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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  24756.99
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   128.3
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.453
   ET - UTC  (sec) :   67.18
   UT1 - UTC (sec) :    0.00
 
 
   Maneuvers contained within the current ephemeris are as follows:
 
 
   IMPULSIVE TIG (GMT)   M50 DVx(FPS)      LVLH DVx(FPS)      DVmag(FPS) 
   IMPULSIVE TIG (MET)   M50 DVy(FPS)      LVLH DVy(FPS)      Invar Sph HA
   DT                    M50 DVz(FPS)      LVLH DVz(FPS)      Invar Sph HP 
   ------------------------------------------------------------------------
   115/06:40:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              215.9  
   000/00:00:00.000           0.0               0.0              213.5  
   
   126/05:15:45.661          -1.8               4.9              4.9    
   N/A                       -3.1              -0.1              216.2  
   000/00:11:31.322          -3.4              -0.0              214.5  
   
 
 
    Coasting Arc #1 (Orbit 1968)
    ---------------------------------------
 
    Vector Time (GMT): 2015/114/13:09:52.075
    Vector Time (MET): N/A
    Weight (LBS)     : 923717.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1930027.54                 A    =         6773462.23  meter
     Y    =       -4240451.84  meter          E    =           .0007573
     Z    =       -4923556.82                 I    =           51.58118
     XDOT =       7293.717625                 Wp   =          123.74576
     YDOT =        704.617939  meter/sec      RA   =          351.41872  deg
     ZDOT =       2250.643866                 TA   =          168.27142
                                              MA   =          168.25377
                                              Ha   =            216.080  n.mi
                                              Hp   =            213.658
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6332111.36                 X    =         2001218.81
     Y    =      -13912243.56  feet           Y    =        -4218471.05  meter
     Z    =      -16153401.65                 Z    =        -4914008.05
     XDOT =      23929.519767                 XDOT =        7274.363469
     YDOT =       2311.738646  feet/sec       YDOT =         786.072887  meter/sec
     ZDOT =       7384.002185                 ZDOT =        2286.028561
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6249732.65                 X    =        -1904918.51
     Y    =      -13997674.67  feet           Y    =        -4266491.24  meter
     Z    =      -16111625.79                 Z    =        -4910823.54
     XDOT =      16427.514702                 XDOT =        5007.106481
     YDOT =     -16014.353200  feet/sec       YDOT =       -4881.174855  meter/sec
     ZDOT =       7535.550602                 ZDOT =        2296.835823
  
  
    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   15114.56057506  .00016717  00000-0  10270-3 0  9003
    2 25544  51.6454 351.9277 0005432 261.9188  98.1349 15.56066373 19691
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15114.56057506   =   yrday.fracday
    Element set:     900
    Inclination:       51.6454  deg
    RA of node:       351.9277  deg
    Eccentricity:     .0005432     
    Arg of perigee:   261.9188  deg
    Mean anomaly:      98.1349  deg
    Mean motion:   15.56066373  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1969
    Checksum:              328
 
 
    Coasting Arc #2 (Orbit 1980)
    ---------------------------------------
 
    Vector Time (GMT): 2015/115/06:40:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909283.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3908732.48                 A    =         6774129.40  meter
     Y    =        2954391.14  meter          E    =           .0004534
     Z    =        4678308.06                 I    =           51.56030
     XDOT =      -6137.061332                 Wp   =          157.87588
     YDOT =       3626.173174  meter/sec      RA   =          347.80751  deg
     ZDOT =       2832.555049                 TA   =          263.96887
                                              MA   =          264.02054
                                              Ha   =            215.862  n.mi
                                              Hp   =            213.514
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12823925.44                 X    =         3852679.66
     Y    =        9692884.31  feet           Y    =         2997787.86  meter
     Z    =       15348779.73                 Z    =         4697159.80
     XDOT =     -20134.715655                 XDOT =       -6190.913514
     YDOT =      11896.893617  feet/sec       YDOT =        3557.243519  meter/sec
     ZDOT =       9293.159611                 ZDOT =        2802.611317
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1382417.75                 X    =          421360.93
     Y    =       15938155.25  feet           Y    =         4857949.72  meter
     Z    =       15429006.37                 Z    =         4702761.14
     XDOT =     -21222.685247                 XDOT =       -6468.674463
     YDOT =      -7046.377023  feet/sec       YDOT =       -2147.735717  meter/sec
     ZDOT =       9164.080003                 ZDOT =        2793.211585
  
  
    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   15115.33123466  .00016717  00000-0  10270-3 0  9019
    2 25544  51.6443 348.0750 0005428 263.4148  96.6388 15.56124781 19818
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15115.33123466   =   yrday.fracday
    Element set:     901
    Inclination:       51.6443  deg
    RA of node:       348.0750  deg
    Eccentricity:     .0005428     
    Arg of perigee:   263.4148  deg
    Mean anomaly:      96.6388  deg
    Mean motion:   15.56124781  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1981
    Checksum:              311
 
 
    Coasting Arc #3 (Orbit 1995)
    ---------------------------------------
 
    Vector Time (GMT): 2015/116/06:40:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909283.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1513913.74                 A    =         6771517.97  meter
     Y    =       -3942405.99  meter          E    =           .0009480
     Z    =       -5301503.19                 I    =           51.52082
     XDOT =       7257.171461                 Wp   =           87.99524
     YDOT =      -2454.630034  meter/sec      RA   =          342.78158  deg
     ZDOT =       -247.078736                 TA   =          179.64518
                                              MA   =          179.64450
                                              Ha   =            215.871  n.mi
                                              Hp   =            213.423
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4966908.58                 X    =        -1443963.45
     Y    =      -12934402.86  feet           Y    =        -3958944.66  meter
     Z    =      -17393383.17                 Z    =        -5308687.46
     XDOT =      23809.617653                 XDOT =        7285.280569
     YDOT =      -8053.248143  feet/sec       YDOT =       -2373.318442  meter/sec
     ZDOT =       -810.625773                 ZDOT =        -211.756252
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6096541.01                 X    =         1858225.70
     Y    =      -12399841.29  feet           Y    =        -3779471.63  meter
     Z    =      -17423399.79                 Z    =        -5310652.25
     XDOT =      21276.945298                 XDOT =        6485.212927
     YDOT =      11386.418261  feet/sec       YDOT =        3470.580286  meter/sec
     ZDOT =       -658.728847                 ZDOT =        -200.780552
  
  
    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   15116.29453118  .00016717  00000-0  10270-3 0  9026
    2 25544  51.6444 343.2579 0005398 268.4955  91.5581 15.56138739 19965
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15116.29453118   =   yrday.fracday
    Element set:     902
    Inclination:       51.6444  deg
    RA of node:       343.2579  deg
    Eccentricity:     .0005398     
    Arg of perigee:   268.4955  deg
    Mean anomaly:      91.5581  deg
    Mean motion:   15.56138739  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1996
    Checksum:              345
 
 
    Coasting Arc #4 (Orbit 2011)
    ---------------------------------------
 
    Vector Time (GMT): 2015/117/06:40:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909283.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1049167.56                 A    =         6773333.31  meter
     Y    =        4603740.28  meter          E    =           .0003835
     Z    =        4857109.94                 I    =           51.49775
     XDOT =      -7229.617262                 Wp   =            9.36651
     YDOT =        891.893666  meter/sec      RA   =          337.75314  deg
     ZDOT =      -2403.036810                 TA   =          104.25271
                                              MA   =          104.21012
                                              Ha   =            215.807  n.mi
                                              Hp   =            213.414
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3442150.80                 X    =        -1124163.86
     Y    =       15104134.77  feet           Y    =         4591588.72  meter
     Z    =       15935400.06                 Z    =         4851830.86
     XDOT =     -23719.216740                 XDOT =       -7227.380187
     YDOT =       2926.160322  feet/sec       YDOT =         811.059744  meter/sec
     ZDOT =      -7883.979034                 ZDOT =       -2438.151697
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13295807.36                 X    =        -4052562.08
     Y    =        7997143.22  feet           Y    =         2437529.25  meter
     Z    =       15911865.74                 Z    =         4849936.68
     XDOT =     -18022.125991                 XDOT =       -5493.144002
     YDOT =     -13950.513843  feet/sec       YDOT =       -4252.116619  meter/sec
     ZDOT =      -8034.669199                 ZDOT =       -2448.967172
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   15117.32201150  .00016717  00000-0  10270-3 0  9039
    2 25544  51.6449 338.1209 0005424 272.5613  87.4919 15.56192463 20123
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15117.32201150   =   yrday.fracday
    Element set:     903
    Inclination:       51.6449  deg
    RA of node:       338.1209  deg
    Eccentricity:     .0005424     
    Arg of perigee:   272.5613  deg
    Mean anomaly:      87.4919  deg
    Mean motion:   15.56192463  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2012
    Checksum:              286
 
 
    Coasting Arc #5 (Orbit 2026)
    ---------------------------------------
 
    Vector Time (GMT): 2015/118/06:40:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909283.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3346481.03                 A    =         6778255.06  meter
     Y    =       -4794102.12  meter          E    =           .0000943
     Z    =       -3428373.67                 I    =           51.48542
     XDOT =       6076.292613                 Wp   =          315.61756
     YDOT =        967.485327  meter/sec      RA   =          332.73563  deg
     ZDOT =       4578.154251                 TA   =            4.10576
                                              MA   =            4.10499
                                              Ha   =            215.759  n.mi
                                              Hp   =            213.437
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10979268.48                 X    =         3416494.99
     Y    =      -15728681.51  feet           Y    =        -4756288.32  meter
     Z    =      -11247945.12                 Z    =        -3411946.66
     XDOT =      19935.343217                 XDOT =        6042.783232
     YDOT =       3174.164458  feet/sec       YDOT =        1035.247312  meter/sec
     ZDOT =      15020.191111                 ZDOT =        4607.590469
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18924015.55                 X    =         5768039.94
     Y    =       -3378954.96  feet           Y    =        -1029905.47  meter
     Z    =      -11176597.27                 Z    =        -3406626.85
     XDOT =      11597.171255                 XDOT =        3534.817799
     YDOT =      14850.345223  feet/sec       YDOT =        4526.385224  meter/sec
     ZDOT =      15146.168300                 ZDOT =        4616.552098
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   15118.28524077  .00016717  00000-0  10270-3 0  9042
    2 25544  51.6446 333.3038 0005563 276.9594  83.0927 15.56242922 20270
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15118.28524077   =   yrday.fracday
    Element set:     904
    Inclination:       51.6446  deg
    RA of node:       333.3038  deg
    Eccentricity:     .0005563     
    Arg of perigee:   276.9594  deg
    Mean anomaly:      83.0927  deg
    Mean motion:   15.56242922  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2027
    Checksum:              316
 
 
    Coasting Arc #6 (Orbit 2042)
    ---------------------------------------
 
    Vector Time (GMT): 2015/119/06:40:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909283.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5023810.33                 A    =         6782380.57  meter
     Y    =        4367959.80  meter          E    =           .0008786
     Z    =        1270660.60                 I    =           51.47270
     XDOT =      -4034.027219                 Wp   =          133.89104
     YDOT =      -2939.291070  meter/sec      RA   =          327.73599  deg
     ZDOT =      -5826.203891                 TA   =           32.24265
                                              MA   =           32.18896
                                              Ha   =            215.763  n.mi
                                              Hp   =            213.326
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16482317.36                 X    =        -5078452.97
     Y    =       14330576.77  feet           Y    =         4311474.82  meter
     Z    =        4168833.99                 Z    =         1246122.66
     XDOT =     -13234.997439                 XDOT =       -3972.557747
     YDOT =      -9643.343407  feet/sec       YDOT =       -2984.058872  meter/sec
     ZDOT =     -19114.842162                 ZDOT =       -5845.651116
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21834174.76                 X    =        -6655056.47
     Y    =       -1083391.86  feet           Y    =         -330217.84  meter
     Z    =        4062815.21                 Z    =         1238346.08
     XDOT =      -2867.440332                 XDOT =        -873.995813
     YDOT =     -14445.674464  feet/sec       YDOT =       -4403.041577  meter/sec
     ZDOT =     -19197.616421                 ZDOT =       -5851.433485
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   15119.31265117  .00016717  00000-0  10270-3 0  9055
    2 25544  51.6453 328.1657 0005553 280.8600  79.1929 15.56297380 20432
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15119.31265117   =   yrday.fracday
    Element set:     905
    Inclination:       51.6453  deg
    RA of node:       328.1657  deg
    Eccentricity:     .0005553     
    Arg of perigee:   280.8600  deg
    Mean anomaly:      79.1929  deg
    Mean motion:   15.56297380  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2043
    Checksum:              311
 
 
    Coasting Arc #7 (Orbit 2058)
    ---------------------------------------
 
    Vector Time (GMT): 2015/120/06:40:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909283.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5820528.80                 A    =         6782278.18  meter
     Y    =       -3270236.42  meter          E    =           .0010733
     Z    =        1155383.34                 I    =           51.44615
     XDOT =       1491.227734                 Wp   =           34.80926
     YDOT =       4729.611082  meter/sec      RA   =          322.74314  deg
     ZDOT =       5856.181159                 TA   =          337.78547
                                              MA   =          337.83194
                                              Ha   =            215.782  n.mi
                                              Hp   =            213.215
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19096223.09                 X    =         5851052.27
     Y    =      -10729122.13  feet           Y    =        -3204976.73  meter
     Z    =        3790627.77                 Z    =         1183733.06
     XDOT =       4892.479441                 XDOT =        1409.781756
     YDOT =      15517.096726  feet/sec       YDOT =        4745.831941  meter/sec
     ZDOT =      19213.192780                 ZDOT =        5863.227225
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21281660.44                 X    =         6486650.10
     Y    =        5092141.04  feet           Y    =         1552084.59  meter
     Z    =        3912759.29                 Z    =         1192609.03
     XDOT =      -6676.757664                 XDOT =       -2035.075736
     YDOT =      13073.960688  feet/sec       YDOT =        3984.943218  meter/sec
     ZDOT =      19242.469890                 ZDOT =        5865.104822
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   15120.34002516  .00016717  00000-0  10270-3 0  9063
    2 25544  51.6448 323.0270 0005672 285.6641  74.3886 15.56349848 20594
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15120.34002516   =   yrday.fracday
    Element set:     906
    Inclination:       51.6448  deg
    RA of node:       323.0270  deg
    Eccentricity:     .0005672     
    Arg of perigee:   285.6641  deg
    Mean anomaly:      74.3886  deg
    Mean motion:   15.56349848  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2059
    Checksum:              311
 
 
    Coasting Arc #8 (Orbit 2073)
    ---------------------------------------
 
    Vector Time (GMT): 2015/121/06:40:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909283.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5681960.74                 A    =         6777765.00  meter
     Y    =        1538973.78  meter          E    =           .0001965
     Z    =       -3360809.92                 I    =           51.40784
     XDOT =       1114.311244                 Wp   =          343.25642
     YDOT =      -6007.926848  meter/sec      RA   =          317.73949  deg
     ZDOT =      -4632.524819                 TA   =          236.11463
                                              MA   =          236.13333
                                              Ha   =            215.911  n.mi
                                              Hp   =            213.036
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18641603.46                 X    =        -5682421.79
     Y    =        5049126.56  feet           Y    =         1475431.61  meter
     Z    =      -11026279.28                 Z    =        -3388413.44
     XDOT =       3655.876784                 XDOT =        1203.913933
     YDOT =     -19711.046090  feet/sec       YDOT =       -5994.965157  meter/sec
     ZDOT =     -15198.572241                 ZDOT =       -4626.893641
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17204537.85                 X    =        -5243943.14
     Y    =       -8624249.03  feet           Y    =        -2628671.10  meter
     Z    =      -11144868.76                 Z    =        -3396956.00
     XDOT =      15313.827122                 XDOT =        4667.654507
     YDOT =     -10931.023787  feet/sec       YDOT =       -3331.776050  meter/sec
     ZDOT =     -15173.276700                 ZDOT =       -4624.814738
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   15121.30315475  .00016717  00000-0  10270-3 0  9072
    2 25544  51.6455 318.2096 0005734 289.7630  70.2906 15.56422236 20744
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15121.30315475   =   yrday.fracday
    Element set:     907
    Inclination:       51.6455  deg
    RA of node:       318.2096  deg
    Eccentricity:     .0005734     
    Arg of perigee:   289.7630  deg
    Mean anomaly:      70.2906  deg
    Mean motion:   15.56422236  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2074
    Checksum:              300
 
 
    Coasting Arc #9 (Orbit 2089)
    ---------------------------------------
 
    Vector Time (GMT): 2015/122/06:40:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909283.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4691167.45                 A    =         6772412.25  meter
     Y    =         626187.08  meter          E    =           .0001379
     Z    =        4844210.67                 I    =           51.36702
     XDOT =      -3351.339251                 Wp   =          156.18052
     YDOT =       6467.358766  meter/sec      RA   =          312.71288  deg
     ZDOT =       2407.977498                 TA   =          270.12057
                                              MA   =          270.13638
                                              Ha   =            215.833  n.mi
                                              Hp   =            213.038
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15390969.33                 X    =         4660284.80
     Y    =        2054419.54  feet           Y    =          678474.32  meter
     Z    =       15893079.61                 Z    =         4866924.84
     XDOT =     -10995.207517                 XDOT =       -3435.106994
     YDOT =      21218.368654  feet/sec       YDOT =        6429.413636  meter/sec
     ZDOT =       7900.188642                 ZDOT =        2391.493268
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10221859.05                 X    =         3115622.64
     Y    =       11554942.13  feet           Y    =         3521946.36  meter
     Z    =       15990292.87                 Z    =         4873841.27
     XDOT =     -21390.435949                 XDOT =       -6519.804877
     YDOT =       8082.778325  feet/sec       YDOT =        2463.630833  meter/sec
     ZDOT =       7828.302020                 ZDOT =        2386.066456
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   15122.33045824  .00016717  00000-0  10270-3 0  9085
    2 25544  51.6450 313.0702 0005806 293.1692  66.8850 15.56473689 20908
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15122.33045824   =   yrday.fracday
    Element set:     908
    Inclination:       51.6450  deg
    RA of node:       313.0702  deg
    Eccentricity:     .0005806     
    Arg of perigee:   293.1692  deg
    Mean anomaly:      66.8850  deg
    Mean motion:   15.56473689  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2090
    Checksum:              307
 
 
    Coasting Arc #10 (Orbit 2104)
    ---------------------------------------
 
    Vector Time (GMT): 2015/123/06:40:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909283.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3099722.89                 A    =         6770413.35  meter
     Y    =       -2900296.11  meter          E    =           .0009777
     Z    =       -5282514.37                 I    =           51.34050
     XDOT =       4901.741844                 Wp   =           78.03541
     YDOT =      -5882.945443  meter/sec      RA   =          307.66874  deg
     ZDOT =        356.214656                 TA   =          195.36135
                                              MA   =          195.39104
                                              Ha   =            216.039  n.mi
                                              Hp   =            212.749
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10169694.53                 X    =        -3041399.69
     Y    =       -9515407.17  feet           Y    =        -2934633.28  meter
     Z    =      -17331083.88                 Z    =        -5297430.79
     XDOT =      16081.830197                 XDOT =        4965.431635
     YDOT =     -19301.002110  feet/sec       YDOT =       -5827.774841  meter/sec
     ZDOT =       1168.683255                 ZDOT =         380.181743
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1622353.35                 X    =         -494493.30
     Y    =      -13752580.21  feet           Y    =        -4191786.45  meter
     Z    =      -17394442.68                 Z    =        -5301826.13
     XDOT =      23705.974611                 XDOT =        7225.581062
     YDOT =      -4395.481562  feet/sec       YDOT =       -1339.742780  meter/sec
     ZDOT =       1272.515593                 ZDOT =         387.862753
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   15123.29352250  .00016717  00000-0  10270-3 0  9096
    2 25544  51.6455 308.2519 0005912 297.8228  62.2327 15.56531203 21052
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15123.29352250   =   yrday.fracday
    Element set:     909
    Inclination:       51.6455  deg
    RA of node:       308.2519  deg
    Eccentricity:     .0005912     
    Arg of perigee:   297.8228  deg
    Mean anomaly:      62.2327  deg
    Mean motion:   15.56531203  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2105
    Checksum:              292
 
 
    Coasting Arc #11 (Orbit 2120)
    ---------------------------------------
 
    Vector Time (GMT): 2015/124/06:40:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909283.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1190372.99                 A    =         6773375.20  meter
     Y    =        4882440.14  meter          E    =           .0007255
     Z    =        4542292.36                 I    =           51.33201
     XDOT =      -5618.459041                 Wp   =           22.98975
     YDOT =       4228.364175  meter/sec      RA   =          302.62557  deg
     ZDOT =      -3064.383272                 TA   =           97.82664
                                              MA   =           97.74427
                                              Ha   =            216.206  n.mi
                                              Hp   =            212.707
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3905423.19                 X    =         1113622.66
     Y    =       16018504.40  feet           Y    =         4895322.58  meter
     Z    =       14902534.00                 Z    =         4547888.62
     XDOT =     -18433.264569                 XDOT =       -5650.438080
     YDOT =      13872.585876  feet/sec       YDOT =        4165.356058  meter/sec
     ZDOT =     -10053.750891                 ZDOT =       -3091.754976
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7087398.52                 X    =        -2160239.07
     Y    =       14863589.48  feet           Y    =         4530422.07  meter
     Z    =       14925576.13                 Z    =         4549315.61
     XDOT =     -21922.950936                 XDOT =       -6682.115445
     YDOT =       -212.194275  feet/sec       YDOT =         -64.676815  meter/sec
     ZDOT =     -10171.849023                 ZDOT =       -3100.379582
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   15124.32075527  .00016717  00000-0  10270-3 0  9102
    2 25544  51.6452 303.1124 0006075 302.3250  57.7316 15.56592259 21216
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15124.32075527   =   yrday.fracday
    Element set:     910
    Inclination:       51.6452  deg
    RA of node:       303.1124  deg
    Eccentricity:     .0006075     
    Arg of perigee:   302.3250  deg
    Mean anomaly:      57.7316  deg
    Mean motion:   15.56592259  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2121
    Checksum:              272
 
 
    Coasting Arc #12 (Orbit 2135)
    ---------------------------------------
 
    Vector Time (GMT): 2015/125/06:40:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909283.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         693529.36                 A    =         6778757.05  meter
     Y    =       -6136933.56  meter          E    =           .0006101
     Z    =       -2785134.71                 I    =           51.33488
     XDOT =       5482.897043                 Wp   =          351.14379
     YDOT =      -1690.183674  meter/sec      RA   =          297.59923  deg
     ZDOT =       5093.985100                 TA   =          337.08726
                                              MA   =          337.11447
                                              Ha   =            216.288  n.mi
                                              Hp   =            212.544
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2275358.80                 X    =          775631.90
     Y    =      -20134296.45  feet           Y    =        -6128718.97  meter
     Z    =       -9137581.07                 Z    =        -2781566.24
     XDOT =      17988.507358                 XDOT =        5476.644370
     YDOT =      -5545.222028  feet/sec       YDOT =       -1628.905343  meter/sec
     ZDOT =      16712.549541                 ZDOT =        5120.605321
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14206909.55                 X    =         4330266.03
     Y    =      -14457922.02  feet           Y    =        -4406774.63  meter
     Z    =       -9121115.67                 Z    =        -2780116.06
     XDOT =      16462.909986                 XDOT =        5017.894964
     YDOT =       5570.609598  feet/sec       YDOT =        1697.921805  meter/sec
     ZDOT =      16826.939065                 ZDOT =        5128.851027
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   15125.28375295  .00016717  00000-0  10270-3 0  9114
    2 25544  51.6460 298.2932 0006168 305.8682  54.1899 15.56636647 21369
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15125.28375295   =   yrday.fracday
    Element set:     911
    Inclination:       51.6460  deg
    RA of node:       298.2932  deg
    Eccentricity:     .0006168     
    Arg of perigee:   305.8682  deg
    Mean anomaly:      54.1899  deg
    Mean motion:   15.56636647  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2136
    Checksum:              337
 
 
    Coasting Arc #13 (Orbit 2150)
    ---------------------------------------
 
    Vector Time (GMT): 2015/126/05:21:31.322
    Vector Time (MET): N/A
    Weight (LBS)     : 908777.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4670530.14                 A    =         6777939.14  meter
     Y    =        2911500.77  meter          E    =           .0002478
     Z    =       -3957915.04                 I    =           51.30986
     XDOT =       -698.080807                 Wp   =             .71805
     YDOT =      -6521.591400  meter/sec      RA   =          292.89643  deg
     ZDOT =      -3971.202803                 TA   =          227.69949
                                              MA   =          227.72049
                                              Ha   =            216.164  n.mi
                                              Hp   =            214.480
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15323261.61                 X    =        -4683513.66
     Y    =        9552167.88  feet           Y    =         2859199.35  meter
     Z    =      -12985285.55                 Z    =        -3980635.48
     XDOT =      -2290.291361                 XDOT =        -605.811939
     YDOT =     -21396.297245  feet/sec       YDOT =       -6528.881795  meter/sec
     ZDOT =     -13028.880588                 ZDOT =       -3974.370052
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16350016.40                 X    =        -4983485.00
     Y    =       -7494717.53  feet           Y    =        -2284389.90  meter
     Z    =      -13083198.05                 Z    =        -3987758.77
     XDOT =      16125.930189                 XDOT =        4915.183522
     YDOT =     -12400.194291  feet/sec       YDOT =       -3779.579220  meter/sec
     ZDOT =     -13041.208583                 ZDOT =       -3974.960376
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   15126.24673201  .00016717  00000-0  10270-3 0  9120
    2 25544  51.6456 293.4744 0006547 273.6836  86.3568 15.55724847 21512
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15126.24673201   =   yrday.fracday
    Element set:     912
    Inclination:       51.6456  deg
    RA of node:       293.4744  deg
    Eccentricity:     .0006547     
    Arg of perigee:   273.6836  deg
    Mean anomaly:      86.3568  deg
    Mean motion:   15.55724847  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2151
    Checksum:              326
 
 
    Coasting Arc #14 (Orbit 2166)
    ---------------------------------------
 
    Vector Time (GMT): 2015/127/05:21:31.322
    Vector Time (MET): N/A
    Weight (LBS)     : 908777.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4467315.02                 A    =         6773590.08  meter
     Y    =        -662137.63  meter          E    =           .0003094
     Z    =        5050868.65                 I    =           51.28414
     XDOT =       -900.373005                 Wp   =          224.88373
     YDOT =       7408.408691  meter/sec      RA   =          287.86438  deg
     ZDOT =       1766.052918                 TA   =          207.94216
                                              MA   =          207.95877
                                              Ha   =            216.081  n.mi
                                              Hp   =            214.580
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14656545.34                 X    =         4449851.54
     Y    =       -2172367.57  feet           Y    =         -612279.02  meter
     Z    =       16571091.37                 Z    =         5072527.92
     XDOT =      -2953.979675                 XDOT =        -991.727644
     YDOT =      24305.802792  feet/sec       YDOT =        7397.829276  meter/sec
     ZDOT =       5794.136869                 ZDOT =        1761.457371
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9990297.30                 X    =         3045042.62
     Y    =       10799936.72  feet           Y    =         3291820.71  meter
     Z    =       16664030.07                 Z    =         5079196.37
     XDOT =     -20980.245525                 XDOT =       -6394.778836
     YDOT =      10492.255129  feet/sec       YDOT =        3198.039363  meter/sec
     ZDOT =       5773.039000                 ZDOT =        1759.622287
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   15127.27449901  .00016717  00000-0  10270-3 0  9133
    2 25544  51.6455 288.3382 0006610 277.5841  82.4562 15.55772962 21671
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15127.27449901   =   yrday.fracday
    Element set:     913
    Inclination:       51.6455  deg
    RA of node:       288.3382  deg
    Eccentricity:     .0006610     
    Arg of perigee:   277.5841  deg
    Mean anomaly:      82.4562  deg
    Mean motion:   15.55772962  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2167
    Checksum:              328
 
 
    Coasting Arc #15 (Orbit 2181)
    ---------------------------------------
 
    Vector Time (GMT): 2015/128/05:21:31.322
    Vector Time (MET): N/A
    Weight (LBS)     : 908777.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3905830.07                 A    =         6772600.58  meter
     Y    =       -1786359.24  meter          E    =           .0007946
     Z    =       -5243466.26                 I    =           51.27304
     XDOT =       2290.998991                 Wp   =           90.62203
     YDOT =      -7274.369411  meter/sec      RA   =          282.82147  deg
     ZDOT =        772.632673                 TA   =          186.79580
                                              MA   =          186.80658
                                              Ha   =            216.358  n.mi
                                              Hp   =            214.387
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12814403.12                 X    =        -3860093.16
     Y    =       -5860758.66  feet           Y    =        -1829780.85  meter
     Z    =      -17202973.28                 Z    =        -5262329.25
     XDOT =       7516.400888                 XDOT =        2368.419240
     YDOT =     -23866.041374  feet/sec       YDOT =       -7248.317112  meter/sec
     ZDOT =       2534.884097                 ZDOT =         783.949809
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2549980.10                 X    =         -777233.93
     Y    =      -13757868.48  feet           Y    =        -4193398.31  meter
     Z    =      -17283470.88                 Z    =        -5268001.92
     XDOT =      22812.550395                 XDOT =        6953.265361
     YDOT =      -7471.536038  feet/sec       YDOT =       -2277.324184  meter/sec
     ZDOT =       2584.752024                 ZDOT =         787.832417
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   15128.23799833  .00016717  00000-0  10270-3 0  9143
    2 25544  51.6460 283.5231 0006706 282.4752  77.5651 15.55831596 21829
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15128.23799833   =   yrday.fracday
    Element set:     914
    Inclination:       51.6460  deg
    RA of node:       283.5231  deg
    Eccentricity:     .0006706     
    Arg of perigee:   282.4752  deg
    Mean anomaly:      77.5651  deg
    Mean motion:   15.55831596  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2182
    Checksum:              326
 
 
    Coasting Arc #16 (Orbit 2197)
    ---------------------------------------
 
    Vector Time (GMT): 2015/129/05:21:31.322
    Vector Time (MET): N/A
    Weight (LBS)     : 908777.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3061299.52                 A    =         6775623.40  meter
     Y    =        4070182.68  meter          E    =           .0005683
     Z    =        4470283.34                 I    =           51.27749
     XDOT =      -3413.956872                 Wp   =           18.60330
     YDOT =       6080.320383  meter/sec      RA   =          277.78249  deg
     ZDOT =      -3191.781759                 TA   =          103.66769
                                              MA   =          103.60440
                                              Ha   =            216.649  n.mi
                                              Hp   =            214.498
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10043633.61                 X    =         2993843.08
     Y    =       13353617.72  feet           Y    =         4104038.80  meter
     Z    =       14666283.91                 Z    =         4484990.98
     XDOT =     -11200.645906                 XDOT =       -3466.190102
     YDOT =      19948.557687  feet/sec       YDOT =        6041.851350  meter/sec
     ZDOT =     -10471.724931                 ZDOT =       -3208.492906
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4884735.21                 X    =        -1488867.29
     Y    =       15921765.85  feet           Y    =         4852954.23  meter
     Z    =       14728553.90                 Z    =         4489263.23
     XDOT =     -21508.900559                 XDOT =       -6555.912890
     YDOT =       3174.807889  feet/sec       YDOT =         967.681445  meter/sec
     ZDOT =     -10544.476648                 ZDOT =       -3213.956482
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   15129.26569583  .00016717  00000-0  10270-3 0  9155
    2 25544  51.6458 278.3871 0006851 287.5406  72.4999 15.55899532 21981
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15129.26569583   =   yrday.fracday
    Element set:     915
    Inclination:       51.6458  deg
    RA of node:       278.3871  deg
    Eccentricity:     .0006851     
    Arg of perigee:   287.5406  deg
    Mean anomaly:      72.4999  deg
    Mean motion:   15.55899532  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2198
    Checksum:              370
 
             

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