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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  16145.87
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   131.8
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.219
   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 
   ------------------------------------------------------------------------
   062/07:21:36.444          -0.6               1.4              1.4    
   N/A                       -1.2              -0.1              222.3  
   000/00:03:12.887          -0.0               0.1              211.3  
   
 
 
    Coasting Arc #1 (Orbit 1098)
    ---------------------------------------
 
    Vector Time (GMT): 2015/058/14:47:24.330
    Vector Time (MET): N/A
    Weight (LBS)     : 905416.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4027816.62                 A    =         6776341.37  meter
     Y    =        2053765.60  meter          E    =           .0012925
     Z    =        5040362.37                 I    =           51.26144
     XDOT =      -1486.856385                 Wp   =           54.85530
     YDOT =       7316.249805  meter/sec      RA   =          270.44553  deg
     ZDOT =      -1782.373945                 TA   =           52.52321
                                              MA   =           52.40574
                                              Ha   =            222.325  n.mi
                                              Hp   =            211.149
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13214621.45                 X    =         3980067.77
     Y    =        6738076.11  feet           Y    =         2098540.67  meter
     Z    =       16536621.94                 Z    =         5059812.27
     XDOT =      -4878.137746                 XDOT =       -1559.899944
     YDOT =      24003.444242  feet/sec       YDOT =        7299.214263  meter/sec
     ZDOT =      -5847.683548                 ZDOT =       -1789.774653
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14556080.94                 X    =         4436693.47
     Y    =        2324207.09  feet           Y    =          708418.32  meter
     Z    =       16619456.18                 Z    =         5065610.24
     XDOT =       3040.271102                 XDOT =         926.674632
     YDOT =      23255.912014  feet/sec       YDOT =        7088.401982  meter/sec
     ZDOT =      -5880.615369                 ZDOT =       -1792.411565
  
  
    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   15058.66140570  .00016717  00000-0  10270-3 0  9005
    2 25544  51.6411 271.0632 0007525  54.6802 305.5054 15.54840182 10994
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15058.66140570   =   yrday.fracday
    Element set:     900
    Inclination:       51.6411  deg
    RA of node:       271.0632  deg
    Eccentricity:     .0007525     
    Arg of perigee:    54.6802  deg
    Mean anomaly:     305.5054  deg
    Mean motion:   15.54840182  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1099
    Checksum:              283
 
 
    Coasting Arc #2 (Orbit 1113)
    ---------------------------------------
 
    Vector Time (GMT): 2015/059/14:47:24.330
    Vector Time (MET): N/A
    Weight (LBS)     : 905416.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3649698.49                 A    =         6779723.00  meter
     Y    =       -3945011.33  meter          E    =           .0013803
     Z    =       -4143957.23                 I    =           51.27471
     XDOT =       2498.142583                 Wp   =           84.43624
     YDOT =      -6210.288194  meter/sec      RA   =          265.41876  deg
     ZDOT =       3724.009066                 TA   =          224.05576
                                              MA   =          224.16583
                                              Ha   =            222.359  n.mi
                                              Hp   =            210.882
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11974076.42                 X    =        -3585183.77
     Y    =      -12942950.56  feet           Y    =        -3985464.26  meter
     Z    =      -13595660.19                 Z    =        -4161529.40
     XDOT =       8196.005849                 XDOT =        2549.312318
     YDOT =     -20374.961266  feet/sec       YDOT =       -6182.065918  meter/sec
     ZDOT =      12217.877514                 ZDOT =        3736.269133
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15471857.87                 X    =        -4715822.28
     Y    =       -8336019.01  feet           Y    =        -2540818.59  meter
     Z    =      -13670144.56                 Z    =        -4166660.06
     XDOT =        388.825549                 XDOT =         118.514027
     YDOT =     -20780.896662  feet/sec       YDOT =       -6334.017303  meter/sec
     ZDOT =      12271.391157                 ZDOT =        3740.320025
  
  
    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   15059.62546516  .00016717  00000-0  10270-3 0  9013
    2 25544  51.6417 266.2515 0007551  58.6290 301.5601 15.54902336 11142
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15059.62546516   =   yrday.fracday
    Element set:     901
    Inclination:       51.6417  deg
    RA of node:       266.2515  deg
    Eccentricity:     .0007551     
    Arg of perigee:    58.6290  deg
    Mean anomaly:     301.5601  deg
    Mean motion:   15.54902336  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1114
    Checksum:              289
 
 
    Coasting Arc #3 (Orbit 1129)
    ---------------------------------------
 
    Vector Time (GMT): 2015/060/14:47:24.330
    Vector Time (MET): N/A
    Weight (LBS)     : 905416.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3053381.93                 A    =         6784053.94  meter
     Y    =        5453096.78  meter          E    =           .0019828
     Z    =        2622607.12                 I    =           51.29191
     XDOT =      -3468.035582                 Wp   =           88.26875
     YDOT =       4456.539845  meter/sec      RA   =          260.40483  deg
     ZDOT =      -5193.971582                 TA   =           62.00435
                                              MA   =           61.80387
                                              Ha   =            222.321  n.mi
                                              Hp   =            210.889
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10017657.24                 X    =         2979437.79
     Y    =       17890737.47  feet           Y    =         5486828.49  meter
     Z    =        8604354.06                 Z    =         2637259.43
     XDOT =     -11378.069494                 XDOT =       -3492.382051
     YDOT =      14621.193717  feet/sec       YDOT =        4417.621382  meter/sec
     ZDOT =     -17040.589179                 ZDOT =       -5210.877845
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15506269.91                 X    =         4726311.07
     Y    =       13376138.86  feet           Y    =         4077047.13  meter
     Z    =        8666103.79                 Z    =         2641428.44
     XDOT =      -4581.756276                 XDOT =       -1396.519313
     YDOT =      16472.156323  feet/sec       YDOT =        5020.713247  meter/sec
     ZDOT =     -17113.668267                 ZDOT =       -5216.246088
  
  
    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   15060.65377441  .00016717  00000-0  10270-3 0  9028
    2 25544  51.6408 261.1185 0007463  61.5935 298.5969 15.54926320 11309
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15060.65377441   =   yrday.fracday
    Element set:     902
    Inclination:       51.6408  deg
    RA of node:       261.1185  deg
    Eccentricity:     .0007463     
    Arg of perigee:    61.5935  deg
    Mean anomaly:     298.5969  deg
    Mean motion:   15.54926320  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1130
    Checksum:              311
 
 
    Coasting Arc #4 (Orbit 1144)
    ---------------------------------------
 
    Vector Time (GMT): 2015/061/14:47:24.330
    Vector Time (MET): N/A
    Weight (LBS)     : 905416.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2296836.82                 A    =         6786621.37  meter
     Y    =       -6331471.44  meter          E    =           .0017405
     Z    =        -782973.84                 I    =           51.30820
     XDOT =       4307.192399                 Wp   =           50.72283
     YDOT =      -2282.623338  meter/sec      RA   =          255.40338  deg
     ZDOT =       5922.497022                 TA   =          300.76937
                                              MA   =          300.94063
                                              Ha   =            222.325  n.mi
                                              Hp   =            210.745
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7535553.86                 X    =        -2222062.79
     Y    =      -20772544.10  feet           Y    =        -6356738.17  meter
     Z    =       -2568811.82                 Z    =         -793948.88
     XDOT =      14131.208659                 XDOT =        4303.628435
     YDOT =      -7488.921711  feet/sec       YDOT =       -2234.476772  meter/sec
     ZDOT =      19430.764509                 ZDOT =        5943.411688
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14490888.66                 X    =        -4416822.86
     Y    =      -16675114.77  feet           Y    =        -5082574.98  meter
     Z    =       -2614698.41                 Z    =         -796960.07
     XDOT =       9158.847272                 XDOT =        2791.616648
     YDOT =     -10969.871319  feet/sec       YDOT =       -3343.616778  meter/sec
     ZDOT =      19520.619356                 ZDOT =        5949.884780
  
  
    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   15061.61779526  .00016717  00000-0  10270-3 0  9036
    2 25544  51.6419 256.3069 0007554  65.6568 294.5373 15.54966832 11459
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15061.61779526   =   yrday.fracday
    Element set:     903
    Inclination:       51.6419  deg
    RA of node:       256.3069  deg
    Eccentricity:     .0007554     
    Arg of perigee:    65.6568  deg
    Mean anomaly:     294.5373  deg
    Mean motion:   15.54966832  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1145
    Checksum:              339
 
 
    Coasting Arc #5 (Orbit 1155)
    ---------------------------------------
 
    Vector Time (GMT): 2015/062/07:23:12.887
    Vector Time (MET): N/A
    Weight (LBS)     : 905275.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3856414.23                 A    =         6775633.63  meter
     Y    =        1829849.60  meter          E    =           .0020979
     Z    =       -5280186.71                 I    =           51.27777
     XDOT =      -2728.102143                 Wp   =           78.53303
     YDOT =      -7135.345761  meter/sec      RA   =          251.95086  deg
     ZDOT =       -477.797813                 TA   =          186.86332
                                              MA   =          186.89209
                                              Ha   =            222.335  n.mi
                                              Hp   =            211.313
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12652277.65                 X    =        -3850940.77
     Y    =        6003443.57  feet           Y    =         1786754.62  meter
     Z    =      -17323447.21                 Z    =        -5298906.96
     XDOT =      -8950.466347                 XDOT =       -2645.789347
     YDOT =     -23409.927038  feet/sec       YDOT =       -7165.393000  meter/sec
     ZDOT =      -1567.578127                 ZDOT =        -490.849336
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6160398.97                 X    =        -1877689.61
     Y    =      -12465118.75  feet           Y    =        -3799368.20  meter
     Z    =      -17403838.27                 Z    =        -5304689.90
     XDOT =      22385.900611                 XDOT =        6823.222506
     YDOT =      -8787.127725  feet/sec       YDOT =       -2678.316530  meter/sec
     ZDOT =      -1622.225774                 ZDOT =        -494.454416
  
  
    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   15062.32473167  .00016717  00000-0  10270-3 0  9048
    2 25544  51.6445 252.7826 0006665  61.0750 299.1070 15.54749983 11567
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15062.32473167   =   yrday.fracday
    Element set:     904
    Inclination:       51.6445  deg
    RA of node:       252.7826  deg
    Eccentricity:     .0006665     
    Arg of perigee:    61.0750  deg
    Mean anomaly:     299.1070  deg
    Mean motion:   15.54749983  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1156
    Checksum:              319
 
 
    Coasting Arc #6 (Orbit 1171)
    ---------------------------------------
 
    Vector Time (GMT): 2015/063/07:23:12.887
    Vector Time (MET): N/A
    Weight (LBS)     : 905275.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4485303.53                 A    =         6776293.56  meter
     Y    =         161907.73  meter          E    =           .0011632
     Z    =        5069570.87                 I    =           51.29106
     XDOT =       1647.626015                 Wp   =           59.76729
     YDOT =       7305.604991  meter/sec      RA   =          246.91905  deg
     ZDOT =      -1682.400965                 TA   =           46.59415
                                              MA   =           46.49737
                                              Ha   =            222.086  n.mi
                                              Hp   =            211.382
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14715562.77                 X    =         4458534.07
     Y    =         531193.34  feet           Y    =          211916.34  meter
     Z    =       16632450.35                 Z    =         5091294.15
     XDOT =       5405.597161                 XDOT =        1573.982880
     YDOT =      23968.520313  feet/sec       YDOT =        7323.617828  meter/sec
     ZDOT =      -5519.688206                 ZDOT =       -1674.577137
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         -95987.67                 X    =          -29257.04
     Y    =       14619214.35  feet           Y    =         4455936.53  meter
     Z    =       16725361.49                 Z    =         5097890.18
     XDOT =     -22728.767506                 XDOT =       -6927.728336
     YDOT =       6161.050004  feet/sec       YDOT =        1877.888041  meter/sec
     ZDOT =      -5487.415590                 ZDOT =       -1672.564272
  
  
    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   15063.35315148  .00016717  00000-0  10270-3 0  9057
    2 25544  51.6442 247.6506 0006552  63.3413 296.8410 15.54808266 11728
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15063.35315148   =   yrday.fracday
    Element set:     905
    Inclination:       51.6442  deg
    RA of node:       247.6506  deg
    Eccentricity:     .0006552     
    Arg of perigee:    63.3413  deg
    Mean anomaly:     296.8410  deg
    Mean motion:   15.54808266  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1172
    Checksum:              299
 
 
    Coasting Arc #7 (Orbit 1186)
    ---------------------------------------
 
    Vector Time (GMT): 2015/064/07:23:12.887
    Vector Time (MET): N/A
    Weight (LBS)     : 905275.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4913393.11                 A    =         6779707.31  meter
     Y    =       -2021093.05  meter          E    =           .0013705
     Z    =       -4223731.03                 I    =           51.31599
     XDOT =       -322.750564                 Wp   =           90.98167
     YDOT =      -6745.628997  meter/sec      RA   =          241.89489  deg
     ZDOT =       3613.255841                 TA   =          216.15360
                                              MA   =          216.24633
                                              Ha   =            222.227  n.mi
                                              Hp   =            211.233
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16120056.13                 X    =        -4869910.62
     Y    =       -6630882.71  feet           Y    =        -2075795.32  meter
     Z    =      -13857385.28                 Z    =        -4247493.04
     XDOT =      -1058.892926                 XDOT =        -264.846920
     YDOT =     -22131.328731  feet/sec       YDOT =       -6748.913911  meter/sec
     ZDOT =      11854.513914                 ZDOT =        3611.829647
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5870263.94                 X    =         1789256.45
     Y    =      -16326237.51  feet           Y    =        -4976237.19  meter
     Z    =      -13958721.71                 Z    =        -4254618.38
     XDOT =      20861.869216                 XDOT =        6358.697737
     YDOT =      -2602.336768  feet/sec       YDOT =        -793.192247  meter/sec
     ZDOT =      11849.505875                 ZDOT =        3611.729391
  
  
    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   15064.31727697  .00016717  00000-0  10270-3 0  9061
    2 25544  51.6445 242.8393 0006565  66.3340 293.8502 15.54800954 11879
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15064.31727697   =   yrday.fracday
    Element set:     906
    Inclination:       51.6445  deg
    RA of node:       242.8393  deg
    Eccentricity:     .0006565     
    Arg of perigee:    66.3340  deg
    Mean anomaly:     293.8502  deg
    Mean motion:   15.54800954  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1187
    Checksum:              324
 
 
    Coasting Arc #8 (Orbit 1202)
    ---------------------------------------
 
    Vector Time (GMT): 2015/065/07:23:12.887
    Vector Time (MET): N/A
    Weight (LBS)     : 905275.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5009248.28                 A    =         6783980.18  meter
     Y    =        3631863.57  meter          E    =           .0019480
     Z    =        2764820.30                 I    =           51.34627
     XDOT =      -1223.530405                 Wp   =           90.48245
     YDOT =       5596.981425  meter/sec      RA   =          236.88415  deg
     ZDOT =      -5104.371229                 TA   =           58.02307
                                              MA   =           57.83386
                                              Ha   =            222.227  n.mi
                                              Hp   =            211.193
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16434541.60                 X    =         4954833.33
     Y    =       11915562.89  feet           Y    =         3687576.43  meter
     Z    =        9070932.73                 Z    =         2789021.20
     XDOT =      -4014.207364                 XDOT =       -1261.231430
     YDOT =      18362.799950  feet/sec       YDOT =        5583.087516  meter/sec
     ZDOT =     -16746.624767                 ZDOT =       -5110.407267
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10839756.98                 X    =        -3303957.93
     Y    =       17108357.73  feet           Y    =         5214627.44  meter
     Z    =        9173896.75                 Z    =         2796203.73
     XDOT =     -17326.882357                 XDOT =       -5281.233742
     YDOT =      -1929.951372  feet/sec       YDOT =        -588.249178  meter/sec
     ZDOT =     -16773.347969                 ZDOT =       -5112.516461
  
  
    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   15065.34565542  .00016717  00000-0  10270-3 0  9075
    2 25544  51.6446 237.7070 0006673  70.1612 290.0260 15.54828492 12036
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15065.34565542   =   yrday.fracday
    Element set:     907
    Inclination:       51.6446  deg
    RA of node:       237.7070  deg
    Eccentricity:     .0006673     
    Arg of perigee:    70.1612  deg
    Mean anomaly:     290.0260  deg
    Mean motion:   15.54828492  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1203
    Checksum:              295
 
 
    Coasting Arc #9 (Orbit 1217)
    ---------------------------------------
 
    Vector Time (GMT): 2015/066/07:23:12.887
    Vector Time (MET): N/A
    Weight (LBS)     : 905275.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4728225.21                 A    =         6786718.51  meter
     Y    =       -4762789.41  meter          E    =           .0015591
     Z    =        -976624.80                 I    =           51.37422
     XDOT =       2836.918604                 Wp   =           52.32561
     YDOT =      -4009.005403  meter/sec      RA   =          231.88586  deg
     ZDOT =       5890.314358                 TA   =          297.05240
                                              MA   =          297.21143
                                              Ha   =            222.126  n.mi
                                              Hp   =            211.167
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15512549.91                 X    =        -4669871.13
     Y    =      -15625949.52  feet           Y    =        -4815337.39  meter
     Z    =       -3204149.60                 Z    =         -999450.90
     XDOT =       9307.475735                 XDOT =        2852.924721
     YDOT =     -13152.904866  feet/sec       YDOT =       -3977.190704  meter/sec
     ZDOT =      19325.178341                 ZDOT =        5904.134938
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14313444.32                 X    =         4362737.83
     Y    =      -16712402.00  feet           Y    =        -5093940.13  meter
     Z    =       -3301061.78                 Z    =        -1006163.63
     XDOT =      12636.466160                 XDOT =        3851.594886
     YDOT =       7040.116228  feet/sec       YDOT =        2145.827426  meter/sec
     ZDOT =      19384.950454                 ZDOT =        5908.532898
  
  
    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   15066.30973796  .00016717  00000-0  10270-3 0  9087
    2 25544  51.6449 232.8952 0006528  72.3084 287.8781 15.54877766 12186
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15066.30973796   =   yrday.fracday
    Element set:     908
    Inclination:       51.6449  deg
    RA of node:       232.8952  deg
    Eccentricity:     .0006528     
    Arg of perigee:    72.3084  deg
    Mean anomaly:     287.8781  deg
    Mean motion:   15.54877766  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1218
    Checksum:              357
 
 
    Coasting Arc #10 (Orbit 1233)
    ---------------------------------------
 
    Vector Time (GMT): 2015/067/07:23:12.887
    Vector Time (MET): N/A
    Weight (LBS)     : 905275.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3958906.93                 A    =         6786768.17  meter
     Y    =        5415116.42  meter          E    =           .0013795
     Z    =       -1014454.45                 I    =           51.39443
     XDOT =      -4424.476490                 Wp   =          116.79216
     YDOT =       2145.507378  meter/sec      RA   =          226.89460  deg
     ZDOT =      -5881.927403                 TA   =           74.23937
                                              MA   =           74.08727
                                              Ha   =            222.173  n.mi
                                              Hp   =            211.204
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12988539.81                 X    =         3902987.40
     Y    =       17766129.99  feet           Y    =         5459074.68  meter
     Z    =       -3328262.64                 Z    =         -995359.62
     XDOT =     -14515.998982                 XDOT =       -4419.567181
     YDOT =       7039.066200  feet/sec       YDOT =        2096.056538  meter/sec
     ZDOT =     -19297.662082                 ZDOT =       -5903.408931
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16397642.44                 X    =        -4998001.42
     Y    =       14696480.33  feet           Y    =         4479487.20  meter
     Z    =       -3247408.47                 Z    =         -989810.10
     XDOT =      -7349.562602                 XDOT =       -2240.146681
     YDOT =     -12434.233504  feet/sec       YDOT =       -3789.954372  meter/sec
     ZDOT =     -19389.920110                 ZDOT =       -5910.047649
  
  
    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   15067.33807198  .00016717  00000-0  10270-3 0  9094
    2 25544  51.6448 227.7629 0006410  76.7525 283.4343 15.54865118 12349
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15067.33807198   =   yrday.fracday
    Element set:     909
    Inclination:       51.6448  deg
    RA of node:       227.7629  deg
    Eccentricity:     .0006410     
    Arg of perigee:    76.7525  deg
    Mean anomaly:     283.4343  deg
    Mean motion:   15.54865118  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1234
    Checksum:              327
 
 
    Coasting Arc #11 (Orbit 1249)
    ---------------------------------------
 
    Vector Time (GMT): 2015/068/07:23:12.887
    Vector Time (MET): N/A
    Weight (LBS)     : 905275.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2765574.51                 A    =         6783664.60  meter
     Y    =       -5504298.57  meter          E    =           .0019844
     Z    =        2819324.73                 I    =           51.40653
     XDOT =       5753.226157                 Wp   =           79.54100
     YDOT =       -278.208857  meter/sec      RA   =          221.89861  deg
     ZDOT =       5073.488991                 TA   =          312.63072
                                              MA   =          312.79786
                                              Ha   =            222.088  n.mi
                                              Hp   =            211.098
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9073407.17                 X    =        -2717513.78
     Y    =      -18058722.33  feet           Y    =        -5534955.89  meter
     Z    =        9249753.05                 Z    =         2806007.68
     XDOT =      18875.413900                 XDOT =        5731.264519
     YDOT =       -912.758718  feet/sec       YDOT =        -213.994585  meter/sec
     ZDOT =      16645.305087                 ZDOT =        5101.383660
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16880881.94                 X    =         5145292.81
     Y    =      -11158635.23  feet           Y    =        -3401152.02  meter
     Z    =        9193627.48                 Z    =         2802217.66
     XDOT =       2261.775876                 XDOT =         689.389287
     YDOT =      17307.263688  feet/sec       YDOT =        5275.253972  meter/sec
     ZDOT =      16764.718078                 ZDOT =        5109.886070
  
  
    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   15068.36638140  .00016717  00000-0  10270-3 0  9109
    2 25544  51.6445 222.6298 0006438  77.7926 282.3948 15.54931786 12500
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15068.36638140   =   yrday.fracday
    Element set:     910
    Inclination:       51.6445  deg
    RA of node:       222.6298  deg
    Eccentricity:     .0006438     
    Arg of perigee:    77.7926  deg
    Mean anomaly:     282.3948  deg
    Mean motion:   15.54931786  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1250
    Checksum:              333
 
 
    Coasting Arc #12 (Orbit 1264)
    ---------------------------------------
 
    Vector Time (GMT): 2015/069/07:23:12.887
    Vector Time (MET): N/A
    Weight (LBS)     : 905275.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1137907.70                 A    =         6779137.80  meter
     Y    =        5135286.86  meter          E    =           .0014615
     Z    =       -4291401.65                 I    =           51.41506
     XDOT =      -6638.475825                 Wp   =           75.02861
     YDOT =      -1467.994750  meter/sec      RA   =          216.89215  deg
     ZDOT =      -3523.296692                 TA   =          158.94304
                                              MA   =          158.88280
                                              Ha   =            221.999  n.mi
                                              Hp   =            211.061
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3733292.98                 X    =         1101245.14
     Y    =       16848054.00  feet           Y    =         5147806.12  meter
     Z    =      -14079401.75                 Z    =        -4285963.66
     XDOT =     -21779.776328                 XDOT =       -6604.452134
     YDOT =      -4816.255741  feet/sec       YDOT =       -1542.040750  meter/sec
     ZDOT =     -11559.372349                 ZDOT =       -3555.462244
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16190599.46                 X    =        -4934894.72
     Y    =        6024215.01  feet           Y    =         1836180.74  meter
     Z    =      -14056929.82                 Z    =        -4284552.21
     XDOT =       2333.625713                 XDOT =         711.289117
     YDOT =     -20972.702247  feet/sec       YDOT =       -6392.479645  meter/sec
     ZDOT =     -11696.799609                 ZDOT =       -3565.184521
  
  
    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   15069.33040016  .00016717  00000-0  10270-3 0  9117
    2 25544  51.6436 217.8178 0006339  81.2860 278.9011 15.54961368 12657
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15069.33040016   =   yrday.fracday
    Element set:     911
    Inclination:       51.6436  deg
    RA of node:       217.8178  deg
    Eccentricity:     .0006339     
    Arg of perigee:    81.2860  deg
    Mean anomaly:     278.9011  deg
    Mean motion:   15.54961368  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1265
    Checksum:              308
 
 
    Coasting Arc #13 (Orbit 1280)
    ---------------------------------------
 
    Vector Time (GMT): 2015/070/07:23:12.887
    Vector Time (MET): N/A
    Weight (LBS)     : 905275.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         722745.81                 A    =         6775652.13  meter
     Y    =       -4363034.33  meter          E    =           .0010570
     Z    =        5124853.61                 I    =           51.42960
     XDOT =       6943.800025                 Wp   =          101.94473
     YDOT =       2913.013667  meter/sec      RA   =          211.87410  deg
     ZDOT =       1495.959256                 TA   =          333.59657
                                              MA   =          333.65039
                                              Ha   =            221.997  n.mi
                                              Hp   =            210.969
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2371213.29                 X    =          746585.97
     Y    =      -14314417.08  feet           Y    =        -4354818.20  meter
     Z    =       16813824.18                 Z    =         5128422.99
     XDOT =      22781.496144                 XDOT =        6903.443133
     YDOT =       9557.131453  feet/sec       YDOT =        2990.438301  meter/sec
     ZDOT =       4908.002807                 ZDOT =        1529.592490
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14490658.89                 X    =         4416752.83
     Y    =          95995.95  feet           Y    =           29259.57  meter
     Z    =       16829779.03                 Z    =         5129716.65
     XDOT =      -6036.546538                 XDOT =       -1839.939385
     YDOT =      22867.824617  feet/sec       YDOT =        6970.112943  meter/sec
     ZDOT =       5051.500370                 ZDOT =        1539.697313
  
  
    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   15070.35866514  .00016717  00000-0  10270-3 0  9121
    2 25544  51.6437 212.6849 0006471  84.4837 275.7055 15.54978690 12819
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15070.35866514   =   yrday.fracday
    Element set:     912
    Inclination:       51.6437  deg
    RA of node:       212.6849  deg
    Eccentricity:     .0006471     
    Arg of perigee:    84.4837  deg
    Mean anomaly:     275.7055  deg
    Mean motion:   15.54978690  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1281
    Checksum:              334
 
 
    Coasting Arc #14 (Orbit 1295)
    ---------------------------------------
 
    Vector Time (GMT): 2015/071/07:23:12.887
    Vector Time (MET): N/A
    Weight (LBS)     : 905275.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2673132.98                 A    =         6774858.48  meter
     Y    =        3349249.48  meter          E    =           .0020955
     Z    =       -5265713.80                 I    =           51.45360
     XDOT =      -6495.409625                 Wp   =           93.61682
     YDOT =      -3975.741392  meter/sec      RA   =          206.84956  deg
     ZDOT =        769.982899                 TA   =          183.76509
                                              MA   =          183.78088
                                              Ha   =            221.889  n.mi
                                              Hp   =            210.768
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8770121.32                 X    =        -2684807.58
     Y    =       10988351.30  feet           Y    =         3319290.92  meter
     Z    =      -17275963.92                 Z    =        -5278728.06
     XDOT =     -21310.399031                 XDOT =       -6454.209473
     YDOT =     -13043.770972  feet/sec       YDOT =       -4048.146856  meter/sec
     ZDOT =       2526.190615                 ZDOT =         738.530017
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12276870.93                 X    =        -3741990.26
     Y    =       -6707567.69  feet           Y    =        -2044466.63  meter
     Z    =      -17332189.64                 Z    =        -5282851.40
     XDOT =       8816.583533                 XDOT =        2687.294661
     YDOT =     -22306.825850  feet/sec       YDOT =       -6799.120519  meter/sec
     ZDOT =       2392.174210                 ZDOT =         729.134699
  
  
    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   15071.32263944  .00016717  00000-0  10270-3 0  9138
    2 25544  51.6423 207.8717 0006392  87.6943 272.4942 15.55048973 12967
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15071.32263944   =   yrday.fracday
    Element set:     913
    Inclination:       51.6423  deg
    RA of node:       207.8717  deg
    Eccentricity:     .0006392     
    Arg of perigee:    87.6943  deg
    Mean anomaly:     272.4942  deg
    Mean motion:   15.55048973  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1296
    Checksum:              329
 
 
    Coasting Arc #15 (Orbit 1311)
    ---------------------------------------
 
    Vector Time (GMT): 2015/072/07:23:12.887
    Vector Time (MET): N/A
    Weight (LBS)     : 905275.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4454273.13                 A    =         6777378.26  meter
     Y    =       -2170330.51  meter          E    =           .0014106
     Z    =        4613822.81                 I    =           51.49142
     XDOT =       5337.294662                 Wp   =           76.31325
     YDOT =       4664.725899  meter/sec      RA   =          201.83156  deg
     ZDOT =      -2947.599932                 TA   =           43.12663
                                              MA   =           43.01621
                                              Ha   =            221.672  n.mi
                                              Hp   =            210.863
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14613756.98                 X    =         4455799.09
     Y    =       -7120506.92  feet           Y    =        -2120510.94  meter
     Z    =       15137213.94                 Z    =         4635464.63
     XDOT =      17510.809258                 XDOT =        5299.054195
     YDOT =      15304.218828  feet/sec       YDOT =        4724.196907  meter/sec
     ZDOT =      -9670.603453                 ZDOT =       -2921.765836
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9664198.99                 X    =         2945647.85
     Y    =       12963144.74  feet           Y    =         3951166.52  meter
     Z    =       15230196.79                 Z    =         4642163.98
     XDOT =     -10870.773559                 XDOT =       -3313.411781
     YDOT =      19378.633717  feet/sec       YDOT =        5906.607557  meter/sec
     ZDOT =      -9560.729595                 ZDOT =       -2914.110381
  
  
    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   15072.35085581  .00016717  00000-0  10270-3 0  9142
    2 25544  51.6426 202.7388 0006257  90.9837 269.2033 15.55084802 13122
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15072.35085581   =   yrday.fracday
    Element set:     914
    Inclination:       51.6426  deg
    RA of node:       202.7388  deg
    Eccentricity:     .0006257     
    Arg of perigee:    90.9837  deg
    Mean anomaly:     269.2033  deg
    Mean motion:   15.55084802  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1312
    Checksum:              308
 
 
    Coasting Arc #16 (Orbit 1326)
    ---------------------------------------
 
    Vector Time (GMT): 2015/073/07:23:12.887
    Vector Time (MET): N/A
    Weight (LBS)     : 905275.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5833738.69                 A    =         6781675.46  meter
     Y    =         993373.37  meter          E    =           .0011124
     Z    =       -3322440.15                 I    =           51.53451
     XDOT =      -3502.846853                 Wp   =           92.07498
     YDOT =      -4947.373149  meter/sec      RA   =          196.82607  deg
     ZDOT =       4684.488918                 TA   =          229.22459
                                              MA   =          229.32117
                                              Ha   =            221.751  n.mi
                                              Hp   =            210.699
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19139562.63                 X    =        -5828274.19
     Y    =        3259098.97  feet           Y    =          928166.94  meter
     Z    =      -10900394.18                 Z    =        -3350765.94
     XDOT =     -11492.279701                 XDOT =       -3470.019154
     YDOT =     -16231.539202  feet/sec       YDOT =       -4986.360281  meter/sec
     ZDOT =      15369.058131                 ZDOT =        4667.553084
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7016072.09                 X    =        -2138498.77
     Y    =      -18029345.77  feet           Y    =        -5495344.59  meter
     Z    =      -11021823.83                 Z    =        -3359451.90
     XDOT =      12261.747279                 XDOT =        3737.380571
     YDOT =     -14097.115606  feet/sec       YDOT =       -4296.800837  meter/sec
     ZDOT =      15297.309118                 ZDOT =        4662.619819
  
  
    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   15073.31478750  .00016717  00000-0  10270-3 0  9154
    2 25544  51.6412 197.9253 0006378  94.7138 265.4744 15.55114579 13271
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15073.31478750   =   yrday.fracday
    Element set:     915
    Inclination:       51.6412  deg
    RA of node:       197.9253  deg
    Eccentricity:     .0006378     
    Arg of perigee:    94.7138  deg
    Mean anomaly:     265.4744  deg
    Mean motion:   15.55114579  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1327
    Checksum:              329
 
             

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