Return to Human Space Flight home page

    
   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  27986.17
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   132.3
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.252
   ET - UTC  (sec) :   67.18
   UT1 - UTC (sec) :    0.00
 
 
   Maneuvers contained within the current ephemeris are as follows:
 
 
   IMPULSIVE TIG (GMT)   M50 DVx(FPS)      LVLH DVx(FPS)      DVmag(FPS) 
   IMPULSIVE TIG (MET)   M50 DVy(FPS)      LVLH DVy(FPS)      Invar Sph HA
   DT                    M50 DVz(FPS)      LVLH DVz(FPS)      Invar Sph HP 
   ------------------------------------------------------------------------
    There are no maneuvers.
 
 
    Coasting Arc #1 (Orbit 3620)
    ---------------------------------------
 
    Vector Time (GMT): 2014/328/13:11:16.604
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1798964.71                 A    =         6788485.39  meter
     Y    =       -4722037.77  meter          E    =           .0016800
     Z    =       -4550085.78                 I    =           51.78818
     XDOT =       6960.062347                 Wp   =           65.82349
     YDOT =        382.880813  meter/sec      RA   =           24.00011  deg
     ZDOT =      -3151.635110                 TA   =          172.56590
                                              MA   =          172.54096
                                              Ha   =            227.713  n.mi
                                              Hp   =            216.574
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5902115.21                 X    =        -1723924.85
     Y    =      -15492249.90  feet           Y    =        -4741735.08  meter
     Z    =      -14928102.95                 Z    =        -4558643.09
     XDOT =      22834.850219                 XDOT =        6970.573484
     YDOT =       1256.170646  feet/sec       YDOT =         460.771723  meter/sec
     ZDOT =     -10340.010205                 ZDOT =       -3117.797970
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16244954.08                 X    =         4951462.00
     Y    =       -3143821.40  feet           Y    =         -958236.76  meter
     Z    =      -14963652.05                 Z    =        -4560921.15
     XDOT =      -5284.169845                 XDOT =       -1610.614969
     YDOT =      21185.421831  feet/sec       YDOT =        6457.316574  meter/sec
     ZDOT =     -10195.785693                 ZDOT =       -3107.675479
  
  
    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   14328.57122376  .00016717  00000-0  10270-3 0  9008
    2 25544  51.6463  24.4416 0006991  61.3984 298.7870 15.51409505 36212
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14328.57122376   =   yrday.fracday
    Element set:     900
    Inclination:       51.6463  deg
    RA of node:        24.4416  deg
    Eccentricity:     .0006991     
    Arg of perigee:    61.3984  deg
    Mean anomaly:     298.7870  deg
    Mean motion:   15.51409505  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3621
    Checksum:              314
 
 
    Coasting Arc #2 (Orbit 3636)
    ---------------------------------------
 
    Vector Time (GMT): 2014/329/13:11:16.604
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1224280.69                 A    =         6786827.06  meter
     Y    =        4514447.17  meter          E    =           .0012111
     Z    =        4907169.75                 I    =           51.75310
     XDOT =      -7286.154407                 Wp   =           91.52416
     YDOT =       -567.649017  meter/sec      RA   =           19.04002  deg
     ZDOT =       2334.741960                 TA   =          335.64885
                                              MA   =          335.70603
                                              Ha   =            227.697  n.mi
                                              Hp   =            216.405
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4016668.92                 X    =         1149870.34
     Y    =       14811178.38  feet           Y    =         4527721.49  meter
     Z    =       16099638.30                 Z    =         4912936.77
     XDOT =     -23904.706061                 XDOT =       -7290.606865
     YDOT =      -1862.365540  feet/sec       YDOT =        -649.152567  meter/sec
     ZDOT =       7659.914567                 ZDOT =        2299.335547
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15231811.47                 X    =        -4642656.14
     Y    =        1653258.34  feet           Y    =          503913.14  meter
     Z    =       16123326.08                 Z    =         4914389.79
     XDOT =       5547.169794                 XDOT =        1690.777353
     YDOT =     -22293.208916  feet/sec       YDOT =       -6794.970078  meter/sec
     ZDOT =       7509.034634                 ZDOT =        2288.753756
  
  
    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   14329.60184007  .00016717  00000-0  10270-3 0  9013
    2 25544  51.6451  19.3245 0007158  64.9126 295.2767 15.51470324 36376
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14329.60184007   =   yrday.fracday
    Element set:     901
    Inclination:       51.6451  deg
    RA of node:        19.3245  deg
    Eccentricity:     .0007158     
    Arg of perigee:    64.9126  deg
    Mean anomaly:     295.2767  deg
    Mean motion:   15.51470324  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3637
    Checksum:              303
 
 
    Coasting Arc #3 (Orbit 3651)
    ---------------------------------------
 
    Vector Time (GMT): 2014/330/13:11:16.604
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -571210.98                 A    =         6785661.62  meter
     Y    =       -4361834.85  meter          E    =           .0020882
     Z    =       -5185150.32                 I    =           51.72061
     XDOT =       7480.133572                 Wp   =           75.12019
     YDOT =        715.612507  meter/sec      RA   =           14.07546  deg
     ZDOT =      -1425.599882                 TA   =          181.14165
                                              MA   =          181.14643
                                              Ha   =            227.669  n.mi
                                              Hp   =            216.311
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1874051.78                 X    =         -497205.46
     Y    =      -14310481.78  feet           Y    =        -4367808.41  meter
     Z    =      -17011648.02                 Z    =        -5187745.70
     XDOT =      24541.120643                 XDOT =        7478.500649
     YDOT =       2347.810061  feet/sec       YDOT =         799.251161  meter/sec
     ZDOT =      -4677.164967                 ZDOT =       -1389.266054
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14419890.57                 X    =         4395182.64
     Y    =         147903.09  feet           Y    =           45080.86  meter
     Z    =      -17021839.14                 Z    =        -5188256.57
     XDOT =      -5575.806658                 XDOT =       -1699.505869
     YDOT =      22989.968539  feet/sec       YDOT =        7007.342411  meter/sec
     ZDOT =      -4522.360604                 ZDOT =       -1378.415512
  
  
    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   14330.56801380  .00016717  00000-0  10270-3 0  9021
    2 25544  51.6463  14.5270 0007113  67.9932 292.1974 15.51497911 36527
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14330.56801380   =   yrday.fracday
    Element set:     902
    Inclination:       51.6463  deg
    RA of node:        14.5270  deg
    Eccentricity:     .0007113     
    Arg of perigee:    67.9932  deg
    Mean anomaly:     292.1974  deg
    Mean motion:   15.51497911  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3652
    Checksum:              302
 
 
    Coasting Arc #4 (Orbit 3667)
    ---------------------------------------
 
    Vector Time (GMT): 2014/331/13:11:16.604
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -136597.23                 A    =         6784868.52  meter
     Y    =        4220911.40  meter          E    =           .0009562
     Z    =        5302075.91                 I    =           51.68671
     XDOT =      -7611.109093                 Wp   =           80.63989
     YDOT =       -840.746365  meter/sec      RA   =            9.10703  deg
     ZDOT =        474.014028                 TA   =            4.84841
                                              MA   =            4.83916
                                              Ha   =            227.677  n.mi
                                              Hp   =            216.119
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -448153.65                 X    =         -209542.23
     Y    =       13848134.51  feet           Y    =         4218975.79  meter
     Z    =       17395262.17                 Z    =         5301235.34
     XDOT =     -24970.830359                 XDOT =       -7603.444616
     YDOT =      -2758.354215  feet/sec       YDOT =        -925.815887  meter/sec
     ZDOT =       1555.164134                 ZDOT =         437.058681
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13692340.16                 X    =        -4173425.28
     Y    =       -2155391.67  feet           Y    =         -656963.38  meter
     Z    =       17390828.75                 Z    =         5300724.60
     XDOT =       5470.519027                 XDOT =        1667.414199
     YDOT =     -23495.310002  feet/sec       YDOT =       -7161.370489  meter/sec
     ZDOT =       1397.737204                 ZDOT =         426.030300
  
  
    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   14331.59856690  .00016717  00000-0  10270-3 0  9030
    2 25544  51.6450   9.4091 0007305  71.5848 288.6097 15.51566420 36682
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14331.59856690   =   yrday.fracday
    Element set:     903
    Inclination:       51.6450  deg
    RA of node:         9.4091  deg
    Eccentricity:     .0007305     
    Arg of perigee:    71.5848  deg
    Mean anomaly:     288.6097  deg
    Mean motion:   15.51566420  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3668
    Checksum:              326
 
 
    Coasting Arc #5 (Orbit 3682)
    ---------------------------------------
 
    Vector Time (GMT): 2014/332/13:11:16.604
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         874280.69                 A    =         6784872.40  meter
     Y    =       -4150928.00  meter          E    =           .0021620
     Z    =       -5313893.74                 I    =           51.65675
     XDOT =       7572.222719                 Wp   =           87.31378
     YDOT =        949.567673  meter/sec      RA   =            4.13629  deg
     ZDOT =        506.860144                 TA   =          187.51700
                                              MA   =          187.54946
                                              Ha   =            227.603  n.mi
                                              Hp   =            216.101
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2868374.97                 X    =          946445.69
     Y    =      -13618530.19  feet           Y    =        -4140747.59  meter
     Z    =      -17434034.59                 Z    =        -5309471.41
     XDOT =      24843.250391                 XDOT =        7558.579467
     YDOT =       3115.379504  feet/sec       YDOT =        1034.168880  meter/sec
     ZDOT =       1662.926981                 ZDOT =         543.612035
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13260474.15                 X    =         4041792.52
     Y    =        4305579.50  feet           Y    =         1312340.63  meter
     Z    =      -17414342.14                 Z    =        -5307891.48
     XDOT =      -5232.577476                 XDOT =       -1594.889615
     YDOT =      23437.608573  feet/sec       YDOT =        7143.783093  meter/sec
     ZDOT =       1819.459341                 ZDOT =         554.571207
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14332.56468139  .00016717  00000-0  10270-3 0  9046
    2 25544  51.6460   4.6117 0007215  74.4589 285.7359 15.51587131 36831
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14332.56468139   =   yrday.fracday
    Element set:     904
    Inclination:       51.6460  deg
    RA of node:         4.6117  deg
    Eccentricity:     .0007215     
    Arg of perigee:    74.4589  deg
    Mean anomaly:     285.7359  deg
    Mean motion:   15.51587131  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3683
    Checksum:              321
 
 
    Coasting Arc #6 (Orbit 3698)
    ---------------------------------------
 
    Vector Time (GMT): 2014/333/13:11:16.604
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1637717.36                 A    =         6785327.31  meter
     Y    =        4098482.07  meter          E    =           .0011928
     Z    =        5145119.75                 I    =           51.62645
     XDOT =      -7445.407737                 Wp   =           68.38985
     YDOT =      -1080.633700  meter/sec      RA   =          359.16250  deg
     ZDOT =      -1502.004019                 TA   =           36.11169
                                              MA   =           36.03119
                                              Ha   =            227.608  n.mi
                                              Hp   =            215.896
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5373088.45                 X    =        -1708419.34
     Y    =       13446463.48  feet           Y    =         4079772.67  meter
     Z    =       16880314.13                 Z    =         5136992.21
     XDOT =     -24427.190739                 XDOT =       -7425.474171
     YDOT =      -3545.386154  feet/sec       YDOT =       -1163.781604  meter/sec
     ZDOT =      -4927.834708                 ZDOT =       -1538.124623
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12957493.02                 X    =        -3949443.87
     Y    =       -6555714.78  feet           Y    =        -1998181.87  meter
     Z    =       16844834.31                 Z    =         5134305.50
     XDOT =       5041.224819                 XDOT =        1536.565325
     YDOT =     -23081.266416  feet/sec       YDOT =       -7035.170004  meter/sec
     ZDOT =      -5081.641612                 ZDOT =       -1548.884363
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14333.59517190  .00016717  00000-0  10270-3 0  9053
    2 25544  51.6448 359.4933 0007348  78.0935 282.1039 15.51662523 36998
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14333.59517190   =   yrday.fracday
    Element set:     905
    Inclination:       51.6448  deg
    RA of node:       359.4933  deg
    Eccentricity:     .0007348     
    Arg of perigee:    78.0935  deg
    Mean anomaly:     282.1039  deg
    Mean motion:   15.51662523  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3699
    Checksum:              335
 
 
    Coasting Arc #7 (Orbit 3713)
    ---------------------------------------
 
    Vector Time (GMT): 2014/334/13:11:16.604
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2370453.98                 A    =         6786562.88  meter
     Y    =       -4116263.03  meter          E    =           .0018443
     Z    =       -4863874.92                 I    =           51.59971
     XDOT =       7143.014586                 Wp   =           97.01835
     YDOT =       1225.102284  meter/sec      RA   =          354.18882  deg
     ZDOT =       2450.218232                 TA   =          197.07242
                                              MA   =          197.13455
                                              Ha   =            227.525  n.mi
                                              Hp   =            215.916
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7777079.99                 X    =         2439934.20
     Y    =      -13504799.98  feet           Y    =        -4089366.56  meter
     Z    =      -15957594.89                 Z    =        -4852190.74
     XDOT =      23435.087225                 XDOT =        7116.881823
     YDOT =       4019.364448  feet/sec       YDOT =        1304.833972  meter/sec
     ZDOT =       8038.773728                 ZDOT =        2484.854884
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12972470.59                 X    =         3954009.03
     Y    =        8728769.97  feet           Y    =         2660529.09  meter
     Z    =      -15906948.55                 Z    =        -4848437.92
     XDOT =      -4876.974241                 XDOT =       -1486.501749
     YDOT =      22131.463710  feet/sec       YDOT =        6745.670139  meter/sec
     ZDOT =       8186.215604                 ZDOT =        2495.158516
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14334.56122790  .00016717  00000-0  10270-3 0  9060
    2 25544  51.6451 354.6958 0007309  80.9581 279.2398 15.51677244 37141
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14334.56122790   =   yrday.fracday
    Element set:     906
    Inclination:       51.6451  deg
    RA of node:       354.6958  deg
    Eccentricity:     .0007309     
    Arg of perigee:    80.9581  deg
    Mean anomaly:     279.2398  deg
    Mean motion:   15.51677244  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3714
    Checksum:              335
 
 
    Coasting Arc #8 (Orbit 3729)
    ---------------------------------------
 
    Vector Time (GMT): 2014/335/13:11:16.604
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3091593.36                 A    =         6788115.72  meter
     Y    =        4137127.75  meter          E    =           .0016712
     Z    =        4393334.78                 I    =           51.57350
     XDOT =      -6738.726683                 Wp   =           76.30616
     YDOT =      -1439.371796  meter/sec      RA   =          349.21327  deg
     ZDOT =      -3371.952376                 TA   =           47.89424
                                              MA   =           47.75228
                                              Ha   =            227.475  n.mi
                                              Hp   =            215.724
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10143022.83                 X    =        -3158967.61
     Y    =       13573253.78  feet           Y    =         4102178.79  meter
     Z    =       14413828.02                 Z    =         4378152.45
     XDOT =     -22108.683344                 XDOT =       -6705.750365
     YDOT =      -4722.348413  feet/sec       YDOT =       -1514.544189  meter/sec
     ZDOT =     -11062.835879                 ZDOT =       -3404.608530
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13078095.01                 X    =        -3986203.36
     Y    =      -10861090.55  feet           Y    =        -3310460.40  meter
     Z    =       14348265.10                 Z    =         4373351.20
     XDOT =       4962.889187                 XDOT =        1512.688624
     YDOT =     -20838.119701  feet/sec       YDOT =       -6351.458885  meter/sec
     ZDOT =     -11201.781883                 ZDOT =       -3414.303118
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14335.59165581  .00016717  00000-0  10270-3 0  9070
    2 25544  51.6440 349.5768 0007327  84.4443 275.7544 15.51761155 37304
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14335.59165581   =   yrday.fracday
    Element set:     907
    Inclination:       51.6440  deg
    RA of node:       349.5768  deg
    Eccentricity:     .0007327     
    Arg of perigee:    84.4443  deg
    Mean anomaly:     275.7544  deg
    Mean motion:   15.51761155  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3730
    Checksum:              328
 
 
    Coasting Arc #9 (Orbit 3744)
    ---------------------------------------
 
    Vector Time (GMT): 2014/336/13:11:16.604
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3722395.83                 A    =         6790081.14  meter
     Y    =       -4207460.65  meter          E    =           .0013330
     Z    =       -3826317.50                 I    =           51.54936
     XDOT =       6190.139777                 Wp   =           94.27432
     YDOT =       1694.076212  meter/sec      RA   =          344.23943  deg
     ZDOT =       4170.798306                 TA   =          219.76856
                                              MA   =          219.86635
                                              Ha   =            227.435  n.mi
                                              Hp   =            215.713
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12212584.75                 X    =         3787755.31
     Y    =      -13804004.77  feet           Y    =        -4165468.87  meter
     Z    =      -12553535.11                 Z    =        -3808075.67
     XDOT =      20308.857537                 XDOT =        6150.475423
     YDOT =       5557.992822  feet/sec       YDOT =        1763.076493  meter/sec
     ZDOT =      13683.721475                 ZDOT =        4200.773326
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13432032.78                 X    =         4094083.59
     Y    =       12698266.50  feet           Y    =         3870431.63  meter
     Z    =      -12474916.47                 Z    =        -3802354.54
     XDOT =      -5234.507036                 XDOT =       -1595.477745
     YDOT =      19067.592158  feet/sec       YDOT =        5811.802090  meter/sec
     ZDOT =      13811.177848                 ZDOT =        4209.647008
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14336.55765351  .00016717  00000-0  10270-3 0  9089
    2 25544  51.6438 344.7789 0007414  87.6208 272.5792 15.51773252 37459
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14336.55765351   =   yrday.fracday
    Element set:     908
    Inclination:       51.6438  deg
    RA of node:       344.7789  deg
    Eccentricity:     .0007414     
    Arg of perigee:    87.6208  deg
    Mean anomaly:     272.5792  deg
    Mean motion:   15.51773252  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3745
    Checksum:              342
 
 
    Coasting Arc #10 (Orbit 3760)
    ---------------------------------------
 
    Vector Time (GMT): 2014/337/13:11:16.604
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4303664.90                 A    =         6791999.67  meter
     Y    =        4244685.24  meter          E    =           .0020357
     Z    =        3077933.58                 I    =           51.52596
     XDOT =      -5542.404214                 Wp   =           93.71555
     YDOT =      -2055.504221  meter/sec      RA   =          339.26470  deg
     ZDOT =      -4888.225022                 TA   =           50.86280
                                              MA   =           50.68204
                                              Ha   =            227.301  n.mi
                                              Hp   =            215.573
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14119635.50                 X    =        -4365761.97
     Y    =       13926132.68  feet           Y    =         4196211.54  meter
     Z    =       10098207.29                 Z    =         3056875.96
     XDOT =     -18183.740860                 XDOT =       -5495.261316
     YDOT =      -6743.780251  feet/sec       YDOT =       -2117.219185  meter/sec
     ZDOT =     -16037.483668                 ZDOT =       -4915.035293
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13746429.82                 X    =        -4189911.81
     Y    =      -14358241.82  feet           Y    =        -4376392.11  meter
     Z    =       10007578.51                 Z    =         3050309.93
     XDOT =       5926.538008                 XDOT =        1806.408785
     YDOT =     -16992.889558  feet/sec       YDOT =       -5179.432737  meter/sec
     ZDOT =     -16151.369526                 ZDOT =       -4922.937432
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14337.58801866  .00016717  00000-0  10270-3 0  9096
    2 25544  51.6432 339.6592 0007324  90.7758 269.4233 15.51859336 37614
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14337.58801866   =   yrday.fracday
    Element set:     909
    Inclination:       51.6432  deg
    RA of node:       339.6592  deg
    Eccentricity:     .0007324     
    Arg of perigee:    90.7758  deg
    Mean anomaly:     269.4233  deg
    Mean motion:   15.51859336  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3761
    Checksum:              344
 
 
    Coasting Arc #11 (Orbit 3775)
    ---------------------------------------
 
    Vector Time (GMT): 2014/338/13:11:16.604
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4750431.83                 A    =         6793724.46  meter
     Y    =       -4293591.80  meter          E    =           .0012210
     Z    =       -2273091.15                 I    =           51.50269
     XDOT =       4812.678805                 Wp   =           71.78807
     YDOT =       2469.034194  meter/sec      RA   =          334.29193  deg
     ZDOT =       5421.841193                 TA   =          262.90620
                                              MA   =          263.04506
                                              Ha   =            227.300  n.mi
                                              Hp   =            215.476
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15585406.26                 X    =         4809132.84
     Y    =      -14086587.27  feet           Y    =        -4240141.04  meter
     Z    =       -7457648.13                 Z    =        -2249871.50
     XDOT =      15789.628626                 XDOT =        4758.373789
     YDOT =       8100.505885  feet/sec       YDOT =        2522.548729  meter/sec
     ZDOT =      17788.192890                 ZDOT =        5445.089150
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14158177.40                 X    =         4315412.47
     Y    =       15567987.35  feet           Y    =         4745122.55  meter
     Z    =       -7357793.64                 Z    =        -2242655.50
     XDOT =      -6895.554913                 XDOT =       -2101.765137
     YDOT =      14681.224897  feet/sec       YDOT =        4474.837348  meter/sec
     ZDOT =      17886.805453                 ZDOT =        5451.898302
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14338.55395752  .00016717  00000-0  10270-3 0  9108
    2 25544  51.6428 334.8606 0007513  94.8822 265.3188 15.51885387 37764
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14338.55395752   =   yrday.fracday
    Element set:     910
    Inclination:       51.6428  deg
    RA of node:       334.8606  deg
    Eccentricity:     .0007513     
    Arg of perigee:    94.8822  deg
    Mean anomaly:     265.3188  deg
    Mean motion:   15.51885387  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3776
    Checksum:              346
 
 
    Coasting Arc #12 (Orbit 3791)
    ---------------------------------------
 
    Vector Time (GMT): 2014/339/13:11:16.604
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5118907.13                 A    =         6794982.81  meter
     Y    =        4256563.76  meter          E    =           .0020728
     Z    =        1317428.80                 I    =           51.47987
     XDOT =      -4006.733869                 Wp   =          112.35307
     YDOT =      -3000.036944  meter/sec      RA   =          329.31823  deg
     ZDOT =      -5809.715147                 TA   =           53.28085
                                              MA   =           53.09063
                                              Ha   =            227.122  n.mi
                                              Hp   =            215.434
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16794314.72                 X    =        -5172524.30
     Y    =       13965104.19  feet           Y    =         4199020.93  meter
     Z    =        4322272.96                 Z    =         1292431.59
     XDOT =     -13145.452326                 XDOT =       -3944.666819
     YDOT =      -9842.640894  feet/sec       YDOT =       -3044.495362  meter/sec
     ZDOT =     -19060.745234                 ZDOT =       -5829.029056
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14327990.51                 X    =        -4367171.51
     Y    =      -16513598.15  feet           Y    =        -5033344.72  meter
     Z    =        4214848.73                 Z    =         1284685.89
     XDOT =       8354.633087                 XDOT =        2546.492165
     YDOT =     -12191.005684  feet/sec       YDOT =       -3715.818533  meter/sec
     ZDOT =     -19142.478527                 ZDOT =       -5834.627455
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14339.58425982  .00016717  00000-0  10270-3 0  9112
    2 25544  51.6430 329.7402 0007365  97.6799 262.5190 15.51947914 37928
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14339.58425982   =   yrday.fracday
    Element set:     911
    Inclination:       51.6430  deg
    RA of node:       329.7402  deg
    Eccentricity:     .0007365     
    Arg of perigee:    97.6799  deg
    Mean anomaly:     262.5190  deg
    Mean motion:   15.51947914  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3792
    Checksum:              344
 
 
    Coasting Arc #13 (Orbit 3806)
    ---------------------------------------
 
    Vector Time (GMT): 2014/340/13:11:16.604
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5335662.13                 A    =         6795461.76  meter
     Y    =       -4185934.30  meter          E    =           .0016502
     Z    =        -365377.72                 I    =           51.45538
     XDOT =       3195.833454                 Wp   =           65.60182
     YDOT =       3570.850724  meter/sec      RA   =          324.34524  deg
     ZDOT =       5980.010975                 TA   =          290.45392
                                              MA   =          290.63102
                                              Ha   =            227.076  n.mi
                                              Hp   =            215.291
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17505453.18                 X    =         5383848.57
     Y    =      -13733380.26  feet           Y    =        -4125998.01  meter
     Z    =       -1198745.82                 Z    =         -339340.86
     XDOT =      10485.017894                 XDOT =        3126.616541
     YDOT =      11715.389513  feet/sec       YDOT =        3606.201061  meter/sec
     ZDOT =      19619.458579                 ZDOT =        5995.368257
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14405015.52                 X    =         4390648.73
     Y    =       16964603.82  feet           Y    =         5170811.24  meter
     Z    =       -1086904.37                 Z    =         -331288.45
     XDOT =     -10067.772641                 XDOT =       -3068.657101
     YDOT =       9758.885272  feet/sec       YDOT =        2974.508231  meter/sec
     ZDOT =      19684.210550                 ZDOT =        5999.747376
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14340.55013890  .00016717  00000-0  10270-3 0  9123
    2 25544  51.6428 324.9413 0007499 102.7050 257.4940 15.52003862 38079
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14340.55013890   =   yrday.fracday
    Element set:     912
    Inclination:       51.6428  deg
    RA of node:       324.9413  deg
    Eccentricity:     .0007499     
    Arg of perigee:   102.7050  deg
    Mean anomaly:     257.4940  deg
    Mean motion:   15.52003862  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3807
    Checksum:              296
 
 
    Coasting Arc #14 (Orbit 3822)
    ---------------------------------------
 
    Vector Time (GMT): 2014/341/13:11:16.604
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5463979.18                 A    =         6795204.48  meter
     Y    =        3972676.68  meter          E    =           .0017063
     Z    =        -680967.36                 I    =           51.43095
     XDOT =      -2349.218931                 Wp   =          125.24750
     YDOT =      -4230.332413  meter/sec      RA   =          319.36997  deg
     ZDOT =      -5944.620079                 TA   =           62.12246
                                              MA   =           61.94973
                                              Ha   =            226.918  n.mi
                                              Hp   =            215.320
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17926440.89                 X    =        -5504688.54
     Y    =       13033716.13  feet           Y    =         3911347.37  meter
     Z    =       -2234144.89                 Z    =         -707609.31
     XDOT =      -7707.411190                 XDOT =       -2272.862494
     YDOT =     -13879.043349  feet/sec       YDOT =       -4256.175401  meter/sec
     ZDOT =     -19503.346716                 ZDOT =       -5955.847280
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14018231.31                 X    =        -4272756.90
     Y    =      -17152261.62  feet           Y    =        -5228009.34  meter
     Z    =       -2348521.80                 Z    =         -715829.44
     XDOT =      12182.558375                 XDOT =        3713.243793
     YDOT =      -7328.929229  feet/sec       YDOT =       -2233.857629  meter/sec
     ZDOT =     -19550.362246                 ZDOT =       -5958.950413
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14341.58037776  .00016717  00000-0  10270-3 0  9137
    2 25544  51.6439 319.8208 0007361 105.2018 254.9948 15.52034441 38231
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14341.58037776   =   yrday.fracday
    Element set:     913
    Inclination:       51.6439  deg
    RA of node:       319.8208  deg
    Eccentricity:     .0007361     
    Arg of perigee:   105.2018  deg
    Mean anomaly:     254.9948  deg
    Mean motion:   15.52034441  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3823
    Checksum:              312
 
 
    Coasting Arc #15 (Orbit 3838)
    ---------------------------------------
 
    Vector Time (GMT): 2014/342/13:11:16.604
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5454345.82                 A    =         6794029.89  meter
     Y    =       -3686891.97  meter          E    =           .0019799
     Z    =        1651555.32                 I    =           51.40457
     XDOT =       1567.226104                 Wp   =           79.39018
     YDOT =       4892.401490  meter/sec      RA   =          314.39284  deg
     ZDOT =       5691.191243                 TA   =          298.74886
                                              MA   =          298.94763
                                              Ha   =            226.811  n.mi
                                              Hp   =            215.218
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17894835.37                 X    =         5487145.37
     Y    =      -12096102.25  feet           Y    =        -3625714.70  meter
     Z    =        5418488.58                 Z    =         1678131.19
     XDOT =       5141.817926                 XDOT =        1484.755567
     YDOT =      16051.185992  feet/sec       YDOT =        4909.465573  meter/sec
     ZDOT =      18671.887279                 ZDOT =        5698.604782
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13372024.11                 X    =         4075792.95
     Y    =       16925749.17  feet           Y    =         5158968.35  meter
     Z    =        5532524.51                 Z    =         1686313.47
     XDOT =     -14407.303037                 XDOT =       -4391.345966
     YDOT =       5211.661487  feet/sec       YDOT =        1588.514421  meter/sec
     ZDOT =      18702.517196                 ZDOT =        5700.527241
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14342.61058279  .00016717  00000-0  10270-3 0  9144
    2 25544  51.6439 314.7016 0007396 110.2632 249.9315 15.52101772 38399
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14342.61058279   =   yrday.fracday
    Element set:     914
    Inclination:       51.6439  deg
    RA of node:       314.7016  deg
    Eccentricity:     .0007396     
    Arg of perigee:   110.2632  deg
    Mean anomaly:     249.9315  deg
    Mean motion:   15.52101772  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3839
    Checksum:              307
 
             

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