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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  6458.35
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   127.1
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.568
   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 
   ------------------------------------------------------------------------
    There are no maneuvers.
 
 
    Coasting Arc #1 (Orbit 2512)
    ---------------------------------------
 
    Vector Time (GMT): 2015/149/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6013219.92                 A    =         6783829.92  meter
     Y    =        2180167.73  meter          E    =           .0009386
     Z    =       -2247959.61                 I    =           51.67317
     XDOT =      -3515.273280                 Wp   =           25.41075
     YDOT =      -4088.316700  meter/sec      RA   =          176.20174  deg
     ZDOT =       5454.940227                 TA   =          309.58678
                                              MA   =          309.66963
                                              Ha   =            219.697  n.mi
                                              Hp   =            212.750
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19728411.80                 X    =        -6026232.25
     Y    =        7152781.28  feet           Y    =         2112851.33  meter
     Z    =       -7375195.56                 Z    =        -2277202.59
     XDOT =     -11533.048820                 XDOT =       -3495.793930
     YDOT =     -13413.112534  feet/sec       YDOT =       -4127.518138  meter/sec
     ZDOT =      17896.785522                 ZDOT =        5437.910571
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1522226.45                 X    =         -463974.62
     Y    =       20884976.42  feet           Y    =         6365740.81  meter
     Z    =       -7501107.13                 Z    =        -2286337.45
     XDOT =     -15478.701395                 XDOT =       -4717.908185
     YDOT =       5254.291582  feet/sec       YDOT =        1601.508074  meter/sec
     ZDOT =      17824.363671                 ZDOT =        5432.866047
  
  
    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   15149.50454785  .00016717  00000-0  10270-3 0  9005
    2 25544  51.6427 177.3246 0004296 357.9989   2.1146 15.55255957 25132
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15149.50454785   =   yrday.fracday
    Element set:     900
    Inclination:       51.6427  deg
    RA of node:       177.3246  deg
    Eccentricity:     .0004296     
    Arg of perigee:   357.9989  deg
    Mean anomaly:       2.1146  deg
    Mean motion:   15.55255957  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2513
    Checksum:              331
 
 
    Coasting Arc #2 (Orbit 2528)
    ---------------------------------------
 
    Vector Time (GMT): 2015/150/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6673260.97                 A    =         6786082.04  meter
     Y    =       -1197213.65  meter          E    =           .0010288
     Z    =         209619.41                 I    =           51.71084
     XDOT =       1029.352812                 Wp   =          113.49371
     YDOT =       4644.505762  meter/sec      RA   =          171.22770  deg
     ZDOT =      -6013.284903                 TA   =           64.24981
                                              MA   =           64.14366
                                              Ha   =            219.911  n.mi
                                              Hp   =            212.687
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21893900.82                 X    =         6685134.25
     Y    =       -3927866.31  feet           Y    =        -1122522.51  meter
     Z    =         687727.74                 Z    =          242066.13
     XDOT =       3377.141772                 XDOT =        1006.551104
     YDOT =      15237.879798  feet/sec       YDOT =        4655.889552  meter/sec
     ZDOT =     -19728.625009                 ZDOT =       -6008.339509
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4995511.36                 X    =         1522631.86
     Y    =      -21670360.63  feet           Y    =        -6605125.92  meter
     Z    =         827244.02                 Z    =          252143.98
     XDOT =      13805.755813                 XDOT =        4207.994372
     YDOT =       2406.273208  feet/sec       YDOT =         733.432074  meter/sec
     ZDOT =     -19708.177706                 ZDOT =       -6007.052565
  
  
    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   15150.53265247  .00016717  00000-0  10270-3 0  9014
    2 25544  51.6415 172.1903 0004406   1.8956 358.2214 15.55236087 25295
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15150.53265247   =   yrday.fracday
    Element set:     901
    Inclination:       51.6415  deg
    RA of node:       172.1903  deg
    Eccentricity:     .0004406     
    Arg of perigee:     1.8956  deg
    Mean anomaly:     358.2214  deg
    Mean motion:   15.55236087  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2529
    Checksum:              293
 
 
    Coasting Arc #3 (Orbit 2544)
    ---------------------------------------
 
    Vector Time (GMT): 2015/151/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6522186.65                 A    =         6784743.69  meter
     Y    =         108486.80  meter          E    =           .0016673
     Z    =        1830880.12                 I    =           51.73700
     XDOT =       1512.444611                 Wp   =           52.28506
     YDOT =      -4962.842388  meter/sec      RA   =          166.25748  deg
     ZDOT =       5656.716486                 TA   =          327.84608
                                              MA   =          327.94765
                                              Ha   =            220.051  n.mi
                                              Hp   =            212.620
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21398250.17                 X    =        -6531808.91
     Y    =         355927.82  feet           Y    =           35497.49  meter
     Z    =        6006824.54                 Z    =         1799172.69
     XDOT =       4962.088618                 XDOT =        1540.349210
     YDOT =     -16282.291300  feet/sec       YDOT =       -4945.773689  meter/sec
     ZDOT =      18558.781121                 ZDOT =        5664.131142
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7758364.92                 X    =        -2364749.63
     Y    =       19985919.37  feet           Y    =         6091708.22  meter
     Z    =        5870650.45                 Z    =         1789374.26
     XDOT =     -11791.868282                 XDOT =       -3594.161452
     YDOT =     -10063.365324  feet/sec       YDOT =       -3067.313751  meter/sec
     ZDOT =      18591.466056                 ZDOT =        5666.678854
  
  
    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   15151.56074953  .00016717  00000-0  10270-3 0  9021
    2 25544  51.6411 167.0565 0004533   5.3205 354.7996 15.55240819 25459
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15151.56074953   =   yrday.fracday
    Element set:     902
    Inclination:       51.6411  deg
    RA of node:       167.0565  deg
    Eccentricity:     .0004533     
    Arg of perigee:     5.3205  deg
    Mean anomaly:     354.7996  deg
    Mean motion:   15.55240819  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2545
    Checksum:              304
 
 
    Coasting Arc #4 (Orbit 2559)
    ---------------------------------------
 
    Vector Time (GMT): 2015/152/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5627540.84                 A    =         6780601.30  meter
     Y    =        1110471.46  meter          E    =           .0007839
     Z    =       -3625713.52                 I    =           51.75329
     XDOT =      -3820.199820                 Wp   =           49.61202
     YDOT =       4965.024542  meter/sec      RA   =          161.27890  deg
     ZDOT =      -4410.056237                 TA   =          173.25779
                                              MA   =          173.24724
                                              Ha   =            220.043  n.mi
                                              Hp   =            212.596
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18463060.50                 X    =         5632317.67
     Y    =        3643279.06  feet           Y    =         1173429.38  meter
     Z    =      -11895385.56                 Z    =        -3598363.85
     XDOT =     -12533.463975                 XDOT =       -3854.013234
     YDOT =      16289.450598  feet/sec       YDOT =        4922.115959  meter/sec
     ZDOT =     -14468.688440                 ZDOT =       -4428.695955
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10094831.99                 X    =         3076904.79
     Y    =      -15969614.42  feet           Y    =        -4867538.47  meter
     Z    =      -11778118.07                 Z    =        -3589970.39
     XDOT =       9527.413733                 XDOT =        2903.955706
     YDOT =      16750.117348  feet/sec       YDOT =        5105.435768  meter/sec
     ZDOT =     -14549.592009                 ZDOT =       -4434.715644
  
  
    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   15152.52458274  .00016717  00000-0  10270-3 0  9031
    2 25544  51.6405 162.2427 0004504   8.3806 351.7421 15.55251945 25603
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15152.52458274   =   yrday.fracday
    Element set:     903
    Inclination:       51.6405  deg
    RA of node:       162.2427  deg
    Eccentricity:     .0004504     
    Arg of perigee:     8.3806  deg
    Mean anomaly:     351.7421  deg
    Mean motion:   15.55251945  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2560
    Checksum:              288
 
 
    Coasting Arc #5 (Orbit 2575)
    ---------------------------------------
 
    Vector Time (GMT): 2015/153/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4105839.90                 A    =         6776181.45  meter
     Y    =       -2360908.67  meter          E    =           .0007325
     Z    =        4839496.17                 I    =           51.76746
     XDOT =       5601.988023                 Wp   =           83.07805
     YDOT =      -4612.145905  meter/sec      RA   =          156.28713  deg
     ZDOT =       2500.366148                 TA   =          342.40641
                                              MA   =          342.43177
                                              Ha   =            220.247  n.mi
                                              Hp   =            212.364
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13470603.34                 X    =        -4102643.28
     Y    =       -7745763.35  feet           Y    =        -2406805.55  meter
     Z    =       15877612.11                 Z    =         4819558.00
     XDOT =      18379.225796                 XDOT =        5640.999775
     YDOT =     -15131.712286  feet/sec       YDOT =       -4549.282979  meter/sec
     ZDOT =       8203.301011                 ZDOT =        2527.674119
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11953616.55                 X    =        -3643462.32
     Y    =       10063018.76  feet           Y    =         3067208.12  meter
     Z    =       15792380.29                 Z    =         4813517.51
     XDOT =      -7139.349955                 XDOT =       -2176.073866
     YDOT =     -21552.124239  feet/sec       YDOT =       -6569.087468  meter/sec
     ZDOT =       8321.393594                 ZDOT =        2536.360767
  
  
    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   15153.55266465  .00016717  00000-0  10270-3 0  9045
    2 25544  51.6396 157.1079 0004607  12.1713 347.9551 15.55259931 25763
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15153.55266465   =   yrday.fracday
    Element set:     904
    Inclination:       51.6396  deg
    RA of node:       157.1079  deg
    Eccentricity:     .0004607     
    Arg of perigee:    12.1713  deg
    Mean anomaly:     347.9551  deg
    Mean motion:   15.55259931  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2576
    Checksum:              322
 
 
    Coasting Arc #6 (Orbit 2590)
    ---------------------------------------
 
    Vector Time (GMT): 2015/154/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2208405.07                 A    =         6774077.78  meter
     Y    =        3573108.57  meter          E    =           .0016769
     Z    =       -5328495.24                 I    =           51.78934
     XDOT =      -6640.365970                 Wp   =           73.33019
     YDOT =       3810.510735  meter/sec      RA   =          151.28655  deg
     ZDOT =       -192.726098                 TA   =          194.80987
                                              MA   =          194.85904
                                              Ha   =            220.191  n.mi
                                              Hp   =            212.336
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7245423.45                 X    =         2194169.68
     Y    =       11722797.15  feet           Y    =         3597725.48  meter
     Z    =      -17481939.77                 Z    =        -5317801.25
     XDOT =     -21785.977593                 XDOT =       -6681.546282
     YDOT =      12501.675639  feet/sec       YDOT =        3736.023593  meter/sec
     ZDOT =       -632.303470                 ZDOT =        -225.083592
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13489100.61                 X    =         4111477.86
     Y    =       -3089781.72  feet           Y    =         -941765.47  meter
     Z    =      -17436621.40                 Z    =        -5314682.20
     XDOT =       4412.661997                 XDOT =        1344.979377
     YDOT =      23698.615891  feet/sec       YDOT =        7223.338124  meter/sec
     ZDOT =       -771.971483                 ZDOT =        -235.296908
  
  
    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   15154.51648365  .00016717  00000-0  10270-3 0  9056
    2 25544  51.6397 152.2948 0004601  14.9327 345.1961 15.55262489 25914
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15154.51648365   =   yrday.fracday
    Element set:     905
    Inclination:       51.6397  deg
    RA of node:       152.2948  deg
    Eccentricity:     .0004601     
    Arg of perigee:    14.9327  deg
    Mean anomaly:     345.1961  deg
    Mean motion:   15.55262489  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2591
    Checksum:              324
 
 
    Coasting Arc #7 (Orbit 2606)
    ---------------------------------------
 
    Vector Time (GMT): 2015/155/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -148606.50                 A    =         6775438.19  meter
     Y    =       -4599062.74  meter          E    =           .0010242
     Z    =        4970067.33                 I    =           51.82137
     XDOT =       6901.634829                 Wp   =           40.55676
     YDOT =      -2565.645687  meter/sec      RA   =          146.28571  deg
     ZDOT =      -2157.675979                 TA   =           70.45991
                                              MA   =           70.34933
                                              Ha   =            220.202  n.mi
                                              Hp   =            212.149
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -487554.14                 X    =         -121310.52
     Y    =      -15088788.52  feet           Y    =        -4600572.58  meter
     Z    =       16305995.19                 Z    =         4969411.13
     XDOT =      22643.158889                 XDOT =        6940.292794
     YDOT =      -8417.472728  feet/sec       YDOT =       -2488.250666  meter/sec
     ZDOT =      -7078.989434                 ZDOT =       -2124.055389
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14515243.04                 X    =        -4424246.08
     Y    =       -4157239.60  feet           Y    =        -1267126.63  meter
     Z    =       16303981.29                 Z    =         4969453.50
     XDOT =      -1202.966046                 XDOT =        -366.664051
     YDOT =     -23123.908402  feet/sec       YDOT =       -7048.167281  meter/sec
     ZDOT =      -6934.087932                 ZDOT =       -2113.510002
  
  
    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   15155.54454955  .00016717  00000-0  10270-3 0  9061
    2 25544  51.6393 147.1598 0004675  17.7047 342.4269 15.55295236 26070
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15155.54454955   =   yrday.fracday
    Element set:     906
    Inclination:       51.6393  deg
    RA of node:       147.1598  deg
    Eccentricity:     .0004675     
    Arg of perigee:    17.7047  deg
    Mean anomaly:     342.4269  deg
    Mean motion:   15.55295236  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2607
    Checksum:              335
 
 
    Coasting Arc #8 (Orbit 2621)
    ---------------------------------------
 
    Vector Time (GMT): 2015/156/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1752213.80                 A    =         6779605.90  meter
     Y    =        5291416.43  meter          E    =           .0008381
     Z    =       -3863854.73                 I    =           51.86142
     XDOT =      -6371.799556                 Wp   =           71.19454
     YDOT =        920.098245  meter/sec      RA   =          141.29791  deg
     ZDOT =       4159.576416                 TA   =          242.39203
                                              MA   =          242.47716
                                              Ha   =            220.319  n.mi
                                              Hp   =            212.015
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5748732.96                 X    =        -1792484.26
     Y    =       17360290.11  feet           Y    =         5271597.34  meter
     Z    =      -12676688.74                 Z    =        -3872463.82
     XDOT =     -20904.854185                 XDOT =       -6401.820459
     YDOT =       3018.695031  feet/sec       YDOT =         848.676241  meter/sec
     ZDOT =      13646.904252                 ZDOT =        4128.550565
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14899242.43                 X    =         4541289.09
     Y    =       10558275.76  feet           Y    =         3218162.45  meter
     Z    =      -12714614.77                 Z    =        -3875414.58
     XDOT =      -2567.230797                 XDOT =        -782.491947
     YDOT =      19856.651863  feet/sec       YDOT =        6052.307488  meter/sec
     ZDOT =      13513.419545                 ZDOT =        4118.890277
  
  
    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   15156.50835461  .00016717  00000-0  10270-3 0  9074
    2 25544  51.6396 142.3468 0004780  21.6509 338.4845 15.55280754 26221
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15156.50835461   =   yrday.fracday
    Element set:     907
    Inclination:       51.6396  deg
    RA of node:       142.3468  deg
    Eccentricity:     .0004780     
    Arg of perigee:    21.6509  deg
    Mean anomaly:     338.4845  deg
    Mean motion:   15.55280754  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2622
    Checksum:              319
 
 
    Coasting Arc #9 (Orbit 2637)
    ---------------------------------------
 
    Vector Time (GMT): 2015/157/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3356672.35                 A    =         6783893.38  meter
     Y    =       -5497534.16  meter          E    =           .0015039
     Z    =        2114950.69                 I    =           51.90058
     XDOT =       5204.792152                 Wp   =           91.37616
     YDOT =       1034.439488  meter/sec      RA   =          136.32603  deg
     ZDOT =      -5538.157416                 TA   =           65.26941
                                              MA   =           65.11296
                                              Ha   =            220.294  n.mi
                                              Hp   =            211.877
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11012704.55                 X    =         3407623.98
     Y    =      -18036529.38  feet           Y    =        -5459713.00  meter
     Z    =        6938814.60                 Z    =         2131379.88
     XDOT =      17076.089736                 XDOT =        5219.740247
     YDOT =       3393.830340  feet/sec       YDOT =        1092.727084  meter/sec
     ZDOT =     -18169.807796                 ZDOT =       -5512.837131
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14244755.01                 X    =        -4341801.33
     Y    =      -15578335.15  feet           Y    =        -4748276.55  meter
     Z    =        7010394.47                 Z    =         2136768.24
     XDOT =       6932.566883                 XDOT =        2113.046386
     YDOT =     -14515.847445  feet/sec       YDOT =       -4424.430301  meter/sec
     ZDOT =     -18061.171472                 ZDOT =       -5505.045065
  
  
    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   15157.53640479  .00016717  00000-0  10270-3 0  9082
    2 25544  51.6398 137.2118 0004854  23.7453 336.3923 15.55333448 26381
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15157.53640479   =   yrday.fracday
    Element set:     908
    Inclination:       51.6398  deg
    RA of node:       137.2118  deg
    Eccentricity:     .0004854     
    Arg of perigee:    23.7453  deg
    Mean anomaly:     336.3923  deg
    Mean motion:   15.55333448  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2638
    Checksum:              327
 
 
    Coasting Arc #10 (Orbit 2652)
    ---------------------------------------
 
    Vector Time (GMT): 2015/158/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4436771.36                 A    =         6785764.38  meter
     Y    =        5122757.29  meter          E    =           .0016517
     Z    =         -71339.86                 I    =           51.92926
     XDOT =      -3613.189700                 Wp   =           40.75451
     YDOT =      -3056.327935  meter/sec      RA   =          131.36796  deg
     ZDOT =       6040.698389                 TA   =          318.47938
                                              MA   =          318.60473
                                              Ha   =            220.322  n.mi
                                              Hp   =            211.758
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14556336.47                 X    =        -4493378.96
     Y    =       16806946.50  feet           Y    =         5072825.91  meter
     Z    =        -234054.66                 Z    =          -93029.80
     XDOT =     -11854.296916                 XDOT =       -3608.087965
     YDOT =     -10027.322620  feet/sec       YDOT =       -3096.705043  meter/sec
     ZDOT =      19818.564267                 ZDOT =        6023.158340
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12380599.65                 X    =         3773606.77
     Y    =       18466949.02  feet           Y    =         5628726.06  meter
     Z    =        -328191.77                 Z    =         -100032.85
     XDOT =     -11479.951084                 XDOT =       -3499.089090
     YDOT =       8014.114072  feet/sec       YDOT =        2442.701969  meter/sec
     ZDOT =      19743.716453                 ZDOT =        6017.884775
  
  
    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   15158.50019526  .00016717  00000-0  10270-3 0  9094
    2 25544  51.6398 132.3990 0004708  29.6662 330.4758 15.55354855 26533
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15158.50019526   =   yrday.fracday
    Element set:     909
    Inclination:       51.6398  deg
    RA of node:       132.3990  deg
    Eccentricity:     .0004708     
    Arg of perigee:    29.6662  deg
    Mean anomaly:     330.4758  deg
    Mean motion:   15.55354855  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2653
    Checksum:              331
 
 
    Coasting Arc #11 (Orbit 2668)
    ---------------------------------------
 
    Vector Time (GMT): 2015/159/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5004875.39                 A    =         6784090.33  meter
     Y    =       -4106563.51  meter          E    =           .0006923
     Z    =       -2031439.00                 I    =           51.94463
     XDOT =       1790.561263                 Wp   =           98.22883
     YDOT =       4935.541275  meter/sec      RA   =          126.41080  deg
     ZDOT =      -5582.986900                 TA   =          104.11849
                                              MA   =          104.04154
                                              Ha   =            220.431  n.mi
                                              Hp   =            211.739
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16420194.85                 X    =         5060291.95
     Y    =      -13472977.38  feet           Y    =        -4050285.70  meter
     Z    =       -6664826.11                 Z    =        -2006992.03
     XDOT =       5874.544827                 XDOT =        1762.357812
     YDOT =      16192.720719  feet/sec       YDOT =        4955.407250  meter/sec
     ZDOT =     -18316.886156                 ZDOT =       -5574.356821
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8995473.97                 X    =        -2741820.46
     Y    =      -19277570.29  feet           Y    =        -5875803.42  meter
     Z    =       -6559005.84                 Z    =        -1999184.98
     XDOT =      15762.835316                 XDOT =        4804.512204
     YDOT =      -1155.074367  feet/sec       YDOT =        -352.066667  meter/sec
     ZDOT =     -18280.669697                 ZDOT =       -5571.948124
  
  
    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   15159.52822980  .00016717  00000-0  10270-3 0  9105
    2 25544  51.6406 127.2639 0004901  30.9710 329.1732 15.55346055 26697
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15159.52822980   =   yrday.fracday
    Element set:     910
    Inclination:       51.6406  deg
    RA of node:       127.2639  deg
    Eccentricity:     .0004901     
    Arg of perigee:    30.9710  deg
    Mean anomaly:     329.1732  deg
    Mean motion:   15.55346055  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2669
    Checksum:              306
 
 
    Coasting Arc #12 (Orbit 2684)
    ---------------------------------------
 
    Vector Time (GMT): 2015/160/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5015911.52                 A    =         6779705.27  meter
     Y    =        2533405.99  meter          E    =           .0014415
     Z    =        3778601.58                 I    =           51.94854
     XDOT =         -5.836320                 Wp   =           79.73579
     YDOT =      -6385.051044  meter/sec      RA   =          121.44522  deg
     ZDOT =       4261.929933                 TA   =          325.38637
                                              MA   =          325.48012
                                              Ha   =            220.462  n.mi
                                              Hp   =            211.619
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16456402.61                 X    =        -5062222.93
     Y    =        8311699.43  feet           Y    =         2477055.59  meter
     Z    =       12396986.80                 Z    =         3754122.89
     XDOT =        -19.148032                 XDOT =          44.860389
     YDOT =     -20948.330196  feet/sec       YDOT =       -6384.833134  meter/sec
     ZDOT =      13982.709755                 ZDOT =        4262.024290
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4286661.86                 X    =         1306574.53
     Y    =       18003646.49  feet           Y    =         5487511.45  meter
     Z    =       12291300.14                 Z    =         3746388.28
     XDOT =     -19097.381007                 XDOT =       -5820.881731
     YDOT =      -5025.559487  feet/sec       YDOT =       -1531.790532  meter/sec
     ZDOT =      13984.262126                 ZDOT =        4262.403096
  
  
    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   15160.55625449  .00016717  00000-0  10270-3 0  9112
    2 25544  51.6407 122.1301 0004695  34.2187 325.9268 15.55386384 26858
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15160.55625449   =   yrday.fracday
    Element set:     911
    Inclination:       51.6407  deg
    RA of node:       122.1301  deg
    Eccentricity:     .0004695     
    Arg of perigee:    34.2187  deg
    Mean anomaly:     325.9268  deg
    Mean motion:   15.55386384  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2685
    Checksum:              314
 
 
    Coasting Arc #13 (Orbit 2699)
    ---------------------------------------
 
    Vector Time (GMT): 2015/161/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4600481.06                 A    =         6775451.17  meter
     Y    =        -528015.42  meter          E    =           .0016424
     Z    =       -4961245.42                 I    =           51.94997
     XDOT =      -1597.911536                 Wp   =           63.65526
     YDOT =       7145.835032  meter/sec      RA   =          116.46363  deg
     ZDOT =      -2240.875340                 TA   =          184.52205
                                              MA   =          184.53691
                                              Ha   =            220.477  n.mi
                                              Hp   =            211.662
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15093441.79                 X    =         4630143.53
     Y    =       -1732334.06  feet           Y    =         -476403.66  meter
     Z    =      -16277051.89                 Z    =        -4938825.04
     XDOT =      -5242.491915                 XDOT =       -1666.813821
     YDOT =      23444.340656  feet/sec       YDOT =        7127.581031  meter/sec
     ZDOT =      -7351.953216                 ZDOT =       -2248.804618
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1546595.44                 X    =          471402.29
     Y    =      -15216854.99  feet           Y    =        -4638097.40  meter
     Z    =      -16180567.09                 Z    =        -4931836.85
     XDOT =      20686.878835                 XDOT =        6305.360669
     YDOT =       9962.510937  feet/sec       YDOT =        3036.573334  meter/sec
     ZDOT =      -7387.336841                 ZDOT =       -2251.660269
  
  
    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   15161.52002234  .00016717  00000-0  10270-3 0  9122
    2 25544  51.6408 117.3157 0004872  37.3075 322.8416 15.55362110 27001
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15161.52002234   =   yrday.fracday
    Element set:     912
    Inclination:       51.6408  deg
    RA of node:       117.3157  deg
    Eccentricity:     .0004872     
    Arg of perigee:    37.3075  deg
    Mean anomaly:     322.8416  deg
    Mean motion:   15.55362110  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2700
    Checksum:              267
 
 
    Coasting Arc #14 (Orbit 2715)
    ---------------------------------------
 
    Vector Time (GMT): 2015/162/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3827395.67                 A    =         6773686.46  meter
     Y    =       -1664178.84  meter          E    =           .0006809
     Z    =        5330508.83                 I    =           51.95810
     XDOT =       2903.191807                 Wp   =           54.48190
     YDOT =      -7103.834190  meter/sec      RA   =          111.47346  deg
     ZDOT =       -129.297398                 TA   =           36.76709
                                              MA   =           36.72041
                                              Ha   =            220.608  n.mi
                                              Hp   =            211.435
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12557072.42                 X    =        -3834395.81
     Y    =       -5459904.32  feet           Y    =        -1707018.82  meter
     Z    =       17488546.04                 Z    =         5311898.80
     XDOT =       9524.907504                 XDOT =        2983.040891
     YDOT =     -23306.542619  feet/sec       YDOT =       -7070.922328  meter/sec
     ZDOT =       -424.204061                 ZDOT =        -115.000713
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7840026.89                 X    =        -2389640.20
     Y    =       11349281.61  feet           Y    =         3459261.04  meter
     Z    =       17408838.30                 Z    =         5306213.91
     XDOT =     -20153.803909                 XDOT =       -6142.879431
     YDOT =     -13347.659776  feet/sec       YDOT =       -4068.366700  meter/sec
     ZDOT =       -361.436397                 ZDOT =        -110.165814
  
  
    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   15162.54803130  .00016717  00000-0  10270-3 0  9130
    2 25544  51.6412 112.1816 0004877  39.9481 320.2031 15.55386343 27161
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15162.54803130   =   yrday.fracday
    Element set:     913
    Inclination:       51.6412  deg
    RA of node:       112.1816  deg
    Eccentricity:     .0004877     
    Arg of perigee:    39.9481  deg
    Mean anomaly:     320.2031  deg
    Mean motion:   15.55386343  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2716
    Checksum:              285
 
 
    Coasting Arc #15 (Orbit 2730)
    ---------------------------------------
 
    Vector Time (GMT): 2015/163/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2866766.13                 A    =         6775683.29  meter
     Y    =        3747697.71  meter          E    =           .0014560
     Z    =       -4875281.10                 I    =           51.97568
     XDOT =      -3838.507624                 Wp   =           90.06919
     YDOT =       6148.802792  meter/sec      RA   =          106.48362  deg
     ZDOT =       2475.901616                 TA   =          204.12203
                                              MA   =          204.19029
                                              Ha   =            220.544  n.mi
                                              Hp   =            211.444
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9405400.68                 X    =         2848327.95
     Y    =       12295596.16  feet           Y    =         3779653.11  meter
     Z    =      -15995016.73                 Z    =        -4861399.20
     XDOT =     -12593.528949                 XDOT =       -3919.006851
     YDOT =      20173.237507  feet/sec       YDOT =        6105.427765  meter/sec
     ZDOT =       8123.036798                 ZDOT =        2457.059721
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13800985.12                 X    =         4206540.26
     Y    =       -7145612.12  feet           Y    =        -2177982.58  meter
     Z    =      -15936023.47                 Z    =        -4857299.95
     XDOT =      17055.342177                 XDOT =        5198.468296
     YDOT =      15054.570917  feet/sec       YDOT =        4588.633216  meter/sec
     ZDOT =       8040.883781                 ZDOT =        2450.861377
  
  
    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   15163.51178205  .00016717  00000-0  10270-3 0  9147
    2 25544  51.6413 107.3674 0004887  43.1334 317.0201 15.55385007 27311
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15163.51178205   =   yrday.fracday
    Element set:     914
    Inclination:       51.6413  deg
    RA of node:       107.3674  deg
    Eccentricity:     .0004887     
    Arg of perigee:    43.1334  deg
    Mean anomaly:     317.0201  deg
    Mean motion:   15.55385007  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2731
    Checksum:              282
 
             

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