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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  12916.69
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   127.1
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.568
   ET - UTC  (sec) :   67.18
   UT1 - UTC (sec) :    0.00
 
 
   Maneuvers contained within the current ephemeris are as follows:
 
 
   IMPULSIVE TIG (GMT)   M50 DVx(FPS)      LVLH DVx(FPS)      DVmag(FPS) 
   IMPULSIVE TIG (MET)   M50 DVy(FPS)      LVLH DVy(FPS)      Invar Sph HA
   DT                    M50 DVz(FPS)      LVLH DVz(FPS)      Invar Sph HP 
   ------------------------------------------------------------------------
    There are no maneuvers.
 
 
    Coasting Arc #1 (Orbit 2402)
    ---------------------------------------
 
    Vector Time (GMT): 2015/142/09:37:06.327
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6170076.78                 A    =         6785300.23  meter
     Y    =        2319565.31  meter          E    =           .0010704
     Z    =        1591707.02                 I    =           51.46279
     XDOT =       -430.160337                 Wp   =          107.50051
     YDOT =       5089.583631  meter/sec      RA   =          211.69204  deg
     ZDOT =      -5720.842317                 TA   =           55.03691
                                              MA   =           54.93643
                                              Ha   =            219.060  n.mi
                                              Hp   =            213.810
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20243034.05                 X    =         6135948.31
     Y    =        7610122.40  feet           Y    =         2388372.18  meter
     Z    =        5222135.89                 Z    =         1621597.53
     XDOT =      -1411.287195                 XDOT =        -459.251437
     YDOT =      16698.109024  feet/sec       YDOT =        5084.611108  meter/sec
     ZDOT =     -18769.167706                 ZDOT =       -5723.002207
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21574360.04                 X    =         6575864.94
     Y    =        -943387.73  feet           Y    =         -287544.58  meter
     Z    =        5349962.84                 Z    =         1630668.67
     XDOT =       5304.358908                 XDOT =        1616.768595
     YDOT =      14287.640973  feet/sec       YDOT =        4354.872969  meter/sec
     ZDOT =     -18779.306001                 ZDOT =       -5723.932469
  
  
    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   15142.43611671  .00016717  00000-0  10270-3 0  9009
    2 25544  51.6430 212.6115 0003805 324.1845  35.9052 15.55127154 24031
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15142.43611671   =   yrday.fracday
    Element set:     900
    Inclination:       51.6430  deg
    RA of node:       212.6115  deg
    Eccentricity:     .0003805     
    Arg of perigee:   324.1845  deg
    Mean anomaly:      35.9052  deg
    Mean motion:   15.55127154  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2403
    Checksum:              264
 
 
    Coasting Arc #2 (Orbit 2418)
    ---------------------------------------
 
    Vector Time (GMT): 2015/143/09:37:06.327
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5880897.80                 A    =         6786294.02  meter
     Y    =       -3342093.82  meter          E    =           .0014107
     Z    =         430771.31                 I    =           51.49423
     XDOT =       2701.145703                 Wp   =           33.60526
     YDOT =      -3971.070174  meter/sec      RA   =          206.70517  deg
     ZDOT =       5984.629241                 TA   =          331.05320
                                              MA   =          331.13137
                                              Ha   =            219.178  n.mi
                                              Hp   =            213.713
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19294284.13                 X    =        -5845181.17
     Y    =      -10964874.74  feet           Y    =        -3407658.19  meter
     Z    =        1413291.70                 Z    =          402289.45
     XDOT =       8862.026586                 XDOT =        2716.279197
     YDOT =     -13028.445454  feet/sec       YDOT =       -3940.779992  meter/sec
     ZDOT =      19634.610370                 ZDOT =        5997.787423
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -22098499.67                 X    =        -6735622.70
     Y    =       -2117353.96  feet           Y    =         -645369.49  meter
     Z    =        1291664.14                 Z    =          393699.23
     XDOT =       2495.146067                 XDOT =         760.520521
     YDOT =     -13848.471119  feet/sec       YDOT =       -4221.013997  meter/sec
     ZDOT =      19691.740307                 ZDOT =        6002.042446
  
  
    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   15143.46427256  .00016717  00000-0  10270-3 0  9018
    2 25544  51.6435 207.4778 0003985 330.3509  29.7418 15.55152292 24193
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15143.46427256   =   yrday.fracday
    Element set:     901
    Inclination:       51.6435  deg
    RA of node:       207.4778  deg
    Eccentricity:     .0003985     
    Arg of perigee:   330.3509  deg
    Mean anomaly:      29.7418  deg
    Mean motion:   15.55152292  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2419
    Checksum:              315
 
 
    Coasting Arc #3 (Orbit 2433)
    ---------------------------------------
 
    Vector Time (GMT): 2015/144/09:37:06.327
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4896209.07                 A    =         6783835.44  meter
     Y    =        4023244.57  meter          E    =           .0002288
     Z    =       -2422312.79                 I    =           51.51447
     XDOT =      -4817.578889                 Wp   =           99.04538
     YDOT =       2650.710233  meter/sec      RA   =          201.71873  deg
     ZDOT =      -5339.825898                 TA   =          108.09255
                                              MA   =          108.06762
                                              Ha   =            219.222  n.mi
                                              Hp   =            213.615
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16063678.04                 X    =         4862623.02
     Y    =       13199621.28  feet           Y    =         4077809.52  meter
     Z    =       -7947220.45                 Z    =        -2398609.22
     XDOT =     -15805.705016                 XDOT =       -4820.922737
     YDOT =       8696.555882  feet/sec       YDOT =        2596.818512  meter/sec
     ZDOT =     -17519.113837                 ZDOT =       -5363.236829
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       20192132.84                 X    =         6154562.09
     Y    =        5113226.45  feet           Y    =         1558511.42  meter
     Z    =       -7846193.59                 Z    =        -2391519.81
     XDOT =     -10148.067473                 XDOT =       -3093.130966
     YDOT =      13060.798030  feet/sec       YDOT =        3980.931240  meter/sec
     ZDOT =     -17620.015873                 ZDOT =       -5370.580838
  
  
    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   15144.42815399  .00016717  00000-0  10270-3 0  9025
    2 25544  51.6430 202.6657 0003945 332.9970  27.0978 15.55183036 24346
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15144.42815399   =   yrday.fracday
    Element set:     902
    Inclination:       51.6430  deg
    RA of node:       202.6657  deg
    Eccentricity:     .0003945     
    Arg of perigee:   332.9970  deg
    Mean anomaly:      27.0978  deg
    Mean motion:   15.55183036  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2434
    Checksum:              315
 
 
    Coasting Arc #4 (Orbit 2449)
    ---------------------------------------
 
    Vector Time (GMT): 2015/145/09:37:06.327
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3290773.13                 A    =         6779287.63  meter
     Y    =       -4334822.34  meter          E    =           .0009186
     Z    =        4033207.27                 I    =           51.52985
     XDOT =       6482.769347                 Wp   =           80.84307
     YDOT =      -1287.626725  meter/sec      RA   =          196.72115  deg
     ZDOT =       3899.347408                 TA   =          328.66275
                                              MA   =          328.71746
                                              Ha   =            219.312  n.mi
                                              Hp   =            213.409
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10796499.76                 X    =        -3261647.44
     Y    =      -14221858.08  feet           Y    =        -4371459.25  meter
     Z    =       13232307.30                 Z    =         4017291.80
     XDOT =      21268.928304                 XDOT =        6477.744422
     YDOT =      -4224.497129  feet/sec       YDOT =       -1215.160428  meter/sec
     ZDOT =      12793.134540                 ZDOT =        3930.827334
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16026590.90                 X    =        -4884904.91
     Y    =       -7984836.83  feet           Y    =        -2433778.27  meter
     Z    =       13164739.86                 Z    =         4012612.71
     XDOT =      16587.255509                 XDOT =        5055.795479
     YDOT =     -11943.948972  feet/sec       YDOT =       -3640.515647  meter/sec
     ZDOT =      12928.442430                 ZDOT =        3940.589253
  
  
    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   15145.45627854  .00016717  00000-0  10270-3 0  9037
    2 25544  51.6434 197.5315 0004000 337.2800  22.8176 15.55228651 24500
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15145.45627854   =   yrday.fracday
    Element set:     903
    Inclination:       51.6434  deg
    RA of node:       197.5315  deg
    Eccentricity:     .0004000     
    Arg of perigee:   337.2800  deg
    Mean anomaly:      22.8176  deg
    Mean motion:   15.55228651  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2450
    Checksum:              291
 
 
    Coasting Arc #5 (Orbit 2464)
    ---------------------------------------
 
    Vector Time (GMT): 2015/146/09:37:06.327
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1234178.78                 A    =         6775394.60  meter
     Y    =        4354395.87  meter          E    =           .0013276
     Z    =       -5053764.06                 I    =           51.54682
     XDOT =      -7433.750371                 Wp   =           58.39581
     YDOT =        -42.055441  meter/sec      RA   =          191.71208  deg
     ZDOT =      -1848.406862                 TA   =          193.63984
                                              MA   =          193.67575
                                              Ha   =            219.388  n.mi
                                              Hp   =            213.356
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4049142.96                 X    =         1209944.61
     Y    =       14286075.67  feet           Y    =         4368061.95  meter
     Z    =      -16580590.75                 Z    =        -5047827.32
     XDOT =     -24388.944787                 XDOT =       -7423.748674
     YDOT =       -137.977170  feet/sec       YDOT =        -125.128506  meter/sec
     ZDOT =      -6064.326975                 ZDOT =       -1884.494533
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10202183.53                 X    =         3109625.54
     Y    =       10826957.18  feet           Y    =         3300056.55  meter
     Z    =      -16555843.56                 Z    =        -5046221.12
     XDOT =     -20953.652920                 XDOT =       -6386.673410
     YDOT =      10218.342220  feet/sec       YDOT =        3114.550709  meter/sec
     ZDOT =      -6219.200251                 ZDOT =       -1895.612237
  
  
    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   15146.42013318  .00016717  00000-0  10270-3 0  9040
    2 25544  51.6429 192.7195 0004098 340.6033  19.4964 15.55212484 24650
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15146.42013318   =   yrday.fracday
    Element set:     904
    Inclination:       51.6429  deg
    RA of node:       192.7195  deg
    Eccentricity:     .0004098     
    Arg of perigee:   340.6033  deg
    Mean anomaly:      19.4964  deg
    Mean motion:   15.55212484  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2465
    Checksum:              304
 
 
    Coasting Arc #6 (Orbit 2480)
    ---------------------------------------
 
    Vector Time (GMT): 2015/147/09:37:06.327
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1041606.57                 A    =         6774045.53  meter
     Y    =       -4101892.07  meter          E    =           .0005101
     Z    =        5288447.06                 I    =           51.57485
     XDOT =       7548.557779                 Wp   =           16.46239
     YDOT =       1277.946196  meter/sec      RA   =          186.69477  deg
     ZDOT =       -490.631682                 TA   =           78.24871
                                              MA   =           78.19148
                                              Ha   =            219.324  n.mi
                                              Hp   =            213.129
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3417344.38                 X    =         1061707.96
     Y    =      -13457651.14  feet           Y    =        -4090131.94  meter
     Z    =       17350548.11                 Z    =         5293555.71
     XDOT =      24765.609510                 XDOT =        7536.089779
     YDOT =       4192.736863  feet/sec       YDOT =        1362.289412  meter/sec
     ZDOT =      -1609.683995                 ZDOT =        -453.992148
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3413168.05                 X    =        -1040333.62
     Y    =      -13429504.40  feet           Y    =        -4093312.94  meter
     Z    =       17373164.13                 Z    =         5295340.43
     XDOT =      22854.968694                 XDOT =        6966.194458
     YDOT =      -7708.699977  feet/sec       YDOT =       -2349.611753  meter/sec
     ZDOT =      -1452.633734                 ZDOT =        -442.762762
  
  
    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   15147.44822764  .00016717  00000-0  10270-3 0  9057
    2 25544  51.6433 187.5853 0004171 344.5029  15.5996 15.55285108 24811
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15147.44822764   =   yrday.fracday
    Element set:     905
    Inclination:       51.6433  deg
    RA of node:       187.5853  deg
    Eccentricity:     .0004171     
    Arg of perigee:   344.5029  deg
    Mean anomaly:      15.5996  deg
    Mean motion:   15.55285108  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2481
    Checksum:              322
 
 
    Coasting Arc #7 (Orbit 2495)
    ---------------------------------------
 
    Vector Time (GMT): 2015/148/09:37:06.327
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3214834.44                 A    =         6776398.39  meter
     Y    =        3650964.99  meter          E    =           .0009857
     Z    =       -4725782.01                 I    =           51.61343
     XDOT =      -6743.311431                 Wp   =           86.93276
     YDOT =      -2380.545556  meter/sec      RA   =          181.68293  deg
     ZDOT =       2753.666577                 TA   =          210.32531
                                              MA   =          210.38238
                                              Ha   =            219.513  n.mi
                                              Hp   =            212.833
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10547357.08                 X    =        -3232465.11
     Y    =       11978231.58  feet           Y    =         3614916.21  meter
     Z    =      -15504534.14                 Z    =        -4741441.92
     XDOT =     -22123.725167                 XDOT =       -6729.566863
     YDOT =      -7810.188831  feet/sec       YDOT =       -2455.876934  meter/sec
     ZDOT =       9034.339162                 ZDOT =        2720.941773
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3317655.18                 X    =        -1011221.30
     Y    =       15543802.95  feet           Y    =         4737751.14  meter
     Z    =      -15572369.96                 Z    =        -4746458.36
     XDOT =     -22048.607543                 XDOT =       -6720.415579
     YDOT =       4186.648199  feet/sec       YDOT =        1276.090371  meter/sec
     ZDOT =       8894.262930                 ZDOT =        2710.971341
  
  
    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   15148.41205479  .00016717  00000-0  10270-3 0  9064
    2 25544  51.6423 182.7730 0004239 351.2877   8.8202 15.55290738 24968
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15148.41205479   =   yrday.fracday
    Element set:     906
    Inclination:       51.6423  deg
    RA of node:       182.7730  deg
    Eccentricity:     .0004239     
    Arg of perigee:   351.2877  deg
    Mean anomaly:       8.8202  deg
    Mean motion:   15.55290738  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2496
    Checksum:              316
 
 
    Coasting Arc #8 (Orbit 2511)
    ---------------------------------------
 
    Vector Time (GMT): 2015/149/09:37:06.327
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5043039.30                 A    =         6780832.07  meter
     Y    =       -2987958.99  meter          E    =           .0012700
     Z    =        3402951.14                 I    =           51.66070
     XDOT =       5119.813297                 Wp   =           69.88470
     YDOT =       3361.421678  meter/sec      RA   =          176.68431  deg
     ZDOT =      -4617.605563                 TA   =           70.31593
                                              MA   =           70.17894
                                              Ha   =            219.523  n.mi
                                              Hp   =            212.756
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16545404.51                 X    =         5059546.05
     Y    =       -9803015.05  feet           Y    =        -2931472.29  meter
     Z    =       11164537.88                 Z    =         3427489.56
     XDOT =      16797.287720                 XDOT =        5104.275484
     YDOT =      11028.286345  feet/sec       YDOT =        3418.588124  meter/sec
     ZDOT =     -15149.624549                 ZDOT =       -4592.771718
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9354677.58                 X    =         2851305.73
     Y    =      -16732148.91  feet           Y    =        -5099958.99  meter
     Z    =       11270386.90                 Z    =         3435213.93
     XDOT =      18924.036013                 XDOT =        5768.046177
     YDOT =        407.145563  feet/sec       YDOT =         124.097967  meter/sec
     ZDOT =     -15043.576667                 ZDOT =       -4585.282168
  
  
    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   15149.44012022  .00016717  00000-0  10270-3 0  9079
    2 25544  51.6426 177.6385 0004392 353.8326   6.2773 15.55329260 25124
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15149.44012022   =   yrday.fracday
    Element set:     907
    Inclination:       51.6426  deg
    RA of node:       177.6385  deg
    Eccentricity:     .0004392     
    Arg of perigee:   353.8326  deg
    Mean anomaly:       6.2773  deg
    Mean motion:   15.55329260  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2512
    Checksum:              297
 
 
    Coasting Arc #9 (Orbit 2526)
    ---------------------------------------
 
    Vector Time (GMT): 2015/150/09:37:06.327
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6229367.67                 A    =         6784842.64  meter
     Y    =        2162720.07  meter          E    =           .0011731
     Z    =       -1571844.09                 I    =           51.70431
     XDOT =      -2892.756609                 Wp   =           24.23040
     YDOT =      -4169.256063  meter/sec      RA   =          171.70315  deg
     ZDOT =       5753.389077                 TA   =          318.58522
                                              MA   =          318.67408
                                              Ha   =            219.692  n.mi
                                              Hp   =            212.695
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20437557.98                 X    =        -6245453.19
     Y    =        7095538.29  feet           Y    =         2092969.37  meter
     Z    =       -5156968.80                 Z    =        -1602144.59
     XDOT =      -9490.671288                 XDOT =       -2873.868262
     YDOT =     -13678.661624  feet/sec       YDOT =       -4201.499507  meter/sec
     ZDOT =      18875.948415                 ZDOT =        5739.382013
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13828661.36                 X    =        -4214975.98
     Y    =       16596564.58  feet           Y    =         5058632.88  meter
     Z    =       -5287431.90                 Z    =        -1611609.24
     XDOT =     -14074.548972                 XDOT =       -4289.922527
     YDOT =      -5758.730137  feet/sec       YDOT =       -1755.260946  meter/sec
     ZDOT =      18816.513638                 ZDOT =        5735.273357
  
  
    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   15150.40391912  .00016717  00000-0  10270-3 0  9086
    2 25544  51.6416 172.8254 0004458 358.2065   1.9071 15.55292338 25271
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15150.40391912   =   yrday.fracday
    Element set:     908
    Inclination:       51.6416  deg
    RA of node:       172.8254  deg
    Eccentricity:     .0004458     
    Arg of perigee:   358.2065  deg
    Mean anomaly:       1.9071  deg
    Mean motion:   15.55292338  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2527
    Checksum:              301
 
 
    Coasting Arc #10 (Orbit 2542)
    ---------------------------------------
 
    Vector Time (GMT): 2015/151/09:37:06.327
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6666734.88                 A    =         6785644.48  meter
     Y    =       -1126640.96  meter          E    =           .0008510
     Z    =        -549582.12                 I    =           51.73898
     XDOT =        319.780085                 Wp   =          117.01564
     YDOT =       4776.699453  meter/sec      RA   =          166.73253  deg
     ZDOT =      -5988.213361                 TA   =           68.90668
                                              MA   =           68.81572
                                              Ha   =            219.787  n.mi
                                              Hp   =            212.449
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21872489.76                 X    =         6681507.47
     Y    =       -3696328.62  feet           Y    =        -1052006.53  meter
     Z    =       -1803090.95                 Z    =         -517160.06
     XDOT =       1049.147260                 XDOT =         295.431120
     YDOT =      15671.586133  feet/sec       YDOT =        4780.139786  meter/sec
     ZDOT =     -19646.369296                 ZDOT =       -5986.718660
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16596848.72                 X    =         5058719.49
     Y    =      -14734197.77  feet           Y    =        -4490983.48  meter
     Z    =       -1663676.49                 Z    =         -507088.60
     XDOT =       8227.106298                 XDOT =        2507.622000
     YDOT =      11454.685081  feet/sec       YDOT =        3491.388013  meter/sec
     ZDOT =     -19640.764159                 ZDOT =       -5986.504916
  
  
    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   15151.43195545  .00016717  00000-0  10270-3 0  9095
    2 25544  51.6418 167.6906 0004466   4.1247 355.9943 15.55357813 25435
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15151.43195545   =   yrday.fracday
    Element set:     909
    Inclination:       51.6418  deg
    RA of node:       167.6906  deg
    Eccentricity:     .0004466     
    Arg of perigee:     4.1247  deg
    Mean anomaly:     355.9943  deg
    Mean motion:   15.55357813  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2543
    Checksum:              324
 
 
    Coasting Arc #11 (Orbit 2558)
    ---------------------------------------
 
    Vector Time (GMT): 2015/152/09:37:06.327
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6271996.37                 A    =         6783106.51  meter
     Y    =         -55781.51  meter          E    =           .0016068
     Z    =        2558237.59                 I    =           51.75999
     XDOT =       2207.767736                 Wp   =           61.08423
     YDOT =      -5111.783821  meter/sec      RA   =          161.76070  deg
     ZDOT =       5283.844123                 TA   =          327.65585
                                              MA   =          327.75426
                                              Ha   =            220.010  n.mi
                                              Hp   =            212.337
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20577415.92                 X    =        -6283333.62
     Y    =        -183010.20  feet           Y    =         -125982.72  meter
     Z    =        8393167.94                 Z    =         2527741.40
     XDOT =       7243.332468                 XDOT =        2239.097481
     YDOT =     -16770.944293  feet/sec       YDOT =       -5086.920473  meter/sec
     ZDOT =      17335.446597                 ZDOT =        5294.644793
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17402165.89                 X    =        -5304180.16
     Y    =       11081938.00  feet           Y    =         3377774.70  meter
     Z    =        8262207.87                 Z    =         2518320.96
     XDOT =      -2341.530426                 XDOT =        -713.698474
     YDOT =     -16680.091793  feet/sec       YDOT =       -5084.091978  meter/sec
     ZDOT =      17382.707888                 ZDOT =        5298.249364
  
  
    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   15152.45997696  .00016717  00000-0  10270-3 0  9107
    2 25544  51.6409 162.5559 0004547   9.5274 350.5965 15.55344223 25595
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15152.45997696   =   yrday.fracday
    Element set:     910
    Inclination:       51.6409  deg
    RA of node:       162.5559  deg
    Eccentricity:     .0004547     
    Arg of perigee:     9.5274  deg
    Mean anomaly:     350.5965  deg
    Mean motion:   15.55344223  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2559
    Checksum:              336
 
 
    Coasting Arc #12 (Orbit 2573)
    ---------------------------------------
 
    Vector Time (GMT): 2015/153/09:37:06.327
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5150091.90                 A    =         6778318.33  meter
     Y    =        1385918.48  meter          E    =           .0010788
     Z    =       -4195298.12                 I    =           51.77516
     XDOT =      -4387.352665                 Wp   =           50.32978
     YDOT =       5064.292889  meter/sec      RA   =          156.77761  deg
     ZDOT =      -3712.496072                 TA   =          181.57673
                                              MA   =          181.58014
                                              Ha   =            219.900  n.mi
                                              Hp   =            212.277
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16896626.96                 X    =         5154590.93
     Y    =        4546976.63  feet           Y    =         1443535.81  meter
     Z    =      -13764101.43                 Z    =        -4170268.52
     XDOT =     -14394.201656                 XDOT =       -4425.622547
     YDOT =      16615.134149  feet/sec       YDOT =        5015.017095  meter/sec
     ZDOT =     -12180.105224                 ZDOT =       -3733.901654
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16623991.97                 X    =         5066992.75
     Y    =       -5723223.07  feet           Y    =        -1744438.39  meter
     Z    =      -13656833.31                 Z    =        -4162602.79
     XDOT =      -3002.941887                 XDOT =        -915.296687
     YDOT =      20566.206637  feet/sec       YDOT =        6268.579783  meter/sec
     ZDOT =     -12272.921632                 ZDOT =       -3740.786513
  
  
    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   15153.42373123  .00016717  00000-0  10270-3 0  9119
    2 25544  51.6417 157.7419 0004477  12.6719 347.4546 15.55391476 25745
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15153.42373123   =   yrday.fracday
    Element set:     911
    Inclination:       51.6417  deg
    RA of node:       157.7419  deg
    Eccentricity:     .0004477     
    Arg of perigee:    12.6719  deg
    Mean anomaly:     347.4546  deg
    Mean motion:   15.55391476  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2574
    Checksum:              318
 
 
    Coasting Arc #13 (Orbit 2589)
    ---------------------------------------
 
    Vector Time (GMT): 2015/154/09:37:06.327
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3451894.32                 A    =         6774423.36  meter
     Y    =       -2739672.01  meter          E    =           .0005548
     Z    =        5140090.77                 I    =           51.79036
     XDOT =       5955.009293                 Wp   =           74.47777
     YDOT =      -4585.093220  meter/sec      RA   =          151.78113  deg
     ZDOT =       1555.361831                 TA   =             .57634
                                              MA   =             .57570
                                              Ha   =            220.056  n.mi
                                              Hp   =            211.992
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11325112.60                 X    =        -3445971.00
     Y    =       -8988425.24  feet           Y    =        -2778240.88  meter
     Z    =       16863814.85                 Z    =         5123335.99
     XDOT =      19537.432064                 XDOT =        5998.282863
     YDOT =     -15042.956759  feet/sec       YDOT =       -4518.258653  meter/sec
     ZDOT =       5102.893146                 ZDOT =        1584.394960
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14518804.84                 X    =        -4425331.71
     Y    =        -812808.75  feet           Y    =         -247744.11  meter
     Z    =       16792315.59                 Z    =         5118297.79
     XDOT =       7303.542936                 XDOT =        2226.119887
     YDOT =     -22446.462794  feet/sec       YDOT =       -6841.681859  meter/sec
     ZDOT =       5228.412492                 ZDOT =        1593.620128
  
  
    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   15154.45172057  .00016717  00000-0  10270-3 0  9127
    2 25544  51.6408 152.6069 0004548  16.9945 343.1360 15.55420575 25905
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15154.45172057   =   yrday.fracday
    Element set:     912
    Inclination:       51.6408  deg
    RA of node:       152.6069  deg
    Eccentricity:     .0004548     
    Arg of perigee:    16.9945  deg
    Mean anomaly:     343.1360  deg
    Mean motion:   15.55420575  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2590
    Checksum:              306
 
 
    Coasting Arc #14 (Orbit 2604)
    ---------------------------------------
 
    Vector Time (GMT): 2015/155/09:37:06.327
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1463391.62                 A    =         6773820.70  meter
     Y    =        4003376.77  meter          E    =           .0016163
     Z    =       -5278037.09                 I    =           51.81733
     XDOT =      -6713.016119                 Wp   =           80.74259
     YDOT =       3585.237753  meter/sec      RA   =          146.77862  deg
     ZDOT =        862.922677                 TA   =          197.47025
                                              MA   =          197.52592
                                              Ha   =            220.007  n.mi
                                              Hp   =            211.969
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4801153.61                 X    =         1444155.04
     Y    =       13134438.22  feet           Y    =         4019634.50  meter
     Z    =      -17316394.64                 Z    =        -5270974.37
     XDOT =     -22024.331098                 XDOT =       -6756.799959
     YDOT =      11762.591054  feet/sec       YDOT =        3509.923497  meter/sec
     ZDOT =       2831.111146                 ZDOT =         830.206035
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11686064.04                 X    =         3561912.32
     Y    =        7747659.46  feet           Y    =         2361486.60  meter
     Z    =      -17286750.62                 Z    =        -5269001.59
     XDOT =     -10371.897042                 XDOT =       -3161.354218
     YDOT =      21611.013540  feet/sec       YDOT =        6587.036927  meter/sec
     ZDOT =       2689.917302                 ZDOT =         819.886794
  
  
    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   15155.41544674  .00016717  00000-0  10270-3 0  9133
    2 25544  51.6422 147.7930 0004557  19.0178 341.1144 15.55419754 26057
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15155.41544674   =   yrday.fracday
    Element set:     913
    Inclination:       51.6422  deg
    RA of node:       147.7930  deg
    Eccentricity:     .0004557     
    Arg of perigee:    19.0178  deg
    Mean anomaly:     341.1144  deg
    Mean motion:   15.55419754  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2605
    Checksum:              304
 
 
    Coasting Arc #15 (Orbit 2620)
    ---------------------------------------
 
    Vector Time (GMT): 2015/156/09:37:06.327
    Vector Time (MET): N/A
    Weight (LBS)     : 892082.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         594733.23                 A    =         6776639.87  meter
     Y    =       -4998954.06  meter          E    =           .0012546
     Z    =        4531916.00                 I    =           51.85253
     XDOT =       6670.358338                 Wp   =           52.66580
     YDOT =      -2088.126001  meter/sec      RA   =          141.78179  deg
     ZDOT =      -3165.254436                 TA   =           69.03989
                                              MA   =           68.90569
                                              Ha   =            219.989  n.mi
                                              Hp   =            211.704
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1951224.50                 X    =          628574.11
     Y    =      -16400767.91  feet           Y    =        -4992114.72  meter
     Z    =       14868490.80                 Z    =         4534886.67
     XDOT =      21884.377748                 XDOT =        6708.588167
     YDOT =      -6850.807089  feet/sec       YDOT =       -2013.319540  meter/sec
     ZDOT =     -10384.693033                 ZDOT =       -3132.758437
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8371246.26                 X    =        -2551555.86
     Y    =      -14223528.31  feet           Y    =        -4335331.43  meter
     Z    =       14882135.68                 Z    =         4536074.95
     XDOT =      12389.504696                 XDOT =        3776.321031
     YDOT =     -18056.950030  feet/sec       YDOT =       -5503.758369  meter/sec
     ZDOT =     -10244.687333                 ZDOT =       -3122.580699
  
  
    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   15156.44340462  .00016717  00000-0  10270-3 0  9147
    2 25544  51.6412 142.6577 0004649  23.6137 336.5229 15.55485375 26217
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15156.44340462   =   yrday.fracday
    Element set:     914
    Inclination:       51.6412  deg
    RA of node:       142.6577  deg
    Eccentricity:     .0004649     
    Arg of perigee:    23.6137  deg
    Mean anomaly:     336.5229  deg
    Mean motion:   15.55485375  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2621
    Checksum:              308
 
             

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