Return to Human Space Flight home page

    
   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  12916.69
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   132.9
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.186
   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 
   ------------------------------------------------------------------------
   028/18:42:24.270           1.4              -2.2              2.2    
   N/A                        1.0               0.3              220.2  
   000/00:04:48.540          -1.4              -0.0              216.8  
   
 
 
    Coasting Arc #1 (Orbit 599)
    ---------------------------------------
 
    Vector Time (GMT): 2015/026/13:33:24.481
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2929316.41                 A    =         6780170.61  meter
     Y    =       -3495206.32  meter          E    =           .0010246
     Z    =       -5025971.34                 I    =           51.97385
     XDOT =       3925.020291                 Wp   =           47.54013
     YDOT =       6249.209168  meter/sec      RA   =           70.44072  deg
     ZDOT =      -2054.173409                 TA   =          202.53454
                                              MA   =          202.57957
                                              Ha   =            221.065  n.mi
                                              Hp   =            217.270
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9610618.14                 X    =         2992596.96
     Y    =      -11467212.35  feet           Y    =        -3462095.09  meter
     Z    =      -16489407.28                 Z    =        -5011587.65
     XDOT =      12877.363159                 XDOT =        3864.826758
     YDOT =      20502.654750  feet/sec       YDOT =        6292.764693  meter/sec
     ZDOT =      -6739.414073                 ZDOT =       -2035.252945
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14312455.02                 X    =         4362436.29
     Y    =       -4589398.80  feet           Y    =        -1398848.75  meter
     Z    =      -16427189.12                 Z    =        -5007007.24
     XDOT =       -223.098980                 XDOT =         -68.000569
     YDOT =      23189.401339  feet/sec       YDOT =        7068.129528  meter/sec
     ZDOT =      -6659.603880                 ZDOT =       -2029.847263
  
  
    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   15026.58448633  .00016717  00000-0  10270-3 0  9002
    2 25544  51.6457  71.0684 0005930 307.3895  52.6717 15.53630755  6002
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15026.58448633   =   yrday.fracday
    Element set:     900
    Inclination:       51.6457  deg
    RA of node:        71.0684  deg
    Eccentricity:     .0005930     
    Arg of perigee:   307.3895  deg
    Mean anomaly:      52.6717  deg
    Mean motion:   15.53630755  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             600
    Checksum:              308
 
 
    Coasting Arc #2 (Orbit 615)
    ---------------------------------------
 
    Vector Time (GMT): 2015/027/13:33:24.481
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3645637.09                 A    =         6778748.59  meter
     Y    =        2060897.78  meter          E    =           .0003876
     Z    =        5331926.85                 I    =           51.95684
     XDOT =      -3409.174626                 Wp   =          330.27614
     YDOT =      -6859.575035  meter/sec      RA   =           65.46817  deg
     ZDOT =        323.762659                 TA   =          116.67000
                                              MA   =          116.63030
                                              Ha   =            221.320  n.mi
                                              Hp   =            216.936
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11960751.60                 X    =        -3694311.85
     Y    =        6761475.64  feet           Y    =         2019857.78  meter
     Z    =       17493198.32                 Z    =         5314098.97
     XDOT =     -11184.956121                 XDOT =       -3333.788573
     YDOT =     -22505.167438  feet/sec       YDOT =       -6897.277133  meter/sec
     ZDOT =       1062.213449                 ZDOT =         307.384861
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13830559.72                 X    =        -4215554.60
     Y    =        -412492.99  feet           Y    =         -125727.86  meter
     Z    =       17416503.28                 Z    =         5308550.20
     XDOT =       1954.167601                 XDOT =         595.630285
     YDOT =     -24047.197452  feet/sec       YDOT =       -7329.585783  meter/sec
     ZDOT =        993.413079                 ZDOT =         302.792307
  
  
    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   15027.61363941  .00016717  00000-0  10270-3 0  9016
    2 25544  51.6446  65.9411 0005914 312.4508  47.6144 15.53657534  6169
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15027.61363941   =   yrday.fracday
    Element set:     901
    Inclination:       51.6446  deg
    RA of node:        65.9411  deg
    Eccentricity:     .0005914     
    Arg of perigee:   312.4508  deg
    Mean anomaly:      47.6144  deg
    Mean motion:   15.53657534  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             616
    Checksum:              299
 
 
    Coasting Arc #3 (Orbit 630)
    ---------------------------------------
 
    Vector Time (GMT): 2015/028/13:33:24.481
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4328949.34                 A    =         6779415.72  meter
     Y    =        -600107.72  meter          E    =           .0009472
     Z    =       -5190371.40                 I    =           51.94567
     XDOT =       2688.475116                 Wp   =           79.48380
     YDOT =       7029.337525  meter/sec      RA   =           60.49505  deg
     ZDOT =       1433.451376                 TA   =          204.23976
                                              MA   =          204.28435
                                              Ha   =            221.433  n.mi
                                              Hp   =            216.973
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14202589.71                 X    =         4360550.78
     Y    =       -1968857.35  feet           Y    =         -551521.88  meter
     Z    =      -17028777.54                 Z    =        -5169265.66
     XDOT =       8820.456416                 XDOT =        2602.708499
     YDOT =      23062.130989  feet/sec       YDOT =        7058.922249  meter/sec
     ZDOT =       4702.924462                 ZDOT =        1446.303046
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13379759.86                 X    =         4078150.80
     Y    =        5444658.64  feet           Y    =         1659531.95  meter
     Z    =      -16938327.45                 Z    =        -5162802.21
     XDOT =      -3514.176828                 XDOT =       -1071.121097
     YDOT =      23393.517115  feet/sec       YDOT =        7130.344017  meter/sec
     ZDOT =       4756.588291                 ZDOT =        1449.808111
  
  
    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   15028.57845745  .00016717  00000-0  10270-3 0  9020
    2 25544  51.6452  61.1355 0006040 315.7940  44.2726 15.53657682  6318
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15028.57845745   =   yrday.fracday
    Element set:     902
    Inclination:       51.6452  deg
    RA of node:        61.1355  deg
    Eccentricity:     .0006040     
    Arg of perigee:   315.7940  deg
    Mean anomaly:      44.2726  deg
    Mean motion:   15.53657682  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             631
    Checksum:              302
 
 
    Coasting Arc #4 (Orbit 634)
    ---------------------------------------
 
    Vector Time (GMT): 2015/028/18:44:48.540
    Vector Time (MET): N/A
    Weight (LBS)     : 949862.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -895653.39                 A    =         6781515.28  meter
     Y    =        5142886.59  meter          E    =           .0003796
     Z    =        4325215.98                 I    =           51.95363
     XDOT =      -5543.514746                 Wp   =           84.95564
     YDOT =      -3944.203300  meter/sec      RA   =           59.45769  deg
     ZDOT =       3539.570180                 TA   =          329.15493
                                              MA   =          329.17723
                                              Ha   =            220.191  n.mi
                                              Hp   =            216.775
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2938495.37                 X    =         -974105.85
     Y    =       16872987.49  feet           Y    =         5132432.13  meter
     Z    =       14190341.15                 Z    =         4320674.60
     XDOT =     -18187.384336                 XDOT =       -5516.191459
     YDOT =     -12940.299541  feet/sec       YDOT =       -4006.041736  meter/sec
     ZDOT =      11612.763059                 ZDOT =        3512.707484
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10532721.47                 X    =         3210373.50
     Y    =       13526766.88  feet           Y    =         4122958.55  meter
     Z    =       14169918.84                 Z    =         4318991.26
     XDOT =     -20841.125401                 XDOT =       -6352.375022
     YDOT =       4174.794184  feet/sec       YDOT =        1272.477267  meter/sec
     ZDOT =      11498.541723                 ZDOT =        3504.755517
  
  
    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   15028.83572381  .00016717  00000-0  10270-3 0  9033
    2 25544  51.6451  59.8530 0006398 301.3253  58.7273 15.54093666  6358
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15028.83572381   =   yrday.fracday
    Element set:     903
    Inclination:       51.6451  deg
    RA of node:        59.8530  deg
    Eccentricity:     .0006398     
    Arg of perigee:   301.3253  deg
    Mean anomaly:      58.7273  deg
    Mean motion:   15.54093666  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             635
    Checksum:              315
 
 
    Coasting Arc #5 (Orbit 649)
    ---------------------------------------
 
    Vector Time (GMT): 2015/029/18:44:48.540
    Vector Time (MET): N/A
    Weight (LBS)     : 949862.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2062312.75                 A    =         6778429.02  meter
     Y    =       -3979066.42  meter          E    =           .0010293
     Z    =       -5093843.31                 I    =           51.92719
     XDOT =       5400.158608                 Wp   =           48.21342
     YDOT =       5123.520606  meter/sec      RA   =           54.48413  deg
     ZDOT =      -1811.596780                 TA   =          204.28216
                                              MA   =          204.33070
                                              Ha   =            220.314  n.mi
                                              Hp   =            216.642
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6766117.95                 X    =         2131397.99
     Y    =      -13054679.85  feet           Y    =        -3955617.95  meter
     Z    =      -16712084.34                 Z    =        -5083657.38
     XDOT =      17717.055802                 XDOT =        5351.264790
     YDOT =      16809.450808  feet/sec       YDOT =        5183.635336  meter/sec
     ZDOT =      -5943.558989                 ZDOT =       -1785.482890
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5361184.36                 X    =        -1634088.99
     Y    =      -13745677.19  feet           Y    =        -4189682.41  meter
     Z    =      -16667718.55                 Z    =        -5080320.62
     XDOT =      23328.644088                 XDOT =        7110.570718
     YDOT =      -2008.854131  feet/sec       YDOT =        -612.298739  meter/sec
     ZDOT =      -5832.774940                 ZDOT =       -1777.829802
  
  
    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   15029.80027610  .00016717  00000-0  10270-3 0  9042
    2 25544  51.6456  55.0448 0006396 306.1622  53.8939 15.54119433  6503
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15029.80027610   =   yrday.fracday
    Element set:     904
    Inclination:       51.6456  deg
    RA of node:        55.0448  deg
    Eccentricity:     .0006396     
    Arg of perigee:   306.1622  deg
    Mean anomaly:      53.8939  deg
    Mean motion:   15.54119433  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             650
    Checksum:              299
 
 
    Coasting Arc #6 (Orbit 665)
    ---------------------------------------
 
    Vector Time (GMT): 2015/030/18:44:48.540
    Vector Time (MET): N/A
    Weight (LBS)     : 949862.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3263099.75                 A    =         6777260.60  meter
     Y    =        2618423.86  meter          E    =           .0005131
     Z    =        5334105.29                 I    =           51.90435
     XDOT =      -4911.752396                 Wp   =          328.48036
     YDOT =      -5885.936852  meter/sec      RA   =           49.50374  deg
     ZDOT =       -111.206554                 TA   =          122.60048
                                              MA   =          122.55094
                                              Ha   =            220.477  n.mi
                                              Hp   =            216.407
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10705707.84                 X    =        -3318047.72
     Y    =        8590629.46  feet           Y    =         2581626.45  meter
     Z    =       17500345.42                 Z    =         5318120.62
     XDOT =     -16114.673215                 XDOT =       -4845.029225
     YDOT =     -19310.816444  feet/sec       YDOT =       -5940.490190  meter/sec
     ZDOT =       -364.850898                 ZDOT =        -134.904526
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        -358114.75                 X    =         -109153.38
     Y    =       13809076.53  feet           Y    =         4209006.53  meter
     Z    =       17431418.30                 Z    =         5313096.30
     XDOT =     -24142.674834                 XDOT =       -7358.687289
     YDOT =        -21.426678  feet/sec       YDOT =          -6.530851  meter/sec
     ZDOT =       -465.141006                 ZDOT =        -141.774979
  
  
    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   15030.82911598  .00016717  00000-0  10270-3 0  9054
    2 25544  51.6454  49.9164 0006527 309.0852  50.9720 15.54160767  6660
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15030.82911598   =   yrday.fracday
    Element set:     905
    Inclination:       51.6454  deg
    RA of node:        49.9164  deg
    Eccentricity:     .0006527     
    Arg of perigee:   309.0852  deg
    Mean anomaly:      50.9720  deg
    Mean motion:   15.54160767  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             666
    Checksum:              318
 
 
    Coasting Arc #7 (Orbit 680)
    ---------------------------------------
 
    Vector Time (GMT): 2015/031/18:44:48.540
    Vector Time (MET): N/A
    Weight (LBS)     : 949862.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4385231.85                 A    =         6778666.27  meter
     Y    =       -1220519.03  meter          E    =           .0007681
     Z    =       -5029160.60                 I    =           51.88818
     XDOT =       4036.414249                 Wp   =           81.09245
     YDOT =       6192.554633  meter/sec      RA   =           44.52157  deg
     ZDOT =       2020.521127                 TA   =          208.46596
                                              MA   =          208.50793
                                              Ha   =            220.664  n.mi
                                              Hp   =            216.345
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14387243.61                 X    =         4422983.36
     Y    =       -4004327.53  feet           Y    =        -1171269.38  meter
     Z    =      -16499870.72                 Z    =        -5007766.73
     XDOT =      13242.828900                 XDOT =        3957.052914
     YDOT =      20316.780292  feet/sec       YDOT =        6237.248688  meter/sec
     ZDOT =       6629.006322                 ZDOT =        2039.936161
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5997680.80                 X    =         1828093.11
     Y    =      -13786824.30  feet           Y    =        -4202224.05  meter
     Z    =      -16408060.59                 Z    =        -5001176.87
     XDOT =      23093.261999                 XDOT =        7038.826257
     YDOT =       2074.310241  feet/sec       YDOT =         632.249761  meter/sec
     ZDOT =       6710.899627                 ZDOT =        2045.482206
  
  
    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   15031.79364230  .00016717  00000-0  10270-3 0  9067
    2 25544  51.6459  45.1077 0006463 313.6878  46.3748 15.54150891  6817
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15031.79364230   =   yrday.fracday
    Element set:     906
    Inclination:       51.6459  deg
    RA of node:        45.1077  deg
    Eccentricity:     .0006463     
    Arg of perigee:   313.6878  deg
    Mean anomaly:      46.3748  deg
    Mean motion:   15.54150891  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             681
    Checksum:              318
 
 
    Coasting Arc #8 (Orbit 696)
    ---------------------------------------
 
    Vector Time (GMT): 2015/032/18:44:48.540
    Vector Time (MET): N/A
    Weight (LBS)     : 949862.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5336015.95                 A    =         6781905.55  meter
     Y    =        -148261.79  meter          E    =           .0009292
     Z    =        4183308.84                 I    =           51.87562
     XDOT =      -2770.756176                 Wp   =           37.72111
     YDOT =      -6092.511102  meter/sec      RA   =           39.54474  deg
     ZDOT =      -3738.613811                 TA   =           90.64159
                                              MA   =           90.53512
                                              Ha   =            220.764  n.mi
                                              Hp   =            216.051
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17506614.01                 X    =        -5354281.96
     Y    =        -486423.19  feet           Y    =         -208034.72  meter
     Z    =       13724766.52                 Z    =         4157343.73
     XDOT =      -9090.407402                 XDOT =       -2684.261982
     YDOT =     -19988.553484  feet/sec       YDOT =       -6123.011884  meter/sec
     ZDOT =     -12265.793342                 ZDOT =       -3751.863219
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11208351.15                 X    =        -3416305.43
     Y    =       13569397.53  feet           Y    =         4135952.37  meter
     Z    =       13613657.59                 Z    =         4149442.83
     XDOT =     -20313.334160                 XDOT =       -6191.504252
     YDOT =      -4379.034788  feet/sec       YDOT =       -1334.729803  meter/sec
     ZDOT =     -12321.311721                 ZDOT =       -3755.535813
  
  
    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   15032.82245449  .00016717  00000-0  10270-3 0  9073
    2 25544  51.6455  39.9789 0006445 317.9161  42.1496 15.54171861  6977
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15032.82245449   =   yrday.fracday
    Element set:     907
    Inclination:       51.6455  deg
    RA of node:        39.9789  deg
    Eccentricity:     .0006445     
    Arg of perigee:   317.9161  deg
    Mean anomaly:      42.1496  deg
    Mean motion:   15.54171861  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             697
    Checksum:              334
 
 
    Coasting Arc #9 (Orbit 711)
    ---------------------------------------
 
    Vector Time (GMT): 2015/033/18:44:48.540
    Vector Time (MET): N/A
    Weight (LBS)     : 949862.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5976627.96                 A    =         6785608.07  meter
     Y    =        1346292.86  meter          E    =           .0007128
     Z    =       -2908091.12                 I    =           51.86417
     XDOT =       1186.999510                 Wp   =             .20269
     YDOT =       5640.961456  meter/sec      RA   =           34.57545  deg
     ZDOT =       5057.939366                 TA   =          326.75926
                                              MA   =          326.80402
                                              Ha   =            220.908  n.mi
                                              Hp   =            215.865
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19608359.44                 X    =         5975255.27
     Y    =        4416971.31  feet           Y    =         1413119.68  meter
     Z    =       -9540981.36                 Z    =        -2879061.89
     XDOT =       3894.355347                 XDOT =        1099.263758
     YDOT =      18507.091392  feet/sec       YDOT =        5653.744776  meter/sec
     ZDOT =      16594.289258                 ZDOT =        5063.492255
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15361658.56                 X    =         4682233.53
     Y    =      -13052486.13  feet           Y    =        -3978397.77  meter
     Z    =       -9416993.83                 Z    =        -2870299.72
     XDOT =      16111.409033                 XDOT =        4910.757473
     YDOT =       6989.843583  feet/sec       YDOT =        2130.504324  meter/sec
     ZDOT =      16616.950615                 ZDOT =        5064.846548
  
  
    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   15033.78695154  .00016717  00000-0  10270-3 0  9082
    2 25544  51.6462  35.1697 0006478 321.1755  38.8932 15.54205275  7125
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15033.78695154   =   yrday.fracday
    Element set:     908
    Inclination:       51.6462  deg
    RA of node:        35.1697  deg
    Eccentricity:     .0006478     
    Arg of perigee:   321.1755  deg
    Mean anomaly:      38.8932  deg
    Mean motion:   15.54205275  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             712
    Checksum:              321
 
 
    Coasting Arc #10 (Orbit 727)
    ---------------------------------------
 
    Vector Time (GMT): 2015/034/18:44:48.540
    Vector Time (MET): N/A
    Weight (LBS)     : 949862.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6226057.91                 A    =         6788477.70  meter
     Y    =       -2366963.13  meter          E    =           .0008302
     Z    =        1297029.51                 I    =           51.84710
     XDOT =        644.927424                 Wp   =          102.97479
     YDOT =      -4916.166391  meter/sec      RA   =           29.61469  deg
     ZDOT =      -5846.111390                 TA   =           62.95787
                                              MA   =           62.87315
                                              Ha   =            220.931  n.mi
                                              Hp   =            215.735
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20426699.19                 X    =        -6205427.57
     Y    =       -7765627.06  feet           Y    =        -2436471.57  meter
     Z    =        4255346.17                 Z    =         1266835.48
     XDOT =       2115.903623                 XDOT =         728.250728
     YDOT =     -16129.154827  feet/sec       YDOT =       -4908.488699  meter/sec
     ZDOT =     -19180.155480                 ZDOT =       -5842.775995
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18305557.69                 X    =        -5579533.98
     Y    =       11980855.31  feet           Y    =         3651764.70  meter
     Z    =        4126577.03                 Z    =         1257780.68
     XDOT =     -10860.269563                 XDOT =       -3310.210163
     YDOT =      -9957.880008  feet/sec       YDOT =       -3035.161827  meter/sec
     ZDOT =     -19164.915012                 ZDOT =       -5841.466096
  
  
    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   15034.81573482  .00016717  00000-0  10270-3 0  9097
    2 25544  51.6462  30.0405 0006376 324.7287  35.3443 15.54190271  7287
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15034.81573482   =   yrday.fracday
    Element set:     909
    Inclination:       51.6462  deg
    RA of node:        30.0405  deg
    Eccentricity:     .0006376     
    Arg of perigee:   324.7287  deg
    Mean anomaly:      35.3443  deg
    Mean motion:   15.54190271  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             728
    Checksum:              298
 
 
    Coasting Arc #11 (Orbit 743)
    ---------------------------------------
 
    Vector Time (GMT): 2015/035/18:44:48.540
    Vector Time (MET): N/A
    Weight (LBS)     : 949862.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5996272.30                 A    =         6788905.94  meter
     Y    =        3131893.99  meter          E    =           .0015330
     Z    =         438584.19                 I    =           51.82166
     XDOT =      -2549.472415                 Wp   =           24.56801
     YDOT =       4030.724721  meter/sec      RA   =           24.65627  deg
     ZDOT =       6011.370946                 TA   =          340.15285
                                              MA   =          340.21243
                                              Ha   =            221.042  n.mi
                                              Hp   =            215.419
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19672809.39                 X    =         5958674.65
     Y    =       10275242.73  feet           Y    =         3198738.01  meter
     Z    =        1438924.50                 Z    =          467620.72
     XDOT =      -8364.410811                 XDOT =       -2623.555720
     YDOT =      13224.162469  feet/sec       YDOT =        4001.800942  meter/sec
     ZDOT =      19722.345622                 ZDOT =        5998.806266
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19699110.05                 X    =         6004288.74
     Y    =      -10206563.59  feet           Y    =        -3110960.58  meter
     Z    =        1562584.22                 Z    =          476275.67
     XDOT =       5215.454684                 XDOT =        1589.670588
     YDOT =      13105.624601  feet/sec       YDOT =        3994.594379  meter/sec
     ZDOT =      19667.778966                 ZDOT =        5994.739029
  
  
    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   15035.84450062  .00016717  00000-0  10270-3 0  9101
    2 25544  51.6466  24.9107 0006588 328.7058  31.3702 15.54243202  7442
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15035.84450062   =   yrday.fracday
    Element set:     910
    Inclination:       51.6466  deg
    RA of node:        24.9107  deg
    Eccentricity:     .0006588     
    Arg of perigee:   328.7058  deg
    Mean anomaly:      31.3702  deg
    Mean motion:   15.54243202  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             744
    Checksum:              287
 
 
    Coasting Arc #12 (Orbit 758)
    ---------------------------------------
 
    Vector Time (GMT): 2015/036/18:44:48.540
    Vector Time (MET): N/A
    Weight (LBS)     : 949862.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5276189.07                 A    =         6786988.02  meter
     Y    =       -3688532.50  meter          E    =           .0001497
     Z    =       -2152431.91                 I    =           51.78649
     XDOT =       4372.786458                 Wp   =           40.63966
     YDOT =      -3041.100936  meter/sec      RA   =           19.69490  deg
     ZDOT =      -5508.515269                 TA   =          163.16238
                                              MA   =          163.15741
                                              Ha   =            221.112  n.mi
                                              Hp   =            215.314
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17310331.61                 X    =        -5224095.43
     Y    =      -12101484.57  feet           Y    =        -3747243.15  meter
     Z    =       -7061784.47                 Z    =        -2177935.25
     XDOT =      14346.412263                 XDOT =        4433.225469
     YDOT =      -9977.365274  feet/sec       YDOT =       -2991.864020  meter/sec
     ZDOT =     -18072.556657                 ZDOT =       -5487.126607
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19692279.55                 X    =        -6002206.81
     Y    =        7534225.74  feet           Y    =         2296432.01  meter
     Z    =       -7170207.63                 Z    =        -2185479.29
     XDOT =        373.335014                 XDOT =         113.792512
     YDOT =     -16132.682729  feet/sec       YDOT =       -4917.241696  meter/sec
     ZDOT =     -17980.423416                 ZDOT =       -5480.433057
  
  
    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   15036.80895556  .00016717  00000-0  10270-3 0  9110
    2 25544  51.6468  20.1022 0006522 330.8197  29.2591 15.54236359  7597
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15036.80895556   =   yrday.fracday
    Element set:     911
    Inclination:       51.6468  deg
    RA of node:        20.1022  deg
    Eccentricity:     .0006522     
    Arg of perigee:   330.8197  deg
    Mean anomaly:      29.2591  deg
    Mean motion:   15.54236359  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             759
    Checksum:              311
 
 
    Coasting Arc #13 (Orbit 774)
    ---------------------------------------
 
    Vector Time (GMT): 2015/037/18:44:48.540
    Vector Time (MET): N/A
    Weight (LBS)     : 949862.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4079014.63                 A    =         6783282.93  meter
     Y    =        4022601.84  meter          E    =           .0010569
     Z    =        3619437.81                 I    =           51.74443
     XDOT =      -5934.522123                 Wp   =           59.98630
     YDOT =       2040.578147  meter/sec      RA   =           14.72245  deg
     ZDOT =       4415.713410                 TA   =          342.87196
                                              MA   =          342.90760
                                              Ha   =            221.234  n.mi
                                              Hp   =            215.030
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13382593.94                 X    =         4016148.27
     Y    =       13197512.61  feet           Y    =         4067864.82  meter
     Z    =       11874795.97                 Z    =         3639099.47
     XDOT =     -19470.216940                 XDOT =       -5978.348738
     YDOT =       6694.810194  feet/sec       YDOT =        1973.969747  meter/sec
     ZDOT =      14487.248720                 ZDOT =        4386.778627
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18320221.74                 X    =         5584003.59
     Y    =       -3956148.59  feet           Y    =        -1205834.09  meter
     Z    =       11958147.96                 Z    =         3644843.50
     XDOT =      -5343.822539                 XDOT =       -1628.797110
     YDOT =      18712.442576  feet/sec       YDOT =        5703.552497  meter/sec
     ZDOT =      14363.024706                 ZDOT =        4377.849930
  
  
    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   15037.83769234  .00016717  00000-0  10270-3 0  9128
    2 25544  51.6469  14.9721 0006654 336.7134  23.3716 15.54267643  7759
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15037.83769234   =   yrday.fracday
    Element set:     912
    Inclination:       51.6469  deg
    RA of node:        14.9721  deg
    Eccentricity:     .0006654     
    Arg of perigee:   336.7134  deg
    Mean anomaly:      23.3716  deg
    Mean motion:   15.54267643  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             775
    Checksum:              321
 
 
    Coasting Arc #14 (Orbit 789)
    ---------------------------------------
 
    Vector Time (GMT): 2015/038/18:44:48.540
    Vector Time (MET): N/A
    Weight (LBS)     : 949862.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2511010.06                 A    =         6779366.43  meter
     Y    =       -4199695.33  meter          E    =           .0012537
     Z    =       -4703464.01                 I    =           51.70061
     XDOT =       7044.079390                 Wp   =           38.08772
     YDOT =      -1049.254973  meter/sec      RA   =            9.73752  deg
     ZDOT =      -2818.081258                 TA   =          203.92392
                                              MA   =          203.98223
                                              Ha   =            221.288  n.mi
                                              Hp   =            214.814
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8238221.98                 X    =        -2441014.17
     Y    =      -13778527.99  feet           Y    =        -4227384.10  meter
     Z    =      -15431312.37                 Z    =        -4715491.44
     XDOT =      23110.496685                 XDOT =        7068.977830
     YDOT =      -3442.437577  feet/sec       YDOT =        -970.344508  meter/sec
     ZDOT =      -9245.673419                 ZDOT =       -2783.802508
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15999282.46                 X    =        -4876581.29
     Y    =        -416569.54  feet           Y    =         -126970.39  meter
     Z    =      -15481956.18                 Z    =        -4718900.24
     XDOT =       9350.816655                 XDOT =        2850.128916
     YDOT =     -20295.681757  feet/sec       YDOT =       -6186.123799  meter/sec
     ZDOT =      -9098.784926                 ZDOT =       -2773.309646
  
  
    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   15038.80211667  .00016717  00000-0  10270-3 0  9139
    2 25544  51.6465  10.1633 0006704 338.5233  21.5637 15.54314771  7905
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15038.80211667   =   yrday.fracday
    Element set:     913
    Inclination:       51.6465  deg
    RA of node:        10.1633  deg
    Eccentricity:     .0006704     
    Arg of perigee:   338.5233  deg
    Mean anomaly:      21.5637  deg
    Mean motion:   15.54314771  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             790
    Checksum:              288
 
 
    Coasting Arc #15 (Orbit 805)
    ---------------------------------------
 
    Vector Time (GMT): 2015/039/18:44:48.540
    Vector Time (MET): N/A
    Weight (LBS)     : 949862.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         668953.69                 A    =         6777008.74  meter
     Y    =        4225360.32  meter          E    =           .0004751
     Z    =        5254714.67                 I    =           51.66182
     XDOT =      -7616.395128                 Wp   =           10.97049
     YDOT =         86.240737  meter/sec      RA   =            4.74104  deg
     ZDOT =        904.688110                 TA   =           70.40676
                                              MA   =           70.35548
                                              Ha   =            221.415  n.mi
                                              Hp   =            214.653
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2194729.96                 X    =          596129.92
     Y    =       13862730.70  feet           Y    =         4232434.25  meter
     Z    =       17239877.53                 Z    =         5257787.04
     XDOT =     -24988.172992                 XDOT =       -7621.188003
     YDOT =        282.942049  feet/sec       YDOT =           1.042522  meter/sec
     ZDOT =       2968.136843                 ZDOT =         867.678008
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12950823.43                 X    =         3947410.98
     Y    =        5370609.20  feet           Y    =         1636961.68  meter
     Z    =       17252195.48                 Z    =         5258469.18
     XDOT =     -12274.192105                 XDOT =       -3741.173753
     YDOT =      20619.025717  feet/sec       YDOT =        6284.679039  meter/sec
     ZDOT =       2809.760576                 ZDOT =         856.415024
  
  
    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   15039.83082244  .00016717  00000-0  10270-3 0  9141
    2 25544  51.6468   5.0337 0006611 343.1635  16.9297 15.54326241  8060
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15039.83082244   =   yrday.fracday
    Element set:     914
    Inclination:       51.6468  deg
    RA of node:         5.0337  deg
    Eccentricity:     .0006611     
    Arg of perigee:   343.1635  deg
    Mean anomaly:      16.9297  deg
    Mean motion:   15.54326241  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             806
    Checksum:              295
 
 
    Coasting Arc #16 (Orbit 820)
    ---------------------------------------
 
    Vector Time (GMT): 2015/040/18:44:48.540
    Vector Time (MET): N/A
    Weight (LBS)     : 949862.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1228517.05                 A    =         6777079.43  meter
     Y    =       -4145448.64  meter          E    =           .0013118
     Z    =       -5228683.51                 I    =           51.62971
     XDOT =       7532.869096                 Wp   =           70.54652
     YDOT =        842.943892  meter/sec      RA   =          359.73818  deg
     ZDOT =       1108.129041                 TA   =          210.04814
                                              MA   =          210.12348
                                              Ha   =            221.435  n.mi
                                              Hp   =            214.487
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4030567.74                 X    =         1300179.83
     Y    =      -13600553.26  feet           Y    =        -4131310.28  meter
     Z    =      -17154473.47                 Z    =        -5222541.30
     XDOT =      24714.137455                 XDOT =        7517.500426
     YDOT =       2765.563951  feet/sec       YDOT =         927.095499  meter/sec
     ZDOT =       3635.593965                 ZDOT =        1144.684446
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9693454.61                 X    =        -2954564.96
     Y    =      -10401261.56  feet           Y    =        -3170304.52  meter
     Z    =      -17127381.04                 Z    =        -5220425.74
     XDOT =      14014.325576                 XDOT =        4271.566436
     YDOT =     -19269.151281  feet/sec       YDOT =       -5873.237310  meter/sec
     ZDOT =       3791.831827                 ZDOT =        1155.750341
  
  
    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   15040.79521793  .00016717  00000-0  10270-3 0  9156
    2 25544  51.6456    .2238 0006652 345.9515  14.1452 15.54373097  8217
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15040.79521793   =   yrday.fracday
    Element set:     915
    Inclination:       51.6456  deg
    RA of node:          .2238  deg
    Eccentricity:     .0006652     
    Arg of perigee:   345.9515  deg
    Mean anomaly:      14.1452  deg
    Mean motion:   15.54373097  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             821
    Checksum:              297
 
             

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