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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  18298.65
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   128.3
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.453
   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 
   ------------------------------------------------------------------------
   118/13:07:34.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              215.7  
   000/00:00:00.000           0.0               0.0              213.4  
   
   126/05:20:56.664          -0.7               4.9              4.9    
   N/A                       -4.1              -0.0              216.6  
   000/00:11:53.328          -2.7               0.2              215.2  
   
 
 
    Coasting Arc #1 (Orbit 2014)
    ---------------------------------------
 
    Vector Time (GMT): 2015/117/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 911686.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -863628.71                 A    =         6771585.49  meter
     Y    =       -4186362.04  meter          E    =           .0009009
     Z    =       -5259803.54                 I    =           51.48642
     XDOT =       7221.844501                 Wp   =           96.17101
     YDOT =      -2452.602088  meter/sec      RA   =          336.65490  deg
     ZDOT =        766.462950                 TA   =          181.16982
                                              MA   =          181.17193
                                              Ha   =            215.790  n.mi
                                              Hp   =            213.427
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2833427.51                 X    =         -791201.31
     Y    =      -13734783.60  feet           Y    =        -4195615.02  meter
     Z    =      -17256573.29                 Z    =        -5263822.76
     XDOT =      23693.715553                 XDOT =        7245.010123
     YDOT =      -8046.594776  feet/sec       YDOT =       -2371.713134  meter/sec
     ZDOT =       2514.642225                 ZDOT =         801.601876
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9994460.83                 X    =        -3046311.66
     Y    =       -9809022.19  feet           Y    =        -2989789.96  meter
     Z    =      -17272977.44                 Z    =        -5264803.53
     XDOT =      14302.928707                 XDOT =        4359.532670
     YDOT =     -19266.450557  feet/sec       YDOT =       -5872.414130  meter/sec
     ZDOT =       2665.740515                 ZDOT =         812.517709
  
  
    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   15117.51467619  .00016717  00000-0  10270-3 0  9001
    2 25544  51.6459 337.1587 0005548 275.7924  84.2597 15.56185828 20156
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15117.51467619   =   yrday.fracday
    Element set:     900
    Inclination:       51.6459  deg
    RA of node:       337.1587  deg
    Eccentricity:     .0005548     
    Arg of perigee:   275.7924  deg
    Mean anomaly:      84.2597  deg
    Mean motion:   15.56185828  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2015
    Checksum:              341
 
 
    Coasting Arc #2 (Orbit 2030)
    ---------------------------------------
 
    Vector Time (GMT): 2015/118/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 911686.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1607645.60                 A    =         6774909.58  meter
     Y    =        4872250.17  meter          E    =           .0005223
     Z    =        4424217.87                 I    =           51.46959
     XDOT =      -6885.258533                 Wp   =           36.18443
     YDOT =        731.144173  meter/sec      RA   =          331.62741  deg
     ZDOT =      -3300.982206                 TA   =           87.22040
                                              MA   =           87.16062
                                              Ha   =            215.809  n.mi
                                              Hp   =            213.471
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5274427.82                 X    =        -1683500.14
     Y    =       15985072.74  feet           Y    =         4853848.57  meter
     Z    =       14515150.49                 Z    =         4416223.64
     XDOT =     -22589.430882                 XDOT =       -6876.887568
     YDOT =       2398.766973  feet/sec       YDOT =         654.195316  meter/sec
     ZDOT =     -10829.994114                 ZDOT =       -3334.409430
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4859835.85                 X    =         1481277.97
     Y    =       16147609.17  feet           Y    =         4921791.28  meter
     Z    =       14479932.55                 Z    =         4413483.44
     XDOT =     -15814.878830                 XDOT =       -4820.375067
     YDOT =      14617.874174  feet/sec       YDOT =        4455.528048  meter/sec
     ZDOT =     -10973.408249                 ZDOT =       -3344.694834
  
  
    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   15118.54214514  .00016717  00000-0  10270-3 0  9010
    2 25544  51.6462 332.0213 0005739 280.0944  79.9562 15.56242261 20319
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15118.54214514   =   yrday.fracday
    Element set:     901
    Inclination:       51.6462  deg
    RA of node:       332.0213  deg
    Eccentricity:     .0005739     
    Arg of perigee:   280.0944  deg
    Mean anomaly:      79.9562  deg
    Mean motion:   15.56242261  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2031
    Checksum:              283
 
 
    Coasting Arc #3 (Orbit 2031)
    ---------------------------------------
 
    Vector Time (GMT): 2015/118/13:07:34.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926120.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6227689.05                 A    =         6780792.37  meter
     Y    =       -1256441.37  meter          E    =           .0008926
     Z    =        2355165.62                 I    =           51.48575
     XDOT =       -950.136296                 Wp   =           58.40438
     YDOT =       5390.063786  meter/sec      RA   =          331.43464  deg
     ZDOT =       5377.481007                 TA   =          327.96994
                                              MA   =          328.02416
                                              Ha   =            215.668  n.mi
                                              Hp   =            213.408
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20432050.70                 X    =         6229835.42
     Y    =       -4122182.98  feet           Y    =        -1186787.14  meter
     Z    =        7726921.32                 Z    =         2385424.05
     XDOT =      -3117.245067                 XDOT =       -1036.460656
     YDOT =      17683.936305  feet/sec       YDOT =        5378.956399  meter/sec
     ZDOT =      17642.654221                 ZDOT =        5372.655390
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9221651.02                 X    =         2810759.23
     Y    =      -18638598.70  feet           Y    =        -5681044.88  meter
     Z    =        7856856.39                 Z    =         2394769.83
     XDOT =      10646.285756                 XDOT =        3244.987898
     YDOT =      12709.435452  feet/sec       YDOT =        3873.835926  meter/sec
     ZDOT =      17620.915893                 ZDOT =        5370.855164
  
  
    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   15118.60636138  .00016717  00000-0  10270-3 0  9028
    2 25544  51.6439 331.6984 0005667 278.1856  81.8655 15.56229474 20320
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15118.60636138   =   yrday.fracday
    Element set:     902
    Inclination:       51.6439  deg
    RA of node:       331.6984  deg
    Eccentricity:     .0005667     
    Arg of perigee:   278.1856  deg
    Mean anomaly:      81.8655  deg
    Mean motion:   15.56229474  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2032
    Checksum:              332
 
 
    Coasting Arc #4 (Orbit 2046)
    ---------------------------------------
 
    Vector Time (GMT): 2015/119/13:07:34.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926120.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5287720.49                 A    =         6775506.32  meter
     Y    =        -517587.43  meter          E    =           .0004648
     Z    =       -4209353.93                 I    =           51.44004
     XDOT =       3467.853293                 Wp   =           28.80038
     YDOT =      -5786.756571  meter/sec      RA   =          326.42532  deg
     ZDOT =      -3642.398415                 TA   =          203.77535
                                              MA   =          203.79683
                                              Ha   =            215.913  n.mi
                                              Hp   =            213.237
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17348164.34                 X    =        -5261092.02
     Y    =       -1698121.50  feet           Y    =         -576569.56  meter
     Z    =      -13810216.30                 Z    =        -4234976.21
     XDOT =      11377.471433                 XDOT =        3549.998042
     YDOT =     -18985.421822  feet/sec       YDOT =       -5747.517701  meter/sec
     ZDOT =     -11950.126032                 ZDOT =       -3625.352185
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11693309.76                 X    =        -3564120.82
     Y    =       12808849.69  feet           Y    =         3904137.39  meter
     Z    =      -13919927.20                 Z    =        -4242793.81
     XDOT =      -7419.043214                 XDOT =       -2261.324372
     YDOT =     -19687.191103  feet/sec       YDOT =       -6000.655848  meter/sec
     ZDOT =     -11875.941093                 ZDOT =       -3619.786845
  
  
    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   15119.56959020  .00016717  00000-0  10270-3 0  9033
    2 25544  51.6430 326.8815 0005543 283.1097  76.9438 15.56255501 20476
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15119.56959020   =   yrday.fracday
    Element set:     903
    Inclination:       51.6430  deg
    RA of node:       326.8815  deg
    Eccentricity:     .0005543     
    Arg of perigee:   283.1097  deg
    Mean anomaly:      76.9438  deg
    Mean motion:   15.56255501  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2047
    Checksum:              313
 
 
    Coasting Arc #5 (Orbit 2062)
    ---------------------------------------
 
    Vector Time (GMT): 2015/120/13:07:34.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926120.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3606941.58                 A    =         6771622.72  meter
     Y    =        2425925.84  meter          E    =           .0002148
     Z    =        5194170.41                 I    =           51.40066
     XDOT =      -5306.639908                 Wp   =          255.82255
     YDOT =       5416.995636  meter/sec      RA   =          321.39360  deg
     ZDOT =       1154.931843                 TA   =          183.06897
                                              MA   =          183.07029
                                              Ha   =            215.986  n.mi
                                              Hp   =            213.374
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11833797.84                 X    =         3554314.54
     Y    =        7959074.27  feet           Y    =         2465967.08  meter
     Z    =       17041241.49                 Z    =         5211564.49
     XDOT =     -17410.235919                 XDOT =       -5372.429944
     YDOT =      17772.295395  feet/sec       YDOT =        5357.285537  meter/sec
     ZDOT =       3789.146465                 ZDOT =        1128.992724
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13314103.83                 X    =         4058138.85
     Y    =       -4856977.42  feet           Y    =        -1480406.72  meter
     Z    =       17115313.49                 Z    =         5216747.55
     XDOT =       3869.040787                 XDOT =        1179.283632
     YDOT =      23564.259158  feet/sec       YDOT =        7182.386191  meter/sec
     ZDOT =       3676.931224                 ZDOT =        1120.728637
  
  
    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   15120.59700940  .00016717  00000-0  10270-3 0  9044
    2 25544  51.6428 321.7423 0005543 287.1487  72.9060 15.56239921 20632
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15120.59700940   =   yrday.fracday
    Element set:     904
    Inclination:       51.6428  deg
    RA of node:       321.7423  deg
    Eccentricity:     .0005543     
    Arg of perigee:   287.1487  deg
    Mean anomaly:      72.9060  deg
    Mean motion:   15.56239921  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2063
    Checksum:              300
 
 
    Coasting Arc #6 (Orbit 2077)
    ---------------------------------------
 
    Vector Time (GMT): 2015/121/13:07:34.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926120.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1521490.62                 A    =         6771828.75  meter
     Y    =       -4187427.92  meter          E    =           .0008092
     Z    =       -5107017.75                 I    =           51.37741
     XDOT =       6222.443526                 Wp   =           96.93013
     YDOT =      -4188.801541  meter/sec      RA   =          316.35220  deg
     ZDOT =       1581.949832                 TA   =          188.37848
                                              MA   =          188.39200
                                              Ha   =            216.020  n.mi
                                              Hp   =            213.118
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4991767.14                 X    =        -1449744.32
     Y    =      -13738280.57  feet           Y    =        -4204041.34  meter
     Z    =      -16755307.57                 Z    =        -5114234.48
     XDOT =      20414.840963                 XDOT =        6261.136581
     YDOT =     -13742.787209  feet/sec       YDOT =       -4119.001678  meter/sec
     ZDOT =       5190.124120                 ZDOT =        1612.271983
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14070589.63                 X    =        -4288715.72
     Y    =       -3829686.67  feet           Y    =        -1167288.50  meter
     Z    =      -16785423.18                 Z    =        -5116196.99
     XDOT =         67.795176                 XDOT =          20.663970
     YDOT =     -23553.117527  feet/sec       YDOT =       -7178.990222  meter/sec
     ZDOT =       5320.874711                 ZDOT =        1621.802612
  
  
    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   15121.56018837  .00016717  00000-0  10270-3 0  9050
    2 25544  51.6424 316.9241 0005515 289.6096  70.4462 15.56326531 20783
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15121.56018837   =   yrday.fracday
    Element set:     905
    Inclination:       51.6424  deg
    RA of node:       316.9241  deg
    Eccentricity:     .0005515     
    Arg of perigee:   289.6096  deg
    Mean anomaly:      70.4462  deg
    Mean motion:   15.56326531  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2078
    Checksum:              307
 
 
    Coasting Arc #7 (Orbit 2093)
    ---------------------------------------
 
    Vector Time (GMT): 2015/122/13:07:34.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926120.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -631235.69                 A    =         6776314.80  meter
     Y    =        5479802.48  meter          E    =           .0007054
     Z    =        3934235.84                 I    =           51.37002
     XDOT =      -6171.008715                 Wp   =           54.00920
     YDOT =       2171.404958  meter/sec      RA   =          311.31994  deg
     ZDOT =      -4005.449314                 TA   =           77.97636
                                              MA   =           77.89731
                                              Ha   =            216.181  n.mi
                                              Hp   =            213.167
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2070983.22                 X    =         -711576.65
     Y    =       17978354.59  feet           Y    =         5472294.54  meter
     Z    =       12907597.89                 Z    =         3930973.98
     XDOT =     -20246.091586                 XDOT =       -6175.373876
     YDOT =       7124.032016  feet/sec       YDOT =        2102.372131  meter/sec
     ZDOT =     -13141.237908                 ZDOT =       -4035.438165
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13740306.80                 X    =         4188045.51
     Y    =       11794154.18  feet           Y    =         3594858.19  meter
     Z    =       12892563.15                 Z    =         3929653.25
     XDOT =      -4441.994558                 XDOT =       -1353.919941
     YDOT =      19713.720182  feet/sec       YDOT =        6008.741911  meter/sec
     ZDOT =     -13270.162819                 ZDOT =       -4044.745627
  
  
    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   15122.58755494  .00016717  00000-0  10270-3 0  9061
    2 25544  51.6421 311.7852 0005668 293.3109  66.7448 15.56349842 20947
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15122.58755494   =   yrday.fracday
    Element set:     906
    Inclination:       51.6421  deg
    RA of node:       311.7852  deg
    Eccentricity:     .0005668     
    Arg of perigee:   293.3109  deg
    Mean anomaly:      66.7448  deg
    Mean motion:   15.56349842  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2094
    Checksum:              332
 
 
    Coasting Arc #8 (Orbit 2108)
    ---------------------------------------
 
    Vector Time (GMT): 2015/123/13:07:34.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926120.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2492999.75                 A    =         6781176.04  meter
     Y    =       -5997954.54  meter          E    =           .0007974
     Z    =       -1929743.79                 I    =           51.36703
     XDOT =       5250.205609                 Wp   =          356.09226
     YDOT =        388.486203  meter/sec      RA   =          306.30567  deg
     ZDOT =       5581.610096                 TA   =          342.52644
                                              MA   =          342.55387
                                              Ha   =            216.256  n.mi
                                              Hp   =            212.968
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8179133.05                 X    =         2569259.20
     Y    =      -19678328.55  feet           Y    =        -5969649.84  meter
     Z    =       -6331180.42                 Z    =        -1917447.65
     XDOT =      17225.084020                 XDOT =        5218.357295
     YDOT =       1274.561033  feet/sec       YDOT =         447.019493  meter/sec
     ZDOT =      18312.369081                 ZDOT =        5607.037760
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12080523.83                 X    =        -3682143.66
     Y    =      -17574830.20  feet           Y    =        -5356808.24  meter
     Z    =       -6277337.40                 Z    =        -1913332.44
     XDOT =       9065.605163                 XDOT =        2763.196454
     YDOT =     -12803.525240  feet/sec       YDOT =       -3902.514493  meter/sec
     ZDOT =      18421.251674                 ZDOT =        5614.797510
  
  
    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   15123.55068777  .00016717  00000-0  10270-3 0  9071
    2 25544  51.6426 306.9666 0005552 297.1387  62.9201 15.56399782 21093
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15123.55068777   =   yrday.fracday
    Element set:     907
    Inclination:       51.6426  deg
    RA of node:       306.9666  deg
    Eccentricity:     .0005552     
    Arg of perigee:   297.1387  deg
    Mean anomaly:      62.9201  deg
    Mean motion:   15.56399782  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2109
    Checksum:              338
 
 
    Coasting Arc #9 (Orbit 2124)
    ---------------------------------------
 
    Vector Time (GMT): 2015/124/13:07:34.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926120.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3857248.11                 A    =         6782376.38  meter
     Y    =        5550944.28  meter          E    =           .0005637
     Z    =        -514614.72                 I    =           51.35367
     XDOT =      -3687.132668                 Wp   =          154.58203
     YDOT =      -3112.133515  meter/sec      RA   =          301.30463  deg
     ZDOT =      -5962.094532                 TA   =           30.99573
                                              MA   =           30.96247
                                              Ha   =            216.394  n.mi
                                              Hp   =            212.754
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12655013.48                 X    =        -3916533.55
     Y    =       18211759.45  feet           Y    =         5507478.52  meter
     Z    =       -1688368.50                 Z    =         -533496.92
     XDOT =     -12096.891956                 XDOT =       -3623.095750
     YDOT =     -10210.411794  feet/sec       YDOT =       -3153.007418  meter/sec
     ZDOT =     -19560.677599                 ZDOT =       -5979.850746
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8800092.66                 X    =         2682268.24
     Y    =       20349260.25  feet           Y    =         6202454.52  meter
     Z    =       -1770342.62                 Z    =         -539600.43
     XDOT =     -13507.851591                 XDOT =       -4117.193165
     YDOT =       4141.182764  feet/sec       YDOT =        1262.232506  meter/sec
     ZDOT =     -19636.164614                 ZDOT =       -5985.102974
  
  
    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   15124.57800244  .00016717  00000-0  10270-3 0  9088
    2 25544  51.6424 301.8273 0005748 303.1843  56.8760 15.56479811 21253
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15124.57800244   =   yrday.fracday
    Element set:     908
    Inclination:       51.6424  deg
    RA of node:       301.8273  deg
    Eccentricity:     .0005748     
    Arg of perigee:   303.1843  deg
    Mean anomaly:      56.8760  deg
    Mean motion:   15.56479811  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2125
    Checksum:              305
 
 
    Coasting Arc #10 (Orbit 2140)
    ---------------------------------------
 
    Vector Time (GMT): 2015/125/13:07:34.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926120.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4570064.32                 A    =         6778956.02  meter
     Y    =       -4111091.99  meter          E    =           .0010033
     Z    =        2843343.08                 I    =           51.32728
     XDOT =       1794.362744                 Wp   =           58.21250
     YDOT =       5493.367798  meter/sec      RA   =          296.29768  deg
     ZDOT =       5050.676027                 TA   =          334.31635
                                              MA   =          334.36615
                                              Ha   =            216.308  n.mi
                                              Hp   =            212.637
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14993649.34                 X    =         4601883.68
     Y    =      -13487834.61  feet           Y    =        -4059808.67  meter
     Z    =        9328553.42                 Z    =         2865621.27
     XDOT =       5887.016876                 XDOT =        1708.266424
     YDOT =      18022.860230  feet/sec       YDOT =        5512.952073  meter/sec
     ZDOT =      16570.459406                 ZDOT =        5059.183829
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3918395.72                 X    =        -1194327.01
     Y    =      -19737589.03  feet           Y    =        -6016017.14  meter
     Z    =        9424800.61                 Z    =         2872679.22
     XDOT =      16999.179312                 XDOT =        5181.349854
     YDOT =       4566.947080  feet/sec       YDOT =        1392.005470  meter/sec
     ZDOT =      16605.864355                 ZDOT =        5061.467455
  
  
    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   15125.60529243  .00016717  00000-0  10270-3 0  9091
    2 25544  51.6430 296.6875 0005617 304.8235  55.2390 15.56492595 21411
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15125.60529243   =   yrday.fracday
    Element set:     909
    Inclination:       51.6430  deg
    RA of node:       296.6875  deg
    Eccentricity:     .0005617     
    Arg of perigee:   304.8235  deg
    Mean anomaly:      55.2390  deg
    Mean motion:   15.56492595  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2141
    Checksum:              316
 
 
    Coasting Arc #11 (Orbit 2150)
    ---------------------------------------
 
    Vector Time (GMT): 2015/126/05:26:53.328
    Vector Time (MET): N/A
    Weight (LBS)     : 925597.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4641432.08                 A    =         6775186.93  meter
     Y    =        1050259.95  meter          E    =           .0006108
     Z    =       -4827824.46                 I    =           51.29960
     XDOT =        915.428672                 Wp   =           40.47181
     YDOT =      -7207.656908  meter/sec      RA   =          292.88070  deg
     ZDOT =      -2445.241316                 TA   =          205.38900
                                              MA   =          205.41902
                                              Ha   =            216.628  n.mi
                                              Hp   =            215.195
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15227795.54                 X    =        -4629379.15
     Y    =        3445734.75  feet           Y    =          998423.93  meter
     Z    =      -15839319.11                 Z    =        -4850342.78
     XDOT =       3003.374909                 XDOT =        1007.836671
     YDOT =     -23647.168333  feet/sec       YDOT =       -7196.903244  meter/sec
     ZDOT =      -8022.445264                 ZDOT =       -2440.569973
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11432946.46                 X    =        -3484762.08
     Y    =      -10486857.31  feet           Y    =        -3196394.11  meter
     Z    =      -15936010.60                 Z    =        -4857296.03
     XDOT =      20426.625535                 XDOT =        6226.035463
     YDOT =     -10096.929227  feet/sec       YDOT =       -3077.544028  meter/sec
     ZDOT =      -8001.054029                 ZDOT =       -2438.721268
  
  
    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   15126.24734467  .00016717  00000-0  10270-3 0  9100
    2 25544  51.6463 293.4808 0007354 278.5605  81.4715 15.55549506 21513
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15126.24734467   =   yrday.fracday
    Element set:     910
    Inclination:       51.6463  deg
    RA of node:       293.4808  deg
    Eccentricity:     .0007354     
    Arg of perigee:   278.5605  deg
    Mean anomaly:      81.4715  deg
    Mean motion:   15.55549506  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2151
    Checksum:              317
 
 
    Coasting Arc #12 (Orbit 2166)
    ---------------------------------------
 
    Vector Time (GMT): 2015/127/05:26:53.328
    Vector Time (MET): N/A
    Weight (LBS)     : 925597.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4048440.67                 A    =         6773078.92  meter
     Y    =        1255930.95  meter          E    =           .0005194
     Z    =        5287047.24                 I    =           51.28142
     XDOT =      -2318.344596                 Wp   =          286.93716
     YDOT =       7308.626971  meter/sec      RA   =          287.84251  deg
     ZDOT =         40.587314                 TA   =          162.68298
                                              MA   =          162.66526
                                              Ha   =            216.890  n.mi
                                              Hp   =            215.484
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13282285.67                 X    =         4008412.74
     Y    =        4120508.36  feet           Y    =         1300979.26  meter
     Z    =       17345955.50                 Z    =         5306616.92
     XDOT =      -7606.117441                 XDOT =       -2400.096259
     YDOT =      23978.434943  feet/sec       YDOT =        7282.244625  meter/sec
     ZDOT =        133.160480                 ZDOT =          29.126743
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4322806.52                 X    =         1317591.43
     Y    =       13107367.80  feet           Y    =         3995125.71  meter
     Z    =       17429576.22                 Z    =         5312534.83
     XDOT =     -22965.121514                 XDOT =       -6999.769038
     YDOT =       7470.568730  feet/sec       YDOT =        2277.029349  meter/sec
     ZDOT =         82.663953                 ZDOT =          25.195973
  
  
    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   15127.27523717  .00016717  00000-0  10270-3 0  9119
    2 25544  51.6463 288.3456 0007535 282.2541  77.7769 15.55596171 21671
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15127.27523717   =   yrday.fracday
    Element set:     911
    Inclination:       51.6463  deg
    RA of node:       288.3456  deg
    Eccentricity:     .0007535     
    Arg of perigee:   282.2541  deg
    Mean anomaly:      77.7769  deg
    Mean motion:   15.55596171  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2167
    Checksum:              334
 
 
    Coasting Arc #13 (Orbit 2181)
    ---------------------------------------
 
    Vector Time (GMT): 2015/128/05:26:53.328
    Vector Time (MET): N/A
    Weight (LBS)     : 925597.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3195287.27                 A    =         6774945.22  meter
     Y    =       -3491795.08  meter          E    =           .0004328
     Z    =       -4851489.48                 I    =           51.27945
     XDOT =       3419.736286                 Wp   =          108.08339
     YDOT =      -6436.065684  meter/sec      RA   =          282.80318  deg
     ZDOT =       2380.400014                 TA   =          185.36341
                                              MA   =          185.36804
                                              Ha   =            217.092  n.mi
                                              Hp   =            215.188
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10483225.94                 X    =        -3132436.68
     Y    =      -11456020.59  feet           Y    =        -3527175.26  meter
     Z    =      -15916960.23                 Z    =        -4866859.24
     XDOT =      11219.607238                 XDOT =        3479.888499
     YDOT =     -21115.701063  feet/sec       YDOT =       -6397.487722  meter/sec
     ZDOT =       7809.711333                 ZDOT =        2397.158499
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3004191.12                 X    =          915677.45
     Y    =      -15166846.46  feet           Y    =        -4622854.80  meter
     Z    =      -15982166.97                 Z    =        -4871364.49
     XDOT =      22504.210694                 XDOT =        6859.283420
     YDOT =      -3847.449071  feet/sec       YDOT =       -1172.702477  meter/sec
     ZDOT =       7882.739277                 ZDOT =        2402.658932
  
  
    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   15128.23886484  .00016717  00000-0  10270-3 0  9120
    2 25544  51.6467 283.5314 0007570 286.8131  73.2192 15.55610955 21824
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15128.23886484   =   yrday.fracday
    Element set:     912
    Inclination:       51.6467  deg
    RA of node:       283.5314  deg
    Eccentricity:     .0007570     
    Arg of perigee:   286.8131  deg
    Mean anomaly:      73.2192  deg
    Mean motion:   15.55610955  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2182
    Checksum:              318
 
 
    Coasting Arc #14 (Orbit 2197)
    ---------------------------------------
 
    Vector Time (GMT): 2015/129/05:26:53.328
    Vector Time (MET): N/A
    Weight (LBS)     : 925597.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2160717.17                 A    =         6779454.09  meter
     Y    =        5340499.62  meter          E    =           .0006033
     Z    =        3572643.51                 I    =           51.28853
     XDOT =      -4203.428861                 Wp   =           55.33807
     YDOT =       4656.818943  meter/sec      RA   =          277.77578  deg
     ZDOT =      -4410.250736                 TA   =           82.17608
                                              MA   =           82.10760
                                              Ha   =            217.428  n.mi
                                              Hp   =            215.050
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7088967.09                 X    =         2083483.11
     Y    =       17521324.21  feet           Y    =         5364230.20  meter
     Z    =       11721271.37                 Z    =         3582952.56
     XDOT =     -13790.777103                 XDOT =       -4233.766561
     YDOT =      15278.277371  feet/sec       YDOT =        4609.643987  meter/sec
     ZDOT =     -14469.326563                 ZDOT =       -4430.743891
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9602701.49                 X    =        -2926903.41
     Y    =       16248821.81  feet           Y    =         4952640.89  meter
     Z    =       11764453.79                 Z    =         3585805.51
     XDOT =     -19277.048927                 XDOT =       -5875.644513
     YDOT =       -831.457579  feet/sec       YDOT =        -253.428270  meter/sec
     ZDOT =     -14558.020341                 ZDOT =       -4437.284600
  
  
    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   15129.26670909  .00016717  00000-0  10270-3 0  9138
    2 25544  51.6465 278.3965 0007573 291.5182  68.5164 15.55648693 21981
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15129.26670909   =   yrday.fracday
    Element set:     913
    Inclination:       51.6465  deg
    RA of node:       278.3965  deg
    Eccentricity:     .0007573     
    Arg of perigee:   291.5182  deg
    Mean anomaly:      68.5164  deg
    Mean motion:   15.55648693  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2198
    Checksum:              353
 
 
    Coasting Arc #15 (Orbit 2212)
    ---------------------------------------
 
    Vector Time (GMT): 2015/130/05:26:53.328
    Vector Time (MET): N/A
    Weight (LBS)     : 925597.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1026898.54                 A    =         6783601.09  meter
     Y    =       -6487132.72  meter          E    =           .0009670
     Z    =       -1670694.63                 I    =           51.29958
     XDOT =       4663.476978                 Wp   =          346.59180
     YDOT =      -2200.795190  meter/sec      RA   =          272.76374  deg
     ZDOT =       5681.658263                 TA   =          354.99418
                                              MA   =          355.00385
                                              Ha   =            217.536  n.mi
                                              Hp   =            214.880
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3369089.71                 X    =         -946165.89
     Y    =      -21283243.84  feet           Y    =        -6498164.73  meter
     Z    =       -5481281.58                 Z    =        -1675487.21
     XDOT =      15300.121319                 XDOT =        4660.140632
     YDOT =      -7220.456660  feet/sec       YDOT =       -2148.663946  meter/sec
     ZDOT =      18640.611100                 ZDOT =        5704.304528
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14557210.79                 X    =         4437037.85
     Y    =      -15880883.28  feet           Y    =        -4840493.22  meter
     Z    =       -5500621.97                 Z    =        -1676589.58
     XDOT =      13953.217314                 XDOT =        4252.940637
     YDOT =       6302.926729  feet/sec       YDOT =        1921.132067  meter/sec
     ZDOT =      18738.074017                 ZDOT =        5711.364960
  
  
    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   15130.23028887  .00016717  00000-0  10270-3 0  9140
    2 25544  51.6467 273.5815 0007740 295.2562  64.7790 15.55689236 22132
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15130.23028887   =   yrday.fracday
    Element set:     914
    Inclination:       51.6467  deg
    RA of node:       273.5815  deg
    Eccentricity:     .0007740     
    Arg of perigee:   295.2562  deg
    Mean anomaly:      64.7790  deg
    Mean motion:   15.55689236  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2213
    Checksum:              326
 
 
    Coasting Arc #16 (Orbit 2228)
    ---------------------------------------
 
    Vector Time (GMT): 2015/131/05:26:53.328
    Vector Time (MET): N/A
    Weight (LBS)     : 925597.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -171984.09                 A    =         6784691.77  meter
     Y    =        6757591.44  meter          E    =           .0004603
     Z    =        -543823.97                 I    =           51.30216
     XDOT =      -4796.103477                 Wp   =          175.55440
     YDOT =       -600.513364  meter/sec      RA   =          267.76276  deg
     ZDOT =      -5953.150695                 TA   =           10.34309
                                              MA   =           10.33362
                                              Ha   =            217.751  n.mi
                                              Hp   =            214.741
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -564252.25                 X    =         -244894.59
     Y    =       22170575.58  feet           Y    =         6755260.54  meter
     Z    =       -1784199.38                 Z    =         -544836.46
     XDOT =     -15735.247629                 XDOT =       -4760.113575
     YDOT =      -1970.188203  feet/sec       YDOT =        -653.945228  meter/sec
     ZDOT =     -19531.334301                 ZDOT =       -5976.361975
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17441640.20                 X    =        -5316211.93
     Y    =       13697520.32  feet           Y    =         4175004.19  meter
     Z    =       -1789774.73                 Z    =         -545523.34
     XDOT =      -7426.058681                 XDOT =       -2263.462686
     YDOT =     -12017.572888  feet/sec       YDOT =       -3662.956216  meter/sec
     ZDOT =     -19630.706385                 ZDOT =       -5983.439306
  
  
    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   15131.25808388  .00016717  00000-0  10270-3 0  9156
    2 25544  51.6463 268.4462 0007747 298.1227  61.9143 15.55680681 22299
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15131.25808388   =   yrday.fracday
    Element set:     915
    Inclination:       51.6463  deg
    RA of node:       268.4462  deg
    Eccentricity:     .0007747     
    Arg of perigee:   298.1227  deg
    Mean anomaly:      61.9143  deg
    Mean motion:   15.55680681  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2229
    Checksum:              329
 
 
    Coasting Arc #17 (Orbit 2244)
    ---------------------------------------
 
    Vector Time (GMT): 2015/132/05:26:53.328
    Vector Time (MET): N/A
    Weight (LBS)     : 925597.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1382257.76                 A    =         6781587.09  meter
     Y    =       -6072843.45  meter          E    =           .0009833
     Z    =        2666747.19                 I    =           51.29393
     XDOT =       4598.224829                 Wp   =           42.61676
     YDOT =       3318.815400  meter/sec      RA   =          262.75648  deg
     ZDOT =       5170.273357                 TA   =          347.67442
                                              MA   =          347.69845
                                              Ha   =            217.899  n.mi
                                              Hp   =            214.392
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4534966.39                 X    =         1437108.85
     Y    =      -19924027.05  feet           Y    =        -6057079.44  meter
     Z    =        8749170.59                 Z    =         2673595.23
     XDOT =      15086.039464                 XDOT =        4535.655845
     YDOT =      10888.501970  feet/sec       YDOT =        3369.885926  meter/sec
     ZDOT =      16962.839098                 ZDOT =        5192.458832
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18049155.44                 X    =         5501382.58
     Y    =       -9551283.16  feet           Y    =        -2911231.11  meter
     Z    =        8779620.60                 Z    =         2676028.36
     XDOT =        768.749896                 XDOT =         234.314968
     YDOT =      17144.241482  feet/sec       YDOT =        5225.564804  meter/sec
     ZDOT =      17057.327684                 ZDOT =        5199.073478
  
  
    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   15132.28585193  .00016717  00000-0  10270-3 0  9167
    2 25544  51.6456 263.3093 0007956 304.0703  55.9695 15.55746495 22452
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15132.28585193   =   yrday.fracday
    Element set:     916
    Inclination:       51.6456  deg
    RA of node:       263.3093  deg
    Eccentricity:     .0007956     
    Arg of perigee:   304.0703  deg
    Mean anomaly:      55.9695  deg
    Mean motion:   15.55746495  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2245
    Checksum:              333
 
             

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