Return to Human Space Flight home page

    
   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  22604.21
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   127.9
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.423
   ET - UTC  (sec) :   67.18
   UT1 - UTC (sec) :    0.00
 
 
   Maneuvers contained within the current ephemeris are as follows:
 
 
   IMPULSIVE TIG (GMT)   M50 DVx(FPS)      LVLH DVx(FPS)      DVmag(FPS) 
   IMPULSIVE TIG (MET)   M50 DVy(FPS)      LVLH DVy(FPS)      Invar Sph HA
   DT                    M50 DVz(FPS)      LVLH DVz(FPS)      Invar Sph HP 
   ------------------------------------------------------------------------
   265/11:30:45.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              227.2  
   000/00:00:00.000           0.0               0.0              219.8  
   
 
 
    Coasting Arc #1 (Orbit 2595)
    ---------------------------------------
 
    Vector Time (GMT): 2014/262/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 912103.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3334540.28                 A    =         6790068.99  meter
     Y    =       -3398438.20  meter          E    =           .0013072
     Z    =       -4853283.82                 I    =           51.58533
     XDOT =       6609.759280                 Wp   =           77.88886
     YDOT =      -2957.625534  meter/sec      RA   =          351.60840  deg
     ZDOT =      -2473.301199                 TA   =          167.76399
                                              MA   =          167.73221
                                              Ha   =            227.390  n.mi
                                              Hp   =            219.791
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10940092.78                 X    =        -3272714.75
     Y    =      -11149731.62  feet           Y    =        -3435382.02  meter
     Z    =      -15922847.17                 Z    =        -4869331.93
     XDOT =      21685.561942                 XDOT =        6654.355323
     YDOT =      -9703.495847  feet/sec       YDOT =       -2883.461843  meter/sec
     ZDOT =      -8114.505246                 ZDOT =       -2441.083446
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10340009.10                 X    =         3151634.77
     Y    =       11615831.06  feet           Y    =         3540505.31  meter
     Z    =      -15990493.67                 Z    =        -4873902.47
     XDOT =     -21293.950814                 XDOT =       -6490.396208
     YDOT =       7987.388038  feet/sec       YDOT =        2434.555874  meter/sec
     ZDOT =      -7976.916745                 ZDOT =       -2431.364224
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14262.52042369  .00016717  00000-0  10270-3 0  9003
    2 25544  51.6475 352.0341 0001801 119.7772 240.3558 15.50440897 25964
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14262.52042369   =   yrday.fracday
    Element set:     900
    Inclination:       51.6475  deg
    RA of node:       352.0341  deg
    Eccentricity:     .0001801     
    Arg of perigee:   119.7772  deg
    Mean anomaly:     240.3558  deg
    Mean motion:   15.50440897  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2596
    Checksum:              301
 
 
    Coasting Arc #2 (Orbit 2611)
    ---------------------------------------
 
    Vector Time (GMT): 2014/263/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 912103.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3075828.59                 A    =         6789100.33  meter
     Y    =        3369103.77  meter          E    =           .0007489
     Z    =        5023694.48                 I    =           51.55235
     XDOT =      -6693.021395                 Wp   =          122.67026
     YDOT =       3185.112482  meter/sec      RA   =          346.64303  deg
     ZDOT =       1955.741200                 TA   =          308.28493
                                              MA   =          308.35227
                                              Ha   =            227.195  n.mi
                                              Hp   =            219.770
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10091301.15                 X    =         3013522.50
     Y    =       11053490.08  feet           Y    =         3403151.91  meter
     Z    =       16481937.27                 Z    =         5038484.61
     XDOT =     -21958.731612                 XDOT =       -6737.640941
     YDOT =      10449.844100  feet/sec       YDOT =        3110.017539  meter/sec
     ZDOT =       6416.473753                 ZDOT =        1923.118826
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9688857.16                 X    =        -2953163.66
     Y    =      -11317354.98  feet           Y    =        -3449529.80  meter
     Z    =       16544237.10                 Z    =         5042683.47
     XDOT =      21444.355613                 XDOT =        6536.239591
     YDOT =      -9153.368193  feet/sec       YDOT =       -2789.946625  meter/sec
     ZDOT =       6277.132818                 ZDOT =        1913.270083
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14263.55168243  .00016717  00000-0  10270-3 0  9018
    2 25544  51.6477 346.9213 0001805 120.2827 239.8503 15.50515188 26126
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14263.55168243   =   yrday.fracday
    Element set:     901
    Inclination:       51.6477  deg
    RA of node:       346.9213  deg
    Eccentricity:     .0001805     
    Arg of perigee:   120.2827  deg
    Mean anomaly:     239.8503  deg
    Mean motion:   15.50515188  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2612
    Checksum:              298
 
 
    Coasting Arc #3 (Orbit 2626)
    ---------------------------------------
 
    Vector Time (GMT): 2014/264/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 912103.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2793115.55                 A    =         6788535.09  meter
     Y    =       -3409551.54  meter          E    =           .0015257
     Z    =       -5176616.91                 I    =           51.51939
     XDOT =       6716.056973                 Wp   =           83.50822
     YDOT =      -3390.357812  meter/sec      RA   =          341.67551  deg
     ZDOT =      -1392.556269                 TA   =          173.05789
                                              MA   =          173.03673
                                              Ha   =            227.271  n.mi
                                              Hp   =            219.716
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9163764.94                 X    =        -2729635.29
     Y    =      -11186192.71  feet           Y    =        -3440431.72  meter
     Z    =      -16983651.29                 Z    =        -5190030.79
     XDOT =      22034.307653                 XDOT =        6760.234159
     YDOT =     -11123.221167  feet/sec       YDOT =       -3315.007693  meter/sec
     ZDOT =      -4568.754165                 ZDOT =       -1359.822940
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8950201.65                 X    =         2728021.46
     Y    =       11272939.11  feet           Y    =         3435991.84  meter
     Z    =      -17040089.22                 Z    =        -5193819.20
     XDOT =     -21345.007032                 XDOT =       -6505.958143
     YDOT =      10261.423557  feet/sec       YDOT =        3127.681900  meter/sec
     ZDOT =      -4428.915865                 ZDOT =       -1349.933556
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14264.51846888  .00016717  00000-0  10270-3 0  9024
    2 25544  51.6470 342.1291 0001732 120.4779 239.6543 15.50503346 26271
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14264.51846888   =   yrday.fracday
    Element set:     902
    Inclination:       51.6470  deg
    RA of node:       342.1291  deg
    Eccentricity:     .0001732     
    Arg of perigee:   120.4779  deg
    Mean anomaly:     239.6543  deg
    Mean motion:   15.50503346  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2627
    Checksum:              309
 
 
    Coasting Arc #4 (Orbit 2641)
    ---------------------------------------
 
    Vector Time (GMT): 2014/265/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4466201.49                 A    =         6796605.36  meter
     Y    =       -4311758.16  meter          E    =           .0005808
     Z    =       -2769137.95                 I    =           51.51809
     XDOT =       5263.459422                 Wp   =           72.13777
     YDOT =       2170.486062  meter/sec      RA   =          336.77610  deg
     ZDOT =       5120.170274                 TA   =          256.50289
                                              MA   =          256.56761
                                              Ha   =            227.227  n.mi
                                              Hp   =            219.806
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14652892.04                 X    =         4527536.22
     Y    =      -14146188.20  feet           Y    =        -4261471.66  meter
     Z    =       -9085098.27                 Z    =        -2747292.17
     XDOT =      17268.567656                 XDOT =        5213.925202
     YDOT =       7121.017263  feet/sec       YDOT =        2229.069252  meter/sec
     ZDOT =      16798.458905                 ZDOT =        5145.618789
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16300661.13                 X    =        -4968441.51
     Y    =       12280221.89  feet           Y    =         3743011.63  meter
     Z    =       -8991412.18                 Z    =        -2740582.43
     XDOT =     -15288.584432                 XDOT =       -4659.960535
     YDOT =      -7941.138443  feet/sec       YDOT =       -2420.458998  meter/sec
     ZDOT =      16906.302535                 ZDOT =        5153.041013
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14265.48523419  .00016717  00000-0  10270-3 0  9034
    2 25544  51.6473 337.3359 0001703 119.9019 240.2301 15.50540793 26427
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14265.48523419   =   yrday.fracday
    Element set:     903
    Inclination:       51.6473  deg
    RA of node:       337.3359  deg
    Eccentricity:     .0001703     
    Arg of perigee:   119.9019  deg
    Mean anomaly:     240.2301  deg
    Mean motion:   15.50540793  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2642
    Checksum:              295
 
 
    Coasting Arc #5 (Orbit 2657)
    ---------------------------------------
 
    Vector Time (GMT): 2014/266/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4549762.34                 A    =         6797480.49  meter
     Y    =        4495663.08  meter          E    =           .0015609
     Z    =        2278895.40                 I    =           51.49276
     XDOT =      -4940.444179                 Wp   =          109.04238
     YDOT =      -2241.453812  meter/sec      RA   =          331.81061  deg
     ZDOT =      -5416.255217                 TA   =           45.56016
                                              MA   =           45.43255
                                              Ha   =            227.185  n.mi
                                              Hp   =            219.660
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14927041.81                 X    =        -4610765.92
     Y    =       14749550.79  feet           Y    =         4444443.95  meter
     Z    =        7476690.95                 Z    =         2256644.37
     XDOT =     -16208.806361                 XDOT =       -4888.702013
     YDOT =      -7353.851089  feet/sec       YDOT =       -2296.412572  meter/sec
     ZDOT =     -17769.866198                 ZDOT =       -5440.129262
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16411675.29                 X    =         5002278.63
     Y    =      -13131666.42  feet           Y    =        -4002531.92  meter
     Z    =        7381259.01                 Z    =         2249807.75
     XDOT =      14296.981954                 XDOT =        4357.720100
     YDOT =       7775.345795  feet/sec       YDOT =        2369.925398  meter/sec
     ZDOT =     -17870.995424                 ZDOT =       -5447.079405
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14266.51642915  .00016717  00000-0  10270-3 0  9043
    2 25544  51.6468 332.2231 0001803 118.6984 241.4348 15.50597001 26587
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14266.51642915   =   yrday.fracday
    Element set:     904
    Inclination:       51.6468  deg
    RA of node:       332.2231  deg
    Eccentricity:     .0001803     
    Arg of perigee:   118.6984  deg
    Mean anomaly:     241.4348  deg
    Mean motion:   15.50597001  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2658
    Checksum:              304
 
 
    Coasting Arc #6 (Orbit 2672)
    ---------------------------------------
 
    Vector Time (GMT): 2014/267/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4575005.02                 A    =         6798314.67  meter
     Y    =       -4695058.67  meter          E    =           .0007906
     Z    =       -1793696.37                 I    =           51.46790
     XDOT =       4616.106786                 Wp   =           49.90828
     YDOT =       2350.916003  meter/sec      RA   =          326.84351  deg
     ZDOT =       5641.752742                 TA   =          290.37452
                                              MA   =          290.45942
                                              Ha   =            227.135  n.mi
                                              Hp   =            219.716
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15009858.99                 X    =         4635879.49
     Y    =      -15403735.81  feet           Y    =        -4643557.91  meter
     Z    =       -5884830.62                 Z    =        -1771322.91
     XDOT =      15144.707304                 XDOT =        4562.069194
     YDOT =       7712.979013  feet/sec       YDOT =        2402.235018  meter/sec
     ZDOT =      18509.687473                 ZDOT =        5664.045683
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16311962.00                 X    =        -4971886.02
     Y    =       14057427.01  feet           Y    =         4284703.75  meter
     Z    =       -5788852.79                 Z    =        -1764442.33
     XDOT =     -13285.950174                 XDOT =       -4049.557613
     YDOT =      -7785.126526  feet/sec       YDOT =       -2372.906565  meter/sec
     ZDOT =      18604.068202                 ZDOT =        5670.519988
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14267.48315369  .00016717  00000-0  10270-3 0  9051
    2 25544  51.6463 327.4298 0001649 118.9982 241.1334 15.50590217 26731
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14267.48315369   =   yrday.fracday
    Element set:     905
    Inclination:       51.6463  deg
    RA of node:       327.4298  deg
    Eccentricity:     .0001649     
    Arg of perigee:   118.9982  deg
    Mean anomaly:     241.1334  deg
    Mean motion:   15.50590217  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2673
    Checksum:              326
 
 
    Coasting Arc #7 (Orbit 2688)
    ---------------------------------------
 
    Vector Time (GMT): 2014/268/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4585226.16                 A    =         6798788.43  meter
     Y    =        4854180.73  meter          E    =           .0015448
     Z    =        1239364.98                 I    =           51.44440
     XDOT =      -4280.959202                 Wp   =          120.99105
     YDOT =      -2544.169618  meter/sec      RA   =          321.87505  deg
     ZDOT =      -5827.176250                 TA   =           45.51387
                                              MA   =           45.38769
                                              Ha   =            227.028  n.mi
                                              Hp   =            219.557
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15043392.90                 X    =        -4645186.44
     Y    =       15925789.80  feet           Y    =         4802570.69  meter
     Z    =        4066158.07                 Z    =         1216944.01
     XDOT =     -14045.141740                 XDOT =       -4223.884679
     YDOT =      -8347.013184  feet/sec       YDOT =       -2591.723812  meter/sec
     ZDOT =     -19118.032315                 ZDOT =       -5847.833760
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16125562.87                 X    =         4915071.56
     Y    =      -14855091.29  feet           Y    =        -4527831.82  meter
     Z    =        3969959.36                 Z    =         1210043.61
     XDOT =      12235.773021                 XDOT =        3729.463617
     YDOT =       8108.137545  feet/sec       YDOT =        2471.360324  meter/sec
     ZDOT =     -19205.420022                 ZDOT =       -5853.812023
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14268.51430530  .00016717  00000-0  10270-3 0  9065
    2 25544  51.6461 322.3163 0001757 118.6956 241.4372 15.50669322 26898
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14268.51430530   =   yrday.fracday
    Element set:     906
    Inclination:       51.6461  deg
    RA of node:       322.3163  deg
    Eccentricity:     .0001757     
    Arg of perigee:   118.6956  deg
    Mean anomaly:     241.4372  deg
    Mean motion:   15.50669322  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2689
    Checksum:              307
 
 
    Coasting Arc #8 (Orbit 2703)
    ---------------------------------------
 
    Vector Time (GMT): 2014/269/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4535878.96                 A    =         6799283.77  meter
     Y    =       -5010604.59  meter          E    =           .0011100
     Z    =        -701880.26                 I    =           51.42116
     XDOT =       3969.954391                 Wp   =           48.53136
     YDOT =       2771.674993  meter/sec      RA   =          316.90487  deg
     ZDOT =       5937.498087                 TA   =          303.87596
                                              MA   =          303.98152
                                              Ha   =            227.059  n.mi
                                              Hp   =            219.590
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14881492.66                 X    =         4594981.14
     Y    =      -16438991.43  feet           Y    =        -4959551.09  meter
     Z    =       -2302756.76                 Z    =         -679701.06
     XDOT =      13024.784748                 XDOT =        3909.822969
     YDOT =       9093.421893  feet/sec       YDOT =        2815.734187  meter/sec
     ZDOT =      19479.980599                 ZDOT =        5956.637391
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15721252.74                 X    =        -4791837.84
     Y    =       15651543.51  feet           Y    =         4770590.46  meter
     Z    =       -2207566.45                 Z    =         -672866.25
     XDOT =     -11275.777122                 XDOT =       -3436.856867
     YDOT =      -8600.016075  feet/sec       YDOT =       -2621.284900  meter/sec
     ZDOT =      19560.869417                 ZDOT =        5962.152998
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14269.48098959  .00016717  00000-0  10270-3 0  9078
    2 25544  51.6454 317.5223 0001673 116.9452 243.1870 15.50643451 27047
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14269.48098959   =   yrday.fracday
    Element set:     907
    Inclination:       51.6454  deg
    RA of node:       317.5223  deg
    Eccentricity:     .0001673     
    Arg of perigee:   116.9452  deg
    Mean anomaly:     243.1870  deg
    Mean motion:   15.50643451  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2704
    Checksum:              319
 
 
    Coasting Arc #9 (Orbit 2719)
    ---------------------------------------
 
    Vector Time (GMT): 2014/270/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4477035.63                 A    =         6799213.36  meter
     Y    =        5107548.44  meter          E    =           .0013970
     Z    =         103484.52                 I    =           51.40001
     XDOT =      -3661.317879                 Wp   =          131.60789
     YDOT =      -3077.558757  meter/sec      RA   =          311.93318  deg
     ZDOT =      -5988.261192                 TA   =           47.27515
                                              MA   =           47.15763
                                              Ha   =            226.912  n.mi
                                              Hp   =            219.436
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14688437.11                 X    =        -4534319.38
     Y    =       16757048.67  feet           Y    =         5057163.05  meter
     Z    =         339516.15                 Z    =           81595.62
     XDOT =     -12012.197766                 XDOT =       -3597.542286
     YDOT =     -10096.977549  feet/sec       YDOT =       -3118.146118  meter/sec
     ZDOT =     -19646.526219                 ZDOT =       -6005.892348
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15255282.27                 X    =         4649810.04
     Y    =      -16244389.94  feet           Y    =        -4951290.05  meter
     Z    =         245549.56                 Z    =           74843.50
     XDOT =      10350.983408                 XDOT =        3154.979743
     YDOT =       9387.250012  feet/sec       YDOT =        2861.233804  meter/sec
     ZDOT =     -19720.947042                 ZDOT =       -6010.944658
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14270.51209780  .00016717  00000-0  10270-3 0  9081
    2 25544  51.6457 312.4081 0001792 119.7497 240.3832 15.50733850 27206
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14270.51209780   =   yrday.fracday
    Element set:     908
    Inclination:       51.6457  deg
    RA of node:       312.4081  deg
    Eccentricity:     .0001792     
    Arg of perigee:   119.7497  deg
    Mean anomaly:     240.3832  deg
    Mean motion:   15.50733850  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2720
    Checksum:              301
 
 
    Coasting Arc #10 (Orbit 2735)
    ---------------------------------------
 
    Vector Time (GMT): 2014/271/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4365237.01                 A    =         6799186.60  meter
     Y    =       -5184563.11  meter          E    =           .0013731
     Z    =         464171.82                 I    =           51.37886
     XDOT =       3399.075303                 Wp   =           56.86903
     YDOT =       3406.671314  meter/sec      RA   =          306.95988  deg
     ZDOT =       5963.664966                 TA   =          308.14811
                                              MA   =          308.27177
                                              Ha   =            226.979  n.mi
                                              Hp   =            219.434
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14321643.74                 X    =         4420632.73
     Y    =      -17009721.50  feet           Y    =        -5135438.42  meter
     Z    =        1522873.43                 Z    =          485512.96
     XDOT =      11151.821859                 XDOT =        3331.758457
     YDOT =      11176.743156  feet/sec       YDOT =        3444.306208  meter/sec
     ZDOT =      19565.829940                 ZDOT =        5980.013588
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14599437.79                 X    =        -4449908.64
     Y    =       16763322.82  feet           Y    =         5109460.79  meter
     Z    =        1614519.46                 Z    =          492105.53
     XDOT =      -9613.921873                 XDOT =       -2930.323387
     YDOT =     -10300.052819  feet/sec       YDOT =       -3139.456099  meter/sec
     ZDOT =      19634.740110                 ZDOT =        5984.668785
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14271.54318544  .00016717  00000-0  10270-3 0  9095
    2 25544  51.6451 307.2941 0001778 116.7349 243.3984 15.50709130 27366
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14271.54318544   =   yrday.fracday
    Element set:     909
    Inclination:       51.6451  deg
    RA of node:       307.2941  deg
    Eccentricity:     .0001778     
    Arg of perigee:   116.7349  deg
    Mean anomaly:     243.3984  deg
    Mean motion:   15.50709130  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2736
    Checksum:              315
 
 
    Coasting Arc #11 (Orbit 2750)
    ---------------------------------------
 
    Vector Time (GMT): 2014/272/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4255523.65                 A    =         6798524.69  meter
     Y    =        5184876.27  meter          E    =           .0011203
     Z    =       -1079635.28                 I    =           51.36030
     XDOT =      -3151.816488                 Wp   =          138.40908
     YDOT =      -3798.233297  meter/sec      RA   =          301.98481  deg
     ZDOT =      -5860.762804                 TA   =           53.32958
                                              MA   =           53.22667
                                              Ha   =            226.814  n.mi
                                              Hp   =            219.323
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13961691.76                 X    =        -4307941.25
     Y    =       17010748.91  feet           Y    =         5136995.07  meter
     Z    =       -3542110.48                 Z    =        -1100436.10
     XDOT =     -10340.605277                 XDOT =       -3080.639390
     YDOT =     -12461.395331  feet/sec       YDOT =       -3833.081499  meter/sec
     ZDOT =     -19228.224421                 ZDOT =       -5875.900881
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13936259.77                 X    =         4247771.98
     Y    =      -17012764.63  feet           Y    =        -5185490.66  meter
     Z    =       -3631454.96                 Z    =        -1106867.47
     XDOT =       8980.752562                 XDOT =        2737.333381
     YDOT =      11445.092956  feet/sec       YDOT =        3488.464333  meter/sec
     ZDOT =     -19291.921435                 ZDOT =       -5880.177653
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14272.50980579  .00016717  00000-0  10270-3 0  9107
    2 25544  51.6459 302.4992 0001855 123.1302 237.0027 15.50792210 27510
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14272.50980579   =   yrday.fracday
    Element set:     910
    Inclination:       51.6459  deg
    RA of node:       302.4992  deg
    Eccentricity:     .0001855     
    Arg of perigee:   123.1302  deg
    Mean anomaly:     237.0027  deg
    Mean motion:   15.50792210  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2751
    Checksum:              291
 
 
    Coasting Arc #12 (Orbit 2766)
    ---------------------------------------
 
    Vector Time (GMT): 2014/273/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4106655.06                 A    =         6797877.50  meter
     Y    =       -5151714.70  meter          E    =           .0015049
     Z    =        1649214.30                 I    =           51.34155
     XDOT =       2966.380421                 Wp   =           69.73432
     YDOT =       4196.857367  meter/sec      RA   =          297.00816  deg
     ZDOT =       5686.199767                 TA   =          308.38362
                                              MA   =          308.51870
                                              Ha   =            226.857  n.mi
                                              Hp   =            219.287
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13473277.75                 X    =         4155946.05
     Y    =      -16901951.11  feet           Y    =        -5105515.69  meter
     Z    =        5410808.07                 Z    =         1669284.22
     XDOT =       9732.219228                 XDOT =        2891.607654
     YDOT =      13769.217084  feet/sec       YDOT =        4229.611722  meter/sec
     ZDOT =      18655.511047                 ZDOT =        5700.428248
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13143344.84                 X    =        -4006091.51
     Y    =       17132340.80  feet           Y    =         5221937.48  meter
     Z    =        5497034.96                 Z    =         1675496.25
     XDOT =      -8602.905945                 XDOT =       -2622.165732
     YDOT =     -12643.329883  feet/sec       YDOT =       -3853.686948  meter/sec
     ZDOT =      18715.275849                 ZDOT =        5704.416079
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14273.54084885  .00016717  00000-0  10270-3 0  9118
    2 25544  51.6451 297.3851 0001882 119.9636 240.1702 15.50787370 27674
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14273.54084885   =   yrday.fracday
    Element set:     911
    Inclination:       51.6451  deg
    RA of node:       297.3851  deg
    Eccentricity:     .0001882     
    Arg of perigee:   119.9636  deg
    Mean anomaly:     240.1702  deg
    Mean motion:   15.50787370  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2767
    Checksum:              326
 
 
    Coasting Arc #13 (Orbit 2781)
    ---------------------------------------
 
    Vector Time (GMT): 2014/274/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3976708.95                 A    =         6796683.53  meter
     Y    =        5030125.33  meter          E    =           .0007792
     Z    =       -2248404.59                 I    =           51.32562
     XDOT =      -2804.536797                 Wp   =          133.84571
     YDOT =      -4631.540346  meter/sec      RA   =          292.02943  deg
     ZDOT =      -5418.415540                 TA   =           71.23123
                                              MA   =           71.14671
                                              Ha   =            226.699  n.mi
                                              Hp   =            219.228
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13046945.39                 X    =        -4021739.30
     Y    =       16503035.88  feet           Y    =         4985403.25  meter
     Z    =       -7376655.49                 Z    =        -2267832.81
     XDOT =      -9201.236211                 XDOT =       -2726.216250
     YDOT =     -15195.342341  feet/sec       YDOT =       -4662.464985  meter/sec
     ZDOT =     -17776.953873                 ZDOT =       -5431.849115
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12422045.76                 X    =         3786239.55
     Y    =      -16941879.83  feet           Y    =        -5163884.97  meter
     Z    =       -7460128.03                 Z    =        -2273847.02
     XDOT =       8373.466772                 XDOT =        2552.232672
     YDOT =      13967.804148  feet/sec       YDOT =        4257.386704  meter/sec
     ZDOT =     -17833.270728                 ZDOT =       -5435.580918
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14274.50742780  .00016717  00000-0  10270-3 0  9121
    2 25544  51.6458 292.5902 0001880 128.0397 232.0924 15.50851913 27826
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14274.50742780   =   yrday.fracday
    Element set:     912
    Inclination:       51.6458  deg
    RA of node:       292.5902  deg
    Eccentricity:     .0001880     
    Arg of perigee:   128.0397  deg
    Mean anomaly:     232.0924  deg
    Mean motion:   15.50851913  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2782
    Checksum:              311
 
 
    Coasting Arc #14 (Orbit 2797)
    ---------------------------------------
 
    Vector Time (GMT): 2014/275/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3826605.22                 A    =         6795481.15  meter
     Y    =       -4867387.03  meter          E    =           .0014758
     Z    =        2786217.54                 I    =           51.30981
     XDOT =       2710.226271                 Wp   =           85.20656
     YDOT =       5054.623816  meter/sec      RA   =          287.04878  deg
     ZDOT =       5085.807681                 TA   =          306.51251
                                              MA   =          306.64834
                                              Ha   =            226.677  n.mi
                                              Hp   =            219.190
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12554479.06                 X    =         3867214.44
     Y    =      -15969117.54  feet           Y    =        -4824368.16  meter
     Z    =        9141133.67                 Z    =         2804905.78
     XDOT =       8891.818475                 XDOT =        2628.797514
     YDOT =      16583.411469  feet/sec       YDOT =        5084.476441  meter/sec
     ZDOT =      16685.720738                 ZDOT =        5098.775449
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11653521.32                 X    =        -3551993.30
     Y    =       16593635.16  feet           Y    =         5057740.00  meter
     Z    =        9221425.99                 Z    =         2810690.64
     XDOT =      -8422.977917                 XDOT =       -2567.323669
     YDOT =     -15258.131212  feet/sec       YDOT =       -4650.678393  meter/sec
     ZDOT =      16739.993946                 ZDOT =        5102.350155
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14275.53842507  .00016717  00000-0  10270-3 0  9134
    2 25544  51.6447 287.4759 0001900 126.2770 233.8556 15.50871125 27989
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14275.53842507   =   yrday.fracday
    Element set:     913
    Inclination:       51.6447  deg
    RA of node:       287.4759  deg
    Eccentricity:     .0001900     
    Arg of perigee:   126.2770  deg
    Mean anomaly:     233.8556  deg
    Mean motion:   15.50871125  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2798
    Checksum:              327
 
 
    Coasting Arc #15 (Orbit 2812)
    ---------------------------------------
 
    Vector Time (GMT): 2014/276/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3715307.92                 A    =         6793928.78  meter
     Y    =        4613400.57  meter          E    =           .0006289
     Z    =       -3330931.89                 I    =           51.29693
     XDOT =      -2640.632634                 Wp   =          103.79261
     YDOT =      -5479.200711  meter/sec      RA   =          282.06575  deg
     ZDOT =      -4652.339713                 TA   =          115.11584
                                              MA   =          115.05057
                                              Ha   =            226.564  n.mi
                                              Hp   =            219.140
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12189330.44                 X    =        -3750439.25
     Y    =       15135828.63  feet           Y    =         4571656.83  meter
     Z    =      -10928254.23                 Z    =        -3349066.16
     XDOT =      -8663.492895                 XDOT =       -2556.567041
     YDOT =     -17976.380284  feet/sec       YDOT =       -5508.260386  meter/sec
     ZDOT =     -15263.581737                 ZDOT =       -4664.962854
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11048296.27                 X    =         3367520.70
     Y    =      -15934234.87  feet           Y    =        -4856754.79  meter
     Z    =      -11006140.74                 Z    =        -3354671.70
     XDOT =       8623.867948                 XDOT =        2628.554951
     YDOT =      16538.833283  feet/sec       YDOT =        5041.036385  meter/sec
     ZDOT =     -15316.329118                 ZDOT =       -4668.417115
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14276.50496170  .00016717  00000-0  10270-3 0  9144
    2 25544  51.6448 282.6809 0001863 133.1427 226.9880 15.50917056 28132
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14276.50496170   =   yrday.fracday
    Element set:     914
    Inclination:       51.6448  deg
    RA of node:       282.6809  deg
    Eccentricity:     .0001863     
    Arg of perigee:   133.1427  deg
    Mean anomaly:     226.9880  deg
    Mean motion:   15.50917056  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2813
    Checksum:              320
 
 
    Coasting Arc #16 (Orbit 2827)
    ---------------------------------------
 
    Vector Time (GMT): 2014/277/11:30:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3604885.77                 A    =         6792409.25  meter
     Y    =       -4317767.18  meter          E    =           .0012934
     Z    =        3799003.20                 I    =           51.28531
     XDOT =       2632.962558                 Wp   =          102.25875
     YDOT =       5874.046837  meter/sec      RA   =          277.08045  deg
     ZDOT =       4162.988677                 TA   =          303.57479
                                              MA   =          303.69820
                                              Ha   =            226.461  n.mi
                                              Hp   =            219.146
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11827053.06                 X    =         3634445.73
     Y    =      -14165902.82  feet           Y    =        -4277289.29  meter
     Z    =       12463921.25                 Z    =         3816587.57
     XDOT =       8638.328603                 XDOT =        2546.859398
     YDOT =      19271.807208  feet/sec       YDOT =        5903.009382  meter/sec
     ZDOT =      13658.099335                 ZDOT =        4175.569452
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10485496.49                 X    =        -3195979.33
     Y    =       15123452.97  feet           Y    =         4609628.47  meter
     Z    =       12539412.00                 Z    =         3822012.78
     XDOT =      -9076.384190                 XDOT =       -2766.481901
     YDOT =     -17700.754343  feet/sec       YDOT =       -5395.189924  meter/sec
     ZDOT =      13710.613260                 ZDOT =        4178.994922
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14277.53591194  .00016717  00000-0  10270-3 0  9151
    2 25544  51.6435 277.5659 0001836 133.9338 226.1965 15.50951021 28285
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14277.53591194   =   yrday.fracday
    Element set:     915
    Inclination:       51.6435  deg
    RA of node:       277.5659  deg
    Eccentricity:     .0001836     
    Arg of perigee:   133.9338  deg
    Mean anomaly:     226.1965  deg
    Mean motion:   15.50951021  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2828
    Checksum:              330
 
             

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