Return to Human Space Flight home page

    
   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  9687.52
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   128.2
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.453
   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 1803)
    ---------------------------------------
 
    Vector Time (GMT): 2014/211/10:50:54.029
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3710299.68                 A    =         6788086.41  meter
     Y    =        2079311.46  meter          E    =           .0010741
     Z    =       -5298891.54                 I    =           51.29837
     XDOT =      -3491.211188                 Wp   =           63.18634
     YDOT =      -6809.389175  meter/sec      RA   =          244.19391  deg
     ZDOT =       -223.080051                 TA   =          204.64809
                                              MA   =          204.69946
                                              Ha   =            226.266  n.mi
                                              Hp   =            222.093
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12172899.22                 X    =        -3707535.38
     Y    =        6821887.99  feet           Y    =         2037835.98  meter
     Z    =      -17384814.76                 Z    =        -5316908.63
     XDOT =     -11454.104946                 XDOT =       -3413.723930
     YDOT =     -22340.515667  feet/sec       YDOT =       -6847.996892  meter/sec
     ZDOT =       -731.889931                 ZDOT =        -239.851416
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10518833.07                 X    =         3206140.32
     Y    =        9021938.59  feet           Y    =         2749886.88  meter
     Z    =      -17461620.50                 Z    =        -5322301.93
     XDOT =     -16452.380187                 XDOT =       -5014.685481
     YDOT =      17602.122586  feet/sec       YDOT =        5365.126964  meter/sec
     ZDOT =       -801.959500                 ZDOT =        -244.437256
  
  
    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   14211.46855137  .00016717  00000-0  10270-3 0  9005
    2 25544  51.6451 245.0583 0006830 309.9810  50.0740 15.50456387 18041
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14211.46855137   =   yrday.fracday
    Element set:     900
    Inclination:       51.6451  deg
    RA of node:       245.0583  deg
    Eccentricity:     .0006830     
    Arg of perigee:   309.9810  deg
    Mean anomaly:      50.0740  deg
    Mean motion:   15.50456387  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1804
    Checksum:              290
 
 
    Coasting Arc #2 (Orbit 1819)
    ---------------------------------------
 
    Vector Time (GMT): 2014/212/10:50:54.029
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3845960.27                 A    =         6787969.57  meter
     Y    =       -1822103.81  meter          E    =           .0005923
     Z    =        5290535.79                 I    =           51.31275
     XDOT =       3672.575427                 Wp   =          336.46300
     YDOT =       6714.036134  meter/sec      RA   =          239.20919  deg
     ZDOT =       -352.220501                 TA   =          116.94397
                                              MA   =          116.88345
                                              Ha   =            226.329  n.mi
                                              Hp   =            221.972
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12617979.90                 X    =         3840350.24
     Y    =       -5978030.86  feet           Y    =        -1779127.16  meter
     Z    =       17357400.87                 Z    =         5309205.04
     XDOT =      12049.131977                 XDOT =        3598.935533
     YDOT =      22027.677606  feet/sec       YDOT =        6754.693496  meter/sec
     ZDOT =      -1155.579072                 ZDOT =        -334.558767
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10042758.99                 X    =        -3061032.94
     Y    =       -9556462.92  feet           Y    =        -2912809.90  meter
     Z    =       17436933.30                 Z    =         5314777.27
     XDOT =      15586.122809                 XDOT =        4750.650232
     YDOT =     -18383.884846  feet/sec       YDOT =       -5603.408101  meter/sec
     ZDOT =      -1081.699356                 ZDOT =        -329.701964
  
  
    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   14212.49980598  .00016717  00000-0  10270-3 0  9010
    2 25544  51.6450 239.9455 0006809 314.4989  45.5605 15.50500473 18207
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14212.49980598   =   yrday.fracday
    Element set:     901
    Inclination:       51.6450  deg
    RA of node:       239.9455  deg
    Eccentricity:     .0006809     
    Arg of perigee:   314.4989  deg
    Mean anomaly:      45.5605  deg
    Mean motion:   15.50500473  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1820
    Checksum:              321
 
 
    Coasting Arc #3 (Orbit 1834)
    ---------------------------------------
 
    Vector Time (GMT): 2014/213/10:50:54.029
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4010671.29                 A    =         6788257.58  meter
     Y    =        1610623.33  meter          E    =           .0010384
     Z    =       -5242668.73                 I    =           51.33100
     XDOT =      -3828.029645                 Wp   =           71.05468
     YDOT =      -6566.471698  meter/sec      RA   =          234.22523  deg
     ZDOT =        915.948539                 TA   =          207.73206
                                              MA   =          207.78747
                                              Ha   =            226.579  n.mi
                                              Hp   =            221.666
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13158370.36                 X    =        -4002916.63
     Y    =        5284197.28  feet           Y    =         1565816.75  meter
     Z    =      -17200356.73                 Z    =        -5262132.98
     XDOT =     -12559.152377                 XDOT =       -3758.766682
     YDOT =     -21543.542315  feet/sec       YDOT =       -6608.891918  meter/sec
     ZDOT =       3005.080509                 ZDOT =         897.520965
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9763414.34                 X    =         2975888.69
     Y    =       10143144.25  feet           Y    =         3091630.37  meter
     Z    =      -17283231.41                 Z    =        -5267928.94
     XDOT =     -14568.359589                 XDOT =       -4440.436003
     YDOT =      18985.228504  feet/sec       YDOT =        5786.697648  meter/sec
     ZDOT =       2927.912337                 ZDOT =         892.427680
  
  
    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   14213.46660189  .00016717  00000-0  10270-3 0  9020
    2 25544  51.6457 235.1519 0006852 318.6831  41.3801 15.50480093 18356
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14213.46660189   =   yrday.fracday
    Element set:     902
    Inclination:       51.6457  deg
    RA of node:       235.1519  deg
    Eccentricity:     .0006852     
    Arg of perigee:   318.6831  deg
    Mean anomaly:      41.3801  deg
    Mean motion:   15.50480093  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1835
    Checksum:              300
 
 
    Coasting Arc #4 (Orbit 1850)
    ---------------------------------------
 
    Vector Time (GMT): 2014/214/10:50:54.029
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4218006.86                 A    =         6788576.85  meter
     Y    =       -1395707.17  meter          E    =           .0008112
     Z    =        5134781.53                 I    =           51.35078
     XDOT =       3941.009664                 Wp   =          358.28527
     YDOT =       6398.218317  meter/sec      RA   =          229.24304  deg
     ZDOT =      -1490.351617                 TA   =          106.18334
                                              MA   =          106.09404
                                              Ha   =            226.651  n.mi
                                              Hp   =            221.510
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13838605.20                 X    =         4208357.56
     Y    =       -4579091.77  feet           Y    =        -1348592.65  meter
     Z    =       16846396.10                 Z    =         5155248.42
     XDOT =      12929.821732                 XDOT =        3876.410010
     YDOT =      20991.529913  feet/sec       YDOT =        6441.928031  meter/sec
     ZDOT =      -4889.605044                 ZDOT =       -1471.363800
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9551777.55                 X    =        -2911381.80
     Y    =      -10876414.39  feet           Y    =        -3315131.11  meter
     Z    =       16933496.17                 Z    =         5161329.63
     XDOT =      13516.413095                 XDOT =        4119.802711
     YDOT =     -19399.090211  feet/sec       YDOT =       -5912.842696  meter/sec
     ZDOT =      -4810.019082                 ZDOT =       -1466.093816
  
  
    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   14214.49784188  .00016717  00000-0  10270-3 0  9031
    2 25544  51.6450 230.0391 0006809 323.3786  36.6898 15.50525462 18516
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14214.49784188   =   yrday.fracday
    Element set:     903
    Inclination:       51.6450  deg
    RA of node:       230.0391  deg
    Eccentricity:     .0006809     
    Arg of perigee:   323.3786  deg
    Mean anomaly:      36.6898  deg
    Mean motion:   15.50525462  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1851
    Checksum:              321
 
 
    Coasting Arc #5 (Orbit 1865)
    ---------------------------------------
 
    Vector Time (GMT): 2014/215/10:50:54.029
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4439035.70                 A    =         6789262.26  meter
     Y    =        1242417.15  meter          E    =           .0008918
     Z    =       -4991196.28                 I    =           51.37507
     XDOT =      -4018.438899                 Wp   =           73.99405
     YDOT =      -6190.545582  meter/sec      RA   =          224.26272  deg
     ZDOT =       2038.384402                 TA   =          215.89934
                                              MA   =          215.95929
                                              Ha   =            226.861  n.mi
                                              Hp   =            221.252
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14563765.43                 X    =        -4428353.29
     Y    =        4076171.74  feet           Y    =         1192836.76  meter
     Z    =      -16375315.88                 Z    =        -5012734.41
     XDOT =     -13183.854656                 XDOT =       -3958.817900
     YDOT =     -20310.188918  feet/sec       YDOT =       -6235.149017  meter/sec
     ZDOT =       6687.612866                 ZDOT =        2019.008256
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9571768.51                 X    =         2917475.04
     Y    =       11579740.34  feet           Y    =         3529504.86  meter
     Z    =      -16466944.79                 Z    =        -5019124.77
     XDOT =     -12386.741256                 XDOT =       -3775.478735
     YDOT =      19608.049507  feet/sec       YDOT =        5976.533490  meter/sec
     ZDOT =       6606.333358                 ZDOT =        2013.610407
  
  
    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   14215.46462356  .00016717  00000-0  10270-3 0  9040
    2 25544  51.6462 225.2458 0006902 327.0006  33.0713 15.50504012 18660
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14215.46462356   =   yrday.fracday
    Element set:     904
    Inclination:       51.6462  deg
    RA of node:       225.2458  deg
    Eccentricity:     .0006902     
    Arg of perigee:   327.0006  deg
    Mean anomaly:      33.0713  deg
    Mean motion:   15.50504012  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1866
    Checksum:              274
 
 
    Coasting Arc #6 (Orbit 1881)
    ---------------------------------------
 
    Vector Time (GMT): 2014/216/10:50:54.029
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4695511.45                 A    =         6789971.98  meter
     Y    =       -1091858.25  meter          E    =           .0010092
     Z    =        4782833.23                 I    =           51.39950
     XDOT =       4037.612613                 Wp   =           18.36833
     YDOT =       5973.469690  meter/sec      RA   =          219.28410  deg
     ZDOT =      -2589.341728                 TA   =           97.31449
                                              MA   =           97.19977
                                              Ha   =            226.943  n.mi
                                              Hp   =            221.070
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15405221.28                 X    =         4684138.53
     Y    =       -3582212.10  feet           Y    =        -1039413.71  meter
     Z    =       15691710.06                 Z    =         4805615.59
     XDOT =      13246.760542                 XDOT =        3983.093945
     YDOT =      19597.997672  feet/sec       YDOT =        6018.316107  meter/sec
     ZDOT =      -8495.215642                 ZDOT =       -2569.859957
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9676367.60                 X    =        -2949356.84
     Y    =      -12388329.09  feet           Y    =        -3775962.71  meter
     Z    =       15788605.49                 Z    =         4812366.95
     XDOT =      11298.823307                 XDOT =        3443.881344
     YDOT =     -19593.336890  feet/sec       YDOT =       -5972.049084  meter/sec
     ZDOT =      -8413.441297                 ZDOT =       -2564.416907
  
  
    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   14216.49584854  .00016717  00000-0  10270-3 0  9053
    2 25544  51.6448 220.1326 0006873 331.6215  28.4560 15.50551708 18822
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14216.49584854   =   yrday.fracday
    Element set:     905
    Inclination:       51.6448  deg
    RA of node:       220.1326  deg
    Eccentricity:     .0006873     
    Arg of perigee:   331.6215  deg
    Mean anomaly:      28.4560  deg
    Mean motion:   15.50551708  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1882
    Checksum:              309
 
 
    Coasting Arc #7 (Orbit 1896)
    ---------------------------------------
 
    Vector Time (GMT): 2014/217/10:50:54.029
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4946537.80                 A    =         6790980.29  meter
     Y    =        1012983.98  meter          E    =           .0007020
     Z    =       -4545341.38                 I    =           51.42808
     XDOT =      -4017.666483                 Wp   =           66.12763
     YDOT =      -5735.181946  meter/sec      RA   =          214.30856  deg
     ZDOT =       3100.720263                 TA   =          235.02916
                                              MA   =          235.09509
                                              Ha   =            227.120  n.mi
                                              Hp   =            220.858
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16228798.55                 X    =        -4935417.91
     Y    =        3323438.27  feet           Y    =          957730.96  meter
     Z    =      -14912537.32                 Z    =        -4569343.76
     XDOT =     -13181.320483                 XDOT =       -3968.297967
     YDOT =     -18816.213732  feet/sec       YDOT =       -5779.834165  meter/sec
     ZDOT =      10172.966741                 ZDOT =        3081.322822
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10015851.09                 X    =         3052831.41
     Y    =       13078497.82  feet           Y    =         3986326.14  meter
     Z    =      -15014610.73                 Z    =        -4576453.35
     XDOT =     -10217.497033                 XDOT =       -3114.293096
     YDOT =      19385.605439  feet/sec       YDOT =        5908.732538  meter/sec
     ZDOT =      10091.500119                 ZDOT =        3075.889236
  
  
    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   14217.46261565  .00016717  00000-0  10270-3 0  9063
    2 25544  51.6455 215.3397 0006976 334.9611  25.1201 15.50527237 18976
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14217.46261565   =   yrday.fracday
    Element set:     906
    Inclination:       51.6455  deg
    RA of node:       215.3397  deg
    Eccentricity:     .0006976     
    Arg of perigee:   334.9611  deg
    Mean anomaly:      25.1201  deg
    Mean motion:   15.50527237  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1897
    Checksum:              313
 
 
    Coasting Arc #8 (Orbit 1912)
    ---------------------------------------
 
    Vector Time (GMT): 2014/218/10:50:54.029
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5222363.56                 A    =         6791968.23  meter
     Y    =        -939635.00  meter          E    =           .0011700
     Z    =        4239637.23                 I    =           51.45653
     XDOT =       3927.853279                 Wp   =           37.15117
     YDOT =       5501.440609  meter/sec      RA   =          209.33437  deg
     ZDOT =      -3604.660549                 TA   =           89.90062
                                              MA   =           89.76655
                                              Ha   =            227.212  n.mi
                                              Hp   =            220.659
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17133738.72                 X    =         5211888.03
     Y    =       -3082791.98  feet           Y    =         -881293.94  meter
     Z    =       13909570.97                 Z    =         4264981.01
     XDOT =      12886.657739                 XDOT =        3883.553102
     YDOT =      18049.345829  feet/sec       YDOT =        5545.116878  meter/sec
     ZDOT =     -11826.314136                 ZDOT =       -3585.687094
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10435416.98                 X    =        -3180715.10
     Y    =      -13826097.70  feet           Y    =        -4214194.58  meter
     Z    =       14017341.69                 Z    =         4272485.75
     XDOT =       9258.812211                 XDOT =        2822.085962
     YDOT =     -18944.674801  feet/sec       YDOT =       -5774.336879  meter/sec
     ZDOT =     -11746.597180                 ZDOT =       -3580.362820
  
  
    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   14218.49382498  .00016717  00000-0  10270-3 0  9077
    2 25544  51.6439 210.2260 0006995 339.1242  20.9622 15.50577965 19131
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14218.49382498   =   yrday.fracday
    Element set:     907
    Inclination:       51.6439  deg
    RA of node:       210.2260  deg
    Eccentricity:     .0006995     
    Arg of perigee:   339.1242  deg
    Mean anomaly:      20.9622  deg
    Mean motion:   15.50577965  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1913
    Checksum:              322
 
 
    Coasting Arc #9 (Orbit 1927)
    ---------------------------------------
 
    Vector Time (GMT): 2014/219/10:50:54.029
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5471980.11                 A    =         6793164.99  meter
     Y    =         941002.57  meter          E    =           .0006465
     Z    =       -3913871.89                 I    =           51.48800
     XDOT =      -3802.574994                 Wp   =           41.99880
     YDOT =      -5267.480230  meter/sec      RA   =          204.36407  deg
     ZDOT =       4058.523851                 TA   =          270.58249
                                              MA   =          270.65658
                                              Ha   =            227.363  n.mi
                                              Hp   =            220.476
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17952690.65                 X    =        -5463083.85
     Y    =        3087278.77  feet           Y    =          879861.31  meter
     Z    =      -12840787.04                 Z    =        -3940431.99
     XDOT =     -12475.639745                 XDOT =       -3763.104949
     YDOT =     -17281.759284  feet/sec       YDOT =       -5309.782599  meter/sec
     ZDOT =      13315.366965                 ZDOT =        4040.147311
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11060602.47                 X    =         3371271.63
     Y    =       14372889.16  feet           Y    =         4380856.62  meter
     Z    =      -12953738.21                 Z    =        -3948299.41
     XDOT =      -8386.449895                 XDOT =       -2556.189928
     YDOT =      18359.593340  feet/sec       YDOT =        5596.004050  meter/sec
     ZDOT =      13238.133102                 ZDOT =        4034.982969
  
  
    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   14219.46057717  .00016717  00000-0  10270-3 0  9089
    2 25544  51.6440 205.4329 0007059 342.7633  17.3277 15.50551109 19285
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14219.46057717   =   yrday.fracday
    Element set:     908
    Inclination:       51.6440  deg
    RA of node:       205.4329  deg
    Eccentricity:     .0007059     
    Arg of perigee:   342.7633  deg
    Mean anomaly:      17.3277  deg
    Mean motion:   15.50551109  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1928
    Checksum:              308
 
 
    Coasting Arc #10 (Orbit 1943)
    ---------------------------------------
 
    Vector Time (GMT): 2014/220/10:50:54.029
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5733703.21                 A    =         6794267.43  meter
     Y    =        -946255.04  meter          E    =           .0012763
     Z    =        3518319.99                 I    =           51.51986
     XDOT =       3601.718119                 Wp   =           54.71474
     YDOT =       5053.208663  meter/sec      RA   =          199.39511  deg
     ZDOT =      -4491.782109                 TA   =           83.86405
                                              MA   =           83.71864
                                              Ha   =            227.466  n.mi
                                              Hp   =            220.268
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18811362.25                 X    =         5726767.75
     Y    =       -3104511.27  feet           Y    =         -882176.01  meter
     Z    =       11543044.60                 Z    =         3546156.13
     XDOT =      11816.660497                 XDOT =        3566.763537
     YDOT =      16578.768579  feet/sec       YDOT =        5093.290156  meter/sec
     ZDOT =     -14736.817942                 ZDOT =       -4474.370455
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11738571.78                 X    =        -3577916.68
     Y    =      -14931984.01  feet           Y    =        -4551268.73  meter
     Z    =       11661432.35                 Z    =         3554404.58
     XDOT =       7711.100231                 XDOT =        2350.343351
     YDOT =     -17561.432335  feet/sec       YDOT =       -5352.724576  meter/sec
     ZDOT =     -14663.632861                 ZDOT =       -4469.475296
  
  
    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   14220.49177024  .00016717  00000-0  10270-3 0  9099
    2 25544  51.6429 200.3186 0007145 346.2035  13.8919 15.50603457 19444
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14220.49177024   =   yrday.fracday
    Element set:     909
    Inclination:       51.6429  deg
    RA of node:       200.3186  deg
    Eccentricity:     .0007145     
    Arg of perigee:   346.2035  deg
    Mean anomaly:      13.8919  deg
    Mean motion:   15.50603457  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1944
    Checksum:              297
 
 
    Coasting Arc #11 (Orbit 1958)
    ---------------------------------------
 
    Vector Time (GMT): 2014/221/10:50:54.029
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5949376.64                 A    =         6795469.52  meter
     Y    =        1021860.61  meter          E    =           .0008677
     Z    =       -3113964.26                 I    =           51.55336
     XDOT =      -3376.185296                 Wp   =           22.30301
     YDOT =      -4859.467588  meter/sec      RA   =          194.43038  deg
     ZDOT =       4868.018178                 TA   =          301.86813
                                              MA   =          301.95255
                                              Ha   =            227.588  n.mi
                                              Hp   =            220.100
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19518952.24                 X    =        -5945234.85
     Y    =        3352561.05  feet           Y    =          955354.08  meter
     Z    =      -10216418.17                 Z    =        -3142854.78
     XDOT =     -11076.723411                 XDOT =       -3345.241441
     YDOT =     -15943.135131  feet/sec       YDOT =       -4897.049377  meter/sec
     ZDOT =      15971.188248                 ZDOT =        4851.692537
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12564425.91                 X    =         3829637.02
     Y    =       15226233.41  feet           Y    =         4640955.94  meter
     Z    =      -10339312.36                 Z    =        -3151422.41
     XDOT =      -7182.956121                 XDOT =       -2189.365026
     YDOT =      16698.727916  feet/sec       YDOT =        5089.772269  meter/sec
     ZDOT =      15902.570665                 ZDOT =        4847.103539
  
  
    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   14221.45850722  .00016717  00000-0  10270-3 0  9101
    2 25544  51.6429 195.5253 0007138 350.4534   9.6480 15.50578830 19595
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14221.45850722   =   yrday.fracday
    Element set:     910
    Inclination:       51.6429  deg
    RA of node:       195.5253  deg
    Eccentricity:     .0007138     
    Arg of perigee:   350.4534  deg
    Mean anomaly:       9.6480  deg
    Mean motion:   15.50578830  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1959
    Checksum:              310
 
 
    Coasting Arc #12 (Orbit 1974)
    ---------------------------------------
 
    Vector Time (GMT): 2014/222/10:50:54.029
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6164277.04                 A    =         6796501.48  meter
     Y    =       -1094869.65  meter          E    =           .0013113
     Z    =        2640668.28                 I    =           51.58756
     XDOT =       3076.635631                 Wp   =           70.77766
     YDOT =       4699.721307  meter/sec      RA   =          189.46745  deg
     ZDOT =      -5207.985270                 TA   =           79.48814
                                              MA   =           79.34043
                                              Ha   =            227.707  n.mi
                                              Hp   =            219.892
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20224006.03                 X    =         6163234.77
     Y    =       -3592092.03  feet           Y    =        -1025942.55  meter
     Z    =        8663609.83                 Z    =         2670610.23
     XDOT =      10093.948922                 XDOT =        3049.151728
     YDOT =      15419.033159  feet/sec       YDOT =        4733.972556  meter/sec
     ZDOT =     -17086.565847                 ZDOT =       -5193.106519
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13395834.53                 X    =        -4083050.36
     Y    =      -15499731.34  feet           Y    =        -4724318.11  meter
     Z    =        8790996.87                 Z    =         2679495.85
     XDOT =       6906.966551                 XDOT =        2105.243405
     YDOT =     -15671.572735  feet/sec       YDOT =       -4776.695370  meter/sec
     ZDOT =     -17024.056577                 ZDOT =       -5188.932445
  
  
    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   14222.48968381  .00016717  00000-0  10270-3 0  9117
    2 25544  51.6428 190.4109 0007282 353.2324   6.8727 15.50626455 19754
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14222.48968381   =   yrday.fracday
    Element set:     911
    Inclination:       51.6428  deg
    RA of node:       190.4109  deg
    Eccentricity:     .0007282     
    Arg of perigee:   353.2324  deg
    Mean anomaly:       6.8727  deg
    Mean motion:   15.50626455  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1975
    Checksum:              315
 
 
    Coasting Arc #13 (Orbit 1989)
    ---------------------------------------
 
    Vector Time (GMT): 2014/223/10:50:54.029
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6316831.58                 A    =         6797501.14  meter
     Y    =        1226929.32  meter          E    =           .0012298
     Z    =       -2171426.70                 I    =           51.62184
     XDOT =      -2768.859272                 Wp   =           18.88259
     YDOT =      -4578.193235  meter/sec      RA   =          184.50872  deg
     ZDOT =       5488.041505                 TA   =          317.04701
                                              MA   =          317.14297
                                              Ha   =            227.788  n.mi
                                              Hp   =            219.739
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20724513.06                 X    =        -6319534.05
     Y    =        4025358.66  feet           Y    =         1156275.27  meter
     Z    =       -7124103.34                 Z    =        -2202118.88
     XDOT =      -9084.183964                 XDOT =       -2744.117616
     YDOT =     -15020.319014  feet/sec       YDOT =       -4609.017921  meter/sec
     ZDOT =      18005.385514                 ZDOT =        5474.651298
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14297387.50                 X    =         4357843.71
     Y    =       15473063.11  feet           Y    =         4716189.64  meter
     Z    =       -7254710.96                 Z    =        -2211235.90
     XDOT =      -6810.067353                 XDOT =       -2075.708529
     YDOT =      14677.967003  feet/sec       YDOT =        4473.844342  meter/sec
     ZDOT =      17949.170944                 ZDOT =        5470.907304
  
  
    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   14223.45640516  .00016717  00000-0  10270-3 0  9123
    2 25544  51.6430 185.6176 0007206 357.8406   2.2713 15.50612385 19903
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14223.45640516   =   yrday.fracday
    Element set:     912
    Inclination:       51.6430  deg
    RA of node:       185.6176  deg
    Eccentricity:     .0007206     
    Arg of perigee:   357.8406  deg
    Mean anomaly:       2.2713  deg
    Mean motion:   15.50612385  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1990
    Checksum:              290
 
 
    Coasting Arc #14 (Orbit 2005)
    ---------------------------------------
 
    Vector Time (GMT): 2014/224/10:50:54.029
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6457666.74                 A    =         6798285.96  meter
     Y    =       -1345384.55  meter          E    =           .0012596
     Z    =        1637021.73                 I    =           51.65648
     XDOT =       2396.439506                 Wp   =           84.61290
     YDOT =       4501.614372  meter/sec      RA   =          179.55210  deg
     ZDOT =      -5714.649364                 TA   =           77.50216
                                              MA   =           77.36127
                                              Ha   =            227.928  n.mi
                                              Hp   =            219.543
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21186570.66                 X    =         6464279.22
     Y    =       -4413991.29  feet           Y    =        -1273133.70  meter
     Z    =        5370806.20                 Z    =         1668407.68
     XDOT =       7862.334337                 XDOT =        2373.682708
     YDOT =      14769.076025  feet/sec       YDOT =        4528.285405  meter/sec
     ZDOT =     -18748.849618                 ZDOT =       -5703.063501
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15144207.64                 X    =        -4615954.49
     Y    =      -15412796.87  feet           Y    =        -4697820.49  meter
     Z    =        5504391.21                 Z    =         1677738.44
     XDOT =       6989.161806                 XDOT =        2130.296519
     YDOT =     -13590.517141  feet/sec       YDOT =       -4142.389625  meter/sec
     ZDOT =     -18700.282591                 ZDOT =       -5699.846134
  
  
    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   14224.48756512  .00016717  00000-0  10270-3 0  9132
    2 25544  51.6436 180.5034 0007372    .3465 359.7690 15.50645192 20060
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14224.48756512   =   yrday.fracday
    Element set:     913
    Inclination:       51.6436  deg
    RA of node:       180.5034  deg
    Eccentricity:     .0007372     
    Arg of perigee:      .3465  deg
    Mean anomaly:     359.7690  deg
    Mean motion:   15.50645192  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2006
    Checksum:              296
 
 
    Coasting Arc #15 (Orbit 2020)
    ---------------------------------------
 
    Vector Time (GMT): 2014/225/10:50:54.029
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6525603.40                 A    =         6798895.60  meter
     Y    =        1505986.10  meter          E    =           .0015851
     Z    =       -1120303.03                 I    =           51.68966
     XDOT =      -2035.353116                 Wp   =           23.96178
     YDOT =      -4475.697573  meter/sec      RA   =          174.59915  deg
     ZDOT =       5882.448383                 TA   =          323.90025
                                              MA   =          324.00717
                                              Ha   =            227.964  n.mi
                                              Hp   =            219.405
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21409459.97                 X    =        -6536516.69
     Y    =        4940899.27  feet           Y    =         1432951.51  meter
     Z    =       -3675534.87                 Z    =        -1152029.61
     XDOT =      -6677.667703                 XDOT =       -2013.728187
     YDOT =     -14684.047156  feet/sec       YDOT =       -4498.336981  meter/sec
     ZDOT =      19299.371335                 ZDOT =        5872.613834
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15975164.36                 X    =         4869230.10
     Y    =       15051925.16  feet           Y    =         4587826.79  meter
     Z    =       -3810602.46                 Z    =        -1161471.63
     XDOT =      -7346.027585                 XDOT =       -2239.069208
     YDOT =      12637.375931  feet/sec       YDOT =        3851.872184  meter/sec
     ZDOT =      19258.238095                 ZDOT =        5869.910971
  
  
    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   14225.45427014  .00016717  00000-0  10270-3 0  9143
    2 25544  51.6436 175.7102 0007265   4.7069 355.4149 15.50648121 20215
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14225.45427014   =   yrday.fracday
    Element set:     914
    Inclination:       51.6436  deg
    RA of node:       175.7102  deg
    Eccentricity:     .0007265     
    Arg of perigee:     4.7069  deg
    Mean anomaly:     355.4149  deg
    Mean motion:   15.50648121  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2021
    Checksum:              282
 
             

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