, 4.261585712432861, "The Imaging Mission of the SSOT Satellite is High-resolution."]
[11.807683944702148, 2.981750011444092, "The Orbital Inclination of the Swarm-A (Alpha) Satellite is 87.4\u00ba."]
[6.8627848625183105, 0.6277129054069519, "The Year of Launch of the SORCE Satellite is 2003."]
[8.387892723083496, 9.808359146118164, "The Mapping Resolution of the EIS Imaging System is 330 feet (100 m) per pixel."]
[3.9814047813415527, 5.866069793701172, "The Data Volume of the Ground Segment Communication System is 750 Mbit per orbit."]
[9.97619342803955, 1.446203351020813, "The Period of the ANUSat Satellite is ~90 minutes."]
[6.751769065856934, 0.9582680463790894, "The Test Date of the HEPS Satellite Component is Beginning of the second calibration and validation phase."]
[4.735989093780518, 2.0720441341400146, "The Mass of the Flock-4v Satellite is Not provided."]
[8.527291297912598, 6.406110763549805, "The Length of the Boom Assembly Assembly is 1.2 m."]
[8.231855392456055, 10.27883529663086, "The Integration Time of the PMC-2 Imagers Imaging System is 1~96 levels."]
[6.498891830444336, 1.2200655937194824, "The Milestones of the PRISMA Satellites Satellite is Two new milestones achieved."]
[6.810279369354248, 0.5758568644523621, "The Launch Date of the Sich-2 Satellite is April 17, 2007."]
[8.607430458068848, 6.938619136810303, "The Magnetic Impulse of the Ground-based sensors Sensor is Recorded."]
[6.946631908416748, 0.015787122771143913, "The End of Life Date of the FITSat-1 Satellite is 4 July 2013."]
[11.667071342468262, -1.23591148853302, "The Mass (kg) of the TerraSAR-X Satellite is 1230."]
[3.663581609725952, 6.330312728881836, "The Uplink Beacon Data Rate of the RF Communications Communication System is 20 bit/s."]
[9.531332969665527, 1.2916165590286255, "The LEOP Duration of the TeLEOS-1 Satellite is Two weeks."]
[7.928651809692383, 8.386401176452637, "The Number of Spectrometers of the SOLSPEC-SOLAR Spectrometer is 3."]
[5.194518089294434, 1.5493873357772827, "The Launch Vehicle Utilization of the PODSat Payload Delivery System is Excessive capacity on launch vehicles delivering a primary payload to geostationary orbit."]
[11.829426765441895, 3.0011940002441406, "The Orbital Inclination of the Swarm-C (Charlie) Satellite is 88\u00ba."]
[7.851528167724609, 9.751117706298828, "The Spectral Range of the Instrument Spectral Imager is 8.80-15.39 \u00b5m."]
[8.785310745239258, 8.501421928405762, "The Manufacturer of the TIR detector Detector is TNO, SSTL."]
[4.340445041656494, 6.465914249420166, "The Beacon Frequency of the RF Communication System Communication System is 436.8475 MHz."]
[8.456801414489746, 7.162793159484863, "The Dynamic Range of the FIELDS suite Sensor Suite is 140 dB."]
[8.797019958496094, 10.181563377380371, "The Susceptibility of the CMOS Sensors Sensor is SEU and latchup effects."]
[7.239455223083496, 5.676870346069336, "The Dissolved Inorganic Carbon of the Marine Chemistry Study Parameter is Unknown."]
[8.767406463623047, 8.975817680358887, "The Average Efficiency of the Grating Grating is Greater than 60%."]
[8.409982681274414, 4.721172332763672, "The Observation of the Cluster Satellite Constellation is Magnetic Reconnection Events."]
[12.625042915344238, 6.915450096130371, "The Pulse period (ms) of the B0540-69 Pulsar is 50.499."]
[10.369891166687012, 2.9590394496917725, "The Altitude in Orbit of the Electric Thruster Thruster is 410 km."]
[9.164652824401855, 7.449389934539795, "The Principle of the Sensor Gas Sensor is Amperometric three electrode principle."]
[11.639140129089355, 4.523404121398926, "The Shock Wave Speed of the Tycho Supernova Remnant is Millions of miles per hour."]
[7.459600448608398, 8.904473304748535, "The Swath Width of the OMI Spectrograph is 2600 km to 725 km."]
[10.2907075881958, 5.157423973083496, "The Regulated Pressure of the EPTA Electric Propulsion Thruster Assembly is 2.2 bar."]
[7.977242469787598, 0.990451455116272, "The Press Release Date of the AgNeo Precision Agriculture Solution is 6 March 2020."]
[10.033051490783691, 1.4753961563110352, "The Period of the OrbView-2 Satellite is 98.2 minutes."]
[5.391208171844482, 1.5486881732940674, "The Serial Number of the Rocket 3.3 Rocket is LV0007."]
[3.599135637283325, 2.29071307182312, "The Size of the TEPCE Satellite is 3U."]
[8.367713928222656, 10.341521263122559, "The Spectral Data Utilization of the Focal Plane Camera Component is Less than 20%."]
[5.564933776855469, 3.8983819484710693, "The Use of the PREMOS Instrument is Entry point for GCM simulations."]
[5.237890243530273, 4.609918117523193, "The Communication Network of the Pl\u00e9iades-Neo satellites Satellite is EDRS (European Data Relay System)."]
[7.065293312072754, 1.8135632276535034, "The Age of the Tropical Rainfall Measuring Mission Satellite is 15 years."]
[8.939725875854492, 1.8181843757629395, "The Image Capture Date of the BepiColombo Spacecraft is 19 April."]
[8.678404808044434, 6.861523151397705, "The Magnetic Field Range of the iMTQ Magnetorquer is \u00b163 mT."]
[6.717060565948486, 4.757875442504883, "The Radar Altimeter System of the Envisat Satellite is RA-2."]
[4.492550373077393, 2.2337167263031006, "The Number of Operational Satellites of the Starlink Satellite Constellation is About 1,350."]
[11.234427452087402, 3.521824359893799, "The Geological Process of the 67P/Churyumov-Gerasimenko Comet is Mechanical shear stress."]
[8.540438652038574, 2.7966787815093994, "The Role of the Martin Popek Individual is His photographs are proving a very valuable to the team\u2019s research."]
[9.201111793518066, 7.875376224517822, "The Operating Temperature of the WFS&C Wavefront Sensing and Control Subsystem is < 45 K."]
[5.31788969039917, 9.60798454284668, "The Accuracy Assured Rate of the STOs and STAEs Analog Electronic units is 0.0608 \u00b1 0.0008\u00ba/s (H); 0.005\u00ba/s (V)."]
[8.304163932800293, 9.915572166442871, "The Array Size of the NIR Detector is 80 x 640."]
[10.495922088623047, 6.0976057052612305, "The Objective of the Micro-gravity experiment Experiment is Investigate the coupling between heat capillary convection and buoyancy convection, and other phenomena."]
[9.662281036376953, 1.6977897882461548, "The Observation Duration of the TESS Satellite is 27 days."]
[4.996477127075195, 1.8301540613174438, "The Number of Passes Over a Storm of the Weather Satellites Satellite is One or two in an entire day."]
[9.334920883178711, 0.49924659729003906, "The Exceeded Design Life of the EO-1 Satellite is Yes."]
[10.363908767700195, 3.6731584072113037, "The Deployment Velocity of the Dispensers Satellite Component is 1 to 2 m/s."]
[8.701461791992188, 8.896867752075195, "The Number of Sets of the HETG Grating is 2."]
[7.974515438079834, 10.029245376586914, "The Swath of the IIR Imager is 64 km x 64 km."]
[8.974069595336914, 2.488236427307129, "The Measurement of the Planck Telescope is Direction of the polarized light emitted by the dust."]
[5.19359827041626, 6.612548351287842, "The Antenna Type of the Antenna Reflector is Offset Feed Paraboloidal Reflector Antenna."]
[11.4496431350708, 4.023019790649414, "The Visibility of the Event Celestial Event is About 2,000 years."]
[10.363393783569336, 2.871713876724243, "The Altitude of the CeREs CubeSat Satellite is 500 km."]
[5.696896076202393, 9.217608451843262, "The Power of the FGM Instrument is 2..5 W."]
[4.2529425621032715, 2.559277057647705, "The Service Cost of the Starlink Satellite Internet Service is $99 per month."]
[8.698594093322754, 10.32606315612793, "The Optics Type of the LISS-3 Linear Imaging Self-Scanning Sensor is Refractive optics in four spectral bands."]
[4.508973121643066, 4.739952087402344, "The User Request of the DPE Data Processor Element is Via the Data Delivery subscription service."]
[9.400650978088379, 5.071755409240723, "The Spin Rate of the P2 Satellite is Unknown."]
[11.660744667053223, -1.2265033721923828, "The Mass of the BRITE spacecraft Satellite is about 7 kg."]
[6.957852840423584, 7.7134690284729, "The Sensor Type of the HARP Imaging Polarimeter is Polarimeter."]
[4.32184362411499, 2.008751153945923, "The Quantity of the Tyvak 61C Satellite is 1."]
[7.4746174812316895, -0.35309937596321106, "The Article Date of the Clyde Space Rocket Rocket is Feb. 1, 2011."]
[6.660891532897949, 7.1808271408081055, "The Signal Injection Window of the Time Delaying Transponder Calibration Device is Noise measurement slot."]
[11.513630867004395, -1.0071848630905151, "The AM Mass of the DSX Spacecraft Payload Module Satellite is  180 kg."]
[8.396631240844727, 9.88287353515625, "The Spectral Bands of the Focal Plane Array Detector Array is Multiple."]
[8.507246017456055, 7.575291633605957, "The Function of the OBA Instrument Component is Contains all of the instrument optical subassemblies."]
[7.084904670715332, 0.9710812568664551, "The Announcement Date of the Hickson Galaxy Group (HCG16) Satellite is Jan. 30, 2000."]
[8.09022331237793, 8.25910472869873, "The Presentation Date of the Michelson Interferometer Instrument is May 27-31, 1991."]
[9.448824882507324, 0.4854445159435272, "The Design Life of the GEISAT Constellation Satellite is Five years."]
[5.276968955993652, 3.359976291656494, "The Door Latch of the CSD Satellite Component is Automatically resettable."]
[4.97599458694458, 6.067847728729248, "The Frequency Requirement of the SRMSat Satellite is > 90 Hz in longitudinal and > 45 Hz in lateral directions."]
[3.4767186641693115, 5.72689962387085, "The Image Size of the File Transfer Test Communication is 150 MByte."]
[9.240477561950684, 1.6835994720458984, "The Coverage of the Active Schedule Planning Product is Next fourteen 24-hour operational days."]
[11.765287399291992, -0.9697202444076538, "The S/C Launch Mass of the Payload Satellite Payload is 1,900 \u2013 2,100 kg."]
[8.518159866333008, 7.844520092010498, "The Data of the RADMON Radiation Monitor is Research Data."]
[11.735429763793945, 4.955660343170166, "The X-ray Emission of the Ophiuchus galaxy cluster Galaxy Cluster is Reveals the edge of a large cavity, carved in the hot gas by the black hole jets."]
[9.160765647888184, 4.216624736785889, "The Size of the SI-300 Satellite Bus is 1.5 m in diameter and 1.95 m in height."]
[7.225653648376465, 5.281203746795654, "The Function of the Green City Watch Application is Quantify the CO2 uptake of urban green spaces."]
[9.674298286437988, -0.6246239542961121, "The Assembly of the SIMPL-Microsat Microsatellite is Manual crew member assembly in microgravity of eight subassemblies utilizing minimal tools and simple mechanical and electrical connections."]
[9.656451225280762, 3.6098215579986572, "The Objective of the CRaTER Cosmic Ray Telescope is Characterize the global lunar radiation environment and its biological impacts."]
[8.119760513305664, 0.7439156770706177, "The Presentation Date of the Megha-Tropiques Satellite Mission is November 7-11, 2011."]
[8.888911247253418, 3.2869675159454346, "The Orbit of the SBSS Satellite System is Low Earth Orbit (LEO)."]
[7.8879265785217285, 2.8930203914642334, "The LTDN of the CartoSat-2D Satellite is Local Time on Descending Node."]
[9.588754653930664, 5.981991767883301, "The Measurement Model of the ADCS Attitude Determination and Control System is Comprised of sensory inputs and computed attitudes."]
[8.992652893066406, 6.966677665710449, "The Ion Density of the PAP Plasma Analyzer is 5 x 10^2 ~ 1 x 10^7 cm^-3."]
[9.522212028503418, 8.936331748962402, "The Sun Angle Constraint of the CHEOPS Telescope is Larger than 120\u00ba."]
[10.2814359664917, 2.8372185230255127, "The Altitude of the SCD-2 Satellite is 750 km."]
[11.359487533569336, 2.307094097137451, "The Altitude at Autonomous Landing of the Hayabusa-2 Spacecraft is About 500 m."]
[4.936026096343994, 1.5215086936950684, "The Number of Private Launch Companies of the China Country is More than 10."]
[7.822159290313721, 1.8155497312545776, "The Testing Period of the ExoMars Mission is Since April."]
[9.77109146118164, 6.667492866516113, "The UK's Record Maximum Temperature of the Meteosat-10 Satellite is 38.5\u00b0C."]
[5.534121990203857, 4.721108436584473, "The Spatial Acquisition Duration of the Alphasat TDP1 GEO-relay is Reliably achieved within 7 s."]
[3.633758544921875, 5.11629581451416, "The Function of the SSRU Data Processing Unit is Receive, process, store and transmit the image data."]
[8.538873672485352, 2.3062853813171387, "The Model of the Parker Solar Probe Satellite is WSA model."]
[6.036205768585205, 0.6594944000244141, "The Design Presentation Date of the Star Tracker CubeSat Component is March 3-10, 2012."]
[7.091089248657227, 0.9184792637825012, "The Orbital Commissioning Finish Date of the Satellite Satellite is September 29, 2013."]
[5.375765323638916, 5.63095235824585, "The Average Number of Jointly Tracked Satellites of the T3000G2 receiver GPS Receiver is 2-3."]
[7.390103816986084, -0.17712779343128204, "The Launch Date of the Indian rocket Rocket is April 15, 2017."]
[7.1451334953308105, 3.0878279209136963, "The Mission Status of the Satellite Spacecraft is Unspecified."]
[5.138411521911621, 2.672534465789795, "The Affiliation of the MAYA-1 1U CubeSat is PHL-Microsat Program of the University of the Philippines Diliman."]
[2.332392454147339, 4.474279403686523, "The Instrument Power Requirements of the FLP Satellite is Approximately 100 W."]
[10.251337051391602, 4.964156627655029, "The Thruster Quantity of the EPPS Electric Propulsion Subsystem is 8."]
[4.5333571434021, 4.313874244689941, "The Components of the Sensor Suite Payload is IMU, magnetometer."]
[9.036274909973145, 9.278433799743652, "The Transmitted Wavefront Error of the Photon Sieve Optic is \u03bb/10."]
[11.520709037780762, 6.175136566162109, "The Number of Thermistors of the XMM-Newton Satellite is 8."]
[8.10439395904541, 0.38136959075927734, "The Wind Profile Date of the ISS-RapidScat Scatterometer Instrument is Oct. 3, 2014."]
[9.09691333770752, 5.067584037780762, "The Type of the S/C Satellite is three-axis stabilized, zero-momentum satellite."]
[6.7920451164245605, 3.654242753982544, "The INR Performance of the GOES N-P series Satellite is Improved."]
[9.07387638092041, 4.021679878234863, "The Orbit Transfer Method of the LUMIO Satellite is Stable Manifold Injection Maneuver."]
[3.661924362182617, 6.336021423339844, "The Uplink Data Rate of the TT&C Communications RF Communications is 2 kbit/s."]
[11.539578437805176, -1.321743130683899, "The Mass of the IOD-1 GEMS Satellite is Approximately 4 kg."]
[5.876829624176025, 3.921945095062256, "The Location of the ERSDAC Data Analysis Center is Japan."]
[5.972994804382324, 3.1903188228607178, "The Developer of the MSG Satellite Fleet is Airbus Defence and Space."]
[3.1458792686462402, 6.795329570770264, "The Output Power of the STX-01 S-band Transmitter/Transceiver is 30 dBm."]
[11.54849624633789, 5.286929130554199, "The Brighter than a trillion stars of the Flare Brightness Measurement is In less than 48 hours the system appears to quadruple in brightness."]
[8.366744995117188, 3.1967713832855225, "The Formation Flying of the TanDEM-X Satellite is Yes."]
[9.770885467529297, 4.599946975708008, "The Tank Diameter of the Launcher Test Facility is 3 m."]
[6.907938480377197, 3.1312780380249023, "The Mission Status of the FormoSat-2 Satellite is Currently operating."]
[7.3597517013549805, 0.7102607488632202, "The Deorbit Date of the ORBCOMM Satellite is Oct. 15, 2012."]
[6.6783037185668945, 2.747471809387207, "The Principal Investigator of the SEOPS-PGTIDE (P&G Tide in Space) Research Project is Dr. Mark Sivik."]
[10.874432563781738, 3.3731584548950195, "The Closest Exploration Distance of the New Horizons spacecraft Spacecraft is 4 billion miles from the Sun."]
[1.538913607597351, 4.831389427185059, "The Voltage of the 60V link Power Link is 60V."]
[11.003649711608887, 5.020343780517578, "The Source of the Solar Energetic Particle Events Space Phenomenon is Super active region 11944."]
[6.55514669418335, 7.824991226196289, "The Output Pulse Energy of the InnoSlab laser Laser is About 30 mJ."]
[1.9637881517410278, 3.825385332107544, "The Components of the IRAS project Technology is 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."]
[6.318309307098389, 4.265626430511475, "The Science Objectives of the TROPICS Constellation of CubeSats is Assimilate microwave radiances and/or retrievals in mesoscale and global numerical weather prediction models to assess impacts on storm track and intensity."]
[8.416625022888184, 0.8604810833930969, "The Observation Frequency of the Megha-Tropiques Satellite is Up to 5 (3) observations per day."]
[11.271389961242676, 2.673482894897461, "The Diameter of the Great Blue Hole Underwater Sinkhole is Over 300 m."]
[7.399412631988525, 5.437551975250244, "The Rayleigh Impact of the Aeolus Satellite is Gradually declining as the instrument noise increases."]
[8.613737106323242, 0.13289493322372437, "The Number of Visitors of the International Space Station Space Station is More than 230 people."]
[8.646944046020508, 5.313682556152344, "The Pointing Knowledge of the QuikTOMS spacecraft Satellite is < 0.25\u00ba."]
[7.5635085105896, 4.482453346252441, "The Imaging Modes of the ICEYE-X2 Satellite is High resolution and very wide swath."]
[8.232318878173828, 2.2991790771484375, "The Solar Occulting Disk of the SOHO Satellite is LASCO C2 and C3 camera."]
[10.855927467346191, 4.117954730987549, "The Follow-up Targets of the CHEOPS Satellite is Targets from the planned TESS (Transiting Exoplanet Survey Satellite) mission of NASA."]
[6.584295749664307, 3.6595265865325928, "The Function of the GOES Satellite is Relay data from remotely located in-situ sites to properly equipped receiving stations."]
[9.502601623535156, 0.9987877011299133, "The Operation Duration of the GHGSat-D Satellite is Over three years."]
[5.289510250091553, 2.7876806259155273, "The Purpose of the Unisat-7 smallsat Satellite is Tryout of technology for the precise orbit insertion of small satellites of CubeSat format."]
[7.673299312591553, 2.9364383220672607, "The Sensor Complement of the MASCOT Sample Return Capsule Capsule is Unknown."]
[7.953357696533203, 8.743616104125977, "The Detector of the ELVIS Spectrometer is UV coated back-illuminated e2V CCD 30-11."]
[9.226198196411133, 7.926199913024902, "The Global Maps Resolution of the LEND Neutron Detector is 5-20 km."]
[7.857193470001221, 4.752532005310059, "The Resolution of the SMOS Satellite is 100 m."]
[8.826873779296875, 2.2394728660583496, "The Research Center of the MEMS Space Telescope Telescope is Unknown."]
[6.966674327850342, 5.4123334884643555, "The Usage of the AOPOD Data Products is Weather forecasting."]
[9.905183792114258, 3.999168872833252, "The Solar Sail Deployment Date of the IKAROS Small Solar Power Sail Demonstrator is June 11, 2010."]
[2.561276435852051, 3.9810054302215576, "The Solar Panels of the IOD-1 GEMS Satellite is CSL Double Deploy Solar Panels."]
[7.962800979614258, 1.9705865383148193, "The Full Science Mission Start of the ExoMars Trace Gas Orbiter Orbiter is 2018."]
[11.354104995727539, 6.971491813659668, "The Measurement Capability of the NICER X-ray Instrument is Intrinsic clock stabilities of MSPs."]
[9.023215293884277, 10.638371467590332, "The Observation Wavelength of the DCAM3 Camera is Visible."]
[7.901496410369873, 7.73532247543335, "The Measurement Rate of the FFRF Sensor Instrument is 1 Hz."]
[5.211813449859619, 4.4650774002075195, "The Ground Network of the FormoSat-7 / COSMIC-2 mission Satellite Mission is U.S., European, Asian, and polar ground networks."]
[5.6277923583984375, 2.4899682998657227, "The Manufacturer of the SBSS Satellite System is Boeing Space and Intelligence Systems."]
[9.513970375061035, 8.120380401611328, "The Scintillator Thickness of the Gamma-ray Counter Detector is 5 mm."]
[7.311628341674805, 4.192070007324219, "The Measurement Domain of the DMC-3 Satellite Constellation is Land."]
[5.968048095703125, 1.569698452949524, "The Operation of the HTV Spacecraft is Berthing to the ISS."]
[7.338907718658447, 2.2318837642669678, "The Delay Announcement Date of the Orbiting Carbon Observatory-2 Satellite is Feb. 10, 2012."]
[10.007746696472168, 4.59714937210083, "The Propulsion System Type of the Lunar Flashlight 6U CubeSat Satellite is \u201cgreen\u201d monopropellant."]
[10.458375930786133, 4.904222011566162, "The Dry Mass of the DMC Propulsion Subsystem Electric Propulsion is < 6 kg."]
[4.986745357513428, 6.667982578277588, "The Gain of the Ku-band Antenna Antenna is Greater than 42.5dB."]
[3.6162614822387695, 4.746985912322998, "The Processing Power of the VPU Video Processing Unit is More than 1000 MIPS."]
[7.845037937164307, 9.222900390625, "The Spectral Range of the LR Spectrometer Spectrometer is 500\u2013758 nm."]
[11.300893783569336, 3.554762840270996, "The Small Lobe Dimensions of the Comet Celestial Body is 2.6 x 2.3 x 1.8 km."]
[1.4884495735168457, 4.949057102203369, "The Voltage Ripple of the SBVR Power Supply is < 600 mVpp."]
[7.770931720733643, 3.681915044784546, "The Tasking Rate of the Pl\u00e9iades Neo constellation Satellite Constellation is Five times higher than previous constellations."]
[4.468493938446045, 6.19379186630249, "The Flight Heritage of the CanX-2 S-band Transmitter/Transceiver is 1 mission."]
[9.450003623962402, 9.372971534729004, "The Pupil Diameter for LR of the Instrument Hyperspectral Imager is 36.1 mm."]
[7.506769180297852, 1.3531666994094849, "The Scanner Portion Failure Date of the ERBE Instrument is Feb. 28, 1990."]
[5.2400007247924805, 6.908848762512207, "The IFOV (beam width) of the Antenna Reflector is 0.94\u00ba."]
[6.140047550201416, 4.403520107269287, "The Experiment of the Tokyo Institute of Technology Organization is Evaluation of the robot arm's vibrations."]
[3.282468557357788, 5.58161735534668, "The Data Size of the Raw Science Data Packet Data Packet is 256 bytes."]
[5.215505599975586, 6.491977214813232, "The Antenna Polarization of the TUC Transponder Microwave Transponder is Circular."]
[7.548998832702637, 9.564435958862305, "The Spectral Region of the ERIP Earth Remote-Sensing Imaging Package is 252 - 340 nm."]
[4.9445037841796875, 1.8560701608657837, "The Number of Satellites of the Terra Bella Satellite Constellation is 13."]
[4.229804515838623, 7.203300952911377, "The Mass of the Antenna Communication is < 400 kg."]
[8.027227401733398, 9.119945526123047, "The Bandpass of the Long Wavelength Band Spectrometer is 1335-1750 \u00c5."]
[6.631547451019287, 3.8343188762664795, "The Broadcasting Service Channels of the GK2A satellite Satellite is LRIT, HRIT, UHRIT."]
[11.591560363769531, 4.503895282745361, "The Brightness of the Red Dwarfs Star Type is Much less than our Sun."]
[7.727291107177734, 1.1376680135726929, "The Submission Date of the Copernicus Masters 2021 Competition is 2021."]
[9.182665824890137, 3.20875883102417, "The Orbit Type of the Anand Satellite is Sun-synchronous."]
[7.633665084838867, 8.01718521118164, "The Satellite Altitude of the MXT Instrument is 600 km."]
[4.498417377471924, 5.371006011962891, "The Type of the TT&C and Payload Data Communication System Satellite is Flexible."]
[9.020081520080566, 6.962893962860107, "The Ion Composition of the PAP Plasma Analyzer is H+, He+, O+."]
[9.520892143249512, 1.0531808137893677, "The Reentry Time of the 3U CubeSat Satellite is 72 days."]
[13.115316390991211, 4.05531120300293, "The Monitoring Period of the Gaia Space Astrometric Mission is 5 years."]
[9.662007331848145, 6.000929832458496, "The Components of the ADCS Attitude Determination and Control Subsystem is Wheels, gyroscopes, magnetic control system, magnetorquers, magnetometer."]
[6.4001264572143555, 4.551709175109863, "The Product Type of the Sentinel-1 Satellite is SLC (Slant-Range Single-Look Complex)."]
[7.985457420349121, 7.291136264801025, "The Components of the Instrument Calibration is SEDF (Spatial Response), Alignment Parameters, ISRF Shape, SSI, SR, Smile, CU, Radiance Calibration Coefficients, Response Linearity, Noise, Detector PRNU, Detector DSNU."]
[11.2652587890625, 6.584808826446533, "The Unknown of the X-ray Pulsars Navigation Method is Unknown."]
[5.096165657043457, 7.594874858856201, "The Data Rate of the FGM Instrument is 0.80 kbit/s."]
[9.702613830566406, 1.224838137626648, "The Autonomous Operations of the Solar Orbiter Satellite is 15 days without ground contact."]
[12.1173095703125, 3.3103506565093994, "The Inclination of the OrbView-2 Satellite is 98.2\u00ba."]
[8.045450210571289, 1.488426685333252, "The Good Solar Pointing Start Date of the SOVAP Instrument is 22/7/2010."]
[4.944206237792969, 4.988825798034668, "The Transmission Band of the Delft ground station Ground Station is S-band."]
[8.18267822265625, 9.517671585083008, "The Number of Bands of the SWIR Detector is 80."]
[6.610767364501953, 8.388731002807617, "The Channels of the MERSI-RM Radiometer is 8."]
[10.268104553222656, 6.83854341506958, "The Type of the TCS Thermal Control Subsystem is Semi-active."]
[7.479295253753662, 0.5665266513824463, "The Launch Date of the Euclid Satellite is 2022."]
[8.85728645324707, 7.802021026611328, "The Energy Range of the MIPA Ion Mass Analyzer is Optimized to cover accelerated ionospheric ions."]
[9.688916206359863, 1.578467845916748, "The Orbit Repeat Cycle of the GOCE Satellite is 61 days."]
[3.960042953491211, 4.676340103149414, "The Redundancy of the OBC On-Board Computer is Yes."]
[10.396870613098145, 5.13241720199585, "The Propulsion Systems of the MTM Transfer Module is Chemical Propulsion System and Electrical Propulsion System."]
[6.2655768394470215, 2.221602201461792, "The Managing Organization of the Jason-3 Satellite is NASA's Jet Propulsion Laboratory in Pasadena, California."]
[9.420878410339355, 5.138082504272461, "The Speed of the Flywheel Satellite Component is 4500 rpm."]
[9.418915748596191, 4.7876386642456055, "The Acceleration of the Microgravity Regime Environment is <10-4 g for all directions."]
[2.234797239303589, 4.439002990722656, "The Bus Power Consumption of the EROS-A Satellite is 300 W."]
[7.691059589385986, 7.197524547576904, "The Launch Provider of the TEMPO Instrument is SpaceX Falcon-9."]
[3.8454997539520264, 4.304708480834961, "The Number of Applications of the C&DH Subsystem Command and Data Handling is 17."]
[11.516033172607422, -0.9970481395721436, "The PM Mass of the DSX Spacecraft Payload Module Satellite is 180 kg."]
[9.503950119018555, 5.53293514251709, "The Attitude Knowledge of the AOCS Attitude and Orbit Control Subsystem is 0.01\u00ba."]
[7.880964756011963, 9.893309593200684, "The Spectral Bands of the WV-3 Imager Imager is 29."]
[7.656885147094727, 2.9194445610046387, "The Mission Status of the MASCOT Sample Return Capsule Capsule is Unknown."]
[8.798757553100586, 7.583426475524902, "The Manufacturer of the IVM Ion Velocity Meter is University of Texas, Dallas."]
[6.148787021636963, 0.5462028980255127, "The CDR (Critical Design Review) of the SOURCE 3U CubeSat Satellite is Passed in July 2021."]
[3.156416416168213, 4.847553253173828, "The NOR Flash of the GomSpace NanoMind A3200 Onboard Computer is 128 MB."]
[5.605721950531006, 6.131374835968018, "The Antenna Diameter of the Satellite Satellite is 1.2 m, 1.84\u00ba (Ku-band), 6.2\u00ba (S-band)."]
[8.653841018676758, 1.9026929140090942, "The Project Status Presentation of the James Webb Space Telescope Space Telescope is Phil Sabelhaus, \"James Webb Space Telescope (JWST) Project Status for the AAS Town Hall,\" January 5, 2010."]
[4.93931770324707, 5.945605278015137, "The Destination of the Dutch Radio Antenna Antenna is Moon."]
[3.876051902770996, 2.302621603012085, "The CubeSat Size of the SUNSTORM Satellite is 3U."]
[5.27457332611084, 5.872895240783691, "The Quantity of the GPS Antennas Antennas is 2."]
[4.85012674331665, 5.997321128845215, "The Frequency Band of the SWOT Satellite is 8.025-8.400 GHz."]
[6.290426731109619, 3.432410478591919, "The Agency of the CryoSat Satellite is ESA."]
[9.017605781555176, 9.871169090270996, "The Dark Current Source of the Photodiode Detector is Thermal and ionizing radiation effects."]
[11.720544815063477, 5.070606231689453, "The Host Galaxy of the Sw J1644+57 Supermassive Black Hole is Distant."]
[9.730547904968262, 1.7337939739227295, "The Plasma Irregularities Model of the C/NOFS Satellite is Equatorial plasma bubbles age and irregularity spectra evolution."]
[9.347723960876465, 9.445357322692871, "The Pupil Diameter of the NAOMI Imager is Driven by the MTF (Modulation Transfer Function) requirement."]
[9.18381118774414, 7.928782939910889, "The Temperature of the Instrument Optical Subsystems is 130 K."]
[7.371291160583496, 1.0222041606903076, "The Mission Date of the JEM-EUSO Satellite is June 5-12, 2011."]
[8.736016273498535, 8.376755714416504, "The Quantity of the Microcalorimeter Microcalorimeter is 14."]
[9.382157325744629, 7.420598030090332, "The Temperature Range of the DE probe Charged Particle Probe is 0.1 - 1.5 eV."]
[6.670593738555908, 7.450069904327393, "The Receiver Channels of the DIAL Instrument LIDAR is 2."]
[9.184981346130371, 6.355846405029297, "The Guide Stars Selection of the DPU Data Processing Unit is Up to 10 stars from the full OM image."]
[9.407876014709473, 5.818447113037109, "The Capability of the Torque Rods Attitude Control is 15 Am2."]
[6.977905750274658, 9.173007011413574, "The Azimuth Imaging Length of the P Mode Observation Mode is 10 km."]
[7.450745582580566, 8.881810188293457, "The Resolution Cell, Horizontal of the Instrument Spectrometer is 16 km."]
[8.394401550292969, 2.189307689666748, "The Antenna Location of the Voyager 2 Spacecraft is Canberra, Australia."]
[11.259997367858887, 6.716439247131348, "The Components of the SEXTANT System is 1) the NICER XTI, 2) the flight software and algorithms, 3) the ground testbed, and 4) the ground system."]
[10.334798812866211, 7.041387557983398, "The Number of Concepts of the ALBus R&R Design is Three."]
[6.977238178253174, 4.561698913574219, "The Mission Priority of the GOSAT Satellite is Short wave infrared observation."]
[4.438088417053223, 2.3235883712768555, "The Number of Satellites of the Starlink Satellite Constellation is More than 500."]
[8.353514671325684, 8.528766632080078, "The Hydrogen Cell of the Instrument Sensor is Pyrex vessel (MgF 2  lens windows-distance 76 mm)."]
[11.514055252075195, 5.98045539855957, "The Mission Type of the XMM-Newton Satellite is Follow-up of Gravitational Wave Detections."]
[7.935948371887207, 4.937509059906006, "The Science Instruments of the Solar Orbiter Satellite is 10."]
[7.844385147094727, 9.350373268127441, "The Spectral Bands of the Maps Data is 400-500 nm, 500-600 nm, 600-700 nm, 750-925 nm."]
[11.50590991973877, -1.2938568592071533, "The Mass of the TUBSAT-N Satellite is 8.5 kg."]
[8.970169067382812, 10.607034683227539, "The Pixel Size of the LISS-3 Camera is 13 \u00b5m."]
[7.013434410095215, 5.849559783935547, "The Measurement Type of the Argo Ocean Buoys is Subsurface-salinity."]
[8.615989685058594, 5.930454254150391, "The Boom Length of the Spacecraft Satellite is 10.6 m."]
[6.9224700927734375, 7.789572715759277, "The Duty Cycle of the Instrument General is 20%."]
[4.187747955322266, 3.2207436561584473, "The Impact of the 5G Communications System is 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."]
[4.047411918640137, 4.473715305328369, "The Manufacturer of the CPU Board Processor is BAE Systems."]
[10.09033203125, 3.0823724269866943, "The Orbit Altitude of the KSF1 satellites Satellite is 525 km."]
[6.941788196563721, 1.1168832778930664, "The Merger Date of the Spire Company is Aug. 17."]
[7.401890277862549, 1.7694127559661865, "The NASA Press Release of the Gravity Probe B Satellite is May 4, 2011."]
[10.361283302307129, 2.6917738914489746, "The Orbital Altitude of the SZ-7 Spaceship is ~330 km."]
[9.620850563049316, 3.8315539360046387, "The Module Assembly of the CanX-7 Satellite is Two decks."]
[8.466436386108398, 7.094917297363281, "The Magnetic Field Measurement Range of the Plasma Wave Instrument Instrument is 1 Hz to 10 kHz."]
[10.337964057922363, 5.218860626220703, "The Quantity of the Propellant Tanks Propellant is 2."]
[3.543527364730835, 5.987473964691162, "The Peak Data Rate of the EAN Connectivity System is 100 Mbit/s."]
[3.6773784160614014, 6.614186763763428, "The Data Transfer Frequency of the SSRNI Data Acquisition and Registration System is X-band at 8.2 GHz."]
[10.639521598815918, -1.6911174058914185, "The ULC Cargo of the HTV-7 Cargo spacecraft is 1.9 metric tons."]
[5.576681613922119, 2.6126439571380615, "The New Factory Location of the Satellogic Satellite Company is Netherlands."]
[4.891870975494385, 2.064207077026367, "The Quantity of the CubeSats Satellite is 4."]
[9.256402969360352, -0.5818295478820801, "The Presentation Date of the Nanosatellite Tracking Ships Nanosatellite is April 27\u201330, 2009."]
[8.336108207702637, 4.606437683105469, "The Swath width of the ALOS-3/PRISM-2 Satellite is 50 km."]
[3.610781669616699, 6.2890143394470215, "The Data Rate (Downlink) of the S-band telemetry system Telemetry System is 1 Mbit/s."]
[6.063547134399414, 5.1363139152526855, "The Location Knowledge of the GFO Satellite is Redundant GPS receivers."]
[8.262128829956055, 6.329980373382568, "The Cost (sensor + spacecraft) of the Framer Sensor is Very low."]
[5.50581169128418, 3.90861177444458, "The Software Code Reuse of the VMOC Mission Operations Center is About two-thirds between TacSat-4 and ORS-1 missions."]
[3.952103853225708, 6.439087867736816, "The Modulation and Coding of the Unit Communication System is BPSK, Rate 1/2, K=7."]
[10.881555557250977, 5.117948532104492, "The Impact of the Solar Energetic Particles Space Weather Phenomenon is Can fry sensitive spacecraft electronics and pose serious risks to human astronauts."]
[7.630547523498535, 4.515633583068848, "The Daily Global Composite Products of the PROBA-V Satellite is 728."]
[5.191174507141113, 3.7086620330810547, "The Technologies of the IXV Communications Network Network is Serial leased lines, Ethernet lines, ISDN, IP Satellite Networks."]
[6.6052350997924805, 1.0918570756912231, "The Separation Date of the PRISMA Satellites Satellite is August 12, 2010."]
[6.570858478546143, 7.7112717628479, "The Model of the Diode Pumped Nd:YAG Laser Component is RLU."]
[7.5547871589660645, 8.957327842712402, "The Angular Coverage of the STAFF/DWP Instrument is Polar(range/interval) = 180\u00ba/12 (IIMS), = 180\u00ba/9 (IES)."]
[8.02627182006836, 4.431841850280762, "The Ground Resolution of the Mars Express Orbiter is Approximately 20 m/pixel."]
[11.441828727722168, 5.132388114929199, "The Light Emission of the Transient Luminous Events Atmospheric Phenomena is Weak."]
[5.691402435302734, 3.9488067626953125, "The Location of the FOS Flight Operations Segment is ESOC in Darmstadt."]
[9.935002326965332, 4.007657051086426, "The Mission Duration of the NanoSail-D2 Solar Sail is 70 and 120 days."]
[5.894829273223877, 2.764397621154785, "The Manufacturer of the ELSA-d Satellite is Astroscale UK Ltd."]
[5.752406597137451, 9.16598129272461, "The Power of the MW Instrument is 1 W."]
[11.298385620117188, 5.705925941467285, "The Detector Type of the LISA Space Observatory is Gravitational Waves."]
[8.802189826965332, 7.632170677185059, "The PI of the IVM Ion Velocity Meter is Rod Heelis."]
[9.511734962463379, 1.1015899181365967, "The Satellite Launches of the Space Flight Laboratory Organization is Five in Two Weeks."]
[7.963393211364746, 7.266861915588379, "The Design of the Radiometric Responsivity Tracking Method Method is For optical sensors without on-board calibration systems."]
[9.778225898742676, 6.897923469543457, "The Temperature of Spacecraft and Instruments at Closest Approach to the Sun of the Heat Shield Parker Solar Probe Component is About 85 degrees Fahrenheit (29\u00baC)."]
[4.763840675354004, 4.047194004058838, "The Components of the AFSS Autonomous Flight Safety System is GPS, IMU, algorithms."]
[3.637434720993042, 6.332221031188965, "The Data Rate of the RF Communications TT&C is 2.5 or 15 kbit/s."]
[8.517544746398926, 9.93474292755127, "The Number of Arrays of the Detector Arrays Optical Component is 2."]
[11.766180992126465, -0.936818540096283, "The Mass of the Telesupport Payload is 27 kg."]
[4.958887100219727, -3.106816530227661, "The Affiliation of the Kazifumi Fukuda Author is Unknown."]
[10.332351684570312, 6.0654191970825195, "The Angular Resolution of the RHESSI Satellite is Few arcseconds."]
[11.58434772491455, 5.962662696838379, "The Typical X-ray Flare Duration of the X-ray Source Celestial Object is Up to a few hours or even days."]
[7.199561595916748, 1.6202143430709839, "The Operational Date of the ERS-1 Satellite is Unknown."]
[9.332601547241211, 8.480911254882812, "The Design Requirement 2 of the OCO-3 PMA Pointing Mirror Assembly is Movement not affect the measurements through angular dependent polarization or radiance changes."]
[5.929192066192627, 6.3647141456604, "The L-band Resolution of the SAR-XL Payload SAR Instrument is 5 m class."]
[4.093023777008057, 7.1218461990356445, "The Mass of the NovAtel OEMV-2 L1/L2-F GPS unit GPS Unit is 56 g."]
[9.795783996582031, -0.9800655245780945, "The Orbit Type of the JL-1-GF03D Microsatellite is SSO."]
[4.270715713500977, 6.908152103424072, "The Receive Frequency (MHz) of the HRIT HiRID Data Receiver is 2029.1."]
[7.964784622192383, 1.6746293306350708, "The Observation Period of the Dynamics of the Radiative Environment Observation is 11/2000-11/2001."]
[10.18300724029541, 6.830473899841309, "The Orientation Requirement of the Radiator Thermal Control System is Oriented on cold, deep space."]
[6.810268878936768, 1.3533623218536377, "The Imagery Capture Date of the WorldView-3 and GeoEye-1 Satellites is Northern California Wildfires."]
[7.172863006591797, 1.5027400255203247, "The Mission Start Date of the THEMIS Satellite is Unknown."]
[8.459280014038086, 8.77427864074707, "The Spectrometer Type of the SPEXone Spectrometer is Compact and lightweight all-reflective imaging grating spectrometer."]
[5.255439758300781, 5.905455589294434, "The Antenna of the Lunar Pathfinder's Receiver Satellite Receiver is High-gain satnav antenna."]
[9.138962745666504, 10.573617935180664, "The Cadence of the Fast Cameras Camera is 2.5 seconds."]
[6.999631881713867, 4.544528007507324, "The Type of the MTG-I Satellite is Imager."]
[2.3234665393829346, 3.821028470993042, "The Solar Panel Deployment of the LightSail Satellite is Possibly ajar or deployed."]
[6.521334171295166, -0.14156366884708405, "The Atomic Clocks of the Indian Regional Navigation Satellite System (IRNSS) Satellite System is Break."]
[9.592619895935059, 8.986815452575684, "The Aperture Diameter of the ALI Telescope is 12.5 cm."]
[9.009300231933594, 8.204142570495605, "The Function of the SMA Scan Mechanism Assembly is 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."]
[6.636937141418457, 3.0961484909057617, "The Managing Center of the Chandra X-ray Observatory is NASA's Marshall Space Flight Center."]
[5.849616050720215, 8.606122016906738, "The Data Rate of the MWHS-II Microwave Humidity Sounder is 15 kbit/s."]
[5.910708904266357, 2.73885178565979, "The Manufacturer of the STPSat-3 Satellite is Ball Aerospace."]
[5.405635833740234, 9.258814811706543, "The Power Consumption of the SEIS Instrument Seismometer is Around 1W."]
[9.936776161193848, -0.7010365128517151, "The Body Dimensions of the Nanosatellite Satellite is 20 x 20 x 20 cm."]
[8.124604225158691, 2.1792802810668945, "The Manned Moon Landing Deadline of the Artemis Program Space Exploration Program is 2024."]
[17.72828483581543, 7.162690162658691, "The J2000 right ascension (deg) of the B0540-69 Pulsar is 85.04668."]
[9.421844482421875, 1.5222636461257935, "The Frequency of the Request for Information Process is Every 12 to 18 months."]
[11.260846138000488, 6.724348068237305, "The Conference Presentation Date of the SEXTANT X-ray Timing and Navigation Technology is 5-9 Jan. 2015."]
[7.440446853637695, 7.919602394104004, "The Data Sensitivity of the PAMELA Instrument is Exceeds current data by several orders of magnitude."]
[8.704404830932617, 2.578813076019287, "The Injection Velocity Shortfall of the ARTEMIS Spacecraft is About 500 m/s."]
[6.613788604736328, 4.578368663787842, "The Mission Objective of the Copernicus Sentinel-6 Satellite is Monitor sea-level change."]
[4.46458101272583, 4.549893379211426, "The Function of the IDE System is Controls instrument operations and collects instrument telemetry."]
[11.437202453613281, 4.530267238616943, "The Neon Temperature of the Sun's Lower Atmosphere Celestial Body is 630,000\u00baC."]
[8.636443138122559, 8.037403106689453, "The Data Collection Period of the Liulin-MO dosimeter Radiation Dosimeter is Six-month interplanetary cruise to Mars."]
[5.046756267547607, 4.299470901489258, "The Functions of the SMC Secure Management Center is TC authentication/ciphering and key management."]
[8.506674766540527, 9.069623947143555, "The Filter Type of the FUV channel Spectrometer is Calcium Fluoride."]
[5.303866386413574, 10.376297950744629, "The Missed Lightning in Northern Hemisphere of the ISS-LIS Lightning Detection Instrument is Nearly all of that lightning."]
[8.5901460647583, 10.427583694458008, "The Focal Plane CCD Lines of the Camera Imaging Device is 3."]
[10.2996244430542, 5.981325626373291, "The TGF Association of the RHESSI Satellite is Intracloud lightning."]
[7.721160888671875, 9.070955276489258, "The Resolving Power of the Spectrometers Spectrometers is 3 x 10^5 for the narrowband ones."]
[9.138684272766113, 8.390695571899414, "The L1 Detectors Purpose of the HIT Sensor is Sweep out a 4\u03c0, full-sky coverage."]
[7.335320949554443, 3.6415154933929443, "The Onboard Recorder of the Satellite Satellite is No."]
[4.302005767822266, 5.447752475738525, "The Downlink Contacts per Day of the IXPE Satellite is Up to 9."]
[2.2544822692871094, 4.462936878204346, "The Nominal Power of the IMP-8 Spacecraft is 150 W."]
[6.441458225250244, 4.039738178253174, "The Ground Stations of the PROBA Project Satellite Project is ESA station in Redu (Belgium), second ground station used in S-band during LEOP and the first part of the commissioning phase."]
[5.555307388305664, 5.084451198577881, "The Launch Configuration of the OSIRISv3 Laser Communication Terminal is Soft-stowed."]
[7.184530258178711, 5.2569708824157715, "The Value of Information (VOI) of the COS Climate Observing System is Computed by IGW-SCC."]
[9.509033203125, 5.622490406036377, "The Tuning of the AOCS Control System is Solar array natural mode damping, optimised wheel zero crossing management."]
[4.578148365020752, 4.017671585083008, "The Data Bus of the Suomi-NPP Satellite is MIL-STD-1553."]
[9.40032958984375, -0.7518119812011719, "The Launch Date of the ESAIL Microsatellite is 3 September 2020."]
[5.993649482727051, 0.6394990682601929, "The Publication Date of the SpooQy-1 CubeSat is 2017."]
[7.929079055786133, 10.742595672607422, "The Data Quantization of the Pushbroom imager Optics is 12 bit."]
[5.06025505065918, 6.744614601135254, "The Size of the Antenna Communication Device is 3.3 m x 2.7 m."]
[5.9972004890441895, 3.4034531116485596, "The Agency of the KySat-2 Satellite is MSU (Morehead State University), University of Kentucky (UKy), Kentucky Space LLC."]
[8.662790298461914, 1.9730721712112427, "The URL of the James Webb Space Telescope Space Telescope is http://www.stsci.edu/jwst/operations."]
[4.299878120422363, 4.654386043548584, "The Software of the Modem Processor Signal-Processing Chain is Iris software."]
[6.37852668762207, 3.6965808868408203, "The Access Capability of the JAXA Flight Controller Control System is Laptops in JEM."]
[6.578641414642334, 0.5604878067970276, "The Launch Year of the RADARSAT-1 Satellite is 1995."]
[7.365675926208496, 6.805819034576416, "The Capture Date of the MODIS Imaging Spectroradiometer is June 16, 2022."]
[8.517555236816406, 5.224338054656982, "The Pointing Performance of the S/C Satellite is Better than 0.05\u00ba (3 \u03c3)."]
[8.490347862243652, 10.999565124511719, "The Pixel Size of the Eastman Kodak KLI14403 linear CCD sensor Sensor is 5.0 x 5.0 \u00b5m."]
[6.800194263458252, 5.47732400894165, "The URL of the Soil Moisture Active Passive (SMAP) Mission is http://secure.ntsg.umt.edu/publications/2010/ENOKCEEGJJKPKMMMMRSSTTV10/Entekhabi_IEEEProceedings_05_10.pdf."]
[7.007778167724609, 9.208328247070312, "The Azimuth Resolution of the Stripmap Imaging Mode is 3.3 m (single pol.), 6.6 m (dual pol.)."]
[10.596010208129883, 5.210565567016602, "The Thrust of the CNAPS Propulsion System is 10 mN/thruster."]
[11.41940975189209, 6.404260158538818, "The Manufacturer of the XMM-Newton X-ray space observatory is ESA."]
[6.675593376159668, 1.4020036458969116, "The Presentation Date of the Capella X-band SAR constellation Satellite Constellation is 28 July - 2 August 2019."]
[3.5610122680664062, 2.3254029750823975, "The Size of the CICERO-4 Satellite is 3U."]
[4.618391513824463, 9.03136920928955, "The Operation Pause Duration of the InSight Mars Lander is Several weeks."]
[4.167384147644043, 5.18108606338501, "The Redundancy of the Transmit chain Transmit Chain is Two chains."]
[6.0497660636901855, 4.364808559417725, "The Manufacturer of the ERA Robotic Arm is Fokker Space."]
[9.337199211120605, 1.59923255443573, "The Data Production of the Sentinel-1, -2, and -3 Satellites is Approximately 4 TByte per day."]
[8.072613716125488, 8.008747100830078, "The Arrival Date of the E-THEMIS Thermal Emission Imaging Instrument is Unknown."]
[5.927049160003662, 5.7300286293029785, "The Function of the SAR Antenna Assembly SAR Antenna Assembly is The SAA is an active phased array and it is able to operate different beam characteristics for transmission and reception."]
[7.4138102531433105, 5.699254989624023, "The Role of the Thermohaline Circulation Oceanic Phenomenon is Supplying heat to the polar regions."]
[7.442428112030029, 6.977314472198486, "The Commissioning Phase of the RPW Radio and Plasma Waves Instrument is Before 15 June."]
[8.33581829071045, 9.056855201721191, "The Signal-to-Noise Ratio of the NISP Photometer Instrument is Magnitude 24.0."]
[6.564487457275391, 3.4571805000305176, "The Operator of the Resurs-DK1 Earth Observation Satellite is Russia's Science Center for Remote Sensing of Earth, NTs OMZ."]
[8.150529861450195, 10.322456359863281, "The Spectral Band of the Band Cameras Camera is 762.4 nm."]
[8.691935539245605, 7.959872722625732, "The Output of the MCP Multi-Channel Plate is Proportional to the number of ions at its input."]
[7.296111583709717, 4.50720739364624, "The Secondary Objectives of the PROBA Satellite is Space environment investigation and Earth observation."]
[11.38143539428711, 3.0514559745788574, "The Composition of the Fortescue Group Rock Formation is Volcanic and sedimentary rocks."]
[7.669106483459473, 9.165477752685547, "The Band-to-band co-registration of the Spectrometer Spectrometer is < 1.4%."]
[4.4047532081604, 6.006957054138184, "The TT&C Frequency of the Payload Communication System is S-band."]
[11.70742416381836, -1.1745927333831787, "The Maximum Satellite Mass of the ALMASpace AD-SS Satellite Dispenser is 35 kg."]
[9.226625442504883, 5.001145839691162, "The Orientation Stabilization of the Solar Orbiter Spacecraft is After the first command was sent."]
[9.284448623657227, 10.168207168579102, "The Lens of the TV Camera Camera is Augeniux 50 mm f/0.95 lens."]
[7.248418807983398, 6.261343002319336, "The URL of the Aerosol Polarimetry Sensor Sensor is http://glory.giss.nasa.gov/aps/docs/SPIE_6786_67865L.pdf."]
[6.9289751052856445, 3.6677401065826416, "The Operation Support of the GeoXO Satellite System is Weather, ocean, and climate operations in the United States."]
[5.362332820892334, 2.1654205322265625, "The Number of Products of the EnMAP Satellite is 3 + 1 internal product."]
[9.32605266571045, 6.395891189575195, "The Usage of the ASC (Advanced Stellar Compass) Star Tracker is Only at a low (<4.5 rpm) spin rate."]
[8.033698081970215, 1.4249937534332275, "The Final Report Date of the Solar Mass Ejection Imager (SMEI) Satellite is Oct. 25, 2007."]
[9.299153327941895, 6.401521682739258, "The Catalog of the Star Tracker Attitude Determination Device is 3746 stars."]
[7.677229404449463, 10.211546897888184, "The Instrument Dimensions of the SEVIRI Imager is Diameter of about 1 m and a height of 2.1 m."]
[5.89214563369751, 5.740184783935547, "The Provider of the Keramis-2 Ceramic Microwave Circuits is IMST GmbH."]
[3.9927287101745605, 4.500514030456543, "The Interface of the OBC On-Board Computer is 1553 RIU interface with the S-band transceiver."]
[11.4910888671875, -1.3302615880966187, "The AD-SS Mass of the ALMASat-1 Satellite is 6.54 kg."]
[7.272918701171875, 0.7331482172012329, "The Operation End Date of the PROBA-2 Satellite is December 31, 2016."]
[9.720260620117188, 8.44408130645752, "The Mirror Material of the Limb Imager Telescope is Aluminium."]
[7.530799388885498, 1.8938870429992676, "The Regular Technology Demonstration Mode Start Date of the ICIR IceCube Cloud\u2013Ice Radiometer is June 16, 2017."]
[6.298614978790283, 3.0860536098480225, "The Agency of the DeMi Satellite is MIT."]
[6.329647064208984, 1.1188446283340454, "The Launch Dates of the COSMO-SkyMed Satellite Constellation is 2007, 2008, 2010."]
[8.1012544631958, 10.008774757385254, "The Maximum Upper Band Edge of the MS8 (NIR2) Imager is 1043 nm."]
[6.16359806060791, 5.543553352355957, "The Calibration and Validation Team of the PALSAR Ground Data System is M. Shimada, H. Wakabayashi, T. Tadono, A. Rosenqvist, T. Igarashi."]
[10.608351707458496, -1.05572509765625, "The Mass of the TeleSat LEO Phase 1 Minisatellite is 168 kg."]
[11.769808769226074, 4.599318027496338, "The Distance from Earth of the M33 galaxy Galaxy is Three million light years."]
[5.926716327667236, 6.7520012855529785, "The Spatial Resolution (Azimuth) of the Radar Radar is 50 m."]
[3.762666940689087, 4.332737922668457, "The Functionality of the DHU Data Handling Unit is 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."]
[7.737112045288086, 4.417424201965332, "The Purpose of the COBE (COsmic Background Explorer) Satellite is Measure the leftover radiation from the big bang."]
[8.89120864868164, 3.120493173599243, "The Orbit Decay Rate of the GOCE Satellite is Less than 35 cm per day."]
[6.690834999084473, 0.6848832964897156, "The Year of the RSATS Study is 2004."]
[8.295636177062988, 3.065114736557007, "The Calibration and Mosaicking Chain Operational Date of the TanDEM-X Satellite is End of 2013."]
[7.401009559631348, 9.641002655029297, "The CCD Line Array of the MSU-E Multispectral Scanner is 1024 pixels."]
[6.610103607177734, 0.5640771985054016, "The Launch Date of the MTSAT Satellite is 15 Nov 1999."]
[10.19437026977539, 4.98387336730957, "The Thrust Capability of the Propulsion System Satellite Component is Variable impulse."]
[11.695686340332031, 2.5928401947021484, "The Primary Body Diameter of the Didymos Asteroid is Approximately 800 meters."]
[9.057587623596191, 6.893902778625488, "The Quantity of the Star sensor Sensor is 2 units."]
[5.234653472900391, 4.654503345489502, "The Location of the DLR ground station Ground Station is Neustrelitz."]
[3.693321943283081, 6.212522029876709, "The 100 pps (pulses per second) of the TT&C Communications Command Rate is Command rate - 100 pps (pulses per second)."]
[7.3438334465026855, 5.123388290405273, "The | of the IASI-New Generation Satellite is IASI-New Generation onboard EPS-SG: Expected impact on accuracy and vertical resolution for atmospheric variables."]
[6.654721260070801, 2.215034008026123, "The Constellation of the GPM Mission is Various satellites."]
[8.835698127746582, 7.072481155395508, "The Components of the SWEA Solar Wind Electron Analyzer is SWEA (Solar Wind Electron Analyzer) and STE (Suprathermal Electron Telescope)."]
[10.642374992370605, 9.226468086242676, "The Image Location of the CaSSIS Instrument is 29.2\u00baS/66.8\u00baE."]
[11.999658584594727, 3.414979934692383, "The Orbit Inclination of the ISS International Space Station is 51\u00b0."]
[1.7846769094467163, 4.110766410827637, "The Efficiency of the SFINKS Solar Cell Array is 32%."]
[4.771740436553955, 1.9575614929199219, "The Number of Maneuvers of the SkySat-6 Satellite is 5."]
[5.016583442687988, 3.8386409282684326, "The Purpose of the Airlock Stowage Platform Hardware is 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."]
[12.114725112915039, 2.2014029026031494, "The Conference Presentation of the OSIRIS-REx Asteroid Sample Return Mission is SpaceOps 2014, 13th International Conference on Space Operations, Pasadena, CA, USA, May 5-9, 2014."]
[6.622323513031006, 3.7603306770324707, "The Operator of the INSAT-3DR Satellite is ISRO (Indian Space Research Organisation)."]
[10.650516510009766, 6.839494228363037, "The Energy Range of the RHESSI Imaging Instrument is Soft X-rays (about 3 keV) to gamma-rays (up to about 17 MeV)."]
[12.15687370300293, 2.1901164054870605, "The Sample Site Selection Board Chair of the OSIRIS-REx Spacecraft is Heather Enos."]
[7.088315963745117, 3.323251485824585, "The Unknown of the Extraterrestrial Material Unknown is Unknown."]
[4.937718868255615, 4.0670599937438965, "The Operation of the EDR-2 European Drawer Rack is Run in parallel with the original European Drawer Rack."]
[7.2549357414245605, 0.4548448622226715, "The Launch Date of the Chinese satellite Satellite is Aug. 16, 2016."]
[7.302591323852539, 4.490710735321045, "The MS Camera of the Payload Satellite Subsystem is B1:0.45~0.52 \u00b5m, B2: 0.52~0.59 \u00b5m, B3: 0.63~0.69 \u00b5m, B4: 0.77 ~0.89 \u00b5m."]
[8.307016372680664, 6.400598049163818, "The Area Collection Rate of the Push Frame Framer with a fast steering mirror Sensor is Low."]
[6.568307399749756, 1.1685227155685425, "The Voyage Article Date of the Argo Ocean Observing System is Feb. 28, 2002."]
[7.121535301208496, 2.601952075958252, "The Data Availability of the Carbon Mapper Satellite Project is Freely available."]
[8.84904670715332, 4.970607280731201, "The Magnetorquers of the NEMO-AM Satellite is Quantity: 3, Manufacturer: SFL, Current-Controlled up to 100 mA."]
[7.992459297180176, 10.661381721496582, "The Maximum Range of the TDC-GPX Time-to-digital converter is 7 \u00b5s."]
[7.144761085510254, 6.863204002380371, "The Test Phase Start Date of the IASI-NG Instrument is Early 2021."]
[10.268843650817871, 4.88313102722168, "The Conference Presentation Date of the Micro-Cathode Arc Thruster Thruster is 5-12 March 2016."]
[9.581916809082031, 6.0647077560424805, "The Redundancy of the ADCS Attitude Determination and Control System is Full redundant backup with magnetorquers and reaction wheels."]
[4.845390796661377, -3.37583327293396, "The Member of the Richard Bevilacqua Individual is True."]
[11.620514869689941, 5.086244583129883, "The Study Subject of the Quasars Celestial Objects is Gravity in the very strong field of the supermassive black holes."]
[8.68843936920166, 3.1650466918945312, "The Ion Propulsion System of the GOCE Satellite is Commissioned."]
[10.802637100219727, 3.3855576515197754, "The Speed of the New Horizons Spacecraft is Over 30,000 miles per hour."]
[7.204838275909424, 1.2177925109863281, "The Operation End Date of the ERBS satellite Satellite is Summer of 2005."]
[5.619845867156982, 4.609908580780029, "The Type of the Q/V-band transponder Technology Demonstration Payload is Unknown."]
[6.1065497398376465, 0.8269877433776855, "The Targeted Date of the Iridium-5 Satellite Launch is March 29, 2018."]
[6.9198760986328125, 0.8550911545753479, "The Presentation Date of the BEESAT-3 Satellite is Oct. 10-13, 2012."]
[8.986495971679688, 5.215695381164551, "The Attitude Control Stability of the BRITE spacecraft Satellite is 1 arcmin rms."]
[9.422112464904785, 0.9663544297218323, "The Duration of the Performance Tests Process is Over long periods of time (many orbits)."]
[10.039527893066406, 4.023439407348633, "The Development Location of the NEA Scout Spacecraft is NASA Marshall in Huntsville, Alabama, and JPL in Southern California."]
[6.230449199676514, 3.9699904918670654, "The Testing Location of the Gaia SVM Satellite is EMC chamber at Intespace, Toulouse."]
[5.730749130249023, 1.993857502937317, "The Fairing Envelope Requirement of the TacSat-4 Satellite is Must fit within the fairing envelope of the Minotaur IV launch vehicle."]
[7.553055763244629, 0.4593695402145386, "The Launch Date of the JPSS-2 Satellite is 2019."]
[7.576392650604248, 3.663013219833374, "The Daily system capacity of the WorldView-4 Satellite is 1x."]
[9.318751335144043, 5.771697998046875, "The FDC Algorithms of the ACS Attitude Control System is Included in ACS flight software (FSW)."]
[8.75393295288086, 7.487336158752441, "The Number of Piezoelectric Sensors of the IS Diaphragm is 5."]
[4.090804576873779, 4.443427562713623, "The Process of the Personal Computer Computer is Plug-and-play."]
[6.955138683319092, 11.289068222045898, "The Wavelength FWHM of an unresolved line of the Spectrometer Instrument is 0.020 \u00b5m."]
[6.130622386932373, 6.726766109466553, "The Doppler Correction of the Communication System Satellite Subsystem is Pre-correcting Doppler."]
[5.1008172035217285, 2.057140588760376, "The Number of Experiments of the SMART-1 Satellite is 7."]
[11.84333324432373, 1.008840799331665, "The Landing Date of the Chang'e-4 Mission is 3 January 2019."]
[9.422929763793945, 4.437993049621582, "The Ballistic Coefficient of the SpinSat Spacecraft is Well-determined and characterized."]
[10.269953727722168, 3.010406017303467, "The Altitude of the Meteor-M2 Satellite is ~ 825 km."]
[5.444746017456055, 1.318319320678711, "The Location of the NanoRacks LLC Company is Houston, TX."]
[6.2373366355896, 5.014172077178955, "The Data Access Level of the SAPHIR and SCARAB Instruments is 1A and 1A2."]
[5.025963306427002, 3.7789063453674316, "The Components of the Central Propulsion Module Propulsion Module is Propellant tanks, LAE (Liquid Apogee Engine), East panel with the L-band antenna feed, West panel with the IOL (Inter Orbit Link) antenna."]
[10.238892555236816, 5.678177356719971, "The Operation of the Tether System Satellite Component is Voltage is on when the tether moves downwind with respect to the plasma ram flow and off when it moves upwind."]
[2.090776205062866, 3.886592388153076, "The Power Source of the Jason-3 Satellite is Two solar panels."]
[5.665773391723633, 9.178613662719727, "The Power Consumption of the Instrument Interface Module Interface Module is ~350 mW."]
[8.541923522949219, 1.3333792686462402, "The Image Production of the GOCI Geostationary Ocean Color Imager is 3 times per day."]
[11.748534202575684, 5.001175403594971, "The Distance from Earth of the GRB 150101B Gamma Ray Burst is About 1.7 billion light years."]
[8.662674903869629, 8.955099105834961, "The Spectral Ranges of the Dichroics Optical Component is 4."]
[5.65892219543457, 5.017331123352051, "The Backup Location of the PAZ SAR Processor Ground Segment Processor is Maspalomas (Canary Islands)."]
[11.608263969421387, 6.127588272094727, "The Exposure Time per Frame of the XMM-Newton X-ray Observatory is About three minutes."]
[8.551139831542969, 6.950970649719238, "The Uncertainty of the . Magnetometer Instrument is \u00b114 nT."]
[5.88602876663208, 6.645890712738037, "The System Mode of the KaRIn Radar is Non Ping Pong mode."]
[8.382593154907227, 8.877845764160156, "The Spectral Cube Size of the Observation Instrument Telescope/Spectrograph is 1900 (spectral) x 1150 (spatial)."]
[8.999138832092285, 5.188693046569824, "The Tolerance of the SVOM Attitude Satellite Attitude is 5\u00b0."]
[9.154698371887207, 8.04073715209961, "The LYSO crystals of the Range Calorimeter Particle Detector is Height of 4 cm."]
[11.639065742492676, 6.158747673034668, "The Data Collection Period of the XMM-Newton Satellite is 2016 and 2018."]
[5.177192211151123, 3.0692291259765625, "The Observation Type of the DICE CubeSats Satellite is Plasma."]
[11.677797317504883, -1.1664003133773804, "The Mass of the M3S Satellite is 2800 kg."]
[5.1018385887146, 3.004918098449707, "The Delivery of the CAPSTONE 12U CubeSat is Rapid commercial delivery."]
[8.089646339416504, 4.662535667419434, "The Spatial Resolution of the Oceanography Basin scale Satellite is 200 km."]
[9.216100692749023, 5.824835777282715, "The Interaction with Magnetic Fields of the Cosmic Rays Charged Particles is Their path is bent by magnetic fields."]
[9.975203514099121, 1.4457913637161255, "The Period of the WV-1 Satellite is 94.6 minutes."]
[7.34358024597168, 1.0056709051132202, "The Product Specification Date of the RadidEye Imagery Satellite Imagery is January 2016."]
[4.0123419761657715, 2.347460985183716, "The Spacecraft Size of the ArgoMoon CubeSat is 6U."]
[11.837864875793457, 1.0203790664672852, "The Components of the Chang'e-5 Lunar Mission is Orbiter, lander, ascender and reentry module."]
[5.518702507019043, 3.728562831878662, "The Identification Time of the CSpOC Catalog Catalog is L+20."]
[9.565800666809082, 3.8731820583343506, "The Sponsors of the CanX-7 Satellite is 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."]
[10.354875564575195, 9.616480827331543, "The Development Time of the IRIS Payload is One year."]
[5.257343292236328, 5.212707042694092, "The Accuracy of the UFF TLE Data Product is Less Accurate."]
[4.1536173820495605, 5.6605448722839355, "The Maximum Daily High-Speed Downlinks of the NEMO-AM Satellite is 2."]
[7.7625956535339355, 1.5818250179290771, "The Conference Presentation Date of the Near Earth Asteroid Scout Satellite is 2-9 March 2019."]
[1.062290906906128, 4.293970108032227, "The Li-ion Battery of the EPS Electric Power Subsystem is ABSL (UK), 35 kg, 126 Ah."]
[4.728898048400879, 1.7998095750808716, "The Number of Satellites of the Satellite Constellation Non-Geostationary Satellites (NGS) is 4425."]
[8.933009147644043, 2.095993995666504, "The Public Engagement of the New Horizons Spacecraft is Broke NASA records, touched lives, and awed the world."]
[5.540844917297363, 6.14032506942749, "The Number of Elements of the ICEYE SAR Antenna Antenna is 5."]
[11.594441413879395, 0.7504444122314453, "The Spacecraft Weight of the Tianwen-1 Mars Mission is Five-ton."]
[4.954167366027832, 7.083893775939941, "The Measurement Parameters of the CITRIS Receiver is Total electron content (TEC) and scintillation parameters."]
[6.891228675842285, 7.280942440032959, "The Technology Readiness Levels of the SWOT Instruments Instrument is 3 to 5."]
[7.26943302154541, 1.782773494720459, "The Presentation Date of the SWOT Mission Satellite Mission is 2012."]
[5.388143539428711, 1.602880835533142, "The Core Stage of the SLS Rocket Rocket is Assembled with four of the five parts."]
[10.331619262695312, 3.1593973636627197, "The Orbit Altitude of the CBAS Primary Payload is 39,000 km."]
[3.9200940132141113, 2.3217921257019043, "The CubeSat of the Satellite KickSat is 3U."]
[9.85328483581543, 3.11376690864563, "The Freezing Level Height of the GPM Satellite is Higher than 4 km."]
[8.30481243133545, 7.893637657165527, "The Data Transfer of the Webb's Fine Guidance Sensor (FGS) Sensor is Limited communications bandwidth between L2 and Earth."]
[11.550436019897461, 6.316138744354248, "The Observation Date of the XMM-Newton X-ray Telescope is 2016."]
[6.860076427459717, 1.498607873916626, "The Launch Date of the RapidEye Satellite is Unknown."]
[5.038528919219971, 4.889303684234619, "The Location of the EARS Data Receiving Station is Multiple."]
[7.679043292999268, 9.771343231201172, "The Spectral Range of the VNIR Spectrometer Spectrometer is 420 nm to 1000 nm."]
[3.828390121459961, 6.287335395812988, "The Modulation of the TT&C Data Communication is MSK (Minimum Shift Keying)."]
[4.584073543548584, 6.608645915985107, "The Manufacturer of the LF Receiver Receiver is Sierra Lobo Inc.."]
[6.564359664916992, 2.7126972675323486, "The Manufacturer of the SPIDER Imaging System is Lockheed Martin."]
[9.300843238830566, 5.769845008850098, "The Size of the iADCS100 Attitude Determination and Control System is Two standard CubeSat PCBs."]
[7.463018417358398, 2.5211875438690186, "The URL of the Rosetta Satellite is http://sci.esa.int/rosetta/55295-getting-to-know-rosetta-s-comet/."]
[5.098853588104248, 7.009860515594482, "The RF Bandwidth (MHz) of the Antenna Reflector is 600."]
[8.204142570495605, 5.399895668029785, "The Spatial Resolution of the IRS Sounder Satellite is 800 m at SSP."]
[8.686467170715332, 7.09637975692749, "The Number of Voltage Probes of the FIELDS suite Sensor Suite is 5."]
[6.175344944000244, 2.6429500579833984, "The Location of the Tyvak 61C Satellite is Irvine CA, USA."]
[6.241147994995117, 7.787675857543945, "The Polarization of the ICI-6 Radiometer is V."]
[8.286086082458496, 10.244377136230469, "The Height of the Spectral Block Focal Plane Component is 240 pixels."]
[11.778261184692383, -1.029557704925537, "The Propellant Mass of the XMM-Newton Satellite is 140 kg."]
[12.145483016967773, 3.2337493896484375, "The Inclination of the Beijing-1 Satellite is 98.8\u00ba."]
[11.696660041809082, 2.5962774753570557, "The Diameter of the Didymos Asteroid is 780 m."]
[6.074582099914551, 5.779892444610596, "The NESZ of the TerraSAR-X SAR System is Unknown."]
[8.604785919189453, 1.7483018636703491, "The Ground System Review Date of the Roman Space Telescope Space Telescope is 24 July 2020."]
[2.3264636993408203, 4.446019649505615, "The Power of the Capability Satellite is 24 W."]
[6.515374660491943, 7.785579204559326, "The Laser Diodes Wavelength of the SILEX Terminal is 0.8 to 0.86 \u00b5m."]
[10.142065048217773, 3.045761823654175, "The Altitude of the TSX and TDX Satellites is About 514 km."]
[8.172195434570312, 4.9866108894348145, "The Geolocation accuracy of the ALOS-3/PRISM-2 Satellite is Better than PRISM."]
[8.66942024230957, 5.328582763671875, "The Rate Stability of the QuikTOMS spacecraft Satellite is < 0.01\u00ba/s."]
[6.707671642303467, 6.179228782653809, "The Swath Width of the ISS-RapidScat Scatterometer is Similar to the EUMETSAT ASCAT (Advanced Scatterometer)."]
[6.5185866355896, 7.500947952270508, "The Sub-contractor of the Laser Transmitter Laser is TESAT."]
[9.335105895996094, 5.690011024475098, "The Measurement of the DFACS Attitude Control System is Accurately measures the spacecraft accelerations in 6-DoF (Six Degrees of Freedom)."]
[3.6780738830566406, 6.451260566711426, "The Data Compression Steps of the RFA Computer Signal Processing Device is 3."]
[8.438267707824707, 1.6925441026687622, "The Launch Year of the ATHENA Advanced Telescope for High-ENergy Astrophysics is 2031."]
[4.189177989959717, 3.707554817199707, "The Global Average Detection Rate of the exact Earth Satellite AIS Receiver is 42 Messages/s."]
[10.617918014526367, 6.0564398765563965, "The X-Ray Flares Count of the RHESSI Satellite is Forty Thousand."]
[2.941876173019409, 6.727257251739502, "The Electrical Power of the TXS S-band Transmitter/Transceiver is 4 W."]
[7.196578025817871, 2.201280117034912, "The Collaboration Members of the IceCube-Gen2 Satellite is M. G. Aartsen, R. Abbasi, M. Ackermann, .... M. Z\u00f6cklein."]
[7.290700912475586, 6.738874912261963, "The Operational Mode of the Aquarius Radiometer System is  Survival."]
[7.285738468170166, 0.5474473834037781, "The Launch Date of the Light-1 Satellite is December 21, 2021."]
[9.56968879699707, 5.497830867767334, "The Subsystem Type of the AOCS Attitude and Orbit Control Subsystem is Attitude and Orbit Control."]
[9.002342224121094, 5.1735734939575195, "The Attitude Prediction Accuracy of the ISS Satellite is Approx 0.2\u00ba for up to 4 days."]
[9.366434097290039, 9.469755172729492, "The Photodetector Sensing Area Size of the Optical Head Optical Device is 6.66 mm x 5.32 mm."]
[9.529155731201172, 0.5691820383071899, "The Orbital Lifetime of the InflateSail Satellite is 72 days."]
[9.257570266723633, 4.169692516326904, "The Size of the MEPSI Satellite is 100 mm x 100 mm x 125 mm."]
[11.753405570983887, 1.1755484342575073, "The Landing Camera (LCAM) of the Chang\u2019e-4 Lander Lander is Payload."]
[11.851334571838379, 1.0157811641693115, "The Measurement Date of the Chang'e-4 Lunar Probe is 15 August 2020."]
[4.149255275726318, 6.545065879821777, "The Frequency of the Downlink Signal is 880f0."]
[6.8375725746154785, 1.974051594734192, "The Rainfall Accumulation Observation Period of the GPM Satellite Mission is May 27 to June 5, 2020."]
[8.262520790100098, 6.333841800689697, "The Conference Presentation of the Sensor Web Sensing System is 7th International Symposium Reducing the Costs of Spacecraft Ground Systems and Operations (RCSGSO 2007)."]
[11.111366271972656, 6.7969441413879395, "The Detector of the SEXTANT Technology is Required to provide source and background count rates."]
[8.337115287780762, 5.171624183654785, "The Precision of Post Event Processing of the GF-3 Satellite Satellite is Better than 20 cm (1\u03c3)."]
[6.0936055183410645, 3.0343434810638428, "The Service Commissioning Status of the Lacuna Space Company is Underway."]
[6.189718723297119, 0.855096697807312, "The Launch Date of the Argos-4 Satellite Instrument is November 26, 2022."]
[3.545114755630493, 4.732931137084961, "The Type of the Microprocessor Hardware is 32-bit ~200 MHz ARM."]
[10.362466812133789, 4.467995643615723, "The Mission Duration of the Electric Thruster Thruster is 2.5 years."]
[6.99658203125, -0.09123451262712479, "The End of Life Date of the COMS Satellite is 1 April 2021."]
[9.102073669433594, 10.662103652954102, "The Calibration Mode of the LISS-3 camera Camera is Pulsed."]
[6.301305770874023, 3.27262282371521, "The Outreach Program of the EduSat Satellite is Italian Space Agency."]
[10.47853946685791, 7.573256015777588, "The Interface Bracket Material of the ASM Satellite Component is CFRP (Carbon Fiber Reinforced Polymer)."]
[8.088003158569336, 5.618044853210449, "The Position Determination Accuracy of the XNAV Navigation System is Expected to be on the order of hundreds of meters."]
[7.8150553703308105, 9.091083526611328, "The NER of the Spectral Band D Spectrometer is 5.2 x 10^-7 W/(cm^2 sr \u00b5m)."]
[3.4541075229644775, 5.288506984710693, "The Data Storage of the Sentinel-1 Satellite is Large on-board science data storage."]
[6.2049641609191895, 3.9378468990325928, "The Data Downlink Frequency of the GFO Satellite is Real-time at sea, approximately every 12 hours at CONUS ground sites."]
[7.517666816711426, 9.837220191955566, "The FOV of the Hyperion Imaging Spectrometer is 0.624\u00ba."]
[11.865089416503906, 0.994338870048523, "The Goal of the Chang'e-5 Lunar Mission is Establish an international lunar research station."]
[10.972330093383789, 6.955158710479736, "The Temperature Range of the XRT X-Ray Telescope is 0.5 to 20 MK."]
[4.303402423858643, 5.59202766418457, "The Tape Recorder of the CBERS-1 Satellite is High Density Tape Recorder (HDTR)."]
[5.980875015258789, 1.6110312938690186, "The Operational Status of the PAZ Satellite is Unknown."]
[6.10434627532959, 3.8014299869537354, "The Function of the VISTA Satellite is Complement AERO."]
[5.844651222229004, 5.276939868927002, "The Purpose of the Jamming and Spoofing Protection Mechanisms Security System is Safeguard Galileo signals."]
[9.364062309265137, 4.220252513885498, "The Solar Array Span of the Resurs-DK1 Spacecraft is about 14 m."]
[6.8906683921813965, 4.026212215423584, "The Function of the CIRAS Satellite is Measuring temperature and water vapor profiles."]
[5.046212196350098, 2.018217086791992, "The NASA Instruments of the Rosetta spacecraft Spacecraft is Three."]
[7.228428363800049, 3.1308555603027344, "The Mission Status of the ALL-STAR Satellite is Unknown."]
[9.280326843261719, 6.017301082611084, "The Range of the Pitch momentum wheel Actuator is \u00b11.7 mNms."]
[5.9945759773254395, 8.968086242675781, "The Power Consumption of the MI Radiometer Instrument is < 195 W."]
[7.756547927856445, 13.182250022888184, "The Pixel Resolution of the SPIM2 Spectrometer is 14 bit."]
[9.93074893951416, 7.748162269592285, "The Low Energy Telescope Energy of the CRS Cosmic Ray Subsystem is 5MeV."]
[7.021748065948486, 0.18802085518836975, "The Clone Date of the Satellite Vu\u2019s original satellite Satellite is July 21, 2022."]
[6.414529800415039, 2.9832396507263184, "The Capability of the Carbonite Smallsat Satellite is Multi payload."]
[8.279504776000977, 4.595219612121582, "The Swath Width of the Satellite Imaging Satellite is 48 km."]
[4.905183792114258, 3.657608985900879, "The Lower Module Components of the Merlin Satellite Device is `generic processor board', power conditioning, microprocessor, analog-to-digital converter, memory, I/O ports, data interfaces."]
[2.0908584594726562, 4.793346405029297, "The Power Output of the Fission Surface Power System Power System is Up to 10 kilowatts."]
[6.710043430328369, 10.083288192749023, "The Band of the Nighttime SST Product Dataset is Band 7 (3.9 \u00b5m wavelength)."]
[9.168791770935059, 5.525781154632568, "The Attitude Control System of the NorSat-3 Satellite is Star tracker, attitude sensors and reaction wheels."]
[2.2657949924468994, 3.8410825729370117, "The Type of the Solar Arrays Satellite is Articulating."]
[11.768739700317383, 4.549510478973389, "The Typical Number of Stars of the Young Moving Groups Stellar Groups is Only a few tens of stars."]
[8.500423431396484, 4.615482330322266, "The Method of the Cluster spacecraft Satellite is Triangulation."]
[7.860647201538086, 9.074862480163574, "The Spectral stability of the UV/VIS Spectrometer Spectrometer is 0.04 nm."]
[5.8883280754089355, 3.1542274951934814, "The Experimental Payloads of the DoT-1 satellite Satellite is Flying further experimental payloads as part of SSTL\u2019s ongoing R&D program."]
[6.9038777351379395, 0.560818076133728, "The Launch Date of the GeoEye-1 Satellite is Sept. 2008."]
[4.397592067718506, 7.7498931884765625, "The Center Frequency of the Channel 4 Sensor is 31.5 GHz."]
[5.406010627746582, 1.9345210790634155, "The Status of the P-PODs Device is Needed to be de-manifested."]
[6.580087184906006, 4.157651901245117, "The Data Availability of the Sentinel-3 Satellite Constellation is Full, free and open basis."]
[7.124420166015625, 7.11807107925415, "The Operation Period of the TOMS Instrument is October 1978 to May 1993."]
[9.526172637939453, 8.151153564453125, "The Spectrometer Components of the Natalya-2M High energy radiation spectrometer is Two spectrometers, eight scintillation modules with CsI(Tl) crystals each, anti-coincident protection detectors from polystyrene."]
[10.05650806427002, 4.860833644866943, "The Propulsion Systems of the MEV-1 Satellite is Hybrid chemical and electric."]
[7.682112216949463, 9.95757007598877, "The VNIR Channels of the PROBA-V Satellite is 3."]
[11.667574882507324, 2.596275806427002, "The Diameter of the Potentially Hazardous Asteroid (PHA) Asteroid Type is ~140 m or larger."]
[1.79881751537323, 4.848296165466309, "The Peak Power of the EPS Electric Power Subsystem is 230 W."]
[7.273159027099609, 4.51870059967041, "The Band 3 of the Landsat TM Satellite is Chlorophyll absorption, plant type discrimination."]
[11.623358726501465, 4.509307384490967, "The Surface Temperature of the Zeta Puppis Star is Seven times hotter than our sun."]
[8.997339248657227, 7.303842544555664, "The Photodiodes per Suite of the Sun Sensor Suites Sensor is 4."]
[6.827462673187256, 1.663679599761963, "The Presentation Date of the CEBRAS SAR System is July 26-31, 2015."]
[4.793859004974365, 1.8445557355880737, "The Number of Satellites of the DMSP (Defense Meteorological Satellite Program) Satellite Program is 19."]
[2.21773099899292, 4.448502063751221, "The Power Generation of the Spacecraft Satellite is 450 W @ EOL."]
[11.267337799072266, 4.162145614624023, "The Number of Planets of the TOI-178 Exoplanet System is 6."]
[4.422379016876221, 2.4472289085388184, "The Type of the ALL-STAR Satellite is 3U CubeSat."]
[11.20402717590332, 2.898272752761841, "The Diameter of the Von K\u00e1rm\u00e1n crater Lunar Crater is 180 km."]
[11.582235336303711, 2.6574978828430176, "The Discovery Year of the Lutetia Asteroid is 1852."]
[1.9725875854492188, 3.898637533187866, "The Cover Glass Thickness of the TFSC Thin Film Solar Cell is 0.1 mm."]
[8.91470718383789, 3.2849233150482178, "The Orbit of the CSSWE Satellite is Low Earth Orbit."]
[9.208386421203613, 9.055327415466309, "The Typical high cadence of the HRI Lyman-\u03b1 1216 \u00c5 Passband center is Sub-second."]
[7.542817115783691, 6.205617427825928, "The Purpose of the EMIT Imaging Spectrometer is Map the surface composition of minerals in Earth\u2019s dust-producing regions."]
[9.486236572265625, 1.0659334659576416, "The Duration of the Orbital Express Satellite Mission is 3 months."]
[10.079741477966309, 1.4758317470550537, "The Period of the Anand Satellite is 94.6 minutes."]
[10.823698043823242, 3.9413514137268066, "The Data Volume of the Nancy Grace Roman Space Telescope is 20,000 terabytes (20 petabytes) over the course of its five-year primary mission."]
[7.589913368225098, 3.1455166339874268, "The Status of the CartoSat-2B Satellite is Operational."]
[5.353396892547607, 5.488921642303467, "The Number of Stations of the Satellite Laser Ranging Stations Tracking Stations is 3 in Russia, 10 outside Russia."]
[6.880732536315918, 3.5986671447753906, "The Operational of the BDS-3 Satellite System is Yes."]
[7.476997375488281, -0.004899079445749521, "The Number of Professionals of the SAOCOM-1A Satellite is As many as 600."]
[6.94715690612793, 5.362452983856201, "The Monitoring Purpose of the SMOS Satellite is Antarctic ice sheet."]
[5.466762065887451, 4.518060207366943, "The Ground Stations of the HYPSO-1 Satellite is KSAT Puertollano, Spain."]
[9.457144737243652, 2.5205156803131104, "The Number of Planned Propulsive Maneuvers of the ICE (International Cometary Explorer) Spacecraft is 4."]
[8.067570686340332, 9.734922409057617, "The Band Spacing of the NIR Detector is 11.4 nm."]
[9.789933204650879, 1.571556806564331, "The Direct Transmission Delivery Time of the Polar Satellite Data Data is Virtually at the time of measurement."]
[6.29825496673584, 8.258956909179688, "The Operating Frequencies of the SMMR Microwave Radiometer is 21.0 GHz."]
[3.803954601287842, 5.810484409332275, "The Data Rate of the IREI Data Source is 1.92 Mbit/s."]
[2.231097459793091, 4.44392728805542, "The Power of the Power Satellite is 275 W."]
[5.196368217468262, 4.657905101776123, "The Functions of the ARF Acquisition & Routing Facility is Second level of synchronization, generation of ISP files and routing to the Nominal PDGS or the Defence one."]
[7.631114482879639, 2.434295654296875, "The Symposium Date of the NISAR Spaceborne SAR Mission is 21-26 July 2013."]
[7.807023525238037, 2.581062078475952, "The Ground Sites of the ARTEMIS Satellite is MOD (Ministry of Defense) ground sites."]
[9.1000337600708, -0.5740982294082642, "The Launch Date of the GomX-4B Nanosatellite is 2 February 2018."]
[6.504304885864258, -0.5333603620529175, "The Operation Declaration Date of the QZS-1/Michibiki Satellite is July 2011."]
[8.894576072692871, 8.341796875, "The Geometric Factor of the ELENA Sensor is 2 x 10 -5 cm 2 sr."]
[9.984953880310059, 7.210470199584961, "The Purpose of the Thermal Shrouds Thermal Isolation is Isolate the cold detector plate from the warm ROEs."]
[8.792501449584961, 6.548442840576172, "The Mounting of the LAD Instrument is Rotating actuator platform."]
[4.235922813415527, 6.615356922149658, "The Frequency of the RF Output Frequency Communication System is 2214.97 MHz."]
[4.9574408531188965, -3.115478515625, "The Affiliation of the Nobuo Sugimura Author is Unknown."]
[6.749238967895508, 1.7064950466156006, "The Launch Date of the Envisat Satellite is March 01, 2002."]
[4.930398464202881, 9.185733795166016, "The Data Monitor of the Seismic Experiment for Interior Structure (SEIS) Seismometer is Marsquake Service."]
[10.177084922790527, 2.986835241317749, "The Altitude of the GEO Satellite Satellite is About 35,800 km."]
[9.712688446044922, 8.677471160888672, "The Number of Mirrors of the Shafer Telescope Optical System is 5."]
[8.848184585571289, 7.391293525695801, "The Function of the V1-V4 Voltage Probes Sensor is Current-biased double probe electric fields sensors and capacitively-coupled radio and plasma wave sensors."]
[10.346800804138184, 5.667855739593506, "The Launch Date of the ProSEDS Tether Demonstration Experiment is 2003."]
[5.8128485679626465, 0.8190664052963257, "The Uptime of the AlSat Nano Satellite is 27.4 days."]
[11.062971115112305, 5.255232810974121, "The Magnetic Field Strength of the Rho Ophiuchi A Star is 500 times stronger than that of the Sun."]
[2.245668649673462, 4.342897891998291, "The Power of the DubaiSat-1 Satellite is 53.2 W."]
[10.286304473876953, 6.777963161468506, "The Spacecraft Mass of the TCS Thermal Control System is 55 kg."]
[6.094629287719727, 0.593381404876709, "The Launch Date of the CubeSat ELaNa III Satellite is October 2011."]
[7.973855495452881, 0.2526656687259674, "The Structure Tolerances of the CXBN-2 Spacecraft is Better than \u00b10.1 mm."]
[7.057690620422363, 3.6961936950683594, "The Data Access of the Landsat-7 Satellite is Free access to the entire user community."]
[11.392860412597656, -1.3638479709625244, "The Weight of the PeruSat-1 Satellite is Up to 500 kg."]
[7.647345542907715, 4.752836227416992, "The Measurement Range of the ACE Mission Satellite is Low energies of the solar wind up to the high energies of the galactic cosmic rays."]
[4.40575647354126, 6.323925018310547, "The Uplink Frequency of the Communication System Satellite System is 145.95 MHz."]
[6.330623626708984, 11.88955020904541, "The Baseline Length of the Three-axis diagonal gradiometer Gradiometer is 0.5 m."]
[6.595227241516113, 1.1668100357055664, "The Conference Date of the AlphaSat TDP Operations Support is May 15-17, 2013."]
[11.429534912109375, -1.3374954462051392, "The Weight of the NorSat-3 Satellite is 16 kg."]
[5.441858291625977, 5.611415386199951, "The Compatibility of the NovAtel OEM-615 GPS Module is GOMSpace Nanodock DMC-3 Motherboard."]
[7.335261821746826, 2.1295220851898193, "The Author of the IceCube Satellite is Madeleine O'Keefe."]
[2.106093645095825, 3.986663341522217, "The Mounting Location of the SAWs Solar Array Wings is Externally."]
[7.009279727935791, 0.5554099678993225, "The Loss of Contact Date of the TSUBAME Satellite is January 27, 2015."]
[11.719661712646484, -1.0525792837142944, "The Mass of the Harness Harness is 3 kg."]
[5.923038005828857, 3.42496919631958, "The Responsibilities of the CAS Organization is Propulsion Module, Service Module, Spacecraft Prime, Mission Operations (with ESA contribution), Chinese instruments."]
[10.80610179901123, 3.2691009044647217, "The Rate of Movement Away from Earth of the Moon Celestial Body is 3.8 cm/year."]
[6.0407304763793945, -0.024498917162418365, "The Initial Operations Start Date of the Galileo Satellite Navigation System is December 2016."]
[8.023711204528809, 4.114290237426758, "The Resolution of the EarthDaily Constellation Satellite Constellation is 5-metre."]
[9.40184211730957, 8.707643508911133, "The Substrate Material of the Primary Mirror Optical Component is Fused silica."]
[9.604599952697754, -0.2259497195482254, "The Mission Duration of the AIST-2 Microsatellite is 3 years."]
[9.022615432739258, 6.9460978507995605, "The Accuracy of the Star sensor Sensor is +1.0-6.0 m v 0.02\u00ba (3\u03c3)."]
[5.561426639556885, 6.649729251861572, "The Antenna Length of the Instrument DC Electric Fields Investigation is 60 m."]
[7.520544052124023, 1.8363394737243652, "The URL of the MICROSCOPE Spacecraft is http://missions-scientifiques.cnes.fr/MICROSCOPE/GP_segment_sol.htm."]
[8.025264739990234, 3.443333864212036, "The Mission of the THEMIS Satellite is Uncover the mysteries behind the formation of auroral beads."]
[8.49643325805664, 10.519768714904785, "The Effective Area of the Detector E2V CCD-22 (Frame Store) is 200 cm 2 @ 1.5 keV."]
[8.137323379516602, 11.12016773223877, "The Type of the Linear Encoder Sensor is Non-contacting."]
[10.431600570678711, 8.417350769042969, "The Mass of the MiniCOR Coronagraph is <3.6 kg."]
[7.8534393310546875, 1.8910739421844482, "The Arrival Date at Mars of the ExoMars 2020 Mission is March 2021."]
[3.871772050857544, 2.3096883296966553, "The Size of the APSS-1 Satellite is 1U CubeSat."]
[5.287602424621582, 5.685080528259277, "The Operating Mode of the T3000G2 receiver GPS Receiver is Dual-frequency mode."]
[7.078395366668701, 4.943803310394287, "The Sensor Type of the SeaWiFS Satellite is Scanning telescope."]
[3.132943868637085, 5.88134241104126, "The Flexibility of Satellite Operations of the MTP Transponder is True."]
[7.5745320320129395, 9.6003999710083, "The Number of Spectral Bands of the ERIP Earth Remote-Sensing Imaging Package is 7."]
[11.84866714477539, 1.009405255317688, "The Landing Date of the Chang'e-5 Lunar Probe is 1 December 2020."]
[9.589956283569336, -0.640766441822052, "The Onboard Innovations of the PROBA-1 Microsatellite is Gallium-arsenide solar cells, star trackers for gyroless attitude control, lithium-ion batteries, ESA\u2019s first ERC32 microprocessors."]
[9.229493141174316, 3.0737648010253906, "The Science Mission Orbit of the LRO Satellite is Quasi-circular orbit (50 \u00b1 15km)."]
[8.07433795928955, 11.141901969909668, "The Sensitivity of the Channel 5 Sensor is 0.3 K/pixel."]
[4.245105743408203, 4.771917343139648, "The Data Encoding of the MIU Interface is CCSDS."]
[4.142412185668945, 6.701663494110107, "The Operating Frequency Range (TC) of the EWC31 S-band transceiver module Communication Module is 2025-2110 MHz."]
[4.417721271514893, 4.098819255828857, "The Availability of the Avionics Components Components is Flight model version."]
[9.042566299438477, 8.678627967834473, "The Mirror Rotation Capability of the TIR Subsystem Imaging System is 180\u00ba from the nadir position."]
[6.762638568878174, 3.2021875381469727, "The Mission of the CEDEX Payload Payload is GIOVE-A."]
[6.638180732727051, 2.294508934020996, "The Constellation Partners of the GPM Constellation Satellite Constellation is 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."]
[5.8594160079956055, 6.838803291320801, "The Pulse Repetition Interval of the RainCube Radar is 1660 \u00b5s."]
[6.828115463256836, 0.719359278678894, "The Test Completion Date of the Integrated Circuit Boards Hardware is June 2019."]
[8.430814743041992, 7.682833671569824, "The Data Display of the TechDemoSat-1's radiation monitor Radiation Monitor is Google Earth."]
[7.3304033279418945, 2.6954691410064697, "The URL of the FORUM Mission is https://www.esa.int/Our_Activities/Observing_the_Earth/Two_new_Earth_Explorer_concepts_to_understand_our_rapidly_changing_world."]
[7.24747371673584, -0.749965488910675, "The Contacted Satellites of the CYGNSS Satellite Constellation is Eight."]
[11.71870231628418, 7.512674331665039, "The Purpose of the Ultra Stable Oscillator (USO) Oscillator is Precise time tagging."]
[8.186591148376465, 3.2533442974090576, "The Data Processing of the TanDEM-X Satellite is More than 400,000 datasets."]
[5.314202785491943, 10.387889862060547, "The Data-handling infrastructure of the LIS Lightning Imaging Sensor is TRMM."]
[8.524283409118652, 1.7211698293685913, "The Presentation Date of the Membrane Photon Sieve Space Telescope Telescope is May 21, 2013."]
[7.623686790466309, 1.0204505920410156, "The Announcement Year of the European Sentinel Satellites Satellite is 2020."]
[5.021575450897217, 4.482641220092773, "The Delivery of the CSG GS Ground Segment is Responsible for the delivery to the final user."]
[10.334980010986328, 2.9807913303375244, "The Orbit Altitude of the PhiSat-1 Satellite is About 329 miles (530 km)."]
[7.66164493560791, 3.3817098140716553, "The Data Availability of the Landsat 5 TM Satellite is All TM data December 2008."]
[5.646646022796631, 0.3938019871711731, "The Date of the West coast wildfires Natural Disaster is 11 September 2020."]
[7.907493591308594, 7.1438798904418945, "The In-Flight Calibration Strategy of the TRUTHS Reference Sensor is Radiometric gain/bias, linearity, spectral performance."]
[3.9579691886901855, 6.404987335205078, "The Modulation of the Transmitter Communication Device is 1200 bit/s FSK / 1 bit/s CW."]
[2.3708763122558594, 5.565134525299072, "The Conversion Type of the ADC Analog-to-Digital Converter is Linear analog to digital conversion of dV in 256 channels."]
[1.3465784788131714, 4.1841816902160645, "The Maximum Battery Power in Uncontrolled Tumble of the Satellite Spacecraft is 3 hrs."]
[9.36287784576416, 8.036810874938965, "The Operating Temperature of the CCD Charge Coupled Device is 155 K."]
[8.504844665527344, 6.755486011505127, "The Developer of the Magnetometer Sensor is GAUSS team."]
[7.61610746383667, 2.0447142124176025, "The Presentation Date of the Remote Sensing Activities Activity is Feb. 6-17, 2012."]
[10.077144622802734, 1.3933806419372559, "The Local Time of Ascending Node of the Satellite Communication is 9:15 AM."]
[9.815325736999512, -0.9738281965255737, "The Spatial Resolution of the JL-1-GF03D Microsatellite is 0.75 m."]
[3.6063010692596436, 6.564108848571777, "The Data Transmission Rate of the RF Communications Transmitter is 9.6 to 100 kbit/s in S-band."]
[8.121603965759277, 9.767082214355469, "The Moving Mirror Scan Time of the MSASI Imager is 80 seconds."]
[4.998341083526611, 5.253138542175293, "The Number of Stations of the SVOM VHF Network Ground Station Network is 45."]
[7.648429870605469, 1.6697874069213867, "The Mission Start Date of the SMAP Satellite is March 3, 2012."]
[1.7504583597183228, 4.7669782638549805, "The Nominal power generation of the EPS Electric Power Subsystem is 2 W."]
[8.734155654907227, 7.1884965896606445, "The Error (RMS) of the Rate sensor Sensor is <0.05/s."]
[6.87378454208374, 10.002437591552734, "The Bandwidth of the Band 1 Spectral Band is 402-422 nm."]
[7.619743347167969, 5.259753227233887, "The Instruments of the Solar Orbiter Satellite is In-situ instruments and Remote sensing equipment."]
[8.899441719055176, 8.211938858032227, "The NE\u0394T @ specified scene temperature of the Instrument Spectral Imager is 0.3-1.2 K @ 250 K."]
[4.826900005340576, 1.8908525705337524, "The Number of Satellites of the FFRF Subsystem Relative Positioning System is 2 to 4."]
[8.062294960021973, 0.8705272078514099, "The Launch Date of the Landsat-9 Satellite is December of 2020."]
[8.887043952941895, 1.8812915086746216, "The Presentation Date of the BepiColombo Mission is 2012."]
[8.498231887817383, 9.568577766418457, "The Active Area of the ICON FUV Instrument Detector is 25 mm (circular)."]
[8.899995803833008, 0.7442167401313782, "The Science Mission Duration of the RapidScat Instrument is Two years."]
[5.349189281463623, 3.132561683654785, "The Constellation Architecture of the CIRCE Mission is Dual satellite bus."]
[6.354986667633057, 4.965891361236572, "The Description of the Orthorectified Product (L1C) Data Product is 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)."]
[6.7157368659973145, 4.2891950607299805, "The Former Name of the Copernicus Program is GMES."]
[6.297402858734131, 8.220349311828613, "The 18.7 GHz Channel Function of the JMR Microwave Radiometer is Correction for effects of wind-induced enhancements in the sea surface background emission."]
[7.991197109222412, 5.067663669586182, "The Orbit Localization Accuracy of the WEOS Satellite is About 30 m."]
[7.439635276794434, 8.448508262634277, "The Signal-to-Noise Ratio of the SNR Spectrometer is \u2265 100."]
[10.337708473205566, 5.176367282867432, "The Thrusting Modes of the T3\u00b5PS Micropropulsion System is Continuous thrust mode, Burst thrust mode."]
[7.4491868019104, -0.2271358072757721, "The Reentry Date of the Long March 5B Rocket Stage is 9 March 2021."]
[8.1865816116333, 8.48552417755127, "The Distortion of the SHS Interferograms Interferometer Output is Figure errors distort the individual (carrier) fringes to a greater extent than the envelope (visibility) of the fringes."]
[8.027122497558594, 6.568878173828125, "The Frequency of the Solar Measurements Instrument is Every orbit."]
[4.552188396453857, 3.6652791500091553, "The Monitoring of the AIS Automatic Identification System is Ships."]
[5.98895788192749, 2.7188034057617188, "The Deputy CEO of the Galileo 2nd Generation Satellites Satellite is Massimo Claudio Comparini."]
[5.6514506340026855, 9.160799026489258, "The Working Principle of the Instrument Unknown is Balance between the total amount of power received in the first and second half of the Dicke cycle."]
[5.726137638092041, 2.984992027282715, "The Manufacturer of the OPTSAT 3000 Satellite is IAI."]
[5.469761371612549, 2.2612249851226807, "The Observations per Day of the Sapphire Satellite is More than 3000."]
[7.912557125091553, 6.841804504394531, "The Length of Operation of the Full Calibration of HIS Calibration Process is 1 day accumulated."]
[10.249969482421875, 2.918764591217041, "The Altitudes of Operation of the Starlink Satellite Constellation is Around 550 kilometers."]
[4.018216133117676, 4.715043544769287, "The Communication Interfaces of the MCU Microcontroller Unit is Up to 8 communication interfaces."]
[9.214332580566406, 1.5445653200149536, "The Arc Duration of the BepiColombo Spacecraft is Two months."]
[4.393342018127441, 4.602729797363281, "The Function of the Instrument Control Unit (NI-ICU) Control Unit is Housekeeping management."]
[4.074132442474365, 1.2187424898147583, "The Mission Type of the Arachne Satellite is Non-EO."]
[10.288150787353516, 3.1675517559051514, "The Altitude after Five Years of the GRACE Satellite Satellite is About 300 km."]
[9.286325454711914, 0.714323878288269, "The Life Expectancy of the RapidEye Satellite Constellation is 6 years of operations, with full image performance for another 5 or more operational years."]
[10.337382316589355, 4.951540946960449, "The Number of Firings of the IEPS Ion Electric Propulsion System is 22."]
[8.459169387817383, 8.602158546447754, "The Grating Type of the OCO-2 Spectrometer is Regularly-spaced series of grooves on a very flat surface."]
[7.546768665313721, 0.7633830308914185, "The Final Preparations Date of the ESAIL Satellite is 8 July 2019."]
[8.276129722595215, 9.203412055969238, "The Pixels per FWHM of the Spectrometer Instrument is 3030."]
[3.2138843536376953, 5.3035969734191895, "The Storage of the SDR Host Computer Computer is 250 GB SSD."]
[9.770658493041992, 3.0889859199523926, "The Orbit Parameters of the GEOS-2 Satellite is 1,079 km x 1,572 km x 105.8\u00ba."]
[9.533738136291504, 5.517332077026367, "The Field of Regard of the AOCS Attitude and Orbit Control Subsystem is \u00b126\u00ba."]
[7.762622356414795, 10.40939998626709, "The Electronic Outputs Resolution of the SEVIRI Spectral Imager is 10 bit."]
[9.911774635314941, 3.9514458179473877, "The Orbit Duration of the NanoSail-D2 Satellite is 95 days."]
[6.096160411834717, 2.9309206008911133, "The Spacecraft Builder of the Lucy Satellite is Lockheed Martin Space Systems."]
[7.267989635467529, 0.5605648159980774, "The Launch Date of the Solar-A / Yohkoh Satellite is 30 August 1991."]
[7.087976932525635, 5.1972880363464355, "The SO2 Emissions of the San Nicolas refinery Refinery is Roughly 350 kilotons per year."]
[9.850044250488281, 6.60288667678833, "The Temperature of the Tank B1 Fuel Tank is Daily average."]
[11.701238632202148, 2.611290216445923, "The Size of the Didymos B Asteroid is About 530 feet (~160 m) across."]
[9.458514213562012, 2.95607590675354, "The Impact Features of the Eureca Satellite is More than 1000 on the front sides of the solar arrays."]
[10.100845336914062, 2.398996591567993, "The Orbit velocity of the KOMPSAT-3A Satellite is 7.60 km/second."]
[5.216473579406738, 5.589738845825195, "The Ku-band antennas of the Spire Global Satellite is High-capacity."]
[7.859830379486084, 9.087576866149902, "The Spectral Range of the Instrument Spectrometer is 420 nm to 2450 nm."]
[11.798320770263672, -0.9695823192596436, "The Total Mass of the Aquajet Satellite Propulsion System is ~0.5 kg."]
[10.782801628112793, 5.318482398986816, "The Impact on Xenon Consumption of the Solar Activity Natural Phenomenon is Lower than what was expected in the mission design phase."]
[9.389310836791992, 9.976183891296387, "The Capability of the Visible and SWIR Cameras Imaging System is Imaging the Earth's surface and clouds when illuminated by moonlight and the airglow."]
[6.579776763916016, -0.0916682630777359, "The Launch Date of the PSLV-C26 Satellite is Unknown."]
[4.91813850402832, 5.294151306152344, "The Developer of the Transponder Device is Italian company IDS."]
[4.957339286804199, 1.505488395690918, "The Sensor Complement of the FormoSat-7 / COSMIC-2 Satellite Constellation is Unknown."]
[8.413084983825684, 10.472219467163086, "The Bands of the CCD Camera Optical Device is 430-520 nm, 520-600 nm, 630-690 nm, 760-900 nm."]
[5.875603675842285, 3.7748587131500244, "The Manager of the Space Weather Network Network is ESOC."]
[11.215384483337402, 3.498598098754883, "The Distance from the Sun of the Comet 67P/C-G Comet is About 1.7 au."]
[9.931022644042969, -0.5886530876159668, "The Apolune Altitude of the Rstar Data Relay Microsatellite is ~2400 km."]
[8.742497444152832, 4.8028974533081055, "The Altitude of the NEMO-AM Satellite is 650 km."]
[8.39433765411377, 8.879708290100098, "The Effective Area of the Observation Instrument Telescope/Spectrograph is 0.6 cm 2 @ 125 nm."]
[3.1319162845611572, 5.294413089752197, "The Capacity of the Solid State Recorders Data Recorders is 24 GB."]
[8.716774940490723, 2.5787205696105957, "The Maximum Range of the ARTEMIS Spacecraft is 1.2 million km."]
[8.597962379455566, 10.786731719970703, "The Effective Pixel Dimensions of the Kodak KAI-11002 CCD CCD is 4008 x 2672."]
[5.482666492462158, 5.64877462387085, "The Model of the NovAtel OEM-615 GPS Module is NovAtel OEM-615."]
[8.289271354675293, 4.442968368530273, "The Observation Purpose of the Integral Satellite is Measure the cosmic X-ray background."]
[6.763702869415283, 3.08854603767395, "The Mission Status of the FormoSat-1 Satellite is Mission complete."]
[5.884031772613525, 3.838916540145874, "The Instrument Type of the QBITO CubeSat is Imaging multi-spectral radiometers (vis/IR)."]
[8.37137508392334, 10.043083190917969, "The TDI Levels of the Pan band Detector Array is 5 selectable levels from 7 to 20."]
[7.457901477813721, 5.133326053619385, "The Swath Width of the SMAP Satellite is Approximately 1000 km."]
[10.565675735473633, 8.495355606079102, "The Image Sequence Specification of the COR1 Coronagraph1 imager is 3 white light images at 3 different polarization angles."]
[7.9686713218688965, 6.051990032196045, "The Calibration Mode Components of the LIBRA Satellite is Rotating mirror, middle optics, two monochromators, avalanche photodiodes."]
[3.18412446975708, 4.937270641326904, "The Memory of the protos Software is 128 kB of flash memory."]
[8.019391059875488, 8.754122734069824, "The Spectra Captured of the Limb Sensor Sensor is Six."]
[7.482809543609619, 2.91164493560791, "The Role of the Kimiya Yui Astronaut is Manipulate the SSRMS (Space Station Remote Manipulator System) for the operation of capturing Kounotori-5."]
[8.987943649291992, 2.109679698944092, "The Team Size of the New Horizons Spacecraft is About 200."]
[8.090187072753906, 5.595787525177002, "The Vector Components Random Error of the Air Drag Satellite System is < 5 x 10 -8  ms -2."]
[2.235525608062744, 6.504419803619385, "The Latency of the ATL12 Ocean Elevation Data is 45 days from receipt of last data in product."]
[8.969311714172363, 6.918222904205322, "The Ion Drift Velocity of the PAP Plasma Analyzer is -3 ~ +3 km/s."]
[8.402859687805176, 9.487588882446289, "The Color Composition of the False-color image Image is Shortwave infrared, near-infrared, and green light in the red, green, and blue channels of an RGB picture."]
[9.4775390625, 4.411310195922852, "The Dimensions of the Research Facility Facility is 26 inches high, 35 inches wide, 24 inches deep."]
[4.656595230102539, 4.584933757781982, "The Technique of the Level-2 Data Processor is Empirical."]
[4.783942222595215, 4.5174760818481445, "The Integration Levels of the Cooperation by Expansion Data Exchange is Within CSK boundaries and with other EO systems."]
[9.451099395751953, 5.867776393890381, "The Pointing Accuracy of the Attitude Control Subsystem (ACS) Attitude Control System is 0.05\u00b0."]
[6.8102521896362305, 0.7526291012763977, "The Launch Date of the GeneSat-1 Satellite is December 16, 2006."]
[5.230008602142334, 2.476604700088501, "The Technology Readiness Level of the CubeSats Satellite is Higher."]
[8.719545364379883, 8.020926475524902, "The Data Collection Period of the Liulin-MO dosimeter Radiation Dosimeter is Since the spacecraft reached orbit around the planet."]
[7.49902868270874, 6.511579513549805, "The On-Orbit Spectral Characterization Duration of the Terra MODIS Satellite Instrument is Five Years."]
[11.73908519744873, 4.657727241516113, "The Distance from Earth of the GW170817 Gravitational Wave Event is About 130 million light years."]
[7.062758445739746, 7.993778705596924, "The Antenna Aperture Size of the GMI Instrument is 1.2 m."]
[10.596071243286133, 4.79058313369751, "The Testing Focus of the RAMIS Payload is Reduced gravitational force."]
[8.325418472290039, 8.615228652954102, "The Co-Alignment of the OSIRIS Optical Sensor is With a reference spot in the measurement devices."]
[11.112722396850586, 2.516329765319824, "The Heat Shield Material of the Schiaparelli Module is Norcoat Liege."]
[10.466519355773926, 3.5690548419952393, "The Impact Location of the SMART-1 Satellite is 34.262\u00b0 south, 46.193\u00b0 west."]
[4.961676597595215, 6.538471698760986, "The Diagram of the TEC Antennas Antennas is Circular with 3 db."]
[7.0043044090271, 1.6099505424499512, "The Development Date of the China High-resolution Earth Observation System (CHEOS) Satellite System is 2014."]
[7.702258110046387, 9.480184555053711, "The Spatial Resolution of the Visible Spectral Band Spectral Band is 1.25 km x 1.25 km."]
[6.195887565612793, 4.309494495391846, "The Download Time of the QuakeSat Satellite is Premium."]
[7.27500581741333, 0.31950265169143677, "The Constellation Full Operational Date of the Arktika-M N1 Satellite is 2025."]
[8.80734920501709, 6.5968017578125, "The Location of the Translation Stage Actuator is Between the electronics bus and the sail storage area."]
[7.454043865203857, -0.2450471669435501, "The Reentry Date of the Kounotori-6 Cargo Ship is February 5, 2017."]
[4.774345874786377, 7.021584510803223, "The Frequency Bands of the CITRIS Receiver is 401.25 and 2036.25 MHz, 150, 400 and 1067 MHz."]
[7.48479700088501, 7.248728275299072, "The Scan Modes of the CERES on TRMM Instrument is Cross-track, along-track, and rotating azimuth plane (RAP) mode."]
[11.519832611083984, -0.747992753982544, "The Hydrazine Consumption of the Envisat Satellite is 25.8 kg on average per year."]
[7.872666835784912, 9.144989013671875, "The Data Channels of the SAGE-III Spectrometer is 8 spectral channels + 1 zero-order light channel."]
[8.078959465026855, 11.126333236694336, "The Sensitivity of the Channel 7 Sensor is 0.4 K/pixel."]
[7.895019054412842, 4.5529279708862305, "The Horizontal Spatial Resolution of the Tomorrow-R1 and -R2 Satellite is 5 km."]
[10.217918395996094, 2.9615516662597656, "The Altitude of the QuakeSat Satellite is 820 km."]
[6.41521692276001, 5.052311420440674, "The Content of the L2A Products Data is Ground reflectance cube, maps for estimated WV, AOT and image masks for land, water, haze, clouds, cloud-shadows and snow."]
[9.926203727722168, 7.384697437286377, "The Infrared Emissivity of the Cube Corner Reflectors (CCRs) Satellite Component is \u03b5."]
[7.373056888580322, 9.971550941467285, "The Information Source of the Remote Sensing Observation Method is Reflected light in the solar domain."]
[8.72376823425293, 7.783787250518799, "The Science Instruments of the Dellingr Satellite is Boom-mounted fluxgate magnetometer, gated time-of-flight ion-neutral mass spectrometer (INMS)."]
[9.455292701721191, -0.7582340836524963, "The Launch Date of the PROBA-1 Microsatellite is 22 October 2001."]
[4.8374762535095215, 7.007185459136963, "The Environment Requirement of the CITRIS Receiver is Electromagnetically pristine."]
[4.358648777008057, 3.690239906311035, "The Signal Spectrum of the AIS Automatic Identification System is Entire signal spectrum is downloaded for de-collision of the AIS messages."]
[4.375603675842285, 2.5691184997558594, "The Type of the Twin 6U CubeSats Satellite is CubeSat."]
[4.770325660705566, 6.04376220703125, "The Quantity of the Rx Channels Receiver is 2."]
[3.815932512283325, 6.714068412780762, "The TRL of the Myriad RF board RF Board is 3."]
[3.618112325668335, 6.198184967041016, "The Data Rates of the Downlink Communication System is 1.024 to 1048.576 kbit/s."]
[6.82144832611084, 0.46124234795570374, "The Launch Date of the Badr-B Satellite is 10 December 2001."]
[5.827396869659424, 5.2571120262146, "The Equipment of the GPS Spoofing Activity is GSE (Ground Support Equipment)."]
[6.460315704345703, 6.262624263763428, "The HPA of the ASCAT Scatterometer is High Power Amplifier."]
[10.616669654846191, 3.052534818649292, "The Distance Between Satellites of the DICE nanosatellites Satellite is ~300 km."]
[8.407865524291992, 3.3560056686401367, "The Radial Baselines of the Tandem-L Satellite is 0 m to 600 m."]
[9.021990776062012, 9.879481315612793, "The Type of the Photodetector Sensor is 3 mm FCI InGaAs quadrant photodiode with amplifier board."]
[10.645678520202637, 9.217470169067383, "The Image Capture Date of the CaSSIS Camera is 23 April 2020."]
[2.1189393997192383, 3.9861032962799072, "The Solar Panels Span of the INTEGRAL Satellite is 16 m."]
[5.379741191864014, 4.609682083129883, "The Ground Station Locations of the KazSTSAT Satellite is Svalbard, Astana and Guildford."]
[11.753908157348633, 7.487790107727051, "The Authors of the ACES Space Clock Experiment is L. Cacciapuoti, Ch. Salomon."]
[7.243051052093506, 1.5603870153427124, "The Operation Start Date of the Cluster Satellite Mission is 2009."]
[7.416820049285889, 0.8616597056388855, "The Year of Launch of the QuikSCAT Satellite is 1999."]
[7.8153486251831055, 2.1939172744750977, "The Publication Year of the Observation of the Earth and Its Environment: Survey of Missions and Sensors Documentation is 2002."]
[11.699167251586914, -1.1329984664916992, "The Propellant Capacity of the Spacecraft Satellite is 23 kg."]
[1.5730245113372803, 4.58831262588501, "The Efficiency of the SABR DC/DC Converter is Above 95%."]
[3.8140151500701904, 6.174520492553711, "The LEO-to-ground Communication Link Speed of the Optical Ground Station Ground Station is 5.625 Gbit/s."]
[4.041191101074219, 1.2063740491867065, "The Mission Type of the Genesis Satellite is Non-EO."]
[5.998031139373779, 2.9110028743743896, "The Partner of the TanSat Satellite Mission is University of Edinburgh."]
[6.228701591491699, 8.186776161193848, "The Frequency of the MWR Radiometer is 36.5 GHz."]
[10.21294116973877, 3.017814874649048, "The Altitude of the OrbView-2 Satellite is 705 km."]
[4.960135459899902, 5.909131050109863, "The Technology of the Radiating Board Antenna Component is Based on the same technology developed in the frame of CSK."]
[9.003613471984863, 9.172625541687012, "The IFOV of the SAGE-III Instrument is 1-2 km."]
[7.322073459625244, 6.767662048339844, "The Acquisition Date of the MODIS Imaging Spectroradiometer is July 30, 2019."]
[6.726790428161621, 3.7100672721862793, "The Type of the NIU VShE \u2014 DZZ Satellite is Earth Observation spacecraft."]
[4.903261661529541, 1.9743640422821045, "The Number of Satellites of the SAR-Lupe Satellite System is 5."]
[8.114384651184082, 8.479005813598633, "The Optical Path of the IASI-NG Interferometer is Refractive material which thickness changes with the OPD."]
[7.2596845626831055, 3.7628698348999023, "The Location of the CryoVEx Campaign is Arctic."]
[9.493271827697754, 6.129917144775391, "The Digital sun sensors of the ADCS Attitude Determination and Control Subsystem is 1\u00ba (accuracy), \u00b160\u00ba (range)."]
[6.357612609863281, 9.180826187133789, "The Power Bus Voltage of the MuREM Radiation Monitor is +5V."]
[7.5683274269104, 0.8197647929191589, "The Launch Dates of the Orbiting Astronomical Observatories Satellite is 1966-1972."]
[11.4464750289917, -1.3239647150039673, "The Mass of the HawaiiSat-1 Satellite is 55 kg."]
[11.636799812316895, -1.2010449171066284, "The Mass (kg) of the HJ-1C Satellite is 890."]
[10.139015197753906, -0.9633283019065857, "The Size of the Dove-1 Nanosatellite is 10 cm x 10 cm x 30 cm."]
[8.38237476348877, -0.05135113000869751, "The Liftoff of the Antares Rocket is Ten minutes."]
[8.09733772277832, 8.54390811920166, "The Spectral Stability of the FTS Interferometer Interferometer is 3 x 10 -7  rms for 180 s."]
[7.062943935394287, 9.584433555603027, "The Band 4 of the MSS Instrument Spectral Band is 0.8 - 1.1 \u00b5m."]
[9.572440147399902, 3.7605271339416504, "The Wavelengths of the Lunar Flashlight Spacecraft is ~1.495 \u00b5m, ~1.990 \u00b5m, ~1.064 \u00b5m, ~1.850 \u00b5m."]
[7.752979755401611, 7.896754741668701, "The Instrument Type of the BUV Sensor is Backscatter Ultraviolet (BUV) sensor."]
[4.211194038391113, 5.947672367095947, "The RF Communications of the IRIS Satellite is X-band for payload downlink at 15 Mbit/s."]
[8.630130767822266, 1.7149311304092407, "The Vision Date of the Spitzer Space Telescope is 1946."]
[4.798071384429932, 1.7808904647827148, "The Total Satellites of the ICEYE Satellite Constellation Satellite Constellation is 21."]
[6.181130409240723, 5.812726020812988, "The Imaging Modes of the Capella X-SAR Constellation Satellite Constellation is Stripmap, spotlight, and sliding spotlight."]
[5.882704734802246, 7.595534801483154, "The Signal Amplification Approach of the ATMS Instrument is Amplify first and then split into the various channels."]
[8.059535026550293, 1.1975669860839844, "The Date of the Pacific Tic-Tac-Toe Image is 29 December 2021."]
[9.832119941711426, 8.373784065246582, "The Celestial Sphere Coverage of the Telescope Optical Instrument is 100% annually."]
[11.685705184936523, -1.1663753986358643, "The Mass of the Total with contingency Satellite is 8.83 kg."]
[5.639098644256592, 2.972867727279663, "The Manufacturer of the ALTIUS Satellite is QinetiQ Space."]
[9.935136795043945, 4.7137017250061035, "The Magnitude of the Trajectory Correction Maneuver Maneuver is 22 cm/s."]
[9.262128829956055, 6.427094459533691, "The Attitude Measurements of the Star Sensor Sensor is Roll, pitch, and yaw."]
[8.54253101348877, 6.307514190673828, "The Length of the Booms Deployment System is 30 cm."]
[7.241990566253662, 0.32703283429145813, "The Launch Date of the CRISTAL Satellite is 2028."]
[4.584689140319824, 0.21417517960071564, "The Planned Number of Satellites of the OneWeb Satellite Constellation is Up to 672."]
[10.336331367492676, 3.0119986534118652, "The Altitude in Orbit of the Electric Thruster Thruster is 720 km."]
[11.650728225708008, 6.157113552093506, "The Mission Duration of the XMM-Newton X-ray Space Observatory is 20 years."]
[7.533798694610596, 9.413655281066895, "The Swath width at nadir of the Imager Satellite Instrument is ~57 km."]
[3.4566993713378906, 4.651495933532715, "The Speed Requirement of the MOBC Main On-board Computer is Modest."]
[4.916317939758301, 1.547488808631897, "The Data Collection Area of the FORMOSAT-7/COSMIC-2 Satellite Constellation is Low- and mid-latitudes."]
[6.515418529510498, 3.7859866619110107, "The Data Service of the Spire Satellite Constellation is Provides reliable and accurate global weather forecast."]
[9.481806755065918, 7.350753307342529, "The Purpose of the Cold Atom Laboratory (CAL) Facility is Produces clouds of atoms chilled to temperatures much colder than deep space."]
[8.041522979736328, 5.47634220123291, "The Measured Position Accuracy of the DIOGENE Navigator is ~ 5 m (3D, 1\u03c3)."]
[7.216795444488525, 4.99354887008667, "The Total Cost of the GHGSat-D Satellite System is 1% of other greenhouse gas measurement missions."]
[1.5897752046585083, 4.802131175994873, "The Fully Charged Bus Voltage of the EPS Electric Power Subsystem is 33.6 V."]
[7.073179244995117, 1.582911729812622, "The Development Phase of the Spacebus Neo Satellite is Passed the Preliminary Design Review in early 2015."]
[10.976552963256836, 5.030986785888672, "The Compensates for of the LISA Pathfinder Spacecraft is Other forces acting upon it."]
[7.213904857635498, 2.779054641723633, "The URL of the STEREO Satellite is http://www.nasa.gov/mission_pages/stereo/news/five-years.html."]
[4.851150035858154, 1.917141318321228, "The Number of CubeSats of the Spire Satellite Operator is More than 70."]
[4.933815002441406, -3.2010176181793213, "The | of the J.-H. Yeh Author is J.-H. Yeh."]
[5.146145820617676, 7.089938163757324, "The Reflector Size of the Harris Corporation Manufacturer is 12-meter."]
[8.563983917236328, 7.888830184936523, "The Unknown of the RadMon Radiation Measurement Device is Unknown."]
[6.506397247314453, 4.851466655731201, "The Precision of the Sentinel-6 Michael Freilich Satellite is Millimeter-scale."]
[9.996386528015137, 1.6322197914123535, "The Deployment Sequence of the SkySat-16 to -18 Satellite is SkySat satellites first, about 13 minutes after liftoff, followed by the Starlink satellites about 39 minutes after liftoff."]
[10.55783462524414, 7.522321701049805, "The Material of the Structural Frame Trusses Satellite Component is Flat stock graphite/epoxy (Gr/E)."]
[5.071096897125244, 7.58030891418457, "The Data Rate of the HEPD Instrument is 0.19 kbit/s."]
[4.372704029083252, 3.9380011558532715, "The Purpose of the Automated Beacon Network Anomaly Detection System is Provide cost-effective anomaly detection and notification capabilities."]
[9.06441879272461, 5.185386657714844, "The Attitude Measurement Periodicity of the ISS Satellite is ~\u00b10.5\u00ba in each axis over one orbit."]
[5.90717887878418, 10.842304229736328, "The No of Passbands of the Channel 4 Sensor is 1."]
[5.356664657592773, 1.8863708972930908, "The Mission Number of the Swarm Satellite Constellation is 4th."]
[10.954334259033203, 5.181268692016602, "The Structure of the Solar Plumes Solar Phenomenon is Bundle of denser, flowing plumelets."]
[7.629570484161377, 4.045255184173584, "The Sea Level Rise Contribution of the CryoSat Satellite is 0.21 mm per year for Gulf of Alaska, 0.05 mm per year for High Mountain Asia."]
[8.408498764038086, 9.572210311889648, "The Detector Elements of the AHI Scanner is 77,400."]
[7.414100170135498, 0.7252228260040283, "The Announcement Date of the PROBA-V Satellite is 20 April 2020."]
[8.728300094604492, 5.30206823348999, "The Pointing of the MicroSat-70 Satellite is Nadir pointing."]
[6.444082736968994, 1.8342965841293335, "The Conference Presentation Date of the EnMAP Satellite is March 6-13, 2010."]
[2.3554182052612305, 4.463603496551514, "The Power of the ISEE-1 Spacecraft is 175 W."]
[8.153276443481445, 0.45606404542922974, "The Developer of the CIMON Astronaut Assistant is Airbus."]
[7.08189058303833, 0.21935437619686127, "The Launch Date of the DMC-3 Satellite Constellation is 10 Jul 2015."]
[7.882710933685303, 9.271588325500488, "The Spectral Range of the Detector Instrument Component is 0.25-50 \u00b5m."]
[5.831439018249512, 2.8418753147125244, "The Operator of the GeoEye-1 Satellite is Maxar Technologies."]
[5.703971862792969, 1.7925387620925903, "The Launch Vehicle of the SkySat-16 to -18 Satellite is Falcon 9 rocket."]
[3.764829158782959, 4.138596057891846, "The Power Consumption of the Core-DHS Avionics Module is Reduced."]
[9.640898704528809, 1.600895643234253, "The Repeat Cycle of the HY-2B Satellite is 14 days."]
[6.813112735748291, 1.2682987451553345, "The Conference Date of the NPOESS Satellite System is Sept. 9-11, 2008."]
[9.039870262145996, 9.85084342956543, "The Components of the Interactive Operation Mode Observation Mode is Video camera mode."]
[6.03734016418457, 8.472396850585938, "The Effect of Diffraction of the Geostationary Infrared Sounder Satellite Instrument is Increased compared to sounding from LEO."]
[7.554972171783447, 3.5060956478118896, "The Ground Segment of the ERS-2 Satellite is Unknown."]
[5.797142028808594, 5.5003461837768555, "The Interface of the Phoenix GPS Receivers GPS Receiver is AOCS interface box."]
[7.407011985778809, 4.9723896980285645, "The Focus of the RAIDS Instrumentation is Remote sensing of the ionosphere."]
[8.339461326599121, 3.4423582553863525, "The DEM Resolution of the TanDEM-X Satellite is 12 m."]
[6.739709377288818, 7.616735458374023, "The Accuracy of the Laser Rangefinder Device is Within 1 m."]
[4.041653156280518, 4.345363616943359, "The Microprocessor of the Beresheet lander Lander is GR712RC."]
[8.10636043548584, 2.6995389461517334, "The Commissioning Phase Duration of the TerraSAR-X Satellite is Until the end of 2007."]
[6.5741682052612305, 5.128951072692871, "The Mode of the RADARSAT-2 Satellite is ScanSAR Wide mode."]
[7.031170845031738, 2.8353195190429688, "The Design Influence of the SWEM Satellite is THEMIS, HESSI, STEREO, and MAVEN."]
[4.017596244812012, 4.648548126220703, "The Model of the EC Digital Signal Processor is SMJ3320C30."]
[4.85625696182251, 1.9350556135177612, "The Number of Satellites of the Iridium Satellite LLC Satellite Operator is 66."]
[7.591495037078857, 8.603082656860352, "The Pixel Size of the OCO-3 Instrument is About 1.3 miles (2.2 km)."]
[10.280991554260254, 5.7153706550598145, "The Electromagnetic Waves of the Tether Spacecraft Component is ULF, ELF, VLF."]
[6.343087196350098, 0.6978718042373657, "The Launch Date of the ECSAT Space Center is 14 June 2017."]
[6.946966171264648, 6.818268775939941, "The Manufacturer of the GOES Sounder Instrument is NASA."]
[5.241203308105469, 6.903524398803711, "The IFOV (beam width) of the Antenna Reflector is 1.57\u00ba."]
[6.422574996948242, 2.7016825675964355, "The Refurbishment Locations of the OMS-E Orbital Maneuvering System-Engine is NASA\u2019s White Sands Test Facility in New Mexico, Johnson Space Center in Houston."]
[8.630443572998047, 8.928189277648926, "The Filter Type of the FUV channel Spectrometer is Block with Aluminum."]
[5.2038397789001465, 2.3626604080200195, "The Mechanism Failure Rate of the CubeSats Satellite is Less than 10%."]
[7.109620571136475, 1.7324506044387817, "The Cyclone Yasi Rainfall Date of the TRMM Satellite is Feb. 7, 2011."]
[5.895820617675781, 10.848993301391602, "The No of Passbands of the Channel 2 Sensor is 1."]
[6.048246383666992, -0.04932984337210655, "The Launch Date of the Galileo Satellites 13 and 14 Satellites is 24 May."]
[9.750703811645508, 7.016826629638672, "The Operating Temperature Range of the FEEU Payload Assembly Subsystem is 10:45\u00baC."]
[9.369765281677246, 5.763796806335449, "The Designation of the DFACS Attitude Control System is DFACS (aka AACS)."]
[11.254507064819336, 6.7712273597717285, "The X-ray Spectrum of the SXT Soft X-ray Telescope is 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."]
[9.299631118774414, 8.257628440856934, "The Thickness of the High LET Detector Detector is 140 \u00b5m."]
[3.9254682064056396, 2.337043285369873, "The Size of the PACE CubeSat is 2U."]
[9.383587837219238, 8.152613639831543, "The Instrument Size of the RAMIS Radiation Detector is 140 x 140 x 35 mm3."]
[3.6127846240997314, 6.272756576538086, "The Downlink Rates of the LLCD PAT Systems Communication System is Up to 311 Mbit/s."]
[1.8314168453216553, 5.33315372467041, "The Input Voltage of the Receiver Communication Device is 5 V."]
[7.0495781898498535, 6.5842390060424805, "The Function of the TROPOMI Sensing Instrument is Bring a significant improvement in the precision as well as temporal and spatial resolution of derived atmospheric constituents."]
[7.580329895019531, 7.768941402435303, "The Operating Range of the FFRF Sensor Instrument is 3 m-30 km."]
[9.190727233886719, 1.3878912925720215, "The Data Stream Availability of the Sentinel-6 Satellite is Within hours of collection."]
[9.2735013961792, 8.322593688964844, "The Area of the High LET Detector Detector is 9.6 cm^2."]
[10.35123062133789, 4.9779953956604, "The Thrust of the PROP unit Propulsion System is 130 mN."]
[9.287575721740723, 7.174160003662109, "The Max Recorded Pressure of the T3\u00b5PS Pressure Sensor is 3000 mbar."]
[8.25026798248291, 8.921262741088867, "The Number of Bands of the CIRiS Infrared Imaging System is 3."]
[9.109556198120117, 2.163909912109375, "The Propulsion System Control of the BepiColombo Spacecraft is Mercury Planetary Orbiter\u2019s onboard computer."]
[4.082368850708008, 4.7795186042785645, "The Unknown of the DLTU Data-Link Transmission Unit is Unknown."]
[9.72121810913086, 1.3100240230560303, "The Mean Revisit Time of the TeLEOS-1 Satellite is 12-16 hours."]
[9.433755874633789, 8.556144714355469, "The Observation Type of the OCO-3 PMA Pointing Mirror Assembly is Non-nadir."]
[6.836635589599609, 4.585372447967529, "The Products of the AMSR3 Satellite is 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."]
[6.1122050285339355, 6.0182271003723145, "The Ground Resolution of the StriX-\u03b1 SAR Satellite is 1-3 m."]
[3.384183168411255, 5.245145320892334, "The Memory of the Satellite Memory Satellite is Limited."]
[6.215360164642334, 2.162971258163452, "The Bus Provider of the Jason-2 Satellite is CNES."]
[7.3036274909973145, 9.819723129272461, "The Image Footprint of the HyperScout Earth-observing Instrument is Approximately 200 x 150 km2."]
[10.515867233276367, 2.4089858531951904, "The Perigee (km) of the Meteor-1-2 Satellite is 630."]
[4.977449417114258, -0.13619057834148407, "The Planned Satellite Launch of the OneWeb Company is December."]
[6.362925052642822, 1.0877368450164795, "The Partnership Date of the Skybox Imaging Company is May 14, 2013."]
[7.226806640625, 4.043507099151611, "The Instruments of the SPOT-5 Satellite is Vegetation, HRS, DORIS-NG (SPOT), HRG."]
[8.737957000732422, 7.71917200088501, "The Function of the Magnetic Spectrometer Instrument Component is Track charged particles and determine the sign of their charge and their rigidity."]
[8.392518997192383, 10.106185913085938, "The Spectral Range of the Current GOES imager Sensor is 5.77-6.6."]
[6.6197309494018555, 3.585581064224243, "The Mission Objectives of the ITUpSat-1 Satellite is Capture imagery of the CMOS payload and to study the behavior of the passive stabilization system of the CubeSat."]
[9.10031509399414, 4.861557483673096, "The S/C Pointing of the DSX Spacecraft Payload Module Satellite is 1.0\u00ba, 1.0\u00ba."]
[10.47008228302002, -1.1409531831741333, "The Mass of the DeOrbitSail Nanosatellite is 7 kg."]
[7.43252420425415, 9.781342506408691, "The Spectral Bands of the HyperScout Earth-observing Instrument is 45 visible and near-infrared spectral bands."]
[3.8201067447662354, 0.2902697026729584, "The URL of the GRAIL Mission is http://moon.mit.edu/index.html."]
[5.90839958190918, 3.674466371536255, "The Location of the SOC Science Operations Center is Villafranca near Madrid."]
[4.8676557540893555, 1.8547906875610352, "The Number of Satellites of the COSMO-SkyMed Satellite Constellation is 4."]
[11.747285842895508, -1.0822352170944214, "The Servicer Mass of the ELSA-d Mission is ~175 kg."]
[6.7581987380981445, 2.9498491287231445, "The Mission Status of the CryoSat Satellite is Mission complete."]
[6.59085750579834, 2.486417770385742, "The URL of the Alphabus Satellite Platform is http://www.esa.int/esaTE/SEMSIGKTYRF_index_0.html."]
[3.439450740814209, 5.325003147125244, "The Onboard Storage of the Kanopus-V 1 Satellite is 24 GB."]
[7.376098155975342, 1.9786819219589233, "The First Precipitation Observation Date of the RainCube Satellite is August 27, 2018."]
[8.509360313415527, 10.185279846191406, "The Detector Type of the Imager Satellite Instrument is CCD."]
[2.985907793045044, 6.6729865074157715, "The Output Power of the XBT X-band Transmitter is 10.5 W."]
[7.460048198699951, 0.9327040314674377, "The Position Date of the Storm Hunter Satellite is 13 April, 2018."]
[8.86978530883789, 1.0823289155960083, "The Operational Duration of the MADRAS Instrument is Up to the end of January 2013."]
[7.29312801361084, 9.23344898223877, "The Lens Aperture of the MSI-0 and MSI-1 MSI Instruments is 180 mm."]
[6.3548150062561035, 9.174034118652344, "The Power of the MuREM Radiation Monitor is Low."]
[9.315184593200684, 6.3954010009765625, "The Exposure time of the Star Tracker Attitude Determination Device is 100 ms."]
[8.015318870544434, 4.646080017089844, "The Spatial Resolution - MS of the Spacecraft Satellite is 4 m GSD."]
[5.330958366394043, 5.950368404388428, "The Deployment of the Antenna Dish Satellite Component is Outer portion of the rib must be folded before the inner portion of the rib."]
[9.283668518066406, 5.211836338043213, "The Overview of the Air Force ESEX Flight Experiment Flight Experiment is Not provided."]
[5.600095748901367, 2.351745843887329, "The Deep-Space Observations of the SBSS-1 Satellite System is 3.8 million in first year."]
[5.2428083419799805, 6.88553524017334, "The Beamwidth of the Antenna Conically-scanning reflector is 2.7\u00ba."]
[5.9797539710998535, 0.6087537407875061, "The One Year on Orbit Date of the MaSat-1 CubeSat is Feb. 13, 2013."]
[8.036171913146973, -0.7005112171173096, "The Electromagnetic Interference Chamber Testing Location of the Crew Dragon Spacecraft is SpaceX factory in Hawthorne, California."]
[10.475826263427734, -1.1567096710205078, "The Mass of the Venta-1 Nanosatellite is ~5 kg."]
[8.294563293457031, 3.059683084487915, "The Bistatic Phase of the TanDEM-X Satellite is October 2015 to End of the Year."]
[7.518366813659668, 3.5645604133605957, "The Observation of the ERG (Arase) spacecraft Satellite is Chorus waves and scattered electrons in the magnetosphere."]
[2.9138951301574707, 4.466864585876465, "The Functions of the PCU Power Control Unit is Battery charge / discharge control, peak power tracking (PPT) control for power generation of the solar cells."]
[10.076272964477539, 4.355781555175781, "The Structure Shape of the Clementine Spacecraft is Octagonal prism."]
[7.81801700592041, 9.318720817565918, "The Spectral Range of the VIS Visible region of spectrum is 403-803 nm."]
[10.545090675354004, 2.3630728721618652, "The Inclina. (\u00ba) of the Intercosmos- Bulgaria 1300 (Intercosmos-22) Satellite is 81.2."]
[7.235244274139404, 1.3010156154632568, "The Launch Date of the EarthCARE Satellite is 2015."]
[7.375722408294678, 7.954535484313965, "The Accuracy of the Ozone Measurement Instrument Atmospheric Measurement Device is Greater of (20%, 0.1 ppmv) below 15 km."]
[7.715414524078369, 1.3599621057510376, "The Date of the New NASA Model Finds Landslide Threats Event is 22 March 2018."]
[8.158445358276367, 8.217615127563477, "The Design of the E-THEMIS Thermal Emission Imaging Instrument is Infrared camera."]
[6.244288444519043, 0.856015682220459, "The Launch Date of the Argos-3 Instrument is November 6th \u2013 November 7th."]
[10.150066375732422, 3.2152962684631348, "The Height of the Falcon 9 first stage Rocket is 42 m."]
[12.105948448181152, 3.2915141582489014, "The Inclination of the Satellite Imaging Satellite is 98.1\u00ba."]
[7.937807083129883, 1.3757885694503784, "The Date of the Plugging-in Sub-Saharan Africa Image is 22 March 2021."]
[6.802589416503906, 5.85507345199585, "The Hosted Instrument of the PLATiNO 2 Satellite is MAIA instrument."]
[6.146945953369141, 0.6023359894752502, "The Ready for Flight Date of the CubeSats Satellite is Dec. 16, 2011."]
[7.4594621658325195, 5.534163475036621, "The Instrument of the EMIT Satellite is Imaging Spectrometer."]
[10.153227806091309, 1.2897710800170898, "The Separation Time of the OG2-1 Satellite is Approximately 9:00 pm EST."]
[8.14620590209961, 4.692832946777344, "The Swath Width of the Spotlight-2A Satellite is 10km."]
[7.554664134979248, 4.793415069580078, "The Image Acquisition Files of the PROBA-V Satellite is 1.392."]
[5.703015327453613, 4.106320381164551, "The Operations Location of the Ground Segment Satellite Ground Segment is ESOC (Darmstadt, Germany)."]
[7.894919395446777, 4.412121772766113, "The Resolution of the Deimos-2 Earth Observation Satellite is 75 cm per pixel."]
[9.5237455368042, 0.7156538963317871, "The Structural Qualification Time of the SSTL-300 S1 Satellite is 24 months."]
[10.416025161743164, -0.9824084043502808, "The Mass of the Rising-2 Microsatellite is 43 kg."]
[7.7818989753723145, 3.6707711219787598, "The ACS Testing Device of the AeroCube-4 Satellite is Simple single degree-of-freedom hanging string."]
[6.283194541931152, 8.239566802978516, "The Frequency Bands of the JMR Microwave Radiometer is 18.7, 23.8, and 34 GHz."]
[5.905075550079346, 1.9744813442230225, "The Launch Vehicle of the AeroCube-4 Satellite is Atlas-5-411."]
[1.8889133930206299, 3.9803833961486816, "The Number of Arrays of the Solar Panel Power Generator is 6."]
[7.65944242477417, 1.0863159894943237, "The Launch Plans of the Sentinel-1C Satellite is In force to launch as soon as possible."]
[13.172654151916504, 4.022017002105713, "The Survey Date of the Gaia Satellite is 13 May 2022."]
[8.422868728637695, -0.07697364687919617, "The Orbit Reach Time of the Kick Stage Rocket Stage is About 10 minutes later."]
[7.714646339416504, 4.166815280914307, "The Observation Capabilities of the Aditya-L1 Satellite is Sun's Photosphere (soft and hard X-ray), Chromosphere (UV) and corona (Visible and NIR)."]
[9.825758934020996, 1.6424375772476196, "The Data Delivery Time of the HRFI Imagery Satellite is 150 seconds."]
[10.913322448730469, 5.725101947784424, "The Within about one to three weeks of the Flare Prediction Accuracy Model Performance is They demonstrated that their model was correct by predicting the appearance of a flare in December 2015 to within three weeks."]
[5.902418613433838, 6.43930196762085, "The Center Frequency of the Instrument SAR is 435 MHz."]
[9.435901641845703, 8.699980735778809, "The Telescope Type of the ISAMS Instrument is Movable off-axis reflecting telescope."]
[9.241591453552246, 10.09910774230957, "The Purpose of the Space Cameras Imaging Device is Monitor forests."]
[9.442719459533691, 1.0955122709274292, "The Operation Duration of the Landsat 5 Satellite is Unknown."]
[8.23084545135498, 3.2526309490203857, "The Number of Tiles of the TanDEM-X Satellite is More than 19,000."]
[9.221752166748047, 3.1947553157806396, "The Orbit Type of the FY-3E Satellite is Sun-synchronous near-circular orbit."]
[4.59877347946167, 4.053464889526367, "The Spacecraft Housekeeping Data Bus of the SAMPEX Satellite is Mil-Std-1773B fiber optic data bus."]
[7.800229072570801, 10.007633209228516, "The Number of Bands of the VNIR Detector is 40."]
[4.052554130554199, 6.628718852996826, "The Downlink of the Miniaturized X-band transponders Communications System is 100 kbit/s."]
[17.72847557067871, 7.162752151489258, "The J2000 right ascension (deg) of the B1617-155 (Sco X-1) Pulsar is 244.979."]
[7.3208112716674805, 6.741815567016602, "The Manufacturer of the DESIS Instrument is German Aerospace Center (DLR)."]
[4.973974227905273, 4.525482654571533, "The Role of the Electrical GSE Ground Support Equipment is Simulating the LEU and taking all of the required data needed to record laser performance."]
[7.4076924324035645, 7.527513027191162, "The Measurement Synergy of the GMI Radiometer Radiometer is Mutual overlap of actively sensed, vertically-profiled, radar data at two frequencies in combination with the multi-channel passive data of GMI."]
[7.025874614715576, 2.471046209335327, "The URL of the Glory Satellite is http://glory.gsfc.nasa.gov/launch.html."]
[10.011070251464844, 1.4208928346633911, "The Local Solar Time on Descending Node of the CBERS-2B Satellite is 10:30 hours."]
[9.352957725524902, 11.607738494873047, "The Pixel size of the Channel 2 Sensor is 32 km x 32 km."]
[8.005500793457031, 3.8585057258605957, "The Operation of the Pleiades System Satellite System is Coordinated operation of the Pleiades satellites, spaced 180\u00ba apart in orbit."]
[7.3052473068237305, 0.875220000743866, "The Workshop Date of the PROBA-1 Satellite is April 28, 2004."]
[11.639754295349121, -1.1812291145324707, "The Total Allowable Mass of the Supernova-Beta Satellite is 12 kg."]
[6.533154010772705, 2.1838860511779785, "The Radar Signature Change of the ENVISAT satellite Satellite is Increased with rainfall, then shrank at a rate of 2.4 cm/hr."]
[4.74148416519165, 1.7651443481445312, "The Planned Number of Satellites for 2020 of the Satellite Constellation Satellite Constellation is 16."]
[7.228192329406738, 2.8895552158355713, "The Status of the STEREO-A Satellite is Operating fully."]
[7.592408657073975, 4.791117191314697, "The Mission Focus of the ACE Satellite is Solar wind and ICME (Interplanetary Coronal Mass Ejections), solar and interplanetary energetic particles, cosmic rays and heliosphere/interstellar interactions, and space weather."]
[8.107454299926758, 4.15079927444458, "The Ground Resolution of the Pl\u00e9iades-Neo satellites Satellite is 30 cm."]
[10.297510147094727, 4.967495918273926, "The Engines of the Propulsion Qualification Model Model is 21."]
[1.6969528198242188, 4.560360908508301, "The Efficiency of the Transponders Device is 40%."]
[8.397846221923828, -0.04907190799713135, "The Reentry Burn Duration of the First Stage Rocket Stage is 19 seconds."]
[10.58523178100586, -1.0588304996490479, "The Total Mass of the Minisatellite Satellite is 150 kg."]
[7.583864688873291, 0.9806312322616577, "The Launch Date of the Sentinel-6 Satellite is 30 September 2020."]
[8.05601692199707, 8.130566596984863, "The Detection Threshold of the Instrument Sensor is 4.7 \u00b5J m -2  sr -1."]
[9.832901000976562, -0.9604932069778442, "The Altitude of the JL-1-GF03B Microsatellite is 535 km."]
[6.710518836975098, 2.0663070678710938, "The Rainfall Accumulation of the GPM Satellite Mission is Particularly intense in the Mexican states of Yucat\u00e1n, Campeche, and Quintana Roo."]
[6.287275314331055, 7.933638572692871, "The Polarization of the MWR Radiometer is V."]
[8.126893997192383, 0.9343367218971252, "The Anniversary Date of the Landsat Satellite is July 23, 2012."]
[1.6683812141418457, 4.545948028564453, "The Losses of the Harness Component is 1%."]
[5.025986671447754, -0.15548107028007507, "The Greg Wyler Testimony Date of the OneWeb Satellite Constellation is October 25, 2017."]
[7.510937690734863, 3.742164373397827, "The Drag Profile of the AC4-B Satellite is Larger."]
[8.389139175415039, 0.6202769875526428, "The USC Operation End Date of the Hitomi X-ray Astronomy Satellite is March 26."]
[3.1284420490264893, 4.73794412612915, "The Maximum Firing Rate of the CU Control Unit is 55 Hz."]
[5.234770774841309, 5.389697074890137, "The Terminal Type of the Pl\u00e9iades Neo Satellite Constellation is Reactive Ka-band."]
[6.330472469329834, 11.878044128417969, "The Design Bandwidth of the Three-axis diagonal gradiometer Gradiometer is 5 x 10 -3 to 10 -1 Hz."]
[11.567917823791504, 4.993216514587402, "The Use of the Quasars Celestial Objects is Probes of the expansion history of the Universe."]
[4.551283359527588, 2.0542151927948, "The Total Impulse of the SkySat-5 Satellite is 150 Ns."]
[4.848098278045654, 1.715733528137207, "The Number of Substorms Caught of the THEMIS Constellation Satellite Constellation is More than five dozen."]
[3.602344036102295, 6.637807369232178, "The Data Rate of the X-band Data Acquisition is 18.4 Mbit/s."]
[9.674394607543945, 1.59983491897583, "The Repeat Cycle of the Orbit Satellite Orbit is 24 days."]
[6.693687915802002, 0.8902738094329834, "The Delivery Date of the FORMOSAT-7 Satellite Constellation is May 1, 2015."]
[4.165506362915039, 6.849921226501465, "The Bandwidth of the Ranging Channel Communication System is Approximately 800 kHz."]
[8.81682014465332, 7.272798538208008, "The Measurement Method of the Electrodes Displacement Detection is Differential capacitive measurement."]
[6.413540363311768, 4.257359981536865, "The Abbreviation of the MTSAT Satellite is Multifunction Transport Satellite."]
[7.6228251457214355, 7.078882217407227, "The Dust Velocity Distribution Analysis of the GIADA Contamination Monitor is Dust ejection velocity depends both on the grain size and on time."]
[8.580754280090332, 10.566749572753906, "The Spectral Range of the CCD Detector System Imaging System is 450 nm to 900 nm."]
[7.961601257324219, 10.219903945922852, "The Spectral Range of the WV60 imager Imaging System is 0.45 \u00b5m- 0.90 \u00b5m."]
[8.683245658874512, 9.796650886535645, "The Technology of the EXI instrument Imaging Instrument is CMOS."]
[6.402870178222656, 5.591301918029785, "The Minimum Variance Wind Speed Estimator of the Spaceborne GNSS-R Device is Spaceborne GNSS-R Minimum Variance Wind Speed Estimator."]
[9.439229965209961, 0.5884091258049011, "The Lifetime of the Satellite Satellite is 7 years."]
[9.31128215789795, 7.797140598297119, "The Field of View of the Electron Spectrometer Spectrometer is Nearly 4\u03c0."]
[8.863615036010742, 2.7704856395721436, "The Operation Status of the Kepler Spacecraft is Nominal."]
[7.789425849914551, 3.922205924987793, "The Sector Ice Discharge Increase of the Austfonna Ice Cap is 45-fold."]
[9.797051429748535, 4.857629299163818, "The Firing Duration of the X-axis Bang-Bang Maneuver Satellite Maneuver is 10 s."]
[8.382399559020996, 2.781024932861328, "The Publication Date of the \"Discrete and broadband electron acceleration in Jupiter's powerful aurora\" Research Paper is 7 September 2017."]
[9.524755477905273, 0.6547226905822754, "The Attitude Control System Design Life of the ANUSat Satellite is 6 months."]
[5.490217685699463, 3.6000280380249023, "The Experiment of the STAR-Dundee Company is Testing a next-gen high-speed communication protocol called SpaceFibre."]
[6.518179416656494, 5.37158203125, "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)."]
[9.40125560760498, 1.0903069972991943, "The Constellation Deployment Timeframe of the Satellite Constellation Satellite Constellation is Over the course of 24 months."]
[4.874427318572998, 3.4231090545654297, "The Number of AIS Transmissions Captured of the AprizeSat-3 and AprizeSat-4 Satellites is Over 200,000."]
[8.544174194335938, 2.3365283012390137, "The Purpose of the Parker Solar Probe Spacecraft is Answer questions about solar physics."]
[8.618906021118164, 6.957464694976807, "The Field Range of the Magnetic Field Sensor Magnetoresistive Sensor is 64 \u00b5T."]
[5.284346103668213, 4.42440128326416, "The Implementation of the PGS Ground Segment is Heterogeneous Mission Access (HMA)."]
[6.165386199951172, 5.31466817855835, "The Performance of the GPS Navigation System is Degraded."]
[2.502934217453003, 5.251502513885498, "The Power Consumption of the DPU Digital Processing Unit is 130 W."]
[5.46881103515625, 4.150121688842773, "The Data Processing Location of the Ground Segment Satellite System is MOC (Mission Operations Center) facility at Cordoba."]
[6.366722106933594, 5.017791748046875, "The Deliverable of the Product Level 2A (L2A) Data is Earth located pixel values converted to ground surface reflectance."]
[2.097348928451538, 4.276902675628662, "The Solar Panels Power of the EROS-A Satellite is 450 W."]
[9.081485748291016, 10.634886741638184, "The Size of the MSU-100 Camera is 210 x 200 x 200 mm."]
[4.770209312438965, 0.8339072465896606, "The SPAC Valuation of the Satellogic Satellite Company is $1.1 billion."]
[5.138661861419678, 4.010337829589844, "The Failure Detection System of the SMART-1 Satellite is FDIR system."]
[10.307881355285645, 5.643366813659668, "The Braking Method of the Tether Spacecraft Component is Mechanical friction."]
[4.023073673248291, 2.3486342430114746, "The Size of the SPORT 6U CubeSat Satellite is 6U."]
[5.547292709350586, 3.686068296432495, "The Data Products Archive of the IXPE Observatory Satellite is NASA's HEASARC."]
[7.575605869293213, 7.907704830169678, "The Calibration Stability of the CERES on TRMM Instrument is 0.25%."]
[9.648326873779297, 0.967313826084137, "The Satellite Build Time of the \u00c5AC Microtec group Manufacturer is 4 months."]
[1.0970343351364136, 3.9426488876342773, "The Battery Capacity of the XI-IV Picosatellite is 780 mAh."]
[7.323225021362305, 8.103524208068848, "The Spatial resolution at nadir of the TOU Total Ozone Unit is 50 km."]
[9.837642669677734, -1.0074822902679443, "The LTDN of the JL-1-GF03D Microsatellite is 10:00."]
[11.738576889038086, 7.490540027618408, "The Accuracy of the Atomic Clock Timekeeping Device is One second in three million years."]
[4.7674994468688965, 1.7928135395050049, "The Number of Satellites in Orbit of the Satellogic Satellite Company is 68."]
[5.0178985595703125, 7.578314304351807, "The Wavelength of the W-band Band is 3.9 mm."]
[11.120092391967773, 5.135653018951416, "The Operations Phase Duration of the LISA Pathfinder Satellite is 6 months."]
[7.22399377822876, 1.475301742553711, "The Conference Date of the MicroMAS Project Satellite is August 13-16, 2012."]
[4.995448112487793, 4.694726467132568, "The Purpose of the Ground Station Ground Station is Send commands or receive data."]
[11.495380401611328, 4.170976161956787, "The Size of the KELT-11b Planet is About 30% larger in size than Jupiter."]
[6.419921398162842, 4.689617156982422, "The Level-1 SLC Products of the Sentinel-1 Satellite is Focused data in slant-range geometry, single look, containing phase and amplitude information."]
[7.806981086730957, 9.866291999816895, "The Calibration of the Advanced Land Imager Imaging Device is Spectral and Radiometric."]
[7.8323750495910645, 7.973318576812744, "The Gases Measured of the FTS Fourier Transform Spectrometer is CO2, CH4, carbon monoxide (CO), and other gases."]
[7.59697151184082, 7.052511692047119, "The Ground Segment Components of the TEMPO Satellite is IOC (Instrument Operations Centre) and the interface to the host SOC (Spacecraft Operations Centre)."]
[6.991359710693359, 3.2395179271698, "The Mission Status of the YES Satellite is Failure."]
[5.140264987945557, 2.256164312362671, "The Composition of the CAM Core Team Team is 2 MSc students, 3 PhD students, 3 MSc graduates."]
[9.182476043701172, 5.449783802032471, "The Attitude Control System of the Bus Satellite Component is Reaction Control Subsystem (RCS) - a hydrazine blowdown system pressurised with helium."]
[3.660243272781372, 4.783656120300293, "The Real Time Clock and Calendar (RTCC) of the dsPIC33F microcontroller Microcontroller is Unknown."]
[7.887779235839844, 4.697999954223633, "The Image Resolution of the VSSC Satellite is 10 m."]
[10.280898094177246, 8.75072956085205, "The Instrument Suite of the EUI Extreme UV Imager is 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."]
[9.158185005187988, 7.779298305511475, "The Detector Temperature of the ATSR-1 Instrument is < 95 K."]
[7.27649450302124, 9.267658233642578, "The Alignment of the FG Filtergraph is Unknown."]
[9.373015403747559, 8.95538330078125, "The Spatial Resolution & Stability of the Telescope Optical Instrument is PSF stability better than 1%."]
[5.823872089385986, 4.5691728591918945, "The Operator of the Argos/DCS Satellite System is NOAA."]
[5.425780773162842, 2.8375141620635986, "The Manufacturer of the SeaHawk-1 CubeSat is AAC Clyde Space."]
[7.93035364151001, -0.2192583680152893, "The De-orbit Date of the Tiangong-2 Space Lab is July 2019."]
[4.166863918304443, 4.664923191070557, "The Processing Functions of the DCU-S(TC) module Communication Module is CLTU delimitation, BCH decoding, de-randomization, Security Header extraction, TC Transfer Frame (TF) authenticated decryption and anti-replay control, pseudorandomization and BCH encoding."]
[7.110254764556885, 4.603425979614258, "The Measurement Category of the EXPORTS Satellite Mission is Ocean colour/biology, Multi-purpose imagery (ocean)."]
[6.7866363525390625, 4.464007377624512, "The Environmental Qualification of the Prometheus Satellite is GEVS (General Environmental Verification Specification)."]
[11.84529972076416, 0.9858432412147522, "The Rocket Type of the Chang'e-5 Lunar Mission is Long March 5."]
[7.986638069152832, 4.039271831512451, "The Freezing Temperature of the Carbon Dioxide Ice Substance is -193\u00b0C."]
[7.984294414520264, 3.8886499404907227, "The Orbit Location of the ACE Mission Satellite is First Lagrangian orbit point (L1)."]
[6.627315044403076, 2.989637851715088, "The Objective of the PhoneSat-1 and -2 Satellite is Use a commercial mobile telephone (smartphone) as an avionics system in a nanosatellite."]
[8.0797119140625, 2.677945137023926, "The LEOP Completion Date of the TerraSAR-X Satellite is June 21, 2007."]
[1.3139102458953857, 4.200840473175049, "The Battery Quantity of the HTV Spacecraft is 6."]
[13.807821273803711, 0.7670930624008179, "The Orbital Slot of the GSAT-0210 Satellite is A02."]
[7.257081031799316, 9.45071792602539, "The Spatial Resolution of the TopSAR narrow Imaging Mode is 30 - 50 m."]
[7.367856979370117, 5.681612014770508, "The Temperature Increase of the Surrounding Ocean Ocean is Yes."]
[8.11083698272705, 4.639024257659912, "The Spatial Resolution of the Solid Earth Continental lithosphere Satellite is 50-100 km."]
[8.257003784179688, 4.510806083679199, "The Swath of the Megha-Tropiques Satellite is ~2200 km."]
[8.62438678741455, 7.045738697052002, "The Error (RMS) of the Magnetometer Sensor is <40 nT."]
[10.339238166809082, 3.4176135063171387, "The Apocenter Distance of the SMART-1 Satellite is 4644.004 km."]
[10.77939510345459, 4.8390607833862305, "The Formation of the Shocks Phenomenon is When a supersonic \u2013 faster-than-sound \u2013 flow encounters an obstacle."]
[10.498983383178711, -1.017795205116272, "The Mass of the CBNT-1 (Carbonite-1) Earth Observation Microsatellite is 91 kg."]
[8.535234451293945, 10.393279075622559, "The Detector Types of the Instrument CCD Imaging Camera is NIR and narrow-band VIS (630 nm)."]
[8.652932167053223, 0.18712018430233002, "The Planned Crew Capacity of the Tiangong Space Lab Space Lab is 3."]
[8.121142387390137, 1.0250073671340942, "The Image Acquisition Date of the Landsat 8 Satellite is February 5."]
[13.728190422058105, 1.6102192401885986, "The Date of the Vega flight VV16 Launch is Unknown."]
[5.870161533355713, 3.779287576675415, "The Control Station Location of the JERS-1 Satellite is Tracking and Control Center (TACC), located at the Tsukuba Space Center."]
[7.182591915130615, 3.9271719455718994, "The Propulsion of the TEPCE Satellite is Earth's magnetic field."]
[7.349284648895264, 10.063024520874023, "The Design of the Hyperion HSI (Hyperspectral Imager) is Telescope, two grating spectrometers with supporting focal plane electronics, and a cooling system."]
[6.894024848937988, 0.23776724934577942, "The Cooperation Agreement Date of the Astroscale UK Company is December 2018."]
[7.0926594734191895, 4.877833366394043, "The | of the GOSAT-2 Satellite is Space.based Carbon Monitoring by GOSAT and GOSAT-2."]
[10.173110008239746, 3.0063204765319824, "The Orbit Altitude of the TEMPO Satellite is 35,786 km."]
[6.010570049285889, 2.1459264755249023, "The Launch Site of the STPSat-3 Satellite is MARS (Mid-Atlantic Regional Spaceport) on Wallops Island, VA."]
[6.019526958465576, 8.903702735900879, "The Operational Power Consumption of the MIS Instrument Microwave Radiometer is 357 W."]
[5.705146312713623, 1.3465434312820435, "The Number of Launches of the Arianespace Company is Fourth launch of the year."]
[10.122064590454102, 1.397111415863037, "The Equatorial Nodal Crossing Time of the NigeriaSat-2 Satellite is 10:15 LTAN."]
[7.308581829071045, 0.5569863319396973, "The Launch Date of the ORBCOMM Satellite is Oct. 8, 2012."]
[8.668451309204102, 6.885620594024658, "The Connection to Electronics Boards of the MAG Sensor Sensor is Accomplished by a tuned circuit, including the harness."]
[7.0198516845703125, 1.2866835594177246, "The Conference Date of the EarthCARE Satellite is Dec. 8, 2011."]
[8.48440170288086, 7.311893939971924, "The Magnetic Field Measurement Rate of the ULF Sensor Sensor is 0.03 to 3 Hz."]
[7.583192348480225, 6.567227363586426, "The Typical Value of the C2H2O2 Satellite Instrument is 0.2."]
[8.075179100036621, 9.97258472442627, "The Ground Sampling Distance of the TrueColour Imager Optical Imager is 5 m."]
[6.939512729644775, 0.42692381143569946, "The Launch Date of the Cesium Satellite 1 Satellite is 27 September 2021."]
[5.000929355621338, 4.628459930419922, "The Services of the Ground Station Ground Segment is Monitoring and control."]
[6.741977214813232, 3.1013519763946533, "The Operational of the Resurs-P3 Satellite is True."]
[3.6284401416778564, 6.535378456115723, "The Data Rate of the S-band Communication Band is 665.4 kbit/s."]
[8.212703704833984, 2.6020145416259766, "The URL of the Jupiter's Auroras Natural Phenomenon is https://www.nasa.gov/feature/jpl/jupiter-s-aurora-presents-a-powerful-mystery."]
[10.209183692932129, 3.0142972469329834, "The Altitude of the ExoMars Orbiter Satellite is Approximately 400 km."]
[4.8402533531188965, 4.759731769561768, "The Tracking of the Ground System Communication System is Imprecise."]
[7.029041290283203, 6.595382213592529, "The Unknown of the TROPOMI satellite instrument Satellite Instrument is Unknown."]
[11.191126823425293, -1.517669677734375, "The Mass of the CNUSail-1 CubeSat is 4 kg."]
[7.239081382751465, 4.40438985824585, "The Wavefront Sensing of the DeMi Satellite is Image plane and pupil plane (Shack-Hartmann)."]
[10.206121444702148, 5.261869430541992, "The Leak of the MarCO-B CubeSat is Thruster Valve."]
[8.021218299865723, 9.579009056091309, "The Nr. of spectral or frequency bands of the Optical System Imaging System is 4 in VIS and 1 in SWIR."]
[6.544035911560059, 0.5388857126235962, "The Replacement Date for Meteosat-7 of the Meteosat-8 Satellite is First quarter of 2017."]
[4.043610572814941, 1.1924391984939575, "The Mission Type of the HTV-9 Cargo Transfer Spacecraft is Non-EO."]
[6.302701473236084, 2.6405866146087646, "The Affiliated Institutions of the Bluecrab supercomputer cluster Supercomputer Cluster is Johns Hopkins University and University of Maryland."]
[4.390003204345703, 4.919073581695557, "The Interface Type of the GOES-R Access System Data Distribution System is Subscription-based and ad hoc data requests."]
[7.307124137878418, 8.420087814331055, "The Flight Time for Ions of the COSIMA Mass Spectrometer is 16 \u00b5s."]
[17.72844123840332, 7.1627678871154785, "The J2000 right ascension (deg) of the B1509-58 Pulsar is 228.48175."]
[5.634817600250244, 1.4449809789657593, "The Launch Site of the Falcon 9 Launch Vehicle is Launch Complex 39A (LC-39A) at NASA\u2019s Kennedy Space Center in Florida."]
[7.867708206176758, 0.9360882639884949, "The Service Module Assembly Start Date of the Orion Spacecraft is May 19, 2016."]
[6.940558910369873, 4.984365463256836, "The Detection Capability of the Copernicus Sentinel-5P Satellite is Methane cloud, nitrogen dioxide plumes from individual ships."]
[8.454997062683105, 5.783322334289551, "The Effect of the South Atlantic Anomaly Magnetic Anomaly is Affects the amount of cosmic radiation reaching the passengers and crew of any plane and spacecraft led to cross it."]
[6.7264251708984375, 7.295456886291504, "The Data Production Period of the IMERG Data Processing System is Seven day period from 23-30 November 2018."]
[6.627716541290283, 3.5302977561950684, "The Mission Type of the TUBSAT Satellite is EO."]
[10.192875862121582, 3.2874419689178467, "The Floating Distance of the Orihime Satellite is About 200 mm."]
[11.386555671691895, 4.073462963104248, "The Number of Planets of the TRAPPIST-1 Star System is 7."]
[8.875772476196289, 8.409390449523926, "The Angular Resolution of the ELENA Sensor is 4.5\u00ba x 4.5\u00ba."]
[7.279055595397949, 7.5237531661987305, "The Type of the PRARE space segment oscillator Quartz-Crystal Oscillator is Voltage-controlled."]
[11.742587089538574, 4.468077182769775, "The Age Difference of the IC 4665 and Collinder 350 Star Clusters is More than 500 million years."]
[7.712469100952148, 1.218611240386963, "The Launch Date of the Earth Science Sensor Sensor is 2021."]
[9.312649726867676, 6.4304938316345215, "The Technology of the Procyon star tracker Attitude Determination Device is Active Pixel Sensor (APS)."]
[9.278206825256348, 7.973428726196289, "The Charge Range of the ULEIS Spectrometer is He through Ni."]
[5.7662553787231445, 7.009622097015381, "The Pulse Length of the RA-1 Radar Altimeter is 20 \u03bcs."]
[7.8435468673706055, 4.478519916534424, "The Panchromatic Band Off-nadir Resolution of the WorldView-3 Satellite is 0.34 m."]
[3.8587234020233154, 2.2979137897491455, "The Size of the Maya-3 CubeSat is 1U."]
[4.903232574462891, 12.082476615905762, "The Uncertainty of the Responsivity Measurement Instrument is <0.1%."]
[7.650797367095947, 6.288783073425293, "The Precision of the OCO-2 Satellite is <0.3% (1 ppm)."]
[3.7301571369171143, 4.4912333488464355, "The Processor of the ODHS Processor Module Onboard Data Handling System is Atmel 32 bit processor of ARM9 architecture."]
[7.915793418884277, 2.602461814880371, "The Impact Test Date of the DebriSat Satellite is 15 April, 2014."]
[7.519697666168213, 1.1205308437347412, "The Date of the High-Latitude Cold-Season Snowfall Campaign Field Campaign is January 15, 2012 until March 3, 2012."]
[7.37646484375, 0.8673235774040222, "The Development Start Date of the MMO Spacecraft is March 19, 2015."]
[9.786333084106445, -0.5403217077255249, "The Bus Concept of the MS-2 Minisatellite is 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."]
[4.755952835083008, 1.798323154449463, "The Number of Satellites in Orbit of the Satellogic Satellite Manufacturer is 8."]
[4.966283321380615, 3.334237813949585, "The Subsystem Microprocessor of the CubeSat Satellite is Each subsystem has its own microprocessor."]
[7.582347869873047, 2.7310988903045654, "The Data Revealed of the Hinode Spacecraft is The source of the SEP events."]
[7.057547569274902, 1.3871315717697144, "The Conference Date of the Dove Satellite is Aug. 5-10, 2017."]
[11.330768585205078, 3.59842586517334, "The Density of the Comet Celestial Body is 470 kg/m3."]
[8.951118469238281, 5.752997398376465, "The Navigation System of the Resurs-P Satellite is Star and sun sensors for attitude data, GLONASS/GPS system for orbital position determination."]
[7.9870219230651855, 3.5994067192077637, "The Image Content of the INTEGRAL Satellite is Shows the auroras forming a rough semi-circle at Earth\u2019s northern latitudes."]
[7.716729640960693, 3.0022315979003906, "The Presentation Date of the CartoSat-2 Satellite is Sept. 29 to Oct. 3, 2008."]
[6.26480770111084, 2.175650119781494, "The Overview of the TECSAR Satellite Hardware and Mosaic Mode of the TecSAR Satellite is Ury Naftaly, Ronit Levy-Nathansohn, \u201cOverview of the TECSAR Satellite Hardware and Mosaic Mode,\u201d Geoscience and Remote Sensing Letters, IEEE Geoscience and Remote Sensing Letters, IEEE Vol. 5, Issue 3, July 2008, pp.:423 - 426."]
[8.849867820739746, 7.07841157913208, "The | of the Plasma Experiment for Planetary Exploration (PEPE) Plasma Experiment is Plasma Experiment for Planetary Exploration (PEPE)."]
[9.664417266845703, 5.395619869232178, "The Objective of the PLEGPAY Experiment is Study of spacecraft/space environment interactions in LEO with reference to electrostatic charging/discharging phenomena."]
[9.056539535522461, 10.653740882873535, "The Spatial Resolution of the spaceCam c4000 Video Camera is 6 m."]
[12.936365127563477, 4.839840412139893, "The Observation Area of the IBEX Spacecraft is Outside the heliosphere."]
[6.617660045623779, 4.145546913146973, "The Application of the RISAT-2 Satellite is Radar satellite imagery for assessing cyclone damages."]
[1.6601755619049072, 4.703581809997559, "The Number of PCBs of the EPS Electric Power Subsystem is 5."]
[6.013969898223877, 4.2049241065979, "The Primary Role of the Dextre Robotic System is ISS Handyman, replacing failed components, unloading cargo, supporting technology demonstrations."]
[4.048933029174805, 2.409456253051758, "The Satellite Size of the Sounder Instrument Instrument is 6U."]
[9.636460304260254, 1.763757586479187, "The Image Frequency of the TESS Satellite is Every 30 minutes."]
[1.9468088150024414, 5.547155380249023, "The Voltage of the Voltage 7 Power Amplifier is 3.5\u00b12%."]
[7.604254245758057, 0.596076488494873, "The Mission Start Date of the DSCOVR Satellite is March 3, 2012."]
[8.610185623168945, 8.965863227844238, "The Wavelength of the Telescope Optical Instrument is 0.6 - 29 \u00b5m."]
[8.28093433380127, 3.091876983642578, "The Conference Date of the TanDEM-X Satellite is April 25-30, 2010."]
[9.50283432006836, 5.705240726470947, "The Redundancy of the Reaction Wheels Attitude Control Device is 1 RW loss allowed."]
[8.487887382507324, 10.422592163085938, "The Array Size of the CCD Detector Matrix Detector is 576 lines x 780 columns."]
[9.01794719696045, 8.962913513183594, "The Mask at Intermediate Image Plane FOV of the TIR Subsystem Imaging System is \u00b111.3\u00ba."]
[8.800436019897461, 0.7944200038909912, "The Rotation Capability of the JUICE Spacecraft is True."]
[8.399652481079102, 8.795960426330566, "The Operation Principle of the Imaging Pushbroom Spectrometer Spectrometer is 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 ."]
[13.80874252319336, 0.7666243314743042, "The Orbital Slot of the GSAT-0211 Satellite is A06."]
[9.102664947509766, 7.884061813354492, "The Measurement Modes of the Sensor Particle Detector is Count Mode, List Mode."]
[12.067821502685547, 3.2654292583465576, "The Orbit Inclination of the Secondary Payloads Satellite is 102\u00ba."]
[11.784558296203613, 1.0880876779556274, "The Components of the Chang'e-5 Lunar Probe is Lander, orbiter, ascender, returner."]
[8.05882740020752, 4.907808303833008, "The Processed Imagery of the Image Location Knowledge Satellite Component is < 100 m."]
[5.8713788986206055, 1.9393242597579956, "The Launch Site of the ALL-STAR-1 Satellite is Cape Canaveral, FL."]
[4.889670372009277, 3.3513612747192383, "The Conference Presentation of the EDSN Intersatellite Communications Architecture Communications Architecture is AIAA/USU Pre-Conference: CubeSat Developers' Workshop, Logan, Utah, USA, August 2-3, 2014."]
[10.064106941223145, 1.5333105325698853, "The Period of the Molniya Orbit Orbit is 11 hours and 58 minutes."]
[9.998892784118652, 5.115105152130127, "The Orientation of the ESP Thrusters Maneuvering System is 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."]
[7.059893608093262, 0.14275430142879486, "The End of Life Date of the ALOS-3 Satellite is 7 March 2023."]
[4.880152225494385, 4.318572998046875, "The About Author of the Optical Inter-orbit Communications Engineering Test Satellite (OICETS) Satellite is Yasuhiro Morita."]
[5.135769844055176, 6.040958404541016, "The Antennas of the Antenna System Communication System is Four broadband feed-horn antennas."]
[13.080636978149414, 4.068279266357422, "The Number of Asteroids of the Gaia Satellite is 154,741."]
[7.1837568283081055, 6.826045989990234, "The Data Release of the NISTAR National Institute of Standards and Technology Advanced Radiometer is Expected shortly after EPIC data."]
[3.815514087677002, 4.373863220214844, "The Daughter card of the C&DH subsystem Onboard Computer System is Cortex A8 processor."]
[6.941681861877441, 4.732255935668945, "The Panchromatic Mode Band of the SPOT satellite constellation Satellite Constellation is Single wide band in the visible part of the spectrum."]
[9.349794387817383, 5.300962448120117, "The Type of the Microwheel 10SP-M Reaction Wheel is Small Satellite."]
[9.269743919372559, 8.354211807250977, "The Area of the Low LET Detector Detector is 9.6 cm^2."]
[7.119012832641602, 8.807700157165527, "The Spectral Region (Infrared Channel) of the VIRR Instrument is 10.5 - 12.5 \u00b5m."]
[5.65602445602417, 3.881077527999878, "The Location of the GSOC Operations Center is Oberpfaffenhofen."]
[8.26867389678955, 5.010463714599609, "The Positioning of the GNB Satellite is \u00b120\u00ba about the magnetic field vector."]
[3.8797478675842285, 4.500906467437744, "The Hardware and Software Design of the OBC Onboard Computer is Exactly the same as PDH."]
[10.395697593688965, 5.656583309173584, "The Tether Length of the ATEx Tether Experiment is 22 m."]
[11.172320365905762, 6.358928203582764, "The Image Credit of the Chandra X-ray Observatory X-ray Observatory is X-ray: NASA/CXC/NCSU/K. Borkowski et al; Optical: DSS."]
[9.02324104309082, 10.814837455749512, "The Revisit Cycle of the LISS-4 Camera is 5 days."]
[7.778841018676758, 9.869765281677246, "The Band Spacing of the VNIR Detector is 11.4 nm."]
[7.518138408660889, 1.6766221523284912, "The Presentation Date of the Magnetospheric Multiscale (MMS) Mission is 2008."]
[6.900896072387695, 1.2804752588272095, "The Constellation Update Date of the Planet Company is 24 January 2021."]
[7.230461120605469, 0.3122190535068512, "The Launch Date of the Tomorrow-R1 and -R2 Satellite is April 2023 and June 2023."]
[8.178561210632324, 2.9812307357788086, "The Presentation Date of the TerraSAR-X, TanDEM-X, EnMAP Satellites is June 18-19, 2009."]
[5.830860614776611, 8.16130256652832, "The Bandwidth (GHz) of the ICI-2 Radiometer is 3."]
[7.57931661605835, 4.004669666290283, "The Unknown of the ALOS-3 Satellite is Unknown."]
[6.076849460601807, 8.450541496276855, "The Sounder Type of the MLS Instrument is Three-channel heterodyne limb sounder."]
[7.547379970550537, 8.486326217651367, "The SNR of the Instrument Spectrometer is \u2265900."]
[7.657354831695557, 7.477744102478027, "The Application of the MCP Multi-Channel Plate is Measure the gas density in the upper atmosphere."]
[7.72550106048584, 9.00121784210205, "The Spectral Resolution of the MAHRSI Instrument is 0.026 nm at 215 nm."]
[6.22383451461792, 3.9201934337615967, "The Functional Architecture of the EO-ALERT Satellite System is Modular, scalable and reconfigurable."]
[8.401078224182129, 8.597342491149902, "The Objective of the GAS Grating Spectrometer is Measurement of CO2, CH4, CO, N2O."]
[7.277012825012207, 9.26359748840332, "The Size of the Optical Scanning Design Imaging Spectrometer is 1.3 m3."]
[6.636641979217529, 10.666849136352539, "The Nominal SNR of the Band 5 Spectral Band is 1010."]
[7.33751106262207, 0.5788078904151917, "The Launch Date of the Hisea-1 Satellite is 6 November 2020."]
[7.33973503112793, 10.12944221496582, "The Image Compression of the HyperScout Imaging System is 2x2."]
[5.555966854095459, 9.028083801269531, "The Power of the SPEU Device is ~2.5 W."]
[7.71240234375, 1.5528559684753418, "The Launch Date of the Trace Gas Orbiter (TGO) Satellite is 2016."]
[9.417970657348633, 0.37206435203552246, "The Exceeded Design Life of the TRMM Satellite is Yes."]
[8.05712890625, 4.652604103088379, "The Spatial Resolution of the Geodesy Unification of worldwide height systems Satellite is 100-20000 km."]
[7.980493068695068, 3.1258976459503174, "The Quantity of the Kuiper Belt Object Celestial Object is More than 100,000 objects."]
[6.29042387008667, 5.62219762802124, "The Interferometry Mode of the TerraSAR-X SAR Satellite is ATI (Along Track Interferometric) mode."]
[7.118470191955566, 0.8920895457267761, "The Launch Date of the Vietnamese satellite Satellite is Unknown."]
[12.977068901062012, 4.855432510375977, "The Observation Date of the IBEX Spacecraft is Oct. 2009."]
[12.130105018615723, 3.2806012630462646, "The Orbit Inclination of the KSF1 satellites Satellite is 97.6\u00ba."]
[13.721955299377441, 1.612154245376587, "The Launch Date of the Vega Launch Vehicle is 17 August 2021."]
[2.0569581985473633, 4.203746318817139, "The Solar Panels of the ALTIUS Satellite is Two deployable solar panels with 120 W of power."]
[11.555537223815918, 6.344416618347168, "The Venting Date of the SXT Soft X-ray Telescope is October 2015."]
[3.257648229598999, 4.859245300292969, "The Microcontroller RAM of the CC430 SoC System on Chip is 4 kB."]
[3.402076244354248, 5.327241897583008, "The On-board Data Recording Capacity of the RF Communications Communication System is 64 Gbit."]
[6.8890061378479, 0.41851916909217834, "The Control System Development and Verification of the Delfi-C3 Satellite is Oct. 2-6, 2006."]
[11.165948867797852, 7.120155334472656, "The X-ray Systems Interval of the Diagnostic Instruments Test Facility is 2 \u00b5s."]
[10.327001571655273, 4.562344074249268, "The \u0394V of the Propulsion System Satellite Component is Up to 200 m/s."]
[5.610940456390381, 3.98419189453125, "The Ground System of the UNIFORM-1 Satellite is Mission Planning, Scheduling, Control, and Data Processing."]
[9.576863288879395, 0.5712024569511414, "The Planned Operational Lifetime of the Heinrich Hertz Satellite is 15 years."]
[7.296017169952393, -0.7504526972770691, "The Validation Data Source of the CYGNSS Satellite is IWARP."]
[11.686779022216797, 4.594264984130859, "The Data Collection of the EPIC248847494 star Star is Light Curve."]
[8.192541122436523, 3.7258999347686768, "The Observation Result of the Integral Satellite is Unexpectedly strong auroras illuminating the Earth."]
[6.9686665534973145, -0.0677393302321434, "The End of Life Date of the Myriade/AstroSat-100 Satellite is June 2030."]
[7.721089839935303, 7.672210216522217, "The Measurement Domain of the OCO-3 Instrument is Atmosphere."]
[8.459195137023926, 3.9441933631896973, "The Attitude Control of the LAGEOS Satellite is None."]
[11.224745750427246, 2.879621744155884, "The Displacement of the Boulders Geological Feature is More than 3cm."]
[8.240078926086426, 8.745421409606934, "The Input Port Field of View of the FTS Fourier Transform Spectrometer is 2.6 arcmin diameter."]
[9.405881881713867, 0.35778847336769104, "The Exceeded Design Life of the GRACE Satellite is Yes."]
[6.825481414794922, 3.240697145462036, "The Mission Status of the OSCAR-QUBE Satellite is Operational (nominal)."]
[8.443849563598633, 2.6717662811279297, "The Types of Maneuvers of the THEMIS (and ARTEMIS) spacecraft Satellite is 4 orbit change maneuvers, one attitude, and one spin rate adjustment per probe."]
[7.9691386222839355, 1.3027007579803467, "The Article Release Date of the Solar Orbiter Satellite is 27 April 2021."]
[6.441681861877441, 8.545658111572266, "The Swath width of the MWRI Microwave Radiation Imager is 1400 km."]
[4.900144100189209, 2.3303427696228027, "The BCRs Configuration of the DubaiSat-2 Satellite is Three BCRs in a hot redundancy configuration."]
[11.408647537231445, 1.371422290802002, "The Weight of the Yutu 2 Lunar Rover is 140 kg."]
[6.426888465881348, 0.8770124316215515, "The Eruption Observation of the GOSAT Satellite is October 2017."]
[6.954404354095459, 7.644257068634033, "The Resolution of the HARP-2 Polarimeter is <6 km."]
[2.3050293922424316, 5.418684959411621, "The Qualification Runs of the GaN-based Power Transistors Transistors is 15 W and 80 W."]
[9.872450828552246, 1.3695393800735474, "The Experiment Time of the Sloshsat-FLEVO Satellite is Until the gas supply of the cold-gas reaction control system is exhausted."]
[6.633027076721191, 3.6008830070495605, "The Mission Type of the CHORUS Satellite Constellation is EO."]
[7.935606002807617, -0.6502490639686584, "The URL of the SpaceX CRS-25 Dragon Spacecraft is https://www.nasa.gov/mission_pages/station/research/news/spacex-25-research-highlights."]
[7.271536350250244, 0.25220614671707153, "The Launch Date of the Biomass Satellite is 2023."]
[5.312742233276367, 9.63339614868164, "The Star Position Accuracy (3\u03c3) of the STOs and STAEs Analog Electronic units is Random Bias 3.1 arcsec (4 mag), 9 arcsec (6 mag); 13.7 arcsec (6.5 mag)."]
[9.036148071289062, 3.0016655921936035, "The Orbit of the LunaH-Map Spacecraft is Elliptical science orbit."]
[7.111720085144043, 1.8146945238113403, "The Conference Presentation Date of the High Spatio-Temporal Resolution Land Surface Temperature Mission Satellite is 22-27 July 2018."]
[3.9260337352752686, 5.5168914794921875, "The UART Channels of the CSI Data Communication is 4."]
[9.521967887878418, 0.6135573387145996, "The Orbit Maintenance Capabilities of the PACE Satellite is 10 years."]
[9.002739906311035, 10.633079528808594, "The Purpose of the DCAM3 Camera is Obtain close up views of impact."]
[6.486687660217285, 6.228499412536621, "The ICU of the ASCAT Scatterometer is Instrument Control Unit."]
[10.019485473632812, -0.6893885135650635, "The Platform Size of the Tsubame Microsatellite is 45 cm x 45 cm x 56 cm (H)."]
[10.366700172424316, 9.469917297363281, "The Eclipse Operation of the IRIS Spacecraft is Not operated for 4 months."]
[7.82535457611084, 1.8151578903198242, "The Observation Date of the ISEE-1 and ISEE-2 Satellites is July 1978."]
[12.117087364196777, 3.2664854526519775, "The Inclination of the Landsat 9 Satellite is 98.2\u00ba."]
[9.493184089660645, 7.8076171875, "The Particles Detected of the Carmen-2 Radiation Detector is e-, p+ (high-energy particle flux of electrons and protons) and ion fluxes."]
[8.028444290161133, 1.2798253297805786, "The Date of the Dungeness Spit Image is 13 April 2022."]
[5.184611797332764, 2.5883665084838867, "The Platform of the Inmarsat S \u2013 Europasat / Hellas-Sat 3 Satellite is Spacebus 4000 C4."]
[11.672207832336426, -1.249218225479126, "The Mass of the PSat-2 Satellite is 2 kg."]
[7.060299396514893, 6.605266094207764, "The Purpose of the TROPOMI Instrument is Map a multitude of trace gases such as nitrogen dioxide, ozone, formaldehyde, sulphur dioxide, methane, carbon monoxide and aerosols."]
[8.101238250732422, 4.582123279571533, "The Spatial Resolution of the Solid Earth Seismic hazards Satellite is 100-200 km."]
[7.8259429931640625, 4.504749298095703, "The Hyperspectral Imagery Resolution of the Satellogic Satellite Manufacturer is 30 meters."]
[10.901758193969727, -1.3961478471755981, "The Mass Range of the CubeSats and nanosatellites Satellite is 1-10 kg."]
[7.677844047546387, -0.07555615156888962, "The Daily Operation Time of the SAOCOM-1A Satellite is 450 minutes per day."]
[11.10150146484375, 6.305077075958252, "The Flux and Energy Spectrum of the Neutrons Radiation is Variable."]
[4.2117438316345215, 6.58418083190918, "The Uplink Frequency of the RF Communications Communication System is 144 MHz."]
[5.867345809936523, 7.590366840362549, "The Program Manager of the ATMS Instrument is Danielle Gallegos."]
[4.553528785705566, 3.6513335704803467, "The Unknown of the AIS-PEM Payload Electronics Module is Onboard the satellite was an Automatic Identification System - Payload Electronics Module (AIS-PEM)."]
[5.959761619567871, 2.7409143447875977, "The Manufacturer of the Strela-3/Rodnik Military Reconnaissance Satellite is NPO Prikladnoi Mekhaniki."]
[6.69915246963501, 8.302838325500488, "The Optical Pulse Size of the LI Instrument is 10 km - 100 km circular pulse diameter."]
[17.728809356689453, 7.162847995758057, "The J2000 right ascension (deg) of the B1758-250 Pulsar is 270.284."]
[7.950342178344727, -0.27890723943710327, "The Launch Schedule of the Shenzhou XV Manned Spacecraft is This year."]
[11.39222526550293, 6.4898295402526855, "The PDR Date of the IXPE observatory X-ray Observatory is August 8, 2018."]
[10.584198951721191, 3.1827659606933594, "The Orbit Perihelion Distance of the V7GA Mission is 9.86 RS."]
[5.160593032836914, 4.2718000411987305, "The Design Goal of the EGS Ground System is Disassociate space missions from pipeline ground system approaches and standardize ground system software, hardware, and interfaces."]
[5.840574264526367, 8.1082124710083, "The Frequency Range of the ICI Instrument is 183 GHz up to 664 GHz."]
[5.21717643737793, 6.731006622314453, "The Beamwidth of the Yagi Antenna Antenna is 45\u00ba."]
[9.257646560668945, 0.688511312007904, "The Operation Duration of the EO-1 Satellite is 10 years."]
[9.644706726074219, 1.3897345066070557, "The Landing Site Data Transfer Time of the Spacecraft Satellite is Two days."]
[9.061908721923828, 4.437528610229492, "The Dimensions of the S/C Structure Satellite Structure is 90 cm x 90 cm x 107 cm."]
[9.559476852416992, 5.952419281005859, "The Pointing Accuracy of the ADCS Attitude Determination and Control Subsystem is \u22640.01\u00ba (3\u03c3, 3-axis)."]
[7.4933762550354, 0.7981132864952087, "The Installation Date of the Y-3 Detector is January 1974."]
[7.953527450561523, 2.0644142627716064, "The Fast Plasma Experiment of the SEE-1 and ISEE-2 Spacecraft is Unknown."]
[7.061044692993164, 1.513214111328125, "The Paper Number of the ERG Satellite Satellite is 2011-r-51."]
[9.184444427490234, 0.7680185437202454, "The Test Duration of the Modern ICs Electronic Components is Unrealistic 7.6 years."]
[7.804019451141357, 8.984541893005371, "The Spectral Resolution of the Spectrometer Spectrometer is <2.5 cm -1."]
[9.091758728027344, 10.729609489440918, "The Calibration Cycle Time of the LISS-3 camera Camera is 7.3 s."]
[7.230041980743408, 6.225766181945801, "The Publication Year of the Aerosol Polarimetry Sensor Sensor is 2007."]
[5.89215612411499, 3.1539900302886963, "The Project Partners of the TRACERS Satellite Mission is University of Iowa (UI), SwRI, MSS, UCB, UCLA."]
[8.374262809753418, 4.920354843139648, "The Observation of the Satellite Observation Satellite is Particle energization, solar flares, reconnection and plasma jet interaction with the local magnetic field structure."]
[9.44360065460205, -0.7734602689743042, "The Deployment Date of the DIWATA-1 Microsatellite is April 27, 2016."]
[6.9369730949401855, 2.5969655513763428, "The URL of the Landsat-9 Satellite is https://landsat.gsfc.nasa.gov/landsat-9/."]
[8.729961395263672, 2.346458911895752, "The Solar Encounters of the Parker Solar Probe Spacecraft is 7."]
[7.6119561195373535, 8.820536613464355, "The Spectral Resolution of the CO2Image Satellite is 1.0 nm - 1.3 nm."]
[3.8505666255950928, 2.287381887435913, "The Size of the OSCAR-QUBE CubeSat is 1U."]
[9.581014633178711, 4.922098159790039, "The Recovery Method of the Kepler Space Telescope Space Telescope is Maneuvering the spacecraft so that the solar pressure is evenly distributed across the surfaces of the spacecraft."]
[7.4511823654174805, 8.371869087219238, "The SNR of the Instrument General is Between 350 and 450."]
[7.128396034240723, 8.859761238098145, "The No of bands/channels of the VIRR Visible and Infrared Radiometer is 10."]
[6.395654201507568, 3.2358193397521973, "The Interaction of the CNES and ONERA centers Centers is Illustrated in Figure 34."]
[9.279693603515625, 10.257769584655762, "The f/number of the 1000 mm camera Camera is f/11."]
[6.755566120147705, 0.5121875405311584, "The Launch Date of the OTB-1 minisatellite Satellite is 25 June 2019."]
[4.163397789001465, 5.290219783782959, "The Purpose of the Data Compression Method Telemetry System is Prevent crowding out payload data."]
[9.227136611938477, 5.331694602966309, "The Attitude Actuation of the QuickBird-2 Satellite is Reaction wheels."]
[8.773969650268555, 10.531246185302734, "The Resolution of the False Color Composite Image Image is 250 m."]
[6.911634922027588, 1.1596657037734985, "The Conference Date of the BIROS Satellite is June 11-15, 2012."]
[8.929594993591309, 10.421768188476562, "The Camera Module Interface of the Frame Grabber Data Interface is Correct interface to the camera module."]
[7.7535786628723145, 8.793006896972656, "The Amplitude Spectral Density of the DOSS system System is Measured."]
[6.513213157653809, 7.561377048492432, "The Hermetic Sealing of the Laser Optical Communication Device is True."]
[9.12237548828125, 3.238563060760498, "The Orbit of the GRACE-FO satellites Satellite is Co-planar polar orbit."]
[5.047504425048828, 4.868043899536133, "The Number of Transmission Attempts of the Fixed Platforms Ground Segment is 3."]
[6.8224263191223145, 8.26135540008545, "The Instrument Type of the AVHRR/3 Instrument is Whiskbroom-type."]
[4.8790669441223145, 6.115228176116943, "The Center Frequency of the Satellite Device Unknown is 89.0 GHz."]
[8.591392517089844, 5.177165985107422, "The Spacecraft pointing capability of the ALOS-3/PRISM-2 Satellite is \u00b160\u00ba (cone, max)."]
[6.898797512054443, 1.102921724319458, "The Launch Date of the ResourceSat-2A Satellite is December 7, 2016."]
[8.916471481323242, 3.5474023818969727, "The Orbit of the Eutelsat 172B Satellite is GEO at 172\u00baE longitude."]
[11.572725296020508, 6.276955604553223, "The First Pictures Date of the XMM-Newton X-ray Space Observatory is Feb. 9, 2000."]
[4.994294166564941, 4.640644550323486, "The Components of the Ground Segment Ground Station is Laptop computer, radio/RF unit, antenna rotator and antennas."]
[6.001007556915283, 0.608017086982727, "The Conference Date of the LUMIO CubeSat is 1-5 October 2018."]
[11.650077819824219, -1.2996615171432495, "The Masses of the Aluminum Spheres Satellite is 1 kg, 1.5 kg, 2 kg."]
[7.431488037109375, 9.033387184143066, "The Swath Width of the HIRDLS Spectrometer is 2000 - 3000 km."]
[11.746720314025879, 7.50644588470459, "The Technology Readiness Level of the DSAC Atomic Clock is 5 to 7."]
[9.274055480957031, -0.5625703930854797, "The Design, AIT, Launch & Early-Operations of the Galassia Nanosatellite Satellite is Unknown."]
[9.074265480041504, 8.97420597076416, "The Angular Resolution of the IBEX-Lo sensor Sensor is 3.5\u00ba x 3.5\u00ba FWHM."]
[5.087677001953125, 4.9319562911987305, "The Requirement of the EUMETCast Data Dissemination Service is Users to purchase new satellite reception equipment and pay for the transmission fee."]
[0.9156081676483154, 4.186565399169922, "The Capacity of the Battery Power Storage is 12 Ah."]
[7.003355503082275, 4.980700969696045, "The Methane Detection of the Copernicus Sentinel-5P Satellite is True."]
[8.870965003967285, 8.263026237487793, "The NE\u0394T @ specified scene temperature of the Instrument Spectral Imager is 0.15-0.4 K @ 250 K."]
[1.901795506477356, 4.121280670166016, "The Backup Power Output of the Solar Array Power Generation is 55Ah NiCd (Nickel-Cadmium) battery charge power requirement."]
[5.872218608856201, 4.002677917480469, "The Communication System of the Bartolomeo Payload Communication System is OSIRISv3."]
[7.8814287185668945, 8.378482818603516, "The Optics Design of the ACE-FTS Instrument is Highly folded design."]
[7.735769271850586, 8.594995498657227, "The Solar F10.7 cm fluxes Range of the PEM (Parameterized Exospheric Model) Theoretical Model is 80-230 x 10-22 W m-2 Hz-1."]
[8.425939559936523, 8.654894828796387, "The Grating Order of the Spectrometer Instrument is 3."]
[7.258580207824707, 0.865787923336029, "The Launch Date of the MMS Satellite is March 13, 2015."]
[8.35411262512207, 6.563941955566406, "The Mounting of the SCM Instrument is 1 m deployable boom."]
[13.809136390686035, 0.7669654488563538, "The Orbital Slot of the GSAT-0204 Satellite is B03."]
[9.081941604614258, 5.698060512542725, "The Attitude Control of the Satellite Spacecraft is Hybridization of star sensor and accelerometer measurements."]
[7.806023597717285, -0.5380300283432007, "The Telemetry Monitor of the SpaceX CRS-17 Mission is Christina Koch."]
[3.934713125228882, 4.459919452667236, "The Flight Computers of the Payload Instruments Satellite Components is Dual redundant flight computers based on Intel 80386EX processors, configured with 32 MByte capacity."]
[3.6140944957733154, 4.36362361907959, "The Internal Data Speed of the DHU Data Handling Unit is Up to 10 Mbit/s."]
[7.413813591003418, 4.631383419036865, "The Data Collection of the ASTRO-H Satellite is Gas dynamics, particle acceleration, maximum energy of the accelerated particles."]
[8.271240234375, 1.003747820854187, "The Mission Duration of the CM1 Satellite is September 2021 through 2026."]
[8.23945140838623, 3.123612403869629, "The Conference Presentation Date of the TanDEM-X Satellite is April 23-26, 2012."]
[11.815821647644043, -1.1304805278778076, "The Launch Mass of the Konnect Satellite is 3619 kg."]
[7.53187370300293, 1.250138521194458, "The Date of the Space-based Automatic Identification System Experiment (SPAISE) Experiment is June 5-12, 2011."]
[8.252961158752441, 3.6231391429901123, "The Number of Satellites of the HawkEye 360 Satellite Constellation is Not Provided."]
[5.951311111450195, 3.7825043201446533, "The Location of the ESA Data Node is Esrange, Kiruna, Sweden."]
[7.770837783813477, 8.97777271270752, "The Spectral Range of the UV-1 Spectrometer is 270 - 314 nm."]
[1.8336436748504639, 4.008445739746094, "The Number of Cells per Array of the Solar Panel Power Generator is 26."]
[6.098024368286133, 8.002623558044434, "The Frequency Range of the MTVZA-GY Radiometer is 10-48 GHz."]
[5.958342552185059, 2.1809117794036865, "The Endurance of the TSUBAME Satellite is Able to endure the Dnepr rocket vibrations."]
[6.8413591384887695, 1.0847758054733276, "The Datasheet Release Date of the ADS-B Receiver Space Application Receiver is 22 Sept. 2015."]
[10.658378601074219, 2.776362419128418, "The Orbit Shift Distance of the GomX-4A Satellite is Up to 2000 km."]
[9.225539207458496, 3.1903457641601562, "The Orbit of the Resurs-P1 Satellite is Sun-synchronous near circular orbit."]
[7.8817138671875, 6.855415344238281, "The Duration of the Calibration Phases Process is Not specified."]
[8.304572105407715, 6.2857255935668945, "The Required Spacecraft Stability of the Framer Sensor is Low."]
[7.934520721435547, 9.303078651428223, "The Spectral Sampling Distance of the SWIR Spectrometer Spectrometer is 10 nm."]
[7.141835689544678, 8.854877471923828, "The Spatial Resolution of the GMI Instrument is Excellent."]
[3.073693037033081, 5.9675493240356445, "The Data Delivery Time of the SafetyNetTM Data Collection Architecture is 75% within 15 minutes, 95% within 26 minutes."]
[11.337008476257324, 3.5689263343811035, "The Total Volume of the Comet Celestial Body is 21.4 km3."]
[9.862083435058594, -0.9129081964492798, "The Size of the Triton-1 Nanosatellite is 3U."]
[9.515873908996582, 3.0776596069335938, "The Orbit of the Herschel Telescope Telescope is Large Lissajous orbit around the L2 point at a distance of around 1.5 million km from Earth."]
[6.339019298553467, 3.2938382625579834, "The Mission Operator of the SPOT 6-7 Satellite is Airbus Defence and Space."]
[8.749844551086426, 3.173144817352295, "The Orbit Decay Cause of the GOCE mission Satellite Mission is Uncompensated atmospheric drag."]
[6.9597086906433105, 5.446589946746826, "The Monitoring Purpose of the SMOS Satellite is Ocean acidification."]
[6.973893165588379, 0.075533427298069, "The End of Life Date of the FormoSat-1 Satellite is June 17, 2004."]
[4.022442817687988, 5.23402738571167, "The Power Consumption of the ODTML Data Collection System is < 0.1 Joule per bit transmitted."]
[6.908188343048096, 1.0552617311477661, "The Conference Date of the Space Technology 5 Satellite is Feb. 3-7, 2007."]
[4.425176620483398, 4.6224684715271, "The Components of the SIR-2 Instrument is Sensor unit, power unit, ICU."]
[10.32776165008545, 2.924984931945801, "The Orbit Altitude of the QSat Satellite is 500-700 km."]
[4.32826566696167, 7.194490909576416, "The Weight of the RPU Receiver Processor Unit is 16 kg."]
[11.717766761779785, 1.6871458292007446, "The Mission Status of the Philae Lander is Active."]
[9.369833946228027, 4.939139366149902, "The Slew Maneuvers of the MicroSat-70 Satellite is Within \u00b115\u00ba about the roll axis (or \u00b1180\u00ba about the yaw axis)."]
[4.7416791915893555, 1.8190419673919678, "The Number of Passes over Stations of the SPOT-6 Satellite is 4 passes over the Toulouse station and 8 passes over the Kiruna station."]
[6.131157875061035, 3.4577958583831787, "The Service of the Spire Global UK Company is Predict vessel locations and the ship\u2019s estimated time of arrival at port."]
[6.784893035888672, 3.818162441253662, "The Mission of the INSAT-3DR Satellite is Provide service continuity to earlier ISRO meteorological missions."]
[6.73588228225708, 4.003387928009033, "The Satellite of the Sentinel-4 Mission is MTG."]
[9.025141716003418, 0.5495186448097229, "The Planned Operation Duration of the Tiangong Space Station is 15 years."]
[5.818626403808594, 3.0741629600524902, "The Manufacturer of the SPOT 7 Satellite is Astrium."]
[10.021784782409668, 1.5500667095184326, "The Nodal Period of the Satellite HY-1B is 100.8 minutes."]
[8.573387145996094, 8.940826416015625, "The Wavefront Error of the Sentinel-4 GRU Grating Reflection Unit is 19.8 nm (rms)."]
[4.0038251876831055, 4.43279504776001, "The Operation of the OBC Architecture On-Board Computer Architecture is Independent real time tasks to be executed simultaneously."]
[10.316210746765137, 9.548903465270996, "The Usage of the Iris Radio is Raw measurements transfer and remote control of the spacecraft."]
[5.757007598876953, 9.112393379211426, "The 2.5 W/sensor head of the Instrument Power Sensor is Instrument power 2.5 W/sensor head."]
[8.44752311706543, 9.503089904785156, "The Pore Size of the ICON FUV Instrument MCP is 6 mm."]
[5.801553249359131, 2.151153802871704, "The Launch Site of the COPPER CubeSat Satellite is MARS (Mid-Atlantic Regional Spaceport), located at NASA's Wallops Flight Facility,Wallops Island, VA."]
[1.785260796546936, 5.375603675842285, "The Current of the Voltage 6 Modulator is 200."]
[6.936516761779785, 2.5123777389526367, "The URL of the Dellingr Satellite is http://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=3614&context=smallsat."]
[8.593781471252441, 10.2294340133667, "The Purpose of the SPIDER Imaging Sensor is 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."]
[8.53940200805664, 10.907105445861816, "The Size of the Kodak KAI-11002 CCD CCD is 37.25 mm (H) by 25.7 mm (V)."]
[10.273728370666504, 4.779125690460205, "The Propellant of the Aquajet Satellite Propulsion System is Water & anti-freeze."]
[7.228719234466553, 8.022768020629883, "The Integration Time of the Optics Device is 15 ms."]
[8.0669527053833, 11.135431289672852, "The Sensitivity of the Channel 1 Sensor is 0.5 K/pixel."]
[5.545128345489502, 2.7150533199310303, "The Manufacturer of the Hiber-3 Satellite is Hiber."]
[9.573795318603516, 7.466125965118408, "The Stages of the Cooler Passive Cooler is 4."]
[7.540208339691162, 8.1183443069458, "The Spectral Channels of the CERES Scanner is 3."]
[6.883151054382324, 2.342792510986328, "The Data Collection of the Galileo Spacecraft is Flyby of Europa in 2000."]
[6.428041934967041, 4.646828651428223, "The Level-1 GRD Products of the Sentinel-1 Satellite is Focused data projected to ground range, detected and multi-looked."]
[8.05324935913086, 2.1693837642669678, "The Launch Date of the Artemis-I Mission is 16 November 2022."]
[7.425372123718262, 5.938023567199707, "The Observation of the Suomi NPP satellite Satellite is Huge Saharan dust plume streaming over the North Atlantic Ocean."]
[4.314449310302734, 4.469249725341797, "The Interface of the MuREM Radiation Monitor is CAN bus."]
[3.167235851287842, 5.292177677154541, "The Capacity of the Solid-State Recorder Data Storage is 3 Gbit."]
[7.670516014099121, 0.9166431427001953, "The Release Date of the Imja glacier, Himalayas Location is March 14, 2014."]
[7.923214912414551, 8.33482837677002, "The Advance in Accuracy Over Current Instruments of the CLARREO\u2019s infrared and reflected solar spectrometers Spectrometers is Unknown."]
[5.80119514465332, 3.74360990524292, "The Data Handling of the Stensat Satellite is Keeps the most recent science packet as part of a beacon packet."]
[5.24905252456665, 3.218229055404663, "The Bus Type of the BILSAT-1 Satellite is MicroSat-100 bus."]
[11.470405578613281, 5.9821696281433105, "The Launch Date of the Chandra X-ray Observatory X-ray Observatory is July 23, 1999."]
[5.727636814117432, 1.6818931102752686, "The Communication Links of the GomX-4A and GomX-4B CubeSats is UHF and S-band."]
[4.7627668380737305, 1.8462318181991577, "The Number of Supersites of the MAPS Satellite is 19."]
[9.329442024230957, 6.447619438171387, "The Components of the Astro-APS Star Tracker is Camera head, electronics, and a shorter baffle."]
[4.840936183929443, 5.062781810760498, "The Communication of the LightSail 2 Satellite is Successful."]
[10.377777099609375, 8.332883834838867, "The Purpose of the Pumbaa and Timon smallsats Satellite is Obtain images of solar corona."]
[6.885325908660889, 8.828751564025879, "The Backscatter of the Mie co-polar channel Channel is 8 x 10 -7 sr -1 m -1."]
[8.644453048706055, 6.999323844909668, "The Ranges of the MAG Sensor Sensor is \u00b11024, \u00b14096, \u00b116,384, \u00b165,536 nT."]
[5.069478988647461, 7.56514835357666, "The Data Rate of the HIA Instrument is 3.12 kbit/s."]
[11.57741928100586, 4.3846235275268555, "The Roundness of the Kepler 11145123 Star is More round than the Sun."]
[9.475569725036621, 5.832753658294678, "The Attitude Restitution of the Attitude Control Subsystem (ACS) Attitude Control System is 6 x 10-5 radians."]
[8.307883262634277, 0.5924225449562073, "The Communication Failure of the Hitomi Satellite is March 26, 2016."]
[7.249120712280273, 7.118354320526123, "The SDR Validation of the VIIRS Instrument is Unknown."]
[2.0066823959350586, 3.8677330017089844, "The Examples of Technologies of the CubeSats Satellite is Advanced multi-junction solar cells and carbon nanotube batteries."]
[10.437483787536621, 2.6328060626983643, "The Apogee of the Satellite Orbit is 1500 km."]
[8.674294471740723, 1.9913440942764282, "The URL of the James Webb Space Telescope Telescope is http://www.roe.ac.uk/ukatc/consortium/miri/index.html."]
[1.2893126010894775, 4.167592525482178, "The Battery Capacity of the Spacecraft Bus (Avionics Module=AM) Satellite is 60 Ah."]
[9.342506408691406, 2.8220362663269043, "The Brightness Temperature Channels of the GCOM-W1 Satellite is 89.0 GHz, 23.8 GHz."]
[11.067941665649414, 4.237333297729492, "The Speed Before Jettisoning of the Orion Spacecraft is 480 km/hr."]
[6.7533488273620605, 0.8381329774856567, "The Launch Date of the FormoSat-5 Satellite is July 17, 2017."]
[9.075632095336914, 3.316199779510498, "The Orbit Decay of the LAGEOS Satellite is Won't decay."]
[6.919266700744629, 5.7665114402771, "The Development Period of the Argo Float Oceanographic Instrument is 1990-1997."]
[8.9444580078125, 2.2003586292266846, "The Observation of the New Horizons Spacecraft is How the volcanic gases from Io are ionized, trapped and energized by Jupiter's magnetic field, then ultimately ejected from the system."]
[8.537299156188965, 8.14355754852295, "The Not specified of the HTSSE-II Sensor is Not specified."]
[8.174259185791016, 7.525711536407471, "The Accuracy of the MEMS Rate Sensor Sensor is High."]
[5.169375419616699, 1.9693975448608398, "The Number of Tests of the SuperDraco Engines Spacecraft Component is Hundreds."]
[11.1989107131958, -1.5334343910217285, "The Mass of the Landmapper-BC CubeSat is 11 kg."]
[11.592933654785156, 4.307429790496826, "The Rotation Period of the Zeta Puppis Star is 1.78 days."]
[12.129343032836914, 3.2858355045318604, "The Orbit Inclination of the CBERS-4 Satellite is 98.55\u00ba."]
[7.316141605377197, 3.763256311416626, "The Purpose of the SPOT-4 Satellite is Environmental studies, crop monitoring and management, environmental forecasting."]
[9.484331130981445, 5.8970794677734375, "The Type of the Magnetorquers Attitude Control Device is Two cylindrical coils with ferrite cores, one flat square with no core."]
[6.399571895599365, 5.153979301452637, "The Instrument of the Tandem-L Satellite is L-band Synthetic Aperture Radar (L-SAR)."]
[7.803025722503662, 10.808314323425293, "The A/D Conversion of the VEU Video Electronic Unit is 12-bit."]
[8.28338623046875, 4.04807710647583, "The Field of View of the INTEGRAL Satellite is Large."]
[8.862496376037598, 3.5234689712524414, "The EMC Testing Configuration of the MPO Orbiter Spacecraft is Mercury orbiting mode."]
[7.14696741104126, 9.328536987304688, "The Spatial Resolution of the Stripmap Imaging Mode is 10 m."]
[4.055927753448486, 5.639001369476318, "The Download Transmission Rate of the DubaiSat-2 Satellite is 160 Mbit/s."]
[5.155582904815674, 3.7136287689208984, "The Components of the Spacecraft Bus Satellite is Star tracker, GPS receiver, IMU, fine sun sensor, magnetometer, reaction wheels, EPS, batteries, radio, antenna."]
[8.5753812789917, 2.068938970565796, "The Communications Link of the James Webb Space Telescope Space Telescope is Malindi ground station in Kenya."]
[9.991382598876953, -0.6473796367645264, "The Inclination of the IDEA-OSG 1 Microsatellite is 98\u00ba."]
[7.708507061004639, 10.683612823486328, "The Resolution of the A/D converter Data Converter is 16 MHz."]
[8.182372093200684, 8.499794960021973, "The Design Goals Met of the SHIMMER Spectroscopy Instrument is Yes."]
[8.549560546875, 2.164030075073242, "The Final Flyby Date of the Parker Solar Probe Satellite is November 2024."]
[9.2135009765625, 5.309853553771973, "The Actuators of the Slew Mode Satellite Mode is Reaction wheels as the primary actuators, and torque rods."]
[5.33865213394165, 2.4704461097717285, "The Post-Project Careers of the SAPPHIRE Satellite is Three are involved in strong system-based research and management in industrial or government laboratories."]
[6.687674522399902, 2.2573392391204834, "The Purpose of the UN Disaster Charter Agreement is Gives front-of-the-line access to information needed to respond to major disasters."]
[8.926738739013672, 7.388028621673584, "The Operation of the MERIS Sensor is Only out of eclipse and when the sun's zenith angle at the subsatellite point is less than 80\u00ba."]
[8.428848266601562, 10.146279335021973, "The Spectral Range of the Current GOES imager Sensor is 7.24-7.44."]
[8.161211013793945, 3.296959638595581, "The Imaging Frequency Band of the TanDEM-X Satellite is X."]
[7.186827182769775, 3.072187662124634, "The Unknown of the AIDA Mission is Unknown."]
[8.36673355102539, 6.375240325927734, "The Function of the CAL LR Calibration Launch Restraint is Provide an alternate load path to support the mass of the calibration targets without over loading the Despin Assembly."]
[9.654640197753906, 8.550932884216309, "The Mirror Shell Material of the ART-XC Instrument Telescope is Nickel-cobalt alloy with iridium coating."]
[8.363551139831543, 7.702270030975342, "The Manufacturer of the IREM Radiation Environment Monitor is ESA."]
[6.826749324798584, 1.2572054862976074, "The Partnership Date of the SpaceChain Company is Sept. 28."]
[7.372915744781494, 3.200706958770752, "The Student Collaboration Goal of the IMAP Mission is Provides scientific involvement in studying the origin of EPs in the innermost magnetosphere."]
[4.65200662612915, 3.4330008029937744, "The Configurations of the SATSIM Simulation System is GAS, SATLAB."]
[8.305068016052246, 9.060667037963867, "The Spatial Resolution of the HPT Sensor is High."]
[11.517085075378418, 2.143759250640869, "The URL of the Hayabusa2 Asteroid Explorer is http://global.jaxa.jp/activity/pr/brochure/files/sat33.pdf."]
[6.825767993927002, 5.532930850982666, "The Soil Moisture Accuracy of the SMAP Satellite is 0.04 cm3/cm3."]
[6.787085056304932, 1.30640709400177, "The Agreement Date of the BRITE-PL Satellite Project is May 2010."]
[10.237693786621094, 1.0120998620986938, "The LTDN of the Optsat-3000 Satellite is 10:30 hours."]
[10.890486717224121, 4.042236328125, "The 3D Visualization of the Exploded Star Celestial Object is Built with Help from NASA's Great Observatories."]
[10.934640884399414, 3.35174560546875, "The Distance from the Sun of the New Horizons Spacecraft is 50 AU."]
[11.754660606384277, 4.998992919921875, "The Mass of the J1820 Black Hole is Lower than supermassive black holes."]
[10.532660484313965, 7.523594379425049, "The Material of the Habitat Structure is Regolith mixed with water and bovine serum albumin."]
[5.6197733879089355, 9.186800003051758, "The Power Consumption of the FREND Instrument is 14 W."]
[2.325406312942505, 4.415623188018799, "The Electric Power of the FLP Satellite is 270 W."]
[1.5404086112976074, 4.902547836303711, "The Output Voltage of the PPM Power Processing Module is 28 V."]
[6.143200874328613, 3.3396999835968018, "The Agency of the Galileo Satellite Navigation System is ESA."]
[7.8744683265686035, 10.21364688873291, "The Swath of the WV60 imager Imaging System is 17.9 km."]
[7.286779403686523, 1.1742370128631592, "The Launch Date of the Kaber Spacecraft is Unknown."]
[2.14314866065979, 4.970004081726074, "The Output Power of the PPM Power Processing Module is 300 W."]
[6.4851789474487305, 5.288607597351074, "The Deformation Mode of the Tandem-L Satellite is Repeat-pass interferometry."]
[7.849618434906006, 9.913949012756348, "The Swath Width of the TrueColour Imager Optical Imager is 120 km."]
[8.671356201171875, 8.6726655960083, "The Field-of-View of the ISEM Instrument is 1\u00b0."]
[9.130202293395996, 9.944574356079102, "The Field of View (Individual) of the HRV Imager is 4.13\u00b0."]
[10.733088493347168, 10.29508113861084, "The ADC type of the PHA Detector is Wilkinson ADC."]
[7.599761486053467, 2.791123390197754, "The Eclipse Encounters of the Hinode Satellite is Total: 3."]
[3.52829647064209, 2.283622980117798, "The Size of the QBSout-1S FemtoSat is 2.5U."]
[3.5137107372283936, 4.112970352172852, "The RAM of the STRV-2 DHS Data Handling System is 512 k."]
[6.40437650680542, 5.489861965179443, "The Observation Method of the Global Positioning System Satellite System is Radio occultation."]
[7.379250526428223, 10.086947441101074, "The Spectral Channels of the HSI Hyperspectral Imaging System is Variable."]
[11.003351211547852, 3.414184093475342, "The Orbital Period of the Juno Spacecraft is 43 days."]
[4.517425060272217, 4.608259677886963, "The Instrument Control Document of the Advanced Data Collection System Data Collection System is Advanced Data Collection System Instrument Control Document, (A-DCS ICD)."]
[4.487936019897461, 5.553153038024902, "The Communication of the Dove-2 Satellite is TT&C over UHF radio."]
[11.742254257202148, 1.219112753868103, "The Landing Accuracy of the Chang'e-3 lander Lander is Better than 0.6 km."]
[7.240173816680908, 0.3993616998195648, "The Launch Date of the MoonLIGHT Satellite is 2024."]
[4.00549840927124, 5.59705924987793, "The Download Marking Behavior of the Data Download System Satellite System is All downloaded files are marked as downloaded after the completion of the download."]
[9.424694061279297, 4.794870376586914, "The Solar Elongation Range of the NEOSSat Satellite is 45\u00ba to 55\u00ba."]
[6.872007846832275, 1.1647177934646606, "The GNC 2011 Conference Date of the SEOSat/Ingenio Satellite is June 5-10, 2011."]
[10.939620018005371, 2.8392908573150635, "The Embankment Height of the Ataturk Dam Dam is 184 m."]
[4.211392402648926, 6.579675197601318, "The Transmit Frequency (MHz) of the Imager data Data Receiver is 1677.0."]
[10.6119384765625, 6.029336452484131, "The Flare List Events with Emission above 300 keV of the RHESSI Satellite is 35."]
[8.631484985351562, 2.5611109733581543, "The Original Orbit Parameters of the ARTEMIS Spacecraft is Perigee: 592 km, Apogee: 17,518 km, Inclination: 3\u00ba."]
[7.752002716064453, 8.307111740112305, "The Atmospheric Species of the UVS Instrument is K, Na, Al, Si, Ca, Li, OH, H2O."]
[10.29883861541748, 2.9199953079223633, "The Altitude of the ELaNa-4 CubeSats Satellite is 500 km."]
[9.560040473937988, 7.696247577667236, "The Energy Range of the ECT Suite Instrument Suite is 1 eV to 10's of MeV."]
[2.2128188610076904, 3.8488523960113525, "The Solar Panels Configuration of the LF spacecraft Spacecraft is Shown in Figure 2(a)."]
[7.411037921905518, 0.2391178011894226, "The Kick-off Meeting Date of the SMILE Satellite is Sept. 3-4, 2015."]
[11.747435569763184, 7.491247653961182, "The Time Uncertainty of the Deep Space Atomic Clock Atomic Clock is One nanosecond."]
[6.236631393432617, 3.1850786209106445, "The Partners of the ExoMars Program is ESA and Roscosmos."]
[7.786189556121826, 2.905796527862549, "The Launch Date of the CartoSat-2D Satellite is February 15, 2017."]
[6.523496150970459, 6.51680850982666, "The Resolution of the Scatterometer Antenna Antenna is 25 km."]
[9.173870086669922, -0.6235846877098083, "The Deployment Date of the Flock 1a Nanosatellites is February 2014."]
[7.087610244750977, 0.898848295211792, "The Launch Date of the EMIT Satellite is Unknown."]
[5.316659927368164, 10.380732536315918, "The Data Sharing of the ISS LIS Lightning Imaging Sensor is National forecast offices, NOAA/AWA."]
[8.274833679199219, 5.240617752075195, "The Objectives of the S 331 Satellite is Measurement of the three components of the DC and ULF magnetic field."]
[7.872638702392578, -0.13209639489650726, "The Planned Docking Date of the Nauka Laboratory Module is 23 July 2021."]
[3.6685009002685547, 6.171061038970947, "The Downlink Speed of the Communication links Communication subsystem is 9.6 - 38.4 kbit/s."]
[8.368297576904297, 0.35000520944595337, "The Length Increase of the BEAM Expandable Habitat is Nearly doubled."]
[5.148970127105713, 2.3760323524475098, "The Failure Rate of the CubeSats Satellite is 40%."]
[12.989295959472656, 4.86122465133667, "The Science Operations Support Conference Date of the IBEX Satellite is March 3-10, 2012."]
[7.836886405944824, 0.6708855628967285, "The Installation Date of the UrtheCast Cameras Camera is Jan. 28, 2014."]
[1.4839699268341064, 4.382815361022949, "The Unknown of the FEE Power Convertors Power Convertors is Unknown."]
[6.090627193450928, 1.9352127313613892, "The Launch Vehicle of the OneWeb Satellite Communications Company is PSLV (Polar Satellite Launch Vehicle) and GSLV-MkIII (Geosynchronous Satellite Launch Vehicle)."]
[11.622268676757812, 6.1672682762146, "The Observation Date of the XMM Newton telescope Telescope is June 29, 2021."]
[10.587614059448242, 7.520080089569092, "The External Parts of the WISA Woodsat Satellite is Corner aluminum rails, metal selfie stick."]
[6.914494514465332, 0.3176769018173218, "The Data User's Manual Edition of the IRS-P6 Satellite is Oct. 1, 2003."]
[5.715882778167725, 6.713006973266602, "The Polarization of the C-RADAR Phased Array Antenna System is V and H."]
[7.9859089851379395, 4.010821342468262, "The Dimensions of the Carbon Dioxide Ice Patch Surface Feature is 80 m x 60 m."]
[9.290821075439453, 0.4393719732761383, "The Design Life of the Jason-2 Satellite is 3 years."]
[5.001398086547852, 2.023007392883301, "The Mission Number of the CubeSat Satellite is 17."]
[7.566230297088623, 7.528676986694336, "The Type of the OSIRIS Instrument is Atmospheric chemistry."]
[10.197834968566895, 3.100604295730591, "The Dynamic Range of the SXI Spacecraft is 1000."]
[6.439530849456787, 3.454537868499756, "The Development of the TRISHNA Satellite is Joint by the French Space Agency (CNES) and the Indian Space Research Organization (ISRO)."]
[6.444394588470459, -0.6922050714492798, "The L1-SAIF Signal Augmentation Performance Presentation of the QZSS Satellite System is ION NTM (National Technical Meeting) 2007, San Diego, CA, USA, January 22-24, 2007."]
[5.747999668121338, 2.2636497020721436, "The Goal of the Small Photon Entangling Quantum System (SPEQS) Quantum Light Source is Enable a QKD link between satellites, or between a satellite and an optical ground station."]
[6.082045078277588, 9.72592544555664, "The Mass of the Space Comb Spectroscopy Setup is Below 10 kg."]
[9.709869384765625, 1.2779189348220825, "The Orbit Lagging Time of the Observatories Satellite is About 1 month later."]
[5.28141450881958, 4.974604606628418, "The Type of the Kurushima Kaikyo Bridge Bridge is Continuous suspension."]
[12.16828441619873, 2.134614944458008, "The Deep Space Maneuver Date of the OSIRIS-REx Spacecraft is 3 July 2018."]
[10.186904907226562, 9.817475318908691, "The Development Initiation Date of the IRIS Imager Camera is April 2002."]
[8.37356948852539, 1.2438697814941406, "The Data Distribution Start Date of the GOCI Geostationary Ocean Color Imager is April 20, 2011."]
[7.630824565887451, 0.4454764127731323, "The Launch Date of the GRACE-FO Satellite is Early 2018."]
[7.264869689941406, 8.86234188079834, "The Pixel Size at Nadir of the CIPS Instrument is ~2 km."]
[8.409380912780762, 9.278966903686523, "The Spectral Resolution of the ICON FUV instrument Spectrometer is High enough to reject unwanted contamination by the bright optically thick 130.4 nm O line."]
[7.717608451843262, 5.598117351531982, "The SNR Saturation of the SCATSat-1 Satellite is 50%."]
[10.14209270477295, 4.422731876373291, "The Thruster of the Clementine Spacecraft is 489 N."]
[5.063076972961426, 7.551764011383057, "The Data rate of the Spectrometer Spectrometer is 1.5 Mbit/s (average), 1.5 Mbit/s (max)."]
[6.9220290184021, 1.1715291738510132, "The Presentation Date of the Small Satellites Satellite is Sept. 29 to Oct. 3, 2008."]
[8.503313064575195, 1.1132359504699707, "The Update Date of the LROC Robotic Spacecraft is Sept. 25, 2013."]
[7.863384246826172, 7.235355377197266, "The Operational Cadence of the Instrument Satellite Instrument is Rotate to 120\u00ba in < 2 minutes to nadir view."]
[4.034426212310791, 4.772994518280029, "The Downlink Subsystem Interface of the Frame Grabber Data Interface is Ethernet."]
[9.419708251953125, 8.683675765991211, "The Coating of the FPI Mirrors Component is Silver coating (thickness 50 nm)."]
[6.682581424713135, 2.48714017868042, "The URL of the Aleph-1 Constellation Satellite Constellation is https://satellogic.com/technology/constellation/."]
[6.867196559906006, 4.32037353515625, "The Provider of Earth observation data of the Copernicus Environmental Monitoring Satellites is Yes."]
[8.536080360412598, 1.7229361534118652, "The Status Update Date of the James Webb Space Telescope Space Telescope is May 19, 2009."]
[7.354761600494385, 10.044705390930176, "The Function of the Hyperspectral Imaging Remote Sensing Technology is Enables the observation and monitoring of surface measurements."]
[10.642523765563965, 9.224224090576172, "The Image Capture Date of the CaSSIS Imaging System is 31 May 2018."]
[8.555074691772461, 7.865335464477539, "The Installation Location of the REM Radiation Environment Monitor is Externally on the fore panel."]
[5.696685314178467, 3.5318121910095215, "The Design Philosophy of the SMEX Satellite Program is Emphasis on design simplicity, functional independence at subsystem level, and flexibility to accommodate growth."]
[6.479365825653076, 7.544992446899414, "The Type of the T2L2 Time Transfer Device is Laser Link."]
[9.978713035583496, 5.06242036819458, "The Technology Demonstrations of the BeaverCube Satellite is Use of low-cost commercial cameras to obtain measurements and operation of Tiled Ionic Liquid Electrospray (TILE) propulsion technology."]
[5.038506984710693, 4.638665676116943, "The Components of the Ground Station Ground Segment is Receiving antenna, antenna rotating and control system, low noise amplifier, receiver, ground station control software."]
[6.8757476806640625, 5.720649242401123, "The Deployment Methods of the Argo Floats Oceanographic Instrument is Volunteer Observing Ships (VOS), aircraft, naval ships and research vessels."]
[10.190934181213379, 3.0040268898010254, "The Orbit Altitude of the ResourceSat-1 Satellite is 817 km."]
[5.382726192474365, 3.398350715637207, "The Manufacturer of the OBI Component is EADS Astrium."]
[9.961714744567871, 1.42507803440094, "The Orbit (Local Sun Time) of the Spacecraft Satellite is 12:00 \u00b1 15 min."]
[8.579682350158691, 2.5971734523773193, "The Orbit of the JPSS Joint Polar Satellite System is Afternoon (13:30 hours)."]
[4.930328369140625, -3.2086541652679443, "The | of the Michele Piana Author is Michele Piana."]
[7.614024639129639, 8.413918495178223, "The Polarization of the Atmospheric-sounding instrument Spectrometer is Lower than 0.1% in both nadir and glint modes."]
[8.908266067504883, 4.800560474395752, "The Operational Control of the MEV-1 Satellite is Full 6-DOF (Degree of Freedom)."]
[9.874576568603516, 3.947014570236206, "The Flight Status Presentation Date of the IKAROS Solar Sail Demonstrator is Sept. 27-Oct. 1, 2010."]
[11.890743255615234, -1.0831588506698608, "The Launch Mass of the Falcon-9 Rocket Rocket is 13,620 kg."]
[5.795016765594482, 2.6278717517852783, "The Manufacturer of the SOAR Satellite is GomSpace."]
[7.6880059242248535, 2.5566768646240234, "The URL of the ARTEMIS satellite Satellite is http://telecom.esa.int/telecom/www/object/index.cfm?fobjectid=31816."]
[7.635005950927734, 4.460104465484619, "The Observation Frequency of the ALOS-2 Satellite is Four times a year."]
[7.4522552490234375, 4.531078815460205, "The Image Type of the ALOS-3 Satellite is Pan-sharpened images with simultaneous acquisition of panchromatic images and four-band multi-spectral images."]
[10.070905685424805, 4.538437843322754, "The Propulsion System of the Psyche Spacecraft is Solar Electric."]
[4.388413906097412, 3.241673707962036, "The Target Markets of the Satellite for 5G Satellite is Transport sector (maritime, aviation and land), public safety, and media and broadcasting."]
[3.8965518474578857, 5.614189147949219, "The Data Allocation of the Remote Sensing Instruments Instruments is Insufficient to downlink the full raw data."]
[9.055235862731934, 9.23197078704834, "The Cross-Track Tilt of the Geoton-1 Imaging Instrument is \u00b1 30\u00ba."]
[9.211813926696777, 4.292003631591797, "The Canister Size of the IAE Experiment Satellite Component is 2.04 m x 1.08 m x 0.5 m."]
[8.49172306060791, 1.8749221563339233, "The Mission Proposal Year of the Euclid Space Telescope is 2007."]
[8.85245418548584, 7.048882007598877, "The Science Focus of the IMPACT Instrument is Magnetic connections to the sun, topology of interplanetary CME-related interplanetary disturbances, and the energetic particles."]
[8.170636177062988, 8.469103813171387, "The Detector Focus of the SHS System Interferometer is Nearly focused."]
[7.671998977661133, 8.967787742614746, "The Spectral Resolution of the Miniature High-Resolution Imaging Spectrometer Imaging Spectrometer is 0.1 nm."]
[11.344468116760254, 1.5088818073272705, "The Travel Distance of the Yutu 2 Lunar Rover is 590 meters."]
[4.96389627456665, 4.473609924316406, "The Acquisition Planning follow-up of the CSK GS Ground Segment is Provide the S-IM with the planning of its acquisition requests."]
[4.769505500793457, 5.172699928283691, "The Communication System of the TRMM Satellite is Telemetry, Tracking and Control (TT&C) transponders."]
[6.855220317840576, 0.718071699142456, "The Acquisition Date of the OHB AG Company is June 28, 2011."]
[7.872514724731445, 1.278417706489563, "The Science Data Collection Start Date of the CloudSat Satellite is June 2, 2006."]
[10.515311241149902, 7.228771209716797, "The Material of the Tether Satellite Component is Spectra woven around yarn."]
[9.529641151428223, 1.1880601644515991, "The Mission Duration of the TIMED Satellite is Ongoing."]
[9.621848106384277, 1.8338031768798828, "The Image Capture Frequency of the Elektro-L Satellite is Every 15-30 minutes."]
[8.234613418579102, 4.920496940612793, "The Relative Positioning Accuracy of the PRISMA Satellite is Sub-centimeter level."]
[6.714492321014404, 2.6735177040100098, "The URL of the Galileo Satellite System is http://m.esa.int/Our_Activities/Navigation/Europe_s_next_Galileo_satellites_in_place_atop_Ariane_5."]
[2.049468755722046, 3.7828431129455566, "The Solar Array Type of the TacSat-2 Satellite is Thin-film."]
[3.023528575897217, 6.572397708892822, "The Transmitting Power of the Transmitter Device is Use of power monitor."]
[6.435788154602051, 2.905444622039795, "The Function of the Galileo App Mobile Application is Overlaid Satellites in Real Time."]
[7.801846504211426, -0.5483095049858093, "The Launch Date of the SpaceX CRS-13 Mission is December 15, 2017."]
[12.155312538146973, 3.279773712158203, "The Orbit Inclination of the HY-2C Satellite is 66\u00ba."]
[3.649061918258667, 6.066310405731201, "The Data Rate of the IPS Pointing System is 16 Mbit/s."]
[5.582054615020752, 6.164802074432373, "The Number of Panels of the SAR Antenna Antenna is 8."]
[6.946712493896484, 8.689757347106934, "The Ground Resolution of the LISS-IIM Instrument is 32 m x 37 m."]
[9.40260124206543, 8.504444122314453, "The Design Requirement 1 of the OCO-3 PMA Pointing Mirror Assembly is Allow quick movement through a large range of angles."]
[9.404573440551758, 1.782968521118164, "The Yaw Flip Frequency of the Spacecraft Satellite is Twice during the one-year mission."]
[5.281828880310059, 6.400277137756348, "The Polarization of the VDES Antenna Antenna is Circular."]
[7.157641887664795, 3.847905397415161, "The Remarks/Sensors of the OrbView-1 Satellite is OTD."]
[5.4172563552856445, 2.9106104373931885, "The Manufacturer of the MEOLUT Next Local User Terminal is Thales Alenia Space."]
[7.75400972366333, 0.9805863499641418, "The Presentation Date of the SLS-Orion Missions Space Missions is Oct.12-16, 2015."]
[4.41524600982666, 6.258239269256592, "The Band of the RF Communications Transmitter is Ku-band and S-band."]
[7.209959030151367, 2.5632243156433105, "The URL of the Chandra Satellite is https://www.nature.com/articles/s41467-018-06558-7.pdf."]
[3.921243667602539, 2.2980639934539795, "The Size of the CHEFSat-2 CubeSat is 3U."]
[7.419454097747803, 7.941186428070068, "The Precision of the Ozone Measurement Instrument Atmospheric Measurement Device is 3 DU+0.5% total ozone or better."]
[9.185213088989258, 0.6132401823997498, "The Safety Criterion of the EO-1 Satellite is The six-second tolerance."]
[6.68698787689209, 7.601620674133301, "The Model of the Laser Rangefinder Device is Jenoptik DLEM-SR."]
[8.386273384094238, 6.994924545288086, "The Purpose of the CDE Sensor is Measure the temporal variability of meteoric material."]
[3.9562766551971436, 2.3741462230682373, "The Size of the ExoCube Satellite is 3U CubeSat."]
[9.374225616455078, 1.0096945762634277, "The Mission Duration of the SeaWiFS Satellite is Thirteen Years."]
[4.720588207244873, 6.110771179199219, "The Data Communications Transceiver Frequency of the OSSI-1 Satellite is 435 MHz."]
[4.708942890167236, 1.7891467809677124, "The Number of Satellites per Orbital Plane of the T1TL Prototype Constellation Satellite Constellation is 21."]
[8.621370315551758, 7.004640579223633, "The Magnitude Random Error of the Magnetic Field In-Situ Sensor is < 0.3 nT."]
[8.60498332977295, 5.1167144775390625, "The Observation Demonstration of the FORTE Satellite is Multisatellite observations of oceanic lightning."]
[7.082252502441406, 0.7773325443267822, "The Internet Demonstration Time Frame of the UoSAT-12 Satellite is April-June 2000."]
[6.6786885261535645, 0.698203444480896, "The Data Set Release Date of the GEOSAT Satellite is June 1997."]
[4.181210517883301, 5.614577770233154, "The TT&C Downlink of the Spacecraft bus Satellite is 30 kbit/s."]
[8.6379976272583, 6.952240943908691, "The Range of the Magnetometer Sensor is \u00b160 \u00b5Tesla."]
[3.536393880844116, 4.545251369476318, "The FPGA of the SHU Science Handling Unit is Altera EP3SL70F780I3 (Stratix-III)."]
[9.213418006896973, 4.21398401260376, "The Central Hole Diameter of the XMM Service Module Satellite Module is 2.10 m."]
[9.604851722717285, 1.3163503408432007, "The Daily Visibility of the Galileo Satellites 13 and 14 Satellites is Three to nine hours."]
[8.532818794250488, 4.230194568634033, "The Ultimate Goal of the BRITE Constellation Satellite is Provide photometric data on all 286 stars brighter than visual magnitude +3.5."]
[9.270319938659668, 3.3188016414642334, "The Daughterships Shape of the OPAL Satellite is Similar to a hockey puck."]
[9.015219688415527, 8.069786071777344, "The Bands of the SEM Particle Detector is 2 XRS bands, 5 EUV bands, 7 proton bands, 6 alpha particle bands, 3 electron bands."]
[5.959042549133301, 3.4147887229919434, "The Predecessor Organization of the DLR German Aerospace Center is DFVLR."]
[9.262651443481445, 6.450637340545654, "The Tracking Rates of the Astro-APS Star Tracker is 10 Hz."]
[10.410727500915527, 5.667906761169434, "The Upper and Lower End Masses Configuration of the ATEx Tether Experiment is In orbit as one object connected by a 22 m tether."]
[4.8398613929748535, -3.3871304988861084, "The Member of the Gary Egbert Individual is True."]
[5.035676956176758, 5.992132186889648, "The Operating Center Frequencies of the Satellite Satellite is 13.575 GHz (Ku-band), and 3.2 GHz (S-band)."]
[6.415653228759766, 9.609638214111328, "The Mass of the Miniature High-Resolution Imaging Spectrometer Imaging Spectrometer is 5.4 kg."]
[8.386958122253418, 3.88480544090271, "The Data Processing of the GPSP Instrument is No changes."]
[9.943338394165039, -0.7108952403068542, "The Telescope Aperture of the NEOSSat Microsatellite is 15 cm."]
[8.160120964050293, 8.595949172973633, "The Sun Angle of the OLCI Spectral Imaging Instrument is 12.2\u00b0."]
[5.770316123962402, 4.357448101043701, "The Data Encryption Capability of the NPOESS Program is Capable of encrypting selected mission data in all satellite links, excluding the S&RSAT and ADCS real-time downlinks."]
[7.6891584396362305, 3.4464480876922607, "The Data Availability of the Landsat 4 Satellite is All TM data January 2009."]
[11.174361228942871, 9.342561721801758, "The Channels of the Earth Radiation Budget Experiment (ERBE) Instrument is Total radiance (0.3 to 100 \u00b5m); Shortwave (0.3 to 5 \u00b5m); Window (8 to 12 \u00b5m)."]
[5.079719543457031, 5.468599796295166, "The Band of the Eutelsat Quantum Satellite is Ku-band."]
[7.155804634094238, 2.378976583480835, "The Orbit of the Konnect Satellite is GEO."]
[9.657075881958008, 0.8141171336174011, "The Loss of Communication of the AeroCube-3 Satellite is After 205 days on orbit."]
[4.614212512969971, 9.054083824157715, "The Operation Pause Date of the InSight Mars Lander is Around Oct. 7."]
[9.218404769897461, 9.241678237915039, "The Spatial Pixels of the Telescope Optical Instrument is 1024."]
[5.806926727294922, 2.9791200160980225, "The Manufacturer of the BlackSky\u2019s Global-4 Earth-imaging satellite is BlackSky."]
[7.274997234344482, 7.139345645904541, "The Affiliation of the SPADUS Instrument is A. J. Tuzzolino, R. B. McKibben, J. A. Simpson, S. BenZvi, H. D. Voss, H. Gursky."]
[7.805063724517822, 8.621672630310059, "The Exposure Time of the NISP Spectrograph Instrument is About 4000 seconds."]
[8.852808952331543, 5.1499786376953125, "The Attitude Pointing Accuracy of the GF-2 spacecraft Satellite is 0.0025\u00ba."]
[9.359174728393555, 10.241007804870605, "The Tilt of the PAN-F Camera is 26\u00ba."]
[9.900546073913574, 4.097175121307373, "The Purpose of the NanoSail-D2 Satellite is Demonstrate and test the deorbiting capabilities of a large low mass high surface area sail."]
[7.8536763191223145, 3.4515578746795654, "The PI of the SPARCS Satellite is Evgenya Shkolnik."]
[7.7831926345825195, 9.102550506591797, "The Spectrometer Bands of the GeoCarb Instrument is 0.76 \u00b5m, 1.61 \u00b5m, 2.06 \u00b5m and 2.32 \u00b5m."]
[12.138856887817383, 3.32357120513916, "The Orbit Inclination of the HTV-8 Spacecraft is 51.6\u00ba."]
[7.643617630004883, 3.131589651107788, "The URL of the CartoSat-1 Satellite is http://www.gaf.de/.../pr_germany_euromap_antrix_01-2008.pdf."]
[6.47199010848999, 6.782708644866943, "The Data Upload Frequency of the Base Station Data Collection System is Every half an hour."]
[8.105733871459961, 1.3736087083816528, "The Observation Date of the Eruption Solar Event is March 12 and 13, 2016."]
[4.9967360496521, 3.2499494552612305, "The Concept Developed of the CubeSat-based Optical Crosslink Nodes Satellite is Yes."]
[1.685887098312378, 4.237792015075684, "The Solar Cells of the EPS Electric Power Subsystem is 24."]
[8.102575302124023, 3.080643892288208, "The Operation as Radar Interferometer of the TerraSAR-X and TanDEM-X Satellites is Since December 2010."]
[7.966290473937988, 10.289487838745117, "The Field of Regard of the WV60 imager Imaging System is 900 km."]
[4.657082557678223, 9.043981552124023, "The Marsquake Discovery Date of the InSight Mars Lander is 22 September 2021."]
[9.34876823425293, 7.834646701812744, "The Ion Energy Threshold of the DIDM Instrument is Certain threshold potential."]
[12.092185020446777, 2.136337995529175, "The Sample Mass of the OSIRIS-REx Spacecraft is At least 60 gram."]
[4.981632709503174, 4.632065773010254, "The Position and Attitude Determination of the Ground Station System is Automatic."]
[8.035228729248047, 3.6057403087615967, "The Ability of the THEMIS Satellite is Orbit Adjustment."]
[2.4689431190490723, 5.536539554595947, "The Manufacturer of the AD9694 Analog-to-Digital Converter is Analog Devices."]
[8.700231552124023, 5.425869464874268, "The Alignment of the GT Fine-Pointing Error Signal Provider is Nominally aligned with the spacecraft axes."]
[10.2774658203125, 6.840047836303711, "The Development Methodology of the TCS Thermal Control Subsystem is Corresponded to the recommendations of the ECSS."]
[7.092093467712402, 4.691275119781494, "The Short Range Navigation of the ATV-5 Spacecraft is Optical sensors on ATV."]
[8.056294441223145, 4.3776679039001465, "The DEM Resolution of the Terra/ASTER system Satellite System is 30 m."]
[5.030685901641846, 1.8954403400421143, "The Number of Non-Separating Components of the ORS-3 Mission is 2."]
[6.395492076873779, 1.5314029455184937, "The Launch Date of the Jason-1 Satellite is Dec. 07, 2001."]
[2.23922061920166, 4.691598892211914, "The Power Dissipation of the SVM Service Module is 330 W."]
[4.8861308097839355, 4.87605619430542, "The Data Transmission of the Ground Station Contact Communication is Occurs above the corresponding minimum elevation."]
[4.12404203414917, 5.590877532958984, "The Optical Link Bandwidth (Uplink) of the OICETS satellite Satellite is 2 Mbit/s."]
[11.418659210205078, -1.3529709577560425, "The Mass (kg) of the RADARSAT-2 Satellite is 2200."]
[11.84093952178955, -1.0306825637817383, "The Launch Mass of the EROS-A Satellite is 260 kg."]
[8.472776412963867, 4.374196529388428, "The Single Pass Mono Coverage of the QuickBird-2 Satellite is 1 strip of 350 km."]
[6.8790106773376465, 0.3563744127750397, "The Acta Astronautica Publication Date of the IRS-P6 Satellite is Jan. 2007."]
[7.463958263397217, 8.382987022399902, "The MTF of the Instrument General is About 20% at Nyquist frequency."]
[2.224895477294922, 3.7916619777679443, "The Solar Panels of the GaoJing / SuperView minisatellites Satellite is Two on each of the pair of solar panel wings."]
[8.778478622436523, 0.7735449075698853, "The Destination of the Juice mission Spacecraft is Jupiter."]
[3.9807987213134766, 6.474721431732178, "The Duplex of the High-speed link Radio Link is Half."]
[9.890769958496094, 7.8058390617370605, "The Energy Range of the HIT High-energy Ion Telescope is ~2 to ~40 MeV/nuc."]
[8.08385181427002, 0.18077616393566132, "The Transfer Date of the BEAM Space Station Module is 21 January 2022."]
[4.151431560516357, 6.257251262664795, "The Protocol of the RF communication subsystem Communication Subsystem is AX-25."]
[5.999072551727295, 9.577186584472656, "The Mass of the PEACE Instrument is 6.5 kg."]
[6.483945369720459, 2.1008920669555664, "The Status in 2004 of the OPAL Satellite is Semi-operational."]
[8.4173002243042, 9.04809856414795, "The Perigee of the BUV Sensor is 1092 km."]
[4.536801815032959, 5.802629470825195, "The XPD of the SWOT Satellite is ~25dB."]
[4.806118965148926, 1.6175975799560547, "The Production Capacity of Factory of the Satellogic Satellite Company is 25 satellites a quarter."]
[3.2046854496002197, 5.14286470413208, "The Data Storage of the MMU Memory Management Unit is 32 Gbit."]
[8.8157320022583, 3.594944715499878, "The Formation Geometry of the TDX and TSX Satellites Satellites is Bistatic Close formation with Large Perpendicular Baseline."]
[10.410200119018555, 4.720430850982666, "The Delta V of the PROP unit Propulsion System is 10 m/s."]
[10.235702514648438, 2.9937336444854736, "The Orbit of the Restore-L Satellite is More than 600 km above Earth."]
[9.207338333129883, 9.058502197265625, "The Angular resolution (2 px) of the HRI Lyman-\u03b1 1216 \u00c5 Passband center is 1 arcsec."]
[8.568563461303711, 4.050488471984863, "The Moving Parts of the BRITE Telescope is None."]
[7.886624813079834, 4.532869815826416, "The Multispectral Imagery Resolution of the Satellogic Satellite Manufacturer is 1 meter."]
[11.708415985107422, -1.139443278312683, "The Mass of the Spacecraft Satellite is 1700 kg."]
[7.387446880340576, 9.205157279968262, "The Instrument size of the Spectrometer Spectrometer is 71 cm x 88 cm x 94 cm."]
[8.828614234924316, 3.622891664505005, "The Along-Track Separation of the TDX and TSX Satellites Satellites is 76 km."]
[7.27018928527832, 5.395661354064941, "The Background Concentration of the CO2 Greenhouse Gas is 415 ppm."]
[7.004255294799805, 0.13042819499969482, "The Terra Carta Supporter Date of the Satellite Vu Company is September 21, 2022."]
[4.034467697143555, 10.34892463684082, "The NE\u0394T (K) of the ICI-6 Radiometer is 1.2."]
[6.720316410064697, 6.119615077972412, "The Power Source of the RapidScat Scatterometer Instrument is Space station."]
[7.606707572937012, 9.744956970214844, "The Covered Area of the Image Data is Approximately 30 km x 50 km."]
[11.29578971862793, 3.7980010509490967, "The Comet Discovery Count of the SOHO Satellite is 2875."]
[9.563368797302246, 3.877082586288452, "The Payload of the CanX-7 Satellite is ADS-B."]
[10.87593936920166, 5.695395469665527, "The Authors of the Submerged Sources of Transient Acoustic Emission from Solar Flares Research Paper is 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."]
[6.790735721588135, 1.0589972734451294, "The Update Date of the CSDA Program is January 28, 2022."]
[6.77304744720459, 2.56819748878479, "The Download URL of the Earth Observation Constellation Satellites Satellite Constellation is http://www.nspo.narl.org.tw/ICGPSRO2013/download/2nd_ICGPSRO_U3-4A-102-02_Chen-Joe_Fong_05-16-2013.pdf."]
[5.338311195373535, 4.680922985076904, "The Command Transmission Capability of the Argos System Data Collection System is S/C-to-platform."]
[7.329570293426514, 0.6365842819213867, "The Launch Date of the OrbView-3 Satellite is June 26, 2003."]
[9.189085006713867, 5.852546215057373, "The Sensors of the Attitude Control Subsystem Attitude Control System is Sun sensors, star sensors and gyroscopes."]
[6.879763603210449, 4.072144985198975, "The Mission Objective of the DIDO-3 Satellite is Gather data by researching the effects of a microgravity environment on biological materials."]
[11.71993350982666, 1.6397467851638794, "The Regained Contact Time of the Philae Lander is 22:19 GMT."]
[3.819636821746826, 2.3490283489227295, "The Size of the JY1-Sat CubeSat is 1U."]
[8.6173677444458, 5.285323619842529, "The Pointing Knowledge of the HY-2A Satellite is < 0.05\u00ba."]
[9.59310245513916, -0.7284327745437622, "The Deployment Date of the BX-1 Microsatellite is Sept. 27, 2008."]
[7.524453163146973, 4.057791709899902, "The Measurement Category of the CryoSat Satellite is Gravity, Magnetic and Geodynamic measurements, Landscape topography, Ocean topography/currents, Sea ice cover, edge and thickness, Ice sheet topography."]
[5.654362201690674, 3.198612928390503, "The Recipient of the Payload Satellite Component is Clyde Space."]
[8.304285049438477, 3.8758254051208496, "The Onboard Sensors of the LAGEOS Satellite is None."]
[9.531258583068848, 7.716102123260498, "The Mode of Operation of the EPI-Lo Electron Detector is Single parameter measurement."]
[10.621480941772461, 6.041243553161621, "The Flare List Events with Gamma-ray Line Emission of the RHESSI Satellite is 27."]
[3.66536808013916, 5.205511569976807, "The Data Processing Capacity of the IDPS Interface Data Processing Segment is 100 times the volume of legacy data."]
[6.108456611633301, 0.6322574615478516, "The Launch Date of the ArgoMoon CubeSat is 16 November 2022."]
[11.274237632751465, 6.488063335418701, "The Publication Date of the SphinX Solar Photometer in X-rays is Nov. 2008."]
[6.428438663482666, -0.7150148749351501, "The SIS/URE of the QZS-1 Satellite is 40 cm (rms)."]
[8.524128913879395, 3.8082680702209473, "The Sky Coverage of the TESS Satellite is 85 percent."]
[3.868384838104248, 5.715035438537598, "The Average Duration of the LEO-LEO Inter-satellite Link Communication System is About 20 minutes."]
[9.16848373413086, 3.230659008026123, "The Orbit Type of the ResourceSat-2A Satellite is Sun-synchronous orbit."]
[4.884299278259277, 1.9747084379196167, "The Number of Hosted Payloads in Testing of the GHGSat Company is 3."]
[7.215904712677002, 3.2642414569854736, "The Mission Status of the ZY 1-02C Spacecraft is Operational."]
[5.852570533752441, 2.931684970855713, "The Structure and Power Systems Provider of the SloshSat-FLEVO Satellite is Dutch Space, Leiden, The Netherlands."]
[1.9847347736358643, 3.8215103149414062, "The Manufacturing of the SFINKS Solar Array is Made by depositing layers of thin-film of photovoltaic material on a flexible plastic."]
[4.083318710327148, 5.674160957336426, "The Ground Monitoring Data Rate of the EROS-A Satellite is 2.5 or 15 kbit/s."]
[8.026482582092285, 3.2930116653442383, "The Dimensions of the Fragments Space Debris is 2-D or 3-D."]
[7.965854644775391, 6.993908882141113, "The Parameter Estimation of the User Segment Geometrical Calibration Tool Calibration Tool is Exterior Orientation parameters and Interior Orientation deformations."]
[6.290706634521484, 8.172209739685059, "The 34 GHz Channel Function of the JMR Microwave Radiometer is Correction for non-raining clouds."]
[6.794496536254883, 0.31842195987701416, "The Operation Status of the FY-3C Satellite is Operating in 2016."]
[8.783970832824707, 6.975125312805176, "The Measurement of the SSAS Sensor is Spin rate."]
[6.395637512207031, 2.797741651535034, "The Manufacturer of the VRSS-1 Satellite is CGWIC (China Great Wall Industry Corporation)."]
[4.018064022064209, 6.433194637298584, "The Modulation of the RF communications Communication System is FSK."]
[8.168936729431152, 5.706337928771973, "The Accuracy of the Ionosphere Plasma Density Satellite System is < 20% (\u03c1=10 9  -10 11  m -3 ) \u2013 5% (\u03c1 >10 11  m -3 )."]
[9.341832160949707, 3.222266435623169, "The Orbit Type of the Secondary Payloads Satellites is Near-circular orbit."]
[9.590036392211914, 3.845566749572754, "The ISL Range of the CanX-4&5 Satellite is 5 km."]
[9.405928611755371, 5.5395708084106445, "The Pointing Accuracies of the AOCS Attitude and Orbit Control System is Pitch and roll = 0.2\u00ba, yaw = 0.4\u00ba."]
[7.617307186126709, 6.586433410644531, "The Typical Value of the AAOD Satellite Instrument is 0-0.05."]
[6.417867183685303, 1.0167313814163208, "The Launch Date of the Eutelsat Quantum Satellite is 2nd half of 2020."]
[6.087982654571533, -0.02883884496986866, "The Test Date of the Galileo Satellites Satellite is 4 December 2018."]
[10.498394966125488, 8.458998680114746, "The Volume of the MiniCOR Coronagraph is ~2U."]
[9.520442008972168, 0.5954196453094482, "The Mission Life of the CLARREO Pathfinder Satellite is 1 year."]
[5.255154609680176, 4.573694229125977, "The Locations of the Ground Stations Ground Stations is Oberpfaffenhofen, Neustrelitz, Adelaide/Australia and Iza\u00f1a/Tenerife."]
[1.6087466478347778, 4.841461658477783, "The Power Bus Voltage Range of the EPS Electric Power Subsystem is 25-32.8 VDC."]
[7.463906764984131, 1.178831934928894, "The Calibration Date of the Sentinel-1 Satellite is Sept. 9-13, 2013."]
[6.122673988342285, 4.866225719451904, "The Instrument of the Odin Satellite is OSIRIS."]
[1.3308029174804688, 4.162797451019287, "The Battery Capacity of the Spacecraft Satellite is > 30Ah @ EOL."]
[7.090259552001953, 2.5588290691375732, "The Presentation URL of the SVOM Satellite is https://indico.in2p3.fr/event/12490/session/3/contribution/7/material/slides/0.pdf."]
[11.345560073852539, 1.5292681455612183, "The Antennas of the Yutu-2 Lunar Rover is Three 5-meter antennas."]
[7.309683799743652, 3.630770683288574, "The Unknown of the GeoSTAR-III Satellite System is Unknown."]
[6.104204177856445, 0.5614902973175049, "The Launch Date of the ALBus CubeSat Satellite is December 16, 2018."]
[7.702741622924805, 3.26274037361145, "The Mission Objective of the IMAP Satellite is Learn more about the generation of cosmic rays in the heliosphere."]
[11.379459381103516, -1.3452237844467163, "The Total Mass of the QuakeSat Satellite is about 4.5 kg."]
[4.295331001281738, 5.468557357788086, "The Model of the USRP Transceiver is USRP N210."]
[8.040589332580566, 3.9807486534118652, "The Image Receiving Stations of the Pleiades System Satellite System is Japan, China and Canada."]
[4.5634260177612305, 5.609388828277588, "The LISS-I Data Downlink of the Satellite Satellite is S-band."]
[8.947516441345215, 7.343106746673584, "The Solar Environment of the SPC (Solar Probe Cup) Sensor is More severe than all previous experience."]
[9.50925064086914, 1.0181329250335693, "The Start Time of the Planning Process Satellite Mission is About three years before launch."]
[6.91551399230957, 0.3750118017196655, "The Rescheduled Launch Date of the OFT-2 Uncrewed Test Flight is No earlier than Aug. 3."]
[9.621831893920898, 3.9290611743927, "The Minimum Impulse Bit of the CanX-4&5 Satellite is 0.1 mNs."]
[7.306673049926758, 5.500632286071777, "The Dead Zone Impact of the Gulf of Mexico Body of Water is Impacts fish and the regional economy."]
[9.041385650634766, 9.353716850280762, "The Total FOV of the Sensor Unit Sensor is > 2\u03c0 sr."]
[9.472127914428711, 5.047021389007568, "The Spin Stabilization of the IMP-8 Spacecraft is 22.3 rpm."]
[7.229614734649658, 1.6276711225509644, "The Tandem Operations Start Date of the ERS-1 and ERS-2 Satellites is September 1995."]
[4.793468475341797, 1.80353581905365, "The Number of Satellites of the Constellation Satellite Constellation is 10."]
[7.694638252258301, 4.632234573364258, "The Precision of the ALOS-4 Satellite is Five times more than ALOS-2."]
[8.370194435119629, 3.394944429397583, "The Cumulated Absolute Height Error of the TanDEM-X Satellite is 3.5 m."]
[6.991500377655029, 4.740122318267822, "The Purpose of the Biomass satellite Satellite is Chart all the forests on Earth."]
[9.6776704788208, 7.474996089935303, "The Energy Range of the IMAP Satellite is 10 eV to 100 keV."]
[10.108603477478027, 7.698012828826904, "The Artists of the Sojourner 2020 Art Payload is Nine."]
[7.837150573730469, 7.150130748748779, "The Pointing Knowledge Stability of the Instrument Satellite Instrument is \u00b19.7 \u00b5radians over 34 minutes."]
[7.91092586517334, 4.676926136016846, "The Resolution of the Spotlight-1B Satellite is Finest."]
[9.322582244873047, -0.7959145903587341, "The Launch Provider of the SOCRATES Microsatellite is MHI (Mitsubishi Heavy Industries, Ltd.)."]
[6.410671234130859, 7.625383377075195, "The Operation Basis of the SILEX Laser Communication System is Direct-detection system."]
[8.330946922302246, 1.0690579414367676, "The Image Capture Date of the LRO Satellite is October 12, 2014."]
[9.591227531433105, 1.697629690170288, "The Repeat Orbit Cycle of the Sentinel-1A and Sentinel-1B Satellites is 12 days."]
[5.963373184204102, 2.6799509525299072, "The CEO of the CesiumAstro Company is Shey Sabripour."]
[6.716732978820801, 8.28587532043457, "The Global Coverage of the MERSI-RM Radiometer is Once per day on VIS/NIR/SWIR channels, and twice per day on MWIR/TIR."]
[9.29891586303711, 0.976810872554779, "The Record Duration of the Landsat Satellite is Four decades."]
[7.610926151275635, 2.121060848236084, "The URL of the ISEE-1 and ISEE-2 Satellites is http://www-ssc.igpp.ucla.edu/personnel/russell/papers/ISEE_fluxgate/."]
[9.145113945007324, 3.3014376163482666, "The Reference Orbit of the Spacecraft Satellite is SSO (Sun-synchronous Orbit)."]
[6.6629791259765625, 4.601093769073486, "The Data Contribution of the Sentinel-6 Satellite is Sea-level rise estimates."]
[6.442399024963379, 3.5979068279266357, "The Provider of the YouthSat Satellite is ISRO."]
[7.467111110687256, 3.5745527744293213, "The Access of the Airbus Constellation Satellite Constellation is Pl\u00e9iades, SPOT, TerraSAR-X, TanDEM-X radar and DMC Constellation."]
[6.4677300453186035, 3.4879822731018066, "The Mission Title of the Firefly Satellite Satellite is Understanding Earth\u2019s most Powerful Natural Particle Accelerator."]
[10.459955215454102, -1.153207778930664, "The Mass of the Max Valier Nanosatellite is 16 kg."]
[11.741739273071289, 1.6896636486053467, "The New Landing Site of the Philae lander Lander is Abydos."]
[9.145363807678223, 10.224944114685059, "The FOV of the LWIR Cameras Camera is 16\u00b0."]
[10.083264350891113, 1.590768814086914, "The Engine Firing Duration of the ExoMars TGO Orbiter is 52 minutes."]
[4.870347023010254, 6.6417460441589355, "The Antenna Gain of the LNA Low Noise Amplifier is 6 dBi."]
[6.5974555015563965, 2.721264362335205, "The URL of the SPIDER Imaging System is https://lockheedmartin.com/content/dam/lockheed-martin/eo/documents/webt/spider-infographic.pdf."]
[8.429931640625, 9.255355834960938, "The Slit 2 Spectral Range of the MEGS-A Spectrograph is 17.0 -37.0 nm."]
[6.4560160636901855, 0.6364201307296753, "The Launch Announcement Date of the MethaneSAT Satellite is 13 January 2021."]
[3.8115670680999756, 0.2801729142665863, "The Conference Date of the GRAIL Mission is June 11-15, 2012."]
[7.435300827026367, 1.0466612577438354, "The Acquisition Year of the Amptek X123 SDD Silicon Drift Detector is 2012."]
[8.823928833007812, 10.7836275100708, "The CCD Array of the WFC CCD Camera is 512 x 512."]
[4.0503973960876465, 6.6084699630737305, "The Uplink Frequency of the Myriad RF board RF Board is 300 MHz up to 3.8 GHz."]
[8.809480667114258, 6.54400110244751, "The Composition of the Plasma Matter is Gaseous and highly conductive charged particles."]
[11.148558616638184, 1.7839773893356323, "The Locomotion Mode of the Rosalind Franklin ExoMars rover Rover is Wheel walking."]
[3.565610885620117, 6.30539083480835, "The Uplink Rates of the LLCD PAT Systems Communication System is Up to 20 Mbit/s."]
[10.633001327514648, 8.557483673095703, "The Common Electronics of the COR1 Coronagraph1 imager is Common electronics, 1 MHz readout rate, 14 bit/pixel quantization."]
[3.813978910446167, 5.397773742675781, "The Digital I/O Pins of the CSI Data Communication is 32."]
[8.547947883605957, 6.831481456756592, "The Sampling Rate of the OVM Overhauser scalar magnetometer is 1 Hz."]
[8.147414207458496, 9.196966171264648, "The Transmitted Wavefront Distortion of the VPW42 Optical Window is \u03bb/8 at 633 nm."]
[11.633590698242188, -0.856301486492157, "The Mass of the OPSAT-1000 satellite bus Satellite Bus is 178 kg."]
[9.898764610290527, 4.558389663696289, "The Propulsion System of the Lunar Flashlight 6U CubeSat Satellite is Novel technology developed by VACCO Industries, Inc.."]
[10.547102928161621, 7.497097969055176, "The Material of the Delrin Spacers Component is Delrin."]
[5.985096454620361, 1.0207933187484741, "The Payload Status of the RAVAN CubeSat is Powered off."]
[11.6210355758667, -0.9324529767036438, "The Dry Mass of the Satellite Bus is 270 kg."]
[7.39204216003418, 9.042217254638672, "The Ground Resolution of the Scanner Assembly Instrument is 1 km."]
[10.92104434967041, 3.9641354084014893, "The Discovery of the TESS Satellite is Young Neptune-size world orbiting AU Microscopii."]
[2.2757046222686768, 4.4036335945129395, "The Power for Payload of the Spacecraft Satellite is 511 W."]
[8.15479850769043, 7.482854843139648, "The Calibration of the DDM Device is Relative."]
[9.834415435791016, 7.070295810699463, "The Material of the Bulkhead Structural Component is Two shells brazed together."]
[8.310102462768555, 2.4812498092651367, "The Occupation of the Max Valier Person is Science-fiction writer and an amateur astronomer."]
[7.147109508514404, 3.1386940479278564, "The Program Status of the Roshydrometsatellite Satellite is Unknown."]
[6.518404006958008, 9.080988883972168, "The Volume of the Electronics volume Spectrometer is 320 mm x 210 mm x 150 mm."]
[1.9785507917404175, 3.8449156284332275, "The Solar Panel Type of the AprizeSat Satellite is UTJ (Ultra Triple Junction) GaAs."]
[8.292129516601562, 7.888052463531494, "The Test Subject of the Biofilms Experiment is Laser-structured metal surfaces such as steel, copper and brass."]
[7.493587493896484, 0.7716158032417297, "The Eclipse Observation Date of the PROBA-2 Satellite is March 20, 2015."]
[4.889922142028809, 2.0170364379882812, "The Quantity of the Iridium NEXT satellites Satellite is 10."]
[9.197702407836914, -0.6587916016578674, "The Deployment Date of the BRO-2 and BRO-3 Nanosatellites is November 20, 2020."]
[12.121016502380371, 3.2683870792388916, "The Inclination of the SEOSAT-Ingenio Satellite is 98\u00ba."]
[7.0797858238220215, 0.42272961139678955, "The End of Operations of the SPOT-2 Satellite is July 2009."]
[9.234962463378906, 9.177976608276367, "The Photon Index Below the Break of the First Broken Powerlaw Model Component is 1.54."]
[9.677826881408691, 1.5862646102905273, "The Repeat Cycle of the PanMUX Instrument is 52 days."]
[8.89372730255127, 10.506767272949219, "The Pixel Size of the Acquisition and Tracking Camera (ATC) Camera is 20 \u00b5m x 20 \u00b5m."]
[6.922025680541992, 1.2168580293655396, "The Conference Date of the CHIPS Satellite is Aug. 13-16, 2001."]
[11.526930809020996, 4.1343817710876465, "The Diameter of the Kepler-442b Exoplanet is 33% bigger than Earth."]
[6.615401268005371, 3.2638649940490723, "The Activity of the COVE payload Payload is Complete."]
[11.242866516113281, 3.494121551513672, "The Brightness of the McNaught Comet is High."]
[10.980851173400879, 5.350330352783203, "The Magnetic Field Strength of the Sunspot Solar Phenomenon is 6,250 gauss."]
[11.226885795593262, -1.5111829042434692, "The Mass of the Spacecraft 3U CubeSat is 3.2 kg."]
[2.3991575241088867, 5.554579734802246, "The Channels of the DAC Digital Analog Converter is 4."]
[3.626817464828491, 6.190240859985352, "The Uplink Speed of the Communication links Communication System is 9.6 kbit/s."]
[11.524127006530762, 6.2409186363220215, "The Observations Management Center of the XMM-Newton Satellite is ESAC (European Space Astronomy Center), formerly known as VILSPA) at Villafranca, Spain."]
[9.50104808807373, 7.987496852874756, "The Neutron Converter of the LND Particle Telescope is Natural Gd foil."]
[7.780508041381836, 10.870891571044922, "The A/D Conversion of the Satellite Satellite is 8 bit."]
[8.33994197845459, 9.237789154052734, "The Imaging Modes of the Optical Sensor Assembly (OSA) Instrument is Simultaneous imaging in both panchromatic and multispectral modes."]
[7.541932582855225, 0.7762085795402527, "The Date of the SLAP Simulator is 2015."]
[6.431881904602051, 1.344862699508667, "The Tester of the ISIM Compartment is Matt Greenhouse."]
[6.153539657592773, 9.632566452026367, "The Mass of the Photometer Instrument Instrument is \u2264 0.9 kg."]
[4.696125507354736, 3.9715843200683594, "The Data Interface of the SAMPEX Satellite is SEDS (Small Explorer Data System)."]
[7.22563362121582, 8.952492713928223, "The Baseline Requirement of the Interferometric Mode Observation Mode is 17 days."]
[9.482301712036133, 5.70581579208374, "The Attitude Control of the XI-IV Picosatellite is Passive stabilization of a permanent magnet."]
[3.4885008335113525, 5.901971817016602, "The Average Session Time of the EAN Connectivity System is 1 hour."]
[7.24491548538208, 7.007392883300781, "The Activity Date of the GIADA Instrument is March 17-21, 2014."]
[9.481352806091309, 0.8918733596801758, "The Duration of the Station Keeping Satellite Maneuver is 15+ years."]
[8.664308547973633, 6.863295555114746, "The Measurement Range of the FGM Fluxgate Magnetometer is \u00b164,000 nT."]
[9.494989395141602, 1.0017297267913818, "The Mission Duration of the GOCE Satellite is More than four years."]
[10.58154010772705, 7.515707492828369, "The Face sheets material of the Bus structure Satellite Structure is Aluminum (AA2024-T3)."]
[6.911597728729248, 1.5728083848953247, "The Conference Date of the NASA Optical Communications and Sensor Demonstration Program Program is August 6-11, 2016."]
[7.856561183929443, 7.462903022766113, "The Oscillation Types of the GOLF Instrument is P and g mode oscillations."]
[5.610828876495361, 7.533822059631348, "The Tx Pulse Width of the KaRIn Instrument is 4.5 \u00b5s."]
[7.426214218139648, 7.385890483856201, "The Award Date of the Ozone Monitoring Instrument Instrument is 3 May 2019."]
[9.534955978393555, 7.450482368469238, "The Manufacturer of the EPIC Energetic Particle and Ion Composition Experiment is Not provided."]
[8.441572189331055, 5.581690788269043, "The Data Transmission of the GT Fine-Pointing Error Signal Provider is Five 250-Hz samples every 20 ms."]
[6.79164457321167, 9.045303344726562, "The Dimensions of the TEP Absorber 2 Absorber is 2.7 cm cylinder."]
[5.110591411590576, 7.049487113952637, "The Diameter (mm) of the Antenna Reflector is 600."]
[6.493947982788086, 3.1755940914154053, "The Payload Module Components of the Euclid Space Telescope is Telescope, Visual Imager, Near-Infrared Spectrometer and Photometer."]
[7.9840617179870605, 4.599995136260986, "The Image Resolution of the Earth Observation System Satellite System is 0.8 m."]
[7.9502434730529785, 5.214731216430664, "The Position Knowledge of the GPS Receiver Satellite Component is \u00b160 m."]
[6.729960918426514, 10.179167747497559, "The Primary Use of the Band 6 Spectral Band is Soil humidity, provision of ice/snow cover distinguishing capability."]
[8.623579025268555, 6.417335510253906, "The Length of the Gravity Gradient Boom Attitude Actuation Device is 1.4 m."]
[6.749501705169678, 8.497381210327148, "The Type of the MSU-GS Instrument is 10-channel radiometer."]
[8.531829833984375, 5.363678932189941, "The Pointing Accuracy of the Spacecraft Satellite is 0.24 arcsec relative pointing accuracy over 1 minute."]
[7.545134544372559, 10.056849479675293, "The Swath Width of the HySI Hyperspectral Imager is 20 km."]
[9.788458824157715, -0.8652541041374207, "The Attitude Control of the SOHLA-1 Microsatellite is Spin-stabilized."]
[8.731514930725098, 10.347434997558594, "The Electromagnetic Spectrum Range of the LISS-3 Imaging Sensor is Unknown."]
[5.151491165161133, 2.187868118286133, "The Fourth Set of the Iridium\u00ae NEXT Satellites Satellite Constellation is True."]
[10.58316421508789, -1.1087900400161743, "The Service System Mass of the Microsatellite Satellite is 18.2 kg."]
[7.734745025634766, 7.79280424118042, "The Composition of the Ozone Molecule is Three oxygen atoms."]
[2.0613033771514893, 4.477472305297852, "The Power Generation of the Spacecraft Satellite is 4 kW."]
[4.0554914474487305, 4.314021587371826, "The Basis of the OBC Software Software is RTOS (Real Time Operating System)."]
[6.205506801605225, 2.122166156768799, "The Receiver Channels of the Jason 2 Satellite is 8 channels."]
[2.2121734619140625, 1.7333247661590576, "The CCSDS ID of the GSAT-0103 Satellite is 3A7."]
[7.021865367889404, 2.47597599029541, "The URL of the ISEE-1 and ISEE-2 Satellites is http://www.ann-geophys.net/25/2633/2007/angeo-25-2633-2007.pdf."]
[11.397503852844238, 1.0044749975204468, "The Orbiter Orbit of the Tianwen-1 Probe is Polar elliptical orbit (265 km x 12,000 km)."]
[7.0659379959106445, 0.5190050005912781, "The Launch Date of the ICEYE-X1 Satellite is January, 2018."]
[10.492095947265625, 7.862613677978516, "The Grasp (500 eV) of the X-ray Imager Instrument is 27.5 cm 2 deg 2."]
[7.396221160888672, 1.4116665124893188, "The Launch Date of the MICROSCOPE Satellite is April 2016."]
[11.61618423461914, 2.5641117095947266, "The Closest Approach to Earth of the Bennu Asteroid is Every 6 years."]
[12.020852088928223, 3.308920383453369, "The Orbit Inclination of the SPOT-1, -2 and -3 Satellites is 98.7\u00b0."]
[7.647391319274902, 6.751901149749756, "The Measurement Range of the O3 Profile Satellite Instrument is 0-2 km(ppbv)."]
[7.842414379119873, 1.149219036102295, "The Image Capture Date of the Copernicus Sentinel-2 Satellite is January 28, 2022."]
[10.253745079040527, 2.918893337249756, "The Orbit Altitude of the HY-2C Satellite is 957 km."]
[7.779420375823975, 0.452640563249588, "The Launch Date of the Chandrayaan-1 Orbiter is 2008."]
[10.35216999053955, 1.27332603931427, "The LTAN of the DMC-3 Constellation Satellite Constellation is 10:30 hours."]
[4.604145050048828, 0.20963485538959503, "The Band Frequency of the OneWeb Satellite Constellation is 12 GHz."]
[10.27829360961914, 4.867883205413818, "The Firing Durations of the IEPS Ion Electric Propulsion System is Three 3-minute firings, eighteen 10-minute firings."]
[8.178071022033691, 8.811986923217773, "The Wavelength Coverage of the UVS Instrument Spectrometer Telescope is 215 nm (cha. 1), 236.5 nm (cha. 2)."]
[9.502459526062012, 5.908296585083008, "The Testing of the Magnetorquers Attitude Control Device is Prototypes of the design have been successfully tested with excellent performance."]
[9.065088272094727, 10.82208251953125, "The Multispectral Mode Swath Width of the LISS-4 Camera is 23.9 km."]
[9.555924415588379, 8.151254653930664, "The Scintillator Material of the Gamma-ray Counter Detector is CsI (Tl)."]
[8.106752395629883, 4.48748779296875, "The Swath of the Sentinel-2 Satellite is 290 km."]
[4.273251056671143, 6.9575605392456055, "The Downlink Signal Bandwidth of the HRIT HiRID Data Receiver is 1687.1."]
[10.159279823303223, 2.9505627155303955, "The Altitude of the Satellite LEO (Low Earth Orbit) is ~ 700 km."]
[7.695309162139893, 8.781134605407715, "The Absolute radiometric uncertainty of the Spectrometer Spectrometer is <0.8% (SWIR), <0.6% (MWIR), <0.45% (TIR)."]
[5.181661605834961, 6.097572326660156, "The Radiation Pattern of the Antenna High-Gain Antenna is Steerable with a gimbal capable of continuously pointing toward the ground station."]
[5.546383857727051, 6.553579330444336, "The Elevation Dimension of the Active Phased Array Antenna Antenna is 1.232 m."]
[6.548245906829834, 6.604889869689941, "The Manufacturer of the SGR-ReSI Instrument is SSTL."]
[10.532882690429688, 7.5222930908203125, "The Affiliation of the Hard X-Ray Burst Spectrometer Spectrometer is Solar Maximum Mission."]
[11.88829231262207, 3.277463436126709, "The Targeted Orbit of the Galileo FOC satellites Satellite is Circular, inclined at 56\u00ba with a semi major axis of 29,900 km."]
[6.891702175140381, 3.2376456260681152, "The End-of-Mission (EOM) Altitude of the PUNCH Mission Satellite is Passivated and naturally reenter within 22 years."]
[4.53851318359375, 3.673905849456787, "The Signal Collection of the AIS (Automated Identification System) Hardware is Successful from space over extensive areas of open water."]
[8.440417289733887, 1.636932373046875, "The Original Mission End Date of the Kepler Space Telescope Space Telescope is 2013."]
[6.435652732849121, 8.46622371673584, "The Conference Presentation Date of the Korean Spaceborne Microwave Radiometer on STSat-2 Radiometer is July 25-29, 2005."]
[9.826519012451172, -0.6351820230484009, "The Orbit Apogee of the BX-1 Microsatellite is 296 km."]
[6.775187969207764, 8.587807655334473, "The LOS Wind Error Requirement of the Mie Channel Instrument is 0.6 m/s."]
[9.45744514465332, 6.826075553894043, "The Number of Degrees of Freedom of the Grid Fins Control Surface is Two."]
[9.216875076293945, 4.265045166015625, "The Volume of the Instrument Satellite Component is 100 mm x 100 mm x 50 mm."]
[10.109590530395508, 4.353632926940918, "The Bipropellant System Total \u0394V Capability of the Clementine Spacecraft is About 1900 m/s."]
[6.1523027420043945, 3.2417454719543457, "The Coordinator of the ESEO Satellite is University of Bologna."]
[5.2138848304748535, 2.373098611831665, "The Mission Status of the ABEX CubeSat is Planned."]
[3.617938995361328, 2.2907071113586426, "The Size of the CSSWE Satellite is 3U."]
[8.21447467803955, 0.33260297775268555, "The AI Technology of the CIMON Astronaut Assistant is Watson from IBM Cloud."]
[8.227436065673828, 9.13492202758789, "The Pixel Sampling Interval of the Spectrometer Instrument is 28 \u00b5m."]
[9.505419731140137, 9.041205406188965, "The Solar Image Diameter of the Telescope Optical Instrument is 25 mm."]
[7.035776138305664, 4.468739986419678, "The Sensor Complement of the LAICE Satellite is In-situ measurements of wave perturbations in the ionosphere and remote sensing of the middle atmosphere."]
[4.93245792388916, -3.2062313556671143, "The | of the S. Krucker Author is S. Krucker."]
[6.612122058868408, 7.925394535064697, "The Pause Time of the Lasers Light Source is 1 to 6 ms."]
[3.5526440143585205, 5.396083354949951, "The Total Data Volume per Orbit of the Satellite Satellite is 77.7 Gbit."]
[7.344121932983398, 10.128653526306152, "The Applications of the HyperScout Imager is Monitoring of natural disasters such as floods delineation, forest fires hazard and desertification."]
[12.044095039367676, 2.2368578910827637, "The Stowage Process Duration of the OSIRIS-REx Spacecraft is Multiple days."]
[5.270472526550293, 6.400694847106934, "The Polarization of the Antenna for Navigation Antenna is RHCP (Right Hand Circular Polarization)."]
[8.328215599060059, 10.089756965637207, "The TDI (Time Delay Integration) of the Imager Imaging System is 6 selectable levels from 8 to 64 in Pan and MS."]
[8.479928016662598, 10.49058723449707, "The CCD Lines of the FPM (Focal Plane Module) Focal Plane is 3 linear CCD lines."]
[9.444877624511719, -0.26510798931121826, "The Objective of the SMDC-ONE Nanosatellite is Over-the-horizon communications of unattended ground station (UGS) data."]
[9.473474502563477, 0.5078033208847046, "The Design Life of the Odin Satellite is 2 years."]
[11.35339641571045, 1.5157374143600464, "The Distance Traveled of the Yutu 2 Lunar Rover is 565.9 meters."]
[3.2525107860565186, 4.858818054199219, "The Static RAM of the OBDH Data Handling and Processing is 256 kB."]
[7.4362688064575195, 7.424732208251953, "The Data Collection Period of the Ozone Monitoring Instrument (OMI) Instrument is 150-day period from 2015 through 2019."]
[9.134347915649414, 6.036301612854004, "The Operating Modes of the IPS Instrument Pointing System is Dependent on whether the gimbal resolver or gyro was used for feedback control of attitude."]
[8.25497817993164, 1.5668998956680298, "The Publication Date of the Rosetta Satellite is 26 January 2015."]
[4.044419765472412, 10.347757339477539, "The NEP of the Detector Instrument Component is < 3.7 nW at 17 Hz."]
[7.6993255615234375, 1.5885854959487915, "The Phase C/D Start Date of the SMOS Satellite is Mid-2004."]
[7.73275899887085, 8.30136775970459, "The Viewing Range of the TWINS Instrument is \u00b190\u00ba."]
[5.547641277313232, 1.6783777475357056, "The Publication Date of the National Scientific Foundation (NSF) CubeSat-based science missions for Geospace and Atmospheric Research Report is October 2013."]
[8.164925575256348, 5.620235919952393, "The Ground Noise Power of the RAX-1 Satellite is -110 dBm."]
[9.399323463439941, 7.644835472106934, "The Design of the Electron Sensor Sensor is Specialized."]
[11.220197677612305, 4.2181477546691895, "The Number of Stars with Multiple Planetary Candidates of the Kepler Satellite is 170."]
[10.326278686523438, 5.346513271331787, "The Volume of the Propellant Tanks Propellant is 1106 liter."]
[7.074299335479736, 3.222850799560547, "The Mission Status of the PACE Satellite is Construction and testing phase."]
[2.302825927734375, 4.425862789154053, "The Power of the Total with contingency Satellite is 18 W."]
[9.9730224609375, 2.8252103328704834, "The Operational Altitude of the OneWeb Satellite Constellation is Around 1,200 km."]
[6.509999752044678, 5.394130229949951, "The Radio Occultation Profiles of the Spire Satellite Data Provider is 3,000 profiles a day for six months."]
[6.256514072418213, 2.0182182788848877, "The Objectives of the DubaiSat-2 Satellite is Further develop the space program and associated sectors in the UAE, provide continuity and major improvements to the previous DubaiSat mission."]
[8.546674728393555, 3.348660469055176, "The Altitude of the Tandem-L satellites Satellite is 745 km."]
[9.03740119934082, 4.954082489013672, "The Airplane (AP) Mode of the ICESat Satellite is XG axis (plus or minus) is closely aligned with the velocity vector."]
[3.9706480503082275, 6.4425811767578125, "The Modulation of the Channel Communication System is QPSK, 8PSK, 16APSK, 32APSK."]
[5.993224620819092, 6.399994850158691, "The Cross-polarization Ratio of the Instrument SAR is \u2264-25 dB."]
[9.691007614135742, 8.06501293182373, "The Type of the GMOD Gamma Ray Detector is Compact, silicon-based."]
[8.325922966003418, 1.053133249282837, "The Operation Start Date of the RAIDS Instrument is October 23, 2009."]
[4.657738208770752, 9.042308807373047, "The Launch Date of the InSight Satellite is May 2018."]
[11.789599418640137, -1.0854076147079468, "The Client Mass of the ELSA-d Satellite Mission is ~20 kg."]
[1.6434358358383179, 4.551108360290527, "The Processor of the EPS Electrical Power Subsystem is Dedicated."]
[11.267170906066895, 3.7747249603271484, "The Comet Discoveries of the SOHO Satellite is 3000."]
[2.335301637649536, 5.1215500831604, "The Power Consumption of the PSU Power Supply Unit is 75 W."]
[7.54793643951416, -0.4942232668399811, "The Booster's Failure Date of the Falcon 9 Rocket is Feb. 15."]
[8.541757583618164, 10.270750999450684, "The Manufacturer of the Focal Plane Detector is e2v for Astrium."]
[6.284842491149902, 8.569413185119629, "The Spectral range of the Microwave System Microwave System is 6.9, 10.6, 18.7, 23.8, 31, 36.5, 42, 48, 52.3-57.0, 89, 183.31 (GHz)."]
[7.70226526260376, 9.081886291503906, "The Resolving Power of the Spectrometers Spectrometers is 15 x 10^3 for the broadband measurements."]
[7.204647064208984, 2.7176225185394287, "The URL of the STEREO Satellite is http://www.nasa.gov/mission_pages/stereo/news/farside-060111.html."]
[4.840700626373291, 9.179781913757324, "The Potential Mission End Date of the InSight Seismic Experiment for Interior Structure (SEIS) is Within a year from June 22, 2021."]
[7.538992881774902, 2.1859090328216553, "The Utilization of the ICI-8 Radiometer is Cloud ice water path and cirrus."]
[3.5806314945220947, 4.52907133102417, "The Output of the CU Control Unit is Impulses to all channels."]
[7.647779941558838, 8.779619216918945, "The Spectral Range of the Nadir Sensor Wide-Field Telescope Sensor is 300-380 nm."]
[4.537074565887451, 7.217505931854248, "The Size of the LALT-TR Transmitter is 360 mm x 450 mm x 408 mm."]
[2.210430860519409, 1.733458399772644, "The CCSDS ID of the GSAT-0210 Satellite is 26A."]
[8.59355640411377, 8.864185333251953, "The Filter Type of the NUV channel Spectrometer is Fused Silica Window."]
[6.952106952667236, 4.770883083343506, "The Product of the Sustainability Tech Company is Satellite-connected sensors that monitor wetland hydrology."]
[7.578198432922363, 2.2841672897338867, "The Technology Objectives of the ExoMars Mission is 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 braki."]
[9.843865394592285, 5.528876304626465, "The Energy Storage Margin (120 minute window) of the RASP Maneuver Planning System is 71.1%."]
[7.653459548950195, 1.2526907920837402, "The Announcement Date of the Copernicus Program is December 11, 2012."]
[3.88136625289917, 4.410312652587891, "The Type of the OBC On-Board Computer is RCM3400 of Z-World based on the microcontroller Rabbit 3000."]
[6.544917106628418, 4.170690059661865, "The Information Delivery of the Satellite Earth Observation Satellite is Actionable, affordable and timely."]
[8.61849308013916, 5.625759124755859, "The Acquisition Range of the GT Fine-Pointing Error Signal Provider is Slightly >15 arcmin."]
[9.259632110595703, 4.756711959838867, "The Gravitational Stability of the Spacecraft Satellite is < 5 x 10-11 g."]
[4.476637363433838, 6.263514518737793, "The Design Purpose of the SKOUT Ka-band Communications System is To connect government and commercial relay satellite constellations as well as direct-to-ground communications networks."]
[7.270556449890137, 5.194598197937012, "The Spatial Coverage of the SMOS Satellite is Lower at the edges of the swath."]
[6.925259113311768, 4.036026954650879, "The Data Usage of the Resurs-DK1 Earth Observation Satellite is 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."]
[8.412643432617188, 9.960840225219727, "The Quality Requirement of the Beam Splitter and Field Widening Prisms Optical Components is Good quality over the area sampled by one spatial resolution element on the detector."]
[6.525539398193359, 6.831900119781494, "The Launch Date of the AltiKa Altimeter is 2011/12."]
[5.601117134094238, 2.327103853225708, "The Objective of the SpooQySat CubeSat is Demonstrate in-orbit a space-compatible quantum light source."]
[5.342085361480713, 1.5483137369155884, "The Deployment Mission of the CubeSats Satellite is 14th."]
[3.91161847114563, 4.314750671386719, "The Manufacturer of the CDHS Command and Data Handling Subsystem is Pumpkin Inc.."]
[11.747270584106445, 4.628739356994629, "The Number of Stellar Streams of the Milky Way Galaxy is At least 70."]
[5.9167866706848145, 1.9687860012054443, "The Provider of the NSSL Phase 2 Launch Program is ULA and SpaceX."]
[6.310335636138916, 2.8277671337127686, "The User of the STK Scheduler Software is NASA."]
[4.787035942077637, 0.88504958152771, "The Cost of the Prometheus Satellite Satellite is Less than $100,000."]
[5.033092021942139, 6.011361598968506, "The Dataset Rate of the GEOSAT Satellite is 10 Hz."]
[8.870965957641602, 5.201928615570068, "The Attitude Dynamics Analysis Presentation of the Aalto-1 Satellite is Oct. 1-5, 2012."]
[7.816458702087402, 4.244971752166748, "The Resolution of the ZY-3 Satellite is High."]
[8.842878341674805, 9.16240119934082, "The On-Ground Separation of the Slits Optical Instrument is 15.9 km."]
[9.37205982208252, 5.880666732788086, "The Accuracy of the SA Drive Mechanism Attitude Control Device is > 1%."]
[11.519661903381348, 3.891726493835449, "The Formation Start of the Azores archipelago Geographic Location is About 10 million years ago."]
[6.756195068359375, 3.2927796840667725, "The Mission Status of the Sich-2 Satellite is Mission complete."]
[6.092067241668701, 9.645755767822266, "The Mass of the Instrument Spectrometer is < 10 kg."]
[6.243971347808838, 2.0705840587615967, "The Utility Assess Date of the TacSat-4 Satellite is Trident Warrior 2012."]
[2.2916600704193115, 5.704043388366699, "The Function of the SSPA-C Solid State Power Amplifier is Rebroadcast data processed by the EUMETSAT control center."]
[7.974435329437256, 5.798382759094238, "The Jitter of the SPARCS Satellite is 1\u03c3 ~6\" over 10 minutes."]
[8.460050582885742, 7.971254348754883, "The Channels Quantity of the REM Radiation Environment Monitor is 16."]
[7.177978992462158, 2.3452625274658203, "The URL of the Evaluation Process is https://earthdata.nasa.gov/esds/csdap/csdap-pilot-evaluation."]
[9.259368896484375, 8.99626350402832, "The F-number of the Telescope Optical Instrument is 2.2."]
[6.0816545486450195, 1.7428234815597534, "The Full Operational Service Date of the SAR-Lupe Constellation Satellite Constellation is 2008."]
[7.028413772583008, 6.581428050994873, "The Data Collection Period of the TROPOMI Tropospheric Monitoring Instrument is January 1-20, 2020 and February 10-25, 2020."]
[8.636253356933594, 8.909078598022461, "The Ellipse Axis A of the Short Wavelength Band Spectrometer is 180 mm."]
[7.58928918838501, 7.83547830581665, "The Predecessor of the TOMS Total Ozone Mapping Spectrometer is BUV."]
[7.402686595916748, 2.482464075088501, "The URL of the ExoplanetSat Satellite is https://dspace.mit.edu/handle/1721.1/61644."]
[1.7676469087600708, 4.833399772644043, "The Payload Power of the EPS Electric Power Subsystem is Up to 130 W average."]
[8.98461627960205, 4.549332618713379, "The Primary Structure Components of the S/C Satellite is Central cylinder, main platform, propulsion platform, four shear panels."]
[7.713891983032227, 13.595558166503906, "The No. of Bins of the SPIM2 Spectrometer is 68, 136, or 272."]
[6.219095230102539, 0.37730979919433594, "The End of Life Date of the PW-Sat CubeSat is October 28, 2014."]
[8.210365295410156, 4.030454158782959, "The Light Pollution of the Satellites Satellite is Not specified."]
[7.597362995147705, 7.4904680252075195, "The Objective of the MOMA Instrument is Analyze volatile and refractory organic compounds in martian surface and subsurface sediments."]
[6.1570940017700195, 2.9896833896636963, "The Managing Contractor of the YES2 Satellite is Delta-Utec SRC (Space Research & Consultancy)."]
[5.048099517822266, 2.667081117630005, "The Affiliation of the UiTMSAT-1 1U CubeSat is Malaysia."]
[11.521477699279785, 4.488070011138916, "The Temperature of the Red Dwarfs Star Type is Roughly a third of our Sun\u2019s temperature."]
[7.150859832763672, 9.373819351196289, "The Resolution of the Stripmap mode (SM) Operational Mode is 5 m x 5 m."]
[7.004982948303223, 4.265139102935791, "The Measurement Domain of the HJ-1 Satellite is Atmosphere, Ocean, Land, Snow & Ice."]
[7.6052961349487305, 4.007342338562012, "The Measurement Importance of the CryoSat-2 Satellite is Understanding the links between ice and climate."]
[7.528360843658447, 2.8191075325012207, "The Unknown of the Asteroid Deflection Mission Mission is Unknown."]
[10.414775848388672, 2.5228395462036133, "The Orbit Perigee of the Beijing-3B Satellite is 601 km."]
[9.674803733825684, 1.6055777072906494, "The Revisit Cycle of the Satellite Imaging Satellite is 1-3 days (for observations at 40\u00ba latitude or higher)."]
[12.026455879211426, 4.422397613525391, "The Observatory Collaboration Date of the Crab Nebula Nebula is May 10, 2017."]
[6.01678991317749, -0.07778361439704895, "The Stakeholder Involvement Timeline of the Galileo Second Generation Satellite System is In the next eight months."]
[8.018564224243164, 8.257547378540039, "The Radiometric Accuracy of the Optical Scanning Design Imaging Spectrometer is <2% with reference to the sun."]
[5.807432651519775, 5.483004570007324, "The Signal Processing of the TriG receiver GNSS Receiver is Multiple reconfigurable FPGAs."]
[5.822987079620361, 2.9341509342193604, "The Manufacturer of the ZY-3 Satellite is CAST/BISSE (China's Academy of Space Technology/Beijing Institute of Spacecraft System Engineering)."]
[6.332223415374756, 11.88547420501709, "The Proof-mass Positioning Error of the Three-axis diagonal gradiometer Gradiometer is 6 x 10 -8  m Hz -1/2."]
[11.42489242553711, 1.0401208400726318, "The Lander/Rover Landing Site of the Tianwen-1 Probe is Utopia Planitia."]
[9.725680351257324, 4.2713117599487305, "The Shape of the Drag Sail Modules Satellite Component is Wedge-shaped."]
[3.581214427947998, 4.972259521484375, "The CPU Cores of the Mission Operation System Data Processing System is More than 3000."]
[12.160636901855469, 5.379615306854248, "The Lyman-alpha Forest Percentage of the Universe Cosmology is 28 percent."]
[5.036323547363281, 2.6610405445098877, "The Operator of the Hellas Sat 3 Satellite is Hellas Sat."]
[8.846137046813965, 10.788777351379395, "The Coverage of the CCD Camera Imaging System is 6250 km x 300 km per scan line."]
[11.849214553833008, 1.0234400033950806, "The Landing Trajectory Reconstruction of the Chang'e-4 Lunar Spacecraft is Completed."]
[7.515844345092773, 7.198156356811523, "The Calibration Function of the GMI Radiometer Radiometer is Constellation precipitation transfer standard."]
[9.267451286315918, 6.408263206481934, "The FOV (Field of View) of the Star Tracker Attitude Determination Device is 7:5\u00ba (half axis)."]
[7.059722423553467, 8.835945129394531, "The Dynamic Range (Visible Channel) of the VIRR Instrument is 65 - 10,000 fL (scene brightness)."]
[7.025290012359619, 6.684999942779541, "The Spectral Range of the TROPOMI Instrument is Short Wave Infrared around 2.3 \u00b5m."]
[8.35686206817627, 3.244535446166992, "The Orbit Concept of the TanDEM-X Satellite is Double helix formation."]
[7.4607086181640625, 1.2089686393737793, "The BCP Distribution Interval of the INTEGRAL Satellite is Every 8 s."]
[6.145528793334961, 5.273065567016602, "The Location of the GPS Network GNET Ground-based Measurement System is Greenland."]
[9.2008056640625, 6.125516414642334, "The Maximum Torque Output of the CMG Control Moment Gyroscope is 0.8 mNm."]
[8.289371490478516, 3.7784206867218018, "The Earth Coverage of the Planet Satellite Imaging Company is At least 85% of the Earth\u2019s landmass every 15 days."]
[10.244523048400879, 2.9342386722564697, "The Orbital Altitude of the LDEF Satellite is 335 km."]
[6.209973335266113, 4.506341934204102, "The Data and Satellite Solutions of the SAR Satellites Satellite is Government and commercial use."]
[9.348388671875, 11.601371765136719, "The Pixel size of the Channel 3 Sensor is 32 km x 32 km."]
[9.215084075927734, 10.266647338867188, "The Mounting Range of the WFI Camera is -24\u00ba to +24\u00ba."]
[5.281607151031494, 6.6045942306518555, "The Accuracy of the Onboard Antenna Antenna is 5\u00ba."]
[4.004282474517822, 7.036874771118164, "The Form Factor Weight of the Compact Laser Comms Terminals (CLCT) Communication Device is Less than 2 kg."]
[7.666297435760498, 8.752450942993164, "The Transmission x QE of the Instrument Spectrometer is 3%."]
[10.209582328796387, 4.936812400817871, "The Operating Mode of the Solar Electric Propulsion System (SEPS) Propulsion System is Twin thruster mode."]
[7.245638847351074, 0.7421468496322632, "The Operation Start Date of the PROBA-2 Satellite is July 1, 2013."]
[8.419219970703125, 4.018819808959961, "The Primary Science Missions of the MIRIS Satellite is (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 origi."]
[4.845636367797852, -3.3753600120544434, "The Member of the Jennifer Comstock Individual is True."]
[7.560793876647949, 3.559404134750366, "The Data Distribution of the Landsat-7 Satellite is ETM+ data will be distributed from the archive in an essentially raw form."]
[8.80764389038086, 1.4055330753326416, "The Current Status of the Van Allen Probes Satellite is Operating in a bridge phase."]
[6.00514554977417, 9.602994918823242, "The Instrument Package Mass of the LCROSS Satellite is 12.4 kg."]
[9.162920951843262, 6.394545078277588, "The Purpose of the OB Optical Bench is Transference of the attitude from the star trackers to the magnetometer field components."]
[9.970458030700684, -0.6608169674873352, "The Altitude Range of the NEOSSat Microsatellite is 15,000 and 40,000 km."]
[4.941671848297119, 5.127985954284668, "The Network of the KSAT Ground Station is S-band uplink and X-band downlink."]
[4.83034086227417, 9.189510345458984, "The Solar Panel Dust Accumulation Date of the InSight Seismic Experiment for Interior Structure (SEIS) is June 22, 2021."]
[9.80339241027832, 2.797563314437866, "The Momentum Factor of the Impact Ejecta Phenomenon is 3 to 5."]
[7.664544582366943, 0.5107840299606323, "The Launch Date of the JPSS Satellite Program is March 2017."]
[6.407277584075928, 5.795168876647949, "The Grid Resolution of the L2SMP Soil Moisture Product is 36 km EASE-2."]
[6.704538345336914, 4.296357154846191, "The | of the Spanish Earth Observation Program Satellite Program is The Spanish Earth Observation Program."]
[9.78385066986084, 1.5553629398345947, "The Repeat Cycle of the MTG-S Spacecraft Satellite is 10 minutes."]
[1.919464111328125, 4.127023696899414, "The Unknown of the Solar Power Technology Technology is Unknown."]
[8.786832809448242, 10.163689613342285, "The Catastrophic Burnout of the CMOS Sensors Sensor is Did not occur."]
[9.378029823303223, 9.045197486877441, "The Instrument Size of the Telescope Optical Instrument is 430 mm x 190 mm x 135 mm."]
[9.3251953125, 0.6805402040481567, "The Design Lifetime of the SPOT satellite constellation Satellite Constellation is 3 years."]
[4.641508102416992, 9.047014236450195, "The Conference Date of the InSight Mars Mission Mission is May 28-June 1, 2018."]
[11.588594436645508, 1.2605000734329224, "The Quantity of the Landing Legs Landing System is 4."]
[7.099175453186035, 9.675006866455078, "The Band 3 of the RBV Instrument Spectral Band is 0.70 - 0.83 \u00b5m."]
[7.564438819885254, 1.1934685707092285, "The Evaluation Date of the Evaluation Process is 8 December 2021."]
[8.231195449829102, 5.446240425109863, "The Navigation Algorithm Optimization of the Lander Spacecraft is Required."]
[5.8400983810424805, 8.130401611328125, "The Frequency (GHz) of the ICI-6 Radiometer is 325.15\u00b13.5."]
[8.721126556396484, 8.845508575439453, "The Function of the Diffraction Grating Optical Component is Disperses the light."]
[10.133218765258789, 5.147440433502197, "The Firing Tests of the AQT-D Propulsion System is Standalone and Integrated."]
[6.7111334800720215, 7.259704113006592, "The Control of the Scanning LIDAR LIDAR is Predefined timeline."]
[6.567871570587158, 8.315375328063965, "The Purpose of the Microwave Imager Instrument Instrument is Remote sensing."]
[10.067673683166504, 6.783493518829346, "The Energy of the TWINS Satellite is 10 keV."]
[7.822686672210693, 8.881111145019531, "The Radiometric Accuracy of the Spectral Band B Spectrometer is 3."]
[1.7193710803985596, 4.796866416931152, "The Power of the EPS Electric Power Subsystem is 4.3 kW @ EOL (End of Life)."]
[6.534934997558594, 5.091011047363281, "The Instrument of the Copernicus Sentinel-6 Satellite is Radar Altimeter."]
[9.511373519897461, 6.035180568695068, "The Charging and SciD Mode Operation of the ADCS Attitude Determination and Control System is Solar panels towards the sun with constrain +Y of the spacecraft pointing as close as possible towards the nadir direction."]
[9.067877769470215, 7.639400959014893, "The Design of the LINAS Ionization Gauge is IGS (Ionization Gauge Streak)."]
[9.370129585266113, 8.151901245117188, "The Purpose of the RAMIS Payload is Radiation Measurements In Space."]
[6.024373531341553, 4.756953239440918, "The Test Location of the OSIRIS Device is Stuttgart and Oberpfaffenhofen."]
[9.521699905395508, 0.4768015742301941, "The Goal of the Satellite Design Life is 5 years."]
[4.6591057777404785, 3.851839780807495, "The Mission Preprint of the SAMPEX Satellite is 93-128."]
[9.358705520629883, 9.136331558227539, "The Focal Ratio of the Telescope Optical Instrument is F/5."]
[4.604705810546875, 5.6290154457092285, "The RF Communications System of the JWST Spacecraft is CCTS (Common Command and Telemetry System)."]
[3.7016761302948, 6.074431896209717, "The Bandwidth of the Bartolomeo Payload Communication System is 0.1 Mbit/s."]
[7.268518924713135, 0.6748114228248596, "The Launch Date of the ALOS-3 Satellite is February 16, 2023."]
[7.020935535430908, 6.229849338531494, "The Uncertainty of the Sea Ice Concentration (SIC) Measurement is <5%."]
[5.354106903076172, 1.3190292119979858, "The Number of Fires of the Fregat Upper Stage is Two."]
[3.502793550491333, 5.311229705810547, "The Telemetry Data Storage of the RF Communications Communication System is Onboard memory."]
[8.188794136047363, 4.5739426612854, "The Ground Resolution of the GeoCARB Satellite is 5 to 10 km."]
[9.24843978881836, 1.283158540725708, "The Duration of the CALET Telescope is Two to five years."]
[6.29508638381958, 1.1352653503417969, "The Launch Year of the COSMO-SkyMed Satellite is 2007."]
[4.784383296966553, 1.8051873445510864, "The Planned Satellite Constellation Size of the Capella Space Company is 36."]
[6.890157699584961, 1.4702513217926025, "The Date of the Symposium on Small Satellite Systems and Services (4S) Conference is May 31-June 4, 2010."]
[9.306281089782715, 5.948929309844971, "The Application of the Attitude Determination System System is Small asteroid lander."]
[10.89395809173584, 7.131725311279297, "The X-ray Spectral Band of the AstroSat Astronomy Satellite is 0.3 \u2013 100 keV."]
[6.590644836425781, 5.154879093170166, "The Interferometric Configuration of the TerraSAR-X Satellite is Single-pass."]
[9.037240982055664, 10.613300323486328, "The Design of the DCAM3 Camera is Similar to IKAROS DCAM1,2."]
[9.122806549072266, 2.533818244934082, "The Arrival Date of the DART Spacecraft is October 2022."]
[5.315169334411621, 2.921457052230835, "The Separation of the T9 Payload Fairing\u2019s Base Ring Satellite Component is Verified."]
[4.9055495262146, -3.249054431915283, "The | of the Fred A. Best Individual is Fred A. Best, Douglas P. Adler, Claire Pettersen, Henry E. Revercomb, P. Jonathan Gero, Joseph K. Taylor, Robert O. Knuteson, John H. Perepezko."]
[3.8776063919067383, 2.2904140949249268, "The Size of the ALICE CubeSat is 3U."]
[7.6020402908325195, 7.42423152923584, "The Detection Method of the Radio Emissions Phenomenon is Juno Waves instrument."]
[7.106517314910889, 8.5986909866333, "The Ground Resolution of the SUCHI Instrument is ~220 m."]
[7.842930316925049, 8.553778648376465, "The Spectral Range of the SOLSPEC-ATLAS Spectrometer is 210-2400 nm."]
[4.271660804748535, 6.485058784484863, "The Components of the ADE Altimeter Duplexer Equipment is Single ferrite switch on the transmit path and four ferrite switches on the receive path."]
[6.990602970123291, 5.019254684448242, "The Usage of the SOFIE and MLS Satellite Data is Categorized the inter-annual variability of winter and springtime upper stratospheric methane (CH4)."]
[4.241378307342529, 7.204597473144531, "The Weight of the TxU Transmitter Unit is 8 kg."]
[11.374410629272461, 1.0159903764724731, "The Communication Support of the Tianwen 1 Probe is Argentina's deep space tracking antenna, ESA's global network of ground stations."]
[4.657539367675781, 5.537642478942871, "The Link Reversion of the LLITED satellites Satellite is Passive receive mode."]
[11.7598237991333, 4.574609756469727, "The Distance from Earth of the Kepler supernova remnant Supernova remnant is About 20,000 light years."]
[7.744009494781494, 6.322213649749756, "The Publication Date of the Intercalibration of Satellite Instruments Process is March 2013."]
[8.895702362060547, 2.0646517276763916, "The Exploration Date of the Ultima Thule Kuiper Belt Object is January 1, 2019."]
[6.518950939178467, 4.0618791580200195, "The Components of the Second-Generation Platform Earth Observation (EO) remote sensing platform is High-resolution dual-mode optical camera, Video optical camera, Dual-band Synthetic Aperture Radar (SAR) instrument."]
[13.17059326171875, 4.022055625915527, "The Data Publication Date of the Gaia Star-Observer is February 13, 2020."]
[7.0557661056518555, 2.069045305252075, "The Validation Scope of the KONNECT satellite Satellite is Complete end-to-end system of the new Spacebus Neo product line, including the fully electric orbit-raising phase."]
[9.4436616897583, 0.5331794023513794, "The Design Life of the SPOT-2 Satellite is Three years."]
[4.169540882110596, 5.922419548034668, "The Availability of the Strandatoga protocol Ground-based negative acknowledgement protocol is Available."]
[4.720293998718262, 4.345735549926758, "The Technology of the SpaceLink Satellite Network is Optical communications."]
[8.550565719604492, 5.713403224945068, "The Density of the Proton Component Measurement Range of the DSCOVR Satellite is 1 \u2013100 particles/cm3."]
[10.235422134399414, 2.969092607498169, "The Altitude of the ANUSat Satellite is 550 km."]
[8.727301597595215, 10.690348625183105, "The Dynamic Range of the CCD Camera Imaging System is 0-100% albedo."]
[4.8450164794921875, 5.430155277252197, "The Netherlands-China Low-Frequency Explorer (NCLE) of the Relay Satellite Satellite is International Joint Collaboration Payload."]
[6.741641521453857, 4.8026347160339355, "The Instruments of the MTG-S Satellite is Infrared Sounder (IRS) and the UV-visible- near infrared imaging spectrometer (UVN)."]
[6.677614212036133, 0.76345294713974, "The FCI Instrument Testing Date of the MTG Satellite is 4 July 2018."]
[6.5305681228637695, 3.741575241088867, "The Security System of the SEOSat/Ingenio Satellite is SEOSat/Ingenio Security System."]
[10.547624588012695, 1.5846498012542725, "The Time in Lunar Orbit of the Service Module Module is 6-7 days."]
[8.1126070022583, 1.2382856607437134, "The Operation Period of the MAG Magnetic Field Instrument is January 2012 to May 2014."]
[12.981011390686035, 4.855197429656982, "The Launch Date of the IBEX Spacecraft is October 19, 2008."]
[9.522160530090332, 9.042659759521484, "The Stray Light/Sun Disk Light Rejection of the Telescope Optical Instrument is 5 x 10^8."]
[10.701559066772461, 10.272895812988281, "The Power of the PHA Detector is 11 mW per active PHA."]
[7.778212547302246, 9.121192932128906, "The Infrared Wavelength Detection Range of the Mapping Channel Spectrometer is 0.95 \u00b5m to 5 \u00b5m."]
[3.898632764816284, 2.3251287937164307, "The Size of the OPS-SAT CubeSat is 30-cm."]
[9.183540344238281, 9.271737098693848, "The Field of View of the Focal Plane Optical Instrument is 0.4\u00ba."]
[3.0318455696105957, 6.0191731452941895, "The Target Timeliness of the EARS Data Services Data Service is 15 to 30 minutes from instrument sensing."]
[8.02656078338623, -0.25431180000305176, "The Docking Time of the Soyuz MS-17 Spacecraft is Three hours later."]
[5.382428169250488, 3.8487045764923096, "The Components of the TEPCE Satellite is High voltage supplies, magnetorquers, GPS, camera, plasma sensors."]
[11.78996467590332, -1.1446208953857422, "The Launch Mass of the NigeriaSat-2 Satellite is 286 kg."]
[9.035664558410645, 10.760466575622559, "The Swath Width of the EOS Camera is 12 km."]
[1.747369408607483, 4.070547580718994, "The Redundancy of the Solar Array Power Generation Device is 4 strings loss allowed."]
[9.990043640136719, 3.0985312461853027, "The Orbit Altitude of the Argos-4 Satellite Instrument is 850 km."]
[5.379002094268799, 4.56389045715332, "The Technology Demonstration Boards of the AEEF Assembly is SIOS (Sistema de Interconexiones \u00d3pticas para Sat\u00e9lites) optical link demonstration board and one GaN (Gallium Nitride) board."]
[6.935683727264404, 0.5560983419418335, "The Debut Flight Date of the Dellingr Satellite is 2 Aug.2017."]
[8.686053276062012, 10.62761116027832, "The Operation of the CCD Readout Image Sensor is Vertical shift of the image rows."]
[4.34218168258667, 7.135889053344727, "The Weight of the Wireless Compose-2 Wireless Network Infrastructure is One kilogram."]
[7.157135486602783, 1.548588514328003, "The Phase B Completion of the Spacebus Neo Satellite is 2015."]
[7.095240592956543, 0.05829044431447983, "The End of Life of the S3A Satellite is 2026."]
[9.345608711242676, 10.220877647399902, "The Tilt of the PAN-A Camera is -5\u00ba."]
[9.5781888961792, 1.2903201580047607, "The Revisit Time of the Platform Satellite is Within 3 days."]
[2.2441139221191406, 4.77644157409668, "The Heater Power of the SVM Service Module is 80 W."]
[8.979625701904297, 10.322501182556152, "The Star Magnitude Range of the Normal Cameras Camera is Fainter than mV = 8."]
[6.565243721008301, 0.8164798021316528, "The Launch Date of the DubaiSat-2 Satellite is November 2013."]
[10.153759002685547, 2.933680295944214, "The Spatial Scale of the GOSAT Satellite is 100-1000 km."]
[7.935108661651611, 8.171850204467773, "The Exposure Time of the Satellite Imaging Instrument is 100 ks."]
[6.674098014831543, 0.6650894284248352, "The Launch Date of the SEOSAT/Ingenio Satellite is First half of 2020."]
[8.761428833007812, 3.446331739425659, "The Support Goal of the MinXSS mission Satellite is To study the \"dynamics and energetics of the upper atmosphere, with particular emphasis on the hard to observe region between 80 and 150 km\"."]
[6.6253838539123535, 2.648653984069824, "The Expected Discoveries of the Lucy Space Mission is Open new insights into the origins of our Earth and ourselves."]
[9.678504943847656, 3.949917793273926, "The Drag Sail Modules of the CanX-7 Satellite is 4."]
[9.674631118774414, 7.369546890258789, "The Compressor Units of the Stirling Cycle Cooler Cooler is Pair of linear motor reciprocating compressor units."]
[7.098974227905273, 6.721360683441162, "The Type of the TROPOMI Instrument is Passive grating pushbroom imaging spectrometer."]
[11.292703628540039, -1.4700030088424683, "The Mass of the Inmarsat S \u2013 Europasat / Hellas-Sat 3 Satellite is About 5.8 tons."]
[6.453075885772705, 1.654523491859436, "The Project Status Meeting Date of the Jason-1 Satellite is Oct. 19-21, 2011."]
[6.544637680053711, 0.40976351499557495, "The Operational Concept Presentation Date of the SMART-1 Satellite is Sept. 29, - Oct. 3, 2003."]
[9.390318870544434, 0.9171956181526184, "The Mission Duration of the CASS Satellite is Originally planned as a two-year mission."]
[12.979423522949219, 4.863729476928711, "The Operation Status of the IBEX Spacecraft is Nominal in 2012."]
[10.805062294006348, 3.4674222469329834, "The Closest Approach to Sun's Surface of the Solar Orbiter Satellite is Within 48 million km."]
[6.11685037612915, 3.0614569187164307, "The Cooperation Agreement of the OICETS Satellite is JAXA (formerly NASDA) and the ESA signed an agreement regarding cooperation in optical communications in space."]
[8.626399040222168, 0.15840429067611694, "The Number of Research Investigations of the International Space Station Space Station is More than 2,500."]
[1.7506332397460938, 4.32884407043457, "The Solar Panel Size of the EPS Electric Power Subsystem is 2.4 m2."]
[7.851069927215576, 3.8460843563079834, "The Orbit Adjustment of the VNREDSat-1 Satellite is Second."]
[7.193365097045898, 0.43829160928726196, "The Launch Date of the SOAR Satellite is 3 June 2021."]
[4.967864036560059, 1.9574153423309326, "The Number of CubeSat Missions of the ELaNa-4 Satellite Mission is 8."]
[6.950199127197266, 4.58042573928833, "The Observation Capability of the GEO Satellite Satellite is Constant monitoring of quickly developing weather phenomena or diurnal variations in weather events."]
[8.501201629638672, 6.340709686279297, "The Objectives of the EFI Electric Fields Instrument is Study of the ambient vector electric field structure of the high-latitude magnetosphere, the cusp, and the plasma mantle."]
[9.2271089553833, 9.301920890808105, "The Optics System of the Collecting Optics Lens Assembly is f/5."]
[5.315695762634277, 2.3104701042175293, "The Constellation Configuration of the UrtheCast Company is 16-satellite constellation of eight optical and eight SAR (Synthetic Aperture Radar) satellites in LEO (Low Earth Orbit)."]
[4.955111980438232, 1.5709933042526245, "The Ground Segment of the FormoSat-7 / COSMIC-2 Satellite Constellation is Unknown."]
[8.073128700256348, 8.30599308013916, "The Quantity of the OMPS Spectrometer is 3."]
[9.688857078552246, 6.032774448394775, "The Control Law of the ADCS Attitude Determination and Control System is B-dot control law."]
[6.581623077392578, 0.5847395658493042, "The Launch Date of the TechEdSat Satellite is 21 July 2012."]
[7.459208965301514, 0.5475217700004578, "The Launch Date of the ISILaunch19 Campaign is June 23, 2017."]
[5.0603742599487305, 3.7488484382629395, "The Development Approach of the Service Module Satellite Module is Parallel development, assembly, integration and test of the service and payload modules."]
[6.430740833282471, 5.026004791259766, "The Radio Occultation Payload of the Sentinel-6 Satellite is GPS and GLONASS satellites."]
[7.322136878967285, 7.269651412963867, "The Launch Date of the COWVR Radiometer is 21 December 2021."]
[7.777188301086426, -0.4453432261943817, "The Grappling Astronaut of the SpaceX CRS-17 Mission is David Saint-Jacques."]
[8.05125617980957, 1.2652548551559448, "The Date of the The Changing Seas of the Florida Keys Image is 31 May 2022."]
[6.965839385986328, -0.04945028945803642, "The End of Life Date of the GovSat-1 Communication Satellite is 2033."]
[4.5203728675842285, 2.075883626937866, "The Total Impulse of the SkySat-4 Satellite is 57 Ns."]
[7.296876907348633, 2.3038601875305176, "The Launch Confirmation Date of the CARBONITE-2 Satellite is 12 Jan. 2018."]
[9.944361686706543, 1.4801634550094604, "The Period of the SAOCOM-1A and -1B Satellites is 97.1 minutes."]
[9.114442825317383, 5.569240093231201, "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."]
[2.135136365890503, 3.953152656555176, "The Power Generation of the SPOT-1 Satellite is Solar array."]
[4.516880035400391, 6.374691963195801, "The Type of the Ka-band payload Communication System is Circularly polarized."]
[9.07078742980957, 10.581564903259277, "The Image Resolution of the NAVCAM Camera is 1024 x 1024 pixels."]
[11.614264488220215, 1.8854657411575317, "The Descent Altitude of the MASCOT Lander is 51 meters."]
[7.265474319458008, 0.5770501494407654, "The Launch Date of the Satellite Satellite is April 26."]
[6.803958415985107, 8.50991153717041, "The Ground Resolutions of the MSR Radiometer is 32 km and 23 km."]
[7.298095226287842, 0.7966291904449463, "The Mission Date of the PROBA Satellite is Sept. 23-26,1999."]
[7.821042537689209, 8.55675220489502, "The Spectral Range of the SOLSPEC-SOLAR Spectrometer is 165-3080 nm."]
[9.564138412475586, 1.2796001434326172, "The Revisit Period of the ZY-3A Satellite is 59 days."]
[3.9957239627838135, 6.472697734832764, "The Uplink Frequency of the CMC Transceiver Communication Device is 140-150 MHz."]
[6.504489898681641, 5.178898811340332, "The Radiometric Sensitivity of the TerraSAR-X Satellite is Improved."]
[9.812703132629395, 4.869325160980225, "The Firing Duration of the Y-axis Bang-Bang Maneuver Satellite Maneuver is 10 s."]
[10.193617820739746, 2.9469451904296875, "The Orbit Altitude of the CBERS-4 Satellite is 778 km."]
[10.321737289428711, 5.41601037979126, "The Components of the T3\u00b5PS Micropropulsion System is MEMS based valve and nozzle, MEMS-based pressure transducer and filter, CGG (Cool Gas Generator)."]
[9.564718246459961, 7.401938438415527, "The Suburban Neighborhood Temperature of the ECOSTRESS Instrument is Averaged about 14 F (8 C) cooler than pavement."]
[8.604463577270508, 4.835596084594727, "The Maximum Daily Observations of the NEMO-AM Satellite is 2."]
[7.8840227127075195, 3.9854366779327393, "The Area Coverage of the EROS-B Satellite is 450 km."]
[9.440184593200684, 5.494106292724609, "The Attitude Control of the ADCS unit Satellite Component is 3-axis stabilization."]
[7.65412712097168, 3.7307169437408447, "The Location of the Tyndall Glacier Glacier is Chile."]
[8.424617767333984, 10.036917686462402, "The Payload of the Planet Satellite Satellite is Telescope and a frame CCD camera equipped with Bayer-mask filter."]
[7.062681198120117, 3.593386650085449, "The Operational of the WorldView 4 Satellite is Yes."]
[3.2248082160949707, 5.291027069091797, "The Capacity of the Onboard Data Storage Data Storage System is 8 GByte."]
[7.628821849822998, 7.790816783905029, "The Sample Capture Method of the TAGSAM Sample Acquisition Mechanism is Nitrogen gas will blow onto the surface to roil up dust and small pebbles, which will then be captured in the TAGSAM head."]
[4.469095230102539, 7.117072105407715, "The Design Features of the Receivers Communication is 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."]
[7.693221569061279, 1.0439342260360718, "The Scheduled Launch Date of the Sentinel-1C Satellite is March 2024."]
[8.305377960205078, 3.4602200984954834, "The Baseline Vector Accuracy of the TanDEM-X Satellite is 1 mm."]
[9.340473175048828, 8.78684139251709, "The Reflectance of the Primary Mirror Optical Component is >0.27 between 40 nm and 200 nm."]
[5.54660701751709, 3.158399820327759, "The Bus Provider of the TRACERS Satellite Mission is Millennium."]
[7.038753509521484, 9.785467147827148, "The Wavelength Range of the Band No 3 Spectral Band is 1.60 \u00b10.50 - 1.80 \u00b1 0.50 \u00b5m."]
[2.3794138431549072, 3.777884006500244, "The Deployment of the Solar Array Satellite Component is Elastically deployable."]
[9.449394226074219, 5.874388217926025, "The Filter of the ACS Attitude Control System is Extended Kalman filter."]
[9.346848487854004, 0.4925076365470886, "The Life Expectancy of the SPOT-4 Satellite is End of 2012."]
[8.01009464263916, 1.4049137830734253, "The Article Publication Date of the Solar Orbiter Satellite is 26 April 2021."]
[10.391702651977539, 4.9739861488342285, "The Chamber Pressures of the LM thruster Thruster is Approximately 700,000-2,100,000 Pa."]
[11.290353775024414, 4.232589244842529, "The Density of the Venus' Orbital Dust Space Dust is About 10% more dense than in neighboring regions."]
[9.130560874938965, 6.093813419342041, "The Control Mode of the CMG Control Moment Gyroscope is Three-axis."]
[5.225622653961182, 3.857330560684204, "The Manufacturer of the Data Storage System Satellite Component is RUAG Space."]
[3.3268649578094482, 5.36124849319458, "The On-board Storage Capacity of the RF Communications Communication System is 32 Gbit."]
[10.24887752532959, 3.11321759223938, "The Orbital Altitude of the HPT High Precision Telescope is 400 km."]
[7.841922283172607, 6.010262966156006, "The Imager Calibration Frequency of the TRUTHS Satellite is Daily."]
[6.734579563140869, 10.163222312927246, "The Primary Use of the Band 4 Spectral Band is SST, day/night clouds."]
[8.685066223144531, 8.884318351745605, "The Field of View of the CHIPS Spectrometer is 5\u00ba \u00d7 26.7\u00ba."]
[7.844883441925049, 9.228438377380371, "The Spectral Sampling Interval of the HSC Spectrometer Spectrometer is 1.2 nm \u2013 16 nm."]
[9.563156127929688, 7.774490833282471, "The Energy Range of the ELS-A Electron Measurement Instrument is 400 \u2013 490 keV."]
[9.577127456665039, 7.557440757751465, "The Nominal Cooling Capacity of the Stirling-cycle cryocooler Cryocooler is 780 mW at 75 K."]
[4.649834156036377, 9.046182632446289, "The Presentation Date of the InSight Mars Mission Mission is 27 April 2017."]
[5.856992244720459, 6.813153266906738, "The Pulse Bandwidth of the SIRAL Radar is 320 MHz."]
[7.170036315917969, 6.854272365570068, "The Launch Date of the OCO-3 Instrument is May 2019."]
[8.21674633026123, 0.9979661703109741, "The Swath Mapping of the UV/VIS Camera Camera is First and second month."]
[7.301363468170166, 0.40875163674354553, "The Launch Date of the EMIT Satellite is 2022."]
[8.583433151245117, 9.425025939941406, "The Sensitivity of the NIRSpec MIRI Optical Instrument is 368 nJy (3.5 \u03bcm, \u03c4 i =10,000 s, and \u03bb/\u0394\u03bb = 100)."]
[10.192983627319336, 1.0985133647918701, "The LTDN of the Satellite SuperView Constellation is 10:30 hours."]
[7.432980060577393, 1.031545639038086, "The Check-out Result Date of the ALOS Ground Data System Ground Data System is July 31-Aug. 4, 2006."]
[12.973807334899902, 4.8498358726501465, "The Mission Duration of the IBEX Spacecraft is Seven years."]
[8.104496955871582, 0.3379977345466614, "The Meeting Date of the ISS-RapidScat Satellite is May 5-8, 2013."]
[4.916834831237793, 2.0682437419891357, "The Quantity of the Aluminum Spheres Satellite is 3."]
[6.727548599243164, 3.8593475818634033, "The Purpose of the COSMO-SkyMed Satellite Constellation is Military and civil (research and commercial) data use."]
[7.338052749633789, 0.21358971297740936, "The Launch Date of the MEV-2 Satellite is August 2020."]
[9.549468994140625, 9.102956771850586, "The Telescope Diameter of the SILEX Terminal is 25 cm."]
[9.470057487487793, 0.6088579893112183, "The Design Lifetime of the TerraSAR-X Satellite is 5 years."]
[7.041967868804932, 4.353894233703613, "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."]
[6.582149505615234, 4.6192803382873535, "The Project of the CFOSAT Satellite is Unknown."]
[8.319918632507324, 4.570581912994385, "The Swath Width of the Antenna Subsystem Satellite Component is 180 km."]
[9.31861686706543, 6.379242897033691, "The Availability of the Star Tracker Attitude Determination Device is >99.9%."]
[8.75755786895752, 6.930067539215088, "The Number of Fluxgate Sensors of the SOSMAG Magnetometer is 2."]
[8.58740234375, 1.653847336769104, "The News Release Date of the WFIRST Space Telescope is 30 March 2020."]
[11.733931541442871, 1.6973344087600708, "The Landing Date of the Philae Lander is 12 November 2014."]
[12.057415962219238, 3.310925245285034, "The Orbit Inclination of the OPAL Satellite is 51.6\u00ba."]
[7.31416130065918, 2.4411532878875732, "The Hold Period of the RISESAT Project is True."]
[9.341565132141113, 7.857811450958252, "The Purpose of the Carmen-2 Radiation Detector is Study the influence of space radiation on advanced components."]
[4.09722900390625, 6.373380184173584, "The Frequency Band of the TT&C Telemetry, Tracking and Command Subsystem is 435-438 MHz."]
[9.183079719543457, 10.169692039489746, "The Number of Cameras of the LROC Camera System is 3."]
[7.82139253616333, 8.704730033874512, "The Mass Measurement Range of the NMS Mass and Velocity Spectrometer is 1-40 AMU."]
[6.4495439529418945, 5.637668609619141, "The Measurement Precision of the GNSS-RO Instrument Instrument is Higher than other radio occultation instruments."]
[1.5218936204910278, 4.896203517913818, "The Output Voltage Levels of the CS-XUEPS2-41 Electrical Power Subsystem is 3.3, 5, or 12 V."]
[6.1669020652771, 5.132009983062744, "The Affiliation of the Global Navigation System GPS Satellite-based Measurement System is Various."]
[7.035473346710205, 1.4375401735305786, "The Launch Date of the Alba Cluster 3 Satellite Cluster is Q2 2021."]
[6.061222553253174, 9.664754867553711, "The Mass of the Instrument Optical Bench is 18.20 kg."]
[5.759683609008789, 2.8783624172210693, "The Manufacturer of the Lightspeed Satellites Satellite is Thales Alenia Space."]
[5.334469795227051, 6.602362632751465, "The Offset Angle of the Antenna Communication is 52.5\u00ba."]
[8.647359848022461, 8.026327133178711, "The Heritage of the DOSTEL Radiation Detector is Mir station (Oct. 1997 - Jan. 1998), Shuttle flights STS-76, -81, and -84, US Lab of the ISS (March to August 2001)."]
[6.95098352432251, 4.673603534698486, "The Sponsors of the RECCAP-2 Activity is Global Carbon Project, European Space Agency, National Institute for Environmental Studies, International Carbon Coordination Project."]
[6.52783727645874, 8.360544204711914, "The RFI Mitigation of the MWI Instrument is Implemented at the lowest frequency channel."]
[4.390857219696045, 5.620755195617676, "The Components of the TT&C subsystem Telemetry, Tracking & Command subsystem is Low power S-band transceiver, microstrip antenna, two full duplex VHF/UHF transceivers, deployable turnstile antennas."]
[9.265214920043945, 8.555890083312988, "The Operation Characterization of the Deformable Mirror Actuator is Requires stable wavefront."]
[6.462606906890869, 4.706051349639893, "The Purpose of the FY-2 Satellite is Cloud profile and rain radars."]
[7.105734348297119, 7.28865909576416, "The Development Announcement Date of the MIRAS Radiometer is Nov. 1997."]
[1.9546185731887817, 4.207917213439941, "The Max. Power of the Solar Panels Power Source is 14 W."]
[8.710126876831055, 6.864330291748047, "The Quantity of the Magnetometers Instrument is 3."]
[9.33897876739502, 6.561083793640137, "The Connection Type of the Lower Barrel and Inner Sleeve Satellite Component is Double lap shear bonded connection."]
[6.73803186416626, 4.365139007568359, "The Expansion of the Copernicus Earth Observation Program is With a suite of new, high-priority satellite missions."]
[6.936103343963623, 7.741818428039551, "The Type of the POLDER-P Instrument is Radiometer/Polarimeter."]
[6.026623249053955, 9.628520965576172, "The Mass of the Instrument DC Electric Fields Investigation is 11.5 kg."]
[7.119548320770264, 8.837953567504883, "The Spatial Resolution Comparison of the GMI Instrument is 50-60% better than TMI on TRMM."]
[3.169707775115967, 4.9089531898498535, "The SDRAM of the Stamp9G20 Microcontroller is 54 MB."]
[11.674134254455566, -0.6623843908309937, "The Flight Altitudes of the MERLIN Satellite is Low."]
[5.636023044586182, 3.3143632411956787, "The Name of the STCUI-RAS Developer is STCUI-RAS."]
[9.144352912902832, 10.608797073364258, "The Ground Pixel Size of the VIS Camera Camera is ~100 m."]
[7.488617897033691, 8.73615837097168, "The Vertical Resolution of the Detector Instrument is 250 m to 2 km or more."]
[4.729614734649658, 0.40870386362075806, "The Number of OneWeb Gen 2 satellites of the Terran R Launch Vehicle is Not Disclosed."]
[5.7998785972595215, 2.9932618141174316, "The Manufacturer of the Terra Satellite is Lockheed Martin Missiles and Space (LMMS)."]
[9.291739463806152, 6.393765926361084, "The Quantity of the Star Tracker Heads Attitude Determination System is 3."]
[7.505218982696533, 8.070273399353027, "The Spatial Resolution of the CERES on TRMM Instrument is Approximately 10 km."]
[8.120454788208008, 4.651971340179443, "The Spatial Resolution of the Solid Earth Tectonic motions Satellite is 100 km."]
[6.285606861114502, 2.114222764968872, "The Components of the Jason-1 Ground Segment Ground Segment is Altimetric and Orbitography Mission Center (SSALTO), located in Toulouse and the Jason Science Data System at JPL in Pasadena."]
[7.2387614250183105, 0.9723366498947144, "The Launch Date of the Rain and Snow Satellite Satellite is Unknown."]
[10.455038070678711, 2.701294422149658, "The Perigee of the Explorer 36 Satellite is 1082 km."]
[7.5550103187561035, 8.763113021850586, "The Cross-Track Swath of the OMPS Nadir Sensor Spectrometer is 2800 km."]
[11.447765350341797, 4.373606204986572, "The Density of the Giant Molecular Clouds Interstellar Medium is Up to a thousand atoms per cubic centimeter."]
[7.810658931732178, 10.100417137145996, "The Sub-Tasks of the Systematic and Radiometric Correction Processor Data Processor is 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 spe."]
[3.8025400638580322, 6.159604549407959, "The Bandwidth of the Ground Station Communication System is 19.2 kbit/s CPFSK and 38.4 kbit/s BPSK/QPSK \u00bd k=7."]
[9.632534980773926, 5.963263034820557, "The Control Method of the ADCS Attitude Determination and Control Subsystem is Magnetic torque control."]
[9.604808807373047, 7.766510009765625, "The Objective of the NINA-2 Telescope is 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)."]
[9.510663032531738, 0.480898916721344, "The Design Lifetime of the FLP Satellite is Two years."]
[5.664056777954102, 9.216316223144531, "The Power of the HIA Instrument is 3.0 W."]
[7.762500286102295, 7.767380237579346, "The Accuracy of the FFRF Sensor Instrument is 1 cm and 1\u00b0."]
[8.681028366088867, 9.143054962158203, "The Entrance Aperture Diameter of the Instrument Spectrometer is 29.5 x 24 mm2."]
[4.355971813201904, 4.5207366943359375, "The Function of the Control and Timing Unit (CTU) Subsystem is Receives commands from the satellite platform and sends state monitoring data to it."]
[8.896841049194336, 5.239354610443115, "The Attitude Subsystem Pointing Error of the Spacecraft Satellite is 0.15\u00ba (3\u03c3)."]
[4.535185813903809, 7.135451316833496, "The IF bandwidth of the Millimeterwave receiver Receiver is 1 \u2013 1.5 GHz."]
[7.34281063079834, 2.6326076984405518, "The Article Title of the Daniel Wang Astronomer is Chandra large-scale mapping of the Galactic Centre: probing high-energy structures around the central molecular zone."]
[5.06705904006958, 6.972045421600342, "The Main Beam Efficiency (%) of the Antenna Reflector is 86."]
[6.081781387329102, 2.5747528076171875, "The Capability of the ORS Office is Develop the capability to augment or replace space capabilities on very short timescales."]
[11.385220527648926, -0.8131232261657715, "The Launch Vehicle compatibility of the DSX Spacecraft Payload Module  Payload Module is 12 months."]
[8.441210746765137, 10.116530418395996, "The Pixel Size of the Detector Array Assembly Detector Array is 13 \u00b5m."]
[5.7742743492126465, 7.192342758178711, "The Central Transmission Frequencies of the RA Imaging System is 13.58 GHz and 5.25 GHz."]
[6.08005952835083, 2.817218780517578, "The Structure of the STPSat-1 Satellite is AeroAstro SpaceFrame."]
[8.895642280578613, 2.1526589393615723, "The Program of the New Horizons Spacecraft is New Frontiers Program."]
[9.447455406188965, 5.542959690093994, "The Attitude Pointing Accuracy of the AOCS Attitude and Orbit Control Subsystem is \u2264 0.4\u00ba (3\u03c3)."]
[8.742711067199707, 5.264107704162598, "The Spatial Resolution of the Attitude Determination & Control System Satellite System is Better than 100 m."]
[10.493805885314941, -0.9717432856559753, "The Mass of the Hodoyoshi-3 Microsatellite is 60 kg."]
[10.25313949584961, 4.943109512329102, "The Mission of the Colloid Micro-Newton Thrusters Thruster is Space Technology 7."]
[9.147268295288086, 4.195629119873047, "The Bus Size of the Spacecraft Satellite is 1300 mm x 1310 mm x 1988 mm."]
[6.6258463859558105, 3.7072131633758545, "The Payload of the PLATiNO 2 Satellite is Thermal Infrared (TIR)."]
[5.92957878112793, 9.336368560791016, "The Mass Resolution of the STROFIO Instrument is m/Dm = 60."]
[9.522884368896484, 1.1340893507003784, "The Programming Horizon of the MUS Subsystem is 72 hours."]
[8.507874488830566, 6.553686618804932, "The Boom Length of the NewMag Magnetometer is 2.55 m."]
[6.412365913391113, 6.40548849105835, "The Antenna Mechanism Lifespan of the SeaWinds instrument Scatterometer is More than a decade."]
[5.158590316772461, 4.937724590301514, "The Rotor Type of the Knudsen Station Ground Station is AlphaSpid's RAS rotor."]
[9.487202644348145, 0.6113117933273315, "The Lifetime of the Satellite Spacecraft is Up to 12 years."]
[4.704100131988525, 5.781301498413086, "The RF Communications of the Spacecraft Satellite is VHF beacon."]
[6.322821140289307, 3.1563546657562256, "The Deployment Location of the Astro Pi Computer is Columbus module and looking through a hatch window towards the Earth."]
[8.383207321166992, 1.5560722351074219, "The Descent Date of the Rosetta Spacecraft is 30 September."]
[2.0257580280303955, 5.108969688415527, "The Maximum Temperature Differential of the PC5 Power Supply is 85 \u00b0C."]
[9.026692390441895, 4.548433780670166, "The Position of the WFI Mosaic Plate Assembly Focal Plane is Much farther outboard towards the anti-sun side of the Observatory."]
[4.946791172027588, 1.8790189027786255, "The Number of Springs and Flaps of the Dellingr mission Satellite Mission is One."]
[4.8019843101501465, 6.095449924468994, "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."]
[4.471923828125, 5.763868808746338, "The X-band Downlink Frequencies of the Landsat-6 Satellite is 8082.5, 8212.5, and 8342.5 MHz."]
[7.100630283355713, 1.1321338415145874, "The Mission End Date of the D-Sat Satellite is October 10, 2017."]
[10.393969535827637, 7.67034387588501, "The Material of the Magnet Component is AlNiCo."]
[5.562808036804199, 2.9643197059631348, "The Task of the Restore-L Satellite is Refuel."]
[9.180556297302246, -0.6105742454528809, "The Extension Date of the ANGELS Nanosatellite is 13 October 2020."]
[7.152300834655762, 1.88023841381073, "The Formation Configuration Parameters of the SJ-9A and SJ-9B Satellites is Eccentricity difference, phase difference, ascending node difference, argument of perigee difference."]
[9.541193962097168, 0.5716462731361389, "The Goal Life of the Resurs-DK1 Spacecraft is 5 years."]
[6.005142688751221, 9.570003509521484, "The Mass of the Instrument Instrument is 2.7 kg."]
[7.823392868041992, 8.423198699951172, "The Data Set of the EPIC Instrument is Single-pixel images taken multiple times per day, in 10 wavelengths, over an extended period."]
[7.757543563842773, -0.44946572184562683, "The Launch Window of the SpaceX Company is 5-hour window that opens at 8:02 p.m. EDT Sept. 15."]
[10.278616905212402, 6.859522342681885, "The Purpose of the HS Heater System is Keep equipment temperatures above the minimum non-operational limits (\u201320 \u00baC for most of the units) during satellite SHM and PLM Off modes."]
[7.378501892089844, 1.11150324344635, "The Observation Date of the RHESSI Satellite is SOL2017-09-10."]
[8.192615509033203, 10.5044584274292, "The Data Output of the TDI Detector Detector is 58 Mpixel/s."]
[8.44560718536377, 10.269983291625977, "The Sensor Read Noise of the Sensor Image Sensor is 2.48 ADU."]
[6.422020435333252, 1.8555091619491577, "The Operation Status of the Gokturk-2 Satellite is Nominal."]
[11.775556564331055, 4.5634331703186035, "The Diameter of the Cassiopeia A Supernova Remnant is 15 light years."]
[8.173235893249512, 7.200818061828613, "The Simultaneous Check Method of the Data Processing System Instrument Component is Comparison of the known power of the reference electrical source with the precision measurement of the servo-system."]
[11.008359909057617, 3.3647117614746094, "The Measurement Depth of the Juno Spacecraft is About 3,000 km."]
[9.309054374694824, 4.189177989959717, "The Total Solar Array Size of the Resurs-DK1 Spacecraft is 36 m2."]
[7.85235595703125, -0.09656216204166412, "The Initial Launch Date of the Nauka Laboratory Module is 2007."]
[9.338668823242188, -0.6812697649002075, "The Developer of the Venta-1 Nanosatellite is OHB Systems."]
[6.184998035430908, 0.5917872190475464, "The Launch Date of the CubeSats Satellite is Dec. 9, 2013."]
[1.882934331893921, 4.038723468780518, "The Total Array Area of the Solar Panels Power Source is 9.5 m2."]
[9.557046890258789, 0.5338369607925415, "The Design Life of the SA-200HP Spacecraft Platform is 5 years."]
[9.318316459655762, 10.308557510375977, "The Boresight Deviation of the PamCam Camera is -0.27\u00b0 to -0.25\u00b0 in horizontal and 0.40\u00b0 to 0.48\u00b0 in vertical direction."]
[8.51478385925293, 2.296661615371704, "The Lead Author Affiliation of the Parker Solar Probe Satellite is BWX Technologies, Inc. and University of Michigan."]
[1.5077463388442993, 4.959879398345947, "The Specific Power of the SBVR Power Supply is 373 W/kg."]
[2.346022844314575, 5.020560264587402, "The Capability of the PTT-A3, PTT-ZE, PMT-A3 Argos-3 Platforms is Very low-power consumption."]
[10.26031494140625, 8.75952434539795, "The Telescope Heritage of the EUVI Extreme Ultraviolet Imager is EIT (EUV Imaging Telescope) heritage on SOHO and of TRACE (Transition Region and Coronal Explorer) mission heritage."]
[6.991637706756592, 5.2115797996521, "The Data Usage of the JAXA Organization is Precipitation Monitoring."]
[9.63564395904541, -0.33660799264907837, "The Propulsion System of the BIROS Minisatellite is Equipped."]
[9.408244132995605, -0.07426392287015915, "The Flight Nanosats Quantity of the SMDC-ONE program Satellite Program is 8."]
[3.6966960430145264, 6.1789350509643555, "The Data Rate of the Flight Modem Modem is 72 Mbit/s to 2.88 Gbit/s."]
[4.786588668823242, 0.7932343482971191, "The Equity Investment of the Eutelsat Satellite Operator is $550 million."]
[5.587709426879883, 2.9618935585021973, "The Grasp, refuel, and relocate of the Restore-L Servicer is Landsat-7."]
[7.800510883331299, 9.469693183898926, "The Number of Bands of the Spectral Bands Data is 15."]
[8.237858772277832, 2.5682432651519775, "The Longitude of the Himawari-8 Satellite is ~140.7\u00ba east."]
[8.244595527648926, 8.077548027038574, "The Arrival Date of the Europa-UVS Ultraviolet Spectrograph is March."]
[7.778724670410156, 9.791555404663086, "The Spectral Band of the Band Photometers Photometer is 337.0 nm."]
[4.398672103881836, 4.447718143463135, "The Function of the RIU Interface Unit is Acquiring the housekeeping information of the spacecraft, managing the propulsion module items, managing the AOCS components, controlling the configuration of the satellite units."]
[9.239595413208008, 3.183786392211914, "The Orbit Type of the ZY 1-02C Spacecraft is Sun-synchronous near circular orbit."]
[8.183394432067871, 9.372482299804688, "The Ground Resolution of the HgCdTe Detector is 120m."]
[7.854919910430908, 8.97919750213623, "The Spectral bands of the UV/VIS Spectrometer Spectrometer is 248-371/387-693 nm."]
[9.082437515258789, 2.6532866954803467, "The Wavelengths of the NGC 7538 Star Factory is 70 \u00b5m (blue), 160 \u00b5m (green) and 250 \u00b5m (red)."]
[2.1899054050445557, 4.561991214752197, "The Orbit Average Power of the COMMx Payload is 200 W."]
[8.995035171508789, 6.6717705726623535, "The Impact Area of the Solar Storm Natural Phenomenon is Earth's ionosphere."]
[7.26669979095459, 1.3771058320999146, "The Presentation Date of the GMES Missions Sentinel-4, Sentinel-5 and Sentinel-5p Satellites is June 18-22, 2012."]
[9.219256401062012, 8.61085033416748, "The Components of the NAOMI family of optical instruments Technology is Silicon carbide (SiC) optics and structures, multiple-line detectors, integrated focal planes and ultra-compact optical configurations."]
[7.050078392028809, 9.828447341918945, "The Wavelength Range of the Band 3 Spectral Band is 862-877 nm."]
[9.637602806091309, 5.901852607727051, "The Slew Time, 180\u00ba pitch of the ADCS Attitude Determination & Control Subsystem is \u2264 14 minutes."]
[6.690845489501953, 3.534764528274536, "The Mission Type of the MULA Satellite is EO."]
[7.617642402648926, 5.895997047424316, "The Confidence Limits of the CLARREO Satellite is 3\u03c3 or 99%."]
[6.115270614624023, 1.7183518409729004, "The On-Orbit Service Time of the SAR-Lupe Constellation Satellite Constellation is More than 20 years."]
[6.128326416015625, 3.0430657863616943, "The Construction Location of the BRITE Satellites Satellite is UTIAS/SFL."]
[7.6467509269714355, 3.80770206451416, "The Orbital Predictions of the LARES Satellite is Unknown."]
[11.650164604187012, -1.22024405002594, "The Mass of the Bayi Kepu Weixing-1 Satellite is 2 kg."]
[4.581099033355713, 3.650023937225342, "The Sensor of the ESAIL Microsatellite is AIS (Automatic Identification System)."]
[9.592511177062988, 6.008574485778809, "The Attitude Knowledge Precision of the ADCS Unit Attitude Determination and Control System is Better than 2\u00ba."]
[10.418194770812988, 4.776054859161377, "The Propellant of the Propulsion System Propulsion System is Hydrazine."]
[6.7727131843566895, 9.048860549926758, "The Size of the Instrument Optical Instrument is 30 cm x 30.8 cm x 37 cm."]
[3.355153799057007, 4.4246344566345215, "The Components of the PCU Power Control Unit is Antifuse FPGA."]
[8.538047790527344, 10.483366966247559, "The CCD Line Pixel Count of the FPM (Focal Plane Module) Focal Plane is 12,000 pixels."]
[7.111733913421631, 5.084695816040039, "The Volume Range of the Methane Leak Environmental Event is Between five and 20 tonnes of methane per hour."]
[7.366690158843994, 0.3618191182613373, "The Launch Date of the Cheollian 2B Satellite is February 19."]
[7.860435962677002, 1.8763890266418457, "The Mission Name of the ExoMars 2020 Spacecraft is ExoMars 2022."]
[7.321408748626709, -0.13023196160793304, "The Launch Date of the H-IIA Launch Vehicle No. 23 Launch Vehicle is Dec. 26, 2013."]
[4.785582542419434, 7.240268230438232, "The Data Band of the GimmeRF Radio Instrument is 0-30 MHz."]
[1.745688557624817, 4.827130317687988, "The Bus Total Power of the EPS Electrical Power Subsystem is ~286 W."]
[4.284342288970947, 6.353474140167236, "The Frequency of the X-band Data Downlink is Unknown."]
[10.192720413208008, 3.02822208404541, "The Altitude of the ETS-VIII Spacecraft is 35,786 km above the equator."]
[7.638145923614502, 6.487429618835449, "The Micro Vibration Test of the Instrument Satellite Instrument is Successful."]
[6.274415969848633, 8.814552307128906, "The Volume of the AMU Altimeter Microwave Unit is 325 x 305 x 250 mm."]
[10.084845542907715, 3.4805054664611816, "The Volcanic Activity of the Moon Celestial Body is Prolonged."]
[7.590723991394043, 2.5632519721984863, "The Client Docking Plate of the ELSA-d Mission is Ferromagnetic."]
[7.717750549316406, 9.952786445617676, "The Field of View of the VNIR-NP channels Sensor is 70\u00ba."]
[7.09703254699707, 2.498774528503418, "The URL of the PROCYON Deep Space Probe is https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=3348&context=smallsat."]
[7.383659839630127, 6.340946197509766, "The Purpose of the STARFM Data Fusion Model is Combine MODIS data with Landsat data to produce synthetic Landsat-like imagery on a daily basis."]
[5.20841646194458, 3.1148507595062256, "The Purpose of the CubeSats Satellite is 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."]
[9.67082691192627, 1.7588579654693604, "The Imaging Frequency of the Meteosat-10 Geostationary Satellite is Every five minutes."]
[11.416871070861816, 6.46904993057251, "The Detection Band of the XMM-Newton X-ray Observatory is Low energy part of the X-ray band."]
[12.172770500183105, 5.376170635223389, "The Hot Intergalactic Gas Percentage of the Universe Cosmology is 40 percent."]
[5.953495025634766, 9.473596572875977, "The Instrument Mass of the AATSR Instrument is 101 kg."]
[12.134674072265625, 3.3020617961883545, "The Inclination of the ZY 1-02C Spacecraft is 98.5\u00ba."]
[8.02452278137207, 9.899314880371094, "The Size of the Subarray Array is 400 mm x 22 m."]
[9.27699089050293, 10.370942115783691, "The Air Pressure of the Metric Camera Camera is About 1020 mbar."]
[6.673400402069092, 3.551497459411621, "The Mission Type of the JERS-1 Satellite is EO."]
[6.809483528137207, 3.342369556427002, "The Mission Status of the Satellite EO is Planned."]
[7.500184535980225, 8.852867126464844, "The Detector Element Size of the Sounder Satellite Instrument is 10 km x 10 km."]
[9.212656021118164, 4.139004230499268, "The Dimensions of the Spacecraft Satellite is 765 x 730 x 830 mm."]
[9.844658851623535, 1.8339316844940186, "The Observation Type of the TIMED spacecraft Satellite is Plasma distribution around the magnetic equator."]
[9.828978538513184, 8.501581192016602, "The Celestial Sphere Coverage of the Telescope Optical Instrument is Continuous within 5\u00ba of ecliptic poles."]
[9.261383056640625, 8.072346687316895, "The Plastic Scintillator Counters of the Veto System Particle Detector is 5 mm thick."]
[7.8194146156311035, 9.605439186096191, "The Resolving Power of the IR Channel Imaging Device is 70."]
[9.473691940307617, 0.059429872781038284, "The Actual Orbit Duration of the SMDC-ONE Nanosatellite is 35 days."]
[7.773762226104736, -0.5068913102149963, "The Launch Date of the SpaceX CRS 14 Satellite is 16 Jan. 2018."]
[7.203066825866699, 3.901214122772217, "The Onboard Sensors of the SPOT 6-7 Satellite is HRV, HRVIR, HRG and NAOMI."]
[7.110928535461426, 1.5816586017608643, "The Phase C/D Contract Signing of the Spacebus Neo Satellite is Separate Phase C/D contracts were signed with both primes at the end of 2015."]
[6.016737937927246, 3.002626419067383, "The Prime Contractor of the Sentinel-1 Satellite is TAS-I (Thales Alenia Space Italia)."]
[5.091622352600098, 0.4417763650417328, "The Suitability for Satellite Flight of the Silkworm Insect is Duration of the development of each stage, especially, the embryo state is well matched with the satellite flight period of SJ-10."]
[6.840321063995361, 5.4798808097839355, "The Workshop Report URL of the Soil Moisture Active Passive (SMAP) Mission is http://nasascience.nasa.gov/earth-science/decadal-surveys/Volz1_SMAP_11-20-07.pdf."]
[10.198260307312012, 2.9340620040893555, "The Orbit Altitude of the Genesis-2 Satellite is 560 km."]
[9.46843147277832, 5.120431423187256, "The Spin Motion of the GMS Satellite is 100 rpm."]
[11.504932403564453, -1.3175777196884155, "The Mass at Launch of the Eutelsat Quantum Satellite is 3.5 tons."]
[9.861838340759277, -0.9933997988700867, "The S/C Mass of the JL-1-GF03B Microsatellite is <45 kg."]
[10.063386917114258, 9.885749816894531, "The Funding of the IRIS Imager Camera is DSO National Laboratories."]
[7.231717109680176, 4.451414585113525, "The Goal of the Satellite Constellation RMIB SIMBA program is Measure the Earth radiation imbalance."]
[6.420221328735352, 5.5081706047058105, "The Technology of the MiRaTA Satellite is Radio Occultation."]
[6.0925726890563965, 9.746081352233887, "The Mass of the Experiment Telescope is 11 kg."]
[7.845636367797852, 4.095058917999268, "The Number of Images for Signal to Noise Ratio of the EyeSat Satellite is 10 images."]
[6.888618469238281, 0.5190846920013428, "The Bulletin Date of the GEOS-1 Satellite is May 1977."]
[4.009408473968506, 6.499780178070068, "The Bandwidth of the Spacecraft Repeater Communication Device is 100 kHz."]
[5.068227291107178, 5.20165491104126, "The Total Satellite Passes of the KSAT Ground Station Network is 50,000 a month."]
[9.878660202026367, 6.668196678161621, "The B1 and B2 Tank Temperatures Increase of the Advanced Composition Explorer Spacecraft is By 5\u00b0 C."]
[9.061248779296875, 8.72822093963623, "The Scan Angle of the Rotating Telescope Scanner Optical Instrument is \u00b153\u00b0."]
[9.720276832580566, 9.010064125061035, "The Diameter of the Main Mirror Optical Component is 64 cm."]
[11.047364234924316, 4.659414768218994, "The Observation Speed of the Solar Dynamics Observatory Satellite is 200 times faster than real time."]
[4.041111946105957, 1.2036008834838867, "The Mission Type of the ARMADILLO Satellite is Non-EO."]
[8.205948829650879, 3.2776598930358887, "The Dual Receive Antenna Configuration of the TanDEM-X Satellite is Introduced during the TanDEM-X Science phase."]
[6.714446067810059, 0.8232104778289795, "The Data Release Date of the ICESat-2 Satellite is May 2019."]
[11.65321159362793, -1.1393927335739136, "The Total Mass of the Spacecraft Satellite is 25.5 kg."]
[2.2601544857025146, 4.4211344718933105, "The Power of the Spacecraft Satellite is 350 W."]
[7.839001178741455, 7.851916790008545, "The Detection Efficiency of the Instrument Sensor is ~90%."]
[7.559505939483643, 3.6705591678619385, "The Mean Motion of the AC4-B Satellite is Higher."]
[6.339693546295166, 8.398368835449219, "The Wavelength/Frequency of the RM-08 Passive Microwave Scanning Radiometer is 0.8 cm / 36.6 GHz."]
[7.978724002838135, 1.3918101787567139, "The Image Capture Date of the Solar Orbiter Satellite is 7 March."]
[4.711208820343018, 1.6728557348251343, "The Number of Batch 3 Satellites of the Galileo Satellite Navigation System is 12."]
[11.594724655151367, 2.6427857875823975, "The Surface Composition of the Ryugu Asteroid is Two different types of material, one slightly redder and the other slightly bluer."]
[1.9107656478881836, 3.866900682449341, "The Fabrication Technology of the Solar Cells Energy Device is D-HVPE (Dynamic Hydride Vapor Phase Epitaxy)."]
[9.05006217956543, 7.636112689971924, "The Manufacturer of the LINAS Ionization Gauge is Cannon Corp.."]
[10.162914276123047, 5.447246074676514, "The CT Scans of the Valves Spacecraft Component is Scheduled."]
[8.48904800415039, 10.445235252380371, "The CCD Line Read-Out Rate of the FPM (Focal Plane Module) Focal Plane is 6.5 MHz."]
[1.659611701965332, 4.59663200378418, "The Power Bus System of the SpriteSat Satellite is Experienced a low voltage condition."]
[9.740877151489258, 4.434840679168701, "The Sail Assembly and Boom Mechanical Assembly of the Sail Subsystem Components is Two primary components."]
[2.633467197418213, -1.4555284976959229, "The Brigthness Temperature (BT) Sensitivity of the Antenna Reflector is \u00b10.26 K."]
[6.477226734161377, 4.405187606811523, "The Carried Instruments of the Flying Laptop Satellite is Scientific instruments for multispectral Earth observation as well as spaceborne maritime ship surveillance."]
[7.834041595458984, 9.641626358032227, "The Number of Bands of the Optical Scanning Design Imaging Spectrometer is 21 bands (nominal Earth View)."]
[6.8980889320373535, 0.37071844935417175, "The Launch Date of the AISSat-1 Satellite is July 2010."]
[11.661240577697754, -1.1630960702896118, "The Payload Module Mass of the Euclid Spacecraft is 800 kg."]
[9.601826667785645, 7.787662982940674, "The Energy Range of the EPD-E Energetic Particle Detector - Electrons is 50 keV \u2013 4 MeV."]
[9.524089813232422, 0.496923565864563, "The Design Life of the Spacecraft Satellite is \u226512 years in space."]
[7.544256687164307, 2.3587474822998047, "The URL of the Arrokoth Celestial Body is https://www.aaas.org/news/close-arrokoth-reveals-how-planetary-building-blocks-were-constructed."]
[9.178484916687012, 10.150221824645996, "The Quantity of the LROC Camera is 2."]
[12.13417911529541, 2.214923858642578, "The Sample Collection Sites of the OSIRIS-REx Spacecraft is Nightingale, Kingfisher, Osprey and Sandpiper."]
[11.669453620910645, 1.9679791927337646, "The Rebound Distance of the Philae Lander Spacecraft is A kilometer above the comet."]
[10.192130088806152, 3.030881404876709, "The Altitude of the Satellites Satellite is 35,786 km."]
[4.972706317901611, -0.12095573544502258, "The Commercial Connectivity Services Start of the OneWeb Company is Late 2021."]
[9.319668769836426, 2.0933339595794678, "The Closest Approach Time of the New Horizons spacecraft Spacecraft is 10:29 a.m. EST."]
[11.036952018737793, 4.863083362579346, "The Speed of the Solar Energetic Particles Space Weather Phenomenon is Close to the speed of light."]
[11.461861610412598, -1.3409488201141357, "The Instrument Mass of the DubaiSat-1 Satellite is 38.67 kg."]
[11.19670295715332, -1.5254385471343994, "The Mass of the SeaHawk-1 CubeSat is ~5 kg."]
[9.472989082336426, 5.902378559112549, "The Current Purpose of the CRS Cosmic Ray Subsystem is Study the heliosphere\u2019s charged particles and the particles in the interstellar medium."]
[8.25290298461914, 5.521553993225098, "The Image Processing of the NASA's Solar Dynamics Observatory Satellite is Reduce noise."]
[9.575631141662598, 3.114379644393921, "The Orbit Type of the NanoRacks-QB50 CubeSats Satellite is Near-circular."]
[8.500481605529785, 2.775223731994629, "The Orbit of the JPSS-1 Satellite is Polar."]
[8.506412506103516, 10.468657493591309, "The Format of the CCD Detector Array Imaging Device is 2 k x 2 k."]
[9.605826377868652, 5.9530487060546875, "The Pointing Accuracy of the ADCS Attitude Determination and Control Subsystem is \u00b15\u00ba."]
[9.962258338928223, 9.538702011108398, "The Monitored Parameters of the SAGE-III Monitoring Instrument is Aerosols, ozone and other gases in Earth\u2019s high atmosphere."]
[7.8007588386535645, 9.004378318786621, "The Spectral Resolution of the VIS Spectrometer is 0.63 nm."]
[6.413887977600098, 4.140517711639404, "The Testing Location of the CO2M Satellite is ESA\u2019s ESTEC testing facilities in the Netherlands."]
[3.606921434402466, 2.281018018722534, "The Size of the AeroCube-8A Satellite is 1.5U."]
[1.2841001749038696, 4.53462028503418, "The Voltage of the Power Storage Battery is 1.2 V."]
[9.573229789733887, 3.842066526412964, "The ADS-B Receiver of the CanX-7 Satellite is Included."]
[11.720450401306152, 1.0972776412963867, "The Lunar Orbit Period of the Chang'e-1 Satellite is 127 minutes."]
[11.53432559967041, 2.650285482406616, "The Discovery Date of the Asteroid 162173 Ryugu Asteroid is Unknown."]
[1.9444341659545898, 4.000509738922119, "The Solar Panels Area of the IRS-1A Satellite is 8.6 m2."]
[11.70186710357666, 4.5937180519104, "The Mythological Names of the Pleiades Open Cluster is Alcyone, Maia, Electra, Merope, Taygete, Celaeno, and Sterope."]
[11.698385238647461, 2.633544445037842, "The Distance from Earth of the Didymos Binary System is Within 0.08 AU."]
[8.156383514404297, 8.69428539276123, "The Spectral Coverage of the Instrument Spectrometer is 3.74 - 15.4 \u00b5m for the array grating spectrometer (IR bands)."]
[5.959418773651123, 6.738353252410889, "The Single-look Resolution of the Radar Instrument is 250 m x 400 m."]
[4.042805194854736, 1.197522521018982, "The Mission Type of the ALL-STAR Satellite is Non-EO."]
[5.780157566070557, 6.883082389831543, "The Bandwidth of the Radar Sensor is 1 MHz."]
[7.910263538360596, 9.086155891418457, "The Passband of the VIS Visual Instrument is 550-900 nm."]
[8.155021667480469, 5.690837383270264, "The NDVI NIR Band to Red Band Balance of the R3 System Satellite is Off."]
[6.466212272644043, 3.5957329273223877, "The Launch Site of the Sentinel-1C Satellite is Guiana Space Center, Europe\u2019s Spaceport in French Guiana."]
[7.0374932289123535, 3.5065648555755615, "The Mission Phase of the PROBA-V Satellite is Operational."]
[9.298895835876465, 6.479525566101074, "The Components of the OSP Optical Sensor Package is One boresighted fixed-head star tracker and two skewed fixed-head star trackers."]
[9.079318046569824, 1.4683040380477905, "The Mission Duration of the Ulysses Spacecraft is 16 years."]
[9.545069694519043, 0.4371197819709778, "The Design Life of the GEISAT Precursor Satellite is Four years."]
[9.137311935424805, 7.342822074890137, "The Operation Temperature of the Calibration Motor Home Sensor Sensor is Low temperatures."]
[6.435388088226318, 3.9809165000915527, "The Data Processing and Distribution Infrastructure of the GeoSat-2 Satellite is ENTICE."]
[8.239141464233398, 4.497555732727051, "The Scientific Goals of the INTEGRAL Satellite is High resolution spectroscopy with fine imaging and accurate positioning of celestial sources in the gamma-ray domain."]
[7.299266815185547, -0.745841920375824, "The Validation Data Source of the CYGNSS Satellite is GPS dropsondes, SFMR, IWARP."]
[8.007205963134766, 7.6102213859558105, "The Manufacturer of the RadFET Sensor is Tyndall National Institute in Ireland."]
[8.620296478271484, 6.790097236633301, "The Magnet Configuration of the AMS-02 Instrument is Permanent."]
[9.302992820739746, 5.257617950439453, "The Yaw Axis Flip Angle of the Trail Spacecraft Spacecraft is 180\u00ba."]
[7.872896194458008, 9.281052589416504, "The Spectral Range of the SWIR Spectrometer Spectrometer is 900 nm to 2450 nm."]
[6.0505452156066895, -0.2277604043483734, "The Launch Date of the Oculus-ASR Satellite is 25 June 2019."]
[8.379021644592285, 9.43252944946289, "The Surface Roughness of the Mandrels Manufacturing Component is Better than 4 \u00c5 (0.4 nm)."]
[8.1034574508667, 9.329497337341309, "The GIFOV of the SWIR Detector is 4 km."]
[11.732208251953125, -1.2663816213607788, "The Mass of the KazEOSat-2 Satellite is ~185 kg."]
[4.411860466003418, 4.59430456161499, "The Function of the MCCM Multi-chip Control Module is Control the illumination coefficients (attenuation or phase) of the RF signal received from each subarray for the beam synthesis."]
[7.903248310089111, 9.944764137268066, "The Bands of the AaSI Spectral Imager is One to three."]
[6.643742084503174, 1.5262010097503662, "The Contract Signing Date of the Jason-CS / Sentinel-6 Satellite Mission is May 11, 2015."]
[8.869908332824707, 6.642833232879639, "The Theoretical Performance of the Lateral Shearing Angular Period Device is 41 mas."]
[8.008810997009277, 8.682937622070312, "The Wavelength of the UVSP Instrument is About 2760 \u00c5 in first order."]
[8.863122940063477, 2.304871082305908, "The Research Topics of the MEMS Space Telescope Telescope is Unknown."]
[7.718615531921387, 4.128082752227783, "The Orbits of the Deimos-2 Earth Observation Satellite is Approximately 5,300 times during this year."]
[8.589828491210938, 9.745485305786133, "The Off-nadir tilted field of view of the OLCI Camera Assembly is Implemented for OLCI cameras."]
[7.742539405822754, 2.948946237564087, "The Impact Test Outcome of the DebriSat Satellite is Planned catastrophic outcome."]
[7.478755474090576, 8.96223258972168, "The Spatial Resolution of the TES Spectrometer is 0.43 km x 5.3 km."]
[9.54185676574707, 1.041367530822754, "The Tracking Time of the MarCO-B CubeSat is Several More Weeks."]
[1.536397933959961, 4.8814215660095215, "The voltage of the Bus Bus is  28\u00b15 V."]
[7.56898832321167, 6.590878009796143, "The Typical Value of the H2CO Satellite Instrument is 10."]
[7.117612361907959, 4.317698955535889, "The Mission Productivity of the Clementine Satellite is Scientifically Productive."]
[7.773394584655762, 0.446927547454834, "The Orbit Phase Orbit Determination Date of the Chandrayaan-1 Satellite is Oct. 12-16, 2009."]
[7.3501787185668945, 3.5634734630584717, "The Unknown of the ZY-1-02C Satellite Images Satellite Images is Unknown."]
[7.988785266876221, 2.0703752040863037, "The Mission of the TGO Trace Gas Orbiter is Measure the abundance and distribution of rare gases in the atmosphere."]
[6.090211868286133, 0.8633031845092773, "The Data Resolution of the RAVAN Satellite is 10\u00b0 x 10\u00b0 latitude\u2013longitude geographic grid."]
[10.255668640136719, 3.0236754417419434, "The Periapsis Altitude of the Satellite Spacecraft is 879 km."]
[1.8994641304016113, 3.9849233627319336, "The Type of the Solar Panels Power Source is Silicon cells."]
[8.32366943359375, 8.556442260742188, "The Detector Type of the SPIRIT-III Interferometer-Spectrometer is Arsenic-doped silicon, blocked impurity-band conductor detectors."]
[11.486743927001953, -1.2164278030395508, "The Mass of the ROBUSTA picosatellite Satellite is \u2264 1 kg."]
[7.297948360443115, -0.4176558256149292, "The Starlink Satellites Launch Date of the SpaceX Company is 11 March 2021."]
[5.903102874755859, 6.269402027130127, "The Centre Frequency of the XSAR SAR is 9.59 GHz."]
[1.2821217775344849, 4.147585391998291, "The Battery Capacity of the GHGSat-D Microsatellite is 26 W hr."]
[10.820510864257812, 2.017136812210083, "The Altitude Difference of the Swarm-A and Swarm-C Satellite Constellation is Less than 5 km."]
[11.62781810760498, -0.9253437519073486, "The Mass of the Spacecraft bus Satellite is 1750 kg."]
[8.404329299926758, 7.949541091918945, "The Data Transfer of the Webb's Fine Guidance Sensor (FGS) Sensor is Up to two science instruments at a time."]
[8.391331672668457, 4.366653919219971, "The Single Pass Stereo Coverage of the QuickBird-2 Satellite is Single scene (<10\u00ba off nadir track)."]
[8.415335655212402, 11.076186180114746, "The Preferred Number of Perfect Rows of the QWIP Array Sensor Array is 2."]
[2.3349478244781494, 5.089561462402344, "The Operational Power Consumption of the PPU System is Approximately 15 W."]
[4.41844367980957, 5.600403785705566, "The Downlink Rate of the Sentinel-1 Satellite is Very high X-band downlink rate."]
[6.867868423461914, 1.1208343505859375, "The Commencement Date of the SERVIR Program is 2004."]
[7.942022323608398, 8.012978553771973, "The Overall Relative Measurement Error of Radiance in Bands 1-3 of the Scanning geometry Instrument is 10%."]
[3.96643328666687, 5.651107311248779, "The Data Download of the STRaND-1 Satellite is 274 kB over 65 k packets."]
[4.905823707580566, 6.349404335021973, "The Antenna Diameter of the PRARE ground transponder Ground Station Equipment is 60 cm."]
[10.238298416137695, 2.9831995964050293, "The Orbit Altitude of the Satellite Constellation Non-Geostationary Satellites (NGS) is 1100 and 1300 km."]
[7.086789608001709, 7.610799789428711, "The Objective of the MWI Instrument is Measure precipitation, provide measurements of cloud products, water vapor and temperature profiles, and surface imagery."]
[8.181741714477539, 6.955947399139404, "The Manufacturer of the Phasemeter Assembly Component is University of Birmingham."]
[8.157383918762207, 11.133506774902344, "The Manufacturer of the Linear Encoder Sensor is Not provided."]
[7.1945481300354, 9.243414878845215, "The Cross-Track Angle of the MSI-0 and MSI-1 MSI Instruments is 3\u00ba."]
[3.8847780227661133, 4.874621391296387, "The Unknown of the DSP ASIC Data Signal Processor is Unknown."]
[7.535163402557373, 8.453160285949707, "The SNR of the Instrument Spectrometer is \u2265450 @ 620 nm, \u2265300 @ 2100 nm, \u2265200 (for each band)."]
[5.919308662414551, 4.652567386627197, "The Augmentation of the L1-SAIF+ Satellite Message is GPS satellites."]
[6.521407127380371, 6.373963832855225, "The Mass of the SeaWinds scatterometer Scatterometer is 205 kg."]
[4.461350440979004, 5.977665424346924, "The Bandwidth Allocation of the TerraSAR-NG System Satellite System is 1,200 MHz."]
[8.974320411682129, 2.753929376602173, "The Tasks of the Kepler Mission is 4."]
[5.613452434539795, 2.3555893898010254, "The Reduction in Satellite Loss of the SBSS-1 Satellite System is 66%."]
[6.435845851898193, 9.172374725341797, "The Component of the MuREM Payload is Radiation effects board."]
[6.403999328613281, 4.31679630279541, "The Navigation Payload Builder of the MTSAT-1R Satellite is Alcatel Space of France."]
[8.667171478271484, 3.3965859413146973, "The Coverage of the Satellite LEO (Low Earth Orbit) is Global."]
[6.173677444458008, 4.667946815490723, "The Recent Efforts of the ICEYE Satellite Constellation is Tracking and analyzing flood events globally, launching new SAR satellites."]
[7.455792427062988, 4.2219367027282715, "The Purpose of the TRIO-CINEMA Satellite Constellation is Provide stereo ENA imaging of the ring current."]
[7.7334723472595215, 3.8396894931793213, "The Average Ice Thickness of the Vatnaj\u00f6kull Glacier Glacier is More than 900 m."]
[7.1332244873046875, 9.122097969055176, "The Swath of the Extra Wide Swath mode (EWS) Operational Mode is 400 km."]
[8.807441711425781, 1.4106988906860352, "The Operation Status of the Van Allen Probes Satellite is Nominal."]
[9.406143188476562, 0.9842716455459595, "The Launch Timeframe of the Lightspeed Satellites Satellite is Around two years."]
[3.3721365928649902, 5.267167091369629, "The Onboard Mass Memory of the Solar Orbiter Satellite is Yes."]
[8.803507804870605, 9.169286727905273, "The Focal Length of the Long Wavelength Band Spectrometer is 12.5 cm (f/2.2)."]
[9.547810554504395, 0.438802033662796, "The Design Life of the SEOSat Satellite is 7 years."]
[5.618642330169678, 3.7990164756774902, "The Operational Date of the F-DUGS Center is 2010."]
[8.432001113891602, 6.9155802726745605, "The Mounting Location of the CDE Sensor is Top of the spacecraft."]
[9.566145896911621, 3.8749148845672607, "The Formation Ranges of the CanX-5 Satellite is 50 m."]
[6.166292667388916, 1.5391013622283936, "The Symposium Date of the PAZ Satellite is July 26-31, 2015."]
[9.508346557617188, 0.7997351288795471, "The Mission Time of the ROBUSTA picosatellite Satellite is Up to three years."]
[9.470218658447266, 0.8963879942893982, "The Recovery Operation Duration of the STEREO-B Satellite is 22 months."]
[9.859460830688477, 1.3194894790649414, "The Time to Full Control of the Satellite Spacecraft is Three hours."]
[5.7171759605407715, 1.6749330759048462, "The Launch Vehicle of the Beresheet Spacecraft is SpaceX Falcon 9 rocket."]
[9.240278244018555, 2.608834743499756, "The Impact Date of the DART Double Asteroid Redirect Test is Late 2022."]
[11.221330642700195, 6.709501266479492, "The System Focus of the Xona Company is Satellite navigation system."]
[6.561047077178955, 3.394091844558716, "The Mission Type of the Kolibri-2000 Satellite is EO."]
[5.655526161193848, 5.359675884246826, "The Architecture of the SSTI GPS Receiver is Lagrange architecture."]
[5.8547682762146, 8.142889022827148, "The Frequency (GHz) of the ICI-4 Radiometer is 243.2\u00b12.5."]
[8.748169898986816, 10.39052677154541, "The Detector Array of the Payload 2 CMOS Camera is 640 x 480 pixels."]
[10.096302032470703, 1.3996325731277466, "The ECT (Equatorial Crossing Time) of the WV-1 Satellite is 1030 hours on a descending node."]
[7.427133560180664, 8.907258987426758, "The 30 bins in polar angle direction of the Angular Resolution Sensor is Angular resolution 30 bins in polar angle direction."]
[3.4894580841064453, 4.57842493057251, "The Function of the FPGA Code Software is Did not allow the motor to move without a valid home command."]
[5.476716041564941, 3.4384379386901855, "The Manufacturer of the STX Communication Subsystem is Clyde Space."]
[5.655001640319824, 2.4601857662200928, "The Telescope Type of the SBSS Satellite System is Two-axis, gimballed optical telescope."]
[7.21529483795166, 5.589682579040527, "The Function of the Phytoplankton Marine Organism is Absorbing atmospheric carbon dioxide into solution at the sea surface, using carbon dioxide to create their organic biomass via photosynthesis."]
[5.613167762756348, 4.041790962219238, "The Location of the GFZ Data Center is Potsdam, Germany."]
[7.170758247375488, 1.011048436164856, "The Arrival Date of the Electro-L Satellite is February 3, 2011."]
[7.532227516174316, 8.902947425842285, "The Vertical Resolution of the MLS Spectrometer is 3 km."]
[7.747619152069092, 7.794250965118408, "The Absolute Accuracy of the FFRF sensor Metrology Instrument is 1o on LOS."]
[8.197894096374512, 7.144769191741943, "The Absolute Accuracy of the Instrument Sensor is Checked at regular time intervals with stellar calibrations."]
[10.689857482910156, -1.0687661170959473, "The Launch Mass of the GaoJing / SuperView minisatellites Satellite is 560 kg."]
[6.510270118713379, 5.675219535827637, "The GNOS and Radiosonde Refractivity Profile Difference of the GNOS Instrument Occultation Measurement Device is <3%."]
[9.525578498840332, 1.2123656272888184, "The Mission Duration of the Galileo spacecraft Spacecraft is 1995 and 2003."]
[5.256690979003906, 3.9321086406707764, "The Function of the ISSAC SOC Space Operations Center is Receive ISSAC imagery requests."]
[1.085835337638855, 4.314022541046143, "The Batteries of the EPS Electrical Power Subsystem is 2 Rose Li-ion batteries."]
[8.847907066345215, 7.066558837890625, "The Measurement of the SWAP Instrument is Interactions of Pluto with the solar wind."]
[9.810257911682129, 4.542222499847412, "The Manufacturer of the Terminator Tape Deorbit Module Deorbit Device is TUI (Tethers Unlimited Inc.)."]
[5.422453880310059, 2.2596435546875, "The Number of Observations of the Claire Satellite is Over 4000."]
[9.78207778930664, 7.1303510665893555, "The Publication Date of the Supercapacitors Energy Storage is 1999."]
[11.710301399230957, 5.005078315734863, "The Size of the Cygnus A jet Black Hole Jet is One of the largest and most powerful."]
[8.701993942260742, 2.3735556602478027, "The Imaging of the Parker Solar Probe Satellite is Night Side of Venus."]
[6.032957553863525, 3.5541293621063232, "The Development Scope of the Neosat program Satellite Program is In-orbit validation of the new satellite product lines."]
[1.2984044551849365, 4.171319484710693, "The Battery Capacity of the Spacecraft Satellite is 50 Ah."]
[9.147217750549316, 4.220208168029785, "The Shape of the PM Satellite Component is Cylindrical."]
[7.2132463455200195, 4.072947025299072, "The Sensor Data of the PSSCT-2 Satellite is Collected."]
[7.269190788269043, 8.174440383911133, "The IFOV/line (pixels/scan line) of the TOU Total Ozone Unit is 31."]
[8.530360221862793, 6.058274745941162, "The Magnetometer Status of the Solar Orbiter Satellite is Good health."]
[6.319555282592773, 1.0162440538406372, "The Arrival Date in Final Orbit Position of the COSMO-SkyMed-4 Satellite is April 2011."]
[5.080146789550781, 6.054598808288574, "The Antenna of the GIOVE-B Satellite is 42-element planar array."]
[9.90924072265625, 7.366740703582764, "The Heat Transfer of the Cube Corner Reflectors (CCRs) Satellite Component is Mainly governed by radiation."]
[7.69049072265625, 1.401757836341858, "The Demonstration Date of the Space Weather Observation System Observation System is August 18, 2010."]
[8.998820304870605, 4.269684314727783, "The Spacecraft Bus Size of the QuickBird-2 Satellite is 3 m x 1.6 m \u00d8."]
[10.505019187927246, 2.519366502761841, "The Orbit of the BRO-2 and BRO-3 Nanosatellites is Sun-synchronous orbit of 500 km altitude."]
[8.188986778259277, 9.161681175231934, "The Pixel Sampling FWHM of the Instrument Spectrometer is \u22652."]
[3.613543748855591, 6.214816093444824, "The Data Downlink Rate of the SGLS Link Communication System is 1024 kbit/s."]
[4.427657127380371, 4.280989170074463, "The Components of the Recovery Subsystem Subsystem is Inflation devices, floatation devices, localization devices."]
[6.274161338806152, 5.952723979949951, "The Distribution Time of the SAR Data Products Data is ~ 6 months after launch."]
[1.289794921875, 4.1522040367126465, "The Battery Status of the Rumba Satellite is Weak."]
[6.811014175415039, 4.444460391998291, "The Instrument Type of the JPSS-2/NOAA-21 Satellite is Atmospheric chemistry, Atmospheric temperature and humidity sounders."]
[8.249910354614258, 10.190949440002441, "The Resolution of the ALI Imager is 30 m."]
[6.9200286865234375, 5.448425769805908, "The Detection Depth of the SMAP Satellite is Top 5 cm (2 inches) of the ground."]
[8.133214950561523, 9.799949645996094, "The Imaging Mode of the Pushbroom System Imaging System is Continuous."]
[6.195825576782227, 3.572845935821533, "The Satellite Usage of the Surveying System Navigation System is EGNOS and Galileo satellites."]
[9.177376747131348, 3.240462303161621, "The Orbit Type of the Satellite Satellite is Sun-synchronous orbit."]
[5.583375453948975, 4.00782585144043, "The Ground Segment Sections of the Helios-2 Satellite is User ground segment, programming loop."]
[4.961328029632568, 6.160954475402832, "The Frequency (MHz) of the GLONASS L1 OC Signal Carrier is 1575.42."]
[5.010582447052002, 4.95074987411499, "The Design of the Mobile Station Ground Station is Move to an adequate atmospheric condition area."]
[7.101372241973877, 0.4668677747249603, "The Launch Date of the SJ-9 Technology Demonstration Satellite Satellite is Oct. 13, 2012."]
[8.009976387023926, 7.048373699188232, "The Collaboration of the AstroRad vest Radiation Protection is Lockheed Martin."]
[4.157639503479004, 5.626809120178223, "The Performance Evaluation of the Microhard MHX2420 Satellite is Unknown."]
[6.236538410186768, 7.07168436050415, "The Operating Frequency of the ALT Experiment Altimeter is 13.56 GHz."]
[6.286172389984131, 5.8030242919921875, "The Purpose of the SGR-ReSI Satellite Instrument is Sensing the Earth using GNSS Signals."]
[11.13000202178955, 5.34252405166626, "The Performance Requirement of the LISA LTP Interferometer is \u2264 10-15 ms-2 Hz-1/2 in the bandwidth 10-3 to 10-1 Hz."]
[2.953913450241089, 6.69362211227417, "The Transmitter Output Power of the S-band transponder Communication Device is 5 W."]
[10.340452194213867, 2.777085542678833, "The Orbit of the MIMOSA Payload is Elliptical orbit of 820 km x 320 km."]
[8.729232788085938, 1.9167494773864746, "The Additional Evidence Gathering of the Hubble Space Telescope Space Telescope is A few years later."]
[9.592328071594238, 1.0179916620254517, "The Observing Duration of the IMP-8 Satellite is 28 years."]
[5.395292282104492, 3.050665855407715, "The Architecture of the AstroSat-250 Satellite is AstroBus-L."]
[7.079046249389648, 8.803999900817871, "The Spectral Region (Visible Channel) of the VIRR Instrument is 0.49 - 0.94 \u00b5m."]
[11.457616806030273, 5.419536113739014, "The X-ray Light Source of the SS 433 Cosmic Object is Bright."]
[4.937480449676514, 4.670070648193359, "The Number of Weather Centrals in the United States of the IDPS Interface Data Processing Segment is 4."]
[5.7336297035217285, 6.330296516418457, "The Spotlight Scene Centre Wavelength of the SAR Antenna Antenna is 31 mm."]
[6.277791976928711, 0.8534142374992371, "The Launch Date of the OSCAR-QUBE Satellite is 29 August 2021."]
[6.3796000480651855, 5.500324726104736, "The Mission Goals of the ARMADILLO Satellite is 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."]
[8.329204559326172, 3.6443374156951904, "The Separation Status of the BRITE-Montreal satellite Satellite is Did not separate from its Dnepr launch vehicle."]
[11.164495468139648, 9.332879066467285, "The Instrument Pointing Requirements of the Earth Radiation Budget Experiment (ERBE) Instrument is Control Knowledge Stability 720 arcsec 180 arcsec 79 arcsec/6.6 sec."]
[5.093539237976074, 4.188625335693359, "The Function of the COSMOS Mission Operations Tool is 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."]
[9.864452362060547, 1.3789101839065552, "The Ignition Time of the ALOS-3 Satellite is 8:37 p.m. EST."]
[3.2548553943634033, 5.613739967346191, "The Size of the Processed Science Data Packet Data Packet is 60 bytes."]
[3.4475619792938232, 4.898406982421875, "The Mass of the Spacecraft 406 MHz Processor Processor is 27.5 kg."]
[7.465112209320068, 5.7084245681762695, "The Direction of the Japan Current Ocean Current is North."]
[7.038113594055176, 4.483156681060791, "The Imager Type of the ResourceSat-2 Satellite is Multispectral pushbroom scanners."]
[5.137883186340332, 1.8274959325790405, "The Constellation Expansion Plan of the ICEYE Company is More satellite additions later this year."]
[9.35859203338623, 5.956957817077637, "The Coverage of the SpinKF Attitude Determination System is Every orbit perigee-to-perigee."]
[8.482074737548828, 2.1826353073120117, "The Launch Site of the Herschel Telescope Telescope is Kourou."]
[6.934317588806152, 3.9352309703826904, "The Measurement Type of the GRACE-FO Satellite is Groundwater Storage and Root Zone Soil Moisture."]
[9.884654998779297, 3.1991829872131348, "The Altitude of the ICEYE-X1 Satellite is 505 km."]
[5.640475749969482, 1.625727891921997, "The Launch Vehicle of the CANYVAL-X CubeSats CubeSats is PSLV-40 flight vehicle (XL configuration) of ISRO."]
[5.981818675994873, 6.267280101776123, "The SAR Payload Mass of the RCM Satellite is Approximately 600 kg."]
[4.068445682525635, 10.275202751159668, "The NE\u0394T of the Satellite Device Unknown is 1.0 K."]
[7.629290580749512, 4.90399694442749, "The Multi-function component assembly of the BEESAT-2 Satellite is Yes."]
[9.667215347290039, 5.977690696716309, "The Attitude Jitter of the ADCS Attitude Determination & Control Subsystem is \u2264 0.28 \u00b5rad, 0.1-1.0 Hz."]
[7.581457614898682, 5.358506679534912, "The Model Intercomparison Project (MIP) of the OCO-2 Satellite is Organized by the OCO-2 Science Team."]
[11.209076881408691, 2.800842761993408, "The Height of the Cliff Geological Feature is 50 m."]
[9.952804565429688, 6.3188347816467285, "The Temperature of the Tank B2 Fuel Tank is Increased."]
[7.400320053100586, 5.116505146026611, "The Incident Spectral Passband Wavelength of the GHGSat-D Satellite is 1600-1700 nm."]
[5.384754180908203, 6.211187839508057, "The Antenna Orientation of the GPS Reflectometry Receiver Instrument is Zenith side and Nadir side."]
[8.127008438110352, 8.441184997558594, "The Nominal Value for L of the Michelson Interferometer Interferometer is Given in the table."]
[10.551255226135254, -1.0641916990280151, "The Total Mass of the Microsatellite Satellite is 40 kg."]
[7.625138759613037, 1.3452720642089844, "The Launch Date of the LADEE Satellite is September 7, 2013."]
[11.831581115722656, 1.031411051750183, "The URL of the Chang'E-1 Lunar Probe is http://www.cjss.ac.cn/qikan/manage/wenzhang/2008-05-03.pdf."]
[4.664544105529785, 6.634766101837158, "The Function of the MC34072 Amplifier Amplifier is Controls the gain of the intermediate amplifier."]
[10.761434555053711, 3.6355042457580566, "The Data Stack Height of the Hubble Space Telescope is About 5,000 miles (8,000 km) high."]
[17.7283878326416, 7.162808418273926, "The J2000 declination (deg) of the B1617-155 (Sco X-1) Pulsar is -15.640."]
[3.5853617191314697, 6.583489894866943, "The Rate of the Data Output to X-band Transmitter Data Handling System is 30.72 Mbit/s."]
[8.146150588989258, -0.6779391765594482, "The Deorbit Burn Duration of the Crew Dragon spacecraft Resilience Spacecraft is 50 minutes."]
[8.86823558807373, 6.999377250671387, "The Purpose of the SWIPS Plasma Sensor is Measure the properties of solar wind ions originating from the Sun."]
[3.313464403152466, 5.32058572769165, "The HSDR Capacity of the SSTL-100 Satellite is Up to 48 GByte."]
[1.4350913763046265, 4.698976516723633, "The Voltage of the Battery Energy Storage is 28 V."]
[7.186008453369141, 4.289821624755859, "The Sensor complement / remarks of the Meteor-1-2 Satellite is TV, IR, AC."]
[6.103066444396973, 5.087613582611084, "The Journal Article of the GPS-aided Automatic Landslide Monitoring System Monitoring System is 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."]
[4.089782238006592, 6.6192216873168945, "The FIFO Buffer of the X-band transmitter Transmitter is On-board."]
[8.419702529907227, 4.504286289215088, "The Ground Sample Distance of the Carbonite-1 Satellite is 1 m."]
[4.890735626220703, 4.311980247497559, "The Communication Changes Article of the Optical Inter-orbit Communications Engineering Test Satellite (OICETS) Satellite is Takashi Jono."]
[7.483278751373291, 1.3009454011917114, "The Testing Completion Date of the Parachute System Spacecraft Component is Unknown."]
[8.878668785095215, 7.045992374420166, "The Mission Objectives of the MiniCOR Instrument is Improved measurements of CME kinematics and CME-shock standoff distance, Analysis of small-scale structures in the corona and solar wind."]
[9.454505920410156, 9.970937728881836, "The Interface of the Google Earth Application is ActiveX server interface."]
[6.445611953735352, 4.238647937774658, "The Services of the MTSAT Satellite is Aeronautical communications and navigation, and meteorological observations."]
[7.57001256942749, 3.612682580947876, "The Imagery Remapping Goals of the Satellogic Satellite Company is Weekly remapping of the entire globe with high-resolution imagery in 2023, daily remapping when the full constellation is in place in 2025."]
[9.158767700195312, 4.2265400886535645, "The Bus Structure Dimensions of the EURECA Spacecraft is 4.6 m x 2.6 m."]
[11.4358549118042, 4.434237003326416, "The Study Date of the Stardust Grain Particle is Last year."]
[6.742456436157227, 8.046238899230957, "The Pulse Frequency of the Laser Instrument is 500 Hz ~ 10 kHz."]
[6.008874416351318, 9.553664207458496, "The Mass of the Instrument Device is 600 g."]
[7.771088123321533, 7.3125410079956055, "The Noise Levels of the SOFIE Instrument is At or below laboratory values."]
[8.108258247375488, 10.141575813293457, "The Swath of the DMC-2G imager Imager is >600 km."]
[9.433999061584473, 5.075563907623291, "The Spin of the Satellite Satellite is Up to 5 rpm."]
[4.046999454498291, 5.618337154388428, "The Dual X-band Links Speed of the NigeriaSat-2 Satellite is 105 Mbit/s."]
[4.9152512550354, -3.238431930541992, "The | of the Herbert Gunell, Charlotte Goetz, Cyril Simon Wedlund, Jesper Lindkvist, Maria Hamrin, Hans Nilsson, Kristie Llera, Anders Eriksson and Mats Holmstr\u00f6m Researchers is | False."]
[6.269903182983398, 1.1281274557113647, "The Mission Status Presentation of the COSMO-SkyMed Satellite is EUSAR 2018 (12th European Conference on Synthetic Aperture Radar), Aachen, Germany, June 4-7, 2018."]
[9.441944122314453, 9.990147590637207, "The Camera Properties of the Google Earth Application is Focus point, range, tilt, azimuth."]
[8.943873405456543, 2.1531283855438232, "The Data Resolution Improvement of the New Horizons Spacecraft is Ten times."]
[8.537505149841309, 10.393813133239746, "The Detector of the Instrument CCD Imaging Camera is E2V CCD67."]
[6.096724510192871, 9.090777397155762, "The Instrument Mass of the JPL Microwave Radiometer Radiometer is 7 kg."]
[5.768309116363525, 3.550445795059204, "The Prime Contractor of the FGS Science Instrument is COM DEV Space Systems of Ottawa Canada."]
[8.974889755249023, 8.489776611328125, "The Scanning Method of the OCTS Sensor is Mechanical rotating with a mirror."]
[10.321622848510742, 4.946976661682129, "The Design of the Resistojets Propulsion System is Simple design consisting of a resistive wire wound round a mandrel."]
[8.698652267456055, 3.193434715270996, "The Contribution of the GOCE Satellite is Map changes in gravity over time."]
[4.367518424987793, 3.250321865081787, "The Program Name of the Satellite for 5G Satellite is Satellite for 5G (S45G)."]
[8.322998046875, 8.544517517089844, "The Detector of the Spectral Band A Spectrometer is Si-PIN."]
[7.729069232940674, 1.0230133533477783, "The Launch Date of the Sentinel-5P Satellite is Planned for the timeframe 2020."]
[5.304149627685547, 1.905136227607727, "The Satellite Configuration of the OptiSAR\u2122 Constellation Satellite Constellation is 8 X- and L-band SAR satellites and 8 high-resolution optical satellites."]
[11.298519134521484, 3.5470504760742188, "The Large Lobe Dimensions of the Comet Celestial Body is 4.1 x 3.3 x 1.8 km."]
[5.11369514465332, 7.578489780426025, "The Measurement Speed of the OLA Instrument is Up to 10,000 measurements/s."]
[9.107659339904785, 4.457570552825928, "The Effective Active Area of Solar Arrays of the CHEOPS Satellite is Just over 2.1 m2."]
[10.236974716186523, 4.831529140472412, "The RCS Thrust of the ARTEMIS Spacecraft is 10 N."]
[8.889227867126465, 9.123571395874023, "The FOVs of the CrIS Instrument is 9."]
[5.941614627838135, 1.9215675592422485, "The Launch Vehicle of the Atlas V Rocket is Atlas V."]
[6.3247904777526855, 1.7690868377685547, "The ADS-B Messages Received of the Aireon Air Traffic Surveillance System is 6,935."]
[9.33872127532959, 9.708395957946777, "The Purpose of the EUV Camera Observation Device is Observe Earth's plasmasphere."]
[8.702999114990234, 0.20785170793533325, "The Duration of Human Presence of the International Space Station Space Station is More than 18 years."]
[9.265387535095215, 0.9800223112106323, "The Design Lifetime of the ERBE Instrument is 3 years."]
[11.741134643554688, 1.2026275396347046, "The Sample Collection Time of the Chang'e-5 Lander Lander is 20 hours."]
[4.891063213348389, 12.09827709197998, "The Responsivity Requirement of the Responsivity Measurement Instrument is >1.05 A/W."]
[9.320043563842773, 0.6672611236572266, "The Design Lifetime of the RapidEye Satellite Constellation is 7.25 years."]
[2.3031222820281982, 4.476848602294922, "The Power Consumption of the Satellite Satellite is < 5000 W (BOL) and 4500 W (EOL) without EPPS operation in GEO."]
[9.8347806930542, 1.69304358959198, "The Mission Aim of the TIMED Satellite is Provide a better understanding of the properties of energy and its redistribution in the Mesosphere and Lower-Thermosphere/Ionosphere (MLTI) region."]
[7.522805690765381, 2.95290470123291, "The Applications of Data of the KOMPSAT-2 Satellite is Unknown."]
[4.737074851989746, 7.2246174812316895, "The Passes per Day of the GimmeRF Radio Instrument is About two."]
[9.421594619750977, 1.268822431564331, "The Number of Profiles/Hour of the Aeolus Satellite is 100."]
[2.304889440536499, 4.440773010253906, "The Background Energy Consumption of the FLP Satellite is 40 W."]
[10.178691864013672, 3.1472208499908447, "The TGF Altitude of the RHESSI Satellite is Around 15 km."]
[9.461219787597656, 0.8809686303138733, "The Estimated Mission Duration of the Spacecraft 3U CubeSat is \u2264 1 month."]
[7.379347324371338, 3.422450065612793, "The Sensor Complement of the CXBN-2 Satellite is Unknown."]
[5.035752296447754, -2.371629238128662, "The Affiliation of the Jonathan Gebbie Engineer is Unknown."]
[11.166122436523438, 4.056589126586914, "The URL of the TOI-178 Exoplanet System is https://arxiv.org/pdf/2101.09260.pdf."]
[7.477766036987305, 6.94075345993042, "The Measures of the WAF-P Device is Vertical column densities of CO2 and CH4."]
[3.891550064086914, 2.30734920501709, "The CubeSat Size of the RadFxSat Satellite is 1U."]
[9.988608360290527, -0.7383481860160828, "The Size of the SERB Nanosatellite Satellite is 10 x 10 x 33 cm."]
[6.941503047943115, 3.2823636531829834, "The Mission Status of the SPOT-5 Satellite is Mission complete."]
[6.750512599945068, 1.1900938749313354, "The Funding Date of the BRITE Satellites Satellite is January 2011."]
[7.12817907333374, 1.3394432067871094, "The Presentation Date of the ERG Satellite Satellite is Oct. 3-7, 2011."]
[5.3767170906066895, 4.682384014129639, "The Operational Parameters of the ICPS Upper Stage is 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."]
[9.053665161132812, 10.247126579284668, "The IFOV of the LWIR Camera Camera is 143 \u00b5rad."]
[8.559486389160156, 6.604673385620117, "The Height of the Magnetic Bottle-like Structure Magnetic Field Structure is Nearly 20,000 kilometers."]
[9.319113731384277, 3.2638297080993652, "The Orbit Type of the Explorer 36 Satellite is Elliptical polar retrograde orbit."]
[6.960123538970947, 0.8239494562149048, "The Communication Loss Date of the STEREO-B Satellite is Oct. 1, 2014."]
[6.574779510498047, 5.230961799621582, "The Mission Features of the TerraSAR-X NG Satellite is Full polarimetry and improved near-real-time capabilities."]
[9.334790229797363, 1.1019212007522583, "The Data Analysis and Validation Duration of the GP-B mission Mission is Approximately 1 1/2 years."]
[7.502130031585693, 0.14839810132980347, "The Maiden Flight Date of the Automated Transfer Vehicle Spacecraft is March 9, 2008."]
[8.44452953338623, 3.393325090408325, "The Orbital Height of the Tandem-L Satellite is 745 km."]
[10.241913795471191, 2.92406964302063, "The Orbit Altitude of the HY-2B Satellite is 963 km."]
[6.26616096496582, 2.7968697547912598, "The Role of the Jared Isaacman Crew Member is Mission Commander."]
[6.538641929626465, 6.274819850921631, "The Data Product Grids of the OSCAT-2 Instrument is 25 km and 50 km."]
[6.864662170410156, 4.911444664001465, "The Monitoring of the Copernicus Sentinel-4 and Sentinel-5 Satellite Missions is Key air quality trace gases, stratospheric ozone, and aerosols."]
[7.906371116638184, 0.7024335861206055, "The Landing Date of the Starliner Spacecraft is 22 December 2019."]
[11.520610809326172, -1.292020559310913, "The Weight of the SPOT satellite constellation Satellite Constellation is 1869 kg."]
[1.2794173955917358, 4.246800899505615, "The Power Source of the Telemetry System System is Non-rechargeable battery."]
[9.216904640197754, 10.115177154541016, "The Manufacturer of the LISS-II Camera Imaging Device is ISRO."]
[9.385234832763672, 5.915132522583008, "The Gyros, magnetometers, sun sensors, magnetorquers of the Spacecraft Attitude Determination and Control System is Attitude sensors on board are the gyros, magnetometers and sun sensors (or photodiodes), while the only actuators are magnetorquers."]
[12.15327262878418, 5.4076714515686035, "The Expansion of the Universe Cosmological Entity is Not Uniform."]
[6.0982666015625, 9.010293960571289, "The Mass of the MIS Instrument Microwave Radiometer is 475 kg."]
[4.6478142738342285, 5.782081127166748, "The RF Communications Radios of the Neutron-1 Spacecraft is Gamalink Radio, GlobalStar radio, GlobalStar simplex radio."]
[4.837828159332275, -3.3861215114593506, "The Member of the Phil Townsend Individual is True."]
[5.065169811248779, 1.9350471496582031, "The P-PODs Quantity of the Secondary Payloads Nanosatellites and CubeSat is 4."]
[7.147031784057617, 5.794358730316162, "The Wind Speeds of the Global Models Weather Model is Higher than 20 m/s."]
[10.169151306152344, 9.365954399108887, "The Methane Detection Resolution of the Iris Satellite is 25 m on the ground."]
[3.225297212600708, 5.1086955070495605, "The Non-volatile Memory of the Frame Grabber Storage is Sufficient on-board non-volatile storage."]
[11.364631652832031, 3.9073410034179688, "The Orbital Periods of the TRAPPIST-1 Star System is 1.5 to 20 Earth days."]
[8.917243957519531, 8.008317947387695, "The Designer of the BGO Calorimeter Detector is Prof. LIU Shubin from USTC."]
[9.861655235290527, -0.5853749513626099, "The Orbit Inclination of the BX-1 Microsatellite is 42.4\u00ba."]
[7.306504249572754, 0.3126662075519562, "The Launch Date of the Carruthers Geocorona Observatory (GLIDE) Satellite is 2025."]
[9.664498329162598, 9.013474464416504, "The Height of the TOGS Telescope is 3.5 m."]
[4.986659049987793, 4.732483386993408, "The Data Transmission of the McMurdo Ground Station Ground Station is Darmstadt."]
[7.740159034729004, 3.661999464035034, "The Source of Scatter for L\u03b1D of the IMAP Satellite is Dim unresolved stars."]
[7.18328332901001, 7.379300594329834, "The Mission Heritage of the POLDER-P Instrument is ADEOS and ADEOS-II."]
[8.292134284973145, 10.064997673034668, "The Spacing Between Consecutive Lines of the MS Bands Detector Line Arrays is 936 \u00b5m."]
[6.828296661376953, 3.1579339504241943, "The Mission Status of the Eutelsat 172B Satellite is Entered full commercial service."]
[6.138490676879883, 4.776791095733643, "The Direct Data Reception Locations of the TerraSAR-X Satellite System is US, Japan, and Germany."]
[9.208830833435059, 10.323237419128418, "The Type of the DECA Camera is Descent."]
[4.068798065185547, 5.796676158905029, "The S-band 1Mbit/s Downlink of the UoSAT-12 Satellite is 1."]
[6.927465438842773, 5.94642972946167, "The Development Period of the Neutrally Buoyant Floats Oceanographic Instrument is Mid-1950s."]
[9.470088005065918, -0.7532421946525574, "The Release Date of the DIWATA-1 Microsatellite is Spring."]
[3.8193235397338867, 0.2830352485179901, "The Publication Date of the Gravity Recovery and Interior Laboratory (GRAIL) Mission is 2013 Feb 8."]
[8.086073875427246, 2.7136998176574707, "The Data Supply Agreement of the TerraSAR-X Satellite is Until the end of 2020."]
[10.513298034667969, 7.4237284660339355, "The Material of the Main Tank Propulsion Subsystem is Ti."]
[7.862290859222412, 8.43652057647705, "The Measurement Interval of the FTS Fourier Transform Spectrometer is Approximately every two minutes."]
[7.061684608459473, 0.48572254180908203, "The Launch Date of the Genesis Satellite is August 8, 2001."]
[8.260430335998535, 9.747319221496582, "The Camera Types of the Optical Payload Imaging System is One in the VNIR (Visible Near Infrared) range and two imagers in the infrared region."]
[7.143634796142578, 6.313427448272705, "The Laser-Illuminated Area Movement Time of the Spectral Bands Measurement Device is Corresponding to the desired mapping resolution of water ice (10 km or less)."]
[2.179328441619873, 4.4513115882873535, "The Power Supply for ISM Release of the Satellite Spacecraft is Two activations."]
[7.847105503082275, 10.012094497680664, "The Technology of the VNIR Range Imaging System is Photodiode-silicon readout."]
[9.177284240722656, 10.82895565032959, "The Distance from Mercury of the Monitoring Camera 3 Camera is 2687 km."]
[8.482471466064453, 9.028663635253906, "The Displacement Range of the Piezo Instrument is \u00b16 \u00b5m (\u00b11 arcmin)."]
[5.2114644050598145, 1.2231510877609253, "The Payload Capacity of the Terran R Launch Vehicle is More than 20,000 kg."]
[7.450469493865967, 0.06519845128059387, "The Launch Date of the SAOCOM-1A Satellite is 2015."]
[7.108458995819092, 1.8273932933807373, "The Conference Date of the Tandem-L SAR System is June 4-7, 2018."]
[8.164297103881836, 5.623607635498047, "The On Orbit Noise Power of the RAX-1 Satellite is -113 dBm."]
[8.750537872314453, 7.818018913269043, "The Purpose of the MIPA Ion Mass Analyzer is Provide monitoring of the precipitating ions."]
[7.949949264526367, 9.208324432373047, "The Bands of the Spectral Bands Spectrometer is SWIR, MWIR, TIR."]
[6.7690863609313965, 2.3633460998535156, "The URL of the PSLV Satellite is 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."]
[7.8459625244140625, 7.008655071258545, "The Unknown of the MAXI/SEDA Experiment is Unknown."]
[8.54447078704834, 5.947404861450195, "The Paper Title of the Nikolai A. Tsyganenko Researcher is Data-based modeling of the geomagnetosphere with an IMF-dependent magnetopause."]
[7.09931755065918, 0.49765050411224365, "The End of Operations of the Resurs-P1 Satellite is 2021."]
[7.125357151031494, 3.8538224697113037, "The Remarks/Sensors of the OrbView-1 Satellite is GPS."]
[10.425856590270996, 3.365464687347412, "The Autonomous Abort Response Distance of the ASTRO Satellite is 120 m."]
[9.316454887390137, 0.6024115085601807, "The Mission Planned Life-cycle of the SAMPEX Satellite is Three years."]
[8.629252433776855, 10.268641471862793, "The Array Size of the Camera Sensor Imaging System is 578 x 576 array."]
[7.185810089111328, 10.131340980529785, "The Instrument Mass of the HySI Hyperspectral Imager is 4 kg."]
[10.294231414794922, 5.192582130432129, "The Function of the XFS Xenon Gas System is Stores xenon gas in a high pressure vessel and provides the xenon gas for the thruster head."]
[5.27419900894165, 2.659571409225464, "The Role of the UNM (University of New Mexico) team Organization is Integrators of the CubeSat."]
[9.123396873474121, 8.00307846069336, "The Hamamatsu PMTs of the Range Calorimeter Particle Detector is 2 per plane."]
[8.648770332336426, 4.152313232421875, "The Filter of the BRITE Telescope is Different from Another BRITE Satellite."]
[6.457683086395264, 2.801401138305664, "The Managing Office Location of the Lucy Discovery Program Mission is NASA's Marshall Space Flight Center in Huntsville, Alabama."]
[11.176011085510254, 6.820673942565918, "The Time Resolution of the X-ray Satellite Navigation Navigation System is 1 \u00b5s."]
[10.251867294311523, 7.0219807624816895, "The Back Plate Coating of the Thermal Control Louvers Thermal Regulation Device is Highly emissive coating."]
[8.030536651611328, 9.714615821838379, "The Operating Mode of the CIRiS Infrared Imaging System is Pushbroom."]
[11.45807933807373, 2.1962954998016357, "The Edge Design of the Hayabusa-2 Sampler Horn is Folded back inward."]
[5.081773281097412, 5.521233081817627, "The D-STAR Capability of the OUFTI-1 Satellite is Provides a repeater functionality to any D-STAR equipped ham-radio operator."]
[8.202595710754395, 1.8162721395492554, "The Mission Status of the Rosetta Spacecraft is Active."]
[10.512298583984375, 6.180752277374268, "The Purpose of the RHESSI Satellite is Imaging spectroscopy of hard X-ray (HXR) and gamma-ray continua emitted by energetic electrons, and gamma-ray lines produced by energetic ions."]
[5.124201774597168, 1.8319518566131592, "The Type of the ELaNa X Payload is 3 P-PODs (Poly Picosatellite Orbital Deployers) containing a total of four CubeSats."]
[8.534717559814453, 8.749682426452637, "The Grating Figure of the Short Wavelength Band Spectrometer is Ellipse of rotation."]
[9.276686668395996, 6.482745170593262, "The Sensor Type of the Astro-APS Star Tracker is CMOS Active Pixel Sensor."]
[9.119901657104492, 3.3799471855163574, "The Purpose of Orbit Parameters of the LAGEOS Satellite is Minimizing the effects of disturbing forces."]
[9.916624069213867, 1.5885472297668457, "The Time to Scan a Full Disk of the GK-2A Satellite is About one-fifth of the current 28 minutes."]
[9.130002975463867, 5.436194896697998, "The Attitude Control Error of the ETS-VIII LRRA Satellite is Roll (< \u00b10.05\u00ba), Pitch (< \u00b10.05\u00ba), Yaw (< \u00b10.15\u00ba)."]
[5.655728816986084, 7.538969993591309, "The Physical Baseline Length of the KaRIn Instrument is 10 m."]
[11.606717109680176, 4.428955554962158, "The Rotation Period of the Kepler 11145123 Star is Three times more slowly than the Sun."]
[7.392723083496094, 6.861213684082031, "The Installation Date of the DESIS Instrument is July 2, 2018."]
[7.671864986419678, 4.553354740142822, "The Tracking Direction of the NEOSSat and Sapphire Satellites is Antisolar direction."]
[6.316894054412842, 2.319807767868042, "The Missions of the Altimetry Satellites Satellites is TOPEX/Poseidon (1992-2006), Jason-1 (2001-2013), Ocean Surface Topography Mission/Jason-2 (2008-2019), and Jason-3 (2016 to present)."]
[6.272191524505615, 2.1542272567749023, "The Partner Responsibilities of the Jason-2 Satellite is 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."]
[8.631708145141602, 2.0081944465637207, "The 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 Astronomers is 28 February 2020."]
[6.115217685699463, 2.6355645656585693, "The Cooperative Research and Development Agreement Partner of the SpaceX Company is U.S. Space Force."]
[8.895501136779785, 5.386610984802246, "The Robotic Arms Function of the Satellite Platform is Orientation of the satellite's electric propulsion thrusters and to control thrust direction and attitude."]
[5.547247409820557, 2.975994348526001, "The Task of the Restore-L Satellite is Manipulate its fill and drain valve."]
[10.075725555419922, 7.7195820808410645, "The Structure of the Sojourner 2020 Art Payload is Three-layer telescoping structure."]
[4.51456356048584, 4.8139214515686035, "The Function of the DPP Signal Processing Device is Digitizes the preamplifier output, applies real-time digital processing to the signal, detects the peak amplitude, and bins this in its histogram memory."]
[11.155081748962402, 2.8905797004699707, "The Diameter of the South Pole-Aitken Basin Impact Region is Roughly 2,500 km."]
[5.000645160675049, 3.5367584228515625, "The Disaggregation Capability of the Cellular Satellite Architecture Satellite Architecture is Allows the disaggregation of typical space vehicles into as many or as few cardinal pieces (called satlets) as required."]
[6.6342597007751465, 2.0381953716278076, "The Observation Location of the ENVISAT satellite Satellite is Luzon Strait."]
[9.073171615600586, 3.253661870956421, "The Orbit Type of the DSX spacecraft Satellite is Elliptical MEO."]
[7.209224224090576, 5.744562149047852, "The Wind Random Errors of the Aeolus Satellite is Compliant to the mission requirements in the free troposphere for the Mie channel for laser output energies above about 65 mJ."]
[9.816575050354004, 9.421883583068848, "The Aperture Diameter of the IRIS Instrument Spectral Scanner is 120 mm."]
[7.906318187713623, -0.07063242048025131, "The Number of Docking Ports of the Prichal Module Docking Port is 5."]
[9.285266876220703, 1.0730870962142944, "The Cryogen Lifespan of the Instrument Dewar/Heat Exchanger is 15 months."]
[2.210108995437622, 1.7311339378356934, "The CCSDS ID of the GSAT-0102 Satellite is 3A6."]
[12.123427391052246, 3.2769720554351807, "The Inclination of the Anand Satellite is 97.4\u00b0."]
[6.01317024230957, 2.675334930419922, "The Ownership of the TecSAR Satellite is Government owned."]
[8.62404727935791, 9.188057899475098, "The Slit Width of the Short Wavelength Band Spectrometer is 150 \u00b5m."]
[7.797541618347168, 10.870497703552246, "The Data Quantization of the Instrument Satellite Instrument is 10 bit."]
[8.385008811950684, 9.281442642211914, "The FWHM at 40 nm of the EUV Simulation Simulation is 5.1 arcmin."]
[9.534540176391602, 0.5379258990287781, "The Design Life of the Satellite Spacecraft is 3-5 years."]
[11.644706726074219, 4.506418704986572, "The Material Collision Speed of the Cassiopeia A (Cas A) Supernova Remnant is 10 million miles per hour."]
[7.881284236907959, 9.771659851074219, "The Spectral Range of the Instrument Spectral Imager is 3.92-4.64 \u00b5m."]
[4.6633148193359375, 4.326878070831299, "The Database of the Payload Data Processing Software is MongoDB."]
[6.9798126220703125, 0.8757686614990234, "The Establishment Date of the MERSEA Project is January 2003."]
[6.77139139175415, 6.986166954040527, "The Development Status of the ALTIKA Instrument is Unknown."]
[8.082234382629395, 9.453351020812988, "The Wavelength Range of the PAN Detector is 0.50 - 0.90 \u00b5m."]
[9.267359733581543, 6.540596008300781, "The Number of Star Images of the Star Tracker Optical Sensor is One or two."]
[11.543490409851074, 4.195999622344971, "The Diameter of the Ceres Dwarf Planet is 950 km."]
[7.334684371948242, 0.6727856993675232, "The News Date of the SCD-2 Satellite is Dec. 17, 2014."]
[9.425699234008789, 5.777432918548584, "The Control Devices of the Attitude Control Subsystem Attitude Control System is Reaction wheels and magnetic torquers."]
[7.563688278198242, 0.49713262915611267, "The Installation Date of the Bartolomeo Platform is 2 April 2020."]
[3.5029640197753906, 5.848849296569824, "The Data Rate from OBC to FPGA of the Transmission Module FPGA Module is 10 Mbit/s."]
[4.900322437286377, 3.518246650695801, "The Bays of the Bus Structure Satellite Component is 9."]
[7.682549476623535, 2.523202419281006, "The Mission Type of the Hera Space Probe is Rendezvous with a binary asteroid system."]
[8.42288875579834, 3.3943099975585938, "The Orbital Tube Diameter of the Tandem-L Satellite is 500 m."]
[5.570773601531982, 3.8915460109710693, "The Location of the F-DUGS Center is France."]
[6.5239033699035645, 0.5445273518562317, "The Re-entry Date of the AeroCube-3 Satellite is January 6, 2011."]
[5.960318565368652, 8.576183319091797, "The Spatial resolution at nadir of the MWTS Microwave Temperature Sounder is 50/75 km."]
[8.916293144226074, 3.7799575328826904, "The Formation of the MMS Satellite is Four spacecraft flown around Earth in a pyramid formation."]
[10.148740768432617, 7.870140075683594, "The TEC of the X123-SDD X-ray Spectrometer is Active 2 stage."]
[10.059337615966797, 6.9968061447143555, "The Effective Emissivity of the MLI Thermal Control Device is \u03b5 < 0.05."]
[11.6207914352417, 0.7854333519935608, "The Chang'e 5 Weight of the Chang'e-5 Lunar Mission is 8.2 metric tons."]
[8.816125869750977, 6.448925018310547, "The Abundance in Plasmasphere of the He+ ions Ion is Up to 15% of the total plasma density."]
[7.115679740905762, 2.52817964553833, "The URL of the SwissCube Satellite is https://phys.org/news/2016-09-swisscubeseven-years-space.html."]
[5.329504013061523, 9.593478202819824, "The Timing Accuracy of the STOs and STAEs Analog Electronic units is \u00b11 \u00b5s."]
[3.222136974334717, 5.235869407653809, "The Capacity of the Memory Data Acquisition System is 50 GB."]
[9.424493789672852, 5.774847507476807, "The Momentum Capacity of the Reaction Wheels Attitude Control is 80 mNms."]
[5.761410236358643, 2.773317813873291, "The Manufacturer of the TecSAR Satellite is Israel Aerospace Industries Ltd (IAI)."]
[6.918573379516602, 1.2609981298446655, "The SpaceOps 2010 Conference Date of the Resourcesat-1 Satellite is April 25-30, 2010."]
[12.143142700195312, 5.403182029724121, "The Normal Matter Percentage of the Universe Cosmology is Under 5%."]
[11.966290473937988, 3.3808395862579346, "The Inclination of the BeaverCube Satellite is 51.6\u00b0."]
[8.91274356842041, 5.264545917510986, "The Attitude Control Accuracy of the Spacecraft Satellite is < 1.0\u00ba."]
[6.507307052612305, 2.664430856704712, "The URL of the Galileo Satellite System is http://m.esa.int/Our_Activities/Space_Engineering_Technology/Combined_orbital_Galileo-GPS_position_fix_achieved_aboard_ISS."]
[10.104276657104492, 5.126693248748779, "The Test Location of the Power Subsystem Satellite Subsystem is Thruster manufacturer's vacuum chamber."]
[7.3271002769470215, 1.4398870468139648, "The Status Report Date of the Space Situational Awareness System is Oct. 8, 2015."]
[9.241419792175293, 4.21023416519165, "The Diameter at the Base of the Nimbus-7 S/C Satellite is 1.52 m."]
[7.939914703369141, 0.23030073940753937, "The Structure Assembly Time of the CXBN-2 Spacecraft is Months rather than years."]
[6.70106840133667, 7.608058452606201, "The Low-Energy Transmitter Range of the OLA LIDAR Instrument is 500 m to 1 km."]
[5.809690952301025, 6.826847076416016, "The Bandwidth of the Radar Radar is 5 MHz."]
[7.720921516418457, 4.10713005065918, "The Number of HTS Experiments of the HTSSE-II cryogenic subsystem Cryogenic Subsystem is 8."]
[8.49463939666748, 8.69597339630127, "The Components of the Offner Spectrometer Optical System is Relay mirror and a spherical convex diffraction grating."]
[7.524316787719727, 4.798551559448242, "The Justification of the ACE Satellite is Better understand the consequences of the declining phase of the solar cycle and a very low solar minimum."]
[9.513358116149902, -0.6772045493125916, "The Affiliation of the ALMASat Microsatellite is University of Bologna."]
[5.866298675537109, 3.6217470169067383, "The Control Location of the FORTE Satellite is Sandia Labs."]
[7.286252498626709, -0.4371177554130554, "The Starlink Satellites Launch Date of the SpaceX Company is 16 February 2021."]
[3.63065505027771, 6.5133891105651855, "The Command Data Rate of the S-band transponder Communication Device is 2 kbit/s."]
[11.53121280670166, -0.9945905208587646, "The Total Mass of the DSX Spacecraft Payload Module Satellite is 600 kg."]
[8.440176963806152, 3.366844654083252, "The Horizontal Baselines of the Tandem-L Satellite is 1 km to 18 km."]
[2.2090604305267334, 1.730944275856018, "The Targets of the GSPC Instrument is 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."]
[7.067348003387451, 1.5065995454788208, "The Conference Presentation Date of the THEMIS Satellite is Aug. 8-11, 2005."]
[2.0258922576904297, 4.024785041809082, "The Photoresistor of the Solar Panel Power System is Mounted to its outer face."]
[11.644128799438477, 2.599299907684326, "The Diameter of the Bennu asteroid Asteroid is 525-m."]
[6.316279411315918, 10.037689208984375, "The Instrument Mass of the EIC Camera is 2.5 kg."]
[10.316164016723633, 2.9210751056671143, "The Orbit Altitude of the CubeSats Satellite is 550 km."]
[11.658866882324219, 1.8606866598129272, "The Separation Time from Hayabusa-2 of the MASCOT Lander is 03:58 CEST."]
[9.400811195373535, -0.5404924750328064, "The Communication Protocol of the Nanosatellite Satellite is Bluetooth."]
[7.627493381500244, 7.115339279174805, "The Principal Investigator of the GIADA Contamination Monitor is Luigi Colangelo."]
[8.529706001281738, 7.100187301635742, "The Function of the ISIS Instrument is Provide access to the nominal direction of the Parker Spiral magnetic field."]
[5.318634510040283, 5.903125762939453, "The Antenna of the Phoenix GPS Receivers GPS Receiver is L1/L2 antenna."]
[10.428299903869629, 4.923792839050293, "The Output of the HET-X Hall-effect Thruster is 20 - 150 millinewtons."]
[3.64667010307312, 6.238399505615234, "The Uplink Lock Time of the LLCD PAT Systems Communication System is Within seconds."]
[8.441831588745117, 3.83414888381958, "The Orbit of the EnviSat Satellite is Not provided."]
[3.233846664428711, 4.872656345367432, "The Microcontroller Flash Memory of the CC430 SoC System on Chip is 32 kB."]
[3.848991870880127, 6.425786018371582, "The Locking Time of the Carrier Offset Frequency Frequency is T0+84 s."]
[10.273905754089355, 3.488081455230713, "The Eccentricity of the SMART-1 Satellite is 0.359146."]
[9.505831718444824, -0.6943174600601196, "The Design Presentation Date of the Microsatellites Satellite is Oct. 10, 2002."]
[5.844515800476074, 6.688281059265137, "The Subswaths of the C-RADAR Phased Array Antenna System is 4 C-band subswaths."]
[4.611834526062012, 2.579582929611206, "The Antennas of the SOURCE 3U CubeSat Satellite is 2."]
[1.879898190498352, 4.034912109375, "The Power Area of the Solar Panels Power Source is 80 square meters."]
[7.0379204750061035, 1.0793126821517944, "The Product Announcement Date of the Spire Global Satellite Operator is September 11, 2019."]
[3.6654317378997803, 6.546389102935791, "The Data Transmission Rate of the X-band Communication Band is 5 Mbit/s."]
[11.112505912780762, 2.8683764934539795, "The Area of the Colorado River basin Basin is 246,000 square miles (637,000 km2)."]
[7.112211227416992, 1.5011688470840454, "The Orbit Date of the Cluster Satellite Constellation is December 29, 2006."]
[8.257744789123535, 9.10398006439209, "The Transmitted Wavefront Distortion of the Optical Window Component is \u03bb/8 at 633 nm."]
[8.561318397521973, 9.222524642944336, "The Color of the Laser Source Optical Component is Orange."]
[7.065860748291016, 4.503904342651367, "The Disintegration Recording of the ATV-5 Satellite is Camera."]
[3.9859137535095215, 5.0303544998168945, "The Orbits of the DSLP Data Acquisition System is 5500."]
[8.00157356262207, 4.100307941436768, "The Freeboard Measurement Data Source of the A-68A Iceberg is ESA\u2019s CryoSat mission, US ICESat-2 mission."]
[7.106995582580566, 9.780683517456055, "The Band 7 Wavelength of the OCM Payload is From 760 nm to 740 nm."]
[10.708478927612305, -1.5558712482452393, "The Unpressurized Trunk Mass of the Dragon Resupply Vehicle Resupply Vehicle is 960 kg."]
[11.708183288574219, -1.044988751411438, "The Mass of the Spacecraft structure Satellite Subsystem is 0.48 kg."]
[9.334122657775879, 8.185074806213379, "The Power Supply of the RAMIS Radiation Detector is 12 V (M1), 28 V (M2)."]
[7.809054851531982, 2.272993326187134, "The Publisher of the Observation of the Earth and Its Environment Book is Springer Verlag."]
[10.060172080993652, 2.357473611831665, "The Ground speed of the KOMPSAT-3 Satellite is 6.78 km/second."]
[10.660659790039062, -1.5701383352279663, "The Cargo Weight of the Dragon Spacecraft is More than 5,700 pounds."]
[8.594294548034668, 5.308585166931152, "The Pointing Accuracy of the Spacecraft Satellite is < 0.02\u00ba."]
[8.211228370666504, 1.565342903137207, "The Conference Date of the Solar Orbiter /PHI Full Disk Telescope Telescope is Oct. 7-10, 2014."]
[5.714303970336914, 1.4954440593719482, "The Launch Location of the SpaceX Launch Provider is Cape Canaveral Air Force Station in Florida."]
[6.891078472137451, 6.6584553718566895, "The Mission of the ALADIN LIDAR Instrument is AEOLUS."]
[11.130343437194824, 2.87239933013916, "The Depth of the South Pole-Aitken Basin Impact Region is 13 km."]
[6.440525054931641, 6.189780235290527, "The DPU of the ASCAT Scatterometer is Digital Processing Unit."]
[7.756870269775391, 1.1767473220825195, "The Date of the Close Approach Event Orbital Event is April 9, 2015."]
[9.062982559204102, 8.120841979980469, "The URL of the Cosmic Ray Isotope Spectrometer Spectrometer is http://www.srl.caltech.edu/ACE/CRIS_SIS/cris.html."]
[7.194021701812744, 9.378884315490723, "The Swath Width of the ScanSAR-1 Mode is 100 x 2500 km."]
[7.28868293762207, -0.05969374254345894, "The Launch Date of the H-IIB Launch Vehicle No. 2 Launch Vehicle is Jan. 22, 2011."]
[5.55005407333374, 1.9842519760131836, "The Deployment of the Flock-4v Satellite is ISL\u2019s QuadPack deployers and D-Orbit\u2019s InOrbit Now (ION) free-flying deployment platform."]
[6.258145332336426, 8.445323944091797, "The Channels of the MIS Instrument Microwave Radiometer is 39."]
[3.691330909729004, 5.301425933837891, "The Data Transport of the SPA-1 Interface is Unknown."]
[6.9073567390441895, 4.262804985046387, "The Instruments of the CAS500 Satellite is CSAR, Compact Advanced Payload Wide Swath, High Resolution Optical Sensor."]
[10.647553443908691, 9.217848777770996, "The Image License of the CaSSIS Instrument is CC BY-SA 3.0 IGO."]
[6.762565612792969, 6.430364608764648, "The Spatial Resolution of the SST Product Dataset is 2 km."]
[4.740767955780029, 4.613944053649902, "The Types of Environmental Data Records (EDRs) of the IDPS Interface Data Processing Segment is Cloud coverage, temperature, humidity, ozone distribution, snow cover, vegetation, sea surface temperatures, aerosols, space environment, earth radiation budget information."]
[7.903618812561035, 3.85390567779541, "The Sun Aspect Sensors of the ERG Satellite is 2."]
[8.370636940002441, 9.74579906463623, "The Mission of the Medium Energy Neutral Atom (MENA) Imager Imager is IMAGE."]
[9.228911399841309, 7.762723445892334, "The Observable Particle of the Particle Detector Instrument is Proton, deuteron, tritium, helium."]
[8.343435287475586, 2.709775924682617, "The Transport Destination of the Beresheet Spacecraft is Cape Canaveral Air Force Station."]
[4.531716823577881, 5.780793190002441, "The RF Communications of the Spacecraft Satellite is 0.5 W (S-band downlink)."]
[4.907865524291992, 7.539610862731934, "The Energy of the S-band Band is 10 \u00b5eV."]
[8.673768997192383, 7.101273536682129, "The Measurement Error of the Angular Rate Sensor is Random < 0.1\u00ba/s (1\u03c3), Bias < 0.6\u00ba/s, Nonlinearity < 0.5%."]
[9.394670486450195, 7.369091510772705, "The Probe Type of the Electron Temperature Part Experiment is Three simple circular planar probes with guarding rings."]
[11.835543632507324, 4.5800395011901855, "The Observation Date of the Space Sparkle Supernova Remnant is 7 January 2019."]
[4.443228721618652, 2.4892470836639404, "The Type of the LituanicaSAT-2 Satellite is 3U CubeSat."]
[10.337053298950195, 9.2945556640625, "The Flare Eruption Time of the IRIS Observatory is 19:40 UTC."]
[6.548458099365234, 0.5777156949043274, "The Agreement Date of the COMSAT, Inc. Service Provider is February 19, 2018."]
[4.436789512634277, 5.500940322875977, "The Communication Links of the TT&C subsystem Satellite Subsystem is S-band (2 GHz, command uplink and telemetry downlink)."]
[6.097002983093262, 2.290966033935547, "The Mission Type of the TacSat-3 Satellite is Technology demonstration."]
[8.220763206481934, 0.18335701525211334, "The Launch Date of the CIMON-2 Crew Interactive MObile companioN is 5 December 2019."]
[1.9258263111114502, 4.251655101776123, "The Solar Array Power of the Power Subsystem Subsystem is 35 W."]
[7.510876655578613, 7.1818528175354, "The Manufacturer of the SCM Instrument is CNRS/CETP."]
[1.4619226455688477, 4.982126235961914, "The Instrument Size of the SBVR Power Supply is 750 mm x 247 mm x 348 mm."]
[8.165305137634277, 8.814986228942871, "The Redshift Range of the NISP Spectrograph Instrument is 0.7 to 2.0."]
[9.667827606201172, 6.003396511077881, "The Heritage of the ADCS Attitude Determination and Control Subsystem is Previous GNB missions."]
[4.720402240753174, 2.165517807006836, "The Number of Photo MOSFET Switches of the DLP System Satellite System is 5."]
[6.870527267456055, 4.363288402557373, "The Atmospheric Species of the SciSat-1/ACE Satellite is Over sixty."]
[8.999192237854004, 7.618871688842773, "The Phase Transition Temperature of the Gallium Black Bodies Calibration Source is 29.76\u00b0C."]
[7.174887657165527, 1.365302324295044, "The Launch Date of the Global Surface Water Survey Mission Satellite Mission is Unknown."]
[10.92741870880127, 3.4422905445098877, "The Closest Approach Distance to Ganymede of the Juno Spacecraft is 645 miles (1,038 km)."]
[6.807164669036865, 2.911292552947998, "The Mission Status of the SOHLA-1 Satellite is Retired."]
[2.106182813644409, 4.529130458831787, "The Power of the ADEOS spacecraft Satellite is 4.5 kW."]
[9.151956558227539, 2.3270039558410645, "The Number of Venus Flybys of the V7GA Mission is 7."]
[9.783534049987793, 5.552385330200195, "The Planning Window Length of the RASP Maneuver Planning System is 60 minutes."]
[9.936738014221191, -0.646275520324707, "The Bus Structure of the Tsubame Microsatellite is Lattice structure (CFRP material)."]
[4.894376277923584, 4.305145740509033, "The Brochure URL of the Optical Inter-orbit Communications Engineering Test Satellite (OICETS) Satellite is http://global.jaxa.jp/activity/pr/brochure/files/sat09.pdf."]
[6.069836139678955, 9.669187545776367, "The Mass of the ROMAP ROMAG is 0.7 kg."]
[8.358346939086914, 3.392200469970703, "The Cumulative Absolute Height Error of the TanDEM-X Satellite is 0.9 m."]
[11.652458190917969, 5.065248489379883, "The Jet Behavior of the V404 Cygni Black Hole is Strange."]
[7.167707920074463, 0.8463008999824524, "The Launch Dates of the GeoOptics Satellite Manufacturer is June 2017 and January 2018."]
[8.276217460632324, 3.1183996200561523, "The T/R Modules Design and Performance Presentation Date of the TanDEM-X Satellite is June 2-5, 2008."]
[5.1567535400390625, 2.3714523315429688, "The Team Communication of the HORYU-4 Satellite is Problems."]
[3.9184746742248535, 4.3086042404174805, "The Microcontroller Architecture of the CDHS Command and Data Handling Subsystem is 16 bit, modified Harvard architecture."]
[5.805191516876221, 3.411180019378662, "The Hosting Spacecraft Provider of the DSAC Demonstration Unit is Surrey Satellite Technologies US LLC."]
[5.1309494972229, 2.12740159034729, "The Population of the Kolkata City is Over 14 million inhabitants."]
[10.31318187713623, 2.9031267166137695, "The Altitude of the PhoneSat-2.5 1U CubeSat Satellite is ~400 km."]
[10.741116523742676, 4.151099681854248, "The Photometric Precision of the CHEOPS Satellite is Similar to the Kepler mission of NASA."]
[7.228837966918945, 0.4837661683559418, "The Launch Date of the ALTIUS Satellite is May 2025."]
[8.61525821685791, 8.778568267822266, "The Pointing Axis Off-Pointing Angle of the Spectrometer (SPI) Spectrometer is 2.17\u00ba."]
[10.259224891662598, 5.100225448608398, "The Propellant Tank Capacity of the Cold Gas System Attitude and Orbit Control Subsystem is 132 l."]
[4.6526665687561035, 5.8845744132995605, "The Design of the Transceivers Communication Device is Dual receive (Rx)/transmit (Tx)."]
[10.980283737182617, 3.4063076972961426, "The Travel Time from Ganymede to Jupiter of the Juno Spacecraft is 14 hours, 50 minutes."]
[5.132045269012451, 1.5007699728012085, "The Number of PHM Clocks of the GIOVE-A Satellite is 2."]
[6.819921970367432, 1.9985320568084717, "The Availability of the Global Satellite Mapping of Precipitation (GSMaP) Satellite Data is Since March 2000."]
[8.322144508361816, 1.6118024587631226, "The Observation Continuation of the SoloHI Heliospheric Imager is Until it leaves its field of view on 22 December."]
[6.4693522453308105, 3.517669677734375, "The Payload of the MetOp Second Generation Satellite is Unknown."]
[5.919034481048584, 2.5929503440856934, "The Funding Source of the ELFIN Satellite is AFRL (Air Force Research Laboratory)."]
[9.299185752868652, 10.328447341918945, "The Rotation per Image of the M-CAM 1 Monitoring Camera is 3\u00ba."]
[9.384349822998047, 7.364652633666992, "The Operating Temperature of the FEU Faraday Cup Electronics Unit is Approximately 70\u00baC."]
[8.42662239074707, 11.095973014831543, "The Number of Rows to Make Two Perfect Rows of the QWIP Array Sensor Array is 3."]
[11.718542098999023, -1.2022699117660522, "The Satellite Mass of the ADEOS spacecraft Satellite is 3560 kg."]
[7.209076404571533, 5.680753707885742, "The Data of the Aeolus Satellite is Vertical distribution of aerosol and cloud layers."]
[9.27770709991455, 9.644933700561523, "The Photodetector Technology of the Optical Head Optical Device is CMOS Active Pixel Sensor (APS)."]
[8.46467113494873, 8.723424911499023, "The Grating Order of the Spectrometer Instrument is 1."]
[5.785460948944092, 5.251447677612305, "The Program Start of the SIR-C/X-SAR Payload is SIR-A in l98l."]
[7.0048136711120605, 2.486222505569458, "The URL of the SARah project Satellite Project is https://www.ohb.de/en/news/2019/satellite-based-radar-reconnaissance-for-germany."]
[7.458345890045166, 0.5203436613082886, "The Year of Launch of the GRACE Satellite is 2002."]
[4.220317840576172, 4.405459880828857, "The Components of the ACU Control and Data Handling Subsystem is 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)."]
[7.188663005828857, 0.7471272945404053, "The Handover Date of the Diwata-1 Satellite is January 13, 2016."]
[4.154521942138672, 6.039068222045898, "The Payload Data Modulation of the Satellite Satellite is PCM/BPSK."]
[5.855890274047852, 8.615065574645996, "The Swath width of the MWHS Microwave Humidity Sounder is 2700 km."]
[3.2142791748046875, 5.113290786743164, "The Data Backup of the ASAP-Light Camera System is Non-volatile flash memory."]
[1.7747673988342285, 4.12925386428833, "The Solar Panels of the EPS Electrical Power System is 3."]
[8.908880233764648, 2.7880897521972656, "The Renaming Date of the GCOM-C Satellite is July 14, 2017."]
[9.885298728942871, 7.862682819366455, "The Energy Measurement Range of the Telescope Telescope is 1-40 MeV/n."]
[6.1705451011657715, 3.2009365558624268, "The Interest of the SDA Agency is Algorithms and compute capabilities on orbit."]
[9.455185890197754, 5.825376510620117, "The Maximum Torque of the Reaction Wheels Attitude Control is 5 mNm."]
[7.298977851867676, 7.248520851135254, "The In-Orbit Calibration Types of the MIRAS Instrument is External, internal."]
[6.067436218261719, 2.647242546081543, "The Constellation of the Strela-3/Rodnik Military Reconnaissance Satellite is Strela."]
[7.8003249168396, 3.464552879333496, "The Coverage of the ERS Tandem Mission Satellite Mission is Nearly the whole global land surface."]
[7.109181880950928, 7.856375694274902, "The Position of the AMSR3 Instrument is Fourth in the AMSR series."]
[3.5525271892547607, 4.733249187469482, "The Clock Frequency of the AIM Reconfigurable Computing Hardware Device is 48 MHz."]
[4.024144172668457, 5.6771345138549805, "The Data Download Speed of the NEMO-HD Satellite is Up to 50 Mbit/s."]
[5.923855781555176, 6.719213008880615, "The Azimuth Coverage of the SWIM Real Aperture Radar is 180 km."]
[11.226696014404297, 6.881774425506592, "The Optics Presenter of the Imaging X-ray Polarimetry Explorer Satellite is Brian D. Ramsey."]
[9.69379711151123, 9.023238182067871, "The Length of the Secondary Mirror Support Structure Support Structure is Almost 25 feet."]
[7.939759254455566, 4.572872638702393, "The Flashes Measurement of the Tatiana-2 Satellite is More than 1000."]
[5.656247138977051, 1.6661460399627686, "The Stage Type of the Soyuz Rocket is Kerosene-fueled first stage boosters."]
[7.861251354217529, 1.173457145690918, "The Lunar Eclipse Date of the Spacecraft Satellite is June 4."]
[10.271137237548828, 8.730755805969238, "The Telescope Sensitivity of the EUVI Extreme Ultraviolet Imager is Higher sensitivity."]
[9.905524253845215, 1.5409224033355713, "The Duration of the Solar Eclipse Event is About two hours."]
[8.743063926696777, 0.1568259298801422, "The Design of the Skylab-1 Space Station is Use leftover Apollo lunar hardware."]
[5.931307792663574, 6.3969526290893555, "The Observing Frequency of the L-SAR Satellite is 1.275 GHz."]
[6.946279525756836, -0.0806191936135292, "The End of Life Date of the TUBSAT Satellite is Spring 2007."]
[5.9957475662231445, 9.549192428588867, "The Mass of the LCT instrument Instrument is 53 kg."]
[9.010505676269531, 9.149174690246582, "The Length of the Graded Index Multimode Fiber Fiber is 30 meters."]
[11.78564739227295, -1.0005327463150024, "The Mass of the IPEX-II boom ADAM mast is 112 kg."]
[6.909135818481445, 3.564265489578247, "The Unknown of the Table 1 Information Table is Unknown."]
[7.224611282348633, 9.344383239746094, "The Swath of the Stripmap mode (SM) Operational Mode is 80 km."]
[5.901965141296387, 4.256420612335205, "The Full Form of the ESP-MACCS Satellite is Earth System Processes Monitored in the Atmosphere by a Constellation of CubeSats."]
[8.853290557861328, 9.789759635925293, "The Functions of the Electronics Imager Electronics is Detector and image data operation, calibration mechanism operation and temperature control, cryocooler operation and supervision."]
[7.913623332977295, 8.262526512145996, "The Design Components of the CHRIS Imaging Spectrometer is Catadioptric telescope, imaging spectrometer, area detector array."]
[9.744183540344238, -0.705121636390686, "The NORAD ID of the BX-1 Microsatellite is 33392."]
[9.003708839416504, 7.258703708648682, "The Objective of the Electron Spectrometer Spectrometer is Provide high time resolution (<1 s) solar wind electron, full 3D distribution function observations."]
[3.27412486076355, 5.312604904174805, "The Onboard Data Storage Capacity of the DTS Data Transmission Subsystem is 128 Gbit."]
[7.18993616104126, 1.5081981420516968, "The Meeting Date of the SHIZUKU and IBUKI Satellites is May 30-June 1, 2012."]
[0.9349278211593628, 4.197941780090332, "The Capacity of the Battery Energy Storage is 11.8 Ahr."]
[1.7558506727218628, 4.83551025390625, "The Mass of the EPS Electrical Power Subsystem is 167 g."]
[3.7772469520568848, 6.1937689781188965, "The Telemetry Data Rate Range of the TTCS Telemetry & Telecommand Subsystem is 4-16 kbit/s."]
[8.588644981384277, 6.834158420562744, "The Sampling Coordination of the Magnetometer Instrument is Coordinated with pulsing by the magnetorquers."]
[11.151593208312988, 2.5434887409210205, "The Maximum Slope of the Schiaparelli Lander is 12.5\u00ba."]
[7.549617767333984, 1.1849937438964844, "The Validation Date of the NASA ESTO technologies Technologies is July 22-27, 2012."]
[7.296577453613281, 9.324901580810547, "The Width of the Umbra Shadow is 50-100 km."]
[9.77286434173584, 5.537492752075195, "The Maneuver Execution Time (60 minute window) of the RASP Maneuver Planning System is 176.7 minutes."]
[6.005087375640869, 2.7982401847839355, "The Purpose of Funding of the Brazilian Ministry of Defense Government Agency is Buy an undisclosed satellite imaging system for Amazon monitoring, both for civilian and military use."]
[7.01686429977417, 0.0786711573600769, "The End of Life Date of the DMC-3 Satellite Constellation is 10 Oct 2022."]
[9.296574592590332, 2.341732978820801, "The Number of Lunar Flybys of the ICE (International Cometary Explorer) Spacecraft is 5."]
[7.8597798347473145, 4.653288841247559, "The Spatial Resolution of the Satellite Imaging Instrument is High."]
[6.2481184005737305, 5.899640083312988, "The Spotlight High Resolution (HS) Image Size of the TSX-SAR Satellite is 5-10km x 5km."]
[8.78608512878418, 3.6283226013183594, "The Components of the Stack Level Testing Configuration is MPO (and Japanese orbiter MMO), MTM ion propulsion with twin thruster operation."]
[11.450011253356934, -1.3138020038604736, "The Mass of the PRESat Satellite is ~4.5 kg."]
[5.086245536804199, 6.867862701416016, "The Volume of the Radio and Antenna Communication System is 0.25U (2.5 cm x 2.5 cm x 10 cm)."]
[7.2753987312316895, 6.881619930267334, "The Use as Transfer Radiometer of the S-NPP VIIRS Satellite Instrument is Unknown."]
[7.594393253326416, 7.737525463104248, "The Spectral Calibration of the SUCHI Instrument is Pre-flight."]
[9.547640800476074, 0.5055093765258789, "The Design Life of the Spacecraft bus Satellite is 5 years."]
[7.475803852081299, 0.4655120372772217, "The Launch Date of the JPSS-2/NOAA-21 Satellite is 10-11-2022."]
[4.1246442794799805, 7.292758464813232, "The Mass of the S-band Transmitter Transmitter is 0.1 kg."]
[7.281429767608643, 3.561264991760254, "The Unknown of the Formosat-2 Satellite is Unknown."]
[7.815748691558838, 9.934945106506348, "The Swath Width (Simultaneous) of the HRV Imager is 117 km."]
[10.623434066772461, -1.4070477485656738, "The Propellant Transfer of the Tianzhou-2 Cargo Spacecraft is 1.95 tons."]
[3.2749767303466797, 4.918584823608398, "The SpaceWire Transfer Rate of the OBC On-Board Computer is 10 Mbit/s."]
[12.117105484008789, 3.2791059017181396, "The Orbit Inclination of the ResourceSat-1 Satellite is 98.7\u00b0."]
[5.798719882965088, 9.146402359008789, "The Power Dissipation of the LCT Optical Instrument is Varies."]
[8.293506622314453, 9.763635635375977, "The Detector Type of the OSIRIS Infrared Imager is One-dimensional InGaAs (128 pixel) linear arrays."]
[5.613104343414307, 9.112064361572266, "The Electronics Package Power of the FlaPS Instrument Package is 1.5 W."]
[6.625482559204102, 2.9716413021087646, "The URL of the Resurs-P1 Satellite is http://eng.ntsomz.ru/news/news_center/resurs-p_images_gallery_201308."]
[6.685075759887695, 2.1390154361724854, "The Based on of the Beijing-3B Satellite is Beijing-3A."]
[6.761981964111328, 1.6551225185394287, "The Launch Date of the Envisat Satellite is March 1, 2002."]
[9.1171236038208, 10.568609237670898, "The Image Capture Time of the Monitoring Camera 3 Camera is 23:44:57 UTC."]
[7.65285062789917, 9.08899974822998, "The No. of Detectors/Channels of the Visible Spectral Band Spectral Band is 4 (+4 spare)."]
[11.417126655578613, -1.3613115549087524, "The Mass (kg) of the RISAT-1 Satellite is 300."]
[4.098929405212402, 7.297623157501221, "The Mass of the STX-01 S-band Transmitter/Transceiver is 80 g."]
[7.117597579956055, 0.2884080410003662, "The Launch Date of the JERS-1 Satellite is 11 Feb 1992."]
[6.795069694519043, 0.4594883620738983, "The Launch Date of the Resurs-P3 Satellite is March 2016."]
[4.966305732727051, 7.511132717132568, "The Bit Rate of the LIMS Instrument is 4 kbit/s."]
[9.120064735412598, 9.347256660461426, "The Camera FOV of the Observation of non-cooperative objects Experiment is 14o."]
[8.0697603225708, 7.763706207275391, "The Frequency Response of the SCM Sensor is ELF/VLF range."]
[6.22819709777832, 6.926916122436523, "The Deployment Switches of the Radar Instrument is 4."]
[8.008641242980957, 7.382569313049316, "The Calibration of the AVHRR/3 Instrument is Calibration of the IR channels is performed with four internal blackbodies every scan line."]
[7.0431060791015625, 9.144795417785645, "The Spatial Resolution of the Lunar Flashlight Spacecraft is 10 km or better."]
[9.411544799804688, 0.35051947832107544, "The Exceeded Design Life of the Terra Satellite is Yes."]
[8.405424118041992, 0.6041545271873474, "The Radio Signals of the Hitomi Satellite is 3/28 22:06 (for about 10 sec) @ USC."]
[8.420687675476074, 11.072969436645508, "The Number of Rows of the QWIP Array Sensor Array is 512."]
[5.372422218322754, 10.404657363891602, "The Location Accuracy of the LIS Lightning Image Sensor is Within one pixel."]
[8.682699203491211, 10.01417350769043, "The Number of Focal Plane Modules of the OLI Imaging System is 14."]
[9.385239601135254, 9.082408905029297, "The Function of the Array of Cylindrical Lenses Optical Component is Image the telescope pupil onto the detector."]
[8.39466667175293, 0.5996994972229004, "The Break-out Time of the Hitomi Satellite is 10:42\u00b111M."]
[6.2496771812438965, 7.540061950683594, "The Polarization, Left Swath of the KaRIn Instrument is HH."]
[5.466806888580322, 1.8812006711959839, "The Post-Flight Analysis Recommendations of the Automated Transfer Vehicle Spacecraft is 130 technical recommendations."]
[12.1355562210083, 2.184884786605835, "The Sample Collection Opportunities of the OSIRIS-REx Spacecraft is 3."]
[8.555631637573242, 2.2630844116210938, "The Lead Author of the Kepler space telescope Telescope is Steve Bryson."]
[9.691534042358398, 7.032243251800537, "The Heat Shield Maximum Temperature of the Orion Spacecraft is 2750\u00baC."]
[7.093542575836182, 9.544520378112793, "The Band 5 of the MSS Instrument Spectral Band is 0.6 - 0.7 \u00b5m."]
[7.986952304840088, 8.559930801391602, "The Observation Range of the Limb Sensing Instrument Spectrometer is Tangent radius upward."]
[6.185260772705078, 3.5079023838043213, "The Provider of the MetOp-B Satellite is EUMETSAT."]
[8.822453498840332, 3.4812703132629395, "The Science Objective of the MinXSS Satellite is 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)."]
[6.405900955200195, 1.7223161458969116, "The Ground Segment Design Presentation Date of the EnMAP Satellite is 7 March 2013."]
[6.942649841308594, 4.164581775665283, "The Measurement Category of the SkySat Constellation Satellite Constellation is Multi-purpose imagery (ocean), Multi-purpose imagery (land)."]
[9.510503768920898, 8.635191917419434, "The Fabrication Finesse of the Etalon Filter is \u2265 30."]
[4.1980133056640625, 5.525162220001221, "The Downlink Data Volume of the IXPE Satellite is ~600 MB/day."]
[5.0200300216674805, -0.1393216997385025, "The Launch Date of the OneWeb Satellite Communications Company is From 2022."]
[6.355696201324463, 8.263015747070312, "The Number of Channels of the AMSU Microwave Radiometer is 15."]
[7.163558006286621, 0.8357529044151306, "The Launch Date of the ORS-3 Mission Satellite Mission is August 2013."]
[5.730855464935303, 3.0487253665924072, "The Manufacturer of the SARah system Satellite System is OHB and Astrium."]
[4.758815288543701, 2.728055000305176, "The Control Type of the Tom 2U CubeSat is Active."]
[4.780272960662842, 0.8342745304107666, "The Contract Award of the PlanetIQ Satellite Manufacturer is $3.5 million."]
[10.969891548156738, 2.8286120891571045, "The Depth of the Tohoku-Kanto earthquake Earthquake is 32 km."]
[3.5138955116271973, 4.876544952392578, "The Output Data Rate of the Spacecraft 406 MHz Processor Processor is 2.4 kbit/s."]
[8.03760051727295, -0.675067126750946, "The Launch Time of the Crew Dragon Spacecraft is 8:02 p.m. EDT."]
[1.6216235160827637, 4.785155296325684, "The DET System of the EPS Electric Power Subsystem is 21-35 V."]
[8.506265640258789, 2.1847357749938965, "The Launch Date of the Parker Solar Probe Satellite is Summer of 2018."]
[12.046481132507324, 3.2760775089263916, "The Orbit Inclination of the CINEMA satellites Satellite is High."]
[11.557099342346191, 6.248307704925537, "The URL of the XMM-Newton Satellite is http://www.esa.int/Science_Exploration/Space_Science/XMM-Newton_maps_black_hole_surroundings."]
[4.418631553649902, 7.551464557647705, "The Design Features of the Channelizers/filters Signal Processing is 4 channel input multiplexer @ 4 GHz, 4 channel filter @ 4GHz, 5 channel input multiplexer @ 8 GHz."]
[1.9498499631881714, 5.557205677032471, "The Current of the Voltage 7 Power Amplifier is 475."]
[8.757515907287598, 2.397054433822632, "The View of Venus of the Parker Solar Probe Spacecraft is Stunning."]
[11.365480422973633, 4.165572166442871, "The Orbits of Planets of the Kepler-11 Star System is Smaller than Venus and Mercury's."]
[7.9640607833862305, 6.845835208892822, "The Calibration Activities Duration of the SGLI Sensor is First year."]
[6.949078559875488, 3.2038791179656982, "The Unknown of the NASA Cargo Cargo is Unknown."]
[4.8783860206604, 1.89747154712677, "The Number of Satellites of the CIMR Satellite is Three."]
[9.213427543640137, 5.195526599884033, "The Torque of the Canopus Pipper Satellite is 1.6 x 10 -4 Nm."]
[5.121550559997559, 6.591546058654785, "The Beam Pointing Error of the Antenna Communication is Less than 0.83\u00ba (static)/0.0045\u00ba (dynamic)."]
[8.102250099182129, 8.304581642150879, "The Temperature Uncertainty of the Instrument Spectrometer is 0.1K at the bottom of the limb to 13 K at 140 km."]
[8.47083854675293, 8.75940990447998, "The Purpose of the Grating Reflection Unit Spectrometer Component is Manipulation and compression of high-power ultra-short laser pulses."]
[4.173077583312988, 3.7817635536193848, "The Number of Channels of the NorAIS-2 Receiver AIS Receiver is Four."]
[6.9511308670043945, 4.336738586425781, "The Measurement Domain of the JPSS-2/NOAA-21 Satellite is Atmosphere, Land."]
[7.782167911529541, 5.601588249206543, "The SNR Linearity of the SCATSat-1 Satellite is Even at SNRs as low as -45 dB."]
[6.43134069442749, -0.6717336177825928, "The Design and Performance Presentation of the QZSS Satellite System is ION NTM (National Technical Meeting) 2007, San Diego, CA, USA, January 22-24, 2007."]
[4.525001525878906, 2.229250192642212, "The Number of Deorbited Relay Stations of the Starlink Communication Satellite is 3."]
[8.283215522766113, 0.40814751386642456, "The Prototype Name of the BEAM Module is Bigelow Expandable Activity Module."]
[7.836065769195557, 9.011378288269043, "The Spectral Resolution of the UV-2 Spectrometer is 0.45 nm."]
[10.578619956970215, 7.530293941497803, "The Structure Material of the HIT-Sat Satellite is Aluminum alloys, AL2219 and AL5052."]
[5.663683891296387, 9.142821311950684, "The Power of the GeoCarb Instrument is 128 W."]
[7.215322494506836, 1.5452549457550049, "The Operation Start Date of the Cluster Satellite Mission is 1 September 2000."]
[7.139570236206055, 4.549315452575684, "The CCD Cameras of the HJ-1A Satellite is 2."]
[8.498571395874023, 7.0597453117370605, "The Magnetic Field Measurement Channels of the IOF Plasma Wave Instrumentation is 7."]
[4.626239776611328, 2.7365872859954834, "The Architecture of the TechEdSat Satellite is 1U cubesat."]
[8.946346282958984, 10.556425094604492, "The Operational Capability of the MRC (Medium-Resolution Camera) Camera is Achieved."]
[12.044182777404785, 4.4859747886657715, "The Motion of the Blue Ring Nebula Nebula is One cone moving almost directly toward Earth, while the other is moving almost directly away."]
[10.50528621673584, 8.475852966308594, "The Imaging Target of the COR-2 Coronagraph is Sun\u2019s outer atmosphere, or corona."]
[7.9441304206848145, 6.856349945068359, "The Frequency of the MPA Calibration System is After every burn."]
[7.29797887802124, 2.2936851978302, "The News Release Date of the NASA's Spaceborne Carbon Counter Satellite is Dec. 18, 2014."]
[7.677676200866699, 9.604732513427734, "The Data Rate of the VIS Visible region of spectrum is 7.2 Mbit/s."]
[8.916979789733887, 3.1941404342651367, "The Orbit of the OTB-1 minisatellite Satellite is Earth's orbit."]
[4.410648822784424, 4.249533653259277, "The Operating System of the Control Room Facility is Linux."]
[2.2174341678619385, 3.847844362258911, "The Solar Panels of the MicroMAS-1 Satellite is Four 3U double-sided deployable solar panels oriented at 120\u00ba angles to the structure."]
[11.133269309997559, 4.37860107421875, "The Speed of the Heliosphere Interstellar Medium is 52,000 miles per hour."]
[7.205526828765869, 3.175605535507202, "The Mission Status of the Satellite Spacecraft is Unknown."]
[11.843290328979492, 5.628054618835449, "The Measure of Precision Cosmology of the Gravitational Weak Lensing Phenomenon is Yes."]
[6.671627998352051, 7.342763423919678, "The Scanning Frequency of the Scanning LIDAR LIDAR is Varied according to a predefined scanning scheme."]
[8.796091079711914, 7.654958724975586, "The Altitude of the IVM Ion Velocity Meter is Above 250 km."]
[9.448161125183105, 7.323134899139404, "The Insulators of the FSU Solar Wind Faraday Cup is Machined sapphire rods."]
[7.140215873718262, 4.205583095550537, "The Measurement Domain of the SPOT-5 Satellite is Ocean, Land, Snow & Ice."]
[6.440398216247559, 9.146771430969238, "The Volume of the Instrument Device is < 6800 cm^3."]
[7.02617073059082, 0.3650476038455963, "The Retirement Date of the Ikonos Imaging Satellite is March 31, 2015."]
[10.591931343078613, 7.520553112030029, "The Structure Material of the QuakeSat Satellite is 6061 aluminum."]
[8.248920440673828, 8.926553726196289, "The Film Transmission of the MXT Instrument is t70."]
[5.774458408355713, 6.686685562133789, "The Antenna Aperture of the Radar Radar is 1.5 m x 1.5 m."]
[7.601025104522705, 9.916570663452148, "The Operational Temperature Range of the Instrument Hyperspectral Imager is 293.15 K \u00b1 2 K."]
[5.811518669128418, 8.162213325500488, "The Bandwidth (GHz) of the ICI-9 Radiometer is 4."]
[5.6024909019470215, 1.6589182615280151, "The Stage Type of the Soyuz Rocket is Core stage."]
[6.902320861816406, 5.323662281036377, "The Additional Capability of the SMOS Satellite is Map the extent and thickness of sea ice."]
[5.088171482086182, 3.060807943344116, "The Architecture of the CubeSat Satellite is Decentralized."]
[8.275810241699219, 4.578481197357178, "The Swath Width of the DubaiSat-1 Satellite is 20 km."]
[6.934455871582031, 2.9153475761413574, "The Development Status of the Orion Vehicle Spacecraft is Unknown."]
[5.969501495361328, 3.5483667850494385, "The Provider of the HW-BOSS System is Fraunhofer-Gesellschaft FIRST."]
[7.4879841804504395, 1.7688931226730347, "The Copyright Year of the eoPortal Website is 2024."]
[3.8821892738342285, 4.394992351531982, "The Manufacturer of the OBC On-Board Computer is Atmel."]
[4.018086910247803, 5.907303333282471, "The Maximum Simultaneous CDMA Channels of the Mission Uplink Subsystem Communication System is 6."]
[9.892926216125488, 1.5335636138916016, "The Time of the Mirror Retrace Process is 2.5 minutes."]
[3.6078057289123535, 6.6671142578125, "The Data Rate of the X-band transmitter Transmitter is Up to 100 Mbit/s."]
[8.188207626342773, 4.759437561035156, "The Mission Type of the NEMO-HD Satellite is High Definition Video and Multispectral Earth Imaging."]
[7.14424467086792, 7.2848944664001465, "The Observation Geometry of the MIPAS Instrument is Limb."]
[7.355475902557373, 1.9890689849853516, "The Research Area of the B2-1 Experiment is Gravitational Biology."]
[9.308704376220703, 7.201894760131836, "The Ignition Power of the T3\u00b5PS Pressure Sensor is 10.1 W."]
[9.33143424987793, -0.6557981967926025, "The Documentary Team Member of the AzTechSat Nanosatellite is Ana Belen Urrutia Bartsch."]
[10.135517120361328, 2.8593907356262207, "The Injection Errors of the PUNCH Mission Satellite is 10 km on the injection apse, 80 km on the non-injection apse, and 0.15\u00b0 on inclination."]
[7.0358734130859375, 9.76358699798584, "The Spectral Range (\u00b5m) of the Band 6 Spectral Band is 1.58 - 1.64."]
[5.65023136138916, 2.3901360034942627, "The Reflector Technology of the SARah Satellite Constellation is Based on SAR-Lupe and enhanced for SARah."]
[5.982943534851074, 9.572504997253418, "The Mass of the FREND Instrument is 36 kg."]
[6.027406215667725, 2.1370773315429688, "The Launch Site of the Yubileyniy-2/MiR Satellite is Plesetsk Cosmodrome, Russia."]
[6.5557122230529785, 0.7487859725952148, "The Progress Update of the TET-1 Satellite is Aug. 10, 2012."]
[6.049428462982178, 3.827827215194702, "The Experiment of the Kyoto University Organization is Robot teleoperation experiment."]
[10.382431030273438, 3.3829429149627686, "The Spacing of the GRACE-FO satellites Satellite is 220 km."]
[7.046533107757568, 5.113396167755127, "The Warming Cause of the Earth Planet is Human influences, such as deforestation, particulate pollution, and the release of greenhouse gases from the burning of fossil fuels."]
[11.244176864624023, 2.8516571521759033, "The Maximum Displacement of the Disturbed Areas Geological Feature is 10 cm."]
[8.597803115844727, 8.86432933807373, "The 20 ms / 16 energy steps of the Time Resolution Sensor is Time resolution 20 ms / 16 energy steps."]
[7.797048091888428, 10.667072296142578, "The ADC Resolution of the Rx Module Digital Receiver is 14 bit."]
[9.373138427734375, -0.7885010838508606, "The Launch Date of the KazSTSAT Microsatellite is 3 December 2018."]
[5.3023834228515625, 4.446404933929443, "The Locations of the PDHS Data-Handling Station is Frascati (Ka-band), Kiruna, Sweden (X-band), Svalbard."]
[9.124064445495605, 3.370922088623047, "The Orbit Stability of the LAGEOS Satellite is Very stable."]
[10.319519996643066, 7.041521072387695, "The Reason for Concept Change of the ALBus R&R Design is Critical thermal issue and mass budget constraints."]
[4.153009414672852, 5.703953742980957, "The X-band Downlink Data Rate of the Spacecraft Satellite is 320 Mbit/s."]
[8.275148391723633, 4.516026020050049, "The Swath of the Megha-Tropiques Satellite is ~1700 km."]
[11.144691467285156, 6.771337509155273, "The Attitude Sensing of the X-ray Navigation Navigation System is High-accuracy without optics."]
[11.19265365600586, 4.228518962860107, "The Number of Confirmed Exoplanets of the Kepler Satellite is 100+."]
[5.333347320556641, 3.9531984329223633, "The Capability of the Remote Agent Software is Detected, diagnosed and fixed simulated problems."]
[3.857675313949585, 2.2984490394592285, "The Size of the CUAVA-1 CubeSat is 3U."]
[7.00111198425293, 6.201977729797363, "The Quantity Used of the ALACE Floats Oceanographic Instrument is About 1000."]
[7.356117248535156, 0.6214439868927002, "The Launch Date of the OrbView-2 Satellite is August 1, 1997."]
[10.037378311157227, 1.5074701309204102, "The Track Duration of the CTECS Satellite is 30.6 minutes."]
[8.771974563598633, 0.9807530641555786, "The End of Operation of the LS-7 Satellite is 2012."]
[4.608943462371826, 5.8495965003967285, "The RF Communications of the Spacecraft Satellite is 145.89 MHz."]
[7.7885355949401855, 2.0778987407684326, "The Instruments of the Europa Clipper Spacecraft is EIS, E-THEMIS, Europa-UVS, MISE, ECM, PIMS, Gravity & Radio Science, REASON, MISE, MASPEx, SUDA."]
[10.166849136352539, 6.795188903808594, "The Thermal Control of the G\u00f6kt\u00fcrk-1A Satellite is Passive radiators along with a heater system."]
[1.5361499786376953, 4.895303249359131, "The Voltage of the Main Power Bus Power Distribution is 28 to 33 V."]
[1.8322683572769165, 4.264873504638672, "The Model of the GSE Power Supplies Power Supply is Solar eclipse."]
[4.857663631439209, 0.9826485514640808, "The Funding Allocation of the Brazilian Ministry of Defense Government Agency is 145 million real."]
[7.135613441467285, 2.501288652420044, "The URL of the HITSAT Satellite is http://astronomy.activeboard.com/forum.spark?aBID=58381&p=3&topicID=18351197&page=1&sort=newestFirst."]
[9.54728889465332, 3.198765993118286, "The Orbit Type of the Primary Payload Unknown is Circular."]
[7.760822772979736, 1.053493857383728, "The Article Date of the Earth-observing satellite Satellite is 25 May 2022."]
[6.076839923858643, 9.725817680358887, "The Instrument Mass of the Telescope Optical Instrument is 88 kg."]
[10.43957805633545, -1.1398406028747559, "The Mass of the AISSat-3 Nanosatellite is 6.5 kg."]
[9.706804275512695, 1.6771148443222046, "The FDC (Failure Detection and Correction) Scheme of the Dellingr Satellite is 25-hour reset."]
[8.126115798950195, 5.287144184112549, "The Navigation Accuracy of the Spacecraft Satellite is 60 m."]
[6.611924648284912, 3.167909622192383, "The Platforms of the Satshot GIS Mapping Engine is Mapcenter, Landscout and iCue."]
[9.696694374084473, 1.0745242834091187, "The Orbit Transition Duration of the WorldView-1 Satellite is 18 months."]
[0.9831141829490662, 4.322476387023926, "The Cd-Ni Battery Capacity of the EPS Electrical Power Subsystem is 55 Ah."]
[4.31520414352417, 4.969375133514404, "The Protocol of the TT&C S-band Communications Communication System is CCSDS."]
[7.785918235778809, 0.7192491888999939, "The Congress Date of the ADM-Aeolus Satellite is Oct. 2-6, 2006."]
[6.9230241775512695, 1.5250866413116455, "The Launch Date of the Observer Mission (KSF3) Satellite Cluster is Mid-2022."]
[4.006068229675293, 6.555935859680176, "The Components of the Group Delay Parameter is Data generator, modulator, up converter, travelling-wave tube amplifier (TWTA), cable, and integration components."]
[8.518373489379883, 2.213041305541992, "The Award Date of the Parker Solar Probe Satellite is 1 July 2021."]
[2.205177068710327, 6.522078990936279, "The Latency of the ATL07 Arctic/Antarctic Sea Ice Elevation Data is 45 days."]
[12.038666725158691, 3.3258423805236816, "The Transition Orbit Inclination of the LUMIO Satellite is Lies within the parking orbit bounds."]
[4.169022560119629, 7.370323181152344, "The Mass of the Card Mass Communication System is <0.6 kg."]
[9.614431381225586, 0.7518956661224365, "The Balloon Diameter of the AeroCube-3 Satellite is ~ 60 cm."]
[7.272154808044434, 5.4731221199035645, "The Impact of the Aeolus Satellite is Amongst the most important satellite missions."]
[6.741277694702148, 7.448572635650635, "The Manufacturer of the MSU-GS Instrument is FSUE/RISDE (Federal State Unitary Enterprise) / Russian Scientific Institute of Space Device Engineering."]
[8.22162914276123, 9.915414810180664, "The Scanning Technique of the WV-3 Imager Imager is Pushbroom."]
[2.0160837173461914, 7.848015785217285, "The Solar Wind Speed and Beta of the ACE Satellite is ~11% lower on average from 2009 through the day 79 of 2013."]
[8.626810073852539, 0.15581467747688293, "The Crew Capacity of the Space Station Space Station is 7 members."]
[7.722262859344482, 8.541130065917969, "The Instrument Type of the LISS-III Instrument is Imaging multi-spectral radiometers (vis/IR)."]
[9.292296409606934, 5.247976779937744, "The Attitude Control of the KOMPSAT-6 Satellite is 3-axis attitude control with zero momentum bias."]
[6.533462047576904, 4.074416160583496, "The Data Access of the Vision-1 Satellite is Free basis to a range of stakeholders."]
[8.802727699279785, 2.4010517597198486, "The Successful Swings around the Sun of the Parker Solar Probe Spacecraft is 7."]
[8.710098266601562, 10.643134117126465, "The Size of the PPL1 and PPL2 Hyperspectral Camera Systems is 131 x 221 x 262 mm."]
[6.793097019195557, 4.770086765289307, "The Mission Type of the Sentinel-5 Satellite is European operational atmospheric chemistry mission in polar orbit."]
[9.568307876586914, 7.855525016784668, "The Electron energy of the Microdosimeter A Instrument is > 50 keV."]
[7.8901824951171875, 6.768397808074951, "The Feasibility Analysis Frequency of the MUS Subsystem is Daily."]
[6.773689270019531, 5.628842353820801, "The Importance of the Soil Moisture Measurement is Relevant for a variety of applications, particularly farming."]
[9.049091339111328, 10.670591354370117, "The Integration Time of the WiFS camera Camera is 28.42 ms."]
[7.621382713317871, 1.766451120376587, "The Data Flow Start Date of the SMAP Satellite is November 19."]
[6.232304096221924, 8.525349617004395, "The Conical scanning period of the Microwave System Microwave System is 2.88 s."]
[7.843880653381348, 9.803489685058594, "The Swath Width of the Pushbroom imager Optics is 10.15 km."]
[8.919758796691895, 2.4332563877105713, "The Observation Spectrum of the Herschel Space Telescope is Far-infrared and submillimeter."]
[2.2132046222686768, 6.516434192657471, "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."]
[8.494260787963867, 8.972456932067871, "The Grating Lines of the Offner-type spectrometer Spectrometer is 500 lines/mm."]
[5.0461015701293945, 4.678267002105713, "The Current User of the Ground Station Ground Segment Component is IRS."]
[4.544773101806641, 4.2699384689331055, "The Function of the Payload Control Unit Sensor Component is Provide the command and control interface between the platform and the payload."]
[5.4225311279296875, 2.026777982711792, "The Goal of the MoonKAM Education and Public Outreach Program is Engage middle schools in the GRAIL mission and lunar exploration."]
[9.125265121459961, 10.767143249511719, "The Swath Width of the Main Camera Camera is 2250 km."]
[7.835690975189209, 9.629193305969238, "The Measurement Range of the PRI Photochemical Reflectance Index is 500\u2013600 nm."]
[5.0722575187683105, 2.3235490322113037, "The Number of Transponders of the Inmarsat S \u2013 Europasat / Hellas-Sat 3 Satellite is 44 Ku and 1 Ka."]
[4.356671333312988, 4.257822036743164, "The Development Status of the MEP Main Electronics Package is Not provided."]
[11.54648208618164, -1.3937089443206787, "The Mass (kg) of the ERS-1 Satellite is 2384."]
[3.5686371326446533, 5.434453010559082, "The Number of Channels of the FODB Data Interface is 12."]
[9.406136512756348, 1.0138605833053589, "The Prime Mission Duration of the EMIT Satellite is One year."]
[8.51352310180664, 10.396053314208984, "The CCD Type of the Pan band Detector Array is PhotoMOS-type."]
[6.165559768676758, 2.90805721282959, "The Developers of the Carruthers Geocorona Observatory (GLIDE) Satellite is Ball Aerospace and University of California (UC) Berkeley."]
[6.274355888366699, 3.8042123317718506, "The Testing Location of the Galileo Satellites 13 and 14 Satellites is Oberpfaffenhofen, Germany."]
[7.701470851898193, 9.04932689666748, "The Spatial Resolution of the Ma_MISS Spectrometer is 120\u2009\u00b5m."]
[10.26189136505127, 2.910013198852539, "The Perigee Altitude of the Satellite Constellation Satellite Constellation is ~ 300 km."]
[8.457077980041504, 4.691378116607666, "The Measurement Objectives of the Cluster Satellite Mission is Study of small-scale plasma structures and current densities."]
[7.374839782714844, 10.0462646484375, "The Manufacturer of the Hyperion HSI (Hyperspectral Imager) is Northrop Grumman (formerly TRW)."]
[8.177823066711426, 8.853476524353027, "The GSD at Nadir of the Telescope Optical Instrument is 30 m."]
[5.1977715492248535, 4.526195526123047, "The Location of the IDPS Integrated Data Processing System is NOAA Satellite Operations Facility in Suitland, MD."]
[6.305455207824707, 2.3086562156677246, "The Role of the Jason-3 Satellite is High Precision Ocean Altimetry reference mission."]
[1.6146759986877441, 4.716732978820801, "The Power Source of the Electronics Imager Electronics is Spacecraft 28 V bus."]
[7.630762100219727, 9.203845977783203, "The Spectral Range of the Spectral Band A Spectrometer is 0.45 - 0.52 \u00b5m."]
[8.362278938293457, 8.802726745605469, "The Number of Infrared Detectors of the CrIS Instrument is 27."]
[4.063185691833496, 1.167974591255188, "The Mission Type of the Oculus-ASR Satellite is Non-EO."]
[4.063146114349365, 6.490930557250977, "The Laser Connection of the SpaceDataHighway Communication System is More than 50,000 within the first five years."]
[8.999650955200195, 7.248716831207275, "The Presentation Location of the Micro Digital Sun Sensor Sensor is Banff, Alberta, Canada."]
[9.990596771240234, 2.420196533203125, "The Ground Target Coverage of the KOMPSAT-5 Satellite is Up to 490 km width in a single orbit."]
[9.744519233703613, 1.3501712083816528, "The Observation Duration of the Integral Satellite is Four weeks."]
[9.515297889709473, 0.8284416198730469, "The Time in Orbit of the Vesselsat-1 & -2 Satellite is 3 years."]
[4.877943992614746, 2.8365116119384766, "The Expected Number of Tracked Cargo Vessels of the MDASat-i Satellite is 60000."]
[7.6379876136779785, 7.687958717346191, "The Calibration Concept of the Atmospheric-sounding instrument Spectrometer is Extensive on-ground characterization and in-flight calibration concept."]
[2.218792200088501, 6.515503883361816, "The Latency of the ATL08 Land Water Vegetation Elevation Data is 45 days."]
[4.279374599456787, 2.4805827140808105, "The Baseline Design of the SpooQySat Satellite is GomX-313 with modifications."]
[7.342376232147217, 0.15235644578933716, "The Planned Launch Year of the ESP-MACCS Satellite is 2024."]
[7.182022571563721, 9.316166877746582, "The Swath Width of the ScanSAR-2 Mode is 200 x 2500 km."]
[6.639500141143799, 0.3787727952003479, "The Retirement Date of the CBERS-1 Satellite is Aug. 2003."]
[9.204249382019043, 9.133840560913086, "The Field of View of the Optics Device is 10\u00ba."]
[8.914657592773438, 2.4265944957733154, "The Survey of the Herschel Space Observatory is Hi-GAL, the Herschel infrared Galactic Plane Survey."]
[8.801419258117676, 0.2184375375509262, "The Expected Orbit Duration of the Skylab-1 Space Station is 8-10 years."]
[6.7009429931640625, 1.7433173656463623, "The Mission End Date of the Envisat Satellite is May 9, 2012."]
[7.472997665405273, 8.429099082946777, "The MTF at Nyquist Frequency of the Spacecraft Satellite is > 10% for Pan."]
[6.660394668579102, 3.5843722820281982, "The Mission Type of the Deimos-1 Satellite is Fully Commercial EO Mission."]
[7.646549224853516, 0.3875148594379425, "The Launch Date of the Meteor-2-1 Satellite is 11.07.1975."]
[4.706665992736816, 5.700926780700684, "The Radio Glitch of the AeroCube-3 Satellite is The satellite radio suffered a glitch where it would not acknowledge that the ground station was talking to it."]
[6.889331340789795, 2.5607540607452393, "The URL of the PSAT Satellite is http://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=3549&context=smallsat."]
[10.640893936157227, 9.258530616760254, "The Image Capture Location of the CaSSIS Imaging System is 26.8\u00baS/34.8\u00baW."]
[9.410501480102539, 1.4689922332763672, "The Revisit Time of the Satellite Constellation Constellation is Better than 10 hours globally."]
[6.5837931632995605, 0.5713838338851929, "The Data Distribution Start Date of the Meteosat-8 Satellite is 4 October."]
[3.8422601222991943, 5.151702880859375, "The Topology of the FODB Data Interface is Ring."]
[7.117646217346191, 9.335858345031738, "The Resolution of the ScanSAR-2 Mode is 6 x 20m."]
[8.217476844787598, 9.723268508911133, "The Slew Angles of the TeLEOS-1 Imager Imaging Device is Up to \u00b145\u00ba from nadir."]
[1.9514697790145874, 5.3812255859375, "The Output Range of the DAC Digital Analog Converter is 0-5 V."]
[8.366631507873535, 3.734492540359497, "The In-track Separation of the AeroCube-OCSD-B and -C Satellites is 151 meters."]
[4.836737155914307, 0.8626689910888672, "The Development Cost of the EPS-MACCS Satellite Mission is Maximum of \u20ac30 million."]
[6.272636890411377, 0.7420400977134705, "The Program Overview of the CBERS Satellite is URL: http://www.dpi.inpe.br/gilberto/present/cbers_overview.ppt."]
[11.684189796447754, -1.0817419290542603, "The Total Mass of the Secondary Payloads Satellites is 243 kg."]
[4.484169006347656, 4.287224292755127, "The Functionality of the Software System is Networking, file I/O operations, low-level hardware configuration, and many basic commands."]
[9.15373420715332, 9.722259521484375, "The Challenge of the DarkCarb image sensor Photon Detector is Wavelengths to which it is sensitive are emitted by all objects that are at the Earth\u2019s temperature."]
[6.707424163818359, 9.108890533447266, "The Size of the OCM Instrument is 701 mm x 527 mm x 470 mm."]
[10.294929504394531, 1.3334027528762817, "The LTAN of the Spacecraft Satellite is 10:30 hours."]
[4.261785507202148, 6.5128068923950195, "The Downlink Frequency of the RF Communication System Communication System is 437.490 MHz."]
[10.758479118347168, 5.902071952819824, "The Number of X-class flares of the SOHO Satellite is 11."]
[8.109169006347656, 9.44568157196045, "The Ground Resolution of the SiPD Detector is 1m."]
[5.071896076202393, 6.931222438812256, "The Main Beam Efficiency (%) of the Antenna Reflector is 89."]
[1.27704656124115, 4.152973651885986, "The NiCd Batteries of the EURECA Spacecraft is 4 NiCd batteries."]
[8.143329620361328, 8.31008243560791, "The Type of the MAESTRO Instrument is Dual channel optical spectrometer."]
[5.910035610198975, 4.031797409057617, "The Data Policy of the NPOESS Program is Large subset of data available free of charge."]
[0.9179922342300415, 4.228119850158691, "The Capacity of the Battery Power is 12 Ah."]
[8.877363204956055, 9.540772438049316, "The Components of the STP-H6-NISTEx II Hardware is 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."]
[7.721038818359375, 9.117056846618652, "The Spectral Range of the Spectral Band C Spectrometer is 0.62 - 0.68 \u00b5m."]
[9.275627136230469, 0.8819201588630676, "The Mission Lifetime of the Instrument Spectrometer is 7.5 years."]
[4.913817405700684, 3.2552602291107178, "The Housekeeping Computers of the GNB Satellite is 1 ARM7."]
[8.828994750976562, 10.361804962158203, "The Data Type of the CMOS Camera Camera is UYVY, 8 bit."]
[10.7351713180542, 10.33087158203125, "The Leakage current balancing of the PHA Detector is Up to 32 \u00b5A with 10-bit resolution."]
[6.654243469238281, 3.282806873321533, "The Payload of the MPQ442 Satellite is SuperLab."]
[4.547888278961182, 5.667809963226318, "The S-band Downlink of the Spacecraft Satellite is Completed."]
[11.675952911376953, 5.100752830505371, "The Quasi-Periodic Oscillations of the Sw J1644+57 Black Hole is Present."]
[7.0799336433410645, 0.13912098109722137, "The End of Life Date of the Ikonos-2 Satellite is 31 Mar 2015."]
[9.612451553344727, 7.240949630737305, "The Depth Requirement of the Heat Probe Instrument is At least 10 feet (3 meters)."]
[9.141336441040039, 3.334758758544922, "The Orbit Type of the NEMO-AM Satellite is Sun-synchronous orbit."]
[10.422614097595215, 2.70395827293396, "The Perigee of the UK-DMC-2 Satellite is ~ 632 km."]
[8.789336204528809, 8.090456008911133, "The Quantity of the RADFET dosimeters Dosimeters is 2."]
[8.029768943786621, 8.683429718017578, "The Dynamic Range of the Limb Sensor Sensor is 4-5 orders in magnitude variation."]
[8.104506492614746, 9.056904792785645, "The Function of the Low-Frequency Radio Spectrometers Spectrometer is Detect the 21 cm hydrogen line radiation."]
[6.7772016525268555, 7.084283828735352, "The Mission Duration of the CATS Lidar Instrument is 33 months."]
[10.308170318603516, 3.0236449241638184, "The Altitude of the Satellite Communication is 1012 km."]
[9.467690467834473, -0.6325669288635254, "The Spacecraft Controller of the TNS-0 Nanosatellite is Single chip microcontroller (C8051F022) of the Silicon Laboratories Company."]
[7.283748149871826, 2.6203606128692627, "The Publication Date of the Super Dual Auroral Radar Network Radar Network is 2007."]
[7.89022970199585, 0.618992030620575, "The Launch Date of the Starliner Spacecraft is Thursday, May 19."]
[4.776483535766602, 1.9666712284088135, "The Number of Accelerometers of the SloshSat Satellite is 6."]
[6.032464027404785, 9.628480911254883, "The Mass of the Instrument Optical Instrument is 27.7 kg."]
[10.204115867614746, 2.8998520374298096, "The Proposed Altitudes of Operation of the Starlink Satellite Constellation is Between 340 and 614 kilometers."]
[6.890878200531006, 7.0729756355285645, "The Telescope Type of the GOES Sounder Sounder is Cassegrain telescope."]
[4.233221054077148, 5.751110553741455, "The Modulation of the CBERS-1 Satellite is QPSK for HRCC and WFI data streams and BPSK for IRMSS."]
[11.490188598632812, 2.7011148929595947, "The Science Goals of the Psyche Mission Space Mission is 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 typ."]
[8.078743934631348, 5.0212531089782715, "The Geolocation Accuracy of the PROBA-V Mission Satellite Mission is RMSE accuracy <50 m."]
[4.840055465698242, 1.8818517923355103, "The Number of Nanosatellites Launched of the Astrocast Satellite is 5."]
[7.000101089477539, 2.4940526485443115, "The URL of the MidSTAR-1 Satellite is http://www.usna.edu/Satellite/midstar/downloads/ops/MidSTAR-1%20Ops%20Concept.doc."]
[8.129361152648926, 0.8106352686882019, "The Development Timeline of the EPS-MACCS Satellite Mission is From kick-off to launch within three years."]
[6.634547710418701, 3.9653477668762207, "The Mission Type of the Sentinel-6 Satellite is Reference."]
[7.659038066864014, 9.310651779174805, "The Range of the Spectral Bands Sensor is 0.32 - 4.0 \u00b5m."]
[5.374368190765381, 3.7088217735290527, "The Objective of the CAPS SW Software is Provide full autonomous navigation onboard the CAPSTONE spacecraft."]
[6.437382698059082, 3.0555570125579834, "The Principal Investigators of the SMILE Satellite is 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)."]
[5.099611282348633, 5.406669616699219, "The Number of Antennas of the TRACKER Ground Station is Multiple."]
[9.334016799926758, 9.753719329833984, "The Number of Fast Cameras of the PLATO Telescope is 2."]
[5.637663841247559, 3.0366945266723633, "The Innovation Spin-off of the BepiColombo Satellite is Terrestrial industry products."]
[7.3169965744018555, 2.388925790786743, "The URL of the NASA Moon Mission Mission is http://www.jpl.nasa.gov/news/news.php?feature=6662&utm_source=iContact&utm_medium=email&utm_campaign=NASAJPL&utm_content=weekly20161028-5."]
[9.688447952270508, 7.737956523895264, "The Energy: 0.53 keV (2.3 nm) of the O K-edge Atmospheric Cross Section Feature is O at 0.53 keV (2.3 nm)."]
[8.307479858398438, 7.411884784698486, "The Integration of the OB Optical Bench is Instruments are calibrated as stand alone, and once integrated in the OB, an intercalibration and system verification is carried out."]
[7.717629909515381, 7.207827568054199, "The Calibration of the MADRAS Instrument is Unknown."]
[5.0832839012146, 5.0848164558410645, "The Number of Supported Satellite Missions of the KSAT Company is More than 100."]
[8.689934730529785, 10.048026084899902, "The Subaperture Area Percentage of the PAIS Imaging System is Above some value."]
[7.713818073272705, 13.595959663391113, "The No. of Bins of the SPIM5 Spectrometer is 68, 136, or 272."]
[9.837440490722656, 4.8731536865234375, "The Firing Pressure of the Y-axis Bang-Bang Maneuver Satellite Maneuver is 1.62 bar."]
[2.16925311088562, 4.06309700012207, "The Deployable Solar Array Angle of the UK-DMC-2 Satellite is 110\u00ba."]
[7.596103191375732, 4.8751373291015625, "The Mission of the BeeSat Satellite is Berlin Experimental Educational Satellite."]
[9.337224006652832, -0.5182069540023804, "The Mission Status of the TechnoSat Nanosatellite is Operational (extended)."]
[9.037619590759277, 3.646475076675415, "The Orbit Position of the BeiDou-1B Satellite is GEO, 80\u00ba E."]
[8.759583473205566, 7.205125331878662, "The Principal Investigator of the IMPACT Instrument is Janet G. Luhmann."]
[7.856055736541748, 2.8846659660339355, "The Detection of the Debris Cloud Space Object is Mid-2018."]
[4.974338531494141, 6.690431118011475, "The Gain of the Antenna Communication System is 15 dBi per polarization."]
[5.42303991317749, 0.31227928400039673, "The Containment of the Cooks Peak fire Wildfire is 72 percent."]
[3.6394083499908447, 3.534144878387451, "The Purpose of the CICERO-4 Satellite is Weather satellite."]
[13.07110595703125, 4.092794895172119, "The Purpose of the Gaia Satellite is Precisely measuring the distance and movement of more than a billion stars in our galaxy."]
[6.01158332824707, 1.989723801612854, "The Launch Site of the AeroCube-4 Satellite is VAFB, CA."]
[8.680608749389648, 7.827231407165527, "The Cadence of the Thermal Neutron Counts Measurement is 5 minutes."]
[9.253875732421875, 0.8147678375244141, "The Testing Duration of the GaN-based Power Transistors Transistors is More than 3000 hours."]
[7.850480556488037, 4.502350330352783, "The Multispectral Bands Ground Resolution of the WorldView-3 Satellite is 1.24 m."]
[6.485547065734863, 6.236621856689453, "The SFE of the ASCAT Scatterometer is Scatterometer Front End."]
[7.460127830505371, 8.077025413513184, "The Altitude Range of the Atomic Oxygen (AO) Density Measurement Device Instrument is 180-200 km."]
[5.3380045890808105, 5.892331600189209, "The Design of the Antenna Dish Satellite Component is Rib consists of an inner and outer portion, connected by a spring-loaded hinge joint."]
[10.022512435913086, -0.6524825692176819, "The Altitude of the Tsubame Microsatellite is 504 km."]
[8.273209571838379, 4.369720458984375, "The Purpose of the Integral Satellite is Observing particles thrown off by extreme phenomena such as black holes, neutron stars, and supernova explosions."]
[10.331579208374023, 2.9203848838806152, "The Orbit Altitude of the 3U CubeSat Satellite is 505 km."]
[6.499685287475586, 8.19904899597168, "The Brightness Temperature Stability of the MWR Dicke Radiometer is 1 K."]
[9.292176246643066, 6.04923677444458, "The Nominal Angular Momentum of the MW Momentum Wheel is 0.125 Nms."]
[8.821610450744629, 3.3194546699523926, "The Deployment Orbit of the OG2-1 Satellite is Lower than intended."]
[6.3247857093811035, 7.701499938964844, "The Laser Diodes Power of the SILEX Terminal is 60 mW."]
[3.5534660816192627, 6.534628868103027, "The S-band TxRx Data Rate (TC) of the RF communications Communication System is 64 kbit/s."]
[7.431421756744385, 6.729503631591797, "The Instrument of the TEMPEST-D Satellite is Radiometer."]
[9.640979766845703, 1.3105895519256592, "The Science Data Duration of the Colorado Student Space Weather Experiment (CSSWE) Satellite is 3 weeks."]
[4.995094299316406, 4.932824611663818, "The Back-up Ground Station of the IXPE Observatory Satellite is NEN ground station in Singapore."]
[8.214089393615723, 9.138148307800293, "The Photometric Sensitivity of the Instrument Sensor is 0.75 counts /s /Rayleigh /1\u00ba pixel."]
[3.981574535369873, 5.633486747741699, "The Downlink Rate of the ResourceSat-1 Satellite is 1-16 kbit/s."]
[7.456493377685547, 3.2290191650390625, "The Sensor Complement of the Solar-B / Hinode Satellite is Unknown."]
[11.518409729003906, 6.367818832397461, "The Catalog Use of the XMM-Newton X-ray Satellite is Get new information about their research objects and to search for rare and as yet unknown sources of X-rays."]
[7.8637776374816895, 7.51800012588501, "The Sensor Type of the ECOSTRESS Instrument is Radiometer."]
[8.047663688659668, 4.611415386199951, "The Photometric Precision of the PicSat Satellite is Sub-milimag."]
[9.379355430603027, 0.8075916171073914, "The Nominal Lifetime of the Sentinel-6 Satellite is 5.5 years."]
[10.577248573303223, 8.57292366027832, "The CCD Detectors of the COR1 Coronagraph1 imager is EEV 42-40, 2k x 2K, 13.5 \u03bcm pixels, backside illuminated, AR coated (except EUVI), >100 k e -  full well."]
[9.48417854309082, 5.955611705780029, "The Pointing Accuracy of the ADCS Attitude Determination and Control System is \u00b13\u00ba."]
[3.3859751224517822, 5.288686752319336, "The Onboard Data Storage of the Spacecraft Satellite is 128 GB."]
[2.2569055557250977, 4.5057597160339355, "The Array Power Peak of the Spacecraft Bus (Avionics Module=AM) Satellite is 790 W."]
[9.526761054992676, 9.02537727355957, "The Elevation/Azimuth Coud\u00e9-mount Telescope Size of the OCTL Telescope is 1 m."]
[8.56541919708252, 10.068826675415039, "The Detector Unit Components of the MSASI Imager is High speed CMOS image sensor and an image intensifier."]
[6.147181510925293, 9.293509483337402, "The Mass of the Herley MD2000C-1 Transponder Module is 425 gram."]
[6.549897193908691, -0.07302931696176529, "The Launch Date of the PSLV-C37 Satellite Launch Vehicle is Unknown."]
[8.677045822143555, 8.892705917358398, "The Ellipse Axis C of the Long Wavelength Band Spectrometer is 242.6 mm."]
[6.356877326965332, 4.976497173309326, "The Image Re-sampling Methods of the Product Level 1C (L1C) Data is Bi-cubic convolution interpolation and nearest neighbor."]
[4.13010311126709, 5.551091194152832, "The Data Compression of the TTTC Imaging System is Optional."]
[6.900240898132324, 5.400820732116699, "The New Applications of the SMOS Satellite is Permafrost and thawing monitoring in the boreal forest, ice thickness determination in the Arctic Ocean, hurricane wind observations."]
[4.958291053771973, -3.1751155853271484, "The | of the Tim Fuller-Rowell, Mihail Codrescu, Bela G. Fejer, W. Borer, F. Marcos, D.N. Anderson Authors is Tim Fuller-Rowell, Mihail Codrescu, Bela G. Fejer, W. Borer, F. Marcos, D.N. Anderson."]
[6.405117034912109, 9.89421272277832, "The Instrument mass of the Optical System Imaging System is 120 kg."]
[3.9431378841400146, 4.401690483093262, "The Task of the OBC On-Board Computer is Marshalling of images from the smartphone, via the HPC to the transmitter."]
[5.424229621887207, 0.30597007274627686, "The Containment of the Cerro Pelado fire Wildfire is 10 percent."]
[3.132420778274536, 6.800877571105957, "The Output Power of the MHX-2400 S-band Transmitter/Transceiver is 30 dBm."]
[11.679656982421875, 4.512974262237549, "The Type of the HD 93396 Star is Subgiant yellow."]
[6.33162784576416, 3.911717176437378, "The Display Location of the Copernicus Sentinel-6 Satellite is IAGB space test center in Ottobrunn near Munich."]
[6.995065689086914, 1.1677230596542358, "The EFI Deployment Completion Date of the THEMIS Constellation Satellite Constellation is 14 January 2008."]
[8.548810958862305, 4.331478595733643, "The Visual Magnitude Limit of the BRITE Satellite is +3.5."]
[7.788114070892334, 9.811633110046387, "The Spectral Band of the Band Photometers Photometer is 762.4 nm."]
[9.764184951782227, 1.4004400968551636, "The Time of the Spacecraft Stabilization Process is 2.5 minutes."]
[6.605629920959473, 7.505309104919434, "The Objective of the LALT Laser Altimeter is Measure the vertical distance between the Main Orbiter and the subsatellite point on the lunar surface."]
[6.074612140655518, 6.245143413543701, "The Radiometric Resolution of the SAR Synthetic Aperture Radar is 5-bit raw data."]
[7.489480972290039, 5.244661331176758, "The Image Credit of the Orbiting Carbon Observatory-2 (OCO-2) Satellite is NASA/JPL-Caltech/University of Utah."]
[7.487021446228027, 7.452198028564453, "The Detection Capability of the OMI Satellite Instrument is Emissions Changes."]
[9.125509262084961, 1.0515806674957275, "The Orbit Duration of the LRO Spacecraft is Four Years."]
[9.217148780822754, 5.210251808166504, "The Torque Coil Power of the Canopus Pipper Satellite is ~ 500 mA."]
[7.653900146484375, 1.0097097158432007, "The Launch Date of the Sentinel-6A Satellite is November 2020."]
[5.2435455322265625, 4.053725242614746, "The Operation Mode of the SMOS Satellite is Autonomous mode using the FDIR (Failure Detection Isolation and Recovery) concept."]
[8.413850784301758, 1.2926305532455444, "The Data Collection Date of the GOCI Geostationary Ocean Color Imager is May 12, 2016."]
[7.661782741546631, 7.627213478088379, "The Sunphotometers of the SOVA Experiment is Degradation in Space."]
[9.224430084228516, 0.8865360617637634, "The Orbit Duration of the SMOS Satellite is Almost 1 Year."]
[12.628259658813477, 6.91878604888916, "The Pulse period (ms) of the B1758-250 Pulsar is 3.000."]
[5.83041524887085, 2.996904134750366, "The Operator of the UWE-1 Satellite is Student team at the University of W\u00fcrzburg."]
[7.636951446533203, 5.549381732940674, "The Cal_solar data Collection of the OCO-2 Satellite is Spectral Wavelength Calibration."]
[6.190246105194092, 2.7033421993255615, "The Chief Strategy Officer of the HawkEye 360 Company is Kari Bingen."]
[6.747291564941406, 4.811974048614502, "The Instrument of the CO2M Satellite is Near-infrared and shortwave-infrared spectrometer."]
[5.116175651550293, 5.445703029632568, "The Band Frequency of the Starlink Satellite Constellation is 10.7 GHz to 12.7 GHz."]
[8.162259101867676, 5.6936140060424805, "The Tuning of the Focal Plane Skew Settings of the R3 System Satellite is Possible cause of noise in the NIR band."]
[8.40179443359375, 9.972404479980469, "The Array Size of the Detector Optical Instrument is 256 x 256 pixels."]
[7.514586448669434, 1.0478006601333618, "The Experiment Date of the ETS-VII Satellite is March 14, 2000."]
[7.442924976348877, 7.4435577392578125, "The Data Source of the OMI (Ozone Monitoring Instrument) Instrument is OMI (Ozone Monitoring Instrument) on NASA\u2019s Aura satellite."]
[3.8351893424987793, 4.375265598297119, "The Type of the SCIP Processor is Stack based."]
[7.069394111633301, 1.478571891784668, "The Meeting Date of the GMES Sentinel-3 Satellite is 18-20 January 2010."]
[5.764352321624756, 1.6644915342330933, "The Additional Component of the GomX-4B Satellite is Extra transceiver in the Software Defined Radio for ISL operations."]
[1.0576146841049194, 4.26572322845459, "The Quantity of the NiH2 batteries Power Source is 4."]
[11.011612892150879, 4.894987106323242, "The Journey Time to Earth of the Solar Energetic Particles Space Weather Phenomenon is Under an hour."]
[7.225372791290283, 5.667162895202637, "The Alkalinity of the Marine Chemistry Study Parameter is Unknown."]
[3.65411639213562, 6.1913533210754395, "The Uplink Speed of the Communication links Communication subsystem is 9.6 kbit/s."]
[10.901934623718262, 2.0442922115325928, "The \u0394RAAN of the Swarm-A (Alpha) Satellite is 1.4\u00ba difference between A and B."]
[6.7751922607421875, 4.336424827575684, "The Mission Scenario of the DLR SAR Satellite is Climate research and environmental monitoring."]
[4.474582195281982, 4.159750461578369, "The Origin of the SPA Architecture is Expanded and refined from the appliqu\u00e9 sensor network."]
[6.945769309997559, 3.699695110321045, "The Expected Outcome of the TEPCE Satellite is New propulsion capability for spacecraft."]
[6.183795928955078, 6.155134201049805, "The Mode of the SAR Sensor Subsystem SAR Sensor is HR (High Resolution)."]
[4.913050651550293, 2.0420501232147217, "The Quantity of the Secondary Payloads Nanosatellites and CubeSat is 4 nanosatellites and 1 CubeSat."]
[10.406166076660156, 5.516233444213867, "The Tether Length of the TEPCE Satellite is 1 km."]
[7.847562313079834, 8.514928817749023, "The Citation of the SOLSPEC Spectrometer is 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."]
[10.042461395263672, 1.5930759906768799, "The Formation of the Equatorial Ridge Surface Feature is During a period when it only took Ryugu 3 hours to rotate."]
[5.552350044250488, 4.637269496917725, "The Data Processor Developer of the GOME Instrument is German Remote Sensing Data Center (DFD) of DLR."]
[9.132086753845215, 10.855195045471191, "The Swath Width of the TAC Camera is 51 km."]
[7.5327582359313965, 2.8857107162475586, "The Operation Status of the KOMPSAT-5/Arirang-5 spacecraft Satellite is Nominal."]
[7.953082084655762, 10.290020942687988, "The Revisit Time at 1 m - 0.5 m GSD of the WV60 imager Imaging System is 1.7 days."]
[3.635239362716675, 4.585754871368408, "The Timer Validity of the MOBC Main On-board Computer is 200 days."]
[8.172799110412598, 2.3652050495147705, "The Mission Type of the SOHO Satellite is Solar Study."]
[5.356575012207031, 1.5943701267242432, "The Original Manifest of the Falcon-9 CRS-2 Rocket is ELaNa-4 CubeSats."]
[6.5984673500061035, 4.268895149230957, "The Data Policy of the Copernicus Space Component Satellite Component is Open access to Sentinel data by anybody and for any use."]
[8.026784896850586, 9.581265449523926, "The Wavelengths of the SPIRE Far-infrared camera is 160 \u00b5m (green)."]
[3.852031707763672, 2.3077609539031982, "The Size of the LICIACube CubeSat is Hand-sized."]
[7.202463626861572, 8.851401329040527, "The Footprint Size of the CNSCAT Scatterometer is 19 km x 24 km."]
[11.491524696350098, 4.261282444000244, "The Rotation Period of the Stars Celestial Bodies is Ranged from one to as many as 11 Earth-days."]
[6.734676837921143, 1.3142236471176147, "The Date of the Data Distribution Policy Agreement Agreement is 2008."]
[6.728681564331055, 3.080207586288452, "The Operational Status of the PhoneSat 2.5 Satellite is Operational."]
[10.012067794799805, 1.5380865335464478, "The Period of the ExoMars Orbiter Satellite is ~2 hours."]
[7.203935146331787, 1.6279634237289429, "The Symposium Location of the WatER Satellite Mission is Venice, Italy."]
[8.017311096191406, 4.635593414306641, "The Multispectral Resolution of the EROS-C Satellite is 2.8 m GSD."]
[9.609854698181152, 0.9954464435577393, "The Time in Spacecraft of the Valves Spacecraft Component is 46 days."]
[9.728131294250488, 8.995555877685547, "The Secondary Mirror Size of the Telescope Telescope is 0.3 m."]
[6.239978313446045, 2.7526118755340576, "The Developer of the TransHab Space Habitat is William Schneider."]
[6.2890472412109375, 2.7865824699401855, "The Development Team of the BioSentinel Satellite is Hugo Sanchez, James Chartres, Robert Hanel, Sharmila Bhattacharya, Antonio Ricco."]
[8.516587257385254, 7.543518543243408, "The Temperature Control of the OBA Instrument Component is Yes."]
[8.379164695739746, 4.603559970855713, "The Swath Width of the Spacecraft Satellite is 23 km."]
[9.413783073425293, 8.825857162475586, "The Type of the Telescope Optical Instrument is Zeiss 1 m \u2205 Ritchey-Chr\u00e9tien/Coud\u00e9 telescope."]
[10.268990516662598, 8.733651161193848, "The Telescope Optics of the EUVI Extreme Ultraviolet Imager is Fully baffled."]
[10.213691711425781, 6.92977237701416, "The Function of the TET Radiator Thermal Interface is Allows the complete radiation of all thermal energy into free space during the \"hot\" phases."]
[8.997878074645996, 9.9164457321167, "The Function of the PIC Device is Create images of extended scenes."]
[9.292057037353516, 5.516425609588623, "The Attitude Control of the Bus Satellite Bus is Control using magnetorquers only, except short term."]
[8.505463600158691, 4.650350093841553, "The Energy Dissipation Location of the Cluster Satellite is Swirling vortices, or O-lines."]
[9.605940818786621, 6.009856700897217, "The Components of the ADCS Attitude Determination and Control Subsystem is 3-axis gyro sensor, 3-axis magnetometer, sun sensor, Earth sensor."]
[9.444290161132812, 9.355069160461426, "The Number of Holes of the Optical Head Optical Device is 1 / 100 (enhanced configuration)."]
[6.188969135284424, 8.106637001037598, "The Frequencies of the MM Radiometer Sensor is 89, 165, 176, 180 and 182 GHz."]
[8.128071784973145, 8.296335220336914, "The Measurement of the Imaging Spectrometer Instrument is Visible and infrared light reflecting from surfaces below."]
[9.443500518798828, 5.815672397613525, "The Winding of the Torque Rods Attitude Control is Dual-wound."]
[6.4150004386901855, 4.018182277679443, "The Project of the SumbandilaSat Satellite is 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."]
[10.269404411315918, 4.543888568878174, "The Propulsion System Performance of the Advanced Composition Explorer Spacecraft is Nominally for the first 16 years of the mission."]
[8.265275001525879, 4.55574369430542, "The Swath Width of the Satellite Imaging Satellite is 80 km."]
[5.88175106048584, 6.754730224609375, "The Antenna Position of the SIR-C Radar System is 38\u00ba."]
[10.359416007995605, 4.84033727645874, "The Operation Hours of the Ion Engine Propulsion System is 1346 hours."]
[6.779182434082031, 1.748499870300293, "The Mission Design of the RapidEye Satellite is G. Tyc, J. Tulip, D. Schulten, M. Krischke, M. Oxfort."]
[6.591278076171875, 3.597130298614502, "The Mission Type of the IMAGE Satellite is EO."]
[10.350698471069336, 5.248927116394043, "The Quantity of the Commercial Off-the-Shelf (COTS) Air Tanks Hardware is Sixteen."]
[7.764893531799316, 3.7844629287719727, "The Volcano Status of the Hofsj\u00f6kull Glacier is Largest active volcano in Iceland."]
[5.0075788497924805, -0.1577296257019043, "The Service Availability of the OneWeb Satellite Constellation is Before the end of the year."]
[10.302074432373047, 2.979094982147217, "The Mission Altitude of the MicroSat-2b Satellite is 1125 km."]
[8.577353477478027, 4.007852077484131, "The Satellite Dimensions of the Terra Bella Satellite Constellation is 60 x 60 x 95 cm."]
[8.714301109313965, 8.094198226928711, "The NEDT (Noise Equivalent Differential Temperature) at 300 K of the Scanning geometry Instrument is Band 4 - Band 5 - Band 6 \u2264 1 K \u2264 0.2 K \u2264 0.2 K."]
[8.342053413391113, 2.6817617416381836, "The Orbit Coverage of the JPSS Satellite Program is Global."]
[8.557127952575684, 3.8621888160705566, "The Celestial Sphere Coverage of the Spacecraft Satellite is 64% during the first two years of the mission."]
[11.156713485717773, 2.77561354637146, "The Elliptical Orbit Dimensions of the Lunar Landing Vehicle Vehicle is 100 km x 15 km."]
[11.168200492858887, 9.33901596069336, "The Thermal Operating Range of the Earth Radiation Budget Experiment (ERBE) Instrument is 38\u00b10.1\u00baC (detectors)."]
[9.333823204040527, 6.401942253112793, "The Location Accuracy of the Autonomous star tracker Star Tracker is Less than 50 m."]
[4.1549787521362305, 3.706826686859131, "The Peak Detection Rate of the Simple Receiver AIS Receiver is Not tabulated."]
[8.755544662475586, 8.642251014709473, "The Material of the HiRAIS Optical Instrument is CFRP."]
[12.117775917053223, 5.357754230499268, "The Hypothetical Energy Component of the Dark Energy Cosmology is Unknown."]
[10.034233093261719, 1.5066174268722534, "The Period of the Resurs-P1 Satellite is 94 minutes."]
[7.446397304534912, 9.673319816589355, "The Instrument Power of the ERIP Earth Remote-Sensing Imaging Package is 3 W."]
[7.805295944213867, 8.539631843566895, "The Visible Spectral Range / Bandwidth of the SOLSPEC-ATLAS Spectrometer is 350-880/1.4/1."]
[9.51890754699707, -0.6717832088470459, "The Website of the Kolibri-2000 Microsatellite is http://www.energia.ru/english/energia/sci-education/microsat/microsat-02.html."]
[6.087942600250244, 6.662825584411621, "The Frequency Band of the AltiKa Radar Altimeter is Ka-band."]
[7.3830437660217285, 7.892100811004639, "The Precision of the Ozone Measurement Instrument Atmospheric Measurement Device is 3%, 15-50 km."]
[9.610465049743652, -0.5995072722434998, "The Avionics Components of the Microsatellite Satellite is Four boards for C&DH, and power."]
[5.053791522979736, 6.688172340393066, "The Gain of the Yagi Antenna Antenna is 7.5 dBi."]
[3.2242021560668945, 4.839030742645264, "The Memory of the OBC On-Board Computer is 16 MByte."]
[6.590045928955078, 7.6665191650390625, "The Pumping Scheme of the Laser Device is Unknown."]
[10.22036361694336, 2.9946439266204834, "The Altitude of the ResourceSat-2 Satellite is 817 km."]
[5.949450969696045, 2.937115430831909, "The PI of the SORCE Satellite is G. J. Rottman."]
[7.181150436401367, 7.258925914764404, "The Spectral Bands of the VIIRS Instrument is 22."]
[6.835517883300781, 2.764810562133789, "The Website of the TUBSAT Satellite is http://www.raumfahrttechnik.tu-berlin.de/tubsat."]
[8.97485637664795, 1.2873696088790894, "The Mission Duration of the Van Allen Probes Satellite is 3 years."]
[4.157614707946777, 3.7168290615081787, "The Global Average Detection Rate of the Simple Receiver AIS Receiver is 2 to 3 Messages/s."]
[11.419475555419922, 3.9033331871032715, "The Gravity of the Mars Planet is About one-third that of Earth\u2019s."]
[9.051539421081543, 5.159719944000244, "The Attitude Variation During Docking Operations of the ISS Satellite is Several degrees."]
[12.079741477966309, 3.276108503341675, "The Inclination of the Secondary Payloads Satellites is ~51.6\u00ba."]
[8.077482223510742, 8.582389831542969, "The Components of the FGS Science Instrument is Two Guider channels and one Near-Infrared Slitless Spectrometer (NIRISS) channel."]
[7.406628131866455, -0.22086778283119202, "The Release Date of the HTV-6 Resupply Ship is January 27."]
[10.168938636779785, 2.9259772300720215, "The Orbit of the MKS-PN2 (Relek) Satellite is Elliptical orbit of 632 km x 824 km."]
[5.373620510101318, 1.3738714456558228, "The First Stage Flights of the Rocket Launch Vehicle is 15."]
[10.175371170043945, 2.9907705783843994, "The Altitude of the OrbView-3 Satellite is ~435 km."]
[6.182737827301025, 3.261598825454712, "The Launch Site of the Galileo FOC-3 and FOC-4 satellites Satellite is Europe's Spaceport (Kourou, ELS) in French Guiana."]
[7.8086466789245605, 3.1605560779571533, "The Launch Status of the Galaxy Spacecraft is Not Launched."]
[10.26404094696045, 2.9955854415893555, "The Orbit Altitude of the Fregat Upper Stage is Around 450 km."]
[8.535821914672852, 8.765592575073242, "The Grating Figure of the Long Wavelength Band Spectrometer is Ellipse of rotation."]
[8.313058853149414, 10.036426544189453, "The Number of Elements of the MS Bands Detector Line Arrays is 1,500."]
[5.094557762145996, 4.398924350738525, "The Communication Network of the Spacecraft Satellite is NASA's Deep Space Network."]
[9.667062759399414, 1.3155523538589478, "The Time Resolution of the IMAP Satellite is Six-month timescales."]
[8.794783592224121, 9.574898719787598, "The Pixel Size of the IFOV Sensor is 44.6 km x 39.3 km."]
[10.528915405273438, 7.48453426361084, "The Material of the Reaction Wheels Satellite Component is Mu-metal."]
[9.834183692932129, -1.0014255046844482, "The Swath Width of the JL-1-GF03B Microsatellite is 17 km."]
[11.264912605285645, 6.68695068359375, "The XNAV Type of the SEXTANT Technology Demonstration is X-ray Pulsar-based Navigation."]
[6.9113664627075195, 0.40874534845352173, "The Launch Date of the GEOS-3 Satellite is 9 April 1975."]
[9.008138656616211, 2.4592435359954834, "The Observation Distance of the Herschel Telescope is Within 1500 light years from the Sun."]
[9.128581047058105, 7.078808784484863, "The Challenges of the Langmuir Probe Plasma Measurement Device is Ground handling equipment and testing methods."]
[8.553152084350586, 4.38072395324707, "The Average Spacing of the GNOS-2 Satellite is 710 km."]
[4.39381217956543, 6.665013790130615, "The Chirp Generation Method of the Ty module Module is Direct digital synthesis at an IF of 150 MHz."]
[6.313811302185059, 8.258118629455566, "The Type of the SMMR Instrument is Scanning Multichannel Microwave Radiometer."]
[7.5704545974731445, 8.265902519226074, "The Range of the NGAVGS Sensor is Up to 3000 meters."]
[7.9925994873046875, 2.4279539585113525, "The URL of the Star-circling bubble of gas Unknown is http://m.esa.int/spaceinimages/Images/2018/06/Star-circling_bubble_of_gas."]
[9.716402053833008, 8.9752836227417, "The Primary Mirror Size of the Telescope Telescope is 3.5 m."]
[7.053390979766846, 4.730929374694824, "The | Very high-resolution imagery and machine learning of the Trees Mapping Method Mapping Method is The use of very high-resolution imagery and machine learning represents a significant breakthrough."]
[9.475298881530762, 1.7702375650405884, "The Global Scan Frequency of the NISAR Satellite is Every 12 days."]
[8.846378326416016, 3.1802849769592285, "The Orbit Type of the Viasat Satellite Operator is Geostationary."]
[4.424685001373291, 3.6942336559295654, "The Frequency Band of the AIS Automatic Identification System is VHF."]
[4.756106376647949, 0.8685580492019653, "The Total Cost of the LEO Constellation Satellite Constellation is $5 billion."]
[8.414834022521973, 4.703042984008789, "The Unique Capability of the Cluster Satellite Mission is Allows multipoint measurements of the magnetosphere in different regions and at different scales."]
[4.618271350860596, 0.20126724243164062, "The Total Satellites in Orbit of the OneWeb Satellite Constellation is 182."]
[5.728652000427246, 0.9010754227638245, "The Airlock Cycle Dates of the NanoRacks CubeSat Deployer Missions CubeSat Deployer is May 16-17, 2017."]
[5.758572578430176, 1.3409759998321533, "The Launch Site of the SpaceX CRS-19 Mission is Space Launch Complex 40 (SLC-40) at Cape Canaveral Air Force Station, Florida."]
[4.831172943115234, 8.986523628234863, "The Number of Detected Marsquakes of the InSight lander Seismic Instrument is More than a thousand."]
[9.787453651428223, 7.1404547691345215, "The Conference Date of the Supercapacitors Energy Storage is 2011."]
[3.0102152824401855, 6.564444065093994, "The Transmitting Power of the Iris Radio Communication Device is 2 W."]
[6.287843227386475, 1.310186743736267, "The Readiness Date of the EUMETSAT ground segment Ground Segment is 5 December 2017."]
[4.051657199859619, 5.757955551147461, "The Data Rate of the Satellite Satellite is 25 Mbit/s."]
[3.662332534790039, 3.507699489593506, "The Partnership Date of the CICERO Satellite System is Dec. 4, 2009."]
[9.446593284606934, 8.836376190185547, "The Components of the TOU Telescope Optical Unit is 6 lenses."]
[6.797744274139404, 5.556267738342285, "The Soil Moisture Refresh Rate of the SMAP Satellite is 3 days."]
[8.856677055358887, 6.706370830535889, "The Gyro Tilt Detection of the SQUID Magnetometer is 0.1 milliarcseconds."]
[6.7864089012146, 1.2635184526443481, "The Meeting Date of the NPOESS Satellite System is Sept. 29 to Oct. 3, 2008."]
[6.871387004852295, 5.415448188781738, "The Mission of the SMOS Satellite is Soil Moisture and Ocean Salinity."]
[12.116053581237793, 2.2083165645599365, "The Principal Investigator of the OSIRIS-REx Spacecraft is Dante Lauretta."]
[8.443429946899414, 8.712870597839355, "The Optical Windows Coatings of the Instrument Spectrometer is Broadband AR coatings with R < 2%."]
[3.92631459236145, 4.380015850067139, "The Base carrier board of the C&DH subsystem Onboard Computer System is Contains all the peripheral ports."]
[5.734374046325684, 3.395740270614624, "The Institute of the CIP Payload is NCU (National Central University), Taiwan."]
[7.6560845375061035, 8.626324653625488, "The Chopper Wheels Frequency of the SBUV Spectrometer is 25 Hz."]
[6.045459270477295, 4.019802093505859, "The Royal Institute of Technology in Stockholm, Sweden of the Odin Mission Archive Location is The archive of the Odin mission is located at the Royal Institute of Technology in Stockholm, Sweden."]
[4.966738224029541, 6.658544540405273, "The Gain of the TEC Antennas Antennas is Not less than 45 dB."]
[5.549463748931885, 3.3303980827331543, "The Operator of the CPOD Service Data Service is GMV-led consortium of Spain."]
[3.6094295978546143, 6.349195957183838, "The Data Transmission Rate of the S-band Communication Band is 1 Mbit/s."]
[6.4780964851379395, 2.140315055847168, "The Presentation of the NROL-36/OUTSat Satellite is Workshop."]
[3.4337570667266846, 4.749148368835449, "The Memory of the AIM Reconfigurable Computing Hardware Device is 128 k x 16 EEPROM for boot and application code."]
[-4.981231689453125, 4.407580375671387, "The Support Phase Time Period of the Mango Tango Satellite Formation is 11.08 to 08.09.2010."]
[11.605070114135742, 6.212414741516113, "The Mission Extension Approval Date of the XMM-Newton X-ray observatory is November 20, 2014."]
[4.84938383102417, 2.130079746246338, "The Payload Number of the Inmarsat S EAN Satellite is Ninth."]
[7.519016265869141, 2.865908145904541, "The Country of Origin of the KOMPSat-5 Satellite is South Korea."]
[7.094533920288086, 1.4241511821746826, "The Presentation Date of the MERLIN Climate Mission is Oct. 3-7, 2011."]
[3.321988821029663, 4.4434990882873535, "The Control Function of the PCU Power Control Unit is Controls the power supply subsystem."]
[3.425943374633789, 4.703042984008789, "The Microprocessor Speed of the RAD750 SBC Single Board Computer is 132 MHz."]
[9.482987403869629, 9.11941909790039, "The Aperture of the FUV Channel Telescope Channel is ~380 mm."]
[3.7258265018463135, 6.230447769165039, "The Data Rate of the Ka-band telecom system Telecom System is 3.5 Gbit/s."]
[11.391046524047852, 1.0433504581451416, "The Landing Technology Status of the Tianwen-1 Mars Lander is Ready for 2020."]
[4.094303607940674, 3.1644082069396973, "The Deployment Options of the Open5GCore Rel. 4 5G Core Network is Containers or virtual machines on top of a large number of virtualization environments."]
[7.145454406738281, 6.255319118499756, "The Sensor Description and Mission Overview of the WindSat Spaceborne Polarimetric Radiometer is The WindSat Space Borne Polarimetric Microwave Radiometer: Sensor Description and Mission Overview."]
[6.924263954162598, 8.709716796875, "The Swath width of the VIRR Visible and Infrared Radiometer is 2800 km."]
[8.078693389892578, 4.583782196044922, "The Spatial Resolution of the Ice sheets Rock basement Satellite is 50-100 km."]
[7.522326469421387, 1.9689792394638062, "The Event of the Incheon Glacier Memorial Glacier is Meeting of the IPCC to consider the special report of global warming of 1.5\u00b0C in 2015."]
[7.408341884613037, -0.2538602650165558, "The Berth Duration of the Kounotori H-II Transfer Vehicle is Until November."]
[5.333148956298828, 6.89002799987793, "The Beamwidth of the Antenna Satellite Component is 2.2\u00ba (Nyquist-sampling in both along-scan & down-track directions)."]
[5.608866214752197, 1.912381649017334, "The Payload Fairing Material of the Minotaur Launch Vehicle is Carbon fibers and epoxy."]
[1.2553352117538452, 4.156054973602295, "The Battery of the QuickBird-2 Satellite is 40 Ah NiH2."]
[9.176634788513184, 5.535287857055664, "The Gyroscopic Attitude Control Channels of the Electro-L Satellite is 4."]
[7.603389739990234, 6.611079692840576, "The Required Precision of the AAOD Satellite Instrument is 0.03."]
[7.362005233764648, -0.646144688129425, "The Deployment Date of the CYGNSS Satellite Constellation is Dec. 15, 2016."]
[8.916280746459961, 1.6677454710006714, "The Extended Mission Duration of the Juno Spacecraft is Through September 2025."]
[9.72850513458252, 6.993483543395996, "The Thermal Operational Range of the Instrument Satellite Instrument is 0 / +20\u00baC."]
[6.781932353973389, 5.89878511428833, "The Data of the RapidScat Satellite is Semi-diurnal differences."]
[9.130684852600098, 10.619885444641113, "The Operation Periods of the VWFC Camera is Orbits 84 to 91, 94 to 96, and 98."]
[8.062843322753906, 10.537629127502441, "The Algorithms of the Instrument Computer Data Processing is Lossless (2:1 Rice compression) and lossy (JPEG)."]
[8.286385536193848, 2.138488531112671, "The Solar Cycle Observation of the SOHO Satellite is 24."]
[5.289596080780029, 3.8957061767578125, "The Function of the Remote Agent Software is Planned DS1 activities on-board and carried out the plan without ground intervention."]
[7.84993314743042, 4.007978439331055, "The Ice Thickness of the Landsat 8 Satellite is 12 to 28 inches (30 to 71 cm)."]
[7.064368724822998, 0.3229878544807434, "The Launch Date of the ZY-3 Satellite is January 9, 2012."]
[4.980473041534424, 4.758319854736328, "The Purpose of the KE Ground Station Ground Station is Support the singular KE Block I satellite."]
[11.514119148254395, 6.352704048156738, "The Data Archive of the XMM-Newton X-ray Telescope is Rich."]
[10.261030197143555, 4.940666198730469, "The Main Engine Thrust of the ExoMars TGO Orbiter is 424 N."]
[3.1190693378448486, 6.801962852478027, "The RF Output Power of the EWC31 S-band transceiver module Communication Module is +27 to +33 dBm."]
[9.036623001098633, 4.101758003234863, "The Dimensions of the GNB Satellite Platform is 20 cm side length."]
[5.472592353820801, 7.970905303955078, "The Optimum Bandwidth of the Etalon Filter is 80-120 m\u00c5."]
[5.755458354949951, 2.72113037109375, "The Manufacturer of the Iridium NEXT Satellite Constellation is Thales Alenia Space."]
[8.553865432739258, 10.14940357208252, "The Application of the CMT Imager is Localized Real-Time Security Assessment."]
[3.6276514530181885, 6.67239236831665, "The Data Rate of the X-band transmitter Transmitter is Up to 384Mbit/s."]
[7.469546794891357, 2.4586637020111084, "The URL of the Rosetta Satellite is http://www.esa.int/Our_Activities/Space_Science/Rosetta/Rosetta_overview."]
[9.435534477233887, 1.8605438470840454, "The Orbit Frequency of the Space Station Satellite is About 16 times per day."]
[10.429015159606934, 2.7378315925598145, "The Closest Distance to ISS of the SZ-7 Spaceship is Within 47 km."]
[7.675959587097168, 7.051438808441162, "The Data Processing of the RPW Radio and Plasma Waves Instrument is Relatively easy and quick once behavior is known."]
[9.030037879943848, 0.39324361085891724, "The ISS Onboard Waiting Period of the MicroMAS-1 Satellite is 8 months."]
[5.9930806159973145, 0.7229114770889282, "The Conference Presentation Date of the PnP Cube Satellite CubeSat is March 3-10, 2012."]
[6.008747577667236, 2.6436259746551514, "The Funding of the MAST Satellite is Combination of private and government research funds."]
[4.108084201812744, 6.683818817138672, "The Clock Frequency of the X-band transmitter Transmitter is 48 MHz."]
[7.257662296295166, 9.727783203125, "The Type of the HISUI Instrument is Hyperspectral and multispectral pushbroom imager."]
[11.147482872009277, 4.049942970275879, "The Drift Speed of the Great Blue Spot Magnetic Anomaly on Jupiter is About 2 inches (4 cm) per second."]
[9.06124496459961, 9.826803207397461, "The Imaging Frequency of the AgCam/ISSAC Imaging System is 2-4 images per orbit for 4 consecutive orbits."]
[8.409849166870117, 8.499744415283203, "The Number of Arms of the Spectrometer Arms Optical Component is 4."]
[9.245999336242676, 3.2186596393585205, "The Orbit Type of the LAGEOS Satellite is Near-circular."]
[10.8739595413208, 5.720657825469971, "The Basis of the Kappa Scheme Flare Prediction Method is Theory of \"double-arc instability,\" a magnetohydrodynamic (MHD) instability triggered by magnetic reconnection."]
[7.341538906097412, 7.09317684173584, "The Percentage of Detections from Vessels without AIS or VMS of the VIIRS Instrument is More than 85 percent."]
[7.065054893493652, 0.25611475110054016, "The Calibration Update of the Ikonos-2 Satellite is 2007."]
[5.920132637023926, -0.2830379009246826, "The Model Building of the Oculus-ASR Satellite is 3D Predictive Satellite Models."]
[5.11024284362793, 4.5018744468688965, "The Mission Scenarios of the Ground Station System is Links to and from aircraft, UAVs, and satellites."]
[6.717841625213623, 4.10863733291626, "The Authors of the NISAR Spaceborne SAR Mission is Paul Rosen, Yunjin Kim, Howard Eisen, Scott Shaffer, Louise Veilleux, Scott Hensley, Manab Chakraborty, Tapan Misra, R. Satish, Deepak Putrevu, Rakesh Bhan."]
[7.1755051612854, 3.0911786556243896, "The Mission Status of the LightSail 2 Satellite is Unknown."]
[11.183694839477539, -1.5214710235595703, "The Mass of the D-SAT CubeSat is 3.5 kg."]
[6.217974662780762, 3.1512770652770996, "The Agency of the CAS500 Satellite is KARI."]
[10.047235488891602, 1.5351229906082153, "The Orbit Period of the Genesis-2 Satellite is 96 minutes."]
[7.876882076263428, 6.267271995544434, "The Calibration of the Calibration Satellite is Total calibration of instrument artifacts <0.5% at top-of-atmosphere."]
[9.276734352111816, 7.771888256072998, "The Operating Temperature of the Near-infrared instruments Instrument is About 30 K."]
[6.770586013793945, 3.140604257583618, "The Operations with 2 satellites of the Dove-2 Satellite is True."]
[7.161468505859375, 1.5300341844558716, "The Symposium Date of the WatER Satellite Mission is March 13-18, 2006."]
[9.933806419372559, 1.399268627166748, "The Signal Reception Time of the MarCO-B Satellite is 11:16 am."]
[8.889182090759277, 5.357040882110596, "The Requirement of the Focus Mechanism Satellite Component is Independent feedback on movement."]
[7.748319149017334, 7.237421989440918, "The Air Quality Prediction Accuracy Improvement of the TEMPO Instrument is 50 percent."]
[11.669852256774902, 6.171377182006836, "The Launch Date of the XMM-Newton Satellite is December 1999."]
[7.5821003913879395, 4.717535972595215, "The Prioritized Science Goals of the ACE Satellite is 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."]
[10.227165222167969, 4.964739799499512, "The Thruster Pairs of the Propulsion Subsystem Propulsion System is 3."]
[6.269454002380371, 3.4609999656677246, "The Office Locations of the Spire Satellite Constellation is San Francisco, Boulder, Washington DC, Cambridge, Ontario, Glasgow, Oxfordshire, Luxembourg, and Singapore."]
[12.106146812438965, 2.20440936088562, "The Mission Status of the OSIRIS-REx Spacecraft is Rehearsal Time for NASA\u2019s Asteroid Sampling Spacecraft."]
[5.794465065002441, 3.1014645099639893, "The Manufacturer of the SPOT 6 Satellite is Astrium."]
[4.274759292602539, 6.757066249847412, "The Up-Conversion Frequency of the Ty module Module is Nominal 5.405 GHz center frequency."]
[7.29663610458374, 8.7543306350708, "The Center Wavelengths of the AATSR Instrument is 0.55 \u00b5m, 0.66 \u00b5m, 0.87 \u00b5m, 1.6 \u00b5m, 3.7 \u00b5m, 11 \u00b5m, 12 \u00b5m."]
[5.645819664001465, 1.632638931274414, "The Manufacturer of the Falcon 9 Launch Vehicle is SpaceX."]
[5.9202961921691895, -0.2751729488372803, "The Ground-Truth Characterization of the Oculus-ASR Satellite is Successful."]
[11.272082328796387, -1.335226058959961, "The Mass of the MicroSat-2b Satellite is 400 kg."]
[9.548237800598145, 5.5006561279296875, "The Stability of the AOCS Attitude and Orbit Control Subsystem is < 5 arcsec/s of the X and Y axis."]
[8.356118202209473, 7.269484996795654, "The Frequency Range of the Field Measurement Device Sensor is DC to 10 Hz."]
[10.737236022949219, 3.511582851409912, "The Distance from Sun at Arrival of the Parker Solar Probe Satellite is 18.8 solar radii (around 8.1 million miles)."]
[8.830802917480469, 10.482890129089355, "The Resolution of the LISS-4 Imaging System is 6 m."]
[7.755427837371826, 5.426826000213623, "The Accuracy of the NIDEM Elevation Model is Less accurate for rocky shores."]
[10.736536026000977, 10.292792320251465, "The Cross-talk between PHAs of the PHA Detector is <0.2%."]
[9.594552993774414, 0.43945178389549255, "The Design Life of the ACTS/TOS Communication Technology Satellite is 4 years."]
[5.7589335441589355, 4.694967746734619, "The Positioning Accuracy of the Argos DCS Satellite System is Up to 150 m."]
[9.1071138381958, 5.263038635253906, "The Attitude Modes of the Spacecraft Satellite is Nadir-pointing, Ram-pointing, Inertial-pointing, Slew-pointing."]
[10.017794609069824, 3.6715095043182373, "The Neutron Production of the Lunar Surface Surface is Constant bombardment by cosmic ray protons."]
[6.0858683586120605, 2.547287702560425, "The Space Act Agreement Partner of the SpaceX Company is NASA."]
[3.8713278770446777, 6.755026817321777, "The Technology of the LRO Mini-RF Transmitter Transmitter is MPM (Microwave Power Module)."]
[10.905996322631836, 3.066037654876709, "The Distance Traveled of the InSight Spacecraft is 172 million miles (277 million kilometers)."]
[9.415989875793457, 5.9417643547058105, "The Quantity of the Magnetorquers Attitude and Orbit Control Subsystem is 3."]
[7.629486083984375, 1.8591545820236206, "The Authors of the Magnetospheric Multiscale (MMS) Satellite is 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. Strang."]
[8.529098510742188, 7.843722343444824, "The Instrument Type of the RadMon Radiation Monitor is Miniature Particle Telescope."]
[5.217782497406006, 2.620447874069214, "The Development Team of the Binar-1 CubeSat is Team of students and engineers at Curtin University's Space Science and Technology Centre."]
[6.938724994659424, 3.157992362976074, "The Data Center Members of the Euclid Satellite is 1000+ members of the Euclid Consortium."]
[9.067413330078125, 9.711067199707031, "The Background Components of the Optical Receiver Receiver is Detector dark current, detected thermal emission of the receiver, detected solar illumination reflected from the lunar surface."]
[5.191839694976807, 6.608606338500977, "The HPBW AZ of the Antenna ADS-B Antenna is 33\u00ba."]
[6.465136528015137, 2.8029215335845947, "The Development of the Galileo App Mobile Application is Internal Competition for ESA Trainees."]
[6.5922698974609375, 3.5920228958129883, "The Mission Type of the KySat-2 Satellite is EO."]
[7.110072135925293, 9.174918174743652, "The Cross-Track Coverage of the MSI-0 and MSI-1 MSI Instruments is 60 km."]
[6.3026838302612305, 7.921586036682129, "The Satellite Launch Dates of the AMSU Advanced Microwave Sounding Unit is NOAA-15 (1998), NOAA-16 (2000), NOAA-17 (2002)."]
[7.28089714050293, 0.5280019044876099, "The Launch Date of the CAS500 Satellite is 22 March, 2021."]
[7.365957260131836, 7.979111671447754, "The Average Concentration of the Ozone Layer Atmospheric Layer is 220 Dobson Units."]
[9.801980018615723, 6.49201774597168, "The Thermal Stability of the Euclid Satellite is Maintained during slew maneuvers."]
[11.044819831848145, 4.047153472900391, "The Kinematic properties of the Ejecta cloud Materials on the Mercury surface, regolith is > 0 km/s."]
[6.563316345214844, 6.5744242668151855, "The Polarization Channels of the SGLI Imager is 3 directions."]
[9.579870223999023, 3.8386404514312744, "The Ground Station of the CanX-7 Satellite is SFL ground station in Toronto."]
[5.34517765045166, 3.5085766315460205, "The GaN Manufacturing Process of the UMS Company is Placed onto the European Preferred Parts List of the European Space Components Coordination."]
[9.359975814819336, 10.21666431427002, "The Field of View (FOV) of the PamCam Panoramic Camera is 20\u00ba x 16\u00ba."]
[9.57017707824707, 8.454145431518555, "The Heater Rings of the FPA Focus Control System is Lower and upper sides of the telescope attachment."]
[9.962362289428711, 7.356819152832031, "The Cube Corner Reflectors (CCRs) of the LARES Satellite is 92."]
[7.559412002563477, 1.1164064407348633, "The Launch Year of the Sentinel-1A/B Satellite is 2014."]
[9.476442337036133, 0.9057869911193848, "The Mission Duration of the STEREO Satellite is 5 years."]
[11.676795959472656, 6.118330478668213, "The Expected Lifespan of the Automation System System is Another decade of safe operations with XMM-Newton."]
[7.26798152923584, 5.1934003829956055, "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."]
[8.921874046325684, 3.475969076156616, "The Orbit Capability of the Spacecraft Bus (Avionics Module=AM) Satellite is LEO, MEO."]
[3.5094261169433594, 4.083038330078125, "The Radiation hardness of the STRV-2 DHS Data Handling System is about 100 krad."]
[13.140779495239258, 4.046339988708496, "The Data Release 3 and Data Release 4 of the Gaia Satellite is In production."]
[11.883109092712402, 2.3784875869750977, "The Matchpoint Maneuver Altitude of the OSIRIS-REx Spacecraft is Approximately 246 ft (75 m)."]
[6.2797346115112305, 5.79218864440918, "The Resolution of the TerraSAR-X SAR Satellite is 3 m or better in stripmap and spotlight mode."]
[9.614693641662598, 1.235856533050537, "The Observation Period of the BRITE satellites Satellite is Hours to Months."]
[1.8450322151184082, 3.836381435394287, "The Cell Type of the Photo-Voltaic Array Power Generation is Triple junction GaAs cells (3G-28%)."]
[9.487595558166504, 7.947958946228027, "The Gd Cross Section for Thermal Neutrons of the LND Particle Telescope is 48\u2019890 b."]
[6.730295658111572, 4.4985032081604, "The Measurement Capabilities of the Copernicus Sentinel-3 Satellite is Earth\u2019s oceans, land, ice and atmosphere."]
[11.30684757232666, 6.259585857391357, "The Emission Types of the Pulsars Neutron Stars is Radio, other types of radiation, thermal radiation, non-thermal radiation."]
[7.83234167098999, 8.91098403930664, "The Radiometric stability of the Spectrometer Spectrometer is <0.65% (SWIR, <0.5% (MWIR), <0.4% (TIR)."]
[11.888218879699707, 2.3782336711883545, "The Sampling Arm Length of the OSIRIS-REx Spacecraft is 11-foot (3.35-meter)."]
[11.145992279052734, 4.724326133728027, "The Speed of Particles of the SS 433 Microquasar is Close to a quarter the speed of light."]
[9.06185245513916, 10.890158653259277, "The Mono Mode Swath of the LISS-4 Camera is 70 km."]
[10.054060935974121, 6.669192790985107, "The Thermal Environment After Separation of the MMO Spacecraft is High temperature, illuminated by sunlight."]
[5.655186653137207, 3.9023642539978027, "The Location of the MOC Mission Operations Center is Darmstadt."]
[9.571358680725098, 7.275581359863281, "The Length of the Heat Probe Instrument is 16 inches (40 centimeters)."]
[10.218151092529297, 2.9884157180786133, "The Orbit Altitude of the CHORUS Satellite is Approximately 588-602 km."]
[6.582108020782471, 0.37111419439315796, "The Launch Date of the SMART-1 Satellite is September 27, 2003."]
[7.747093200683594, 3.731058120727539, "The Mission Status of the Tandem-L Satellite is Proposal."]
[7.425944805145264, 2.345867395401001, "The URL of the Near Earth Asteroid Scout Satellite is https://web.archive.org/web/20220815171855/https://ieeexplore.ieee.org/document/8742190."]
[4.281800270080566, 4.751087665557861, "The Function of the Device Sample and Hold Stage is Transfer information at the end of the integration cycle."]
[8.75852108001709, 8.148776054382324, "The Number of RadFETs of the CDE Dosimeter is 8."]
[7.500367641448975, 1.2354933023452759, "The Mission Overview Date of the Sentinel-1 Satellite is July 12-17, 2009."]
[5.864339351654053, 6.930561542510986, "The Observation Range of Doppler Velocity of the CPR Millimeter-Wave Radar is \u00b110m/s."]
[8.87810230255127, 5.921327590942383, "The Components of the Integrated Navigation System Navigation System is INS, star tracker (2), altimeter (2), velocimeter (2) and image sensor (2)."]
[6.941761493682861, 9.076560020446777, "The Size of the Satellite Observation Instrument is 35.7 x 36.2 x 15.8 cm."]
[4.8587517738342285, 4.982015132904053, "The Contact Initiation Time of the Microhard Ground Station Ground Station is Five to ten minutes after the expected scheduled contact."]
[3.7877562046051025, 6.101039886474609, "The Data Rate of the Optical link Communication System is 2.8 Gbit/s (1.8 Gbit/s user data)."]
[8.004571914672852, 8.3827543258667, "The Band of the IASI Infrared Atmospheric Sounding Interferometer is 3."]
[7.802524089813232, 8.939391136169434, "The Wavelength Range (UV) of the Sentinel-4/UVN Instrument is 305-400 nm."]
[10.51459789276123, -1.0232892036437988, "The Mass of the SpinSat Microsatellite is 57 kg."]
[10.304582595825195, 3.0498886108398438, "The Operating Distance of the OE Satellite is Up to 7 km."]
[9.039031028747559, 3.6402499675750732, "The Orbit Position of the BeiDou-1C Satellite is GEO, 110.5\u00ba E."]
[7.146685600280762, 7.991117000579834, "The Instrument Type of the AWiFS Instrument is High resolution optical imagers."]
[7.803828716278076, 8.047022819519043, "The Phase of the UV2VIS SO Instrument is Engineering and Qualification Model."]
[9.643485069274902, 6.012362003326416, "The Computer Interface of the ADCS Attitude Determination and Control Subsystem is Attitude sensors and actuators."]
[6.3598504066467285, 1.6616888046264648, "The Launch Date of the Jason-3 Satellite is 2014."]
[6.6375908851623535, 3.8613765239715576, "The LRIT and HRIT Broadcasting Service of the GK2A satellite Satellite is L-band."]
[12.101146697998047, 3.2862775325775146, "The Inclination of the Satellite Orbit is 97.7\u00b0."]
[7.7330217361450195, 2.223616600036621, "The Parachute Manufacturer of the ExoMars mission Mars Mission is Arescosmo."]
[10.54132080078125, -1.1044102907180786, "The Maximum Microsatellite Mass of the NanoRacks Microsat Deployer Satellite Deployer is 100 kg."]
[10.189597129821777, 4.8901166915893555, "The Thrusters of the KOMPSAT-6 Satellite is 1 N thrusters for precise orbit correction."]
[7.0943922996521, 7.408509254455566, "The Duty Cycle of the Instrument Satellite Instrument is 100%."]
[5.140361785888672, 6.022073745727539, "The Use of the Turnstile antennas Antenna is Communications with the spacecraft bus."]
[6.5346879959106445, 3.8602325916290283, "The Conference Location of the Sentinel-3 Satellite is Oslo, Norway."]
[5.826916217803955, 6.723723411560059, "The Bandwidths of the Ku-band Radar Altimeter Frequency Band is 320, 80 and 20 MHz."]
[8.591185569763184, 10.158218383789062, "The Background Area of the Detector Imaging Device is 10 x."]
[6.767402648925781, 3.83937668800354, "The Payload of the Sich-2 Satellite is Multispectral scanner, middle IR scanner, platform command & data handling subsystem, X-band communication subsystem."]
[6.350700378417969, 1.3883646726608276, "The Simulation Models of the PRISMA project Satellite Project is 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 (VB."]
[9.928278923034668, 9.506875038146973, "The Science Objectives of the SAGE-III Instrument is Extend the SAM II, SAGE I and SAGE II self-calibrating solar occultation data sets."]
[6.447065830230713, 3.2275853157043457, "The Manufacturer of the Resurs-P1 Satellite is NTs OMZ (Research Center for Earth Operative Monitoring)."]
[9.146805763244629, 8.593217849731445, "The Correction Level of the Sun and Galactic Glint Optical Phenomenon is Level-2."]
[8.50783920288086, 11.05898380279541, "The Swath per channel of the Eastman Kodak KLI14403 linear CCD sensor Sensor is > 300 km."]
[0.9922070503234863, 4.3299479484558105, "The Battery Capacity of the EPS Electric Power Subsystem is 125 Ah."]
[3.4888343811035156, 4.095794677734375, "The RAM of the STRV-1d DHS Data Handling System is 1024 k."]
[9.0568265914917, 7.788261413574219, "The Temperature Difference of the WISPR Imaging Instrument is 85 degrees Fahrenheit."]
[3.8661677837371826, 5.622249603271484, "The Data of the UKube-1 Satellite is < 36 kB per orbit."]
[9.137178421020508, 5.136097431182861, "The Sailboat (SB) Mode of the ICESat Satellite is YG axis (plus or minus) is closely coincident with the satellite velocity vector."]
[9.47095775604248, 0.7494686245918274, "The Mission Life of the ANUSat Satellite is 2 years."]
[6.674739360809326, 4.922490119934082, "The Cross-Calibration Precision of the Copernicus Sentinel-6 Satellite is Within 1 mm."]
[7.369833946228027, 7.699941158294678, "The Measurement Domain of the VHRR Instrument is Atmosphere, Ocean, Land."]
[7.646474838256836, 3.752272367477417, "The Daily system capacity of the WorldView Legion Satellite System is 3x."]
[9.494691848754883, 0.5241910219192505, "The Design Life of the MEV-1 Satellite is Redundant and high reliability 15+ years."]
[6.65853214263916, 3.7228965759277344, "The Rendezvous Target of the OSMA-1 Satellite is Landsat-7 spacecraft."]
[1.7773845195770264, 5.3583173751831055, "The Voltage of the Voltage 4 Modulator is 5.5\u00b12%."]
[1.8167753219604492, 3.9864583015441895, "The Solar cells type of the EPS Electrical Power Subsystem is GaAs multijunction cell."]
[6.022694110870361, 2.4664676189422607, "The Approach of the New Space Companies Companies is Make access to space affordable through innovation, flexibility, and miniaturization."]
[7.554215908050537, 9.65645980834961, "The Band 13 Detector of the S-192 optomechanical scanner Scanner is Photoconductive HgCdTe."]
[7.8812456130981445, -0.5494831204414368, "The URL of the SpaceX 2 Mission is http://www.nasa.gov/pdf/729030main_spacex_2_cargo_manifest.pdf."]
[7.4985127449035645, 2.98565673828125, "The Mission Planning Verification System of the KOMPSAT-2 Satellite is Unknown."]
[11.895561218261719, 2.361811876296997, "The Altitude of Checkpoint Rehearsal of the OSIRIS-REx Spacecraft is 246 feet (75 meters)."]
[6.029819965362549, 3.977614641189575, "The Standards of the Data Processing Chain Satellite System is OGC (Open Geospatial Consortium) standards, EO GML meta data, OGC WPS, ESA's Generic Interface for Instrument Data Processing."]
[8.391311645507812, 8.664595603942871, "The Builders of the SCIAMACHY Spectrometer is DASA/DSS, Fokker Space, TNO, SRON."]
[6.552868366241455, -0.1260078251361847, "The Launch Date of the PSLV Launch Vehicle is 12 Jan. 2018."]
[6.347025394439697, 3.0043253898620605, "The Management of the InSight Spacecraft is JPL, a division of Caltech in Pasadena, California."]
[10.6216402053833, 9.26285457611084, "The Image Segment Size of the CaSSIS Imaging System is 7 x 38 km."]
[9.195326805114746, 4.2921905517578125, "The Dimensions of the Trius SX9 Package is 70 mm long and 75 mm in diameter."]
[1.1447985172271729, 4.2702836990356445, "The Energy Storage of the Electric Power Subsystem Power System is Lithium-ion batteries."]
[6.598213195800781, 1.1718159914016724, "The Presentation Date of the Prisma Satellites Satellite is June 4-8, 2012."]
[8.799769401550293, 6.881834983825684, "The Mounting Locations of the OPS systems Sensor is 5 different sides of the cuboid."]
[7.038835525512695, 9.769424438476562, "The Spectral Range (\u00b5m) of the Band 4 Spectral Band is 10.3 - 11.3."]
[9.826764106750488, -0.9887619614601135, "The Spatial Resolution of the JL-1-GF03B Microsatellite is 1 m."]
[4.591728687286377, 0.24523015320301056, "The Number of Additional Satellites of the OneWeb Satellite Constellation is 34."]
[7.428036212921143, 8.816322326660156, "The Wavelength Range of the Spectral Channels Satellite Instrument is 0.55 - 0.75 \u00b5m."]
[9.773398399353027, 8.983114242553711, "The M1 Mirror Diameter of the TX Telescope Telescope is ~220 mm."]
[9.933867454528809, 1.3997539281845093, "The Orbital Plane Interval of the S/C Satellite is 19 minutes."]
[10.41403865814209, 4.74934196472168, "The Propulsion System of the GFO Satellite is Hydrazine."]
[6.884723663330078, 3.2242960929870605, "The Mission Status of the ST5 Satellite is Mission complete."]
[5.657191276550293, 9.171577453613281, "The Power Requirement of the DORIS Instrument is 20 W."]
[6.2604193687438965, 3.4033658504486084, "The Technology of the Cesium Mission 1 Satellite is Electronically steerable, multibeam APA (Active Phased Array)."]
[8.83624267578125, 9.166264533996582, "The F Number of the CIRiS Instrument is F/1.8."]
[9.066019058227539, 10.197432518005371, "The Manufacturer of the HRC High-Resolution Camera is ESA."]
[7.803356647491455, 8.730056762695312, "The Velocity Measurement Range of the NMS Mass and Velocity Spectrometer is 0.1-2 km/s."]
[6.9300456047058105, 2.584827184677124, "The URL of the ICEYE X1 Satellite is https://www.iceye.com/press/press-releases/first-iceye-x1-radar-image-from-space-published."]
[7.79279899597168, 1.7377479076385498, "The Build Date of the IUE (International Ultraviolet Explorer) Satellite is 1970s."]
[7.848011493682861, 9.03843879699707, "The Performance Range of the VIS Spectrometer is 365 - 500 nm."]
[4.209023952484131, 6.457850456237793, "The Coverage of the Ka-band Channels Communication System is Two contiguous sectors in north-eastern US plus sixteen isolated spot beams."]
[8.664685249328613, 10.046951293945312, "The Imaging Resolution of the Direct Imaging System Imaging System is Lower than PAIS with eight subapertures."]
[12.07797622680664, 2.2383384704589844, "The Orbit of the OSIRIS-REx Spacecraft is Bennu\u2019s orbital plane."]
[9.45445728302002, 1.8056612014770508, "The Pass Frequency of the Satellite Orbit Type is Once per orbit."]
[7.6864848136901855, 0.9272011518478394, "The Next Release of the Request for Information Process is Q2 of CY 2022."]
[7.348548889160156, 9.501541137695312, "The Telescope Diameter of the S-192 optomechanical scanner Scanner is 30 cm."]
[8.751543998718262, 5.234489917755127, "The Pointing Adjustment of the Kepler Spacecraft is Slight."]
[7.847218990325928, 9.4462251663208, "The Spectral Bands of the Imager Satellite Instrument is 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."]
[4.018049240112305, 2.364448308944702, "The Size of the NanoAvionics M6P 6U satellite bus Satellite Bus is 6U."]
[8.34307861328125, 3.7506425380706787, "The Not Used for Payload Synchronization of the SpaceWire Data Distribution is Not used for payload synchronization."]
[5.024571895599365, 7.515740871429443, "The Telemetry Data Rate of the Instrument Sensor is 8 kbit/s."]
[8.095725059509277, 1.3602715730667114, "The Date of the Manam Volcano, Papua New Guinea Image is 30 May 2022."]
[9.836956024169922, -0.5630903244018555, "The Orbit Type of the Rstar Data Relay Microsatellite is Elliptical."]
[9.568668365478516, 3.6441166400909424, "The Measurement Goal of the Lunar Flashlight Satellite is 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."]
[4.943266868591309, 4.898802757263184, "The Responsibilities of the X-band stations Ground Stations is Scientific satellite tracking, science data reception, raw data recording, formatted outputting, data transfer to the Mission Center."]
[10.651358604431152, 9.239625930786133, "The Image Center Coordinates of the CaSSIS Instrument is 28.36\u00baS/79.75\u00baE."]
[8.28012752532959, 10.267314910888672, "The Instrument power of the Optical System Imaging System is 200 W."]
[8.63243579864502, 6.896554946899414, "The Tracking of the FPM Fine Pointing Mechanism is \u00b120 \u00b5radians."]
[5.363687038421631, 4.994123458862305, "The Components of the NRD Navigation Radar Detector is Antenna and receiver electronics."]
[6.492848873138428, 2.843719482421875, "The Orbit of the NigeriaSat-X Satellite is Unknown."]
[6.049551010131836, 4.309762001037598, "The Cargo Capacity of the Canadarm2 Robotic Arm is About 4500 kg."]
[6.3488569259643555, 5.5181097984313965, "The Polarimetric SAR Interferometry of the TDX/TSX Satellite is Combines interferometric with polarimetric measurements."]
[-4.981277942657471, 4.407576560974121, "The Support Phase Time Period of the Mango Tango Satellite Formation is 20.06 to 01.07.2010."]
[5.8207221031188965, 9.178140640258789, "The Power of the LCT instrument Instrument is 160 W."]
[6.918712139129639, 3.6620559692382812, "The Mission of the GRACE-FO Satellite is Gravity Recovery and Climate Experiment Follow-On."]
[10.578202247619629, 7.500842571258545, "The Structure of the SCD-2 Satellite is Aluminum honeycomb."]
[6.976950645446777, 1.3389428853988647, "The Date of the 28th Annual AIAA/USU Conference on Small Satellites Conference is August 2014."]
[5.068717956542969, 4.416900634765625, "The Components of the C3S Command, Control and Communication Segment is Ground Station (GS) element, Mission Management Center (MMC) element, Data Routing and Retrieval (DRR) element."]
[10.225180625915527, 4.996237754821777, "The Thrust of the Propulsion System Satellite Propulsion is 10 N."]
[10.187915802001953, -0.8303000926971436, "The Configuration of the O/OREOS nanosatellite Satellite is 3U CubeSat."]
[10.079965591430664, 5.461814880371094, "The Powering of the Valves Controller Board Propulsion System is Telecommands."]
[5.415605545043945, 4.327005863189697, "The Service Area of the ASF Data Node is North, Central and South America."]
[8.319758415222168, 8.657465934753418, "The Type of the NISP Near Infrared Spectrometer and Photometer is Instrument."]
[8.911559104919434, 8.301952362060547, "The NE\u0394T @ specified scene temperature of the Instrument Spectral Imager is 0.1-0.7 K @ 250 K."]
[11.741402626037598, 1.6854325532913208, "The Historic Landing Date of the Philae lander Lander is 12 November 2014."]
[8.971014976501465, 2.484069585800171, "The Image Resolution of the Herschel Telescope is 2 arcmin by 2 arcmin."]
[6.413532257080078, 8.419228553771973, "The Frequency Range of the MWRI Microwave Radiometer Imager is 10.65-89 GHz."]
[11.986210823059082, 4.502269268035889, "The Frequency of Stellar Mergers of the Blue Ring Nebula Nebula is Once every 10 years in our Milky Way galaxy."]
[7.016661643981934, 7.654084205627441, "The Performance Evaluation of the ASTER Instrument is Not Provided."]
[8.012063980102539, 4.8014984130859375, "The Mission Objective of the TWINS Satellite is 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."]
[7.257166385650635, 5.370827674865723, "The XCO2 Changes of the CO2 Greenhouse Gas is < 1 ppm."]
[17.728378295898438, 7.162844657897949, "The J2000 declination (deg) of the B1758-250 Pulsar is -25.079."]
[11.795544624328613, -1.1046595573425293, "The Mass of the Spacecraft Satellite is ~2500 kg (launch mass)."]
[9.518714904785156, 0.5888504385948181, "The Planned Total In-Orbit Lifetime of the GHOSt satellites Satellite is Just over 5 years."]
[7.490968704223633, 4.9597578048706055, "The Objective 2 of the CITRIS Receiver is Provide a global map of ionospheric densities and irregularities to improve current models of the ionosphere."]
[6.46501350402832, 9.186932563781738, "The Board Standard of the MuREM Radiation Monitor is PC104."]
[7.519616603851318, 2.377676010131836, "The Partner of the ELSA-d IOD Mission is SSTL."]
[6.035666465759277, 6.7743916511535645, "The Operation Duration of the SuperDARN HF Radar is Not specified."]
[5.583815574645996, 3.097895860671997, "The Manufacturer of the SoftRide Isolation System Satellite Component is CSA Engineering."]
[5.347996711730957, 5.656793594360352, "The Quantity of the GPS receiver Receiver is 1 unit."]
[11.174946784973145, 9.340144157409668, "The Data Rate of the Earth Radiation Budget Experiment (ERBE) Instrument is 10.5 kbit/scanner (average)."]
[5.024352550506592, 5.19891357421875, "The Number of Stations of the DRDC Ground Station Network Ground Station Network is 6."]
[6.553901672363281, 2.8512182235717773, "The Program Affiliation of the IMAP Satellite is Solar Terrestrial Probes (STP) Program."]
[8.924125671386719, 2.6557352542877197, "The Shape of the Heliosphere Space Phenomenon is Deflated croissant."]
[2.04954195022583, 3.9308366775512695, "The Number of Solar Panels of the AprizeSat Satellite is 6."]
[3.817195177078247, 0.2777647376060486, "The Data Release Date of the GRAIL Satellite is 2014."]
[3.0411977767944336, 6.630856037139893, "The Transmitter Power of the RF Communications Data Transmission is 1.5 W."]
[1.5671850442886353, 4.968406677246094, "The Regulated Bus Voltage of the Power Subsystem Subsystem is 5 V."]
[5.767792701721191, 2.2106242179870605, "The Communication Objective of the QUESS satellite Satellite is \"hack-proof\" quantum communications."]
[3.654736042022705, 6.114562034606934, "The Speed of the 5G Network Telecommunications Network is Faster than current data speeds."]
[6.961050510406494, 1.577502727508545, "The Development Date of the GMV Company is 24 June 2021."]
[9.378379821777344, 10.061266899108887, "The Field of View of the Lightning Imager Camera is Atlantic Ocean, a small part of Africa and part of South America."]
[6.930905342102051, 3.8304266929626465, "The Payload of the MANTIS Satellite is High resolution Earth observation camera."]
[6.937557697296143, 0.9237081408500671, "The Final Terrestrial Trip Date of the SmallGEO Communications Satellite is Dec. 1, 2016."]
[10.609756469726562, -1.6796571016311646, "The Cargo of the Kounotori H-II Transfer Vehicle is Six new lithium-ion batteries and corresponding adapter plates."]
[7.541934967041016, 3.7498881816864014, "The Common Functionality of the KazEOSat-2 Satellite is Antenna scheduling, user office and image processing facilities."]
[9.385228157043457, 9.118619918823242, "The Focal Length of the Telescope Optical Instrument is 234.5 mm."]
[7.211245059967041, 5.658548831939697, "The Toxin Production of the Blue-Green Algae Microorganism is Can produce toxins that can make you or your pets sick if swallowed or possibly cause skin and/or eye irritation due to contact."]
[5.528526782989502, 2.6773524284362793, "The Proximate Cause of the Fairing Satellite Component is Fairing separation failed."]
[10.014030456542969, 1.4527242183685303, "The Period of the Satellite Satellite is 103.2 minutes."]
[5.955502510070801, 0.7503125667572021, "The Conference Presentation Date of the Trailblazer CubeSat is March 29-31, 2011."]
[11.353819847106934, 5.786016941070557, "The Mission Type of the INTEGRAL Satellite is Follow-up of Gravitational Wave Detections."]
[12.113720893859863, 2.2462522983551025, "The Laser Altimeter of the OSIRIS-REx Spacecraft is OLA."]
[6.4168171882629395, 3.3736300468444824, "The Owner of the NeuSAR Satellite is DSO National Laboratories, Singapore, with support from the Office for Space Technology and Industry (OSTIn)."]
[8.0623197555542, 8.630270957946777, "The Polarization Measurement of the WUPPE Spectrophotometer is Function of wavelength."]
[7.785140037536621, 8.202779769897461, "The Type of the TANSO-FTS Instrument is Imaging multi-spectral radiometers (vis/IR)."]
[8.840815544128418, 2.8395872116088867, "The Purpose of the LRO Satellite is Observing the moon."]
[9.837002754211426, 7.9594950675964355, "The Event Rates of the LET Low Energy Telescope is Up to ~10 kHz."]
[12.957164764404297, 4.84501838684082, "The Orbital Period of the IBEX Spacecraft is 7.5 days."]
[8.58271312713623, 1.6958088874816895, "The Image Release Date of the Spitzer Space Telescope Space Telescope is 27 January 2020."]
[5.268392562866211, 2.1828136444091797, "The Peak Manufacturing Rate of the SSTL-300 S1 Satellite is 4 units per year."]
[5.290886878967285, 4.28824520111084, "The Monitoring of Technology Advancement of the Proving Ground Space is Close."]
[8.24069881439209, 9.680953025817871, "The Wavelength of the EUV Imager Imaging System is 30.4 nm."]
[5.426684379577637, 3.2364320755004883, "The Bus of the Suomi-NPP Satellite is Ball Commercial Platform 2000 (BCP 2000)."]
[5.921361446380615, 4.353094577789307, "The Operation of the Mx Satellite Instrument is For most of the orbits based on the user demands."]
[13.063859939575195, 4.04783296585083, "The Asteroid Survey of the Gaia Satellite is 156 thousand rocky bodies."]
[4.755888938903809, 4.384520530700684, "The Advantages of Optical Communications of the OICETS Satellite is 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."]
[7.538172245025635, 1.6682316064834595, "The Presentation Date of the Magnetospheric Multiscale (MMS) Mission is Feb. 28 - March 4, 2011."]
[10.832487106323242, 3.5902390480041504, "The Heliocentric Range of the S/C Spacecraft is 1.34 to 5.4 AU."]
[10.361889839172363, 1.9929317235946655, "The Period (min) of the Meteor-3-1 Satellite is 110.3."]
[4.6271138191223145, 0.18022815883159637, "The Total Satellites of the OneWeb Satellite Constellation is 218."]
[11.363795280456543, 1.3701685667037964, "The Expected Resume Date of the Yutu-2 Lunar Rover is Next Thursday (10 January)."]
[7.449136734008789, 8.125913619995117, "The Altitude at Entry Interface Point of the Experiment Data Telemetry is 120 km."]
[7.636290550231934, 4.792534351348877, "The Geometric Error Types of the PROBA-V Mission Satellite Mission is Absolute, inter-band and multi-temporal."]
[6.802622318267822, 3.2100446224212646, "The Mission Status of the Megha-Tropiques Satellite is Operational (extended)."]
[7.3050384521484375, -0.7146416306495667, "The Data Application of the CYGNSS Satellite is Flood Inundation Mapping."]
[8.269018173217773, 9.212909698486328, "The Pixels per FWHM of the Spectrometer Instrument is 1400."]
[7.698734760284424, 8.797950744628906, "The Ground Sample Distance of the GSD Spectrometer is 12 m at nadir."]
[11.78150463104248, 1.1512166261672974, "The Low Frequency Spectrometer (LFS) of the Chang\u2019e-4 Lander Lander is Payload."]
[6.196990489959717, 2.663161277770996, "The Senior Director of Human Spaceflight Programs of the SpaceX Company is Benji Reed."]
[7.041655540466309, 6.568925857543945, "The Primary Applications of the AATSR Instrument is Chlorophyll, Vegetation index, Cloud clearing, SST."]
[8.854597091674805, 7.360614776611328, "The Position of the SPC (Solar Probe Cup) Sensor is Extends beyond the TPS."]
[6.307916164398193, 8.264815330505371, "The Operating Frequencies of the MWR Noise Injection Radiometer is 23.8 and 36.5 GHz."]
[8.5665922164917, 10.338353157043457, "The CCD Packages of the Focal Plane Module Imaging Device is 2."]
[2.247591257095337, 4.433895111083984, "The Power of the BRITE spacecraft Satellite is 5.4 W to 10 W."]
[7.383681297302246, 4.51845121383667, "The Imaging System of the NewSat Satellite is Panchromatic imager."]
[6.037460803985596, 3.579585552215576, "The Hosted Payload Mission Objectives of the Alphasat Satellite is Fulfillment of each TDP experimentation plan."]
[6.508099555969238, 5.624800205230713, "The Components of the CrIMSS OPS-EDR Product Data Product is (a) CrIMSS second stage \u2018IR+MW\u2019 retrieval; (b) ATMS-only retrieval; (c) Corresponding ECMWF analysis; (d) Aqua-AIRS retrieval; (e) Aqua-AMSU retrieval; (f) corresponding ECMWF analysis."]
[6.323498725891113, 5.381561756134033, "The Calibration Method of the TerraSAR-X SAR Satellite is Antenna model approach."]
[11.219816207885742, 6.710996627807617, "The Purpose of the SEXTANT Engineering Demonstration is Realizable in a single package with NICER."]
[3.9399988651275635, 2.2908103466033936, "The Size of the GRIFEX CubeSat is 3U."]
[10.888206481933594, 5.060161590576172, "The Impact Time of the Geomagnetic Storm Space Weather Event is Less than a day."]
[10.511028289794922, 6.07700252532959, "The Field of the Micro-gravity experiment Experiment is Fluid mechanics."]
[10.231629371643066, 2.9877729415893555, "The Orbit Altitude of the ResourceSat-2A Satellite is 817 km."]
[4.809604167938232, 0.937790036201477, "The Total system cost of the WorldView Legion Satellite System is $600 million."]
[6.669997692108154, 0.8981194496154785, "The Falcon 1e Launch Date of the FormoSat-5 Satellite is June 15, 2010."]
[8.845688819885254, 1.9935965538024902, "The Publication Date of the New Horizons Spacecraft is 15 November 2021."]
[11.62568473815918, -0.8528690934181213, "The Mass of the Satellite Bus Spacecraft Component is Approximately 3850 kg."]
[10.547327041625977, 7.59760856628418, "The Material of the Spacecraft Structure Satellite Component is Aluminum 7075-T6."]
[10.402859687805176, 3.500659942626953, "The Additional Velocity of the Objects Orbiting at LEO Satellite Components is ~7700 m s-1."]
[3.831123113632202, 6.146202087402344, "The Data Format of the Optical link Communication System is 1064 nm, BPSK (Bi-Phase Shift Keying) modulated, homodyne."]
[6.696327209472656, 4.048274993896484, "The Application Areas of the ResourceSat-2 Satellite is Agricultural crop discrimination and monitoring, crop acreage/yield estimation, precision farming, water resources, forest mapping, rural infrastructure development, disaster management."]
[10.11867904663086, 4.894944190979004, "The Nozzle Throat Diameter of the Propulsion System Satellite Component is 700 \u00b5m."]
[9.604968070983887, -0.62000972032547, "The Secondary Objective of the BIRD Satellite is Demonstrate new microsatellite technologies."]
[10.37019157409668, 3.159144401550293, "The Measurement Distance of the Autonomous Wireless Payload Payload is 635 km."]
[6.436634063720703, 3.4956700801849365, "The Goal of the RASAT Satellite Mission is to test the equipments."]
[8.43789291381836, 4.390206336975098, "The Monoscopic Area Coverage of the QuickBird-2 Satellite is 1 x > 4 x."]
[7.65733528137207, 2.0606400966644287, "The Overview Date of the Terrestrial Imaging Spectroscopy Missions Missions is 21\u201326 July 2013."]
[9.58045768737793, 1.52922523021698, "The Observation Cycle of the Landsat-8 Satellite is Every eight days."]
[9.589941024780273, 0.4864436686038971, "The Goal Life of the Gokturk-2 Satellite is 7 years."]
[6.042757987976074, -0.07370468974113464, "The Development Start Date of the Galileo Second Generation Satellites Satellite is Unknown."]
[7.153388977050781, 7.209183216094971, "The Correction Types of the Atmospheric Correction Image Processing is Flat and rugged terrain, haze/cirrus detection."]
[6.511838912963867, 1.3345246315002441, "The Launch Date of the G\u00f6kt\u00fcrk-1 Satellite is December 5, 2016."]
[8.041625022888184, 4.355118751525879, "The Swath Width of the DMC-3 Satellite Constellation is 23 km."]
[6.295436859130859, 1.9309494495391846, "The Workshop Presentation Date of the EnMAP Satellite is March 16-18, 2009."]
[6.2436089515686035, 1.4101313352584839, "The Operational Date of the PAZ-TerraSAR Constellation Satellite Constellation is Late 2017."]
[9.767685890197754, 8.17671012878418, "The Anticoincidence Efficiency of the GRS Gamma-Ray Spectrometer is \u226590%."]
[9.597432136535645, 5.905140399932861, "The Type of the ADCS Attitude Determination and Control Subsystem is Passive magnetic attitude stabilization system."]
[8.077072143554688, 5.507925033569336, "The Position Calculation Method of the DIOGENE Navigator is Least squares method."]
[5.574544906616211, 4.084667682647705, "The Disciplines of the EuTEF Payload Facility is Material science, physics, astrobiology and astronomy."]
[6.454283714294434, 3.781453847885132, "The Operations Support of the TGO Satellite is Yes."]
[10.413524627685547, 6.142090797424316, "The Study Phenomena of the RUBI Fluid Science Experiment is Phase transition and heat transfer during the evaporation of fluids."]
[9.573629379272461, 8.872854232788086, "The Clear Aperture of the Etalon Filter is 50 mm."]
[9.343729972839355, 1.886806845664978, "The Coverage of the Coverage Satellite is 2-day global coverage at 1 km resolution."]
[9.06639575958252, 4.836885929107666, "The Nominal FOV of the SPARCS Satellite is 2\u00b0."]
[9.619318962097168, 1.3683782815933228, "The Forecast Duration of the HWRF Model is 24 hours."]
[6.783165454864502, 4.468489170074463, "The Data Source of the Green City Watch Application is Copernicus Sentinel satellite data."]
[4.200152397155762, 6.276656627655029, "The DVB-RCS/DVB-S2 On-Board Processors (OBPs) of the Repeater subsystem Communication System is 4 channels in Ku-band."]
[7.259409427642822, 6.171220779418945, "The Geolocation and Pointing Accuracy of the WindSat Sensor is Not provided."]
[12.16581916809082, 3.271623134613037, "The Orbit Inclination of the PAZ Satellite is 98\u00ba."]
[6.892862796783447, 9.151984214782715, "The Antenna Aperture in the Azimuth of the UF Mode Observation Mode is 7.5 m."]
[9.619194030761719, 3.9213690757751465, "The Expected Stabilization Effect of the CanX-7 Satellite is Aerodynamically stabilize due to the so-called \"shuttlecock\" effect."]
[9.903803825378418, 1.3146443367004395, "The Various Times of the Notional Pass Time Task Schedule is 12:00 pm, 1:30 pm, 12:00 am, 1:30 am, 8:00 am, 2:00 pm, 11:30 am."]
[7.576054096221924, -0.4887903332710266, "The Launch Date of the SpaceX Falcon 9 Rocket is Nov. 14."]
[9.888636589050293, -0.9749919772148132, "The Altitude of the JL-1-GF03D Microsatellite is 535 km."]
[7.606588840484619, 2.099330425262451, "The Launch Date of the Emirates Mars Mission (Hope) Satellite is 17 April 2020."]
[10.045378684997559, 1.5149811506271362, "The Orbit Period of the ResourceSat-1 Satellite is 101.35 minutes."]
[11.720268249511719, 1.2148672342300415, "The Lunar Lander Neutrons and Dosimetry(LND) of the Chang\u2019e-4 Lander Lander is International Joint Collaboration Payload."]
[7.797595024108887, 9.157868385314941, "The Spectral Ranges of the Spectrometer Modules Spectrometer is 190-735 nm (UV-VIS) and 350-1100 nm (VNIR)."]
[9.416573524475098, 8.714856147766113, "The Random Acceleration of the PP Twin Telescopes Telescope is Up to 88.1g."]
[5.7620344161987305, 6.201801300048828, "The Fairing Extension Length of the TerraSAR-X Satellite is 1.5 m."]
[6.57494592666626, 0.3731505572795868, "The Launch Date of the SMART-1 Satellite is 2003."]
[3.940040349960327, 6.695677280426025, "The Transmit Power of the LCT Laser Communication Terminal is 2.2 W."]
[11.353036880493164, 4.2660322189331055, "The Estimated Start of the Oort Cloud Space Phenomenon is About 1,000 astronomical units (AU) from the Sun."]
[8.190474510192871, 0.8436493873596191, "The Re-entry Date of the HITSAT Satellite is June 18, 2008."]
[5.278106212615967, 3.8765182495117188, "The Function of the ISSAC SOC Space Operations Center is Coordinate with NASA for ISS and WORF rack operations."]
[3.8114776611328125, 0.2761680781841278, "The Presentation Date of the GRAIL Mission is March 18-21, 2013."]
[8.5492582321167, 10.134000778198242, "The Size of the Detector Imaging Device is 2048 x 2048 pixels."]
[8.228337287902832, 5.502045631408691, "The Navigation of the Lander Spacecraft is Absolute sensors determine the position and velocity with respect to the landing site."]
[9.201033592224121, 4.216720104217529, "The Inner Diameter of the PM Satellite Component is 4.2 m."]
[9.591387748718262, 1.195642113685608, "The Testing Duration of the Galileo Satellites 13 and 14 Satellites is Lengthy."]
[7.416222095489502, 9.086880683898926, "The Swath Width of the Instrument Spectrometer is 1650 km for IR bands."]
[6.709591865539551, 5.689760208129883, "The Application of the GeoSTAR Scattering Approach is Detect and track hurricanes and other severe storms."]
[11.539457321166992, 2.691868305206299, "The Mission Goals of the Psyche Asteroid is Understand the building blocks of planet formation, determine Psyche's age and formation process, and study its surface."]
[9.665559768676758, 1.5699231624603271, "The Repeat Cycle of the Satellite Orbit Orbit is 17 days."]
[8.193103790283203, 5.622929573059082, "The Vector Components Random Error of the Electrical Field Satellite System is < 10 mV/m."]
[6.854811191558838, 2.0374739170074463, "The URL of the China High-resolution Earth Observation System (CHEOS) Satellite System is http://spacenews.com/article/civil-space/39665china-pushing-ahead-on-hi-res-satellite-system."]
[8.210550308227539, 3.7721920013427734, "The Proximity Operations Plan of the AeroCube-OCSD-B and -C Satellites is Co-orbital corkscrew orbit."]
[8.947857856750488, 7.510921478271484, "The Purpose of the STIS Ion Sensor is Measures solar energetic particles and provide advance warning if a shock wave produced by those particles is headed for Earth."]
[8.502785682678223, 5.0902934074401855, "The Image Processing of the NASA's Solar Dynamics Observatory Satellite is Enhance small features."]
[4.0090556144714355, 6.4529194831848145, "The Modulation Scheme of the S-band transmitter Transmitter is BPSK."]
[9.063035011291504, 7.081068515777588, "The Placement of the Langmuir Probe Plasma Measurement Device is On long protruding booms."]
[4.569768905639648, 6.107349872589111, "The Uplink/Downlink Frequency of the OPAL Satellite is 420-450 MHz."]
[8.883625984191895, 5.786862373352051, "The Antenna Subsystem Rotation Speed of the GMI Instrument is 32 rpm."]
[7.352705001831055, 0.7530052065849304, "The Arrival Date of the NICER Payload is June 8, 2016."]
[3.564246892929077, 6.538656234741211, "The Data Transmission Rate of the S-band Communication Band is 16 kbit/s."]
[7.8416032791137695, 3.218177080154419, "The Mission Objective of the IMAP Satellite is Understand the boundary of the heliosphere."]
[9.444340705871582, 5.135876178741455, "The Maneuver Scheme of the P2 Satellite is Spin control maneuver scheme."]
[4.414331912994385, 6.291350841522217, "The Downlink Frequency of the Communication System Satellite System is 437.325 MHz."]
[7.249534606933594, 9.487025260925293, "The Swath Width of the MSU-M Multispectral Scanner is 1900 km."]
[8.760658264160156, 10.408160209655762, "The Image Transfer Modes of the Payload 2 CMOS Camera is 8/16 bit."]
[9.182985305786133, 3.1569721698760986, "The Mission of the LunaH-Map Satellite is Map hydrogen within craters and other permanently shadowed regions throughout the moon\u2019s south pole."]
[6.531053066253662, 3.620832681655884, "The Type of the ExoCube Payload is Space weather nanosatellite."]
[6.187549591064453, 2.1221418380737305, "The Bus Type of the Jason-2 Satellite is Proteus."]
[8.117073059082031, 1.2352961301803589, "The Date of the Divine Providencia Image is 27 March 2022."]
[9.080330848693848, 5.141476154327393, "The Attitude Variation During Maneuvers of the ISS Satellite is ~2-3\u00ba."]
[9.760004997253418, 6.672618389129639, "The Number of Temperature-Controlled Zones of the HTSSE-II payload Satellite Payload is 5."]
[3.4022676944732666, 5.395731449127197, "The Packet Storage of the LT Device is Queue."]
[10.696389198303223, 3.8268797397613525, "The Data Volume of the Hubble Space Telescope is 172 terabytes of data since its launch in 1990."]
[9.483338356018066, 5.566535949707031, "The Attitude Control of the ADCS unit Satellite Component is Y-momentum 3-axis stabilization."]
[9.290358543395996, 7.570115089416504, "The Measurement Range of the Faraday Cup Ion Detectors Sensor is Up to 8 keV."]
[6.906054973602295, 1.055464506149292, "The Journal Publication Date of the GPS/MET Satellite is 1997."]
[7.737576007843018, 4.0236124992370605, "The OAP Increase of the UK-DMC-2 Satellite is 60%."]
[6.970474720001221, 4.195290565490723, "The Measurement Domain of the JERS-1 Satellite is Land, Snow & Ice."]
[6.4250874519348145, 3.4392898082733154, "The Mission Type of the Myriade/AstroSat-100 Satellite is EO."]
[5.706423759460449, 9.142888069152832, "The Instrument Power of the Instrument Spectrometer is 220 W."]
[5.7308454513549805, 1.6794010400772095, "The Configuration of the PSLV-C38 Launch Vehicle is XL."]
[6.6427507400512695, 0.5909212827682495, "The Launch Date of the OPTSAT-3000 Satellite is Aug. 2, 2017."]
[10.516585350036621, 7.475578308105469, "The Hardening Process of the Bricks Building Material is Water evaporation."]
[9.026166915893555, 7.77640438079834, "The Temperature of the OBCT Calibration Target is Approx. 273 K."]
[6.999594688415527, 4.496321201324463, "The Instrument Type of the HJ-1 Satellite is Imaging multi-spectral radiometers (vis/IR)."]
[7.917416095733643, 5.666413307189941, "The Movement of the SAA South Atlantic Anomaly is Slow-moving."]
[11.847810745239258, -1.0874607563018799, "The Mass at Launch of the Spacecraft Satellite is 2093 kg."]
[4.07098913192749, 1.2281537055969238, "The Mission Type of the FITSat-1 Satellite is Non-EO."]
[9.543177604675293, 0.5678500533103943, "The S/C Design Life of the Payload Satellite Payload is Up to 12 years."]
[6.562950134277344, 0.3416984975337982, "The Crash Date of the SMART-1 Satellite is 3 September 2018."]
[8.517398834228516, 10.287296295166016, "The CCDs Read-Out Chain of the MATS Satellite is Characterized."]
[7.577517032623291, -0.45829305052757263, "The Launch Date of the Falcon 9 Rocket is Early 2018."]
[7.775730609893799, 4.184376239776611, "The Tracking Data Source of the A-68A Iceberg is Copernicus Sentinel-3 mission, MODIS instrument on the US Terra mission, Copernicus Sentinel-1 mission."]
[6.503746032714844, 0.3528691530227661, "The Development and Lessons Learnt Presentation Date of the SMART-1 Satellite is Oct. 4-8, 2004."]
[3.696676254272461, 6.171125411987305, "The Baud Rate of the Command and Telemetry Interface Interface is 19.2 kbit/s."]
[9.38106918334961, 7.621622562408447, "The Cryogen Volume of the Instrument Dewar/Heat Exchanger is 944 liter."]
[8.737235069274902, 10.243006706237793, "The Dark Current of the Sensor Image Sensor is Negligible."]
[9.987716674804688, 1.6434175968170166, "The Orbital Period of the MMO Spacecraft is 9.2 hours."]
[10.12743854522705, 1.4928579330444336, "The Period of the Satellite Communication is 105.33 min."]
[6.05484676361084, 6.617897987365723, "The Bands of the SRAL SAR Radar Altimeter is C+Ku."]
[12.03084659576416, 3.2969422340393066, "The Orbit Inclination of the CBAS Primary Payload is 0\u00ba."]
[7.862574577331543, 2.300053834915161, "The Publisher of the Observation of the Earth and Its Environment Documentation is Herbert J. Kramer."]
[8.481063842773438, 8.665815353393555, "The Grating Type of the OCO-3 Spectrometer is Reflection gratings."]
[6.231086254119873, 2.0235769748687744, "The NRL Review Date of the TacSat-4 Satellite is 2009."]
[8.4341402053833, 9.627098083496094, "The New spectral channels of the OLCI Camera Assembly is Implemented in OLCI."]
[10.490804672241211, 8.526126861572266, "The Field of View of the MiniCOR Coronagraph is 60% of the C3 FOV."]
[6.520200252532959, 2.5523829460144043, "The Critical Design Review Start Date of the Lucy Discovery Program Mission is Oct. 15."]
[8.518601417541504, 8.742260932922363, "The Grating Type of the Grating Reflection Unit Spectrometer Component is Dielectric reflection grating."]
[9.154816627502441, -0.6093342900276184, "The Launch Date of the LitianicaSAT-2 Nanosatellite is June 23, 2017."]
[8.89659309387207, 6.630550861358643, "The Purpose of the DSLP Instrument is Studying characteristic macroscopic properties of ionospheric plasmas and identifying observed irregularities with possible solar-terrestrial connection related to sudden space weather events."]
[5.503074645996094, 3.8625142574310303, "The Components of the ESEX Satellite is PFS (Propellant Feed System), power subsystem, command and telemetry modules, onboard diagnostics, arcjet assembly."]
[9.938138961791992, 5.359702110290527, "The Stress Level of the Reflector Film Satellite Component is 82.5 bar (1200 psi)."]
[4.93445348739624, 0.8178661465644836, "The Total Value of the Joint Polar Satellite System Common Ground System contract Contract is Approximately $1,919,705,269."]
[7.290779113769531, 5.817386150360107, "The Effect of Traffic Levels of the Model Atmospheric Model is Increased coverage from contrail cirrus clouds, with an increased optical thickness of the ice clouds."]
[7.084880828857422, 3.761965751647949, "The Operator of the OrbView-1 Satellite is Orbital Imaging Corporation (ORBIMAGE)."]
[8.591323852539062, 1.6100140810012817, "The Closest Approach Date of the Rosetta Spacecraft is 13 November 2007."]
[7.7679643630981445, 3.8076391220092773, "The Size of the Hofsj\u00f6kull Glacier is Third largest in Iceland."]
[6.505990028381348, 8.17818546295166, "The Impact on Numerical Weather Prediction Models of the MiniRad Microwave Radiometer is Largest positive impact of any assimilated observation."]
[7.747924327850342, 8.270702362060547, "The Spectral Coverage of the TANSO-FTS Sensor is Unknown."]
[11.601959228515625, 0.759462833404541, "The Mass of the Chang'e-4 lunar probe Lunar Probe is 400 kg."]
[7.921927452087402, 7.466851711273193, "The Spectrometer Type of the The Rossi Explorer Satellite is Timing."]
[6.068898677825928, 5.682440757751465, "The Antenna Type of the XSAR SAR Sensor Subsystem is Active phased array antenna."]
[5.081910610198975, 7.058406352996826, "The Volume of the ORA Offset Reflector Antenna is 1230 x 1010 x 905 mm."]
[6.036965370178223, 9.597786903381348, "The Mass of the HEPD Instrument is 2.2 kg."]
[3.844961166381836, 2.3330304622650146, "The Size of the DTUSat-2 CubeSat is 1U."]
[7.583380222320557, 1.0309840440750122, "The Observation Date of the ACE - Advanced Composition Explorer Satellite is April 21, 2016."]
[6.002470970153809, 2.610366106033325, "The Planned Satellite Name of the Capella Space Company is Sequoia."]
[7.331077575683594, 1.5354419946670532, "The Contract Signing Date of the Arctic Weather Satellite Satellite is 09 March 2021."]
[11.263288497924805, 4.259310245513916, "The Number of Stars' Rotation Rates Measured of the Kepler Telescope is More than 750."]
[4.0510640144348145, 5.623117923736572, "The X-band Transmission Speed of the NigeriaSat-2 Satellite is Up to 210 Mbit/s."]
[9.678057670593262, 7.791987419128418, "The Energy Measurement Range of the HEPD High Energy Proton Detector is 1 - 1000 MeV."]
[11.764771461486816, 1.6743708848953247, "The Final Parking Time of the Philae Lander is 17:31:17 GMT."]
[6.858172416687012, 4.128225803375244, "The Imagery of the ResourceSat-2 LISS-3 Satellite is Data."]
[8.906285285949707, 8.438321113586426, "The Viewing Angle of the ELENA Sensor is 4.5\u00ba x 76\u00ba."]
[11.604116439819336, 4.4532270431518555, "The Mass of the Companion Star Star is About half the mass of the Sun."]
[7.957181453704834, 1.4823188781738281, "The Start Time of the Asteroid Day TV Online Program is 30 June at 12:00 CEST."]
[6.136612415313721, 9.635687828063965, "The Mass of the MUPUS Sensor is 2.2 kg."]
[1.6948752403259277, 4.5838398933410645, "The Manufacturer of the Electrical Power Subsystem (EPS) Power Regulation System is Clyde Space."]
[8.012243270874023, 5.627434253692627, "The Real-time Navigation Data Frequency of the DIOGENE Navigator is Every 30 s."]
[8.274932861328125, 3.086733102798462, "The Pursuit Monostatic Phase of the TanDEM-X Satellite is Sept. 20, 2014, to the end of March 2015."]
[8.745793342590332, 0.269519180059433, "The Orbital Period of the ISS Space Station is 90 minutes."]
[10.874129295349121, 5.70394229888916, "The URL of the Submerged Sources of Transient Acoustic Emission from Solar Flares Research Paper is https://iopscience.iop.org/article/10.3847/2041-8213/abad2a/pdf."]
[1.5337960720062256, 4.837261199951172, "The Survive Without Damage of the DC-DC converter Power Converter is \u00b150 V on input terminals."]
[10.122536659240723, 1.366257667541504, "The Local Equatorial Crossing Time of the Tatiana-2 Satellite is 12:00 hours."]
[8.497146606445312, 10.561626434326172, "The Pixel Count of the Kruiz CCD Detector is 1024 x 128."]
[6.4080939292907715, 4.704059600830078, "The Level-0 Products of the Sentinel-1 Satellite is Compressed, unprocessed instrument source packets, with additional annotations and auxiliary information to support the processing."]
[9.036876678466797, 10.505997657775879, "The Pixel size of the 16 mm camera Camera is 8 \u03bcm x 8 \u03bcm."]
[11.035445213317871, 2.8167734146118164, "The Embankment Length of the Ataturk Dam Dam is 1,820 m."]
[5.957674503326416, 4.036829948425293, "The Prime Contractor of the IASI Instrument is CNES."]
[7.195821285247803, 5.5403923988342285, "The Maps of the Free-air and Bouguer Gravity Anomaly Data is Free-air (left), Bouguer (right)."]
[6.697031497955322, 4.661348342895508, "The Instrument Types of the Megha-Tropiques Satellite is Earth radiation budget radiometers, Imaging multi-spectral radiometers (passive microwave), Atmospheric temperature and humidity sounders."]
[4.8219990730285645, 1.6570851802825928, "The Number of Satellites of the Falcon 9 Rocket is 60."]
[1.5617271661758423, 4.475198268890381, "The Input Current of the Buck-Boost Converter Solar Array Regulator is 0 - 16 A."]
[5.9981369972229, 0.7890290021896362, "The Conference Presentation Date of the CubeSat TestBed 1 Satellite is Aug. 10-13, 2009."]
[6.643341064453125, 3.5504069328308105, "The Mission Type of the NeuSAR Satellite is EO."]
[8.1395263671875, 3.9628970623016357, "The Area Coverage of the CHORUS Satellite is 63% of the area around the ice limit border."]
[9.483147621154785, -0.7855938673019409, "The Launch Date of the IDEA OSG 1 Microsatellite is 2018."]
[11.094375610351562, 2.8083877563476562, "The Discharge of the Yellowstone River River is 51,400 cubic feet per second."]
[9.039101600646973, 3.6489272117614746, "The Orbit Position of the BeiDou-1D Satellite is GEO, 58.75\u00ba E."]
[9.162208557128906, 3.235504388809204, "The Orbit Type of the Satellite PAZ is Sun-synchronous dawn-dust orbit."]
[6.578113555908203, 2.4450550079345703, "The Coverage of the Konnect Satellite is Sub-Saharan Africa."]
[7.285403728485107, 0.9743430614471436, "The Global Coverage Date of the BeiDou-2 Navigation Satellite System Satellite System is 2020."]
[6.597469329833984, 5.534450054168701, "The Presentation Date of the Navy GEOSAT follow-on altimeter Altimeter is Feb. 1-8, 1997."]
[8.080631256103516, 1.4255338907241821, "The Mission Start Date of the Solar Dynamics Observatory Satellite is Feb. 5, 2010."]
[3.879755973815918, 2.2930407524108887, "The Cube Volume of the E1P-2 CubeSat Satellite is 10 cm."]
[11.711904525756836, -1.1811625957489014, "The Dry Mass of the G\u00f6kt\u00fcrk-1A Satellite is 1,060 kg."]
[6.654839992523193, 1.2886673212051392, "The Funding Date of the BRITE Satellites Satellite is 2010."]
[3.625580072402954, 4.498525142669678, "The Manufacturer of the Safe-mode Computer Computer is \u00c5AC Microtec."]
[9.061068534851074, 3.8765037059783936, "The Transfer Phase End of the LUMIO Satellite is Halo Injection Maneuver."]
[7.4665141105651855, 1.9737164974212646, "The Event of the Stockholm Glacier Memorial Glacier is IPCC fifth assessment report approval session in 2014."]
[7.24777364730835, 5.129335403442383, "The Measurement of the GeoCARB Satellite is Solar-induced fluorescence."]
[9.59388542175293, 7.794352054595947, "The Electron Energy Resolution of the REPT Instrument is 25%."]
[6.164918422698975, 3.253969669342041, "The Members of the Providers Forum Committee is China (CNSS), EU (Galileo, EGNOS), India (IRNSS, GAGAN), Japan (QZSS, MSAS), Russia (GLONASS), and USA (GPS, WAAS)."]
[5.095618724822998, 2.9884769916534424, "The Purpose 3 of the PW-Sat CubeSat is Testing of the satellite communication system."]
[6.764583587646484, 6.132016181945801, "The Sustained Winds of the RapidScat Scatterometer is 45 m/s (162 km/hr)."]
[5.473017692565918, 4.696780204772949, "The Functionalities of the ICPS System is Generation of image collection plan, management of image collection planning status, managing resources related to the SAR payload operation."]
[8.504851341247559, 7.093980312347412, "The Dynamic Range of the Magnetic Field Measurement System Instrument is 60 dB."]
[6.0660600662231445, 9.342921257019043, "The Mass of the MW Instrument is 1.625 kg."]
[10.319063186645508, 4.1199469566345215, "The Anomalous Jet Firing ?V of the ICE (International Cometary Explorer) Spacecraft is 32 m/s."]
[7.487787246704102, 8.066548347473145, "The Quantity of the CERES Scanner is 2."]
[5.677475929260254, 9.398488998413086, "The Operation Principle of the STROFIO Instrument is 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."]
[11.84216022491455, 1.0264698266983032, "The Landing Date of the Chang'e-4 Lunar Spacecraft is January of this year."]
[9.092137336730957, 9.869319915771484, "The Function of the VMC Camera is Visual Monitoring."]
[1.5633916854858398, 4.523022651672363, "The Input Voltage of the Buck-Boost Converter Solar Array Regulator is 60 - 150 V."]
[2.26393985748291, 3.7979445457458496, "The Solar Panels of the DebriSat Satellite is 3 deployable."]
[4.480688571929932, 6.211461544036865, "The Frequency of the Space Micro \u00b5STDN S-band Transponder is S-band."]
[7.876717567443848, 9.693017959594727, "The Number of Pixels of the Band 1 Spectral Band is 1600."]
[6.985301971435547, 8.039475440979004, "The Potential Repeat Cycle of the MSU-SK Radiometer is 3-5 days."]
[1.7361265420913696, 4.784540176391602, "The Average Power Supply of the EPS Electrical Power Subsystem is 50 W."]
[3.543816566467285, 5.657799243927002, "The Data Transport Standards of the SPA Interface Standard is USB 1.1 limited to 12 Mbit/s, SpaceWire 400~600 Mbit/s."]
[9.086627960205078, 5.832372188568115, "The Attitude Measurement Devices of the Spacecraft Satellite is Miniature Spinning Sun Sensor (MSSS), two single-axis Inertial Reference Units (IRU), and a Flux Gate Magnetometer (FGM)."]
[4.528216361999512, 6.4177727699279785, "The Components of the Communications Payloads Payloads is Common, monolithic LNAs (Low Noise Amplifiers) and T/R (Transmit / Receive) switching protection circuits."]
[3.9473118782043457, 6.429089546203613, "The Modulation Scheme of the VHF and UHF Links Communication Links is GMSK (Gaussian Minimum Shift Keying)."]
[7.266080379486084, 7.884638786315918, "The Coverage Regions of the MOMS-02 Instrument is General."]
[10.432522773742676, 3.5213491916656494, "The Velocity of the QUESS Satellite is 8 km/s."]
[9.912797927856445, 7.77083683013916, "The Energy Threshold of the CRaTER Cosmic Ray Telescope is >10 MeV."]
[6.618193626403809, 0.898059606552124, "The Agreement Date of the FormoSat-7/COSMIC-2 Satellite Satellite is October 2017."]
[7.151559352874756, 3.2756950855255127, "The Communication Status of the MarCO CubeSat is Silent."]
[9.593406677246094, 2.3137314319610596, "The Cross-Calibration Target of the CloudSat Satellite is Ocean surface."]
[7.045044422149658, 0.768308162689209, "The On-Orbit Operations of the SENSE Satellites Satellite is August 8-13, 2015."]
[10.314619064331055, 5.31447696685791, "The Volume of the Xenon Gas Tank Propellant Storage is 49 liter."]
[7.692692756652832, 0.1155725046992302, "The Testing Start Date of the Prichal Module is Early October 2021."]
[9.54085922241211, 9.556733131408691, "The Mass of the SAGE-III Instrument is 76 kg."]
[8.837967872619629, 1.4022589921951294, "The Risk of the Van Allen Probes Satellite is Earth could be at risk for up to trillions of dollars of damage."]
[8.79670524597168, 10.744385719299316, "The Time Resolution of the MTEL Space Telescope Telescope is 1,000 times better than CCD cameras."]
[7.26206636428833, 3.85825252532959, "The Instrument Concept of the GeoSTAR-III Satellite System is Unknown."]
[9.188599586486816, 3.2284095287323, "The Orbit Type of the QuakeSat Satellite is Near-circular sun-synchronous dawn-dusk orbit."]
[10.1516752243042, 5.137941837310791, "The Operation Principle of the EMP (Electromagnetic Pump) Pump is Utilizes the Lorentz body force to propel the electrically conductive fluid inside the toroidal channel."]
[8.684720039367676, 9.168546676635742, "The Entrance Slit Dimensions of the Spectrometer Instrument is 0.3 mm x 7 mm."]
[11.786728858947754, -0.9646486639976501, "The Mass of the SCCO Payload is 28 kg."]
[7.040868759155273, 3.6507694721221924, "The Purpose of the Vizca\u00edno Biosphere Reserve Biosphere Reserve is Important whale sanctuary for the North Pacific grey whale."]
[12.982735633850098, 4.859463691711426, "The Imager Start Date of the IBEX Satellite is Late 2016."]
[7.864943027496338, 7.76576042175293, "The Bore Site Shift of the OCO Instrument CO2 Channel is ~70 arcsec."]
[13.107502937316895, 4.055604934692383, "The Device Operating Temperature of the Gaia Satellite is 130 K."]
[9.924337387084961, 7.11706018447876, "The Thermal Conductivity of the Carbon-Carbon Radiator panel Radiator Panel is 230 W/m K."]
[8.569611549377441, 10.397293090820312, "The CCD Detector of the PS0 Optical Instrument is 11MP."]
[8.033194541931152, 8.940412521362305, "The Wavelength Range of the S-020 XUV Spectrograph is 1-20 nm (or 10 - 200 \u00c5)."]
[7.836314678192139, 9.187715530395508, "The Spectral Sampling Interval of the HR Spectrometer Spectrometer is 0.0933 nm/pixel."]
[9.019866943359375, 5.337566375732422, "The Challenge of the Attitude Control System Satellite System is Inability to achieve sustained nadir pointing."]
[8.866711616516113, 8.737762451171875, "The Detector Type of the TIR Subsystem Imaging System is Mercury cadmium telluride (HgCdTe)."]
[7.557143211364746, 4.791662216186523, "The Primary Images of the PROBA-V Satellite is 14.021."]
[7.292394161224365, 8.19635009765625, "The Pointing Accuracy of the MWI Instrument Scan Mechanism Assembly is Unknown."]
[6.405858993530273, 8.329055786132812, "The Number of Channels of the SMMR Scanning Multispectral Microwave Radiometer is 10."]
[2.979809045791626, 6.663251876831055, "The Power of the L-band Transmitter Radio Transmitter is 10 W."]
[7.211395740509033, 6.887601375579834, "The Operational Mode of the Aquarius Radiometer System is Standby."]
[7.6209259033203125, 8.54527473449707, "The Vertical Resolution of the OMPS UV Hyperspectral Imaging Spectrometer is 1 km."]
[5.046137809753418, 4.646875858306885, "The Staffing of the Ground Segment Ground Segment is 24 hour period during the mission."]
[11.703775405883789, 2.599400520324707, "The Primary Semi-Major Axis of the Didymos Binary System is 1.1 km."]
[4.680156230926514, 4.27628231048584, "The Components of the Drum Mounting Assembly is Digital data subsystem, power and the signal transfer assembly."]
[7.714195251464844, 13.590850830078125, "The No. of Bins of the SPIM1 Spectrometer is 68, 136, or 272."]
[6.101292610168457, 2.757315158843994, "The Role of the Space Development Agency Agency is Accelerate delivery of needed space-based capabilities to the joint warfighter."]
[6.422937870025635, 4.792586326599121, "The Contents of the Level-3 Data is Spatially and temporally averaged data of geophysical parameters."]
[5.3119049072265625, 10.39382266998291, "The Measurement Domain of the ISS:LIS Lightning Imaging Sensor is Atmosphere."]
[6.523021221160889, 8.535874366760254, "The Swath Width of the MWR Dicke Radiometer is 380 km."]
[11.596588134765625, -1.261332631111145, "The Mass of the MKA-N 2 Satellite is 10 kg."]
[4.60313081741333, 0.20877309143543243, "The Initial Size of the OneWeb Satellite Constellation is 650."]
[10.852317810058594, 3.986917018890381, "The Transiting Exoplanet Survey Satellite of the TESS Space Mission is Upcoming."]
[7.90501594543457, 9.297555923461914, "The Spectral Bandwidth of the SWIR Spectrometer Spectrometer is 10 nm."]
[9.107860565185547, 10.7835111618042, "The Swath Width of the PamCam Panoramic Camera is Approximately 250 km."]
[11.373466491699219, 3.9221158027648926, "The Orbital Period of the Planet Candidate Exoplanet is Roughly every 70 years."]
[4.1401519775390625, 5.593443870544434, "The Upload Data Rate of the IXPE Satellite is 2 kbit/s."]
[7.611259460449219, 7.599973678588867, "The Function of the POAM-II Payload System is Provide a measurement of the vertical distribution of atmospheric ozone, nitrogen dioxide, aerosol extinction, water vapour and temperature."]
[8.462129592895508, 5.059254169464111, "The Fine-Pointing Capability of the ATLAS-1 Satellite Mission is Limited."]
[6.302274703979492, 4.957383632659912, "The Contents of the Level-1A Data is Granule scene sensor output data with geolocation and radiometric correction information."]
[8.554102897644043, 8.565969467163086, "The Number of Detectors of the SIS (Scanning Imaging Spectrograph) Spectrograph is 2."]
[11.201781272888184, 3.0634663105010986, "The Diameter Range of the Kuiper Belt Object Celestial Object is 50 to 2,000 kilometers."]
[9.843213081359863, 7.935018062591553, "The Resolution of the HIT High-energy Ion Telescope is 1 min."]
[5.718648433685303, 9.141139030456543, "The Power of the Instrument Sensor is 35 W average."]
[6.7511091232299805, 10.167378425598145, "The Primary Use of the Band 2 Spectral Band is Daytime clouds, vegetation, water."]
[11.710524559020996, -1.1529754400253296, "The Mass of the SARAL spacecraft Satellite is 407 kg."]
[11.4838228225708, 4.198840618133545, "The Sun Size Comparison of the TRAPPIST-1 Star System is Not much bigger than Jupiter."]
[10.333061218261719, 7.177738666534424, "The Material of the Cold Plates Thermal Management Component is Stainless steel channelling enclosed in an aluminum casting."]
[7.362125396728516, 1.4135240316390991, "The Forecast Date of the Hurricane Michael Tropical Cyclone is 8 Oct 2018."]
[9.423017501831055, 9.054808616638184, "The Mask Material of the Optical Head Optical Device is Steel."]
[8.570021629333496, 6.946707725524902, "The Magnetic Cleanliness Requirement of the Magnetometers Instrument is Sub nT-range for VFM and ASM."]
[6.987259387969971, 1.005152702331543, "The Communication Reestablishment Date of the STEREO-B Satellite is Aug. 21, 2016."]
[2.2432801723480225, 6.499667167663574, "The Latency of the ATL16 ATLAS Atmosphere Weekly Data is 45 days from receipt of last data in product."]
[10.43359375, 4.775830268859863, "The Isp of the Hydrazine system Orbit control subsystem is 210 s."]
[3.813161849975586, 4.447498321533203, "The Model of the OBC On-Board Computer is GomSpace NanoMind A712D."]
[8.267528533935547, 9.2395601272583, "The Bands of the Optical Sensor Assembly (OSA) Instrument is Four multispectral bands and one panchromatic band."]
[11.625410079956055, 6.2275848388671875, "The Announcement Date of the XMM-Newton Satellite is Dec. 21 2007."]
[7.297482013702393, 0.028807731345295906, "The End of life date of the Meteor-M-2 Satellite is 31 Dec 2030."]
[10.361235618591309, 1.3198851346969604, "The LTAN of the Main Payload Satellite is 10:39 hours."]
[11.187088012695312, 3.497303009033203, "The Distance from the Sun at Expected Perihelion of the Comet ATLAS Comet is Around 37 million kilometers."]
[4.7058024406433105, 1.839209794998169, "The Number of Satellites of the Lightspeed Satellites Satellite is Nearly 300."]
[7.120168209075928, 0.2970355153083801, "The Launch Start Date of the Transport Layer Satellite Network is Late 2024."]
[7.774700164794922, 9.444234848022461, "The Spectral Resolution of the HR Bands (677\u2013686 nm, 740\u2013759 nm and 769\u2013780 nm) Spectral Bands is Principally driven by the slit width (Figure 23a)."]
[6.168887615203857, 4.1106181144714355, "The Ground Segment of the CO2Image Satellite is DLR\u2019s Space Operations facility."]
[6.058638572692871, 0.6159910559654236, "The Manifested Date of the ELaNa-4 CubeSats Satellite is March 1, 2013."]
[5.931477069854736, 5.40964937210083, "The GPS Receiver of the RAX-1 Satellite is Operated as predicted and maintained lock in the experimental zones."]
[5.124847412109375, 5.481825351715088, "The Broadcast Bands of the First Batch of Satellites Satellite is \"Ku\" band."]
[7.840835094451904, 10.016765594482422, "The FOV for VNIR-P pushbroom scanning of the VNIR-NP Imager is 55\u00ba."]
[4.681640625, 4.484805583953857, "The Conference Date of the High Data Rate Optical Inter-Satellite Links Communication System is Sept. 20-24, 2009."]
[11.790555000305176, 4.707147121429443, "The Outflow Channels of the Milky Way Galaxy is Above and below the plane of the Milky Way."]
[8.910304069519043, 6.673835754394531, "The Period of the Lateral Shearing Angular Period Device is 200 \u00b5rad."]
[5.7267842292785645, 9.1249418258667, "The Instrument Power of the AATSR Instrument is 100 W."]
[8.178764343261719, 8.652142524719238, "The Measurement Accuracy - Location of the Instrument Sensor is 1 pixel."]
[9.546815872192383, 4.106875896453857, "The Size of the Sundancer Spacecraft is ~180 m3."]
[7.892696857452393, 8.003738403320312, "The Sample Rate of the MGF Instrument is 160 per second."]
[5.636347770690918, 9.160099983215332, "The Average Power Consumption of the Instrument Instrument is 5.6 W."]
[6.85128927230835, 6.792932033538818, "The Impact of the CATS Lidar Instrument is Enabled more accurate aerosol modeling and forecasting."]
[9.058446884155273, 10.639440536499023, "The Spatial Resolution of the TAC Camera is 2.1 m."]
[6.503304481506348, 0.5388383865356445, "The Launch Date of the FASat-Alfa Satellite is August 31, 1995."]
[10.668235778808594, 3.423917770385742, "The 3\u03c3 Low Result of the Close Approach Distance Parameter is 1.45 km."]
[3.402420997619629, 5.280274391174316, "The Mass Data Storage of the DubaiSat-2 Satellite is 256 GBit."]
[6.515391826629639, 0.5777730345726013, "The Launch Date of the SkySat-4-7 Satellite is September 16, 2016."]
[5.397286415100098, 2.9786288738250732, "The Alias of the AstroBus-L platform Satellite Platform is AstroSat-250 (AS250)."]
[4.534691333770752, 2.1912097930908203, "The Number of Satellites Launched of the Starlink Communication Satellite is 60."]
[5.013270378112793, 4.5957231521606445, "The Scanning Pattern Loss of the OGS Ground Station is Applies during initial acquisition."]
[6.909966468811035, 0.356147438287735, "The Launch Date of the OFEQ-1 Satellite is September 1988."]
[3.24877667427063, 5.61881685256958, "The Checksum Size of the Raw Science Data Packet Data Packet is 1 byte."]
[10.441298484802246, -0.9602082967758179, "The Mass of the ZASat-002 Microsatellite is 82 kg."]
[8.577632904052734, 1.6868399381637573, "The Retirement Date of the Kepler space telescope Telescope is 2018."]
[11.340594291687012, 6.990330696105957, "The Energy Resolution Improvement of the NICER X-ray Timing Instrument is A factor of 8 improvement."]
[5.848968029022217, 4.983869552612305, "The Function of the SAR Controller Electronics SAR Controller Electronics is In charge of the command and control of the SSS to achieve the SAR mission."]
[9.561112403869629, 0.7640473246574402, "The On-Orbit Duration of the CanX-5 Satellite is More than one year."]
[9.5782470703125, 7.928990364074707, "The Ion energy of the Microdosimeter A Instrument is > 1 MeV."]
[0.9233404397964478, 4.260723114013672, "The Capacity of the NiH2 batteries Power Source is 12 Ah."]
[11.827527046203613, 3.1816670894622803, "The Inclination of the Secondary Payloads Nanosatellites and CubeSat is ~51.6o."]
[10.800782203674316, 3.419640064239502, "The Closest Edge Distance from Earth of the Heliosphere Space Phenomenon is More than ten billion miles."]
[8.120177268981934, 1.2555891275405884, "The Mirror Alignment Continues Date of the Webb Satellite is 25 February 2022."]
[7.859866142272949, 8.760820388793945, "The Minimum Value of the Spectral Angle Measurement is Achieved when the yellow-gold reflection of the satellite bus is prominent."]
[8.128063201904297, 9.627464294433594, "The Band of the SWIR Camera Imaging System is 0.9 to 1.7 \u00b5m."]
[6.603428363800049, 1.3610621690750122, "The Launch Year of the Capella X-SAR Constellation Satellite Constellation is 2018."]
[10.631827354431152, 8.501049041748047, "The Bandpass of the COR1 Coronagraph1 imager is 648-750 nm."]
[8.572638511657715, 5.344860076904297, "The Pointing Accuracy of the S/C Satellite is Within 5-10\u00ba."]
[10.258646011352539, -0.919965922832489, "The Volume of the GHGSat-D Microsatellite is 20 x 30 x 42 cm."]
[9.63623046875, 2.273122787475586, "The Cross-Calibration Latitude of the CloudSat Satellite is 12 degrees."]
[8.298676490783691, 6.460198879241943, "The Area Collection Rate of the Pushbroom Sensor is Very high."]
[5.228785514831543, 3.0224359035491943, "The Signal Data Provider of the AMBER IOD-3 CubeSat is National Maritime Information Centre (NMIC)."]
[11.344039916992188, 2.2507903575897217, "The Size of the Hayabusa-2 Space Probe is Fridge-sized."]
[11.554102897644043, 3.3753113746643066, "The Signal to Noise of the Polar Scout Satellite is Best at high elevation angles."]
[6.057684421539307, 9.667991638183594, "The Mass of the Satellite Observation Instrument is 19.6 kg."]
[2.169736623764038, 4.5586256980896, "The Up to 15 W of the CLAVIS Power Generation is True."]
[9.168723106384277, 1.110487461090088, "The Operational Duration of the OPAL Satellite is 29 months."]
[8.614225387573242, 7.928464889526367, "The SRAMs Memory of the RADMON Radiation Monitor is 4-kbit each."]
[11.824291229248047, 4.646256923675537, "The Distance from Earth of the Carina Nebula Nebula is 7500 light-years."]
[7.372747421264648, 1.5544443130493164, "The Presentation Date of the MICROSCOPE Satellite is Sept. 27-Oct. 1, 2010."]
[6.0622382164001465, 0.89741051197052, "The Re-Entry Survival of the QARMAN CubeSat is Yes."]
[7.599066257476807, 4.4901957511901855, "The Decade-Daily Global Composite Products of the PROBA-V Satellite is 36."]
[6.883078575134277, 8.05191707611084, "The Design and Performance of the Dual-channel Radiometers for Earth and Atmosphere Monitoring (DREAM) Radiometer is Protoflight Model."]
[10.018592834472656, 3.0399248600006104, "The Orbit of the AVUM Spacecraft is Final Orbit (1450 km x 1450 km, i=69.5\u00ba)."]
[9.457866668701172, 5.786953926086426, "The Size of the Reaction Wheels Attitude Control System is Large (0.2 Nm, 12 Nms)."]
[6.4434003829956055, 1.0148006677627563, "The Flight Results Presentation Date of the BIRD Onboard Navigation System Navigation System is Oct. 22-25, 2002."]
[10.739733695983887, 10.295516014099121, "The Threshold programmability of the PHA Detector is Up to 6% of full scale."]
[9.667123794555664, 8.667136192321777, "The Manufacturer of the PP Twin Telescopes Telescope is SAGEM-REOSC."]
[7.012547969818115, 5.023824691772461, "The Data Usage of the Copernicus Sentinel-5P Satellite is Track and attribute methane emissions."]
[9.592081069946289, 5.9318742752075195, "The Power of the ADCS Attitude Determination and Control System is 0.66 W."]
[6.63820219039917, 0.909907341003418, "The Power Protection Design of the FormoSat-5 Satellite is Unknown."]
[6.154503345489502, 6.809514045715332, "The Minimum Separation for Distinguishing Spacecraft of the TIRA Radar Tracking Station is 5 km."]
[9.978161811828613, 9.482254981994629, "The Spatial Resolution of the IRIS Instrument Spectral Scanner is 10 m GSD."]
[7.688908576965332, 9.946240425109863, "The Channels of the VNIR Sensor is 14."]
[6.78842830657959, 0.37131190299987793, "The Launch Date of the MSG-3 Satellite is July 5, 2012."]
[8.048784255981445, 9.452412605285645, "The Wavelength Range of the SWIR Detector is 1.58 - 2.49 \u03bcm."]
[6.997029781341553, 1.2708745002746582, "The Conference Date of the EarthCARE/CPR Satellite is Sept. 24-27, 2012."]
[8.9862060546875, 8.942429542541504, "The Focal Length of the TIR Subsystem Imaging System is 31.14 mm."]
[6.854050636291504, 4.797216415405273, "The Imaging Mode of the CHORUS Satellite is WideFine mode with 8m resolution."]
[6.859543800354004, 5.5612993240356445, "The Freeze/Thaw State Refresh Rate of the SMAP Satellite is 2 days."]
[8.815781593322754, 7.613067626953125, "The Electric Field Property of the IVM Ion Velocity Meter is Direction parallel to the Earth's magnetic field is an electric equipotential for horizontal scales greater than 25 km."]
[8.349937438964844, 7.476894378662109, "The Purpose of the SES Instrument is Calibrate and control the photon flux."]
[5.26609468460083, 3.1692540645599365, "The Satellite Bus of the Tomorrow-R1 and -R2 Satellite is Corvus-XL satellite platform."]
[8.640512466430664, 7.418270587921143, "The Components of the KSEM Instrument is Particle Detector (PD), Magnetometer (MAG), and a Satellite Charging Monitor (SCM)."]
[6.210775375366211, 2.140719413757324, "The Conference Presentation Date of the TacSat-4 Satellite is Feb. 24-26, 2009."]
[5.848676681518555, 8.619559288024902, "The Units of the MWHS-II Microwave Humidity Sounder is Antenna and receiver unit, power supply unit and electronic unit."]
[6.631083965301514, 8.723711967468262, "The Swath Width of the MWNIR Imaging System is 1600 km."]
[9.385345458984375, 3.860630989074707, "The Platform Reference of the BRITE Satellites Satellite is CanX-3."]
[7.600078582763672, 5.742988109588623, "The Calibration Resolution of the Satellite Device Unknown is 1.3 k."]
[4.605146884918213, 3.6730029582977295, "The Objective of the AIS Automatic Identification System is Provide a SAR data fusion capability for maritime surveillance from space with AIS data services."]
[8.477152824401855, 11.07551383972168, "The Array of the Eastman Kodak KLI14403 linear CCD sensor Sensor is 14,400."]
[7.990169048309326, 4.092291831970215, "The Image Resolution of the RapidEye Satellite Constellation is 30 cm."]
[4.45615291595459, 3.9937026500701904, "The Software of the TIE Payload is BASH."]
[4.700052738189697, 5.7131028175354, "The Communication Frequency of the Spacecraft Satellite is S-band RF (radio frequency)."]
[6.740096092224121, 1.7656351327896118, "The Mini-commissioning Phase of the Envisat Satellite is November and December 2010."]
[7.897304534912109, 3.5587868690490723, "The Orbit Offset of the ERS-2 Satellite is 2 km versus nominal ground track."]
[7.261153697967529, 0.9776382446289062, "The Deployment Date of the MicroMAS-1 Satellite is March 4, 2015."]
[10.32149600982666, 3.107588052749634, "The Orbit Altitude of the Secondary Payloads Satellite is ~820 km."]
[3.558922529220581, 2.2795889377593994, "The Size of the QBus-1 Satellite is 2U."]
[9.648970603942871, 3.89998459815979, "The Deployment Mechanism of the CanX-7 Satellite is Stored mechanical energy."]
[7.879208087921143, 1.0695043802261353, "The Image Release Date of the MERIS Satellite is Nov. 15, 2013."]
[8.608880043029785, 9.371169090270996, "The Ground Pixel Size of the HORUS Sensor is 14.6 m."]
[4.804596900939941, 3.2357254028320312, "The Expected Number of AIS Signals of the ZACUBE-2 Satellite is 6000."]
[8.435224533081055, 10.367136001586914, "The CCD Array Size of the Instrument Sensor is 128 x 128 pixels."]
[3.632370710372925, 2.270737648010254, "The Size of the Tyvak 61C Satellite is 3U."]
[7.551069736480713, 4.396439075469971, "The Contribution to Environmental Monitoring of the LARES Satellite is Unknown."]
[7.3081254959106445, 0.19392754137516022, "The Development Status of the DRACO System is Ongoing."]
[8.894447326660156, 10.181854248046875, "The Type of the Camera Sensor Imaging System is EEV CCD04-06 image sensor + chip set."]
[8.522062301635742, 5.518889427185059, "The On-Orbit Calibration Method of the RAX-1 Satellite is Used the IGRF magnetic field model and current satellite measurements."]
[11.348396301269531, 1.1205191612243652, "The Rover Operation Duration of the Tianwen-1 Probe is About 90 Martian days."]
[8.514192581176758, 0.15532644093036652, "The Storage and Reuse Capability of the OWS Space Station is Yes."]
[7.332886219024658, 5.206832408905029, "The Goal of the RAIDS Experiment is Obtain a set of simultaneous airglow profiles at a number of wavelengths."]
[8.137408256530762, 9.358650207519531, "The Wavelength Range of the NIR Detector is 0.83 - 1.74 \u03bcm."]
[4.232423782348633, 5.855715274810791, "The Ka-band System of the STPSat-6 Satellite is Transmit up to 622 Mbit/s."]
[8.839089393615723, 3.656442165374756, "The Cross-Track Separation of the TDX and TSX Satellites Satellites is 3600 m over the equator."]
[9.022507667541504, 4.99489164352417, "The Operation Attitude of the Satellite Communication is Maximum power generation attitude with the \u2013Z satellite face sun pointing."]
[8.883042335510254, 1.9904818534851074, "The URL of the BepiColombo Mission is http://sait.oat.ts.astro.it/MSAIS/20/PDF/127.pdf."]
[8.811490058898926, 1.4979294538497925, "The Whistler Waves Amplitudes of the Van Allen Probes Satellite is Unusually large."]
[5.063198089599609, 8.716750144958496, "The Position Accuracy (RMS orbit) of the S-3 NTC Product is 3 cm threshold with a target of 2 cm (radial)."]
[9.919943809509277, 5.056949615478516, "The Purpose of the Gasket Satellite Component is Create a light-tight seal."]
[9.40465259552002, 9.960265159606934, "The Objective of the APD detector Experiment is Observe the low energy charged particle density distribution in LEO (Low Earth Orbit)."]
[8.434435844421387, 4.3787841796875, "The Groundtrack Mission Requirement of the EO-1 Satellite is Fly over the current groundtrack of Landsat-7 within \u00b13 km."]
[9.522801399230957, 5.481849193572998, "The Stabilization of the AOCS Attitude and Orbit Control Subsystem is Three-axis."]
[7.093276500701904, 2.542613983154297, "The NASA URL of the BioSentinel Satellite is https://www.nasa.gov/centers/ames/engineering/projects/biosentinel.html."]
[3.374225378036499, 5.682357311248779, "The Data Delivery of the Science Data Interface Interface is 1/8/64 science data packet(s) every 3 seconds."]
[10.997511863708496, 4.09806489944458, "The Mission of the Roman Satellite is Provide 3D images of the universe."]
[6.919137001037598, 0.5427790880203247, "The Operational Date of the QUESS satellite Satellite is January 19, 2017."]
[11.675873756408691, -1.029160499572754, "The Mass of the Propulsion Satellite Subsystem is 1.1 kg."]
[5.003758430480957, -0.14685598015785217, "The Launch Date of the OneWeb Satellite Constellation is 7 February, 2020."]
[6.3409743309021, 6.730461597442627, "The Performance Check Modes of the ARC Active Radar Calibrator is Receiver mode, Transmitter mode, Transponder mode with delay."]
[8.287994384765625, 3.646293878555298, "The Mission Concept & Status of the TanDEM-X Satellite is Not Provided."]
[2.219334840774536, 1.7338961362838745, "The GMU Modification of the I-COUPS Satellite is Addition of CTU and modification of GMU."]
[9.996413230895996, 4.135630130767822, "The Simulation Study of the Solar Wind Electric Sail Propulsion System is P. Janhunen, A. Sandroos."]
[2.261037826538086, 3.8860208988189697, "The Solar Panels of the Lander Spacecraft is Vertical panels."]
[9.480472564697266, 5.687753200531006, "The Attitude Error of the AOCS Attitude Control System is <0.3\u00ba."]
[10.361495971679688, 4.997226715087891, "The Thrust of the Steam Propulsion Unit Propulsion is 4 mN."]
[6.546573162078857, 1.3324368000030518, "The Additional Contract Award Date of the SARah project Satellite Project is 7 August 2019."]
[6.077455043792725, 11.250031471252441, "The Approx. peak sensitivity altitude of the Channel 8 Sensor is Unknown."]
[3.7368433475494385, 4.565413951873779, "The Microcontroller of the On-board Computer Computer is Motorola 68332."]
[3.5551247596740723, 4.083746910095215, "The SCI ports of the STRV-2 DHS Data Handling System is Six RS-422, MIL-STD-1553 S/C bus."]
[8.034940719604492, 1.2563815116882324, "The Date of the Phytoplankton Productivity Down in Gulf of Maine Natural Event is 8 June 2022."]
[5.491811752319336, 4.6161112785339355, "The Application of the Geostationary Communication Relays Satellite-based Service is Communication."]
[3.0807173252105713, 5.875023365020752, "The Low Cost of the MTP Transponder is True."]
[4.736402988433838, 1.7537903785705566, "The Number of Satellites of the PanGeo Fleet Satellite Fleet is 9."]
[8.095585823059082, 8.737298011779785, "The URL of the Miniature Integrated Camera and Imaging Spectrometer Imaging Spectrometer is http://nmp.nasa.gov/ds1/tech/micas.html."]
[8.803380966186523, 6.507167816162109, "The Purpose of the BPP Bi-axial Pointing Platform is Enable the High-Resolution Camera to point in the direction of its targets and keep its field of view stable."]
[12.124960899353027, 3.301666259765625, "The Inclination of the SAOCOM-1A and -1B Satellites is 97.86\u00b0."]
[7.610818862915039, 6.623978137969971, "The Total O3 of the O3 Profile Satellite Instrument is 9 x 10 3."]
[9.759635925292969, 4.920287609100342, "The Firing Duty Cycle of the Y-axis Bang-Bang Maneuver Satellite Maneuver is 90%."]
[6.083869457244873, 6.249283313751221, "The Application of the SAR Mode Synthetic Aperture Radar Mode is Fully polarimetric 3-D structure mode and the ultra-wide swath deformation mode."]
[6.941572189331055, 3.007855176925659, "The Data Center of the Euclid Satellite is CosmoHub hosted by PIC."]
[7.146020889282227, 9.48515510559082, "The Band 2 of the CIRiS Instrument is 9.85 \u00b5m to 11.35 \u00b5m."]
[6.564418792724609, 3.3507888317108154, "The Payload of the MPQ442 Satellite is OpenSpace365."]
[4.861588001251221, 2.2115113735198975, "The Mission Quantity of the CubeStack Multi CubeSat Adapter is 2."]
[6.878059387207031, 1.2350184917449951, "The Conference Date of the CHIPS Satellite is Aug. 11-14, 2003."]
[6.779015064239502, 5.475882053375244, "The Importance of the SMAP Satellite is Understanding of Earth's cycles."]
[6.597695350646973, 3.2117390632629395, "The Operator of the Resurs-P1 Satellite is Roskosmos."]
[3.4030210971832275, 5.277072906494141, "The Onboard Data Storage Capacity of the XMM-Newton Satellite is None."]
[8.732022285461426, 5.33305549621582, "The Axis Orientation Accuracy of the Resurs-DK1 Spacecraft is 0.2 arcmin."]
[7.860891819000244, -0.575140655040741, "The URL of the SpaceX CRS-24 Mission is https://www.issnationallab.org/iss360/spacex-crs-24-mission-overview/."]
[7.959237098693848, 10.100215911865234, "The Geolocation Accuracy of the Imager Imaging System is \u2264 3 m."]
[10.335556030273438, 6.193305969238281, "The URL of the THERME experiment Experiment is http://esmat.esa.int/Materials_News/ISME09/pdf/10-In-flight/Remaury%20Paper.pdf."]
[5.567305088043213, 0.4577644169330597, "The Extreme to Exceptional Dryness Percentage of the U.S. Drought Monitor Report is 83 percent."]
[8.191070556640625, 0.9210113883018494, "The Long-Term Acquisition Plan Publication Date of the Landsat-7 Satellite is Oct. 2006."]
[8.483420372009277, 8.5037841796875, "The Detector Operation of the SIS (Scanning Imaging Spectrograph) Spectrograph is Selected by a \u201cpop-up\u201d mirror."]
[8.05125904083252, 9.453743934631348, "The Wavelength Range of the SiPD Detector is 0.50 - 0.90 \u00b5m."]
[7.581658363342285, 7.954351902008057, "The Manufacturer of the Ozone Mapping and Profiler Suite-Nadir (OMPS-N) Instrument is Ball Aerospace."]
[5.434543132781982, 3.529500722885132, "The Manufacturing Process Controls of the Frangible Joint System Satellite Component is Sufficient to assure that variability in materials properties and hardware component dimensions, within both maximum and minimum tolerances, will not invalidate design performance requirements."]
[8.004212379455566, 9.72120189666748, "The Number of Bands of the OHIS Imaging System is 80."]
[11.651312828063965, -1.1655827760696411, "The Mass of the FLP Satellite is 120 kg."]
[3.8132283687591553, 6.065362930297852, "The Ku-band Link Availability of the Bartolomeo Payload Communication System is 70 - 90%."]
[5.139895439147949, 4.198098659515381, "The Contact Operations of the COSMOS Mission Operations System is Pre-contact operations, real-time contact operations, and post-contact operations."]
[4.498590469360352, 2.2525205612182617, "The Number of Satellites of the Starlink Communication Satellite is 422."]
[9.327466011047363, 0.337787002325058, "The Exceeded Design Life of the Jason-1 Satellite is Yes."]
[5.076071739196777, 6.274169921875, "The Connector Type of the Antennas Communication is MMCX."]
[5.047543525695801, 3.3007054328918457, "The Payload of the ZACUBE-2 Satellite is SDR-based payload that will provide AIS and VDES services."]
[3.91117525100708, 5.671604156494141, "The RF Link Speed of the BILSAT-1 Satellite is 2 Mbit/s."]
[7.858150005340576, 3.4711599349975586, "The Mission of the Satellogic Company is Build an accurate and up-to-date picture of our planet."]
[6.582196235656738, 3.772007465362549, "The Weather Data of the Spire Global Satellite is Improve Maritime Vessel Performance and Reduce Carbon Emissions."]
[9.626813888549805, 9.470331192016602, "The Activation and Calibration Time of the SAGE-III Instrument is Approximately 90 days."]
[6.648120880126953, 0.43303337693214417, "The Docking Date of the Intelsat 901 Satellite Communication Satellite is 27 February 2020."]
[11.712820053100586, -1.151462197303772, "The Maximum Satellite Mass of the AD-SS 200 Satellite Dispenser is 200 kg."]
[5.93046760559082, 6.7816643714904785, "The Minimum Looks in Range of the Radar Sensor is 12 looks for 3 km cells."]
[3.7409658432006836, 6.552696228027344, "The Telemetry S-band of the RF communications Communication Subsystem is 0.1 W, 9.6 kbit/s."]
[7.769226551055908, 2.4970202445983887, "The Mission Date of the NovaSAR-1 Satellite is Sept. 13-14, 2012."]
[7.539840221405029, 1.3062688112258911, "The Mission Start Date of the HEOSS High Earth Orbit Space Surveillance is Late 2015."]
[8.760137557983398, 10.194682121276855, "The Components of the DDS Deployment Detection Subsystem is COTS camera."]
[7.632176876068115, 5.417438983917236, "The Instrument Behavior of the OCO-2 Satellite is Change in flight."]
[9.954183578491211, 7.679039478302002, "The High Energy Telescope Energy of the CRS Cosmic Ray Subsystem is 70MeV."]
[4.188870906829834, 3.7964046001434326, "The Faraday Rotation of the AIS System Communication System is Inversely proportional to the square of the frequency."]
[5.383425235748291, 2.5164647102355957, "The Network Type of the Iridium NEXT Satellite Constellation is IP-based, broadband."]
[11.60706615447998, 4.3830060958862305, "The Distance from Earth of the Kepler-1649c Exoplanet is 300 light-years."]
[5.4219465255737305, 3.2459166049957275, "The Bus Design of the ERG Satellite is Small science satellite bus design."]
[9.188522338867188, 10.137964248657227, "The Number of Cameras of the MoonKAM Camera System is 4 on each vehicle."]
[9.55654525756836, 7.808548927307129, "The Range of the Incident Particle Energy Range Parameter is > 20 MeV (H), > 87 MeV/nucleon (Fe)."]
[8.460201263427734, 9.1616849899292, "The Band 5 of the R3 Sensor Sensor is Red."]
[7.735430717468262, 9.089701652526855, "The Spectral Range of the TIR Thermal Infrared region is 2.15-2.25 \u00b5m."]
[7.245236396789551, 5.887747287750244, "The Mechanisms of the Aerosol Indirect Effect Atmospheric Phenomenon is 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."]
[7.284359931945801, 0.4693942666053772, "The Actual Launch Date of the Spacelab-1 Satellite is End of November 1983."]
[4.712370872497559, 6.013792037963867, "The Function of the Antenna System Communication System is Receive GRB and legacy GVAR downlinks."]
[7.850440502166748, 0.7295783162117004, "The Release Date of the DCAM3 Deployable Camera is 5 April 5 at 2:14 UT."]
[5.930750370025635, 5.927807807922363, "The Aperture Size of the Reflector Assembly Satellite Component is 14 m."]
[3.475956439971924, 4.80974006652832, "The Data Compression of the Onboard Data Handling Subsystem (OBDH) Data Handling System is Achieving compression ratios of 2.28 - 2.8."]
[9.31958293914795, 7.886279106140137, "The Detection Limit for Water Ice of the LEND Neutron Detector is ~0.1 wt%."]
[8.559917449951172, 3.4042248725891113, "The Orbit Position of the Vigil Spacecraft is L5 (Langrage Point 5)."]
[6.088377475738525, 4.375894546508789, "The Manufacturer of the European Robotic Arm Robotic Arm is Unknown."]
[8.847890853881836, 0.22424376010894775, "The Actual Orbit Duration of the Skylab-1 Space Station is Prematurely decayed."]
[7.3509111404418945, -0.13283225893974304, "The Launch Date of the Dnepr Rocket Rocket is June 19, 2014."]
[5.848690509796143, 2.259890079498291, "The L0 Product Destination of the EnMAP Satellite is DIMS Product Library."]
[6.983936786651611, 1.5259288549423218, "The Integration Date with GEOSS of the GMES Program is 2016."]
[8.737589836120605, 7.089833736419678, "The Mechanical Coupling of the Readout Electronics Electronics is No."]
[7.522377967834473, 3.7120022773742676, "The Relative Position of the AC4-B Satellite is Below AC4-A."]
[4.342207431793213, 5.039190769195557, "The Method of the Data Transmission Process is Placing it into an ftp-site with password protection."]
[8.514066696166992, 3.6959011554718018, "The Track Spacing of the ERS-1 Satellite is ~8 km at the equator."]
[8.727971076965332, 7.225098133087158, "The Function of the V5 Sensor Sensor is Makes a simple voltage measurement near the magnetometer boom and may be used to infer the sunward electric field for plasma waves."]
[11.858763694763184, 2.386422634124756, "The Checkpoint Maneuver Altitude of the OSIRIS-REx Spacecraft is 410 feet (125 meters)."]
[5.978599548339844, 2.6455230712890625, "The Purchase of the THEMIS Satellite Constellation is Alliant Techsystems Inc. (ATK)."]
[1.9271177053451538, 4.21394681930542, "The Power of the Solar panels Power subsystem is about 35 W/panel (BOL)."]
[7.173166751861572, 6.926009654998779, "The Design Review Date of the IRIS instrument Instrument is December 2010."]
[7.560277938842773, -0.4928036630153656, "The Launch Pad Explosion Date of the SpaceX Falcon-9 Rocket is Sept. 1, 2016."]
[7.676352500915527, 9.638387680053711, "The Spatial Resolution of the SLSTR Spectral Imaging Instrument is 1 km."]
[8.858747482299805, 10.750962257385254, "The Data Rate of the LISS-4 Camera is 105 Mbit/s."]
[6.902170181274414, 0.5626545548439026, "The Launch Date of the GeoEye-1 Satellite is September 2008."]
[11.077558517456055, 2.7877542972564697, "The Previous Record Discharge of the Yellowstone River River is 32,200 cubic feet per second."]
[9.64742374420166, 1.1636102199554443, "The Validation Tests of the OCK (Orbit Control Kit) Orbit Control System is Three short tests lasting up to several days, followed by a 4th extended test that lasted two weeks."]
[11.26712417602539, 6.7190022468566895, "The Operation of the SEXTANT XFSW Navigation System is Observes MSPs, processes photon events, updates spacecraft state."]
[8.615480422973633, 10.006464958190918, "The Grid of the Phantoms Mannequin Torsos is Three-centimeter grid embedded throughout the torsos."]
[12.525410652160645, 6.893974781036377, "The Photon Counting Rate of the PSR B0531+21 Pulsar is Poisson Distribution."]
[10.525362968444824, 7.491739273071289, "The Type of the DERA-patented carbon-composite joint Spacecraft Structure is Novel."]
[9.496360778808594, 9.2811279296875, "The Diameter of the Central Obstruction Optical Component is 68 mm."]
[10.316681861877441, 4.8538737297058105, "The Thrusters of the Hydrazine system Orbit control subsystem is Four 1 N thrusters."]
[7.637171268463135, 7.886967182159424, "The Measures of the EMUS Spectrometer is Oxygen and carbon monoxide in the thermosphere and the variability of hydrogen and oxygen in the exosphere."]
[4.996519088745117, 4.935314655303955, "The Maximum Number of Transmission Attempts of the Drifting (Mobile) Platforms Ground Segment is 5 - 6."]
[6.2632575035095215, 6.320050239562988, "The Along-Track Resolution of the Copernicus Sentinel-6 Poseidon-4 Radar Altimeter is About 300 m."]
[5.431238651275635, 7.299690246582031, "The Beam width of the X-band Band is 0.15 rad."]
[8.193037033081055, -0.14893032610416412, "The Time to First Stage Landing of the Falcon 9 Rocket is Eight and a half minutes."]
[9.020895004272461, 5.923931121826172, "The IMU of the PSSCT-2 Satellite is COTS MEMS IMU (Inertial Measurement Unit) from Analog Devices."]
[2.297848701477051, 5.117830276489258, "The Average of the Power Consumption System is 2.4 W."]
[8.720601081848145, 7.938263893127441, "The Spectrometer Type of the INMS Ion Neutral Mass Spectrometer is Gated time-of-flight."]
[6.669651985168457, 1.2736027240753174, "The Research Contract Date of the Capella Space Company is 17 June 2021."]
[7.295319557189941, 8.243167877197266, "The Image Delivery Time of the 24/7 Emergency Image Delivery Service Service is Averaging two hours after acquisition."]
[9.50988483428955, 0.5062216520309448, "The Lifetime of the OFEQ-2 Satellite is 6 months."]
[6.928531646728516, 9.158354759216309, "The Antenna Aperture in the Azimuth of the P Mode Observation Mode is 7.5 m."]
[2.4696106910705566, 4.362981796264648, "The Budgets of the Spacecraft Spacecraft is Mass, Power, Data."]
[4.1612935066223145, 4.527054309844971, "The Function of the Microprocessor Component is Grouping the measurements into a packet and sending them over the I2C bus to the OBC for downlink transmission."]
[7.903420448303223, 9.181844711303711, "The Magnification of the HSC Spectrometer Spectrometer is 1:1."]
[10.449886322021484, 7.5759053230285645, "The Material of the RX-M2 Tower Structure is CFRP skins."]
[10.298810958862305, 2.722180128097534, "The Perigee of the COMPASS-2 Satellite is 402 km."]
[7.903467655181885, 5.893431186676025, "The Calibration Status of the Satellite Spacecraft is Calibrated."]
[6.578930377960205, 1.2373871803283691, "The Development Start Date of the SARah project Satellite Project is 19 September 2013."]
[5.126588344573975, 2.12862491607666, "The Number of Participating Students of the YES2 Satellite is About 400."]
[7.755163669586182, 8.950068473815918, "The Performance Improvement of the IASI-NG Instrument Spectral Resolution is 2 times."]
[6.985037326812744, 0.7270115613937378, "The Operation Status of the Genesis-2 Satellite is Nominal in 2013."]
[5.037795543670654, -2.3703842163085938, "The Affiliation of the Carlos Flores Engineer is Unknown."]
[4.7001423835754395, 1.8329739570617676, "The Constellation Size for Weekly Remapping of the Satellite Constellation Satellite Constellation is About 90 satellites."]
[3.794327735900879, 3.826110363006592, "The Communication of the CICERO satellites Satellite is X-band downlink of payload data."]
[6.86670446395874, 0.3461930453777313, "The Launch Date of the POPSAT-HIP1 Satellite is June 3, 2014."]
[9.980027198791504, 1.5249735116958618, "The Orbit Period of the Sentinel-2 satellites Satellite is 101 minutes."]
[5.842515468597412, 6.831982612609863, "The Center Frequency of the Radar Instrument is 1.26 GHz."]
[8.062877655029297, -0.7340965867042542, "The Launch Site of the Crew Dragon Spacecraft is Kennedy Space Center."]
[8.124541282653809, 2.264583110809326, "The Communication Experiment Date of the ARTEMIS satellite Satellite is Sept. 23-27, 2013."]
[6.449683666229248, 2.9751908779144287, "The Payloads of the Carbonite Series Small Satellite Platforms is Visible, MWIR, and X-band radar wavelengths."]
[6.990601539611816, 3.661864995956421, "The Purpose of the GeoXO Satellite System is Advance Earth observations from geostationary orbit."]
[6.210583209991455, 8.064746856689453, "The Antenna Scan of the MSR Radiometer is Oscillating 10\u00b0 either side of nadir."]
[6.0306525230407715, 9.618755340576172, "The Mass of the KGI-4C Instrument is 12 kg."]
[3.1632843017578125, 4.954841613769531, "The SCI of the OBC Onboard Data Handling is 38.4 kbit/s."]
[6.547965049743652, 5.592644691467285, "The Number of Alerts Per Day of the SKA Square Kilometre Array is Unknown."]
[10.33823013305664, 4.911715507507324, "The Thruster Type of the GPIM Propulsion System is Aerojet Rocketdyne GR-1 1-N class."]
[8.487637519836426, 8.481904983520508, "The Detector Technology of the SIS (Scanning Imaging Spectrograph) Spectrograph is Position-sensitive anode."]
[11.834959983825684, 1.046495795249939, "The Mission Tasks of the Chang'e-4 Probe is 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."]
[3.9039435386657715, 2.3054516315460205, "The Size of the OSIRIS CubeSat is 3U."]
[8.146158218383789, 10.014419555664062, "The Center Wavelength of the MS1 (NIR1) Imager is 831 nm."]
[11.561049461364746, 1.2207751274108887, "The Apogee of the Chang'e-1 Satellite is 51000 km."]
[7.902876377105713, 4.673852920532227, "The Spatial Resolution of the SPOT 1-5 Satellite is From 20 m to 1.5 m."]
[6.348187446594238, 4.223732948303223, "The Magnetometer Collections of the QuakeSat Satellite is Nearly 2000."]
[8.587427139282227, 10.242728233337402, "The Pixel Size of the Detector Imaging Device is 15 \u00b5m."]
[9.442512512207031, 5.530679225921631, "The Ground Location Accuracy of the AOCS Attitude and Orbit Control Subsystem is < 220 m."]
[5.637292385101318, 4.539651393890381, "The Type of the LCT Technology Demonstration Payload is Unknown."]
[7.061558246612549, 9.833677291870117, "The Center Wavelength of the Band No. 30 Spectral Band is 891.11 nm."]
[7.316061973571777, 10.178679466247559, "The On-Board Processing Time of the HyperScout 1 Hyperspectral Imager is About one minute."]
[7.156674385070801, 2.373933792114258, "The URL of the Next Generation Gravity Mission Elements of the Mass Change and Geoscience International Constellation Satellite Mission is URL:\u00a0https://www.mdpi.com/2072-4292/13/19/3935."]
[5.030472278594971, 4.450033664703369, "The Function of the Ground Software Data Processing is Search the optical counterparts of the GRB."]
[9.44140338897705, 9.375563621520996, "The Pupil Diameter for HR of the Instrument Hyperspectral Imager is 75.6 mm."]
[1.1622469425201416, 3.833773612976074, "The Project Name of the XI-IV Picosatellite is XI-IV."]
[9.488629341125488, -2.4977364540100098, "The Charge Range for Elements of the LEICA Particle Detector is 1 - 26."]
[10.145922660827637, 2.96878719329834, "The Altitude of the First Batch of Satellites Satellite is 550 km."]
[6.667356014251709, 0.8352156281471252, "The Launch Year of the RADARSAT-2 Satellite is 2007."]
[9.554405212402344, 4.115000247955322, "The Attitude Control of the CanX-4&5 Satellite is 1.0\u00ba."]
[8.009185791015625, -0.7190975546836853, "The Spacecraft of the SpaceX Launch Provider is Dragon."]
[7.979970455169678, 0.5466642379760742, "The Mission Start Date of the CryoSat Satellite is Unknown."]
[4.615578651428223, 3.9556803703308105, "The Conference Presentation Date of the Plug-and-play System Spacecraft Components System is Aug. 13-16, 2007."]
[6.370903015136719, 1.595472812652588, "The Operational Status of the Jason-3 Satellite is Operational as of August 2022."]
[7.035848617553711, 2.127507209777832, "The Test Completion Date of the Konnect satellite Satellite is 6 September 2019."]
[7.63788366317749, 6.570138454437256, "The Required Precision of the O3 Profile Satellite Instrument is 3%."]
[7.229166507720947, 4.2447099685668945, "The Sensor complement / remarks of the Meteor-2-1 Satellite is TV, IR, SM, RMK-2 (experimental)."]
[9.283820152282715, 8.996496200561523, "The Focal Length of the UVS Instrument Spectrometer Telescope is 250 mm."]
[10.280879020690918, 7.525027275085449, "The Energy Range of the Satellite Imaging Instrument is Above 10 keV."]
[9.823675155639648, 8.322010040283203, "The Support Component Material of the TX Telescope Telescope is Invar."]
[8.890868186950684, 9.30347728729248, "The FOV of the VIS Visible region of spectrum is \u00b144\u00ba (700 km swath)."]
[8.61817741394043, 10.517541885375977, "The Full Well Charge of the Image Sensor Imaging is 60,000 e-."]
[6.510945796966553, 8.290717124938965, "The URL of the Copernicus Imaging Microwave Radiometer (CIMR) Radiometer is https://agupubs.onlinelibrary.wiley.com/doi/epdf/10.1029/2021JC017610."]
[5.229897499084473, 3.1046359539031982, "The Bus of the NorSat-3 Satellite is NEMO bus from UTIAS/SFL."]
[7.72500467300415, 13.579825401306152, "The Resolution \u0394\u03bb (0.05\u00ba slit) of the SPIM1 Spectrometer is 0.5 nm."]
[8.163174629211426, 9.953116416931152, "The Center Wavelength of the Pan (WorldView-1) Imager is 650 nm."]
[10.971033096313477, 7.2049055099487305, "The Transverse Dimensions of the HXT-C X-ray Optics is 417 mm x 376 mm."]
[8.656538009643555, 6.642250061035156, "The | of the SFL Magnetorquer Magnetorquer is SFL magnetorquer."]
[6.0151238441467285, 9.549798965454102, "The LI Mass of the LI Instrument is 93 kg."]
[7.56191873550415, 7.936075210571289, "The Total Range of the CERES Instrument is 0.3 - 100 \u00b5m."]
[7.447866916656494, 4.335651397705078, "The Payload of the PROBA-II Satellite is PROBA-II Payload: A Belgian Mini Space Weather Observatory."]
[6.087505340576172, 9.72754955291748, "The Mass of the Telescope Optical Instrument is 1.7 kg."]
[6.605830192565918, 5.4410247802734375, "The Post-facto baseline reconstruction accuracy of the TDX/TSX Satellite is 1 mm."]
[5.032070159912109, 5.542952537536621, "The Antenna Size of the Reception Station Ground Station is 2.4 m."]
[9.488801002502441, -2.5067973136901855, "The Energy Range for Electrons of the LEICA Particle Detector is 0.4-30 MeV."]
[5.525550365447998, 10.184950828552246, "The Activation Time of the LIRIS Laser Infrared Imaging Sensors is Two and a half hours before docking."]
[5.012239456176758, 6.722278118133545, "The Gain of the C-band Antenna Antenna is More than 32.5dB."]
[8.083854675292969, 2.962817430496216, "The Mapping of the Magellan Spacecraft is 1990s."]
[8.536419868469238, 6.022669792175293, "The Potential Return of the Magnetic Pole Geomagnetic Feature is Canada."]
[9.885621070861816, 8.60453987121582, "The Pointing Method of the ASTRO-1 UV payload UV Telescopes is Shuttle maneuvers and slews of the IPS."]
[4.633411407470703, 7.235184669494629, "The Number of channels of the Millimeterwave receiver Receiver is 4096."]
[7.5457377433776855, 2.9600765705108643, "The Unknown of the Kompsat-2 Satellite is Unknown."]
[8.071331977844238, 11.128172874450684, "The Sensitivity of the Channel 3 Sensor is 0.3 K/pixel."]
[6.733612537384033, 0.7404840588569641, "The Industry Day Date of the SEOSat/Ingenio Satellite is Nov. 17, 2008."]
[7.819344520568848, 7.800621509552002, "The Components of the ORA Instrument Atmospheric Measurement Instrument is UV-visible module, infrared unit, electronics unit."]
[8.401862144470215, 7.383128643035889, "The Image Credit of the AIP (Advanced Ionospheric Probe) Probe is NCU."]
[7.787315368652344, 8.393625259399414, "The Manufacturer of the OAPs Optical System is Thorlabs Inc."]
[5.940912246704102, 3.8333494663238525, "The PLSO Location of the FOS Satellite is ESTEC."]
[8.867951393127441, 10.48068618774414, "The Resolution of the Comedia C328 Camera is VGA."]
[3.828878164291382, 5.188394069671631, "The Performance of the FACT Data Distribution System is Fine."]
[7.901407241821289, 4.6565260887146, "The Temporal Resolution of the GK-2A Satellite is Improved."]
[9.711196899414062, 7.799996376037598, "The Energy Range for Neutrons of the FREND Instrument is 0.4\u2013500 keV."]
[8.783653259277344, 2.12491512298584, "The URL of the New Horizons Spacecraft is https://www.nasa.gov/feature/nasa-s-new-horizons-reaches-a-rare-space-milestone."]
[8.836952209472656, 9.003358840942383, "The Entrance Slit of the UVS Instrument Spectrometer Telescope is 0.31 x 3.2 mm."]
[8.964438438415527, 2.453481674194336, "The Image Span of the Herschel Space Observatory is 2 x 2 degrees."]
[11.645462036132812, 6.181315898895264, "The Catalogue Release Date of the XMM-Newton Satellite is May 15, 2017."]
[10.179534912109375, 3.060507297515869, "The Orbit Altitude of the Light-1 Satellite is Approximately 400 km."]
[10.11225414276123, 1.5292588472366333, "The Period of the Yubileyniy-2/MiR Satellite is 115.8 minutes."]
[8.454590797424316, 7.758395195007324, "The Purpose of the MOIS Event Monitor Event Monitor is React to different types of events, Check the consistency of the anomaly, Request the start of the contingency recovery procedure."]
[8.995908737182617, 9.149622917175293, "The Iron Particle Speeds of the WISPR Optics Optical System is 0.5 - 8 km/s."]
[5.839062690734863, 2.8549458980560303, "The Manufacturer of the CesiumAstro Company is Full-scale manufacturer advancing airborne and next-generation aerospace platforms."]
[6.810564994812012, 3.816673755645752, "The Ownership of the Deimos-2 Earth Observation Satellite is Elecnor."]
[4.727085113525391, 6.112026214599609, "The Beacon Transmission Frequency of the ELFIN-B Satellite is 437.475 MHz."]
[7.136071681976318, 9.25742244720459, "The Ground Range x Product Length of the Stripmap Imaging Mode is 30 x 50 km (single pol.); 15 x 50 km (dual pol.)."]
[6.1242194175720215, 2.2372727394104004, "The Launch Site of the GFO Satellite is VAFB (Vandenberg Air Force Base), CA."]
[3.6114933490753174, 6.07098913192749, "The Nominal Operating Speed of the DCU-S(TC) module Communication Module is 64 kbit/s."]
[5.616400718688965, 0.3743290305137634, "The Start Date of the Cerro Pelado fire Wildfire is April 22."]
[4.602118015289307, 7.189402103424072, "The Spectral resolution of the Millimeterwave receiver Receiver is 44 kHz."]
[3.8289542198181152, 4.338191509246826, "The Processor of the C&DH Command and Data Handling is 2 x C8051F120 microcontroller."]
[7.686769962310791, 1.6387145519256592, "The Assembly Date of the MARFEQ Equipment is 10-19 Oct. 10-19, 2002."]
[7.669675827026367, 5.295553207397461, "The Observation of the OCO-3 Satellite is First dawn-to-dusk observations of how SIF varies over the course of a day."]
[6.950489521026611, 11.290498733520508, "The Wavelength FWHM of an unresolved line of the Spectrometer Instrument is 0.036 \u00b5m."]
[7.869482040405273, 9.967290878295898, "The VNIR Resolution of the PROBA-V Satellite is 5200 pixel."]
[8.244925498962402, 9.230547904968262, "The Roughness of the Ir Layer Optical Instrument Component is 1.3 nm rms."]
[6.555534839630127, 2.9481704235076904, "The Development Partners of the SOHLA-1 Satellite is JAXA, Tokyo University, Osaka University, Osaka Prefecture University."]
[8.438464164733887, 2.0090694427490234, "The Discovery Date of the Herschel Space Observatory is November 27, 2017."]
[5.6721625328063965, 3.3854820728302, "The Mission Objective of the LLITED CubeSat Satellite is Provide ionosphere and thermosphere measurements."]
[1.276329517364502, 4.142269134521484, "The Batteries Capacity of the EROS-A Satellite is 14 Ah."]
[10.957555770874023, 3.3758790493011475, "The Comet Distance from Earth of the TESS Satellite is About 29 million miles (48 million km)."]
[8.598769187927246, 1.6765600442886353, "The News Release Date of the Spitzer Space Telescope Space Telescope is 19 December 2019."]
[3.844546318054199, 0.30193060636520386, "The URL of the Gravity Recovery and Interior Laboratory (GRAIL) Satellite is http://www.lpi.usra.edu/meetings/lpsc2013/pdf/1777.pdf."]
[9.996404647827148, 9.94339370727539, "The Manufacturer of the Iris camera Camera is UrtheCast Corp.."]
[5.703803062438965, 2.7917392253875732, "The Manufacturer of the Composite Dispenser Dispenser is RUAG Space in Sweden."]
[6.804624080657959, 2.126164436340332, "The Rainfall Amount of the IMERG Rainfall Estimation System is Up to 10 cm (4 inches)."]
[8.69955825805664, 4.542669773101807, "The Latitude Range of the PRISMA Payload Satellite Payload is 70\u00b0S - 70\u00b0N."]
[7.14877986907959, 0.929776668548584, "The Design Completion Date of the Development Status Satellite is June 16, 2016."]
[5.638213157653809, 5.13811731338501, "The Global Coverage of the ILRS Tracking Service is Yes."]
[4.738928318023682, 2.625427484512329, "The System Racks of the PM Satellite Component is 11."]
[4.1848297119140625, 6.346590995788574, "The Protocol of the RF Communications Subsystem Communications Subsystem is Strandatoga."]
[8.05273151397705, 7.70508337020874, "The Frequency Response of the SCM Sensor is LF/MF range."]
[10.215333938598633, 9.4744291305542, "The Spectral Regions of the IRIS Satellite is FUV (Far Ultraviolet) and NUV (Near Ultraviolet)."]
[3.931326389312744, 4.42589807510376, "The Risk Mitigation of the On-Board Computer (OBC) Computer System is In Progress."]
[8.37848949432373, 3.818836212158203, "The Attitude Range of the CHEOPS Satellite is Not provided."]
[8.599818229675293, 5.544223785400391, "The Pointing Accuracy of the IPS Pointing System is Within 1.2 arcseconds."]
[10.727498054504395, 10.273003578186035, "The Gain temperature coefficient of the PHA Detector is <50 ppm/\u00baC."]
[6.947813034057617, 11.30044174194336, "The Wavelength FWHM of an unresolved line of the Spectrometer Instrument is 0.098 \u00b5m."]
[11.729219436645508, 5.335459232330322, "The Gamma-Ray Measurement of the GRB 031203 Gamma-Ray Burst is About one thousand times less than expected."]
[6.494809150695801, 1.562511920928955, "The Program Timeframe of the Jason-CS Satellite Mission is 2015-2020."]
[7.793810844421387, -0.49034586548805237, "The Backup Astronaut of the SpaceX CRS-17 Mission is Nick Hague."]
[6.8502912521362305, 4.892526626586914, "The Productivity Decline of the Cropland Land is 15 percent in 2019 from 2018 levels."]
[5.48803186416626, 5.392562389373779, "The Frequency Band of the ICEYE Constellation Satellite Constellation is X-band."]
[8.450129508972168, 7.105146884918213, "The Magnetic Field Measurement Frequency Range of the IOF Plasma Wave Instrumentation is 40 Hz to 1.78 kHz."]
[7.649198055267334, 9.306230545043945, "The Spectral Bands of the ECOSTRESS Instrument is Five."]
[9.377898216247559, 1.1435035467147827, "The Length of Observational Data Set of the Aeolus Satellite is 3 years."]
[8.114171981811523, 9.84534740447998, "The Imager Type of the Satellite Vu Satellite is MWIR."]
[6.985398769378662, 7.678923606872559, "The Cloud Area Coverage of the HARP Imaging Polarimeter is < 4 km x 4 km."]
[8.54910659790039, 2.3543589115142822, "The Principal Investigator of the Juno Space Probe is Scott Bolton."]
[3.576963186264038, 6.62893009185791, "The Data Rate of the S-band transmitter Transmitter is Up to 144 kbit/s."]
[7.633325099945068, 7.670804023742676, "The Objective of the SOVA Radiometer is Measurement of the solar constant, its variability and its spectral distribution."]
[11.644332885742188, 2.974414825439453, "The Orbit Inclination of the HORYU-4 Nanosatellite is 31\u00ba."]
[10.362176895141602, 2.8213999271392822, "The Orbital Altitude of the International Space Station Space Station is Relatively low over our planet."]
[8.380681991577148, 8.654081344604492, "The Project Funding of the SCIAMACHY Spectrometer is DLR/NIVR."]
[7.123795032501221, 0.8457502126693726, "The Launch Date of the OPAL Satellite is Late 2016."]
[8.841200828552246, 10.540006637573242, "The High-speed raw image data processing of the Frame Grabber Computational Capacity is Sufficient computational capacity to receive and store the high-speed raw image data."]
[8.160354614257812, 1.0621589422225952, "The Image Capture Date of the Payload Camera Instrument is July 29, 2018."]
[5.917482852935791, 3.638535261154175, "The Ground Station of the KySat-1 Satellite is Space Science Center at Morehead State University (MSU)."]
[7.201223373413086, 4.536075592041016, "The Mission Goals of the Tandem-L Satellite is 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."]
[8.144218444824219, 0.31965357065200806, "The End Date of the ISS-RapidScat Earth Science Mission is Nov. 28, 2016."]
[4.322554588317871, 4.313823699951172, "The Operation of the Command and Data Handling Subsystem Subsystem is Autonomously schedules GPS acquisitions and uplink/downlink operations."]
[7.561624050140381, 7.249014377593994, "The Principal Investigators of the Rhodium Synthetic Cryptobiology Research Project is Drs. Heath Mills and Aindrila Mukhopadhay."]
[4.448549747467041, 5.720854759216309, "The Ka-band System of the STPSat-6 Satellite is Ability to be reconfigured on orbit."]
[5.4401021003723145, 5.538084030151367, "The Bandwidth of the Capella X-SAR Constellation Satellite Constellation is 500 - 700 MHz."]
[9.452654838562012, 10.55437183380127, "The Frame Coverage of the Iris Video Camera Camera is Approximately 3.8 km x 2.2 km (UHD); Approximately 1.9 km x 1.1 km (HD)."]
[9.46551513671875, 0.22719186544418335, "The Minimum Success Criteria of the SMDC-One Satellite is 6 months."]
[9.260777473449707, 9.213033676147461, "The Fiber Optic Cable Diameter of the Detector Box Instrument is 3 mm."]
[11.883645057678223, 2.3870997428894043, "The Sampling Latitude Range of the OSIRIS-REx Spacecraft is 85\u00ba North to 85\u00ba South."]
[9.026442527770996, 10.827981948852539, "The Swath of the LISS-4 Camera is 70 km."]
[8.952993392944336, 5.0963358879089355, "The Attitude Stabilization Time of the GF-2 spacecraft Satellite is Within 150 s."]
[8.489675521850586, 5.956436634063721, "The Position of the Magnetic Pole Geomagnetic Feature is Shifting towards Siberia."]
[6.248538970947266, 2.159627676010132, "The Launch Vehicle of the SEOSAT-Ingenio Satellite is Vega."]
[11.175013542175293, 6.7523345947265625, "The Optics URL of the Imaging X-ray Polarimetry Explorer Satellite is https://doi.org/10.1117/12.2275502."]
[10.935286521911621, 5.790165424346924, "The Strongest X-class flare date of the SOHO Satellite is October-November 2003."]
[9.320762634277344, 5.336418628692627, "The Function of the Reaction Wheels Satellite Component is Desaturate."]
[10.151976585388184, 3.0570740699768066, "The Altitude of the EFT-1 Spacecraft is Approximately 5800 km."]
[4.076898097991943, 5.692836761474609, "The Communication Rate of the TSUBAME Satellite is More than 10 kbit/s."]
[7.158816337585449, 4.358695983886719, "The Objective of the Tatiana-2 Satellite is Measurement of TLEs (Transient Luminous Events) in Earth's atmosphere."]
[4.281281471252441, 5.666586399078369, "The Communication Bandwidth of the Pl\u00e9iades Neo Satellite Constellation is Up to 1.8 Gbit/s."]
[9.371554374694824, 7.440868854522705, "The Light Intensity of the Faraday Cup Sensor is Roughly 10 kilowatts."]
[5.630431652069092, 6.449027061462402, "The Dimensions of the SAR Antenna Antenna is 3.3 m x 2.7 m."]
[6.107830047607422, 9.500024795532227, "The Quantity of the GARI-1 Instrument is Two identical GAGG instruments."]
[8.463326454162598, 6.750194549560547, "The Other Missions of the NewMag Magnetometer is ISEE-1/2 (launch Oct. 2, 1977), AMPTE-UKS (launch Aug. 16, 1984), POLAR (launch Feb. 24, 1996), and Galileo (launch 1989)."]
[8.537988662719727, 8.743085861206055, "The Function of the Rowland circle Spectrograph Component is Determines the locations of slit, grating, and detector in a concave grating spectrograph."]
[8.782330513000488, 8.488615989685059, "The Field of View of the ISIS Instrument is Within 10\u00ba of the Sun-Probe line."]
[7.982306003570557, 8.76679515838623, "The Spectral Range of the Limb Sensor Sensor is 290 to 1000 nm."]
[10.034943580627441, 1.5464366674423218, "The Timing of the Satnav Signals Signal is Precisely timed to a few billionths of a second."]
[9.46331787109375, 0.5235552787780762, "The Age of the Cosmos 2251 Satellite is Older."]
[6.94140625, -0.017604781314730644, "The Data Collection Status of the STP-H7 and H8 Scientific Payloads is Ongoing."]
[8.116300582885742, 6.363868713378906, "The Best Measurement Position of the IMAP Satellite is He 58.4 glow from the crosswind position."]
[7.71741247177124, 7.247875690460205, "The Gases Measured of the TEMPO Instrument is Ozone, nitrogen dioxide and formaldehyde."]
[7.176243305206299, 1.405657172203064, "The Conference Presentation Date of the Eu:CROPIS Satellite is May 16-20, 2016."]
[5.662856578826904, 4.490562915802002, "The Type of the AEEF Technology Demonstration Payload is Unknown."]
[11.426262855529785, 6.033425331115723, "The Resumption of Science Observations Date of the Chandra X-ray Observatory X-ray Observatory is Sept. 12."]
[10.089250564575195, -0.8420681357383728, "The Size of the PROBA-V Microsatellite is 1 cubic meter."]
[7.178441047668457, 9.190495491027832, "The Ground Range x Product Length of the ScanSAR Imaging Mode is 100 x 150 km."]
[3.219691276550293, 6.087029457092285, "The Type of the APL\u2019s Frontier radio Radio is Software-defined."]
[7.767878532409668, 0.3181512951850891, "The Build Date of the Maspalomas MEOLUT Ground Station is Oct. 8, 2013."]
[11.357305526733398, 1.3753705024719238, "The 14-Day Lunar Night of the Yutu Lunar Rover is Feb. 13, 2014."]
[10.149578094482422, 9.503997802734375, "The Data Rate for Spectra of the IRIS Observatory is Every 1\u20132 s."]
[10.459175109863281, 7.550775051116943, "The Primary Structure Material of the KOMPSAT-6 Satellite is CFRP (Carbon Fiber Reinforced Polymer)."]
[10.399782180786133, 7.214254856109619, "The Function of the TEMBOTM EMC Material is Allows for strain energy to be \"frozen\" into an EMC structure by cooling the deformed laminate below the critical temperature."]
[7.012223720550537, 0.4275101125240326, "The Launch Date of the PhoneSat-1 and -2 Satellite is 21 April 2013."]
[5.881505489349365, 6.904284477233887, "The Swath Width of the SIR-C Phased Array is 40 to 90 km for mapping mode (ScanSAR) images."]
[13.098057746887207, 4.0543437004089355, "The Mission Type of the Gaia Satellite is Astrometric Survey."]
[1.294326663017273, 4.155155181884766, "The Eclipse Capability of the Satellite Satellite is 100 % payload operation; battery max. 75% EOL."]
[8.767168045043945, 0.17148557305335999, "The Operation Period of the Skylab-1 Space Station is Up to 84 days."]
[5.969037055969238, 3.7200164794921875, "The Control Room of the Aeolus Satellite is Earth Explorer control room at ESOC."]
[7.517416000366211, 2.272775173187256, "The Utilization of the ICI-5 Radiometer is Cloud ice effective radius."]
[8.012682914733887, 7.54473876953125, "The Purpose of the ASIM Instrument is Measures electric events in Earth\u2019s upper atmosphere with cameras, photometers and X- and gamma-ray detectors."]
[5.721710681915283, 3.952159881591797, "The Components of the Robotic Servicing Platform Satellite Servicing Technology is Camera, robotic arm, fuel reserve, GN&C rendezvous and proximity operations capabilities."]
[6.98860502243042, -0.06426332145929337, "The End of Life Date of the ALL-STAR Satellite is 26 May 2014."]
[7.0641045570373535, 9.766267776489258, "The Spectral Range (\u00b5m) of the Band 9 Spectral Band is 0.53 - 0.58."]
[6.197067737579346, 6.553908824920654, "The Features of the Poseidon-4 Altimeter is Higher performance than the previous generation, new \"interleaved\" SAR operating mode, new architecture improving the role of the digital functions."]
[8.958985328674316, 1.873082160949707, "The Arrival in Mercury orbit of the BepiColombo Spacecraft is 2025."]
[9.14730167388916, 8.299114227294922, "The L1 Detectors Thickness of the HIT Sensor is 1000 \u00b5m."]
[4.30564022064209, 6.670416355133057, "The Frequency of the Receiver Communication Device is 435 MHz."]
[8.52330493927002, 7.3990936279296875, "The Unknown of the Thermal Plasma Measurement Unit Measurement Unit is Unknown."]
[5.426959037780762, 5.663883686065674, "The Tracking of the Topstar GPS receiver GPS Receiver is Dual-frequency."]
[2.355935573577881, 5.7628173828125, "The PRF of the HPA High Power Amplifier is 3050 Hz."]
[8.502219200134277, 7.906187534332275, "The Number of Physical Modules of the MIRO Instrument is 4."]
[7.647162914276123, 3.99945330619812, "The Meteoritic Origin of NLCs of the AIM spacecraft Satellite is About 3% of each ice crystal."]
[9.055392265319824, 10.786406517028809, "The Steering Capability of the LISS-4 Camera is \u00b126\u00ba in the cross-track direction."]
[6.12973165512085, 3.861992597579956, "The Service Provision of the MetOp program Satellite Program is Continuous broadcast of its meteorological data to the worldwide user community."]
[7.849775314331055, 5.522262096405029, "The Orbit Determination Accuracy of the AutoNav Autonomous Navigation System is Later refinements improved these values substantially."]
[7.269623279571533, 5.733312606811523, "The Data of the Aeolus Satellite is Most of the dust was 3\u20146 km above the ground."]
[9.812749862670898, 4.854702949523926, "The Payload Spin of the Bloostar Launch Vehicle is Up to 10 rpm."]
[8.074034690856934, 8.882733345031738, "The Wavelengths of the Telescope Optical Instrument is Fe XIV 530.3 nm; He I 587.6 nm."]
[5.402613639831543, 2.7317726612091064, "The Affiliation of the OSIRIS CubeSat is PSU (Penn State University), University Park, PA, USA."]
[13.657114028930664, 1.6123100519180298, "The Launch Vehicle of the Aeolus Spacecraft is Vega vehicle."]
[6.557896137237549, 7.8124213218688965, "The Calibration Time of the LD Output Laser Diode is Unknown."]
[4.106319904327393, 4.439799785614014, "The Manufacturer of the MCU Microcontroller Unit is Texas Instruments."]
[9.21416187286377, 3.20408296585083, "The Orbit Type of the ICEYE-X14 and ICEYE-X16 Satellites is Sun-synchronous."]
[9.092432975769043, 5.075606822967529, "The Configuration of the MTG Satellite System is Twin configuration of 3-axis stabilized satellites."]
[8.181714057922363, 6.8398871421813965, "The Target of the External Calibration Calibration is Deep space, the moon, the sun, or known ground targets."]
[4.519109725952148, 4.035848140716553, "The Self-identification of the SPA Components Components is Provide information about their functions and use to the system."]
[6.622498035430908, 10.653873443603516, "The Estimated SNR of the Band 5 Spectral Band is 416.39 \u00b1 129.03."]
[7.099781513214111, 2.674377918243408, "The Orbit Information of the SWOT Satellite is http://www.aviso.altimetry.fr/es/misiones/future-missions/swot/orbit.html."]
[6.738545894622803, 7.692071914672852, "The Manufacturer of the AMSU-A Instrument is Aerojet, a subsidiary of GenCorp."]
[9.175952911376953, 10.23741340637207, "The Number of Images of the POLO data set Image Dataset is Over 1000."]
[6.78195858001709, 2.0060715675354004, "The Memorandum of Understanding Date of the Global Precipitation Measurement (GPM) Satellite is Aug. 3, 2009."]
[9.06588077545166, 7.709151268005371, "The Mass Determination Method of the EIS Sensor is Measuring velocity and total energy."]
[5.404239654541016, 4.204796314239502, "The Location of the DMMC Downlink Messages Management Center is Toulouse."]
[7.191806316375732, 8.867895126342773, "The Cloud Deck Resolution of the CIPS Instrument is 2 km."]
[8.873306274414062, 7.722874164581299, "The Ion Analysis of the Time-of-flight/position sensing section Component is Mass, energy, and angle."]
[7.8492512702941895, 3.0129446983337402, "The Eclipse Depth-of-Discharge of the Power Subsystem Satellite System is Only slightly higher than the LOI (Lunar Orbit Insertion) depth-of-discharge."]
[1.1907395124435425, 3.816835641860962, "The Control System of the CUTE-1.7 Picosatellite is PDA-Controlled."]
[9.530341148376465, 4.319580554962158, "The Height of the Large Space Simulator (LSS) Vacuum Chamber is 15 m."]
[10.645697593688965, 3.360258102416992, "The Closest Approach Distance of the Rosetta Satellite is 3162 km."]
[7.354117393493652, 6.845475673675537, "The Final Results of the SPADUS Instrument is Planetary Space Science, Vol. 53, 2005, pp. 903-923."]
[9.081799507141113, 5.979745388031006, "The Star Sensors of the R3 Spacecraft Satellite is Two 90\u00b0 offset star sensors."]
[9.047905921936035, 10.521185874938965, "The Resolution of the EIC Camera is 250 m x 250 m."]
[5.123315334320068, 5.993920803070068, "The Quantity of the Coils Antenna is 2."]
[6.602192401885986, 10.68272590637207, "The Nominal SNR of the Band 2 Spectral Band is 1090."]
[10.796923637390137, 3.4238812923431396, "The Distance from the Sun at First Perihelion of the Solar Orbiter Satellite is Around 77 million kilometers."]
[7.051351547241211, 4.894042491912842, "The Mission of the TANGO satellite Satellite is Monitoring greenhouse gas emissions."]
[4.9640021324157715, -3.1033079624176025, "The Affiliation of the Junichi Kurihara Author is Hokkaido University."]
[11.747757911682129, 4.552669525146484, "The Length of the Hyades Tidal Tails Tidal Tails is Thousands of light years."]
[7.619913101196289, 9.774118423461914, "The Energy of the VNIR Band is 1.17 eV."]
[11.354765892028809, 3.944016218185425, "The Orbital Period of the Kepler-438b Exoplanet is 35.2 days."]
[9.739641189575195, 10.087384223937988, "The Funding Source of the MOMS Optical Camera is German Ministry for Research and Technology."]
[7.089923858642578, 3.9006786346435547, "The Operation of the DMC Constellation Satellite Constellation is Independently owned and operated by one nation or organization."]
[7.670133113861084, 0.36816099286079407, "The Launch Date of the Meteor-1/Meteor-2/Meteor-Priroda Series Satellite Mission is 01 Jan 1993."]
[6.2955641746521, 2.7918760776519775, "The Roles of the Hayley Arceneaux, Sian Proctor and Chris Sembroski Crew Members is Not specified."]
[8.365077018737793, 10.052926063537598, "The Size of the Detector Array Assembly Detector Array is 5 x 6000 (30,000 pixels or samples in cross-track)."]
[3.863091468811035, 2.284970283508301, "The Sensor Volume of the R3 spacecraft CubeSat is Less than 1.5U."]
[6.001511096954346, 9.605509757995605, "The Mass of the SDST Device is 3 kg."]
[5.889209270477295, 3.7897632122039795, "The Operator of the Bartolomeo External Payload Hosting Facility is Airbus DS."]
[9.268148422241211, 9.334187507629395, "The Focal Ratio of the Lens Optical Instrument is f/1.4."]
[6.321310997009277, 1.0549323558807373, "The Launch Date of the COSMO-SkyMed-4 Satellite is Nov. 6, 2010 (UTC)."]
[6.809832572937012, 1.2084131240844727, "The Decommission Date of the GIOVE-A Satellite is 24 November 2021."]
[5.961630821228027, -0.2421417385339737, "The Conference Date of the Oculus-ASR Satellite is Sept. 11-14, 2012."]
[10.995237350463867, 5.066080570220947, "The Relative Acceleration of the LISA Pathfinder Spacecraft is Lower than ten millionths of a billionth of Earth's gravitational acceleration."]
[4.245824813842773, 4.837550640106201, "The Standard of the TM Synchronization and Channel Coding Data System is CCSDS 131.0-B-2."]
[7.198691368103027, 0.8786441087722778, "The Delivery Date to ISS of the OPALS Optical PAyload for Lasercomm Science is April 20, 2014."]
[11.735809326171875, 3.269977569580078, "The Forward of the S-193 Ground Coverage is 48\u00ba."]
[5.647366523742676, 6.414736270904541, "The Dimensions of the SAR Antenna Antenna is 2.2 m x 1.5 m panels, measuring 2.2 m x 11.9 m in total."]
[7.518700122833252, -0.5397782325744629, "The Arrival Date of the Cygnus Cargo Spacecraft is 14 Nov. 2017."]
[5.648375034332275, 3.5281598567962646, "The Objectives of the UWE-2 Satellite is Continue the communication protocol experiments and to include technology tests related to attitude determination."]
[1.770060658454895, 4.133502006530762, "The Efficiency of the Solar Panels Power Source is 28%."]
[4.480980396270752, 4.172377109527588, "The Bus of the Payload Instruments Satellite Components is Redundant CAN (Control Area Network) bus."]
[10.651477813720703, -1.6709253787994385, "The Cargo Mass of the HTV-3 H-II Transfer Vehicle is About 4600 kg."]
[13.176857948303223, 4.010797500610352, "The Launch Date of the Gaia Satellite is 2013."]
[9.1964750289917, 10.128914833068848, "The Image Quantity of the LROC Camera is Over 3,000."]
[10.35019302368164, 5.2582478523254395, "The Maximum Operating Pressure of the Xenon Gas Tank Propellant Storage is 150 bar."]
[7.732430458068848, 1.065650224685669, "The Launch Date of the Apollo 15, 16, 17 Missions is 1960s."]
[8.371748924255371, 1.0285553932189941, "The Event Date of the LROC Camera System is October 13, 2014."]
[7.297929286956787, 5.390625, "The Purpose of the CLARREO Satellite is Accurately measuring and attributing climate change."]
[9.687820434570312, 1.5811848640441895, "The Repeat Cycle of the ALOS-3 Satellite is 35 days."]
[8.847563743591309, 4.415041923522949, "The Target Size of the PRISMA Payload Satellite Payload is 30 km x 30 km."]
[5.157519340515137, 5.465420246124268, "The Frequency Bands of the GovSat-1 Communication Satellite is X-band and Military Ka-band."]
[4.111717224121094, 6.257192611694336, "The Protocol of the RF Communications Communication System is AX.25."]
[3.6696701049804688, 6.542267799377441, "The Data Transmission Rate of the RF Communications Transmitter is 9.6 to 500 kbit/s in Ku-band."]
[3.7955403327941895, 4.325407028198242, "The Branch of the Level-1 Processor v700 Data Processor is ALL-LICEF."]
[10.353642463684082, 5.622416019439697, "The Tether Break of the AeroCube-3 Satellite is The tether to the upper stage broke within hours."]
[5.935932159423828, 3.8759143352508545, "The Payload Sites of the Bartolomeo research platform Research Platform is 13 (12 active, 1 passive)."]
[9.559968948364258, 7.343445777893066, "The Golf Course Temperature of the ECOSTRESS Instrument is 23 F (13 C) cooler."]
[9.219629287719727, -0.605247437953949, "The Development Timeline of the Dellingr Nanosatellite is February 2014 to February 2015."]
[7.8075456619262695, 8.957974433898926, "The Spectral Resolution of the UV-1 Spectrometer is 0.42 nm."]
[5.77481746673584, 2.2368459701538086, "The Capacity Reservation of the Eutelsat Quantum Satellite is Majority."]
[5.2691731452941895, 3.0674068927764893, "The Mission Objectives of the BeaverCube CubeSat is Demonstrate the use of a CubeSat platform to gather important ocean and atmospheric measurements, support teaching and outreach."]
[2.016784906387329, 7.847965240478516, "The Solar Wind Speed and Beta of the ACE Satellite is ~31% lower on average from 2009 through the day 79 of 2013."]
[4.18895959854126, 6.771313190460205, "The Channel Bandwidth of the Channel Communication System is 100 MHz."]
[9.957225799560547, 1.4139882326126099, "The Time to Point to the Sun and Balance Electrical Power of the TSUBAME Satellite is Within 33873 seconds after rocket separation."]
[7.505075931549072, 1.0343444347381592, "The Imaging Date of the ALOS satellite Satellite is September 2013."]
[7.465807914733887, 5.574126720428467, "The Bias Error of the Aeolus Satellite is 0.4 m/s."]
[6.6868462562561035, 9.125328063964844, "The Size of the CEASE-1 Instrument is 10 cm x 10 cm x 8.2 cm."]
[4.600026607513428, 6.624039173126221, "The Amplifier Gain of the Ka-band Signal is 36 dB."]
[9.486908912658691, 2.878591299057007, "The Impact Punctures of the Eureca Satellite is 71 in the outer layer of the thermal blankets."]
[6.563507080078125, 8.027830123901367, "The Applications of the MiniRad Microwave Radiometer is Improved weather forecasting, better crop yields, safer and more efficient route planning for aviation and shipping."]
[4.6681389808654785, 6.573720932006836, "The Gain Setting Ability of the Intermediate Frequency Amplifier Signal Processing Component is Yes."]
[8.255995750427246, 8.334510803222656, "The Components of the FWS Band and Polarization State Selector is OPC (Optical Path Compensator), BP (Band Pass) filter, POL (Linear Polarizer) or optical path compensator, ND (Neutral Density) filter."]
[7.006038665771484, 1.2786744832992554, "The Conference Date of the EarthCARE Satellite is Oct. 4-8, 2010."]
[11.122568130493164, 5.136517524719238, "The Start of Science Mission of the LISA Pathfinder Satellite is 1 March 2016."]
[10.081504821777344, 3.7112693786621094, "The Enrichment of the Moon Celestial Body is Heat-producing elements."]
[6.233036518096924, 2.5836703777313232, "The Coverage of the EUTELSAT KONNECT Satellite is Up to 40 countries across Africa and 15 over Europe."]
[9.739956855773926, 1.4914790391921997, "The Target Availability of the SPARCS Satellite is ~3 months for targets in the ecliptic plane."]
[6.886799335479736, 0.2698504328727722, "The Launch Date of the AstroSat Astronomy Satellite is 28 September 2015."]
[6.577446460723877, 3.807534694671631, "The Data Enhancement Technique of the Spire Satellite Constellation is Cutting-edge machine learning techniques."]
[7.655673980712891, 3.5216197967529297, "The Science Objectives of the IMAP Satellite is LISM (Local Inter-Stellar Medium) Properties and Composition."]
[10.604079246520996, 8.497363090515137, "The Spatial Resolution of the COR1 Coronagraph1 imager is \u2264 16.0 arcsec."]
[6.403382778167725, 3.0843498706817627, "The Agency of the IMAGE Satellite is NASA."]
[5.084463596343994, 6.297402381896973, "The Antenna Design of the Radio Communication Device is Omnidirectional/medium gain."]
[6.3054704666137695, 3.990321636199951, "The Operation of the THEIA Satellite is Data Processing."]
[6.824862480163574, 1.3370360136032104, "The Coast Phase Dates of the THEMIS Constellation Satellite Constellation is July 1 to Aug. 31, 2007."]
[9.403382301330566, 4.8331780433654785, "The Slew Rate of the Spacecraft Satellite is 0.25 to 1.0\u00ba/s."]
[10.063028335571289, 1.5142396688461304, "The Period of the SPOT-1, -2 and -3 Satellites is 101 minutes."]
[5.9851908683776855, 9.597124099731445, "The Mass of the CEASE-1 Instrument is 1 kg."]
[3.2387473583221436, 5.882015228271484, "The Data Retrieval Time of the SafetyNet Ground Data Receptor Network is Less than 28 minutes."]
[8.825652122497559, 9.050735473632812, "The length of the toroidal holographic diffraction grating grating is 50 mm."]
[11.57379150390625, 6.183669567108154, "The X-ray Nova Detection Date of the ISS, Swift Instruments is Oct. 25, 2010."]
[9.365832328796387, 0.8088508248329163, "The Operational Duration of the Meteosat-7 Satellite is 17 years."]
[9.56197452545166, 0.4810807704925537, "The Design Life of the G\u00f6kt\u00fcrk-1A Satellite is Seven years."]
[6.104234218597412, 8.042478561401367, "The Frequency Range of the MTVZA-GY Radiometer is 52-57, 91 and 183 GHz."]
[7.819363594055176, 0.585407018661499, "The Bankruptcy Filing Date of the UrtheCast Company is October 24, 2020."]
[4.895563125610352, 1.9191334247589111, "The Number of Satellites of the SARah Satellite Constellation is 3."]
[8.383638381958008, 9.471067428588867, "The Pan Camera of the Payload Satellite Subsystem is 0.45~0.89 \u00b5m."]
[5.5552544593811035, 4.086295127868652, "The Operation Location of the Ground Segment Satellite System is CONAE Control Center at Cordoba, Argentina."]
[10.194064140319824, 3.1455636024475098, "The Orbit Altitude of the TecSAR SAR is 450 km x 580 km."]
[6.896664142608643, 0.9801923036575317, "The Conference Date of the STRaND-1 Satellite is Oct. 3-7, 2011."]
[8.5172758102417, 3.7960662841796875, "The Observation Coverage of the GEO Satellite Satellite is About 40% of the Earth's surface."]
[7.015275955200195, 5.940287113189697, "The Wind Speeds of the Hurricane Models Weather Model is Up to category 5 strength."]
[9.359917640686035, 10.232083320617676, "The Field of View of the VIS Camera Camera is 30\u00ba x 19\u00ba."]
[9.140457153320312, 9.135502815246582, "The Pixel Size of the SXI Spacecraft is 5 arcsec x 5 arcsec."]
[5.5761189460754395, 3.6247339248657227, "The Payload Systems of the SPOT-4 Spacecraft is PASTEC, POAM-II."]
[5.8387370109558105, 8.142167091369629, "The Frequency (GHz) of the ICI-11 Radiometer is 664\u00b14.2."]
[6.992989540100098, 1.5709723234176636, "The Conference Presentation Date of the Earth Observation System of the Republic of Kazakhstan Satellite System is Sept. 23-27, 2013."]
[7.950471878051758, 5.327759742736816, "The Orbit Position Accuracy of the GPS Receiver Navigation System is 50 m (1\u03c3)."]
[7.131710052490234, 2.255693197250366, "The URL of the Shuttle Radar Topography Mission Satellite Mission is http://www2.jpl.nasa.gov/srtm/srtmBibliography.html."]
[9.20948600769043, 3.2058911323547363, "The Orbit Type of the ICEYE-X10 Satellite is Sun-synchronous."]
[7.547979354858398, 8.8493070602417, "The Nominal Vertical Resolution of the Detector Instrument is 1 km."]
[6.397702693939209, 9.204267501831055, "The Board Quantity of the MuREM Radiation Monitor is 3."]
[10.287445068359375, 5.135611057281494, "The Pressure of the Gas Tank Propulsion System is 1.78 bar."]
[11.833468437194824, 1.059321641921997, "The Landing Site of the Chang'e-4 Lunar Spacecraft is Von Karman crater in the South-Pole-Aitken (SPA) basin."]
[8.123394012451172, 4.85319185256958, "The Geolocation Method of the NigeriaSat-2 Satellite is Precise measurement of the position and attitude of the payload."]
[5.968710899353027, 5.016374588012695, "The Processing Levels of the OSIRIS Data Processing is 1 and 2."]
[4.129044055938721, 7.211313724517822, "The Mass of the TRSR GPS Receiver is 4 kg."]
[4.356480598449707, 5.177388668060303, "The Network Redundancy of the MTG satellites Satellite is Full cross-strapping redundancy with SpW-10X routers."]
[5.920793056488037, 0.6216111183166504, "The Last Data Received of the MaSat-1 CubeSat is January 9, 2015."]
[7.024494647979736, 5.833840370178223, "The Sensing Ability of the TEMPEST Sensor is Atmospheric moisture and its vertical distribution."]
[7.195235729217529, 9.278275489807129, "The Swath Width of the Scanning geometry Instrument is 2800 km."]
[8.44074821472168, 9.238892555236816, "The Tuned Wavelengths of the FUV Instrument Spectrometer is 135.6 and 155.0 nm."]
[2.1419777870178223, 4.612019062042236, "The Payload Power of the SmallGEO Satellite Platform is Up to 3 kW."]
[8.345980644226074, 10.996148109436035, "The Data Quantization of the Eastman Kodak KLI14403 linear CCD sensor Sensor is 8 bit or 10 bit."]
[11.214496612548828, 0.9879817366600037, "The Launch Date of the Tianwen-1 Spacecraft is July 23, 2020."]
[5.897021770477295, 6.39989709854126, "The BAQ Data Compression of the CSG-SAR Synthetic Aperture Radar is 10:6, 10:5, 10:4, 10:3, 10:2, 10:1, 10:10."]
[7.101668357849121, 0.7265474200248718, "The Fabrication Project Date of the MIMOSA Satellite is April 2-6, 2001."]
[7.030945301055908, 9.840506553649902, "The Wavelength Range of the Band 5 Spectral Band is 1628-1654 nm."]
[12.051573753356934, 3.335740327835083, "The Orbit Inclination of the Starlink Group 4-14 Satellite Group is 53.2\u00ba."]
[2.0157110691070557, 5.044872283935547, "The Function of the PC5 Power Supply is 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."]
[3.475661039352417, 4.637501239776611, "The Memory Type of the Second FPGA FPGA is SRAM."]
[4.711123466491699, 2.071276903152466, "The Mass of the Flock-4v Satellite is Undisclosed."]
[5.449429988861084, 4.1220221519470215, "The Interaction of the Mission Planning System is Uptakes CTDA requests into its planning cycle."]
[6.0234856605529785, 2.7843170166015625, "The Collaborating Institution of the MAST Satellite is Stanford University's SSDL."]
[10.269488334655762, 8.693052291870117, "The CCD Detector Assembly of the EUVI Extreme Ultraviolet Imager is Backside-illuminated, backside-thinned and pacified array of size 2k x 2k with an EUV quantum efficiency >70%."]
[8.432055473327637, 0.8239701390266418, "The Observation Frequency of the Megha-Tropiques Satellite is A minimum of 4 per day over the 22\u00b0S-22\u00b0N band."]
[6.86768913269043, 3.119001626968384, "The Mission Status of the Beijing-1 Satellite is Operating nominally in 2012."]
[9.45683479309082, -0.6291430592536926, "The Partner of the Weather Observation Satellite Satellite is NanoAvionics."]
[7.4806036949157715, 2.0086095333099365, "The Event of the Glasgow Glacier Memorial Glacier is COP26 being held in Glasgow, Scotland, UK in October 2021."]
[7.981814861297607, -0.6835079193115234, "The Launch Date of the SpaceX Dragon Spacecraft is October 8, 2012."]
[5.410223960876465, 0.2863854467868805, "The Firefighters of the Calf Canyon-Hermits Peak fire Fire is 1,800."]
[7.01189661026001, 4.506546974182129, "The Instrument Type of the ST5 Satellite is Magnetic field, Atmospheric chemistry, Data collection."]
[5.824719429016113, 3.0992283821105957, "The Structure Designer of the Biomass Satellite is OHB in Italy."]
[4.958286762237549, -3.0967397689819336, "The Affiliation of the Yukihoro Takahashi Author is Unknown."]
[8.223822593688965, 4.011210918426514, "The Senegal Population Coverage of the Astrocast Satellite Operator is Almost 5%."]
[1.6063458919525146, 4.7969136238098145, "The CDH Boot Sector Voltage of the MarCO-B Satellite is Approximately 3.3 V."]
[7.971897602081299, 9.829534530639648, "The Multi-channel Observation Capability of the AMI Advanced Meteorological Imager is 16 channels (4 VIS and 12 infrared)."]
[9.053068161010742, 6.1827263832092285, "The Components of the Microstrain 3DM-GX2 Inertial Measurement Unit is 3-axis magnetometer, three accelerometers, and a rate gyroscope."]
[8.277716636657715, 9.663848876953125, "The Number of Detector Pixels of the Long Wavelength Band Spectrometer is 512 x 512."]
[5.56181526184082, 3.457625389099121, "The URL of the Intermediate Experimental Vehicle Spacecraft is http://www.spaceflight101.com/ixv.html."]
[9.220451354980469, 5.830999374389648, "The Attitude Sensing of the AOCS Attitude and Orbit Control System is Star tracker assembly (3 star tracker heads), 3 magnetometers, and a CESS (Coarse Earth and Sun Sensor) assembly."]
[8.493956565856934, 2.876502513885498, "The Science Investigations of the ARTEMIS Probes Spacecraft is 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."]
[9.297857284545898, 4.208409309387207, "The Instrument Size of the Aquajet Satellite Propulsion System is 100 mm x 100 mm x 30 mm."]
[4.840950012207031, -3.3863487243652344, "The Member of the Mark Bourassa Individual is True."]
[5.143687725067139, 4.665473461151123, "The Purpose of the In-Space Relay Network Communication System is Allow continuous communications from space to ground."]
[3.814573287963867, 6.669490814208984, "The Clock Rate of the DPSK Transmitter Transmitter is 2.88 GHz."]
[7.94325590133667, -0.24711643159389496, "The Launch Schedule of the Shenzhou XIV Manned Spacecraft is This year."]
[8.41242790222168, 7.49616003036499, "The Intrinsic Noise Level of the ISA Accelerometer is About 10-10g/\u221aHz."]
[2.3043746948242188, 5.134815216064453, "The Power Consumption of the Power Electrical System is 43.5 W."]
[8.538152694702148, 9.5141019821167, "The CCD Detector Type of the MEGS Spectrograph is Back-thinned, back-illuminated."]
[2.2156870365142822, 4.451406002044678, "The S/C Power of the QuikTOMS spacecraft Satellite is 228 W EOL."]
[9.300933837890625, 4.074245452880859, "The Size of the GRACE-FO satellites Satellite is 3 m x 3 m x 0.8 m."]
[6.928173065185547, 8.671088218688965, "The Depth Resolution of the FREND Instrument is ~1 m."]
[7.477271556854248, 5.316872596740723, "The Noctilucent Cloud Observation Frequency of the AIM Satellite is Late spring and early summer."]
[9.438316345214844, 5.4471306800842285, "The ADCS of the MiRaTA Satellite is 3-axis stabilized."]
[8.21934986114502, 8.805842399597168, "The IR Bands of the CrIS Instrument is 3."]
[6.075797080993652, 11.248055458068848, "The Approx. peak sensitivity altitude of the Channel 6 Sensor is Unknown."]
[5.770936012268066, 2.3735365867614746, "The URL of the Space Based Space Surveillance (SBSS) Satellite is http://www.afspc.af.mil/library/factsheets/factsheet.asp?id=20523."]
[6.200474739074707, 4.440533638000488, "The SAR Constellation Data Distribution of the Spacety Company is Worldwide."]
[8.087037086486816, 1.3847297430038452, "The Next Close Pass of the Sun of the Solar Orbiter Satellite is March 2022."]
[6.481789588928223, -0.6188814043998718, "The Control Date of the QZS-1 Satellite is Feb. 22, 2017."]
[7.30094051361084, 1.149411916732788, "The Mission Date of the KazSTSAT Satellite is Unknown."]
[10.002734184265137, 4.112578868865967, "The URL of the Electric Solar Wind Sail (E-sail) Solar Sail is http://www.electric-sailing.com/."]
[1.3558827638626099, 4.179201126098633, "The Fabrication Defect of the Robusta Satellite is Prevents the CubeSat\u2019s batteries from being charged."]
[7.075295448303223, 6.704780578613281, "The Type of the TROPOMI Instrument is Pushbroom type imaging spectrometer."]
[9.03805160522461, 6.285732269287109, "The Function of the Gyroscopes Gyroscopes is Derive the satellite rates."]
[7.2209062576293945, 8.723283767700195, "The Ground Swath of the AEISS-A Instrument is Around 12 km."]
[8.839323043823242, 3.3506693840026855, "The Orbital Position of the ACTS/TOS Communication Technology Satellite is GEO (Geosynchronous Earth Orbit) at longitude 100\u00ba West."]
[8.479387283325195, 6.857263565063477, "The Function of the OSCAR-QUBE Experiment is Perform extremely rapid and precise magnetic field measurements."]
[11.073892593383789, 4.937547206878662, "The Electron Production Time of the Solar storm Natural Phenomenon is 60 seconds."]
[9.266684532165527, 10.303603172302246, "The Number of Images of the DECA Descent Camera is 15."]
[9.987525939941406, -0.7583664655685425, "The Upper Plate Shape of the Baumanets-2 Microsatellite is Hexagonal."]
[5.385319232940674, 4.285758018493652, "The Function of the PPS Precipitation Processing System is 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."]
[7.766272068023682, 2.525580644607544, "The Tandem Passes Separation of the Envisat / ERS-2 SAR Satellite is 28 minutes."]
[5.86060094833374, 2.2042672634124756, "The QKD Channel Collaborator of the QUESS Satellite is Anton Zeilinger and colleagues at the University of Vienna."]
[8.305913925170898, 8.642062187194824, "The Prime Contractor of the NIRCam Near-Infrared Camera is University of Arizona."]
[10.371826171875, 5.675380229949951, "The Orbit of the ProSEDS Tether Demonstration Experiment is Circular."]
[4.338068962097168, 6.509664535522461, "The Frequency of the Ka-band Channels Communication System is 30 GHz uplink, 20 GHz downlink."]
[5.305048942565918, 6.886005401611328, "The Rotation Rate of the Antenna Conically-scanning reflector is 14.6 rpm."]
[8.204146385192871, 9.191242218017578, "The Pixels per FWHM of the Spectrometer Instrument is 1650."]
[9.894488334655762, 6.460605144500732, "The Temperature of the Solar Panel Satellite Component is Variable."]
[6.852660655975342, 3.9826555252075195, "The Mission of the BioSentinel Satellite is Detect, measure and compare the impact of deep space radiation on living organisms over long durations in deep space."]
[12.122279167175293, 3.315222978591919, "The Inclination of the ExoMars Orbiter Satellite is 74\u00ba."]
[7.286721229553223, 1.3466330766677856, "The Meeting Date of the BioSentinel Satellite is 2-3 September 2-3 2015."]
[7.156791687011719, 5.019489765167236, "The Methane Detection Threshold of the iSIM-90 Imager is 150 kg/h."]
[6.686496257781982, 2.8978002071380615, "The Data Receiving and Processing Stations Locations of the Kolibri-2000 Satellite is Tarusa, Obninsk (Russia), and Sydney (Australia)."]
[6.899610996246338, 2.128103017807007, "The Unknown of the RapidEye Satellite Constellation is Unknown."]
[4.909241676330566, -3.242988109588623, "The | of the Douglas P. Adler Individual is Fred A. Best, Douglas P. Adler, Claire Pettersen, Henry E. Revercomb, P. Jonathan Gero, Joseph K. Taylor, Robert O. Knuteson, John H. Perepezko."]
[6.146009922027588, 0.5364173650741577, "The Launch Date of the GRIFEX 3U CubeSat is January 31, 2015."]
[6.008133888244629, 9.556632995605469, "The Weight of the Windsat Instrument is 450 kg."]
[4.782679080963135, 0.8673375844955444, "The Contract Value of the GeoOptics Satellite Manufacturer is $1 million."]
[6.509161472320557, 1.1506433486938477, "The Announcement Date of the 2Operate and GomSpace Companies is 5 March 2019."]
[6.367452621459961, 4.791069984436035, "The Data Processing of the Sentinel-4 Satellite is Level-0 data into Level-1B data."]
[4.089287757873535, 4.479869365692139, "The Components of the Communications PCPMU Communication System is PU (Processing Unit), DSU (Data Storage Unit), MDMs (Modulator/Demodulator) assemblies, FGMs (Frequency Generator Modules), EPCs (Electric Power Control) cards."]
[5.8570332527160645, 8.59932804107666, "The Frequency of the HSB Humidity Sounder is 183.3 GHz."]
[7.760695934295654, 3.903010606765747, "The Width of the Pluto's Glacier Nitrogen Glacier is 1,000 kilometers."]
[3.633618116378784, 6.360321998596191, "The Uplink Data Rate of the RF Communications Communication System is 4.8 kbit/s."]
[9.261787414550781, 4.174950122833252, "The Antenna Length of the Cluster spacecraft Satellite is 88 m."]
[1.4965771436691284, 4.292111396789551, "The Controls the state of charge of a 40 Wh battery pack and distributes power to all satellite subsystems of the PCDU Function is True."]
[3.6837708950042725, 4.80142068862915, "The Interrupts of the dsPIC33F microcontroller Microcontroller is Unknown."]
[11.494234085083008, -0.9738451838493347, "The Payload Mass (max) of the  DSX Spacecraft Payload Module Satellite is 170 kg."]
[7.108905792236328, 8.873977661132812, "The Swath Width of the Instrument Satellite Instrument is 40 km (full mode)."]
[1.9486712217330933, 4.0633392333984375, "The Solar Panel Efficiency of the AprizeSat Satellite is 28.3%."]
[8.008036613464355, 0.6207446455955505, "The End of Life Date of the Megha-Tropiques Satellite is 15 Dec 2021."]
[8.644013404846191, 0.1667185127735138, "The Number of Crews of the Skylab-1 Space Station is Three."]
[8.02383041381836, -0.706572949886322, "The Arrival Date at Space Station of the Cargo Dragon Spacecraft is December 7."]
[11.855914115905762, 1.0092804431915283, "The Previous Lunar Landings of the Chang'e-5 Spacecraft is Chang\u2019e-3 and Chang\u2019e-4 missions."]
[5.290344715118408, 1.053567886352539, "The Launch Cost Savings of the ORS-6 Satellite Mission is 25-50%."]
[7.362034797668457, 3.653960943222046, "The Sensors of the SPOT-4 Satellite is Unknown."]
[8.251044273376465, 4.488566875457764, "The Sensitivity of the INTEGRAL Satellite is High sensitivity to gamma rays."]
[10.103272438049316, 1.5436714887619019, "The Period of the ZY 1-02C Spacecraft is 100.3 minutes."]
[3.633283853530884, 6.51565408706665, "The Symbol Rate of the Transmitter Communication Device is 200 Msample/s."]
[4.813271999359131, 1.9414669275283813, "The Number of Satellite Pairs of the MetOp-SG Satellite Program is 3."]
[4.672021865844727, 7.167850017547607, "The Size of the Receiver Communication Device is 70 mm x 60 mm x 30 mm."]
[2.2663354873657227, 4.462976455688477, "The Power of the Spacecraft Satellite is 1260 W."]
[10.055047988891602, 1.5095254182815552, "The Period of the CSG and CSK satellites Satellite is 97 minutes."]
[10.136680603027344, -1.0253276824951172, "The Magnetic Field Alignment of the Dove-1 Nanosatellite is About 1\u00ba."]
[1.2100409269332886, 4.129260540008545, "The Battery Type of the TacSat-4 Satellite is Lithium ion."]
[2.286367416381836, 6.489947319030762, "The Latency of the ATL00 Telemetry Data Data is Downlinked 8 times/day."]
[8.18922233581543, -0.48490655422210693, "The Collection Location of the Yuanwang-21 and -22 Cargo Ships is Tianjin."]
[9.466681480407715, -0.7506140470504761, "The Launch Site of the IDEA-OSG 1 Microsatellite is Vostochny launch site."]
[11.6326322555542, 6.133091926574707, "The Main Tank Replenishing Procedure of the XMM-Newton Satellite is Under development."]
[4.612357139587402, 0.20852643251419067, "The Planned Number of Satellites of the OneWeb Satellite Constellation is 648."]
[9.960677146911621, -0.7542010545730591, "The Bottom Plate Shape of the Baumanets-2 Microsatellite is Hexagonal."]
[7.848359107971191, 2.962326765060425, "The Impact Experiment Initiation Year of the DebriSat Satellite is 2011."]
[9.50291633605957, 0.5129222273826599, "The Mission Design Life of the Spacecraft Satellite is 1.5 years."]
[5.911510467529297, 6.749783039093018, "The Ground Truth of the LPR Radar is Stratigraphic architecture of an ejecta deposit."]
[4.955933094024658, 2.2307395935058594, "The Payloads of the TDS-1 Satellite is 8."]
[4.393676280975342, 5.780951976776123, "The Uplink Band of the Spacecraft Satellite is S-band (2 kbit/s)."]
[8.008593559265137, 4.6069841384887695, "The Spatial Resolution of the Pixxel\u2019s planned satellites Satellite is 5 m."]
[8.620508193969727, 2.019444704055786, "The Purpose of the Webb Space Observatory is To see farther into our origins: from the formation of stars and planets to the birth of the first galaxies in the early Universe."]
[4.360683441162109, 4.455955505371094, "The Router Internal Connections of the SpaceWire ASIC Application-Specific Integrated Circuit is 2."]
[5.787409782409668, 3.897566795349121, "The Provider of the LRR Instrument is GFZ Potsdam."]
[7.357184886932373, 7.964252471923828, "The Minimum Concentration in 2016 of the Ozone Layer Atmospheric Layer is 114 Dobson Units."]
[7.200005054473877, 1.4758788347244263, "The Launch Year of the ESA\u2019s Space Situational Awareness (SSA) program Program is 2009."]
[7.591516494750977, 9.017754554748535, "The Wavelength Bands of the SBUV Spectrometer is 0.250 - 0.340 \u00b5m."]
[7.102818489074707, 4.893853187561035, "The Mission of the GOSAT Satellite is Greenhouse Gases Observing."]
[1.7728537321090698, 4.821292400360107, "The Bus Voltage of the Spacecraft Satellite is 4.0 V."]
[9.340587615966797, 8.524545669555664, "The External Surface Coating of the Receiver Housing Housing is Gold."]
[5.421433448791504, 2.4111485481262207, "The Affiliated Countries of the PUTC Program is France, Belgium, Spain, Sweden and Austria."]
[11.331793785095215, 4.16666841506958, "The Type of the 55 Cancri e Exoplanet is Rocky."]
[9.585074424743652, 5.984540939331055, "The Actuators of the iADCS-100 ADCS System is Miniature reaction wheels."]
[8.693856239318848, 2.419764995574951, "The Imaging of the Parker Solar Probe Satellite is Visible Light."]
[9.284893035888672, 1.3203352689743042, "The Observation Duration of the Kepler space telescope Telescope is Nine years."]
[8.672706604003906, 10.041398048400879, "The Imaging Resolution of the PAIS Imaging System is Higher than an equivalent direct imaging system."]
[6.565497398376465, 4.586665153503418, "The Instruments of the MTSAT Satellite is Imager, JAMI, MTSAT DCS, MTSAT Comms, GPS receiver."]
[10.290786743164062, 2.8737633228302, "The Orbit Altitude of the Tianhe Space Station Module is 370 kilometers."]
[4.410308361053467, 6.691975116729736, "The Frequency Selectivity of the LICEF Receiver is High."]
[9.711458206176758, 8.75133228302002, "The Signal Strength Level of the RRA RetroReflector Array is Between LAGEOS and ETALON."]
[8.669145584106445, 1.9692727327346802, "The URL of the James Webb Space Telescope Space Telescope is http://www.stsci.edu/jwst/."]
[8.253531455993652, 0.6784037351608276, "The Years on Orbit of the Megha-Tropiques Satellite is 3."]
[8.621871948242188, 6.227480888366699, "The Deployment Position Reporting of the AstroTubeTM Boom Boom is Yes."]
[8.95840072631836, 3.2993712425231934, "The Purpose of the MEO Medium Earth Orbit is Cellular telephone communication and navigation."]
[9.487549781799316, 1.6201742887496948, "The Pass-Prediction Frequency of the SpinSat Satellite is Once every two weeks."]
[8.935503959655762, 2.7455453872680664, "The Mission Status Presentation of the GCOM-W Satellite is August 13, 2005."]
[8.158193588256836, 8.445775032043457, "The Mechanism of the IASI-NG Interferometer is Patented mechanism allows performing simultaneously the OPD scan and the compensation using a single actuator."]
[11.683798789978027, -1.1397777795791626, "The Mass of the Spacecraft Satellite is 1.22 kg."]
[2.279848098754883, 4.416323184967041, "The Total Power of the Spacecraft Satellite is 5.4-11 W (6 W average)."]
[7.5082197189331055, 1.0831726789474487, "The Discovery Date of the NASA Satellite Satellite is June 1, 2016."]
[4.7213263511657715, 1.6758960485458374, "The Number of Satellites of the Galileo Satellite Constellation is 2."]
[6.122289657592773, 1.7070515155792236, "The Launch Vehicle of the ALOS-2 Satellite is Mitsubishi vehicle - an H-IIA F24 bus."]
[8.093168258666992, 4.045339107513428, "The Hubble Space Telescope Images Containing Satellite Streaks of the Starlink Satellite Constellation is Currently 8% of all images."]
[7.2340006828308105, 0.4393782913684845, "The Launch Date of the SAMPEX Satellite is July 3, 1992."]
[6.458384037017822, 4.763312339782715, "The Radar of the Sentinel-1A Satellite is C-band."]
[5.336511611938477, 2.7212841510772705, "The Designing University of the VisionCube-1 CubeSat is Korea Aerospace University (KAU)."]
[7.342000484466553, 10.067702293395996, "The Wavelength Separation Direction of the HyperScout\u00ae Imaging System is Along track."]
[8.446451187133789, 10.55198860168457, "The Dynamic Range of the Kruiz CCD Detector is 2500."]
[7.373569011688232, 3.6575767993927, "The Satellite Configuration of the RADARSAT Constellation Satellite Constellation is Orbiting in formation, each dephased by 120\u00b0."]
[8.731201171875, 0.2639339864253998, "The Mission Duration of the Falcon Heavy Launch Vehicle is Over six hours."]
[6.200710773468018, 2.240793228149414, "The Renamed By of the KhalifaSat Satellite is His Highness Sheikh Mohammed Bin Rashid Al Maktoum."]
[7.797666549682617, 9.840497016906738, "The Spectral Bands of the EarthDaily Optical Imager Optical Imager is 22."]
[5.624881744384766, 0.4707867205142975, "The Year Founded of the Saltworks Salt Production Facility is 1954."]
[5.146116256713867, 1.9755064249038696, "The Record Load of the Minotaur I Rocket Rocket is 28 CubeSats."]
[8.201220512390137, 10.030117988586426, "The Spatial Resolution of the MSASI Imager is 1.25 km."]
[6.969161033630371, 0.5631306171417236, "The Launch Date of the Resurs-P2 Satellite is December 2014."]
[7.239196300506592, 6.038334846496582, "The Location of the Aerosol Images Image is Ganges river."]
[7.181395530700684, 4.036123752593994, "The Imaging Capability of the SEOSAT\u2013Ingenio Satellite is Sideways with access to any point on Earth within three days."]
[8.695443153381348, 9.078255653381348, "The Energy Optimization of the MEG Grating is Medium."]
[7.543454170227051, 7.984199047088623, "The DEM/DSM Accuracy of the HRS Instrument is 5 m (relative) and 10/15 m (absolute)."]
[4.67145299911499, 1.9351011514663696, "The Number of Satellites of the Transport Layer Satellite Network is Up to 150."]
[7.775208473205566, 7.761378765106201, "The Geometric Factor of the Instrument Instrument is 0.52 sr cm2."]
[9.267354965209961, 5.484142780303955, "The Attitude Actuators of the SUNSAT Satellite is 3-axis reaction wheels, 3-axis magnetic torquer coils."]
[8.767510414123535, 9.977818489074707, "The Number of Subapertures of the Direct Imaging System Imaging System is 8."]
[12.172632217407227, 3.2843291759490967, "The Inclination of the CBERS-2B Satellite is 98.5\u00ba."]
[8.924367904663086, 9.700638771057129, "The Optics Unit Architecture of the Imager Payload is Extendable."]
[10.715396881103516, 10.24429988861084, "The Measurement of the PHA HiLRS is Spectrum of ionizing particle energy, charge, and mass."]
[9.019937515258789, 9.661948204040527, "The Imaging System of the Rosetta Satellite is OSIRIS camera."]
[11.486286163330078, -1.3503834009170532, "The Mass of the TechDemoSat-1 Satellite is 150 kg."]
[8.647811889648438, 9.157004356384277, "The Slit Width of the Long Wavelength Band Spectrometer is 150 \u00b5m."]
[9.486842155456543, 3.945493221282959, "The Semi-Major Axis Adjustment of the CanX-5 Satellite is Within Meters of What Was Planned."]
[8.740452766418457, 3.1940555572509766, "The Orbit Altitude of the GOCE Satellite is Varies."]
[4.890147686004639, 12.099248886108398, "The Responsivity Measurement of the Responsivity Measurement Instrument is 106 A/W."]
[8.460530281066895, 6.809813022613525, "The Manufacturer of the GMAG Magnetometer is NASA\u2019s Goddard Space Flight Center."]
[4.442699909210205, 2.787330389022827, "The Toolkit of the Ubotica CogniSAT-XE1TM CubeSat Board Satellite Device is Intel\u00ae\u2019s OpenVINO\u2122."]
[10.337461471557617, 7.823396682739258, "The Material of the TOGS Telescope is Aluminum."]
[6.347525596618652, 8.219488143920898, "The Beamwidth of the AMSU Microwave Radiometer is 3.3\u00ba."]
[9.936230659484863, 7.838640213012695, "The Energy Range of the LET Low Energy Telescope is ~1.5 to ~60 MeV/nucleon."]
[9.080692291259766, 5.331911087036133, "The Attitude Subsystem Agile Platform of the Spacecraft Satellite is \u00b145\u00ba pointing in cross-track (max), \u00b130\u00ba pointing in cross-track (nominal)."]
[10.040752410888672, 1.5299136638641357, "The Osculating Orbital Period of the SMART-1 Satellite is 4.978457 hours."]
[6.158102989196777, 2.259427547454834, "The Receiver Type of the Jason-1 Satellite is Miniaturized 2nd generation receiver (5.6 kg), a bi-frequency system in 2 channels."]
[6.901005744934082, 3.9361062049865723, "The Operator of the Deimos-2 Earth Observation Satellite is Elecnor Deimos."]
[5.126923561096191, 2.1711933612823486, "The Number of Teams of the PRISMA Satellite Network is 3."]
[8.100086212158203, 5.025125980377197, "The Data Usage of the Iridium Constellation Satellites Satellite is Characterize the variation of the Birkeland currents with interplanetary conditions, particularly during magnetic storms."]
[9.429447174072266, 9.981679916381836, "The Purpose of the Google Earth Application is Earth surface image generator."]
[6.909150123596191, 0.47420763969421387, "The Launch Date of the GEOS-1 Satellite is 6 November 1965."]
[5.659420013427734, 5.504098415374756, "The Type of the SGR-07 GPS Receiver is Space."]
[11.529212951660156, 6.194124698638916, "The X-ray Nova Detection Date of the ISS Instrument Instrument is Oct. 4, 2010."]
[9.469965934753418, 7.3033833503723145, "The Materials of the FSU Solar Wind Faraday Cup is Molybdenum TZM."]
[8.482586860656738, 5.247236728668213, "The Control Accuracy of the CALIPSO Satellite is \u00b1 10 km at equator crossing."]
[3.046649932861328, 4.136568546295166, "The Platform of the IOD-1 GEMS Satellite is CSL 3U structure."]
[7.5871076583862305, 0.8009266257286072, "The Mission Overview Date of the WindSat Satellite is Polar Max 2006."]
[9.060822486877441, 7.707865238189697, "The Sensor Type of the LINAS Ionization Gauge is Hot-filament ionization gauge."]
[9.702168464660645, 10.058082580566406, "The Funding Source of the Small Monitor Camera (CAM-H) Camera is Contributions from the public."]
[11.738112449645996, -1.1354248523712158, "The Maximum Satellite Mass of the AD-SS 150 Satellite Dispenser is 150 kg."]
[11.74606990814209, 4.494777202606201, "The Number of Stars of the Lower Centaurus Crux Star Cluster is 97."]
[3.6117115020751953, 6.739051818847656, "The Radio Frequency Output Power of the X-band transmitter Transmitter is Programmable."]
[9.453049659729004, 0.6572063565254211, "The Mission Lifetime of the Satellite Communication Satellite is ~17 years."]
[9.053533554077148, 9.108613967895508, "The IFOV of the Telescope Optical Instrument is 0.004\u00ba."]
[7.212881565093994, 4.994866847991943, "The Measurement Importance of the FORUM Satellite Mission is Important for understanding atmospheric processes linked to climate change."]
[10.027875900268555, 2.180050849914551, "The No of revolutions of the KOMPSAT-3A Satellite is 15.1 revolutions/day."]
[13.048503875732422, 4.104194164276123, "The Number of Stars of the Gaia EDR3 Satellite Data is More than 1.8 billion."]
[5.6222243309021, 5.539346694946289, "The Type of the GPS receiver Receiver is SGR-20 model."]
[7.464138507843018, 1.1340116262435913, "The News Archive Date of the INTEGRAL Satellite is 5 Aug. 2011."]
[6.658977031707764, 0.9749046564102173, "The Presentation Date of the COSMIC-2 Satellite Constellation is April 3, 2015."]
[6.844165325164795, 7.681387424468994, "The Range Measurement Accuracy of the RA-1 Instrument is Better than 10 cm."]
[10.179980278015137, 2.1197123527526855, "The Fast Plasma Investigation Event Duration of the MMS Satellite is 45 milliseconds."]
[7.3503336906433105, 7.628701686859131, "The Heritage of the SUSIM Spectrometer Instrument is Spacelab-2 (STS-19, July 29-August 6, 1985) and on UARS."]
[5.0491132736206055, 6.783230304718018, "The Input Matching of the Array Radiator Antenna is Better than -18 dB in the full 300 MHz bandwidth."]
[3.8637194633483887, 6.507987976074219, "The Instrument Data Rate of the GNSS-RO Receiver Receiver is About 53 kbit/s."]
[8.930126190185547, 9.574973106384277, "The Design of the Optic with SDD Optic and Detector is Low-cost, low-mass."]
[6.122925758361816, 3.997915267944336, "The Transmission Type of the AISat Satellite is From space."]
[4.317727088928223, 4.300496578216553, "The Software of the Control Room Facility is SCOS-2000."]
[6.276257514953613, 1.8224492073059082, "The Deployment Goal of the ADS-B Air Traffic Surveillance System is End of 2019."]
[6.459014415740967, 4.103894233703613, "The Purpose of the S&RSAT Search&Rescue Satellite Aided Tracking System is Support search and rescue operations for aviators, mariners, and land travellers in distress."]
[3.8959176540374756, 5.164421558380127, "The Protocol of the FODB Data Interface is Asynchronous Transfer Mode (ATM) based."]
[8.336628913879395, 3.6627726554870605, "The Mission Plan of the TanDEM-X Satellite is Not provided."]
[11.733654022216797, -0.9373533129692078, "The Mass of the Stone Payload is 1 kg."]
[7.305129528045654, 1.077301263809204, "The Publication Date of the Onboard Processing Satellite System is 27 February 2018."]
[10.307772636413574, 2.9400575160980225, "The Orbit Altitude of the R3 CubeSat Satellite is 500 km."]
[9.1370267868042, 9.168631553649902, "The FOV of the Microdosimeter A Instrument is 38\u00ba."]
[7.511814117431641, 1.930025339126587, "The First-Light Measurement Date of the ICIR IceCube Cloud\u2013Ice Radiometer is June 6, 2017."]
[7.222152233123779, 5.4494500160217285, "The Effect on Climate of the El Ni\u00f1o Weather Phenomenon is Above-average winter rainfall in California, drier-than-normal winters in Oregon and Washington."]
[8.185220718383789, 8.34461784362793, "The Operation of the UV/VIS Spectrometer Spectrometer is Continuously over full orbit."]
[8.747775077819824, 5.188652992248535, "The Attitude Knowledge of the GFO Satellite is Derived from horizon scanners."]
[4.453917980194092, 1.4871290922164917, "The Complexity of the EIRSAT-1 Satellite is Equivalent to a standard space mission."]
[6.118225574493408, 0.7211712598800659, "The Survey Date of the CubeSat Communication Systems Satellite System is April 18, 2008."]
[6.2772369384765625, 3.419769525527954, "The URL of the GFO Satellite is http://ibis.grdl.noaa.gov/SAT/gfo/."]
[1.9153878688812256, 4.075535774230957, "The Size of the Solar Cells Power Generation is 40 x 80 cm."]
[7.744124412536621, 3.8271570205688477, "The Size of the Langj\u00f6kull Glacier is Iceland\u2019s second largest ice cap."]
[10.343069076538086, 1.9570417404174805, "The Period (min) of the Meteor-2-1 Satellite is 102.5."]
[10.365036964416504, 5.670966625213623, "The Tether Composition of the ProSEDS Tether Demonstration Experiment is 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)."]
[8.210477828979492, 8.21139907836914, "The Imaging Spectrometers of the CASA-212-200 aircraft Aircraft is Three."]
[8.064388275146484, 1.249323844909668, "The Date of the Hunting Milky Seas by Satellite Image is 2 November 2021."]
[6.510400295257568, 6.239537715911865, "The Swath of the OSCAT Scatterometer is 1400 km."]
[1.9238860607147217, 4.076079845428467, "The Cost of the Low Cost Solar Panel Solar Panel is Low."]
[9.466954231262207, -0.740984320640564, "The Contract Award Date of the M3MSat Microsatellite is June 23, 2008."]
[5.523382663726807, 4.457484245300293, "The Ground Stations of the Sentinel-1 Satellite is Svalbard, Maspalomas, Matera."]
[6.021729469299316, 6.384946823120117, "The Residual Phase Error of the Instrument SAR is \u226410\u00ba."]
[8.23282241821289, 1.1305615901947021, "The Image Capture Time of the Long Range Reconnaissance Imager (LORRI) Imager is 11:04 Universal Time on February 28, 2007."]
[9.136616706848145, 3.2190792560577393, "The Orbit Type of the Satellite SuperView Constellation is Sun-synchronous orbit."]
[6.33208703994751, 4.339682102203369, "The Purpose of the TROPICS Constellation of CubeSats is Study the development of tropical cyclones through rapid-revisit sampling."]
[9.624773979187012, 8.50455093383789, "The Transmission Profile of the Etalon Etalon is Unknown."]
[10.416932106018066, 7.210711479187012, "The Properties Below Critical Temperature of the TEMBOTM EMC Material is Comparable to the conventional \"rigid\" composite structures."]
[8.125938415527344, 5.041459083557129, "The Geo-Referencing Precision of the Claire Satellite is With sufficient precision to identify facilities of interest."]
[9.311901092529297, 5.711258888244629, "The | of the iADCS Flight Model is Preparing the First Flight Model of iADCS - Results of Air Bearing Tests."]
[6.172940254211426, 2.283198118209839, "The Leading Organization of the TacSat-3 Satellite is AFRL."]
[1.2924177646636963, 4.243654251098633, "The Actual Battery DoD of the IXV Spacecraft is 10%."]
[8.16484260559082, 3.4843497276306152, "The Development Status of the Space Weather Mission Satellite is Not Launched."]
[4.8872857093811035, 1.57735276222229, "The Constellation Operations of the FormoSat-7 / COSMIC-2 mission Satellite Mission is 6 satellite constellation operations."]
[10.686983108520508, 5.279850482940674, "The Maximum Relative Distance of the CNAPS Propulsion System is 1000 m."]
[8.342623710632324, 3.648033618927002, "The Product Definition of the TanDEM-X Satellite is Not provided."]
[6.453351020812988, 3.333695888519287, "The Test Transmission Location of the Herschel Spacecraft is ESA's ESTRACK (ESA Tracking stations network) station at New Norcia, Australia."]
[3.8594539165496826, 6.450618267059326, "The Beacon Ku-band of the RF communications Communication Subsystem is 1 mW."]
[8.227025032043457, 10.244587898254395, "The Data Density of the DMC-2G imager Imager is Doubled."]
[9.52254581451416, 6.060854434967041, "The Sensor Suites of the ADCS Attitude Determination and Control Subsystem is Four sun sensor suites and five two-axis magnetic sensors."]
[7.373579025268555, 0.22547267377376556, "The Previous Planned Launch Year of the NEMO-AM Satellite is 2017."]
[7.92179012298584, 3.8963425159454346, "The Images Collected per Day of the Landsat-8 Satellite is Approximately 1,500."]
[1.8746894598007202, 5.002862930297852, "The Mass of the PSU Power Supply Unit is 8 kg."]
[9.177408218383789, 10.597283363342285, "The Ground Sample Distance of the PamCam Panoramic Camera is Around 200 m."]
[6.733664512634277, 1.2194396257400513, "The Presentation Date of the JC2Sat-FF Satellite is April 23-25, 2008."]
[6.394551753997803, 3.1827921867370605, "The Satellite Mission Types of the Spacety Company is Science experiments or observation, in-orbit demonstrations and/or validations of space technologies and products, or space systems."]
[8.132328033447266, 1.489529013633728, "The Publication Date of the Solar Mass Ejection Imager Imager is 1997."]
[4.485276222229004, 5.642823219299316, "The Data Downlink of the GHOSt satellites Satellite is Ka-band, S-band for high speed data (HSD) transmissions."]
[3.5439658164978027, 6.448480606079102, "The Received Eb/No of the Unit Communication System is 7.52 dB."]
[10.130480766296387, 3.0020461082458496, "The Altitude of the Satellite GEO (Geostationary Earth Orbit) is 35,786 km."]
[4.886861324310303, 12.101934432983398, "The Responsivity Requirement of the Responsivity Measurement Instrument is >1.04 A/W."]
[8.858302116394043, 10.803403854370117, "The Data Rate of the WFC CCD Camera is 26 kbit/s."]
[9.029749870300293, 5.806127071380615, "The Temperature Sensors of the SEEDS-2 Satellite is Installed in 14 locations within the spacecraft."]
[11.880084991455078, 2.3832826614379883, "The Collector Head Depth of the OSIRIS-REx Spacecraft is 1.6 feet (48.8 cm)."]
[9.136052131652832, -0.612744927406311, "The Launch Site of the HORYU-2 Nanosatellite is TNSC (Tanegashima Space Center), Japan."]
[6.696736812591553, 9.107415199279785, "The Size of the CEASE-2 Instrument is 10 cm x 10 cm x 8.2 cm."]
[7.999477863311768, 1.9948567152023315, "The Image Content of the ExoMars Trace Gas Orbiter Orbiter is The region where the ancient Uzboi Vallis enters the Holden crater."]
[10.132628440856934, 3.038429021835327, "The Orbit of the MOST Payload is Sun-synchronous orbit of 820 km near-circular altitude."]
[11.56136703491211, 6.0137858390808105, "The Brightness Change of the X-ray Source Celestial Object is Up to 50 times its normal level."]
[9.290912628173828, 7.923601150512695, "The Temperature of the PICNIC IR detector Detector is Around 90 K."]
[8.053110122680664, 8.80056095123291, "The Optical Gains of the Limb Sensor Sensor is Two."]
[8.365568161010742, 2.817070245742798, "The URL of the \"Discrete and broadband electron acceleration in Jupiter's powerful aurora\" Research Paper is https://doi.org/10.1038/nature23648."]
[11.705462455749512, -1.0426572561264038, "The Solar Array of the Orion Spacecraft is Weight 260 kg."]
[5.027827262878418, 4.6028571128845215, "The Antenna Quantity of the Ground Segment Ground Control Infrastructure is 2."]
[6.1025776863098145, 0.5694056153297424, "The Solar Panel Deployment Date of the ALBus CubeSat Satellite is December 16, 2018."]
[6.361762523651123, 3.3768367767333984, "The Services of the Galileo Constellation Navigation Satellite is Positioning, navigation and timing services to our planet."]
[4.608702182769775, 0.1915382444858551, "The Number of Satellites of the OneWeb Satellite Constellation is 648."]
[4.49580717086792, 5.970102310180664, "The Communication Bands of the BioSentinel Spacecraft is Higher frequency bands."]
[4.380788803100586, 7.778158664703369, "The Center Frequency of the Channel 9 Sensor is 53.30 GHz."]
[7.818235874176025, 7.808365821838379, "The Shape Knowledge of the ISRF Instrument Spectral Response Function is Within 1%."]
[6.036868095397949, 3.6628570556640625, "The Location of the MBB Predecessor Organization of DASA is Ottobrunn, Germany."]
[9.96867847442627, 4.008953094482422, "The Payload Fairing Diameter of the CBAS and EAGLE Spacecraft is 5 m."]
[8.574959754943848, 5.418132305145264, "The Pointing Accuracy of the Spacecraft Satellite is 2.1 arcsec absolute pointing accuracy."]
[7.66659688949585, 9.67935848236084, "The Swath Width of the Instrument Spectral Imager is 2250 km."]
[6.9018025398254395, 5.622838020324707, "The Freeze/Thaw State Resolution of the SMAP Satellite is 3 km."]
[1.5306386947631836, 4.84871768951416, "The Voltage of the TriTel Electrical System Electrical System is 60 V."]
[5.178694725036621, 1.4804326295852661, "The Number of RAFS Clocks of the GIOVE-A Satellite is 2."]
[9.195301055908203, -0.6218520402908325, "The Launch Vehicle of the HORYU-2 Nanosatellite is H-IIA of Japan."]
[8.588375091552734, 8.779973030090332, "The Grating Angle of the Offner-type spectrometer Spectrometer is 5\u00ba at 325 nm."]
[5.879637718200684, 6.813319206237793, "The Frequency of the SIRAL Radar is 13.575 GHz."]
[10.24467658996582, 2.991525411605835, "The Altitude of the Orbit Centaur AV-042 upper stage is 467 km x 883 km."]
[9.695507049560547, 7.556111812591553, "The Energy Overlap of the IMAP-Ultra Instrument is Overlaps in energy with IMAP-Hi for heliospheric energetic H."]
[2.2537477016448975, 4.487027168273926, "The Transmitter Power of the OPAL Satellite is 2.2 W."]
[6.0136260986328125, 6.332664966583252, "The Total Ambiguity Ratio of the Instrument SAR is \u2264 -18 dB."]
[9.19294548034668, 3.235893487930298, "The Orbit Type of the COMPASS-1 Satellite is Sun-synchronous circular polar orbit."]
[7.266290187835693, 5.199554920196533, "The CO2 Reactivity of the AIRS Satellite is Does not react with other gases in the atmosphere."]
[6.613724708557129, 6.019647121429443, "The Presentation Date of the SWIM Scatterometer is July 12-17, 2009."]
[6.030691146850586, 9.57353687286377, "The Mass of the NewMag Magnetometer is 3 kg."]
[6.992419242858887, 7.971473217010498, "The Orbit Repeat Cycle of the MSU-SK Radiometer is 21 days."]
[6.925183296203613, 5.326758861541748, "The Dataset of the SMOS Satellite is Vegetation optical depth dataset."]
[6.8147735595703125, 3.850675344467163, "The Purpose of the Mouse Cells and Fruit Flies Biological Models is Obtain gene expression profiles and identify sensitive biological molecules as space radiation markers."]
[7.35693359375, 4.208561897277832, "The Calibration Phase of the DEIMOS-2 Satellite is Coming days."]
[8.799480438232422, 5.24091911315918, "The Attitude Accuracy of the Sentinel-1 Satellite is Stringent requirements on attitude accuracy."]
[7.754819869995117, 7.327290058135986, "The Calibration Requirements of the MOPITT Instrument is Unknown."]
[7.768544673919678, 9.653752326965332, "The Scan Lines of the Visible Spectral Band Spectral Band is 2500 x 4."]
[8.330927848815918, 10.50496768951416, "The Deviation of Center Wavelength of the 4-band CCD Imager Instrument is < 5 nm."]
[7.8453898429870605, 0.7196931838989258, "The Test Flight Date of the Starliner Spacecraft is Late Summer."]
[8.130594253540039, 8.950177192687988, "The Detection Limit of the VIS Visual Instrument is AB 24.5 magnitude."]
[6.714481830596924, 1.3433579206466675, "The Symposium Date of the ALOS PRISM Satellite is 14 \u2013 16 May 2014."]
[9.458459854125977, 0.5399594902992249, "The Design Life of the Odin Satellite is Two years."]
[7.905213356018066, 2.0632290840148926, "The Stationkeeping Maneuvers of the ISEE-3 Spacecraft is 15."]
[7.024470806121826, 1.2367310523986816, "The Consortium Leadership Date of the Planet Company is 27 January 2021."]
[6.707023620605469, 0.8771222233772278, "The Presentation Date of the FormoSat-7 /COSMIC-2 Satellite is September 6-11, 2010."]
[6.977626323699951, 4.818246841430664, "The Focus of the Sustainability Tech Company is Tropical forest ecosystems in Southeast Asia."]
[10.219632148742676, 5.208153247833252, "The Dimensions of the FENIX micropropulsion device Micropropulsion Device is 10 cm long and 2 cm wide."]
[11.189301490783691, 6.458553791046143, "The URL of the NICER Neutron star Interior Composition Explorer is https://heasarc.gsfc.nasa.gov/docs/nicer/gallery/slides/NICER_Science_Overview.pdf."]
[7.315184593200684, 3.3778269290924072, "The GIFOV of the TRUTHS Satellite is Unknown."]
[8.485358238220215, 4.446445465087891, "The Error of Amplitude Spectrum of the BRITE Satellite is 2 x 10-5 (20 ppm)."]
[7.512945175170898, 7.935739994049072, "The Accuracy of the CERES Instrument is 0.8 Wm -2  sr -1."]
[5.140438079833984, 4.45902681350708, "The Developer of the Ground Segment Data Processing is Spacebel in Belgium with scientific support from the Belgian institute for Space Aeronomy (BISA) and the University of Saskatchewan (USASK) in Canada."]
[8.66125202178955, 6.618712425231934, "The Purpose of the PlasMag Fluxgate Magnetometer Magnetometer is Provide crucial continuity of observation of interplanetary solar wind parameter."]
[6.980408668518066, 8.621381759643555, "The Resolution (IR) of the VHRR Very High-Resolution Radiometer is 11 km."]
[5.5811262130737305, 7.46867561340332, "The PRF of the KaRIn Instrument is 2 x 4420 Hz."]
[7.713739395141602, 13.595898628234863, "The No. of Bins of the SPIM4 Spectrometer is 68, 136, or 272."]
[7.685757637023926, 3.959348201751709, "The Arctic Sea Ice Volume of the CryoSat-2 Satellite is 10,200 km3."]
[11.397809028625488, 1.3508447408676147, "The Operation Status of the China's Moon Rover Rover is Sleeps."]
[5.12498140335083, 4.926800727844238, "The Data Collection Method of the EARS-ASCAT Data Service is Collects ASCAT instrument data from MetOp satellite passes via a network of Direct Readout stations."]
[7.486757278442383, 0.5063543915748596, "The Deployment Timing of the KE-2M satellite Satellite is After ISS reboost."]
[9.946843147277832, 9.5309476852417, "The Science Objectives of the SAGE-III Instrument is Investigate the spatial and temporal variability of the measured species."]
[3.861987590789795, 6.112766265869141, "The Data Rate of the SIOS Optical Link Demonstration Board Technology Demonstration Board is 100 Mbit/s."]
[6.773508548736572, 0.7461186051368713, "The Declaration Date of the STRaND-1 Satellite is March 07, 2013."]
[10.967700958251953, 7.212462902069092, "The Energy Range of the HXCP Hard X-ray Polarimeter is 30-100 keV."]
[4.244551181793213, 5.735352993011475, "The Downlink Frequency of the NEMO-AM Satellite is S-band."]
[8.097609519958496, 3.226163387298584, "The Additional Data Sources of the TanDEM-X Satellite is \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."]
[3.783628463745117, 4.5632805824279785, "The Reprogrammable of the MCU Microcontroller Unit is Reprogrammable."]
[7.556321620941162, 7.461966514587402, "The Manufacturer of the MOMA Mars Organics Molecule Analyzer is ESA."]
[9.570194244384766, 5.860085487365723, "The ADCS Equipments of the TDS-1 Satellite is Gyros and magnetometers."]
[5.676750659942627, 1.8719322681427002, "The Launch Vehicle of the LightSail-2 Solar Sailing CubeSat is SpaceX Falcon Heavy rocket."]
[5.97943639755249, 2.830138683319092, "The Owner of the Beijing-3 Satellite Constellation is Twenty First Century Aerospace Technology Co., Ltd (21AT)."]
[8.204931259155273, 0.20917795598506927, "The Meeting Date of the ISSP International Space Station Program is January 2011."]
[7.923065185546875, 1.4097741842269897, "The Date of the Solar Storms Natural Phenomenon is October and November of 2003."]
[4.113293170928955, 7.205531120300293, "The Mass of the COPS Ka-band Communication Payload is 316 kg."]
[11.381905555725098, -1.0359686613082886, "The Mainframe Launch Size of the SRMSat Satellite is 286 mm x 286 x 294 mm."]
[9.17611026763916, 4.231087684631348, "The Width with Solar Paddles Extended of the Nimbus-7 S/C Satellite is 3.96 m."]
[7.44305944442749, 3.9914488792419434, "The Sensor of the CartoSat-2B Satellite is PAN Camera."]
[8.056296348571777, 7.482799530029297, "The Type of the EFI Instrument is Electric Field Instrument."]
[9.592719078063965, 1.3711012601852417, "The Solar Array Deployment Time of the James Webb Space Telescope Space Telescope is Approximately 30 minutes after launch."]
[8.923348426818848, 5.206272125244141, "The Attitude Control Strategy of the Microsatellite Satellite is Interactive spacecraft pointing for event monitoring support."]
[7.903584003448486, 5.650810718536377, "The Area of the SAA South Atlantic Anomaly is Stretching from Africa to South America."]
[5.661263465881348, 3.0051562786102295, "The Manufacturer of the Satellite Vu Satellite is SSTL."]
[6.623875617980957, 3.3713767528533936, "The Payload of the MPQ442 Satellite is SuperSprite."]
[7.139625072479248, 0.12208221107721329, "The Launch Year of the S3C Satellite is 2024."]
[7.983111381530762, 9.258583068847656, "The Bands of the SCIAMACHY Spectrometer is 8."]
[8.133829116821289, 2.0299718379974365, "The DOI of the Herschel Satellite is 10.1088/0004-637X/773/2/102."]
[4.871901512145996, 1.7856322526931763, "The Number of Satellites of the SAR-Lupe Constellation Satellite Constellation is 5."]
[6.825923442840576, 2.9588398933410645, "The Development Locations of the POPSAT-HIP1 Satellite is Italy, Japan, and Singapore."]
[7.222568035125732, 4.303788661956787, "The Carries of the Beijing-3B Satellite is Larger and higher resolution optical imager."]
[6.84253454208374, 4.056326389312744, "The Imaging Sensor of the ResourceSat-2 Satellite is LISS-3."]
[4.189609050750732, 5.6633453369140625, "The TT&C Uplink of the Spacecraft bus Satellite is 2 kbit/s."]
[11.766234397888184, 1.069948673248291, "The Orbit Transfer Time of the Chang'e-1 Satellite is 8-9 days."]
[4.9985551834106445, -0.14061984419822693, "The Groundbreaking Date of the OneWebSatellites Spacecraft Integration Facility is March 16, 2017."]
[4.491422653198242, 3.619851589202881, "The Developer of the ADAM Data Acquisition and Messaging System is ITR (Institute for Telecommunications Research) at the University of South Australia."]
[6.815941333770752, 8.497045516967773, "The Spatial Resolution of the MSU-SK Radiometer is 170 m (in VIS) and 600 m (TIR)."]
[11.708460807800293, 1.2147904634475708, "The Hibernation Mode of the EDM Lander is Yes."]
[7.895398139953613, 7.9122843742370605, "The Dynamic Range of the Instrument Sensor is >100."]
[8.066129684448242, 4.166766166687012, "The Planned Image Resolution Improvement of the Satellite Constellation Satellite Constellation is 70 centimeters."]
[5.011620044708252, 7.107013702392578, "The Objective 1 of the CITRIS Receiver is Reconstruct real-time phase screens for multiple frequency scintillation estimation."]
[8.478357315063477, 2.071641445159912, "The Communication Status During Upgrade of the Voyager 2 Spacecraft is Still be able to receive science data from Voyager 2."]
[7.357522487640381, 9.950454711914062, "The Frame Rate of the Hyperion Imaging Spectrometer is 225 Hz."]
[6.839285850524902, 3.302382707595825, "The Hosting of the HISats Satellite is In an unused recess on the host spacecraft."]
[9.174403190612793, 10.382139205932617, "The Filter Diameter of the LWIR Camera Camera is 15.5mm."]
[9.388579368591309, 1.5679171085357666, "The Global Revisit Opportunities of the NigeriaSat-2 Satellite is At least every 2 days."]
[10.73120403289795, 10.269532203674316, "The Purpose of the PHA HiLRS is Monitor the effect of high energy particles on spacecraft electronics."]
[7.106988906860352, 2.320702314376831, "The URL of the IceCube Satellite is https://icecube.wisc.edu."]
[4.711151599884033, 2.2408130168914795, "The Quantity of the AeroCube-5a and -5b CubeSats is 2."]
[7.139435291290283, 2.331049919128418, "The URL of the IceCube-Gen2 Satellite is https://arxiv.org/pdf/2008.04323.pdf."]
[11.04851245880127, 2.8009259700775146, "The Length of the Ganges River River is Over 2400 km."]
[8.323528289794922, 4.860866546630859, "The Observation of the Satellite Observation Satellite is Wave-particle interactions in Earth\u2019s magnetotail."]
[6.115635395050049, 2.78123140335083, "The Assets Ownership Transfer of the Copernicus Space Component Satellite Component is Defined in Agreement."]
[9.439778327941895, 9.375483512878418, "The Focal Length of the Lenses Optical System is 2.6 m."]
[7.7732930183410645, 10.736358642578125, "The Logarithm Resolution Adjustment of the RFA Computer Signal Processing Device is 8 bits."]
[9.963204383850098, 9.545124053955078, "The Data Usage of the SAGE-III on ISS Satellite Instrument is Help to re-institute aerosol measurements crucial for more-accurate, long-term climate and O3 concentration and distribution models."]
[6.654078483581543, 2.3406848907470703, "The URL of the TeleSupport-2-bis Onboard System is http://www.prismasatellites.se/filearchive/3/3615/2005%20tsuengelsk.pdf."]
[7.102991104125977, 6.62619161605835, "The Integration Date of the TROPOMI Space Air Quality Sensor is May 26-30, 2014."]
[9.237290382385254, 4.06026029586792, "The Gouge Dimensions of the SMART-1 Satellite is 4 m-wide and 20 m-long."]
[7.875469207763672, 1.6782227754592896, "The Launch Date of the ExoMars 2020 Spacecraft is 2022."]
[7.584079265594482, 1.4007501602172852, "The Response Date of the NASA Organization is July 10, 2015."]
[10.841815948486328, 4.180117607116699, "The Mission Purpose of the CHEOPS Satellite is Characterize exoplanets orbiting nearby stars."]
[9.17239761352539, 8.090782165527344, "The Cadence of the 3 He Spectrum Measurement is Up to roughly 20 MeV/nuc."]
[7.051743030548096, 4.500112056732178, "The Measurement Domain of the EXPORTS Satellite Mission is Ocean."]
[10.25603199005127, 2.936704397201538, "The Altitude of the Orbit Satellite is ~1075 km x 1089 km."]
[7.295293807983398, 9.021560668945312, "The Swath Width of the Instrument Spectrometer is 19.3 km."]
[1.7284877300262451, 4.178400039672852, "The Maximum Efficiency of the Solar Cell Assemblies Power Source is 25%."]
[9.44529914855957, 4.861256122589111, "The Slew Rate of the Spacecraft Satellite is 15\u00ba / minute."]
[3.1497654914855957, 5.300897121429443, "The Solid State Recorder Capacity of the C&DH Command & Data Handling is 4 TB @ BOL and 3.1 TB @ EOL."]
[3.9283339977264404, 6.074438095092773, "The Data Rate of the Reception Station Ground Station is 16 Mbit/s."]
[7.671658039093018, 5.588240623474121, "The Data Usage of the TRUTHS Satellite is Global hyperspectral data."]
[11.040863990783691, 4.100709915161133, "The Mission Prediction of the Roman Space Telescope Space Telescope is Find 100,000 Transiting Planets."]
[8.115548133850098, 1.291888952255249, "The Image Capture Date of the Solar Dynamics Observatory Satellite is March 31, 2022."]
[9.24380111694336, 7.148571968078613, "The Height of the Langmuir Probe Assembly Probe is 10 mm."]
[9.201553344726562, 3.204848051071167, "The Orbit Type of the Aalto-1 Satellite is Sun-synchronous near-circular orbit."]
[6.263413906097412, 9.868021965026855, "The Mass of the 4-band CCD Imager Instrument is 15 kg."]
[5.034557819366455, -2.3819236755371094, "The Affiliation of the Giacomo Peretto Engineer is Unknown."]
[7.289305210113525, 1.6554622650146484, "The Tandem Mission Completion Date of the ERS-1 and ERS-2 Satellites is May/June 1996."]
[6.476468086242676, 9.00906753540039, "The Size of the LALT-E Electronics is 241 mm x 301 mm x 88 mm."]
[8.46928882598877, 2.17362117767334, "The Current Location of the Voyager 2 Spacecraft is Beyond the heliopause."]
[9.231224060058594, 9.632694244384766, "The Photodetector Resolution of the Optical Head Optical Device is 1280 x 1024 pixels."]
[4.1481852531433105, 5.733779430389404, "The S-band Downlink of the UoSAT-12 Satellite is 2."]
[7.466404914855957, 8.222685813903809, "The Altitude Range of the Methane VMR Measurement Device is 40 - 95 km."]
[10.475665092468262, 2.7818753719329834, "The Perigee of the Molniya Orbit Orbit is 1043 km."]
[3.4925458431243896, 4.699221134185791, "The Memory of the AIM Reconfigurable Computing Hardware Device is 512 k x 16 SRAM for instructions and data for the microcontroller."]
[9.778564453125, 5.3271803855896, "The Propulsion System of the AOCS Attitude and Orbit Control System is Bi-propellants."]
[1.8244142532348633, 3.991250991821289, "The Solar Array Type of the EPS Electric Power Subsystem is Triple-junction solar cells."]
[10.561372756958008, 8.498163223266602, "The Observable of the COR1 Coronagraph1 imager is K-corona and CMEs."]
[8.575532913208008, 9.626218795776367, "The Dynamic Range of the EXI instrument Imaging Instrument is 12 bit, 13,500 e full well."]
[8.667737007141113, 1.9564826488494873, "The Ground Control of the James Webb Space Telescope Space Telescope is Space Telescope Science Institute in Baltimore."]
[9.354253768920898, -0.7959703803062439, "The Launch Date of the SOCRATES Microsatellite is May 24, 2014."]
[5.9437689781188965, 3.006713628768921, "The Mission Lead of the SORTIE Satellite is ASTRA LLC."]
[5.860363006591797, 6.374317169189453, "The Bandwidth of the CSG-SAR Synthetic Aperture Radar is Programmable."]
[4.113272666931152, 5.626564979553223, "The Percentage of InSight EDL Data Sent of the MarCO-B Satellite is 97%."]
[9.893438339233398, -0.6545043587684631, "The Dimensions of the Microsatellite Satellite is 315 mm x 315 mm x 260 mm."]
[7.427078723907471, 2.6614620685577393, "The Collaboration URL of the Hinode Satellite is http://www.jaxa.jp/article/special/solar-b/1/index_e.html."]
[10.167580604553223, 3.0255537033081055, "The Orbit Altitude of the SPOT 1-5 Satellite is 832 km."]
[11.581220626831055, -1.331343650817871, "The Mass of the Anand Satellite is Less than 15 kg."]
[8.235880851745605, 10.120282173156738, "The GSD of the SLIM6 Line Scan Imager Imager is 32 m."]
[5.067257881164551, 5.489783763885498, "The L-band region of the Inmarsat Satellite Communication is Fourth full-service."]
[9.292952537536621, 1.146769404411316, "The Science Phase Duration of the GP-B mission Mission is 50 weeks."]
[7.374595642089844, -0.6179036498069763, "The Publication Date of the CYGNSS Satellite is 19 June 2018."]
[7.786304473876953, 9.44014835357666, "The Spectral Resolution of the HR Bands (677\u2013686 nm, 740\u2013759 nm and 769\u2013780 nm) Spectral Bands is Principally driven from the aggregated pixel size (140 \u00b5m)."]
[11.375887870788574, 6.662240982055664, "The Detectors Service Unit Status of the IXPE observatory X-ray Observatory is Complete."]
[9.202048301696777, 10.319615364074707, "The CIR Film Type of the Metric Camera Camera is KODAK Aerochrome Infrared Film 2443."]
[11.587326049804688, 2.6639509201049805, "The Type of the Lutetia Asteroid is M-type (metallic)."]
[9.384224891662598, 10.02214241027832, "The Interface of the Google Earth Application is Camera."]
[4.854842185974121, 1.857695460319519, "The Number of Satellites of the Spacety Company is 21."]
[5.356991291046143, 6.5969157218933105, "The Dynamic Range of the Satellite Device Unknown is 3-340 K."]
[3.461493968963623, 5.255433082580566, "The Data Storage of the Spacecraft Satellite is 500 Mbit bus + 2 Gbit fpr payload data at EOL."]
[8.312214851379395, 8.44616413116455, "The URL of the MERTIS Thermal Infrared Spectrometer is https://www.researchgate.net/publication/224798007_Thermal_infrared_spectroscopy_to_investigate_the_composition_of_mercury_-_The_MERTIS_instrument_on_BepiColombo."]
[7.958860397338867, 1.9456032514572144, "The Trace Gas Orbiter (TGO) of the ExoMars Mission is Launched in 2016."]
[6.195927619934082, 2.351917266845703, "The Launch Location of the RASAT Satellite is Orenburg Region, Russia."]
[9.104666709899902, 5.106911659240723, "The Stabilization of the S/C Satellite is Three-axis."]
[6.181922912597656, 0.5731276273727417, "The Launch Date of the CubeSat Satellite is July 21, 2010."]
[6.916275501251221, 4.970456123352051, "The Nitrogen Dioxide Emission Reduction of the Copernicus Sentinel-5P Satellite is Decline of air pollution, specifically nitrogen dioxide emissions, over Italy."]
[5.228909969329834, 5.033608436584473, "The Ground Terminals of the ETS-VIII LRRA Satellite is Portable terminal, Handheld terminal."]
[2.0959081649780273, 4.426265716552734, "The Solar Array Power of the Orion Spacecraft is 11.1 kW."]
[8.384210586547852, 7.809971332550049, "The Funding of the FGS Fine Guidance Sensor is CSA (Canadian Space Agency)."]
[11.347590446472168, 6.108135223388672, "The Observation Date of the Chandra X-ray Telescope is Unknown."]
[8.706424713134766, 3.2489678859710693, "The Centre of Pressure Position of the GOCE Satellite is Behind Centre of Mass."]
[6.700663089752197, 7.176780700683594, "The Presentation Date of the LIDAR Instrument is March 16-20, 2015."]
[6.352477550506592, 5.422432899475098, "The Description of the RO Proposals Payload is Polarimetric Global Navigation Satellite System (GNSS) Radio-Occultation (RO) payload."]
[4.1150593757629395, 5.857041835784912, "The Ka-band Data Rate of the CASCADE Satellite Communication System is Up to 1.4 Gbit/s (QPSK modulation)."]
[7.429488658905029, 1.8025577068328857, "The Presentation Date of the Gravity Probe B Satellite is 23-24 July 1992."]
[10.337387084960938, 4.860635280609131, "The Orbit Transfer Thrusters of the EURECA Spacecraft is Redundant 4 x 21 N hydrazine thrusters."]
[8.303373336791992, 5.130767822265625, "The Location Accuracy of the SPOT-6 Satellite is 19.3 m CE90 @30\u00ba."]
[7.941470146179199, 10.735027313232422, "The Output Resolution of the Detector Sensor is 12 bits."]
[6.698240756988525, 2.235536575317383, "The URL of the GPM Satellite is http://www.esmats.eu/esmatspapers/pastpapers/pdfs/2011/sexton.pdf."]
[3.995570659637451, 6.966951847076416, "The Total payload mass of the Repeater subsystem Communication System is 400 kg."]
[7.416347503662109, 1.1790387630462646, "The Date of the ESA Space19+ ministerial conference Conference is End of 2019."]
[10.298937797546387, 6.249495029449463, "The Energy Resolution of the RHESSI Satellite is One- to a few- keV."]
[1.4539207220077515, 4.96446418762207, "The Power Generation Capability of the SBVR Power Supply is 20.3 kW max."]
[6.828202247619629, 2.6461455821990967, "The URL of the GFO Satellite is http://gfo.wff.nasa.gov/."]
[7.940734386444092, 6.841507911682129, "The Frequency of the Calibration Phases Process is Periodically."]
[6.846116542816162, 0.5620872974395752, "The Launch Date of the Dellingr Satellite is 2017."]
[5.566991329193115, 0.4240706264972687, "The Area Covered of the Saltworks Salt Production Facility is 33,000 hectares (82,000 acres)."]
[9.62166976928711, 7.759230136871338, "The Weight of the Electrons Particle is 2000 times lighter than other particles."]
[8.3150053024292, 3.140756130218506, "The Change DEM Availability of the TanDEM-X Satellite is Mid-2021."]
[8.274699211120605, 3.1049411296844482, "The Conference Presentation Date of the TanDEM-X Satellite is July 22-27, 2012."]
[11.560274124145508, 6.297828674316406, "The Image Capture Dates of the XMM-Newton X-ray Space Observatory is 19-25 January."]
[5.004290580749512, 5.054357051849365, "The Functionalities of the DIS System is 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."]
[10.306746482849121, 7.629357814788818, "The Energy Range of the EPIC Cameras Imaging System is 0.15 to 15 keV."]
[3.5919079780578613, 4.605423450469971, "The Performance Advantage of the FPGA based parallel computing Processing Technology is 100 x."]
[7.177849292755127, 1.7421833276748657, "The Drift Start Date of the ERS-2 Satellite is After the completion of the tandem mission."]
[7.601207733154297, 1.1496530771255493, "The Date of the Autonomous Sciencecraft Experiment Experiment is June 27-29, 2006."]
[8.794976234436035, 3.243529796600342, "The Orbit of the Queqiao Relay Satellite is Halo orbit around the second Lagrangian (L2) point of the Earth-moon system."]
[8.462601661682129, 8.786540985107422, "The Wavelength Range of the Grating Reflection Unit Spectrometer Component is 750nm to 775nm."]
[10.30102825164795, 2.9365248680114746, "The Nominal Altitude of the DubaiSat-1 Satellite is 680 km."]
[4.816318988800049, 1.8368850946426392, "The Number of Satellites of the UrtheCast Satellite Constellation is 16."]
[9.281500816345215, 2.240682601928711, "The Orbital Energy of the BepiColombo Spacecraft is Same as Earth's."]
[5.694337368011475, 3.3307042121887207, "The Technology Demonstrator of the SIMBA Satellite RMIB SIMBA program is Intended."]
[11.08115291595459, 2.414477825164795, "The Mass of the Schiaparelli Module is 600 kg."]
[12.006623268127441, 3.345792055130005, "The Orbit Inclination of the Light-1 Satellite is 51.6\u00b0."]
[7.429468154907227, 8.438668251037598, "The MTF at Nyquist Frequency of the Spacecraft Satellite is > 20% for MS."]
[6.332437992095947, 2.0554416179656982, "The Operator of the G\u00f6kt\u00fcrk-1 Satellite is Turkish Ministry of National Defense."]
[7.227138996124268, 6.529647350311279, "The Instrument of the GeoSTAR Geostationary Synthetic Thinned Aperture Radiometer is Utilizes the same established approach as is being used with the AMSU instrument."]
[9.099332809448242, 5.183557033538818, "The Attitude of the ISS Space Station is Torque Equilibrium Attitude (TEA)."]
[1.8096200227737427, 5.358401298522949, "The Power of the Voltage 5 Digital is 2."]
[11.535587310791016, 4.145282745361328, "The Location of the Ceres Dwarf Planet is Asteroid belt, between the orbits of Mars and Jupiter."]
[10.307866096496582, 2.8930459022521973, "The Perigee Height of the INTEGRAL Satellite is 9,049.6 km."]
[4.160179138183594, 5.9421515464782715, "The Protocol of the UoSAT-12 Satellite is AX.25 (Amateur radio X.25)."]
[8.225554466247559, 8.90158462524414, "The Spectral Resolution of the Observation Instrument Telescope/Spectrograph is <0.6 nm (point source), <1.2 nm (extended source)."]
[9.624610900878906, 6.005458831787109, "The Actuators of the Coarse ADCS ADCS System is Magnetotorquers."]
[7.971473217010498, 10.771855354309082, "The Data Quantization of the Visual Sensor Array Sensor Array is 6 bit."]
[7.856983184814453, -0.09687113761901855, "The Planned Launch Date of the Nauka Laboratory Module is 15 July 2021."]
[11.263648986816406, 5.263538360595703, "The Cone Tilt of the SS 433 Cosmic Object is Periodically tilts slightly toward Earth."]
[10.819476127624512, 5.908816814422607, "The Width of the HXR Flare Ribbons Solar Phenomenon is ~1 arcsec."]
[9.349201202392578, 11.60510540008545, "The Pixel size of the Channel 5 Sensor is 32 km x 32 km."]
[9.512720108032227, 0.550357460975647, "The Operational Lifetime of the KazEOSat-2 Satellite is 7 years."]
[7.013908386230469, 5.231791019439697, "The Accuracy of the Climate Models Computer Models is Agree fairly well with observed data."]
[11.45944595336914, 2.1907732486724854, "The Catcher Compartments of the Hayabusa-2 Sampler Mechanism is Three compartments."]
[8.519381523132324, 6.930629730224609, "The Frequency Range of the NewMag Magnetometer Experiment is 0.1 Hz to 1 kHz."]
[12.04765510559082, 3.2667605876922607, "The Inclination Angle of the Suomi-NPP Satellite is 98.74\u00b0."]
[5.932455539703369, 3.655294418334961, "The Program Management Location of the SSETI Express Satellite is ESA Education Department at ESTEC."]
[4.888462066650391, 1.6851067543029785, "The Number of Substorms Observed of the THEMIS Constellation Satellite Constellation is 57."]
[5.322067737579346, 6.967341423034668, "The Size of the VPU Video Processing Unit is 195 x 120 x 253 mm."]
[7.241954326629639, -0.7534556984901428, "The Constellation Redundancy of the CYGNSS Satellite Constellation is Full."]
[4.865218162536621, 1.8104387521743774, "The Planned Satellite Launches of the ICEYE Satellite Operator is At least eight more satellites in the coming year."]
[7.289975166320801, 7.652167797088623, "The Optics Type of the ALTIUS Instrument Satellite Instrument is Reflective optics."]
[4.266068458557129, 4.592317581176758, "The Manufacturer of the EC Digital Signal Processor is TI."]
[7.016222953796387, 0.6464276909828186, "The Launch Date of the ICEYE Satellite is June 13, 2023."]
[12.113975524902344, 3.2910242080688477, "The Orbit Inclination of the ERBS Satellite is 57\u00ba."]
[5.024454116821289, 4.531721115112305, "The Base Component of the GSCG Ground Station Control System is ESA SCOS2000 NIS."]
[12.100204467773438, 3.2248988151550293, "The Orbit Inclination of the EURECA Satellite is 28.45\u00ba."]
[5.499825954437256, 4.130711555480957, "The Provided through a secure communication channel via VPN of the Real-time network communications Communication Services is Links the SCC of GISTDA to the RTS of NSPO and the SOCC of NSPO to the SBS of GISTDA."]
[4.024931907653809, 5.656800270080566, "The Image Telemetry Link of the SPOT-2 Satellite is 50 Mbit/s at 8 GHz."]
[1.5287481546401978, 4.8666672706604, "The Regulators of the EPS Electrical Power Subsystem is 3.3 and 5 V."]
[4.209774494171143, 2.405632972717285, "The Platform of the SpooQySat Satellite is 3U GomX CubeSat."]
[6.041670799255371, 2.2209417819976807, "The Launch Vehicle of the NigeriaSat-1 Satellite is Kosmos-3M."]
[6.526232719421387, 1.1806381940841675, "The Launch Date of the GOMS-1 Satellite is October 31, 1994."]
[10.436833381652832, 2.624238967895508, "The Apogee Height of the INTEGRAL Satellite is 153,657.2 km."]
[10.202091217041016, 3.1736979484558105, "The Ground Sample Distance of the GHOSt Constellation Satellite Constellation is 8 metres."]
[7.689236640930176, 3.524571657180786, "The Latency of the Satellite Constellation Constellation is Minimum."]
[11.171904563903809, 2.7529616355895996, "The Booster Segments Trip Distance of the SLS Rocket is 2,800 miles."]
[11.791909217834473, 3.3975064754486084, "The Maximum Latitude Coverage of the ISS Satellite is \u00b154.33\u00ba."]
[11.300281524658203, 2.989686965942383, "The Age of the Site Kingfisher Crater is Relatively young."]
[3.268942356109619, 6.017869472503662, "The Power Consumption of the TOTEM SDR SDR Platform is Low."]
[8.983318328857422, 6.911561965942383, "The Power of the PAP Plasma Analyzer is 7 W."]
[6.844423294067383, 8.477591514587402, "The Dynamic Range of Earth Background of the LI Instrument is 0 - 296.5 W/m 2 /\u00b5m/sr."]
[8.24764633178711, 3.1170895099639893, "The Presentation of the TerraSAR-X, TanDEM-X, EnMAP Satellites is GSCB (Ground Segment Coordination Body) Workshop."]
[7.824606895446777, 5.415414810180664, "The Accuracy of the NIDEM Elevation Model is High."]
[8.91934871673584, 3.3223512172698975, "The Orbit of the EO Satellite Satellite is LEO."]
[8.251908302307129, 4.481045722961426, "The MS Resolution at Nadir of the QuickBird-2 Satellite is 2.4 m - 1.8 m (8 bands)."]
[3.932412624359131, 5.524003982543945, "The Spatial Resolution (Playback Mode) of the OCM Data Transmission System is 2.16 km."]
[9.26418685913086, 9.150256156921387, "The FOV (Field of View) of the Telescope Optical Instrument is 41.3 x 41.3 arcmin."]
[8.233099937438965, 1.9590665102005005, "The Mission Extension of the SOHO Satellite is End of 2016."]
[7.845804214477539, 4.074953556060791, "The Daily Imaging Capacity of the PRISMA System Satellite Ground Segment is Up to 200,000 km2."]
[7.259719371795654, 1.024037480354309, "The Launch Date of the Space Weather Mission Satellite is Unknown."]
[7.474373817443848, 0.7148228287696838, "The Launch Date of the NICER-SEXTANT Mission is 3 June."]
[6.2114338874816895, 3.999063014984131, "The Location of the Hertz Chamber Test Chamber is ESA's ESTEC technical center in the Netherlands."]
[10.272233963012695, 2.9814844131469727, "The Reentry Altitude of the First Stage Rocket Stage is 70 km."]
[9.085439682006836, 9.709541320800781, "The Components of the DarkCarb image sensor Photon Detector is Optical elements, detector, temperature sensors."]
[7.818999767303467, 2.5926711559295654, "The International Participants of the ARTEMIS Satellite is The United Kingdom, Canada, and Australia."]
[7.467028617858887, 8.87802791595459, "The Along-Track Resolution of the MLS Spectrometer is 500 km."]
[6.267569065093994, 9.93586254119873, "The Weight of the mvBlueFOX-IGC (200w) Visual Sensor is 80 g."]
[11.107471466064453, -1.201370120048523, "The Design Class of the QSAT Satellite is 50 kg."]
[4.012950897216797, 5.734498977661133, "The Telecommand Uplink Data Rate of the GIOVE-B Satellite is 2 kbit/s."]
[8.119400978088379, 9.915397644042969, "The Pixel Type of the MWIR Imager Imaging Device is MWIR."]
[7.496311187744141, 2.901580333709717, "The Mission Status of the KOMPSAT-2 Satellite is Operational."]
[5.99398136138916, 9.642142295837402, "The Quantity of Proof Masses of the Electrode Housing Box Component is 1."]
[11.473655700683594, 6.336528778076172, "The Discovery Date of the NICER X-ray Pulsar Mission is 10 May 2018."]
[9.097278594970703, 8.29314136505127, "The Actuation Method of the SMA Scan Mechanism Assembly is Inductively using a network of voice coils and magnets."]
[1.5424280166625977, 4.942836761474609, "The Voltage Levels of the Power Regulation System is 5V and 8V."]
[7.392043113708496, 10.071468353271484, "The Function of the Systematic and Radiometric Correction Processor Data Processor is Corrects the raw hyperspectral image (HSI) data for systematic effects and converts them to physical at-sensor radiance values."]
[5.937641143798828, 6.254685401916504, "The SAR Payload Swath Width of the RCM Satellite is 20 - 350 km."]
[6.7974162101745605, 1.7678989171981812, "The Hydrazine Exhaustion of the Envisat Satellite is End of 2010."]
[3.6958653926849365, 6.23365592956543, "The Data Rate of the TT&C Downlink Communication System is 38.4 kbit/s."]
[1.8351095914840698, 4.050024509429932, "The Area of the Solar Panels Power Generation is 2.44 m2."]
[8.939491271972656, 7.2053375244140625, "The Measurement of the WISPR Instrument is SEP-Producing Shocks and CME Drivers."]
[5.901080131530762, 10.85307788848877, "The No of Passbands of the Channel 1 Sensor is 1."]
[7.033721446990967, 0.9694415926933289, "The Launch Date of the IASI-NG Satellite is Unknown."]
[8.55983829498291, 6.483154773712158, "The Magnetic Field Profile of the Current Sheet Magnetic Field Structure is Matched the theoretical prediction."]
[5.61848258972168, 2.4952728748321533, "The Program Purpose of the SBSS-1 Pathfinder Satellite is Develop and initiate operations."]
[10.310157775878906, 7.689504146575928, "The Material of the Baffle Telescope Component is CFRP laminate."]
[8.978019714355469, 4.252135276794434, "The Instrument Module Length of the Resurs-P1 Satellite is About 1 m."]
[7.5163187980651855, 9.34083080291748, "The Spectral Band of the VIS Channel is 0.4 - 1.1 \u00b5m."]
[5.8586015701293945, 8.61426830291748, "The Swath Width of the MWHS-II Microwave Humidity Sounder is 2600 km."]
[8.702431678771973, 3.224047899246216, "The Sampling of the Satellite GEO (Geostationary Earth Orbit) is Excellent sampling of one region of the globe."]
[7.322293281555176, 8.556788444519043, "The Wavelengths of the AVGS Laser System is 808 nm and 850 nm."]
[6.035356521606445, 3.9313199520111084, "The Operations Concept of the Spacecraft Satellite is Unattended with distributed science operations."]
[3.710137128829956, 6.481030464172363, "The Data Transmission Rate of the RF Communications Transmitter is 1 kbit/s FSK modulated in S-band."]
[8.88862133026123, 3.2749223709106445, "The Orbit Type of the Space Station Satellite is Low-Earth orbit."]
[7.139842510223389, 5.196190357208252, "The Emission Sources of the Nitrogen Dioxide (NO2) Gas is Burning of gasoline, coal, and diesel fuel by motor vehicles, power plants, and industrial facilities."]
[7.861385822296143, 0.8775508403778076, "The Splashdown Date of the Orion Spacecraft is Dec. 5, 2014."]
[8.586054801940918, 7.0815653800964355, "The Components of the Plasma Wave Instrument Instrument is Triaxial magnetic search coils, pair of electric dipole antennas, two sweep-frequency receivers, multichannel analyzer, low frequency waveform receiver, wideband waveform receiver."]
[7.417630195617676, 1.429352879524231, "The Expected Data Processing End Date of the MICROSCOPE Satellite is 2019."]
[6.723001956939697, 7.126493453979492, "The Data Availability of the CATS Lidar Instrument is Freely available."]
[9.207839965820312, 5.382836818695068, "The Attitude Control of the GCOM-W1 Satellite is 4 reaction wheels in response to the signal from IRU (Inertial Reference Unit) calibrated by Star Trackers and GPS receivers."]
[7.5084919929504395, 0.8407247066497803, "The Program Launch Date of the Polar Scout Satellite is 11 December 2018."]
[9.488805770874023, 5.493474006652832, "The Attitude Control of the AOCS Attitude Orbit Control Subsystem is 3-axis."]
[7.450265407562256, 3.622969627380371, "The Unknown of the DORIS Satellite System is Unknown."]
[5.717949390411377, 2.5946576595306396, "The Manufacturer of the Fregat Upper Stage is RUAG Space in Sweden."]
[5.787237167358398, 3.891538619995117, "The Flight Control Team Location of the Gaia Satellite is ESA's ESOC mission control center in Darmstadt."]
[10.588831901550293, 2.4950058460235596, "The Orbit Altitude of the HORYU-4 Nanosatellite is ~575 km."]
[8.749842643737793, 6.189320087432861, "The Strength of the Earth's Magnetic Field Natural Phenomenon is 0.5 gauss, 5 x 10-5 tesla."]
[9.617323875427246, -0.6444782614707947, "The Architecture of the Microsatellite Satellite is Single string hardware architecture."]
[4.776801109313965, 0.8749627470970154, "The Capital Raise of the Astrocast Satellite Manufacturer is Up to 50 million Francs."]
[8.171380043029785, 10.231955528259277, "The Total Number of Spectral Bands of the MSU-50 Camera is 6."]
[7.948734283447266, 5.138062477111816, "The Observation Angle of the VSSC Satellite is Constant for all data acquisition at a given site."]
[8.241169929504395, 3.6001274585723877, "The DEM Extraction of the CartoSat-1 Satellite is Not Available."]
[5.381763458251953, 3.96182918548584, "The Operation Center of the EDR-2 European Drawer Rack is CADMOS, the French User Support Operations Centre located in Toulouse, France."]
[6.832403659820557, 0.7061497569084167, "The Launch Contract Date of the 90-satellite constellation Satellite Constellation is January 15, 2019."]
[7.221459865570068, 9.307902336120605, "The Swath Width of the Scanner Assembly Instrument is 800 km."]
[6.411596775054932, 4.729715824127197, "The Level 0 Products of the Sentinel-6 Satellite is 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."]
[9.321393013000488, 6.403170585632324, "The Angular Rate Tolerance of the Procyon Star Tracker is 2\u00b0/s."]
[9.226516723632812, 9.105422973632812, "The F-Number of the Telescope Optical Instrument is 3.1."]
[7.891162395477295, 7.720464706420898, "The Purpose of the PREMOS Instrument is Measure UV solar radiance."]
[7.20374059677124, 8.049726486206055, "The Scanning Time per Image of the VHRR Very High-Resolution Radiometer is 30 minutes."]
[8.95565128326416, 4.565155982971191, "The Look Angle of the ICEYE-X1 Satellite is 11\u00ba."]
[8.718364715576172, 10.6807222366333, "The Large Window Imaging Area Pixels of the CCD Image Sensor is 300 x 300."]
[11.215439796447754, 6.329698085784912, "The Director of the Chandra X-ray Observatory Telescope is Harvey Tananbaum."]
[6.833852291107178, 5.4202070236206055, "The Data Type of the SMAP Satellite is Soil moisture data."]
[8.481125831604004, 6.77351713180542, "The Location of the NewMag Magnetometer Experiment is New South Wales, Australia."]
[7.255252361297607, 4.129948616027832, "The Camera Data of the PSSCT-2 Satellite is Used for Understanding."]
[6.229256629943848, 6.487152099609375, "The Radar Frequency of the SeaWinds Scatterometer Scatterometer is 110 W pulse at 189 Hz pulse repetition frequency (PRF)."]
[9.974979400634766, 4.171851634979248, "The Propulsion of the LightSail Satellite is Solar sailing."]
[9.81242847442627, 7.856247425079346, "The Energy Measurement Range for Particles of the Telescope 1 Solid-State Telescope is 1.6-12 MeV/n."]
[3.584909200668335, 6.068981170654297, "The Channel Data Rate of the Communication System Data Transmission is 310 Mbit/s."]
[4.0929460525512695, 3.158763885498047, "The Data path diversity of the Open5GCore Rel. 4 5G Core Network is Supporting local offloading and backhaul control."]
[8.183542251586914, 8.46528148651123, "The Optical Path of the IASI-NG Interferometer is Two opposite prisms moving synchronously with the OPD change."]
[6.563494682312012, 0.5878039598464966, "The Reentry Date of the TechEdSat-1 Satellite is May 5, 2013."]
[10.278975486755371, 2.9390063285827637, "The Orbit Altitude of the Optsat-3000 Satellite is 720 km."]
[10.546923637390137, 7.57452917098999, "The Prism Material of the LAGEOS Satellite is 422 fused silica glass, 4 germanium."]
[6.7367634773254395, 8.514140129089355, "The Resolution of the MWR Radiometer is 40 km."]
[4.937046527862549, 7.431826591491699, "The Data Rate of the DH Data Handling Component is 4.2 Msample/s."]
[8.451455116271973, 8.315757751464844, "The Type of the Detector Instrument is 2D microchannel plate."]
[4.172901630401611, 7.261929988861084, "The Mass of the X-band Transmitter Transmitter is 2.7 kg."]
[7.157470703125, 2.818344831466675, "The Ocean Surface Resolution of the SWOT Satellite is 10 times current technologies."]
[7.443056583404541, 6.835190296173096, "The Image Capture Date of the DESIS Instrument is 13 January 2020."]
[9.205473899841309, 5.235119342803955, "The Attitude Control of the S/C Satellite is 3-axis stabilization with four reaction wheels and three torque rods as actuators."]
[8.684416770935059, 6.31261682510376, "The Transverse Propagation of Wave-like Drift Perturbations of the Plasma Drifts Phenomenon is Account for a phase difference between local maxima in the plasma drift and the plasma density."]
[7.733554840087891, 2.486269235610962, "The Collaboration Start Date of the NISAR Earth Observation Satellite is September 30, 2014."]
[9.0266695022583, 1.0308459997177124, "The Operation Duration of the LRO Satellite is 9 years."]
[5.764256954193115, 2.9169161319732666, "The Ground Station of the LightSail Satellite is Cal Poly San Luis Obispo."]
[8.030948638916016, 4.233059883117676, "The Data Resolution of the ICEYE-X1 Satellite is 10 x 10 meters."]
[1.9131580591201782, 4.499319553375244, "The Small Size of the DC-DC converter Power Converter is 95 mm x 60 mm x 19 mm."]
[4.310578346252441, 4.905447006225586, "The Protocol of the RF Communications Communication Subsystem is CCSDS compatible."]
[9.131888389587402, 5.7893195152282715, "The Sensor Subsystems of the SEEDS-2 Satellite is 3-axis geomagnetic sensors, 3-axis gyro sensors, temperature sensors, solar battery cell galvanometers, and voltage sensors."]
[4.4716477394104, 4.292434215545654, "The Subsystems of the Instrument Electronics Assembly Electronics is Instrument controller, Detector readout electronics, HVPS, LVPS."]
[10.228340148925781, 2.9333372116088867, "The Altitude of the Satellite Constellation Satellite is About 500 km."]
[12.110247611999512, 3.292649745941162, "The Inclination of the KOMPSAT-3A Satellite is 97.513\u00ba."]
[6.321053504943848, 0.6774881482124329, "The Development Timeline of the GHGSat-D Satellite System is Spring 2013 to Summer 2015."]
[8.590106964111328, 3.0316929817199707, "The Dark-Adapted Experiment of the Apollo 9 mission Space Mission is Unknown."]
[7.909578800201416, 5.792539596557617, "The Time Synchronization of the Spacecraft Plug-n-Play Avionics (SPA) Standards is One pulse per second (1PPS) signal."]
[1.147216796875, 3.8636741638183594, "The Power Consumption of the XI-IV Picosatellite is Average consumption of 620 mW."]
[3.7773828506469727, 4.460384845733643, "The CPU of the OBC On-Board Computer is ERC-32."]
[9.940324783325195, -0.772744357585907, "The Operational Life of the Kestrel Eye II Microsatellite is Greater than one year in low earth orbit."]
[7.255433082580566, 2.628777503967285, "The Development Status of the TRUTHS Mission is Preliminary design phase."]
[9.347137451171875, 4.2120513916015625, "The Span of the Spacecraft Satellite is 14.67 m."]
[3.631173610687256, 6.324831008911133, "The Downlink Data Rate of the RF Communications Communication System is 4.8 kbit/s."]
[6.611434459686279, 3.427701711654663, "The Payload of the MPQ442 Satellite is OrbitView."]
[9.761636734008789, 3.960085153579712, "The Length of the Kurushima Kaikyo Bridge Bridge is 4,015 meters (13,173 feet)."]
[6.783228874206543, 0.38087281584739685, "The Launch Date of the GF-3 Satellite is 10 Aug 2016."]
[9.85838794708252, 8.376105308532715, "The Celestial Sphere Coverage of the Telescope Optical Instrument is 30% for > 197 days."]
[3.4603121280670166, 5.256939888000488, "The Data Stream Treatment Capacity of the PLCDHS Data Handling System is 48 Mbit/s."]
[7.933494567871094, 5.4608588218688965, "The Ocean Current Speed Accuracy of the Satellite System Earth Observation is 0.2 m/s."]
[10.350613594055176, 5.114473342895508, "The Xenon Pressure of the EPTA Electric Propulsion Thruster Assembly is 150 bar BOL."]
[6.296219348907471, 0.5857542157173157, "The Launch Date of the CubeSat - Launch 4 Satellite is 17 April 2006."]
[5.964548110961914, 5.8416666984558105, "The Reflector Aperture of the Biomass Satellite is 12 m circular projected aperture."]
[8.468384742736816, 5.610152721405029, "The Interplanetary Vector Magnetic Field Measurement Accuracy of the DSCOVR Satellite is \u00b11 nT."]
[5.969028472900391, 2.05532169342041, "The Launch Vehicle of the DubaiSat-2 Satellite is Dnepr."]
[4.650566577911377, 4.708641529083252, "The Unknown of the Direct Readout Data Users Organizations is Multiple."]
[10.535089492797852, 6.042897701263428, "The Technology of the Micro-gravity experiment Experiment is Important for improving the quality of crystals."]
[7.1490960121154785, 8.839941024780273, "The Spectral range of the VIRR Visible and Infrared Radiometer is 0.43-12.5 \u00b5m."]
[5.2336015701293945, 4.837646007537842, "The TT&C Station of the Ground Segment Satellite Ground Segment is Kiruna."]
[9.321128845214844, -0.6326491832733154, "The Project Management Importance of the AzTechSat Nanosatellite is Main step for successfully completing any project."]
[8.18796443939209, 1.0370609760284424, "The Image Capture Date of the Small Monitor Camera Camera is April 16, 2018."]
[3.8485376834869385, 4.051045894622803, "The Mass and Volume of the Core-DHS Avionics Module is Reduced."]
[7.162346363067627, 1.26679527759552, "The Meeting Date of the EarthCARE Mission is April 19, 2017."]
[7.3405866622924805, 2.1779391765594482, "The Conference Presentation Date of the RISESAT Satellite is August 13-16, 2012."]
[1.7627590894699097, 5.334286689758301, "The Power of the Voltage 4 Modulator is 1.38."]
[9.63963794708252, 8.726855278015137, "The Design of the Imaging Subsystem Telescope is Dall-Kirkham."]
[7.257278919219971, 6.984599590301514, "The Caption Author of the VIIRS Imaging Radiometer is Adam Voiland."]
[7.34544563293457, 2.595644474029541, "The URL of the Electron Tunneling Infrared Detector Detector is http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910005078_1991005078.pdf."]
[4.031531810760498, 1.2038774490356445, "The Mission Type of the MidSTAR-1 Satellite is Non-EO."]
[5.603619575500488, 2.8925836086273193, "The Manufacturer of the BILSAT-1 Satellite is BILTEN."]
[4.792109489440918, 0.8974087238311768, "The New Fundraising Goal of the Inspiration4 Mission is $200 million."]
[11.858752250671387, 1.0080519914627075, "The Microprocessor Core of the Chang'e-4 Mission is LEON2-FT."]
[6.0396199226379395, 6.53181791305542, "The Polarization of the CSG-SAR Synthetic Aperture Radar is Single, Dual, Quad."]
[6.207375526428223, 4.546299457550049, "The Satellites of the MHS Instrument is NOAA-N (NOAA-18) and NOAA-N' (NOAA-19)."]
[8.696672439575195, 8.05649185180664, "The Other Components of the DOSTEL Radiation Detector is Two PIN diodes fixed to the one print board and mounted towards the other two directions."]
[5.708940505981445, 1.5591256618499756, "The Launch Type of the ORS-6 Satellite Mission is Commercial rideshare."]
[8.138442039489746, 3.288355588912964, "The Data Processing Method of the TanDEM-X Satellite is Special algorithms that first evaluate each image individually and then combines them to form a global map."]
[9.735355377197266, 9.44800853729248, "The Swath Width of the IRIS Instrument Spectral Scanner is 50 km."]
[9.061396598815918, 9.249069213867188, "The Field of View of the FOV Spectrometer is 4.2\u00ba."]
[7.485218048095703, -0.252083420753479, "The Departure Date from ISS of the Kounotori-6 Cargo Ship is Jan. 27."]
[8.950292587280273, 9.303351402282715, "The Function of the Imager Device is Regulate the temperature of the metering struts."]
[11.66653060913086, 2.608696460723877, "The Diameter of the Secondary Body Asteroid is 160 m."]
[9.139755249023438, 0.773146390914917, "The Time in Orbit of the Aeolus Satellite is 20 months."]
[4.056084156036377, 1.2078697681427002, "The Mission Type of the CXBN-2 Satellite is Non-EO."]
[5.607547283172607, 6.866080284118652, "The Peak RF Power of the SAR antenna Antenna is 1.8 kW."]
[2.977088451385498, 6.625491619110107, "The Power of the TxU Transmitter Unit is 26 W."]
[4.033199310302734, 5.726543426513672, "The Safe Mode Data Rate of the LunaH-Map Satellite is 62.5 bit/s."]
[6.859217166900635, 4.942835807800293, "The Type of the Imager Satellite Instrument is Pushbroom with TDI capability."]
[6.7123212814331055, 2.9157187938690186, "The Technology Transfer Program of the SOHLA-1 Satellite is Ongoing."]
[6.0807390213012695, 3.0021963119506836, "The Provider of the RS2000 Spacecraft is NASA."]
[4.0862298011779785, 4.529545307159424, "The Secure Commands of the DCU Data Control Unit is OTAR (Over-The-Air-Rekeying), key integrity checks and key disabling."]
[7.7024946212768555, 7.174886703491211, "The Manufacturer of the TEMPO Instrument is Ball Aerospace."]
[7.277074337005615, 0.955687940120697, "The Acquisition Completion Date of the ICON Satellite is 6 June 2018."]
[6.685032844543457, 1.176224708557129, "The Satellite Launch Date of the Capella Space Company is December 2018."]
[5.957949161529541, 6.109950542449951, "The Multi-Look of the Non-Capella radar SAR System is 1."]
[8.987527847290039, 2.745605945587158, "The Operational Start Date of the GCOM-W1 Satellite is Mid-2013."]
[6.961620330810547, 0.44877126812934875, "The Launch Date of the SPOT-4 Satellite is March 24, 1998."]
[6.722372531890869, 7.151850700378418, "The Receiver Telescope Type of the DIAL Instrument LIDAR is Cassegrain."]
[10.540188789367676, -1.050878643989563, "The Mass at Launch of the PARASOL microsatellite Satellite is 120 kg."]
[2.1724414825439453, 3.8405985832214355, "The Solar Array of the Orion Spacecraft is Four wings of three panels."]
[7.503223419189453, 2.210279703140259, "The Contact Email of the eoPortal Website is eoportal@symbios.space."]
[5.875877380371094, 5.230882167816162, "The Navigation Signal Provider of the GPS satellites Satellite is Broadcast navigation signals."]
[8.170143127441406, 8.350648880004883, "The Architecture of the UVNS Spectrometer is Modular."]
[5.673724174499512, 9.138998031616211, "The Power Consumption of the Instrument Optical Bench is 32 W."]
[7.801540851593018, 10.176124572753906, "The Pan of the Pushbroom imager Spectral Band is 0.45-0.9 \u00b5m."]
[6.238749980926514, 9.815860748291016, "The Mass of the Imager Satellite Instrument is 135 kg."]
[8.807307243347168, 0.6041076183319092, "The Duration of the Crew-1 Mission is Six-month."]
[9.451858520507812, 0.537239670753479, "The Design Life of the ERBS Satellite is 2 years."]
[4.564544200897217, 6.988502502441406, "The Frequency of the W-band Band is 77 GHz."]
[8.150167465209961, 7.816479206085205, "The Bacteria Test Subject of the Biofilms Experiment is Staphylococcus capitis."]
[9.711530685424805, 1.2320597171783447, "The Checkout Period of the FASTRAC satellites Satellite is About two weeks."]
[9.25826358795166, 0.7491271495819092, "The Possible Extension of the SAMPEX Satellite is One year."]
[9.41556453704834, 9.110864639282227, "The Aperture of the Optics Device is 20 mm."]
[8.241724967956543, 1.836704969406128, "The Interstellar Space Survey Start Date of the Voyager 1 Satellite is 11 May 2021."]
[7.221549034118652, 6.9266815185546875, "The Image Date of the VIIRS Imaging Radiometer Suite is 7 April 2022."]
[4.328142166137695, 4.267210483551025, "The Computer Memory Interfaces of the SMEX Satellite Program is Four EIA RS422 Direct Memory Access (DMA) interfaces."]
[10.245200157165527, 4.863798141479492, "The Development Steps Date of the RF-Ion Thrusters RIT Ion Thruster is 2001."]
[8.100625038146973, 0.35397371649742126, "The Launch Date of the BEAM Module is 8 April 2016."]
[10.227534294128418, 5.006645679473877, "The Number of Thrusters of the PROP unit Propulsion System is 4."]
[5.6924519538879395, 6.387943744659424, "The Antenna Beam Surface Incidence Angle of the SMAP Satellite is Approximately 40\u00ba."]
[8.736126899719238, 8.501511573791504, "The Shutter Operation Frequency of the ELENA Instrument is Above 20 kHz and up to 50 kHz."]
[7.1887969970703125, 5.451086521148682, "The Mediating Percentage of the Photosynthesis Biological Process is 90% of carbon and water fluxes in the coupled biosphere-atmosphere system."]
[4.961935043334961, 0.871700644493103, "The Expected Profitability of the Astrocast Satellite Manufacturer is Loss-making for at least 2022 and 2023."]
[10.496895790100098, 6.788783073425293, "The Presentation Date of the CMC Windward TPS and Nose of the IXV Vehicle Thermal Protection System is Oct.12-16, 2015."]
[9.209698677062988, 3.2055468559265137, "The Orbit Type of the OceanSat-1 Satellite is Sun-synchronous near-circular orbit."]
[3.713789939880371, 5.365179538726807, "The Data Throughput of the AIS Data Collection System Data Collection System is 30 MB per day."]
[5.059620380401611, 4.0153069496154785, "The Diagnostic Port Function of the EDSN satellites Satellite is Data interface and battery charging during I&T activities."]
[4.7438740730285645, 0.8422045111656189, "The Satellite Production Cost of the Satellogic Satellite Imaging Company is One-tenth the cost."]
[6.814142227172852, 3.9525351524353027, "The Ground Stations of the DEIMOS-2 Satellite is Puertollano, Kiruna, and Inuvik."]
[5.274374961853027, 5.62780237197876, "The Hardware of the FFRF Subsystem Relative Positioning System is One terminal and up to 4 sets of antennas on each satellite."]
[9.741148948669434, 4.91219425201416, "The Firing Duty Cycle of the X-axis Bang-Bang Maneuver Satellite Maneuver is 90%."]
[6.636908531188965, 8.864169120788574, "The Performance of the CSS Instrument is \u00b10.115\u00ba."]
[7.124645233154297, 3.1938323974609375, "The Communication Status of the YES Satellite is Not Re-established."]
[8.769953727722168, 9.927398681640625, "The Scale of the Image Data is Indicated on the image."]
[7.246728420257568, 2.643322229385376, "The URL of the SwRI-led team Team is https://www.swri.org/press-release/high-fidelity-images-sun-atmosphere?."]
[9.248885154724121, 4.880670547485352, "The Array Pointing Requirement of the IXPE Mission Satellite Mission is Within \u00b125 degrees of sun normal."]
[9.571734428405762, 3.935478687286377, "The Relative Position Measurements Accuracy of the CanX-4&5 Satellite is Centimeter-levels."]
[5.008493423461914, 3.5486669540405273, "The Function of the Single-function satlets Satellite Subsystem Type is Incorporate one individual satellite subsystem function per satlet."]
[10.170896530151367, 7.831789493560791, "The Shape of the Baffle Telescope Component is Closely follows the RX beam."]
[9.472851753234863, 10.520508766174316, "The Frame Format of the Iris Video Camera Camera is 4096 x 20 pixels (UHD); 1920 x 1080 pixels (HD)."]
[10.541948318481445, 8.451108932495117, "The Location of the COR-2 Coronagraph is On board NASA\u2019s STEREO-A (Solar and Terrestrial Relations Observatory-A)."]
[10.103857040405273, 6.863619804382324, "The Thermal Design of the Antennas, Solar Array, Sun Sensors, MLI Satellite Components is Dedicated high temperature technologies."]
[7.325981140136719, 2.6839447021484375, "The URL of the Chandra Satellite is http://chandra.harvard.edu/press/18_releases/press_101218.html."]
[11.101194381713867, 4.782666206359863, "The Speed of the Solar Particles Space Phenomenon is Fastest."]
[8.05724811553955, 7.383475303649902, "The Input Spectral Radiance Sources of the ICU Internal Calibration Unit is The Sun (ICU_S mode) or by Internal Sources (ICU_IS mode)."]
[6.696816444396973, 1.7322086095809937, "The Owner of the RapidEye Earth Observation Constellation is BlackBridge."]
[9.304673194885254, 8.252957344055176, "The Threshold of the High LET Detector Detector is 2 MeV."]
[4.81101131439209, 0.9083388447761536, "The Investment of the IOD Program Program is \u01531.5 million."]
[6.996898651123047, 3.41544771194458, "The Development Status of the CIMR Satellite Mission is Proposed."]
[4.090602397918701, 5.79335355758667, "The Data Rate of the OPAL Satellite is 9.6 kbit/s."]
[1.894680142402649, 4.145395278930664, "The Minimum Power of the Solar Arrays Power Source is 4kW."]
[8.501986503601074, 9.259554862976074, "The Number of IFOVs of the Spectrometer Spectrometer is 3 x 3 at 14 km diameter for each band."]
[5.035496711730957, 4.318247318267822, "The Functionality of the Ground Software Architecture System is Automatic query and validation of real-time telemetry, downloading stored spacecraft telemetry, and command and control of the platform and its experiments."]
[9.733749389648438, -0.6770372986793518, "The ACS Development of the Chibis-M Microsatellite Satellite is Unknown."]
[7.210368633270264, 5.011777877807617, "The Applications of the Optical Payload Payload is Monitoring plankton blooms to changes in the polar ice caps."]
[6.6055989265441895, 1.3398269414901733, "The Calibration Conference Date of the GOMS Geostationary Operational Meteorological Satellite is March 15\u201319, 1999."]
[7.423593521118164, 7.308017730712891, "The Mission of the COWVR Radiometer is Space Test Program-Houston 8 (STP-H8)."]
[11.687314987182617, -1.3041601181030273, "The Total Mass of the TiPS Satellite is 54 kg."]
[9.368125915527344, 1.155275821685791, "The Duration of the Request for Proposal Process is 12\u2013 to 18\u2013month period."]
[6.0522284507751465, 2.95528507232666, "The Integration of the OCSE Satellite is Minotaur rocket."]
[6.697018623352051, 6.138150691986084, "The Measurement Category of the ISS-RapidScat Instrument is Ocean surface winds."]
[6.244176864624023, 0.7995112538337708, "The Mission Timeframe of the RAVAN Satellite is Six months."]
[6.434770584106445, -0.6964683532714844, "The Clock 1 Function of the QZS-1 Satellite is Generating positioning signals."]
[4.301065444946289, 6.693570137023926, "The Frequency Range of the Receiver Communication System is 7145 to 7235 MHz."]
[7.807356834411621, 3.7625858783721924, "The Equipment Health of the Satellite Spacecraft is Nominal."]
[8.194353103637695, 5.270447731018066, "The Science Objective of the ELFIN Satellite is Identify the magnetospheric source location of ionospheric field aligned currents (FACs), in relation to tail boundaries."]
[9.092755317687988, 6.413012981414795, "The Function of the GYRO Inertial Sensor is Pick up the resulting angular rates of the system."]
[7.430418968200684, 7.447972297668457, "The Data Collection Duration of the OMI Ozone Monitoring Instrument is Over a decade."]
[8.26030158996582, 3.5654773712158203, "The Star Scanner of the ERG Satellite is Spin-type."]
[7.640506267547607, 1.8337788581848145, "The Publication Date of the System Concept for Wide-Field-Of View Observations of Ocean Phenomena from Space Publication is 1987."]
[7.505605220794678, 8.067790031433105, "The Altitude Range of the SOFIE Instrument is 40-95 km for T, 55-95 km for O3, 20-95 km for H2O, 20-75 km for CH4."]
[8.178943634033203, 8.73250675201416, "The Configuration of the NIRISS Near-Infrared Slitless Spectrometer is Grisms and filters optimized for first-light science and exo-planet observations."]
[9.9481782913208, 5.323143005371094, "The Pressure of the Airtight Vessel Satellite Component is 1200 mbar."]
[10.360784530639648, 2.7300546169281006, "The Altitude of the Beijing-1 Satellite is 686 km."]
[4.8933258056640625, 12.091156959533691, "The Integration Time of the Responsivity Measurement Instrument is Almost cancel the noise on the measurements."]
[5.035922050476074, 5.66161584854126, "The Receiver Type of the Satellite Spacecraft is Dual-frequency."]
[10.292885780334473, 6.8359785079956055, "The Design Type of the TCS Thermal Control Subsystem is Passive and Active."]
[9.414382934570312, -0.5937764048576355, "The Mission Goal of the Nanosatellite Satellite is Micro imaging system, GPS receiver, MEMS based IMU."]
[5.3940958976745605, 1.3340989351272583, "The Deployment Services of the NanoRacks LLC Company is Small satellites."]
[8.84099292755127, 5.209602355957031, "The Attitude Subsystem Knowledge of the Spacecraft Satellite is 0.1\u00ba (3\u03c3)."]
[6.933077812194824, 3.3204360008239746, "The Unknown of the Space Environment Data Acquisition Equipment Data Acquisition Equipment is Unknown."]
[6.768034934997559, 2.823460340499878, "The Measurement Category of the Kolibri-2000 Satellite is Radiation budget, Gravity, Magnetic and Geodynamic measurements."]
[6.507367134094238, 6.246085166931152, "The Function of the OSCAT-3 Radar Scatterometer is Measure wind speeds and vectors at sea level."]
[6.760970115661621, 0.8104616403579712, "The Test Date of the Narrow-Band IoT Technology is 17 October 2019."]
[6.693355083465576, 3.268627882003784, "The Software of the HISat Satellite is Enables HISats to be aggregated together informationally so that satlet resource exposure and sharing is transparent to the operation of the system."]
[6.317427635192871, 3.5081193447113037, "The Science Payload Sensor Type of the Neutron-1 Satellite is Elpasolite sensor."]
[3.4787635803222656, 6.287971019744873, "The Data Rate from FPGA to S-band transmitter of the Transmission Module FPGA Module is 1 Mbit/s."]
[8.430851936340332, 0.162334606051445, "The Operational Period of the ISS Space Station is Until 2030."]
[6.976963043212891, 7.402613162994385, "The Percentage of Components with No New Technology of the Instrument Assembly System is 80%."]
[8.293238639831543, 8.58446216583252, "The Type of the Spectrographs Optical Instrument is Aberration-corrected Offner-type."]
[7.910355567932129, 8.074357032775879, "The Resolution of the MGF Instrument is ~0.1 nT."]
[3.8268489837646484, 6.480064392089844, "The Encryption of the Transceivers Communication Device is 128 AES."]
[6.094295024871826, 6.5151286125183105, "The Polarisation of the CSG-SAR Satellite is Dual."]
[9.520215034484863, 8.564901351928711, "The Components of the SOT Telescope is OTA (Optical Telescope Assembly), FPP (Focal Plane Package)."]
[7.220364570617676, 6.332620620727539, "The Deep-Space Calibration of the WindSat Radiometer is Not provided."]
[8.31297779083252, 10.329532623291016, "The Linearity of the PMC-2 Imagers Imaging System is Better than 3%."]
[4.904354572296143, 9.178365707397461, "The Desired Quake Magnitude of the InSight Seismic Experiment for Interior Structure (SEIS) is Bigger than 4.0."]
[4.690769672393799, 4.460229873657227, "The Cooperation Paradigms of the Multisensory feature Data Management is Federation and Expansion."]
[5.938417911529541, 7.6167707443237305, "The Material Used for Signal Amplification of the ATMS Instrument is Indium Phosphide."]
[8.7813138961792, 8.910558700561523, "The Field of View, horizontal of the Instrument Spectrometer is 24\u00ba."]
[7.796610355377197, 9.17364501953125, "The Spectral Range of the HR Spectrometer Spectrometer is 740\u2013780 nm."]
[7.091377258300781, 0.8839839100837708, "The Launch Date of the FireBird Mission is April 8, 2013."]
[6.685187339782715, 8.260878562927246, "The Maximum Number of Optical Pulses in the FOV of the LI Instrument is 25 in 1 millisecond, 800 in 1 second."]
[11.365825653076172, 6.552295684814453, "The I&T Start Date of the IXPE observatory X-ray Observatory is March 2020."]
[3.198505163192749, 5.902599811553955, "The Data Processing Time of the C3S Command, Control and Communications Segment is Less than 30 minutes."]
[4.734415531158447, 5.627682685852051, "The Communication System of the CAPSTONE Satellite is S-band telecommunication system."]
[6.501218795776367, 1.015356421470642, "The Launch Date of the GOES-S Satellite is March 2018."]
[4.21436882019043, 4.482866287231445, "The Interfaces of the CIU Control and Interface Unit is CAN interface to the bus, PPS interface to the GPS."]
[9.442686080932617, -0.6810216903686523, "The Mission Date of the Kolibri-2000 Microsatellite is April 4-8, 2005."]
[9.015716552734375, 3.979173183441162, "The Structure of the Lander Spacecraft is Truncated pyramid around a cylinder."]
[6.077733516693115, 9.233016014099121, "The Mass of the MI Radiometer Instrument is 139 kg."]
[11.292280197143555, 1.3065240383148193, "The Wake Up Time of the Jade Rabbit-2 Rover is 10:51 a.m. last Thursday (28 February)."]
[8.962430000305176, 8.575355529785156, "The Mounting Method of the Optomechanical System System is Epoxy bed of Stycast 2850FT."]
[11.851560592651367, 1.0158815383911133, "The Photo Transmission Date of the Chang'e-3 Lunar Probe is Dec. 15, 2913."]
[6.719331741333008, 1.4394358396530151, "The Presentation Date of the RapidEye Earth Observation Constellation is Oct. 4-8, 2004."]
[10.995905876159668, 3.444089651107788, "The Number of Orbits around Jupiter of the Juno Spacecraft is 35 times."]
[10.968025207519531, 4.021241664886475, "The URL of the Roman Space Telescope Space Telescope is https://www.nasa.gov/feature/goddard/2021/nasa-s-roman-mission-predicted-to-find-thousands-of-transiting-planets."]
[4.498759746551514, 4.59423828125, "The Data Provider of the IDE System is Provides the stream of science data to the C&DHS."]
[7.789219856262207, 10.879157066345215, "The Data Quantization of the Instrument General is 10 bits."]
[9.735150337219238, 8.954497337341309, "The Primary Mirror Diameter of the Optics Assembly Telescope is 200 mm."]
[6.855165958404541, 0.4312867820262909, "The Launch Date of the Resurs-P1 Satellite is May 2015."]
[6.710608959197998, 1.1173673868179321, "The Launch Date of the FalconSAT-3 Satellite is Unknown."]
[6.871809959411621, 3.2244510650634766, "The AIS Status of the AISSat-1 Satellite is Fully operational."]
[8.331174850463867, 3.687910318374634, "The Operational Experience of the Copernicus POD Service Service is Not provided."]
[7.234409809112549, 1.074346899986267, "The Mission Start Date of the Deep Space 1 Satellite is Unknown."]
[9.282776832580566, 1.7548096179962158, "The Update Frequency of the Active Schedule Planning Product is Minimum of once per week."]
[11.3456392288208, 6.850462913513184, "The Purpose of the NICER XTI X-ray Timing Instrument is Observations of neutron stars with high time resolution."]
[2.994901657104492, 6.549619674682617, "The Power of the TRSR GPS Receiver is 7-15 W."]
[7.273096561431885, 1.157939076423645, "The Attitude Control Strategy Presentation Date of the LAPAN-A2 Satellite is April 8-12, 2013."]
[5.036837577819824, -0.1496107280254364, "The Next Satellite Launch Date of the OneWeb Low-Earth-Orbit Broadband Venture is July 1."]
[4.184418678283691, 6.250406742095947, "The Uplink Modulation of the S-band transponder Communication Device is NRZ (Non-Return to Zero) bi-phase modulated synchronously on a 16 kHz subcarrier."]
[11.161764144897461, 6.810221195220947, "The Telemetry of the X-ray Satellite Navigation Navigation System is 40 kbit/s."]
[6.84251070022583, 4.038282871246338, "The Observation System of the SEOSAT/Ingenio Satellite is Combined radar and optical images."]
[5.586909294128418, 3.9554903507232666, "The Location of the MOC Mission Operations Center is MBRSC."]
[8.665157318115234, 6.933091163635254, "The Vector Components Random Error of the Magnetic Field In-Situ Sensor is < 1 nT."]
[9.308714866638184, 6.455058574676514, "The Size of the Star Tracker Attitude Determination Device is 59 x 56 x 31.5 mm."]
[7.176304817199707, 3.432314872741699, "The Status and Instrument Performance of the SUOMI National Polar-orbiting Partnership Satellite is Unknown."]
[7.634199619293213, 8.581990242004395, "The MTF of the Instrument Spectrometer is \u22650.2, \u22650.3."]
[5.037230014801025, 5.392148971557617, "The Antenna Dish Size of the KSAT Ground Station is 3.7 meter."]
[8.515222549438477, 10.671232223510742, "The Power Consumption of the Imager Camera is 1 W."]
[7.185001373291016, 3.955697774887085, "The Operation of the DMC Constellation Satellite Constellation is Can act as a single coordinated instrument if required."]
[11.615922927856445, -1.1934473514556885, "The Mass of the WNISAT-1R Satellite is 43 kg."]
[3.4242935180664062, 4.694574356079102, "The Pin Count of the Virtex-4 FPGA Data Processing Unit is 1140."]
[9.829476356506348, 7.829274654388428, "The Energy Measurement Range for Protons of the Telescope 1 Solid-State Telescope is 0.05 and 25 MeV."]
[6.247916221618652, 3.1431384086608887, "The BAA Framework Name of the NRO National Reconnaissance Office is Framework for Strategic Commercial Enhancements."]
[5.990882873535156, 1.8062355518341064, "The Subsidiary Location of the Spacety Company is Luxembourg."]
[5.988103866577148, 3.072273015975952, "The Partner of the TanSat Satellite Mission is University of Leicester."]
[11.739607810974121, 4.546307563781738, "The Number of Stars of the Pleiades Open Cluster is Several hundred."]
[10.247675895690918, 2.9546942710876465, "The Altitude of the ZY 1-02C Spacecraft is 781 km."]
[2.5006234645843506, 5.230293273925781, "The Power of the RPU Receiver Processor Unit is 36 W."]
[6.667327880859375, 8.495680809020996, "The On-Ground Footprint Range of the MWI Instrument is 50 km down to 10 km."]
[6.533076286315918, 4.173738479614258, "The Payload of the VisionCube-1 CubeSat is Multi-anode photon multiplier tube(MaPMT), a camera, and a real-time image processing engine."]
[2.0663657188415527, 3.855421781539917, "The Solar Panels of the NSat Satellite is 4."]
[7.203693866729736, 4.197373867034912, "The Sensor complement / remarks of the Cosmos-1066 (Astrofizika) Satellite is Exp. payload on Meteor-1 satellite technology,special geophysical experiment (look for artificial light sources on Earth)."]
[8.58593463897705, 1.7136993408203125, "The Launch Date of the James Webb Space Telescope Space Telescope is 25 December 2021."]
[2.042137861251831, 4.175790786743164, "The Solar Panel Power Output of the AprizeSat Satellite is 15 W."]
[7.192086696624756, 9.346758842468262, "The Components of the HISUI Instrument is A multispectral sensor (MSS) and a hyperspectral sensor (HSS)."]
[8.586732864379883, 6.91573429107666, "The Range of the Magnetometer Sensor is \u00b160 \u00b5T."]
[10.096951484680176, 2.4514098167419434, "The Altitude of the KOMPSAT-3 Satellite is 625 km."]
[9.281291007995605, 1.7432149648666382, "The Operations Schedule of the Mission Plan Document is Weekly."]
[6.384023189544678, 8.646784782409668, "The Volume of the RCU Radiometer Calibration Unit is 300 x 240 x 80 mm."]
[5.500063419342041, 4.356448650360107, "The Location of the JPSS Ground System Satellite Ground System is Global."]
[8.521855354309082, 9.314277648925781, "The Type of the FUV Instrument Spectrometer is Off-axis Czerny-Turner."]
[6.463486194610596, 1.7817623615264893, "The Inauguration Date of the Kleos Headquarters Facility is December 14, 2021."]
[7.9835591316223145, 10.262726783752441, "The Stereo Imaging Capability of the WV60 Satellite is Yes."]
[11.748470306396484, 1.7065277099609375, "The Final Stop of the Philae Lander is A few meters away from the bounce."]
[9.450943946838379, 5.9135308265686035, "The Function of the Magnetorquer Attitude Actuation Device is Liberation damping in the event that the gravity gradient boom deployment erroneously causes the patch antennas to settle in zenith pointing attitude."]
[6.073925971984863, 6.10385799407959, "The Spatial Resolution of the SAR Sensor Subsystem SAR Sensor is 20 m x 20 m."]
[9.654117584228516, 0.9154504537582397, "The Orbit Period of the S/C Spacecraft is 6.2 years."]
[8.489874839782715, 3.654919147491455, "The Deployment Repeatability of the RDA Deployment System is Not provided."]
[9.397506713867188, 5.834883689880371, "The URL of the Drag-Free and Attitude Control System Control System is http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=39981."]
[4.043205261230469, 1.1908069849014282, "The Mission Type of the SMART Satellite is Non-EO."]
[6.061047077178955, -0.03876110911369324, "The Launch Date of the Galileo Satellite Navigation System is 22 August 2014."]
[7.091499328613281, 0.8844575881958008, "The First Contact Date of the RASAT Satellite is August 17, 2011."]
[6.50246524810791, 4.5895304679870605, "The Application of the FY-3 (FengYun-3) Satellite is Ocean."]
[5.1474528312683105, 6.14321756362915, "The Mechanism of the HGA Antenna is Two-axis gimbal."]
[3.9444985389709473, 4.323215007781982, "The Data Bus of the C&DH Command & Data Handling is MIL-STD-1553B."]
[7.129621505737305, 8.618451118469238, "The Spatial resolution at nadir of the SBUS Solar Backscattering UV Sounder is 70/10 km."]
[6.446418762207031, 1.100059151649475, "The Contracts Awarded Date of the Joint Polar Satellite System Satellite System is Unknown."]
[9.581146240234375, -0.4346606731414795, "The Mission Status of the Tsubame microsatellite Satellite is Stopped receiving uplink commands."]
[10.414880752563477, 4.864164352416992, "The Propellant Mass of the Propulsion Subsystem Propulsion is 2.3 kg."]
[6.116848468780518, 3.1085872650146484, "The Developer of the Unicorn-2A PocketQube is Alba Orbital UG (Germany)."]
[9.03972339630127, 7.644011974334717, "The Measurement Type of the EIS Sensor is Ion Composition and Angular Distributions."]
[8.512449264526367, 11.011307716369629, "The Total FOV of the Eastman Kodak KLI14403 linear CCD sensor Sensor is 52\u00ba."]
[5.929931163787842, 1.718900442123413, "The Launch Vehicle of the COSMO-SkyMed-1 Satellite is Delta-2."]
[6.356393337249756, 3.560117483139038, "The Role of the COSMIAC Organization is Build the satellite and collect the data from it."]
[7.491344928741455, 7.081491470336914, "The Calibration Data Acquisition of the Mini-RF Instrument is During spacecraft integration and test."]
[7.74954080581665, 9.048135757446289, "The Spectral Resolution of the Instrument Spectrometer is 10 nm, 12.5 nm."]
[6.361629009246826, 8.25199031829834, "The Data Coverage of the AMSU Microwave Radiometer is Up to 50 km."]
[8.400171279907227, 7.248185634613037, "The Dynamic Range of the Electric Field Measurement System Instrument is 80 dB."]
[9.156578063964844, 4.305335521697998, "The Solar Array of the Spacecraft Satellite is 10.6 m2."]
[7.2502336502075195, 1.2345274686813354, "The Announcement Date of the Water mission Satellite Mission is Sept. 3, 2010."]
[6.186955451965332, 6.61260461807251, "The Interruption Period of the S-193 Radar System is 4-year and 30-day."]
[9.282017707824707, 5.342695713043213, "The Actuation Type of the Canopus Pipper Satellite is Magnetic torque coils."]
[2.0545172691345215, 3.89388108253479, "The Power Source of the PhoneSat-2.5 Satellite is Solar cells."]
[1.6833027601242065, 4.286281585693359, "The Function of the EPS board Power Management and Protection is Interface many solar arrays, integrate active solar array maximum power point tracking, protect the battery from under-voltage."]
[7.9068450927734375, 7.3607025146484375, "The Measuring Cadence of the CLARA Instrument Satellite Instrument is 30 s."]
[4.588928699493408, 4.675076961517334, "The Data Products of the DPE Data Processor Element is RDRs (Raw Data Records), Sensor Data Records, EDRs (Environmental Data Products), TDRs (Temperature Data Records)."]
[6.9238200187683105, 4.254135608673096, "The Purpose of the GHOSt Satellite Constellation is Provide enhanced hyperspectral imagery for use in industrial, government, agriculture, environmental and defence sectors."]
[10.320725440979004, 4.935542583465576, "The Test Phases of the IEPS Ion Electric Propulsion System is Dec. 10, 2012."]
[6.9841437339782715, 8.380749702453613, "The IADP of the LI Instrument is 90% for latitude 45\u00ba, 70% as average over the FOV, 40% over EUMETSAT member states."]
[10.412274360656738, 7.596311569213867, "The Composition of the Galinstan Eutectic Liquid Metal Alloy is Gallium, Indium, Tin."]
[6.674159526824951, 2.2088098526000977, "The Presentation of the GPM Satellite is 28th ISTS (International Symposium on Space Technology and Science)."]
[9.233163833618164, 10.60573673248291, "The Width at 1000 km distance of the LWIR Camera Camera is About 17.5 km."]
[8.55819034576416, 9.56673526763916, "The Polarization Dependence of the Scanning Systems Optical System is Problematic."]
[10.072063446044922, 1.5217591524124146, "The Orbit Period of the JAWSAT Satellite is 100.36 min."]
[9.598645210266113, 7.782861232757568, "The Energy Range of the EPI-Lo Electron Detector is ~25 keV to 1000 keV."]
[7.102077960968018, 9.717790603637695, "The Spectral Range (\u00b5m) of the Band 2 Spectral Band is 0.84 - 0.89."]
[8.169626235961914, 9.909151077270508, "The Optics Components of the MSASI Imager is Fabry-Perot etalon and a temperature-stable narrow band filter."]
[9.16560173034668, 9.02544116973877, "The Slit Dimensions of the Imaging Subsystem Telescope is 1/2 x 5 arcmin."]
[7.221795082092285, 0.8253024220466614, "The Launch Date of the Satellite EO is 18 Dec 1999."]
[7.808200359344482, 9.84544849395752, "The Bandwidth of the Band Photometers Photometer is 90 nm."]
[5.314393043518066, 3.932439088821411, "The Function of the POIC Payload Operations and Integration Center is Coordinates allocation of onboard resources."]
[8.285085678100586, 8.516119956970215, "The Detector Elements of the VIS Channel Detector Satellite Instrument is 4."]
[7.140441417694092, 3.072697162628174, "The Mission Status of the ADM-Aeolus Satellite is Unknown."]
[10.480988502502441, -0.985794186592102, "The Mass of the Hodoyoshi-1 Microsatellite is 60 kg."]
[6.119562149047852, 0.5650293827056885, "The Launch Date of the PW-Sat CubeSat is February 13, 2012."]
[5.424140453338623, 3.18253755569458, "The Manufacturer of the Bus Satellite Component is  Blue Canyon Technologies."]
[4.3315348625183105, 6.671168804168701, "The Frequency of the OCXO Oscillator is 222 Hz."]
[6.231865406036377, 8.536855697631836, "The Calibration of the MIS Instrument Microwave Radiometer is 2-point."]
[6.78139066696167, 3.5657501220703125, "The Qualification and Test Activity of the Taurus Frangible Joint System Satellite Component is 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."]
[9.420697212219238, 9.74690055847168, "The Dimensions of the ShadowCam Instrument is 118 cm long and 27 cm in diameter."]
[7.826969146728516, 2.271852970123291, "The Author of the Observation of the Earth and Its Environment: Survey of Missions and Sensors Documentation is Herbert J. Kramer."]
[6.624805450439453, 3.5627105236053467, "The Collaboration of the JEM-EUSO Satellite is 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. Catal."]
[5.354195594787598, 2.7999415397644043, "The Designing Institution of the ZACube-2 CubeSat is F'SATI (French South African Institute of Technology) at CPUT (Cape Peninsula University of Technology)."]
[8.72653865814209, 7.792174339294434, "The Electrical Noise of the APS-A and APS-B Sensors is Smaller than a digit of the ADC."]
[7.3672003746032715, 3.767028331756592, "The Preparatory Campaigns of the CryoSat-2 Satellite is Arctic Arc Expedition, Antarctic 2008/9 CroVEx campaign."]
[6.069990634918213, 11.254117012023926, "The Approx. peak sensitivity altitude of the Channel 5 Sensor is Unknown."]
[11.708792686462402, -1.2068921327590942, "The Mass of the KOMPSAT-3 Satellite is 970 kg."]
[9.53145980834961, 9.067055702209473, "The Aperture Diameter of the Instrument Telescope is 35 cm."]
[7.157926082611084, 2.54668927192688, "The URL of the LRO Satellite is http://www.nasa.gov/mission_pages/LRO/news/lro-topo.html."]
[10.148603439331055, 2.9142794609069824, "The Orbit of the ERBS satellite Satellite is 507 km x 559 km."]
[12.63659954071045, 6.92411470413208, "The Pulse period (ms) of the B1813-140 Pulsar is 3.300."]
[7.736586093902588, 8.860783576965332, "The Vertical Sampling of the Instrument Spectrometer is \u22641 km."]
[6.186138153076172, 5.571008205413818, "The Radar Wavelength of the Biomass satellite Satellite is Around 70 cm."]
[6.556786060333252, 4.266067028045654, "The Mission Type of the CO2M Satellite is Two-satellite mission, with the option of a third satellite."]
[10.966822624206543, 5.317677021026611, "The Formation Mechanism of the Sunspot Solar Phenomenon is Mystery of the formation mechanism of a stronger field outside an umbra than in the umbra."]
[8.764744758605957, 1.6606910228729248, "The Arrival Date at Jupiter of the Juno Spacecraft is July 4, 2016."]
[7.69988489151001, 5.308444976806641, "The Observation Modes of the OCO Satellite is Nadir, Glint, Target."]
[7.755740165710449, 10.314221382141113, "The VIS Channel Detectors of the SEVIRI Spectral Imager is Photo-voltaic silicon diodes."]
[11.264432907104492, 4.3755388259887695, "The Number of Galaxies to be Mapped of the Euclid Space Telescope is Up to two billion."]
[7.61053991317749, 1.1810153722763062, "The On-Orbit Verification Date of the Space Inflatable Structures Technology is June 1-8, 2008."]
[9.229129791259766, 4.195770263671875, "The Wing Span of the Spacecraft bus Satellite is 13.7 m."]
[6.574136734008789, 4.249617099761963, "The Purpose of the RADARSAT-1 Satellite is Produced radar imagery for applications in agriculture, cartography, hydrology, forestry, oceanography, geology, ice and ocean monitoring, arctic surveillance, and detecting ocean oil slicks."]
[9.241899490356445, 0.9310740828514099, "The Operation Duration of the e-POP RRI Radio Receiver Instrument is Three Years."]
[10.22071647644043, 2.934563636779785, "The Altitude of the Satellite Orbit is 572 km."]
[10.367077827453613, -0.953835666179657, "The Mass of the GOMX-1 Nanosatellite is Up to 2.66 kg."]
[9.355515480041504, 9.549625396728516, "The Photodetector Model of the Optical Head Optical Device is MT 9M001 by Micron Technology, Inc.."]
[8.826979637145996, 6.50399923324585, "The Objective of the FlaPS Instrument Package is 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."]
[9.528169631958008, 1.347538709640503, "The Shift Length of the On-call Operations Operations is 16 hours."]
[7.729596138000488, 7.399761199951172, "The Manufacturer of the MM Radiometer Sensor is NASA/JPL."]
[4.109433650970459, 6.66616678237915, "The BER of the Miniaturized X-band transponders Communications System is < 1 x 10-5 for downlink."]
[7.310419082641602, 5.477133750915527, "The Impact of the Aeolus Satellite is Comparable to the impact from other satellite-based observations which have been assimilated for many years and have much larger data volumes."]
[5.348555088043213, 6.578098773956299, "The Number of Independent Samples of the PR Phased Array System is 64."]
[8.771883010864258, 3.589090347290039, "The Formation of the TSX and TDX Satellites is Close Helix."]
[4.798581123352051, 1.827185034751892, "The Number of Satellites of the BRITE Constellation Satellite Constellation is 5."]
[9.486282348632812, 0.4697609543800354, "The Design Life of the TRMM Satellite is 3 years."]
[2.2530670166015625, 4.484753608703613, "The Array Power Average of the Spacecraft Bus (Avionics Module=AM) Satellite is 650 W."]
[4.8497700691223145, 3.124572992324829, "The Side Panels of the CSTB1 Satellite is P0 through P5."]
[7.615006446838379, 0.38536548614501953, "The Launch Date of the Meteor-1-2 Satellite is 06.10.1969."]
[9.210698127746582, 1.1311761140823364, "The System AI&T Duration of the RRSW Integration Facility is Six months."]
[10.244048118591309, 5.713271141052246, "The Function of the Tether Spacecraft Component is Antenna."]
[7.539911270141602, 5.6747870445251465, "The Direction of the Japan Current Ocean Current is South."]
[4.223320484161377, 2.5723767280578613, "The Service Cost of the Starlink Premium Satellite Internet Service is $500 per month."]
[5.4631500244140625, 10.420026779174805, "The Swath Width of the LIS Lightning Image Sensor is 550 km."]
[5.7185235023498535, 2.168056011199951, "The Security of the QKD Quantum Key Distribution is Provable security against future hacks from advanced computers."]
[8.807476997375488, 7.328989028930664, "The Number of Sensors per Instrument of the PIMS Plasma Instrument is 2."]
[7.004368305206299, 2.5809993743896484, "The URL of the OSCAR-QUBE Satellite is https://www.esa.int/Education/Orbit_Your_Thesis/."]
[10.399538040161133, -1.2244648933410645, "The Orbit of the Tianzhou-2 Cargo Spacecraft is 343 by 371 kilometers."]
[1.8553258180618286, 3.980971574783325, "The Quantity of the Solar Panels Power Source is 2 sets."]
[4.668842792510986, 3.723494529724121, "The Purpose of the Proof-of-Concept Prototype Prototype is Test future options for maritime autonomous vessel navigation."]
[6.015194892883301, 3.2548723220825195, "The Ground Stations of the NigeriaSat-2 Satellite is Abuja and Guildford."]
[4.9631218910217285, -3.169938564300537, "The | of the R. A. Schwartz Author is R. A. Schwartz."]
[8.636286735534668, 8.879809379577637, "The Ellipse Axis A of the Long Wavelength Band Spectrometer is 180 mm."]
[7.062239170074463, 3.561096668243408, "The Launch Status of the OrbView-4 Satellite is Failure."]
[11.828481674194336, 1.0386778116226196, "The Landing Date of the Chang'e-3 Lunar Probe is Dec. 14, 2013."]
[6.730456829071045, 4.097928524017334, "The System Overview of the Sentinel-1 Satellite is Unknown."]
[7.702205181121826, 0.864827036857605, "The Launch Date of the Landsat Satellite is Unknown."]
[6.51464319229126, 0.6471443176269531, "The Program Start Date of the OICETS Satellite is 1993."]
[7.128428936004639, 0.7773263454437256, "The Launch Date of the OPS-SAT Satellite is 2012."]
[8.123993873596191, 10.52579402923584, "The Functions of the TDP Signal Processor is Gamma (spike) event circumvention, detector responsivity correction, background subtraction, time delay and integration (TDI), matched filtering, and thresholding."]
[8.202927589416504, 7.9776530265808105, "The Publication Date of the Very-Wide-Filed Ultraviolet Sky Survey Instrument is July 13, 1984."]
[3.6884350776672363, 4.49249792098999, "The CPU of the SCU Satellite Central Unit is HD64F7145FW50."]
[8.483358383178711, 1.6231507062911987, "The First Image Release Date of the Webb Telescope Space Telescope is 12 July 2022."]
[10.400586128234863, 3.3611817359924316, "The Separation Distance of the GRACE Satellite Satellite is Between 170 to 270 km."]
[7.823745250701904, 1.9490854740142822, "The System Integration Review Date of the Europa Clipper Spacecraft is Late 2021."]
[4.48373556137085, 5.328596591949463, "The BDH Subsystem of the ResourceSat-2 Satellite is X-band data transmission system."]
[9.25366497039795, 3.208125591278076, "The Orbit Type of the BUV Sensor is Sun-synchronous near-circular polar orbit."]
[3.177490472793579, 6.662210941314697, "The Transmission Power of the SSRNI Data Acquisition and Registration System is 8 W."]
[6.891176223754883, 4.913005352020264, "The Location of the Wetlands Ecosystem is Iran's border with Afghanistan."]
[3.2741312980651855, 5.215069770812988, "The File System of the Data Storage System is FAT32."]
[7.890194892883301, 7.774298191070557, "The Source Data of the \u00b5SCIA Monitoring Instrument is Planned to be posted onto the Internet."]
[9.003621101379395, 9.266812324523926, "The Flatness Requirement of the Photon Sieve Optic is Approximately 3\u03bb."]
[7.183003902435303, 2.7867836952209473, "The URL of the ICON Satellite is https://icon.ssl.berkeley.edu/science/."]
[10.053885459899902, 3.0625877380371094, "The Orbit Altitude of the SuperView-1 01 and Superview-1 02 Satellite is 530 km."]
[8.319392204284668, 9.154165267944336, "The Detector Technology of the Optical Sensor Assembly (OSA) Instrument is Pushbroom detector technology."]
[7.196468353271484, 7.000792980194092, "The Integration Date of the Second Scientific Instrument Scientific Instrument is Unknown."]
[5.0116801261901855, -0.16158552467823029, "The Announcement Date of the OneWeb Satellite Constellation is June 25, 2015."]
[8.3858060836792, 9.922589302062988, "The Support Mode of the SLIM6 Imager is Window Pseudo Real-Time Imaging."]
[9.606180191040039, 8.519453048706055, "The Temperature Sensitivity of the Etalon Filter is 2.9 pm/K."]
[8.682951927185059, 1.9698957204818726, "The URL of the James Webb Space Telescope Telescope is http://www.stfc.ac.uk/ukatc/resources/pdf/miri5487-28.pdf."]
[6.764235973358154, 1.539459228515625, "The Presentation Date of the RapidEye Earth Observation Constellation is Oct. 12-16, 2009."]
[7.786696910858154, 5.73868465423584, "The Accuracy of the CLARREO Pathfinder Satellite is 4 to 8 times more accurate than current best available sensors on orbit."]
[8.439984321594238, 11.097949981689453, "The Number of Eligible Rows of the QWIP Array Sensor Array is Not specified."]
[6.64251184463501, 1.2453974485397339, "The Presentation Date of the Texas 2 STEP Satellite Mission is Aug. 11-14, 2008."]
[6.686094760894775, 7.899508476257324, "The Type of the AMSU-A Instrument is Cross-track, line-scanning instrument (whiskbroom type)."]
[3.738909959793091, 2.2841317653656006, "The Size of the MCubed/COVE-2 CubeSat is 1U."]
[7.964802265167236, 5.271092414855957, "The Ranging Accuracy of the Galileo Satellite Navigation System is Better than 1.07 m."]
[8.42839527130127, 10.147526741027832, "The Application of the CMT Imager is Local Mapping."]
[7.191874980926514, 5.336504936218262, "The Accelerating Rate of the Sea Level Climate Parameter is 3 mm/year."]
[4.755324363708496, 1.7524670362472534, "The Satellite Constellation Goal of the Satellogic Satellite Company is 300 satellites by 2025."]
[10.260042190551758, 4.914073944091797, "The Mission of the Colloid Microthruster Thruster is Space Technology 7 and LISA."]
[9.4098539352417, 9.882914543151855, "The Function of the ShadowCam Instrument is Capture images in lunar orbit."]
[6.644252300262451, 1.023484706878662, "The Launch Date of the FalconSat-3 Satellite is 9 March 2007."]
[7.178576469421387, 8.579574584960938, "The Mass Resolution of the COSIMA Mass Spectrometer is 2000."]
[5.754129886627197, 3.226067304611206, "The Platform of the DoT-1 satellite Satellite is SSTL-Micro."]
[4.970252990722656, 5.384251117706299, "The Antenna Sizes of the Ground Station Ground Station is 9.1m, 4.6m."]
[10.64364242553711, 9.265835762023926, "The Crater Location of the CaSSIS camera Camera is 134\u00b012'13.0\"W/43\u00b014'59.7\"N."]
[7.70245361328125, 5.9929633140563965, "The Calibration Methods of the SeaWiFS Satellite is Short-period solar calibration, long-term lunar calibration."]
[7.085470676422119, 1.3939849138259888, "The Workshop Date of the China Earth Observation Satellite Program Satellite Program is Feb. 11-13, 2009."]
[4.744699001312256, 2.487797260284424, "The Downlink Channels of the CubeSat Satellite is 2."]
[11.118295669555664, 2.8447389602661133, "The Depth of the Sognefjord Fjord is 1308 m."]
[3.360105276107788, 5.039985179901123, "The Mass memories of the Data Handling Unit Subsystem is MM0, MM1, MM2, MM4."]
[4.710182189941406, 1.811532974243164, "The Maximum Satellites Launched of the New Glenn rocket Rocket is Around 30."]
[7.047638893127441, 0.9593712091445923, "The Symposium Date of the Flying Laptop Satellite is April 8-12, 2013."]
[9.16640567779541, 5.499618053436279, "The Attitude Control Subsystem of the TUBSAT-N Satellite is CCD star sensor, 3-D magnetic compass, two magnetic coils, reaction wheel."]
[3.197488784790039, 5.294522762298584, "The Capacity of the S/C Data Recorders Data Storage is 54 Gbit."]
[4.611304759979248, 9.026178359985352, "The Landing Date of the InSight Mars Lander is 29 November 2018."]
[8.571349143981934, 2.3125216960906982, "The Heritage of the LET Low Energy Telescope is SOHO/ERNE."]
[9.527042388916016, 0.4622410833835602, "The Design Life of the ACRIMSat Satellite is 5 years."]
[8.506807327270508, 2.6547467708587646, "The Planned Operation of the ARTEMIS Probes Spacecraft is Routinely operate in the most eccentric lunar science orbits of any mission to date."]
[10.57519817352295, 7.518093585968018, "The Structure Material of the GNB Satellite Platform is Al 6061-T6."]
[7.770302772521973, 9.00372314453125, "The Sensitivity of the GOME-2 Spectrometer is Negligible."]
[11.530587196350098, 4.060398578643799, "The Mass of the Beta Pictoris b Planet is At least 50 times more massive than AU Mic b."]
[9.539831161499023, -0.7060942649841309, "The Development of the PACE nanosatellite Satellite is Carried out by students of the PACELAB research laboratory at NCKU."]
[6.712053298950195, 2.091583251953125, "The Purpose of the GPM (Global Precipitation Measurement) Mission Satellite Constellation is Study global precipitation, evaporation and the water cycle."]
[7.702845096588135, 3.424898386001587, "The Purpose of the ICON Satellite is Explore the boundary between Earth and space \u2013 the ionosphere."]
[4.010223865509033, 6.365309238433838, "The Frequency of the TT&C Telemetry Tracking & Command is 437.385 MHz."]
[9.341962814331055, 6.471141338348389, "The Location of the Star Trackers Device is Zenith end assembly."]
[3.760159492492676, 6.071020603179932, "The User Data Rates of the Optical Downlink Communication System is 39 \u2013 620 Mbit/s."]
[7.129014015197754, 2.5075061321258545, "The URL of the FireBird Satellite is http://www.int-arch-photogramm-remote-sens-spatial-inf sci.net/XL-7-W3/461/2015/isprsarchives-XL-7-W3-461-2015.pdf."]
[3.840101480484009, 6.5793657302856445, "The Transmitter Modulation Bandwidth of the S-band transponder Communication Device is 3 MHz."]
[8.575921058654785, 3.8379924297332764, "The Along-Track Separation of the ATI Experiments Satellite Experiment is Optimal observation conditions."]
[11.664335250854492, -1.2794358730316162, "The Satellite Class of the Cheollian 2B Satellite is 3.4-ton class."]
[5.174994468688965, 6.449841499328613, "The Polarization of the Antenna ADS-B Antenna is Right Hand Circular."]
[6.415976524353027, 1.5953245162963867, "The Launch Date of the Jason 2 Satellite is June 20, 2008."]
[10.599754333496094, 8.512348175048828, "The Aperture Diameter of the COR1 Coronagraph1 imager is 36 mm."]
[9.566391944885254, 8.83802604675293, "The Field of View of the ALI Telescope is 15\u00ba x 1.26\u00ba."]
[6.535099983215332, 4.201673984527588, "The Mission Scientist of the CO2M Satellite is Yasjka Meijer."]
[7.637937068939209, 3.230587959289551, "The Solar Panels of the CartoSat-2B Satellite is Deployed."]
[8.094902992248535, 8.526744842529297, "The Moving Parts of the Spatial Heterodyne Spectroscopy (SHS) Interferometric Fourier transform technique is None."]
[5.644146919250488, 4.11688756942749, "The Design Approach of the Sentinel FOS Flight Operations Segment is Extensive re-use of elements developed in the context of previous Earth Observation ground segments."]
[9.005228042602539, 2.4989256858825684, "The Wavelengths of the Herschel Space Telescope is 70 \u00b5m (blue), 160 \u00b5m (green) and 250 \u00b5m (red)."]
[7.08317756652832, 0.09436646848917007, "The Launch Date of the MEPSI Satellite is July 19, 2000."]
[9.498367309570312, 9.041844367980957, "The Acquisition Telescope Size of the OCTL Telescope is 20 cm."]
[4.741419315338135, 5.635559558868408, "The Amplifier Power of the Knudsen Station Ground Station is 500 W."]
[9.223398208618164, 7.355434894561768, "The Temperature at which it stopped working of the Home Switch Switch is Unknown."]
[5.676512718200684, 1.7153064012527466, "The Launch Vehicle of the ICEYE-X2 Satellite is SpaceX Falcon 9 rocket."]
[7.146364688873291, 1.1301668882369995, "The IAC Presentation Date of the D-Sat Satellite is 25-29 Sept. 2017."]
[6.2674713134765625, 0.42869430780410767, "The Launch Date of the AQT-D 3U CubeSat Satellite is 24 September 2019."]
[5.99092435836792, 3.566072463989258, "The TDP Command Release of the Inmarsat Automated Procedure Execution System System is Automatic."]
[7.051604270935059, 1.4288994073867798, "The Conference Presentation Date of the Stuttgart Micro Satellite Satellite is May 5-9, 2014."]
[7.7887372970581055, 9.406996726989746, "The Wavelength Range of the IR Channel Imaging Device is 1.3 \u2013 4.5 \u00b5m."]
[6.139702320098877, 6.198841094970703, "The Imaging Modes of the SAR Instrument Synthetic Aperture Radar is Strip imaging, spot imaging."]
[7.834939956665039, 6.139784812927246, "The On-board Calibration System of the CLARREO Satellite is Uses the Sun as part of its on-board calibration system."]
[6.163044452667236, 6.301785469055176, "The Features of the ASAR Instrument is 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."]
[12.116209983825684, 2.2591028213500977, "The Visible and Infrared Spectrometer of the OSIRIS-REx Spacecraft is OVIRS."]
[6.198287487030029, 5.9758429527282715, "The Experimental Mode Coverage of the TSX-SAR Satellite is 5 x 10."]
[7.041183948516846, 1.9300897121429443, "The URL of the Swarm Satellite Mission is http://www.dsri.dk/~nio/papers/EPS_58040359.pdf."]
[5.8206682205200195, 4.089912414550781, "The Data Transmission of the QARMAN CubeSat is Iridium telecom satellites."]
[7.0358662605285645, 3.6665091514587402, "The Atmospheric Measurements of the POPACS Satellite is Data."]
[8.5338773727417, 6.836300373077393, "The Measurement Range of the OVM Overhauser scalar magnetometer is 16,000 - 64,000 nT."]
[5.997447490692139, 3.752690553665161, "The Publication Journal of the Telerobotics Space Technology is Science Robotics."]
[9.190457344055176, 9.347636222839355, "The Field-of-View (FOV) Defining Apertures of the TR Integrating Sphere is 2."]
[7.114508628845215, 1.8485355377197266, "The Tandem Mission Start Date of the Envisat / ERS-2 SAR Satellite is Nov. 23, 2008."]
[7.8233962059021, 10.8372802734375, "The Bit Depth of the MSS Instrument Radiometric Signal is 6 bit per pixel."]
[8.663097381591797, 8.611091613769531, "The Solar Elevation Angle of the Instrument Spectrometer is 30-90\u00ba."]
[6.310282230377197, 10.041130065917969, "The Weight of the Kowa LM16JC lens Lens is 55 g."]
[4.842785358428955, 0.921529233455658, "The Budget Allocation of the Galileo Global Navigation Satellite System is 8 billion euros."]
[7.729751110076904, 8.779991149902344, "The Instantaneous spectral coverage of the Spectrometer Instrument is 1.56 km/s."]
[9.53675651550293, 0.486380934715271, "The Design Life of the Gokturk-2 Satellite is 5 years."]
[1.6412913799285889, 4.8698577880859375, "The Bias Voltage of the Suppressor Grid Satellite Component is -12 V."]
[10.376748085021973, 1.2829335927963257, "The LTAN of the Max Valier Satellite is 17:00 hours."]
[9.246354103088379, 6.347182750701904, "The Guide Stars Monitoring Interval of the DPU Data Processing Unit is 10-20 seconds."]
[7.614005088806152, 0.8387625813484192, "The Formulation Date of the CLERREO Mission is 2009."]
[2.9488682746887207, 6.735294818878174, "The Electrical Power of the MHX-2400 S-band Transmitter/Transceiver is 4.85 W."]
[10.191182136535645, 4.488775253295898, "The Propulsion System of the Clementine Spacecraft is Bipropellant nitrogen tetraoxide and monomethyl hydrazine system for the maneuvers in space."]
[8.624810218811035, 1.6953011751174927, "The Flare Detection Date of the Spitzer Space Telescope Telescope is July 31, 2019."]
[8.986607551574707, 3.823855400085449, "The Design of the MMS Satellite is Four spacecraft flying in a tight tetrahedral formation."]
[10.061469078063965, 1.5463465452194214, "The Orbital Period of the Main Payload Satellite is About 97.7 minutes."]
[5.966329097747803, 6.677045822143555, "The Beam Incidence Span of the SWIM Real Aperture Radar is Up to 10\u00ba."]
[8.428640365600586, 7.78120231628418, "The Purpose of the Webb's Fine Guidance Sensor (FGS) Sensor is Enable accurate science measurements and imaging with precision pointing."]
[6.62367582321167, 3.7235159873962402, "The Verification Process of the ASAP Autonomy System is Closed loop manner, take over control of the satellite by manipulating SONATE\u2019s active command list."]
[9.119707107543945, 5.389616966247559, "The Torque Input of the Attitude Control System Satellite System is Minute and continuous."]
[9.944939613342285, 7.368221759796143, "The Solar Absorptivity of the Cube Corner Reflectors (CCRs) Satellite Component is \u03b1s."]
[6.165959358215332, 6.545058727264404, "The Mode Name of the Poseidon 4 Radar Altimeter is InterLeaved Mode."]
[7.145914077758789, 1.5615683794021606, "The Symposium Date of the GMES Sentinel-3 Satellite is July 25-30, 2010."]
[9.14177131652832, 7.764176845550537, "The Thermosphere Temperature of the Instrument Spectrometer is Typically > 600 K."]
[8.619239807128906, 5.614307403564453, "The Pointing Accuracy of the IPS Pointing System is Within 2 arcseconds."]
[9.264528274536133, -0.5789610743522644, "The Development Schedule of the ANGELS Nanosatellite is Particularly short."]
[1.710152506828308, 4.690282344818115, "The Radio and Reaction Wheels Voltage of the MarCO-B Satellite is Greater than 8V."]
[11.610391616821289, 4.509891033172607, "The Mass of the Giant Molecular Clouds Interstellar Medium is Up to 10 million times the mass of the Sun."]
[7.601099491119385, 7.951234340667725, "The Backup Purpose of the CIRAS Instrument is Gap filler in the event of a failure of the CrIS."]
[9.974480628967285, 9.55553150177002, "The Purpose of the SAGE-III on ISS Satellite Instrument is Monitor the health of the ozone layer and track the recovery of stratospheric O3."]
[6.473820209503174, -0.1602078527212143, "The Atomic Clocks of the Indian Regional Navigation Satellite System (IRNSS) Satellite System is Failed."]
[6.6769256591796875, 0.4407239556312561, "The Launch Date of the CBERS-1 Satellite is Oct. 14, 1999."]
[7.495467185974121, 8.908435821533203, "The Measurement Range of the Spectral Channels Satellite Instrument is 1.6 to100% albedo."]
[6.213480472564697, 7.072705268859863, "The Improvement of the DDA Delay-Doppler Altimeter is Capturing more reflected energy and requiring smaller transmitted power."]
[5.737907409667969, 7.094676971435547, "The Instrument Mass of the RA-1 Radar Altimeter is 96 kg."]
[0.9967247247695923, 4.347723007202148, "The Battery Capacity of the EPS Electric Power Subsystem is < 7600 mAhr."]
[7.676864147186279, 2.246617317199707, "The Launch Target of the NISAR Earth Observation Satellite is 2022."]
[6.848363876342773, 1.0900191068649292, "The Publication Date of the Small GEO Programme Satellite Programme is 2012."]
[7.911749839782715, 3.7287023067474365, "The Impact on Astronomical Observations of the Satellite Constellations Satellite System is Not specified."]
[8.956358909606934, 6.02544641494751, "The Technology of the LOFTID Project is Hypersonic Inflatable Aerodynamic Decelerator (HIAD)."]
[1.590600848197937, 4.870506763458252, "The Power Output of the PDC Power/Data Controller is Conditioned 28 VDC and 12 VDC."]
[9.201268196105957, 3.2058017253875732, "The Orbit Type of the Tandem-L satellites Satellite is Sun-synchronous dawn/dusk orbit."]
[8.543334007263184, 5.414973735809326, "The Absolute Performance Error of the Spacecraft Satellite is < 20 arcsec (95%)."]
[11.175225257873535, 9.346261024475098, "The Mass of the Earth Radiation Budget Experiment (ERBE) Instrument is 57 kg/scanner."]
[6.538477897644043, 6.3414530754089355, "The Purpose of the SGLI Imager is Measure ocean color, SST (Sea Surface Temperature), land use and vegetation, snow and ice, clouds, aerosols and water vapor."]
[9.559389114379883, 1.2983661890029907, "The Ability to Revisit of the ZY-3A Satellite is 4-5 days."]
[5.019160747528076, 4.9322428703308105, "The Repetition Rate of the Drifting (Mobile) Platforms Ground Segment is 90 - 150 seconds."]
[2.172734260559082, 4.283604621887207, "The Solar Panel Power of the DubaiSat-2 Satellite is More than 450 W."]
[4.546115875244141, 5.743018627166748, "The TT&C Function of the COSMO-SkyMed-1 Satellite is S-band."]
[11.590906143188477, 4.461333751678467, "The Current Distance of the IC 4665 and Collinder 350 Star Clusters is More than twice as large as the diameters of the biggest molecular clouds."]
[3.626336097717285, 6.182112693786621, "The Downlink Speed of the Communication links Communication System is 9.6 - 38.4 kbit/s."]
[10.954388618469238, 5.129709243774414, "The Motion of the Solar Plumelets Solar Phenomenon is Move individually, oscillating on its own."]
[11.706933975219727, 4.798068523406982, "The Quasar Diminishment of the The Teacup Quasar is Only fading by a factor of 25 or less over the past 100,000 years."]
[7.220963954925537, 0.8346863985061646, "The Contract Date of the AERO-VISTA mission Satellite Mission is May 7, 2020."]
[9.592552185058594, 1.5314620733261108, "The Repeat Cycle of the CERES on TRMM Instrument is 46 days."]
[7.999794960021973, 1.3387823104858398, "The Article Release Date of the Solar Orbiter Satellite is 17 May 2021."]
[1.8121534585952759, 3.992144823074341, "The Number of Cells per String of the Solar Array Power Generation is 39."]
[7.502037048339844, 0.9879472851753235, "The Last Spinup Maneuver Date of the Satellite Spacecraft is July 2, 2014."]
[9.204444885253906, 3.234069585800171, "The Type of the Orbit Satellite is Sun-synchronous near-circular."]
[5.320114612579346, 5.986487865447998, "The Function of the Antenna Payload is Easily removed from the spacecraft without removing any of the spacecraft panels."]
[7.097207069396973, 8.851995468139648, "The Swath Width of the SAM-II Instrument is 5 - 40 km vertical."]
[6.047000885009766, 4.434362411499023, "The Operation of the JEMRMS Robotic Arm is Catches EP and carries it to EFU."]
[8.111283302307129, 2.6210031509399414, "The Data Collection Start Date of the TerraSAR-X Satellite is Early 2011."]
[6.1999077796936035, 3.971369743347168, "The Payload Sizes of the Bartolomeo Platform Satellite Platform is Airlock-compatible size, FRAM-based standard size."]
[8.254138946533203, 0.6779789328575134, "The Calibration Phase Start Date of the Hitomi X-ray Astronomy Satellite is Middle of April."]
[11.55836009979248, 7.375914573669434, "The Development of the MONTE Software is Precision one-way radiometric measurement modeling, high fidelity clock modeling, and appropriate filter methods."]
[10.332738876342773, 2.9135186672210693, "The Orbit Altitude of the ALBus CubeSat Satellite is 500 km."]
[6.549281120300293, 2.8866515159606934, "The Phase A/B1 Study Contracts of the OPS-SAT Satellite is Awarded to TU Graz and GOMSPACE."]
[9.98492431640625, 3.7793257236480713, "The Overall Length of the GSLV-F05 Rocket is 49.1 m."]
[6.3720808029174805, 8.504386901855469, "The Size of the OMS Radiometer Radiometer is 10 x 10 x 15cm."]
[9.393733024597168, 9.393584251403809, "The Focal Length of the Optical Head Optical Device is 3 mm."]
[4.884575843811035, 8.988295555114746, "The Reach of the InSight lander Robotic Arm is Nearly 2 meters."]
[7.915090560913086, 8.303071022033691, "The Band of the IASI Infrared Atmospheric Sounding Interferometer is 1."]
[5.644989490509033, 3.758484363555908, "The Control Center of the Colony I Satellite is SOC (Satellite Operations Center) at BPTF (Blossom Point Test Facility), located near LaPlata, MD."]
[7.0416178703308105, 1.1732810735702515, "The New Deadline for Completion of the SpaceIL Nonprofit Group is December 2017."]
[7.077566146850586, 4.666635036468506, "The Long Range Navigation of the ATV-5 Spacecraft is Relative GPS navigation."]
[8.106048583984375, 9.346320152282715, "The Type of the MWIR Sensor Sensor is Miniature high temperature Mid-Wave Infra-Red (MWIR)."]
[5.9867987632751465, 8.908777236938477, "The Power Consumption of the AMU Altimeter Microwave Unit is < 39 W."]
[9.69726276397705, 1.0099810361862183, "The Minimum Duration of the PACE Satellite is Three years."]
[7.168483734130859, 7.108607769012451, "The Unknown of the BELA Instrument is Unknown."]
[9.491239547729492, 7.808177471160889, "The Electronic Noise Contribution to Energy Resolution of the Detector Instrument is 400 eV."]
[10.482919692993164, 4.823340892791748, "The Propellant Mass of the DMC Propulsion Subsystem Electric Propulsion is 2.35 kg."]
[8.472575187683105, 3.255544900894165, "The Formation Geometries of the TanDEM-X Satellite is Bistatic Close formation."]
[7.376880168914795, 8.79379940032959, "The S/N or NEDT of the Spectral Channels Satellite Instrument is 150:1."]
[9.577226638793945, 6.616271018981934, "The Redesign Purpose of the SMA Hinge Spring Component is Increase area to reduce stress on the part by more than 20%."]
[7.6347503662109375, 2.664602041244507, "The URL of the Space Debris IADC Assessment Report for 2010 Report is http://www.iadc-online.org/Documents/IADC-2011-04,%20IADC%20Annual%20Report%20for%202010.pdf."]
[4.615474700927734, 3.652026653289795, "The AIS of the LAPAN-A2 Satellite is Automatic Identification System."]
[4.534660816192627, 7.4089226722717285, "The Mass of the EPDP Technology Payload is 2.3 kg."]
[13.17425537109375, 4.022028923034668, "The Data Release 2 of the Gaia Satellite is April 25, 2018."]
[7.690866470336914, 3.4632327556610107, "The Spectrometers of the DebriSat Satellite is 2."]
[8.842052459716797, 1.7354627847671509, "The Solar Wing Deployment Test of the BepiColombo Satellite is March 6, 2017."]
[3.8971059322357178, 2.282538652420044, "The Inflatable Mast Length of the 3U CubeSat Satellite is 1 m."]
[8.761146545410156, 10.018312454223633, "The Function of the Front-End Electronics Module (F2EM) Electronics Module is Provides the detectors with all the necessary biasing and clocking signals and performs preamplification and transmission of the video signal to the MEV."]
[10.833658218383789, 4.154709339141846, "The Mission Type of the Cheops Satellite is Study of exoplanets."]
[8.448371887207031, 2.546027421951294, "The Maneuvers Events of the ARTEMIS Satellite is 170."]
[8.630910873413086, 6.073304653167725, "The Anomalies of the Earth's Magnetic Field Natural Phenomenon is Deviations from the idealized field of a centered bar magnet."]
[9.622015953063965, 7.93510103225708, "The Ion energy of the Microdosimeter B Instrument is > 50 keV."]
[6.564088344573975, 3.7619736194610596, "The Unique Feature of the Spire Satellite Constellation is Reaching remote areas like the open oceans."]
[6.050076484680176, 5.001570701599121, "The Developers of the CPR Cloud Profiling Radar is NASA/JPL and CSA."]
[11.49128532409668, -1.310003638267517, "The Adapter and Separation System Mass of the ALMASat-1 Satellite is 20.5 kg."]
[5.935951232910156, 3.5386815071105957, "The Recommendation of the Commercial Smallsat Data Acquisition Program Program is Put into statute and robustly fund."]
[9.224453926086426, 9.253874778747559, "The Field of View of the Collecting Optics Lens Assembly is \u00b1 7\u00ba."]
[8.449882507324219, 4.678457260131836, "The Mission Type of the Cluster Satellite is Magnetosphere Measurement."]
[11.247543334960938, -1.4943240880966187, "The Mass of the CICERO-6 6U CubeSat is ~10 kg."]
[3.319800615310669, 5.15880012512207, "The Storage Media of the Data Storage System is CompactFlash\u00ae card."]
[7.496023654937744, -0.04080931097269058, "The Flight Model Manufacturing Start Date of the CHEOPS Instrument is End of 2015."]
[8.023041725158691, 3.9380123615264893, "The Resolution of the Pl\u00e9iades Neo Satellite Constellation is 30cm."]
[9.267620086669922, 4.770079612731934, "The High Pressure Tank Size of the I-COUPS Satellite is 2.0 L."]
[11.640877723693848, -1.158586859703064, "The Mass of the Sloshsat-FLEVO Satellite is 50-150 kg."]
[7.852285385131836, 8.290550231933594, "The Development Date of the CHRIS Imaging Spectrometer is Unknown."]
[7.894033432006836, 4.222497940063477, "The Percentage of New Subscribers of the SecureWatch Service is 70%."]
[7.439132213592529, -0.33759605884552, "The Launch Date of the Minotaur I Rocket Rocket is Nov. 19, 2013."]
[8.56110954284668, 9.200579643249512, "The Slit 2 Material of the MEGS-A Spectrograph is Si."]
[11.41315746307373, 2.2336912155151367, "The Capsule Drop Altitude of the Hayabusa-2 Spacecraft is About 120 miles (or 200 km) above Earth\u2019s surface."]
[7.669007301330566, 9.11643123626709, "The Wavelength Bands of the B. subtilis Microorganism is 470, 525, and 615 nm."]
[5.717383861541748, 2.1702582836151123, "The Number of Orbits of the Kolibri-2000 Satellite is 711."]
[10.447999954223633, 6.038820266723633, "The Purpose of the MVP Cell-03 Experiment is Examine whether microgravity increases the production of heart cells from human-induced pluripotent stem cells (hiPSCs)."]
[11.889984130859375, 0.980767011642456, "The Launch Date of the Chang'e-5 Spacecraft is Nov. 23."]
[4.580868244171143, 4.827328205108643, "The Manufacturer of the DWP Control System is University of Sheffield."]
[5.420825481414795, 4.556110382080078, "The Ground Station of the HYPSO-1 Satellite is KSAT Svalbard, Norway."]
[3.5366499423980713, 5.678032875061035, "The Bandwidth of the FODB Data Interface is Gbit/s."]
[3.915067195892334, 6.691225528717041, "The Uplink Frequency of the DRT Data Relay Transponder is 402.75 MHz."]
[11.702008247375488, -1.1056116819381714, "The Mass of the Deimos-2 Satellite is ~310 kg."]
[9.27945327758789, 3.8159379959106445, "The Dimensions of the DART spacecraft with ROSA Spacecraft is 12.5 meters by 2.4 meters."]
[6.085728168487549, 0.5993953347206116, "The Observation Date of the DICE CubeSats Satellite is March 16-17, 2013."]
[6.963817596435547, 0.5618472099304199, "The Launch Date of the ZACUBE-01 Satellite is Unknown."]
[5.314209461212158, 4.6872758865356445, "The Access Method of the Argos Communication System is Pure (i.e. unslotted) ALOHA."]
[6.11902379989624, 1.6452910900115967, "The Launch Vehicle of the Herschel Telescope Telescope is Ariane-5 ECA."]
[7.993341445922852, 3.9206080436706543, "The Anomaly of the ALOS-3 Satellite is Ignition signals for the SRB-3s were not sent."]
[8.937567710876465, 3.212818145751953, "The Orbit of the Queqiao Lunar Relay Satellite is Halo orbit."]
[6.467640399932861, 3.2454030513763428, "The Mission Outcome of the ESEO Satellite is Reduced success in achieving the science objectives."]
[8.420037269592285, 7.963558197021484, "The Pixel Classification of the JWST Fine Guidance Sensor Sensor is Not Provided."]
[10.952163696289062, 3.2951266765594482, "The Distance from New Horizons of the Hydra Moon is About 231,000 km."]
[11.54792594909668, 6.3042120933532715, "The Leader of the XMM-Newton Survey Science Center Consortium is Professor Mike Watson."]
[4.401064395904541, 4.160661697387695, "The Interface of the Formation Flying Computer Computer is Propulsion system and GPS receiver."]
[11.714929580688477, -1.001389503479004, "The Mass of the PROCYON Deep Space Probe is 50 kg."]
[7.131645679473877, 3.8487985134124756, "The Remarks/Sensors of the OrbView-3 Satellite is commercial imaging PAN +MS."]
[9.687664985656738, 1.3546404838562012, "The Observation Duration of the DELPHINUS Satellite is Long-time and continuous."]
[5.360678195953369, 2.55708646774292, "The Manufacturer of the ArgoMoon CubeSat is Argotec S.r.I.."]
[7.0410075187683105, 9.581527709960938, "The Band 7 of the MSS Instrument Spectral Band is 0.8 - 1.1 \u00b5m."]
[7.740274906158447, 0.4229288399219513, "The Launch Date of the Chandrayaan-2 Spacecraft is 6 September."]
[4.97721529006958, 4.294382572174072, "The Data Interfaces of the EuTEF Payload Facility is MIL-STD-1553B data bus and a redundant Ethernet."]
[7.294358253479004, 5.679236888885498, "The Vertical Resolution (Stratosphere) of the Aeolus Satellite is 2.0 km."]
[5.962557315826416, 3.8510189056396484, "The Ground Segment Operator of the Galileo Satellite System is European Global Navigation Satellite System Agency (GSA)."]
[7.2214131355285645, 7.247044563293457, "The Image Acquisition Time of the VIIRS Imaging Radiometer is 1:35 p.m. local time (19:35 Universal Time) on May 30, 2022."]
[4.235621452331543, 4.839990139007568, "The Version of the CCSDS Space Data Link Security Protocol Protocol is 355.0-R-2."]
[8.617671966552734, 6.994601726531982, "The Magnitude Stability of the Magnetic Field In-Situ Sensor is < 0.12 nT over 3 months."]
[8.211928367614746, 9.936357498168945, "The Critical Design Review Status of the MSASI Imager is Finished."]
[7.616769313812256, 7.669801712036133, "The Calibration of the DESIS Hyperspectral Instrument is Pre-launch and post-launch."]
[8.169219017028809, 4.761434078216553, "The GSD (Panchromatic) of the GF-2 Satellite is 0.81 m."]
[9.42691707611084, 9.470151901245117, "The Optics Unit Focal Length of the Imager Payload is 10.5 cm."]
[5.720924377441406, 6.256629467010498, "The Number of Phase Centers of the SAR antenna Antenna is 18."]
[7.032607078552246, 9.184199333190918, "The Azimuth Resolution of the ScanSAR Imaging Mode is 18.5 m."]
[10.003347396850586, 3.0496609210968018, "The Orbit of the Dove-2 Satellite is 575 km x 575 km."]
[7.128279685974121, 9.27766227722168, "The Resolution of the ScanSAR-1 Mode is 4 x 20m."]
[9.950569152832031, 1.4818259477615356, "The Period of the Satellite Constellation Satellite Constellation is 136 minutes."]
[11.30613899230957, 3.6951119899749756, "The Journey Time towards the Sun of the ISON Comet is About 3 million years."]
[5.79064416885376, 3.0428566932678223, "The Manufacturer of the SAOCOM-1A Satellite is ArSat."]
[8.919107437133789, 5.297431945800781, "The Image Registration Accuracy of the Attitude Determination & Control System Satellite System is 100 m."]
[6.6890645027160645, 3.7594330310821533, "The LRIT and HRIT Broadcasting Service Provider of the GK2A satellite Satellite is KMA (Korean Meteorological Administration)."]
[7.333374500274658, 0.2217836081981659, "The Planned Launch Year of the SMILE Satellite is 2022."]
[6.923099517822266, -0.06883363425731659, "The End of Life Date of the TechEdSat Satellite is 5 May 2013."]
[10.29671859741211, 5.62106466293335, "The Tether Pull Force of the ENT EVR Nozzle Tool is Up to 40-50 N."]
[5.04849100112915, 4.4516282081604, "The Feasibility Analysis of the CSK GS Ground Segment is 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."]
[6.080225467681885, 3.0239412784576416, "The Integration and Testing of the BRITE-PL Satellite Project is By the Polish team with mentoring and supervising support from UTIAS/SFL."]
[5.729348659515381, 0.8508042097091675, "The TFSC Data of the AlSat Nano Satellite is Regularly returned."]
[3.197690010070801, 6.137141227722168, "The Power Requirement of the APL\u2019s Frontier radio Radio is Less than other deep-space radios."]
[2.3067567348480225, 3.7753961086273193, "The Solar Array Deployment of the MicroSCOPE Satellite is 3 pyrolock mechanisms for release and 2 Carpenter blades for deployment."]
[3.745944023132324, 4.957833290100098, "The Calibration Frequency of the MAC Memory System Module is Periodic basis."]
[4.907158374786377, 9.090887069702148, "The Seismometer Distance from Lander of the InSight Lander Lander is 1.636 m."]
[5.898181438446045, 10.856191635131836, "The No of Passbands of the Channel 7 Sensor is 1."]
[7.0992536544799805, 2.608945369720459, "The Design of the Orion spacecraft Spacecraft is Uniquely designed for long-duration deep space flight."]
[8.796501159667969, 8.759291648864746, "The Viewing Angle of the ISS-LIS Instrument is Nadir or 5\u00ba off-nadir."]
[8.781825065612793, 8.999592781066895, "The Flatness of the Grating Optical Component is 1 \u03bb (634.8 nm)."]
[6.570636749267578, 1.3043180704116821, "The Test Date of the ISIM Compartment is Summer 2015."]
[9.562482833862305, 9.575539588928223, "The Power of the SAGE-III Instrument is 80 W average."]
[9.493412017822266, 3.0899088382720947, "The Largest Crater Diameter of the Eureca Satellite is 6.4 mm on the solar arrays."]
[12.155092239379883, 5.395616054534912, "The Ordinary Matter Percentage of the Universe Cosmology is 5 percent."]
[10.167219161987305, 7.6608991622924805, "The Media of the Sojourner 2020 Art Payload is Carved stone sculpture, liquid pigment experiments, sculptures made of transgender hormone replacement meds."]
[6.891711235046387, 3.2457728385925293, "The Mission Status of the GOSAT Satellite is Operational (extended)."]
[9.509556770324707, 0.6180781126022339, "The Lifespan of the Dove Satellites Satellite is Five to six years."]
[9.144012451171875, 7.587038516998291, "The Energy Range of the Electrostatic Analysers Sensor is 0.2 to 20 keV."]
[6.604933738708496, 3.3798930644989014, "The Agency of the FormoSat-1 Satellite is NSPO."]
[8.158717155456543, 4.831046104431152, "The GSD of the Spacecraft Satellite is 1 m (PAN), ~ 4 m (MS) @ 600 km altitude, nadir view."]
[8.148369789123535, 5.051731586456299, "The Geo-location Accuracy of the Satellite Satellite is <50 m without GCP, 20 m with GCP."]
[7.8435564041137695, 2.2868423461914062, "The Editor of the Observation of the Earth and Its Environment Documentation is Herbert J. Kramer."]
[9.507107734680176, 1.059403419494629, "The Total Transfer Time of the Transfer Orbit Orbital Maneuver is 3 to 4 months."]
[9.06805419921875, 9.101237297058105, "The Field of View Resolution of the IBEX-Lo sensor Sensor is 7\u00b0 x 7\u00b0 FWHM."]
[1.3845727443695068, 4.4041266441345215, "The WDT Function of the Phoenix EPS Electrical Power System is Count up to 12 hours then power cycle the entire spacecraft for 10 seconds."]
[3.043422222137451, 5.870975494384766, "The Small Size, Low Mass, Low Power Consumption of the MTP Transponder is True."]
[6.592183589935303, -0.1394067257642746, "The Launch Date of the PSLV-C32/IRNSS-1F Satellite is March 10, 2016."]
[2.395777940750122, 4.453749656677246, "The Worst-Case Depth-of-Discharge of the Power Subsystem Satellite System is Well below the limit allowed by FP (Fault Protection)."]
[6.377674102783203, 8.505035400390625, "The Swath Width of the SMMR Microwave Radiometer is Approximately 600 km."]
[8.44681453704834, 4.485942840576172, "The Swath Width of the QuickBird-2 Satellite is 16.5 km."]
[9.546509742736816, 8.696516036987305, "The Type of the Telescope Optical Instrument is Off-axis three mirror anastigmat type (TMA)."]
[3.6465797424316406, 6.5771660804748535, "The Data Rate of the S-band Frequency Band is 4 kbit/s."]
[10.463288307189941, -1.0108836889266968, "The Mass of the Microsat of ISRO Microsatellite is 100 kg."]
[9.245420455932617, 7.925325870513916, "The IR Detector Temperature of the OCTS Sensor is 100 K."]
[12.176300048828125, 2.1372733116149902, "The Sample Stowage of the OSIRIS-REx Spacecraft is Originally scheduled for Nov. 2."]
[4.286116123199463, 6.404208183288574, "The Frequency Band of the X-band downlink transmitters Downlink Transmitters is X-band."]
[3.599872350692749, 6.31068754196167, "The TT&C Uplink Data Rate of the RF Communications Communication Subsystem is 125 kbit/s."]
[3.486985683441162, 5.375675201416016, "The On-board Storage Capacity of the ALOS-3 Satellite is Greater than 200 Gbit."]
[5.932224273681641, 2.718747854232788, "The CEO of the Galileo 2nd Generation Satellites Satellite is Herv\u00e9 Derrey."]
[8.578924179077148, 6.8416428565979, "The Manufacturer of the Magnetometer Sensor is Honeywell."]
[6.49565315246582, 0.7982653379440308, "The Mission Status of the TET-1 Satellite is On-Orbit Verification."]
[9.895535469055176, 7.151708126068115, "The Component Manufacturing of the Structure General is Machining components from solid."]
[9.332612991333008, 9.614470481872559, "The Focusing Method of the Camera Camera is Adjusting the focal plane position resulting from the adjustment of the flat mirror assembly position."]
[6.0306196212768555, 0.6481952667236328, "The Image Capture Date of the MarCO CubeSat is 22 October 2018."]
[8.10912799835205, 7.684298992156982, "The Manufacturer of the DRF Radiation and Ultraviolet Detector is Nuclear Physics institute (NIIYaF) of the Moscow State University (MSU)."]
[4.890321731567383, 1.6017345190048218, "The Plane Spacing of the FormoSat-3/COSMIC-1 Satellite Constellation is 24\u00ba."]
[7.6700921058654785, 7.682283878326416, "The Goal of the Ma_MISS Spectrometer is Study the martian subsurface environment."]
[4.937741279602051, 9.195516586303711, "The Provider of the Seismic Experiment for Interior Structure (SEIS) Seismometer is Centre National d'\u00c9tudes Spatiales (CNES)."]
[9.178860664367676, 9.152397155761719, "The Across-track FOV of the Telescope Optical Instrument is \u00b11.31\u00b0."]
[3.8618357181549072, 5.691237449645996, "The Source Data Rate of the Payload Satellite Component is 336 Mbit/s."]
[7.65265417098999, 0.6298067569732666, "The Launch Date of the SEASAT Satellite is June 27, 1978."]
[9.451900482177734, 5.776889324188232, "The Function of the Hysteresis (Memory) Material Attitude Control is Memorizes the current magnetic field and resists changes in KySat-2's orientation."]
[7.4578375816345215, 8.643577575683594, "The Servo Bandwidths of the Guider Instrument is 0 to a few Hz (platform), <50 Hz (prime mirror fine guiding)."]
[6.024599552154541, 3.58767032623291, "The OBR of the Payload Satellite Payload is Special Operations, one unit only (emergency use)."]
[7.292663097381592, -0.7197728157043457, "The Scatterometer of the CYGNSS Satellite is OSCAT and ASCAT."]
[8.955893516540527, 2.7165002822875977, "The Conference Date of the GCOM-W1 Satellite is 5-9 September 2011."]
[6.62766695022583, 5.126311302185059, "The Stability of the Satnav Signals Signal is Highly stable."]
[8.139617919921875, 10.094121932983398, "The Provider of the CAVIS Imager is BATC (Ball Aerospace and Technologies Corporation)."]
[3.4916598796844482, 5.755399703979492, "The Data Transfer Interfaces of the UVN-DEMs and SWIR modules FPGA-based modules is 140 Mbit/s Channel Link interfaces, 80 Mbit/s SpaceWire interface."]
[6.3003315925598145, 2.9985194206237793, "The Manufacturer of the InSight Spacecraft is Lockheed Martin Space, Denver."]
[9.699532508850098, 2.8288960456848145, "The Jacobi Constants Range of the Quasi-Halo Orbits Orbit is Cj = 3.04 to Cj = 3.1613263."]
[10.175644874572754, 4.513823509216309, "The Propulsion System of the Clementine Spacecraft is Non-propellant hydrazine system for attitude control."]
[6.678539276123047, 4.433157920837402, "The Monitoring Capabilities of the Copernicus Sentinel-3 Satellite is Wildfires, land use, vegetation state, sea surface temperature, sea surface color, sea surface height."]
[9.685354232788086, 1.6102041006088257, "The Repeat Cycle of the Satellite Satellite is 22 days."]
[3.8011205196380615, 4.639589786529541, "The Radiation Hardened of the MCM (Multi-Tip-Module) Main On-board Computer is True."]
[7.942936420440674, 7.991034030914307, "The Current Detection Scale Sizes of the MGF Instrument is 100 m or larger."]
[2.1442151069641113, 4.6468186378479, "The Average Power of the Payload Satellite Payload is 1 kW."]
[7.635108947753906, 4.890252113342285, "The Multi-function component assembly of the BEESAT-3 Satellite is Yes."]
[6.364510536193848, 4.159151554107666, "The Collection Mode of the QuakeSat Satellite is Unknown."]
[8.703472137451172, 3.304042339324951, "The Gradiometer Instrument Position of the GOCE Satellite is Near the Centre of Mass."]
[3.2429425716400146, 5.313748836517334, "The Capacity of the HSDR Data Recorder is 16 GByte."]
[9.01167106628418, 3.2290167808532715, "The Spacecraft Provider of the PTD series Satellite is Terran Orbital."]
[7.187001705169678, 8.162313461303711, "The Maintenance Schedule of the COSIMA Mass Spectrometer is Checkouts every 6 months."]
[8.766508102416992, 3.630064010620117, "The Relative Orbit of the TSX and TDX Satellites is TDX has a relative orbit to TSX."]
[10.29492473602295, 4.979391098022461, "The Thruster of the PLATiNO-2 Satellite is HT 100."]
[9.109969139099121, 9.39163875579834, "The FOV of the FSS Photodiode Detector is 128\u00ba x 128\u00ba."]
[9.962221145629883, 3.0257656574249268, "The Orbit of the NanoRacks CubeSat Satellite is Near-circular orbit of the ISS, altitude of ~400 km, inclination of 51.6o."]
[8.33122730255127, 7.752084255218506, "The Purpose of the LPT Radiation Environment Characterization Instrument is Improve the radiation environment knowledge and characterize the local radiation environment."]
[7.38135290145874, 1.794930100440979, "The Publication Date of the IceCube-Gen2 Satellite is August 2020."]
[5.02568244934082, 4.660943031311035, "The Use of the ROBUSTA ground station Ground Station is Future GENSO (Global Educational Network for Satellite Operation) use."]
[6.132998466491699, 3.244323968887329, "The Development Oversight of the Galileo Second Generation Satellite System is ESA."]
[10.713004112243652, 7.349727630615234, "The Energy Range of the X-ray Imager Instrument is 0.1\u20132 keV."]
[7.666492462158203, 0.016451489180326462, "The Docking System Compatibility of the MEV-1 Satellite is 80 percent of all geosynchronous satellites."]
[11.929034233093262, 2.3561959266662598, "The Lighting Requirement of the OSIRIS-REx Spacecraft is At least a 5\u00ba elevation."]
[8.627647399902344, 0.283049613237381, "The Handover to Crew-4 of the Crew-3 Spacecraft is Timed to maintain a U.S. presence on board."]
[8.467259407043457, 7.4199910163879395, "The Sampling Rate of the ULF Sensor Sensor is 10 Hz."]
[6.254930019378662, 2.1567556858062744, "The Platform of the G\u00f6kt\u00fcrk-1A Satellite is Proteus."]
[10.075959205627441, 1.500150203704834, "The Duration of the Asteroid Day TV Online Program is Five hours."]
[6.373224258422852, 2.834334135055542, "The Sponsor of the DebriSat project Satellite is NASA and DoD."]
[7.348758697509766, 8.909988403320312, "The Spatial Resolution (PAN) of the PP Instrument is 2.5 m."]
[4.794989109039307, 0.8769655823707581, "The Funding Raised of the Xona Company is About $10 million."]
[6.530020713806152, 7.541235446929932, "The Deliverables of the Laser Team Team is ETU laser, three flight units, and a flight spare."]
[4.164861679077148, 5.442854404449463, "The Data Interface of the NSat Satellite is UART and I2C."]
[5.033167839050293, 4.661087989807129, "The Control Ground Segment of the Ground Segment Communication is CNES station network."]
[13.046192169189453, 4.106990337371826, "The Variable Stars of the Gaia Satellite is 10 million."]
[8.363883972167969, 9.673782348632812, "The Detector Array of the X-ray Spectrometer Spectrometer is 36-pixel."]
[6.277776718139648, 7.470022678375244, "The Components of the DBCP Pseudo-depolarizer is Four wedges of birefringent material."]
[10.678349494934082, 5.27732515335083, "The Intersatellite Link Data Rate of the CNAPS Propulsion System is 10 kbit/s."]
[4.939115524291992, 5.00154972076416, "The Technology of the EARS System is DVB-S2."]
[9.734091758728027, -0.7262239456176758, "The Sensor Complement of the BX-1 Microsatellite is WFOV (Wide Field of View) and a NFOV (Narrow Field of View) camera."]
[5.000053882598877, -0.14469970762729645, "The Broadband Start of the OneWeb Satellite Constellation is Early 2022."]
[11.759258270263672, -0.9268159866333008, "The Mass of the Cygnus capsule mass simulator Payload is ~3800 kg."]
[7.817885875701904, 6.010011672973633, "The Full Calibration Mode Frequency of the TRUTHS Satellite is Bi-monthly."]
[11.226350784301758, 2.9187533855438232, "The Location of the Crater Surface Feature is 55\u00ba16'51.6\"N/106\u00ba25'3.4\"W."]
[7.6654052734375, 3.645711660385132, "The Data Quality Assessment of the Landsat-7 ETM+ Satellite is Not provided."]
[10.46368408203125, 4.808622360229492, "The Hydrazine Capacity of the Propulsion Subsystem Propulsion is Up to 28 kg."]
[6.299215316772461, 9.844301223754883, "The Mass of the Instrument Spectral Imager is 120 kg."]
[7.413601398468018, -0.31893929839134216, "The Release Date of the HTV-6/Kounotori-6 Cargo Ship is January 23, 2017."]
[8.279250144958496, 9.169937133789062, "The Pixels per FWHM of the Spectrometer Instrument is 715."]
[6.4901957511901855, 3.91326904296875, "The Next Deployment Test Location of the Copernicus Sentinel-1C Satellite is France."]
[10.488435745239258, -1.1306592226028442, "The Mass of the SEAM Nanosatellite is 4.7 kg."]
[7.3463311195373535, 6.949240207672119, "The Operation Start Date of the MAP-PACE Plasma Analyzer is 14 December 2007."]
[10.357348442077637, 5.014664649963379, "The Pressure of the Steam Propulsion Unit Propulsion is Atmospheric pressure."]
[6.999316692352295, 1.1761877536773682, "The Agreement Date of the Spire Global Satellite Operator is August 14, 2019."]
[9.398041725158691, 4.3805975914001465, "The Printed Circuit Board Thickness of the Sprite Tiny Spacecraft is A few millimeters."]
[7.167736053466797, 5.0408854484558105, "The Total CO2 Equivalent Mitigated of the GHGSat Company is Over 10 million tons."]
[9.69204330444336, 9.096107482910156, "The Exposure Time of the Active Regions Imaging Device is < 100 ms."]
[9.718602180480957, -0.0990423634648323, "The LTDN of the LitianicaSAT-2 Nanosatellite is 9:30 hours."]
[2.134211778640747, 4.559767246246338, "The Power of the Spacecraft bus Satellite is 3.8 kW."]
[9.656323432922363, 1.4302928447723389, "The Pass Prediction Accuracy of the SpinSat Satellite is About three weeks."]
[10.423407554626465, 2.6077582836151123, "The Apogee of the COMPASS-2 Satellite is 494 km."]
[10.66608715057373, -1.091238021850586, "The Mass of the Tyvak-0171 Minisatellite is 138 kg."]
[4.48048734664917, 4.488051891326904, "The Number of Nodes of the TacSat-4 SpaceWire Link Communication Link is 2."]
[7.385014533996582, 5.164068698883057, "The CO2 Relative Accuracy of the GOSAT Satellite is 1%."]
[11.207474708557129, -1.5183273553848267, "The Mass of the SPACE HAUC CubeSat is 4 kg."]
[6.361703872680664, 7.594220161437988, "The Receiver Function of the SILEX Laser Communication System is Power detection device."]
[6.264339923858643, 6.974687099456787, "The Measurement Technique of the RISE Instrument is Doppler shift of radio signals."]
[3.6711039543151855, 6.828089237213135, "The Mass of the Myriad RF board RF Board is 50 g."]
[6.2955756187438965, 6.525789260864258, "The Every two days of the Radar Data Interval is At an interval of every two days."]
[4.1638312339782715, 6.580281734466553, "The Uplink Frequency of the Cadet-U UHF radio RF Communication Device is 449.75 MHz."]
[5.206343173980713, 1.8428075313568115, "The Number of the Columbus ESA ISS Science & System Operations Report is 78."]
[4.891801357269287, 9.17848014831543, "The Deployment Date on Mars of the Seismic Experiment for Interior Structure (SEIS) Seismometer is Late 2018."]
[6.580197811126709, 0.3593748211860657, "The Scheduled Launch Date of the CBERS-3 Satellite is 2012."]
[7.63261079788208, 0.5631028413772583, "The Mission Move Forward Date of the DSCOVR Satellite is 2015."]
[8.623295783996582, 6.878068447113037, "The Sampling Rates of the FGM Fluxgate Magnetometer is 32 Hz (both sensors active) or 64 Hz (one sensor active)."]
[11.741713523864746, 1.2051206827163696, "The Relay Hazard Avoidance Method of the Chang'e-3 lander Lander is Large-scale rough-hazard avoidance, three-dimensional imaging in hovering status, small-scale precise-hazard avoidance of the final landing site."]
[4.487396717071533, 7.101707458496094, "The Size of the Transmitter Communication Device is 230 mm x 136 mm x 30 mm."]
[7.874954700469971, 9.043465614318848, "The Spectral Resolution of the EO System Earth Observation System is <8 nm."]
[9.641460418701172, 8.642451286315918, "The Lightweighting of the PP Twin Telescopes Telescope is Up to 72%."]
[6.7952423095703125, 3.954094886779785, "The Eclipse Period of the QuakeSat Satellite is Current."]
[7.868234157562256, 10.00290584564209, "The Array Size of the VNIR Detector is 40 x 640."]
[9.423074722290039, 2.84550404548645, "The Landing of the OMOTENASHI Satellite is On the moon."]
[4.916507720947266, 4.268560409545898, "The Components of the FDIR System Failure Detection, Isolation and Recovery System is On-ground system, Automation system, MOIS Event Monitor."]
[11.687274932861328, 4.693971633911133, "The Brightness of Star at High Noon of the Kepler-186f Exoplanet is As bright as our sun appears to us about an hour before sunset."]
[7.002117156982422, -0.07238751649856567, "The End of Life Date of the LADEE Satellite is April 18, 2014."]
[6.805970191955566, 1.3171195983886719, "The Workshop Date of the Peregrine Satellite is April 18-20, 2012."]
[12.158488273620605, 3.276475191116333, "The Orbit Inclination of the HY-2B Satellite is 99.3\u00ba."]
[9.027076721191406, 5.22283411026001, "The Detection Target of the SVOM Attitude Satellite Attitude is GRB on the night side."]
[9.966096878051758, 1.5473463535308838, "The Dwell Time of the IRS Sounder Satellite is About 9 seconds."]
[7.167868614196777, 5.586672306060791, "The Global Wind Field Measurement of the Atmospheric Dynamics Mission Satellite Mission is True."]
[7.085025787353516, 0.10844437777996063, "The Launch Date of the VRSS-1 Satellite is Sept. 29, 2012."]
[7.781929016113281, 10.305581092834473, "The Spectral Channels of the SEVIRI Spectral Imager is 12."]
[5.670670986175537, 9.513080596923828, "The Mass of the SEIS Instrument Seismometer is 29.5 kg."]
[7.950501441955566, 4.518713474273682, "The Spectral Channels of the Resurs-P1 Imaging Satellite is Seven."]
[11.55733585357666, 6.069854259490967, "The Activation Date of the LAXPCs X-ray Proportional Counters is October 2015."]
[7.4533305168151855, 5.102565765380859, "The Noctilucent Cloud Observation Locations of the AIM Satellite is Arctic, Antarctica, Utah, Colorado."]
[8.460643768310547, 6.184208869934082, "The Function of the IBS LR Launch Restraint is 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."]
[7.841910362243652, 8.895479202270508, "The Spectral Range of the ELVIS Spectrometer is 200-650 nm."]
[7.60802698135376, 9.100142478942871, "The Resolving Power of the Atmospheric Chemistry Suite Spectrometer is 10,000 or more."]
[10.159919738769531, 3.3586885929107666, "The Cold Start Time of the DORIS Receiver is Less than 1 orbit."]
[4.087811470031738, 4.384515762329102, "The Process Management of the FreeRTOS Real-time Operating System is Separation of a program in several processes, managing the assignment of processor internal resources like processor time and memory to the various processes."]
[9.192564964294434, 3.2592601776123047, "The Orbit Type of the Odin Satellite is Sun-synchronous polar orbit."]
[8.61805534362793, 8.89640998840332, "The Wavefront Error of the Sentinel-4 GRU Grating Reflection Unit is 6.0 nm (rms)."]
[9.309402465820312, 9.181417465209961, "The Paraxial Focal Length (mm) of the FCI-TA Instrument is 1650."]
[4.526122093200684, 4.01999044418335, "The Components of the Spacecraft Plug-n-Play Avionics (SPA) Standards is Electronic datasheet."]
[9.382569313049316, 1.5927335023880005, "The Yaw Maneuvers Frequency of the ERBE Instrument is Approximately every 36 days."]
[9.365586280822754, -0.583827555179596, "The Functionality of the HISats Nanosatellites is Independent and fully functional with their own propulsion, power, navigation, data processing, communications and payload accommodations."]
[7.471108436584473, 8.151161193847656, "The Altitude Range of the Air Density Measurement Device Instrument is ~200 km."]
[11.02151107788086, 3.405020236968994, "The Jupiter's Day of the Juno Spacecraft is About 10 hours."]
[5.4167985916137695, 4.3926897048950195, "The Location of the Ganges Delta River Delta is Bangladesh and the State of West Bengal in India."]
[11.887606620788574, 1.001315712928772, "The Sample Collection of the Chang'e-5 Lunar Mission is Younger than those brought back last century by the Apollo missions."]
[11.975634574890137, 3.391812562942505, "The Orbit Direction of the Space Station Satellite is From west to east."]
[8.69503116607666, 8.854593276977539, "The Number of Optical Elements of the Grating Wheel Assembly Optical Assembly is 8."]
[7.400344371795654, 4.901014804840088, "The Purpose of the Beesat-5,-6,-7,-8 smallsats Satellite is Unknown."]
[5.801656723022461, 8.18283748626709, "The Bandwidth (GHz) of the ICI-10 Radiometer is 2.4."]
[10.292272567749023, 3.138288974761963, "The Altitude of the Main Payload Satellite is ~661 km."]
[11.876364707946777, -1.1057162284851074, "The Launch Mass of the ACTS/TOS Communication Technology Satellite is 2800 kg."]
[6.942327499389648, 3.174726724624634, "The Mission Status of the IRS-P6 Satellite is Mission Complete."]
[11.03292465209961, 2.857637405395508, "The Volume of the Lake Atat\u00fcrk Dam Reservoir is 48.7 km3."]
[7.037230491638184, 8.865710258483887, "The Dynamic Range (Infrared Channel) of the VIRR Instrument is 180-330 K (scene temperature)."]
[5.395087718963623, 3.2270877361297607, "The Number of Antennas of the Heinrich Hertz Satellite is 8."]
[4.731078624725342, 4.544701099395752, "The Objective of the DCS Data Collection System is Collect and relay environmental data from unattended land- and ocean-based automatic data collection platforms."]
[6.90523624420166, 4.967405319213867, "The Emissions Contribution in 2020 of the Sudd wetlands in South Sudan Wetlands is Unknown."]
[4.436728000640869, 5.279510498046875, "The Connection of the TTC End-to-End Tests Test Type is Hardwired connections to the spacecraft TTC transmitters and the data umbilical will be connected."]
[1.9480077028274536, 3.8236570358276367, "The Provider of the Flexible thin-layer solar cells Solar Cells is Solarion GmbH."]
[3.3474230766296387, 6.51448392868042, "The Optical Transmit Power of the Optical link Communication System is 2.2 W."]
[4.439611911773682, 6.295136451721191, "The Band of the Electra Radio is UHF."]
[11.680197715759277, -1.194029688835144, "The Total Mass of the Spacecraft Satellite is 236 kg."]
[8.353201866149902, 9.129523277282715, "The Number of Bands of the R3 Sensor Sensor is 6."]
[6.771310806274414, 8.671843528747559, "The LI Optical Head Envelope of the LI Instrument is 718 mm x 1200 mm x 1456 mm."]
[11.480986595153809, 2.621758460998535, "The Water Loss Date of the Asteroid 162173 Ryugu Asteroid is Unknown."]
[6.214059829711914, 5.890625, "The Imaging Modes of the TSX-SAR Satellite is Spotlight (SL), Spotlight High Resolution (HS), Experimental Mode."]
[7.227896213531494, 0.6619786620140076, "The Failure Date of the NEOSSat Satellite is Late 2016."]
[6.312524318695068, 9.965996742248535, "The Mass of the Lens Assembly Lens Assembly is 266 g."]
[9.291605949401855, 3.254115104675293, "The Orbit Type of the ANUSat Satellite is Near-circular."]
[5.98276424407959, 9.568541526794434, "The Mass of the KaRIN Instrument is ~294 kg."]
[7.135563850402832, 5.637041091918945, "The Utilization of the ESP-MACCS Satellite is Quantify atmospheric processes in the upper troposphere and stratosphere."]
[4.9597578048706055, 6.029210567474365, "The PSD Limit Frequency of the Payload Satellite Component is Until 6.5Hz."]
[8.126855850219727, 4.155040740966797, "The Darkening of the Satellite Communication is Surfaces on the satellite that scatter light or reflect light diffusely."]
[8.875835418701172, 1.3406846523284912, "The Extended Mission End Date of the Van Allen Probes Satellite is June 2019."]
[6.874733924865723, 5.5271525382995605, "The Measurement Depth of the SMAP Satellite is 5 cm."]
[9.727890968322754, 7.170653820037842, "The Operational Temperature of the Supercapacitor Energy Storage Device is -40\u00b0C to +70\u00b0C."]
[7.066112995147705, 9.783265113830566, "The Spectral Range (\u00b5m) of the Band 7 Spectral Band is 0.43 - 0.48."]
[7.119458198547363, 6.261472702026367, "The Calibration/Validation of the WindSat Spaceborne Polarimetric Radiometer is Special Issue (18 papers) on the WindSat Spaceborne Polarimetric Radiometer -Calibration/Validation and Wind Vector Retrieval."]
[6.034564018249512, 2.1464054584503174, "The Launch Site of the CHAMP Satellite is Plesetsk Cosmodrome in Russia."]
[11.701536178588867, -1.2014020681381226, "The Chassis Mass of the Supernova-Beta Satellite is 1.64 kg."]
[9.603001594543457, 8.058578491210938, "The Device Mass of the Gamma-ray Counter Detector is 260 g / unit."]
[7.092534065246582, 2.521813154220581, "The URL of the Dellingr Satellite is https://www.nasa.gov/sites/default/files/atoms/files/cuttingedge_-_vol._13_issue_1_-_fall_2016.pdf."]
[9.299543380737305, 6.428243160247803, "The Type of the Star Tracker Technology Demonstration Payload is Unknown."]
[7.114894866943359, 4.331457138061523, "The Deployment Camera Verification of the Spacecraft Satellite is Completed."]
[6.992610931396484, 0.8937885761260986, "The Launch Date of the UKube-1 Satellite is July 2014."]
[10.851940155029297, 3.80428147315979, "The Orbital Period of the XMM-Newton Satellite is Exactly two times the Earth rotation period."]
[3.6154401302337646, 4.797733306884766, "The Timer Interrupt Frequency of the AT91SAM9G20 Microprocessor is 1 millisecond."]
[10.42270278930664, 7.246842384338379, "The Design of the TEMBOTM EMC Material is Elastic Memory Composite."]
[9.649821281433105, 5.994608402252197, "The Computer of the ADCS Attitude Determination and Control System is ARM 7 MCU."]
[8.361743927001953, 1.5633004903793335, "The Operation Period of the Rosetta Satellite is August 2014 to September 2016."]
[4.780847072601318, 4.717565059661865, "The Beacon Detection of the Ground System Communication System is At least one beacon per pass."]
[5.420799255371094, 1.3123763799667358, "The First Stage Flights of the Falcon 9 Rocket is 7."]
[8.12331771850586, 10.024473190307617, "The Maximum Upper Band Edge of the MS1 (NIR1) Imager is 901 nm."]
[7.1926350593566895, 0.7097850441932678, "The End of Mission Date of the CHAMP Satellite is September 19, 2010."]
[10.277828216552734, 8.35135555267334, "The Conference Presentation of the Solar Orbiter/METIS Coronagraph/Spectrometer is The optimization of the inverted occulter."]
[8.125105857849121, 4.012058258056641, "The Presentation of the POLO Satellite is http://smsc.cnes.fr/PLEIADES/Fr/PDF/presentation_pleiades.pdf."]
[8.990824699401855, 10.357927322387695, "The Spectral Range of the LWIR Cameras Camera is 7.5 - 13.5 \u00b5m."]
[11.129026412963867, 6.292236328125, "The Sources of the Neutrons Radiation is Galactic Cosmic Radiation (GCR), Earth's radiation belt, Solar Particle Events (SPE)."]
[11.376375198364258, 3.7583072185516357, "The Time to Fly Beyond Oort Cloud of the Voyager 2 Space Probe is Possibly 30,000 years."]
[8.997039794921875, 6.590909957885742, "The Range of the Rate gyro Sensor is \u00b15\u00ba/s."]
[7.871007442474365, 7.219207286834717, "The Calibration Parameters of the SOFIE Instrument is Measurement background and noise, FOV, response linearity, relative spectral response, time response, absolute gain, difference signal gain."]
[7.062254428863525, 0.16041307151317596, "The International Astronautical Congress Date of the VRSS-1 Satellite is Sept. 23-27, 2013."]
[5.487720966339111, 2.683859348297119, "The GMDSS Service Provider of the Iridium Satellite Communication Provider is Iridium."]
[7.3379058837890625, 9.152417182922363, "The Ground Coverage of the Scanner Assembly Instrument is 96 km."]
[10.455072402954102, 5.936356067657471, "The Funding Agency of the Microage Experiment is UK Space Agency."]
[3.596808433532715, 6.275877475738525, "The Uplink Rate of the SGLS Link Communication System is 2 kbit/s."]
[3.9376590251922607, 4.528853416442871, "The Hardware and Software Design of the PDH Payload Data Handling is Exactly the same as OBC."]
[10.64737319946289, 9.200368881225586, "The Image Capture Date of the CaSSIS Instrument is 22 December 2018."]
[8.941631317138672, 6.1238508224487305, "The Technology of the MARIN Inertial Measuring Unit is Microelectromechanical systems (MEMS)."]
[7.169096946716309, 4.255512714385986, "The Measurement Category of the Badr-B Satellite is Gravity, Magnetic and Geodynamic measurements."]
[10.457810401916504, -0.9926535487174988, "The Mass of the DIWATA-1 Microsatellite is 50kg."]
[4.332479476928711, 5.926522731781006, "The DT Band of the DTS Data Transmission Subsystem is X-band."]
[10.468929290771484, 4.759490966796875, "The Hydrazine Quantity of the Hydrazine system Orbit control subsystem is 4.5 kg."]
[4.789273738861084, 5.921543598175049, "The Quantity of the 12-Port Ethernet switches Network Equipment is 2 units."]
[7.57512903213501, 0.4875763952732086, "The Launch Readiness Capability of the JPSS Joint Polar Satellite System is FY 2015 and FY 2018."]
[9.590861320495605, 7.858035564422607, "The Energy Range for Ions of the MagEIS Magnetic Electron Ion Spectrometer is 20 keV to 1 MeV."]
[7.564525127410889, 8.53139591217041, "The SNR of the UV/VIS Spectrometer Spectrometer is >12."]
[4.303772926330566, 2.4361941814422607, "The Preorder Count in India of the Starlink Satellite Internet Service is Over 5,000."]
[11.737300872802734, 4.528684616088867, "The Explosion Frequency of the Massive Star Star Type is About every fifty years."]
[11.733243942260742, -1.1439327001571655, "The Per spacecraft mass of the  WorldView Legion Satellite System is 750kg."]
[6.819405555725098, 5.506472587585449, "The Purpose of the SMAP Satellite is Provide information on water availability and environmental stress for estimating plant productivity and potential yield."]
[4.158413410186768, 6.595945358276367, "The Frequency Stability of the Receiver Communication System is \u00b11 x10 -9 dB."]
[6.386134147644043, 3.43833327293396, "The Affiliated Organizations of the MANTIS Earth Observation Satellite is ESA, UK Space Agency, Open Cosmos, Satlantis, Terrabotics."]
[1.1996235847473145, 4.209084510803223, "The Energy Comparison of the Lightning Natural Phenomenon is 1 bolt of ordinary lightning = enough energy to charge 20 electric cars."]
[6.677794456481934, 3.299281358718872, "The Science Control Location of the Chandra X-ray Center Center is Cambridge, Massachusetts."]
[6.598424434661865, 4.558122634887695, "The Objective of the Sentinel-1 Satellite is Assure C-band SAR data continuity for the user community currently provided by Envisat and ERS-2."]
[7.8714399337768555, 4.5165629386901855, "The NDVI Map Spatial Resolution of the Landsat-8 Satellite is Unknown."]
[7.538907527923584, 8.549104690551758, "The MTF of the Instrument Spectrometer is > 0.2 @ Nyquist frequency."]
[4.407410621643066, 7.643955707550049, "The Bandwidth of the A/D converter Data Converter is 500 MHz."]
[5.059292793273926, 2.7206335067749023, "The Services of the Hellas Sat 3 Satellite is Direct-to-home (DTH) TV broadcast and telecommunications services, distribution of high-definition (HD) and ultra-high definition (UHD) video content."]
[3.841486692428589, 6.4877824783325195, "The Communication Link Speed of the GEO LCT Laser Communication Terminal is 2.8 Gbit/s."]
[6.288794994354248, 3.7077763080596924, "The Mission Type of the MetOp Second Generation Satellite is Weather forecast and climate monitoring."]
[9.506240844726562, -0.558230459690094, "The Imaging Improvement of the Nanosatellite System Satellite System is Better imagery at lower cost."]
[4.991044998168945, 7.496255874633789, "The Data Rate of the DORIS Instrument is 4 kbit/s."]
[9.038664817810059, 4.32011604309082, "The Face sheets thickness of the Bus structure Satellite Structure is t = 0.8 mm."]
[6.138056755065918, 6.10979700088501, "The Mission Objectives of the SAR-RCM Synthetic Aperture Radar is Monitoring of glacier cover, motion and topography, ice sheet and land surface topography, and sea-ice cover and type."]
[10.375804901123047, 5.678776264190674, "The Deployment Method of the SEDS Tether Experiment Demonstration Program is Deployer system."]
[7.186079978942871, 0.512281060218811, "The End of Operations of the SPOT-1 Satellite is November 2003."]
[7.410016059875488, 4.064225196838379, "The Orbital Plane of the Sentinel-1A and Sentinel-1B Satellites is Same."]
[7.008286952972412, 2.1729462146759033, "The Expected Service Start of the Konnect Satellite is Fall."]
[10.098458290100098, 3.0794413089752197, "The Altitude of the Resurs-P1 Satellite is 475 km."]
[8.175912857055664, 0.9856158494949341, "The Duration of the NSSL Phase 2 Launch Program is 2022 until 2027."]
[5.850091457366943, 6.8763227462768555, "The Image Size of the SIR-C Phased Array is 100 km (azimuth, flight direction) x 50 km (swath)."]
[8.22344970703125, 8.640384674072266, "The Configuration Change of the NIRISS Near-Infrared Slitless Spectrometer is Summer of 2011."]
[5.851213455200195, 6.426551342010498, "The Center Frequency of the CSG-SAR Synthetic Aperture Radar is 9.6 GHz."]
[6.758825778961182, 0.47803258895874023, "The Connection Check Date of the MetOp-C Satellite is 4 October 2018."]
[4.462401390075684, 6.381716728210449, "The Function of the RFGeo Product is Identifies and geolocates RF signals."]
[8.414437294006348, 7.279589653015137, "The Position of the Electric Field Antennas Sensor is Extends beyond the TPS."]
[6.612087726593018, 1.8877798318862915, "The Observation Date of the ENVISAT satellite Satellite is 2006."]
[10.210053443908691, 6.580341815948486, "The Energy Range of the RHESSI Satellite is 3 keV - 17 MeV."]
[10.506731986999512, 8.449241638183594, "The Volume Comparison of the MiniCOR Coronagraph is ~10 smaller volume than LASCO C3."]
[7.595410346984863, 2.578869581222534, "The Target of the Hera Satellite is Didymos."]
[9.444275856018066, 1.8156810998916626, "The Revisit Rate of the Planet SkySats Satellite is As high as 10 times per day."]
[5.930647850036621, 3.2552855014801025, "The Software Load Location of the NigeriaSat-2 Satellite is On-Board Computer."]
[7.416322231292725, 6.863296985626221, "The Installation Time of the DESIS Instrument is One day."]
[8.37962532043457, 8.250253677368164, "The Number of Detectors of the SBUV Spectrometer is 3."]
[6.167686462402344, 6.650771141052246, "The Operation Period of the S-193 Radar System is Over 600 days."]
[6.25682258605957, 4.583612442016602, "The Applications of the SAR Satellites Satellite is Defense and intelligence, supply chain, insurance, maritime."]
[12.110489845275879, 3.2577195167541504, "The Orbit Inclination of the GF-3 Satellite Satellite is 98.41\u00ba."]
[10.878667831420898, 5.711156368255615, "The Technique Developers of the Solar Flare Solar Event is Charles Lindsey and Douglas Braun."]
[9.716164588928223, 8.437546730041504, "The Application of the Compact off-axis telescope Telescope is Satellite-borne instrument for atmospheric research."]
[7.501113414764404, 5.251026630401611, "The Calibration of the HY-2A Satellite Satellite is Unknown."]
[6.911158084869385, 5.372427940368652, "The Additional Capability of the SMOS Satellite is Map the thickness of ice floating in the polar seas."]
[7.430911540985107, 10.007780075073242, "The Spectral Range of the HySI Hyperspectral Imager is 400-950 nm (VNIR)."]
[4.854263782501221, 1.8491566181182861, "The Number of Paths of the Payload Hosting Paths Satellite is Two."]
[4.227300643920898, 5.761331558227539, "The Uplink and Downlink Frequency of the NEMO-AM Satellite is S-band."]
[8.127854347229004, 5.148571968078613, "The DC electric field measurement of the Geotail spacecraft Spacecraft is Unknown."]
[7.111682891845703, 2.8219494819641113, "The URL of the SPOT 6 Satellite is http://www.astrium-geo.com/files/pmedia/edited/r18072_9_spot_6_technical_sheet.pdf."]
[5.986556053161621, 4.839613437652588, "The Mission Status of the OSIRISv3 System is Unknown."]
[5.128357410430908, 6.256650924682617, "The Design of the Antenna array Antenna is Adaptive nulling design, 4 elements, f c =5 GHz."]
[7.491182804107666, 7.3636155128479, "The Detection Capability of the OMI Satellite Instrument is Gas and Oil Facilities Emissions."]
[4.165228366851807, 5.2037129402160645, "The Function of the Baseband Processor Processor is Demodulation, storage and remodulation of LBR (Low Burst Rate) data."]
[4.783143997192383, 0.8766000866889954, "The Total Cost of the Satellogic Satellite Constellation is $20 million in total per year."]
[7.787906169891357, 8.15421199798584, "The Altitude Error Type of the OMPS Sensor is Rigid vertical shift."]
[4.160554885864258, 4.927894115447998, "The Presentation Date of the Data Volume Increase Solution Data Communication System is May 4-7, 2009."]
[9.231402397155762, 7.411917686462402, "The Operating Temperature of the Sensor Gas Sensor is Approximately 660\u00b0C."]
[8.114642143249512, 0.3543512523174286, "The Data Collection of the ISS-RapidScat Satellite Instrument is Started on October 6, 2014."]
[3.3632779121398926, 5.15806245803833, "The Memory Module Capacity of the IRIS Satellite is 8 Gbit."]
[7.104760646820068, 0.23434405028820038, "The Planned Launch of the Resurs-P4 Satellite is 2023."]
[10.707502365112305, 2.891435384750366, "The Argument of Perigee of the Molniya Orbit Orbit is 270\u00b0."]
[6.941055774688721, 2.497713327407837, "The URL of the PROBA-V-CC Satellite is https://space.oscar.wmo.int/satellites/view/proba_v_cc."]
[9.612001419067383, 4.175495147705078, "The Diameter of the Tianhe Space Station Module is 4.2 meters."]
[11.747589111328125, 1.0089540481567383, "The Rocket Height of the Chang'e-5 Lunar Mission is 57 meters."]
[5.321371555328369, 2.5124266147613525, "The Mission Type of the ArgoMoon CubeSat is EO."]
[7.505255222320557, 8.751575469970703, "The Cross-track Swath of the Nadir total column spectrometer Spectrometer is 50 km x 2800 km."]
[7.825943470001221, 0.2807807922363281, "The Launch Date of the Orbital ATK Mission Space Station Research is 21 May 2018."]
[8.881670951843262, 1.7944040298461914, "The Mercury Orbit Arrival Date of the BepiColombo Satellite is End of 2025."]
[11.698799133300781, -1.2080566883087158, "The Mass of the M2S Satellite is 848 kg."]
[7.870794773101807, 1.8279063701629639, "The Launch Date of the ExoMars Mission is 2020."]
[7.46289587020874, 4.095216751098633, "The Mission Purpose of the CryoSat Satellite is Determine the Fluctuations in Earth's Land and Marine Ice Fields."]
[2.2121963500976562, 4.500243186950684, "The Power Capacity of the Bus Satellite Component is 140 W."]
[7.8278632164001465, 9.819249153137207, "The Bands of the GOES Imager Imager is 1 VIS band, 2 MWIR bands, 2 TIR bands."]
[10.17776107788086, 5.192835330963135, "The Number of Valves of the PROP unit Propulsion System is 6."]
[7.922532558441162, 7.349676132202148, "The Operational Cadence of the Instrument Satellite Instrument is Stare for ~30 seconds."]
[9.84389877319336, 8.755494117736816, "The Focal Length of the ART-XC Instrument Telescope is 2700 mm."]
[4.000049591064453, 5.663171291351318, "The Optical Downlink Rate of the Follow-on Optical Downlink Demonstrators Satellite is Approaching 1 Gbit/s."]
[11.536434173583984, 2.683810234069824, "The Age of the Ryugu asteroid Asteroid is 100 million years old."]
[9.581832885742188, 3.866037130355835, "The Formation Ranges of the CanX-4 Satellite is 1000 m, 500 m, 100 m."]
[7.101108074188232, 4.927030086517334, "The Purpose of the Remote Sensing Satellite Satellite is Remote sensing of terrestrial vegetation fluorescence."]
[7.1182966232299805, 0.696441113948822, "The Launch Date of the Unknown Satellite is Dec. 17, 2015."]
[7.631576061248779, 4.902578830718994, "The Universal TC/TM system of the BEESAT-3 Satellite is Yes."]
[7.849784851074219, 7.06104850769043, "The Observation of the FAUST Instrument is Gas trail behind the cloud."]
[11.737607955932617, -1.1181573867797852, "The Dry Mass of the Spacecraft Satellite is 1400 kg."]
[1.7582916021347046, 4.818973541259766, "The Power Draw of the EPS Electrical Power Subsystem is < 50 mW."]
[7.559866428375244, 5.146459579467773, "The Cloud Brightness Trend of the AIM Satellite is Getting brighter."]
[5.416440486907959, 4.208164215087891, "The Development Locations of the CPE Communications Payload/Experiment is 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."]
[8.227629661560059, 6.321516513824463, "The | of the VIRGO Helioseismology and Solar Irradiance Monitoring Experiment is http://www.ias.u-psud.fr/virgo/."]
[3.4681010246276855, 4.455323696136475, "The FPGA of the PCU Power Control Unit is Actel RTSX32SU-CQ84B."]
[8.889425277709961, 6.625828266143799, "The Measurement Method of the RISE Instrument is Estimation of the precession and nutation of the spin axis."]
[5.319467544555664, 4.401256561279297, "The Location of the PDGS Payload Data-processing Ground Segment is DLR in Oberpfaffenhofen."]
[9.407502174377441, 0.8245617747306824, "The Mission Life of the YouthSat Satellite is 2 years."]
[7.750241279602051, 4.009521484375, "The Daily Imaging Capacity of the SEOSat Satellite is 2,500,000 km2."]
[5.84127950668335, 1.8380893468856812, "The Constellation Purpose of the Kleos Space S.A. Company is Monitoring global events and key locations of interest."]
[11.986101150512695, 4.48922061920166, "The Study Duration of the Blue Ring Nebula Nebula is 16 years."]
[8.840978622436523, 2.94159197807312, "The Delivery Location of the LunaH-Map Spacecraft is NASA's Kennedy Space Center."]
[7.6036152839660645, 2.0044376850128174, "The DOI of the NICER Satellite is 10.1117/12.2056811."]
[8.5386381149292, 9.285804748535156, "The Color of the Optical Elements Components is Light red."]
[10.238715171813965, 3.015998601913452, "The Reentry Plan of the NPP Satellite is Lower the orbit perigee to approximately 50 km and target any surviving debris for open ocean entry."]
[8.272527694702148, 4.805541515350342, "The Optical Axis Displacement of the Satellite Imaging Satellite is \u00b130\u00ba in steps of 2\u00ba."]
[5.7853851318359375, 0.8316270709037781, "The Launch Date of the NanoRacks-QB50 Satellite is April 5, 2017."]
[8.265912055969238, 9.176955223083496, "The Pixels per FWHM of the Spectrometer Instrument is 1220."]
[7.448870658874512, 6.214563369750977, "The Purpose of the CO2 Dry Air Mole Fraction Atmospheric Measurement is Integral constraint on the sum of these in the form of a net flux of CO2 to and from the atmosphere at the surface."]
[7.5873703956604, 6.427140235900879, "The Response to Gravity Wave Activity of the O2 Atmospheric Band airglow and NLC Atmospheric Emissions is Both feature horizontal and vertical structures that are a direct response to gravity wave activity."]
[6.956577777862549, 1.8026447296142578, "The Meeting Date of the Swarm Satellite is April 21, 2017."]
[6.253317832946777, 2.683424472808838, "The Benefits of the Planet Orbit Partner Program is Access to Planet-certified partners with specific domain expertise."]
[6.848180770874023, 1.62307870388031, "The Mission Design of the RapidEye Satellite is Acta Astronautica Volume 56, Issues 1-2, January 2005, pp. 213-219."]
[9.451125144958496, 5.547938346862793, "The Yaw Maneuver Capability of the ADCS Attitude Determination and Control Subsystem is \u00b190\u00ba/180\u00ba."]
[7.610350131988525, 3.9613471031188965, "The Observation Data of the CryoSat-2 Satellite is Changes in ice thickness for March/April 2011, 2012 and 2013."]
[11.810323715209961, -1.0974276065826416, "The Launch Mass of the Spacecraft Satellite is 588 kg."]
[6.99357795715332, 2.4382240772247314, "The URL of the VAMOS Verification System is http://elib.dlr.de/84313/1/IFAC2013_VAMOS_03.pdf."]
[10.109845161437988, 3.1147074699401855, "The Orbit Altitude of the SpaceEye-T Satellite is 600 km."]
[9.16486930847168, 10.498421669006348, "The Zoom Capability of the Zoom-in Camera Camera is Yes."]
[7.306136608123779, 0.5373451113700867, "The Launch Date of the OrbView-1 Satellite is April 1, 1995."]
[9.416589736938477, -0.763620913028717, "The Mission Date of the FedSat Microsatellite is 1998."]
[2.0510730743408203, 3.859333038330078, "The Solar Array of the Orion Spacecraft is 1242 cells per panel."]
[8.941895484924316, 2.423213481903076, "The Function of the Herschel Telescope Telescope is Look deep into space by detecting light emitted in the far-infrared and sub-millimeter regions of the spectrum."]
[4.0373148918151855, 2.367753267288208, "The Bus Size of the CubeSat Satellite is 6U."]
[8.673043251037598, 6.092939853668213, "The Movement of the Earth's Magnetic Field Natural Phenomenon is Up to tens of km every year."]
[7.8550190925598145, 8.02106761932373, "The Measurement Type of the FTS Fourier Transform Spectrometer is Amount of direct sunlight absorbed by atmospheric gases."]
[9.638075828552246, 1.116843819618225, "The Drift Recovery Phase Duration of the CanX-4&5 Satellite is Several Days."]
[9.313277244567871, 6.376774787902832, "The Capabilities of the Procyon star tracker Attitude Determination Device is Excellent rate estimates, \u2018lost in space' capability."]
[5.855189800262451, 6.549383163452148, "The Isolation Method of the KaRIn Radar is Offset feed reflectarray antennas."]
[1.3538738489151, 4.194894790649414, "The Maximum Battery Power Before 100% Depletion of the Satellite Spacecraft is 10 hrs."]
[9.445208549499512, 2.692931652069092, "The Flight Dynamics of the Retrieval of the Eureca Satellite is Unknown."]
[7.278449058532715, 0.9698262214660645, "The Launch Date of the Satellite EO is Announced on 7 October 2021."]
[9.441267013549805, 0.9525452852249146, "The Mission Duration of the PSAT Satellite is 18 months."]
[11.72933578491211, -1.1092121601104736, "The Mass of the Trailblazer spacecraft Satellite is 83.5 kg."]
[8.61691951751709, 9.64167594909668, "The Detector Pixel Count of the Telescope Optical Instrument is 2 k x 1 k pixels."]
[7.148014545440674, 3.2892045974731445, "The Communication Status of the UWE-1 Satellite is No communication signals can be received."]
[10.93071174621582, 2.827810525894165, "The Coordinates of the Tohoku-Kanto earthquake Earthquake is 38.32\u00baN, 142.37\u00baE."]
[10.869087219238281, 5.7090301513671875, "The Developer Affiliation of the Kappa Scheme Flare Prediction Method is Institute for Space-Earth Environmental Research, Nagoya University."]
[9.835168838500977, 9.033652305603027, "The Diameter of the M1 Mirror is 415 mm."]
[11.62838077545166, -1.149711012840271, "The Platform Weight of the Satellite Vu Satellite is 100 kg."]
[5.0680718421936035, 6.972854137420654, "The Center Frequency (GHz) of the Antenna Reflector is 19.35."]
[5.285831928253174, 3.1590356826782227, "The Function of the APEX CubeSat CubeSat is Perform a multispectral mineral survey of its makeup."]
[9.932449340820312, -0.7961687445640564, "The Additional Camera Resolution of the PROBA-1 Microsatellite is 5 m."]
[6.485962867736816, 4.727112293243408, "The Unknown of the CFOSat Ground Segment is Unknown."]
[8.52245044708252, 1.6436481475830078, "The Last Update of the Spitzer Satellite is 16 December 2020."]
[9.40372085571289, 8.74106502532959, "The Mirror Coating of the PAN Camera Imaging Device is Enhanced AlO2coating."]
[7.442623615264893, 8.19757080078125, "The Altitude Range of the CO2 VMR Measurement Device is 50 - 100 km."]
[9.23063850402832, 10.293221473693848, "The Dimensions of the DECA Camera is about 9 cm x 9 cm x 9 cm."]
[4.837909698486328, -3.3883378505706787, "The Member of the Andrew Dessler Individual is True."]
[6.0391459465026855, 6.413368225097656, "The Radiometric Stability of the Instrument SAR is \u2264 0.5 dB."]
[5.685817718505859, 3.4437906742095947, "The Illustration of the Drag Augmentation Device Satellite Component is Figure 16."]
[9.537498474121094, 6.088278770446777, "The Sensors of the iADCS-100 ADCS System is ST-200 star tracker."]
[4.154289245605469, 3.7148289680480957, "The Datasheet Revision of the QubeAIS Software-Defined AIS Receiver is 1.4."]
[9.022455215454102, 10.437856674194336, "The Image Resolution of the EXI Camera is 12 megapixels."]
[7.9974446296691895, 4.514233112335205, "The Multispectral Resolution of the SuperView 1A and 1B Satellite is 2 m."]
[7.434751510620117, 7.448795795440674, "The Default Measurement Mode of the SOVAP Instrument is Shuttered open/close sequence of the right channel."]
[11.650287628173828, -1.2157937288284302, "The Mass of the SDS-4 Satellite is ~48 kg."]
[8.448013305664062, 8.972943305969238, "The Nadir Footprint of the Instrument Spectrometer is 60 x 0.3 arcmin2."]
[6.947229862213135, 0.09220398217439651, "The End of Life Date of the SARAL Satellite is 31 Dec 2023."]
[7.428417682647705, 0.1822776198387146, "The Launch Year of the NEMO-AM Satellite is 2023."]
[8.345826148986816, 2.8375790119171143, "The Landing Site of the Beresheet Spacecraft is Moon."]
[4.285750389099121, 6.9863786697387695, "The 2nd LO of the HRIT HiRID Data Receiver is 1558."]
[9.232878684997559, 7.955652713775635, "The Temperature of the Cold Focal Plane Imaging Device Component is 91 K."]
[8.009110450744629, 1.374986171722412, "The Launch Date of the Solar Orbiter Spacecraft is February 10, 2020."]
[7.147238731384277, 0.9166275858879089, "The Commissioning Phase Start Date of the Electro-L Satellite is March 2011."]
[11.117986679077148, 6.268691062927246, "The URL of the Chandra X-Ray Observatory Satellite is https://arxiv.org/ftp/arxiv/papers/1110/1110.4020.pdf."]
[11.203831672668457, 4.30460262298584, "The Number of Monitored Stars of the Kepler Space Telescope Space Telescope is More than 150,000."]
[9.174787521362305, 6.805004119873047, "The Star Magnitude Registration of the Camera System Sensor is 4 and brighter."]
[8.840782165527344, 8.967108726501465, "The Field of View, vertical of the Instrument Spectrometer is -8 to -32 (20\u00ba)."]
[5.8954620361328125, 8.618949890136719, "The Spatial Resolution of the MWHS-II Microwave Humidity Sounder is ~15 km diameter at nadir, About 41 km x 27 km at outer edge of swath."]
[10.464865684509277, 4.720470905303955, "The Minimum Impulse Time of the PROP unit Propulsion System is 40 ms."]
[13.727245330810547, 1.6100412607192993, "The Return to Flight Date of the Vega Launch Vehicle is 3 September 2020."]
[5.451783180236816, 3.225898504257202, "The In-orbit digital IP routing of the Heinrich Hertz Satellite Technology is Enabled."]
[10.612873077392578, 2.772132396697998, "The Orbit Shift Distance of the GomX-4B Satellite is Up to 2000 km."]
[7.14888334274292, 0.840241014957428, "The Launch Date of the OPS-SAT Satellite is 18 December 2019."]
[7.5928497314453125, 1.1433100700378418, "The Observation Start Date of the SAGE-II Satellite is 1984."]
[9.441410064697266, 5.806230068206787, "The Development Tool of the ACS Attitude Control System is Matlab/Simulink."]
[8.344609260559082, 8.195454597473145, "The Page Numbers of the Very-Wide-Filed Ultraviolet Sky Survey Instrument is 179-180."]
[7.7566046714782715, 13.185797691345215, "The Pixel Resolution of the SPIM3 Spectrometer is 14 bit."]
[7.11667013168335, 2.7432680130004883, "The Mission of the SWOT Satellite is Future Project."]
[7.603803634643555, 1.7975329160690308, "The Article Author of the Magnetospheric Multiscale Mission Satellite is Mara Johnson-Groh."]
[5.7663655281066895, 2.971299648284912, "The Manufacturer of the Satellite Spacecraft is Nanyang Technological University."]
[9.600576400756836, 5.649643421173096, "The Attitude Control of the ADCS unit Satellite Component is Nutation damping."]
[9.17005729675293, 4.693398475646973, "The Acceleration of the NigeriaSat-2 Satellite is 0.35\u00b0/s2."]
[10.293723106384277, 8.723287582397461, "The Observation Target of the EUVI Extreme Ultraviolet Imager is Chromosphere and innermost corona."]
[6.721008777618408, 2.4765262603759766, "The URL of the Eutelsat Quantum Satellite is https://news.eutelsat.com/pressreleases/universal-eutelsat-quantum-satellite-to-revolutionise-telecoms-markets-1190652."]
[7.950765132904053, 9.856410026550293, "The Spectral Bands of the Focal Plane Array Detector is VNIR and SWIR."]
[4.041830062866211, 1.1975219249725342, "The Mission Type of the RHESSI Satellite is Non-EO."]
[5.023837089538574, 6.01647424697876, "The Stable Roll Frequency of the GP-B satellite Satellite is 0.081 rad/sec (13 mHz)."]
[11.23082160949707, 2.641122817993164, "The Length of the Pas Moraine Moraine is 300 kilometers (185 miles)."]
[6.099771976470947, 3.0596277713775635, "The International Designation of the GFO Satellite is 1998-007A."]
[7.01954984664917, 4.991261959075928, "The Carbon Source of the Tropical Forests Ecosystem is True."]
[3.5903894901275635, 2.2941555976867676, "The Size of the ZACube-2 Satellite is 3U."]
[5.256563663482666, 6.66274881362915, "The Chirp Signal Bandwidth of the P Mode Observation Mode is 240 MHz."]
[6.192411422729492, 4.016619682312012, "The Image Processing Chain of the EO-ALERT Satellite System is Payload on-board the satellite, on-board data processing unit, flight-to-ground communications subsystem, ground units for decryption/decompression."]
[9.482064247131348, -2.5232274532318115, "The Energy Range for Si of the LEICA Particle Detector is 0.33 - 5.5 9.6 - 177 21 - 330 54 - 195 MeV/n."]
[9.627304077148438, 1.2436985969543457, "The Deployment Time of the STPSat-6 Satellite is About 6 hours, 30 minutes after launch."]
[5.629497528076172, 4.333547115325928, "The Centrals of the DRR Data Routing and Retrieval is 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 Oceanograph."]
[8.21207332611084, 5.666517734527588, "The Leading Noise Terms of the Satellite Spacecraft is Thermal effects."]
[8.396550178527832, 10.145124435424805, "The Central Wavelength of the Current GOES imager Sensor is 6.19."]
[7.469095706939697, 1.130609393119812, "The Clues Date of the INTEGRAL Satellite is 14 Nov. 2008."]
[7.149378776550293, 6.619808197021484, "The Mission Status of the GeoSTAR Geostationary Synthetic Thinned Aperture Radiometer is Expected to be used during the NOAA and Aqua missions."]
[6.4205322265625, 4.6936116218566895, "The Instruments of the NeuSAR Satellite is SAR."]
[10.160825729370117, 4.848042964935303, "The Maneuverable of the T6 thrusters Ion Thrusters is True."]
[11.810004234313965, 1.219987392425537, "The Candidate Landing Region of the Chang\u2019e-4 Lunar Lander is 45\u00b0S-46\u00b0S and 176.4\u00b0E-178.8\u00b0E."]
[6.534010887145996, 5.537510395050049, "The Purpose of the STRATOS instrument Instrument is Makes use of GPS occultation measurements to determine temperature, pressure and humidity profiles of Earth's atmosphere for application in operational meteorology."]
[7.194538593292236, 0.363271564245224, "The Strategic Cooperation Sign Date of the Beijing Space View Company is 5 Dec. 2017."]
[4.7466278076171875, 1.7670726776123047, "The Objective of the Unseenlabs' Constellation Satellite Constellation is Create a constellation of 20 to 25 nanosatellites."]
[6.850914478302002, 0.5469523072242737, "The Launch Date of the SARAL Satellite is 2012."]
[3.92999267578125, 6.622523784637451, "The Modes of the Myriad RF board RF Board is Full duplex."]
[10.279129028320312, 4.941183567047119, "The Nominal Thrust of the Chemical Propulsion Thrusters Orbit Maintenance is 10 N."]
[5.703086853027344, 4.894248008728027, "The Software Package of the PRISMA POD Facility is GHOST (GPS High precision Orbit determination Software Tools)."]
[9.048969268798828, 10.089049339294434, "The Function of the Imaging System Camera System is Capture high resolution pictures."]
[2.145157814025879, 3.9581823348999023, "The Deployment Length of the ROSA Solar Array is 8.6 meters."]
[10.2770414352417, 2.986829996109009, "The Altitude for Extended Mission of the SELENE/Kaguya Satellite is 50 km."]
[8.470252990722656, 10.189093589782715, "The Detector Type of the Instrument Spectrometer is 2D CCD of 1024 x1024 pixels in VIS; 2D InGaAs detector of 320 x 240 pixels in NIR."]
[7.43776273727417, 4.524020195007324, "The Imaging Frequency Band of the ALOS-2 Satellite is L."]
[10.354408264160156, 7.096273899078369, "The Concepts Investigated of the ALBus R&R Design is Piston design, Collet design."]
[6.696781158447266, 4.637275695800781, "The Sea Level Rise of the Copernicus Sentinel-6 Satellite is 4.8 mm per year."]
[11.430883407592773, 6.000135898590088, "The Discovery Date of the Chandra X-Ray Observatory Observatory is 31 March 2021."]
[4.9795823097229, 6.022258281707764, "The Signal Wavelength of the Clementine Satellite is 13.19 cm."]
[9.264068603515625, 5.528892993927002, "The Publication Date of the Active magnetic attitude control algorithms for a CubeSat for astrophysics research Document is 2014."]
[7.905031681060791, 9.714420318603516, "The Number of Pixels of the Band 5 Spectral Band is 800."]
[11.630146980285645, -1.2534816265106201, "The Mass of the VEN\u00b5S Satellite is 264 kg."]
[6.2401204109191895, 5.949234962463379, "The Spotlight (SL) Spectral Resolution of the TSX-SAR Satellite is 2m."]
[5.630673408508301, 3.64536714553833, "The Data Transmission of the CSSS Canadian Space Surveillance System is JSpOC (Joint Space Operations Center)."]
[6.417476654052734, 2.969792604446411, "The Affiliation of the SwissCube Satellite is EPFL (Ecole Polytechnique Federale de Lausanne)."]
[5.546286582946777, 0.4812946319580078, "The 2021 Fires of the U.S. Drought Monitor Report is 672."]
[6.094341278076172, 9.650150299072266, "The Mass of the CIVA Analyzer is 3.4 kg."]
[3.9812746047973633, 5.683353900909424, "The Optical Downlink Rate of the NASA OCSD Satellite is Up to 200 Mbit/s."]
[7.1699323654174805, 3.3443310260772705, "The Ground Segment and Distributed Operations Concept of the BRITE-Austria Satellite is Unknown."]
[9.981039047241211, 4.578066349029541, "The Accomplished ?V Maneuver of the Satellite Spacecraft is 0.15 m/s."]
[9.484304428100586, 7.7558369636535645, "The ESA: 12 eV-12 keV, ISA: 10 eV/ q-12 keV/q of the Energy Range Sensor is Energy range ESA: 12 eV-12 keV, ISA: 10 eV/ q-12 keV/q."]
[5.271448612213135, 6.510761260986328, "The Temperature Jump of the NIR_AB Antenna Antenna is Self-recovered in a few weeks."]
[9.051310539245605, 4.754501819610596, "The Solar Panel Orientation of the STRaND-1 nanosatellite Satellite is +Y body direction."]
[9.346084594726562, 4.557801723480225, "The Instrument Unit Volume of the Solar Orbiter Spacecraft is Tightly controlled."]
[5.517801761627197, 6.313056468963623, "The Electric Antennas Length of the ISEE-3 Satellite is 0.6 and 45 m."]
[7.793127536773682, 10.785969734191895, "The Data Quantization of the CSG-SAR Synthetic Aperture Radar is 10 bit."]
[9.261796951293945, 0.937092661857605, "The Outlived Design Lifetime of the ERBE Instrument is Factor of 5."]
[7.797384738922119, 8.950217247009277, "The Spectral Range of the UV-2 Spectrometer is 306 - 380 nm."]
[7.408280849456787, -0.22340039908885956, "The Launch Date of the HTV-9 Cargo Transfer Spacecraft is 20 May 2020."]
[7.797573566436768, 4.3910298347473145, "The Operation Strategy of the SLIM6 Satellite is Maximum imaging time in the sunlit phase of the orbit."]
[4.86540412902832, 8.952498435974121, "The Detection of the InSight Spacecraft is Thousands of passing whirlwinds."]
[7.029445648193359, 5.92825174331665, "The Strongest Winds of the Nor'easter Weather System is 78 miles per hour."]
[7.622880458831787, 6.416107654571533, "The Spectrum Comparison of the Vibration Testing Test Type is GSFC-7000 standard random vibration spectrum that is commonly used for CubeSats and the in-house SSTL Spectrum C random vibration spectrum."]
[6.354808807373047, 5.005287170410156, "The Description of the Orthorectified and Atmospheric Corrected Product (L1A) Data Product is The product is derived from the LevelC product, atmospherically corrected and the data converted to ground surface reflectance values."]
[9.642989158630371, 3.9206430912017822, "The Drag Sails of the CanX-7 Satellite is 4."]
[6.300107955932617, 1.8145068883895874, "The URL of the Space-based ADS-B Surveillance System is http://www.icao.int/Meetings/anconf12/WorkingPapers/ANConfWP141.1.1.ENonly.pdf."]
[9.601177215576172, 5.939294338226318, "The Earth Observation Precision of the ADCS Attitude Determination and Control Subsystem is Sub-degree."]
[7.159185409545898, 1.4026466608047485, "The Symposium Date of the European Student Earth Orbiter Satellite is May 26-30, 2014."]
[7.829373359680176, 2.0135483741760254, "The Expected Completion Date of the Europa Clipper Spacecraft is End of 2022."]
[10.309334754943848, 4.600420951843262, "The Remaining Propellant of the Advanced Composition Explorer Spacecraft is Approximately 46 kg."]
[1.5549107789993286, 4.65800142288208, "The Sunlight Power Conversion Efficiency of the SBVR Power Supply is 98%."]
[9.198343276977539, 8.857317924499512, "The Aperture Area of the IBEX-Lo sensor Sensor is Fourth of the aperture area for IBEX-Lo."]
[7.365036964416504, 9.974376678466797, "The Spatial Co-registration of Spectral Bands of the Hyperion Imaging Spectrometer is < 20% of pixel."]
[6.740524768829346, 8.229354858398438, "The Maximum In-Storage Period of the MWI Instrument Instrument is 19 years."]
[9.964306831359863, 9.54871940612793, "The Measurements of the SAGE-III Satellite is Vertical distribution of aerosols and ozone, temperature in the stratosphere and mesosphere, profiles of trace gases such as water vapor and nitrogen dioxide."]
[7.655985355377197, 9.640260696411133, "The Scan Step Increment of the Visible Spectral Band Spectral Band is 140 \u00b5rad (N-S scanning)."]
[9.847283363342285, -0.9243115186691284, "The Form Factor of the MicroMAS Nanosatellite is 3U CubeSat."]
[10.520849227905273, 7.480778217315674, "The Material of the Propulsion System Satellite Component is Plastic."]
[7.555273056030273, 0.09574276208877563, "The Presentation Date of the CHEOPS Satellite is April 20-24, 2015."]
[8.722631454467773, 9.041598320007324, "The Color of the Optomechanics Mechanical Component is Blue."]
[4.1867289543151855, 6.5897650718688965, "The Modulation of the Ranging Tones Signal is Onto the downlink."]
[6.7469611167907715, 0.4971771836280823, "The Operational Status of the OFEQ-3 Satellite is Operational as of 2002."]
[8.085750579833984, 8.125641822814941, "The Function of the EIS (Extreme Ultraviolet Imaging Spectrometer) Instrument is Scanned the active region, breaking the light into spectral lines used to identify specific elements."]
[8.27165699005127, 3.8622987270355225, "The Glare Impact of the ISS-LIS Instrument is Will not impact ISS-LIS."]
[7.291069984436035, 5.683432579040527, "The Vertical Resolution (Troposphere) of the Aeolus Satellite is 1.0 km."]
[4.027566432952881, 1.190744400024414, "The Mission Type of the LADEE Satellite is Non-EO."]
[1.8706048727035522, 4.010612964630127, "The Directional Impact Proportion of the Solar-cell cover glasses Component is About 30%."]
[10.35498046875, 3.1596503257751465, "The Orbit Altitude of the EAGLE Secondary Payload is 39,000 km."]
[7.97695779800415, 0.43740084767341614, "The Launch Date of the CryoSat Satellite is 08 Oct 2005."]
[7.430130958557129, 4.2270283699035645, "The Target Tracking Capability of the BILSAT-1 Satellite is Yes."]
[7.672701835632324, 8.583354949951172, "The Spectral Range of the SIM Solar Irradiation Monitor is 0.2~50 \u00b5m."]
[7.184067249298096, 9.281664848327637, "The Angle of Incidence of the Stripmap Imaging Mode is 20\u00b0 - 50\u00b0."]
[3.597838878631592, 4.647071361541748, "The Microcontroller of the AIM Reconfigurable Computing Hardware Device is Intel 80C196 architecture."]
[8.19391918182373, 9.170364379882812, "The Field of View Directions of the CIRiS Infrared Imaging System is Four orthogonal directions."]
[2.3251683712005615, 4.516474723815918, "The Average Power Consumption (Observation Mode) of the COMIS Satellite is 14 W."]
[7.966857433319092, 0.47553035616874695, "The Map Date of the CryoSat-2 Satellite is Dec. 15, 2014."]
[2.2245004177093506, 4.472436904907227, "The Required Power at EOL of the KOMPSAT-6 Satellite is 2,250 W."]
[7.640733242034912, 1.2537286281585693, "The Operation Start Date of the Metcomp experiment Materials Science Experiment is 3 December."]
[6.81577730178833, 1.6619186401367188, "The Last Operation Date of the Envisat Satellite is Nov. 2, 2010."]
[9.432720184326172, 5.825897693634033, "The Torque Provider of the Permanent Magnets Attitude Control is Small amount."]
[7.797236919403076, 9.83638858795166, "The Swath width of the Optical System Imaging System is 2000 km."]
[6.900964736938477, 5.602615833282471, "The Design and Implementation Date of the Argo Ocean Observing System is 1998."]
[6.813894748687744, 1.3166348934173584, "The Symposium Date of the Geosat Follow-On Satellite is March 13-18, 2006."]
[5.793313980102539, 1.6472734212875366, "The External Configurations of the GomX-4 Satellite is Antennas, sensors, solar panels, radiation shields and radiative surfaces."]
[5.273345470428467, 7.699548721313477, "The Data Rate of the AATSR Instrument is 625 kbit/s."]
[7.522600173950195, 0.10035630315542221, "The In Orbit Commissioning (IOC) Start Date of the CHEOPS Satellite is 7th January."]
[7.254185199737549, 4.187615871429443, "The Instrument Type of the DMC-3 Satellite Constellation is High resolution optical imagers."]
[9.344869613647461, 8.167572021484375, "The Threshold of the Low LET Detector Detector is 0.2 MeV."]
[7.700460910797119, 9.942567825317383, "The Non-Polarized Channels of the VNIR Sensor is 11."]
[9.309815406799316, 4.0845842361450195, "The Size of the STARLETTE and Stella Satellites is 24 cm in diameter."]
[6.117325782775879, 3.1035313606262207, "The Mission Lead of the TEMPEST-D Satellite is Colorado State University."]
[7.64636754989624, 8.46537971496582, "The Design of the OMPS UV Hyperspectral Imaging Spectrometer is Limb- and nadir-viewing."]
[7.490245342254639, 8.762847900390625, "The Cross-Track Swath of the Nadir Sensor Wide-Field Telescope Sensor is 2800 km."]
[6.243320465087891, 1.4577387571334839, "The Presentation Date of the PAZ and TerraSAR-X Satellite Constellation is Sept. 23-27, 2013."]
[3.4550395011901855, 5.228959560394287, "The Storage Capacity of the GOES-R Access System Data Distribution System is Seven days."]
[5.256872653961182, 3.9293973445892334, "The Function of the ISSAC SOC Space Operations Center is Uplink image acquisition and other ISSAC operational commands to the ISSAC payload software."]
[6.184732437133789, 2.701974868774414, "The Project Contributor of the MIMOSA Satellite is Ladislav Sehnal."]
[7.929035186767578, 4.6618146896362305, "The Resolution of the Spotlight-2A Satellite is 0.8m."]
[8.870917320251465, 7.9415483474731445, "The Temperature Resolution of the AMSU-A Instrument is 0.25 - 1.2 K."]
[11.691590309143066, -1.2238503694534302, "The Satellite Mass of the Kleos S.A. Company is 8 kg."]
[7.210831642150879, 9.66755199432373, "The Size of the HyperScout Satellite Instrument is Milk-carton-sized."]
[5.042182922363281, 4.570974826812744, "The Subsystems of the Ground Station Ground Station is Monitor and Control, Atmospheric Monitoring Instruments, Laser Safety Systems."]
[10.770308494567871, 3.1534764766693115, "The Travel Distance of the Envisat Satellite is 2.25 billion km."]
[1.2217681407928467, 4.115195274353027, "The Battery Design of the TacSat-4 Satellite is Rapid, in the field replacement without spacecraft disassembly."]
[9.102925300598145, 7.680386066436768, "The Temperature Difference of the Hot and Cold Target Calibration Components is 50-60 K."]
[10.0235013961792, 1.531811237335205, "The Period of the Satellite Imaging Satellite is 98 min."]
[7.119673252105713, 3.8083395957946777, "The Mission Type of the Etalon Satellite is Solid Earth Studies."]
[4.375478267669678, 5.764582633972168, "The RF Communications of the Spacecraft Satellite is 2 MByte (typical)."]
[5.05679178237915, 7.034792423248291, "The Reflector Dimension of the Antenna System Communication System is 60 cm."]
[9.457159996032715, 0.8887845277786255, "The Orbital Operations Duration of the CubeRRT Satellite is ~1 year."]
[9.3829927444458, 8.906675338745117, "The Maximum Azimuth Slewing Rate of the OCTL Telescope is 20\u00ba/s."]
[7.89405632019043, 9.045018196105957, "The Spectral Resolution of the CHIPS Spectrometer is Near 170 \u00c5."]
[3.8306193351745605, 5.718958377838135, "The Upgradable Speed of the Iridium Certus Satellite Communication Service is 704 kbit/s."]
[7.246389865875244, 0.07529047131538391, "The Date of the Dnepr-1 Satellite Launch is April 18, 2007."]
[8.14299201965332, 10.021818161010742, "The Pixel Array Pitch of the MWIR Imager Imaging Device is 8 \u03bcm."]
[6.914663791656494, 0.3810453712940216, "The Initial Scheduled Launch Date of the OFT-2 Uncrewed Test Flight is July 30."]
[4.5898027420043945, 6.8259501457214355, "The Tracking System of the DORIS Receiver is CNES."]
[7.812129497528076, 9.080832481384277, "The Spectral Range of the GOME-2 Spectrometer is 240-790 nm."]
[7.786048412322998, 10.149608612060547, "The Manufacturer of the SEVIRI Imager is EADS Astrium SAS, France."]
[2.043333053588867, 3.815453052520752, "The Solar Cells Quantity of the H3 and H4 Spacecraft is 140 cells."]
[11.297405242919922, 3.524979591369629, "The Size of the Comets Celestial Bodies is Roughly 5 km."]
[7.385222911834717, 0.14874187111854553, "The Planned Launch Date of the SAOCOM-2A Satellite is 2025."]
[7.910315036773682, 0.75995272397995, "The Landing Date of the Starliner Spacecraft is December 22, 2019."]
[9.202000617980957, 4.089114189147949, "The Dimensions of the TUBSAT-N Satellite is 320 mm x 320 mm x 104 mm."]
[7.035851955413818, 8.752161026000977, "The Ground Resolution (Visible Channel) of the VIRR Instrument is 2.3 km."]
[9.419353485107422, 1.8444526195526123, "The Orbit Determination Frequency of the ASNARO Ground Segment Ground Station is Twice per day."]
[10.193985939025879, 2.894362211227417, "The Altitude of the STPSat-3 Satellite is 500 km."]
[10.481534957885742, 7.473964214324951, "The Energy Range of the ART-XC Instrument Telescope is 5 to 30 keV."]
[8.522343635559082, 1.601991891860962, "The Testing Date of the BepiColombo Antenna Pointing Mechanism Antenna Pointing Mechanism is 23\u201325 September 2015."]
[11.88932991027832, -1.159812331199646, "The Launch Mass of the Satellite Spacecraft is 3100 kg."]
[11.145915985107422, 2.8928864002227783, "The Quantity of the Impact Craters Surface Feature is 77."]
[4.816819190979004, 0.9093124270439148, "The Funding of the Hiber BV Satellite and Communications Start-up is \u20ac26 million."]
[6.591259956359863, 7.77923059463501, "The Heat Source of the Laser Diode Optical Unit Component is Significant."]
[10.296191215515137, 8.322806358337402, "The Purpose of the Bragg-crystal telescope-spectrometer Mg1 and Mg2 Telescope-spectrometer is Imaging hot plasma (T ~ 10 MK) of the solar corona."]
[7.902637481689453, 4.454193115234375, "The Image Resolution of the RISING-2 Satellite is ~5m."]
[6.515106201171875, 4.131384372711182, "The Service Impact of the Lacuna Space Company is Monitor peatland restoration impact."]
[2.3320045471191406, 3.6597206592559814, "The MZ-Surface Function of the H3 and H4 Spacecraft is Faces to the sun."]
[5.783630847930908, 2.0150890350341797, "The Components of the NLS-1 Launch System is CanX-1, AAUSat, DTUSat, XI, CUTE-I."]
[8.068584442138672, 10.070940971374512, "The Swath of the CAVIS Imager is Slightly wider than main instrument."]
[2.2562761306762695, 4.461043834686279, "The Power of the Propulsion Satellite Subsystem is 0.53 W."]
[7.903520107269287, 5.390616416931152, "The SNR of the ALOS-3/PRISM-2 Satellite is >200."]
[8.004955291748047, 4.464219093322754, "The Image Resolution of the ExoMars TGO Trace Gas Orbiter is 460 km/pixel."]
[4.035073280334473, 6.482035160064697, "The Modulator Module of the Transmitter Communication Device is Xilinx Virtex-5 SX FPGA."]
[4.914910793304443, 2.050107479095459, "The Quantity of the CINEMA nanosatellite Satellite is 3."]
[9.214961051940918, 7.129823684692383, "The Measurement Range - Plasma Density of the ISL Instrument Langmuir Probe is 100 to 5 x 10^6 particles/cm3."]
[6.5918073654174805, 7.395817279815674, "The Operation Mode of the LEDs Light Source is Pulse mode at higher currents."]
[6.614658832550049, 6.854115962982178, "The Sampling Frequency of the Precipitation Data Data is Every half hour."]
[8.519042015075684, 1.6679359674453735, "The Observation Period of the Spitzer Space Telescope is 2015-2019."]
[1.7890223264694214, 4.5635762214660645, "The Expected Electrical Power Levels of the GSE Power Supplies Power Supply is Not provided."]
[11.897316932678223, -1.1275899410247803, "The Launch Mass: 1670 kg of the Spacecraft Mass is Over half the launch mass of the entire spacecraft, about 1670 kg."]
[6.0771894454956055, 4.326762676239014, "The User of the Canadarm2 Robotic Arm is NASA astronaut Megan McArthur."]
[6.779637336730957, 1.87785804271698, "The Symposium Date of the Universat-Tatyana-2 Small Spacecraft is Sept. 21-24, 2010."]
[7.812396049499512, 8.998674392700195, "The Locking Performance of the Rb Spectroscopy Unit Spectroscopy Unit is Stayed locked during vertical accelerations reaching 12.5 g."]
[6.063034534454346, 9.713955879211426, "The 1.4 kg/sensor head (including HVPS and preamplifier) of the Instrument Mass Sensor is Instrument mass 1.4 kg/sensor head (including HVPS and preamplifier)."]
[5.923195838928223, 6.465824127197266, "The Number of TRMs of the CSG-SAR Synthetic Aperture Radar is 1280 @ H polarization and 1280 @ V polarization."]
[7.818846225738525, 10.798822402954102, "The Useful Data Bits of the MEV Electronics Module is 10."]
[11.269784927368164, 3.791292428970337, "The Non-Group Comet Sightings Frequency of the SOHO Satellite is A few times a year."]
[6.839897155761719, 9.98686408996582, "The Bandwidth of the Band 3 Spectral Band is 480-500 nm."]
[6.188972473144531, 5.466641426086426, "The Sensor of the TanDEM-X Satellite is SAR sensors."]
[9.256662368774414, 1.7968943119049072, "The Impact on Mission Planning of the GOCE Satellite is Weekly replanning activity required."]
[3.555987596511841, 6.355551719665527, "The Downlink Data Rate of the RF Communication System Communication System is 1.2 kbit/s."]
[8.641031265258789, 4.680809020996094, "The Phase Difference Adjustment Method of the SJ-9A and SJ-9B Satellites is Adjusting the orbit semi-major axis and changing the phase relative drift ratio."]
[5.133236408233643, 4.357718467712402, "The Function of the GSD Ground Systems Division is Provide expertise in satellite ground systems design."]
[11.986283302307129, 4.484055519104004, "The Components of the Wolf-Rayet bubble Nebula is Blue, Yellow-Green, Red."]
[9.5923490524292, 7.830382823944092, "The Proton Energy Resolution of the REPT Instrument is 30%."]
[7.208383083343506, 2.9610507488250732, "The Operator of the ICON Satellite is UCB/SSL (Space Sciences Laboratory)."]
[11.709246635437012, 6.1937408447265625, "The Launch Date of the XMM-Newton X-ray Satellite is End of 1999."]
[7.716256141662598, 7.742891788482666, "The Formation Mechanism of the Ozone Layer Atmospheric Layer is Photodissociation of stratospheric molecular oxygen by solar middle and far ultraviolet radiation."]
[4.410372257232666, 3.002394914627075, "The TRL Level of the RadSat Satellite is 9."]
[7.943726062774658, 0.5736923813819885, "The Mission End Date of the CryoSat Satellite is Unknown."]
[8.707091331481934, 7.018932819366455, "The Range of the Angular Rate Sensor is \u00b1200\u00ba/s(3-axis)."]
[7.6575608253479, 8.204476356506348, "The Modes of the VLF Experiment Scientific Experiment is Slow, Fast."]
[3.8217155933380127, 2.2998201847076416, "The Size of the STARS-Me CubeSat is 1U."]
[6.754650592803955, 4.512831211090088, "The Developer of the CO2M Monitoring and Verification Support Capacity System is ECMWF (European Centre for Medium-Range Weather Forecasts)."]
[11.835676193237305, 1.049934983253479, "The Landing Site Name of the Chang'e-4 Probe is Statio Tianhe."]
[4.011958122253418, 6.686581134796143, "The TRL Level of the Computer System Payload is 5."]
[6.0458664894104, 2.989060878753662, "The Business Focus of the Lacuna Space Satellite Company is IoT (Internet of Things)."]
[6.662641525268555, 4.057477951049805, "The Modes of the Satellite Operation Modes is Open-loop, Interactive mode, Closed-loop, Automatic target pointing."]
[5.057398319244385, 6.316150188446045, "The Antenna Type of the ADS Antenna Deployment System is VHF/UHF."]
[12.024471282958984, 2.2726731300354004, "The Checkpoint Rehearsal Duration of the OSIRIS-REx Spacecraft is Four hours."]
[7.909947872161865, -0.16895921528339386, "The Docking Date of the Tianzhou-3 Spacecraft is 20 September 2021."]
[8.529821395874023, 6.830562591552734, "The Developer of the NewMag Magnetometer Experiment is University of Newcastle."]
[10.993035316467285, 7.122730731964111, "The Quantity of the LAXPCs X-ray Proportional Counters is 3."]
[8.435988426208496, 3.0756194591522217, "The Formation Maintenance of the TanDEM-X and TerraSAR-X Satellites is 3 months."]
[7.588648319244385, 3.7182092666625977, "The Image Quality of the CartoSat-2B Satellite is High."]
[6.9624409675598145, 1.563789963722229, "The Establishment Date of the GMES Bureau is 2006."]
[8.48615550994873, 2.3406424522399902, "The Project Scientist Affiliation of the Parker Solar Probe Spacecraft is Johns Hopkins University Applied Physics Laboratory."]
[9.056017875671387, 1.9139363765716553, "The Struggle Duration of the New Horizons Spacecraft is 17 years."]
[10.376635551452637, 2.65655255317688, "The Apogee Alignment of the MMS Satellite is Opposing."]
[8.054560661315918, 4.635490417480469, "The Spatial Resolution of the Oceanography Short scale Satellite is 100 km."]
[7.023169040679932, 0.6285623908042908, "The Mission Approval Year of the Aditya-L1 Satellite is 2015."]
[9.645309448242188, 8.49474811553955, "The Components of the TT Telescope Tube is Upper and lower tubes, VOD, OGB."]
[7.48378849029541, 0.8095817565917969, "The Eclipse Observation Date of the PROBA-2 Satellite is Sept. 14, 2015."]
[8.114519119262695, 8.475862503051758, "The Maximum Optical Path Difference of the Michelson Interferometer Interferometer is \u00b10.8 cm."]
[6.370718955993652, -0.7931464314460754, "The GPS L1 Complementary Signal Improvement of the QZS-1 Satellite is Approximately 1.7 to 2.5 times."]
[7.216161251068115, 4.466385841369629, "The Band 4 of the Landsat TM Satellite is Biomass surveys, water body delineation."]
[10.351336479187012, 2.9117391109466553, "The Orbit Altitude of the SeaHawk-1 CubeSat is ~590 km."]
[7.034460544586182, 0.5360840559005737, "The Launch Date of the AAUSAT3 Satellite is 25. February 2013."]
[1.0263391733169556, 4.1768412590026855, "The Configuration of the Lithium-ion batteries Battery is 3 parallel cells."]
[7.212802410125732, -0.37584060430526733, "The Public Beta Test Plan of the Starlink Satellite Constellation is Before the end of the year."]
[11.276759147644043, 3.5492093563079834, "The Dust Production of the McNaught Comet is High."]
[6.005681991577148, 9.80119514465332, "The Mass of the CAI Telescope is 8 kg."]
[9.254029273986816, 4.141871929168701, "The Size of the Spacecraft Satellite is 100 mm x 100 mm x 243 mm."]
[6.6816229820251465, 7.715292930603027, "The Sequence Steps of the AVGS Laser System is 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)."]
[9.301624298095703, -0.6903979778289795, "The Developer of the Aalto-1 Nanosatellite is Aalto University."]
[6.482674598693848, 3.675809621810913, "The Mission Type of the MTSAT Satellite is EO."]
[10.320338249206543, 9.557680130004883, "The Observation Time of the IRIS Observatory is Eight months per year."]
[4.553591251373291, 4.006516933441162, "The Interface of the ASIM Payload is CEPA."]
[3.6492717266082764, 6.385185718536377, "The Uplink Data Rate of the RF Communications Communication System is 2 kbit/s."]
[6.282662391662598, 4.816244125366211, "The Image Type of the ICEYE-X2 Satellite is Radar."]
[11.513908386230469, 6.36350679397583, "The Targeted Regions of the XMM-Newton X-ray Space Observatory is LMC, Hickson Cluster Group 16 (HCG-16), HR 1099."]
[4.165424823760986, 6.539218425750732, "The Downlink Frequency of the Astrodev Lithium 2 Radio RF Communication Device is 401.3 MHz."]
[5.602556228637695, 4.133648872375488, "The Location of the EuTEF Payload Facility is Outside of the Columbus laboratory."]
[9.026694297790527, 7.170172214508057, "The | of the SFL Sun Sensor Sensor is SFL sun sensor."]
[9.424860954284668, 1.4751062393188477, "The Orbit of the DMSP Follow-on program Satellite Program is Early morning (05:30 hours)."]
[7.309569835662842, 2.728027105331421, "The Earth Explorer of the FORUM Mission is Ninth."]
[6.006894588470459, 3.3349454402923584, "The Responsibilities of the ESA Organization is Payload Module, launcher, AIT facilities for spacecraft integration and testing."]
[3.4398722648620605, 4.724732875823975, "The Processor of the OBC Onboard Computer is 80C186+16 MByte, 80C386+64 MByte."]
[7.885331153869629, 4.735236644744873, "The Spectral Resolution of the GK-2A Satellite is Improved."]
[7.618223667144775, 5.441662311553955, "The Purpose of the OCO-3 Satellite is Response to growing populations and varying patterns of fossil fuel consumption."]
[4.47048282623291, 5.8588666915893555, "The TT&C Communication Frequency of the SCD-2 Satellite is S-band."]
[6.465602397918701, 0.5954418778419495, "The HPGP Commissioning Date of the SkySat-3 Satellite is August 3, 2016."]
[9.573332786560059, 7.802695274353027, "The Electron Energy Range of the EPAM Particle Detector is Ee >30 keV."]
[9.07793140411377, 5.052462100982666, "The Stabilization of the G\u00f6kt\u00fcrk-1A Satellite is 3-axis."]
[4.2777605056762695, 4.690846920013428, "The Data Rate Control of the MIU Interface is Based on commands from the FC."]
[8.645088195800781, 6.161750316619873, "The Amplitude of the daily variation of the horizontal magnetic intensity (\u0394H) of the EEJ (Equatorial Electrojet) Phenomenon is 3\u20135 fold higher than the variation of data from other regions of Earth."]
[10.24453067779541, 2.915951728820801, "The Altitude of the Anand Satellite is Approximately 510 km."]
[10.29352855682373, 8.745315551757812, "The Emission Lines of the EUVI Extreme Ultraviolet Imager is Four EUV emission lines between 17.1 and 30.4 nm."]
[5.026353359222412, 3.5611672401428223, "The Microcontroller Type of the Subsystems Satellite Subsystems is FPGA-based."]
[9.318758010864258, 3.146484613418579, "The Orbit Type of the EQUULEUS Satellite is 1:4 synodic resonant periodic orbit."]
[7.258789539337158, 5.166479587554932, "The Measurement of the GeoCARB Satellite is Total concentration of carbon dioxide, methane and carbon monoxide in the atmosphere."]
[6.7433319091796875, 8.746585845947266, "The Height of the Instrument Instrument is 140 mm."]
[2.2185022830963135, 4.417263507843018, "The Average Power Generation of the MicroMAS-1 Satellite is 14.5 W in sunlight (12.7 W orbit average) at a 400 km altitude orbit."]
[5.998871326446533, 6.355605125427246, "The Line-of-Sight Deformation Rate Maps Generation Period of the SAR Synthetic Aperture Radar is One year."]
[8.977319717407227, 9.23869800567627, "The FOV Motion of the MAHRSI Instrument is 0.01\u00ba x 1.13\u00ba."]
[6.631180763244629, 2.1569368839263916, "The Conference Presentation of the DoD Space Test Program Satellite Program is 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."]
[6.027560710906982, 2.856144666671753, "The Effect of the Moonlight Lunar Telecommunications and Navigation Satellite Network is Reducing the design complexity and weight of individual missions."]
[9.234945297241211, 5.529828071594238, "The Rotation Modes of the AMSR2 Device is Lower (11 rpm), Regular observation mode (40 rpm)."]
[2.3814048767089844, 4.531495094299316, "The Instrument Package Power Consumption of the LCROSS Satellite is 27 W."]
[7.970980167388916, 10.709112167358398, "The Data Quantization of the TeLEOS-1 Imager Imaging Device is 10 bit."]
[8.878569602966309, 8.367342948913574, "The Mass Resolution of the ELENA Sensor is M/\u0394M H and heavy species."]
[1.7859514951705933, 3.958559274673462, "The Quantity of the Solar Cells Power Generation is 64."]
[9.667892456054688, 3.9480197429656982, "The Enclosure Purpose of the CanX-7 Satellite is Converts the uncoiling motion of the tape springs into linear motion of the booms."]
[4.9790496826171875, 4.492528915405273, "The (International) Harmonization of the CSK GS Ground Segment is Verify and harmonize the Service Request lists coming from the different Partners."]
[9.456413269042969, 5.598239898681641, "The Pointing Requirements of the AOCS Attitude and Orbit Control System is 2\u00ba about all axes."]
[7.5348334312438965, 0.9812268614768982, "The Launch Date of the Sentinel-3A Satellite is 2013."]
[8.635293960571289, 8.960208892822266, "The Color Filters of the LORRI Imaging Instrument is No."]
[6.415537357330322, 0.5919854044914246, "The Launch Date of the ANGELS Satellite is 18 December 2019."]
[7.421238899230957, 4.982266426086426, "The Function of the BEESAT-4 CubeSat is 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."]
[6.156561374664307, 2.2426774501800537, "The Mission Selection Criteria of the TacSat-3 Satellite is Specific capabilities to meet user needs."]
[7.782225131988525, 10.391898155212402, "The Detector Elements of the SEVIRI Spectral Imager is 3."]
[8.910133361816406, 2.1541635990142822, "The Extended Mission Objective of the New Horizons Spacecraft is Study the Kuiper Belt environment, observe numerous Kuiper Belt Objects (KBOs) and Centaurs, make the first close flyby of the KBO 486958 2014 MU69."]
[7.202324390411377, 6.834332466125488, "The Launch Date of the OCO-3 Instrument is May 1, 2019."]
[6.5502543449401855, 4.170690059661865, "The Image Credit of the Copernicus Sentinel-3 Satellite is ESA."]
[5.934790134429932, 4.79824161529541, "The Purpose of the MONTE Software is Deep space navigation."]
[8.336548805236816, 0.6141795516014099, "The Published Online Date of the Hitomi Satellite is 13 November 2017."]
[8.132986068725586, 9.568421363830566, "The Detector Array of the SWIR Spectrometer Spectrometer is 160 x 250 channels."]
[3.9098432064056396, 5.069874286651611, "The Potential Difference of the DSLP Data Acquisition System is A few tenths of Volts."]
[7.0473833084106445, 4.760220050811768, "The Content of the Dataset Data is Location and crown diameter of trees in western Africa."]
[7.934267520904541, 8.676572799682617, "The Operating Phases of the NMS Neutral Mass Spectrometer is Perigee and near-perigee."]
[7.050890922546387, 1.6900264024734497, "The Symposium Date of the Small Satellite Hyperspectral Mission Satellite is Sept. 20-24, 2004."]
[3.5925586223602295, 4.512526512145996, "The Symposium Presentation Date of the Centralized Computation Service Architecture Computation Service Architecture is April 4-8, 2005."]
[7.882673263549805, 6.156821250915527, "The Objective of the SOSP Satellite is Study of solar physics and solar-terrestrial relationships in aeronomy and climatology."]
[2.6327266693115234, -1.4565099477767944, "The Brigthness Temperature (BT) Sensitivity of the Antenna Reflector is \u00b10.43 K."]
[3.906805992126465, 6.393577575683594, "The Modulation Type of the Low-rate Modulation Communication System is 9 kbit/s residual carrier PM."]
[5.932352542877197, 1.942162036895752, "The Launch Vehicle of the Deployment Systems Satellite is Dnepr-1."]
[6.6865692138671875, 7.615419864654541, "The High-Energy Laser Transmitter Range of the OLA LIDAR Instrument is 1\u20137.5 km."]
[10.388385772705078, 5.0307464599609375, "The Deceleration of the OMS-E engine Engine is 0.3 g."]
[9.171979904174805, 1.2379040718078613, "The Coolant Supply Duration of the Herschel Space Observatory is More than three years."]
[4.725208759307861, 1.8648357391357422, "The Number of Satellites of the Transport Layer Tranche 1 Satellite Network is 42."]
[9.299758911132812, 7.887171268463135, "The Cooling Temperature of the IRFPA Infrared Focal Plane Array is 70 K."]
[11.073659896850586, 2.6112418174743652, "The Thruster Firing Duration of the Schiaparelli module Spacecraft is 3 sec."]
[7.766794204711914, 9.076969146728516, "The Resolution of the GOME-2 Spectrometer is 0.22-0.50 nm."]
[10.996960639953613, 2.8551032543182373, "The Distance to Ingenuity Mars Helicopter of the InSight Mars Lander is Roughly 2,145 miles (3,452 km)."]
[6.905028820037842, 4.910951614379883, "The Data Collection of the Copernicus Sentinel-5P Satellite is Nitrogen dioxide concentrations."]
[9.164983749389648, 8.518198013305664, "The Drive Signal of the Fast-Steering Mirror Device is Sinusoidal voltage signal."]
[5.784144878387451, 3.164761781692505, "The Manufacturer of the X-band transponder Transponder is Lockheed Martin."]
[8.772571563720703, 6.937253475189209, "The Sensor Quantity of the MAGIC Magnetometer is 2."]
[9.47620964050293, 5.951231479644775, "The Operating Modes of the iADCS100 Attitude Determination and Control System is Tracking mode."]
[10.676644325256348, 5.276638984680176, "The Specific Impulse of the CNAPS Propulsion System is 40 s."]
[11.744148254394531, 1.6762776374816895, "The Primary Science Mission Duration of the Philae Lander is Nearly 57 hours."]
[5.854022026062012, 8.609532356262207, "The Number of Pixels of the MWHS-II Microwave Humidity Sounder is 98/scan."]
[6.573436737060547, 1.1626091003417969, "The Collision Avoidance Maneuver Date of the PRISMA Satellites Satellite is July 7, 2010."]
[4.900306224822998, 2.5984392166137695, "The Payload of the Iraz\u00fa CubeSat Satellite is Secondary OBC which acts as an IMU."]
[8.218228340148926, 8.074244499206543, "The Material of the Reflection Diffuser Calibration Device is Spectralon."]
[6.047365188598633, 1.5716352462768555, "The Concept Type of the PAZ-TerraSAR Constellation Satellite Constellation is Coordinated Constellation Concept (CCC)."]
[9.72062873840332, 8.063987731933594, "The Energy Range of the Natalya-2M High energy radiation spectrometer is 0.3 to 2 GeV."]
[8.988489151000977, 2.737415075302124, "The CDR Date of the GCOM-W1 Satellite is December 2009."]
[9.334643363952637, 4.682023048400879, "The Off-nadir Angle of the Cartosat-2E Satellite is Up to 45\u00b0."]
[6.341700553894043, 9.245110511779785, "The Mass of the MuREM Radiation Monitor is < 1 kg."]
[11.387115478515625, 5.118401527404785, "The Energy Comparison of the Transient Luminous Event Natural Phenomenon is Energy produced by a transient luminous event would be enough to charge more than 800 vehicles."]
[6.797272205352783, 0.6305260062217712, "The Launch Date of the STPSat-3 iMESA Technology is Nov. 2013."]
[7.28925085067749, 3.886195421218872, "The Function of the Pelican Satellites Satellite is Distinguish road markings on the ground."]
[7.3975605964660645, 7.145572662353516, "The Launch Date of the ECOSTRESS ECOsystem Spaceborne Thermal Radiometer is June 2018."]
[5.0676374435424805, 3.542430877685547, "The Quad-stack of the Satellite Bus Configuration is True."]
[7.530803203582764, 1.9042301177978516, "The Event Name of the IceCube Neutrino Observatory Neutrino Detector is IceCube-170922A."]
[9.98111343383789, 6.824965000152588, "The Thermal Design of the Instrument Equipment Satellite Component is Classical thermal environment."]
[7.899331569671631, 1.8506066799163818, "The Arrival Date of the ExoMars Mission is June 2023."]
[11.190753936767578, 3.4845216274261475, "The Perihelion Distance of the Comet 67P/C-G Comet is 1.24 au."]
[8.273521423339844, 0.6946622133255005, "The Precession Cycle of the Megha-Tropiques Satellite is Clearly seen."]
[8.226980209350586, 2.4892711639404297, "The Death Year of the Max Valier Person is 1930."]
[9.602892875671387, 5.3349432945251465, "The Function of the Micro-propulsion thrusters Attitude Control is Control the spin and precession motion of the spacecraft."]
[9.445624351501465, 0.9299821853637695, "The Mission Extension of the WIND Satellite is 10 years."]
[3.892435312271118, 2.302253007888794, "The Size of the TacSat-6 CubeSat is 3U."]
[3.6173794269561768, 4.793121337890625, "The Processor Speed of the Spacecraft Satellite is 12 MHz."]
[6.68404483795166, 7.1851983070373535, "The Laser Production Date of the GEDI Lidar is April 19-20, 2016."]
[7.976163387298584, -0.0254440288990736, "The Arrival Date of the Docking Module Space Station Module is 26 November 2021."]
[3.201059103012085, 4.885429859161377, "The Flash Memory of the OBC On Board Computer is 256 MB."]
[9.487548828125, -2.515352964401245, "The Energy Range for Fe of the LEICA Particle Detector is 0.21 - 3.1 11 - 90 27 - 450 70 - 270 MeV/n."]
[9.848299026489258, 3.068293571472168, "The Freezing Level Height of the GPM Satellite is Above 3 km."]
[4.767578601837158, 3.982422113418579, "The Ground Segment Elements of the SAMPEX Satellite is Ground stations, POCC, PACOR, UMSOC."]
[3.2478411197662354, 5.971725940704346, "The Application of the SDR Software Defined Radio is Space applications."]
[6.719427585601807, 5.111778736114502, "The Altimetry of the Geosat Satellite is W. H. F. Smith, D. T. Sandwell."]
[9.071610450744629, 9.182741165161133, "The FOV of the Optics and detector assembly Assembly is \u00b10.25\u00ba."]
[11.528912544250488, 0.8389302492141724, "The Mass of the Tianwen-1 Probe is 5 tons."]
[7.5723490715026855, 8.609207153320312, "The Modulation Transfer Function of the MTF Spectrometer is \u2265 15% (@Nyquist frequency)."]
[11.419878959655762, 5.168355464935303, "The Visibility of the Transient Luminous Events Atmospheric Phenomena is Rarely seen from the ground."]
[7.0854105949401855, 4.130856990814209, "The Objective of the Landsat Next Satellite Constellation is Extend the ability to detect and quantitatively characterise changes on the global land surface."]
[7.69007682800293, 2.611936330795288, "The Viewing Geometry of the MRO Mars Reconnaissance Orbiter is West."]
[8.268694877624512, 3.087588310241699, "The Presentation Date of the TanDEM-X Satellite is July 23\u201328, 2017."]
[12.148734092712402, 2.1737029552459717, "The Mission Status of the OSIRIS-REx Spacecraft is Ready for Touchdown on Asteroid Bennu."]
[12.039996147155762, 3.3207645416259766, "The Orbital Inclination of the IceCube Satellite is 51.6\u00b0."]
[9.714455604553223, 1.485796332359314, "The Orbit (Revisit Time) of the Spacecraft Satellite is 14 days."]
[11.661274909973145, 1.8363821506500244, "The Contact with Asteroid Surface of the MASCOT Lander is Approximately 20 minutes after separation."]
[6.973967552185059, 0.7371638417243958, "The Launch Date of the RadSat Satellite is 2018."]
[9.294453620910645, 2.7222959995269775, "The Impact Speed of the DART Space Probe is 6.6 km/s."]
[4.5413408279418945, 4.247010707855225, "The Components of the Descent Subsystem Subsystem is Supersonic pilot, supersonic ribbon drogue, subsonic ribbon drogue, ringsail main parachute, mortar, strap-cutters."]
[5.021615982055664, 6.081542491912842, "The Frequency in Inertial Mode of the FEP Satellite Device is 1.7 x 10-4 Hz."]
[9.4826078414917, -0.5997648239135742, "The Resonance Survey Requirement of the SERB Nanosatellite Satellite is First global mode > 250 Hz."]
[10.514829635620117, -1.0706281661987305, "The Fluxgate Magnetometer Mass of the Microsatellite Satellite is 3.6 kg."]
[5.84360408782959, 8.642946243286133, "The Spatial resolution at nadir of the MWHS Microwave Humidity Sounder is 15 km."]
[6.785120487213135, 3.394751787185669, "The Operator of the SEOSat Satellite is Unknown."]
[5.957548141479492, 3.8818070888519287, "The Service Area of the Bartolomeo External Payload Hosting Facility is Low Earth Orbit."]
[5.83111572265625, 2.9325759410858154, "The Manufacturer of the DSP satellites Satellite is DFHSat (DFH Satellite Co. Ltd.)."]
[7.21790075302124, 8.195268630981445, "The Operation Period of the IMA Mass Spectrometer is Limited to several hours/day."]
[9.239760398864746, 10.301015853881836, "The Field of View of the LWIR Camera Camera is 1\u00ba x 1\u00ba."]
[3.2139148712158203, 5.169980525970459, "The Capacity of the OBR Onboard Recorder is 256 Gbit."]
[6.249880790710449, 2.945993423461914, "The owner of the Insight lander lander is NASA."]
[7.178177356719971, 2.4704508781433105, "The Program URL of the DRACO System is [DRACO Program URL](https://www.darpa.mil/program/demonstration-rocket-for-agile-cislunar-operations)."]
[10.749126434326172, 5.216066837310791, "The Potential Damage of the Geomagnetic Storm Space Weather Event is Collapse the whole telegraph system in North America and Europe."]
[6.794188022613525, 4.026346683502197, "The Relation to Sentinel-4A of the Sentinel-4B Satellite is Follow up satellite."]
[6.615517616271973, 7.802066326141357, "The Type of the PMDs Polarization Measurement Device is Identical."]
[8.389068603515625, 8.026894569396973, "The Cadence of the MEGS Spectrograph is 10 seconds."]
[8.773667335510254, 10.522699356079102, "The Image Resolution of the PMC Camera is 10 m."]
[10.008803367614746, 6.748988151550293, "The Thruster Temperature of the BepiColombo Spacecraft is Minus 150 C."]
[9.42092227935791, 5.801839828491211, "The Achievable of the Pointing Accuracies Attitude Control System is < 1arcsec."]
[6.761626243591309, 3.778826951980591, "The Purpose of the MANTIS Earth Observation Satellite is Monitor climate change, map the environment, forecast the weather, find new resources."]
[8.575569152832031, 7.204684734344482, "The Sample Rate of the Acceleration Sensor is 125 Hz."]
[8.301118850708008, 2.905097484588623, "The Lunar Eclipse Survival Plan of the Spacecraft Satellite is Developed baseline spacecraft configuration to use prior to and during the lunar eclipse."]
[4.998739242553711, 3.6155292987823486, "The Components of the Bus Structure Satellite Structure is Metallic cube (aluminum panels), four motherboards."]
[5.836366653442383, 6.305245399475098, "The SAR Antenna Length of the StriX-\u03b1 SAR Satellite is 5 m."]
[4.2312846183776855, 6.597397327423096, "The Frequency of the RF communication subsystem Communication is 437 MHz (UHF), in uplink and downlink."]
[4.215418338775635, 6.6029510498046875, "The Operating Frequency of the C&DH Subsystem Subsystem is 8 MHz."]
[9.14578914642334, 7.981964588165283, "The Operating Temperature of the OHIS Imaging System is 90 K."]
[7.280954837799072, 0.2980633080005646, "The Integration Date of the SpIRIT Satellite is 2022."]
[6.960553169250488, 4.041417598724365, "The Geolocation and Ortho-rectification Methods of the Deimos-2 Satellite is Physical sensor model, RFM (Rational Function Model)."]
[4.544956207275391, 5.9380717277526855, "The Signal Modulation of the Signal Generator Subsystem Signal Generation System is Modulated with the relevant subcarriers according to the Galileo Navigation Signal in Space ICD."]
[11.133801460266113, 2.0560197830200195, "The Drill Depth of the Rosalind Franklin Rover is Up to two meters."]
[9.136215209960938, 3.194143056869507, "The Orbit of the TOMS Instrument is Polar orbit."]
[7.865983009338379, -0.048440344631671906, "The Alternate Name of the Prichal Module Docking Port is Prichal Node Module (UM) or Progress M-UM."]
[8.541175842285156, 1.135749340057373, "The Lunar Orbit Entry Date of the LRO Orbiter is June 23, 2009."]
[11.328078269958496, 3.8806347846984863, "The Continental Crust Thickness of the Earth Planet is Averages from 35 to 40 kilometers."]
[9.541321754455566, 9.084151268005371, "The Focal Length of the Telescope Optical Instrument is 5.6 m."]
[6.230881214141846, 1.9466469287872314, "The Launch Vehicle of the G\u00f6kt\u00fcrk-1 Satellite is Europe's new Vega small-satellite launch vehicle."]
[5.340597629547119, 5.148106098175049, "The States of the LCRD Payload Optical Space Terminal is 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 re."]
[9.419947624206543, 9.104183197021484, "The Effective Focal Length of the Telescope Optical Instrument is 1600 mm."]
[4.201214790344238, 3.6944639682769775, "The Peak Detection Rate of the exact Earth Satellite AIS Receiver is TBD."]
[11.846454620361328, -1.1619760990142822, "The Launch Mass of the CartoSat-2D Satellite is 1378 kg."]
[9.644160270690918, 4.18310546875, "The Reflector Dish Diameter of the COMMx Payload is ~3.75 m."]
[6.033453464508057, 6.417574882507324, "The PSLR of the Instrument SAR is \u2264-16 dB."]
[10.257730484008789, 5.698034763336182, "The Voltage source and the tether of the Negative Tether Charging Mode Test Procedure is The negative mode requires only a voltage source and the tether itself."]
[11.442161560058594, 3.807635545730591, "The Age of the Magma Ocean Planets Planets is Less than 100 million years old."]
[12.14051628112793, 2.163980484008789, "The Fly-over Date of the OSIRIS-REx Spacecraft is April 7."]
[9.514912605285645, 0.6378297209739685, "The Mission Life of the TechEdSat-1 Satellite is 7-8 months."]
[11.05250072479248, 7.172887802124023, "The Field of View of the HXCP Hard X-ray Polarimeter is \u00b115\u00ba."]
[10.108911514282227, 1.6518751382827759, "The Orbital Period of the SZ-7 Spaceship is 91 minutes."]
[7.188801288604736, 9.766075134277344, "The Band 6 Wavelength of the OCM Payload is From 670 nm to 620 nm."]
[10.508493423461914, 7.3717875480651855, "The Material of the Thermal Isolation Components Satellite Component is Delrin."]
[5.998934268951416, 9.612274169921875, "The Total Mass of the SMILES Instrument is 475 kg."]
[9.009378433227539, 1.0875128507614136, "The Extended Science Mission Duration of the LRO Satellite is 9/17/2012 - 9/16/2014."]
[4.302168846130371, 4.469470500946045, "The Interface of the RM Radiation Monitor is CAN bus."]
[9.378209114074707, 5.740090847015381, "The Propulsion System of the DFACS Attitude Control System is CGPS (Cold Gas Propulsion System)."]
[6.668871879577637, 6.124878883361816, "The Measurement Objective of the ASCAT Instrument is Measure wind speed and direction over the oceans."]
[5.00318717956543, 6.212345600128174, "The Antenna Type of the UHF Transceiver Transceiver is Quadcanted monopole antenna array."]
[7.623232841491699, 0.48457077145576477, "The Launch Date of the Bartolomeo Payload Platform is June 2, 2016."]
[5.832283973693848, 9.062976837158203, "The Power Consumption of the UVS Instrument is 1 W."]
[7.146786689758301, 1.8851544857025146, "The Symposium Date of the SWOT Mission Satellite Mission is Sept. 24-29, 2012."]
[9.947022438049316, 5.241507530212402, "The Pressurized Module Interior Pressure of the JEM/Kibo Japanese Experiment Module is 1 atmosphere (1atm)."]
[11.063858032226562, 5.016481876373291, "The Speed of the CME Coronal Mass Ejection is Between 1.5 and 1.8 million miles an hour (700 and 800 km/s)."]
[9.407285690307617, -0.23938621580600739, "The Mission Objective of the FASTRAC Satellite is Perform on-orbit real-time GPS relative navigation between satellites."]
[7.334008693695068, 8.58530330657959, "The Wavelength of the LIDAR Instrument is 1064 nm."]
[6.719580173492432, 7.322998523712158, "The Telescopes of the IPDA LIDAR Instrument is Two separate telescopes for the transmission (TX) and reception (RX) of the laser."]
[4.451136589050293, 6.836071014404297, "The Frequencies of the DORIS Receiver is 2.03625 GHz, 401.25 MHz."]
[6.350271224975586, 6.0282745361328125, "The Function of the SGR-ReSI GNSS Reflectometry Instrument is Collect more data and allow processing on-board."]
[3.447772264480591, 4.604702949523926, "The Processor Speed of the Safe-mode Computer Computer is 400 MHz."]
[3.5231070518493652, 5.340573787689209, "The Total Capacity of the EUTELSAT KONNECT Satellite is 75 Gbit/s."]
[5.3111491203308105, 5.595147609710693, "The Signal of the FFRF Subsystem Relative Positioning System is GPS C/A navigation signal modulated on two S-band carrier frequencies (S1 and S2) with BPSK/QPSK modulation."]
[11.557068824768066, -1.2718241214752197, "The Mass (kg) of the TecSAR Satellite is 300."]
[9.090038299560547, 9.309483528137207, "The FOV (Field of View) of the CIPS Instrument is 80\u00ba x 120\u00ba."]
[8.773454666137695, 6.762086391448975, "The Purpose of the PME Plasma Measurement Equipment is Studying characteristic macroscopic properties of ionospheric plasmas."]
[9.520675659179688, 0.4628322422504425, "The Design Life of the Terra Satellite is 6 years."]
[6.163259983062744, 6.871876239776611, "The Zero Doppler Calibration of the Overall System System is Use of Tx leak signal."]
[6.870120525360107, 4.70929479598999, "The Product of the Climate Change Initiative Program is Maps that provide a global view of above-ground biomass."]
[10.354462623596191, 2.7984960079193115, "The Orbit Altitude of the Tiangong Space Station is About 400 kilometers."]
[8.307546615600586, 5.2309675216674805, "The Geometric Accuracy of the L1C Products Satellite Data is About 15 m (linear Root Mean Square)."]
[6.53063440322876, 2.73516583442688, "The URL of the Galileo Satellite System is http://m.esa.int/spaceinimages/Images/2018/07/Galileo_satellites_viewed_in_smartphone_app."]
[11.692502975463867, 1.6922086477279663, "The Landing Year of the Venera 9 Lander is 1975."]
[7.430717468261719, 8.892162322998047, "The Cross-Track Resolution of the MLS Spectrometer is 5 km."]
[9.867185592651367, 8.965442657470703, "The Telescope Type of the GOES Imager Imager is Cassegrain telescope."]
[5.993062973022461, 3.9620437622070312, "The Funding of the IASI Instrument is EUMETSAT."]
[9.473732948303223, 7.758355617523193, "The IR Detector Cooling of the Instrument Spectrometer is Two-stage passive radiative cooler with retractable earth shield."]
[7.692598342895508, 4.924816608428955, "The 3-axis stabilization of the BEESAT-2 Satellite is Yes."]
[6.638331890106201, 2.2726352214813232, "The Data Source of the IMERG Algorithm is GPM Core Observatory, GPM Constellation."]
[6.783023834228516, 6.133183002471924, "The Measurement Domain of the ISS-RapidScat Instrument is Ocean."]
[6.802000522613525, 3.8558244705200195, "The Image of the SEOSAT/Ingenio Satellite is SEOSAT in the cleanroom."]
[6.779202938079834, 4.344705581665039, "The Purpose of the CRISTAL Satellite Mission is Monitor remote regions from space over long periods of time."]
[5.353447914123535, 4.441642761230469, "The Location of the IMGEOS Ground Segment Facility is NRSC (National Remote Sensing Center), Shadnagar, Hyderabad Complex."]
[4.213134765625, 6.339777946472168, "The Frequency of the TT&R Telemetry, Telecommand & Ranging is Ku-band."]
[4.783102989196777, 0.20940209925174713, "The Investment in OneWeb of the Hughes Company is $50 million."]
[9.935379981994629, 2.8246712684631348, "The Altitude of the OneWeb Satellite Constellation is 1,200 kilometers."]
[5.725996494293213, 9.21146297454834, "The Power of the FSS Instrument is 0.1 W."]
[11.257516860961914, 6.746403217315674, "The Purpose of the NICER Mission is Observing X-ray MSPs for navigational purposes."]
[11.057734489440918, 3.514927625656128, "The Speed Relative to Jupiter of the Juno Spacecraft is Almost 130,000 mph (210,000 km/h)."]
[10.022787094116211, 2.8705832958221436, "The Altitude of Final Orbit of the OneWeb Satellites Satellite Manufacturer is 1,200 kilometers."]
[5.649781703948975, 9.147905349731445, "The Power of the ST (Star Tracker) Instrument is 6.5 W."]
[8.592000007629395, 0.40012818574905396, "The Projected Annual Crewed Missions of the SpaceX Company is Five or six."]
[5.734434127807617, 2.7396347522735596, "The Development Authors of the SpaceCube MINI Satellite is Michael Lin, Tom Flatley, Alessandro Geist, Dave Petrick."]
[7.122422218322754, 4.919713020324707, "The End Date of the Methane Leak Environmental Event is 26 September."]
[6.5981831550598145, 1.133512020111084, "The Presentation Date of the PRISMA mission Mission is May 29-31, 2013."]
[4.582695484161377, 5.549069404602051, "The NRT Data Downlink Frequency of the Sentinel-6 Satellite is X-band contact."]
[9.541053771972656, 6.07346248626709, "The Sun sensors of the ADCS Attitude Determination and Control Subsystem is 6."]
[9.492937088012695, 9.098591804504395, "The Entrance Aperture Diameter of the Telescope Optical Instrument is 50 mm."]
[4.550025463104248, 4.809398651123047, "The Function of the DWP Control System is Data compaction and compression, event selection, particle/wave correlation, and control of WHISPER."]
[8.825116157531738, 10.537683486938477, "The Image Resolution of the PMC Camera is 2.5 m."]
[7.274730205535889, 7.770341396331787, "The Observation Period of the MOMS-2P Instrument is May 5, 1996 to August 1999."]
[9.99988842010498, 3.5251901149749756, "The Current Orbit of the Galileo FOC satellites Satellite is Elliptical, with an eccentricity of 0.23, a semi major axis of 26,200 km and inclined at 49.8\u00ba."]
[7.534031391143799, 8.218865394592285, "The PI of the SOLSPC Radiometer is G. O. Thuillier."]
[5.751605033874512, 3.4818081855773926, "The Ground Control Location of the SSOT Satellite is Chile."]
[10.984265327453613, 4.767598628997803, "The Solar Wind Speed of the Solar Wind Satellite Satellite is Speeding up."]
[5.430539608001709, 2.8553316593170166, "The Designers of the Oculus-ASR Satellite is Undergraduate students of MTU (Michigan Technological University)."]
[6.712131977081299, 2.248347043991089, "The URL of the GPM Satellite is http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20110011761_2011012112.pdf."]
[7.492644309997559, 3.8078579902648926, "The Imaging Modes of the KazEOSat-2 Satellite is Agile."]
[7.76813268661499, 4.119230270385742, "The Proposed Mission of the Aditya-L1 Satellite is Conference on Coupling and Dynamics of the Solar Atmosphere\", Pune, India, Nov. 10-14, 2014."]
[6.833532810211182, 0.41962793469429016, "The Launch Date of the SGR-ReSI receiver Satellite Receiver is Q4 2016."]
[6.521995544433594, 3.3900396823883057, "The Development Partners of the ZACube-2 Satellite is CPUT, French South African Institute of Technology, South African Council for Scientific and Industrial Research (CSIR)."]
[6.401289463043213, 7.98204231262207, "The Launch Year of the AMSU Microwave Radiometer is 1998."]
[6.513333797454834, 7.405508995056152, "The Polarization of the High Resolution Spotlight Imaging Mode is Single or dual."]
[11.743261337280273, 4.686511993408203, "The Luminosity of the Eta Carinae Stellar System is One of the most luminous and massive stellar systems in our galaxy."]
[8.902682304382324, 0.9704850316047668, "The On-Orbit Operations of the LS-7 Satellite is 11 years."]
[4.117469310760498, 5.653807163238525, "The Transmit-Mode Duty Cycle of the RainCube Satellite is 25%."]
[7.174722671508789, 6.919456958770752, "The Study Date of the EPIC Instrument is June 27."]
[9.32404613494873, 7.749968528747559, "The Operating Temperature of the Detector Imaging Device is < 60\u00baC."]
[9.259634017944336, 7.7975239753723145, "The Measurement Range of the SWE Strahl sensor Sensor is 5 eV to 5 keV."]
[8.086196899414062, 2.7015700340270996, "The 10 Year Anniversary Date of the TerraSAR-X Satellite is June 14, 2017."]
[6.216770648956299, 0.5819349884986877, "The Launch Date of the CubeSat Satellite is 24 May 2022."]
[9.527852058410645, 0.8364859223365784, "The On-Orbit Duration of the CanX-4 Satellite is More than one year."]
[7.393928527832031, 10.05924129486084, "The Spectral Range of the High-Resolution Hyperspectral Imager Imager is 0.4 to 2.5 \u00b5m."]
[8.653732299804688, 9.149855613708496, "The Slit Width of the Spectrometer Instrument is 84 \u00b5m."]
[6.775726795196533, 5.8612380027771, "The Target Application of the SGR-ReSI receiver Satellite Receiver is Take wind speed measurements within hurricanes."]
[8.487946510314941, 8.95577621459961, "The Noise of the NISP IR Detector Detector is CDS readout noise shows the same performances demonstrated during the NRE phase."]
[9.765400886535645, 1.5888067483901978, "The Repeat Cycle of the IRS-1B Satellite is 22 days."]
[3.185835599899292, 5.1163554191589355, "The Capacity of the MMU Mass Memory Unit is 16 Gbit."]
[8.298942565917969, 8.880520820617676, "The Dithering Maneuver Requirement of the Spectrometer (SPI) Spectrometer is Required."]
[11.160165786743164, 6.998391628265381, "The Presenters of the An Efficient Photoelectric X-ray Polarimeter Device is Enrico Costa, Paolo Soffitta, Ronaldo Bellazzini, Alessandro Brez, Nicholas Lumb & Gloria Spandre."]
[9.861335754394531, 7.129899024963379, "The Joint Type of the Structure General is Brazed joint."]
[9.208077430725098, 8.335140228271484, "The Silicon Thickness of the L0 Detector Detector is 12 \u00b5m."]
[10.273904800415039, 4.249202728271484, "The Orbit Raising Time of the Safran/Snecma PPS-5000 Electric Propulsion is Approximately four months."]
[5.980597496032715, 2.5849552154541016, "The Launch Site of the EMIT Satellite is Kennedy Space Center in Florida."]
[8.625819206237793, 8.631628036499023, "The Optical System of the OCTS Sensor is Catoptric."]
[10.412147521972656, 3.1856672763824463, "The Initial Altitude of the NRCSD Payload is 385-400 km."]
[5.92754602432251, 6.758319854736328, "The Altitude of the SWIM Real Aperture Radar is 519 km."]
[7.230088710784912, 5.0203633308410645, "The Ability of the GHGSat Satellite Fleet is Pinpoint the source of even small leaks."]
[5.332540512084961, 10.381609916687012, "The Time Series of the ISS LIS Lightning Imaging Sensor is 16 years."]
[7.17903470993042, 8.515109062194824, "The Wavelength of the Laser Head Unit (LHU) Laser Unit is 1064 nm."]
[7.247404098510742, 0.35052675008773804, "The Launch Date of the LAICE Satellite is > 2023."]
[3.802938938140869, 4.467499732971191, "The Computing Power of the SCP Spacecraft Process Controller is 1 MIPS."]
[9.419917106628418, -0.7613208293914795, "The Launch Date of the Carbonite-1 Microsatellite is July 2015."]
[7.573069095611572, 2.4381635189056396, "The Safety Measures of the ELSA-d Mission is 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."]
[8.032013893127441, 2.7210073471069336, "The SAR Products Release Time of the TerraSAR-X Satellite is 5.5 months after launch."]
[6.221079349517822, 3.932734251022339, "The Function of the Lunar Ops E/PO Payload is Image the lunar surface."]
[6.333942890167236, 7.240805625915527, "The Measurement Accuracy of the D2P Radar Altimeter Altimeter is 1-3 cm average."]
[8.90335464477539, 9.055594444274902, "The Face Sheet Thickness of the Grating Optical Component is 1mm."]
[6.533173561096191, 8.525344848632812, "The Swath Width of the MESSR Radiometer is 200 km."]
[8.700336456298828, 3.6726980209350586, "The Operational Position of the GOES-S Satellite is 137.2\u00b0 West."]
[5.743930816650391, 3.083524227142334, "The Manufacturer of the VNREDSat-1A Satellite is Astrium."]
[10.033101081848145, 4.123493671417236, "The Propulsion of the NEA Scout CubeSat is Solar sail."]
[8.370894432067871, 7.369241714477539, "The Purpose of the CERN Radiation Testing Facility is Simulate conditions within Jupiter's massive magnetic field."]
[7.031766414642334, 6.575004577636719, "The Data Type of the Tropospheric Monitoring Instrument (TROPOMI) Instrument is High-resolution fluorescence data."]
[7.811662673950195, 9.165709495544434, "The Wavelength Detection Range of the Mapping Channel Spectrometer is 0.25 \u00b5m to 1 \u00b5m."]
[6.962970733642578, 5.595198631286621, "The Objective of the Gulfstream Supersite Experiment Location is Investigate oceanographic phenomena."]
[8.930022239685059, 9.766366958618164, "The Response of the Photodiode Detector is Linear."]
[11.840639114379883, -1.0178418159484863, "The Dry Mass of the IMP-8 Spacecraft is 371 kg."]
[10.546860694885254, 7.48466682434082, "The Structure Material of the CeREs Satellite is Teflon."]
[12.142228126525879, 3.3201029300689697, "The Orbit Inclination of the Aalto-1 Satellite is 97.44\u00ba."]
[2.145728349685669, 4.574885368347168, "The Payload Power of the Spacecraft Bus (Avionics Module=AM) Satellite is 350 W, 1.1 kW."]
[5.77971887588501, 3.008232593536377, "The AVGS Manufacturer of the ASTRO Satellite is NASA/MSFC."]
[9.488794326782227, 0.5664125680923462, "The Lifetime of the Spacecraft Platform Satellite is 7 years."]
[9.323954582214355, 3.1285336017608643, "The Orbit Type of the ELaNa-4 CubeSats Satellite is Near-circular orbit."]
[6.633807182312012, 1.264625906944275, "The Development Cooperation Agreement Date of the Alphabus Telecommunications Platform is March 2006."]
[8.176573753356934, 10.028901100158691, "The PAN Detector Array of the WV-3 Imager Imager is 35,000 pixel."]
[5.160946846008301, 4.136932849884033, "The Description of the SV-4 diagrams DoDAF 2 Viewpoint is Hierarchy of systems and system Functions."]
[7.938512802124023, 3.6934268474578857, "The Sensor Complement of the OPAL CubeSat is Not provided."]
[10.336365699768066, 5.083222389221191, "The Pressurant of the ACE propulsion system Propulsion System is Gaseous nitrogen."]
[2.022487163543701, 7.844107627868652, "The Solar Wind Speed and Beta of the ACE Satellite is Typically observed from the mid-1970s through the mid-1990s."]
[5.026510238647461, 6.084606647491455, "The Pulse Repetition Frequency (PRF) of the Satellite Satellite is 1795.33 Hz (Ku-band), 448.83 Hz (S-band)."]
[5.2243523597717285, 3.173424005508423, "The Bus Type of the NorSat-1 Satellite is Nanosatellite and a small microsatellite."]
[6.5346574783325195, 6.5387091636657715, "The Channels of the SGLI Imager is 11."]
[5.642762184143066, 2.853930950164795, "The Manufacturer of the SeaWiFS Satellite is Raytheon SBRC."]
[7.34813928604126, -0.18119966983795166, "The Launch Date of the Dnepr Rocket Launch Vehicle is Nov. 6, 2014."]
[5.457935333251953, 3.883800506591797, "The Purpose of the SIM Simulator is Testing and validation of operational procedures and databases, support the training of operators, and execution of simulation campaigns."]
[6.421245098114014, 5.862082004547119, "The Spatial Resolution of the L2SMP Soil Moisture Product is About 40 km."]
[2.9870896339416504, 6.708403587341309, "The Power of the X-band Transmitter Transmitter is 3.4 W."]
[6.73070764541626, 2.194796323776245, "The URL of the The Charter Satellite Program is http://www.disasterscharter.org/c/document_library/get_file?folderId=33636&name=DLFE-2502.pdf."]
[9.869780540466309, 1.4151884317398071, "The Period of the Landsat 9 Satellite is 99 minutes."]
[8.407601356506348, 2.901653289794922, "The Authors of the \"Discrete and broadband electron acceleration in Jupiter's powerful aurora\" Research Paper is 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."]
[7.604062557220459, 4.250110626220703, "The Image Type of the TWINS Satellite is Stereo ENA."]
[6.52390718460083, 1.2546534538269043, "The Launch Date of the Gokturk-2 Satellite is Dec. 18, 2012."]
[9.538056373596191, 0.9895673990249634, "The Mission Duration of the UKube-1 Satellite is Over 14 months."]
[7.533595561981201, 3.1208808422088623, "The Sensitivity of the Solar-B / Hinode Satellite is Unknown."]
[8.162903785705566, 7.37031364440918, "The Principal Investigator of the EFI Electric Fields Instrument is F. Mozer."]
[8.748744010925293, 6.603608131408691, "The | of the Coarse Pointing and Fine Pointing mechanism Pointing Mechanism is Coarse Pointing and Fine Pointing mechanism (CPA and FPA) for an optical communication link."]
[11.104816436767578, 5.30354118347168, "The Performance Requirement of the LISA Pathfinder Satellite is As close as possible to 10-12 ms-2 Hz-1/2 in the frequency band 10-3 to 10-1 Hz."]
[10.575366020202637, 8.503113746643066, "The FOV Overlap of the COR1 Coronagraph1 imager is Pointing stability required 1.5 arcsec over pB sequence (7 s)."]
[4.1148505210876465, 7.300031661987305, "The Mass of the TXS S-band Transmitter/Transceiver is 75 g."]
[7.513783931732178, 0.9406214952468872, "The Launch Date of the Sentinel-3B Satellite is Spring 2018."]
[5.9847540855407715, 3.7756030559539795, "The Contact Establishment of the Aeolus Spacecraft is Through the Troll ground station in Antarctica."]
[10.21667766571045, 2.9442641735076904, "The Altitude of the Satellite Satellite is 500-700 km."]
[5.241401195526123, 3.2553937435150146, "The Architecture of the MERLIN Satellite Satellite is Based on the AS250 (AstroSat) avionics core and integrates all Myriade Evolutions common units."]
[2.260991334915161, 3.89599609375, "The Solar Array Cells of the MarCO CubeSats Satellite is 42."]
[4.776247978210449, 1.6889609098434448, "The Space Segment of the Galileo Satellite Navigation System is 30 MEO satellites in 3 planes inclined at 56\u00ba."]
[7.613507270812988, 5.1212944984436035, "The Laser Observations Basis of the Starlette and Stella Satellites is Orbits and SLR stations' coordinates determination."]
[4.786842346191406, 9.05923843383789, "The Camera Function of the InSight Mars Lander is Guiding the placement of the SEIS and HP3 instruments, taking pictures of the surrounding landscape."]
[9.038947105407715, 6.5483574867248535, "The Type of the FOG 120 HR Gyro is High precision Fiber Optic Gyro."]
[7.333955764770508, 9.244003295898438, "The Number of Wavelength Positions of the FG (Filtergraph) Instrument is One for the continuum."]
[4.05970573425293, 5.120757579803467, "The Redundancy Approach of the SSTL Company is High degree of cold parallel redundancy."]
[5.955674648284912, 1.800018310546875, "The Product of the Kleos Space Company is GEOINT DaaS."]
[7.02092981338501, 2.500241279602051, "The URL of the Dove Satellite is https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=3797&context=smallsat."]
[5.690051555633545, 6.672113418579102, "The Length of the LRS (Lunar Radar Sounder) antennas Instrument is 15 m."]
[8.84837818145752, 9.371247291564941, "The Optical Efficiency of the Overall System is 0.6."]
[9.1033296585083, 10.740141868591309, "The Swath Width of the MSU-100 Camera is 960 km."]
[4.9170989990234375, 3.575080394744873, "The Decks of the Bus Satellite Structure is Bottom deck, top deck and payload deck."]
[7.359856605529785, 1.853115439414978, "The Mission Update of the Gravity Probe B Satellite is Sept. 26, 2008."]
[11.614110946655273, -1.2324469089508057, "The Mass of the Spacecraft Satellite is 80 kg."]
[7.297171115875244, 2.4000723361968994, "The Design Purpose of the First Arab mission to Mars Satellite is To inspire youth."]
[10.373833656311035, 1.3238873481750488, "The LTAN of the KOMPSAT-6 Satellite is 6 hours."]
[9.253067970275879, 4.194100856781006, "The Size of the Jugnu Satellite is 10 cm x 10 cm x 32 cm."]
[8.798221588134766, 6.370748519897461, "The Characteristic of the Plasmapause Boundary of Plasmasphere is Sudden drop in plasma density by the order of one magnitude."]
[12.101438522338867, 3.252406120300293, "The Inclination of the Orbit Centaur AV-042 upper stage is ~120.5\u00ba."]
[6.672166347503662, 7.7410664558410645, "The Operating Temperature of the GEDI Laser Laser System is 350 (\u00b12)\u00baC."]
[7.880552768707275, 1.9015629291534424, "The Arrival Date at Mars of the ExoMars 2020 mission Mission is March 2021."]
[9.099539756774902, 9.245901107788086, "The FOV of the Instrument Satellite Instrument is 19.3\u00ba."]
[7.308373928070068, 8.190963745117188, "The Spectrum Acquisition Time of the SOLSPC Radiometer is 11 minutes."]
[8.33278751373291, 6.719589710235596, "The Usage of the Testing Filters SWIR Instrument Component is During testing in ambient conditions."]
[8.673727989196777, 4.559363842010498, "The Stowed Configuration of the LF spacecraft Spacecraft is Illustrated in Figure 2(b)."]
[11.234166145324707, 6.683594703674316, "The Testing Date of the Xona's Navigation System Navigation System is Earlier this year."]
[8.126784324645996, 4.052095890045166, "The Ground Resolution of the Pl\u00e9iades Neo Satellite is Larger."]
[6.775591850280762, 6.091547012329102, "The Climatology Comparison of the ASCAT Satellite is RapidScat."]
[4.49448823928833, 5.8174872398376465, "The RF Communications of the Spacecraft Satellite is Up to 4 kbit/s."]
[11.805127143859863, -1.1180204153060913, "The Launch Mass of the GSAT-30 Satellite is 3357 kg."]
[4.419753074645996, 3.7757086753845215, "The Software of the TIE Payload is AIS (Automated Identification System)."]
[10.256081581115723, 2.949125051498413, "The Orbit Altitude of the MicroSat-2b Satellite is 514 km."]
[8.569832801818848, 1.6832412481307983, "The Approval Date of the WFIRST Space Telescope is 02 March 2020."]
[5.90997838973999, 2.307363748550415, "The Leading Company of the EPS-MACCS Satellite Mission is GomSpace in Denmark."]
[4.1487555503845215, 6.66135835647583, "The Wide Band Mode of the Receiver Communication System is \u00b1 10.0 kHz (- 3 dB )."]
[7.934237480163574, 6.783257484436035, "The Receiver Operation of the ColAIS Experiment is Alternating, switching every three months."]
[8.772248268127441, 8.345060348510742, "The Sample Diameter of the Microcalorimeter Microcalorimeter is 2.5 cm."]
[9.35336971282959, 3.366689682006836, "The Orbit Type of the ExoMars Orbiter Satellite is Elliptical."]
[8.215142250061035, 1.3476574420928955, "The Release Date of the Comet landscape Image is 01 October 2018."]
[6.531283855438232, 0.6262311339378357, "The Establishment Year of the Cospas-Sarsat Satellite-based emergency detecting and locating system is 1982."]
[10.18033504486084, 3.0222063064575195, "The Altitude of the OceanSat-1 Satellite is 720 km."]
[5.900022029876709, 0.7145296335220337, "The Image Capture Date of the AlSat Nano CubeSat is January 9, 2017."]
[8.435320854187012, 8.39553451538086, "The Detector Types of the Spectrometer Instrument is Silicon and extended InGaAs photodiodes."]
[11.877432823181152, 0.9838240146636963, "The Launch Center of the Chang'e-5 Spacecraft is Wenchang Space Center."]
[4.113163471221924, 3.934915781021118, "The Satellite Speed of the AIS System Communication System is ~7 km/s."]
[7.308612823486328, 3.1346092224121094, "The Design and Verification Status of the EarthCARE/CPR Satellite is Unknown."]
[6.273136138916016, 4.937459468841553, "The Deliverable of the Product Level 1C (L1C) Data is Level 1b data orthorectified, re-sampled to a specified grid."]
[13.183564186096191, 4.017977237701416, "The Scheduled Launch Date of the Gaia Satellite is 20 December."]
[7.39752197265625, 4.331081390380859, "The Calibration of the Landsat-7 ETM+ Satellite is On-orbit."]
[9.544217109680176, 9.092565536499023, "The Secondary Diameter of the Telescope Optical Instrument is 34 mm."]
[6.99240255355835, 4.280436038970947, "The Measurement Domain of the Tatiana-2 Satellite is Atmosphere."]
[5.350555419921875, 7.8719563484191895, "The Bandwidth of the SAW Filters Filters is 14 MHz."]
[7.218504905700684, 1.2617725133895874, "The Approval Date of the EPS-SG Satellite is Nov. 16, 2012."]
[9.087318420410156, 9.174656867980957, "The ACT FOV Incidence Angles of the Sentinel-5 instrument Instrument is Up to 54\u00b0."]
[3.854322910308838, 4.305638313293457, "The Components of the Data Handling System (DHS) System is Baseband Data Handling (DH) and Solid State Recorder (SSR)."]
[3.6669106483459473, 4.768980979919434, "The Processor of the PROBA-2 Satellite is 32-bit LEON2-FT RISC processor with up to 100 MIPS."]
[7.986780166625977, 7.4052348136901855, "The URL of the Airborne Lunar Spectral Irradiance (Air-LUSI) Instrument is https://airbornescience.nasa.gov/instrument/Air-LUSI."]
[7.375899791717529, 7.973383903503418, "The Minimum Concentration in 2015 of the Ozone Layer Atmospheric Layer is 101 Dobson Units."]
[4.07587194442749, 6.635818004608154, "The Clock Source of the X-band transmitter Transmitter is Local TXCO (Thermally Controlled Crystal Oscillator)."]
[9.782958030700684, 8.649495124816895, "The Configuration of the UVIT Telescope Assembly is Two telescopes."]
[10.347149848937988, 4.988551139831543, "The Thrust of the CUS Cryogenic Upper Stage is 73.55 kN."]
[1.599165678024292, 4.8780083656311035, "The Voltage of the S/C Power Satellite Power System is 28 V."]
[7.537100791931152, 0.6224024295806885, "The Mission Status of the SVOM Satellite is Planned."]
[9.641229629516602, -0.6317527294158936, "The Design Presentation Proceedings Date of the Microsatellites Satellite is Jan. 2005."]
[9.480632781982422, 0.9746889472007751, "The Mission Duration of the Spacecraft Satellite is 2 years."]
[4.024788856506348, 2.36946439743042, "The Size of the Dellingr CubeSat is 6U."]
[6.8409576416015625, 1.1622145175933838, "The Publication Date of the CONGO GPS/GIOVE Tracking Network is Sept. 1, 2009."]
[9.065139770507812, 9.079256057739258, "The FOV of the Particle Detector Instrument is \u00b121.8\u00ba."]
[9.785398483276367, 7.661801815032959, "The Energy: 0.4 keV (3.1 nm) of the N K-edge Atmospheric Cross Section Feature is N at 0.4 keV (3.1 nm)."]
[10.293205261230469, 4.921909332275391, "The Development Status of the 20 N Thruster Propulsion System is Near-flight-ready."]
[4.736586093902588, 4.318535804748535, "The Functions of the Satellite Management Unit Management Unit is Onboard Data Handling, power and control distribution."]
[6.7684807777404785, 4.320496082305908, "The Objective of the CRISTAL Satellite Mission is Simultaneously monitor snow depth and sea-ice thickness change over the Arctic."]
[9.317680358886719, 3.194045066833496, "The Orbit of the Telescope Optical Instrument is Lissajous orbit about L2."]
[5.335322380065918, 3.6238467693328857, "The | of the IXV Spaceplane is IXV."]
[9.600027084350586, -0.725080132484436, "The Objective of the Kent Ridge 1 Microsatellite is Integrate a VNIR/SWIR FTR (Fourier Transform Recovery) instrument into a microsatellite in support of disaster monitoring in Asia."]
[4.739254951477051, 6.059811592102051, "The Beacon Signal Frequency of the ALBus CubeSat Satellite is 400.4 MHz."]
[6.659780025482178, 8.975435256958008, "The Dimensions of the InP amplifier Amplifier is 900 x 560 \u00b5m2."]
[4.502015113830566, 4.688779830932617, "The Data Acquisition of the DAC Data Acquisition Card is Acquires temperature, current, and logic state values from sensors."]
[4.031491279602051, 10.349353790283203, "The NE\u0394T (K) of the ICI-9 Radiometer is 1.5."]
[10.81812858581543, 5.852432727813721, "The Flare Class of the Solar Dynamics Observatory Satellite is X1-class."]
[5.2269062995910645, 6.413755893707275, "The Reflector Type of the Antenna Subsystem Communication is 1m parabolic dish."]
[5.287115097045898, 4.320738315582275, "The Objective of the SOTA/SOCRATES mission Mission is Fundamental experiment for laser communication between LEO and the ground."]
[3.6212997436523438, 6.478391170501709, "The Data Rate of the Cadet-U UHF radio RF Communication Device is 3 Mbit/s."]
[5.879086494445801, 6.858593940734863, "The Azimuth Resolution of the SIR-C Phased Array is 7 m for the selected area."]
[7.9346537590026855, 4.74321174621582, "The Number of Instrument Units of the Solar Orbiter Spacecraft is 33."]
[6.2125773429870605, 6.838736057281494, "The Usage of the Radar Altimeter Altitude Measurement Device is Vertical descent phase."]
[8.277666091918945, 1.9122556447982788, "The Publication Date of the Herschel Satellite is Aug. 20, 2013."]
[8.154470443725586, 2.5454821586608887, "The Years on Orbit of the TerraSAR-X Satellite is 10."]
[11.725419044494629, 5.342005729675293, "The Environment Density of the GRB 130925A Gamma-Ray Burst is Low."]
[11.744250297546387, 4.53468132019043, "The Number of Identified Stars of the Delta Scuti stars Star Type is 60."]
[10.180795669555664, 2.947728395462036, "The Altitude of the Landsat 9 Satellite is 705 km."]
[10.68188762664795, 10.245372772216797, "The Number of Charge-to-Voltage Conversion Settings of the CTIA Charge Sensitive TransImpedance Amplifier is 4."]
[4.704853534698486, 2.0147197246551514, "The Quantity of the Flock 4v SuperDoves Satellite is 26."]
[5.910197734832764, 6.845494747161865, "The Pulse Amplitude of the RainCube Radar is Variable."]
[6.922359943389893, 1.9575610160827637, "The Launch Date of the EUTELSAT KONNECT Satellite is 17 January 2020."]
[3.5514936447143555, 4.093077659606934, "The PROM of the STRV-2 DHS Data Handling System is 32 k PROM."]
[8.201356887817383, 3.681359052658081, "The Magnetization of the Rosetta Spacecraft is Not magnetized."]
[5.398282527923584, 4.283592700958252, "The Services of the EuTEF Payload Facility is Delivers EuTEF downlinked TM Data to EuTEF Ground Segment."]
[6.052699089050293, 8.085113525390625, "The Data Transmission Rate of the MSR Radiometer is 2000 MHz."]
[10.166895866394043, 2.950676679611206, "The Orbit Altitude of the Hinode Satellite is 680 km."]
[3.7966580390930176, 6.630000114440918, "The Function of the Shaping Circuit Circuit is Reduce the length of the impulses and modify them to allow a numerical encoding."]
[9.28004264831543, 8.013047218322754, "The Components of the Focal Plane Cryostat Assembly Subsystem is Infra-red detectors, cold optics, cryocoolers, detection chain electronics."]
[7.156389236450195, 1.0377544164657593, "The EOL Operations Date of the D-Sat Satellite is October 10, 2017."]
[6.738358497619629, 0.06521117687225342, "The First TLE Payload Data Received of the Tatiana-2 Satellite is Oct. 21, 2009."]
[11.721153259277344, 1.7184213399887085, "The Number of Contacts with the Comet of the Philae lander Lander is Four times."]
[7.510863780975342, 2.7529702186584473, "The URL of the Tunneling Horizon Detector Detector is http://micromachine.stanford.edu/projects/tunneling_sensors/THD/THDSummary.html."]
[8.349807739257812, 10.396306037902832, "The Size, Weight, Power Reduction of the SPIDER Imaging Technology is 10 to 100 times."]
[6.077683925628662, 0.5871813297271729, "The Release Date of the CubeSats Satellite is January 16, 2017."]
[7.491690158843994, 2.5494725704193115, "The URL of the GaN Experiment Space Experiment is http://www.av.it.pt/medidas/space/Flayer/IT%20no%20Espa%C3%A7o%20EN_IT.pdf."]
[4.0908026695251465, 3.163980722427368, "The Implementing control-user plane split of the Open5GCore Rel. 4 5G Core Network is PFCP [N4]."]
[5.9936442375183105, 10.770743370056152, "The Thermal Gradients of the PF1 Passband Filter is Unknown."]
[8.228650093078613, 8.114480972290039, "The Calibration of the UVNS Spectrometer is High absolute accuracy using sunlight and on-board illumination sources every orbit."]
[9.588577270507812, 7.302624702453613, "The Burrowing Depth of the HP3 Instrument is 3 to 5 meters."]
[11.070530891418457, 3.5104644298553467, "The Closest Approach to the Sun of the ISON Comet is Unknown."]
[10.89055061340332, 3.356868267059326, "The Distance from Mars of the TGO Trace Gas Orbiter is About 41 million km."]
[6.38270378112793, 3.491523265838623, "The Risk Mitigation of the Autonomous Satellite Avoidance Program (ASAP) Satellite System is In Progress."]
[9.522500038146973, 6.0819220542907715, "The Sun Model of the ADCS Attitude Determination and Control System is Computes sun vectors."]
[3.9809927940368652, 2.342487335205078, "The Size of the SOAR Satellite is 3U CubeSat."]
[10.26357364654541, 4.946576118469238, "The Number of Thrusters of the Propulsion Subsystem Propulsion is 8 (2 x 4)."]
[11.578394889831543, 2.6330723762512207, "The Polar Regions of the Ryugu Asteroid is Very few craters."]
[7.8036065101623535, 5.940657138824463, "The Calibration Targets of the TRUTHS Satellite is Deserts and the moon."]
[9.156932830810547, 10.786445617675781, "The Swath Width of the MSU-50 Camera is 940 km."]
[10.134143829345703, 3.715276002883911, "The Vehicle Height with 5 m short PLF of the CBAS and EAGLE Spacecraft is Approximately 60 m."]
[1.208863615989685, 4.129733562469482, "The Battery Type of the CubeSat power module Power Control is Lithium-polymer."]
[6.447439670562744, 2.8864479064941406, "The Deployment Contract of the Diwata-1 Satellite is JAXA and Tohoku University."]
[8.616300582885742, 5.604865074157715, "The Mass of the IPS Pointing System is 1,180 kg."]
[5.980355262756348, 9.53635025024414, "The Mass of the MTQ Instrument is 225 g."]
[1.1684949398040771, 4.1443657875061035, "The Batteries Type of the Power Subsystem Satellite is Lithium-ion."]
[7.39572811126709, 6.823356628417969, "The Observation Dates of the MODIS Imaging Spectroradiometer is February 8-12, January 22-29, and January 14-17."]
[4.199650764465332, 3.745182514190674, "The Data Sampling Capacity of the NorAIS-2 Receiver AIS Receiver is Up to 512 MByte."]
[8.307921409606934, 10.42844295501709, "The Spectral Ranges of the 4-band CCD Imager Instrument is 0.42 - 0.50, 0.52 - 0.60, 0.61 - 0.69, 0.76 - 0.89 \u00b5m."]
[3.646038770675659, 4.7019147872924805, "The Processing Capability of the Processor Satellite Component is 14 MIPS."]
[4.678736686706543, 2.018592357635498, "The Quantity of the Flock-4v Satellite is 14."]
[6.543224334716797, 2.468494415283203, "The Website of the GOCE Satellite is http://www.amptek.com/didm.html."]
[10.191025733947754, 5.489254474639893, "The Connector of the ENT EVR Nozzle Tool is Quick Disconnect Connector."]
[9.771993637084961, 4.105325698852539, "The Deorbiting Technology of the CanX-7 Satellite is Drag Sail."]
[1.8191161155700684, 4.1561479568481445, "The Voltage of the Solar Array Power Source is 20\u201340 V."]
[9.3885498046875, 5.7664265632629395, "The Current Design of the DFACS Attitude Control System is CGPS (Cold Gas Propulsion System)."]
[4.335216045379639, 5.688518524169922, "The Experimental Uplink of the QSat Satellite is Ku-band, 10 Mbit/s."]
[9.808119773864746, 1.3461244106292725, "The Time to Stabilize of the Satellite Spacecraft is More than six hours."]
[5.155465602874756, 4.64047384262085, "The Backup for Rumpin of the Rancabungur Ground Station is True."]
[7.79342794418335, 8.958654403686523, "The Interference filter - Bandwidth of the Instrument Sensor is 1 nm."]
[8.403570175170898, 10.44227123260498, "The QE Variation of the Detector Arrays Sensor is Sub-pixel level."]
[9.335878372192383, 0.5110031962394714, "The Life Expectancy of the SPOT-4 Satellite is Unchanged at the end of 2012."]
[9.357626914978027, 7.822843551635742, "The Focal Plane Cooling of the Spectrometers Instrument is Passively cooled."]
[6.268070697784424, 2.837632894515991, "The Quote Source of the Carruthers Geocorona Observatory Spacecraft is Dr. Mackenzie Lystrup."]
[8.737947463989258, 0.16582341492176056, "The Reentry Date of the Skylab-1 Space Station is July 11, 1979."]
[3.559311866760254, 4.83888053894043, "The Processor of the MCM Memory System Module is TS68EN360 and XPC860."]
[9.263928413391113, 7.745695114135742, "The Operating Temperature of the Telescope Optical Instrument is 150 K."]
[7.032405853271484, 9.807138442993164, "The Wavelength Range of the Band No 4 Spectral Band is 3.50 \u00b1 0.50 - 4.10 \u00b1 0.50 \u00b5m."]
[7.232131004333496, 1.1865334510803223, "The Mission Start Date of the Triana Satellite is October 2, 2000."]
[5.023950099945068, 7.059995174407959, "The Reflector Dimension of the Antenna System Communication System is 65 cm."]
[5.8198018074035645, 3.040963649749756, "The Operating System of the UWE-1 Satellite is \u00b5CLinux."]
[11.337318420410156, 3.934558153152466, "The Orbital Period of the HAT-P-7 Exoplanet is 2.2 days."]
[11.89041805267334, 2.3705363273620605, "The Size of Mount Doom of the OSIRIS-REx Spacecraft is The size of a small parking lot."]
[6.264214515686035, 3.3159379959106445, "The Mission Type of the NigeriaSat-2 Satellite is Imaging."]
[10.370322227478027, 2.8684542179107666, "The Orbit Altitude of the CANYVAL-X CubeSats CubeSats is 505 km."]
[3.7134170532226562, 6.243891716003418, "The Data Rate of the TT&C Data Communication is 32 kbit/s."]
[7.298819541931152, 1.673033356666565, "The Data Analysis Plan of the THEMIS Probes Spacecraft is Look through archival THEMIS data for more events around Earth and determine how often the magnetopause may be booming like a drum."]
[8.634100914001465, 10.605610847473145, "The Resolution of the CCD Image Sensor is 512 x 2048 image pixels."]
[9.394325256347656, -0.7457727193832397, "The Launch Date of the M3MSat Microsatellite is Unknown."]
[6.99661922454834, 5.176122188568115, "The Data Source of the GEOS Model Weather and Climate Model is Actual measurements of physical properties."]
[6.5721540451049805, 2.714674711227417, "The Development Organizations of the SPIDER Imaging Sensor is Lockheed Martin Advanced Technology Center (LM ATC) and University of California at Davis (UC Davis)."]
[6.5252532958984375, 6.270124435424805, "The Observation Functions of the SGLI Satellite Instrument is NUV and polarization observations."]
[6.961283206939697, 1.8705388307571411, "The End of Mission Date of the Kolibri-2000 Satellite is May 3, 2002."]
[5.646646022796631, 3.508587598800659, "The Mission Objective of the UWE-1 Satellite is Analyze and optimize different implementations of Internet protocols in space."]
[7.978912353515625, 4.044164180755615, "The Mass of the Carbon Dioxide Ice Patch Surface Feature is 57 kg."]
[9.685446739196777, 7.796444892883301, "The Energy Range for Charged Particles of the FREND Instrument is 0.5\u201310 MeV."]
[9.334420204162598, 1.7617830038070679, "The Measurement Frequency of the Satellite RMIB TSI is Twice per day."]
[8.416637420654297, 3.039579153060913, "The Auroral Potentials of the Earth Planet is Several thousands of volts."]
[7.122702598571777, 8.760398864746094, "The Scan Rate of the VIRR Instrument is 48 rpm."]
[8.93709945678711, 10.130393981933594, "The Camera Quantity of the LED-arrays Lighting System is 2."]
[10.213565826416016, 4.974611282348633, "The Quantity of the Propulsion System Satellite Propulsion is 8."]
[3.653412103652954, 6.331447124481201, "The Downlink Beacon Data Rate of the RF Communications Communication System is 20 bit/s."]
[9.018641471862793, 8.692225456237793, "The Full-Aperture Reference Surface Temperature of the TIR Subsystem Imaging System is 340 K."]
[7.057007312774658, 0.7552078366279602, "The Launch Date of the Space Technology 5 Satellite is Unknown."]
[6.19201135635376, 0.6111352443695068, "The Launch Date of the TROPICS cubesats Satellite is 12 June 2022."]
[8.886857986450195, 5.632270336151123, "The Platform of the CASPR Experiment is Gimbal-actuated platform."]
[11.415167808532715, 4.426458358764648, "The Average Upper Atmosphere Temperature of the Jupiter Planet is About minus 100 \u00ba Fahrenheit or a chilly minus 73\u00ba Celsius."]
[6.375510215759277, 8.551767349243164, "The Vertical Resolution of the JPL Microwave Radiometer Radiometer is 240 m."]
[9.41436767578125, 0.7337625622749329, "The Operation Lifetime of the TerraSAR-X Satellite is 10 years."]
[5.003345012664795, 6.753807544708252, "The Antenna Gain (dB) of the Antenna Reflector is >30."]
[8.511171340942383, 7.8136515617370605, "The Cadence of the Composition of the Radiation Measurement is 30 minutes."]
[8.194940567016602, 5.0092620849609375, "The Geolocation Accuracy Test Location of the Ikonos-2 Satellite is Big Spring, TX."]
[5.073038578033447, 4.343533992767334, "The Operation of the Payload Data Data is Continuous throughout the mission life."]
[4.579268932342529, 2.059541702270508, "The Total Impulse of the SkySat-6 Satellite is 269 Ns."]
[7.446741580963135, 0.8109707236289978, "The Image Acquisition Date of the PROBA-V Satellite is Feb. 7, 2014."]
[5.298525810241699, 4.131834983825684, "The Ground Segment Components of the SARah system Satellite System is All necessary components for the ground segment."]
[11.429737091064453, 4.253962993621826, "The Planet of the AU Microscopii Star is Yes."]
[8.074956893920898, 11.138811111450195, "The Sensitivity of the Channel 4 Sensor is 0.3 K/pixel."]
[9.925093650817871, 8.642033576965332, "The Telescopes of the ROLO Robotic Lunar Observatory is 2."]
[6.554910182952881, 3.250568389892578, "The Operator of the Resurs-P1 Satellite is Roscosmos (Russian Federal Space Agency)."]
[6.136211395263672, 0.8754249811172485, "The Launch Date of the Iridium NEXT Satellite Constellation is June 2010."]
[9.277316093444824, 5.1633429527282715, "The Attitude Control Mode of the Hayabusa-2 Spacecraft is One wheel control mode."]
[9.767633438110352, -0.6184598207473755, "The Orbit Period of the BX-1 Microsatellite is 90.1 minutes."]
[7.419979095458984, 0.8051590919494629, "The Development Start Date of the Satellites around the Moon Satellite Constellation is 20 May 2021."]
[9.368282318115234, 10.24488353729248, "The Orbital Angles of the PolyCam Camera is Northern hemisphere, equator, southern hemisphere."]
[8.973370552062988, 4.492711544036865, "The S/C Structure of the IRS-1C and IRS-1D Spacecraft is Main platform and the payload platform (aluminium honeycomb structure)."]
[7.956820964813232, -0.09567248821258545, "The Usage of the MDA Dock is Dock for the command and service modules."]
[3.6312053203582764, 6.325626373291016, "The Downlink Data Rate of the RF Communications Communication System is 320 Mbit/s."]
[10.508500099182129, 8.517685890197754, "The Cadence of the MiniCOR Coronagraph is ~15 images/hour."]
[10.532432556152344, -1.0373106002807617, "The Mass of the Microsatellites Satellite is < 100 kg."]
[5.500611782073975, 4.277052402496338, "The Service Spectrum of the NPOESS Program is Onboard acquisition and transmission (broadcast) of telemetry data in real-time to field terminals of the user community."]
[7.303377628326416, 7.017516613006592, "The Comparison of the CUMULOS Data is VIIRS, MODIS, DMSP, CIRC, and related on-orbit microbolometers."]
[4.112399578094482, 7.356058597564697, "The Mass of the OSIRISv3 Laser Communication Terminal is 1.65 kg."]
[10.083200454711914, 5.169113636016846, "The Force of the ESP Thrusters Maneuvering System is Provides force in the normal direction."]
[7.776975154876709, 1.5151870250701904, "The Arrival Date of the Hera Spacecraft is November 2024."]
[3.755312919616699, 5.884869575500488, "The Data Transfer Rate of the LCRD Payload is Approximately 1.2 Gbit/s."]
[6.528761386871338, 5.784908771514893, "The Refractivity Profile Comparison Time of the GNOS Instrument Occultation Measurement Device is Within 1 hour."]
[5.854454517364502, 3.846944570541382, "The Ground Segment Locations of the Dove-2 Satellite is 5."]
[7.747150897979736, 2.905444860458374, "The Launch Date of the CartoSat-1 Satellite is May 5, 2005."]
[5.842495441436768, 5.479036331176758, "The URL of the TriG GNSS Receiver is http://authors.library.caltech.edu/21729/1/."]
[4.715378761291504, 7.220154762268066, "The On-board Data Analysis of the GimmeRF Radio Instrument is Up to 2 TFLOPs."]
[6.442890167236328, -0.611413836479187, "The Clocks of the QZS-1 Satellite is Two rubidium atomic clocks."]
[3.6335160732269287, 6.198803901672363, "The Downlink Data Rate of the S-band system Communication System is 102 MB/day."]
[9.414959907531738, 4.52671480178833, "The Ecliptic Latitude Range of the NEOSSat Satellite is Tentatively \u00b1 40\u00ba."]
[9.22263240814209, 3.2969138622283936, "The Orbit of the DSCOVR Spacecraft is Lissajous orbit about L1."]
[6.700892448425293, 0.799334704875946, "The Launch Date of the SEOSAT-Ingenio Satellite is Later this year."]
[4.577020645141602, 4.726761817932129, "The Science Data Collection Modes of the DPU Data Processing Unit is Two."]
[11.18691635131836, 4.232576847076416, "The Number of Planets of the Kepler space telescope Telescope is Billions."]
[6.1373395919799805, 3.539477586746216, "The Ground Support Provider of the TanSat Satellite Mission is NSMC (National Satellite Meteorological Center)."]
[10.736573219299316, 10.293517112731934, "The Differential non-linearity of the PHA Detector is <1%."]
[3.5854263305664062, 2.290609359741211, "The Size of the E-TBEx Satellite is 3U."]
[9.238253593444824, 4.117829322814941, "The Size of the Spacecraft Satellite is 7.5 m (high), 4 m x 4 m overall cross section."]
[9.326647758483887, 4.847986698150635, "The Solar Array Normal Vector and Sun Vector Difference of the Spacecraft Satellite is Up to 30 degrees during eclipse seasons."]
[7.300022125244141, 4.06675910949707, "The Instrument of the DMC-3 Satellite Constellation is MSI (BJ-2)."]
[8.384308815002441, 1.6280326843261719, "The Date of the Next Flyby of Jupiter Event is July 21."]
[6.325962543487549, 1.6571048498153687, "The Update Date of the Jason-3 Satellite is Feb. 12, 2016."]
[10.38199520111084, 2.8004236221313477, "The Orbit Altitude of the ISS Space Station is ~400 km."]
[8.219635963439941, 1.1098390817642212, "The Capture Time of the Images Image is Around 10:30 JST on 6 January 2018."]
[4.850886344909668, 2.1259243488311768, "The Quantity of the CubeSats Satellite is 12."]
[9.815475463867188, -0.9729986786842346, "The Attitude Control of the JL-1-GF03B Microsatellite is 3-axis, 4 flywheels."]
[8.120136260986328, 11.1417875289917, "The Radiation Tolerance of the Linear Encoder Sensor is <1 krad TID."]
[11.391297340393066, 1.0509381294250488, "The Manufacturer of the Tianwen-1 Mars Lander is China."]
[11.342869758605957, 1.3975715637207031, "The Design Life of the Yutu-2 Lunar Rover is Three months."]
[6.40071964263916, 4.839681625366211, "The Level 1 Products of the Sentinel-6 Satellite is 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 ar."]
[5.8443474769592285, 7.177088260650635, "The Antenna Size of the Altimetry Instrument Instrument is 1.2 m."]
[4.716945648193359, 1.8286035060882568, "The Number of Satellites of the T1TL Prototype Constellation Satellite Constellation is 42."]
[3.6858437061309814, 4.291904449462891, "The On-board Computer of the IOD-1 GEMS Satellite is CSL On-board Computer (OBC) with integrated GPS receiver."]
[9.01950740814209, 9.67162036895752, "The Control of the Shutter Optical System Component is Sun Sensor."]
[7.983622074127197, 5.563599586486816, "The Signal to Noise Ratio (SNR) of the Climate Observatory Satellite is ~300 in the vis-NIR."]
[8.893386840820312, 2.7752132415771484, "The Launch Date of the GCOM-C Satellite is 23 December 2017."]
[12.181647300720215, 5.383894443511963, "The Warm Component Percentage of the Universe Cosmology is 15 percent."]
[5.045395374298096, 7.481105327606201, "The Average Data Rate Over Land of the KaRIN Instrument is ~271 Mbit/s."]
[7.623000621795654, 4.059496879577637, "The Observation Location of the ALOS satellite Satellite is Al Jawf oasis in southeastern Libya."]
[7.436981201171875, 1.0932186841964722, "The Utilization Presentation Date of the ISERV Pathfinder EO Sensor is Oct. 1-5, 2012."]
[6.11466121673584, 5.730957508087158, "The Conference Presentation Date of the ROSA Radio-Occultation Receiver Receiver is Dec. 8-10, 2010."]
[11.2330961227417, 3.5199975967407227, "The Solar Wind Behavior of the Comet 67P Comet is Beforehand, particles had been slower-moving, and the solar wind had been generally weaker."]
[7.530418395996094, 4.255166053771973, "The Primary Instrument of the CryoSat-2 Satellite is SIRAL (SAR (Synthetic Aperture Radar) Interferometer Radar Altimeter)."]
[6.357694625854492, 9.725467681884766, "The Mass of the Optical Scanning Design Imaging Spectrometer is 150 kg."]
[9.439295768737793, 0.46376001834869385, "The Design Life of the OceanSat-2 Satellite is 5 years."]
[6.844372272491455, 3.2930378913879395, "The Mission Status of the Satellite EO is Operational (extended)."]
[10.365785598754883, 5.094935417175293, "The Pressure of the PROP unit Propulsion System is 300 bar."]
[9.366637229919434, 10.375504493713379, "The Installation Location of the Metric Camera Camera is Inside the pressurized cabin of the Spacelab module."]
[7.3059821128845215, 2.2478442192077637, "The Launch Date of the NASA Orbiting Carbon Observatory-2 Satellite is Unknown."]
[6.306184768676758, 5.463974952697754, "The Sensor Type of the Satellite STRATOS is GNSS receiver."]
[9.931476593017578, -0.6966744661331177, "The Boom Length of the Microsatellite Satellite is 2 m."]
[8.81556224822998, 0.2396862804889679, "The Duration of the Spacewalk Activity is About five-and-a-half hours."]
[9.259015083312988, 10.108660697937012, "The Principal Investigator of the LROC Camera System is Mark Robinson."]
[4.338508129119873, 5.670510768890381, "The Downlink Band of the Spacecraft Satellite is S-band (variable to 2 Mbit/s)."]
[9.358651161193848, 7.788477420806885, "The Measurement Range of the Particle Detector Instrument is Deuteron : 8 MeV/n ~ 26 MeV/n."]
[5.683538913726807, 2.6801583766937256, "The Manufacturer of the SBSS-1 Pathfinder Satellite is Boeing."]
[12.994811058044434, 4.858297824859619, "The Mission Start Date of the IBEX Spacecraft is Unknown."]
[4.401725769042969, 7.033977508544922, "The Electronics Unit Weight of the PRARE ground transponder Ground Station Equipment is 35 kg."]
[11.478044509887695, 1.527279019355774, "The Activation Time of the NGC Lander Lander is Before the separation from orbiter."]
[7.860352039337158, 7.75294303894043, "The Relative Accuracy of the Instrument Sensor is Better than 1% for 45 s counting time on IP signal."]
[9.22618293762207, 2.628185272216797, "The Impact Date of the DART Spacecraft is October, 2022."]
[9.56313419342041, 0.4664630591869354, "The Spacecraft Design Life of the QuickBird-2 Satellite is 5 years."]
[11.23057746887207, 3.545290946960449, "The Shape of the 67P/Churyumov-Gerasimenko Comet is Dual-lobed."]
[8.40926742553711, 4.619411945343018, "The Swath width of the ALOS/PRISM Satellite is 35 km / 70 km."]
[9.642874717712402, 4.20463752746582, "The Aperture Antenna Diameter of the COMMx Payload is 3.66 m."]
[6.739367485046387, 6.148350238800049, "The Measurement Swath of the ISS-RapidScat Scatterometer is Smaller by a factor of two compared to QuikSCAT."]
[8.44742202758789, 8.020699501037598, "The Percentage of Sky Observed in Three Exposures of the Euclid Reference Survey Survey is 47%."]
[5.976484775543213, 9.610939979553223, "The Mass of the DORIS Instrument is 15 kg."]
[11.711283683776855, -1.0523974895477295, "The Payload Mass of the Spacecraft Satellite is 33.3 kg."]
[5.928711414337158, 0.6735644340515137, "The Presentation Date of the MinXSS CubeSat is June 3-5, 2013."]
[8.90321159362793, 10.4813871383667, "The Resolution of the CMOS Camera Sensor is 3000 x 2000 pixels."]
[3.8866477012634277, 5.865421772003174, "The Operation Time of the LEO-to-ground radio link Communication System is Twelve minutes."]
[6.990383625030518, 3.5082709789276123, "The Headquarters of the EROS-B Satellite is Netherlands Antilles (Cayman Islands)."]
[7.134005069732666, 0.671854555606842, "The Launch Date of the ASNARO Satellite is Nov. 6, 2014."]
[6.03593111038208, 9.626839637756348, "The Instrument Mass of the DUST sensor Cosmic Dust Sensor is 3.8 kg."]
[3.4750730991363525, 5.332251071929932, "The Storage Capacity of the TUBSAT-N Satellite is Over 6000 messages at 134 bytes in length."]
[7.061274528503418, 3.6246495246887207, "The Location of the ORBIMAGE Satellite Operations Center Satellite Operations Center is Dulles, VA."]
[3.8064606189727783, 2.2925825119018555, "The Size of the Irvine 02 CubeSat is 1U."]
[7.353294849395752, 2.6691277027130127, "The URL of the ACE - Advanced Composition Explorer Satellite is http://www.nasa.gov/press-release/goddard/2016/ace-cosmic-ray."]
[6.61819314956665, 0.6304943561553955, "The Launch Date of the NorSat-2 Satellite is July 2017."]
[6.536457538604736, -0.12328317761421204, "The Flight of the PSLV-C16 Satellite is Successful."]
[8.259212493896484, 1.4674991369247437, "The Image Posting Date of the Rosetta Satellite is March 4, 2015."]
[3.606445074081421, 6.376356601715088, "The Symbol Rate of the Channel Communication System is 76.8 Msps."]
[7.827023506164551, 4.475447654724121, "The Image Resolution of the RISING-2 Satellite is Unknown."]
[8.382956504821777, 10.522850036621094, "The Number of CCD Elements in Cross-track of the MSU-100 Camera is 8000."]
[9.883464813232422, 1.4259867668151855, "The Commissioning Phase Duration of the CALIPSO Satellite is 38 days."]
[9.418340682983398, 6.483436584472656, "The | of the MicroASC Star Tracker is MicroASC A Miniature Star Tracker."]
[8.252946853637695, 9.111754417419434, "The Swath Width of the HORUS Sensor is 15 km."]
[5.994584560394287, 6.270157337188721, "The Ka-band Radar Frequency of the Tomorrow-R1 and -R2 Satellite is 35.75 GHz."]
[7.7169904708862305, 7.156850814819336, "The Measurement Frequency of the TEMPO Instrument is Hourly."]
[6.510830879211426, 1.2649662494659424, "The Bulletin Date of the GOCE Satellite is February 2008."]
[6.892719268798828, 3.541438579559326, "The RPO Capability of the GSSAP Satellite is Yes."]
[7.263317584991455, 3.0070948600769043, "The Mission Status of the BeiDou-2 Satellite is Unknown."]
[2.285917043685913, 4.399085521697998, "The Power Requirement of the CubeSats Satellite is None."]
[9.83939266204834, 6.7501220703125, "The Cooling Temperature of the Baseplate of the Vessel Satellite Component is 15\u00b0C."]
[9.486699104309082, -2.5054194927215576, "The Mass of the LEICA Particle Detector is 7.4 kg."]
[6.879539966583252, 3.153672218322754, "The Operational Status of the MTSAT-2 Satellite is Operational."]
[6.501132965087891, 5.063243389129639, "The Imaging Frequency Band of the TerraSAR-X Satellite is X."]
[11.403389930725098, 6.650301456451416, "The Detector Units Status of the IXPE observatory X-ray Observatory is Complete."]
[10.972003936767578, 2.5457608699798584, "The Touchdown Requirement of the Lander Module Spacecraft Module is < 5 m/s in vertical and horizontal velocity."]
[7.553806781768799, 1.000429630279541, "The Launch Date of the Sentinel-1A Satellite is 2013+."]
[9.69083309173584, -0.8147852420806885, "The Form Factor of the PACE nanosatellite Satellite is 2U CubeSat standard."]
[2.282773494720459, 4.343403339385986, "The Power of the QSat Satellite is 74 W."]
[5.249100685119629, 5.512334823608398, "The Manufacturer of the Antenna Device is TICRA."]
[9.282413482666016, 7.639925479888916, "The Electrical Noise Measurement of the ELS-A Sensor is 16.3 keV."]
[10.204035758972168, 4.916614055633545, "The Propellant of the OSAM-1 Satellite is Bi-propellant and mono-propellant."]
[1.5364304780960083, 4.891413688659668, "The Main Bus Voltage of the MRU Main Regulator Unit is 28 V."]
[6.686518669128418, 5.2956342697143555, "The Geometric Resolution of the TerraSAR-X Satellite is Up to 0.25 m."]
[7.906620979309082, 3.1822128295898438, "The Predicted Quantity of the Fragments Debris is 85 k."]
[12.073352813720703, 5.303930759429932, "The Effect of the Dark Energy Hypothetical Energy is Shoving galaxies away from each other."]
[8.652219772338867, 6.900525093078613, "The Sensitivity of the Magnetic Field Sensor Sensor is Sub-picotesla."]
[9.080806732177734, 10.810476303100586, "The Swath Width of the TAC Camera is 52 km."]
[1.591286301612854, 4.490479469299316, "The Output Current of the Buck-Boost Converter Solar Array Regulator is 0 - 8 A."]
[8.202438354492188, 5.637039661407471, "The Leading Noise Terms of the Satellite Spacecraft is Magnetic disturbances."]
[7.681767463684082, 1.0736334323883057, "The Anomaly Update of the Copernicus Sentinel-1B Satellite is 25 February 2022."]
[7.190456390380859, 6.968767166137695, "The Number of Thermal Emissive Bands of the VIIRS Satellite is 7."]
[5.162497043609619, 5.669948101043701, "The Dish Size of the Stanford Research International Ground Station is 18.3 m."]
[5.355158805847168, 2.6016242504119873, "The Manufacturer of the NanoSatC-Br1 1U CubeSat is Southern Regional Space Research Center and of INPE."]
[9.49858570098877, 1.539019227027893, "The Observation Goal of the DELPHINUS Satellite is Detect over a hundred LIFs in a month."]
[8.058027267456055, 4.798422813415527, "The Value of the Spatial Resolution Satellite Instrument is 8.4 x 4.4 km."]
[10.411133766174316, 5.473795413970947, "The Length of the Tether Satellite Component is 4 km."]
[6.121646881103516, 2.012000799179077, "The Launch Site of the NPP Satellite is VAFB, CA."]
[8.708841323852539, 5.361508369445801, "The Attitude Determination of the Spacecraft Satellite is 10 arcsec."]
[7.2833685874938965, 0.17300380766391754, "The Launch Date of the MEV-1 Satellite is October 2019."]
[11.915844917297363, 3.364844560623169, "The Inclination of the SMART-1 Satellite is 90.188\u00ba."]
[9.334300994873047, 7.653237819671631, "The Apparent Cooling of the GeoSTAR Scattering Approach is Can exceed 100 K."]
[5.610818862915039, 3.090945243835449, "The Manufacturer of the SPOT-6 Satellite is Astrium Services Division of EADS."]
[7.562610149383545, 1.8336526155471802, "The Impact Status of the LADEE Satellite is Planned."]
[4.934471130371094, 1.7301077842712402, "The Mission Count of the X-37B space plane Space Plane is 4."]
[7.5944504737854, 8.819075584411621, "The LOS IAR Rotation Angle of the Integer Ambiguity Resolution Process is 50o."]
[10.20119571685791, 5.0014543533325195, "The Thrust of the Electric Propulsion Test Subsystem Satellite Subsystem is 40 mN\u00b14mN."]
[6.310303211212158, 10.051838874816895, "The Mass of the MSU-100 Camera is 2.9 kg."]
[9.280447006225586, 5.502234935760498, "The Attitude Control of the GNB Satellite is Passive magnetic attitude control."]
[8.573701858520508, 9.835258483886719, "The Field of View of the EPIC Cameras Imaging System is 30 arcmin."]
[9.918595314025879, -0.5776932239532471, "The Stabilization of the Tsubame Microsatellite is 3-axis."]
[7.019648551940918, 0.7853195071220398, "The Operation End Date of the BIRD Satellite is December 2005."]
[1.7954741716384888, 5.321489334106445, "The Voltage of the Voltage 3 Digital is 5.5\u00b12%."]
[8.822774887084961, 9.272954940795898, "The FOV of the Short Wavelength Band Spectrometer is 4\u00ba x 5'."]
[8.420416831970215, 5.384793758392334, "The Pointing Stability Requirement of the IRS Sounder Satellite is 300 m at SSP."]
[5.963549613952637, 9.573325157165527, "The Mass of the DIDM Instrument is 2.2 kg."]
[7.228099346160889, 2.3809757232666016, "The Purpose of the Emirates Mars Mission Mission is Accelerate the development of the UAE\u2019s space sector, education and science community."]
[7.184289455413818, 2.4423980712890625, "The URL of the SMAP Satellite is http://smap.jpl.nasa.gov/mission/description."]
[6.3412041664123535, 1.0568879842758179, "The Workshop Date of the COSMO-SkyMed Satellite is June 12-13, 2007."]
[9.0658597946167, 10.600604057312012, "The Pixel Size of the Main Camera Camera is 300 m."]
[9.408167839050293, 0.49431437253952026, "The Operational Life of the Spacecraft Satellite is \u2265 7.5 years from the end of IOT."]
[7.913531303405762, 8.257524490356445, "The Purpose of the CHRIS Imaging Spectrometer is Terrestrial and aquatic observation."]
[2.632460117340088, -1.4565706253051758, "The Brigthness Temperature (BT) Sensitivity of the Antenna Reflector is \u00b10.29 K."]
[10.285966873168945, 2.951225519180298, "The Altitude of the Satellite Satellite is 904 km."]
[2.5689570903778076, 5.337263584136963, "The Power Consumption of the DPU Digital Processing Unit is < 29 W."]
[9.773282051086426, 6.878737926483154, "The Thermal Operational Stability of the Instrument Satellite Instrument is \u00b11\u00baC."]
[8.228543281555176, 3.7157349586486816, "The Risk of Collision of the AeroCube-OCSD-B and -C Satellites is Little risk."]
[4.996330738067627, -0.13086570799350739, "The Full Commercial Service Launch of the OneWeb Satellite Constellation is 2022."]
[5.912070274353027, 1.8583581447601318, "The Launch Vehicle of the Starliner Spacecraft is United Launch Alliance Atlas 5 rocket."]
[3.850963830947876, 6.009134292602539, "The Data Samples of the Experiment Data Telemetry is Roughly 1.3 million."]
[7.984339237213135, 9.731171607971191, "The High Spatial Resolution of the AMI Advanced Meteorological Imager is 0.5-1.0 km for VIS and 2 km for the infrared channels."]
[8.65683650970459, 10.377769470214844, "The CCD Array Elements of the LISS-3 Linear Imaging Self-Scanning Sensor is 6000."]
[4.512322425842285, 7.097020626068115, "The Frequency of the Millimeterwave receiver Receiver is 188.5 \u2013 191.5 GHz."]
[6.333835601806641, 3.5290863513946533, "The Benefits of the ASAP Autonomy System is Fast response to external events, reduces overall mission costs."]
[8.631047248840332, 5.631106853485107, "The Internal Magnetometer Calibration Method of the RAX-1 Satellite is Scalar based method that involved simple rotations of the satellite in a known magnetic field during ground calibration."]
[7.8330583572387695, 9.08980655670166, "The NER of the Spectral Band A Spectrometer is 3.0 x 10^-5 W/(cm^2 sr \u00b5m)."]
[7.393312931060791, 0.7886111736297607, "The Arrival Date to Lunar Orbit of the CAPSTONE Satellite is November 13, 2022."]
[6.921448707580566, 4.719664573669434, "The Measurement Domain of the Biomass Satellite is Land."]
[9.303579330444336, 0.3536101281642914, "The Exceeded Design Life of the Landsat-7 Satellite is Yes."]
[4.941554069519043, 2.5325024127960205, "The Minimum BCRs for Normal Function of the DubaiSat-2 Satellite is Two BCRs."]
[1.2192643880844116, 4.168159484863281, "The NiCd Batteries Capacity of the EURECA Spacecraft is 40 Ah."]
[8.222593307495117, 4.900652885437012, "The GSD (nadir) of the Payload Satellite Subsystem is Pan = \u22642.5 m, MS = \u226410 m."]
[7.037367343902588, 8.790128707885742, "The Ground Resolution (Infrared Channel) of the VIRR Instrument is 4.4 km."]
[7.444469451904297, 4.689850807189941, "The Monitoring Area of the PROBA-V Satellite is Europe and Africa."]
[7.747330188751221, 10.709245681762695, "The Sampling Interval of the sADC A/D Converter is 12 \u00b5s."]
[10.84292984008789, 5.635838985443115, "The Occurrence of the Solar Flare Natural Phenomenon is Second largest to have occurred from the past 11-year solar cycle."]
[5.131723880767822, 4.408284664154053, "The Functions of the Ground Segment System is 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, gene."]
[6.158637046813965, 2.0664823055267334, "The Launch Vehicle of the Yubileyniy-2/MiR Satellite is Rockot/Briz-KM."]
[7.796419143676758, 1.826611042022705, "The Newsletter Issue of the SHADOZ Ozonesondes is 11."]
[8.322686195373535, 4.809596538543701, "The Purpose of the MMS Satellite is Capture the show of charged particles in the magnetosphere."]
[7.282815933227539, 6.974185943603516, "The Operation Period of the ACLS Air and Oxygen System is Until the end of 2019."]
[2.2840445041656494, 4.473062038421631, "The Power of the TRMM Satellite is 1100 W."]
[7.961899757385254, 5.021203517913818, "The Objectives of the PIXIE Satellite is 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 ionizati."]
[7.726612091064453, 13.577255249023438, "The Resolution \u0394\u03bb (0.10\u00ba slit) of the SPIM2 Spectrometer is 1.2 nm."]
[9.332025527954102, 1.1639643907546997, "The Contact Separation of the PROBA Project Satellite Project is 14h for the nominal operations."]
[4.809356212615967, 1.8166316747665405, "The Total Satellite Missions of the ICEYE Satellite Operator is 10."]
[8.61529541015625, 1.6970930099487305, "The Mission End Date of the Spitzer Space Telescope Space Telescope is 30 January 2020."]
[6.1490092277526855, 0.9890682697296143, "The Mission Status of the RAVAN CubeSat is Still operating."]
[5.009930610656738, -0.14968697726726532, "The Partial Service Launch Timeline of the OneWeb Satellite Constellation is Next 60-90 days."]
[8.639650344848633, 4.990040302276611, "The Separation Method of the ASTRO and NextSat Satellites is ASTRO's robotic arm."]
[10.019187927246094, 1.4461357593536377, "The Period of the CBERS-2B Satellite is 100.26 minutes."]
[4.337026596069336, 4.542159080505371, "The Main Communication Bus of the CSI Data Communication is CAN (Controller Area Network)."]
[9.432920455932617, -0.5878199934959412, "The Resonance Survey Requirement of the SERB Nanosatellite Satellite is First resonant frequency > 90 Hz."]
[9.058982849121094, 5.245985984802246, "The Issue of the Attitude Control System Satellite System is Eclipse attitude control not achieved."]
[8.166337966918945, 9.260711669921875, "The Removability of the Optical Filters SWIR Instrument Component is Required."]
[8.265046119689941, 9.185880661010742, "The Spatial Resolution of the OLI-2 Sensor is 15 m."]
[9.445389747619629, 2.4692676067352295, "The Mission Duration of the EURECA Satellite is 336 days."]
[5.80108642578125, 6.3305559158325195, "The Radar Reflector Antenna Boom Length of the NISAR Satellite is 30 feet (9 meters)."]
[9.552724838256836, 0.5569368600845337, "The Mission Design Life of the DSP satellites Satellite is >18 months for the near-equatorial S/C, and >12 months for the polar S/C."]
[7.893923282623291, 4.900047779083252, "The Multitemporal Registration of the VSSC Satellite is Better than 3 m."]
[6.922656059265137, 4.6190714836120605, "The Focus of the RECCAP-2 Satellite Mission is Reconcile and constrain the global GHGs budget with the aggregation of regional budgets."]
[9.981553077697754, 3.1997122764587402, "The Altitude of the GPS Signal Environment Mapping is Up to geosynchronous orbit (35,900 km)."]
[6.3026652336120605, 9.348955154418945, "The Volume of the PHM Instrument is 28 liters."]
[7.208180904388428, 4.12802267074585, "The Potential Evaluation of the Indian Remote Sensing Satellite Satellite is \"Potential of High-resolution Indian Remote Sensing Satellite Imagery for Large Scale Mapping\"."]
[6.95821475982666, 4.435014247894287, "The Measurement Category of the SARAL Satellite is Atmospheric Humidity Fields, Ocean topography/currents, Ocean surface winds, Ocean wave height and spectrum."]
[8.841548919677734, 10.236414909362793, "The Sensor Technology of the C3D Instrument CMOS Sensor is 0.18 \u00b5m CMOS technology."]
[4.995899200439453, 5.912310600280762, "The Bands of the CubeRRT Satellite is Tuned over 10 different bands commonly used for Earth observing microwave radiometers."]
[7.23898458480835, 7.112111568450928, "The Measurement Start Date of the SOVAP Instrument is 21/7/2010."]
[7.572740077972412, 5.309240818023682, "The Observation Modes of the OCO-2 Satellite is Nadir, Glint, Target."]
[3.82458758354187, 0.2867353558540344, "The DOI of the Gravity Recovery and Interior Laboratory (GRAIL) Mission is 10.1126/science.1231507."]
[9.312149047851562, 7.4645280838012695, "The Testing Temperature of the Faraday Cup Sensor is Exceeding 1650 \u00baC."]
[7.5195136070251465, 0.9185675978660583, "The Launch Date of the Polar Scout Satellite is 3 December 2018."]
[9.01746940612793, 7.10453987121582, "The Quantity of the Sun Sensor Suites Sensor is 4."]
[7.817744731903076, 1.109622597694397, "The Image Capture Date of the Sentinel-2 Satellite is 25 January 2022."]
[1.239306926727295, 4.1728010177612305, "The Battery Type of the Spacecraft Satellite is Li-ion."]
[6.830275535583496, 1.2366060018539429, "The Restructured Program Date of the NPOESS Satellite System is Nov. 2006."]
[3.184765100479126, 6.813843250274658, "The RF Output Power of the S-band transmitter Transmitter is Adjustable from 27 to 33 dBm."]
[6.821876049041748, 5.476812839508057, "The Purpose of the SMAP Satellite is Measuring the water content of soils."]
[2.13423490524292, 4.607966899871826, "The Power Consumption of the Nexus Electrical Power Subsystem is 1 watt."]
[7.711973667144775, 7.393951892852783, "The Purpose of the RISE Instrument is Deduce the size and density of the martian core."]
[9.098979949951172, 4.125405788421631, "The Size of the BRITE-Austria Satellite is 20 cm x 20 cm x 20 cm."]
[8.744523048400879, 10.657323837280273, "The Large Window Time Resolution of the CCD Image Sensor is 0.6 seconds."]
[7.000206470489502, 4.966245651245117, "The Greening of the Northern Forests Ecosystem is Rare benevolent effects of our warming climate."]
[7.778790473937988, 2.828087568283081, "The Launch Time of the CartoSat-2D Satellite is 3:58 UTC."]
[7.859210014343262, -0.09231910109519958, "The Launch Date of the Nauka Module is July 21."]
[5.499075889587402, 4.689664363861084, "The Spatial Acquisition Duration of the Alphasat TDP1 GEO-relay is Achieved in no more than 80 s."]
[5.718469142913818, 3.84580659866333, "The Location of the PDCC Control Center is ESA/ESRIN, in Frascati, Italy."]
[5.416043758392334, 2.7568728923797607, "The Manufacturer of the PolyITAN-1 CubeSat is KPI (Kiev Polytechnic Institute)."]
[6.614727020263672, 10.693451881408691, "The Nominal SNR of the Band 6 Spectral Band is 870."]
[9.69333553314209, 4.2756524085998535, "The Model Scale of the Juice Spacecraft is 1:18."]
[9.945398330688477, 6.709345817565918, "The Telecom, Landing Site Tilt Accommodation, Flight Hardware Thermal Safety of the Mission Requirements Satellite is Identified and Analyzed."]
[9.10348892211914, 9.278017044067383, "The FOV of the HIRES Instrument is 0.3\u00ba x 0.4\u00ba."]
[7.7711100578308105, 8.469295501708984, "The Solar Spectral Irradiance Measurement Range of the SOLSPEC Spectrometer is 200 to 2400 nm."]
[5.397082328796387, 4.172105312347412, "The Location of the TAFF Software Package is OBC of the TDX spacecraft."]
[7.838519096374512, 10.019886016845703, "The FOV for VNIR-NP pushbroom scanning of the VNIR-NP Imager is 70\u00ba."]
[6.190907955169678, 5.1375017166137695, "The | of the Upper Atmospheric Research Radar Facility Radar Facility is National Science Foundation Awards a Grant to SRI International for Upper Atmospheric Research Radar Facility."]
[8.612045288085938, 10.528426170349121, "The Exposure Levels of the CCD Detector Imaging Device is Six non-zero levels."]
[6.802675724029541, 1.3551409244537354, "The Conference Presentation Date of the STSat-2 Satellite is Aug. 11-14, 2003."]
[11.509520530700684, -1.2420763969421387, "The Mass of the Tyvak-0171 Satellite is 138 kg."]
[9.65612506866455, 1.4537211656570435, "The Potential Loss Time of the NextSat Satellite is First day of the mission."]
[8.970786094665527, 8.437644958496094, "The Rotation of the Scanning Platform Platform is Continuous."]
[1.8928921222686768, 3.961530923843384, "The Quantity of the CSS Solar Cells is 6."]
[8.034223556518555, -0.12293484061956406, "The Docking of the Pirs ISS Module is Autonomously docked to the Zvezda service module\u2019s nadir."]
[10.968633651733398, 7.177361011505127, "The Coded Masks Distance of the JEM-X X-Ray Monitor is 3.2 m."]
[10.641927719116211, -1.6909263134002686, "The Cargo Capacity of the HTV-8 Spacecraft is Up to six tons."]
[8.227849960327148, 4.578935623168945, "The Swath Width of the SLIM6 Satellite is 600 km."]
[13.110199928283691, 4.0603928565979, "The Monitoring Frequency of the Gaia Space Astrometric Mission is About 70 times."]
[6.141380786895752, 0.5291527509689331, "The Launch Time of the COPPER CubeSat Satellite is 01:15:00."]
[12.981836318969727, 4.147748947143555, "The Number of Stars with Parallax and Proper Motion of the Gaia EDR3 Satellite Data is Almost 1.5 billion."]
[8.644676208496094, 10.78769588470459, "The Intensity Variation of the STL-11000M SBIG Camera CCD Camera is Approximately 6%."]
[8.558736801147461, 10.427127838134766, "The Sensitivity of the Detector E2V CCD-22 (Frame Store) is 10 \u00b5Crab or better."]
[7.582536697387695, 8.549485206604004, "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.."]
[7.412801265716553, 0.7261504530906677, "The End of Mission of the PROBA-V Satellite is April 20, 2020."]
[8.827936172485352, 1.3672206401824951, "The Mission Start Date of the Van Allen Probes Satellite is 2012."]
[5.953024387359619, 3.830463171005249, "The Operator of the Bartolomeo Platform is Airbus DS."]
[7.727680683135986, 13.574874877929688, "The Resolution \u0394\u03bb (0.10\u00ba slit) of the SPIM4 Spectrometer is 2.8 nm."]
[6.003593444824219, 6.389267444610596, "The Noise Equivalent \u03c30 of the Instrument SAR is \u2264 \u201327 dB."]
[8.147745132446289, 0.696609616279602, "The Close Call Classification of the Starliner Spacecraft is High-visibility close call."]
[6.787287712097168, 1.1688085794448853, "The Launch Date of the GIOVE-B Satellite is October 13, 2008."]
[9.404675483703613, 8.041345596313477, "The Temperature of the CCDs Detector is -22\u00baC."]
[4.015708923339844, 6.669259548187256, "The Downlink Frequency of the Myriad RF board RF Board is 300 MHz up to 3.8 GHz."]
[3.672030448913574, 6.362275123596191, "The Real-time Downlink Speed of the RF Communications Communication System is 150 Mbit/s."]
[12.110136985778809, 3.2716054916381836, "The Inclination of the SkySat-16 to -18 Satellite is ~98\u00ba."]
[9.104718208312988, 10.58530044555664, "The Purpose of the VWFC Camera is Take wide-angle ultraviolet-light photographs of vast regions of sky not observable from Earth."]
[10.19990348815918, 5.089161396026611, "The Thrust of the Thrusters Attitude Control is 10 N."]
[5.07125186920166, 2.6075148582458496, "The Quantity of the IOV Units Satellite Payload is 10."]
[7.590799808502197, 8.16622257232666, "The Altitude of the AMSR-E Instrument is 705 km."]
[5.994718551635742, 6.068292617797852, "The Surface Movement Detection of the NISAR Satellite is As small as 0.4 inches (1 cm)."]
[1.0956640243530273, 4.277979850769043, "The Battery Type of the EPS Electrical Power Subsystem is Rechargeable lithium ion 18650."]
[9.97022819519043, 1.5463787317276, "The Period of the IRS-1B Satellite is 103.2 minutes."]
[8.288990020751953, 7.827395915985107, "The Science Team Lead of the MIRI Instrument is George Rieke with the University of Arizona."]
[6.255445957183838, 4.452882766723633, "The Instruments of the NPOESS-C1 Mission is CERES and TSIS."]
[5.784154415130615, 7.438666820526123, "The Beam Width of the RA-1 Instrument is 1.3\u00ba."]
[10.300496101379395, 4.972768783569336, "The Thrust of the Thrusters Satellite Component is ~10 \u00b5N."]
[9.50665283203125, 2.683584213256836, "The Design of the SMP Sampler Mechanism is Small projectile to be shot as soon as the tip of a cylinder-shaped horn touches the asteroid surface."]
[7.567698955535889, 2.6362431049346924, "The Launch Date of the KOMPSat-5 Satellite is August 22, 2013."]
[9.439737319946289, 0.5859993100166321, "The Expected Lifetime of the TSX Satellite is Several more years."]
[8.344559669494629, 8.532939910888672, "The Publication Date of the Solar XUV grazing incidence spectrograph Spectrograph is April 1977."]
[9.333183288574219, 5.088145732879639, "The Reaction Wheel Test of the SONATE CubeSat Satellite is Successful."]
[8.02556037902832, 2.880993366241455, "The Mission Cost Cap of the IMAP Interstellar Mapping and Acceleration Probe is $492 million."]
[9.418749809265137, 7.287989139556885, "The Energy Range of the FSU Solar Wind Faraday Cup is Modulator sized to withstand 8 kV."]
[11.966085433959961, 3.3962838649749756, "The Inclination of the BUV Sensor is 80.1\u00ba."]
[6.3310699462890625, 11.888519287109375, "The Absolute / Relative Misalignment of the Three-axis diagonal gradiometer Gradiometer is 10 -3  rad / 10 -5  rad."]
[6.984724998474121, 0.6357176303863525, "The Launch Date of the FormoSat-1 Satellite is January 26, 1999."]
[6.518514156341553, 6.247395992279053, "The RFU of the ASCAT Scatterometer is Radio Frequency Unit."]
[11.723166465759277, 4.590965747833252, "The Mass of the Infinity-shaped loop Gas and Dust Formation is 30 million solar masses."]
[4.540057182312012, 3.690142869949341, "The Purpose of the AIS Automatic Identification System is Broadcasts a ship's identification, position and other maritime navigational data."]
[1.4262388944625854, 4.368159294128418, "The Modularity of the BCR Battery Charge Regulator is Can be combined in parallel."]
[6.35693883895874, 1.6231051683425903, "The Launch Date of the Jason-3 Satellite is March 16, 2016."]
[5.294373989105225, 4.103868007659912, "The Installation Location of the Data Storage System Satellite Component is Coud\u00e9 laboratory of the OGS."]
[7.55122709274292, 2.994537830352783, "The Observation Capability of the KOMPSAT-5 Satellite is Left or right-looking."]
[7.026083469390869, 2.5922749042510986, "The URL of the Sentinel-5 Satellite is http://www.space-airbusds.com/media/document/10607tl-sentinel-5-lr.pdf."]
[6.104462623596191, 1.8309202194213867, "The Launch Vehicle of the OCO-2 Spacecraft is Delta-2 7320-10C."]
[4.732004642486572, 3.93021821975708, "The Function of the Node-3 Module is Provides a pressurized passageway between berthed habitable volumes."]
[7.727015972137451, 13.57845687866211, "The Resolution \u0394\u03bb (0.10\u00ba slit) of the SPIM1 Spectrometer is 0.8 nm."]
[5.844916820526123, 5.524320125579834, "The Data Quality of the TriG receiver GNSS Receiver is Increased."]
[11.667076110839844, 3.353090524673462, "The Angular Speed of the Polar Scout Satellite is Higher at high elevation angles."]
[5.224592685699463, 3.556567430496216, "The Connector Type of the Satellite Satellite is 51-pin connector."]
[6.705347061157227, 7.189462661743164, "The Data Gathering Start Date of the GEDI Lidar is 1 February 2019."]
[6.342562198638916, 10.093912124633789, "The Mass of the LISS-3 Camera is 106.1 kg."]
[5.005383014678955, -0.14957799017429352, "The Collision Risk CONOPS Presentation of the OneWeb Satellite Constellation is Mike Lindsay, \u201dOneWeb Collision Risk CONOPS,\u201d SSA Operators' Workshop, Denver, Colorado, Nov. 3-5, 2016."]
[4.568772315979004, 4.71634578704834, "The Function of the DPE Data Processor Element is Ingests mission data, ancillary data, and auxiliary data to produce NPOESS data products."]
[7.313484191894531, 2.672642230987549, "The Purpose of the Orion spacecraft Spacecraft is Return astronauts to the Moon and eventually take the first humans to Mars."]
[8.438888549804688, 7.75467586517334, "The | of the COTS EEE components Radiation Test is Application specific radiation tests for COTS EEE components."]
[9.754538536071777, 8.095050811767578, "The Expected GRB Detections per Year of the GMOD Detector is Approximately 20."]
[7.220235347747803, 0.4222780466079712, "The Launch Date of the ALOS-3 Satellite is 7 March 2023."]
[9.482397079467773, 7.346488952636719, "The Principal Investigator of the Heat Probe Instrument is Tilman Spohn."]
[11.012871742248535, 3.424406051635742, "The Landing Site of the Rosetta Spacecraft is Comet 67P/Churyumov\u2013Gerasimenko."]
[11.494099617004395, -1.2701876163482666, "The Weight of the SPOT-2 Satellite is 1800 kg."]
[11.797979354858398, 4.678382873535156, "The Star Formation Rate of the M83 Galaxy is A handful of new stars being born every year."]
[7.918182373046875, 4.062254905700684, "The Imaging Capability of the Terra Bella Satellite Constellation is Sub-meter color imagery and up to 90-second clips of HD video with 30 frames/s."]
[5.868983745574951, 3.926337242126465, "The Ground Segment Software of the GeoSat-2 Satellite is gs4EO."]
[11.34747314453125, 6.743587493896484, "The Quantity of Telescopes of the Imaging X-ray Polarimetry Explorer (IXPE) Space Telescope is 3."]
[6.811196327209473, 1.7764341831207275, "The Conference Presentation Date of the UK Disaster Monitoring Constellation Satellite Satellite is September 2002."]
[3.4309775829315186, 4.590420246124268, "The Quantity of the Virtex-4 FPGA Data Processing Unit is 2."]
[11.754034042358398, 4.605299949645996, "The Star Formation of the The Horse and the Dragon Pair of distinct massive galaxies is Teeming with star formation, 10 to 100 times more massive than most galaxies at the same epoch."]
[6.4227728843688965, 2.707364797592163, "The Mean Sea Level Rise Measurement of the Jason-3 Satellite is About 3mm per year."]
[4.947334289550781, -0.10373015701770782, "The Date of the OneWeb Partnership is 2 November 2021."]
[3.2085347175598145, 5.879860877990723, "The Data Retrieval Time of the DMSP and POES systems Data Retrieval Systems is About two hours."]
[8.18324089050293, 8.561566352844238, "The Technology of the SHIMMER Spectroscopy Instrument is SHS (Spatial Heterodyne Spectroscopy)."]
[4.559177398681641, 3.132355213165283, "The Microcontroller of the SCARAB 1U CubeSat bus is PIC24-based CubeSat Kit."]
[5.4784674644470215, 2.593130350112915, "The Command and Data Path of the Iridium NEXT Satellite is MPLS cloud."]
[2.2646524906158447, 5.078650951385498, "The Maximal Power Consumption of the PPU System is 22 W."]
[7.962783336639404, 9.21880054473877, "The Spectral Band of the Instrument Spectrometer is SWIR."]
[5.464455604553223, 5.004066467285156, "The Design Basis of the NRD Navigation Radar Detector is Experimental terrestrial navigation radar detector systems developed by FFI."]
[10.574033737182617, 7.502742290496826, "The Structure Material of the IRS-1A Satellite is Aluminum/aluminum honeycomb."]
[8.3316011428833, 1.5567480325698853, "The International Astronautical Congress Date of the BepiColombo Mercury Probe is Sept. 29-Oct. 3, 2014."]
[7.388154983520508, -0.26175031065940857, "The Undock Date of the H-II Transfer Vehicle \"KOUNOTORI3\" (HTV3) Cargo Craft is Sept. 17, 2012."]
[6.9351019859313965, 8.118658065795898, "The Global Coverage Time of the MSR Radiometer is 5 days."]
[10.25230884552002, 5.0013837814331055, "The Propellant of the HEMPT Thruster Assembly Electric Propulsion Thruster is Xenon."]
[4.9335737228393555, 4.7634992599487305, "The Uplink Verification Method of the Ground System Satellite Ground System is Transmitting signals in a safe direction while verifying their emissions from the antenna with an on-site technician and a hand-held spectrum analyzer."]
[6.0618672370910645, 9.19081974029541, "The Mass of the RMU Radiometer Microwave Unit is 1.6 kg."]
[7.325577259063721, 0.12767860293388367, "The Launch Date of the HYLAS-2 Communication Satellite is August 2, 2012."]
[5.052918910980225, 8.701812744140625, "The Position Accuracy (RMS orbit) of the S-1 NRT Product is < 10 cm (2D)."]
[6.121722221374512, 4.166748046875, "The Requirement of the RCM Satellite is High-volume automated information processing capacity at the users\u2019 premises."]
[4.692531585693359, 1.773976445198059, "The Number of Satellites of the First Batch of Satellites Satellite is 1600."]
[9.021610260009766, 9.319245338439941, "The FOV of the MSU-E Multispectral Scanner is 2.5\u00ba."]
[7.483880996704102, 10.007818222045898, "The Number of Spectral Bands of the Instrument Hyperspectral Imager is Up to 200."]
[10.428729057312012, 3.565868616104126, "The Light Levels of the Rosetta Spacecraft is 4% of those on Earth."]
[9.273097038269043, 6.405008316040039, "The Quantity of the Star Trackers Attitude Sensing is 2."]
[10.46863079071045, 6.025263786315918, "The Testing Environments of the Bricks Building Material is Microgravity, 1 g, less than 1 g."]
[6.855129718780518, 3.585861921310425, "The Autonomous Functionality of the INTEGRAL Satellite is Yes."]
[7.7852654457092285, 0.41558799147605896, "The Safe Mode Entry Date of the Chandra Satellite is 12 October 2018."]
[7.926082611083984, 0.2589356303215027, "The Release Date of the Zaatari Refugee Camp, Jordan Location is May 23, 2014."]
[5.920268535614014, 6.616781711578369, "The Application of the Mie Scattering Theory Theory is Estimation of specific attenuation and radar reflectivity for Ku-band."]
[7.27962589263916, 0.4973297119140625, "The Launch Date of the Hinode Satellite is Sept. 23, 2006."]
[5.135109901428223, 4.978776454925537, "The Controller Type of the Knudsen Station Ground Station is Green Heron RT-21 Az-El controller."]
[8.178323745727539, 9.412906646728516, "The IFOV of the SiPD Detector is 0.45 - 0.52 \u00b5rad."]
[8.569140434265137, 6.822149753570557, "The Dynamic Range of the NewMag Magnetometer is \u00b165536 nT."]
[12.00072193145752, 3.402264356613159, "The Inclination of the LAGEOS Satellite is 109.84\u00ba."]
[8.02816390991211, 7.639384746551514, "The Data Frequency of the FGS Sensor is 1 Hz."]
[11.125767707824707, -1.4801384210586548, "The Mass of the Dove Satellites CubeSats is 4.7 kg each."]
[7.765713214874268, 7.69369649887085, "The Field of View Map of the EPI-Lo Instrument is Unknown."]
[7.592803001403809, 1.223724603652954, "The Date of the Bistatic Radar Experiment Experiment is April 9-10, 1994."]
[7.241779327392578, 0.1442400962114334, "The Launch Year of the HJ-1C Satellite is 2012."]
[11.696573257446289, 1.2228162288665771, "The Operation Status of the China's Lunar Lander Lander is Spotted."]
[3.820068120956421, 6.202853679656982, "The Downlink Data Rate of the X-band phased array antenna Antenna is 105 Mbit/s."]
[8.493273735046387, 8.098835945129395, "The Number of Exposures of the Exposures Data Collection is 3."]
[7.953190803527832, 5.886000633239746, "The Jitter Values of the ASTERIA Satellite is 1\u03c3 ~5\"."]
[8.469229698181152, 8.734914779663086, "The Grating Type of the Offner-type spectrometer Spectrometer is Mechanically ruled."]
[6.968571186065674, 8.123028755187988, "The Period of Orbit of the ICIR Radiometer is Approximately 1.55 hours."]
[4.916067123413086, 4.8048624992370605, "The Function of the MOT Communication System is 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."]
[8.062287330627441, 3.9648349285125732, "The Calibration Methods of the Pleiades Program Satellite Program is Unknown."]
[4.071169376373291, 5.7501749992370605, "The S-band 1Mbit/s Downlink Data Rate Range of the UoSAT-12 Satellite is 1 Mbit/s - 64 kbit/s."]
[3.813786745071411, 4.450960636138916, "The Industrial grade embedded computers of the Frame Grabber Type is Industrial grade embedded computers were selected for this application."]
[8.280326843261719, 3.2134714126586914, "The Propulsion System of the TanDEM-X Satellite is Cold gas propulsion system."]
[9.430278778076172, 0.945103645324707, "The Test Duration of the D-Orbit Company is Four months."]
[6.005443572998047, 9.504488945007324, "The Mass of the FSS Instrument is 87.5 g."]
[6.050145149230957, -0.008868537843227386, "The Operations Start of the Galileo Second Generation (G2) Satellite Constellation is Later in this decade."]
[8.784387588500977, 8.217692375183105, "The Views of the Calibration Mirror TIR Subsystem Component is Cold space, \"warm\" blackbody."]
[1.9133687019348145, 3.898872137069702, "The Solar Cells Type of the Power Subsystem Satellite is Triple-junction."]
[4.834908485412598, 3.7726938724517822, "The Power, Thermal, Propulsion, Mechanisms of the Bus Satellite Bus is Nominal."]
[9.43200397491455, 0.7463192343711853, "The Lifespan of the Sentinel-2 Satellite is 7 years."]
[10.332616806030273, 4.958096504211426, "The Impulse Density of the Thruster Propulsion System is High."]
[7.270362854003906, 9.070236206054688, "The Spatial Resolution (Band 1) of the PanMUX Instrument is 5 m."]
[5.697207450866699, 2.842994451522827, "The Satellite Network Provider of the Kongsberg Satellite Services Company is True."]
[6.489674091339111, 4.641864776611328, "The Models of the FengYun LEO satellites Satellite is FY-3A/B, FY-3C/D/E/F."]
[9.552947044372559, 1.033928632736206, "The Mission Duration of the WIND Satellite is Almost two complete solar cycles."]
[8.545465469360352, 5.73546028137207, "The Density of the Proton Component Measurement Accuracy of the DSCOVR Satellite is 20%."]
[6.633913040161133, 9.621992111206055, "The Estimated Mass of the Subarray Array is 80 gram."]
[11.173774719238281, -1.5329439640045166, "The Mass of the COPPER CubeSat is 1.3 kg."]
[3.2582666873931885, 5.6407599449157715, "The Checksum Size of the Processed Science Data Packet Data Packet is 1 byte."]
[9.421826362609863, 0.34511780738830566, "The Exceeded Design Life of the Aqua Satellite is Yes."]
[9.060617446899414, 3.589963912963867, "The Orbit Position of the BeiDou-1A Satellite is GEO, 140\u00ba E."]
[7.086960315704346, 0.5561406016349792, "The Launch Date of the SuperView-1 Observation Satellites is 9 Jan. 2018."]
[9.429239273071289, -0.76663738489151, "The Launch Date of the IDEA-OSG 1 Microsatellite is 28 Nov. 2017."]
[7.039323329925537, 0.8186779618263245, "The Development Date of the Embedded Systems Satellite Component is 2010."]
[13.809603691101074, 0.7659677267074585, "The Orbital Slot of the GSAT-0205 Satellite is A08."]
[8.413729667663574, 7.864213943481445, "The Field of View of the FGS Fine Guidance System is \u00b13 arcmin."]
[5.867545127868652, 6.90319299697876, "The Pulse Length of the Radar Instrument is 15 \u00b5s."]
[10.83115291595459, 3.3795013427734375, "The Line-of-Sight Distance to Mars of the ExoMars TGO Trace Gas Orbiter is 41 million km."]
[8.937376022338867, 4.470248222351074, "The Structure of the CXBN-2 Spacecraft is Robust 2-wall structure matched to a central mounting block."]
[5.442253112792969, 3.1804428100585938, "The Interconnection of the Heinrich Hertz Satellite Technology is Direct single-hop."]
[11.268954277038574, 2.9068689346313477, "The Location of the Cendrillon Crater is Eastern Hemisphere near the meridian."]
[6.806422710418701, 0.36582791805267334, "The Launch Date of the OFEQ-3 Satellite is April 15, 1995."]
[7.29444694519043, 3.7570457458496094, "The Unknown of the PROBA-2 Satellite is Unknown."]
[6.17518949508667, 2.123394727706909, "The Conference Presentation of the TacSat-4 Satellite is Space, Propulsion and Energy Sciences International Forum (SPESIF 2009)."]
[5.618616580963135, 2.3211638927459717, "The Average Daily Observations of the SBSS Satellite System is 15,000."]
[9.773935317993164, 8.662501335144043, "The Model of the UVIT Telescope Assembly is Engineering model."]
[6.995122909545898, 8.267648696899414, "The Repeatability of the MWI Instrument Scan Mechanism Assembly is Unknown."]
[7.542520999908447, 5.214275360107422, "The Scientific Instruments of the Trace Gas Orbiter Satellite is High-resolution color imaging system, High-resolution neutron detector, Two spectrometer suites."]
[7.7349443435668945, 1.4397096633911133, "The Storm System Analysis Date of the NASA Organization is March 7, 2016."]
[11.647734642028809, 6.127716541290283, "The Propellant Consumption Rate of the XMM-Newton Satellite is Approximately 6 kg per year."]
[6.654015064239502, 3.182443618774414, "The Mission Status of the Myriade/AstroSat-100 Satellite is Operational (extended)."]
[10.039422035217285, 5.011609077453613, "The Activation of the He-repressurization system Propulsion Subsystem is Shortly after the LOI maneuver is completed."]
[4.696547985076904, 1.6304177045822144, "The Number of Spare Satellites of the Galileo Constellation Satellite Constellation is 6."]
[11.708720207214355, 4.567421913146973, "The Red Giant Oscillations of the HD 181068 Star System is Not detected."]
[10.215688705444336, 6.739090442657471, "The Orbit Control and Maintenance of the Spacecraft Satellite is TCS (Thermal Control Subsystem)."]
[8.358720779418945, 10.085735321044922, "The Central Wavelength of the Current GOES imager Sensor is 6.95."]
[4.698896408081055, 5.395572662353516, "The Measurement of the Ka-band ground station Ground Station is High data rate by SNR (Signal-to-Noise) measurement."]
[5.806280136108398, 6.341551303863525, "The Radar Reflector Antenna Diameter of the NISAR Satellite is 40 feet (12 meters)."]
[9.26567268371582, 4.1235175132751465, "The Size of the Spacecraft Satellite is 2.6 m x 1.8 m x 2.8 m."]
[11.682687759399414, 2.6021220684051514, "The Diameter of the [65803] Didymos Asteroid is ~160 m."]
[5.404575347900391, 0.2867257595062256, "The Containment of the Calf Canyon-Hermits Peak fire Fire is 29 percent."]
[6.430567264556885, 3.397782802581787, "The Project Management of the TRISHNA Satellite is Joint Indian-French project team."]
[7.956241607666016, 7.048480033874512, "The Experimental Area of the ARC Calibration System is Can be changed."]
[7.254673480987549, -0.10052095353603363, "The Launch Date of the H-IIB Launch Vehicle No. 3 Launch Vehicle is July 21, 2012."]
[7.820840358734131, 0.0800783559679985, "The Date of the OA-7 Space Station Cargo Resupply Mission is April 18, 2017."]
[3.499668836593628, 4.430656909942627, "The Function of the \u00b5C Control Unit is Regulates the direct current power supply of the pump."]
[8.154203414916992, 7.733942031860352, "The Magnetic Footprint Displacement of the MGF Instrument is Up to 5 km for every 100 km of altitude."]
[9.034322738647461, 10.740180969238281, "The Calibration Cycle of the LISS-3 camera Camera is 2048 scan lines."]
[9.268969535827637, 7.900096893310547, "The Temperature Stability of the Filter Wheel Optics Subsystem is \u00b11 K."]
[7.99635124206543, 3.0364091396331787, "The Flux of the Small Near-Earth Objects Space Debris is Unknown."]
[4.372745513916016, 3.89339280128479, "The Operation of the Automated Beacon Network Anomaly Detection System is Forwards the message to a central monitoring workstation."]
[11.42742919921875, 4.292449951171875, "The Composition of the Cloud of gas and dust Protoplanetary Nebula is Mostly hydrogen and helium, with a small amount of heavier elements such as carbon, nitrogen, oxygen and iron."]
[10.301494598388672, 2.9633736610412598, "The Perigee Altitude of the Satellite Orbit Orbit is Above 7.3 RE."]
[9.876474380493164, 1.5878089666366577, "The Operator of the TIMED Satellite is Johns Hopkins University Applied Physics Laboratory (JHU/APL)."]
[3.7190494537353516, 4.601424694061279, "The Processor of the Spacecraft Satellite is Mongoose V processor."]
[6.011796474456787, 8.872675895690918, "The Power Consumption of the MWR Dicke Radiometer is 96 W."]
[7.7004876136779785, 4.3899736404418945, "The Image Acquisition of the ALOS-3 Satellite is Satellite body-pointing."]
[7.226975917816162, 5.604856014251709, "The Data of the Aeolus Satellite is Profiles of Earth's wind on a global scale."]
[5.266497611999512, 5.884342670440674, "The Antenna Type of the AISSat-1 Satellite is VHF monopole payload antenna."]
[4.617255687713623, 6.017052173614502, "The Bandwidth of the Satellite Device Unknown is 1500 MHz."]
[7.0917792320251465, 6.122182846069336, "The Application of the OLCI Instrument is Supporting global land and ocean monitoring services."]
[5.116825103759766, 1.9024637937545776, "The Organizational Interfaces of the MSX Flight Operations Team Team is Figure 38."]
[11.554887771606445, 2.059783935546875, "The Function of the MASCOT Science Landing Package is Augment the science capabilities of the Hayabusa-2 mission."]
[5.222403049468994, 4.668837547302246, "The Main Node Location of the Ground System Ground System is IKI of Moscow."]
[7.049647331237793, 4.126954078674316, "The Orbit Analysis and Control of the Sentinel-1 Satellite is Unknown."]
[9.276171684265137, 10.357375144958496, "The Number of BW Photographs of the Metric Camera Camera is 473."]
[11.622482299804688, 6.181251049041748, "The Response Time of the XMM-Newton Observatory is A few hours later."]
[12.171154975891113, 3.3951871395111084, "The Orbit Inclination of the IRIS Spacecraft is 97.9\u00ba."]
[8.571161270141602, 8.816258430480957, "The Central Output Angle of the Short Wavelength Band Spectrometer is -5.28\u00ba."]
[4.172482967376709, 3.7245163917541504, "The Global Average Detection Rate of the Complex Receiver AIS Receiver is 6 Messages/s."]
[10.002703666687012, 1.446085810661316, "The Period of the COMPASS-2 Satellite is 93.5 minutes."]
[10.395051002502441, 3.7114083766937256, "The Differential Velocity of the LARES Satellite is 0.75 \u00b1 20% m/s."]
[9.408164024353027, 7.346890926361084, "The AC Current of the FSU Faraday Cup Sensor Unit is Produced on the collector plates."]
[7.482852935791016, 8.593613624572754, "The Spectral range of the IRAS Infrared Atmospheric Sounder is 0.69-15.5 \u00b5m."]
[6.275864124298096, 2.2436583042144775, "The Partners of the Jason-2 Satellite is NASA, CNES, NOAA, EUMETSAT."]
[12.172453880310059, 3.2283849716186523, "The Inclination of the NigeriaSat-2 Satellite is 98.24\u00ba."]
[9.656156539916992, 7.724380970001221, "The Electron Energy Range of the REPT Instrument is 1.6 to 18.9 MeV."]
[10.37192440032959, 1.2850943803787231, "The LTAN of the GCOM-W1 Satellite is 13:30 hours."]
[7.572474002838135, 8.723847389221191, "The Dynamic Range of the Instrument Spectrometer is Saturated at \u226570% albedo."]
[6.027670383453369, 4.111423015594482, "The Mission Control Center Location of the Odin Satellite is Solna, Sweden."]
[6.757102012634277, 0.7448323965072632, "The Image Capture Date of the NigeriaSat-2 Satellite is 8 days after launch."]
[8.411477088928223, 3.4127039909362793, "The Horizontal Baseline of the TanDEM-X Satellite is 200 m to 3000 m."]
[7.272023677825928, 0.5763541460037231, "The Deployment Date of the SOAR Satellite is 14 June 2021."]
[9.260679244995117, 1.291466236114502, "The NRT Data Freshness of the Sentinel-6 Satellite is Not older than 3 hours."]
[6.252318859100342, 3.077760696411133, "The Managed By of the TEMPEST-D Satellite is NASA/JPL."]
[8.495022773742676, 5.997358322143555, "The Prediction of the Magnetic Field Models Geophysical Models is Pole will continue to drift towards Siberia."]
[3.6052167415618896, 3.505410671234131, "The Number of Cicero Satellites of the GeoOptics Satellite Manufacturer is At least two."]
[4.830121994018555, 1.9043587446212769, "The Number of Satellites of the HY-2 Satellite is 8."]
[2.5119690895080566, 6.004037857055664, "The Power On of the Smartphone Device is 45 minutes after deployment."]
[6.910335063934326, 3.621974229812622, "The INR Performance of the GOES-N spacecraft Satellite is Improved."]
[6.842014312744141, 7.545281887054443, "The Function of the LRA Instrument is Acts as a reference target for laser tracking measurements."]
[4.896886825561523, 2.0014233589172363, "The Number of Payloads of the Spaceflight SSO-A: SmallSat Express Satellite is 64."]
[4.077297210693359, 3.160921335220337, "The Hardware Platforms of the Open5GCore Rel. 4 5G Core Network is Common hardware platforms."]
[5.30389928817749, 2.3775155544281006, "The Design and Build Contributors of the SAPPHIRE Satellite is Students at Stanford University."]
[7.572539329528809, 2.192765951156616, "The Launch Status of the Al Amal Mars Probe is Launched."]
[8.597140312194824, 6.848307132720947, "The Readings of the Magnetometer Sensor is Unknown."]
[10.635051727294922, 3.6441707611083984, "The Speed of the Rosetta Spacecraft is 31 000 km/h."]
[5.93794584274292, 1.1044707298278809, "The Commercial Availability of the Iridium Certus Satellite Communication Service is Mid-2018."]
[8.91895866394043, 2.4806900024414062, "The Observation Capabilities of the Herschel Space Observatory is Far-infrared imaging."]
[9.336199760437012, 7.904082298278809, "The Time to Reach Temperature of the PICNIC IR detector Detector is About nine hours."]
[5.964755535125732, 5.511003017425537, "The Sensitivity of the Phoenix receiver Navigation Device is High levels of radiations."]
[9.86534595489502, 5.5426716804504395, "The Thrust of the ADCS Thrusters Attitude Determination and Control Subsystem is 150 N."]
[5.852490425109863, 2.4613699913024902, "The L1B, L1C and L2A Product Destination of the EnMAP Satellite is Temporary storage on the pick-up points for delivery."]
[3.5482871532440186, 2.2789995670318604, "The Size of the QBus-2 Satellite is 2U."]
[8.595067024230957, 6.98983907699585, "The Range of the MAG Magnetometer is -350 nT to +350 nT."]
[5.2676167488098145, 6.334708213806152, "The Deployment Phases of the VDES Antenna Antenna is Two phases of approximately two seconds and 30 seconds duration."]
[7.33684778213501, 5.6141486167907715, "The Vertical Resolution (PBL) of the Aeolus Satellite is 0.5 km."]
[5.1562066078186035, 3.7094085216522217, "The Protocol of the IXV Communications Network Network is IP."]
[17.728221893310547, 7.162813186645508, "The J2000 declination (deg) of the B0531+21 (Crab) Pulsar is 22.01449."]
[7.323896884918213, 0.6109524965286255, "The Camera Installation Date of the OPTSAT 3000 Satellite is Dec. 6, 2012."]
[7.637067794799805, 7.404576301574707, "The Measurement Locations per Day of the OCO-3 Instrument is Up to 40."]
[7.6533355712890625, 0.2719159722328186, "The Article Date of the CXO Satellite is 14 February 2019."]
[5.60398530960083, 3.812769651412964, "The Affected Activities of the CPOM Data Processing Center is Shipping, tourism, Arctic exploration, search and rescue."]
[8.405245780944824, 10.47245979309082, "The CCD Pixel Format of the HIRES Instrument is 384 x 288."]
[12.141968727111816, 3.2662458419799805, "The Inclination of the GRACE Satellite Satellite is 89\u00ba."]
[7.999469757080078, 9.578401565551758, "The Band Spacing of the SWIR Detector is 11.4 nm."]
[9.534096717834473, 0.47960203886032104, "The Design Lifetime of the QuakeSat Satellite is One year."]
[7.1226630210876465, 4.087194442749023, "The Operation with MUIR radar of the Receiver Device is Yes."]
[6.882910251617432, 7.385107517242432, "The Manufacturer of the AATSR Instrument is Astrium Ltd., UK."]
[6.222254753112793, 2.884878158569336, "The Partner Organizations of the OPS-SAT Satellite is BST (Berlin Space Technologies) and MEW Aerospace (Germany), GOMSPACE (Denmark) as well as MAGNA STEYR Engineering and Unitel (Austria)."]
[7.282967567443848, 3.953744411468506, "The Benefits Categories of the Landsat 7 Satellite is Technical, Scientific, Programmatic, Organizational."]
[8.1787691116333, 8.463776588439941, "The Fringe Distortions of the SHS Interferometer is Degrade the instrumental profile and reduce the signal-to-noise ratio."]
[6.360965251922607, 8.3353271484375, "The Filter Wheel Filters of the GOES Sounder Radiometer is 18."]
[1.7818078994750977, 3.9524543285369873, "The Solar cells of the EPS Electric Power Subsystem is 20 x Triple Junction GaAs."]
[6.940804481506348, 1.3170506954193115, "The Publication Date of the GNSS in Space Satellite is Nov/Dec. 2008."]
[4.839544296264648, -3.387660264968872, "The Chair of the George Hurtt Individual is True."]
[5.953986644744873, 3.8705713748931885, "The Mission Service of the Bartolomeo External Payload Hosting Facility is Fast, cost-efficient and reliable access to low Earth orbit."]
[6.766626834869385, 4.249804496765137, "The Mission Objectives of the FSSCat Satellite is Polar Ice and Snow monitoring, soil moisture monitoring, terrain classification and terrain change detection."]
[8.157660484313965, 5.043493747711182, "The Geo-location Accuracy of the SEOSat Satellite is 20 m."]
[6.115816116333008, 3.4017059803009033, "The Satellite Development Locations of the MetOp-SG Satellite Program is Toulouse, France and Friedrichshafen, Germany."]
[4.806526184082031, 0.8451393842697144, "The Cost of the Dellingr Nanosatellite is Fraction of the cost of more traditional satellite missions."]
[6.92361307144165, 0.3188788890838623, "The Launch Date of the OFEQ-2 Satellite is April 1990."]
[11.444731712341309, -1.344651699066162, "The Mass (kg) of the RADARSAT-1 Satellite is 2200."]
[12.03752613067627, 3.2378597259521484, "The Orbit Inclination of the ALOS-3 Satellite is 97.9\u00b0."]
[7.10680627822876, 5.5150532722473145, "The Measurement Proxy of the ClO Chemical Compound is Dynamical effects on the high-latitude upper stratosphere."]
[6.910518646240234, 7.090830326080322, "The Operation Mode of the Radar Instrument is Standby."]
[9.221383094787598, 4.138712406158447, "The Structure Dimensions (Deployed) of the FY-3 series spacecraft Satellite is 4.4 m x 10 m x 3.8 m."]
[5.619665145874023, 7.500423431396484, "The Deployed Configuration Size of the KaRIN Instrument is 5.0 m x 10.6 m x 1.5 m."]
[9.440081596374512, 9.272246360778809, "The Aperture Diameter of the Lenses Optical System is 26 cm."]
[7.467102527618408, 9.056867599487305, "The Wavelength Range of the RAVAN Radiometer is UV (200 nm) to far infrared (200 \u00b5m)."]
[7.250588417053223, 2.4756269454956055, "The Configuration of the RISESat Satellite is Launch and deployed."]
[9.400683403015137, 7.3617939949035645, "The Inventor of the Electron Temperature Probe Instrument is K. Hirao."]
[8.293891906738281, 5.166560649871826, "The Measurement of the Swarm Satellites Satellite is Earth's magnetic field strength and direction."]
[6.153639793395996, 0.5182308554649353, "The Launch Date of the R3 CubeSat Satellite is December 16th, 2018."]
[9.158042907714844, 4.209470748901367, "The Dimensions of the COVE Board Data Transfer Device is 90 mm x 90 mm."]
[9.596689224243164, 8.175868034362793, "The Detection Area of the SXD Detector is 1 cm2."]
[7.1919660568237305, 0.265072226524353, "The Launch Date of the Stingray satellite Satellite is January 2024."]
[5.977240085601807, 2.972484827041626, "The Service Emphasis of the Lacuna Space Satellite Company is Lowest price."]
[7.405893802642822, 1.3945298194885254, "The Observation Data Acquisition Date of the SHIKISAI Satellite is Jan. 12, 2018."]
[7.067262172698975, 9.608460426330566, "The Band 1 of the RBV Instrument Spectral Band is 0.48 - 0.58 \u00b5m."]
[7.553528308868408, 1.070332646369934, "The Unexpected Observation Date of the Integral Satellite is 10 November 2015."]
[11.671046257019043, -0.7068543434143066, "The Subsystem Selection Aspects of the MERLIN Satellite is Power consumption, mass and volume allocations, thermal behaviour, radiation hardness."]
[10.472687721252441, -1.1619956493377686, "The Mass of the AprizeSat-10 Nanosatellite is 12 kg."]
[9.776785850524902, 8.569863319396973, "The Observation Capability of the MTEL Space Telescope Telescope is Space-time development of TLEs."]
[8.200264930725098, 0.6785693168640137, "The Workshop Date of the Megha-Tropiques Satellite is October 7-10, 2014."]
[7.933347225189209, 1.124443531036377, "The Publication Date of the The Space Mission at Kwajalein Space Mission is 2012."]
[7.2261128425598145, 0.3169112801551819, "The Booked for Launch Date of the SpIRIT Satellite is Early 2023."]
[10.238495826721191, 1.186265468597412, "The LTDN of the NEMO-AM Satellite is 9:30 hours."]
[7.381921291351318, 9.004377365112305, "The Swath of the TES Spectrometer is 5.3 km x 8.5 km."]
[8.545904159545898, 10.495697021484375, "The Operation Modes of the CCD Detector Imaging System is TDI."]
[6.097726821899414, 6.244387149810791, "The Performance of the SAR Mode Synthetic Aperture Radar Mode is Excellent."]
[7.738658905029297, 8.621660232543945, "The Spectral Coverage of the Atmospheric Chemistry Suite Spectrometer is From 0.7 to 17 micrometers."]
[9.594898223876953, 1.7951288223266602, "The Snapshot Frequency of the TESS Satellite is Every two minutes."]
[10.253320693969727, 4.967678546905518, "The Thruster Type of the Propulsion Subsystem Propulsion is Water micro-resistojet."]
[7.1228346824646, 9.183145523071289, "The Spatial Resolution of the Multispectral Instrument (MSI) Instrument is 60 m."]
[8.22598648071289, -0.5551078915596008, "The Transport Destination of the Yuanwang-21 and -22 Cargo Ships is Qinglan, Hainan island."]
[11.685800552368164, -1.203001618385315, "The Mass of the LAGEOS Satellite is 411 kg."]
[6.084434509277344, -0.022722244262695312, "The Lives Saved Annually of the Galileo Satellite Constellation is More than 2000."]
[7.073605060577393, 4.783926010131836, "The Satellite Ocean-Color Data Record of the NASA Organization is Data."]
[5.200066566467285, 4.484506130218506, "The Stations of the Ground Network Network is Aussaguel (France), Fairbanks (AK, Poker Flats location), Wallops Island, VA, and Hartebeesthoek, South Africa."]
[3.401275157928467, 5.309154510498047, "The Data Generation of the MicroCarb Satellite is 500 Gbit/day."]
[4.448323726654053, 2.5016233921051025, "The Antennas of the Starlink Satellite Satellite is Multiple high-throughput."]
[11.359617233276367, 7.023049354553223, "The Timing Precision of the NICER X-ray Instrument is Few \u00b5s."]
[7.341495037078857, 1.106956958770752, "The Development to Commercialization Date of the AIS Technology is Nov. 19, 2010."]
[11.519179344177246, 2.175018072128296, "The Sample Collection Date of the Hayabusa-2 Spacecraft is February 21, 2019."]
[4.487947463989258, 2.229214668273926, "The Number of Satellites of the Starlink Group 4-14 Satellite Group is 53."]
[9.505208969116211, 8.827771186828613, "The Design of the Telescope Optical Instrument is Compact, folded optical path, no optical obstruction."]
[7.83740234375, 9.144834518432617, "The Spatial Resolution of the OLCI Spectral Imaging Instrument is 300 m."]
[7.410146236419678, 0.3968909680843353, "The Launch Date of the SVOM Satellite is Scheduled for Mid-2023."]
[1.2465413808822632, 4.154976844787598, "The Battery Capacity of the BRITE spacecraft Satellite is 5.3 Ah."]
[3.576643705368042, 6.308805465698242, "The Data Rate (Uplink) of the S-band telemetry system Telemetry System is 256 kbit/s."]
[4.720053195953369, 0.37377169728279114, "The Ownership Stake in OneWeb of the Eutelsat Satellite Operator is 17.6%."]
[9.251514434814453, 4.124805450439453, "The Size of the Spacecraft Satellite is 320 mm x 340 mm x 362 mm."]
[12.134081840515137, 2.1730127334594727, "The Status Report Date of the OSIRIS-REx Mission is Sept. 15, 2016."]
[3.9676320552825928, 2.3849754333496094, "The Cion Power of the CICERO-6 6U CubeSat is 8 W."]
[7.264839172363281, 1.8796566724777222, "The Science Requirements Document Date of the SWOT Satellite is March 19, 2009."]
[10.243637084960938, 2.957252264022827, "The Orbit Altitude of the AERO-VISTA mission Satellite Mission is Approximately 450 - 600 km."]
[1.1036369800567627, 4.27473783493042, "The Battery Type of the EPS Electrical Power Subsystem is Li-ion."]
[7.104701995849609, 9.130576133728027, "The Ground Range x Product Length of the High Resolution Spotlight Imaging Mode is 10 x 5 km."]
[9.922637939453125, 1.460215449333191, "The Anomaly Duration of the ASTRO Satellite is 22 hours."]
[5.4809770584106445, 2.804487466812134, "The Manufacturer of the AMBER IOD-3 CubeSat is Horizon Space Technologies (UK)."]
[5.384662628173828, 4.057684898376465, "The Data Destination of the EMIT Satellite is NASA Land Processes Distributed Active Archive Center (DAAC)."]
[7.825823783874512, 9.840072631835938, "The IFOV/line (pixels/scan line) of the MERSI Medium Resolution Spectral Imager is 2048/8192."]
[9.608983039855957, 3.9054105281829834, "The Enclosure Shape of the CanX-7 Satellite is Circular."]
[7.648627758026123, 0.6655005216598511, "The Launch Date of the ETS-VIII Spacecraft is Dec. 18, 2006."]
[8.723870277404785, 10.499272346496582, "The CCD Detector Array of the PAN Camera Imaging Device is 12,288 pixels."]
[9.526930809020996, 8.919236183166504, "The Ground Swath of the ALI Telescope is 185 km."]
[11.25106143951416, 3.6318771839141846, "The Encounter of the Solar Orbiter Satellite is First time that we have encountered a comet tail inside Earth's orbit."]
[8.418399810791016, 4.512655735015869, "The Ground Sample Distance of the Resurs-P1 Imaging Satellite is 1 m."]
[7.875407695770264, 7.478026866912842, "The Oscillation Frequencies of the GOLF Instrument is Between 10-7 and 6 x 10-2 Hz."]
[4.770475387573242, 6.0232157707214355, "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."]
[5.138405799865723, 2.019334316253662, "The Payloads of the SLS Rocket is 13 CubeSats/Nanosatellites."]
[7.349058628082275, 7.962397575378418, "The Range of the Ozone Measurement Instrument Atmospheric Measurement Device is 0.1 - 15 ppmv."]
[1.9074333906173706, 3.8364264965057373, "The Cell Type of the AzurSpace 3G30 Triple Junction GaAs/Ge cells Solar Cell is AzurSpace 3G30 Triple Junction GaAs/Ge cells."]
[8.058159828186035, 11.154001235961914, "The Sensitivity of the Channel 8 Sensor is 0.4 K/pixel."]
[9.492680549621582, 0.9053974747657776, "The Deployment Timeline of the NRCSD Payload is 1 month after berthing."]
[5.560384750366211, 4.096646308898926, "The Support of the Test Station Testing Equipment is Rapid AI&T (Assembly, Integration, and Test)."]
[7.373490333557129, 7.300158977508545, "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."]
[9.440495491027832, 5.051253318786621, "The Spin Rate Change of the Satellite Spacecraft is Large, easily detectable change in the spin rate after a few hours or less."]
[11.0822172164917, 2.4595391750335693, "The Parachute of the Schiaparelli Module is Disk-Gap-Band canopy, 12 m diameter."]
[9.563262939453125, 1.8531625270843506, "The Data Release of the TESS Satellite is Sectors 1 and 2, observed between July 25 and September 20, 2018."]
[1.8966768980026245, 3.96370530128479, "The Mass of the SFINKS Solar Cell Array is 30 grams."]
[4.42360258102417, 6.64456844329834, "The Band of the LICEF Receiver is L-band."]
[9.056526184082031, 4.399392604827881, "The S/C Bus of the IRS-1C and IRS-1D Spacecraft is Central cylinder (930 mm diameter x 1123 mm)."]
[10.120256423950195, 5.231167316436768, "The Power Source of the Integrated Firing Test Test is Battery."]
[7.856187343597412, 7.384286403656006, "The Manufacturer of the Scanning Shack Hartmann Sensor Wavefront Measurement Device is AMO WaveFront Sciences, LLC."]
[5.479881286621094, 3.2727184295654297, "The Bus Design of the QuickBird-2 Satellite is BCP 2000 (Ball Commercial Platform 2000)."]
[8.439337730407715, 3.9066433906555176, "The Sky Coverage of the INTEGRAL Satellite is Almost full-sky coverage for brief events."]
[11.729931831359863, 5.410404682159424, "The Detection Date of the GRB 031203 Gamma-Ray Burst is 3 December 2003."]
[8.780065536499023, 6.942159175872803, "The Quantity of the Fluxgate Sensors Sensor is 3 orthogonal sensors per unit."]
[6.609005928039551, 4.658114910125732, "The Purpose of the Copernicus Sentinel-6 Michael Freilich Satellite is Provide accurate measurements of sea-level change."]
[6.639725685119629, 2.674833059310913, "The Manufacturer of the SCD-2 Satellite is INPE/Brazil."]
[5.580698490142822, 4.019082069396973, "The Function of the European Mission Tasking Center Center is Receives observation requests and incorporates them into its tasking/planning cycle."]
[8.69473934173584, 6.921047210693359, "The Sensor Quantity of the MAG Magnetometer is 2."]
[8.572649002075195, 10.092070579528809, "The Detector Area of Interest of the BEO Back-End Optics is 200 x 200 pixels."]
[6.214880466461182, 4.8478288650512695, "The Instrument Type of the ICEYE-X2 Satellite is SAR (Synthetic Aperture Radar)."]
[6.02462911605835, 2.25136137008667, "The Arrival Location of the STPSat-3 Satellite is Wallops Flight Facility in Virginia."]
[5.004012107849121, 1.920307993888855, "The Number of Missions of the MISSE Experiment is Nine."]
[9.160310745239258, 9.245086669921875, "The FOV of the X-ray Imager Instrument is 4.6\u00ba x 4.6\u00ba."]
[6.94615364074707, 8.772159576416016, "The Focal Length of the LISS-IIM Instrument is 324.4 mm."]
[9.421834945678711, 10.55678939819336, "The Dynamic Range of the Iris Video Camera Camera is 16 bit."]
[5.364556789398193, 4.5422797203063965, "The Ground Stations of the LAPAN-TUBSAT Satellite is Biak (Papua, east of Indonesia) and Rumpin (near Jakarta, Indonesia)."]
[4.021198749542236, 5.010555744171143, "The Redundancy Support of the DPU Data Processing Unit is Full duplication of DPU hardware."]
[6.657886505126953, 3.3970212936401367, "The Flight Operations Location of the Chandra X-ray Center Center is Burlington, Massachusetts."]
[7.392805576324463, 3.6516878604888916, "The Unknown of the Spot-1/5 \u2013Spot-6 Satellite Constellation is Unknown."]
[10.737650871276855, 10.29332447052002, "The Integral non-linearity of the PHA Detector is <0.05% of full scale."]
[6.70180082321167, 6.1893696784973145, "The Autonomy of the RapidScat Scatterometer Instrument is Autonomous."]
[7.919285774230957, 9.505168914794922, "The Spectral Range of the Spectrally modified current sounder Sensor is 8.3-8.7."]
[10.177042961120605, 2.946390151977539, "The Altitude at Final Breakup of the S/C Satellite is Little more than 100 km."]
[4.7552313804626465, 1.6874089241027832, "The Number of Wire Boom Deploys of the THEMIS Constellation Satellite Constellation is 20."]
[6.2043843269348145, 3.1689980030059814, "The Agency of the TechEdSat Satellite is JAXA, NASA, ARC."]
[4.9803242683410645, 4.565130710601807, "The Interface Standard of the GSCG Ground Station Control System is CCSDS SLE."]
[10.338744163513184, 3.4199724197387695, "The Speed of the PhiSat-1 Satellite is Over 17,000 mph (27,500 km/h)."]
[3.9958958625793457, 5.707312107086182, "The Downlink Data Rate of the Satellite Satellite is 115.2 kbit/s."]
[6.965301036834717, 4.875370502471924, "The Monitoring Program of the MicroCarb Satellite is CNES / MicroCarb Atmospheric CO2 Monitoring Program."]
[7.347850799560547, 5.5771684646606445, "The Effect of the Sea Surface Natural Feature is Mimics the ocean floor."]
[11.489760398864746, -1.1455297470092773, "The Operation of the DSA Device is Not designed to support its own weight in the one-g environment at Earth's surface."]
[4.764705181121826, 0.8625532984733582, "The Revenue Projection of the Satellogic Satellite Imaging Company is $7 million in 2021 to $787 million in 2025."]
[9.152169227600098, 8.345152854919434, "The L1 Detectors Active Area of the HIT Sensor is 2 cm2."]
[7.779535293579102, 2.7352988719940186, "The Collaboration of the Hinode, IRIS and SOHO Solar Missions is Provide a suite of complementary instruments to study our Sun."]
[6.169355869293213, 3.9487133026123047, "The Platform Shape of the Spacelab Pallet Equipment is Open, U-shaped."]
[6.490712642669678, 4.653453350067139, "The Product Levels of the Sentinel-3 Ocean Surface Topography Mission is Level 1, Level 2."]
[8.459827423095703, 9.34020709991455, "The Upgrades of the NIRSpec Instrument is New detectors and microshutters."]
[5.952324390411377, 6.478781700134277, "The PRF of the SAR Radar is About 18 kHz."]
[5.902849197387695, 10.853494644165039, "The No of Passbands of the Channel 6 Sensor is 1."]
[6.090759754180908, 5.449009895324707, "The Data Collection Purpose of the ATOVS Advanced TIROS Operational Vertical Sounders is Support regional NWP over Europe."]
[7.9363017082214355, 4.59647274017334, "The Resolution of the Planet SkySats Satellite is 50-centimeter-per-pixel."]
[8.6806001663208, 6.12254524230957, "The Peak strength of the EEJ (Equatorial Electrojet) Phenomenon is ~80 nT at 12:00 hours LT (Local Time)."]
[7.723257541656494, 8.447664260864258, "The Field of View of the OMPS Nadir Sensor Spectrometer is 110\u00b0."]
[9.366866111755371, 7.144449710845947, "The First Actuation Pressure of the T3\u00b5PS Pressure Sensor is 711 mbar."]
[5.045717716217041, 3.5311148166656494, "The Types of the Satlet Satellite Subsystem is Single-function satlets, System satlets."]
[4.815509796142578, 4.629312992095947, "The Planned Connection of the Ground Communication Links Communication System is Between ISTRAC and MOSDAC."]
[4.684331893920898, 6.120288372039795, "The Frequency Band of the ELFIN-A Satellite is 435-438 MHz."]
[4.518476963043213, 2.465515375137329, "The Type of the Hiber-3 Satellite is 3U CubeSat."]
[7.423071384429932, 1.3195059299468994, "The Calibration Date of the NOAA-11 Satellite is 1989 to 1993."]
[7.796783447265625, 0.3797469437122345, "The Launch Date of the Crew-4 Spacecraft is Spring of 2022."]
[5.311805725097656, 9.624735832214355, "The Power Consumption of the STOs and STAEs Analog Electronic units is 150.4 W (for 3 STO configuration)."]
[11.771888732910156, -0.9359117150306702, "The Mass of the Biopan Payload is 27 kg."]
[6.734423637390137, 8.394072532653809, "The Optical Pulse Spectral Range of the LI Instrument is 777.4 \u00b1 0.17 nm."]
[8.444454193115234, 3.8409647941589355, "The Propulsion System of the CASSIOPE mission Satellite Mission is None."]
[8.153241157531738, 4.996102333068848, "The Orbit Prediction Accuracy of the Picosatellite Satellite is Meter Level."]
[5.148024559020996, 9.26144790649414, "The Number of Sensors of the SEIS Seismometer is Six."]
[9.27359676361084, 6.376406192779541, "The Attitude Accuracy of the Procyon Star Tracker is 5 arcsec on X/Y and 50 arcsec on Z."]
[12.627936363220215, 6.919582843780518, "The Pulse period (ms) of the J1846-0258 Pulsar is 325.684."]
[8.846258163452148, 0.3625834584236145, "The Investigation Duration of the SpaceX Falcon-9 Rocket is Over the past four months."]
[10.47614574432373, -1.148573637008667, "The Mass of the SPROUT Nanosatellite is ~7 kg."]
[10.958439826965332, 3.443127155303955, "The Orbital Path of the Juno spacecraft Spacecraft is Over Jupiter's poles."]
[8.789565086364746, 7.090299606323242, "The Data Processing Unit of the PLASTIC Solar Wind Ion Instrument is IMPACT IDPU."]
[10.326730728149414, 1.3135789632797241, "The LTAN of the Satellite Orbit Orbit is 6:00/18 hours."]
[11.506418228149414, 4.081870079040527, "The Mass of the AU Mic b Planet is Less than 58 times Earth's mass."]
[8.041744232177734, 4.379008769989014, "The DEM Resolution of the SRTM Satellite is 30 m."]
[7.782081127166748, 9.195562362670898, "The Spectral Bands of the NEMO-HD Satellite is 450-520 nm, 520-600 nm, 630-690 nm, and 760-900 nm."]
[9.678409576416016, 3.5299272537231445, "The Mission Type of the Moon Impact Probe Probe is Surface Impact."]
[6.06904411315918, 9.728525161743164, "The Mass of the Instrument Telescope is 967 kg."]
[8.71450138092041, 8.987775802612305, "The Filter Thickness of the FUV channel Spectrometer is 2.50 mm."]
[7.612882614135742, 4.059206008911133, "The Potential Use of the Space Moss Moss is Space and future bases on the Moon or Mars."]
[5.021483421325684, 2.2272579669952393, "The Coverage of the Payload Satellite Component is Eight spot beams."]
[7.261850833892822, 10.020906448364258, "The Mission Operations Blocks of the HyperScout\u00ae Satellite is Radiometric Calibration, Line of Sight Model Correction and Instrument Functionality Testing; Intensive Observations L2 Data Validation; On Board Processing Experiments."]
[6.114340305328369, 0.5475668907165527, "The Launch Date of the COPPER CubeSat Satellite is Nov. 20, 2013."]
[10.261507987976074, 5.69205379486084, "The Control Method of the Barber Pole Friction Device is Tether deployment."]
[5.67059850692749, 3.239668130874634, "The Changes of the iMESA-R Flights Technology is 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."]
[10.413795471191406, 2.6270480155944824, "The Apogee Alignment of the MMS and THEMIS Satellites is Roughly 90\u00ba."]
[8.519186973571777, 3.2332160472869873, "The Application of the Generic Radio-Frequency Subsystem Subsystem is High-Altitude Formation-Flying Missions."]
[3.8674561977386475, 5.647853851318359, "The Downlink Speed of the COSMO-SkyMed-1 Satellite is 300 Mbit/s."]
[9.209041595458984, 3.2301840782165527, "The Orbit Type of the Satellite HY-1B is Sun-synchronous near-circular orbit."]
[6.7972798347473145, 1.3243231773376465, "The Presentation Date of the RazakSAT Satellite is Nov. 7-11, 2005."]
[6.169332027435303, 2.030535936355591, "The Total Ionized Dose Radiation of the TacSat-4 Satellite is 100 MRad."]
[10.935165405273438, 4.070040225982666, "The Climate Patterns of the XO-3b Exoplanet is Map provided by Spitzer data."]
[9.064458847045898, 10.120370864868164, "The Type of the Earth sensor Sensor is CMOS camera with a fisheye lens and an image sensor of 1.3 Mpixel."]
[7.850419998168945, 3.0891058444976807, "The Operation Status of the TSX (TerraSAR-X) Satellite is Nominal."]
[6.848689079284668, 8.067778587341309, "The Measurement of the Sea and Land Surface Temperature Radiometer Instrument is Real amount of energy radiating from Earth."]
[9.60057258605957, 0.48827627301216125, "The Consumable Supply Life of the SA-200HP Spacecraft Platform is 10 years."]
[10.942240715026855, 7.21070671081543, "The Longitudinal Dimension of the HXT-C X-ray Optics is 1400 mm."]
[8.834242820739746, 1.4333831071853638, "The Revisit Time for Ocean Color Scanner of the Satellite HY-1B is Every day."]
[4.236597061157227, 2.4781177043914795, "The Form Factor of the TechEdSat Satellite is 1U CubeSat."]
[8.855523109436035, 6.1583476066589355, "The Components of the Automatic target pointing mode Observation Mode is Star sensor assembly, GPS receiver, attitude control actuator."]
[11.767215728759766, -0.9693840146064758, "The Mass of the DIMAC Payload is 9 kg."]
[4.777775764465332, 0.8603460192680359, "The Contract Amount of the HawkEye 360 Company is $15.5 million."]
[8.056469917297363, 10.782387733459473, "The Data Quantization of the MSU-100 Camera is 8 bit."]
[3.6334869861602783, 6.476665019989014, "The Data Rate of the RF Communications Communication System is 1.2 kbit/s."]
[7.208833694458008, 2.5207104682922363, "The URL of the RHESSI Satellite is http://berkeley.edu/news/media/releases/2005/02/18_magnetar.shtml."]
[9.222318649291992, 4.02725887298584, "The Body Size of the NorSat-2 Satellite is Smaller than 62 x 62 x 73 cm."]
[5.042241096496582, 6.662620544433594, "The Gain of the Antenna ADS-B Antenna is 11.2 dBi."]
[5.950249195098877, 6.413535118103027, "The Polarization of the SAR Synthetic Aperture Radar is HH."]
[3.3271498680114746, 5.213317394256592, "The Storage Memory of the Satellite Satellite is > 512 Gbit."]
[10.724767684936523, -1.640405297279358, "The Cargo Return of the Starliner Spacecraft is 600 pounds."]
[10.369394302368164, 3.430327892303467, "The Closest Separation Distance of the Cluster spacecraft Satellite is 4 km."]
[11.115337371826172, -1.571582555770874, "The Mass of the QB50P1 and QB50P2 2U CubeSats is 2 kg each."]
[7.785811901092529, 3.8567240238189697, "The Previous Sea Ice Coverage Record of the Global Change Observation Mission 1st \u2013 Water \u201cSHIZUKU\u201d Satellite is 19.44 million km2."]
[7.2280402183532715, 1.0049028396606445, "The Capture Date of the WorldView-1 Satellite is 19 August 2021."]
[6.621496200561523, 0.549419641494751, "The Launch Date of the FedSat Satellite is 14 Dec 2002."]
[10.195755004882812, 6.839913368225098, "The Thermal Control Methods of the Neutron-1 Spacecraft is Passive, Conducting heat through copper strapping, Using external spacecraft surfaces as thermal radiators, Turning off subsystem hardware."]
[9.565558433532715, 4.1051716804504395, "The Size of the LightSail-2 Spacecraft is Small washing machine."]
[9.133685111999512, 9.189337730407715, "The FOV in Vertical Plane of the THD Horizon Detector is 22\u00ba."]
[7.492568492889404, 2.0073416233062744, "The Operator of the IceCube Radiometer is NASA and GSFC (Goddard Space Flight Centre)."]
[11.149282455444336, 4.486019134521484, "The Previous Believed Speed of the Heliosphere Interstellar Medium is Faster than 52,000 miles per hour."]
[9.644830703735352, 7.804906368255615, "The Proton Energy Range of the REPT Instrument is 17 to >100 MeV."]
[9.51163101196289, 3.8322737216949463, "The Formation Flight of the CanX-4 & CanX-5 Satellites is Accomplished."]
[10.155426979064941, 3.0040791034698486, "The Orbit of the Prox-1 Spacecraft is Circular, 720-kilometer-high."]
[9.740551948547363, 1.588718295097351, "The Repeat Cycle of the SARAL spacecraft Satellite is 35 days."]
[9.203531265258789, 4.12840461730957, "The Size of the TechEdSat Satellite is 10 cm x 10 cm x 11.3 cm."]
[8.523408889770508, 1.0410000085830688, "The Launch Date of the LRO Satellite is June 18, 2009."]
[8.662040710449219, 9.298632621765137, "The Detector Size of the Long Wavelength Band Spectrometer is 2.5 cm x 2.5 cm."]
[8.313250541687012, 3.2938921451568604, "The Formation Type of the TanDEM-X Satellite is Bistatic interferometric."]
[4.288008689880371, 4.347533226013184, "The Interface of the Spacecraft Emulator Testing Equipment is MCS to OBC and back again."]
[9.851543426513672, 7.585837364196777, "The Thermal Control of the Telescope Tube Assembly Telescope is On-board heaters."]
[5.951784133911133, 2.6407692432403564, "The CEO of the Maxar Space Solutions Company is Jablonsky."]
[8.398577690124512, 9.941638946533203, "The Spectral Resolution of the EPIC Cameras Imaging System is E/\u0394E ~ 20-50."]
[9.303557395935059, 1.2045897245407104, "The Required Contacts of the PROBA Project Satellite Project is 2 or 3 per day for S-band (U/D)."]
[11.451417922973633, 2.2125487327575684, "The Communication Disruption of the Hayabusa-2 Spacecraft is During solar conjunction operation."]
[7.641611576080322, 7.2724785804748535, "The Function of the RISE Experiment is Uses the spacecraft's radio connection with Earth to assess perturbations of Mars' rotation axis."]
[4.0057291984558105, 4.907192707061768, "The Redundancy of the CIB Control and Interface Board is Cold."]
[9.345380783081055, 7.93829345703125, "The Cadence of the Alpha-Particle Spectrum Measurement is Up to around 20 MeV /nuc."]
[4.458929061889648, 5.234909534454346, "The Data Latency of the SENSE Satellite is Operational SEM data latency requirements are satisfied."]
[3.2262775897979736, 5.33718729019165, "The Data Rate of the SSDRs Solid-State Data Recorders is 20 Mbit/s."]
[9.298108100891113, -0.5432596802711487, "The Catalyst for Establishing a Nanosatellite Manufacturing Sector of the MDASat-1 Satellite is Yes."]
[8.362712860107422, 3.664578437805176, "The Requirements of the LunaNet Device is No extra requirements on the hardware."]
[7.434703826904297, -0.24755285680294037, "The Arrival Date at ISS of the HTV-7 Cargo Vessel is 27 September."]
[5.39285945892334, 7.294886589050293, "The Beam width of the UHF Band is 3.6 rad."]
[7.696372985839844, 8.48799991607666, "The Field of View of the OMPS Limb Profiler Spectrometer is 8.5\u00b0."]
[10.397332191467285, 4.826766014099121, "The Propellant of the Propulsion System Propulsion Subsystem is Hydrazine."]
[11.78244400024414, 4.569976329803467, "The Distance of the Cassiopeia A Supernova Remnant is 10,000 light years."]
[9.616262435913086, 7.189671993255615, "The Peak Temperature of the Orion Spacecraft is 2,200\u00b0C."]
[6.7424540519714355, 5.733897686004639, "The Stereo Observations Area of the GIS Instrument Satellite Instrument is Up to 6270 km2 daily."]
[5.316090106964111, 6.0214924812316895, "The Publication Date of the Dual Gimbal Antenna Antenna is January 2009."]
[6.649017333984375, 5.919224262237549, "The System Level Specifications Retained of the SCATSat-1 Satellite is OSCAT instrument."]
[6.675983905792236, 5.485023498535156, "The Applications of the Satellite STRATOS is Weather model assimilation of RO, space weather monitoring, ionosphere corrections for navigation, thermospheric density (POD)."]
[2.2346622943878174, 3.8126111030578613, "The Solar Array of the Starlink Satellite Satellite is Single."]
[10.22940444946289, 6.990819931030273, "The Components of the Thermal Control Louvers Thermal Regulation Device is Front and back plates, flaps, springs."]
[6.550924301147461, 3.662444591522217, "The Mission Type of the Flying Laptop Satellite is EO."]
[8.851000785827637, 4.601034164428711, "The Orbit Control of the MEV-2 Satellite is Does not control the orbit."]
[9.824621200561523, 2.869826316833496, "The Orbit Reach of the Akatsuki Spacecraft is 2016."]
[5.981413841247559, 6.085057735443115, "The SAR Payload Repeat Cycle of the RCM Satellite is 12 days."]
[6.170970916748047, 6.544510841369629, "The Signal Type of the Radar Altimeters Instruments is Pulses of radio waves (microwaves)."]
[9.616990089416504, 4.259309768676758, "The Diameter after Expansion of the Genesis-2 Spacecraft is 2.54 m."]
[11.302559852600098, 3.8565144538879395, "The Bedrock Rise Rate of the Earth Planet is About 10 mm a year."]
[5.60307502746582, 9.255936622619629, "The Power of the ASPOC Instrument is 3.0 W."]
[8.95549201965332, 5.362904071807861, "The Attitude Control of the Payload Satellite Payload is Pointing Accuracy."]
[3.539973497390747, 6.613079071044922, "The Bit Rate of the S-band Transmitter Transmitter is Up to 1 Mbit/s."]
[8.276198387145996, 9.210067749023438, "The Smile and Keystone of the Instrument Spectrometer is \u22641 image pixel."]
[5.408845901489258, 4.736424922943115, "The Data Relay System of the Alphasat and Sentinel-1A Satellites is LCTs."]
[6.538107395172119, 6.175071716308594, "The Mission of the OSCAT-3 Radar Scatterometer is Oceansat-3."]
[6.505249500274658, 7.751986026763916, "The Foot Print of the RA-1 Instrument is 16 - 20 m."]
[9.000316619873047, 1.1355233192443848, "The Rock Deposits Age of the LRO Satellite is Less than 100 million years old."]
[5.741793155670166, 1.6347179412841797, "The Satellite Launch Vehicle of the Kleos S.A. Company is SpaceX Falcon 9."]
[7.925121784210205, 0.6641080379486084, "The New Launch Date of the Starliner Spacecraft is Unknown."]
[2.18673038482666, 4.462828636169434, "The Power On of the Watchdog Device is Immediately after the spacecraft has been ejected from the launch vehicle."]
[10.884788513183594, 2.0083446502685547, "The Mean Anomaly at Epoch of the Swarm-A (Alpha) Satellite is \u0394t = 2-10 s difference between A and B."]
[7.39435338973999, 4.264726161956787, "The Imaging Capability of the BILSAT-1 Satellite is Stereoscopic."]
[12.154488563537598, 2.1460468769073486, "The Sample Collection Attempt Date of the OSIRIS-REx Spacecraft is Late August."]
[5.809715270996094, 8.649940490722656, "The Beam Pointing Accuracy of the MWHS-II Microwave Humidity Sounder is \u22640.1\u00ba."]
[7.993108749389648, 1.45438551902771, "The Presentation Date of the SCARLET Solar Array Solar Array is 2000."]
[8.070233345031738, -0.7411975264549255, "The Live Mammals of the Dragon Spacecraft is 20 rodents."]
[5.888967990875244, 3.128296136856079, "The Manufacturer of the Sentinel-5 Satellite is Airbus DS."]
[4.67579460144043, 2.582305908203125, "The Configuration of the Spacecraft Satellite is 3U CubeSat carrying a Ka-band payload."]
[11.789687156677246, -0.9261234402656555, "The Mass of the Experiment Payload is 55 kg."]
[7.101220607757568, 2.7752950191497803, "The Operational Interface of the SWOT Satellite is Unique."]
[5.417691230773926, 5.540124416351318, "The Tracking Capability of the OEM628 Receiver Receiver is Up to 120 signals (60 dual frequency satellites) at any time."]
[3.676934242248535, 5.2159013748168945, "The Time Synchronization Accuracy of the Data Handling Subsystem Subsystem is < 10 \u00b5s."]
[10.579934120178223, -1.031352162361145, "The Cables, Connectors Mass of the Microsatellite Satellite is 5.1 kg."]
[10.228901863098145, 5.109954357147217, "The NASA Participation of the DRACO Demonstration Rocket is Goal of using nuclear thermal propulsion for long-duration human spaceflight missions."]
[13.170772552490234, 4.026730537414551, "The Release Date of the Gaia EDR3 Satellite Data is 3 December 2020."]
[9.603808403015137, 5.97379732131958, "The Actuation of the ADCS Attitude Determination & Control Subsystem is 6 reaction wheels and 3 torque rods."]
[4.018359661102295, 6.44154691696167, "The Packet modulation of the RF communication subsystem Communication is FSK 1200 baud."]
[11.030054092407227, 6.3418073654174805, "The Mission of the Neutron-1 Satellite is Study low energy neutron flux in Low Earth Orbit (LEO) as a function of time and location."]
[4.144099235534668, 3.7165825366973877, "The Peak Detection Rate of the Complex Receiver AIS Receiver is 19 Messages/s."]
[6.300084114074707, 1.0348273515701294, "The Launch Date of the COSMO-SkyMed Second Generation Satellite is 18 December 2019."]
[9.592450141906738, -0.5815562605857849, "The On-board Computer of the Microsatellite Satellite is Not implemented."]
[6.841226577758789, 0.6894625425338745, "The Launch Year of the Pl\u00e9iades Neo constellation Satellite Constellation is 2020."]
[9.02078628540039, 10.372735023498535, "The Resolution of the Z-panel camera Camera is 3 Mpixel."]
[6.09415864944458, 3.530689239501953, "The Experiment Approach of the Scientific Payload Satellite Payload is Baseline is to run most of the experiments sequentially."]
[6.072336196899414, 11.253018379211426, "The Approx. peak sensitivity altitude of the Channel 7 Sensor is Unknown."]
[7.435192584991455, 8.00798225402832, "The Horizontal Cell Size of the Ozone Measurement Instrument Atmospheric Measurement Device is 250 km."]
[5.52555513381958, 5.955235481262207, "The Antenna Mounting Plane Clearance of the KySat-1 Satellite is 6.5 mm."]
[8.04619026184082, 2.351961374282837, "The Conference Location of the SWAP EUV Telescope is Toulouse, France."]
[4.1910319328308105, 6.655025005340576, "The Frequency of the VHF Transmitter Radio Transmitter is 137 MHz."]
[4.752915859222412, 1.7819799184799194, "The Number of Satellites of the MSG Satellite Fleet is 6."]
[7.710743427276611, 5.258004188537598, "The Target Observation Frequency of the OCO-2 Satellite is Roughly once each day."]
[9.673357963562012, 5.982376575469971, "The Algorithm Type of the Control algorithm ADCS is B-dot based algorithm."]
[5.031420707702637, 4.494266510009766, "The Purpose of the NICT's New OGS Ground Station is Satellite Laser Communication and SOTA/Socrates experiment."]
[5.374814510345459, 1.3954013586044312, "The Deployment Method of the NanoRacks CubeSat Satellite is JEM airlock slide table."]
[6.721878528594971, 1.2411065101623535, "The Installation Date of the Capella Company is 9 November 2021."]
[10.147522926330566, -0.8525194525718689, "The Dimensions of the GOMX-1 Nanosatellite is 10 cm x 10 cm x 20 cm."]
[7.979160785675049, 2.5186092853546143, "The Sale Approval of the ARTEMIS Satellite is ESA approves sale of Artemis telecom satellite to Avanti."]
[7.042675018310547, 7.450599193572998, "The Image Frequency of the Data Flow System is One image per minute."]
[8.53683090209961, 10.595890045166016, "The Mass of the FLIR Boson camera Thermal Imaging Camera is <38 g."]
[8.292170524597168, 3.675615072250366, "The Acquisition Timeline of the TanDEM-X Satellite is Not provided."]
[11.883573532104492, 0.9589047431945801, "The Launch Date of the Chang'e-5 Spacecraft is 23 November 2020."]
[8.32424545288086, 4.843132019042969, "The Research Focus of the MMS Satellite is How electrons move through the magnetosphere."]
[11.645502090454102, -0.7239509224891663, "The Hydrazine Fuel Mass of the MERLIN Satellite is 28 kg."]
[6.445700645446777, 3.959648847579956, "The Location of the LPVEx Field Campaign is Helsinki Testbed and the Gulf of Finland."]
[10.223883628845215, 3.0143091678619385, "The Orbit Altitude of the Max Valier Satellite is 600 km."]
[9.251068115234375, 3.215045213699341, "The Type of the Orbit Satellite is Sun-synchronous near circular orbit."]
[10.483909606933594, -1.023281216621399, "The Mass of the IITMSAT Microsatellite is 11 kg."]
[9.442390441894531, 5.767485618591309, "The Power Consumption of the Passive Attitude Control System Attitude Control System is None."]
[6.48468542098999, 8.235081672668457, "The Publication Date of the Copernicus Imaging Microwave Radiometer (CIMR) Radiometer is December 2021."]
[3.9996261596679688, 2.3358154296875, "The CubeSat of the Satellite SporeSat is 3U."]
[4.863399505615234, 0.9707139730453491, "The Mission Budget of the Carruthers Geocorona Observatory Spacecraft is $75 million."]
[9.787555694580078, 1.445094108581543, "The Revisit Period of the CBERS-2B Satellite is 26 days."]
[10.302652359008789, 9.335929870605469, "The Velocity Resolution of the IRIS Satellite is 0.4 km/s."]
[7.03902006149292, 9.65992546081543, "The SNR of the RBV Instrument Radiometric Signal is 33 dB in bands 1 and 2, 30 dB in band 3."]
[5.817943572998047, 8.16650676727295, "The Bandwidth (GHz) of the ICI-3 Radiometer is 3."]
[5.7719831466674805, 2.5154833793640137, "The Acquisition of the Maxar Technologies Company is Vricon."]
[8.469808578491211, 3.1782331466674805, "The Local Time of the Tandem-L Satellite is 6 h / 18 h."]
[9.219456672668457, 4.142068862915039, "The Size of the Spacecraft Satellite is 80 cm x 60 cm x 60 cm."]
[7.146420001983643, 1.4000141620635986, "The Mission Start Date of the Eu:CROPIS Satellite is May 24, 2016."]
[9.356337547302246, 11.608957290649414, "The Pixel size of the Channel 6 Sensor is 32 km x 32 km."]
[6.6056294441223145, 10.69184684753418, "The SNR of the Band 4 Spectral Band is 180."]
[3.941603660583496, 6.522830486297607, "The Modulation Scheme of the XMOD X-band Modulator is QPSK."]
[8.225159645080566, 0.6739873886108398, "The Launch Date of the Megha Tropiques Satellite is Oct. 12, 2011."]
[5.43400239944458, 4.292672157287598, "The Location of the Precipitation Processing System Data Processing System is GSFC."]
[7.355788707733154, 0.9414477348327637, "The Conference Presentation Date of the PROBA-2 Satellite is April 25-27, 2006."]
[8.664928436279297, 3.8988306522369385, "The Ground-Controlled Formation Geometry of the ATI Experiments Satellite Experiment is Minimum satellite distances of 150 m in the plane perpendicular to the flight direction."]
[7.669519424438477, 3.1781723499298096, "The Tracking Capability of the Hinode Satellite is Continuous tracking of sunspots with high spatial resolution for several days."]
[9.13919734954834, 6.1791300773620605, "The Mass of the CMG Control Moment Gyroscope is 500 g."]
[9.777721405029297, 7.978699684143066, "The Gamma-ray Energy Range of the MGNS Neutron and Gamma-ray Spectrometer is 300 keV to 10 MeV."]
[4.816652774810791, 5.155373573303223, "The Required Reception System of the UHRIT Data Dissemination System is X-band reception system."]
[9.699263572692871, 8.039384841918945, "The Detectable Count Rates of the Gamma-ray Counter Detector is > 10 Hz."]
[3.5430195331573486, 2.2845957279205322, "The Size of the VisionCube-1 Satellite is 2U."]
[6.8833160400390625, 1.8122156858444214, "The Launch Date of the Kolibri-2000 Satellite is March 20, 2002."]
[11.26684284210205, 3.7804477214813232, "The Non-Group Comet Sightings per Year of the SOHO Satellite is Over 100."]
[5.878155708312988, 2.7999258041381836, "The General Manager of the GHGSat-C2 Satellite is Marc Corriveau."]
[9.232463836669922, 1.1313802003860474, "The Mission Duration of the GPM Satellite is Expected to last to the mid-2030\u2019s or beyond."]
[10.503923416137695, -1.0086158514022827, "The Mass of the Sterkh-2 Microsatellite is ~ 171 kg."]
[6.0586256980896, 3.515704393386841, "The Execution Responsibility of the TDP Operations Satellite Operations is Inmarsat."]
[11.205705642700195, -1.5140790939331055, "The Mass of the PicSat CubeSat is 3.5 kg."]
[10.037151336669922, 2.8977303504943848, "The Altitude of Initial Orbit of the OneWeb Satellites Satellite Manufacturer is 450 kilometers."]
[7.470930576324463, -0.3076540529727936, "The Predicted Reentry Date of the Chinese Rocket Stage Rocket Stage is May 8, 2021."]
[11.69378662109375, 4.584146499633789, "The Heliacal Rising Significance of the Pleiades Open Cluster is Marked the opening of seafaring and farming seasons."]
[10.620522499084473, 9.27014446258545, "The Image Segment Location of the CaSSIS Imaging System is Margin of the South PLD."]
[12.14116096496582, 3.2910380363464355, "The Orbit Inclination of the HY-2A Satellite is 99.3\u00ba."]
[8.42992877960205, 8.819503784179688, "The Spatial Resolution of the Observation Instrument Telescope/Spectrograph is 0.16\u00ba (Airglow Port), 0.06\u00ba (High-spatial-resolution Port)."]
[6.848757743835449, 0.5127151608467102, "The Report Date of the GEOS-1 Satellite is Jan. 1977."]
[9.456936836242676, 5.816343307495117, "The Controlled Axes of the Permanent Magnets Attitude Control is Two."]
[9.161811828613281, 3.215501070022583, "The Orbit of the SEOSAT-Ingenio Satellite is Sun-synchronous circular orbit."]
[6.537502765655518, 5.264415264129639, "The Objective of the GEOSAT Radar Altimeter (GRAS) Instrument is Study the marine gravity field as accurately as possible."]
[7.090646743774414, 2.879666328430176, "The Mission Status of the SwRI Small Satellite Satellite is Forward."]
[9.021459579467773, 9.2525634765625, "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."]
[7.837279796600342, 9.846996307373047, "The Spectral Bands of the IRS Imager is 4."]
[9.77973747253418, 8.563196182250977, "The Observing Capability of the Ground-based Telescopes Telescopes is Decreases as air mass increases at low altitudes."]
[7.469098091125488, 3.8928472995758057, "The Purpose of the TeLEOS-1 Satellite is Environmental Monitoring."]
[5.229141712188721, 6.226451396942139, "The Design of the Antenna Payload is Pre-deployed and designed to survive launch conditions in any orientation."]
[8.138501167297363, 2.561504364013672, "The Ground Segment of the Himawari-8/9 Satellite is Unknown."]
[6.144210338592529, 3.886296272277832, "The Data Provided of the MetOp Satellites Satellites is ATOVS, AVHRR, ASCAT and IASI Data."]
[9.7181978225708, 1.529137134552002, "The Resilience Strategy of the Dellingr Satellite is 25-hour reset."]
[5.662073135375977, 7.514123439788818, "The Technology Readiness Levels of the KaRIn Instrument is 3 to 5."]
[7.337821006774902, 0.9387003779411316, "The Conference Presentation Date of the PROBA-2 Satellite is Oct. 17-20, 2005."]
[5.233057022094727, 2.254737138748169, "The Total Student Contributors of the SAPPHIRE Satellite is More than 70 Stanford students and 30 WU students."]
[1.855175256729126, 5.094451904296875, "The Operating Voltage of the NovAtel OEMV-2 L1/L2-F GPS unit GPS Unit is 3.3 VDC."]
[9.627297401428223, 3.579324245452881, "The Mission Title of the LUMIO CubeSat is Characterizing lunar meteoroid impacts."]
[6.021057605743408, 2.736488103866577, "The CEO of the Lacuna Space Company is Rob Spurrett."]
[7.596721172332764, 7.2322492599487305, "The Symposium Date of the ECOSTRESS Instrument is July 23\u201328, 2017."]
[8.85362720489502, 10.699052810668945, "The CCD array size of the 16 mm camera Camera is 750 x 580 pixels."]
[7.308166027069092, 9.470122337341309, "The Radius of Circular Scan of the S-192 optomechanical scanner Scanner is 42 km."]
[7.068787097930908, 0.024668043479323387, "The End of Life Date of the ST5 Satellite is 30 June 2006."]
[4.156618595123291, 6.161328315734863, "The Receiver Locking Sequence of the Transponder Communication Device is Residual carrier, command subcarrier."]
[3.4183475971221924, 6.605401515960693, "The Power of the Spacecraft Repeater Communication Device is 53 W."]
[11.133304595947266, 2.7496695518493652, "The Crest Height of the Yellowstone River River is 13.88 feet."]
[8.60948371887207, 6.898502349853516, "The Angular Resolution of the Vector Magnetometer Instrument is 1 arcsec."]
[7.386317729949951, 10.115457534790039, "The Spectral Resolution of the HySI Hyperspectral Imager is \u2264 15 nm."]
[3.818702459335327, 6.104292869567871, "The Multiplexed Subchannels of the Optical Downlink Communication System is Up to 16."]
[3.6169347763061523, 6.55156946182251, "The Data Rates (TC) of the EWC31 S-band transceiver module Communication Module is 8 kbit/s to 256 kbit/s."]
[3.5392425060272217, 2.3019888401031494, "The Size of the Wren FemtoSat is 2.5U."]
[7.896274566650391, 4.262248992919922, "The Altitude of the DMC-3 Constellation Satellite Constellation is 651 km."]
[9.290565490722656, -0.6042617559432983, "The Purpose of the NEMO Bus Nanosatellite is Earth Monitoring and Observation."]
[6.611352443695068, 4.692155361175537, "The Data Measurement of the Sentinel-6 Satellite is Ocean Heat, Movement, Sea Level."]
[6.46477746963501, 2.8970537185668945, "The Agency of the Arachne Satellite is USAF."]
[2.4050302505493164, 6.32966947555542, "The Latency Requirement of the S-2 NRT Product is Restituted 90 minutes before Sentinel-2 A/B ANX is crossed."]
[-4.981341361999512, 4.407576560974121, "The Support Phase Time Period of the Mango Tango Satellite Formation is 02.07 to 02.08.2010."]
[10.537156105041504, 3.0863327980041504, "The Distance from Earth of the MarCO CubeSat is 1 million kilometers."]
[10.58337688446045, 8.465786933898926, "The Stray Light/Disk Light Rejection of the COR1 Coronagraph1 imager is 10 -6  B sun."]
[7.7411322593688965, 2.509305953979492, "The Impact Site of the MRO Mars Reconnaissance Orbiter is Confirmed."]
[5.125333786010742, 4.633692741394043, "The Number of Ground Station of the PRISMA Satellite Network is 2."]
[5.077511787414551, 7.155755043029785, "The Pixel Size (km x km) of the Antenna Reflector is 32."]
[10.487069129943848, 2.489896774291992, "The Apogee (km) of the Intercosmos- Bulgaria 1300 (Intercosmos-22) Satellite is 906."]
[7.237054347991943, 0.5166135430335999, "The Flight Operation Date of the Cute-1.7+APD Nano-Satellite is June 25-29, 2007."]
[6.63437557220459, 7.464064121246338, "The Operation Power Level of the Scanning LIDAR LIDAR is Not operated at its highest power-level."]
[5.602802276611328, 9.120935440063477, "The Power of the Instrument Satellite Instrument is 6 W."]
[6.7117791175842285, 0.7023390531539917, "The Launch Date of the SEOSAT-Ingenio Satellite is November."]
[11.650847434997559, -1.195416808128357, "The Mass (Dry) of the Satellite Satellite is \u2264 1700 kg."]
[9.222947120666504, 9.477762222290039, "The Observation Target of the EUV Imager Imaging System is Plasmasphere."]
[4.732553482055664, 6.604682922363281, "The Frequencies of the Low Noise Amplifier Amplifier is L1 and L2."]
[7.6286492347717285, 7.622997760772705, "The Objectives of the ACE-FTS Instrument is Measure the vertical distribution of atmospheric trace gases, in particular the regional ozone budget, as well as temperature and pressure."]
[9.28808879852295, 3.815019369125366, "The Antenna Size of the DART Spacecraft is 4.5 m."]
[9.013545989990234, 2.4879298210144043, "The Image Bands of the Herschel Space Observatory is 70 \u00b5m (blue), 160 \u00b5m (green) and 250 \u00b5m (red)."]
[7.966220855712891, 4.487710475921631, "The Multispectral Resolution of the Resurs-P1 Imaging Satellite is 3-4 m."]
[8.062780380249023, 2.6514837741851807, "The Contact Date of the TerraSAR-X Satellite is June 19, 2007."]
[2.30794620513916, 4.443398952484131, "The Output Power of the Satellite Navigation Satellite is Equivalent to the light from a 60 watt lamp."]
[9.283510208129883, 10.04257869720459, "The Purpose of the PRIma (PR-Imager) Camera is Earth observation and to test the camera in space."]
[9.877756118774414, -0.729486882686615, "The Object Detection Limit of the NEOSSat Microsatellite is 20th V magnitude."]
[6.658756732940674, 9.144089698791504, "The Dimensions of the Instrument CEB (Common Electronics Box) is 120 mm x 300 mm x 250 mm."]
[7.857511043548584, 8.98211669921875, "The Wavelengths of the PACS and SPIRE Instruments is 250, 350 and 500 \u00b5m."]
[2.9459097385406494, 6.7346272468566895, "The Power of the S-band Transmitter Transmitter is 0.5 W."]
[6.708127021789551, 4.161260604858398, "The Function of the BRO-1 Satellite is Maritime monitoring."]
[9.640007972717285, 7.748281002044678, "The Electron Energy Ranges of the EPE Energetic Particle Experiment is 30-90 keV, 100-200 keV."]
[8.327383995056152, 4.585626602172852, "The Swath Width of the ALOS-3 Satellite is 50 km."]
[11.496224403381348, 0.8833066821098328, "The Rover Mass of the Tianwen-1 Probe is ~240 kg."]
[5.511406421661377, 3.215672492980957, "The Mission Goals of the Heinrich Hertz Satellite is See List."]
[7.546720027923584, 7.753827095031738, "The Manufacturer of the SOLSPC Radiometer is CNRS, France."]
[10.248846054077148, 1.0447336435317993, "The LTDN of the PRISMA Satellite is 1030 hours."]
[10.591303825378418, 3.2444515228271484, "The Communication Range of the SATTLA-2 PocketQube is Over 600 km."]
[3.5063014030456543, 6.6558837890625, "The Data Rate (max) of the MHX-2400 S-band Transmitter/Transceiver is 83 kbit/s."]
[7.974924564361572, 4.402474880218506, "The Spatial Resolution of the ICEYE-X1 Satellite is 10 m x 10 m."]
[6.276736259460449, 9.954371452331543, "The Mass of the FPU Focal Plane Unit is 16 kg."]
[10.452946662902832, 2.52453875541687, "The Operating Orbits of the MS-2 Minisatellite is Near-Earth orbits in the altitude range from 500 to 700 km."]
[1.8432810306549072, 3.998162269592285, "The Quantity of the Solar Panels Power Generation is 2."]
[2.327000617980957, 6.449732780456543, "The Latency of the ATL01 Reformatted Telemetry Data is 2 days."]
[6.070130825042725, 11.252753257751465, "The Approx. peak sensitivity altitude of the Channel 4 Sensor is Unknown."]
[10.4361572265625, 3.481966972351074, "The True Anomaly of the SMART-1 Satellite is 180.000\u00ba."]
[4.46701717376709, 4.627039909362793, "The Function of the IDHS and CNM Facilities is X-band payload data reception, processing and archiving/delivering the PRISMA data and products."]
[5.8201117515563965, 1.5987486839294434, "The Conference Presentation of the GOMX-1 Satellite is 4S (Small Satellites Systems and Services) Symposium."]
[8.796092987060547, 0.38916340470314026, "The Duration of the Experiment Space Station Experiment is Up to 4 months."]
[9.350004196166992, 7.923462390899658, "The Purpose of the FREND Neutron Detector is Fine-Resolution Epithermal Neutron Detector for ExoMars Project."]
[8.883261680603027, 3.719301700592041, "The Transfer Parameters of the LUMIO Satellite is Cj = 3.09."]
[5.756883144378662, 0.8712486028671265, "The Deployment Date of the NanoRacks CubeSat Deployer is March 11, 2015."]
[6.995110988616943, 1.0879780054092407, "The Reentry Date of the OCSE Satellite is March 5, 2001."]
[4.790421962738037, 0.8415378928184509, "The Contract Value of the JPSS-3 and -4 Satellite is $460 million."]
[5.034235000610352, 3.296264171600342, "The Project Management of the Power subsystem Satellite Subsystem is Osaka Prefecture University, Kagawa University, Keio University, Tokyo Metropolitan College, Osaka Prefecture College."]
[9.339569091796875, 1.9564316272735596, "The Closest Approach Time of the Rosetta Satellite is 18:10 CEST."]
[8.894675254821777, 3.61649751663208, "The Configuration of the MPO Satellite is Equipment panel perpendicular to radiator."]
[3.809197187423706, 6.3564453125, "The Delayed TM Playbacks of the Telemetry Data Transmission is Five complete during the visibility window."]
[9.434005737304688, 0.9426891803741455, "The Duration of the Satellite Orbit Orbit is Ten years."]
[10.56865119934082, 7.516626834869385, "The Material of the Platform Structure Satellite Component is Composite honeycomb aluminium panels."]
[8.621063232421875, 10.203009605407715, "The Image Capture of the EPIC European Photon Imaging Camera is Figure 81."]
[5.369588851928711, 2.7424139976501465, "The Development Authors of the CubeSats for Technology Maturation Satellite is Charles D. Norton, Steve A. Chien, Paula J. Pingree, David M. Rider, John Bellardo, James W. Cutler, Michael P. Pasciuto."]
[5.782232761383057, 2.7623233795166016, "The Owner of the WorldView-1 Satellite is Maxar Technologies Inc.."]
[3.8655014038085938, 5.687686920166016, "The Data Rate of the ALOS-3 Satellite is 800 Mbit/s."]
[7.381840705871582, 1.1214873790740967, "The Publication Date of the NICER Satellite is 14 August 2018."]
[7.316522121429443, 10.111921310424805, "The Development Team of the EnMAP Hyperspectral Imager Imaging Satellite is S. Hofer, H. J. Kaufmann, T. Stuffler, B. Penn\u00e9, G. Schreier, A. M\u00fcller, A. Eckardt, H. Bach, U. C. Benz, R. Haydn."]
[7.489067077636719, 3.3657166957855225, "The Attitude and Orbit Control System of the CHAMP Satellite is Unknown."]
[9.37486743927002, 0.5852971076965332, "The Design Life of the Landsat-7 Satellite is 5 years."]
[5.035271644592285, -2.371976613998413, "The Affiliation of the Stephane Dussy Engineer is Unknown."]
[11.706727981567383, -1.175649881362915, "The Payload Mass of the ADEOS spacecraft Satellite is 1300 kg."]
[11.122135162353516, 2.5187957286834717, "The Altitude of Front Heat Shield Release of the Schiaparelli Lander is About 7 km."]
[9.061349868774414, 4.8977179527282715, "The Attitude Stability of the Nanosatellite Satellite is Arc-Minute."]
[9.470351219177246, 4.867393493652344, "The Expected Initial Tumbling Rates of the Satellite Spacecraft is Less than 30\u00ba/s."]
[10.117537498474121, 4.924118995666504, "The Thruster Type of the Eutelsat 172B Satellite is Electric."]
[6.74484920501709, 4.318291187286377, "The Characteristics of the Data Products Satellite Data is High-accuracy, high spatial resolution, fast global coverage."]
[10.395859718322754, 4.322597503662109, "The \u0394V Decrease of the Bloostar Launch Vehicle is ~8%."]
[8.926487922668457, 10.449821472167969, "The Minimum Exposure Time of the Sensor Image Sensor is 10 \u00b5s."]
[7.135397911071777, 0.22915923595428467, "The Launch Year of the S3D Satellite is 2028."]
[3.9165637493133545, 6.775582790374756, "The Size of the Spacecraft Repeater Communication Device is 0.034 m3."]
[5.455092430114746, 3.448582649230957, "The Manufacturer of the TRXU Communication Subsystem is Space Quest."]
[7.433798789978027, 0.12345365434885025, "The Planned Launch Date of the SAOCOM-2B Satellite is 2026."]
[12.11887264251709, 2.1399853229522705, "The Mission Preparation Date of the REX-J Robot is June 5-12, 2011."]
[9.984959602355957, 7.961035251617432, "The Transverse Dimensions of the HXT-S Detector Modules is 465 mm x 392 mm."]
[8.286009788513184, 9.487282752990723, "The Objective of the Optical Payload Imaging System is Detection and quantitative analysis of HTE (High Temperature Events) like wildfires and volcanoes."]
[7.744133472442627, 7.196270942687988, "The Project Lead of the TEMPO Instrument is Kelly Chance from the Smithsonian Astrophysical Observatory (SAO)."]
[5.5133748054504395, 2.271371603012085, "The Increase in Observations of the SBSS-1 Satellite System is Fivefold."]
[7.250329971313477, 0.3617842197418213, "The Launch Date of the TEMPO Satellite is 7 April 2023."]
[7.35054874420166, 1.4801857471466064, "The Operation Extension Deadline of the Cluster Satellite Mission is October 1, 2010."]
[8.08915901184082, 5.1641764640808105, "The Electric Field Measurement of the GEOTAIL Satellite Satellite is Unknown."]
[2.274141311645508, 6.48065710067749, "The Latency of the ATL19 Mean Sea Surface (MSS) Data is 45 days from receipt of last data in product."]
[8.020010948181152, 2.490330219268799, "The Objectives of the Rosetta Mission Space Mission is 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."]
[9.506007194519043, 0.5439382791519165, "The Nominal Lifetime of the HY-2A Satellite is 3 years."]
[7.4033026695251465, 7.9166131019592285, "The Vertical Coverage of the Ozone Measurement Instrument Atmospheric Measurement Device is Tropopause height to 60 km."]
[5.670628070831299, 4.631725311279297, "The Ground Segment Platforms of the Argos/DCS Satellite System is Buoys, free-floating balloons, wildlife, remote weather stations."]
[7.581246852874756, 0.5840076208114624, "The Watch Start Date of the Space Station Satellite is June 15, 2010."]
[2.2490341663360596, 4.456679344177246, "The Payload Power of the Spacecraft Satellite is 40 W."]
[9.181863784790039, 4.107488632202148, "The Size of the MMS Satellite is The size of a baseball field."]
[7.860917568206787, 9.074573516845703, "The Wavelength Range (NIR) of the Sentinel-4/UVN Instrument is 750-775 nm."]
[9.625130653381348, 5.933709144592285, "The Roll Maneuver Capability of the ADCS Attitude Determination and Control Subsystem is \u00b135\u00ba."]
[7.942436218261719, 6.917266368865967, "The Overpass Duration of the ARC Calibration System is Less than 1 second."]
[6.846101760864258, 5.551421642303467, "The URL of the Global Ocean Observing System (GOOS) Ocean Observing System is http://www.gosic.org/goos/Argo-data-access.htm."]
[11.535395622253418, -1.3016098737716675, "The Mass of the ICEYE-X1 Satellite is <100 kg."]
[6.0791239738464355, 9.635655403137207, "The Mass of the Field Measurement Device Sensor is < 0.1 kg."]
[9.38379955291748, 0.511351466178894, "The Design Life of the EROS-A Satellite is 4 years."]
[8.683794021606445, 4.91578483581543, "The Off-Track Look Capability of the NEMO-AM Satellite is 30\u00ba."]
[9.394099235534668, 8.759490966796875, "The Mirror Material of the PAN Camera Imaging Device is Zerodur glass."]
[6.7267913818359375, 0.7544227242469788, "The Launch Date of the NigeriaSat-2 Satellite is November 2011."]
[10.156607627868652, 2.9145731925964355, "The Orbital Altitude of the IceCube Satellite is Approximately 400 km."]
[10.140181541442871, 5.178800106048584, "The Pressure and Temperature Monitoring of the Propulsion System Satellite Component is Inside the plenum."]
[7.836260795593262, 8.978900909423828, "The Measurement Range of the FLEX Mission is 500\u2013600 nm."]
[10.775359153747559, 1.9120280742645264, "The Ascending Node Crossing Time Differences of the Swarm-A and Swarm-C Satellite Constellation is Between 4 and 10 seconds."]
[9.09488582611084, 8.63403606414795, "The Construction Material of the LORRI Imaging Instrument is Silicon carbide."]
[2.6728098392486572, 5.354117393493652, "The Power Consumption of the OBC-Combo On-board Computer is 10 W."]
[9.345513343811035, 9.070164680480957, "The Importance of the Full Width at Half Maximum (FWHM) Parameter is Critical for telescope performance."]
[10.28464412689209, 4.929821491241455, "The Thruster Configuration of the GPIM Propulsion System is 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."]
[6.361682891845703, 9.956772804260254, "The Mass of the Imager Imaging System is ~130 kg."]
[4.5713982582092285, 3.9840753078460693, "The Avionics Architecture of the CHEOPS Satellite is OBC, RIU, two redundant 1553 buses."]
[7.483401775360107, 8.939574241638184, "The Spatial Resolution of the Spectrometer Instrument is 4.5 km x 9 km."]
[7.52885627746582, 6.000781536102295, "The Objective 2 of the EMIT Mission is Predict how future climate scenarios might change the amount and type of mineral dust emitted into the Earth\u2019s atmosphere."]
[7.4569268226623535, 1.059933066368103, "The Mission Date of the NASA's First Mission to the Trojan Asteroids Spacecraft is Unknown."]
[6.352691650390625, 5.0166778564453125, "The SAR Bands of the NISAR Earth Observation Satellite is L and S-band."]
[8.532848358154297, 1.0302045345306396, "The Anniversary Date of the LRO Orbiter is June 18, 2014."]
[8.072612762451172, 1.378186583518982, "The First Perihelion of the Solar Orbiter Satellite is 15 June."]
[5.990790367126465, 9.597433090209961, "The Mass of the LAP Instrument is 6.3 kg."]
[12.060647964477539, 3.2208468914031982, "The Orbit Inclination of the Beijing-3B Satellite is 97.94\u00b0."]
[7.357770919799805, 4.556127071380615, "The Imaging System of the NewSat Satellite is Hyperspectral imagery."]
[7.467294692993164, 9.957096099853516, "The Conference Presentation of the EarthCARE Multispectral Imager Imaging System is ICSO 2010 (International Conference on Space Optics), Rhodes Island, Greece, Oct. 4-8, 2010."]
[9.385427474975586, 4.9510393142700195, "The Drift Rate of the IRS-1C and IRS-1D Spacecraft is 3.6 x 10-4 \u00ba/s."]
[11.862967491149902, 1.0084437131881714, "The Sample Collection of the Chang'e-5 Lunar Probe is Completed."]
[7.423818111419678, 7.986191272735596, "The Horizontal Cell Size of the Ozone Measurement Instrument Atmospheric Measurement Device is 50 km @ nadir."]
[6.697648048400879, 0.07215913385152817, "The Arrival Date at RRSW of the MSV bus and payloads Satellite is May 2013."]
[4.79748010635376, 0.8752012848854065, "The Cost per Flight of the Super Strypi Launch System is $15 million."]
[1.5306966304779053, 4.816329479217529, "The Operational Input Voltage Range of the DC-DC converter Power Converter is 22 to 34 V."]
[8.744531631469727, 5.294456958770752, "The Platform Fixings of the Hard Stack Satellite Assembly is Torqued to correct levels."]
[7.547296524047852, 6.241810321807861, "The Data Collection of the ISS-EMIT Instrument is Composition of minerals that become airborne dust."]
[8.586970329284668, 9.38535213470459, "The Sensitivity of the NIRSpec MIRI Optical Instrument is 3.4 x 10 -21  Wm -2  (9.2 \u00b5m, \u03c4 i =10,000 s, R=2400)."]
[8.607982635498047, 1.7349776029586792, "The Launch Date of the JWST James Webb Space Telescope is 2019."]
[4.621579647064209, 0.22177886962890625, "The Number of Satellites of the OneWeb Low-Earth-Orbit Broadband Venture is 648."]
[7.778692722320557, 8.531105995178223, "The IR Spectral Range / Bandwidth of the SOLSPEC-SOLAR Spectrometer is 650-3080/8."]
[5.102282524108887, 2.1666908264160156, "The Number of Koranic schools of the University of Sankore Educational Institution is 180."]
[4.432363033294678, 2.9941489696502686, "The PRN of the GSAT-0205 Satellite is 24."]
[12.090619087219238, 3.299373149871826, "The Inclination of the ANUSat Satellite is 41\u00ba."]
[5.671381950378418, 2.9046950340270996, "The Manufacturer of the exactView-1 Satellite is SSTL."]
[12.014129638671875, 3.263559103012085, "The Orbit Inclination of the ALMASat-1 Satellite is 69.5\u00ba."]
[6.7922234535217285, 3.2223830223083496, "The Ship Detection of the RADARSAT Constellation Mission Satellite Mission is Operational."]
[5.348489761352539, 3.974384069442749, "The Data Source of the Ursa Space Systems Space Data Analytics Company is Space-based data from satellites."]
[8.071660995483398, 7.807458400726318, "The Sensitivity of the SCM Sensor is 3000 nT."]
[4.2154693603515625, 6.557635307312012, "The Downlink Frequency of the Cadet-U UHF radio RF Communication Device is 468 MHz."]
[7.33171272277832, 8.87368106842041, "The Temporal Decorrelation of the Interferometric Mode Observation Mode is Within the requirements."]
[5.44173002243042, 4.104389190673828, "The Purpose of the Emergency Egress System Safety System is Provide quick escape in the unlikely event of an emergency."]
[7.210598945617676, 5.114006519317627, "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."]
[6.320675849914551, 2.987074613571167, "The Location of the Lockheed Martin Solar and Astrophysics Lab Lab is USA."]
[10.422980308532715, 6.138562202453613, "The Developer of the RUBI Fluid Science Experiment is Airbus."]
[1.505290150642395, 4.896321773529053, "The Input Voltage of the Instrument Power Unit Power Converter is 28 V DC."]
[6.9296746253967285, 0.1359812170267105, "The End of Life Date of the IRS-P6 Satellite is 07 Dec 2013."]
[10.269309997558594, -0.8465887904167175, "The Mass of the Tsubame Microsatellite is 49 kg."]
[9.466103553771973, -0.7377617359161377, "The Decommission Date of the Carbonite-1 Microsatellite is November 2018."]
[7.244117259979248, 3.0507915019989014, "The Mission Status of the CAPSTONE Satellite is Unknown."]
[6.7169060707092285, 7.173832893371582, "The URL of the LIDAR Instrument is http://www.hou.usra.edu/meetings/lpsc2015/pdf/1863.pdf."]
[9.562233924865723, 9.186823844909668, "The Optics of the Imager Imaging System is TMA telescope with an aperture diameter of 1.1 m, focal length = 13.3 m, f/12."]
[9.286823272705078, 10.254704475402832, "The Focal length of the 16 mm camera Camera is 16 mm."]
[5.484496116638184, 3.6884326934814453, "The Qualification Approach of the Curtiss Wright Manufacturer is Space COTS Qualification."]
[11.399158477783203, 4.211972713470459, "The Location of Exoplanets of the WFIRST Telescope is Between three and 10 times Earth\u2019s distance from the Sun."]
[9.145648002624512, 4.217796325683594, "The Size of the Satellite Bus is 954 mm x 954 mm x 1000 mm."]
[6.671620845794678, 0.7190574407577515, "The Conference Date of the Meteosat Second Generation (MSG) Radiometer/Imager Satellite is May 16-20, 2016."]
[6.964766502380371, 0.4785018861293793, "The Launch Date of the SPOT-5 Satellite is 04 May 2002."]
[3.5999627113342285, 3.5081121921539307, "The Orbit of the CICERO-4 Satellite is 500 km orbit."]
[3.7779581546783447, 5.6575140953063965, "The Data Generation Rate of the Artemis I mission Space Mission is About 100 MB/s."]
[5.4259209632873535, 4.80166482925415, "The Payload Data System of the KazSTSAT Satellite is Delivered."]
[7.357475280761719, 2.330672025680542, "The URL of the First Arab mission to Mars Satellite is https://www.marsdaily.com/reports/First_Arab_mission_to_Mars_designed_to_inspire_youth_999.html."]
[6.832066535949707, 4.907347679138184, "The Atmospheric Constituents of the Sentinel-5 Satellite is Ozone, nitrogen dioxide, sulphur dioxide, carbon monoxide, methane, formaldehyde, and aerosol properties."]
[6.985640048980713, -0.06250885128974915, "The End of Life Date of the Satellite EO is 30 Sep 2023."]
[5.541844367980957, 5.942441463470459, "The Ka-band Advantages of the SARAL/AltiKa Satellite is Reduction of ionosphere effects, smaller footprint, better horizontal resolution, higher vertical resolution."]
[1.112690806388855, 4.213221073150635, "The Type of the Power Storage Battery is NiCd."]
[9.036439895629883, 9.188627243041992, "The Angle Resolution of the FSS Photodiode Detector is Up to 0.03\u00ba."]
[5.013326644897461, 1.7815684080123901, "The Nominal Eclipses of the Cluster Satellite Constellation is 12."]
[11.592693328857422, 6.273197174072266, "The First Light Image Capture Date of the MAXI X-ray Telescope is Aug. 18, 2009."]
[4.266878128051758, 6.618463039398193, "The Data Collection Frequency of the DCS Data Collection System is UHF (~401 MHz)."]
[8.86912727355957, 5.258121013641357, "The Impact of the Attitude Control System Satellite System is Hindered the performance of the GPS receiver."]
[4.956920623779297, 8.804840087890625, "The Number of Alerts Per Day of the LSST Large Synoptic Survey Telescope is Thousands."]
[10.030728340148926, -0.767087459564209, "The Frame Size of the NIUSAT Nanosatellite is 50 km x 50 km."]
[6.754598617553711, 4.336036205291748, "The Program of the CRISTAL Satellite is Copernicus Expansion program."]
[7.024919033050537, 4.663972854614258, "The Navigation Technology of the ATV-5 Spacecraft is Cooperative rendezvous technology."]
[4.758459091186523, 5.688322067260742, "The Detector of the skCUBE Satellite is Very-low-frequency radio waves."]
[9.656118392944336, 1.5472092628479004, "The Repeat Cycle of the Optsat-3000 Satellite is 2 days."]
[10.821599960327148, 3.185162305831909, "The Lunar Orbit Distance of the Probes Spacecraft is Approximately 400,000 km."]
[11.170750617980957, 6.802194595336914, "The Operating Wavelengths of the X-ray Navigation Navigation System is Ground cannot be seen."]
[12.12407112121582, 3.2868599891662598, "The Inclination of the WorldView-3 Satellite is 98\u00ba."]
[7.791424751281738, 9.698119163513184, "The Spectral Band of the Band Photometers Photometer is 650-740 nm."]
[4.190069675445557, 3.7650206089019775, "The Transmitted Information of the NorAIS-2 Receiver AIS Receiver is Identity, position, speed and heading."]
[4.719321250915527, 7.3558807373046875, "The Beam size of the Millimeterwave receiver Receiver is 22 arcmin."]
[4.8467512130737305, 0.9441409707069397, "The Development Cost of the Lucy Discovery Program Mission is Approximately $450 million."]
[7.026381015777588, -0.010404570959508419, "The End of Life Date of the SVOM Satellite is Planned for 3 Years."]
[8.175479888916016, 3.6401944160461426, "The Shape Options of the SPIDER Telescope is Squares to hexagons and even conformal concepts."]
[6.975099563598633, 1.7206780910491943, "The Information Date of the Swarm Satellite is June 22, 2017."]
[8.71678638458252, 3.2085039615631104, "The Spacecraft Body Shape of the GOCE Satellite is Aerodynamic."]
[5.3488383293151855, 9.27078628540039, "The Power Consumption of the SEIS Instrument Seismometer is Up to 8.5 W."]
[7.854798316955566, 9.025002479553223, "The Spectral Range of the VIS Spectrometer is 350 - 500 nm."]
[2.206127166748047, 6.519096374511719, "The Latency of the ATL03 Global Geolocated Photon Data Data is 21 days."]
[8.758270263671875, 7.887742042541504, "The Entrance Aperture Location of the INMS Ion-neutral Mass Spectrometer is +Y 2U face."]
[6.926167011260986, 0.9374387860298157, "The Launch Date of the NPP Satellite is October 28, 2011."]
[8.31363582611084, 1.4049819707870483, "The Date of the Wolf Awakens at Night Image is 8 January 2022."]
[5.9450578689575195, 6.31607723236084, "The Single Pol Swath Width of the SAR Processor Data Processor is 350 km."]
[8.936352729797363, 3.7512474060058594, "The Formation Shape of the MMS Satellite Formation is Tight pyramid."]
[7.789754867553711, 1.4316691160202026, "The Date of the Floods Swamp Bangladesh Natural Event is 24 June 2022."]
[9.774775505065918, 8.799633026123047, "The Diameter of the RRA RetroReflector Array is 60 mm."]
[5.651575088500977, 4.074248790740967, "The MCS of the FOS Satellite is Multi-domain distributed system."]
[10.794919967651367, 5.684384346008301, "The Observation Focus of the Solar Dynamics Observatory Satellite is Solar flares and sunquakes."]
[7.132731914520264, 9.742749214172363, "The Wavelength Range of the Visible Spectral Band Spectral Band is 0.55 - 1.05 \u00b5m."]
[7.71260929107666, 9.850573539733887, "The View of the VNIR Calibration is Spectralon plate at the poles."]
[7.602845191955566, 0.4006500244140625, "The Launch Date of the Meteor-M2-2 Satellite is 5 July 2019."]
[5.891726493835449, 6.734396934509277, "The Ground Cross-Track Range Resolution of the KaRIn Radar is 70 m to 10 m."]
[6.848913669586182, 1.4218230247497559, "The Presentation Date of the Small Satellite Constellation for Environment and Disaster Monitoring and Forecasting Satellite Constellation is Sept. 14-16, 2009."]
[9.329794883728027, 4.197831153869629, "The Solar Arrays Length of the BepiColombo Spacecraft is 15 m."]
[7.285139083862305, 9.32013988494873, "The Spectral Range (Band 1) of the PanMUX Instrument is 0.51-0.85 \u00b5m."]
[4.6075310707092285, 0.21114392578601837, "The Total Fleet Size of the OneWeb Satellite Constellation is 648."]
[6.4321088790893555, -0.6971694827079773, "The Interoperable Signals of the QZS Satellite is L1C, L1-C/A, L2C, L5."]
[7.727197647094727, 5.882718086242676, "The Lunar Calibration Method of the SeaWiFS Satellite is S/C maneuver to view the moon during the nighttime portion of an orbit."]
[7.29176139831543, 0.5191737413406372, "The Operation Start Date of the SAMPEX Satellite is Before 1997."]
[1.7909561395645142, 5.248583793640137, "The Supply Voltage of the Myriad RF board RF Board is 5 V."]
[7.784088134765625, 0.2419232577085495, "The Original Launch Date of the Crew-1 Commercial Crew Mission is Oct. 31."]
[7.2323527336120605, 5.609338283538818, "The Effect on Marine Ecosystem of the Ocean Acidification Environmental Phenomenon is Potential damaging knock-on effects."]
[11.262789726257324, 6.7289228439331055, "The Technology Objective of the NICER/SEXTANT Instrument is Demonstrate celestial-based XNAV ( X-ray Navigation)."]
[8.439831733703613, 4.662882328033447, "The Environment of the Cluster Satellite is Magnetosheath."]
[7.800844192504883, 9.279972076416016, "The Resolution of the AEISS-A Instrument is 0.5 m for panchromatic imagery."]
[6.073712348937988, 2.8980295658111572, "The Purpose of the Moonlight Lunar Telecommunications and Navigation Satellite Network is To create a lasting lunar link to enable sustainable space exploration."]
[5.021214962005615, 4.627363204956055, "The Operational Modes of the Ground Station Ground Station is Command and Control (C2) and UGS (Unattended Ground Sensor)."]
[9.180031776428223, 10.14406681060791, "The Quantity of Cameras of the Earth Observation Compartment Compartment is 3."]
[10.375224113464355, 5.678050518035889, "The Tether Angle Sensor of the ATEx Tether Experiment is Triggered the jettison mechanism."]
[5.9174723625183105, 1.701709270477295, "The Launch Site of the HTV Spacecraft is Tanegashima Space Center."]
[3.9389331340789795, 2.2953710556030273, "The Sail Surface Area of the Spacecraft 3U CubeSat is 10 m^2."]
[6.001883029937744, 3.057624340057373, "The Number of Universities of the ESEO Satellite is 13."]
[6.795535087585449, 1.1641846895217896, "The Launch Date of the GIOVE-B Satellite is April 27, 2008."]
[9.225438117980957, 10.048468589782715, "The Earth Imaging Mode of the Imaging System Camera is Scheduled snapshot basis."]
[11.375683784484863, 4.545939922332764, "The Oxygen Temperature of the Sun's Lower Atmosphere Celestial Body is 320,000\u00baC."]
[8.650208473205566, 4.876627445220947, "The Ground Sampling Distance of the NEMO-AM Satellite is Approximately 42 m."]
[7.015513896942139, 4.450957775115967, "The Instrument Type of the Myriade/AstroSat-100 Satellite is High resolution optical imagers, Other, Atmospheric chemistry, Communications, Data collection, Lightning sensors."]
[12.134082794189453, 3.358206033706665, "The Inclination of the KOMPSAT-6 Satellite is 97.42\u00ba."]
[7.138725280761719, 8.342667579650879, "The No of bands/channels of the TOU Total Ozone Unit is 6."]
[9.06742000579834, 8.009892463684082, "The Geometric Factor of the Particle Detector Instrument is 0.0085 cm 2  sr."]
[12.146951675415039, 3.308339834213257, "The Inclination of the Tatiana-2 Satellite is 98.8\u00ba."]
[9.234970092773438, 8.04116439819336, "The Geometric Factor of the Particle Detector Instrument is 0.0442 cm 2  sr."]
[8.146507263183594, 4.964920520782471, "The Measurement Range of the Cluster S/C Satellite is DC to 10 Hz."]
[7.419615268707275, 2.5475869178771973, "The URL of the Solar Dynamics Observatory Satellite is http://science.nasa.gov/science-news/science-at-nasa/2010/05feb_sdo/."]
[7.583745956420898, 8.767128944396973, "The Bandpass of the CIPS Instrument is UV bandpass of 265 nm (\u00b15 nm)."]
[4.81343936920166, 0.03052600845694542, "The Builder of the OneWeb Teleport is Telstra."]
[10.08740234375, 1.5892417430877686, "The Primary Orbit Period of the Didymos Binary System is 11.9 hours."]
[7.103686809539795, 8.897195816040039, "The Instrument Swath of the Optsat-3000 Satellite is 27 km x 27 km."]
[8.448762893676758, 7.1824049949646, "The Measurement Range of the Field Measurement Device Sensor is \u00b1 64 000 nT."]
[9.411747932434082, 0.6817758083343506, "The Expected Orbit Lifespan of the Meteosat Satellites Geostationary Satellites is At least seven years."]
[7.785945415496826, 4.25341796875, "The Image Resolution of the EROS-B Satellite is Up to 50 cm."]
[6.287712097167969, 5.115878105163574, "The Instrument of the Odin Satellite is SMR (Sub-Millimeter Radiometer)."]
[7.603051662445068, 0.5447790622711182, "The Launch Year of the DSAC Demonstration Unit is 2015."]
[7.8926544189453125, 9.199431419372559, "The Wavelength Range of the HSC Spectrometer Spectrometer is 450-900 nm."]
[5.364883899688721, 4.635437488555908, "The URL of the Argos-3 Data Collection and Location System is https://web.archive.org/web/20110814035457/http://www.argos-system.org/html/system/enhancements_en.html."]
[1.8071626424789429, 4.797069072723389, "The Voltage of the Spacecraft Bus Spacecraft Component is Monitored."]
[6.5455851554870605, 0.5975186228752136, "The First Signal Received of the Robusta Satellite is Feb. 16, 2012."]
[7.219998836517334, 3.142893075942993, "The Mission Status of the BRITE-Austria Satellite is Unknown."]
[9.65432071685791, 5.962831497192383, "The Power Savings of the ADCS Attitude Determination and Control Subsystem is Individual OBCs can be powered off without the operation of the others."]
[3.5809099674224854, 6.466402530670166, "The Required Eb/No of the Unit Communication System is 5 dB."]
[7.195359706878662, 1.031532645225525, "The Launch Date of the AgilSpace GeoPortal E-commerce Hub is May 31, 2016."]
[5.69907283782959, 9.252779960632324, "The Power of the HI-SCALE Instrument is 4.0 W."]
[8.031479835510254, 7.150268077850342, "The Function of the Machine Learning Algorithm Calibration Tool is Compare specific structures across the wavelengths and strengthen its assessments."]
[3.138442277908325, 5.376645565032959, "The Microcontroller/Processors of the SSR Solid State Recorder is None."]
[5.512110233306885, 3.24141526222229, "The Spacecraft Bus Type of the QuickBird-2 Satellite is BCP-2000."]
[10.993939399719238, 5.0045390129089355, "The Predictability of the Solar Energetic Particles Space Weather Phenomenon is Extraordinarily hard to predict."]
[9.285565376281738, 10.204939842224121, "The Lens Focal Length of the Camera System Sensor is 16 mm."]
[4.326211929321289, 4.835817813873291, "The Command Type of the TDP Commanding Process is Time tagged commands (TTC)."]
[7.72355318069458, 7.6220855712890625, "The Solar Total Irradiance Variability of the SOVA Experiment is Detected."]
[3.8311684131622314, 4.47641134262085, "The Programming Space of the SCP Spacecraft Process Controller is 64K words."]
[6.398171901702881, 5.802613258361816, "The L-band Radar Frequency of the SMAP Satellite is 1.26 GHz."]
[8.469228744506836, 5.374668598175049, "The Pointing Accuracy of the Antenna Antenna is 0.1\u00ba."]
[7.831769943237305, 9.80703353881836, "The Spatial resolution at nadir of the MERSI Medium Resolution Spectral Imager is 1.1/0.250 km."]
[10.268386840820312, 2.9149580001831055, "The Altitude of the CBERS-2B Satellite is 778 km."]
[3.949852228164673, 4.4146504402160645, "The Operating System of the OBC On-Board Computer is RTEMS (Real-Time Executive for Multiprocessor Systems)."]
[7.126906394958496, 3.628793954849243, "The Manufacturing Facility of the Pelican Satellite Constellation is San Francisco."]
[6.79451322555542, -0.014410831965506077, "The Fourth Flight Date of the MEPSI Satellite is July 4-17, 2006."]
[6.17933988571167, 4.900561332702637, "The Instruments of the MOMS Satellite is GPS receiver."]
[8.64692497253418, 9.105862617492676, "The Slit Width of the Instrument Spectrometer is 4 arcmin."]
[8.151700019836426, 9.85859203338623, "The Spectral Resolution of the MSASI Imager is 80,000 (\u03bb/\u0394\u03bb)."]
[9.588542938232422, 6.048027515411377, "The Sensors of the Coarse ADCS ADCS System is Sun sensors and magnetometers."]
[7.466256618499756, 4.259322166442871, "The Nadir-pointing face of the PSSCT-2 Satellite is +Z face."]
[7.070121765136719, 7.068197250366211, "The Limb Sounder of the EnviSat Satellite is MIPAS."]
[6.668399333953857, 3.3870272636413574, "The Parameters of the Optional Payloads Payloads is Mass, Power, Data Requirements."]
[9.214264869689941, 4.159343242645264, "The Size of the Spacecraft Satellite is \u00d8 1,500 x 1,940 mm height."]
[9.408422470092773, 0.9744328260421753, "The Age of the Atmospheric Chemistry Experiment (ACE) satellite Satellite is 15 years."]
[8.363157272338867, 7.318853855133057, "The Scheduled Launch of the Space Comb Spectroscopy Setup is 2017."]
[6.028329849243164, 6.289309024810791, "The Measurement Accuracy of the SAR Instrument SAR Instrument is 3.5 cm/year, 1.6 cm/year."]
[7.751893520355225, 2.9567179679870605, "The Launch Date of the CartoSat-2B Satellite is July 21, 2010."]
[4.7595062255859375, 7.374972343444824, "The Beam size of the Submillimeterwave receiver Receiver is 7 arcmin."]
[2.994077682495117, 6.584834098815918, "The Power of the Transmitters Communication Device is 40 W."]
[3.338775396347046, 5.5426506996154785, "The Input Buffer Size of the Transmission Module FPGA Module is 1115 bytes."]
[11.63575553894043, -1.2357650995254517, "The Mass of the BLITS Satellite is 7.5 kg."]
[10.482086181640625, 8.436379432678223, "The Spectral Range of the HeII Coronagraph Coronagraph is 295-315 \u00c5."]
[3.2212038040161133, 5.891904830932617, "The Data Processing Time of the CPOM Data Processing Center is Within two days of acquisition."]
[5.219533443450928, 4.624218463897705, "The Location of the Ground Station Ground Segment is ITU."]
[4.261127948760986, 5.763223648071289, "The Downlink Transmission of the L-band telemetry subassembly Telemetry Device is Image data."]
[9.330896377563477, 0.5555482506752014, "The Operational Duration of the Jason-3 Satellite is More than 25 years."]
[7.237080097198486, 2.9490678310394287, "The Mission Status of the Philae Spacecraft is Unknown."]
[5.401481628417969, 0.2847965657711029, "The Perimeter Length of the Calf Canyon-Hermits Peak fire Fire is 50 miles (80 km)."]
[2.9547204971313477, 6.711824417114258, "The S-band TxRx Power of the RF communications Communication System is 5W."]
[9.50422191619873, 0.6241464614868164, "The Mission Lifetime of the Platform Satellite is ~ 15 years."]
[4.493223667144775, 5.634069919586182, "The Function of the PDD Payload Data-Downlink is Payload data acquisition and high rate downlink in Ka-band."]
[12.115189552307129, 3.3322603702545166, "The Inclination of the Bion-M1 Spacecraft is 64.9\u00ba."]
[8.289381980895996, 9.645698547363281, "The Detector Array of the SCIAMACHY Spectrometer is 1024-pixel."]
[6.464216232299805, 4.899627208709717, "The Instrument of the Sentinel-6 Michael Freilich Satellite is GNSS-RO."]
[0.9000057578086853, 4.208623886108398, "The Capacity of the BAT Battery is 50 Ah."]
[6.9306840896606445, 4.9550275802612305, "The Nitrogen Dioxide Emission Reduction of the Copernicus Sentinel-5P Satellite is Around 40% over Chinese cities."]
[3.2914960384368896, 5.886620998382568, "The Listening Duration of the CPT Data Processing System is Entire transaction duration."]
[10.505134582519531, 2.4489054679870605, "The Perigee (km) of the Intercosmos- Bulgaria 1300 (Intercosmos-22) Satellite is 825."]
[5.348681449890137, 2.709033966064453, "The Developer of the skCube 1U CubeSat is SOSA (Slovak Organization for Space Activities ) at the University of Zilina."]
[6.085529804229736, 6.243812561035156, "The Function of the Dual-Frequency Synthetic Aperture Radar (DF-SAR) Synthetic Aperture Radar is Studying planetary surfaces and subsurface."]
[7.98001766204834, 9.096491813659668, "The Spectral Band of the Instrument Spectrometer is TIR."]
[3.1926770210266113, 4.189826488494873, "The HSTX of the IOD-1 GEMS Satellite is CPUT HSTX (High-Speed S-Band Transmitter) with SANT (S-band Patch Antenna)."]
[3.786877155303955, 6.211638927459717, "The Data Rate of the SIOS Optical Link Demonstration Board Technology Demonstration Board is 1 Mbit/s."]
[7.651731491088867, 7.836587905883789, "The XY Accuracy of the Planimetric Accuracy Assessment Assessment is <0.2 m."]
[4.4111809730529785, 6.190948963165283, "The Frequency Band of the S-band system Communication System is S-band."]
[5.094289302825928, 6.97972297668457, "The IF Bandwidth (MHz) of the Antenna Reflector is 400."]
[9.382078170776367, 4.037083625793457, "The Size of the Lunar Flashlight CubeSat is About the size of a briefcase."]
[7.099541187286377, 3.1537277698516846, "The Telemetry of the YES Satellite is Not Switched On."]
[8.30325698852539, 7.978535175323486, "The Sensor Type of the RPA Retarding Potential Analyzer is Planar sensor with a circular aperture."]
[3.981079578399658, 4.357815265655518, "The Antennas of the ESPA Ring Interface is 2 S-band omni antennas, and 2 medium-gain horns."]
[7.308252334594727, 2.4339237213134766, "The Image Credit of the RISESat Satellite is RISESat consortium."]
[6.978006839752197, 4.450778961181641, "The Cross Correlation Validation of the Image Processing Facility Facility is Global Landsat Survey GLS 2000 cloud free dataset."]
[7.817478179931641, 8.595308303833008, "The Movement Between Observations of the SCIAMACHY Spectrometer is About 1000 km."]
[5.605459213256836, 4.097143650054932, "The Ground Segment Operation of the Helios-2 Satellite is Image acquisition, priority discussion, transmission of plans, satellite control, image processing."]
[4.875953197479248, 7.531574726104736, "The Energy of the X-band Band is 42 \u00b5eV."]
[8.305649757385254, 8.500321388244629, "The Location of the VIS Unit is Payload Module."]
[3.604710340499878, 6.559615612030029, "The Data Rate of the VHF Transmitter Radio Transmitter is 64 kbit/s."]
[5.895567417144775, 6.454223155975342, "The Center Radar Frequency of the SAR-RCM Synthetic Aperture Radar is 5.405 GHz."]
[8.706558227539062, 0.1493140608072281, "The Program of the Skylab-1 Space Station is Apollo Applications Program (AAP)."]
[3.8366379737854004, 4.296878814697266, "The Number of Libraries of the C&DH Subsystem Command and Data Handling is 8."]
[5.321402072906494, 2.5072734355926514, "The Affiliation of the OSCAR-QUBE Team is Hasselt University (Belgium)."]
[2.343903064727783, 3.911144971847534, "The Solar Array Efficiency of the PARASOL microsatellite Satellite is 26%."]
[9.344344139099121, -0.6700701713562012, "The Presentation Location of the SERB Nanosatellite is Guadalajara, Mexico."]
[7.180666923522949, 5.132111072540283, "The Emissions Measurement of the GHGSat-D Satellite is Carbon dioxide and methane."]
[4.972960472106934, 1.9090296030044556, "The Number of Satellites of the Swarm Satellite Constellation is Three."]
[3.795060157775879, 4.380858421325684, "The Interface Protocol of the DHU Data Handling Unit is 1553 link."]
[7.760505676269531, 7.972357273101807, "The Relative Semi-Diameter Precision of the Instrument Optical Instrument is Better than 1 marcsec."]
[1.7285051345825195, 4.130538463592529, "The Cell Efficiency of the Solar Array Power Generation is 28.7%."]
[8.458975791931152, 11.074345588684082, "The SNR of the Eastman Kodak KLI14403 linear CCD sensor Sensor is > 100."]
[9.992193222045898, 1.600053310394287, "The Orbit Period of the Satellite Imaging Satellite is 97 minutes."]
[6.701292991638184, 3.029343843460083, "The Version of the Alexander, Graham, Bell PhoneSats is 1.0, 1.0, 2.0 \u03b2."]
[5.847048759460449, 8.579800605773926, "The Spectral range of the MWHS Microwave Humidity Sounder is 150-183 GHz."]
[4.144334316253662, 7.255725860595703, "The Mass of the X-band Transmitter Transmitter is 3.25 kg."]
[7.7811689376831055, 3.210963726043701, "The Number of Verified Fragments of the DebriSat project Satellite is Close to 3,000."]
[5.9293904304504395, 3.8584420680999756, "The Host of the Bartolomeo Platform is ESA."]
[5.424766540527344, 3.818936586380005, "The Responsibilities of the SC Science Center is Scientific experimental plan proposal, high-level data products generation, research and application functions organization."]
[9.48425579071045, 8.61577320098877, "The Type of the OTA Telescope Component is 50 cm aperture Gregorian telescope with a collimating lens unit and an active tip-tilt mirror for image-stabilization."]
[7.026820659637451, 2.51686954498291, "The URL of the MicroMAS Project Satellite is http://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=1015&context=smallsat."]
[6.435731887817383, 4.6626434326171875, "The Purpose of the FY-3 (FengYun-3) Satellite is Cloud profile and rain radars."]
[8.338958740234375, 10.064496040344238, "The Detector Size of the MSI-0 and MSI-1 MSI Instruments is 1024 x 1024 pixels."]
[2.1244354248046875, 3.8970019817352295, "The Solar Panel Fixing Tool of the Skylab Space Station is Pair of wire cutters at the end of a 8 m long pole."]
[3.555030345916748, 6.4945292472839355, "The Margin of the Unit Communication System is 2.52 dB."]
[7.313565254211426, 1.3317257165908813, "The Mission End Date of the Triana Satellite is Unknown."]
[6.038825511932373, 2.654603958129883, "The Manufacturer of the STPSat-1 Satellite is Comtech-AeroAstro Inc.."]
[10.378331184387207, 9.666866302490234, "The Acquisition Date of the Iris Satellite is January 15, 2016."]
[7.574169635772705, 7.080281734466553, "The Function of the GIADA Instrument is Grain Impact Analyser and Dust Accumulator."]
[5.155376434326172, 4.266330242156982, "The Function of the EGS Ground System is Run from any Space Operations Center and work with the Air Force Satellite Control Network or Universal Space Network ground stations."]
[11.292523384094238, 4.262428283691406, "The Number of Lowest-Mass, Tiniest, and Dimmest Cluster Members' Rotation Rates Measured of the Kepler Telescope is About 500."]
[7.983572483062744, 10.031634330749512, "The Swath Width of the PMC Imager is 69 km."]
[10.526670455932617, -1.0889006853103638, "The Construction and Temperature Control System Mass of the Microsatellite Satellite is 9.3 kg."]
[10.748950958251953, 7.3245768547058105, "The Solar X-ray Flux Level of the XRS instrumentation Instrumentation is A0.3."]
[9.707657814025879, 1.2942298650741577, "The Observation Duration of the Observation Region Satellite is One year."]
[8.562732696533203, 5.222195625305176, "The Pointing Accuracy of the CeREs Satellite is Exceeds mission requirements."]
[6.999387264251709, 4.2892560958862305, "The Measurement Category of the CAS500 Satellite is Multi-purpose imagery (land)."]
[9.138335227966309, 10.581015586853027, "The Maximum Frame Rate of the PamCam Panoramic Camera is Up to 27 images per second."]
[11.65009593963623, -1.3031845092773438, "The On-orbit Mass of the INSAT-2A/2B Satellite is 911 kg."]
[10.116386413574219, 1.5640119314193726, "The Orbit Period of the HY-2A Satellite is 104.5 minutes."]
[3.8188390731811523, 4.29993200302124, "The Number of Sub-Processes of the EMOC Process is Five."]
[8.532984733581543, 9.80062198638916, "The Imaging Modes of the Imager Imaging System is Panchromatic (Pan), Multispectral (MS)."]
[5.2471208572387695, 2.272611141204834, "The Graduate Student Contributors of the SAPPHIRE Satellite is Dozen graduate students."]
[11.565030097961426, -1.2924631834030151, "The Mass of the MKA-N 1 Satellite is 10 kg."]
[8.504125595092773, 8.312947273254395, "The Type of Detector of the Instrument Sensor is Solar blind MgF2 / CsI Cathode - Multi-anode MCP."]
[7.5041093826293945, 7.886423587799072, "The Observation Capability of the SUSIM Spectrometer Instrument is Ozone and molecular oxygen profiles."]
[8.546347618103027, 10.75582218170166, "The Current Consumption of the LinkSprite JPEG color VGA camera Camera is 80-100 mA."]
[6.368349075317383, 7.842445373535156, "The Launch Year of the 118 GHz Radiometer Radiometer is 2019."]
[10.203413963317871, 3.0150983333587646, "The Altitude of the NigeriaSat-2 Satellite is 700 km x 733 km."]
[5.191074371337891, 1.6500794887542725, "The Total Deployments from Space Station of the CubeSats Satellite is 185."]
[6.717237949371338, 10.189159393310547, "The Primary Use of the Band 10 Spectral Band is Water vapor."]
[6.134300708770752, 2.2364542484283447, "The Capability of the TacSat-4 Satellite is Transmitting and receiving multiple carriers simultaneously."]
[11.516060829162598, 6.34520959854126, "The Testing Location of the XMM-Newton mirror modules Optical Instrument is Panter facility of the MPE (Max-Planck Institut f\u00fcr Extraterrestrische Physik) Garching, Germany."]
[8.6171875, 3.1985220909118652, "The Controller Gains of the GOCE Satellite is Unknown."]
[7.7449846267700195, 3.592960834503174, "The Tasking Priority of the SPOT or Pleiades constellations Satellite Constellations is Highest."]
[10.512213706970215, 6.031599998474121, "The Technology of the Micro-gravity experiment Experiment is Important for developing the methods of space crystal material growth."]
[4.134951591491699, 5.805546760559082, "The RF Communications Data Rate of the Kanopus-V 1 Satellite is 300 Mbit/s."]
[7.580546855926514, 9.009629249572754, "The Total Channels of the Spectral Bands Spectrometer is 159."]
[5.290344715118408, 3.8806591033935547, "The Leads of the Project System Engineer Engineer is Mission-level engineering efforts."]
[5.2592620849609375, 7.407675266265869, "The Data Delivery of the Mini-RF Instrument is More than 40 TB."]
[9.82426643371582, 8.370821952819824, "The Celestial Sphere Coverage of the Telescope Optical Instrument is Observatory ~80.7%."]
[5.711202144622803, 0.5292244553565979, "The Date of the U.S. Drought Monitor Report is April 26, 2022."]
[6.433356285095215, -0.6909818649291992, "The Interface Specification of the QZSS Satellite System is http://qzss.jaxa.jp/is-qzss/index_e.html."]
[4.563674449920654, 4.259731292724609, "The Components of the DLP System Satellite System is Probe biasing circuit, analog measurement circuit, controlling electronics."]
[9.252837181091309, 7.84593391418457, "The Operative Detector Temperature of the Detector Instrument is 238 K \u00b10.10 K."]
[8.197616577148438, 1.5706669092178345, "The Launch Date of the Solar Probe Plus Spacecraft is 2018."]
[8.98616886138916, 6.469569206237793, "The Quantity of the MTs Magnetic Torquers is 3."]
[8.586873054504395, 1.699013113975525, "The Launch Date of the Spitzer Space Telescope Telescope is August 25, 2003."]
[8.96890640258789, 5.1933393478393555, "The Attitude Accuracy of the DubaiSat-2 Satellite is 0.15\u00ba."]
[8.219801902770996, 2.9700493812561035, "The Science Mission End of the TanDEM-X and TerraSAR-X Satellites is End of 2015."]
[7.387439250946045, 5.455214977264404, "The Dead Zone Area of the Gulf of Mexico Body of Water is Variable, average size about the same as the state of Connecticut."]
[10.196478843688965, 7.420569896697998, "The Eutectic Point of the Galinstan Eutectic Liquid Metal Alloy is T= -19.5\u00b0C."]
[8.236793518066406, 9.572251319885254, "The Bands of the HRV Imager is PAN, Green, Red and Near Infrared (NIR)."]
[4.140134334564209, 5.792619705200195, "The S-band 1Mbit/s Downlink Data Rate of the UoSAT-12 Satellite is 1Mbit/s."]
[6.630858898162842, 2.627197504043579, "The URL of the FalconSAT-3 Satellite is http://www.globalsecurity.org/space/library/news/2009/space-091216-afns01.htm."]
[9.549612045288086, 1.0291255712509155, "The System and Software Integration and Testing Duration of the PhiSat-1 Satellite is Four months."]
[4.356409549713135, 4.572101593017578, "The Function of the MSPR-2 Rack is Provides power and communication interface to each experiment device."]
[8.786357879638672, 5.458713531494141, "The Mounting Orientation of the Sensor Satellite Component is Approximately along the satellite velocity."]
[11.658387184143066, -1.3509443998336792, "The Mass of the ZACube-2 Satellite is 4 kg."]
[8.566476821899414, 1.670374870300293, "The Observation Date of the NICER Telescope Telescope is 8 March 2022."]
[5.563505172729492, 2.7066078186035156, "The Purpose of the Hiber-3 Satellite is Providing connectivity for IoT sensors and devices."]
[6.965184211730957, 1.7719544172286987, "The Extension Approval Date of the Swarm Satellite is 20 Nov. 2017."]
[9.798759460449219, 9.475570678710938, "The Detector Array Elements of the IRIS Instrument Spectral Scanner is 5000 active elements."]
[6.914853096008301, 7.450836181640625, "The Objective of the LRR Instrument is Spacecraft POD (Precise Orbit Determination) to cm-level accuracy by SLR (Satellite Laser Ranging)."]
[7.390839576721191, 1.8132017850875854, "The Presentation Date of the Gravity Probe B Satellite is 1991."]
[6.315162181854248, 0.6045579314231873, "The Maiden Flight Date of the CubeSat Satellite is Unknown."]
[6.99669885635376, 3.6334822177886963, "The Ballistic Coefficients Comparison of the POPACS Satellite is DANDE mission results."]
[7.170487403869629, 4.513944149017334, "The CCD Cameras of the HJ-1B Satellite is 2."]
[6.33842658996582, 9.89775276184082, "The Instrument Mass of the SEVIRI Imager is 270 kg."]
[7.610093593597412, 7.662299156188965, "The Field of View Map of the EPI-Hi Instrument is Unknown."]
[4.794401168823242, 1.9757031202316284, "The Quantity of the 4 piggyback microsatellites Satellites is 4."]
[9.449026107788086, 0.4390355050563812, "The Design Life of the SPOT-3 Satellite is Four years."]
[8.967428207397461, 5.914394378662109, "The Sun Sensors of the S/C Satellite is 8."]
[9.146808624267578, 9.114264488220215, "The Typical cadence of the FSI dual EUV 174 \u00c5 and 304 \u00c5 alternatively Passband center is 600 s."]
[8.645978927612305, 1.9741770029067993, "The URL of the James Webb Space Telescope Telescope is http://ircamera.as.arizona.edu/MIRI/miricooler.pdf."]
[5.242859840393066, 5.755496501922607, "The Structure Type of the Satellite Communication is Monoblock frame."]
[9.385251998901367, -0.6081122159957886, "The Purpose of the MANTIS Nanosatellite is Provide low-latency and targeted imagery tailored to the data needs of the oil and gas sector."]
[9.306533813476562, 10.249463081359863, "The Focal length of the 50 mm camera Camera is 50 mm."]
[7.885849952697754, 10.035933494567871, "The FOV for SWIR/TIR for whiskbroom scanning of the VNIR-NP Imager is 80\u00ba."]
[5.570058822631836, 9.129562377929688, "The Power Consumption of the CLARA Instrument Satellite Instrument is 5.6 W."]
[11.085466384887695, 5.154719352722168, "The Pioneering Mission Concluded Date of the LISA Space Observatory is June 2017."]
[4.045836925506592, 1.2150089740753174, "The Mission Type of the PhoneSat-1 and -2 Satellite is Non-EO."]
[6.333717346191406, 2.4814212322235107, "The Objective 3 Requirement of the Jason-CS Satellite Mission is Global sea surface height to an accuracy of < 4 cm every 10 days."]
[2.2253990173339844, 4.436436176300049, "The Power of the Satellite Spacecraft is 250 - 1000 W."]
[7.40187406539917, 8.636521339416504, "The Precision of the S-193 Beam Scanning is Better than 5%."]
[6.818336486816406, 5.3494343757629395, "The URL of the SMAP Satellite is http://www.nasa.gov/press-release/nasa-soil-moisture-mission-begins-science-operations."]
[6.787010192871094, 9.140667915344238, "The Dimensions - Sensor head assembly of the Instrument Sensor is 20 x 37 cm."]
[3.41896390914917, 5.30445671081543, "The Onboard Data Storage of the QuickBird-2 Satellite is 128 Gbit."]
[8.628447532653809, 6.872771739959717, "The Resolution of the FGM Fluxgate Magnetometer is 1 to 2 nT."]
[10.123307228088379, 6.75937032699585, "The Development Date of the Microelectromechanical System Small Satellite Thermal Control is May 6, 2004."]
[8.453987121582031, 8.613683700561523, "The Grating Structure of the OCO-3 Spectrometer is Very regularly-spaced series of grooves on a very flat surface."]
[1.9536006450653076, 4.843814849853516, "The Purpose of the SPS Spacecraft Potential Sensor is Understand Dione\u2019s charging environment."]
[11.243645668029785, 3.494410753250122, "The Pit Depth of the Ma'at Region on Comet 67P/Churyumov\u2013Gerasimenko is 50\u201360 m."]
[7.776017665863037, 7.152616500854492, "The Instrument Type of the TEMPO Satellite is Spectrometer."]
[7.990844249725342, 1.9807738065719604, "The Purpose of the ExoMars Trace Gas Orbiter Spacecraft is Hunting for atmospheric gases linked to biological or geological activity, as well as understanding the past and present water inventory of the planet."]
[7.33546781539917, 6.802740097045898, "The Image Acquisition Date of the MODIS Instrument is January 30, 2022."]
[8.599945068359375, 9.442965507507324, "The Sensitivity of the NIRSpec MIRI Optical Instrument is 120 nJy (3.0 \u03bcm, \u03c4 i =10,000 s, and \u03bb/\u0394\u03bb = 100)."]
[5.956315040588379, 1.6024236679077148, "The Operation of the HTV Spacecraft is Unloading and Loading."]
[9.002622604370117, 2.5758228302001953, "The Onboard Software Reset of the Kepler Spacecraft is Five-day break in science data collection."]
[11.669454574584961, -1.2145036458969116, "The Mass of the Athena Satellite is 138 kg."]
[7.632792949676514, 3.993551254272461, "The Ice Loss of the CryoSat Satellite is 76 Gt per year for Gulf of Alaska, 28 Gt of ice per year for High Mountain Asia."]
[6.366216659545898, 4.10459041595459, "The Data Types of the EO-ALERT Satellite System is Optical and SAR data."]
[4.061670780181885, 6.644748210906982, "The Gain Control Method of the Ranging Channel Communication System is Apportioning the ranging channel the correct predetermined modulation index in the transmit modulator."]
[7.182210922241211, 1.590744972229004, "The Data Collection Period of the Cluster, Polar, Geotail, THEMIS Spacecraft is 1995\u20132012."]
[8.359366416931152, 2.7991833686828613, "The Mission of the Beresheet Spacecraft is Journey to the moon."]
[11.709015846252441, -1.0544930696487427, "The Mass of the S/C Satellite is 98 kg."]
[10.26824951171875, 5.239140033721924, "The Propellant of the FENIX micropropulsion device Micropropulsion Device is Solid."]
[9.660845756530762, 1.5865991115570068, "The Standard Deviation of Time Between Resets of the BRMM Spacecraft is 6 days."]
[8.821272850036621, 1.4185820817947388, "The Antenna Fields of View of the Van Allen Probes Spacecraft is Initially from boresight to 70\u00ba."]
[7.125583648681641, 7.4658284187316895, "The Measurement Scenario of the MIPAS Instrument is Enhanced Vertical Resolution and Regularization."]
[8.256851196289062, 4.859576225280762, "The GSD (Ground Sample Distance) of the ALOS/PRISM Satellite is 2.5 m."]
[7.330872058868408, 0.6069870591163635, "The Launch Preparations Date of the Galaxy 30 Satellite Satellite is 30 June 2020."]
[4.536557674407959, 5.927552223205566, "The Doppler Beacon of the GFO Satellite is CW (Continuous Wave) transmitter."]
[10.623064994812012, -1.6919126510620117, "The Supplies Capacity of the HTV Spacecraft is Up to 6,000 kg."]
[7.244024753570557, 8.64177417755127, "The Radiometric Resolution of the AATSR Instrument is 0.1 K."]
[3.4215805530548096, 3.619845390319824, "The Power of the CICERO satellites Satellite is Around 21 W."]
[7.348569869995117, 1.4996227025985718, "The Development Date of the Microscope Mission Satellite is Unknown."]
[7.055689811706543, -0.012329308316111565, "The End of Life Date of the Biomass Satellite is April 2029."]
[6.696406364440918, 7.614895820617676, "The Range of the Rangefinder Module Laser Altimeter is 500 km."]
[5.559360027313232, 3.8847148418426514, "The Operation of the F-DUGS Center is Request programming and pre-feasibility analysis, satellite data acquisition, data processing and distribution, archiving and cataloguing."]
[11.775530815124512, 4.789228439331055, "The Black Hole Mass of the OJ 287 galaxy Galaxy is 18 billion times the mass of our Sun."]
[5.03467321395874, -2.3739261627197266, "The Affiliation of the Nuria P\u00e9rez Engineer is Unknown."]
[11.109992980957031, 2.5553526878356934, "The Velocity After Engine Shutdown of the Schiaparelli Lander is Less than 2 km/h."]
[6.829740524291992, 1.190494418144226, "The Conference Date of the GIOVE-B Satellite is Sept. 22-25, 2009."]
[3.7989144325256348, 5.957004070281982, "The TT&C Downlink Rate of the MERLIN Satellite is 625 kbit/s."]
[8.24445915222168, 5.621791362762451, "The Noise of the Thrusters Satellite Component is 0.1 \u00b5N / Hz."]
[4.5989556312561035, 3.404270887374878, "The Number of Components of the JEM Module is 6."]
[8.537633895874023, 9.450418472290039, "The Material of the ICON FUV Instrument Photocathode is CsI."]
[3.5790176391601562, 2.2941341400146484, "The Size of the OptiCube-1 Satellite is 3U."]
[3.142472267150879, 4.821440696716309, "The SDRAM of the GomSpace NanoMind A3200 Onboard Computer is 32 MB."]
[9.425904273986816, 5.932743549346924, "The Pointing Accuracy of the ACS Attitude Control Subsystem is 0.14\u00ba (8.4 arcmin)."]
[6.927006721496582, 1.04693603515625, "The Launch Contract Date of the SpaceIL Nonprofit Group is October 2015."]
[3.192660331726074, 5.423015117645264, "The Onboard Time Code of the SSRNI Data Acquisition and Registration System is Yes."]
[9.507299423217773, 0.5874857902526855, "The Service Life of the FY-3E Satellite is At least eight years."]
[8.025603294372559, 9.435758590698242, "The Imaging Spectrum of the Elektro-L Satellite is Infrared (MWIR, TIR) and VNIR."]
[7.266101360321045, 5.4260382652282715, "The Vulnerable Species of the Pteropods Marine Snails is True."]
[10.511220932006836, -1.0315302610397339, "The Mass of the Microsatellite Satellite is ~ 10 kg."]
[9.805288314819336, -0.7344685196876526, "The Frequency Range of the Chibis-M Microsatellite is ULF-VLF."]
[8.357833862304688, 7.662294387817383, "The Components of the Microwave Calibration System Calibration System is Small mirror and a hot reference absorber."]
[6.477532386779785, 8.493812561035156, "The Size of the MEOLUT Next Local User Terminal is Less than six square meters."]
[8.171022415161133, 5.240654468536377, "The Accuracy of the Geoid Satellite is cm."]
[7.597667217254639, 5.452055931091309, "The Function of the OCO-3 Satellite is Monitors carbon dioxide and its changes throughout space and time."]
[9.367465019226074, 8.461509704589844, "The Components of the OTES Instrument is Sunshade, telescope, aft optics plate, electronics board, instrument enclosure."]
[7.671867847442627, 4.900478839874268, "The Reaction wheels of the BEESAT-1 Satellite is Yes."]
[8.015217781066895, 1.2147653102874756, "The Observation Date of the Earth from Space: Lofoten, Norway Imaging is 11 March 2022."]
[7.358546257019043, 9.975532531738281, "The Measurand of the HIS Hyperspectral Imaging Spectrometer is Spectrally resolved incoming and Earth-reflected solar radiation."]
[11.454428672790527, 4.395292282104492, "The Description of the R. R. Hodges-model Theoretical Model is Describes the terrestrial hydrogen exosphere up to ~60,000 km from the geocenter, based on a third-order spherical harmonic expansion."]
[7.6566948890686035, 1.4348688125610352, "The Presentation Date of the Hera Mission is November."]
[6.24221658706665, 0.5632834434509277, "The Launch Date of the BioSentinel 6U CubeSat is Second half of 2021."]
[5.771114349365234, 2.0843615531921387, "The Launch Site of the GeneSat-1 Satellite is NASA's Wallops Flight Facility, Wallops Island, VA, USA."]
[7.6080522537231445, 2.2755136489868164, "The URL of the ExoMars Mars Orbiter is http://m.esa.int/spaceinimages/Images/2016/10/Thumbs_up."]
[10.037609100341797, 1.535301923751831, "The Orbital Period of the SARAL spacecraft Satellite is 100.6 minutes."]
[6.584548473358154, 3.9557132720947266, "The Purpose of the Odin Satellite is Aeronomy and astronomy minisatellite with applications for atmospheric research, stratospheric ozone chemistry, mesospheric ozone science and summer mesospheric science."]
[7.192831516265869, 4.776027202606201, "The Sensor Types of the Trishna Satellite is Thermal InfraRed (TIR) telescope, optical Visible and Near Infrared (VNIR)/Short Wave InfraRed (SWIR) sensor (VSWIR)."]
[5.608382225036621, 9.133499145507812, "The Power Consumption of the KGI-4C Instrument is 6.8 W."]
[7.334911346435547, 10.037834167480469, "The Purpose of the Hyperspectral Imaging Remote Sensing Technology is Characterization and quantification of Earth's surface materials."]
[5.643590450286865, 1.959021806716919, "The Launch Vehicle of the GeneSat-1 Satellite is Minotaur."]
[6.128260612487793, 2.6906726360321045, "The Funding of the SEXTANT Technology Demonstration is NASA funded."]
[6.090559005737305, 9.566150665283203, "The Mass of the AltiKa Altimeter is 150 kg."]
[6.702016830444336, 2.296682834625244, "The Participation of the Vision-1 Satellite is International Disasters Charter."]
[7.07308292388916, 5.441267013549805, "The Inclusion of Aeolus data of the ECMWF Forecast Center is Since January."]
[8.042543411254883, 8.135947227478027, "The Overall Absolute Measurement Error at 333 K in Bands 4-6 of the Scanning geometry Instrument is 0.5 K."]
[7.246849536895752, 0.23657460510730743, "The Launch Date of the HY-2 (Haiyang-2) Satellite is Aug. 15, 2011."]
[7.983030796051025, 5.413262367248535, "The SNR of the VSSC Satellite is Around 100."]
[7.121289253234863, 7.1516876220703125, "The Unknown of the SOLSPEC Instrument is Unknown."]
[6.8012213706970215, 1.9698573350906372, "The Concept and International Collaboration of the Chinese Environment and Disaster Monitoring Satellite System (EDMSS) Satellite System is UNESCAP Meeting, Bangkok, Thailand, June 22-24, 2005."]
[7.448464870452881, 4.19797420501709, "The Instrument 2 of the CryoSat-2 Satellite is LRR."]
[9.532999992370605, 10.513508796691895, "The Video Format of the Iris Video Camera Camera is Ultra High Definition and High Definition (H.264 encoding)."]
[9.028227806091309, 4.80742073059082, "The Mode of the Solar Panels Power Generation is Nominally in sun-pointing mode."]
[8.744332313537598, 4.776409149169922, "The Orbit Altitude of the NEMO-HD Satellite is 600 km."]
[6.159488201141357, 6.289122104644775, "The Operation of the Staggered SAR Radar Mode is Continuously varying the PRI in a cyclic manner."]
[4.783615589141846, 0.7130361199378967, "The Shareholding of the Eutelsat Communications Company is 22.9%."]
[5.8072509765625, 6.114911079406738, "The Technology of the SAR Antennas Antennas is DBF (Digital Beam Forming)."]
[1.101593017578125, 4.194780349731445, "The Type of the Battery Energy Storage is Li-ion."]
[9.223954200744629, 8.956263542175293, "The Focal Length of the UVS Instrument Spectrometer Telescope is 125 mm."]
[4.987373352050781, 3.9020750522613525, "The Communication Network Type of the EDSN Swarm Satellite Network is Hub-and-spoke network."]
[12.142890930175781, 3.2000772953033447, "The Inclination of the Chang'e-1 Satellite is 31\u00ba."]
[3.574481725692749, 5.881967067718506, "The Number of Users of the EAN Connectivity System is 16.5 million IAG passengers."]
[8.317319869995117, 1.0583802461624146, "The Operation Start Date of the RAIDS Instrument is October 22, 2009."]
[4.201760292053223, 7.500912666320801, "The Mass of the Iris Radio Communication Device is 0.4 kg."]
[6.45662260055542, 1.5501329898834229, "The Launch Date of the OCO-2 Spacecraft is July 2, 2014."]
[8.455215454101562, 3.855860471725464, "The Sun-Earth based spin axis determination of the IKAROS Interplanetary Mission is Not provided."]
[6.7685956954956055, 0.585181713104248, "The Development Date of the ROCSat-1 Satellite is Unknown."]
[5.019021034240723, 6.259219169616699, "The Type of the Antenna Communication is Dual-feed collocated UHF and L-band antenna."]
[6.7117109298706055, 7.599952220916748, "The Operation of the LRF-S2 Laser Device is During touchdown, the sampler horn will compress as it touches the surface of Ryugu."]
[3.6450283527374268, 5.991092205047607, "The Downlink Data Rate of the Payload Communication System is 278 Mbit/s."]
[8.541790008544922, 1.6577229499816895, "The News Release Date of the Webb Telescope Telescope is 12 July 2022."]
[7.25467586517334, 6.742523670196533, "The Launch Vehicle of the OCO-3 Instrument is Falcon 9 rocket."]
[5.728503704071045, 6.482378005981445, "The Antenna Radiating Area Dimensions of the SAR Synthetic Aperture Radar is 10 m by 3.5 m."]
[6.2443132400512695, 5.574836730957031, "The Application Topics of the Cross-track SAR Interferometry Application is 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 co."]
[11.04999828338623, 6.366756916046143, "The Energy Loss of the Neutron-Element Collisions Particle Interaction is More like a ping pong ball hitting a bowling ball."]
[8.995134353637695, 10.827665328979492, "The Swath Width of the CCD Pushbroom Camera Camera is 60 km."]
[7.34952974319458, 0.8795642852783203, "The Mission Status Report Date of the QuikSCAT Satellite is Nov. 23, 2009."]
[9.50019359588623, 0.5593960881233215, "The Design Life of the PROBA-1/-2 Satellite is Nominal mission life of 2.5 years (with a possible extension of up to 5 years)."]
[8.25577449798584, 9.393930435180664, "The Image Capture of the OLI-2 Imaging Device is During the wildfires."]
[5.087499618530273, 6.733944416046143, "The Polarization Purity of the Array Radiator Antenna is Cross-polar better than -20 dB."]
[1.4281758069992065, 4.947233200073242, "The Battery Charge Current of the SBVR Power Supply is Up to 40 A."]
[6.594316482543945, 4.038161277770996, "The Application of the RISAT-2 Satellite is Resource conservation & sustainable development planning."]
[7.377970218658447, 1.9612581729888916, "The Team Members of the Advanced On-Board Calibration of Space Systems Calibration System is John C. Fleming, Sandra Collins, Beth Kelsic, Nathan Schwartz, David Osterman, Bevan Staple."]
[7.799221992492676, 9.157951354980469, "The Spectral Range of the HIRDLS Spectrometer is 6 - 18 \u03bcm."]
[6.21179723739624, 2.0725882053375244, "The Operation Status of the TacSat-2 Minisatellite is Nominal as of 2007."]
[10.817753791809082, 4.1341872215271, "The Imagined View of the Planet Kepler-10b Exoplanet is Artist's depiction."]
[6.7767653465271, 3.1278600692749023, "The Mission Status of the Vesselsat-1 & -2 Satellite is Completed."]
[6.6779375076293945, 3.5249392986297607, "The Mission Type of the ST5 Satellite is EO."]
[7.422388076782227, 8.448518753051758, "The Dependency of the Signal to Noise Ratio (SNR) Performance Metric is Dependent on the choice of GIFOV and spectral bandwidth."]
[10.300577163696289, 3.616779327392578, "The Altitude at Supersonic Parachute Opening of the Experiment Data Telemetry is 25 km."]
[9.56386947631836, 0.7180915474891663, "The Continuous Attitude Mode Duration of the ICESat Satellite is Approximately six months."]
[7.444094181060791, 4.725017547607422, "The Mission of the PROBA-V Satellite is Vegetation monitoring."]
[8.589859008789062, 9.973566055297852, "The Resolution Improvement of the EIS Imaging System is 100 times better."]
[6.992906093597412, 2.5285637378692627, "The URL of the OMI Satellite is http://www.atmos-meas-tech.net/9/6035/2016/amt-9-6035-2016.pdf."]
[6.220013618469238, 4.465832233428955, "The Successor Instruments of the TES Satellite Instrument is CrIS instrument on the NOAA-NASA Suomi-NPP satellite and the IASI series."]
[7.67750883102417, 5.569731712341309, "The Detectors of the INTEGRAL Satellite is Imager (IBIS) and a Spectrometer (SPI)."]
[8.131143569946289, 10.066415786743164, "The Filter Band Pass Targets of the EXI Camera is 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."]
[5.025684356689453, 1.7862058877944946, "The Eclipses of the Cluster Satellite Constellation is 19."]
[6.923529624938965, 1.1831165552139282, "The Conference Date of the CHIPS Satellite is Aug. 21-24, 2000."]
[6.882028102874756, 0.3680223524570465, "The Retirement Date of the FY-3A Satellite is January 5, 2015."]
[9.614684104919434, 8.176400184631348, "The CsI Shield Thickness of the GRS Gamma-Ray Spectrometer is Approximately 3 cm."]
[6.6549506187438965, 2.5110764503479004, "The URL of the RADARSAT Constellation Mission Satellite Constellation is https://www.youtube.com."]
[7.050815105438232, 9.14084529876709, "The Ground Range x Product Length of the Spotlight Imaging Mode is 10 x 10 km."]
[6.473941802978516, 6.242056369781494, "The Antennas of the ASCAT Scatterometer is 6."]
[8.073863983154297, 3.1866769790649414, "The Bistatic X-band Experiment Result of the TerraSAR-X Satellite is Success."]
[6.662848472595215, 2.630152940750122, "The Mission Objective of the Lucy Satellite is Explore the diversity of Trojan asteroids and their satellites."]
[9.443720817565918, 9.37193775177002, "The Thickness of the Aperture Function Image Processing is a."]
[8.051443099975586, 2.2088606357574463, "The User Information Presentation of the Himawari-8/9 Satellite is May 13, 2013."]
[6.962654113769531, 1.4884822368621826, "The Launch Date of the GPM Satellite is 27 February 2014."]
[7.447148323059082, 1.8087652921676636, "The Launch Date of the Gravity Probe A Satellite is June 18, 1976."]
[8.849804878234863, 5.560450553894043, "The Selection Criteria of the Hexapod Mounting System is Lifetime and lubrication tests."]
[9.203812599182129, 5.192931175231934, "The Attitude Control of the FY-3 series spacecraft Satellite is Three-axis stabilization (bias momentum control)."]
[8.683706283569336, 9.130738258361816, "The F-number of the Instrument Spectrometer is F73.7."]
[8.493597984313965, 8.387406349182129, "The Components of the GARI-1 Instrument is Two cerium-doped gadolinium aluminum gallium garnet (GAGG (Gd3(Al,Ga)5O12 :Ce)) scintillation detectors."]
[6.285284519195557, 4.3495402336120605, "The Measurement Frequency of the TROPICS CubeSat Satellite is Higher than previous satellites."]
[6.942401885986328, 2.585890054702759, "The URL of the CNES Satellite is http://www.ies.univ-montp2.fr/robusta/satellite/IMG/pdf/DD_GN_2010.02.16__ISU2010.pdf."]
[2.2547948360443115, 5.733487606048584, "The Average Power Level of the EDFA Amplifier is 0.5 W."]
[9.05345344543457, 7.631081581115723, "The Phase Transition Temperature of the Gallium Calibration Source Radiometer Calibration is 29.76\u00b0C."]
[7.362987995147705, 9.196916580200195, "The Wavelength Shift of the FG (Filtergraph) Instrument is Up to 26 km/s."]
[8.6469087600708, 1.9369356632232666, "The URL of the James Webb Space Telescope Space Telescope is http://www.sciencecodex.com/james_webb_space_telescope_begins_to_take_shape_at_goddard."]
[9.165255546569824, 8.019288063049316, "The Components of the Instrument Optical Subsystems is Two sets of electronics, two cryogenic coolers for the detectors."]
[4.636246681213379, 1.831573724746704, "The Spectral Bands of the EarthDaily Constellation Satellite Constellation is Over 21."]
[9.640329360961914, 4.013132095336914, "The Thruster Location of the CanX-4&5 Satellite is One face only."]
[11.425321578979492, 2.2250783443450928, "The Attitude Maneuver of the Hayabusa-2 Spacecraft is Around the Z-axis."]
[2.2057766914367676, 4.424213886260986, "The Power Generation of the SPOT satellite constellation Satellite Constellation is 1,000 W."]
[6.164257526397705, 4.3804497718811035, "The Future Satellite of the TIM and SIM instruments Instruments is NPOESS series spacecraft."]
[9.4796724319458, 4.294421195983887, "The Total Height of the ESM Module is 4.0 m."]
[7.064897537231445, 1.5221006870269775, "The Event of the MATS Satellite is SPIE Astronomical Telescopes + Instrumentation, 2018, Austin, Texas, United States."]
[6.549776077270508, 7.8666205406188965, "The Transfer Time from CSAR to TR of the LD Output Laser Diode is About 1 min."]
[7.41534948348999, 7.447832107543945, "The Data Collection Period of the OMI Ozone Monitoring Instrument is More than 15 years."]
[6.325759410858154, 9.085076332092285, "The Volume of the DPU Digital Processing Unit is 230 x 300 x 250 mm."]
[8.161964416503906, 3.30436635017395, "The Imaging Mode of the TanDEM-X Satellite is Left-looking."]
[9.912635803222656, 1.3512758016586304, "The Revisit Time of the SuperView-1 01 and Superview-1 02 Satellite is 4 days."]
[10.497527122497559, 3.295850992202759, "The Orbit Sunlight of the ALMASat-1 Satellite is About 75%."]
[9.229774475097656, 10.468803405761719, "The Depth of Field of the CMOS Camera Camera is 120 cm."]
[9.617780685424805, 7.243100166320801, "The Designed Depth of the \"the mole\" Heat Probe is 5 meters underground."]
[6.319799423217773, 8.296883583068848, "The Spatial Resolution of the SMMR Microwave Radiometer is Ranged from 22 km at 37 GHz to 100 km at 6.6 GHz."]
[7.321786880493164, 0.0680868998169899, "The Launch Date of the HREP Payload is Sept. 10, 2009."]
[7.086431503295898, 4.93776273727417, "The Detection Type of the Spaceborne Detection System Satellite System is Localized carbon dioxide sources."]
[3.8270950317382812, 0.2975778579711914, "The Purpose of the GRAIL Probes Spacecraft is Learn about the moon's internal structure and composition."]
[5.443950653076172, 3.9730687141418457, "The Network Support and Space Operations Services of the GISTDA and NSPO Organizations is Provided to each other."]
[9.056829452514648, 10.633018493652344, "The Image Resolution of the NAVCAM Camera is 84.6 cm/pixel."]
[8.888864517211914, 6.328712463378906, "The Mounting of the TWINS Instrument is Rotating actuator platform."]
[8.667132377624512, 6.757070064544678, "The Magnetic Field Strength of the 1E1547.0-5408 Magnetar is 1014G -1015G."]
[7.295106887817383, 3.051273822784424, "The Availability of the Visualization Product is Worldwide to planetariums and other centers of informal learning."]
[6.960610866546631, 1.2050809860229492, "The Presentation Date of the Small Satellites Satellite is Oct. 4-8, 2004."]
[7.411805152893066, 0.004888058640062809, "The Flight Demonstration Goal of the DRACO Demonstration Rocket is Fiscal year 2026."]
[4.081862449645996, 3.15213680267334, "The Scalability of the Open5GCore Rel. 4 5G Core Network is Raspberry PI to a complete rack of servers."]
[9.176558494567871, 7.318208694458008, "The Provider of the FIPEX Sensor is Institute of Aerospace Engineering of TU Dresden, Germany."]
[11.367742538452148, 3.968987464904785, "The Orbital Period of the Planet Orbiting AU Microscopii Exoplanet is Just over a week."]
[9.945808410644531, 5.2451300621032715, "The Performance of the Cold Gas Pressurization System Satellite Component is Satisfactory."]
[4.443605422973633, 4.699875354766846, "The Function of the PCM Module Module is Dissipates the thermal power emitted by the lasers during operation, forms the mechanical structure to which the receiver module is attached."]
[7.03860330581665, 0.584091305732727, "The Launch Date of the Flying Laptop Satellite is 14 Jul 2017."]
[4.160706996917725, 6.172988414764404, "The Protocol of the Communication System Satellite System is AX25 radio-amateur protocol."]
[6.936285018920898, 1.211919903755188, "The Conference Date of the LARES Satellite is Sept. 23-25, 2003."]
[11.827446937561035, -1.1404826641082764, "The Launch Mass of the Spacecraft Satellite is 790\u00b130kg."]
[4.031954288482666, 10.350677490234375, "The NE\u0394T (K) of the ICI-2 Radiometer is 0.7."]
[10.090638160705566, 1.614416241645813, "The Orbital Period of the Secondary Payloads Unknown is 103 minutes."]
[9.014354705810547, 10.839776992797852, "The Swath Width of the CCD Camera Optical Device is 700 km."]
[8.957181930541992, 9.261757850646973, "The FOV Resolution of the HSRS Sensor is 2.22 arcmin."]
[8.637166023254395, 9.361592292785645, "The Earth Rotation Effect of the Band-64 Satellite Instrument is Limit to about 0.1 pixels."]
[7.568521022796631, 0.02085142396390438, "The Operation Start Date of the Cheops Satellite is Beginning of April."]
[6.586920261383057, 6.403689384460449, "The Structure Type of the WFS&C Wavefront Sensing and Control Subsystem is Semi-rigid."]
[9.397534370422363, 3.199112892150879, "The Target of the Periselene-1 Spacecraft is Sun-Earth WSB (Weak Stability Boundary)."]
[10.420851707458496, 7.69874382019043, "The Material of the Enclosure Optical Unit Enclosure is Black anodized aluminum."]
[10.434733390808105, 3.470506191253662, "The Semimajor Axis of the SMART-1 Satellite is 3416.853 km."]
[5.434970855712891, 5.6365132331848145, "The Modes of the BlackJack GPS Instrument is C/A, P, or codeless."]
[6.91394567489624, 0.4074917435646057, "The End of Operations Date of the GEOS-3 Satellite is July 1979."]
[8.094172477722168, 10.093018531799316, "The Spatial Resolution of the HRV Imager is 10 m for PAN, 20 m for MS."]
[9.186756134033203, 3.2618746757507324, "The Type of the Satellite Orbit Orbit is Sun-synchronous near circular dawn-dusk."]
[7.156064510345459, -0.08430466055870056, "The End of Life Date of the HySIS Satellite is 5 years."]
[7.889703750610352, 5.355567455291748, "The Mission of the CSSWE Satellite is Measure outer belt electrons and SEP protons."]
[8.965313911437988, 7.440965175628662, "The Photodiode Rotation of the Sun Sensor Suites Sensor is 90\u00ba."]
[6.22796106338501, 2.777719497680664, "The Mission Manager of the RADARSAT Constellation Mission Satellite Constellation is Daniel De Lisle."]
[6.637065887451172, 4.373125076293945, "The Payload of the SciSat/ACE spacecraft Satellite is Instruments provide information about more than 30 different molecular species."]
[3.9164059162139893, 6.123234748840332, "The Data Rate of the GSN Ground Station Network is Up to 622 Mbit/s."]
[6.856252670288086, 4.559468746185303, "The Imaging Frequency Band of the HJ-1C Satellite is S."]
[9.48957347869873, -2.5167853832244873, "The Energy Range for C of the LEICA Particle Detector is 0.44 - 11.4 7.2 - 160 14 - 210 34 - 120 MeV/n."]
[9.166687965393066, 6.693391799926758, "The Interface of the Star Sensor Sensor is MIL-STD-1553 bus."]
[9.843462944030762, 8.065892219543457, "The Energy Resolution of the GRS Gamma-Ray Spectrometer is \u2264 9% at 662 keV."]
[10.214735984802246, 5.051222324371338, "The Purpose of the He-repressurization system Propulsion Subsystem is Raise the pressure in the main tank to an adequate pressure to complete the GRAIL mission."]
[7.778653144836426, 3.2872161865234375, "The Number of Interferometric Pairs of the ERS Tandem Mission Satellite Mission is Five or six for Europe and North America."]
[9.304567337036133, -0.7540714144706726, "The Country of the Aalto-1 Nanosatellite is Finland."]
[9.210332870483398, 10.8506441116333, "The Distance Range of the MCAM-3 Camera is Approximately 984 km \u2013 6194 km."]
[9.318493843078613, 0.8819230198860168, "The Operations Duration of the MOPITT Satellite Instrument is 2.5 Years."]
[9.531540870666504, 4.12235689163208, "The Attitude Pointing Requirements of the CanX-4&5 Satellite is Placed on the attitude determination and control system for accurate thruster pointing."]
[12.15609073638916, 3.268306016921997, "The Inclination of the Satellite Constellation Satellite is 98.2\u00b0."]
[6.207625865936279, 5.941844463348389, "The Experimental Mode Spatial Resolution of the TSX-SAR Satellite is 1m."]
[11.396678924560547, 5.920041084289551, "The Launch Date of the Chandra X-Ray Observatory Satellite is 22 November 2021."]
[8.65977954864502, 1.911866545677185, "The Development Status Presentation of the James Webb Space Telescope Space Telescope is Jon Arenberg, \"JWST Development Status,\" 213th AAS (American Astronomical Society) Meeting, Long Beach, CA, USA, Jan. 4-8, 2009."]
[8.626297950744629, 6.984031677246094, "The Accuracy of the Magnetometer Sensor is 30 nT (3\u03c3)."]
[7.397512435913086, 10.018112182617188, "The Spatial Resolution of the Instrument Hyperspectral Imager is 8 m."]
[8.278831481933594, 2.5962953567504883, "The Orbit of the Himawari-8 Satellite is Geostationary orbit."]
[10.304917335510254, 2.99104642868042, "The Orbit Altitude of the Rocket 3.3 Rocket is 500 km."]
[9.087594985961914, 10.801281929016113, "The Overlapping Swath of the WFI Camera is 830 km."]
[11.308499336242676, 6.69235897064209, "The Telescope Type of the Swift Satellite is High-resolution X-ray."]
[6.801112651824951, 0.6750040054321289, "The Development Start Year of the MiRaTA Satellite is 2012."]
[7.375645637512207, 8.70957088470459, "The Number of Channels of the Spectral Channels Satellite Instrument is 5."]
[7.590956211090088, 1.686334490776062, "The Presentation Date of the MICROSCOPE Spacecraft is Oct.12-16, 2015."]
[4.677557945251465, 0.17797166109085083, "The Number of Satellites in Orbit of the OneWeb Company is 74."]
[11.176466941833496, 4.203637599945068, "The Survey Sample of the ARIEL Satellite is About 1000 extrasolar planets."]
[4.8738603591918945, 9.048652648925781, "The Distance to Seismically Active Region of the InSight lander Seismic Instrument is More than 1,000 kilometers."]
[7.19244384765625, 0.23277199268341064, "The Launch Date of the Beijing-3B Satellite is 24 August 2022."]
[10.101358413696289, 5.188174724578857, "The Test Conduct of the Integrated Firing Test Test is \u0394V thruster and RCS thrusters."]
[7.315751075744629, 9.215858459472656, "The Number of Wavelength Positions of the FG (Filtergraph) Instrument is Six."]
[8.966928482055664, 7.016779899597168, "The Objective of the SWOOPS Instrument is Observation of the solar-wind flow at middle-to-high solar latitudes for the construction of a representative model of the heliosphere."]
[9.347756385803223, -0.6566009521484375, "The Presentation Date of the SERB Nanosatellite is Sept. 26-30, 2016."]
[9.41932201385498, 1.8009675741195679, "The Roll Maneuver Frequency of the EarthCARE satellite Satellite is Once a month."]
[6.3847222328186035, 5.5255584716796875, "The Data Gathered of the Global Navigation Satellite System - Radio Occultation (GNSS-RO) Instrument is Temperature and humidity."]
[8.371082305908203, 8.993974685668945, "The Microchannel Plate Area of the FlaPS Instrument Package is 25 cm2."]
[7.698894023895264, 3.3574256896972656, "The Data Availability of the Landsat 7 ETM+ SLC-off and Landsat 5 TM Satellites is All data September 2008."]
[9.52035140991211, 6.607278823852539, "The Electrical Isolation Method of the Hinge Pin Mechanical Component is Shrink tube."]
[5.3138837814331055, 5.921523571014404, "The Access of the Antenna Dish Satellite Component is Cannot be readily accessed from the front due to the mesh."]
[3.9080655574798584, 4.507216930389404, "The Core Processors of the Hayabusa-1 SRC Instrument Module is Discontinued."]
[3.830381393432617, 6.457996845245361, "The User Data Link Speed of the GEO LCT Laser Communication Terminal is 1.8 Gbit/s."]
[7.8089494705200195, 8.903322219848633, "The Radiometric Accuracy of the Spectral Band D Spectrometer is 3."]
[9.192530632019043, 7.132419586181641, "The Probe Types of the ISL Instrument Langmuir Probe is One cylindrical, one spherical with a 6 cm diameter segmented probe."]
[9.222258567810059, 10.213655471801758, "The Observation Directions of the MSU-50 Camera is \u00b117\u00ba, 0\u00ba (nadir)."]
[9.962273597717285, 1.4809293746948242, "The Orbit MLST of the Envisat Satellite is 22:00 ANX \u00b1 5 minutes."]
[6.942560195922852, 1.2563130855560303, "The Merger Date of the Planet Company is 7 July 2021."]
[7.719906806945801, -0.4334857165813446, "The Launch Time of the Falcon 9 Rocket is 1:19 a.m. Eastern (06:19 UTC)."]
[7.834414005279541, 1.3089838027954102, "The Observation Period of the NASA Satellite Sensors Sensors is May 29 to June 6."]
[5.885317325592041, 6.971157550811768, "The Swath Width of the SIR-C Phased Array is 15 to 65 km for calibrated images."]
[9.372774124145508, 2.026432752609253, "The Operation Frequency of the SONATE CubeSat Satellite is Daily."]
[7.205353736877441, 2.52972674369812, "The URL of the INTEGRAL Satellite is http://iopscience.iop.org/article/10.3847/2041-8205/820/2/L36/pdf."]
[11.765143394470215, -1.1156318187713623, "The Mass (kg) of the ALOS-2 Satellite is 2120."]
[7.611847400665283, 7.505776882171631, "The In-flight Performance of the Gas Scintillation Proportional Counter Instrument is Unknown."]
[4.878542900085449, 0.5591785907745361, "The Economic Impact of the Silkworm Insect is More than 30 billion dollars income for silkworm breeders, commercial as well as industry."]
[7.501749515533447, 8.27658462524414, "The Altitude Range of the Detector Instrument is Limited to 30 km."]
[7.3803558349609375, 8.898008346557617, "The Spectral Response of the VACNTs Radiometer Absorber is Extremely flat over a wide wavelength range."]
[9.45274829864502, 10.315433502197266, "The Location of the FAI Camera is Novaya Zemlya, Russia."]
[4.573960304260254, 5.993823528289795, "The Splitting of the Baseband Signal Signal Type is Three ways."]
[6.918522834777832, 5.388134479522705, "The Spectral Bands of the MTG-S Spacecraft Satellite is 16."]
[6.049893379211426, 3.6423635482788086, "The Members of the SPEXone Steering Committee Committee is Two Airbus DS NL and two SRON members including the Principle Investigator."]
[4.034945487976074, 5.020758152008057, "The Data Format of the HSM High-Speed Multiplexer is Virtual Channel Data Units."]
[10.085356712341309, -0.4688607156276703, "The Inclination of the Vstar Gravity-field Measurement Microsatellite is 90\u00ba."]
[10.212002754211426, 5.627573490142822, "The Attachment of the ENT EVR Nozzle Tool is Attached to a spring-loaded pressurized hose."]
[3.259326934814453, 5.058309078216553, "The Memory Space of the NanoSat MO Framework Software Framework is Dedicated memory space allocated specifically for them."]
[11.765116691589355, 4.781656742095947, "The Smaller Black Hole Mass of the OJ 287 galaxy Galaxy is About 150 million times the mass of our Sun."]
[8.406013488769531, 9.533238410949707, "The Detector Elements Downlinked of the AHI Scanner is 7,856."]
[5.8377838134765625, 6.178343772888184, "The Conference Presentation of the CSG System Synthetic Aperture Radar is EUSAR 2016, 11th European Conference on Synthetic Aperture Radar, Hamburg, Germany, June 6-9, 2016."]
[3.9934704303741455, 2.355448007583618, "The Size of the BioSentinel Spacecraft is 6U."]
[8.530145645141602, 4.649270534515381, "The Importance of the Cluster Satellite is Study turbulence and its role in fundamental processes."]
[7.352574825286865, 4.346372604370117, "The Image Assessment System (IAS) of the Landsat-7 Satellite is Provides users with ancillary information needed to generate useful, radiometrically calibrated and geometrically corrected ETM+ digital imagery."]
[10.605710983276367, 7.46926736831665, "The Structure Material of the Bus Satellite Component is Graphite."]
[8.83608341217041, 5.160839080810547, "The Attitude Control Accuracy of the GFO Satellite is 0.25\u00ba (3\u03c3)."]
[8.42060661315918, 7.477063179016113, "The Function of the SES Instrument is Validate the optical and thermal performance of the instrument."]
[6.4352216720581055, 6.628081798553467, "The Spatial Resolution of the SGR-ReSI Instrument is Lower."]
[6.559516429901123, 4.060503005981445, "The Mission of the PhiSat-1 Satellite is Monitor polar ice and soil moisture, test intersatellite communication systems."]
[4.706966876983643, 1.8566266298294067, "The Number of Subscribers of the SecureWatch Service is 20."]
[10.292360305786133, 3.0043723583221436, "The Altitude of the Shakuntala Satellite is 480 km."]
[4.338819980621338, 6.2599053382873535, "The Frequency Band of the RF Communications Communication System is X-band for the payload data downlink."]
[8.067468643188477, 1.2124031782150269, "The Date of the Arabian Night Lights Image is 17 May 2021."]
[6.3415141105651855, 8.520297050476074, "The Horizontal Resolution of the JPL Microwave Radiometer Radiometer is 3.1 km."]
[10.411886215209961, 3.2937049865722656, "The Altitude of the Computer System Payload is 120,000 feet."]
[7.62199592590332, 8.917684555053711, "The Spatial Resolution of the Miniature High-Resolution Imaging Spectrometer Imaging Spectrometer is Under 50 m."]
[12.986724853515625, 4.139410018920898, "The Number of Objects of the Gaia Catalogue of Nearby Stars Stellar Census is 331,312."]
[9.659769058227539, 1.2593415975570679, "The Estimated Time Before Blackout of the Spacecraft Satellite is Just three hours."]
[8.383526802062988, 0.5815954804420471, "The Radio Signals of the Hitomi Satellite is 3/26 23:49~23:52 (for 3 min) @USC,23:48~23:51(for 3 min) @ KTU."]
[8.53857707977295, 5.486013412475586, "The Gaia's Position Accuracy of the GBOT Ground Based Orbit Tracking is Good to 20 m arcsec."]
[8.678021430969238, 1.967112421989441, "The Primer Version of the James Webb Space Telescope Space Telescope is 1.0."]
[6.996591091156006, 1.6049139499664307, "The Capacity Establishment Deadline of the GMES Initiative is 2008."]
[10.177281379699707, 5.323503017425537, "The Volume of the Gas Cartridge Component is 20 ml."]
[7.815797328948975, 8.525903701782227, "The Spectral Bands of the CHRIS Imaging Spectrometer is Up to 63."]
[5.633649826049805, 1.6904969215393066, "The Stage Type of the Soyuz Rocket is Payload shroud."]
[11.388102531433105, 5.086196422576904, "The Extension of the Gaseous Atmosphere Atmospheric Feature is Several hundred miles from the neutron star."]
[4.391627311706543, 6.171840667724609, "The Frequency Band of the Telemetry, Tracking and Command System Telemetry, Tracking and Command System  is S-band."]
[9.381884574890137, 9.074433326721191, "The Size of the Telescope Optical Instrument is 17 cm x 12 cm x 12 cm."]
[5.852417469024658, 8.597081184387207, "The Measurement of the MHS Microwave Humidity Sounder is Microwave radiation emitted from Earth\u2019s surface."]
[3.8221049308776855, 5.7146430015563965, "The Data Transfer Capacity of the Satellite Communication is 100 MByte/day."]
[7.443111419677734, 0.6087936162948608, "The Orbit Reach Date of the Cheollian 2B Satellite is March 6."]
[9.536499977111816, 8.746809005737305, "The Design of the Telescope Optical Instrument is Off-axis unobscured TMA without intermediate focus locations."]
[8.70833683013916, 3.1382601261138916, "The Orbit Maintenance System of the GOCE Satellite is Ion Propulsion Unit."]
[7.514565467834473, 2.3790273666381836, "The URL of the ANTRIX Corporation Limited Corporation is http://www.antrix.gov.in/irsonline/eosatellites.html."]
[3.87595272064209, 5.708104610443115, "The Downlink Data Rate of the Spacecraft Satellite is From 9.6 kbit/s to 8.0 Mbit/s."]
[11.218056678771973, 2.8721580505371094, "The Diameter of the Haydn crater Crater is 251 km."]
[4.7776899337768555, 5.6065521240234375, "The RF Communications of the Satellite Satellite is S-band and X-band."]
[8.182316780090332, 5.101157188415527, "The Geolocation accuracy of the ALOS/PRISM Satellite is 6.1 m (rms)."]
[6.129779815673828, 3.079497814178467, "The Project Partners of the DSP Satellite Project is ESA (European Space Agency), CNSA (China National Space Administration)."]
[9.408151626586914, 7.365298271179199, "The Material of the Faraday Cup Sensor is Refractory metals and sapphire crystal insulators."]
[4.885168075561523, 1.9252833127975464, "The Number of Targets of the IXPE Satellite is 6."]
[8.62282943725586, 9.43222427368164, "The Pixel Angular View of the EXI instrument Imaging Instrument is 23 arcsec per pixel."]
[5.381338596343994, 1.4617010354995728, "The CubeSat Deployments of the NanoRacks Company is 185th from the Space Station."]
[8.086078643798828, 11.14412784576416, "The Sensitivity of the Channel 2 Sensor is 0.4 K/pixel."]
[8.433478355407715, 5.1849589347839355, "The Pointing Accuracy of the Satellite Satellite is Better than 200 m."]
[5.305877685546875, 2.1715312004089355, "The Number of Scientists or Institutional Teams of the PUTC Program is More than 60."]
[6.423489570617676, 4.740431308746338, "The Instruments of the JERS-1 Satellite is L-band SAR, OPS, JERS-1 Comms."]
[7.380342960357666, 4.815814018249512, "The Rescaling Method of the Landsat images Images is Bilinear interpolation."]
[6.1398844718933105, 2.670123338699341, "The Deputy Director of the Roman Space Mission is Nancy Levenson."]
[3.223353624343872, 4.915249347686768, "The EEPROM of the OBC Onboard Data Handling is 524 kB."]
[2.0991363525390625, 4.559175491333008, "The Max Power of the PM Satellite Component is 24 kW."]
[7.22739315032959, 6.919584274291992, "The Image Acquisition Date of the VIIRS Instrument is June 3 and 5, 2022."]
[8.799147605895996, 5.782926559448242, "The Magnetometers of the S/C Satellite is Two 3-axis magnetometers."]
[10.394987106323242, 9.60446834564209, "The Mission Duration of the Iris Radio Communication Device is Nominal 90 days."]
[1.1630040407180786, 3.819852113723755, "The Objective of the XI-IV Picosatellite is Demonstrate and validate a picosatellite bus system and the space use of commercial-of-the-shelf (COTS) parts."]
[7.796382904052734, -0.5084578990936279, "The Launch Date of the SpaceX CRS-17 Mission is 04 May 2019."]
[11.222771644592285, 4.206535816192627, "The Number of Planets Discovered of the UBC student Astronomer is 17."]
[6.648939609527588, 9.079161643981934, "The Size of the HIRES Instrument is 17 cm x 18 cm x 36.5 cm."]
[9.239998817443848, 10.598004341125488, "The Ground Surface Side Length of the LSI-1 Camera is 342 km."]
[9.464910507202148, 1.1688615083694458, "The Tandem Flight Duration of the Sentinel-3B Satellite is 4-5 months."]
[5.600292682647705, 6.203864574432373, "The Panel Quantity of the SAR Antenna Antenna is 5."]
[7.07587194442749, 8.837334632873535, "The Spatial Resolution of the SAM-II Instrument is 1 km (vertical)."]
[4.831617832183838, 1.8606683015823364, "The Number of Commands of the Admiral Paul F. Zukunft Coast Guard Commandant is 8."]
[6.7727885246276855, 3.0353000164031982, "The Management Contractor of the IMAP Mission is SwRI (Southwest Research Institute)."]
[5.275423049926758, 1.4306062459945679, "The Total Small Satellite Deployments by NanoRacks of the CubeSats Satellite is 217."]
[9.601053237915039, -0.10976400971412659, "The Orbital Life Goal of the Nanosatellite Satellite is 25 years."]
[7.3766021728515625, 8.547945976257324, "The No of bands/channels of the IRAS Infrared Atmospheric Sounder is 26."]
[11.680174827575684, 2.5285301208496094, "The Distance from Earth of the OSIRIS-REx Spacecraft is More than 200 million miles (321 million km)."]
[9.912001609802246, 1.6329240798950195, "The Thermal Vacuum Test Duration of the MMO Spacecraft is Three weeks."]
[6.485302925109863, 0.8941012024879456, "The Article Date of the Nav Canada Air Navigation Service Provider is March 8, 2010."]
[4.970476150512695, 4.022919654846191, "The Purpose of the Oxygen Generator Assembly (OGA) Pump Assembly Hardware is Critical spare to a support oxygen generation capability in support of the crew on board the International Space Station."]
[7.638363838195801, 9.525795936584473, "The Swath of the SLSTR Spectral Imaging Instrument is 1420 km."]
[5.988255977630615, 3.113354206085205, "The Strategic Partnership of the Spire Company is ICEYE."]
[9.435345649719238, 7.772475242614746, "The Detection Type of the EPISEM Instrument is Detects penetrating beta/gamma radiation from energetic particles above a certain energy threshold."]
[3.968576431274414, 5.702512741088867, "The Data Rate of the MTG-S Spacecraft Satellite is Around 60 Mbit/s."]
[9.757439613342285, 8.608575820922852, "The Pointing Stability of the VT Telescope is High."]
[10.765559196472168, 3.4304277896881104, "The Maximum Distance from the Sun of the Rosetta Spacecraft is Over 850 million km."]
[8.252197265625, 0.6004217863082886, "The Launch Date of the Hitomi Satellite is Unknown."]
[9.270584106445312, 9.935445785522461, "The Function of the ROLIS Camera is Down-looking imager that acquires images during the descent and doubles as a multispectral close-up camera after the landing."]
[9.35218334197998, 7.839754581451416, "The Incoming Energy Range of the INMS Ion and Neutral Mass Spectrometer is 0-50 eV."]
[6.7452778816223145, 4.335534572601318, "The Purpose of the Copernicus Programme Earth Observation Program is Monitor and collect information across different parts of the Earth."]
[10.34687328338623, 3.5167670249938965, "The Orbital Speed of the Cluster spacecraft Satellite is Up to 23,000 km/h."]
[11.733795166015625, -1.1452339887619019, "The Mass of the Norton Satellite End-body is 10.8 kg."]
[8.277460098266602, 10.369762420654297, "The Spectral Bands of the WiFS camera Camera is 0.62 - 0.68 \u00b5m, 0.77 - 0.86 \u00b5m."]
[6.224506855010986, 0.9016740918159485, "The Release Date of the Argos-3 Instrument is May 24, 2005."]
[6.142791271209717, 6.205747127532959, "The Intended Replacement of the TOPSAR SAR Mode is Conventional ScanSAR mode."]
[3.956042528152466, 6.427510738372803, "The Modulation Scheme of the RF Communications Communication System is FSK."]
[5.278430461883545, 4.762173652648926, "The Locations of the TT&C stations Ground Stations is Saint-Hubert and in Saskatoon, Saskatchewan."]
[11.253695487976074, 6.301044464111328, "The Data Source of the Chandra X-ray Observatory X-ray Observatory is Astronomers obtained this result using data from NASA's Chandra X-ray Observatory."]
[5.922024250030518, 0.706716775894165, "The Launch Date of the AlSat Nano CubeSat is September 2016."]
[8.331645965576172, 3.810894727706909, "The Communication of the LAGEOS Satellite is None."]
[7.57739782333374, 0.4931947588920593, "The Purpose of the SVOM Satellite is Observe and characterize gamma-ray bursts."]
[6.712368011474609, 4.838652610778809, "The Purpose of the CFOSAT Satellite is Study ocean surface wind and wave conditions."]
[10.308680534362793, 1.7417731285095215, "The Expected Duration of the Lunar Orbit Orbital Phase is Minimum of 6 months."]
[6.190338134765625, 1.8964955806732178, "The Launcher of the MEPSI Satellite is MightySat II.1."]
[5.193882465362549, 4.632383823394775, "The Ground Network of the FormoSat-7 / COSMIC-2 mission Satellite Mission is USN ground stations for the first 2 years, and then service provision by NOAA's ground stations for the following 3~5 years."]
[11.694438934326172, -1.2128483057022095, "The Mass of the PM Satellite Component is 14,800 kg."]
[11.751138687133789, 4.655997276306152, "The Size of the Cluster XDCPJ0044.0-2033 Galaxy Cluster is Over one and half million light years across."]
[6.902219772338867, 10.026644706726074, "The Bands of the HawkEye Ocean Color Instrument is 8-band multispectral."]
[6.017319679260254, 3.1729249954223633, "The Contractor of the CAPSTONE Satellite is Advanced Space of Boulder, Colorado."]
[6.871151924133301, 4.732285976409912, "The Medium-sized Aperture Camera (MAC) of the RazakSAT Satellite is Unknown."]
[7.828771591186523, 2.851809501647949, "The Destination of the Sample Return Capsule Capsule is Earth."]
[7.960705757141113, 0.03793451562523842, "The Execution Start Date of the CIBORG Program is Early 2017."]
[3.4065966606140137, 6.6524152755737305, "The Transmitter Power of the Spacecraft Repeater Communication Device is 8 W."]
[8.16659164428711, 2.1044998168945312, "The Mission Name of the Radiation Belt Storm Probes Satellite is Radiation Belt Storm Probes."]
[9.430915832519531, 5.6551971435546875, "The Position of the ADACS Attitude Determination and Control System is Front of the satellite."]
[8.479544639587402, 5.527388572692871, "The Interplanetary Vector Magnetic Field Measurement Range of the DSCOVR Satellite is 0 \u2013 100 nT."]
[5.6658782958984375, 3.5238893032073975, "The Function of the Astronode S Integration Device is Allow remote monitoring and significant maintenance cost reduction."]
[6.737283706665039, 0.9400469660758972, "The Observation Operation Completion of the MTSAT-2 Satellite is Around 2015."]
[9.767186164855957, 7.142322063446045, "The Publication Date of the Supercapacitors Energy Storage is 2009."]
[7.765169143676758, 7.277349472045898, "The Pointing Knowledge Stability of the Instrument Satellite Instrument is \u00b19.7 \u00b5radians over 2.5 seconds."]
[10.084174156188965, 1.5309650897979736, "The Orbit Period of the SEOSat Satellite is 98 minutes."]
[8.423700332641602, 8.664846420288086, "The Principal Investigators of the SCIAMACHY Spectrometer is J. P. Burrows, H. van Dop."]
[7.3078413009643555, 8.550040245056152, "The Wavelength of the Laser Instrument is 1556 nm."]
[7.882382392883301, 0.5372985005378723, "The Launch Year of the Aeolus Satellite is 2018."]
[8.989192008972168, 1.6123746633529663, "The Interstellar Dust Measurements of the Ulysses Spacecraft is October 20, 2015."]
[9.141131401062012, 10.665950775146484, "The Nadir image size (1000 km altitude) of the 16 mm camera Camera is 110 km x 120 km x 92.8 km."]
[3.846844434738159, 5.7512030601501465, "The LVDS Link Speed of the IRIS Satellite is 50 Mbit/s."]
[7.961904048919678, 3.3032846450805664, "The Shadow of the Debris Spacecraft Debris is One pixel."]
[4.2800469398498535, 4.2356133460998535, "The Function of the CSS Consumable Storage Subsystem is Provides potable water, oxygen and nitrogen to the CM."]
[6.372601509094238, 3.611398935317993, "The Agency of the Biomass Satellite is ESA."]
[7.03524923324585, 5.937808990478516, "The Wind Speed Range of the Numerical Weather Model Weather Model is 3 m/s to approximately 20 m/s."]
[7.057089328765869, 3.6633241176605225, "The Size of the Vizca\u00edno Biosphere Reserve Biosphere Reserve is Largest protected area in Mexico."]
[6.498106479644775, 7.3582634925842285, "The Polarization of the Spotlight Imaging Mode is Single or dual."]
[6.760944843292236, 0.7558233737945557, "The Launch Date of the NigeriaSat-2 Satellite is Unknown."]
[5.151928424835205, 3.0750579833984375, "The Payloads of the ZACube-2 CubeSat is Medium resolution matrix imager and a number of communication subsystems."]
[7.014710426330566, -0.197414830327034, "The End of Life Date of the CAPSTONE Satellite is June 28, 2023."]
[11.758871078491211, 4.777638912200928, "The Black Hole Mass of the PG211+143 Galaxy is 40 million solar masses."]
[7.585886478424072, 1.8274072408676147, "The Data Management Plan of the Small Explorer (SMEX) Satellite is Unknown."]
[8.49354362487793, 4.97768497467041, "The Target Reflectivity of the NEMO-HD Satellite is 30%."]
[9.2593994140625, 9.069440841674805, "The Telescope FOV of the Telescope Optical Instrument is 166 arcmin x 166 arcmin."]
[5.313649654388428, 6.776051044464111, "The Beamwidth of the Antenna Satellite Component is 1.1\u00ba."]
[8.71127700805664, 10.055497169494629, "The Number of Subapertures of the PAIS Imaging System is 4."]
[8.144103050231934, 4.821667194366455, "The Ground Instantaneous Field of View (GIFOV) of the Climate Observatory Satellite is 50 m."]
[3.9942455291748047, 2.338620662689209, "The Size of the NEA Scout CubeSat is 6U."]
[7.191396236419678, 0.9506440162658691, "The Funding Renewal Date of the CUTE Satellite is May 2019."]
[4.913191318511963, 5.105600833892822, "The Ground Station Communication of the IXPE Observatory Satellite is ASI-contributed Malindi ground station via S-band link."]
[6.669353485107422, 2.606267213821411, "The URL of the RADARSAT Constellation Mission Satellite Constellation is http://eofsac.org/sites/default/files/2018-02/McNairn%20Delisle%20RADARSAT%20Constellation_0.pdf."]
[9.3667631149292, 5.534134387969971, "The Type of the Attitude Subsystem Satellite Subsystem is Passive magnetic stabilization."]
[4.941104888916016, 1.9483979940414429, "The AMOS Terminator Passes of the SpinSat Satellite is 3."]
[9.102579116821289, 0.8959055542945862, "The Possible Mission Extension of the SELENE/Kaguya Satellite is Half a year."]
[4.01353120803833, 4.5313615798950195, "The Mission of the Parallel Processing Unit (PPU) Computing Payload is Secondary."]
[1.5809285640716553, 4.56568717956543, "The Efficiency of the Secondary Converter Converter is 70%."]
[4.680044651031494, 5.75063943862915, "The RF Communications of the Spacecraft Satellite is UHF."]
[7.9369611740112305, 6.907172203063965, "The Measurement Frequency of the Dark Reference Calibration Device is Every 2\u20133 orbits."]
[6.961462497711182, 0.43021127581596375, "The Launch Date of the SARAL/AltiKa Satellite is February 2013."]
[11.630563735961914, 4.38100528717041, "The Distance from Earth of the Kepler-438b Exoplanet is 475 light-years."]
[11.018043518066406, 4.158444404602051, "The Field of View of the Roman Satellite is Wide."]
[8.70395565032959, 9.177384376525879, "The Slit Length of the Spectrometer Spectrometer is 3 mm."]
[9.498678207397461, 1.2536492347717285, "The Operation Duration of the KOMPSAT-2 Satellite is Until the mission end."]
[9.837733268737793, 4.357856273651123, "The Control Method of the Solar or drag sails Deorbiting Device is Constantly controlled relative to either the solar vector for steered sailing or the satellite velocity vector to maximize drag."]
[10.115239143371582, 3.070504903793335, "The Operating Altitude of the GRAIL Satellite is 23 km."]
[9.539430618286133, 3.814455032348633, "The Formation Flight Mission of the CanX-4/CanX-5 Satellite is Unknown."]
[8.934362411499023, 1.7642937898635864, "The Arrival Date at Europe\u2019s Spaceport of the BepiColombo Spacecraft is May 11, 2018."]
[4.439002990722656, 4.147329330444336, "The Purpose of the Storage Box Component is Store the inflatable tubes and the membrane."]
[7.390938758850098, 0.7176312804222107, "The Announcement Date of the PROBA-V Satellite is 9 July 2020."]
[11.880301475524902, -1.1005769968032837, "The Launch Mass of the IAE Experiment Satellite Component is 60 kg."]
[12.11536979675293, 3.278944253921509, "The Inclination of the Satellite Communication is 99.63\u00ba."]
[7.196917533874512, 7.961096286773682, "The Integrating Time of the GOCI Instrument Instrument is Up to 8 seconds."]
[10.253056526184082, 7.7161054611206055, "The Material of the Baffles Instrument Component is SiC."]
[10.220161437988281, 1.3074790239334106, "The Braking Burn Time of the Queqiao Communication Satellite is 13:32 UTC."]
[9.261334419250488, 10.352420806884766, "The Number of Photographs of the Metric Camera Camera is 1019."]
[12.987359046936035, 4.861518859863281, "The Mission End Date of the IBEX Spacecraft is Unknown."]
[9.527861595153809, 9.11669635772705, "The Aperture Diameter of the SOT Telescope is 50 cm."]
[9.142975807189941, 3.3071980476379395, "The Orbit of the SMAP Satellite is Near-polar, sun synchronous."]
[4.619352340698242, 0.18028733134269714, "The Number of User Terminals of the OneWeb Satellite Constellation is Unknown."]
[6.389423847198486, 1.7518507242202759, "The Ground Segment Design Team of the EnMAP Satellite is 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."]
[1.5933870077133179, 4.833580017089844, "The Power Bus of the EPS Electric Power Subsystem is Unregulated 22 V - 36 V."]
[8.704925537109375, 10.750783920288086, "The Spectral Range of the HSC CCD Imaging Camera is 450 - 850 nm."]
[7.070343494415283, 2.624260663986206, "The URL of the SPOT 7 Satellite is http://www.astrium-geo.com/files/pmedia/edited/r18072_9_spot_6_technical_sheet.pdf."]
[6.161364555358887, 3.3721837997436523, "The Purpose of the Military Payload Satellite Payload is Provision of military Satcom services over the whole visible Earth."]
[11.870063781738281, 0.9853136539459229, "The Planned Launch of the Chang'e-5 Lunar Probe is 2020."]
[12.129817008972168, 5.375403881072998, "The Composition of the Dark Matter Cosmological Component is ~27%."]
[8.664656639099121, 10.634418487548828, "The Imaging Area Pixels of the CCD Image Sensor is 600 x 600."]
[10.356322288513184, -0.8887125849723816, "The Microgravity Environment of the O/OREOS nanosatellite Satellite is Below 500 \u00b5g."]
[7.125235080718994, 9.208704948425293, "The Spatial Resolution of the MSI-0 and MSI-1 MSI Instruments is 32.5 m."]
[9.05615234375, 7.43111515045166, "The Energetic-Particle Detector of the Juno Spacecraft is Instrument."]
[7.2825026512146, 3.2696566581726074, "The Communication Status of the Robusta Satellite is No further communication has been received."]
[5.954960823059082, 5.358874320983887, "The Tracking Capabilities of the Phoenix receiver Navigation Device is Good."]
[8.591930389404297, 1.7275773286819458, "The Rob Gutro Article Date of the JWST Telescope is March 20, 2014."]
[12.145944595336914, 5.382787704467773, "The Composition of the Dark Energy Cosmological Component is ~68%."]
[7.755117416381836, 13.196755409240723, "The Pixel Resolution of the SPIM1 Spectrometer is 14 bit."]
[13.71667766571045, 1.6083734035491943, "The Mission Number of the Vega Launch Vehicle is 18."]
[4.453268527984619, 6.046143054962158, "The Frequency Band of the RF Communications Communication System is S-band for TT&C data."]
[8.73909854888916, 10.394896507263184, "The Detector Format of the Camera Imaging Device is 512 x 512 pixels."]
[12.023233413696289, 4.481462478637695, "The Discovery Year of the Blue Ring Nebula Nebula is 2004."]
[8.233104705810547, 3.016690492630005, "The Mission Purpose of the Euclid Satellite is Investigate dark matter and dark energy."]
[2.2619857788085938, 6.47784948348999, "The Latency of the ATL13 Inland Water Elevation Data is 45 days from receipt of last data in product."]
[7.610136032104492, 4.071901321411133, "The 3D Map Compilation Capacity of the DAICHI project Satellite Project is 150,000 maps per month."]
[1.5612831115722656, 4.570501804351807, "The Output Voltage of the Buck-Boost Converter Solar Array Regulator is 65 - 106.6 V."]
[3.2300119400024414, 4.875479221343994, "The Code Memory Storage of the CPU Board Processor is 3 MB of EEPROM."]
[8.172842979431152, 0.15891191363334656, "The Extension Date of the International Space Station Space Station is 27 April 2023."]
[1.934061884880066, 3.9007716178894043, "The Purpose of the SFINKS Solar Array is Test the efficiency of thin film solar arrays."]
[7.861859321594238, 9.01655387878418, "The Wavenumber of the Instrument Spectrometer is 4250\u20132630 cm -1."]
[8.304883003234863, 3.1131794452667236, "The Global DEM Production Completion Date of the TanDEM-X Satellite is September 2016."]
[3.6282997131347656, 6.2772722244262695, "The Data Rate of the S-band downlink system Communication System is 8 Mbit/s."]
[8.873058319091797, 2.026798725128174, "The Imaging Date of the New Horizons Spacecraft is July 14, 2015."]
[10.26848316192627, 2.895200729370117, "The Orbit Altitude of the MicroSat-2a Satellite is 514 km."]
[9.104201316833496, 8.07537841796875, "The Plastic Scintillator of the Range Calorimeter Particle Detector is 1cm thick."]
[6.19516658782959, 7.044614791870117, "The Function of the DDA Delay-Doppler Altimeter is Measure the across-track angle of the range measurement."]
[6.853073596954346, 4.916227340698242, "The Pollutants Monitored of the Copernicus Sentinel-5P Satellite is Nitrogen dioxide, ozone, formaldehyde, sulphur dioxide, carbon monoxide, methane."]
[3.968402147293091, 5.650918483734131, "The Uplink Rate of the ResourceSat-1 Satellite is 100 bit/s."]
[6.611692428588867, 10.682901382446289, "The Estimated SNR of the Band 4 Spectral Band is 544.65 \u00b1 88.66."]
[7.246007919311523, 0.36552733182907104, "The Deployment Date of the DarkCarb MWIR Payload Payload is 2022."]
[4.039691925048828, 1.1943331956863403, "The Mission Type of the CAPSTONE Satellite is Non-EO."]
[8.555699348449707, 10.72069263458252, "The Power Consumption of the MSU-100 Camera is 6.8 W."]
[8.557677268981934, 4.951807022094727, "The Ground Pointing Accuracy of the NEMO-HD Satellite is Approximately 260 m."]
[7.553529739379883, -0.4941907227039337, "The Resupply Mission Finish Date of the Cygnus Commercial Cargo Ship Cargo Ship is August 15, 2014."]
[4.668078899383545, 9.067513465881348, "The First Instrument Placement Date of the InSight Mars Lander is 19 December 2018."]
[8.04953384399414, 1.240376591682434, "The Meeting Date of the LunaH-Map Satellite is 20-22 October, 2015."]
[7.01100492477417, 1.250861406326294, "The Signing Date of the Statement of Intent Agreement is March 28, 2019."]
[6.2099432945251465, 7.7808332443237305, "The Polarization of the ICI-11 Radiometer is V, H."]
[11.80173397064209, 2.4211628437042236, "The Descent Distance of the OSIRIS-REx Spacecraft is About a half-mile (805 meters)."]
[10.23123836517334, 2.9890408515930176, "The Altitude of the ALL-STAR-1 Satellite is ~350-400 km."]
[5.8637003898620605, 5.720312595367432, "The Antenna Type of the Biomass Satellite is SAR antenna with a large deployable reflector."]
[4.054320812225342, 6.665149688720703, "The Delay Variation of the Ranging Channel Communication System is Varies slightly with RF uplink power and temperature."]
[7.222645282745361, 0.8534554839134216, "The Launch Date of the OPS-SAT Satellite is Unknown."]
[6.190303802490234, 3.7534260749816895, "The Purpose of the GFP Satellite Payload is FSS (Fixed Service Satellite), DBS (Direct Broadcast Satellite) and broadband missions."]
[2.8974621295928955, 6.763899326324463, "The Electrical Power of the CanX-2 S-band Transmitter/Transceiver is 5 W."]
[6.809678077697754, 3.0872647762298584, "The Mission Status of the OPS-SAT Satellite is Operational."]
[9.628789901733398, 1.0900672674179077, "The Mission Duration of the Kolibri-2000 Satellite is 45 days."]
[8.512195587158203, 10.113457679748535, "The Detector of the Telescope Optical Instrument is FDCCD (Full-depletion CCD)."]
[6.145824909210205, 5.353034019470215, "The Sensor of the TSX Satellite is X-band SAR sensor."]
[8.25059986114502, 9.317159652709961, "The Wavelength of the EUV Simulation Simulation is 80 nm."]
[9.035266876220703, 3.145148277282715, "The Orbit Type of the Euclid Satellite is Large-amplitude libration halo orbit."]
[5.868391036987305, 5.8824849128723145, "The f/d Ratio of the Reflector Assembly Satellite Component is 0.5."]
[7.156889915466309, 0.5354477167129517, "The Activation Date of the TOR Payload is February 16, 2009."]
[11.350736618041992, 1.0662720203399658, "The Orbiter Observation Duration of the Tianwen-1 Probe is One Martian year."]
[6.366231918334961, 4.899235248565674, "The Total Uncertainty Cone of the Alphasat TDP1 and Sentinel-1A Optical Link is Initially set to 2250 \u00b5rad and reduced to 1000 \u00b5rad."]
[8.02192497253418, 10.461263656616211, "The Image Rejection of the Image-Reject Mixer Mixer is > 40 dB."]
[9.200368881225586, 9.25282096862793, "The Ion Acceleration of the Extraction Lens Component is 20 kV."]
[8.753826141357422, 6.280655860900879, "The Folding Method of the Inflatable boom Component is Origami pattern."]
[3.5386996269226074, 4.617556095123291, "The FPGA of the AIM Reconfigurable Computing Hardware Device is Xilinx XQR4062XL."]
[4.731592178344727, 7.251399040222168, "The Data Reduction Factor of the GimmeRF Radio Instrument is About 2.4 x 10^6."]
[9.602036476135254, 7.388844966888428, "The Detector's Temperature of the EyeSat Satellite is 0\u00b0C."]
[6.292018413543701, 4.291338920593262, "The Science Objectives of the TROPICS Constellation of CubeSats is Relate the precipitation structure evolution, including the diurnal cycle, to the evolution of the upper-level warm core and associated intensity changes."]
[7.409637928009033, 3.9281182289123535, "The Imaging Modes of the TeLEOS-1 Satellite is Various."]
[10.395920753479004, 10.095497131347656, "The Input Power of the X-123SDD Detector is +5 VDC, 300 mA."]
[7.206420421600342, 6.733695030212402, "The Mission Status of the OCO-3 Instrument is Operational (nominal)."]
[10.392990112304688, -1.1171317100524902, "The Mass of the TurkSat-3USat Nanosatellite is ~ 4 kg."]
[8.530633926391602, 6.568770408630371, "The Boom Length of the SOSMAG Magnetometer is 1m."]
[9.222039222717285, 0.8329026699066162, "The Operation Duration of the FAST Program Technology Demonstration Program is Up to 12 months."]
[11.222508430480957, -1.0513900518417358, "The Unknown of the Reference Mass Material is Material that will not degrade in a LEO."]
[10.887277603149414, 7.232232093811035, "The Energy Range of the LAXPCs X-ray Proportional Counters is 3-80 keV."]
[8.109108924865723, 2.880828380584717, "The Mission Position of the IMAP Interstellar Mapping and Acceleration Probe is One million miles (1.5 million kilometers) away from Earth towards the Sun."]
[2.338449478149414, 4.425536155700684, "The Total Power of the Satellite Satellite is 161 W."]
[10.708772659301758, -1.559590220451355, "The Total Cargo Mass of the Dragon Resupply Vehicle Resupply Vehicle is 2490 kg."]
[7.35038948059082, 0.977584183216095, "The Mission Overview Date of the ICON Satellite is 3 Nov. 2017."]
[8.25721549987793, 2.9339094161987305, "The Science Goals of the Euclid Satellite is 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 a."]
[9.4849271774292, 1.0739927291870117, "The Campaign Duration of the KORUS-OC Korea-United States Ocean Color Mission is 18 days."]
[7.636150360107422, 1.5966659784317017, "The Date of the NASA's IMERG Shows Devastating Rainfall Over East Africa Event is 4 May 2018."]
[2.6913833618164062, 5.8540730476379395, "The Power Consumption of the Transponders Device is 2.7 W."]
[9.225303649902344, 2.258286237716675, "The Flybys of the BepiColombo Spacecraft is 9 (at Earth, Venus and Mercury)."]
[3.2392003536224365, 6.02568244934082, "The Architecture of the Frontier Radio Radio is SDR (Software Defined Radio)."]
[4.666349411010742, 4.779715061187744, "The Manufacturer of the CMC Transceiver Communication Device is ClydeSpace."]
[5.469728469848633, 3.1517934799194336, "The Bus Provider and Integrator of the ALTAIR and AQUILA satellites Satellite is Millennium."]
[8.76126480102539, 9.975637435913086, "The Dynamic Range of the Target Sensor Photodiode is Six orders of magnitude."]
[5.937385559082031, 1.557579517364502, "The Function of the HSRC Reentry Capsule is Demonstrate reentry technology and cargo recovery from the ISS."]
[6.9729437828063965, 2.8866207599639893, "The Operational Status of the WorldView-1 Satellite is Operational as of July 2022."]
[6.612416744232178, 9.997615814208984, "The Mass of the Pushbroom Imager Imaging Device is 380 kg."]
[5.603755950927734, 4.219886302947998, "The Function of the AutoConTM Technology is Automated EO-1's maneuver planning and formation control."]
[5.343697547912598, 5.623900890350342, "The Operation Modes of the TRSR GPS Receiver is C/A and P code, P-codeless (cross-correlation)."]
[7.401568412780762, 4.107447624206543, "The Receiver Type of the CryoSat Satellite is DIODE added another feature: inertial J2000 on-board position and velocity bulletins to be used by the AOCS."]
[10.362327575683594, 5.425267696380615, "The Plenum Pressure of the T3\u00b5PS Micropropulsion System is 4.5 bar."]
[11.811419486999512, 1.0629771947860718, "The Mission Duration of the Chang'e-4 Lunar Spacecraft is 2019."]
[9.807719230651855, 1.7176920175552368, "The Data Latency of the MetOp Satellite Satellite is 130 minutes."]
[9.460492134094238, -0.5481798052787781, "The Onboard Computers of the Nanosatellite Satellite is 2."]
[5.25007438659668, 5.054131507873535, "The Contact Attempt Options of the UFF TLE Data Product is Inertial Pointing or Scanning."]
[7.729781150817871, 1.135817050933838, "The Anomaly Updates of the Copernicus Sentinel-1B Satellite is 1."]
[9.95083999633789, 7.79381799697876, "The Energy Measurement Range for Nuclei of the Telescope 2 Telescope is 4-20 MeV/n."]
[5.229838848114014, 4.033290386199951, "The Hosting Location of the CTDA Component is GMES Security Coordination Center."]
[11.715669631958008, -1.1773585081100464, "The Propellant for Initial Orbit Raising of the Geo Satellite Satellite is 2 tons."]
[9.489935874938965, 8.745065689086914, "The Optics System of the Telescope Optical Instrument is Ritchey-Chretien type, with 2 aspherical mirrors and 3 folding mirrors."]
[9.22209644317627, 9.054329872131348, "The FOV of the Telescope Optical Instrument is 1.02 R sun \u00b1 2.7/3 R sun."]
[7.113195419311523, 5.036381244659424, "The Carbon Dioxide Absorption of the Earth's Forests Natural Feature is Around 8 Gigatons a year."]
[9.308826446533203, -0.5219290256500244, "The Source of Skills and Innovation for MDASat-i missions of the CPUT/F'SATI nanosatellite program Program is Yes."]
[11.801834106445312, 4.573610782623291, "The Size of the Manatee Nebula Supernova Remnant is Spanning the equivalent size of four full Moons."]
[7.9253387451171875, 9.620697975158691, "The Scanning Type of the Instrument Spectral Imager is 58 pixels / scan line, arranged in 2 x 2 arrays."]
[10.809749603271484, 5.82140588760376, "The Flare Intensity of the Solar Dynamics Observatory Satellite is X1."]
[7.165033340454102, 1.449066400527954, "The Date of the NASA\u2019s Exploration Enterprise Workshop Workshop is May 2010."]
[8.71882438659668, 5.192978858947754, "The Body-Pointing Capability of the Resurs-DK1 Spacecraft is \u00b1 30o into the cross-track direction."]
[11.41336727142334, 3.9001548290252686, "The Atmospheric Water Equivalent of the Mars Planet is Global layer 10 \u00b5m thick."]
[9.131111145019531, -0.5708662867546082, "The Launch Date of the Jugnu Nanosatellite is October 12, 2011."]
[7.088805675506592, 4.174680709838867, "The Instruments of the Meteor-M-2 Satellite is DCS, KMSS, IKFS-2, MTVZA-GY, MSU-MR, GGAK-M, Severyanin-M."]
[3.5852859020233154, 4.984943389892578, "The Redundancy of the MMU Memory Management Unit is Two MSM (Memory System Module) in cold redundancy."]
[5.272870063781738, 6.8957743644714355, "The Look Angle of the Antenna Conically-scanning reflector is 35.5\u00ba."]
[4.798222064971924, 6.681852340698242, "The Scan Mechanism Rate of the Antenna Subsystem Communication is 20.5 rpm."]
[6.370695114135742, 1.0587769746780396, "The Propulsion System Contract Date of the Skybox Imaging Company is Jan. 15, 2013."]
[7.767125606536865, 2.1467814445495605, "The Parachute System Qualification Team of the ExoMars Mission is ESA, TASinI, TASinF, Vorticity, Arescosmo."]
[12.092612266540527, 3.282841444015503, "The Orbit (Inclination) of the Spacecraft Satellite is 97.9\u00ba."]
[10.112846374511719, 6.871519565582275, "The Thermal Stability Requirement of the PAS Payload Assembly Subsystem is Better than 2 mK at fep (peak to peak value)."]
[6.1873626708984375, 3.5025763511657715, "The Objectives of the COTS 3 Mission is On-Orbit Operations \u2014 Approach, ISS \u2014 Attached Operations, On-Orbit Operations \u2014 Departure, Recovery."]
[6.523331165313721, 2.8183672428131104, "The Mission Type of the SPIDER Imaging Sensor is EO."]
[4.262837886810303, 5.6484575271606445, "The Downlink Modulation of the NEMO-AM Satellite is Variable."]
[5.5887627601623535, 3.491323232650757, "The Radiation Levels of the LEO Satellites Satellite is More amenable to Commercial-Of-The-Self (COTS) components of automotive or industrial grade."]
[6.096554756164551, 4.053562641143799, "The Data Relay of the TGO Satellite is NASA rovers."]
[7.051807880401611, 4.615611553192139, "The Detector of the GHGSat-C1/-C2 Satellite is IR camera."]
[3.6323869228363037, 4.625101566314697, "The Interval of Writing Timer Information to ROM of the MOBC Main On-board Computer is Unknown."]
[5.227794170379639, 6.775302410125732, "The Half-Power Half-Beamwidth of the High Gain Antenna Antenna is 4.0\u00ba."]
[10.253484725952148, 3.033318281173706, "The Orbit Altitude of the Primary Mission Satellite is 824 km."]
[11.760323524475098, 4.834636688232422, "The Energy Release of the Ophiuchus Galaxy Cluster Galaxy Cluster is Hundreds of thousands of times more than typical clusters."]
[6.224701404571533, 3.3464548587799072, "The Responsible Parties of the ESEO Satellite is ALMASpace and UniBO."]
[6.937382698059082, 6.041003704071045, "The Error Requirement of the Wind Speed Retrieval Algorithm Algorithm is 2 m/s or 10% of the wind speed, whichever is greater."]
[7.136758327484131, 9.647110939025879, "The Spectral Range (Band 2) of the MUX Instrument is 0.52-0.59 \u00b5m."]
[5.738030910491943, 2.7707083225250244, "The Developer of the skCube Satellite is SOSA (Slovak Organization for Space Activities ) ."]
[6.630378246307373, 4.138434886932373, "The Type of the BLITS Satellite is Ball Lens In The Space."]
[10.18936824798584, 3.027329683303833, "The Altitude of the LAGEOS Satellite is 5858 km x 5958 km."]
[8.097529411315918, 8.080965995788574, "The Manufacturer of the ALICE UV Spectrometer is SwRI."]
[3.8145737648010254, 5.62553071975708, "The Downlink Speed of the EV-9 Satellite is 2 Mbit/s."]
[9.320819854736328, 7.935972213745117, "The Cadence of the Fast Neutrons Measurement is In the range 1-20 MeV."]
[6.0419816970825195, 2.3211405277252197, "The Launch Site of the NigeriaSat-1 Satellite is Plesetsk, Russia."]
[9.330924034118652, -0.6465027928352356, "The Teamwork Importance of the AzTechSat Nanosatellite is Crucial."]
[5.054921627044678, 1.949607253074646, "The Number of Experiments of the ORS-3 Mission is 26."]
[9.220575332641602, 3.246471643447876, "The Orbit Type of the CBERS-2B Satellite is Sun-synchronous orbit."]
[6.898609161376953, 1.278227686882019, "The Collaboration Announcement Date of the Astrocast Satellite Operator is December 14, 2021."]
[8.68925952911377, 6.359101295471191, "The Deployment of the Origami booms Component is Straight-line."]
[10.477913856506348, 7.699492454528809, "The Material of the Gnome Chompski Space Component is Titanium."]
[11.87446403503418, -1.063180685043335, "The Launch Mass of the Ascent Vehicle Vehicle is Roughly 500 kg."]
[4.807229042053223, 4.890446662902832, "The Impact on ACS Algorithm Test-Replace Cycle of the Ground Station Ground Equipment is Almost twice as fast."]
[7.42937707901001, 9.726724624633789, "The Frequency of the VIS (red) Band is 460 THz."]
[6.800998210906982, 0.6191346049308777, "The Launch Date of the TechDemoSat-1 Satellite is 2014."]
[2.9502437114715576, 6.581408977508545, "The DC Power Consumption of the Channel Communication System is 50 W."]
[9.63496208190918, 6.023926734924316, "The Magnetorquer of the ADCS Attitude Determination and Control Subsystem is \u00b10.2 Am 2."]
[8.902060508728027, 2.1629445552825928, "The Mission Team of the New Horizons Spacecraft is 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, M."]
[9.357277870178223, 11.609495162963867, "The Pixel size of the Channel 8 Sensor is 48 km x 48 km."]
[6.82611608505249, 0.6117516756057739, "The Launch Date of the TeLEOS-1 Satellite is Dec 16, 2015."]
[9.135759353637695, 5.303223609924316, "The Attitude Control of the Payload Satellite Payload is 3-axis control."]
[3.2461955547332764, 4.834509372711182, "The RAM of the Model calculator Data Handling and Processing is 512 kB."]
[7.127853870391846, 9.169940948486328, "The Spatial Resolution of the Multispectral Instrument (MSI) Instrument is 20 m."]
[9.32813835144043, 10.379833221435547, "The Field of View of the LSI-1 Camera is 29\u00ba."]
[6.8264923095703125, 7.04550313949585, "The Concept Presentation of the ALTIKA Instrument is Unknown."]
[4.837976932525635, -3.3900957107543945, "The Member of the Liz Ritchie Individual is True."]
[4.326617240905762, 3.9159562587738037, "The Operation of the Automated Beacon Network Anomaly Detection System is Receives the health message."]
[9.824949264526367, 8.286765098571777, "The 3He Separation of the LET Low Energy Telescope is ~1%."]
[4.793187141418457, 3.304457902908325, "The Prime Objective of the ZACube-2 CubeSat is Demonstrate AIS (Automatic Identification System) message reception using its SDR-based payload."]
[5.868222713470459, 3.1194379329681396, "The Manufacturer of the SPL Deployment System is Astro und Feinwerktechnik Adlershof GmbH."]
[9.54782772064209, 9.104687690734863, "The Aperture Diameter of the Telescope Optical Instrument is 0.7 m."]
[10.504354476928711, -0.9981666803359985, "The Mass of the Tatiana-2 Microsatellite is 100 kg."]
[4.2674150466918945, 6.410761833190918, "The Redundancy of the Ka-band Channels Communication System is 1 standby channel (4 for 3 redundancy)."]
[7.282686710357666, 6.691679954528809, "The Satellite of the VIIRS Imaging Radiometer Suite is NOAA-NASA Suomi NPP."]
[5.41996955871582, 5.57070255279541, "The GPS Receivers of the TanDEM-X Satellite is Dual-frequency."]
[12.071160316467285, 3.2354586124420166, "The Coplanar Orbit of the Landsat 9 Satellite is Landsat-8, 180\u00ba apart."]
[4.762723922729492, 0.8550462126731873, "The Business Opportunities of the Satellogic Satellite Imaging Company is $2.1 billion in the near and longer term."]
[1.8603241443634033, 4.0421247482299805, "The Short Circuit Current of the CSS Solar Cells is 34 mA."]
[11.615974426269531, -1.1963907480239868, "The Total Mass of the Satellite Satellite is 110 kg."]
[7.121933937072754, 9.467371940612793, "The Band 1 of the CIRiS Instrument is 7.4 \u00b5m to 13.72 \u00b5m."]
[8.812040328979492, 9.388476371765137, "The Image Scale of the Galileo Spacecraft is 1.6 km/pixel."]
[5.743978977203369, 2.340874195098877, "The Size, Weight and Power (SWaP) of the Small Photon Entangling Quantum System (SPEQS) Quantum Light Source is Miniaturized."]
[11.76274299621582, 1.1314289569854736, "The Design Life of the Chang'e-3 Moon Lander is Exceeded by 14 months."]
[11.808501243591309, 1.0896000862121582, "The Landing Date of the Chang'e-3 Moon Lander is December 2013."]
[9.769805908203125, 5.524317264556885, "The Energy Storage Margin (60 minute window) of the RASP Maneuver Planning System is 62.9%."]
[7.681099891662598, 3.587165117263794, "The Headwaters of River of the Saskatchewan Glacier Glacier is North Saskatchewan River."]
[4.88523530960083, 1.8913295269012451, "The Quantity of the U.S. Weather Satellites Satellite is 2."]
[6.743395805358887, 4.492934703826904, "The Mission of the MTG-S Satellite is Sounding."]
[10.265887260437012, 4.9839253425598145, "The Acceleration of the iCPS engine Engine is 0.5 g."]
[3.7304508686065674, 6.064098358154297, "The Data Amount of the Experiment Data Telemetry is 130 Mbit."]
[6.247520446777344, 7.789610385894775, "The Polarization of the ICI-5 Radiometer is V."]
[7.184198379516602, 4.931779384613037, "The Instrument Type of the METIS Telescope is Multi-Element Telescope for Imaging and Spectroscopy."]
[6.037196636199951, 9.501603126525879, "The Mass of the STAFF/DWP Instrument is 5.0 kg."]
[9.807497024536133, 1.6173784732818604, "The Delivery Latency of the Tactical Mode Satellite Mode is Less than 30 minutes."]
[8.481621742248535, 3.2026102542877197, "The Formation Distance of the TanDEM-X and TerraSAR-X Satellites is 20 km."]
[8.973977088928223, 5.236828804016113, "The Attitude Control Accuracy of the BRITE spacecraft Satellite is better than 1.0\u00ba."]
[6.739315986633301, 4.114068508148193, "The Measurement Category of the Satellite EO is 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."]
[2.219352960586548, 6.515463829040527, "The Latency of the ATL17 ATLAS Atmosphere Monthly Data is 45 days from receipt of last data in product."]
[5.843044281005859, 3.051459312438965, "The Reflector Manufacturers of the Biomass Satellite is Harris Corporation (HC) and Northrop Grumman (NG)."]
[11.776206970214844, 4.539958477020264, "The Explosion Date of the Cassiopeia A Supernova Remnant is 320 years ago."]
[7.917248725891113, 9.99291706085205, "The Detector Line Arrays of the Whiskbroom Scanner Imaging Device is 16 for VNIR bands, 32 for PAN, and 8 detectors for TIR."]
[7.796597480773926, 0.673234224319458, "The First Earth Imagery Release Date of the UrtheCast Company is April 3, 2014."]
[2.924935817718506, 6.582936763763428, "The Power of the Travelling Wave Tube Amplifier Device is 20 W."]
[8.408623695373535, 2.5504612922668457, "The Orbit Raising of the ARTEMIS Satellite is In-Flight Experience with Ion Propulsion."]
[1.4666179418563843, 4.409365653991699, "The Operation of the BCR Battery Charge Regulator is Independent."]
[5.006383419036865, 4.377664089202881, "The Purpose of the LEO Network Communication Network is Minimize or eliminate the need for new satellite companies to develop their own ground network."]
[9.225586891174316, 5.4109578132629395, "The Attitude and Pointing Control System of the Skylab Space Station is Unknown."]
[7.231003761291504, 9.422253608703613, "The Spatial Resolution of the TopSAR wide Imaging Mode is 50 - 100 m."]
[8.141341209411621, 9.274343490600586, "The Detectors of the FTS Interferometer Interferometer is InSb, HgCdTe."]
[11.331077575683594, 1.5648443698883057, "The Distance Traveled of the Yutu 2 Lunar Rover is 600 meters."]
[7.0478997230529785, 3.8829152584075928, "The Purpose of the CIRAS Instrument is Demonstrate a critical science and meteorological measurement in a significantly smaller package enabling use in constellations for improved latency."]
[9.478157997131348, -0.38692182302474976, "The Mission Objective of the FASTRAC Satellite is Demonstrate two-way intersatellite crosslink with verified data exchange."]
[7.5844292640686035, 5.4204816818237305, "The Rainfall Impact of the OCO-2 Satellite is Increased carbon release."]
[7.995814323425293, 7.560043811798096, "The Monitoring Method of the Bioburden Monitoring System System is Essays taken at regular intervals."]
[6.330153465270996, 7.620656967163086, "The Polarization Directions of the POL Linear Polarizer is -60\u00b0, 0\u00b0 and +60\u00b0."]
[4.924513339996338, -0.06586720049381256, "The Launch Success Rate of the OneWeb Satellite Constellation is 100%."]
[8.935169219970703, 0.7534879446029663, "The Testing Duration of the JUICE Spacecraft is 1 month."]
[5.331806659698486, 10.33517074584961, "The Coverage of the International Space Station Space Station is Areas where thunderstorms are common."]
[6.8513641357421875, 3.273784875869751, "The Mission Status of the GRIFEX Satellite is Operational."]
[7.442609786987305, 1.203912615776062, "The Observation Date of the INTEGRAL Satellite is 27 Jan. 2009."]
[7.340151309967041, 1.0610644817352295, "The Office Launch Date of the ESA Organization is 9 February 2022."]
[9.842960357666016, 1.4712697267532349, "The Data Usage of the Iridium Constellation Satellites Satellite is Characterize the large scale FACs in both hemispheres on time scales of several hours or less."]
[9.09321117401123, 9.748323440551758, "The Viewing Angle Range of the POLO data set Image Dataset is -115\u00ba to +115\u00ba."]
[5.671444892883301, 9.21697998046875, "The Power of the HEPD Instrument is 2.0 W."]
[8.602616310119629, 5.583503246307373, "The Accuracy for 2000 kg payload of the IPS Pointing System is 0.4 arcseconds lateral and 11.2 arcseconds for roll under star tracker control."]
[6.338278770446777, 10.10340690612793, "The Mass of the LISS-4 Camera is 169.5 kg."]
[6.400950908660889, 1.613826036453247, "The Year of Launch of the Jason-2 Satellite is 2008."]
[8.089837074279785, 4.013878345489502, "The Moon Image Resolution of the Pleiades-1A and Pleiades-1B Satellites is ~300 m."]
[7.815013885498047, 1.4012609720230103, "The Cloud Profiling Radar (CPR) Transition to Operate Mode Date of the CloudSat Satellite is May, 20, 2006."]
[8.015003204345703, 3.849578619003296, "The Availability of the Pleiades System Satellite System is Close to 100%."]
[4.337029457092285, 4.39739465713501, "The Unique Label of the CAN Bus Data Communication is Yes."]
[8.070971488952637, 8.400229454040527, "The Number of Spectrometers of the SOLSPEC-ATLAS Spectrometer is 3."]
[7.841464042663574, 4.041448593139648, "The Maximum Acquisition Capability of the Satellite Imaging Satellite is 1800 images in a 24 hour period."]
[8.55859661102295, 6.66641902923584, "The | of the SFL Boom-Mounted Magnetometer Magnetometer is SFL boom-mounted magnetometer."]
[11.270872116088867, 3.7806215286254883, "The Comets Discovered of the SOHO Satellite is More than 3000."]
[7.577575206756592, 4.131460666656494, "The Image Quality of the SPOT 6 Satellite is Unknown."]
[8.477579116821289, 4.61592435836792, "The Observation Goal of the SHIMMER Satellite is Observe the equatorward edge of the polar mesospheric cloud (PMC) region."]
[10.856339454650879, 1.83517587184906, "The Total Maneuvering Mass of the Swarm-A Satellite is Approximately 80 g."]
[8.00263786315918, -0.7373515367507935, "The Mission Completion Date of the CRS-18 Dragon Spacecraft is 27 August 2019."]
[1.5579980611801147, 4.651469707489014, "The Load Regulation of the DC-DC converter Power Converter is \u00b11% from 40% load to 100% load."]
[5.408002853393555, 4.73598051071167, "The Geostationary Data Relay System of the Sentinel-1, -2 Satellites is EDRS (European Data Relay System)."]
[7.168994426727295, 3.0203311443328857, "The Unknown of the Universat-Tatyana-2 Small Spacecraft is Unknown."]
[10.124149322509766, 3.5156240463256836, "The Daily Atmospheric Profiles of the TOR Payload is About 250."]
[7.99981164932251, 7.089495658874512, "The Presentation Date of the Long-term stable internal calibration chain for a space-borne Integrated Path Differential Absorption LIDAR system Calibration System is Oct. 3-7, 2011."]
[5.0355658531188965, -2.3693788051605225, "The Affiliation of the Steven De Cuyper Engineer is Unknown."]
[5.375072002410889, 3.1982240676879883, "The Purpose of the AERO-VISTA Interactive Spectrogram Display Software is Scientific Operations of Twin 6U CubeSats."]
[11.67066478729248, 5.028268337249756, "The X-ray Source Obscuration of the The Teacup Quasar is Heavily obscured."]
[11.494230270385742, -1.312821865081787, "The Average Crust Density of the InSight Satellite is 2,582 kg/m3."]
[7.948748588562012, 3.7313232421875, "The Sensor Performance of the Landsat-7 Satellite is Not provided."]
[11.277107238769531, 6.586451530456543, "The Conference Presentation Date of the SEXTANT X-ray Pulsar Navigation Testbed is March 7-14, 2015."]
[5.651658058166504, 3.6322131156921387, "The User Platform Simulator of the LCRD Satellite is UPS."]
[6.163908958435059, 4.889873504638672, "The SAR Technology of the ICEYE Company is Synthetic Aperture Radar."]
[4.563342571258545, 6.189772129058838, "The Downlink Frequency of the CUTE-1.7+APD Satellite is UHF (437.505 MHz)."]
[4.090134620666504, 6.299441814422607, "The Bandwidth of the Spacecraft Repeater Communication Device is 46 kHz."]
[7.195954322814941, 0.18770049512386322, "The Planned Launch of the Resurs-P5 Satellite is 2023."]
[4.362008094787598, 3.978257179260254, "The Software of the TIE Payload is Payload Control (PLC) software."]
[3.170673370361328, 5.206636428833008, "The Power Consumption of the DSU Data Storage Unit is Significantly reduced compared to the traditional solid state mass memory solutions."]
[11.146095275878906, 2.0969467163085938, "The Drill Depth of the Rosalind Franklin rover Mars Rover is 2 m underground."]
[9.539572715759277, 0.5461372137069702, "The Service Life of the Prometheus Satellite Satellite is 3 to 5 years."]
[4.628116130828857, 2.177537202835083, "The Quantity of the TSAT CubeSat is 1."]
[6.696470260620117, 3.4088821411132812, "The Mission Type of the ExoMars TGO Satellite is Red Planet Investigation."]
[8.321063995361328, 5.308623790740967, "The Precision of the Satellite Position MOD is < 1.5 m (rms)."]
[11.682071685791016, 1.6184061765670776, "The Impact Point of the Vikram Lander Lander is Unknown."]
[7.024024963378906, 4.629677772521973, "The Camera Modes of the Optical Satellite Satellite is Multi-spectral pushbroom and RGB color video."]
[6.777027606964111, 1.8358981609344482, "The Conference Presentation of the UK Disaster Monitoring Constellation Satellite Satellite is ION 2003."]
[8.573192596435547, 10.52692699432373, "The Operation Mode of the CCDs Detector is Frame-transfer mode."]
[7.6115336418151855, 4.949080467224121, "The Sun sensors of the BEESAT-2 Satellite is Yes."]
[6.9307756423950195, 1.848185658454895, "The Mission Update Date of the GPM Core Satellite is Feb. 27, 2014."]
[11.548556327819824, 4.314794540405273, "The Size of the Kepler 11145123 Star is More than twice the size of the Sun."]
[7.717565536499023, 1.0307987928390503, "The Announcement Date of the Copernicus Sentinel-5P Satellite is May 04, 2020."]
[5.106751918792725, 4.278407096862793, "The Purpose of the COSMOS Software System is Support the development and operations of one or more small spacecraft throughout the life cycle."]
[9.415440559387207, 7.898609161376953, "The Temperature of the CCD Cooling Cooling System is -20\u00b0C."]
[10.019941329956055, 1.2126106023788452, "The Overhead Pass Time of the WorldView-1 Satellite is Approximately 13:30 hours local time."]
[8.520915985107422, 8.182650566101074, "The Gain Control of the MCP (Microchannel Plate) Detector Detector is Voltage applied across the MCP."]
[9.138004302978516, 1.3999055624008179, "The Realtime Data Availability of the SAPHIR Instrument is Since May 2013."]
[4.674224853515625, 6.861641883850098, "The Orbit Determination Accuracy of the DORIS Receiver is 0.2 m - 0.6 m."]
[10.567763328552246, 7.552922248840332, "The Material of the Canopy Satellite Component is 1/4 mil mylar."]
[5.036912441253662, 2.442274808883667, "The Signal Strength of the AAUSat-1 CubeSat is Very weak."]
[7.455769062042236, 0.942218542098999, "The Wind Sensor Failure Date of the QuikSCAT Satellite is Nov. 24, 2009."]
[11.733080863952637, 7.451023101806641, "The Mission Presentation Date of the Deep Space Atomic Clock Clock is Oct. 29- Nov. 2, 2012."]
[9.567605018615723, -0.5938863754272461, "The Avionics of the Microsatellite Satellite is PUNCH avionics."]
[5.810267448425293, 5.176443099975586, "The Tool of the GPS Spoofing Activity is STK (Satellite Tool Kit)."]
[11.683198928833008, 1.1498173475265503, "The Perigee of the Chang'e-1 Satellite is 200 km."]
[8.02358627319336, 8.609097480773926, "The Boresight Pointing Measurement of the OVIRS Spectrometer is With respect to an optical alignment cube on OVIRS."]
[9.253518104553223, -0.7373520135879517, "The | of the Aalto-1 Nanosatellite is Aalto-1 nanosatellite \u2013 technical description and mission objectives."]
[7.362671375274658, 8.228918075561523, "The Dynamic Spectrum Production of the SWAVES Instrument is 1 minute averaged."]
[9.146078109741211, 5.098566055297852, "The  Spacecraft control of the  Spacecraft Bus (Avionics Module=AM) Satellite is 3-axis stabilized."]
[10.782927513122559, 3.223553419113159, "The Distance from the Moon of the Satellite Spacecraft is 18,000 km."]
[5.616621494293213, 6.455780982971191, "The Array Width of the ICEYE SAR Antenna Antenna is 3.2 m."]
[8.658851623535156, 10.159741401672363, "The Dynamic Range of the Detector Imaging Device is 16 bit."]
[3.7205965518951416, 6.21502685546875, "The Speed of the Telemetry Data Data Transmission is 640 Mbps."]
[7.859708309173584, 8.316741943359375, "The Instrument Type of the ACE-FTS Instrument is Compact high performance instrument."]
[7.521237850189209, 9.990616798400879, "The Spectral Range of the Instrument Hyperspectral Imager is 0.4 - 2.5 \u03bcm."]
[6.052618980407715, 4.371091365814209, "The Hold Distance of the Canadarm2 Robotic Arm is 10 m."]
[6.647543430328369, 0.5840120911598206, "The Date of Malfunction of the MeteoSat-8 Weather Satellite is Oct. 17, 2002."]
[7.685858726501465, 2.2805404663085938, "The Objectives of the ExoMars Mission is 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."]
[10.134822845458984, 3.0453336238861084, "The Altitude of the Galileo Navigation Satellite is 23,222 km."]
[9.5347318649292, 3.6370596885681152, "The Mission of the Lunar Flashlight Satellite is Look for ice deposits and identify locations where resources may be extracted from the lunar surface."]
[9.518403053283691, 2.9639976024627686, "The Resonance of the Satellite Orbit Orbit is 3:1."]
[9.421008110046387, 5.001437187194824, "The Image Orientation of the Galileo Spacecraft is The north pole of the moon is to the right."]
[11.32619857788086, 6.782968044281006, "The Measurement Capability of the NICER X-ray Instrument is Neutron star's rotation rate."]
[9.259349822998047, 2.5643935203552246, "The Orbit of the ISS Satellite is Diurnal and sub-diurnal cycles."]
[8.842774391174316, 8.384976387023926, "The Calibration Method of the TIR Subsystem Calibration System is Light from the ground enters the TIR subsystem through the \u201cEarth window\u201d and is reflected into the imaging optics by a calibration mirror."]
[8.206596374511719, 1.9352554082870483, "The Solar Observation of the SOHO Satellite is March 19, 2015."]
[7.003036975860596, 0.7437613606452942, "The Launch Date of the QuickBird-2 Satellite is Oct. 21, 2001."]
[5.081066608428955, 7.156118392944336, "The Pixel Size (km x km) of the Antenna Reflector is 16."]
[5.2915849685668945, 6.408639430999756, "The Operating Band of the VDES Antenna Antenna is VHF maritime band."]
[3.790036201477051, 4.505805015563965, "The Type of the UT 699 LEON 3 FT microprocessor Microprocessor is UT 699 LEON 3 FT."]
[6.602299213409424, 6.302680015563965, "The Direction Accuracy of the SeaWinds scatterometer Scatterometer is 20\u00ba."]
[9.716014862060547, 1.194828987121582, "The Operational Autonomy Period of the Spacecraft Satellite is 24 hours."]
[11.082786560058594, 4.079840660095215, "The Kinematic properties of the IPD Interplanetary Dust is < 77 km/s."]
[6.994666576385498, 9.169166564941406, "The Ground Resolution of the P Mode Observation Mode is 2.29 m~0.98 m."]
[5.098385810852051, 7.593235492706299, "The Data Rate of the HI-SCALE Instrument is 160 bit/s."]
[4.561680316925049, 5.573813438415527, "The RF Communications of the Spacecraft Satellite is S-band for TT&C support."]
[9.056867599487305, 8.499598503112793, "The Rotation Range of the Pointer Mirror Device is 0 to 360\u00ba."]
[8.06207275390625, 9.805071830749512, "The Spectral range of the Optical System Imaging System is 0.37-0.45, 0.45-0.51, 0.58-0.68, 0.68-0.78, 3.55-3.93 \u00b5m."]
[11.002677917480469, 6.8095383644104, "The Quantity of Silicon Detectors of the NICER/SEXTANT Instrument is Not provided."]
[3.555636405944824, 5.504543304443359, "The Number of Nodes of the FODB Data Interface is 2 to 128."]
[10.418310165405273, 5.962297439575195, "The Observation Type of the RHESSI Satellite is Global wave generation."]
[2.1396944522857666, 4.175014495849609, "The Solar Cell Average Power of the S/C Satellite is 1.4 W."]
[2.2126364707946777, 1.7328165769577026, "The CCSDS ID of the GSAT-0208 Satellite is 268."]
[9.357306480407715, 1.7820285558700562, "The Data Playback Frequency of the SAMPEX Satellite is Twice per day."]
[8.082235336303711, 2.16896390914917, "The Date of the Impact Event SCI is 5 April 5 at 2:37 UT."]
[10.220002174377441, -0.8835045695304871, "The Mass of the Kestrel Eye II Microsatellite is ~50 kg."]
[8.416255950927734, 2.175183057785034, "The Current Location of the Voyager 1 Spacecraft is Interstellar space."]
[9.363120079040527, 0.8935084939002991, "The Operation Duration of the SWFO Satellite is 5 years."]
[7.704657554626465, 6.842939376831055, "The Function of the Hertz Chamber Test Chamber is Assess radio signals from antennas."]
[9.969209671020508, 5.004369735717773, "The Function of the Propulsion Subsystem Spacecraft Subsystem is Support trajectory maneuvers to L2 and maintain the halo orbit at L2."]
[11.852874755859375, 1.0049749612808228, "The Number of International Joint Collaboration Payloads of the Chang\u2019e-4 Mission is 3."]
[7.919538497924805, 1.1013438701629639, "The Testing Date of the Orion Spacecraft is May 11, 2016."]
[7.24376916885376, 1.6319198608398438, "The Discovery Date of the Cluster Satellite is Spring of 2009."]
[9.418852806091309, 11.53651237487793, "The Effective FOV of the Channel 8 Sensor is 21 km x 48 km."]
[3.8106203079223633, 2.242601156234741, "The Size of the PR-CuNaR2 CubeSat is 3U."]
[8.795785903930664, 0.2525070309638977, "The Spacewalk Duration of the UrtheCast Cameras Camera is Six Hours."]
[9.76844596862793, 7.132209300994873, "The Application of the Supercapacitor Energy Storage Device is Launchers and satellites."]
[8.849757194519043, 6.111734867095947, "The Applications of the Drag-Free Technology Technology is Navigation, Earth science, fundamental physics, and astrophysics."]
[2.371633529663086, 4.424775123596191, "The Power/energy provider for EDM of the TGO Satellite is Yes."]
[10.800397872924805, 3.3488609790802, "The Distance from the Sun of the Vigil Spacecraft is 150 million km."]
[7.362848281860352, 8.857714653015137, "The Detector Head Assembly Footprint of the Sounder Satellite Instrument is 10 km x 40 km."]
[5.191065788269043, 3.2299234867095947, "The Bus Type of the NorSat-1 Satellite is Next-generation satellite bus."]
[6.950954914093018, 0.3189741373062134, "The Launch Date of the Myriade/AstroSat-100 Satellite is 29 June 2004."]
[6.409510135650635, 8.521008491516113, "The IFOV/line (pixels/scan line) of the MWRI Microwave Radiation Imager is 240."]
[9.95130729675293, 1.4194319248199463, "The Return Link Delivery Time of the Galileo Satellite Constellation is A couple of minutes in the majority of cases, up to 30 minutes maximum."]
[6.727745056152344, 10.166022300720215, "The Primary Use of the Band 1 Spectral Band is Daytime clouds, ice and snow, vegetation."]
[4.8292646408081055, -3.395003318786621, "The Member of the Peter Cornillon Individual is True."]
[5.622803211212158, 3.569016933441162, "The Leveraging of the COTS technology Technology is Reuse of commercial design tools, foundry, processes, masks."]
[8.27631950378418, 9.769588470458984, "The Slew Rate of the TeLEOS-1 Imager Imaging Device is 2.5\u00ba/s."]
[10.204599380493164, 7.051757335662842, "The Thermal Isolation of the VGT-P Instrument is Multi-layer insulation (MLI) and titanium quasi isostatic mounting feet."]
[6.991987705230713, 7.910914897918701, "The Type of the POLAS-128 AOS Instrument is Polarization-sensitive Acousto-optic Spectrometer."]
[5.972089767456055, 6.669556140899658, "The Number of Beams of the SWIM Instrument Radar is 6."]
[11.326407432556152, 6.991664886474609, "The Time Accuracy of the NICER X-ray telescope Telescope is Better than 100 ns."]
[7.271678447723389, 5.42420768737793, "The Units of the CO2 Concentration Atmospheric Parameter is ppm (parts per million)."]
[11.792634963989258, 4.5175700187683105, "The Age of the Manatee Nebula Supernova Remnant is Around 30,000 years."]
[7.037013530731201, 0.5877171158790588, "The Launch Year of the IceEye-1 Satellite is 2018."]
[8.144583702087402, 5.604946136474609, "The UHF Lithium-1 Radio of the RAX-1 Satellite is Performed extremely well."]
[7.245813846588135, 0.177361860871315, "The Launch Year of the SWFO Satellite is 2025."]
[5.266245365142822, 5.046285629272461, "The Minimum Elevation Horizon Mask of the Panama ground station Ground Station is 3\u00ba."]
[11.531582832336426, 4.447962760925293, "The Galaxy Catalog Size of the Euclid Satellite is More than 2 thousand million galaxies."]
[5.95901346206665, 8.458651542663574, "The Operation Mode of the GeoSTAR Atmospheric Microwave Sounder is Continuous."]
[8.504524230957031, 6.832512855529785, "The Objective of the NewMag Magnetometer Experiment is Measure electrical currents and perturbations in the Earth's magnetic field."]
[5.148540019989014, 3.7876477241516113, "The Topology of the IXV Communications Network Network is Star."]
[3.7709150314331055, 5.5875115394592285, "The Maximum Data Volume of the ALOS-3 Satellite is 1400 Gbit per day."]
[6.845663547515869, 0.517747163772583, "The Testing Date of the GEOS-1 Satellite is Unknown."]
[7.553354263305664, 2.3529574871063232, "The URL of the ELSA-d IOD Mission is https://astroscale.com/missions/elsa-d/."]
[4.7638044357299805, 4.49464225769043, "The Operations Workflow of the Optical Inter-Satellite Links (OISL) Satellite Communication System is Joint concept for the ASA-S1A Optical Inter-Satellite Links operations, based on the two missions\u2019 planning cycle and operations execution scenario."]
[6.839817523956299, 0.7712147831916809, "The Launch Date of the SEOSat Satellite is Unknown."]
[7.426668167114258, 0.7911040186882019, "The First Light Image Date of the SeaHawk-1 Satellite is 22 March 2019."]
[6.41627836227417, -0.7284926176071167, "The Orbit Determination Accuracy of the QZS-1 Satellite is Sub-meter."]
[8.172036170959473, 0.6506635546684265, "The Launch Date of the Megha-Tropiques Satellite is 12 Oct 2011."]
[7.661530017852783, 9.787160873413086, "The Lava Area of the Image Data is Roughly 10 km2."]
[6.063473224639893, 2.734684467315674, "The Contact of the LAPAN Organization is Robertus Heru Triharjanto."]
[4.754151821136475, 1.9814624786376953, "The Number of Maneuvers of the SkySat-7 Satellite is 14."]
[11.19900894165039, 1.2861014604568481, "The Actual Mission Duration of the Jade Rabbit Moon Rover is 31 months."]
[10.3236665725708, 3.0194976329803467, "The Orbit Altitude of the ALMASat-1 Satellite is 354 km x 1450 km."]
[5.766551971435547, 9.322657585144043, "The Power of the HEED Instrument is 2.0 W."]
[4.115053653717041, 5.611190319061279, "The Emergency Support Data Rate of the IXPE Satellite is 32 kbit/s."]
[6.61500358581543, 7.673604965209961, "The Location of the Batteries Device is Below the laser."]
[11.54560375213623, 4.362723350524902, "The Oblateness of the Kepler 11145123 Star is Less than implied by its rotation rate."]
[7.120985507965088, 2.396592140197754, "The URL of the LUMIO CubeSat is https://iafastro.directory/iac/proceedings/IAC-18/."]
[9.423995018005371, 6.118471622467041, "The Type of the Attitude Determination System System is Histogram filter."]
[9.643064498901367, 7.282317161560059, "The Detector Module Temperature Change Limit of the Neutron-1 Spacecraft is 0.5\u00b0C/min."]
[6.487839221954346, 5.7795634269714355, "The Spectral Scans of the ISEE-3 Satellite is Two per second."]
[7.255304336547852, 2.9723734855651855, "The Meeting Location of the ICON Satellite is San Francisco, CA, USA."]
[6.698715686798096, 9.142892837524414, "The Dimensions of the CLARA Instrument Satellite Instrument is 114 mm x 141 mm x 155 mm."]
[6.743467807769775, 4.416693687438965, "The Mission Status of the Biomass Satellite is Approved."]
[5.918787002563477, 2.1572141647338867, "The Presentation of the Atlas V Aft Bulkhead Carrier & Operationally Unique Technologies Satellite Satellite is Workshop."]
[8.307552337646484, 5.273589611053467, "The Precision of the Satellite Position POD is < 10 cm (rms)."]
[7.96734094619751, 10.192643165588379, "The Methods of the Image Smearing Correction Image Processing is Fast readout, binning, skipping rows outside the region of interest, post-processing."]
[9.91502857208252, 1.63536536693573, "The Passes Less Than 150 Seconds of the GNOMES-1 Satellite is Less than 5% of passes are less than 150 seconds for either sets of ground stations."]
[8.597557067871094, 6.860016822814941, "The Principle of the Magnetometer Instrument is Magneto-inductive."]
[9.136833190917969, 5.232208251953125, "The On-orbit performance evaluation of the Propellant-free attitude control system Attitude Control System is Not provided."]
[7.329359531402588, 0.43922093510627747, "The Original Launch Date of the Spacelab-1 Satellite is Summer of 1980."]
[10.586969375610352, 7.292043209075928, "The URL of the SXI Imager is http://www.research.noaa.gov/spotlite/archive/spot_sxi.html."]
[8.74785327911377, 3.4268710613250732, "The Sun's Activity of the ICON Satellite is Quiet phase during solar minimum."]
[7.696298122406006, 8.542038917541504, "The Spectral Resolution of the OMPS Limb Profiler Spectrometer is 0.75 nm to 25 nm."]
[6.632511615753174, 4.590207099914551, "The Altitude of the FY-3 (FengYun-3) Satellite is +105."]
[5.689300060272217, 3.126814603805542, "The Regulator of the IMSO International Mobile Satellite Organization is GMDSS."]
[4.588351726531982, 5.807375431060791, "The Field of View of the Data Receiver Satellite Component is 15 \u00b5rad."]
[9.939933776855469, -0.9998290538787842, "The S/C Mass of the JL-1-GF03D Microsatellite is <45 kg."]
[11.289897918701172, -1.3057783842086792, "The Mass of the MicroSat-2a Satellite is 400 kg."]
[8.239012718200684, 8.385974884033203, "The Type of the GeoCarb Instrument is 4-Infrared channel, single-slit imaging spectrograph."]
[11.383086204528809, -1.3519365787506104, "The Mass of the Optsat-3000 Satellite is 368 kg."]
[9.0950345993042, 0.738789975643158, "The Duration of the Simulation Test is About 11 days."]
[6.996079444885254, 5.008646488189697, "The Purpose of the Global Carbon Cycle Earth Science is Understanding the global carbon cycle and how it responds to human and natural forcing."]
[9.832210540771484, 4.18778133392334, "The Attitude Control Duration of the Active solar or drag sails Deorbiting Device is Months or even years."]
[7.133297443389893, 4.557374954223633, "The Sensor Complement of the HJ-1B Satellite is Wide View CCD Cameras (WVC), Infrared Multispectral Scanner (IRMSS)."]
[8.677155494689941, 9.443543434143066, "The Enclosure Color of the VLF Receiver Receiver is White."]
[9.54468822479248, 0.5355047583580017, "The Design Life of the Genesis-2 Spacecraft is 5 years."]
[5.374882221221924, 3.1589155197143555, "The Services of the ALTAIR bus Satellite Bus is Navigation, propulsion, data processing and communications for the five TRACERS science instruments."]
[1.9105932712554932, 3.8430099487304688, "The Solar Cell Quantity of the TUBSAT-N Satellite is 34 cells per string."]
[7.696824073791504, 4.964011192321777, "The Instrument Types of the Solar Orbiter Satellite is In situ and remote sensing."]
[6.732542991638184, 4.14677619934082, "The Sea Level Rise of the Topex-Poseidon and Jason missions Satellite Missions is 3.2 mm per year."]
[8.258720397949219, 8.64493465423584, "The Detector Type of the WUPPE Spectrophotometer is Intensified diode-array."]
[8.461481094360352, 7.987009525299072, "The Wide Survey Coverage of the Euclid Reference Survey Survey is 15000 deg2."]
[4.95017671585083, -3.1871097087860107, "The | of the A. Gordon Emslie Author is A. Gordon Emslie."]
[5.368553161621094, 3.6319987773895264, "The URL of the IXV Spacecraft is http://esamultimedia.esa.int/multimedia/publications/ixv/offline/download.pdf."]
[10.17880630493164, 2.9889862537384033, "The Altitude of the CSG and CSK satellites Satellite is 620km."]
[6.038874626159668, 3.0182673931121826, "The Contractor of the BRITE-PL Satellite Project is UTIAS/SFL."]
[7.9122796058654785, 6.718228816986084, "The Observation of the FAUST Instrument is Galaxy clusters in the Virgo, Telescopium, Dorado, and Ophicus constellations."]
[7.860569953918457, 3.997816801071167, "The Number of Images Collected of the Landsat-9 Satellite is More than 57,000."]
[11.466667175292969, 4.739442825317383, "The Temperature of the Solar Corona Solar Feature is More than a million degree Kelvin."]
[6.720220565795898, 2.263234853744507, "The Lead Scientist of the GPM Satellite is George Huffman."]
[7.676509380340576, 1.5426851511001587, "The Launch Date of the SMOS Satellite is May 21, 2010."]
[6.574400424957275, 1.2701739072799683, "The Test Date of the ISIM Compartment is April 2013."]
[11.673768043518066, 2.624948024749756, "The Diameter of the Dimorphos Asteroid is 160 meters."]
[9.13650131225586, 10.57491397857666, "The Mounting Location of the VWFC Camera is Spacelab scientific airlock."]
[4.254302978515625, 4.822921276092529, "The Protocol of the Downlink Framer Communication System is CCSDS compatible protocol."]
[9.27556037902832, 10.325414657592773, "The Field of View of the CMOS Camera Camera is 58\u00ba."]
[9.375797271728516, 1.0219213962554932, "The Operation Duration of the RadSat Satellite is ~12 months."]
[8.956476211547852, 10.832808494567871, "The Band-3 Data of the LISS-4 Camera is Nominally observed and transmitted in mono mode."]
[5.876027584075928, 6.859339237213135, "The Pulse Duration of the SIRAL Radar is 50 \u00b5s."]
[8.593180656433105, 1.6325514316558838, "The Number of Radiation Belts Discovered of the Van Allen Probes Satellite is 3."]
[3.4814345836639404, 4.456953525543213, "The FPGA of the ACU Attitude Control Unit is Xilinx XC4VFX12-10FFG668I (Virtex4)."]
[4.825714111328125, 0.8902780413627625, "The Potential Cost of the Geomagnetic Storm Space Weather Event is Up to several trillion dollars."]
[5.760399341583252, 3.886759042739868, "The Locations of the POCs Instrument Operations Centers is 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)."]
[5.545262336730957, 1.3883808851242065, "The Landing Location of the Falcon 9 first stage Rocket is Autonomous spaceport drone ship."]
[7.53123140335083, 0.6030224561691284, "The Launch Date of the Cosmos-1066 (Astrofizika) Satellite is 23.12.1978."]
[5.9516215324401855, 1.703122615814209, "The Manager of the PAZ Satellite is HISDESAT."]
[4.512939453125, 4.132168769836426, "The Data Bus of the JWST Avionics Spacecraft Avionics is MIL\u2010STD\u20101553."]
[11.207697868347168, 2.851384162902832, "The Elevation Difference of the Burroughs Crater Crater is About 400 km."]
[7.897329807281494, 4.657909870147705, "The Spatial Resolution of the GK-2A Satellite is 2 km for the 10 infrared channels and 1 km for 6 visible channels."]
[3.9675891399383545, 5.743190288543701, "The Downlink Data Rate of the Satellite Communication System is 620 Mbit/s."]
[4.870139122009277, 1.969193935394287, "The Number of satellites per system of the WorldView-4 Satellite is 1."]
[4.342639446258545, 4.527435302734375, "The Components of the MCCM Multi-chip Control Module is Thin film passive circuits, MMIC low-noise amplifiers (LNAs), phase shifter and attenuator chips, ASICs and other discrete components for control and telemetry."]
[8.944862365722656, 4.775538444519043, "The Illumination of the Solar Panels Satellite Component is Provided during rotation."]
[3.4415998458862305, 4.588464260101318, "The Qualification Status of the Virtex-4 FPGA Data Processing Unit is Not space-qualified in Europe."]
[9.087289810180664, 6.533625602722168, "The Manufacturer of the Gyros Sensor is Analog Devices."]
[7.797743320465088, 9.255539894104004, "The Spectroscopy Range of the CUTE NUV Imaging Spectrograph is 255 to 330 nm."]
[10.014187812805176, 1.5093350410461426, "The Period of the Orbit Satellite is 99.31 min."]
[7.2169952392578125, 1.4568947553634644, "The Mission Start Date of the Eu:CROPIS Satellite is April 24, 2014."]
[9.009719848632812, 8.364259719848633, "The Stability of the Optomechanical System Optomechanical System is Athermal and actively temperature-controlled."]
[8.456603050231934, 10.51022720336914, "The Number of Lines of the CCDs Detector is 576."]
[7.814619541168213, 0.7112637162208557, "The Journal Publication Date of the OCEANSAT-2 Satellite is October, 2007."]
[10.873527526855469, 4.130940914154053, "The Primary Contribution of the Orbital Astronomical Observatories Telescopes is Enable humanity to explore beyond our frontier of knowledge."]
[11.975193977355957, 3.4175796508789062, "The Orbital Inclination of the International Space Station Satellite is Between 52 degrees north and 52 degrees south latitudes."]
[6.882808685302734, 1.2008455991744995, "The Presentation Date of the NPOESS Satellite is Oct. 4-8, 2004."]
[7.72113037109375, 9.731046676635742, "The Spatial Resolution of the SLSTR Imaging Device is 500 m."]
[6.713454723358154, 6.2658796310424805, "The Wind Direction Blur of the LG-mod Wind and Wave Information Calculation is 180\u00b0."]
[6.941835880279541, 5.415571689605713, "The Core Objective of the SMOS Satellite is Improving our understanding of Earth\u2019s water cycle."]
[6.986878871917725, 2.0965611934661865, "The Launch Date of the Konnect Satellite is 16 January 2020."]
[4.5810346603393555, 4.374837398529053, "The Issue of the Diagnostic Port Port is Beginning to separate the mechanical ground connectors from the PCB."]
[8.516926765441895, 10.168375968933105, "The Application of the CMT Imager is Support for Local Emergencies."]
[7.154542446136475, 0.23227401077747345, "The Launch Date of the Beijing-3 Satellite Constellation is 11 June 2021."]
[7.2131524085998535, 0.3399738073348999, "The Launch Date of the Beijing-1 Satellite is Oct. 27, 2005."]
[3.673874855041504, 6.288605213165283, "The Downlink Data Rate of the TT&C Communications RF Communications is Up to 8 kbit/s."]
[10.567911148071289, 8.5250883102417, "The Image Sequence Cadence of the COR1 Coronagraph1 imager is \u2265 1 min."]
[6.073795795440674, 11.249469757080078, "The Approx. peak sensitivity altitude of the Channel 1 Sensor is Unknown."]
[4.730905055999756, 5.539337635040283, "The Command Communication Band of the SWFO-L1 Satellite is S-band."]
[11.19894790649414, 4.676169395446777, "The Velocity before being Swallowed up by the Hole of the Earth-sized clump of matter Unknown is A third of the velocity of light."]
[9.156047821044922, 3.1963987350463867, "The Orbit Type of the EarthDaily Constellation Satellite Constellation is Sun-synchronous."]
[4.616357803344727, 5.911637306213379, "The Antenna Performance Verification of the Spacecraft Satellite is TRL 7."]
[9.345325469970703, 10.047842979431152, "The Function of the UrtheCast Camera System is Offer near-live images of Earth."]
[6.844803810119629, 3.0270886421203613, "The Payloads of the Orion Vehicle Spacecraft is Unknown."]
[7.108541488647461, 4.454785346984863, "The Measurement Domain of the FedSat Satellite is Gravity and Magnetic Fields."]
[6.558743953704834, -0.09185943752527237, "The Launch Date of the PSLV-C34 Satellite is June 22, 2016."]
[7.581277370452881, 2.2866322994232178, "The URL of the ExoMars Mission is http://exploration.esa.int/mars/48088-mission-overview/."]
[6.6919708251953125, 9.083062171936035, "The Envelope Dimensions of the MIRAD Instrument is 100 mm x 105 mm x 105 mm."]
[5.8836669921875, 6.728665351867676, "The PRF of the LRM Radar is 1-4 kHz."]
[9.407809257507324, 6.157859802246094, "The Purpose of the Attitude Determination Quaternion Filter Experiment is Perform spacecraft attitude tests in LEO."]
[6.027632236480713, 1.3549672365188599, "The Launch Date of the Ariane 5 ECA Launch Vehicle is August 2, 2012."]
[6.624729156494141, 0.3400941789150238, "The Retirement Date of the CBERS-2B Satellite is May 10, 2010."]
[7.1403117179870605, 9.648673057556152, "The Spectral Range (Band 3) of the MUX Instrument is 0.63-0.69 \u00b5m."]
[1.5799797773361206, 4.472531318664551, "The Topology of the Buck-Boost Converter Solar Array Regulator is Buck-Boost."]
[8.12552261352539, 3.014517068862915, "The Mission Position of the IMAP Interstellar Mapping and Acceleration Probe is First L1 (Lagrange point)."]
[7.628778457641602, 6.564333915710449, "The Typical Value of the AOD Satellite Instrument is 0.1-1."]
[5.643029689788818, 2.283926010131836, "The Technology of the OSCAR-QUBE Experiment is Diamond-based quantum technology."]
[5.52511739730835, 2.97137188911438, "The Task of the Restore-L Satellite is Lock on to it."]
[10.638492584228516, -1.6943124532699585, "The PLC Cargo of the HTV-7 Cargo spacecraft is 4.3 metric tons."]
[9.290315628051758, 8.952247619628906, "The FMC Mode Rotation Speed of the Telescope Optical Instrument is 0.6\u00ba/s."]
[5.38090705871582, 5.829658508300781, "The Antenna Configuration of the Satellite Satellite is Single downward pointing antenna."]
[4.8843560218811035, 0.937092661857605, "The Test Cost of the Modern ICs Electronic Components is >$46 M."]
[10.735477447509766, 10.292932510375977, "The Deadtime per trigger of the PHA Detector is 4\u201367 \u00b5s."]
[7.674515724182129, 9.471094131469727, "The Spectral Range of the M16 filter Infrared Filter is 11.5 - 12.5 \u00b5m."]
[9.118020057678223, 10.755274772644043, "The Resolution of the T1 Trigger Camera is 20 km x 20 km."]
[7.664060115814209, 7.914280414581299, "The Components of the Prime Instrument Ozone Monitor is Two nadir-pointing UV cameras, one operating with CCD detectors, the other with UV photodiodes."]
[10.151847839355469, 2.984839916229248, "The Altitude of the Satellite SuperView Constellation is 530 km."]
[7.1953630447387695, 8.625361442565918, "The IFOV/line (pixels/scan line) of the SBUS Solar Backscattering UV Sounder is 240."]
[8.69244384765625, 7.414509296417236, "The Thermal Capacitance of the Sensor Node Node is Large."]
[7.6120734214782715, 10.59970474243164, "The Sampling Frequency of the fADC A/D Converter is 80 MHz."]
[10.780813217163086, 5.692550182342529, "The Magnetic Field Profile of the Solar Flare Natural Phenomenon is Matched the theoretical prediction."]
[13.725430488586426, 1.609201192855835, "The Maiden Flight Date of the Vega Launcher is Feb. 13, 2012."]
[9.192584037780762, 4.1823954582214355, "The Height of the Nimbus-7 S/C Satellite is 3.04 m."]
[9.24606990814209, 4.151875019073486, "The Dimensions of the IMP-8 Spacecraft is 135.6 cm diameter and 157.4 cm high."]
[10.576382637023926, 8.49128532409668, "The Absolute Pointing Required of the COR1 Coronagraph1 imager is 7 arcsec."]
[6.698761463165283, 0.9127127528190613, "The Launch Date of the CFOSAT Satellite is 2018."]
[5.605498790740967, 7.000184535980225, "The Peak Transmit Power of the Radar Instrument is 500 W."]
[7.209466457366943, 6.231019496917725, "The Authors of the Aerosol Polarimetry Sensor Sensor is Richard J. Peralta, Carl Nardell, Brian Cairns, Edgar E. Russell, Larry D. Travis, Michael I. Mishchenko, Bryan A. Fafaul, Ronald J. Hooker."]
[5.14706563949585, 1.1638233661651611, "The Number of Satellites of the Terran R Launch Vehicle is Not Disclosed."]
[8.218231201171875, 4.626410961151123, "The Swath (nadir) of the Payload Satellite Subsystem is \u226530 km."]
[9.020259857177734, 5.169843673706055, "The Optical Performance of the Euclid Satellite is Very stable under extreme attitude changes."]
[11.035391807556152, 3.4072065353393555, "The Data Collected of the Juno Spacecraft is About three terabits."]
[5.890851020812988, 9.153295516967773, "The Power Consumption of the NewMag Magnetometer is 3 W."]
[7.3982672691345215, 0.42960676550865173, "The Phase C Review Date of the SVOM Satellite is Unknown."]
[2.3288614749908447, 4.440700531005859, "The Maximum Satellite Demand of the Satellite Satellite is 850 W."]
[1.232305884361267, 4.151514053344727, "The Battery Type of the HTV Spacecraft is Lithium ion."]
[11.306950569152832, 6.610931873321533, "The Mirror Module Assemblies URL of the IXPE Satellite is https://doi.org/10.1117/12.2531956."]
[3.430272340774536, 4.741955280303955, "The Memory of the AIM Reconfigurable Computing Hardware Device is 64 kbyte I/O space mapped into Xilinx FPGA."]
[2.224283218383789, 1.7536994218826294, "The Unique Identifiers of the LT Device is J and K."]
[11.862899780273438, -1.1051290035247803, "The Total Satellite Launch Mass of the Vega Rideshare Mission Satellite Launch is 1,327 kg."]
[9.212979316711426, 5.773009777069092, "The Attitude Sensing of the IRS-1C and IRS-1D Spacecraft is Star sensors, Earth sensors and gyros."]
[8.522581100463867, 7.82360315322876, "The Information Collected of the TechDemoSat-1's radiation monitor Radiation Monitor is Total ionizing dose, dose rate, and particle flux (protons and heavy ions)."]
[7.064253330230713, 1.1793535947799683, "The Launch Date of the BRITE-Austria Satellite is Unknown."]
[2.2516028881073, 4.511622428894043, "The Array Power Average of the DSX Spacecraft Payload Module Satellite is 650 W."]
[7.974174499511719, 5.3393659591674805, "The Accuracy of the GPS receiver Receiver is 50 m (1\u03c3)."]
[4.246662616729736, 4.414095401763916, "The Interface of the ACU Control and Data Handling Subsystem is CAN bus."]
[7.668905258178711, 0.09674540162086487, "The End of Life Date of the CXBN-2 Satellite is 1 March 2019."]
[11.756322860717773, 4.766220569610596, "The Type of the M83 Galaxy is Barred spiral galaxy."]
[7.828035831451416, 5.710326671600342, "The Instrument of the Cheops Satellite is Detector."]
[10.251702308654785, 6.851632595062256, "The Function of the Heat Pipes Thermal Control System is Transport waste heat to the radiator."]
[9.267561912536621, 2.606962203979492, "The Mission Objective of the DART Space Probe is Collide with an asteroid and deflect it from its orbit."]
[9.556527137756348, 4.02871036529541, "The Size of the REXJ Astrobot is Small as a microwave oven."]
[8.124649047851562, 4.598336696624756, "The Spatial Resolution of the Solid Earth Rifts Satellite is 100-500 km."]
[4.9805731773376465, 9.217447280883789, "The Health Check Date of the SEIS Seismometer is July 19."]
[10.802387237548828, 3.216421604156494, "The Earth-Moon Transfer Distance of the Probes Spacecraft is Up to 1.6 million km."]
[4.602555751800537, 4.936014175415039, "The Ground of the Data Transmission Process is Real time."]
[7.3532819747924805, -0.20844998955726624, "The Launch Date of the Atlas V Rocket Rocket is Dec. 6, 2013."]
[8.550619125366211, 10.408285140991211, "The Image Formats of the C3D2 Payload is Compressed and uncompressed."]
[11.176215171813965, 2.6046266555786133, "The Altitude Above Ground of the Lunar Landing Vehicle Vehicle is 4 m."]
[4.369098663330078, 5.028653144836426, "The Purpose of the TTTC Time-Tagged Telecommand is Commanding tasks with parameters and time tag."]
[6.6053466796875, 2.9776053428649902, "The Agency of the PhoneSat-1 and -2 Satellite is NASA."]
[9.35770034790039, -0.5771926641464233, "The Mission of the BRITE Nanosatellite Network is BRIght Target Explorer."]
[6.14722204208374, 0.5478841662406921, "The Launch Date of the PSat-2 CubeSat is June 25, 2019."]
[9.397159576416016, 0.7855756878852844, "The Project Duration of the ESEO Satellite is 1.5 years."]
[9.106630325317383, 5.853858470916748, "The Absolute Attitude Sensors of the PSSCT-2 Satellite is Aerospace-developed sun and Earth nadir sensors, plus COTS (Commercial-of-the-Shelf) magnetic field sensors from Honeywell."]
[11.551279067993164, 6.290759086608887, "The Science Data Processing Center of the XMM-Newton Satellite is XMM-Newton Survey Science Center at the University of Leicester, England."]
[7.538863658905029, 6.190924167633057, "The Purpose of the EMIT Imaging Spectrometer is Map the world\u2019s mineral dust source regions and provide information on the color and composition of dust sources."]
[7.40901517868042, 2.4955992698669434, "The URL of the Rosetta Satellite is http://sci.esa.int/rosetta/12198-new-louvers-ensure-that-rosetta-is-real-cool/."]
[11.771241188049316, -1.0438117980957031, "The Mass of the Sundancer Spacecraft is about 8,200 kg."]
[8.182278633117676, 1.5076184272766113, "The Release Date of the Wide-Field Imager for Solar Probe Plus Imager is July 2016."]
[3.6094672679901123, 6.246074199676514, "The Downlink Rates of the LLCD PAT Systems Communication System is 622 Mbit/s."]
[8.529512405395508, 6.443131923675537, "The Length of the Gravity-Gradient Boom Stabilization Device is 3 m."]
[6.421609878540039, 5.934071063995361, "The Radar Measurements Grid Resolution of the L2SMAP Soil Moisture Product is 9 km EASE-2."]
[3.6513731479644775, 2.246748685836792, "The Satellite Size of the OMS Radiometer Radiometer is 3U."]
[2.105879306793213, 4.534809589385986, "The Electric Power of the Satellite Spacecraft is 2.8 kW."]
[5.540868759155273, 4.33078145980835, "The Processes of the BJ3A1 satellite ground pre-processing system Data Processing System is 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."]
[8.019110679626465, 8.97214126586914, "The Calibration Lamp Wavelength of the Telescope Optical Instrument is 546.1 nm."]
[5.70289945602417, 3.818730592727661, "The Location of the Tracking and Control Center (TACC) Control Center is Tsukuba Space Center."]
[10.363333702087402, 2.804438591003418, "The Orbit Altitude of the ISS International Space Station is 405km."]
[9.575769424438477, 1.313165545463562, "The Connection Time of the Deployment Specialists Personnel is 11 hours."]
[6.611222267150879, 0.7219319939613342, "The Failure Date of the MWTS-2 Satellite Instrument is Feb. 2, 2015."]
[9.012104034423828, 8.952832221984863, "The Optics of the CASPR Experiment is iSIM-90 optics."]
[7.8028059005737305, 10.689589500427246, "The Data Quantization of the Instrument Hyperspectral Imager is 12 bit."]
[4.03291654586792, 10.35112476348877, "The NE\u0394T (K) of the ICI-3 Radiometer is 0.7."]
[2.2195563316345215, 1.7404886484146118, "The CCSDS ID of the GSAT-0209 Satellite is 269."]
[9.875554084777832, -0.21420297026634216, "The LTDN of the Tsubame Microsatellite is 11:00 hours."]
[7.587227821350098, 2.6196112632751465, "The Prototype Development Status of the ELSA-M Spacecraft Servicer is Ongoing."]
[5.773985862731934, 3.017801523208618, "The Avionics Subsystems Manufacturer of the CHORUS Satellite is Magellan Aerospace Corporation."]
[5.205733776092529, 3.702838182449341, "The Components of the Instrument Carrier Carrier is IOA, WFI, CGI, and the Spacecraft\u2019s Star Tracker/Inertial Reference Unit."]
[10.00401496887207, 2.986081600189209, "The Radius of the Orbital Phase 2 Orbit is Ca. 19 km."]
[9.5321626663208, -0.7389585971832275, "The Components of the PACE nanosatellite Satellite is COTS (Commercial off-the-Shelf) components as well as in-house developed parts."]
[11.376113891601562, 4.360267162322998, "The Temperature of the Jupiter's Atmosphere Planetary Atmosphere is Much higher than it is at the top."]
[1.2311135530471802, 4.159397125244141, "The NiH2 Batteries Capacity of the DSP satellites Satellite is 36 Ah."]
[9.745928764343262, 1.2970305681228638, "The TLE Maintenance of the Orbit Dynamic System System is 5.5 hours to 10 hours."]
[4.896601676940918, 7.190884590148926, "The Maximum Data Rate of the Instrument Satellite Instrument is 115 Mbit/s."]
[7.3327412605285645, 4.193699836730957, "The Camera Type of the GF-2 Satellite is PAN/MS."]
[6.591307163238525, 0.6101270914077759, "The Launch Date of the GovSat-1 Communication Satellite is 31 Jan 2018."]
[4.691044330596924, 2.2423064708709717, "The Quantity of the SMDC-ONE-2.3 and SMDC-ONE-2.4 CubeSats is 2."]
[9.056660652160645, 6.518654823303223, "The Update of the Accelerometer and Gyro Sensors is Before the first burn."]
[11.520870208740234, -1.3828226327896118, "The Mass (kg) of the ERS-2 Satellite is 2384."]
[6.084043502807617, 9.650574684143066, "The Mass of the DPU Digital Processing Unit is 9 kg."]
[8.33055305480957, 1.432979941368103, "The Expected Perihelion of the Comet ATLAS Comet is 31 May."]
[10.227740287780762, 4.862456321716309, "The Development Date of the Miniature Ion Propulsion System Propulsion System is Unknown."]
[8.773961067199707, 0.7742865681648254, "The Orbital Energy Source of the Juice mission Spacecraft is Earth, Venus and Mars."]
[7.3626837730407715, 4.129703521728516, "The Measurement Domain of the CryoSat Satellite is Ocean, Land, Gravity and Magnetic Fields, Snow & Ice."]
[7.214340686798096, 5.843671798706055, "The Degree of Coverage of the Partially Overlapping Contrails of the Model Atmospheric Model is Four times greater."]
[10.340044021606445, 9.307381629943848, "The Orbit Altitude of the IRIS Spacecraft is 620 km x 670 km."]
[8.942496299743652, 1.9702047109603882, "The Funding Cycle of the New Horizons Spacecraft is Every three years."]
[10.30408763885498, 9.5335111618042, "The Compatibility of the Iris Radio Communication Device is Deep-space and CubeSat."]
[8.09335994720459, 0.8470234274864197, "The Mission Operations Review Date of the Landsat 9 Satellite is Unknown."]
[7.617600440979004, 1.7674070596694946, "The Peak of the Drift Ice Season Natural Phenomenon is February."]
[9.06939697265625, 3.3790199756622314, "The Orbit Type of the MPO Spacecraft is Lower elliptical orbit."]
[8.269765853881836, 7.451827526092529, "The Radiometric Calibration of the OBA Instrument Component is Provided by views of blackbody and solar targets mounted on the yoke."]
[5.679811954498291, 2.1551873683929443, "The Orbit Count of the Envisat Satellite is 50,000."]
[11.884571075439453, -1.1323115825653076, "The Launch Mass of the Kanopus-V 1 Satellite is 450 kg."]
[3.0038304328918457, 6.623993873596191, "The RF Output Power of the Channel Communication System is 1 W per polarization."]
[7.41180944442749, 10.05759048461914, "The Spatial Resolution of the High-Resolution Hyperspectral Imager Imager is 30-meter."]
[7.154158592224121, 6.802755355834961, "The Meeting Date of the AMPERE System is December 14, 2010."]
[7.93981409072876, 0.7472228407859802, "The Date of the Mackenzie River Location is 01 October 2021."]
[6.726150035858154, 7.9373087882995605, "The Sample Rate of the MPO-MAG instrument Instrument is 128 Hz."]
[7.162418842315674, 9.62545394897461, "The Spectral Range (Band 4) of the MUX Instrument is 0.77-0.89 \u00b5m."]
[6.069766521453857, -0.06794251501560211, "The Deployment Start Date of the Galileo Second Generation Satellites Satellite is By 2024."]
[9.788403511047363, 1.5435738563537598, "The 25 hours of the Minor Cycle Duration Satellite Operation is Nine full minor cycles of 25 hours each."]
[11.502397537231445, 6.126415729522705, "The Number of Propellant Tanks of the XMM-Newton Satellite is 4."]
[7.326200008392334, 9.251775741577148, "The Transmission Profile of the FG Filtergraph is Unknown."]
[8.715805053710938, 7.85767126083374, "The Components of the INMS Ion and Neutral Mass Spectrometer is Front-end optics, post acceleration, gated time of flight, ESA (Electrostatic Analyzer) and CEM (Channel Electron Multiplier) or MCP (Micro Channel Plate) detectors."]
[9.056482315063477, 3.227836847305298, "The TLE Accuracy of the Orbit Dynamic System System is Low distance difference of the appropriate time zone."]
[9.00307559967041, 3.241994857788086, "The Orbit Type of the GNSS Satellites Satellite is Medium Earth Orbit (MEO)."]
[7.206077575683594, 0.5061707496643066, "The Launch Date of the ARMADILLO Satellite is 25 June 2019."]
[7.782933712005615, 10.892101287841797, "The Data Quantization of the DubaiSat-2 Satellite is 10 bit."]
[9.288264274597168, 0.8706011176109314, "The Maturity Prediction of the SPIDER Telescope is Five to ten years away from being fully matured."]
[10.2017240524292, 6.829973220825195, "The Application of the Loop Heat Pipe Radiator (LHPR) Heat Rejection Technology is Future spacecraft."]
[4.498154163360596, 6.774970054626465, "The Activation Window of the Experiment Data Telemetry is 1200 seconds."]
[9.219061851501465, -0.5608925819396973, "The Launch Date of the TechnoSat Nanosatellite is 14 July 2017."]
[8.165782928466797, 1.194582462310791, "The Release Date of the Dusty deities Image is 6 August 2018."]
[7.052576065063477, 4.223426342010498, "The Measurement domain of the Meteor-M-2 Satellite is Atmosphere, Ocean, Land, Gravity and Magnetic Fields, Snow & Ice."]
[8.966728210449219, 1.118691325187683, "The Planned Overlap of the Sentinel-6 Satellite is At least 6 months."]
[3.425913095474243, 5.64686393737793, "The Issue of the File Transfer Test Communication is Long strings of zeros in various places in each file."]
[6.653844356536865, 3.111945867538452, "The Mission Status of the OCSE Satellite is Completed."]
[12.950529098510742, 4.8636555671691895, "The Observation Duration of the IBEX Spacecraft is Six months."]
[6.701476097106934, 7.798361301422119, "The Activation Distance of the LIRIS Laser Infrared Imaging Sensors is 3500 m from the Space Station."]
[4.409021377563477, 6.405847072601318, "The Frequency Bands of the Communication System UAS Communication is Ku-/Ka-bands."]
[8.29367446899414, 1.483620524406433, "The Image Time Interval of the Rosetta Satellite is 25 and 27 February 2015."]
[8.198796272277832, 9.874850273132324, "The Body-Pointing Capability of the Pushbroom Imager Imaging Device is \u00b140\u00ba into the along-track and cross-track directions."]
[7.13087797164917, 5.63195276260376, "The Wind Profiling of the Aeolus Satellite is Yes."]
[5.000791072845459, 6.522704601287842, "The Stiffness Requirement of the COMMx Payload is 50 Hz or greater."]
[9.239277839660645, 8.437271118164062, "The Mirror Material of the SMA Scan Mechanism Assembly is Silicon carbide."]
[7.400116920471191, 0.7552838921546936, "The Announcement Date of the Boeing Pico-Satellite Mission Satellite Mission is April 19, 2007."]
[9.440042495727539, 5.042492866516113, "The Spin Rate of the AlSat Nano Satellite is Low."]
[4.777349472045898, 1.7526887655258179, "The Number of Satellites of the Satellite Constellation Satellite Constellation is 8."]
[3.8705365657806396, 4.38947057723999, "The Modification Time of the SCIP Processor is Too long."]
[3.7362730503082275, 6.235944747924805, "The Data Rate of the TT&C Telemetry Tracking & Command is 9600 baud."]
[10.003752708435059, 8.569737434387207, "The Angular Resolution of the ART-XC Instrument Telescope is HPD~ 30\u201d on-axis at 8 keV."]
[10.236554145812988, 2.9438021183013916, "The Altitude of the Spacecraft Satellite is 650 km."]
[8.783114433288574, 8.006486892700195, "The Developer of the Neutron Dosimeter Dosimeter is Germany."]
[10.282979011535645, 2.9575092792510986, "The Orbit Altitude of the SEOSat Satellite is 670 km."]
[3.9430344104766846, 6.163914680480957, "The Coverage of the TT&C System Tracking, Telemetry and Command System is Full spherical coverage in uplink and downlink."]
[5.444952011108398, 2.699737548828125, "The Manufacturer of the CIRiS CubeSat is Utah State University."]
[9.169912338256836, 10.571098327636719, "The Ground Resolution of the VIS Camera Camera is 150 m."]
[5.840658187866211, 2.9801487922668457, "The Provider of the LICIA CubeSat is ASI, the Italian Space Agency."]
[1.5837972164154053, 4.441629886627197, "The Solar Panel Connection of the Phoenix EPS Electrical Power System is COTS buck/boost voltage regulator."]
[8.51456069946289, 8.396451950073242, "The Number of Ground Receptors of the SafetyNetTM Data Collection Architecture is 15."]
[10.024582862854004, 3.9789559841156006, "The Mission of the NEA Scout Satellite is Reconnaissance of an asteroid, take pictures and observe its position in space."]
[7.427906513214111, 7.349557876586914, "The Award Date of the Ozone Monitoring Instrument Instrument is 1 April 2019."]
[9.371932983398438, 10.284374237060547, "The Orientation of the Metric Camera Camera is Open cargo bay oriented towards Earth."]
[5.569485664367676, 1.9942137002944946, "The Launch Vehicle of the COPPER CubeSat Satellite is Minotaur-1 of OSC (Orbital Sciences Corporation)."]
[7.1421122550964355, 0.9721844792366028, "The Mission Date of the LCROSS Satellite is May 31-June 4, 2010."]
[7.228517532348633, 10.215652465820312, "The Development and Launch Funding of the HyperScout 1 Hyperspectral Imager is Through the ESA GSTP program with contributions from the Dutch, Belgian and Norwegian national space organizations."]
[6.476144790649414, -0.6364802718162537, "The On-board and Ground Time Management System Presentation of the QZSS Satellite System is ION NTM (National Technical Meeting) 2007, San Diego, CA, USA, January 22-24, 2007."]
[3.966489553451538, 5.637471675872803, "The Payload Data Transmission Rate of the ResourceSat-1 Satellite is 105 Mbit/s."]
[6.9190754890441895, 4.953220367431641, "The Function of the Copernicus Sentinel-5P Satellite is Maps a multitude of air pollutants around the globe."]
[6.227804660797119, 8.497323036193848, "The Main Reflector Size of the MIS Instrument Microwave Radiometer is 1.8 m."]
[6.114787578582764, 5.459685802459717, "The Type of the L-SAR Instrument Sensor is SAR."]
[7.712577819824219, 0.5480234026908875, "The Forecast Duration of the JPSS Satellite Program is 3-7 days."]
[9.675182342529297, 4.625804901123047, "The Diameter of the Lorentz Chamber Testing Chamber is 2.8 m."]
[11.6773099899292, -1.1785142421722412, "The Mass (Wet) of the Satellite Satellite is \u2264 3200 kg."]
[4.42073392868042, 4.399170875549316, "The Components of the DEM (Digital Electronics Module) Electronics Module is ICU (Instrumental Control Unit) and a DPU."]
[9.007791519165039, 7.643671989440918, "The Components of the EPAM Electron, Proton, and Alpha-particle Monitor is LEMS (Low Energy Magnetic Spectrometers), LEFS (Low Energy Foil Spectrometers), CA (Composition Aperture)."]
[6.203091621398926, 7.7601776123046875, "The Polarization of the ICI-4 Radiometer is V, H."]
[7.648067474365234, 0.7825531363487244, "The Presentation Date of the ADM-Aeolus Satellite is April 24-28, 2006."]
[9.021740913391113, 5.367594242095947, "The Function of the Torque Rods Satellite Component is Apply constant open-loop dipole to counteract the body-fixed residual dipole disturbance torque."]
[6.260002136230469, 5.108310222625732, "The | of the AMISR Radar is http://isr.sri.com/iono/amisr/."]
[7.995927333831787, 5.638421058654785, "The Accuracy of the EO System Earth Observation System is 0.3%, k = 2."]
[7.30695915222168, 3.14296293258667, "The Instruments of the GEO-KOMPSAT-2A Satellite is Advanced Meteorological Imager (AMI) and the Korean Space Environment Monitor (KSEM)."]
[11.667009353637695, 4.520305156707764, "The Mass of the Zeta Puppis Star is 60 times more massive than our sun."]
[5.377191543579102, 5.637935161590576, "The Number of Satellites of the GPS Receiver Navigation Device is 4 or more."]
[5.001590251922607, 5.513784885406494, "The Cost Scaling of the Ground Station Network Communication System is Does not scale with the size of the satellites."]
[5.143905162811279, 6.575875282287598, "The Type of the RA/SCAT Antenna is Paraboloidal reflector antenna."]
[6.553515434265137, 2.7702646255493164, "The Communication Sessions of the Kolibri-2000 Satellite is Over 230."]
[5.808624267578125, 5.146386623382568, "The Program Start of the SIR-C/X-SAR Payload is MRSE (Microwave Remote Sensing Experiment) flown aboard the Shuttle on the first SPACELAB mission in l983."]
[7.102658271789551, 0.6022008657455444, "The End Date of the SRL-1 (STS-59) Mission is April 20, 1994."]
[5.1649346351623535, 4.918644905090332, "The Rotor Type of the Knudsen Station Ground Station is AlphaSpid's Big RAS rotor."]
[5.363940238952637, 10.33202838897705, "The Early-2024 of the Lightning Imager Data Availability is Data from the Lightning Imager will be available for operational use in early-2024."]
[9.484384536743164, 10.517884254455566, "The Aspect Ratio of the Iris Video Camera Camera is 16:9."]
[10.573535919189453, 8.54153823852539, "The Exposure Time Range of the COR1 Coronagraph1 imager is (0.1, 1)."]
[8.45681095123291, 10.522444725036621, "The Interface of the ROE Device is 3 CCDs."]
[5.891407489776611, 6.424098491668701, "The Pulse Transmission Rate of the SAR Synthetic Aperture Radar is 1,500 pulses/s."]
[6.9204277992248535, 3.741492748260498, "The Access of the Copernicus EMS Service is Planet\u2019s SkySat constellation."]
[5.485213756561279, 4.4974284172058105, "The Integration Status of the Instrument Flight Model System is Near completion."]
[10.179842948913574, 4.857640743255615, "The Type of the NEXT-C Ion Propulsion System is Solar electric ion propulsion system."]
[7.7978410720825195, 9.803508758544922, "The Swath width of the MERSI Medium Resolution Spectral Imager is 2800 km."]
[10.283618927001953, -0.8682242631912231, "The Total Mass of the Tsubame Microsatellite is ~ 49 kg."]
[8.365131378173828, 0.8921920657157898, "The Presentation Date of the OCAMS Camera Suite is March 18-22, 2013."]
[11.223149299621582, -1.511238694190979, "The Wet Mass of the Standard 3U CubeSat Satellite is < 3.78 kg."]
[4.075109481811523, 4.991762161254883, "The Redundancy of the OSDP Onboard Signal Data Processor is Fully redundant."]
[4.1781907081604, 4.764105319976807, "The Communication Standard of the OBC On-Board Computer is CCSDS (Consultative Committee for Space Data Systems) protocols."]
[10.65804672241211, -1.6923989057540894, "The Cargo Weight of the HTV-7 Cargo Vessel is 6200 kg."]
[8.433602333068848, 7.910861968994141, "The Boresight Direction of the MIRO Instrument is Aligned with the Rosetta payload line of sight."]
[10.135418891906738, 2.944183111190796, "The Altitude of the Yubileyniy-2/MiR Satellite is ~ 1400 km."]
[8.013338088989258, 3.2649500370025635, "The Ground Segments of the TanDEM-X Satellite is Mission Operations Segment (MOS), Payload Ground Segment (PGS), Instrument Operations and Calibration Segment (IOCS)."]
[10.275404930114746, 4.959303855895996, "The Manufacturer of the Resistojets Propulsion System is SSTL."]
[4.639015197753906, 6.137253284454346, "The Manufacturer of the Space Micro \u00b5STDN S-band Transponder is Space Micro."]
[12.003682136535645, 3.361335039138794, "The Orbit Inclination of the SpaceX CRS-17 Mission is 51.6\u00ba."]
[8.07988166809082, 3.4773612022399902, "The Mission Objectives of the Picard Satellite is Solar Diameter, Irradiance, Climate, Differential Rotation, Solar Constant and their variations."]
[6.670177936553955, 2.6438307762145996, "The Purpose of the Lucy Space Mission is Show us the diversity of the primordial bodies that built the planets."]
[5.474732875823975, 3.991776704788208, "The Task of the OPS&GRND Subsystem is Automate as much work as possible to simplify the future operation of the satellite."]
[10.252216339111328, 2.9413347244262695, "The Orbit Altitude of the Starlink Satellite Satellite is 550 km."]
[4.033767223358154, 1.1937099695205688, "The Mission Type of the DeMi Satellite is Non-EO."]
[11.487615585327148, 2.5181000232696533, "The Orbit of the Asteroid 1999JU3 Asteroid is From just inside the orbit of the Earth to just outside the orbit of Mars."]
[9.463407516479492, 0.6043898463249207, "The Predicted Operational Life of the SAR spacecraft Satellite is Three years."]
[10.881080627441406, 4.196781158447266, "The Mission Objective of the ARIEL Satellite is Measure the chemical composition and thermal structures of exoplanets, linking them to the host star\u2019s environment."]
[7.780240535736084, 7.200442314147949, "The Image Credit of the TEMPO Instrument is BATC."]
[10.58423137664795, 7.533358097076416, "The Structure Material of the SRMSat Satellite is Al-6061 alloy."]
[9.584975242614746, 1.120002031326294, "The Mapping Duration of the TIMED Satellite is 10 Years."]
[8.126248359680176, 1.0697556734085083, "The Start of Science Operations Date of the RAIDS Experiment is October 22, 2009."]
[8.382068634033203, 0.6409627795219421, "The Operation Start Date of the Hitomi Satellite is March 26, 2016."]
[0.9146162867546082, 4.197857856750488, "The Capacity of the Battery Energy Storage is 10.5 Ah."]
[11.708494186401367, 5.335675239562988, "The Progenitor Type of the GRB 130925A Gamma-Ray Burst is PopIII-like."]
[6.8139848709106445, 0.6178503036499023, "The Year of Launch of the TRMM Satellite is 1997."]
[9.49073600769043, 0.40380924940109253, "The Design Life of the SMDC-One Satellite is 1 year."]
[7.656054496765137, 0.25567519664764404, "The Presentation Date of the CXBN-2 Satellite is April 22-24, 2015."]
[10.271985054016113, 5.617656707763672, "The Date of the Electrodynamic Tethers for Space Propulsion Presentation is Jan. 12-15, 1998."]
[3.703648567199707, 6.197854995727539, "The 1024 bit/s of the TT&C Communications Telemetry Capacity is Telemetry capacity - 1024 bit/s."]
[7.775618553161621, 3.497711420059204, "The Imaging Capability of the ICON Space Mission is Provides the ability to separate the drivers and pinpoint the real cause of ionospheric variability."]
[6.559685230255127, 8.437216758728027, "The Antenna Size of the MWI Instrument is Moderate."]
[4.687495708465576, 1.767535924911499, "The Number of Satellites in Production of the Eurostar E3000 Satellite Platform is 6."]
[9.296944618225098, 4.233443260192871, "The Size of the LCRD Payload is About the size of a king-sized mattress."]
[7.1893510818481445, 0.25104761123657227, "The Launch Date of the Stingray Satellite is Early 2024."]
[4.929808616638184, 0.37273770570755005, "The Target for Researchers of the Silkworm Insect is Development of new silkworm strains for multiple purposes."]
[1.2451175451278687, 4.083916187286377, "The Battery Capacity of the Canopus Pipper Satellite is 2200 mAh."]
[7.733011245727539, 1.159129023551941, "The Announcement Date of the NASA Moon Mission Mission is Oct. 27, 2016."]
[11.279725074768066, 3.766824960708618, "The Number of Sun-grazing comets discovered by amateurs of the SOHO Satellite is Over 1100."]
[9.858153343200684, -0.8499525785446167, "The Deployment Date of the Kestrel Eye II Microsatellite is 24 October 2017."]
[5.624884128570557, 9.180529594421387, "The Power Usage of the Instrument Device is < 4 W."]
[5.863112926483154, 3.9744739532470703, "The Function of the CMS Constellation Management System is Analysis of orbit data and planning of orbit correction maneuvers."]
[4.75523567199707, 4.583131313323975, "The Purpose of Point-to-Point Communication of the MCS Communication System is Commanding."]
[6.705289363861084, 0.4137689769268036, "The Launch Date of the CBERS-2B Satellite is Sept. 19, 2007."]
[7.182934761047363, 5.74933385848999, "The Accuracy of Wind Velocity (Troposphere) of the Aeolus Satellite is 2-3 m/s."]
[7.386639595031738, 1.7748527526855469, "The Publication Date of the IceCube Satellite is 10 March 2021."]
[5.349889755249023, 5.788727283477783, "The Antennas of the SGR-10 Space GPS Receiver is Two antennas."]
[5.284215927124023, 3.4579477310180664, "The | of the Automatic Packet Reporting System (APRS) Satellite Communication System is | False."]
[6.363175392150879, 10.066232681274414, "The Mass of the PAN Camera Imaging Device is 200 kg."]
[4.698519229888916, 2.242997407913208, "The Quantity of the Hiber-1 and Hiber-2 CubeSats is 2."]
[9.403753280639648, 4.862042427062988, "The Canting Angle of the SAWs Satellite Component is -60\u00ba / 0\u00ba."]
[6.306574821472168, 2.825960874557495, "The Affiliation of the Harrison Agrusa PhD Student is University of Maryland."]
[9.44241714477539, 8.261279106140137, "The Retroreflector Coating of the Norton Satellite Component is Reflects both transmitted wavelengths."]
[10.244277954101562, 2.975191831588745, "The Orbit Altitude of the Landsat-9 Satellite is 705 km."]
[1.224238634109497, 4.176706314086914, "The Battery Type of the TUBSAT-N Satellite is NiCd."]
[7.9214582443237305, 1.8748619556427002, "The Planned Timeframe of the Mars Sample Return Mission Mission is Around 2028-30."]
[9.958858489990234, 6.499789714813232, "The Passive Temperature Control of the SVM Service Module is Mirror solar reflectors on the Sun-side, white paint on the anti-sun side."]
[6.974125862121582, 5.241943836212158, "The Indicators of the Atmospheric Measurements Climate Data is Surface temperature, water vapor, sea ice."]
[10.374829292297363, 5.025844097137451, "The Propellant of the Propellant Tank Tank is AF-M315E."]
[7.139505863189697, 0.5574702620506287, "The Launch Date of the EduSat Satellite is 2012."]
[9.559560775756836, 10.158712387084961, "The Design and Development Organizations of the MOMS Optical Camera is DLR, LMU, EADS Astrium GmbH."]
[3.402771472930908, 6.7426018714904785, "The TX Power of the Myriad RF board RF Board is Max. 10 dBm."]
[5.083658218383789, 6.166209697723389, "The Mounting of the S-band receive and transmit antenna Antenna is Nadir-facing deployable boom."]
[8.574555397033691, 6.916961669921875, "The Range of the . Magnetometer Instrument is \u00b1 100,000 nT."]
[6.904124736785889, 5.412195682525635, "The Expanded Applications of the SMOS Satellite is Monitoring and improving forecasting of large storms."]
[6.183363914489746, 1.608376383781433, "The URL of the PAZ and TerraSAR-X Satellite Constellation is http://www.dlr.de/dlr/en/desktopdefault.aspx/tabid-10081/151_read-7994/year-2013/%23gallery/12103#gallery/12103."]
[1.6472349166870117, 4.489386558532715, "The Components of the EPS Electrical Power System is COTS (Commercial-off-the-Shelf) components, MPTT (Maximum Power Point Tracking) ICs, FRAM (Ferroelectric Random Access Memory), AVR microcontroller."]
[4.05419921875, 5.957696437835693, "The Data Transmission of the VT Data Processing is Immediate downlink to the ground through the VHF network."]
[11.042704582214355, 7.154272556304932, "The Minimum Detectable Polarization of the HXCP Hard X-ray Polarimeter is 6.2%."]
[5.633013725280762, 3.2074241638183594, "The Operator of the CASA-212-200 aircraft Aircraft is Spanish National Institute for Aerospace Technology (INTA)."]
[7.275624752044678, 1.2036597728729248, "The Presentation Date of the GSC Missions Satellite Missions is June 6-7, 2012."]
[6.289995193481445, 8.255670547485352, "The Operating Frequencies of the SMMR Microwave Radiometer is 6.6 GHz."]
[11.76202392578125, -0.9827077388763428, "The Total Mass of the SILEX Terminal is 150 kg."]
[6.872233867645264, 0.5108597278594971, "The New Orbit Date of the SPOT-4 Satellite is Jan. 29, 2013."]
[7.0964741706848145, 8.828798294067383, "The Eastward Movement of the Band-64 Satellite Instrument is 17.4 km."]
[8.086857795715332, 2.6518518924713135, "The Launch Year of the TerraSAR-X Satellite is 2007."]
[4.514551639556885, 6.26236629486084, "The Antenna Type of the S-band Transmitter Transmitter is SFL-developed patch antennas."]
[8.164624214172363, 9.599991798400879, "The Image Scene Length of the Geoton-1 Imaging Instrument is Up to 2000 km."]
[6.35020112991333, 9.218724250793457, "The Internal Power Lines of the MuREM Radiation Monitor is +1.5V, +3.3V, -5V, \u00b110V, +20V."]
[9.454504013061523, 8.600789070129395, "The Sensor Type of the LPT Light Particle Telescope is Light Particle."]
[8.245905876159668, 9.167933464050293, "The Pixels per FWHM of the Spectrometer Instrument is 1720."]
[10.452461242675781, 8.389018058776855, "The Operating Modes of the Coronagraph Instrument is \"Video mode\" for display for the astronauts or TV transmission to the ground."]
[6.686788558959961, 0.7551683187484741, "The Launch Date and Time of the Spaceflight SSO-A: SmallSat Express Satellite is Monday, December 3rd at 10:34 a.m. PST (18:34 GMT)."]
[8.915729522705078, -0.3443444073200226, "The Deorbiting Requirement of the IDEA OSG 1 Satellite is IDEA OSG 1 should, after termination of its mission, attempt to deorbit in order to meet the 25 year debris mitigation guideline."]
[5.036722660064697, 6.21414852142334, "The Failure Cause of the S-band antenna Antenna is Lightning strikes."]
[11.58585262298584, 4.40905237197876, "The Circumstellar Gas Disk of the HD 172555 Star is Contains Exocomets."]
[4.55910587310791, 8.979545593261719, "The Solar Panels Lifespan of the InSight Mars Lander is Over four years."]
[9.843881607055664, 4.507547378540039, "The Type of the Terminator Tape Deorbit Module Deorbit Device is Passive de-orbit device."]
[5.987287998199463, 6.330304145812988, "The Swath Width of the SAR Synthetic Aperture Radar is 100 km."]
[6.845361232757568, 0.5463295578956604, "The Launch Date of the ST5 Satellite is 22 March 2006."]
[5.997866153717041, 6.357854843139648, "The SAR Payload Polarization of the RCM Satellite is Hybrid polarimetry."]
[11.325790405273438, 7.0400071144104, "The Background of the NICER X-ray timing instrument is < 0.2 counts/s."]
[8.556358337402344, 1.7209954261779785, "The Mission Status Date of the James Webb Space Telescope Space Telescope is Dec. 5. 2012."]
[10.411772727966309, -1.1346392631530762, "The Mass of the Dove-2 Nanosatellite is ~ 5.8 kg."]
[9.467732429504395, 3.0894622802734375, "The Largest Feature Size of the Eureca Satellite is 2 mm hole in the ESA/ERNO logo plate."]
[11.83346176147461, 1.060235857963562, "The Design Life of the Chang'e-4 lunar probe Lunar Probe is Three years."]
[5.334345817565918, 2.8896214962005615, "The Manufacturer of the CubeSat power module Power Control is Clyde Space Ltd."]
[6.615391254425049, 3.4145188331604004, "The Launch Vehicle of the NeuSAR Satellite is ISRO Indian Polar Satellite Launch Vehicle."]
[7.244633197784424, 7.640671730041504, "The Purpose of the HARP-2 Instrument is Improve OCI measurements."]
[6.254430770874023, 3.5004847049713135, "The Launch Site of the Aeolus Spacecraft is Kourou, French Guiana."]
[5.803986072540283, 3.815768241882324, "The Data Processing Center of the Satellite GFO is POC (Payload Operations Center) located at NavOceano (Naval Oceanographic Office)."]
[3.2384512424468994, 6.127275466918945, "The Size of the APL\u2019s Frontier radio Radio is Smaller than other deep-space radios."]
[3.9080452919006348, 5.572033882141113, "The Bandwidth of the OCM Payload is Not specified."]
[7.174091339111328, 6.868989944458008, "The EMC Qualification Date of the Instrument Satellite Instrument is Summer 2021."]
[7.926900863647461, 7.938861846923828, "The Measurement Target of the OCO-3 Spectrometer is Sunlight reflected off the Earth's surface."]
[6.899906635284424, 5.00980281829834, "The Data Collection of the Aqua Satellite is Cloud formation, precipitation, radiative properties, air-sea fluxes of energy, carbon and moisture, sea ice concentrations and extents."]
[10.462261199951172, 4.923151969909668, "The Weight of the HET-X Hall-effect Thruster is Less than 2 kg."]
[1.6607593297958374, 4.504914283752441, "The Redundancy of the EPS Electrical Power System is MPPT system and regulators had been duplicated."]
[10.338894844055176, 5.227018356323242, "The Quantity of the Propulsion Tanks Spacecraft Component is 2."]
[10.367375373840332, 4.910802364349365, "The Propellant of the GPIM Propulsion System is AF-M315E advanced green monopropellant."]
[9.255940437316895, 1.2302685976028442, "The Time Lost for Maneuvering of the Telescope Observation Equipment is Significant for tens of thousands of satellites."]
[6.364363670349121, 8.098601341247559, "The Bandwidth of the SCM Instrument is 10 Hz-8 kHz."]
[5.7525954246521, 6.2230329513549805, "The Radar Antenna Length of the Spacecraft Satellite is 16 m."]
[8.353499412536621, 4.2283430099487305, "The Contributions of the Cluster Satellite is Measurements of electric currents in space, revealed the nature of black aurorae, discovered plasma waves."]
[7.768191337585449, 0.7205549478530884, "The Image Acquisition Date of the DSCOVR Satellite is June 3 and June 4."]
[5.40401029586792, 3.7988803386688232, "The Implementation of the SIM Simulator is ESA SIMULUS Simulation framework."]
[6.057265758514404, 9.278651237487793, "The Mass of the RCU Radiometer Calibration Unit is 2.3 kg."]
[6.334620475769043, 1.0823334455490112, "The Program Date of the COSMO-SkyMed Satellite is May 18, 2001."]
[10.679060935974121, 5.293502330780029, "The Attitude Control of the CNAPS Propulsion System is 5\u00ba (3\u03c3)."]
[7.320137977600098, -0.7378333806991577, "The Validation Data Source of the CYGNSS Satellite is SFMR."]
[10.501424789428711, 6.4485087394714355, "The Spectroscopy of the RHESSI Imaging Instrument is Up to \u03b3-ray energies of about 17 MeV."]
[8.546695709228516, 10.568828582763672, "The Format of the Detector E2V CCD-22 (Frame Store) is 600 x 600 pixels."]
[2.539919137954712, 5.244236946105957, "The Power Consumption of the MCU Microcontroller Unit is 65 mA - active."]
[5.333132743835449, 1.319624662399292, "The First Stage Booster Flights of the Falcon-9 Rocket Rocket is 3."]
[6.933219909667969, 0.23521266877651215, "The Launch Date of the FY-3 (FengYun-3) Satellite is Sep 10, 2023."]
[8.69432258605957, 1.8411688804626465, "The Upgrade Duration of the Voyager 2 Spacecraft is About 11 months."]
[5.204922199249268, 5.644121170043945, "The Size of the Canberra DSN station Antenna is 70-meter."]
[5.915083885192871, 6.828488349914551, "The Azimuth Resolution of the Radar Sensor is 1500 m."]
[6.455405235290527, 4.015852451324463, "The Ground Segment of the CO2Image Satellite is Earth Observation Centre (EOC)."]
[5.855392932891846, 1.9828649759292603, "The Launch Vehicle of the CubeSat - Launch 4 Satellite is Dnepr."]
[7.5844621658325195, 1.1553717851638794, "The Observation Date of the Perseus Satellite is 29 October 2018."]
[7.375051498413086, 4.313842296600342, "The Calibration Approach of the Sentinel-1 Satellite is In-orbit."]
[8.177535057067871, 7.961273670196533, "The Function of the \u00b5CPT Spectrometer is Measure radiation flux."]
[3.800208568572998, 2.2938785552978516, "The Size of the NanoSatC-Br1 CubeSat is 1U."]
[8.429466247558594, 2.9500572681427, "The Purpose of the Euclid Space Telescope is Measure the shapes and distances of billions of galaxies."]
[8.082934379577637, 8.729330062866211, "The Optical Configuration of the ELVIS Spectrometer is Czerny-Turner."]
[6.188709735870361, 4.977035045623779, "The Host of the OSIRISv3 Instrument is ISS."]
[1.5445502996444702, 4.8279924392700195, "The Output Short Circuit Protection of the DC-DC converter Power Converter is Yes."]
[8.592034339904785, 6.8382720947265625, "The Design of the MAG Instrument Magnetometer is \"Dual mag\" implementation of two identical racetrack magnetometers on a 6-meter boom."]
[9.247638702392578, 10.07472038269043, "The Image Content of the LROC Camera is Earth and moon."]
[5.115342140197754, 4.492642402648926, "The Mission Ground Segment of the Ground Segment Communication is CLS network."]
[8.545897483825684, 1.6844265460968018, "The Test Date of the James Webb Space Telescope Space Telescope is Summer 2014."]
[4.464029312133789, 6.877853870391846, "The Antialiasing Filter Cut-off Frequency of the Rx Module Digital Receiver is 18 MHz."]
[5.9044647216796875, 4.984064102172852, "The SAR system of the Payload Satellite Payload is Nominal operations, no redundancy."]
[7.335276126861572, 6.788994789123535, "The Image Acquisition Date of the MODIS Instrument is May 5, 2022."]
[11.083120346069336, 2.528611183166504, "The Velocity Before Engine Shutdown of the Schiaparelli Lander is Nearly 270 km/h."]
[9.20467758178711, 7.76759147644043, "The Sensor System of the EPI-Hi Particle Measurement Instrument is Ion-implanted silicon SSDs."]
[9.18227767944336, 8.858912467956543, "The Subsystems of the CrIS Optical System is 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."]
[10.792126655578613, 1.836835503578186, "The Swarm Size of the Desert Locusts Insect is 40 million locusts."]
[7.8589959144592285, 9.50770378112793, "The Central Wavelength of the Spectrally modified current sounder Sensor is 8.5."]
[7.476778984069824, 6.021261692047119, "The Calibration of the Suomi NPP VIIRS Satellite is Unknown."]
[2.3313186168670654, 4.217992305755615, "The Power Experiment Conditions of the Scientific Payload Satellite Payload is Adequate Solar Illumination."]
[9.38316822052002, 6.878543853759766, "The Authors of the Wide-Field Imager for Solar Probe+ Imager is 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. DeJ."]
[6.723639488220215, 7.755927085876465, "The Optical Cavity Layout of the GEDI Laser Laser is 22 bounce slab and a GRM."]
[8.002532958984375, 7.156550884246826, "The Onboard Means of the Internal Calibration Calibration is 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."]
[11.176987648010254, 9.342717170715332, "The Spatial Resolution of the Earth Radiation Budget Experiment (ERBE) Instrument is 20 km at nadir."]
[5.852416515350342, 3.802730083465576, "The Control Center of the Aeolus Spacecraft is ESA's ESOC (European Space Operations Center) in Darmstadt, Germany."]
[10.913050651550293, 7.226263046264648, "The Angular Resolution of the JEM-X X-Ray Monitor is 3 arcmin."]
[3.999349355697632, 4.923198699951172, "The Redundancy Type of the Computer System Fault-Tolerant System is Cold redundant."]
[11.083060264587402, 4.558356761932373, "The Speed of the Reconnecting Jets Plasma Phenomenon is Up to 100 kilometers per second."]
[9.529480934143066, 0.7304130792617798, "The Mission Life of the Spacecraft Satellite is 1 year min (2 year goal)."]
[6.995069980621338, 5.932285785675049, "The Strongest Winds of the Tropical Cyclone Nathan Cyclone is 40 knots."]
[5.824795246124268, 1.9646376371383667, "The Manufacturer of the GomX-4B Satellite is GomSpace in Denmark."]
[7.287672519683838, 4.50311803817749, "The Band 6 of the Landsat TM Satellite is Plant heat stress, thermal mapping, soil mapping."]
[1.5675688982009888, 4.977972984313965, "The Instrument Mass of the SBVR Power Supply is 54.5 kg."]
[5.082656383514404, 6.250602722167969, "The Type of the Antennas Communication is Microstrip."]
[6.190563678741455, 3.854295015335083, "The Location of the SPIRE Instrument Control Center is RAL (Rutherford Appleton Laboratory, Didcot, UK."]
[6.936463832855225, 1.5685175657272339, "The Establishment Date of the GMES Initiative is 1998."]
[6.576664924621582, 4.67488431930542, "The Mission Goals of the Sentinel-6 Michael Freilich Satellite is Gather data for atmosphere information, climate change, and environment monitoring."]
[6.029411792755127, 8.925151824951172, "The Power Consumption of the MI Radiometer Radiometer is < 195 W."]
[4.8113226890563965, 5.663665294647217, "The Communication of the CAPSTONE Satellite is Two-way, coherent range and Doppler measurements."]
[11.20784854888916, 2.875685930252075, "The Orientation of the Burroughs Crater Crater is North is up."]
[6.991632461547852, 3.0190279483795166, "The Student Collaboration Goal of the IMAP Mission is Contributes to diversifying space science."]
[11.236638069152832, -1.499487280845642, "The Mass of the CubeSats Satellite is 14 kg."]
[9.142938613891602, 2.8512635231018066, "The Orbit Position of the GCOM-W1 Satellite is International A-Train orbit."]
[7.840587615966797, 1.7541676759719849, "The Launch Date of the ExoMars Mission is September 2022."]
[3.817134141921997, 6.207483768463135, "The Ground Station-pointing Mode Downlink Data Rate of the S-band system Communication System is Up to 204 MB/day."]
[3.5287582874298096, 2.302975654602051, "The Parasitic Bias of the Keithley 6430 Femtoammeter is <1 mV."]
[6.103686332702637, 3.33971905708313, "The | of the ESA Organization is ESA."]
[8.78339958190918, 6.951659679412842, "The Number of Magnetometers of the FIELDS suite Sensor Suite is 3."]
[8.359284400939941, 2.2429771423339844, "The Plasma Instrument Status of the Voyager 1 Spacecraft is Damaged during a fly-by of Saturn."]
[10.907394409179688, 3.357313632965088, "The Distance from Earth of the New Horizons Spacecraft is More than 5 billion miles."]
[5.978939533233643, 9.575751304626465, "The Total Mass of the IMS-2 Instrument is 199 kg."]
[7.238935470581055, 8.011381149291992, "The Resolution Time of the LAP Instrument is < 2 minutes."]
[6.883284091949463, 0.42012909054756165, "The Launch Date of the SARAL Satellite is 25 Feb 2013."]
[4.176662445068359, 4.625037670135498, "The Data Input Interface of the Modem Processor Signal-Processing Chain is SpaceWire over LVDS (Low Voltage Differential Signaling) link."]
[2.432863712310791, 6.354263782501221, "The Latency Requirement of the S-3 NTC Product is Within 28 days."]
[5.116751670837402, 6.274170398712158, "The Antenna Type of the CTAGS Antenna Array Antenna Array is Patch antennas."]
[7.1109161376953125, 2.6915695667266846, "The Overview of the Aditya I Satellite is URL: http://www.iiap.res.in/meet/sol2011/sol_ppt/RPrasad.pdf."]
[7.643573760986328, 8.553717613220215, "The Spectral Range of the SOSP Satellite is 170 - 3200 nm."]
[7.805735111236572, 7.942624092102051, "The Calibration Date of the SSBUV Solar Backscatter Ultraviolet is 1989 to 1993."]
[6.4096808433532715, 8.486700057983398, "The No of bands/channels of the MWRI Microwave Radiation Imager is 6."]
[6.440297603607178, 1.0690295696258545, "The Launch Site of the SEEDS-2 Satellite is SDSC (Satish Dhawan Space Centre), the SHAR launch range (Sriharikota, India)."]
[8.506464958190918, 1.0819971561431885, "The Release Date of the LRO Satellite is Nov. 16, 2011."]
[7.08068323135376, 5.167911052703857, "The Emission Sources of the CH4 Greenhouse Gas is Intense emission plumes from pipelines to large scale, weakly emitting wetlands and agricultural sources."]
[1.5754313468933105, 4.8755717277526855, "The Regulated Output of the EPS Electrical Power System is +5 Vdc."]
[3.5680627822875977, 2.2783610820770264, "The Size of the Phoenix Satellite is 2U."]
[7.070281982421875, 0.21569478511810303, "The Launch Date of the DMC-3 Constellation Satellite Constellation is July 10, 2015."]
[7.887165069580078, 6.7650885581970215, "The Frequency of the EMOC Process is Monthly."]
[9.153837203979492, 9.21821403503418, "The FOV of the Telescope Optical Instrument is 4.4\u00ba."]
[7.556334972381592, 8.158262252807617, "The S/C Subsatellite Point Travel of the AMSR-E Instrument is 10 km in 1.5 seconds."]
[9.598968505859375, 7.885383605957031, "The Energy Deposition of the RAMIS Radiation Detector is Minimal ionizing protons up to relativistic iron nuclei."]
[4.1102728843688965, 4.58722448348999, "The Interface Type of the Bus Interface Communication System is PCI."]
[10.507538795471191, 2.4629628658294678, "The Perigee (km) of the Meteor-2-1 Satellite is 872."]
[10.672085762023926, 5.297800064086914, "The Relative Position Determination of the CNAPS Propulsion System is 10 cm."]
[5.8853759765625, 6.258484363555908, "The Radar Antenna Length of the Copernicus Sentinel-1C Satellite is 12 m."]
[10.635903358459473, 9.239684104919434, "The Image Credit of the CaSSIS Imaging System is ESA/Roscosmos/CaSSIS."]
[9.4906587600708, -2.51080322265625, "The FOV of the LEICA Particle Detector is 24 x 20 \u00ba."]
[6.182333469390869, 3.690709352493286, "The Spacecraft of the MHS Instrument is MetOp-A spacecraft of EUMETSAT."]
[6.0483317375183105, 9.655861854553223, "The Mass of the Instrument Sensor is 25 kg."]
[6.829283714294434, 2.4166290760040283, "The Mission Status of the IMAGE Satellite is Cancelled."]
[7.633029937744141, 4.059210777282715, "The Additional Role of the CryoSat-2 Satellite is Measure the height of the surface of the sea."]
[5.849457263946533, 5.670344352722168, "The Instruments of the SARAL Satellite is A-DCS3, AltiKa."]
[6.601076602935791, 0.5557793974876404, "The Flight Experiment Date of the TUBSAT Satellite is Sept. 25-29, 2006."]
[9.215218544006348, 7.377927303314209, "The Sensor Operating Temperature of the FIPEX Instrument is Approximately 660\u00b0C."]
[6.90029764175415, 2.516850709915161, "The URL of the GeoEye-1 Satellite is http://launch.geoeye.com/LaunchSite/assets/documents/geoeye1_factsheet.pdf."]
[8.583900451660156, 6.895622253417969, "The Sensor Distance of the MAG Magnetometer is 80 cm apart."]
[11.770094871520996, 4.636183261871338, "The Temperature of the Cas A Supernova Remnant is 50 million degrees."]
[5.288232326507568, 5.049030780792236, "The Challenges of the LCRD Laser Communications Relay Demonstration is Susceptibility to cloud cover, scintillation, scattering and other atmospheric effects."]
[4.914549827575684, 1.652269721031189, "The Number of Private Launch Companies Prepared to Make First Attempts to Reach Orbit of the China Country is 4."]
[6.100988864898682, 6.269961357116699, "The | of the Advanced Modular Incoherent Scatter Radar Radar is The Advanced Modular Incoherent Scatter Radar (AMISR)."]
[6.958261966705322, 0.494817316532135, "The Launch Date of the GEOS-2 Satellite is 11 January 1968."]
[8.42276668548584, 10.579327583312988, "The Power Consumption of the Imager Imaging System is 85 W."]
[7.227682113647461, 5.1714067459106445, "The Measured Gases of the GeoCarb Satellite is CO2, CH4, CO."]
[7.363411903381348, 0.9438369870185852, "The Status Report Date of the PRARE Satellite Observation System is Sept. '90."]
[9.385196685791016, 8.966917037963867, "The Spatial Resolution & Stability of the Telescope Optical Instrument is Strehl ratio of ~ 0.86 at 2 \u00b5m."]
[10.291595458984375, -0.6732878088951111, "The Attitude Control of the O/OREOS nanosatellite Satellite is Permanent magnets and hysteresis rods."]
[7.03411865234375, 1.8748159408569336, "The Conference Presentation Date of the SJ-9 Technology Demonstration Satellite Satellite is Sept. 23-27, 2013."]
[8.949501037597656, 9.272313117980957, "The FOV Resolution of the HORUS Sensor is 5.35 arcsec."]
[9.448062896728516, 0.4977753460407257, "The Life Expectancy of the Almaz-1B Satellite is 5 years."]
[5.336410045623779, 2.0766825675964355, "The Mission Status of the Buccaneer CubeSat is Mission complete."]
[4.451735973358154, 2.5324549674987793, "The Incorporation of Laser Intersatellite Links of the Starlink Satellite Constellation is Undergoing Technology Improvements."]
[6.744740962982178, 10.167123794555664, "The Primary Use of the Band 3 Spectral Band is Heat source, night cloud."]
[2.2654120922088623, 4.385967254638672, "The Power Generation of the ALBus 3U CubeSat Satellite is 5 - 20 W."]
[4.04124641418457, 5.718775749206543, "The Command Uplink Data Rate of the NEMO-HD Satellite is 4 kbit/s."]
[9.397185325622559, 5.570313453674316, "The Description of the Inertial Attitude Control Mode (IRC) Control Mode is Provided spacecraft control using a propagated inertial quaternion."]
[11.728386878967285, -1.1390931606292725, "The Mass of the SAOCOM-1B Satellite is 3050 kg."]
[7.886218070983887, 3.266554355621338, "The Data Analysis of the ICON Satellite is First year of observations coincided with solar minimum."]
[11.218274116516113, 4.207566738128662, "The Confirmation of the Hot Jupiters Exoplanets is Across the galaxy and even in our stellar neighborhood."]
[7.576376438140869, 5.53660249710083, "The Materials for Photo-Electron Current Measurement of the HORYU-4 Satellite is Gold, KaptonR (polyimide), and Black KaptonR."]
[8.913243293762207, 9.533586502075195, "The Components of the Infrared Imager Sensor is Telescope, filter wheel, optical focal plane assembly, cryostat, video proximity electronics unit, payload control unit, X-band payload telemetry chain."]
[9.517572402954102, 4.408725261688232, "The Workspace Volume of the Research Facility Facility is 15 cubic feet."]
[8.54310417175293, 9.233756065368652, "The Slit 1 Material of the MEGS-A Spectrograph is Mo/C."]
[7.209836483001709, 1.0682401657104492, "The Mission Support Start Date of the RRA RetroReflector Array is 1 May 2002."]
[4.857839107513428, 1.9823225736618042, "The Number of Satellites of the BDS-3 Satellite System is 30."]
[1.237784504890442, 4.54578161239624, "The Battery Voltage of the EPS Electrical Power Subsystem is 4.2 V."]
[7.974154472351074, 1.933963418006897, "The Discovery Date of the ExoMars Trace Gas Orbiter Spacecraft is February 10, 2021."]
[9.57096004486084, 2.949103832244873, "The Resonance Ratio of the Satellite Orbit Orbit is 3:1."]
[7.848390579223633, 1.0256385803222656, "The Release Date of the Haa Alif Atoll, Maldives Location is June 5, 2014."]
[4.165186882019043, 4.609854698181152, "The Processor of the ICM Instrument Control Module is Leon ll processor."]
[10.534847259521484, -1.0711795091629028, "The Power Supply System Mass of the Microsatellite Satellite is 1.9 kg."]
[7.598005294799805, 1.6803098917007446, "The Presentation Date of the MICROSCOPE Spacecraft is Oct. 2-6, 2006."]
[9.053228378295898, 1.1473712921142578, "The Image Processing Time of the SMOS Satellite is Less than a second."]
[8.650618553161621, 8.870174407958984, "The Filter Type of the NUV channel Spectrometer is Block with Aluminum."]
[7.142500877380371, 0.5407354831695557, "The Launch Date of the RHESSI Satellite is Jun 13, 2012."]
[7.187457084655762, 1.9527368545532227, "The Study Purpose of the SJ-10 satellite Satellite is Enhance the comprehension of fire mechanism under microgravity."]
[4.640192985534668, 1.6680914163589478, "The Total Satellites of the Planet Satellite Operator is 149."]
[9.02938175201416, 10.674857139587402, "The Spatial Resolution of the LISS-4 Camera is 5.8 m."]
[7.880155563354492, 9.0127534866333, "The Wavelengths of the Spectrometer Instrument is 1020, 940, 600, 525, 453, 448, and 385 nm."]
[8.636948585510254, 1.7898699045181274, "The Spacecraft Operations Location of the Spitzer Space Telescope Telescope is Lockheed Martin Space in Littleton, Colorado."]
[13.105807304382324, 4.050998210906982, "The Measurement of the Gaia Satellite is The trajectory of the Solar System."]
[7.591418266296387, 8.022408485412598, "The Signal-to-Noise Ratio of the Atmospheric-sounding instrument Spectrometer is High."]
[8.905949592590332, 4.779703140258789, "The Platform Orientation of the Sich-2 Satellite is Sun-oriented in standby mode."]
[9.228544235229492, 10.545378684997559, "The Field of View of the Trigger Camera Camera is Wide."]
[8.655502319335938, 6.41935396194458, "The Direction of the Wire Boom Deployment System is Counterclockwise."]
[6.237216472625732, 3.2849643230438232, "The Agency of the FedSat Satellite is CSIRO, CRCSS."]
[7.248288154602051, 9.441905975341797, "The Swath Width of the Stripmap Imaging Mode is 20 - 40 km."]
[3.8836607933044434, 6.4536638259887695, "The Uplink Frequency of the TT&C Data Communication is 2089 MHz."]
[4.802135467529297, 5.746465682983398, "The Transient Classification of the FORTE Satellite is Rf transients in space using digital signal processing and neural network techniques."]
[5.3275909423828125, 4.270806312561035, "The Ground Systems of the CU-E3 Satellite is Two separate ground systems."]
[3.858447551727295, 2.3243257999420166, "The CubeSat Size of the FITSat-1 Satellite is 1U."]
[6.981425762176514, 4.861389636993408, "The Mission of the MicroCarb Satellite is MicroCarb mission: a CNES initiative for monitoring the CO2 exchanges."]
[8.55441665649414, 10.492822647094727, "The Mode of the EPIC CCDs Imaging Device is Photon counting mode."]
[11.121050834655762, 2.4720115661621094, "The Structure of the Schiaparelli Module is Aluminum sandwich with CFRP skins."]
[7.905230522155762, 4.991473197937012, "The Tracking System Position of the MMS Satellite is Far side of Earth."]
[7.087890625, 4.983981132507324, "The Monitoring Capability of the Satellite Constellation Satellite Constellation is Daily facility-scale methane monitoring."]
[5.885903835296631, 2.437547206878662, "The URL of the Iridium NEXT Satellite Constellation is http://multivu.prnewswire.com."]
[9.489055633544922, 0.5854952335357666, "The Available Consumables Lifetime of the Spacecraft Satellite is 7 years."]
[5.980302333831787, 9.556477546691895, "The Mass of the Instrument Interface Module Interface Module is 75 g."]
[6.820914268493652, 5.822601795196533, "The Daily Soundings of the GeoCarb Instrument is ~10,000,000 soundings per day."]
[8.553848266601562, 10.249822616577148, "The Architecture of the DU Detector Unit is Figure 37."]
[4.875339984893799, 2.0512044429779053, "The Quantity of the SmallSats Satellite is 38."]
[9.366177558898926, 8.900219917297363, "The Maximum Elevation Slewing Rate of the OCTL Telescope is 10\u00ba/s."]
[9.709490776062012, 6.915908336639404, "The Alpha (\u03b1) of the FCA Flow Control Assembly is 0.2."]
[2.292741298675537, 4.009705543518066, "The Service of the Maxar Space Solutions Company is Providing a high-power solar electric propulsion spacecraft chassis."]
[9.4557466506958, 2.891288995742798, "The Altitude of the GCOM-W1 Satellite is 699.6 km."]
[4.785312652587891, 0.836762011051178, "The Contract Award of the York Space Company is $382 million."]
[8.284406661987305, 7.8193206787109375, "The European Principal Investigator of the MIRI Instrument is Gillian Wright."]
[11.441695213317871, 4.174755573272705, "The Speculated Size of the Planet Candidate Exoplanet is The size of Saturn."]
[8.785831451416016, 4.36637544631958, "The Image Type of the Image Data is 360\u00b0 colored image of the Milky Way."]
[10.745573997497559, 3.8507637977600098, "The Temperature of the Farside Hemisphere Moon's Hemisphere is Cooler."]
[10.367465019226074, 8.350701332092285, "The Purpose of the Telescope-coronagraph 132 \u00c5 Telescope is Imaging hot plasma (T ~ 10 MK) of the solar corona."]
[7.429029941558838, 0.91996830701828, "The Operation Completion Date of the DAICHI (ALOS) Satellite is May 12, 2011."]
[9.9091157913208, 3.565967082977295, "The Neutron Moderation of the Lunar Regolith Regolith is More enriched in hydrogen."]
[6.0082879066467285, 3.460700035095215, "The Platform Series of the GovSat-1 Communication Satellite is Advanced GEOStar-3."]
[3.8104896545410156, 4.478282928466797, "The Processor of the SCP Spacecraft Process Controller is Honeywell 1750A processor."]
[7.699298858642578, 5.835056304931641, "The Natural Targets for Calibration of the EarthCARE satellite Satellite is Sea surface, Desert."]
[10.276163101196289, 4.950194358825684, "The Thruster Quantity of the GPIM Propulsion System is 5."]
[7.274620532989502, 9.265148162841797, "The Operation Life of the FG Filtergraph is Unknown."]
[6.89045524597168, 2.4997177124023438, "The URL of the PSLV Satellite is https://spaceflightnow.com/2018/01/12/pslv-c-40-coverage/."]
[5.606185436248779, 2.1780929565429688, "The Mission Count of the Solar Terrestrial Probes (STP) Program Program is 5."]
[10.41124153137207, -1.0114176273345947, "The Launch Mass of the GHGSat-D Microsatellite is 15 kg."]
[0.9982430338859558, 4.1867451667785645, "The Quantity of the Lithium-cobalt cells Energy Storage is 8."]
[11.504671096801758, 4.135225772857666, "The Mass of the Kepler-442b Exoplanet is About twice the mass of the Earth."]
[9.493480682373047, 5.2304158210754395, "The Solar Elevation Angle in TC Operation of the Instrument Satellite Instrument is < 40\u00ba."]
[11.095341682434082, 4.288815975189209, "The Cosmic Ray Susceptibility Occurrences of the Kepler Spacecraft is Four."]
[7.693793773651123, 1.4722832441329956, "The Date of the Rain Drenches Kauai Event is 2 May 2018."]
[6.582033634185791, 2.65071964263916, "The Destination Count of the Lucy Space Mission is Unknown."]
[8.422850608825684, 5.008333683013916, "The Minimum SNR of the NEMO-HD Satellite is 75."]
[9.401639938354492, 3.512518882751465, "The Launch Date of the CanX-6/NTS Satellite is Apr. 28, 2008."]
[4.792015075683594, 4.372378826141357, "The Functions of the FMC FOS Monitoring and Control is Segment monitoring and G/S interfacing."]
[5.008082389831543, 7.488526344299316, "The Contact Number of the Randomizer for High Data Rates Device is 20959/07/D/MRP."]
[7.745605945587158, 9.029484748840332, "The Spectral Resolution of the Optical Scanning Design Imaging Spectrometer is 1.25 nm."]
[4.810965061187744, 2.487534284591675, "The Spacecraft Type of the ARMADILLO Satellite is Nanosatellite (3U CubeSat)."]
[5.428308486938477, 5.587001800537109, "The Tracking of the TRSR GPS Receiver is Dual-frequency code and cross-correlation, data output of up to eight GPS satellites simultaneously."]
[7.61873197555542, 0.709398090839386, "The Overview Meeting Date of the CLARREO Mission is October 20-22, 2009."]
[3.586764097213745, 2.2860970497131348, "The Size of the AeroCube-8B Satellite is 1.5U."]
[5.295015811920166, 3.25628924369812, "The Manufacturer of the Nauka Laboratory Module is RSC Energia."]
[8.854368209838867, 5.020832061767578, "The Commanded Rate of the MicroSCOPE Satellite is 5 x 10-3 rad/s around the X-axis."]
[11.327251434326172, -1.4165840148925781, "The Mass of the E1P-2 CubeSat Satellite is \u2264 1 kg."]
[10.471528053283691, 8.411153793334961, "The Modes of the Instrument Coronagraph is Four."]
[7.704287528991699, 8.104059219360352, "The Observation Data of the TANSO-3 Ground Segment is AMSR3."]
[10.475074768066406, 2.477750778198242, "The Perigee (km) of the Cosmos-1066 (Astrofizika) Satellite is 848."]
[9.396385192871094, 9.954031944274902, "The Design of the APD Optical Radiation Detector is Compact, lightweight, mechanically hard, low power consumption, high quantum efficiency."]
[9.211014747619629, 5.121542453765869, "The Control of the Satellite Spacecraft is Full 3-axes and continuous drag-free satellite control."]
[7.6501078605651855, 4.49807071685791, "The Cameras of the Hypatia Satellite is Sub-meter multispectral and 30 m hyperspectral."]
[3.527480363845825, 4.1004252433776855, "The Analog channel of the STRV-1d DHS Data Handling System is Sixteen."]
[5.004298210144043, 6.096242427825928, "The Frequency L2 of the GPS receiver Receiver is 1227.6 MHz."]
[7.351795673370361, 1.8956828117370605, "The Mission Update of the Gravity Probe B Satellite is Nov. 12, 2009."]
[7.542843818664551, 2.5506045818328857, "The Launch Date of the KOMPSAT-3A Satellite is April 14, 2015."]
[11.568053245544434, -0.9386203289031982, "The Mass of the Service Module Spacecraft Component is 35 ton."]
[4.410120964050293, 4.798052787780762, "The Function of the Signal Processor Signal Processing System is Works only when the MAPMTs and the APDs detect a signal simultaneously."]
[1.4109340906143188, 4.183324813842773, "The Battery Energy of the Satellite Spacecraft is 60 Ah."]
[4.783954620361328, 1.6755090951919556, "The Maximum Satellites Launched of the Falcon 9 Rocket is 15-16 to an inclined orbit, \"something like 13\u201d to a polar orbit."]
[4.108902454376221, 4.974754810333252, "The Location of the SDC Redundant operations capability is LASP."]
[6.956613540649414, 11.282554626464844, "The Wavelength FWHM of an unresolved line of the Spectrometer Instrument is 0.124 \u00b5m."]
[7.216421127319336, 0.6592921614646912, "The Year of Launch of the Aqua Satellite is 2002."]
[7.396734714508057, 7.695291996002197, "The Long-term Stability of the Ozone Measurement Instrument Atmospheric Measurement Device is 1% over 7 years or better."]
[4.642209053039551, 9.05336856842041, "The First Selfie Date of the InSight Mars Lander is 11 December 2018."]
[7.943534851074219, 4.186098575592041, "The Coverage Area of the Ikonos Imaging Satellite is More than 400 millionkm2."]
[10.189595222473145, 5.3698296546936035, "The Valve Upgrade of the Propulsion System Satellite Component is Number and Flow Capacity."]
[3.7836227416992188, 5.667385578155518, "The Data Transfer Capability of the CASCADE Satellite Communication System is Large digital data files (10s to 100s of GBytes) within hours."]
[4.783074855804443, 4.89230489730835, "The Main Control Capabilities of the Antenna Satellite Component is Providing the TM (Telemetry), Processing the TC (Telecommands), Controlling the switching on/off of the active subassemblies."]
[6.234617710113525, 3.4994924068450928, "The Ground Stations of the Herschel Spacecraft is New Norcia (Australia) and Cebreros (Spain)."]
[7.540388584136963, 8.489910125732422, "The Radiometric SNR of the Instrument Spectrometer is 400 at the bottom of the limb to 40 at the top."]
[8.44498348236084, 7.154296875, "The Type of the PWI Instrument is Plasma Waves Investigation."]
[4.0720343589782715, 5.7939066886901855, "The ISL Data Rate of the CanX-4&5 Satellite is 10 kbit/s."]
[3.7807974815368652, 4.466344356536865, "The CPU Model of the OBC On-Board Computer is LEON2-FT."]
[8.480819702148438, 4.697775363922119, "The Method of the Cluster spacecraft Satellite is 3D electric field measurements."]
[7.876010894775391, 5.163023948669434, "The Instrument Speed of the MMS Satellite is Incredibly fast."]
[5.04723596572876, 7.550629138946533, "The Data Rate of the HID Instrument is 0.64 kbit/s."]
[10.884934425354004, 4.240442752838135, "The Maximum Velocity of the Dust Accelerator Testing Facility is Up to 60 km/s."]
[5.300981044769287, 2.227530002593994, "The Formation Flying of the DelFFi Satellite is QB50 Constellation."]
[7.560328006744385, 4.58456563949585, "The Tracking Direction for Geostationary satellites of the NEOSSat and Sapphire Satellites is Antisolar direction."]
[6.948036193847656, 0.6985107660293579, "The Service Start Year of the Satelles PNT Service Provider is 2016."]
[7.372270584106445, 7.304999351501465, "The Purpose of the COWVR Radiometer is Forecast ocean surface winds."]
[6.761171340942383, 10.141741752624512, "The Primary Use of the Band 8 Spectral Band is Ocean color."]
[11.695780754089355, -1.1228091716766357, "The Mass of the Payload Satellite Subsystem is 3.00 kg."]
[3.9415266513824463, 6.5700860023498535, "The Uplink of the Miniaturized X-band transponders Communications System is 1 kbit/s."]
[6.997678756713867, -0.010285197757184505, "The Installation Date of the STP-H7 and H8 Scientific Payloads is Unknown."]
[7.798714637756348, 7.68636417388916, "The Observation Capability of the MIGHTI Instrument is Day and night."]
[9.220808029174805, 2.8385605812072754, "The Dimensions of the GCOM-W1 Satellite is 5.1 m (X) x 17.5 m (Y) x 3.4 m (Z)."]
[8.258668899536133, 4.269935131072998, "The Image Span of the Herschel Satellite is Over 1\u00ba on the long side."]
[6.343311786651611, 7.252536296844482, "The Resolution of the Altimeter Sensor is About 0.9 m."]
[4.464605331420898, 5.043010234832764, "The Conference Date of the SOTA Optical Transponder is May 11-13, 2011."]
[9.195054054260254, 6.075001239776611, "The Function of the SSTs Stellar Star Trackers is Derive the satellite attitude."]
[6.683645248413086, 3.0316433906555176, "The Operating System of the PhoneSats Satellite is Android."]
[6.93778133392334, 1.7482221126556396, "The Conference Presentation Location of the Earth Observation System of the Republic of Kazakhstan Satellite System is Beijing, China."]
[9.173135757446289, 4.263586044311523, "The Bus Height of the OSAM-1 Satellite is 14-foot-tall."]
[5.2464094161987305, 6.761831760406494, "The Frequency Compatibility of the TUC Transponder Microwave Transponder is European and international altimetry missions in the microwave range."]
[8.463817596435547, 8.595504760742188, "The Light Energy Separation Method of the OCO-3 Instrument is Diffraction grating."]
[8.304089546203613, 8.611742973327637, "The Internal Surface Treatment of the Instrument Spectrometer is Flat-black surface treatments, e.g. Z306 paint with diffuse reflectance Rdiff ~ 5%."]
[4.0275702476501465, 5.722601890563965, "The Data Rate of the Solar Orbiter Satellite is 100 kbit/s."]
[10.22916316986084, 2.9390411376953125, "The Orbit Altitude of the SPOT 6-7 Satellite is 694 km."]
[4.891408443450928, 12.097509384155273, "The Responsivity Measurement of the Responsivity Measurement Instrument is 0.51 A/W."]
[8.760161399841309, 6.860853672027588, "The Linearity of the Position Sensing and Actuation System is Along the instrument sensitive axis."]
[10.35163688659668, 7.2195210456848145, "The Family of the TEMBOTM EMC Material is Booms."]
[8.804763793945312, 8.975503921508789, "The Groove Density of the Convex Holographic Grating Grating is 1450 grooves/mm."]
[8.581337928771973, 7.092006683349609, "The Position of the Reference Absorbers Calibration Components is Mounted on the non-rotating part of the instrument."]
[8.47351360321045, 9.196293830871582, "The Slit Image Coalignment Requirement of the Spectrometer Channel Optical System is Within a small fraction of their size on the focal plane (~250 \u00b5m)."]
[3.193619728088379, 5.310214996337891, "The Capacity of the SSDRs Solid-State Data Recorders is 2 GByte."]
[7.572826862335205, 1.3201080560684204, "The Sample Dispersal Deadline of the JAXA Organization is By the close of 2021."]
[9.582718849182129, 2.001168966293335, "The ACS Parameters of the MarCO Satellite is Working for both TCMs and flight."]
[7.945603370666504, 9.381840705871582, "The Spectral Range of the SWIR Short Wave Infrared region is 843-1043 nm."]
[9.107002258300781, 2.7755770683288574, "The Position in Constellation of the GCOM-W1 Satellite is Prior to the Aqua spacecraft."]
[3.963840961456299, 4.317076206207275, "The Main Processor of the Command and Data Handling Subsystem Subsystem is Nexus S smartphone."]
[9.799427032470703, 4.107172012329102, "The Payload Fairing Diameter of the GSLV-F05 Rocket is 3.4 m."]
[6.919050693511963, 5.631396770477295, "The Sea Surface Salinity Accuracy of the SMOS Satellite is 0.3-0.5 psu."]
[9.063285827636719, 10.595906257629395, "The Time of the Calibration Cycle Camera Calibration is Approximately 1.8 s."]
[5.496306896209717, 6.057772159576416, "The Panels of the SAR Antenna Antenna is One fixed and four deployable panels."]
[4.158506393432617, 5.6508049964904785, "The Downlink Transmission Data Rates of the CBERS-1 Satellite is 2 x 53 Mbit/s."]
[11.636574745178223, 4.456398010253906, "The Predicted Mass of the White Dwarf Celestial Body is Two tenths the mass of the Sun."]
[10.890217781066895, 5.73896598815918, "The Developer of the Kappa Scheme Flare Prediction Method is Professor Kanya Kusano."]
[1.0270440578460693, 4.195074081420898, "The Cell Configuration of the Battery Energy Storage is 2P24S."]
[7.441906452178955, -0.000775617198087275, "The Development Time of the SAOCOM-1A Satellite is since 2011."]
[1.8337018489837646, 4.1282429695129395, "The Current of the Solar Array Power System is Unknown."]
[3.9324655532836914, 5.6897101402282715, "The High-Gain Dish Link Speed of the TGO Trace Gas Orbiter is 2 Mbit/s."]
[7.771998405456543, 5.9537129402160645, "The Wavelength Calibration Frequency of the TRUTHS Satellite is At least one wavelength per orbit."]
[7.372753620147705, 10.119111061096191, "The Spatial Resolution of the HySI Hyperspectral Imager is 80 m."]
[8.877777099609375, 8.791752815246582, "The Viewing Angle Range of the Moon Calibration Site is -115\u00ba to +115\u00ba."]
[8.619495391845703, 10.299270629882812, "The Spectral Range of the LWIR Camera Camera is 8-9.5 \u00b5m."]
[8.745354652404785, 8.144672393798828, "The Value of the Geometric factor Parameter is 0.1 cm^2 sr."]
[4.833560466766357, 1.9743990898132324, "The Number of Maneuvers of the SkySat-4 Satellite is 3."]
[8.12844467163086, -0.7060698866844177, "The Attachment Duration of the SpaceX Dragon Spacecraft is 18 days."]
[4.777813911437988, 9.097331047058105, "The Detection Date of the InSight lander Seismic Instrument is Late 2018."]
[8.025727272033691, -0.711679220199585, "The Installation Date of the Dragon Spacecraft is 8 December 2019."]
[8.724806785583496, 9.823912620544434, "The Operation of the Interferometer Arrays Imaging Technology is Take a snapshot, process it and there's your image."]
[8.918115615844727, 10.293188095092773, "The Control of the CMOS Camera Camera is I2C I/F."]
[11.385697364807129, -1.3624217510223389, "The Mass of the NorSat-1 Satellite is < 30 kg."]
[1.5776962041854858, 4.437062740325928, "The Redundancy of the Buck-Boost Converter Solar Array Regulator is 2 of 3 Red.."]
[9.261460304260254, 10.404095649719238, "The Imaging Mode of the FAI Camera is Slew."]
[7.211336135864258, 0.9047011137008667, "The Opening Date of the ESA's first UK Center Center is July 9, 2015."]
[7.5604166984558105, 5.655215263366699, "The Mission Goals of the ARMADILLO Satellite is Characterize in-situ sub-millimeter level dust and debris particles in LEO (Low Earth Orbit) by sensing impacts at varying times, directions and locations."]
[10.425115585327148, -0.9509732723236084, "The Mass of the Baumanets-2 Microsatellite is 86 kg."]
[1.7038350105285645, 4.220149517059326, "The Solar Cells Power Conversion Efficiency of the EPS Electric Power Subsystem is 27%."]
[3.1826536655426025, 4.8870768547058105, "The Memory of the C&DH Command and Data Handling is 16 MByte Flash."]
[9.086405754089355, 5.108427047729492, "The Stabilization of the COMS Satellite is 3-axis."]
[6.874220371246338, 3.2466704845428467, "The Operational Status of the TSX Satellite is Operational."]
[10.233257293701172, 2.8390259742736816, "The Altitude of the COMPASS-1 Satellite is 830 km."]
[9.075855255126953, 9.898700714111328, "The Operation Mode of the Camera Sensor Imaging System is Snapshot or staring mode."]
[9.080487251281738, 3.2858481407165527, "The Orbit of the MinXSS-2 Satellite is Sun-synchronous, polar orbit."]
[10.171696662902832, 3.010889768600464, "The Altitude of the Hodoyoshi-4 Satellite is 600 km."]
[9.520905494689941, 9.095293045043945, "The Diameter of the Telescope Optical Instrument is 620 mm."]
[12.112650871276855, 3.306765079498291, "The Inclination of the SZ-7 Spaceship is 42.4\u00ba."]
[5.021363258361816, 1.9915266036987305, "The Number of Satellites of the Iridium NEXT Satellite is 70."]
[9.69466495513916, 5.909737586975098, "The Slew Time, 15\u00ba roll of the ADCS Attitude Determination & Control Subsystem is \u2264 4.5 minutes."]
[3.5330214500427246, 6.389610767364502, "The Data Rates (Uplink) of the RF Communications Communication System is 1.2 kbit/s."]
[4.815963268280029, 0.16247497498989105, "The Prime Minister of India of the OneWeb Satellite Communications Company is Narendra Modi."]
[1.8025435209274292, 4.770697116851807, "The Power Output of the EPS Electric Power Subsystem is 550 W."]
[4.253821849822998, 5.734653472900391, "The Image Transmission of the Spacecraft Satellite is X-band with 160 Mbit/s downlink rate."]
[8.228323936462402, 5.429593086242676, "The Navigation of the Lander Spacecraft is Configured for inertial navigation from separation to the end of rough braking."]
[9.393950462341309, -0.5390214920043945, "The Communication Protocol of the Nanosatellite Satellite is FM."]
[8.48112678527832, 3.198621988296509, "The Initial Separation of the TanDEM-X and TerraSAR-X Satellites is 15700 km."]
[9.630440711975098, 0.7227156162261963, "The Design Storage Time of the Valves Spacecraft Component is Up to 60 days."]
[6.598545074462891, 8.455479621887207, "The Distress Signal Detection Range of the MEOLUT Next Local User Terminal is More than 5,000 km."]
[5.201764106750488, 2.800842761993408, "The Communication Test of the ArgoMoon CubeSat is Optical communication capabilities between the CubeSat and Earth."]
[11.782477378845215, 1.6542924642562866, "The Operation Time on Primary Batteries of the Philae Lander is Approximately 5 days."]
[8.862390518188477, 10.282078742980957, "The Focal Plane of the R3 Sensor Imaging System is ON Semiconductor LUPA 1300-2 Si:CMOS focal plane."]
[7.486514091491699, 1.2199320793151855, "The Launch Date of the Planet Orbit Partner Program is October 14, 2019."]
[7.556099891662598, 8.71485424041748, "The Cross-Track Swath of the OMPS Limb Profiler Spectrometer is 500 km."]
[5.8433427810668945, 2.9303786754608154, "The Manufacturer of the ICEYE-X2 Satellite is ICEYE Ltd.."]
[4.715193271636963, 1.8146064281463623, "The Planned Number of the Future Satellites Satellite is 2200."]
[5.76257848739624, 1.7691465616226196, "The Manufacturer of the GomX-4A and GomX-4B CubeSats is GomSpace."]
[7.821336269378662, 8.96867561340332, "The Spectral Sampling Distance of the UV-1 Spectrometer is 0.32 nm."]
[7.794605255126953, 10.874799728393555, "The Data Quantization of the Spacecraft Satellite is 10 bit."]
[9.450904846191406, 0.8315193057060242, "The Mission Duration of the SORTIE CubeSat is 6 months."]
[5.025069713592529, -0.15189258754253387, "The Serial Production Initiation Date of the OneWeb Satellite Constellation is June 27, 2017."]
[6.967124938964844, 1.590578317642212, "The Presentation Date of the Tuomas Tikka Person is October 14-16, 2014."]
[5.76094388961792, 6.508984088897705, "The Polarizations of the SAR antenna Antenna is HH,VV,HV,VH."]
[7.454190731048584, 2.3151705265045166, "The Utilization of the ICI-1 Radiometer is Water vapor profile and snowfall."]
[1.8132705688476562, 4.16157865524292, "The Voltage of the Solar Arrays Power Generation is 23 to 37 Volts."]
[9.004121780395508, 10.191246032714844, "The Unknown of the Multispectral Camera Camera is Unknown."]
[6.796384334564209, 2.448059558868408, "The Deployment Readiness of the DoD Human Space Flight Support Office Rescue Division Organization is Prepared to deploy at a moment\u2019s notice."]
[8.634063720703125, 9.088652610778809, "The Grating Type of the MEGS Spectrograph is Single, holographic, spherical grating."]
[2.341791868209839, 4.402525424957275, "The Power Topology of the Bus Satellite Component is Direct Energy Transfer (DET)."]
[11.69853401184082, 4.465540409088135, "The Distance from Earth of the Kepler-186 Star System is About 500 light-years."]
[1.2986366748809814, 4.133594036102295, "The Battery Capacity of the Spacecraft Satellite is 5.3 Ah."]
[9.004923820495605, 5.405566215515137, "The Attitude Control of the STPSat-1 Satellite is Momentum-biased about the pitch axis."]
[10.11106014251709, 1.5374661684036255, "The Period of the Satellite Orbit is 98.5 minutes."]
[8.868888854980469, 2.0224406719207764, "The Next Proposal Due Date of the New Horizons Spacecraft is Early 2022."]
[6.329075336456299, 1.5470592975616455, "The Date of the Ground Segment Coordination Body Workshop Workshop is June 19-20, 2007."]
[11.722661018371582, -1.1415214538574219, "The Mass of the Spacecraft Satellite is 670 kg."]
[9.013520240783691, 10.616534233093262, "The Image Resolution of the WMC Camera is 16 m."]
[5.048917770385742, 4.433645725250244, "The Communication Network of the SBSS Satellite System is Air Force Satellite Control Network and commercial USN (Unified Space Network) ground stations."]
[8.213953971862793, 10.556878089904785, "The Power Consumption of the FPU Focal Plane Unit is 85 W."]
[3.559138536453247, 6.663554668426514, "The Data Rate (max) of the HiSPiCO S-band Transmitter/Transceiver is 2000 kbit/s."]
[7.546065807342529, 1.0638701915740967, "The Testing Start Date of the OCK (Orbit Control Kit) Orbit Control System is Summer of 2007."]
[7.067455768585205, 1.8375663757324219, "The Conference Presentation Date of the SJ-9 Technology Demonstration Satellite Satellite is Oct. 1-5, 2012."]
[5.03895902633667, 1.9524595737457275, "The Close Passes of the Mariner 10 Spacecraft is 3."]
[6.902814865112305, 3.241637706756592, "The Mission Status of the PIXL-1 mission Satellite is In commissioning."]
[8.022758483886719, -0.7509113550186157, "The Arrival Method of the Dragon CRS-14 Spacecraft is Snagged by the orbiting lab's huge Canadarm2 robotic arm."]
[1.5129976272583008, 4.936323165893555, "The Operating Voltage Range of the LVPS Board Power Supply is 26 - 29 V."]
[9.405440330505371, 9.373705863952637, "The Field of View of the Optical Head Optical Device is 52\u00ba x 28\u00ba / 90\u00ba x 74\u00ba (multi-hole mask: 10 x 10 spots / 3 x 3 spots)."]
[7.141201496124268, 9.260908126831055, "The Bands of the Multispectral Instrument (MSI) Instrument is 13."]
[6.9411821365356445, 4.6551737785339355, "The Focus of the RECCAP-2 Satellite Mission is Regional GHG budgets."]
[6.8084282875061035, 3.354527473449707, "The Assembly Options of the HISat Satellite is Flexible assembly options resulting in multiple possible configurations."]
[4.953308582305908, 4.671039581298828, "The Communication System of the Ground Station Ground Segment is MHX modem (Microhard Systems)."]
[8.688677787780762, 10.327381134033203, "The Image Resolution of the Infrared Sensors Sensor is 6688 x 2500 pixels."]
[7.0990424156188965, 6.897721767425537, "The Band of the Trasser AOS Instrument is Visible."]
[4.252915859222412, 5.586224555969238, "The Ability to Support HDLC Framing of the UoSAT-12 Satellite is True."]
[4.327049732208252, 4.441242694854736, "The Technology Options of the ORS Communication Bus Communication Bus is Firewire, SpaceWire, and Ethernet."]
[6.560454368591309, 2.199979782104492, "The Purpose of the EnviSat Satellite is Earth observation."]
[6.204261302947998, 3.35185170173645, "The Type of the Payload Accommodation Satellite is Large."]
[6.822340488433838, 5.541687965393066, "The Importance of the SMAP Satellite is Timely and accurate knowledge of the root-zone soil moisture is very important for farmers, stakeholders, and agricultural agencies."]
[7.193510055541992, 2.525270938873291, "The URL of the RHESSI Satellite is http://hesperia.gsfc.nasa.gov/hessi/news/aug_11_03.htm."]
[9.318506240844727, -0.7536547780036926, "The Launch Time (UTC) of the ESAIL Microsatellite is 01:51."]
[8.055817604064941, 4.624543190002441, "The Resolution of the Satellite LEO (Low Earth Orbit) is \u0394x = 1.2 km for \u0394\u03b8 = 0.1\u00ba."]
[9.080977439880371, 5.095270156860352, "The G&C System of the STEREO spacecraft Satellite is Three-axis-stabilized with fixed solar arrays for power generation as well as a steerable HGA (High Gain Antenna) for heliocentric orbit communications."]
[11.801961898803711, 1.113821268081665, "The Mission Objective of the Chang'e-3 Moon Lander is One year operation on the lunar surface."]
[8.399682998657227, 8.661393165588379, "The Purpose of the GRNS Instrument is Detect, measure, and map Psyche\u2019s elemental composition."]
[7.399384021759033, 5.4729437828063965, "The Data Correction of the Aeolus Satellite is Corrected certain biases."]
[8.748650550842285, 0.7277741432189941, "The Arrival Date of the Juice Spacecraft is 2029."]
[7.852179050445557, 9.06562614440918, "The Spectral Range of the UV to NIR Satellite is Ultraviolet (340 nm) to near-infrared (890 nm)."]
[4.718058109283447, 4.180233478546143, "The Data Loss Tolerance of the EDSN Data Network is Accepts data packet loss."]
[10.70567512512207, 3.202887535095215, "The Distance Traveled of the D-Sat Satellite is More than 12 million km."]
[6.484683990478516, 2.42940616607666, "The URL of the Alphabus Satellite Platform is http://telecom.esa.int/telecom/www/object/index.cfm?fobjectid=30203."]
[5.654632091522217, 9.158865928649902, "The Value of the Peak Power Consumption Instrument is < 35 W."]
[7.856618404388428, 7.906174659729004, "The Precision of the Method Calibration Method is Better than 0.5%."]
[7.6946258544921875, 1.3921703100204468, "The Release Date of the Halloween Space Weather Storms of 2003 Space Weather Event is June 2004."]
[7.312905311584473, 6.752569675445557, "The Image Acquisition Date of the MODIS Instrument is March 2002 and February 2022."]
[8.158663749694824, 2.7255594730377197, "The Calibration Method of the ARTEMIS Satellite is Solar radiation-based."]
[8.929500579833984, 4.971503734588623, "The Orientation Adjustment of the PSSCT-2 Satellite is Continuous."]
[7.19924783706665, 8.711296081542969, "The Spatial Resolution of the AATSR Instrument is 1 km x 1 km."]
[8.275566101074219, 0.36846286058425903, "The First Entry Date of the BEAM Expandable Habitat is June 6, 2016."]
[4.774481296539307, 7.195613384246826, "The Wavelength of the S-band Band is 12 cm."]
[8.060230255126953, 4.658803939819336, "The Spatial Resolution - Pan of the Spacecraft Satellite is 1 m GSD."]
[9.006586074829102, 5.40491247177124, "The Components of the Reaction Dynamics Study Experiment is 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 ."]
[7.427817344665527, 9.573831558227539, "The Spectral Range of the S-192 optomechanical scanner Scanner is 0.4-12.5 \u00b5m."]
[5.221377372741699, 5.941235065460205, "The Quantity of the Patch Antennas Antennas is 2."]
[9.883749008178711, 7.754003524780273, "The Data Products of the CRaTER Cosmic Ray Telescope is LET spectra of galactic and solar cosmic rays (particularly above 10 MeV)."]
[10.460267066955566, -1.1075000762939453, "The Mass of the GHGSat-C2 (Hugo) Nanosatellite is 16 kg."]
[6.992082595825195, 1.3869974613189697, "The Conference Date of the SPARCS Satellite is Aug. 4-9, 2018."]
[5.619661331176758, 1.9340769052505493, "The Payload Fairing Technology of the Minotaur Launch Vehicle is Advanced Grid-Stiffened Composite."]
[6.689527988433838, 0.7078841924667358, "The Mission End Date of the ICESat Satellite is Aug. 31, 2010."]
[7.0129547119140625, 1.3211517333984375, "The Presentation Date of the Hokkaido Satellite Project Satellite is June 4-11, 2006."]
[6.553775787353516, 1.2658544778823853, "The User Workshop Date of the GOCE Satellite is Nov. 6-8, 2006."]
[8.797290802001953, 10.589872360229492, "The Data Compression Algorithm of the HRC Instrument Camera is JPEG2000."]
[6.945387363433838, 0.30603453516960144, "The Launch Date of the BRO-4 Satellite is 17 August 2021."]
[6.096513271331787, 3.5374999046325684, "The Payload of the SV-1 Satellite is CTIP (Compact Tiny Ionospheric Photometer)."]
[4.861173152923584, 1.9141772985458374, "The Number of Decommissioned Satellites of the HY-2 Satellite is 1."]
[8.951220512390137, 5.358833312988281, "The Bearing Assemblies Configurations of the Central Bulkhead Assembly Satellite Component is 2 and 3 degree-of constraint."]
[8.33528995513916, 4.567495822906494, "The Swath Width of the DubaiSat-2 Satellite is 12 km."]
[6.944382190704346, 2.034423351287842, "The Rainfall Accumulation of the IMERG Product is April 12 to April 19."]
[11.84296989440918, 1.0277140140533447, "The Resumed Work Days of the Chang'e-4 Lunar Probe is 23 days."]
[3.8107542991638184, 0.27718034386634827, "The Conference Presentation Date of the GRAIL Mission is March 10-14, 2008."]
[5.82850980758667, 9.01087760925293, "The Power Consumption of the Photometer Instrument Instrument is \u2264 3.5 W."]
[8.547408103942871, 9.911744117736816, "The width of the Detector Instrument is 32 pixels."]
[8.508455276489258, 10.545822143554688, "The Pixel Size of the CCD Detector Array Imaging Device is < 12 \u00b5m."]
[6.5939154624938965, 4.3046040534973145, "The Camera of the Pico Dragon CubeSat is OmniVision CMOS VGA color sensor with low power consumption."]
[7.629613876342773, 0.4314897954463959, "The Launch Date of the Chandrayaan-1 Satellite is Oct. 22, 2008."]
[6.6649980545043945, 4.639010429382324, "The Imaging Frequency Band of the RISAT-1 Satellite is X."]
[8.864133834838867, 7.055169105529785, "The Measurement of the IMPACT Instrument is Solar wind ion measurements."]
[7.598556041717529, 1.2696453332901, "The Operation End Date of the Metcomp experiment Materials Science Experiment is 17 December."]
[8.367644309997559, 9.082275390625, "The Spatial Resolution of the AWiFS sensor Sensor is 56 m."]
[5.069457054138184, 3.771385431289673, "The Components of the Spacecraft Satellite is Solar panels, spacecraft bus."]
[9.453866004943848, 5.84232759475708, "The Controllers of the ACS Attitude Control System is Proportional\u2013Integral\u2013Derivative."]
[2.1191322803497314, 4.001097679138184, "The Power Range of the ROSA Roll-Out Solar Array is Hundreds of watts to the megawatt range."]
[9.343323707580566, 1.5845171213150024, "The Workshop Frequency of the SSETI Express Satellite is Twice a year."]
[7.26292085647583, 3.4432373046875, "The Torque Rods Status of the NEOSSat Satellite is Failed."]
[6.484988689422607, 3.007160186767578, "The Manufacturer of the Resurs-P1 Satellite is TsSKB Progress (Progress State Research and Production Space Center)."]
[7.664083003997803, 6.925158977508545, "The Design of the SCM Device is Very compact."]
[10.324018478393555, 3.1260452270507812, "The Altitude of the Secondary Payloads Unknown is 354 km x 1450 km."]
[5.637265205383301, 6.459243297576904, "The Dimensions of the SAR antenna Antenna is 3 m x 1 m."]
[11.705184936523438, -1.1184622049331665, "The Mass of the Payload Satellite is 149 kg."]
[9.932812690734863, -0.6706785559654236, "The Perigee Altitude of the IDEA-OSG 1 Microsatellite is 600 km."]
[7.10834264755249, 9.388959884643555, "The Bands of the MSU-MR Instrument is Six bands in the VIS and IR spectral regions."]
[5.6899733543396, 2.0548155307769775, "The Integration Partner of the LightSail-2 Solar Sailing CubeSat is Prox-1."]
[4.848350524902344, 9.004517555236816, "The Seismic Exploration of the InSight Spacecraft is Can feel whirlwinds pulling on the surface."]
[6.764612674713135, 4.427494525909424, "The Data Sources of the Green City Watch Application is Copernicus Sentinel-2 mission, Sentinel-1 SAR imagery, SkySat and RapidEye."]
[6.5500569343566895, 6.239518165588379, "The Revisit Time of the OSCAT Scatterometer is 2 days."]
[7.135166645050049, 9.171204566955566, "The Spatial Resolution of the Multispectral Instrument (MSI) Instrument is 10 m."]
[3.1947622299194336, 5.963146209716797, "The Modulation Schemes of the MTP Transponder is 4."]
[7.367501735687256, 2.351794958114624, "The Construction Time of the Carbonite-1 Satellite is 6 months."]
[9.058555603027344, 4.213140487670898, "The Body Shape of the Bus Satellite Component is Square-shaped."]
[10.270630836486816, -0.8799710869789124, "The Mass of the Kestrel Eye-2M Microsatellite is ~50 kg."]
[7.307815074920654, 1.6653039455413818, "The Date of the 32nd Space Symposium Conference is April 11-14, 2016."]
[8.504260063171387, 10.450040817260742, "The Peak Quantum Efficiency of the Imager Camera is 50%."]
[6.92368221282959, 0.7656805515289307, "The Operation Start Date of the BIRD Satellite is October 2001."]
[7.309512615203857, 10.159317970275879, "The Development Consortium of the HyperScout Hyperspectral Imager is cosine, VITO, S&T, Technical University of Delft."]
[9.434219360351562, 1.7538014650344849, "The Orbit Maneuvers Frequency of the GRACE Satellite Satellite is About every 50 days."]
[11.300387382507324, 4.286365509033203, "The Data of the Roman Satellite is More than 10 million galaxies."]
[9.591899871826172, 1.8008180856704712, "The Image Capture Time of the TESS Satellite is Over the course of 17 hours on July 25."]
[4.102163791656494, 2.270014524459839, "The Satellite Size of the ANGELS Nanosatellite is 12U."]
[6.8591742515563965, 8.518301010131836, "The SSS Spatial Resolution of the CIMR Radiometer Imager is 5 km."]
[6.542670249938965, 7.597862720489502, "The Quantity of the Laser Transmitters Device is 2."]
[8.890149116516113, 2.773102283477783, "The Mission of the Kepler Satellite is K2."]
[8.332072257995605, 2.7881226539611816, "The Photo and Measurement Activities of the Beresheet Spacecraft is Landing Site."]
[9.222726821899414, 10.34960651397705, "The Nominal Focal Parameters of the PamCam Camera is Unknown."]
[5.324280738830566, 4.358397006988525, "The Location of the Ground Stations Communication is New Norcia, Australia (DSA 1), Cebreros, Spain (DSA 2), Malarg\u00fce, Argentina (DSA 3), Kourou, Maspalomas and Perth."]
[6.8035888671875, 2.8589696884155273, "The Development Status of the Arachne Satellite is Unknown."]
[7.9759745597839355, 0.3436940014362335, "The Return Date of the Crew-1 Mission is April 2021."]
[5.553887844085693, 4.58845329284668, "The Earth Station Location of the WINDS Satellite is Higashimatsushima."]
[4.943591117858887, 3.5506792068481445, "The Structure Components of the HIT-Sat Satellite is Four angle bars, six surface panels and two inner panels."]
[13.723584175109863, 1.6097557544708252, "The Launch Date of the Vega Launch Vehicle is Aug. 2, 2017."]
[12.122514724731445, 2.240156412124634, "The Thermal Spectrometer of the OSIRIS-REx Spacecraft is OTES."]
[9.24238109588623, 10.251965522766113, "The Number of Cameras of the spaceCam c4000 Video Camera is 2."]
[3.1552042961120605, 5.335325241088867, "The Fault Isolation of the SSR Solid State Recorder is The division of the storage space into independent banks."]
[9.141284942626953, 10.0123291015625, "The Image Type of the LROC Camera is Black-and-white and color."]
[6.552810192108154, 7.545767784118652, "The Intended Use of the Laser Oscillators Component is DWL, GIFTS and ALADIN."]
[7.0359392166137695, 4.204854965209961, "The Measurement Domain of the IRS-P6 Satellite is Land, Snow & Ice."]
[4.9292073249816895, 4.975886344909668, "The Technology of the EUMETCast Dissemination System is Standard DVB-S2."]
[8.940157890319824, 2.1825456619262695, "The Observation of the New Horizons Spacecraft is Tons of material from Io's volcanoes move down the tail in large, dense, slow-moving blobs."]
[8.95367431640625, 6.634139537811279, "The Nominal Magnetic Moment of the MTs Magnetic Torquers is 1 Am2."]
[6.087222576141357, 3.160700559616089, "The Partnership with Spire Global of the Myriota IoT Service Provider is Myriota will use Spire's constellation of smallsats to expand its network."]
[6.184177875518799, 3.24932861328125, "The Agency of the Myriade/AstroSat-100 Satellite is CNES, ASTRIUM."]
[7.560690402984619, 2.635937452316284, "The Mission Type of the Hera Satellite is Surveying Didymos."]
[5.864187240600586, 5.531944274902344, "The Beamforming Technology of the TriG receiver GNSS Receiver is Digital."]
[11.601778984069824, 4.662250995635986, "The Purpose of the Tereza's Computer Model Simulation Model is Simulate the various perturbations that escaping stars in the cluster might feel during their hundreds of millions of years in space."]
[6.16184139251709, 2.5898404121398926, "The Sponsor of the STPSat-3 Satellite is ORS (Operationally Responsive Space) Office."]
[6.705864429473877, 7.76196813583374, "The Precision of the Laser System Measurement Device is Subatomic scale."]
[13.148021697998047, 4.053192138671875, "The Survey Date of the Gaia Satellite is 13 June 2022."]
[8.855855941772461, 10.143930435180664, "The Image Type of the UV/VIS Camera Camera is UV/VIS."]
[7.177101135253906, 3.401278018951416, "The Image Content of the OPS-SAT Satellite is Arctic Laptev Sea with large amounts of drift ice."]
[9.13197135925293, 8.284102439880371, "The Mirror Position Measurement of the SMA Scan Mechanism Assembly is Differential Impedance Transducers."]
[8.458245277404785, 7.1371941566467285, "The Frequency Range of the Plasma Wave Instrument Instrument is 5 Hz - 800 kHz."]
[7.597651958465576, 4.564998149871826, "The Observation Frequency of the ALOS-4 Satellite is More frequent than ALOS-2."]
[6.911246299743652, 1.002137541770935, "The Start Year of the SOHLA Initiative is 2002."]
[5.581164360046387, 2.784461498260498, "The Manufacturer of the GHGSat-C2 Satellite is ABB."]
[5.9917893409729, 8.974756240844727, "The Power Consumption of the RCU Radiometer Calibration Unit is < 3 W."]
[4.168298244476318, 4.5635552406311035, "The Management Interface of the DCU Data Control Unit is PUS (Packet Utilization Standard) TCs."]
[5.955196380615234, 9.54456615447998, "The Mass of the MAG Instrument is 40 g."]
[9.124560356140137, 3.245215654373169, "The Orbit Type of the SPOT 6-7 Satellite is Sun-synchronous."]
[4.409920692443848, 5.1170878410339355, "The Evaluation of the Small Optical Transponder (SOTA) Optical Transponder is Unknown."]
[9.464472770690918, 0.4860464036464691, "The Actual Lifetime of the QuakeSat Satellite is 1 \u00bd years."]
[8.17646598815918, 7.885357856750488, "The Number of Experiment Cultures of the Biofilms Experiment is 24."]
[5.947027683258057, 9.557845115661621, "The Mass of the CMS Instrument is 4 kg."]
[6.1520867347717285, 4.56708288192749, "The Expertise of the ICEYE Satellite Constellation is Risk finance, climate risk management."]
[7.314421653747559, 1.0408008098602295, "The Meeting Date of the ICON Satellite is Dec. 3-7, 2012."]
[8.261817932128906, 3.2196757793426514, "The Expected Number of Final DEM Geocells of the TanDEM-X Satellite is Nearly 20,000."]
[3.5298397541046143, 6.488358974456787, "The Free Space Loss of the Unit Communication System is 182.7 dB."]
[8.381885528564453, 1.5451867580413818, "The End of Operations Date of the Rosetta Spacecraft is 30 September."]
[5.429326057434082, 3.872177839279175, "The Experiment of the VisionSpace Company is Testing the use of artificial intelligence to allow a spacecraft to analyze images on board and schedule and plan activities autonomously."]
[9.53537654876709, 8.59602165222168, "The Quantity of the LPT Light Particle Telescope is 1."]
[7.752893447875977, 3.2548747062683105, "The Number of Collected Fragments of the DebriSat project Satellite is Over 20,000."]
[10.559043884277344, 3.4196040630340576, "The Image Distances of the Rosetta Satellite is 80-100 km."]
[6.84144926071167, 10.038296699523926, "The Bandwidth of the Band 4 Spectral Band is 545-565 nm."]
[10.31099796295166, 5.686342239379883, "The Structure of the Tether Spacecraft Component is Mesh."]
[5.497778415679932, 0.39030012488365173, "The 2022 Acres Burned of the U.S. Drought Monitor Report is 230,000 acres."]
[2.149949789047241, 4.234086990356445, "The Solar Array Power of the DSP satellites Satellite is 260 W (BOL) and 210 W (EOL)."]
[7.5081467628479, 8.455333709716797, "The SNR (Signal to Noise Ratio) of the Instrument Sensor is 6."]
[6.741353988647461, 9.126495361328125, "The Dimensions - Electronics box of the Instrument Sensor is 31 x 22 x 27 cm."]
[6.485141754150391, 3.375613212585449, "The Data Distributor of the Resurs-P1 Satellite is Sovzond JSC of Moscow."]
[7.2015061378479, 6.90177583694458, "The Presentation Date of the VIIRS Satellite Instrument is April 28, 2015."]
[8.579318046569824, 5.266851425170898, "The Pointing Performance of the CALIPSO Satellite is < 0.02\u00ba about each axis."]
[9.341361045837402, 3.923220634460449, "The Design of the SpinSat Satellite is Spherical."]
[4.937295436859131, -3.1989049911499023, "The | of the R. Lin Author is R. Lin."]
[11.680914878845215, 6.157397747039795, "The Article Date of the XMM-Newton Satellite is 18 May 2018."]
[6.74985933303833, 7.151611804962158, "The Development Location of the ATLID Lidar Instrument is Selex-Galileo, Florence, Italy."]
[6.681150436401367, 2.4842209815979004, "The URL of the FalconSAT-3 Satellite is http://www.satnews.com/cgi-bin/story.cgi?number=207495260."]
[11.531614303588867, 4.68153715133667, "The Behavior of the Alpha Circini Star is Shows complex behavior due to both rotation and pulsation."]
[4.354914665222168, 2.287540912628174, "The Type of the GRIFEX Payload is 3U CubeSat flight test experiment."]
[4.456664085388184, 4.5623369216918945, "The Operating Modes of the DCS Data Collection System is 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."]
[6.386958599090576, 8.299492835998535, "The Channels of the AMSU Microwave Radiometer is 20."]
[6.389970302581787, 3.302248001098633, "The Program of the MYriade Satellite is Performances, Missions, Tool for education and cooperation."]
[11.97814655303955, 3.4002840518951416, "The Inclination of the Solar Orbiter Satellite is Increasing to a minimum of 30\u00ba."]
[7.747915744781494, 9.200676918029785, "The Spectral Range of the Spectral Band B Spectrometer is 0.52 - 0.60 \u00b5m."]
[5.907691478729248, 6.7983717918396, "The Range Resolution of the SIRAL Radar is Approximately 0.45 m."]
[6.587648868560791, 1.4652059078216553, "The Launch Time of the OCO-2 Spacecraft is 09:56:23 UTC."]
[5.827620029449463, 3.570482015609741, "The Entities of the GMES program Initiative is ESA, CNES, DLR, EUMETSAT, ASI, INTA, CSA, DMCii."]
[8.445463180541992, 7.373743534088135, "The Noise of the EZ probe Electric Field Probe is 0.4 \u00b5V/Hz^(1/2)."]
[5.899109363555908, 7.595876693725586, "The Components of the ATMS Instrument is Antenna, motor, radio frequency system, electronic system."]
[9.1863431930542, 5.3875555992126465, "The Yaw Pointing Accuracy of the Attitude Control Satellite Subsystem is \u00b10.3\u00ba."]
[9.809416770935059, 4.560672760009766, "The Design of the Terminator Tape Deorbit Module Deorbit Device is Cubesat tether design."]
[9.37172794342041, 7.793841361999512, "The Spatial Distribution of the EPISEM Instrument is 54% in the SAA, 26% in the Polar Regions, 20% Galactic Cosmic Rays."]
[12.051071166992188, 3.5147011280059814, "The Inclination of the IBEX Spacecraft is 11\u00ba."]
[5.191845417022705, 4.185184001922607, "The Purpose of the OPS&GRND Subsystem is Planned operation of the satellite and the infrastructure required to operate the ground segment."]
[8.511605262756348, 10.504353523254395, "The Position Accuracy of the Detector E2V CCD-22 (Frame Store) is 30 arcsec."]
[7.719983100891113, 3.5401675701141357, "The Drifted Orbit of the ERS-2 Satellite is Reference Orbit."]
[10.213104248046875, 3.000861883163452, "The Orbit Altitude of the STP-S26 mission Satellite Mission is 650 km."]
[7.737627029418945, 8.925914764404297, "The Wavelength Range of Sensitivity of the MAHRSI Instrument is 195-320 nm."]
[7.330885887145996, 0.82889723777771, "The Mission Definition Date of the NICER Satellite is June 22, 2014."]
[7.436824798583984, 9.278030395507812, "The Spatial Resolution of the EOS-T Instrument is 0.3 m in its panchromatic band and 1.2 m in its multispectral bands."]
[9.175049781799316, 2.1935513019561768, "The Number of Essential Ground-Support Equipment Containers of the BepiColombo Spacecraft is Approximately 40."]
[7.757153511047363, 2.638939619064331, "The Coordination Office of the ARTEMIS Satellite is Air Force International Affairs Office."]
[4.008634567260742, 2.355225086212158, "The CubeSat of the Satellite TSAT is 2U."]
[5.851163387298584, 3.5698580741882324, "The Data Receiver of the TRMM Satellite is NASA/GSFC and JAXA/EORC (Earth Observation Research Center)."]
[10.425800323486328, 2.6847474575042725, "The Apogee of the Transfer Orbit Orbital Maneuver is 1.5 x 10^6 km."]
[5.338706970214844, 1.3527816534042358, "The Number of Launches for Booster of the Falcon 9 Rocket is Fifth flight."]
[7.9397406578063965, 1.1441282033920288, "The Image Capture Date of the TopSat Satellite is March 2, 2007."]
[9.18543815612793, 8.194945335388184, "The Mean Dark of the NISP IR Detector Detector is Around 0,005 e\u2013/pix/s at 100 K."]
[9.011408805847168, 10.486516952514648, "The Resolution of the OSIRIS Camera is About 3 m per pixel."]
[5.939187049865723, 1.8661901950836182, "The Launch Vehicle of the CHAMP Satellite is Kosmos-3M."]
[9.557857513427734, 3.9060816764831543, "The Formation Ranges of the CanX-5 Satellite is 1000 m, 500 m, 100 m."]
[7.514886379241943, 8.983946800231934, "The Ground Swath of the Miniature High-Resolution Imaging Spectrometer Imaging Spectrometer is 15 km."]
[4.100188255310059, 4.2590413093566895, "The Avionics of the ESPA Ring Interface is Independent set."]
[7.833876609802246, 9.434270858764648, "The Resolution of the AEISS-A Instrument is 2.0 m for multispectral MWIR images."]
[9.47741985321045, 9.300728797912598, "The Entrance Pupil Diameter of the Lens Optical Instrument is 10.5 cm."]
[6.306276321411133, 10.062577247619629, "The Mass of the MSU-50 Camera is 2.3 kg."]
[7.661070346832275, 4.766404628753662, "The Incidence Angles of the PROBA-1 Satellite is Five different."]
[6.346420764923096, 1.8986436128616333, "The Purpose of the G\u00f6kt\u00fcrk-1 Satellite is 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."]
[7.33214807510376, 2.234506130218506, "The URL of the Emirates Mars Mission Satellite is https://aetoswire.com/en/news/emirates-mars-mission-hope-probe-ready-for-launch-from-japans-tanegashima-space-centre."]
[9.629752159118652, 1.130602478981018, "The Nominal Mission Start of the Observatories Satellite is About 90 days after launch."]
[6.274576187133789, 4.899713516235352, "The Instrument Subsystems of the CSG-SAR Satellite is SES (SAR Electronic Subsystem) and SAS (SAR Antenna Subsystem)."]
[10.593521118164062, 3.2880349159240723, "The Satellite Connection Distance of the SpaceDataHighway Communication System is Up to 45,000 km."]
[8.05958366394043, -0.7303087711334229, "The Splashdown Location of the Crew Dragon Spacecraft is Atlantic Ocean or Gulf of Mexico."]
[7.504722595214844, 8.872020721435547, "The Angular Resolution of the Channels Spectrometer is 3''."]
[9.340967178344727, 1.0652835369110107, "The Launch Window of the Launch Mission Event is 12 days."]
[2.175567388534546, 4.54707670211792, "The Power of the GCOM-W1 Satellite is 4.05 kW at EOL (End of Life)."]
[5.8609819412231445, 8.112600326538086, "The Frequency Band of the ISA Accelerometer is 3 x 10-5 \u2014 1 x 10-1 Hz."]
[6.479633331298828, 2.749906063079834, "The Affiliations of the Keith Masback Individual is Mapping Sciences Committee of The National Academies of Sciences, Engineering, and Medicine."]
[5.948515892028809, 9.599881172180176, "The Mass of the HID Instrument is 2.2 kg."]
[6.682971954345703, 4.554766654968262, "The Ocean Measurements of the Copernicus Sentinel-3 Satellite is Temperature, colour and height of the sea surface."]
[7.1124043464660645, 1.8790233135223389, "The Research Targets of the SJ-10 Satellite Satellite is Gene expression pattern, Proteome, Mutation discovery, Embryo development."]
[8.906649589538574, 9.503830909729004, "The IFOV of the Sensor Unit Sensor is 25 pixels of 1\u00ba x 1\u00ba = 5\u00ba x 5\u00ba."]
[8.119940757751465, 1.1261837482452393, "The Image Creation Date of the SwRI-led team Team is 18 July 2018."]
[7.4556169509887695, 1.8807328939437866, "The Detection Date of the IceCube Satellite is 10 March 2021."]
[8.106415748596191, 8.3302001953125, "The Publication Date of the Solar-B EUV Imaging Spectrometer Spectrometer is 2005."]
[6.912165641784668, 6.747343063354492, "The Industrial Consortium of the GOME Instrument is Officine Galileo, Laben, British Aerospace, TPD."]
[7.074337005615234, 0.7006871104240417, "The Launch Date of the Pleiades-1A Satellite is Unknown."]
[10.626263618469238, 9.275679588317871, "The Image Resolution of the CaSSIS Imaging System is 5 x 10 km."]
[3.1796398162841797, 4.883750915527344, "The RAM Capacity of the FC Computer is 3 MB."]
[8.440973281860352, 7.243191242218018, "The Transformation Factor of the Field Measurement Device Sensor is 64 \u00b1 0.6 (\u00b5V/nT)."]
[10.463754653930664, 8.399293899536133, "The Purpose of the Coronagraph Instrument is Block out the image of the sun's disc and take pictures of the faint corona."]
[7.7950944900512695, 9.808554649353027, "The Spectral Band of the Band Photometers Photometer is 391.4 nm."]
[11.102051734924316, 5.146938800811768, "The Extended Mission Start Date of the LISA Pathfinder Spacecraft is 1 November."]
[4.266610622406006, 6.726913928985596, "The Operating Frequency of the Herley MD2000C-1 Transponder Module is 5.4\u20135.9 GHz."]
[7.316211700439453, 8.889846801757812, "The Spatial Resolution at Nadir of the Scanning geometry Instrument is 1 km."]
[7.5199432373046875, 2.0584981441497803, "The Report Recommendation of the SMAP Satellite is Recommended for implementation in the first phase of new missions (2010-2013)."]
[11.648650169372559, -1.2194949388504028, "The Mass of the MBA Satellite is 418 kg."]
[8.597309112548828, 10.584310531616211, "The Frame Read-out Frequency of the EPIC CCDs Imaging Device is Fixed, mode dependent."]
[8.89404582977295, 10.298625946044922, "The Sensor Type of the CMOS Camera Camera is CMOS."]
[6.006568908691406, 0.6213587522506714, "The First Photo of the MarCO-B CubeSat is 9 May."]
[7.091810703277588, 4.295503616333008, "The Measurement Domain of the MOMS Satellite is Ocean, Land."]
[6.189172267913818, 3.4842529296875, "The Objectives of the Deployment Mechanism Satellite Component is 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."]
[5.530651092529297, 2.0667343139648438, "The Launch Vehicle of the ArgoMoon CubeSat is NASA's Orion EM-1."]
[8.87094497680664, 10.679944038391113, "The Multispectral GSD of the CCD Pushbroom Camera Camera is 10m."]
[11.636218070983887, -1.246158242225647, "The Mass of the Total Satellite is 40 kg."]
[9.380992889404297, 6.023661136627197, "The Gyroscope Range of the ACS Attitude Control Subsystem is \u00b1 200\u00ba/s."]
[1.9459810256958008, 4.1559343338012695, "The Average Power of the Solar Panels Power Source is 28.5 W."]
[7.553297996520996, 4.091116428375244, "The Measurement Coverage of the CryoSat-2 Satellite is Polar oceans, Greenland, Antarctica."]
[6.722600936889648, 6.1459455490112305, "The Intersection Frequency of the ISS-RapidScat Scatterometer is Approximately every hour."]
[5.113602638244629, 5.506837844848633, "The Band of the EUTELSAT KONNECT Satellite is Ka-band."]
[5.256344795227051, 5.095450401306152, "The Architecture of the LCRD Laser Communications Relay Demonstration is Optical-to-optical relay."]
[10.288554191589355, 6.749943733215332, "The Electrical Connection of the SMA Heaters Deployment Control is In series."]
[6.8362650871276855, 0.9813069701194763, "The Launch Date of the COMS Satellite is 26 June 2010."]
[4.367708683013916, 6.547440052032471, "The Frequency Bands of the RF Communications Communication System is UHF/VHF (436/145 MHz)."]
[6.34513521194458, 2.3924498558044434, "The Focus of the Astroscale Company is Developing technologies to service satellites and remove orbital debris."]
[6.817914962768555, 3.3031961917877197, "The Mission Status of the CAS500 Satellite is Operational (nominal)."]
[1.9038935899734497, 3.8771135807037354, "The Type of the Solar Array Power Source is Triple-junction GaAs cells."]
[8.140742301940918, 2.530654191970825, "The Band Number of the Himawari-8 Geostationary Satellite is 16 bands."]
[8.34263801574707, 2.0457706451416016, "The Completion Date of the Canberra DSN station Antenna is January 2021."]
[3.8676185607910156, 6.407834053039551, "The Data Rate of the LLCD Laser Communication System is High."]
[8.557623863220215, 3.8378963470458984, "The Sky Coverage of the SPARCS Satellite is 60% over a year."]
[11.688358306884766, 2.597201108932495, "The Diameter of the Didymos Asteroid is 780 meters."]
[9.585979461669922, 6.020699501037598, "The Gyroscope of the ADCS Attitude Determination and Control Subsystem is 12.5 mV/\u00ba/s, \u00b1150\u00ba/s."]
[9.64115047454834, 3.915168523788452, "The Propellant Status of the CanX-4 Satellite is Close to a full tank."]
[11.741548538208008, -0.9997921586036682, "The Payload Mass of the SmallGEO Satellite Platform is Up to 300 kg."]
[10.30896282196045, 6.868696212768555, "The Active Thermal Control of the TCS Thermal Control Subsystem is Polyimide heating film."]
[8.203889846801758, 1.0369372367858887, "The Image Capture Date of the Small Monitor Camera (CAM-H) Camera is 14 August."]
[8.6168851852417, 7.039429187774658, "The Response Time of the Magnetic Field Sensor Sensor is <200 ns."]
[5.2436137199401855, 6.394561767578125, "The Size of the Transmit Antenna Antenna is 3.3 m dish."]
[3.7301769256591797, 4.302637577056885, "The Main Processor of the DHU Data Handling Unit is MA 31750."]
[6.476753234863281, 6.207660675048828, "The Instrument Type of the OSCAT-3 Radar Scatterometer is Radar scatterometer."]
[6.129443645477295, 5.404240608215332, "The Development Team of the PALSAR Ground Data System is Hiroshi Watanabe, Shiro Ohkawa, Kenji Tatsumi, Hidekuni Kikuchi, Yasutaka Onoda."]
[7.288398265838623, 3.5806186199188232, "The Communication Band of the SPOT-6 & SPOT-7 Satellite Constellation is S-band."]
[7.292651653289795, 6.855903625488281, "The Malfunction Date of the OHRIS Imager is March 4, 2007."]
[8.392971992492676, 2.234412908554077, "The Onboard Instruments of the Voyager 2 Spacecraft is Cosmic ray subsystem, low energy charged particle instrument, magnetometer."]
[8.395614624023438, 7.375631809234619, "The Measurement of the Electric Field Instrument Instrument is 25 km-wide ribbon of gas flowing westward at about 6 km/s."]
[9.632328987121582, 5.564239978790283, "The ADCS System of the DeorbitSail Satellite is Stabilized."]
[9.497665405273438, 10.508393287658691, "The Revolutions/Day of the Iris Video Camera Camera is 16."]
[9.688238143920898, 7.029626369476318, "The Thermal Survival Range of the Instrument Satellite Instrument is -50 / +40\u00baC."]
[5.318911552429199, 9.607552528381348, "The Maximum Acquisition Rate of the STOs and STAEs Analog Electronic units is 0.1\u00ba/s."]
[6.455867290496826, 3.5216212272644043, "The Components of the ROE Observatory is UKTAC, Institute of Astronomy, ROE Visitor Center."]
[1.5391943454742432, 4.619631767272949, "The Solar Array Voltage Input of the SABR DC/DC Converter is Up to 65 V."]
[3.311480760574341, 6.048558235168457, "The Noise Figure of the TOTEM SDR SDR Platform is 2 dB."]
[7.427298069000244, 1.416871190071106, "The ERBS S/C Operational on One Battery Date of the ERBE Instrument is June 2001."]
[1.8088897466659546, 4.025813102722168, "The Number of Strings per Panel of the Solar Array Power Generation is 11."]
[7.074938774108887, 9.839752197265625, "The Center Wavelength of the Band No. 17 Spectral Band is 644.64 nm."]
[6.0487847328186035, 3.151250123977661, "The Prime Contractor of the SEOSAT-Ingenio Satellite is Spain."]
[6.168467044830322, 2.544834852218628, "The Collaboration Director of the Astrocast Satellite Operator is Renaud de Watteville."]
[9.996867179870605, -0.8200089335441589, "The Cost of the Kestrel Eye II Microsatellite is Approximately $2 million per spacecraft."]
[7.181411266326904, 3.1019420623779297, "The Architecture Elements of the FORUM Mission is Platform, payload and main mission performance."]
[7.712893486022949, 4.552312850952148, "The Purpose of the ALMA Atacama Large Millimeter/submillimeter Array is High-resolution observations."]
[3.700932741165161, 4.400362491607666, "The Additional Protection of the Avionics Components Components is Error correcting code on all memories and triple modular redundancy on logic gates in the used FPGAs."]
[11.666858673095703, -1.209315538406372, "The Mass of the Starlink Satellite Satellite is ~227 kg."]
[10.465963363647461, -1.1428004503250122, "The Mass of the HORYU-2 Nanosatellite is 7.1 kg."]
[9.686490058898926, -0.6676058769226074, "The Planned Number of Microsatellites of the PlanetIQ Satellite Manufacturer is 12."]
[7.89719820022583, 8.316620826721191, "The Absolute Accuracy Requirement of the CLARREO\u2019s infrared and reflected solar spectrometers Spectrometers is Unknown."]
[3.948303699493408, 4.385820388793945, "The Components of the Electrical System System is 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 ."]
[7.497546195983887, 7.00435209274292, "The Acquisition Frequency of the Navigation Images Imaging System is About every 4 hours."]
[7.799952507019043, 4.1073317527771, "The Number of Images Transmitted of the Tyvak-0130 Satellite is More than 4,500."]
[7.266488075256348, 0.5255593657493591, "The Launch Date of the EXPORTS Satellite Mission is July, 2018."]
[6.6945672035217285, 3.644503116607666, "The Module of the RAIDS Instrument is Kibo module of the ISS."]
[9.381604194641113, 0.7818911075592041, "The Years on Orbit of the AISSat-1 Satellite is 3 years."]
[4.7505784034729, 3.8943450450897217, "The Conference Location of the Space Plug-and Play Avionics Avionics is Los Angeles, CA, USA."]
[9.29267692565918, 5.350351333618164, "The Function of the MPACS Micro Propulsion Attitude Control System is Attitude control of the spacecraft."]
[9.72177505493164, 5.699183464050293, "The Ejection Mechanism of the Picosat Launcher Satellite Component is Latched door with a dual-release mechanism."]
[10.367813110351562, 2.758737325668335, "The Apogee Altitude of the Satellite Constellation Satellite Constellation is ~ 4,500 km."]
[11.720005989074707, 4.901852130889893, "The Brightness of the Quasars Energetic Sources is Up to 10 000 times brighter than the Milky Way."]
[9.387545585632324, 9.964576721191406, "The Objective of the PanCam Camera is Acquire 3D imagery of the lunar surface."]
[5.102523326873779, 3.5271875858306885, "The Spacing of the EDSN Swarm Satellite Network is ~20 km."]
[11.71328067779541, -1.0801594257354736, "The Mass of the ISEE-1 Spacecraft is 340 kg."]
[7.614511013031006, -0.2839021682739258, "The Date of the LPVEx Field Campaign is September and October 2010."]
[8.782864570617676, 7.299943447113037, "The Type of the AIDA Impact Detector Assembly is Advanced."]
[5.96905517578125, 3.5244977474212646, "The Initial Launch Service Procurement Plan of the Transport Layer Tranche 1 Satellite Network is Under commercial contracts."]
[7.581199645996094, 7.929859161376953, "The Reliability of the CERES Instrument is Highly reliable."]
[10.259510040283203, 2.956217050552368, "The Orbit Altitude of the AFSPC-11 Satellite Mission is 39,000 km."]
[8.558426856994629, 5.337865829467773, "The 0.035\u00ba of the Satellite Pointing Accuracy is S/C pointing accuracy = 0.035\u00ba."]
[9.126784324645996, 4.590470790863037, "The Wave Speed of the STEREO spacecraft Satellite is 250 km/s."]
[9.19221305847168, 9.175606727600098, "The Ensquared Energy of the Lens Optical Instrument is 90% within 60 x 60 \u00b5m."]
[4.803743839263916, 1.8393518924713135, "The Number of Satellites of the RapidEye Earth Observation Constellation is 5."]
[8.201634407043457, 8.715444564819336, "The FOV of the FTS Interferometer Interferometer is 1.25 mrad."]
[11.639896392822266, 6.162740707397461, "The Extension Approval Date of the XMM-Newton Satellite is Nov. 14, 2007."]
[10.744665145874023, 3.2328543663024902, "The Test Transmission Distance from Earth of the Herschel Spacecraft is 280,000 km."]
[7.117875099182129, 5.324485778808594, "The Data Distribution of the Aeolus Satellite is Near-real time."]
[6.358884811401367, 5.811593055725098, "The Wavelength Threshold of the CFOSAT Satellite is Larger than about 70 m."]
[7.547379016876221, 2.6010308265686035, "The URL of the ARTEMIS satellite Satellite is http://www.esa.int/Our_Activities/Operations/Artemis_the_ATV_whisperer."]
[6.76682710647583, 4.936490058898926, "The Data Usage of the CFOSAT Satellite is Improve the inversion algorithms for estimating wind speed and significant wave height, characterize the small scale roughness of all types of surfaces."]
[9.298685073852539, -0.6813228130340576, "The URL of the Aalto-1 Nanosatellite is http://blogs.aalto.fi/satellite/."]
[9.630223274230957, 1.5550917387008667, "The Ambient Ionosphere Forecast of the C/NOFS Satellite is Several hours ahead."]
[8.799798965454102, 10.624025344848633, "The Image Repetivity of the CCD Camera Imaging System is One scan line per minute."]
[6.908695220947266, 4.127545356750488, "The Measurement Category of the ZACUBE-2 Satellite is Multi-purpose imagery (land)."]
[3.9485437870025635, 6.579224109649658, "The Modulation of the XBT X-band Transmitter is QPSK."]
[10.301898002624512, 2.9997506141662598, "The Orbit Altitude of the Long March 5B Rocket Stage is 162 by 306 kilometers."]
[7.70596170425415, 0.893307626247406, "The Planned Date of the Maneuvers Orbital Adjustment is June 2015."]
[6.984534740447998, 4.225325107574463, "The Measurement Category of the KySat-2 Satellite is Multi-purpose imagery (land)."]
[9.958282470703125, 9.543073654174805, "The Objective of the SAGE-III Satellite is Provide global, long-term measurements of key components of the Earth's atmosphere."]
[10.501494407653809, 2.4153122901916504, "The Perigee (km) of the Meteor-1-1 Satellite is 644."]
[8.06483268737793, 9.805147171020508, "The Band Spacing of the OHIS Imaging System is 25 nm."]
[9.098116874694824, 8.906344413757324, "The Boresight Pointing Accuracy of the SXI Spacecraft is Within 3 arcmin elevation, within 3.5 arcmin azimuth."]
[8.22990608215332, 1.045478105545044, "The Image Capture Date of the Small Monitor Camera Camera is August 14, 2018."]
[4.013571262359619, 5.677063941955566, "The Image Telemetry Link of the SPOT-3 Satellite is 50 Mbit/s at 8 GHz."]
[8.58385181427002, 10.736194610595703, "The Power Supply of the LinkSprite JPEG color VGA camera Camera is 3.3 -5 V."]
[6.3902153968811035, 7.7599897384643555, "The Function of the AMR-C Microwave Radiometer is Provide a correction for the wet tropospheric path delay for the altimeter range measurement."]
[9.595293998718262, 1.3451789617538452, "The Retrieval Planned Time of the LDEF Satellite is 10 months."]
[10.17154598236084, 5.465376853942871, "The Testing of the Valves Spacecraft Component is Ongoing."]
[9.501544952392578, 8.843213081359863, "The Spatial Resolution & Stability of the Telescope Optical Instrument is Encircled Energy of 75% at 1 \u00b5m for 150 mas radius."]
[5.268312931060791, 3.111839532852173, "The Funding of the NorSat-3 Satellite is NCA (Norwegian Coastal Administration)."]
[8.139716148376465, 2.102656602859497, "The URL of the Van Allen Probes Satellite is http://www.nasa.gov/feature/goddard/2016/nasa-s van-allen-probes-revolutionize-view-of-radiation-belts."]
[6.025998592376709, 9.650707244873047, "The Cargo Mass of the CREAM Cosmic-Ray Instrument is 1,258 kg."]
[5.930505275726318, 4.402804374694824, "The Data Encryption of the SeaWiFS Satellite is Real time LAC data are encrypted."]
[6.618940353393555, 1.1635288000106812, "The Conference Date of the Alphasat Concept Hosted Payload Operations is May 5-9, 2014."]
[9.061275482177734, 9.803129196166992, "The Function of the Target Sensor Photodiode is Solar and lunar acquisition."]
[3.366978406906128, 4.459701061248779, "The Distribution Function of the PDU Power Distribution Unit is Distributes power to the equipment."]
[7.3127760887146, 8.555583000183105, "The Spatial Resolution of the HIRES Instrument is About 2 km at 400 km altitude."]
[5.781115531921387, 6.785914421081543, "The Transmitting Pulses of the Instrument Radar Instrument is H or V."]
[5.117376327514648, 9.250462532043457, "The Sensitivity of the SEIS Seismometer is High."]
[7.389771938323975, 10.002388000488281, "The Instrument Type of the Hyperion HSI (Hyperspectral Imager) is Pushbroom."]
[5.794824600219727, 2.6548311710357666, "The Manufacturer of the ION CubeSat Carrier Satellite is D-Orbit."]
[5.71399450302124, 6.826876163482666, "The Reception of the Receive Chain Radar Instrument is Either H or V."]
[7.177335262298584, 7.955356121063232, "The Registration Time of the RFA Instrument is 50 ms."]
[7.876243591308594, 9.784319877624512, "The | of the SpectraAalto-1 Spectral Imager Spectral Imager is Miniature SpectraAalto-1 Spectral Imager."]
[7.413298606872559, 9.888265609741211, "The Spectral Resolution of the Hyperion Imaging Spectrometer is 10 nm in VNIR and SWIR."]
[8.103130340576172, 10.797412872314453, "The Digitization of the Camera Electronics Data is 10 bits."]
[4.372765064239502, 5.3600382804870605, "The Redundancy of the TT&C Transmitter Communication Device is Half Satellite."]
[7.175400733947754, 3.273441791534424, "The Operation Status of the NEOSSat Satellite is Operating well."]
[4.239512920379639, 4.59688138961792, "The Interface of the Instrument Control Unit (NI-ICU) Control Unit is 1553 bus."]
[6.66753625869751, 7.674464702606201, "The Output Information of the AVGS Laser System is Azimuth, elevation, range, and relative attitude."]
[1.8073899745941162, 4.0928955078125, "The Connector Type of the Satellite Satellite is Second connector provides access to the battery and charging circuitry."]
[8.8292818069458, 10.40310001373291, "The Mode of the LISS-4 Imaging System is Mx mode."]
[5.853549957275391, 4.304192066192627, "The Function of the Satellite Satellite is Create a random string of numbers to represent an encryption key."]
[9.378861427307129, -0.7077697515487671, "The Launch Date of the Carbonite-2 Microsatellite is January 2018."]
[7.874197483062744, 5.179164886474609, "The Mission of the SPATIUM-I CubeSat is Demonstrate technology aimed at electron density measurement and three-dimensional mapping of ionosphere."]
[7.91563606262207, 4.432450294494629, "The Resolution of the WorldView 4 Satellite is High."]
[2.016895055770874, 7.847270965576172, "The Solar Wind Speed and Beta of the ACE Satellite is ~55% lower on average from 2009 through the day 79 of 2013."]
[5.315484046936035, 10.39404296875, "The Measurement Components of the LI System Lightning Information System is IC (Intra Cloud) and CG (Cloud Ground)."]
[9.134271621704102, 3.2268917560577393, "The Orbit Type of the MMO Spacecraft is Polar elliptical orbit."]
[10.181669235229492, 6.782864570617676, "The Solar Cells per Panel of the TCS Thermal Control System is 19."]
[3.1238412857055664, 4.845902919769287, "The FRAM of the GomSpace NanoMind A3200 Onboard Computer is 32 kB."]
[9.661577224731445, 6.013189792633057, "The Components of the ADCS Attitude Determination and Control Subsystem is Attitude sensor, actuator interface assembly, four digital sun sensors, magnetic coils, momentum wheel."]
[9.390420913696289, 1.8059440851211548, "The Pass Frequency of the Satellite Orbit Type is Between two and four times per day."]
[8.485950469970703, 3.631535291671753, "The Deployment Duration of the RDA Deployment System is Not provided."]
[1.7341227531433105, 4.173912525177002, "The Solar Cells Manufacturer of the EPS Electric Power Subsystem is Emcore."]
[6.440094470977783, 8.235756874084473, "The Data Coverage of the AMSU Microwave Radiometer is Vertical temperature profiles up to 50 km."]
[5.906990051269531, 2.8306634426116943, "The Focus of the Bigelow Aerospace Aerospace Company is Space Agencies, Commercial Users."]
[8.734561920166016, 9.152143478393555, "The entrance slit width of the Spectrograph Instrument is  6\u00ba."]
[4.384284973144531, 6.12610387802124, "The Band of the RF Communications Data Transmission is X-band."]
[8.155917167663574, 8.901081085205078, "The Spectral Range of the Observation Instrument Telescope/Spectrograph is 55-210 nm."]
[11.018402099609375, 2.8555850982666016, "The Name Meaning of the Watoga Lake Lake is Cherokee word for \u201cstarry waters\u201d."]
[9.555214881896973, 0.4953111410140991, "The Design Life of the QuikTOMS spacecraft Satellite is Three years."]
[9.59671401977539, 7.280215263366699, "The Optimal Ground Condition of the HP3 (Heat Flow and Physical Properties Package) Heat-flow probe is Level ground without rocks larger than about 1.5 cm."]
[2.218207836151123, 4.485343933105469, "The Power Generation of the IRIS Satellite is 340 W."]
[4.039984703063965, 1.2021358013153076, "The Mission Type of the FalconSat-3 Satellite is Non-EO."]
[4.2381486892700195, 2.5435073375701904, "The Actual Starlink Terminals of the Starlink Satellite Internet Service is Much lower than 200,000 or even zero."]
[6.7559099197387695, 1.7308850288391113, "The Calibration and Validation Approach Date of the Envisat Satellite is Oct. 2000."]
[7.50916051864624, 3.6214518547058105, "The Fishing Spot of the Shikisai Satellite is Japanese pilchard (Sardinops melanostictus)."]
[4.791337013244629, 0.9232873320579529, "The Funding Round Amount of the Aleph-1 Constellation Satellite Constellation is $27 million."]
[8.427091598510742, 8.93864917755127, "The Period of the BUV Sensor is 107.2 minutes."]
[4.611196517944336, 4.586559295654297, "The Message Bus Function of the MCS Communication System is Provides a publish/subscribe mechanism."]
[9.158467292785645, 0.764227569103241, "The Years on Orbit of the Landsat-7 Satellite is 19 years."]
[8.477341651916504, 10.250147819519043, "The Construction of the Focal Plane Structure Structural Component is Complex 3d structures built rapidly from sheet metal primitives."]
[5.195237636566162, 6.084654331207275, "The Location of the X-band antenna Antenna is Nadir face."]
[3.6340854167938232, 4.458090305328369, "The CPU of the ACU Attitude Control Unit is HD64F7145FW50."]
[6.748455047607422, 0.9098498225212097, "The End of Life Date of the FalconSat-3 Satellite is 1 April 2017."]
[4.755350112915039, 4.0788373947143555, "The Issue of the Starliner Spacecraft is Timing error in the software."]
[8.311025619506836, 9.191946983337402, "The Spatial Resolution of the TIRS-2 Sensor is 100 m."]
[7.767397403717041, 3.9041004180908203, "The Data Release Frequency of the COSMIC-2 Satellite Constellation is Daily."]
[7.972435474395752, 1.908842921257019, "The Image Acquisition Date of the ExoMars Trace Gas Orbiter Orbiter is 27 June 2018."]
[7.578540325164795, 0.5510565042495728, "The Mission Date of the GRACE Satellite is 21 Dec. 2017."]
[4.197546005249023, 5.697798252105713, "The X-band Downlink Transmission Data Rates of the CBERS-2B Satellite is 60 Mbit/s."]
[4.8928303718566895, 9.14892292022705, "The Seismometer of the InSight Lander Lander is SEIS (Seismic Experiment for Interior Structure)."]
[7.65521240234375, 7.966325283050537, "The Type of the TANSO-CAI Instrument is Atmospheric chemistry."]
[6.977303981781006, 7.703262805938721, "The Design Improvement of the HARP Imaging Polarimeter is Advance over POLDER\u2019s (POLarization and Directionality of the Earth's Reflectances) filter wheel system."]
[8.755331039428711, 1.514330267906189, "The Nonlinear Wave Structures Effect of the Van Allen Probes Satellite is Rapidly energize very low energy (~10 electron volts) electrons up to intermediate energies (~100 keV)."]
[8.955501556396484, 0.7151333093643188, "The Testing Duration of the JUICE Spacecraft is Several weeks."]
[9.656716346740723, 3.9023945331573486, "The Specific Impulse of the CanX-4&5 Satellite is 35 s."]
[4.524868965148926, 4.821409702301025, "The Integration Status of the Optical Module Subsystem is Completed."]
[7.695024013519287, 4.297059059143066, "The Objectives of the ATLAS-1 Satellite Mission is 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 u."]
[10.256171226501465, 5.649599552154541, "The Energy Conversion of the Electrodynamic Tether (Power or Drag System) Propulsion and Power Generation Device is Converts the orbital energy of the host S/C into electrical power."]
[9.858238220214844, -0.5151575803756714, "The Design Life of the Tsubame Microsatellite is 1 year."]
[9.391021728515625, 8.149169921875, "The TM/TC Interface of the RAMIS Radiation Detector is RS-485."]
[11.498146057128906, -1.328494906425476, "The Mass of the TDS-1 Satellite is 150 kg."]
[8.782344818115234, 8.880953788757324, "The Thickness of the Aluminum Film Optical Instrument Component is 70 nm."]
[10.351049423217773, 1.9582462310791016, "The Period (min) of the Meteor-1-1 Satellite is 97.9."]
[6.658818244934082, 0.3965274393558502, "The Launch Date of the INSAT-3DR Satellite is Sep 9, 2016."]
[6.487003326416016, 2.879805088043213, "The Signal Usability of the Galileo Satellite Constellation is Usable in all new mobile phones."]
[9.329952239990234, 1.91031014919281, "The Global Coverage of the GNOS-2 Satellite is 2 weeks."]
[11.66686725616455, 2.5830929279327393, "The Size of the Psyche Asteroid is About the size of Massachusetts."]
[5.5526442527771, 3.6252737045288086, "The Lead of the Science Office Office is \u201cScience Systems Engineering\u201d effort."]
[5.305509567260742, 2.3984668254852295, "The Post-Project Careers of the SAPPHIRE Satellite is Nine hold significant spacecraft systems or management responsibilities with aerospace contractors, the Air Force or academia."]
[6.660281181335449, 2.974139451980591, "The Mission Extension of the Envisat Satellite is Yes."]
[6.836972713470459, 5.498305320739746, "The Purpose of the SMAP Satellite is Measure soil moisture."]
[4.746431827545166, 1.8897038698196411, "The Number of Satellites of the Unseenlabs' Constellation Satellite Constellation is 3."]
[9.087224006652832, 10.587594032287598, "The Spatial Resolution of the MSU-50 Camera is 120 m."]
[4.091207981109619, 4.345056056976318, "The Function of the OBCS On-Board Computer Subsystem is Main flight computer which runs the flight software (FSW)."]
[11.871928215026855, 2.384584426879883, "The Distance from Bennu of the OSIRIS-REx Spacecraft is 155 miles (250 km)."]
[4.7453436851501465, 0.853346049785614, "The Contract Value of the Planet Satellite Imaging Company is $20 million."]
[9.452381134033203, 7.285958290100098, "The Probe Development Location of the Electron Temperature Part Experiment is IKI (Institute of Space Research) Moscow, Russia."]
[6.87647008895874, 4.248599052429199, "The Measurement Domain of the Odin Satellite is Atmosphere."]
[9.416654586791992, 0.9639924764633179, "The Planned Mission Duration of the Wind Satellite is 5 years."]
[8.214316368103027, 5.31046724319458, "The Purpose of the GEOTAIL Satellite is Determine the overall plasma, electric and magnetic field characteristics of the distant and geomagnetic tail."]
[6.259766101837158, 0.012456650845706463, "The Launch Time of the Galileo FOC-3 and FOC-4 satellites Satellite is 21:46 UTC."]
[9.195539474487305, 9.061646461486816, "The Angular resolution (2 px) of the HRI dual EUV 174 \u00c5 and 335 \u00c5 alternatively Passband center is 1 arcsec."]
[6.148593425750732, 5.665856838226318, "The | of the SGR-ReSI GNSS Receiver is Introducing the SGR-ReSI: A Next Generation Spaceborne GNSS Receiver for Navigation and Remote-Sensing."]
[8.511456489562988, 7.33351993560791, "The Position of the ULF Sensor Sensor is Tip of the gravity gradient boom."]
[9.626103401184082, 3.1466031074523926, "The Operational Orbit of the Spacecraft Satellite is Lissajous orbit at an average distance of 800,000 km from L2."]
[4.507286071777344, 2.765779495239258, "The VPU of the Ubotica CogniSAT-XE1TM CubeSat Board Satellite Device is Intel\u00ae Movidius\u2122 Myriad\u2122 2."]
[8.999329566955566, 4.281027317047119, "The Side Length of the HIT-Sat Satellite is 12 cm."]
[4.163153171539307, 2.411484718322754, "The Form Factor of the 6U CubeSat Satellite is 6U."]
[11.167973518371582, 6.757150650024414, "The Horizon Sensing of the X-ray Navigation Navigation System is Only the upper atmosphere is traversed by a ray grazing the effective horizon."]
[6.0785932540893555, 3.1429455280303955, "The Status of the M3MSat Satellite is In storage."]
[7.210049152374268, 0.5663360357284546, "The Launch Date of the TOPEX/Poseidon Satellite is Aug. 10, 1992."]
[9.909358978271484, 4.517016887664795, "The Volume Occupation of the Solar Sail Subsystem Spacecraft Subsystem is Lower 2/3 of the spacecraft."]
[7.550922393798828, 3.7292988300323486, "The Relative Position of the AC4-B Satellite is Catch up with and pass AC4-A."]
[7.2729597091674805, 10.166504859924316, "The Launch Date of the HyperScout Hyperspectral Imager is 2 February 2018."]
[8.842985153198242, 3.30407977104187, "The Orbit of the SuperView-1 Observation Satellites is Low Earth."]
[10.121460914611816, 4.897618770599365, "The Propulsion Subsystem of the SGEO Satellite is Electric."]
[7.940042018890381, 5.946699619293213, "The Pointing Capability of the Satellite Imaging Satellite is Allows calibration using the sun, moon and stars."]
[7.876987457275391, 9.103507995605469, "The Spectral Bands of the OLCI Spectral Imaging Instrument is 21."]
[10.608455657958984, 3.8355085849761963, "The Mission of the Solar Orbiter Spacecraft is Perform unprecedented close-up observations of the Sun."]
[4.893717288970947, 0.9442371726036072, "The Annual Spending on Commercial Data of the NASA Organization is Roughly $30 million."]
[5.037853240966797, 6.1546149253845215, "The Type of the Beacon station antenna Antenna is 7-element Yagi antenna."]
[4.301766872406006, 3.2118172645568848, "The Key Technologies of the SATis5 Testbed is 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 environ."]
[4.41572380065918, 6.346860408782959, "The Layout of the Transponder Communication System Component is Downconverter, LNA, RF switch matrix, Upconverter, channel amplifier, TWT."]
[6.64668607711792, 1.1320396661758423, "The Launch Date of the Alphabus Satellite Platform is Jan. 29, 2010."]
[8.153615951538086, -0.6385595202445984, "The Mission Duration of the Crew Dragon Spacecraft is Three days."]
[4.2464680671691895, 6.572532653808594, "The Downlink Frequency of the RF Communications Communication System is 430 MHz."]
[10.183198928833008, 3.0358450412750244, "The Operating Altitude of the Sentinel-6 and Jason-3 Satellites is 1330 km."]
[7.569216251373291, 6.282471179962158, "The Measurement Range of the Cloud Top Pressure Satellite Instrument is 200-900 hPa."]
[5.8307905197143555, 8.511210441589355, "The Measurement Difference of the CDN1 transponder Transponder is Less than 2 mm."]
[8.88145637512207, 7.652372360229492, "The Measurement of the Electric Field Instrument Instrument is Temperature 300 km above Earth\u2019s surface jumped by 3000\u00baC."]
[6.023216724395752, 8.111308097839355, "The Operating Frequency of the 183 GHz radiometers Radiometer is 183 GHz."]
[11.135188102722168, 2.7804200649261475, "The Previous Record Crest Height of the Yellowstone River River is 11.5 feet."]
[3.6545088291168213, 6.171523094177246, "The Data Rate of the X-band downlink system Communication System is Up to 80 Mbit/s."]
[7.314908981323242, 1.173541784286499, "The Operation Period of the Nimbus-7 Satellite is 1978 until 1994."]
[8.350425720214844, 3.419942855834961, "The Data Resolution of the TanDEM-X Satellite is 50 m x 50 m."]
[10.090177536010742, 5.232522010803223, "The Force of the Thrusters Attitude Control is 10 Newton."]
[8.381839752197266, 5.255159854888916, "The Pointing Accuracy of the Alphasat TDP1 and Sentinel-1A Optical Link is Better than 500 \u00b5rad."]
[6.5619683265686035, 0.8402632474899292, "The Launch Date of the GOSAT-2 Satellite is October 2018."]
[5.263638496398926, 3.1335480213165283, "The Purpose of the QSAT Satellite is Polar Plasma Observation."]
[7.712751865386963, 0.6188944578170776, "The Launch Year of the RemoveDebris Mission is 2018."]
[7.886801242828369, 2.0524494647979736, "The Objectives of the ISEE-1 Spacecraft is 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."]
[9.212035179138184, 7.93784236907959, "The EUV Imager of the SWAP Instrument is Unknown."]
[3.268200635910034, 5.478105545043945, "The Data Transfer Rate of the SSRNI Data Acquisition and Registration System is 7.68 Mbit/s."]
[9.207064628601074, -0.6274568438529968, "The Launch Date and Time of the GHGSat-C2 (Hugo) Nanosatellite is January 24, 2021, at 15:00 UTC."]
[7.905586242675781, 4.6350297927856445, "The Image Resolution Comparison of the Solar Orbiter Satellite is Ten times better than what a 4k TV screen can display."]
[9.64453125, 1.318389892578125, "The Survey Mode Duration of the C/NOFS Satellite is 9 months."]
[8.936346054077148, 9.222403526306152, "The FPA NEDT of the CIRiS Instrument is < 50 mK."]
[7.23361349105835, 6.861035346984863, "The Priority of the LEP-EA and LEP-E Instruments is High."]
[5.3132643699646, 10.390462875366211, "The Application of the Falcon Neuro Neuromorphic Cameras is Sprite and lightning detection on the International Space Station."]
[10.181255340576172, 4.823416709899902, "The Thrust Level of the Satellite Spacecraft is Varying."]
[9.953579902648926, 4.452338218688965, "The Propellant of the Lunar Flashlight CubeSat is \"Green\" propellant."]
[8.27813720703125, 1.0562028884887695, "The Commissioning Completion Date of the RAIDS Experiment is October 22, 2009."]
[8.888354301452637, 7.589510917663574, "The Type of the HPCA Electrostatic Analyzer is Toroidal top-hat."]
[6.960084915161133, 6.183199405670166, "The Temporal Sampling of the Sea Surface Temperature (SST) Measurement is Sub-daily."]
[6.654388904571533, 3.730308771133423, "The Manufacturer of the Sich-2 Satellite is Yuzhnoye State Design Office (SDO)."]
[5.591047763824463, 2.7887496948242188, "The Constellation Builder of the UrtheCast Company is SSTL (Surrey Satellite Technology Ltd.),UK."]
[7.992833137512207, 4.150697708129883, "The Route of the A-68A Iceberg is Across the Drake Passage."]
[7.34954833984375, 0.5329223871231079, "The Scheduled Launch of the Hugo Satellite is By the end of the year."]
[7.480484485626221, 8.434881210327148, "The SNR in bands 1 and 2, in band 3 of the Scanning geometry Instrument is \u2265 200, \u2265 100."]
[11.809341430664062, 2.4281811714172363, "The Distance from Bennu of the OSIRIS-REx Spacecraft is 1,635 miles (2,200 km)."]
[3.4683635234832764, 6.678409099578857, "The Data Rate (max) of the CanX-2 S-band Transmitter/Transceiver is 1024 kbit/s."]
[5.280966758728027, 5.3601531982421875, "The Coverage Zones of the Scientific Payload Satellite Payload is 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): anch."]
[6.859622478485107, 6.245538234710693, "The Applications of the ASAR Instrument is 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,."]
[6.55280876159668, 6.3942389488220215, "The Grid Size of the RAS Product Data Product is 25 km."]
[7.962881088256836, 4.182818412780762, "The Spatial Resolution of the GHOSt Satellite Constellation is 8 m."]
[7.112736701965332, 2.4844722747802734, "The URL (paper) of the Cute-1.7+APD Nano-Satellite is http://lss.mes.titech.ac.jp/ssp/cute1.7/paper/aca2007.pdf."]
[9.057819366455078, 10.658534049987793, "The Spatial Resolution of the MSC Camera is 5.8 m."]
[6.622721195220947, 0.6397605538368225, "The Mission Operations Date of the SkySat Satellite is May 28-June 1, 2018."]
[9.118268966674805, 9.314602851867676, "The | 100 x100 km2 of the IASI-NG Instrument Field Of View (FOV) Size is The resulting FOV is in the order of 100 x100 km2."]
[7.949639797210693, 4.589789390563965, "The Spatial Resolution of the DubaiSat-2 Satellite is 1.0 m (Pan), 4 m (MS)."]
[7.278666973114014, 7.846100330352783, "The Jitter of the GOCI Instrument Instrument is Less than 10 \u00b5rad."]
[8.914359092712402, 2.4528262615203857, "The Observation Results of the Herschel Space Observatory is Gas filaments become unstable and form clumps of material bound together by gravity."]
[8.979924201965332, 7.287347793579102, "The Range of the Horizon sensor Sensor is \u00b15.5\u00ba."]
[9.343472480773926, 9.110490798950195, "The Aperture of the Instrument Optical Instrument is 8 cm."]
[6.321243762969971, 3.014115571975708, "The Agency of the MidSTAR-1 Satellite is USNA (United States Naval Agency)."]
[10.355082511901855, 1.3177162408828735, "The LTAN of the Satellite Orbit is 18:00 hours."]
[5.953526020050049, 1.638506531715393, "The Mission of the PAZ Satellite is Dual-use (civil/defence)."]
[9.058202743530273, 10.574943542480469, "The Image Size of the NAVCAM Camera is 866 x 866 m."]
[1.173271656036377, 4.259454250335693, "The Protection of the Batteries Power Storage is Integrated over current protection."]
[10.43368911743164, 4.940189361572266, "The Thrust of the DMC Propulsion Subsystem Electric Propulsion is 50 mN."]
[11.686954498291016, -1.1239147186279297, "The Mass of the SpinSat Spacecraft is 57 kg."]
[12.9456205368042, 4.84354305267334, "The Particle Detection Location of the IBEX Spacecraft is Outer heliosphere."]
[8.572164535522461, 2.778294563293457, "The Role of the Martin Popek Individual is Passionate about capturing sprites, jets and elves on camera."]
[10.630842208862305, -1.6903258562088013, "The Transportation Capacity of the HTV-9 Cargo Transfer Spacecraft is World's largest."]
[10.353352546691895, 1.2888206243515015, "The LTAN of the NEMO-HD Satellite is 10:30 hours."]
[4.461556911468506, 2.4649291038513184, "The Close Approach Coordination of the Starlink Satellite Constellation is With multiple government and commercial satellite operators."]
[8.194404602050781, 7.99023962020874, "The Scanning Capability of the ISAMS Instrument is Vertically and to either side of the UARS observatory."]
[7.9709792137146, 8.969956398010254, "The Wavelength Range of the BEO Back-End Optics is 400-1100 nm."]
[10.058589935302734, 9.259642601013184, "The Optics Design of the NFOV Imagers Imaging System is Cassegrain design."]
[8.606980323791504, 10.489190101623535, "The Data Acquisition Method of the CCD Detector Imaging System is Rotating the imaging system, including the CCD, at a rated synchronization with a vertical charge transfer of the CCD detector."]
[6.952543258666992, 0.4349055588245392, "The Launch Date of the ZACUBE-2 Satellite is 27 Dec 2018."]
[4.965364456176758, 7.696234703063965, "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."]
[4.7984700202941895, 0.8819490075111389, "The Development Cost of the SAOCOM-1A Satellite is $500 million."]
[4.988882541656494, 1.5106319189071655, "The Mission Status of the FormoSat-7 / COSMIC-2 Satellite Constellation is Unknown."]
[6.364627361297607, 4.004271507263184, "The Dataset Sizes of the EO-ALERT Satellite System is Wide range."]
[5.357186794281006, 6.582187175750732, "The Number of Elements of the PR Phased Array System is 128."]
[7.148492813110352, 5.078641891479492, "The Measurement Targets of the GeoCARB Satellite is Carbon dioxide, carbon monoxide, methane and Solar-Induced Fluorescence quantities."]
[8.73688793182373, 10.361543655395508, "The Frame Rate of the ROIC/FPA Imaging System is 16 kHz."]
[4.051941871643066, 5.618277072906494, "The Data Downlink Rate of the MinXSS-2 Satellite is At least a factor of 6 increase from 1 MB per day."]
[9.436022758483887, 5.562494277954102, "The Antenna pointing accuracy of the AOCS Attitude and Orbit Control System is < 0.1\u00ba (3\u03c3) half cone."]
[4.887500286102295, 5.006779670715332, "The Duration of the Ground Station Passes Ground Station is 8 hours."]
[6.349305629730225, 7.236967086791992, "The Wave Height Measurement Accuracy of the ALT Experiment Altimeter is 10% or 0.5 m, whichever was greater."]
[9.382614135742188, 9.343621253967285, "The Bandwidth of the Aperture Function Image Processing is 2D."]
[7.478410720825195, 0.7962164282798767, "The First Image Download Date of the LightSail Satellite is June 2, 2015."]
[7.359900951385498, 4.533758163452148, "The Measurement of the FORUM Satellite Mission is Far-infrared radiation emitted from Earth."]
[9.182527542114258, 3.2393510341644287, "The Orbit Type of the DMC-3 Constellation Satellite Constellation is Sun-synchronous orbit."]
[6.353079319000244, 2.445558786392212, "The Leader of the Marsquake Service Service is ETH Zurich."]
[6.970751762390137, 4.283506393432617, "The Measurement Category of the OSCAR-QUBE Satellite is Gravity, Magnetic and Geodynamic measurements."]
[11.420217514038086, 2.187178134918213, "The Journey Duration of the Hayabusa-2 Spacecraft is 42 months."]
[9.62522029876709, 5.955048561096191, "The Control Methods of the ADCS Attitude Determination and Control System is Unique control method using aerodynamic drag."]
[1.489194393157959, 4.983625888824463, "The Voltage of the HVSA High Voltage Experiment System is 350 V."]
[10.67562484741211, 4.113349437713623, "The Purpose of the Humanity Star Artistic Light Beacon is Purely artistic."]
[11.40983772277832, 4.1437153816223145, "The Composition of the TRAPPIST-1 Planets Planets is Similar Stuff."]
[8.033447265625, 5.857706069946289, "The Pointing Jitter of the ASTERIA Satellite is 1\u03c3 ~0.5\"."]
[6.515432357788086, 7.913672924041748, "The Wavelength Stability of the LD Output Laser Diode is <0.1%."]
[8.177465438842773, 10.01315975189209, "The Manufacturer of the C3D Imager Imager is Clyde Space."]
[8.920310020446777, 4.823488712310791, "The Residual Acceleration of the GP-B satellite Satellite is 4\u00d710-11 m s-2."]
[6.861405849456787, 4.714366912841797, "The Instruments of the FORUM Satellite is Cloud Radar, Imager, Sounder."]
[4.301738262176514, 2.47149920463562, "The Design of the BRO-1 Satellite is 6U CubeSat."]
[8.6139497756958, 3.2082979679107666, "The Development Status of the GCOM-C1 Satellite System is Unknown."]
[5.553915023803711, 1.524583339691162, "The Manufacturer of the NanoRacks Airlock Module Airlock Module is NanoRacks."]
[3.9884192943573, 2.33970308303833, "The Size Comparison of the ORS-3/STPSat-3 Satellite is 6 times bigger than TechEdSat."]
[6.538887977600098, 6.337008953094482, "The Development Partners of the SGR-ReSI Instrument is SSTL, University of Surrey, National Oceanographic Centre, University of Bath, Polar Imaging Ltd.."]
[7.380039215087891, 2.6942548751831055, "The Return to NASA's Kennedy Space Center of the Orion Spacecraft is Will return to NASA's Kennedy Space Center."]
[9.394889831542969, 8.087879180908203, "The Low-Energy Threshold of the Detector Instrument is 2.5 keV."]
[5.629392147064209, 9.195819854736328, "The Power Consumption of the SIR-2 Instrument is 2.2 W."]
[9.541035652160645, 6.103765487670898, "The Safe Mode Operation of the ADCS Attitude Determination and Control System is Coarse sun pointing."]
[9.318316459655762, -0.574978232383728, "The Ground Station of the Nanosatellite Satellite is Kagawa University."]
[9.439594268798828, 5.077240467071533, "The Reaction Wheel Spin Rate of the Integral Satellite is About 17 degrees per minute."]
[11.281363487243652, 4.5934529304504395, "The Discovery Year of the W\u2013 boson Particle is 1983."]
[11.390048027038574, -1.3342549800872803, "The Mass of the TechnoSat Satellite is 18 kg."]
[9.468121528625488, 0.9573786854743958, "The Anniversary of the TIMED Satellite is 10 Years."]
[8.344304084777832, 1.0812292098999023, "The Manifestation Date of the HICO and RAIDS Instruments is Spring of 2007."]
[3.2526943683624268, 6.039275646209717, "The Compatibility of the Frontier Radio Radio is NASA's STRS (Space Telecommunications Radio System) architecture."]
[9.37865924835205, 9.28469181060791, "The Mask Thickness of the Optical Head Optical Device is 0.1 mm."]
[7.355578422546387, 1.6482489109039307, "The Publication Date of the Colliding star clusters Article is 3 January 2022."]
[9.488435745239258, -2.5151865482330322, "The Telemetry of the LEICA Particle Detector is 1.3 kbit/s."]
[10.845014572143555, 4.215473651885986, "The Mission Purpose of the SPARCS Satellite is Understand the Impact of Stars in Exoplanets."]
[6.100602626800537, 0.8210197687149048, "The Launch Date of the Iridium-4 NEXT Mission Satellite Mission is December 2017."]
[5.849700450897217, 4.785552024841309, "The Manufacturer of the Cupola Window is TAS-I."]
[3.8737030029296875, 4.527842998504639, "The Data Bus Interface of the PCU Power Control Unit is SpaceWire type."]
[6.717161655426025, 7.61666202545166, "The Range of the Laser Rangefinder Device is Up to 2 km."]
[7.969557285308838, 9.3431396484375, "The Wavelength of the FAI Auroral Imager is 630 nm."]
[8.271893501281738, 6.360588073730469, "The Cost (sensor + spacecraft) of the Pushbroom Sensor is High."]
[5.13555383682251, 1.368590235710144, "The Interface Requirement Document of the FORMOSAT-7/COSMIC-2 Satellite is FS7-IRD-0002."]
[7.899413108825684, 4.452254295349121, "The Spatial Resolution of the Ikonos-2 Satellite is 0.82 m."]
[10.619384765625, 9.27270793914795, "The Image Segment Size of the CaSSIS Imaging System is 22.7 x 6.6 km."]
[7.117794036865234, 7.142877101898193, "The Unknown of the MIPAS Instrument is Unknown."]
[5.778037071228027, 2.6217989921569824, "The Country of the skCube Satellite is Slovakia."]
[6.235241889953613, 1.1879552602767944, "The International Cooperation Presentation of the COSMO-SkyMed Satellite is 68th IAC (International Astronautical Congress), Adelaide, Australia, 25-29 Sept. 2017."]
[7.920424461364746, 0.6509509682655334, "The Launch Date of the Starliner Spacecraft is Dec. 20."]
[11.336874961853027, 3.6180877685546875, "The Mass of the Comet Celestial Body is 10 billion tons."]
[4.9196295738220215, 4.917494297027588, "The Data Transmission of the EUMETCast Dissemination System is Multicast files."]
[5.312851428985596, 10.38976001739502, "The Data Usage of the ISS LIS Lightning Imaging Sensor is Air-traffic advisories, climate monitoring."]
[8.24477481842041, 3.0517072677612305, "The Conference Date of the TanDEM-X Satellite is May 29-31, 2013."]
[2.2534518241882324, 4.4347429275512695, "The Power Requirement of the Payload Satellite Component is 100 W."]
[3.21406888961792, 4.782205581665039, "The Architecture of the GomSpace NanoMind A3200 Onboard Computer is AVR32."]
[11.667899131774902, -1.2813706398010254, "The Mass of the BRITE-Austria Satellite is 6.5 kg."]
[11.045936584472656, 2.855041742324829, "The Length of the Krishna River River is 1,300 km."]
[5.330591678619385, 3.3466458320617676, "The Initiator of the CSD Satellite Component is Reusable."]
[5.547888278961182, 3.178224563598633, "The Bus Type of the GFO Satellite is BCP 600 (Ball Commercial Platform)."]
[7.236271858215332, 4.0471906661987305, "The Designed for of the Landsat-7 Satellite is Earth-observing."]
[7.101404666900635, 3.9019176959991455, "The Remarks/Sensors of the OrbView-2 Satellite is SeaWiFS."]
[7.196231365203857, 9.754661560058594, "The Spectral Range of the DNB Spectral Band is 0.5-0.9 \u00b5m."]
[7.25242280960083, 3.390014886856079, "The Magnetometer Status of the NEOSSat Satellite is Failed."]
[5.819395065307617, 6.8055500984191895, "The Sigma 0 Range of the Radar Radar is HV, VH: +5~-35 dB."]
[13.088479042053223, 4.014249324798584, "The Lagrange Point of the Gaia Satellite is Lagrange point 2."]
[3.8452587127685547, 4.600178241729736, "The Components of the OBDH On Board Data Handling and Communications is Microcontroller and the other circuits needed for data storage, communication, conversions, timing and execution of the tasks."]
[10.211675643920898, 5.024994373321533, "The Propulsion of the Spacecraft Satellite is Slanted N2H4 monopropellant thrusters."]
[6.6951446533203125, 0.7580220103263855, "The Launch Date of the NigeriaSat-X Satellite is 17 Aug 2011."]
[6.7520880699157715, 0.7741935849189758, "The Separation Date of the STRaND-1 Satellite is February 25, 2013."]
[7.893967151641846, 4.489057540893555, "The NDVI Map Spatial Resolution of the RISING-2 Satellite is About 10 m."]
[8.60033130645752, 6.918516159057617, "The Function of the Fluxgate and search coil magnetometers Sensor is Measure low frequency and wave magnetic fields."]
[6.197447776794434, 3.054750442504883, "The Assistants of the COMS Satellite is Astrium, KARI (Korean Aerospace Research Institute), and KIOST (Korean Institute of Ocean Science and Technology)."]
[9.45594310760498, 5.898712158203125, "The Attitude Control of the ACS Attitude Control Subsystem is \u00b10.05\u00ba."]
[8.91038990020752, 6.509033203125, "The Components of the SIA Science Instrument Assembly is Four quartz gyroscopes aligned in a fused-quartz block."]
[3.8965988159179688, 6.3183088302612305, "The Data Rate of the OSIRISv3 Laser Communication Terminal is Up to 1 Gbit/s."]
[9.566519737243652, 8.747485160827637, "The Manufacturer of the NESSI Telescope is Spectral Applied Research Inc.."]
[9.15749454498291, 4.213337421417236, "The Bus Dimensions of the PRISMA Satellite is 1.751 x 1.545 x 3.4 m."]
[9.20711612701416, 10.6173095703125, "The Footprint of the LWIR Cameras Camera is 9911 km2."]
[6.120959281921387, 6.59616231918335, "The Bands of the Poseidon 4 Radar Altimeter is Ku- and C- band."]
[6.8249006271362305, 0.6341916918754578, "The Launch Date of the VNREDSat-1A Satellite is Unknown."]
[7.3359174728393555, 5.726761817932129, "The Mission Objective of the CALIPSO Satellite is Assess the impact of aerosols on Earth\u2019s radiation budget through the aerosol direct and indirect effects."]
[8.576237678527832, 10.062257766723633, "The Focal Planes of the ETM+ Scanner Imaging Device is 2."]
[8.858859062194824, 3.212373971939087, "The Orbit of the Spacecraft Satellite is GEO (Geostationary Orbit)."]
[6.2563934326171875, 2.9502170085906982, "The Launch Initiative of the MoonLIGHT Satellite is NASA's Commercial Lunar Payload Services."]
[8.140552520751953, 10.291176795959473, "The Spectral Band of the Spectral Block Focal Plane Component is 758 \u2013 768 nm."]
[6.025618553161621, 2.6973814964294434, "The CEO of the Lacuna Space Satellite Company is Rob Spurrett."]
[3.172666549682617, 5.288896560668945, "The Capacity of the Solid-State Recorder Data Storage is 58.9 GB."]
[5.014084339141846, 1.9215561151504517, "The Probability Value of the Contamination Probability Mission Requirement is Smaller than 10\u20132."]
[10.649195671081543, 9.234806060791016, "The Image Center Coordinates of the CaSSIS Instrument is 28.79\u00baS/193.84\u00baE."]
[1.8960850238800049, 3.852245807647705, "The Solar Cells Type of the Solar Array Power Subsystem is High-efficiency dual-junction gallium-arsenide (GaAs)."]
[9.424497604370117, 7.823945999145508, "The Status of the LND Lunar Lander Neutrons and Dosimetry is Turned on for testing."]
[8.904960632324219, 10.38122844696045, "The Detector Array of the LWIR Camera Camera is HgCdTe detector array of 128 x 128 pixels."]
[11.607463836669922, -1.258043646812439, "The Mass of the Corvus-BC 2 Satellite is 10 kg."]
[11.622273445129395, -1.266437292098999, "The Mass of the UniSat-5 Satellite is 28 kg."]
[10.053740501403809, -0.7706732153892517, "The Telescope Diameter of the CE-SAT-1 Microsatellite is 40 cm."]
[7.876611232757568, 4.303045749664307, "The Image Capture Period of the DEIMOS-2 Satellite is 12 hours."]
[7.158580303192139, 4.392234802246094, "The Applications of the Landsat TM Satellite is Global change research, agriculture, forestry, geology, resources management, geography, water quality, and oceanography."]
[4.278680324554443, 5.735171318054199, "The RF Communications of the Kanopus-V Satellite is X-band (8.2 GHz) downlink of payload data, data rate of 300 Mbit/s, onboard data storage of 24 GB."]
[9.640095710754395, 1.6673039197921753, "The Daily Reset of the Dellingr Satellite is Part of daily operations."]
[4.027661323547363, 4.781090259552002, "The Redundancy of the OBC On-Board Computer is Each board is available twice for redundancy reasons."]
[6.717607021331787, 8.769344329833984, "The Length of the Instrument Instrument is 204 mm."]
[8.5405855178833, 10.794914245605469, "The Pixel Size of the Kodak KAI-11002 CCD CCD is 9 \u00b5m x 9 \u00b5m."]
[7.083852767944336, 2.9233925342559814, "The URL of the Whale Ecology Observation Satellite Satellite is http://www2.nict.go.jp/mt/b150/SJR/English/eng12-1/smallsatelliteweose.pdf."]
[5.688817501068115, 9.502341270446777, "The Mass of the SEIS Instrument Seismometer is 3 kg."]
[6.404933929443359, 4.405760288238525, "The Ground Architecture of the SENSE Satellite is SMC/SD."]
[6.248289585113525, 3.1458442211151123, "The Developer of the JPSS-1 Satellite is NASA."]
[5.435110092163086, 6.016429901123047, "The Antenna Type of the OPAL Satellite is 1/4 wavelength monopole."]
[8.961587905883789, 9.919944763183594, "The Components of the PMC Camera Set is Camera mainframe, camera management & control unit, DC/DC converter, baffle."]
[4.873083114624023, 1.7040506601333618, "The Constellation Size of the Aurora Satellite is Six-satellite."]
[6.249920845031738, 5.650564193725586, "The SAR Data Acquisition of the X-UGS UGS is Lack of capability to acquire directly SAR data."]
[1.129510521888733, 3.894993782043457, "The Battery of the XI-IV Picosatellite is Manganese type lithium-ion battery."]
[6.525124549865723, 8.303380966186523, "The Purpose of the CZCS Multichannel Scanning Radiometer is Ocean colour measurements."]
[4.015295028686523, 5.683690547943115, "The Downlink Data Rate of the ERBS Satellite is 128 kbit/s."]
[6.008718490600586, 0.5255757570266724, "The Operations Date of the MCubed-2 CubeSat is April 22, 2014."]
[11.21045970916748, 2.6099469661712646, "The Altitude Above Ground of the Lunar Landing Vehicle Vehicle is 100 m."]
[5.901501655578613, 5.409372806549072, "The Control Interface of the Yaesu G-5500 rotators Rotators is Yaesu GS-232."]
[4.403441905975342, 7.763531684875488, "The Center Frequency of the Channel 8 Sensor is 52.80 GHz."]
[5.859789848327637, 8.123557090759277, "The Frequency (GHz) of the ICI-1 Radiometer is 183.31\u00b18.4."]
[10.704523086547852, 10.225570678710938, "The Operating temperature range of the PHA Detector is -30 to +50\u00baC."]
[6.098595142364502, 8.309755325317383, "The Size of the Millimeterwave receiver radiometer is ~ 1.6 mm."]
[7.321105003356934, -0.728130042552948, "The Spatial Matchup Window of the CYGNSS Satellite is 25 km."]
[5.429773807525635, 2.390986442565918, "The Geographic Site Sizes of the PUTC Program is Vary from 100 km2 up to 3500 km2."]
[1.20321524143219, 4.300469875335693, "The Battery Storage of the EPS Electrical Power Subsystem is Capable of sustaining subsystems during operating loads and orbit eclipses."]
[7.433964252471924, 1.0843348503112793, "The Launch Date of the Exoplanet mission Satellite is Unknown."]
[5.665434837341309, 5.486074924468994, "The Model of the GPS Receiver Payload Module is SGR-10."]
[6.3126349449157715, 4.145849227905273, "The Earth Observation Constellation Type of the Spacety Company is Microwave-based (Synthetic Aperture Radar) satellite."]
[4.240171432495117, 5.449770450592041, "The Downlink Acquire Time of the IXPE Satellite is 60 s."]
[7.675503253936768, 1.6234898567199707, "The Conference Date of the SMEX-LITE Satellite is Sept. 16-19, 1996."]
[9.021712303161621, 3.8429746627807617, "The Formation Size of the MMS Satellite Formation is 10 km."]
[9.99770450592041, -0.6075801253318787, "The Mean Altitude of the Vstar Gravity-field Measurement Microsatellite is ~100 km."]
[9.844206809997559, 1.180965542793274, "The Operation Time of the MEPSI Satellite is Up to 24 hours."]
[10.451147079467773, -1.008162260055542, "The Mass of the SOHLA-1 Microsatellite is 50 kg."]
[4.533496856689453, 4.096301555633545, "The Communication Bus of the SMEX Satellite Program is MIL-STD-1553 data bus."]
[9.799674987792969, 1.6586462259292603, "The Observation Duration of the SPARCS Satellite is 1 to 3 stellar rotations."]
[5.788910388946533, 1.607660174369812, "The Mission Purpose of the GomX-1 Nano-satellite is Demonstrate Improved Situational Awareness for Air Traffic Control."]
[4.403896808624268, 4.328220844268799, "The Developer of the Electronic Unit Component is Shandong Institute of Aerospace Engineering."]
[7.5707807540893555, 9.965030670166016, "The Sensor Mode of the HyperScout\u00ae Imaging System is Pushbroom."]
[11.628168106079102, -1.0051947832107544, "The Propulsion System Fuel Capacity of the EAGLE ESPAStar Satellite is Up to 310 kg."]
[6.4602789878845215, 3.3204944133758545, "The Purpose of the Sentinel-6 Satellite is Ensure the \u2018continuity of service' of the Jason missions."]
[8.943721771240234, 9.275702476501465, "The Pixel Scale of the Telescope Optical Instrument is 15 \u00b5m."]
[7.7786946296691895, 6.565488815307617, "The Source of the Arrokoth Celestial Body is AAAS."]
[5.920757293701172, 2.840038776397705, "The Prime Contractor of the Euclid Space Telescope is Thales Alenia Space."]
[10.349349021911621, 4.819531440734863, "The Thrusters of the Satellite Bus Spacecraft Component is 12 hydrazine thrusters."]
[4.995137691497803, 6.164780616760254, "The Downlink Frequency Band of the GPS-DASS Payload is 2226 MHz (S-band)."]
[5.3383307456970215, 2.7074127197265625, "The Designing Institution of the WeissSat 1 CubeSat is Weiss School."]
[8.441970825195312, 0.24629347026348114, "The Crew Return Time to Earth of the Proving Ground Space is Matter of days."]
[5.0825958251953125, 4.0880022048950195, "The Function of the SCL Spacecraft Command Language is Enable event-driven processing and low-level autonomy."]
[2.2504842281341553, 4.422778129577637, "The Dimensions of the PowerCell Hardware is ~21 x 29 x 8 cm."]
[1.7789746522903442, 4.278562068939209, "The Solar Array Output of the EPS Electrical Power Subsystem is 1418 W (EOL)."]
[4.735053539276123, 0.9200572967529297, "The Satellite Cost of the Astrocast Satellite Manufacturer is Half a million dollars."]
[9.541914939880371, 0.5673595070838928, "The On-Orbit Spare Lifetime of the GOES-R Satellite is 5 years."]
[10.159627914428711, 8.367791175842285, "The Purpose of the TESIS Telescope-spectrometer is 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."]
[7.135621070861816, 2.850708246231079, "The Validation Facilities of the SWOT Satellite is Efficient."]
[4.325687408447266, 4.308096408843994, "The Function of the PMC Payload Module Computer is Controls all PLM equipment and instruments."]
[5.395467281341553, 4.283355712890625, "The Interfaces of the HMA Project is Catalog Service, Ordering Service, Programming Service, Mission Planning Service, Online Data Access Services."]
[8.188175201416016, 9.009482383728027, "The Signal-to-Noise Ratio of the NISP Photometer Instrument is At least 5."]
[7.890854358673096, 8.531105995178223, "The Radiometer of the OLS Imaging Sensor is VIS/IR."]
[3.43084716796875, 5.347395896911621, "The Data Storage Capacity of the Data Transmission Subsystem Satellite Subsystem is 128 Gbit."]
[6.897100925445557, 3.30169939994812, "The Mission Status of the EXPORTS Satellite Mission is Operational (nominal)."]
[6.414890289306641, 2.5298404693603516, "The Leader of the GRNS Team is David Lawrence."]
[11.701986312866211, 5.09771728515625, "The Luminosity of the Sw J1644+57 Supermassive Black Hole is Temporarily boosted."]
[10.264631271362305, 2.998746871948242, "The Altitude of the Suomi-NPP Satellite is 824 km."]
[11.617579460144043, 4.366369247436523, "The Distance from Earth of the Kepler-442b Exoplanet is Around 1,200 light years."]
[9.730137825012207, -0.7061710953712463, "The Complex Investigation of the Chibis-M Microsatellite Satellite is Unknown."]
[7.856040954589844, -0.10989437997341156, "The Launch Date of the Nauka Module is No earlier than 15 July."]
[5.014967918395996, 4.528247833251953, "The Ordering of the CSK GS Ground Segment is Allow S-IM to submit production requests towards the FM when receiving confirmation that the acquisition is planned."]
[11.666949272155762, -0.6481682658195496, "The Solar Array Capacity of the MERLIN Satellite is Unknown."]
[8.012466430664062, 1.107125997543335, "The Image Capture Date of the MERIS Satellite is April 2, 2012."]
[6.817763328552246, 5.486049652099609, "The Workshop Date of the Soil Moisture Active and Passive (SMAP) Mission Satellite Mission is Sept. 22-23, 2008."]
[6.1619648933410645, 2.1158909797668457, "The Conference Presentation Date of the TacSat-4 Satellite is Aug. 10-15, 2013."]
[4.186598300933838, 5.093770503997803, "The Presentation Date of the Scalable Payload Downlink Chain Data Communication System is June 11-13, 2009."]
[6.308239936828613, 1.6196386814117432, "The Update Date of the Jason-3 Satellite is Feb. 11, 2016."]
[9.435994148254395, 6.1881937980651855, "The Algorithm Selection Criteria of the Attitude Determination Quaternion Filter Experiment is Maximum trace of the associated information rate matrix."]
[7.370896339416504, 10.043198585510254, "The Resolution of the Aurora Sensor Hyperspectral Sensor is Approximately 30 metres per pixel."]
[7.660436630249023, 0.5881419777870178, "The Launch Date of the Psyche spacecraft Spacecraft is Next year."]
[3.993837356567383, 5.622120380401611, "The Downlink Chains Data Rate of the ResourceSat-2 Satellite is 105 Mbit/s."]
[6.395681381225586, 1.584074854850769, "The Launch Services Contract Date of the Jason-3 Satellite is July 16, 2012."]
[8.08856201171875, 9.412055969238281, "The Number of Turrets of the Mechanical Turrets Mounting is 3 for each spectral range."]
[5.035697937011719, -2.3772165775299072, "The Affiliation of the Nico Fleurink Engineer is Unknown."]
[11.0546236038208, 7.1478753089904785, "The Modulation Factor of the HXCP Hard X-ray Polarimeter is 47.8%."]
[4.372860908508301, 6.426798343658447, "The Radiation Pattern of the Ka-band payload Communication System is Modified to distribute higher power at angles \u00b1 50\u00ba from boresight."]
[6.018628120422363, 9.631823539733887, "The Mass of the Instrument Satellite Instrument is 202 kg with the NG reflector and 275 kg with the HC reflector."]
[10.872759819030762, 3.390754222869873, "The Distance from the Sun of the New Horizons Spacecraft is Almost 5 billion miles (7.5 billion kilometers)."]
[9.936326026916504, -0.701399028301239, "The Dimensions of the Microsatellite Satellite is 540 mm (height), 370 mm (full diameter)."]
[6.331779956817627, 4.841486930847168, "The Map Projection of the L1C Products Satellite Data is User Selectable."]
[10.22403335571289, 1.0351295471191406, "The LTDN of the Polar Scout 6U CubeSat Satellite is 10:30 hours."]
[9.327289581298828, 7.702672004699707, "The Outer Shell Temperature of the Dewar Component is ~254.5 K."]
[8.19179916381836, 8.480241775512695, "The Design of the Interferometer Device is Birefringent gratings, Wollaston prisms, and LSI spacers to create the grating lateral shearing interferometer."]
[10.017120361328125, 5.051792144775391, "The Redundancy of the Thrusters Propulsion Device is 1 THR loss allowed."]
[10.479351997375488, -1.1621778011322021, "The Mass of the HORYU-4 Nanosatellite is 10 kg."]
[7.323894500732422, 9.614700317382812, "The IFOV of the S-192 optomechanical scanner Scanner is 79 m."]
[7.325516223907471, 10.126504898071289, "The Authors of the HyperScout Hyperspectral Imaging System is 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."]
[4.559674263000488, 3.393000841140747, "The Responsibilities of the SatsimIF Application is 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."]
[4.203240394592285, 4.552585124969482, "The Purpose of the Interposer Board Interface is Provide the interface between the 51-pin connector, the second connector, and the payload."]
[10.266586303710938, 5.654850482940674, "The Voltage of the Electrodynamic Tether Propulsion and Power Generation Device is Up to several hundred volts per km."]
[7.7674336433410645, -0.41226470470428467, "The Timeline of Events of the SpaceX Falcon-9 Rocket is 93 milliseconds from the first sign of anomalous data to the loss of the second stage."]
[6.0128374099731445, 3.9827234745025635, "The Location of the PACS Instrument Control Center is MPE (Max Planck Institute for Extraterrestrial Physics), Garching, Germany."]
[11.182266235351562, 9.342403411865234, "The FOV of the Earth Radiation Budget Experiment (ERBE) Instrument is \u00b178\u00ba cross-track, 360\u00ba azimuth."]
[9.257102966308594, 7.297092914581299, "The Sensor Operating Pressure of the FIPEX Instrument is Down to 10-10 mbar."]
[7.935934543609619, 2.765293836593628, "The Collision Date of the Small Near-Earth Objects Space Debris is 21 November 2002."]
[5.713396072387695, 7.131519794464111, "The Frequency of the RA-1 Radar Altimeter is 13.8 GHz."]
[9.878355026245117, 5.24423360824585, "The RCS Thrusters Fuel of the AOCS Attitude and Orbit Control System is 12 years."]
[9.498284339904785, 7.704501152038574, "The Operating Temperature of the Telescope Optical Instrument is -50\u00baC to ~ 100\u00baC."]
[6.617066860198975, 10.660541534423828, "The SNR of the Band 3 Spectral Band is 400."]
[9.347607612609863, 10.344342231750488, "The FMC (Forward Motion Compensation) system of the Metric Camera Camera is Not added."]
[7.478323936462402, 8.885417938232422, "The Along-Track Resolution of the OMI Spectrograph is 13 km x 48 km to 13 km x 12 km."]
[5.527524948120117, 7.509487152099609, "The Peak Transmit Power of the KaRIn Instrument is 1500 W."]
[5.358959674835205, 5.636203289031982, "The Channels of the GPS receiver Receiver is 24 channels."]
[7.122557640075684, 1.5463005304336548, "The Mystery Solve Date of the Cluster Satellite Constellation is July 14, 2015."]
[5.447964191436768, 1.7041288614273071, "The Purpose of the Automated Transfer Vehicle (ATV) Spacecraft is Provided reliable cargo deliveries to the Space Station."]
[4.525737285614014, 3.997257709503174, "The Component Detection of the SPA System System is Automatic."]
[7.752570152282715, 3.242429256439209, "The Tests of the Characterization Process Satellite Debris Analysis is Repeatability and reproducibility tests."]
[9.549970626831055, 0.4166256785392761, "The Design Life of the RADARSAT-1 Satellite is 5 years."]
[6.854902267456055, 1.271604061126709, "The Conference Date of the Telemetry Monitoring and Analysis System System is April 25-30, 2010."]
[5.396066665649414, 1.3455199003219604, "The Services of the NanoRacks LLC Company is On-board and on-ground services to the general 'small payload' research community of the International Space Station (ISS)."]
[7.9170355796813965, 9.67807674407959, "The Spectral Resolution of the Instrument Spectral Imager is 2.5 cm -1."]
[9.159790992736816, 6.283015251159668, "The Quantity of the Ithaco Inc. 60 Am2 electromagnetic torque rods Torque Rods is Three."]
[10.458972930908203, 4.973055362701416, "The Power of the PPS-1350-G Hall-effect thruster is Nominal input power (in Watt)."]
[9.604032516479492, 5.941638946533203, "The Stability of the ADCS Attitude Determination and Control Subsystem is \u2264 5 x10-4 \u00ba/s."]
[7.340158939361572, 3.3047616481781006, "The Sensor Complement of the BRITE-Austria Satellite is Unknown."]
[9.409300804138184, 1.7071584463119507, "The Frequency of the Formation Flying Maintenance Maneuver is Once per week or longer."]
[3.8116044998168945, 5.884756088256836, "The Payload Data Downlink Rate of the MERLIN Satellite is 180 to 310 Mbit/s."]
[9.277791023254395, 0.8051942586898804, "The In Orbit Operations Duration of the RapidEye Constellation Satellite Constellation is 10 years."]
[9.328179359436035, 10.02613639831543, "The Size of the APD Avalanche Photodiode is Very small."]
[7.686950206756592, 4.015054702758789, "The Payloads of the Aditya-L1 Satellite is Particle payloads, magnetometer payload."]
[4.875336647033691, 6.1975860595703125, "The Chirp Bandwidths of the Satellite Satellite is 320, 80, 20 MHz (Ku-band), 160 MHz (S-band)."]
[3.2496259212493896, 4.7722344398498535, "The SRAM Capacity of the RAD750 SBC Single Board Computer is 36 MB."]
[7.760385513305664, 7.894848823547363, "The Orientation of the \u00b5SCIA Monitoring Instrument is Nadir-oriented."]
[6.8361029624938965, 1.9609951972961426, "The Launch Date of the Global Precipitation Measurement (GPM) Mission Satellite Mission is Unknown."]
[4.86981201171875, 1.9754550457000732, "The Number of Satellites of the Iridium Communications Inc. Company is 5."]
[10.863774299621582, 5.732516288757324, "The Technique Developer of the Solar Flare Solar Event is Alina-Catalina Donea."]
[11.742521286010742, -1.1359221935272217, "The Mass of the Satellite Spacecraft is 100-400 kg."]
[11.74611759185791, 1.1031527519226074, "The Lunar Orbit Altitude of the Chang'e-3 Lunar Lander is 100 km."]
[8.440961837768555, 4.655863285064697, "The Measurement Regions of the Cluster Satellite Mission is Solar wind and bow shock, magnetopause, polar cusps, magnetotail, auroral zone."]
[7.427671432495117, 7.333487033843994, "The Award Date of the Ozone Monitoring Instrument Instrument is 29 April 2019."]
[4.021442890167236, 5.254825115203857, "The Bandwidth of the ODTML Data Collection System is > 50 kbit per node per day."]
[5.793329238891602, 3.4899685382843018, "The Services of the GMES Global Monitoring for Environment and Security is 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."]
[4.920629501342773, 9.191776275634766, "The Instrument Type of the SEIS Seismic Experiment for Interior Structure is Seismic."]
[8.423798561096191, 6.535929203033447, "The Mounting of the GRNS Instrument is 6-foot (2-meter) boom."]
[8.871771812438965, 7.303035736083984, "The URL of the Omni-Directional Differential Sun Sensor Sensor is http://citeseerx.ist.psu.edu/viewdoc/download?doi=10.1.1.34.9657&rep=rep1&type=pdf."]
[1.5431920289993286, 4.928099155426025, "The Power Bus Voltage of the PCDU Power Control and Distribution Unit is 28 V."]
[9.521546363830566, 0.414113312959671, "The Design Life of the Aqua Satellite is 6 years."]
[10.289985656738281, 3.000115394592285, "The Altitude of the Himawari-8 Satellite is ~35,800 km."]
[11.188815116882324, 6.640196323394775, "The URL of the SphinX Solar Photometer in X-rays is http://www.cbk.pan.wroc.pl/body/publikacje/2008/JC_JS_Sphinx_2008_11_06.ppt."]
[8.710799217224121, 2.618744134902954, "The Parking Orbit Altitude of the ARTEMIS Spacecraft is 31,000 km."]
[8.612000465393066, 7.365356922149658, "The Function of the SES Instrument is Demonstrate that the instrument can survive the extreme thermal gradients and mechanical strains."]
[7.9357781410217285, 7.321939468383789, "The Operational Cadence of the Instrument Satellite Instrument is Stare nadir for 30-40 minutes."]
[11.807821273803711, 4.469412803649902, "The Number of Stars of the Upper Centaurus Lupus Star Cluster is 134."]
[10.021088600158691, 5.313728332519531, "The Pressure Change of the Airtight Vessel Satellite Component is 1.6%."]
[9.61844539642334, 6.061224460601807, "The Magnetometer of the ADCS Attitude Determination and Control Subsystem is 1.0 V/gauss, \u00b11.9 gauss."]
[5.961127281188965, 2.6281490325927734, "The Funding Source of the ELFIN Satellite is NASA/NSF."]
[6.528812885284424, 4.199156284332275, "The Project Manager of the CO2M Satellite is Valerie Fernandez."]
[5.050714015960693, 4.299381732940674, "The Functionalities of the UIS System is Reception, management of product order, generating image collection proposal, image collection request, submitting product generation request."]
[8.44275951385498, 6.541049003601074, "The Load Range of Shaker Tests of the Boom Structure is 0.048 to 0.00055 kg."]
[7.062359809875488, 2.6757044792175293, "The Concept of the TransHab Space Habitat is URL: http://spaceflight.nasa.gov/history/station/transhab/."]
[5.981905937194824, 6.402743816375732, "The Average Sigma Naught of the SAR Instrument is -7.5 dB."]
[6.85623836517334, 0.33142492175102234, "The Launch Date of the IRS-P6 Satellite is 17 Oct 2003."]
[9.494998931884766, 0.9704959988594055, "The Mission Duration of the D-Sat Satellite is More than three months."]
[4.768423557281494, 0.795650064945221, "The Consideration of the Eutelsat Communications Company is $165 million."]
[4.92687463760376, 1.9780601263046265, "The Quantity of the GEMSat/ELaNa-2 Satellite is 12 CubeSats/nanosatellites."]
[5.542270183563232, 3.7012972831726074, "The Mission Objectives of the M3MSat Satellite is The primary mission objective is to provide maritime surveillance for both commercial customers, and for the Canadian government, by detecting AIS messages from space."]
[5.0500593185424805, 6.622542858123779, "The Gain of the Antenna for Navigation Antenna is Greater than \u2013 4 dBic for elevations > 5\u00b0."]
[7.216062068939209, 7.837525367736816, "The Channels of the ALTIUS Instrument Satellite Instrument is Three channels."]
[8.029921531677246, 8.875929832458496, "The Stability Requirements of the Individual Spectrometers Instrument is 15 pm."]
[5.642873764038086, 3.7910873889923096, "The User Mission Operations Center Simulator of the LCRD Satellite is UMS."]
[8.164444923400879, 7.029702663421631, "The Power On Command of the SPAN Sensors Sensor is Via command from the SPP DPU to the SWEM."]
[5.737807273864746, 3.562272787094116, "The Beacon Packet Content of the StenSat Satellite is The most recent science packet."]
[7.937188148498535, 1.9594992399215698, "The Data Relay Services Start of the ExoMars Trace Gas Orbiter Orbiter is 2023."]
[8.393579483032227, 4.509690284729004, "The Principal Investigator of the Cluster S/C Satellite is A. Balogh."]
[10.647425651550293, 9.22083854675293, "The Image Orientation of the CaSSIS Instrument is North is up."]
[7.7286529541015625, 9.509491920471191, "The Temporal Resolution of the Visible Spectral Band Spectral Band is 30 minutes (frame time)."]
[7.322291374206543, 4.806673526763916, "The Radiation Exposure of the O/OREOS Satellite is Unknown."]
[5.288287162780762, 3.0765857696533203, "The Developer of the NorSat-3 Satellite is FFI in collaboration with Kongsberg Seatex."]
[7.254014492034912, 5.268947124481201, "The Mid-tropospheric CO2 Measurements per Day of the AIRS Satellite is About 15,000."]
[11.223788261413574, 3.515498638153076, "The Magnetic Field Behavior of the Comet 67P Comet is Became stronger and more turbulent when the forming bow shock washed over Rosetta."]
[6.621323108673096, 3.7624495029449463, "The Geographic Region of Interest of the ZACUBE-2 Satellite is Southern African coastal regions."]
[4.851221561431885, 6.051527500152588, "The Signal Frequency of the Clementine Satellite is 2.273 GHz."]
[9.527814865112305, 7.353161334991455, "The Pavement Temperature of the ECOSTRESS Instrument is Exceeded 122 F (50 C)."]
[7.966786861419678, 1.5387547016143799, "The Senior Review Date of the Heliophysics Operating Missions Satellite is June 11, 2015."]
[7.547882556915283, 1.7449040412902832, "The Mission of the MMS Satellite is Magnetospheric Multiscale Mission."]
[5.504861354827881, 2.0589725971221924, "The Number of Orbits of the Envisat Satellite is 10,000."]
[8.697994232177734, 6.497865676879883, "The Direction of the Spool Deployment System is Counterclockwise."]
[7.197840213775635, 6.875758171081543, "The Launch Date of the VIIRS Sensor is Oct. 28, 2011."]
[6.596325397491455, 0.5250921249389648, "The Launch Date of the Intelsat 20 Communication Satellite is August 2, 2012."]
[5.068109512329102, 7.129507541656494, "The Pixel Size (km x km) of the Antenna Reflector is 11."]
[4.492952823638916, 4.157766342163086, "The Interface Module of the Non-SPA COTS components Components is ASIM (Appliqu\u00e9 Specific Interface Module)."]
[5.494503498077393, 3.128164768218994, "The Hardware Source of the TBIRD Satellite is Existing commercial, telecommunications hardware products."]
[1.3621097803115845, 4.133021831512451, "The Battery Discharge of the Integral Satellite is The first estimates of the charge remaining before blackout and the loss of the satellite was just three hours."]
[7.340688228607178, 0.9439051151275635, "The Event Date of the ALOS Data Utilization is Dec. 5-7, 2006."]
[9.391862869262695, 9.324563980102539, "The Field of View of the Optical Head Optical Device is 94\u00ba x 81\u00ba (1-hole mask)."]
[6.8038859367370605, 2.002980947494507, "The Public Data Release Date of the Global Precipitation Measurement (GPM) Mission Satellite Mission is Unknown."]
[8.19623851776123, 5.169949054718018, "The Orbit Determination Accuracy of the GF-3 Satellite Satellite is 4 cm."]
[1.4898970127105713, 4.937262535095215, "The Voltage of the MTM main power bus Power Bus is 28 V."]
[8.43049430847168, 8.755389213562012, "The Wavelength Bandpass of the UVS Instrument Spectrometer Telescope is 1:3.8 (cha. 1); 2:3.7 (cha. 2)."]
[6.67099142074585, 0.9795294404029846, "The Launch Date of the SARah-1 Earth Observation Satellite is 13 June 2022."]
[11.774527549743652, 4.7708916664123535, "The Black Hole Mass of the OJ 287 galaxy Galaxy is Over 18 billion times the mass of our Sun."]
[6.975451946258545, 6.4552693367004395, "The Developer of the PLEGPAY Instrument is Thales Alenia Space."]
[9.574414253234863, 5.087676048278809, "The Spin of the ICU Container is 1 to 10 rpm."]
[10.514647483825684, -0.9552116394042969, "The Mass of the Hodoyoshi-4 Microsatellite is 65 kg."]
[9.719483375549316, 6.92738151550293, "The Internal Average Temperature of the SVM Service Module is 15\u00b0C."]
[9.226200103759766, 10.859004974365234, "The Distance Range of the MCAM-2 Camera is 920 km \u2013 6099 km."]
[11.503713607788086, 6.328949451446533, "The URL of the XMM-Newton Satellite is http://sci.esa.int/xmm-newton/60950-from-gamma-rays-to-x-rays-new-method-pinpoints-previously-unnoticed-pulsar-emission/."]
[7.822037696838379, 3.4789271354675293, "The Roll Maneuvers of the RapidEye Satellite Constellation is \u00b120\u00ba."]
[4.9697370529174805, 5.030434608459473, "The Communication Links of the SSR Satellite Subsystem is UART link to OIM module, high speed differential LVDS links to XBT subsystem and IRIS and PPU payloads."]
[2.040450096130371, 3.831139087677002, "The Deployment System Material of the LFSA Photovoltaic Solar Array System is Shape Memory Alloys (SMA)."]
[6.061883449554443, 3.2316884994506836, "The Prime Contractor for B series of the MetOp-SG Satellite Program is Airbus Defence and Space of Germany."]
[5.17073392868042, 3.1534483432769775, "The Mission Purpose of the SPORT CubeSat is Understand the preconditions leading to equatorial plasma bubbles."]
[8.4929838180542, 1.465467929840088, "The Hibernation Duration of the Rosetta Spacecraft is 31 months."]
[4.793293476104736, 1.8903815746307373, "The Number of Earth Stations of the LAGEOS Satellite is 14."]
[6.23723840713501, 3.8864855766296387, "The Operational Countries of the JJ-FAST Forest Early Warning System is 77."]
[7.4169440269470215, 9.58645248413086, "The Beam width of the VIS (red) Band is 3.4 \u00b5rad."]
[6.9715166091918945, 4.269371509552002, "The Video Camera Assembly of the LAPAN-A2 Satellite is COTS (Commercial-of-the-Shelf) RGB medium format video camera."]
[7.811117172241211, 6.315714359283447, "The Radiometric Accuracy of the Calibration Techniques Satellite Instrument Calibration is Specified."]
[7.120236396789551, 4.373321056365967, "The Instrument Type of the SkySat Constellation Satellite Constellation is High resolution optical imagers."]
[11.505803108215332, 2.162057399749756, "The URL of the Hayabusa 2 Project Mission is https://web.archive.org/web/20120222130748/http://b612.jspec.jaxa.jp/hayabusa2/e/hayabusa2_e.html."]
[7.36908483505249, 10.083128929138184, "The Spectral Bands of the HyperScout Hyperspectral Imager is 45 visible and near-infrared."]
[9.573246955871582, 3.7281415462493896, "The Water Ice Concentration Useful Quantity of the Lunar Flashlight Spacecraft is 0.5 wt%."]
[9.283935546875, 4.216057777404785, "The Printed Circuit Board Area of the Sprite Tiny Spacecraft is 3.5 by 3.5 cm."]
[6.084588527679443, 4.412144660949707, "The Components of the ERA Robotic Arm is Two end effectors, two wrists, two limbs, one elbow joint, electronics, and cameras."]
[6.967234134674072, 1.4168014526367188, "The Delegated Regulation Date of the GMES-S Satellite is December 2013."]
[7.107088565826416, 9.190101623535156, "The Resolution of the Interferometric Wide Swath mode (IWS) Operational Mode is 5 m x 20 m."]
[5.2575483322143555, 1.2699187994003296, "The Projected Payload Capacity of the Terran R Launch Vehicle is In the same class as SpaceX\u2019s Falcon 9."]
[4.35244083404541, 6.413345813751221, "The G/T of the System Communication System is Unknown."]
[8.093859672546387, 2.6621599197387695, "The Fuel Supply of the TSX (TerraSAR-X) Satellite is Until at least 2026."]
[8.490606307983398, 9.615681648254395, "The Pixel Offset of the Band-64 Satellite Instrument is 34 pixels out of 256 pixels."]
[7.610445499420166, 1.2806179523468018, "The Launch Date of the JPL-Built Earth Science Experiment Earth Science Experiment is Nov. 2, 2011."]
[8.508462905883789, 10.502803802490234, "The Input and Output of the CCD (Charge-Coupled Device) Imaging Device is LVDS (Low Voltage Differential Signaling)."]
[9.635025024414062, -0.5733156204223633, "The Observation Purpose of the TARANIS Microsatellite is To observe luminous, radiative and electromagnetic phenomena occurring at altitudes of 20 to 100 km over thunderstorms."]
[7.733309745788574, 10.817595481872559, "The Data Inputs of the Front End Electronics Electronics is 5."]
[5.6329827308654785, 9.14704704284668, "The Power Efficiency of the VGT-P Instrument is Required to be very efficient in its power use."]
[8.636401176452637, 5.270877361297607, "The Pointing Knowledge of the DSP satellites Satellite is <0.5\u00ba."]
[7.082212448120117, -0.02415202371776104, "The End of Life Date of the FORUM Satellite is December 2031."]
[7.617940425872803, 1.60041081905365, "The Mission Start Date of the SMOS Satellite is Unknown."]
[7.299600601196289, 0.34520477056503296, "The Launch Date of the FORUM Satellite is July 2027."]
[9.748730659484863, -0.5672628879547119, "The Revisit Time of the BlackSky's Satellites Microsatellites is Every 30 minutes."]
[5.862191200256348, 6.750277519226074, "The Swath of the Radar Radar is > 1000 km."]
[6.138582706451416, 9.710925102233887, "The Mass of the COSAC Evolved Gas Analyzer is 4.9 kg."]
[4.983689785003662, 3.3134756088256836, "The Conference Date of the CubeSat Laser Communication Crosslink Pointing Demonstration Satellite Communication System is August 3-8, 2019."]
[7.1997575759887695, 5.60017204284668, "The Systems of the WIND Satellite is Equipped with heavy shielding and double-redundant systems."]
[8.914741516113281, 7.8999247550964355, "The Detection Energy of the CZTI Instrument is Greater than about 60 keV."]
[9.000307083129883, 10.643564224243164, "The Spatial Resolution of the WiFS camera Camera is 188 m."]
[8.720805168151855, 6.806814193725586, "The Orientation of the Magnetic Field Sensor Sensor is Four different orientations."]
[7.015505313873291, 0.32085198163986206, "The Launch Date of the SPOT-1 Satellite is February 1986."]
[13.031445503234863, 4.122485160827637, "The Number of Extragalactic Sources of the Gaia EDR3 Satellite Data is More than 1.6 million."]
[9.888511657714844, 8.962961196899414, "The Telescope Mirror Diameter of the Euclid Spacecraft is 1.2 m."]
[9.224271774291992, 1.971581220626831, "The Closest Approach Time of the BepiColombo Spacecraft is 23:34:41 UTC."]
[9.812371253967285, 7.187848091125488, "The Cooling Method of the Chamber with a heat exchanger Air Ventilation System is Direct contact to the base plate of the payload compartment."]
[7.713659286499023, 4.207172393798828, "The Resolution of the TeLEOS-1 Satellite is Down to one-meter."]
[9.36632251739502, 2.5888671875, "The Deployment Date of the EURECA Satellite is Aug. 2, 1992."]
[3.1668906211853027, 5.2458176612854, "The Maximum Capacity of the DSU Data Storage Unit is Up to 8 Tbit at EOL."]
[7.848802089691162, 4.721173286437988, "The Red-IR/UV Ratio of the Tatiana-2 Satellite is Varies."]
[11.72056770324707, -1.1044288873672485, "The Mass of the Cabling/harness Satellite Subsystem is 0.1 kg."]
[3.516984224319458, 6.6230034828186035, "The Data Rate (max) of the TXS S-band Transmitter/Transceiver is 100 kbit/s."]
[9.043477058410645, 6.585290431976318, "The Power of the Rate gyro Sensor is 1.4 W."]
[5.370921611785889, 5.712158679962158, "The Frequency Tracking of the Phoenix GPS Receivers GPS Receiver is Single-frequency."]
[8.697446823120117, 5.332695960998535, "The Alignment of the Spacecraft Satellite is Nominally aligned with the instrument LoS."]
[9.826301574707031, -0.9978525638580322, "The Phase Angle of the JL-1-GF03D Microsatellite is 120\u00ba."]
[5.852810859680176, 1.8139334917068481, "The Launch Vehicle of the Meteosat-1 Satellite is Thor-Delta."]
[8.618583679199219, 5.743471622467041, "The Bulk Velocity of the Proton Component Measurement Range of the DSCOVR Satellite is 200 \u2013 1250 km/s."]
[9.231566429138184, 5.358400344848633, "The Platform of the BILSAT-1 Satellite is Three-axis controlled platform with agile maneuvering capability."]
[11.549215316772461, -1.3534808158874512, "The Mass of the Corvus-BC 1 Satellite is 10 kg."]
[7.736929416656494, 9.11440658569336, "The GSD of the Spectral Band D Spectrometer is 5."]
[11.774271965026855, 1.6536171436309814, "The Communication Loss Time of the Philae Lander is 09:58 GMT."]
[5.358034133911133, 9.311365127563477, "The Data Volume of the SEIS Instrument Seismometer is ~38 Mbit/day."]
[10.783865928649902, 7.328371524810791, "The Energy Range of the HEAO-1 A2 X-ray Detector is 3 to about 45 keV."]
[10.649619102478027, 9.222386360168457, "The Imaging Date of the CaSSIS Camera Imaging Device is 7 June 2021."]
[5.439844608306885, 0.3087591230869293, "The Wildfires of the British Columbia Province is More than 40 wildfires."]
[1.9039595127105713, 4.039788722991943, "The Size of the Solar Panels Power Source is 320 mm x 320 mm."]
[8.795604705810547, 10.730504035949707, "The Spectral Coverage of the WFC CCD Camera is 620-670 nm."]
[5.606313228607178, 3.7951059341430664, "The Location of the MCF Mission Control Facility is CSA in Saint-Hubert, Quebec."]
[3.7811636924743652, 6.6447296142578125, "The Convolutional Encoding of the X-band Transmitter Transmitter is \u00bd rate k=7."]
[8.831083297729492, 8.3148775100708, "The Detector Type of the X-ray Spectrometer Spectrometer is Microcalorimeter."]
[8.255133628845215, 5.450744152069092, "The Navigation Information Utilization Time of the Lander Spacecraft is Unknown."]
[4.878835201263428, 1.9921015501022339, "The Number of Satellites of the NLS-8 Nanosatellite Launch Services program is 3."]
[5.236262798309326, 4.50282621383667, "The Location of the Ground Segment Data Processing is Belgian user Support and Operation Centre (B.USOC) in Brussels, Belgium."]
[10.243850708007812, 7.569107532501221, "The Components of the COPV Pressure Vessel is Aluminum inner liner with a carbon over-wrap."]
[7.165327548980713, 8.791665077209473, "The Swath of the AVHRR/3 Instrument is 2900 km."]
[7.327105522155762, 2.4973278045654297, "The URL of Presentation of the RISESAT Satellite is http://digitalcommons.usu.edu/cgi/viewcontent.cgi?."]
[4.164373874664307, 5.263124942779541, "The Number of Sensors of the Experiment Layer Data Management System is Hundreds."]
[7.733896255493164, 3.239776134490967, "The Quantity of the Debris Satellite Components is More than 250 pieces."]
[11.41752815246582, 1.3572361469268799, "The Operation Status of the China's Moon Rover Rover is Awaken."]
[4.0438456535339355, 6.484029769897461, "The Excitation Frequency of the MCAc Mode is 0.005 Hz."]
[7.56393575668335, 6.553116321563721, "The Typical Value of the H2O Satellite Instrument is 3 x 10 8."]
[6.84083890914917, 1.3550939559936523, "The Imagery Capture Date of the WorldView-3 and GeoEye-1 Satellites is Northern California Firestorm."]
[6.323785305023193, 3.4797563552856445, "The Generation of the MetOp Satellite is Second."]
[6.00797176361084, 2.6697332859039307, "The Partners of the STPSat-1 Satellite is Northrop Grumman TASC, and Avidyne."]
[9.502298355102539, 3.9622344970703125, "The Form Factor of the Lunar Flashlight 6U CubeSat Satellite is 116.2 x 239.4 x 366 mm."]
[5.166470527648926, -0.08203043043613434, "The Initial Services in the United Kingdom of the Lightspeed Satellite Constellation is 2026."]
[7.5477142333984375, 3.055609941482544, "The Purpose of the Star Simulator Simulator is Improvement of the HILS environment."]
[8.31687068939209, 1.5208944082260132, "The Imaging Date of the STEREO-A Spacecraft is June 5, 2020."]
[8.599550247192383, 6.868715763092041, "The Field Change Detection Capability of the SQUID Magnetometer is 5 x 10-14 Gauss."]
[6.350959777832031, 3.237697124481201, "The Goal of the SERVIR Program is Supplement local facilities, technology, and skills with expanded satellite imagery and tools."]
[5.540411949157715, 4.210836887359619, "The Function of the Sentinel MCS Mission Control System is Monitoring and control of all spacecraft."]
[5.534025192260742, 3.369898796081543, "The Name of the VNIIFTRI Developer is VNIIFTRI (All-Russian Scientific Research Institute of Physical and Radio-Engineering Measurements)."]
[6.7799072265625, 1.7568681240081787, "The Launch Date of the EnviSat Satellite is Unknown."]
[6.291520595550537, 3.27268385887146, "The Owner of the SAOCOM constellation Satellite Constellation is CONAE (Comision Nacional de Actividades Espaciales)."]
[5.681456089019775, 2.3285558223724365, "The Acquisition Cost of the Maxar Technologies Company is $140 million."]
[9.513187408447266, 9.141305923461914, "The Aperture Diameter of the Telescope Optical Instrument is 30 cm."]
[5.003681659698486, 6.105924606323242, "The Frequency (MHz) of the GPS L5 Signal Carrier is 1176.45."]
[7.532925605773926, 0.7666025757789612, "The Installation Date of the NICER-SEXTANT Mission is June 13."]
[13.054315567016602, 4.098789215087891, "The Data Collection Capacity of the Gaia Satellite is 100 TB."]
[7.574294090270996, 1.2721980810165405, "The Science Mode Start Date of the Colorado Student Space Weather Experiment (CSSWE) Satellite is Oct. 4, 2012."]
[7.618691444396973, 7.3326263427734375, "The Data Coverage Area of the OCO-3 Instrument is 80 km2."]
[7.677669525146484, 3.694587469100952, "The Location of the Land Glacier Glacier is West Antarctica."]
[9.439895629882812, 0.4561253488063812, "The Design Life of the SORCE Satellite is 5 years."]
[3.6004083156585693, 6.229019641876221, "The Downlink Lock Time of the LLCD PAT Systems Communication System is Within seconds."]
[2.014537811279297, 7.849463939666748, "The Solar Wind Speed and Beta of the ACE Satellite is ~34% lower on average from 2009 through the day 79 of 2013."]
[10.641332626342773, 2.4622654914855957, "The Orbit Altitude of the LitianicaSAT-2 Nanosatellite is 505 km."]
[5.817318439483643, 8.155586242675781, "The Bandwidth (GHz) of the ICI-6 Radiometer is 4.8."]
[8.337664604187012, 9.991861343383789, "The Support Mode of the SLIM6 Imager is Strip Real-Time Imaging."]
[6.224659442901611, 4.748706817626953, "The Data of the ICEYE Satellite is SAR data."]
[5.9938063621521, 9.603986740112305, "The Payload Mass of the IMS-2 Instrument is 147 kg."]
[11.397889137268066, 4.5025410652160645, "The Carbon Temperature of the Sun's Lower Atmosphere Celestial Body is 32,000\u00baC."]
[9.49313735961914, 9.020626068115234, "The Focal Length of the NESSI Telescope is 893 mm."]
[7.653227806091309, 1.1572524309158325, "The Start Date of the ColAIS Experiment is Summer of 2010."]
[9.301605224609375, 6.1175217628479, "The Quantity of the Magnetotorquers AOCS Actuators is 3."]
[7.0087361335754395, 4.824102401733398, "The Campaign Location of the KORUS-OC Korea-United States Ocean Color Mission is East Sea (Sea of Japan), South Sea, and Yellow Sea."]
[10.252029418945312, 4.980535507202148, "The Hall Effect Propulsion of the Electric Propulsion Test Subsystem Satellite Subsystem is Isp = 1600 s \u00b1 160 s."]
[7.814525604248047, 2.0986597537994385, "The Parachute Size of the ExoMars 2020 Mission is Largest ever to fly on a Mars mission."]
[5.177862644195557, 5.97661018371582, "The Antenna Type of the Spacecraft Satellite is Steerable medium gain antenna."]
[6.631547927856445, 4.74464225769043, "The Imaging Frequency Band of the Sentinel-1A/B Satellite is C."]
[7.438016891479492, 1.5670629739761353, "The Test Completion Date of the ExoMars Analytical Laboratory Drawer Laboratory Drawer is Unknown."]
[8.216622352600098, 2.5105555057525635, "The Years in Orbit of the TerraSAR-X Satellite is 11 years."]
[5.400834560394287, 6.618623733520508, "The Number of Pulses per Angle Bin of the PR Phased Array System is 32."]
[6.107272624969482, 5.324917793273926, "The GPS Receiver of the BEESAT-4 CubeSat is Phoenix."]
[8.143186569213867, 8.452184677124023, "The Field-Widened Gains of the Spatial Heterodyne Spectroscopy (SHS) Interferometric Fourier transform technique is Typically 100."]
[9.506959915161133, 7.810774803161621, "The Energy Suppression of the IBEX-Lo sensor Sensor is External electrons below ~600 eV and the external ions below 10 keV."]
[6.960455417633057, 6.2158894538879395, "The Uncertainty of the Sea Surface Temperature (SST) Measurement is <0.3 K."]
[7.302280902862549, 2.6304798126220703, "The URL of the INTEGRAL Satellite is http://sci.esa.int/integral/57257-integral-x-rays-earths-aurora/."]
[9.405467987060547, 9.34951400756836, "The Hole Diameter of the Optical Head Optical Device is 0.2 mm."]
[6.601749897003174, 3.6183342933654785, "The Mission Type of the Tatiana-2 Satellite is EO."]
[5.07703971862793, 4.5347371101379395, "The Tradeoffs of the Ground-based Analysis Techniques Data Collection is Between spatial and temporal resolution."]
[7.868429183959961, 1.910057783126831, "The Status of the ExoMars Mission is Performing flawlessly."]
[9.02212142944336, 7.608027935028076, "The FOV of the FSS Fine Sun Sensor is 128\u00ba x 128\u00ba."]
[0.9548503756523132, 4.17372989654541, "The Energy Storage of the Lithium ion battery Battery is Two to four times more than proven technology."]
[6.132218837738037, 3.4230408668518066, "The Company Headquarters of the SAR Satellites Satellite is San Francisco, California."]
[11.644463539123535, -1.2119247913360596, "The Mass of the Mass Satellite is 241 kg."]
[10.248770713806152, 2.964949131011963, "The Orbit Altitude of the Starlink Group 4-14 Satellite Group is 550 km."]
[5.164120674133301, 4.972127437591553, "The Receiving Antenna Location of the Pontianak and Biak Ground Station is To cover the satellite operation in the Central and Eastern part of Indonesia."]
[8.627973556518555, 1.6904600858688354, "The Shutdown Date of the Spitzer Space Telescope Telescope is January 30, 2020."]
[7.93473482131958, 6.735710144042969, "The Frequency of the LED Light Source Linearity Checks Calibration is Weekly."]
[7.018662452697754, 1.1133745908737183, "The Calibration Date of the Resourcesat-2A Satellite is July 12-19, 2016."]
[10.239405632019043, 4.95503044128418, "The Development Status of the 1 N Thruster Propulsion System is Flight-ready."]
[8.321012496948242, 1.5700267553329468, "The Data of the Rosetta Spacecraft is 2015, 2016."]
[8.45120620727539, 7.316920757293701, "The Operation Mode of the ASAR Sensor is High-rate mode."]
[9.192291259765625, 3.2378344535827637, "The Orbit of the AERO-VISTA mission Satellite Mission is Sun-synchronous, near-polar orbit."]
[6.553717136383057, 4.618790149688721, "The Application Categories of the Sentinel-3 Ocean Surface Topography Mission is Marine meteorology, Operational oceanography, Climate change."]
[3.198551654815674, 5.047476768493652, "The Type of the DDR2 SDRAM Memory is Double Data Rate Synchronous Dynamic Random Access Memory."]
[7.219050884246826, 2.450460195541382, "The Documentation Concern of the RISESAT Project is True."]
[9.828960418701172, 4.197194576263428, "The Area of the Icarus-1 Drag Sail is Approximately 6.7 m2."]
[7.73462438583374, 7.199077129364014, "The Components of the TEMPO Instrument is Off-axis reflective Schmidt telescope and an Offner spectrometer."]
[8.159676551818848, 4.916013717651367, "The Geolocation Error Requirement of the Satellite Satellite is Smaller than approximately 10% of the footprint size."]
[6.276906490325928, 2.076960802078247, "The Orbit of the JASON-3 Satellite is Same as JASON-2."]
[0.9375884532928467, 4.198688507080078, "The Capacity of the Lithium-polymer battery assembly Power Storage is 3.4 Ah."]
[5.637882709503174, 9.175048828125, "The Power Consumption of the CEASE-1 Instrument is 1 W."]
[7.629678726196289, 9.493612289428711, "The Requirement of the Spectral Channel Detector is >200."]
[3.7231152057647705, 6.112173557281494, "The Data Delivery of the Command and Telemetry Interface Interface is 19-byte status of health information of the AIP."]
[11.371179580688477, 6.663040637969971, "The Boom Status of the IXPE observatory X-ray Observatory is Delivered."]
[9.490850448608398, 5.764056205749512, "The Torque Coils of the ACS Attitude Control Subsystem is Six."]
[3.3191585540771484, 5.175384998321533, "The Lossless Compression Ratio of the HSDR FPGA Hardware is 2.8:1."]
[7.776518821716309, 0.8969730138778687, "The Launch Date of the Orion/ EFT-1 Spacecraft is 5 Dec 2014."]
[11.261085510253906, 2.6191444396972656, "The Height of the Tvashtar Volcano Plume Volcanic Plume is 290 km (180 miles)."]
[6.952867031097412, 7.239303112030029, "The Degradation of the Piezoelectric Cantilevers Component is Systematic errors."]
[11.719155311584473, 7.5104827880859375, "The Ovenized Crystal USO Frequency Drift of the DSAC Demonstration Unit is Below 1 x 10 -10/day."]
[9.345809936523438, 9.284209251403809, "The Focal Length of the Geoton-L1 imager Optical Subsystem is 400 cm."]
[11.6106595993042, 1.8924354314804077, "The Descent Speed of the MASCOT Lander is Slower than an earthly pedestrian."]
[5.347926139831543, 2.699235677719116, "The Agency of the QBITO CubeSat is UPM (Universidad Polit\u00e9cnica de Madrid)."]
[3.709520101547241, 6.242286205291748, "The Downlink Baud Rate of the CMC Transceiver Communication Device is 9600 baud."]
[9.319327354431152, 9.194624900817871, "The Telescope of the VIRUS-W Instrument is McDonald Observatory\u2019s 2.7-meter Harlan J. Smith Telescope."]
[9.324419975280762, 7.7661943435668945, "The ESA: electrons, ISA: ions of the Particle Species Sensor is ESA electrons, ISA: ions."]
[12.623515129089355, 6.918618202209473, "The Pulse period (ms) of the GROJ1744-28 Pulsar is 467.000."]
[10.25350284576416, 6.965926647186279, "The Purpose of the Thermal Protection and Hot Structures Technology is Validation of the flight performance of thermal protection materials and complex design solutions."]
[9.62761402130127, 1.620176911354065, "The Orbit Repeat Cycle of the TSX and TDX Satellites is 11 days."]
[7.4896321296691895, 2.9932823181152344, "The Unknown of the DART Spacecraft is Unknown."]
[8.311224937438965, 3.87770676612854, "The Shutter of the Satellite Instrument Instrument is Not used."]
[2.2334256172180176, 5.7060699462890625, "The Power of the SSPA Solid-State Power Amplifier is 8 W."]
[10.22144889831543, -0.8824684023857117, "The Mezzanine Size of the GHGSat-D Microsatellite is 7 x 18 x 42 cm."]
[7.209483623504639, 4.267770290374756, "The Sensor complement / remarks of the Meteor-1-1 Satellite is TV, IR, AC."]
[1.249327301979065, 4.146214485168457, "The Battery Type of the GHGSat-D Microsatellite is Li-Ion."]
[8.234776496887207, 3.1358864307403564, "The Global Forest/Non-Forest Map Publication Date of the TanDEM-X Satellite is Feb. 2018."]
[7.693185329437256, 5.817521095275879, "The Accuracy of the CLARREO Satellite is 0.1 K in brightness temperature."]
[10.354547500610352, 7.695157051086426, "The Flexural Rigidity of the Aluminum-polymer laminate Material is 5.6 x 10-4 Nm."]
[12.127679824829102, 3.324843645095825, "The Inclination of the STPSat-3 Satellite is 40.5\u00ba."]
[9.046072006225586, 3.385650157928467, "The Orbital Plane of the CSG and CSK satellites Satellite is Same."]
[11.548752784729004, -1.298504114151001, "The Mass (kg) of the Sentinel-1A/B Satellite is 2300."]
[6.6933159828186035, 2.0848913192749023, "The Patrick Blau of the Global Precipitation Measurement (GPM) Satellite is GPM Core - Mission & Spacecraft Overview."]
[8.89764404296875, 7.327798843383789, "The Error (RMS) of the Coarse sun sensor Sensor is <10\u00ba."]
[7.782120704650879, 6.665752410888672, "The Solving Scheme of the MLFMM (Multilevel Fast Multipole Method) Algorithm is Recursive."]
[3.8938159942626953, 4.3846354484558105, "The Programming Language of the SCIP Processor is Forth."]
[7.803711891174316, -0.4905203580856323, "The Installation Date of the SpaceX CRS-17 Mission is May 6."]
[8.394709587097168, 2.193115472793579, "The Communication Method of the Voyager 2 Spacecraft is Deep Space Network's 70-meter-wide (230-feet-wide) radio antenna in Canberra, Australia."]
[9.658393859863281, 5.566897869110107, "The ADCS System of the DeorbitSail Satellite is First demonstration of this Cubesat-specific ADCS."]
[1.5609793663024902, 4.220086097717285, "The Mission Purpose of the HORYU-4 Satellite is Estimate the photo-electron emission current influence on spacecraft charging."]
[6.785016059875488, 5.499046802520752, "The Purpose of the SMAP Satellite is Measure freeze/thaw timing, soil moisture, monitor droughts."]
[9.216641426086426, 9.181544303894043, "The Photon Index Below the Break of the Second Broken Powerlaw Model Component is 1.96."]
[3.8377535343170166, 6.526609420776367, "The Number of RF Hybrids of the TTDL Component is 3."]
[7.349870204925537, 4.333459854125977, "The Imaging Instrument of the Landsat-7 Satellite is ETM+ (Enhanced Thermal Mapper Plus)."]
[10.32907485961914, 7.05975866317749, "The Material of the Thermal Protection System System is Ceramic materials."]
[8.900455474853516, 5.898032188415527, "The Attitude Determination of the S/C Satellite is Magnetometer and sun sensors."]
[7.934292793273926, 4.812392711639404, "The SGSD Goal of the HYPSO-1 Satellite is Better than 100 m/pixel."]
[5.578535556793213, 5.58341646194458, "The | of the Novatel GPS Receiver GPS Receiver is Novatel GPS receiver."]
[5.753542423248291, 6.655933380126953, "The Dimensions of the IPEX-II boom ADAM mast is 2.35 m x 0. 3 m x 0.3 m."]
[5.456810474395752, 2.8841896057128906, "The Avionics of the Platform Satellite is SSTL-100, SSTL-150 and SSTL-300."]
[11.517343521118164, 5.951741695404053, "The Observation Date of the Murchison Widefield Array (MWA) Radio Telescope is Unknown."]
[8.808259963989258, 5.984370708465576, "The Function of the MARIN Inertial Measuring Unit is Monitor the position, orientation, and movement of the satellite."]
[7.397266387939453, 7.934980869293213, "The Ozone Concentration Measurement Altitudes of the UVSP Instrument is 50 - 75 km."]
[6.980263710021973, 0.288758248090744, "The Launch Date of the MetOp-SG Satellite is 2024-2039."]
[4.396350383758545, 5.358255386352539, "The Bi-directional sharing of the TT&C Services Communication Services is Enhances effectiveness and reduces the risk for both agencies."]
[6.31685733795166, 8.170600891113281, "The RIN Performance of the ASM Instrument Instrument is -105 dB (Hz)^1/2 at 2 mW of output power around 1 kHz."]
[7.496715545654297, 8.595880508422852, "The Total Column Ozone Data Resolution of the Nadir Sensor Wide-Field Telescope Sensor is About 50 km x 50 km at nadir."]
[1.862563133239746, 4.044102668762207, "The Size of the Solar Panels Power Generation is 0.81m x 0.72 m."]
[7.575894355773926, 7.954344749450684, "The Accuracy of the CERES Instrument is 1.0%."]
[6.128837585449219, 3.060150384902954, "The Program Partners of the MYriade Satellite is CNES, Alcatel, Astrium."]
[4.279220104217529, 5.868301868438721, "The Downlink communications (Ka-band) of the Spacecraft Satellite is 278 Mbit/s (QPSK)."]
[4.842984199523926, -3.3787810802459717, "The Member of the Hans-Peter Marshall Individual is True."]
[7.741343021392822, 0.9327626824378967, "The Scheduled Lift Off of the EM-2 Exploration Mission-2 is As soon as 2021."]
[7.966203689575195, -0.7260245084762573, "The Arrival Date of the SpaceX-CRS-4 Dragon capsule Cargo Capsule is Sept. 23, 2014."]
[11.345856666564941, 7.014048099517822, "The Sensitivity of the NICER X-ray Timing Instrument is 30 times the sensitivity of RXTE to background-dominated sources."]
[7.200898170471191, -0.010812332853674889, "The Launch Time of the Cesium Satellite 1 Satellite is 18:12 UTC."]
[8.72861099243164, 5.274011135101318, "The Pointing Control of the QuikTOMS spacecraft Satellite is 0.5\u00ba."]
[8.265421867370605, 10.242531776428223, "The PAN Spatial Resolution of the PMC Imager is 2 m."]
[7.6021318435668945, 2.258711576461792, "The URL of the ExoMars Mission is http://www.russianspaceweb.com/exomars2018-2017.html."]
[10.169986724853516, 4.867978572845459, "The Manufacturer of the NEXT-C Ion Propulsion System is NASA's Glenn Research Center."]
[6.503545761108398, 1.5731759071350098, "The Development Start Date of the Jason-CS / Sentinel-6 Satellite Mission is Late 2013."]
[5.081860542297363, 6.976785182952881, "The Main Beam Efficiency (%) of the Antenna Reflector is 88."]
[9.000226974487305, 2.1913223266601562, "The Components of the BepiColombo Spacecraft is Star trackers, spectrometer, magnetometer boom."]
[6.877316951751709, 1.3730978965759277, "The Meeting Date of the TriG GNSS Receiver is September 22-25, 2009."]
[7.96602725982666, 1.2139477729797363, "The Release Date of the Arctide2017 Tidal Model is 15 September 2018."]
[4.4977335929870605, 2.9605038166046143, "The PRN of the GSAT-0102 Satellite is 12."]
[7.436189651489258, 7.776595592498779, "The Incidence Angle Measurement of the Radiometer Sensor is From the surface."]
[8.4480562210083, 3.227440357208252, "The Formation Flying Separation of the TanDEM-X Satellite is 200m."]
[7.266616344451904, 0.7805824279785156, "The Mission Date of the O/OREOS Sat Satellite is Oct. 12-16, 2009."]
[5.069989204406738, 2.4158308506011963, "The New Avionics of the TDS-1 Satellite is 25."]
[8.062931060791016, -0.6736370921134949, "The Splashdown Time of the Crew Dragon spacecraft Resilience Spacecraft is 7:06 p.m. EDT."]
[8.130703926086426, 4.724480152130127, "The Video Resolutions of the NEMO-HD Satellite is 1920 x 1080 pixels, 2.8 m GSD, 75 m GSD."]
[7.20458459854126, 3.271449565887451, "The Ground Segment of the BRITE-Austria Satellite is Unknown."]
[9.330349922180176, -0.651703953742981, "The Project Team Members of the AzTechSat Nanosatellite is Maria de la Luz Garcia Cruz, Rosa Reyna Gonzalez Cancino, Ana Belen Urrutia Bartsch."]
[4.818403244018555, 1.814064621925354, "The Number of satellites per system of the WorldView Legion Satellite System is 6."]
[7.0446929931640625, -0.0653085857629776, "The End of Life of the THEIA Satellite is Shutdown Procedure."]
[4.019588470458984, 6.372701168060303, "The Downlink Frequency of the Payload Imagery Imaging is 8246.56 MHz."]
[6.167119979858398, 2.628556489944458, "The Affiliation of the Nicolas Multan Director of Space Systems and Vice President is Nexeya."]
[6.216005802154541, 2.266627550125122, "The Project Management of the Jason-2 Satellite is NASA and CNES."]
[6.345329284667969, 3.1904208660125732, "The Unknown of the COIN Collaboration Research Collaboration is Unknown."]
[3.808455467224121, 2.301862955093384, "The Size of the CUNYSAT-1 CubeSat is 1U."]
[7.258678436279297, 7.917447090148926, "The Test Duration of the Myriad 2 Vision Processing Unit is 36 straight hours."]
[8.028752326965332, -0.7378035187721252, "The Installation Date of the Dragon Spacecraft is 27 July 2019."]
[6.983915328979492, 0.8793244957923889, "The Launch Date of the TeLEOS-1 Satellite is Unknown."]
[8.820911407470703, 9.37503719329834, "The Instantaneous Field of View (IFOV) of the Detector Sensor is 0.182 mrad."]
[7.519534587860107, -0.4576259255409241, "The Launch Date of the Falcon 9 Rocket is March 14, 2021."]
[7.53032112121582, 0.6497225165367126, "The Operation Review Date of the Grace Mission Satellite is June 30, 2011."]
[1.4502047300338745, 4.200567245483398, "The Battery Energy of the QuikTOMS spacecraft Satellite is 10 Ah."]
[7.325500011444092, 0.9401010870933533, "The Mission Selection Date of the ICON Satellite is April 12, 2013."]
[8.903745651245117, 6.8715643882751465, "The Number of Accelerometers of the Truss Structure is 22."]
[3.7645742893218994, 5.5973734855651855, "The Mission Data Downlink of the Spacecraft bus Satellite is 120 Mbit/s."]
[9.672001838684082, -0.6674282550811768, "The Bus Structure of the SOHLA-1 Microsatellite is Isogrid panels."]
[4.9371514320373535, -0.09590829163789749, "The Close Approach Complaint of the OneWeb Company is Filed in Federal Communications Commission."]
[7.766191005706787, 2.211495876312256, "The URL of the Exo-Brake Parachute is https://gameon.nasa.gov/2016/12/13/nasas-exo-brake."]
[7.431050777435303, 8.455238342285156, "The Spectral Sample of the SUCHI Instrument is Seven wave channels between 7 and 14 \u00b5m."]
[6.109518527984619, 9.68761920928955, "The Mass of the PTOLEMY Evolved Gas Analyzer is 4.5 kg."]
[6.995622634887695, 2.632169723510742, "The URL of the VNREDSat-1 Satellite is 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."]
[6.977834701538086, 6.218267917633057, "The Spatial Resolution of the Sea Surface Temperature (SST) Measurement is 15 km."]
[7.290500164031982, -0.7571102380752563, "The Input Data of the CYGNSS Satellite Constellation is Winds."]
[3.888247489929199, 4.53666877746582, "The Manufacturer of the Stamp9G20 Microcontroller is Taskit."]
[9.196834564208984, -0.5640875697135925, "The Publication Date of the Galassia Nanosatellite Satellite is 31 May 2016."]
[3.9444282054901123, 5.681294918060303, "The Data Downlink Speed of the NorSat-3 Satellite is Up to 2 Mbit/s."]
[9.804971694946289, 8.676501274108887, "The Telescope of the Tyvak-0130 Satellite is One with a narrow field of view."]
[9.214935302734375, -0.6369181871414185, "The Deployment Date of the Flock 1b Nanosatellites is August 19, 2014."]
[5.267463207244873, 10.442876815795898, "The Error Assimilation Purpose of the LI System Lightning Information System is Improve very short range forecasts of severe convective events."]
[4.179325103759766, 5.8466362953186035, "The Downlink communications (X-band) of the Spacecraft Satellite is 800 Mbit/s (16 QAM), 400/200 Mbit/s (QPSK)."]
[12.634136199951172, 6.926131725311279, "The Pulse period (ms) of the B1509-58 Pulsar is 150.658."]
[9.51624584197998, 8.833288192749023, "The Limitation of the Optical Telescopes Instrument is Orbiting objects become unresolvable at high orbits or small telescope apertures."]
[11.799633026123047, 4.541399002075195, "The Age of the Cassiopeia A (Cas A) Supernova Remnant is 320 years."]
[6.771459102630615, 7.291676044464111, "The Manufacturer of the Scanning LIDAR LIDAR is Jena-Optronik GmbH."]
[8.36971378326416, 8.549768447875977, "The Alignment of the OSIRIS Optical Sensor is Tracking sensor aligned to the collimator."]
[2.285123348236084, 4.409788131713867, "The Power Consumption of the Scientific Payload Satellite Payload is High."]
[9.38288402557373, 8.1732759475708, "The Power Consumption of the RAMIS Radiation Detector is 3 W \u2013 4 W."]
[1.7432947158813477, 4.109848976135254, "The Efficiency of the Solar Cells Power Generation is 30%."]
[9.836892127990723, 2.813615560531616, "The Burn Altitude Change of the EURECA Satellite is From 420 km to 508 km."]
[7.810263156890869, 5.823655128479004, "The Observation Purpose of the MIRIS Satellite is Functional test purposes without any proper calibration process."]
[9.338624000549316, 2.777463912963867, "The Impact Speed of the DART Spacecraft is Approximately 3.7 miles per second."]
[3.9382169246673584, 4.348991870880127, "The Data Bus of the C&DH Subsystem Command & Data Handling is MIL-STD-1553B."]
[11.636908531188965, -1.3319742679595947, "The Mass of the KazEOSat-2 Satellite is 185 kg."]
[6.427728176116943, 3.652864933013916, "The Design and Operational Concept of the Mission Operations Facility Facility is The Mission Operations Facility design and operational concept for EUMETSAT\u2019s next generation geostationary satellite program (MTG)."]
[6.891552925109863, 6.297815799713135, "The Wind Direction Range of the SCAT Wind Measurement System is \u00b120\u00ba."]
[6.594170570373535, 5.744925022125244, "The Implementation Complexity of the Occultation Techniques Atmospheric Study Method is Easy to implement in principle."]
[11.853728294372559, 1.017186164855957, "The Launch Date of the Chang'e-4 Lunar Spacecraft is December 8, 2018."]
[6.07540225982666, 2.8737449645996094, "The Consortia of the Moonlight Lunar Telecommunications and Navigation Satellite Network is Telespazio leads the first consortium."]
[6.204192161560059, 8.183884620666504, "The Frequency Range of the Spectrum Analyzer Device is \u00b1 7 MHz."]
[7.109702110290527, 5.264167785644531, "The Social Value of the COS Climate Observing System is Lost if information is not used."]
[4.99662446975708, 3.3621692657470703, "The Conference Location of the CubeSat Laser Communication Crosslink Pointing Demonstration Satellite Communication System is Logan, UT, USA."]
[7.567092418670654, 4.181209087371826, "The Orbital Deviation of the Sentinel-1A and Sentinel-1B Satellites is \u00b150 m radius."]
[5.8686370849609375, 2.9907562732696533, "The Manufacturer of the Phi-Sat-1 Satellite is \u03a6 Department of the Earth Observation Directorate."]
[5.439526557922363, 4.225487232208252, "The Location of the DFD Data Center is Germany."]
[10.216403007507324, 3.461245059967041, "The Separation Distance of the ASTRO and NextSat Satellites is 10 m."]
[6.260809898376465, 3.727691650390625, "The Testing Location of the Solar Orbiter Spacecraft is IABG facilities in Ottobrunn, Germany."]
[4.769895553588867, 1.7294349670410156, "The Number of Satellites of the Indian rocket Rocket is 31."]
[7.669698715209961, 0.28822705149650574, "The End of Life Date of the Meteor-1/Meteor-2/Meteor-Priroda Series Satellite Mission is 01 Jan 2001."]
[8.968589782714844, 6.932701110839844, "The Sensitivity of Ion Density Fluctuation of the PAP Plasma Analyzer is 1 x 10^27."]
[9.735383033752441, 1.581946849822998, "The Repeat Cycle of the SPOT 1-5 Satellite is 26 days."]
[8.277986526489258, 0.7447689771652222, "The Mission Extension of the Megha-Tropiques Satellite is 2 years."]
[6.100135326385498, 0.8488360643386841, "The Technology of the RAVAN Satellite is Carbon nanotubes that absorb outbound radiation and a gallium phase change blackbody for calibration."]
[10.118548393249512, 5.2118144035339355, "The Setup of the Integrated Firing Test Test is Spacecraft installed the propulsion system was mounted on the thrust stand."]
[6.16806173324585, 4.059606075286865, "The Data Processing Requirement of the SVOM Satellite is Super-computers to process the data in real-time and smart algorithms to broker which transients to focus on with follow-up facilities."]
[7.323679447174072, 2.620997905731201, "The URL of the Chandra X-Ray Observatory Satellite is https://www.nasa.gov/sites/default/files/108075main_REVchandra.pdf."]
[5.346579551696777, 4.467994689941406, "The Installation Location of the ELF Device is Upper part of MSPR-2, called the Work Volume (WV)."]
[8.278244018554688, 6.6725006103515625, "The Mounting Technique of the MPO-MAG instrument Instrument is Boom mounting technique."]
[8.582775115966797, 9.275955200195312, "The Color of the Transmit Collimator Optical Component is Yellow."]
[6.294517517089844, 2.2741448879241943, "The Data Products of the Jason-1 Mission Mission is Sea surface topography, Significant wave height, Surface wind speed, Ocean tides, Vertically integrated atmospheric water vapor, Vertically integrated ionospheric electron content."]
[2.0990054607391357, 3.913043975830078, "The Power Generation of the SPOT-3 Satellite is Solar array."]
[4.2178168296813965, 3.795860528945923, "The Operating Frequencies of the NorAIS-2 Receiver AIS Receiver is Set to any frequency within the maritime VHF band."]
[9.906585693359375, 9.611715316772461, "The Expected O3 Recovery of the SAGE-III on ISS Satellite Instrument is About half of the amount lost from pre-1980 levels by the 2020s."]
[8.365352630615234, 3.4016661643981934, "The Absolute Height Accuracy of the TanDEM-X Satellite is About 1m."]
[4.530406475067139, 5.5609307289123535, "The Data Acquisition Channels of the PDS Data Services is X-band channel, ARTEMIS data-relay satellite's Ka-band channel."]
[10.22614860534668, 7.657358646392822, "The Material of the Phantoms Mannequin Torsos is Mimic human bones, soft tissues, and organs of an adult female."]
[9.406042098999023, 6.169226169586182, "The Telemetry Information of the Attitude Determination Quaternion Filter Experiment is Probability distributions for the selection of each different measurement matrix."]
[6.743090629577637, 2.0719799995422363, "The Purpose of the GPM Satellite is 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."]
[7.116995334625244, 4.996097564697266, "The Mission Goals of the PACE Satellite is 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."]
[10.963600158691406, 4.167612075805664, "The Observation of the ExoplanetSat Satellite is Exoplanets."]
[5.817267417907715, 3.736593723297119, "The Steps of the Deployment Sequence Process is 1) Prior to launch, the inflatable tubes and the membrane are placed into the hold structure."]
[9.446735382080078, 7.858590126037598, "The Measurement Range of the IRM Mass Spectrometer is 0.5-100 eV ions."]
[7.821385383605957, 2.9502861499786377, "The Revisit Time with Orbital Manoeuvres of the Cartosat-2E Satellite is One day."]
[8.764898300170898, 3.6370396614074707, "The Formation Control of the TSX and TDX Satellites is Precise."]
[8.205711364746094, 5.632416248321533, "The Leading Noise Terms of the Satellite Spacecraft is Optical sensing."]
[7.38013219833374, 2.9324896335601807, "The Mission Overview of the STEREO Satellite is  Solar Terrestrial Relations Observatory."]
[5.44040584564209, 1.2563725709915161, "The First Stage Landings of the Falcon 9 Rocket is 9."]
[6.218017578125, 4.292097091674805, "The Responsible Agency of the JPSS Satellite is NOAA."]
[7.849684715270996, 8.798261642456055, "The Wavelengths of the OLI-2 Instrument is Nine."]
[10.24105167388916, 5.720160007476807, "The 1\u20133 electron guns of the Positive Tether Charging Mode Test Procedure is The positive mode will need additionally 1\u20133 electron guns."]
[6.9614033699035645, 9.179283142089844, "The Azimuth Resolution of the High Resolution Spotlight Imaging Mode is 2.2 m (dual pol.)."]
[10.491665840148926, 4.628547668457031, "The Operation Time of the HPS Hall-thrust Propulsion Subsystem is Under 10 minutes."]
[5.691411018371582, 2.8744029998779297, "The Satellite Manufacturer of the Surrey Satellite Technology Limited Company is True."]
[10.614836692810059, 7.556121349334717, "The Material of the Bus Satellite Structure is Aluminium honeycomb panels."]
[6.939960956573486, 0.9013257622718811, "The Launch Date of the ELISA Satellite is Unknown."]
[6.616429805755615, 10.684210777282715, "The Estimated SNR of the Band 1 Spectral Band is 845.85 \u00b1 89.97."]
[7.262681007385254, 9.267678260803223, "The Thermal Gradients of the FG Filtergraph is Unknown."]
[4.02421760559082, 5.58670711517334, "The Download Flag Reset of the Data Download System Satellite System is Download flag can easily be set back to \u201cnot downloaded\u201d."]
[5.314018726348877, 10.397037506103516, "The Mission Status of the ISS:LIS Lightning Imaging Sensor is Operational (extended)."]
[7.292187213897705, 5.42749547958374, "The Radiation Resistance of the Bdelloids Species of Rotifers is Extremely resistant to radiation."]
[7.270840644836426, 1.3655451536178589, "The Contract Signing Date of the Three high-priority environmental missions Missions is 13 November 20220."]
[9.235742568969727, 4.145811557769775, "The Size of the Gnome Chompski Space Component is 150 mm."]
[6.838070392608643, 1.2144792079925537, "The Conference Date of the Roshydromet Program Satellite Program is Sept. 19-23, 2005."]
[6.084732532501221, 3.292257070541382, "The Responsibilities of the ALMASpace Consortium is Managing the project, formal interfaces to ESA/ESTEC, payload selection, qualification and integration onboard the spacecraft, mission implementation management."]
[7.391013145446777, 3.5864031314849854, "The Destination of the CE-4R satellite Satellite is Moon Earth L2 point."]
[8.182713508605957, 7.911887168884277, "The Maximum Misalignment of the Optical Sensor Systems Calibration Laboratory is 0.001\u00ba."]
[7.735426425933838, 8.75029468536377, "The Instantaneous spectral coverage of the Spectrometer Instrument is 2.16 km/s."]
[8.161890983581543, 10.534737586975098, "The Advantages of the Coherent Detection Technology is Enables the maximum data rate at minimum power."]
[7.9556779861450195, 5.248238563537598, "The Affiliation of the DTU's Geomagnetic Measuring Stations Ground-based Measurement System is DTU."]
[3.669259786605835, 2.287139892578125, "The Size of the FIREBIRD-2 A and B Satellite is 1.5U CubeSat."]
[4.428234577178955, 7.675776481628418, "The Bandwidth of the Channel 7 Sensor is 1000 MHz."]
[8.09880256652832, 2.1616525650024414, "The Launch Date of the ARTEMIS Satellite is July 12, 2001."]
[8.279563903808594, 1.8836673498153687, "The Article Date of the Herschel Satellite is July 1, 2014."]
[7.0311126708984375, 3.5511300563812256, "The Proximity of the POPACS Satellite is DANDE."]
[9.588546752929688, -0.521236002445221, "The Purpose of the KMSL smallsat Satellite is Experiments in microgravity."]
[5.092272758483887, 4.207075119018555, "The Selects the interesting opportunities to execute links during increment N of the LCT Operations Team Operations Team is The LCT Operations Team at TES selects the interesting opportunities to execute links during increment N."]
[8.021636009216309, 3.8802402019500732, "The System Status of the Pleiades Satellite is Unknown."]
[7.9795002937316895, 7.266446590423584, "The Location of the Spectral Calibration Calibration is Ground."]
[4.8054280281066895, 1.7844289541244507, "The Staff Count of the Orbital Sidekick Company is 33."]
[4.485657691955566, 5.434980869293213, "The Supplier of the TT&C transponders Communication is COM DEV."]
[7.029388427734375, 1.0313044786453247, "The System of Systems Presentation Date of the UrtheCast Satellite is October 20-24, 2014."]
[7.128724575042725, 5.843038558959961, "The Instrument of the Aeolus satellite Satellite is Space Doppler wind lidar."]
[5.536838531494141, 6.410781383514404, "The Length of the Spin Axis Dipole Antenna Antenna is 15 m."]
[4.491755485534668, 3.9908688068389893, "The Electrical Connection of the SPA Components Components is SPA standard connector."]
[8.548398971557617, 8.285989761352539, "The Number of Detectors of the ULEIS Spectrometer is Six."]
[8.013614654541016, 9.459811210632324, "The Wavelength of the SWIR Detector is 3.75 \u00b5m."]
[10.562858581542969, 7.531742095947266, "The Material of the Bushings Component is Polyimide plastic with impregnated graphite."]
[4.831250190734863, 1.779980182647705, "The Number of Satellites of the Landsat Next Satellite Constellation is 3."]
[6.704868316650391, 7.619191646575928, "The Accuracy of the Laser Rangefinder Device is Better than 1 meter."]
[2.351851463317871, 4.436894416809082, "The Power Initialization of the Satellite Spacecraft is Autonomously perform the initialization sequence."]
[6.208231449127197, 5.0861382484436035, "The Tracking System of the MMS Satellite is GPS signals."]
[7.171772480010986, 8.83070182800293, "The Swath Width of the AATSR Instrument is 500 km."]
[10.40285873413086, 5.693634033203125, "The Deployment Duration of the ATEx Tether Experiment is 18 minutes."]
[7.3795294761657715, 3.556644916534424, "The Sensor of the ZY 1-02C Spacecraft is PMS (Panchromatic/Multispectral) Camera."]
[10.459124565124512, -1.003199815750122, "The Mass of the VesselSat-1 Microsatellite is 29 kg."]
[5.647029876708984, 1.4872794151306152, "The Landing Location of the Starliner Spacecraft is White Sands Space Harbor in New Mexico."]
[7.573401927947998, 2.6931402683258057, "The Presentation Date of the KOMPSAT-5 Satellite is July 25-30, 2010."]
[8.657415390014648, 5.255416393280029, "The Pointing Accuracy of the QuickBird-2 Satellite is \u00b10.016o (3? steady state in all three axes)."]
[9.88411808013916, -0.7705103158950806, "The Main Imager Spatial Resolution of the PROBA-1 Microsatellite is 17 m."]
[5.76205587387085, 3.010186195373535, "The Customer Industries of the Climavision Company is Delivery companies and airlines."]
[7.812236785888672, 10.113837242126465, "The MS B4 of the Pushbroom imager Spectral Band is 0.76-0.89 \u00b5m."]
[4.705410003662109, 2.286438465118408, "The Quantity of the CM1 and CM2 6U CubeSats is 2."]
[5.059340000152588, 8.712355613708496, "The Position Accuracy (RMS orbit) of the S-2 NRT Product is < 3 m (3D) 3-sigma."]
[1.8663986921310425, 4.012082576751709, "The Quantity of the Solar Panels Power Source is 4."]
[11.244909286499023, 6.850456237792969, "The Optics Presentation Date of the Imaging X-ray Polarimetry Explorer Satellite is 2017."]
[5.28909969329834, 3.663818120956421, "The Presentation of the IXV Mission and Flight Mechanics is Mission and Flight Mechanics of IXV from design to postflight."]
[10.147697448730469, 2.9495413303375244, "The Orbit Altitude of the ALOS-3 Satellite is 618 km."]
[5.391623020172119, 4.7927565574646, "The Satellite Type of the EUMETCast Dissemination System is Geostationary."]
[7.177020072937012, 2.8524420261383057, "The Mission of the SWOT Satellite is Surface Water and Ocean Topography."]
[6.965252876281738, 3.328631639480591, "The Operating Status of the Odin Satellite is Nominal."]
[7.7852983474731445, 10.522515296936035, "The ADC Resolution of the RADFET Circuit Circuit is 10 bit."]
[7.689835548400879, 1.5695487260818481, "The Meeting Date of the SMOS Satellite is Sept. 30, 2015."]
[7.870602130889893, 0.5562726259231567, "The Launch Date of the Aeolus Spacecraft is 22 August 2018."]
[6.785074234008789, 1.3207017183303833, "The Conference Presentation Date of the JC2Sat-FF Satellite is 18 - 21 August 18-21, 2008."]
[7.717858791351318, 13.597878456115723, "The Passband Range of the SPIM3 Spectrometer is 251-388 nm."]
[4.314628601074219, 5.297788619995117, "The Telemetry Module Mode of the TTCS Telemetry & Telecommand Subsystem is PCM/DPSK/PM."]
[5.926234722137451, 6.809004306793213, "The PRF of the Radar Instrument is 2.9 kHz."]
[7.805879592895508, 4.341280460357666, "The Image Capture of the Rosetta Satellite is 76,000 high-resolution images."]
[6.484387397766113, 2.983959674835205, "The Manager of the Chandra Program is NASA's Marshall Space Flight Center."]
[4.355722904205322, 5.859597682952881, "The Data Acquisition Rate of the HARP-2 Satellite is Minimum two frames/second."]
[12.134757995605469, 3.2405927181243896, "The Orbit Inclination of the Primary Mission Satellite is 98.7\u00ba."]
[9.42652702331543, -0.28048422932624817, "The Mission Objective of the FASTRAC Satellite is Demonstrate autonomous thruster operation using single-antenna on-orbit real-time GPS attitude determination."]
[7.763427734375, 9.040361404418945, "The ILP of the Instrument Spectrometer is 0.5 cm -1."]
[9.227670669555664, 3.0954089164733887, "The Mission of the LunaH-Map Satellite is Map hydrogen within craters and other permanently shadowed regions throughout the moon's south pole."]
[4.378683567047119, 7.781625270843506, "The Center Frequency of the Channel 6 Sensor is 42 GHz."]
[3.891209602355957, 5.1597723960876465, "The Data Samples of the DSLP Data Acquisition System is More than 35 million."]
[9.434650421142578, 5.7779645919799805, "The Attitude Control of the EURECA Spacecraft is Magnetorquers."]
[8.702596664428711, 8.737452507019043, "The Scan of the VISSR Mirror Instrument is 20\u00ba x 20\u00ba."]
[7.045698165893555, 2.924940347671509, "The Development Status of the SwRI Small Satellite Satellite is Unknown."]
[6.388053894042969, 1.7336357831954956, "The Ground Segment Design Presentation Date of the EnMAP Satellite is March 17-19, 2010."]
[7.064192295074463, 4.723659992218018, "The Detection Capability of the JJ-FAST Forest Early Warning System is Areas of deforestation in the order of a few hectares."]
[6.611326694488525, 10.686619758605957, "The Estimated SNR of the Band 6 Spectral Band is 427.81 \u00b1 136.32."]
[8.660835266113281, 3.327221155166626, "The Mission Aim of the SOAR Satellite is Test and characterize new materials that can reduce the experienced drag and increase aerodynamic performance in low altitude orbits."]
[8.143393516540527, 7.535625457763672, "The Calibration of the DDM Device is Absolute."]
[6.594199180603027, 2.8011982440948486, "The Attached to of the PEST Satellite is JAWSAT."]
[6.906698703765869, 1.241719126701355, "The Announcement Date of the OceanFinder Vessel Identification and Route Prediction System is 18 September 2019."]
[3.1436824798583984, 5.460252285003662, "The 1 Second Labels of the SSRNI Data Acquisition and Registration System is Yes."]
[3.5192623138427734, 4.075262069702148, "The Power of the STRV-2 DHS Data Handling System is 6 W."]
[7.839590072631836, 9.889371871948242, "The Power of the Instrument Spectral Imager is 129 W."]
[6.745856761932373, 10.151674270629883, "The Primary Use of the Band 7 Spectral Band is Ocean color."]
[5.879028797149658, 2.9194347858428955, "The Service Prime Capacity of the Surrey Satellite Technology Limited Company is Lunar services brand SSTL Lunar."]
[11.428529739379883, 5.162959575653076, "The Duration of the Transient Luminous Events Atmospheric Phenomena is Less than a millisecond to two seconds."]
[5.291819095611572, 6.192660808563232, "The Antenna Pattern of the Antenna Device is Cross-track direction."]
[9.985180854797363, -0.7381809949874878, "The Constellation Size of the ESAIL Microsatellite is More than 60."]
[6.606196880340576, 10.694294929504395, "The Estimated SNR of the Band 2 Spectral Band is 797.02 \u00b1 53.34."]
[10.131884574890137, 1.3812958002090454, "The Local Equator Crossing Time of the QuakeSat Satellite is 6:00 and 18:00."]
[6.311686992645264, 2.710191249847412, "The Objective 3 Purpose of the Jason-CS Satellite Mission is For determining tides, ocean circulation, climate change and sea level rise."]
[10.143804550170898, 3.9949469566345215, "The Target Asteroid Size of the NEA Scout Spacecraft is Less than 100 meters (330 feet) across."]
[9.040453910827637, 4.8730854988098145, "The Corrected FOV of the SPARCS Satellite is 1\u00b0."]
[6.474056243896484, 0.5607447624206543, "The Launch Date of the AeroCube-4 Satellite is Sept. 13, 2012."]
[7.552539348602295, 0.7278103828430176, "The Checkout Date of the Y-3 Detector is January 15 to 17, 1974."]
[10.17676830291748, 2.967846393585205, "The Orbit Altitude of the GEISAT Precursor Satellite is 520 km."]
[8.103090286254883, 9.783215522766113, "The Resolution of the TeLEOS-1 Imager Imaging Device is 1m nominal at nadir."]
[7.099188804626465, -0.08090858906507492, "The End of Life Date of the HJ-1 Satellite is 31 Dec 2022."]
[7.442694664001465, 4.74924373626709, "The Detection Capability of the PROBA-V Satellite is Aircraft."]
[10.645974159240723, 5.318909645080566, "The Position Control of the CNAPS Propulsion System is 1 m."]
[4.275876522064209, 7.265927314758301, "The Total Mass of the XPAA Phased Array Antenna is 5.5 kg."]
[6.875955581665039, 0.7812389731407166, "The Launch Date of the Estonia's student cubesat satellite Satellite is Unknown."]
[8.415846824645996, 9.876938819885254, "The Image Lines of the Focal Plane Array Detector Array is Recorded Simultaneously."]
[11.244779586791992, 3.5099616050720215, "The Peak Distance from the Sun of the Water Production Comet Activity is About 1.7 au."]
[7.441203594207764, 10.004714965820312, "The Spectral Bands of the Hyperspectral Imager Sensor is 150."]
[11.21406364440918, 4.250262260437012, "The Discovery of the Hubble Space Telescope is Myriad galaxies beyond our own."]
[11.073259353637695, 2.8942553997039795, "The Maximum Depth of the Lake Cedar Lake is 10 meters (32 feet)."]
[10.674675941467285, 3.4018356800079346, "The Distance of the Closest Approach Parameter is 0.71 km."]
[8.670147895812988, 4.857015132904053, "The Earth Footprint of the NEMO-AM Satellite is 35 km x 95 km."]
[5.530797958374023, 4.259108066558838, "The Instrument Operations of the Spacecraft Satellite is Performed \"offline\" of the MOC."]
[4.2840986251831055, 4.8649702072143555, "The File Transfer Capability of the JAXA Flight Controller Control System is Between SSIPC and JAXA laptops in JEM."]
[8.537569046020508, 0.14857430756092072, "The Environment of the ISS Space Station is Permanently crewed operational environment."]
[3.916736602783203, 6.403622150421143, "The Modulation Schemes of the Lithium 2 radio Communication Device is GMSK for low Earth to near Earth orbit, theoretically supports BPSK."]
[3.88055419921875, 4.793037414550781, "The Failure of the STM32 microcontroller Microcontroller is Loss of communication."]
[6.558498382568359, 1.415610671043396, "The Launch Year of the OCO-2 Satellite is 2014."]
[3.79533052444458, 2.291215419769287, "The Size of the Duchifat-1 CubeSat is 1U."]
[11.865504264831543, 4.54507303237915, "The Distance from Earth of the Crab Nebula Nebula is 6,500 light-years."]
[17.728548049926758, 7.162878036499023, "The J2000 declination (deg) of the B1813-140 Pulsar is -14.036."]
[5.901875972747803, 0.586866557598114, "The Reentry Date of the MaSat-1 CubeSat is January 9, 2015."]
[6.6104350090026855, 10.696287155151367, "The Nominal SNR of the Band 4 Spectral Band is 1070."]
[7.59417200088501, 0.49055060744285583, "The Launch Date of the JPSS Satellite is 2017."]
[9.526243209838867, 5.972369194030762, "The Mass of the ADCS Attitude Determination and Control System is 0.78 kg."]
[1.5811434984207153, 4.461434364318848, "The Efficiency of the Solar Array Regulator Buck-Boost Converter is Above 94%."]
[10.491799354553223, -1.1186598539352417, "The Mass of the Nanosatellite Satellite is 5.5 kg."]
[5.199819564819336, 3.991933584213257, "The Function of the ISSAC SOC Space Operations Center is Convert these requests into specific sets of commands for uplink to ISSAC."]
[2.937875509262085, 6.5609941482543945, "The Power of the DC Power Communication System is 1.0 W conditioned power (standby)."]
[11.434734344482422, 6.037769794464111, "The Funding Status of the Chandra X-ray Observatory X-ray Observatory is Funded through 2025 with options to extend through 2030."]
[2.209731340408325, 5.70615291595459, "The Amplification of the SSPA Solid State Power Amplifier is 2 W."]
[7.400393486022949, 3.230053424835205, "The Doppler and differential VLBI techniques of the Kaguya (SELENE) Satellite is 4-way."]
[6.834662914276123, 1.0046170949935913, "The News Release of the TecSAR Satellite is IAI news, First Quarter 2008, Issue 25."]
[6.112817764282227, 2.632124423980713, "The Preference for Working with U.S. companies of the NASA Organization is Strong."]
[6.340832710266113, 4.977795600891113, "The Contents of the Level-1B Data is Granule scene radiance data after radiometric correction and geometric correction processing."]
[7.979252815246582, 9.13317584991455, "The Resolving Power of the CHIPS Spectrometer is f/150."]
[11.606908798217773, -1.269777536392212, "The Mass of the GHOSt satellites Satellite is 91.4 kg."]
[7.977993011474609, 9.266919136047363, "The Spectral Band of the Instrument Spectrometer is MWIR."]
[3.5806961059570312, 6.600643634796143, "The X-band Tx Data Rate of the RF communications Communication System is 76.53 Mbit/s."]
[6.743736267089844, 7.148341178894043, "The Manufacturer of the ATLID Lidar Instrument is Airbus DS."]
[9.699236869812012, 1.5876528024673462, "The Repeat Cycle of the CBERS-4 Satellite is 26 days."]
[5.169084072113037, 5.109388828277588, "The Service of the KSAT Satellite Operations Provider is Satellite operations as-a-service for ESA's Arctic Weather Satellite."]
[5.000074863433838, 1.7405171394348145, "The Number of Satellites of the OptiSAR\u2122 Constellation Satellite Constellation is 16."]
[7.07620096206665, 0.5499393939971924, "The Launch Date of the STREAK Satellite is Sept. 23, 2005."]
[10.138352394104004, 4.833315372467041, "The Diameter of the T6 thrusters Ion Thrusters is 22 cm."]
[10.336033821105957, -0.8581938147544861, "The Payload Volume of the GOMX-1 Nanosatellite is 9 cm x 9 cm x 12 cm."]
[13.724764823913574, 1.608941674232483, "The Launch Date of the Vega Launch Vehicle is 28 April 2021."]
[8.610967636108398, 4.946243762969971, "The Capture Method of the ASTRO and NextSat Satellites is Docking mechanism."]
[5.417462348937988, 1.937742829322815, "The Design Incorporations of the Automated Transfer Vehicle Spacecraft is About 30."]
[9.426935195922852, 5.775152683258057, "The Attitude Control of the ACS Attitude Control Subsystem is Reaction wheels and magnetic torquers."]
[8.849472999572754, 9.109719276428223, "The Dimensions of the Slits Optical Instrument is 84 \u00b5m x 44.1 mm."]
[6.4488911628723145, 4.648186206817627, "The Instruments of the SciSat-1/ACE Satellite is MAESTRO, ACE-FTS."]
[4.751967430114746, 3.8826026916503906, "The Provider of the Sensor bus system System is Kayser-Threde GmbH."]
[10.177297592163086, 7.873940944671631, "The Baffle Material of the TX Telescope Telescope is CFRP."]
[8.561339378356934, 4.370359897613525, "The Telescope Aperture of the QuickBird-2 Satellite is 60 cm \u00d8."]
[9.194368362426758, 6.1588239669799805, "The Power Consumption of the CMG Control Moment Gyroscope is 3 W (peak)."]
[6.226418972015381, 5.007004737854004, "The OLI Bands of the Landsat-8 Satellite is 7-5-2."]
[8.266016960144043, 1.668168067932129, "The Renaming Date of the Solar Probe Plus Spacecraft is May 31, 2017."]
[10.734153747558594, 3.453522205352783, "The Tail Ray Length of the Parker Solar Probe Satellite is Nearly 5,000 miles."]
[6.2084197998046875, 2.877958059310913, "The Title of the Kevin Murphy Individual is NASA Earth Science Division chief science data officer."]
[7.780421257019043, 6.345409870147705, "The Testing of the Prometheus Satellite is 3-axis random vibration and lengthy thermal vacuum cycling."]
[10.649044036865234, 3.61557936668396, "The Current Position of the Solar Orbiter Satellite is Between the orbits of Venus and Mercury."]
[7.697192192077637, 5.0061845779418945, "The CH4 Relative Accuracy of the GOSAT Satellite is 2%."]
[5.217438220977783, 6.671176910400391, "The Mobility of the TUC Transponder Microwave Transponder is Mobile."]
[13.106585502624512, 4.058765411376953, "The Discovery of the Gaia Satellite is Detection of Starquakes."]
[3.22440767288208, 6.588749885559082, "The EIRP of the Steerable Beam Communication System is 57 dBW."]
[5.807349681854248, 6.53077507019043, "The Reflector Diameter of the L-band SAR instrument Instrument is 12-m."]
[6.631984233856201, 4.76295804977417, "The Imaging Frequency Band of the IceEye-1 Satellite is X."]
[9.301219940185547, 3.227246046066284, "The Orbit Type of the Main Payload Satellite is Sun-synchronous near-circular orbit."]
[4.665489673614502, 5.595505714416504, "The RF Communications Band of the ETS-VIII Spacecraft is S-band."]
[1.9596673250198364, 5.553071975708008, "The Power of the Voltage 7 Power Amplifier is 1.66."]
[8.357536315917969, 9.94818115234375, "The Array Size of the Detector Instrument is 1k x 1k."]
[5.177373886108398, 1.9887043237686157, "The SSBUV Instrumentation Flights of the Space Shuttle Spacecraft is Multiple."]
[8.497031211853027, 7.842374324798584, "The Data Provider of the RADMON Radiation Monitor is Aalto-1."]
[9.324365615844727, 5.02165412902832, "The Proton Dynamic Pressure of the ACE Satellite is ~1.4 nPa."]
[8.961076736450195, 5.206724643707275, "The Avoidance Targets of the SVOM Attitude Satellite Attitude is Sco X1 source, Galactic Plane."]
[10.155835151672363, 3.5248050689697266, "The Orbit Eccentricity of the UniCubeSat Satellite is Less than 0.2."]
[12.088478088378906, 3.2959418296813965, "The Orbit Inclination of the Sentinel-2 satellites Satellite is 98.6\u00b0."]
[9.457231521606445, 1.014743685722351, "The Flight Duration of the Spacecraft Satellite is About two months."]
[9.928502082824707, 3.985621213912964, "The Deorbiting of the NanoSail-D2 Satellite is Ongoing."]
[9.504733085632324, 0.48202961683273315, "The Design Life of the SCD-2 Satellite is 2 years."]
[7.038174152374268, 6.224972248077393, "The Spatial Resolution of the Sea Ice Concentration (SIC) Measurement is 5 km."]
[12.01989459991455, 4.493131160736084, "The Formation Event of the Blue Ring Nebula Nebula is Stellar merger between a star similar to our Sun and another star only about one-tenth that size."]
[5.269023895263672, 2.530405044555664, "The Location of the CubeSat Yonsei team Team is Korea."]
[9.541062355041504, 3.737884283065796, "The Formation Flying Mission of the CanX-4/CanX-5 Satellite is One Month."]
[9.197613716125488, 7.09445333480835, "The Deployment of the Langmuir Probe Plasma Measurement Device is Must be made deployable."]
[9.772336959838867, 8.983622550964355, "The Diameter of the Primary Mirror Telescope is 450 mm."]
[6.228972434997559, 3.456613540649414, "The Payload of the Cesium Satellite 1 Satellite is Cesium Nightingale 1 active phased array."]
[10.145734786987305, 3.094273328781128, "The Orbit Altitude of the Sentinel-2 satellites Satellite is 786 km."]
[7.652641773223877, 3.961493492126465, "The Measurement Type of the CryoSat-2 Satellite is Height of ice."]
[6.835187911987305, 0.4141305088996887, "The Review Date of the GEOS-1 Satellite is 1978."]
[9.101765632629395, 9.183061599731445, "The FOV in Transverse Spin Plane of the THD Horizon Detector is 6\u00ba."]
[11.350735664367676, 1.448163390159607, "The Location of the Yutu-2 Lunar Rover is Arrived at preset location A."]
[8.286941528320312, 3.085404634475708, "The Bistatic Recordings of the TanDEM-X Satellite is Since June 2020."]