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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  15846.6289
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   69.3
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   1.922
   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 
   ------------------------------------------------------------------------
   057/02:24:45.635          -2.8               2.9              2.9    
   N/A                       -0.5               0.3              224.4  
   000/00:07:31.270          -0.6              -0.2              215.6  
   
   057/14:52:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              224.3  
   000/00:00:00.000           0.0               0.0              215.6  
   
   060/17:27:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              224.6  
   000/00:00:00.000           0.0               0.0              215.5  
   
   061/07:48:58.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              224.3  
   000/00:00:00.000           0.0               0.0              215.6  
   
   062/10:55:42.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              224.4  
   000/00:00:00.000           0.0               0.0              215.5  
   
 
 
    Coasting Arc #1 (Orbit 3711)
    ---------------------------------------
 
    Vector Time (GMT): 2019/051/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900744.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -145442.13                 A    =         6782244.80  meter
     Y    =        4855739.32  meter          E    =           .0016476
     Z    =       -4748809.31                 I    =           51.37287
     XDOT =      -6600.209347                 Wp   =           63.53667
     YDOT =      -2808.552760  meter/sec      RA   =          220.35256  deg
     ZDOT =      -2669.665963                 TA   =          179.94456
                                              MA   =          179.94438
                                              Ha   =            224.174  n.mi
                                              Hp   =            214.266
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -477172.35                 X    =         -176663.14
     Y    =       15930903.28  feet           Y    =         4853937.88  meter
     Z    =      -15580083.04                 Z    =        -4749592.06
     XDOT =     -21654.230142                 XDOT =       -6555.345389
     YDOT =      -9214.411942  feet/sec       YDOT =       -2882.110305  meter/sec
     ZDOT =      -8758.746598                 ZDOT =       -2701.617184
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8465379.36                 X    =        -2580247.63
     Y    =       13499491.93  feet           Y    =         4114645.14  meter
     Z    =      -15584012.00                 Z    =        -4750006.86
     XDOT =     -12862.981017                 XDOT =       -3920.636614
     YDOT =     -18343.644418  feet/sec       YDOT =       -5591.142818  meter/sec
     ZDOT =      -8902.762620                 ZDOT =       -2713.562047
  
  
    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   19051.52092202  .00016717  00000-0  10270-3 0  9005
    2 25544  51.6364 221.3435 0005752  47.8879 312.2761 15.53289859 37129
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19051.52092202   =   yrday.fracday
    Element set:     900
    Inclination:       51.6364  deg
    RA of node:       221.3435  deg
    Eccentricity:     .0005752     
    Arg of perigee:    47.8879  deg
    Mean anomaly:     312.2761  deg
    Mean motion:   15.53289859  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3712
    Checksum:              308
 
 
    Coasting Arc #2 (Orbit 3727)
    ---------------------------------------
 
    Vector Time (GMT): 2019/052/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900744.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1347085.96                 A    =         6780359.85  meter
     Y    =       -4132409.51  meter          E    =           .0007902
     Z    =        5197040.60                 I    =           51.39147
     XDOT =       6672.290815                 Wp   =           80.49610
     YDOT =       3613.041386  meter/sec      RA   =          215.34566  deg
     ZDOT =       1143.218150                 TA   =          358.51154
                                              MA   =          358.51389
                                              Ha   =            224.200  n.mi
                                              Hp   =            214.301
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4419573.35                 X    =         1367951.86
     Y    =      -13557773.98  feet           Y    =        -4117228.22  meter
     Z    =       17050658.12                 Z    =         5203635.21
     XDOT =      21890.717896                 XDOT =        6625.839881
     YDOT =      11853.810321  feet/sec       YDOT =        3687.396004  meter/sec
     ZDOT =       3750.715715                 ZDOT =        1175.515670
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10467432.42                 X    =         3190473.40
     Y    =       -9630748.93  feet           Y    =        -2935452.27  meter
     Z    =       17080759.35                 Z    =         5206215.45
     XDOT =      12393.434635                 XDOT =        3777.518877
     YDOT =      20381.573889  feet/sec       YDOT =        6212.303721  meter/sec
     ZDOT =       3896.249791                 ZDOT =        1187.576936
  
  
    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   19052.55031992  .00016717  00000-0  10270-3 0  9019
    2 25544  51.6355 216.2174 0005732  51.3966 308.7699 15.53253010 37284
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19052.55031992   =   yrday.fracday
    Element set:     901
    Inclination:       51.6355  deg
    RA of node:       216.2174  deg
    Eccentricity:     .0005732     
    Arg of perigee:    51.3966  deg
    Mean anomaly:     308.7699  deg
    Mean motion:   15.53253010  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3728
    Checksum:              307
 
 
    Coasting Arc #3 (Orbit 3742)
    ---------------------------------------
 
    Vector Time (GMT): 2019/053/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900744.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2592938.99                 A    =         6779868.46  meter
     Y    =        3375618.76  meter          E    =           .0019564
     Z    =       -5293884.95                 I    =           51.41969
     XDOT =      -6394.289845                 Wp   =           83.54735
     YDOT =      -4178.189097  meter/sec      RA   =          210.33987  deg
     ZDOT =        471.371461                 TA   =          190.95042
                                              MA   =          190.99307
                                              Ha   =            224.223  n.mi
                                              Hp   =            214.071
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8507017.70                 X    =        -2604779.11
     Y    =       11074864.71  feet           Y    =         3346555.92  meter
     Z    =      -17368388.94                 Z    =        -5306509.38
     XDOT =     -20978.641224                 XDOT =       -6349.382540
     YDOT =     -13707.969478  feet/sec       YDOT =       -4249.443369  meter/sec
     ZDOT =       1546.494294                 ZDOT =         440.420495
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12685493.62                 X    =        -3866538.46
     Y    =        5666371.15  feet           Y    =         1727109.93  meter
     Z    =      -17425653.58                 Z    =        -5311339.21
     XDOT =     -11383.479266                 XDOT =       -3469.684480
     YDOT =     -21194.227334  feet/sec       YDOT =       -6460.000491  meter/sec
     ZDOT =       1407.066017                 ZDOT =         428.873722
  
  
    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   19053.51537736  .00016717  00000-0  10270-3 0  9024
    2 25544  51.6372 211.4137 0005665  55.7185 304.4503 15.53288820 37436
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19053.51537736   =   yrday.fracday
    Element set:     902
    Inclination:       51.6372  deg
    RA of node:       211.4137  deg
    Eccentricity:     .0005665     
    Arg of perigee:    55.7185  deg
    Mean anomaly:     304.4503  deg
    Mean motion:   15.53288820  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3743
    Checksum:              304
 
 
    Coasting Arc #4 (Orbit 3758)
    ---------------------------------------
 
    Vector Time (GMT): 2019/054/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900744.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3809635.21                 A    =         6781257.38  meter
     Y    =       -2581316.76  meter          E    =           .0011683
     Z    =        4974180.45                 I    =           51.45368
     XDOT =       5806.274253                 Wp   =           58.36591
     YDOT =       4569.960249  meter/sec      RA   =          205.33453  deg
     ZDOT =      -2065.779396                 TA   =           51.82352
                                              MA   =           51.71834
                                              Ha   =            224.216  n.mi
                                              Hp   =            214.163
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12498803.17                 X    =         3814055.61
     Y    =       -8468887.02  feet           Y    =        -2538689.55  meter
     Z    =       16319489.65                 Z    =         4992696.96
     XDOT =      19049.456210                 XDOT =        5764.774404
     YDOT =      14993.307905  feet/sec       YDOT =        4634.657818  meter/sec
     ZDOT =      -6777.491456                 ZDOT =       -2037.676343
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14908454.11                 X    =         4544096.81
     Y    =       -1713927.14  feet           Y    =         -522404.99  meter
     Z    =       16403302.12                 Z    =         4999726.49
     XDOT =       9775.631136                 XDOT =        2979.612370
     YDOT =      21079.463268  feet/sec       YDOT =        6425.020404  meter/sec
     ZDOT =      -6650.936007                 ZDOT =       -2027.205295
  
  
    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   19054.54477108  .00016717  00000-0  10270-3 0  9035
    2 25544  51.6375 206.2871 0005712  59.5442 300.6274 15.53254633 37592
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19054.54477108   =   yrday.fracday
    Element set:     903
    Inclination:       51.6375  deg
    RA of node:       206.2871  deg
    Eccentricity:     .0005712     
    Arg of perigee:    59.5442  deg
    Mean anomaly:     300.6274  deg
    Mean motion:   15.53254633  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3759
    Checksum:              311
 
 
    Coasting Arc #5 (Orbit 3773)
    ---------------------------------------
 
    Vector Time (GMT): 2019/055/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900744.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4898671.89                 A    =         6783764.60  meter
     Y    =        1852662.38  meter          E    =           .0013235
     Z    =       -4323398.27                 I    =           51.49361
     XDOT =      -4873.135225                 Wp   =           92.11558
     YDOT =      -4766.001204  meter/sec      RA   =          200.33856  deg
     ZDOT =       3488.013225                 TA   =          213.44290
                                              MA   =          213.52655
                                              Ha   =            224.279  n.mi
                                              Hp   =            213.959
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16071758.16                 X    =        -4898024.38
     Y    =        6078288.65  feet           Y    =         1797885.27  meter
     Z    =      -14184377.51                 Z    =        -4347192.48
     XDOT =     -15987.976461                 XDOT =       -4836.420907
     YDOT =     -15636.486890  feet/sec       YDOT =       -4820.290434  meter/sec
     ZDOT =      11443.612943                 ZDOT =        3464.431209
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17000300.12                 X    =        -5181691.48
     Y    =       -1781223.06  feet           Y    =         -542916.79  meter
     Z    =      -14291977.08                 Z    =        -4356194.62
     XDOT =      -7415.875186                 XDOT =       -2260.358757
     YDOT =     -19960.495068  feet/sec       YDOT =       -6083.958897  meter/sec
     ZDOT =      11337.473655                 ZDOT =        3455.661970
  
  
    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   19055.50982336  .00016717  00000-0  10270-3 0  9047
    2 25544  51.6382 201.4833 0005720  62.2003 297.9728 15.53283376 37743
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19055.50982336   =   yrday.fracday
    Element set:     904
    Inclination:       51.6382  deg
    RA of node:       201.4833  deg
    Eccentricity:     .0005720     
    Arg of perigee:    62.2003  deg
    Mean anomaly:     297.9728  deg
    Mean motion:   15.53283376  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3774
    Checksum:              314
 
 
    Coasting Arc #6 (Orbit 3789)
    ---------------------------------------
 
    Vector Time (GMT): 2019/056/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900744.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5805625.78                 A    =         6787055.30  meter
     Y    =       -1136049.15  meter          E    =           .0017833
     Z    =        3313546.70                 I    =           51.53537
     XDOT =       3639.771795                 Wp   =           83.96063
     YDOT =       4860.550893  meter/sec      RA   =          195.35020  deg
     ZDOT =      -4687.196260                 TA   =           57.42129
                                              MA   =           57.24921
                                              Ha   =            224.254  n.mi
                                              Hp   =            214.031
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19047328.66                 X    =         5801802.73
     Y    =       -3727195.36  feet           Y    =        -1071147.74  meter
     Z    =       10871216.20                 Z    =         3341738.72
     XDOT =      11941.508515                 XDOT =        3607.916768
     YDOT =      15946.689282  feet/sec       YDOT =        4901.074943  meter/sec
     ZDOT =     -15377.940484                 ZDOT =       -4669.593503
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18702783.37                 X    =         5700608.37
     Y    =        4910388.32  feet           Y    =         1496686.36  meter
     Z    =       10998637.95                 Z    =         3352384.85
     XDOT =       4253.993556                 XDOT =        1296.617236
     YDOT =      18235.816395  feet/sec       YDOT =        5558.276837  meter/sec
     ZDOT =     -15298.800182                 ZDOT =       -4663.074295
  
  
    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   19056.53921253  .00016717  00000-0  10270-3 0  9053
    2 25544  51.6375 196.3577 0005653  66.7447 293.4300 15.53273468 37904
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19056.53921253   =   yrday.fracday
    Element set:     905
    Inclination:       51.6375  deg
    RA of node:       196.3577  deg
    Eccentricity:     .0005653     
    Arg of perigee:    66.7447  deg
    Mean anomaly:     293.4300  deg
    Mean motion:   15.53273468  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3790
    Checksum:              331
 
 
    Coasting Arc #7 (Orbit 3798)
    ---------------------------------------
 
    Vector Time (GMT): 2019/057/02:28:31.270
    Vector Time (MET): N/A
    Weight (LBS)     : 900442.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1605161.19                 A    =         6781498.73  meter
     Y    =        3949783.94  meter          E    =           .0017611
     Z    =       -5288801.82                 I    =           51.53297
     XDOT =      -7324.507351                 Wp   =           86.90420
     YDOT =      -2125.479879  meter/sec      RA   =          192.36870  deg
     ZDOT =        638.421818                 TA   =          189.19556
                                              MA   =          189.22785
                                              Ha   =            224.365  n.mi
                                              Hp   =            215.638
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5266276.86                 X    =        -1623519.73
     Y    =       12958608.72  feet           Y    =         3931730.96  meter
     Z    =      -17351712.00                 Z    =        -5296643.81
     XDOT =     -24030.535929                 XDOT =       -7303.296327
     YDOT =      -6973.359183  feet/sec       YDOT =       -2207.269002  meter/sec
     ZDOT =       2094.559769                 ZDOT =         602.894170
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2366902.43                 X    =          721431.86
     Y    =      -13741036.42  feet           Y    =        -4188267.90  meter
     Z    =      -17387432.60                 Z    =        -5299689.46
     XDOT =      23963.261201                 XDOT =        7304.002014
     YDOT =       1691.651765  feet/sec       YDOT =         515.615458  meter/sec
     ZDOT =       1934.237746                 ZDOT =         589.555665
  
  
    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   19057.11824430  .00016717  00000-0  10270-3 0  9068
    2 25544  51.6395 193.4804 0003712  52.4628 307.6860 15.52747465 37994
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19057.11824430   =   yrday.fracday
    Element set:     906
    Inclination:       51.6395  deg
    RA of node:       193.4804  deg
    Eccentricity:     .0003712     
    Arg of perigee:    52.4628  deg
    Mean anomaly:     307.6860  deg
    Mean motion:   15.52747465  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3799
    Checksum:              326
 
 
    Coasting Arc #8 (Orbit 3806)
    ---------------------------------------
 
    Vector Time (GMT): 2019/057/14:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900442.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2327362.72                 A    =         6782005.79  meter
     Y    =        3755600.78  meter          E    =           .0016502
     Z    =       -5159812.69                 I    =           51.55235
     XDOT =      -7117.316601                 Wp   =           93.28602
     YDOT =      -2405.988732  meter/sec      RA   =          189.78861  deg
     ZDOT =       1462.217670                 TA   =          190.81486
                                              MA   =          190.85038
                                              Ha   =            224.281  n.mi
                                              Hp   =            215.633
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7635704.46                 X    =        -2344122.75
     Y    =       12321524.86  feet           Y    =         3729480.61  meter
     Z    =      -16928519.32                 Z    =        -5171158.90
     XDOT =     -23350.776250                 XDOT =       -7096.985736
     YDOT =      -7893.663819  feet/sec       YDOT =       -2485.465786  meter/sec
     ZDOT =       4797.302067                 ZDOT =        1427.694361
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3277962.39                 X    =         -999122.94
     Y    =       14058141.24  feet           Y    =         4284921.45  meter
     Z    =      -16980057.47                 Z    =        -5175521.52
     XDOT =     -23653.059103                 XDOT =       -7209.452414
     YDOT =         78.671430  feet/sec       YDOT =          23.979052  meter/sec
     ZDOT =       4641.526190                 ZDOT =        1414.737183
  
  
    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   19057.63311763  .00016717  00000-0  10270-3 0  9076
    2 25544  51.6401 190.9169 0003402  58.5960 301.5524 15.52760682 38076
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19057.63311763   =   yrday.fracday
    Element set:     907
    Inclination:       51.6401  deg
    RA of node:       190.9169  deg
    Eccentricity:     .0003402     
    Arg of perigee:    58.5960  deg
    Mean anomaly:     301.5524  deg
    Mean motion:   15.52760682  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3807
    Checksum:              306
 
 
    Coasting Arc #9 (Orbit 3822)
    ---------------------------------------
 
    Vector Time (GMT): 2019/058/14:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900442.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3467185.97                 A    =         6783800.16  meter
     Y    =       -3446005.64  meter          E    =           .0011281
     Z    =        4697285.77                 I    =           51.59196
     XDOT =       6575.694584                 Wp   =           62.51010
     YDOT =       2781.985343  meter/sec      RA   =          184.80089  deg
     ZDOT =      -2802.511926                 TA   =           55.33551
                                              MA   =           55.22923
                                              Ha   =            224.195  n.mi
                                              Hp   =            215.650
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11375282.07                 X    =         3482646.04
     Y    =      -11305792.79  feet           Y    =        -3407146.50  meter
     Z    =       15411042.56                 Z    =         4714165.50
     XDOT =      21573.801130                 XDOT =        6557.709761
     YDOT =       9127.248502  feet/sec       YDOT =        2855.418670  meter/sec
     ZDOT =      -9194.592932                 ZDOT =       -2770.613961
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6910415.38                 X    =         2106294.61
     Y    =      -14390959.33  feet           Y    =        -4386364.40  meter
     Z    =       15487565.15                 Z    =         4720609.86
     XDOT =      22385.198660                 XDOT =        6823.008552
     YDOT =        972.759746  feet/sec       YDOT =         296.497171  meter/sec
     ZDOT =      -9050.683180                 ZDOT =       -2758.648233
  
  
    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   19058.66286444  .00016717  00000-0  10270-3 0  9088
    2 25544  51.6405 185.7937 0003464  60.2378 299.9118 15.52780819 38237
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19058.66286444   =   yrday.fracday
    Element set:     908
    Inclination:       51.6405  deg
    RA of node:       185.7937  deg
    Eccentricity:     .0003464     
    Arg of perigee:    60.2378  deg
    Mean anomaly:     299.9118  deg
    Mean motion:   15.52780819  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3823
    Checksum:              349
 
 
    Coasting Arc #10 (Orbit 3837)
    ---------------------------------------
 
    Vector Time (GMT): 2019/059/14:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900442.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4471389.50                 A    =         6786387.93  meter
     Y    =        3181755.78  meter          E    =           .0009943
     Z    =       -4001470.49                 I    =           51.63258
     XDOT =      -5761.081466                 Wp   =           94.76156
     YDOT =      -3120.383559  meter/sec      RA   =          179.82166  deg
     ZDOT =       3964.178679                 TA   =          216.52347
                                              MA   =          216.59132
                                              Ha   =            224.316  n.mi
                                              Hp   =            215.502
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14669913.05                 X    =        -4487199.90
     Y    =       10438831.29  feet           Y    =         3131665.00  meter
     Z    =      -13128184.01                 Z    =        -4023228.96
     XDOT =     -18901.185913                 XDOT =       -5745.015712
     YDOT =     -10237.478868  feet/sec       YDOT =       -3184.717994  meter/sec
     ZDOT =      13005.835561                 ZDOT =        3936.233172
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10067100.97                 X    =        -3068452.37
     Y    =       14840198.75  feet           Y    =         4523292.58  meter
     Z    =      -13226743.44                 Z    =        -4031511.40
     XDOT =     -20275.192056                 XDOT =       -6179.878539
     YDOT =      -2296.890262  feet/sec       YDOT =        -700.092152  meter/sec
     ZDOT =      12879.788714                 ZDOT =        3925.759600
  
  
    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   19059.62825186  .00016717  00000-0  10270-3 0  9098
    2 25544  51.6392 180.9923 0003514  65.9421 294.2098 15.52777580 38383
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19059.62825186   =   yrday.fracday
    Element set:     909
    Inclination:       51.6392  deg
    RA of node:       180.9923  deg
    Eccentricity:     .0003514     
    Arg of perigee:    65.9421  deg
    Mean anomaly:     294.2098  deg
    Mean motion:   15.52777580  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3838
    Checksum:              345
 
 
    Coasting Arc #11 (Orbit 3853)
    ---------------------------------------
 
    Vector Time (GMT): 2019/060/14:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900442.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5326659.05                 A    =         6789243.87  meter
     Y    =       -2894673.21  meter          E    =           .0016179
     Z    =        3042320.94                 I    =           51.67585
     XDOT =       4725.361571                 Wp   =           90.13581
     YDOT =       3488.187310  meter/sec      RA   =          174.84912  deg
     ZDOT =      -4931.876750                 TA   =           54.99366
                                              MA   =           54.84191
                                              Ha   =            224.282  n.mi
                                              Hp   =            215.555
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17475915.52                 X    =         5343854.62
     Y    =       -9496959.35  feet           Y    =        -2835010.49  meter
     Z    =        9981367.92                 Z    =         3068237.22
     XDOT =      15503.154759                 XDOT =        4709.960298
     YDOT =      11444.184087  feet/sec       YDOT =        3540.943245  meter/sec
     ZDOT =     -16180.698000                 ZDOT =       -4908.960774
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12786439.80                 X    =         3897306.85
     Y    =      -15157524.99  feet           Y    =        -4620013.62  meter
     Z    =       10098710.78                 Z    =         3078087.05
     XDOT =      17590.697132                 XDOT =        5361.644486
     YDOT =       4078.509815  feet/sec       YDOT =        1243.129792  meter/sec
     ZDOT =     -16077.389199                 ZDOT =       -4900.388228
  
  
    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   19060.65799505  .00016717  00000-0  10270-3 0  9100
    2 25544  51.6397 175.8694 0003510  66.9084 293.2437 15.52779515 38542
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19060.65799505   =   yrday.fracday
    Element set:     910
    Inclination:       51.6397  deg
    RA of node:       175.8694  deg
    Eccentricity:     .0003510     
    Arg of perigee:    66.9084  deg
    Mean anomaly:     293.2437  deg
    Mean motion:   15.52779515  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3854
    Checksum:              346
 
 
    Coasting Arc #12 (Orbit 3855)
    ---------------------------------------
 
    Vector Time (GMT): 2019/060/17:27:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900442.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6108152.86                 A    =         6790671.75  meter
     Y    =       -1439403.83  meter          E    =           .0017599
     Z    =        2572514.99                 I    =           51.68252
     XDOT =       3289.815783                 Wp   =           74.34367
     YDOT =      -4505.784714  meter/sec      RA   =          174.35813  deg
     ZDOT =       5264.848478                 TA   =          314.56656
                                              MA   =          314.71010
                                              Ha   =            224.644  n.mi
                                              Hp   =            215.531
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20039871.59                 X    =        -6104098.66
     Y    =       -4722453.50  feet           Y    =        -1507686.66  meter
     Z    =        8440009.81                 Z    =         2542854.42
     XDOT =      10793.358869                 XDOT =        3314.383067
     YDOT =     -14782.758247  feet/sec       YDOT =       -4468.858065  meter/sec
     ZDOT =      17273.124928                 ZDOT =        5280.888728
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14079497.23                 X    =        -4291430.76
     Y    =       15096649.72  feet           Y    =         4601458.83  meter
     Z    =        8306064.73                 Z    =         2531688.53
     XDOT =      -6425.261170                 XDOT =       -1958.419605
     YDOT =     -15582.421364  feet/sec       YDOT =       -4749.522032  meter/sec
     ZDOT =      17345.954012                 ZDOT =        5287.046783
  
  
    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   19060.78671466  .00016717  00000-0  10270-3 0  9110
    2 25544  51.6388 175.2295 0003968  67.2698 292.8873 15.52735568 38566
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19060.78671466   =   yrday.fracday
    Element set:     911
    Inclination:       51.6388  deg
    RA of node:       175.2295  deg
    Eccentricity:     .0003968     
    Arg of perigee:    67.2698  deg
    Mean anomaly:     292.8873  deg
    Mean motion:   15.52735568  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3856
    Checksum:              370
 
 
    Coasting Arc #13 (Orbit 3864)
    ---------------------------------------
 
    Vector Time (GMT): 2019/061/07:48:58.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900442.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4337311.08                 A    =         6787340.35  meter
     Y    =       -3641918.39  meter          E    =           .0015007
     Z    =        3729920.76                 I    =           51.68967
     XDOT =       5831.946860                 Wp   =           80.71532
     YDOT =       2537.269032  meter/sec      RA   =          171.33384  deg
     ZDOT =      -4287.149593                 TA   =           54.78070
                                              MA   =           54.64030
                                              Ha   =            224.324  n.mi
                                              Hp   =            215.588
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14230023.24                 X    =         4359596.21
     Y    =      -11948551.14  feet           Y    =        -3593290.73  meter
     Z    =       12237272.85                 Z    =         3751043.66
     XDOT =      19133.683925                 XDOT =        5823.965091
     YDOT =       8324.373463  feet/sec       YDOT =        2602.441062  meter/sec
     ZDOT =     -14065.451422                 ZDOT =       -4258.840345
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13400386.85                 X    =         4084437.91
     Y    =       12780399.66  feet           Y    =         3895465.82  meter
     Z    =       12333016.63                 Z    =         3759103.47
     XDOT =      -5274.702800                 XDOT =       -1607.729413
     YDOT =      19034.032144  feet/sec       YDOT =        5801.572997  meter/sec
     ZDOT =     -13937.683442                 ZDOT =       -4248.205913
  
  
    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   19061.36594202  .00016717  00000-0  10270-3 0  9128
    2 25544  51.6368 172.3449 0003516  69.0960 291.0568 15.52754565 38654
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19061.36594202   =   yrday.fracday
    Element set:     912
    Inclination:       51.6368  deg
    RA of node:       172.3449  deg
    Eccentricity:     .0003516     
    Arg of perigee:    69.0960  deg
    Mean anomaly:     291.0568  deg
    Mean motion:   15.52754565  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3865
    Checksum:              326
 
 
    Coasting Arc #14 (Orbit 3879)
    ---------------------------------------
 
    Vector Time (GMT): 2019/062/07:48:58.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900442.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5139424.97                 A    =         6789992.84  meter
     Y    =        3481436.44  meter          E    =           .0008437
     Z    =       -2753298.00                 I    =           51.73201
     XDOT =      -4797.612748                 Wp   =           66.88803
     YDOT =      -3019.397376  meter/sec      RA   =          166.36651  deg
     ZDOT =       5153.311215                 TA   =          262.02012
                                              MA   =          262.11587
                                              Ha   =            224.458  n.mi
                                              Hp   =            215.408
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16861630.47                 X    =        -5164599.73
     Y    =       11422035.58  feet           Y    =         3423822.85  meter
     Z    =       -9033129.93                 Z    =        -2778324.20
     XDOT =     -15740.199306                 XDOT =       -4788.523767
     YDOT =      -9906.159371  feet/sec       YDOT =       -3072.996449  meter/sec
     ZDOT =      16907.189024                 ZDOT =        5130.029048
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13426785.04                 X    =        -4092484.08
     Y    =      -15245902.72  feet           Y    =        -4646951.15  meter
     Z    =       -9146518.96                 Z    =        -2787858.98
     XDOT =       6739.702041                 XDOT =        2054.261182
     YDOT =     -15985.010771  feet/sec       YDOT =       -4872.231283  meter/sec
     ZDOT =      16802.163211                 ZDOT =        5121.299347
  
  
    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   19062.33132224  .00016717  00000-0  10270-3 0  9139
    2 25544  51.6374 167.5421 0003774  75.1457 285.0112 15.52768261 38805
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19062.33132224   =   yrday.fracday
    Element set:     913
    Inclination:       51.6374  deg
    RA of node:       167.5421  deg
    Eccentricity:     .0003774     
    Arg of perigee:    75.1457  deg
    Mean anomaly:     285.0112  deg
    Mean motion:   15.52768261  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3880
    Checksum:              298
 
 
    Coasting Arc #15 (Orbit 3881)
    ---------------------------------------
 
    Vector Time (GMT): 2019/062/10:55:42.000
    Vector Time (MET): N/A
    Weight (LBS)     : 935659.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5477709.71                 A    =         6791000.02  meter
     Y    =        3277518.86  meter          E    =           .0009060
     Z    =       -2315215.37                 I    =           51.74215
     XDOT =      -4272.534329                 Wp   =           57.42499
     YDOT =      -3324.819859  meter/sec      RA   =          165.72533  deg
     ZDOT =       5422.103959                 TA   =          276.83953
                                              MA   =          276.94260
                                              Ha   =            224.439  n.mi
                                              Hp   =            215.502
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17971488.54                 X    =        -5502706.97
     Y    =       10753014.62  feet           Y    =         3216123.34  meter
     Z    =       -7595850.97                 Z    =        -2341884.36
     XDOT =     -14017.501080                 XDOT =       -4261.374665
     YDOT =     -10908.201638  feet/sec       YDOT =       -3372.535530  meter/sec
     ZDOT =      17789.054982                 ZDOT =        5401.377426
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20817072.52                 X    =        -6345043.70
     Y    =       -1844296.94  feet           Y    =         -562141.71  meter
     Z    =       -7716653.17                 Z    =        -2352035.89
     XDOT =      -5151.731990                 XDOT =       -1570.247910
     YDOT =     -15617.414064  feet/sec       YDOT =       -4760.187807  meter/sec
     ZDOT =      17695.602814                 ZDOT =        5393.619738
  
  
    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   19062.46003923  .00016717  00000-0  10270-3 0  9147
    2 25544  51.6402 166.9023 0003640  74.9219 285.2335 15.52747501 38828
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19062.46003923   =   yrday.fracday
    Element set:     914
    Inclination:       51.6402  deg
    RA of node:       166.9023  deg
    Eccentricity:     .0003640     
    Arg of perigee:    74.9219  deg
    Mean anomaly:     285.2335  deg
    Mean motion:   15.52747501  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3882
    Checksum:              299
 
 
    Coasting Arc #16 (Orbit 3897)
    ---------------------------------------
 
    Vector Time (GMT): 2019/063/10:55:42.000
    Vector Time (MET): N/A
    Weight (LBS)     : 935659.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5988479.84                 A    =         6792773.64  meter
     Y    =       -2999528.18  meter          E    =           .0016536
     Z    =        1091493.80                 I    =           51.77971
     XDOT =       3020.757624                 Wp   =          114.90446
     YDOT =       3862.790850  meter/sec      RA   =          160.76786  deg
     ZDOT =      -5894.940442                 TA   =           53.28183
                                              MA   =           53.13005
                                              Ha   =            224.455  n.mi
                                              Hp   =            215.483
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19647243.57                 X    =         6016274.59
     Y    =       -9840971.72  feet           Y    =        -2932405.30  meter
     Z    =        3581016.39                 Z    =         1120650.68
     XDOT =       9910.622127                 XDOT =        3005.971977
     YDOT =      12673.198327  feet/sec       YDOT =        3896.487877  meter/sec
     ZDOT =     -19340.355782                 ZDOT =       -5880.303333
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21716158.59                 X    =         6619085.14
     Y    =        3210018.46  feet           Y    =          978413.63  meter
     Z    =        3713060.77                 Z    =         1131740.92
     XDOT =       1178.113812                 XDOT =         359.089090
     YDOT =      14555.938780  feet/sec       YDOT =        4436.650140  meter/sec
     ZDOT =     -19274.462099                 ZDOT =       -5874.856048
  
  
    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   19063.48977480  .00016717  00000-0  10270-3 0  9159
    2 25544  51.6399 161.7798 0003596  81.7627 278.3932 15.52759211 38988
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19063.48977480   =   yrday.fracday
    Element set:     915
    Inclination:       51.6399  deg
    RA of node:       161.7798  deg
    Eccentricity:     .0003596     
    Arg of perigee:    81.7627  deg
    Mean anomaly:     278.3932  deg
    Mean motion:   15.52759211  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3898
    Checksum:              371
 
 
    Coasting Arc #17 (Orbit 3913)
    ---------------------------------------
 
    Vector Time (GMT): 2019/064/10:55:42.000
    Vector Time (MET): N/A
    Weight (LBS)     : 935659.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6236216.46                 A    =         6793273.52  meter
     Y    =        2674252.20  meter          E    =           .0015419
     Z    =         146700.57                 I    =           51.81404
     XDOT =      -1740.105386                 Wp   =           54.93999
     YDOT =      -4412.339160  meter/sec      RA   =          155.81474  deg
     ZDOT =       6023.896755                 TA   =          306.63581
                                              MA   =          306.77750
                                              Ha   =            224.454  n.mi
                                              Hp   =            215.492
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20460027.74                 X    =        -6266369.79
     Y    =        8773793.31  feet           Y    =         2604345.89  meter
     Z    =         481301.08                 Z    =          116334.52
     XDOT =      -5709.007171                 XDOT =       -1719.896139
     YDOT =     -14476.178347  feet/sec       YDOT =       -4431.684611  meter/sec
     ZDOT =      19763.440798                 ZDOT =        6015.493705
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21866574.84                 X    =        -6664932.01
     Y    =       -4190291.44  feet           Y    =        -1277200.83  meter
     Z    =         343798.46                 Z    =          104789.77
     XDOT =       2961.151385                 XDOT =         902.558942
     YDOT =     -13668.777924  feet/sec       YDOT =       -4166.243511  meter/sec
     ZDOT =      19725.768408                 ZDOT =        6012.414211
  
  
    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   19064.51950676  .00016717  00000-0  10270-3 0  9163
    2 25544  51.6415 156.6575 0003658  82.4294 277.7273 15.52771709 39146
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19064.51950676   =   yrday.fracday
    Element set:     916
    Inclination:       51.6415  deg
    RA of node:       156.6575  deg
    Eccentricity:     .0003658     
    Arg of perigee:    82.4294  deg
    Mean anomaly:     277.7273  deg
    Mean motion:   15.52771709  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3914
    Checksum:              343
 
 
    Coasting Arc #18 (Orbit 3928)
    ---------------------------------------
 
    Vector Time (GMT): 2019/065/10:55:42.000
    Vector Time (MET): N/A
    Weight (LBS)     : 935659.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6260925.41                 A    =         6792442.75  meter
     Y    =       -2203706.59  meter          E    =           .0011098
     Z    =       -1429853.27                 I    =           51.84073
     XDOT =        435.688058                 Wp   =          126.83450
     YDOT =       4981.475933  meter/sec      RA   =          150.86351  deg
     ZDOT =      -5807.365080                 TA   =           68.70052
                                              MA   =           68.58207
                                              Ha   =            224.506  n.mi
                                              Hp   =            215.475
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20541093.88                 X    =         6292047.86
     Y    =       -7230008.50  feet           Y    =        -2133518.70  meter
     Z    =       -4691119.64                 Z    =        -1399364.78
     XDOT =       1429.422763                 XDOT =         408.159815
     YDOT =      16343.424977  feet/sec       YDOT =        4986.193504  meter/sec
     ZDOT =     -19053.035038                 ZDOT =       -5805.316152
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21184708.39                 X    =         6457099.12
     Y    =        5166596.77  feet           Y    =         1574778.69  meter
     Z    =       -4553083.82                 Z    =        -1387779.95
     XDOT =      -7236.045042                 XDOT =       -2205.546529
     YDOT =      12999.433047  feet/sec       YDOT =        3962.227193  meter/sec
     ZDOT =     -19044.136075                 ZDOT =       -5804.652676
  
  
    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   19065.48487706  .00016717  00000-0  10270-3 0  9170
    2 25544  51.6410 151.8553 0003671  86.3908 273.7664 15.52776414 39298
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19065.48487706   =   yrday.fracday
    Element set:     917
    Inclination:       51.6410  deg
    RA of node:       151.8553  deg
    Eccentricity:     .0003671     
    Arg of perigee:    86.3908  deg
    Mean anomaly:     273.7664  deg
    Mean motion:   15.52776414  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3929
    Checksum:              342
 
 
    Coasting Arc #19 (Orbit 3943)
    ---------------------------------------
 
    Vector Time (GMT): 2019/066/10:55:42.000
    Vector Time (MET): N/A
    Weight (LBS)     : 935659.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6051656.88                 A    =         6790486.47  meter
     Y    =        1645669.27  meter          E    =           .0017302
     Z    =        2584089.43                 I    =           51.86283
     XDOT =        763.273003                 Wp   =           79.09156
     YDOT =      -5516.577276  meter/sec      RA   =          145.91147  deg
     ZDOT =       5274.015758                 TA   =          309.87923
                                              MA   =          310.03125
                                              Ha   =            224.531  n.mi
                                              Hp   =            215.449
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19854517.32                 X    =        -6082161.33
     Y    =        5399177.39  feet           Y    =         1577825.17  meter
     Z    =        8477983.69                 Z    =         2554618.92
     XDOT =       2504.176519                 XDOT =         799.286367
     YDOT =     -18099.006811  feet/sec       YDOT =       -5507.839801  meter/sec
     ZDOT =      17303.201307                 ZDOT =        5277.811551
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19737857.46                 X    =        -6016098.95
     Y    =       -6001179.23  feet           Y    =        -1829159.43  meter
     Z    =        8344579.84                 Z    =         2543427.93
     XDOT =      11199.096959                 XDOT =        3413.484753
     YDOT =     -12625.662968  feet/sec       YDOT =       -3848.302073  meter/sec
     ZDOT =      17320.777068                 ZDOT =        5279.372850
  
  
    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   19066.51460283  .00016717  00000-0  10270-3 0  9187
    2 25544  51.6411 146.7332 0003714  88.8150 271.3427 15.52790598 39448
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19066.51460283   =   yrday.fracday
    Element set:     918
    Inclination:       51.6411  deg
    RA of node:       146.7332  deg
    Eccentricity:     .0003714     
    Arg of perigee:    88.8150  deg
    Mean anomaly:     271.3427  deg
    Mean motion:   15.52790598  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3944
    Checksum:              319
 
             

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