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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  16684.06
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   127.9
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.423
   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 
   ------------------------------------------------------------------------
   281/17:02:31.522          -0.7               3.1              3.2    
   N/A                       -3.0              -0.5              226.3  
   000/00:07:03.044           0.8               0.1              221.1  
   
 
 
    Coasting Arc #1 (Orbit 2750)
    ---------------------------------------
 
    Vector Time (GMT): 2014/272/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -972272.76                 A    =         6791109.73  meter
     Y    =       -5095914.13  meter          E    =           .0010759
     Z    =       -4393485.99                 I    =           51.33412
     XDOT =       5622.801933                 Wp   =          112.37966
     YDOT =      -3962.647236  meter/sec      RA   =          301.85860  deg
     ZDOT =       3354.473312                 TA   =          191.75771
                                              MA   =          191.78285
                                              Ha   =            226.969  n.mi
                                              Hp   =            219.407
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3189871.25                 X    =         -893874.35
     Y    =      -16718878.37  feet           Y    =        -5106348.75  meter
     Z    =      -14414324.11                 Z    =        -4398018.34
     XDOT =      18447.512903                 XDOT =        5650.400075
     YDOT =     -13000.811142  feet/sec       YDOT =       -3899.614816  meter/sec
     ZDOT =      11005.489870                 ZDOT =        3381.855878
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5210304.57                 X    =         1588100.83
     Y    =       16186992.70  feet           Y    =         4933795.37  meter
     Z    =      -14432702.65                 Z    =        -4399087.77
     XDOT =     -15385.463002                 XDOT =       -4689.489123
     YDOT =      14861.887838  feet/sec       YDOT =        4529.903413  meter/sec
     ZDOT =      11122.603595                 ZDOT =        3390.169576
  
  
    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   14272.50997117  .00016717  00000-0  10270-3 0  9002
    2 25544  51.6457 302.5077 0001867 122.7816 237.3515 15.50717336 27512
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14272.50997117   =   yrday.fracday
    Element set:     900
    Inclination:       51.6457  deg
    RA of node:       302.5077  deg
    Eccentricity:     .0001867     
    Arg of perigee:   122.7816  deg
    Mean anomaly:     237.3515  deg
    Mean motion:   15.50717336  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2751
    Checksum:              308
 
 
    Coasting Arc #2 (Orbit 2766)
    ---------------------------------------
 
    Vector Time (GMT): 2014/273/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         873008.40                 A    =         6792253.34  meter
     Y    =        5397216.38  meter          E    =           .0012161
     Z    =        4020530.76                 I    =           51.32163
     XDOT =      -5412.724601                 Wp   =           84.61002
     YDOT =       3784.644992  meter/sec      RA   =          296.87570  deg
     ZDOT =      -3893.937591                 TA   =           46.02471
                                              MA   =           45.92449
                                              Ha   =            226.844  n.mi
                                              Hp   =            219.370
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2864200.79                 X    =          793059.91
     Y    =       17707402.81  feet           Y    =         5406532.22  meter
     Z    =       13190717.71                 Z    =         4024577.15
     XDOT =     -17758.282811                 XDOT =       -5435.727362
     YDOT =      12416.814277  feet/sec       YDOT =        3723.987480  meter/sec
     ZDOT =     -12775.385796                 ZDOT =       -3920.288328
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5316522.45                 X    =        -1620476.04
     Y    =      -17119024.02  feet           Y    =        -5217878.52  meter
     Z    =       13206983.00                 Z    =         4025488.42
     XDOT =      14444.486796                 XDOT =        4402.679575
     YDOT =     -14457.413703  feet/sec       YDOT =       -4406.619697  meter/sec
     ZDOT =     -12888.078781                 ZDOT =       -3928.286412
  
  
    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   14273.54105683  .00016717  00000-0  10270-3 0  9017
    2 25544  51.6446 297.3936 0001873 124.7296 235.4032 15.50771928 27673
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14273.54105683   =   yrday.fracday
    Element set:     901
    Inclination:       51.6446  deg
    RA of node:       297.3936  deg
    Eccentricity:     .0001873     
    Arg of perigee:   124.7296  deg
    Mean anomaly:     235.4032  deg
    Mean motion:   15.50771928  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2767
    Checksum:              324
 
 
    Coasting Arc #3 (Orbit 2781)
    ---------------------------------------
 
    Vector Time (GMT): 2014/274/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -838659.80                 A    =         6793539.72  meter
     Y    =       -5690983.30  meter          E    =           .0007152
     Z    =       -3621848.42                 I    =           51.31376
     XDOT =       5193.430260                 Wp   =          105.37984
     YDOT =      -3542.107056  meter/sec      RA   =          291.89323  deg
     ZDOT =       4368.501305                 TA   =          211.57478
                                              MA   =          211.61771
                                              Ha   =            226.866  n.mi
                                              Hp   =            219.338
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2751508.52                 X    =         -757365.65
     Y    =      -18671205.06  feet           Y    =        -5699907.47  meter
     Z    =      -11882704.77                 Z    =        -3625724.65
     XDOT =      17038.813188                 XDOT =        5211.431972
     YDOT =     -11621.086142  feet/sec       YDOT =       -3483.929774  meter/sec
     ZDOT =      14332.353363                 ZDOT =        4393.774464
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5663086.74                 X    =         1726108.84
     Y    =       17992931.22  feet           Y    =         5484245.44  meter
     Z    =      -11898203.45                 Z    =        -3626572.41
     XDOT =     -13532.223767                 XDOT =       -4124.621804
     YDOT =      13796.492145  feet/sec       YDOT =        4205.170806  meter/sec
     ZDOT =      14440.420277                 ZDOT =        4401.440101
  
  
    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   14274.50768561  .00016717  00000-0  10270-3 0  9025
    2 25544  51.6456 292.5995 0001908 126.7421 233.3905 15.50777460 27827
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14274.50768561   =   yrday.fracday
    Element set:     902
    Inclination:       51.6456  deg
    RA of node:       292.5995  deg
    Eccentricity:     .0001908     
    Arg of perigee:   126.7421  deg
    Mean anomaly:     233.3905  deg
    Mean motion:   15.50777460  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2782
    Checksum:              326
 
 
    Coasting Arc #4 (Orbit 2797)
    ---------------------------------------
 
    Vector Time (GMT): 2014/275/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         814831.80                 A    =         6794796.50  meter
     Y    =        5963110.28  meter          E    =           .0014478
     Z    =        3138825.13                 I    =           51.30605
     XDOT =      -5014.678762                 Wp   =           98.56003
     YDOT =       3229.765963  meter/sec      RA   =          286.91045  deg
     ZDOT =      -4817.091456                 TA   =           45.10769
                                              MA   =           44.99025
                                              Ha   =            226.749  n.mi
                                              Hp   =            219.326
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2673332.67                 X    =          732842.87
     Y    =       19564010.10  feet           Y    =         5971764.09  meter
     Z    =       10297982.72                 Z    =         3142583.86
     XDOT =     -16452.358144                 XDOT =       -5027.022041
     YDOT =      10596.345024  feet/sec       YDOT =        3173.619169  meter/sec
     ZDOT =     -15804.105826                 ZDOT =       -4841.482431
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6064251.69                 X    =        -1848383.92
     Y    =      -18783334.65  feet           Y    =        -5725160.40  meter
     Z    =       10312945.16                 Z    =         3143385.68
     XDOT =      12825.075033                 XDOT =        3909.082870
     YDOT =     -12905.618374  feet/sec       YDOT =       -3933.632480  meter/sec
     ZDOT =     -15908.365402                 ZDOT =       -4848.869774
  
  
    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   14275.53873898  .00016717  00000-0  10270-3 0  9030
    2 25544  51.6441 287.4849 0001853 128.5268 231.6049 15.50817910 27982
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14275.53873898   =   yrday.fracday
    Element set:     903
    Inclination:       51.6441  deg
    RA of node:       287.4849  deg
    Eccentricity:     .0001853     
    Arg of perigee:   128.5268  deg
    Mean anomaly:     231.6049  deg
    Mean motion:   15.50817910  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2798
    Checksum:              346
 
 
    Coasting Arc #5 (Orbit 2812)
    ---------------------------------------
 
    Vector Time (GMT): 2014/276/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -852090.36                 A    =         6795947.59  meter
     Y    =       -6204268.35  meter          E    =           .0005712
     Z    =       -2641550.01                 I    =           51.30227
     XDOT =       4850.816269                 Wp   =           73.18565
     YDOT =      -2868.826777  meter/sec      RA   =          281.92901  deg
     ZDOT =       5184.304860                 TA   =          256.94843
                                              MA   =          257.01220
                                              Ha   =            226.742  n.mi
                                              Hp   =            219.281
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2795572.05                 X    =         -769817.62
     Y    =      -20355211.11  feet           Y    =        -6213337.21  meter
     Z    =       -8666502.64                 Z    =        -2645488.92
     XDOT =      15914.751538                 XDOT =        4857.351860
     YDOT =      -9412.161342  feet/sec       YDOT =       -2814.544763  meter/sec
     ZDOT =      17008.874214                 ZDOT =        5207.885666
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6671201.20                 X    =         2033382.13
     Y    =       19426078.97  feet           Y    =         5921068.87  meter
     Z    =       -8682202.54                 Z    =        -2646335.33
     XDOT =     -12243.595534                 XDOT =       -3731.847919
     YDOT =      11835.479337  feet/sec       YDOT =        3607.454102  meter/sec
     ZDOT =      17109.624327                 ZDOT =        5215.013495
  
  
    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   14276.50533648  .00016717  00000-0  10270-3 0  9045
    2 25544  51.6444 282.6909 0001932 132.1786 227.9529 15.50839205 28133
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14276.50533648   =   yrday.fracday
    Element set:     904
    Inclination:       51.6444  deg
    RA of node:       282.6909  deg
    Eccentricity:     .0001932     
    Arg of perigee:   132.1786  deg
    Mean anomaly:     227.9529  deg
    Mean motion:   15.50839205  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2813
    Checksum:              322
 
 
    Coasting Arc #6 (Orbit 2828)
    ---------------------------------------
 
    Vector Time (GMT): 2014/277/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         886276.44                 A    =         6797028.73  meter
     Y    =        6406645.97  meter          E    =           .0015551
     Z    =        2065263.82                 I    =           51.29910
     XDOT =      -4742.327000                 Wp   =          113.21685
     YDOT =       2440.153967  meter/sec      RA   =          276.94682  deg
     ZDOT =      -5507.375492                 TA   =           43.84256
                                              MA   =           43.71923
                                              Ha   =            226.626  n.mi
                                              Hp   =            219.309
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2907731.11                 X    =          804537.56
     Y    =       21019179.68  feet           Y    =         6416100.10  meter
     Z    =        6775799.93                 Z    =         2069369.95
     XDOT =     -15558.815617                 XDOT =       -4742.507766
     YDOT =       8005.754484  feet/sec       YDOT =        2387.120543  meter/sec
     ZDOT =     -18068.817230                 ZDOT =       -5530.413833
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7266676.39                 X    =        -2214882.96
     Y    =      -19930726.08  feet           Y    =        -6074885.31  meter
     Z    =        6792190.49                 Z    =         2070259.66
     XDOT =      11937.403117                 XDOT =        3638.520470
     YDOT =     -10573.778182  feet/sec       YDOT =       -3222.887590  meter/sec
     ZDOT =     -18167.185104                 ZDOT =       -5537.358020
  
  
    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   14277.53635642  .00016717  00000-0  10270-3 0  9057
    2 25544  51.6430 277.5756 0001774 133.5477 226.5821 15.50863973 28293
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14277.53635642   =   yrday.fracday
    Element set:     905
    Inclination:       51.6430  deg
    RA of node:       277.5756  deg
    Eccentricity:     .0001774     
    Arg of perigee:   133.5477  deg
    Mean anomaly:     226.5821  deg
    Mean motion:   15.50863973  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2829
    Checksum:              334
 
 
    Coasting Arc #7 (Orbit 2843)
    ---------------------------------------
 
    Vector Time (GMT): 2014/278/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -969070.44                 A    =         6797771.49  meter
     Y    =       -6559151.92  meter          E    =           .0008144
     Z    =       -1489727.14                 I    =           51.29881
     XDOT =       4668.505360                 Wp   =           51.19663
     YDOT =      -1987.102858  meter/sec      RA   =          271.96623  deg
     ZDOT =       5738.470995                 TA   =          292.48955
                                              MA   =          292.57576
                                              Ha   =            226.597  n.mi
                                              Hp   =            219.240
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3179364.96                 X    =         -888415.81
     Y    =      -21519527.30  feet           Y    =        -6569537.93  meter
     Z    =       -4887556.25                 Z    =        -1494237.99
     XDOT =      15316.618636                 XDOT =        4662.502847
     YDOT =      -6519.366333  feet/sec       YDOT =       -1934.929399  meter/sec
     ZDOT =      18827.004576                 ZDOT =        5761.135725
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7999100.18                 X    =         2438125.73
     Y    =       20224627.51  feet           Y    =         6164466.47  meter
     Z    =       -4905656.03                 Z    =        -1495243.96
     XDOT =     -11823.441046                 XDOT =       -3603.784831
     YDOT =       9245.589060  feet/sec       YDOT =        2818.055546  meter/sec
     ZDOT =      18923.705140                 ZDOT =        5767.945327
  
  
    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   14278.50292171  .00016717  00000-0  10270-3 0  9062
    2 25544  51.6427 272.7812 0001940 138.8214 221.3083 15.50903187 28443
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14278.50292171   =   yrday.fracday
    Element set:     906
    Inclination:       51.6427  deg
    RA of node:       272.7812  deg
    Eccentricity:     .0001940     
    Arg of perigee:   138.8214  deg
    Mean anomaly:     221.3083  deg
    Mean motion:   15.50903187  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2844
    Checksum:              299
 
 
    Coasting Arc #8 (Orbit 2859)
    ---------------------------------------
 
    Vector Time (GMT): 2014/279/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1029130.71                 A    =         6798397.10  meter
     Y    =        6659080.78  meter          E    =           .0015016
     Z    =         845564.13                 I    =           51.30016
     XDOT =      -4659.293492                 Wp   =          127.33637
     YDOT =       1477.924274  meter/sec      RA   =          266.98470  deg
     ZDOT =      -5904.770484                 TA   =           43.48324
                                              MA   =           43.36492
                                              Ha   =            226.495  n.mi
                                              Hp   =            219.302
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3376413.07                 X    =          950483.32
     Y    =       21847377.87  feet           Y    =         6670149.56  meter
     Z    =        2774160.54                 Z    =          850371.55
     XDOT =     -15286.395970                 XDOT =       -4646.789969
     YDOT =       4848.832920  feet/sec       YDOT =        1425.890089  meter/sec
     ZDOT =     -19372.606576                 ZDOT =       -5927.374706
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8630313.20                 X    =        -2630519.46
     Y    =      -20349889.59  feet           Y    =        -6202646.35  meter
     Z    =        2793517.39                 Z    =          851464.10
     XDOT =      12021.617223                 XDOT =        3664.188929
     YDOT =      -7799.334078  feet/sec       YDOT =       -2377.237027  meter/sec
     ZDOT =     -19468.963625                 ZDOT =       -5934.140113
  
  
    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   14279.53390701  .00016717  00000-0  10270-3 0  9075
    2 25544  51.6420 267.6652 0001684 139.3752 220.7525 15.50910287 28600
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14279.53390701   =   yrday.fracday
    Element set:     907
    Inclination:       51.6420  deg
    RA of node:       267.6652  deg
    Eccentricity:     .0001684     
    Arg of perigee:   139.3752  deg
    Mean anomaly:     220.7525  deg
    Mean motion:   15.50910287  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2860
    Checksum:              309
 
 
    Coasting Arc #9 (Orbit 2874)
    ---------------------------------------
 
    Vector Time (GMT): 2014/280/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1118663.49                 A    =         6798514.32  meter
     Y    =       -6697800.90  meter          E    =           .0011351
     Z    =        -219941.98                 I    =           51.30333
     XDOT =       4696.582950                 Wp   =           53.13298
     YDOT =       -973.361315  meter/sec      RA   =          262.00475  deg
     ZDOT =       5975.010325                 TA   =          304.48982
                                              MA   =          304.59697
                                              Ha   =            226.427  n.mi
                                              Hp   =            219.231
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3670155.80                 X    =        -1042615.56
     Y    =      -21974412.41  feet           Y    =        -6709885.35  meter
     Z    =        -721594.43                 Z    =         -225190.67
     XDOT =      15408.736712                 XDOT =        4678.093172
     YDOT =      -3193.442635  feet/sec       YDOT =        -920.943590  meter/sec
     ZDOT =      19603.052246                 ZDOT =        5997.781190
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9308305.24                 X    =         2837171.44
     Y    =       20240286.51  feet           Y    =         6169239.33  meter
     Z    =        -742831.54                 Z    =         -226415.05
     XDOT =     -12434.052130                 XDOT =       -3789.899089
     YDOT =       6415.416465  feet/sec       YDOT =        1955.418939  meter/sec
     ZDOT =      19700.034655                 ZDOT =        6004.570563
  
  
    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   14280.50043905  .00016717  00000-0  10270-3 0  9086
    2 25544  51.6417 262.8703 0001903 146.7283 213.3988 15.50965523 28755
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14280.50043905   =   yrday.fracday
    Element set:     908
    Inclination:       51.6417  deg
    RA of node:       262.8703  deg
    Eccentricity:     .0001903     
    Arg of perigee:   146.7283  deg
    Mean anomaly:     213.3988  deg
    Mean motion:   15.50965523  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2875
    Checksum:              315
 
 
    Coasting Arc #10 (Orbit 2890)
    ---------------------------------------
 
    Vector Time (GMT): 2014/281/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1161880.70                 A    =         6798473.24  meter
     Y    =        6676619.50  meter          E    =           .0012714
     Z    =        -458206.55                 I    =           51.30886
     XDOT =      -4798.590810                 Wp   =          139.22103
     YDOT =        433.131801  meter/sec      RA   =          257.02400  deg
     ZDOT =      -5959.956092                 TA   =           45.73704
                                              MA   =           45.63277
                                              Ha   =            226.355  n.mi
                                              Hp   =            219.305
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3811944.55                 X    =         1089360.70
     Y    =       21904919.63  feet           Y    =         6689206.86  meter
     Z    =       -1503302.32                 Z    =         -452739.27
     XDOT =     -15743.408169                 XDOT =       -4774.125479
     YDOT =       1421.036092  feet/sec       YDOT =         379.606823  meter/sec
     ZDOT =     -19553.661719                 ZDOT =       -5983.208011
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9785242.53                 X    =        -2982541.92
     Y    =      -19966763.44  feet           Y    =        -6085869.50  meter
     Z    =       -1481124.39                 Z    =         -451446.72
     XDOT =      13146.424027                 XDOT =        4007.030043
     YDOT =      -5010.463776  feet/sec       YDOT =       -1527.189359  meter/sec
     ZDOT =     -19652.603255                 ZDOT =       -5990.113472
  
  
    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   14281.53138858  .00016717  00000-0  10270-3 0  9093
    2 25544  51.6422 257.7540 0001603 146.5850 213.5403 15.50958466 28918
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14281.53138858   =   yrday.fracday
    Element set:     909
    Inclination:       51.6422  deg
    RA of node:       257.7540  deg
    Eccentricity:     .0001603     
    Arg of perigee:   146.5850  deg
    Mean anomaly:     213.5403  deg
    Mean motion:   15.50958466  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2891
    Checksum:              315
 
 
    Coasting Arc #11 (Orbit 2893)
    ---------------------------------------
 
    Vector Time (GMT): 2014/281/17:06:03.044
    Vector Time (MET): N/A
    Weight (LBS)     : 946249.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4442570.30                 A    =         6790006.17  meter
     Y    =       -1546921.05  meter          E    =           .0010853
     Z    =       -4906617.36                 I    =           51.27997
     XDOT =         42.357060                 Wp   =          113.62823
     YDOT =      -7310.249393  meter/sec      RA   =          255.94189  deg
     ZDOT =       2266.102512                 TA   =          178.67553
                                              MA   =          178.67265
                                              Ha   =            226.310  n.mi
                                              Hp   =            221.055
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14575361.87                 X    =        -4401106.87
     Y    =       -5075200.30  feet           Y    =        -1596369.58  meter
     Z    =      -16097825.98                 Z    =        -4928098.21
     XDOT =        138.966732                 XDOT =         113.090612
     YDOT =     -23983.757852  feet/sec       YDOT =       -7309.379930  meter/sec
     ZDOT =       7434.719526                 ZDOT =        2266.481075
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4328895.43                 X    =         1319447.33
     Y    =      -14714563.04  feet           Y    =        -4484998.81  meter
     Z    =      -16188920.04                 Z    =        -4934382.83
     XDOT =      22883.380593                 XDOT =        6974.854405
     YDOT =      -1451.581417  feet/sec       YDOT =        -442.442016  meter/sec
     ZDOT =       7437.499484                 ZDOT =        2266.949843
  
  
    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   14281.72468999  .00016717  00000-0  10270-3 0  9108
    2 25544  51.6457 256.7948 0001932 243.1739 116.9214 15.50375526 28941
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14281.72468999   =   yrday.fracday
    Element set:     910
    Inclination:       51.6457  deg
    RA of node:       256.7948  deg
    Eccentricity:     .0001932     
    Arg of perigee:   243.1739  deg
    Mean anomaly:     116.9214  deg
    Mean motion:   15.50375526  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2894
    Checksum:              343
 
 
    Coasting Arc #12 (Orbit 2909)
    ---------------------------------------
 
    Vector Time (GMT): 2014/282/17:06:03.044
    Vector Time (MET): N/A
    Weight (LBS)     : 946249.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4582156.42                 A    =         6790654.90  meter
     Y    =        1731439.45  meter          E    =           .0005866
     Z    =        4699906.37                 I    =           51.29128
     XDOT =        131.006099                 Wp   =           60.91688
     YDOT =       7149.952999  meter/sec      RA   =          250.95784  deg
     ZDOT =      -2756.340631                 TA   =           56.55576
                                              MA   =           56.49968
                                              Ha   =            226.036  n.mi
                                              Hp   =            221.147
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15033321.59                 X    =         4539623.39
     Y    =        5680575.61  feet           Y    =         1782442.82  meter
     Z    =       15419640.32                 Z    =         4722062.79
     XDOT =        429.810036                 XDOT =          64.433632
     YDOT =      23457.851048  feet/sec       YDOT =        7151.045442  meter/sec
     ZDOT =      -9043.112305                 ZDOT =       -2755.866752
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4647447.20                 X    =        -1416541.91
     Y    =       15289375.84  feet           Y    =         4660201.75  meter
     Z    =       15513581.99                 Z    =         4728539.79
     XDOT =     -22253.986306                 XDOT =       -6783.015026
     YDOT =       2428.305539  feet/sec       YDOT =         740.147528  meter/sec
     ZDOT =      -9042.236188                 ZDOT =       -2756.073590
  
  
    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   14282.75600769  .00016717  00000-0  10270-3 0  9116
    2 25544  51.6458 251.6825 0001955 249.3044 110.7898 15.50429996 29102
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14282.75600769   =   yrday.fracday
    Element set:     911
    Inclination:       51.6458  deg
    RA of node:       251.6825  deg
    Eccentricity:     .0001955     
    Arg of perigee:   249.3044  deg
    Mean anomaly:     110.7898  deg
    Mean motion:   15.50429996  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2910
    Checksum:              332
 
 
    Coasting Arc #13 (Orbit 2924)
    ---------------------------------------
 
    Vector Time (GMT): 2014/283/17:06:03.044
    Vector Time (MET): N/A
    Weight (LBS)     : 946249.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4760715.83                 A    =         6791574.13  meter
     Y    =       -1890339.48  meter          E    =           .0008014
     Z    =       -4467832.59                 I    =           51.30603
     XDOT =       -267.788117                 Wp   =          119.49224
     YDOT =      -6938.731917  meter/sec      RA   =          245.97462  deg
     ZDOT =       3221.630308                 TA   =          183.13602
                                              MA   =          183.14105
                                              Ha   =            226.131  n.mi
                                              Hp   =            221.052
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15619146.44                 X    =        -4717520.02
     Y    =       -6201901.17  feet           Y    =        -1943335.80  meter
     Z    =      -14658243.41                 Z    =        -4490854.87
     XDOT =       -878.569937                 XDOT =        -205.827691
     YDOT =     -22764.868495  feet/sec       YDOT =       -6941.379742  meter/sec
     ZDOT =      10569.653240                 ZDOT =        3220.480581
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4852607.00                 X    =         1479074.61
     Y    =      -16000080.12  feet           Y    =        -4876824.42  meter
     Z    =      -14755848.16                 Z    =        -4497582.52
     XDOT =      21432.985889                 XDOT =        6532.774099
     YDOT =      -3242.350425  feet/sec       YDOT =        -988.268410  meter/sec
     ZDOT =      10565.864802                 ZDOT =        3220.475592
  
  
    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   14283.72285202  .00016717  00000-0  10270-3 0  9126
    2 25544  51.6464 246.8892 0002000 252.3309 107.7623 15.50431136 29256
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14283.72285202   =   yrday.fracday
    Element set:     912
    Inclination:       51.6464  deg
    RA of node:       246.8892  deg
    Eccentricity:     .0002000     
    Arg of perigee:   252.3309  deg
    Mean anomaly:     107.7623  deg
    Mean motion:   15.50431136  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2925
    Checksum:              286
 
 
    Coasting Arc #14 (Orbit 2940)
    ---------------------------------------
 
    Vector Time (GMT): 2014/284/17:06:03.044
    Vector Time (MET): N/A
    Weight (LBS)     : 946249.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4950919.09                 A    =         6792462.42  meter
     Y    =        2036604.12  meter          E    =           .0008189
     Z    =        4175360.13                 I    =           51.32318
     XDOT =        351.281621                 Wp   =           74.12525
     YDOT =       6712.392925  meter/sec      RA   =          240.99337  deg
     ZDOT =      -3682.374992                 TA   =           53.89678
                                              MA   =           53.82098
                                              Ha   =            225.906  n.mi
                                              Hp   =            221.092
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16243172.86                 X    =         4907494.37
     Y    =        6681772.05  feet           Y    =         2091726.04  meter
     Z    =       13698688.09                 Z    =         4199305.84
     XDOT =       1152.498756                 XDOT =         294.084139
     YDOT =      22022.286499  feet/sec       YDOT =        6716.001081  meter/sec
     ZDOT =     -12081.282781                 ZDOT =       -3680.807946
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4989250.56                 X    =        -1520723.57
     Y    =       16757162.91  feet           Y    =         5107583.25  meter
     Z    =       13800205.35                 Z    =         4206302.59
     XDOT =     -20556.862023                 XDOT =       -6265.731545
     YDOT =       3846.350582  feet/sec       YDOT =        1172.367657  meter/sec
     ZDOT =     -12075.678869                 ZDOT =       -3680.666919
  
  
    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   14284.75413322  .00016717  00000-0  10270-3 0  9137
    2 25544  51.6465 241.7769 0001984 258.2346 101.8583 15.50486764 29415
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14284.75413322   =   yrday.fracday
    Element set:     913
    Inclination:       51.6465  deg
    RA of node:       241.7769  deg
    Eccentricity:     .0001984     
    Arg of perigee:   258.2346  deg
    Mean anomaly:     101.8583  deg
    Mean motion:   15.50486764  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2941
    Checksum:              326
 
 
    Coasting Arc #15 (Orbit 2955)
    ---------------------------------------
 
    Vector Time (GMT): 2014/285/17:06:03.044
    Vector Time (MET): N/A
    Weight (LBS)     : 946249.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5167856.87                 A    =         6793551.25  meter
     Y    =       -2142537.55  meter          E    =           .0004582
     Z    =       -3859489.54                 I    =           51.34254
     XDOT =       -389.448646                 Wp   =          116.70135
     YDOT =      -6451.490786  meter/sec      RA   =          236.01322  deg
     ZDOT =       4104.690602                 TA   =          196.64701
                                              MA   =          196.66206
                                              Ha   =            225.959  n.mi
                                              Hp   =            221.051
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16954910.99                 X    =        -5124765.93
     Y    =       -7029322.68  feet           Y    =        -2200087.20  meter
     Z    =      -12662367.25                 Z    =        -3884489.90
     XDOT =      -1277.718655                 XDOT =        -337.217263
     YDOT =     -21166.308354  feet/sec       YDOT =       -6455.553535  meter/sec
     ZDOT =      13466.832684                 ZDOT =        4102.925984
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4959226.04                 X    =         1511572.10
     Y    =      -17595194.97  feet           Y    =        -5363015.43  meter
     Z    =      -12768364.02                 Z    =        -3891797.35
     XDOT =      19566.645240                 XDOT =        5963.913469
     YDOT =      -4248.748705  feet/sec       YDOT =       -1295.018605  meter/sec
     ZDOT =      13460.341651                 ZDOT =        4102.712135
  
  
    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   14285.72094247  .00016717  00000-0  10270-3 0  9147
    2 25544  51.6463 236.9834 0002099 261.0036  99.0877 15.50485791 29567
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14285.72094247   =   yrday.fracday
    Element set:     914
    Inclination:       51.6463  deg
    RA of node:       236.9834  deg
    Eccentricity:     .0002099     
    Arg of perigee:   261.0036  deg
    Mean anomaly:      99.0877  deg
    Mean motion:   15.50485791  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2956
    Checksum:              338
 
 
    Coasting Arc #16 (Orbit 2971)
    ---------------------------------------
 
    Vector Time (GMT): 2014/286/17:06:03.044
    Vector Time (MET): N/A
    Weight (LBS)     : 946249.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5384965.53                 A    =         6794553.60  meter
     Y    =        2232459.60  meter          E    =           .0010130
     Z    =        3481985.60                 I    =           51.36460
     XDOT =        361.979702                 Wp   =           88.84422
     YDOT =       6184.034371  meter/sec      RA   =          231.03561  deg
     ZDOT =      -4513.063587                 TA   =           50.12370
                                              MA   =           50.03466
                                              Ha   =            225.798  n.mi
                                              Hp   =            221.032
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17667209.76                 X    =         5342686.81
     Y    =        7324342.53  feet           Y    =         2292441.60  meter
     Z    =       11423837.26                 Z    =         3508042.56
     XDOT =       1187.597446                 XDOT =         314.724837
     YDOT =      20288.826678  feet/sec       YDOT =        6187.817761  meter/sec
     ZDOT =     -14806.639064                 ZDOT =       -4511.420285
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4849464.29                 X    =        -1478116.71
     Y    =       18431558.67  feet           Y    =         5617939.08  meter
     Z    =       11534326.72                 Z    =         3515662.79
     XDOT =     -18577.532610                 XDOT =       -5662.431939
     YDOT =       4397.852061  feet/sec       YDOT =        1340.465308  meter/sec
     ZDOT =     -14800.615498                 ZDOT =       -4511.227604
  
  
    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   14286.75218610  .00016717  00000-0  10270-3 0  9154
    2 25544  51.6462 231.8709 0002048 266.6651  93.4266 15.50542842 29728
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14286.75218610   =   yrday.fracday
    Element set:     915
    Inclination:       51.6462  deg
    RA of node:       231.8709  deg
    Eccentricity:     .0002048     
    Arg of perigee:   266.6651  deg
    Mean anomaly:      93.4266  deg
    Mean motion:   15.50542842  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2972
    Checksum:              316
 
             

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