Return to Human Space Flight home page

    
   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  20451.43
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   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 
   ------------------------------------------------------------------------
   265/11:30:45.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              227.3  
   000/00:00:00.000           0.0               0.0              219.8  
   
 
 
    Coasting Arc #1 (Orbit 2564)
    ---------------------------------------
 
    Vector Time (GMT): 2014/260/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 912103.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3778235.16                 A    =         6792124.79  meter
     Y    =       -3569108.47  meter          E    =           .0010374
     Z    =       -4382765.64                 I    =           51.65345
     XDOT =       6359.023195                 Wp   =           76.47288
     YDOT =      -2537.043017  meter/sec      RA   =            1.52808  deg
     ZDOT =      -3420.313596                 TA   =          158.80957
                                              MA   =          158.76657
                                              Ha   =            227.558  n.mi
                                              Hp   =            219.877
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12395784.65                 X    =        -3716753.76
     Y    =      -11709673.45  feet           Y    =        -3611015.74  meter
     Z    =      -14379152.36                 Z    =        -4400970.08
     XDOT =      20862.936991                 XDOT =        6403.535112
     YDOT =      -8323.631944  feet/sec       YDOT =       -2465.683712  meter/sec
     ZDOT =     -11221.501300                 ZDOT =       -3389.314129
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11351460.22                 X    =         3459925.07
     Y    =       12637325.51  feet           Y    =         3851856.81  meter
     Z    =      -14455943.65                 Z    =        -4406171.63
     XDOT =     -20598.571719                 XDOT =       -6278.444660
     YDOT =       5834.291384  feet/sec       YDOT =        1778.292014  meter/sec
     ZDOT =     -11089.157982                 ZDOT =       -3379.975353
  
  
    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   14260.52228398  .00016717  00000-0  10270-3 0  9009
    2 25544  51.6472   1.9376 0001888 115.1223 245.0124 15.50361128 25651
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14260.52228398   =   yrday.fracday
    Element set:     900
    Inclination:       51.6472  deg
    RA of node:         1.9376  deg
    Eccentricity:     .0001888     
    Arg of perigee:   115.1223  deg
    Mean anomaly:     245.0124  deg
    Mean motion:   15.50361128  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2565
    Checksum:              284
 
 
    Coasting Arc #2 (Orbit 2580)
    ---------------------------------------
 
    Vector Time (GMT): 2014/261/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 912103.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3582014.28                 A    =         6790994.00  meter
     Y    =        3449852.74  meter          E    =           .0010180
     Z    =        4618504.49                 I    =           51.61939
     XDOT =      -6504.635838                 Wp   =          114.63674
     YDOT =       2753.509977  meter/sec      RA   =          356.56906  deg
     ZDOT =       2978.768409                 TA   =          305.60031
                                              MA   =          305.69512
                                              Ha   =            227.386  n.mi
                                              Hp   =            219.837
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11752015.36                 X    =         3520735.90
     Y    =       11318414.50  feet           Y    =         3489566.95  meter
     Z    =       15152573.79                 Z    =         4635756.16
     XDOT =     -21340.668759                 XDOT =       -6549.412617
     YDOT =       9033.825383  feet/sec       YDOT =        2680.520850  meter/sec
     ZDOT =       9772.862233                 ZDOT =        2947.060934
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10943616.91                 X    =        -3335614.43
     Y    =      -12010136.50  feet           Y    =        -3660689.60  meter
     Z    =       15225332.00                 Z    =         4640681.19
     XDOT =      21037.597420                 XDOT =        6412.259694
     YDOT =      -6913.360389  feet/sec       YDOT =       -2107.192247  meter/sec
     ZDOT =       9637.473541                 ZDOT =        2937.501935
  
  
    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   14261.55359874  .00016717  00000-0  10270-3 0  9018
    2 25544  51.6474 356.8252 0001907 115.3403 244.7945 15.50431723 25816
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14261.55359874   =   yrday.fracday
    Element set:     901
    Inclination:       51.6474  deg
    RA of node:       356.8252  deg
    Eccentricity:     .0001907     
    Arg of perigee:   115.3403  deg
    Mean anomaly:     244.7945  deg
    Mean motion:   15.50431723  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2581
    Checksum:              308
 
 
    Coasting Arc #3 (Orbit 2595)
    ---------------------------------------
 
    Vector Time (GMT): 2014/262/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 912103.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3343607.72                 A    =         6790148.84  meter
     Y    =       -3394461.15  meter          E    =           .0013122
     Z    =       -4849994.37                 I    =           51.58511
     XDOT =       6603.916558                 Wp   =           77.60662
     YDOT =      -2963.501705  meter/sec      RA   =          351.60774  deg
     ZDOT =      -2481.585212                 TA   =          167.95872
                                              MA   =          167.92732
                                              Ha   =            227.444  n.mi
                                              Hp   =            219.806
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10969841.61                 X    =        -3281841.97
     Y    =      -11136683.57  feet           Y    =        -3431506.71  meter
     Z    =      -15912055.01                 Z    =        -4866086.67
     XDOT =      21666.392906                 XDOT =        6648.618985
     YDOT =      -9722.774624  feet/sec       YDOT =       -2889.402758  meter/sec
     ZDOT =      -8141.683768                 ZDOT =       -2449.395584
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10370369.00                 X    =         3160888.47
     Y    =       11604102.53  feet           Y    =         3536930.45  meter
     Z    =      -15979890.23                 Z    =        -4870670.54
     XDOT =     -21276.672652                 XDOT =       -6485.129824
     YDOT =       8005.270013  feet/sec       YDOT =        2440.006300  meter/sec
     ZDOT =      -8004.213833                 ZDOT =       -2439.684376
  
  
    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   14262.52043972  .00016717  00000-0  10270-3 0  9026
    2 25544  51.6472 352.0332 0001819 116.9302 243.2034 15.50418238 25963
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14262.52043972   =   yrday.fracday
    Element set:     902
    Inclination:       51.6472  deg
    RA of node:       352.0332  deg
    Eccentricity:     .0001819     
    Arg of perigee:   116.9302  deg
    Mean anomaly:     243.2034  deg
    Mean motion:   15.50418238  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2596
    Checksum:              283
 
 
    Coasting Arc #4 (Orbit 2611)
    ---------------------------------------
 
    Vector Time (GMT): 2014/263/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 912103.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3093889.82                 A    =         6789198.09  meter
     Y    =        3360507.97  meter          E    =           .0007549
     Z    =        5018404.44                 I    =           51.55217
     XDOT =      -6682.413831                 Wp   =          121.94747
     YDOT =       3196.753772  meter/sec      RA   =          346.64259  deg
     ZDOT =       1973.009389                 TA   =          308.83331
                                              MA   =          308.90067
                                              Ha   =            227.255  n.mi
                                              Hp   =            219.789
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10150557.14                 X    =         3031704.20
     Y    =       11025288.60  feet           Y    =         3394758.75  meter
     Z    =       16464581.50                 Z    =         5033282.61
     XDOT =     -21923.929891                 XDOT =       -6727.248223
     YDOT =      10488.037310  feet/sec       YDOT =        3121.776251  meter/sec
     ZDOT =       6473.127918                 ZDOT =        1940.438022
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9748952.43                 X    =        -2971480.70
     Y    =      -11290745.51  feet           Y    =        -3441419.23  meter
     Z    =       16527257.34                 Z    =         5037508.04
     XDOT =      21412.882963                 XDOT =        6526.646727
     YDOT =      -9188.089163  feet/sec       YDOT =       -2800.529577  meter/sec
     ZDOT =       6334.001833                 ZDOT =        1930.603759
  
  
    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   14263.55171466  .00016717  00000-0  10270-3 0  9031
    2 25544  51.6475 346.9206 0001828 117.5801 242.5536 15.50489304 26129
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14263.55171466   =   yrday.fracday
    Element set:     903
    Inclination:       51.6475  deg
    RA of node:       346.9206  deg
    Eccentricity:     .0001828     
    Arg of perigee:   117.5801  deg
    Mean anomaly:     242.5536  deg
    Mean motion:   15.50489304  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2612
    Checksum:              304
 
 
    Coasting Arc #5 (Orbit 2626)
    ---------------------------------------
 
    Vector Time (GMT): 2014/264/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 912103.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2821629.47                 A    =         6788645.25  meter
     Y    =       -3395212.68  meter          E    =           .0015283
     Z    =       -5170745.27                 I    =           51.51922
     XDOT =       6700.897785                 Wp   =           83.15364
     YDOT =      -3408.602889  meter/sec      RA   =          341.67533  deg
     ZDOT =      -1420.304098                 TA   =          173.13910
                                              MA   =          173.11816
                                              Ha   =            227.338  n.mi
                                              Hp   =            219.739
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9257314.53                 X    =        -2758335.95
     Y    =      -11139149.20  feet           Y    =        -3426412.76  meter
     Z    =      -16964387.37                 Z    =        -5184298.12
     XDOT =      21984.572784                 XDOT =        6745.414908
     YDOT =     -11183.080345  feet/sec       YDOT =       -3333.420393  meter/sec
     ZDOT =      -4659.790348                 ZDOT =       -1387.643582
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9044312.23                 X    =         2756706.37
     Y    =       11226783.52  feet           Y    =         3421923.62  meter
     Z    =      -17021418.98                 Z    =        -5188128.51
     XDOT =     -21299.781709                 XDOT =       -6492.173465
     YDOT =      10314.890895  feet/sec       YDOT =        3143.978745  meter/sec
     ZDOT =      -4520.258451                 ZDOT =       -1377.774776
  
  
    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   14264.51851830  .00016717  00000-0  10270-3 0  9049
    2 25544  51.6467 342.1284 0001762 117.8558 242.2772 15.50474306 26274
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14264.51851830   =   yrday.fracday
    Element set:     904
    Inclination:       51.6467  deg
    RA of node:       342.1284  deg
    Eccentricity:     .0001762     
    Arg of perigee:   117.8558  deg
    Mean anomaly:     242.2772  deg
    Mean motion:   15.50474306  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2627
    Checksum:              307
 
 
    Coasting Arc #6 (Orbit 2641)
    ---------------------------------------
 
    Vector Time (GMT): 2014/265/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4434992.45                 A    =         6796626.33  meter
     Y    =       -4324605.20  meter          E    =           .0005864
     Z    =       -2799377.82                 I    =           51.51760
     XDOT =       5296.819619                 Wp   =           72.99799
     YDOT =       2138.073025  meter/sec      RA   =          336.77576  deg
     ZDOT =       5099.188583                 TA   =          255.26094
                                              MA   =          255.32593
                                              Ha   =            227.299  n.mi
                                              Hp   =            219.832
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14550500.17                 X    =         4496620.05
     Y    =      -14188337.28  feet           Y    =        -4274666.07  meter
     Z    =       -9184310.43                 Z    =        -2777682.94
     XDOT =      17378.017124                 XDOT =        5247.747293
     YDOT =       7014.675279  feet/sec       YDOT =        2197.031850  meter/sec
     ZDOT =      16729.621335                 ZDOT =        5124.800283
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16204688.30                 X    =        -4939188.99
     Y    =       12334282.62  feet           Y    =         3759489.34  meter
     Z    =       -9091263.81                 Z    =        -2771017.21
     XDOT =     -15406.487075                 XDOT =       -4695.897260
     YDOT =      -7855.738252  feet/sec       YDOT =       -2394.429019  meter/sec
     ZDOT =      16838.164828                 ZDOT =        5132.272640
  
  
    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   14265.48530272  .00016717  00000-0  10270-3 0  9051
    2 25544  51.6471 337.3353 0001740 117.4695 242.6633 15.50509431 26421
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14265.48530272   =   yrday.fracday
    Element set:     905
    Inclination:       51.6471  deg
    RA of node:       337.3353  deg
    Eccentricity:     .0001740     
    Arg of perigee:   117.4695  deg
    Mean anomaly:     242.6633  deg
    Mean motion:   15.50509431  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2642
    Checksum:              296
 
 
    Coasting Arc #7 (Orbit 2657)
    ---------------------------------------
 
    Vector Time (GMT): 2014/266/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4511268.32                 A    =         6797501.38  meter
     Y    =        4513006.62  meter          E    =           .0015633
     Z    =        2320885.41                 I    =           51.49225
     XDOT =      -4985.280598                 Wp   =          108.28128
     YDOT =      -2196.824423  meter/sec      RA   =          331.81035  deg
     ZDOT =      -5393.356221                 TA   =           45.81895
                                              MA   =           45.69059
                                              Ha   =            227.263  n.mi
                                              Hp   =            219.691
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14800749.09                 X    =        -4572672.67
     Y    =       14806452.16  feet           Y    =         4462215.72  meter
     Z    =        7614453.44                 Z    =         2298820.40
     XDOT =     -16355.907473                 XDOT =       -4934.145392
     YDOT =      -7207.429208  feet/sec       YDOT =       -2252.287962  meter/sec
     ZDOT =     -17694.738258                 ZDOT =       -5417.449556
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16292772.51                 X    =         4966037.06
     Y    =      -13201179.09  feet           Y    =        -4023719.39  meter
     Z    =        7519809.50                 Z    =         2292037.94
     XDOT =      14453.763835                 XDOT =        4405.507217
     YDOT =       7653.544654  feet/sec       YDOT =        2332.800411  meter/sec
     ZDOT =     -17796.808054                 ZDOT =       -5424.467095
  
  
    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   14266.51652013  .00016717  00000-0  10270-3 0  9065
    2 25544  51.6466 332.2226 0001841 116.4851 243.6488 15.50562100 26581
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14266.51652013   =   yrday.fracday
    Element set:     906
    Inclination:       51.6466  deg
    RA of node:       332.2226  deg
    Eccentricity:     .0001841     
    Arg of perigee:   116.4851  deg
    Mean anomaly:     243.6488  deg
    Mean motion:   15.50562100  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2658
    Checksum:              290
 
 
    Coasting Arc #8 (Orbit 2672)
    ---------------------------------------
 
    Vector Time (GMT): 2014/267/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4529319.68                 A    =         6798339.29  meter
     Y    =       -4718015.87  meter          E    =           .0007818
     Z    =       -1849149.70                 I    =           51.46736
     XDOT =       4673.014642                 Wp   =           50.58130
     YDOT =       2292.050053  meter/sec      RA   =          326.84335  deg
     ZDOT =       5618.853788                 TA   =          289.06572
                                              MA   =          289.15037
                                              Ha   =            227.217  n.mi
                                              Hp   =            219.751
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14859972.71                 X    =         4590723.64
     Y    =      -15479054.68  feet           Y    =        -4667023.03  meter
     Z    =       -6066764.11                 Z    =        -1826996.88
     XDOT =      15331.412868                 XDOT =        4619.742310
     YDOT =       7519.849255  feet/sec       YDOT =        2344.009723  meter/sec
     ZDOT =      18434.559671                 ZDOT =        5641.425049
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16170231.53                 X    =        -4928686.57
     Y    =       14145236.52  feet           Y    =         4311468.09  meter
     Z    =       -5971720.46                 Z    =        -1820180.40
     XDOT =     -13482.592092                 XDOT =       -4109.494070
     YDOT =      -7619.084960  feet/sec       YDOT =       -2322.297096  meter/sec
     ZDOT =      18530.134423                 ZDOT =        5647.984972
  
  
    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   14267.48326771  .00016717  00000-0  10270-3 0  9072
    2 25544  51.6460 327.4294 0001693 116.9516 243.1808 15.50552902 26731
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14267.48326771   =   yrday.fracday
    Element set:     907
    Inclination:       51.6460  deg
    RA of node:       327.4294  deg
    Eccentricity:     .0001693     
    Arg of perigee:   116.9516  deg
    Mean anomaly:     243.1808  deg
    Mean motion:   15.50552902  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2673
    Checksum:              317
 
 
    Coasting Arc #9 (Orbit 2688)
    ---------------------------------------
 
    Vector Time (GMT): 2014/268/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4533303.64                 A    =         6798833.94  meter
     Y    =        4884489.89  meter          E    =           .0015536
     Z    =        1309466.85                 I    =           51.44392
     XDOT =      -4350.947674                 Wp   =          120.01785
     YDOT =      -2469.377351  meter/sec      RA   =          321.87498  deg
     ZDOT =      -5807.470837                 TA   =           45.70799
                                              MA   =           45.58066
                                              Ha   =            227.117  n.mi
                                              Hp   =            219.597
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14873043.44                 X    =        -4593947.25
     Y    =       16025229.30  feet           Y    =         4833456.67  meter
     Z    =        4296151.08                 Z    =         1287296.45
     XDOT =     -14274.762710                 XDOT =       -4294.800017
     YDOT =      -8101.631730  feet/sec       YDOT =       -2517.719380  meter/sec
     ZDOT =     -19053.382012                 ZDOT =       -5828.470608
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15963885.04                 X    =         4865792.16
     Y    =      -14965900.51  feet           Y    =        -4561606.48  meter
     Z    =        4201012.46                 Z    =         1280468.60
     XDOT =      12474.005238                 XDOT =        3802.076796
     YDOT =       7890.895163  feet/sec       YDOT =        2405.144846  meter/sec
     ZDOT =     -19142.238333                 ZDOT =       -5834.554244
  
  
    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   14268.51444594  .00016717  00000-0  10270-3 0  9082
    2 25544  51.6458 322.3161 0001800 116.7487 243.3848 15.50628384 26891
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14268.51444594   =   yrday.fracday
    Element set:     908
    Inclination:       51.6458  deg
    RA of node:       322.3161  deg
    Eccentricity:     .0001800     
    Arg of perigee:   116.7487  deg
    Mean anomaly:     243.3848  deg
    Mean motion:   15.50628384  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2689
    Checksum:              327
 
 
    Coasting Arc #10 (Orbit 2703)
    ---------------------------------------
 
    Vector Time (GMT): 2014/269/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4477883.37                 A    =         6799359.17  meter
     Y    =       -5050149.48  meter          E    =           .0010931
     Z    =        -787747.92                 I    =           51.42074
     XDOT =       4052.905090                 Wp   =           48.34879
     YDOT =       2679.069013  meter/sec      RA   =          316.90491  deg
     ZDOT =       5923.680206                 TA   =          303.12334
                                              MA   =          303.22819
                                              Ha   =            227.151  n.mi
                                              Hp   =            219.638
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14691218.42                 X    =         4537849.18
     Y    =      -16568731.89  feet           Y    =        -4999739.71  meter
     Z    =       -2584474.81                 Z    =         -765848.36
     XDOT =      13296.932710                 XDOT =        3993.870168
     YDOT =       8789.596499  feet/sec       YDOT =        2724.061944  meter/sec
     ZDOT =      19434.646346                 ZDOT =        5943.225154
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15539678.37                 X    =        -4736493.97
     Y    =       15790828.28  feet           Y    =         4813044.46  meter
     Z    =       -2490466.50                 Z    =         -759094.19
     XDOT =     -11553.310072                 XDOT =       -3521.448910
     YDOT =      -8323.836883  feet/sec       YDOT =       -2537.105482  meter/sec
     ZDOT =      19517.276310                 ZDOT =        5948.865819
  
  
    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   14269.48115718  .00016717  00000-0  10270-3 0  9093
    2 25544  51.6451 317.5223 0001720 115.3579 244.7750 15.50599680 27048
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14269.48115718   =   yrday.fracday
    Element set:     909
    Inclination:       51.6451  deg
    RA of node:       317.5223  deg
    Eccentricity:     .0001720     
    Arg of perigee:   115.3579  deg
    Mean anomaly:     244.7750  deg
    Mean motion:   15.50599680  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2704
    Checksum:              315
 
 
    Coasting Arc #11 (Orbit 2719)
    ---------------------------------------
 
    Vector Time (GMT): 2014/270/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4413970.55                 A    =         6799340.33  meter
     Y    =        5159118.64  meter          E    =           .0014195
     Z    =         205450.12                 I    =           51.39972
     XDOT =      -3757.743178                 Wp   =          130.54966
     YDOT =      -2966.163890  meter/sec      RA   =          311.93336  deg
     ZDOT =      -5984.806818                 TA   =           47.23239
                                              MA   =           47.11306
                                              Ha   =            227.011  n.mi
                                              Hp   =            219.488
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14481530.68                 X    =        -4472330.98
     Y    =       16926242.25  feet           Y    =         5109432.47  meter
     Z    =         674048.94                 Z    =          183864.96
     XDOT =     -12328.553733                 XDOT =       -3695.222841
     YDOT =      -9731.508824  feet/sec       YDOT =       -3007.836559  meter/sec
     ZDOT =     -19635.192974                 ZDOT =       -6002.909465
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15056399.98                 X    =         4589190.71
     Y    =      -16420523.26  feet           Y    =        -5004975.49  meter
     Z    =         581364.70                 Z    =          177199.96
     XDOT =      10666.885505                 XDOT =        3251.266702
     YDOT =       9047.328727  feet/sec       YDOT =        2757.625796  meter/sec
     ZDOT =     -19711.638095                 ZDOT =       -6008.107292
  
  
    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   14270.51229619  .00016717  00000-0  10270-3 0  9107
    2 25544  51.6455 312.4082 0001838 118.0822 242.0515 15.50686696 27202
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14270.51229619   =   yrday.fracday
    Element set:     910
    Inclination:       51.6455  deg
    RA of node:       312.4082  deg
    Eccentricity:     .0001838     
    Arg of perigee:   118.0822  deg
    Mean anomaly:     242.0515  deg
    Mean motion:   15.50686696  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2720
    Checksum:              293
 
 
    Coasting Arc #12 (Orbit 2735)
    ---------------------------------------
 
    Vector Time (GMT): 2014/271/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4296928.22                 A    =         6799378.07  meter
     Y    =       -5250831.55  meter          E    =           .0013579
     Z    =         345917.13                 I    =           51.37878
     XDOT =       3508.262573                 Wp   =           55.91811
     YDOT =       3275.100728  meter/sec      RA   =          306.96026  deg
     ZDOT =       5973.838630                 TA   =          307.81855
                                              MA   =          307.94139
                                              Ha   =            227.082  n.mi
                                              Hp   =            219.494
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14097533.52                 X    =         4353644.49
     Y    =      -17227137.62  feet           Y    =        -5202463.36  meter
     Z    =        1134898.73                 Z    =          366929.64
     XDOT =      11510.047813                 XDOT =        3442.359444
     YDOT =      10745.081129  feet/sec       YDOT =        3313.964530  meter/sec
     ZDOT =      19599.208105                 ZDOT =        5990.721125
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14381512.44                 X    =        -4383484.99
     Y    =       16984516.53  feet           Y    =         5176880.64  meter
     Z    =        1225159.20                 Z    =          373428.52
     XDOT =      -9963.101862                 XDOT =       -3036.753448
     YDOT =      -9890.446309  feet/sec       YDOT =       -3014.608035  meter/sec
     ZDOT =      19670.411232                 ZDOT =        5995.541343
  
  
    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   14271.54341685  .00016717  00000-0  10270-3 0  9110
    2 25544  51.6448 307.2944 0001823 115.4434 244.6905 15.50658262 27363
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14271.54341685   =   yrday.fracday
    Element set:     911
    Inclination:       51.6448  deg
    RA of node:       307.2944  deg
    Eccentricity:     .0001823     
    Arg of perigee:   115.4434  deg
    Mean anomaly:     244.6905  deg
    Mean motion:   15.50658262  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2736
    Checksum:              307
 
 
    Coasting Arc #13 (Orbit 2750)
    ---------------------------------------
 
    Vector Time (GMT): 2014/272/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4182671.29                 A    =         6798800.30  meter
     Y    =        5269569.97  meter          E    =           .0011613
     Z    =        -946130.02                 I    =           51.36044
     XDOT =      -3273.817247                 Wp   =          137.77232
     YDOT =      -3647.000370  meter/sec      RA   =          301.98546  deg
     ZDOT =      -5890.046985                 TA   =           52.49781
                                              MA   =           52.39229
                                              Ha   =            226.923  n.mi
                                              Hp   =            219.386
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13722674.85                 X    =        -4236689.91
     Y    =       17288615.37  feet           Y    =         5222494.51  meter
     Z    =       -3104101.11                 Z    =         -966580.82
     XDOT =     -10740.870234                 XDOT =       -3204.179948
     YDOT =     -11965.224311  feet/sec       YDOT =       -3683.221476  meter/sec
     ZDOT =     -19324.301132                 ZDOT =       -5905.781487
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13699960.67                 X    =         4175748.01
     Y    =      -17290629.28  feet           Y    =        -5270183.81  meter
     Z    =       -3191972.27                 Z    =         -972913.15
     XDOT =       9360.059256                 XDOT =        2852.946061
     YDOT =      10966.094876  feet/sec       YDOT =        3342.465718  meter/sec
     ZDOT =     -19390.560380                 ZDOT =       -5910.242804
  
  
    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   14272.51007014  .00016717  00000-0  10270-3 0  9124
    2 25544  51.6456 302.4997 0001904 121.6947 238.4390 15.50738180 27519
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14272.51007014   =   yrday.fracday
    Element set:     912
    Inclination:       51.6456  deg
    RA of node:       302.4997  deg
    Eccentricity:     .0001904     
    Arg of perigee:   121.6947  deg
    Mean anomaly:     238.4390  deg
    Mean motion:   15.50738180  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2751
    Checksum:              297
 
 
    Coasting Arc #14 (Orbit 2766)
    ---------------------------------------
 
    Vector Time (GMT): 2014/273/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4028362.03                 A    =         6798247.16  meter
     Y    =       -5258106.83  meter          E    =           .0015017
     Z    =        1501495.31                 I    =           51.34201
     XDOT =       3100.290519                 Wp   =           68.05611
     YDOT =       4025.430395  meter/sec      RA   =          297.00922  deg
     ZDOT =       5738.169402                 TA   =          308.38935
                                              MA   =          308.52414
                                              Ha   =            226.972  n.mi
                                              Hp   =            219.358
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13216410.87                 X    =         4079566.13
     Y    =      -17251006.68  feet           Y    =        -5212772.67  meter
     Z    =        4926165.73                 Z    =         1521189.55
     XDOT =      10171.556820                 XDOT =        3027.172281
     YDOT =      13206.792636  feet/sec       YDOT =        4059.691474  meter/sec
     ZDOT =      18826.015100                 ZDOT =        5753.052440
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12883511.52                 X    =        -3926894.31
     Y    =       17476977.20  feet           Y    =         5326982.65  meter
     Z    =        5010813.83                 Z    =         1527296.05
     XDOT =      -9006.195146                 XDOT =       -2745.088281
     YDOT =     -12092.340760  feet/sec       YDOT =       -3685.745464  meter/sec
     ZDOT =      18888.592679                 ZDOT =        5757.243049
  
  
    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   14273.54115052  .00016717  00000-0  10270-3 0  9131
    2 25544  51.6449 297.3859 0001925 118.7520 241.3824 15.50729346 27673
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14273.54115052   =   yrday.fracday
    Element set:     913
    Inclination:       51.6449  deg
    RA of node:       297.3859  deg
    Eccentricity:     .0001925     
    Arg of perigee:   118.7520  deg
    Mean anomaly:     241.3824  deg
    Mean motion:   15.50729346  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2767
    Checksum:              318
 
 
    Coasting Arc #15 (Orbit 2781)
    ---------------------------------------
 
    Vector Time (GMT): 2014/274/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3893059.15                 A    =         6797158.96  meter
     Y    =        5162438.17  meter          E    =           .0008291
     Z    =       -2089365.51                 I    =           51.32635
     XDOT =      -2950.265810                 Wp   =          135.59547
     YDOT =      -4442.654613  meter/sec      RA   =          292.03099  deg
     ZDOT =      -5498.920821                 TA   =           67.59877
                                              MA   =           67.51096
                                              Ha   =            226.820  n.mi
                                              Hp   =            219.306
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12772503.77                 X    =        -3940347.83
     Y    =       16937133.11  feet           Y    =         5118638.90  meter
     Z    =       -6854873.71                 Z    =        -2108392.85
     XDOT =      -9679.349769                 XDOT =       -2873.655524
     YDOT =     -14575.638493  feet/sec       YDOT =       -4475.218457  meter/sec
     ZDOT =     -18041.078808                 ZDOT =       -5513.066501
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12136053.28                 X    =         3699069.04
     Y    =      -17366390.46  feet           Y    =        -5293275.81  meter
     Z    =       -6936664.70                 Z    =        -2114295.40
     XDOT =       8797.247308                 XDOT =        2681.400979
     YDOT =      13352.880533  feet/sec       YDOT =        4069.957986  meter/sec
     ZDOT =     -18100.455971                 ZDOT =       -5517.018980
  
  
    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   14274.50776646  .00016717  00000-0  10270-3 0  9141
    2 25544  51.6456 292.5912 0001929 126.8054 233.3274 15.50790284 27820
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14274.50776646   =   yrday.fracday
    Element set:     914
    Inclination:       51.6456  deg
    RA of node:       292.5912  deg
    Eccentricity:     .0001929     
    Arg of perigee:   126.8054  deg
    Mean anomaly:     233.3274  deg
    Mean motion:   15.50790284  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2782
    Checksum:              325
 
 
    Coasting Arc #16 (Orbit 2796)
    ---------------------------------------
 
    Vector Time (GMT): 2014/275/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3735758.85                 A    =         6796057.55  meter
     Y    =       -5029098.80  meter          E    =           .0014938
     Z    =        2618379.29                 I    =           51.31091
     XDOT =       2867.349664                 Wp   =           82.80216
     YDOT =       4848.864041  meter/sec      RA   =          287.05105  deg
     ZDOT =       5198.442648                 TA   =          306.80449
                                              MA   =          306.94146
                                              Ha   =            226.803  n.mi
                                              Hp   =            219.271
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12256426.68                 X    =         3778998.43
     Y    =      -16499667.97  feet           Y    =        -4987081.14  meter
     Z    =        8590483.23                 Z    =         2636632.61
     XDOT =       9407.315171                 XDOT =        2787.662935
     YDOT =      15908.346591  feet/sec       YDOT =        4880.483472  meter/sec
     ZDOT =      17055.258033                 ZDOT =        5212.177951
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11331880.55                 X    =        -3453957.19
     Y    =       17108277.54  feet           Y    =         5214602.99  meter
     Z    =        8668953.99                 Z    =         2642297.17
     XDOT =      -8862.986861                 XDOT =       -2701.438395
     YDOT =     -14580.901121  feet/sec       YDOT =       -4444.258662  meter/sec
     ZDOT =      17112.829882                 ZDOT =        5215.990548
  
  
    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   14275.53880541  .00016717  00000-0  10270-3 0  9156
    2 25544  51.6445 287.4771 0001942 125.0927 235.0406 15.50806716 27979
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14275.53880541   =   yrday.fracday
    Element set:     915
    Inclination:       51.6445  deg
    RA of node:       287.4771  deg
    Eccentricity:     .0001942     
    Arg of perigee:   125.0927  deg
    Mean anomaly:     235.0406  deg
    Mean motion:   15.50806716  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2797
    Checksum:              319
 
             

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