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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  20451.43
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   104.7
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   3.055
   ET - UTC  (sec) :   67.18
   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 
   ------------------------------------------------------------------------
   048/10:49:56.623           1.5               2.9              2.9    
   N/A                       -2.3              -0.4              222.1  
   000/00:09:53.245           0.8               0.2              213.2  
   
 
 
    Coasting Arc #1 (Orbit 2542)
    ---------------------------------------
 
    Vector Time (GMT): 2016/043/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2360510.86                 A    =         6775827.48  meter
     Y    =       -3518121.42  meter          E    =           .0021176
     Z    =       -5306312.78                 I    =           51.41132
     XDOT =       6265.592107                 Wp   =           94.61517
     YDOT =      -4393.802513  meter/sec      RA   =          324.21494  deg
     ZDOT =        124.637340                 TA   =          176.58585
                                              MA   =          176.57137
                                              Ha   =            222.485  n.mi
                                              Hp   =            211.425
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7744458.21                 X    =        -2295219.49
     Y    =      -11542393.13  feet           Y    =        -3544153.66  meter
     Z    =      -17409162.66                 Z    =        -5317620.47
     XDOT =      20556.404550                 XDOT =        6313.653597
     YDOT =     -14415.362577  feet/sec       YDOT =       -4323.467767  meter/sec
     ZDOT =        408.915157                 ZDOT =         155.190743
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1301108.36                 X    =          396577.83
     Y    =      -13777732.74  feet           Y    =        -4199452.94  meter
     Z    =      -17457480.18                 Z    =        -5321039.96
     XDOT =      24044.096466                 XDOT =        7328.640603
     YDOT =       1578.456506  feet/sec       YDOT =         481.113543  meter/sec
     ZDOT =        542.216145                 ZDOT =         165.267481
  
  
    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   16043.51582261  .00016717  00000-0  10270-3 0  9001
    2 25544  51.6429 324.7451 0006414 103.6899 256.4968 15.54658685 25433
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16043.51582261   =   yrday.fracday
    Element set:     900
    Inclination:       51.6429  deg
    RA of node:       324.7451  deg
    Eccentricity:     .0006414     
    Arg of perigee:   103.6899  deg
    Mean anomaly:     256.4968  deg
    Mean motion:   15.54658685  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2543
    Checksum:              328
 
 
    Coasting Arc #2 (Orbit 2558)
    ---------------------------------------
 
    Vector Time (GMT): 2016/044/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         660163.94                 A    =         6777374.61  meter
     Y    =        4612351.04  meter          E    =           .0011745
     Z    =        4912205.80                 I    =           51.39099
     XDOT =      -6557.358347                 Wp   =           81.81791
     YDOT =       3314.413742  meter/sec      RA   =          319.19396  deg
     ZDOT =      -2224.628151                 TA   =           29.98337
                                              MA   =           29.91616
                                              Ha   =            222.345  n.mi
                                              Hp   =            211.517
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2165892.18                 X    =          584677.30
     Y    =       15132385.30  feet           Y    =         4619311.78  meter
     Z    =       16116160.77                 Z    =         4915228.94
     XDOT =     -21513.642870                 XDOT =       -6583.127419
     YDOT =      10874.060834  feet/sec       YDOT =        3240.940739  meter/sec
     ZDOT =      -7298.648790                 ZDOT =       -2256.544675
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7664641.96                 X    =        -2336182.87
     Y    =       13211365.68  feet           Y    =         4026824.26  meter
     Z    =       16128356.78                 Z    =         4915923.15
     XDOT =     -22656.274327                 XDOT =       -6905.632415
     YDOT =      -4039.503777  feet/sec       YDOT =       -1231.240751  meter/sec
     ZDOT =      -7437.634274                 ZDOT =       -2266.990927
  
  
    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   16044.54429414  .00016717  00000-0  10270-3 0  9016
    2 25544  51.6424 319.6140 0006341 107.2950 252.8897 15.54702407 25593
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16044.54429414   =   yrday.fracday
    Element set:     901
    Inclination:       51.6424  deg
    RA of node:       319.6140  deg
    Eccentricity:     .0006341     
    Arg of perigee:   107.2950  deg
    Mean anomaly:     252.8897  deg
    Mean motion:   15.54702407  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2559
    Checksum:              303
 
 
    Coasting Arc #3 (Orbit 2573)
    ---------------------------------------
 
    Vector Time (GMT): 2016/045/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         940384.16                 A    =         6781111.28  meter
     Y    =       -5462100.22  meter          E    =           .0012882
     Z    =       -3920809.43                 I    =           51.38057
     XDOT =       6252.895378                 Wp   =          108.18099
     YDOT =      -1812.794174  meter/sec      RA   =          314.17874  deg
     ZDOT =       4032.134325                 TA   =          204.15858
                                              MA   =          204.21905
                                              Ha   =            222.329  n.mi
                                              Hp   =            211.516
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3085249.86                 X    =         1020438.24
     Y    =      -17920276.31  feet           Y    =        -5451136.89  meter
     Z    =      -12863548.00                 Z    =        -3916046.50
     XDOT =      20514.748616                 XDOT =        6253.115584
     YDOT =      -5947.487448  feet/sec       YDOT =       -1742.868637  meter/sec
     ZDOT =      13228.787155                 ZDOT =        4062.509686
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13292533.09                 X    =         4051564.09
     Y    =      -12430677.63  feet           Y    =        -3788870.54  meter
     Z    =      -12841836.11                 Z    =        -3914191.65
     XDOT =      19001.524464                 XDOT =        5791.664657
     YDOT =       6540.005264  feet/sec       YDOT =        1993.393604  meter/sec
     ZDOT =      13360.791172                 ZDOT =        4072.369149
  
  
    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   16045.50846845  .00016717  00000-0  10270-3 0  9025
    2 25544  51.6430 314.8025 0006364 111.0521 249.1313 15.54723810 25741
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16045.50846845   =   yrday.fracday
    Element set:     902
    Inclination:       51.6430  deg
    RA of node:       314.8025  deg
    Eccentricity:     .0006364     
    Arg of perigee:   111.0521  deg
    Mean anomaly:     249.1313  deg
    Mean motion:   15.54723810  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2574
    Checksum:              280
 
 
    Coasting Arc #4 (Orbit 2589)
    ---------------------------------------
 
    Vector Time (GMT): 2016/046/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2354104.73                 A    =         6785234.56  meter
     Y    =        5892853.23  meter          E    =           .0020150
     Z    =        2374631.51                 I    =           51.37250
     XDOT =      -5498.691745                 Wp   =          109.10098
     YDOT =        -26.244905  meter/sec      RA   =          309.17497  deg
     ZDOT =      -5355.285268                 TA   =           44.24337
                                              MA   =           44.08244
                                              Ha   =            222.309  n.mi
                                              Hp   =            211.560
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7723440.73                 X    =        -2431359.93
     Y    =       19333507.98  feet           Y    =         5866096.24  meter
     Z    =        7790785.80                 Z    =         2363008.02
     XDOT =     -18040.327246                 XDOT =       -5471.976202
     YDOT =        -86.105333  feet/sec       YDOT =         -87.585843  meter/sec
     ZDOT =     -17569.833557                 ZDOT =       -5381.931360
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17635561.51                 X    =        -5375319.15
     Y    =       11100594.59  feet           Y    =         3383461.23  meter
     Z    =        7739262.30                 Z    =         2358927.15
     XDOT =     -13659.092536                 XDOT =       -4163.291405
     YDOT =      -9299.377739  feet/sec       YDOT =       -2834.450335  meter/sec
     ZDOT =     -17685.312753                 ZDOT =       -5390.483327
  
  
    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   16046.53690216  .00016717  00000-0  10270-3 0  9039
    2 25544  51.6427 309.6705 0006395 115.4524 244.7291 15.54726308 25908
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16046.53690216   =   yrday.fracday
    Element set:     903
    Inclination:       51.6427  deg
    RA of node:       309.6705  deg
    Eccentricity:     .0006395     
    Arg of perigee:   115.4524  deg
    Mean anomaly:     244.7291  deg
    Mean motion:   15.54726308  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2590
    Checksum:              311
 
 
    Coasting Arc #5 (Orbit 2604)
    ---------------------------------------
 
    Vector Time (GMT): 2016/047/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3419768.48                 A    =         6787308.44  meter
     Y    =       -5832891.74  meter          E    =           .0013717
     Z    =        -560107.06                 I    =           51.36111
     XDOT =       4388.116433                 Wp   =           67.26865
     YDOT =       2012.544302  meter/sec      RA   =          304.17964  deg
     ZDOT =       5955.490911                 TA   =          286.66434
                                              MA   =          286.81488
                                              Ha   =            222.139  n.mi
                                              Hp   =            211.562
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11219712.86                 X    =         3487459.88
     Y    =      -19136783.93  feet           Y    =        -5794271.16  meter
     Z    =       -1837621.60                 Z    =         -543330.23
     XDOT =      14396.707457                 XDOT =        4336.356704
     YDOT =       6602.835637  feet/sec       YDOT =        2061.325993  meter/sec
     ZDOT =      19539.012174                 ZDOT =        5976.681192
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       20164315.93                 X    =         6146083.49
     Y    =       -9260925.62  feet           Y    =        -2822730.13  meter
     Z    =       -1763782.56                 Z    =         -537600.93
     XDOT =       7244.581075                 XDOT =        2208.148312
     YDOT =      12114.726535  feet/sec       YDOT =        3692.568648  meter/sec
     ZDOT =      19630.461713                 ZDOT =        5983.364730
  
  
    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   16047.50103925  .00016717  00000-0  10270-3 0  9044
    2 25544  51.6433 304.8592 0006218 118.7206 241.4572 15.54779802 26053
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16047.50103925   =   yrday.fracday
    Element set:     904
    Inclination:       51.6433  deg
    RA of node:       304.8592  deg
    Eccentricity:     .0006218     
    Arg of perigee:   118.7206  deg
    Mean anomaly:     241.4572  deg
    Mean motion:   15.54779802  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2605
    Checksum:              301
 
 
    Coasting Arc #6 (Orbit 2619)
    ---------------------------------------
 
    Vector Time (GMT): 2016/048/10:54:53.245
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1389771.33                 A    =         6780351.15  meter
     Y    =       -4885294.58  meter          E    =           .0013471
     Z    =       -4505441.74                 I    =           51.31609
     XDOT =       5389.431160                 Wp   =          116.45760
     YDOT =      -4435.357565  meter/sec      RA   =          299.37540  deg
     ZDOT =       3148.293494                 TA   =          185.31959
                                              MA   =          185.33392
                                              Ha   =            222.071  n.mi
                                              Hp   =            213.249
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4559617.22                 X    =        -1313154.33
     Y    =      -16027869.34  feet           Y    =        -4900407.72  meter
     Z    =      -14781632.99                 Z    =        -4512006.49
     XDOT =      17681.860761                 XDOT =        5423.335073
     YDOT =     -14551.698048  feet/sec       YDOT =       -4374.899670  meter/sec
     ZDOT =      10329.046895                 ZDOT =        3174.556101
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9471684.40                 X    =         2886969.40
     Y    =      -13680486.82  feet           Y    =        -4169812.38  meter
     Z    =      -14809147.64                 Z    =        -4513828.20
     XDOT =      21452.643858                 XDOT =        6538.765848
     YDOT =       3552.507993  feet/sec       YDOT =        1082.804436  meter/sec
     ZDOT =      10443.721631                 ZDOT =        3183.246353
  
  
    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   16048.46516015  .00016717  00000-0  10270-3 0  9059
    2 25544  51.6432 300.0467 0004038 131.8477 228.3021 15.54252646 26207
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16048.46516015   =   yrday.fracday
    Element set:     905
    Inclination:       51.6432  deg
    RA of node:       300.0467  deg
    Eccentricity:     .0004038     
    Arg of perigee:   131.8477  deg
    Mean anomaly:     228.3021  deg
    Mean motion:   15.54252646  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2620
    Checksum:              280
 
 
    Coasting Arc #7 (Orbit 2635)
    ---------------------------------------
 
    Vector Time (GMT): 2016/049/10:54:53.245
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         255028.16                 A    =         6784224.67  meter
     Y    =        5896793.25  meter          E    =           .0015767
     Z    =        3328117.32                 I    =           51.31391
     XDOT =      -5388.115992                 Wp   =          101.57572
     YDOT =       2867.524560  meter/sec      RA   =          294.36471  deg
     ZDOT =      -4652.198889                 TA   =           39.43094
                                              MA   =           39.31628
                                              Ha   =            221.999  n.mi
                                              Hp   =            213.329
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         836706.55                 X    =          172903.57
     Y    =       19346434.56  feet           Y    =         5899186.12  meter
     Z    =       10919020.07                 Z    =         3329156.41
     XDOT =     -17677.545904                 XDOT =       -5397.182983
     YDOT =       9407.888978  feet/sec       YDOT =        2807.220158  meter/sec
     ZDOT =     -15263.119713                 ZDOT =       -4678.394637
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14162365.25                 X    =        -4316688.93
     Y    =       13203716.09  feet           Y    =         4024492.66  meter
     Z    =       10922403.54                 Z    =         3329148.60
     XDOT =     -17634.998298                 XDOT =       -5375.147481
     YDOT =      -6152.617800  feet/sec       YDOT =       -1875.317906  meter/sec
     ZDOT =     -15377.200476                 ZDOT =       -4686.970705
  
  
    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   16049.49390278  .00016717  00000-0  10270-3 0  9065
    2 25544  51.6429 294.9173 0004083 135.6829 224.4651 15.54266131 26368
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16049.49390278   =   yrday.fracday
    Element set:     906
    Inclination:       51.6429  deg
    RA of node:       294.9173  deg
    Eccentricity:     .0004083     
    Arg of perigee:   135.6829  deg
    Mean anomaly:     224.4651  deg
    Mean motion:   15.54266131  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2636
    Checksum:              327
 
 
    Coasting Arc #8 (Orbit 2650)
    ---------------------------------------
 
    Vector Time (GMT): 2016/050/10:54:53.245
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         747120.70                 A    =         6787383.40  meter
     Y    =       -6498563.82  meter          E    =           .0007611
     Z    =       -1810443.98                 I    =           51.31325
     XDOT =       5114.751306                 Wp   =           68.96271
     YDOT =       -972.496298  meter/sec      RA   =          289.36301  deg
     ZDOT =       5623.342983                 TA   =          271.05540
                                              MA   =          271.14260
                                              Ha   =            221.846  n.mi
                                              Hp   =            213.352
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2451183.40                 X    =          828527.88
     Y    =      -21320747.43  feet           Y    =        -6489753.95  meter
     Z    =       -5939776.83                 Z    =        -1806616.63
     XDOT =      16780.680139                 XDOT =        5097.930710
     YDOT =      -3190.604653  feet/sec       YDOT =        -915.393478  meter/sec
     ZDOT =      18449.288003                 ZDOT =        5648.147797
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17572993.77                 X    =         5356248.50
     Y    =      -12328166.96  feet           Y    =        -3757625.29  meter
     Z    =       -5921968.35                 Z    =        -1805015.95
     XDOT =      12567.814299                 XDOT =        3830.669798
     YDOT =       9035.108398  feet/sec       YDOT =        2753.901040  meter/sec
     ZDOT =      18556.980367                 ZDOT =        5656.167616
  
  
    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   16050.45833035  .00016717  00000-0  10270-3 0  9077
    2 25544  51.6434 290.1079 0003950 140.1702 219.9741 15.54320476 26519
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16050.45833035   =   yrday.fracday
    Element set:     907
    Inclination:       51.6434  deg
    RA of node:       290.1079  deg
    Eccentricity:     .0003950     
    Arg of perigee:   140.1702  deg
    Mean anomaly:     219.9741  deg
    Mean motion:   15.54320476  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2651
    Checksum:              290
 
 
    Coasting Arc #9 (Orbit 2666)
    ---------------------------------------
 
    Vector Time (GMT): 2016/051/10:54:53.245
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1650321.18                 A    =         6788836.59  meter
     Y    =        6576763.77  meter          E    =           .0016118
     Z    =          41610.80                 I    =           51.30791
     XDOT =      -4662.641107                 Wp   =          136.82337
     YDOT =      -1123.483383  meter/sec      RA   =          284.36811  deg
     ZDOT =      -5987.574037                 TA   =           42.72615
                                              MA   =           42.60094
                                              Ha   =            221.801  n.mi
                                              Hp   =            213.471
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5414439.58                 X    =        -1723943.65
     Y    =       21577308.94  feet           Y    =         6557897.14  meter
     Z    =         136518.36                 Z    =           33414.84
     XDOT =     -15297.378960                 XDOT =       -4620.647155
     YDOT =      -3685.969104  feet/sec       YDOT =       -1175.389771  meter/sec
     ZDOT =     -19644.271776                 ZDOT =       -6010.121347
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19530598.28                 X    =        -5952926.36
     Y    =       10651799.37  feet           Y    =         3246668.45  meter
     Z    =          99776.18                 Z    =           30411.78
     XDOT =      -6800.401632                 XDOT =       -2072.762417
     YDOT =     -12226.527299  feet/sec       YDOT =       -3726.645521  meter/sec
     ZDOT =     -19741.790775                 ZDOT =       -6017.297828
  
  
    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   16051.48703651  .00016717  00000-0  10270-3 0  9082
    2 25544  51.6432 284.9781 0004006 145.5685 214.5728 15.54298849 26671
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16051.48703651   =   yrday.fracday
    Element set:     908
    Inclination:       51.6432  deg
    RA of node:       284.9781  deg
    Eccentricity:     .0004006     
    Arg of perigee:   145.5685  deg
    Mean anomaly:     214.5728  deg
    Mean motion:   15.54298849  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2667
    Checksum:              337
 
 
    Coasting Arc #10 (Orbit 2682)
    ---------------------------------------
 
    Vector Time (GMT): 2016/052/10:54:53.245
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2387559.31                 A    =         6787426.45  meter
     Y    =       -6117303.08  meter          E    =           .0014861
     Z    =        1696755.32                 I    =           51.29633
     XDOT =       4077.839799                 Wp   =           78.81649
     YDOT =       3174.224925  meter/sec      RA   =          279.37190  deg
     ZDOT =       5666.486075                 TA   =          299.88098
                                              MA   =          300.02855
                                              Ha   =            221.612  n.mi
                                              Hp   =            213.470
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7833199.84                 X    =         2447545.16
     Y    =      -20069891.98  feet           Y    =        -6090268.24  meter
     Z    =        5566782.54                 Z    =         1708499.46
     XDOT =      13378.739497                 XDOT =        4014.517082
     YDOT =      10414.123770  feet/sec       YDOT =        3219.472502  meter/sec
     ZDOT =      18590.833578                 ZDOT =        5686.140619
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19899143.92                 X    =         6065259.07
     Y    =       -8222029.55  feet           Y    =        -2506074.61  meter
     Z    =        5618803.50                 Z    =         1712611.31
     XDOT =       1025.209987                 XDOT =         312.484004
     YDOT =      15331.411992  feet/sec       YDOT =        4673.014375  meter/sec
     ZDOT =      18675.444022                 ZDOT =        5692.275338
  
  
    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   16052.51572228  .00016717  00000-0  10270-3 0  9092
    2 25544  51.6427 279.8477 0003722 147.8288 212.3092 15.54356478 26839
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16052.51572228   =   yrday.fracday
    Element set:     909
    Inclination:       51.6427  deg
    RA of node:       279.8477  deg
    Eccentricity:     .0003722     
    Arg of perigee:   147.8288  deg
    Mean anomaly:     212.3092  deg
    Mean motion:   15.54356478  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2683
    Checksum:              335
 
 
    Coasting Arc #11 (Orbit 2697)
    ---------------------------------------
 
    Vector Time (GMT): 2016/053/10:54:53.245
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3035713.18                 A    =         6783978.12  meter
     Y    =        5097416.31  meter          E    =           .0007266
     Z    =       -3291199.00                 I    =           51.28028
     XDOT =      -3383.505235                 Wp   =          120.80859
     YDOT =      -5033.423236  meter/sec      RA   =          274.36862  deg
     ZDOT =      -4686.303405                 TA   =           97.63522
                                              MA   =           97.55269
                                              Ha   =            221.445  n.mi
                                              Hp   =            213.566
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9959688.92                 X    =        -3076501.28
     Y    =       16723806.78  feet           Y    =         5063240.52  meter
     Z    =      -10797896.97                 Z    =        -3306045.02
     XDOT =     -11100.738961                 XDOT =       -3304.205267
     YDOT =     -16513.855762  feet/sec       YDOT =       -5070.816966  meter/sec
     ZDOT =     -15375.011170                 ZDOT =       -4702.546077
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18845936.22                 X    =        -5744241.36
     Y    =        4722081.56  feet           Y    =         1439290.46  meter
     Z    =      -10863163.86                 Z    =        -3311092.35
     XDOT =       4355.911198                 XDOT =        1327.681733
     YDOT =     -18060.219713  feet/sec       YDOT =       -5504.754969  meter/sec
     ZDOT =     -15444.507484                 ZDOT =       -4707.485881
  
  
    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   16053.48009814  .00016717  00000-0  10270-3 0  9107
    2 25544  51.6423 275.0381 0003688 155.0076 205.1256 15.54369225 26986
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16053.48009814   =   yrday.fracday
    Element set:     910
    Inclination:       51.6423  deg
    RA of node:       275.0381  deg
    Eccentricity:     .0003688     
    Arg of perigee:   155.0076  deg
    Mean anomaly:     205.1256  deg
    Mean motion:   15.54369225  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2698
    Checksum:              307
 
 
    Coasting Arc #12 (Orbit 2713)
    ---------------------------------------
 
    Vector Time (GMT): 2016/054/10:54:53.245
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3548879.28                 A    =         6779952.56  meter
     Y    =       -3647057.46  meter          E    =           .0011849
     Z    =        4475262.07                 I    =           51.26525
     XDOT =       2623.504682                 Wp   =          123.95460
     YDOT =       6469.666137  meter/sec      RA   =          269.35326  deg
     ZDOT =       3179.355004                 TA   =          293.88906
                                              MA   =          294.01317
                                              Ha   =            221.341  n.mi
                                              Hp   =            213.575
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11643304.71                 X    =         3567659.37
     Y    =      -11965411.61  feet           Y    =        -3607265.96  meter
     Z    =       14682618.34                 Z    =         4492547.35
     XDOT =       8607.298824                 XDOT =        2535.520672
     YDOT =      21225.938769  feet/sec       YDOT =        6498.512362  meter/sec
     ZDOT =      10430.954738                 ZDOT =        3191.884550
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16621653.99                 X    =         5066280.14
     Y    =        -483108.76  feet           Y    =         -147251.55  meter
     Z    =       14758188.42                 Z    =         4498295.83
     XDOT =      -8765.713351                 XDOT =       -2671.789430
     YDOT =      19937.229258  feet/sec       YDOT =        6076.867478  meter/sec
     ZDOT =      10484.114716                 ZDOT =        3195.558165
  
  
    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   16054.50874862  .00016717  00000-0  10270-3 0  9115
    2 25544  51.6420 269.9073 0003612 155.1700 204.9627 15.54398806 27140
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16054.50874862   =   yrday.fracday
    Element set:     911
    Inclination:       51.6420  deg
    RA of node:       269.9073  deg
    Eccentricity:     .0003612     
    Arg of perigee:   155.1700  deg
    Mean anomaly:     204.9627  deg
    Mean motion:   15.54398806  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2714
    Checksum:              309
 
 
    Coasting Arc #13 (Orbit 2728)
    ---------------------------------------
 
    Vector Time (GMT): 2016/055/10:54:53.245
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3987018.93                 A    =         6776933.46  meter
     Y    =        1847310.92  meter          E    =           .0014954
     Z    =       -5172058.09                 I    =           51.25609
     XDOT =      -1756.428752                 Wp   =           93.53029
     YDOT =      -7344.507254  meter/sec      RA   =          264.32654  deg
     ZDOT =      -1273.359027                 TA   =          164.18405
                                              MA   =          164.13730
                                              Ha   =            221.167  n.mi
                                              Hp   =            213.497
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13080770.76                 X    =        -3982256.50
     Y    =        6060731.37  feet           Y    =         1802751.35  meter
     Z    =      -16968694.52                 Z    =        -5191414.37
     XDOT =      -5762.561523                 XDOT =       -1667.984790
     YDOT =     -24096.152409  feet/sec       YDOT =       -7363.654460  meter/sec
     ZDOT =      -4177.687095                 ZDOT =       -1281.675353
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13590984.55                 X    =        -4142532.09
     Y    =       -4500971.22  feet           Y    =        -1371896.03  meter
     Z    =      -17052918.21                 Z    =        -5197729.47
     XDOT =      12046.457953                 XDOT =        3671.760384
     YDOT =     -20466.037696  feet/sec       YDOT =       -6238.048290  meter/sec
     ZDOT =      -4212.446922                 ZDOT =       -1283.953822
  
  
    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   16055.47308891  .00016717  00000-0  10270-3 0  9127
    2 25544  51.6410 265.0964 0003481 161.5351 198.5929 15.54460734 27291
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16055.47308891   =   yrday.fracday
    Element set:     912
    Inclination:       51.6410  deg
    RA of node:       265.0964  deg
    Eccentricity:     .0003481     
    Arg of perigee:   161.5351  deg
    Mean anomaly:     198.5929  deg
    Mean motion:   15.54460734  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2729
    Checksum:              322
 
 
    Coasting Arc #14 (Orbit 2744)
    ---------------------------------------
 
    Vector Time (GMT): 2016/056/10:54:53.245
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4293264.17                 A    =         6776515.28  meter
     Y    =          82019.07  meter          E    =           .0004099
     Z    =        5238980.47                 I    =           51.25931
     XDOT =        800.834480                 Wp   =          117.32474
     YDOT =       7590.914152  meter/sec      RA   =          259.29604  deg
     ZDOT =       -776.493509                 TA   =          340.12260
                                              MA   =          340.13857
                                              Ha   =            220.945  n.mi
                                              Hp   =            213.707
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14085512.38                 X    =         4266579.58
     Y    =         269091.44  feet           Y    =          129880.72  meter
     Z    =       17188256.14                 Z    =         5259770.95
     XDOT =       2627.409711                 XDOT =         719.663296
     YDOT =      24904.573989  feet/sec       YDOT =        7599.415652  meter/sec
     ZDOT =      -2547.550884                 ZDOT =        -772.801515
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10141318.44                 X    =         3091073.86
     Y    =        9618844.42  feet           Y    =         2931823.78  meter
     Z    =       17278359.60                 Z    =         5266444.01
     XDOT =     -14130.890927                 XDOT =       -4307.095555
     YDOT =      19440.135160  feet/sec       YDOT =        5925.353197  meter/sec
     ZDOT =      -2532.862468                 ZDOT =        -772.016480
  
  
    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   16056.50170151  .00016717  00000-0  10270-3 0  9139
    2 25544  51.6413 259.9658 0003493 166.0398 194.0852 15.54480593 27459
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16056.50170151   =   yrday.fracday
    Element set:     913
    Inclination:       51.6413  deg
    RA of node:       259.9658  deg
    Eccentricity:     .0003493     
    Arg of perigee:   166.0398  deg
    Mean anomaly:     194.0852  deg
    Mean motion:   15.54480593  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2745
    Checksum:              322
 
 
    Coasting Arc #15 (Orbit 2759)
    ---------------------------------------
 
    Vector Time (GMT): 2016/057/10:54:53.245
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4475798.79                 A    =         6778747.07  meter
     Y    =       -1981902.18  meter          E    =           .0012938
     Z    =       -4702040.78                 I    =           51.27283
     XDOT =        276.111640                 Wp   =          122.58371
     YDOT =      -7143.451355  meter/sec      RA   =          254.26688  deg
     ZDOT =       2746.826891                 TA   =          174.79439
                                              MA   =          174.78092
                                              Ha   =            220.950  n.mi
                                              Hp   =            213.616
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14684379.23                 X    =        -4430463.77
     Y    =       -6502303.75  feet           Y    =        -2031700.69  meter
     Z    =      -15426642.98                 Z    =        -4723672.47
     XDOT =        905.878085                 XDOT =         342.628204
     YDOT =     -23436.520194  feet/sec       YDOT =       -7139.991404  meter/sec
     ZDOT =       9011.899249                 ZDOT =        2748.330683
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6641837.85                 X    =        -2024432.18
     Y    =      -14522592.68  feet           Y    =        -4426486.25  meter
     Z    =      -15520069.36                 Z    =        -4730517.14
     XDOT =      15072.497052                 XDOT =        4594.097102
     YDOT =     -16537.013529  feet/sec       YDOT =       -5040.481724  meter/sec
     ZDOT =       9019.641823                 ZDOT =        2749.186828
  
  
    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   16057.46600801  .00016717  00000-0  10270-3 0  9146
    2 25544  51.6402 255.1541 0003418 170.4893 189.6325 15.54511672 27607
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16057.46600801   =   yrday.fracday
    Element set:     914
    Inclination:       51.6402  deg
    RA of node:       255.1541  deg
    Eccentricity:     .0003418     
    Arg of perigee:   170.4893  deg
    Mean anomaly:     189.6325  deg
    Mean motion:   15.54511672  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2760
    Checksum:              297
 
 
    Coasting Arc #16 (Orbit 2775)
    ---------------------------------------
 
    Vector Time (GMT): 2016/058/10:54:53.245
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4447488.38                 A    =         6782525.48  meter
     Y    =        3653616.81  meter          E    =           .0012415
     Z    =        3575024.75                 I    =           51.29623
     XDOT =      -1464.284472                 Wp   =          101.77440
     YDOT =       6107.365499  meter/sec      RA   =          249.24956  deg
     ZDOT =      -4409.470498                 TA   =           35.68551
                                              MA   =           35.60259
                                              Ha   =            220.600  n.mi
                                              Hp   =            213.796
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14591497.31                 X    =         4388936.40
     Y    =       11986931.80  feet           Y    =         3703024.66  meter
     Z    =       11729083.84                 Z    =         3596486.67
     XDOT =      -4804.082914                 XDOT =       -1511.050586
     YDOT =      20037.288382  feet/sec       YDOT =        6090.728848  meter/sec
     ZDOT =     -14466.766726                 ZDOT =       -4416.697935
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3283200.20                 X    =         1000719.42
     Y    =       18537598.11  feet           Y    =         5650259.90  meter
     Z    =       11821496.87                 Z    =         3603192.25
     XDOT =     -15222.580592                 XDOT =       -4639.842564
     YDOT =      11964.072156  feet/sec       YDOT =        3646.649193  meter/sec
     ZDOT =     -14499.132974                 ZDOT =       -4419.335731
  
  
    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   16058.49458144  .00016717  00000-0  10270-3 0  9152
    2 25544  51.6407 250.0232 0003240 176.5699 183.5476 15.54572147 27768
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16058.49458144   =   yrday.fracday
    Element set:     915
    Inclination:       51.6407  deg
    RA of node:       250.0232  deg
    Eccentricity:     .0003240     
    Arg of perigee:   176.5699  deg
    Mean anomaly:     183.5476  deg
    Mean motion:   15.54572147  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2776
    Checksum:              324
 
             

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