"GEOTAIL POST MANEUVER ELEMENTS"
These Cartesian GEI elements are in Mean Equator/Equinox of 1950.
    EPOCH            X                Y                Z (km)
YYMMDDHHMMSS        VX               VY               VZ (km/s)
920725144500     89803.35654     -163131.5707     -65006.79863
                 .9195422870     -.9584426991     -.3043759517
920729140000     240447.6620     -252467.2869     -80322.67033
                 .7712495858D-01  .1983615615      .1161496891
920802150000     32392.95791      662.9659949      6686.354254
                -4.248545171      1.994859015      .1726752809
920807150000     250968.0163     -275734.8351     -89816.26339
                 .1644766905      .1044344644      .8358924749D-01
920812143000     31681.79815      1636.361178      6821.427611
                -4.356040830      1.925606059      .1333313783
920814120000     145499.5225     -228387.6391     -86159.18831
                 .7136131234     -.6425465651     -.1852006003
920821120000     263265.6063     -214488.8664     -58155.68966
                -.3449561491      .5450606904      .2165856071
920826113000     174359.3377     -244882.8867     -92965.82385
                 .6484115375     -.5032930271     -.1319417639
920902113000     265026.7136     -196406.6470     -50345.05216
                -.3976434207     .59400951532     .22675314315
920926120000     861583.5869     -6480.721113      113946.4111
                -.1172597672D-01  .3182823365      .1313233078
921014235004     165980.0935      303257.5893      138314.7964
                -.9257916654     -.4622533383     -.3034258057
921028210000     353297.9461      331292.7346      166788.4758
                -.3775029267      .1274215264      .0097965437
921107130000     310198.3383      51151.03597      53296.03047
                 .7669739743      .6783692565      .3453123839
921210120000    -32860.21956      1111456.364      423122.3302
                -.2433002444      .8952052571D-02 -.2280370565D-01
930108130000    -323160.6308      374575.6284      121335.9462
                 .2117638828     -.8444760704     -.2977071041
930110104716    -264685.7176      217921.5685      67262.28878
                 .6307874986     -.9862117046     -.3272890434
930129120000    -324901.1002      326909.7708      109142.2792
                 .2458232392     -.5551881089     -.1962647545
930209103000    -375572.4340      499205.6262      198729.3002
                -.6262706917      .2886088104      .1517124006
930307120000    -1075885.180      443000.3301      236559.7704
                -.9820414662D-01 -.1842538371     -.9759926898D-01
930402140000    -691600.6626     -130850.7159     -72558.28222
                 .5972831313     -.2844379815     -.1511861275
930510120000    -666807.1085     -350696.4696     -224343.9724
                -.1748659066     -.5335050148     -.2587270107
930618130000    -159802.5265     -1211455.913     -531759.2851
                 .2709462884     -.4302852009D-01  .2137056718D-01
930727140000     639430.9155     -600297.8202     -167815.9427
                 .0306488761      .5196923201      .2101185893
930915130000     443389.9740     -185295.2589     -40681.93583
                 .1590162987      .2908924810      .1160941743
930925100000     158104.7531     -206090.7889     -65210.03820
                 1.127496685     -.4351576423     -.8991394092D-01
930927015408     299241.0535     -244085.9782     -70399.49056
                 1.067703492     -.1713140445      .1630861928D-01
931115120000     740372.4970      1037367.032      432811.2313
                -.1959720978      .1308274514      .2270087191D-01
931231120243    -257612.1025      246282.2109      78141.50019
                 .2912217702     -1.083235167     -.3846645242
940114120000    -191965.4258      547183.0431      206106.9126
                -.3009947722     -.6866406235D-01 -.4973132668D-01
940220201057     59691.75746      350161.7376      140429.2043
                -.5083639286      .9819383947      .3390450402
940304103000    -564844.6084      691421.9254      211238.0143
                -.4995107912      .3195428225D-01 -.3238524704D-01
940425140000    -1056934.689     -652401.8413     -270787.7440
                 .2153198480     -.3522698016     -.1100193993
940519150000    -417905.3678     -1124980.139     -409655.5940
                 .3657187366     -.1012107687     -.2597576469D-01
940624170000     464199.4192     -369586.0053     -141119.9412
                -.8442173702D-01  .7758420495      .2709917840
940628100519     367406.9207     -87276.28213     -39103.10568
                -.6437294134      .9337035379      .3825057304
940723143000     459840.8254     -672852.7776     -307862.4954
                 .3081204527      .1810125997      .1008962812
940809153000     403711.3456     -25649.33969      5925.931336
                -.7388551541      .6818902920      .3009295003
940919123000     1078426.851     -324983.7977     -53453.75394
                 .9105828637D-01  .3598420253      .1357275494
941017130000     480414.3384      511054.7191      199553.5340
                -.6766039868      .1426509060      .6803885652D-02
941104180000     55191.74336      381922.1848      108345.8776
                -.4923563809      .2129588010      .4156956942D-01
941112034000    -27205.23774     -53331.62416     -15702.00355
                 3.199683160     -.8904640225     -.1452023636
941112063000     6906.839014     -57203.01188     -15686.60898
                 3.351385190      .1623278521      .1514570416
941112092000     39473.72220     -50435.23429     -12771.54895
                 2.942844226      1.103508152      .3997362468
950219181000    -33634.62700     -57655.42315     -15977.37437
                 2.908745203     -.9112130830     -.2713030625
950219210000    -2372.236585     -62805.26086     -17591.67310
                 3.120665642     -.6529303128D-01 -.3541464356D-01
950219235000     28867.69956     -58896.95542     -16667.45835
                 2.918510051      .8067476981      .2101028740
950226201000    -33408.19245     -57629.46801     -15905.52119
                 2.825034586     -.9182853367     -.2765261098
950226231000    -1145.971311     -62877.68736     -17596.71610
                 3.045421951     -.1983189496D-01 -.2569077193D-01
950227021000     30958.31494     -57993.43049     -16441.52445
                 2.794526126      .8949612800      .2328556796
950302140000    -77958.53901      149517.2846      42443.97304
                -.8141939453     -.8805600247     -.2408292444
950713070000    -11224.51356      187037.6747      53680.93505
                -1.001944895     -.3980601490D-01  .1529560720D-01
950810080000    -109603.1792      114438.4703      36063.39031
                -.4878753016     -1.213523335     -.3316235836
950824010000     67850.75142      150376.8794      40764.06657
                -.8504040687      .8889126030      .2819499404
950928080000    -90790.10837     -20458.12770     -2765.360836
                 1.419174774     -1.773756800     -.5580317329
951026190000     91387.24210      119372.2070      31187.35043
                -.6342124802      1.247831210      .3833816195
951123210000    -19965.60201      185136.3131      54586.43799
                -1.007443859     -.9552966010D-01 -.1216589480D-01
951214140000     35237.99010      173106.5268      48894.42256
                -.9791353989      .5131152476      .1915427335
951220133000    -19858.19321      185684.3977      55011.30355
                -1.002399729     -.4152139805D-01 -.1943543564D-01
960215000000     65562.91805     -30588.34339     -9108.682083
                 1.887820301      1.982558069      .5841976582
960301000000    -117171.0016      14076.47553      4456.172602
                 .7312155518     -1.692630658     -.5017563829
960306210000    -37967.30563     -59569.31239     -17502.43010
                 2.683228757     -.7777036160     -.2363805794
960325000000     18221.25145      173289.7166      51196.73263
                -1.049373800      .4300431000      .1287222000
960401000000    -113677.5693      126452.2261      37780.39666
                -.5696000650     -1.034441652     -.3036599436
960501000000     45360.45845      158502.5592      46756.07239
                -.9818517887      .7370874236      .2234036817
960530150000    -111049.6304      2718.832732      1681.606255
                 .9414168987     -1.711126639     -.5155118469
960624090000    -56937.11937      177899.4593      43465.12173
                -.9532299932     -.3023605037     -.7903189627D-01
960701000000    -129548.0845      87044.80138      27414.32901
                -.1715153036     -1.323789048     -.3907813453
961072503000     49221.35811      149067.0307      43429.41843
                -0.960083472      0.896444629      0.280058108
960801000000    -85713.97246      165219.3750      50264.17305
                -0.848039341     -0.552098401     -0.150016858
960829090000    -112141.8338     -9221.254214     -714.2291409
                 1.104819612     -1.591536283     -.4899771858
960901000000    -883.8135551      174251.9255      51503.52259
                -1.082296313      0.321838648      0.114562343
960926220000     65010.67102      126134.6851      36163.85916
                -.8848409218      1.194338053      0.369900959
961031220000    -134631.1303      47065.19217      16757.54820
                 .2409902023     -1.481395646     -.4442456583
961128020000    -98902.45034     -23302.68614     -4633.100059
                 1.450116499     -1.545597705     -.4927894735
961205180000     12178.78446      168924.5373      49933.56103
                -1.075764859      .4834260937      .1693574780
961206153000    -68383.60483      173135.3538      53113.92430
                -.9476200375     -.3401344321     -.7832504532D-01
970116140000     63285.97965      118484.2395      37965.81023
                -.8648373339      1.306733289      .3958294660
970201000000     85524.17930      36610.00234      12486.49476
                 .1033717137      2.214636582      .6911060229
970226230000    -10766.94119     -64515.37426     -20111.69598
                 2.919944619      .1347264659      .7262749949D-01
970301000000    -20001.21489      172015.1102      53106.58363
                -1.113833533      .2383071699      .6209997784D-01
970327140000    -21226.19380      170909.5154      52635.06837
                -1.127516574      .2246856734      .5864349596D-01
970401000000     62085.60350      114365.8588      35953.83610
                -.9127474295      1.343439676      .4066091205
970424150000    -133961.8157      117016.0656      34973.14766
                -.4789585658     -.9832654658     -.3080682732
970501000000    -125402.4457     -1049.099598     -1409.966308
                 .9112073856     -1.489746383     -.4525215427
970522170000    -57202.55498     -55775.72461     -17622.49587
                 2.391689918     -.9150710230     -.2656919669
970626100000    -104957.1114      156176.3987      47676.64436
                -.7823950283     -.5578575800     -.1743285324
970701000000    -57903.24787      173105.3794      53040.64510
                -1.014436161     -.8221816157D-01 -.2842560083D-01
970724140000    -27903.85837     -59665.53317     -18230.18774
                 2.904946552     -.2544706891     -.7774131422D-01
970828070000    -146354.4579      102787.8873      31665.98673
                -.2958925810     -1.023751467     -.3094535217
970901000000    -53313.70138      169331.8870      51513.31641
                -1.073346098      .2679826548D-01  .1188358760D-01
970925220000     41908.14742      121865.5337      36669.54063
                -1.069584079      1.226389831      .3753936172
971001000000     52894.18239      107258.0216      32129.05193
                -.9904752849      1.450826650      .4428056950
971030040000    -139357.2148      14530.68806      5208.479727
                 .6547297012     -1.388500449     -.4228196421
971101000000     59460.67647      99027.87441      29532.16024
                -.9154590831      1.571031571      .4795386027
971127200000    -34681.87266      165900.3052      50268.16352
                -1.144131999      .2025734663      .7036164672D-01
971201000000    -35243.69209     -61681.82073     -18285.25002
                 2.750882414     -.3569010314     -.1304989247
971225210000    -149648.0734      44831.43207      15187.56565
                 .2913371527     -1.296560674     -.3919731900
980101000000    -51803.65878     -57354.97174     -16526.71721
                 2.532178188     -.6779587931     -.2342685427
980201000000    -75111.91246     -51021.92387     -13879.79856
                 2.118883958     -.9651481439     -.3211433198
980226200000    -89870.17467     -45419.25982     -11662.32968
                 1.849609715     -1.077629664     -.3523972181
980323130000    -159438.8211      75986.42386      25523.62305
                -.9828131240D-01 -1.096042106     -.3198008943
980423140000    -159431.3778      74177.18587      25165.76901
                -.1025901189     -1.10574563      -.3222176296
                  Planned elements
980501000000     68466.19675      63457.31326      17164.97015
                -.6184770108      2.111754499      .6333742601
980601000000     69837.97394      45402.49634      11485.98103
                -.3321942741      2.389669982      .7063069921
980701000000    -99844.21093     -42271.86182     -9330.830439
                 1.672579896     -1.111652646     -.3711901329
980801000000    -112448.5507     -35158.01791     -6338.393489
                 1.458128352     -1.155095415     -.3797580941
Please respond to matu@d1.nas.nec.co.jp
To:   len.efron@jpl.nasa.gov, kevin.criddle@jpl.nasa.gov,
      earl.higa@jpl.nasa.gov, Joan.L.Pojman@jpl.nasa.gov,
      john.f.adams-jr@jpl.nasa.gov, istpfds@listserv.gsfc.nasa.gov
cc:   matu@d1.nas.nec.co.jp (bcc: Heather Franz/SSD/CSC)
Subject:  [Weekly] GEOTAIL Latest orbit data(7/17)
To: Dr. L. Efron, Dr. K. Criddle, Dr. E.higa
To:  istpfds@listserv.gsfc.nasa.gov,  john.f.adams-jr@jpl.nasa.gov
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
The following data is updated orbit solution based on
3-path data. (J2000.0EQ orbit elements)
               Best regards,
                 Masatoshi Matsuoka
---------------------------------------------------------
  GEOTAIL STATE VECTOR for JPL FORMAT( Cartesian )
  ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
  ( Unit is UTC, KM, KM/Sec )
ITIM=     '16-Jul-1998 06:00:00.000 UTC',
IC=    -132535.580444,
        -14565.956968,
          -334.167350,
         1.0520352150,
        -1.2510294464,
        -0.3915213342,
  DYNAMIC MODELING PARAMETERS
  ~~~~~~~~~~~~~~~~~~~~~~~~~~~
===========================================================================
====
  (Discriptions)
===========================================================================
====
 S/C cross sectional area for drag cal.  : NOT USE : 4.2170  [m**2]
 Dimensionless drag coefficient          : NOT USE : 0.0000  [ -- ]
 Dimensionless drag scaling parameter    : NOT USE : 00.000  [ -- ]
 S/C cross sectional area for S.R.F. cal.:   USE   : 4.2170  [m**2]
 Dimensionless solar reflectivity coefficient: USE : 1.3220  [ -- ]
 F10.7 solar flux at epoch               :   USE   : 200.00
[1e-22*W/m**2/Hz]
 Dimensionless geomagnetic index         : NOT USE : 000.00  [ -- ]
===========================================================================
====
=======================================================================
  (DATA)    (FREQ.) (STAT.)  (First point[UTC])  -> (Last point[UTC])
=======================================================================
 range       S/S     UDSC     98-07-14 00:16:36  ->  98-07-16 05:16:02
 range rate  S/S     UDSC     98-07-14 00:02:30  ->  98-07-16 05:25:30
=======================================================================
 GEOTAIL STATE VECTOR
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 1998 07 16 06 00 00.0000 [UTC]  S/C MASS : 655.504 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -132535.580444  [km]    Vx:  1.0520352150  [km/s]
             Y:  -14565.956968  [km]    Vy: -1.2510294464  [km/s]
             Z:    -334.167350  [km]    Vz: -0.3915213342  [km/s]
(Keplerian)  a:  126385.974918  [km]    an:   5.776415148  [deg]
             e:  0.542242322160 [ - ]   ap: 308.111539233  [deg]
             i:  16.1666279623  [deg]   ma: 295.089234452  [deg]
ORIGIN OF COORDINATE AND REFERENCE PLANE:
 [ @ ] 1= Geocentric,    Earth equator
 [   ] 2= Heliocentric,  Earth equator
 [   ] 3= Heliocentric,  ecliptic
 [   ] 4= Selenocentric, Earth equator
 [   ] 5= Selenocentric, Moon  equator
COORDINATE SYSTEM:
 [   ] 1= Greenwich true of date rotating
 [   ] 2= Greenwich true of date nonrotating
 [   ] 3= EME50
 [ @ ] 4= EME2000
 [   ] 5= true of date (B1950.0)
 [   ] 6= true of date (J2000.0)
 [   ] 7= Selenographic
VECTOR TYPE:
 [ @ ] 1= Routine on-orbit
 [   ] 2= Special on-orbit update
 [   ] 3= Spare
 [   ] 4= Maneuver ignition
 [   ] 5= Maneuver cut off
 [   ] 6= Reentry
 [   ] 7= Powered flight
 [   ] 8= Stationary

From:	AMES::"matu@d1.nas.nec.co.jp" "Masatoshi Matsuoka" 24-JUL-1998 07:44:59.04
To:	jpl.nasa.gov::stefan.waldherr, jpl.nasa.gov::jose.valencia
CC:	d1.nas.nec.co.jp::matu
Subj:	[Monthly] GEOTAIL Latest Orbit Data(7/24)
To: Waldherr-san, Valencia-san
To: Dr. Sardi
^^^^^^^^^^^^^^~~~~~~~~~~~~~~~~
===================================================
Follow data is change coordinate system from EME50
to J2000.0 EQ.
===================================================
The following data is updated orbit solution based on
3-path data.
Attached orbit elements every one month to the last of this mail.
			Best regards,
				Masatoshi Matsuoka
			(E-mail: matu@d1.nas.nec.co.jp(in office))
			(backup: matu@net203.newslan.isas.ac.jp(in ISAS))
---------------------------------------------------------
 GEOTAIL STATE VECTOR(J2000EQ:GEOCENTRIC COORDINATE)
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 1998 07 22 22 00 00.0000 [UTC]  S/C MASS : 655.504 [kg]
                                                   ~~~~~~~~~~
(Cartesian)  X:   55022.259302  [km]    Vx: -0.9427484016  [km/s]
             Y:   82779.511792  [km]    Vy:  1.8602411966  [km/s]
             Z:   22216.622766  [km]    Vz:  0.5639867976  [km/s]
(Keplerian)  a:  126146.055351  [km]    an:   5.885847567  [deg]
             e:  0.546354006990 [ - ]   ap: 307.740112148  [deg]
             i:  16.1538312325  [deg]   ma:  40.064278705  [deg]
=====================================================================
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
					      ^^^^^^^^^
              EPOCH : 1998/07/22 22:00:00 (UTC)
                  R(KM)                V(KM/S)
               55022.2593022800    -0.9427484015861000
               82779.5117922200     1.8602411965600001
               22216.6227656700     0.5639867976469000
              EPOCH : 1998/08/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -112010.9916514838     1.4728940279232690
              -36415.4833561601    -1.1386678667349523
               -6885.3337852232    -0.3726327950144916
              EPOCH : 1998/09/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -125396.1703894752     1.2452912664746048
              -28140.5912409490    -1.1627622354635827
               -3658.4900704168    -0.3729335201767809
              EPOCH : 1998/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -167760.4470153365    -0.1392313205336155
               73337.3677845155    -1.0263541414519435
               26783.5983533663    -0.2855086209162156
              EPOCH : 1998/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -166889.7003409113    -0.1825918366783869
               75235.9598125775    -1.0208326309095348
               27530.2385335464    -0.2821984347090732
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% Date: Fri, 24 Jul 1998 20:44:53 +0900
% Message-Id: <9807241144.AA15421@ayame.d1.nas.nec.co.jp>
% From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
% To: ncf.span.nasa.gov::sardi
% To: jpl.nasa.gov::stefan.waldherr, jpl.nasa.gov::jose.valencia
% Cc: d1.nas.nec.co.jp::matu
% Subject: [Monthly] GEOTAIL Latest Orbit Data(7/24)
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From:	AMES::"matu@d1.nas.nec.co.jp" "Masatoshi Matsuoka" 17-JUL-1998 13:01:01.06
To:	ncf.span.nasa.gov::sardi
CC:	d1.nas.nec.co.jp::matu
Subj:	Re: [Monthly] Geotail Latest Orbit Data
Dear Dr. sardi
I send Geotail Orbit Elements(monthly data) on June 26.........
Resend same data  the last of this e-mail.
This data is EME50 GEOCENTRIC coordinate.
I will next monthly data on July 24.
The coordinate is changed to J2000.0EQ from next monthly data.
					Best regards,
					   Masatoshi Matsuoka
>>>>> "r" == r parthasarathy,nssdc/wdc-a-r&s <sardi@ncf.span.nasa.gov> writes:
r> Looking into our Geotail collection, I notice that
r> we have not received any more after your email dated 24 April 98. Do you
r> think you could continue this help? We have no problem about the change
r> from EME50 to J2000.  Thanks very much for your help.
r> sardi
r> R. "Sardi" Parthasarathy
------
Return-Path: <matu@net203.newslan.isas.ac.jp>
Date: Sat, 27 Jun 1998 00:05:01 +0900
From: Masatoshi Matsuoka <matu@net203.newslan.isas.ac.jp>
To: sardi@ncf.span.nasa.gov
Cc: matu@d1.nas.nec.co.jp
Reply-To: matu@d1.nas.nec.co.jp
Subject: [Monthly] GEOTAIL Latest Orbit Data(6/26)
Mime-Version: 1.0
Content-Type: text/plain; charset=US-ASCII
Content-Length: 2691
To: Dr. Sardi
^^^^^^^^^^^^^^
The following data is updated orbit solution based on
3-path data.
Attached orbit elements every one month to the last of this mail.
			Best regards,
				Masatoshi Matsuoka
			(E-mail: matu@d1.nas.nec.co.jp(in office))
			(backup: matu@net203.newslan.isas.ac.jp(in ISAS))
---------------------------------------------------------
 GEOTAIL STATE VECTOR(EME-50,GEOCENTRIC-COORDINATE)
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 1998 06 25 13 00 00.0000 [UTC]  S/C MASS : 655.504 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS:
( Cartesian )X: -131715.042901  [km]    Vx:  1.0243218971  [km/s]
             Y:  -10618.523507  [km]    Vy: -1.2862530591  [km/s]
             Z:     641.370524  [km]    Vz: -0.4028622499  [km/s]
(Keplerian)  a:  125866.832029  [km]    an:   5.561347965  [deg]
             e:  0.544811658426 [ - ]   ap: 306.317552152  [deg]
             i: 16.2800171395   [deg]   ma: 295.832267101  [deg]
=====================================================================
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;EME50;GEO-CENTRIC) >>>
              EPOCH : 1998/06/25 13:00:00 (UTC)
                  R(KM)                V(KM/S)
             -131715.0429010000     1.0243218971099999
              -10618.5235069000    -1.2862530591400001
                 641.3705242020    -0.4028622499000001
              EPOCH : 1998/07/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
              -99842.3458051911     1.6726288375644358
              -42271.8218952288    -1.1116323861330368
               -9331.3709407963    -0.3711816685331337
              EPOCH : 1998/08/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -112446.1655800417     1.4581876940803937
              -35158.7650557653    -1.1550725746791863
               -6339.1904562338    -0.3797503455565049
              EPOCH : 1998/09/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -125728.7484909494     1.2302290887133149
              -26731.8362538046    -1.1766035621548567
               -3046.4167440500    -0.3789357269159996
              EPOCH : 1998/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -166800.3481653421    -0.1521713562571646
               75209.9181934389    -1.0246849076211311
               27596.7159617072    -0.2847793831889281
              EPOCH : 1998/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -165903.6845624952    -0.1954871111333344
               77097.9354866683    -1.0186824938898373
               28338.7419161138    -0.2812595351290520
% ====== Internet headers and postmarks (see DECWRL::GATEWAY.DOC) ======
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% Date: Fri, 17 Jul 1998 13:16:53 +0900
% Message-Id: <9807170416.AA05227@ayame.d1.nas.nec.co.jp>
% From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
% To: ncf.span.nasa.gov::sardi
% Cc: d1.nas.nec.co.jp::matu
% In-Reply-To: <199807161522.IAA00790@mg.nsi.net> (sardi@ncf.span.nasa.gov)
% Subject: Re: [Monthly] Geotail Latest Orbit Data
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From:	AMES::"matu@d1.nas.nec.co.jp" "Masatoshi Matsuoka" 28-AUG-1998 07:29:14.95
To:	jpl.nasa.gov::stefan.waldherr, jpl.nasa.gov::jose.valencia
CC:	d1.nas.nec.co.jp::matu
Subj:	[Monthly] GEOTAIL Latest Orbit Data(8/28)
To: Waldherr-san, Valencia-san
To: Dr. Sardi
^^^^^^^^^^^^^^~~~~~~~~~~~~~~~~
The following data is updated orbit solution based on
3-path data.
Attached orbit elements every one month to the last of this mail.
			Best regards,
				Masatoshi Matsuoka
			(E-mail: matu@d1.nas.nec.co.jp(in office))
			(backup: matu@net203.newslan.isas.ac.jp(in ISAS))
---------------------------------------------------------
 GEOTAIL STATE VECTOR(J2000EQ:GEOCENTRIC COORDINATE)
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 1998 08 27 21 00 00.0000 [UTC] S/C MASS : 655.504 [kg]
                                                   ~~~~~~~~~~
(Cartesian)  X:   64499.674870  [km]    Vx:  0.6768522923  [km/s]
             Y:    3619.542645  [km]    Vy:  2.8475746967  [km/s]
             Z:   -1186.253679  [km]    Vz:  0.7853068278  [km/s]
(Keplerian)  a:  126349.178280  [km]    an:   6.893046443  [deg]
             e:  0.542766442799 [ - ]   ap: 310.522727634  [deg]
             i:  15.9609114141  [deg]   ma:  12.270003712  [deg]
====
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 1998/08/27 21:00:00 (UTC)
                  R(KM)                V(KM/S)
               64499.6748696400     0.6768522923467000
                3619.5426453540     2.8475746966830000
               -1186.2536789550     0.7853068278027000
              EPOCH : 1998/09/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -125404.0300444560     1.2451860486597834
              -28138.8187370686    -1.1627334177140676
               -3658.8439793931    -0.3729016973673931
              EPOCH : 1998/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -167764.5244982436    -0.1392333026874613
               73334.2866127447    -1.0263333735376210
               26780.6928399403    -0.2854972262414144
              EPOCH : 1998/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -166893.9362467496    -0.1825856860749385
               75231.7792525536    -1.0208173702064127
               27527.0285667714    -0.2821888600846592
% ====== Internet headers and postmarks (see DECWRL::GATEWAY.DOC) ======
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% Date: Fri, 28 Aug 1998 20:28:56 +0900
% Message-Id: <199808281128.UAA08280@ayame.d1.nas.nec.co.jp>
% From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
% To: ncf.span.nasa.gov::sardi
% To: jpl.nasa.gov::stefan.waldherr, jpl.nasa.gov::jose.valencia
% Cc: d1.nas.nec.co.jp::matu
% Subject: [Monthly] GEOTAIL Latest Orbit Data(8/28)
% Mime-Version: 1.0
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From:	AMES::"matu@d1.nas.nec.co.jp" "Masatoshi Matsuoka" 23-OCT-1998 05:43:07.98
To:	csc.com::hfranz
CC:	d1.nas.nec.co.jp::matu
Subj:	[Monthly] GEOTAIL Latest Orbit Data(10/23)
The following data is updated orbit solution based
 on 3 path data.(DV maneuver data included)
We execute DV-maneuver on 10/18 at 9:00UT. (about 1.2m/s)
After DV maneuver, SC weight is 655.017 kg.
Best regards,
			Masatoshi Matsuoka
-----
  GEOTAIL STATE VECTOR for JPL FORMAT( Cartesian )
  ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
  ( Unit is UTC, KM, KM/Sec )
ITIM=	'22-Oct-1998 04:00:00.000 UTC',
IC=    -164103.924824,
         26963.875218,
         13676.896381,
         0.3486328740,
        -1.1779966922,
        -0.3461541410,
  DYNAMIC MODELING PARAMETERS
  ~~~~~~~~~~~~~~~~~~~~~~~~~~~
===============================================================================
  (Discriptions)
===============================================================================
 S/C cross sectional area for drag cal.  : NOT USE : 4.2170  [m**2]
 Dimensionless drag coefficient          : NOT USE : 0.0000  [ -- ]
 Dimensionless drag scaling parameter    : NOT USE : 00.000  [ -- ]
 S/C cross sectional area for S.R.F. cal.:   USE   : 4.2170  [m**2]
 Dimensionless solar reflectivity coefficient: USE : 1.3220  [ -- ]
 F10.7 solar flux at epoch               :   USE   : 200.00  [1e-22*W/m**2/Hz]
 Dimensionless geomagnetic index         : NOT USE : 000.00  [ -- ]
===============================================================================
=======================================================================
  (DATA)    (FREQ.) (STAT.)  (First point[UTC])  -> (Last point[UTC])
=======================================================================
 range       S/S     UDSC     98-10-19 15:24:16  ->  98-10-22 03:15:47
 range rate  S/S     UDSC     98-10-19 15:00:30  ->  98-10-22 03:25:30
=======================================================================
 GEOTAIL STATE VECTOR
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 1998 10 22 04 00 00.0000 [UTC]  S/C MASS : 655.504 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -164103.924824  [km]    Vx:  0.3486328740  [km/s]
             Y:   26963.875218  [km]    Vy: -1.1779966922  [km/s]
             Z:   13676.896381  [km]    Vz: -0.3461541410  [km/s]
(Keplerian)  a:  126602.021504  [km]    an:   7.420843295  [deg]
             e:  0.524559359674 [ - ]   ap: 311.709875532  [deg]
             i:  15.9251994123  [deg]   ma: 256.579456977  [deg]
RIGIN OF COORDINATE AND REFERENCE PLANE:
 [ @ ] 1= Geocentric,    Earth equator
 [   ] 2= Heliocentric,  Earth equator
 [   ] 3= Heliocentric,  ecliptic
 [   ] 4= Selenocentric, Earth equator
 [   ] 5= Selenocentric, Moon  equator
COORDINATE SYSTEM:
 [   ] 1= Greenwich true of date rotating
 [   ] 2= Greenwich true of date nonrotating
 [   ] 3= EME50
 [ @ ] 4= EME2000
 [   ] 5= true of date (B1950.0)
 [   ] 6= true of date (J2000.0)
 [   ] 7= Selenographic
VECTOR TYPE:
 [ @ ] 1= Routine on-orbit
 [   ] 2= Special on-orbit update
 [   ] 3= Spare
 [   ] 4= Maneuver ignition
 [   ] 5= Maneuver cut off
 [   ] 6= Reentry
 [   ] 7= Powered flight
 [   ] 8= Stationary
=====
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 1998/10/22 04:00:00 (UTC)
                  R(KM)                V(KM/S)
             -164103.9248244000     0.3486328739792000
               26963.8752183900    -1.1779966922480001
               13676.8963814800    -0.3461541410122000
              EPOCH : 1998/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -166522.0909012324    -0.2225565332313001
               79515.6884919814    -0.9996775776787369
               28722.3009656265    -0.2747417212629504
              EPOCH : 1998/12/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
              -98322.6119678065    -1.0418416374684625
              149130.4510275833    -0.2894260379523370
               46059.4644173390    -0.0397352776671313
              EPOCH : 1999/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
              -86278.8304690682    -1.1086983372282224
              152554.3858726213    -0.1472404388413603
               46575.0421535129     0.0090121943970104
              EPOCH : 1999/02/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
              -78662.2234578588    -1.1632751655033187
              151989.8999569704    -0.0508550606438207
               45866.0966080847     0.0431990277035393
% ====== Internet headers and postmarks (see DECWRL::GATEWAY.DOC) ======
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% Received: by ayame.d1.nas.nec.co.jp (SMI-8.6/3.4Wbeta5) id SAA08279; Fri, 23 Oct 1998 18:42:51 +090
% Date: Fri, 23 Oct 1998 18:42:51 +0900
% Message-Id: <199810230942.SAA08279@ayame.d1.nas.nec.co.jp>
% From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
% To: ncf.span.nasa.gov::sardi
% To: jpl.nasa.gov::stefan.waldherr, jpl.nasa.gov::jose.valencia
% To: csc.com::hfranz
% Cc: d1.nas.nec.co.jp::matu
% Subject: [Monthly] GEOTAIL Latest Orbit Data(10/23)
% Mime-Version: 1.0
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From:	AMES::"matu@d1.nas.nec.co.jp" "Masatoshi Matsuoka" 27-NOV-1998 04:23:21.24
To:	csc.com::hfranz
CC:	d1.nas.nec.co.jp::matu
Subj:	[Monthly] GEOTAIL Latest Orbit Data(11/27)
The following data is updated orbit solution based
 on 3 path data.
Best regards,
			Masatoshi Matsuoka(matu@d1.nas.nec.co.jp)
==
 GEOTAIL STATE VECTOR
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 1998 11 26 22 00 00.0000 [UTC]  S/C MASS : 655.504 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -165024.895104  [km]    Vx: -0.2851936009  [km/s]
             Y:   85798.488241  [km]    Vy: -0.9666553380  [km/s]
             Z:   30829.914062  [km]    Vz: -0.2614544378  [km/s]
(Keplerian)  a:  126769.105527  [km]    an:   8.075663395  [deg]
             e:  0.524962963887 [ - ]   ap: 311.086150548  [deg]
             i:  15.9137898788  [deg]   ma: 213.056014447  [deg]
=======
       <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 1998/11/26 22:00:00 (UTC)
                  R(KM)                V(KM/S)
       X     -165024.8951044000    -0.2851936008809000
       Y       85798.4882408000    -0.9666553379743000
       Z       30829.9140615200    -0.2614544378346000
              EPOCH : 1998/12/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
              -98320.8783845109    -1.0418640951901483
              149127.9489900977    -0.2894684741963401
               46058.6013929629    -0.0397445817641774
              EPOCH : 1999/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
              -86278.5749215878    -1.1087135335713625
              152552.2078403555    -0.1472968983039445
               46574.3591421458     0.0089983606500025
              EPOCH : 1999/02/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
              -78663.0612135076    -1.1632846501342691
              151988.3083533658    -0.0509230994619007
               45865.6715100533     0.0431815555351659
              EPOCH : 1999/03/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -173628.6679565991     0.2575071004631999
               31877.6920100749    -1.0901325019025465
               17873.8694310293    -0.3104730472576567
              EPOCH : 1999/04/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -176411.9647095202     0.1132552837979275
               41587.0086057190    -1.0610280088979831
               20876.8763636268    -0.2946330141193896
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% Received: by ayame.d1.nas.nec.co.jp (SMI-8.6/3.4Wbeta5) id SAA20819; Fri, 27 Nov 1998 18:23:48 +090
% Date: Fri, 27 Nov 1998 18:23:48 +0900
% Message-Id: <199811270923.SAA20819@ayame.d1.nas.nec.co.jp>
% From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
% To: ncf.span.nasa.gov::sardi
% To: jpl.nasa.gov::stefan.waldherr, jpl.nasa.gov::jose.valencia
% To: csc.com::hfranz
% Cc: d1.nas.nec.co.jp::matu
% Subject: [Monthly] GEOTAIL Latest Orbit Data(11/27)
% Mime-Version: 1.0 (generated by tm-edit 7.106)
% Content-Type: text/plain; charset=US-ASCII

From:	AMES::"matu@d1.nas.nec.co.jp" "Masatoshi Matsuoka" 25-DEC-1998 04:18:57.71
To:	csc.com::hfranz
CC:	d1.nas.nec.co.jp::matu
Subj:	[Monthly] GEOTAIL Latest Orbit Data(12/25)
The following data is updated orbit solution based on
3-path data.
Attached orbit elements every one month to the last of this mail.
I wish you a Merry Christmas and a Happy New Year!
			Best regards,
				Masatoshi Matsuoka
			(E-mail: matu@d1.nas.nec.co.jp(in office))
---------------------------------------------------------
 GEOTAIL STATE VECTOR
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 1998 12 23 22 00 00.0000 [UTC]  S/C MASS : 655.504 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -144819.545878  [km]    Vx:  0.8907304671  [km/s]
             Y:  -11651.286396  [km]    Vy: -1.1847998009  [km/s]
             Z:    3128.826735  [km]    Vz: -0.3710641400  [km/s]
(Keplerian)  a:  126501.819585  [km]    an:   8.956835246  [deg]
             e:  0.539083744483 [ - ]   ap: 310.665972259  [deg]
             i:  15.8261708311  [deg]   ma: 283.668373087  [deg]
RIGIN OF COORDINATE AND REFERENCE PLANE:
 [ @ ] 1= Geocentric,    Earth equator
 [   ] 2= Heliocentric,  Earth equator
 [   ] 3= Heliocentric,  ecliptic
 [   ] 4= Selenocentric, Earth equator
 [   ] 5= Selenocentric, Moon  equator
COORDINATE SYSTEM:
 [   ] 1= Greenwich true of date rotating
 [   ] 2= Greenwich true of date nonrotating
 [   ] 3= EME50
 [ @ ] 4= EME2000
 [   ] 5= true of date (B1950.0)
 [   ] 6= true of date (J2000.0)
 [   ] 7= Selenographic
VECTOR TYPE:
 [ @ ] 1= Routine on-orbit
 [   ] 2= Special on-orbit update
 [   ] 3= Spare
 [   ] 4= Maneuver ignition
 [   ] 5= Maneuver cut off
 [   ] 6= Reentry
 [   ] 7= Powered flight
 [   ] 8= Stationary
==
   <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 1998/12/23 22:00:00 (UTC)
                  R(KM)                V(KM/S)
             -144819.5458780000     0.8907304671361000
              -11651.2863957000    -1.1847998009050000
                3128.8267353630    -0.3710641399863000
              EPOCH : 1999/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
              -86271.5898224555    -1.1087423420830518
              152552.9328654141    -0.1472795141741827
               46575.9692373514     0.0090026320650926
              EPOCH : 1999/02/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
              -78653.3078603960    -1.1633225833498364
              151989.0059135459    -0.0508785350632679
               45867.1476625561     0.0431942524797548
              EPOCH : 1999/03/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -173626.9066355908     0.2574547350708813
               31880.4188893832    -1.0901547762370007
               17874.6786336214    -0.3104900030836084
              EPOCH : 1999/04/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -176409.8675219867     0.1131671919556104
               41593.3597851221    -1.0610388406552871
               20878.7420756734    -0.2946447574881907
% ====== Internet headers and postmarks (see DECWRL::GATEWAY.DOC) ======
% Received: Fri, 25 Dec 1998 01:15:29 -0800 from TYO203.gate.nec.co.jp by mg.nsi.net (8.9.0/1.3) with ESMTP
% Received: from mailsv.nec.co.jp (mailsv-le1 [192.168.1.90]) by TYO203.gate.nec.co.jp (8.9.1a/3.7W98121813) with ESMTP id SAA19899; Fri, 25 Dec 1998 18:20:12 +0900 (JS
% Received: from india.d1.nas.nec.co.jp (india.d1.nas.nec.co.jp [10.52.9.1]) by mailsv.nec.co.jp (8.9.1a/3.7W-MAILSV-NEC) with SMTP id SAA19713; Fri, 25 Dec 1998 18:20:11 +0900 (JST
% Received: from ayame.d1.nas.nec.co.jp by india.d1.nas.nec.co.jp (SMI-8.6/6.4JAIN-NAS-d1-1.3) id SAA19495; Fri, 25 Dec 1998 18:13:39 +090
% Received: by ayame.d1.nas.nec.co.jp (SMI-8.6/3.4Wbeta5) id SAA00379; Fri, 25 Dec 1998 18:20:08 +090
% Date: Fri, 25 Dec 1998 18:20:08 +0900
% Message-Id: <199812250920.SAA00379@ayame.d1.nas.nec.co.jp>
% From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
% To: ncf.span.nasa.gov::sardi
% To: jpl.nasa.gov::stefan.waldherr, jpl.nasa.gov::jose.valencia
% To: csc.com::hfranz
% Cc: d1.nas.nec.co.jp::matu
% Subject: [Monthly] GEOTAIL Latest Orbit Data(12/25)
% Mime-Version: 1.0 (generated by tm-edit 7.106)
% Content-Type: text/plain; charset=US-ASCII

From:	AMES::"matu@d1.nas.nec.co.jp" "Masatoshi Matsuoka" 29-JAN-1999 06:41:14.91
To:	csc.com::hfranz
CC:	d1.nas.nec.co.jp::matu
Subj:	[Monthly] GEOTAIL Latest Orbit Data(1/29)
The following data is updated orbit solution based on
3-path data. We executed attitude maneuver on Jan 26
(at 10:00 utc). After attitude maneuver, SC weight is
654.917kg.
Attached orbit elements every one month to the last of this mail.
			Best regards,
				Masatoshi Matsuoka
			(E-mail: matu@d1.nas.nec.co.jp)
==
 GEOTAIL STATE VECTOR
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 1999 01 28 21 00 00.0000 [UTC]  S/C MASS : 654.917 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -166085.505835  [km]    Vx:  0.3824063525  [km/s]
             Y:   25663.310202  [km]    Vy: -1.1444062454  [km/s]
             Z:   15201.297217  [km]    Vz: -0.3350011367  [km/s]
(Keplerian)  a:  126289.918453  [km]    an:  10.015161599  [deg]
             e:  0.551074097393 [ - ]   ap: 310.866834942  [deg]
             i:  15.6791520393  [deg]   ma: 257.430351113  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 1999/01/28 21:00:00 (UTC)
                  R(KM)                V(KM/S)
             -166085.5058350000     0.3824063525054000
               25663.3102024300    -1.1444062453740000
               15201.2972173200    -0.3350011366958000
              EPOCH : 1999/02/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
              -78657.5256728291    -1.1632625537208110
              151991.7420957299    -0.0509739196952565
               45866.8982183420     0.0431624020640268
              EPOCH : 1999/03/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -173608.6490101967     0.2579987117946700
               31834.9634169662    -1.0903091265359073
               17860.7524110667    -0.3105527519714410
              EPOCH : 1999/04/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -176393.6125990544     0.1140985868233876
               41510.2914644479    -1.0613193970538803
               20854.6438101712    -0.2947644450239202
              EPOCH : 1999/05/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -137307.4915406731    -0.8237525720591180
              124665.5466938838    -0.5910229137654954
               41652.0242471504    -0.1151243043768270
------- foward message -------------------------------------------
The following data is updated orbit solution based on
3-path data.
Attached orbit elements every one month to the last of this mail.
			Best regards,
				Masatoshi Matsuoka
			(E-mail: matu@d1.nas.nec.co.jp)
==
==
  GEOTAIL STATE VECTOR for JPL FORMAT( Cartesian )
  ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
  ( Unit is UTC, KM, KM/Sec )
ITIM=	'27-Apr-1999 14:00:00.000 UTC',
IC=    -149280.749092,
        -21871.558078,
          2349.432890,
         0.8962068606,
        -1.1028793414,
        -0.3504388694,
  DYNAMIC MODELING PARAMETERS
  ~~~~~~~~~~~~~~~~~~~~~~~~~~~
===============================================================================
  (Discriptions)
===============================================================================
 S/C cross sectional area for drag cal.  : NOT USE : 4.2170  [m**2]
 Dimensionless drag coefficient          : NOT USE : 0.0000  [ -- ]
 Dimensionless drag scaling parameter    : NOT USE : 00.000  [ -- ]
 S/C cross sectional area for S.R.F. cal.:   USE   : 4.2170  [m**2]
 Dimensionless solar reflectivity coefficient: USE : 1.3220  [ -- ]
 F10.7 solar flux at epoch               :   USE   : 200.00  [1e-22*W/m**2/Hz]
 Dimensionless geomagnetic index         : NOT USE : 000.00  [ -- ]
===============================================================================
=======================================================================
  (DATA)    (FREQ.) (STAT.)  (First point[UTC])  -> (Last point[UTC])
=======================================================================
 range       S/S     UDSC     99-04-24 06:55:02  ->  99-04-27 13:35:26
 range rate  S/S     UDSC     99-04-24 06:32:30  ->  99-04-27 13:41:30
=======================================================================
 GEOTAIL STATE VECTOR
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 1999 04 27 14 00 00.0000 [UTC]  S/C MASS : 654.917 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -149280.749092  [km]    Vx:  0.8962068606  [km/s]
             Y:  -21871.558078  [km]    Vy: -1.1028793414  [km/s]
             Z:    2349.432890  [km]    Vz: -0.3504388694  [km/s]
(Keplerian)  a:  126906.805523  [km]    an:  11.544714386  [deg]
             e:  0.526356285014 [ - ]   ap: 314.801285863  [deg]
             i:  15.5434932437  [deg]   ma: 277.102882538  [deg]
RIGIN OF COORDINATE AND REFERENCE PLANE:
 [ @ ] 1= Geocentric,    Earth equator
 [   ] 2= Heliocentric,  Earth equator
 [   ] 3= Heliocentric,  ecliptic
 [   ] 4= Selenocentric, Earth equator
 [   ] 5= Selenocentric, Moon  equator
COORDINATE SYSTEM:
 [   ] 1= Greenwich true of date rotating
 [   ] 2= Greenwich true of date nonrotating
 [   ] 3= EME50
 [ @ ] 4= EME2000
 [   ] 5= true of date (B1950.0)
 [   ] 6= true of date (J2000.0)
 [   ] 7= Selenographic
VECTOR TYPE:
 [ @ ] 1= Routine on-orbit
 [   ] 2= Special on-orbit update
 [   ] 3= Spare
 [   ] 4= Maneuver ignition
 [   ] 5= Maneuver cut off
 [   ] 6= Reentry
 [   ] 7= Powered flight
 [   ] 8= Stationary
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 1999/04/27 14:00:00 (UTC)
                  R(KM)                V(KM/S)
             -149280.7490918000     0.8962068606238000
              -21871.5580783100    -1.1028793413930000
                2349.4328897750    -0.3504388693866000
              EPOCH : 1999/05/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -137301.1045249201    -0.8237348142263734
              124681.4649050949    -0.5909403531571857
               41653.0274478543    -0.1150988081287263
              EPOCH : 1999/06/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -124147.8657201431    -0.9386359862730519
              132960.0557889145    -0.4807854225104943
               43489.7100664334    -0.0754749113708513
              EPOCH : 1999/07/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
                1323.4952686999    -1.4741554939135211
              123020.4499070225     0.9077654756403560
               33005.8195753125     0.3375461625150198

From:	SMTP%"hfranz@csc.com" 16-FEB-2000 10:20:30.61
To:	SARDI
CC:
Subj:	[Monthly] GEOTAIL Latest Orbit Data(6/25)
X-Lotus-FromDomain: CSC
From: hfranz@csc.com
To: sardi@nssdca.gsfc.nasa.gov
Message-ID: <85256887.00527C93.00@csc.com>
Date: Wed, 16 Feb 2000 10:00:46 -0500
Subject: [Monthly] GEOTAIL Latest Orbit Data(6/25)
Mime-Version: 1.0
Content-type: text/plain; charset=us-ascii
Content-Disposition: inline
---------------------- Forwarded by Heather Franz/CIV/CSC on 02/16/2000 09:55 AM
---------------------------
matu@d1.nas.nec.co.jp on 06/25/99 10:41:18 AM
To:   sardi@ncf.span.nasa.gov, stefan.waldherr@jpl.nasa.gov,
      jose.valencia@jpl.nasa.gov, Heather Franz/CIV/CSC,
      FERRIER@nssdca.gsfc.nasa.gov
cc:   matu@d1.nas.nec.co.jp
Subject:  [Monthly] GEOTAIL Latest Orbit Data(6/25)
The following data is updated orbit solution
based on 3 path data.
Best regards,
==
NEC Aerospace Systems,Ltd
                 Masatoshi Matsuoka
                 matu@d1.nas.nec.co.jp
--
  GEOTAIL STATE VECTOR for JPL FORMAT( Cartesian )
  ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
  ( Unit is UTC, KM, KM/Sec )
ITIM=     '24-Jun-1999 20:00:00.000 UTC',
IC=      27404.489657,
        -53386.651366,
        -16103.161038,
         2.4937590539,
         1.8306356745,
         0.3368893854,
  DYNAMIC MODELING PARAMETERS
  ~~~~~~~~~~~~~~~~~~~~~~~~~~~
===============================================================================
  (Discriptions)
===============================================================================
 S/C cross sectional area for drag cal.  : NOT USE : 4.2170  [m**2]
 Dimensionless drag coefficient          : NOT USE : 0.0000  [ -- ]
 Dimensionless drag scaling parameter    : NOT USE : 00.000  [ -- ]
 S/C cross sectional area for S.R.F. cal.:   USE   : 4.2170  [m**2]
 Dimensionless solar reflectivity coefficient: USE : 1.3220  [ -- ]
 F10.7 solar flux at epoch               :   USE   : 200.00  [1e-22*W/m**2/Hz]
 Dimensionless geomagnetic index         : NOT USE : 000.00  [ -- ]
===============================================================================
=======================================================================
  (DATA)    (FREQ.) (STAT.)  (First point[UTC])  -> (Last point[UTC])
=======================================================================
 range       S/S     UDSC     99-06-22 01:11:31  ->  99-06-24 19:19:47
 range rate  S/S     UDSC     99-06-22 01:00:30  ->  99-06-24 19:36:30
=======================================================================
 GEOTAIL STATE VECTOR
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 1999 06 24 20 00 00.0000 [UTC]  S/C MASS : 654.917 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:   27404.489657  [km]    Vx:  2.4937590539  [km/s]
             Y:  -53386.651366  [km]    Vy:  1.8306356745  [km/s]
             Z:  -16103.161038  [km]    Vz:  0.3368893854  [km/s]
(Keplerian)  a:  126656.639835  [km]    an:  13.100313746  [deg]
             e:  0.532485362857 [ - ]   ap: 313.721373722  [deg]
             i:  15.4638636319  [deg]   ma: 351.960351100  [deg]
RIGIN OF COORDINATE AND REFERENCE PLANE:
 [ @ ] 1= Geocentric,    Earth equator
 [   ] 2= Heliocentric,  Earth equator
 [   ] 3= Heliocentric,  ecliptic
 [   ] 4= Selenocentric, Earth equator
 [   ] 5= Selenocentric, Moon  equator
COORDINATE SYSTEM:
 [   ] 1= Greenwich true of date rotating
 [   ] 2= Greenwich true of date nonrotating
 [   ] 3= EME50
 [ @ ] 4= EME2000
 [   ] 5= true of date (B1950.0)
 [   ] 6= true of date (J2000.0)
 [   ] 7= Selenographic
VECTOR TYPE:
 [ @ ] 1= Routine on-orbit
 [   ] 2= Special on-orbit update
 [   ] 3= Spare
 [   ] 4= Maneuver ignition
 [   ] 5= Maneuver cut off
 [   ] 6= Reentry
 [   ] 7= Powered flight
 [   ] 8= Stationary
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 1999/06/24 20:00:00 (UTC)
                  R(KM)                V(KM/S)
               27404.4896567600     2.4937590539349999
              -53386.6513655600     1.8306356744660000
              -16103.1610378900     0.3368893854097000
              EPOCH : 1999/07/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
                1318.0276348595    -1.4741580556807234
              123021.6275368300     0.9077089865686897
               33008.7674934192     0.3375507437378745
              EPOCH : 1999/08/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
               14372.7915331505    -1.4809330424789520
              110284.5948428321     1.1932737181693294
               28309.6126282420     0.4164757614741601
              EPOCH : 1999/09/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
               38709.9946308732    -1.3476864856309085
               83132.9716308857     1.7958980893698600
               19207.5535721281     0.5669941087347343
              EPOCH : 1999/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
              -94689.5471381356     1.7685113663800349
              -69069.5403990595    -0.6412114680369356
              -11419.0761797389    -0.2947538685737059
              EPOCH : 2000/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
             -182214.0596469779    -0.1439921765522321
               52965.4757122789    -0.9625781645605903
               28645.5226553743    -0.2386928341048419

From:	SMTP%"hfranz@csc.com" 16-FEB-2000 09:59:31.52
To:	SARDI
CC:
Subj:	[Monthly] GEOTAIL Latest Orbit Data(7/30)
X-Lotus-FromDomain: CSC
From: hfranz@csc.com
To: sardi@nssdca.gsfc.nasa.gov
Message-ID: <85256887.00528754.00@csc.com>
Date: Wed, 16 Feb 2000 10:01:14 -0500
Subject: [Monthly] GEOTAIL Latest Orbit Data(7/30)
Mime-Version: 1.0
Content-type: text/plain; charset=us-ascii
Content-Disposition: inline
---------------------- Forwarded by Heather Franz/CIV/CSC on 02/16/2000 09:56 AM
---------------------------
matu@d1.nas.nec.co.jp on 07/30/99 05:54:35 AM
To:   sardi@ncf.span.nasa.gov, stefan.waldherr@jpl.nasa.gov,
      jose.valencia@jpl.nasa.gov, Heather Franz/CIV/CSC,
      FERRIER@nssdca.gsfc.nasa.gov
cc:   matu@d1.nas.nec.co.jp
Subject:  [Monthly] GEOTAIL Latest Orbit Data(7/30)
The following data is updated orbit solution
based on 3 path data.
Best regards,
==
NEC Aerospace Systems,Ltd
                 Masatoshi Matsuoka
                 matu@d1.nas.nec.co.jp
--
 GEOTAIL STATE VECTOR(J2000.0EQ GEO CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 1999 07 29 06 00 00.0000 [UTC]  S/C MASS : 654.917 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -179073.779827  [km]    Vx: -0.0614619441  [km/s]
             Y:   56678.456195  [km]    Vy: -0.9902871537  [km/s]
             Z:   27113.381570  [km]    Vz: -0.2589567920  [km/s]
(Keplerian)  a:  126570.457395  [km]    an:  14.219136963  [deg]
             e:  0.550693957041 [ - ]   ap: 313.708764094  [deg]
             i:  15.3267823691  [deg]   ma: 218.233495139  [deg]
              EPOCH : 1999/07/29 06:00:00 (UTC)
                  R(KM)                V(KM/S)
             -179073.7798269000    -0.0614619440672100
               56678.4561947200    -0.9902871536955000
               27113.3815701800    -0.2589567920332000
              EPOCH : 1999/08/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
               14372.1253905781    -1.4809438238210437
              110283.8406880362     1.1932816841380645
               28308.9213312332     0.4164870317851314
              EPOCH : 1999/09/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
               38711.7828251135    -1.3476638726211816
               83128.9353223974     1.7959878255785213
               19205.7645498786     0.5670217996393809
              EPOCH : 1999/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)
              -94697.8635463013     1.7684048716421221
              -69066.9733367061    -0.6412736235148507
              -11416.8292779320    -0.2947756394585940

From:	SMTP%"hfranz@csc.com" 16-FEB-2000 09:59:49.30
To:	SARDI
CC:
Subj:	[Monthly] GEOTAIL Latest Orbit Data(8/27)
X-Lotus-FromDomain: CSC
From: hfranz@csc.com
To: sardi@nssdca.gsfc.nasa.gov
Message-ID: <85256887.00529135.00@csc.com>
Date: Wed, 16 Feb 2000 10:01:40 -0500
Subject: [Monthly] GEOTAIL Latest Orbit Data(8/27)
Mime-Version: 1.0
Content-type: text/plain; charset=us-ascii
Content-Disposition: inline
---------------------- Forwarded by Heather Franz/CIV/CSC on 02/16/2000 09:57 AM
---------------------------
matu@d1.nas.nec.co.jp on 08/27/99 07:41:56 AM
To:   sardi@ncf.span.nasa.gov, stefan.waldherr@jpl.nasa.gov,
      jose.valencia@jpl.nasa.gov, Heather Franz/CIV/CSC@CSC,
      FERRIER@nssdca.gsfc.nasa.gov
cc:   matu@d1.nas.nec.co.jp
Subject:  [Monthly] GEOTAIL Latest Orbit Data(8/27)
The following data is updated orbit solution
based on 3 path data.
We will be planning next DV on Oct. 27. (about 0.75m/s)
Its purpose is eclipse start time change.(eclipse on next winter)
Best regards,
==
NEC Aerospace Systems,Ltd
                 Masatoshi Matsuoka
                 matu@d1.nas.nec.co.jp
--
 GEOTAIL STATE VECTOR(J2000.0EQ:GEO CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 1999 08 26 20 00 00.0000 [UTC]  S/C MASS : 654.917 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:   33073.272878  [km]    Vx: -1.4051782643  [km/s]
             Y:   90132.145356  [km]    Vy:  1.6423509953  [km/s]
             Z:   21440.735640  [km]    Vz:  0.5303080985  [km/s]
(Keplerian)  a:  126509.859985  [km]    an:  14.789221412  [deg]
             e:  0.549859630621 [ - ]   ap: 315.241495402  [deg]
             i:  15.2389007589  [deg]   ma:  37.329248409  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 1999/08/26 20:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
               33073.2728775600    -1.4051782642849999    0.0000000000000000
               90132.1453560900     1.6423509952510000    0.0000000000000000
               21440.7356396400     0.5303080985010000    0.0000000000000000
              EPOCH : 1999/09/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
               38709.9521214787    -1.3476997870198715    0.0000000000000000
               83129.9497958064     1.7959616246576726    0.0000000000000000
               19206.5196512819     0.5669951935636464    0.0000000000000000
              EPOCH : 1999/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
              -94695.7657752747     1.7684338222142038    0.0000000000000000
              -69068.2450587733    -0.6412433257824663    0.0000000000000000
              -11418.3646302641    -0.2947442035971555    0.0000000000000000
              EPOCH : 1999/10/22 12:53:28 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
               52156.9442799988     1.4534371041796454    0.0003370521499224
              -24579.2359144661     2.8185382515826314    0.0006536191862741
              -10276.9831423541     0.6349021819726980    0.0001472338533322
              EPOCH : 1999/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
             -118930.7016344239     1.4380134118733252    0.0000000000000000
              -58288.9260947654    -0.8277543969018609   -0.0000000000000000
               -6486.2734703003    -0.3244911084521494    0.0000000000000000

From:	SMTP%"hfranz@csc.com" 16-FEB-2000 10:00:25.76
To:	SARDI
CC:
Subj:	[Monthly] GEOTAIL Latest Orbit Data(10/01)
X-Lotus-FromDomain: CSC
From: hfranz@csc.com
To: sardi@nssdca.gsfc.nasa.gov
Message-ID: <85256887.00529CCD.00@csc.com>
Date: Wed, 16 Feb 2000 10:02:09 -0500
Subject: [Monthly] GEOTAIL Latest Orbit Data(10/01)
Mime-Version: 1.0
Content-type: text/plain; charset=us-ascii
Content-Disposition: inline
---------------------- Forwarded by Heather Franz/CIV/CSC on 02/16/2000 09:57 AM
---------------------------
matu@d1.nas.nec.co.jp on 10/03/99 10:04:39 AM
To:   sardi@ncf.span.nasa.gov, stefan.waldherr@jpl.nasa.gov,
      jose.valencia@jpl.nasa.gov, Heather Franz/CIV/CSC@CSC,
      FERRIER@nssdca.gsfc.nasa.gov
cc:   matu@d1.nas.nec.co.jp
Subject:  [Monthly] GEOTAIL Latest Orbit Data(10/01)
The following data is updated orbit solution
based on 3 path data.
We will be planning next DV on Oct. 22. (about 0.76m/s)
Its purpose is eclipse start time change.(eclipse on next winter)
Best regards,
==
NEC Aerospace Systems,Ltd
                 Masatoshi Matsuoka
                 matu@d1.nas.nec.co.jp
--
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 1999/09/30 05:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
     X:      -170382.0837587000     0.5538921647400999    0.0000000000000000
     Y:        -5112.5381738350    -1.0559590693670000    0.0000000000000000
     Z:        10796.0754213100    -0.3170686727022000    0.0000000000000000
              EPOCH : 1999/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
              -94694.8430001265     1.7684382222553701    0.0000000000000000
              -69069.8434441794    -0.6412174085488236   -0.0000000000000000
              -11417.7998517875    -0.2947611363500793    0.0000000000000000
              EPOCH : 1999/10/22 12:53:28 (UTC)
                  R(KM)              V(KM/S)=pre-DV=         DV(KM/S)
               52156.6300602233     1.4534568241881800    0.0003517929223928
              -24580.2052293450     2.8185199027993444    0.0006187645258989
              -10277.9207894127     0.6348854498872206    0.0002664060833454
              EPOCH : 1999/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
             -118929.6522626079     1.4380267002818359    0.0000000000000000
              -58289.5499531694    -0.8277359322336789   -0.0000000000000000
               -6489.4916002066    -0.3245121363049182    0.0000000000000000
              EPOCH : 1999/12/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
             -182572.9442141713    -0.0360813339676075    0.0000000000000000
               43661.8778211241    -1.0035835828206550    0.0000000000000000
               25577.6540157757    -0.2615762471806082    0.0000000000000000
              EPOCH : 2000/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
             -179449.3542731727    -0.2858906266224348    0.0000000000000000
               66352.5293385251    -0.9152771830574199    0.0000000000000000
               31903.5281878539    -0.2149480634894784    0.0000000000000000

From:	SMTP%"hfranz@csc.com" 16-FEB-2000 10:00:38.51
To:	SARDI
CC:
Subj:	[Monthly] GEOTAIL Latest Orbit Data(10/29)
X-Lotus-FromDomain: CSC
From: hfranz@csc.com
To: sardi@nssdca.gsfc.nasa.gov
Message-ID: <85256887.0052A504.00@csc.com>
Date: Wed, 16 Feb 2000 10:02:30 -0500
Subject: [Monthly] GEOTAIL Latest Orbit Data(10/29)
Mime-Version: 1.0
Content-type: text/plain; charset=us-ascii
Content-Disposition: inline
---------------------- Forwarded by Heather Franz/CIV/CSC on 02/16/2000 09:58 AM
---------------------------
matu@d1.nas.nec.co.jp on 10/29/99 03:39:33 AM
To:   sardi@ncf.span.nasa.gov, stefan.waldherr@jpl.nasa.gov,
      jose.valencia@jpl.nasa.gov, Heather Franz/CIV/CSC@CSC,
      FERRIER@nssdca.gsfc.nasa.gov
cc:   matu@d1.nas.nec.co.jp
Subject:  [Monthly] GEOTAIL Latest Orbit Data(10/29)
The following data is updated orbit solution
based on 3 path data.(post DV24 data)
Best regards,
==
NEC Aerospace Systems,Ltd
                 Masatoshi Matsuoka
                 matu@d1.nas.nec.co.jp
=
 GEOTAIL STATE VECTOR
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 1999 10 28 21 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:  -48396.740964  [km]    Vx: -1.4684710550  [km/s]
             Y:  133970.206270  [km]    Vy:  0.2689644141  [km/s]
             Z:   38891.757592  [km]    Vz:  0.1787913471  [km/s]
(Keplerian)  a:  127013.204067  [km]    an:  15.558703695  [deg]
             e:  0.532324410349 [ - ]   ap: 318.051746937  [deg]
             i:  15.3125305935  [deg]   ma:  78.735138283  [deg]
RIGIN OF COORDINATE AND REFERENCE PLANE:
 [ @ ] 1= Geocentric,    Earth equator
 [   ] 2= Heliocentric,  Earth equator
 [   ] 3= Heliocentric,  ecliptic
 [   ] 4= Selenocentric, Earth equator
 [   ] 5= Selenocentric, Moon  equator
COORDINATE SYSTEM:
 [   ] 1= Greenwich true of date rotating
 [   ] 2= Greenwich true of date nonrotating
 [   ] 3= EME50
 [ @ ] 4= EME2000
 [   ] 5= true of date (B1950.0)
 [   ] 6= true of date (J2000.0)
 [   ] 7= Selenographic
VECTOR TYPE:
 [ @ ] 1= Routine on-orbit
 [   ] 2= Special on-orbit update
 [   ] 3= Spare
 [   ] 4= Maneuver ignition
 [   ] 5= Maneuver cut off
 [   ] 6= Reentry
 [   ] 7= Powered flight
 [   ] 8= Stationary
 <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000.0EQ;GEO-CENTRIC) >>>
        EPOCH : 1999/10/28 21:00:00 (UTC)
(Cartesian)  X:  -48396.740964  [km]    Vx: -1.4684710550  [km/s]
             Y:  133970.206270  [km]    Vy:  0.2689644141  [km/s]
             Z:   38891.757592  [km]    Vz:  0.1787913471  [km/s]
        EPOCH : 1999/11/01 00:00:00 (UTC)
(Cartesian)  X: -118869.626618  [km]    Vx:  1.4388332009  [km/s]
             Y:  -58322.653619  [km]    Vy: -0.8273672342  [km/s]
             Z:   -6504.961756  [km]    Vz: -0.3244327975  [km/s]
        EPOCH : 1999/12/01 00:00:00 (UTC)
(Cartesian)  X: -182572.615070  [km]    Vx: -0.0345488234  [km/s]
             Y:   43512.595100  [km]    Vy: -1.0039908907  [km/s]
             Z:   25533.555650  [km]    Vz: -0.2617908097  [km/s]
        EPOCH : 2000/01/01 00:00:00 (UTC)
(Cartesian)  X: -179519.502132  [km]    Vx: -0.2833091439  [km/s]
             Y:   66108.452701  [km]    Vy: -0.9162476365  [km/s]
             Z:   31840.828588  [km]    Vz: -0.2154039101  [km/s]

From:	SMTP%"hfranz@csc.com" 16-FEB-2000 10:01:30.58
To:	SARDI
CC:
Subj:	[Monthly] GEOTAIL Latest Orbit Data(11/26)
X-Lotus-FromDomain: CSC
From: hfranz@csc.com
To: sardi@nssdca.gsfc.nasa.gov
Message-ID: <85256887.0052AFEE.00@csc.com>
Date: Wed, 16 Feb 2000 10:02:59 -0500
Subject: [Monthly] GEOTAIL Latest Orbit Data(11/26)
Mime-Version: 1.0
Content-type: text/plain; charset=us-ascii
Content-Disposition: inline
---------------------- Forwarded by Heather Franz/CIV/CSC on 02/16/2000 09:58 AM
---------------------------
matu@d1.nas.nec.co.jp on 11/26/99 06:48:06 AM
To:   sardi@ncf.span.nasa.gov, stefan.waldherr@jpl.nasa.gov,
      jose.valencia@jpl.nasa.gov, Heather Franz/CIV/CSC@CSC,
      FERRIER@nssdca.gsfc.nasa.gov
cc:   matu@d1.nas.nec.co.jp
Subject:  [Monthly] GEOTAIL Latest Orbit Data(11/26)
The following data is updated orbit solution
based on 3 path data.
Best regards,
==
NEC Aerospace Systems,Ltd
                 Masatoshi Matsuoka
                 matu@d1.nas.nec.co.jp
=
 GEOTAIL STATE VECTOR(J2000.0EQ)
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 1999 11 24 22 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -149808.827675  [km]    Vx: -0.7674824089  [km/s]
             Y:  109740.984047  [km]    Vy: -0.6634718121  [km/s]
             Z:   40391.553064  [km]    Vz: -0.1167657307  [km/s]
(Keplerian)  a:  126462.181898  [km]    an:  16.086992712  [deg]
             e:  0.529730103567 [ - ]   ap: 316.920844000  [deg]
             i:  15.3685867978  [deg]   ma: 152.089803368  [deg]
====
 <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000.0EQ;GEO-CENTRIC) >>>
        EPOCH : 1999/11/24 22:00:00 (UTC)
(Cartesian)  X: -149808.827675  [km]    Vx: -0.7674824089  [km/s]
             Y:  109740.984047  [km]    Vy: -0.6634718121  [km/s]
             Z:   40391.553064  [km]    Vz: -0.1167657307  [km/s]
        EPOCH : 1999/12/01 00:00:00 (UTC)
(Cartesian)  X: -182569.726439  [km]    Vx: -0.0345454178  [km/s]
             Y:   43513.365822  [km]    Vy: -1.0040055825  [km/s]
             Z:   25538.240597  [km]    Vz: -0.2618077656  [km/s]
        EPOCH : 2000/01/01 00:00:00 (UTC)
(Cartesian)  X: -179496.994407  [km]    Vx: -0.2835556341  [km/s]
             Y:   66152.352621  [km]    Vy: -0.9162043491  [km/s]
             Z:   31867.551997  [km]    Vz: -0.2153401581  [km/s]
        EPOCH : 2000/02/01 00:00:00 (UTC)
(Cartesian)  X: -173640.233520  [km]    Vx: -0.4790466712  [km/s]
             Y:   84088.525970  [km]    Vy: -0.8097390485  [km/s]
             Z:   36511.792920  [km]    Vz: -0.1666270576  [km/s]

From:	SMTP%"hfranz@csc.com" 16-FEB-2000 10:01:40.24
To:	SARDI
CC:
Subj:	[Monthly] GEOTAIL Latest Orbit Data(12/24)
X-Lotus-FromDomain: CSC
From: hfranz@csc.com
To: sardi@nssdca.gsfc.nasa.gov
Message-ID: <85256887.0052BD92.00@csc.com>
Date: Wed, 16 Feb 2000 10:03:18 -0500
Subject: [Monthly] GEOTAIL Latest Orbit Data(12/24)
Mime-Version: 1.0
Content-type: text/plain; charset=us-ascii
Content-Disposition: inline
---------------------- Forwarded by Heather Franz/CIV/CSC on 02/16/2000 09:59 AM
---------------------------
matu@net203.newslan.isas.ac.jp on 12/24/99 01:09:27 AM
To:   sardi@ncf.span.nasa.gov, stefan.waldherr@jpl.nasa.gov,
      jose.valencia@jpl.nasa.gov, Heather Franz/CIV/CSC@CSC,
      FERRIER@ndadsb-f.gsfc.nasa.gov
cc:   matu@d1.nas.nec.co.jp
Subject:  [Monthly] GEOTAIL Latest Orbit Data(12/24)
The following data is updated orbit solution
based on 3 path data.
Best regards,
==
NEC Aerospace Systems,Ltd
                 Masatoshi Matsuoka
                 matu@d1.nas.nec.co.jp
-
 GEOTAIL STATE VECTOR
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 1999 12 21 20 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -181664.213493  [km]    Vx: -0.0365793794  [km/s]
             Y:   44267.722053  [km]    Vy: -1.0031620547  [km/s]
             Z:   26005.932740  [km]    Vz: -0.2608925597  [km/s]
(Keplerian)  a:  126653.358643  [km]    an:  16.737517813  [deg]
             e:  0.529076710241 [ - ]   ap: 316.331929922  [deg]
             i:  15.3542391651  [deg]   ma: 213.367690708  [deg]
 <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000.0EQ;GEO-CENTRIC) >>>
        EPOCH : 1999/12/21 20:00:00 (UTC)
(Cartesian)  X: -181664.213493  [km]    Vx: -0.0365793794  [km/s]
             Y:   44267.722053  [km]    Vy: -1.0031620547  [km/s]
             Z:   26005.932740  [km]    Vz: -0.2608925597  [km/s]
        EPOCH : 2000/01/01 00:00:00 (UTC)
(Cartesian)  X: -179512.857094  [km]    Vx: -0.2833286793  [km/s]
             Y:   66114.620375  [km]    Vy: -0.9162688538  [km/s]
             Z:   31850.352313  [km]    Vz: -0.2154026608  [km/s]
        EPOCH : 2000/02/01 00:00:00 (UTC)
(Cartesian)  X: -173662.529384  [km]    Vx: -0.4787899002  [km/s]
             Y:   84048.569720  [km]    Vy: -0.8098754970  [km/s]
             Z:   36495.103727  [km]    Vz: -0.1667202794  [km/s]
        EPOCH : 2000/03/01 00:00:00 (UTC)
(Cartesian)  X:   50552.758524  [km]    Vx: -1.0818702050  [km/s]
             Y:   53601.240695  [km]    Vy:  2.4302948824  [km/s]
             Z:    9266.473748  [km]    Vz:  0.7164188819  [km/s]
        EPOCH : 2000/04/01 00:00:00 (UTC)
(Cartesian)  X:   50404.592576  [km]    Vx:  1.4397792749  [km/s]
             Y:  -26593.401496  [km]    Vy:  2.8532576126  [km/s]
             Z:  -11321.532474  [km]    Vz:  0.6037138898  [km/s]

From:	SMTP%"hfranz@csc.com" 16-FEB-2000 10:02:28.59
To:	SARDI
CC:
Subj:	[Monthly] GEOTAIL Latest Orbit Data(1/28)
X-Lotus-FromDomain: CSC
From: hfranz@csc.com
To: sardi@nssdca.gsfc.nasa.gov
Message-ID: <85256887.0052C1C7.00@csc.com>
Date: Wed, 16 Feb 2000 10:03:43 -0500
Subject: [Monthly] GEOTAIL Latest Orbit Data(1/28)
Mime-Version: 1.0
Content-type: text/plain; charset=us-ascii
Content-Disposition: inline
---------------------- Forwarded by Heather Franz/CIV/CSC on 02/16/2000 09:59 AM
---------------------------
matu@d1.nas.nec.co.jp on 01/28/2000 01:48:19 AM
To:   sardi@ncf.span.nasa.gov, stefan.waldherr@jpl.nasa.gov,
      jose.valencia@jpl.nasa.gov, Heather Franz/CIV/CSC@CSC,
      FERRIER@ndadsb-f.gsfc.nasa.gov
cc:   matu@d1.nas.nec.co.jp
Subject:  [Monthly] GEOTAIL Latest Orbit Data(1/28)
The following data is updated orbit solution
based on 3 path data.
Best regards,
==
NEC Aerospace Systems,Ltd
                 Masatoshi Matsuoka
                 matu@d1.nas.nec.co.jp
-
 GEOTAIL STATE VECTOR(J2000.0EQ)
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2000 01 27 22 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -173128.041204  [km]    Vx:  0.5539363428  [km/s]
             Y:   -8107.069096  [km]    Vy: -1.0195963126  [km/s]
             Z:   12703.691122  [km]    Vz: -0.3089826594  [km/s]
(Keplerian)  a:  126722.835941  [km]    an:  18.403943034  [deg]
             e:  0.551252144767 [ - ]   ap: 317.021488242  [deg]
             i:  15.1354000055  [deg]   ma: 250.991236413  [deg]
 <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000.0EQ;GEO-CENTRIC) >>>
        EPOCH : 2000/01/27 22:00:00 (UTC)
(Cartesian)  X: -173128.041204  [km]    Vx:  0.5539363428  [km/s]
             Y:   -8107.069096  [km]    Vy: -1.0195963126  [km/s]
             Z:   12703.691122  [km]    Vz: -0.3089826594  [km/s]
        EPOCH : 2000/02/01 00:00:00 (UTC)
(Cartesian)  X: -173690.233269  [km]    Vx: -0.4785223705  [km/s]
             Y:   83998.426912  [km]    Vy: -0.8100201478  [km/s]
             Z:   36476.506074  [km]    Vz: -0.1668267795  [km/s]
        EPOCH : 2000/03/01 00:00:00 (UTC)
(Cartesian)  X:   50548.402022  [km]    Vx: -1.0821438234  [km/s]
             Y:   53593.136735  [km]    Vy:  2.4304166549  [km/s]
             Z:    9268.851443  [km]    Vz:  0.7164626772  [km/s]
        EPOCH : 2000/04/01 00:00:00 (UTC)
(Cartesian)  X:   50375.615386  [km]    Vx:  1.4415836918  [km/s]
             Y:  -26652.868948  [km]    Vy:  2.8522390274  [km/s]
             Z:  -11331.784191  [km]    Vz:  0.6034232197  [km/s]

From:	SMTP%"hfranz@csc.com" 16-FEB-2000 10:03:54.13
To:	SARDI
CC:
Subj:	Re: Geotail elements
X-Lotus-FromDomain: CSC
From: hfranz@csc.com
To: SARDI@nssdca.gsfc.nasa.gov
Message-ID: <85256887.0052EF99.00@csc.com>
Date: Wed, 16 Feb 2000 10:05:42 -0500
Subject: Re: Geotail elements
Mime-Version: 1.0
Content-type: text/plain; charset=us-ascii
Content-Disposition: inline
Sardi,
I've forwarded to you all Geotail monthly element sets since May 1999. It looks
like both you and Frank were in the distribution list for the original messages,
so maybe Mr. Matsuoka has an incorrect e-mail address for you.
Heather
SARDI@nssdca.gsfc.nasa.gov on 02/16/2000 08:50:06 AM
To:   Heather Franz/CIV/CSC@CSC
cc:   SARDI@nssdca.gsfc.nasa.gov
Subject:  Geotail elements
Dear Heather, As you may have known, we used to store in an FTP site the
orb elemnts of Geotail and many others. A Russian colleague of mine has
alerted me that the site carries Geotail elements only up to May 99. Looks like
Masutoshi Matsuoka (Matu@d1.nas.nec.co.jp) forgot to include my name
since May 99!
If you have received sets after May 99, could you transmit them to me?
Many thanx,
sardi
---------------

From:	SMTP%"matu@d1.nas.nec.co.jp" 23-FEB-2000 06:03:40.43
To:	SARDI
CC:
Subj:	Re: Geotail Elements
To: SARDI@nssdca.gsfc.nasa.gov
CC: matu@d1.nas.nec.co.jp
Subject: Re: Geotail Elements
X-Mailer: Mew version 1.94.1 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20000223200603I.matu@d1.nas.nec.co.jp>
Date: Wed, 23 Feb 2000 20:06:03 +0900 (JST)
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
X-Dispatcher: imput version 990905(IM130)
Lines: 17
Dear Dr. Sardi
I apologazed that not quickly response.
I send updated elements to "sardi@ncf.span.nasa.gov" in last year
and this january.
I change your address to "SARDI@nssdca.gsfc.nasa.gov"
from the next distribution(perhaps this weekend) .
Best regards,
Masatosi
==
NEC Aerospace Systems,Ltd
Masatoshi Matsuoka

From:	SMTP%"matu@d1.nas.nec.co.jp" 25-FEB-2000 06:07:24.48
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL Latest Orbit Data(2/25)
To: SARDI@nssdca.gsfc.nasa.gov, stefan.waldherr@jpl.nasa.gov,
        jose.valencia@jpl.nasa.gov, hfranz@csc.com,
        FERRIER@nssdca.gsfc.nasa.gov
CC: matu@d1.nas.nec.co.jp
Subject: [MONTHLY] GEOTAIL Latest Orbit Data(2/25)
X-Mailer: Mew version 1.94.1 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
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Message-Id: <20000225200951C.matu@d1.nas.nec.co.jp>
Date: Fri, 25 Feb 2000 20:09:51 +0900 (JST)
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
X-Dispatcher: imput version 990905(IM130)
Lines: 70
The following data is updated orbit solution
based on 3 path data.
GEOTAIL survive the longest eclipse(Feb. 21) in this season.
The next eclipse seaon start on June 3.
Best regards,
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
-
 GEOTAIL STATE VECTOR
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2000 02 23 22 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:  -64579.923567  [km]    Vx:  2.1132219202  [km/s]
             Y:  -79479.223708  [km]    Vy: -0.2042324164  [km/s]
             Z:  -14676.837658  [km]    Vz: -0.2369919347  [km/s]
(Keplerian)  a:  126854.082490  [km]    an:  18.877248291  [deg]
             e:  0.551040931412 [ - ]   ap: 318.322327923  [deg]
             i:  15.1224797409  [deg]   ma: 319.307816473  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2000/02/23 22:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -64579.9235672970     2.1132219201885998    0.0000000000000000
      Y:     -79479.2237079450    -0.2042324164141900    0.0000000000000000
      Z:     -14676.8376576800    -0.2369919347179200    0.0000000000000000
              EPOCH : 2000/03/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      50535.7663861721    -1.0827747180945251    0.0000000000000000
      Y:      53604.8282230864     2.4301232303228812    0.0000000000000000
      Z:       9279.1944772004     0.7164025121963487    0.0000000000000000
              EPOCH : 2000/04/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      50354.5470083164     1.4428538847143442    0.0000000000000000
      Y:     -26695.8495470231     2.8515209384223414    0.0000000000000000
      Z:     -11336.6919724865     0.6033154633573529    0.0000000000000000
              EPOCH : 2000/05/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -152459.3378483584     0.9687763119604939    0.0000000000000000
      Y:     -47774.2606547474    -0.8990093616893475   -0.0000000000000000
      Z:       1567.8113994270    -0.3203899329910120    0.0000000000000000
              EPOCH : 2000/06/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -165534.0786320254     0.7381808655591339    0.0000000000000000
      Y:     -32688.5135982581    -0.9646919852796298   -0.0000000000000000
      Z:       7150.3181899096    -0.3193975107998843    0.0000000000000000
Date: Fri, 26 May 2000 15:41:33 +0900
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
X-Dispatcher: imput version 20000228(IM140)
Lines: 60
The following data is updated orbit solution
based on 3 path data.
Best regards,
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
-
 GEOTAIL STATE VECTOR(J2000.0EQ GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2000 05 25 14 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -177672.577796  [km]    Vx: -0.4450592736  [km/s]
             Y:   69568.147760  [km]    Vy: -0.8576838050  [km/s]
             Z:   34675.506384  [km]    Vz: -0.1800011254  [km/s]
(Keplerian)  a:  126756.242023  [km]    an:  19.958394987  [deg]
             e:  0.533187936455 [ - ]   ap: 321.102319420  [deg]
             i:  15.3828137685  [deg]   ma: 170.337236124  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2000/05/25 14:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -177672.5777963500    -0.4450592736050900    0.0000000000000000
      Y:      69568.1477602230    -0.8576838050045700    0.0000000000000000
      Z:      34675.5063842400    -0.1800011253597900    0.0000000000000000
              EPOCH : 2000/06/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -165444.7203934217     0.7402724152370578    0.0000000000000000
      Y:     -32898.2230994869    -0.9638620955318317   -0.0000000000000000
      Z:       7045.7882209187    -0.3192958160587813    0.0000000000000000
              EPOCH : 2000/07/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -178203.1166074168    -0.4202099953155641    0.0000000000000000
      Y:      68238.5955734169    -0.8647577694454093    0.0000000000000000
      Z:      35068.4154299961    -0.1817844572346023    0.0000000000000000
              EPOCH : 2000/08/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -166734.9402774003    -0.6769593884577420    0.0000000000000000
      Y:      88038.5943908276    -0.7395811162445709    0.0000000000000000
      Z:      39441.9079346983    -0.1194516350567001    0.0000000000000000

From:	SMTP%"matu@d1.nas.nec.co.jp" 30-JUN-2000 02:58:54.32
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL Latest Orbit Data(2000/6)@hanako.d1.nas.nec.co.jp
To: gtl_month@ayame.d1.nas.nec.co.jp
Subject: [MONTHLY] GEOTAIL Latest Orbit Data(2000/6)@hanako.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.28 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20000630160026B.matu@d1.nas.nec.co.jp>
Date: Fri, 30 Jun 2000 16:00:26 +0900
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
X-Dispatcher: imput version 20000228(IM140)
Lines: 65
The following data is updated orbit solution
based on 3 path data.
Best regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
-
 GEOTAIL STATE VECTOR(J2000.0EQ Geo centric)
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2000 06 29 07 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:  -16026.268566  [km]    Vx: -1.6895826205  [km/s]
             Y:  115241.332844  [km]    Vy:  0.7062637285  [km/s]
             Z:   31324.704435  [km]    Vz:  0.3471259292  [km/s]
(Keplerian)  a:  126856.087094  [km]    an:  20.681937028  [deg]
             e:  0.533089316038 [ - ]   ap: 320.153076447  [deg]
             i:  15.4321591323  [deg]   ma:  54.192901048  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2000/06/29 07:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -16026.2685661920    -1.6895826205180000    0.0000000000000000
      Y:     115241.3328441500     0.7062637284708200    0.0000000000000000
      Z:      31324.7044346450     0.3471259291507900    0.0000000000000000
              EPOCH : 2000/07/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -178230.2082027560    -0.4199024855768000    0.0000000000000000
      Y:      68183.9645378976    -0.8648797428720826    0.0000000000000000
      Z:      35041.5034502900    -0.1818816754309352    0.0000000000000000
              EPOCH : 2000/08/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -166767.5121746208    -0.6767173574459242    0.0000000000000000
      Y:      87990.2830864244    -0.7397563906435861    0.0000000000000000
      Z:      39418.1845145209    -0.1195731585832706    0.0000000000000000
              EPOCH : 2000/09/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -155265.3300107649    -0.8425608695798874    0.0000000000000000
      Y:      95438.7820766874    -0.6340770083477916    0.0000000000000000
      Z:      40216.1075317566    -0.0716613245000603    0.0000000000000000
              EPOCH : 2000/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -12018.1272230547    -1.8194428555958930    0.0000000000000000
      Y:     105134.8189803709     0.8168626092326485    0.0000000000000000
      Z:      28198.1739244996     0.4014350206395152    0.0000000000000000

From:	SMTP%"matu@d1.nas.nec.co.jp" 28-JUL-2000 08:54:18.04
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL Latest Orbit Data(2000/7)
To: gtl_month@ayame.d1.nas.nec.co.jp
Subject: [MONTHLY] GEOTAIL Latest Orbit Data(2000/7)
X-Mailer: Mew version 1.94.2 on Emacs 19.28 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20000728215807M.matu@d1.nas.nec.co.jp>
Date: Fri, 28 Jul 2000 21:58:07 +0900
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
X-Dispatcher: imput version 20000228(IM140)
Lines: 65
The following data is updated orbit solution
based on 3 path data.
Best regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
-
 GEOTAIL STATE VECTOR(J2000.0EQ)
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2000 07 23 13 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -126132.061569  [km]    Vx:  1.3384702286  [km/s]
             Y:  -67861.885495  [km]    Vy: -0.7286557322  [km/s]
             Z:   -4751.108949  [km]    Vz: -0.3205646898  [km/s]
(Keplerian)  a:  127037.614298  [km]    an:  21.351520333  [deg]
             e:  0.539160088581 [ - ]   ap: 320.697379306  [deg]
             i:  15.3727812602  [deg]   ma: 286.265877023  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2000/07/23 13:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -126132.0615694900     1.3384702285554999    0.0000000000000000
      Y:     -67861.8854951020    -0.7286557321839900    0.0000000000000000
      Z:      -4751.1089493680    -0.3205646897885200    0.0000000000000000
              EPOCH : 2000/08/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -166793.9512368931    -0.6764694418656109    0.0000000000000000
      Y:      87953.1999213346    -0.7399100926319286    0.0000000000000000
      Z:      39404.3581487753    -0.1196900991014213    0.0000000000000000
              EPOCH : 2000/09/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -155308.1370518884    -0.8421786577153415    0.0000000000000000
      Y:      95397.1473126282    -0.6343564578683484    0.0000000000000000
      Z:      40203.5319948237    -0.0718304815562822    0.0000000000000000
              EPOCH : 2000/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -12089.5823790962    -1.8195092646967186    0.0000000000000000
      Y:     105154.5190039808     0.8156683387476464    0.0000000000000000
      Z:      28211.8561225323     0.4010510942268438    0.0000000000000000
              EPOCH : 2000/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      37576.2702376218    -1.5955728523851911    0.0000000000000000
      Y:      67797.3663458333     1.9924794340142529    0.0000000000000000
      Z:      13585.7334302363     0.6896713613950787    0.0000000000000000

From:	SMTP%"matu@d1.nas.nec.co.jp" 25-AUG-2000 01:55:20.11
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/08)
To: gtl_month@ayame.d1.nas.nec.co.jp
Reply-to: matu@d1.nas.nec.co.jp
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/08)
X-Mailer: Mew version 1.94.2 on Emacs 20.7 / Mule 4.0
 =?iso-2022-jp?B?KBskQjJWMWMbKEIp?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20000825145833W.matu@d1.nas.nec.co.jp>
Date: Fri, 25 Aug 2000 14:58:33 +0900
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
X-Dispatcher: imput version 20000228(IM140)
Lines: 49
The following data is updated orbit solution
based on 3 path data.
Best regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
 GEOTAIL STATE VECTOR(J2000.0EQ GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2000 08 24 14 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:   -3517.711469  [km]    Vx:  2.4436499169  [km/s]
             Y:  -75550.246522  [km]    Vy:  1.0562299802  [km/s]
             Z:  -18804.391963  [km]    Vz:  0.0164735823  [km/s]
(Keplerian)  a:  126871.372042  [km]    an:  22.080493147  [deg]
             e:  0.551698322793 [ - ]   ap: 322.142877539  [deg]
             i:  15.3107167629  [deg]   ma: 336.959092697  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2000/09/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -155345.0570315008    -0.8419495568748547    0.0000000000000000
      Y:      95354.6991883666    -0.6345751085568405    0.0000000000000000
      Z:      40185.9613697864    -0.0720030369350585    0.0000000000000000
              EPOCH : 2000/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -12046.4811327411    -1.8199348668338988    0.0000000000000000
      Y:     105116.1140742100     0.8165106832364836    0.0000000000000000
      Z:      28199.0804069839     0.4011740803618901    0.0000000000000000
              EPOCH : 2000/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      37700.4222046518    -1.5934186092103138    0.0000000000000000
      Y:      67624.2450642905     1.9971017824172499    0.0000000000000000
      Z:      13532.0439286193     0.6905454073462305    0.0000000000000000

From:	SMTP%"matu@d1.nas.nec.co.jp" 29-SEP-2000 07:34:24.31
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/09/29)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/09/29)
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.28 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20000929204023M.matu@d1.nas.nec.co.jp>
Date: Fri, 29 Sep 2000 20:40:23 +0900
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
X-Dispatcher: imput version 20000228(IM140)
Lines: 48
The following data is updated orbit solution
based on 3 path data.
Best regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
 GEOTAIL STATE VECTOR J2000.0EQ
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2000 09 25 22 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:  -39207.066878  [km]    Vx: -1.7158720540  [km/s]
             Y:  114254.276297  [km]    Vy:  0.4266028008  [km/s]
             Z:   33151.801988  [km]    Vz:  0.2888693738  [km/s]
(Keplerian)  a:  126352.316025  [km]    an:  22.490283244  [deg]
             e:  0.559697508677 [ - ]   ap: 323.277602952  [deg]
             i:  15.3749942612  [deg]   ma:  57.051170811  [deg]
 <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000.0EQ;GEO-CENTRIC) >>>
        EPOCH : 2000/10/01 00:00:00 (UTC)
(Cartesian)  X:  -12153.727136  [km]    Vx: -1.8201695983  [km/s]
             Y:  105138.215381  [km]    Vy:  0.8146963081  [km/s]
             Z:   28218.981363  [km]    Vz:  0.4006051892  [km/s]
        EPOCH : 2000/11/01 00:00:00 (UTC)
(Cartesian)  X:   37570.322587  [km]    Vx: -1.5962624399  [km/s]
             Y:   67761.482667  [km]    Vy:  1.9929970589  [km/s]
             Z:   13587.164982  [km]    Vz:  0.6897094371  [km/s]
        EPOCH : 2000/12/01 00:00:00 (UTC)
(Cartesian)  X:  -98012.567240  [km]    Vx:  1.6196900980  [km/s]
             Y:  -88328.847715  [km]    Vy: -0.4066979539  [km/s]
             Z:  -12241.541033  [km]    Vz: -0.2854274707  [km/s]
        EPOCH : 2001/01/01 00:00:00 (UTC)
(Cartesian)  X: -122474.516939  [km]    Vx:  1.3597014809  [km/s]
             Y:  -78789.029567  [km]    Vy: -0.6099927723  [km/s]
             Z:   -6513.779652  [km]    Vz: -0.3144177263  [km/s]

From:	SMTP%"matu@d1.nas.nec.co.jp" 28-OCT-2000 03:46:56.99
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/10/28)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/10/28)
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.28 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20001028165512H.matu@d1.nas.nec.co.jp>
Date: Sat, 28 Oct 2000 16:55:12 +0900
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
X-Dispatcher: imput version 20000228(IM140)
Lines: 65
The following data is updated orbit solution
based on 3 path data.
Best regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
 GEOTAIL STATE VECTOR(J2000.0EQ GEO CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2000 10 26 14 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:   57888.155011  [km]    Vx: -0.4501396236  [km/s]
             Y:   20755.391067  [km]    Vy:  2.9903790446  [km/s]
             Z:    -811.515787  [km]    Vz:  0.8227183447  [km/s]
(Keplerian)  a:  126928.335469  [km]    an:  22.424109842  [deg]
             e:  0.538874195377 [ - ]   ap: 326.739198463  [deg]
             i:  15.6539327312  [deg]   ma:   7.949714780  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC)>>>
              EPOCH : 2000/10/26 14:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      57888.1550110470    -0.4501396236334300    0.0000000000000000
      Y:      20755.3910673410     2.9903790446309002    0.0000000000000000
      Z:       -811.5157872424     0.8227183447002100    0.0000000000000000
              EPOCH : 2000/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      37555.6838862227    -1.5967655096362259    0.0000000000000000
      Y:      67763.9902856239     1.9927586420378196    0.0000000000000000
      Z:      13593.5378430966     0.6896272654166792    0.0000000000000000
              EPOCH : 2000/12/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -98122.5781249820     1.6184593854261726    0.0000000000000000
      Y:     -88320.5864301659    -0.4074910298909200   -0.0000000000000000
      Z:     -12236.0875268722    -0.2853881338284940    0.0000000000000000
              EPOCH : 2001/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -122669.2836982022     1.3574235520302611    0.0000000000000000
      Y:     -78724.6646694285    -0.6112107421066895   -0.0000000000000000
      Z:      -6485.1952530096    -0.3143853315531645    0.0000000000000000
              EPOCH : 2001/02/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -147368.3030592013     1.0596491315544585    0.0000000000000000
      Y:     -66182.6482833296    -0.7547694051174465   -0.0000000000000000
      Z:        -15.8263456787    -0.3202808456137621    0.0000000000000000

From:	SMTP%"matu@d1.nas.nec.co.jp" 24-NOV-2000 01:35:52.46
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/11/24)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/11/24)
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20001124154239H.matu@d1.nas.nec.co.jp>
Date: Fri, 24 Nov 2000 15:42:39 +0900
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
X-Dispatcher: imput version 20000228(IM140)
Lines: 56
The following data is updated orbit solution
based on 3 path data.
Best regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
 GEOTAIL STATE VECTOR(J2000.0EQ GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2000 11 22 21 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -108270.499191  [km]    Vx: -1.3116329423  [km/s]
             Y:  109915.209210  [km]    Vy: -0.3514581349  [km/s]
             Z:   40474.759345  [km]    Vz:  0.0522905715  [km/s]
(Keplerian)  a:  126487.270969  [km]    an:  22.837409154  [deg]
             e:  0.537484895763 [ - ]   ap: 326.756274149  [deg]
             i:  15.7700565757  [deg]   ma:  92.136787886  [deg]
         <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC)>>>
              EPOCH : 2000/11/22 21:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -108270.4991906800    -1.3116329423234001    0.0000000000000000
      Y:     109915.2092098000    -0.3514581349018800    0.0000000000000000
      Z:      40474.7593446920     0.0522905715020210    0.0000000000000000
              EPOCH : 2000/12/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -97914.6395304702     1.6205004375616885    0.0000000000000000
      Y:     -88386.5938778840    -0.4054338206792317   -0.0000000000000000
      Z:     -12285.9871002636    -0.2849829046664799    0.0000000000000000
              EPOCH : 2001/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -122379.3567022445     1.3606955504258467    0.0000000000000000
      Y:     -78870.6711594872    -0.6089650754610271   -0.0000000000000000
      Z:      -6567.7370644962    -0.3141043559833094    0.0000000000000000
              EPOCH : 2001/02/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -147084.4712708795     1.0633102017413949    0.0000000000000000
      Y:     -66404.6197707129    -0.7530157205685637   -0.0000000000000000
      Z:       -119.4089614638    -0.3202060309669246    0.0000000000000000

From:	SMTP%"matu@d1.nas.nec.co.jp" 22-DEC-2000 00:31:02.65
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/12/22)
To: gtl_month@ayame.d1.nas.nec.co.jp
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/12/22)
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20001222143810P.matu@d1.nas.nec.co.jp>
Date: Fri, 22 Dec 2000 14:38:10 +0900
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
X-Dispatcher: imput version 20000228(IM140)
Lines: 56
The following data is updated orbit solution
based on 3 path data.
This update is the last data in this year.
Merry Xmas and a happy new millennium.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
 GEOTAIL STATE VECTOR(J2000.0EQ GEO centric)
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2000 12 20 22 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -177901.973711  [km]    Vx:  0.5526232646  [km/s]
             Y:  -31806.182065  [km]    Vy: -0.9272061796  [km/s]
             Z:   11779.409753  [km]    Vz: -0.3041149844  [km/s]
(Keplerian)  a:  126771.256206  [km]    an:  23.399303609  [deg]
             e:  0.536143114055 [ - ]   ap: 325.439996473  [deg]
             i:  15.8602880369  [deg]   ma: 235.379303618  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2000/12/20 22:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -177901.9737112200     0.5526232645969600    0.0000000000000000
      Y:     -31806.1820652060    -0.9272061795555300    0.0000000000000000
      Z:      11779.4097533230    -0.3041149844461800    0.0000000000000000
              EPOCH : 2001/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -122341.7887655387     1.3610716639697471    0.0000000000000000
      Y:     -78910.7258429261    -0.6084834627152037   -0.0000000000000000
      Z:      -6595.7530348898    -0.3139288246124629    0.0000000000000000
              EPOCH : 2001/02/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -147043.6456928062     1.0638605616306531    0.0000000000000000
      Y:     -66485.1680474847    -0.7524150686794925   -0.0000000000000000
      Z:       -173.6107897305    -0.3199911821514207    0.0000000000000000
              EPOCH : 2001/03/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:       3703.4544375961    -1.9349284728264726    0.0000000000000000
      Y:      90877.3251328459     1.1516049577696952    0.0000000000000000
      Z:      23295.4620891984     0.5296154977050683    0.0000000000000000

From:	SMTP%"matu@d1.nas.nec.co.jp" 26-JAN-2001 07:22:48.77
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/01/26)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/01/26)
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20010126213449A.matu@d1.nas.nec.co.jp>
Date: Fri, 26 Jan 2001 21:34:49 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 107
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
 GEOTAIL STATE VECTOR(J2000.0EQ)
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2001 01 25 21 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -191759.270086  [km]    Vx:  0.1193769981  [km/s]
             Y:    4797.972269  [km]    Vy: -0.9498225982  [km/s]
             Z:   23603.070470  [km]    Vz: -0.2613020009  [km/s]
(Keplerian)  a:  126934.849149  [km]    an:  24.111539873  [deg]
             e:  0.543511165749 [ - ]   ap: 324.852750044  [deg]
             i:  15.9261788664  [deg]   ma: 204.522927645  [deg]
------
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2001/01/25 21:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -191759.2700857000     0.1193769980987800    0.0000000000000000
      Y:       4797.9722693602    -0.9498225981833500    0.0000000000000000
      Z:      23603.0704702840    -0.2613020009311900    0.0000000000000000
              EPOCH : 2001/02/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -147042.6260562211     1.0638639340322678    0.0000000000000000
      Y:     -66485.0561954937    -0.7524289520365113   -0.0000000000000000
      Z:       -173.4159335023    -0.3199938289275155    0.0000000000000000
              EPOCH : 2001/03/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:       3706.8452433258    -1.9349022897327812    0.0000000000000000
      Y:      90877.2307053570     1.1516508613841534    0.0000000000000000
      Z:      23294.7806473035     0.5296225648491727    0.0000000000000000
              EPOCH : 2001/04/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      38889.8496212090    -1.6162585975451182    0.0000000000000000
      Y:      56441.8318227780     2.2619600414453056    0.0000000000000000
      Z:      10246.9344139590     0.7918209824057376    0.0000000000000000
              EPOCH : 2001/07/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -193281.1405626627    -0.0226371662035535    0.0000000000000000
      Y:       2489.5423282521    -0.9336998378920764   -0.0000000000000000
      Z:      25590.0221355299    -0.2536202738644504    0.0000000000000000
              EPOCH : 2001/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -70997.7868776831    -1.7644231976105873    0.0000000000000000
      Y:      97535.1531778735    -0.0716195542466095    0.0000000000000000
      Z:      37407.0911436053     0.2181671501992647    0.0000000000000000
              EPOCH : 2002/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -66014.4207481950     1.7268425934732039    0.0000000000000000
      Y:    -108406.4966527833     0.1001476683363375    0.0000000000000000
      Z:     -23275.9726685247    -0.2199052742291963    0.0000000000000000
              EPOCH : 2002/04/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -25366.7571800792    -2.1971888824455297    0.0000000000000000
      Y:      85448.3288868046     0.4797242943125729    0.0000000000000000
      Z:      31415.4816791690     0.4898915959501698    0.0000000000000000
              EPOCH : 2002/07/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -179526.7721449895     0.4972936775741232    0.0000000000000000
      Y:     -69191.5128887443    -0.7938440595047991   -0.0000000000000000
      Z:       5561.3827512375    -0.3528765669538315    0.0000000000000000
              EPOCH : 2002/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -141894.4216305260    -1.1376502419400512    0.0000000000000000
      Y:      52556.2954745165    -0.7844533718631631    0.0000000000000000
      Z:      43222.7222370163    -0.0916133259811976    0.0000000000000000
              EPOCH : 2003/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:       2481.4700794918     1.7518590898197879    0.0000000000000000
      Y:     -97235.4083763263     1.1753856836240306    0.0000000000000000
      Z:     -38928.5093190676     0.1421533655304170    0.0000000000000000

From:	SMTP%"matu@d1.nas.nec.co.jp" 23-FEB-2001 05:51:08.66
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/02/23)
To: gtl_month@ayame.d1.nas.nec.co.jp
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/02/23)
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20010223195238N.matu@d1.nas.nec.co.jp>
Date: Fri, 23 Feb 2001 19:52:38 +0900
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
X-Dispatcher: imput version 20000228(IM140)
Lines: 56
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
 GEOTAIL STATE VECTOR(J2000.0EQ)
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2001 02 21 20 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -154921.011975  [km]    Vx:  0.9659376889  [km/s]
             Y:  -64101.597759  [km]    Vy: -0.7633932404  [km/s]
             Z:    1612.385516  [km]    Vz: -0.3131717070  [km/s]
(Keplerian)  a:  126910.729417  [km]    an:  24.404003072  [deg]
             e:  0.552847898264 [ - ]   ap: 327.106012454  [deg]
             i:  15.9705461898  [deg]   ma: 260.271190310  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2001/02/21 20:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -154921.0119754400     0.9659376889403700    0.0000000000000000
      Y:     -64101.5977589690    -0.7633932403526900    0.0000000000000000
      Z:       1612.3855164872    -0.3131717070296600    0.0000000000000000
              EPOCH : 2001/03/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:       3707.5227096325    -1.9348844345654130    0.0000000000000000
      Y:      90878.4197927416     1.1516590443000909    0.0000000000000000
      Z:      23293.4487978360     0.5295971946364487    0.0000000000000000
              EPOCH : 2001/04/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      38889.3336228970    -1.6162728495706866    0.0000000000000000
      Y:      56444.2614421910     2.2619086800644213    0.0000000000000000
      Z:      10246.7274385486     0.7917645604455970    0.0000000000000000
              EPOCH : 2001/05/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -93382.7709317840     1.6235297861339613    0.0000000000000000
      Y:     -95674.2217600322    -0.2658865115064815   -0.0000000000000000
      Z:     -14320.3926595605    -0.2708601324199389    0.0000000000000000

********NOTE: THESE VECTORS BELOW REPLACE Sep 94 - Mar 95 VECTORS.******
From:	SMTP%"matu@d1.nas.nec.co.jp" 16-MAR-2001 12:16:40.91
To:	SARDI
CC:
Subj:	Re: Geotail
To: SARDI@nssdca.gsfc.nasa.gov
Cc: matu@d1.nas.nec.co.jp
Reply-To: matu@d1.nas.nec.co.jp
Subject: Re: Geotail
In-Reply-To: <010312151106.16464ac@nssdca.gsfc.nasa.gov>
References: <010312151106.16464ac@nssdca.gsfc.nasa.gov>
X-Mailer: Mew version 1.94.2 on Emacs 19.28 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20010317021751J.matu@net203.newslan.isas.ac.jp>
Date: Sat, 17 Mar 2001 02:17:51 +0900 (JST)
From: Masatoshi Matsuoka <matu@net203.newslan.isas.ac.jp>
X-Dispatcher: imput version 20000228(IM140)
Lines: 131
From: "r.parthasarathy,nssdc/wdc/gsfc/nasa" <SARDI@nssdca.gsfc.nasa.gov>
Subject: Re: Geotail
Date: Mon, 12 Mar 2001 15:11:06 -0500
Dear Sardi,
The Geotail state vector is attached the end of this mail.
I expect this data makes good result.
Masatoshi.
==
Masatoshi Matsuoka(matu@d1.nas.nec.co.jp)
NEC Aerospace Systems.
-------- data -----------------------------------------
The executed maneuver dates are shown as Table-1 and
Table-2 shows each state vector(J2000.0EQ).
Table-1: delta-v epoch between from Sep.'94 to Mar.'95
-------------------------------------------------
DV14          EPOCH : 1994/09/19 12:30:00 (UTC)
DVT14         EPOCH : 1994/10/17 13:00:00 (UTC)
DV15          EPOCH : 1994/11/04 18:00:00 (UTC)
DV16-1        EPOCH : 1994/11/12 03:40:00 (UTC)
    -2        EPOCH : 1994/11/12 06:30:00 (UTC)
    -3        EPOCH : 1994/11/12 09:20:00 (UTC)
DV17-1        EPOCH : 1995/02/19 18:10:00 (UTC)
    -2        EPOCH : 1995/02/19 21:00:00 (UTC)
    -3        EPOCH : 1995/02/19 23:50:00 (UTC)
DV18-1        EPOCH : 1995/02/26 20:10:00 (UTC)
    -2        EPOCH : 1995/02/26 23:10:00 (UTC)
    -3        EPOCH : 1995/02/27 02:10:00 (UTC)
--------------------------------------------------
Table-2: state vector(post delta-v)
 <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000.0EQ;GEO-CENTRIC) >>>
        EPOCH : 1994/09/19 12:30:00 (UTC)
(Cartesian)  X: 1082240.234720  [km]    Vx:  0.0863684506  [km/s]
DV14         Y: -312903.617553  [km]    Vy:  0.3608340098  [km/s]
             Z:  -48204.212859  [km]    Vz:  0.1361586227  [km/s]
        EPOCH : 1994/10/17 13:00:00 (UTC)
(Cartesian)  X:  473694.652648  [km]    Vx: -0.6781818101  [km/s]
DVT14        Y:  516389.094928  [km]    Vy:  0.1350763672  [km/s]
             Z:  201871.627797  [km]    Vz:  0.0035123081  [km/s]
        EPOCH : 1994/11/04 18:00:00 (UTC)
(Cartesian)  X:   50390.731944  [km]    Vx: -0.4949029707  [km/s]
DV15         Y:  382512.491517  [km]    Vy:  0.2074390861  [km/s]
             Z:  108602.398491  [km]    Vz:  0.0391709310  [km/s]
        EPOCH : 1994/11/12 03:40:00 (UTC)
(Cartesian)  X:  -26530.593081  [km]    Vx:  3.2100075006  [km/s]
DV16-1       Y:  -53632.058531  [km]    Vy: -0.8546183261  [km/s]
             Z:  -15832.559500  [km]    Vz: -0.1296296688  [km/s]
        EPOCH : 1994/11/12 06:30:00 (UTC)
(Cartesian)  X:    7621.161579  [km]    Vx:  3.3485851169  [km/s]
DV16-2       Y:  -57121.792211  [km]    Vy:  0.1997870475  [km/s]
             Z:  -15651.314070  [km]    Vz:  0.1677352363  [km/s]
        EPOCH : 1994/11/12 09:20:00 (UTC)
(Cartesian)  X:   40096.786221  [km]    Vx:  2.9275856905  [km/s]
DV16-3       Y:  -49990.359652  [km]    Vy:  1.1341213113  [km/s]
             Z:  -12578.224871  [km]    Vz:  0.4135420144  [km/s]
        EPOCH : 1994/11/17 22:00:00 (UTC)
(Cartesian)  X:  -55748.289425  [km]    Vx: -0.5990302798  [km/s]
(no-DV)      Y:  275699.594619  [km]    Vy: -0.4094083856  [km/s]
             Z:   75170.079524  [km]    Vz: -0.1327402848  [km/s]
        EPOCH : 1994/12/07 22:00:00 (UTC)
(Cartesian)  X: -130671.519130  [km]    Vx: -0.0641957102  [km/s]
(no-DV)      Y:  133949.074835  [km]    Vy: -1.3657863425  [km/s]
             Z:   34442.840722  [km]    Vz: -0.3834089758  [km/s]
        EPOCH : 1994/12/21 19:00:00 (UTC)
(Cartesian)  X:   47447.441485  [km]    Vx: -0.5949022213  [km/s]
(no-DV)      Y:  286225.525471  [km]    Vy:  0.3218517292  [km/s]
             Z:   81044.412737  [km]    Vz:  0.0800823760  [km/s]
        EPOCH : 1995/01/04 20:00:00 (UTC)
(Cartesian)  X: -112750.551321  [km]    Vx:  0.9369749920  [km/s]
(no-DV)      Y:   26328.048500  [km]    Vy: -1.8864272023  [km/s]
             Z:    6276.399976  [km]    Vz: -0.5195396910  [km/s]
        EPOCH : 1995/01/26 14:00:00 (UTC)
(Cartesian)  X:   75388.486725  [km]    Vx: -0.5745492167  [km/s]
(no-DV)      Y:  265946.166071  [km]    Vy:  0.5315081528  [km/s]
             Z:   74827.097324  [km]    Vz:  0.1479010870  [km/s]
        EPOCH : 1995/02/09 18:00:00 (UTC)
(Cartesian)  X: -136611.608923  [km]    Vx:  0.2506669450  [km/s]
(no-DV)      Y:   84531.604940  [km]    Vy: -1.5748725548  [km/s]
             Z:   24071.502522  [km]    Vz: -0.4417214861  [km/s]
        EPOCH : 1995/02/19 18:10:00 (UTC)
(Cartesian)  X:  -32909.819989  [km]    Vx:  2.9200359999  [km/s]
DV17-1       Y:  -58027.469845  [km]    Vy: -0.8786246634  [km/s]
             Z:  -16139.050014  [km]    Vz: -0.2571414978  [km/s]
        EPOCH : 1995/02/19 21:00:00 (UTC)
(Cartesian)  X:   -1584.326302  [km]    Vx:  3.1213358652  [km/s]
DV17-2       Y:  -62827.381866  [km]    Vy: -0.0303943170  [km/s]
             Z:  -17601.285694  [km]    Vz: -0.0202491253  [km/s]
        EPOCH : 1995/02/19 23:50:00 (UTC)
(Cartesian)  X:   29605.096659  [km]    Vx:  2.9082516193  [km/s]
DV17-3       Y:  -58570.037037  [km]    Vy:  0.8393248285  [km/s]
             Z:  -16525.393072  [km]    Vz:  0.2242595254  [km/s]
        EPOCH : 1995/02/26 20:10:00 (UTC)
(Cartesian)  X:  -32684.041615  [km]    Vx:  2.8364360614  [km/s]
DV18-1       Y:  -57998.986402  [km]    Vy: -0.8866323420  [km/s]
             Z:  -16066.098147  [km]    Vz: -0.2627710415  [km/s]
        EPOCH : 1995/02/26 23:10:00 (UTC)
(Cartesian)  X:    -357.317825  [km]    Vx:  3.0455421956  [km/s]
DV18-2       Y:  -62886.092241  [km]    Vy:  0.0142223772  [km/s]
             Z:  -17600.368233  [km]    Vz: -0.0108922131  [km/s]
        EPOCH : 1995/02/27 02:10:00 (UTC)
(Cartesian)  X:   31684.356099  [km]    Vx:  2.7831799942  [km/s]
DV18-3       Y:  -57643.198552  [km]    Vy:  0.9261459535  [km/s]
             Z:  -16289.328079  [km]    Vz:  0.2464072272  [km/s]

From:	SMTP%"matu@d1.nas.nec.co.jp" 30-MAR-2001 03:59:44.21
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/03/30)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/03/30)
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20010330180345V.matu@d1.nas.nec.co.jp>
Date: Fri, 30 Mar 2001 18:03:45 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 53
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
 GEOTAIL STATE VECTOR(J2000.0EQ)
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2001 03 29 13 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -192761.972509  [km]    Vx:  0.2363189984  [km/s]
             Y:  -14570.240923  [km]    Vy: -0.9107876426  [km/s]
             Z:   19242.539414  [km]    Vz: -0.2683988695  [km/s]
(Keplerian)  a:  126692.170116  [km]    an:  24.430501283  [deg]
             e:  0.558804887790 [ - ]   ap: 329.854828788  [deg]
             i:  16.1479393599  [deg]   ma: 206.897820514  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2001/03/29 13:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -192761.9725085400     0.2363189983785100    0.0000000000000000
      Y:     -14570.2409232780    -0.9107876425722300    0.0000000000000000
      Z:      19242.5394141180    -0.2683988694681300    0.0000000000000000
              EPOCH : 2001/04/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      38888.4263303645    -1.6162846777580686    0.0000000000000000
      Y:      56446.3740448053     2.2618864328590131    0.0000000000000000
      Z:      10245.8713283412     0.7916885219445409    0.0000000000000000
              EPOCH : 2001/05/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -93376.2544459542     1.6236040931547437    0.0000000000000000
      Y:     -95674.0245180715    -0.2658445284733292   -0.0000000000000000
      Z:     -14318.5840008279    -0.2708453486492977    0.0000000000000000
              EPOCH : 2001/06/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -132348.6712789652     1.2033562630388095    0.0000000000000000
      Y:     -87742.7913923098    -0.5787192253184295   -0.0000000000000000
      Z:      -7459.2038216575    -0.3104926082147613    0.0000000000000000

From:	SMTP%"matu@d1.nas.nec.co.jp" 27-APR-2001 04:38:38.88
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/04/27)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/04/27)
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20010427173358D.matu@d1.nas.nec.co.jp>
Date: Fri, 27 Apr 2001 17:33:58 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 58
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
 GEOTAIL STATE VECTOR(GEO CENTRIC J2000.0EQ)
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2001 04 25 18 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -101466.299591  [km]    Vx:  1.5420722518  [km/s]
             Y:  -94991.888702  [km]    Vy: -0.3366543636  [km/s]
             Z:  -13208.574020  [km]    Vz: -0.2787480049  [km/s]
(Keplerian)  a:  126909.411229  [km]    an:  24.363365699  [deg]
             e:  0.546382192083 [ - ]   ap: 331.039959606  [deg]
             i:  16.4706071898  [deg]   ma: 290.213959549  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2001/04/25 18:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -101466.2995907200     1.5420722517612000    0.0000000000000000
      Y:     -94991.8887016430    -0.3366543636079200    0.0000000000000000
      Z:     -13208.5740195590    -0.2787480049472100    0.0000000000000000
              EPOCH : 2001/05/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -93381.9665606042     1.6235597019430938    0.0000000000000000
      Y:     -95671.4962877457    -0.2658955436552801   -0.0000000000000000
      Z:     -14322.9606320805    -0.2708508771446435    0.0000000000000000
              EPOCH : 2001/06/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -132356.9783998700     1.2032730132644445    0.0000000000000000
      Y:     -87737.4760712862    -0.5787729712147291   -0.0000000000000000
      Z:      -7462.4455390525    -0.3105121252209154    0.0000000000000000
              EPOCH : 2001/07/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -193280.8127246245    -0.0225935500264003    0.0000000000000000
      Y:       2490.4256756047    -0.9337060889516217   -0.0000000000000000
      Z:      25587.2769618233    -0.2536275916963927    0.0000000000000000

From:	SMTP%"matu@d1.nas.nec.co.jp" 25-MAY-2001 03:39:43.19
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/05/25)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/05/25)
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20010525163804M.matu@d1.nas.nec.co.jp>
Date: Fri, 25 May 2001 16:38:04 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 64
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
 GEOTAIL STATE VECTOR(J2000.0EQ:GEOCENTRIC)
 ~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2001 05 24 14 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -157165.789985  [km]    Vx: -0.8692038102  [km/s]
             Y:   74454.030857  [km]    Vy: -0.7466569804  [km/s]
             Z:   40050.180731  [km]    Vz: -0.0960147368  [km/s]
(Keplerian)  a:  126747.275420  [km]    an:  24.512748257  [deg]
             e:  0.533248164682 [ - ]   ap: 331.675761577  [deg]
             i:  16.7644320223  [deg]   ma: 120.247793315  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2001/05/24 14:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -157165.7899846100    -0.8692038101983000    0.0000000000000000
      Y:      74454.0308570130    -0.7466569803563200    0.0000000000000000
      Z:      40050.1807310170    -0.0960147367607310    0.0000000000000000
              EPOCH : 2001/06/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -132360.2771281240     1.2032500078924508    0.0000000000000000
      Y:     -87734.1712331426    -0.5787859213694646   -0.0000000000000000
      Z:      -7463.9027621221    -0.3105321249243183    0.0000000000000000
              EPOCH : 2001/07/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -193281.7084619936    -0.0226488187305108    0.0000000000000000
      Y:       2496.5159982823    -0.9336872613877825   -0.0000000000000000
      Z:      25589.1188166683    -0.2536457745966253    0.0000000000000000
              EPOCH : 2001/08/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -192699.3452419016    -0.1704576659239707    0.0000000000000000
      Y:      16421.9629606947    -0.9180332368224438    0.0000000000000000
      Z:      29953.0005416006    -0.2308962974130619    0.0000000000000000
              EPOCH : 2001/09/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -188395.3585412372    -0.3885251390293857    0.0000000000000000
      Y:      32327.1171153287    -0.8854698512199350    0.0000000000000000
      Z:      34202.6935287402    -0.1959851615969169    0.0000000000000000

From:	SMTP%"matu@d1.nas.nec.co.jp" 29-JUN-2001 05:01:18.49
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/06/29)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/06/29)
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20010629180001G.matu@d1.nas.nec.co.jp>
Date: Fri, 29 Jun 2001 18:00:01 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 65
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
------
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2001 06 27 14 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:  -65344.872011  [km]    Vx:  1.8362728518  [km/s]
             Y: -100303.984685  [km]    Vy:  0.0587194625  [km/s]
             Z:  -19128.072119  [km]    Vz: -0.2203392063  [km/s]
(Keplerian)  a:  126457.952306  [km]    an:  25.124762513  [deg]
             e:  0.543485397615 [ - ]   ap: 332.113305358  [deg]
             i:  16.8719389979  [deg]   ma: 305.411704875  [deg]
--
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2001/06/27 14:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -65344.8720105490     1.8362728518039999    0.0000000000000000
      Y:    -100303.9846853000     0.0587194625314660    0.0000000000000000
      Z:     -19128.0721193520    -0.2203392062930700    0.0000000000000000
              EPOCH : 2001/07/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -193282.6009458281    -0.0225946044168878    0.0000000000000000
      Y:       2491.6330773662    -0.9336827697403455   -0.0000000000000000
      Z:      25590.4268998259    -0.2536191086523167    0.0000000000000000
              EPOCH : 2001/08/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -192701.7790050232    -0.1703538737377509    0.0000000000000000
      Y:      16412.6874818409    -0.9180370473806765    0.0000000000000000
      Z:      29952.9618540212    -0.2308775542208566    0.0000000000000000
              EPOCH : 2001/09/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -188401.3960254153    -0.3883845694948563    0.0000000000000000
      Y:      32314.7827701464    -0.8854886829141377    0.0000000000000000
      Z:      34201.7656309735    -0.1959745119294151    0.0000000000000000
              EPOCH : 2001/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -71027.8629697369    -1.7641580925740166    0.0000000000000000
      Y:      97536.2640157485    -0.0718975361870519    0.0000000000000000
      Z:      37410.9921594857     0.2180485107448029    0.0000000000000000
ayame{matu}102:

From:	SMTP%"matu@d1.nas.nec.co.jp" 27-JUL-2001 00:45:42.87
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/07/27)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/07/27)
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20010727134902I.matu@d1.nas.nec.co.jp>
Date: Fri, 27 Jul 2001 13:49:02 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 63
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
------
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2001 07 26 10 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -182349.108393  [km]    Vx: -0.5009108601  [km/s]
             Y:   45161.139889  [km]    Vy: -0.8578156750  [km/s]
             Z:   36268.012712  [km]    Vz: -0.1695396565  [km/s]
(Keplerian)  a:  126492.207510  [km]    an:  25.541391096  [deg]
             e:  0.552734120379 [ - ]   ap: 331.202646298  [deg]
             i:  16.9002895800  [deg]   ma: 146.167841991  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2001/07/26 10:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -182349.1083927900    -0.5009108601100000    0.0000000000000000
      Y:      45161.1398886320    -0.8578156749566400    0.0000000000000000
      Z:      36268.0127117130    -0.1695396564645400    0.0000000000000000
              EPOCH : 2001/08/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -192702.6517339308    -0.1703585486093077    0.0000000000000000
      Y:      16412.5927889689    -0.9180257402249031    0.0000000000000000
      Z:      29953.4731003370    -0.2308808360168667    0.0000000000000000
              EPOCH : 2001/09/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -188401.2771230069    -0.3884117601287677    0.0000000000000000
      Y:      32316.5551285676    -0.8854739386367032    0.0000000000000000
      Z:      34202.7748891391    -0.1959735159669719    0.0000000000000000
              EPOCH : 2001/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -71018.9093127686    -1.7642381892963832    0.0000000000000000
      Y:      97535.5926228040    -0.0717940933573059    0.0000000000000000
      Z:      37410.5385688973     0.2180905459730865    0.0000000000000000
              EPOCH : 2001/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -37832.7395158337    -2.0262115114668973    0.0000000000000000
      Y:      93663.1021730650     0.3334853646874665    0.0000000000000000
      Z:      32543.1210650033     0.3768680700963247    0.0000000000000000

From:	SMTP%"matu@d1.nas.nec.co.jp" 30-AUG-2001 03:49:19.55
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/08/30)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/08/30)
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20010830165103G.matu@d1.nas.nec.co.jp>
Date: Thu, 30 Aug 2001 16:51:03 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 63
The following data is updated orbit solution
based on 2 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
------
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2001 08 28 07 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS:
(Cartesian)  X: -149886.193816  [km]    Vx:  1.0095754575  [km/s]
             Y:  -79702.858928  [km]    Vy: -0.6594014635  [km/s]
             Z:   -2311.753108  [km]    Vz: -0.3191139566  [km/s]
(Keplerian)  a:  126953.812385  [km]    an:  25.483810670  [deg]
             e:  0.551060247802 [ - ]   ap: 333.069218905  [deg]
             i:  17.2199370088  [deg]   ma: 257.226446604  [deg]
_
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2001/08/28 07:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -149886.1938159900     1.0095754575345000    0.0000000000000000
      Y:     -79702.8589276990    -0.6594014634990100    0.0000000000000000
      Z:      -2311.7531083139    -0.3191139566226700    0.0000000000000000
              EPOCH : 2001/09/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -188402.4838399479    -0.3884002881853749    0.0000000000000000
      Y:      32314.4383327133    -0.8854731174795087    0.0000000000000000
      Z:      34201.7786452258    -0.1959682516651505    0.0000000000000000
              EPOCH : 2001/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -71019.2089613694    -1.7642525691642248    0.0000000000000000
      Y:      97534.5249049002    -0.0717946193354440    0.0000000000000000
      Z:      37409.3638671748     0.2180903452477491    0.0000000000000000
              EPOCH : 2001/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -37831.1603884128    -2.0262436347331469    0.0000000000000000
      Y:      93661.7296900384     0.3335166901700938    0.0000000000000000
      Z:      32541.6905871179     0.3768762726359720    0.0000000000000000
              EPOCH : 2001/12/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -21063.6961362875     1.9865782726036785    0.0000000000000000
      Y:     -98562.8240141603     0.7490214670686353    0.0000000000000000
      Z:     -26483.6298191449    -0.0574098379810612    0.0000000000000000

From:	SMTP%"matu@d1.nas.nec.co.jp" 28-SEP-2001 03:30:40.10
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/09/28)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/09/28)
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20010928163618G.matu@d1.nas.nec.co.jp>
Date: Fri, 28 Sep 2001 16:36:18 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 64
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
-------
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2001 09 25 21 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:  -82516.621616  [km]    Vx: -1.6631136078  [km/s]
             Y:   97438.634200  [km]    Vy: -0.1898974174  [km/s]
             Z:   38886.047839  [km]    Vz:  0.1707117379  [km/s]
(Keplerian)  a:  126880.633199  [km]    an:  25.398691226  [deg]
             e:  0.559891812655 [ - ]   ap: 335.852485486  [deg]
             i:  17.4890149407  [deg]   ma:  63.384783090  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2001/09/25 21:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -82516.6216155780    -1.6631136078186000    0.0000000000000000
      Y:      97438.6342001280    -0.1898974173621500    0.0000000000000000
      Z:      38886.0478390760     0.1707117379260700    0.0000000000000000
              EPOCH : 2001/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -71025.4785192835    -1.7642158565992654    0.0000000000000000
      Y:      97532.8104218100    -0.0718738736508330    0.0000000000000000
      Z:      37409.6212311423     0.2180890428255920    0.0000000000000000
              EPOCH : 2001/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -37850.4136420035    -2.0261411263495024    0.0000000000000000
      Y:      93663.7017933759     0.3332130444557059    0.0000000000000000
      Z:      32544.5229977691     0.3768000432140207    0.0000000000000000
              EPOCH : 2001/12/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -21037.9450494227     1.9866576910569693    0.0000000000000000
      Y:     -98553.8590537961     0.7494879177052426    0.0000000000000000
      Z:     -26483.4138778524    -0.0573184399590028    0.0000000000000000
              EPOCH : 2002/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -65976.0718150615     1.7271536296858840    0.0000000000000000
      Y:    -108401.1105655195     0.1006348243621514    0.0000000000000000
      Z:     -23277.9611424616    -0.2198257284093545    0.0000000000000000

From:	SMTP%"matu@d1.nas.nec.co.jp" 26-OCT-2001 01:46:51.60
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/10/26)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/10/26)
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20011026144657G.matu@d1.nas.nec.co.jp>
Date: Fri, 26 Oct 2001 14:46:57 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 55
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
-------
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2001 10 25 08 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:  -69602.473875  [km]    Vx:  1.7392126973  [km/s]
             Y: -105300.237800  [km]    Vy:  0.0877632235  [km/s]
             Z:  -21026.870734  [km]    Vz: -0.2137781502  [km/s]
(Keplerian)  a:  126474.699724  [km]    an:  25.332868585  [deg]
             e:  0.560409514978 [ - ]   ap: 337.541181693  [deg]
             i:  17.8249926608  [deg]   ma: 300.898044431  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2001/10/25 08:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -69602.4738753820     1.7392126972937001    0.0000000000000000
      Y:    -105300.2377996100     0.0877632234807500    0.0000000000000000
      Z:     -21026.8707335540    -0.2137781502143000    0.0000000000000000
              EPOCH : 2001/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -37837.5005941474    -2.0262316458334317    0.0000000000000000
      Y:      93660.8930535618     0.3334021206082446    0.0000000000000000
      Z:      32543.4219324282     0.3768491609191370    0.0000000000000000
              EPOCH : 2001/12/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -21059.2091448278     1.9865622254194115    0.0000000000000000
      Y:     -98562.5444689138     0.7491041304462079    0.0000000000000000
      Z:     -26485.2346169084    -0.0573787602731171    0.0000000000000000
              EPOCH : 2002/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -66004.0092240701     1.7269451177976467    0.0000000000000000
      Y:    -108403.3354471999     0.1003068800305830    0.0000000000000000
      Z:     -23277.5403326351    -0.2198696259842990    0.0000000000000000

From:	SMTP%"matu@d1.nas.nec.co.jp" 30-NOV-2001 00:59:40.78
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/11/30)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/11/30)
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20011130150026Y.matu@d1.nas.nec.co.jp>
Date: Fri, 30 Nov 2001 15:00:26 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 61
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
-------
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2001 11 27 20 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -144593.427214  [km]    Vx: -1.0604860684  [km/s]
             Y:   71243.769667  [km]    Vy: -0.7172718330  [km/s]
             Z:   41652.370406  [km]    Vz: -0.0639548451  [km/s]
(Keplerian)  a:  126734.020855  [km]    an:  25.360060968  [deg]
             e:  0.542829412431 [ - ]   ap: 338.430093236  [deg]
             i:  18.2508570576  [deg]   ma:  99.915401690  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2001/11/27 20:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -144593.4272138100    -1.0604860683638000    0.0000000000000000
      Y:      71243.7696666860    -0.7172718329533200    0.0000000000000000
      Z:      41652.3704057520    -0.0639548450579790    0.0000000000000000
              EPOCH : 2001/12/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -21057.2048743864     1.9865493440201143    0.0000000000000000
      Y:     -98563.5171031845     0.7491167980159703    0.0000000000000000
      Z:     -26485.1314973257    -0.0573454388848248    0.0000000000000000
              EPOCH : 2002/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -66001.0097133015     1.7269527208285815    0.0000000000000000
      Y:    -108404.6198723152     0.1003279211622809    0.0000000000000000
      Z:     -23278.2742771797    -0.2198347105722727    0.0000000000000000
              EPOCH : 2002/02/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -110688.6694561604     1.3724809826588189    0.0000000000000000
      Y:    -104273.9347504846    -0.2975821187502091   -0.0000000000000000
      Z:     -15464.8396626942    -0.2926955383147746    0.0000000000000000
              EPOCH : 2002/03/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -87912.9616178469    -1.6671060507998579    0.0000000000000000
      Y:      89592.6923328633    -0.2848737210382391    0.0000000000000000
      Z:      40609.1819334092     0.1600294705433400    0.0000000000000000

From:	SMTP%"matu@d1.nas.nec.co.jp" 28-DEC-2001 01:15:00.76
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/12/28)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/12/28)
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20011228150958J.matu@d1.nas.nec.co.jp>
Date: Fri, 28 Dec 2001 15:09:58 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 63
The following data is updated orbit solution
based on 3 path data. And....
 A Happy New Year!!
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
-------
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2001 12 27 05 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:    1373.016912  [km]    Vx:  2.0141622150  [km/s]
             Y:  -88833.527031  [km]    Vy:  1.1763429995  [km/s]
             Z:  -27108.594169  [km]    Vz:  0.0652317302  [km/s]
(Keplerian)  a:  127043.449350  [km]    an:  25.506937155  [deg]
             e:  0.532752822662 [ - ]   ap: 338.719954277  [deg]
             i:  18.5539030465  [deg]   ma: 326.660269415  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2001/12/27 05:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:       1373.0169118890     2.0141622149690002    0.0000000000000000
      Y:     -88833.5270311180     1.1763429994857999    0.0000000000000000
      Z:     -27108.5941689420     0.0652317301575720    0.0000000000000000
              EPOCH : 2002/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -66000.8491716926     1.7269405191580438    0.0000000000000000
      Y:    -108405.5305271847     0.1003260101982927    0.0000000000000000
      Z:     -23278.0876857966    -0.2198649845775018    0.0000000000000000
              EPOCH : 2002/02/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -110692.3353542197     1.3724357382400278    0.0000000000000000
      Y:    -104274.0132343242    -0.2976181492886654   -0.0000000000000000
      Z:     -15463.2087173751    -0.2927277933151250    0.0000000000000000
              EPOCH : 2002/03/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -87899.4084328946    -1.6672167790004697    0.0000000000000000
      Y:      89594.7897442367    -0.2847686078260768    0.0000000000000000
      Z:      40610.2894263358     0.1601061529357743    0.0000000000000000
              EPOCH : 2002/04/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -25374.4315033607    -2.1971739878714831    0.0000000000000000
      Y:      85448.3104252539     0.4795972607006960    0.0000000000000000
      Z:      31417.0667489073     0.4898506560473496    0.0000000000000000

From:	SMTP%"matu@d1.nas.nec.co.jp" 27-JAN-2002 20:39:54.94
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/1/28)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/1/28)
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20020128103923P.matu@d1.nas.nec.co.jp>
Date: Mon, 28 Jan 2002 10:39:23 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 57
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
-------
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2002 01 24 18 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -181891.733107  [km]    Vx: -0.5026843955  [km/s]
             Y:   29813.348520  [km]    Vy: -0.8991527448  [km/s]
             Z:   35748.016004  [km]    Vz: -0.2003881365  [km/s]
(Keplerian)  a:  126754.062800  [km]    an:  25.681728867  [deg]
             e:  0.544931846628 [ - ]   ap: 338.939731800  [deg]
             i:  18.6864974244  [deg]   ma: 137.373819704  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2002/01/24 18:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -181891.7331065900    -0.5026843954806300    0.0000000000000000
      Y:      29813.3485203600    -0.8991527447877800    0.0000000000000000
      Z:      35748.0160039740    -0.2003881364554500    0.0000000000000000
              EPOCH : 2002/02/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -110687.4798690657     1.3724719288649068    0.0000000000000000
      Y:    -104276.3978652514    -0.2976036028907410   -0.0000000000000000
      Z:     -15460.8292379962    -0.2926949952803237    0.0000000000000000
              EPOCH : 2002/03/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -87902.5207058663    -1.6671886069794575    0.0000000000000000
      Y:      89596.5396495918    -0.2848010421249924    0.0000000000000000
      Z:      40605.4902789652     0.1600853195745784    0.0000000000000000
              EPOCH : 2002/04/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -25381.9994500968    -2.1971333362753138    0.0000000000000000
      Y:      85451.8936993664     0.4794709046950659    0.0000000000000000
      Z:      31414.5197538315     0.4897513361339627    0.0000000000000000

From:	SMTP%"matu@d1.nas.nec.co.jp" 28-FEB-2002 09:17:23.35
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/2/28)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/2/28)
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20020228231745A.matu@d1.nas.nec.co.jp>
Date: Thu, 28 Feb 2002 23:17:45 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 62
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
-------
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2002 02 21 20 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -100408.920192  [km]    Vx:  1.4594544508  [km/s]
             Y: -106938.298931  [km]    Vy: -0.1975554419  [km/s]
             Z:  -18032.433111  [km]    Vz: -0.2770844303  [km/s]
(Keplerian)  a:  126611.882514  [km]    an:  25.711225020  [deg]
             e:  0.561531928851 [ - ]   ap: 339.591434266  [deg]
             i:  18.8596894990  [deg]   ma: 283.379215827  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2002/02/21 20:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -100408.9201922100     1.4594544507633000    0.0000000000000000
      Y:    -106938.2989312100    -0.1975554418860600    0.0000000000000000
      Z:     -18032.4331112860    -0.2770844303229500    0.0000000000000000
              EPOCH : 2002/03/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -87903.8751836299    -1.6671554625116345    0.0000000000000000
      Y:      89596.1318203727    -0.2848165738349846    0.0000000000000000
      Z:      40610.8738110017     0.1600700566872250    0.0000000000000000
              EPOCH : 2002/04/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -25391.8538558743    -2.1970451133069639    0.0000000000000000
      Y:      85454.2099060148     0.4792640558027703    0.0000000000000000
      Z:      31421.3830951033     0.4897066311159488    0.0000000000000000
              EPOCH : 2002/05/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -51955.3496109652     1.7323022098877636    0.0000000000000000
      Y:    -111735.4971951975     0.3621247362311183    0.0000000000000000
      Z:     -28875.0342708175    -0.1501957745502525    0.0000000000000000
              EPOCH : 2002/06/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -71861.6155008759     1.5935306603385739    0.0000000000000000
      Y:    -115420.6639603829     0.1151686021853982    0.0000000000000000
      Z:     -27423.0485454493    -0.2156106702201837    0.0000000000000000

From:	SMTP%"matu@d1.nas.nec.co.jp" 28-MAR-2002 23:14:16.24
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/3/29)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/3/29)
From: Masatoshi Matsuoka <matu@d1.nas.nec.co.jp>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20020329131323E.matu@d1.nas.nec.co.jp>
Date: Fri, 29 Mar 2002 13:13:23 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 61
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
			  matu@d1.nas.nec.co.jp
** e-mail addres will be changed. (from Apr. 1st)
  The new address is  m-matsuoka@ps.jp.nec.com
-------
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2002 03 28 19 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -196785.837834  [km]    Vx:  0.0647107191  [km/s]
             Y:  -26676.770065  [km]    Vy: -0.8883318055  [km/s]
             Z:   21129.295303  [km]    Vz: -0.2923987847  [km/s]
(Keplerian)  a:  128042.155697  [km]    an:  25.314497408  [deg]
             e:  0.560095571027 [ - ]   ap: 342.569289070  [deg]
             i:  19.3916306217  [deg]   ma: 176.618891316  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2002/03/28 19:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -196785.8378341300     0.0647107191258140    0.0000000000000000
      Y:     -26676.7700645060    -0.8883318054555500    0.0000000000000000
      Z:      21129.2953031170    -0.2923987847442900    0.0000000000000000
              EPOCH : 2002/04/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -25390.5674677362    -2.1970248149690663    0.0000000000000000
      Y:      85455.5287520052     0.4792920472373352    0.0000000000000000
      Z:      31420.6919860320     0.4897154015165374    0.0000000000000000
              EPOCH : 2002/05/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -51958.0614654219     1.7322974340659287    0.0000000000000000
      Y:    -111735.6748267773     0.3620808064524170    0.0000000000000000
      Z:     -28873.1648849800    -0.1502207130547424    0.0000000000000000
              EPOCH : 2002/06/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -71866.4974963291     1.5935086737688169    0.0000000000000000
      Y:    -115420.3600596352     0.1151060588646520    0.0000000000000000
      Z:     -27420.5417851551    -0.2156362261757563    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com" 26-APR-2002 04:36:21.50
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/4/26)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/4/26)
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20020426173219I.m-matsuoka@ps.jp.nec.com>
Date: Fri, 26 Apr 2002 17:32:19 +0900
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
X-Dispatcher: imput version 20000228(IM140)
Lines: 56
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2002 04 22 14 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -129352.794058  [km]    Vx: -1.2733339712  [km/s]
             Y:   70191.463566  [km]    Vy: -0.6714497829  [km/s]
             Z:   42877.787643  [km]    Vz: -0.0229933891  [km/s]
(Keplerian)  a:  127434.297366  [km]    an:  25.269228201  [deg]
             e:  0.555684917335 [ - ]   ap: 344.635214423  [deg]
             i:  19.8623681660  [deg]   ma:  81.773901800  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2002/04/22 14:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -129352.7940580100    -1.2733339712092000    0.0000000000000000
      Y:      70191.4635661270    -0.6714497828991600    0.0000000000000000
      Z:      42877.7876434860    -0.0229933891086420    0.0000000000000000
              EPOCH : 2002/05/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -51957.4539242512     1.7323135679673030    0.0000000000000000
      Y:    -111734.5288632976     0.3620929167485530    0.0000000000000000
      Z:     -28872.3689278735    -0.1502377130143913    0.0000000000000000
              EPOCH : 2002/06/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -71862.0104324533     1.5935497279586923    0.0000000000000000
      Y:    -115418.9755005818     0.1151575815449473    0.0000000000000000
      Z:     -27420.1204623231    -0.2156425465427596    0.0000000000000000
              EPOCH : 2002/07/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -179516.9357438168     0.4974904576955032    0.0000000000000000
      Y:     -69203.3424093769    -0.7937831205808664   -0.0000000000000000
      Z:       5557.4926069857    -0.3528854899908411    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com" 31-MAY-2002 00:38:46.39
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/5/31)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/5/31)
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20020531133748P.m-matsuoka@ps.jp.nec.com>
Date: Fri, 31 May 2002 13:37:48 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 62
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2002 05 30 14 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -187464.399226  [km]    Vx:  0.3200481065  [km/s]
             Y:  -54662.970317  [km]    Vy: -0.8438420381  [km/s]
             Z:   11499.293901  [km]    Vz: -0.3352729666  [km/s]
(Keplerian)  a:  126597.784021  [km]    an:  25.347787197  [deg]
             e:  0.550809463038 [ - ]   ap: 345.870498537  [deg]
             i:  20.4396008911  [deg]   ma: 192.757839882  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2002/05/30 14:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -187464.3992257200     0.3200481065227200    0.0000000000000000
      Y:     -54662.9703170510    -0.8438420380659299    0.0000000000000000
      Z:      11499.2939007310    -0.3352729665961300    0.0000000000000000
              EPOCH : 2002/06/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -71867.3316157834     1.5935362911004021    0.0000000000000000
      Y:    -115418.0678224160     0.1150971774923633    0.0000000000000000
      Z:     -27416.5552287573    -0.2156466524616490    0.0000000000000000
              EPOCH : 2002/07/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -179518.9933808602     0.4974766647608256    0.0000000000000000
      Y:     -69199.8538926187    -0.7937931788644710   -0.0000000000000000
      Z:       5559.0735816359    -0.3528594184185433    0.0000000000000000
              EPOCH : 2002/08/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -189620.5856929055     0.2298120046960128    0.0000000000000000
      Y:     -48476.8320626448    -0.8697507020468487   -0.0000000000000000
      Z:      14448.7179096230    -0.3409496992426257    0.0000000000000000
              EPOCH : 2002/09/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -193320.0182661938     0.0203874565735930    0.0000000000000000
      Y:     -32930.7812603797    -0.8906933322355072   -0.0000000000000000
      Z:      20617.0302115303    -0.3197272956714408    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com" 30-JUN-2002 18:53:52.30
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/6/28)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/6/28)
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20020701075404X.m-matsuoka@ps.jp.nec.com>
Date: Mon, 01 Jul 2002 07:54:04 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 61
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2002 06 27 18 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:   44377.353521  [km]    Vx:  1.4252974333  [km/s]
             Y:  -50147.782505  [km]    Vy:  2.3820633669  [km/s]
             Z:  -24399.943207  [km]    Vz:  0.5834350055  [km/s]
(Keplerian)  a:  126965.216086  [km]    an:  25.443701460  [deg]
             e:  0.538948608604 [ - ]   ap: 345.738060577  [deg]
             i:  20.7656714983  [deg]   ma: 342.420868755  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2002/06/27 18:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      44377.3535207760     1.4252974333068000    0.0000000000000000
      Y:     -50147.7825054870     2.3820633668904998    0.0000000000000000
      Z:     -24399.9432065870     0.5834350055049100    0.0000000000000000
              EPOCH : 2002/07/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -179521.1025121388     0.4974529104145448    0.0000000000000000
      Y:     -69198.2157469335    -0.7937825384972783   -0.0000000000000000
      Z:       5556.6502755467    -0.3528783691812422    0.0000000000000000
              EPOCH : 2002/08/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -189622.3819334857     0.2297769278187672    0.0000000000000000
      Y:     -48474.3289644241    -0.8697405064906216   -0.0000000000000000
      Z:      14447.1478816667    -0.3409704477308761    0.0000000000000000
              EPOCH : 2002/09/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -193321.1075260315     0.0203422373892621    0.0000000000000000
      Y:     -32927.5593662301    -0.8906823743138976   -0.0000000000000000
      Z:      20616.0595080732    -0.3197479619633695    0.0000000000000000
              EPOCH : 2002/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -141929.0438782010    -1.1372181464387030    0.0000000000000000
      Y:      52537.5431881604    -0.7845635557785239    0.0000000000000000
      Z:      43220.4758069736    -0.0917367331203813    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com" 30-AUG-2002 03:12:06.08
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/8/30)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/8/30)
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20020830161201U.m-matsuoka@ps.jp.nec.com>
Date: Fri, 30 Aug 2002 16:12:01 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 54
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2002 08 28 11 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:  -90374.670539  [km]    Vx:  1.4454987893  [km/s]
             Y: -117188.608023  [km]    Vy: -0.0377603591  [km/s]
             Z:  -26456.957919  [km]    Vz: -0.2549678877  [km/s]
(Keplerian)  a:  126663.851789  [km]    an:  25.231556709  [deg]
             e:  0.563565881005 [ - ]   ap: 347.783511474  [deg]
             i:  21.4077786645  [deg]   ma: 281.096290450  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2002/08/28 11:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -90374.6705394490     1.4454987892535001    0.0000000000000000
      Y:    -117188.6080225200    -0.0377603591126980    0.0000000000000000
      Z:     -26456.9579185860    -0.2549678877208100    0.0000000000000000
              EPOCH : 2002/09/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -193323.0338282719     0.0202821467014314    0.0000000000000000
      Y:     -32924.1741613844    -0.8906732959537671   -0.0000000000000000
      Z:      20617.7085453202    -0.3197338905473004    0.0000000000000000
              EPOCH : 2002/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -141921.3214346362    -1.1373347199542043    0.0000000000000000
      Y:      52541.5420122392    -0.7845152147585234    0.0000000000000000
      Z:      43220.6794549391    -0.0916982453938796    0.0000000000000000
              EPOCH : 2002/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -100651.8204057457    -1.6203673973055279    0.0000000000000000
      Y:      71062.2155793009    -0.5699020088059458    0.0000000000000000
      Z:      44329.7616414200     0.0691806723166424    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com" 27-SEP-2002 03:48:23.03
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/9/27)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/9/27)
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20020927164511F.m-matsuoka@ps.jp.nec.com>
Date: Fri, 27 Sep 2002 16:45:11 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 64
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2002 09 26 07 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -178158.593669  [km]    Vx: -0.5880680243  [km/s]
             Y:   16218.415463  [km]    Vy: -0.9062291175  [km/s]
             Z:   36061.341101  [km]    Vz: -0.2285977699  [km/s]
(Keplerian)  a:  126578.269062  [km]    an:  25.070195051  [deg]
             e:  0.572582764785 [ - ]   ap: 349.055796213  [deg]
             i:  21.7952854267  [deg]   ma: 119.615844006  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2002/09/26 07:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -178158.5936694000    -0.5880680243023100    0.0000000000000000
      Y:      16218.4154628600    -0.9062291175094200    0.0000000000000000
      Z:      36061.3411012330    -0.2285977699228600    0.0000000000000000
              EPOCH : 2002/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -141922.7623276110    -1.1373160622887086    0.0000000000000000
      Y:      52538.9040405956    -0.7845319945133493    0.0000000000000000
      Z:      43220.9558746790    -0.0916929575747145    0.0000000000000000
              EPOCH : 2002/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -100655.6166213353    -1.6203302380118119    0.0000000000000000
      Y:      71059.4789753512    -0.5699453882276329    0.0000000000000000
      Z:      44330.0517139620     0.0691757913626176    0.0000000000000000
              EPOCH : 2002/12/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      17989.4012043788     1.7170718849286126    0.0000000000000000
      Y:     -82787.8128009563     1.5755874032298964    0.0000000000000000
      Z:     -35503.7214018452     0.3033062298392557    0.0000000000000000
              EPOCH : 2003/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:       2513.0833854556     1.7519008317250415    0.0000000000000000
      Y:     -97208.8287696448     1.1760860836739815    0.0000000000000000
      Z:     -38923.5517166961     0.1424175456806917    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com" 25-OCT-2002 01:34:34.05
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/10/25)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/10/25)
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20021025143402Z.m-matsuoka@ps.jp.nec.com>
Date: Fri, 25 Oct 2002 14:34:02 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 56
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2002 10 24 06 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -137001.403518  [km]    Vx:  1.0255393704  [km/s]
             Y: -113050.378591  [km]    Vy: -0.4116352740  [km/s]
             Z:  -18526.357177  [km]    Vz: -0.3330360611  [km/s]
(Keplerian)  a:  127272.332480  [km]    an:  24.918523562  [deg]
             e:  0.560796644040 [ - ]   ap: 351.539542049  [deg]
             i:  22.4651665250  [deg]   ma: 246.366154906  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2002/10/24 06:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -137001.4035179000     1.0255393704114999    0.0000000000000000
      Y:    -113050.3785905100    -0.4116352739731600    0.0000000000000000
      Z:     -18526.3571774740    -0.3330360610773100    0.0000000000000000
              EPOCH : 2002/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -100653.2293700212    -1.6203656005771239    0.0000000000000000
      Y:      71059.1644591831    -0.5699333527436349    0.0000000000000000
      Z:      44329.7873060555     0.0691610343948895    0.0000000000000000
              EPOCH : 2002/12/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      17984.6353590809     1.7170841302275495    0.0000000000000000
      Y:     -82792.7455180099     1.5754464460681541    0.0000000000000000
      Z:     -35505.9114715730     0.3032917673861703    0.0000000000000000
              EPOCH : 2003/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:       2505.9901669043     1.7518892436347586    0.0000000000000000
      Y:     -97214.2245967906     1.1759314059773467    0.0000000000000000
      Z:     -38925.8152555026     0.1423952326500926    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com" 29-NOV-2002 01:44:21.36
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/11/29)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/11/29)
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20021129154304X.m-matsuoka@ps.jp.nec.com>
Date: Fri, 29 Nov 2002 15:43:04 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 62
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2002 11 27 20 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -170031.447672  [km]    Vx: -0.6859320555  [km/s]
             Y:   16745.573052  [km]    Vy: -0.9472246858  [km/s]
             Z:   37024.658261  [km]    Vz: -0.2433926022  [km/s]
(Keplerian)  a:  127220.183436  [km]    an:  24.897393891  [deg]
             e:  0.553187923749 [ - ]   ap: 353.862305292  [deg]
             i:  23.1075034268  [deg]   ma: 109.213324408  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2002/11/27 20:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -170031.4476719500    -0.6859320555165400    0.0000000000000000
      Y:      16745.5730518200    -0.9472246858100000    0.0000000000000000
      Z:      37024.6582610020    -0.2433926021927700    0.0000000000000000
              EPOCH : 2002/12/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      17987.3072111164     1.7170526241739075    0.0000000000000000
      Y:     -82792.0480307550     1.5754839966322292    0.0000000000000000
      Z:     -35505.5914400583     0.3033101768626114    0.0000000000000000
              EPOCH : 2003/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:       2508.9642389089     1.7518682003611552    0.0000000000000000
      Y:     -97214.0079004594     1.1759656664196867    0.0000000000000000
      Z:     -38925.7274098168     0.1424126889934607    0.0000000000000000
              EPOCH : 2003/02/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -33233.3237294712     1.6823194369983190    0.0000000000000000
      Y:    -114508.1054075284     0.6050066140338355    0.0000000000000000
      Z:     -39864.6263873757    -0.0708695852010221    0.0000000000000000
              EPOCH : 2003/03/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -122904.3328745191    -1.3644398880470237    0.0000000000000000
      Y:      54873.9730937330    -0.7763164519564361    0.0000000000000000
      Z:      45988.5074124274    -0.0617391190363026    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com" 27-DEC-2002 00:32:03.60
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/12/27)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/12/27)
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20021227142807D.m-matsuoka@ps.jp.nec.com>
Date: Fri, 27 Dec 2002 14:28:07 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 58
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2002 12 24 22 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -182726.687998  [km]    Vx:  0.3537394213  [km/s]
             Y:  -71171.854885  [km]    Vy: -0.8009925854  [km/s]
             Z:    5428.302484  [km]    Vz: -0.3788657388  [km/s]
(Keplerian)  a:  126399.397609  [km]    an:  24.948276309  [deg]
             e:  0.553695044369 [ - ]   ap: 353.608341795  [deg]
             i:  23.4011614694  [deg]   ma: 186.942391606  [deg]
--
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2002/12/24 22:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -182726.6879978200     0.3537394212694600    0.0000000000000000
      Y:     -71171.8548852130    -0.8009925854078600    0.0000000000000000
      Z:       5428.3024838119    -0.3788657388416600    0.0000000000000000
              EPOCH : 2003/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:       2510.7332387665     1.7518521353363448    0.0000000000000000
      Y:     -97214.0227034799     1.1759866128968006    0.0000000000000000
      Z:     -38925.9486376164     0.1423974671154053    0.0000000000000000
              EPOCH : 2003/02/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -33228.5076700973     1.6823250428879399    0.0000000000000000
      Y:    -114507.4803985163     0.6050655631243974    0.0000000000000000
      Z:     -39864.6962728362    -0.0708715356177962    0.0000000000000000
              EPOCH : 2003/03/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -122907.9344360723    -1.3643817620052086    0.0000000000000000
      Y:      54871.1267112785    -0.7763551650660787    0.0000000000000000
      Z:      45989.7934552709    -0.0617462497716712    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com" 31-JAN-2003 00:40:05.12
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/01/31)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/01/31)
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20030131143726W.m-matsuoka@ps.jp.nec.com>
Date: Fri, 31 Jan 2003 14:37:26 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 55
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2003 01 30 21 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -155176.651133  [km]    Vx:  0.7987216627  [km/s]
             Y: -103756.500645  [km]    Vy: -0.5770165988  [km/s]
             Z:  -12752.880047  [km]    Vz: -0.3814188370  [km/s]
(Keplerian)  a:  126766.957724  [km]    an:  24.909544088  [deg]
             e:  0.543990115685 [ - ]   ap: 353.697848275  [deg]
             i:  23.9239506486  [deg]   ma: 224.052209794  [deg]
--
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2003/01/30 21:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -155176.6511325800     0.7987216626838800    0.0000000000000000
      Y:    -103756.5006452700    -0.5770165988299000    0.0000000000000000
      Z:     -12752.8800472270    -0.3814188370138300    0.0000000000000000
              EPOCH : 2003/02/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -33224.8567434505     1.6823349204912754    0.0000000000000000
      Y:    -114506.9432503641     0.6050904778448120    0.0000000000000000
      Z:     -39865.3900361024    -0.0708540365264221    0.0000000000000000
              EPOCH : 2003/03/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -122908.9906172153    -1.3643594142519526    0.0000000000000000
      Y:      54871.5133530998    -0.7763681771752939    0.0000000000000000
      Z:      45989.4256063686    -0.0617632368166384    0.0000000000000000
              EPOCH : 2003/04/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -95890.0311350079    -1.7151031743884810    0.0000000000000000
      Y:      62573.7298044762    -0.6151849140298892    0.0000000000000000
      Z:      45140.1746672890     0.0705898079901253    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com" 28-FEB-2003 00:39:48.92
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/02/28)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/02/28)
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20030228143741P.m-matsuoka@ps.jp.nec.com>
Date: Fri, 28 Feb 2003 14:37:41 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 69
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2003 02 26 21 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:  -68553.185066  [km]    Vx:  1.4899043820  [km/s]
             Y: -123693.204333  [km]    Vy:  0.2067721114  [km/s]
             Z:  -38064.681694  [km]    Vz: -0.1974721313  [km/s]
(Keplerian)  a:  126868.986914  [km]    an:  24.690068939  [deg]
             e:  0.556344155285 [ - ]   ap: 355.159032290  [deg]
             i:  24.4419904257  [deg]   ma: 284.515898684  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2003/02/26 21:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -68553.1850662140     1.4899043819675000    0.0000000000000000
      Y:    -123693.2043330800     0.2067721113935600    0.0000000000000000
      Z:     -38064.6816938020    -0.1974721313382900    0.0000000000000000
              EPOCH : 2003/03/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -122906.0383468873    -1.3643871934536480    0.0000000000000000
      Y:      54874.0974028830    -0.7763522666954851    0.0000000000000000
      Z:      45990.4681927020    -0.0617455007060016    0.0000000000000000
              EPOCH : 2003/04/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -95884.0575354112    -1.7151625639585641    0.0000000000000000
      Y:      62576.8347592873    -0.6151376791954182    0.0000000000000000
      Z:      45140.7737636366     0.0706286250771159    0.0000000000000000
              EPOCH : 2003/05/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      27473.4335939146     1.5755172514361875    0.0000000000000000
      Y:     -74751.4342137471     1.7850530679002061    0.0000000000000000
      Z:     -38069.0470808543     0.4657448398631284    0.0000000000000000
              EPOCH : 2003/06/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -15158.3192366725     1.6126252938372929    0.0000000000000000
      Y:    -112715.3541307837     0.8556162192429070    0.0000000000000000
      Z:     -47393.8988543710     0.0534078005426741    0.0000000000000000
              EPOCH : 2003/07/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -147310.5539136669     0.8109891961384464    0.0000000000000000
      Y:    -116566.3371274310    -0.5016296164756094   -0.0000000000000000
      Z:     -22492.9733479244    -0.3968085475795344    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com" 28-MAR-2003 00:44:00.49
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/03/28)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/03/28)
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20030328144134G.m-matsuoka@ps.jp.nec.com>
Date: Fri, 28 Mar 2003 14:41:34 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 62
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2003 03 26 14 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:  -57041.440729  [km]    Vx: -2.1422329276  [km/s]
             Y:   72296.930614  [km]    Vy: -0.2149187784  [km/s]
             Z:   41634.950771  [km]    Vz:  0.3227244771  [km/s]
(Keplerian)  a:  126598.724333  [km]    an:  24.515017103  [deg]
             e:  0.571395221268 [ - ]   ap: 356.637330526  [deg]
             i:  24.9603861246  [deg]   ma:  38.698885900  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2003/03/26 14:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -57041.4407287170    -2.1422329276366998    0.0000000000000000
      Y:      72296.9306141990    -0.2149187784027800    0.0000000000000000
      Z:      41634.9507709450     0.3227244770571600    0.0000000000000000
              EPOCH : 2003/04/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -95882.1159758327    -1.7151812411956264    0.0000000000000000
      Y:      62578.9289885522    -0.6151105161957178    0.0000000000000000
      Z:      45140.3975642715     0.0706338945129513    0.0000000000000000
              EPOCH : 2003/05/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      27472.3876179640     1.5755383894501416    0.0000000000000000
      Y:     -74752.9388233435     1.7850125659516722    0.0000000000000000
      Z:     -38068.9917422960     0.4657272321419722    0.0000000000000000
              EPOCH : 2003/06/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -15160.2447156907     1.6126316018591660    0.0000000000000000
      Y:    -112716.2410737233     0.8555780455368275    0.0000000000000000
      Z:     -47393.4901758050     0.0533976926844558    0.0000000000000000
              EPOCH : 2003/07/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -147313.0428312802     0.8109689527967024    0.0000000000000000
      Y:    -116563.6742940341    -0.5016591377076175   -0.0000000000000000
      Z:     -22491.7959229082    -0.3968090122473529    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com" 25-APR-2003 04:30:33.84
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/04/25)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/04/25)
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20030425172829T.m-matsuoka@ps.jp.nec.com>
Date: Fri, 25 Apr 2003 17:28:29 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 56
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2003 04 24 14 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -124406.558165  [km]    Vx:  1.0692326496  [km/s]
             Y: -124216.296464  [km]    Vy: -0.2747003118  [km/s]
             Z:  -29389.043161  [km]    Vz: -0.3309856873  [km/s]
(Keplerian)  a:  126769.510407  [km]    an:  24.470375103  [deg]
             e:  0.567645833531 [ - ]   ap: 358.338065274  [deg]
             i:  25.5321208416  [deg]   ma: 247.060524672  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2003/04/24 14:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -124406.5581650000     1.0692326495930999    0.0000000000000000
      Y:    -124216.2964636400    -0.2747003117544200    0.0000000000000000
      Z:     -29389.0431606600    -0.3309856873225100    0.0000000000000000
              EPOCH : 2003/05/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      27475.3976105677     1.5755227997459673    0.0000000000000000
      Y:     -74748.2689468139     1.7850902034743790    0.0000000000000000
      Z:     -38068.5553582951     0.4658292873768680    0.0000000000000000
              EPOCH : 2003/06/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -15147.2910249003     1.6126724290164329    0.0000000000000000
      Y:    -112707.7035722191     0.8557648877768769    0.0000000000000000
      Z:     -47394.6505035379     0.0535205989390840    0.0000000000000000
              EPOCH : 2003/07/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -147301.5864874207     0.8111041854024811    0.0000000000000000
      Y:    -116569.0280635647    -0.5015564997085311   -0.0000000000000000
      Z:     -22501.6267468508    -0.3967815261773558    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com" 30-MAY-2003 01:20:35.33
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/05/30)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/05/30)
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20030530141912B.m-matsuoka@ps.jp.nec.com>
Date: Fri, 30 May 2003 14:19:12 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 56
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2003 05 29 11 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -182061.859721  [km]    Vx: -0.2648083284  [km/s]
             Y:  -29365.277789  [km]    Vy: -0.9668894750  [km/s]
             Z:   24036.918068  [km]    Vz: -0.3786151939  [km/s]
(Keplerian)  a:  127013.214220  [km]    an:  24.528071824  [deg]
             e:  0.552722225805 [ - ]   ap:   0.967659604  [deg]
             i:  26.1924659378  [deg]   ma: 129.937343556  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2003/05/29 11:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -182061.8597212500    -0.2648083283637200    0.0000000000000000
      Y:     -29365.2777891660    -0.9668894749620400    0.0000000000000000
      Z:      24036.9180675070    -0.3786151938622800    0.0000000000000000
              EPOCH : 2003/06/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -15159.1031742196     1.6126634008213481    0.0000000000000000
      Y:    -112713.5859884153     0.8556025724957176    0.0000000000000000
      Z:     -47392.7234653395     0.0534305085801981    0.0000000000000000
              EPOCH : 2003/07/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -147311.7334391318     0.8110050372813228    0.0000000000000000
      Y:    -116562.9065716514    -0.5016389848680755   -0.0000000000000000
      Z:     -22494.2508533407    -0.3967916430196947    0.0000000000000000
              EPOCH : 2003/08/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -159633.0079054511     0.6776165625848094    0.0000000000000000
      Y:    -106846.2838022506    -0.5913193606136212   -0.0000000000000000
      Z:     -16055.4216835024    -0.4148756975613954    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com" 29-JUN-2003 22:37:10.64
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/06/30)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/06/30)
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20030630113733J.m-matsuoka@ps.jp.nec.com>
Date: Mon, 30 Jun 2003 11:37:33 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 62
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2003 06 26 11 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:  -88963.648644  [km]    Vx:  1.2758567934  [km/s]
             Y: -132229.884135  [km]    Vy:  0.0051260581  [km/s]
             Z:  -41744.623598  [km]    Vz: -0.2624899920  [km/s]
(Keplerian)  a:  126854.966138  [km]    an:  24.505450663  [deg]
             e:  0.547684230823 [ - ]   ap:   1.803125865  [deg]
             i:  26.5844762909  [deg]   ma: 263.249289979  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2003/06/26 11:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -88963.6486439620     1.2758567933974001    0.0000000000000000
      Y:    -132229.8841353400     0.0051260581386550    0.0000000000000000
      Z:     -41744.6235984890    -0.2624899919914100    0.0000000000000000
              EPOCH : 2003/07/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -147317.3344831952     0.8109618700144792    0.0000000000000000
      Y:    -116559.0622931692    -0.5016729353330850   -0.0000000000000000
      Z:     -22492.8927024160    -0.3967894005664519    0.0000000000000000
              EPOCH : 2003/08/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -159640.5451488573     0.6775385631495288    0.0000000000000000
      Y:    -106839.8745372603    -0.5913677791826103   -0.0000000000000000
      Z:     -16052.5661003555    -0.4148742748006616    0.0000000000000000
              EPOCH : 2003/09/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -172458.7725325015     0.4939070019716303    0.0000000000000000
      Y:     -95714.2152746789    -0.6953572895331427   -0.0000000000000000
      Z:      -8874.3598739683    -0.4345780326534560    0.0000000000000000
              EPOCH : 2003/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -160217.2723430087    -0.7671775627011665    0.0000000000000000
      Y:       2994.4887870258    -1.0029466586840505    0.0000000000000000
      Z:      36670.5924648676    -0.3244879556595968    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com" 28-JUL-2003 01:15:36.80
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/07/28)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/07/28)
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20030728141535N.m-matsuoka@ps.jp.nec.com>
Date: Mon, 28 Jul 2003 14:15:35 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 62
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2003 07 22 15 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:  -66540.597515  [km]    Vx:  1.4135000279  [km/s]
             Y: -129271.000618  [km]    Vy:  0.2252735085  [km/s]
             Z:  -45640.656090  [km]    Vz: -0.1915088187  [km/s]
(Keplerian)  a:  126699.637185  [km]    an:  24.395823478  [deg]
             e:  0.548095551310 [ - ]   ap:   1.329825337  [deg]
             i:  26.8276035853  [deg]   ma: 277.466782700  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2003/07/22 15:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -66540.5975151120     1.4135000278747001    0.0000000000000000
      Y:    -129271.0006179900     0.2252735084713800    0.0000000000000000
      Z:     -45640.6560901240    -0.1915088187346300    0.0000000000000000
              EPOCH : 2003/08/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -159642.8744668194     0.6775113017727963    0.0000000000000000
      Y:    -106839.1187795001    -0.5913648657302313   -0.0000000000000000
      Z:     -16049.1426007386    -0.4148924122872250    0.0000000000000000
              EPOCH : 2003/09/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -172461.0678975371     0.4938731110637306    0.0000000000000000
      Y:     -95712.8347359438    -0.6953554343229427   -0.0000000000000000
      Z:      -8870.2795903037    -0.4345932254562548    0.0000000000000000
              EPOCH : 2003/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -160214.2624842977    -0.7672365995367815    0.0000000000000000
      Y:       2997.0619268971    -1.0029353199638718    0.0000000000000000
      Z:      36675.5413584964    -0.3244673363549022    0.0000000000000000
              EPOCH : 2003/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -145925.5748304756    -1.0048905757884810    0.0000000000000000
      Y:      16300.6885105568    -0.9983493602360588    0.0000000000000000
      Z:      40966.8038151896    -0.2766491291877320    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com"  3-SEP-2003 08:26:44.96
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/09/03)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/09/03)
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20030903212649Q.m-matsuoka@ps.jp.nec.com>
Date: Wed, 03 Sep 2003 21:26:49 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 61
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2003 08 28 08 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:  -28413.264840  [km]    Vx:  1.5927515584  [km/s]
             Y: -116622.815572  [km]    Vy:  0.6845004599  [km/s]
             Z:  -48787.631271  [km]    Vz: -0.0145481227  [km/s]
(Keplerian)  a:  126658.531371  [km]    an:  24.189813922  [deg]
             e:  0.554009544475 [ - ]   ap:   0.929913012  [deg]
             i:  27.2468415394  [deg]   ma: 299.336958224  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2003/08/28 08:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -28413.2648404180     1.5927515583794001    0.0000000000000000
      Y:    -116622.8155722500     0.6845004599093700    0.0000000000000000
      Z:     -48787.6312713640    -0.0145481226754770    0.0000000000000000
              EPOCH : 2003/09/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -172460.7854155054     0.4938893024193393    0.0000000000000000
      Y:     -95714.8220907560    -0.6953309367911410   -0.0000000000000000
      Z:      -8877.3949990577    -0.4345895979246677    0.0000000000000000
              EPOCH : 2003/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -160218.1680560665    -0.7671778821841000    0.0000000000000000
      Y:       2990.9773230944    -1.0029283142856646    0.0000000000000000
      Z:      36669.5776968691    -0.3245157364359423    0.0000000000000000
              EPOCH : 2003/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -145933.5034027580    -1.0047763875629623    0.0000000000000000
      Y:      16291.6886921333    -0.9983577435462686    0.0000000000000000
      Z:      40960.6517431657    -0.2767227102022765    0.0000000000000000
              EPOCH : 2003/12/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      56779.9116269509    -0.8224381984810115    0.0000000000000000
      Y:      11995.9533928325     2.7096849063516122    0.0000000000000000
      Z:      -6863.1673583548     1.5759731698752082    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com" 26-SEP-2003 07:31:57.81
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/09/26)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/09/26)
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20030926202904S.m-matsuoka@ps.jp.nec.com>
Date: Fri, 26 Sep 2003 20:29:04 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 62
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2003 09 25 03 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:  -95121.235826  [km]    Vx: -1.7228523558  [km/s]
             Y:   56491.724813  [km]    Vy: -0.7162007293  [km/s]
             Z:   47757.483037  [km]    Vz:  0.0260441332  [km/s]
(Keplerian)  a:  127187.565884  [km]    an:  24.086943253  [deg]
             e:  0.556160997234 [ - ]   ap:   2.800824942  [deg]
             i:  27.8486648292  [deg]   ma:  52.851768815  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2003/09/25 03:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:     -95121.2358263400    -1.7228523557758000    0.0000000000000000
      Y:      56491.7248126610    -0.7162007293358200    0.0000000000000000
      Z:      47757.4830366550     0.0260441331923410    0.0000000000000000
              EPOCH : 2003/10/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -160216.4172374131    -0.7671978687479230    0.0000000000000000
      Y:       2991.6935233639    -1.0029368961143543    0.0000000000000000
      Z:      36675.8787328696    -0.3244577863238539    0.0000000000000000
              EPOCH : 2003/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -145929.6674936821    -1.0048240441635350    0.0000000000000000
      Y:      16294.0803147601    -0.9983613823188900    0.0000000000000000
      Z:      40966.7426086068    -0.2766481093106551    0.0000000000000000
              EPOCH : 2003/12/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      56781.6549227890    -0.8220410070333809    0.0000000000000000
      Y:      11987.7430666392     2.7097977497953645    0.0000000000000000
      Z:      -6870.5303922079     1.5759217651404047    0.0000000000000000
              EPOCH : 2004/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      47699.9503322699     1.1438949542813748    0.0000000000000000
      Y:     -58953.0419815666     2.0318669765787409    0.0000000000000000
      Z:     -41782.2629028880     0.7917930368649504    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com" 30-OCT-2003 23:31:03.65
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/10/31)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/10/31)
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20031031133016D.m-matsuoka@ps.jp.nec.com>
Date: Fri, 31 Oct 2003 13:30:16 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 61
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2003 10 30 05 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X:   11301.664866  [km]    Vx:  1.5519388877  [km/s]
             Y:  -94873.724350  [km]    Vy:  1.3163969313  [km/s]
             Z:  -50260.442136  [km]    Vz:  0.3135665441  [km/s]
(Keplerian)  a:  126755.376977  [km]    an:  24.062895323  [deg]
             e:  0.567428800054 [ - ]   ap:   5.829170045  [deg]
             i:  28.8493473750  [deg]   ma: 316.531623008  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2003/10/30 05:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      11301.6648663020     1.5519388876527000    0.0000000000000000
      Y:     -94873.7243503110     1.3163969313135999    0.0000000000000000
      Z:     -50260.4421358400     0.3135665441228900    0.0000000000000000
              EPOCH : 2003/11/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -145931.3537798052    -1.0047932633901464    0.0000000000000000
      Y:      16290.1076452654    -0.9983735761395549    0.0000000000000000
      Z:      40964.3489925381    -0.2766828155039200    0.0000000000000000
              EPOCH : 2003/12/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      56781.9619129829    -0.8220305629558933    0.0000000000000000
      Y:      11986.6219299766     2.7097848959980362    0.0000000000000000
      Z:      -6870.5806176159     1.5759440964398483    0.0000000000000000
              EPOCH : 2004/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      47699.4871671712     1.1438954925880724    0.0000000000000000
      Y:     -58955.1420405452     2.0318154165395055    0.0000000000000000
      Z:     -41783.6179789744     0.7918017135518784    0.0000000000000000
              EPOCH : 2004/02/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      22364.7156036033     1.4592629344446792    0.0000000000000000
      Y:     -90532.0748535578     1.4109722996406167    0.0000000000000000
      Z:     -53083.6664741560     0.4048052618837562    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com" 28-NOV-2003 03:43:02.37
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/11/28)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/11/28)
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20031128174128O.m-matsuoka@ps.jp.nec.com>
Date: Fri, 28 Nov 2003 17:41:28 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 62
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2003 11 26 20 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -124906.597606  [km]    Vx: -1.3065585811  [km/s]
             Y:   32428.294071  [km]    Vy: -0.9729847185  [km/s]
             Z:   45191.207930  [km]    Vz: -0.1986055559  [km/s]
(Keplerian)  a:  127057.191710  [km]    an:  24.111987616  [deg]
             e:  0.550385699038 [ - ]   ap:   7.678424261  [deg]
             i:  29.2708397066  [deg]   ma:  66.720332734  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2003/11/26 20:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -124906.5976059800    -1.3065585810608999    0.0000000000000000
      Y:      32428.2940714820    -0.9729847184579899    0.0000000000000000
      Z:      45191.2079297220    -0.1986055558644700    0.0000000000000000
              EPOCH : 2003/12/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      56782.1803990425    -0.8220612485856645    0.0000000000000000
      Y:      11986.9034962733     2.7098187961898308    0.0000000000000000
      Z:      -6871.4997847693     1.5758416629161820    0.0000000000000000
              EPOCH : 2004/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      47702.0710565203     1.1438166416345159    0.0000000000000000
      Y:     -58953.7431934558     2.0318962603344839    0.0000000000000000
      Z:     -41781.1741830741     0.7917549892371668    0.0000000000000000
              EPOCH : 2004/02/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      22370.5688789074     1.4592078409001228    0.0000000000000000
      Y:     -90530.0430493508     1.4110881046660992    0.0000000000000000
      Z:     -53079.9817014144     0.4047972589919092    0.0000000000000000
              EPOCH : 2004/03/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -173714.3503288695     0.3061761106463290    0.0000000000000000
      Y:     -89214.6009322878    -0.7745128320439968   -0.0000000000000000
      Z:      -7101.1189838175    -0.4892243371907344    0.0000000000000000

From:	SMTP%"m-matsuoka@ps.jp.nec.com" 25-DEC-2003 23:43:25.71
To:	SARDI
CC:
Subj:	[MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/12/26)
Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/12/26)
From: Masatoshi Matsuoka <m-matsuoka@ps.jp.nec.com>
To: gtl_month@ayame.d1.nas.nec.co.jp
X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3
 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?=
Mime-Version: 1.0
Content-Type: Text/Plain; charset=us-ascii
Content-Transfer-Encoding: 7bit
Message-Id: <20031226134122O.m-matsuoka@ps.jp.nec.com>
Date: Fri, 26 Dec 2003 13:41:22 +0900
X-Dispatcher: imput version 20000228(IM140)
Lines: 63
The following data is updated orbit solution
based on 3 path data.
regards,
Masatoshi
==
NEC Aerospace Systems,Ltd
  			  Masatoshi Matsuoka
                          m-matsuoka@ps.jp.nec.com
-----
 GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC)
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
EPOCH  : 2003 12 25 05 00 00.0000 [UTC]  S/C MASS : 654.612 [kg]
                                                   ~~~~~~~~~~
ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2]
(Cartesian)  X: -128553.735733  [km]    Vx:  0.9097694453  [km/s]
             Y: -131065.246395  [km]    Vy: -0.3500346718  [km/s]
             Z:  -38219.554031  [km]    Vz: -0.3938072425  [km/s]
(Keplerian)  a:  126703.674375  [km]    an:  24.120475392  [deg]
             e:  0.540891182079 [ - ]   ap:   9.129202474  [deg]
             i:  29.6700890359  [deg]   ma: 221.729612497  [deg]
           <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>>
              EPOCH : 2003/12/25 05:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -128553.7357326600     0.9097694453117000    0.0000000000000000
      Y:    -131065.2463954300    -0.3500346717816000    0.0000000000000000
      Z:     -38219.5540306700    -0.3938072425491600    0.0000000000000000
              EPOCH : 2004/01/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      47704.0899050717     1.1437870050338297    0.0000000000000000
      Y:     -58951.6063886564     2.0318794785523133    0.0000000000000000
      Z:     -41781.6366320001     0.7918486562564666    0.0000000000000000
              EPOCH : 2004/02/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:      22373.5471294516     1.4591956446983370    0.0000000000000000
      Y:     -90527.2894059196     1.4110954516667953    0.0000000000000000
      Z:     -53081.7972371544     0.4048839574166222    0.0000000000000000
              EPOCH : 2004/03/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -173713.8228567744     0.3061913804616233    0.0000000000000000
      Y:     -89213.3591272777    -0.7745061607245813   -0.0000000000000000
      Z:      -7107.5027891565    -0.4892424929779011    0.0000000000000000
              EPOCH : 2004/04/01 00:00:00 (UTC)
                  R(KM)                V(KM/S)               DV(KM/S)
      X:    -177891.1389899360     0.0867522492058356    0.0000000000000000
      Y:     -72688.6509738762    -0.8661772713538958   -0.0000000000000000
      Z:       2662.7388220795    -0.4984663869541716    0.0000000000000000