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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  15234.4853
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   69.0
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   1.995
   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 
   ------------------------------------------------------------------------
   143/16:17:59.113          -4.8               7.1              7.1    
   N/A                        3.2              -0.7              226.0  
   000/00:19:54.227           4.2              -0.1              220.4  
   
   143/19:55:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              226.2  
   000/00:00:00.000           0.0               0.0              220.4  
   
   143/21:05:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              226.0  
   000/00:00:00.000           0.0               0.0              220.5  
   
   144/08:35:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              226.0  
   000/00:00:00.000           0.0               0.0              220.2  
   
   147/06:36:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              226.4  
   000/00:00:00.000           0.0               0.0              219.9  
   
   154/16:09:25.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              227.3  
   000/00:00:00.000           0.0               0.0              218.6  
   
   155/08:42:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              227.5  
   000/00:00:00.000           0.0               0.0              218.3  
   
 
 
    Coasting Arc #1 (Orbit 1125)
    ---------------------------------------
 
    Vector Time (GMT): 2019/142/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 965984.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4960358.62                 A    =         6792450.31  meter
     Y    =       -4348557.35  meter          E    =           .0007010
     Z    =       -1611816.08                 I    =           51.95448
     XDOT =       2151.051153                 Wp   =          129.59202
     YDOT =       4579.014087  meter/sec      RA   =          127.73663  deg
     ZDOT =      -5754.950023                 TA   =           67.94960
                                              MA   =           67.87516
                                              Ha   =            223.579  n.mi
                                              Hp   =            216.748
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16274142.45                 X    =         5016446.12
     Y    =      -14266920.45  feet           Y    =        -4292773.32  meter
     Z    =       -5288110.51                 Z    =        -1587584.75
     XDOT =       7057.254438                 XDOT =        2127.641953
     YDOT =      15023.012096  feet/sec       YDOT =        4602.938546  meter/sec
     ZDOT =     -18881.069629                 ZDOT =       -5744.557188
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3807416.69                 X    =        -1160500.61
     Y    =      -21331907.21  feet           Y    =        -6501965.32  meter
     Z    =       -5177852.60                 Z    =        -1578209.47
     XDOT =      15018.834397                 XDOT =        4577.740724
     YDOT =       1873.936058  feet/sec       YDOT =         571.175710  meter/sec
     ZDOT =     -18834.336707                 ZDOT =       -5740.705828
  
  
    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   19142.52913619  .00016717  00000-0  10270-3 0  9000
    2 25544  51.6368 128.6541 0001985  14.7360 345.3850 15.52691816 11264
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19142.52913619   =   yrday.fracday
    Element set:     900
    Inclination:       51.6368  deg
    RA of node:       128.6541  deg
    Eccentricity:     .0001985     
    Arg of perigee:    14.7360  deg
    Mean anomaly:     345.3850  deg
    Mean motion:   15.52691816  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1126
    Checksum:              308
 
 
    Coasting Arc #2 (Orbit 1141)
    ---------------------------------------
 
    Vector Time (GMT): 2019/143/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 965984.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4952995.05                 A    =         6790324.45  meter
     Y    =        3744835.38  meter          E    =           .0014341
     Z    =        2730103.85                 I    =           51.96743
     XDOT =      -1286.659811                 Wp   =           72.22598
     YDOT =      -5498.669769  meter/sec      RA   =          122.79237  deg
     ZDOT =       5190.063170                 TA   =          318.50414
                                              MA   =          318.61294
                                              Ha   =            223.522  n.mi
                                              Hp   =            216.726
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16249983.76                 X    =        -5007764.11
     Y    =       12286205.30  feet           Y    =         3689140.93  meter
     Z    =        8957033.64                 Z    =         2705911.45
     XDOT =      -4221.324840                 XDOT =       -1250.287001
     YDOT =     -18040.255149  feet/sec       YDOT =       -5512.855395  meter/sec
     ZDOT =      17027.766307                 ZDOT =        5183.900676
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2459708.18                 X    =          749719.05
     Y    =       20271210.21  feet           Y    =         6178664.87  meter
     Z    =        8846984.62                 Z    =         2696560.91
     XDOT =     -16305.035394                 XDOT =       -4969.774788
     YDOT =      -5467.227694  feet/sec       YDOT =       -1666.411001  meter/sec
     ZDOT =      17000.301746                 ZDOT =        5181.691972
  
  
    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   19143.55891986  .00016717  00000-0  10270-3 0  9017
    2 25544  51.6370 123.5326 0001750  13.5677 346.5521 15.52729014 11428
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19143.55891986   =   yrday.fracday
    Element set:     901
    Inclination:       51.6370  deg
    RA of node:       123.5326  deg
    Eccentricity:     .0001750     
    Arg of perigee:    13.5677  deg
    Mean anomaly:     346.5521  deg
    Mean motion:   15.52729014  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1142
    Checksum:              299
 
 
    Coasting Arc #3 (Orbit 1143)
    ---------------------------------------
 
    Vector Time (GMT): 2019/143/16:27:56.227
    Vector Time (MET): N/A
    Weight (LBS)     : 965074.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3014277.70                 A    =         6797742.85  meter
     Y    =        6030639.78  meter          E    =           .0014199
     Z    =        -794045.72                 I    =           51.98410
     XDOT =      -4566.409862                 Wp   =           10.05097
     YDOT =      -1499.668875  meter/sec      RA   =          121.83980  deg
     ZDOT =       5974.459382                 TA   =          341.41097
                                              MA   =          341.46279
                                              Ha   =            226.019  n.mi
                                              Hp   =            220.437
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9889362.52                 X    =        -3077632.96
     Y    =       19785563.57  feet           Y    =         5996577.87  meter
     Z    =       -2605136.88                 Z    =         -808841.10
     XDOT =     -14981.659651                 XDOT =       -4578.321420
     YDOT =      -4920.173473  feet/sec       YDOT =       -1550.801024  meter/sec
     ZDOT =      19601.244693                 ZDOT =        5952.248300
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21735607.40                 X    =         6625013.14
     Y    =       -4058868.58  feet           Y    =        -1237143.14  meter
     Z    =       -2672772.30                 Z    =         -814661.00
     XDOT =       4895.380171                 XDOT =        1492.111876
     YDOT =      13436.393167  feet/sec       YDOT =        4095.412637  meter/sec
     ZDOT =      19500.641416                 ZDOT =        5943.795504
  
  
    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   19143.68764416  .00016717  00000-0  10270-3 0  9029
    2 25544  51.6408 122.8911 0007360 326.1202  33.9478 15.51143083 11447
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19143.68764416   =   yrday.fracday
    Element set:     902
    Inclination:       51.6408  deg
    RA of node:       122.8911  deg
    Eccentricity:     .0007360     
    Arg of perigee:   326.1202  deg
    Mean anomaly:      33.9478  deg
    Mean motion:   15.51143083  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1144
    Checksum:              290
 
 
    Coasting Arc #4 (Orbit 1146)
    ---------------------------------------
 
    Vector Time (GMT): 2019/143/19:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 965074.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4363226.92                 A    =         6786900.47  meter
     Y    =        -594212.16  meter          E    =           .0003384
     Z    =        5163706.14                 I    =           51.95068
     XDOT =       2787.511541                 Wp   =          358.62894
     YDOT =      -6967.495145  meter/sec      RA   =          121.15007  deg
     ZDOT =       1556.921722                 TA   =           76.44061
                                              MA   =           76.40292
                                              Ha   =            226.177  n.mi
                                              Hp   =            220.432
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14315048.94                 X    =        -4381340.45
     Y    =       -1949514.95  feet           Y    =         -643106.74  meter
     Z    =       16941293.10                 Z    =         5142467.10
     XDOT =       9145.379071                 XDOT =        2857.654210
     YDOT =     -22859.236039  feet/sec       YDOT =       -6935.931241  meter/sec
     ZDOT =       5108.010899                 ZDOT =        1570.631931
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14392219.29                 X    =         4386748.44
     Y    =        2199560.68  feet           Y    =          670426.09  meter
     Z    =       16845017.17                 Z    =         5134361.23
     XDOT =      -9347.572768                 XDOT =       -2849.140180
     YDOT =      21647.103619  feet/sec       YDOT =        6598.037183  meter/sec
     ZDOT =       5170.809956                 ZDOT =        1576.062875
  
  
    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   19143.88092002  .00016717  00000-0  10270-3 0  9037
    2 25544  51.6412 121.9322 0007410 326.7363  33.3321 15.51133737 11477
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19143.88092002   =   yrday.fracday
    Element set:     903
    Inclination:       51.6412  deg
    RA of node:       121.9322  deg
    Eccentricity:     .0007410     
    Arg of perigee:   326.7363  deg
    Mean anomaly:      33.3321  deg
    Mean motion:   15.51133737  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1147
    Checksum:              268
 
 
    Coasting Arc #5 (Orbit 1146)
    ---------------------------------------
 
    Vector Time (GMT): 2019/143/21:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 965074.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2557613.95                 A    =         6797338.75  meter
     Y    =        6165082.78  meter          E    =           .0013272
     Z    =       -1240320.55                 I    =           51.98478
     XDOT =      -4853.472866                 Wp   =            5.76688
     YDOT =       -834.875506  meter/sec      RA   =          120.88395  deg
     ZDOT =       5876.623347                 TA   =          340.82425
                                              MA   =          340.87416
                                              Ha   =            225.992  n.mi
                                              Hp   =            220.473
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8391121.87                 X    =        -2620338.78
     Y    =       20226649.55  feet           Y    =         6136131.19  meter
     Z    =       -4069293.13                 Z    =        -1252896.08
     XDOT =     -15923.467407                 XDOT =       -4872.321752
     YDOT =      -2739.092866  feet/sec       YDOT =        -889.256558  meter/sec
     ZDOT =      19280.260325                 ZDOT =        5853.001063
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2255940.63                 X    =          687610.70
     Y    =      -21770784.41  feet           Y    =        -6635735.09  meter
     Z    =       -4126875.69                 Z    =        -1257871.71
     XDOT =      14579.756782                 XDOT =        4443.909867
     YDOT =      -2112.481705  feet/sec       YDOT =        -643.884424  meter/sec
     ZDOT =      19173.195922                 ZDOT =        5843.990117
  
  
    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   19143.88091881  .00016717  00000-0  10270-3 0  9042
    2 25544  51.6394 121.9306 0007440 325.1939  34.8724 15.51148117 11474
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19143.88091881   =   yrday.fracday
    Element set:     904
    Inclination:       51.6394  deg
    RA of node:       121.9306  deg
    Eccentricity:     .0007440     
    Arg of perigee:   325.1939  deg
    Mean anomaly:      34.8724  deg
    Mean motion:   15.51148117  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1147
    Checksum:              310
 
 
    Coasting Arc #6 (Orbit 1154)
    ---------------------------------------
 
    Vector Time (GMT): 2019/144/08:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 965074.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         482404.06                 A    =         6793781.12  meter
     Y    =       -6010945.72  meter          E    =           .0010537
     Z    =        3127101.06                 I    =           51.98242
     XDOT =       5501.672545                 Wp   =           61.57910
     YDOT =      -2113.568300  meter/sec      RA   =          118.50493  deg
     ZDOT =      -4894.051855                 TA   =           82.66493
                                              MA   =           82.54518
                                              Ha   =            226.019  n.mi
                                              Hp   =            220.230
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1582690.49                 X    =          534394.58
     Y    =      -19720950.51  feet           Y    =        -6005260.81  meter
     Z    =       10259517.90                 Z    =         3129569.96
     XDOT =      18050.106774                 XDOT =        5548.670781
     YDOT =      -6934.279198  feet/sec       YDOT =       -2051.781384  meter/sec
     ZDOT =     -16056.600575                 ZDOT =       -4867.212860
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1769080.62                 X    =         -539215.77
     Y    =      -19698990.13  feet           Y    =        -6004252.19  meter
     Z    =       10271253.47                 Z    =         3130678.06
     XDOT =      15323.576076                 XDOT =        4670.625988
     YDOT =      -9714.360075  feet/sec       YDOT =       -2960.936951  meter/sec
     ZDOT =     -15934.677709                 ZDOT =       -4856.889766
  
  
    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   19144.39632340  .00016717  00000-0  10270-3 0  9051
    2 25544  51.6405 119.3734 0007145 329.5529  30.5206 15.51178791 11556
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19144.39632340   =   yrday.fracday
    Element set:     905
    Inclination:       51.6405  deg
    RA of node:       119.3734  deg
    Eccentricity:     .0007145     
    Arg of perigee:   329.5529  deg
    Mean anomaly:      30.5206  deg
    Mean motion:   15.51178791  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1155
    Checksum:              301
 
 
    Coasting Arc #7 (Orbit 1169)
    ---------------------------------------
 
    Vector Time (GMT): 2019/145/08:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 965074.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -589465.46                 A    =         6795185.28  meter
     Y    =        6276633.36  meter          E    =           .0009760
     Z    =       -2521062.71                 I    =           52.00362
     XDOT =      -5258.694051                 Wp   =            5.35225
     YDOT =       1642.323005  meter/sec      RA   =          113.56875  deg
     ZDOT =       5329.523747                 TA   =          326.53713
                                              MA   =          326.59876
                                              Ha   =            226.165  n.mi
                                              Hp   =            219.998
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1933941.80                 X    =         -647362.83
     Y    =       20592629.14  feet           Y    =         6269718.09  meter
     Z    =       -8271203.12                 Z    =        -2524066.08
     XDOT =     -17252.933237                 XDOT =       -5302.556013
     YDOT =       5388.198834  feet/sec       YDOT =        1583.270801  meter/sec
     ZDOT =      17485.314131                 ZDOT =        5303.872608
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1908182.82                 X    =          581614.12
     Y    =       20589325.69  feet           Y    =         6275626.47  meter
     Z    =       -8285397.58                 Z    =        -2525389.18
     XDOT =     -14594.413122                 XDOT =       -4448.377119
     YDOT =       8327.375697  feet/sec       YDOT =        2538.184113  meter/sec
     ZDOT =      17368.807766                 ZDOT =        5294.012607
  
  
    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   19145.36270512  .00016717  00000-0  10270-3 0  9069
    2 25544  51.6420 114.5778 0007090 333.5661  26.5127 15.51190299 11700
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19145.36270512   =   yrday.fracday
    Element set:     906
    Inclination:       51.6420  deg
    RA of node:       114.5778  deg
    Eccentricity:     .0007090     
    Arg of perigee:   333.5661  deg
    Mean anomaly:      26.5127  deg
    Mean motion:   15.51190299  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1170
    Checksum:              293
 
 
    Coasting Arc #8 (Orbit 1185)
    ---------------------------------------
 
    Vector Time (GMT): 2019/146/08:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 965074.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         676503.53                 A    =         6796508.28  meter
     Y    =       -6505445.49  meter          E    =           .0010080
     Z    =        1841415.09                 I    =           52.01804
     XDOT =       5036.983482                 Wp   =           84.28511
     YDOT =      -1088.272428  meter/sec      RA   =          108.63533  deg
     ZDOT =      -5667.612438                 TA   =           75.60486
                                              MA   =           75.49300
                                              Ha   =            226.348  n.mi
                                              Hp   =            219.847
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2219499.78                 X    =          740254.42
     Y    =      -21343325.09  feet           Y    =        -6497524.07  meter
     Z    =        6041388.09                 Z    =         1844855.54
     XDOT =      16525.536358                 XDOT =        5076.308637
     YDOT =      -3570.447599  feet/sec       YDOT =       -1031.724951  meter/sec
     ZDOT =     -18594.528996                 ZDOT =       -5643.049217
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2117181.16                 X    =         -645316.82
     Y    =      -21349124.80  feet           Y    =        -6507213.24  meter
     Z    =        6057597.66                 Z    =         1846355.77
     XDOT =      14047.649275                 XDOT =        4281.723499
     YDOT =      -6663.077150  feet/sec       YDOT =       -2030.905915  meter/sec
     ZDOT =     -18482.997912                 ZDOT =       -5633.617763
  
  
    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   19146.39351157  .00016717  00000-0  10270-3 0  9079
    2 25544  51.6400 109.4624 0007183 337.8936  22.1904 15.51168275 11867
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19146.39351157   =   yrday.fracday
    Element set:     907
    Inclination:       51.6400  deg
    RA of node:       109.4624  deg
    Eccentricity:     .0007183     
    Arg of perigee:   337.8936  deg
    Mean anomaly:      22.1904  deg
    Mean motion:   15.51168275  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1186
    Checksum:              310
 
 
    Coasting Arc #9 (Orbit 1199)
    ---------------------------------------
 
    Vector Time (GMT): 2019/147/06:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 965074.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4381456.10                 A    =         6788066.30  meter
     Y    =       -1769867.21  meter          E    =           .0013382
     Z    =       -4884620.60                 I    =           51.99970
     XDOT =        165.298931                 Wp   =           40.20629
     YDOT =       7242.398032  meter/sec      RA   =          104.14033  deg
     ZDOT =      -2469.738188                 TA   =          205.58745
                                              MA   =          205.65373
                                              Ha   =            226.446  n.mi
                                              Hp   =            219.928
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14374855.97                 X    =         4424648.46
     Y    =       -5806650.95  feet           Y    =        -1720628.79  meter
     Z    =      -16025658.15                 Z    =        -4863232.31
     XDOT =        542.319327                 XDOT =          96.296733
     YDOT =      23761.148399  feet/sec       YDOT =        7243.860907  meter/sec
     ZDOT =      -8102.815578                 ZDOT =       -2469.102226
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15555111.74                 X    =         4741198.06
     Y    =       -1223963.25  feet           Y    =         -373064.00  meter
     Z    =      -15928459.16                 Z    =        -4854994.35
     XDOT =      -6606.597445                 XDOT =       -2013.690901
     YDOT =      21722.785456  feet/sec       YDOT =        6621.105007  meter/sec
     ZDOT =      -8100.612313                 ZDOT =       -2469.066633
  
  
    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   19147.29546722  .00016717  00000-0  10270-3 0  9084
    2 25544  51.6411 104.9856 0007149 339.5502  20.5362 15.51151160 12008
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19147.29546722   =   yrday.fracday
    Element set:     908
    Inclination:       51.6411  deg
    RA of node:       104.9856  deg
    Eccentricity:     .0007149     
    Arg of perigee:   339.5502  deg
    Mean anomaly:      20.5362  deg
    Mean motion:   15.51151160  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1200
    Checksum:              286
 
 
    Coasting Arc #10 (Orbit 1215)
    ---------------------------------------
 
    Vector Time (GMT): 2019/148/06:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 965074.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4261793.81                 A    =         6786916.46  meter
     Y    =        1235265.77  meter          E    =           .0004638
     Z    =        5132535.69                 I    =           52.00290
     XDOT =       -130.331820                 Wp   =           29.35933
     YDOT =      -7475.451672  meter/sec      RA   =           99.19753  deg
     ZDOT =       1694.208493                 TA   =           44.37275
                                              MA   =           44.33560
                                              Ha   =            226.736  n.mi
                                              Hp   =            219.505
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13982263.16                 X    =        -4300221.30
     Y    =        4052709.23  feet           Y    =         1187392.16  meter
     Z    =       16839027.86                 Z    =         5111740.14
     XDOT =       -427.597836                 XDOT =         -54.959068
     YDOT =     -24525.760078  feet/sec       YDOT =       -7476.487825  meter/sec
     ZDOT =       5558.426815                 ZDOT =        1693.757892
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14666078.39                 X    =        -4470220.69
     Y    =         -82366.76  feet           Y    =          -25105.39  meter
     Z    =       16744561.94                 Z    =         5103742.48
     XDOT =       6459.164844                 XDOT =        1968.753444
     YDOT =     -22592.993391  feet/sec       YDOT =       -6886.344385  meter/sec
     ZDOT =       5557.100978                 ZDOT =        1693.804378
  
  
    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   19148.32627018  .00016717  00000-0  10270-3 0  9098
    2 25544  51.6409  99.8697 0007260 344.5645  15.5284 15.51171142 12164
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19148.32627018   =   yrday.fracday
    Element set:     909
    Inclination:       51.6409  deg
    RA of node:        99.8697  deg
    Eccentricity:     .0007260     
    Arg of perigee:   344.5645  deg
    Mean anomaly:      15.5284  deg
    Mean motion:   15.51171142  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1216
    Checksum:              316
 
 
    Coasting Arc #11 (Orbit 1230)
    ---------------------------------------
 
    Vector Time (GMT): 2019/149/06:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 965074.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4200382.30                 A    =         6786293.30  meter
     Y    =        -699873.51  meter          E    =           .0015521
     Z    =       -5296130.64                 I    =           52.00611
     XDOT =        133.204210                 Wp   =           55.20100
     YDOT =       7599.975316  meter/sec      RA   =           94.25480  deg
     ZDOT =       -891.925210                 TA   =          206.25547
                                              MA   =          206.33423
                                              Ha   =            226.762  n.mi
                                              Hp   =            219.528
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13780781.83                 X    =         4233622.18
     Y    =       -2296172.94  feet           Y    =         -652715.64  meter
     Z    =      -17375756.70                 Z    =        -5275645.90
     XDOT =        437.021685                 XDOT =          52.541731
     YDOT =      24934.302217  feet/sec       YDOT =        7601.013953  meter/sec
     ZDOT =      -2926.263813                 ZDOT =        -891.473495
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14008624.12                 X    =         4269828.63
     Y    =        1471172.26  feet           Y    =          448413.31  meter
     Z    =      -17282748.09                 Z    =        -5267781.62
     XDOT =      -6066.264390                 XDOT =       -1848.997386
     YDOT =      23140.540083  feet/sec       YDOT =        7053.236617  meter/sec
     ZDOT =      -2924.961653                 ZDOT =        -891.528312
  
  
    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   19149.29264711  .00016717  00000-0  10270-3 0  9104
    2 25544  51.6421  95.0742 0007308 347.4990  12.5979 15.51155723 12317
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19149.29264711   =   yrday.fracday
    Element set:     910
    Inclination:       51.6421  deg
    RA of node:        95.0742  deg
    Eccentricity:     .0007308     
    Arg of perigee:   347.4990  deg
    Mean anomaly:      12.5979  deg
    Mean motion:   15.51155723  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1231
    Checksum:              305
 
 
    Coasting Arc #12 (Orbit 1246)
    ---------------------------------------
 
    Vector Time (GMT): 2019/150/06:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 965074.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4175515.85                 A    =         6785978.63  meter
     Y    =         114238.03  meter          E    =           .0007295
     Z    =        5346725.34                 I    =           52.00487
     XDOT =       -140.059661                 Wp   =           11.49197
     YDOT =      -7663.772644  meter/sec      RA   =           89.31096  deg
     ZDOT =         61.303329                 TA   =           77.96743
                                              MA   =           77.88569
                                              Ha   =            227.002  n.mi
                                              Hp   =            219.134
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13699198.98                 X    =        -4202454.68
     Y    =         374796.67  feet           Y    =           67393.42  meter
     Z    =       17541749.80                 Z    =         5326376.59
     XDOT =       -459.513323                 XDOT =         -54.648540
     YDOT =     -25143.611038  feet/sec       YDOT =       -7664.861331  meter/sec
     ZDOT =        201.126407                 ZDOT =          60.829778
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13476214.51                 X    =        -4107550.18
     Y    =       -3071012.94  feet           Y    =         -936044.74  meter
     Z    =       17449413.55                 Z    =         5318581.25
     XDOT =       5581.080290                 XDOT =        1701.113272
     YDOT =     -23485.944135  feet/sec       YDOT =       -7158.515772  meter/sec
     ZDOT =        199.750472                 ZDOT =          60.883944
  
  
    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   19150.32344862  .00016717  00000-0  10270-3 0  9117
    2 25544  51.6404  89.9584 0007329 352.6548   7.4495 15.51168880 12475
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19150.32344862   =   yrday.fracday
    Element set:     911
    Inclination:       51.6404  deg
    RA of node:        89.9584  deg
    Eccentricity:     .0007329     
    Arg of perigee:   352.6548  deg
    Mean anomaly:       7.4495  deg
    Mean motion:   15.51168880  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1247
    Checksum:              326
 
 
    Coasting Arc #13 (Orbit 1261)
    ---------------------------------------
 
    Vector Time (GMT): 2019/151/06:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 965074.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4213342.72                 A    =         6786224.13  meter
     Y    =         433180.29  meter          E    =           .0014961
     Z    =       -5313375.55                 I    =           52.00515
     XDOT =        158.916968                 Wp   =           66.86157
     YDOT =       7615.187263  meter/sec      RA   =           84.36816  deg
     ZDOT =        754.248104                 TA   =          210.27837
                                              MA   =          210.36489
                                              Ha   =            227.021  n.mi
                                              Hp   =            219.195
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13823302.89                 X    =         4233995.42
     Y    =        1421195.18  feet           Y    =          480412.84  meter
     Z    =      -17432334.50                 Z    =        -5292858.21
     XDOT =        521.381129                 XDOT =          70.086190
     YDOT =      24984.210182  feet/sec       YDOT =        7616.467626  meter/sec
     ZDOT =       2474.567271                 ZDOT =         754.805070
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13230506.42                 X    =         4032658.36
     Y    =        4614387.64  feet           Y    =         1406465.35  meter
     Z    =      -17339288.07                 Z    =        -5285015.00
     XDOT =      -4967.140156                 XDOT =       -1513.984319
     YDOT =      23455.403262  feet/sec       YDOT =        7149.206914  meter/sec
     ZDOT =       2476.305770                 ZDOT =         754.777999
  
  
    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   19151.28982357  .00016717  00000-0  10270-3 0  9121
    2 25544  51.6416  85.1632 0007378 354.4386   5.6682 15.51151485 12622
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19151.28982357   =   yrday.fracday
    Element set:     912
    Inclination:       51.6416  deg
    RA of node:        85.1632  deg
    Eccentricity:     .0007378     
    Arg of perigee:   354.4386  deg
    Mean anomaly:       5.6682  deg
    Mean motion:   15.51151485  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1262
    Checksum:              317
 
 
    Coasting Arc #14 (Orbit 1277)
    ---------------------------------------
 
    Vector Time (GMT): 2019/152/06:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 965074.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4289638.41                 A    =         6786784.76  meter
     Y    =       -1010800.47  meter          E    =           .0010989
     Z    =        5160230.27                 I    =           52.00253
     XDOT =       -145.436348                 Wp   =           20.68266
     YDOT =      -7498.715757  meter/sec      RA   =           79.42406  deg
     ZDOT =      -1578.744280                 TA   =           84.53231
                                              MA   =           84.40697
                                              Ha   =            227.206  n.mi
                                              Hp   =            218.814
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14073616.82                 X    =        -4303082.46
     Y    =       -3316274.52  feet           Y    =        -1058846.00  meter
     Z    =       16929889.35                 Z    =         5139359.71
     XDOT =       -477.153374                 XDOT =         -53.903977
     YDOT =     -24602.085816  feet/sec       YDOT =       -7499.830149  meter/sec
     ZDOT =      -5179.607219                 ZDOT =       -1579.229346
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13141321.08                 X    =        -4005474.67
     Y    =       -6289978.73  feet           Y    =        -1917185.52  meter
     Z    =       16835301.25                 Z    =         5131399.82
     XDOT =       4402.847499                 XDOT =        1341.987918
     YDOT =     -23163.108464  feet/sec       YDOT =       -7060.115460  meter/sec
     ZDOT =      -5181.009741                 ZDOT =       -1579.171769
  
  
    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   19152.32062115  .00016717  00000-0  10270-3 0  9139
    2 25544  51.6411  80.0469 0007468 359.2965    .8174 15.51178250 12784
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19152.32062115   =   yrday.fracday
    Element set:     913
    Inclination:       51.6411  deg
    RA of node:        80.0469  deg
    Eccentricity:     .0007468     
    Arg of perigee:   359.2965  deg
    Mean anomaly:        .8174  deg
    Mean motion:   15.51178250  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1278
    Checksum:              297
 
 
    Coasting Arc #15 (Orbit 1292)
    ---------------------------------------
 
    Vector Time (GMT): 2019/153/06:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 965074.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4420138.95                 A    =         6787863.97  meter
     Y    =        1512428.97  meter          E    =           .0012474
     Z    =       -4933103.87                 I    =           51.99829
     XDOT =        118.422290                 Wp   =           70.92914
     YDOT =       7285.844607  meter/sec      RA   =           74.48259  deg
     ZDOT =       2348.656616                 TA   =          221.93475
                                              MA   =          222.03034
                                              Ha   =            227.332  n.mi
                                              Hp   =            218.796
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14501768.20                 X    =         4426860.67
     Y    =        4962037.31  feet           Y    =         1561896.35  meter
     Z    =      -16184723.98                 Z    =        -4911615.61
     XDOT =        388.524573                 XDOT =          25.532449
     YDOT =      23903.689655  feet/sec       YDOT =        7286.649175  meter/sec
     ZDOT =       7705.566327                 ZDOT =        2349.007296
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13335894.74                 X    =         4064780.72
     Y    =        7760039.94  feet           Y    =         2365260.17  meter
     Z    =      -16087388.76                 Z    =        -4903436.09
     XDOT =      -3845.010134                 XDOT =       -1171.959089
     YDOT =      22523.684562  feet/sec       YDOT =        6865.219054  meter/sec
     ZDOT =       7706.360183                 ZDOT =        2348.898584
  
  
    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   19153.28699340  .00016717  00000-0  10270-3 0  9142
    2 25544  51.6408  75.2522 0007557   2.4964 357.6224 15.51148135 12936
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19153.28699340   =   yrday.fracday
    Element set:     914
    Inclination:       51.6408  deg
    RA of node:        75.2522  deg
    Eccentricity:     .0007557     
    Arg of perigee:     2.4964  deg
    Mean anomaly:     357.6224  deg
    Mean motion:   15.51148135  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1293
    Checksum:              312
 
 
    Coasting Arc #16 (Orbit 1308)
    ---------------------------------------
 
    Vector Time (GMT): 2019/154/06:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 965074.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4578816.89                 A    =         6789130.60  meter
     Y    =       -2022309.97  meter          E    =           .0013987
     Z    =        4584807.24                 I    =           51.99189
     XDOT =        -26.867584                 Wp   =           38.28150
     YDOT =      -7007.756791  meter/sec      RA   =           69.54041  deg
     ZDOT =      -3102.141031                 TA   =           82.71080
                                              MA   =           82.55183
                                              Ha   =            227.369  n.mi
                                              Hp   =            218.536
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15022365.12                 X    =        -4578133.28
     Y    =       -6634875.24  feet           Y    =        -2073510.43  meter
     Z    =       15042018.49                 Z    =         4562566.09
     XDOT =        -88.148243                 XDOT =          66.565829
     YDOT =     -22991.328053  feet/sec       YDOT =       -7007.534320  meter/sec
     ZDOT =     -10177.628056                 ZDOT =       -3102.045748
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13668273.63                 X    =        -4166089.80
     Y    =       -9267709.00  feet           Y    =        -2824797.70  meter
     Z    =       14941325.56                 Z    =         4554116.03
     XDOT =       3476.440602                 XDOT =        1059.619095
     YDOT =     -21617.283916  feet/sec       YDOT =       -6588.948138  meter/sec
     ZDOT =     -10176.408773                 ZDOT =       -3101.769394
  
  
    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   19154.31778900  .00016717  00000-0  10270-3 0  9158
    2 25544  51.6398  70.1364 0007578   5.3299 354.7931 15.51186845 13099
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19154.31778900   =   yrday.fracday
    Element set:     915
    Inclination:       51.6398  deg
    RA of node:        70.1364  deg
    Eccentricity:     .0007578     
    Arg of perigee:     5.3299  deg
    Mean anomaly:     354.7931  deg
    Mean motion:   15.51186845  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1309
    Checksum:              331
 
 
    Coasting Arc #17 (Orbit 1314)
    ---------------------------------------
 
    Vector Time (GMT): 2019/154/16:09:25.000
    Vector Time (MET): N/A
    Weight (LBS)     : 945398.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2166260.88                 A    =         6797838.51  meter
     Y    =       -6418614.52  meter          E    =           .0007784
     Z    =        -567153.20                 I    =           52.01852
     XDOT =       4639.286666                 Wp   =           94.15715
     YDOT =      -1041.702912  meter/sec      RA   =           67.60273  deg
     ZDOT =      -6002.105339                 TA   =           91.91879
                                              MA   =           91.82964
                                              Ha   =            227.334  n.mi
                                              Hp   =            218.581
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7107155.11                 X    =        -2091570.15
     Y    =      -21058446.59  feet           Y    =        -6442421.45  meter
     Z    =       -1860738.84                 Z    =         -577495.89
     XDOT =      15220.756779                 XDOT =        4679.745730
     YDOT =      -3417.660472  feet/sec       YDOT =        -989.595924  meter/sec
     ZDOT =     -19691.946651                 ZDOT =       -5979.471050
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10462795.95                 X    =        -3189060.21
     Y    =       19604225.25  feet           Y    =         5975367.86  meter
     Z    =       -1906942.26                 Z    =         -581236.00
     XDOT =     -11586.652601                 XDOT =       -3531.611713
     YDOT =      -8067.046532  feet/sec       YDOT =       -2458.835783  meter/sec
     ZDOT =     -19589.123073                 ZDOT =       -5970.764713
  
  
    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   19154.70433761  .00016717  00000-0  10270-3 0  9165
    2 25544  51.6423  68.2191 0007601   5.1015 355.0213 15.51154314 13155
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19154.70433761   =   yrday.fracday
    Element set:     916
    Inclination:       51.6423  deg
    RA of node:        68.2191  deg
    Eccentricity:     .0007601     
    Arg of perigee:     5.1015  deg
    Mean anomaly:     355.0213  deg
    Mean motion:   15.51154314  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1315
    Checksum:              264
 
 
    Coasting Arc #18 (Orbit 1325)
    ---------------------------------------
 
    Vector Time (GMT): 2019/155/08:42:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 931350.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3049244.48                 A    =         6786414.60  meter
     Y    =        3074161.78  meter          E    =           .0006941
     Z    =        5220747.57                 I    =           51.97075
     XDOT =      -4165.833085                 Wp   =           40.42659
     YDOT =      -6308.181926  meter/sec      RA   =           64.20297  deg
     ZDOT =       1285.562544                 TA   =           37.30888
                                              MA   =           37.26069
                                              Ha   =            227.510  n.mi
                                              Hp   =            218.327
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10004082.93                 X    =        -3108753.73
     Y    =       10085832.60  feet           Y    =         3039729.32  meter
     Z    =       17128436.92                 Z    =         5205791.36
     XDOT =     -13667.431381                 XDOT =       -4101.228187
     YDOT =     -20696.134928  feet/sec       YDOT =       -6354.406189  meter/sec
     ZDOT =       4217.724882                 ZDOT =        1265.482081
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5576266.83                 X    =        -1699646.13
     Y    =       13154593.08  feet           Y    =         4009519.97  meter
     Z    =       17060216.15                 Z    =         5199953.88
     XDOT =     -19520.635583                 XDOT =       -5949.889726
     YDOT =     -13609.697907  feet/sec       YDOT =       -4148.235922  meter/sec
     ZDOT =       4127.331319                 ZDOT =        1258.010586
  
  
    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   19155.41300835  .00016717  00000-0  10270-3 0  9170
    2 25544  51.6414  64.7016 0007686   8.4007 351.7271 15.51196475 13265
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19155.41300835   =   yrday.fracday
    Element set:     917
    Inclination:       51.6414  deg
    RA of node:        64.7016  deg
    Eccentricity:     .0007686     
    Arg of perigee:     8.4007  deg
    Mean anomaly:     351.7271  deg
    Mean motion:   15.51196475  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1326
    Checksum:              299
 
 
    Coasting Arc #19 (Orbit 1340)
    ---------------------------------------
 
    Vector Time (GMT): 2019/156/08:42:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 931350.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3317352.32                 A    =         6786047.12  meter
     Y    =       -2592576.47  meter          E    =           .0018459
     Z    =       -5336726.55                 I    =           51.95366
     XDOT =       4213.921838                 Wp   =           62.43662
     YDOT =       6368.941517  meter/sec      RA   =           59.25622  deg
     ZDOT =       -467.556210                 TA   =          203.07133
                                              MA   =          203.15432
                                              Ha   =            227.571  n.mi
                                              Hp   =            218.289
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10883701.82                 X    =         3372019.65
     Y    =       -8505828.30  feet           Y    =        -2555172.85  meter
     Z    =      -17508945.38                 Z    =        -5320479.73
     XDOT =      13825.202882                 XDOT =        4144.660467
     YDOT =      20895.477419  feet/sec       YDOT =        6415.677364  meter/sec
     ZDOT =      -1533.977066                 ZDOT =        -447.253505
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6780549.87                 X    =         2066711.60
     Y    =      -12141462.57  feet           Y    =        -3700717.79  meter
     Z    =      -17434915.50                 Z    =        -5314162.25
     XDOT =      20039.425603                 XDOT =        6108.016924
     YDOT =      13296.209931  feet/sec       YDOT =        4052.684787  meter/sec
     ZDOT =      -1442.592240                 ZDOT =        -439.702115
  
  
    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   19156.37937576  .00016717  00000-0  10270-3 0  9185
    2 25544  51.6413  59.9052 0007771  12.5494 347.5850 15.51172150 13418
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19156.37937576   =   yrday.fracday
    Element set:     918
    Inclination:       51.6413  deg
    RA of node:        59.9052  deg
    Eccentricity:     .0007771     
    Arg of perigee:    12.5494  deg
    Mean anomaly:     347.5850  deg
    Mean motion:   15.51172150  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1341
    Checksum:              317
 
 
    Coasting Arc #20 (Orbit 1356)
    ---------------------------------------
 
    Vector Time (GMT): 2019/157/08:42:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 931350.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3638313.22                 A    =         6785983.24  meter
     Y    =        2089393.30  meter          E    =           .0009564
     Z    =        5329990.58                 I    =           51.93541
     XDOT =      -4226.964594                 Wp   =           29.02515
     YDOT =      -6385.949567  meter/sec      RA   =           54.30927  deg
     ZDOT =       -373.613443                 TA   =           64.57272
                                              MA   =           64.47377
                                              Ha   =            227.775  n.mi
                                              Hp   =            217.999
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11936723.17                 X    =        -3687297.11
     Y    =        6854964.89  feet           Y    =         2048432.27  meter
     Z    =       17486845.74                 Z    =         5312198.44
     XDOT =     -13867.994074                 XDOT =       -4153.426123
     YDOT =     -20951.278108  feet/sec       YDOT =       -6432.807197  meter/sec
     ZDOT =      -1225.765890                 ZDOT =        -393.968992
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8205678.32                 X    =        -2501090.75
     Y    =       11178938.73  feet           Y    =         3407340.53  meter
     Z    =       17405856.77                 Z    =         5305305.14
     XDOT =     -20388.742279                 XDOT =       -6214.488647
     YDOT =     -12871.523290  feet/sec       YDOT =       -3923.240299  meter/sec
     ZDOT =      -1317.380654                 ZDOT =        -401.537623
  
  
    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   19157.41016609  .00016717  00000-0  10270-3 0  9197
    2 25544  51.6410  54.7905 0007837  16.2042 343.9359 15.51185061 13574
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19157.41016609   =   yrday.fracday
    Element set:     919
    Inclination:       51.6410  deg
    RA of node:        54.7905  deg
    Eccentricity:     .0007837     
    Arg of perigee:    16.2042  deg
    Mean anomaly:     343.9359  deg
    Mean motion:   15.51185061  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1357
    Checksum:              305
 
             

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