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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 3493)
    ---------------------------------------
 
    Vector Time (GMT): 2015/212/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 906095.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5749171.04                 A    =         6782704.45  meter
     Y    =        1803499.08  meter          E    =           .0013289
     Z    =        3102991.06                 I    =           51.39921
     XDOT =        783.195747                 Wp   =           89.56106
     YDOT =       5888.206331  meter/sec      RA   =          221.69159  deg
     ZDOT =      -4855.263184                 TA   =           54.57676
                                              MA   =           54.45274
                                              Ha   =            219.800  n.mi
                                              Hp   =            213.150
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18862109.70                 X    =         5713503.77
     Y    =        5916991.73  feet           Y    =         1867590.52  meter
     Z    =       10180416.86                 Z    =         3130832.22
     XDOT =       2569.539851                 XDOT =         740.878703
     YDOT =      19318.262241  feet/sec       YDOT =        5896.728140  meter/sec
     ZDOT =     -15929.341154                 ZDOT =       -4851.561187
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6894203.17                 X    =        -2101353.13
     Y    =      -18461110.25  feet           Y    =        -5626946.40  meter
     Z    =       10299914.18                 Z    =         3139413.84
     XDOT =      12242.450781                 XDOT =        3731.498998
     YDOT =     -13483.735483  feet/sec       YDOT =       -4109.842575  meter/sec
     ZDOT =     -15914.421644                 ZDOT =       -4850.715717
  
  
    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   15212.53863689  .00016717  00000-0  10270-3 0  9006
    2 25544  51.6406 222.5769 0001285  18.2485 341.8714 15.54968923 34941
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15212.53863689   =   yrday.fracday
    Element set:     900
    Inclination:       51.6406  deg
    RA of node:       222.5769  deg
    Eccentricity:     .0001285     
    Arg of perigee:    18.2485  deg
    Mean anomaly:     341.8714  deg
    Mean motion:   15.54968923  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3494
    Checksum:              331
 
 
    Coasting Arc #2 (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    =       -5897026.00                 A    =         6786010.42  meter
     Y    =       -3075238.45  meter          E    =           .0009826
     Z    =       -1327130.61                 I    =           51.43533
     XDOT =       1232.080413                 Wp   =           36.77960
     YDOT =      -4855.525897  meter/sec      RA   =          216.69595  deg
     ZDOT =       5806.613613                 TA   =          308.72678
                                              MA   =          308.81459
                                              Ha   =            219.812  n.mi
                                              Hp   =            213.079
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19347198.18                 X    =        -5855753.12
     Y    =      -10089364.98  feet           Y    =        -3140952.06  meter
     Z    =       -4354103.05                 Z    =        -1355676.37
     XDOT =       4042.258572                 XDOT =        1258.078808
     YDOT =     -15930.203075  feet/sec       YDOT =       -4841.602714  meter/sec
     ZDOT =      19050.569598                 ZDOT =        5812.661732
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4294057.77                 X    =         1308828.81
     Y    =       21367971.04  feet           Y    =         6512957.57  meter
     Z    =       -4476433.59                 Z    =        -1364416.96
     XDOT =     -13295.303277                 XDOT =       -4052.408439
     YDOT =       6648.302108  feet/sec       YDOT =        2026.402483  meter/sec
     ZDOT =      19077.422372                 ZDOT =        5814.798339
  
  
    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   15213.50265733  .00016717  00000-0  10270-3 0  9011
    2 25544  51.6411 217.7653 0001145  27.0467 333.0746 15.54997484 35097
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15213.50265733   =   yrday.fracday
    Element set:     901
    Inclination:       51.6411  deg
    RA of node:       217.7653  deg
    Eccentricity:     .0001145     
    Arg of perigee:    27.0467  deg
    Mean anomaly:     333.0746  deg
    Mean motion:   15.54997484  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3509
    Checksum:              302
 
 
    Coasting Arc #3 (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    =        5440748.86                 A    =         6786726.30  meter
     Y    =        3993360.91  meter          E    =           .0010228
     Z    =        -675133.96                 I    =           51.46252
     XDOT =      -3315.663081                 Wp   =          133.11449
     YDOT =       3522.284425  meter/sec      RA   =          211.70757  deg
     ZDOT =      -5950.015893                 TA   =           54.19645
                                              MA   =           54.10143
                                              Ha   =            219.951  n.mi
                                              Hp   =            213.130
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17850225.91                 X    =         5398969.25
     Y    =       13101577.78  feet           Y    =         4053969.33  meter
     Z    =       -2215006.43                 Z    =         -648805.90
     XDOT =     -10878.159715                 XDOT =       -3325.901359
     YDOT =      11556.051263  feet/sec       YDOT =        3485.149253  meter/sec
     ZDOT =     -19521.049517                 ZDOT =       -5966.147266
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1417589.55                 X    =         -432081.29
     Y    =      -22107887.54  feet           Y    =        -6738484.12  meter
     Z    =       -2102357.59                 Z    =         -640798.59
     XDOT =      14150.064724                 XDOT =        4312.939728
     YDOT =        934.702938  feet/sec       YDOT =         284.897455  meter/sec
     ZDOT =     -19591.071389                 ZDOT =       -5971.358559
  
  
    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   15214.53093837  .00016717  00000-0  10270-3 0  9020
    2 25544  51.6402 212.6314 0001311  25.3776 334.7442 15.54963530 35258
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15214.53093837   =   yrday.fracday
    Element set:     902
    Inclination:       51.6402  deg
    RA of node:       212.6314  deg
    Eccentricity:     .0001311     
    Arg of perigee:    25.3776  deg
    Mean anomaly:     334.7442  deg
    Mean motion:   15.54963530  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3525
    Checksum:              282
 
 
    Coasting Arc #4 (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    =       -4393619.85                 A    =         6784074.29  meter
     Y    =       -4484962.17  meter          E    =           .0014428
     Z    =        2551189.02                 I    =           51.48161
     XDOT =       5186.137715                 Wp   =           72.29452
     YDOT =      -2076.868735  meter/sec      RA   =          206.71886  deg
     ZDOT =       5260.142055                 TA   =          316.46551
                                              MA   =          316.57930
                                              Ha   =            219.853  n.mi
                                              Hp   =            213.133
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14414763.29                 X    =        -4355533.88
     Y    =      -14714442.82  feet           Y    =        -4533881.52  meter
     Z    =        8370042.73                 Z    =         2529938.62
     XDOT =      17014.887516                 XDOT =        5183.424976
     YDOT =      -6813.873801  feet/sec       YDOT =       -2018.889029  meter/sec
     ZDOT =      17257.683909                 ZDOT =        5285.328295
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1644875.23                 X    =         -501357.97
     Y    =       20569519.90  feet           Y    =         6269589.67  meter
     Z    =        8279316.39                 Z    =         2523535.64
     XDOT =     -14718.753025                 XDOT =       -4486.275922
     YDOT =      -8194.087933  feet/sec       YDOT =       -2497.558002  meter/sec
     ZDOT =      17366.442818                 ZDOT =        5293.291771
  
  
    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   15215.55920983  .00016717  00000-0  10270-3 0  9035
    2 25544  51.6403 207.4988 0001198  22.0096 338.1108 15.55007721 35417
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15215.55920983   =   yrday.fracday
    Element set:     903
    Inclination:       51.6403  deg
    RA of node:       207.4988  deg
    Eccentricity:     .0001198     
    Arg of perigee:    22.0096  deg
    Mean anomaly:     338.1108  deg
    Mean motion:   15.55007721  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3541
    Checksum:              296
 
 
    Coasting Arc #5 (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    =        2794683.92                 A    =         6779786.45  meter
     Y    =        4626180.15  meter          E    =           .0008392
     Z    =       -4102239.34                 I    =           51.49566
     XDOT =      -6618.786455                 Wp   =           65.24451
     YDOT =        624.299428  meter/sec      RA   =          201.71906  deg
     ZDOT =      -3807.760368                 TA   =          165.34017
                                              MA   =          165.31582
                                              Ha   =            219.952  n.mi
                                              Hp   =            213.123
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9168910.50                 X    =         2762672.02
     Y    =       15177756.41  feet           Y    =         4657253.08  meter
     Z    =      -13458790.48                 Z    =        -4088741.33
     XDOT =     -21715.178659                 XDOT =       -6606.779185
     YDOT =       2048.226470  feet/sec       YDOT =         550.350878  meter/sec
     ZDOT =     -12492.652127                 ZDOT =       -3839.883547
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5116688.86                 X    =         1559566.76
     Y    =      -17023305.77  feet           Y    =        -5188703.60  meter
     Z    =      -13401447.93                 Z    =        -4084761.33
     XDOT =      14729.955013                 XDOT =        4489.690288
     YDOT =      14364.066276  feet/sec       YDOT =        4378.167401  meter/sec
     ZDOT =     -12631.040833                 ZDOT =       -3849.941246
  
  
    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   15216.52321010  .00016717  00000-0  10270-3 0  9040
    2 25544  51.6401 202.6858 0001381  28.2257 331.8971 15.54979083 35561
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15216.52321010   =   yrday.fracday
    Element set:     904
    Inclination:       51.6401  deg
    RA of node:       202.6858  deg
    Eccentricity:     .0001381     
    Arg of perigee:    28.2257  deg
    Mean anomaly:     331.8971  deg
    Mean motion:   15.54979083  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3556
    Checksum:              295
 
 
    Coasting Arc #6 (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    =        -825273.08                 A    =         6775975.66  meter
     Y    =       -4438776.60  meter          E    =           .0005538
     Z    =        5048754.72                 I    =           51.51301
     XDOT =       7417.929652                 Wp   =          110.17254
     YDOT =        707.064312  meter/sec      RA   =          196.70885  deg
     ZDOT =       1830.675439                 TA   =          322.06180
                                              MA   =          322.10080
                                              Ha   =            219.907  n.mi
                                              Hp   =            213.068
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2707588.86                 X    =         -800100.98
     Y    =      -14562915.35  feet           Y    =        -4447864.53  meter
     Z    =       16564155.91                 Z    =         5044806.95
     XDOT =      24337.039540                 XDOT =        7400.579130
     YDOT =       2319.764802  feet/sec       YDOT =         789.919483  meter/sec
     ZDOT =       6006.153016                 ZDOT =        1866.667771
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8755663.52                 X    =        -2668726.24
     Y    =       11970232.75  feet           Y    =         3648526.94  meter
     Z    =       16547890.69                 Z    =         5043797.08
     XDOT =     -13961.576232                 XDOT =       -4255.488436
     YDOT =     -18745.222657  feet/sec       YDOT =       -5713.543866  meter/sec
     ZDOT =       6160.992708                 ZDOT =        1877.870577
  
  
    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   15217.55146748  .00016717  00000-0  10270-3 0  9058
    2 25544  51.6400 197.5531 0001418  24.5748 335.5472 15.55000754 35721
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15217.55146748   =   yrday.fracday
    Element set:     905
    Inclination:       51.6400  deg
    RA of node:       197.5531  deg
    Eccentricity:     .0001418     
    Arg of perigee:    24.5748  deg
    Mean anomaly:     335.5472  deg
    Mean motion:   15.55000754  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3572
    Checksum:              303
 
 
    Coasting Arc #7 (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    =       -1317071.13                 A    =         6774870.70  meter
     Y    =        4026599.98  meter          E    =           .0015546
     Z    =       -5300270.26                 I    =           51.54021
     XDOT =      -7413.726402                 Wp   =           88.56431
     YDOT =      -1874.549059  meter/sec      RA   =          191.69178  deg
     ZDOT =        419.604221                 TA   =          185.43945
                                              MA   =          185.45636
                                              Ha   =            219.952  n.mi
                                              Hp   =            212.948
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4321099.50                 X    =        -1336253.14
     Y    =       13210629.86  feet           Y    =         4011764.37  meter
     Z    =      -17389338.14                 Z    =        -5306714.88
     XDOT =     -24323.249351                 XDOT =       -7394.252002
     YDOT =      -6150.095338  feet/sec       YDOT =       -1957.345328  meter/sec
     ZDOT =       1376.654268                 ZDOT =         383.637383
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12440568.54                 X    =         3791885.29
     Y    =       -6118496.09  feet           Y    =        -1864917.61  meter
     Z    =      -17417749.08                 Z    =        -5308929.92
     XDOT =      11981.620773                 XDOT =        3651.998012
     YDOT =      20896.393711  feet/sec       YDOT =        6369.220803  meter/sec
     ZDOT =       1222.099953                 ZDOT =         372.496066
  
  
    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   15218.51545161  .00016717  00000-0  10270-3 0  9068
    2 25544  51.6402 192.7407 0001462  30.6666 329.4572 15.54998848 35876
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15218.51545161   =   yrday.fracday
    Element set:     906
    Inclination:       51.6402  deg
    RA of node:       192.7407  deg
    Eccentricity:     .0001462     
    Arg of perigee:    30.6666  deg
    Mean anomaly:     329.4572  deg
    Mean motion:   15.54998848  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3587
    Checksum:              328
 
 
    Coasting Arc #8 (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    =        3378694.40                 A    =         6776937.00  meter
     Y    =       -3417182.32  meter          E    =           .0008657
     Z    =        4774306.52                 I    =           51.57874
     XDOT =       6616.079052                 Wp   =           56.19358
     YDOT =       2868.047535  meter/sec      RA   =          186.67897  deg
     ZDOT =      -2621.162989                 TA   =           59.70117
                                              MA   =           59.61555
                                              Ha   =            219.809  n.mi
                                              Hp   =            212.969
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11084955.38                 X    =         3393463.44
     Y    =      -11211228.10  feet           Y    =        -3379317.03  meter
     Z    =       15663735.30                 Z    =         4790755.25
     XDOT =      21706.296101                 XDOT =        6596.248656
     YDOT =       9409.604775  feet/sec       YDOT =        2941.922033  meter/sec
     ZDOT =      -8599.616106                 ZDOT =       -2589.071750
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15694332.17                 X    =        -4783632.45
     Y    =         118817.95  feet           Y    =           36215.71  meter
     Z    =       15735129.33                 Z    =         4796067.42
     XDOT =      -8668.891017                 XDOT =       -2642.277982
     YDOT =     -20918.046526  feet/sec       YDOT =       -6375.820581  meter/sec
     ZDOT =      -8461.895991                 ZDOT =       -2579.185898
  
  
    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   15219.54369286  .00016717  00000-0  10270-3 0  9075
    2 25544  51.6400 187.6078 0001484  28.9394 331.1841 15.55028034 36033
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15219.54369286   =   yrday.fracday
    Element set:     907
    Inclination:       51.6400  deg
    RA of node:       187.6078  deg
    Eccentricity:     .0001484     
    Arg of perigee:    28.9394  deg
    Mean anomaly:     331.1841  deg
    Mean motion:   15.55028034  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3603
    Checksum:              312
 
 
    Coasting Arc #9 (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    =       -5090113.16                 A    =         6781185.02  meter
     Y    =        2692110.16  meter          E    =           .0006229
     Z    =       -3586497.53                 I    =           51.62465
     XDOT =      -5060.388923                 Wp   =           85.53155
     YDOT =      -3664.546536  meter/sec      RA   =          181.67920  deg
     ZDOT =       4438.352199                 TA   =          232.06245
                                              MA   =          232.11876
                                              Ha   =            219.925  n.mi
                                              Hp   =            212.860
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16699846.34                 X    =        -5102416.99
     Y    =        8832382.42  feet           Y    =         2635120.47  meter
     Z    =      -11766724.18                 Z    =        -3611253.89
     XDOT =     -16602.325862                 XDOT =       -5040.594624
     YDOT =     -12022.790474  feet/sec       YDOT =       -3721.024563  meter/sec
     ZDOT =      14561.522963                 ZDOT =        4413.818036
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18078679.77                 X    =         5510381.59
     Y    =        5246536.78  feet           Y    =         1599144.41  meter
     Z    =      -11873787.71                 Z    =        -3619130.49
     XDOT =       3984.043006                 XDOT =        1214.336308
     YDOT =      18936.627944  feet/sec       YDOT =        5771.884197  meter/sec
     ZDOT =      14456.462713                 ZDOT =        4406.329835
  
  
    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   15220.50766151  .00016717  00000-0  10270-3 0  9086
    2 25544  51.6401 182.7956 0001562  32.6574 327.4676 15.55018592 36182
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15220.50766151   =   yrday.fracday
    Element set:     908
    Inclination:       51.6401  deg
    RA of node:       182.7956  deg
    Eccentricity:     .0001562     
    Arg of perigee:    32.6574  deg
    Mean anomaly:     327.4676  deg
    Mean motion:   15.55018592  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3618
    Checksum:              312
 
 
    Coasting Arc #10 (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    =        6262251.42                 A    =         6785141.05  meter
     Y    =       -1824468.35  meter          E    =           .0014348
     Z    =        1847288.37                 I    =           51.67040
     XDOT =       2925.551163                 Wp   =          107.54739
     YDOT =       4298.026971  meter/sec      RA   =          176.69538  deg
     ZDOT =      -5640.740980                 TA   =           52.12617
                                              MA   =           51.99647
                                              Ha   =            219.896  n.mi
                                              Hp   =            212.842
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20545444.28                 X    =         6273214.32
     Y    =       -5985788.56  feet           Y    =        -1754378.51  meter
     Z    =        6060657.39                 Z    =         1877735.36
     XDOT =       9598.264969                 XDOT =        2904.672417
     YDOT =      14101.138357  feet/sec       YDOT =        4330.625839  meter/sec
     ZDOT =     -18506.368044                 ZDOT =       -5626.579978
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19049778.68                 X    =        -5806372.54
     Y    =       -9666451.32  feet           Y    =        -2946334.36  meter
     Z    =        6192105.01                 Z    =         1887353.61
     XDOT =       1856.928582                 XDOT =         565.991832
     YDOT =     -15541.128745  feet/sec       YDOT =       -4736.936041  meter/sec
     ZDOT =     -18446.078756                 ZDOT =       -5622.364805
  
  
    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   15221.53588648  .00016717  00000-0  10270-3 0  9094
    2 25544  51.6405 177.6620 0001562  34.5866 325.5388 15.55050641 36340
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15221.53588648   =   yrday.fracday
    Element set:     909
    Inclination:       51.6405  deg
    RA of node:       177.6620  deg
    Eccentricity:     .0001562     
    Arg of perigee:    34.5866  deg
    Mean anomaly:     325.5388  deg
    Mean motion:   15.55050641  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3634
    Checksum:              318
 
 
    Coasting Arc #11 (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    =       -6721915.30                 A    =         6786587.31  meter
     Y    =         875622.81  meter          E    =           .0013779
     Z    =         128101.58                 I    =           51.70708
     XDOT =       -494.028949                 Wp   =           45.92624
     YDOT =      -4730.442041  meter/sec      RA   =          171.72330  deg
     ZDOT =       6018.971436                 TA   =          315.45321
                                              MA   =          315.56389
                                              Ha   =            219.887  n.mi
                                              Hp   =            212.848
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -22053527.88                 X    =        -6731829.40
     Y    =        2872778.23  feet           Y    =          800398.50  meter
     Z    =         420280.77                 Z    =           95424.29
     XDOT =      -1620.829884                 XDOT =        -470.332728
     YDOT =     -15519.822970  feet/sec       YDOT =       -4735.834281  meter/sec
     ZDOT =      19747.281613                 ZDOT =        6016.628993
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18270933.77                 X    =         5568980.61
     Y    =       12683947.27  feet           Y    =         3866067.13  meter
     Z    =         279362.39                 Z    =           85149.66
     XDOT =      -8202.647936                 XDOT =       -2500.167091
     YDOT =      11338.378980  feet/sec       YDOT =        3455.937913  meter/sec
     ZDOT =      19737.969135                 ZDOT =        6016.132992
  
  
    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   15222.56410215  .00016717  00000-0  10270-3 0  9104
    2 25544  51.6406 172.5289 0001512  38.6215 321.5046 15.55072134 36500
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15222.56410215   =   yrday.fracday
    Element set:     910
    Inclination:       51.6406  deg
    RA of node:       172.5289  deg
    Eccentricity:     .0001512     
    Arg of perigee:    38.6215  deg
    Mean anomaly:     321.5046  deg
    Mean motion:   15.55072134  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3650
    Checksum:              268
 
 
    Coasting Arc #12 (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    =        6438027.55                 A    =         6784705.77  meter
     Y    =         208838.92  meter          E    =           .0006370
     Z    =       -2128013.48                 I    =           51.73335
     XDOT =      -1979.391722                 Wp   =          125.29988
     YDOT =       4938.420054  meter/sec      RA   =          166.75262  deg
     ZDOT =      -5518.984081                 TA   =           78.24921
                                              MA   =           78.17775
                                              Ha   =            219.932  n.mi
                                              Hp   =            212.847
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21122137.63                 X    =         6445550.67
     Y    =         685167.06  feet           Y    =          280875.28  meter
     Z    =       -6981671.53                 Z    =        -2096721.11
     XDOT =      -6494.067331                 XDOT =       -2007.658568
     YDOT =      16202.165533  feet/sec       YDOT =        4916.127265  meter/sec
     ZDOT =     -18106.903152                 ZDOT =       -5528.667950
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15473774.50                 X    =        -4716406.47
     Y    =      -14458230.91  feet           Y    =        -4406868.78  meter
     Z    =       -6846878.93                 Z    =        -2086928.70
     XDOT =      14416.648503                 XDOT =        4394.194464
     YDOT =      -6858.516009  feet/sec       YDOT =       -2090.475680  meter/sec
     ZDOT =     -18149.439702                 ZDOT =       -5531.949221
  
  
    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   15223.52804703  .00016717  00000-0  10270-3 0  9111
    2 25544  51.6418 167.7163 0001579  38.1233 322.0031 15.55082205 36654
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15223.52804703   =   yrday.fracday
    Element set:     911
    Inclination:       51.6418  deg
    RA of node:       167.7163  deg
    Eccentricity:     .0001579     
    Arg of perigee:    38.1233  deg
    Mean anomaly:     322.0031  deg
    Mean motion:   15.55082205  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3665
    Checksum:              279
 
 
    Coasting Arc #13 (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    =       -5452366.60                 A    =         6780511.19  meter
     Y    =       -1348439.19  meter          E    =           .0012549
     Z    =        3787924.87                 I    =           51.75070
     XDOT =       4151.781336                 Wp   =           91.27747
     YDOT =      -4876.101594  meter/sec      RA   =          161.77423  deg
     ZDOT =       4227.938503                 TA   =          314.11902
                                              MA   =          314.22219
                                              Ha   =            219.984  n.mi
                                              Hp   =            212.774
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17888341.87                 X    =        -5455282.73
     Y    =       -4424013.10  feet           Y    =        -1409427.47  meter
     Z    =       12427575.04                 Z    =         3761431.80
     XDOT =      13621.329844                 XDOT =        4185.461206
     YDOT =     -15997.708642  feet/sec       YDOT =       -4829.485367  meter/sec
     ZDOT =      13871.189313                 ZDOT =        4248.188389
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10863603.87                 X    =         3311226.46
     Y    =       14978846.58  feet           Y    =         4565552.44  meter
     Z    =       12313632.86                 Z    =         3753195.29
     XDOT =     -19570.018173                 XDOT =       -5964.941539
     YDOT =       2684.328386  feet/sec       YDOT =         818.183292  meter/sec
     ZDOT =      13959.251314                 ZDOT =        4254.779801
  
  
    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   15224.55624584  .00016717  00000-0  10270-3 0  9123
    2 25544  51.6422 162.5836 0001497  43.0261 317.1009 15.55103453 36811
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15224.55624584   =   yrday.fracday
    Element set:     912
    Inclination:       51.6422  deg
    RA of node:       162.5836  deg
    Eccentricity:     .0001497     
    Arg of perigee:    43.0261  deg
    Mean anomaly:     317.1009  deg
    Mean motion:   15.55103453  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3681
    Checksum:              288
 
 
    Coasting Arc #14 (Orbit 3695)
    ---------------------------------------
 
    Vector Time (GMT): 2015/225/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 906095.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3910582.84                 A    =         6776292.79  meter
     Y    =        2545716.44  meter          E    =           .0013484
     Z    =       -4926316.43                 I    =           51.76728
     XDOT =      -5792.303892                 Wp   =           70.20868
     YDOT =       4453.894925  meter/sec      RA   =          156.78262  deg
     ZDOT =      -2297.086671                 TA   =          177.34938
                                              MA   =          177.34223
                                              Ha   =            219.902  n.mi
                                              Hp   =            212.797
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12829996.21                 X    =         3905755.06
     Y    =        8352088.04  feet           Y    =         2589420.11  meter
     Z    =      -16162455.49                 Z    =        -4907331.75
     XDOT =     -19003.621694                 XDOT =       -5830.519786
     YDOT =      14612.516158  feet/sec       YDOT =        4388.907881  meter/sec
     ZDOT =      -7536.373593                 ZDOT =       -2325.316796
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4735897.67                 X    =        -1443501.61
     Y    =      -14647938.22  feet           Y    =        -4464691.57  meter
     Z    =      -16081054.82                 Z    =        -4901505.51
     XDOT =      22855.767454                 XDOT =        6966.437920
     YDOT =       1016.086532  feet/sec       YDOT =         309.703175  meter/sec
     ZDOT =      -7658.768656                 ZDOT =       -2334.392686
  
  
    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   15225.52017521  .00016717  00000-0  10270-3 0  9139
    2 25544  51.6429 157.7709 0001611  44.3003 315.8279 15.55114113 36964
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15225.52017521   =   yrday.fracday
    Element set:     913
    Inclination:       51.6429  deg
    RA of node:       157.7709  deg
    Eccentricity:     .0001611     
    Arg of perigee:    44.3003  deg
    Mean anomaly:     315.8279  deg
    Mean motion:   15.55114113  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3696
    Checksum:              287
 
 
    Coasting Arc #15 (Orbit 3711)
    ---------------------------------------
 
    Vector Time (GMT): 2015/226/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 906095.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2017198.51                 A    =         6774375.57  meter
     Y    =       -3671206.38  meter          E    =           .0003547
     Z    =        5321068.52                 I    =           51.79056
     XDOT =       6747.346017                 Wp   =           75.40319
     YDOT =      -3654.016350  meter/sec      RA   =          151.78391  deg
     ZDOT =         37.703194                 TA   =           14.24352
                                              MA   =           14.23353
                                              Ha   =            219.872  n.mi
                                              Hp   =            212.680
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6618105.33                 X    =        -2001843.46
     Y    =      -12044640.36  feet           Y    =        -3693678.03  meter
     Z    =       17457573.88                 Z    =         5311306.97
     XDOT =      22136.961999                 XDOT =        6787.521491
     YDOT =     -11988.242617  feet/sec       YDOT =       -3578.338458  meter/sec
     ZDOT =        123.698143                 ZDOT =          70.577452
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2170555.80                 X    =         -661585.41
     Y    =       13623789.26  feet           Y    =         4152530.97  meter
     Z    =       17416102.30                 Z    =         5308427.98
     XDOT =     -23812.108804                 XDOT =       -7257.930764
     YDOT =      -4130.220820  feet/sec       YDOT =       -1258.891306  meter/sec
     ZDOT =        265.991841                 ZDOT =          81.074313
  
  
    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   15226.54835641  .00016717  00000-0  10270-3 0  9144
    2 25544  51.6432 152.6384 0001486  43.4673 316.6597 15.55149011 37120
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15226.54835641   =   yrday.fracday
    Element set:     914
    Inclination:       51.6432  deg
    RA of node:       152.6384  deg
    Eccentricity:     .0001486     
    Arg of perigee:    43.4673  deg
    Mean anomaly:     316.6597  deg
    Mean motion:   15.55149011  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3712
    Checksum:              308
 
             

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