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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  7534.74
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   124.9
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.730
   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 3462)
    ---------------------------------------
 
    Vector Time (GMT): 2015/210/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 906095.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4065241.85                 A    =         6775423.45  meter
     Y    =       -1553314.71  meter          E    =           .0004686
     Z    =        5190508.11                 I    =           51.33215
     XDOT =       3944.420440                 Wp   =           48.23806
     YDOT =       6480.060125  meter/sec      RA   =          231.72577  deg
     ZDOT =      -1146.333889                 TA   =           52.81566
                                              MA   =           52.77289
                                              Ha   =            219.726  n.mi
                                              Hp   =            213.297
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13337407.66                 X    =         4057096.14
     Y    =       -5096176.88  feet           Y    =        -1507900.47  meter
     Z    =       17029226.09                 Z    =         5210236.03
     XDOT =      12941.011941                 XDOT =        3877.234058
     YDOT =      21260.039781  feet/sec       YDOT =        6523.793651  meter/sec
     ZDOT =      -3760.937955                 ZDOT =       -1127.335653
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11894834.16                 X    =        -3625545.45
     Y    =       -7711236.50  feet           Y    =        -2350384.88  meter
     Z    =       17114372.76                 Z    =         5216460.82
     XDOT =       9023.648527                 XDOT =        2750.408071
     YDOT =     -22114.524577  feet/sec       YDOT =       -6740.507091  meter/sec
     ZDOT =      -3680.342913                 ZDOT =       -1121.768520
  
  
    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   15210.54630617  .00016717  00000-0  10270-3 0  9008
    2 25544  51.6412 232.5206 0001041  14.5956 345.5227 15.54932361 34630
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15210.54630617   =   yrday.fracday
    Element set:     900
    Inclination:       51.6412  deg
    RA of node:       232.5206  deg
    Eccentricity:     .0001041     
    Arg of perigee:    14.5956  deg
    Mean anomaly:     345.5227  deg
    Mean motion:   15.54932361  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3463
    Checksum:              272
 
 
    Coasting Arc #2 (Orbit 3477)
    ---------------------------------------
 
    Vector Time (GMT): 2015/211/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 906095.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5098379.36                 A    =         6778441.69  meter
     Y    =        -198366.30  meter          E    =           .0009496
     Z    =       -4471829.19                 I    =           51.36322
     XDOT =      -2563.554580                 Wp   =          104.00273
     YDOT =      -6465.517711  meter/sec      RA   =          226.70154  deg
     ZDOT =       3213.036812                 TA   =          198.45219
                                              MA   =          198.48666
                                              Ha   =            219.859  n.mi
                                              Hp   =            213.194
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16726966.41                 X    =        -5074060.24
     Y    =        -650808.08  feet           Y    =         -255243.46  meter
     Z    =      -14671355.61                 Z    =        -4496536.57
     XDOT =      -8410.612140                 XDOT =       -2506.672484
     YDOT =     -21212.328448  feet/sec       YDOT =       -6493.867220  meter/sec
     ZDOT =      10541.459357                 ZDOT =        3200.721559
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9481608.55                 X    =         2889994.29
     Y    =       13681534.07  feet           Y    =         4170131.58  meter
     Z    =      -14777630.27                 Z    =        -4504221.71
     XDOT =     -10851.330855                 XDOT =       -3307.485645
     YDOT =      18837.879969  feet/sec       YDOT =        5741.785815  meter/sec
     ZDOT =      10489.594044                 ZDOT =        3197.228265
  
  
    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   15211.51034084  .00016717  00000-0  10270-3 0  9013
    2 25544  51.6418 227.7090 0001129  11.9170 348.2009 15.54916617 34789
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15211.51034084   =   yrday.fracday
    Element set:     901
    Inclination:       51.6418  deg
    RA of node:       227.7090  deg
    Eccentricity:     .0001129     
    Arg of perigee:    11.9170  deg
    Mean anomaly:     348.2009  deg
    Mean motion:   15.54916617  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3478
    Checksum:              286
 
 
    Coasting Arc #3 (Orbit 3493)
    ---------------------------------------
 
    Vector Time (GMT): 2015/212/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 906095.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5749216.76                 A    =         6782707.58  meter
     Y    =        1803433.43  meter          E    =           .0013268
     Z    =        3102890.81                 I    =           51.39894
     XDOT =        783.175927                 Wp   =           89.84225
     YDOT =       5888.179412  meter/sec      RA   =          221.69018  deg
     ZDOT =      -4855.345736                 TA   =           54.29660
                                              MA   =           54.17320
                                              Ha   =            219.788  n.mi
                                              Hp   =            213.160
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18862259.73                 X    =         5713550.71
     Y    =        5916776.34  feet           Y    =         1867525.39  meter
     Z    =       10180087.96                 Z    =         3130732.20
     XDOT =       2569.474825                 XDOT =         740.859586
     YDOT =      19318.173925  feet/sec       YDOT =        5896.701004  meter/sec
     ZDOT =     -15929.611994                 ZDOT =       -4851.643833
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6894466.58                 X    =        -2101433.41
     Y    =      -18461097.71  feet           Y    =        -5626942.58  meter
     Z    =       10299586.26                 Z    =         3139313.89
     XDOT =      12242.420968                 XDOT =        3731.489911
     YDOT =     -13483.612031  feet/sec       YDOT =       -4109.804947  meter/sec
     ZDOT =     -15914.692885                 ZDOT =       -4850.798391
  
  
    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   15212.53863657  .00016717  00000-0  10270-3 0  9023
    2 25544  51.6403 222.5754 0001217  18.3157 341.8039 15.54967928 34948
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15212.53863657   =   yrday.fracday
    Element set:     902
    Inclination:       51.6403  deg
    RA of node:       222.5754  deg
    Eccentricity:     .0001217     
    Arg of perigee:    18.3157  deg
    Mean anomaly:     341.8039  deg
    Mean motion:   15.54967928  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3494
    Checksum:              315
 
 
    Coasting Arc #4 (Orbit 3508)
    ---------------------------------------
 
    Vector Time (GMT): 2015/213/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 906095.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5897167.31                 A    =         6786013.06  meter
     Y    =       -3075004.12  meter          E    =           .0009761
     Z    =       -1327252.37                 I    =           51.43505
     XDOT =       1231.787482                 Wp   =           36.88762
     YDOT =      -4855.645897  meter/sec      RA   =          216.69451  deg
     ZDOT =       5806.517010                 TA   =          308.61744
                                              MA   =          308.70479
                                              Ha   =            219.801  n.mi
                                              Hp   =            213.090
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19347661.78                 X    =        -5855896.44
     Y    =      -10088596.19  feet           Y    =        -3140719.33  meter
     Z    =       -4354502.53                 Z    =        -1355798.82
     XDOT =       4041.297513                 XDOT =        1257.787710
     YDOT =     -15930.596774  feet/sec       YDOT =       -4841.725979  meter/sec
     ZDOT =      19050.252659                 ZDOT =        5812.563711
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4294945.49                 X    =         1309099.39
     Y    =       21367846.49  feet           Y    =         6512919.61  meter
     Z    =       -4476836.09                 Z    =        -1364539.64
     XDOT =     -13295.015864                 XDOT =       -4052.320835
     YDOT =       6649.230768  feet/sec       YDOT =        2026.685538  meter/sec
     ZDOT =      19077.099348                 ZDOT =        5814.699881
  
  
    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   15213.50265760  .00016717  00000-0  10270-3 0  9033
    2 25544  51.6407 217.7638 0001078  27.4510 332.6700 15.54996520 35098
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15213.50265760   =   yrday.fracday
    Element set:     903
    Inclination:       51.6407  deg
    RA of node:       217.7638  deg
    Eccentricity:     .0001078     
    Arg of perigee:    27.4510  deg
    Mean anomaly:     332.6700  deg
    Mean motion:   15.54996520  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3509
    Checksum:              295
 
 
    Coasting Arc #5 (Orbit 3524)
    ---------------------------------------
 
    Vector Time (GMT): 2015/214/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 906095.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5441095.48                 A    =         6786729.54  meter
     Y    =        3992903.81  meter          E    =           .0010251
     Z    =        -674626.09                 I    =           51.46224
     XDOT =      -3315.035581                 Wp   =          133.47295
     YDOT =       3522.837094  meter/sec      RA   =          211.70611  deg
     ZDOT =      -5950.101261                 TA   =           53.83254
                                              MA   =           53.73774
                                              Ha   =            219.938  n.mi
                                              Hp   =            213.143
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17851363.12                 X    =         5399318.49
     Y    =       13100078.11  feet           Y    =         4053516.12  meter
     Z    =       -2213340.18                 Z    =         -648296.34
     XDOT =     -10876.100989                 XDOT =       -3325.279672
     YDOT =      11557.864483  feet/sec       YDOT =        3485.708907  meter/sec
     ZDOT =     -19521.329598                 ZDOT =       -5966.229600
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1419462.52                 X    =         -432652.18
     Y    =      -22107789.11  feet           Y    =        -6738454.12  meter
     Z    =       -2100683.98                 Z    =         -640288.48
     XDOT =      14150.140034                 XDOT =        4312.962682
     YDOT =        932.095692  feet/sec       YDOT =         284.102767  meter/sec
     ZDOT =     -19591.338505                 ZDOT =       -5971.439976
  
  
    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   15214.53093926  .00016717  00000-0  10270-3 0  9041
    2 25544  51.6399 212.6298 0001243  25.4261 334.6953 15.54962525 35257
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15214.53093926   =   yrday.fracday
    Element set:     904
    Inclination:       51.6399  deg
    RA of node:       212.6298  deg
    Eccentricity:     .0001243     
    Arg of perigee:    25.4261  deg
    Mean anomaly:     334.6953  deg
    Mean motion:   15.54962525  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3525
    Checksum:              312
 
 
    Coasting Arc #6 (Orbit 3540)
    ---------------------------------------
 
    Vector Time (GMT): 2015/215/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 906095.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4394457.18                 A    =         6784078.59  meter
     Y    =       -4484613.19  meter          E    =           .0014379
     Z    =        2550492.76                 I    =           51.48133
     XDOT =       5185.305251                 Wp   =           72.47190
     YDOT =      -2077.782093  meter/sec      RA   =          206.71737  deg
     ZDOT =       5260.523246                 TA   =          316.27944
                                              MA   =          316.39324
                                              Ha   =            219.839  n.mi
                                              Hp   =            213.147
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14417510.45                 X    =        -4356371.67
     Y    =      -14713297.87  feet           Y    =        -4533541.91  meter
     Z    =        8367758.41                 Z    =         2529238.30
     XDOT =      17012.156334                 XDOT =        5182.600935
     YDOT =      -6816.870384  feet/sec       YDOT =       -2019.811650  meter/sec
     ZDOT =      17258.934533                 ZDOT =        5285.705462
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1642220.63                 X    =         -500548.85
     Y    =       20570835.29  feet           Y    =         6269990.60  meter
     Z    =        8277014.50                 Z    =         2522834.02
     XDOT =     -14719.127846                 XDOT =       -4486.390167
     YDOT =      -8190.249153  feet/sec       YDOT =       -2496.387942  meter/sec
     ZDOT =      17367.676278                 ZDOT =        5293.667729
  
  
    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   15215.55921134  .00016717  00000-0  10270-3 0  9056
    2 25544  51.6400 207.4973 0001131  21.6310 338.4891 15.55006762 35415
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15215.55921134   =   yrday.fracday
    Element set:     905
    Inclination:       51.6400  deg
    RA of node:       207.4973  deg
    Eccentricity:     .0001131     
    Arg of perigee:    21.6310  deg
    Mean anomaly:     338.4891  deg
    Mean motion:   15.55006762  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3541
    Checksum:              275
 
 
    Coasting Arc #7 (Orbit 3555)
    ---------------------------------------
 
    Vector Time (GMT): 2015/216/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 906095.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2795996.96                 A    =         6779791.80  meter
     Y    =        4625982.67  meter          E    =           .0008332
     Z    =       -4101499.18                 I    =           51.49538
     XDOT =      -6618.157674                 Wp   =           65.50330
     YDOT =        625.590078  meter/sec      RA   =          201.71755  deg
     ZDOT =      -3808.740990                 TA   =          165.06949
                                              MA   =          165.04488
                                              Ha   =            219.937  n.mi
                                              Hp   =            213.139
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9173218.37                 X    =         2763983.57
     Y    =       15177108.50  feet           Y    =         4657070.27  meter
     Z    =      -13456362.14                 Z    =        -4087994.80
     XDOT =     -21713.115727                 XDOT =       -6606.160119
     YDOT =       2052.460885  feet/sec       YDOT =         551.648505  meter/sec
     ZDOT =     -12495.869390                 ZDOT =       -3840.861138
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5113340.43                 X    =         1558546.16
     Y    =      -17026068.25  feet           Y    =        -5189545.60  meter
     Z    =      -13398992.10                 Z    =        -4084012.79
     XDOT =      14731.513995                 XDOT =        4490.165466
     YDOT =      14359.932177  feet/sec       YDOT =        4376.907327  meter/sec
     ZDOT =     -12634.245266                 ZDOT =       -3850.917957
  
  
    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   15216.52321221  .00016717  00000-0  10270-3 0  9066
    2 25544  51.6398 202.6842 0001313  28.0350 332.0873 15.54978097 35564
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15216.52321221   =   yrday.fracday
    Element set:     906
    Inclination:       51.6398  deg
    RA of node:       202.6842  deg
    Eccentricity:     .0001313     
    Arg of perigee:    28.0350  deg
    Mean anomaly:     332.0873  deg
    Mean motion:   15.54978097  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3556
    Checksum:              294
 
 
    Coasting Arc #8 (Orbit 3571)
    ---------------------------------------
 
    Vector Time (GMT): 2015/217/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 906095.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -827230.24                 A    =         6775980.65  meter
     Y    =       -4438980.37  meter          E    =           .0005524
     Z    =        5048309.76                 I    =           51.51272
     XDOT =       7417.650841                 Wp   =          110.85172
     YDOT =        705.462271  meter/sec      RA   =          196.70733  deg
     ZDOT =       1832.241537                 TA   =          321.36650
                                              MA   =          321.40600
                                              Ha   =            219.890  n.mi
                                              Hp   =            213.085
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2714009.97                 X    =         -802053.55
     Y    =      -14563583.89  feet           Y    =        -4448090.16  meter
     Z    =       16562696.06                 Z    =         5044352.48
     XDOT =      24336.124807                 XDOT =        7400.310648
     YDOT =       2314.508762  feet/sec       YDOT =         788.314382  meter/sec
     ZDOT =       6011.291132                 ZDOT =        1868.232540
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8751790.43                 X    =        -2667545.72
     Y    =       11975385.98  feet           Y    =         3650097.65  meter
     Z    =       16546389.98                 Z    =         5043339.67
     XDOT =     -13964.406767                 XDOT =       -4256.351182
     YDOT =     -18741.234459  feet/sec       YDOT =       -5712.328263  meter/sec
     ZDOT =       6166.125369                 ZDOT =        1879.435013
  
  
    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   15217.55147021  .00016717  00000-0  10270-3 0  9075
    2 25544  51.6397 197.5515 0001351  24.0162 336.1054 15.54999774 35720
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15217.55147021   =   yrday.fracday
    Element set:     907
    Inclination:       51.6397  deg
    RA of node:       197.5515  deg
    Eccentricity:     .0001351     
    Arg of perigee:    24.0162  deg
    Mean anomaly:     336.1054  deg
    Mean motion:   15.54999774  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3572
    Checksum:              309
 
 
    Coasting Arc #9 (Orbit 3586)
    ---------------------------------------
 
    Vector Time (GMT): 2015/218/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 906095.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1314848.56                 A    =         6774873.13  meter
     Y    =        4027182.81  meter          E    =           .0015503
     Z    =       -5300348.99                 I    =           51.53991
     XDOT =      -7414.290653                 Wp   =           88.73906
     YDOT =      -1872.869291  meter/sec      RA   =          191.69023  deg
     ZDOT =        417.644186                 TA   =          185.24626
                                              MA   =          185.26252
                                              Ha   =            219.934  n.mi
                                              Hp   =            212.966
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4313807.61                 X    =        -1334036.87
     Y    =       13212542.02  feet           Y    =         4012372.02  meter
     Z    =      -17389596.42                 Z    =        -5306782.82
     XDOT =     -24325.100568                 XDOT =       -7394.825474
     YDOT =      -6144.584289  feet/sec       YDOT =       -1955.671921  meter/sec
     ZDOT =       1370.223708                 ZDOT =         381.674585
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12436892.82                 X    =         3790764.93
     Y    =       -6125079.32  feet           Y    =        -1866924.18  meter
     Z    =      -17417961.04                 Z    =        -5308994.52
     XDOT =      11986.367889                 XDOT =        3653.444933
     YDOT =      20894.148076  feet/sec       YDOT =        6368.536334  meter/sec
     ZDOT =       1215.657214                 ZDOT =         370.532319
  
  
    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   15218.51545494  .00016717  00000-0  10270-3 0  9089
    2 25544  51.6398 192.7391 0001395  30.2522 329.8711 15.54997874 35871
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15218.51545494   =   yrday.fracday
    Element set:     908
    Inclination:       51.6398  deg
    RA of node:       192.7391  deg
    Eccentricity:     .0001395     
    Arg of perigee:    30.2522  deg
    Mean anomaly:     329.8711  deg
    Mean motion:   15.54997874  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3587
    Checksum:              344
 
 
    Coasting Arc #10 (Orbit 3602)
    ---------------------------------------
 
    Vector Time (GMT): 2015/219/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 906095.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3376227.21                 A    =         6776936.27  meter
     Y    =       -3418342.81  meter          E    =           .0008586
     Z    =        4775241.98                 I    =           51.57842
     XDOT =       6617.674427                 Wp   =           56.27285
     YDOT =       2866.319556  meter/sec      RA   =          186.67740  deg
     ZDOT =      -2618.974720                 TA   =           59.59851
                                              MA   =           59.51368
                                              Ha   =            219.790  n.mi
                                              Hp   =            212.989
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11076860.92                 X    =         3391004.87
     Y    =      -11215035.46  feet           Y    =        -3380505.06  meter
     Z    =       15666804.40                 Z    =         4791678.75
     XDOT =      21711.530272                 XDOT =        6597.852605
     YDOT =       9403.935551  feet/sec       YDOT =        2940.211942  meter/sec
     ZDOT =      -8592.436744                 ZDOT =       -2586.875710
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15691308.43                 X    =        -4782710.81
     Y    =         127255.11  feet           Y    =           38787.36  meter
     Z    =       15738147.10                 Z    =         4796987.24
     XDOT =      -8675.953565                 XDOT =       -2644.430647
     YDOT =     -20917.947096  feet/sec       YDOT =       -6375.790275  meter/sec
     ZDOT =      -8454.682879                 ZDOT =       -2576.987341
  
  
    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   15219.54369682  .00016717  00000-0  10270-3 0  9097
    2 25544  51.6397 187.6061 0001418  28.2721 331.8508 15.55027010 36034
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15219.54369682   =   yrday.fracday
    Element set:     909
    Inclination:       51.6397  deg
    RA of node:       187.6061  deg
    Eccentricity:     .0001418     
    Arg of perigee:    28.2721  deg
    Mean anomaly:     331.8508  deg
    Mean motion:   15.55027010  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3603
    Checksum:              305
 
 
    Coasting Arc #11 (Orbit 3617)
    ---------------------------------------
 
    Vector Time (GMT): 2015/220/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 906095.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5088061.21                 A    =         6781182.74  meter
     Y    =        2693707.58  meter          E    =           .0006180
     Z    =       -3588218.31                 I    =           51.62433
     XDOT =      -5063.068308                 Wp   =           85.98320
     YDOT =      -3663.061198  meter/sec      RA   =          181.67758  deg
     ZDOT =       4436.510753                 TA   =          231.58549
                                              MA   =          231.64099
                                              Ha   =            219.905  n.mi
                                              Hp   =            212.881
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16693114.22                 X    =        -5100374.70
     Y    =        8837623.29  feet           Y    =         2636740.78  meter
     Z    =      -11772369.78                 Z    =        -3612964.72
     XDOT =     -16611.116497                 XDOT =       -5043.281475
     YDOT =     -12017.917317  feet/sec       YDOT =       -3719.569229  meter/sec
     ZDOT =      14555.481473                 ZDOT =        4411.963555
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18077475.39                 X    =         5510014.50
     Y    =        5238062.32  feet           Y    =         1596561.39  meter
     Z    =      -11879390.75                 Z    =        -3620838.30
     XDOT =       3993.098156                 XDOT =        1217.096318
     YDOT =      18939.317555  feet/sec       YDOT =        5772.703991  meter/sec
     ZDOT =      14450.364843                 ZDOT =        4404.471204
  
  
    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   15220.50766607  .00016717  00000-0  10270-3 0  9105
    2 25544  51.6397 182.7939 0001496  32.0262 328.0982 15.55017588 36182
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15220.50766607   =   yrday.fracday
    Element set:     910
    Inclination:       51.6397  deg
    RA of node:       182.7939  deg
    Eccentricity:     .0001496     
    Arg of perigee:    32.0262  deg
    Mean anomaly:     328.0982  deg
    Mean motion:   15.55017588  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3618
    Checksum:              321
 
 
    Coasting Arc #12 (Orbit 3633)
    ---------------------------------------
 
    Vector Time (GMT): 2015/221/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 906095.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6260815.41                 A    =         6785139.80  meter
     Y    =       -1826670.21  meter          E    =           .0014311
     Z    =        1849919.69                 I    =           51.67008
     XDOT =       2929.394454                 Wp   =          107.74056
     YDOT =       4296.898831  meter/sec      RA   =          176.69373  deg
     ZDOT =      -5639.629193                 TA   =           51.90262
                                              MA   =           51.77364
                                              Ha   =            219.876  n.mi
                                              Hp   =            212.863
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20540732.98                 X    =         6271790.26
     Y    =       -5993012.51  feet           Y    =        -1756596.36  meter
     Z    =        6069290.32                 Z    =         1880359.74
     XDOT =       9610.874194                 XDOT =        2908.522637
     YDOT =      14097.437108  feet/sec       YDOT =        4329.540715  meter/sec
     ZDOT =     -18502.720449                 ZDOT =       -5625.449504
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19051245.20                 X    =        -5806819.54
     Y    =       -9657922.51  feet           Y    =        -2943734.78  meter
     Z    =        6200708.39                 Z    =         1889975.92
     XDOT =       1845.839969                 XDOT =         562.612023
     YDOT =     -15546.934495  feet/sec       YDOT =       -4738.705634  meter/sec
     ZDOT =     -18442.350484                 ZDOT =       -5621.228428
  
  
    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   15221.53589168  .00016717  00000-0  10270-3 0  9115
    2 25544  51.6402 177.6603 0001496  33.8761 326.2487 15.55049624 36347
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15221.53589168   =   yrday.fracday
    Element set:     911
    Inclination:       51.6402  deg
    RA of node:       177.6603  deg
    Eccentricity:     .0001496     
    Arg of perigee:    33.8761  deg
    Mean anomaly:     326.2487  deg
    Mean motion:   15.55049624  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3634
    Checksum:              316
 
 
    Coasting Arc #13 (Orbit 3649)
    ---------------------------------------
 
    Vector Time (GMT): 2015/222/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 906095.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6721670.55                 A    =         6786590.41  meter
     Y    =         878199.56  meter          E    =           .0013706
     Z    =         125079.67                 I    =           51.70677
     XDOT =       -498.535023                 Wp   =           45.85829
     YDOT =      -4729.870364  meter/sec      RA   =          171.72160  deg
     ZDOT =       6019.002115                 TA   =          315.48862
                                              MA   =          315.59864
                                              Ha   =            219.865  n.mi
                                              Hp   =            212.870
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -22052724.91                 X    =        -6731598.81
     Y    =        2881232.16  feet           Y    =          802977.91  meter
     Z    =         410366.38                 Z    =           92403.53
     XDOT =      -1635.613592                 XDOT =        -474.845009
     YDOT =     -15517.947390  feet/sec       YDOT =       -4735.313028  meter/sec
     ZDOT =      19747.382266                 ZDOT =        6016.637768
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18275968.98                 X    =         5570515.34
     Y    =       12677102.54  feet           Y    =         3863980.85  meter
     Z    =         269452.55                 Z    =           82129.14
     XDOT =      -8190.933621                 XDOT =       -2496.596568
     YDOT =      11346.550997  feet/sec       YDOT =        3458.428744  meter/sec
     ZDOT =      19737.975331                 ZDOT =        6016.134881
  
  
    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   15222.56410799  .00016717  00000-0  10270-3 0  9123
    2 25544  51.6402 172.5272 0001446  37.8959 322.2296 15.55071124 36503
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15222.56410799   =   yrday.fracday
    Element set:     912
    Inclination:       51.6402  deg
    RA of node:       172.5272  deg
    Eccentricity:     .0001446     
    Arg of perigee:    37.8959  deg
    Mean anomaly:     322.2296  deg
    Mean motion:   15.55071124  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3650
    Checksum:              300
 
 
    Coasting Arc #14 (Orbit 3664)
    ---------------------------------------
 
    Vector Time (GMT): 2015/223/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 906095.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6439136.70                 A    =         6784714.45  meter
     Y    =         205824.84  meter          E    =           .0006352
     Z    =       -2124829.23                 I    =           51.73305
     XDOT =      -1974.559175                 Wp   =          125.92499
     YDOT =       4938.686480  meter/sec      RA   =          166.75091  deg
     ZDOT =      -5520.542262                 TA   =           77.58698
                                              MA   =           77.51590
                                              Ha   =            219.910  n.mi
                                              Hp   =            212.870
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21125776.56                 X    =         6446677.97
     Y    =         675278.35  feet           Y    =          277873.71  meter
     Z    =       -6971224.50                 Z    =        -2093531.43
     XDOT =      -6478.212518                 XDOT =       -2002.821790
     YDOT =      16203.039633  feet/sec       YDOT =        4916.447755  meter/sec
     ZDOT =     -18112.015296                 ZDOT =       -5530.202646
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15482975.65                 X    =        -4719210.98
     Y    =      -14453144.91  feet           Y    =        -4405318.57  meter
     Z    =       -6836408.00                 Z    =        -2083737.16
     XDOT =      14405.642011                 XDOT =        4390.839685
     YDOT =      -6868.967933  feet/sec       YDOT =       -2093.661426  meter/sec
     ZDOT =     -18154.450703                 ZDOT =       -5533.476574
  
  
    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   15223.52805349  .00016717  00000-0  10270-3 0  9130
    2 25544  51.6414 167.7145 0001515  37.2560 322.8698 15.55081167 36656
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15223.52805349   =   yrday.fracday
    Element set:     913
    Inclination:       51.6414  deg
    RA of node:       167.7145  deg
    Eccentricity:     .0001515     
    Arg of perigee:    37.2560  deg
    Mean anomaly:     322.8698  deg
    Mean motion:   15.55081167  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3665
    Checksum:              310
 
 
    Coasting Arc #15 (Orbit 3680)
    ---------------------------------------
 
    Vector Time (GMT): 2015/224/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 906095.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5455016.13                 A    =         6780522.71  meter
     Y    =       -1345288.58  meter          E    =           .0012498
     Z    =        3785321.22                 I    =           51.75041
     XDOT =       4147.268457                 Wp   =           91.38505
     YDOT =      -4877.287283  meter/sec      RA   =          161.77251  deg
     ZDOT =       4230.905554                 TA   =          313.97132
                                              MA   =          314.07433
                                              Ha   =            219.962  n.mi
                                              Hp   =            212.798
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17897034.53                 X    =        -5457954.64
     Y    =       -4413676.43  feet           Y    =        -1406306.61  meter
     Z    =       12419032.86                 Z    =         3758815.22
     XDOT =      13606.523808                 XDOT =        4180.947507
     YDOT =     -16001.598699  feet/sec       YDOT =       -4830.721527  meter/sec
     ZDOT =      13880.923732                 ZDOT =        4251.133515
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10876873.67                 X    =         3315271.10
     Y    =       14976531.90  feet           Y    =         4564846.92  meter
     Z    =       12305034.46                 Z    =         3750574.50
     XDOT =     -19561.345404                 XDOT =       -5962.298079
     YDOT =       2695.930727  feet/sec       YDOT =         821.719686  meter/sec
     ZDOT =      13968.891456                 ZDOT =        4257.718116
  
  
    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   15224.55625294  .00016717  00000-0  10270-3 0  9144
    2 25544  51.6419 162.5817 0001433  42.1563 317.9700 15.55102396 36812
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15224.55625294   =   yrday.fracday
    Element set:     914
    Inclination:       51.6419  deg
    RA of node:       162.5817  deg
    Eccentricity:     .0001433     
    Arg of perigee:    42.1563  deg
    Mean anomaly:     317.9700  deg
    Mean motion:   15.55102396  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3681
    Checksum:              300
 
             

Curator: Kim Dismukes | Responsible NASA Official: Amiko Kauderer | Updated: 06/08/2009
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