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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  9687.52
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   126.0
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.637
   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 
   ------------------------------------------------------------------------
   191/02:58:39.135           3.2               3.9              3.9    
   N/A                       -2.1              -0.4              219.4  
   000/00:11:54.271           0.6               0.0              214.0  
   
 
 
    Coasting Arc #1 (Orbit 3104)
    ---------------------------------------
 
    Vector Time (GMT): 2015/187/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892160.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3191407.64                 A    =         6777611.18  meter
     Y    =        4198003.15  meter          E    =           .0011991
     Z    =        4247951.96                 I    =           51.55753
     XDOT =      -6636.084060                 Wp   =           85.34006
     YDOT =      -1396.552447  meter/sec      RA   =          346.99317  deg
     ZDOT =      -3595.734396                 TA   =           41.43947
                                              MA   =           41.34859
                                              Ha   =            219.764  n.mi
                                              Hp   =            211.588
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10470497.50                 X    =        -3258748.21
     Y    =       13772976.23  feet           Y    =         4161937.92  meter
     Z    =       13936850.26                 Z    =         4232285.66
     XDOT =     -21771.929330                 XDOT =       -6602.507768
     YDOT =      -4581.864985  feet/sec       YDOT =       -1470.573494  meter/sec
     ZDOT =     -11797.028858                 ZDOT =       -3627.889331
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15835613.66                 X    =         4826695.04
     Y    =        7103326.52  feet           Y    =         2165093.92  meter
     Z    =       13868600.50                 Z    =         4227149.43
     XDOT =       1054.396959                 XDOT =         321.380193
     YDOT =      21013.877749  feet/sec       YDOT =        6405.029938  meter/sec
     ZDOT =     -11935.008776                 ZDOT =       -3637.790675
  
  
    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   15187.54157560  .00016717  00000-0  10270-3 0  9002
    2 25544  51.6407 347.3666 0002960 129.9602 230.1812 15.55544982 31050
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15187.54157560   =   yrday.fracday
    Element set:     900
    Inclination:       51.6407  deg
    RA of node:       347.3666  deg
    Eccentricity:     .0002960     
    Arg of perigee:   129.9602  deg
    Mean anomaly:     230.1812  deg
    Mean motion:   15.55544982  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3105
    Checksum:              306
 
 
    Coasting Arc #2 (Orbit 3119)
    ---------------------------------------
 
    Vector Time (GMT): 2015/188/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892160.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4967142.51                 A    =         6782247.13  meter
     Y    =       -3804075.83  meter          E    =           .0006337
     Z    =       -2621922.27                 I    =           51.54396
     XDOT =       4875.906651                 Wp   =           79.57822
     YDOT =       2775.772843  meter/sec      RA   =          341.99348  deg
     ZDOT =       5221.819830                 TA   =          250.84643
                                              MA   =          250.91504
                                              Ha   =            219.644  n.mi
                                              Hp   =            211.580
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16296399.31                 X    =         5022047.62
     Y    =      -12480563.76  feet           Y    =        -3748222.84  meter
     Z    =       -8602107.17                 Z    =        -2597659.96
     XDOT =      15997.069065                 XDOT =        4819.139511
     YDOT =       9106.866282  feet/sec       YDOT =        2829.980700  meter/sec
     ZDOT =      17131.954822                 ZDOT =        5245.368099
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16133084.09                 X    =        -4917364.03
     Y    =      -12761590.85  feet           Y    =        -3889732.89  meter
     Z    =       -8496984.56                 Z    =        -2589880.89
     XDOT =       3971.701757                 XDOT =        1210.574696
     YDOT =     -16468.643255  feet/sec       YDOT =       -5019.642464  meter/sec
     ZDOT =      17232.631062                 ZDOT =        5252.505948
  
  
    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   15188.50520785  .00016717  00000-0  10270-3 0  9013
    2 25544  51.6420 342.5523 0003010 132.7661 227.3746 15.55584669 31205
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15188.50520785   =   yrday.fracday
    Element set:     901
    Inclination:       51.6420  deg
    RA of node:       342.5523  deg
    Eccentricity:     .0003010     
    Arg of perigee:   132.7661  deg
    Mean anomaly:     227.3746  deg
    Mean motion:   15.55584669  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3120
    Checksum:              292
 
 
    Coasting Arc #3 (Orbit 3135)
    ---------------------------------------
 
    Vector Time (GMT): 2015/189/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892160.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6052357.16                 A    =         6784906.47  meter
     Y    =        3006955.47  meter          E    =           .0015721
     Z    =         507972.22                 I    =           51.52247
     XDOT =      -2540.309588                 Wp   =          130.47083
     YDOT =      -4084.187618  meter/sec      RA   =          337.00562  deg
     ZDOT =      -5978.918697                 TA   =           44.03507
                                              MA   =           43.90995
                                              Ha   =            219.467  n.mi
                                              Hp   =            211.585
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19856814.82                 X    =        -6087999.35
     Y    =        9865339.46  feet           Y    =         2939074.72  meter
     Z    =        1666575.52                 Z    =          478484.84
     XDOT =      -8334.349042                 XDOT =       -2465.407253
     YDOT =     -13399.565677  feet/sec       YDOT =       -4112.175848  meter/sec
     ZDOT =     -19615.874990                 ZDOT =       -5991.077279
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14753789.61                 X    =         4496955.07
     Y    =       16563579.52  feet           Y    =         5048579.04  meter
     Z    =        1539161.11                 Z    =          469136.31
     XDOT =      -9555.435643                 XDOT =       -2912.496784
     YDOT =      10375.840417  feet/sec       YDOT =        3162.556159  meter/sec
     ZDOT =     -19667.301952                 ZDOT =       -5994.593635
  
  
    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   15189.53306993  .00016717  00000-0  10270-3 0  9021
    2 25544  51.6412 337.4164 0002808 135.4775 224.6604 15.55620135 31369
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15189.53306993   =   yrday.fracday
    Element set:     902
    Inclination:       51.6412  deg
    RA of node:       337.4164  deg
    Eccentricity:     .0002808     
    Arg of perigee:   135.4775  deg
    Mean anomaly:     224.6604  deg
    Mean motion:   15.55620135  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3136
    Checksum:              304
 
 
    Coasting Arc #4 (Orbit 3151)
    ---------------------------------------
 
    Vector Time (GMT): 2015/190/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892160.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6304804.15                 A    =         6783708.07  meter
     Y    =       -1857664.48  meter          E    =           .0014941
     Z    =        1655877.30                 I    =           51.49114
     XDOT =          5.083277                 Wp   =           75.04932
     YDOT =       5133.786798  meter/sec      RA   =          332.01907  deg
     ZDOT =       5700.787780                 TA   =          303.14223
                                              MA   =          303.28550
                                              Ha   =            219.426  n.mi
                                              Hp   =            211.506
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20685053.00                 X    =         6317064.81
     Y    =       -6094699.75  feet           Y    =        -1787091.60  meter
     Z    =        5432668.31                 Z    =         1686534.36
     XDOT =         16.677418                 XDOT =         -80.016535
     YDOT =      16843.132541  feet/sec       YDOT =        5133.367405  meter/sec
     ZDOT =      18703.371981                 ZDOT =        5700.606151
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11635633.30                 X    =        -3546541.03
     Y    =      -18115600.51  feet           Y    =        -5521635.04  meter
     Z    =        5564865.08                 Z    =         1696170.88
     XDOT =      14877.940287                 XDOT =        4534.796200
     YDOT =      -3772.613421  feet/sec       YDOT =       -1149.892571  meter/sec
     ZDOT =      18701.523230                 ZDOT =        5700.224280
  
  
    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   15190.56092059  .00016717  00000-0  10270-3 0  9032
    2 25544  51.6424 332.2810 0002978 140.8775 219.2594 15.55644453 31526
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15190.56092059   =   yrday.fracday
    Element set:     903
    Inclination:       51.6424  deg
    RA of node:       332.2810  deg
    Eccentricity:     .0002978     
    Arg of perigee:   140.8775  deg
    Mean anomaly:     219.2594  deg
    Mean motion:   15.55644453  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3152
    Checksum:              312
 
 
    Coasting Arc #5 (Orbit 3160)
    ---------------------------------------
 
    Vector Time (GMT): 2015/191/03:04:36.271
    Vector Time (MET): N/A
    Weight (LBS)     : 891730.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         869706.24                 A    =         6777979.77  meter
     Y    =       -4859778.99  meter          E    =           .0009795
     Z    =       -4653730.27                 I    =           51.44856
     XDOT =       6936.677952                 Wp   =          119.35214
     YDOT =      -1514.526230  meter/sec      RA   =          328.83904  deg
     ZDOT =       2877.812092                 TA   =          179.35511
                                              MA   =          179.35385
                                              Ha   =            219.400  n.mi
                                              Hp   =            213.960
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2853366.91                 X    =          946590.83
     Y    =      -15944156.81  feet           Y    =        -4849623.10  meter
     Z    =      -15268143.93                 Z    =        -4649319.07
     XDOT =      22758.129763                 XDOT =        6939.118900
     YDOT =      -4968.918078  feet/sec       YDOT =       -1436.942344  meter/sec
     ZDOT =       9441.640721                 ZDOT =        2911.514852
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9858970.44                 X    =         3005014.19
     Y    =      -12875096.18  feet           Y    =        -3924329.31  meter
     Z    =      -15248169.01                 Z    =        -4647641.92
     XDOT =      21544.384508                 XDOT =        6566.728398
     YDOT =       5143.049443  feet/sec       YDOT =        1567.601470  meter/sec
     ZDOT =       9586.857263                 ZDOT =        2922.074094
  
  
    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   15191.13908314  .00016717  00000-0  10270-3 0  9047
    2 25544  51.6440 329.3958 0001887 225.1426 134.9574 15.54885070 31614
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15191.13908314   =   yrday.fracday
    Element set:     904
    Inclination:       51.6440  deg
    RA of node:       329.3958  deg
    Eccentricity:     .0001887     
    Arg of perigee:   225.1426  deg
    Mean anomaly:     134.9574  deg
    Mean motion:   15.54885070  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3161
    Checksum:              315
 
 
    Coasting Arc #6 (Orbit 3176)
    ---------------------------------------
 
    Vector Time (GMT): 2015/192/03:04:36.271
    Vector Time (MET): N/A
    Weight (LBS)     : 891730.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2601488.81                 A    =         6782275.93  meter
     Y    =        5255799.38  meter          E    =           .0011181
     Z    =        3396107.26                 I    =           51.43590
     XDOT =      -6138.730448                 Wp   =           96.57147
     YDOT =        -57.212344  meter/sec      RA   =          323.83114  deg
     ZDOT =      -4602.065600                 TA   =           43.56842
                                              MA   =           43.48017
                                              Ha   =            219.396  n.mi
                                              Hp   =            213.981
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8535068.28                 X    =        -2676564.05
     Y    =       17243436.29  feet           Y    =         5226287.72  meter
     Z    =       11142084.18                 Z    =         3383287.94
     XDOT =     -20140.191759                 XDOT =       -6115.279392
     YDOT =       -187.704540  feet/sec       YDOT =        -125.728067  meter/sec
     ZDOT =     -15098.640421                 ZDOT =       -4631.829333
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15288999.98                 X    =        -4660087.19
     Y    =       11733680.15  feet           Y    =         3576425.71  meter
     Z    =       11085880.90                 Z    =         3378976.50
     XDOT =     -17080.644697                 XDOT =       -5206.180504
     YDOT =      -7833.422452  feet/sec       YDOT =       -2387.627163  meter/sec
     ZDOT =     -15226.591969                 ZDOT =       -4641.065232
  
  
    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   15192.16741098  .00016717  00000-0  10270-3 0  9056
    2 25544  51.6437 324.2636 0001860 228.3288 131.7706 15.54887399 31774
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15192.16741098   =   yrday.fracday
    Element set:     905
    Inclination:       51.6437  deg
    RA of node:       324.2636  deg
    Eccentricity:     .0001860     
    Arg of perigee:   228.3288  deg
    Mean anomaly:     131.7706  deg
    Mean motion:   15.54887399  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3177
    Checksum:              334
 
 
    Coasting Arc #7 (Orbit 3191)
    ---------------------------------------
 
    Vector Time (GMT): 2015/193/03:04:36.271
    Vector Time (MET): N/A
    Weight (LBS)     : 891730.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3953187.90                 A    =         6785831.28  meter
     Y    =       -5246868.51  meter          E    =           .0006018
     Z    =       -1689668.22                 I    =           51.42384
     XDOT =       4819.952381                 Wp   =           32.00323
     YDOT =       1806.182877  meter/sec      RA   =          318.83381  deg
     ZDOT =       5682.502067                 TA   =          309.41698
                                              MA   =          309.47023
                                              Ha   =            219.238  n.mi
                                              Hp   =            213.986
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12969776.59                 X    =         4019773.57
     Y    =      -17214135.53  feet           Y    =        -5202288.88  meter
     Z    =       -5543530.89                 Z    =        -1670303.35
     XDOT =      15813.492064                 XDOT =        4771.793648
     YDOT =       5925.796839  feet/sec       YDOT =        1859.812826  meter/sec
     ZDOT =      18643.379484                 ZDOT =        5705.799586
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19059502.01                 X    =         5809336.21
     Y    =      -10109644.16  feet           Y    =        -3081419.54  meter
     Z    =       -5459192.21                 Z    =        -1663961.79
     XDOT =      10984.165001                 XDOT =        3347.973492
     YDOT =      10612.669704  feet/sec       YDOT =        3234.741726  meter/sec
     ZDOT =      18743.168882                 ZDOT =        5712.917875
  
  
    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   15193.13145673  .00016717  00000-0  10270-3 0  9062
    2 25544  51.6445 319.4514 0001888 235.9786 124.1188 15.54926475 31927
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15193.13145673   =   yrday.fracday
    Element set:     906
    Inclination:       51.6445  deg
    RA of node:       319.4514  deg
    Eccentricity:     .0001888     
    Arg of perigee:   235.9786  deg
    Mean anomaly:     124.1188  deg
    Mean motion:   15.54926475  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3192
    Checksum:              333
 
 
    Coasting Arc #8 (Orbit 3207)
    ---------------------------------------
 
    Vector Time (GMT): 2015/194/03:04:36.271
    Vector Time (MET): N/A
    Weight (LBS)     : 891730.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4852310.61                 A    =         6787037.51  meter
     Y    =        4728284.44  meter          E    =           .0011243
     Z    =        -281143.29                 I    =           51.40472
     XDOT =      -3168.011068                 Wp   =          146.52367
     YDOT =      -3599.731279  meter/sec      RA   =          313.84366  deg
     ZDOT =      -5986.786525                 TA   =           36.51720
                                              MA   =           36.44059
                                              Ha   =            219.190  n.mi
                                              Hp   =            214.051
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15919654.24                 X    =        -4903457.11
     Y    =       15512744.23  feet           Y    =         4673736.78  meter
     Z    =        -922386.14                 Z    =         -304838.35
     XDOT =     -10393.737099                 XDOT =       -3098.441225
     YDOT =     -11810.141991  feet/sec       YDOT =       -3634.768344  meter/sec
     ZDOT =     -19641.688073                 ZDOT =       -6002.007444
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20847565.27                 X    =        -6354337.89
     Y    =        7698009.19  feet           Y    =         2346353.20  meter
     Z    =       -1025230.62                 Z    =         -312490.29
     XDOT =      -4014.285681                 XDOT =       -1223.554275
     YDOT =     -13447.303357  feet/sec       YDOT =       -4098.738063  meter/sec
     ZDOT =     -19706.387429                 ZDOT =       -6006.506888
  
  
    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   15194.15976263  .00016717  00000-0  10270-3 0  9073
    2 25544  51.6448 314.3188 0001948 238.6954 121.4008 15.54903043 32080
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15194.15976263   =   yrday.fracday
    Element set:     907
    Inclination:       51.6448  deg
    RA of node:       314.3188  deg
    Eccentricity:     .0001948     
    Arg of perigee:   238.6954  deg
    Mean anomaly:     121.4008  deg
    Mean motion:   15.54903043  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3208
    Checksum:              317
 
 
    Coasting Arc #9 (Orbit 3223)
    ---------------------------------------
 
    Vector Time (GMT): 2015/195/03:04:36.271
    Vector Time (MET): N/A
    Weight (LBS)     : 891730.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5234428.60                 A    =         6784884.77  meter
     Y    =       -3710336.05  meter          E    =           .0012071
     Z    =        2189234.65                 I    =           51.37670
     XDOT =       1401.410205                 Wp   =           71.24353
     YDOT =       5208.074161  meter/sec      RA   =          308.84991  deg
     ZDOT =       5455.048042                 TA   =          313.17143
                                              MA   =          313.27224
                                              Ha   =            219.081  n.mi
                                              Hp   =            213.979
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17173322.19                 X    =         5264895.08
     Y    =      -12173018.54  feet           Y    =        -3651631.16  meter
     Z    =        7182528.36                 Z    =         2214735.74
     XDOT =       4597.802511                 XDOT =        1316.569847
     YDOT =      17086.857484  feet/sec       YDOT =        5223.270617  meter/sec
     ZDOT =      17897.139247                 ZDOT =        5461.650307
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       20523127.84                 X    =         6255449.37
     Y    =       -4506501.28  feet           Y    =        -1373581.59  meter
     Z    =        7292925.29                 Z    =         2222883.63
     XDOT =      -2883.534309                 XDOT =        -878.901257
     YDOT =      15984.682249  feet/sec       YDOT =        4872.131149  meter/sec
     ZDOT =      17924.461074                 ZDOT =        5463.375735
  
  
    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   15195.18805660  .00016717  00000-0  10270-3 0  9080
    2 25544  51.6449 309.1860 0001808 250.5635 109.5323 15.54937373 32242
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15195.18805660   =   yrday.fracday
    Element set:     908
    Inclination:       51.6449  deg
    RA of node:       309.1860  deg
    Eccentricity:     .0001808     
    Arg of perigee:   250.5635  deg
    Mean anomaly:     109.5323  deg
    Mean motion:   15.54937373  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3224
    Checksum:              316
 
 
    Coasting Arc #10 (Orbit 3238)
    ---------------------------------------
 
    Vector Time (GMT): 2015/196/03:04:36.271
    Vector Time (MET): N/A
    Weight (LBS)     : 891730.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5155054.47                 A    =         6780621.27  meter
     Y    =        2201805.07  meter          E    =           .0004268
     Z    =       -3819526.43                 I    =           51.34371
     XDOT =        321.794244                 Wp   =           74.64534
     YDOT =      -6436.930033  meter/sec      RA   =          303.84487  deg
     ZDOT =      -4147.719318                 TA   =          151.49760
                                              MA   =          151.47426
                                              Ha   =            218.959  n.mi
                                              Hp   =            213.965
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16912908.36                 X    =        -5160738.90
     Y    =        7223769.91  feet           Y    =         2144126.53  meter
     Z    =      -12531254.69                 Z    =        -3844581.86
     XDOT =       1055.755395                 XDOT =         413.897385
     YDOT =     -21118.536854  feet/sec       YDOT =       -6432.816061  meter/sec
     ZDOT =     -13608.003013                 ZDOT =       -4145.933165
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18312875.38                 X    =        -5581764.42
     Y    =         381010.80  feet           Y    =          116132.09  meter
     Z    =      -12639426.05                 Z    =        -3852497.06
     XDOT =       9009.103332                 XDOT =        2745.974696
     YDOT =     -17813.690993  feet/sec       YDOT =       -5429.613015  meter/sec
     ZDOT =     -13599.019512                 ZDOT =       -4144.981147
  
  
    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   15196.15207136  .00016717  00000-0  10270-3 0  9093
    2 25544  51.6451 304.3745 0002016 255.7013 104.3917 15.54958743 32395
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15196.15207136   =   yrday.fracday
    Element set:     909
    Inclination:       51.6451  deg
    RA of node:       304.3745  deg
    Eccentricity:     .0002016     
    Arg of perigee:   255.7013  deg
    Mean anomaly:     104.3917  deg
    Mean motion:   15.54958743  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3239
    Checksum:              302
 
 
    Coasting Arc #11 (Orbit 3254)
    ---------------------------------------
 
    Vector Time (GMT): 2015/197/03:04:36.271
    Vector Time (MET): N/A
    Weight (LBS)     : 891730.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4671801.02                 A    =         6776573.66  meter
     Y    =        -361752.37  meter          E    =           .0005308
     Z    =        4893511.98                 I    =           51.31339
     XDOT =      -1831.680634                 Wp   =          134.92820
     YDOT =       7095.463151  meter/sec      RA   =          298.82430  deg
     ZDOT =       2268.027153                 TA   =          292.78603
                                              MA   =          292.84211
                                              Ha   =            218.869  n.mi
                                              Hp   =            213.992
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15327431.15                 X    =         4651728.58
     Y    =       -1186851.60  feet           Y    =         -309621.97  meter
     Z    =       16054829.33                 Z    =         4916157.49
     XDOT =      -6009.450899                 XDOT =       -1921.904703
     YDOT =      23279.078580  feet/sec       YDOT =        7074.475390  meter/sec
     ZDOT =       7441.033965                 ZDOT =        2258.910958
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14634920.75                 X    =         4460723.85
     Y    =        4361151.43  feet           Y    =         1329278.96  meter
     Z    =       16152267.95                 Z    =         4923211.27
     XDOT =     -13694.746094                 XDOT =       -4174.158609
     YDOT =      18484.639006  feet/sec       YDOT =        5634.117969  meter/sec
     ZDOT =       7400.415101                 ZDOT =        2255.646523
  
  
    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   15197.18034486  .00016717  00000-0  10270-3 0  9105
    2 25544  51.6452 299.2419 0001834 260.7672  99.3274 15.54973796 32552
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15197.18034486   =   yrday.fracday
    Element set:     910
    Inclination:       51.6452  deg
    RA of node:       299.2419  deg
    Eccentricity:     .0001834     
    Arg of perigee:   260.7672  deg
    Mean anomaly:      99.3274  deg
    Mean motion:   15.54973796  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3255
    Checksum:              341
 
 
    Coasting Arc #12 (Orbit 3269)
    ---------------------------------------
 
    Vector Time (GMT): 2015/198/03:04:36.271
    Vector Time (MET): N/A
    Weight (LBS)     : 891730.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3906487.99                 A    =         6774763.88  meter
     Y    =       -1654279.67  meter          E    =           .0012918
     Z    =       -5293277.79                 I    =           51.29242
     XDOT =       3050.022026                 Wp   =           89.87087
     YDOT =      -7026.993233  meter/sec      RA   =          293.79216  deg
     ZDOT =        -54.923975                 TA   =          179.60321
                                              MA   =          179.60218
                                              Ha   =            218.878  n.mi
                                              Hp   =            213.834
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12816561.64                 X    =        -3861986.84
     Y    =       -5427426.73  feet           Y    =        -1697715.29  meter
     Z    =      -17366396.94                 Z    =        -5312146.44
     XDOT =      10006.633942                 XDOT =        3128.639664
     YDOT =     -23054.439741  feet/sec       YDOT =       -6992.446306  meter/sec
     ZDOT =       -180.196768                 ZDOT =         -39.917515
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10072650.73                 X    =        -3070143.94
     Y    =       -9457798.93  feet           Y    =        -2882737.11  meter
     Z    =      -17447197.56                 Z    =        -5317905.82
     XDOT =      16618.574046                 XDOT =        5065.341369
     YDOT =     -17488.659735  feet/sec       YDOT =       -5330.543487  meter/sec
     ZDOT =       -114.280543                 ZDOT =         -34.832709
  
  
    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   15198.14433992  .00016717  00000-0  10270-3 0  9118
    2 25544  51.6444 294.4296 0001971 267.5719  92.5209 15.55018798 32705
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15198.14433992   =   yrday.fracday
    Element set:     911
    Inclination:       51.6444  deg
    RA of node:       294.4296  deg
    Eccentricity:     .0001971     
    Arg of perigee:   267.5719  deg
    Mean anomaly:      92.5209  deg
    Mean motion:   15.55018798  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3270
    Checksum:              337
 
 
    Coasting Arc #13 (Orbit 3285)
    ---------------------------------------
 
    Vector Time (GMT): 2015/199/03:04:36.271
    Vector Time (MET): N/A
    Weight (LBS)     : 891730.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2947705.61                 A    =         6776272.42  meter
     Y    =        3598394.04  meter          E    =           .0004839
     Z    =        4925836.39                 I    =           51.28578
     XDOT =      -3946.212686                 Wp   =           43.18783
     YDOT =       6209.837661  meter/sec      RA   =          288.75956  deg
     ZDOT =      -2170.157258                 TA   =           68.09598
                                              MA   =           68.04454
                                              Ha   =            218.698  n.mi
                                              Hp   =            213.978
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9670950.17                 X    =         2883321.03
     Y    =       11805754.72  feet           Y    =         3630996.87  meter
     Z    =       16160880.56                 Z    =         4939999.37
     XDOT =     -12946.892016                 XDOT =       -4004.817692
     YDOT =      20373.483139  feet/sec       YDOT =        6165.380996  meter/sec
     ZDOT =      -7119.938510                 ZDOT =       -2189.468722
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5183884.84                 X    =         1580048.10
     Y    =       14285703.99  feet           Y    =         4354282.58  meter
     Z    =       16221072.14                 Z    =         4944182.79
     XDOT =     -17808.948814                 XDOT =       -5428.167599
     YDOT =      14660.133942  feet/sec       YDOT =        4468.408826  meter/sec
     ZDOT =      -7204.189210                 ZDOT =       -2195.836871
  
  
    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   15199.17259121  .00016717  00000-0  10270-3 0  9123
    2 25544  51.6444 289.2972 0002077 272.7332  87.3583 15.55046902 32867
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15199.17259121   =   yrday.fracday
    Element set:     912
    Inclination:       51.6444  deg
    RA of node:       289.2972  deg
    Eccentricity:     .0002077     
    Arg of perigee:   272.7332  deg
    Mean anomaly:      87.3583  deg
    Mean motion:   15.55046902  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3286
    Checksum:              324
 
 
    Coasting Arc #14 (Orbit 3300)
    ---------------------------------------
 
    Vector Time (GMT): 2015/200/03:04:36.271
    Vector Time (MET): N/A
    Weight (LBS)     : 891730.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1912795.14                 A    =         6780305.03  meter
     Y    =       -5233073.28  meter          E    =           .0004350
     Z    =       -3868512.45                 I    =           51.28845
     XDOT =       4508.140157                 Wp   =          109.58268
     YDOT =      -4663.936354  meter/sec      RA   =          283.73438  deg
     ZDOT =       4082.338280                 TA   =          203.45548
                                              MA   =          203.47533
                                              Ha   =            218.802  n.mi
                                              Hp   =            213.945
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6275574.61                 X    =        -1835344.06
     Y    =      -17168875.59  feet           Y    =        -5254030.15  meter
     Z    =      -12691969.98                 Z    =        -3877616.43
     XDOT =      14790.486081                 XDOT =        4540.128266
     YDOT =     -15301.628459  feet/sec       YDOT =       -4613.344738  meter/sec
     ZDOT =      13393.498294                 ZDOT =        4104.314983
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        -557260.89                 X    =         -169853.12
     Y    =      -18244812.87  feet           Y    =        -5561018.96  meter
     Z    =      -12730101.78                 Z    =        -3880135.02
     XDOT =      17398.273257                 XDOT =        5302.993689
     YDOT =      -9937.809276  feet/sec       YDOT =       -3029.044267  meter/sec
     ZDOT =      13488.895699                 ZDOT =        4111.415409
  
  
    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   15200.13656880  .00016717  00000-0  10270-3 0  9136
    2 25544  51.6431 284.4844 0002088 276.5915  83.5000 15.55036137 33018
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15200.13656880   =   yrday.fracday
    Element set:     913
    Inclination:       51.6431  deg
    RA of node:       284.4844  deg
    Eccentricity:     .0002088     
    Arg of perigee:   276.5915  deg
    Mean anomaly:      83.5000  deg
    Mean motion:   15.55036137  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3301
    Checksum:              288
 
 
    Coasting Arc #15 (Orbit 3316)
    ---------------------------------------
 
    Vector Time (GMT): 2015/201/03:04:36.271
    Vector Time (MET): N/A
    Weight (LBS)     : 891730.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         835348.61                 A    =         6784468.41  meter
     Y    =        6346260.12  meter          E    =           .0011797
     Z    =        2231759.60                 I    =           51.29599
     XDOT =      -4788.803957                 Wp   =          109.01925
     YDOT =       2545.291231  meter/sec      RA   =          278.72382  deg
     ZDOT =      -5425.604934                 TA   =           46.02809
                                              MA   =           45.93086
                                              Ha   =            218.778  n.mi
                                              Hp   =            213.910
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2740645.05                 X    =          753480.25
     Y    =       20821063.37  feet           Y    =         6355143.69  meter
     Z    =        7322045.92                 Z    =         2235618.90
     XDOT =     -15711.299072                 XDOT =       -4790.554992
     YDOT =       8350.693016  feet/sec       YDOT =        2491.730115  meter/sec
     ZDOT =     -17800.541122                 ZDOT =       -5448.871773
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3548756.72                 X    =        -1081661.05
     Y    =       20693203.63  feet           Y    =         6307288.47  meter
     Z    =        7337426.06                 Z    =         2236447.46
     XDOT =     -15854.201638                 XDOT =       -4832.360659
     YDOT =       3651.436187  feet/sec       YDOT =        1112.957750  meter/sec
     ZDOT =     -17901.070631                 ZDOT =       -5456.246328
  
  
    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   15201.16480039  .00016717  00000-0  10270-3 0  9142
    2 25544  51.6430 279.3517 0002082 284.7738  75.3184 15.55071424 33172
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15201.16480039   =   yrday.fracday
    Element set:     914
    Inclination:       51.6430  deg
    RA of node:       279.3517  deg
    Eccentricity:     .0002082     
    Arg of perigee:   284.7738  deg
    Mean anomaly:      75.3184  deg
    Mean motion:   15.55071424  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3317
    Checksum:              298
 
 
    Coasting Arc #16 (Orbit 3331)
    ---------------------------------------
 
    Vector Time (GMT): 2015/202/03:04:36.271
    Vector Time (MET): N/A
    Weight (LBS)     : 891730.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         205981.01                 A    =         6786608.23  meter
     Y    =       -6771294.22  meter          E    =           .0010730
     Z    =        -292074.34                 I    =           51.29752
     XDOT =       4806.059451                 Wp   =           32.90745
     YDOT =       -106.770294  meter/sec      RA   =          273.72201  deg
     ZDOT =       5977.107256                 TA   =          323.92851
                                              MA   =          324.00086
                                              Ha   =            218.806  n.mi
                                              Hp   =            213.946
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         675790.71                 X    =          283102.71
     Y    =      -22215532.23  feet           Y    =        -6768559.59  meter
     Z    =        -958249.13                 Z    =         -290886.63
     XDOT =      15767.911584                 XDOT =        4777.862054
     YDOT =       -350.296241  feet/sec       YDOT =         -53.183640  meter/sec
     ZDOT =      19609.931941                 ZDOT =        6000.385336
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6822359.86                 X    =         2079455.29
     Y    =      -21153112.59  feet           Y    =        -6447468.72  meter
     Z    =        -951861.34                 Z    =         -290127.34
     XDOT =      13582.008104                 XDOT =        4139.796070
     YDOT =       3510.286834  feet/sec       YDOT =        1069.935427  meter/sec
     ZDOT =      19710.044050                 ZDOT =        6007.621427
  
  
    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   15202.12875885  .00016717  00000-0  10270-3 0  9157
    2 25544  51.6415 274.5382 0002120 286.2583  73.8336 15.55052314 33326
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15202.12875885   =   yrday.fracday
    Element set:     915
    Inclination:       51.6415  deg
    RA of node:       274.5382  deg
    Eccentricity:     .0002120     
    Arg of perigee:   286.2583  deg
    Mean anomaly:      73.8336  deg
    Mean motion:   15.55052314  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3332
    Checksum:              297
 
             

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