Return to Human Space Flight home page

    
   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  21527.82
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   132.3
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.252
   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 3681)
    ---------------------------------------
 
    Vector Time (GMT): 2014/332/11:11:28.187
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6721740.14                 A    =         6796371.84  meter
     Y    =         210463.78  meter          E    =           .0018746
     Z    =         940357.29                 I    =           51.69808
     XDOT =       -990.204862                 Wp   =          107.38413
     YDOT =      -4768.323581  meter/sec      RA   =            4.54718  deg
     ZDOT =      -5918.929447                 TA   =           62.45194
                                              MA   =           62.26160
                                              Ha   =            227.582  n.mi
                                              Hp   =            216.138
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -22052953.21                 X    =        -6728162.00
     Y    =         690497.96  feet           Y    =          135260.99  meter
     Z    =        3085161.72                 Z    =          907688.24
     XDOT =      -3248.703617                 XDOT =        -908.058342
     YDOT =     -15644.106236  feet/sec       YDOT =       -4778.937222  meter/sec
     ZDOT =     -19419.059865                 ZDOT =       -5923.540353
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12314782.86                 X    =         3753545.82
     Y    =      -18330196.48  feet           Y    =        -5587043.89  meter
     Z    =        2945806.49                 Z    =          897881.82
     XDOT =      13194.766361                 XDOT =        4021.764787
     YDOT =       5690.088784  feet/sec       YDOT =        1734.339061  meter/sec
     ZDOT =     -19437.764172                 ZDOT =       -5924.630520
  
  
    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   14332.50030582  .00016717  00000-0  10270-3 0  9003
    2 25544  51.6462   4.9335 0007174  73.7931 286.4009 15.51592790 36821
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14332.50030582   =   yrday.fracday
    Element set:     900
    Inclination:       51.6462  deg
    RA of node:         4.9335  deg
    Eccentricity:     .0007174     
    Arg of perigee:    73.7931  deg
    Mean anomaly:     286.4009  deg
    Mean motion:   15.51592790  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3682
    Checksum:              298
 
 
    Coasting Arc #2 (Orbit 3696)
    ---------------------------------------
 
    Vector Time (GMT): 2014/333/11:11:28.187
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6787935.11                 A    =         6796773.95  meter
     Y    =        -130192.31  meter          E    =           .0018587
     Z    =        -103340.17                 I    =           51.66764
     XDOT =        170.676624                 Wp   =           56.39038
     YDOT =       4752.588474  meter/sec      RA   =          359.59078  deg
     ZDOT =       6012.226630                 TA   =          302.49789
                                              MA   =          302.67740
                                              Ha   =            227.684  n.mi
                                              Hp   =            216.057
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       22270128.32                 X    =         6789388.45
     Y    =        -427140.11  feet           Y    =          -54277.09  meter
     Z    =        -339042.54                 Z    =          -70361.57
     XDOT =        559.962676                 XDOT =          88.313713
     YDOT =      15592.481869  feet/sec       YDOT =        4754.036492  meter/sec
     ZDOT =      19725.152985                 ZDOT =        6012.855767
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12328141.37                 X    =        -3757617.49
     Y    =       18553532.97  feet           Y    =         5655116.85  meter
     Z    =        -198389.93                 Z    =          -60469.25
     XDOT =     -11715.464252                 XDOT =       -3570.873504
     YDOT =      -7620.849621  feet/sec       YDOT =       -2322.834964  meter/sec
     ZDOT =      19726.881505                 ZDOT =        6012.753483
  
  
    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   14333.46641773  .00016717  00000-0  10270-3 0  9010
    2 25544  51.6459    .1362 0007284  76.4424 283.7539 15.51570320 36973
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14333.46641773   =   yrday.fracday
    Element set:     901
    Inclination:       51.6459  deg
    RA of node:          .1362  deg
    Eccentricity:     .0007284     
    Arg of perigee:    76.4424  deg
    Mean anomaly:     283.7539  deg
    Mean motion:   15.51570320  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3697
    Checksum:              307
 
 
    Coasting Arc #3 (Orbit 3712)
    ---------------------------------------
 
    Vector Time (GMT): 2014/334/11:11:28.187
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6744244.82                 A    =         6796230.42  meter
     Y    =         -13501.94  meter          E    =           .0015209
     Z    =        -814073.49                 I    =           51.63597
     XDOT =        715.138641                 Wp   =          115.68341
     YDOT =      -4788.396411  meter/sec      RA   =          354.63189  deg
     ZDOT =      -5938.198521                 TA   =           73.10792
                                              MA   =           72.94120
                                              Ha   =            227.541  n.mi
                                              Hp   =            215.905
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -22126787.48                 X    =        -6739638.04
     Y    =         -44297.71  feet           Y    =          -88894.70  meter
     Z    =       -2670844.78                 Z    =         -846825.22
     XDOT =       2346.255383                 XDOT =         797.476605
     YDOT =     -15709.961979  feet/sec       YDOT =       -4779.938847  meter/sec
     ZDOT =     -19482.278611                 ZDOT =       -5934.524481
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12309430.05                 X    =         3751914.28
     Y    =      -18365978.25  feet           Y    =        -5597950.17  meter
     Z    =       -2810493.37                 Z    =         -856638.38
     XDOT =      10359.179566                 XDOT =        3157.477932
     YDOT =       9877.432926  feet/sec       YDOT =        3010.641556  meter/sec
     ZDOT =     -19465.651777                 ZDOT =       -5933.130662
  
  
    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   14334.49691238  .00016717  00000-0  10270-3 0  9026
    2 25544  51.6466 355.0180 0007317  81.2945 278.9035 15.51649345 37130
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14334.49691238   =   yrday.fracday
    Element set:     902
    Inclination:       51.6466  deg
    RA of node:       355.0180  deg
    Eccentricity:     .0007317     
    Arg of perigee:    81.2945  deg
    Mean anomaly:     278.9035  deg
    Mean motion:   15.51649345  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3713
    Checksum:              320
 
 
    Coasting Arc #4 (Orbit 3728)
    ---------------------------------------
 
    Vector Time (GMT): 2014/335/11:11:28.187
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6580494.33                 A    =         6795329.39  meter
     Y    =         133353.38  meter          E    =           .0021115
     Z    =        1654329.21                 I    =           51.60106
     XDOT =      -1547.318747                 Wp   =           70.57980
     YDOT =       4881.109740  meter/sec      RA   =          349.67030  deg
     ZDOT =       5708.771435                 TA   =          307.54225
                                              MA   =          307.73391
                                              Ha   =            227.596  n.mi
                                              Hp   =            215.799
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21589548.34                 X    =         6570477.76
     Y    =         437511.08  feet           Y    =          206884.71  meter
     Z    =        5427589.28                 Z    =         1686272.43
     XDOT =      -5076.505075                 XDOT =       -1629.517204
     YDOT =      16014.139566  feet/sec       YDOT =        4863.346959  meter/sec
     ZDOT =      18729.565075                 ZDOT =        5701.055072
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12022800.11                 X    =        -3664549.47
     Y    =       17895686.87  feet           Y    =         5454605.36  meter
     Z    =        5563758.45                 Z    =         1695833.58
     XDOT =      -9359.312348                 XDOT =       -2852.718404
     YDOT =     -12152.655563  feet/sec       YDOT =       -3704.129415  meter/sec
     ZDOT =      18695.685009                 ZDOT =        5698.444791
  
  
    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   14335.52738374  .00016717  00000-0  10270-3 0  9035
    2 25544  51.6457 349.9006 0007471  83.9022 276.2981 15.51651747 37292
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14335.52738374   =   yrday.fracday
    Element set:     903
    Inclination:       51.6457  deg
    RA of node:       349.9006  deg
    Eccentricity:     .0007471     
    Arg of perigee:    83.9022  deg
    Mean anomaly:     276.2981  deg
    Mean motion:   15.51651747  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3729
    Checksum:              331
 
 
    Coasting Arc #5 (Orbit 3743)
    ---------------------------------------
 
    Vector Time (GMT): 2014/336/11:11:28.187
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6300835.26                 A    =         6793582.29  meter
     Y    =        -350770.97  meter          E    =           .0011802
     Z    =       -2520933.02                 I    =           51.56560
     XDOT =       2383.987948                 Wp   =          104.44553
     YDOT =      -5001.138151  meter/sec      RA   =          344.70409  deg
     ZDOT =      -5286.341986                 TA   =          103.82195
                                              MA   =          103.69060
                                              Ha   =            227.464  n.mi
                                              Hp   =            215.704
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20672031.71                 X    =        -6284198.48
     Y    =       -1150823.39  feet           Y    =         -421137.92  meter
     Z    =       -8270777.62                 Z    =        -2551501.68
     XDOT =       7821.482769                 XDOT =        2465.414424
     YDOT =     -16407.933565  feet/sec       YDOT =       -4974.023449  meter/sec
     ZDOT =     -17343.641687                 ZDOT =       -5274.563051
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11827843.16                 X    =         3605126.59
     Y    =      -16928903.68  feet           Y    =        -5159929.84  meter
     Z    =       -8401035.55                 Z    =        -2560635.63
     XDOT =       8547.543477                 XDOT =        2605.291252
     YDOT =      14515.477517  feet/sec       YDOT =        4424.317547  meter/sec
     ZDOT =     -17292.417541                 ZDOT =       -5270.728866
  
  
    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   14336.49342530  .00016717  00000-0  10270-3 0  9048
    2 25544  51.6461 345.1020 0007376  88.3989 271.8007 15.51713526 37447
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14336.49342530   =   yrday.fracday
    Element set:     904
    Inclination:       51.6461  deg
    RA of node:       345.1020  deg
    Eccentricity:     .0007376     
    Arg of perigee:    88.3989  deg
    Mean anomaly:     271.8007  deg
    Mean motion:   15.51713526  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3744
    Checksum:              309
 
 
    Coasting Arc #6 (Orbit 3759)
    ---------------------------------------
 
    Vector Time (GMT): 2014/337/11:11:28.187
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5918428.07                 A    =         6791675.05  meter
     Y    =         578597.65  meter          E    =           .0020113
     Z    =        3262975.08                 I    =           51.52822
     XDOT =      -3127.568958                 Wp   =           88.76969
     YDOT =       5163.529163  meter/sec      RA   =          339.73330  deg
     ZDOT =       4732.375171                 TA   =          309.14112
                                              MA   =          309.31971
                                              Ha   =            227.418  n.mi
                                              Hp   =            215.644
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19417414.94                 X    =         5895667.42
     Y    =        1898286.27  feet           Y    =          644653.96  meter
     Z    =       10705298.81                 Z    =         3291671.21
     XDOT =     -10261.053012                 XDOT =       -3208.065056
     YDOT =      16940.712476  feet/sec       YDOT =        5128.104390  meter/sec
     ZDOT =      15526.165260                 ZDOT =        4716.986297
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11527905.98                 X    =        -3513705.74
     Y    =       15656150.88  feet           Y    =         4771994.79  meter
     Z    =       10827522.33                 Z    =         3300228.81
     XDOT =      -8119.351106                 XDOT =       -2474.778217
     YDOT =     -16725.692494  feet/sec       YDOT =       -5097.991072  meter/sec
     ZDOT =      15459.518843                 ZDOT =        4712.061343
  
  
    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   14337.52384769  .00016717  00000-0  10270-3 0  9054
    2 25544  51.6448 339.9838 0007495  91.3406 268.8605 15.51740144 37604
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14337.52384769   =   yrday.fracday
    Element set:     905
    Inclination:       51.6448  deg
    RA of node:       339.9838  deg
    Eccentricity:     .0007495     
    Arg of perigee:    91.3406  deg
    Mean anomaly:     268.8605  deg
    Mean motion:   15.51740144  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3760
    Checksum:              342
 
 
    Coasting Arc #7 (Orbit 3774)
    ---------------------------------------
 
    Vector Time (GMT): 2014/338/11:11:28.187
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5439245.60                 A    =         6789386.91  meter
     Y    =        -927204.08  meter          E    =           .0014045
     Z    =       -3969389.68                 I    =           51.49205
     XDOT =       3808.483198                 Wp   =           83.79270
     YDOT =      -5305.630735  meter/sec      RA   =          334.75673  deg
     ZDOT =      -3990.128288                 TA   =          144.47633
                                              MA   =          144.38274
                                              Ha   =            227.373  n.mi
                                              Hp   =            215.527
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17845293.95                 X    =        -5409190.78
     Y    =       -3042008.14  feet           Y    =         -987860.98  meter
     Z    =      -13022932.03                 Z    =        -3995740.28
     XDOT =      12495.023614                 XDOT =        3886.912032
     YDOT =     -17406.924982  feet/sec       YDOT =       -5262.603053  meter/sec
     ZDOT =     -13090.972073                 ZDOT =       -3971.436701
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11461906.18                 X    =         3493589.00
     Y    =      -13906811.29  feet           Y    =        -4238796.08  meter
     Z    =      -13135082.61                 Z    =        -4003573.18
     XDOT =       7850.523933                 XDOT =        2392.839695
     YDOT =      18725.699725  feet/sec       YDOT =        5707.593276  meter/sec
     ZDOT =     -13010.217472                 ZDOT =       -3965.514285
  
  
    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   14338.48984465  .00016717  00000-0  10270-3 0  9060
    2 25544  51.6449 335.1849 0007419  95.2090 264.9908 15.51785005 37757
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14338.48984465   =   yrday.fracday
    Element set:     906
    Inclination:       51.6449  deg
    RA of node:       335.1849  deg
    Eccentricity:     .0007419     
    Arg of perigee:    95.2090  deg
    Mean anomaly:     264.9908  deg
    Mean motion:   15.51785005  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3775
    Checksum:              351
 
 
    Coasting Arc #8 (Orbit 3790)
    ---------------------------------------
 
    Vector Time (GMT): 2014/339/11:11:28.187
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4890674.16                 A    =         6787320.17  meter
     Y    =        1308637.43  meter          E    =           .0016059
     Z    =        4509593.54                 I    =           51.45644
     XDOT =      -4377.678643                 Wp   =          105.74613
     YDOT =       5455.571119  meter/sec      RA   =          329.77488  deg
     ZDOT =       3150.822338                 TA   =          312.51044
                                              MA   =          312.64598
                                              Ha   =            227.233  n.mi
                                              Hp   =            215.579
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16045518.89                 X    =         4853770.69
     Y    =        4293429.89  feet           Y    =         1363121.44  meter
     Z    =       14795254.41                 Z    =         4533262.57
     XDOT =     -14362.462738                 XDOT =       -4453.664661
     YDOT =      17898.855377  feet/sec       YDOT =        5406.191980  meter/sec
     ZDOT =      10337.343630                 ZDOT =        3129.371710
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11445814.11                 X    =        -3488684.14
     Y    =       11912070.26  feet           Y    =         3630799.02  meter
     Z    =       14895895.10                 Z    =         4540268.83
     XDOT =      -7871.165218                 XDOT =       -2399.131158
     YDOT =     -20429.645827  feet/sec       YDOT =       -6226.956048  meter/sec
     ZDOT =      10244.797241                 ZDOT =        3122.614199
  
  
    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   14339.52021832  .00016717  00000-0  10270-3 0  9077
    2 25544  51.6439 330.0658 0007439  98.4509 261.7486 15.51817089 37912
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14339.52021832   =   yrday.fracday
    Element set:     907
    Inclination:       51.6439  deg
    RA of node:       330.0658  deg
    Eccentricity:     .0007439     
    Arg of perigee:    98.4509  deg
    Mean anomaly:     261.7486  deg
    Mean motion:   15.51817089  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3791
    Checksum:              333
 
 
    Coasting Arc #9 (Orbit 3805)
    ---------------------------------------
 
    Vector Time (GMT): 2014/340/11:11:28.187
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4287324.49                 A    =         6785504.74  meter
     Y    =       -1811521.29  meter          E    =           .0019378
     Z    =       -4955045.86                 I    =           51.42407
     XDOT =       4830.208291                 Wp   =           84.20939
     YDOT =      -5522.980610  meter/sec      RA   =          324.78775  deg
     ZDOT =      -2165.570319                 TA   =          164.59140
                                              MA   =          164.53232
                                              Ha   =            227.271  n.mi
                                              Hp   =            215.424
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14066025.22                 X    =        -4242678.69
     Y    =       -5943311.31  feet           Y    =        -1859214.86  meter
     Z    =      -16256712.13                 Z    =        -4975765.04
     XDOT =      15847.140062                 XDOT =        4902.128322
     YDOT =     -18120.015125  feet/sec       YDOT =       -5468.563771  meter/sec
     ZDOT =      -7104.889499                 ZDOT =       -2141.931361
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11771201.72                 X    =         3587862.28
     Y    =       -9578468.46  feet           Y    =        -2919517.19  meter
     Z    =      -16344676.69                 Z    =        -4981857.46
     XDOT =       7918.236386                 XDOT =        2413.478450
     YDOT =      21650.662848  feet/sec       YDOT =        6599.122036  meter/sec
     ZDOT =      -7003.001522                 ZDOT =       -2134.514864
  
  
    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   14340.48617025  .00016717  00000-0  10270-3 0  9080
    2 25544  51.6440 325.2667 0007431 102.1375 258.0609 15.51850972 38067
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14340.48617025   =   yrday.fracday
    Element set:     908
    Inclination:       51.6440  deg
    RA of node:       325.2667  deg
    Eccentricity:     .0007431     
    Arg of perigee:   102.1375  deg
    Mean anomaly:     258.0609  deg
    Mean motion:   15.51850972  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3806
    Checksum:              301
 
 
    Coasting Arc #10 (Orbit 3821)
    ---------------------------------------
 
    Vector Time (GMT): 2014/341/11:11:28.187
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3654992.08                 A    =         6784265.72  meter
     Y    =        2349254.34  meter          E    =           .0011049
     Z    =        5202105.67                 I    =           51.39470
     XDOT =      -5176.226855                 Wp   =          110.99764
     YDOT =       5550.349274  meter/sec      RA   =          319.79637  deg
     ZDOT =       1124.468140                 TA   =          328.15924
                                              MA   =          328.22599
                                              Ha   =            227.073  n.mi
                                              Hp   =            215.551
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11991443.82                 X    =         3603180.16
     Y    =        7707527.37  feet           Y    =         2389836.64  meter
     Z    =       17067275.82                 Z    =         5219735.62
     XDOT =     -16982.371572                 XDOT =       -5243.369792
     YDOT =      18209.807329  feet/sec       YDOT =        5492.089825  meter/sec
     ZDOT =       3689.199933                 ZDOT =        1099.159995
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12241043.00                 X    =        -3731069.90
     Y    =        7127588.55  feet           Y    =         2172488.99  meter
     Z    =       17141964.73                 Z    =         5224870.85
     XDOT =      -8060.323598                 XDOT =       -2456.786633
     YDOT =     -22499.092953  feet/sec       YDOT =       -6857.723532  meter/sec
     ZDOT =       3580.192658                 ZDOT =        1091.242722
  
  
    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   14341.51649508  .00016717  00000-0  10270-3 0  9097
    2 25544  51.6435 320.1473 0007374 105.4990 254.6976 15.51888717 38220
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14341.51649508   =   yrday.fracday
    Element set:     909
    Inclination:       51.6435  deg
    RA of node:       320.1473  deg
    Eccentricity:     .0007374     
    Arg of perigee:   105.4990  deg
    Mean anomaly:     254.6976  deg
    Mean motion:   15.51888717  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3822
    Checksum:              331
 
 
    Coasting Arc #11 (Orbit 3836)
    ---------------------------------------
 
    Vector Time (GMT): 2014/342/11:11:28.187
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3022645.42                 A    =         6783819.04  meter
     Y    =       -2979578.74  meter          E    =           .0021982
     Z    =       -5311053.36                 I    =           51.37013
     XDOT =       5380.968045                 Wp   =           96.03678
     YDOT =      -5435.646581  meter/sec      RA   =          314.80182  deg
     ZDOT =        -15.276266                 TA   =          173.83030
                                              MA   =          173.80318
                                              Ha   =            227.134  n.mi
                                              Hp   =            215.414
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9916815.69                 X    =        -2963302.93
     Y    =       -9775520.81  feet           Y    =        -3013047.62  meter
     Z    =      -17424715.74                 Z    =        -5325593.15
     XDOT =      17654.094636                 XDOT =        5441.424993
     YDOT =     -17833.486159  feet/sec       YDOT =       -5375.135072  meter/sec
     ZDOT =        -50.118982                 ZDOT =          11.010163
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13073109.19                 X    =         3984683.68
     Y    =       -4566683.15  feet           Y    =        -1391925.02  meter
     Z    =      -17486108.21                 Z    =        -5329765.78
     XDOT =       8026.485299                 XDOT =        2446.472719
     YDOT =      22707.160855  feet/sec       YDOT =        6921.142629  meter/sec
     ZDOT =         63.032239                 ZDOT =          19.212226
  
  
    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   14342.48240145  .00016717  00000-0  10270-3 0  9100
    2 25544  51.6436 315.3481 0007390 108.9902 251.2050 15.51913753 38376
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14342.48240145   =   yrday.fracday
    Element set:     910
    Inclination:       51.6436  deg
    RA of node:       315.3481  deg
    Eccentricity:     .0007390     
    Arg of perigee:   108.9902  deg
    Mean anomaly:     251.2050  deg
    Mean motion:   15.51913753  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3837
    Checksum:              290
 
 
    Coasting Arc #12 (Orbit 3852)
    ---------------------------------------
 
    Vector Time (GMT): 2014/343/11:11:28.187
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2397702.76                 A    =         6784067.76  meter
     Y    =        3621773.22  meter          E    =           .0010005
     Z    =        5202504.24                 I    =           51.34985
     XDOT =      -5505.312775                 Wp   =           93.33254
     YDOT =       5229.625474  meter/sec      RA   =          309.80538  deg
     ZDOT =      -1102.129613                 TA   =            7.27318
                                              MA   =            7.25868
                                              Ha   =            226.910  n.mi
                                              Hp   =            215.534
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7866478.86                 X    =         2331752.92
     Y    =       11882458.09  feet           Y    =         3648216.69  meter
     Z    =       17068583.47                 Z    =         5213992.08
     XDOT =     -18062.049788                 XDOT =       -5558.028703
     YDOT =      17157.563891  feet/sec       YDOT =        5167.766840  meter/sec
     ZDOT =      -3615.910805                 ZDOT =       -1129.001267
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14043995.76                 X    =        -4280609.91
     Y    =        2047130.08  feet           Y    =          623965.25  meter
     Z    =       17116842.08                 Z    =         5217213.47
     XDOT =      -7840.623427                 XDOT =       -2389.822020
     YDOT =     -22554.100382  feet/sec       YDOT =       -6874.489796  meter/sec
     ZDOT =      -3731.510691                 ZDOT =       -1137.364458
  
  
    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   14343.51267704  .00016717  00000-0  10270-3 0  9116
    2 25544  51.6434 310.2287 0007296 112.5910 247.6014 15.51967116 38536
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14343.51267704   =   yrday.fracday
    Element set:     911
    Inclination:       51.6434  deg
    RA of node:       310.2287  deg
    Eccentricity:     .0007296     
    Arg of perigee:   112.5910  deg
    Mean anomaly:     247.6014  deg
    Mean motion:   15.51967116  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3853
    Checksum:              296
 
 
    Coasting Arc #13 (Orbit 3867)
    ---------------------------------------
 
    Vector Time (GMT): 2014/344/11:11:28.187
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1824829.25                 A    =         6785253.29  meter
     Y    =       -4299653.29  meter          E    =           .0019548
     Z    =       -4939909.47                 I    =           51.33470
     XDOT =       5500.139182                 Wp   =          109.50561
     YDOT =      -4845.891109  meter/sec      RA   =          304.80867  deg
     ZDOT =       2186.747041                 TA   =          181.96669
                                              MA   =          181.97439
                                              Ha   =            226.957  n.mi
                                              Hp   =            215.463
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5986972.61                 X    =        -1752617.43
     Y    =      -14106474.04  feet           Y    =        -4319655.59  meter
     Z    =      -16207052.05                 Z    =        -4948599.14
     XDOT =      18045.076058                 XDOT =        5543.295782
     YDOT =     -15898.592878  feet/sec       YDOT =       -4784.143844  meter/sec
     ZDOT =       7174.366932                 ZDOT =        2213.570384
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15282540.00                 X    =         4658118.19
     Y    =         325048.60  feet           Y    =           99074.81  meter
     Z    =      -16243254.03                 Z    =        -4950943.83
     XDOT =       7282.281729                 XDOT =        2219.639471
     YDOT =      21777.394432  feet/sec       YDOT =        6637.749823  meter/sec
     ZDOT =       7289.678525                 ZDOT =        2221.894014
  
  
    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   14344.47853753  .00016717  00000-0  10270-3 0  9128
    2 25544  51.6436 305.4295 0007323 115.7477 244.4431 15.51982191 38681
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14344.47853753   =   yrday.fracday
    Element set:     912
    Inclination:       51.6436  deg
    RA of node:       305.4295  deg
    Eccentricity:     .0007323     
    Arg of perigee:   115.7477  deg
    Mean anomaly:     244.4431  deg
    Mean motion:   15.51982191  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3868
    Checksum:              323
 
 
    Coasting Arc #14 (Orbit 3883)
    ---------------------------------------
 
    Vector Time (GMT): 2014/345/11:11:28.187
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1281106.18                 A    =         6786920.46  meter
     Y    =        4942497.86  meter          E    =           .0014774
     Z    =        4458377.33                 I    =           51.32372
     XDOT =      -5454.158993                 Wp   =           90.78206
     YDOT =       4329.265071  meter/sec      RA   =          299.81275  deg
     ZDOT =      -3223.049340                 TA   =           31.81249
                                              MA   =           31.72333
                                              Ha   =            226.735  n.mi
                                              Hp   =            215.530
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4203104.25                 X    =         1204085.47
     Y    =       16215544.16  feet           Y    =         4956393.11  meter
     Z    =       14627222.23                 Z    =         4464413.97
     XDOT =     -17894.222417                 XDOT =       -5486.507971
     YDOT =      14203.625562  feet/sec       YDOT =        4268.092444  meter/sec
     ZDOT =     -10574.308857                 ZDOT =       -3249.623146
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16539442.86                 X    =        -5041222.18
     Y    =       -2516235.43  feet           Y    =         -766948.56  meter
     Z    =       14651995.66                 Z    =         4465928.28
     XDOT =      -6339.782688                 XDOT =       -1932.365763
     YDOT =     -20739.750684  feet/sec       YDOT =       -6321.476008  meter/sec
     ZDOT =     -10688.448393                 ZDOT =       -3257.839070
  
  
    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   14345.50876373  .00016717  00000-0  10270-3 0  9137
    2 25544  51.6435 300.3100 0007225 119.5428 240.6445 15.52049335 38844
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14345.50876373   =   yrday.fracday
    Element set:     913
    Inclination:       51.6435  deg
    RA of node:       300.3100  deg
    Eccentricity:     .0007225     
    Arg of perigee:   119.5428  deg
    Mean anomaly:     240.6445  deg
    Mean motion:   15.52049335  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3884
    Checksum:              295
 
 
    Coasting Arc #15 (Orbit 3898)
    ---------------------------------------
 
    Vector Time (GMT): 2014/346/11:11:28.187
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -823193.63                 A    =         6789107.17  meter
     Y    =       -5547422.57  meter          E    =           .0013306
     Z    =       -3841367.78                 I    =           51.31643
     XDOT =       5320.847895                 Wp   =          114.12083
     YDOT =      -3640.494993  meter/sec      RA   =          294.81897  deg
     ZDOT =       4123.117122                 TA   =          199.49948
                                              MA   =          199.55042
                                              Ha   =            226.747  n.mi
                                              Hp   =            215.526
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2700766.51                 X    =         -742439.77
     Y    =      -18200205.30  feet           Y    =        -5556176.36  meter
     Z    =      -12602912.67                 Z    =        -3845170.85
     XDOT =      17456.850050                 XDOT =        5341.132553
     YDOT =     -11943.881211  feet/sec       YDOT =       -3580.880595  meter/sec
     ZDOT =      13527.287145                 ZDOT =        4149.014116
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17866401.63                 X    =         5445679.22
     Y    =        4353319.14  feet           Y    =         1326891.67  meter
     Z    =      -12618055.54                 Z    =        -3845983.33
     XDOT =       4923.242819                 XDOT =        1500.604411
     YDOT =      19268.162731  feet/sec       YDOT =        5872.936000  meter/sec
     ZDOT =      13638.400872                 ZDOT =        4156.984586
  
  
    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   14346.47457804  .00016717  00000-0  10270-3 0  9149
    2 25544  51.6436 295.5105 0007258 122.7424 237.4428 15.52060026 38994
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14346.47457804   =   yrday.fracday
    Element set:     914
    Inclination:       51.6436  deg
    RA of node:       295.5105  deg
    Eccentricity:     .0007258     
    Arg of perigee:   122.7424  deg
    Mean anomaly:     237.4428  deg
    Mean motion:   15.52060026  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3899
    Checksum:              317
 
             

Curator: Kim Dismukes | Responsible NASA Official: Amiko Kauderer | Updated: 06/08/2009
Privacy Policy and Important Notices