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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  19920.769
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   73.5
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   1.431
   ET - UTC  (sec) :   68.18
   UT1 - UTC (sec) :    0.00
 
 
   Maneuvers contained within the current ephemeris are as follows:
 
 
   IMPULSIVE TIG (GMT)   M50 DVx(FPS)      LVLH DVx(FPS)      DVmag(FPS) 
   IMPULSIVE TIG (MET)   M50 DVy(FPS)      LVLH DVy(FPS)      Invar Sph HA
   DT                    M50 DVz(FPS)      LVLH DVz(FPS)      Invar Sph HP 
   ------------------------------------------------------------------------
   276/01:38:44.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              229.8  
   000/00:00:00.000           0.0               0.0              222.6  
   
   277/05:58:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              229.8  
   000/00:00:00.000           0.0               0.0              222.5  
   
   278/10:10:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              229.7  
   000/00:00:00.000           0.0               0.0              222.7  
   
   280/09:58:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              229.6  
   000/00:00:00.000           0.0               0.0              222.5  
   
   281/08:14:18.140          -2.3              -2.5              2.5    
   N/A                        1.1              -0.0              228.1  
   000/00:06:36.280           0.1              -0.0              222.6  
   
   283/20:35:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              228.1  
   000/00:00:00.000           0.0               0.0              222.6  
   
 
 
    Coasting Arc #1 (Orbit 802)
    ---------------------------------------
 
    Vector Time (GMT): 2020/272/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922360.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -759042.60                 A    =         6793863.75  meter
     Y    =       -4430423.38  meter          E    =           .0006431
     Z    =        5090354.72                 I    =           51.51362
     XDOT =       7432.096846                 Wp   =          120.81535
     YDOT =        714.184410  meter/sec      RA   =          196.07331  deg
     ZDOT =       1724.974629                 TA   =          312.44441
                                              MA   =          312.49877
                                              Ha   =            229.787  n.mi
                                              Hp   =            222.595
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2490297.25                 X    =         -734169.81
     Y    =      -14535509.77  feet           Y    =        -4438772.11  meter
     Z    =       16700638.84                 Z    =         5086728.32
     XDOT =      24383.519836                 XDOT =        7415.179339
     YDOT =       2343.124706  feet/sec       YDOT =         797.200976  meter/sec
     ZDOT =       5659.365582                 ZDOT =        1761.035589
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4311700.63                 X    =         1314206.35
     Y    =       14122721.36  feet           Y    =         4304605.47  meter
     Z    =       16683882.68                 Z    =         5085247.44
     XDOT =     -23420.432651                 XDOT =       -7138.547872
     YDOT =        249.072750  feet/sec       YDOT =          75.917374  meter/sec
     ZDOT =       5825.898384                 ZDOT =        1775.733827
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   20272.55149341  .00016717  00000-0  10270-3 0  9002
    2 25544  51.6421 197.0085 0001162 100.5667 259.5613 15.48830030  8030
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20272.55149341   =   yrday.fracday
    Element set:     900
    Inclination:       51.6421  deg
    RA of node:       197.0085  deg
    Eccentricity:     .0001162     
    Arg of perigee:   100.5667  deg
    Mean anomaly:     259.5613  deg
    Mean motion:   15.48830030  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             803
    Checksum:              276
 
 
    Coasting Arc #2 (Orbit 817)
    ---------------------------------------
 
    Vector Time (GMT): 2020/273/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922360.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1204823.18                 A    =         6793969.53  meter
     Y    =        4353908.15  meter          E    =           .0014275
     Z    =       -5087343.23                 I    =           51.54782
     XDOT =      -7438.461786                 Wp   =           78.69550
     YDOT =        -20.948621  meter/sec      RA   =          191.12200  deg
     ZDOT =      -1781.086145                 TA   =          174.01478
                                              MA   =          173.99771
                                              Ha   =            229.826  n.mi
                                              Hp   =            222.587
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3952831.96                 X    =         1180758.32
     Y    =       14284475.57  feet           Y    =         4367246.36  meter
     Z    =      -16690758.64                 Z    =        -5081549.50
     XDOT =     -24404.402184                 XDOT =       -7429.023196
     YDOT =        -68.729071  feet/sec       YDOT =        -104.078214  meter/sec
     ZDOT =      -5843.458482                 ZDOT =       -1817.196333
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5968794.33                 X    =        -1819288.51
     Y    =      -13599177.83  feet           Y    =        -4145029.40  meter
     Z    =      -16663985.23                 Z    =        -5079182.70
     XDOT =      23155.904529                 XDOT =        7057.919701
     YDOT =      -2804.716506  feet/sec       YDOT =        -854.877591  meter/sec
     ZDOT =      -6010.236275                 ZDOT =       -1831.920017
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   20273.51934585  .00016717  00000-0  10270-3 0  9012
    2 25544  51.6433 192.2222 0001272  98.3936 261.7358 15.48819907  8185
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20273.51934585   =   yrday.fracday
    Element set:     901
    Inclination:       51.6433  deg
    RA of node:       192.2222  deg
    Eccentricity:     .0001272     
    Arg of perigee:    98.3936  deg
    Mean anomaly:     261.7358  deg
    Mean motion:   15.48819907  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             818
    Checksum:              321
 
 
    Coasting Arc #3 (Orbit 833)
    ---------------------------------------
 
    Vector Time (GMT): 2020/274/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922360.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1649632.45                 A    =         6793985.03  meter
     Y    =       -4216232.11  meter          E    =           .0006775
     Z    =        5061571.67                 I    =           51.58182
     XDOT =       7406.330962                 Wp   =          121.31218
     YDOT =       -672.999570  meter/sec      RA   =          186.17387  deg
     ZDOT =       1847.943585                 TA   =          310.73240
                                              MA   =          310.79120
                                              Ha   =            229.803  n.mi
                                              Hp   =            222.583
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5412179.97                 X    =        -1626948.98
     Y    =      -13832782.50  feet           Y    =        -4234552.16  meter
     Z    =       16606206.25                 Z    =         5053613.87
     XDOT =      24298.986095                 XDOT =        7404.329907
     YDOT =      -2208.003837  feet/sec       YDOT =        -590.187675  meter/sec
     ZDOT =       6062.807036                 ZDOT =        1883.915964
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7574416.75                 X    =         2308682.22
     Y    =       12825202.58  feet           Y    =         3909121.75  meter
     Z    =       16569430.88                 Z    =         5050362.53
     XDOT =     -22699.473668                 XDOT =       -6918.799574
     YDOT =       5336.170839  feet/sec       YDOT =        1626.464872  meter/sec
     ZDOT =       6228.963288                 ZDOT =        1898.588010
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   20274.55171330  .00016717  00000-0  10270-3 0  9029
    2 25544  51.6436 187.1176 0001178 105.0713 255.0568 15.48839673  8342
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20274.55171330   =   yrday.fracday
    Element set:     902
    Inclination:       51.6436  deg
    RA of node:       187.1176  deg
    Eccentricity:     .0001178     
    Arg of perigee:   105.0713  deg
    Mean anomaly:     255.0568  deg
    Mean motion:   15.48839673  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             834
    Checksum:              305
 
 
    Coasting Arc #4 (Orbit 848)
    ---------------------------------------
 
    Vector Time (GMT): 2020/275/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922360.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2066276.83                 A    =         6794054.12  meter
     Y    =        4052645.24  meter          E    =           .0014043
     Z    =       -5059109.18                 I    =           51.61638
     XDOT =      -7286.091918                 Wp   =           78.25638
     YDOT =       1347.647928  meter/sec      RA   =          181.22761  deg
     ZDOT =      -1897.979273                 TA   =          173.29836
                                              MA   =          173.27956
                                              Ha   =            229.800  n.mi
                                              Hp   =            222.580
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6779123.45                 X    =         2045379.81
     Y    =       13296080.17  feet           Y    =         4075634.49  meter
     Z    =      -16598127.22                 Z    =        -5049123.09
     XDOT =     -23904.501043                 XDOT =       -7291.400833
     YDOT =       4421.417088  feet/sec       YDOT =        1266.139751  meter/sec
     ZDOT =      -6226.966118                 ZDOT =       -1933.385560
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9049792.39                 X    =        -2758376.72
     Y    =      -11932032.16  feet           Y    =        -3636883.40  meter
     Z    =      -16551977.40                 Z    =        -5045042.71
     XDOT =      21894.154967                 XDOT =        6673.338434
     YDOT =      -7748.363542  feet/sec       YDOT =       -2361.701207  meter/sec
     ZDOT =      -6390.521187                 ZDOT =       -1947.830858
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   20275.51955493  .00016717  00000-0  10270-3 0  9037
    2 25544  51.6442 182.3319 0001294 100.7312 259.3983 15.48840357  8496
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20275.51955493   =   yrday.fracday
    Element set:     903
    Inclination:       51.6442  deg
    RA of node:       182.3319  deg
    Eccentricity:     .0001294     
    Arg of perigee:   100.7312  deg
    Mean anomaly:     259.3983  deg
    Mean motion:   15.48840357  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             849
    Checksum:              317
 
 
    Coasting Arc #5 (Orbit 857)
    ---------------------------------------
 
    Vector Time (GMT): 2020/276/01:38:44.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922360.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6788547.61                 A    =         6804731.27  meter
     Y    =          98596.05  meter          E    =           .0012655
     Z    =        -364009.99                 I    =           51.66980
     XDOT =       -383.235661                 Wp   =          135.45294
     YDOT =       4752.427023  meter/sec      RA   =          178.40267  deg
     ZDOT =      -5995.252475                 TA   =           48.46054
                                              MA   =           48.35207
                                              Ha   =            229.814  n.mi
                                              Hp   =            222.571
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       22272137.81                 X    =         6788708.71
     Y    =         323477.84  feet           Y    =          174511.32  meter
     Z    =       -1194258.49                 Z    =         -331033.15
     XDOT =      -1257.334846                 XDOT =        -407.228430
     YDOT =      15591.952175  feet/sec       YDOT =        4748.006676  meter/sec
     ZDOT =     -19669.463500                 ZDOT =       -5997.172837
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18431857.81                 X    =         5618030.26
     Y    =      -12520385.52  feet           Y    =        -3816213.51  meter
     Z    =       -1041910.75                 Z    =         -317574.40
     XDOT =       7114.425756                 XDOT =        2168.476970
     YDOT =      12068.685124  feet/sec       YDOT =        3678.535226  meter/sec
     ZDOT =     -19678.313371                 ZDOT =       -5997.949916
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   20276.10025701  .00016717  00000-0  10270-3 0  9044
    2 25544  51.6428 179.4591 0001313 116.7713 243.3571 15.48830213  8589
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20276.10025701   =   yrday.fracday
    Element set:     904
    Inclination:       51.6428  deg
    RA of node:       179.4591  deg
    Eccentricity:     .0001313     
    Arg of perigee:   116.7713  deg
    Mean anomaly:     243.3571  deg
    Mean motion:   15.48830213  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             858
    Checksum:              287
 
 
    Coasting Arc #6 (Orbit 873)
    ---------------------------------------
 
    Vector Time (GMT): 2020/277/01:38:44.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922360.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6771088.63                 A    =         6804871.28  meter
     Y    =         543057.69  meter          E    =           .0013050
     Z    =         293542.37                 I    =           51.70309
     XDOT =       -113.675381                 Wp   =           53.27452
     YDOT =      -4757.686561  meter/sec      RA   =          173.45900  deg
     ZDOT =       6002.124736                 TA   =          309.87897
                                              MA   =          309.99366
                                              Ha   =            229.813  n.mi
                                              Hp   =            222.701
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -22214857.71                 X    =        -6778083.91
     Y    =        1781685.35  feet           Y    =          467299.44  meter
     Z    =         963065.51                 Z    =          260633.54
     XDOT =       -372.950726                 XDOT =         -89.620376
     YDOT =     -15609.207877  feet/sec       YDOT =       -4758.822727  meter/sec
     ZDOT =      19692.010288                 ZDOT =        6001.631386
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16928627.99                 X    =        -5159845.81
     Y    =       14503985.81  feet           Y    =         4420814.88  meter
     Z    =         811018.57                 Z    =          247198.46
     XDOT =      -8528.394744                 XDOT =       -2599.454718
     YDOT =     -11093.757184  feet/sec       YDOT =       -3381.377190  meter/sec
     ZDOT =      19689.710822                 ZDOT =        6001.423858
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   20277.13261532  .00016717  00000-0  10270-3 0  9053
    2 25544  51.6423 174.3542 0001206 114.2976 245.8300 15.48788685  8749
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20277.13261532   =   yrday.fracday
    Element set:     905
    Inclination:       51.6423  deg
    RA of node:       174.3542  deg
    Eccentricity:     .0001206     
    Arg of perigee:   114.2976  deg
    Mean anomaly:     245.8300  deg
    Mean motion:   15.48788685  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             874
    Checksum:              306
 
 
    Coasting Arc #7 (Orbit 875)
    ---------------------------------------
 
    Vector Time (GMT): 2020/277/05:58:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922360.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1764120.09                 A    =         6794181.78  meter
     Y    =        4235861.78  meter          E    =           .0014078
     Z    =       -5023546.89                 I    =           51.67197
     XDOT =      -7345.887852                 Wp   =          105.87587
     YDOT =       -655.907237  meter/sec      RA   =          172.54958  deg
     ZDOT =       2027.580505                 TA   =          183.86868
                                              MA   =          183.87958
                                              Ha   =            229.820  n.mi
                                              Hp   =            222.544
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5787795.56                 X    =        -1786953.75
     Y    =       13897184.33  feet           Y    =         4216006.02  meter
     Z    =      -16481453.04                 Z    =        -5032172.25
     XDOT =     -24100.681930                 XDOT =       -7347.856318
     YDOT =      -2151.926632  feet/sec       YDOT =        -738.065055  meter/sec
     ZDOT =       6652.167012                 ZDOT =        1991.891778
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14730236.83                 X    =         4489776.18
     Y    =        2887169.95  feet           Y    =          880009.40  meter
     Z    =      -16521288.59                 Z    =        -5035688.76
     XDOT =       2757.915996                 XDOT =         840.612796
     YDOT =      23032.931839  feet/sec       YDOT =        7020.437625  meter/sec
     ZDOT =       6487.267824                 ZDOT =        1977.319233
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   20277.26165785  .00016717  00000-0  10270-3 0  9061
    2 25544  51.6404 173.7168 0001291 112.3921 247.7365 15.48810465  8764
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20277.26165785   =   yrday.fracday
    Element set:     906
    Inclination:       51.6404  deg
    RA of node:       173.7168  deg
    Eccentricity:     .0001291     
    Arg of perigee:   112.3921  deg
    Mean anomaly:     247.7365  deg
    Mean motion:   15.48810465  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             876
    Checksum:              319
 
 
    Coasting Arc #8 (Orbit 891)
    ---------------------------------------
 
    Vector Time (GMT): 2020/278/05:58:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922360.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1339829.03                 A    =         6794024.34  meter
     Y    =       -4360958.27  meter          E    =           .0006436
     Z    =        5030175.38                 I    =           51.70509
     XDOT =       7401.514808                 Wp   =           65.65827
     YDOT =        -21.182618  meter/sec      RA   =          167.60893  deg
     ZDOT =      -1985.226698                 TA   =           43.64111
                                              MA   =           43.59023
                                              Ha   =            229.699  n.mi
                                              Hp   =            222.597
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4395764.54                 X    =         1364060.82
     Y    =      -14307605.88  feet           Y    =        -4345839.48  meter
     Z    =       16503200.08                 Z    =         5036743.05
     XDOT =      24283.185067                 XDOT =        7410.844859
     YDOT =        -69.496777  feet/sec       YDOT =          61.638452  meter/sec
     ZDOT =      -6513.210952                 ZDOT =       -1949.249696
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14886952.20                 X    =        -4537543.03
     Y    =       -1186093.66  feet           Y    =         -361521.35  meter
     Z    =       16533535.03                 Z    =         5039421.48
     XDOT =      -5258.240114                 XDOT =       -1602.711587
     YDOT =     -22685.604006  feet/sec       YDOT =       -6914.572101  meter/sec
     ZDOT =      -6346.963741                 ZDOT =       -1934.554548
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   20278.29400787  .00016717  00000-0  10270-3 0  9070
    2 25544  51.6404 168.6112 0001188 114.9589 245.1684 15.48841847  8921
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20278.29400787   =   yrday.fracday
    Element set:     907
    Inclination:       51.6404  deg
    RA of node:       168.6112  deg
    Eccentricity:     .0001188     
    Arg of perigee:   114.9589  deg
    Mean anomaly:     245.1684  deg
    Mean motion:   15.48841847  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             892
    Checksum:              335
 
 
    Coasting Arc #9 (Orbit 894)
    ---------------------------------------
 
    Vector Time (GMT): 2020/278/10:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 937074.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6665967.16                 A    =         6804732.90  meter
     Y    =        1294705.57  meter          E    =           .0013163
     Z    =         337110.46                 I    =           51.74855
     XDOT =       -605.258861                 Wp   =           53.03356
     YDOT =      -4719.502724  meter/sec      RA   =          166.76547  deg
     ZDOT =       6003.120567                 TA   =          310.58644
                                              MA   =          310.70092
                                              Ha   =            229.720  n.mi
                                              Hp   =            222.656
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21869971.01                 X    =        -6681587.04
     Y    =        4247721.70  feet           Y    =         1220074.64  meter
     Z    =        1106005.45                 Z    =          304691.15
     XDOT =      -1985.757417                 XDOT =        -581.599268
     YDOT =     -15483.932820  feet/sec       YDOT =       -4726.138447  meter/sec
     ZDOT =      19695.277450                 ZDOT =        6000.238200
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       22235173.99                 X    =         6777281.03
     Y    =        1498245.99  feet           Y    =          456665.38  meter
     Z    =         956198.81                 Z    =          291449.40
     XDOT =      -1807.389897                 XDOT =        -550.892441
     YDOT =      13888.160867  feet/sec       YDOT =        4233.111432  meter/sec
     ZDOT =      19681.943781                 ZDOT =        5999.056464
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   20278.48757445  .00016717  00000-0  10270-3 0  9088
    2 25544  51.6426 167.6545 0001102 109.3580 250.7689 15.48832660  8952
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20278.48757445   =   yrday.fracday
    Element set:     908
    Inclination:       51.6426  deg
    RA of node:       167.6545  deg
    Eccentricity:     .0001102     
    Arg of perigee:   109.3580  deg
    Mean anomaly:     250.7689  deg
    Mean motion:   15.48832660  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             895
    Checksum:              334
 
 
    Coasting Arc #10 (Orbit 909)
    ---------------------------------------
 
    Vector Time (GMT): 2020/279/10:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 937074.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6525663.17                 A    =         6804732.31  meter
     Y    =       -1882614.20  meter          E    =           .0012600
     Z    =        -313081.09                 I    =           51.78153
     XDOT =       1055.789730                 Wp   =          135.17536
     YDOT =       4632.861572  meter/sec      RA   =          161.82725  deg
     ZDOT =      -6008.117874                 TA   =           48.18472
                                              MA   =           48.07718
                                              Ha   =            229.759  n.mi
                                              Hp   =            222.616
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21409656.06                 X    =         6547750.92
     Y    =       -6176555.76  feet           Y    =        -1809516.07  meter
     Z    =       -1027168.94                 Z    =         -281327.56
     XDOT =       3463.877068                 XDOT =        1033.089824
     YDOT =      15199.677073  feet/sec       YDOT =        4644.540923  meter/sec
     ZDOT =     -19711.672814                 ZDOT =       -6003.044537
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -22272192.62                 X    =        -6788564.31
     Y    =         867516.90  feet           Y    =          264419.15  meter
     Z    =        -880420.18                 Z    =         -268352.07
     XDOT =        209.576512                 XDOT =          63.878921
     YDOT =     -13994.187477  feet/sec       YDOT =       -4265.428343  meter/sec
     ZDOT =     -19688.217931                 ZDOT =       -6000.968825
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   20279.45539765  .00016717  00000-0  10270-3 0  9090
    2 25544  51.6429 162.8685 0001152 115.0702 245.0567 15.48834040  9106
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20279.45539765   =   yrday.fracday
    Element set:     909
    Inclination:       51.6429  deg
    RA of node:       162.8685  deg
    Eccentricity:     .0001152     
    Arg of perigee:   115.0702  deg
    Mean anomaly:     245.0567  deg
    Mean motion:   15.48834040  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             910
    Checksum:              310
 
 
    Coasting Arc #11 (Orbit 924)
    ---------------------------------------
 
    Vector Time (GMT): 2020/280/09:58:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 937074.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3560387.14                 A    =         6799251.89  meter
     Y    =        4569798.77  meter          E    =           .0006346
     Z    =       -3566099.78                 I    =           51.79474
     XDOT =      -6077.711064                 Wp   =          100.83191
     YDOT =      -1242.514814  meter/sec      RA   =          156.90279  deg
     ZDOT =       4481.367260                 TA   =          217.32324
                                              MA   =          217.36735
                                              Ha   =            229.648  n.mi
                                              Hp   =            222.545
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11681060.18                 X    =        -3593900.95
     Y    =       14992778.13  feet           Y    =         4529796.46  meter
     Z    =      -11699802.42                 Z    =        -3583476.67
     XDOT =     -19939.996930                 XDOT =       -6085.133560
     YDOT =      -4076.492173  feet/sec       YDOT =       -1310.521481  meter/sec
     ZDOT =      14702.648490                 ZDOT =        4451.825510
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15235626.61                 X    =         4643818.99
     Y    =      -11279200.81  feet           Y    =        -3437900.41  meter
     Z    =      -11780120.98                 Z    =        -3590580.87
     XDOT =      17358.102124                 XDOT =        5290.749527
     YDOT =       8252.965934  feet/sec       YDOT =        2515.504017  meter/sec
     ZDOT =      14566.100273                 ZDOT =        4439.747363
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   20280.42321805  .00016717  00000-0  10270-3 0  9105
    2 25544  51.6425 158.0825 0001108 117.3371 242.7892 15.48863180  9251
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20280.42321805   =   yrday.fracday
    Element set:     910
    Inclination:       51.6425  deg
    RA of node:       158.0825  deg
    Eccentricity:     .0001108     
    Arg of perigee:   117.3371  deg
    Mean anomaly:     242.7892  deg
    Mean motion:   15.48863180  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             925
    Checksum:              290
 
 
    Coasting Arc #12 (Orbit 939)
    ---------------------------------------
 
    Vector Time (GMT): 2020/281/08:17:36.280
    Vector Time (MET): N/A
    Weight (LBS)     : 936804.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -122172.26                 A    =         6792297.48  meter
     Y    =       -4473682.04  meter          E    =           .0004004
     Z    =        5107460.35                 I    =           51.80361
     XDOT =       7132.233707                 Wp   =           50.35852
     YDOT =      -2190.395118  meter/sec      RA   =          152.32598  deg
     ZDOT =      -1744.585671                 TA   =           56.50148
                                              MA   =           56.46323
                                              Ha   =            228.143  n.mi
                                              Hp   =            222.650
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -400827.63                 X    =          -96946.73
     Y    =      -14677434.51  feet           Y    =        -4474907.11  meter
     Z    =       16756759.67                 Z    =         5106928.22
     XDOT =      23399.716885                 XDOT =        7164.671648
     YDOT =      -7186.335689  feet/sec       YDOT =       -2110.456028  meter/sec
     ZDOT =      -5723.706269                 ZDOT =       -1709.860554
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9051630.02                 X    =        -2758936.83
     Y    =       11564513.86  feet           Y    =         3524863.82  meter
     Z    =       16754305.55                 Z    =         5106712.33
     XDOT =     -21720.603481                 XDOT =       -6620.439941
     YDOT =      -8924.954888  feet/sec       YDOT =       -2720.326250  meter/sec
     ZDOT =      -5563.176197                 ZDOT =       -1695.656105
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   20281.39101646  .00016717  00000-0  10270-3 0  9112
    2 25544  51.6415 153.2963 0001230 252.7414 107.3601 15.49333722  9404
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20281.39101646   =   yrday.fracday
    Element set:     911
    Inclination:       51.6415  deg
    RA of node:       153.2963  deg
    Eccentricity:     .0001230     
    Arg of perigee:   252.7414  deg
    Mean anomaly:     107.3601  deg
    Mean motion:   15.49333722  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             940
    Checksum:              270
 
 
    Coasting Arc #13 (Orbit 954)
    ---------------------------------------
 
    Vector Time (GMT): 2020/282/08:17:36.280
    Vector Time (MET): N/A
    Weight (LBS)     : 936804.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         373708.19                 A    =         6792434.58  meter
     Y    =        4503090.29  meter          E    =           .0012054
     Z    =       -5082413.86                 I    =           51.83421
     XDOT =      -6917.674848                 Wp   =          106.37582
     YDOT =       2682.575979  meter/sec      RA   =          147.38839  deg
     ZDOT =       1868.516254                 TA   =          181.71815
                                              MA   =          181.72229
                                              Ha   =            228.120  n.mi
                                              Hp   =            222.645
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1226076.73                 X    =          348013.38
     Y    =       14773918.27  feet           Y    =         4507125.66  meter
     Z    =      -16674586.15                 Z    =        -5080660.94
     XDOT =     -22695.783623                 XDOT =       -6956.234422
     YDOT =       8801.102293  feet/sec       YDOT =        2605.001991  meter/sec
     ZDOT =       6130.302672                 ZDOT =        1834.818649
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8271986.75                 X    =         2521301.56
     Y    =      -12313242.56  feet           Y    =        -3753076.33  meter
     Z    =      -16666494.57                 Z    =        -5079947.55
     XDOT =      22301.135725                 XDOT =        6797.386169
     YDOT =       6896.727159  feet/sec       YDOT =        2102.122438  meter/sec
     ZDOT =       5974.495161                 ZDOT =        1821.026125
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   20282.35853315  .00016717  00000-0  10270-3 0  9127
    2 25544  51.6422 148.5071 0001174 259.1221 100.9797 15.49339436  9552
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20282.35853315   =   yrday.fracday
    Element set:     912
    Inclination:       51.6422  deg
    RA of node:       148.5071  deg
    Eccentricity:     .0001174     
    Arg of perigee:   259.1221  deg
    Mean anomaly:     100.9797  deg
    Mean motion:   15.49339436  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             955
    Checksum:              303
 
 
    Coasting Arc #14 (Orbit 970)
    ---------------------------------------
 
    Vector Time (GMT): 2020/283/08:17:36.280
    Vector Time (MET): N/A
    Weight (LBS)     : 936804.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -618192.15                 A    =         6792550.08  meter
     Y    =       -4512704.62  meter          E    =           .0004825
     Z    =        5036833.66                 I    =           51.86243
     XDOT =       6688.236261                 Wp   =           49.59364
     YDOT =      -3156.812023  meter/sec      RA   =          142.45477  deg
     ZDOT =      -2003.132163                 TA   =           59.84361
                                              MA   =           59.79582
                                              Ha   =            228.122  n.mi
                                              Hp   =            222.612
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2028189.48                 X    =         -592150.17
     Y    =      -14805461.34  feet           Y    =        -4519472.07  meter
     Z    =       16525044.82                 Z    =         5033893.94
     XDOT =      21943.032353                 XDOT =        6732.769802
     YDOT =     -10356.994826  feet/sec       YDOT =       -3081.770370  meter/sec
     ZDOT =      -6571.955915                 ZDOT =       -1970.534719
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7447946.36                 X    =        -2270134.05
     Y    =       12972731.62  feet           Y    =         3954088.60  meter
     Z    =       16511470.97                 Z    =         5032696.35
     XDOT =     -22748.429240                 XDOT =       -6933.721232
     YDOT =      -4869.592408  feet/sec       YDOT =       -1484.251766  meter/sec
     ZDOT =      -6421.206954                 ZDOT =       -1957.183880
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   20283.39054727  .00016717  00000-0  10270-3 0  9133
    2 25544  51.6421 143.4007 0001165 266.6677  93.4340 15.49355773  9712
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20283.39054727   =   yrday.fracday
    Element set:     913
    Inclination:       51.6421  deg
    RA of node:       143.4007  deg
    Eccentricity:     .0001165     
    Arg of perigee:   266.6677  deg
    Mean anomaly:      93.4340  deg
    Mean motion:   15.49355773  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             971
    Checksum:              309
 
 
    Coasting Arc #15 (Orbit 978)
    ---------------------------------------
 
    Vector Time (GMT): 2020/283/20:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 936804.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2924852.60                 A    =         6791243.56  meter
     Y    =       -3012963.60  meter          E    =           .0001616
     Z    =        5336523.68                 I    =           51.87309
     XDOT =       5724.882145                 Wp   =          136.39735
     YDOT =      -5085.380944  meter/sec      RA   =          139.94398  deg
     ZDOT =        265.347402                 TA   =          311.07243
                                              MA   =          311.08639
                                              Ha   =            228.112  n.mi
                                              Hp   =            222.644
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9595973.10                 X    =        -2916865.44
     Y    =       -9885051.17  feet           Y    =        -3045626.72  meter
     Z    =       17508279.79                 Z    =         5322335.13
     XDOT =      18782.421735                 XDOT =        5780.034000
     YDOT =     -16684.320683  feet/sec       YDOT =       -5021.052833  meter/sec
     ZDOT =        870.562344                 ZDOT =         293.290930
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2708543.19                 X    =         -825563.96
     Y    =      -13592405.41  feet           Y    =        -4142965.17  meter
     Z    =       17442680.61                 Z    =         5316529.05
     XDOT =      23858.011752                 XDOT =        7271.921982
     YDOT =      -3466.115374  feet/sec       YDOT =       -1056.471966  meter/sec
     ZDOT =        999.812435                 ZDOT =         304.742830
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   20283.90655146  .00016717  00000-0  10270-3 0  9143
    2 25544  51.6434 140.8438 0001460 247.9940 112.1055 15.49378318  9798
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20283.90655146   =   yrday.fracday
    Element set:     914
    Inclination:       51.6434  deg
    RA of node:       140.8438  deg
    Eccentricity:     .0001460     
    Arg of perigee:   247.9940  deg
    Mean anomaly:     112.1055  deg
    Mean motion:   15.49378318  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             979
    Checksum:              315
 
 
    Coasting Arc #16 (Orbit 993)
    ---------------------------------------
 
    Vector Time (GMT): 2020/284/20:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 936804.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3066671.43                 A    =         6791343.20  meter
     Y    =        2866599.50  meter          E    =           .0013397
     Z    =       -5350146.85                 I    =           51.89752
     XDOT =      -5339.921116                 Wp   =           90.73583
     YDOT =       5477.661852  meter/sec      RA   =          135.01248  deg
     ZDOT =       -126.328920                 TA   =          178.06444
                                              MA   =          178.05925
                                              Ha   =            228.026  n.mi
                                              Hp   =            222.833
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10061257.96                 X    =         3060376.50
     Y    =        9404854.00  feet           Y    =         2900857.97  meter
     Z    =      -17552975.22                 Z    =        -5335265.35
     XDOT =     -17519.426235                 XDOT =       -5400.163469
     YDOT =      17971.331534  feet/sec       YDOT =        5417.610186  meter/sec
     ZDOT =       -414.464961                 ZDOT =        -152.414759
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3591953.55                 X    =         1094827.44
     Y    =       13386148.37  feet           Y    =         4080098.02  meter
     Z    =      -17484165.15                 Z    =        -5329173.54
     XDOT =     -23427.696771                 XDOT =       -7140.761976
     YDOT =       5589.354579  feet/sec       YDOT =        1703.635276  meter/sec
     ZDOT =       -535.149630                 ZDOT =        -163.113607
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   20284.87406170  .00016717  00000-0  10270-3 0  9152
    2 25544  51.6428 136.0565 0001481 253.7132 106.3855 15.49340325  9947
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20284.87406170   =   yrday.fracday
    Element set:     915
    Inclination:       51.6428  deg
    RA of node:       136.0565  deg
    Eccentricity:     .0001481     
    Arg of perigee:   253.7132  deg
    Mean anomaly:     106.3855  deg
    Mean motion:   15.49340325  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             994
    Checksum:              303
 
 
    Coasting Arc #17 (Orbit 1009)
    ---------------------------------------
 
    Vector Time (GMT): 2020/285/20:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 936804.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3194865.65                 A    =         6791186.58  meter
     Y    =       -2707833.05  meter          E    =           .0000992
     Z    =        5345282.67                 I    =           51.92152
     XDOT =       4941.292197                 Wp   =          109.37629
     YDOT =      -5855.618528  meter/sec      RA   =          130.08171  deg
     ZDOT =        -13.278069                 TA   =          340.74797
                                              MA   =          340.75172
                                              Ha   =            228.053  n.mi
                                              Hp   =            222.675
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10481842.70                 X    =        -3190312.89
     Y    =       -8883966.71  feet           Y    =        -2743534.74  meter
     Z    =       17537016.63                 Z    =         5329774.29
     XDOT =      16211.588574                 XDOT =        5006.468740
     YDOT =     -19211.346878  feet/sec       YDOT =       -5799.997030  meter/sec
     ZDOT =        -43.563218                 ZDOT =          10.883399
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4451431.05                 X    =        -1356796.19
     Y    =      -13095376.23  feet           Y    =        -3991470.68  meter
     Z    =       17465300.63                 Z    =         5323423.63
     XDOT =      22873.040240                 XDOT =        6971.702665
     YDOT =      -7682.676451  feet/sec       YDOT =       -2341.679782  meter/sec
     ZDOT =         68.243835                 ZDOT =          20.800721
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   20285.90606598  .00016717  00000-0  10270-3 0  9164
    2 25544  51.6437 130.9489 0001501 259.3738 100.7243 15.49387251 10100
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20285.90606598   =   yrday.fracday
    Element set:     916
    Inclination:       51.6437  deg
    RA of node:       130.9489  deg
    Eccentricity:     .0001501     
    Arg of perigee:   259.3738  deg
    Mean anomaly:     100.7243  deg
    Mean motion:   15.49387251  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1010
    Checksum:              308
 
 
    Coasting Arc #18 (Orbit 1024)
    ---------------------------------------
 
    Vector Time (GMT): 2020/286/20:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 936804.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3325169.39                 A    =         6791315.37  meter
     Y    =        2556817.18  meter          E    =           .0013418
     Z    =       -5352733.36                 I    =           51.94142
     XDOT =      -4503.366174                 Wp   =           91.52078
     YDOT =       6183.105064  meter/sec      RA   =          125.15273  deg
     ZDOT =        155.914351                 TA   =          179.96235
                                              MA   =          179.96225
                                              Ha   =            228.009  n.mi
                                              Hp   =            222.827
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10909348.41                 X    =         3322331.84
     Y    =        8388507.81  feet           Y    =         2593985.50  meter
     Z    =      -17561461.16                 Z    =        -5336587.90
     XDOT =     -14774.823407                 XDOT =       -4572.930168
     YDOT =      20285.777769  feet/sec       YDOT =        6132.356243  meter/sec
     ZDOT =        511.530024                 ZDOT =         133.869386
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5295174.73                 X    =         1613969.26
     Y    =       12804650.62  feet           Y    =         3902857.51  meter
     Z    =      -17486792.48                 Z    =        -5329974.35
     XDOT =     -22056.800260                 XDOT =       -6722.912719
     YDOT =       9680.532022  feet/sec       YDOT =        2950.626160  meter/sec
     ZDOT =        409.493313                 ZDOT =         124.813562
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   20286.87356795  .00016717  00000-0  10270-3 0  9173
    2 25544  51.6428 126.1611 0001411 268.5360  91.5629 15.49348595 10256
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20286.87356795   =   yrday.fracday
    Element set:     917
    Inclination:       51.6428  deg
    RA of node:       126.1611  deg
    Eccentricity:     .0001411     
    Arg of perigee:   268.5360  deg
    Mean anomaly:      91.5629  deg
    Mean motion:   15.49348595  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1025
    Checksum:              323
 
             

Curator: Kim Dismukes | Responsible NASA Official: Amiko Kauderer | Updated: 06/08/2009
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